c5 c10 c12 c14 c15 c16 c17 c18 c20 c25 c35 c40 c90 c100 c110 c120 c130 c140 c150 c152 c160 c170 c180 c190 c192 c200 c210 c220 c230 c240 c250 c260 c270 c280 c290 c300 c310a c310b c310c c310d c314a c314b c314c c314d c320a c320b c320c c324a c324b c324c c330 c332 c340 c350 c360 c370 c380 c390 c400 c410 c420 c430 c440 c450 c460 c490 c510a c510b c510c c510d c510e c510f c602 c604 c606 c608 c610 c612 c614 c616 c620 c640 c652 c654 c660 eof 2003033100001 20030331 00001 NE 2003 3 31 2003F00158 3 20021126 A 6111 BLADE DHAV DHC8 DHC8103 1386005 NM HAMSTD 14SF 14SF7 NE NR 2 PROPELLER CRACKED A IAHA K NONE O OTHER IN INSP/MAINT 1 WP 13 805WP 353 920913 FOUND CRACK ON NR 1 BLADE OF NR 2 ENGNE PROP ASSEMBLY. REMOVED NR 1 BLADE OF NR 2 ENGINE PROP ASSEMBLY IAW HAMILTON SUN DSTRAND MM 61-10-00, PATE 307-311 PARA 5A. INSTALLED NEW PROP BLADE IAW HAMILTON SUNSTRAND MM 61-10-00, PAGE 705-714 PA R, G/H. GROUND RUN-UP CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 6 C P7NE 2003033100023 20030331 00023 WP 2003 3 31 AALA20021709 1 20021126 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 SW 21 474 49649 DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS AT ROWS 18 AND 19 INOPERATIVE. REPLACED BATTERY PACK AT BS 104. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003033100025 20030331 00025 WP 2003 3 31 AALA20021870 1 20021225 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP BATTERY UNSECURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 480AA 49655 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS ROW 7-11 INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT BATTER Y CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003033100027 20030331 00027 WP 2003 3 31 AALA20021889 1 20021229 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 450AA 49476 DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHTS. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003033100028 20030331 00028 WP 2003 3 31 AALA20021890 1 20021228 A 3020 2026TP DUCT DOUG DC9 DC983 3022083 WP RT ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 595AA 53285 EN ROUTE DFW-MEX, DURING CLIMB-OUT AT APPROXIMATELY 14,000 FT, RT ENGINE FIRE LIGHT ILLUMINATED WITH AURAL WARNING. BO TH LOOP LIGHTS WERE ILLUMINATED, EGT REACHED APPROXIMATELY 520 DEGREES. ENGINE WAS RETARDED TO IDLE. RETURNED AND LAND ED DFW WITHOUT INCIDENT. VISUAL INSPECTION BY FIRE CREW REVEALED NO FIRE OR DAMAGE. ENGINE WAS THEN SHUTDOWN DURING TA XI IN. REPLACED RIGHT ENGINE ANTI-ICE DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2003033100060 20030331 00060 WP 2003 3 31 ASAA0280422 1 20021019 A 3350 0105606 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 21. REPLACED CONNECTOR WIRE. LIGHTS THEN OPERATED PR OPERLY. (M) 2 L 7 2 4F RT A6WE 2003033100082 20030331 00082 WP 2003 3 31 BMAC020003 2 20020421 A 7297 WIRE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE331* 01514 WP RT ENGINE BROKEN A B16A E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 535PA 687 RT EGT FLUCTUATED BETWEEN 450 AND 650, TORQUE DROPPED TO 40. EGT THEN FELL TO 100 C. TORQUE FELL TO 30 WITH CORRESPOND ING LOSS OF POWER. SHUT DOWN RT ENGINE IN FLT. REPAIRED EGT WIRE AT ENGINE DISCONNECT. RAN ENGINE IAW J-31 MM 76-13-0 0 EGT AND TQ INDICATIONS ARE NORMAL AND ALL ENGINE PARAMETERS ARE MATCHED AT THIS TIME. OK TO CONTINUE PER SPECIAL FLIG HT PERMIT. REPAIRED WIRE WAS AT THE TOP OF THE ENGINE HARNESS, ADJACENT TO THE ENGINE CONNECTOR AT THE 12 O'CLOCK POSIT ION, APPROXIMATELY 12 INCHES FORWARD OF THE FIREWALL. WIRE WAS BROKEN AND REQUIRED SPLICING. SPECIAL FLIGHT PERFORMED TO PROVIDE FUNCTIONAL EVALUATION. THE RESULTS OF THE FLIGHT WERE 'ALL ENGINE PARAMETERS ARE NORMAL AT THIS TIME. (M) 2 L 7 2 4T 3 T RT A21EU E2WE 2003040100185 20030401 00185 EU 2003 4 1 DJFA200200003 1 20021222 A 3260 C2384510 PROXIMITY SWITCH AMD FALC50 FALCON50MYST 2730106 EU MLG FAILED E DJFA O OTHER J WARNING INDICATION CL CLIMB 1 EA 23 517CW 17 GEAR WOULD NOT RETRACT AFTER TAKEOFF. PILOTS DIVERTED TO CGF. MAINTENANCE REPLACED NOSE GEAR PROXIMITY SWITCH. LANDIN G GEAR WAS RETRACTED AND FOUND TO BE OK. 2 L 7 3 4F A46EU 2003040100186 20030401 00186 EU 2003 4 1 DJFA200200004 1 20021216 A 2130 22201D071700 SELECTOR AMD FALC50 FALCON50MYST 2730106 EU CABIN PRESSURE FAILED E DJFA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 23 551CW 51 AT FLIGHT LEVEL 350, AIRCRAFT STARTED LOOSING PRESSURIZATION. PILOTS DECLARED AN EMERGENCY AND DESENDED TO 10,000 FEET. AIRCRAFT LANDED AT ITS DESTINATION WITH NO FURTHER PROBLEMS. MAINTENANCE CHANGED AUTOMATIC REGULATION SELECTOR AND OP S CHECKED OK. 2 L 7 3 4F A46EU 2003040200003 20030402 00003 EA 2003 4 2 2003F00176 1 20020829 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA LT AFT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27191 7191 DURING PRE-FLIGHT WALK AROUND, DISCOVERED LEFT AFT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE WAS CALLED. MAINTENAN CE DEFERRED UNDER 33-51-2. DURING OVERNIGHT MAINTENANCE, REPLACED THE LIGHT BULB. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2003040200010 20030402 00010 EA 2003 4 2 2003F00183 1 20020902 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 77278 7278 DURING PREFLIGHT, THE CREW DISCOVERED THAT THE FORWARD BULKHEAD EMERGENCY EXIT SIGN HAD 2 BULBS BURNED OUT. MAINTENANCE MEL'D UNDER 33-51-01-4. AIRCAFT CONTINUED OPS. DURING OVERNIGHT MAINTENANCE, THE LIGHT BULBS WERE REPLACED. OPS CHEC KS GOOD. (M) 2 L 7 2 4F RT A21EA 2003040300004 20030403 00004 SO 2003 4 3 2003F00187 1 20021112 A 2611 902081 WARNING LIGHT EMB 145 EMB145LR 3260212 SO SMOKE DETECT WILL NOT TEST A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 843MJ 145478 BAGGAGE SMOKE LIGHT INOPERATIVE ON TEST. MAINTENANCE REPLACED THE PANEL. (M) 2 L 7 2 4T RT T00011AT 2003040300006 20030403 00006 SO 2003 4 3 2003F00189 1 20021205 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO NR 4 POSITION SHORTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844MJ 145481 AIRCRAFT FOUND TO HAVE THE OVERWING EMERGENCY LIGHTS INOPERATIVE DURING OVERNIGHT MAINTENANCE. AFTER TROUBLESHOOTING, T HE CAUSE WAS FOUND TO BE THE NR 4 EMERGENCY BATTERY CHARGER WAS SHORTED. THE UNIT WAS REMOVED AND REPLACED. OPS CHECK, GOOD AT THIS TIME. ALSO, REPLACED BATTERY. (M) 2 L 7 2 4T RT T00011AT 2003040300007 20030403 00007 EA 2003 4 3 2003F00190 1 20021206 A 3350 LIGHT CNDAIR CL600 CL600* EA CABIN LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77302 7302 THE EMERGENCY EXIT FLOOR LIGHTING COVER LOOSE AT ROW 1. MAINTENANCE SECURED COVER. AIRCRAFT DEPARTED WITHOUT FURTHER I NCIDENT. (M) 2 L 7 2 4F RT A21EA 2003040300011 20030403 00011 EA 2003 4 3 2003F00194 1 20021118 A 7120 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A K NONE O OTHER IN INSP/MAINT 1 SW 07 27185 7185 LT AND RT ENGINE CENTER SUPPORT BEAM UPPER WEB FOUND TO BE CRACKED AND WILL BE REPAIRED IAW BOMBARDIER REO 601R-53-61-34 5. (M) 2 L 7 2 4F RT A21EA 2003040300015 20030403 00015 SO 2003 4 3 2003F00198 1 20021103 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO CABIN BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 831MJ 145273 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE IN ROW 12. MAINTENANCE TROUBLESHOT AND FOUND LAMP BULB INOPERATIVE. RELAMPED , OPS CHECKED GOOD. (M) 2 L 7 2 4T RT T00011AT 2003040300018 20030403 00018 EA 2003 4 3 2003F00201 1 20021112 A 3350 GE1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37208 7208 AT PREFLIGHT, THE RIGHT AFT EXT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BULB. (M) 2 L 7 2 4F RT A21EA 2003040300019 20030403 00019 SO 2003 4 3 2003F00202 1 20021126 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 831MJ 145273 NR 1 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BULB AND OPS CHECK NORMAL. (M) 2 L 7 2 4T RT T00011AT 2003040300020 20030403 00020 SO 2003 4 3 2003F00203 1 20021103 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145359 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND CONNECTOR LOOSE. RESECURED. OPS CHECK GO OD. (M) 2 L 7 2 4T RT T00011AT 2003040300024 20030403 00024 EA 2003 4 3 2003F00207 1 20020913 A 3397 RELAY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27191 7191 EMERGENCY LIGHT WILL NOT ARM IN AUTO MODE. MAINTENANCE REPLACED K1KD RELAY IN JB6. OP CHECKS GOOD. THE AIRCRAFT WAS R ETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2003040300050 20030403 00050 EA 2003 4 3 ASOA02626 1 20021213 A 3397 487191 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT SHORTED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 873AS 7549 FLT 4680, DURING GROUND INSPECTION AT ROA, THE EMERGENCY FLOOR LIGHTS FAILED BETWEEN ROWS 5 TO 9. MAINTENANCE FOUND THE LIGHT SEGMENT CONNECTION AT ROWS 5 TO 9. MAINTENANCE FOUND THE LIGHT SEGMENT CONNECTION AT ROW 5 WET, CAUSING IT TO SH ORT OUT, AND CLEANED THE CONNECTION. SYSTEM AND OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003040300052 20030403 00052 EU 2003 4 3 ASOA02640 1 20021224 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU FUSELAGE INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 533AS 460 FLT 4309 - DURING GROUND INSPECTION IN ATL, SEVERAL EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2003040300053 20030403 00053 EA 2003 4 3 ASOA02641 1 20021224 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 903EV 7621 DURING GROUND INSPECTION IN DFW, THE LT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE BURNED OUT EXTERIOR LIGHT BULB. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003040300054 20030403 00054 EA 2003 4 3 ASOA02642 1 20021224 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA COCKPIT DETECTED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 885AS 7521 FLT 4769 - DURING CRUISE FLIGHT FROM ATL-ILM, WHILE DESCENDING THROUGH 19,000 FEET AND AFTER RETARDING THE POWER TO 50 P ERCENT N1, A STRONG BURNING ODOR OCCURRED IN TEH COCKPIT. THE AIRCRAFT LANDED SAFELY IN ILM. MAINTENANCE INSPECTED BOT H PACKS AND HAD THE CREW OPERATE THE AIRCRAFT. NO SMOKE ODOR COULD BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2003040300056 20030403 00056 EA 2003 4 3 ASOA02644 1 20021224 A 4920 CONTROL VALVE CNDAIR CL600 CL6002B19 1900309 EA APU INOPERATIVE A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 885AS 7521 FLT 4770 - DURING CRUISE FLIGHT FROM ILM-ATL, WHILE DESCENDING THROUGH 20,000 FEET AND AFTER RETARDING THE POWER TO 50 P ERCENT N1, AN ODOR OF SMOKE OCCURRED IN THE COCKPIT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLAC ED THE LOAD CONTROL VALVE IN THE AUXILIARY POWER UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003040300058 20030403 00058 SO 2003 4 3 ASOA02646 1 20021226 A 5320 12010369601 CLIP EMB 120 EMB120RT 3260202 SO FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 238AS 120053 DURING HANGAR INSPECTION IN TXK, THE SKIN SHEAR CLIP ON FRAMES 15 AND 15A WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTE NANCE REMOVED AND REPLACED THE SKIN SHEAR CLIP ON FRAMES 15 AND 15A IAW SRM 53-10-04. (M) 2 L 7 2 4T RT A31SO 2003032800104 20030328 00104 WP 2003 3 28 DHL2002873003 1 20021220 A 2610 BRACKET DOUG DC8 DC873F 302199F WP NR 3 FIRE LOOP FAILED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 873SJ 46091 NR 3 ENGINE SHORT CIRCUIT LIGHT ILLUMINATES INTERMITTENTLY. REMOVED AND REPLACED FIRE LOOP ATTACH BRACKET NR 3 ENGINE A T HIGH STAGE BLEED VALVE AREA PER SRM 51-1-0 AND 51-3-0, OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2003033100007 20030331 00007 NM 2003 3 31 2003F00165 1 20021214 A 2497 WIRE BOEING 727 727200 138407E NM ELECTRICAL SHORTED A P76A K NONE O OTHER IN INSP/MAINT 1 SO 17 894AA 22010 UPON ENTRY INTO COCKPIT FOUND RIGHT DUCT PRESSURE NEEDLE FLUCTUATING W/WPU OFF, NR 2 FUEL HEAT VALVE C/B POPPING, NR 2 E NGINE OIL PRESSURE INDICATOR FLUCTUATING. NR 3 WING ANTI-ICE VALVE C/B POPPING. NR F/F AND NR 2 EPR POPS C/B. SHORTED WIRES FOUND BURNED AT AFT PRESSURE BULKHEAD AREA ABOVE ENTRY DOOR RIGHT SIDE JUST AFT OF PRESSURE BULKHEAD. INITIAL INS PECTION REVEALED WIRE BUNDLE W-082 AT PRESSURE BULKHEAD (AFT) ISOLATION COMPLETELY BURNED ON NUMEROUS WIRES IN SAME BUND LE. ADJACENT WIE BUNDLES AFFECTED ARE W-342, W-350 W-152, W-558, W-843, W-358. REPLACEMETN TO ALL AFFECTED WIRES IN WO RK, AND FULL SYSTEMS OPS CHECKS TO FOLLOW ON ALL AFFECTED SYSTEMS. (M) 2 L 7 3 4F RT A3WE 2003033100024 20030331 00024 WP 2003 3 31 AALA20021778 1 20021209 A 2120 97968011 CONTROL VALVE DOUG DC9 DC982 3022082 WP ACM BAY FAILED A AALA G O2 MASK DEPLOYED J WARNING INDICATION DE DESCENT 1 SW 21 274AA 49271 EN ROUTE PDX-ORD, DURING CRUISE, CABIN GOT VERY COLD. BOTH PACK PRESSURES OK. CABIN STARTED CLIMBING, INITIATED EMERGE NCY DESCENT. CABIN MASKS DEPLOYED AND SPENT. PACK PRESSURE INDICATED ZERO IN DESCENT. BELOW 10,000 FEET PACKS REINSTA TED. LANDED ORD WITHOUT INCIDENT. REPLACED LEFT AND RIGHT WATER SEPARATOR TEMPERATURE CONTROL VALVES. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003040200001 20030402 00001 SO 2003 4 2 2003F00174 1 20020828 A 2750 CONNECTOR EMB 145 EMB145LR 3260212 SO TE FLAPS LOOSE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 855MJ 145614 FLAP FAIL MESSAGE INBOUND. THE CREW DECLARED AN EMERGENCY. MAINTENANCE FOUND A LOOSE CONNECTOR AT THE FECU AND RESECUR ED. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2003040200008 20030402 00008 EA 2003 4 2 2003F00181 1 20020901 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 17217 7217 DISCOVERED THE EMERGENCY FLOOR LIGHTS INOPERATIVE FROM ROW 5 TO 9. MAINTENANCE WAS CALLED. MAINTENANCE SECURED THE CON NECTOR AT ROW 5. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2003040300002 20030403 00002 NM 2003 4 3 2003F00185 1 20021112 A 3350 20131A BATTERY PACK DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE NR 1 BATTERY PACK. (M) 2 H 7 2 4T RT A13NM 2003040300016 20030403 00016 EA 2003 4 3 2003F00199 1 20021112 A 3350 GE1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47239 7239 LEFT AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE RELAMPED. (M) 2 L 7 2 4F RT A21EA 2003040300017 20030403 00017 SO 2003 4 3 2003F00200 1 20021112 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145359 EMERGENCY LIGHTS WILL NOT EXTINGUISH FROM ROW 12 AFT IN CABIN. MAINTENANCE REPLACED THE BATTERY PACK ASSEMBLY. (M) 2 L 7 2 4T RT T00011AT 2003040300048 20030403 00048 EA 2003 4 3 ASOA02624 1 20021209 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 827AS 7212 DURING HANGAR INSPECTION IN BTR, THE NR 3 WINDSHIELD WAS FOUND TO BE CRACKED FROM TOP TO BOTTOM. MAINTENANCE REMOVED AN D REPLACED THE NR 3 WINDSHIELD. OPERATIONAL AND PRESSURE CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003040300055 20030403 00055 EA 2003 4 3 ASOA02643 1 20021224 A 4900 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY SHUTDOWN A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 11 824AS 7203 FLT 4680 - DURING DESCENT INTO ATL AT APPROXIMATELY 13,000 FEET, THE AUXILIARY POWER UNIT SHUT ITSELF DOWN AUTOMATICALLY . THE CREW WAITED APPROXIMATELY TWO MINUTES AND RE-STARTED IT, AFTER WHICH THE ODOR OF FUEL OCCURRED IN THE COCKPIT AND CABIN. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE CLEANED THE OIL PRESSURE SWITCH (P/N 3876001-6) CONNECTOR PLUG AND TIGHTENED THE FUEL LINE (P/N 3883449-1) ON THE FUEL CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE . (M) 2 L 7 2 4F RT A21EA 2003040300062 20030403 00062 EA 2003 4 3 ASOA02650 1 20021228 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 858AS 7417 FLT 4042 - DURING GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 2 THROUGH 5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR FLEXIBLE LAMP STRIP BETWEEN ROWS 2 THROUGH 5. OPERA TIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003040300098 20030403 00098 WP 2003 4 3 DJFA200300002 2 20021227 A 7250 30606901 BLADE BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE7315BR WP TUBINE SECTION BROKEN E DJFA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 23 816CW 258016 P91132 AIRCRAFT DEPARTED SLC, ON CLIMBOUT THE PILOTS EXPERIENCED A VIBRATION. REDUCED POWER AND VIBRATION WENT AWAY. THE PILO TS DECIDED TO RETURN TO SLC AND LANDED WITH NO FURTHER PROBLEMS. INVESTIGATING THE TAIL PIPE OF THE ENGINE, FOUND A PIE CE OF THE THIRD STAGE TURBINE WHEEL BLADE BROKEN OFF AND STUCK IN THE TAIL PIPE OF THE ENGINE. 2 L 7 2 4F 4 F RT A3EU E6WE 2003040400078 20030404 00078 NM 2003 4 4 DL767030092 1 20020126 A 2910 AE70577778 LINE BOEING 767 767232 1385132 NM NR 2 ENGINE CHAFED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 104DA 22216 PILOT REPORT--AT 2500 AFTER T/O RT RSVR AND RT ENG PRESS LIGHT ILLUMINATED TOWER REPORTED SMOKE FROM RT ENGINE. RETURNE D TO LAS NORMAL LANDING. RT HYD QTY ON EICAS IND -0- AND RF OVERWEGHT LANDING ACT LANDING WT 273100. FOUND NR 2 ENGIN E HYD PRESSURE LINE FROM PUMP CHAFED AND LEAKING. REPLACED NR 2 ENG EDP PRESSURE LINE PER M/M, LEAK CHECK OK. 2 L 7 2 4F RT A1NM 2003040400083 20030404 00083 NM 2003 4 4 ASAA0210349 1 20021204 A 5414 657377391 SKIN BOEING 737 7372Q8C 138448S NM NR 1 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL AT NACELLE STATION 205 GOUGED. REMOVED DAMAGE AND REPAIRED NR 1 ENGINE COWL PER SRM. (M) 2 L 7 2 4F A16WE 2003040400085 20030404 00085 NM 2003 4 4 ASAA0210352 1 20021204 A 5410 657377391 CHANNEL BOEING 737 7372Q8C 138448S NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL U-CHANNEL AT NACELLE STATION 170.25 CRACKED .25 INCH. REMOVED DA MAGED U-CHANNEL AND REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2003040400087 20030404 00087 NM 2003 4 4 ASAA0210354 1 20021204 A 5414 657377482 SKIN BOEING 737 7372Q8C 138448S NM NR 2 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL FRAME AT NACELLE STATION 188.64 GOUGED. REMOVED DAMAGED FRAME SE CTION AND REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2003040400088 20030404 00088 NM 2003 4 4 ASAA0210355 1 20021204 A 5410 6552263275 FAIRING BOEING 737 7372Q8C 138448S NM NR 1 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE FIXED FAIRING PLATES AT NACELLE STATION 208.67 GOUGED. REMOVED AND RE PLACED PLATES PER SRM. (M) 2 L 7 2 4F A16WE 2003040400089 20030404 00089 NM 2003 4 4 ASAA0210356 1 20021204 A 5414 65522632 SKIN BOEING 737 7372Q8C 138448S NM NR 2 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL AT NACELLE STATION 222.25 GOUGED. REMOVED DAMAGED AREA AND REPAI RED PER SRM. (M) 2 L 7 2 4F A16WE 2003040400090 20030404 00090 NM 2003 4 4 ASAA0210357 1 20021204 A 5310 654585547 BEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND CREASE BEAM SUPPORT ANGLE AT BODY STATION 207, RIGHT BUTTOCK LINE 60 CORRODED. RE MOVED AND REPLACED CREASE BEAM SUPPORT ANGLE PER SRM. (M) 2 L 7 2 4F A16WE 2003040400095 20030404 00095 NM 2003 4 4 ASAA0210362 1 20021204 A 3233 65448106 ACTUATOR BOEING 737 737290C 138448V NM RT MLG FAULTY A ASAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 01 742AS 12679 23136 ANC - ON APROACH INTO ANC, RIGHT MLG DID NOT EXTEND ON FIRST TRY. RT MLG EXTENDED ON SECOND ATTEMPT. REMOVED AND REPLA CED RIGHT MLG LIB/ROB LOCK ACTUATOR, THEN GEAR CYCLED SEVERAL TIME WITH NO PROBLEMS. (M) 2 L 7 2 4F A16WE 2003040400096 20030404 00096 NM 2003 4 4 ASAA0210363 1 20021205 A 5315 6545811522 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM FLANGE AT BS 986, LEFT BUTTOCK LINE 17-RIGHT BUTTOCK LINE 37 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM FLANGE PER EA. (M) 2 L 7 2 4F A16WE 2003040400098 20030404 00098 NM 2003 4 4 ASAA0210365 1 20021205 A 5414 657377482 SKIN BOEING 737 7372Q8C 138448S NM NR 2 NACELLE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL SKIN AT NACELLE STATION 109.25 DENTED. REMOVED DAMAGED AREA AND REPAIRED LEADING EDGE PER SRM. (M) 2 L 7 2 4F A16WE 2003040400101 20030404 00101 NM 2003 4 4 ASAA0210368 1 20021205 A 5414 657377391 SKIN BOEING 737 7372Q8C 138448S NM NA 1 NACELLE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL AT NACELLE STATION 192.65 WITH AN ELONGATED HOLE. REMOVED AND RE PAIRED DAMAGED AREA PER SRM. (M) 2 L 7 2 4F A16WE 2003040400102 20030404 00102 NM 2003 4 4 ASAA0210370 1 20021207 A 5414 65522632 SKIN BOEING 737 7372Q8C 138448S NM NR 1 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL AT NACELLE STATION 150.25 GOUGED. REMOVED AND REPAIRED DAMAGED A REA PER SRM. (M) 2 L 7 2 4F A16WE 2003040400103 20030404 00103 NM 2003 4 4 ASAA0210371 1 20021207 A 5414 6552263275 CHANNEL BOEING 737 7372Q8C 138448S NM NR 1 NACELLE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL U-CHANNEL AT NACELLE STATION 122.25-149.25 CHAFED. REMOVED AND R EPAIRED DAMAGED AREA PER SRM. (M) 2 L 7 2 4F A16WE 2003040400104 20030404 00104 NM 2003 4 4 ASAA0210372 1 20021207 A 5411 FRAME BOEING 737 7372Q8C 138448S NM NR 1 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL FRAME AT NACELLE STATION 180 GOUGED. REPAIRED DAMAGED AREA PER S RM. (M) 2 L 7 2 4F A16WE 2003040400105 20030404 00105 NM 2003 4 4 ASAA0210373 1 20021207 A 5411 RIB BOEING 737 7372Q8C 138448S NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL RIB AT NACELLE STATION 154 GOUGED. REPAIRED DAMAGED COWL AREA PE R SRM. (M) 2 L 7 2 4F A16WE 2003040400106 20030404 00106 NM 2003 4 4 ASAA0210374 1 20021208 A 5411 RIB BOEING 737 7372Q8C 138448S NM NR 1 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL RIB AT NACELLE STATION 173 GOUGED. REPAIRED DAMAGED COWL PER SRM . (M) 2 L 7 2 4F A16WE 2003040400107 20030404 00107 NM 2003 4 4 ASAA0210375 1 20021208 A 5410 6573769 FAIRING BOEING 737 7372Q8C 138448S NM NR 1 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL FAIRING AT NACELLE STATION 137 GOUGED. REPAIRED DAMAGED COWL FAI RING PER SRM. (M) 2 L 7 2 4F A16WE 2003040400108 20030404 00108 NM 2003 4 4 ASAA0210376 1 20021208 A 5410 6552263125 CHANNEL BOEING 737 7372Q8C 138448S NM NR 1 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL CHANNEL AT NACELLE STATION 180 GOUGED. REPAIRED DAMAGED COWL CHA NNEL PER SRM. (M) 2 L 7 2 4F A16WE 2003040400109 20030404 00109 NM 2003 4 4 ASAA0210377 1 20021208 A 5411 6573774 RIB BOEING 737 7372Q8C 138448S NM NR 1 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL RIB AT NACELLE STATION 200.5 GOUGED. REPAIRED DAMAGED COWL RIB P ER SRM. (M) 2 L 7 2 4F A16WE 2003040400110 20030404 00110 NM 2003 4 4 ASAA0210378 1 20021208 A 5411 65ND7127623 RIB BOEING 737 7372Q8C 138448S NM NR 1 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL RIB AT NACELLE STATION 99.25-116.5 GOUGED. REPAIRED DAMGAED COWL RIB PER SRM. (M) 2 L 7 2 4F A16WE 2003040400111 20030404 00111 NM 2003 4 4 ASAA0210380 1 20021208 A 5320 6577487100 ANGLE BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND ANGLE AT BS 993, LEFT BUTTOCK LINE 14.5 CORRODED. REMOVED AND REPLACED ANGLE PER SRM. (M) 2 L 7 2 4F A16WE 2003040400112 20030404 00112 NM 2003 4 4 ASAA0210382 1 20021209 A 5315 65549067 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 500B, RIGHT BUTTOCK LINE 20, LEFT BUTTOCK LINE 40 CORRODED. REMOV ED AND REPLACED LOWER CHORD PER EA. (M) 2 L 7 2 4F A16WE 2003040400113 20030404 00113 NM 2003 4 4 ASAA0210383 1 20021209 A 5410 6552263275 CHANNEL BOEING 737 7372Q8C 138448S NM NR 1 NACELLE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL U-CHANNEL AT NACELLE STATION 122.25 CHAFED. REMOVED DAMAGED U-CH ANNEL AND FABRICATED REPAIRS PER SRM. (M) 2 L 7 2 4F A16WE 2003040400122 20030404 00122 SO 2003 4 4 ASOA02652 1 20021228 A 3350 WIRE EMB 120 EMB120RT 3260202 SO CABIN BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 283AS 120236 FLT 4056 - DURING GROUND INSPECTION IN ATL, THE EXTEROR RIGHT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE FUSE ABOVE ROWS 7 AND 8, AND ALSO REPAIRED THE BROKEN GROUND WIRE (P/N M22759-20-9) ON THE EXTERIOR RIGHT AFT EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2003040400126 20030404 00126 WP 2003 4 4 GTIA021388 1 20021226 A 5280 DOOR DOUG DC9 DC982 3022082 WP MLG DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND RIGHT MAIN LANDING GEAR FLYING DOOR DELAMINATED. REMOVED RIGHT MAIN LANDING GEAR OUTBOARD GEAR DOOR. REPAIR ED DELAMINATED AREA. INSTALLED RIGHT MLG DOOR. (M) 2 L 7 2 4F A6WE 2003040700002 20030407 00002 WP 2003 4 7 ASAA0280664 1 20021220 A 3350 1001191 BATTERY PACK DOUG DC9 DC982 3022082 WP FWD PAX ENTRY INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 34450 3905 49235 DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY, INCLUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2003040700030 20030407 00030 WP 2003 4 7 GTIA021391 1 20021231 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND L-1 DOOR UPPER FRAME CRACKED IN FORWARD AND AFT RADIUS. STOP, DRILLED AFT AND FORWARD SIDE AT L-1 DOOR UPPE R FRAME. INSTALLED FITTINGS AND DOUBLER. (M) 2 L 7 2 4F A6WE 2003040700032 20030407 00032 NE 2003 4 7 GTIA021394 2 20021224 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LEFT FAILED A GTIA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 23 808NK 49504 718062 DEN - FLT 980 - IN FLIGHT ENGINE FAILURE OF LEFT ENGINE. REMOVED AND REPLACED NR 1 ENGINE. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2003040700034 20030407 00034 WP 2003 4 7 GTIA021396 1 20021225 A 5730 PANEL DOUG DC9 DC982 3022082 WP LT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND LT WING TRAP PANEL DELAMINATED. REMOVED LT WING TRAP PANEL. REPAIRED LT WING TRAP PANEL. INSTALLED LT WIN G TRAP PANEL. (M) 2 L 7 2 4F A6WE 2003040700049 20030407 00049 2003 4 7 I5HA0258008 4 20021101 A 3497 FD108 WIRE CVAC 580 580 2422806 WP FLIGHT DIRECTOR LOOSE A I5HA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 581P 29 WHILE EN ROUTE FROM CVG-PIT, THE CAPTAIN NOTICED A MOMENTARY PUFF OF SMOKE COMING FROM THE FLIGHT DIRECTOR. THE FLIGHT DIRECTOR FUSELAGE WAS REMOVED AND THE FLIGHT WAS CONTINUED UNEVENTFULLY AND TERMINATED IN PIT. A LOOSE POWER WIRE ON TH E FLIGHT DIRECTOR CONNECTOR PLUG HAD ARCED MOMENTARILY AGAINST THE PLUG SHELL. THE WIRE WAS REPAIRED AND THE AIRCRAFT R ETURNED TO SERVICE. NO FURTHER ACTION IS REQUIRED AT THIS TIME. REFER TO AIR TAHOMA LOG PAGE NR 64108. FLIGHT DIRECTO R P/N FD108. (M) 2 L 7 2 4T RT 2003040700059 20030407 00059 EU 2003 4 7 SIMA200234507 1 20021206 A 5230 7241001025 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 375AE 340B375 ABI - DURING AN MBV INSPECTION, A DENT WAS FOUND IN THE LOWER AFT CORNER OF THE CARGO DOOR THAT WAS ALSO DISBONDED. REM OVED THE TOPCOAT DOWN TO, BUT NO THROUGH THE BONDING PRIMER IN THE AFFECTED AREA. PERFORMED A CUTOUT OF THE DISBONDED A REA. FABRICATED A FILLER PLATE AND REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS004764 PARA 3. (M) 2 L 7 2 4T RT A52EU 2003040700061 20030407 00061 SO 2003 4 7 SIMA200300603 1 20021226 A 5553 14540881001 FITTING EMB 135 EMB135LR 3260305 SO VERTICAL STAB GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 700LE 145156 ABI - DURING AN IMBV INSPECTION, VERTICAL STABILIZER FITTINGS THAT ATTACH TO THE HORIZONTAL STABILIZER WERE FOUND TO BE GOUGED. REMOVED GOUGES BY REAMING LEFT AND RIGHT FITTINGS TO 2.2834 INCH. REPAIR DONE IAW EMB GST-3689/02. (M) 2 L 7 2 4F RT T00011AT 2003040700068 20030407 00068 SO 2003 4 7 SIMA200300814 1 20021218 A 5320 14521725001 SILL EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 700LE 145156 ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION GALLEY AREA LEFT SILL HAS CORROSION. REMOVED AND INSTAL LED SERVICEABLE SILL IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2003040700071 20030407 00071 SO 2003 4 7 SIMA200300817 1 20021218 A 5320 14521721009 SILL EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 700LE 145156 ABI - THIS IS LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION SERVICE DOOR FORWARD SILL HAS CORROSION. REMOVED AND INST ALLED SERVICEABLE SILL IAW EMB 135 SRM 51-14-02. (M) 2 L 7 2 4F RT T00011AT 2003032800095 20030328 00095 EU 2003 3 28 CX7A194J26 1 20021219 A 2613 SENSOR SAAB SF340 340B 7860101 EU LT TAIL PIPE CONTAMINATED A CX7A C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 03 307CE 340B204 DURING T/O ROLL LT TAILPIPE HOT IND CAME ON. 2 L 7 2 4T RT A52EU 2003032800096 20030328 00096 EU 2003 3 28 CX7A194J27 1 20021219 A 2613 1734362450 SENSOR SAAB SF340 340B 7860101 EU RT TAILPIPE CONTAMINATED A CX7A C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 03 305CE 340B202 RT ENGINE TAILPIPE HOT CWP ILLUMINATED. ABORTED T/O. 2 L 7 2 4T RT A52EU 2003033100004 20030331 00004 2003 3 31 2003F00162 4 20020320 A 3434 ALV9510R ALTERNATOR CESSNA 421 421B 2076014 CE ENGINE FAILED A BLIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 17 65AE 421B0953 ON PREP FOR DEPARTURE, RETURNED TO RAMP AND CALLED MAINTENANCE. ARRANGED FOR ALTERNATOR REPLACEMENT BY PIEDMONT. AIRCR AFT RETURNED IRS. (M) 1 L 7 2 3O A7CE 2003033100014 20030331 00014 NM 2003 3 31 2003F00166 1 20021211 A 3110 WIRE HARNESS BOEING 727 727223 1384074 NM INSTRUMENT PANEL BURNED A P76A K NONE O OTHER IN INSP/MAINT 1 SO 17 894AA 22010 WHEN APPLYING GROUND POWER TO A/C NOTICED FE PANEL INSTRUMENTS FLUCTUATING AND CIRCUIT BREAKERS POPPING. SHUT DOWN GROU ND POWER AND UPON INSPECTION FOUND WIRE BUNDLES AFT OF 1183 PRESSURE BULKHEAD BURNED. BUNDLES AFFECTED WERE W-082, W-34 2, W-350, W-152, W-558, W-843 AND W-358. REPLACED AFFECTED WIRES AND PERFORMED OPERATIONAL CHECKS ON ALL SYSTEMS. OPS CHECKED OK PER MM. SUSPECT WIRE CHAFFING IN BUNDLE W-082. (M) 2 L 7 3 4F A3WE 2003033100022 20030331 00022 WP 2003 3 31 AALA20021683 1 20021123 A 2150 DUCT DOUG DC9 DC982 3022082 WP RT A/C SYSTEM RUPTURED A AALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 223AA 49173 AFTER TAKEOFF AT APPROXIMATELY 18000 TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED. DECLARED EMERGENCY AND RETURNED TO M CO. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND RUPTURED DUCT ON RT AIR CONDITIONING SYSTEM. REPLACED DUCT. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003033100026 20030331 00026 WP 2003 3 31 AALA20021871 1 20021223 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 480AA 49655 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS IN FIRST CLASS WILL NOT FULLY EXTINGUISH. REPAIRED EMERGENC Y EXIT LIGHT BATTERY WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003033100062 20030331 00062 WP 2003 3 31 ASAA0280438 1 20021025 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP FWD PAX ENTRY INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 949AS 53022 DUIRNG LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY, INCLUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2003033100063 20030331 00063 WP 2003 3 31 ASAA0280624 1 20021209 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP FWD CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING LINE CHECK, FOUND FORWARD CABIN EMERGENCY LIGHTING ON WITH POWER OFF. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2003033100064 20030331 00064 WP 2003 3 31 ASAA0280625 1 20021210 A 3350 1001191 BATTERY PACK DOUG DC9 DC983 3022083 WP FWD PAX ENTRY INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 18473 2119 53023 PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLCED LIGHT ASSEMBLY, INCL UDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2003040100187 20030401 00187 CE 2003 4 1 DJFA200200007 1 20021225 A 7910 O-RING CESSNA 650 650 2076802 CE OIL FILLER TUBE BROKEN E DJFA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 23 381CW 6500111 ENGINE OIL PRESSURE DROPPED. THE PILOTS SHUT DOWN LT ENGINE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFLEY AT SAV. MAINTENANCE FOUND O-RING ON OIL FILLER TUBE BROKEN. REPLACED O-RING AND GROUND RUNS WERE FOUND TO BE OK. 2 L 7 2 4F A9NM 2003040200009 20030402 00009 SO 2003 4 2 2003F00182 1 20020901 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO FAILED INOPERATIVE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 829MJ 145228 DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT THE EMERGENCY EXIT LIGHT AT ROW 3 RIGHT INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE INVERTER. OP CHECKS GOOD. (M) 2 L 7 2 4T RT T00011AT 2003040300001 20030403 00001 EA 2003 4 3 2003F00184 1 20021112 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77181 7181 EMERGENCY ESCAPE PATH LIGHT INOPERATIVE FROM ROW 2 TO ROW 5. MAINTENANCE PERFOREMD OPS CHECK IAW MM 33-51-04 AND LIGHTS FUNCTION NORMALLY. (M) 2 L 7 2 4F RT A21EA 2003040300008 20030403 00008 SO 2003 4 3 2003F00191 1 20021214 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCONNECTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 826MJ 145214 EMERGENCY EXIT SIGN AT ROW 12 DF DOES NOT LIGHT UP. MAINTENANCE TROUBLESHOT AND FOUND WIRES OFF CONNECTOR AND RESECURED WIRE. OPS CHECKED GOOD AT THIS TIME. M) 2 L 7 2 4T RT T00011AT 2003040300009 20030403 00009 SO 2003 4 3 2003F00192 1 20021212 A 3350 210114 CHARGER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 825MJ 145179 PREFLIGHT, ROW 12 EMERGENCY EXIT LIGHTS INOPERATIVE ON LEFT AND RIGHT OVERHEAD. MAINTENANCE REPLACED THE BATTERY CHARGE R ASSEMBLY. (M) 2 L 7 2 4T RT T00011AT 2003040300010 20030403 00010 SO 2003 4 3 2003F00193 1 20021227 A 2611 BULB EMB 145 EMB145LR 3260212 SO CARGO BAY BURNED OUT A K NONE L NO TEST IN INSP/MAINT 1 SW 07 843MJ 145478 BAGGAGE SMOKE DETECTION LIGHT INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND LAMPS BURNED OUT. MAINTENANCE RELAMPED. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2003040300022 20030403 00022 SO 2003 4 3 2003F00205 1 20021103 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145359 OVERHEAD EMERGENCY EXIT LIGHT ABOVE FAS JUMPSEAT INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND CONNECTOR LOOSE. RESEC URED. OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2003040300023 20030403 00023 SO 2003 4 3 2003F00206 1 20021202 A 3350 GE1317 LIGHT EMB 145 EMB145LR 3260212 SO GALLEY INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 846MJ 145507 PILOT REPORTED THE EMEGENCY EXIT LIGHTS IN THE GALLEY AREA INOPERATIVE. MAINTENANCE REPLACED THE LIGHT. (M) 2 L 7 2 4T RT T00011AT 2003040300060 20030403 00060 EA 2003 4 3 ASOA02648 1 20021226 A 5610 NP1393219 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 859AS 7421 FLT 4397 - WHILE BOARDING THE AIRCRAFT IN YUL-ATL, THE CREW DISCOVERED AN APPROXIMATE 8 INCH CRACK AT THE BOTTOM OF THE CAPTAINS WINDSHIELD. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD. OPS AND HEAT CHECKS GOOD. AIRCAFT OK F OR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003040300061 20030403 00061 EU 2003 4 3 ASOA02649 1 20021228 A 3350 3011210 LIGHT AEROSP ATR72 ATR72 EU AIRSTAIR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 640AS 405 DURING HANGAR INSPECTION IN MCN, THE AIR STAIR DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE AIR STAIR DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2003040300063 20030403 00063 EA 2003 4 3 ASOA02651 1 20021228 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 855AS 7395 FLT 4580 - DURING GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR TRACK LIGHTING IN THE FORWARD SECTION WAS FOUND TO BE IN OPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR FLEXIBLE LAMP STRIP BETWEEN ROWS 2 THROUGH 5. OPERATION AL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003040700095 20030407 00095 NM 2003 4 7 TSAA0253116 1 20020404 A 5310 654578832 WINDOW FRAME BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW S/B 737-53A1177R 6 AND DISCOVERED DEFECTS IN WINDOW CORNERS WITH CR ACK INDICATION AT BS 867 RIGHT WINDOW BOTTOM FORWARD CORNER USING HFEC METHODS. TRIMMED OUT THE THREE HOLES IN THE DAMA GED AREA. HFEC THE EDGE OF THE TRIM. ENLARGED TRIM BY .04 INCHS, AN INSURANCE CUT MAINTAINING A .05 INCH MINIMUM CORN ER RADIUS AND 2D EDGE MARGIN FROM FASTENERS. REPAIRED IAW SRM AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003032800051 20030328 00051 SO 2003 3 28 C2XA03TY042 1 20020327 A 5320 14526437001 CHANNEL EMB 145 EMB145LR 3260212 SO LAVATORY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16954 145072 DURING A SCHEDULED INSPECTION THE LAVATORY FLOOR CHANNEL CAP WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE LAVATORY FLOOR CHANNEL CAP IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2003032800052 20030328 00052 NM 2003 3 28 C8GA20020014 1 20021226 A 5754 CARRIAGE BOEING 727 727223 1384074 NM LE FLAP DAMAGED A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 715AA 22470 FLT 041 FROM MIA TO AUA. AFTER TAKEOFF DURING CLIMB, THE OUTBOARD TRAILING EDGE FLAPS WOULD NOT RETRACT, STUCK BETWEEN T WO AND FIVE DEGREES. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. UPON LANDING, DURING INSPECTION FOUND A BROKE N BOLT AND MISSING BEARING ON LEFT FORE FLAP SEQUENCING CARRIAGE. REPLACED BOLT AND BEARING AND CHECKED FLAP RIGGING. AL L FLAPS OPERATIONAL CHECKED GOOD IAW MM 27-50-00 AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2003033100002 20030331 00002 WP 2003 3 31 2003F00160 2 20020215 A 7320 5001T39G29 FUEL CONTROL AMD FALC20 FALCON 2720302 EU GARRTT TPE331 TPE331* 01514 WP NR 1 ENGINE MALFUNCTIONED A CEDA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 05 209CA 7390 71 NR 1 ENGINE HAD FLAME OUT AT FL350 WHILE CLIMBING TO FL370. AIRCRAFT LANDED AT AMA WITH NO FURTHER PROBLEM. MAINTENANC E INSPECTED ENGINE AND RESET FUEL DENSITY SETTING ON FUEL CONTROL. (M) 2 L 7 2 4F 3 T A7EU E2WE 2003033100003 20030331 00003 WP 2003 3 31 2003F00161 2 20021218 A 7532 97881251 BLEED VALVE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP NR 2 ENGINE STICKING A IMJA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 25 50MJ 164 P74519 RIGHT ENGINE DEVELOPED ITT SPLIT 60 DEGREES HOTTER THAN NR 1. EXTENSIVE MAINTENANCE TROUBLESHOOTING WITH NUMEROUS GROUND RUNS COULD NOT DUPLICATE THIS PROBLEM. ENGINE WAS ACCESSED TO SURGE BLEED VALVE DUE TO SUPPOSED INTERMITTENT STICKING. REPLACED SURGE BLEED VALVE. (M) 2 L 7 2 4F 4 F A10CE E6WE 2003033100005 20030331 00005 EU 2003 3 31 2003F00163 1 20021213 A 3210 LANDING GEAR AMD FALC50 FALCON50MYST 2730106 EU MAIN MALFUNCTIONED A I5VA O OTHER J WARNING INDICATION AP APPROACH 1 NE 03 163WW 052 ON APPROACH INTO TEB, THE LANDING GEAR HANDLE WAS MOVED TO LOWER THE GEAR. BOTH MAIN LANDING GEAR TRANSITON LIGHTS CAME ON AND THE GEAR DID NOT EXTEND. THE FLIGHT CREW USED THE EMERGENCY SYSTEM TO LOWER AND LOCK THE GEAR IN PLACE. (M) 2 L 7 3 4F A46EU 2003033100006 20030331 00006 NM 2003 3 31 2003F00164 1 20021120 A 3397 WIRE DHAV DHC8 DHC8103 1386005 NM EMERGENCY LIGHT BROKEN A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807WP 023 EMERGENCY ESCAPE PATH LIGHT ROW 5 BROKEN WIRE IN LAMP MODULE. REMOVED AND REPLACED LAMP MODULE IAW DHC-8 MM 33-52-22 PA GE 201 AND 202. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 2003033100061 20030331 00061 WP 2003 3 31 ASAA0280423 1 20021019 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP FWD CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROWS 1-3. REATTACHED CONNECTOR. LIGHTS THEN OPERATED PRO PERLY. (M) 2 L 7 2 4F RT A6WE 2003033100083 20030331 00083 EU 2003 3 31 BMAC020024S 1 20021031 A 7600 CONNECTOR BAG JETSTM JETSTM3101 1500215 EU ENGINE CONTAMINATED A B16A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 536PA 681 PILOT REPORTED BRIEF ENGINE POWER LOSS ON RT ENGINE FROM 60 PERCENT TO 10 PERCENT TORQUE NOTED, (TWO TIMES) SHUT SRL AND TTL OFF. FLT UNEVENTFUL, WITHOUT INCIDENT FOR LAST 15 MINUTES AND SRL AND TTL STAYED OFF. PILOT ELECTED TO AIR RETURN TO CBE. MAINTENANCE DEFERRED BOTH SRL AND TTL SYSTEMS UNTIL FURTHER INDEPTH T/S CAN BE PERFORMED. AFTER EXTENSIVE TRO UBLE-SHOOTING AND CHECKS, FOUND PLUG ER-2P CONNECTOR CONTAMINATED WITH OIL. AFTER CLEANING, COULD NOT DUPLICATE ORIGINA L DISCREPANCY. AS OF 11-20-2002. THE A/C HAD FLOWN APPROX FORTY FLIGHTS WITH-OUT REPEAT OF DISCREPANCY. 2 L 7 2 4T RT A21EU 2003040200002 20030402 00002 SO 2003 4 2 2003F00175 1 20020903 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT UNSECURE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 826MJ 145214 AFT CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE RESECURRED CONNECTOR PLUG AT LIGHT ASSEMBLY. OPS CHECKS GOO D. (M) 2 L 7 2 4T RT T00011AT 2003040200006 20030402 00006 EA 2003 4 2 2003F00179 1 20020829 A 2611 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA CARGO SMOKE FALSE ACTIVATION A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 27185 7185 WHILE EN ROUTE, CARGO SMOKE ANNUNCIATOR ILLUMINATED MOMENTARILY. WHEN THE AIRCRAFT ARRIVED IN PHX, MAINTENANCE PERFORME D AN OPS CHECK. NO DISCREPANCY WAS FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2003040200007 20030402 00007 EA 2003 4 2 2003F00180 1 20020617 A 3350 1337 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17337 7337 CEILING EMERGENCY LIGHTS NR 1 AND NR 4 INOPERATIVE. MEL'D 33-01-1. MAINTENANCE REPLACED THE LIGHT BULB. OP CHECKS GOO D. (M) 2 L 7 2 4F RT A21EA 2003040300005 20030403 00005 2003 4 3 2003F00188 4 20021202 A 3460 CONNECTOR EMB 145 EMB145 3260210 SO FLT CONTROLLER LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37342 145367 CREW REPORTED SMOKE COMING FROM THE FLIGHT GUIDANCE CONTROLLER. MAINTENANCE SECURED THE CONNECTOR ON THE FLIGHT GUIDANC E CONTROLLER. FERRIED A/C TO CLT FOR REPLACEMENT OF THE FLIGHT GUIDANCE CONTROLLER. (M) 2 L 7 2 4F RT T00011AT 2003040300012 20030403 00012 EA 2003 4 3 2003F00195 1 20021118 A 7120 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 27185 7185 LT AND RT ENGINE SUPPORT BEAM LOWER WEBS FOUND TO BE CRACKED AND WILL BE REPAIRED IAW BOMBARDIER REO 601R-53-61-366. (M ) 2 L 7 2 4F RT A21EA 2003040300013 20030403 00013 EA 2003 4 3 2003F00196 1 20021118 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 27185 7185 DAMAGED PREVIOUS REPAIR ON FUSELAGE SKIN AT FS 310.00 STRINGER 16-17, LEFT SIDE. (M) 2 L 7 2 4F RT A21EA 2003040300014 20030403 00014 EA 2003 4 3 2003F00197 1 20021109 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17217 7217 AT PREFLIGHT, NR 2 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BULB. OPS NORMAL. (M) 2 L 7 2 4F RT A21EA 2003040300049 20030403 00049 EA 2003 4 3 ASOA02625 1 20021208 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA O OTHER O OTHER AP APPROACH 1 SO 11 842AS 7304 FLT 4766 - DURING APPROACH INTO AUS, THE FIRST OFFICER NOTICED WHAT APPEARED TO BE A SCRATCH OR CRACK IN THE UPPER CORNE R ON THE NR 3 WINDSHIELD. THE AIRCRAFT LANDED SAFELY IN AUS. MAINTENANCE DETERMINED THE NR 3 WINDSHIELD TO BE CRACKED, REMOVED AND REPLACED IT. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003040300057 20030403 00057 SO 2003 4 3 ASOA02645 1 20021226 A 5553 ANGLE EMB 120 EMB120ER 3260203 SO VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 502AS 120274 DURING HANGAR INSPECTION IN MCN, THE VERTICAL STABILIZER RIGHT ATTACH ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE REPAIRED THE RIGHT ATTACH ANGLE IAW ASA EO120-55-0009. (M) 2 L 7 2 4T RT A31SO 2003040300059 20030403 00059 SO 2003 4 3 ASOA02647 1 20021226 A 3000 44E221A SEPARATOR EMB 120 EMB120ER 3260203 SO DE ICE SYSTEM LEAKING A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 268AS 120202 FLT 4147 - DURNIG CLIMB-OUT FROM LYH-ATL, WHEN SELECTING BLEEDS TO OPEN, A RT DUCT LEAK INDICATION WAS RECEIVED. THE CR EW PERFORMED THE QRH PROCEDURES AND SHUT THE RT ENGINE DOWN. AFTER THREE MINUTES THE RT ENGINE WAS RESTARTED. THE RT D UCT LEAK LIGHT ILLUMINATED AGAIN AND SUBSEQUENTLY THE PILOT SECURED THE ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCR AFT RETURNED TO LYH, LANDING SAFELY. MAINTENANCE FOUND THE RT SIDE DE-ICE WATER SEPARATOR FILTER ASSEMBLY LOOSE AND TIG HTENED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2003040700031 20030407 00031 WP 2003 4 7 GTIA021392 1 20021226 A 5522 PANEL DOUG DC9 DC982 3022082 WP LT ELEVATOR LE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND LEFT L/E ELEVATOR PANEL HAS CORROSION ALL OVER. FORMED NEW PART. INSTALLED LEFT L/E ELEVATOR PANEL. (M) 2 L 7 2 4F A6WE 2003040700060 20030407 00060 SO 2003 4 7 SIMA200236302 1 20021220 A 5310 14522460013 BEAM EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 700LE 145156 ABI - DURING AN IMBV INSPECTION, THE GALLEY CENTER BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. PERFORMED TWO CUT O T OF DAMAGED AREAS. BOTH CUTOUT AREAS FALL WITHIN THE TOTAL LENGTH OF CUTOUT ALLOWED. FABRICATED A U-SHAPE EXTERNAL DO UBLER. REPAIR DONE IAW EMB 135 SRM (145/1142 REV 20) 53-21-10 PARA 5 FIG 204 SHEET 2. (M) 2 L 7 2 4F RT T00011AT 2003040700062 20030407 00062 SO 2003 4 7 SIMA200300604 1 20021228 A 5320 14525480003 SILL EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 700LE 145156 ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED DAMAGED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM (SRM 145/1142 REV 20) CHAPTER 51-40-02, 51-20-03, AND EMB 145 CPM 51-21-04 THROUGH 51-21-06. (M) 2 L 7 2 4F RT T00011AT 2003040700063 20030407 00063 SO 2003 4 7 SIMA200300605 1 20021227 A 5315 14521721009 FLOORBEAM EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 700LE 145156 ABI - DURING AN IMBV INSPECTION, THE CENTER SECTION OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED 15.5 INCHES BY 21.25 INCH SECTION OF THE FORWARD DIGITAL BY CUTOUT. FABRICATED A REPAIR DOUBLER FOR FLA NGE TO BE INSTALLED IN CONJUNCTION WITH DIGITAL REPAIR. FABRICATED A REPLACEMENT FORWARD DIGITAL CENTER SECTION, DOUBLE RS AND SHIMS. REPAIR DONE IAW EMB145 (SRM 145/1142, REV 20) 53-21-10 PARA 4 FIG 203, EMB GST-3718/02 AND STANDARD SRM P RACTICES. (M) 2 L 7 2 4F RT T00011AT 2003040700066 20030407 00066 SO 2003 4 7 SIMA200300812 1 20021218 A 5315 14521721007 FLOORBEAM EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 700LE 145156 ABI - THIS IS A LEVEL 2 FINDING DURING AN IMBV INSPECTION, GALLEY AREA AFT DIGITAL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE DIGITAL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2003040700069 20030407 00069 SO 2003 4 7 SIMA200300815 1 20021218 A 5320 14521725615 SILL EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 700LE 145156 ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION SERVICE DOOR AFT SILL HAS CORROSION. REMOVED AND INSTAL LED SERVICEABLE SILL IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2003040700070 20030407 00070 SO 2003 4 7 SIMA200300816 1 20021218 A 5310 145425381003 BEAM EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 700LE 145156 ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION, LEFT OMEGA BEAM DOUBLER BETWEEN FRAME 65 AND 68 CORRODE D. REMOVED AND INSTALLED SERVICEABLE BEAM IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2003040200004 20030402 00004 EA 2003 4 2 2003F00177 1 20020907 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37228 7228 IN SLC, IT WAS DISCOVERED THAT THE LEFT EMERGENCY EXIT ILGHT WAS INOPERATIVE. MAINTENANCE RECONNECTED THE WIRES TO THE LIGHT MODULE. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2003040300003 20030403 00003 NM 2003 4 3 2003F00186 1 20021105 A 2611 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM SMOKE DETECT ILLUMINATED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 444YV 444 DURING FLIGHT, THE SMOKE WARNING LIGHT ILLUMINATED FOR 5 SECONDS. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE SMOKE WARNING SYSTEM AND COULD NOT DUPLICATE THE PROBLEM. THE A/C CONTINUED WITHOUT INCIDENT. (M) 2 H 7 2 4T RT A13NM 2003040300021 20030403 00021 SO 2003 4 3 2003F00204 1 20021103 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145359 EMERGENCY EXIT IGHT BELOW COCKPIT DOOR INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND CONNECTOR LOOSE. RESECURED, OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2003040300051 20030403 00051 SO 2003 4 3 ASOA02639 1 20021224 A 5310 WINDOW POST EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 266AS 120188 DURING A HANGAR INSPECTION IN TXK, THE FIRST OFFICERS WINDOW POST SKIN WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED TH E CRACKED SKIN IAW ASA EO 120-53-1119A. (M) 2 L 7 2 4T RT A31SO 2003040400086 20030404 00086 NM 2003 4 4 ASAA0210353 1 20021204 A 5410 657377391 CHANNEL BOEING 737 7372Q8C 138448S NM NR 1 NACELLE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL SKIN AT NACELLE STATION 204.25 CRACKED .5 INCH. REMOVED DAMAGED SKIN SECTION AND REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2003040400091 20030404 00091 NM 2003 4 4 ASAA0210358 1 20021204 A 5414 657377391 SKIN BOEING 737 7372Q8C 138448S NM NR 1 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL SKIN AT NACELLE STATION 165.25 GOUGED. REMOVED DAMAGED SKIN AND REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2003040400093 20030404 00093 NM 2003 4 4 ASAA0210360 1 20021204 A 5411 6573771 RIB BOEING 737 7372Q8C 138448S NM NR 1 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND RN 1 ENGINE COWL RIB AT NACELLE STATION 199 GOUGED. REMOVED DAMAGED AREA AND REPA IRED PER SRM. (M) 2 L 7 2 4F A16WE 2003040400094 20030404 00094 NM 2003 4 4 ASAA0210361 1 20021204 A 5315 65505688 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM WEB AT BS 986-1016, RIGHT BUTTOCK LINE 40 RIGHT BUTTOCK LINE 45 CORRODED . REMOVED AND REPLACED FLOORWEB PER SRM. (M) 2 L 7 2 4F A16WE 2003040400097 20030404 00097 NM 2003 4 4 ASAA0210364 1 20021205 A 5730 6546419183 SKIN BOEING 737 7372Q8C 138448S NM LT WING LE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND LEFT WING LEADING EDGE AT WING STAITON 236-369 CRACKED .75 INCH AND CHAFED. REPAI RED LEADING EDGE PER SRM. (M) 2 L 7 2 4F A16WE 2003040400099 20030404 00099 NM 2003 4 4 ASAA0210366 1 20021205 A 5410 6552263275 CHANNEL BOEING 737 7372Q8C 138448S NM NR 1 NACELLE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL CHANNEL AT NACELLE STATION 199.25 CHAFED. REMOVED AND REPLACED DA MGAED CHANNEL PER SRM. (M) 2 L 7 2 4F A16WE 2003040400100 20030404 00100 NM 2003 4 4 ASAA0210367 1 20021205 A 5410 65522631 GUSSET BOEING 737 7372Q8C 138448S NM NR 1 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL GUSSET AT NACELLE STATION 218.67 GOUGED. REMOVED AND REPLACED DAM AGED GUSSET PER SRM. (M) 2 L 7 2 4F A16WE 2003040400128 20030404 00128 WP 2003 4 4 GTIA021389 1 20021226 A 5310 FRAME DOUG DC9 DC982 3022082 WP BULKHEAD DOOR BULGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND AFT PRESSURE BULKHEAD VAULT DOOR JAMB LOWER FRAME HAS CORROSION BULGE RBL 9 INCHES AT FLOOR LINE. FORMED NE W REPAIR AT LOWER JAMB. INSTALLED NEW REPAIR, FILLER AND DOUBLER. (M) 2 L 7 2 4F A6WE 2003040700033 20030407 00033 WP 2003 4 7 GTIA021395 1 20021231 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND L1 DOOR 2ND FRAME LOWER FRAME AFT RADIUS CRACKED. STOP DRILLED END OF BEAM. (M) 2 L 7 2 4F A6WE 2003040700055 20030407 00055 SO 2003 4 7 SIMA200234302 1 20021206 A 3310 29M426 RHEOSTAT EMB 135 EMB135KL 3260302 SO CABIN INOPERATIVE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 810AE 145525 SYR - FLT 4291 - SYR - DURING DESCENT, CREW REPORTED THE OVERHEAD LIGHTS FLICKERING ON AND OFF WITH A ELECTRICAL ODOR. MAINTENANCE REPLACED THE OVERHEAD LIGHT RHEOSTAT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCAFT WAS RETURNED TO SER VICE. (M) 2 L 7 2 4F RT T00011AT 2003040700057 20030407 00057 EU 2003 4 7 SIMA200234504 1 20021205 A 5347 7253799387 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 375AE 340B375 ABI - DUIRNG A MBV INSPECTION OF AIRCRAFT, THE CABIN SEAT TRACK 18.3L AT THE FORWARD END WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED A 32 SECTION OF CORRODED SEAT TRACK. REPLACED SECTION IWA SAAB 340 SRM (72LKS 3079, REV 40) 53-70 -60 PARA 2 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2003040700058 20030407 00058 EU 2003 4 7 SIMA200234505 1 20021205 A 5311 7271899025 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 375AE 340B375 ABI - DURING A MBV INSPECTION, THE RIGHT FUSELAGE FRAME AT STATION 658.5 WAS FOUND TO BE DENTED. RECONTOURED DENT AND P ERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS FOUND. FABRICATED A REPAIR DOUBLER AND INSTALLED IAW SAAB 340 REPAIR S TATEMENT 340SDS004764 PARA 1. (M) 2 L 7 2 4T RT A52EU 2003040700101 20030407 00101 NM 2003 4 7 UIEA200200063 1 20021115 A 2780 1267629 PDU BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL NR 1 LE FLAP FAILED A UIEA J A DUMP FUEL UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 15 491MC 29252 AIR TURNBACK, AFTER TAKEOFF DURING CLIMB, LEFT OUTBOARD GROUP FAILED TO RETRACT. STATUS MESSAGE 'FLAPS PRIM TO LE FLAP DRIVE'. AFTER CYCLING FLAPS BOTH OUTBOARD GROUPS FAILED. AIRCRAFT RETURNED TO ANC. FUEL DUMPED 83,000 KGS. REMOVED AN D REPLACED LEFT NR 1 LEADING EDGE PDU IAW MM 27-81-03. ADJUSTED TORQUE TUBES, CHECKED SEQUENCE OF FLAPS. ALL OPS OK. GROUND OPS NORMAL. (M) 2 L 7 4 4F 4 F RT 1384945 E23EA 2003040800022 20030408 00022 EA 2003 4 8 SIMA200300101 1 20021229 A 2820 CC670621041 LINE CNDAIR CL600 CL6002C10 1390015 EA CTR FUEL TANK CRACKED A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 502AE 10018 SGF - FLT 3802 - DURING CRUISE FLIGHT, CREW RECEIVED SEVERAL FUEL IMBALANCE MESSAGES THAT THEY WERE ABLE TO CORRECT. RE PORTED THE CENTER WING TANK FILLING RAPIDLY. NO EMERGENCY WAS DECLARED. AIRCRAFT WAS LANDED WITH 4800 LBS IN THE CENTE R TANK WITH FUEL VENTING FROM THE OVERFILL VENTS. MAINTENANCE FOUND A HOLE IN THE ENGINE FEED LINE IN THE CENTER WING T ANK. LINE WAS REPLACED AND AIRCRAFT WAS FERRIED TO DFW FOR FURTHER INSPECTION OF THE CENTER TANK. NO OTHER CRACKS WERE FOUND AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2003041000080 20030410 00080 WP 2003 4 10 MEX2002358 1 20020912 A 3110 INDICATOR DOUG DC9 DC987 3022087 WP RAM AIR TURBINE OVERHEATED A ASMF D RETURN TO BLOCK B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING TX TAXI/GRND HDL 1 SW 23 755RA 49727 FLT 934 - MEX-SAT - AIRCRAFT RETURNED TO PLATFORM DUE RAT AND EPR LIMIT OUR OF SERVICE INDICATIONS. DURING CHECK IT WAS DETECTED THAT THE RAT INDICATOR OVERHEATED. THE R2-5 RAT INDICATOR WAS REPLACED IAW MM 34-10-0, TESTS CORRECT. (M) 2 L 7 2 4F RT A6WE 2003041000083 20030410 00083 WP 2003 4 10 MEX2002359 1 20021112 A 2150 45D16 PRESSURE SWITCH DOUG DC9 DC982 3022082 WP AC PACK FAILED A ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 505MD 49149 FLT 210 - MEX-CUU - AIRCRAFT ABORTED TAKEOFF DUE TO BOTH AIR CONDITIONING PACKAGES SHUTOFF AND FLOW LIGHT TURN ON AT 132 KTS. AIRCRAFT WAS SENT TO THE HANGAR AND BOTH PACKAGES WERE TESTED AT TAKEOFF POWER (2.02), ALL CORRECT. SECOND SEGMEN T SWITCHES WERE CHECKED DETECTING THE S1-297 AND S1-296 DAMAGED, REPLACED IAW MM 21-31-09. ADDITIONALLY RIGHT FLOW VALV E AND PRESSURE REGULATOR VALVE WERE REPLACED IAW MM 21-31-02 AND 31-31-01, TESTS WERE PERFORMED IAW MM 23-31-09, ALL COR RECT. (M) 2 L 7 2 4F A6WE 2003041000110 20030410 00110 SO 2003 4 10 SIMA200235106 1 20021213 A 5330 AL7075T6511 SKIN EMB 145 EMB145LR 3260212 SO WINDSHIELD FRAME CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AE 145158 ABI - DURING AN IMBV INSPECTION, THE THIRD SCREW HOLE ON THE RIGHT WINDSHIELD FRAME WAS FOUND TO BE CORRODED BELOW LIMIT S. REAMED FASTENER HOLE OT .313 INCH AND PERFORMED AN NDT INSPECTION WITH NO DEFECTS FOUND. FABRICATED A REPAIR BUSHIN G. REPAIR DONE IAW EMB REPAIR STATEMENT GAST-3637/02 AND GST-1587/02B. (M) 2 L 7 2 4T RT T00011AT 2003041000114 20030410 00114 SO 2003 4 10 SIMA200236304 1 20021219 A 5330 2024T3 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AE 145158 ABI - DURING AN IMBV INSPECTION, A GOUGE WAS FOUND ON REAR FUSELAGE 1 BETWEEN FRAMES 65 AND 66 AND STRINGERS 20L AND 21L . REMOVED DAMAGE BY MAKING A 2.25 INCH BY 3.12 INCH CUTOUT. FABRICATED A REPAIR FILLER. REPAIR DONE IAW EMB 145 SRM ( 145/1142 REV 20) 53-31-01 PARA 2 FIG 201, AND GST 3655/02. (M) 2 L 7 2 4T RT T00011AT 2003041000117 20030410 00117 SO 2003 4 10 SIMA200300805 1 20021214 A 5320 14520609005 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AE 145158 ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION, RIGHT SILL CORRODED BETWEEN FRAMES 23-27, 32-36, 40, 4 6-47, 50 AND 53-54. REMOVED RIGHT SILL AND INSTLALED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02, 51-20,03 AND 51-40-06. (M) 2 L 7 2 4T RT T00011AT 2003041000118 20030410 00118 SO 2003 4 10 SIMA200300806 1 20021210 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AE 145158 ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTIONS, AFT SERVICE DOOR SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT SILL IAW EMB 145 SRM 51-40-02, 51-20-03. (M) 2 L 7 2 4T RT T00011AT 2003041000119 20030410 00119 SO 2003 4 10 SIMA200300807 1 20021020 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AE 145158 ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION, SERVICE DOOR FORWARD SILL CORRODED. REMOVED AND INSTA LLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003081300103 20030813 00103 EA 2003 8 13 SWIA200212107 1 20020612 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 920SW 7660 FOUND ON PREFLIGHT INSPECTION SECOND EMERGENCY LIGHT AFT OF FORWARD DOOR (LEFT SIDE) BURNED OUT. RE-LAMPED SECOND EMERG ENCY LIGHT ON LEFT OVERWING WITH SERVICEABLE BULB. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 2003040400084 20030404 00084 NM 2003 4 4 ASAA0210350 1 20021204 A 5512 6547529505 SKIN BOEING 737 7372Q8C 138448S NM HORIZONTAL STAB CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND LEFT HORIZONTAL STABILIZER AT ELEVATOR STATION 149.12 CHAFED. REMOVED DAMAGED HOR IZONTAL STABILIZER WEB AND REPAIRED RIB PER EA. (M) 2 L 7 2 4F A16WE 2003040400092 20030404 00092 NM 2003 4 4 ASAA0210359 1 20021204 A 5414 657377482 SKIN BOEING 737 7372Q8C 138448S NM NR 1 NACELLE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL RIB AT NACELLE STATION 207.67 GOUGED. REMOVED DAMAGED AREA AND R EPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2003040400114 20030404 00114 NM 2003 4 4 ASAA0210384 1 20021209 A 5411 65522637 LONGERON BOEING 737 7372Q8C 138448S NM NR 2 NACELLE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURNG SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL LONGERON AT NACELLE STATION 154-184, CORRODED. REMOVED AND REPLACE D NR 2 ENGINE COWL LONGERON PER SRM. (M) 2 L 7 2 4F A16WE 2003041000189 20030410 00189 SO 2003 4 10 FXG2003F00000 1 20021231 A 3210 2057011172 DOWNLOCK CURTIS C46 C46* 2622701 SO MLG INOPERATIVE A FXGA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 01 54514 33285 ON TOUCHDOWN AND ROLL OUT, RT GEAR DOWNLOCK DID NOT ENGAGE AS A/C SLOWED DOWN, GEAR RETRACTED SLOWLY. NR 2 ENG AND PROP SUFFERED A PROP STRIKE AND SUDDEN STOPPAGE. RT WING TIP DRUG ON GROUND, DURING THIS, DEICE BOOT, APPROX 4 FT. OF LOWER SKIN AND THE AILERON WERE DAMAGED. AFTER INSP, REPLACEMENT OF ENG, PROP, AILERON AND WING TIP, REPAIR OF LWR WING SKIN . A/C WAS RELEASED TO SERVICE. 2 L 7 2 4R A772 2003041000239 20030410 00239 NM 2003 4 10 DL76L030069 1 20021217 A 5754 114T411541 WEDGE BOEING 767 767332 1382001 NM L/E SLAT DEBONDED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 178DN 25143 LEFT WING NR 5 SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 418116-14. 2 L 7 2 4F RT A1NM 2003041400039 20030414 00039 EU 2003 4 14 CA030312012 1 20021112 A 7930 IPT20RTPE1000200 TRANSMITTER PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL OIL PRESSURE CORRODED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) IN CLIMB, THE OIL PRESSURE GRADUALLY DESCENDED. THE PILOT PERFORMED A PRECAUTIONARY LANDING. THE OIL SYSTEM WAS IN SPECTED TO ENSURE THAT THE OIL FILTER WAS NOT BLOCKED. WHEN ATTEMPTING TO RESTART THE ENGINE, CODE 50 ILLUMINATED ON TH E (EIS) PANEL INDICATING A PROBLEM WITH THE OIL PRESSURE TRANSMITTER. THE TRANSMITTER WAS REPLACED AND THE SYSTEM WAS SE RVICEABLE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2003041400056 20030414 00056 EU 2003 4 14 XG3R085945 1 20020410 A 6320 FITTING UROCOP EC130 EC130B4 EU TMECA ARRIEL ARRIEL2B NE OIL COOLER LEAKING W XG3R O OTHER K FLUID LOSS NR NOT REPORTED 1 FS 01 26LB 683 6522 3514 23017 RETURN FITTING LEAKING. BEVEL ON FITTING HAS INCREASED RADIUS. REPLACED OIL COOLER. 1 G 7 2 3U 3 U H9EU E00054EN 2003040700029 20030407 00029 WP 2003 4 7 GTIA021390 1 20021223 A 5280 DOUBLER DOUG DC9 DC982 3022082 WP MLG DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND RIGHT MLG WING DOOR FORWARD LOWER DOUBLER IS CRACKED. REMOVED REPAIR DOUBLER. FABRICATED NEW DOUBLER. INS TALLED NEW DOUBLER. (M) 2 L 7 2 4F A6WE 2003040700056 20030407 00056 EU 2003 4 7 SIMA200234503 1 20021205 A 5347 7253799387 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 375AE 340B375 ABI - DURING A MBV INSPECTION, THE CABIN SEAT TRACK BL 0 AT THE FORWARD END WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED A 32 SECTION OF CORRODED SEAT TRACK. INSTALLED REPLACEMENT SECTION IAW SAAB 340 SRM (72LKS 3079 REV 40) 543-70 -60 PARA 2 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2003040700065 20030407 00065 SO 2003 4 7 SIMA200300811 1 20021228 A 5315 14522460013 FLOORBEAM EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 700LE 145156 ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, GALLEY AREA CENTER BEAM HAS CORROSION AT FRAME 20. REMO VED AND INSTALLED SERVICEABLE BEAM IAW EMB 135 SRM 53-21-40. (M) 2 L 7 2 4F RT T00011AT 2003040700067 20030407 00067 SO 2003 4 7 SIMA200300813 1 20021228 A 5310 14522459003 SUPPORT EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 700LE 145156 ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION GALLEY AREA RAMP SUPPORT HAS CORROSION. REMOVED AND INS TALLED SERVICEABLE SUPPORT IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2003040700103 20030407 00103 NM 2003 4 7 UIEA200200066 1 20021207 A 3610 77385619 DUCT BOEING 747 747230B 1384889 NM NR 1 ENGINE RUPTURED A UIEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 EA 15 508MC 21644 JFK-ORD - AIR TURNBACK, AT 10,000 FEET WITH CRUISE POWER, LOUD BANG AND BUMP. NR 1 ENGINE EGT CLIMBED TO 850 DEGREES AN D NACELLE TEMPS TO 4.5 BLEED VALVE CLOSED. EGT CONTINUED ABOUT 100 DEGREES ABOVE OTHER ENGINES. SAW T/R BLOW-OUT PANEL OPEN. RETURNED TO JFK. NO FUEL DUMPED. FOUND INTERMEDIATE CHECK VALVE, Y-DUCT AND ELBOW FAILED. REPLACED CHECK VALVE PER MM 36-11-02. REPLACED DUCT ASSEMBLY P/N 65B94819-2 PER MM 36-11-01. LEAK CHECK OK. REPLACED MANIFOLD P/N 1756M94 603 PER MM 36-11-00. REPLACED TUBE ASSEMBLY 9057M85G02 PER MM 36-11-00. OPS AND LEAK CHECK OK. (M) 2 L 7 4 4F A20WE 2003041000109 20030410 00109 NM 2003 4 10 MEX2002360 1 20021212 A 4960 947F9453 CONTROL UNIT DOUG MD88 MD88 3023688 NM APU FAILED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 168PL 53174 FLT 589 - MEX-CUN - AIRCRAFT RETURNED TO PLATFORM, AFTER ENGINES STARTING RIGHT GENERATORS DID NOT TAKE POWER. DURING C HECK WAS DETECTED THAT THE APU LEFT BAR BLUE LIGHT DID NOT TURN ON. DURING GENERATION TESTS, DETECTED THAT THE APU LEFT BAR WAS NOT WORKING, BUT IT PERMITTED THAT GPU AND ENGINES ENERGIZE THE BAR. GCU AND BCU WERE REPLACED BUT FAIL CONTIN UED. AIRCRAFT WAS DISPATCHED WITH APU OUT OF SERVICE IAW MEL 49-1. (M) 2 L 7 2 4F RT A6WE 2003041000174 20030410 00174 SW 2003 4 10 EGR2003F00004 1 20021227 A 2842 22236684103 PROBE BELL 430 430 1182150 SW LT FUEL CELL FAILED E EGRA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 17 993PA 1704 49050 NR 1 FUEL QUANITY LOW LIGHT ILLUMINATED DURING FLIGHT. INTERNAL PROBE FAILURE. LOW QTY LIGHT ILLUMINATED STILL CORRECT AMOUNT OF FUEL. REPLACED FUEL PROBE, CALIBRATED FUEL SYSTEM OPERATIONAL CHECK, OK. AIRCRAFT RETURNED TO SERVICE. 1 G 7 2 3U RT H9SW 2003041000238 20030410 00238 NM 2003 4 10 DL76L030068 1 20021217 A 5754 114T411542 WEDGE BOEING 767 767332 1382001 NM L/E SLAT DEBONDED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 178DN 25143 RIGHT WING NR 8 SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 418117-14. 2 L 7 2 4F RT A1NM 2003041400090 20030414 00090 SO 2003 4 14 CA030225005 2 20021013 A 8520 CRANKSHAFT CESSNA 206 U206E 2073350 CE CONT O520 IO520F 17032 SO MCAULY D3A34 D3A34C401 GL ENGINE DISCONNECTED W E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 CA (CAN) NR 6 CONNECTING ROD CRANKSHAFT END BECAME DISCONNECTED AND SMASHED THROUGH ENGINE CASE. BOLTS EITHER WRE NOT TORQU ED CORRECTLY OR CLAMPSHELL BOLT FAILURE. 1 H 7 1 3O 3 O A4CE E5CE 5 C P47GL 2003041500022 20030415 00022 EU 2003 4 15 CA030317005 1 20020108 A 6420 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR UNSERVICEABLE W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 CA (CAN) NOTED TAIL ROTOR VIBRATION AND COULD NOT STROBE IT OUT. (1.2 IPS) CHECKED THE HALF SHELL BEARINGS AND NOTICED THAT 2 BEARINGS WERE TORN AND THE OTHER 2 WERE WORN. TAIL ROTOR ASSY REMOVED AND ALL FOUR BEARINGS CHANGED OUT, NEW BEARINGS INSTALLED P/N 355A09-1036-01. ALSO CHANGED OUT THE TEETERING BEARINGS P/N 350A33-2153-00. TAILROTOR SPAR INSPECTION CAR RIED OUT AND NO DEFECTS FOUND. UNIT REINSTALLED AND BALANCED TO BELOW .1 IPS. 1 G 7 1 3U 3 U NC H9EU E19EU 2003041500034 20030415 00034 SO 2003 4 15 CA030318012 1 20021120 A 3222 110P241021 STRUT EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA NLG BROKEN W D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA (CAN) SHIMMY FROM NOSE GEAR WHEN TAXIING. AFTER DISASSEMBLING THE NLG OLEO STRUT ASSEMBLY, IT HAD BEEN FOUND BROKEN. (T HE THREADED SECTION AT THE TOP WHERE NUT P/N 15134 SCREW ON.)CORRECTION: REPLACING NOSE GEAR ASSEMBLY FIXED THE PROBLEM. NO CAUSE HAVE BEEN FOUND FOR THE FAILURE YET. 1 L 7 2 4T 4 T A21SO E4EA 2003040700102 20030407 00102 GL 2003 4 7 UIEA200200065 2 20021202 A 7230 COMPRESSOR WHEEL BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL HP SECTION FAILED A UIEA C E D ABORTED TAKEOFF ENGINE SHUTDOWN RETURN TO BLOCK E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 EA 15 412MC 30559 706123 REJECTED TAKEOFF, LOUD BANG HEARD AT 75 KNOTS ON TAKEOFF ROLL. REJECTED TAKEOFF AND RETURNED UNDER TOW. MAX THRUST WAS SET. AIRCRAFT POSITIONED TO HIGH POWER RUN BAY. ENGINE RUN RESULTS FAILED. NR 2 ENGINE BORESCOPE INSPECTION FOUND HP C STAGE 12 AND 13 FAILED. ENGINE CHANGE REQUIRED. NR 2 ENGINE REPLACED IAW MM 71-00-02. SUBSEQUENT LEAK AND OPS CHECK OK IAW MM 71-00-00. (M) 2 L 7 4 4F 4 F RT 1384945 E23EA 2003041000112 20030410 00112 SO 2003 4 10 SIMA200235702 1 20021220 A 2560 P2070009120 FLASHLIGHT EMB 145 EMB145LR 3260212 SO FWD CABIN INOPERATIVE A SIMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 21 617AE 145093 ORD - FLT 4061 - CREW REPORTED A STRONG ODOR IN CABIN SIMILAR TO ELECTRICAL BURNING SMELL IN FORWARD CABIN NEAR THE FLIG HT ATTENDANT JUMPSEAT. MAINTENANCE FOUND THE FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY OVERHEATED AND MELTED. ALSO, NOTED W IRING HARNESS DAMAGE TO INSULATION. MAINTENANCE REPLACED FLASHLIGHT ASSEMBLY AND REPAIRED DAMAGED WIRES. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2003041000113 20030410 00113 SO 2003 4 10 SIMA200236303 1 20021220 A 5310 14522461011 BEAM EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 652AE 145432 ABI - DURING A MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORR OSION BY PERFORMING A CUTOUT OF THE DAMAGED AREA. FABRICATED A DOUBLER FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SR M (145/1142 REV 20) 53-21-10 PARA 2 FIG 201 SHEET 2 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2003041000120 20030410 00120 SO 2003 4 10 SIMA200300808 1 20021214 A 5310 14522459001 BEAM EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AE 145158 ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION, CENTER BEAM RAMP FOUND CORRODED. REMOVED AND INSTALLE D SERVICEABLE RAMP IAW EMB 145 SRM 51-40-02, 51-20-03. (M) 2 L 7 2 4T RT T00011AT 2003041000121 20030410 00121 SO 2003 4 10 SIMA200300809 1 20021210 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AE 145158 ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION, LEFT FLOOR SILL BETWEEN FRAMES 19 TO 23 CORRODED. REMO VED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003041100019 20030411 00019 NE 2003 4 11 RJ19 2 20021018 A 7200 FAN BLADE PWA JT15D5 BEECH MU300 400BEECH CE PWA JT15 JT15D4 52112 NE #2 ENGINE FOD E ERYA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 CE 07 598JL 5477 136 RJ19 PCE100077 DURING THE T/O ROLL AT APPROXIMATELY 30 KTS, A FUELING PAD (PAD USED BY THE FUELER TO PROTECT THE PAINT DURING FUELING) WAS INGESTED INTO THE NR 2 ENGINE. THE T/O WAS ABORTED AND ENGINE SHUT DOWN AFTER RETURNING TO FBO.LA - TEST 2 H 7 2 4F 4 F RT A16SW E1NE 2003041500106 20030415 00106 NM 2003 4 15 XNOA01094 1 20021213 A 2611 WARNING LIGHT BOEING 727 727227 1384078 NM CARGO FIRE ILLUMINATED A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 79754 21363 LOWER AFT CARGO FIRE WARNING AFTER TAKEOFF. TRANSFERRED TO DMI 2844 IAW ENA 727 MEL 26-19 CAT-C PLACARDS INSTALLED. 2 L 7 3 4F A3WE 2003041500107 20030415 00107 EU 2003 4 15 YENA200233 1 20021212 A 2611 WARNING LIGHT AIRBUS 320 A320232 3930326 EU ECAM FALSE ACTIVATION A YENA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 15 554JB 1898 AVIONICS SMOKE ECAM IN FLIGHT AT FL240. NO VISIBLE SMOKE. NO OVERWEIGHT LANDING PERFORMED WT13T000. FLIGHT 70 PBI-JFK DIVERTED TO FLL. PERFORMED BITE TEST OF AVEC AS PER AMM 21-26-00-710-001, PERFORMED BITE TEST OF SDCU AS PER AM 25-15- 00-710-001. ALL OPS TEST OK. 2 L 7 2 4F RT A28NM 2003041000111 20030410 00111 SO 2003 4 10 SIMA200235107 1 20021213 A 5310 14522460013 BEAM EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AE 145158 ABI - DUIRNG AN IMBV INSPECTION, THE GALLEY FLOOR CENTER BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS AT FRAME 23. BL ENDED THE CORRODED AREA AND PERFORMED NDT INSPECTION APPLIED ALODINE AND EPOXY PRIMER TO THE BLENDED AREA. FILLED THE B LENDED AREA WITH EPOXY RESIN. FABRICATED A REINFORCEMENT DOUBLEF FOR REPAIR. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145/ 1142 REV 20) CHAPTER 53-21-10 FIGURE 207. (M) 2 L 7 2 4T RT T00011AT 2003041000122 20030410 00122 SO 2003 4 10 SIMA200300810 1 20021210 A 5320 14529150001 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AE 145158 ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION, LEFT PROFILE AT FRAME 23 CORRODED. REMOVED AND INSTALL ED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003041500082 20030415 00082 NE 2003 4 15 CA030329001 2 20021116 A 7260 5018T49P01 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ACCESSORY G/B LEAKING W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) 15 MINUTES INTO THE FLT, THE RT ENGINE OIL PRESSURE BEGAN TO FLUCTUATE BETWEEN 25 & 33 PSI FOR FIVE MINUTES (STABL E OIL TEMPERATURE WAS NOTED). THE OIL PRESSURE SLOWLY BEGAN TO DECREASE BELOW 25 PSI, WHEREBY THE FLIGHT CREW INITIATED AN IN-FLIGHT SHUT DOWN. MAINTENANCE ATTRIBUTED THE OIL PRESSURE FLUCTUATION TO HYD EDP CARBON SEAL MOUNTED ON THE ACCES SORY GEAR BOX. THE AIRCRAFT RETURNEDTO SERVICE FOLLOWING THE SEAL REPLACEMENT. 2 L 7 2 4F 4 F RT A21EA E15NE 2003041500105 20030415 00105 EU 2003 4 15 U30A200200034 1 20021209 A 5210 GUST LOCK AIRBUS 320 A320214 3930316 EU PAX DOOR FAILED A U30A K NONE O OTHER IN INSP/MAINT 1 EA 17 262AV 1725 IN EWR AFTER FLT 257, LEFT FORWARD PAX/CREW ENTRANCE DOOR (L1) GUST LOCK FAILED TO ENGAGE. UPON FURTHER INSPECTION, FOU ND DEBRIS IN DOOR GAS ROD BUSHING (WHICH CAUSED ROD TO BIND ON BUSHING). CLEARED DEBRIS AND FREED UP DOOR GAS ROD AND G UST LOCK MECHANISM OPERATED NORMALLY. OPERATIONALLY CHECKED THE OPENINING IAW AMM 52-10-00-010-001 AND THE CLOSING IAW AMM 52-10-00-410-001. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2003041500109 20030415 00109 NE 2003 4 15 UPS02639987 2 20021216 A 7320 CONNECTOR BOEING 767 76734AF 1385212 NM GE CF6 CF680 30025 NE RT ENGINE LEAKING A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 320UP 27747 INFLIGHT SHUTDOWN DUE TO FUEL IMBALANCE RT ENGINE SHUT DOWN PER CHECKLIST RETURNED TO LOUISVILLE FUEL LEAKING INTERNALLY IN HMU AND COMING OUT BOTTOM CHANNEL A AND CHANNEL B CANNON PLUG PLATE. REMOVED HMU UP TO STEP 6 IAW M/M REF 73-21-14- 4. INSTALLED HMU NR 2 PER MM 73-21-14-4. RAN ENGINE, ALL CHECKS NORMAL. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A1NM E13NE 2003041500110 20030415 00110 NE 2003 4 15 UPS02839989 2 20021217 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 3 FLAMED OUT A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION NR NOT REPORTED 1 SO 01 744UP 45944 NR 3 ENGINE FLAMED OUT IFSD AT 35000 FT N1 WINDMILLING AT 30 PERCENT N2 AT 15 PERCENT OIL PRESSURE = 1PSI, QUANTITY AND TEMP NORMAL TIME = 1235 TIME 1340 N1 = 14.5 PERCENT N2 = 0 OIL PRESSURE 0. PERFORMED T/S 71-00-00 PG 165-167, ADJUSTED GROUND AND FLIGHT IDLE IAW MM 73-20-01 PG 533. REF CFM MM 71-00-00 FAULT 51. PERFORMED ENGINE RUNS IAW 71-00-00, NO DE FECTS NOTED. 2 L 7 4 4F 4 F RT 4A25 E2GL 2003041500111 20030415 00111 SO 2003 4 15 SWIA200211583 1 20021217 A 7312 312007502 FUEL HEATER EMB 120 EMB120ER 3260203 SO RT ENGINE FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 297SW 120327 RECEIVED LOW OIL AURAL WARNING ON TAKEOFF ROLL, AS WELL AS OIL PRESS NR 2 RED MAP LIGHT. ABORTED TAKEOFF. DUE TO HIGH OIL CONSUMPTION ON RT ENGINE, REPLACED RT ENGINE FUEL OIL HEATER ASSEMBLY AND INSPECT CENTRIFUGAL BREATHER SHAFT WHERE C ARBON SEAL RIDES FOR SCORING.  ADDED TWO QUARTS OF OIL. REMOVED AND REPLACED RIGHT ENGINE FUEL OIL HEATER IAW 73-12-00 EMB 120 MM. LEAK CHECK GOOD. NO LEAKS NOTED. PN: 3120075-02 SN OFF: WA14980 SN ON: WA16483. 2 L 7 2 4T RT A31SO 2003041500112 20030415 00112 SO 2003 4 15 SWIA200211584 1 20021216 A 3297 WIRE HARNESS EMB 120 EMB120ER 3260203 SO RT MLG MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 187SW 120037 ON TAKEOFF FROM PSP, THE RT GEAR GREEN SYS A LIGHT REMAINED ON. UPON PUTTING GEAR DOWN AT LAX, THE GEAR DID NOT COME DO WN. PERFORMED ELECTRIC OVERRIDE QRH PROCEDURE AND THE GEAR CAME DOWN OK. REMOVED RIGHT A-HARNESS, REPAIRED AND REINST ALLED IAW 32-60-00. PERFORMED GEAR SWING A-GATE LIGHT FOR RIGHT GEAR, OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003041500114 20030415 00114 SO 2003 4 15 SWIA200211594 1 20021218 A 2133 OUTFLOW VALVE EMB 120 EMB120ER 3260203 SO CABIN PRESSURE MALFUNCTIONED A SWIA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 292UX 120292 PRESSURIZATION WAS WORKING IN MANUAL MODE AT FL230. AUTOMATIC MODE WAS DEFERRED. DURING CRUISE THE CABIN CLIMBED INSTA NTLY TOWARD CRUISE ALTITUDE AND WAS THERE WITHIN 10 SECONDS. THE MASKS DROPPED. INITIATED EMERGENCY DESCENT AFTER ATC CLEARANCE 5 MINUTES LATER. INSTALLED PNEUMATIC OUTFLOW VALVE IAW 21-30-00. INSTALLED ELECTRO-PNEUMATIC VALVE IAW 21-30 -00. PRESSURIZED AIRCRAFT, ALL CHECKS OK AT THIS TIME. 2 L 7 2 4T RT A31SO 2003041500115 20030415 00115 SO 2003 4 15 SWIA200211595 1 20021215 A 5270 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PAX DOOR FALSE ACTIVATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 292UX 120292 FORWARD DOOR WARNING ACTIVATED DURING TAKEOFF ROLL. ABORTED TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. FORWARD DOOR WA RNING CHECKS GOOD. 2 L 7 2 4T RT A31SO 2003041500119 20030415 00119 NE 2003 4 15 XNOA01096 2 20021221 A 7230 COMPRESSOR AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 2 ENGINE STALLED A XN0A A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 23 224KW 073 DURING DESCENT 12,000 FT NR 2 ENG BEGAN TO COMPRESSOR STALL. FUEL FLOW NORMAL. EGT ENG STABLE AT IDLE POSITION. INSPE CTED 2 ENG MAIN FUEL FILTER, NO DEFECTS NOTED. INSPECTED NR 2 ENG FUEL PUMP STRAINER, NORMAL. NO DEFECTS NOTED. INSPE CTED NR 2 ENG VSVS, NO DEFECTS. INSPECTED VBVS, NO DEFECTS NOTED. PERFORMED STALL INSPECTION IAW A300 MM 72-00-00 PG 6 28. REMOVED AND REPLACED NR 2 ENG IP CHECK VALVE. OPS CHECK NORMAL IAW A300 MM 71-00-00. 2 L 7 2 4F 4 F RT A35EU E23EA 2003041500123 20030415 00123 NE 2003 4 15 SWIA200211599 2 20021216 A 7261 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 2 LACK OF LUBE A SWIA C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 NM 07 297SW 120327 RECEIVED A LOW OIL AURAL WARNING ON TAKEOFF ROLL WITH OIL PRESS NR 2 RED MAP LIGHT. ABORTED TAKEOFF. OIL PRESSURE REMA INED IN THE NORMAL RANGE. ADDED TWO QUARTS OF OIL. RAN ENGINE. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2003041500125 20030415 00125 NE 2003 4 15 SWIA200211602 2 20021218 A 7397 WIRE HARNESS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE EEC MALFUNCTIONED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 07 298SW 120328 ON CLIMBOUT THE RT ENGINE TQ STARTED TO FLUCTUATE 5 PERCENT TO 20 PERCENT. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AND RETURNED TO THE FIELD. REPLACED RIGHT ENGINE EEC ELECTRICAL WIRING HARNESS IAW PW MM 22-01-10. ALL OPS CHECKS GOOD. P /N: 3115911-01 SN OFF: AR4013. 2 L 7 2 4T 4 T RT A31SO E20NE 2003041500127 20030415 00127 EA 2003 4 15 SWIA200211604 1 20021220 A 3020 300013000 VALVE CNDAIR CL600 CL6002B19 1900309 EA RT COWL ANTI-ICE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 925SW 7682 RT COWL ANTI-ICE MESSAGE WHEN SELECTED ON. RETURNED TO FAT. REMOVED AND REPLACED RIGHT COWL ANTI-ICE VALVE IAW CRJ MM 30-22-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2003041500131 20030415 00131 2003 4 15 SWIA200211608 4 20021221 A 2210 6229968001 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NR 1 MALFUNCTIONED A SWIA D RETURN TO BLOCK J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 403SW 5805 4966 7028 YAW DAMPER NR 1 INOP (STATUS MESSAGE), WOULD NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPER ACTUATOR IAW CRJ MM 22-22-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2003041500135 20030415 00135 EA 2003 4 15 SWIA200211612 1 20021126 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 FS 621.0 RT & LT FLOOR SUPPORT ANGLES CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED AREAS IAW CRJ REO 601 R-53-61-117 REV A. ANGLE P/N: 601R-53-61-117-2, REPAIR ANGLE P/N: 601R-53-61-117-4. 2 L 7 2 4F RT A21EA 2003041500137 20030415 00137 SO 2003 4 15 SWIA200211616 1 20021222 A 2750 12064207615 SELECTOR SWITCH EMB 120 EMB120ER 3260203 SO TE FLAPS INOPERATIVE A SWIA O OTHER N FALSE WARNING AP APPROACH 1 NM 07 270YV 1265 1265 120270 BELOW 500 FT ON APPROACH RECEIVED A -TOO LOW- FLAPS AURAL WARNING. REPLACED FLAP SELECTOR SWITCH, TEST OK. P/N: 120-64 207-615, S/N OFF: 296356-317, S/N ON: 120237. 2 L 7 2 4T RT A31SO 2003041500143 20030415 00143 SO 2003 4 15 SWIA200211623 1 20021225 A 2797 WIRE EMB 120 EMB120ER 3260203 SO LT ELEV TRIM CHAFED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 271YV 120271 AFTER TAKEOFF RECEIVED A TRIM FAIL AURAL WARNING AND THE TRIM FAIL LIGHT ON THE MAP CAME ON AND CONTINUED FOR APPROXIMAT ELY 5 MINUTES. RETURNED TO LAX. INSPECTED ELEVATOR TRIM WIRING ON TOP OF TAIL. FOUND CHAFED WIRE TO LEFT PROXIMITY SE NSOR AND CORRODED CONNECTOR TO RIGHT SENSOR. REPAIRED WIRE AND REPLACED CONNECTORS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003041500145 20030415 00145 SO 2003 4 15 SWIA200211626 1 20021217 A 2731 52991 ACTUATOR EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM FROZEN A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 NM 07 301YV 455 455 120301 TRIM ACTUATOR FROZE UP DURING CRUISE AT 22,000 FT. RETURNED TO SFO. REPLACED BOTH ELEVATOR TRIM TAB ACTUATORS IAW EMB 120 MM. OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2003041500149 20030415 00149 EA 2003 4 15 SWIA200211630 1 20021206 A 2740 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA CHANNEL 1 INOPERATIVE A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 906SW 7510 STAB CHANNEL 1 INOP WHILE STAB IS INTRANIT (HSTCU BITE CHECK INDICATES HSTCU CHANNEL 1 FAILURE). FOUND DURING C-CHECK I NSPECTION - INCOMING RUNS. REPLACED HSTCU IAW AMM TASKS 27-41-01-000-801 AND 27-41-01-400-801. TESTED HSTCU SYSTEM IAW CRJ AMM TASKS 27-40-00-710-801, TASK 27-40-00-720-801 AND TEST 27-41-00-740-801. TESTED SERVICEABLE. 2 L 7 2 4F RT A21EA 2003041500150 20030415 00150 EA 2003 4 15 SWIA200211631 1 20021206 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 906SW 7510 FS 280 RBL AND LBL 9.0 FLOORBEAMS INBOARD AND OUTBOARD ANGLES CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED ANGLE S IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13 AND 51-42-21. P/N: 601R31113-58. 2 L 7 2 4F RT A21EA 2003041500151 20030415 00151 EA 2003 4 15 SWIA200211632 1 20021206 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA INTERCOSTAL CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 906SW 7510 FS 625 STR 14 LT AND RT INTERCOSTAL ANGLES CRACKED. FOUND DURING C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40 -11, 51-42-06. P/N: 601-35012-51. 2 L 7 2 4F RT A21EA 2003041500152 20030415 00152 EA 2003 4 15 SWIA200211633 1 20021206 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 906SW 7510 FS 621 RIGHT FLOOR SUPPORT ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV 'A'. ANGLE P/N: 601R-53-61-004-2 REPAIR ANGLE P/N: 601R-53-61-004-6. 2 L 7 2 4F RT A21EA 2003041500154 20030415 00154 GL 2003 4 15 P5CA0200714 1 20021222 A 5610 60B100281 WINDSHIELD BOEING 747 747300 GL COCKPIT FAILED A P5CA O OTHER O OTHER DE DESCENT 1 WP 23 24837 24837 L1 WINDOW SHATTERED ON DESCENT. REPLACED WINDOW PER 56-11-02. 2 L 7 4 4F RT A20WE 2003041500155 20030415 00155 EU 2003 4 15 XNOA01098 1 20021229 A 2150 A/C PACK AIRBUS 300 A300B4203 3930306 EU NR 1 CONTAMINATED A XN0A O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 371PC 157 ACRID FUMES EMANATING FROM AIR CONDITIONING SYSTEM WITH NR 1 PACK IN USE WITH EITHER APU OR ENGINE BLEED. INSPECTED AND FOUND RESIDUAL HYDRAULIC FLUID CONTAMINATION IN NR 1 PAC SYS. A FUNCTION OF HYD SYS OIL SERVICING. CLEANED HYD FLUID AND OPERATED NR 1 PAC FOR 3 HRS WITH NO RECURRENCE OF FUMES. NR 1 PAC OPS CHECK GOOD IAW A300 MM 21-00-00. 2 L 7 2 4F RT A35EU 2003041500156 20030415 00156 WP 2003 4 15 U2RB100102 1 20021028 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76520 514 46088 DURING B-4 CHECK, FOUND RIVET POPPED AT FUSELAGE STATION -12, LEFT LONGERON NR 30. INVESTGATION REVEALED STRESS CRACK I N FUSELAGE SKIN AT RIVET HEAD. REMOVED DAMAGE SKIN, CLEANED AND TREATED IAW DC8 SRM 51-1-8 AND REPAIRED IAW DC8 SRM 53- 2-0 /51-1-21 AND REFINISHED. 2 L 7 4 4F 4A25 2003041500160 20030415 00160 SO 2003 4 15 SWIA200211646 1 20021112 A 2730 BOLT EMB 120 EMB120ER 3260203 SO ELE BELLCRANK CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 THE BOLTS THAT HOLD THE ELEVATOR BELLCRANK MOUNT TO THE VERTICAL STABILIZER HAVE CORROSION ON THEM. FOUND DURING C-CHEC K INSPECTION. REPLACED 8 BOLTS ON ELEVATOR BELLCRANK MOUNT WITH NEW ONES IAW 55-30-01. 2 L 7 2 4T RT A31SO 2003041500161 20030415 00161 SO 2003 4 15 SWIA200211647 1 20021112 A 2730 BUSHING EMB 120 EMB120ER 3260203 SO LT ELEVATOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 LT ELEVATOR ATTACHMENT BRACKET INBOARD BUSHINGS ARE CORRODED (HAT AND FLOAT BUSHINGS). FOUND DURING C-CHECK INSPECTION. REMOVED AND REPLACED BOTH HAT AND FLOAT BUSHINGS ON LEFT INBOARD ELEVATOR ATTACH BRACKET IAW 20-40-03. 2 L 7 2 4T RT A31SO 2003041500163 20030415 00163 SO 2003 4 15 SWIA200211649 1 20021112 A 5311 FRAME EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 FRAME 13 RT AND LT SIDE INBOARD AND OUTBOARD, PREVIOUS REPAIRS CRACKED OUTBOARD SIDE. CRACK GOES BEYOND DOUBLER ON THE RIGHT SIDE. FOUND DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED DOUBLERS TO CRACKED AREAS IAW EMB SRM 51-00-00 A ND 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 2003041500165 20030415 00165 SO 2003 4 15 SWIA200211651 1 20021112 A 5320 INTERCOSTAL EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 COCKPIT LEFT SIDE CRACK IN INTERCOSTAL BETWEEN FRAME 12A AND 13 (2 CRACKED RIVETS NEAR CRACK). FOUND DURING C-CHECK INS PECTION. STOP-DRILLED CRACK AND FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-40-02 AND 51-00-00. 2 L 7 2 4T RT A31SO 2003041500169 20030415 00169 SO 2003 4 15 SWIA200211655 1 20021224 A 5753 HINGE EMB 120 EMB120ER 3260203 SO LEFT FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 563SW 120338 LEFT NACELLE FLAP BY INBOARD HINGE IS CRACKED. FOUND DURING LINE INSPECTION. REPLACED NACELLE FLAP WITH SERVICEABLE UN IT IAW MM 27-50-02. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2003041500171 20030415 00171 SO 2003 4 15 SWIA200211657 1 20021231 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 233SW 120307 LEFT FORWARD OUTBOARD EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY WITH NEW ASSEMBLY IAW 33-52-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003041500173 20030415 00173 SO 2003 4 15 SWIA200211659 1 20021228 A 2731 52991 ACTUATOR EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM FROZEN A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 233SW 120307 ELEVATOR TRIM FROZE IN FLIGHT AT 24,000 FT -31C DEGREES. AFTER DESCENDING TO ABOUT 12,000 FT WITH OAT AT -5C DEGREES IT RETURNED TO NORMAL. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR TRIM ACTUATORS IAW MM 27-32-02. CABLES TENSIONED IAW MM 27-00-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003041500175 20030415 00175 EA 2003 4 15 SWIA200211661 1 20021231 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA STAIR LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 413SW 7102 MIDDLE STAIR LIGHT IS INOP. RE-LAMPED STAIR LIGHT IAW MM 33-23-04. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2003041600001 20030416 00001 SO 2003 4 16 SWIA200211662 1 20021220 A 4990 CAP EMB 120 EMB120ER 3260203 SO APU OIL SYS LOOSE A SWIA O OTHER B W SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C TX TAXI/GRND HDL 1 NM 07 235SW 120310 SMOKE IN THE CABIN WITH THE APU AND PACKS ON. SECURED APU OIL FILLER CAP AFTER SERVICING OIL TO PROPER LEVEL. NO FURTH ER EVIDENCE OF SMOKE OBSERVED. 2 L 7 2 4T RT A31SO 2003041600005 20030416 00005 EA 2003 4 16 SWIA200211667 1 20021229 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA LT SPOILER MALFUNCTIONED A SWIA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 NM 07 438SW 7574 RECEIVED LT SPOILERON FAULT MESSAGE ON TAKEOFF ROLL AT 80 KTS. ABORTED TAKEOFF. RETURNED TO GATE. FOUND LT INBOARD PC U (SPOILERON) FAULTY. REMOVED AND REPLACED LEFT SPOILERON INBOARD PCU IAW MM 27-64-01. OPS CHECK, LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2003041600007 20030416 00007 SO 2003 4 16 SWIA200211669 1 20021230 A 3150 COMPUTER EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 564SW 120339 ABORTED TAKEOFF AT 70 KTS DUE TO TRIPLE CHIME WARNING, WITHOUT ANY OTHER ANNUNCIATIONS ACCOMPANYING IT. ALL TAKEOFF PAR AMETERS WERE SET. RESET AURAL WARNING COMPUTER AND CHECK ALL WARNING SYSTEM. OPS CHECK GOOD ON GROUND. 2 L 7 2 4T RT A31SO 2003041400098 20030414 00098 EU 2003 4 14 CA030228002 1 20021205 A 3222 5322012200 LANDING GEAR PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL NOSE FAILED W C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA (CAN) NOSE GEAR DID NOT LOCK WHEN THE LANDING GEAR WAS RETRACTED. - NOSE GEAR OLEO FOUND NOT EXTENDING COMPLETELY.- NOSE GER FORK RUBBED ON NOSE GEAR DOOR ACTUATING ROD. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2003041500122 20030415 00122 SO 2003 4 15 SWIA200211598 1 20021216 A 2997 WIRE EMB 120 EMB120ER 3260203 SO HYD AUX PUMP BURNED A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 234SW 120308 BURNING ODOR STARTED 20 MIN INTO FLIGHT. PACKS WERE TURNED OFF ONE AT A TIME TO ISOLATE THE PROBLEM. ODOR STILL REMAIN ED AND AT FL240 PRESSURE COULD NOT BE MAINTAINED ON ONE PACK. FOUND NUT LOOSE AT RCCB, CB0256 FOR BLUE HYDRAULIC AUX PU MP, AND BURNED WIRE. TIGHTENED NUT, REMOVED AND REPLACED WIRE W208-0240-2. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003041500124 20030415 00124 2003 4 15 SWIA200211601 4 20021219 A 2210 10231007 DAMPER CNDAIR CL600 CL6002B19 1900309 EA LT AILERON MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 426SW 195 195 7468 DURING FLIGHT, RECEIVED A -FLUTTER DAMPER- STATUS MESSAGE FOR THE LEFT AILERON. REMOVED AND REPLACED LEFT AILERON FLUT TER DAMPER IAW CRJ 27-15-05. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2003041500126 20030415 00126 2003 4 15 SWIA200211603 4 20021219 A 3418 C818061 COMPUTER EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 198SW 6706 6706 120227 STALL SYSTEM NR 2, STICK SHAKER AND STICK PUSHER, ACTIVATED ON GROUND. REMOVED AND REPLACED FIRST OFFICER'S STALL WARNI NG COMPUTER IAW MM 27-34-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003041500130 20030415 00130 EA 2003 4 15 SWIA200211607 1 20021220 A 2750 7805013 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 595SW 7292 FLAP FAIL MESSAGE AFTER LANDING WHEN RAISING FLAPS FROM 45 TO 30 DEGREES. REMOVED AND REPLACED FLAP CONTROL LEVER PER M M 27-51-01. OPS CHECKED GOOD. NO SKEWING OR DEFORMATION NOTED ON FLAPS. 2 L 7 2 4F RT A21EA 2003041500133 20030415 00133 2003 4 15 SWIA200211610 4 20021223 A 3420 6229336400 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA NR 2 AHRS MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 499SW 4363 4363 7398 FIRST OFFICER'S HEADING KEPT DRIFTING LEFT IN FLIGHT CAUSING EFIS COMP MONITOR CAUTION MESSAGE. FOLLOWED QRH, SWITCHED TO DG MODE AND HEADING KEPT DRIFTING. RETURNED TO DFW. REPLACED NR 2 AHARS COMPUTER IAW 34-21-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2003041500136 20030415 00136 EA 2003 4 15 SWIA200211613 1 20021126 A 5310 SILL CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 CARGO DOOR FLOOR SILL FS 575.5 CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-61- 620 'NC'. NDT-HFEC CARRIED OUT IAW REO 601R-53-61-620. NO CRACKS NOTED. 2 L 7 2 4F RT A21EA 2003041500139 20030415 00139 EA 2003 4 15 SWIA200211619 1 20021225 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 597SW 7293 EMERGENCY FLOOR LIGHTING ROW 9 THROUGH 12 INOP. FOUND NR 4 EMERGENCY BATTERY CHARGER INOP. REMOVED AND REPLACED NR 4 E MERGENCY BATTERY CHARGER WITH SERVICEABLE UNIT IAW MM 33-51-05. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY WITH SERVIC EABLE UNIT IAW MM 33-51-04. EMERGENCY LIGHTS OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2003041500147 20030415 00147 SO 2003 4 15 SWIA200211628 1 20021223 A 2797 WIRE EMB 120 EMB120ER 3260203 SO RUDDER TRIM ACT FRAYED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 234SW 120308 DURING FIRST FLIGHT OF THE DAY AUTOPILOT TEST, RECEIVED -YAW DIS- ON FIRST OFFICER'S FLIGHT CONTROL PANEL AND ASSOCIATED -YAW DIS- ON AP CONTROL PANEL. ALSO -R- ON AUTOPILOT CONTROL PANEL. UPON INSPECTION FOUND RUDDER TRIM ACTUATOR CABLE WIRE FRAYED AND BINDING. REMOVED AND REPLACED CABLE WITH SERVICEABLE RUDDER TRIM ACTUATOR CABLE AND TENSIONED TRIM CABL ES IAW EMB120 MM 27-00-01. OPS CHECK GOOD. AFTER REPLACEMENT OF RUDDER TRIM ACTUATOR, OPS CHECK OF AUTOPILOT GOOD. 2 L 7 2 4T RT A31SO 2003041500153 20030415 00153 2003 4 15 YENA200236 4 20021224 A 2370 DISPLAY AIRBUS 320 A320232 3930326 EU VIDEO SYS ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 524JB 1528 ACRID ELECTRICAL ODOR REPORTED AROUND ROW 14, 15 ABC. CREW TURNED OFF TV DISPLAY AT THESE ROWS AND ODOR DISSIPATED. OD OR WAS REPORTED FROM PAX AND F/A'S. INSPECTED S/S WIRING FROM ROWS 13-15. CHECKED SEB FOR SPILLAGE OR FOD. NO FAULTS NOTED. ALL LIVE TV OPS CHECK NORMAL. NO ELECTRICAL ODOR NOTED. IN ADDITION TO LIVETV INSP & OPS CHECK, QC INSPECTED W IRING IN AREA OF ROWS MENTIONED. ALL OK. 2 L 7 2 4F RT A28NM 2003041500162 20030415 00162 SO 2003 4 15 SWIA200211648 1 20021112 A 5320 BRACKET EMB 120 EMB120ER 3260203 SO HYD BAY CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 CRACKED ALUMINUM BRACKET IN THE RIGHT SIDE OF THE HYDRAULIC BAY (AGAINST THE FIRE WALL, NEAREST TO THE INBOARD SIDE). F OUND DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED REPAIR ANGLE IAW EMB SRM 51-70-06 & 51-40-02. 2 L 7 2 4T RT A31SO 2003041500164 20030415 00164 SO 2003 4 15 SWIA200211650 1 20021112 A 5320 BRACKET EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT HYD RESERVOIR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 LEFT HYDRAULIC RESERVOIR INBOARD VERTICAL BRACKET MOUNTING HAS 3 INCH + VERTICAL CRACK INSIDE THE BRACKET. FOUND DURING C-CHECK INSPECTION. REMOVED VERTICAL MOUNTING BRACKET AND INSTALLED NEW HYDRAULIC RESERVOIR MOUNTING BRACKET IN ITS PL ACE IAW EMB SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 2003041500170 20030415 00170 SO 2003 4 15 SWIA200211656 1 20021224 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 233SW 120307 ROW 6C EMERGENCY EXIT LIGHT FIXTURE IS BROKEN. INSTALLED SERVICEABLE LIGHT FIXTURE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003041600003 20030416 00003 SO 2003 4 16 SWIA200211664 1 20021231 A 7712 CONNECTOR EMB 120 EMB120ER 3260203 SO TORQUE SIGNAL CO LOOSE A SWIA C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 NM 07 212SW 120276 ON TAKEOFF RECEIVED AN AUTOFEATHER WARNING. ABORTED THE TAKEOFF AND RETURNED TO THE GATE. FOUND CONNECTOR ON LT ENGINE TORQUE SIGNAL CONDITIONER LOOSE. RE-TIGHTENED, RAN AND OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2003041600010 20030416 00010 SO 2003 4 16 SWIA200211672 1 20021229 A 1220 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 1 LACK OF LUBE A SWIA C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 NM 07 297SW 120327 ON TAKEOFF ROLL AT ABOUT 90 KTS, RECEIVED A TRIPLE CHIME AND OIL AURAL WARNING. ABORTED TAKEOFF (NO MAP PANEL LIGHT). OIL PRESSURE GAUGE INDICATED IN GREEN AREA. REPLACED RIGHT ENGINE OIL PRESSURE SWITCH AND CARBON SEAL WITH SERVICEABLE UNITS. ADDED 2 QUARTS OF OIL TO RIGHT ENGINE AND 1 QUART TO LEFT ENGINE. PERFORMED ENGINE RUNUP OF BOTH ENGINES. ALL PARAMETERS FOUND TO BE WITHIN LIMITS. NO WARNINGS. LEAK CHECK AND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2003041600019 20030416 00019 NE 2003 4 16 SWIA200211677 2 20021231 A 7230 BLADE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT ENGINE BIRD STRIKE A SWIA A UNSCHED LANDING C X J F.O.D. ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 NM 07 934SW 7722 AFTER TAKEOFF FROM SMF, THE LEFT NOSE SECTION WAS STRUCK BY BIRD. SHORTLY AFTER BIRD IMPACT, THE LEFT ENGINE FAILED DUE TO BIRD INGESTION. NO FIRE INDICATIONS. FOLLOWED QRH PROCEDURE. C/W BIRDSTRIKE INSPECTION CHECKLIST IAW ST12-413. N O DAMAGE TO RADOME. FOUND DAMAGE TO NR 1 ENGINE FAN BLADES. REMOVED DAMAGED FANS FROM LEFT ENGINE BLADES AND REPLACED WITH SERVICEABLE UNITS. DAMAGED BLADES ARE 1, 2, 3, 4, 5,14,15, 22, 25, 26, 27 & 28. REINSTALLED SPINNER AND NOSE CONE , ENGINE COWLINGS. BOROSCOPED FIRST, SECOND AND THIRD COMPRESSORS. NO DAMAGE FOUND IN COMPRESSOR SECTION. RAN ENGINE TO TAKEOFF POWER. ALL CHECKS GOOD. FAN BLADES CHECK IAW SEI-756 SP 50. 2 L 7 2 4F 4 F RT A21EA E15NE 2003041600027 20030416 00027 WP 2003 4 16 UPS03840001 1 20021231 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C2, MAIN CABIN BEAR TRAP LOCATION SEAT TRACK F STA 774 HAS WORN SCALLOPS. BLENDED SCALLOP AND FOUND O UT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED DAMAGE AREA IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INST ALLED PLUG AND CHANNEL IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2003041600029 20030416 00029 WP 2003 4 16 UPS03840003 1 20021230 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C2, SEAT TRACK WORN FS 710 LBL 50 DOT EO314. BLENDED AREA AND FOUND OUT OF LIMITS AT FS 685 AND 690. ROUTED OUT DAMAGE IAW DC8 SRM 53-2-3. ALODINED, PRIMED AND INSTALLED PLUG IAW DC8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2003041600030 20030416 00030 WP 2003 4 16 AALA20021726 1 20020912 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE TORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - FOUND CUSP TORN STATION 218 FORWARD OF NR 4 SLAT IN CABIN. REPLACED CUSP DIAPHRAGM PER 53-00-00-13. (M) 2 L 7 2 4F A6WE 2003041600032 20030416 00032 WP 2003 4 16 AALA20021727 1 20021203 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - FOUND FLOOR PAN CRACKED. INSTALLED DOUBLER PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 2003041600034 20030416 00034 WP 2003 4 16 AALA20021729 1 20020913 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - FOUND CORROSION AT FASTENER HOLE STATION 1338. INSTALLED DOUBLER AND FILLER SRM 53-05 FIG 20A. (M) 2 L 7 2 4F A6WE 2003041600036 20030416 00036 WP 2003 4 16 AALA20021730 1 20021204 A 5345 MOUNT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - FOUND STATION 212, G2 INBOARD FLOOR TIE DOWN HAS CORROSION. REMOVED AND REPLACED G2 FLOOR TIE DOWN STATION 212. (M) 2 L 7 2 4F A6WE 2003041600038 20030416 00038 WP 2003 4 16 AALA20021731 1 20021204 A 5345 MOUNT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - FOUND STATION 218 G2 INBOARD FLOOR TIEDOWN HAS CORROSION. REPAIRED G2 INBOARD FLOOR TIEDOWN PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2003041600040 20030416 00040 WP 2003 4 16 AALA20021733 1 20020912 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - FOUND WINDOW PANEL FRAME CRACKED AT FORWARD LOWER CORNER. TRIMMED OUT CRACK. FABRICATED AND INSTALLED DOUBLER PE R AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2003041600042 20030416 00042 WP 2003 4 16 AALA20021736 1 20020918 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - FOUND CUSP CRACKED AFT STATION 1287 INBOARD OF NR 1 SEAT TRACK. STOP DRILLED CRACK. INSTALLED DOUBLER PER SRM 53 -01. (M) 2 L 7 2 4F A6WE 2003041600044 20030416 00044 WP 2003 4 16 AALA20021739 1 20021203 A 5310 9911840 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND SHEAR TIE CRACKED AT FASTENER HOLE, RIGHT SIDE OF L2R. REPLACED WITH SERVICEABLE SHEAR TIE PER SRM 51-30. (M) 2 L 7 2 4F A6WE 2003041600046 20030416 00046 WP 2003 4 16 AALA20021740 1 20021203 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND SHEAR TIE CRACKED STATION 1437, RIGHT SIDE OF LONGERON 1R AFT SIDE. REMOVED AND REPLACED SHEAR TIE PER SRM 51-30. (M) 2 L 7 2 4F A6WE 2003041600047 20030416 00047 WP 2003 4 16 AALA20021741 1 20021119 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND CORROSION IN FUSELAGE SKIN INBOARD AREA OF FORWARD LAVATORY DRAIN ACCESS AREA BEYOND MANUAL LIMITS. INSTALL ED DOUBLER PER ESO 80559, DATED 11-18-2002. (M) 2 L 7 2 4F A6WE 2003041600049 20030416 00049 WP 2003 4 16 AALA20021742 1 20021119 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND STATION 636 FORWARD SIDE OF DOOR JAMB DAMAGE TO STRUCTURE FROM TO LONGERON SCREW BEING INSTALLED IN FLOORBOA RD. INSTALLATION OF DOUBLER PER AARD 53-10-00-24. (M) 2 L 7 2 4F A6WE 2003041600053 20030416 00053 WP 2003 4 16 AALA20021744 1 20021120 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND CORROSION ON BOTTOM SIDE OF CLIP NUT TABS, BEYOND MANUAL LIMITS. SPLICE IN NEW SECTION OF NR 2 SEAT TRACK P ER SRM 53-05. (M) 2 L 7 2 4F A6WE 2003041600056 20030416 00056 WP 2003 4 16 AALA20021746 1 20021115 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND TWO CRACKS ON BELL FRAME STATION 1174, L6L. INSTALLED DOUBLER, STOP DRILLED CRACKS PER 53-10-00-30. (M) 2 L 7 2 4F A6WE 2003041600057 20030416 00057 WP 2003 4 16 AALA20021747 1 20021112 A 5320 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND CORROSION ON HORIZONTAL AND VERTICAL SURFACES OF MID CARGO DOOR BEAM. REMOVED CORROSION PER SRM 51-10-03. INSTALLED DOUBLER ON DOOR BEAM WHERE CORROSION REMOVAL WAS BEYOND MANUAL LIMITS PER AARD 53-10-00-8. (M) 2 L 7 2 4F A6WE 2003041600058 20030416 00058 WP 2003 4 16 AALA20021748 1 20021114 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE TORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND RIGHT CUSP TORN AT STATION 1000. REPLACED CUSP, RIGHT SIDE, STATION 1000 PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2003041600061 20030416 00061 WP 2003 4 16 AALA20021751 1 20021115 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND LONGERON 17L CRACKED WHERE IT INTERSECTS FRAME 237. INSTALLED LONGERON SPLICE PER SRM 53-02-00 FIG 18. (M) 2 L 7 2 4F A6WE 2003041600062 20030416 00062 WP 2003 4 16 AALA20021752 1 20021115 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND LONGERON 17L CRACKED AT STATION 332. INSTALLED LONGERON SPLICE PER SRM 53-02-00 FIG 18. (M) 2 L 7 2 4F A6WE 2003041600065 20030416 00065 NE 2003 4 16 SWIA200211614 2 20021224 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE RIGHT MALFUNCTIONED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 07 592SW 7279 ENGINE NR 2 FAILURE INFLIGHT. DURING CRUISE FLIGHT THE RT ITT WAS 50 DEGREES HIGHER THAN ENGINE NR 1 WITH A REDUCTION O F N1 ON ENGINE NR 2 OF 4 PERCENT. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY IAW CRJ MM 71-00-00 DUE TO COMPRESSOR BLAD E DAMAGE. 2 L 7 2 4F 4 F RT A21EA E15NE 2003041600079 20030416 00079 WP 2003 4 16 AALA20021757 1 20021118 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 435AA 49453 TUL - FOUND CORROSION IN NR 2 SEAT TRACK AT APPROX STATION 1304. REMOVED CORRODED AREA AND INSTALLED SEAT TRACK PLUG RE PAIR PER 53-20-00-10. (M) 2 L 7 2 4F RT A6WE 2003041600084 20030416 00084 WP 2003 4 16 AALA20021760 1 20021120 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND CORROSION ON CUSP STATION 1174 AROUND HOLES FOR NR 1 SEAT TRACK. REMOVED CORROSION PER SRM 51-10-03. INSTA LLED REPAIR DOUBLER PER SRM 53-01-00 FIG 4 SHEET 3 PAGE 10. (M) 2 L 7 2 4F A6WE 2003041600087 20030416 00087 WP 2003 4 16 AALA20021762 1 20021126 A 5311 59360751 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND CORROSION ON FRAME 1218 L27R-L28R. INSTALLED DOUBLER PER SRM 53-01 FIG 1 SHEET 3. (M) 2 L 7 2 4F A6WE 2003041600089 20030416 00089 WP 2003 4 16 AALA20021764 1 20021120 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND FORWARD ENTRY DOOR JAM WEB CRACKED. INSTALLED DOUBLER PER 53-01 FIG 38. (M) 2 L 7 2 4F A6WE 2003041600091 20030416 00091 WP 2003 4 16 AALA20021765 1 20021120 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND FORWARD GIRT BAR SUPPORT CORROSION, FORWARD SERVICE DOOR. INSTALLED DOUBLER PER 53-01 FIG 38. (M) 2 L 7 2 4F A6WE 2003041600092 20030416 00092 WP 2003 4 16 AALA20021766 1 20021204 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND CORROSION ON LOWER HORIZONTAL LEG OF FORWARD CARGO DOOR JAMB PAN STATION 389-417. REPLACED BOTTOM SECTION O F DOOR PAN PER SRM 53-05-00 FIG 44. (M) 2 L 7 2 4F A6WE 2003041600094 20030416 00094 WP 2003 4 16 AALA20021768 1 20021126 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND CORROSION ON WEB AT TOP OF DOOR BEAM. REMOVED AND REPLACED AFT CARGO DOOR BEAM WEB 53-10-00-24 AARD. (M) 2 L 7 2 4F A6WE 2003041600098 20030416 00098 WP 2003 4 16 AALA20021793 1 20021126 A 5311 991960317 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND CORROSION ON FRAME STATION 1231, FORWARD SIDE ABOVE L30. INSTALLED DOUBLER PER AARD 53-10-00-14 W/PR 1422. (M) 2 L 7 2 4F A6WE 2003041600106 20030416 00106 NE 2003 4 16 AALA20021872 2 20021227 A 7532 BLEED VALVE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535* NE LT ENGINE MALFUNCTIONED A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 629AA 24587 DEN - FLT 432 - EN ROUTE DEN-DFW, AFTER TAKEOFF, THE LEFT ENGINE HAD WHAT APPEARED TO BE A PRESSURE STALL. THE ENGINE W AS SHUT DOWN AND THE AIRCRAFT RETURNED TO DEN WITHOUT INCIDENT. PERFORMED ENGINE BORESCOPE PER MM. REPLACED THE LEFT A ND RIGHT HP3 SOLENOIDS, HP2 SOLENOID, LEFT AND RIGHT HP3 BLEED VALVES AND HP2 BLEED VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2003041600108 20030416 00108 NM 2003 4 16 AALA20021875 1 20021222 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 606AA 27057 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING ROW 9 THROUGH 15 INOPERATIVE. REPLACED EMERGENCY LIG HT BATTERY PACK AND CHARGER AT M10952 UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003041600120 20030416 00120 NM 2003 4 16 AALA20021876 1 20021220 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 676AN 29426 JFK - DURING OVERNIGHT MAINTENANCE, FLOOR MOUNTED EMERGENCY EXIT LIGHTS IN FIRST CLASS INOPERATIVE. SECURED LOOSE CONNE CTOR AT SEAT 1E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003041600128 20030416 00128 WP 2003 4 16 AALA20021887 1 20021228 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 285AA 49297 DFW - DURING OVERNIGHT MAINTENANCE, AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003041600129 20030416 00129 WP 2003 4 16 AALA20021888 1 20021228 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 288AA 49300 AUS - DURING OVERNIGHT MAINTENANCE, FORWARD CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATT ERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003041600142 20030416 00142 WP 2003 4 16 AALA20030026 1 20021216 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 580AA 53157 TUL - FOUND NR 5 SEAT TRACK CORRODED FROM STATION 200-206. INSTALLED NEW SEAT TRACK FROM STATION 200R-247R PER SRM 53-0 5. (M) 2 L 7 2 4F A6WE 2003041600145 20030416 00145 WP 2003 4 16 AALA20030028 1 20021211 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 580AA 53157 TUL - FOUND BELL FRAME END FITTING CORRODED AT STATION 579 AT RIGHT CUSP. REPLACED BELL FRAME END FITTING RIGHT SIDE ST ATION 579 SRM 51-01. (M) 2 L 7 2 4F A6WE 2003041600147 20030416 00147 WP 2003 4 16 AALA20030029 1 20021216 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 580AA 53157 TUL - FOUND NR 6 SEAT TRACK CORRODED AT 1ST FASTENER HOLE, STATION 216. REMOVED AND REPLACED NR 6 SEAT TRACK FROM STATI ON 216-303 PER SRM 53-05-00, FIG 4F, SHEET 1 THROUGH SHEET 11. (M) 2 L 7 2 4F A6WE 2003041500083 20030415 00083 EA 2003 4 15 CA030329002 1 20020915 A 7830 A33721 BRACE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE THRUST REVERSER UNSECURE W E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA (CAN) FLT CREW REPORTED THAT THE NR 1 THRUST LEVER JAMMED AT 90 PERCENT THRUST AND WERE UNABLE TO REDUCE POWER. LT ENGIN E HAD TO BE SHUT DOWN USING FIRE PUSH SWITCH. AIRCRAFT LANDED IN ORLANDO WITHOUT INCIDENTMAINTENANCE FOUND THAT THE UPP ER CORE COWL HOLD OPEN ROD HAD COME LOOSE AND JAMMED THE ENGINE CONTROLS. 2 L 7 2 4F 4 F RT A21EA E15NE 2003041500113 20030415 00113 EA 2003 4 15 SWIA200211593 1 20021218 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 597SW 1991 761 7293 EMERGENCY LIGHTS SEGMENT WILL NOT TEST. REMOVED AND REPLACED NR 4 EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-00. OPS C HECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2003041500116 20030415 00116 NM 2003 4 15 XNOA01095 1 20021220 A 5270 WARNING LIGHT BOEING 727 727227 1384078 NM CARGO DOOR ILLUMINATED A XN0A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 79754 21363 PRIOR TO TAKEOFF ROLL CARGO DOOR WARNING LIGHT ILLUMINATED. ADJUSTED FWD VENT DOOR SWITCH IAW STC WAI9815-6 PG 6.5. OP S CHECK GOOD. 2 L 7 3 4F A3WE 2003041500128 20030415 00128 EA 2003 4 15 SWIA200211605 1 20021220 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 920SW 7660 RT COCKPIT SIDE WINDOW CRACKED. REPLACED RIGHT COCKPIT SIDE WINDOW. OPS CHECK GOOD. NO LEAKS NOTED IAW MM 56-11-01 AN D 56-12-01. P/N: NP-139322-6 S/N OFF: 02052H9140. 2 L 7 2 4F RT A21EA 2003041500129 20030415 00129 EA 2003 4 15 SWIA200211606 1 20021220 A 2740 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM ILLUMINATED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 906SW 7510 STAB TRIM CH 1 MESSAGE ILLUMINATED IN FLIGHT. RETURNED TO DEN. INSTALLED SERVICEABLE HSTCU. OPS CHECK GOOD. NO DEFEC TS NOTED. 2 L 7 2 4F RT A21EA 2003041500132 20030415 00132 EA 2003 4 15 SWIA200211609 1 20021222 A 2740 70607 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 589SW 2 2 7072 STAB CHANNEL NR 2 WILL NOT ENGAGE. REPLACED HSTCU IAW 27-41-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2003041500134 20030415 00134 EA 2003 4 15 SWIA200211611 1 20021126 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA INTERCOSTAL CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 FS 625.0 RIGHT INTERCOSTAL ANGLE AT STR 14R CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL ANGLE IAW C RJ SRM 51-40-11 AND 51-42-06. P/N: 601-35012-52. 2 L 7 2 4F RT A21EA 2003041500138 20030415 00138 EA 2003 4 15 SWIA200211618 1 20021225 A 2740 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA CHANNEL 2 MALFUNCTIONED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 589SW 2169 2169 7072 STAB TRIM CHANNEL NR 2 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU WITH SERVICEABLE UNIT IAW MM 27-41-01. PERFORMED OP S CHECK 5 TIMES FROM BOTH TRIM SWITCHES. OPS CHECK GOOD. PERFORMED HSTCU SELF-TEST IAW MM 27-41-00 4 TIMES. NO FAULTS NOTED. OPS CHECK GOOD. RETURNED TO CAT II STATUS. P/N OFF: 7060-8, S/N OF: 1117, P/N ON: 7060-7, S/N ON: 174. 2 L 7 2 4F RT A21EA 2003041500141 20030415 00141 SO 2003 4 15 SWIA200211621 1 20021220 A 2435 SEAL EMB 120 EMB120ER 3260203 SO RT STARTER GEN LEAKING A SWIA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 NM 07 297SW 120327 TWO ABORTED TAKEOFFS IN A ROW FOR TRIPLE CHIME 'OIL'. ADDED OIL TWO LEGS PRIOR. ON SHUTDOWN NR 2 ENGINE WAS AT 'ADD 3' . REPLACED RT ENGINE STARTER GEN GEARSHAFT SEAL IAW PRATT & WHITNEY MM 72-20-00. NO OTHER SIGNS OF EXTERNAL OIL LEAKS NOTED AT THIS TIME. ADDED 2 QUARTS OIL TO THE RIGHT ENGINE. 2 L 7 2 4T RT A31SO 2003041500142 20030415 00142 SO 2003 4 15 SWIA200211622 1 20021223 A 2750 12064207615 SELECTOR SWITCH EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 270YV 1662 1662 120270 WHEN FLAPS COMMANDED TO 15 DEGREES AND 25 DEGREES, 'CONTROL FAULT' ILLUMINATED. RESET PER THE QRH. REPLACED FLAP SELEC TOR SWITCH. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003041500144 20030415 00144 EA 2003 4 15 SWIA200211625 1 20021223 A 2760 52C52610 MANIFOLD CNDAIR CL600 CL6002B19 1900309 EA GROUND SPOILER MALFUNCTIONED A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 929SW 7703 GROUND SPOILER DEPLOY MESSAGE WOULD NOT GO AWAY. INSTALLED SERVICEABLE INBOARD GROUND SPOILER MANIFOLD ASSEMBLY IAW MM 27-63-05. NO LEAKS NOTED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2003041500148 20030415 00148 SO 2003 4 15 SWIA200211629 1 20021217 A 2731 52991 ACTUATOR EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM FROZEN A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 566SW 2219 2219 120341 AT 16,000 IN ICING CONDITIONS THE ELEVATOR TRIM JAMMED IN MANUAL MODE. ELECTRIC TRIM WORKED NORMALLY AFTER LEAVING ICIN G CONDITIONS. REMOVED AND REPLACED RIGHT AND LEFT ELEVATOR TRIM ACTUATORS IAW EMB MM 27-32-02. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003041500159 20030415 00159 2003 4 15 SWIA200211644 4 20021230 A 3421 6229810016 DISPLAY CNDAIR CL600 CL6002B19 1900309 EA ATTITUDE IND MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 435SW 3516 3516 7555 AFTER TAKEOFF THE FIRST OFFICER'S ATTITUDE INDICATOR FAILED. ATT, FD, AND MAG FLAGS ILLUMINATED. QRH WAS INEFFECTIVE, RETURNED TO SLC. REMOVED AND REPLACED FIRST OFFICER'S PFD IAW MM 31-61-01. OPS CHECK GOOD IAW MM 34-25-00-710-901. 2 L 7 2 4F RT A21EA 2003041500167 20030415 00167 SO 2003 4 15 SWIA200211653 1 20021112 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 FORWARD AND AFT, RIGHT AND LEFT SIDES, FLOOR SEAT TRACKS ARE CORRODED. FOUND DURING C-CHECK INSPECTION. INSTALLED NEW SEAT TRACKS IAW MM 53-01-05. 2 L 7 2 4T RT A31SO 2003041500172 20030415 00172 SO 2003 4 15 SWIA200211658 1 20021227 A 3040 MOTOR EMB 120 EMB120ER 3260203 SO WINDSHIELDWIPER FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 233SW 6941 6941 120307 AFTER TAKEOFF THE RIGHT WINDSHIELD WIPER WOULD NOT PARK. RETURNED TO RDD DUE TO WIPER BOUNCING ON WINDSHIELD. REPLACED RIGHT WINDSHIELD WIPER MOTOR ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003041500174 20030415 00174 EA 2003 4 15 SWIA200211660 1 20021229 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT FAILED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 413SW 7102 EMERGENCY LIGHTS ON FLOOR INOP. FOUND BAD CONNECTION AT FORWARD LIGHT STRIP. REMOVED AND REPLACED CONNECTION AS REQUIR ED. OPS CHECK GOOD. P/N: 5996-5. 2 L 7 2 4F RT A21EA 2003041600006 20030416 00006 EA 2003 4 16 SWIA200211668 1 20021229 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA FLAP INDICATOR DAMAGED A SWIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 405SW 7029 FLAPS INDICATE DIFFERENT VALUES AT 20 DEGREE SETTING. RETURNED TO GATE. REINSTALLED WIRE AT PIN 40 P211, RE-POWERED AN D INITIALIZED FLAP SYSTEM. PERFORMED EXTENSIVE OPS CHECK OF FLAPS. ALL INDICATION FOUND TO BE MATCHED AND NORMAL. 2 L 7 2 4F RT A21EA 2003041600028 20030416 00028 WP 2003 4 16 UPS03840002 1 20021230 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C2, MAIN CABIN SEAT TRACK G GOUGED AT FS 280. DAMAGE FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. R EMOVED DAMAGE SCOLLOPS IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. LOCATED PART IAW DC8 SRM 53-2-3. INSTALLED PART IAW DC8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2003041600039 20030416 00039 WP 2003 4 16 AALA20021732 1 20020912 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - FOUND CORROSION RIGHT WINDOW PANEL FRAME CRACKED FS 1041 AT FORWARD LOWER CORNER. TRIMMED OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER PER AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2003041600055 20030416 00055 WP 2003 4 16 AALA20021745 1 20021121 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND CRACKED .375 INCH IN FUSELAGE SKIN FROM RIVET HEAD STATION 1380 L14L. INSTALLED DOUBLER PER AARD 53-30-00-0 2. (M) 2 L 7 2 4F A6WE 2003041600076 20030416 00076 WP 2003 4 16 AALA20021755 1 20021121 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND CRACK IN FUSELAGE SKIN STATION 1418 JUST ABOVE ENGINE PYLON. INSTALLED DOUBLER PER SRM 53-01-00 PAGE 9. (M ) 2 L 7 2 4F A6WE 2003041600093 20030416 00093 WP 2003 4 16 AALA20021767 1 20021126 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND CORROSION ON VERTICAL AND HORIZONTAL LEGS OF DOOR BEAM. REMOVED AND REPLACED AFT CARGO DOOR BEAM AARD 53-10 -00-3. (M) 2 L 7 2 4F A6WE 2003041600095 20030416 00095 WP 2003 4 16 AALA20021769 1 20021127 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND CORROSION ON DOOR BEAM WEB. REMOVED AND REPLACED AFT CARGO DOOR BEAM WEB 53-10-00-24 AARD. (M) 2 L 7 2 4F A6WE 2003041600125 20030416 00125 WP 2003 4 16 AALA20021884 1 20021229 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 423AA 49335 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY CEILING EXIT LIGHTS AT ROW 17-21 INOPERATIVE. TIGHTENED EMERGENCY EXIT LI GHT CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003041600200 20030416 00200 WP 2003 4 16 AALA22021735 1 20021125 A 5345 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - FOUND CORROSION, G1 FORWARD CENTER FLOOR TIE DOWN. REMOVED AND REPLACED TIE DOWN BRACKET. (M) 2 L 7 2 4F A6WE 2003041600210 20030416 00210 WP 2003 4 16 AALA20030030 1 20021213 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 580AA 53157 TUL - FOUND CUSP IS CRACKED AT STATION 218 AND NR 6 SEAT TRACK. REMOVED AND REPLACED CUSP FROM STATION 218-237 UNDER NR 5 AND NR 6 SEAT TRACKS PER SRM 51-01-00. (M) 2 L 7 2 4F A6WE 2003041600233 20030416 00233 NM 2003 4 16 UPS03240417 1 20020326 A 5310 GUSSET BOEING 727 727173C 1384059 NM TORQUE BOX CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, SUSPECT CRACK AT 1263 UPPER BEAM AT INNER RADIUS OF FLANGE ADJACENT TO THIRD FASTENER VERT, FROM I/ B END, RT TORQUE BOX (GUSSET). HFEC C/W CRACK CONFIRMED AND ENDS MARKED. GUSSET AND ANCILLARY STRUT URE DISPLACED IAW SRM 5130-02. NEW GUSSET INSTALLED IAW DWG 65C1387 4 AND UPS EO B727-5310-1239. 2 L 7 3 4F A3WE 2003041600281 20030416 00281 WP 2003 4 16 UPS03840035 1 20020103 A 5320 5616306171 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE: C2, STA 950 INTERCOSTAL IS CRACKED BETWEEN MAIN LANDING GEAR DOORS AT RBL 4. REMOVED AND REPLACED INT ERCOSTAL IAW DWG 5616306, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2003041600285 20030416 00285 NE 2003 4 16 PCS2003F00000 2 20020617 A 7261 652186718 LINE BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE LOOSE A PCSA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 17 994AJ 20942 CREW REPORTED NR 2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO LOSS OF OIL QUANTITY AND OIL PRESSURE FLUCTUATING IN FLIGHT. AI RCRAFT LANDED AT THE INTENDED DESTINATION WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 2 ENGINE OIL PRESSURE LINE LOO SE. THE LINE WAS TIGHTENED, SERVICED ENGINE OIL, RAN ENGINE, NO LEAKS NOTED AND ALL PARAMETERS CHECK OK. IWA MM. 2 L 7 3 4F 4 F RT A3WE E2EA 2003041600287 20030416 00287 EA 2003 4 16 SWIA200211716 1 20021212 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA E/E BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 ELECTRICAL BAY FLOOR FS 193.0 LEFT AND RIGHT SIDES CRACKED. FOUND DURING C-CHECK INSPECTION. HFEC INSPECTION COMPLIED WITH ON CUTOUT EDGE AND AREA AS REQUESTED IAW RJ NDTM 51-20-06. NO CRACKS FOUND. DAMAGED AREA REPAIRED IAW CRJ REO 601 R-53-11-081 REV 'NC'. 2 L 7 2 4F RT A21EA 2003041600291 20030416 00291 EA 2003 4 16 SWIA200211718 1 20021212 A 1430 BOLT CNDAIR CL600 CL6002B19 1900309 EA WINDSHIELD CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 MOUNTING BOLTS ON BOTH LT AND RT WINDSCREENS ARE CORRODED. FOUND DURING C-CHECK INSPECTION. REPLACED BOLTS IAW CRJ AMM 20-21-00. 2 L 7 2 4F RT A21EA 2003041600295 20030416 00295 EA 2003 4 16 SWIA200211719 1 20021212 A 5411 RIB CNDAIR CL600 CL6002B19 1900309 EA LT PYLON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 LEFT PYLON RIB AT FS 605.00 FOUND CRACKED. FOUND DURING C-CHECK INSPECTION. PYLON RIB INSTALLED AT FS 605.00 IAW CRJ S RM 51-42-20, 51-40-11 & 51-42-06. 2 L 7 2 4F RT A21EA 2003041600297 20030416 00297 SO 2003 4 16 SWIA200211689 1 20021214 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 562SW 120336 FUSELAGE FRAME CRACKED BEHIND CAPTAIN'S DV WINDOW. FOUND DURING C-CHECK INSPECTION. REPLACED AFFECTED BRACKET IAW EMB1 20 SRM 51-10-02. 2 L 7 2 4T RT A31SO 2003041600301 20030416 00301 WP 2003 4 16 UPS03840076 1 20021226 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, R1 LOWER AFT DOOR JAMB CORNER HAS A CRACK FOUND WITH NDT. REMOVED DAMAGE IAW DC8 SRM 53-2-0. FA BBED FILLER, DOUBLER, TRIPLER IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 53-2-0 . 2 L 7 4 4F RT 4A25 2003041600304 20030416 00304 WP 2003 4 16 UPS03840083 1 20021227 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, R1 UPPER FWD DOOR JAMB CORNER EXTERNAL FUSELAGE SKIN CRACKED AT FASTENER HOLE OF FIRST FASTENER R OW AT APPROX 45 DEGREES POINT OF CORNER RADIUS. REMOVED DAMAGE AREA, FABBED FILLER, DOUBLER, TRIPLER IAW DC8 SRM 53- 2- 0 AND REVISION 53-154. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2003041600306 20030416 00306 WP 2003 4 16 UPS03840008 1 20021227 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, FUSELAGE EXTERIOR SKIN CRACKED STA 1750 L15L-16L. CONFIRMED CRACK WITH HFEC IAW NDT SPM 06-10-01 . FABRICATED FILLER AND DOUBLERS IAW DC8 SRM 53-2-1, ALODINED AND PRIMED IAW DC8 SRM 51-1- 8, INSTALLED FILLER AND DOUB LERS IAW DC8 SRM 51-1-20D AND 51-1-21, CONFIRMED CRACK REMOVED IAW HFEC IAW 06-10-01, CLOSED UPPER AND LOWER SIDEWALL PA NELS IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2003041600308 20030416 00308 WP 2003 4 16 UPS03840085 1 20021228 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, AFT PIT SEAT TRACK CORRODED AROUND CLIPNUTS. NUT PLATES IN SEVERAL ARE AS STA 980 TO 1260. REMOV ED DAMAGE SEAT TRACK. INSTALLED NEW TRACK AND UPS SPLICE PARTS IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2003041600309 20030416 00309 WP 2003 4 16 UPS03840081 1 20021228 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, LOWER EXTERIOR FUSELAGE AT STA 1690 BOTTOM AREA SKIN SIGN OF BULGING. CORRODED BEYOND LIMITS IAW DC8 SRM 53-2-0, REMOVED DAMAGED SKIN, FABBED NEW SKIN SECTION IAW DGIS DWG 5649329. ALODINED AND PRIMED IAW DC8 SRM 51 -1-8, INSTALLED NEW SKIN SECTION IAW DGIS DWG 5649329 AND DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2003041600310 20030416 00310 WP 2003 4 16 UPS03840028 1 20021228 A 5754 RIB DOUG DC8 DC871F 302199D WP RT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE: C2, RT LEADING EDGE RIB REPAIR DOUBLER IS CRACKED AT XFS 385.25. REMOVED DOUBLER, FABRICATED AND INST ALLED REPLACEMENT DOUBLER IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2003041600311 20030416 00311 WP 2003 4 16 UPS03840032 1 20021229 A 5751 AILERON DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE: C2, LT WING OUTBOARD AILERON L/E UPPER SKIN IS CRACKED AT XA 684. REMOVED, FABRICATED AND REPLACED SK IN SECTION IAW SRM 57-8-0 FIG 4. 2 L 7 4 4F RT 4A25 2003041600313 20030416 00313 WP 2003 4 16 UPS03840084 1 20021229 A 5320 FITTING DOUG DC8 DC873F 302199F WP TORQUE BOX CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, ALC STA 1400 L33R FITTING UNDER TORQUE BOX WEB CORRODED. REMOVED AND REPLACED FITTING IAW DC8 SR M 51-1-20D. 2 L 7 4 4F RT 4A25 2003041600314 20030416 00314 WP 2003 4 16 UPS03840073 1 20021229 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, INT CABIN CANTED FRAME AFT OF 1710 FRAME DEEP CHAFE ON TRIPLER LONG 29L. INSTALLED DOUBLER ON FR AME IAW UPS DWG DC8-53A-011 AND EO DC8-5310-1 1728-A. 2 L 7 4 4F RT 4A25 2003041600318 20030416 00318 WP 2003 4 16 UPS03840082 1 20021230 A 5240 PANEL DOUG DC8 DC873F 302199F WP SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, R2 AFT SERVICE DOOR HAS CRACK INDICATION AT LOWER AFT CORNER FOUND BY RADIOGRAPHIC INSPECTION. R EMOVED AND ROUTED OUT CRACK IN DOOR PAN. FABBED REPAIR IAW DC8 SRM 53-2-0 AND DAC DWG 5772789. REINSTALLED DOOR PAN ST OPS, AND GUIDES IAW DC8 SRM 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 2003041600321 20030416 00321 WP 2003 4 16 UPS03840077 1 20021231 A 5310 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, AFT FUSELAGE SECTION STA 1690 PRODUCTION RING IS CORRODED BETWEEN L2 6L-L28L. REMOVED AND REPLAC ED SPLICES AND RING ANGLE SECTION AT L26R, L26L, L34L, & L28R DUE TO CRACKED AND CORRODED IAW DC8 SRM 53-2-5 FIG 8C-1 SH T 1, 51-1-20D, & DAC DWG 5612141. 2 L 7 4 4F RT 4A25 2003041600322 20030416 00322 WP 2003 4 16 UPS03840086 1 20021231 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, MAIN CABIN BEAR TRAP LOCATION SEAT TRACK -D- STA 1219 SCOLLOPS WORN. REMOVED AND REPLACED TRACK SECTION AND SPLICED PER UPS EO DC8-5320-5 167-C. 2 L 7 4 4F RT 4A25 2003041600323 20030416 00323 WP 2003 4 16 UPS03840075 1 20021231 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, MAIN CABIN BEAR TRAP LOCATION SEAT TRACK -E- STA 596 WORN. REMOVED AND REPLACED TRACK SECTION IA W DC8 EO-5320-5167-C. 2 L 7 4 4F RT 4A25 2003041600334 20030416 00334 SO 2003 4 16 SIMA200233802 1 20021122 A 5315 14521721009 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 735TS 145386 ABI - DURING AN MBV INSPECTION, THE CENTER SECTION OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. R EMOVED DAMAGED 15.25 BY 21.25 SECTION OF THE FORWARD DIGITAL BY CUTOUT. FABRICATED A REPLACEMENT FORWARD DIGITAL CENTER SECTION. FABRICATED TWO DOUBLERS AND SHIMS AND REPAIRED IAW EMB 145 (SRM 145/1142, CHAPTER 53, REV 20) 53-21-10 PARA 4 , AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2003041500108 20030415 00108 2003 4 15 YENA200234 4 20021212 A 2565 INDICATOR AIRBUS 320 A320232 3930326 EU OVRWING SLIDE INOPERATIVE A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 510JB 1280 RT OVERWING SLIDE ARMED INDICATION INOP. PLACED ON MEL 25-60-04. CLEANED PROX SWITCH. OPS CHECK GOOD IAW AMM 25-60-00 . 2 L 7 2 4F RT A28NM 2003041500117 20030415 00117 NE 2003 4 15 XNOA10196 2 20021221 A 7200 ENGINE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 2 STALLED A XN0A A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 23 224KW 073 DURING DESCENT 12,000 FT NR 2 ENG BEGAN TO COMPRESSOR STALL. FUEL FLOW NORMAL. EGT ENG STABLE AT IDLE POSITION. INSPE CTED NR 2 ENG MAIN FUEL FILTER, NO DEFECTS NOTED. INSPECTED NR 2 ENG FUEL PUMP STRAINER, NORMAL AND NO DEFECTS NOTED. INSPECTED NR 2 ENG VSVS, NO DEFECTS. INSPECTED VBVS, NO DEFECTS NOTED. PERFORMED STALL INSPECTION IAW A300 MM 72-00-00 PG 628. REMOVED AND REPLACED NR 2 ENG IP CHECK VALVE. OPS CHECK NORMAL IAW A300 MM 71-00-00. 2 L 7 2 4F 4 F RT A35EU E23EA 2003041500118 20030415 00118 NM 2003 4 15 XNOA01097 1 20021223 A 2611 SMOKE DETECTOR BOEING 727 727227 1384078 NM CARGO BAY INOPERATIVE A XN0A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 793A 20774 IN FLIGHT, LOWER AFT CARGO FIRE LIGHT ILLUMINATED. PERFORMED EMERGENCY PROCEDURE. SYSTEM PREVIOUSLY DEFERRED. REF DMI 2889 AFT LOWER CARGO SMOKE DETECTION INOP. 2 L 7 3 4F A3WE 2003041500120 20030415 00120 EA 2003 4 15 SWIA200211596 1 20021216 A 4997 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU DAMAGED A SWIA F O ACTIVATE FIRE EXT. OTHER N FALSE WARNING AP APPROACH 1 NM 07 413SW 7102 STARTED APU ON APPROACH AND RECEIVED A DOOR INHIBIT MESSAGE, BUT APU STILL STARTED. SHUTDOWN APU AND RECEIVED APU FIRE MESSAGE. FIRED THE FIRE BOTTLE. FOUND TB202 BLOCK 9 INTERMITTANT. REPLACED TB 202 BLOCK 9. REINSTALLED WIRES INTO BL OCK IAW WM 49-60-00. DUE TO INADVERTANT MECHANIC ACTION, DAMAGED MANY WIRES IN JUNCTION BOX 5. REMOVED AND REPLACED AL L DAMAGED WIRING AND CB B1 IAW WM 24-60-00. APU DOOR AND APU OPS CHECK GOOD IAW MM 49-10-00. FIRE BOTTLE AND SQUIB REP LACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2003041500121 20030415 00121 SO 2003 4 15 SWIA200211597 1 20021217 A 3297 WIRE HARNESS EMB 120 EMB120 3260201 SO LT MLG MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 190SW 120050 ON TAKEOFF COULDN'T GET THE LANDING GEAR TO GO UP. ALL THE LIGHTS WOULD BE ON BUT THE LEFT RED A. RETURNED TO FAT. RE MOVED AND REPLACED LEFT MAIN GEAR A-PROXIMITY HARNESS IAW 32-61-01. OPS CHECK GOOD, LEAK CHECK OF VALVE IS GOOD. 2 L 7 2 4T RT A31SO 2003041500140 20030415 00140 2003 4 15 SWIA200211620 4 20021222 A 3425 RELAY EMB 120 EMB120ER 3260203 SO HSI MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 188SW 120039 FIRST OFFICER'S EHSI WENT BLANK ON TAKEOFF GOING THROUGH 500 FT. RETURNED TO SFO. INSTALLED KNOWN SERVICEABLE RELAYS A T K0394 AND K0396. NR 2 EHSI SCREEN REMAINED UNAFFECTED BY AUX GENERATOR POWER TRANSFERS. HEADING INDICATION CHECKS GO OD. 2 L 7 2 4T RT A31SO 2003041500146 20030415 00146 SO 2003 4 15 SWIA200211627 1 20021209 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO LT NACELLE FLAP MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 227SW 5726 5726 120304 DISAGREEMENT MESSAGE WHEN FLAPS ARE RETRACTED FROM 45 DEGREE FLAPS, DISAGREEMENT FIX THEMSELVES ON TAXI. INSTALLED SERV ICEABLE NACELLE FLAP ACTUATOR ON LEFT SIDE. OPS CHECKS GOOD. PERFORMED IAW MM 27-50-00. 2 L 7 2 4T RT A31SO 2003041500166 20030415 00166 SO 2003 4 15 SWIA200211652 1 20021112 A 5414 SKIN EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 LEFT NACELLE OUTBOARD SIDE JUST AFT OF FRAME 3 FORWARD HOOK FOR FORWARD COWL DOOR LATCH NACELLE IS CRACKED WHERE AFT PAR T OF THE LATCH HOOK GOES INTO THE NACELLE. FOUND DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED REINFORCEMENT PL ATE IAW EMB120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2003041500168 20030415 00168 SO 2003 4 15 SWIA200211654 1 20021112 A 5320 SUPPORT EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 COCKPIT LEFT SIDE LOWER SUPPORT FOR SIDE VIEW WINDOW, NEAR SIDE POST, IS CRACKED. FOUND DURING C-CHECK INSPECTION. REM OVED AND REPLACED LEFT SIDE LOWER SUPPORT IAW SRM 51-40-02 & 51-00-00. P/N: 120-34535-005. 2 L 7 2 4T RT A31SO 2003041600011 20030416 00011 EA 2003 4 16 SWIA200211673 1 20021210 A 2841 73664310 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FUEL QTY MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 407SW 7034 BOTH FUEL QUANTITY AND TOTAL FUEL FAILED AFTER TAKEOFF. RETURNED TO SLC. FUEL CHANNEL 1 FAIL STATUS MESSAGE. LEFT QUA NTITY CAME BACK ON AFTER 2 MINUTES. REMOVED AND REPLACED FUEL QUANTITY COMPUTER PER MM 28-41-16. OPS CHECK GOOD. P/N: 736643-10 S/N OFF: 156 S/N ON: 192. 2 L 7 2 4F RT A21EA 2003041600063 20030416 00063 WP 2003 4 16 AALA20021753 1 20021122 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND DAMAGE ON FORMER AT STATION 522 BETWEEN L20R AND L21R. INSTALLED FORMER REPAIR SPLICE PER SRM 53-03-00 FIG 3. (M) 2 L 7 2 4F A6WE 2003041600078 20030416 00078 WP 2003 4 16 AALA20021756 1 20021121 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND AFT GIRT BAR SUPPORT BRACKET HAS CORROSION UNDER BRACKET ON CUSP AFT SERVICE DOOR. INSTALLED DOUBLER PER 53 -01-00 SRM PAGE 18. (M) 2 L 7 2 4F A6WE 2003041600082 20030416 00082 WP 2003 4 16 AALA20021759 1 20021118 A 5347 5930565561 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND CORROSION IN NR 3 SEAT TRACK AT APPROX STATION 1304. REMOVED CORRODED AREA AND INSTALLED SEAT TRACK PLUG. REPAIR PER 53-20-00-10. (M) 2 L 7 2 4F A6WE 2003041600096 20030416 00096 WP 2003 4 16 AALA20021770 1 20021127 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND CORROSION ON VERTICAL AND HORIZONTAL LEGS OF DOOR BEAM. REMOVED AND REPLACED DOOR BEAM AARD 53-10-00-3. (M ) 2 L 7 2 4F A6WE 2003041600101 20030416 00101 NM 2003 4 16 AALA20021800 1 20021214 A 2121 6067723 FAN BOEING 757 757223 1384957 NM CABIN OVERHEATED A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 684AA 25341 ORD - FLT 288 - EN ROUTE OAK-JFK - AT FLIGHT LEVEL 410, FLIGHT ATTENDANT REPORTED BURNING SMELL AND HAZE NEAR READING LI GHTS THROUGHOUT CABIN. RIGHT AFT LAVATORY SMOKE DETECTORS STARTED CHIMING. EMERGENCY WAS DECLARED AND THE AIRCRAFT DIV ERTED TO ORD WITHOUT INCIDENT. FOUND RIGHT CABIN AIR RECIRCULATION FAN OVERHEATING. REPLACED RECIRCULATION FAN. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003041600122 20030416 00122 NM 2003 4 16 AALA20021877 1 20021220 A 3350 STRIP BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 675AN 29425 ALT - DURING OVERNIGHT MAINTENANCE EMERGENCY ESCAPE PATH LIGHTING STRIP LOOSE AT ROW 14. REATTACHED STRIP AT ROW 14. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003041600124 20030416 00124 2003 4 16 AALA20021879 4 20021226 A 2312 285N002836 CIRCUIT CARD BOEING 757 757223 1384957 NM E/E BAY FAULTY A AALA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 614AA 24490 KIN - FLT 1735 - EN ROUTE MIA-KIN, AFT CARGO LIGHT ILLUMINATED. CARGO FIRE BOTTLE DISCHARGED AND AFT CARGO FIRE LIGHT W ENT OUT AFTER APPROXIMATELY ONE MINUTE. AIRCRAFT LANDED IN KIN WITHOUT INCIDENT. REPLACED FIRE LOGIC CARD, FIRE BOTTLE S AND SQUIB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003041600143 20030416 00143 WP 2003 4 16 AALA20030027 1 20021212 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 580AA 53157 TUL - FOUND NR 2 SEAT TRACK HAS CORROSION AT STATION 1300. REPAIRED PER SRM 53-05 FIG 4A AND AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2003041600296 20030416 00296 EA 2003 4 16 SWIA200211721 1 20021212 A 5510 FITTING CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 ANTI-ROTATION FITTING HAS CORROSION. FOUND DURING C-CHECK INSPECTION. ANTI-ROTATION FITTING REPLACED IAW SB 601R-55-00 7. P/N: 600-21073-7. 2 L 7 2 4F RT A21EA 2003041600305 20030416 00305 WP 2003 4 16 UPS03840062 1 20021227 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE: C2, STA 70 LONGERON 30R IS CRACKED AT END FITTING. TRIMMED OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTO UT. FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE IAW SAA SK 701-098. 2 L 7 4 4F RT 4A25 2003041600324 20030416 00324 WP 2003 4 16 UPS03840087 1 20021231 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, MAIN CABIN SEAT TRACK -E- GOUGED AT FS 220. REMOVED DAMAGE SEAT TRACK, REPLACED WITH NEW TRACK A ND UPS SPLICES IAW UPS EO DC8-5320-5167-C & DC8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2003041600336 20030416 00336 SO 2003 4 16 SIMA200233803 1 20021120 A 5313 STRINGER EMB 135 EMB135LR 3260305 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 735TS 145386 ABI - DURING AN MBV INSPECTION, STRINGER 19R WAS FOUND TO BE CHAFED AT JUNCTION 05. BLENDED CHAFED AREA. PERFORMED EDD Y CURRENT INSPECTION NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142, C HAPTER 53, REV 19) 53-24-02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2003041600341 20030416 00341 SO 2003 4 16 SIMA200233805 1 20021102 A 5320 14521725013 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 ABI - A LEVEL 2 FINDING WAS FOUND DURING IMBV INSPECTION REFERENCE CRIC NR 28015, FORWARD DIAMOND GUSSET CORRODED. REMO VED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-06 AND 51-20-03. (M) 2 L 7 2 4T RT T00011AT 2003041600342 20030416 00342 SO 2003 4 16 SIMA200233806 1 20021102 A 5320 14522400013 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 ABI - A LEVEL 2 FINDING WAS FOUND DURING IMBV INSPECTION REFERENCE CRIC NR 28016, CENTER BEAM GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE CENTER BEAM IAW EMB 145 SRM 51-40-02, 51-40-02 AND 51-20-03. (M) 2 L 7 2 4T RT T00011AT 2003041600351 20030416 00351 SO 2003 4 16 SIMA200233810 1 20021102 A 5320 14524131005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 ABI - A LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 28025, FORWARD PASSENGER DOOR FLOOR SUPPOR T CORRODED. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW EMB 145 SRM 51-40-02, 51-20-03, 51-40-06. (M) 2 L 7 2 4T RT T00011AT 2003041600358 20030416 00358 SO 2003 4 16 SIMA200233811 1 20021102 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 ABI - A LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 28014, RIGHT FORWARD SILL CORRODED. REMOV ED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003041600362 20030416 00362 SO 2003 4 16 SIMA200233812 1 20021122 A 5313 14533897005 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 ABI - STRINGER 19L WAS FOUND TO BE CHAFFED BEYOND SRM LIMITS AT SKIN JUNCTION 05. BLENDED CHAFED AREA. PERFORMED AN ED DY CURRENT INSPECTION OF THE BLENDED AREA. NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW E MB 145 SRM (145/1142, CHAPTER 53, REV 20) 53-24-02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2003041600364 20030416 00364 SO 2003 4 16 SIMA200233813 1 20021125 A 5315 14521721009 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 ABI - DURING AN IMBV INSPECTION, A PREVIOUS REPAIR OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. R EMOVED DAMAGE PREVIOUS REPAIR SECTION OF THE FORWARD DIGITAL. FABRICATED A REPLACEMENT STRAP AND TWO DOUBLERS. REPAIR D ONE IAW EMB-145 (SRN-145/1142, CHAPTER 53, REV 20) 53-21-10 PARA 4 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2003041600008 20030416 00008 EA 2003 4 16 SWIA200211670 1 20021226 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 07 916SW 7634 FLAPS FAILED AT -0- WHEN SELECTED TO 8 DEGREES ON DESCENT. CLEARED FAULTS FROM FECU. CYCLED FLAPS SEVERAL TIMES. NO F AULTS FOUND. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2003041600009 20030416 00009 EA 2003 4 16 SWIA200211671 1 20021228 A 5270 864808 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 412SW 6519 6469 7101 PASSENGER DOOR LATCH CAUTION MESSAGE AFTER TAKEOFF. FOLLOWED QRH NO PRESSURIZATION PROBLEMS. CONTINUED TO GSO. CLIMBI NG THROUGH 20,000 PASSENGER DOOR WARNING. STILL NO PRESSURE PROBLEMS. RETURNED TO DFW. AFTER LEVELING AT 11,000 COMIN G BACK TO DFW, DOOR WARNING BECAME PAX DOOR LATCH WITH DIFFERENTIAL 4.6. CAUTION MESSAGE CLEARED AFTER LANDING. FOUND MDC FLAGGED PSEU. REMOVED AND REPLACED PSEU IAW CL600 MM 32-61-01. PRESSURIZED AIRCRAFT ON GROUND WITH NO DOOR INDICAT ION. NO FURTHER FAULTS IN MDC. SYSTEM OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2003041600013 20030416 00013 EU 2003 4 16 PNSA021201 1 20021213 A 3020 SWITCH SAAB SF340 340B 7860101 EU ANTI ICE VALVE OUT OF ADJUST A PNSA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 685PA 340B212 LT AIR VALVE LIGHT ILLUMINATED ON TAXI OUT. CREW RETURNED TO GATE. MX ADJUSTED SWITCH ON VALVE PER CT7 MM AND OPS CHEC K NORMAL. 2 L 7 2 4T RT A52EU 2003041600033 20030416 00033 WP 2003 4 16 AALA20021728 1 20020912 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - FOUND SUBFLOOR UNDER G1 GALLEY HAS CORROSION. SUBFLOOR UNDER G1 GALLEY IS SCRATCHED, GOUGED, AND DENTED. REMOVED CORROSION. FABRICATED AND INSTALLED DOUBLER PER AARD 53-00-00-02. BLENDED OUT DAMAGE. (M) 2 L 7 2 4F A6WE 2003041600041 20030416 00041 WP 2003 4 16 AALA20021734 1 20021125 A 5345 MOUNT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - FOUND CORROSION, G1 FORWARD INBOARD FLOOR TIE DOWN. REMOVED AND REPLACED TIE DOWN. (M) 2 L 7 2 4F A6WE 2003041600043 20030416 00043 WP 2003 4 16 AALA20021738 1 20021204 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND CRACK ON SKIN STATION 1380 L14R. STOP DRILL, CRACK AND INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3. (M) 2 L 7 2 4F RT A6WE 2003041600051 20030416 00051 WP 2003 4 16 AALA20021743 1 20021112 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE WRINKLED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND 3 INCH WRINKLE ON EXTERNAL SKIN STATION 109, FORWARD OF LONGERON 25R. INSTALLED FILLER A DOUBLER PER SRM 53 -01-00 FIG 2 SHEET 3. (M) 2 L 7 2 4F A6WE 2003041600059 20030416 00059 WP 2003 4 16 AALA20021749 1 20021114 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND TWO DAMAGED HOLES IN FORWARD EDGE OF CUSP AT STATION 984. INSTALLED CUSP DOUBLER AT STATION 984 PER SRM 53- 01 FIG 4. (M) 2 L 7 2 4F A6WE 2003041600060 20030416 00060 WP 2003 4 16 AALA20021750 1 20021114 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND LONGERON 17L IS CRACKED AT STATION 408. CUT OUT DAMAGED SECTION OF LONGERON. INSTALLED LONGERON SPLICE REP AIR PER SRM 53-02-00. (M) 2 L 7 2 4F A6WE 2003041600075 20030416 00075 WP 2003 4 16 AALA20021754 1 20021125 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND CRACK IN FUSELAGE SKIN .375 INCH LONGERON FROM RIVET HEAD AT STATION 1380 L13R. STOP DRILLED CRACK, DYE CHE CKED AND INSTALLED DOUBLER PER SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2003041600081 20030416 00081 WP 2003 4 16 AALA20021758 1 20021118 A 5313 527779485 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND L4L STATION 160 HAS CRACK AROUND FASTENER. FABRICATED AND INSTALLED LONGERON SECTION AND SPLICE PER SRM 53- 02-00 PAGE 48. (M) 2 L 7 2 4F A6WE 2003041600097 20030416 00097 WP 2003 4 16 AALA20021773 1 20021119 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 TUL - FOUND CORROSION BEYOND MANUAL LIMITS. SPLICE NEW SECTION OF SEAT TRACK NR 6 SRM PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2003041600099 20030416 00099 WP 2003 4 16 AALA20021797 1 20021205 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 563AA 49345 SEA - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY DOOR PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD ENTR Y DOOR PORTABLE EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2003041600100 20030416 00100 WP 2003 4 16 AALA20021798 1 20021204 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 552AA 53034 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-175/155-152 DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003041600126 20030416 00126 WP 2003 4 16 AALA20021885 1 20021230 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7526A 49918 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY CEILING EXIT LIGHTS AT ROW 27-31 INOPERATIVE. RESEATED EMERGENCY EXIT LIG HT BATTERY CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003041600127 20030416 00127 WP 2003 4 16 AALA20021886 1 20021229 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 296AA 49308 DFW - DURING OVERNIGHT MAINTENANCE, AFT CABIN EMERGENCY EXIT LIGHTS DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003041600316 20030416 00316 WP 2003 4 16 UPS03840017 1 20021229 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C2, ALL STA 1400 L30R FITTING UNDER TORQUE BOX WEB CORRODED. REMOVEED CORRODED FITTING IAW DC8 SRM 51 -1-21. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2003041600367 20030416 00367 SO 2003 4 16 SIMA200233814 1 20021127 A 5315 14522463001 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 DURING AN IMBV INSPECTION CORROSION AS FOUND ON A PREVIOUS REPAIR TO THE LEFT OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR AND INSPECTED THE UNDERLYING BEAM. NO ADDITIONAL DAMAGE NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS AND PLATE. REPAIR DONE IAW EMB 145 SRM (145/1142, CHAPTER 53, REV 20) 53-21-10 PARA 2, FIG 201 SHEET 1, AND STANDARD SR M PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2003042800052 20030428 00052 NM 2003 4 28 OZIA200343003 1 20021231 A 5313 001A535B6015 LONGERON DORNER DO32 DO328300 NM PWA 306 PW306B NE FUSELAGE CORRODED A OZIA K NONE O OTHER IN INSP/MAINT 1 CE 05 430Z 6656 3127 BAGGAGE COMPARTMENT LONGERON CORRODED. 2 H 7 2 4T 4 F RT A55NM E35NE 2003042500078 20030425 00078 SO 2003 4 25 ZLW2003F00001 1 20021211 A 5751 STRUCTURE GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY511* 54523 EU LT AILERON CORRODED E ZLWA O OTHER O OTHER NR NOT REPORTED 1 SW 15 622RR 11453 12 ON 12-11-2002, A STATIC WICK BASE WAS NOTED TO BE LOOSE ON THE LEFT AILERON. THE STATIC WICH BASE WAS REMOVED AND CORRO SION WAS FOUND BENEATH IT. AFTER BLENDING OUT THE CORROSION, IT WAS NOT TO BE OUT OF MFG LIMITS. 2 L 7 2 4F 4 F RT A12EA E2EU 2003042800051 20030428 00051 NM 2003 4 28 OZIA200343002 1 20021231 A 5310 001A535B6018200 SILL DORNER DO32 DO328300 NM PWA 306 PW306B NE CARGO DOOR CORRODED A OZIA K NONE O OTHER IN INSP/MAINT 1 CE 05 430Z 6656 3127 BAGGAGE COMPARTMENT DOOR SILL, AT THE FLOORBOARD, ATTACH HOLES CORRODED. 2 H 7 2 4T 4 F RT A55NM E35NE 2003042800057 20030428 00057 NM 2003 4 28 OZI2003F00002 1 20021231 A 5310 001A535B6018200 SILL DORNER DO32 DO328300 NM ZONE231 CORRODED A OZIA O OTHER O OTHER NR NOT REPORTED 1 SW 07 430Z 3127 BAGGAGE COMPARTMENT DOOR SILL, AT THE FLOORBOARD ATTACH HOLES CORRODED. 2 H 7 2 4T RT A55NM 2003042800054 20030428 00054 NM 2003 4 28 KPVA200243 1 20021225 A 3350 101095102 LENS DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE EXIT SIGN DISLODGED A KPVA O OTHER O OTHER NR NOT REPORTED 1 WP 13 805WP 353 EXIT SIGN FELL OFF. RESECURED EXIT SIGN OVER GALLEY BY PUSHING INTO POSITION. SECURITY CHECK OF INSTALLATION GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2003042900091 20030429 00091 CE 2003 4 29 Q2A2003F00000 1 20021113 A 5740 FITTING BEECH 90 E90 1152914 CE PWA R2800 R2800* 52026 NE LT WING CRACKED B Q2AR K NONE O OTHER IN INSP/MAINT 1 SW 17 77WF 8633 LW4 WHILE PERFORMING NDT INSPECTION OF WING ATTACH FITTINGS, LEFT LOWER FORWARD FITTING FOUND CRACK IN RADIUS OF BOLT HOLE. SPAR WAS THEN REPLACED. 1 L 7 2 3T 4 R 3A20 5E8 2003042800055 20030428 00055 NM 2003 4 28 OZI2003F00000 1 20021231 A 5313 001A535B6015 LONGERON DORNER DO32 DO328300 NM LT CARGO COMPT CORRODED A OZIA O OTHER O OTHER NR NOT REPORTED 1 SW 07 430Z 6656 3127 BAGGAGE COMPARTMENT LONGERON CORRODED. 2 H 7 2 4T RT A55NM 2003042900233 20030429 00233 SO 2003 4 29 P8L2003F00000 1 20021203 A 2720 4004009 TORQUE TUBE PIPER PA31 PA31325 7103105 SO LYC O540 TIO540* 41532 EA RUDDER CORRODED E P8LA O OTHER O OTHER NR NOT REPORTED 1 GL 25 4503L 6224 318012031 WHILE COMPLYING WITH SB (RUDDER TORQUE TUBE INSPECTION), RUST WAS FOUND ON THE INTERIOR AND EXTERIOR OF THE TORQUE TO BE INSIDE AND OUTSIDE THE RUDDER. THIS PROBLEM MAY HAVE BEEN PREVENTED WITH BETTER INTERNAL AND EXTERNAL PAINT AND RUST C ONTROL. DRAIN HOLES WOULD HAVE HELPED IN THE LOWER RUDDER RIBS. 1 L 7 2 3O 3 O A20SO E14EA 2003042900199 20030429 00199 NM 2003 4 29 CA030411001 1 20020327 A 2612 BACC45ZT18A31P6 CONNECTOR BOEING 727 727217 1384061 NM PWA JT8 JT8D17 52049 NE FIRE DETECTION SHORTED W O OTHER O OTHER LD LANDING 1 CA (CAN) AILERION, SPOILER SHUT OFF VALVE, WHEEL WELL FIRE DETECTION AND PACK COOLING FAN CIRCUIT BREAKERS TRIPPED AFTER LA NDING. FOUND CONNECTOR RECEPTACLE D4658J AT BS 870 (LEFT OF KEELBEAM IN AIR CONDITIONING BAY) SHORTED. REPLACED CONNECTO R IAW STANDARD PRACTICES. 2 L 7 3 4F 4 F RT A3WE E2EA 2003043000233 20030430 00233 SO 2003 4 30 P8L2003F00001 1 20021202 A 2720 4004009 TORQUE TUBE PIPER PA31 PA31325 7103105 SO LYC O540 TIO540* 41532 EA RUDDER CORRODED E P8LA O OTHER O OTHER NR NOT REPORTED 1 GL 25 407TJ 6325 317512069 WHILE COMPLYING WITH SB 1105 (RUDDER TORQUE TUBE INSPECTION), RUST WAS FOUND ON THE INTERIOR AND EXTERIOR OF THAT PORTIO N OF THE TUBE LOCATED INSIDE THE RUDDER. THIS MAY HAVE BEEN PREVENTED BY BETTER VENTILATION OF THE RUDDER IN THAT AREA. (DRAIN HOLES), AND BETTER PAINT AND INTERNAL CORROSION CONTROL INTERNALLY IN THE TUBE. 1 L 7 2 3O 3 O A20SO E14EA 2003043000046 20030430 00046 NM 2003 4 30 2003UALA00393 1 20021224 A 2710 113W70031 ATTACH FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ACTUATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 773UA 26929 2 CRACKED ACTUATOR FITTINGS. REPLACED BOTH INBOARD AND OUTBOARD FITTINGS 2 L 7 2 4F 4 F RT T0001SE E46NE 2003050100003 20030501 00003 WP 2003 5 1 AALA20021807 1 20021210 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 205AA 49155 TUL - FOUND SKIN STATION 1380 ABOUT L14R HAS CRACK. INSTALLED DOUBLER PRE SRM 53-01 FIG 2 AND AARD 53-30-00-02. (M) 2 L 7 2 4F A6WE 2003050100014 20030501 00014 WP 2003 5 1 AALA20021806 1 20021210 A 5330 SKIN DOUG DC9 DC982 3022082 WP VERTICAL STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 205AA 49155 TUL - FOUND VERTICAL STAB SKIN CRACKED RIGHT UPPER CORNER OF AIR INLET, FS 1388. INSTALLED DOUBLER REPAIR PER SRM 55-01 -00 FIG 2 SHEET 2. (M) 2 L 7 2 4F A6WE 2003050100022 20030501 00022 WP 2003 5 1 AALA20021774 1 20021121 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1235-1239. CORROSION REMOVED PER SRM 51-10-3, CORROSION REMOVED BEYOND LIM ITS. A NEW SEAT TRACK WAS INSTALLED STATION 1174-1309 FREEZE PLUG INSTALLED AND GALLEY MOUNT PER AMM 53-40-01. (M) 2 L 7 2 4F A6WE 2003050100031 20030501 00031 WP 2003 5 1 AALA20030063 1 20021216 A 5347 GALLEY TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 458AA 49563 TUL - FOND GALLEY TIE DOWN TRACK CORRODED AT STATION 207 INBOARD OF NR 4 SEAT TRACK. REMOVED AND REPLACED TIE DOWN FITT ING AT STATION 207 INBOARD OF NR 4 SEAT TRACK AS PER 51-01. (M) 2 L 7 2 4F A6WE 2003050100033 20030501 00033 WP 2003 5 1 AALA20021909 1 20021219 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND DENT AND CREASE IN FUSELAGE SKIN AT STATION 21, L18 TO L19 LEFT. COLD WORKED DENT AND DYE CHECKED. NO CRAC KS FOUND. INSTALLED .063 INCH 7075-T6 ALUMINUM EXT DOUBLER PER AARD 53-30 PAGE 1 REF 53-04 FIG 38 AND FIG 12B. (M) 2 L 7 2 4F A6WE 2003050100034 20030501 00034 WP 2003 5 1 AALA20030020 1 20021230 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND CRACK IN CANT FRAME, FS 1474. INSTALLED DOBLER PER ESO 80559 DATED 12-27-02. (M) 2 L 7 2 4F A6WE 2003050100036 20030501 00036 WP 2003 5 1 AALA20021914 1 20021216 A 5320 CHANNEL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND FLOORBOARD SUPPORT CHANNEL BETWEEN NR 2 AND NR 3 SEAT TRACK AT STATION 254 CORRODED. REPLACED SUPPORT CHANN EL WITH NEW CHANNEL PER SRM 51-00-00. (M) 2 L 7 2 4F A6WE 2003050100041 20030501 00041 WP 2003 5 1 AALA20021907 1 20021217 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND CUSP CRACKED OUTBOARD OF SEAT TRACK NR 1, FORWARD OF STATION 1309, APPROX 6 INCHES. CORROSION ON CUSP BETWE EN SEAT TRACK NR 1 AND NR 2 JUST FORWARD OF STATION 1309. OLD CUSP, REMOVED AND REPLACED WITH NEW CUSP MATERIAL, STAITO N 1250-1309. (M) 2 L 7 2 4F A6WE 2003050100047 20030501 00047 WP 2003 5 1 AALA20021799 1 20021209 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 489AA 49682 TUL - FOUND CRACK IN SKIN IN TWO PLACES AROUND RIVET STATION 1380 BETWEEN LONGERON 16 AND 17L. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3. (M) 2 L 7 2 4F A6WE 2003050100048 20030501 00048 WP 2003 5 1 AALA20021771 1 20021205 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 289AA 49301 TUL - FOUND .25 INCH CRACK, FS 1380. INSTALLED DOUBLER PER SRM 53-01-00 AND AARD 53-30-02. (M) 2 L 7 2 4F A6WE 2003050100049 20030501 00049 WP 2003 5 1 AALA20030022 1 20021211 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND CORROSION INSIDE SEAT TRACK NR 1, BEYOND MANUAL LIMITS, TRACK EAR TOO THIN. INSTALLED PLUGPER AARD 53-20-00 -10, REPAIR NR 10. (M) 2 L 7 2 4F A6WE 2003050100050 20030501 00050 WP 2003 5 1 AALA20030023 1 20021212 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND CORROSION ON NR 1 SEAT TRACK AT STATION 672. INSTALLED SEAT TRACK PLUG PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2003050100053 20030501 00053 WP 2003 5 1 AALA20021908 1 20021215 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND FRAME CRACKED AT STATION 1174 LONGERON 6L IN VERTICAL LEG. INSTALLED DOUBLER PER AARD 53-10-00-30. (M) 2 L 7 2 4F A6WE 2003050100054 20030501 00054 WP 2003 5 1 AALA20021913 1 20021212 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND LONGERON NR 2 LEFT SIDE CRACKED AT ATTACH RADIUS. INSTALLED LONGERON SPLICE AT STATION 148-172 PER SRM 53-0 2-00, FIG 18. (M) 2 L 7 2 4F A6WE 2003050100055 20030501 00055 WP 2003 5 1 AALA20021910 1 20021217 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND CORROSION ON CUSP BETWEEN STATION 700-712 RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2003050100056 20030501 00056 WP 2003 5 1 AALA20021911 1 20021217 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND CUSP CRACKED AT FASTENER HOLE STATION 712 RIGHT. INSTALLED DOUBLER PRE AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2003050100057 20030501 00057 WP 2003 5 1 AALA20021912 1 20021218 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND FUSELAGE SKIN HAS TWO SMALL CRACKS, APPROX .050 INCH LONG EACH, AT RIVET THROUGH SKIN AND SHEAR TIE ABOVE LO NGERON 14R AT STATION 1380. INSTALLED DOUBLER PER SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2003050100060 20030501 00060 WP 2003 5 1 AALA20021708 1 20021120 A 5320 CHANNEL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 TUL - FOUND CORROSION ON FLOOR CHANNEL STATION 148-162 RBL 8-12. REMOVED AND REPLACED FLOOR CHANNEL AT STATION 148-162 RBL 8-12 SRM 51-01. (M) 2 L 7 2 4F A6WE 2003050100015 20030501 00015 WP 2003 5 1 AALA20030019 1 20021220 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND CORROSION ON VERTICAL AND HORIZONTAL LEGS, AREA HAD PREVIOUS DOUBLER INSTALLED. REMOVED AND REPLACED WITH N EW BEAM AND REINSTALLED ATTACHING PARTS IAW AARD 53-10-00-3 AND SRM 51-30-5 SHT 2 AND 51-30-2 FIG PAR 3. (M) 2 L 7 2 4F A6WE 2003050100051 20030501 00051 WP 2003 5 1 AALA20030024 1 20021218 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 458AA 49563 TUL - FOUND CRACK IN FUSELAGE SKIN EXTENDING FROM FASTENER HOLE LEFT SIDE STATION 1380 JUST ABOVE LONGERON 14L. REPAIRE D CRACK IN FUSELAGE LEFT SIDE STATION 1380 PER SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2003050100059 20030501 00059 WP 2003 5 1 AALA20021707 1 20021121 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 TUL - FOUND FS 1437 FRAME SHEAR TIE CRACKED AFT SIDE, JUST OUTBOARD OF LARGE TAIL TIE FITTING LEFT OF C/L. REMOVED AND REPLACED SHEAR TIE PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2003050100102 20030501 00102 WP 2003 5 1 AALA20021678 1 20021121 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 298AA 49310 TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET HEAD ABOVE PYLON STATION 1380, 6 INCHES ABOVE PYLON. STOP DRILLED CRACK. IN STALLED DOUBLER PER SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2003050100217 20030501 00217 NM 2003 5 1 2003F00246 1 20021106 A 2910 6517840409 LINE BOEING 727 72721 1384003 NM NR 2 SPOILER CRACKED A RYNA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 07 355QS 19257 IN LEVEL CRUISE FLIGHT FROM DAY TO PHX, COMPLETE LOSS OF 'A' SYSTEM HYDRAULICS. PERFORMED ALL RYAN 'A' SYSTEM HYDRAULIC LOSS CHECKLIST. EMERGENCY DECLARED. AIRCRAFT LANDED PHX WITHOUT INCIDENT. REMOVED AND REPLACED SPOILER RETURN LINE. (M) 2 L 7 3 4F A3WE 2003050100218 20030501 00218 NM 2003 5 1 2003F00247 1 20021029 A 2910 6517840112 LINE BOEING 727 72721 1384003 NM NR 2 SPOILER CRACKED A RYNA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 07 356QS 19258 ON DESCENT INTO RDU, SYSTEM PRESSURE WAS LOST ON 'A' SYSTEM HYDRAULICS. EMERGENCY WAS DECLARED AND EMERGENCY CHECKLIST WAS COMPLIED WITH. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 SPOILER ACTUATOR PRESSURE LINE. (M) 2 L 7 3 4F A3WE 2003050100058 20030501 00058 WP 2003 5 1 AALA20021737 1 20021201 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 439AA 49457 TUL - FOUND CRACK ON SKIN STATION 1380 L14L. STOP DRILLED CRACK TO APPLIED DOUBLER TO AREA SPECIFIED PER SRM 53-01 FIG 2. (M) 2 L 7 2 4F RT A6WE 2003050200012 20030502 00012 NE 2003 5 2 USAABB02005 2 20020111 A 7200 UL11802 PANEL BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE LOOSE A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 630AU 27808 31330 CLT - FLT 803 - AFTER TAKEOFF, CREW NOTED AND IRRITATING, OILY ODOR IN THE COCKPIT. THE ODOR DIMINISHED WHEN THE LT PAC K WAS SECURED, AND RETURNED WHEN THE PACK WAS OPERATED. THE LEFT PACK WAS SECURED FOR THE REMAINDER OF THE FLIGHT. MAI NTENANCE REPLACED THE LT ENGINE. TEAR DOWN OF THE ENGINE SHOWED THAT THE FRONT PANEL FLANGE OF THE 03 MODULE WAS WORN A ND THE RETAINING BOLTS HAD LOST THEIR TORQUE. THE ENGINE WAS REPAIRED TO SB 72-C247 SPECIFICATION. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2003050200013 20030502 00013 2003 5 2 USAABB02107 4 20020601 A 2565 D31041146 SLIDE BOEING 757 757225 1384959 NM L3 DOOR TORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 25474 22199 PHL - DURING AN SLIDE INFLATION OPERATIONAL CHECK ON THE L3 DOOR, THE SLIDE TORE IN THE THRESHOLD AREA. THE TEAR EMANAT ED FROM THE CENTER OF THE MATERIAL AND PROGRESSEDOUT TOWARD THE EDGES. THE EDGES OF THE SLIDE REMAINED INTACT. THE SLI DE INFLATED PROPERLY AND REMAINED ATTACHED TO THE AIRCRAFT. MAINTENANCE REPLACED THE SLIDE. THE VENDOR TEAR-DOWN REPOR T STATED THAT THE 'SLIDE EXHIBITED SEAM DEGRADATION.' IAW US AIRWAYS MAINTENANCE PROCEDURES, TWO MORE OF THIS SLIDE TYP E WERE DEPLOYED, USING SLIDES WITH COMPARABLE TOTAL TIMES. NO PROBLEMS WERE FOUND WITH THESE INFLATIONS. (M) 2 L 7 2 4F RT A2NM 2003050100010 20030501 00010 WP 2003 5 1 AALA20030018 1 20021211 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND LANDING WORN, RIGHT SIDE, ALONG FRAME 1380 FOR ARM DOOR. INSTALLED A DOUBLER PER AARD 53-10-00-34 PAGE 1 TO REPAIR A WEAR AREA WORN LESS THAN 50 PERCENT IN DEPTH. (M) 2 L 7 2 4F A6WE 2003050100023 20030501 00023 WP 2003 5 1 AALA20021772 1 20021205 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 289AA 49301 TUL - FOUND SKIN DAMAGED LEFT SIDE, FS 1380. INSTALLED DOUBLER PER SRM 53-01-00 AND AARD 53-30-02. (M) 2 L 7 2 4F A6WE 2003050100032 20030501 00032 WP 2003 5 1 AALA20021906 1 20021223 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND CORROSION ON TOP SURFACE. INSTALLED NEW WEB/SUPPORT STATION 1211 L29R TO L28L. (M) 2 L 7 2 4F A6WE 2003050100035 20030501 00035 WP 2003 5 1 AALA20030021 1 20021216 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 456AA 49561 TUL - FOUND CUSP CRACKED OUTBOARD OF NR 5 SEAT TRACK, FS 218-219. INSTALLED DOUBLER PER AARD 53-00-002. (M) 2 L 7 2 4F A6WE 2003050100101 20030501 00101 WP 2003 5 1 AALA20021689 1 20021124 A 5320 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 298AA 49310 TUL - FOUND CRACKED CANTED FRAME 1463 ATTACH ANGLE. REPAIRED PER 53-10-00-03. (M) 2 L 7 2 4F A6WE 2003050200088 20030502 00088 NM 2003 5 2 200271902 1 20020619 A 3242 C20508000 BRAKE ASSY BOEING 767 767300 1385204 NM MLG DRAGGING A FWTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 19 316LA 30842 AIRCRAFT IS NEW FROM FACTORY AT TAC 822 AND TAC 737 CHANGED NUMBER 1 AND 5 BRAKE ASSY FOR STUCK AND HOT. TEAR DOWN OF T HESE BRAKES REVEAL THAT ADJUSTER PINS WHERE CUT (SHEARED). THIS DID NOT ALLOW BRAKES TO PROPERLY RELEASE. BRAKE SERIAL NUMBERS 01705 AND 01706. 2 L 7 2 4F RT A1NM 2003050500079 20030505 00079 EU 2003 5 5 MALA030241 1 20020418 A 2110 MOTOR SAAB SF340 340B 7860101 EU COMPRESSOR FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 454XJ 340B454 SMOKE COMING FROM THE AVIONICS BAY ON FLIGHT 3306. MAINTENANCE REPLACED AVIONIC VENT FAN P/N M4401D8A, S/N OFF 598, S/N ON 576 REF: AMM 21-23-10-2. NO FIX. FOUND WHITE SMOKE COMING FROM SUPPLEMENTAL A/C SYSTEM UNDER THE FLOOR AND OUT THE AVIONICS RACK. DEFERRED SUPPLEMENTAL A/C SYSTEM PER MEL 21-50-2 (D) ENTERED INTO DMR, MXC NOTIFIED SUPPLEMENTAL A/C SY S PER MEL 21-50-2 (D) ENTERED INTO DRM, MXC NOTIFIED 0782. C/W MAINTENANCE PROCEDURES. REMOVED AND REPLACED COMPRESSOR MOTOR. 2 L 7 2 4T RT A52EU 2003050200148 20030502 00148 EA 2003 5 2 A6WA200340044 1 20021220 A 2420 761339D ADG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ELECTRICAL FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 2966 7568 MAINTENANCE CHECK REQUIRED FOR INFLIGHT ADG DEPLOYMENT FUNCTION. ADG TEST FAILED. REMOVED AND REPLACED ADG, (S/N OFF: 0611, S/N ON: 0238) TEST FLIGHT OF ADG TEST SATISFACTORY. ADG COMPONENT REPAIR SHOP TEAR-DOWN FINDINGS, NO FAULT FOUND (NFF). 2 L 7 2 4F 4 F RT A21EA E15NE 2003050600249 20030506 00249 CE 2003 5 6 CTU2003F00000 1 20020816 A 1430 AN414 BOLT CESSNA 340 340A 2076405 CE CONT O520 TSIO520* 17040 SO TAIL BENT B CTUR O OTHER O OTHER NR NOT REPORTED 1 GL 21 98560 5464 340A0032 AFTER FAILURE OF BOLT PRIOR TO FLIGHT MAINTENANCE FACILITY PERFORMED INSPECTION OF BOLT WHICH THE ELEVATOR BELLCRANK ROT ATION. BOLT MUST BE REMOVED FOR PROPER INSPECTION. BOLTS HAVE BOTH STRESSED AND BENT. MANUFACTURER SHOULD HAVE BOLT O F LARGER SIZE INSTALLED AND RECURRING INSPECTION OF BEARING. 1 L 7 2 3O 3 O 3A25 E8CE 2003050600252 20030506 00252 CE 2003 5 6 AZN2003F00000 1 20021206 A 1430 RIVET CESSNA 310 310R 2074245 CE CONT O520 IO520MB 17032 SO AFT OB LT WING SHEARED B AZNR K NONE O OTHER IN INSP/MAINT 1 GL 13 3286M 15163 310R1894 TWO FASTENERS FAILED AT OUTBOARD AFT TRAILING EDGE OF LEFT WING. WHERE THE AFT TIP FUEL TANK AND OUTBOARD AILERON HINGE BRACKET MOUNT. CREATING MOVEMENT OF AFT WING SPAR, CAUSING A CRACK IN THE UPPER SKIN. 1 L 7 2 3O 3 O 3A10 E5CE 2003050700117 20030507 00117 EA 2003 5 7 CA030417007 1 20021122 A 5741 BUSHING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WING ATTACHMENT LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS. 2 L 7 2 4F 4 F RT A21EA E15NE 2003050700009 20030507 00009 GL 2003 5 7 CA030407002 3 20021219 A 6114 SEAL BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110UG 01514 WP ROTOL R333 R333482F12 GL PROPELLER DOME BROKEN W O OTHER B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CL CLIMB 1 CA (CAN) AT DEPARTURE, CLIMBING TROUGH 2000 FT, SMOKE WAS NOTICED IN COCKPIT. RECIRCULATION FAN WAS CONFIRMED OFF, BOTH PRE SSURIZATION FLOWS WERE TURNED OFF WHICH REDUCED SMOKE ENTERING COCKPIT. ON LANDING, REVERSE THRUST WAS ASSYMETRIC. AFTER SHUT-DOWN, LT ENGINE COWL WAS FOUND TO BE COVERED IN OIL. BROKEN PROP PISTON O-RING ALLOWED HIGH PRESSURE OIL INTO SPIN NER AND SUBSEQUENTLY INTO ENGINE INTAKE. HIGH TEMP P3 BLEED AIR BROUGHT SMOKE TO THE COCKPIT DUE TO THE LT FLOW FEEDING THE COCKPIT IN THE JETSTREAM 3112. 2 L 7 2 4T 4 T RT A21EU E4WE 6 C P61GL 2003050700109 20030507 00109 EA 2003 5 7 CA030417003 1 20021025 A 5741 BUSHING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE WING ATTACHMENT LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS. 2 L 7 2 4F 4 F RT A21EA E15NE 2003050700115 20030507 00115 EA 2003 5 7 CA030417005 1 20020208 A 5741 BUSHING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE WING ATTACHMENT LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS. 2 L 7 2 4F 4 F RT A21EA E15NE 2003050700145 20030507 00145 EA 2003 5 7 YAD2003F00000 2 20021226 A 7314 PUMP BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA FUEL SYS FAILED E YADA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 AL 03 111AX UC81 32397 IN CRUISE FLIGHT, RT ENGINE LOW FUEL PRESSURE ANNUNCIATOR CAME ON AND THE ENGINE SHUT DOWN (FLAMEOUT)-THE AIRCRAFT MADE AN UNEVENTFUL LANDING AT AN ALTERNATE AIRPORT. POST LANDING VISUAL INSPECTION AND GROUND RUNS DID NOT IDENTIFY ANY ABNO RMALITIES. ENGINE AND AIRFRAME FUEL FILTERS WERE CLEANED OR REPLACED AND THE AIRCRAFT WAS FERRIED BACK TOT HE MAINTENAN CE BASE (80 MINUTES) WITHOUT ANY OBSERVED FAULTS. MAINT REPLACED THE LOW PSI FUEL PUMP AS A PRECAUTION. THE AIRCRAFT W AS PLACED IN A HANGAR TO THAW AND THE FUEL SUMPS WERE DRAINED OF SEDIMENT (SMALL AMOUNT OF WATER WAS REMOVED). 2 L 7 2 4T 4 T RT A24CE E4EA 2003050700152 20030507 00152 CE 2003 5 7 YAD2003F00001 1 20021214 A 3230 P624003 SWITCH BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE NLG INOPERATIVE E YADA O OTHER O OTHER NR NOT REPORTED 1 AL 03 1566C 23722 UC36 PILOT REPORTED NO NOSE GEAR DOWN INDICATION FOR LANDING. MAINTENANCE VERIFIED FAILURE OF THE NOSE GEAR ACTUATOR DOWN LO CK SWITCH-REPLACED NOSE GEAR ACTUATOR. 2 L 7 2 4T 4 T RT A24CE E4EA 2003051300019 20030513 00019 NM 2003 5 13 AALA20021168 1 20020816 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971AN 29547 MIA - DURING OVERNIGHT MAINTENANCE, LEFT OVERWING EMERGENCY EXIT AT SEAT 13A INOPERATIVE. REPLACED LEFT EMERGENCY EXIT LIGHTING ASSEMBLY AT SEAT 13A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2003051300020 20030513 00020 NM 2003 5 13 AALA20021620 1 20021112 A 3397 CONTACTOR BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 ORD - DURING OVERNIGHT MAINTENANCE, LEFT AFT EMERGENCY EXIT SIDE WALL LIGHT INOPERATIVE. RE-SOLDERED BULB RECEPTACLE CO NTACT AT LEFT AFT EMERGENCY EXIT SIDE WALL LIGHT. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2003051300021 20030513 00021 NM 2003 5 13 AALA20021170 1 20020816 A 3350 CHARGER BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AN 29507 LAX - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. REPLACED FORWRAD RIGHT BATTERY CHA RGER AND BATTERY. SYSTEM GORND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2003051300022 20030513 00022 NM 2003 5 13 AALA20021515 1 20021018 A 3350 S283W6032 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 934AN 29531 DEN - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AISLE SEATS 9, 10 AND 11 INOPERATIVE. REPLACED BATTERY PACK SEATS 9, 10 AND 11. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2003051300194 20030513 00194 SO 2003 5 13 000215 1 20021027 A 7830 WARNING SYSTEM EMB 145 EMB145 3260210 SO NR 2 T/R ACTIVATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 291 THRUST REVERSER DISAGREE MESSAGE. ON EICAS WHEN ADVANCED POWER FOR TAKE OFF. DEFERRED NR 2 THRUST REVERSER 2 L 7 2 4F RT T00011AT 2003051300195 20030513 00195 SO 2003 5 13 000216 1 20021027 A 2842 INDICATOR EMB 145 EMB145 3260210 SO NR 1 FUEL QTY MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 293 NR 1 FUEL QUANTITY INOPERATIVE, SHOWING 0. OPS CHECK GOOD 2 L 7 2 4F RT T00011AT 2003051300196 20030513 00196 SO 2003 5 13 000214 1 20021025 A 3610 WARNING LIGHT EMB 145 EMB145 3260210 SO NR 2 BLEED ILLUMINATED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 293 CREW RECEIVED A BLEED NR 2 LEAK ON EICAS ON CLIMBOUT 2 L 7 2 4F RT T00011AT 2003051300267 20030513 00267 WP 2003 5 13 AALA20021703 1 20021120 A 5347 GALLEY TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 FOUND CORROSION ON SEAT TRACK NR 1 AT GALLEY TIE DOWN. REMOVED CORROSION CUTOUT AREA BEYOND LIMITS AND INSTALLED PLUG P ER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2003051300268 20030513 00268 WP 2003 5 13 AALA20021704 1 20021122 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 FOUND CORROSION ON BOTTOM SIDE OF CUSP AT STATION 1174 BELOW NR 1 SEAT TRACK. REMOVED CORROSION. INSTALLED DOUBLER REP AIR PER SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2003051300269 20030513 00269 WP 2003 5 13 AALA20021705 1 20021120 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 TUL - FOUND CORROSION ON LEFT CUSP, STATION 1287 BETWEEN TRACK NR 1 AND NR 2. INSTALLED NEW CUSP SHEET, STATION 1250-13 09 PER SRM 53-05-00 FIG 97. (M) 2 L 7 2 4F A6WE 2003051300284 20030513 00284 WP 2003 5 13 AALA20021690 1 20021112 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 599AA 53289 TUL - FOUND CORROSION ON SEAT TRACK NR 2 FROM STATION 1203 TO 1300. INSTALLED NEW SEAT TRACK NR 2, STATION 1184-1307 AN D INSTALLED NEW SPLICE PER SRM 53-05 PART 1. (M) 2 L 7 2 4F RT A6WE 2003051300287 20030513 00287 WP 2003 5 13 AALA20021680 1 20021108 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 599AA 53289 TUL - FOUND CORROSION ON RIGHT CUSP AT STATION 468. INSTALLED DOUBLER PER SRM 53-01-00. (M) 2 L 7 2 4F RT A6WE 2003051300288 20030513 00288 WP 2003 5 13 AALA20021681 1 20021112 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 599AA 53289 TUL - FOUND CORROSION ON LEFT CUSP AT STATION 1174. INSTALLED CUSP DOUBLER STATION 1174 PER AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2003051300291 20030513 00291 WP 2003 5 13 AALA20021679 1 20021112 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 599AA 53289 FOUND CORROSION ON SEAT TRACK BETWEEN STATION 1207 AND 1299. INSTALLED NEW SEAT TRACK PER SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2003051300293 20030513 00293 WP 2003 5 13 AALA20021700 1 20021125 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 TUL - FOUND FS 1474 CRACKED LOWER RIGHT SIDE JUST INBOARD OF DOOR CUTOUT. REPAIRED CRACKED FRAME PER SRM 53-10-00-15 PA GE 1. (M) 2 L 7 2 4F A6WE 2003051300295 20030513 00295 WP 2003 5 13 AALA20021701 1 20021122 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 FOUND FS 1401 FRAME CRACKED AFT SIDE FROM UNDER RADIUS BLOCK STRINGER 2L AREA. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-15 AND SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2003051300296 20030513 00296 WP 2003 5 13 AALA20021702 1 20021121 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 TUL - FOUND SEVERAL AREAS OF CORROSION ON AFT CARGO DOOR BEAM. REMOVED AND REPLACED BEAM PE SRM 53-10-00. (M) 2 L 7 2 4F A6WE 2003051400005 20030514 00005 NM 2003 5 14 AALA20021541 1 20021027 A 3350 S283W6032 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 954AN 30089 DURING OVERNIGHT MAINTENANCE, EMREGENCY ESCAPE PATH LIGHTING FIRST THREE ROWS OF COACH FOUND INOPERATIVE. REPLACED BATT ERY PACK FOR EMERGENCY LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2003051400011 20030514 00011 2003 5 14 AALA20021725 4 20021203 A 2211 B471AAM7 COMPUTER AIRBUS 300 A300B4605R 3930308 EU E/E BAY DEFECTIVE A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 14068 511 JFK - FLT 647 - EN ROUTE JFK-SJU, DURING CLIMB-OUT, AIRCRAFT ENCOUNTERED TURBULENCE AND AIRCRAFT YAWED SEVERAL TIMES. S LATS EXTENDED WITH TAKEOFF SLATS SET. AIRCRAFT RETURNED TO JFK WITH NO FURTHER INCIDENT. REPLACED NR 1 FLIGHT AUGMENTA TION COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2003051300193 20030513 00193 2003 5 13 000235 4 20021221 A 3414 INDICATOR EMB 145 EMB145 3260210 SO COCKPIT MALFUNCTIONED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 277 IAS FLAG OVER AIRSPEED TAPE ON CAPTAIN SIDE DURING T/O. R & R F/O PITOR DRAIN CAP. 2 L 7 2 4F RT T00011AT 2003051300270 20030513 00270 WP 2003 5 13 AALA20021706 1 20021121 A 5320 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 FOUND WHALE BONE TO KEELBEAM ATTACH ANGLE CRACKED INBOARD END RIGHT GEAR WELL. REMOVED AND REPLACED ANGLE PER SRM 51-01 . (M) 2 L 7 2 4F A6WE 2003051300289 20030513 00289 WP 2003 5 13 AALA20021682 1 20021113 A 5500 PLATE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 599AA 53289 FOUND CORROSION AND PITTING ON 8 HINGE LUG PLATES FOR HORIZONTAL STABILIZER PIVOT, STATION YV170. INSTALLED NEW HINGE P LATES FOR HORIZONTAL STABILIZER PIVOT PER KF0488. (M) 2 L 7 2 4F RT A6WE 2003051300292 20030513 00292 WP 2003 5 13 AALA20021699 1 20021126 A 5320 SUPPORT ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 TUL - FOUND CANT FRAME FS 1474 RIGHT SIDE AFT OF ACCUMULATOR DOOR CUTOUT, ANGLE CRACKED. REMOVED AND REPLACED ANGLE STI FFENER PER SRM 51-01 AT CANT FS 1474 RIGHT SIDE. (M) 2 L 7 2 4F A6WE 2003051400004 20030514 00004 NM 2003 5 14 AALA20021514 1 20021022 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 925AN 29526 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH EXIT LIGHT LOOSE AT RIGHT SIDEWALL FORWARD OF THE FORWARD OVER WING EXIT. REPLACED EMERGENYC EXIT LIGHT ASSEMBLY BRACKET. (M) 2 L 7 2 4F RT A16WE 2003052300002 20030523 00002 EA 2003 5 23 2003F00288 1 20021217 A 3297 601577889 WIRE HARNESS CNDAIR CL600 CL6002B16 1900305 EA NLG INTERMITTENT A O2GA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 03 601VH 5043 NOSE GEAR FAILED TO PROPERLY RETRACT AFTER NORMAL TAKEOFF. GEAR HANDLE FLASHING LIGHT REMAINED ILLUMINATED AND NOSE GEA R DOOR REMAINED OPEN. GEAR SELECTED DOWN, GEAR LOWERED AND EXTENDED NORMALLY WITH PROPER DOWN AND LOCK INDICATION. NOS E GEAR WOW HARNESS WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2003052300004 20030523 00004 WP 2003 5 23 MEX2002380 1 20021225 A 5330 SKIN DOUG DC9 DC987 3022087 WP FUSELAGE SCRATCHED A ASMF O OTHER O OTHER NR NOT REPORTED 1 SW 23 204AM 49404 FLT 218 - MTY-CJS - DURING TRANSIT DETECTED A SCRATCH AT THE LEFT ARE OF THE FUSELAGE LOWER PART, NEAR TO THE WASTE SERV ICE ACCESS. THE SCRATCH WAS APPROXIMATELY 18 INCHES AND 10 INCHES WIDE AND TWO DRILLINGS BETWEEN THE PRESSURIZATION VAL VES. AT GDL, FUSELAGE SKIN LOCATED BETWEEN LONGERON 25 AND 27 AND STA Y=1050 AND Y-1078 WAS TEMPORARY REPAIRED IAW SRM 53-04 FIG 12B SHEET 77. (M) 2 L 7 2 4F RT A6WE 2003052300001 20030523 00001 EU 2003 5 23 2003F00287 1 20021026 A 3350 WIRE HARNESS AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 712US 1038 FOUND THE LEFT, ROW 1, SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE, WITH A WIRE PULLED FROM THE CONNECTOR. MAINTENANCE REP LACED THE EMERGENCY LIGHT WIRE HARNESS AT SEAT 1 ABC. FUNCTIONAL TEST OF SYSTEM OK. (M) 2 L 7 2 4F RT A28NM 2003052300011 20030523 00011 WP 2003 5 23 MEX2002384 1 20021228 A 5270 WARNING LIGHT DOUG DC9 DC982 3022082 WP DOOR WARNING ILLUMINATED A ASMF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 23 1003Y 48068 AIRCRAFT RETURN TO FLIGHT DUE TO ACCESSORY COMPARTMENT DOOR LIGHT TURNED ON. COMPARTMENT DOOR WAS CHECKED DETECTING TWO SECURES UNSAFE, REINSTALLED. DURING OVERNIGHT SERICE ACCESSORY COMPARTMENT DOOR LIGHT WAS CHECKED IAW MM 52-70-06, TES TS OK. (M) 2 L 7 2 4F A6WE 2003052300013 20030523 00013 WP 2003 5 23 MEX2002377 1 20021222 A 3210 LANDING GEAR DOUG DC9 DC987 3022087 WP MAIN OBSTRUCTED A ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 753RA 49587 FLT 920 - MEX-MTY - AIRCRAFT RETURNED DUE TO NOSE LANDNG GEAR RETRACTION WAS CLOGGED. ANTI-RETRACTION SECURE WAS USED A ND NOSE LANDNG GEAR RED LIGHT TURN ON. AIRCRAFT DID NOT PRESSURIZE AND WINDSHEAR AND STALL INDICATION FAILURE LIGHTS TU RN ON. AIRCRAFT WAS SENG TO THE HANGAR TO ATTEND THE FAILURE. NOSE GEAR STRUT SERVICE WAS PERFORMED IAW MM 32-21-02. LANDING GEAR CONTROL LEVER AND ANTI-RETRACTION LATCH WERE INSPECTED FOR OBSTRUCTION AND CONDITION IAW MM 32-31-01, ALL C ORRECT. NOSE LANDING GEAR WAS TESTED IAW MM 32-30-00. (M) 2 L 7 2 4F RT A6WE 2003052300016 20030523 00016 2003 5 23 2003F00297 4 20020519 A 8300 GEARBOX BOEING 727 727200 138407E NM NR 1 ENGINE LEAKING A P9RA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SW 09 906PG 20728 NR 1 ENGINE OIL QUANTITY DECREASED FORM 3 GALLONS TO ONE-FOURTH GALLON, IN ONE HOUR. PERFORMED AND IN FLIGHT PRECAUTION ARY ENGINE SHUTDOWN AS PER AFM PROCEDURES. PERFORMED BREATHER PRESSURE, INSPECTED FOR EXTERNAL LEAKAGE. BOTH CHECKS WE RE SATISFACTORY. AIRCRAFT IS CURRENTLY UNDERGOING A GEARBOX CHANGE. (M) 2 L 7 3 4F RT A3WE 2003052300003 20030523 00003 NM 2003 5 23 MEX2002379 1 20021225 A 7800 EXHAUST STACK DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LT ENGINE DAMAGED A ASMF O OTHER O OTHER NR NOT REPORTED 1 SW 23 161PL 49764 725563 FLT 6571 - MEX - DURING TRANSIT DETECTED DAMAGES AT THE EXHAUST AREA OF THE LT ENGINE. AIRCRAFT WAS SENT TO THE HANGAR. LT ENGINE WAS REPLACED IAW MM 71-00-02, OPERATIONAL TESTS WERE PERFORMED IAW MM 71-0-01, ALL CORRECT. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2003052700112 20030527 00112 EA 2003 5 27 2003F00322 1 20021203 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 17231 7231 ASH - FLT 6011 - COS-PHX - RETURNED TO FIELD FOR NOSE GEAR UP DISAGREE. MAINTENANCE BEING SENT FROM PHX. MAINTENANCE R EPLACED THE NLG PRIORITY VALVE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2003052300007 20030523 00007 WP 2003 5 23 MEX2002378 1 20021224 A 3230 59164605609 VALVE DOUG DC9 DC932 3022066 WP NLG FAILED A ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 1003P 48150 AIRCRAFT RETURN, DUE TO NOSE LANDING GEAR UNSAFE INDICATION. AIRCRAFT WAS SENT TO THE HANGAR TO ATTEND THE FAIL. REPLA CED NOSE LANDING GEAR O-RINGS IAW MM 32-21-2 AND LANDING WITH OVERWEIGHT INSPECTION WAS ACCOMPLISHED IAW MM 05-51-0. ADD ITIONALLY THE FOLLOWING COMPONENTS WERE REPLACED, NOSE LANDING GEAR CONTROL VALVE, ACTUATING CYLINDER AND BUNGEE CYLINDE R IAW MM 32-32-1, 32-32-6 AND 32-32-7, TESTS PERFORMED IAW MM 32-32-0, ALL CORRECT. (M) 2 L 7 2 4F A6WE 2003052900010 20030529 00010 EA 2003 5 29 2003F00327 2 20020117 A 8500 CAP CESSNA 172 172M 2072418 CE LYC O320 O320* 41508 EA RT ENGINE CRACKED A T0DA K NONE O OTHER IN INSP/MAINT 1 CE 03 172C 17262566 DURING PREFLIGHT INSPECTION, FOUND A CRACK ON THE INNER SIDE APPROXIMATELY 3 O'CLOCK POSITION OF THE RIGHT ENGINE INLET NOSE CAP P/N 6352602-2. THE CRACK WAS APPROX .75 OF AN INCH IN LENGTH RUNNING FROM THE EDGE OF THE METAL TO THE ATTACHI NG FASTENER. (M) 1 H 7 1 3O 3 O NT 3A12 E274 2003053000063 20030530 00063 NM 2003 5 30 2003F00338 1 20021230 A 5510 65245711 SUPPORT BOEING 727 72721 1384003 NM HORIZONTAL STAB CORRODED A XP0B O OTHER O OTHER NR NOT REPORTED 1 SO 35 727PX 19261 LEFT HORIZONTAL STABILIZER, INTERGRANULAR CORROSION ON AFT LOWER SUPPORT BEAM UPPER FORWARD FLANGE, 27 INCHES FROM INBOA RD END AT ELEVATOR STATION 17.20 TO 44.20 CUTOUT CORRODED AREA PER SRM 51-10-1. REPAIRED PER SRM 55-10-6. (M) 2 L 7 3 4F A3WE 2003053000066 20030530 00066 NM 2003 5 30 2003F00341 1 20021226 A 5520 10605452 HOUSING BOEING 727 72721 1384003 NM RT ELE BEARING WORN A XP0B O OTHER O OTHER NR NOT REPORTED 1 SO 35 727PX 19261 RIGHT ELEVATOR BEARING HOUSING, POSITIONS NR 5 AND NR 7 WORN BEYOND LIMITS. REMOVED AND REPLACED NR 5 AND NR 7 BEARING HOUSING ASSEMBLIES IAW MM 27-30-5. (M) 2 L 7 3 4F A3WE 2003053000067 20030530 00067 WP 2003 5 30 AALA20021424 1 20020930 A 5280 DOOR DOUG DC9 DC982 3022082 WP LT MLG CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 FOUND LEFT WW DOOR LANDING CRACKED AT OUTBOARD AFT CORNER, FS 1003. STOP DRILLED CRACK, INSTALL DOUBLER PER SRM 53-01 F IG 2. (M) 2 L 7 2 4F A6WE 2003053000068 20030530 00068 EU 2003 5 30 2003F00342 1 20021011 A 3350 311701 POWER SUPPLY BAG JETSTM JETSTM3101 1500215 EU CABIN DISCHARGED A B16A K NONE L NO TEST IN INSP/MAINT 1 NE 05 539PA 741 PSM - FLT 3505 - DURING PREFLIGHT, CREW REPORTED EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED ALL FOUR EMERGENCY EVACUATION POWER SUPPLIES DUE TO LOW VOLTAGE, DUE TO BEING INADVERTENELY LEFT ON FOR A LONG PERIOD OF TIME. (M) 2 L 7 2 4T RT A21EU 2003053000071 20030530 00071 EA 2003 5 30 2003F00344 1 20021210 A 7800 89P12795 EXHAUST STACK GRUMAN SA16 G111 3950410 EA WRIGHT R1820 R182056A 67020 EA ENGINE LOOSE A MY8A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 17 42MY 148329 ON A REPOSITIONING FLIGHT FROM PBI-FPR, AFTER TAKEOFF APPROX 500 FT PILOT REPORTED A LEFT ENGINE FIRE INDICATION. WITH POWER REDUCTION THE LIGHT WENT OUT. AIRCRAFT RETURNED TO PBI. LANDED WITHOUT INCIDENT. INVESTIGATION BY MYI MAINTENAN CE DETERMINED NR 2 CYLINDER EXHAUST ASSEMBLY. ATTACHMENT FLANGE BOLTS WORKED LOOSE, WHICH EXPOSED THE FIRE DETECTION EL EMENT TO HOT EXHAUST GASES. (M) 2 H 7 2 4R 4 R A22SO 5E10 2003053000078 20030530 00078 NM 2003 5 30 2003F00348 1 20021219 A 5520 6572795 BRACKET BOEING 727 72721 1384003 NM LT ELEVATOR CORRODED A XP0B O OTHER O OTHER NR NOT REPORTED 1 SO 35 727PX 19261 LEFT ELEVATOR, INBOARD TRIM BRACKET, HAS INTERGRANULAR CORROSION. REMOVED AND REPLACED BRACKET PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 2003053000082 20030530 00082 NM 2003 5 30 2003F00352 1 20021126 A 7160 65727731 DUCT BOEING 727 72721 1384003 NM NR 2 INTAKE CORRODED A XP0B O OTHER O OTHER NR NOT REPORTED 1 SO 35 727PX 19261 CORROSION ON SKIN OF NR 2 'S' DUCT AT RIB STATIONS 9, 10, 12, 16, 17, 27, 30, 37 AND 38. REMOVED CORROSION AND REPAIRED WITH EXTERIOR SKIN REPAIRS IAW SRM 54-10-3. (M) 2 L 7 3 4F A3WE 2003060200027 20030602 00027 CE 2003 6 2 CA030421010 1 20021221 A 2435 03601018 BEARING LUCAS CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP HARTZL HCB3T HCB3TN5 GL STARTER GEN FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA 285 (CAN) STARTER GEN WAS HAVING NEW BRUSHES SEATED AT MID-TBO USING GEN DRIVESTAND METHOD.APPRX 3 HRS INTO THE PROCESS, THE ANTI-DRIVE END BEARING FAILED COMPLETELY. 5 OF 8 BALLS DISINTEGRATED,AS DID THE CAGE.DAMAGE WAS SUSTAINED TO THE ARMAT URE, STATOR, FAN AND FAN COVER.DISCUSSIONS WITH THE OEM ENG'G SUPPORT LED TO THE CONCLUSION THAT THE OPERATING CONFIGURA TION ON THE AIRCRAFT RESTRICTED THE FLOW OF COOLING AIR TO THE STARTER GEN, AND EXCESSIVE HEAT OVER TIME DAMAGED THE BEA RING NEAREST THE BRUSHES. 1 L 7 2 3T 4 T RT A28CE E4WE 6 C P15EA 2003053000069 20030530 00069 EU 2003 5 30 2003F00343 1 20021022 A 3350 311701 POWER SUPPLY BAG JETSTM JETSTM3101 1500215 EU CABIN DISCHARGED A B16A K NONE L NO TEST IN INSP/MAINT 1 NE 05 536PA 681 PILOT REPORTED EMERGENCY LIGHTS ILLUMINATE FOR THREE MINUTES, THEN GO OUT. MAINTENANCE REPLACED ALL FOUR EMERGENCY LIGH T POWER PACKS. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A21EU 2003053000077 20030530 00077 NM 2003 5 30 2003F00347 1 20021213 A 5330 6572702 SKIN BOEING 727 72721 1384003 NM FUSELAGE CORRODED A XP0B O OTHER O OTHER NR NOT REPORTED 1 SO 35 727PX 19261 PBI - EXFOLIATED CORROSION AT BS 660, RIGHT LAP JOINT STRINGER 19. REMOVED CORROSION, REPAIRED PER SRM 53-30-3, FIG 5 A ND 27. (M) 2 L 7 3 4F A3WE 2003053000080 20030530 00080 EU 2003 5 30 2003F00350 1 20021009 A 3240 AC66867 CONTROL VALVE BAG JETSTM JETSTM3101 1500215 EU BRAKE LEAKING A B16A D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 NE 05 530BA 732 WHILE TAXIING TO THE GATE, PILOT REPORTED NO BRAKE PRESSURE OR BRAKE EFFECT ON RIGHT WHEELS. MAINTENANCE REPLACED DUAL BRAKE CONTROL VALVE AND PERFORMED BLEEDING PROCEDURE. OPERATIONALLY CHECKED GOOD. (M) 2 L 7 2 4T RT A21EU 2003060400046 20030604 00046 SO 2003 6 4 SIMA200302108 1 20021231 A 5320 14521725001 SILL EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 701MH 145162 THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION CORROSION ON LEFT SILL AFT OF PASSENGER DOOR BETWEEN FRAME 18 L AND 22L AT STRINGER 15L. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2003053000076 20030530 00076 NM 2003 5 30 2003F00346 1 20021228 A 5523 1060779112 BEARING BOEING 727 72721 1384003 NM ELEVATOR TAB WORN A XP0B O OTHER O OTHER NR NOT REPORTED 1 SO 35 727PX 19261 LOWER RUDDER TRIM TAB BEARINGS WORN. REMOVED AND REPLACED ROD END BEARINGS IAW MM 27-20-0. (M) 2 L 7 3 4F A3WE 2003053000079 20030530 00079 NM 2003 5 30 2003F00349 1 20021226 A 5520 69302221 HOUSING BOEING 727 72721 1384003 NM ELEVATOR BEARING WORN A XP0B O OTHER O OTHER NR NOT REPORTED 1 SO 35 727PX 19261 LEFT ELEVATOR BEARING HOUSING POSITION NR 4 AND NR 7 WORN BEYOND LIMITS. REMOVED AND REPLACED NR 4 AND NR 7 BEARING HOU SING ASSEMBLIES IAW MM 27-30-5. (M) 2 L 7 3 4F A3WE 2003060500135 20030605 00135 EU 2003 6 5 CA030319002 1 20021102 A 2910 704A37721092 PRESSURE SWITCH SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE HYD SYSTEM INOPERATIVE W A UNSCHED LANDING J WARNING INDICATION HO HOVERING 1 CA (CAN) PILOT WAS LONG LINING, DIRECTING ATTENTION TO VERT REF WINDOW. A/C SUDDENLY PITCHED UP, CONTROLS BECAME STIFF. THE RE WAS NO HORN OF ANY KIND, NOR WAS HYD PRESS DROP WARNING LIGHT (HYD LIGHT)ON WARNING CAUTION ADVIS PNL. PILOT CONTINU ED TO EVALUATE PROBLEMS, AS HE NEARED A LANDING SITE, FOUND THAT COLLECTIVE MOUNTED HYD PRESS CUT-OFF SWITCH WAS IN OFF POSITION. PILOT REDUCED FLT CONTROL PRESS, RETURNED SWITCH TO ON POSITION, FLIGHT CONTROLS, CORRESPONDING HYD PRESSURE S RETURNED TO NORMAL. LANDED A/C NORMALLY, IN INVESTIGATION, ENGINEER FOUND HYD LOW PRESS SWITCH WAS DEFECTIVE. VIB CA USED IT INTO OFF POSITION. BOTH HYD CUT-OFF SWITCH, LOW PRESS SWITCH WERE REPLACED. HORN TEST BUTTON SWITCH WAS CLEANED. 1 G 7 1 3U 3 U H9EU E19EU 2003060500036 20030605 00036 SO 2003 6 5 SIMA200302104 1 20021231 A 5310 14522460013 GUSSET EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 701MH 145162 FOUND DURING AN IMBV INSPECTION, CORROSION ON GUSSET AT CENTER BEAM SECTION BETWEEN FRAME 18 AND 22 ABOVE STRINGER 21L. REMOVED AND INSTALLED SERVICEABLE CENTER BEAM GUSSET IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2003061100043 20030611 00043 NM 2003 6 11 EVAS91009 1 20020315 A 2710 CONTROL QUADRANT DOUG MD11 MD11F 3023600 NM RUDDER TRIM FAILED W QOCF A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 WP 03 16107 48546 DURING CRUISE, CAPTAIN FOUND AILERON AND RUDDER TRIM FUNCTION, MANUAL CONTROL FAIL TOO, AIRCRAFT AIR TURN BACK. ON GROU ND FOUND DRIVE LINKAGE DETACHED, AFTER SECURE AND PERFORM RIGGING CHECK, NORMAL. 2 L 7 3 4F RT A22WE 2003061200070 20030612 00070 WP 2003 6 12 0301069952 1 20020701 A 4990 OIL COOLER HONEYWELL DOUG DC9 DC931 3022065 WP APU LEAKING A NWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 916RW P28140DCA 47144 DURING CLIMB FLIGHT ATTENDANT REPORTED LIGHT SMOKE IN CABIN. FLIGHT ATTENDANT DISCHARGED A HALON FIRE EXTINGUISHER IN T HE AFT RIGHT LAV. FLIGHT CREW RETURNED AC TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. NO EVIDENCE OF A F IRE WAS FOUND. MAINTENANCE DID FIND THE APU OIL COOLER LEAKING OIL. APU DEACTIVATED AND SCHEDULED FOR REPLACEMENT. FO LLOW UP INFORMATION, REFERENCE CONTROL NUMBER 0202119952 SUBMITTED 6/28/02. 2 L 7 2 4F A6WE 2003061700327 20030617 00327 2003 6 17 BAQA081563 4 20021203 A 3421 43800100030 GYRO UROCOP EC135 EC135T1 5620026 EU COCKPIT INTERMITTENT H BAQA O OTHER O OTHER NR NOT REPORTED 1 FS 01 118WS 1589 0089 INTERMITTENTLY INOPERABLE. 1 G 7 2 3U H88EU 2003062300059 20030623 00059 EU 2003 6 23 LDIA200200002 1 20021018 A 3260 MS243311 POSITION SWITCH ISRAEL 1124 1124 4500102 EU MLG FAULTY A LDIA O OTHER N FALSE WARNING AP APPROACH 1 SW 05 290CA 216 UPON APPROACH INTO OMA, LANDING GEAR WAS EXTENDED, RIGHT MAIN GEAR DOWN/LOCKED LIGHT FAILED TO ILLUMINATE. COCKPIT LIGH T TESTED GOOD. EMERGENCY GEAR EXTENSION WAS PERFORMED IAW WITH CHECKLIST. RIGHT GEAR DOWNLOCKED WAS STILL NOT ESTABLISH ED. EMERGENCY LANDING WAS PERFORMED. AIRCRAFT THEN ACCOMPLISHED FERRIED FLIGHT TO DUNCAN AVIATION AT LINCOLN. DUNCAN FOUND DOWNLOCKED INDICATION. REPLACED FAULTY SWITCH. (M) 2 M 7 2 4F A2SW 2003062400090 20030624 00090 NM 2003 6 24 DL757030464 1 20020512 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 627DL 22917 FUSELAGE SKIN WAS FOUND DENTED AND GOUGED AT 2 LOCATIONSBETWEEN FS 605 & 625 AT STRINGER 16L AND JUST BELOW STRINGER17L. THE DAMAGE WAS REMOVED WITH 2 CUTOUTS. THE CUTOUTS WERE REPAIRED WITH A SINGLE ALUMINUM DOUBLER AND TRIPLER REPA IR PER ER/A 385022-14, REV A. 2 L 7 2 4F RT A2NM 2003062300071 20030623 00071 CE 2003 6 23 2003F00381 1 20020904 A 7120 12991004717 TRUSS BEECH 1900 1900D 1154162 CE ENGINE CHAFED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 69547 UE189 AT SCHEDULED ROUTINE MAINTENANCE, CHAFING DAMAGE AT 3 INCHES AFT OF FIRE SEAL FLANGE ON INBOARD SIDE. PERFORMED TRUSS R EPAIR TO CHAFED AREA IAW FAA APPROVED DATA CONTAINED IN RAYTHEON FIELD REPAIR FR-CO-00706 REV. (M) 2 L 7 2 4T RT A24CE 2003062400036 20030624 00036 NM 2003 6 24 CALA0300318 1 20020530 A 5320 SILL BOEING 737 7373T0 1384582 NM PAX DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 INSPECTION FOUND THE L-1 DOOR LOWER SILL CORRODED AT BS 314, LBL 57. THE DOOR SILL WAS REPAIRED IAW ECRA 5312-01146. 2 L 7 2 4F RT A16WE 2003070100028 20030701 00028 EU 2003 7 1 HEEA087880 1 20021230 A 2911 704A34240015 ACCUMULATOR AEROSP AS355 AS355* EU HYD SYSTEM DAMAGED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 4036H 2919 ACCUMULATOR WILL NOT HOLD PRESSURE. TO BE SENT TO VENDOR. 1 G 7 2 3U H11EU 2003070700204 20030707 00204 WP 2003 7 7 ABXA030227 1 20020807 A 5240 SKIN DOUG DC8 DC863F 302198F WP SERVICE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FORWARD SERVICE DOOR LOWER AFT CORNER SKIN HAD A CRACK. CUT OUT DAMAGE IAW DC-8 SRM 53-2-0. FABRICATED DOUBLERS AND FILL ERS IAW DC-8 SRM 53-2-0. INSTALLED DOUBLERS AND FILLERS IAW DC-8 SRM 53-2-0. REINSTALLED INNER TORQUE BOX WEB IAW DC-8 S RM 51-1-20E AND 51-3-0. 2 L 7 4 4F 4A25 2003070700205 20030707 00205 WP 2003 7 7 ABXA030228 1 20020720 A 5313 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 32 LEFT OB CHANNEL AT STA. 370 WAS CORRODED. REMOVED CORRODED SECTION OF LONGERON, FABRICATED LONGERON AND SPL ICES. INSTALLED IAW SRM 51-1-20D, 51-1-24, AND 53-2-2. 2 L 7 4 4F 4A25 2003070700206 20030707 00206 WP 2003 7 7 ABXA030216 1 20020716 A 5311 FRAME DOUG DC8 DC863F 302198F WP PWA JT3D JT3D* 52039 NE FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 AFT CARGO BS 1010, BETWEEN LONGERON 35 LEFT AND 35 RT, FUSELAGE FRAME CORRODED ON UPPER CAP, UPPER AND LOWER SURFACES. R EMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED (1 EA) FRAME CAP, (6 EA) GUSSETS, CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE, FILLERS AND SHIM, INSTALLED REPAIR ANGLE, FILLERS, SHIM, FRAME CAP AND GUSSETTS IAW DC-8 SRM 51-1-20D, 53- 2-0, REA D853-43970MR, AND SRM 51-1-8. 2 L 7 4 4F 4 F 4A25 1E8 2003070700207 20030707 00207 WP 2003 7 7 ABXA030218 1 20020716 A 5340 STRUCTURE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D* 52039 NE SERVICE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FORWARD SERVICE DOOR UPPER FORWARD CORNER HAD A CRACK IN OUTER SKIN. CUT OUT CRACKED AREA, FABRICATED DOUBLER, TRIPLER, FILLER, AND INSTALLED EACH IAW SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D, 51-3-0 AND 51-1-14. 2 L 7 4 4F 4 F 4A25 1E8 2003070700208 20030707 00208 WP 2003 7 7 ABXA030219 1 20020722 A 5230 DOUBLER DOUG DC8 DC863F 302198F WP PWA JT3D JT3D* 52039 NE CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FORWARD LOWER CARGO C1 DOOR, FUSELAGE INNER DOUBLER WAS CRACKED AT FUSELAGE STA. 320, OUTER EDGE AND HAD AN IMPROPER REP AIR. CUT OUT DAMAGED SECTION OF DOUBLER, FABRICATED FILLER, REPAIR DOUBLER SPLICES, AND INSTALLED ALL REPAIRS PARTS IAW DC-8 SRM 51-1-20D, DAC DWG 5753892, REA D853-43966MR, AND SRM 51-1-8. 2 L 7 4 4F 4 F 4A25 1E8 2003070800013 20030708 00013 WP 2003 7 8 ABXA030225 1 20020717 A 5310 DOOR FRAME DOUG DC8 DC863F 302198F WP PWA JT3D JT3D* 52039 NE Z FITTING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 AFT CARGO, BS 1220, FUSELAGE FRAME CORRODED JUST INBOARD OF SLIDING DOOR, LOWER AFT CUTOUT. REPLACED DOOR FRAME ZEE FITT ING, FABRICATED REPAIR SPLICE ANGLES AND FILLERS. INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, AND 51-3-0. 2 L 7 4 4F 4 F 4A25 1E8 2003070800014 20030708 00014 WP 2003 7 8 ABXA030229 1 20020720 A 5313 LONGERON DOUG DC8 DC863F 302198F WP PWA JT3D JT3D* 52039 NE FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 REMOVE AND REPLACE LONGERON 32 LEFT INBOARD CHANNEL STA. 190 - 385. REMOVED CORRODED SECTION, FABRICATED LONGERON AND S PLICES. INSTALLED IAW DC-8 SRM 51-1-20D, 53-2-2, AND 51-1-8. 2 L 7 4 4F 4 F 4A25 1E8 2003070700194 20030707 00194 WP 2003 7 7 ABXA030226 1 20020719 A 5330 57552713N SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 REMOVE AND REPLACE FORWARD LOWER CARGO SKIN FROM F.S. 190 - 450 LONGERON 31 LEFT - 31 RIGHT. (COI NR 41207-001). REPLACE D FORWARD LOWER CARGO SKIN IAW DC-8 SRM. 2 L 7 4 4F 4A25 2003070700212 20030707 00212 WP 2003 7 7 ABXA030224 1 20020715 A 5310 3755842U1F SHEAR TIE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D* 52039 NE FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 AFT LOWER CARGO, SHEARTIE CORRODED AT STA. 1200, LONGERON 28 - 29 LEFT. REMOVED CORROSION, OUT OF LIMITS. REMOVED FITTIN G AND FABRICATED SPLICE, INSTALLED NEW FITTING IAW DC-8 SRM 51-1-8, 53-2-0, AND 51-1-20D. 2 L 7 4 4F 4 F 4A25 1E8 2003070800051 20030708 00051 WP 2003 7 8 ABXA030244 1 20020830 A 5230 LATCH DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 MAIN CARGO DOOR, LATCH NR 8, ATTACHING HOLES HAD 5 CRACKS. REMOVED AND REPLACED FRAME SECTION IAW REA D852-36710MR. 2 L 7 4 4F 4A25 2003070800084 20030708 00084 WP 2003 7 8 ABXA030245 1 20020830 A 5230 FRAME DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 MAIN CARGO DOOR, LATCH NR 9, ATTACHING FASTENER HOLES HAD 5 CRACKS IN HOLES. REMOVED AND REPLACED FRAME SECTION IAW REA D852-36710MR. 2 L 7 4 4F 4A25 2003070800085 20030708 00085 WP 2003 7 8 ABXA030246 1 20020830 A 5230 FRAME DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 MAIN CARGO DOOR, LATCH NR 10, ATTACHING HOLES HAD 5 CRACKS IN HOLES. REMOVED AND REPLACED FRAME SECTION IAW ABX REA D852 -36710MR. 2 L 7 4 4F 4A25 2003070800086 20030708 00086 WP 2003 7 8 ABXA030247 1 20020830 A 5230 FRAME DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 MAIN CARGO DOOR, LATCH NR 11, ATTACHING HOLES HAD 6 FASTENERS CRACKED. REMOVED AND REPLACED FRAME SECTION IAW ABX REA D8 52-36710MR. 2 L 7 4 4F 4A25 2003070700211 20030707 00211 WP 2003 7 7 ABXA030222 1 20020806 A 5754 STRUCTURE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D* 52039 NE LT WING LE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LT WING LEADING EDGE UPPER SECTION APPROXIMATELY, STA. XFS 126.250, CORROSION AROUND FASTENERS. REMOVED CORROSION, FOU ND TO BE OUT OF LIMITS. REPAIRED IAW REA D857-43958MR. 2 L 7 4 4F 4 F 4A25 1E8 2003070800045 20030708 00045 CE 2003 7 8 YAD2003F00002 1 20020820 A 3340 2065521 CONNECTOR BEECH 1900 1900C 1154161 CE NAV LIGHTS SHORTED E YADA O OTHER O OTHER NR NOT REPORTED 1 AL 03 45GL 37312 UC45 DURING SCHEDULED MAINTENANCE, FOUND THAT THE WING STROBE LIGHTS WERE INOPERATIVE WITH THE NAVIGATION LIGHT TURNED ON. T ROUBLESHOOTING REVEALED INTERNAL SHORTING OF THE AFT PRESSURE BULKHEAD CONNECTOR. ALSO DISCOVERED THAT THE ELEVATOR ELE CTRIC TRIM SERVO WIRES THAT RUN THROUGH THE SAME CONNECTOR, WERE SHORTED AND GETTING POWER FROM THE STROBE/NAV LIGHT CI RCUIT BREAKERS THEREBY MAKING THE TRIM SERVO ALWAYS POWERED AND UNABLE TO BE DEENERGIZED BY SECURING THE PROPER TRIM CIR CUIT BREAKER. SAFETY OF FLIGHT ISSUE. IN THE PREVIOUS 30 DAYS, THIS A/C HAD AT LEAST 4 DIFFERENT ELECTRIC ELEVATOR TRI M DISCREPANCIES THAT APPEARED TO BE INTERMITTENT AND MIGHT HAVE BEEN CAUSED BY THIS ELECTRICAL FAULT. 2 L 7 2 4T RT A24CE 2002010200053 20020102 00053 SO 2002 1 2 C2XA01TY225 1 20020101 A 3350 20131A BATTERY EMB 135 EMB135ER 3260203 SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27506 3772 1435 145206 TYS During a scheduled inspection, the emergency overhead lights at both exit rows was found not working. Maintenance r emoved and replaced the #3 Emergency light battery, I.A.W.-EMB-135-MM-33-50-04, operational checks good. Aircraft releas ed to service. 2 L 7 2 4F RT T00011AT 2002010200145 20020102 00145 SO 2002 1 2 LR7A02001 1 20020101 A 2750 C708893 BRAKE ASSY LKHEED 382 382G 526414U SO FS 600 LEAKING A LR7A A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 AL 03 405LC 5364 5025 DURING CLIMB OUT OF OKO FLIGHT CREW REPORTED LOSS OF UTILITY HYDRAULIC SYSTEM PRESSURE. ACCOMPLISHED LANDING GEAR MANUA L EXTENSION AND MANUAL FLAP SETTING. FLIGHT DIVERTED TO NJA AND LANDED WITHOUT INCIDENT.FOUND FLAP DRIVE BRAKE ASSY LEA KING. REPLACED BRAKE ASSY IAW MM SMP 581-27-50, PG 215. OPS AND LEAK CHECK NORMAL. 2 H 7 4 4T A1SO 2002012200157 20020122 00157 NM 2002 1 22 02FDEA00001 1 20020102 A 3211 AYG72991 BOLT DOUG MD11 MD11F 3023600 NM LANDING GEAR LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 CTR L/G TRUNNION FITTING LT & RT AFT BOLT LOOSE. CTR L/G TRUNNION FITTING LT & RT AFT BOLT REMOVED. GENERAL VISUAL INS P CARRIED OUT AND FOUND SATISFACTORY. CTR L/G TRUNNION FITTING LT & RT AFT BOLT INSTALLED AND NUT REMOVED AND REPLACED AS PER MM 32-15-01-4. 2 L 7 3 4F RT A22WE 2002010300099 20020103 00099 SO 2002 1 3 LR7A02002 1 20020103 A 5311 WEB LKHEED 382 382G 526414U SO FS 924 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 504 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB0505 FOUND RH FS 924 BULKHEAD WEB CRACKED AT RBL 60, WL 250.REPAIRED IAW S RM SMP 51-140-17. NR 2009. 2 H 7 4 4T A1SO 2002010300100 20020103 00100 SO 2002 1 3 LR7A02003 1 20020103 A 5311 WEB LKHEED 382 382G 526414U SO FS 902 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 504 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB0505 FOUND LH FS 902 BULKHEAD WEB CRACKED AT LBL 60, WL 238.REPAIRED IAW S RM SMP 51-140-17. NR 2023. 2 H 7 4 4T A1SO 2002010300116 20020103 00116 EA 2002 1 3 COMA0260018 1 20020101 A 7931 6087T04P05 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 912CA 8906 7011 807407 FLIGHT 5958 LEFT ENGINE LOST OIL PRESSURE I.F.S.D.COULD NOT DUPLICATE DISCREPANCY - REPLACED THE ENGINE OIL PUMP FOR TRO UBLE SHOOTING. 2 L 7 2 4F 4 F RT A21EA E15NE 2002010300123 20020103 00123 EA 2002 1 3 COMA0260023 1 20020101 A 5610 NP1393212 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA R/H BROKEN A COMA H DEACTIVATE SYST/CIRCUITS O OTHER DE DESCENT 1 SO 01 954CA 14421 7100 FLIGHT 5956 COPILOTS WINDSHIELD SHATTERED.REPLACED COPILOTS WINDSHIELD. 2 L 7 2 4F RT A21EA 2002010300124 20020103 00124 EA 2002 1 3 COMA0260024 1 20020101 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA R/H INOPERATIVE A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 811CA 3794 7380 FLIGHT 5953 R/H SPOILERON CAUTION MESSAGE, NO TRAVEL INDICATED ON SYN PAGE.REPLACED THE R/H SPOILERON OUTBD PCU. 2 L 7 2 4F RT A21EA 2002010300126 20020103 00126 EA 2002 1 3 COMA0260026 1 20020102 A 2710 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 932CA 7038 FLIGHT 5763 AILERON CONFIG WARNING DURING T/O.RESET TRIPPED AILERON CIRCUIT BREAKER. 2 L 7 2 4F RT A21EA 2002010300138 20020103 00138 NE 2002 1 3 NACA20020001 2 20020102 A 7230 356994 CYLINDER PWA CB3 DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE #1 CRACKED A NACA E ENGINE SHUTDOWN K FLUID LOSS DE DESCENT 1 AL 03 779TA 677 677 P32778 45529 P32778 DISCREPANCY: Shut down #1 engine at 2337Z due to excessive oil loss.CORRECTIVE ACTION: Replaced #1 cylinder on the #1 en gine. 2 L 7 4 4R 4 R A781 5E8 2002010400021 20020104 00021 WP 2002 1 4 CALA0200001 1 20020102 A 3350 FUSE DOUG DC9 DC982 3022082 WP BATT CHARGER BLOWN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND SEAT MOUNTED EMERGENCY LIGHTS AT ROW 5-12 INOPERATIVE. MAINTENANCE FOUND FUSE BLOWN IN BATTERY CHARGER AND WIRING AT ROW 5 SHORTED TO THE SEAT TRACK. REPAIRED WIRING IAW STANDARD WIRING PRACTICES. REPLACED FUSE IAW MM 33-51 -00. 2 L 7 2 4F A6WE 2002010400022 20020104 00022 NM 2002 1 4 CALA0200002 1 20020102 A 5414 SKIN BOEING 737 7373T0 1384582 NM #2 ENG PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND THE #2 ENGINE PYLON ACCESS PLATE #5824R CUTOUT CRACKED AT FORWARD UPPER AND AFT LOWER AREAS. THE CRACKS WERE 1.6" LONG. A DOUBLER AND ANGLE WERE INSTALLED IAW ECRA 5430-01204. 2 L 7 2 4F RT A16WE 2002010800099 20020108 00099 NM 2002 1 8 F3LA200100150 1 20020104 A 5320 INTERCOSTAL BOEING 737 737228 13844AG NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL BENT AND CRACKED AT STA 500, STR 26-L. FABRICATED AND INSTALLED REPLA CEMENT INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2002010900116 20020109 00116 NM 2002 1 9 F3LA200200001 1 20020104 A 5315 FLOORBEAM BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM CORRODED AT FLOOR PANEL SPLICE, STA 770, LBL 2.5. FABRICATED AND INSTAL LED REPAIR PER SRM 53-10-1 AND 53-10-5. 2 L 7 2 4F RT A16WE 2002010400075 20020104 00075 NM 2002 1 4 SWAA020001 1 20020101 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 651SW 27721 EEPLS COVER MISSING AT MID CABIN. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002010900117 20020109 00117 NM 2002 1 9 F3LA200200002 1 20020103 A 5315 FLOORBEAM BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED CARGO BEAM CORRODED AT FLOOR PANEL SPLICE, STA 770, RBL 8. FABRICATED AND INSTALL ED REPAIR PER SRM 53-10-1, 53-10-3 AND 53-10-5. 2 L 7 2 4F RT A16WE 2002011500091 20020115 00091 NM 2002 1 15 02FDEA00007 1 20020103 A 3211 AYG72991 BOLT DOUG MD11 MD11F 3023600 NM CTR LANDING GEAR LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CENTER LAND GEAR LT TRUNNION BOLTS LOOSE. REMOVED AND REPLACED BOLTS PER MM 32-15-01-4. 2 L 7 3 4F RT A22WE 2002011500092 20020115 00092 NM 2002 1 15 02FDEA00008 1 20020103 A 3211 AYG72991 BOLT DOUG MD11 MD11F 3023600 NM CTR LANDING GEAR LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CENTER LAND GEAR RT TRUNNION BOLTS LOOSE. REMOVED AND REPLACED BOLTS PER MM 32-15-01-4. 2 L 7 3 4F RT A22WE 2002010400111 20020104 00111 EU 2002 1 4 MTNA200201 1 20020103 A 3230 ACM28982 RELIEF VALVE FOKKER F27 F27MK500 4990629 EU A MTNA D RETURN TO BLOCK O OTHER CL CLIMB 1 SO 33 717FE 122 10455 DURING CLIMB OUT FROM SGF. THE RIGHT MLG AND NLG WOULD NOT RETRACT, PNEUMATIC PRESSURE HAD DROPPED TO 400 PSI. THE CREW ELCETED TO RETURN TO SGF. WHEN THE CREW SELECTED GEAR DOWN THE PRESSURE BEGAN TO INCREASE AND WAS AT 1000 PSI AT SHUT DO WN. 2 H 7 2 4T A817 2002010400122 20020104 00122 EU 2002 1 4 MTNA20021 1 20020103 A 3200 ACM28982 RELIEF VALVE FOKKER F27 F27MK500 4990629 EU A MTNA D RETURN TO BLOCK O OTHER CL CLIMB 1 SO 33 717FE 122 10455 DURING CLIMB OUT FROM SGF. THE RIGHT MLG AND NLG WOULD NOT RETRACT, PNEUMATIC PRESSURE HAD DROPPED TO 400 PSI. THE CREW ELECTED TO RETURN TO SGF. WHEN THE CREW SELECTED GEAR DOWN THE PRESSURE BEGAN TO INCREASE AND WAS AT 1000 PSI. AT SHUT D OWN. 2 H 7 2 4T A817 2002010400134 20020104 00134 WP 2002 1 4 MWEA020003 1 20020104 A 5340 9910073 WEB DOUG DC9 DC981 3022081 WP STATION 95 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 1/2 INCH CRACK ON CEILING IN NOSE GEAR WHEEL WELL AREA RIGHT HAND TUNNEL AT STATION 95 -- CUT OUT DAMAGED SECTION OF W EB. FABRICATED, DRILLED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2002010400135 20020104 00135 WP 2002 1 4 MWEA020004 1 20020104 A 5340 59366093 SPLICE DOUG DC9 DC981 3022081 WP LONG. 28 & 27 LT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 CARGO TIE DOWN TRACK AND SPLICE CORRODED BETWEEN FUSELAGE 1231 AND 1211 AND LONGERON 28 AND 27 LEFT -- REMOVED CORROSI ON, FABRICATED AND INSTALLED SPLICE. 2 L 7 2 4F A6WE 2002010400136 20020104 00136 WP 2002 1 4 MWEA020005 1 20020104 A 5750 99359328 SKIN DOUG DC9 DC981 3022081 WP STATION 47 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 RIGHT HAND FLAP STATION 47 RIB TO UPPER SKIN, ATTACH TEE HAS EXFOLIATION CORROSION -- REMOVED, FABRICATED AND INSTALLE D RUB STRIPS AND TEE. 2 L 7 2 4F A6WE 2002010700002 20020107 00002 NM 2002 1 7 SWAA020004 1 20020102 A 5330 6545765 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 INCHES AT BS 510, STR 12L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002010700003 20020107 00003 NM 2002 1 7 SWAA020005 1 20020103 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FWD CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 500C PLUS 3 TO 500C PLUS 18, LBL 18. REMOVED AND REPLA CED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2002010700004 20020107 00004 NM 2002 1 7 SWAA020007 1 20020102 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 716SW 27850 DURING SCHEDULED CHECK, FOUND EEPLS COVERS CRACKED AT ROWS 2, 3, 17, 7, 16, 18, 20, 21, 22 AND 13. REMOVED AND REPLACED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2002010700005 20020107 00005 NM 2002 1 7 SWAA020009 1 20020102 A 5754 65C266022 SLAT BOEING 737 7373T5 1384608 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT WEDGE LOWER SKIN CRACKED AT OUTBOARD END. REMOVED AND REPLACED NR 5 L/E SLAT PERMM. 2 L 7 2 4F RT A16WE 2002010700030 20020107 00030 SO 2002 1 7 C2XA01TY224 1 20020101 A 3350 78812 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27506 145206 TYS DURING A SCHEDULED INSPECTION, THE NR 4 (SEAT 8) EMERGENCY LIGHT STRIP WAS FOUND NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE NR 4 LIGHT STRIP, IAW EMB-135-MM-33-50-12. OPERATIONAL CHECKS GOOD. AIRCRAFT RELEASED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002010700031 20020107 00031 SO 2002 1 7 C2XA01TY226 1 20020101 A 3260 852701 PROXIMITY SWITCH EMB 135 EMB135LR 3260305 SO NLG CRACKED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 14514 3057 145303 TYS AT TAKEOFF THE LANDING GEAR/GROUND FAIL MESSAGE INDICATOR CAME ON. CREW RETURNED AND MAINTENANCE REMOVED AND REPL ACED THE NLG WOW PROXIMITY SWITCH AND THEN ON SECOND ATTEMPT THE SWITCH HAD TO BE ADJUSTED TO THE TARGET. THE OPS CHECK WERE GOOD IAW EMB 135MM 32-63-05. AIRCRAFT WAS RELEASED. 2 L 7 2 4F RT TOOO11AT 2002010700047 20020107 00047 EU 2002 1 7 CHQ00085 1 20020102 A 3231 DOOR SAAB SF340 SF340A 7850100 EU LT MLG OUT OF ADJ A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 19 019 GEAR WOULD NOT RETRACT. ADJUSTED LT MAIN GEAR DOOR, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002010700048 20020107 00048 EU 2002 1 7 CHQ00086 1 20020102 A 3231 DOOR SAAB SF340 SF340A 7850100 EU LT MLG OUT OF RIG A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 19 019 GEAR WOULD NOT RETRACT. ADJUSTED LT GEAR DOOR RIGGING AND GEAR SWING GOOD. 2 L 7 2 4T RT A52EU 2002010700049 20020107 00049 SO 2002 1 7 CHQ00087 1 20020102 A 3260 PROXIMITY SWITCH EMB 145 EMB145 3260210 SO LANDING GEAR DIRTY A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 297 145522 CREW RETURNED TO FIELD DUE AUTO PRESSURIZATION INOP. DECIDED TO RAISE GEAR AGAIN AND TRY MANUAL PRESS, GOT LANDING GEAR DISAGREE AND COULD NOT GET GEAR BACK UP. RESET A/C AND CLEANED ALL PROX SWITCHES ON THE LANDING GEAR. TEST FLIGHT GOO D FOR GEAR AND PRESSURIZATION. 2 L 7 2 4F RT T00011AT 2002010700059 20020107 00059 NE 2002 1 7 CG8A20020001 2 20020104 A 7200 378200 PUMP BOEING 727 727223 1384074 NM PWA JT8 JT8D15A 52051 NE SHEARED A C8GA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SO 15 898AA 2617 22014 700574 Flt 707 from DEN to TOL. During cruise level at FL 330 #3 engine flame out. Oil pressure and quantity as well as N1 and N2 were normal. Descended to two engine cruise altitude and conducted engine failure shutdown checklist and all indicati ons were normal, attempted one engine restart without success. Notified ATC, continue to Toledo. Declared an emergency w ith Toledo approach as a precaution and landed without incident. Investigation found the #3 engine driven fuel pump shaf t sheared. Replaced the #3 fuel pump, engine run and leak check good IAW MM 73-11-1 and 71-00-117. Aircraft returned to service. 2 L 7 3 4F 4 F A3WE E2EA 2002010700068 20020107 00068 EU 2002 1 7 QXEA00002 1 20020102 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 11159 SEA- EMERGENCY EXIT SIGN ABOVE GALLEY INOP IN ARM POSITION. MAINTENANCE FOUND A BROKEN WIRE AT THE EXIT SIGN PLUG. REP LACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002010700108 20020107 00108 EA 2002 1 7 COMA0260027 1 20020103 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER LD LANDING 1 SO 01 984CA 7171 FLIGHT 5598 - FLAPS FAILED AT 28 DEGREES AFTER LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002010700109 20020107 00109 EA 2002 1 7 COMA0260028 1 20020103 A 2840 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 987CA 7199 FLIGHT 5371 - L/H FUEL QUANTITY INDICATION FAILED.DEFERRED MAINT. PER M.E.L. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002010700110 20020107 00110 EA 2002 1 7 COMA0260031 1 20020106 A 3230 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS CL CLIMB 1 SO 01 912CA 7011 FLIGHT 5448 - LANDING GEAR DISAGREE MESSAGE.CLEANED MOISTURE FROM THE NLG SELECTOR VALVE ELECTRICAL CONNECTOR. 2 L 7 2 4F RT A21EA 2002010700111 20020107 00111 EA 2002 1 7 COMA0260030 1 20020105 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 933CA 7040 FLIGHT 5839 CABIN DOOR OUTER HANDLE MESSAGE.COULD NOT DUPLICATE OPERATED DOOR AND PRESSURIZED AIRCRAFT. NO DEFECTS. 2 L 7 2 4F RT A21EA 2002010700112 20020107 00112 EA 2002 1 7 COMA0260029 1 20020105 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 982CA 7168 FLIGHT 5480 EMERGENCY FLOOR PATH LIGHTING AFT OF ROW 9 IS INOPERATIVE.CLEANED WIRE CONNECTION AT ROW 9, SYSTEM TEST OK. 2 L 7 2 4F RT A21EA 2002010700113 20020107 00113 WP 2002 1 7 MWEA020032 1 20020107 A 5310 5912365501 FRAME DOUG DC9 DC981 3022081 WP STATION 693 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 STATION 693 FRAME AT LONGERON 17 LEFT IS GOUGED -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002010700114 20020107 00114 WP 2002 1 7 MWEA020033 1 20020107 A 5310 5911447515 FRAME DOUG DC9 DC981 3022081 WP STATION 769 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 STATION 769 FRAME AT LONGERON 17 LEFT IS GOUGED -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002010700115 20020107 00115 WP 2002 1 7 MWEA020034 1 20020107 A 5310 991960421 BRACKET DOUG DC9 DC981 3022081 WP STATION 1257 RT. MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 FUSELAGE FRAME TO FLOOR BRACKET HAS ONE MISSING FASTENER AND HOLE THROUGH FRAME IS MISDRILLED AT STATION 1257 RIGHT -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002010700116 20020107 00116 WP 2002 1 7 MWEA020036 1 20020107 A 5330 5911401179 SKIN DOUG DC9 DC981 3022081 WP STATION 120 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 COMPLY WITH CARRY OVER NUMBER 5843, DENT AT STATION 120 LEFT HAND SIDE BETWEEN 18 AND 19 LEFT. CLASS 2 IAW SRM 53-04 FIG . 38 -- FABRICATED AND INSTALLED REPAIR DOUBLER. CARRY OVER NUMBER 5843 COMPLIED WITH. 2 L 7 2 4F A6WE 2002010700117 20020107 00117 WP 2002 1 7 MWEA020037 1 20020107 A 5330 5911401179 SKIN DOUG DC9 DC981 3022081 WP STATION 133 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 COMPLY WITH CARRY OVER NUMBER 5844, DENT STATION 133 LEFT HAND SIDE BETWEEN LONGERON 18 LEFT AND 19 LEFT, CONDITION 2, R EFERENCE SRM 53-04, FIG. 38 -- FABRICATED AND INSTALLED REPAIR DOUBLER. CARRY OVER NUMBER 5844 COMPLIED WITH. 2 L 7 2 4F A6WE 2002010700118 20020107 00118 WP 2002 1 7 MWEA020038 1 20020107 A 5210 59101419 PAN DOUG DC9 DC981 3022081 WP FWD CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 1 1/4 INCH CRACK INDICATION OF FORWARD EDGE OF FORWARD CARGO DOOR INNER PAN, IN RADIUS. CONFIRMED BY HFEC. LOCATION OF CRACK IS NEAR DOOR UPLATCH CAM -- STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002010700119 20020107 00119 WP 2002 1 7 MWEA020039 1 20020107 A 5750 5930479 ANGLE DOUG DC9 DC981 3022081 WP STATION 47 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 LEFT HAND FLAP INTERNAL AT STATION 47 HAS RIB ANGLE ON THE INBOARD SIDE WITH EXFOLIATION CORROSION -- REMOVED, FABRICA TED AND INSTALLED RIB ANGLE. 2 L 7 2 4F A6WE 2002010700120 20020107 00120 WP 2002 1 7 MWEA030040 1 20020107 A 5740 9936314503 DOUBLER DOUG DC9 DC981 3022081 WP STATION XIS 194 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 LEFT WING LEADING EDGE INTERNAL DOUBLER IS CRACKED AT STATION XIS 194 -- REMOVED, FABRICATED AND INSTALLED INTERNAL DO UBLER. 2 L 7 2 4F A6WE 2002010700134 20020107 00134 WP 2002 1 7 MWEA020035 1 20020107 A 5310 2913044501 GUSSET DOUG DC9 DC981 3022081 WP STA 541 LONG 28R CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 GUSSET CORROSION AT STATION 541, LONGERON 28 RIGHT -- REMOVED CORROSION. REMOVED, FABRICATED AND INSTALLED NEW GUSSET. 2 L 7 2 4F A6WE 2002010700135 20020107 00135 WP 2002 1 7 MWEA020017 1 20020107 A 5311 991224644 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FUSELAGE FORMER CRACKED BELOW LONGERON 15 RIGHT VIEW FROM FORWARD SIDE OF FUSELAGE FRAME 1038. REMOVED AND REPLACED FORM ER. 2 L 7 2 4F A6WE 2002010700136 20020107 00136 WP 2002 1 7 MWEA020018 1 20020107 A 5313 591142811 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 22 RIGHT HAS CHAFE DAMAGE ON UPPER LEG (VIEW THROUGH RIGHT THRUST REVERSER BY PASS DOOR). FABRICATED AND INSTA LLED LONGERON SECTION, LONGERON SPLICE AND NEW STRAPS. REMOVED CORROSION FROM SHOVEL CLIP AND REINSTALLED. 2 L 7 2 4F A6WE 2002010700137 20020107 00137 WP 2002 1 7 MWEA020019 1 20020107 A 5320 99578283 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 WEB AT GALLEY SERVICE DOOR, FROM STATION 150 TO STATION 200, IS CORRODED AT FORWARD SIDE OF SERVICE DOOR OPENING AND AFT SIDE OF SERVICE DOOR OPENING. FABRICATED AND INSTALLED WEB. 2 L 7 2 4F A6WE 2002010700138 20020107 00138 WP 2002 1 7 MWEA020020 1 20020107 A 5311 995774017 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 KEEL AREA FRAME AT STATION 637 IS CRACKED AT OUTBOARD END ON LEFT SIDE. FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2002010700139 20020107 00139 WP 2002 1 7 MWEA020025 1 20020107 A 5411 995815429 SPAR DOUG DC9 DC932 3022066 WP PYLON DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 REMOVE PYLON SPAR WEB (P/N 9958154-29). THE WEB HAS OVERSIZED HOLES. REMOVED DOUBLER. FABRICATED NEW DOUBLER. INSTALLED WEB. 2 L 7 2 4F A6WE 2002010700140 20020107 00140 WP 2002 1 7 MWEA020026 1 20020107 A 5310 995815421 WEB DOUG DC9 DC932 3022066 WP RIGHT PYLON OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RIGHT AFT PYLON SPAR WEB (P/N 9958154-21) UPPER HOLES ARE OVERSIZED. -- FABRICATED AND INSTALLED WEB. 2 L 7 2 4F A6WE 2002010700141 20020107 00141 WP 2002 1 7 MWEA020027 1 20020107 A 5310 991224617 WEB DOUG DC9 DC932 3022066 WP AFT PYLON A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE AFT PYLON BULKHEAD HAS OVERSIZED HOLE WHERE THE UPPER PYLON STRAP ATTACHES TO IT. -- FABRICATED AND INSTALLED WEB AND DOUBLERS. 2 L 7 2 4F A6WE 2002010700142 20020107 00142 WP 2002 1 7 MWEA020028 1 20020107 A 5310 991224697 DOUBLER DOUG DC9 DC932 3022066 WP STATION 1038 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RIGHT AFT PYLON WEB DOUBLER P/N 9912246 AT STATION 1038 HAS CRACKS EMINATING FROM THE UPPER STRAP ATTACHMENT HOLES. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002010700143 20020107 00143 WP 2002 1 7 MWEA020029 1 20020107 A 5230 3914025502H FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 AFT CARGO DOOR BEAM NR 4 END FITTING CRACKED, AFT SIDE OF DOOR. REMOVED AND REPLACED NEW FITTING. 2 L 7 2 4F A6WE 2002010700144 20020107 00144 WP 2002 1 7 MWEA020030 1 20020107 A 5230 4920233505N PAN DOUG DC9 DC932 3022066 WP AFT CARGO DR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 AFT CARGO DOOR INNER PAN IS CRACKED UNDER NUMBER 2 AFT. WORKING CORROSION NRI 12570. -- FABRICATED REPAIR ANGLE AND IN STALLED REPAIR ANGLE AND FITTING. 2 L 7 2 4F A6WE 2002010700145 20020107 00145 WP 2002 1 7 MWEA020031 1 20020107 A 5230 3914025502N BRACKET DOUG DC9 DC932 3022066 WP AFT CARGO DR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 AFT CARGO DOOR BEAM #3 END FITTING CRACKED, AFT SIDE OF DOOR. -- REMOVED FITTING AND ANGLE SUPPORT BRACKET. LOCATED AN D DEBURRED NEW FITTING AND ANGLE SUPPORT BRACKET.INSTALLED END FITTING AND ANGLE SUPPORT BRACKET. 2 L 7 2 4F A6WE 2002010700152 20020107 00152 NM 2002 1 7 SWAA020002 1 20020101 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT AFT END. REMOVED AND REPLACED BULB PER MM. 2 L 7 2 4F A16WE 2002010700154 20020107 00154 WP 2002 1 7 ARWA20020107 1 20020105 A 7714 8DJ116WAY1 INDICATOR LKHEED 1011 1011385115 5265015 WP A ARWA E ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 SO 19 308GB 193U1133 LOG PAGE 21540. DISCREPANCY: #1 ENGINE STARTER ACCELERATES N3 TO 46% VERY RAPIDILY THEN CUTS OUT BEFORE FULL ENGINE LIGH T UP. CORRECTIVE ACTION: REMOVED AND REPLACED N3 INDICATOR IAW MM 77-12-03 OPS CK NORMAL IAW MM 71-00. AIRCRAFT RETURN T O SERVICE. 2 L 7 3 4F A23WE 2002010700156 20020107 00156 NE 2002 1 7 ARWA20020105 2 20020105 A 7532 563883 VALVE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE A ARWA O E OTHER ENGINE SHUTDOWN E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 19 1808E 671351 46105 671351 LOG PAGE 108167. DISCREPANCY:ON ATART UP WHEN # 2 ENGINE THROTTLE IS ADVANCED ENGINE SURGES AND VIBRATES. WHEN REVERSE I S SELECTED TR TRANSLATES AND BUCKET DEPLOYS BUT ENGINE DOES NOT ACCELERATE IN REVERSE. CORRECTIVE ACTION: REMOVED AND RE PLACED #2 ENGINE SURGE BLEED VALVE IAW MM 75-30-3, OPS CK NORMAL IAW MM 71-00. THRUST REVERSER OPS CK IAW MM 78-30-0 AFT ER SURGE BLEED VALVE CHANGE. AIRCRAFT RETURNED TO SERVICE 2 L 7 4 4F 4 F 4A25 1E8 2002010800039 20020108 00039 NM 2002 1 8 VNAA0201004 1 20020103 A 2400 DAU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 442JS 3060 DURING THE TAKE OFF ROLL, THE CREW RECEIVED AN AMBER BOXED NL EICAS AND ABORTED TAKE OFF AND RETURNED TO THE GATE. MAIN TENANCE INSPECTED AND RERACKED THE DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL JIC 24-00-00. OP ERATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT WAS RELESED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002012900043 20020129 00043 NM 2002 1 29 02FDEA00013 1 20020105 A 5314 KEELBEAM BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 KEEL BEAM LWR WEB IS CORRODED ON EDGE OF LIGHTNING HOLE AT BS 766. REMOVED AND REPLACED WEB PER SRM 53-30-1, 53-30-3. 2 L 7 3 4F RT A3WE 2002011600140 20020116 00140 NM 2002 1 16 02FDEA00014 1 20020105 A 5314 KEELBEAM BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 KEELBEAM LOWER WEB IS CORRODED ON EDGE OF LIGHTENING HOLE AT BS 748. REMOVED AND REPLACED PER SRM 51-40-02. 2 L 7 3 4F RT A3WE 2002010800053 20020108 00053 WP 2002 1 8 MWEA020002 1 20020104 A 5730 59127352 PANEL DOUG DC9 DC932 3022066 WP RT WING DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RIGHT WING OUTBOARD TRAILING EDGE PANEL HAS APPROXIMATELY 80 SQUARE INCHES OF DELAMINATION ON THE TOP AREA, INCLUDES MOS T OF THE TRAILING EDGE. REMOVED, LOCATED, DRILLED AND INSTALLED NEW TRAILING EDGE PANEL. 2 L 7 2 4F A6WE 2002010800054 20020108 00054 WP 2002 1 8 MWEA020006 1 20020104 A 5330 59114273 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 STATION 1010, RIGHT HAND SIDE FUSELAGE SKIN HAS A SMALL CRACK ORIGINATING FROM RIVET BETWEEN LONGERON 14 RIGHT AND 16 RI GHT. CUT OUT CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002010800055 20020108 00055 WP 2002 1 8 MWEA020007 1 20020104 A 5320 992348471 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CENTER FLOOR SUPPORT HAS LIGHT CORROSION AROUND SEVERAL FASTENER HOLES FROM STATION 192 TO 200. REMOVED CENTER FLOOR SU PPORT. DRILLED, TRIMMED AND INSTALLED NEW CENTER FLOOR SUPPORT. 2 L 7 2 4F A6WE 2002010800057 20020108 00057 NM 2002 1 8 SWAA020003 1 20020102 A 3350 2330127 LIGHT BOEING 737 7372H4 138448C NM SERVICE DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED PM CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2002010800058 20020108 00058 2002 1 8 SWAA020006 4 20020103 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 743SW 29279 DURING SCHEDULED C3 CHECK, FOUND FWD SVC AND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT PLAY OUT OF ADJUST. ADJUSTED SLID E PER MM. 2 L 7 2 4F RT A16WE 2002010800059 20020108 00059 NM 2002 1 8 SWAA020008 1 20020102 A 3350 57771 CAP BOEING 737 7373T5 1384608 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2002010800060 20020108 00060 NM 2002 1 8 SWAA020010 1 20020102 A 3350 6013211 BATTERY BOEING 737 7372H4 138448C NM CARGO BAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT BATTERY PACK INOP IN FWD CARGO. REMOVED AND REPLACED BATTERY PACK PER M M. 2 L 7 2 4F A16WE 2002010800096 20020108 00096 NM 2002 1 8 F3LA200100148 1 20020103 A 5321 FLOOR PANEL BOEING 737 737228 13844AG NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM PANEL CRACKED AND CORRODED ABOVE STRINGER 25-R AT STA 787. FABRICATED A ND INSTALLED REPLACEMENT PANEL PER BOEING DRAWING 69-43477 AND SRM 51-10-2 AND 51-30-2. 2 L 7 2 4F RT A16WE 2002010800101 20020108 00101 SO 2002 1 8 C2XA02CL001 1 20020103 A 3350 WIRE EMB 145 EMB145ER 3260211 SO CABIN LOOSE A C2XA O OTHER L NO TEST UK UNKNOWN 1 SW 27 15932 145015 CLE FLIGHT# 3154 THE CREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT WAS NOT ILLUMINATING WHEN TESTING.MAINTENANCE INSPE CTED AND RESECURED A LOOSE WIRE ON THE OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002010800110 20020108 00110 SO 2002 1 8 C2XA02CL002 1 20020104 A 3350 1317 BULB EMB 145 EMB145ER 3260211 SO CABIN BURNED OUT A C2XA O OTHER L NO TEST IN INSP/MAINT 1 SW 27 14925 145004 DURING A 2A INSPECTION MAINTENANCE FOUND THE EMERGENCY LIGHT AT ROW 3 WAS INOPERATIVE.MAINTENANCE REPLACED THE EMERGENCY LIGHT BULB AT ROW 3.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002010800111 20020108 00111 WP 2002 1 8 IXXA0200001 1 20020103 A 2910 AE2460101J0134 HYDRAULIC LINE DOUG DC8 DC863 302198A WP NR 3 ENGINE RUPTURED A IXXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 11 786AL 83366 1828 46121 EN ROUTE FROM TOL TO LAX, THE FLIGHT CREW NOTICED A DECLINE IN THE MAIN HYDRAULIC SYSTEM QUANTITY. THE FLIGHT CREW FOLL OWED COMPANY PROCEDURES AND CONTINUED TO LAX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT LOCATING A R UPTURED HYDRAULIC PRESSURE LINE ON THE NUMBER THREE ENGINE DRIVEN HYDRAULIC PUMP. MAINTENANCE REPLACED THE HYDRAULIC LI NE IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002010800116 20020108 00116 NM 2002 1 8 LCQ05 1 20020105 A 5753 6521631144 WEDGE BOEING 727 72721 1384003 NM T/E FLAP DAMAGED B RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 RIGHT WING OUTBOARD FWD FLAP T/E WEDGE COMPOSITE HAS DELAMINATION AND 17 FT 2 INCHES OF THE SECTION OF WEDGE MISSING AND 42 INCHES OF HONEYCOMB REMAINING. 2 L 7 3 4F A3WE 2002010800117 20020108 00117 EU 2002 1 8 MALA020101 1 20020102 A 5210 HANDLE SAAB SF340 340B 7860101 EU PAX DOOR OUT OF POSITION A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 408XJ 340B408 DURING CLIMBOUT ON FLIGHT 3064, MAIN DOOR HANDLE ANNUNCIATOR ILLUMINATED. QRH WAS WORKED AND RETURNED TO MSP. AIR RETU RN TO MSP. F/A NOTICED INDEX MARK WAS NOT LINED UP AND HANDLE DID MOVE. MAINTENANCE CLOSED PAX DOOR NOTED INDEX MARKS MATCHED, RAN AIRCRAFT AND PRESSURIZED TO 3.5 DIFF, NO FAULT NOTED. INSPECTED DOOR, NO DISCREPANCIES NOTED UNALIGNED IND EX MARKS AND PRESSURIZED AGAIN, AND DID NOT DUPLICATE DISCREPANCY. AC RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2002010800118 20020108 00118 NE 2002 1 8 MALA020102 2 20020103 A 7200 LF5071F ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 3 SEIZED A MALA O OTHER Y ENGINE STOPPAGE CL CLIMB 1 GL 15 519XJ E2344 ON TAKEOFF OF FLIGHT 3410 CREW HEARD A LOUD BAND FROM NR 3 ENGINE AND REPORTED THE NR 3 ENGINE FROZE UP, NO OTHER PARAME TER INDICATIONS WERE IDENTIFIED. CONTINUED TO DTW AND DECLARED EMERGENCY AND LANDED WITH NO PROBLEMS. COMPLETED TASK C ARD THREE ENGINE FERRY. MAINTENANCE REMOVED AND REPLACED NR 3 ENGINE ASSEMBLY P/N LF507-1F, S/N ON P07768, S/N OFF P077 70. 2 H 7 4 4F 4 F RT A49EU E6NE 2002010800119 20020108 00119 WP 2002 1 8 MWEA020008 1 20020104 A 5347 59101433 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 NUMBER 3 SET TRACK HAS HEAVY CORROSION FROM STATION 218 TO 248. CUT AND REMOVED SEAT TRACK. LOCATED, DRILLED AND INSTA LLED SEAT TRACK. 2 L 7 2 4F A6WE 2002010800120 20020108 00120 WP 2002 1 8 MWEA020009 1 20020104 A 5320 99100783 WEB DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 SUBFLOOR HAS SEVERAL AREAS OF BARE METAL AND RIVET HEAD WEAR MARKS FROM STATION 200 TO 218 BETWEEN NUMBER 2 SEAT TRACK A ND CENTER FLOOR SUPPORT. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002010800121 20020108 00121 WP 2002 1 8 MWEA020010 1 20020104 A 5311 5913596501 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FUSELAGE FRAME 1059 HAS CHAFE DAMAGE ON UPPER LEG AT LONGERON 21 RIGHT. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED, FIT, DRILLED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2002010800123 20020108 00123 WP 2002 1 8 MWEA020012 1 20020104 A 5320 992348467 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FLOORBOARD SUPPORT LOCATED JUST FORWARD OF NUMBER 4 SEAT TRACK FROM STATION 160 TO 200 HAS TWO AREAS OF CORROSION ON TOP SIDE AND SEVERAL AREAS OF CORROSION ON LOWER SURFACE OF FLANGE AROUND THE HOLES. REMOVED, LOCATED, DRILLED AND INSTALL ED FLOORBOARD SUPPORT. 2 L 7 2 4F A6WE 2002010800124 20020108 00124 WP 2002 1 8 MWEA020013 1 20020107 A 5320 992348461 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FLOORBOARD SUPPORT AT STATION 200 HAS CORROSION BEYOND LIMITS LOCATED BETWEEN CENTER FLOOR SUPPORT AND NR 3 SEAT TRACK. REMOVED AND REPLACED FLOOR SUPPORT. 2 L 7 2 4F A6WE 2002010800125 20020108 00125 WP 2002 1 8 MWEA020014 1 20020107 A 5320 992348463 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FLOORBOARD SUPPORT AT STATION 200 HAS CORROSION BEYOND LIMITS LOCATED BETWEEN NR 3 SEAT TRACK AND NR 4 SEAT TRACK. REMO VED AND REPLACED FLOOR SUPPORT. 2 L 7 2 4F A6WE 2002010800126 20020108 00126 WP 2002 1 8 MWEA020021 1 20020107 A 5311 9912246105 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 STATION 1038 RIGHT FRAME CAP (P/N 9912246-105) HAS TWO OVERSIZED HOLES WHERE THE AFT UPPER ENGINE PYLON STRAP ATTACHES. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002010800127 20020108 00127 WP 2002 1 8 MWEA020022 1 20020107 A 5311 9912246103 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 STATION 1038 RIGHT FRAME CAP (P/N 9912246-103) HAS TWO OVERSIZED HOLES WHERE THE AFT UPPER ENGINE PYLON ATTACHES. REPAI RED PER TELEX MWX-ORD-01-00570H 19 DEC 2001. 2 L 7 2 4F A6WE 2002010800128 20020108 00128 WP 2002 1 8 MWEA020023 1 20020107 A 5320 595602962 CHANNEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORROSION AROUND AND ON NUT PLATES LOCATED ON U-CHANNEL THAT'S ATTACHED TO FLOORBEAM 427 ABOVE FORWARD AT CARGO DOOR OPE NING. FABRICATED AND INSTALLED U-CHANNEL. 2 L 7 2 4F A6WE 2002010800129 20020108 00129 WP 2002 1 8 MWEA020024 1 20020107 A 5320 595602969 CHANNEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORROSION AROUND AND ON NUT PLATES LOCATED AT STATION 351 ON U-CHANNEL THAT'S RIVETED TO FLOORBEAM APPROXIMATELY 28 INCH ES AND 33 INCHES TO THE LEFT OF CENTER. REMOVED CHANNEL, LOCATED HOLES, INSTALLED NUT PLATES ON CHANNEL, AND INSTALLED CHANNEL. 2 L 7 2 4F A6WE 2002010800131 20020108 00131 WP 2002 1 8 MWEA020041 1 20020107 A 5753 993593210 ATTACH ANGLE DOUG DC9 DC981 3022081 WP T/E FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 RIGHT HAND FLAP STATION 47 RIB TO LOWER SKIN, ATTACH TEE HAS EXFOLIATION CORROSION. FABRICATED, LOCATED, DRILLED AND IN STALLED NEW TEE. 2 L 7 2 4F A6WE 2002010800132 20020108 00132 WP 2002 1 8 MWEA020042 1 20020107 A 5753 593590533 ATTACH ANGLE DOUG DC9 DC981 3022081 WP T/E FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 RIGHT HAND FLAP STATION 47 RIB TO AFT SPAR WEB ATTACH TEE HAS EXFOLIATION CORROSION. REMOVED, FABRICATED, LOCATED, DRIL LED AND INSTALLED TEE. 2 L 7 2 4F A6WE 2002010800133 20020108 00133 SO 2002 1 8 C2XA02CL003 1 20020104 A 4900 4950385 VALVE EMB 145 EMB145ER 3260211 SO APU DIRTY A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 14945 145049 CLE FLIGHT#3024 THE CREW REPORTED THE APU STARTED ON THE GROUND WITH STRONG FUEL SMELL FILLING THE CABIN.MAINTENANCE PLA CED THE APU ON MEL 49-00-00.MAINTENANCE REPLACED THE START FUEL CHECK VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WA S RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002010800134 20020108 00134 EU 2002 1 8 WRNA200200001 1 20020103 A 2400 977J1504 GENERATOR AIRBUS 300 A300B4203 3930306 EU UNSERVICEABLE A WRNA A H J UNSCHED LANDING DEACTIVATE SYST/CIRCUITS DUMP FUEL H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 05 820SC 154 #1 ENGINE GENERATOR WENT OFF LINE AND CREW DISCONNECTED CSD #1. GENERATOR OFF LIGHT ILLUMINATED WITH VOLDTS AND FREQ'S R EADING ZERO. APU SHUTDOWN WITH OIL LEVEL LIGHT ILLUMINATING. EMERGENCY PROCEDURES WERE FOLLOWED (FUEL DUMPED) A/C RETURN ED TO AIRPORT. LANDING NORMAL.CORRECTIVE ACTION: OIL SERVICE LEVEL CHECKED ON APU AND GROUND RUN OPERATED SATISFACTORY I /A/W 49-00. #1 GENERATOR PLACED ON MEL 24-11-01 DMI #2249 ASSIGNED. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT A35EU 2002010800137 20020108 00137 SO 2002 1 8 C2XA02CL004 1 20020106 A 2913 PV303211 PUMP EMB 145 EMB145LR 3260212 SO LEFT ENGINE FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 15912 1601 145439 MSP-CLE FLIGHT#3260 THE CREW REPORTED THE #1 HYDRAULIC SYSTEM FELL TO "O" QUANTITY DURING FLIGHT.THE AIRCRAFT DIVERTED T O DTW AND LANDED WITHOUT FURTHER INCIDENT.THE CREW REPORTED THE # 1 ENGINE HYDRAULIC PUMP FAILED AND LOST #1 HYDRAULIC S YSTEM ON ROLLOUT OF LANDING.MAINTENANCE INSPECTED AND REPLACED THE #1 ENGINE HYDRAULIC PUMP.OPERATIONAL CHECKS WERE GOOD .THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002010800143 20020108 00143 NM 2002 1 8 PCAA0201008 1 20020107 A 3350 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 13 819EX 016 LGA-FLIGHT 3551 CREW REPORTED EMERGENCY LIGHTS CYCLED ON DURING PUSHBACK AND WILL NOT GO OUT. MAINTENANCE INSPECTED SY STEM, INSTALLED GROUND POWER UNIT AND CHARGED SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002010800146 20020108 00146 EA 2002 1 8 COMA0260032 1 20020102 A 5346 60135006 BEAM CNDAIR CL600 CL6002B19 1900309 EA FS625.3 TO 640 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 716CA 7773 7250 THE ENGINE SUPPORT BEAM LOWER WEB WAS CRACKED AT THE L/H AND R/H SIDES.REPAIRED THE CRACKED LOWER WEB I/A/W REO 601R-53- 61-366 REV. C. 2 L 7 2 4F RT A21EA 2002010800147 20020108 00147 EA 2002 1 8 COMA0260033 1 20020107 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 959CA 13557 7116 EDDY CURRENT INSPECTION OF R/H LOWER WING ACCESS HOLES INDICATES 2 FLAWS AT 610BB.BLENDED OUT DAMAGE AND ROTO-PEENED I/A /W REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002010800148 20020108 00148 NM 2002 1 8 AWXA200200006 1 20020105 A 2751 BACC63BP16A24S7L PLUG BOEING 737 7373G7 1384595 NM WS 393 CORRODED A AWXA O OTHER F S FLT CONT AFFECTED AFFECT SYSTEMS DE DESCENT 1 WP 28 157AW 23779 PHX - EMERGENCY LANDING - FLT 0228 - "C" - DURING DECENT INTO PHX ENROUTE FROM AUS TRAILING EDGE FLAPS LOCKED OUT, AIRCR AFT MADE UNEVENTFUL LANDING AT SCHEDULED DESTINATION. MAINTENANCE TROUBLESHOT AND FOUND CONNECTOR (D275) FLAP POSITION T RANSMITTER CORRODED AT WING STATION 393. CONNECTOR WAS REPLACED AND OPERATIONALLY CHECKED GOOD IAW BMM 27-58-01. 2 L 7 2 4F RT A16WE 2002010800149 20020108 00149 EA 2002 1 8 COMA0260034 1 20020107 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 959CA 13557 7116 EDDY CURRENT INSPECTION OF R/H LOWER WING ACCESS HOLES INDICATES 2 FLAWS AT 640DB.BLENDED OUT DAMAGE AND ROTO-PEENED I/A /W REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002010800150 20020108 00150 EA 2002 1 8 COMA0260035 1 20020107 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 959CA 13557 7116 EDDY CURRENT INSPECTION OF R/H LOWER WING ACCESS HOLES INDICATES 1 FLAWS AT 640 CB.BLENDED OUT DAMAGE AND ROTO-PEENED I/ A/W REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002010800151 20020108 00151 EA 2002 1 8 COMA0260036 1 20020101 A 5350 6002307014 FITTING CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 973CA 12467 7146 RIGHT HAND HORIZONTAL STABILIZER VISOR FITTING CRACKED.REPAIRED I/A/W 601R-55-11-016. 2 L 7 2 4F RT A21EA 2002010800152 20020108 00152 EA 2002 1 8 COMA0260037 1 20020101 A 5346 6015300 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIPMENT BA CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 973CA 12467 7146 ENGINE SUPPORT BEAM CRACKED.REAPIRED DAMAGE I/A/W REO 601R-53-61-345. 2 L 7 2 4F RT A21EA 2002010900113 20020109 00113 EA 2002 1 9 COMA0260038 1 20020107 A 3234 7455021 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 408CA 1567 7440 FLIGHT 5687 - LANDING GEAR WOULD NOT RETRACT WHEN SELECTED UP. REPLACED THE LANDING GEAR CONTROL HANDLE ASSY. 2 L 7 2 4F RT A21EA 2002010800168 20020108 00168 WP 2002 1 8 MWEA020043 1 20020108 A 2730 5910412505 SPAR DOUG DC9 DC914 3022034 WP STA. XE 169 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 LEFT HAND ELEVATOR FORWARD SPAR HAS CRACK INDICATION VIEWED ON RADIOGRAPH "LK" AT APPROXIMATELY STATION XE 169 -- LOCA TED AND MARKED ENDS OF CRACK. INSTALLED REPAIR SPAR. REBALANCED LEFT HAND ELEVATOR. 2 L 7 2 4F A6WE 2002010800169 20020108 00169 WP 2002 1 8 MWEA020044 1 20020108 A 2730 5910412505 SPAR DOUG DC9 DC914 3022034 WP STA. XE 203 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 LEFT HAND ELEVATOR FORWARD SPAR HAS A CRACK INDICATION VIEWED ON RADIOGRAPH "LM" AT APPROXIMATELY STATION XE 203 -- LO CATED ENDS OF CRACK. FABRICATED AND INSTALLED REPAIR SPAR. REBALANCED LEFT HAND ELEVATOR. 2 L 7 2 4F A6WE 2002010800170 20020108 00170 WP 2002 1 8 MWEA020045 1 20020108 A 2730 5910412506 SPAR DOUG DC9 DC914 3022034 WP STA XE 105 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT HAND ELEVATOR FORWARD SPAR HAS A CRACK INDICATION VIEWED ON RADIOGRAPH "RG" AT APPROXIMATELY STATION XE 105 UPPER CAP LOWER SURFACE -- FABRICATED AND HEAT TREAT PARTS. INSTALLED REPAIR SPAR. REBALANCED RIGHT HAND ELEVATOR. 2 L 7 2 4F A6WE 2002010900058 20020109 00058 NE 2002 1 9 00008 2 20020107 A 7200 ENGINE LEAR 24 24D 5170311 CE GE CJ610 CJ6106 30006 NE LEFT FLAMED OUT E HAEA B EMER. DESCENT X ENGINE FLAMEOUT CR CRUISE 1 SW 05 299TW 24299 251679A DURING CLIMB THROUGH FLT LEVEL 43.8 LT ENGINE FLAMED OUT. AT FL250 AIRSTART PERFORMED AND CONTINUED FLT AT 370. 2 L 7 2 4J 4 J A10CE 1E16 2002011500089 20020115 00089 WP 2002 1 15 02FDEA00006 1 20020103 A 5753 ARC20011 SUPPORT DOUG DC10 DC1030F 3023504 WP T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 305FE 47870 CASTING CRACKED ON O/B SIDE OF LEFT O/B FLAP O/B SUPPORT. REMOVED AND REPLACED RIB ASSY, OUTBOARD CLOSURE, OUTBOARD FLA P PER DRAWING ARC 2217. 2 L 7 3 4F RT A22WE 2002010900067 20020109 00067 2002 1 9 02FDEA00009 4 20020103 A 3425 SYMBOL GENERATOR AIRBUS 310 A310203 3930313 EU COCKPIT INOPERATIVE A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 412FE 360 LOST F/O'S PRIMARY FLT AND NAV DISPLAY. EFIS SGU NR 2 INOP. RELEASED PER MEL 34-7. 2 L 7 2 4F RT A35EU 2002010900068 20020109 00068 NM 2002 1 9 02FDEA00010 1 20020104 A 2612 FIRE WARNING DOUG MD11 MD11F 3023600 NM COCKPIT ACTIVATED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 617FE 48748 2-2 ALERT BELL NR 2 THROTTLE TO IDLE AND LIGHT WENT OUT. ENGINE IND NORMAL. SHUTDOWN NR 2. 2 L 7 3 4F RT A22WE 2002010900069 20020109 00069 NM 2002 1 9 02FDEA00011 1 20020104 A 3211 BOLT DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE LANDING GEAR LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 DURING PFM NR 44 CHECK FOUND RT AFT MOUNTING BOLT OF CTR LANDING GEAR TRUNNION PIN PILLOW BLOCK LOOSE. 2 L 7 3 4F 4 F RT A22WE E31N3 2002010900070 20020109 00070 NM 2002 1 9 02FDEA00012 1 20020101 A 3211 BOLT DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE LANDING GEAR LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 DURING PFM NR 61 B-CK FOUND BOTH LT & RT AFT MOUNTING BOLT OF CTR LANDING GEAR TRUNNION PIN PILLOW BLOCK LOOSE. 2 L 7 3 4F 4 F RT A22WE E31N3 2002012200159 20020122 00159 NM 2002 1 22 02FDEA00015 1 20020101 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 DENT IN FRAME FLANGE BS 580, STR 23-24L. REPAIRED FRAME BS 580 BETWEEN STR 23 & 24L PER FEDEX EA 7-5310-62674. 2 L 7 3 4F A3WE 2002012200160 20020122 00160 NM 2002 1 22 02FDEA00016 1 20020101 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 DENT IN FRAME FLANGE. REPAIRED DENTED FRAME BS 500 2 INCHES BELOW STR 24R PER SRM 51-40-3 & FEDEX EA 7-5310-62673. 2 L 7 3 4F A3WE 2002011600141 20020116 00141 NM 2002 1 16 02FDEA00017 1 20020103 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 EXT FUSELAGE SKIN CHAFED AT BS 720D+13 INCHES AT STR 19L. REMOVED AND REPLACED SKIN PER SRM 53-30-3. 2 L 7 3 4F A3WE 2002011600142 20020116 00142 NM 2002 1 16 02FDEA00018 1 20020102 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 DENT IN FRAME I/B FLANGE BS 1050 BETWEEN STR 26-27R. REMOVED AND REPLACED FRAME PER SRM 51-40-3. 2 L 7 3 4F A3WE 2002010900071 20020109 00071 NM 2002 1 9 SWAA020031 1 20020107 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 EEPLS COVER MISSING AT OVER WING EMERGENCY EXIT. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002010900072 20020109 00072 NM 2002 1 9 SWAA020033 1 20020106 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 786SW 29811 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002010900073 20020109 00073 NM 2002 1 9 SWAA020035 1 20020107 A 5310 6546529 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED D CHECK, FOUND FUSELAGE WEB CRACKED AT BS 294, STR 12L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002010900074 20020109 00074 NM 2002 1 9 SWAA020036 1 20020107 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, LBL 5.4, WL 198 AND WL 201. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002010900075 20020109 00075 NM 2002 1 9 SWAA020038 1 20020106 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 3.5 INCHES LONG AT BS 738, STR 20L. REPAIRED SKIN PER SWA R A. 2 L 7 2 4F RT A16WE 2002010900076 20020109 00076 NM 2002 1 9 SWAA020039 1 20020106 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 10R. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2002010900077 20020109 00077 NM 2002 1 9 SWAA020040 1 20020107 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (6 EA) BETWEEN BS 480 AND BS 486, STR 10R. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2002011600143 20020116 00143 NM 2002 1 16 02FDEA00019 1 20020102 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 DENT IN FRAME I/B FLANGE BS 990 BETWEEN STR 23-24L. REMOVED AND REPLACED FRAME PER SRM 51-40-3. 2 L 7 3 4F A3WE 2002011600144 20020116 00144 NM 2002 1 16 02FDEA00020 1 20020102 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 DENT ON I/B FLANGE OF FRAME BS 950C BETWEEN STR 26-27L. *S/D* REMOVED AND REPLACED FRAME PER SRM 51-40-3. 2 L 7 3 4F A3WE 2002012200161 20020122 00161 NM 2002 1 22 02FDEA00021 1 20020101 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 DENT IN FRAME FLANGE BS 680, STR 24-25R. REPAIRED FRAME BS 680 BETWEEN STR 24R & 25R PER FEDEX EA 7-5310-62673. 2 L 7 3 4F A3WE 2002012200162 20020122 00162 NM 2002 1 22 02FDEA00022 1 20020101 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 DENT IN FRAME FLANGE BS 660, STR 23-24R. REPAIRED FRAME BS 660 BETWEEN STR 23R & 24R PER FEDEX EA 7-5310-62673. 2 L 7 3 4F A3WE 2002012200163 20020122 00163 NM 2002 1 22 02FDEA00023 1 20020101 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 DENT IN FRAME FLANGE BS 600, STR 22-25 LT. REPAIRED FRAME AT BS 600 BETWEEN STR 24L & 25L PER SRM 51-40-3 & PER FEDEX E A 7-5310-62674. 2 L 7 3 4F A3WE 2002012200164 20020122 00164 NM 2002 1 22 02FDEA00025 1 20020101 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 DENT IN FRAME FLANGE BS 560, STR 24L. REPAIRED FRAME BS 560 AT STR 24L PER SRM 51-40-3 & FEDEX EA 7-5310-62674. 2 L 7 3 4F A3WE 2002010900078 20020109 00078 NM 2002 1 9 02FDEA00026 1 20020106 A 5320 WEB BOEING 727 7272S2F 1384O81 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 TWO HOLES IN FLOOR WEB BS 1134, LBL 43-47, WL 208. 2 L 7 3 4F A3WE 2002011600145 20020116 00145 NM 2002 1 16 02FDEA00027 1 20020106 A 5320 WEB BOEING 727 7272S2F 1384O81 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 TWO HOLES IN FLOOR WEB BS 1134, LBL 24-26, WL 208. REMOVED AND REPLACED WEB PER SRM 51-40-2. 2 L 7 3 4F A3WE 2002012900045 20020129 00045 NM 2002 1 29 02FDEA00028 1 20020106 A 5320 WEB BOEING 727 7272S2F 1384O81 NM FUSELAGE PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 THREE PUNCTURES IN FLOOR WEB BS 1134 - 1138, RBL 43 - 47, WL 208. REMOVED AND REPLACED DOUBLER FOR WEB PER SRM 51-40-02 . 2 L 7 3 4F A3WE 2002011600146 20020116 00146 NM 2002 1 16 02FDEA00029 1 20020106 A 5320 WEB BOEING 727 7272S2F 1384O81 NM FUSELAGE PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 THREE PUNCTURES IN FLOOR WEB BS 1134-1138, RBL 24-26, WL 208. REMOVED AND REPLACED WEB PER SRM 51-40-2. 2 L 7 3 4F A3WE 2002010900092 20020109 00092 NM 2002 1 9 ABXA010658 1 20020103 A 3234 257T110315 MODULE BOEING 767 767231 1385131 NM COCKPIT FAULTY A ABXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 23 708AX 22571 EICAS MESSAGE GEAR DISAGREE DISPLAYED AND GEAR AMBER LIGHT ILLUMINATED WITH GEAR. GREEN DOWN LIGHT ILLUMINATED. ALSO E ICAS MESSAGE LANDING MONITOR DISPLAYED WITH LANDING GEAR UP AND LOCKED. DID GEAR RECYCLE AND OVERFLEW STATION. REPLACE D LANDING GEAR CONTROL LEVER MODULE ASSEMBLY IAW B767 MM 32-31-01-04. PERFORMED BITE CHECK ON PSEU. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2002010900093 20020109 00093 WP 2002 1 9 ABXA010659 1 20020104 A 2410 CAP DOUG DC8 DC863F 302198F WP NR 1 CSD LOOSE A ABXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 816AX 46093 LOSS ALL ENGINE OIL QUANTITY FROM NR 1 ENGINE OIL SYSTEM INFLIGHT. PRECAUTIONARY SHUTDOWN, CSD DISCONNECTED. ENGINE MA INTAINED OIL PRESSURE GREATER THAN 5 PSI AFTER SHUTDOWN. FOUND CSD INPUT SPLINE OVER FILL STANDPIPE CAP LOOSE. SECURED CAP AND PERFORMED ENGINE INSPECTION PER P&W MM 72-00. NO DEFECTS NOTED. RECONNECTED CSD. ENGINE RUN GOOD. 2 L 7 4 4F 4A25 2002011500105 20020115 00105 WP 2002 1 15 ARWA20020101 1 20020101 A 2130 LINE DOUG DC8 DC862 3021970 WP CABIN LOOSE A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 8968U 46069 UNABLE TO PRESSURIZE AFTER TAKEOFF. GROUND CHECK OK. AIRCRAFT RETURNED TO DNA AND LANDED UNEVENTFUL. FOUND LOOSE LINE AT RT FLOW CONTROL VALVE, TIGHTENED IAW NASI SYSTEM STC ST466CH, OPS CHECKED FOUND NORMAL. AIRCRAFT RETURN TO SERVICE. 2 L 7 4 4F 4A25 2002010900095 20020109 00095 WP 2002 1 9 ARWA20020102 1 20020103 A 3230 5615545503 CYLINDER DOUG DC8 DC863 302198A WP LT MLG INOPERATIVE A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 345JW 46042 UPON DEPARTURE FROM MIA, BOTH DOOR NOT LATCHED AND GEAR NOT LATCHED ILLUMINATED AFTER GEAR RETRACTION ALL CHECKLIST COMP LIED WITH. FOUND LEFT BOGIE TRIM CYLINDER INOP. REMOVED AND REPLACED LT BOGIE TRIM CYLINDER. OPS CHECK NORMAL IAW 32- 33-1. 2 L 7 4 4F 4A25 2002010900096 20020109 00096 WP 2002 1 9 ARWA20020103 1 20020103 A 3260 WIRE DOUG DC8 DC863F 302198F WP LANDING GEAR DAMAGED A ARWA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 19 441J 45988 UPON ENTERING A/C LANDING GEAR UNSAFE LIGHT ILLUMINATED. REPAIRED WIRE IAW MM 20-50-1. OPS CHECK GOOD IAW MM 33-41-0. 2 L 7 4 4F 4A25 2002012900101 20020129 00101 WP 2002 1 29 ARWA20020104 1 20020104 A 8010 2TL1161 SWITCH DOUG DC8 DC862 3021970 WP COCKPIT BROKEN A ARWA K NONE O OTHER TX TAXI/GRND HDL 1 SO 19 810BN 45905 WHILE STARTING ENGINE NR 4 STARTER SWITCH BROKE. REMOVED AND REPLACED NR 4 ENGINE STARTER SWITCH IAW MM 20-50-01. OPS CHECK ON ENGINE IDLE RUN UP IAW 71-00 FOUND NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002010900097 20020109 00097 WP 2002 1 9 ARWA20020106 1 20020105 A 3220 LANDING GEAR DOUG DC8 DC862 3021970 WP NLG VIBRATION A ARWA K NONE E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 19 8968U 46069 NOSE GEAR VIBRATION FELT AFTER LANDING. 2 L 7 4 4F 4A25 2002020400017 20020204 00017 NE 2002 2 4 ARWA20020108 2 20020106 A 7230 DIFFUSER DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE DAMAGED A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 19 8968U 60310 3617 46069 671368 NR 4 ENGINE SHUT DOWN IN FLIGHT DUE TO FIRE WARNING, POST FLIGHT INSPECTION FOUND 4 INCH HOLE BURNED IN DIFFUSER CASE. AIRCRAFT FERRY FLIGHT TO SINGAPORE. REMOVED AND REPLACED NR 4 ENGINE. PERFORMED ENGINE RUN. ALL PARAMETERS NORMAL. AIRC RAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2002010900098 20020109 00098 EU 2002 1 9 AWXA200200001 1 20020101 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 627AW 1383 66 PHX - EEL - C - EMERGENCY ESCAPE LIGHTS INOPERATIVE ON THE LEFT SIDE OF THE AIRCRAFT. MAINTENANCE REPLACED EMERGENCY PO WER SUPPLY UNIT 11WL, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002010900099 20020109 00099 NM 2002 1 9 AWXA200200002 1 20020103 A 3230 BACV10CD12 CHECK VALVE BOEING 737 7373Y0 1384671 NM LANDING GEAR BYPASSING A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 334AW 23747 AFTER TAKEOFF, WITH THE GEAR HANDLE IN THE UP POSITION THE RED NLG UNSAFE GEAR INDICATION LIGHT REMAINED ILLUM. THE LAN DING GEAR WAS RECYCLED TWICE ENDING WITH THE SAME RESULT. THE ACFT TURNED BACK TO PDX AND THE LANDING GEAR HANDLE WAS S ELECTED TO THE DOWN POSITION BOTH THE HYDRAULIC INDICATION AND LANDING GEAR INDICATION WERE NORMAL WITH 3 GREEN DOWN AND LOCKED LIGHTS. ACFT RETURNED TO BACK PDX WITHOUT ANY FURTHER DIFFICULTIES. MX INSPECTED THE ACFT AND FOUND NO EVIDENC E OF ANY HYDRAULIC LEAK OR OTHER APPARENT ABNORMALITY WITH THE NLG. TWO NOSE WHEEL STEERING CHECK VALVES WERE REPLACED, AND A RETRACTION CHECK AND LEAK CHECK WERE PERFORMED WITH NO FAULTS NOTED IAW BMM 32-51-00. 2 L 7 2 4F RT A16WE 2002010900100 20020109 00100 NM 2002 1 9 AWXA200200004 1 20020106 A 2781 WARNING SYSTEM BOEING 737 7373G7 1384595 NM COCKPIT MALFUNCTIONED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 155AW 23777 SNA - ABORTED TAKEOFF - FLT 264 - C - DURING TAKEOFF INITIATION ON RUNWAY AT SNA FLIGHT CREW RECEIVED SLAT DISAGREE LIGH T INDICATION. TAKEOFF WAS ABORTED AND AIRCRAFT TAXIED TO TAXIWAY WHERE MAINTENANCE CONTROL TALKED FLIGHT CREW THROUGH R ESET PROCEDURES. SYSTEM RESET OK AND AIRCRAFT CONTINUED ON TO SMF WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A16WE 2002010900101 20020109 00101 EU 2002 1 9 AWXA200200007 1 20020105 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 646AW 271 PHX - EEL - C - DURING INSPECTION ALL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. NOTE: AIRCRAFT HAS BEEN PARKED SIN CE 30 NOVEMBER, 2001. MAINTENANCE REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS 10WL-13WL, ZONES 221, 241, 242, AND 2 63 IAW AMM 33-51-38, OPERATIONAL CHECK WAS GOOD IAW T/C F1C33301. 2 L 7 2 4F RT A28NM 2002010900102 20020109 00102 NM 2002 1 9 AWXA200200008 1 20020106 A 3350 321440 BATTERY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 802AW 0924 PHX - EEL - C - DURING INSPECTION EMERGENCY POWER SUPPLY BATTERY WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D POWER SUPPLY BATTERY IAW AMM-33-51-38. 2 L 7 2 4F RT A28NM 2002010900103 20020109 00103 NM 2002 1 9 AWXA200200009 1 20020107 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 185AW 22652 PHX - EEL - C - DURING INSPECTION EMERGENCY LIGHT AT ROW 13 LT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED LIGHT ASSEMBLY AT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002010900104 20020109 00104 SO 2002 1 9 C2XA01TY227 1 20020108 A 2620 14523355403 LINE EMB 145 EMB145 3260210 SO EXTINGUISH SYS DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS, DURING A SCHEDULED 1C/2C INSPECTION, THE NR 2 ENGINE FIRE EXTINGUISHER LINE AT FRAME 70 WAS FOUND DENTED. MAINTENA NCE REMOVED AND REPLACED THE FIRE EXTINGUISHER LINE IAW-EMB-145-AMM-20-10-03. THE REPAIR PROCEDURES WERE SATISFACTORY A ND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002010900105 20020109 00105 SO 2002 1 9 C2XA01TY228 1 20020108 A 2620 14523355403 LINE EMB 145 EMB145 3260210 SO EXTINGUISH SYS DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS, DURING A SCHEDULED 1C/2C INSPECTION, THE NR 1 ENGINE FIRE EXTINGUISHER LINE AT FRAME 70 IN THE CARGO BAY WAS FOUND DENTED. MAINTENANCE REMOVED AND REPLACED THE LINE IAW EMB-145-AMM-20-10-03. REPAIR PROCEDURES WERE SATISFACTORY AND TH E AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2 L 7 2 4F RT T00011AT 2002010900106 20020109 00106 GL 2002 1 9 C2XA02IA001 2 20020104 A 7200 AE3007A ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 1 LEAKING A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 27523 145389 1696 IAH- FLIGHT NUMBER 3792 THE CREW NOTED SMOKE IN THE CABIN AND RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AN D REPLACED THE NUMBER ONE ENGINE, PERFORMED A OPERATIONAL AND LEAK CHECK. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TOOO11AT TE6CH 2002010900108 20020109 00108 NM 2002 1 9 2002UALA00004 1 20020102 A 5330 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT CABIN DECK PLATE CORRODED STATION 1681 LBL 12 - LBL4. MAJOR REPAIR ACCOMPLISHED.DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010900109 20020109 00109 NM 2002 1 9 2002UALA00005 1 20020102 A 5330 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT CABIN DECK PLATE CUT OUT FOR ACCESS AT STATION 1681 AND LBL 33. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010900110 20020109 00110 NM 2002 1 9 2002UALA00006 1 20020102 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 AFT PIT FRAME AT STATION 1420 STRINGER 26L DENTED. MAJOR REPAIR ACCOMPLISHED.REPAIR ANGLE FABRICATED AND INSTALLED UNDE R FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2002010900111 20020109 00111 SO 2002 1 9 C2XA02IA002 1 20020105 A 2750 3631101007 CONTROL HANDLE EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13908 145465 IAH- FLIGHT 3998 IN FLIGHT AFTER DEPARTURE A LANDING GEAR AURAL WARNING INDICATION CONTINUALLY SOUNDING. RECYCLED THE GEAR AND CONTINUED TO GET THE AURAL WARNING. RETURNED TO IAH WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE FLAP SELECTOR LEVER, PERFORMED A OPERATIONAL CHECK AND NO DEFECTS NOTED. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002010900112 20020109 00112 SO 2002 1 9 CHQ00088 1 20020104 A 3000 WARNING SYSTEM EMB 145 EMB145 3260210 SO COCKPIT ACTIVATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 275 145345 ICE CONDITIONS AND A/I INOP ON EICAS. ABORTED TAKEOFF AND CANCELLED FLIGHT. 2 L 7 2 4F RT T00011AT 2002010900114 20020109 00114 NM 2002 1 9 DHL2002742001 1 20020104 A 2611 SMOKE DETECTOR BOEING 727 727224 1384076 NM CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 746DH 22252 DURING SERVICE CHECK, FOUND SMOKE DETECTOR POSITION 5 INOP. SMOKE DETECTOR POSITION NR 5 INOP DEFERRED PER MEL 26-14-1 CAT C DMI 8187 REQUIRES SMOKE DETECTOR P/N 30-284-2. 2 L 7 3 4F A3WE 2002012300182 20020123 00182 NE 2002 1 23 GLBA2002001 2 20020103 A 7314 1143890425 PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 195GL 13448 913 UE195 LEFT LOW FUEL PRESSURE LIGHT ILLUMINATED. REPLACED FUEL PUMP, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2002010900128 20020109 00128 NM 2002 1 9 DL73K020006 1 20020101 A 3350 276005 FUSE BOEING 737 737232 1384475 NM CABIN OPEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 312DL 23084 EMERG LIGHTS ROW 5-9 AND LT AND RT OVERWING HATCH EXIT SIGNS INOP. REPLACED 1EA FUSE IN FWD AND AFT POWER SUPPLIES. SYS OP NOW NORMAL 2 L 7 2 4F RT A16WE 2002010900129 20020109 00129 NM 2002 1 9 DL73K020016 1 20020106 A 3040 5717623134 WINDOW 5717263134 BOEING 737 737232 1384475 NM RT_NO.2 CRACKED A DALA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 SO 27 322DL DL141 23094 R2 WINDOW OUTER PANE CRACKED DURING FLT. DIVERTED TO MCO_C/ARPLD R2 WINDOW AND HEAT CONTROLLER PER M.M. OPN NORMAL 2 L 7 2 4F RT A16WE 2002010900130 20020109 00130 NM 2002 1 9 DL72S020020 1 20020101 A 5500 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 518DA 21469 FOUND ON E2 LETTER CK 3/8 INCH CRACK VERT STAB OUTER SKIN APPROX 6 INCHES ABOVE 3RD FROM TOP VORTEX GENERATOR R/H SIDE. REPAIRED PER SRM 55-30-3. 2 L 7 3 4F A3WE 2002010900131 20020109 00131 NM 2002 1 9 DL72S020023 1 20020108 A 5700 ANGLE BOEING 727 727232 1384082 NM NBR 2 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 1/8 IN CRACK COVE SKIN ATTACH ANGLE BELOW TAI DUCT NBR 2 SLAT REPAIR PER MM 57-54-000-8 2 L 7 3 4F A3WE 2002011000017 20020110 00017 EU 2002 1 10 CHQ00089 1 20020105 A 7710 INDICATOR SAAB SF340 SF340A 7850100 EU COCKPIT ERRATIC A CHQA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 11 40 040 ERRATIC ENGINE INDICATIONS. GROUND RAN IN ALL MODES AND COULD NOT DUPLICATE. 2 L 7 2 4T RT A52EU 2002011000020 20020110 00020 WP 2002 1 10 MWEA020046 1 20020108 A 5313 5936027501 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 GOUGES AND LIGHT CORROSION AROUND FASTENERS IN LONGERON 29 RIGHT BETWEEN FUSELAGE SKIN 1079 AND 1098. BLENDED GOUGES AN D CORROSION. REPAIRED PER BOEING TELEX MWX-01D-02-00002H. INSTALLED 7 FASTENERS. 2 L 7 2 4F A6WE 2002011000027 20020110 00027 NM 2002 1 10 PCAA0201003 1 20020103 A 3060 7826893 BRUSH BLOCK DHAV DHC8 DHC8102 2809003 NM LT & RT INTERFERENCE A PCAA K NONE O OTHER CR CRUISE 1 EA 13 814EX 9948 56 318 PIT FLIGHT 3832. FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY IN FLIGHT, INCLUDING RIGHT FORWAR D FLOOR LEVEL, BOTH EXIT LIGHTS, AND PASSENGER DOOR EXIT LIGHT. MAINTENANCE CLEANED AND RESEATED CANNON PLUG ON EMERGEN CY LIGHTING CONTROL BOX. COULD NOT DUPLICATE PROBLEM. AIRCRAFT RETURNED TO SERVICE. PROBLEM REOCCURRED ON NEXT FLIGHT (3835) IN SYR AS EMERGENCY LIGHTS ILLUMINATING IN FLIGHT WHILE SELECTING PROP HEAT. MAINTENANCE CHECKED CANNON PLUG WI RING AND BATTERY PACKS IN WARDROBE. ALSO CHECKED CANNON PLUG CP9811-P34. NO DEFECTS FOUND. LEFT AND RIGHT BRUSH BLOCK S REPLACED FOR TROUBLESHOOTING. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002011000032 20020110 00032 NM 2002 1 10 PCAA0201007 1 20020105 A 3260 PROXIMITY SWITCH DHAV DHC8 DHC8102 2809003 NM MLG OUT OF POSITION A PCAA K NONE J WARNING INDICATION CL CLIMB 1 EA 13 851EX 343 PHL FLIGHT 3906. CREW REPORTED RIGHT MAIN AMBER GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION, RIGHT MAIN GEAR DOORS REMAINED OPEN. PER THE CREW CHECKLIST GEAR WAS CYCLED, GEAR RETRACTED, DOORS CLOSED THEN LEFT AND RIGHT MAIN GEAR DOORS OPENED AND REMAINED OPEN. MAINTENANCE INSPECTED AND FOUND PROXIMITY SWITCH WAS INTERFERING WITH OVER CENTER MECHANISM. AFT CENTER DOOR RIGGED IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL 32-10-21. PROXIMITY SWITCH RIGGED IN A CCORDANCE WITH DASH 8 MAINTENANCE MANUAL 32-61-50. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002011000034 20020110 00034 NM 2002 1 10 QXEA0200003 1 20020105 A 3260 PROXIMITY SENSOR DHAV DHC8 DHC8* NM LT MLG OUT OF ADJ A QXEA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 NM 09 402QX 4032 PDX - ON APPROACH TO IDA FROM PIH, LEFT MAIN LANDING GEAR SHOWED INTRANSIT ALONG WITH GEAR DOOR OPEN LIGHTS. AIRCRAFT D IVERTED TO PDX BY DISPATCH. ADJUSTED LEFT MAIN LANDING GEAR OUTBOARD PROX SENSOR. NO PARTS REPLACED. OPERATIONAL CHEC K GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002011000035 20020110 00035 NM 2002 1 10 QXEA0200004 1 20020103 A 5410 STRUT DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX - NR 1 ENGINE INBOARD LOWER THRUST STRUT IS GOUGED AND CHAFED. REPAIRED IAW DHC-8-200 RD 8-54-036. 2 H 7 2 4T RT A13NM 2002011000055 20020110 00055 NM 2002 1 10 SWAA020041 1 20020107 A 3220 6544625 ACTUATOR BOEING 737 7373H4 1384600 NM NLG W/W FAULTY A SWAA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 309SW 22948 DURING GEAR EXTENSION, NOSE GEAR LIGHT REMAINED RED, WARNING HORN SOUNDED. PLACED LEVER UP AND GEAR RETRACTED. PLACED LEVER DOWN, THREE GREEN LIGHTS AND NORMAL LANDING. REMOVED AND REPLACED NOSE GEAR UPLOCK ACTUATOR AND ADJUSTED RT NLG D OOR PER MM. 2 L 7 2 4F RT A16WE 2002011000056 20020110 00056 NM 2002 1 10 SWAA020043 1 20020108 A 5510 6547983 STIFFENER BOEING 737 7373H4 1384600 NM LT HORIZ CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED D CHECK, FOUND LT HORIZ STAB MAIN BOX INTERIOR L/E STIFFENER ON INTERSPAR WEB CRACKED AT STA 95. REPAI RED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2002011000057 20020110 00057 NM 2002 1 10 SWAA020044 1 20020107 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES LONG AT BS 360, STR 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002011000058 20020110 00058 NM 2002 1 10 SWAA020045 1 20020107 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES LONG AT BS 460, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002011000059 20020110 00059 NM 2002 1 10 SWAA020046 1 20020107 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES LONG AT BS 500, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002011000060 20020110 00060 NM 2002 1 10 SWAA020047 1 20020107 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 770, STR 14R AND BS 740, STR 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002011000072 20020110 00072 NM 2002 1 10 QXEA0200005 1 20020107 A 5270 SENSOR DHAV DHC8 DHC8* NM EMERGENCY EXIT MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 401QX 4031 BOI - IN FLIGHT, THE MASTER WARNING FOR THE FUSELAGE DOOR SYSTEMS CAME ON INTERMITTENTLY WHILE CLIMBING THROUGH 16,000 F T, AND WAS CONTINUOUS AT 24,000 FT. THE FUSELAGE DOORS SYSTEM PAGE INDICATED THE EMERGENCY EXIT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE COMPLIED WITH INSPECTION OF UPPER EMERGENCY EXIT PROXIMITY SENSOR. FOUND TO BE OKAY. CLEANED AND L UBED SENSOR PLUNGER. GROUND RAN AND PRESSURIZED AIRCRAFT. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002011000074 20020110 00074 NM 2002 1 10 QXEA0200006 1 20020104 A 5330 83010309001 DOUBLER DHAV DHC8 DHC8* NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 646 646 4050 PDX - THE ICE SHIELD ON THE RIGHT SIDE OF AIRCRAFT HAS TWO LARGE HOLES IN IT. MAINTENANCE REPAIRED DAMAGE TO THE ICE SH IELD BY PREPPING AND INSTALLING COMPOSITE REPAIRS IAW EA 6-53-47 AND RD 8-53-883. 2 H 7 2 4T RT A13NM 2002011000076 20020110 00076 EU 2002 1 10 RAIA00201001 1 20020103 A 3350 LIGHT AEROSP ATR42 ATR42300 8680920 EU PAX DOOR INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 423TE 119 MX-STL- PAX DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LAMP IAW ATR MM 33-50. 2 H 7 2 4T RT A53EU 2002011000095 20020110 00095 NM 2002 1 10 SWAA020011 1 20020103 A 3350 6556633 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 RIGHT OVERWING EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002011000099 20020110 00099 NM 2002 1 10 SWAA020032 1 20020107 A 2560 10107451 SIGN BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 OVERWING EMERGENCY EXIT SIGN LOOSE AT CENTER AISLE. SECURED SIGN PER MM. 2 L 7 2 4F A16WE 2002011000100 20020110 00100 2002 1 10 SWAA020034 4 20020107 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT PLAY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002011000101 20020110 00101 NM 2002 1 10 SWAA020037 1 20020106 A 3350 300432 LIGHT BOEING 737 7372T4 1384492 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND FWD LT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F A16WE 2002011000134 20020110 00134 NM 2002 1 10 PCAA0201009 1 20020108 A 5610 NP15790213 WINDOW DHAV DHC8 DHC8102 2809003 NM CAPTS SIDE CRACKED A PCAA K NONE Z SIGNIFICANT FAILURE REPORT NR NOT REPORTED 1 EA 13 981HA 10551 378 SYR-FLIGHT#3555. CREW REPORTED CAPTAINS SIDE WINDOW SHATTERED. MAINTENANCE REPLACED CAPTAINS SIDE WINDOW IN ACCORDANCE W ITH DASH 8 MAINTENANCE MANUAL 56-10-16. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002011000142 20020110 00142 EU 2002 1 10 02FDEA00030 1 20020108 A 2611 SMOKE WARNING AIRBUS 300 A300F4605R 3930327 EU COCKPIT ILLUMINATED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION AP APPROACH 1 SO 25 662FE 761 2-3 RED ECAM RECEIVED MAIN DECK CARGO SMOKE LIGHT ON. BLEED NR 1 FAULT. NO FIRE OR SMOKE. 1 PACK OFF. RELEASE PER MEL . 2 L 7 2 4F RT A35EU 2002011000143 20020110 00143 EU 2002 1 10 02FDEA00031 1 20020108 A 2120 SMOKE AIRBUS 300 A300F4605R 3930327 EU COCKPIT DETECTED A FDEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 662FE 761 2-4 AT GEAR RETRACT GOT AVIONICS SMOKE AND FUMES IN COCKPIT. COMPLIED WITH ECAM RED TABS. 2 L 7 2 4F RT A35EU 2002011400115 20020114 00115 NM 2002 1 14 02FDEA00032 1 20020108 A 5610 B275600101A WINDOW BOEING 727 72722 1384002 NM COCKPIT DEFECTIVE A FDEA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 148FE 19086 AFTER T/O ELECT FIRE BY CAPT'S SEAT. APPEARED TO BE WINDOW HEAT WIRE. REMOVED AND REPLACED SLIDING WINDOW, HARNESS, CI RCUIT BREAKER C153, TRANSFORMER T48 AND BACKSHELL OF CONNECTOR D9489. 2 L 7 3 4F A3WE 2002011000177 20020110 00177 NE 2002 1 10 DL72E020002 2 20020101 A 7230 COMPRESSOR BOEING 727 727247 138408F NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE STALLED A DALA C ABORTED TAKEOFF E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 830WA 57681 21482 700573 AT 70 KTS ON T/O, SEVERE COMPRESSOR STALL ON NR 2 ENGINE WITH 80 DEG CROSSWIND AND 20 KTS. CHECKED NR 2 ENGINE PER MM, NO DISCREPANCIES NOTED. ACTIVATED 6TH STAGE BLD PER MM. NO TROUBLE FOUND. 2 L 7 3 4F 4 F A3WE E2EA 2002011000178 20020110 00178 NM 2002 1 10 DL72E020008 1 20020103 A 3350 RPS1 POWER SUPPLY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 282WA 21484 ON LAYOVER, EMERGENCY LIGHTS FROM 27 AFT INOP INCLUDING 3 EXIT LIGHTS IN AFT CABIN. REPLACED POWER SUPPLY. 2 L 7 3 4F A3WE 2002011000179 20020110 00179 NM 2002 1 10 DL72E020009 1 20020103 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 282WA 21484 ON LAYOVER, RT OVERWING EMERGENCY LIGHT CENTER POSITION FLICKERING. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2002021500040 20020215 00040 EU 2002 2 15 AWXA200200013 1 20020109 A 2121 EVT3454H COOLING FAN AIRBUS 320 A320232 3930326 EU E/E BAY FAILED A AWXA H DEACTIVATE SYST/CIRCUITS E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 28 662AW 1274 LAS - SMOKE FUMES - FLT 729 - S - EN ROUTE FROM LAS TO ORD DURING TOP OF DESCENT FLIGHT CREW NOTICED AN UNUSUAL VIBRATIO N AND THEN A SLIGHT SMELL OF ELECTRICAL SMOKE, THE BLOWER AND EXTRACT FANS WERE TURNED OFF AND THE NOISE AND SMELL WENT AWAY. MAINTENANCE REMOVED AND REPLACED THE AVIONICS COOLING FAN IAW AMM 21-26-51. VENDOR REPAIR STATION CONFIRMED FAIL URE OF AVIONICS FAN S/N 4156, ENTRY TEST OF UNIT FOUND THE FAN SEIZED AND FURTHER TEARDOWN IDENTIFIED THE FRONT BEARINGS AS DISINTEGRATED. 2 L 7 2 4F RT A28NM 2002011000189 20020110 00189 EU 2002 1 10 AWXA200200015 1 20020109 A 3350 2514303 LENS AIRBUS 320 A320232 3930326 EU ZONE 240 MISSING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 CMH - EEL - "C" - DURING INSPECTION R/H AFT OVERWING EXIT SIGN LENS COVER WAS DISCOVERED MISSING. MAINTENANCE REPLACED M ISSING LENS COVER AT R/H AFT OVERWING EXIT IAW 33-51-16-401. 2 L 7 2 4F RT A28NM 2002011000191 20020110 00191 SO 2002 1 10 C2XA02TY002 1 20020101 A 3350 20131A BATTERY EMB 135 EMB135ER 3260203 SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27506 3772 1435 145206 TYS During a scheduled inspection, the emergency overhead lights at both exit rows was found not working. Maintenance r emoved and replaced the #3 Emergency light battery, I.A.W.-EMB-135-MM-33-50-04, operational checks good. Aircraft releas ed to service. 2 L 7 2 4F RT T00011AT 2002011100001 20020111 00001 SO 2002 1 11 C2XA02IA003 1 20020109 A 3350 AD2047 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 57734 120199 IAH- MAINTENANCE, WHILE PERFORMING A SERVICE CHECK THE MECHANIC NOTED THAT THE MIDDLE CABIN EMERGENCY LIGHTS FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND MIDDLE EMERGENCY BATTERY PACK, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE 2 L 7 2 4T RT A31SO 2002011100002 20020111 00002 NM 2002 1 11 P2EA2002M001 1 20020110 A 2910 654496010 ACTUATOR BOEING 737 737297 1384480 NM CRACKED A P2EA O OTHER Z J SIGNIFICANT FAILURE REPORT WARNING INDICATION TX TAXI/GRND HDL 1 CE 05 005WM 22629 After Landing Lost A System Hydraulics upon exiting taxi way at MCI.Inspected and found the #1 Ground Spoiler actuator w ith crack. R&R #1 Ground Spoiler actuator IAW Boeing MM 27-62-101 op's check and leak checks good. 2 L 7 2 4F A16WE 2002011100003 20020111 00003 NM 2002 1 11 C1HA200183011 1 20020102 A 3350 6013211 BATTERY BOEING 727 7272S7 138407Z NM INOPERATIVE A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 FWD SEC OF EMERGENCY FLOOR TRACK LIGHTS OUT ACTION TAKEN: R & RD BATT PWR SUPPLY FOR FWD SEC OF FLOOR TRACK LIGHTS AS REQD OPS NORMAL 2 L 7 3 4F A3WE 2002011100004 20020111 00004 NM 2002 1 11 CALA0200003 1 20020105 A 5330 SKIN BOEING 737 7373T0 1384582 NM FWD CARGO DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17328 23458 INSPECTION FOUND A 1/2" CRACK IN FORWARD BAG BIN DOOR CUTOUT BETWEEN STRINGERS 24-25. REPAIRED IAW ECRA 5310-04013. 2 L 7 2 4F RT A16WE 2002011100005 20020111 00005 NM 2002 1 11 CALA0200004 1 20020108 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 380 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14324 23375 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 380, S17R. REPAIRED SKIN IAW SRM 53-00-01 AND 51-20-01. 2 L 7 2 4F RT A16WE 2002011100006 20020111 00006 NM 2002 1 11 CALA0200005 1 20020109 A 5320 SHEAR TIE BOEING 737 7373T0 1384582 NM STA 787 & 807 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14324 23375 INSPECTION FOUND BELLFRAME SHEAR TIES CORRODED AT STA 807 BETWEEN S27L AND S27R AND AT STA 787 BETWEEN S27R AND S26R. NE W SHEAR TIES WERE INSTALLED AT EACH LOCATION USING FILLER AND SUPPORT ANGLES IAW SRM 53-60-07. 2 L 7 2 4F RT A16WE 2002011100007 20020111 00007 NM 2002 1 11 CALA0200008 1 20020109 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 270 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14324 23375 INSPECTION FOUND FLOORBEAM CORRODED AT STA 270. REPAIRED FLOORBEAM IAW ECRA 5321-01119. 2 L 7 2 4F RT A16WE 2002011100008 20020111 00008 NM 2002 1 11 CALA0200009 1 20020109 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 520-540 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND STRINGER S28R CORRODED AT BS 520-540. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-4 0-00 AND ECRA 5311-01111. 2 L 7 2 4F RT A16WE 2002011100009 20020111 00009 NM 2002 1 11 CALA0200010 1 20020109 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 520 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 520, S28R. A DOUBLER WAS INSTALLED IAW ECRA 5311-01111. 2 L 7 2 4F RT A16WE 2002011100010 20020111 00010 NM 2002 1 11 CALA0200011 1 20020109 A 5743 FITTING BOEING 737 7373T0 1384582 NM R OB MLG BEAM CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND A 1/16" CRACK IN R/H O/B MLG BEAM FITTING. THE FITTING WAS REPLACED IAW TASK CARD 03-5743-1-0002 AND 03 -5743-1-0004, SEQ 579, AND EA 5743-01022. 2 L 7 2 4F RT A16WE 2002011100011 20020111 00011 NM 2002 1 11 CALA0200012 1 20020109 A 5743 FITTING BOEING 737 7373T0 1384582 NM L OB MLG BEAM CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND A 1/16" CRACK IN L/H O/B MLG BEAM FITTING. THE FITTING WAS REPLACED IAW TASK CARD 03-5743-1-0003 AND EA 5743-01022. 2 L 7 2 4F RT A16WE 2002011100012 20020111 00012 SO 2002 1 11 C2XA02CL006 1 20020109 A 4900 164161100 CHECK VALVE EMB 145 EMB145LR 3260212 SO APU COKED A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 15980 145202 CLE FLIGHT# 3199 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT WHEN STARTING THE APU ON THE GROUND OR IN THE AIR. MAINTENANCE PLACED THE APU ON MEL.MAINTENANCE PERFORMED CLEANING OF THE APU COMBUSTOR DRAIN CHECK VALVE.OPERATIONAL CHEC KS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002011100015 20020111 00015 WP 2002 1 11 MWEA020047 1 20020111 A 5310 993648725 FRAME DOUG DC9 DC981 3022081 WP LONG 28 LEFT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 FUSEALAGE FRAME 1022 CORRODED AROUND ATTACH FASTENER TO LONGERON 28 LEFT -- REMOVED CAP FROM FRAME. LOCATED AND INSTAL LED NEW FRAME CAP. 2 L 7 2 4F A6WE 2002011100016 20020111 00016 WP 2002 1 11 MWEA020048 1 20020111 A 5510 59225762 SKIN DOUG DC9 DC981 3022081 WP XHS 2 BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 HORIZONTAL STABILIZER LOWER FORWARD SKIN RIGHT HAND SIDE AT APPROXIMATELY XHS 2 SECOND BARREL NUT BACK IS BROKE OUT -- REMOVED BOLT AND REPAIRED HOLE. REINSTALLED BOLT. 2 L 7 2 4F A6WE 2002011100018 20020111 00018 WP 2002 1 11 MWEA020050 1 20020111 A 5320 59304831 STRAP DOUG DC9 DC981 3022081 WP AFT CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 AFT CARGO DOOR JAMB LOWER PAN STRAP HAS NUMEROUS AREAS OF CORROSION FROM FORWARD TO AFT END -- REMOVED, FABRICATED AND INSTALLED NEW STRAP. 2 L 7 2 4F A6WE 2002011100019 20020111 00019 WP 2002 1 11 MWEA020051 1 20020111 A 5320 5936594525 TRACK DOUG DC9 DC981 3022081 WP STA. 636 TO 608 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 CENTER CARGO BAY RIGHT HAND TIE-DOWN RAIL CORROSION, SEVERAL AREAS FROM STATION 636 TO 608 -- REMOVED, FABRICATED AND INSTALLED TIE-DOWN TRACK. 2 L 7 2 4F A6WE 2002011100020 20020111 00020 WP 2002 1 11 MWEA020053 1 20020111 A 5320 59304811 DOUBLER DOUG DC9 DC981 3022081 WP STA. 646 TO 683 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 SEVERAL AREAS OF SURFACE CORROSION ON LOWER DOOR JAMB DOUBLER OF CENTER BAG PIT DOOR JAMB AT STATIONS 646 TO 683 -- RE MOVED, FABRICATED AND INSTALLED LOWER DOOR JAMB DOUBLER. 2 L 7 2 4F A6WE 2002011100021 20020111 00021 WP 2002 1 11 MWEA020052 1 20020111 A 5750 59304761 SKIN DOUG DC9 DC981 3022081 WP STA XFLS 149-155 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 LEFT HAND OUTBOARD FLAP UPPER SURFACE HAS LIGHT CORROSION AROUND STEEL FASTENERS AND AN AREA OF EXFOLIATION, STATION XFL S 149 TO 155 AT FRONT OF SPAR -- FABRICATED, LOCATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002011100022 20020111 00022 WP 2002 1 11 MWEA020049 1 20020109 A 5310 29524401 STRUCTURE DOUG DC9 DC982 3022082 WP STATION 257 DAMAGED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 808ME 48070 lAVATORY TRUCK DAMAGED AIRCRAFT AT STATION #257-294 AND BETWEEN LONGERON 22-23 LEFT. -- REPAIRED AREA IN ACCORDANCE WI TH STRUCTURAL REPAIR MANUAL ("SRM") 53-04, FIGURE 38 SHEET #23. 2 L 7 2 4F A6WE 2002012200115 20020122 00115 WP 2002 1 22 SABA020001 2 20020107 A 7320 8974575 BYPASS VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UHR WP NR 2 ENGINE FAILED A SABA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 33 959AE 6348 959 P66263C FLIGHT 5001 FROM HTS TO CLT, DURING CLIMBOUT AT 7000 FT PILOT REPORTED 80 PERCENT TORQUE AND ENGINE SURGING ON THE NUMBE R TWO ENGINE. EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO HTS. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. MAINTENANC E REMOVED AND REPLACED THE TTL BYPASS VALVE. AIRCRAFT GROUND RUN AND OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVIC E. 2 L 7 2 4T 4 T RT A56EU E4WE 2002011200001 20020112 00001 SO 2002 1 12 C2XA02TY008 1 20020112 A 5700 14569009407 BRACKET EMB 145 EMB145 3260210 SO R/H WING GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS During a scheduled inspection the right hand aileron PCA rod end attachment bracket was found to be gouged. Maint enance acomplished a blend-out repair including a dye penetrant inspection IAW Embraer GST-0046/02. The repair was foun d to be satisfactory, the aircraft will be released upon completion of inspection. 2 L 7 2 4F RT T00011AT 2002011200002 20020112 00002 SO 2002 1 12 C2XA02TY009 1 20020112 A 5500 14524980 FITTING EMB 145 EMB145 3260210 SO EMPENAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS During a scheduled inspection the right hand horizontal stabilizer bearing forward fitting was found to have a int ernal gouge. Maintenance accomplished a blend-out repair including dye penetrant inspection IAW Embraer GST-0095/02. T he repair was satisfactory, the aircraft will be released upon completion of inspection. 2 L 7 2 4F RT T00011AT 2002011300001 20020113 00001 EU 2002 1 13 RAIA00201002 1 20020105 A 2752 TY175702B ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU OUT OF TOLERANCE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 570HK 12016 10144 41089 5473-STL-WHEN SELECTED AT 0 DEGREES FLOPS DROOPED TO 15 DEGREES. MAINTENANCE REMOVED AND REPLACED BOTH FLAT ACTUATORS. 2 L 7 2 4T RT A41NM 2002011300005 20020113 00005 EU 2002 1 13 RAIA00201011 1 20020108 A 3250 AIR135672 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 567HK 41085 5454-STL-NOSE WHEEL STEERING INOP. MAINTENANCE REMOVED AND REPLACED DOWN LOCK SWITCH. 2 L 7 2 4T RT A41NM 2002011400002 20020114 00002 SO 2002 1 14 C2XA02IA009 1 20020111 A 2750 KRP189510VTZ ROLLER EMB 120 EMB120ER 3260203 SO FLAP DAMAGED A C2XA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 27 12715 120125 IAH- FLIGHT 3664DURING TAKEOFF THE CREW NOTED A FLAP CONTROL FAULT,AND, ABORTED THE TAKEOFF. IAH-MAINTENANCE INSPECTED THE FLAPS,AND, FOUND THE BEARING ON THE RIGHT INBOARD FLAP, INBOARD END TO BE DAMAGED. MAINTENANCE REMOVED and REOPLACE DTHE BEARING,PERFORMED A OPERATIONAL CHECK OF THE FLAP SYSTEM, NO DEFECTS NOTED. A TEST FLIGHT WAS SCHEDULED TO EVALUAT E THE FLAP PROBLEM,AND, THE TEST FLIGHT WAS UNSATISFACTORY. 2 L 7 2 4T RT A31SO 2002011400049 20020114 00049 NM 2002 1 14 SWAA020050 1 20020107 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 703SW 27837 EEPLS COVER BROKEN AT ROW 7. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002011400050 20020114 00050 NM 2002 1 14 SWAA020051 1 20020107 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 EEPLS COVER MISSING AT OVERWING EXIT. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002011400051 20020114 00051 NM 2002 1 14 SWAA020053 1 20020108 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002011400052 20020114 00052 NM 2002 1 14 SWAA020054 1 20020108 A 5510 BAC1506 SPAR BOEING 737 7373H4 1384600 NM RT HORZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED C4 CHECK, FOUND RT HORZ STAB LOWER SURFACE AFT SPAR CRACKED APPROX 3 INCHES FROM INBD END. REPAIRED SP AR PER SRM. 2 L 7 2 4F RT A16WE 2002011400053 20020114 00053 NM 2002 1 14 SWAA020056 1 20020109 A 5310 589358 POST BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED 1/2D CHECK, FOUND F/O'S UPPER WINDOW POST CRACKED. REPAIRED POST PER SRM. 2 L 7 2 4F RT A16WE 2002011400054 20020114 00054 NM 2002 1 14 SWAA020058 1 20020109 A 2731 183A81004 TAB BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 716SW 27850 DURING SCHEDULED RON, SWA SI 11052-55, FOUND RT ELEVATOR TAB BOLT AND BUSHINGS WORN ON CONTROL ROD FITTINGS. REMOVED AN D REPLACEDELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002011400096 20020114 00096 EU 2002 1 14 02004331 1 20020104 A 3350 515390176 GCU JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 331UE 41099 During preflight inspection for the flight from IAD to JFK, the crew reported that the emergency exit lights remained on with the the generators on line and the switch in the "armed" position. Maint6enance personnel removed and replaced th e L/H generator control unit. Engine run operational checks were satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002011400097 20020114 00097 2002 1 14 SWAA020060 4 20020110 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 623SW 27933 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP BRACKETS LOOSE. TIGHTENED BRACKETS PER MM. 2 L 7 2 4F RT A16WE 2002011400098 20020114 00098 NM 2002 1 14 SWAA020062 1 20020109 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 3 INCHES LONG AT BS 961, BELOW STR 21L. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2002011400099 20020114 00099 NM 2002 1 14 SWAA020065 1 20020107 A 5311 6546546 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 6L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002011400100 20020114 00100 NM 2002 1 14 SWAA020066 1 20020110 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 756SA 27872 DURING SCHEDULED RON, SWA SI 11075-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB NR 1 H INGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2002011400102 20020114 00102 EU 2002 1 14 02003310 1 20020103 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU LOOSE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 310UE 41028 During preflight inspection for the flight from IAD to CRW, the crew reported that the emergency floor track lights at s eat rows 8 and 9 came on with the switch in the "armed" position. Maintenance personnel secured a loose connector for t he emergency floor track lights. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002011400103 20020114 00103 EU 2002 1 14 02005318 1 20020105 A 3350 5521421 BATTERY PACK JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 318UE 41041 During preflight inspection for the flight from RDU to IAD, the crew reported that the rear emergency exit lights were i noperative. The aircraft was inspected, determined capable of safe flight, and ferried to IAD for maintenance. At IAd, maintenance personnel removed and replaced the aft emergency exit lighting battery pack. An operational check was sati sfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002011400117 20020114 00117 NM 2002 1 14 02FDEA00033 1 20020109 A 2782 ACTUATOR BOEING 727 727233 138408A NM L/E FLAP FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 284FE 22621 AFTER RETRACT FLAPS AND SLATS 5-6 MIN LATER AMBER LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 L/E FLAP SWITCH AND ACTU ATOR PER MM 27-82-001-4, 27-81-022-4. 2 L 7 3 4F RT A3WE 2002011400119 20020114 00119 WP 2002 1 14 02FDEA00034 1 20020108 A 5347 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 SEAT TRACK AT BS 630 X = 27.50 HAS CRACK IN LWR INBOARD AND OUTBOARD FLANGES. 2 L 7 3 4F RT A22WE 2002011400120 20020114 00120 WP 2002 1 14 02FDEA00035 1 20020108 A 5310 DOOR FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 BS 625 TO 765 UPPER CARGO DOOR FWD AND AFT DOOR JAMB STRUCTURAL DAMAGE. REMOVED AND REPLACED DOOR PER EA 8-5330-56188. 2 L 7 3 4F RT A22WE 2002011400129 20020114 00129 NM 2002 1 14 2002UALA00001 1 20020102 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 BODY STATION 178, WL 200, LBL 5.7 WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011400130 20020114 00130 NM 2002 1 14 2002UALA00002 1 20020102 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 BODY STATION 178, WL 211, LBL 17 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012200170 20020122 00170 NM 2002 1 22 2002UALA00003 1 20020102 A 3231 26702887 SEQUENCE VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 551UA 25399 UNABLE TO RETRACT GEAR DOORS. NOISE CONFIRMED GEAR DOORS NOT UP. CYCLED GEARS, NO HELP. FOUND NOSE GEAR DOORS WOULD N OT CLOSE. REPLACED NOSE GEAR DOOR SEQUENCE VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011400131 20020114 00131 NM 2002 1 14 2002UALA00007 1 20020103 A 5310 CREASE BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 925UA 26646 CABIN STATION 312 TO 344 CREASE BEAM ANGLE AT FORWARD ENTRY DOOR IS CORRODED ADJACENT TO SCUPPER DRAIN. MAJOR REPAIR AC COMPLISHED. REPLACED CREASE BEAM CHORD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011400132 20020114 00132 NM 2002 1 14 2002UALA00008 1 20020103 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSLEAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 STRINGER 18R AT STATION 937 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011400133 20020114 00133 NM 2002 1 14 2002UALA00009 1 20020103 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 LEFT HAND CHORD WL 207 BODY STATION 188 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CHORD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011400134 20020114 00134 NM 2002 1 14 2002UALA00010 1 20020103 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 WEB CRACKED AT BODY STATION 178, WL 218, LBL 12. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020100022 20020201 00022 EU 2002 2 1 2002UALA00011 1 20020101 A 3240 MONITOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE BRAKE TEMP MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 462UA 1272 CREW REPORTS HOT BRAKES ON CLIMB OUT WITH GEAR DOWN. SUPPLEMENTAL DATA UPDATE ORIG INDICATION 370 DEG, CLIMBED TO 425 DE G. SUSPECTED INDICATION PROBLEM, BRAKE TEMP CHECKS NORMAL. BSCU BITE CHECK AND PREVIOUS LEG REPORT FAULT BRAKE TEMPERAT URE MONITORING UNIT 3GW. REPLACED MONITOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2002011400135 20020114 00135 WP 2002 1 14 ABXA010662 1 20020106 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 341 47426 EMERGENCY LIGHTS INTERMITTENTLY INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC-9 MM 33-53-02-4. 2 L 7 2 4F A6WE 2002011400137 20020114 00137 EA 2002 1 14 COMA0260040 1 20020110 A 3010 355483255 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 821CA 7420 FLIGHT 5833 L/H ANTI ICE DUCT WARNING.REPLACED THE FUSELAGE SECTION OF LEAK DETECTOR LOOP A41 WK 2 L 7 2 4F RT A21EA 2002011400138 20020114 00138 EA 2002 1 14 COMA0260041 1 20020109 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 912CA 19983 7011 FLIGHT 5545 NLG FAILED TO RETRACT. GEAR DISAGREE WARNING.RPELACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002011400139 20020114 00139 EU 2002 1 14 02011302 1 20020111 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU LOOSE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 302UE 41013 During preflight inspection, the crew reported that the forward section of emergency floor track lighting was inoperativ e. Maintenance personnel secured a loose connector for the forward emergency floor track light section. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002011400143 20020114 00143 SO 2002 1 14 C2XA02TY001 1 20020101 A 3350 78812 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27506 145206 TYS DURING A SCHEDULED INSPECTION, THE NR 4 (AT SEAT 8 ) EMERGENCY LIGHT STRIP WAS FOUND NOT WORKING. MAINTENANCE REMO VED AND REPLACED THE NR 4 LIGHT STRIP IAW EMB-135-MM-33-50-12, OPERATIONAL CHECKS GOOD. AIRCRAFT RELEASED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002011400144 20020114 00144 SO 2002 1 14 C2XA02TY003 1 20020101 A 3260 852701 PROXIMITY SWITCH EMB 135 EMB135LR 3260305 SO NLG CRACKED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 14514 3057 145303 TYS AT TAKEOFF THE LANDING GEAR/GROUND FAIL MESSAGE INDICATOR CAME ON. CREW RETURNED AND MAINTENANCE REMOVED AND REPL ACED THE NLG WOW PROXIMITY SWITCH AND THEN ON SECOND ATTEMPT THE SWITCH HAD TO BE ADJUSTED TO THE TARGET. THE OPS CHECK WERE GOOD IAW EMB 135 MM 32-63-05. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT TOOO11AT 2002011400145 20020114 00145 SO 2002 1 14 C2XA02TY005 1 20020108 A 2620 14523355403 LINE EMB 145 EMB145 3260210 SO EXTINGUISH SYS DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS DURING A SCHEDULED 1C/2C INSPECTION, THE NR 1 ENGINE FIRE EXTINGUISHER LINE AT FRAME 70 IN THE CARGO BAY WAS FOUND DENTED. MAINTENANCE REMOVED AND REPLACED THE LINE IAW EMB-145-AMM-20-10-03. REPAIR PROCEDURES WERE SATISFACTORY AND TH E AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2 L 7 2 4F RT T00011AT 2002011400146 20020114 00146 NM 2002 1 14 DHL2002712001 1 20020109 A 3350 BATTERY BOEING 727 72729 1384007 NM COCKPIT DISCHARGED A DHLA K NONE L NO TEST NR NOT REPORTED 1 SO 01 712DH 19401 EMERGENCY EXIT LIGHT IN COCKPIT INOP. REMOVED AND REPLACED LT ASSY BATTERIES. OPS CHECK GOOD IAW MM 33-50-111. 2 L 7 3 4F A3WE 2002011400148 20020114 00148 NM 2002 1 14 DL72S020004 1 20020102 A 3350 RPS1 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 520DA 21471 FWD CABIN SEAT MOUNTED EMERGENCY LIGHTS INOP. REPLACED FWD POWER SUPPLY AND FUSES IN AFT POWER SUPPLY. 2 L 7 3 4F A3WE 2002011400149 20020114 00149 NM 2002 1 14 DL72S020011 1 20020106 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 525DA 21585 OVERHEAD AISLE EMERGENCY LIGHT NEXT TO AFT GALLEY INOP. REPLACED BATTERY PACK. OPN NORMAL. 2 L 7 3 4F A3WE 2002011400153 20020114 00153 GL 2002 1 14 DL733020003 2 20020101 A 7230 COMPRESSOR BOEING 737 737347 1384647 NM CFMINT CFM56 CFM563B1US GL NR 2 ENGINE STALLED A DALA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 312WA 36332 6950 23598 721325 ON CLIMBOUT, LOUD THUMP FOLLOWED BY COMP STALL WITH RED EGT LIGHT AND ZERO OIL QTY ON NR 2 ENGINE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011400158 20020114 00158 NM 2002 1 14 HNAA0200002 1 20020113 A 7932 DSC2831 HOSE DHAV DHC8 DHC8102 2809003 NM A HNAA E ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 EA 07 907HA 011 NUMBER 1 OIL PRESSURE WENT TO 20-30 PSI ON CLIMB OUT FROM BWI. SHUT DOWN ENGINE IMMEDIATELY. FOUND FLEXABLE OIL COOLER LINE ON LEFT SIDE OF ENGINE LOOSE. TIGHTENED B-NUT. 2 H 7 2 4T RT A13NM 2002011400163 20020114 00163 NM 2002 1 14 DL73K020022 1 20020108 A 2120 ODOR BOEING 737 737247 138448D NM CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 27 242WA 23516 WITH POWER APPLIED HAD A SMELL LIKE BURNING RUBBER. DISSIPATED WITH POWER BACK, NO INDICATIONS. RAN BOTH ENGINES TO T/ O POWER WITH PACKS ON, NO SMELL. CHECKED AIR MIX DISTRIBUTION PLENUM IN FWD BAG BIN, NO CRACKS OR LEAKS. REPLACED RIGH T AND LEFT WATER SEPARATOR BAGS. LEAK CHECK OK. 2 L 7 2 4F A16WE 2002011400170 20020114 00170 NM 2002 1 14 PCAA0201010 1 20020109 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 835EX 289 DURING ROUTINE MAINTENANCE VISIT THE FURTHEST AFT EMERGENCY FLOOR LIGHT WAS FOUND INOPERATIVE. TWO BROKEN WIRES FOUND A ND INSULATION PULLED AWAY FROM LIGHT SOCKET. NEW LIGHT ASSEMBLY INSTALLED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002011400171 20020114 00171 NM 2002 1 14 QXEA0200007 1 20020104 A 5330 SKIN DHAV DHC8 DHC8* NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - THE RIGHT SIDE OF THE FUSELAGE HAS NUMEROUS DENTS AND SCRATCHES AFT OF SERVICE DOOR TO X 234.475. REPAIRED DAMAGE D AREAS BY BLENDING DAMAGED AREAS, DRILLING AND FILLING DAMAGED AREAS WITH RIVETS WHERE NEEDED. PERFORMED HFEC INSPECTI ON TO VERIFY THAT SKIN THICKNESS IS WITHIN LIMITS AND NO CRACKS ARE PRESENT WHERE REPAIRED. ALL REPAIRS PERFORMED IAW E A 6-53-46, 6-53-46A, AND THE DHC-8-401 STRUCTURAL REPAIR MANUAL, CHAPTER 53-10-31. 2 H 7 2 4T RT A13NM 2002011400172 20020114 00172 NM 2002 1 14 QXEA0200008 1 20020106 A 5210 BUSHING DHAV DHC8 DHC8* NM PAX DOOR MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - CANNOT OPEN MAIN CABIN DOOR FROM OUTSIDE. INSPECTED AND FOUND MAIN CABIN DOOR RUBBER SNUBBER MISSING BUSHING. RE INSTALLED BUSHING TO SNUBBER. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002011400173 20020114 00173 2002 1 14 SWAA020042 4 20020108 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002011400174 20020114 00174 NM 2002 1 14 SWAA020048 1 20020107 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE AT ROWS 14 AND 15. SECURED EEPLS PER MM. 2 L 7 2 4F A16WE 2002011400175 20020114 00175 NM 2002 1 14 SWAA020049 1 20020109 A 3350 90083 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT OVERWING EXIT. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002011400176 20020114 00176 NM 2002 1 14 SWAA020052 1 20020109 A 3297 285A16004 PIN BOEING 737 7377H4 1384404 NM CONNECTOR BENT A SWAA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 747SA 29799 WITH LANDING GEAR HANDLE IN UP OR OFF POSITION, GOT RED NOSE GEAR LIGHT. WITH LANDING GEAR HANDLE IN DOWN POSITION, GOT THREE GREEN LIGHTS ON OVERHEAD PANEL AND FORWARD PANEL, PLUS THREE RED LIGHTS ON FWD PANEL. FOUND DAMAGED PINS IN CONN ECTOR D 10982. REMOVED AND REPLACED PINS PER MM. 2 L 7 2 4F RT A16WE 2002011400177 20020114 00177 2002 1 14 SWAA020055 4 20020106 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 632SW 27707 DURING SCHEDULED BC2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002011400178 20020114 00178 NM 2002 1 14 SWAA020057 1 20020105 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 685, STR 1L AND 2L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002011400179 20020114 00179 2002 1 14 SWAA020059 4 20020110 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM CABIN DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 623SW 27933 DURING SCHEDULED C3 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2 L 7 2 4F RT A16WE 2002011400180 20020114 00180 NM 2002 1 14 SWAA020061 1 20020110 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 395SW 27689 DURING SCHEDULED RON, FOUND EEPLS INOP AT ROW 18. REPAIRED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2002011400181 20020114 00181 NM 2002 1 14 SWAA020063 1 20020109 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2002011400182 20020114 00182 NM 2002 1 14 SWAA020064 1 20020108 A 5320 6551698 SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 907, STR 4L AND 4R. REMOVED AND REPLACED STR SPLI CES PER SRM. 2 L 7 2 4F RT A16WE 2002011400183 20020114 00183 2002 1 14 SWAA020067 4 20020110 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002011400184 20020114 00184 NM 2002 1 14 SWAA020068 1 20020110 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS INOP AT SEVERAL AREAS IN CABIN. RECONNECTED WIRES PER MM. 2 L 7 2 4F RT A16WE 2002011400192 20020114 00192 SO 2002 1 14 SWIA200210486 1 20020101 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT ACTIVATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 292UX 120292 HIGH SPEED AURAL WARNING SOUNDED ON TAKEOFF. PERFORMED PITOT STATIC CHECK IAW MM 34-12-00. HIGH SPEED WARNING SOUNDED AT CORRECT TIME. COULD NOT DUPLICATE. CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002011400193 20020114 00193 SO 2002 1 14 SWIA200210497 1 20020101 A 2612 FIRE LOOP EMB 120 EMB120ER 3260203 SO RT ENGINE FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 198SW 120227 ON CLIMBOUT THROUGH APPROXIMATELY 11,000 FT, RIGHT ENGINE PIPE ZONE DET INOP LIGHT ILLUMINATED STEADY FOR APPROXIMATELY 15 MINUTES; THEREAFTER, THE LIGHT REMAINED ILLUMINATED INTERMITTENTLY AFTER DESCENDING BELOW 11,000 FT AND STAYED INTERM ITTENT UNTIL LANDING. REMOVED AND REPLACED ENGINE PIPE ZONE FIRE LOOP ON RIGHT ENGINE IAW MM 26-11-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002011400194 20020114 00194 SO 2002 1 14 SWIA200210498 1 20020101 A 3230 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJ A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 216SW 120285 UPON GEAR RETRACTION LEFT MAIN GEAR DID NOT COME UP. RED A/B LIGHTS WITH RED B-LIGHT. CYCLED GEAR 3 TIMES. EACH TIME GEAR UP LIGHT INDICATION DID NOT CHANGE. RETURNED AND LANDED. ADJUSTED LT MLG O/B SEQUENCE VALVE CONTROL STOP. OPS CH ECK GOOD. 2 L 7 2 4T RT A31SO 2002011400195 20020114 00195 EA 2002 1 14 SWIA200210499 1 20020101 A 3020 300013000003 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA RT COWL FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 497SW 7482 ON CLIMBOUT RT COWL DE-ICE MESSAGE CAME ON. REMOVED AND REPLACED RIGHT COWL ANTI-ICE VALVE IAW A/C MM 30-22-01. P/N: 300013000-003, S/N OFF: 553. REMOVED AND REPLACED RT COWL ANTI-ICE PRESSURE SWITCH WITH SERVICEABLE UNIT IAW CRJ MM 30 -22-07. OPS CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2002011400196 20020114 00196 NE 2002 1 14 SWIA200210500 2 20020102 A 7321 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE NR 1 ENGINE LOOSE A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 393SW 120330 AT BEGINNING OF TAKEOFF ROLL, NR 1 EEC FAILED. WHITE 'MAN' LIGHT, RED `EEC` LIGHT AND AURAL WARNING SOUNDED. ABORTED T AKEOFF. FOUND LOOSE CANNON PLUG TO 1.8 SENSOR. CLEANED, OHM'S CHECKED AND TIGHTENED CANNON PLUG. ALSO OHM'S CHECKED N H & NP SENSORS AND EEC CONTROL CANNON PLUG. CLEANED AND RESET CIRCUIT BREAKERS IAW EMB120 W/M 76-10-00. SYSTEM CHECKED GOOD WITH ENGINE RUN. 2 L 7 2 4T 4 T RT A31SO E20NE 2002011400197 20020114 00197 SO 2002 1 14 SWIA200210503 1 20020102 A 2750 3472001001 FCU EMB 120 EMB120ER 3260203 SO T/E FLAP FAULTY A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 569SW 120342 WHILE EN ROUTE GOT FLAP WARNING ASYMMETRY ASSOCIATED WITH CONTROL FAULT AND ADVANCED SWS. FLAP PAIR LIGHT BARS ON OUTBO ARD PAIR SHOW ASYMMETRY WARNING, ONLY ONE LIGHT SEGMENT. THERE WERE NO CONTROL PROBLEMS OR ROLL TENDENCIES. PERFORMED SYSTEM SELF-DIAG TEST USING VERSION II ANNUNCIATOR FOUND OUTBOARD EXTEND SOLENOID TO BE STUCK OPEN. CHECKED ACTUATORS I AW 27-50-00. NO FAULTS FOUND. REMOVED AND REPLACED FCU IAW MM 27-50-06. CLEARED FAULT. OPS CHECK GOOD. P/N: 347200 -1001, S/N OFF: 0222. 2 L 7 2 4T RT A31SO 2002011400198 20020114 00198 SO 2002 1 14 SWIA200210504 1 20020102 A 2612 WIRE EMB 120 EMB120ER 3260203 SO FIRE DETECTION CHAFED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 198SW 120227 NR 2 DET INOP PIPE ZONE LIGHT ILLUMINATED. FOUND CHAFED WIRE W110-1114-20 NEAR CONNECTOR J0946. REPLACED WIRE AS NEEDE D. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002011400199 20020114 00199 SO 2002 1 14 SWIA200210505 1 20020101 A 5610 WINDSHIELD EMB 120 EMB120RT 3260202 SO COCKPIT CRACKED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 1117H 120117 DURING TAXI FOR TAKEOFF, CO-PILOT'S WINDSHIELD CRACKED. REPLACED CO-PILOT'S WINDSHIELD WITH SERVICEABLE UNIT IAW MM 56- 10-01 AND RII 56-301. 2 L 7 2 4T RT A31SO 2002011400200 20020114 00200 SO 2002 1 14 SWIA200210506 1 20020101 A 7931 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO NR 1 ENGINE FAULTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 209SW 120269 ABORTED TAKEOFF DUE TO OIL WARNING (AURAL) AND NR 1 OIL LIGHT BLINKING ON. OIL LEVELS WERE SATISFACTORY DURING PREFLIGH T. ABORT INITIATED AT APPROXIMATELY 80 KTS. REPLACED NR 1 ENGINE LOW OIL PRESSURE SWITCH. OPS CHECK AND LEAK CHECK GO OD ON GROUND RUNUP. P/N 1153P0013-01, S/N OFF 1165. 2 L 7 2 4T RT A31SO 2002011400201 20020114 00201 EA 2002 1 14 COMA0260042 1 20020112 A 5320 60034017361 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS280 CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 977CA 11447 7157 THE FORWARD J ANGLE WAS CORRODED AT FS280 BETWEEN LBL9 AND RBL9.REMOVED THE CORRODED J ANGLE AND INSTALLED A NEW ANGLE I /A/W WVAC EO 601R-53-2919. 2 L 7 2 4F RT A21EA 2002011400202 20020114 00202 SO 2002 1 14 SWIA200210513 1 20020103 A 2752 3430001003 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAULTY A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 569SW 7 7 120344 WHILE IN CRUISE, FLAP AND ASYMMETRY AND CONTROL FAULT WARNINGS. POSITIVE ROLL TO THE RIGHT. OUTBOARD PAIR OF LIGHTS FL ASHING. MEGGED-OUT ALL WIRES TO FCU. FOUND NO DISCREPANCIES. UPON RETRACTION TEST FOUND LEFT OUTBOARD FLAP ACTUATOR T O EXTEND AND THEN RETRACT 2 DEGREES, THEN EXTEND A LITTLE MORE THEN RETRACT 2 DEGREES, ALL THE WAY DOWN ON EXTENSION CYC LE. REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW 27-50-09. CYCLED FLAPS 5 TIMES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002011400203 20020114 00203 2002 1 14 SWIA200210515 4 20020102 A 3417 ADC CNDAIR CL600 CL6002B19 1900309 EA NR 1 FAILED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 908SW 7540 ADC NR 1 FAILED INFLIGHT. ERRATIC V/S INDICATIONS. VSI INDICATIONS HAPPENING FOR APPROXIMATELY 4 MINUTES PRIOR TO FAIL URE. INSTALLED SERVICEABLE ADC 850A IAW 34-13-00. ALL CHECKS OK ON GROUND AT THIS TIME. 2 L 7 2 4F RT A21EA 2002011400204 20020114 00204 2002 1 14 SWIA200210516 4 20020102 A 3414 INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT DEFECTIVE A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 292UX 120292 ON TAKEOFF, AT ABOUT 60 KIAS, GOT AN AURAL WARNING - HIGH SPEED. ABORTED TAKEOFF. REPLACED CAPTAIN'S AIRSPEED INDICAT OR PER EMB MM 34-12-01. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002011400205 20020114 00205 EA 2002 1 14 COMA0260043 1 20020110 A 5346 601350061 BEAM CNDAIR CL600 CL6002B19 1900309 EA FS640&625.30 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 977CA 11447 7157 ENGINE SUPPORT BEAM CRACKED AT LOWER FWD INBD CORNER L-H&R-H AT RBL37 AND LBL37.REPAIRED ENGINE SUPPORT BEAM I/A/W CANAD AIR REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2002011400206 20020114 00206 2002 1 14 SWIA200210517 4 20020104 A 3425 6226521009 CONTROL PANEL EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 288SW 2667 2667 120316 AFTER DEPARTURE, BOTH THE EHSI AND THE NAVIGATION SCREENS WENT BLANK ON THE FIRST OFFICER'S SIDE. REMOVED AND REPLACED CTL32 (NR 2). OPS CHECKS GOOD ON GROUND. 2 L 7 2 4T RT A31SO 2002011400207 20020114 00207 2002 1 14 SWIA200210518 4 20020102 A 3425 6227711003 COMPUTER EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA O OTHER I FLT. ATTITUDE INST. CL CLIMB 1 NM 07 295UX 1433 1433 120295 ON TAKEOFF THE FIRST OFFICER'S EADI AND EHIS WENT OUT. SAME OCCURRED ON LANDING. REPLACED K0394, K0396 AND NR 2 DPU. RAN AIRCRAFT AND CYCLED AUXILLARY GENERATORS ON LINE SEVERAL TIMES. EFIS SYSTEMS OPERATIONAL CHECK GOOD IAW MM 34-23-00 . 2 L 7 2 4T RT A31SO 2002011400208 20020114 00208 EA 2002 1 14 SWIA200210519 1 20020105 A 2613 601R593201 SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT WING MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 590SW 7077 DUCT FAIL LIGHT AND MESSAGE RIGHT SIDE WITH WING ANTI-ICE ON. REMOVED ALL RIGHT LEADING EDGES AND INSPECTED PICCOLO TUB ES FOR CRACKS, NONE NOTED. REMOVED AND REPLACED RIGHT WING DUCT LEAK SENSORS IAW 30-11-41. COMPLIED WITH OPS CHECK OF WING ANTI-ICE SYSTEM IAW 30-11-41. OPS CHECK GOOD. P/N: 601R59320-1. 2 L 7 2 4F RT A21EA 2002011400209 20020114 00209 EA 2002 1 14 SWIA200210520 1 20020105 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 590SW 7077 EMERGENCY TRACK AND RIGHT EXIT OVERWING INTERIOR LIGHTING INOP. PLACED EMERGENCY LIGHT SWITCH IN ARM POSITION FOR 30 MI N. EMERGENCY LIGHTS OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002011400210 20020114 00210 EA 2002 1 14 SWIA200210521 1 20020103 A 2730 CONTROL CABLE CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR BINDING A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 431SW 7536 CAPTAIN'S ELEVATOR CONTROL BINDING AND DIFFICULT TO MOVE FORWARD AND AFT. REMOVED AND REPLACED ELEVATOR CAPTAIN AND SER VO MOTOR IAW 27-32-00, 22-11-143. REMOVED AND REPLACED THREE CONTROL CABLES IAW 27-32-00. OPS CHECK GOOD. P/N: 622-5 027-101, S/N OFF: 4AXR, P/N: 822-0260-001, S/N OFF: D18H, P/N: 601R90020-79, 601R90020-81, 601R90020-83. 2 L 7 2 4F RT A21EA 2002011400211 20020114 00211 EA 2002 1 14 SWIA200210522 1 20020105 A 4990 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA APU OVERSERVICED A SWIA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 NM 07 499SW 7398 APU OIL TEMPERATURE CAUTION MESSAGE. DIVERTED TO KGJT. FOUND ENGINE OIL OVERSERVICED. SERVICED TO PROPER LEVEL. RAN, GROUND TEST GOOD. 2 L 7 2 4F RT A21EA 2002011400212 20020114 00212 2002 1 14 AWXA200200014 4 20020109 A 2330 Z040H000720A DECODER AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 636AW 098 PHX - EEL - C - DURING INSPECTION EMERGENCY LIGHT SYSTEM FAILED TEST WITH FAULTS INDICATING EMERGENCY COMM LT. MAINTENA NCE TROUBLESHOT AND REPLACED DEU-B 300RH4 PER AMM 23-73-47-401. 2 L 7 2 4F RT A28NM 2002011400217 20020114 00217 EU 2002 1 14 U30A200200001 1 20020103 A 2750 1111A000001 SOLENOID AIRBUS 320 A320214 3930316 EU T/E FLAP INTERMITTENT A U30A K NONE J WARNING INDICATION CR CRUISE 1 EA 17 261AV 61 61 1615 DURING CRUISE, FLT/CTL FLAP TIP BRK FAULT INDICATION ON ECAM. REPLACED BOTH SOLENOIDS ON LT WING TIP BRAKE. OPS CHECK OK. 2 L 7 2 4F RT A28NM 2002011400218 20020114 00218 EU 2002 1 14 U30A200200002 1 20020103 A 2750 COMPUTER AIRBUS 320 A320214 3930316 EU T/E FLAP MALFUNCTIONED A U30A K NONE N FALSE WARNING CR CRUISE 1 EA 17 261AV 1615 DURING CRUISE, FLT/CTL FLAP TIP BRK FAULT INDICATION ON ECAM. PERFORMED TROUBLESHOOTING IAW AMM 27-51-00-810-837 FOR LT WTB, NO FAULT FOUND. SWAPPED NR 1 & 2 SFCC'S TO THE FOLLOWING POSITIONS; NR 1 POS P/N 49-170-07, S/N 2007, NR 2 POS P/ N 49-170-11, S/N 4189. OPS CHECK IAW AMM 27-51-00-740-002. 2 L 7 2 4F RT A28NM 2002011400219 20020114 00219 EU 2002 1 14 U30A200200003 1 20020103 A 2530 OVEN AIRBUS 320 A320214 3930316 EU GALLEY DIRTY A U30A K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 17 261AV 1615 SMOKE REPORTED COMING FROM NR 4 OVEN (AFT GALLEY) DURING OPERATION. INSPECTED AND CLEANED NR 4 OVEN; REMOVED FOOD SPILL IN BOTTOM OF OVEN. OPS CHECK GOOD, NO SMOKE AFTER CLEANING. 2 L 7 2 4F RT A28NM 2002011400220 20020114 00220 EU 2002 1 14 U30A200200004 1 20020105 A 2750 4917011 COMPUTER AIRBUS 320 A320214 3930316 EU T/E FLAP FAULTY A U30A K NONE N FALSE WARNING CR CRUISE 1 EA 17 261AV 92 92 1615 DURING CRUISE, FLT/CTL WING TIP BRK FAULT ILLUMINATED. TROUBLESHOOTING REVEALED THE NR 2 SLAT FLAP CONTROL COMPUTER (SF CC) FAULTED. R&R WITH A SERVICEABLE UNIT AND OPERATIONALLY CHECKED WITH NO FAULTS FOUND. 2 L 7 2 4F RT A28NM 2002011400225 20020114 00225 EU 2002 1 14 0200063215 1 20020109 A 5740 FITTING AIRBUS 320 A320211 3930320 EU CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 315US 171 During "M" check found corrosion in three holes of inner rear spar anchorage fitting. Repaired per EA 32-184839. 2 L 7 2 4F RT A28NM 2002011400226 20020114 00226 NM 2002 1 14 0200075504 1 20020102 A 5311 WEB BOEING 757 757251 1384970 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 504US 23193 During "H" check found crack in support intercostal web at BS 660 stringer 11L. Repaired per EA 55-187744. 2 L 7 2 4F RT A2NM 2002011400252 20020114 00252 NM 2002 1 14 PCAA0201011 1 20020111 A 3350 2078 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM AFT INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 12964 41 016 DURING ROUTINE MAINTENANCE VISIT EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. FORWARD AND AFT EMERGENCY LIGHT BATTERY PACKS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002011400265 20020114 00265 NM 2002 1 14 AWXA200200026 1 20020103 A 5330 6555074 SKIN BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - MAJOR REPAIR - "C" - DURING C-17 CHECK A CRACK WAS FOUND ON THE F/O'S SLIDING WINDOW FWD POST UPPER CORNER BS 220. MAINTENANCE CUTOUT THE DAMAGED AREA OF CRACKED SKIN AT THE F/O'S SLIDING WINDOW AND PERFORMED HFEC INSPECTION TO CONFIR M CRACK WAS CONTAINED. FABRICATED -2 FILLER AND -1 DOUBLER AND INSTALLED REPAIRS AT BS 220 IAW B737-300 SRM 53-10-01, FI G 210, PG 231-234. 2 L 7 2 4F RT A16WE 2002011400266 20020114 00266 NM 2002 1 14 AWXA200200027 1 20020103 A 5330 6555074 SKIN BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - MAJOR REPAIR - "C" - DURING C-17 CHECK A CRACK WAS FOUND ON THE F/O'S SLIDING WINDOW FWD POST LOWER CORNER BS 210. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC INSPECTION TO CONFIRM CRACK WAS CONTAINED. FABRICATED DOUBLER AND INS TALLED REPAIR AT BS 210 IAW B737-300 SRM 53-10-01, FIG 203, PG 209-212. 2 L 7 2 4F RT A16WE 2002011400267 20020114 00267 NM 2002 1 14 AWXA200200028 1 20020103 A 5315 654541041 WEB BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - MAJOR REPAIR - "C" - DURING C-17 CHECK 2 CRACKS WERE FOUND ON WEB BELOW SEAT TRACKS AT BS 709-710, LBL 24. MAINTEN ANCE REMOVED DAMAGED AREA OF WEB, FABRICATED REINFORCEMENT DOUBLER AND NEW WEB AND INSTALLED REPAIRS IAW AWA ER 03-5715- 02011-ES3. 2 L 7 2 4F RT A16WE 2002011400268 20020114 00268 NM 2002 1 14 AWXA200200030 1 20020103 A 5330 5717733008 SKIN BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - MAJOR REPAIR - "C" - DURING C-17 CHECK 1.3" CRACK WAS FOUND ON SKIN AT CAPTAINS WINDSHIELD ON THE AFT POST UPPER C ORNER BS 200, STR 8L. MAINTENANCE CUTOUT AND REMOVED DAMAGED AREA OF SKIN AT AFT POST UPPER CORNER AND FOUND GUSSET CRAC KED APPROXIMATELY 1" TO A FASTENER HOLE. DAMAGED AREA OF GUSSET WAS CUTOUT AND BOTH AREAS WERE HFEC INSPECTED TO VERIFY CRACKS WERE CONTAINED. FABRICATED A -2 FILLER AND -1 DOUBLER AND INSTALLED REPAIRS IAW B737-300 SRM 53-10-01, PG 231-234 . 2 L 7 2 4F RT A16WE 2002011400269 20020114 00269 NM 2002 1 14 AWXA200200031 1 20020109 A 5712 655075712 RIB BOEING 737 73733A 1384673 NM DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - MAJOR REPAIR - "C" - DURING C-17 CHECK MAINTENANCE DISCOVERD A HOLE DRILLED THROUGH INBOARD L/H MIDFLAP LOWER SURF ACE INTO THE FLAP TRACK SUPPORT RIB AT APPROXIMATELY WBL 116. DAMAGE APPEARED TO BE FROM A DRILLED OUT GREASE FITTING. M AINTENANCE REMOVED INBOARD L/H MIDFLAP RIB AND ATTACH ANGLE AT WBL 111, AND RIB FITTING AT WBL 116. FABRICATED AND INSTA LLED NEW RIB FITTING AT WBL 116 IAW B737-300 SRM 51-40-02, PG 3, AND RE-INSTALLED RIB AND ATTACH ANGLE AT WBL 111 IAW B7 37-300 SRM 51-40-02, PG 3, 10. A NEW GREASE FITTING WAS INSTALLED. 2 L 7 2 4F RT A16WE 2002011500051 20020115 00051 EU 2002 1 15 MALA020108 1 20020108 A 3230 7292520653 HARNESS SAAB SF340 SF340A 7850100 EU DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 340A076 During the Emergency Extension check of AC 76, Maintenance noted the LH Explosive Bolt was not getting Voltage a Cannon plug. Maintenance removed and replaced Left MLG Explosive bolt harness PN 7292520-653 IAW Saab AMM 20-10-00 Performed l anding gear Emergency Extension function check IAW MAL Task Card 323106, also performed MAL Task Card 323108. 2 L 7 2 4T RT A52EU 2002011500061 20020115 00061 SO 2002 1 15 COMA0210001 1 20020111 A 3231 DOOR LATCH EMB 120 EMB120RT 3260202 SO A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 269CA 120263 FLIGHT 5070 L/H MLG DID NOT RETRACT WHEN GEAR SELECTED UP.FOUND L/H MLG DOOR UNLATCH - SECURED DOOR LATCH, NO OTHER DEFE CTS FOUND. 2 L 7 2 4T RT A31SO 2002020500001 20020205 00001 NM 2002 2 5 02FDEA00046 1 20020111 A 5230 6557140132 SKIN BOEING 727 727277 138408S NM CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 N 965 NR 1 LOWER CARGO DOOR HAS GOUGE ON INNER SKIN. R&R SKIN 2 L 7 3 4F RT A3WE 2002020500002 20020205 00002 NM 2002 2 5 02FDEA00048 1 20020110 A 5315 FLOORBEAM BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 N 926 CORROSION ON FLOORBEAM BS 344, RBL 5- LBL 65, WL 208 AT FASTENER HOLES. R&R UPR FLOORBEAM. 2 L 7 3 4F RT A3WE 2002020500003 20020205 00003 NM 2002 2 5 02FDEA00049 1 20020108 A 5310 CREASE BEAM BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 CORROSION AROUND BROKEN FASTENER IN THE CREASE BEAM AT BS 1170, WL 208, RBL 61. R&R CREASE BEAM 2 L 7 3 4F RT A3WE 2002011500062 20020115 00062 EA 2002 1 15 COMA0260044 1 20020113 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 960CA 7117 FLIGHT 5553 FLAPS FAILED AT 30 DEGREES DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002011500063 20020115 00063 EA 2002 1 15 COMA0260045 1 20020113 A 2760 4916405 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 988CA 9220 7204 FLIGHT 5581 CONFIG TRIM AND CONFIG SPOILERS SPOILERS WARNING DURING T/O.REPLACED THE #1 SECU. 2 L 7 2 4F RT A21EA 2002011500064 20020115 00064 EA 2002 1 15 COMA0260046 1 20020113 A 2613 355924400 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 918CA 110 110 7018 FLIGHT 5991 L/H 14TH STAGE BLEED DUCT WARNING.REPLACED THE L/H PYLON LEAK DETECTOR ELEMENT. 2 L 7 2 4F RT A21EA 2002011500065 20020115 00065 EA 2002 1 15 COMA0260047 1 20020112 A 3230 46193 VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 912CA 18616 7011 FLIGHT 5467 LANDING GEAR DISAGREE WARNING. NLG DID NOT RETRACT.REPLACED THE MLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002011500066 20020115 00066 EA 2002 1 15 COMA0260048 1 20020111 A 3150 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 960CA 7117 FLIGHT 5285 CONFIG AILERONS AND CONFIG TRIM AURAL WARNING DURING T/O.COULD NOT DUPLICATE. TEST OF AILERON TRIM SYSTEM W AS NORMAL. 2 L 7 2 4F RT A21EA 2002011500067 20020115 00067 NM 2002 1 15 SWAA020071 1 20020110 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER BROKEN AT ROW NR 4. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002011500068 20020115 00068 NM 2002 1 15 SWAA020072 1 20020111 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT DELAMINATED APPROX 2 INCH SQUARE ON TOP OTBD T/E. REPAIRED L/E SLAT PER SRM. 2 L 7 2 4F RT A16WE 2002011500069 20020115 00069 NM 2002 1 15 SWAA020075 1 20020111 A 2761 6544851 ACTUATOR BOEING 737 7373H4 1384600 NM SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED D CHECK, FOUND NR 4 GROUND SPOILER OTBD ACTUATOR CRACKED. REMOVED AND REPLACED ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2002011500070 20020115 00070 NM 2002 1 15 SWAA020076 1 20020111 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 867, RBL 14. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2002011500071 20020115 00071 NM 2002 1 15 SWAA020078 1 20020112 A 5320 BAC1503 STIFFENER BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 340LV 23738 DURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD STIFFENER CRACKED AT BS 663, LBL 6.5. REPAIRED STIFFENER PER SWA RA. 2 L 7 2 4F RT A16WE 2002011500072 20020115 00072 NM 2002 1 15 SWAA020079 1 20020111 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 927 AND BS 947, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002011500073 20020115 00073 NM 2002 1 15 SWAA020080 1 20020113 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (5 EA) AT STR 8L, BS'S 380, 400, 440, 867 AND 907. REPAIRED FRA MES PER BFG ER. 2 L 7 2 4F RT A16WE 2002011500074 20020115 00074 NM 2002 1 15 SWAA020081 1 20020113 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) AT STR 8R, BS'S 360, 400, 440 AND 867. REPAIRED FRAMES P ER BFG ER. 2 L 7 2 4F RT A16WE 2002011500080 20020115 00080 NM 2002 1 15 0200016303 1 20020101 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21R - 31R, CENTER AND LEFT LIGHTS AT GALLEY 3 A, AND LEFT AND RIGHT LIGHTS AT GALLEY 2A. RECONNECTED WIRES. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002011500081 20020115 00081 WP 2002 1 15 0200029886 1 20020102 A 2150 397271411 VALVE DOUG DC9 DC951 3022051 WP A/C BAY FAULTY A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 600TR 47783 WHILE IN CRUISE AT FL280, THE CAIBN ALTITUDE CLIMBED AT 8000-9000 FPM TO 11,000 FEET. CREW INITIATED EMERGENCY DESCENT TO 10,000 FEET AND CABIN STARTED DESCENDING. LEFT PACK VALVE WENT TO FULL HOT. FLIGHT CONTINUED TO DESTINATION AND LAN DED WITHOUT INCIDENT. MAINTENANCE FOUND A CANNON PLUG LOOSE ON THE LEFT PACK SHUTOFF VALVE AND CORRECTED IT. ALSO, REP LACED THE LEFT PACK PRESSURE REGULATOR AND SHUTOFF VALVE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002011500082 20020115 00082 NE 2002 1 15 0200039960 2 20020107 A 7532 658385 CONTROL VALVE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE RT ENGINE FAILED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 920RW 44553 8266 47163 657027 DURING TAKEOFF ROLL AT 100 KNOTS, THE RIGHT ENGINE EGT INDICATION ENTERED THE RED ARCH ZONE OF THE INDICATOR. CREW ABOR TED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT ENGINE PRESSURE RATIO BLEED CONTROL AND PERFORMED ENGINE BORESCOPE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2002011500083 20020115 00083 WP 2002 1 15 0200049876 1 20020105 A 2780 DUCT DOUG DC9 DC951 3022051 WP L/E SLAT LACK OF LUBE A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 765NC 48110 ON SLAT EXTENSION, THE AIRCRAFT ROLLED RIGHT ACCOMPANIED BY THE AMBER SLAT DISAGREEMENT AND BLUE SLAT EXTEND LIGHT DID N OT ILLUMINATE. THE CREW ACCOMPLISHED COM PROCEDURES AND LANDED WITHOUT SLATS UNEVENTFULLY. MAINTENANCE LUBRICATED THE RIGHT T-DUCT. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002011500085 20020115 00085 WP 2002 1 15 0200059752 1 20020105 A 2780 SEAL DOUG DC9 DC941 302207N WP L/E SLAT DAMAGED A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 752NW 47116 AIRCRAFT ROLLS SHARPLY TO THE LEFT WHEN SLAT EXTENDED. A LOUD BANG WAS HEARD AFTER 5 DEGREES OF FLAP SELECTED AND ROLLI NG MOVEMENT STOPPED. THERE WERE NO ABNORMAL ANNUNCIATOR INDICATIONS. THE FLIGHT LANDED SAFELY AT DTW. MAINTENANCE STA TED THAT SLAT EXTENSION APPEARED NORMAL BUT SLAT RETRACTION WAS SLOW AND JERKY. ALL TRACKS AND TRACK DOORS ARE NORMAL. ALIGNMENT CHECK APPEARS NORMAL. THE RIGHT T-DUCT BINDS ON RETRACTION AND THE INBOARD RIGHT SLAT SEAL WAS FOUND TO BE B ADLY DAMAGED AND WAS REPLACED. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002011500087 20020115 00087 EU 2002 1 15 SABA020004 1 20020114 A 3210 137414B425 DOOR BAG JETSTM JETSTM3201 1500217 EU BENT A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 964AE 964 Flight 5135 from CLT to AHN; After takeoff the left main gear transition light remained on. Landing Gear was cycled down and indicated down and locked. Aircraft returned to CLT and landed with no other problems. No emergency was declared. M aintenance found left main gear door damaged, removed and replaced the main gear door. System ops checked good. Aircraft returned to service. 2 L 7 2 4T RT A56EU 2002011500095 20020115 00095 EU 2002 1 15 02FDEA00036 1 20020110 A 3411 PITOT TUBE AIRBUS 310 A310222 3930315 EU PITOT/STATIC SYS FAULTY A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 422FE 346 REJECTED T/O, F/O'S PFD HAD NO RELIABLE AIRSPEED. REMOVED AND REPLACED F/O'S PITOT PROBE PER MM 34-11-15. 2 L 7 2 4F RT A35EU 2002011500096 20020115 00096 2002 1 15 02FDEA00037 4 20020110 A 3417 ADC AIRBUS 310 A310222 3930315 EU NR 2 FAULTY A FDEA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 25 422FE 346 F/O'S AIRSPEED BECAME UNRELIABLE. REMOVED AND REPLACED NR 2 ADC PER MM 34-11-34-4. 2 L 7 2 4F RT A35EU 2002011500097 20020115 00097 EU 2002 1 15 02FDEA00038 1 20020111 A 2611 SMOKE DETECTOR AIRBUS 300 A300F4605R 3930327 EU CARGO BAY ACTIVATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 665FE 769 ON CLIMBOUT BOTH DETECTORS MID 1 & ONE INDICATED SMOKE IN CARGO COMPT. 2 L 7 2 4F RT A35EU 2002011500098 20020115 00098 NM 2002 1 15 02FDEA00039 1 20020112 A 2131 CONTROLLER BOEING 727 727227 1384078 NM CABIN PRESSURE MALFUNCTIONED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 478FE 21395 ON CLIMBOUT, A/C WOULD NOT PRESSURIZE. INSPECTION PERF PRESSURIZATION CHECK, FWD ENTRY DOOR NORM, OPS NORM. OK FOR SER VICE. 2 L 7 3 4F A3WE 2002012900047 20020129 00047 NM 2002 1 29 02FDEA00040 1 20020112 A 5230 SEAL BOEING 727 7272S2F 1384O81 NM CARGO DOOR DIRTY A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 207FE 22929 A/C WILL NOT PRESSURIZE OR HOLD PRESSURE. NOTED MCD VENT FLAP/DOORS NOT FLUSH AND SEALS LEAKED. CLEANED SEALS. 2 L 7 3 4F A3WE 2002011500099 20020115 00099 EU 2002 1 15 02FDEA00041 1 20020113 A 2910 VALVE AIRBUS 310 A310222 3930315 EU HYDRAULIC SYS CRACKED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 452FE 313 ON T/O, BLUE RESERVOIR LOW AIR PRESSURE ECAM ILLUMINATED. REMOVED AND REPLACED MANIFOLD VALVE PER MM 29-32-13-4. REFIL LED BLUE SYS. OPS AND LEAK CHECK NORMAL. 2 L 7 2 4F RT A35EU 2002011500100 20020115 00100 NE 2002 1 15 ABXA010663 2 20020108 A 7321 77333321 FCU BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE NR 1 ENGINE MALFUNCTIONED A ABXA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 707AX 2754 22570 709653 DURING CLIMB, THE NR 1 ENGINE STARTED TO ACCELERATE UNCOMMANDED. PULLED THE THROTTLE TO IDLE, ENGINE DID NOT RESPOND. THE NR 1 ENGINE WAS SHUTDOWN. THE AIRCRAFT RETURNED TO ILN WHERE IT LANDED UNEVENTFULLY. REPLACED THE LEFT TT2 SENSOR AND THE LEFT FUEL CONTROL UNIT IAW B767 MM. 2 L 7 2 4F 4 F RT A1NM E3NE 2002011500101 20020115 00101 WP 2002 1 15 CALA0200015 1 20020111 A 5530 BRACKET DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND A 1/2" CRACK IN VERTICAL STABILIZER R/H SIDE SUPPORT BRACKET FOR UPPER FAIRING ABOVE JACKSCREW. A DOUBL ER WAS INSTALLED ON THE SUPPORT BRACKET IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2002011500102 20020115 00102 NM 2002 1 15 CALA0200016 1 20020112 A 5347 CHANNEL BOEING 737 7373T0 1384582 NM STA 860 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17317 23368 INSPECTION FOUND AFT BAGGAGE BIN FLOOR CHANNEL CORRODED AT STA 860, RBL 3. THE CORRODED AREA WAS REMOVED AND AN ANGLE RE PAIR WAS INSTALLED IAW ECRA 5320-01603. 2 L 7 2 4F RT A16WE 2002011500103 20020115 00103 NM 2002 1 15 CALA0200020 1 20020114 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 1156 WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17317 23368 INSPECTION FOUND FUSELAGE SKIN WORN BELOW R/H HORIZONTAL STABILIZER AFT ATTACH LUG AT STA 1156. THE WORN SKIN WAS REMOVE D AND NEW SKIN WAS INSTALLED IAW SRM 53-80-01. 2 L 7 2 4F RT A16WE 2002012400037 20020124 00037 WP 2002 1 24 ARWA20020109 1 20020108 A 2424 51508000 GCU DOUG DC8 DC861 3021952 WP NR 4 ENGINE FAILED A ARWA O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 29UA 46159 DURING APPROACH NR 4 GENERATOR UNPARALLEL LIGHT AND BUS POWER FAIL LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST. AI RCRAFT LANDED AT DESTINATION UNEVENTFUL. RESET NR 4 GENERATOR SYSTEM IN ACCORDANCE WITH MM 24-5-1 ENTERED ON DMI 16156 PER MEL 24-1 GEN NR 4 INOP. REMOVED AND REPLACED GENERATOR CONTROL UNIT IAW MM 24-20-1, OPS CHECK NORMAL. DMI CLEARED ON LOG PAGE 107253. 2 L 7 4 4F 4A25 2002011500106 20020115 00106 NE 2002 1 15 ARWA20020110 2 20020110 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE NR 2 MALFUNCTIONED A ARWA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SO 19 308GB 193U1133 NR 2 ENGINE STARTS AFTER 2 MINUTES ENGINE ROLL BACK TO ZERO AND SHUT DOWN. 2 L 7 3 4F 4 F A23WE E12EU 2002011500113 20020115 00113 NE 2002 1 15 C1HA200296001 2 20020106 A 7200 ENGINE BOEING 727 72727 138400K NM PWA JT8 JT8D17 52049 NE NR 2 MALFUNCTIONED A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 696CA 22574 ON RUNWAY ADVANCED THROTTLE TO 1.4 CHECK PARAMETERS GOOD, CONTINUED THROTTLE ADVANCE FORFLEX POWER, LOUD BANG FROM NR 2 ENGINE, ENGINE FAIL LIGHT ILLUMINATED AND PACKS TRIPPED. ACCOMPLISHED THOROUGH EXAMINATION OF ENGINE NR 2 INTAKE AND EX HAUST WITH NO DAMAGE NOTED. CHECKED PRBC SCREENS AND FOUND NO ABNORMALITIES REF MM 72-00. OPERATED NR 2 ENGINE AS WELL AS 1 & 3 AT IDLE UP TO TAKEOFF POWER INCLUDING ACCELERATION CHECKS. SURGE BLEED VALVES OPERATED NORMALLY AND ALL OTHER INDICATIONS WERE NORMAL AS WELL WITH NO STALLS. UNABLE TO DUPLICATE THE REPORTED MALFUNCTION. SUSPECT CROSSWIND GUST. 2 L 7 3 4F 4 F A3WE E2EA 2002011500114 20020115 00114 NE 2002 1 15 C1HA200296002 2 20020106 A 7532 BLEED VALVE BOEING 727 72727 138400K NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE MALFUNCTIONED A C1HA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 15 696CA 22574 POWER UP FOR TAKEOFF NR 2 ENGINE COMPRESSOR STALLED POWER WAS AT 1.6 EPR AND SPEED WAS BELOW 40 KTS. NR 2 PRBC WAS CHAN GED AND OPS CHECK GOOD AND NR 2 GENERATOR PUT ON MEL. NR 2 COMP BLEED SYS OPS NORMAL REF: 75-31. 2 L 7 3 4F 4 F A3WE E2EA 2002011500115 20020115 00115 NM 2002 1 15 C1HA200296005 1 20020114 A 3350 BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 696CA 22574 EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED RT MID OVERWING EMERGENCY LIGHT BATTERY PACK AND REMOVED AND REPLA CED LT FWD EMERGENCY LIGHT BATTERY PACKS IAW MM 33 -54, OPS NORMAL. 2 L 7 3 4F RT A3WE 2002011500116 20020115 00116 NM 2002 1 15 C1HA200296006 1 20020114 A 3350 BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 696CA 22574 DURING TROUBLESHOOTING FOUND INSIDE OVERHEAD EMER LIGHT BY ROW 23 INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK OK . 2 L 7 3 4F RT A3WE 2002011500117 20020115 00117 NM 2002 1 15 C1HA200296007 1 20020114 A 3350 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 696CA 22574 DURING TROUBLESHOOTING FOUND FWD CENTER OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY 33-50-81, OPS CH ECK OK. 2 L 7 3 4F RT A3WE 2002011500118 20020115 00118 NM 2002 1 15 C1HA200296008 1 20020114 A 3350 BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 696CA 22574 DURING TROUBLESHOOTING FOUND WING EMERGENCY LIGHT INOP LT SIDE. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-22, OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2002011500119 20020115 00119 EU 2002 1 15 SABA020005 1 20020112 A 3220 110A703056A STRUT BAG JETSTM JETSTM3201 1500217 EU LEAKING A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 963AE 963 Flight 5167 from LEX to CLT; After takeoff the nose gear unsafe light stayed on. Gear was lowered and indicated down and locked. Aircraft returned to LEX and landed with no other problems. No emergency was declared. Maintenance from CLT ins pected the nose gear and serviced it with nitrogen. Strut was fouund safe for ferry flight to CLT Flight # 9475. Mainte nance in CLT removed and replaced the nose gear strut for not holding nitrogen. Retraction check C/W. Aircraft returned to service. 2 L 7 2 4T RT A56EU 2002011500120 20020115 00120 NM 2002 1 15 C1HA200297001 1 20020110 A 3350 LIGHT BOEING 727 727270 138408P NM CABIN MALFUNCTIONED A C1HA K NONE O OTHER CR CRUISE 1 GL 15 697CA 23052 EMERGENCY EXIT LIGHT REMAINED ON THROUGHOUT FLIGHT. PERFORMED SYSTEM OPS CHECKS IAW 727 MM 33-50-02. ALL CHECKS NORMAL , NO DEFECTS NOTED OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2002011500121 20020115 00121 SO 2002 1 15 C2XA02CL005 1 20020108 A 4930 ODOR EMB 145 EMB145LR 3260212 SO COCKPIT DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 15980 145202 CLE FLIGHT 3198 THE CREW REPORTED A STRONG FUEL SMELL IN COCKPIT WHEN STARTING APU BOTH ON GROUND AND IN FLIGHT. MAINTE NANCE PERFORMED APU OPERATIONAL CHECKS AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002011500122 20020115 00122 SO 2002 1 15 C2XA02CL007 1 20020112 A 3350 7287580509 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 19503 145176 CLE FLIGHT 3084 THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE BY EXIT DOOR. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY AISLE PATH LIGHT STRIP AT ROW 8. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED F OR SERVICE. 2 L 7 2 4F RT T00011AT 2002011500129 20020115 00129 SO 2002 1 15 C2XA02IA008 1 20020110 A 4930 161544001 TANK EMB 120 EMB120ER 3260203 SO APU ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 57734 120199 IAH- AT THE GATE THE CREW NOTED THAT A GAS FUME SMELL IN THE CABIN WITH THE APU RUNNING. MAINTENANCE DRAINED THE APU E PA TANK, PERFORMED A OPERATIONAL CHECK OR THE APU, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002011500137 20020115 00137 SO 2002 1 15 C2XA02IA010 1 20020112 A 2752 320301005 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A C2XA K NONE F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 27 12715 120125 IAH- DURING FLIGHT 4375, A TEST FLIGHT, THE CREW NOTED THAT THE FLAPS FAIL INFLIGHT, CONTROL FAULT WITH FLAPS AT ZERO D EGREES. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND INBOARD FLAP ACTUATOR, PERFORMED A OPERATIONAL CHECK OF THE FLA P SYSTEM, NO DEFECTS NOTED. A TEST FLIGHT WAS FLOWN, THE TEST FLIGHT WAS SATISFACTORY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE AND RELEASED FROM TEST FLIGHT. 2 L 7 2 4T RT A31SO 2002011500138 20020115 00138 SO 2002 1 15 C2XA02IA011 1 20020112 A 2751 3069001017 CONTROL PANEL EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 12715 120125 IAH- DURING FLIGHT 4375, A TEST FLIGHT, THE CREW NOTED THAT THE FLAP ASYMMETRY LIGHT GLOWS THEN THE FLAPS FAIL. MAINTE NANCE REMOVED AND REPLACED THE FLAP ANNUNCIATOR PANEL, PERFORMED A OPERATIONAL TEST OF THE FLAP SYSTEM, NO DEFECTS NOTED . A TEST FLIGHT WAS FLOWN, TEST FLIGHT SATISFACTORY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT WAS RELEASED FROM TEST FLIGHT. 2 L 7 2 4T RT A31SO 2002011500139 20020115 00139 SO 2002 1 15 C2XA02TY006 1 20020111 A 5553 14520736004 HINGE FITTING EMB 145 EMB145 3260210 SO VERTICAL STAB GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS, DURING A SCHEDULED 1C/2C INSPECTION, THE RIGHT HORIZONTAL STAB HINGE FITTING ON VERTICAL STAB WAS FOUND GOUGED ON T HE UPPER SURFACE, ABOVE THE PIN BEARING. MAINTENANCE BLENDED OUT THE DAMAGE, PERFORMED DYE-PENETRATE INSPECTION (NO CRA CKS FOUND) AND RESTORED PROTECTIVE FINISH IAW EMB-GST-0065/02. REPAIR PROCEDURES ARE SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLECTION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002011500140 20020115 00140 SO 2002 1 15 C2XA02TY007 1 20020111 A 5553 14520735004 HINGE FITTING EMB 145 EMB145 3260210 SO VERTICAL STAB GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS, DURING A SCHEDULED 1C/2C INSPECTION THE LEFT HORIZONTAL STAB HINGE FITTING ON VERTICAL STAB WAS FOUND GOUGED ON THE UPPER SURFACE, ABOVE THE PIN BEARING. MAINTENANCE BLENDED OUT THE DAMAGE, PERFORMED DYE-PENETRATE INSPECTION (NO CRACK S FOUND) AND RESTORED PROTECTIVE FINISH IAW EMB-GST-0065/02. REPAIR PROCEDURES ARE SATISFACTORY AND THE AIRCRAFT WILL B E RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002011500141 20020115 00141 SO 2002 1 15 C2XA02TY010 1 20020112 A 5510 14524977001 FITTING EMB 145 EMB145 3260210 SO HORIZ STAB CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS DURING A SCHEDULED INSPECTION THE HORIZONTAL STABILIZER RIGHT HAND FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMBRAER GST-0045/02 WHICH INCLUDED THE DYE PENETRANT INSPECTION. THE RE PAIR WAS FOUND TO BE SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002011500142 20020115 00142 SO 2002 1 15 C2XA02TY011 1 20020112 A 5510 14524977001 FITTING EMB 145 EMB145 3260210 SO HORIZ STAB CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS DURING A SCHEDULED INSPECTION THE HORIZONTAL STABILIZER LEFT HAND FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. M AINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR INCLUDING DYE PENETRANT INSPECTION IAW EMBRAER GST-0045/02, THE REPAIR WAS SA TISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002011500143 20020115 00143 SO 2002 1 15 C2XA02TY012 1 20020111 A 3350 GE1317 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17513 145292 TYS DURING A SCHEDULED INSPECTION THE NR 3 AISLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E NR 3 AISLE EMERGENCY LIGHT ASSEMBLE LIGHT BULB IAW EMB-135 MM 33-50-08, THE OPERATIONAL CHECK WERE SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2002011500144 20020115 00144 WP 2002 1 15 CALA0200006 1 20020109 A 5530 HINGE DOUG DC9 DC982 3022082 WP VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND RIGHT I/B AND O/B VERTICAL STABILIZER HINGE PLATES CORRODED ON MATING SURFACES. NEW HINGE PLATES WERE INSTALLED IAW EA 5530-01238. 2 L 7 2 4F A6WE 2002011500145 20020115 00145 WP 2002 1 15 CALA0200007 1 20020109 A 5530 HINGE DOUG DC9 DC982 3022082 WP VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND LEFT I/B AND O/B VERTICAL STABILIZER HINGE PLATES CORRODED ON MATING SURFACES. NEW HINGE PLATES WERE I NSTALLED IAW EA 5530-01238. 2 L 7 2 4F A6WE 2002011500146 20020115 00146 NM 2002 1 15 CALA0200013 1 20020110 A 5730 SKIN PANEL BOEING 737 7373T0 1384582 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND A 2 INCH CRACK IN RIGHT WING L/E CUTOUT AT O/B AUX TRACK NR 5 SLAT PANEL. REPAIRED IAW SRM 51-70-16. 2 L 7 2 4F RT A16WE 2002011500170 20020115 00170 EA 2002 1 15 COMA0260049 1 20020115 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA AFT FUSELAGE DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 403CA 1318 7428 DURING INSPECTION FOUND FUSELAGE DAMAGE (DENT) AT FS 654.50 EXCEEDING SRM LIMITS.REPAIRED IN ACCORDANCE WITH REO 601R-53 -61-347 ON 5/29/01. 2 L 7 2 4F RT A21EA 2002011500171 20020115 00171 EA 2002 1 15 COMA0260050 1 20020114 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 786CA 5359 7333 FLIGHT 5347 GEAR DISAGREE MESSAGE.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002011500172 20020115 00172 NM 2002 1 15 CALA0200014 1 20020110 A 5347 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14324 23375 INSPECTION FOUND AFT CARGO COMPARTMENT FLOOR LT TIE DOWN TRACK CORRODED AT STA 947 ABOVE S25L. REPAIRED TIE DOWN TRACK IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002011500173 20020115 00173 NM 2002 1 15 DHL2002709001 1 20020111 A 3040 WINDSHIELD WIPER BOEING 727 72782C 1384026 NM WINDSHIELD OUT OF ADJ A DHLA K NONE O OTHER CR CRUISE 1 SO 01 709DH 19968 F/O WINDSHIELD WIPER BLADE WILL NOT RUN IN LOW. ADJUSTED F/O'S WIPER IAW 727 MM CHP 30-42-01, OPS CHECK NORMAL AT THIS TIME. 2 L 7 3 4F A3WE 2002011500174 20020115 00174 NM 2002 1 15 DHL2002724001 1 20020108 A 2612 FIRE DETECTOR BOEING 727 727228 1384083 NM CARGO BAY MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 724DH 19862 LOWER CARGO FIRE DET, SYSTEM INOP. RESET C/B AND PERFORMED SYSTEM TEST IAW MM 26-16 SYSTEM OPS NORMAL. 2 L 7 3 4F RT A3WE 2002011500175 20020115 00175 WP 2002 1 15 DHL2002801001 1 20020110 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 2 ENGINE MALFUNCTIONED A DHLA K NONE L NO TEST NR NOT REPORTED 1 SO 01 801DH 46033 NR 2 ENG FIRE WARNING B-LOOP WILL NOT TEST. DEFERRED NR 2 ENG FIRE WARNING B-LOOP. UNABLE TO DUPLICATE. INSPECTED NR 2 ENG B-FIRE LOOP SYSTEM, OPS NORMAL PER MM 26-10-0. 2 L 7 4 4F RT 4A25 2002011500176 20020115 00176 WP 2002 1 15 DHL2002803001 1 20020110 A 2611 SMOKE DETECTOR DOUG DC8 DC873 302199C WP CABIN WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 803DH 46123 SMOKE DETECTOR 11 DOES NOT TEST. REMOVED AND REPLACED SMOKE DETECTOR IAW MM 26-10-5, TEST OK. 2 L 7 4 4F RT 4A25 2002011500177 20020115 00177 WP 2002 1 15 DHL2002807001 1 20020109 A 2620 WIRE DOUG DC8 DC873F 302199F WP EXTINGUISH SYS BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 ON INSPECTION OF OUTBOARD FIRE EXTINGUISHER NR 4 ENG CONNECTOR P1-1277 TO THE EXPLOSIVE CARTRIDGE HAS A COUPLE OF BROKEN WIRES. REMOVED AND REPLACED CONNECTOR ON NR 4 ENG OUTBOARD FIRE EXTINGUISHER PER MM REF 20-50-1. NO DEFECTS NOTED. O K TO CONTINUE. 2 L 7 4 4F RT 4A25 2002011500181 20020115 00181 NM 2002 1 15 DL757020018 1 20020106 A 3350 767 LIGHT BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 614DL 22821 L-4 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED SAME. CHECKS OK. 2 L 7 2 4F RT A2NM 2002011500182 20020115 00182 NM 2002 1 15 DL757020019 1 20020107 A 3350 0L3071BPEGPL LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 644DL 23998 EMERGENCY LIGHT AT 4C IS INOP. REPLACED BULB. 2 L 7 2 4F RT A2NM 2002011500222 20020115 00222 NM 2002 1 15 P5CA0200625 1 20020112 A 7810 NONE NOZZLE BOEING 747 74746NF 13848BT NM #3 ENG EXHAUST CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 450PA 30808 #3 ENGINE EXHAUST NOZZLE OUTER SKIN IS CRACKED ON THE RIGHT SIDE TOP. REMOVED & REPLACED EXHAUST NOZZLE AS PER 78-11-01 . 2 L 7 4 4F RT A20WE 2002012900173 20020129 00173 EU 2002 1 29 RAIA00201017 1 20020113 A 6120 31056294 BETA SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LEFT INTERMITTENT A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 552HK 1734 41057 5623-STL- DURING TAXI LEFT GREEN BETA LIGHT WAS INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE LEFT BETA SWITCH. 2 L 7 2 4T RT A41NM 2002012900174 20020129 00174 EU 2002 1 29 RAIA00201018 1 20020113 A 2421 8260121 GENERATOR AEROSP ATR72 ATR72202 8680940 EU NR 1 ENGINE MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 721TE 5043 1708 217 5593-MSN- DURING TAXI NR 1 GENERATOR FAULTED. MAINTENANCE REMOVED AND REPLACED NR 1 GENERATOR. OPS OK DURING GROUND RU N. 2 H 7 2 4T RT A53EU 2002012900175 20020129 00175 EU 2002 1 29 RAIA00201019 1 20020114 A 6120 31056294 BETA SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RIGHT MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 551HK 4861 41040 5453-BMI- RIGHT BETA LIGHT CAME ON AT V1. MAINTENANCE REMOVED AND REPLACED RIGHT BETA SWITCH. OPS OK ON GROUND RUN. 2 L 7 2 4T RT A41NM 2002011500223 20020115 00223 2002 1 15 RAIA00201020 4 20020114 A 2300 7510700806 RECEIVER EMB 145 EMB145 3260210 SO INOPERATIVE A RAIA E ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 CE 03 805HK 5556 300 145096 5293-STL- DURING TAXI #1 COMM WOULD NOT RECEIVE. MAINTENANCE REMOVED AND REPLACED #1 RECEIVER TRANSMITTER. 2 L 7 2 4F RT T00011AT 2002011500224 20020115 00224 SO 2002 1 15 C2XA02TY013 1 20020115 A 3350 RPS1B INVERTER EMB 145 EMB145LR 3260212 SO CABIN BLOWN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 TYS DURING A SCHEDULED INSPECTION THE AFT EMERGENCY LIGHTS WERE INOP. MAINTENANCE R/R THE THE AFT EMERGENCY LIGHT INVER TER IAW EMB.145MM 33-50-04. OPS CHECK WAS GOOD AND AIRCRAFT WAS REL. FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002011500225 20020115 00225 SO 2002 1 15 C2XA02TY014 1 20020115 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DEFECTIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 TYS DURING A SCHEDULED INSPECTION THE EMERGENCY BATTERY AT #4 COMPARTMENT WAS INOP. MAINTENANCE R/R THE EMERGENCY BATTE RY IAW EMB. 33-50-04. OPS CHECK WAS GOOD AND WAS REL. FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002011600002 20020116 00002 WP 2002 1 16 ANCF200200001 1 20020111 A 2410 CSD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE ACCESS BAY MALFUNCTIONED W ANCF D RETURN TO BLOCK M OVER TEMP CL CLIMB 1 SW 99 190AN 53190 726972 DURING CLIMB LT CSD OIL OUTLET TEMP.REACHED RED DANGER ZONE AND CONTINUED INCREASING. CSD WAS DISCONNECTED. APU WAS STAR TED AT FL.260 BUT AT FL.305 APU HAD AUTO SHUT DOWN. DESCENT WAS DOWN TO FL.290 WE TRIED TO START APU AGAIN BUT START WAS UNSUCCESSFUL. CREW DESIDED TO RETURN TO BOG. CORRECTIVE ACTION: LT CSD WAS REPLACED IN ACC. WITH AAW.AMM.24-10-01 PA G.401. 2 L 7 2 4F 4 F RT A6WE E9NE 2002011600008 20020116 00008 EU 2002 1 16 02FDEA00051 1 20020115 A 5270 LIGHT AIRBUS 310 A310203 3930313 EU M/D DOOR ILLUMINATED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 412FE 360 02-51 AFTER T/O MAIN DECK DOOR LIGHT CAME ON. A/C RELEASED PER MEL 52-9. 2 L 7 2 4F RT A35EU 2002011600051 20020116 00051 NM 2002 1 16 SWAA020083 1 20020114 A 5320 BAC1518 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 616 BELOW FLOOR LEVEL LT SIDE. REPAIRED STIFFENER P ER SRM. 2 L 7 2 4F RT A16WE 2002011600052 20020116 00052 NM 2002 1 16 SWAA020085 1 20020114 A 5330 6545866 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM LOWER SKIN CRACKED 1.25 INCHES BETWEEN MLG W/W. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002011600053 20020116 00053 NM 2002 1 16 SWAA020086 1 20020114 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED 1.0 INCH AT BS 178, WL 201 AND RBL 5.0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002011600054 20020116 00054 NM 2002 1 16 SWAA020088 1 20020114 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207 LT. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002011600055 20020116 00055 NM 2002 1 16 SWAA020089 1 20020114 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 706SW 27840 EEPLS COVER LOOSE AT ROW NR 1. REINSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002011600056 20020116 00056 NM 2002 1 16 SWAA020090 1 20020114 A 3350 07912 COVER BOEING 737 7373T0 1384582 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 EEPLS WIRES EXPOSED AT AFT LOUNGE AREA.. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002011600057 20020116 00057 NM 2002 1 16 SWAA020092 1 20020112 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 14L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002011600058 20020116 00058 NM 2002 1 16 SWAA020095 1 20020112 A 5320 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, WL 233 AND LBL 17.1. REMOVED AND REPLACED WEB P ER SRM. 2 L 7 2 4F RT A16WE 2002011600059 20020116 00059 NM 2002 1 16 SWAA020100 1 20020114 A 5310 6546569 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 967, BETWEEN STR'S 6L AND 7L. REMOVED AND REPLACED SHEAR TIE PE R SRM. 2 L 7 2 4F RT A16WE 2002011600060 20020116 00060 NM 2002 1 16 SWAA020102 1 20020114 A 5313 6547693 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CORRODED AT BS 787, STR 27R. REPAIRED STR PER SWA RA. 2 L 7 2 4F RT A16WE 2002011600062 20020116 00062 WP 2002 1 16 ABXA010665 1 20020109 A 5730 SKIN DOUG DC8 DC861 3021952 WP RIGHT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 RIGHT WING, TOP SURFACE BY STATION XRS 172, CORROSION ON SKIN. REPAIRED IAW ABX REA D857-40949-MR AND DC8 SRM 57-2-0, 51 -1-26, 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 2002011600063 20020116 00063 CE 2002 1 16 GLBA2002002 1 20020110 A 7700 1303890021 TRANSMITTER BEECH 1900 1900D 1154162 CE #1 INTERMITTENT A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 201GL 7676 7676 UE201 LEFT ENGINE TORQUE FLUX, INSPECTED REPLACED TRANSMITTER OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2002012400059 20020124 00059 NM 2002 1 24 F3LA200200003 1 20020104 A 5411 FRAME BOEING 737 737228 13844AG NM NR 2 NACELLE BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED BROKEN FRAME AT NR 2 ENGINE INBOARD FIXED COWL AFT CROSSOVER RIB. REPLACED BROKEN INTERCOSTAL (FRAME) PER SRM 51-30-2, 51-30-5 AND 51-30-6. 2 L 7 2 4F RT A16WE 2002012300166 20020123 00166 NM 2002 1 23 F3LA200200004 1 20020108 A 5313 STRINGER BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION CORROSION AROUND RIVET HEAD AT STR 16-R, STA 797, ON ANGLE TO WEB ATTACHMENT. FABRICATED R EPLACEMENT ANGLE AND INSTALLED REPAIR PER SRM 51-10-2, 51-30-2 AND SOPM 20-41-2. 2 L 7 2 4F RT A16WE 2002012300038 20020123 00038 NM 2002 1 23 2002UALA00023 1 20020107 A 5230 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 195UA 26899 FORWARD CARGO DOOR AFT LOWER SKIN WAS CRACKED. MAJOR REPAIR WAS ACCOMPLISHED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002011600068 20020116 00068 NM 2002 1 16 2002UALA00025 1 20020107 A 5330 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MISDRILLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 AFT PIT FRAME STATION 1220 ABOVE STRINGER 27L IS MISDRILLED. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600069 20020116 00069 NM 2002 1 16 2002UALA00027 1 20020104 A 5311 FLANGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT PIT BODY FRAME UPPER FLANGE IS GOUGED LOC STATION 1520 BELOW STRINGER 26R. MAJOR REPAIR ACCOMPLISHED. FRAME BLENDED AND FABRICATED STRINGER CLIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600070 20020116 00070 NM 2002 1 16 2002UALA00028 1 20020105 A 5313 CLIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT PIT STATION 1520 STRINGER 22L CLIP MANUFACTURED FROM 2 SEPARATE T-CHORD ANGLES. MAJOR REPAIR ACCOMPLISHED. STRINGER CLIP WAS MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600071 20020116 00071 NM 2002 1 16 2002UALA00034 1 20020104 A 5315 BEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 BODY STATION 874 LBL 12 TRANSVERSE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SPLICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012300041 20020123 00041 NM 2002 1 23 2002UALA00045 1 20020108 A 2910 271N61191 HYDRAULIC LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYDRAULIC SYS FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 29 526UA 24994 LEFT MAIN GEAR DOWNLOCK ACTUATOR LINE RUPTURED. LOSS OF LEFT HYDRAULIC SYSTEM. FATIGUE FAILURE OF HOSE IN BRAIDS AT SW AGGED B-NUT END. REPLACED HOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600072 20020116 00072 NM 2002 1 16 2002UALA00048 1 20020108 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 FUSE SKIN HAS DENT WITH GOUGES AT STATION 620 S16L TO S17L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600073 20020116 00073 NM 2002 1 16 2002UALA00050 1 20020108 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 FORWARD CABIN FLOORBEAM AT STATION 365, RBL9 HAS EXCESSIVE MATERIAL LOSS, MAJOR REPAIR ACCOMPLISHED. REINFORCING REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600074 20020116 00074 NM 2002 1 16 2002UALA00055 1 20020108 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 FORWARD PIT FUSELAGE SKIN HAS EXCESSIVE MATERIAL REMOVED AT STATION 606 BETWEEN STRINGER 19L AND 20L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600075 20020116 00075 NM 2002 1 16 2002UALA00056 1 20020108 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 EXTERNAL FUSELAGE LOWER SKIN DAMAGED STATION 781 BL 0. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLER REPA IR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600076 20020116 00076 NM 2002 1 16 2002UALA00057 1 20020108 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 AFT PIT FRAME AT STATION 1420 AND STRINGER 26L IS DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REINFORCI NG REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600077 20020116 00077 NM 2002 1 16 2002UALA00058 1 20020108 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 RIGHT HAND APU COMPT. DOOR EXTERNAL SKIN DAMAGED AROUND FORWARD LATCH CUTOUT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCO MPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600078 20020116 00078 NM 2002 1 16 2002UALA00059 1 20020108 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 APU COMPT RIGHT HAND DOOR EXTERNAL SKIN DAMAGED AT 2ND FROM FORWARD LATCH CUTOUT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600079 20020116 00079 NM 2002 1 16 2002UALA00060 1 20020108 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 AFT PIT FRAME HAS DENT AT STATION 1580 BELOW STRINGER 25R 2EA. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBL ER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600080 20020116 00080 NM 2002 1 16 2002UALA00061 1 20020108 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 APU COMPT RIGHT HAND DOOR EXTERNAL SKIN DAMAGED AT 2ND FROM THE LATCH CUTOUT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCO MPLISHED. DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600081 20020116 00081 NM 2002 1 16 2002UALA00063 1 20020108 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 APU COMPT RIGHT HAND DOOR EXTERNAL SKIN DAMAGED AT AFT LATCH CUTOUT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600083 20020116 00083 NM 2002 1 16 2002UALA00067 1 20020109 A 5312 BULKHEAD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 BODY STATION 246 RBL 60 BULKHEAD CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED CHORDS AND ANGLES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002011600084 20020116 00084 NM 2002 1 16 2002UALA00072 1 20020110 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT CABIN FLOORBEAM STATION 1681 FORWARD LOWER SURFACE EXCESSIVE MAT REMOVED AT LBL33. MAJOR REPAIR ACCOMPLISHED. ANGL E REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002011600099 20020116 00099 EA 2002 1 16 COMA0260051 1 20020114 A 5320 6003603023 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 718.00 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 916CA 19895 7014 F.S.718.00 FRAME ON L/H SIDE BELOW STRINGER 11 IS CRACKED.REPAIRED L/H 718.00 FRAME BELOW STRINGER 11 I/A/W WVAC EO 601R -53-2725. 2 L 7 2 4F RT A21EA 2002011600100 20020116 00100 WP 2002 1 16 ZW0A0200701 1 20020115 A 3350 0105606002SMI MODULE DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9403W 53139 THE EGRESS LIGHTS WERE INOPERATIVE AT ROWS 7, 8, 9, 19, 27, 29, AND 31. REPLACED THE LAMP ASSEMBLY/MODULE AT EACH LOCAT ION. CHECK-C 9-10-01 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2002011600139 20020116 00139 NE 2002 1 16 00009 2 20020107 A 7200 ENGINE LEAR 24 24D 5170311 CE GE CJ610 CJ6106 30006 NE LEFT FLAMED OUT E HAEA B EMER. DESCENT X ENGINE FLAMEOUT CL CLIMB 1 SW 05 299TW 24299 251679A DURING CLIMB THROUGH FLT LEVEL 43.8 LT ENGINE FLAMED-OUT, AT FL250 AIRSTART PERFORMED AND CONTINUED FLT AT 370. PILOT P ERFORMED VISUAL INSPECTION OF ENGINE AND FUEL SAMPLE. ENGINE INSPECTED AT YIP BY MAINTENANCE WITH NO DEFECTS NOTED. 2 L 7 2 4J 4 J A10CE 1E16 2002020100008 20020201 00008 NM 2002 2 1 02FDEA00047 1 20020106 A 5315 FLOORBEAM BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 N 676 CORROSION AROUND NUTPLATE HOLES ON LWR CHORD OF 1130 BEAM, LBL 1 TO LBL 38. R&R CHORD PER E.A. 7-5310-62713 & SR M 53-10-1. 2 L 7 3 4F RT A3WE 2002011600150 20020116 00150 EU 2002 1 16 AWXA200200019 1 20020109 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 605AW 543 PHX - EEL - C - DURING INSPECTION MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. MAINTENANCE REPLACED BA TTERIES IN EMERGENCY POWER SUPPLY UNITS 10WL (ZONE 221), 11WL (ZONE 241), AND 12WL (ZONE 242) IAW T/C F1C33301. 2 L 7 2 4F RT A28NM 2002011600151 20020116 00151 NM 2002 1 16 AWXA200200020 1 20020107 A 5230 65469212 WEB BOEING 737 7373S3 1384711 NM CARGO DOOR DEFORMED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 MCN - MAJOR REPAIR - C - DURING C-15 CHECK MAINTENANCE FOUND EVIDENCE OF DEFORMED MATERIAL ON THE FWD CARGO DOOR INNER S KIN LIGHTING HOLES, 3RD ROW OF HOLES FROM BOTTOM AT FWD SIDE OF DOOR BS 440 TO BS 460. MAINTENANCE REMOVED DAMAGED PORT ION OF WEB AT TWO POSITIONS ON FWD CARGO DOOR, FABRICATED 2 REPAIR WEBS AND INSTALLED IAW B737-300 SRM 51-40-02, PG 3-4. 2 L 7 2 4F RT A16WE 2002011600152 20020116 00152 EU 2002 1 16 AWXA200200021 1 20020111 A 2910 NAS161212 O-RING AIRBUS 320 A320232 3930326 EU HYDRAULIC SYS RUPTURED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 652AW 0953 LAS - DIVERSION - FLT 522 - C - EN ROUTE FROM PHX TO RNO FLIGHT CREW RECEIVED YELLOW HYDRAULIC SYSTEM FLUID LOSS INDICAT ION FOLLOWED BY FLIGHT CONTROL DEGRADATION TO ALTERNATE LAW, THIS WAS CAUSED BY LOSS OF NR 2 YELLOW YAW DAMPER, NR 1 YAW DAMPER PREVIOUSLY ON MEL. AIRCRAFT DIVERTED SAFELY TO LAS. MAINTENANCE TROUBLESHOT AND FOUND LEAK AT YELLOW HYDRAULIC PTU MANIFOLD QUICK DISCONNECT FITTING. REPLACED O-RING IAW CMM 29-10-05, LEAK TESTED GOOD. POST FLIGHT REPORT REVEALE D ALTERNATE LAW WAS CAUSED BY FAILURE OF RT AILERON BLUE SERVO FOLLOWED BY YELLOW AILERON SERVO FAILURE. 2 L 7 2 4F RT A28NM 2002011600155 20020116 00155 NM 2002 1 16 AWXA200200025 1 20020103 A 5330 65458901 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - MAJOR REPAIR - C - DURING C-17 CHECK L1 DOOR LOWER FUSELAGE HINGE CUTOUT WAS FOUND CRACKED APPROXIMATELY .25 INCH FORWARD BS 305. MAINTENANCE REMOVED DAMAGED AREA OF CUTOUT SKIN AT DOOR HINGE BS 305, FABRICATED A REPAIR PLATE AND INS TALLED REPAIR IAW 53-10-01, FIG 205, PG 217-218. 2 L 7 2 4F RT A16WE 2002011600156 20020116 00156 NM 2002 1 16 AWXA200200029 1 20020102 A 5315 654881138 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - MAJOR REPAIR - C - DURING C-17 CHECK CORROSION WAS FOUND ON FLOORBEAM UPPER FLANGE AT BS 986, RBL 3 TO LBL 18. RE MOVED DAMAGED AREA OF FLOORBEAM UPPER T-CHORD AT BS 986, RBL 3 TO LBL 50. FABRICATED 2 SPLICE STRAPS AND REPAIR ANGLES AND NEW UPPER T-CHORD AND INSTALLED REPAIRS IAW AWA ER 03-5310-02011-ES4. 2 L 7 2 4F RT A16WE 2002011600157 20020116 00157 2002 1 16 DL76L020012 4 20020106 A 2300 PHONE BOEING 767 767332 1382001 NM CABIN INTERMITTENT A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 183DN 27110 INBOARD FLT ATTENDANT REPORTED HOT ELECT SMELL IN AREA OVERHEAD SEATS 3AB AND 4AB. PERFORMED THOROUGH INSPECTION OF FWD CABIN AREA. UNABLE TO DUPLICATE ANY ELECT SMELLS. SUSPECT POSSIBLE AIR PHONE PROBLEM DUE INTERMITTENT AT TIME OF REPO RT. DEACTIVATED AIR PHONE SYS BY PULLING C/B. 2 L 7 2 4F RT A1NM 2002011600159 20020116 00159 NE 2002 1 16 DL76S020013 2 20020106 A 7310 MANIFOLD BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENGINE DEFECTIVE A DALA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SO 27 136DL 31611 580394 23146 580394 ENGINE FLAME-OUT ON CLIMBOUT AT 34000. RETURNED FOR LANDING AT MCO. ENGINE FAILED NO MORE THAN 27 MINUTES FROM LANDING . REPLACED FUEL MANIFOLDS AT 11 O'CLOCK AND 6 O'CLOCK POSITIONS RAN NR 2 ENG PER PFHB TEST 4 T/O POWER AND LEAK CK ALL PARAMETERS OK OK FOR SVC. ALSO REPLACED RIGHT ENGINE FUEL FILTER. 2 L 7 2 4F 4 F RT A1NM E13NE 2002011600163 20020116 00163 NM 2002 1 16 DLM11020007 1 20020103 A 2820 4059025907 CONTROLLER DOUG MD11 MD11 3023602 NM RT WING FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 803DE 48474 TANK 1 FUEL QTY WENT AMBER WITH FSC IN AUTO. REPLACED FSC. 2 L 7 3 4F RT A22WE 2002011700023 20020117 00023 NM 2002 1 17 CALA0200021 1 20020117 A 7110 314A10102 NOSE COWL BOEING 737 7373T0 1384582 NM #1 ENGINE DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND #1 ENGINE NOSE COWL DELAMINATED. THE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-11-01. 2 L 7 2 4F RT A16WE 2002011700024 20020117 00024 NM 2002 1 17 CALA0200022 1 20020117 A 5342 ATTACH ANGLE BOEING 737 7373T0 1384582 NM STA 1104-1121 WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND ATTACH ANGLE ON BOTTOM OF VERTICAL STABILIZER ON R/H SIDE WORN THIN AT STA 1104-1121. THE ATTACH ANGLE WAS REPLACED IAW ECRA 5300-01013, REV B. 2 L 7 2 4F RT A16WE 2002011700025 20020117 00025 WP 2002 1 17 CALA0200023 1 20020115 A 3231 39567851 LINK DOUG DC9 DC981 3022081 WP NLG FWD DOOR FAILED A CALA A D UNSCHED LANDING RETURN TO BLOCK E VIBRATION/BUFFET CL CLIMB 1 SW 09 14871 48022 WHEN THE GEAR WAS RAISED AFTER TAKEOFF, THE GEAR RETRACTED WITH ALL INDICATIONS NORMAL. THERE WAS A LOUD NOISE INDICATIV E OF THE NOSE GEAR DOOR HANGING DOWN AND WHICH WAS ACCOMPANIED BY STRONG VIBRATION IN THE NOSE GEAR AREA. THE GEAR WAS C YCLED WITH NO CHANGE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE R/H NLG F ORWARD DOOR LINK AT FAULT. THE DOOR LINK WAS REMOVED AND REPLACED IAW MM 32-22-01, PAGE 202 AND RIGGING WAS PERFORMED IA W MM 32-22-01, PAGE 202. THE GEAR WAS CYCLED AND OPERATION CHECKED NORMAL. 2 L 7 2 4F A6WE 2002011700031 20020117 00031 NM 2002 1 17 SWAA020103 1 20020111 A 5320 6547977 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D CHECK, FOUND WEB CRACKED AT BS 294.5, STR 16L. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002011700032 20020117 00032 NM 2002 1 17 SWAA020104 1 20020114 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED 1/4D CHECK, FOUND RT BULKHEAD WEB CRACKED AT BS 178. REMOVED AND REPLACED WEB PER SRM AND SWA ACO. 2 L 7 2 4F RT A16WE 2002011700033 20020117 00033 NM 2002 1 17 SWAA020105 1 20020114 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS CRACKED (3 EA) AT BS 747, RBL 14, BS 787, RBL 14 AND BS 945, RBL 3. REPAI RED FLOORBEAMS PER SRM. 2 L 7 2 4F RT A16WE 2002011700034 20020117 00034 NM 2002 1 17 SWAA020107 1 20020114 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002011700043 20020117 00043 NM 2002 1 17 AWXA200200022 1 20020112 A 3241 WARNING SYSTEM BOEING 737 737277 1384570 NM COCKPIT MALFUNCTIONED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 184AW 22651 PHX - ABORTED T/O - FLT 644 - S - UPON RELEASE OF BRAKES FLIGHT CREW RECEIVED AMBER WARNING MESSAGES FOR INBOARD AND OUT BOARD ANTI-SKID CHANNELS INOPERATIVE AND AUTO-BRAKES, AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE. AT GATE MAINTENANC E ISSUED A DPI, MEL 32-2, CONDITION NR 1, BOTH ANTI-SKID CHANNELS INOPERATIVE. MAINTENANCE PERFORMED ANTI-SKID TEST PER BMM 32-42-00-501 AND AUTO-BRAKE TEST PER BMM 32-43-01-401, BOTH SYSTEMS CHECKED GOOD WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 2002011700051 20020117 00051 NM 2002 1 17 AWXA200200032 1 20020113 A 3040 WB0710 CONNECTOR BOEING 757 757225 1384959 NM COCKPIT DEFECTIVE A AWXA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 907AW 22691 AFTER T/O NOTICED BURNING SMELL IN FLT DECK (NO SMOKE), SHUT OFF RECIR FAN, SMELL BEGAN TO DISSIPATE. MX COULD NOT DUPL ICATE. AGAIN NOTICED ELECTRICAL BURNING ODOR IN FLT DECK. LT & RT UTILITY BUSSES WERE SHUT DOWN, ODOR DISSIPATED. MX REPLACED RT RECIR FAN, R & R NR 2 FWD EQUIP COOLING FAN. BOTH AC PACKS, NR 2 EQUIP COOLING FAN RAN FOR HOURS, NO ABNORM . TEST FLT MX ONBOARD, AT 30 TO 40 XA SMOKE & ODOR APPEARED AT RT FWD WINDOW LOWER RT CORNER COMING FROM A WINDOW ANTI- ICE CONNECTOR. POWER TO CONNECTOR WAS SHUTDOWN. MX FOUND J5 CONNECTION POINT LOOSE AT LWR RT CORNER OF F/O'S WINDOW. CLEANED TERMINAL, WINDOW CONTACTS, REPLACED WINDSHIELD CONNECTION PLUG & PACKING. 2 L 7 2 4F RT A2NM 2002011700063 20020117 00063 EU 2002 1 17 MALA020110 1 20020103 A 3230 SELECTOR VALVE BAC 146 AVRO146RJ85A 1500097 EU FAULTY A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 520XJ E2345 During Flight #3631, at 12,000 Ft level Right Main Gear appeared to drop from the well. Indication of down, locked. Al so Aircraft slowed considerably Auto Throttle and Auto Pilot were engaged. Gear appeared to drop at 290 Kt. indicated. All hydraulic pressure and quantity normal. Landed with out incident and gear worked normally. Maintenance suspects fa ulty Landing Gear Selector Valve, replaced Valve IAW AMM, performed several Gear swings with no occurance. All checks g ood at this time. 2 H 7 4 4F RT A49EU 2002011700074 20020117 00074 NM 2002 1 17 AWXA200200033 1 20020113 A 3350 1012621 LIGHT BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 188AW 22655 PHX - EEL - C - DURING INSPECTION EMERGENCY EXIT LIGHT AT L1 DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INDICATOR ASSEMBLY AT STA 328. 2 L 7 2 4F RT A16WE 2002011700075 20020117 00075 NM 2002 1 17 AWXA200200034 1 20020114 A 3350 20121 CHARGER BOEING 737 737317 138447P NM CABIN FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 YVR - EEL - C - DURING C-13 CHECK, LT OVERWING EMERGENCY LIGHT DID NOT REACH TEST VALUE OF 300MA. MAINTENANCE REMOVED A ND REPLACED LT OVERWING EMERGENCY LIGHT BATTERY CHARGER M1134 IAW BMM 33-51-51, PG 206-207, STEP 4A-D. OPERATIONAL CHEC K C/W IAW T/C A1C33005. 2 L 7 2 4F RT A16WE 2002011700077 20020117 00077 NM 2002 1 17 AWXA200200035 1 20020114 A 3350 29131A BATTERY PACK BOEING 757 7572G7 1384963 NM CABIN DEFECTIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 908AW 24233 WHEN MX ARRIVED AT AIRCRAFT FOUND EMERGENCY LIGHTING WAS LEFT ON FOR AN UNDETERMINED PERIOD OF TIME. MX REMOVED AND REP LACED ALL EMERGENCY LIGHT BATTERY PACKS. DURING EMERGENCY LIGHT OPERATIONAL TEST MX FOUND THAT THE AISLE EMERGENCY LIGH TS WERE COMING ON INTERMITTENTLY WITH EMERGENCY LIGHT ARM SWITCH IN OFF POSITION. AT THIS TIME NOTED THAT EMERGENCY EXI T LIGHT OVER L1 DOOR DID NOT ILLUMINATE. FOUND THE L1 DOOR BATTERY PACK THAT HAD JUST BEEN INSTALLED WAS BAD. REPLACED EMERGENCY BATTERY PACK AT L1 DOOR IAW BMM 33-51-07. MX TROUBLESHOT THE INTERMITTENT EMERGENCY AISLE LIGHT PROBLEM TO T HE EMERGENCY LIGHT ARM SWITCH PANEL AND REPLACED THE PANEL. OPERATIONAL CHECK OF EMERGENCY LIGHTING SYS TESTED GOOD. 2 L 7 2 4F RT A2NM 2002011700079 20020117 00079 NM 2002 1 17 AWXA200200036 1 20020113 A 2841 39302601837 INDICATOR BOEING 737 737277 1384570 NM COCKPIT FAULTY A AWXA O OTHER O OTHER CR CRUISE 1 WP 28 182AW 67840 1961 22649 PHX - EMERGENCY LANDING - FLT 624 - EN ROUTE FROM OAK TO PHX AIRCRAFT DECLARED AN EMERGENCY LANDING WHEN THE NR 2 FUEL Q UANTITY INDICATOR BEGAN TO STICK AT EVERY 1000 LBS. THE NR 1 FUEL QUANTITY INDICATOR WAS ALREADY ON MEL, AIRCRAFT MADE UNEVENTFUL LANDING AT SCHEDULED DESTINATION. MAINTENANCE TROUBLESHOT AND REPLACED BOTH THE NR 1 AND NR 2 FUEL QUANTITY INDICATORS IAW BMM 28-41-51, OPERATIONAL CHECK OF BOTH INDICATORS WAS GOOD. 2 L 7 2 4F RT A16WE 2002011700081 20020117 00081 NM 2002 1 17 C1HA200296009 1 20020114 A 3350 BATTERY BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 696CA 22574 R-1 DOOR EMERGENCY EXIT LIGHT ASSY (INSIDE LIGHT) INOPERATIVE. RECHARGED BATTERY ASSEMBLY FROM A/C POWER, OPS CHECKS GO OD. 2 L 7 3 4F RT A3WE 2002011700083 20020117 00083 SO 2002 1 17 C2XA02CL009 1 20020113 A 4990 OIL SYSTEM EMB 145 EMB145LR 3260212 SO APU OVERSERVICED A C2XA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 13975 145163 EWR FLIGHT 3505 THE CREW REPORTED THE APU EMITS STRONG FUMES IN THE CABIN. MAINTENANCE INSPECTED AND PLACED ON MEL. TH EN FOUND APU OIL LEVEL TO BE TOO HIGH. THE OIL LEVEL WAS REDUCED TO PROPER LEVEL AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002011700084 20020117 00084 NM 2002 1 17 CALA0200017 1 20020113 A 5347 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17317 23368 INSPECTION FOUND AFT BAGGAGE BIN RT TIE DOWN RAIL CORRODED AT STA 787-847. THE RT TIE DOWN RAIL WAS REMOVED AND REPLACE D IAW SRM 51-10-02 AND 53-00-53, FIGURE 202. 2 L 7 2 4F RT A16WE 2002011700085 20020117 00085 NM 2002 1 17 CALA0200018 1 20020113 A 5347 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17317 23368 INSPECTION FOUND AFT BAGGAGE BIN FLOOR RAIL CORRODED AT STA 770, RBL 8. THE FLOOR RAIL WAS REPAIRED IAW ECRA 5320-01603 . 2 L 7 2 4F RT A16WE 2002011700086 20020117 00086 NM 2002 1 17 CALA0200019 1 20020113 A 5347 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17317 23368 INSPECTION FOUND AFT BAGGAGE BIN FLOOR RAIL CORRODED AT STA 770, LBL 3 TO LBL 12. THE FLOOR RAIL WAS REPAIRED IAW ECRA 5320-01603. 2 L 7 2 4F RT A16WE 2002011700087 20020117 00087 SO 2002 1 17 CHQ00090 1 20020109 A 3250 B-NUT EMB 145 EMB145 3260210 SO NLG STEERING LOOSE A CHQA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 11 280 145381 LOST NR 1 HYDRAULIC (DECLARED EMERGENCY) LANDED IN CMH. B-NUT WAS FOUND LOOSE ON NOSEWHEEL STEERING MANIFOLD, TIGHTENED SCREW AND OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2002011700088 20020117 00088 SO 2002 1 17 CHQ00091 1 20020113 A 7540 WARNING SYSTEM EMB 145 EMB145 3260210 SO COCKPIT ACTIVATED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 274 145344 LOUD BANG FOLLOWED BY NR 2 BLEED EICAS MESSAGE. 2 L 7 2 4F RT T00011AT 2002011700089 20020117 00089 SO 2002 1 17 CHQ00092 1 20020114 A 3610 FITTING EMB 145 EMB145 3260210 SO BLEED AIR SYS LEAKING A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 274 145344 AIRCRAFT HAD BLEED LEAK. REMOVED AND REPLACED BLEED FITTING. 2 L 7 2 4F RT T00011AT 2002011700115 20020117 00115 NM 2002 1 17 PCAA0201015 1 20020116 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM POSITION 400 INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 835EX 289 DURING ROUTINE MAINTENANCE VISIT RIGHT AFT EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. POWERSUPPLY BOX AT POSITION #400 AN D 2 BATTERIES WERE REPLACED, POSITION #400 AND #600. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002011700123 20020117 00123 NM 2002 1 17 DLM88020001 1 20020101 A 2131 21184901S4 CONTROLLER DOUG MD88 MD88 3023688 NM CABNI PRESSURE FAILED A DALA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 SO 27 972DL 53215 AT FLT LEVEL 230 DURING CLIMB FLOW LIGHT ILLUM, A MAX DESCENT TO 10,000 FT, O2 MASKS DEPLOYED. FINALLY AT 10,000 FT ABL E TO REGAIN AUTO 2. CLIMBED TO FL220 FOR REMAINDER OF FLT. AUTO 2 WORKED OK REST OF FLT. REPLACED AUTO CONTROLLER 1. 2 L 7 2 4F RT A6WE 2002011700125 20020117 00125 NM 2002 1 17 DLM88020015 1 20020106 A 1100 PLACARD DOUG MD88 MD88 3023688 NM ELT TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 995DL 53362 AUTOMATIC ACTIVATION SAFETY PLACARDS TORN ON ELT. REPLACED ELT. FOUND DURING A LAYOVER. 2 L 7 2 4F RT A6WE 2002011700128 20020117 00128 NM 2002 1 17 DLM88020017 1 20020105 A 2120 DUCT DOUG MD88 MD88 3023688 NM A/C BAY DISCONNECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 981DL 53268 SMOKE IN CABIN. FOUND RT ACM DISCHARGE CABIN SUPPLY DUCT DISCONNECTED JUST FWD OF ACM. RECONNECTED SUPPLY DUCT AND RE MOVED WATER SEPARATORS DUE TO INSULATION INGESTION. FOUND RT WATER SEPARATOR BAG MELTED. REPLACED BAGS AND REINSTALLED WATER SEPS. 2 L 7 2 4F RT A6WE 2002011700132 20020117 00132 NM 2002 1 17 DLM88020021 1 20020106 A 4990 APU DOUG MD88 MD88 3023688 NM APU BAY LEAKING A DALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 901DL 12000 49532 P80224 FUMES IN COCKPIT AND CABIN DURING CLIMBOUT FROM PVD. AFT LAV SMOKE ALARMS SOUNDED AND THEN STOPPED. FUMES DISSIPATED B UT NEVER WENT AWAY. PERFORMED OP 5088. INSP RECIR FAN, LT AND RT AIR CYCLE MACHINES. REPLACED WATER SEPARATOR BAGS. PERFORMED DUCT BURNOUT AND FULL PWR RUN. NO ABNORMALITIES NOTED. OK FOR SVC. FOUND APU LEAKING OIL AND INGESTING INTO INLET. REPLACED APU. 2 L 7 2 4F RT A6WE 2002011700139 20020117 00139 SO 2002 1 17 C2XA02CL010 1 20020116 A 4900 DRAIN LINE EMB 145 EMB145ER 3260211 SO APU LOOSE A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 16944 145045 CLE FLIGHT#3275 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AFTER APU START ON THE GROUND OR IN FLIGHT.MAINTENA NCE INSPECTED AND RESECURED DRAIN LINE ON THE APU FUEL PUMP.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR S ERVICE. 2 L 7 2 4F RT T00011AT 2002011700140 20020117 00140 NE 2002 1 17 HNAA0200001 2 20020110 A 7530 310848501 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE FAILED A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 941HA 161 121318 OIL SMELL IN CABIN AND FLIGHT DECK IN FLIGHT WITH POWER BELOW 30 PERCENT TORQUE SETTING. TURNED NR 2 BLEED OFF AND SMEL L WENT AWAY. REPLACED NR 2 AIR SWITCHING VALVE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002011700141 20020117 00141 EU 2002 1 17 MALA020105 1 20020105 A 3620 SENSOR SAAB SF340 SF340A 7850100 EU BLEED AIR SYS DEFECTIVE A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 991XJ 340A091 DURING FLIGHT 3365 OUT OF DTW, RT DUCT OVER TEMP LIGHT CAME ON SEVERAL TIMES EVEN WITH A COLD TEMP SELECTED. A MID-TEMP AND THE TEMP SELECTOR IN MANUAL WHEN BLEED WAS OPEN WARM AIR WAS BEING BLOWN OUT, EVEN WITH TEMP SELECTED TO COLD. AIR RETURN TO DTW. MAINTENANCE INSPECTED SYSTEM, SYSTEM OPERATED NORMALLY IN MANUAL AT ALL TIMES AUTO MODE INTERMITTENT. MAINTENANCE REPLACED DUCT TEMP SENSOR, DUCT OVERTEMP SWITCH, RIGHT DECK CONTROLLER SWAPPED FOR COMPARATIVE MX CONTROL AU TO TEMP SENSOR. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2002011700142 20020117 00142 EU 2002 1 17 MALA020106 1 20020106 A 3230 SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG BROKEN A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 76XJ 340A076 AFTER TAKEOFF IN APN, GOT HYDRAULIC CAUTION LIGHT AFTER GEAR WAS SELECTED UP. COMPLETED (MEMORY ITEMS) AND NOTED MAIN P RESSURE WAS ZERO, EMERGENCY AND BRAKES WERE BOTH GOOD. RAN QRH AND LANDED IN DTW. MAINTENANCE FOUND RT MAIN GEAR DOWNL OCK SWIVEL BROKEN. REMOVED AND REPLACED MAIN GEAR DOWNLOCK SWIVEL AND RT AND LT SEPARATION BOLTS P/N 117510-1 IAW CHAP 32. RETRACTED GEAR SEVERAL TIMES, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002011700143 20020117 00143 WP 2002 1 17 MWEA020054 1 20020115 A 3240 500432114 LINE DOUG DC9 DC981 3022081 WP BRAKE SYSTEM LEAKING A MWEA D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 812ME 48006 NR 1 BRAKE SMOKING DURING TAXI-OUT. REMOVED AFT BRAKE HOSE AND CLEANED RESIDUAL HYDRAULIC FLUID. DEFERRED NR 1 BRAKE L EFT SYSTEM PER MEL 32-10. 2 L 7 2 4F A6WE 2002011700144 20020117 00144 NM 2002 1 17 P2EA2002M002 1 20020110 A 2752 BUSHING BOEING 737 7372Q8 138448K NM FLAP GEAR BOX WORN A P2EA K NONE E VIBRATION/BUFFET AP APPROACH 1 CE 05 121NJ 21735 RIGHT HAND TRAILING EDGE FLAP FLUTTERS VISIBLY AT FLAPS 5 ABOVE 200 KTS. OK AT 190 KTS AND AT ALL OTHER FLAP SETTINGS. INSPECTED AND FOUND THE NR 7 FLAP JACKSCREW GEAR BOX END UNIVERSAL JOINT BUSHINGS WORN. OVERHAULED THE NR 7 FLAP JACKS CREW GEAR BOX END UNIVERSAL JOINT IAW BOEING OVERHAUL MANUAL 27-55-56. OP'S CHECKED FLAPS PER BOEING MM 27-51-73 AND OP 'S CHECKED GOOD. 2 L 7 2 4F RT A16WE 2002011700156 20020117 00156 WP 2002 1 17 ZW0A0200403 1 20020102 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT BETWEEN STA 693 AND 712, LONGERON 29L, THE BOTTOM FLANGE OF INTERCOSTAL WAS CORRODED. INSTALLED NE W INTERCOSTAL WITH NEW FASTENERS PER SRM 51-30-1. 2 L 7 2 4F A6WE 2002011700157 20020117 00157 WP 2002 1 17 ZW0A0200404 1 20020103 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT IN THE AFT CARGO COMPT, STA 1231, THE AFT FACE OF FORMER 29L TO 29R HAD CORROSION. REPLACED SECTIO N OF FORMER WITH NEW. CUT AND SPLICED AT STRINGER 26 TO 27L. SPLICED SECTION PER 53-03, FIGURE 2A OF SRM, REPLACED LEF T SIDE FLOOR SUPPORT. 2 L 7 2 4F A6WE 2002011700158 20020117 00158 WP 2002 1 17 ZW0A0200405 1 20020105 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT IN THE FWD CABIN FOUND CHAIR TRACK CORRODED AT RBL 44, STA 201 TO 237. REPLACED CHAIR TRACK STA 20 1 TO 237 PER SPM 6-70-01, AND SRM 53-04 FIG 4. 2 L 7 2 4F A6WE 2002011700159 20020117 00159 WP 2002 1 17 ZW0A0200406 1 20020107 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND CABIN CHAIR TRACK CORRODED, STA 1127 TO 1136, LBL 36. REMOVED CORRODED TRACK AND REPLACED TR ACK PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2002011700160 20020117 00160 WP 2002 1 17 ZW0A0200407 1 20020108 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND IN CABIN SIDE WALL, CORROSION ON FLOOR MEMBRANE STA 1091 TO 1093, LONGERON 18L. INSTALLED RE PAIR DOUBLER PER SRM 51-70-4, FIG 2. 2 L 7 2 4F RT A6WE 2002011700161 20020117 00161 WP 2002 1 17 ZW0A0200408 1 20020104 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 180, LBL 56. REMOVED OLD SUPPORT AND FABRICATED AND INSTALLED NEW SUPPORT PER SRM 51-30-2. 2 L 7 2 4F RT A6WE 2002011700162 20020117 00162 WP 2002 1 17 ZW0A0200409 1 20020104 A 5320 DOUBLER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT IN THE AFT CARGO COMPT AT LONGERON 25L, THE STIFFENER HAD DOUBLER WITH CORROSION AT STA 1271, STA 1 283, 1250, 1240 AND 1231. THE DOUBLERS WERE ON TOP OF THE STIFFENERS AND FORMERS. REMOVED CORROSION PER SRM 51-10-3. MADE NEW DOUBLER AS NEEDED PER SPM 6-70-01. INSTALLED PER SRM 51-30-2. 2 L 7 2 4F RT A6WE 2002011700163 20020117 00163 WP 2002 1 17 ZW0A0200501 1 20020109 A 5320 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT FOUND CORROSION ON STA 1309 FORMER REPAIR SPLICE, AFT SIDE BETWEEN LONGERON 29L AND 29R. REPLACED FORMER REPAIR SPLICE PER SRM 53-03, FIG 2A. 2 L 7 2 4F A6WE 2002011700164 20020117 00164 NM 2002 1 17 P5CA0200627 1 20020112 A 7603 CONTROL UNIT BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 3 ENGINE OUT OF RIG A P5CA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 23 920FT 22237 702114 NR 3 ENG WOULD NOT ACHIEVE T/O THRUST. 1.58 MAX PWR WAS APPLIED, THRUST LEVER WAS MOVED TO FIREWALL THRUST W/ MAX EPR O F 1.38. OTHER PARAMETERS NORMAL WHEN ASSOCIATED W/ & EPR SETTING OF 1.38 ENG RUN TO MAX POWER FOR OPS CK INTO WIND (250 /11). ENG SLOW TO RESPOND TO THROTTLE MOVEMENT. MAX EPR WAS 1.40. RIGGED NR 3 ENG THRUST LEVER CONTROLS IAW MM 76-11- 00, SECTION 4. OPS CK OK ON ENG RUN, IAW MM 71-00-00. ALL ENG PARAMETERS NORMAL ON GROUND RUN. 2 L 7 4 4F 4 F A20WE E3NE 2002011700166 20020117 00166 WP 2002 1 17 ABXA010666 1 20020110 A 5700 SPAR DOUG DC8 DC861 3021952 WP LEFT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 LEFT WING, FORWARD SPAR CAP AT XFS 520.76 HOLE HAD A CRACK INDICATION WITH HFEC DETERMINE CRACK LENGH AND LOCATION IAW E S00046. REPAIRED CRACKED HOLE IAW DAC DWG 4709980 AND DC-8 SRM 51-1-25. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 2002011700167 20020117 00167 WP 2002 1 17 ZW0A0200801 1 20020116 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP B59004 A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 907TW 49165 THE AFT CABIN EMERGENCY LIGHTS STAYED ILLUMINATED WITH THE COCKPIT SWITCH SELECTED OFF. REPLACED THE BATTERY PACK. CHE CK-C 6-15-01 MCI. --CLOSED-- 2 L 7 2 4F A6WE 2002011700176 20020117 00176 EA 2002 1 17 COMA0260052 1 20020115 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 989CA 7215 FLIGHT 5602 EMERGENCY FLOOR PATH LIGHTING IS INOPERABLE AT LAST ROW.DEFERRED MAINTENANE PER MEL. 2 L 7 2 4F RT A21EA 2002011700177 20020117 00177 EA 2002 1 17 COMA0260053 1 20020115 A 2410 100021101 CHARGER CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP INOPERATIVE A COMA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SO 01 964CA 6344 7129 FLIGHT 5492 MAIN BATTERY CHARGER MESSAGE.REPLACED BATTERY CHARGER. 2 L 7 2 4F RT A21EA 2002011800047 20020118 00047 WP 2002 1 18 IXXA0200001O 1 20020117 A 2933 EA1066A2183 TRANSMITTER DOUG DC8 DC871F 302199D WP FUSELAGE DEFECTIVE A IXXA O OTHER K FLUID LOSS CR CRUISE 1 SW 11 824BX 80532 2000 45946 WHILE ENROUTE FROM JFK TO BDL, THE FLIGHT CREW NOTICED THAT THE MAIN HYDRAULIC QUANTITY SYSTEM WAS DECLINING. THE FLIGH T CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO BDL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT A ND TRACED THE PROBLEM TO A FAULTY HYDRAULIC QUANTITY TRANSMITTER. MAINTENANCE REPLACED THE TRANSMITTER AND PERFORMED OP ERATIONAL CHECKS IN ACCORDENCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002011800048 20020118 00048 NM 2002 1 18 CALA0200024 1 20020117 A 5730 SKIN BOEING 737 7373T0 1384582 NM R/H WING L/E DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND R/H WING LEADING EDGE SKIN UNDER O/B EDGE OF #5 SLAT DELAMINATED. REPAIRED IAW ECRA 5721-01048. 2 L 7 2 4F RT A16WE 2002011800049 20020118 00049 NM 2002 1 18 CALA0200025 1 20020117 A 5730 SKIN BOEING 737 7373T0 1384582 NM L/H WING L/E DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND L/H WING LEADING EDGE SKIN DELAMINATED AND HILOCK PULLED THROUGH SKIN BEHIND #2 SLAT AT O/B END. REPAIR ED IAW ECRA 5721-01048. 2 L 7 2 4F RT A16WE 2002011800050 20020118 00050 NM 2002 1 18 CALA0200026 1 20020117 A 5230 SKIN BOEING 737 7373T0 1384582 NM FWD CARGO DR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17317 23368 INSPECTION FOUND FORWARD CARGO DOOR OUTER SKIN DENTED IN CENTER OF DOOR. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01 . 2 L 7 2 4F RT A16WE 2002011800062 20020118 00062 CE 2002 1 18 00010 1 20020114 A 3610 3001242 O-RING LEAR 24 24D 5170311 CE GE CJ610 CJ610* 30006 NE BLEED AIR SYS DAMAGED E HAEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 05 277TW 277 251458 RIGHT ENGINE FIRE WARNING ILLUMINATED. ENGINE BROUGHT BACK TO FLIGHT IDLE, LIGHT DID NOT GO OUT. SHUT DOWN ENGINE. ME CHANIC DISPATCHED TO AIRCRAFT, INSPECTED ENGINE NO EVIDENCE OF FIRE, FOUND BLEED AIR LEAK AT PYLON REPLACED O-RING AND T WO FIRE BOTTLES RETURN AIRCRAFT TO SERVICE. 2 L 7 2 4J 4 J A10CE 1E16 2002011800069 20020118 00069 NM 2002 1 18 2002UALA00015 1 20020105 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 FUSELAGE HAS SKIN DENT 20 INCHES AFT OF FORWARD LAVATORY SERVICE DOOR, JUST BELOW STRINGER 21R. MAJOR REPAIR ACCOMPLISH ED. EXTERNAL SKIN DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002011800070 20020118 00070 NM 2002 1 18 2002UALA00016 1 20020107 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 CABIN BODY FRAME WEB IS CRACKED AT PSU SUPPORT BRACKET FASTENER BODY STATION 380, STRINGER 8L - 9L. MAJOR REPAIR ACCOMP LISHED. ACCOMPLISHED FRAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002031400176 20020314 00176 NE 2002 3 14 2002UALA00017 2 20020106 A 7230 1B7990 STATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 575UA 1257 26689 726686 NUMBER 1 ENGINE COMPRESSOR STALL. FOUND 10TH STAGE STATOR FAILED. THIS STATOR HAD THE NEW GOLD/NICKEL BRAZE MATERIAL A S PER PWA SERVICE BULLETIN. STATOR HAD 470 CYCLES SINCE 100 PERCENT VANE REPLACEMENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031500081 20020315 00081 NM 2002 3 15 2002UALA00018 1 20020105 A 7500 321697 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 WP 29 547UA 25368 727124 NUMBER 1 ENGINE EGT REACHED 648 DEGREES ON CLIMBOUT. 14TH STAGE CONVERTER VALVE WAS REPLACED DUE TO MESSAGES. ON THE F OLLOWING FLIGHT THE ENGINE HAD HIGH EGT AT TAKEOFF AND RETURNED TO FIELD. CONVERTER VALVE AND THE 14TH STAGE BLEED VALV E (BEANPOT) WAS REPLACED. ENGINE CHECKED GOOD AFTER THIS. SHOP FINDINGS: SERVO VALVE ON CONVERTER VALVE FAILED. 14TH STAGE BLEED VALVE (BEANPOT) CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002012200171 20020122 00171 NM 2002 1 22 2002UALA00019 1 20020103 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EEL LIGHT INOP AT AFT GALLEY LEFT HAND NEXT TO LAV 117. REPLACED EEL STRIP NEXT TO LAV 117. 2 L 7 4 4F 4 F RT A20WE E24NE 2002012200172 20020122 00172 NM 2002 1 22 2002UALA00020 1 20020105 A 3350 ELEMENT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT STRIP AFT ELEMENT IS OUT AT SEAT 5A AND F. FWD ELEMENT IS LOOSE, REPAIRED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002012200173 20020122 00173 NM 2002 1 22 2002UALA00021 1 20020105 A 3350 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 DOOR 3 LEFT AFT GREEN EMERGENCY EXIT LIGHT INOP. REPLACED PWR SUPPLY ABOVE DOOR 3 LEFT. DOOR 3 LEFT AFT GRN EXIT LIGHT AND GALLEY WALL LIGHT ACROSS FROM DOOR 3 LEFT NOW WORKING. 2 L 7 4 4F 4 F RT A20WE E24NE 2002012200174 20020122 00174 NM 2002 1 22 2002UALA00022 1 20020103 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE POWER SUPPLY BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 BOTH FORWARD EXTERIOR OVERWING EMERGENCY LIGHT ASSEMBLY'S INOP ON LEFT HAND SIDE. REPLACED FUSE IN POWER SUPPLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2002011800076 20020118 00076 NM 2002 1 18 P5CA0200626 1 20020112 A 2910 2670169M6 REDUCER BOEING 747 7472U3B 1384846 NM HYDRAULIC SYS CRACKED A P5CA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 923FT 22769 LOST ALL HYD ON NR 1 HYD SYS AFTER LANDING. FOUND RT TRUCK POSITIONER BYPASS REDUCER FLANGE CRACKED. REMOVED AND REPLA CED ASSY PER MM 32-13-16, IPC 32-13-05-02 NR 40. BLED SYSTEM UNTIL NO AIR NOTED. 2 L 7 4 4F RT A20WE 2002011800077 20020118 00077 NM 2002 1 18 SABA020006 1 20020117 A 3350 1013075 LIGHT DHAV DHC8 DHC8102 2809003 NM BLEW OUT A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 841PH 082 Flight 5027 from CLT to CVG: During preflight pilot found two foward emergency floor lights out. Maintenance remoned and replaced Bulbs. System ops checked good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002011800079 20020118 00079 NM 2002 1 18 P5CA0200628 1 20020113 A 7711 ED7472017 TRANSMITTER BOEING 747 747249F 1384849 NM NR 3 ENGINE FAULTY A P5CA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 23 920FT 22237 ON APPLICATION OF PWR AT T/O NR 3 ENG NOT ACCELERATING TO 1.58 EPR SETTING. T/O DISCONTINUED. REMOVED AND REPLACED TT2 SENSOR PER 73-21-04. LEAK CKS GOOD BUT NO HELP. ON ENG RUN IDLE TO 80 PERCENT, N1 TOOK 4.5 SECS, EPR LAGGED AND STABI LIZED - TOOK 10 SECS FROM 80 PERCENT N1 TO IDLE. N1 & N2 DROPPED W/IN TIME BUT EPR WAS SLOW TO COME DOWN. STAYED AT 1. 30 W/ N1 & N2 AT IDLE SPEEDS. EPR PROBLEM SUSPECTED. SWAPPED EPR GAUGES, NO HELP. REMOVED AND REPLACED EPR TRANSMITTE R PER 77-11-02. ALL PARAMETERS W/IN RANGE PER 71-00-00 TEST 9. 2 L 7 4 4F A20WE 2002011800080 20020118 00080 NM 2002 1 18 P5CA0200629 1 20020111 A 3241 WIRE BOEING 747 747249F 1384849 NM NR 11 BRAKE BROKEN A P5CA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 23 806FT 21827 RT BODY GEAR LEFT REAR (NR 11) ANTI-SKID LIGHT CAME ON AND WOULD NOT RESET. WHEEL ASSY RETORQUED FOR PRECAUTION PER MM 32-45-01. NR 11 BRAKE DEACTIVATED PER MEL. REPAIRED BROKEN WIRES AT TRANSDUCER ELECT CONNECTION PER MM STANDARD PRACTI CES. REACTIVATED NR 11 BRAKE. NORMAL OPERATIONS RESTORED. 2 L 7 4 4F A20WE 2002011800087 20020118 00087 SW 2002 1 18 PNSA020101 1 20020107 A 2910 HYDRAULIC LINE SWRNGN SA227 SA227AC 8780603 SW HYDRAULIC SYS LEAKING A PNSA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 640PA AC759B DURING CRUISE BOTH HYDRAULIC PRESSURE WARNING LIGHTS CAME ON. PRESSURE GAUGE DROPPED TO 500 PSI AND SLOWLY DROPPED TO 1 00 PSI. CREW REVIEWED EMERGENCY PROCEDURES FOR NO FLAP AND EMERGENCY GEAR EXTENSION. DISPATCH WAS ADVISED TO NOTIFY MA INTENANCE AND ANC AIRPORT FIRE. NORMAL LANDING WAS MADE AND BRAKES OPERATED NORMAL AS THEY ARE OPERATED BY DIFFERENT SY STEM THAN MAIN. MAINTENANCE FOUND HYDRAULIC LINE UNDER COCKPIT FLOOR WITH A SMALL HOLE IN IT (PN 27-81032-075) LOCALLY FABRICATED LINE AND SERVICED HYDRAULIC SYSTEM. NOTE ALL FLUID WAS CONTAINED BY FLUID CONTAINMENT BAG AND VENTED OVERBOA RD. 2 L 7 2 4T RT A8SW 2002012300167 20020123 00167 NM 2002 1 23 F3LA200200005 1 20020108 A 5315 FLOORBEAM BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 528, RBL 10, CORRODED. REMOVED DAMAGED PORTION OF FLOORBEAM UPPE R CHORD PER SRM 51-30-2. FABRICATED AND INSTALLED REPLACEMENT UPPER CHORD PER SRM 53-10-9. 2 L 7 2 4F RT A16WE 2002012300168 20020123 00168 NM 2002 1 23 F3LA200200006 1 20020108 A 5210 TORQUE BOX BOEING 737 737228 13844AG NM L2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON TORQUE BOX AT UPPER AND LOWER MOUNT PADS AFT END OF L-2 DOOR. REPLAC ED TORQUE BOX ASSY PER OHM 52-16-03. 2 L 7 2 4F RT A16WE 2002011800118 20020118 00118 EU 2002 1 18 QXEA0200010 1 20020108 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 493US 11161 SEA- AFT OVERWING EXIT SIGN HAS SEVERAL BURNED OUT BULBS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002012300169 20020123 00169 NM 2002 1 23 F3LA200200007 1 20020108 A 5320 INTERCOSTAL BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL, STR 25R, AFT OF STA 500. REPLACED INTERCOSTAL PER SRM 5 1-10-02 AND BAC DRAWING 65-20726. 2 L 7 2 4F RT A16WE 2002011800119 20020118 00119 EU 2002 1 18 QXEA0200011 1 20020113 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 11169 PDX- FORWARD EMERGENCY EXIT LOCATING SIGN ABOVE COCKPIT DOOR HAS BURNED OUT LIGHT BULBS. REMOVED AND REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002011800120 20020118 00120 NM 2002 1 18 QXEA0200012 1 20020112 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 379PH 530 PSC- EMERGENCY FLOOR TRACK LIGHT ASSEMBLY NUMBER 4 IS INOPERATIVE. REPLACING NR 4 EMERGENCY FLOOR TRACK LIGHT ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002011800122 20020118 00122 EU 2002 1 18 RAIA00201003 1 20020106 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 551HK 41040 MX-STL- AFT SEGMENT OF EMERGENCY ESCAPE PATH LIGHTS INOP. RECONNECTED CONNECTOR AT SEAT 10A. PATH LIGHTS OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002012300170 20020123 00170 NM 2002 1 23 F3LA200200008 1 20020109 A 5210 TORQUE TUBE BOEING 737 737228 13844AG NM L2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED TORQUE TUBE CORRODED, L-2 DOOR TORQUE BOX. REPLACED TORQUE TUBE PER OHM 52-16-03. 2 L 7 2 4F RT A16WE 2002011800125 20020118 00125 WP 2002 1 18 ABXA010671 1 20020103 A 5310 9913440523 ANGLE DOUG DC9 DC941 302207N WP LT. WHEEL WELL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 LEFT WHEEL WELL ATTACH ANGLE CRACKED IN RADIUS, JUST OUTBOARD OF THE TRAP PANEL, ABOVE THE HYDRAULIC SERVICE ACCESS. REP LACED ANGLE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002011800126 20020118 00126 WP 2002 1 18 ABXA010673 1 20020103 A 5300 99234195 PANEL DOUG DC9 DC941 302207N WP LT. WHEEL WELL CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 LEFT SLANT PANEL CORRODED AROUND NUTPLATES. REPLACED SLANT PANEL IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 2002011800127 20020118 00127 WP 2002 1 18 ABXA010674 1 20020104 A 5310 992341931 PANEL DOUG DC9 DC941 302207N WP RT. WHEEL WELL CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 RIGHT SLANT PANEL HAD CORROSION AROUND NUT PLATES, LOWER EDGE FROM INBOARD TO OUTBOARD. REPLACED SLANT PANEL IAW DC-9 SR M 51-30-2, 51-10-4, 51-30-1 AND 51-20-6. 2 L 7 2 4F A6WE 2002011800129 20020118 00129 WP 2002 1 18 DHL2002805001 1 20020104 A 5712 RIB DOUG DC8 DC873F 302199F WP XFS329.00 CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 46125 LT. WING CENTER LEADING EDGE UPPER SKIN RIB TRAILING EDGE CRARACKED @ XFS 329.000 2 L 7 4 4F RT 4A25 2002011800130 20020118 00130 WP 2002 1 18 DHL2002805002 1 20020104 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 46125 LT. WING CENTER LEADING EDGE UPPER SKIN RIB TRAILING EDGE CRACKED 2" BETWEEN STA. XFS416 AND XFS435.789 2 L 7 4 4F RT 4A25 2002011800131 20020118 00131 EA 2002 1 18 COMA0260054 1 20020116 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS DE DESCENT 1 SO 01 927CA 14323 7031 FLIGHT 5952 LANDING GEAR DISAGREE MESSAGE - MLG DID NOT EXTEND.REPLACED THE #3 HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A21EA 2002011800132 20020118 00132 EA 2002 1 18 COMA0260055 1 20020117 A 5551 600230681 BUSHING CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MISALIGNED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 978CA 11469 7158 R/H AND L/H I/B HORIZONTAL STABILIZER BUSHINGS WERE FOUND TO BE MIGRATING.REMOVED AND REPLACED THE R/H AND L/H I/B STABI LIZER BUSHINGS P/N 600-23068 I/A/W CRJ AMM 20-26-00-910-803 AND DWG #600-23068. 2 L 7 2 4F RT A21EA 2002011800133 20020118 00133 WP 2002 1 18 DHL2002805003 1 20020104 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION HO HOVERING 1 SO 01 805DH 75397 46125 N/R # 2300 LT. WING CTR. L/E LOWER SKIN RIB T/E 1" CRACK BTWN XFS 291.500-310.250 2 L 7 4 4F RT 4A25 2002012300171 20020123 00171 NM 2002 1 23 F3LA200200014 1 20020110 A 5320 INTERCOSTAL BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 767-787, STR 25-R, CORRODED. INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-30-5. 2 L 7 2 4F RT A16WE 2002011800134 20020118 00134 EA 2002 1 18 COMA0260056 1 20020118 A 5346 601R5361345 BEAM CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP BAY CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 978CA 11469 7158 ENGINE SUPPORT BEAM CRACKED, TOP, CENTER.PERFORMED TEMPORARY REPAIR ON THE ENGINE SUPPORT BEAM BETWEEN LBL 21.0 AND RBL 21.0 AND BETWEEN WL 111.05 AND WL 119.12 WITH REPAIR KIT P/N 601R53-61-345KI I/A/W CANADAIR REO 601R-53-61-345 REV B REF LOG PAGE #493696 AND COMAIR W/O #29894. 2 L 7 2 4F RT A21EA 2002012300173 20020123 00173 NM 2002 1 23 F3LA200200016 1 20020110 A 5320 SUPPORT BRACKET BOEING 737 737228 13844AG NM FUSELAGE GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED C-2 THRESHOLD SUPPORT BRACKET AT STA 827 GOUGED. FABRICATED REPLACEMENT SUPPORT B RACKET AND INSTALLED PER SRM 20-41-02. 2 L 7 2 4F RT A16WE 2002012300174 20020123 00174 NM 2002 1 23 F3LA200200017 1 20020110 A 5320 SUPPORT BRACKET BOEING 737 737228 13844AG NM FUSELAGE GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED C-2 THRESHOLD SUPPORT BRACKET AT STA 807 GOUGED. FABRICATED REPLACEMENT SUPPORT B RACKET AND INSTALLED PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 2002012300175 20020123 00175 NM 2002 1 23 F3LA200200018 1 20020110 A 5315 FLOORBEAM BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM IN CARGO COMPARTMENT CORRODED AT RBL 8 AND PANEL SPLICE AT STA 770 OUT O F LIMITS. FABRICATED REPAIR ANGLES AND INSTALLED PER SRM 53-10-5. 2 L 7 2 4F RT A16WE 2002012300176 20020123 00176 NM 2002 1 23 F3LA200200019 1 20020110 A 5315 FLOORBEAM BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON CARGO COMPARTMENT FLOORBEAM, LBL 2.5, STA 770. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 53-10-5. 2 L 7 2 4F RT A16WE 2002012300177 20020123 00177 NM 2002 1 23 F3LA200200020 1 20020110 A 5320 STRAP BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED LOWER FRAME FLANGE STRAP AT STA 794 CORRODED. REPLACED LOWER FRAME FLANGE STRAP P ER SRM 51-10-2 AND 51-30-2. 2 L 7 2 4F RT A16WE 2002011800145 20020118 00145 WP 2002 1 18 DHL2002805004 1 20020104 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R2301LT. WING CTR. L/E UPPER SKIN RIB T/E CRACKED 1" BTWN. 291.500 AND 250 2 L 7 4 4F RT 4A25 2002012300178 20020123 00178 NM 2002 1 23 F3LA200200021 1 20020113 A 5313 STRINGER BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON STR 18-L AT STA 380. REMOVED CORROSION, FABRICATED STRINGER SPLICE A ND DOUBLER, AND PERFORMED REPAIR PER SRM 51-10-1, 51-20-1, 51-30-2, 53-10-1, 53-10-3 AND 53-30-3. 2 L 7 2 4F RT A16WE 2002011800160 20020118 00160 SO 2002 1 18 LR7A02004 1 20020118 A 5312 ANGLE LKHEED 382 382G 526414U SO FS 165 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 552 4698 DURING SCHEDULED B1 INSPECTION PER JOB CARD HB3200 FOUND NLG FS 165 FORWARD PRESSURE DIAPHRAGM ATTACH ANGLE CRACKED AT L BL 18, WL 170.REPAIRED IAW SRM SMP 583 53-30-15. NR 0004. 2 H 7 4 4T A1SO 2002011800161 20020118 00161 SO 2002 1 18 LR7A02005 1 20020118 A 5343 3605879 FITTING LKHEED 382 382G 526414U SO FS 165 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 552 4698 DURING SCHEDULED B1 INSPECTION NR 0004 ACCOMPLISHMENT FOUND FS 165 NLG TRUNNION FITTING CORRODED AT LBL 18, WL 170.REPLA CED FITTING IAW DWG 360587. NR 0144. 2 H 7 4 4T A1SO 2002012300179 20020123 00179 NM 2002 1 23 F3LA200200022 1 20020118 A 5311 FRAME BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED FLOOR FRAME AT STA 480, STR 27-L, IN FWD CARGO COMPARTMENT CORRODED. FABRICATED R EPLACEMENT FLOOR FRAME AND INSTALLED REPAIR PER SRM 53-10-4. 2 L 7 2 4F RT A16WE 2002012300180 20020123 00180 NM 2002 1 23 F3LA200200023 1 20020119 A 5310 DOOR FRAME BOEING 737 737228 13844AG NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED CRACK IN FWD GALLEY DOOR FRAME, UPPER FWD SIDE, STA 294.5. REPLACED FWD GALLEY DO OR FRAME SEGMENT ABOVE DOOR STOP AT STA 294.5 PER SRM 51-10-1 AND EA 53-737-151. 2 L 7 2 4F RT A16WE 2002012100001 20020121 00001 WP 2002 1 21 DHL2002805005 1 20020104 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 2297LT. WING CTR. LEADING EDGE LOWER SKIN RIB T/E CRACKED 1" BTW. XFS404.000 & XFS422.750 2 L 7 4 4F RT 4A25 2002012100002 20020121 00002 WP 2002 1 21 ARWA20020113 1 20020120 A 7933 56B3D SENSOR DOUG DC8 DC863F 302198F WP A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 661AV 45969 LOG PAGE 107160. DISCREPANCY: #4 ENGINE OIL TEMP @ 150 @ 15 MINUTES ENGINE SHUT DOWN AS PER AOM. AIRCRAFT RETURNED TO KM IA AND LANDED OVERWEIGHT UNEVENTFUL. CORRECTIVE ACTION: TROUBLESHOOTING INDICATED OPENED RESISTANCE AT TEMP BULB. REMOVE D AND REPLACED #4 ENGINE OIL TEMPERATURE BULB IAW MM 79-34-1. PERFORMED OPERATIONAL CHECK IAW MM 71-00 AND FOUND NORMAL. PERFORMED OVERWEIGHT LANDING CHECK IAW J/C 6372 "A" INSPECTION NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002012100003 20020121 00003 NM 2002 1 21 HNAA0200004 1 20020116 A 7922 45E041 VALVE DHAV DHC8 DHC8102 2809003 NM MALFUNCTIONED A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 924HA 29007 29007 105 Oil temp on number 1 engine clombed to 110 degrees on climb-out, temp stayed in yellow ark for less than 10 minutes. Re moved and replaced oil temp regulator valve. 2 H 7 2 4T RT A13NM 2002012100004 20020121 00004 NM 2002 1 21 UPS02537424 1 20020112 A 5310 SEAT TRACK BOEING 757 75724APF 1384969 NM BS1192RBL25WL208 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 407UP 23729 INSPECTION TYPE:C CORROSION AROUND NUT-PLATE HOLE ON-OB FLANGE OF SEAT TRACK BS1192- RBL25-WL208. REMOVED & REPLACED DAMAGED SEAT TRACK BS 1180-1230 RBL 25 WL 208 PER SRM 51-40-02 AND E.O. 02-0078. 2 L 7 2 4F RT A2NM 2002012100005 20020121 00005 NM 2002 1 21 UPS02537425 1 20020112 A 5310 SEAT TRACK BOEING 757 75724APF 1384969 NM 1182 1198 45 208 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 407UP 23729 INSPECTION TYPE:C CORROSION AROUND NUTPLATE HOLES ON O/B FLANGE OF SEAT TRACK LBL 45 BS 1182 - 1198 WL 208 REMOVED A ND REPLACED DAMAGED SEAT TRACK FROM BS 1180 - 1230 LBL 45 W L 208 PER SRM 53-00-52 FIG 202 AND UPS EO 02-0078 2 L 7 2 4F RT A2NM 2002012100006 20020121 00006 NM 2002 1 21 ZW0A0200905 1 20020120 A 3242 26130422 BRAKE BOEING 717 717200 1383700 NM A ZW0A O OTHER K FLUID LOSS AP APPROACH 1 CE 13 422TW 55089 A HYDRAULIC FLUID LOSS WAS REPORTED FROM THE RH SYSTEM. CREW MANUALLY EXTENDED THE LANDING GEAR. REPLACED THE NUMBER 1 B RAKE DUE TO A BROKEN INLET FITTING. NO CHECK-C. --CLOSED-- 2 L 7 2 4F TR A6WE 2002012100007 20020121 00007 EA 2002 1 21 SWIA200210560 1 20020115 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA LEFT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 907SW 7511 ON APPROACH FLAPS FAILED WHEN FLAPS SELECTED 8 DEGREES. FLAPS FAILED AT 0 DEGREES. RAN QRH. REPLACED LEFT BPSU AND PE RFORMED RIGGING PER CRJ MM 27-51-10 AND CYCLED FLAPS SEVERAL TIMES. OPS CHECK GOOD. S/N OFF: 1241B 2 L 7 2 4F RT A21EA 2002012200046 20020122 00046 NM 2002 1 22 HNAA0200008 1 20020121 A 2910 DSC252B40124 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM NOSE BAY LEAKING A HNAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 07 907HA 011 After take off the number 2 hydraulic isolation caution light illuminated and roll spoiler outbe caution light illuminaa ted. Upon gear retraction, the gear would not retract. Replaced hydraulic lind to nose gear drag strut actuator and se rviced #2 system. Evaluation flight good. 2 H 7 2 4T RT A13NM 2002012200047 20020122 00047 NM 2002 1 22 SABA0007 1 20020120 A 7710 SEDL0C2P GAUGE DHAV DHC8 DHC8102 2809003 NM SURGES A SABA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 33 813SN 032 Flight 5015 from CLT to GSP: After takeoff number two engine torque started to surg 5% after levers were set at 900 RPM. Aircraft returned to Charlotte and landed with no other problems. No emergency was declared. Maintenance removrd and re placed the number two Torque indicator. System ground run and ops checked good. Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002012300181 20020123 00181 NM 2002 1 23 F3LA200200024 1 20020118 A 2910 6546858236 HYDRAULIC LINE BOEING 737 737228 13844AG NM NR 2 ENGINE LEAKING A F3LA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 03 234TR 40 23004 EN ROUTE FROM PHX TO DEN, FLIGHT CREW REPORTED A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO, WITH SUBSEQUENT SYSTEM FAILU RE. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE HYDRAULIC PRESSURE LINE FOUND TO BE LEAKING AND PERFORMED LEAK CHECK. NO LEAKS NOTED. 2 L 7 2 4F RT A16WE 2002012200048 20020122 00048 EA 2002 1 22 SWIA200210566 1 20020117 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA LEFT SIDE COCKPI A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 597SW 7293 LEFT WINDOW HEAT CAUTION MESSAGE ON CONTINUOUSLY AFTER TAKEOFF. RETURNED TO SLC.REMOVED AND REPLACED THE LEFT SIDE WIND OW IAW AMM 56-12-01. LEAK AND OPS GOOD. P/N: NP-139322-5 S/N OFF: 98294H1164. 2 L 7 2 4F RT A21EA 2002012200049 20020122 00049 NM 2002 1 22 SABA020007 1 20020120 A 7710 SEDL0C2P GAUGE DHAV DHC8 DHC8102 2809003 NM OUT OF TOLERANCE A SABA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 33 813SN 032 Flight 5015 from CLT to GSP: After takeoff number two engine torque started to surge 5% after levers were set at 900 RPM . Aircraft returned to Charlotte and landed with no other problems. No emergency was declared. Maintenance removed and r eplaced the number two torque gauge. System ground run and ops checked good. Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002012200055 20020122 00055 WP 2002 1 22 AT0200001 1 20020119 A 3350 081691 SOCKET DOUG DC9 DC932 3022066 WP ROW 25 MISSING A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 828AT 47274 FOUND ROW 25 EMERGENCY PATH LIGHT ASSEMBLY MISSING. CORRECTIVE ACTION: REPLACED SOCKET. IAW DC9 MM33-53 2 L 7 2 4F A6WE 2002012200057 20020122 00057 NM 2002 1 22 CALA0200027 1 20020119 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 178 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND FUSELAGE SKIN DAMAGED AT STA 178, RBL 5. REPAIRED SKIN IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2002012200058 20020122 00058 NM 2002 1 22 CALA0200028 1 20020121 A 5230 SKIN BOEING 737 7373T0 1384582 NM FWD CARGO DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND A 3/4" CRACK AT LIGHTENING HOLE CUTOUT OF FORWARD CARGO DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW EC RA 5232-01014. 2 L 7 2 4F RT A16WE 2002020600045 20020206 00045 NM 2002 2 6 2002UALA00024 1 20020104 A 5330 141W330911 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 796UA 17685 26931 EXTERNAL SKIN DENTED BETWEEN STA 292 TO 298 AT STRINGER 29L. MAJOR REPAIR ACCOMPLISHED. DENT REMOVED AND DOUBLER INSTA LLED. DENT WAS CUT OUT AND REPAIRED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002012200059 20020122 00059 NM 2002 1 22 2002UALA00026 1 20020105 A 5310 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 DAMAGE TO FRAME BUILD UP AT STATION 740 BETWEEN STRINGER 13R-14R, EXCESS MATERIAL REMOVED ON CLEAN UP TO SHEAR TIE PART. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW SHEAR TIE AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002012200060 20020122 00060 NM 2002 1 22 2002UALA00029 1 20020104 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 BODY STATION 1197-1188 RBL 40-44 RBL 20-25 LBL 6-9 LBL 40-44 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012200061 20020122 00061 NM 2002 1 22 2002UALA00030 1 20020104 A 5313 FASTENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 BODY STATION 1335-1345 STRINGER 20R STRINGER FASTENERS AND WEB CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INS TALLED FASTENERS AND WEB. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012200062 20020122 00062 NM 2002 1 22 2002UALA00031 1 20020104 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 BODY STATION 284 RBL 70 FLOOR EDGE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW EDGE BEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012200063 20020122 00063 NM 2002 1 22 C1HA200292002 1 20020121 A 7800 69537131 SWITCH BOEING 727 727212 138407G NM A C1HA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 292AS 21458 #1 ENGINE THRUST REVERSER OPERATING ANNUNCIATOR CAME ON IN CRUISE AND REMAINED ON FOR DURATION OF FLIGHT. ACTION TAKEN: REMOVED AND REPLACED #1 ENGINE THRUST REVERSER SWITCH SYSTEM CHECKS GOOD ON THE GROUND IAW MM 78-30-00. 2 L 7 3 4F A3WE 2002012200064 20020122 00064 NM 2002 1 22 2002UALA00032 1 20020104 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 BODY STATION 1197 + 66 LBL 25-44 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012200065 20020122 00065 NM 2002 1 22 2002UALA00033 1 20020104 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 BODY STATION 1219 LBL 20-44 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012200066 20020122 00066 NM 2002 1 22 2002UALA00035 1 20020104 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 BODY STATION 1153 RBL 20-25 LBL 2-35 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012200067 20020122 00067 NM 2002 1 22 2002UALA00037 1 20020107 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 CABIN BODY STUB FRAME OUTER FLANGE IS CRACKED AT BODY STATION 296 STRINGER 8R. MAJOR REPAIR ACCOMPLISHED. REPLACED FRA ME STUB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012200068 20020122 00068 NM 2002 1 22 2002UALA00038 1 20020107 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 STATION 312-360, WL 208, LBL 56 INBOARD CHORD ON CREASE BEAM HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. CHORD REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020600046 20020206 00046 NM 2002 2 6 2002UALA00039 1 20020102 A 2781 284T084314 TARGET BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE L/E SLAT MISSING A UALA O OTHER D N INFLIGHT SEPARATION FALSE WARNING UK UNKNOWN 1 WP 29 669UA 30025 NR 4 LEADING EDGE SLAT OUTBOARD AUX TRACK MISSING BOLT, ROLLER, AND SENSE TARGET AFTER LANDING. UNKNOWN, MISSING PARTS WERE DISCOVERED BY EICAS L/E SLAT DISAGREE MESSAGE DUE TO MISSING L/E SLAT POSITION SENSOR TARGET. REPLACED MISSING PAR TS PER APPLICABLE MAINTENANCE PROCEDURES. SENSOR SYSTEM WAS OPS CHECKED PER APPLICABLE MAINTENANCE MANUAL AND ALL OPS C HECKS WERE NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012400024 20020124 00024 NM 2002 1 24 2002UALA00040 1 20020107 A 2121 6454051 FAN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN FAULTY A UALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 29 930UA 3814 26655 LANDED UNDER ALERT DUE TO ELECTRICAL SMELL IN CABIN. SUSPECTED RECIRCULATION FAN FAILURE. INSPECTED ALL CEILING/PSU/SIDE WALL LIGHTING, COFFEE MAKERS AND BOTH AIR CYCLE MACHINE OIL LEVELS, YET NO DISCREPANCIES ISOLATED. REPLACED RECIRCULATIO N FAN AS PRECAUTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012200069 20020122 00069 NM 2002 1 22 2002UALA00043 1 20020108 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 AFT CARGO PIT STRINGER 25L BS 727 TO BS 747 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED 20 INCH SECTION OF STRING ER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012200070 20020122 00070 NM 2002 1 22 2002UALA00044 1 20020108 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 LEFT HAND FUSELAGE DENT AT STA 380 TO STA 391 BETWEEN STR 14L AND STR 15L. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOU BLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020600048 20020206 00048 NM 2002 2 6 2002UALA00049 1 20020108 A 5311 141W31691 FRAME BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 796UA 17685 26931 STA 298.5 LT FRAME OUTER CHORD AT STRINGER 28-30 WAS REPAIRED PER EVA G95-7785A. INTERIM MAJOR REPAIR ACCOMPLISHED. DA MAGE WAS CUT OUT AND REPAIRED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002012200074 20020122 00074 NM 2002 1 22 2002UALA00051 1 20020108 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 LEFT HAND FUSELAGE STATION 1478 STRINGER 25L IS CREASED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002012200076 20020122 00076 NM 2002 1 22 2002UALA00052 1 20020108 A 5310 SHEAR TIE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 796UA 26931 STA 298.5 LT SHEAR TIE CRACKED AT STRINGER 28-29. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002012300046 20020123 00046 NM 2002 1 23 2002UALA00053 1 20020108 A 2820 343N330136 FUEL LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT MAIN TANK CHAFED A UALA K NONE K FLUID LOSS CR CRUISE 1 WP 29 543UA 25698 UNWANTED FUEL TRANSFER FROM RIGHT FUEL TANK TO CENTER TANK. FOUND CHAFED WATER SCAVENGE FUEL LINE. DAMAGE CAUSED FROM COUPLING CONTACT ON ADJACENT FUEL LINE DUE TO INCORRECT CLAMPING. REPLACED WATER SCAVENGE FUEL LINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002012200079 20020122 00079 NM 2002 1 22 2002UALA00054 1 20020108 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 EXTERNAL FUSE IS DENTED APPROX AFT OF DOOR 4R 12 INCHES AND ABOVE EMERGENCY LIGHT. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020600049 20020206 00049 NM 2002 2 6 2002UALA00062 1 20020110 A 2740 285T0015 MODULE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE E/E BAY FAULTY A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION UK UNKNOWN 1 WP 29 601UA 21862 CREW REPORTED EICAS MSG FOR RUDDER RATIO, AILERON LOCKOUT, AND AUTOPILOT PROBLEMS. RETURNED TO SFO. AILERON LOCKOUT ME SSAGE WAS GENERATED BY FAULTED STAB TRIM AILERON LOCKOUT MODULE (SAM). NOTE, SAM ALSO PROVIDES AIR DATA TO RUDDER RATIO CHANGER MODULE. REPLACED SAM PER APPLICABLE MAINTENANCE MANUAL. OPS CHECKED AILERON LOCKOUT SYSTEM, RUDDER RATIO CHAN GER, AND AUTO PILOT SYSTEM PER APPLICABLE MAINTENANCE MANUALS. ALL OPS CHECKS WERE NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 2002012200082 20020122 00082 NM 2002 1 22 2002UALA00065 1 20020109 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 925UA 26646 RIGHT HAND STATION 188 FRAME CHORD CRACKED AT WL 207. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED FRAME DOUB LER AND SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012200083 20020122 00083 NM 2002 1 22 2002UALA00066 1 20020110 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CABIN UPPER LOBE FRAME CRACKED AT BODY STATION 827, STRINGER 9. MAJOR REPAIR ACCOMPLISHED. INSTALLED CHANNEL AND FILLE R REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012200085 20020122 00085 NM 2002 1 22 2002UALA00068 1 20020109 A 5320 BEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 BODY STATION 805-806 RBL 54 TRANSVERSE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIRS AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012200086 20020122 00086 NM 2002 1 22 2002UALA00069 1 20020109 A 5320 BEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 BODY STATION 805-806 RBL 54 TRANSVERSE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIRS AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012200088 20020122 00088 NM 2002 1 22 2002UALA00070 1 20020109 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 BODY STATION 1197 + 132 LBL 40-44 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012200089 20020122 00089 NM 2002 1 22 2002UALA00073 1 20020110 A 5320 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 CABIN FLOOR STATION 1680 SHEAR DECK RIGHT HAND DOUBLER HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002012200090 20020122 00090 NM 2002 1 22 2002UALA00074 1 20020110 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT CABIN FLOORBEAM AT STATION 1681.1 UPPER CAP LOWER SURFACE HAS EXCESSIVE MATERIAL REMOVED FROM LBL 11 TO LBL 13. MAJ OR REPAIR ACCOMPLISHED. DAMAGED AREA TRIMMED OUT AND ANGLE DOUBLER AND TRIPLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002012200092 20020122 00092 2002 1 22 SWAA020122 4 20020118 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 638SW 27711 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2002012200093 20020122 00093 NM 2002 1 22 SWAA020124 1 20020117 A 3350 07912 COVER BOEING 737 7372T4 1384492 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED C2 CHECK, FOUND EEPLS AFT END CAP MISSING AND COVER MISSING AT ROW 14. INSTALLED COVER AND END CAP PER MM. 2 L 7 2 4F A16WE 2002012200094 20020122 00094 NM 2002 1 22 SWAA020126 1 20020118 A 3350 101073 LENS BOEING 737 7373Q8 1384670 NM CABIN DOORS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED C2 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENSES PER MM. 2 L 7 2 4F RT A16WE 2002012200095 20020122 00095 NM 2002 1 22 SWAA020129 1 20020118 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 33. REPAIRED WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2002012200096 20020122 00096 NM 2002 1 22 SWAA020130 1 20020118 A 5330 6545765 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, ABOVE STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002012200097 20020122 00097 NM 2002 1 22 SWAA020131 1 20020118 A 5320 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 602SW 27953 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, WL 177 AND LBL 5.7. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002012200098 20020122 00098 NM 2002 1 22 SWAA020132 1 20020118 A 5523 65C26384 TAB BOEING 737 7373H4 1384600 NM ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 602SW 27953 DURING SCHEDULED SPECIAL VISIT, FOUND LT ELEVATOR TAB DELAMINATED ON TOP T/E. REMOVED AND REPLACED ELEVATOR TAB PER MM . 2 L 7 2 4F RT A16WE 2002012200099 20020122 00099 NM 2002 1 22 SWAA020133 1 20020119 A 5312 6516300 BULKHEAD BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 345SA 23786 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED 1.25 INCHES LONG AT BS 178, WL 201 AND RBL 5.0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002012200100 20020122 00100 NM 2002 1 22 SWAA020109 1 20020115 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 507SW 24184 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 21. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002012200101 20020122 00101 NM 2002 1 22 SWAA020112 1 20020116 A 5751 6546454 AILERON BOEING 737 7372H4 138448C NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING WALK AROUND INSPECTION, FOUND LT AILERON DELAMINATED (4 INCH SPOT) ON LOWER SIDE JUST FWD OF OTBD TRIM TAB HINGE. REMOVED AND REPLACED LT AILERON AND TAB PER MM. 2 L 7 2 4F A16WE 2002012200102 20020122 00102 NM 2002 1 22 SWAA020114 1 20020117 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 602SW 27953 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, LBL 5.0, WL 201 AND WL 199. REPAIRED WEB P ER SRM. 2 L 7 2 4F RT A16WE 2002012200103 20020122 00103 NM 2002 1 22 SWAA020115 1 20020116 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 602SW 27953 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED .50 INCH LONG AT BS 178, RBL 17.1 AND WL 227. REMOVED A ND REPLACED VERTICAL BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2002012200104 20020122 00104 NM 2002 1 22 SWAA020118 1 20020117 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/2 D CHECK, FOUND LT OUTBD T/E AFT FLAP DELAMINATED AT AFT EDGE CENTER. REMOVED AND REPLACED AFT T/E OTBD FLAP PER MM. 2 L 7 2 4F RT A16WE 2002012200105 20020122 00105 NM 2002 1 22 SWAA020119 1 20020117 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED RON, FOUND EEPLS WIRING EXPOSED AT ROW NR 11. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002012200106 20020122 00106 NM 2002 1 22 2002UALA00075 1 20020110 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 STATION 1681 FLOORBEAM UPPER CAP FORWARD FLANGE HAD CORROSION AND EXCESSIVE MAT LOSS AT RBL 30 THROUGH RBL 33 RBL 39 THR OUGH RBL 41 AND RBL 47. MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVED, INSTALLED REPAIR ANGLES. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020100025 20020201 00025 NE 2002 2 1 2002UALA00076 2 20020106 A 7321 7911004094 EEC BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT ENGINE FAILED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 664UA 29236 724189 ON FERRY FLIGHT ON 1/6/02 AND ON ETOPS VERIFICATION FLIGHT ON 1/5/02 RETURNED TO FIELD DUE TO RIGHT ENGINE CONTROL EICAS MSG: EEC CHANEL B LOST POWER FAULT. SUPPLEMENTAL DATA UPDATE: EEC POWER SUPPLY FAULT. REPLACED PERMANENT MAGNET ALTE RNATOR AND ELECTRONIC ENGINE CONTROL (EEC) EEC WILL BE SENT TO HAMILTON SUNDSTRAND FOR OVERHAUL. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012200108 20020122 00108 SO 2002 1 22 RAIA00201010 1 20020108 A 7830 WARNING SYSTEM EMB 145 EMB145ER 3260211 SO COCKPIT MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 808HK 145157 5269-PIT- ON TAKEOFF ROLL, ENGINE NR 1 THRUST REVERSER DISAGREE MESSAGE. MAINTENANCE OPS CHECK NR 1 ENGINE TR WITH NO D EFECTS NOTED. 2 L 7 2 4F RT T00011AT 2002012200109 20020122 00109 EU 2002 1 22 RAIA00201012 1 20020109 A 5270 WARNING SYSTEM JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 555HK 41072 5564-MEM-EMERGENCY EXIT DOOR WARNING ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED ALL EMERGENCY EXIT DOORS FOR SECURITY , FOUND ALL DOORS FUNCTION PROPERLY. 2 L 7 2 4T RT A41NM 2002012200110 20020122 00110 GL 2002 1 22 RAIA00201013 1 20020109 A 3350 LIGHT MEYERS MAC145 MAC145 5650104 GL CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 551 216 MX-STL- ESCAPE PATH LIGHTING NOT FULLY FUNCTIONAL. RECONNECTED ESCAPE PATH LIGHTING STRIP, OPS CHECK OK. 1 L 7 1 3O 3A1 2002012200111 20020122 00111 NE 2002 1 22 RAIA00201014 2 20020112 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LEFT FLUCTUATES A RAIA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 CE 03 566HK 41084 76019R 5509-EVV- ON APPROACH INTO STL, LEFT ENGINE RPM FLUX - SHUT DOWN ENGINE AS PRECAUTION. MAINTENANCE PERFORMED ENGINE OPE RATIONAL CHECKS. INSTALLED HAND HELD TESTER NO FAULTS INDICATED. ENGINE OPS CHECK GOOD AT ALL POWER SETTINGS DURING ON E HOUR OF GROUND OPERATION. 2 L 7 2 4T 4 T RT A41NM E18NE 2002012200112 20020122 00112 EU 2002 1 22 RAIA00201015 1 20020112 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ILLUMINATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 558HK 41071 5517-GRR- BAGGAGE DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. MAINTENANCE DEFERRED DISCREPANCY PER TSA J41 MEL 52-3. 2 L 7 2 4T RT A41NM 2002012200116 20020122 00116 EU 2002 1 22 SABA020002 1 20020110 A 3222 STRUT BAG JETSTM JETSTM3201 1500217 EU NLG LOW A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 963AE 963 FLIGHT 5200 FROM RDU TO CHS, AFTER TAKEOFF PILOT SELECTED LANDING GEAR UP. NOSE GEAR SHOWED AN UNSAFE CONDITION. GEAR WAS CYCLED DOWN AND INDICATED DOWN AND LOCKED. AIRCRAFT WAS DIVERTED TO CLT. NO EMERGENCY WAS DECLARED. AIRCRAFT LAND ED IN CLT WITH NO OTHER PROBLEMS. MAINTENANCE SERVICED THE NOSE GEAR STRUT. RETRACTION CHECK WAS COMPLIED WITH. SYSTE M OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2002012200117 20020122 00117 NE 2002 1 22 SABA020003 3 20020112 A 6140 702537 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE AUTOFEATHER SYS FAILED A SABA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 33 883CC 162 FLIGHT 5025 FROM CLT TO TLH; PILOT ABORTED TAKEOFF FOR NOT GETTING AN AUTO FEATHER LIGHT DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE IN CLT. MAINTENANCE REMOVED AND REPLACED THE GRIMES CONTROL LIGHT BOX. SYSTEM OPS CHECKED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P7NE 2002012200118 20020122 00118 NM 2002 1 22 SWAA020069 1 20020110 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 EEPLS LOOSE AT ROW NR 8. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002012200119 20020122 00119 2002 1 22 SWAA020073 4 20020112 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002012200120 20020122 00120 NM 2002 1 22 QXEA0200070 1 20020118 A 2611 PU90461R2 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 361PH 8823 516 PDX - LAVATORY SMOKE DETECTOR WENT OFF ON CLIMB-OUT. NO EVIDENCE OF SMOKE OR BURNING SMELL. REPLACED LAVATORY SMOKE DETE CTOR. PERFORMED OPERATIONAL TEST OF SMOKE DETECTOR AND OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002012200121 20020122 00121 NM 2002 1 22 2002UALA00041 1 20020115 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 MAIN CABIN FLOOR TRANSVERSE FLOORBEAM CORRODED. STA 784, LBL 33.06 MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR . 2 L 7 2 4F 4 F RT A1NM E24NE 2002012200122 20020122 00122 NM 2002 1 22 2002UALA00042 1 20020115 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 FWD CABIN BS 344, RBL 70R, FLOORBEAM T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012200123 20020122 00123 NM 2002 1 22 2002UALA00120 1 20020118 A 5315 SEAT TRACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 MID CABIN STATION 620 INBOARD RIGHT HAND SEAT TRACK HAS EXCESSIVE MATERIAL LOSS AT FLOOR BOARD HOLE RBL 23.5. MAJOR REP AIR ACCOMPLISHEDINSTALLED REPAIR ANGLE AND STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012200126 20020122 00126 EA 2002 1 22 SWIA200210523 1 20020108 A 3251 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING OUT OF RIG A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 903SW 7425 LOST NOSE WHEEL STEERING AND STEERING INOP CONDITION MESSAGE ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF AT APPROX IMATELY 60 KTS AND RETURNED TO GATE. PERFORMED RIGGING OF ECU AS PER MM 32-51-10. SYSTEM OPS CHECKS GOOD ON TAXI TEST. 2 L 7 2 4F RT A21EA 2002012200129 20020122 00129 SO 2002 1 22 SWIA200210525 1 20020104 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 207SW 120266 CRACK IN SKIN AROUND FWD CORNER OF RT SIDE COCKPIT SIDE WINDOW. DISCOVERED DURING ROUTINE LINE INSPECTION. INSTALLED REPAIR DOUBLER PER SB 120-053-0010. 2 L 7 2 4T RT A31SO 2002012200138 20020122 00138 NM 2002 1 22 SABA020009 1 20020119 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8103 1386005 NM CABIN DISCHARGED A SABA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 33 801WP 086 FLIGHT 5097 FROM CLT TO PGV: DURING PREFLIGHT, AIRCREW FOUND FLOOR EMERGENCY LIGHTS OUT. MAINTENANCE REMOVED AND REPLACE D WIRING HARNESS FOR TWO FORWARD LIGHTS AND REPLACED EMERGENCY BATTERY PACK. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002012200140 20020122 00140 NM 2002 1 22 0200085504 1 20020102 A 5311 CREASE BEAM BOEING 757 757251 1384970 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 504US 23193 During "H" check found corrosion on floor to fuselage crease beam at BS 1636 RBL 60. Repaired per EA 55-187743. 2 L 7 2 4F RT A2NM 2002012200141 20020122 00141 EA 2002 1 22 COMA0260057 1 20020118 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 984CA 10470 7171 FLIGHT 5450 FLAPS FAILED AT 28 DEGREES DURING LANDING ROLL.REPLACED THE L/H BPSU. 2 L 7 2 4F RT A21EA 2002012200142 20020122 00142 EA 2002 1 22 SWIA200210526 1 20020106 A 5270 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 412SW 7101 AFTER TAKEOFF PASSENGER DOOR LATCH CAUTION (AT 1,000 FT) APPEARED FOLLOWED BY PASSENGER DOOR LATCH WARNING AFTER 300 FT GAIN IN ALTITUDE. RETURNED TO THE FIELD. CLEANED AND INSPECTED GAPS ON PS5MB & PS6MB. GAPS CHECKED GOOD. CLEANED PAX DOOR WIRING HARNESS CANNON PLUGS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002012200143 20020122 00143 EA 2002 1 22 SWIA200210527 1 20020101 A 3411 PITOT LINE CNDAIR CL600 CL6002B19 1900309 EA PITOT/STATIC SYS CONTAMINATED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 412SW 7101 INFLIGHT, NR 2 ADC FAILED (IAS AMBER FLAG, EFIS COMP MON CAUTION, STALL FAIL). SWITCHED TO ADC 1 BOTH SIDES. NORMAL OP S TO LANDING IN YYC. PERFORMED CONTAMINATION REMOVAL (WATER) PURGING & FUNCTIONAL TEST OF CAPTAIN'S, F/O'S & STANDBY PI TOT STATIC SYSTEMS. CHECKS GOOD IAW MM 34-11-00. 2 L 7 2 4F RT A21EA 2002012200144 20020122 00144 EA 2002 1 22 SWIA200210528 1 20020104 A 2421 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 ENGINE FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 903SW 7425 IDG NR 2 CAUTION MESSAGE. TAKEOFF DISCONTINUED. REMOVED AND REPLACED RT IDG. NO LEAKS NOTED. OPS CHECKS GOOD. S/N O N 1248GEN3627, S/N OFF 0812GEN1261. 2 L 7 2 4F RT A21EA 2002012200145 20020122 00145 NE 2002 1 22 SWIA200210529 2 20020107 A 7397 WIRE HARNESS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE FAULTY A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 216SW 120285 RT NP GAUGE FLUCTUATES IN FLIGHT. REMOVED AND REPLACED RIGHT ENGINE EEC WIRING HARNESS. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002012200146 20020122 00146 SO 2002 1 22 SWIA200210530 1 20020107 A 2910 HYDRAULIC LINE EMB 120 EMB120ER 3260203 SO HYDRAULIC SYS LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 563SW 120338 LOST GREEN HYD SYSTEM. LEFT MAIN HYD PUMP LOW PRESS LIGHT ILLUMINATED. PER QRH, TURNED LEFT ELEC HYD PUMP ON. AFTER A FEW MINUTES, GREEN HYD QUANTITY DROPPED TO ZERO (EMPTY). EXTENDED GEAR MANUALLY AND MADE EMER LANDING. PRESSURE LINE TO HYDRAULIC RESERVOIR REPLACED. REPLACED LEFT ENGINE HYD DRIVEN PUMP. SERVICED HYDRAULIC FLUID. STEERING CHECK FLAPS , BRAKES, RUDDER CHECKS GOOD. LEAK CHECK GOOD. P/N ON 3-022-29, S/N ON MX-598526, S/N OFF MX-580-77. 2 L 7 2 4T RT A31SO 2002012200152 20020122 00152 EA 2002 1 22 SWIA200210531 1 20020109 A 2133 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 912SW 7595 DEPARTED LAX, PRESSURIZATION DID NOT WORK. FOLLOWED SOP. NO PRESSURIZATION IN ANY MODES OR CONTROLLERS. RETURNED TO L AX. INSTALLED SERVICEABLE SECONDARY OUTFLOW VALVE IAW 21-31-00. OPS CHECK FAILED. DEFERRED THE PRESSURIZATION SYSTEM. 1/9/02 UPDATE: FAT MAINTENANCE WAS UNABLE TO DUPLICATE THE SQUAWK. S/N ON 110-F0399, S/N OFF 81-F0526. 2 L 7 2 4F RT A21EA 2002012200153 20020122 00153 EA 2002 1 22 SWIA200210532 1 20020109 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 418SW 7446 SPOILERONS FAULT MESSAGE WILL NOT GO OUT AFTER FLIGHT CONTROL CHECK PER MEL OPS PROCEDURE. ALSO EXCESSIVE LEFT AILERON TRIM REQUIRED TO MAINTAIN LEVEL FLIGHT PREVIOUS LEG. RIGHT SPOILERON ARROW MOMENTARILY POINTS UP AFTER ENGINE STARTS WI TH CONTROL COLUMN NEUTRAL. REMOVED AND REPLACED RT SPOILERON I/B PCU IAW CRJ MM 27-62-01. OPS CHECK GOOD, LEAK CHECK G OOD. S/N OFF: 3795. 2 L 7 2 4F RT A21EA 2002012200154 20020122 00154 SO 2002 1 22 SWIA200210533 1 20020107 A 5260 SPRING EMB 120 EMB120RT 3260202 SO ENTRY STAIRS OUT OF POSITION A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 1110J 120110 ON DOOR OPENING 3RD AND 4TH STAIRS FROM THE TOP DID NOT EXTEND. REPOSITIONED BOTTOM STEP SPRING AND REPLACED STEP SPRIN G ON 3RD STEP DOWN FROM TOP. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002012200155 20020122 00155 2002 1 22 SWIA200210534 4 20020108 A 3425 COMPUTER EMB 120 EMB120ER 3260203 SO E/E BAY FAULTY A SWIA O OTHER I FLT. ATTITUDE INST. CR CRUISE 1 NM 07 567SW 120342 CAPTAIN SIDE FLIGHT DIRECTOR FLAGGED AND F/O'S FLT DIRECTOR PITCHES +/- 10 DEGREES. REMOVED AND REPLACED CAPTAIN'S AHAR S COMPUTER. S/N OFF: 422. 2 L 7 2 4T RT A31SO 2002012200156 20020122 00156 2002 1 22 SWIA200210535 4 20020112 A 2210 RELAY CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS FAILED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 407SW 7034 YD 2 WILL NOT ENGAGE. REPLACED 2K2CA RELAY (ARM). OPS CHECK GOOD YAW DAMPER SYSTEM. P/N: MS27400-31X. 2 L 7 2 4F RT A21EA 2002012200165 20020122 00165 EU 2002 1 22 02FDEA00052 1 20020112 A 2750 FLAP AIRBUS 300 A300F4605R 3930327 EU WING MALFUNCTIONED A FDEA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 25 676 790 ON LANDING APPROACH FLAPS STUCK AT LESS THAN 15 DEG SLATS NORMAL BOTH OVERHEAD EAD FLAP LIGHTS & FLAPS ON SFPI PANEL ON. 2 L 7 2 4F RT A35EU 2002012200166 20020122 00166 NM 2002 1 22 02FDEA00054 1 20020117 A 2780 FLAP BOEING 727 727233 138408A NM WING OUT OF ADJ A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 275 22040 ON CLIMB NR 5 L/E FLAP POS IND WITHIN SHOW RETRACTED (GREEN) WITH FLAPS 2 DEG SELECTED. ACFT HANDLED AS IF SLAT WAS FUL LY AND CORRECTLY RETRACTED. QRH DIRECT RECYCLING TO 5 DEG POS (EXTENDED) POS AND IND CORRECT THEN FLAPS 2 AND FLAPS UP. LIGHTS WERE OUT TILL PASSED THROUGH 250 KTS ON CLIMB. WENT THROUGH CHECKLIST AGAIN AND NR 5 W/N TO OUT. RETURNED TO AIRPORT. ADJUSTED NR 5 KRUEGER FLAP PER MM 27-82-001-4, OPS CK NORMAL OK FOR SERV. 2 L 7 3 4F RT A3WE 2002020500004 20020205 00004 NM 2002 2 5 02FDEA00055 1 20020118 A 5315 FLOORBEAM BOEING 727 727277 138408S NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245 22016 FLOORBEAM HAS MECHANICAL DAMAGE, AT STA 1090 RBL 67 WL 208. R&R FLOORBEAM PER SRM 53-10-8 & 53-10-1. 2 L 7 3 4F RT A3WE 2002012200168 20020122 00168 NM 2002 1 22 02FDEA00057 1 20020117 A 2781 POSITION SWITCH BOEING 727 7272D4 138407U NM L/E FLAP FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 287FE 21849 AFTER T/O AMBER LIGHT DID NOT EXTINGUISH ON RETRACTION TO FLAPS 2 DEG, S/O AUX PANEL SHOWED A RIGHT NR 5 L/E FLAP INTRAN SIT LIGHT. RECYCLED WITH SAME RESULT. REMOVED AND REPLACED NR 5 L/E FLAP POS SWITCH DUE TO FLT CREW WRITE UP. REF MM 27-82-001-4. 2 L 7 3 4F A3WE 2002012200169 20020122 00169 WP 2002 1 22 02FDEA00058 1 20020120 A 3620 PRESSURE SWITCH DOUG DC10 DC1030F 3023504 WP PNEUMATIC SYS FAILED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 319 47820 NR 3 MANIFOLD FAIL LIGHT ILLUMINATED ON CLIMBOUT SHORTLY AFTER SELECTION OF WING A/I ON. REMOVED AND REPLACED NR 3 MANI FOLD FAILURE DETECTION PRESSURE SWITCH PER MM 36-23-03-4, SYS OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 2002012200175 20020122 00175 2002 1 22 SWAA020074 4 20020112 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 763SW 27877 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002012200176 20020122 00176 NM 2002 1 22 SWAA020077 1 20020111 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 616, STR 1R AND 2R. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002012200181 20020122 00181 EU 2002 1 22 MALA020124 1 20020117 A 2810 621BT PANEL SAAB SF340 SF340A 7850100 EU LEAKING A MALA K NONE K FLUID LOSS NR NOT REPORTED 1 GL 15 27XJ 340A027 Fuel leak RH Wing coming from Top of Wing 2nd manhole cover from Fuselage. No Flight interruption. Maintenance removed , cleaned and reinstalled panel 621BT. All checks good IAW SF340 MM Chap. 28. 2 L 7 2 4T RT A52EU 2002012200191 20020122 00191 NM 2002 1 22 AWXA200200045 1 20020103 A 5330 654580020 SKIN BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - MAJOR REPAIR - "C" - DURING C-17 CHECK 1/4" CRACK WAS FOUND AT 12 OCLOCK POSITION AT HILOC FASTENER HOLE LOWER AFT CORNER OF L1 DOOR CUTOUT BS 340. MAINTENANCE REMOVED DAMAGED AREA OF SKIN AND PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED, FABRICATED DOUBLER AND STRAP AND INSTALLED REPAIRS IAW AWA ER 03-5311-02014-SS2. 2 L 7 2 4F RT A16WE 2002012200192 20020122 00192 NM 2002 1 22 AWXA200200046 1 20020102 A 5315 654680995 TEE CHORD BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - MAJOR REPAIR - "C" - DURING C-17 CHECK CORROSION WAS FOUND ON FLOOR BEAM UPPER FLANGE AT BS 947, LBL 10 TO RBL 10. MAINTENANCE REMOVED 6 EACH FLOOR SUPPORT, 1 EACH INTERCOASTAL BRACKET ASSEMBLY, AND TEE CHORD FROM LBL 32 TO RBL 33. FA BRICATED AND INSTALLED NEW TEE CHORD BS 947, LBL 32 TO RBL 33, REINSTALLED INTERCOASTAL BRACKET AND 6 EACH FLOOR SUPPORT S BS 947 TO BS 967, REPAIRS C/W IAW B737-300 SRM 53-00-51 PG 207-211, SRM 51-40-02 PG 6-7, 16-19, & 45. 2 L 7 2 4F RT A16WE 2002012200193 20020122 00193 NM 2002 1 22 AWXA200200047 1 20020121 A 2910 271N63111073 TUBE BOEING 757 7572S7 1384962 NM #1 ENG. CHAFED A AWXA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 WP 28 901AW 23321 LAS - EMERGENCY LANDING - FLT 085 - "C" - DURING CRUISE ENROUTE FROM JFK TO LAS AT FL 390 THE FLIGHT CREW RECEIVED EICAS MSG FOR L/H HYDRAULIC QUANTITY WITH A L/H RESERVIOR LIGHT ILLUMINATED, L/H HYDRAULIC QUANITY INDICATION WAS .48RF AND D ECREASING .08 EVERY 10 MINUTES. QUANTITY DECREASED TO .04 AND STATUS MESSAGE FOR POWER TRANSFER UNIT APPEARED FOLLOWED B Y L/H HYDRAULIC QUANITY INDICATION OF 0.00. AIRCRAFT CONTINUED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESH OT SYSTEM AND FOUND A PINHOLE SIZE LEAK COMING FROM A CHAFED AREA OF TUBING CAUSED BY A CLAMP ON THE CASE DRAIN LINE. MA INTENANCE PERFORMED A RYNGLOK REPAIR ON TUBING IAW BMM 20-10-09, PG 801, 810, 828-831. LEAK CHECK OF REPAIR WAS GOOD UND 2 L 7 2 4F RT A2NM 2002012200194 20020122 00194 NM 2002 1 22 AWXA200200048 1 20020108 A 5311 65465591 FRAME BOEING 737 737301 1384611 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - DURING INSPECTION OF AIRCRAFT CORROSION WAS FOUND ON FRAME BETWEEN STR 27R AND STR 26R AT BS 927. MAINTENANCE REMO VED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS IAW B737-300 SRM 53-00-07, FIG 101, DETAIL II. REMOVED LOWER FLANGE OF FRAME AND FABRICATED REPAIR PART, INSTALLED REPAIR IAW B737-300 SRM 53-00-07, PG 219-221. 2 L 7 2 4F RT A16WE 2002012200195 20020122 00195 NM 2002 1 22 AWXA200200049 1 20020108 A 5311 65465642 FRAME BOEING 737 737301 1384611 NM BENT A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - "C" - DURING INSPECTION MAINTENANCE FOUND A FRAME BENT AT BS 986 BETWEEN STR 25L AND 24L. MAINTENAN CE REMOVED DAMAGED SECTION OF FRAME AND FABRICATED -1 SHEAR TIE REPAIR AND INSTALLED IAW B737-300 SRM 53-00-07, PG 219-2 21. 2 L 7 2 4F RT A16WE 2002012200196 20020122 00196 NM 2002 1 22 AWXA200200050 1 20020108 A 5311 6551625505 DOUBLER BOEING 737 737301 1384611 NM SHORTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - "C" - DURING INSPECTION INTERNAL DOUBLER WAS FOUND TO HAVE SHORT EDGE DISTANCE AT FASTENER HOLES AT BS 967, STR 26L TO 26R. MAINTENANCE REMOVED INTERNAL DOUBLER AT BS 967, STR 26L TO 26R, FABRICATED NEW DOUBLER AND INST ALLED REPAIR IAW BAC DWG # 65-51625 AND B737-300 SRM 51-40-02, PG 3 & 38. 2 L 7 2 4F RT A16WE 2002012200197 20020122 00197 NM 2002 1 22 AWXA200200051 1 20020108 A 5313 6545776166 STRINGER BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - "C" - DURING INSPECTION A CRACK WAS FOUND ON STRINGER AT FASTENER HOLE BS 939 STR 26L. MAINTENANCE CUTOUT DAMAGED AREA OF STRINGER AND FABRICATED A REPAIR SECTION, 1 FILLER, 2 SHIMS, AND INSTALLED REPAIRS IAW B737-300 S RM 53-00-03, PG 201-207, AND SRM 51-20-01, PG 10 & 47. 2 L 7 2 4F RT A16WE 2002012200198 20020122 00198 NM 2002 1 22 AWXA200200053 1 20020108 A 5311 65465605 FRAME BOEING 737 737301 1384611 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - "C" - DURING INSPECTION CORROSION WAS FOUND ON FRAME BS 947 BETWEEN STR 27R AND 27L. MAINTENANCE RE MOVED CORROSION FROM FRAME BS 947 AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. DAMAGED SECTION OF FRAME WAS REMOVED AND A -1 REPAIR SHEAR TIE AND FILLER WERE FABRICATED AND INSTALLED IAW B737-300 SRM 53-00-07, PG 222-224. 2 L 7 2 4F RT A16WE 2002012200199 20020122 00199 NM 2002 1 22 AWXA200200054 1 20020106 A 5330 6545776100 SKIN BOEING 737 737301 1384611 NM GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - "C" - DURING INSPECTION SKIN WAS FOUND DAMAGED BETWEEN BS 900 AND BS 907, STR 26R AND STR 26L. MAIN TENANCE REMOVED DAMAGED AREA OF SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS. FABRICATED A REPAIR DOUBLER AN D FILLER AND INSTALLED REPAIRS IAW B737-300 SRM 53-00-01, PG 314-319, SRM 51-20-01, PG 10-47, AND SRM 51-40-02 PG 3, 4, & 38. 2 L 7 2 4F RT A16WE 2002012200200 20020122 00200 NM 2002 1 22 AWXA200200055 1 20020108 A 5311 654656315 FRAME BOEING 737 737301 1384611 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - "C" - DURING INSPECTION CORROSION WAS FOUND ON FRAME AT BS 967 BETWEEN STR 27R AND STR 27L. MAINTEN ANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. DAMAGED AREA OF FRAME WAS CUTOUT AND 1 EACH REPAIR SHEAR T IE WAS FABRICATED AND INSTALLED IAW B737-300 SRM 53-00-07, PG 101-104, SRM 53-60-07, PG 8-9, SRM 53-00-07 PG 219-221, AN D SRM 51-20-01 PG 1. 2 L 7 2 4F RT A16WE 2002012200201 20020122 00201 NM 2002 1 22 AWXA200200056 1 20020108 A 5311 65465582 FRAME BOEING 737 737301 1384611 NM BENT A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - "C" - DURING INSPECTION THE FRAME WAS FOUND BENT AT BS 907 BETWEEN STR 27R AND STR 27L. MAINTENANCE REMOVED DAMAGED AREA OF LOWER FLANGE AT BS 907, FABRICATED A NEW LOWER FLANGE AND INSTALLED REPAIR IAW B737-300 SRM 51- 40-02, PG 1, 6-9. 2 L 7 2 4F RT A16WE 2002012200202 20020122 00202 NM 2002 1 22 AWXA200200057 1 20020108 A 5311 65465591 FRAME BOEING 737 737301 1384611 NM BENT A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - "C" - DURING INSPECTION THE FRAME WAS FOUND BENT AT BS 927 BETWEEN STR 27R AND STR 27L. MAINTENANCE REMOVED DAMAGED LOWER FRAME FLANGE, FABRICATED A NEW LOWER FRAME FLANGE AND INSTALLED REPAIR IAW B737-300 SRM 53-00-07 PG 219-221. 2 L 7 2 4F RT A16WE 2002012200220 20020122 00220 NM 2002 1 22 QXEA0200073 1 20020117 A 2420 DH103024600CS INVERTER DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 6250 6250 528 PDX- ACRID SMELL NOTICED IN COCKPIT. AFTER TROUBLE SHOOTING FOUND #1 INVERTER TO BE EMITTING ODOR. REMOVED AND REPLACED #1 INVERTER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002012300030 20020123 00030 NM 2002 1 23 SWAA020138 1 20020121 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 12 DEF. SECURED LIGHT PER M M. 2 L 7 2 4F RT A16WE 2002012300031 20020123 00031 NM 2002 1 23 SWAA020143 1 20020121 A 5311 6545768 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT STR 8R, BS'S 380, 400 AND 867. REPAIRED FRAMES PER BFG ER.. 2 L 7 2 4F RT A16WE 2002012300032 20020123 00032 NM 2002 1 23 SWAA020144 1 20020121 A 5311 6545768 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT STR 8L, BS'S 400, 727, 867, 887 AND 907. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2002012300033 20020123 00033 NM 2002 1 23 SWAA020145 1 20020119 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (3 EA) AT BS 178, WL 188 AND LBL 1.0, WL 201 AND LBL 5.0, WL 199 AND LBL 5.0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002012300034 20020123 00034 NM 2002 1 23 SWAA020147 1 20020118 A 5330 654577678 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED 1/4D CHECK, FOUND VHF ANTENNA BLANKING PLATE CORRODED AT BS 727D TO 727E, BL O. REPAIRED SKIN PER SWA RA AND SRM. 2 L 7 2 4F RT A16WE 2002012300037 20020123 00037 EU 2002 1 23 02FDEA00053 1 20020116 A 2160 SENSOR AIRBUS 310 A310222 3930315 EU AIR CONDITIONING DIRTY A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 416FE 790 REACHING 350 ECAM ADVISED OF VENT BLOWERS LO FLOW FOLLOWED ECAM SELECTED ALTN AND ECAM REAPPEARED LO FLOW. RESET BLOWER SWITCH AFTER 5 MINS AND PRESSED ON IT, REOCCURRED AND DECIDED TO RETURN TO OMDB. CLEANED FLOW SENSOR 79HQ CK BLOWER FA NS FOR OPS CHECK SATISFACTORY. CHECKED DUST EXTRACTOR FOUND CLEAN, CHECKED OVERBOARD EXTRACTOR VALVE 75 HR FOR CLOSING AND OPENING SATISFACTORY. TROUBLESHOT PER TSM 21-20-00 NIL FAULTS AND CND OVER A THREE HR PERIOD. THEN A/C ARRIVED DXB ALT SYS WORKING NORMALLY AND NO ECAM ADVISORY. 2 L 7 2 4F RT A35EU 2002012300051 20020123 00051 NM 2002 1 23 2002UALA00064 1 20020117 A 2750 FLAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WING MALFUNCTIONED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 556UA 26650 TAKEOFF ROLL 120 KTS TRAIL EDGE DISAGREE LIGHT ON EICAS AND FWD PANEL. USING NORMAL FLAP LEVER WOULD NOT MOVE. TRAILIN G EDGE ALTN SWITCH CLEARED DISAGREE LIGHT. USING ALTN METHOD LOWERED FLAPS TO 20. ACP CK OF FLAP SYSTEM. RAN FLAPS UP ELECTRIC AND FULL UP AND DOWN WITH HYD, BITE CK OF FSEU OK. ALL FLAP TRANSMISSIONS CHECKED NO OVERLOAD TRIP, NO ISOL V LV MSG. 2 L 7 2 4F 4 F RT A2NM E17NE 2002012300053 20020123 00053 NM 2002 1 23 2002UALA00077 1 20020111 A 5310 DOOR FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 924UA 26645 AFT CARGO DOOR CUTOUT AFT BEAM STATION 845 WEB CHAFED AND GOUGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300054 20020123 00054 NM 2002 1 23 2002UALA00078 1 20020111 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 924UA 26645 LEFT HAND LOWER FUSELAGE STATION 907 STRINGER 17L SKIN DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER . 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300056 20020123 00056 NM 2002 1 23 2002UALA00079 1 20020112 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CABIN FRAME CRACKED AT STATION 847, STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FRAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300057 20020123 00057 NM 2002 1 23 2002UALA00080 1 20020112 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CABIN FRAME CRACKED, STATION 847, STRINGER 9 LEFT. MAJOR REPAIR ACCOMPLISHED. FRAME DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300059 20020123 00059 NM 2002 1 23 2002UALA00081 1 20020111 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 LEFT WHEEL WELL UPPER BULKHEAD CRACKED AT LBL 31 STATION 663.75 + 2. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. INSTA LLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300060 20020123 00060 NM 2002 1 23 2002UALA00082 1 20020112 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 AFT CABIN FLOORBEAM ANGLED INTERCOSTAL JUST AFT OF FLOORBEAM 986, EXCESSIVE MATERIAL LOSS AT RBL 14 INCHES AT 996. MAJ OR REPAIR ACCOMPLISHED. INTERCOSTAL FLOORBEAM REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300061 20020123 00061 NM 2002 1 23 2002UALA00083 1 20020112 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 AFT GALLEY DOOR CUTOUT FORWARD FUSELAGE FRAME STATION 956 IS CRACKED 1.5 IN BETWEEN STRINGER 9-10R AT UPPER LATCH ROLLER FITTING ATTACHMENT. MAJOR REPAIR ACCOMPLISHED. STUB FRAME REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300063 20020123 00063 NM 2002 1 23 2002UALA00084 1 20020113 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 925UA 26646 FUSELAGE FRAME DENTED AT STATION 747 STRINGER 24R. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FRAME REPAIR. INSTALLED NE W SPLICE PLATE TO INCORPORATE DAMAGED AREA. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300064 20020123 00064 NM 2002 1 23 2002UALA00085 1 20020113 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 RIGHT HAND FORWARD CREASE BEAM NUMEROUS AREAS OF CORROSION FOUND FROM STATION 290 TO STA 358 WL 208 RBL 53 TO RBL 67. M AJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300065 20020123 00065 NM 2002 1 23 2002UALA00086 1 20020113 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CABIN UPPER LOBE FRAME CRACKED AT BODY STATION 887 AND STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300066 20020123 00066 NM 2002 1 23 2002UALA00087 1 20020113 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CABIN UPPER LOBE FRAME CRACKED AT BODY STATION 867 AND STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300067 20020123 00067 NM 2002 1 23 2002UALA00088 1 20020113 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 RIGHT HAND FORWARD GALLEY DOOR THRESHOLD LOWER SILL Z-ANGLE CORRODED NUMEROUS AREAS STATION 314 TO STATION 327 RBL 54 TO RBL 61 WL 209. MAJOR REPAIR ACCOMPLISHED. ANGLE REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300068 20020123 00068 NM 2002 1 23 2002UALA00089 1 20020113 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CABIN FUSELAGE FRAME SKIN WEB CRACKED, BODY STATION 907 LBL 2. MAJOR REPAIR ACCOMPLISHED. FRAME REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300069 20020123 00069 NM 2002 1 23 2002UALA00090 1 20020113 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CABIN FRAME 294.5 IS CRACKED JUST ABOVE STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300070 20020123 00070 NM 2002 1 23 2002UALA00091 1 20020113 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CABIN FRAME STATION 827 CRACKED AT STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300071 20020123 00071 NM 2002 1 23 2002UALA00092 1 20020113 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 FRAME 188 AT WL 207 STRINGER 17L HAS CRACK. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME REPAIR DOUBLER AND INSTALLED EX TERNAL FUSELAGE DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300072 20020123 00072 NM 2002 1 23 2002UALA00093 1 20020109 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 188UA 26877 EEL LAMP IS INOP AT SEAT 58C. RELAMPED EEL LIGHT ASSY. OPS CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002012300073 20020123 00073 NM 2002 1 23 2002UALA00094 1 20020110 A 3350 BPS73 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 172UA 24363 EEL LIGHTING FROM SEATS 55ABC TO AFT LAV BULKHEAD LEFT HAND SIDE, INCLUDING DOOR 5L BLUE EEL SIGN ARE VERY DIM. REPLACE D BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002012300077 20020123 00077 NM 2002 1 23 2002UALA00095 1 20020111 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4090 PW4090 52119 NE CABIN DAMAGED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 197UA 26901 EXIT PATH LIGHTING 6B ON SIDE OF SEAT IS TORN OFF. REPLACED 2 LIGHT ASSEMBLY'S. 2 L 7 4 4F 4 F RT A20WE E46NE 2002012300078 20020123 00078 NM 2002 1 23 2002UALA00096 1 20020114 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 MAIN CABIN WEB CRACKED AT STATION 992 RBL 44. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED WEB. FABRICATED AND INSTALLE D NEW WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300080 20020123 00080 NM 2002 1 23 2002UALA00097 1 20020114 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 CABIN STATION 727B-727C STRINGER 17L WEB HAS CORROSION ON TOP. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300081 20020123 00081 NM 2002 1 23 2002UALA00098 1 20020114 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 AFT PIT FLOOR SUPPORT BODY STATION 773 RBL 3 IS CORRODED AND OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. REMOVED FLOOR S UPPORT. FABRICATED AND INSTALLED NEW SUPPORT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300082 20020123 00082 NM 2002 1 23 2002UALA00099 1 20020114 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 AFT CARGO PIT FLOOR SUPPORT BODY STATION 773 RBL 7 CORRODED AND OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMA GE. FABRICATED AND INSTALLED NEW FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300083 20020123 00083 NM 2002 1 23 2002UALA00100 1 20020114 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 MAIN CABIN LAVATORY SUPPORT BEAM AT STATION 992 BETWEEN RBL 18 TO RBL 44 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOV ED DAMAGE. FABRICATED AND INSTALLED NEW SUPPORT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300085 20020123 00085 NM 2002 1 23 2002UALA00101 1 20020114 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 FORWARD PIT CUTOUT FRAME AT BODY STATION 450 AFT OF DOOR SILL GOUGED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. FABR ICATED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300087 20020123 00087 NM 2002 1 23 2002UALA00102 1 20020114 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 MAIN CABIN FLOORBOARD SUPPORT WEB DAMAGED AT BODY STATION 540 LBL 49-63. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLA CED FLOOR SUPPORT WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300088 20020123 00088 NM 2002 1 23 2002UALA00103 1 20020114 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 LEFT HAND BODY STATION 188 CHORD CRACKED AT WL 207. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLE A ND EXTERNAL DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300089 20020123 00089 NM 2002 1 23 2002UALA00104 1 20020114 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 RIGHT HAND BODY STATION 188 CHORD CRACKED AT WL 207. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ANGLE AND EXT ERNAL DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300091 20020123 00091 NM 2002 1 23 2002UALA00105 1 20020114 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 AFT PIT DOOR CUTOUT FRAME WEB HAS CORROSION FROM STRINGER 22R TO STRINGER 25R BODY STATION 794. MAJOR REPAIR ACCOMPLISH ED. REMOVED CORROSION AND REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300093 20020123 00093 NM 2002 1 23 2002UALA00106 1 20020114 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 FORWARD GALLEY DOOR CUTOUT FRAME 295.5 CRACKED ON FORWARD SIDE AT TOP STOP PAD FITTING. MAJOR REPAIR ACCOMPLISHED. REP LACED STUB FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300094 20020123 00094 NM 2002 1 23 2002UALA00107 1 20020114 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 FUSELAGE STRINGER 10R CLIP TO FRAME STATION 663 CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012300096 20020123 00096 NM 2002 1 23 2002UALA00108 1 20020114 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 FUSELAGE STRINGER 2L CLIP TO FRAME STATION 807 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020600054 20020206 00054 NM 2002 2 6 2002UALA00109 1 20020115 A 3310 KCAE4F RELAY BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT INTERMITTENT A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 606UA 21867 LIGHTS FLICKERING IN COCKPIT. POSSIBLE LOSS OF ALL INSTRUMENT LIGHTING. DIVERTED TO DEN. FOUND LOOSE WIRE AT TERMINAL BLOCK BEHIND P6 PANEL, SECURED WIRE. PROVIDES POWER TO CAPT FLOODLIGHT STBY POWER RELAY. OVERHEAD LIGHTS FLICKER-REPE AT. REPAIRED WIRING, REPLACED K770-AC STBY TRANSFER RELAY AND K105 AC STBY POWER RELAY IN P6 PANEL. 2 L 7 2 4F 4 F RT A1NM E3NE 2002012300098 20020123 00098 NM 2002 1 23 2002UALA00110 1 20020114 A 5270 TARGET BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR BENT A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 395UA 24670 UNSCHEDULED LANDING DUE TO FWD CARGO DOOR WARNING LIGHT. FOUND DOOR LIGHT TARGET BENT. ADJUSTED TARGET. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020600055 20020206 00055 NM 2002 2 6 2002UALA00111 1 20020114 A 5330 148W49129 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 779UA * 26941 LEFT HAND FUSELAGE SKIN STATION 2268.25 DAMAGED NEAR HORIZONTAL STAB CUTOUT. MAJOR REPAIR ACCOMPLISHED ON SKIN PANEL 14 8W4912-9. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002020600061 20020206 00061 NM 2002 2 6 2002UALA00114 1 20020116 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 194UA 26892 EEL LIGHT STRIP AT SEAT 5A IS COMING APART. SECURED EEL LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2002020600062 20020206 00062 NM 2002 2 6 2002UALA00115 1 20020115 A 3350 SOCKET BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN CORRODED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 121UA 29167 EXTERIOR EMERGENCY LIGHT OVERWING RIGHT HAND SIDE THIRD ASSEMBLY AFT HAS FORWARD BULB INOP. REMOVED CORROSION INSIDE LA MP SOCKET, OPERATION CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2002021300061 20020213 00061 NM 2002 2 13 2002UALA00116 1 20020115 A 2121 MR212655 FAN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAILED A UALA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 29 654UA 25392 FLIGHT DECK AND CABIN FILLED WITH SMOKE. EICAS MSG FOR RIGHT RECIRCULATION FAN DISPLAYED. SHUTDOWN RIGHT AND LEFT RECI RCULATION FAN AS WELL AS GASPER FAN. SMOKE DISSIPATED AND CONTINUED TO LHR. FOUND RT RECIRCULATION FAN AT FAULT. REPL ACED RT RECIRCULATION FAN AND NO FURTHER EVENTS OF SMOKE IN THE FLIGHT DECK OR CABIN HAVE BEEN REPORTED. PRELIMINARY SH OP TESTING FOUND BEARINGS SEIZED, THEREFORE PREVENTING FAN FROM TURNING. 2 L 7 2 4F 4 F RT A1NM E24NE 2002020600063 20020206 00063 NM 2002 2 6 2002UALA00117 1 20020115 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 121UA 29167 FORWARD EMERGENCY LIGHT AT DOOR 1R SILL INOP. RELAMPED, OPS CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002020100026 20020201 00026 2002 2 1 2002UALA00118 4 20020116 A 3416 ALTIMETER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT INACCURATE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 30029 STANDBY ALTIMETER 500 FT DIFFERENCE FROM CAPTAIN'S AT FLIGHT LEVEL 390. 400 FT DIFFERENCE AT FLIGHT LEVEL 200 AND 60 FT DIFFERENCE ON THE GROUND. SUPPLEMENTAL DATA UPDATE CAUSE: 500 FT DIFFERENCE FROM CAPTAIN'S ALTIMETER AT FLIGHT LEVEL 390 . CORRECTIVE ACTIONS: ERFORMED LEAK CHECK, REPLACED THE STBY. ALTIMETER, TESTED THE SYSTEM AT 10,000 FT. SHOP FIN DINGS: DURING THE TEST, IT WAS NOTICED THAT THE VIBRATOR WAS NOISY AND THERE WAS SOME STICKING ON THE DESCENT. THE UNI T WAS IN TOLERANCE, VIBRATOR WAS REPLACED AND THE DRUM COUNTER CLEANED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002012300130 20020123 00130 EA 2002 1 23 COMA0260058 1 20020121 A 5270 840534 SWITCH CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 786CA 7333 FLIGHT 6080 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.REPLACED PROXIMITY SWITCH PS2MB. 2 L 7 2 4F RT A21EA 2002012300137 20020123 00137 WP 2002 1 23 DHL2002805006 1 20020104 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 2299LT. WING CTR. L/E LOWER SKIN RIB T/E CRACKED BTWN XFS329.000 & 347.750 2 L 7 4 4F RT 4A25 2002012300139 20020123 00139 WP 2002 1 23 DHL2002805010 1 20020104 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 2396LT. WING , CTR. LEADING EDGE, UPPER SKIN RIB (FORMER) TRAILING EDGE CRACKED 1" @ STA. XFS416.500 2 L 7 4 4F RT 4A25 2002012300141 20020123 00141 WP 2002 1 23 DHL2002805012 1 20020101 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 1991RT. WING L/E UPPER RIB (FORMER) CRACKED .500 @ XFS 701.000 2 L 7 4 4F RT 4A25 2002020600064 20020206 00064 NM 2002 2 6 2002UALA00119 1 20020115 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN CONTAMINATED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 121UA 29167 EEL STRIP ON WALL JUST AFT OF COCKPIT DOOR INOP. CLEANED WATER FROM CONNECTION AND RESECURED. OPS CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002020600065 20020206 00065 NM 2002 2 6 2002UALA00121 1 20020118 A 3350 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 811UA 847 EMERGENCY LIGHT TEST FAILED. FAULT CODE 33-51-38 EMERGENCY POWER SUPPLY UNIT BATTERY AFT LEFT. REPLACED EMERGENCY POWE R SUPPLY UNIT BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2002020600066 20020206 00066 NM 2002 2 6 2002UALA00122 1 20020117 A 3350 BATTERY PACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 819UA 893 EMERGENCY LIGHT TEST FAIL. FAULTS EMERGENCY POWER SUPPLY UNIT BATTERY AFT LEFT. REPLACED BATTERY PACK FOR AFT LEFT POW ER SUPPLY. EMERGENCY LIGHT BUILT IN TEST EQUIPMENT GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2002021300064 20020213 00064 NM 2002 2 13 2002UALA00123 1 20020118 A 5330 147W33113 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 779UA 22754 26941 DENT ON LEFT HAND AFT FUSELAGE STATION 2107. MAJOR REPAIR ACCOMPLISHED. FUSELAGE EXTERNAL SKIN STATION 2107 STRINGER 3 0L REPAIRED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002012300142 20020123 00142 WP 2002 1 23 ABXA010667 1 20020112 A 5320 3755822505N FITTING DOUG DC8 DC861 3021952 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 FORWARD CARGO, STATION 320, BETWEEN LONGERON 28 LEFT - LONGERON 29 LEFT, Z-ANGLE CORRODED. REMOVED OLD FITTING. RECEIV ED NEW FITTING P/N 3155822-505N. FABRICATED REPAIR ANGLES IAW DC-8 SRM 53-2-0. 2 L 7 4 4F 4A25 2002012300143 20020123 00143 WP 2002 1 23 ABXA010668 1 20020112 A 5320 3755822505N FITTING DOUG DC8 DC861 3021952 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 FORWARD CARGO, STATION LONGERON 29 LEFT AND LONGERON 30 LEFT Z-ANGLE CORRODED. REMOVED CORRODED FITTING. RECEIVED NEW FITTING P/N 3755822-505N. FABRICATED REPAIR ANGLES IAW DC-8 SRM 53-2-0. INSTALLED Z-FITTING AND REPAIR ANGLES IAW DC-8 SRM 53-2-0. 2 L 7 4 4F 4A25 2002012300145 20020123 00145 WP 2002 1 23 ABXA010670 1 20020115 A 5320 36410042 FITTING DOUG DC8 DC861 3021952 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 RIGHT MAIN LANDING GEAR WHEEL WELL, LONGERON 24 RIGHT, FITTING HAD EXFOLIATION CORROSION AT STATION 879. REMOVED CORROD ED FITTING. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-0. INSTALLED NEW FITTING AND REPAIR PARTS IAW DC-8 SRM 53-2-0. 2 L 7 4 4F 4A25 2002012300146 20020123 00146 WP 2002 1 23 ABXA010672 1 20020103 A 5320 39248461 ATTACH ANGLE DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 LEFT WHEEL WELL OUTBOARD SLANT PANEL ATTACH ANGLE EXFOLIATED AT LOWER FASTENER. LOCATED AND DRILLED SLANT PANEL ATTACH ANGLE IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002012300147 20020123 00147 WP 2002 1 23 ABXA010675 1 20020118 A 5250 LATCH DOUG DC8 DC861 3021952 WP COCKPIT DOOR OUT OF ADJ A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 COCKPIT ENTRY DOOR LATCH MECHANISM WAS JAMMED. ADJUSTED DOOR LATCH AS NEEDED IAW DC-9 MM CHAPTER 51. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2002012300148 20020123 00148 WP 2002 1 23 ABXA010677 1 20020117 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 CABIN EMERGENCY LIGHTS TEST VERY DIM, OVERHEAD PANEL IN COCKPIT. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC -9 MM 33-53-00-8-0001. 2 L 7 2 4F A6WE 2002012300149 20020123 00149 WP 2002 1 23 ABXA010678 1 20020121 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 EMERGENCY LIGHTS BATTERIES LOW. REPLACED THE EMERGENCY LIGHTS BATTERIES IAW DC-9 AMM 33-53-00-8. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002012300150 20020123 00150 WP 2002 1 23 ABXA010679 1 20020121 A 3350 5708458503 BATTERY DOUG DC8 DC861 3021952 WP CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 808 46017 EMERGENCY LIGHTS WERE DIM. REPLACED EMERGENCY LIGHT BATTERY AND RELAY ASSEMBLY. OPS CHECKED GOOD IAW DC-8 MM 33-50-01- 2-0001. 2 L 7 4 4F 4A25 2002012300151 20020123 00151 SO 2002 1 23 C2XA02BT001 1 20020114 A 2611 SMOKE DETECTOR EMB 135 EMB135LR 3260305 SO LAVATORY DIRTY A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 14505 145192 EWR---CO3443/MX, CREW REPORTED AFTER TAKEOFF FROM DAY, LAV SMOKE MASTER WARNING ON CLIMBOUT. AIRCRAFT RETURNED TO DAY. AIRCRAFT INSPECTED AND RELEASED IAW MEL. AIRCRAFT RETURNED TO SERVICE. UPON ARRIVAL IN NEWARK MAINTENANCE CLEANED SMO KE DETECTOR SENSOR IAW EMB135/145 AMM 26-15-00. OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT TOOO11AT 2002012300152 20020123 00152 SO 2002 1 23 C2XA02CL011 1 20020117 A 3397 CONNECTOR EMB 135 EMB135ER 3260203 SO BATTERY PACK LOOSE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 17507 145215 CLE FLIGHT 4014, THE CREW REPORTED THE EXIT SIGN BY THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESE T THE NR 1 BATTERY PACK CONNECTOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002012300153 20020123 00153 SO 2002 1 23 C2XA02CL012 1 20020118 A 5270 14528235401 SWITCH EMB 135 EMB135ER 3260203 SO EMERGENCY EXIT OUT OF ADJ A C2XA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 27 16510 145251 DURING A 2A INSPECTION MAINTENANCE FOUND THE RIGHT HAND OVERWING EMERGENCY EXIT DID NOT PRODUCE A MESSAGE ON THE EICAS W HEN THE DOOR WAS OPEN. MAINTENANCE ADJUSTED THE MICROSWITCH ON THE RIGHT HAND EMERGENCY EXIT DOOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002012300154 20020123 00154 SO 2002 1 23 C2XA02CL013 1 20020118 A 5210 LOCK EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 14959 145091 CLE FLIGHT 3260, THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO LOCK CLOSED. MAINTENANCE INSPECTED, CLEANED AND LUBRICATED THE MAIN CABIN DOOR ROLLER AND LOCKING MECHANISM. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002012300155 20020123 00155 SO 2002 1 23 C2XA02CL014 1 20020120 A 3350 110049 CHARGER EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14925 145004 DURING ROUTINE MAINTENANCE BOTH OVERWING EMERGENCY LIGHTS WOULD NOT ILLUMINATE DURING TESTING. MAINTENANCE REPLACED THE NR 4 BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002012300156 20020123 00156 SO 2002 1 23 C2XA02CL015 1 20020121 A 3350 110049 POWER SUPPLY EMB 145 EMB145ER 3260211 SO CABIN DISCHARGED A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 14925 145004 CLE FLIGHT 3023, THE CREW REPORTED THE AFT AISLE EMERGENCY LIGHTS WILL NOT TURN OFF. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002012300157 20020123 00157 SO 2002 1 23 C2XA02TY015 1 20020118 A 5751 14569009407 ATTACH FITTING EMB 145 EMB145 3260210 SO AILERON GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND AILERON WAS FOUND TO BE GOUGED AT THE ACTUATOR ATTACHMENT POINT. MAIN TENANCE ACCOMPLISHED A BLEND-OUT REPAIR AND DYE PENETRANT INSPECTION IAW EMBRAER GST 0046/02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED INSPECTION. 2 L 7 2 4F RT T00011AT 2002012900160 20020129 00160 NM 2002 1 29 DHL2002707001 1 20020122 A 2612 SENSOR BOEING 727 72722 1384002 NM APU FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 707DH 18321 APU FIRE TEST INOP. REMOVED AND REPLACED FIRE DETECTOR SENSOR IAW DHL 727 MM 26-15-002. SYSTEM OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2002012300158 20020123 00158 NM 2002 1 23 AWXA200200061 1 20020107 A 5330 6545776 SKIN BOEING 737 737301 1384611 NM FUSELAGE BULGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - "C" - DURING INSPECTION FOR REPAIR OF TAIL DRAG DAMAGE A BULGE IN SKIN WAS FOUND BELOW THE AFT CARG O PIT DOOR BS 807 TO BS 812, STR 27R TO 25R. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN AND PERFORMED HFEC INSPECTION TO VE RIFY CRACKS WERE CONTAINED. FABRICATED A FILLER, DOUBLER, TRIPLER, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5361-02021-5 52. 2 L 7 2 4F RT A16WE 2002012300159 20020123 00159 NM 2002 1 23 AWXA200200065 1 20020120 A 3350 E0052R8B3APNE CONNECTOR AIRBUS A319 A319132 3930340 NM SR 4,10L/R,14,16 DEFECTIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 YWG - EEL - "C" - DURING BC-02 CHECK INSPECTION ROWS #4 L/H, #10 L/H & R/H, #14 L/H, #16 L/H EMERGENCY SEAT LIGHTS CONNE CTORS WERE FOUND TO REQUIRE REPLACEMENT. MAINTENANCE REPLACED EMERGENCY SEAT LIGHT CONNECTORS AT ROWS #4 L/H, #10 L/H & R/H, #14 L/H, #16 L/H IAW ESPM 20-44-32, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002012300160 20020123 00160 NM 2002 1 23 DHL2002709002 1 20020115 A 4900 ELECTRICAL SYS BOEING 727 72782C 1384026 NM APU MALFUNCTIONED A DHLA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 709DH 19968 APU ELECTRICAL TRIPPED OFF. A FEW SECONDS LATER, LEFT PACK TRIP OFF LIGHT ILLUMINATED AND THEN COCKPIT FILLED WITH SMOK E. RAN APU IAW MM 49-00 & JRH 8.1. APU & AIR OPS CHECKS GOOD. APU ELECTRICS WILL NOT HOLD A LOAD. 2 L 7 3 4F A3WE 2002012300161 20020123 00161 NM 2002 1 23 DHL2002746001 1 20020119 A 2611 SMOKE DETECTOR BOEING 727 727224 1384076 NM CABIN FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 746DH 22252 DURING SERVICED CHECK, FOUND SMOKE DETECTOR SYSTEM FAIL TO TEST GREEN LIGHT OFF. T/S SYSTEM FOUND FW SEND DETECTOR BAD. REMOVED AND REPLACED DETECTOR, REPROGRAM SYSTEM IAW M SUPP MANUAL 26-16-01 & ST 300. 2 L 7 3 4F A3WE 2002012300162 20020123 00162 WP 2002 1 23 DHL2002801002 1 20020116 A 2612 CONNECTOR DOUG DC8 DC873F 302199F WP NR 2 ENGINE FAULTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 NR 2 ENGINE SYSTEM A-LOOP FIRE DETECTION INOP. REMOVED AND REPLACED CONNECTOR P1-8051 ON LOOP-A PYLON SECTION IAW WDM 2 6-01-01, TESTED OK. 2 L 7 4 4F RT 4A25 2002012300163 20020123 00163 WP 2002 1 23 DHL2002803002 1 20020116 A 2611 SMOKE DETECTOR DOUG DC8 DC873 302199C WP CARGO BAY INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 803DH 46123 MAIN CARGO DECK SMOKE DETECTOR NR 8 WOULD NOT TEST. RELAMPED AMPLIFIER CHECKS NORMAL IAW M/M 26-16. 2 L 7 4 4F RT 4A25 2002012300164 20020123 00164 WP 2002 1 23 DHL2002803003 1 20020119 A 2611 LIGHT DOUG DC8 DC873 302199C WP SMOKE DETECTOR INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 803DH 46123 NR 4 SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED SMOKE DETECTOR TEST BULB PER MM 26-10-00. 2 L 7 4 4F RT 4A25 2002012300165 20020123 00165 WP 2002 1 23 DHL2002803004 1 20020118 A 2620 FIRE BOTTLE DOUG DC8 DC873 302199C WP NR 3&4 ENGINE LOW A DHLA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 803DH 46123 ENGINES 3 & 4 AGENT LOW PRESSURE LIGHT ILLUMINATED. REPLACED O/B BOTTLE PER DACO 26-20-0. OPS CHECK NORMAL. BOTH LIGH TS EXTINGUISHED. 2 L 7 4 4F RT 4A25 2002012300172 20020123 00172 NM 2002 1 23 F3LA200200015 1 20020110 A 5320 ANGLE BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED THRESHOLD SUPPORT ANGLE, STA 794, STR 25-R, IN AFT CARGO COMPARTMENT CORRODED. RE PLACED SUPPORT ANGLE PER SRM 51-10-2 AND 51-30-2. 2 L 7 2 4F RT A16WE 2002012300183 20020123 00183 CE 2002 1 23 GLBA2002003 1 20020111 A 3230 571302 MOTOR BEECH 1900 1900D 1154162 CE LANDING GEAR FAILED A GLBA O OTHER J WARNING INDICATION AP APPROACH 1 NM 03 228GL UE228 LANDING GEAR WOULD NOT EXTEND. INSPECTED REPLACED HYDRAULIC MOTOR, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002012300184 20020123 00184 CE 2002 1 23 GLBA2002004 1 20020114 A 3610 DUCT BEECH 1900 1900D 1154162 CE BLEED AIR DAMAGED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 201GL UE201 RIGHT BLEED AIR FAIL. INSPECTED AND REPAIRED EVA TUBING, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002021100120 20020211 00120 NE 2002 2 11 GLBA2002005 2 20020115 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT FLUCTUATES A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 201GL UE201 LEFT ENGINE TORQUE FLUX. INSPECTED BLEED VALVE AND BLENDED 1ST STAGE COMPRESSOR BLADES. COULD NOT DUPLICATE. TORQUE F LUX. 2 L 7 2 4T 4 T RT A24CE E26NE 2002012300185 20020123 00185 CE 2002 1 23 GLBA2002007 1 20020117 A 3260 9042292003 ANNUNCIATOR BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 NM 03 118GL UE118 LANDING GEAR DOWNLOCK LIGHT WOULD NOT ILLUMINATE. REPLACED ANNUNICATOR MODULE, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002021200132 20020212 00132 CE 2002 2 12 GLBA2002008 1 20020118 A 5270 SWITCH BEECH 1900 1900D 1154162 CE PAX DOOR OUT OF ADJUST A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 97UX UE97 CABIN DOOR ANNUNCIATOR ILLUMINATED. ADJUSTED DOOR SWITCH, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002012300186 20020123 00186 EU 2002 1 23 MALA020109 1 20020106 A 3230 STRUT BAC 146 AVRO146RJ85A 1500097 EU LT MLG CONTAMINATED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 518XJ E2337 LT MAIN LANDING GEAR DOES NOT COME UP ON INITIAL RETRACTION. LEFT MAIN GEAR IS STICKING IN THE DOWN POSITION AFTER TAKE -OFF. PILOT HAS TO CYCLE GEAR HANDLE THEN GEAR WOULD MOVE. MAINTENANCE BLED GREEN HYDRAULIC SYSTEM AND OLEO LOCK STRUT S. PERFORMED EXTENSION AND RETRACTION ADJUSTMENT TEST PER AMM 32-30-00 501. ALL CHECKS GOOD, 409 CARD 100678 FOR DETAI LS. 2 H 7 4 4F RT A49EU 2002012400026 20020124 00026 CE 2002 1 24 0127 1 20020115 A 7603 NUT BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HMU LEVER LOOSE E DJFA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 EA 23 440CW RK40 PCE100035LNR AIRCRAFT WAS ON DESCENT INTO MSP, AFTER REDUCING POWER THE ENGINE KEPT SPOOLING DOWN AT THAT POINT THE PILOTS SHUT THE E NGINE DOWN. ACFT LANDED WITH NO FURTHER PROBLEMS. INVESTIGATION REVEALED THE HMU LEVER NUT HAD LOOSENED UP ENOUGH TO A LLOW THE LEVER TO SLIP OUT OF THE RIG AND ALLOW THE ENGINE TO SHUT DOWN. 2 H 7 2 4F 4 F RT A16SW E25EA 2002012400027 20020124 00027 CE 2002 1 24 0128 1 20020106 A 3230 UPLOCK BEECH MU300 400A 1155402 CE NLG OUT OF ADJ E DJFA O OTHER J WARNING INDICATION AP APPROACH 1 EA 23 442CW RK42 AIRCRAFT DURING APPROACH NOSE GEAR DEPLOYED. GEAR WAS CYCLED AND THEN DEPLOYED WITH THREE GREEN LIGHTS. FOUND NOSE GEA R UPLOCK HOOK OUT OF ADJUSTMENT AND NOSE STRUT UNDER SERVICED. UPLOCK HOOK WAS REGID AND NOSE GEAR WAS SERVICED. 2 H 7 2 4F RT A16SW 2002020500006 20020205 00006 NM 2002 2 5 02FDEA00061 1 20020123 A 5531 RIB BOEING 727 727277 138408S NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 RIB CRACKED IN VERTICAL STABILIZER LT STR 9, FIN STA 110.4. R&R RIB. 2 L 7 3 4F RT A3WE 2002012400029 20020124 00029 NM 2002 1 24 02015408 1 20020115 A 3350 POWER SUPPLY DORNER DO32 DO328300 NM CABIN OUT OF POSITION A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 408FJ 3160 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTS AT SEAT ROWS 4, 5, & 6 WERE INOPERA TIVE. MAINTENANCE PERSONNEL RE-RACKED THE EMERGENCY LIGHTS POWER SUPPLY. AN OPERATIONAL CHECK OF THE SYSTEM WAS SATISF ACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002012400032 20020124 00032 EU 2002 1 24 02017312 1 20020117 A 2150 CLAMP JETAIR JETSTM JETSTM4101 1500501 EU A/C BAY LOOSE A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 312UE 41025 DURING THE CLIMB OF THE FLIGHT FROM IAD TO EWR, THE CREW REPORTED A STRONG EXHAUST SMELL ENTERED THE CABIN FROM BOTH FLO WS. THE CREW DONNED OXYGEN, RETURNED TO IAD, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL SECURED A CLAMP ON THE ACM DUCT TO THE WATER SEPARATOR. AN ENGINE RUNNING OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002012400034 20020124 00034 EA 2002 1 24 02022651 1 20020122 A 3234 7455021 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 651BR 7426 DURING CLIMB OF THE FLIGHT FROM IAD TO GSP, THE CREW REPORTED THAT UPON LANDING GEAR RETRACTION HAD NO INDICATION OF GEA R RETRACTION ON THE FLIGHT DECK. THE THREE GREEN GEAR DOWN/LOCKED INDICATORS REMAINED ILLUMINATED. THE CREW REPORTED, RECEIVED ANTI-SKID OUTBOARD AND PARKING BRAKE SOV FAIL MESSAGES. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LANDING GEAR SELECTOR. LANDING GEAR EXTENSION/RETRACTION OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002031400154 20020314 00154 NE 2002 3 14 2002UALA00046 2 20020108 A 7261 7T0384 NUT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GEARBOX LOOSE A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 548UA 14125 25396 726688 NUMBER 1 ENGINE OIL QUANTITY DECREASED TO ZERO. OIL TEMPERATURE INCREASING. BREATHER MANIFOLD CRACKED. THIS WAS THE S ECOND TIME IN 30 DAYS THAT THE BREATHER MANIFOLD WAS FOUND CRACKED ON THIS ENGINE. ENGINE WAS REMOVED AND SENT TO THE O VERHAUL SHOP. SHOP FOUND THE LOWER OIL DUCT LOOSE IN THE ANGLE GEARBOX. THIS WAS A RESULT OF A LOOSE LOCK NUT. THE LO OSE DUCT WAS CAUSING VIBRATION TO BE TRANSFERRED INTO THE BREATHER MANIFOLD TUBE THUS CAUSING IT TO CRACK. THE LOWER OI L DUCT AND HARDWARE WAS REPLACED AND THE ENGINE WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002012400035 20020124 00035 WP 2002 1 24 ABXA010676 1 20020116 A 2750 CONTROL CABLE DOUG DC9 DC914 3022034 WP T/E FLAP LACK OF LUBE A ABXA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 23 925AX 45728 FINAL APPROACH, AIRCRAFT IN A TRIMMED DESCENT ON GLIDESLOPE, FLAPS 30, N1-60 PERCENT ON BOTH ENGINES, SPEED 10 + OVER TA RGET 139. WENT TO FLAP 40, AIRCRAFT ROLLED RIGHT NOTICEABLE, 1 1/2 UNITS LEFT TO TRIM. INSPECTED AILERON AND FLAP CABL E SYSTEM. ALSO INSPECTED AILERON TRIM SYSTEM. NO DEFECTS FOUND. VERIFIED FLAP POSITION INDICATION BY USING FLAP PROTR ACTOR, CHECKED GOOD. LUBRICATED FLAP AND AILERON SYSTEM. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002012400036 20020124 00036 SO 2002 1 24 LR7A02006 1 20020122 A 6120 S24715713A STUD HAMSTD 7338725 LKHEED 382 382G 526414U SO HAMSTD 54H 54H60117 NE NR. 3 PUMP HSG LOOSE A LR7A E ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 AL 03 404LC SE10205 4763 229197 AFTER TAKEOFF FROM DNA, FLIGHT CREW NOTED NR. 3 PROP LOW OIL LIGHT ON. RPM INCREASED TO 106%. SHUTDOWN ACCOMPLISHED IA W QRH. CONTINUED TO OKO AND LANDED WITHOUT INCIDENT.FOUND NR. 3 PROPELLER 1 EA. VALVE HOUSING HOLD DOWN STUD LOOSE IN P UMP HOUSING CAUSING FLUID LOSS. REPLACED STUD IAW HAMILTON SUNSTRAND P5606 CH 3, 2-7, HN61135 AND HN7101. 2 H 7 4 4T A1SO 6 C P906 2002012400043 20020124 00043 WP 2002 1 24 ARWA20020111 1 20020118 A 3260 PROXIMITY SWITCH DOUG DC8 DC862 3021970 WP LT MLG MALFUNCTIONED A ARWA O OTHER N FALSE WARNING AP APPROACH 1 SO 19 8968U 46069 WITH LANDING GEAR HANDLE IN DOWN POSITION ALL THREE GREEN LANDING GEAR LIGHTS CAME ON AND DOOR RED LIGHT STAYED ON AND L ANDING GEAR UNSAFE LIGHT STAYED ON. ALSO, WITH FLAPS AT 35 POSITION UNSAFE WARNING HORN CAME ON. REMOVED AND REPLACED LT DOOR PROXIMITY SWITCH IAW MM 32-60-07, OPS CHECK ON THE GROUND NORMAL IAW MM 32-60-07. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002012400045 20020124 00045 WP 2002 1 24 CALA0200031 1 20020123 A 7830 SKIN DOUG DC9 DC982 3022082 WP #2 ENG T/R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND A 1" CRACK IN #2 ENGINE UPPER THRUST REVERSER OUTER SKIN. TWO DOUBLERS WERE INSTALLED IAW ECRA 7830-010 00. 2 L 7 2 4F A6WE 2002012400046 20020124 00046 WP 2002 1 24 CALA0200032 1 20020123 A 7830 SKIN DOUG DC9 DC982 3022082 WP #1 ENG T/R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND A 1" CRACK IN #1 ENGINE UPPER THRUST REVERSER OUTER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 7830-01000. 2 L 7 2 4F A6WE 2002012400047 20020124 00047 NM 2002 1 24 CALA0200033 1 20020123 A 5754 SKIN BOEING 737 7373T0 1384582 NM #4 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND A 1/2" CRACK IN R/H WING #4 SLAT SKIN LOWER AREA, BELOW ACTUATOR ATTACHMENT TO SLAT. THE CRACKED AREA W AS CUTOUT. REPAIR FILLER AND A SPLICE PLATE WERE INSTALLED IAW SRM 57-43-01, FIGURE 206. 2 L 7 2 4F RT A16WE 2002012400048 20020124 00048 WP 2002 1 24 ARWA20020112 1 20020118 A 7997 WIRE DOUG DC8 DC863F 302198F WP OIL SYSTEM DAMAGED A ARWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 661AV 45969 DURING CLIMB NR 2 ENGINE OIL TEMP INDICATION READ 150. SWAPPED GAUGES FOR TROUBLESHOOTING, NO HELP. AFTER RETARDING NR 2 POWER LEVER, OIL TEMPERATURE DECREASED, ADVANCE POWER LEVER, TEMPERATURE INCREASED. NEVER EXCEEDED THE 15 MINUTES LI MIT. AIRCRAFT RETURNED TO KMIA AND LANDED OVERWEIGHT UNEVENTFUL. REMOVED AND REPLACED NR 2 ENGINE FUEL/OIL COOLER IAW DC8 MM 79-20-2, NO LEAKS NOTED. DURING OPS CHECK FOUND NR 2 OIL TEMP ERRATIC AND OSCILLATING. REPAIRED WIRE IAW MM 20- 50-1 CHECK ELECTRICAL SYSTEM IAW MM 77-5-0 FOUND NORMAL. PERFORMED ENGINE RUN UP OPS CHECK NORMAL IAW MM 71-00. OVERWE IGHT LANDING INSPECTION PERFORMED IAW JC 6372 A-INSPECTION, NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002012400051 20020124 00051 WP 2002 1 24 ARWA20020114 1 20020120 A 2760 SWITCH DOUG DC8 DC863F 302198F WP SPOILER FAILED A ARWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 441J 45988 LINE UP FOR TAKEOFF ADVANCED POWER AND GOT CONFIGURATION TAKEOFF WARNING HORN. AIRCRAFT RETURNED TO BLOCKS. REMOVED AN D REPLACED RT SPOILER SWITCH IAW MM 27-63-01, OPS CHECK NORMAL IAW MM 27-63-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002012400054 20020124 00054 NM 2002 1 24 AWXA200200037 1 20020102 A 5230 6546921U235 CROSSBEAM BOEING 737 7373S3 1384711 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23734 MCN - MAJOR REPAIR - C - DURING C-15 CHECK A CRACK WAS FOUND ON THE VERTICAL LEG OF THE FORWARD CARGO DOOR LOWER OUTER T EE CHORD AFT END BS 487. MAINTENANCE CUTOUT DAMAGED SECTION OF CRACKED TEE CHORD AT BS 487, TRIMMED NEW REPLACEMENT SEC TION OF TEE CHORD, FABRICATED 3 RADIUS FILLERS AND 2 REPAIR ANGLES AND INSTALLED REPAIRS IAW AWA EO 52-31-04. 2 L 7 2 4F RT A16WE 2002061300135 20020613 00135 GL 2002 6 13 AWXA200200041 2 20020116 A 7230 COMPRESSOR BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B1US GL NR 2 ENGINE DAMAGED A AWXA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 WP 28 155AW 23777 720772 WHEN THROTTLES ADVANCED NR 2 ENG EXPERIENCED COMPRESSOR STALL, NR 2 ENG BROUGHT BACK TO IDLE. DECLARED EMERG, ACFT LAND ED W/O INCIDENT. MX PERF GROUND RUN NR 2 ENG, WHEN THROTTLE RETARDED ENG EXPERIENCED COMPRESSOR STALL. ENG SHUTDOWN, B ORESCOPE PERF. BORESCOPE REVEALED DAMAGE TO HIGH STAGE COMPRESSOR SECTION, PIECES OF 6, 7, 8, 9 BLADES MISSING. NUMERO US BLADES WITH CURLED TIPS. NR 2 ENG REMOVED. TEARDOWN OF ENG REVEALED MINOR HPC BLADE TIP RUB STAGES 1-4 BLADES, HEAV Y BLADE TIP RUB STAGE 5, HEAVY AIRFOIL DAMAGE TO BLADES STAGES 6-9. EXCESSIVE RUB 4-9 SPOOL BASE MAT IN AREA OF 6TH STA GE BLADES, DUE TO MACHINING CAUSED BY LIBERATED STATIONARY INTERSTAGE AIRSEALS WITHIN REAR COMPRESSOR CASES. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012400056 20020124 00056 EU 2002 1 24 AWXA200200042 1 20020116 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 637AW 099 SAN - EEL - C - DURING TEST OF EMERGENCY EXIT LIGHTING ALL OF THE FWD AND AFT SECTION EMERGENCY EXIT LIGHTS WERE FOUND T O BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS 10WL (ZONE 221) AND 13WL (ZONE 263) IAW AMM 33-51-38, OPERATIO NAL CHECK WAS GOOD IAW T/C F1C33301. 2 L 7 2 4F RT A28NM 2002012400057 20020124 00057 EU 2002 1 24 CHQ00093 1 20020117 A 7600 LEVER SAAB SF340 SF340A 7850100 EU COCKPIT BROKEN A CHQA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 118 118 BROKEN CONDITION LEVER. PERFORMED LSC1 AND THEN FERRIED AIRCRAFT TO IND TO FIX CONDITION LEVER. 2 L 7 2 4T RT A52EU 2002012400058 20020124 00058 EU 2002 1 24 DHL2002367001 1 20020119 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 367DH 265 SMOKE ALARM MAIN CABIN. COOLED A/C DOWN, SMOKE DETECTION CHECKS GOOD IAW M/M 26-14-00. 2 L 7 2 4F RT A35EU 2002012400060 20020124 00060 EU 2002 1 24 MALA020111 1 20020113 A 3010 B-NUT SAAB SF340 SF340A 7850100 EU DEICE SYSTEM LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 76XJ 340A076 DURING FLIGHT 2996, IN LIGHT ICE AT 16,000 FT AT 18'C WITH BOOTS IN CONTINUOUS, GOT TIMER LIGHT RAN QRH, TRIED BOOTS IN MANUAL, COULD NOT GET WITH O/B TO INFLATE, ROLLER WAS AROUND 65 PERCENT. AIR TURNBACK TO MSP. MAINTENANCE WHILE CLEANI NG DISTRIBUTOR VALVE FOUND AIR LEAKING FROM T-FITTING B-NUT ON RT SIDE NACELLE. COMP CLEANED AND TIGHTENED B-NUT LEAK, OPS CHECK GOOD. REF 30-10-00. 2 L 7 2 4T RT A52EU 2002012400074 20020124 00074 EU 2002 1 24 MALA020117 1 20020105 A 5346 HC253H0056006 MOUNT BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C2-CHECK IN CVG, FWD GALLEY MOUNT HAS SERVICE CORROSION ON RT SIDE. MAINTENANCE INSTALLED NEW SERVICEABLE PART P /N HC253H0056-006 IAW AMM 20-10-19. 2 H 7 4 4F RT A49EU 2002012400079 20020124 00079 EU 2002 1 24 MALA020120 1 20020102 A 3350 61004789 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 107XJ 340A107 DURING TURNBACK INSPECTION NOTED EMERGENCY LIGHT POWER SUPPLY 22LN VOLTAGE TO BE LOW. MAINTENANCE REMOVED AND REPLACED BATTERY PAC ON EMERGENCY LIGHTING POWER SUPPLY 22LN WITH A SERVICEABLE BATTERY PACK IAW SF3 AMM 33-50-10. OPS CHECKS GO OD AT THIS TIME. P/N 61-0478-9, S/N OFF 076A, P/N ON 6100478-9, S/N ON 9801228. 2 L 7 2 4T RT A52EU 2002012400080 20020124 00080 SO 2002 1 24 2002F00038 2 20020117 A 8530 654724BP PISTON CESSNA 421 421C 2076016 CE CONT O520 GTSIO520N 17032 SO ENGINE FAILED E A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 07 763CA 1025 421C1019 292066R TRANSISITIONING FROM TAKE-OFF TO CLIMB PHASE OF FLIGHT, AFTER REDUCING POWER NR 1 ENGINE SHUTDOWN. PILOT FEATHERED PROP AND MADE UNEVENTFUL LANDING. REMOVAL OF NR 5 CYLINDER REVEALED SEVERE DAMAGE TO THE TOP OF THE PISTON, WITH BROKEN RINGS . VALVE WERE REALITIVELY INTACT. FURTHER INSPECTION REVEALED DAMAGE TO ALL PISTONS, THOUGH NOT AS SEVERE. 1 L 7 2 3O 3 O A7CE E7CE 2002012400081 20020124 00081 EU 2002 1 24 MALA020121 1 20020115 A 2751 SENSOR BAC 146 AVRO146RJ85A 1500097 EU LT FLAP FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 507XJ E2316 AFTER FLAP RETRACTION ON FLIGHT 3600 FTC, NO CAT 3 LAND, AND WINDSHEAR INOP. LIGHTS STARTED FLASHING RANDOMLY AND CONTI NUOUSLY, AP STILL UNABLE. AFTER SELECTION OF FLAPS 18 FOR LAND ALL LIGHT OUT, THEN STARTED AGAIN AFTER FLAP RETRACTION AND ON GROUND. MAINTENANCE REPLACED LT FLAP DUAL POSITION SENSOR, REFER 409 NR 082583 FOR DETAILS. 2 H 7 4 4F RT A49EU 2002012400084 20020124 00084 EU 2002 1 24 MALA020122 1 20020116 A 3240 HP14081004 CONTROL VALVE SAAB SF340 SF340A 7850100 EU BRAKE SYS FAILED A MALA O OTHER P NO WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 68XJ 340A068 BRAKES FAILED ON TAXI INTO DTW ON FLIGHT 2869. STOPPED A/C WITH REVERSE ACCUMULATOR PRESSURE BRAKE ACCUMULATORS 2400-25 00 NORMAL. SET PB AND WENT TO OVERRIDE ON HYDRAULIC PUMP SYSTEM, PRESSURE WENT UP TO 3000 WHEN THE FAILURE OCCURRED. B OTH CAPT AND F/O'S BRAKE HAD NO EFFECT AFTER BOOSTING THE SYSTEM PRESSURE, CHECKED THE BRAKES AGAIN AND BRAKES WORKED ON BOTH SIDES. MAINTENANCE REPLACED BRAKE CONTROL VALVE P/N HP1408100-4 REFER 409 NR 068802 FOR DETAILS. ALL CHECKS GOO D AT THIS TIME IAW SF340 AMM. 2 L 7 2 4T RT A52EU 2002012400098 20020124 00098 EU 2002 1 24 MALA020123 1 20020116 A 7930 CONNECTOR SAAB SF340 340B 7860101 EU CHIP DETECTOR CONTAMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 402XJ 340B402 ON CLIMBOUT DURING FLIGHT 2826, RT CHIP DETECTOR CAUTION LIGHT ILLUMINATED ALL OTHER INDICATIONS NORMAL. AIR TURNBACK T O DTW. MAINTENANCE CLEANED AND RESECURED CHIP DETECTOR CANNON PLUG FROM MOISTURE, RAN A/C FOR 10 MINUTES. ALL CHECK GO OD ON THE GROUND. 2 L 7 2 4T RT A52EU 2002012400105 20020124 00105 NM 2002 1 24 0200165504 1 20020101 A 5315 SUPPORT BOEING 757 757251 1384970 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 504US 23193 During "H" check found corrosion on seat track support at BS 400 RBL 25. Repaired per EA 55-187555. 2 L 7 2 4F RT A2NM 2002012400106 20020124 00106 EA 2002 1 24 COMA0260059 1 20020122 A 3230 7455021 SELECTOR KNOB CNDAIR CL600 CL6002B19 1900309 EA INST PANEL MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 408CA 126 126 7440 FLIGHT 5471 LANDING GEAR DISAGREE WARNING, HANDLE SELECTED UP LANDING GEAR DID NOT RETRACT.REPLACED THE LANDING GEAR CON TROL HANDLE. 2 L 7 2 4F RT A21EA 2002012400107 20020124 00107 EA 2002 1 24 COMA0260060 1 20020121 A 3220 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 912CA 7011 FLIGHT 6028 LANDING GEAR DISAGREE WARNING. NLG DID NOT RETRACT.CLEANED AND LUBED NLG RETRACT CHECKS WERE SATISFACTORY. 2 L 7 2 4F RT A21EA 2002012400108 20020124 00108 NE 2002 1 24 MALA020126 2 20020119 A 7320 219333010 HMA BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 1 ENGINE MALFUNCTIONED A MALA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 15 509XJ E2321 DURING FLIGHT 3557, NR 1 ENGINE SHUTDOWN INFLIGHT. NO ENGINE DAMAGE SUSPECTED OR OBSERVED ON POST FLIGHT INSPECTION. I NSPECTED ENGINE FOR DAMAGE, NONE NOTED. DOWNLOADED FADAMS. TESTED OVERSPEED PICK UPS AT J13 J14-TEST GOOD. REPLACED H MA P/N 2-193-330-10, S/N OFF 99/AGU811, S/N ON 97AGU592. REPLACED OVERSPEED CONTROLLER P/N 2-313-007-01, S/N OFF 1197, S/N ON 190. GROUND RAN ENGINE AT ALL SETTINGS, CHECKED GOOD. NO LEAKS NOTED, OVERSPEED FUNCTIONS GOOD. REF AMM 76-20- 01. 2 H 7 4 4F 4 F RT A49EU E6NE 2002012400109 20020124 00109 SO 2002 1 24 C2XA02CL017 1 20020121 A 4900 WF336540 FILTER EMB 145 EMB145ER 3260211 SO TAIL LEAKING A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 14945 145049 CLE FLIGHT# 3130 THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN AND COCKPIT AFTER APU START.MAINTENACE INSPECTED AND PLACED ON MEL.ON 1/22/01 MAINTENANCE REPLACED THE APU FUEL FILTER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASE D FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002012400110 20020124 00110 NM 2002 1 24 PCAA0201012 1 20020115 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT EMERGENCY FLOOR LIGHT STRIP ON LEFT SIDE FORWARD SECTION AND PAX DOOR SIGN FOUND TO BE OUT. AFTER TROUBLESHOOTING FOUND BROKEN WIRES ON FLOOR STRIP AND BLOWN FUSES IN BATTERY PACK. WIRES REPAIRED AND FUSES REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002012400111 20020124 00111 WP 2002 1 24 ZW0A0201001 1 20020122 A 2780 3916322613 CABLE DOUG DC9 DC982 3022082 WP A ZW0A K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 CE 13 951U 49245 FOUND FLAP BUS TRAVEL CABLE BROKEN. REPLACED THE CABLE. CHECK-C 8-25-01 STL. ---CLOSED--- 2 L 7 2 4F A6WE 2002012400112 20020124 00112 WP 2002 1 24 ZW0A0201002 1 20020122 A 2780 3916322613 CABLE DOUG DC9 DC982 3022082 WP A ZW0A K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 CE 13 951U 49245 FOUND FLAP BUS TRAVEL CABLE BROKEN. REPLACED THE CABLE. CHECK-C 8-25-01 STL. --CLOSED-- 2 L 7 2 4F A6WE 2002012400113 20020124 00113 NM 2002 1 24 ZW0A0201003 1 20020118 A 3350 80741 LAMP BOEING 767 7673Y0 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 640TW 25411 CABIN EGRESS LIGHT INOPERATIVE. REPLACED THE LAMP. CHECK-C 11-9-01 LAX. --CLOSED-- 2 L 7 2 4F RT A1NM 2002012500002 20020125 00002 CE 2002 1 25 2002F00044 1 20020122 A 5740 NAS464P14A71 ATTACH BOLT CESSNA 500 500CESSNA 2076602 CE WING ROOT WORN B D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 11 913RC 9476 174 5000059 RIGHT FORWARD LOWER WING ATTACH BOLT WORN WHICH ALLOWED MOVEMENT BETWEEN RIGHT LOWER WING AND FUSELAGE ATTACH FITTINGS. THIS CONDITION WAS DETECTED AUDIBLY WHILE TAXING WITH A FULL FUEL LOAD. 1 L 7 2 4F A22CE 2002012500007 20020125 00007 WP 2002 1 25 0200129873 1 20020114 A 5310 BRACKET DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 782NC 48107 During an Mck in ATL a crack was found at the station 69 bracket (x=+/- 10). Repaired per EA 98-185453. 2 L 7 2 4F RT A6WE 2002012500008 20020125 00008 WP 2002 1 25 0200139946 1 20020109 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8926E 45863 DURING HCK IN ATL, A CRACK WAS FOUND IN THE UPPER VERTICLE FLANGE OF THE STATION 237 FLOORBEAM AT X=6. REPAIRED PER EA 9 9-185447. 2 L 7 2 4F A6WE 2002012500009 20020125 00009 WP 2002 1 25 0200149946 1 20020108 A 5720 SKIN DOUG DC9 DC931 3022065 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8926E 45863 During HCK in ATL, corrosion was found on the R/H wing upper skin doubler flange attachment holes for the fuel access do or. Repaired per EA 99-185451. 2 L 7 2 4F A6WE 2002012500010 20020125 00010 WP 2002 1 25 0200159946 1 20020114 A 5310 WEB DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8926E 45863 During Hck in ATL, A crack was found in the lower outboard corner of the diagonal web in the L/H engine pylon just forwa rd of the rear spar. Repaired per EA 99-185474. 2 L 7 2 4F A6WE 2002012500014 20020125 00014 WP 2002 1 25 0200099603 1 20020108 A 5710 PANEL DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 603NW 47101 During HCK in ATL a crack was found in the aft flange of the right trapezoidal panel. Repair accomplished in accordance with EA 96-185424. 2 L 7 2 4F A6WE 2002012500015 20020125 00015 WP 2002 1 25 0200109603 1 20020114 A 5410 RIB DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 603NW 47101 During HCK in ATL the lower cap of the pylon closong rib YN165 was found cracked. Repaired per EA 96-185454. 2 L 7 2 4F A6WE 2002012500016 20020125 00016 NM 2002 1 25 SWAA020149 1 20020121 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 1006, STR 7L. REPAIRED STR PER SRM AND SWA T1. 2 L 7 2 4F RT A16WE 2002012500017 20020125 00017 NM 2002 1 25 SWAA020154 1 20020122 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKINS CRACKED (4 EA) AT STR 4R, BS'S 460, 500A, 500B AND 727E. REPAIRED SKINS PER SWA RA. 2 L 7 2 4F RT A16WE 2002012500018 20020125 00018 NM 2002 1 25 SWAA020161 1 20020123 A 5312 6545409 WEB BOEING 737 7373H4 1384600 NM RT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, RBL 41. REPAIRED WEB PER SRM AND SWA T1. 2 L 7 2 4F RT A16WE 2002012500019 20020125 00019 NM 2002 1 25 SWAA020164 1 20020122 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10R, BS'S 727C, 750 AND 520. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 2002012500020 20020125 00020 NM 2002 1 25 SWAA020165 1 20020122 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, ABOVE STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002012500022 20020125 00022 NM 2002 1 25 SWAA020159 1 20020123 A 5310 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 DURING SCHEDULED 1/2D CHECK, FOUND TIE CLIP CRACKED AT BS 927, 27L. REMOVED AND REPLACED TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002012500025 20020125 00025 NM 2002 1 25 AWXA200200052 1 20020108 A 5330 6545776100 SKIN BOEING 737 737301 1384611 NM FUSELAGE BULGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - C - DURING INSPECTION SKIN WAS FOUND TO HAVE BULGE AT BS 847 BETWEEN STR 27R AND 26R. MAINTENANCE CUTOUT BULGED AREA OF SKIN AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS. FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REPAIRS IAW B737-300 SRM 53-00-01 FIG 201, SHEET 1-3, SRM 53-60-01 FIG 1, SHEETS 7 & 8. 2 L 7 2 4F RT A16WE 2002012500027 20020125 00027 NM 2002 1 25 AWXA200200058 1 20020108 A 5320 6546568519 STIFFENER BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - C - DURING INSPECTION MAINTENANCE FOUND CORROSION ON AFT PRESSURE BULKHEAD STIFFENERS AT BS 1016, B L 0. MAINTENANCE REMOVED CORROSION FROM AFT PRESSURE BULKHEAD STIFFENERS AT BS 1016 AND FOUND MATERIAL LOSS OUT OF LIMI TS. REMOVED SECTION OF DAMAGED STIFFENERS AND FABRICATED REPAIR STIFFENERS AND INSTALLED REPAIRS IAW AWA ER 03-5312-020 11-ES1. 2 L 7 2 4F RT A16WE 2002012500031 20020125 00031 NM 2002 1 25 AWXA200200062 1 20020118 A 3350 1012621 LIGHT BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 LAS - EEL - C - DURING INSPECTION EMERGENCY EXIT LIGHT WAS FOUND BROKEN AT LT OVERWING EXIT SEATS. MAINTENANCE REPLACED THE LT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY IAW 33-51-11, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002012500032 20020125 00032 NM 2002 1 25 AWXA200200063 1 20020120 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 150AW 23218 LAS - EEL - C - EMERGENCY EXIT LAMP AT ROW 7 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSE MBLY SEAT ROW 7 LT, OPERATIONAL TEST WAS GOOD IAW BMM 33-51-02. 2 L 7 2 4F RT A16WE 2002012500033 20020125 00033 NM 2002 1 25 AWXA200200064 1 20020120 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM CARGO BAY DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 181AW 22648 PHX - EEL - C - DURING INSPECTION THE RT EXTERIOR OVERWING AND LOWER FUSELAGE EMERGENCY EXIT LIGHTS WERE FOUND TO BE INO PERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERY PACK IN THE AFT CARGO COMPARTMENT IAW BMM 3 3-51-31, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002012500034 20020125 00034 NM 2002 1 25 AWXA200200066 1 20020121 A 3350 20121 CHARGER BOEING 737 737317 138447P NM CABIN DEFECTIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 YVR - EEL - C - DURING C-13 CHECK THE AFT, AFT LT, AND AFT RT BATTERY CHARGERS DID NOT REACH 300 MILLI AMPS WHEN TESTED. MAINTENANCE REMOVED AND REPLACED THE AFT, AFT LT AND AFT RT BATTERY CHARGER IAW BMM 33-51-51 PG 206 AND 207. OPERATIO NAL TEST WAS GOOD PER W/C A1C33006. 2 L 7 2 4F RT A16WE 2002012500035 20020125 00035 NM 2002 1 25 AWXA200200067 1 20020121 A 3350 BR964412 COVER BOEING 737 737317 138447P NM CABIN WRONG PART A AWXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 28 331AW 23747 YVR - EEL - C - DURING C-13 CHECK EMERGENCY EXIT LIGHT LENS COVERS ON SEATS AT ROWS 10 & 11 WERE FOUND TO BE THE WRONG C OLOR. MAINTENANCE REMOVED THE WHITE EMERGENCY LIGHT LENS COVERS AND REPLACED THEM WITH RED EMERGENCY LIGHT LENS COVERS AS PER AWA GENERAL MAINTENANCE PRACTICES MPPM 9-1,8. 2 L 7 2 4F RT A16WE 2002012500036 20020125 00036 EA 2002 1 25 COMA0260061 1 20020123 A 2410 IDG CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 01 807CA 7364 FLIGHT 5792 - GENERATOR 2 CAUTION MESSAGE DURING T/O.SERVICED IDG WITH OIL, SYSTEM OPERATION NORMAL. 2 L 7 2 4F RT A21EA 2002012500037 20020125 00037 NM 2002 1 25 CALA0200035 1 20020124 A 5330 DOUBLER BOEING 737 7373T0 1384582 NM #2 VHF ANT. CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND A 6" CRACK IN INTERIOR DOUBLER ON #2 VHF ANTENNA AT FWD CARGO COMPARTMENT. THE DOUBLER WAS REPLACED IAW SRM 51-20-01, 51-20-05, 51-40-02, AND 51-40-08. 2 L 7 2 4F RT A16WE 2002012500038 20020125 00038 NM 2002 1 25 CALA0200036 1 20020124 A 5311 FRAME BOEING 737 7373T0 1384582 NM STA 727E CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND BELT FRAME CORRODED BELOW FLOOR OF AFT BAGGAGE BIN AT STA 727E. REPAIRED IAW SRM 53-00-07, FIGURE 203, SHEETS 1-3. 2 L 7 2 4F RT A16WE 2002012500042 20020125 00042 NM 2002 1 25 CALA0200029 1 20020121 A 3220 162A21153 LINK BOEING 737 737824 13844BZ NM NLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24212 12191 28772 INSPECTION FOUND THE NLG AFT LOCK LINK CRACKED DURING PSV INSPECTION. THE LOCK LINK WAS REMOVED AND REPLACED IAW MM 32- 33-51, 401-801. AN ADJUSTMENT/TEST OF NLG LOCK SENSOR WAS PERFORMED IAW MM 32-61-41, PAGE 501. AN FCD IS BEING ISSUED TO PERFORM A DETAILED VISUAL INSPECTION OF THE AFT LOCK LINK ON THE B737-700/800 FLEET. 2 L 7 2 4F RT A16WE 2002012500044 20020125 00044 NE 2002 1 25 CALA0200030 2 20020122 A 7261 SEAL BOEING 737 737524 1384721 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE LEAKING A CALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 37615 27328 857945 SMOKE ENTERED THE COCKPIT AND CABIN ON TAKEOFF FROM EWR. THE APU WAS RUNNING AND BOTH ENGINE BLEEDS WERE ON WITH BOTH P ACKS OPERATING. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. BOTH ENGINES WERE BORESCOPED. MAIN TENANCE FOUND THE AIR/OIL SEAL LEAKING AND OIL HAD ENTERED THE NR 2 ENGINE COMPRESSOR. THE NR 2 ENGINE WAS REMOVED AND REPLACED. A DUCT BURNOUT WAS PERFORMED AND BOTH PACK COALESCER BAGS WERE REMOVED AND REPLACED. A HIGH POWER ENGINE RUN WAS PERFORMED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002012500045 20020125 00045 EU 2002 1 25 CHQ000100 1 20020120 A 3412 INDICATOR SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 150 150 OAT FAILED AFTER GEAR RETRACTION AND RT BLEED CLOSED LIGHT ON. RETURNED TO FIELD. 2 L 7 2 4T RT A52EU 2002012500048 20020125 00048 SO 2002 1 25 CHQ00094 1 20020117 A 2760 CONTROL UNIT EMB 145 EMB145 3260210 SO SPOILER FAILED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 317 145535 SPOILER FAIL MESSAGE DURING T/O ROLL, SPOILER CONTROL UNIT REMOVED AND REPLACED WITH A NEW UNIT. OPS CHECKED SERVICEABL E HIGH SPEED TAXI, CHECK C/O. 2 L 7 2 4F RT T00011AT 2002012500050 20020125 00050 EU 2002 1 25 CHQ00095 1 20020117 A 6120 COMPUTER SAAB SF340 SF340A 7850100 EU ROTOL R389 R3894123F25 NE E/E BAY MALFUNCTIONED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 123 123 DRG855983 AUTO COARSEN PROBLEM CAUSING ABORTED TAKEOFF. PILOT ABORTED T/O AND PERFORMED RUN UP AUTO COARSEN, CHECKED GOOD. 2 L 7 2 4T RT A52EU 6 C P30NE 2002012500052 20020125 00052 NE 2002 1 25 CHQ00096 2 20020119 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT FAILED A CHQA C F ABORTED TAKEOFF ACTIVATE FIRE EXT. J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 11 148 148 RT ENGINE FAILED DURING T/O, AT 100 KNTS TEMP WENT TO 1000 DEG, SMOKE WENT EVERYWHERE. PULLED FIRE HANDLE AND BLEW 1 BO TTLE. REMOVED AND REPLACED RT ENGINE, FIRE BOTTLE, AND SQUIB. ALL OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002012500053 20020125 00053 WP 2002 1 25 MWEA020061 1 20020124 A 5330 5911412191 SKIN DOUG DC9 DC932 3022066 WP STATION 237 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FUSELAGE SKIN DAMAGED AT APPROXIMATLEY STATION 237 LONGERON 30. -- REMOVED DAMAGE INSTALL FLUSH INTERNAL REPAIR PER SR M 53-04 FIGURE 38 SHEET 31 TELEX MWX.MKE-02-00001H. 2 L 7 2 4F A6WE 2002012500054 20020125 00054 SO 2002 1 25 CHQ00099 1 20020120 A 2400 SMOKE EMB 145 EMB145 3260210 SO COCKPIT DETECTED A CHQA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 11 265 145226 PILOT REPORTS SMOKE IN COCKPIT FROM F/O'S RELAY BOX. 2 L 7 2 4F RT T00011AT 2002012500055 20020125 00055 NM 2002 1 25 DHL2002745001 1 20020123 A 2612 FIRE WARNING BOEING 727 727224 1384076 NM COCKPIT MALFUNCTIONED A DHLA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SO 01 745DH 20665 LOWER AFT FIRE LIGHT AND BELL CAME ON WITH MX DISPLAY SHOWING AFT. PERFORMED OPS TEST, SYS NORMAL PER 26-16-00 B727MM. 2 L 7 3 4F A3WE 2002012500057 20020125 00057 WP 2002 1 25 DHL2002807002 1 20020122 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 4 ENGINE MALFUNCTIONED A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 807DH 45990 NR 4 ENGINE FIRE LOOP-B SYSTEM SHORT CIRCUIT LIGHT IS ON. COULD NOT DUPLICATE. SYS OPS CHECKED OK PER M/M 26-00 PG 201 . 2 L 7 4 4F RT 4A25 2002012500058 20020125 00058 NM 2002 1 25 HNAA0200005 1 20020117 A 2930 AE776L0804S CONNECTOR DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS INTERMITTENT A HNAA K NONE N FALSE WARNING CR CRUISE 1 EA 07 926HA 114 NUMBER 2 ISOLATION VALVE CAUTION LIGHT ILLUMINATED IN FLIGHT, QUANTITY AND PRESSURE GOOD. REMOVED CANNON PLUG AND CLEAN ED CONTACTS. BLED NUMBER 2 HYDRAULIC RESERVOIR AND SERVICED. ON THE NEXT FLIGHT, NUMBER 2 ISOLATION VALVE CAUTION LIGH T ILLUMINATED. NUMBER 2 SYSTEM QUANTITY AND PRESSURE REMAINED NORMAL. FOUND CANNON PLUG ON RESERVOIR LEVEL SWITCH INTE RMITTENT. REPLACED CANNON PLUG. 2 H 7 2 4T RT A13NM 2002012500059 20020125 00059 EA 2002 1 25 HNAA0200007 1 20020119 A 2913 570347 PUMP DHAV DHC8 DHC8311 1386006 EA NR 1 ENGINE FAILED A HNAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 07 327EN 261 NUMBER 1 HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED, QUANTITY GOOD SYSTEM PRESSURE 3000 PSI WITH STANDBY PUMP OFF. NUMBER 1 SYSTEM FAILED IN FLIGHT, SYSTEM QUANTITY GOOD. 2 H 7 2 4T RT A13NM 2002012500060 20020125 00060 EU 2002 1 25 MALA020125 1 20020118 A 2440 MS35061 RECEPTACLE SAAB SF340 340B 7860101 EU EXTERNAL POWER BURNED A MALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 408XJ 340B408 DURING FLIGHT 3329, ARC AT GPU PLUG UPON START UP CAUSED FIRE ON PLUG AND RECEPTACLE. NR 2 ENGINE WAS BEING STARTED AND CREW SHUTDOWN ENGINE WITHOUT FURTHER INCIDENT. PAX CABIN WAS EVACUATED AND FLIGHT CREW FIRE EXTINGUISHER USED TO PUT O UT FIRE. MAINTENANCE UPON INSPECTION NOTED MINOR DAMAGE ON EXTERIOR OF GPU RECEPTACLE WITH NO DAMAGE EXTENDING UPSTREAM . REMOVED AND REPLACED GPU RECEPTACLE IAW SAAB MM 244305 PN MS3506-1. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2002012500061 20020125 00061 NM 2002 1 25 MNAA0200006 1 20020120 A 2520 1010815M PSU DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 926HA 114 PSU AT ROW 3DF IS INOP, STRANGE SMELL IN CABIN. DEACTIVATED PSU AT 3DF IAW MP/P VOL 2, NO FURTHER ODOR NOTED IN CABIN. PLACED PSU ON MEL. 2 H 7 2 4T RT A13NM 2002012500062 20020125 00062 2002 1 25 MWEA020055 4 20020119 A 3417 HG280D80 ADC DOUG DC9 DC981 3022081 WP RIGHT FAULTY A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 814ME 48010 FIRST OFFICERS ALTIMETER FLUCTUATED ABOUT 400 FEET. REPLACED NR 2 CADC. 2 L 7 2 4F A6WE 2002012500063 20020125 00063 NE 2002 1 25 NACA20020002 2 20020122 A 8530 356993 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE NR 2 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 99330 526 526 43576 37244 NR 2 ENGINE RAPID LOSS OF BMEP, ROUGH RUNNING. REPLACED NR 2 CYLINDER. 2 L 7 4 4R 4 R 6A3 5E8 2002012500065 20020125 00065 NM 2002 1 25 PCAA0201014 1 20020116 A 5610 NP15790111 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM COCKPIT CRACKED A PCAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 13 817EX 1773 191 LGA-MDT FLIGHT 3829. CREW REPORTED WHILE IN CRUISE FLIGHT AT 14,000 FT OUTER PANEL OF CAPTAINS WINDSHIELD SHATTERED WHI LE WINDSHIELD HEAT WAS ON. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED AT NEAREST SUITABLE AIRPORT WHICH WAS ABE. MAINTE NANCE REPLACED PILOTS WINDSHIELD IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 56-10-11. OPERATIONAL CHECK O F WINDSHIELD HEAT GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002012500067 20020125 00067 EU 2002 1 25 PNSA020103 1 20020117 A 2612 1734362450 PROBE SAAB SF340 340B 7860101 EU RT ENGINE DEFECTIVE A PNSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 695PA 1446 340B310 DEPARTED AKN FOR CDB CLIMBING THRU 3000 FEET, RIGHT TAIL PIPE HOT LIGHT ILLUMINATED. RT ENGINE POWER REDUCED, BLEED AIR SHUT OFF, LIGHT REMAINED ON. ENGINE WAS NOT SHUTDOWN PER EMERGENCY CHECKLIST DUE TO ICING CONDITIONS. COPILOT VISUALL Y CONFIRMED NO INDICATION OF FIRE FROM CABIN AND EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO AKN WITHOUT INCIDENT. LINE MAINTENANCE INSPECTED AIRCRAFT AND AIRCRAFT WAS FERRIED TO ANC MAINTENANCE BASE WHERE TWO FIRE DETECTOR PROBES WERE FOUND CLOSING EARLY. THESE PROBES ARE CHECKED EACH 6000 HOURS PER MRB TASK 26-12-01. 2 L 7 2 4T RT A52EU 2002012500116 20020125 00116 NM 2002 1 25 QXEA0200074 1 20020121 A 2430 23088002A GENERATOR DHAV DHC8 DHC8102 2809003 NM ENGINE INOPERATIVE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 830PH 575 359 314 SEA-#1 DC GENERATOR CAUTION LIGHT ILLUMINATED ON TAXI FOR TAKEOFF. RAN EMERGENCY CHECK LIST. REMOVED AND REPLACED #1 DC GENERATOR AND GCU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002012500117 20020125 00117 NM 2002 1 25 QXEA0200076 1 20020123 A 3230 471515 HARNESS BOMBDR DHC8 DHC8401 NM Zone 700 INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 400QX 4030 SEA-AFTER TAKEOFF, GEAR WOULD NOT RETRACT. TRIED THREE CYCLES WITHOUT SUCCESS.RETURNED TO FIELD, ACCOMPLISHED UNEVENTFUL LANDING. REMOVED AND REPLACED WOW #2 HARNESS. C/W LANDING GEAR OPERATIONAL CHECK. LANDING GEAR RETRACTION AND EXTENSION OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002012500123 20020125 00123 SO 2002 1 25 C2XA02BT002 1 20020124 A 5610 163500111 WINDSHIELD EMB 145 EMB145LR 3260212 SO FUSELAGE FAULTY A C2XA O OTHER Z SIGNIFICANT FAILURE REPORT CR CRUISE 1 SW 27 13997 145298 EWR---CO3395, CREW REPORTED, "CAPTAINS WINDSHIELD CRACKED IN FLIGHT" DECLARED EMERGENCY; AIRCRAFT LANDED UNEVENTFULLY. M AINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD I/A/W EMB145 MM 56-10-01. OPS. CHECKED AND HEAT CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2002013000025 20020130 00025 EU 2002 1 30 SABA020010 1 20020125 A 3350 311701 BATTERY PACK BAG JETSTM JETSTM3201 1500217 EU CABIN DISCHARGED A SABA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 33 965AE 965 AIRCRAFT 965 ON FLIGHT 5222 FROM CLT TO LEX; DURING PREFLIGHT IN CHARLOTTE, PILOT FOUND THE EMERGENCY WOULD NOT TEST. M AINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACKS. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4T RT A56EU 2002012500127 20020125 00127 EU 2002 1 25 RAIA00201027 1 20020122 A 2460 A2105F PDU JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 556HK 9772 245 41073 5587-STL- RIGHT BATTERY ANNUNCIATOR LIGHT ILLUMINATED DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE POWER DISTRIBUTI ON UNIT - OPS CK OK. 2 L 7 2 4T RT A41NM 2002012500128 20020125 00128 EU 2002 1 25 RAIA00201028 1 20020122 A 7930 56774098010 GAUGE AEROSP ATR72 ATR72202 8680940 EU INOPERATIVE A RAIA D RETURN TO BLOCK C F.O.D. TX TAXI/GRND HDL 1 CE 03 722TE 19090 16091 220 5621-STL- LEFT ENGINE OIL TEMPERATURE GAUGE INOP DURING TAXI. MAINTENANCE REMOVED AND REPLACED OIL TEMPERATURE INDICATOR . OPS CK OK 2 H 7 2 4T RT A53EU 2002012500129 20020125 00129 WP 2002 1 25 MWEA020056 1 20020123 A 5310 99118435 FRAME DOUG DC9 DC932 3022066 WP STATION 1168 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 CANTED FRAME AT STATION 1168 HAS A CHAFED AREA ON LOWER AFT SIDE AT 7 O'CLOCK POSITION. -- FABRICATED AND INSTALLED RE PAIR DOUBLERS. 2 L 7 2 4F A6WE 2002012500130 20020125 00130 WP 2002 1 25 MWEA020059 1 20020123 A 5230 591014119 PAN DOUG DC9 DC932 3022066 WP FWD CARGO DR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD CARGO DOOR INNER PAN IS CRACKED BY THE AFT DOOR HINGE LOWER FLANGE. -- FABRICATED AND INSTALLED REPAIR DOUBLER . 2 L 7 2 4F A6WE 2002012500136 20020125 00136 NM 2002 1 25 0200176718 1 20020122 A 2432 401767 BATTERY BOEING 747 747251F 1384898 NM OVERHEATED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 618US 21122 DURING FLIGHT, A STRONG ELECTRICAL FUME EMITTED IN THE COCKPIT. FUME SMELL DID NOT DISSIPATE AFTER COMPLYING WITH THE EM ERGENCY PROCEDURES AND THE COM. CREW DIVERTED TO NRT, DECLARED AN EMERGENCY, AND DUMPED 100,000 LBS OF FUEL. DURING LAND ING WHILE IN REVERSE THRUST, THE NBR 3 ENGINE COMPRESSOR STALLED AND OVERTEMPED. AIRCRAFT TAXIED TO THE GATE WITHOUT FUR THER INCIDENT. REPLACED THE MAIN BATTERY, BATTERY CHARGER, AND THE NBR 3 ENGINE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002012500140 20020125 00140 WP 2002 1 25 ABXA010682 1 20020124 A 5300 2024T3 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 DURING LINE MAINTENANCE VISIT, FUSELAGE SKIN WAS CRACKED AT THE FORWARD ENTRY DOOR, UPPER AFT CORNER, STATION 218, LONGE RON 7 LEFT. REPAIRED FUSELAGE SKIN IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002012500141 20020125 00141 NM 2002 1 25 AWXA200200069 1 20020112 A 5315 6561381 SUPPORT BOEING 737 737317 138447P NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 YVR - MAJOR REPAIR - "C" - DURING C-13 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT AT BS 992, LBL 24. MA INTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED SUPPORT AT BS 992, LBL 24; FABRICATED NEW ATT ACH ANGLE AND INSTALLED REPAIR IAW B737-300 SRM 51-40-2. 2 L 7 2 4F RT A16WE 2002012500142 20020125 00142 NM 2002 1 25 AWXA200200070 1 20020108 A 5315 6546812189 SUPPORT BOEING 737 737317 138447P NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 YVR - MAJOR REPAIR - "C" - DURING C-13 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT AT BS 986 TO BS 1006, LBL 38. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED SUPPORT AT BS 986 TO 1006, LBL 38; FABRICATED NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW B737-300 SRM 51-20-01, PG 10, AND DWG 65-46812. 2 L 7 2 4F RT A16WE 2002012500143 20020125 00143 NM 2002 1 25 AWXA200200071 1 20020105 A 5315 6546811 SUPPORT BOEING 737 737317 138447P NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 YVR - MAJOR REPAIR - "C" - DURING C-13 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT AT BS 986, RBL 24 TO LBL 24. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED SUPPORT AT BS 986, RBL 24 TO LBL 24 ; FABRICATED NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW B737-300 SRM 51-00-51, FIG. 202, PG. 207. 2 L 7 2 4F RT A16WE 2002012500144 20020125 00144 NM 2002 1 25 AWXA200200072 1 20020105 A 5315 6546810 SUPPORT BOEING 737 737317 138447P NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 YVR - MAJOR REPAIR - "C" - DURING C-13 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT AT BS 967, RBL 20. MA INTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED DAMAGED PORTION OF SUPPORT AT BS 967, RBL 20; FABRICATED NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW B737-300 SRM 51-70-12 FIG. 1, PG.1. 2 L 7 2 4F RT A16WE 2002012500145 20020125 00145 NM 2002 1 25 AWXA200200073 1 20020105 A 5315 6546811 SUPPORT BOEING 737 737317 138447P NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 YVR - MAJOR REPAIR - "C" - DURING C-13 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT AT BS 1006, RBL 6. MA INTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED SUPPORT AT BS 1006, RBL 6; FABRICATED NEW ATT ACH ANGLE AND INSTALLED REPAIR IAW B737-300 SRM 51-00-51, FIG 202, PG.207. 2 L 7 2 4F RT A16WE 2002012500147 20020125 00147 NM 2002 1 25 DHL2002746002 1 20020124 A 2910 MS9391130ZE MOTOR BOEING 727 727224 1384076 NM A DHLA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 746DH 22252 A SYSTEM FAILURE, NO PRESSURE NO QUANTITY. CREW ELECTED TO DIVERT INTO KDEN. TOWING OF THE AIRCRAFT WAS PREARRANGED, TOW ER WAS INFORMED OF THE EVENT IN ORDER TO LAND ON RUNWAY WHICH WOULD NOT CLOSE THE AIRPORT. FLIGHT LANDED SAFELY, WAS ABL E TO CLEAR THE RUNWAY, AND WAS TOWED TO THE RAMP.RIGHT WING FLAP DRIVE POWER UNIT FOUND TO BE LEAKING. REMOVED AND REPLA CED FLAP DRIVE HYDRAULIC MOTOR, FLUSHED, OPS CHECKED AND LEAK CHECKED. PERFORMED CASE DRAIN FILTER INSPECTION; NO METAL CONTAMINATION NOTED. INSTALLED NEW FILTER. SERVICED "A" SYS HYD QTY IAW MM 12-12-00. 2 L 7 3 4F A3WE 2002012500176 20020125 00176 NM 2002 1 25 KPVA200126 1 20020103 A 3350 6104789 POWER SUPPLY DHAV DHC8 DHC8103 1386005 NM CABIN DISCHARGED A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 807WP 023 HNL - FOUND EMERGENCY LIGHT POWER SUPPLY AT STATION 3351-PS2 WEAK. REMOVED AND REPLACED POWER SUPPLY AT STATION 3351-PS 2. OPS CHECK GOOD IAW DHC8 MM 33-51-00 PAGE 201-202. NO DEFECTS NOTED. (M) 2 H 7 2 4T RT A13NM 2002012500198 20020125 00198 NM 2002 1 25 P5CA0200633 1 20020124 A 5300 NONE SEAT TRACK BOEING 747 74746NF 13848BT NM FWD CARGO COMPT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 451PA 30809 FORWARD CARGO COMPARTMENT BS 560 - LBL - 225, WL 118 SEAT TRACK CRACKED. REPAIRED BY SPLICED IN SECTION OF SEAT TRACK IA W 400 SRM 53-00-52, PG. 251 2 L 7 4 4F RT A20WE 2002012500199 20020125 00199 NM 2002 1 25 P5CA0200632 1 20020124 A 5300 NONE SEAT TRACK BOEING 747 74746NF 13848BT NM FWD CARGO COMPT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 451PA 30809 FORWARD CARGO COMPARTMENT BS 560 - RBL - 45, WL - 118 SEAT TRACK CRACKED. REPAIRED BY SPLICED IN SECTION OF SEAT TRACK IAW 400F SRM 53-00-52, PG 251 2 L 7 4 4F RT A20WE 2002012800024 20020128 00024 EU 2002 1 28 MALA020127 1 20020116 A 2750 7257800582 HINGE FITTING SAAB SF340 340B 7860101 EU A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 During 4K-Check in CWA, LH Flap Hinge WS 123.38 has play at Flap Attach points. Maintenance installed new fitting PN 72 57800-582 RHOB and new hardware IAW SB57-038. Removed and installed new fitting assembly. Re-installed Hinge with new Ha rdware.Re-installed original Rear Frame IAW EO#S57043 and SRM 51. 2 L 7 2 4T RT A52EU 2002012800025 20020128 00025 EU 2002 1 28 MALA020131 1 20020116 A 5310 FLANGE SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 During 4K-Check in CWA, Upper Flange at Frame Sta 294 is corroded at approximately RBL 18.3. Maintenance performed repa ir of Frame, at Sta 294 IAW EO3 S53108. 2 L 7 2 4T RT A52EU 2002050200088 20020502 00088 CE 2002 5 2 00011 1 20020124 A 1430 FASTENER LEAR 24 24 5170302 CE LT MLG MISSING E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 333TW 168 LANDING GEAR WOULD NOT RETRACT, OBTAINED FERRY PERMIT TO RELOCATE AIRCRAFT TO ADS. MAINTENANCE FOUND LT GEAR SQUAT SWIT CH HARDWARE MISSING. REPLACED AND REPAIRED, OP'S CHECK IAW LEAR 24MM. 2 L 7 2 4J A10CE 2002012800027 20020128 00027 WP 2002 1 28 0200119603 1 20020117 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 603NW 47101 DURING HCK IN ATL, THE VENTRAL DOOR JAMB AND CAP WERE FOUND CRACKED. REPAIRED PER EA 96-185463. 2 L 7 2 4F A6WE 2002012800028 20020128 00028 NM 2002 1 28 2002000170 1 20020123 A 5753 65B170673 FLAP TRACK BOEING 747 7472R7F 1384870 NM T/E FLAP CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 639FE 21650 SURFACE CORROSION, FLAP TRACK NR 3 ROLLER WAY. REPAIR IS ACCOMPLISHED BY BLENDING OUT THE CORROSION PER OHM PROCEDURES WHILE MAINTAINING THE DRAWING FLATNESS AND PERPENDICULARITY REQUIREMENTS. THIS REPAIR IS APPROVED BY THE BOEING COMPAN Y PER ECRA N639FE-57-B747-011-EAC. 2 L 7 4 4F RT A20WE 2002012800029 20020128 00029 NM 2002 1 28 20020010167 1 20020123 A 5753 65B170687 FLAP TRACK BOEING 747 7472R7F 1384870 NM T/E FLAP CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 639FE 21650 SURFACE CORROSION, FLAP TRACK NR 4 ROLLER WAY. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS FOR CORROSION DAMAGE FOUND ON THE NR 4 FLAP TRACK LOWER ROLLER WAY SURFACES. BLENDED OUT THE CORROSION PER OHM PROCEDURES WHILE MAINTAINING THE DRAW ING FLATNESS AND PERPENDICULARITY REQUIREMENTS. THIS REPAIR IS APPROVED BY THE BOEING COMPANY PER ECRA N639FE-57-B747-0 06-EAC. 2 L 7 4 4F RT A20WE 2002012800030 20020128 00030 NM 2002 1 28 200200167 1 20020123 A 5753 65B170687 FLAP TRACK BOEING 747 7472R7F 1384870 NM T/E FLAP CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 639FE 21650 SURFACE CORROSION, FLAP TRACK NR 4 ROLLER WAY. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS FOR CORROSION DAMAGE FOUND ON THE NR 4 FLAP TRACK LOWER ROLLER WAY SURFACES. BLENDED OUT THE CORROSION PER OHM PROCEDURES WHILE MAINTAINING THE DRAW ING FLATNESS AND PERPENDICULARITY REQUIREMENTS. THIS REPAIR IS APPROVED BY THE BOEING COMPANY PER ECRA N639FE-57-B747-0 06-EAC. 2 L 7 4 4F RT A20WE 2002012800032 20020128 00032 NM 2002 1 28 200200168 1 20020123 A 5755 HINGE FITTING BOEING 747 7472R7F 1384870 NM SPOILER DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 639FE 21650 SPOILER HINGE FITTING REPLACEMENT, WSL 876.525. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS FOR REPLACEMENT OF THE TAPER SHANK BOLTS, RADIUS LEAD IN BOLTS, AND DD RIVETS. THIS REPAIR HAS BEEN REVIEWED AND APPROVED BY THE BOEING COMPANY PER ECRA N639FE-57-B747-05-EAC. 2 L 7 4 4F RT A20WE 2002012800034 20020128 00034 NM 2002 1 28 200200169 1 20020123 A 5753 65B170688 FLAP TRACK BOEING 747 7472R7F 1384870 NM T/E FLAP CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 639FE 21650 NUMBER 5 FLAP TRACK, CORROSION TRACK MOUNT HOLE. THIS REWORK INVOLVES REPLACING THE SERVICE BULLETIN 747-57-2207, INSTA LLED BUSHING WITH NEW INCREASED OD BUSHING. THIS OD INCREASE COMPENSATES FOR THE INCREASE BORE DIAMETER THAT REMOVED TH E CORROSION. THIS REPAIR IS APPROVED BY THE BOEING COMPANY PER ECRA N639FE-B747-010-EAC. 2 L 7 4 4F RT A20WE 2002012800036 20020128 00036 NM 2002 1 28 200200170 1 20020123 A 5753 65B170673 FLAP TRACK BOEING 747 7472R7F 1384870 NM T/E FLAP CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 639FE 21650 SURFACE CORROSION, FLAP TRACK NR 3 ROLLER WAY. REPAIR IS ACCOMPLISHED BY BLENDING OUT THE CORROSION PER OHM PROCEDURES WHILE MAINTAINING THE DRAWING FLATNESS AND PERPENDICULARITY REQUIREMENTS. THIS REPAIR IS APPROVED BY THE BOEING COMPANY PER ECRA N639FE-57-B747-011-EAC. 2 L 7 4 4F RT A20WE 2002012800038 20020128 00038 NM 2002 1 28 200200171 1 20020123 A 5720 65B0809514 SUPPORT FITTING BOEING 747 7472R7F 1384870 NM WING CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 639FE 21650 FLAP TRACK WING SKIN AND BACKUP FITTING HOLE CORROSION. REPAIR IS ACCOMPLISHED BY REPLACING THE ORIGINAL BUSHINGS EXCEP T THE OUTER DIAMETER IS INCREASED TO COMPENSATE FOR THE HOLE BORE DIAMETER INCREASE. THIS REPAIR IS APPROVED BY THE BOE ING COMPANY PER ECRA N639FE-57-B747-012-EAC. 2 L 7 4 4F RT A20WE 2002012800041 20020128 00041 NM 2002 1 28 200200172 1 20020123 A 5753 65B170674 FLAP TRACK BOEING 747 7472R7F 1384870 NM T/E FLAP CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 639FE 21650 NUMBER 6 FLAP TRACK, AFT MOUNT SURFACE CORROSION. CORROSION REMOVAL BY MACHINING EXCEEDED THE ALLOWED OHM REPAIR DEPTH. THE AFFECTED PART NUMBER IS 65B17067-4. THE REPAIR IS APPROVED BY THE BOEING COMPANY PER ECRA N639FE-57-B747-013-EAC. 2 L 7 4 4F RT A20WE 2002012800062 20020128 00062 NM 2002 1 28 QXEA0200013 1 20020112 A 5330 SKIN BOMBDR DHC8 DHC8401 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - MULTIPLE DENTS FOUND ON THE FORWARD TO MIDDLE LEFT SIDE OF THE AIRCRAFT FUSELAGE. MAINTENANCE COMPLIED WITH EA 6- 53-48 BY MEASURING AND MAPPING ALL DENTS THAT WERE NOTED BY INSPECTION. DATA WAS FORWARDED TO ENGINEERING. AN HFEC INS PECTION WAS PERFORMED ON ALL DENTS REQUIRED FROM INSPECTION, AND THE RESULTS WERE FORWARDED TO ENGINEERING. 2 H 7 2 4T RT A13NM 2002012800065 20020128 00065 NM 2002 1 28 CALA0200037 1 20020125 A 2150 20405010 ACM BOEING 737 7373T0 1384582 NM R/H PACK LEAKING A CALA A D UNSCHED LANDING RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 14320 38537 23371 SMOKE WAS REPORTED IN THE CABIN AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDEN T. MAINTENANCE FOUND OIL RESIDUE FROM R/H ACM IN DUCTWORK. THE R/H ACM WAS REMOVED AND REPLACED. HOT CYCLES WERE RUN ON R/H PACK FOR 20 MINUTES IAW MM 21-51-11 AND ALL CHECKED GOOD. BOTH COALESCER BAGS WERE REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 2002012800066 20020128 00066 NM 2002 1 28 CALA0200038 1 20020125 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 727B CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND A 5/8" CRACK IN R/H O/B SEAT TRACK AT STA 727B. THE CRACKED AREA WAS TRIMMED OUT AND A REPAIR DOUBLER W AS INSTALLED IAW ECRA 5321-01121. 2 L 7 2 4F RT A16WE 2002012800067 20020128 00067 NM 2002 1 28 CALA0200039 1 20020125 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 787-827 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND WEB CORRODED BETWEEN FLOOR SUPPORT RAILS IN AFT BAGGAGE BIN AT STA 787-827, S28R. A NEW WEB WAS INSTALL ED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002012800068 20020128 00068 NM 2002 1 28 CALA0200040 1 20020125 A 5320 WEB BOEING 737 737524 1384721 NM STA 927-947.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33635 26339 INSPECTION FOUND A 2" CRACK IN WEB AT STA 927-947.5, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2002012800069 20020128 00069 NM 2002 1 28 CALA0200041 1 20020126 A 5320 WEB BOEING 737 737524 1384721 NM STA 380-400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33635 26339 INSPECTION FOUND A 2" CRACK IN WEB AT STA 380-400, BL 0, MAIN DECK FLOOR. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10 -2. 2 L 7 2 4F RT A16WE 2002012800070 20020128 00070 NM 2002 1 28 CALA0200042 1 20020126 A 5320 INTERCOSTAL BOEING 737 737524 1384721 NM STA 344-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33635 26339 INSPECTION FOUND A 1" CRACK IN INTERCOSTAL AT CABIN FLOOR AREA, STA 344-360. THE INTERCOSTAL WAS REMOVED AND REPLACED IA W SRM 51-10-02 AND 51-40-00. 2 L 7 2 4F RT A16WE 2002012800071 20020128 00071 NM 2002 1 28 CALA0200043 1 20020127 A 5320 WEB BOEING 737 737524 1384721 NM STA 927-947.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33635 26339 INSPECTION FOUND A 1" CRACK IN WEB AT STA 927-947.5, LBL 26. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002012800072 20020128 00072 NM 2002 1 28 CALA0200044 1 20020127 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND A 3/8" CRACK IN C-2 DOOR EXTERIOR SKIN AT AFT UPPER CORNER OF DOOR HANDLE CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 202. 2 L 7 2 4F RT A16WE 2002012800073 20020128 00073 NM 2002 1 28 CALA0200045 1 20020127 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 373 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND A 1/2" CRACK IN FUSELAGE EXTERIOR SKIN AT E&E BAY EXHAUST CUTOUT, STA 373. A REPAIR DOUBLER WAS INSTALL ED IAW ECRA 5330-02894. 2 L 7 2 4F RT A16WE 2002012800074 20020128 00074 NM 2002 1 28 CALA0200046 1 20020127 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND STRINGER 26R CORRODED AT STA 1016. THE STRINGER WAS REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002012800075 20020128 00075 NM 2002 1 28 CALA0200047 1 20020127 A 5320 SHEAR TIE BOEING 737 7373T0 1384582 NM STA 1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND BELTFRAME SHEAR TIE CORRODED AT STA 1006 BETWEEN STRINGERS 25R AND 27R. THE SHEAR TIE WAS REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002012800076 20020128 00076 NM 2002 1 28 QXEA0200015 1 20020103 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - OUTBOARD BRACKET FOR LEADING EDGE 611AR AT NACELLE END, LOWER SIDE IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002012800078 20020128 00078 NM 2002 1 28 QXEA0200016 1 20020102 A 7120 STRUT DHAV DHC8 DHC8202 2809007 NM ENGINE MOUNT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - NR 2 ENGINE MOUNT LOWER OUTBOARD STRUT HAS TWO CHAFED SPOTS ON INBOARD SIDE. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002012800079 20020128 00079 NM 2002 1 28 QXEA0200017 1 20020102 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - X220 TO X240, BL45R, Z103 LAV HAS CHAFED SPOTS ON WEB ANGLE. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 7, STEP 3 (1). 2 H 7 2 4T RT A13NM 2002012800082 20020128 00082 NM 2002 1 28 QXEA0200019 1 20020103 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - CARGO DOOR SKIN CHAFED 3 INCHES FROM BOTTOM. REPAIRED IAW RD 8-52-230, RD 8-52-230, DHC-8 SRM 51-40-00 AND SRM 51 -40-11. 2 H 7 2 4T RT A13NM 2002012800084 20020128 00084 NM 2002 1 28 QXEA0200021 1 20020107 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT INBOARD SEAT TRACK HAS CORROSION BETWEEN X504 AND X517. REPAIRED IAW RD 8-53-1102, RD 8-53-4473 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002012800086 20020128 00086 NM 2002 1 28 QXEA0200022 1 20020105 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT INBOARD SEAT TRACK HAS CORROSION AT X540 TO X544. REPAIRED IAW RD 8-53-4963 AND DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002012800088 20020128 00088 NM 2002 1 28 QXEA0200023 1 20020104 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - X600, Y21L, Z100 UNDERSIDE SKIN AT NUT PLATE HAS CORROSION. REPAIRED IAW DHC-8 SRM 53-00-16, PAGE 3, TABLE 1. 2 H 7 2 4T RT A13NM 2002012800089 20020128 00089 NM 2002 1 28 QXEA0200024 1 20020104 A 5320 FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - X594, Y30L, Z100 WEB TIE SKIN UNDER NUT PLATE HAS CORROSION. REPAIRED IAW DHC-8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002012800091 20020128 00091 NM 2002 1 28 QXEA0200025 1 20020103 A 5230 DOUBLER DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - CARGO DOOR SKIN UPPER REPAIR DOUBLER CHAFED. REPAIRED IAW DHC-8 SRM 52-00-16, PAGE 2. 2 H 7 2 4T RT A13NM 2002012800093 20020128 00093 NM 2002 1 28 QXEA0200027 1 20020108 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT FORWARD OUTBOARD SEAT TRACK MOUNTING ANGLE AT STATION X354.150 TORN. REPAIRED IAW HORIZON AIR EA 2-53-359, DHC -8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002012800094 20020128 00094 NM 2002 1 28 QXEA0200028 1 20020105 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - THERE IS CHAFE DAMAGE AT TWO LOCATIONS ON UPPER CARGO DOOR APERTURE. REPAIRED IAW RD 8-53-5461. 2 H 7 2 4T RT A13NM 2002012800095 20020128 00095 NM 2002 1 28 QXEA0200029 1 20020107 A 5320 INTERCOSTAL DHAV DHC8 DHC8202 2809007 NM FUSELAGE BOWED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - INTERCOSTAL WEB IS BOWED WHERE IT ATTACHES TO LEFT HAND INBOARD SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002012800096 20020128 00096 EU 2002 1 28 MALA020139 1 20020123 A 2460 PDU SAAB SF340 SF340A 7850100 EU DEFECTIVE A MALA K NONE I FLT. ATTITUDE INST. CR CRUISE 1 GL 15 114XJ 340A114 During Flight #3185, RH Buss failed inflight. FO's Efis Displays (both) went blank. Maintenance replaced RH PDU then Bu ss failed again. Maintenance replaced LH PDU, and replaced Relay 72 PC. See 409 #080284 for details. 2 L 7 2 4T RT A52EU 2002012800097 20020128 00097 EU 2002 1 28 MALA020140 1 20020124 A 3350 6104789 BATTERY PACK SAAB SF340 SF340A 7850100 EU INOPERATIVE A MALA O OTHER O OTHER IN INSP/MAINT 1 GL 15 142XJ During Line Check, noted several Emergency lights Inop. Maintenance removed and replaced battery pack PN/on 61-0478-9, SN/on 9804441 at 22LN. IAW SF340 AMM 33-50-10-4. 2 L 7 2 4T RT A52EU 2002012800098 20020128 00098 NM 2002 1 28 QXEA0200030 1 20020108 A 5730 SKIN PANEL DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - GOUGE IN UPPER WING SKIN PANEL ON RT WING AT AFT EDGE OF PANEL AT STATION 155.2. REPAIRED IAW DHC-8 51-20-11, PAG E 7, PARAGRAPH 3E-F (1). 2 H 7 2 4T RT A13NM 2002012800102 20020128 00102 NM 2002 1 28 QXEA0200031 1 20020107 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT INBOARD SEAT TRACK IS CORRODED BETWEEN FUSELAGE STATIONS X182.0 AND X222.0. REPAIRED IAW DHC-8 RD 8-53-4693, R D 8-53-4473, RD 8-53-2295 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002012800104 20020128 00104 SO 2002 1 28 DQI2002F00000 1 20020103 A 2140 A23D0475 SHUTOFF VALVE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA FUEL REGULARTOR LEAKING E DQIR O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 4089Y 16 318152101 CREW REPORTED FUEL PRESSURE FOR RIGHT ENGINE WOULD DROP INTERMITTENTLY. THE JANITROL HEATER FUEL SUPPLY COMES FROM FUEL FOR RIGHT ENGINE. TURNED HEATER ON, AND FUEL LEAKED FROM FUEL REGULATOR/SHUTOFF VALVE. THIS WAS A NEW VALVE THAT REPL ACED ANOTHER LEAKING VALVE PER THE REQUIREMENTS OF AD. 1 L 7 2 3O 3 O A20SO E14EA 2002012800106 20020128 00106 NM 2002 1 28 PCAA0201018 1 20020127 A 2720 82710038101 FITTING DHAV DHC8 DHC8102 2809003 NM CAPTIAN SIDE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 834EX 285 BGM -DURING ROUTINE MANTENANCE VISIT AN INSPECTION OF RUDDER PEDAL ADJUSTMENT FITTING PER ALERT SERVICE BULLETIN A8-27-9 1 REVEALED THE CAPTAINS FITTING WAS CRACKED. FITTING WAS REMOVED AND REPLACED WITH POST PN:82710080-101 IN ACCORDANCE EI TH DEHAVILLAND MAINT. MANUAL 27-20-00 AIRCRAFT RETUNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002012800107 20020128 00107 2002 1 28 COMA0260062 4 20020122 A 8300 5018T48P03 SEAL CNDAIR CL600 CL6002B19 1900309 EA R/H ENG LEAKING A COMA A UNSCHED LANDING K Y FLUID LOSS ENGINE STOPPAGE CR CRUISE 1 SO 01 804CA 7352 FLIGHT 5589 R/H ENGINE LOW OIL PRESSURE. IFSD. REPLACED THE ACCESSORY DRIVE CARBON SEALS. 2 L 7 2 4F RT A21EA 2002012800108 20020128 00108 EU 2002 1 28 02026324 1 20020126 A 3260 AIR135022 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 324UE 41017 During climb of the flight from IAD to PIT, the crew reported that upon landing gear retraction they observed a right ma in landing gear "unsafe" red annunciator. The landing gear was cycled down, three green "safe" annunciators were observ ed, the aircraft returned to IAD and landed without incident. Maintenance personnel removed and replaced the right main landing gear uplocked indication microswitch. An operational check was satisfactory and the aircraft was returned to s ervice. 2 L 7 2 4T RT A41NM 2002012800110 20020128 00110 EA 2002 1 28 COMA0260063 1 20020124 A 5270 MS24584C493 SPRING CNDAIR CL600 CL6002B19 1900309 EA AVIONICS STUCK A COMA A UNSCHED LANDING J O WARNING INDICATION OTHER TO TAKEOFF 1 SO 01 960CA 7117 FLIGHT 5602 AVIONICS BAY DOOR WARNING DURING T/O.FOUND AVIONICS DOOR SWITCH JAMMED. REPLACED SWITCH SPRING. 2 L 7 2 4F RT A21EA 2002012800111 20020128 00111 WP 2002 1 28 DHL2002805019 1 20020102 A 5312 ANGLE DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R1840NLG. W/W ... ANGLE ATTACHING BULKHEAD TO INTERCOSTAL @ STA. - 131.000 LH , CRACKED 1" 2 L 7 4 4F RT 4A25 2002013000026 20020130 00026 EU 2002 1 30 SABA020011 1 20020126 A 2611 7211121100 SMOKE DETECTOR BAG JETSTM JETSTM3201 1500217 EU LAVATORY MALFUNCTIONED A SABA K NONE N FALSE WARNING AP APPROACH 1 SO 33 965AE 965 FLIGHT 5121 FROM HKY TO CLT, SMOKE DETECTOR CAUTION LIGHT ILLUMINATED IN LAVATORY DURING SHORT FINAL INTO CLT. NO EMERG ENCY WAS DECLARED. AIRCRAFT LANDED IN CLT WITH NO OTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR, SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2002012800112 20020128 00112 EA 2002 1 28 COMA0260064 1 20020124 A 2740 3094334 SWITCH CNDAIR CL600 CL6002B19 1900309 EA COPILOT INOPERATIVE A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 912CA 7011 FLIGHT 9983 CO-PILOTS STAB TRIM SWITCH IS INOPERABLE.REPLACED SWITCH. 2 L 7 2 4F RT A21EA 2002012800113 20020128 00113 EA 2002 1 28 COMA0260065 1 20020124 A 3240 428853 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 920CA 14137 7022 FLIGHT 5560 ANTI-SKID CAUTION MESSAGE DURING GEAR EXTENSION.REPLACED THE ASCU 2 L 7 2 4F RT A21EA 2002012800114 20020128 00114 EA 2002 1 28 COMA0260066 1 20020117 A 3230 MS27473T10B5S CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA NLG INOPERATIVE A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 912CA 7011 FLIGHT 5521 LANDING GEAR DISAGREE WARNING.REPLACED THE NLG SELECTOR VALVE WIRING CONNECTOR. 2 L 7 2 4F RT A21EA 2002012800115 20020128 00115 2002 1 28 SWIA200210536 4 20020112 A 3425 CAP EMB 120 EMB120ER 3260203 SO COCKPIT LOOSE A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 226SW 120296 PRIOR TO LEVEL OFF AT FL230 CAPTAIN ATTITUDE INDICATOR AND HEADING DISPLAY TUMBLED AND WOULD MOMENTARILY RESET AND THEN TUMBLE AGAIN. FOUND FUSE CAP TO NR 1 AHC85 LOOSE. RECONNECTED CAP HEADING. CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002012800116 20020128 00116 EA 2002 1 28 SWIA200210537 1 20020111 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 426SW 7468 SPOILERON FAULT STATUS MESSAGE ON WITH ALL HYDRAULICS ON. REMOVED AND REPLACED LT O/B SPOILERON PCU ASSEMBLY. OPS CHEC K GOOD. NO DEFECTS NOTED. NO LEAKS NOTED. 2 L 7 2 4F RT A21EA 2002012800117 20020128 00117 NM 2002 1 28 SABA020012 1 20020126 A 2611 PU90461S DETECTOR DHAV DHC8 DHC8103 1386005 NM FALSE INDICATION A SABA O OTHER N FALSE WARNING CR CRUISE 1 SO 33 881CC 294 Flight 5212 from PGV to CLT: During flight the lavatory smoke detector keep going off intermittently. Aircrew checked ar ea but no smoke. Aircraft contuined to CLT with no other problems. No emergency was declared. Maintenance removed and re placed the Smoke Detector, System ops checked good. Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002012800118 20020128 00118 EA 2002 1 28 SWIA200210539 1 20020112 A 5610 NP1393222 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 909SW 7558 AT FL350 CO-PILOT'S WINDOW CRACKED. REMOVED AND REPLACED RT SIDE WINDOW. 2 L 7 2 4F RT A21EA 2002012800119 20020128 00119 NM 2002 1 28 QXEA0200032 1 20020106 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X262 AND X270. REPAIRED IAW DHC-8 RD 8-53-1342, SRM 5 1-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002012800120 20020128 00120 NM 2002 1 28 QXEA0200033 1 20020107 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X340 AND X343. REPAIRED IAW DHC-8 SRM 51-40-11 AND SR M 51-40-00. 2 H 7 2 4T RT A13NM 2002012800121 20020128 00121 NM 2002 1 28 QXEA0200034 1 20020104 A 5220 STOP FITTING DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT FORWARD EMERGENCY EXIT ALL EIGHT DOOR STOPS CHAFED ON BEARING SURFACES. REPAIRED IAW RD 8-52-349. 2 H 7 2 4T RT A13NM 2002012800122 20020128 00122 NM 2002 1 28 QXEA0200035 1 20020106 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X434 AND X438. REPAIRED IAW RD 8-53-1342 AND DHC-8 SR M 51-20-26. 2 H 7 2 4T RT A13NM 2002012800123 20020128 00123 NM 2002 1 28 QXEA0200036 1 20020105 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT OUTBOARD SEAT TRACK HAS CORROSION BETWEEN STATIONS X452 AND X456. REPAIRED IAW RD 8-53-1342 AND DHC-8 SRM 51-2 0-16. 2 H 7 2 4T RT A13NM 2002012800124 20020128 00124 NM 2002 1 28 QXEA0200037 1 20020105 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X467 AND X471. REPAIRED IAW RD 8-53-1342 AND DHC-8 SR M 51-20-16. 2 H 7 2 4T RT A13NM 2002012800125 20020128 00125 NM 2002 1 28 QXEA0200038 1 20020105 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X483 AND X505. REPAIRED IAW DHC-8 RD 8-53-1342 AND SR M 51-20-16. 2 H 7 2 4T RT A13NM 2002012800126 20020128 00126 NM 2002 1 28 QXEA0200039 1 20020105 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT OUTBOARD SEAT TRACK HAS CORROSION BETWEEN STATIONS X514 AND X523. REPAIRED IAW DHC-8 RD 8-53-3644, PAGE 1-2 AN D SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002012800127 20020128 00127 NM 2002 1 28 QXEA0200040 1 20020105 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X530 AND X532. REPAIRED IAW DHC-8 SRM 8-53-3644, PAGE 1-3 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002012800128 20020128 00128 NM 2002 1 28 QXEA0200041 1 20020105 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X541 AND X544. REPAIRED IAW DHC-8 RD 8-53-3644, PAGES 1-2, STEPS 1-2 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002012800129 20020128 00129 NM 2002 1 28 QXEA0200042 1 20020103 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - NR 1 ENGINE FIREWALL CRACKED .25 INCH ABOVE FIRE LOOP SUPPORT BRACKET. REPAIRED IAW DHC-8 RD 8-54-611. 2 H 7 2 4T RT A13NM 2002012800130 20020128 00130 NM 2002 1 28 QXEA0200043 1 20020109 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X392 HAS A CORROSION PIT IN THE CHANNEL. REPAIRED IAW DHC-8 RD 8-53-4473. 2 H 7 2 4T RT A13NM 2002012800131 20020128 00131 NM 2002 1 28 QXEA0200044 1 20020109 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT INBOARD SEAT TRACK X437 HAS A CORROSION PIT IN THE CHANNEL. REPAIRED IAW DHC-8 RD 8-53-4473 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002012800132 20020128 00132 NM 2002 1 28 QXEA0200045 1 20020105 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X541 THERE IS A GOUGE IN THE CHANNEL. REPAIRED IAW DHC-8 RD 8-53-1342 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002012800133 20020128 00133 NM 2002 1 28 QXEA0200046 1 20020105 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X514 TO 517 HAS PITTING CORROSION ON TOP FLANGE AND IN CHANNEL. REPAIRED IAW DHC-8 RD 8-53 -3644 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002012800134 20020128 00134 NM 2002 1 28 AWXA200200080 1 20020121 A 5330 50079452 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A CRACK WAS FOUND ON L1 DOOR UPPER HINGE CUTOUT AT UPPER CORNER BS 319.5. M AINTENANCE STOP DRILLED THE CRACK AND PERFORMED HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED; FABRICATED A REPAIR D OUBLER AND INSTALLED REPAIR IAW B737-300 SRM 52-00-3, PG. 10, AND SRM 51-30-2, PG. 2 & 3. 2 L 7 2 4F RT A16WE 2002012800135 20020128 00135 EU 2002 1 28 AWXA200200084 1 20020127 A 3350 079123 LENS AIRBUS 320 A320231 3930325 EU SEAT 9A MISSING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 CMH - EEL - "C" - EMERGENCY ESCAPE PATH LIGHT RED LENS COVER MISSING AT SEAT 9A. MAINTENANCE INSTALLED RED EMERGENCY ESC APE PATH LIGHT LENS COVER AT SEAT 9A. 2 L 7 2 4F RT A28NM 2002012800136 20020128 00136 NM 2002 1 28 QXEA0200047 1 20020109 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X497 TO 504.5 HAS CORROSION IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8 RD 8-53-1342, SRM 51-40-11 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002012800137 20020128 00137 NM 2002 1 28 QXEA0200048 1 20020109 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X482 TO X487 HAS CORROSION IN THE CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8 RD 8-53-13 42. 2 H 7 2 4T RT A13NM 2002012800138 20020128 00138 NM 2002 1 28 QXEA0200049 1 20020109 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X465 TO X470 HAS CORROSION IN THE CHANNEL AND ON TOP FLANGE. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002012800139 20020128 00139 NM 2002 1 28 QXEA0200050 1 20020109 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X451 TO X455 HAS CORROSION PITS IN THE CHANNEL. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002012800140 20020128 00140 NM 2002 1 28 QXEA0200051 1 20020109 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X454 HAS CORROSION ON THE TOP FLANGE. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002012800141 20020128 00141 NM 2002 1 28 QXEA0200052 1 20020109 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X434 TO X439 HAS CORROSION PITS IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC8 RD 8-53-13 42. 2 H 7 2 4T RT A13NM 2002012800149 20020128 00149 EU 2002 1 28 RAIA00201030 1 20020125 A 2430 1030032 SENSOR AEROSP ATR42 ATR42300 8680920 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 423TE 15000 4035 119 5600-STL- #1 GENERATOR FAULTED. MAINTENANCE REMOVED AND REPLACED THE #1 HALL EFFECTS SENSOR. OPS CK OK. 2 H 7 2 4T RT A53EU 2002012800150 20020128 00150 EU 2002 1 28 RAIA0020131 1 20020125 A 7900 3034508 OIL FILTER AEROSP ATR72 ATR72202 8680940 EU A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 722TE 220 5602- STL- CREW REPORTED SMOKE IN CABIN AND COCKPIT DURING TAXI. MAINTENANCE REMOVED AND REPLACED #1 ENGINE SCAVENGE OIL FILTER. INSPECTED MAIN OIL FILTER FOUND NO DEFECTS. PERFORMED GROUND RUN FOR 80 MINUTES - NO SMOKE - NO OIL WARNING LIG HTS - OIL QUANTITY STABLE. 2 H 7 2 4T RT A53EU 2002012800151 20020128 00151 EU 2002 1 28 RAIA00201032 1 20020127 A 3397 167006 WIRE AEROSP ATR72 ATR72202 8680940 EU AIRSTAIRS BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 722TE 220 5592-STL- EMERGENCY LIGHT AT 11AB AND AIR STAIRS INOP. REPAIRED BROKEN WIRE AT AIR STAIRS. REPLACED BULB AT 11AB. TEST O K. 2 H 7 2 4T RT A53EU 2002012900006 20020129 00006 CE 2002 1 29 F342002F00000 1 20020102 A 3260 P6340005 DOWNLOCK SWITCH CESSNA 210 P210N 2073454 CE CONT O520 TSIO520P 17040 SO MLG INOPERATIVE E F34A O OTHER N FALSE WARNING LD LANDING 1 EA 03 102KY 4240 P21000093 278764R AIRCRAFT WAS IN THE PROCESS OF LANDING WHEN A PASSENGER NOTICED THE RIGHT GER TRAILING AND NOT IN THE DOWN AND LOCK POSI TION. AFTER SEVERAL ATTEMPTS TO PUT GEAR DOWN ELECTRICALLY, PILOT PUMPED THE GEAR DOWN MANUALLY INTO LOCK POSITION. UP ON TROUBLE SHOOTING, FOUND THE RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH STUCK IN THE CLOSED POSITION WHICH MENT, WHEN THE OTER TWO GEARS LOCKED THE PUMP MOTOR QUIT RUNNING BEFORE THE RIGHT GEAR HAD A CHANCE TO LOCK INTO POSITION. INSTALLED NEW SWITCH (PN P6-340005). OPS CHECKED GOOD. TT 4240 1 H 7 1 3O 3 O 3A21 E8CE 2002012900011 20020129 00011 SW 2002 1 29 IIF2002F00000 1 20020109 A 6340 2060400931 INDICATOR BELL 206 206B 1181511 SW ALLSN 250C 250C* GL TRANS OIL LEVEL LEAKING B IIFR K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2069L 4108 3405 TRANSMISSION OIL LEAK DUE TO TRANSMISSION OIL LEVEL INDICATOR PROBLEM. OIL LEVEL INDICATOR (PN 206-040-093-001). PART SEPARATED FROM METAL DISC INDICATOR MOVED BLOCKING OFF HOLES ON METAL PART AS WELL. AS HOLES IN TRANSMISSION SIGHT GLAS S CASTING BOSS ON LOWER TRANSMISSION CASE. VIEWING SIGHT GLASS OIL LEVEL INDICATED LOW. AFTER ADDING 2 QUARTS OF OIL, LEVEL DID NOT MOVE. GROUND RAN AIRCRAFT OIL WAS FORCED OUT FILLER CAP. UPON SHUTDOWN, NOTICED LEVEL TO BE OVER SERVICE D. AFTER DRAINING TO PROPER LEVEL HAD 4 QUARTS IN CONTAINER. SUGGEST HIGHER QUALITY METAL PIECE BE MADE. 1 G 7 1 3U 3 U H2SW E4CE 2002020500008 20020205 00008 NM 2002 2 5 02FDEA00073 1 20020126 A 5310 FITTING BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 CORROSION ON INTERNAL JACK PAD FITTING, BS 1183, STR 3. R&R JACK PAD FITTING PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002012900024 20020129 00024 WP 2002 1 29 IXXA0200002O 1 20020117 A 2933 EA1066A2183 TRANSMITTER DOUG DC8 DC871F 302199D WP FUSELAGE DEFECTIVE A IXXA O OTHER K FLUID LOSS CR CRUISE 1 SW 11 824BX 80532 2000 45946 WHILE ENROUTE FROM JFK TO BDL, THE FLIGHT CREW NOTICED THAT THE MAIN HYDRAULIC QUANTITY SYSTEM WAS DECLINING. THE FLIGH T CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO BDL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT A ND TRACED THE PROBLEM TO A FAULTY HYDRAULIC QUANTITY TRANSMITTER. MAINTENANCE REPLACED THE TRANSMITTER AND PERFORMED OP ERATIONAL CHECKS IN ACCORDENCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002012900025 20020129 00025 EA 2002 1 29 02024701 1 20020124 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 701BR 7448 DURING PREFLIGHT INSPECTION FOR THE FLIGHT FROM LGA TO SAV, THE CREW REPORTED THAT THE CENTER, OVERHEAD, EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE CENTER, OVERHEAD EMERGENCY FLOOD LIG HT. AN OPERATIONAL CHECK OF THE LIGHT WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002012900027 20020129 00027 NM 2002 1 29 SWAA020175 1 20020122 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 951, STRINGER 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2002012900028 20020129 00028 NM 2002 1 29 SWAA020176 1 20020122 A 5320 6545808 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D CHECK, FOUND BS 294.5 ATTACHED WEB CRACKED, STRINGER 12L. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002012900029 20020129 00029 NM 2002 1 29 SWAA020178 1 20020125 A 5311 6546540 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D CHECK, FOUND BS 663 FRAME CRACKED, STRINGER 2L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002012900030 20020129 00030 NM 2002 1 29 SWAA020179 1 20020125 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 277, STRINGER 15R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002012900031 20020129 00031 NM 2002 1 29 SWAA020184 1 20020122 A 3350 101114 LENS BOEING 737 7373L9 1384470 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2002012900032 20020129 00032 NM 2002 1 29 SWAA020185 1 20020125 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED,BS 927, STRINGER 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002012900033 20020129 00033 NM 2002 1 29 SWAA020188 1 20020125 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 559, STRINGER 14L. REPAIRED FRAME PER SWA RA. 2 L 7 2 4F RT A16WE 2002012900034 20020129 00034 NM 2002 1 29 SWAA020189 1 20020125 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAMECRACKED, BS 639, STRINGER 15R. REPAIRED FRAME PER SWA RA. 2 L 7 2 4F RT A16WE 2002012900035 20020129 00035 NM 2002 1 29 SWAA020192 1 20020127 A 2731 183A8410 BUSHING BOEING 737 7377H4 1384404 NM ELEVATORS WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 726SW 27858 DURING SCHEDULED SERVICE CHECK, (SI NR 11038-55), BOTH LT AND RT ELEVATORS FAILED FREE PLAY CHECKS. REMOVED AND REPLACE D LT ELEVATOR TAB ATTACH BUSHINGS AT NR 3 AND NR 4 POSITION, AND REMOVED AND REPLACED RT ELEVATOR TAB ATTACH BUSHINGS AT NR 2 AND NR 4 POSITION PER MM.. 2 L 7 2 4F RT A16WE 2002012900036 20020129 00036 NM 2002 1 29 SWAA020166 1 20020122 A 5310 6545802 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D CHECK, FOUND WEB CRACKED AT BS294.5, STR 7L. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002012900037 20020129 00037 NM 2002 1 29 SWAA020170 1 20020123 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED C3 CHECK, FOUND FUSE SKIN CRACKED (3 EA) AT BS 727E, STR 21R, BS 735, STR 18R AND BS 870, STR 24R. REP AIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002012900038 20020129 00038 NM 2002 1 29 SWAA020171 1 20020123 A 2612 6937307300 CONTROL PANEL BOEING 737 7377H4 1384404 NM COCKPIT FAULTY A SWAA D RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 SW 07 724SW 27856 DIVERSION, AT CRUISE ALTITUDE GOT A WHEEL WELL FIRE WARNING. REMOVED AND REPLACED P8-1 ENG AND APU FIRE CONTROL PANEL. FUNCTIONAL AND OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2002012900039 20020129 00039 NM 2002 1 29 SWAA020172 1 20020123 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 500C, STR 10R, BS 500D, STR 4L AND BS 500C, STR 4L. REPAIREDSKIN PER SRM. 2 L 7 2 4F RT A16WE 2002012900040 20020129 00040 NM 2002 1 29 SWAA020173 1 20020123 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002012900041 20020129 00041 NM 2002 1 29 SWAA020174 1 20020123 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002012900053 20020129 00053 NM 2002 1 29 SWAA020177 1 20020122 A 5310 6558280 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D CHECK, FOUND BS 360 SHEAR TIES CRACKED, STRINGERS 14L-15L AND 14R-15R. REMOVED AND REPLACED SHEAR TI E SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2002012900054 20020129 00054 NM 2002 1 29 SWAA020186 1 20020125 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY EXIT LIGHT LENS BROKEN NEXT TO AFT LAV. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2002012900055 20020129 00055 NM 2002 1 29 SWAA020168 1 20020122 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM SERVICE DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 384SW 26590 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT LENS DAMAGED. REMOVED AND REPLACED EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2002012900056 20020129 00056 WP 2002 1 29 ABXA010684 1 20020109 A 5311 39213163 FRAME DOUG DC9 DC932F 3022067 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 FRAME AT STATION 408 WAS CRACKED AT LONGERON ATTACHMENT 17 RIGHT. REPAIRED FRAME AT STA. 408 IAW DC-9 SRM 53-03. 2 L 7 2 4F A6WE 2002012900057 20020129 00057 WP 2002 1 29 ABXA010686 1 20020110 A 5200 3914025502 FITTING DOUG DC9 DC932F 3022067 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 AFT LOWER CARGO DOOR #1 BEAM AFT END FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2002020500005 20020205 00005 NM 2002 2 5 02FDEA00059 1 20020123 A 2611 CONNECTOR BOEING 727 72722 1384002 NM SMOKE DETECTOR DIRTY A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 149FE 19087 CARGO DOOR SMOKE LIGHT ILLUMINATED. PRESSED BOTTLE NR 1 DISCHARGE PER QRHB. CLEANED CONNECTORS. 2 L 7 3 4F A3WE 2002012900058 20020129 00058 SO 2002 1 29 C2XA02CL019 1 20020124 A 3240 21624 BRAKE EMB 145 EMB145LR 3260212 SO LANDING GEAR BYPASSING A C2XA A B UNSCHED LANDING EMER. DESCENT J O WARNING INDICATION OTHER CL CLIMB 1 SW 27 16999 4953 852 145307 CLE FLIGHT#3738 THE CREW REPORTED AFTER TAKEOFF FROM CLE THEY RECEIVED A #1 HYDRAULIC SYSYTEM LOW QUANTITY INDICATION.TH E AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #1 AND #4 BR AKE ASSEMBLIES.THEY SUSPECTED THE #1 HYDRAULIC SYSTEM FLIUD WAS TRANSFERING TO THE #2 SYSTEM THROUGH THE BRAKES.THE AIRC RAFT WAS TEST FLOWN AND NO DEFECTS WERE NOTED.THE AIRCRAFT WAS RELEASED FOR SERVICE.#4 BRAKE S/N 0663 TSO:3444 TT:3444 C SN:2403 2 L 7 2 4T RT T00011AT 2002012900059 20020129 00059 NM 2002 1 29 CALA0200048 1 20020128 A 5414 SKIN BOEING 737 7373T0 1384582 NM #2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND A 1/2" CRACK AT LOWER AFT CORNER OF #2 PYLON O/B ACCESS SKIN PANEL #5824. A REPAIR DOUBLER WAS INSTALLE D IAW ECRA 5430-01204, FIGURE 3. 2 L 7 2 4F RT A16WE 2002012900061 20020129 00061 NM 2002 1 29 02FDEA00060 1 20020109 A 5230 STRUCTURE BOEING 727 7272S2F 1384O81 NM CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 FWD CARGO DOOR LWR AFT CORNER DENTED. REMOVED AND REPLACED DOOR PER SRM 52-00-3. 2 L 7 3 4F A3WE 2002012900065 20020129 00065 NM 2002 1 29 02FDEA00062 1 20020123 A 2612 FIRE LOOP DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE NR 1 ENGINE FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 590FE 48505 704307 AFTER ROTATION NR 1 ENG FIRE DET NR 1 FAULT CAME ON. REMOVED AND REPLACED FDCU AS PRECAUTION PER MM 26-11. REMOVED AND REPLACED NR 1 LWR TURBINE FIRE DET LOOP-B PER MM 26-11-03-4. CLOSED AND LATCHED NR 1 ENG COWLING PER MM 71-10-00. 2 L 7 3 4F 4 F RT A22WE E31N3 2002012900067 20020129 00067 NM 2002 1 29 02FDEA00063 1 20020124 A 5270 SWITCH BOEING 727 7272S2F 1384O81 NM AFT AIRSTAIRS OUT OF ADJ A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 212FE 22934 ON CLIMBOUT AT 12,000 MSL AFT AIRSTAIRS LIGHT ILLUMINATED. ADJUSTED MICRO SWITCH PER MM 52-62-001-5. 2 L 7 3 4F A3WE 2002020100009 20020201 00009 NE 2002 2 1 02FDEA00064 2 20020124 A 7510 SEAL DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE ANTI-ICE DUCT LEAKING A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 621FE 48792 NR 2 ENG ANTI-ICE DUCT LEVEL 3 ALERT SHUT DOWN ENG. SECURED LOOSE SEAL & R&R PRESS SWITCH PER PRECAUTION. 2 L 7 3 4F 4 F RT A22WE E24NE 2002012900068 20020129 00068 WP 2002 1 29 02FDEA00065 1 20020124 A 3150 CONTROLLER DOUG DC10 DC1030F 3023504 WP COCKPIT MALFUNCTIONED A FDEA J DUMP FUEL N FALSE WARNING CR CRUISE 1 SO 25 302FE 46801 INTERMITTENT PILOT MASTER CAUTION LIGHT WITH NO OTHER IND. REMOVED AND REPLACED MASTER WARN CONTROLLER. GROUND CHECK N ORM. 2 L 7 3 4F RT A22WE 2002012900069 20020129 00069 NM 2002 1 29 02FDEA00066 1 20020125 A 2612 FIRE WARNING BOEING 727 727227 1384078 NM COCKPIT MALFUNCTIONED A FDEA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 25 481FE 21463 ON TAKEOFF FIRE WARNING BELL CUTOUT LIGHTS ILLUMINATED. NEEDS BELL CUTOUT SWITCH. NO DEFECTS NOTED. AC OK TO CONTINUE . 2 L 7 3 4F A3WE 2002061900173 20020619 00173 NE 2002 6 19 02FDEA00067 2 20020125 A 7230 COMPRESSOR AIRBUS 310 A310 EU PWA JT9 JT9D7R4E1 52054 NE NR 1 ENGINE STALLED A FDEA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 25 447FE 251 NR 1 ENGINE COMPRESSOR STALL AT FL 350. THIS WAS FOLLOWED BY COMPLETE LOSS OF OIL PRESS, FOLLOWED ECAM PREC ENGINE SHUT DOWN. ENG WIND MILLED FOR ABOUT 30 MIN. REMOVED AND REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A35EU E3NE 2002012900070 20020129 00070 EU 2002 1 29 02FDEA00068 1 20020126 A 2611 SMOKE DETECTOR AIRBUS 310 A310203 3930313 EU CARGO BAY MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 409FE 273 ON CLIMBOUT AFT AND BULK CARGO SMOKE LIGHT CAME ON. CREW FOUND NO EVIDENCE OF FIRE. 2 L 7 2 4F RT A35EU 2002012900071 20020129 00071 SO 2002 1 29 C2XA02CL020 1 20020124 A 2611 FDS765A2 SENSOR EMB 135 EMB135ER 3260203 SO LAV FALSE ACTIVATION A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 14505 4349 145192 CLE FLIGHT#4010 THE CREW REPORTED A LAV SMOKE WARNIG ON CLIMBOUT.THE MESSAGE CLEARED AFTER 20 SECONDS.MAINTENANCE REPLAC ED THE LAV SMOKE SENSOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002012900072 20020129 00072 WP 2002 1 29 02FDEA00069 1 20020126 A 3244 TIRE DOUG DC10 DC1030F 3023504 WP MLG BLOWN A FDEA O OTHER G Z MULTIPLE FAILURE SIGNIFICANT FAILURE REPORT LD LANDING 1 SO 25 311FE 46871 DURING FLIGHT TEST ALL MAIN LANDING GEAR TIRES BLEW (10) EA. 2 L 7 3 4F RT A22WE 2002012900073 20020129 00073 EU 2002 1 29 02FDEA00070 1 20020125 A 2910 HYDRAULIC SYSTEM AIRBUS 310 A310203 3930313 EU GREEN SYS LOW A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 428FE 248 DURING CLIMB ECAM IND GREEN HYD RESERVOIR LO LEVEL. 2 L 7 2 4F RT A35EU 2002012900074 20020129 00074 SW 2002 1 29 20021 1 20020116 A 3230 2752000225 ARM SWRNGN SA227 SA227AC 8780603 SW UPLOCK ACTUATOR CRACKED E STZA K NONE O OTHER IN INSP/MAINT 1 AL 03 505FS 28330 NOSE GEAR OPERATED NORMALLY ON JACKS. WHEN SPRING PRESSURE WAS REMOVED FROM UPLOCK ACTUATOR ARM, A LARGE AMOUNT OF PLAY WAS NOTED IN THE LEFT SIDE CAM AND SHAFT, AND THE ARM COULD BE ROTATED INSIDE THE SHAFT 15 DEGREES EITHER WAY. THE ARM WAS REMOVED FROM THE SHAFT, AND A CRACK RUNNING ALMOST THE FULL CIRCUMFERENCE OF THE ARM WAS FOUND AT THE ARM ATTACHMEN T HOLE. THIS CRACK COULD ONLY BE SEEN WITH THE UPLOCK ACTUATOR ARM REMOVED, OR FELT WITH THE SPRING TENSION REMOVED. 2 L 7 2 4T RT A8SW 2002012900090 20020129 00090 WP 2002 1 29 ABXA010680 1 20020108 A 5313 39164311 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 LONGERON 13 RIGHT WAS CRACKED BETWEEN FS 1076 AND FS 1087. REPLACED LONGERON IAW DC-9 SRM 54-30-2. 2 L 7 2 4F A6WE 2002012900091 20020129 00091 WP 2002 1 29 ABXA010681 1 20020124 A 3297 WIRE DOUG DC9 DC941 302207N WP MLG BROKEN A ABXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 23 973AX 47511 WHEN EXTENDING GEAR, LEFT MAIN LANDING GEAR GREEN LIGHT DID NOT COME ON. THREE MISSED APPROACHES INTO RIC. THE CREW US ED THE ALTERNATE GEAR EXTENSION AND HAD TO HOLD ON THE RUNWAY FOR MAINTENANCE UPON LANDING. FOUND BROKEN WIRE 1G13B24N AT CONNECTOR P1-431. REPAIRED WIRE IAW DC-9 WDM 32-61-00. 2 L 7 2 4F A6WE 2002012900103 20020129 00103 NM 2002 1 29 C1HA200283001 1 20020122 A 3350 BATTERY PACK BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 683CA 22490 EXTERIOR EMERGENCY SLIDE LIGHTS INOP AT MAIN CABIN DOORS POS 2L & 2R. REMOVED AND REPLACED BATTERY PACK FOR EXTERIOR SL IDE LIGHTS AFT POSITION. DOORS 2L & 2R OP'S CHECK OK. REF MM 33-50-51. 2 L 7 3 4F A3WE 2002012900114 20020129 00114 NM 2002 1 29 C1HA200293001 1 20020122 A 3350 BATTERY PACK BOEING 727 727212 138407G NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 293AS 21348 MID CABIN CEILING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW 727 MM 33-50-71, SYSTEMS CHECK S GOOD. 2 L 7 3 4F A3WE 2002012900117 20020129 00117 NM 2002 1 29 C1HA200295001 1 20020125 A 3397 WIRE HARNESS BOEING 727 727290 138408W NM CARGO BAY FAULTY A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 295AS 22147 EXTERIOR EMERGENCY EXIT LIGHT ON AFT CARGO DOOR INOP. REMOVED AND REPLACED ELEC CABLE FROM AFT CARGO PIT TO AFT CARGO P IT DOOR FOR EMERGENCY LIGHTING (EXT) IAW STD MAINT PRAC, OPS CHECK OK. 2 L 7 3 4F A3WE 2002012900118 20020129 00118 SO 2002 1 29 C2XA02CL016 1 20020119 A 2530 1095 COFFEEMAKER EMB 145 EMB145LR 3260212 SO GALLEY MALFUNCTIONED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14902 145496 CLE FLIGHT 3057 THE CREW REPORTED THE LEFT HOT JUG HAD BURNT ELECTRICAL SMELL EMITTED WHEN POWER WAS ON. MAINTENANCE PL ACED THE ITEM ON MEL. THE AIRCRAFT WAS RELEASED FOR SERVICE. MAINTENANCE INSPECTED AND REPLACED THE LEFT HOT JUG. OPE RATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002012900119 20020129 00119 SO 2002 1 29 C2XA02CL018 1 20020123 A 3350 66369 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 24517 145332 CLE MAINTENANCE FOUND THE 2ND ROW OF EMERGENCY FLOOR PATH LIGHTING WAS INOPERATIVE DURING ROUTINE MAINTENANCE. MAINTENA NCE REPLACED THE FLOOR LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2002012900120 20020129 00120 NM 2002 1 29 QXEA0200053 1 20020110 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X403 TO X408 HAS CORROSION IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8-200 SRM 51-40- 00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002012900121 20020129 00121 NM 2002 1 29 QXEA0200054 1 20020110 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X390 AND X392 HAS CORROSION IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8-200 SRM 51-40 -00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002012900122 20020129 00122 NM 2002 1 29 QXEA0200055 1 20020110 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X360 TO X362 HAS CORROSION IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8-200 SRM 51-40- 00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002012900123 20020129 00123 NM 2002 1 29 QXEA0200056 1 20020110 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X339 TO X344 HAS CORROSION IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8 RD 8-53-1352, SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002012900124 20020129 00124 NM 2002 1 29 QXEA0200057 1 20020110 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X328 TO X330 HAS CORROSION ON TOP FLANGE AND IN CHANNEL. REPAIRED IAW DHC-8 RD 8-53-1342, SRM 651-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002012900125 20020129 00125 NM 2002 1 29 QXEA0200058 1 20020110 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X309 TO X313 HAS CORROSION ON TOP FLANGE AND IN CHANNEL. REPAIRED IAW DHC-8 RD 8-53-1352, SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002012900126 20020129 00126 NM 2002 1 29 QXEA0200059 1 20020110 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT OUTBOARD SEAT TRACK X296 TO X298 HAS CORROSION ON TOP FLANGE AND IN CHANNEL. REPAIRED IAW DHC-8-200 SRM 51-40- 00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002012900127 20020129 00127 NM 2002 1 29 QXEA0200060 1 20020103 A 3220 ARM DHAV DHC8 DHC8202 2809007 NM NLG GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - NOSE LANDING GEAR LOWER TRAILING ARM IS GOUGED. REPAIRED IAW RD 8-32-289. 2 H 7 2 4T RT A13NM 2002012900128 20020129 00128 NM 2002 1 29 QXEA0200061 1 20020107 A 5350 FRAME DHAV DHC8 DHC8202 2809007 NM TAIL CONE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - REAR FUSELAGE TAIL CONE INTERNAL TOP STRUCTURE FRAME FOUR CASTELLATION IS CRACKED AT STRINGER 4R. REPAIRED IAW DH C-8 RD 8-55-199. 2 H 7 2 4T RT A13NM 2002012900129 20020129 00129 NM 2002 1 29 QXEA0200062 1 20020107 A 5350 FRAME DHAV DHC8 DHC8202 2809007 NM TAIL CONE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - REAR TAIL SECTION INTERNAL FRAME 4 STRINGER 4 HAS CRACK NEAR STATION 700.409. REPAIRED IAW DHC-8 RD 8-55-199. 2 H 7 2 4T RT A13NM 2002012900130 20020129 00130 NM 2002 1 29 QXEA0200063 1 20020111 A 5410 WEB DHAV DHC8 DHC8202 2809007 NM NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - WEB RIVET HOLES FOR SPR BOX INBOARD BRACKET HOLES ARE ELONGATED. REPAIRED IAW HORIZON AIR EA 4-54-214. 2 H 7 2 4T RT A13NM 2002012900132 20020129 00132 NM 2002 1 29 QXEA0200064 1 20020109 A 5410 ANGLE DHAV DHC8 DHC8202 2809007 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - TWO CRACKS NOTED IN VERTICAL ANGLE ADJACENT TO FORWARD SPAR AND NACELLE. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002012900133 20020129 00133 NM 2002 1 29 QXEA0200065 1 20020107 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - AFT FIRE WALL OUTBOARD SIDE HAS CRACK AT Z100, YN12-0. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002012900134 20020129 00134 NM 2002 1 29 QXEA0200066 1 20020110 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - RT SEAT TRACK VENT CRACKED 42 INCHES FROM AFT END. REPAIRED IAW HORIZON AIR EA 2-53-360, DHC-8 SRM 51-40-00 AND S RM 51-40-11. 2 H 7 2 4T RT A13NM 2002012900135 20020129 00135 NM 2002 1 29 QXEA0200067 1 20020109 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - AFT SIDE OF WEB FRAME AT X66 HAS NUMEROUS SCRATCHES. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2002012900136 20020129 00136 NM 2002 1 29 QXEA0200068 1 20020110 A 5220 STOP FITTING DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - EMERGENCY DOOR STOPS HAVE APPROXIMATELY .10 WEAR (FRETTING). REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 4 AND SRM 51-2 0-26, PAGE 7, PARAGRAPH 5A. 2 H 7 2 4T RT A13NM 2002012900137 20020129 00137 EA 2002 1 29 QXEA0200069 1 20020115 A 2611 4462531 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA LAVATORY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 606QX 713 10023 SMF - SMOKE AFT LAV MASTER WARNING MESSAGE CAME ON JUST AFTER TAKEOFF. INSPECTED LAVATORY AND FOUND NO EVIDENCE OF FIRE OR SMOKE. RESET SMOKE DETECTOR. GROUND RAN AIRCRAFT. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002012900138 20020129 00138 NM 2002 1 29 QXEA0200071 1 20020115 A 2760 SWITCH DHAV DHC8 DHC8202 2809007 NM SPOILER CLUTCH LOOSE A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 357PH 504 MFR - IN CRUISE FLIGHT, THE NUMBER 1 SPOILER PUSH-OFF LIGHT ILLUMINATED. CREW PERFORMED EMERGENCY PROCEDURES. MAINTENAN CE FOUND THE SPOILER CLUTCH SWITCH LOOSE AND TIGHTENED SAME. ADJUSTED AND GROUND RAN ENGINES. OPERATIONAL CHECK IS GOO D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002012900147 20020129 00147 NM 2002 1 29 QXEA0200072 1 20020121 A 2730 3993001010 ACTUATOR BOMBDR DHC8 DHC8401 NM ELEVATOR FAILED A QXEA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CR CRUISE 1 NM 09 409QX 707 4051 SEA - AFTER LEVELING AT 23,000 FT, MASTER CAUTION LIGHT WITH ELEVATOR FEEL ANNUNCIATOR WARNING LIGHT ILLUMINATED. AUTO- PILOT WAS TURNED OFF. THERE WAS A NOTICEABLE VIBRATION AT ALL AIRSPEEDS. EMERGENCY CHECKLIST WAS PERFORMED, AIRCRAFT R ETURNED TO FIELD WITHOUT FURTHER INCIDENT. AIRCRAFT DOWN FOR MAINTENANCE. MAINTENANCE REPLACED NR 2 PITCH FEEL ACTUATOR . OPERATIONAL CHECK FLIGHT WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002012900148 20020129 00148 EU 2002 1 29 QXEA0200075 1 20020118 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 498US 11181 SEA- EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECK G OOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002012900149 20020129 00149 EA 2002 1 29 QXEA0200078 1 20020123 A 5610 601R3303310 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 606QX 776 10023 FRESNO - ON FLIGHT FROM EUGENE TO LA, FIRST OFFICERS WINDSHIELD SHATTERED. AIRCRAFT WAS DIVERTED TO FRESNO AND CREW COM PLIED WITH EMERGENCY ABNORMAL CHECKLIST. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT DOWN FOR MAINTENANCE. REP LACED RIGHT WINDSHIELD IAW CRJ-700 MM 56-11-01-000-801-A01. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002012900150 20020129 00150 EU 2002 1 29 QXEA020014 1 20020116 A 3350 5515800106 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 496US 11169 PDX- EMERGENCY EXIT LIGHT ABOVE GALLEY IS OUT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS GOOD. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002012900154 20020129 00154 SO 2002 1 29 C2XA02IA012 1 20020114 A 5320 14529150003 ANGLE EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 7006 145133 IAH- DURING C-CHECK INSPECTION, NOTED: THE RIGHT FLOOR CROSS BEAM LOWER ANGLE HAS CORROSION BETWEEN FR 23 AND 24. MAIN TENANCE CUT OUT THE CORRODED SECTION, FABRICATED AND INSTALLED A NEW SECTION. 2 L 7 2 4F RT T00011AT 2002012900155 20020129 00155 SO 2002 1 29 C2XA02IA014 1 20020122 A 4930 4504401 NOZZLE EMB 145 EMB145LR 3260212 SO APU DIRTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 13955 145075 IAH- FLIGHT 3794, STRONG FUEL SMELL IN CABIN AND COCKPIT WHEN APU STARTED ON APPROACH. MAINTENANCE CLEANED APU START F UEL NOZZLES, PERFORMED A OPERATIONAL CHECK OF THE APU, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. 2 L 7 2 4T RT T00011AT 2002012900156 20020129 00156 EA 2002 1 29 SWIA200210592 1 20020125 A 3222 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA NOSE LANDING GEA DISCONNECTED A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 587SW 7062 DURING LANDING GEAR RETRACTION, NOSE GEAR STAYED EXTENDED WITH GEAR DISAGREE AND WOW INPUT CAUTION MESSAGE AND WOW OUTPU T FAIL STATUS MESSAGE. ALL MESSAGES CLEARED WITH QRH EXCEPT FOR WOW INPUT CAUTION.FOUND NOSE GEAR TORQUE LINK DISCONNEC TED. CHECKED PROX BOX. OK FOR SERVICE. 2 L 7 2 4F RT A21EA 2002012900157 20020129 00157 EU 2002 1 29 C2XA02IA015 1 20020125 A 3242 5012609 BRAKE AEROSP ATR42 ATR42320 8680930 EU MLG MALFUNCTIONED A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 93840 271 ILE- WHILE TAXIING TO THE GATE THE CREW NOTED THAT THE BRAKES LOCKED AND WOULD NOT RELEASE. MAINTENANCE REMOVED AND RE PLACED THE NUMBER THREE (3) MAIN BRAKE ASSEMBLY. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002012900158 20020129 00158 SO 2002 1 29 C2XA02IA016 1 20020125 A 3234 12038594001 CONTROL HANDLE EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A C2XA O OTHER O OTHER AP APPROACH 1 SW 27 17728 120182 FLT 3581 - DURING APPROACH INTO IAH THE CREW COULD NOT GET THE LANDING GEAR EXTENDED. ON THE THIRD ATTEMPT THE GEAR EX TENDED AND THE AIRCRAFT LANDED AT IAH WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTR OL HANDLE. THE GEAR SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 2002012900159 20020129 00159 NM 2002 1 29 CALA0200034 1 20020124 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND SIX FLOOR SUPPORTS CORRODED AT STA 767. A DOUBLER WAS INSTALLED AT EACH FLOOR SUPPORT IAW ECRA 5320-01 603. 2 L 7 2 4F RT A16WE 2002020500039 20020205 00039 EA 2002 2 5 COMA0260068 1 20020125 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 7040 THE LEFT SIDE OF THE FUSELAGE WAS DAMAGED AT STA 379-394 AND STR 23L-24L. REMOVED THE DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F RT A21EA 2002020500037 20020205 00037 EA 2002 2 5 COMA0260067 1 20020127 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 7018 LT FUEL BOOST PUMP ACCESS HOLES ARE CRACKED NR 1 (APPROX.125 INCH LONG BY.020 INCHDEEP), NR 9 (APPROX .200 INCH LONG BY. 040 INCH DEEP) AND NR 11 (APPROX .200 INCH LONG BY .040 INCH DEEP). PERFORMED A MAJOR REPAIR TO LT BOOST PUMP ACCESS HO LE NR 1, 9 AND 11 IAW CRJ REO 601R-57-21-164. 2 L 7 2 4F RT A21EA 2002012900161 20020129 00161 NM 2002 1 29 DHL2002708001 1 20020127 A 2510 GLARE SHIELD BOEING 727 72725 1384006 NM COCKPIT OUT OF POSITION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 F/O'S SLIDING WINDOW IS BINDING AGAINST GLARE SHIELD WHEN TRYING TO OPEN WINDOW. REPOSITIONED GLARE SHIELD AT F/O'S SLI DING WINDOW. OPS CHECK SERVICEABLE PER B727 M/M 56-12-11. 2 L 7 3 4F A3WE 2002012900162 20020129 00162 NM 2002 1 29 DHL2002727001 1 20020124 A 3040 WINDSHIELD WIPER BOEING 727 727228 1384083 NM WINDSHIELD OUT OF ADJ A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 727DH 20204 F/O'S WINDSHIELD WIPER IS NOT WORKING. ADJUSTED WIPER TENSION IAW MM 30-42-42. OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 2002012900166 20020129 00166 CE 2002 1 29 GLBA2002009 1 20020122 A 3260 WARNING SYSTEM BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GLBA O OTHER N FALSE WARNING CL CLIMB 1 NM 03 184UX UE184 LANDING GEAR INTRANSIT LIGHT FAILED TO EXTINGUISH, CYCLED GEAR AGAIN LIGHT REMAINED ON FOR APPROX 1 MINUTE. INSPECTED G EAR INDICATION SYSTEM AND PERFORMED TEST FLIGHT. COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4T RT A24CE 2002021200135 20020212 00135 NE 2002 2 12 GLBA2002010 2 20020122 A 7314 1143890425 PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE FAILED A GLBA O OTHER J WARNING INDICATION CR CRUISE 1 NM 03 247GL 251 UE247 RIGHT LOW PRESSURE FUEL LIGHT ILLUMINATED. REPLACED FUEL PUMP, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2002021200137 20020212 00137 CE 2002 2 12 GLBA2002011 1 20020122 A 3260 H111541 SWITCH BEECH 1900 1900D 1154162 CE LANDING GEAR MALFUNCTIONED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 195GL UE195 LANDING GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH. REPLACED UPLOCK SWITCH, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002012900167 20020129 00167 CE 2002 1 29 GLBA2002012 1 20020123 A 2460 CONNECTOR BEECH 1900 1900D 1154162 CE COCKPIT LOOSE A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 150GL UE150 ANNUNCIATOR POWER SOURCE ILLUMINATED IN FLIGHT. RESEATED CONNECTOR ON PCB, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002012900168 20020129 00168 CE 2002 1 29 GLBA2002013 1 20020126 A 7722 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 202UX UE202 NR 1 ITT INDICATOR FAILED ON T/O ROLL. RESET C/B, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002012900171 20020129 00171 CE 2002 1 29 GLBA2002014 1 20020127 A 2752 1295210502 ACTUATOR BEECH 1900 1900D 1154162 CE T/E FLAP FAILED A GLBA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 03 247GL 8967 1694 UE247 FLAPS WOULD NOT EXTEND. REPLACED RIGHT I/B ACTUATOR, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002012900172 20020129 00172 NM 2002 1 29 LCQ07 1 20020122 A 3211 TRUNNION BOEING 727 727222 1384073 NM RT MLG CRACKED B RRXA K NONE O OTHER IN INSP/MAINT 1 GL 05 7638U 19911 RIGHT MLG TRUNNION ATTACHMENT FITTING INBOARD LUG LWR OUTBOARD FACE HAS MINOR CORROSION. LATER FOUND FITTING TO BE CRAC KED. 2 L 7 3 4F A3WE 2002012900176 20020129 00176 EU 2002 1 29 RAIA00201021 1 20020115 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 551HK 41040 MX-STL- ESCAPE PATH LIGHTS INOP. RECONNECTED PATH LIGHT STRIP CONNECTOR. OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002012900178 20020129 00178 SO 2002 1 29 LR7A02007 1 20020126 A 5311 FRAME LKHEED 382 382G 526414U SO FS 836 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 592 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB0505 FOUND LH FS 836 FRAME FLANGE CRACKED AT LBL 75, WL 195-200 AND LBL 82 , WL 215-220.REPAIRED IAW SRM SMP 583 51-140-19. NR 0021. 2 H 7 4 4T A1SO 2002012900179 20020129 00179 SO 2002 1 29 LR7A02008 1 20020126 A 5230 3391113R FITTING LKHEED 382 382G 526414U SO FS 740 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 592 4606 DURING SCHEDULED B2 INSPECTION NR 0008 ACCOMPLISHMENT FOUND RH RAMP HINGE FITTING CRACKED AT FS 740, RBL 45, WL 142.REPL ACED FITTING IAW DWG 339111. NR 0061. 2 H 7 4 4T A1SO 2002012900180 20020129 00180 SO 2002 1 29 LR7A02009 1 20020126 A 5312 BEAM LKHEED 382 382G 526414U SO FS 537 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 592 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB0505 FOUND RMLG WHEEL WELL FS 537 LOWER BOW BEAM UPPER LUG CRACKED AT RBL 62, WL 200.REPAIRED IAW SRM SMP 583 53-40-14. NR 0084. 2 H 7 4 4T A1SO 2002012900181 20020129 00181 SO 2002 1 29 LR7A02010 1 20020126 A 5312 BEAM LKHEED 382 382G 526414U SO FS 497 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 592 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB0505 FOUND LMLG WHEEL WELL FS 497 LOWER BOW BEAM UPPER LUG CRACKED AT LBL 62, WL 200.REPAIRED IAW SRM SMP 583 53-40-14. NR 0163. 2 H 7 4 4T A1SO 2002012900182 20020129 00182 SO 2002 1 29 LR7A02011 1 20020126 A 5230 33911814 WEB LKHEED 382 382G 526414U SO FS 832.8 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 592 4606 DURING SCHEDULED B2 INSPECTION NR 0192 ACCOMPLISHMENT FOUND FS 832.8 (RAMP STA 8) BELLCRANK MOUNT WEB CRACKED AT BL 0.RE PLACED WEB PER DWG 339118-14. NR 0193. 2 H 7 4 4T A1SO 2002013000001 20020130 00001 SO 2002 1 30 C2XA02TY016 1 20020130 A 3350 20131A BATTERY EMB 145 EMB145 3260210 SO BURNED OUT A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A ROUTINE CHECK THE EMERGENCY PROXIMITY STRIPS WERE OUT. MAINTENANCE R/R #4 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK WAS GOOD. AIRCRAFT WAS REL. TO SERVICE UPON COMPLETION OF WORK. 2 L 7 2 4F RT T00011AT 2002013000011 20020130 00011 SO 2002 1 30 C2XA02IA013 1 20020112 A 2120 ODOR EMB 145 EMB145ER 3260211 SO CABIN DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14947 145054 IAH- FLIGHT 4106, WHEN STARTING APU IN THE AIR THE CABIN IS FILLED WITH A STRONG OIL BURNING SMELL (NO SMOKE) FOR SEVER AL MINUTES. MAINTENANCE CLEANED RESIDUAL OIL FROM APU COMPARTMENT, PERFORMED A OPERATIONAL CHECK OF THE APU, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002013000012 20020130 00012 EU 2002 1 30 RAIA00201022 1 20020116 A 7722 CONTACTOR JETAIR JETSTM JETSTM4101 1500501 EU EGT RAKE DIRTY A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 574HK 41093 5519-GRR- RIGHT ENGINE EGT FLUX WITH INTEGRATED ELECTRONIC CONTROL FAULT. MAINTENANCE CLEANED CONTACTS AT EGT RAKE, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002013000013 20020130 00013 SO 2002 1 30 C2XA02CL024 1 20020125 A 2761 3604401003 ACTUATOR EMB 135 EMB135LR 3260305 SO RIGHT WING LEAKING A C2XA A O UNSCHED LANDING OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 12519 1975 145366 CLE FLIGHT#4015 THE CREW REPORTED THE #1 HYDRAULIC SYSTEM INDICATED ZERO QUANTITY IN FLIGHT.THE AIRCRAFT RETURNED TO CLE VELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE RIGHT WING SPOILER ACTUATOR LEAKING.THE A CTUATOR WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2002013000014 20020130 00014 2002 1 30 RAIA00201023 4 20020117 A 3418 STALL WARNING EMB 145 EMB145 3260210 SO COCKPIT MALFUNCTIONED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 802HK 145066 5281-TOL- STALL PROTECTION SYSTEM NR 2 INOP ALERT MESSAGE ON TAKEOFF ROLL. MAINTENANCE INSPECTED AOA VANE AND OPERATION AL CHECKED SYSTEM, NO DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 2002013000016 20020130 00016 2002 1 30 RAIA00201024 4 20020117 A 3418 STALL WARNING EMB 145 EMB145 3260210 SO COCKPIT MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 806HK 145112 5303- PIT- FLAP FAIL/STALL PROTECTION SYSTEM ADVANCED MESSAGE AFTER TAKEOFF. MAINTENANCE RESET FLAP SYSTEM, SYS OPS CHE CK OK. 2 L 7 2 4F RT T00011AT 2002013000017 20020130 00017 NE 2002 1 30 RAIA00201025 2 20020119 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LEFT FAILED A RAIA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 CE 03 550HK 41039 75104 5473-STL- LEFT ENGINE CONTAM LIGHT ILLUMINATED FOLLOWED BY ENGINE IN-FLIGHT FAILURE. MAINTENANCE REMOVED AND REPLACED T HE LEFT ENGINE. 2 L 7 2 4T 4 T RT A41NM E18NE 2002013000018 20020130 00018 2002 1 30 RAIA00201026 4 20020120 A 3418 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU STALL WARNING FAULTY A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 565HK 41082 5512-STL LEFT STALL CAPTION LIGHT ILLUMINATED DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE LEFT AOA SENSOR. 2 L 7 2 4T RT A41NM 2002013000019 20020130 00019 SO 2002 1 30 RAIS00201004 1 20020106 A 2740 WARNING SYSTEM EMB 145 EMB145 3260210 SO COCKPIT MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 801HK 145053 5278-GRR- CREW REPORTED MAIN PITCH TRIM FAILED AFTER TAKEOFF. MAINTENANCE DID FUNCTIONAL CHECK OF PITCH TRIM SYSTEM. S YS OPS CHECK OK. 2 L 7 2 4F RT T00011AT 2002013000020 20020130 00020 EU 2002 1 30 EGR2002F00000 1 20020112 A 2701 365A25315322 CONTROL COLUMN AEROSP AS365 AS365N2 8680815 EU CYCLIC BINDING E EGRA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 17 272NE 6435 CYCLIC CONTROL BINDING LATERALLY IN FLIGHT. CORROSION BETWEEN AND AROUND AREA OF RIVETS AT CENTER OF GIMBAL. ALSO EXCE SSIVE VIBRATION MAY HAVE CAUSED CYCLIC FATIGUE. REPLACE CRACKED ALLUMINUM WITH STRINGER STEEL GIMBAL. 1 G 7 2 3U RT H10EU 2002013000021 20020130 00021 CE 2002 1 30 IJA2002F00000 1 20020114 A 3233 5081016418 ACTUATOR BEECH 90 C90 1152913 CE PWA PT6 PT6* 52043 EA RT MAIN GEAR BINDING E IJAA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 CE 07 402EM 4644 4644 LJ914 PILOT REPORTED VIBRATION DURING GEAR EXTENSION AND RETRACTION. INVESTIGATION SHOWED THAT RIGHT MAIN GEAR ACTUATOR WAS B INDING AND CAUSING GEAR TO OSCILLATE DURING TRANSIT. ACTUATOR EMMITTED A HIGH PITCHED SQUEAL WHILE GEAR WAS IN TRANSIT. ACTUATOR WAS REPLACED WITH SERVICEABLE UNIT AND GEAR RIGGED. OPERATIONS WERE NOTED TO BE NORMAL AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 3 T 3A20 E2NE 2002013000024 20020130 00024 SO 2002 1 30 C2XA02CL025 1 20020129 A 2742 3622001009 ACTUATOR EMB 145 EMB145ER 3260211 SO TAIL INOPERATIVE A C2XA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 14925 8082 4636 145004 CLE FLIGHT#3230 THE CREW REPORTED BOTH CAPTAINS AND FIRST OFFICER'S PITCH TRIM DID NOT WORK.MAINTENANCE INSPECTED AND RE PLACED THE HORIZONTAL STABILIZER ACTUATOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002013000027 20020130 00027 NM 2002 1 30 SWAA020082 1 20020114 A 3350 300432 LIGHT BOEING 737 7372H4 138448C NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED RON, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AFT OF AFT SVC DOOR. RELAMPED LIGHT PER MM. 2 L 7 2 4F A16WE 2002013000028 20020130 00028 2002 1 30 SWAA020084 4 20020114 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002013000029 20020130 00029 NM 2002 1 30 SWAA020087 1 20020113 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM ENTRY DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 602SW 27953 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002013000030 20020130 00030 NM 2002 1 30 SWAA020091 1 20020111 A 3350 BR2013 SOCKET BOEING 737 7372T4 1384492 NM CABIN DEFECTIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 EEPLS INOP AT OVERWING EMERGENCY EXIT. REMOVED AND REPLACED LIGHT SOCKET PER MM. 2 L 7 2 4F A16WE 2002013000031 20020130 00031 NM 2002 1 30 SWAA020093 1 20020113 A 3350 6104781 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP BOTH LT AND RT IN AFT CABIN. REMOVED AND REPLACED BATT ERY PER MM. 2 L 7 2 4F RT A16WE 2002013000032 20020130 00032 NM 2002 1 30 SWAA020094 1 20020112 A 3040 5717623122 SLIDING WINDOW BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 07 797MX 27890 ELECTRICAL SMELL AND SMOKE DUE TO F/O'S SLIDING WINDOW ARCING. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2002013000033 20020130 00033 NM 2002 1 30 SWAA020096 1 20020112 A 5311 96380 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED 1/4D CHECK, FOUND RT SIDE CHORD CRACKED AT BS 178, WL 207 AND RBL 28. REMOVED AND REPLACED CHORD PER S WA ACO. 2 L 7 2 4F RT A16WE 2002013000034 20020130 00034 NM 2002 1 30 SWAA020097 1 20020114 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2) AT STR 8R, BS 520 AND 639. REMOVED AND REPLACED STR CLIPS PE R SRM. 2 L 7 2 4F RT A16WE 2002013000035 20020130 00035 NM 2002 1 30 SWAA020098 1 20020114 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (3) AT STR 8L, BS 482A, 482B AND 520. REMOVED AND REPLACED STR C LIPS PER SRM. 2 L 7 2 4F RT A16WE 2002013000036 20020130 00036 NM 2002 1 30 SWAA020099 1 20020114 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002013000037 20020130 00037 NM 2002 1 30 SWAA020101 1 20020114 A 2170 V1211 COALESCER BAG BOEING 737 7377H4 1384404 NM A/C BAY CONTAMINATED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 411WN 29821 AIR TURNBACK, AFTER T/O THERE WAS A PUNGENT ELECTRICAL ODOR IN THE CABIN ACCOMPANIED BY FAILURE OF ELECTRIC STAB TRIM ON BOTH SIDES. ELECTRIC TRIM BEGAN WORKING AFTER LANDING. REMOVED AND REPLACED WATER SEPARATOR BAGS PER MM AND OPS CK'D STAB TRIM PER MM, NO DISCREPANCIES FOUND. 2 L 7 2 4F RT A16WE 2002013000038 20020130 00038 NM 2002 1 30 SWAA020106 1 20020115 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 26R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002013000039 20020130 00039 2002 1 30 SWAA020108 4 20020114 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM CABIN DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDES PRESS IND OUT OF VIEW. REPOSITIONED SLIDES P ER MM. 2 L 7 2 4F A16WE 2002013000040 20020130 00040 NM 2002 1 30 SWAA020110 1 20020115 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002013000041 20020130 00041 NM 2002 1 30 SWAA020111 1 20020115 A 5230 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT AFT LOWER CORNER. REPAIRED DOOR FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002013000042 20020130 00042 NM 2002 1 30 SWAA020113 1 20020117 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002013000043 20020130 00043 2002 1 30 SWAA020116 4 20020116 A 2565 D31354 GIRT BAR BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED GIRT ASSY PER MM . 2 L 7 2 4F RT A16WE 2002013000044 20020130 00044 NM 2002 1 30 SWAA020117 1 20020116 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM PAX ENTRYWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE FLOOR GIRT BAR BRACKETS (FWD AND AFT) CORRODED. REMOVED AND REPLACED BOTH BRACKETS PER SRM & MM. 2 L 7 2 4F RT A16WE 2002013000045 20020130 00045 NM 2002 1 30 SWAA020120 1 20020116 A 3230 VO4638 SENSE LINE BOEING 737 7373H4 1384600 NM RT MLG OUT OF ADJ A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 316SW 23338 AIR TURNBACK, AFTER T/O, LANDING GEAR HANDLE WOULD NOT GO THE UP POSITION. ADJUSTED GROUND SENSE CABLE, OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2002013000046 20020130 00046 NM 2002 1 30 SWAA020121 1 20020118 A 3350 6556633 LENS BOEING 737 7373Y0 1384671 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002013000047 20020130 00047 2002 1 30 SWAA020123 4 20020119 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM CABIN DOOR OUT OF ADJ A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 785SW 30602 DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDES GIRT ASSY OUT OF ADJUST. ADJUSTED BOTH AFT S LIDES PER MM. 2 L 7 2 4F RT A16WE 2002013000048 20020130 00048 NM 2002 1 30 SWAA020125 1 20020117 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT SEVERAL LOCATIONS IN CABIN. RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2002013000049 20020130 00049 NM 2002 1 30 SWAA020127 1 20020118 A 3350 65C27093 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED C2 CHECK, FOUND BOTH LT CABIN DOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2002013000050 20020130 00050 2002 1 30 SWAA020128 4 20020119 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002013000053 20020130 00053 NM 2002 1 30 SWAA020134 1 20020118 A 5311 96380 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 602SW 27953 DURING SCHEDULED SPECIAL VISIT, FOUND RT SIDE CHORD CRACKED AT BS 178, WL 207 AND RBL 24.0. REMOVED AND REPLACED SIDE C HORD PER SWA ACO. 2 L 7 2 4F RT A16WE 2002013000054 20020130 00054 2002 1 30 SWAA020135 4 20020121 A 2565 D31591 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR DEFECTIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 621SW 28037 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002013000055 20020130 00055 NM 2002 1 30 SWAA020136 1 20020121 A 2560 61020 BATTERY BOEING 737 7373Y0 1384671 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED RON, FOUND EMERGENCY FLASHLIGHT INOP IN AFT CABIN TOP POSITION. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002013000056 20020130 00056 2002 1 30 SWAA020137 4 20020119 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER WHEN DOOR CLOSED. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002013000059 20020130 00059 NM 2002 1 30 SWAA020139 1 20020121 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 640SW 27713 DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002013000060 20020130 00060 NM 2002 1 30 SWAA020140 1 20020120 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 750SA 29802 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW NR 24. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002013000062 20020130 00062 NM 2002 1 30 SWAA020141 1 20020120 A 3350 6104789 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EXIT LIGHTS DIMMED. REMOVED AND REPLACED BATTERY PE R MM. 2 L 7 2 4F RT A16WE 2002013000063 20020130 00063 2002 1 30 SWAA020142 4 20020120 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 648SW 27718 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002013000064 20020130 00064 NM 2002 1 30 SWAA020146 1 20020120 A 5311 654653654 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT BS 559, STR 14R. REPAIRED FRAME CHORD PER SWA RA. 2 L 7 2 4F RT A16WE 2002013000065 20020130 00065 NM 2002 1 30 UHL2002F00000 1 20020103 A 2100 7707277 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE PK TMP CNTRL VLV STUCK A UHLA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NE 03 816EX 329 SMOKE IN CABIN. STARTED NR 2 ENGINE, THEN AFTER START OF NR 1 ENGINE, SMOKE IN COCKPIT. UPON INSPECTION, DISCOVERED DU CT TEMPERATURE AT 60 DEGREE C, OIL BLEED SYSTEM CAUSED BY STUCK PACK TEMP-CONTROL VALVE (FULL HOT) DISCONNECTED VALVE L INKAGE, CYCLED VALVE MANUALLY, RECONNECTED LINKAGE AND OPS CHECKED GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2002013000066 20020130 00066 NM 2002 1 30 SWAA020148 1 20020121 A 5320 6551698 SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002013000067 20020130 00067 NM 2002 1 30 SWAA020150 1 20020121 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 619SW 28035 DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002013000070 20020130 00070 2002 1 30 SWAA020151 4 20020121 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 619SW 28035 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLID E PER MM. 2 L 7 2 4F RT A16WE 2002013000071 20020130 00071 NM 2002 1 30 SWAA020152 1 20020122 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002013000072 20020130 00072 2002 1 30 SWAA020153 4 20020121 A 2565 D31354 SLIDE BOEING 737 7372K6 1364440 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002013000074 20020130 00074 NM 2002 1 30 SWAA020155 1 20020118 A 2612 100064901 FIRE DETECTOR BOEING 737 7373H4 1384600 NM CARGO BAY MALFUNCTIONED A SWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 628SW 27703 DECLARED EMERGENCY AND AIR TURNBACK, SHORTLY AFTER T/O FWD CARGO BAY FIRE ALARM LIGHT ILLUMINATED WITH AUDIO ALARM. EXE CUTED THE CHECKLIST, FIRED BOTH BOTTLES. INSPECTED FWD CARGO BIN, NO EVIDENCE OF FIRE OR OVER HEATING. OK TO CONTINUE PER MEL. LATER AT BWI, REMOVED AND REPLACED CCU, FIRE BOTTLES, METERING VALVE, DIVERTER VALVE AND 4 EA SDU'S FOR FWD C ARGO. PERFORMED PRESS LEAK AND FIRE SUPPRESSION SYSTEM FUNCTIONAL TEST PER MM. SYSTEM TEST NORMAL, NO FAULTS FOUND. 2 L 7 2 4F RT A16WE 2002013000075 20020130 00075 CE 2002 1 30 VE72002F00000 1 20020108 A 3210 NAS561P628 PIN CESSNA CESSNA 441 441 2076020 CE TRUNNION SHEARED E VE7A K NONE O OTHER IN INSP/MAINT 1 WP 07 687AE 4614 4410087 DUE TO SLOTTED PIN FAILURE OF 4410175 THIS AIRCRAFT WAS INSPECTED AND FOUND TO HAVE BOTH FORWARD SLOTTED PINS ON THE MAI N LANDING GEAR TRUNION PIVOT PINS PARTIALLY SHEARED. PINS LOCATED ON FORWARD POSITION LEFT AND RIGHT MAIN LANDING GEAR TRUNNION. 1 L 7 2 3T RT A28CE 2002013000076 20020130 00076 CE 2002 1 30 VE72002F00001 1 20020108 A 3210 NAS561P628 PIN CESSNA CESSNA 441 441 2076020 CE GARRTT TPE331 TPE331* 01514 WP MLG TRUNNION SHEARED E VE7A K NONE O OTHER IN INSP/MAINT 1 WP 07 988AE 4506 4410175 DUE TO SLOTTED PIN FAILURE OF THE OTHER GEAR THIS PIN WAS INSPECTED AND FOUND TO BE PARTIALLY SHEARED. PIN WAS REPLACED WITH NEW NAS561P628 PIN. THE AFT TRUNION SLOTTED PINS ON BOTH MAIN GEAR WERE INSPECTED WITH NO DEFECTS NOTED BUT WERE REPLACED WITH NEW. PIN WAS LOCATED ON THE FORWARD POSITION OF RIGHT MAIN GEAR TRUNION. 1 L 7 2 3T 3 T RT A28CE E2WE 2002013000077 20020130 00077 CE 2002 1 30 VE72002F00002 1 20020108 A 3210 NAS561P628 PIN CESSNA CESSNA 441 441 2076020 CE GARRTT TPE331 TPE331* 01514 WP TRUNNION SHEARED E VE7A K NONE O OTHER IN INSP/MAINT 1 WP 07 988AE 4487 4410175 PREFLIGHT INSPECTION FOUND LANDING GEAR PIVOT PIN BACKED OUT OF TRUNION DUE TO SLOTTED PIN BEING SHEARED. SAFETY WIRE U SED TO RETAIN PIN WAS ALSO SHEARED BUT DUE TO ITS LENGTH AND DIAMETER. IT STAYED IN THE TRUNION GIVING THE IMPRESSION T HAT IT WAS SECURE. LT MAIN LANDING GEAR FORWARD PIVOT PIN. 1 L 7 2 3T 3 T RT A28CE E2WE 2002013000085 20020130 00085 SO 2002 1 30 VJ32002F00004 2 20020111 A 7414 DISTRIBUTOR BLK SLICK BEECH 33 F33A 1151425 CE CONT O520 IO520B 17032 SO MAGNETO DAMAGED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 8173C 502 01051694 CE1541 MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNE TO. CARBON BRUSH WEAR ON THE SIDE OF DISTRIBUTOR BLOCK ASSEMBLY, SHAFT SENT TO MFG FOR INSPECTION. NEW DISTRIBUTOR BLO CK ASSEMBLY INSTALLED IN MAGNETO. 1 L 7 1 3O 3 O 3A15 E5CE 2002013000089 20020130 00089 SO 2002 1 30 WVB2002F00000 1 20020109 A 5343 CHANNEL PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA NLG WW CRACKED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 3582P 24320 318052103 DURING INSPECTION OF THE HYDRAULIC POWER PACK IT WAS DISCOVERED THAT THE CHANNEL THAT REINFORCES THE NOSE WHEEL TUNNEL W HERE THE NOSE GEAR ACTUATOR ATTACHES HAD CRACKED ON THE FORWARD CUTOUT FOR THE HYDRAULIC POWER PACK RELIEF VALVE THE CHA NNEL WAS REMOVED AND INSPECTED WHERE IT WAS DISCOVERED THAT THE OUTBOARD BOLT HOLE FOR THE NOSE GEAR ACTUATOR BRACKET WA S ELONGATED AND CRACKED ON THE BOTTOM SIDE THE PART WAS REMOVED AND REPLACED. IT IS RECOMMENDED THAT THE NOSE GEAR ACTU ATOR ATTACH BRACKET BOLTS BE CHECKED PERIODICALLY FOR SECURITY DURING LANDING GEAR INSPECTIONS AS IT IS SUSPECTED THAT T HE LOOSE BOLT CAUSED THE PART TO STRESS AND CRACK DURING GEAR OPERATIONS. 1 L 7 2 3O 3 O A20SO E14EA 2002013000095 20020130 00095 NE 2002 1 30 ANCF200200002 2 20020121 A 7310 44A2562 SWITCH BOEING 757 757236 1384971 NM RROYCE RB211 RB211535C37 54555 NE LT ENGINE MALFUNCTIONED W ANCF D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 99 951PG 29545 22185 30102 DURING TAKE OFF LEFT ENGINE N3 WENT TO OVER SPEED AND SHOWED DIFFERENCE BETWEEN ENGINE PARAMETERS, LH ENGINE HIGHER THAN THE RT, THE ENGINE DIDN’T SHUT DOWN, THE CREW PROCEEDED TO RETURN TO EDR. CORRECTIVE ACTION: PERFORMED BITE TO BVCU, FOUND ALTITUDE SWITCH FAIL CODE; THE ALTITUDE SWITCH S1042 WAS REPLACED IAW AMM 75-32-07 ADDITIONALLY, SWAPPED THE FUEL FLOW GOVERNOR IAW AMM 76-11-000 PAGE 532 ALSO PERFORMED RIGGING TO FUEL FLOW SYSTEM IAW AMM 71-11-00, LH ENGINE RUN UP PERFORMED IAW AMM 71-00-00, WITH SATISFACTORY RESULTS. 2 L 7 2 4F 4 F RT A2NM E12EU 2002013000096 20020130 00096 NM 2002 1 30 ANCF200200003 1 20020125 A 2840 LG1136AA01 INDICATOR BOEING 767 767284 1385184 NM PWA 4056 PW4056 NE RT FUEL TANK MALFUNCTIONED W ANCF A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 99 988AN 42978 24742 DURING FLIGHT WITH NORMAL FUEL FLOW THE RT TANK SHOWED DIFFERENCE BETWEEN TOTAL FUEL QTY AND FUEL QTY OF FMC ADDITIONALL Y, WAS PRESENTED FUEL DISAGREE PROG 2, AND FUEL CONFIGURATION WAS PRESENT TWICE. CREW PROCEEDED TO RETURN TO EDR. CORR ECTIVE ACTION: PERFORMED TROUBLE SHOOTING IAW FIM 24-41-00; THE FQIS BITE SHOWED D3 FAIL CODE, SO THE DENSITOMETER OF RH TANK WAS REPLACED IAW AMM 28-41-03/401. THE FUEL QTY INDICATION WAS CHECKED WITH ENGINE RUNNING IAW AMM 71-00-00 WITH SATISFACTORY RESULTS; ADDITIONALLY, WAS CHECKED RH TANK FOR LEAK EVIDENCE AND NO FOUND ANY FUEL LEAK EVIDENCE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002021300057 20020213 00057 NM 2002 2 13 2002UALA00112 1 20020120 A 5330 148W23152 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 773UA 26368 26929 REPAIRED FUSELAGE SKIN STATION 2365 LBL 14. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002021300058 20020213 00058 NM 2002 2 13 2002UALA00113 1 20020119 A 5315 141W85191 FLOORBEAM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 773UA 26368 26929 THE BODY STATION 246 FLOORBEAM MID CHORD IS CRACKED IN -T- FLANGE RADIUS LBL 7.88. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002013000098 20020130 00098 NM 2002 1 30 2002UALA00130 1 20020120 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 CABIN FLOORBEAM STATION 365 RBL 39 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE AND TOP STRAP ON FLOORB EAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002013000099 20020130 00099 EA 2002 1 30 COMA0260069 1 20020127 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 819CA 3202 7415 FLIGHT 5480 GEAR DISAGREE WARNING DURING GEAR EXTENSION.REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002013000100 20020130 00100 EA 2002 1 30 COMA0260070 1 20020126 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 982CA 3362 7168 FLIGHT 5032 GEAR DISAGREE WARNING AFTER T/O.REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2002013000101 20020130 00101 EA 2002 1 30 COMA0260071 1 20020126 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 965CA 7131 FLIGHT 5773 LOUD SQUEAL FROM SERVICE DOOR AREA. CABIN DOOR WITNESS MARKS NOT ALIGNED.FOUND STAIR HANDRAIL NOT STOWED PRO PERLY DUE TO BENT PIN RETAINING BRACKET. REPOSITIONED BRACKET. 2 L 7 2 4F RT A21EA 2002013000102 20020130 00102 EA 2002 1 30 COMA0260072 1 20020125 A 3020 300013000003 VALVE CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 719CA 8653 7253 FLIGHT 5519 R/H ENG COWL ANTI-ICE CAUTION MESSAGE.REPLACED THE R/H COWL ANTI ICE VALVE. 2 L 7 2 4F RT A21EA 2002013000103 20020130 00103 EA 2002 1 30 COMA0260073 1 20020125 A 2150 7536893 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA ACM DIRTY A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 932CA 7038 FLIGHT 5561 LARGE AMOUNT OF SMOKE IN CABIN AND COCKPIT AFTER T/O.REPLACED THE WATER COALESCER SOCKS. OPERATIONAL CHECK O F A/C SYSTEM SATISFACTORY. 2 L 7 2 4F RT A21EA 2002013000104 20020130 00104 NM 2002 1 30 CALA0200054 1 20020129 A 5512 SKIN BOEING 737 7373T0 1384582 NM L/H HOR STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND A 3/4" CRACK IN L/H HORIZONTAL STABILIZER SKIN AT REAR SPAR APPROXIMATELY 65" FROM I/B AREA. THE CRACKE D AREA WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01613. 2 L 7 2 4F RT A16WE 2002013000105 20020130 00105 NM 2002 1 30 CALA0200055 1 20020129 A 5230 SKIN BOEING 737 737524 1384721 NM AFT CARGO DR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33635 26339 THE AFT CARGO DOOR SKIN WAS DENTED IN TWO PLACES BY A BELTLOADER. ONE DENT WAS WITHIN LIMITS AND WAS REWORKED TO INITIAL CONTOUR. A DOUBLER WAS INSTALLED AT THE SECOND DENT IAW SRM 52-00-01, FIGURE 203. 2 L 7 2 4F RT A16WE 2002013000106 20020130 00106 NM 2002 1 30 CALA0200056 1 20020129 A 5414 SKIN BOEING 737 7373T0 1384582 NM #2 ENG PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND A 0.2" CRACK AT O/B AFT CORNER OF #2 PYLON I/B UPPER ACCESS SKIN PANEL #5827. A REPAIR DOUBLER WAS INST ALLED IAW ECRA 5430-01230. 2 L 7 2 4F RT A16WE 2002013000107 20020130 00107 NM 2002 1 30 UPS02237520 1 20020110 A 5330 SKIN BOEING 727 727185C 138406N NM BS441 STR18R-22R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:C FUSELAGE CIRCUMFERENTIAL 441 EXHIBIT 10% MATERIAL LOSS STINGER 20R THRU STRINGER 22R. REMOVED FAST ENERS FROM REPAIR AREA, CUT OUT CORROSION ON FUSELAGE SK IN BS 441 FROM STR 18R TO STR 22R IAW EO B727-5310-1371. SIZE O F CUT OUT 4.5" X 34.5". INSTALLED REPAIR AT FUSELAGE SKIN BS 441 FWD SKIN OUT FROM STR 18R TO STR22R AS PER EOB727-531 0-1371. R&R EXISTING DO UBLER AFT SKIN BUTT STA 441 LAP SEAM AS PER B727 SRM 53-30-3. 2 L 7 3 4F A3WE 2002013000108 20020130 00108 NM 2002 1 30 UPS02237521 1 20020110 A 5330 SKIN BOEING 727 727185C 138406N NM BS259.5 STR10RT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:C CIRCUMFERENTIAL 259.5 EXHIBIT MATERIAL LOSS OF 10% AT STR 10RT. REMOVED FASTENERS & CUT OUT DAMAGE SKIN AS PER DRW 69-62161, SIVE OF CUT OUT 3.5" X 4.25". INSTALLED DOUBLER REPAIR AS PER EO B727-5310 -1371 APPENDIX E . DOUBLER SIZE 8" X 6". 2 L 7 3 4F A3WE 2002013000109 20020130 00109 NM 2002 1 30 UPS02237522 1 20020108 A 5330 SKIN BOEING 727 727185C 138406N NM BS640-660 6LT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:C FUSELAGE SKIN MISSING RIVET HEAD AT LAP JOINT 6LT AND SOME OTHER RIV ETS ARE DISHED BS 640 TO 660. REMOVED RIVETS AT FUSELAGE SKIN LAP JOINT 6LT FROM FS640 TO 660 AND FOUND CORROSION ON LOWER SKIN FS 650 OUT OF LIMITS. CUT OUT DAMAGED AREA AT FS 650 STR60 IAW SRM 53-30-3, SIZE OF CUT OUT 5" X 3". INST ALLED DOUBLER REPAIR IAW BOEING CO MPANY SERVICE ENG. UPS MIA-02-000- 1H & SRM53-30-3. 2 L 7 3 4F A3WE 2002013000110 20020130 00110 NM 2002 1 30 2002F00046 1 20020112 A 2450 21B731E CONTROL PANEL BOEING 747 747230B 1384889 NM COCKPIT MALFUNCTIONED A Q2SA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 743SA 22671 BLOCK TURN BACK, NR 3 GEN AFTER ENGINE START FIELD TRIPPED AND WOULD NOT REST. RERACKED NR 3 GENERATOR CONTROL PANEL RA N NR 3 ENGINE AT IDLE POWER NR 3 FIELD AND GENERATOR BREAKER CLOSED NORMALLY VOLTAGE AND FREQUENCY WITHIN LIMITS. OPS C HECK GOOD. (M) 2 L 7 4 4F A20WE 2002013000111 20020130 00111 SO 2002 1 30 2002F00047 1 20020112 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A MASA K NONE N FALSE WARNING CL CLIMB 1 SW 07 832MJ 145310 FLT 5781 - HAD A MOMENTARY LAVATORY SMOKE DETECTION ON EICAS AFTER TAKEOFF FROM CLT. NO SMOKE WAS EVIDENT AND MSG CLEAR ED ON ITS OWN. ONCE A/C ARRIVED IN TYS, MAINTENANCE INSPECTED LAVATORY SMOKE DETECTOR AND PERFORMED OP CHECK. OP CHECK S GOOD. (M) 2 L 7 2 4T RT T00011AT 2002013000118 20020130 00118 EA 2002 1 30 2002F00054 1 20020106 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27318 7318 WHILE PERFORMING AN EXTERIOR LIGHT CHECK, THE CREW FOUND A RIGHT EXTERIOR FORWARD EMERGENCY LIGHT INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE BULB AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002013000119 20020130 00119 EA 2002 1 30 2002F00055 1 20020107 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27173 7173 DURING A PREFLIGHT INSPECTION, THE CREW FOUND THE EMERGENCY FLOOR LIGHT STRIPS 2 THROUGH 5 INOPERATIVE. MAINTENANCE REP LACED THE NR 2 EMERGENCY BATTERY PACK AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002013000126 20020130 00126 NE 2002 1 30 2002F00042 2 20020106 A 7320 FMU AIRBUS 320 A320233 3930329 EU IAE V2527 V2527EA5 NE NR 2 ENGINE MALFUNCTIONED A SOKF O OTHER M OVER TEMP CL CLIMB 1 SO 23 464TA 1353 SJO - FLT 660 - DURING TAKEOFF CLIMB, ENGINE NR 2 HAVE EGT OVERLIMIT BEFORE 1,000 FEET, THIS CONDITION WAS FOR 13 SECOND S EGT PARAMETER WAS 639'C AND N2 98.2 PERCENT. PERFORMED TROUBLESHOOTING IAW AMM 77-00-810, INSPECTED ENGINE INLET AND EXHAUST, FOUND NO DAMAGE. REMOVED AND REPLACED LOW PRESSURE COMPRESSOR MASTER BLEED ACTUATOR. REMOVED AND REPLACED FUE L METERING UNIT, PERFORMED BORESCOPE INSPECTION FOUND NO DAMAGE. PERFORMED ENGINE RUN UP. ALL PARAMETERS SATISFACTORY AND AIRCRAFT RELEASED TO NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A28NM E40NE 2002013000128 20020130 00128 SO 2002 1 30 ASOA02001 1 20020103 A 5320 12046963001 BUTTSTRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 283AS 120236 DURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND STATION 6653.1. MA INTENANCE REMOVED THE CORRODED BUTT STRAP IAW SRM 51-40-02. A NEW BUTT STRAP WAS LOCATED AND DRILLED IAW SRM 51-25-05. MAINTENANCE INSTALLED THE NEW BUTT STRAP IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002013000129 20020130 00129 SO 2002 1 30 ASOA02002 1 20020103 A 5320 12046158001 BUTTSTRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 283AS 120236 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT BUTT STRAP BETWEEN FRAMES 25 AND 30. MAINTENANCE REMO VED THE CORRODED BUTT STRAP IAW SRM 51-40-02. A NEW BUTT STRAP WAS LOCATED AND DRILLED IAW SRM 51-25-05. MAINTENANCE I NSTALLED THE NEW BUTT STRAP IAW WITH SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002013000130 20020130 00130 SO 2002 1 30 ASOA02003 1 20020103 A 5320 SILL EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 283AS 120236 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT SILL PLATE BETWEEN FRAMES 15A AND STATION 6653.1. MAI NTENANCE REMOVED THE LEFT BUTT SILL PLATE. MAINTENANCE LOCATED, DRILLED, ALODINED, AND PRIMED HOLED ON NEW SILL PLATE I AW SRM 51-25-05 AND 51-25-06. THE NUT PLATES AND THE NEW SILL PLATE WERE INSTALLED IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002013000131 20020130 00131 SO 2002 1 30 ASOA02004 1 20020104 A 5330 12019230001 SKIN EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 232AS 120036 DURING A HANGAR INSPECTION IN MCN, CORROSION WAS FOUND ON THE SKIN AT FRAME 21, BETWEEN STRINGER 21 LEFT AND 21 RIGHT. MAINTENANCE REPAIRED CORRODED FRAME IAW ASA EO120-53-0172. THE EO REF ASA EO120-53-0055, SRM 51 AND 53, EXT 290/96, 246 /95, AND 283/96. THIS EO INCLUDES REPAIR SPECIFICATIONS FOR AIRCRAFT. (M) 2 L 7 2 4T RT A31SO 2002013000132 20020130 00132 EA 2002 1 30 ASOA02006 1 20020106 A 3260 16215105 BRACKET CNDAIR CL600 CL6002B19 1900309 EA NLG BENT A ASOA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 857AS 7411 FLT 4404 - AFTER TAKEOFF FROM ATL, THE NOSE LANDING GEAR WOULD NOT RETRACT AND STAYED DOWN AND LOCKED AFTER THE GEAR WAS SELECTED UP. AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO ATL AND MADE AN OVERWEIGHT LANDING. MAINTENANCE PERFORM ED AN OVERWEIGHT LANDING INSPECTION IAW THE CRJ MX MANUAL AND NO DEFECTS WERE NOTED. MAINTENANCE REMOVED AND REPLACED T HE NOSE GEAR PROXIMITY SWITCH BRACKET, WHICH WAS FOUND TO BE BENT. MAINTENANCE ADJUSTED THE PROXIMITY SWITCH AND SWUNG THE GEAR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002013000133 20020130 00133 SO 2002 1 30 ASOA02007 1 20020103 A 5347 12016000003 SEAT TRACK EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 283AS 120236 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT FORWARD SEAT TRACK BETWEEN FRAMES 15 AND 32. MAINTEN ANCE REMOVED THE CORRODED SEAT TRACK IAW SRM 51-40-02. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED THE NEW SEAT TRACK IAW AMM 53-01-05. (M) 2 L 7 2 4T RT A31SO 2002013000134 20020130 00134 SO 2002 1 30 ASOA02008 1 20020103 A 5313 12026335013 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 283AS 120236 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON STRINGER 21 LEFT BETWEEN FRAMES 9 AND 15. MAINTENANCE REMOVED THE CORRODED STRINGER AND INSTALLED THE NEW STRINGER IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002013000135 20020130 00135 SO 2002 1 30 ASOA02009 1 20020103 A 5320 12046158003 BUTTSTRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 283AS 120236 DURING C-CHECK INSPECTION IN BNA, THE RIGHT SIDE BUTT STRAP WAS CORRODED BETWEEN STATION 6653.1 AND FRAME 25. MAINTENAN CE REMOVED THE CORRODED BUTT STRAP AND INSTALLED THE NEW BUTT STRAP IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002013000136 20020130 00136 SO 2002 1 30 ASOA02010 1 20020103 A 5320 12046158001 BUTTSTRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 283AS 120236 DURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS CORRODED BETWEEN FRAMES 30 AND 34. MAINTENANCE REMOVED THE CO RRODED LEFT BUTT STRAP AND INSTALLED THE NEW BUTT STRAP IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002013000137 20020130 00137 SO 2002 1 30 ASOA02011 1 20020103 A 5320 12004149001 CROSSBEAM EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 283AS 120236 DURING C-CHECK INSPECTION IN BNA, THE 3 RIGHT, MOST OUTBOARD CROSS FRAMES HAD CORROSION AT FRAME 20. MAINTENANCE REMOVE D THE 3 CORRODED, RIGHT, OUTBOARD MOST CROSS FRAMES IAW SRM 51-40-02. MAINTENANCE INSTALLED THE NEW CROSSBEAMS IAW SRM 51-21-02. (M) 2 L 7 2 4T RT A31SO 2002013000138 20020130 00138 SO 2002 1 30 ASOA02012 1 20020103 A 5320 12004149002 CROSSBEAM EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 283AS 120236 DURING C-CHECK INSPECTION IN BNA, ALL FOUR FLOOR CROSS FRAMES WERE CORRODED AT FRAME 16. MAINTENANCE REMOVED AND REPLAC ED THE CORRODED FLOOR CROSS FRAMES IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002013000140 20020130 00140 EU 2002 1 30 RAIA00201034 1 20020129 A 5730 14171175417 PANEL JETAIR JETSTM JETSTM4101 1500501 EU MISSING A RAIA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 CE 03 555HK 41072 5562-STL- DURING POST-FLIGHT FLIGHT CREW FOUND LEFT WING TO NACELLE INBOARD PANEL HAD DEPARTED IN FLIGHT. MAINTENANCE RE PLACED PANEL, PER J41 MM. 2 L 7 2 4T RT A41NM 2002021900069 20020219 00069 NM 2002 2 19 SABA020013 1 20020128 A 3350 WL1317 LIGHT DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A SABA K NONE O OTHER CR CRUISE 1 SO 33 883CC 162 AIRCRAFT 883 ON FLIGHT 5028 FROM TLH TO CLT. DURING TURN-AROUND AT CLT, THE EMERGENCY CEILING LIGHT AT ROW 7 WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002013100026 20020131 00026 SO 2002 1 31 C2XA02RI001 1 20020131 A 5230 1SE1 SWITCH EMB 145 EMB145LR 3260212 SO STICKS A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 13949 145057 RIC - FLT #3516 - Crew reported a Baggage door open warning indication on takeoff roll. The crew aborted the take-off an d returned to the gate. Maintenance cleaned the cargo door micro-switch. The system operationally tested satisfactory a nd the aircraft was approved for return to service. 2 L 7 2 4T RT T00011AT 2002020700040 20020207 00040 NM 2002 2 7 F3LA200200028 1 20020128 A 5320 DOUBLER BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED WEB DOUBLER CORRODED BETWEEN STR 23R AND 24R AT STA 787. FABRICATED NEW WEB PER B AC DRAWING 65-47959 AND INSTALLED REPAIR PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 2002013100029 20020131 00029 EA 2002 1 31 COMA0260074 1 20020129 A 7800 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J S WARNING INDICATION AFFECT SYSTEMS TO TAKEOFF 1 SO 01 940CA 7048 FLIGHT 6013 R/H REVERSER UNLOCK MESSAGE DURING T/O.DEFERRED MAINT. PER M.E.L. 2 L 7 2 4F RT A21EA 2002013100030 20020131 00030 EA 2002 1 31 COMA0260075 1 20020129 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 926CA 15744 7027 FLIGHT 5895 LANDING GEAR DISAGREE WARNING AFTER T/O.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002013100031 20020131 00031 NE 2002 1 31 PCAA0201019 2 20020129 A 7200 PW120A ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT DAMAGED A PCAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 13 829EX 32037 6249 146 120438 BWI- FLIGHT#3629. CREW REPORTED ON CLIMB AN INTERMITTANT SCREETCHING NOISE WAS HEARD WITH BOTH ENGINES AT TAKE-OFF POWER SETTINGS. NOISE WAS ACCOMPANIED BY AN INTERMITTANT VIBRATION. NOISE AND VIBRATION WENT AWAY WITH POWER REDUCTION. MAINT ENANCE REPLACED LEFT ENGINE ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002013100032 20020131 00032 NM 2002 1 31 PCAA0201020 1 20020129 A 2910 829510010271 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM LEFT WING BROKEN A PCAA K NONE K FLUID LOSS CR CRUISE 1 EA 13 EICHP 215 HPN-BWI FLIGHT#3595. CREW REPORTED #1 HYDRAULIC QUANTITY INDICATION DOWN TO 3/4 QT. IN FLIGHT. #1 ISOLATION VALVE AND RO LL SPOILER INBOARD CAUTION LIGHTS ILLUMINATED. MAINTENANCE REPLACED SPOILER HYDRAULIC LINE. GROUND RAN AIRCRAFT, NO LEAK S NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002013100037 20020131 00037 EU 2002 1 31 USAABA02001 1 20020105 A 5270 F5237131720051 ROD END AIRBUS 330 A330323 3930335 EU CARGO DOOR LOOSE A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 670UW 0315 PHL - FLT 196 - CLIMBING THROUGH FL230, CREW RECEIVED THE ECAM WARNING 'DOOR AFT CARGO'. FLIGHT RETURNED TO PHL AND LAN DED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE TARGET ROD END ASSEMBLY. (M) 2 L 7 2 4F RT A46NM 2002013100042 20020131 00042 NM 2002 1 31 SWAA020156 1 20020123 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 365SW 26576 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS AT MID CABIN INOP. RECONNECTED WIRES PER MM. 2 L 7 2 4F RT A16WE 2002013100043 20020131 00043 NM 2002 1 31 SWAA020157 1 20020122 A 5311 96380 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D-CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178 WL 184 AND LBL 5.7. REMOVED AND REPLACED VERTICAL CHOR D PER SWA ACO. 2 L 7 2 4F RT A16WE 2002013100048 20020131 00048 NM 2002 1 31 QXEA0200085 1 20020127 A 2760 7G772 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007 NM FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 355PH 500 PDX - ROLL SPOILER INBOARD CAUTION LIGHT ILLUMINATED IN FLIGHT. EMERGENCY CHECKLIST WAS COMPLIED WITH. LIGHT REMAINED IL LUMINATED. REPLACED #1 HYDRAULIC ROLL SPOILER PRESSURE SWITCH. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002013100059 20020131 00059 NM 2002 1 31 AWXA200200089 1 20020130 A 3350 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM SEAT 12 L/H PINCHED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 YVR - EEL - "C" - DURING C-13 CHECK MAINTENANCE DISCOVERED A FLOOR TRACK EMERGENCY ESCAPE PATH LIGHTING WIRE PINCHED JUS T AFT OF SEAT 12 L/H. MAINTENANCE REPAIRED EMERGENCY ESCAPE PATH LIGHTING WIRE WITH A SPLICE AT SEAT 12 L/H AS PER BOEIN G STANDARD WIRING PRACTICES CH. 20-30-12, PG 21-23. 2 L 7 2 4F RT A16WE 2002020100003 20020201 00003 EU 2002 2 1 0130 1 20020102 A 2910 LINE AMD FALC50 FALCON50MYST 2730106 EU HYD SYSTEM CRACKED E DJFA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 23 523CW 23 AIRCRAFT DEPARTED CGF, DURING THE CLIMB THE PILOTS NOTICED THE HYDRAULIC PRESSURE DECREASING IN FLIGHT. THEY CONTACTED T OWER AND RQUESTED RETURN TO CGF. DURING RETURN TO CGF AIRCRAFT LOST HYD PRESSURE. LANDING GEAR WAS EXTENDED AND AIRCRAFT LANDED WITH NO PROBLEMS. TECHNICIANS FOUND STEEL LINE ATTACHED TO HYD ACCUMULATER CRACKED. REPLACED LINE AND ACCUMULATE R AND NUMBER 1 AND 2 ENGINE HYD PUMPS DUE TO THE PSSIBILITY OF OIL STARVATION. 2 L 7 3 4F A46EU 2002020100004 20020201 00004 WP 2002 2 1 0200199876 1 20020107 A 2782 ROD DOUG DC9 DC951 3022051 WP LT SLAT ACTUATOR BROKEN A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 785NC 01998 48110 WHEN SLATS WERE EXTENDED, THE AIRCRAFT ROLLED TO THE RIGHT. SLAT DISAGREEMENT LIGHT ILLUMINATED AND BLUE SLAT EXTEND LIG HT DID NOT ILLUMINATE. COMPLIED WITH COM PROCEDURES AND AIRCRAFT LANDED UNEVENTFULLY WITH SLATS RETRACTED AND FLAPS EXTE NDED. MAINTENANCE REPLACED THE LEFT LOWER SLAT ACTUATOR ROD WHICH WAS FOUND BROKEN AND LUBED THE LEFT WING SLAT ROLLERS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002020100005 20020201 00005 WP 2002 2 1 0200209762 1 20020122 A 2780 GUIDE DOUG DC9 DC941 302207N WP LT SLAT FLANGE WORN A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 762NW 47395 ON SLAT EXTENSION, THE SLAT DISAGREEMENT LIGHT ILLUMINATED ACCOMPANIED WITH A ROLL TO THE RT. CREW RECYCLED THE SLATS AN D DISCREPANCY REPEATED INCLUDING ROLL TO THE RT. IN PROCESS OF APPLYING COM PROCEDURES, LIGHT WENT OUT AND LANDING WAS N ORMAL. MAINTENANCE FOUND THE LT SLAT OUTBOARD FLANGE GUIDE WORN AND GROOVED. REPLACED THE FLANGE GUIDE. SYSTEM CHECKE D OK. 2 L 7 2 4F A6WE 2002020100006 20020201 00006 NM 2002 2 1 0200216303 1 20020123 A 3397 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROW 12JK THROUGH 35 HJK. RESEATED WIRE CONNECTO R. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002020100010 20020201 00010 NE 2002 2 1 02FDEA00071 2 20020125 A 7321 HMU AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 2 FAULTY A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 672FE 779 ON TAKEOFF NR 2 FADEC FAULTED. R&R HMU. 2 L 7 2 4F 4 F RT A35EU E13NE 2002020500007 20020205 00007 NM 2002 2 5 02FDEA00072 1 20020126 A 5310 FASTENER BOEING 727 727277 138408S NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 1 EA MISSING & 10 EA DISHED FASTENERS IN EXTERNAL FUSELAGE SKIN, BS 1168-1183 AT STR 30. R&R STR PER SRM 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 2002020100011 20020201 00011 NM 2002 2 1 02FDEA00074 1 20020128 A 7810 TAILPIPE DOUG MD11 MD11 3023602 NM NR 2 ENGINE FIRE A FDEA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SO 25 587FE 48489 AFTER BLOCK IN & ENGINE SHUTDOWN, NR 2 ENGINE TAILPIPE ON FIRE. R&R APU NR 1 FIRE BOTTLE PER MM 26-21-01-4. 2 L 7 3 4F RT A22WE 2002020500009 20020205 00009 NM 2002 2 5 02FDEA00075 1 20020130 A 3260 WARNING SYSTEM DOUG MD11 MD11 3023602 NM MLG FALSE ACTIVATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 578FE 48458 LAND GEAR AURAL WARN CONSTANTLY ON WHILE GEAR UP. R&R LT OUTBOARD FLAP TRANSMITTER & WIRES. 2 L 7 3 4F RT A22WE 2002020100012 20020201 00012 NM 2002 2 1 02FDEA00076 1 20020131 A 2751 INDICATOR BOEING 727 727247 138408F NM TE FLAPS MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 236FE 21330 AFTER TAKE OFF, HAD INDICATION OF ASYMMETRICAL OUTBOARD FLAPS LOCKED OUT. R&R INDICATOR PER MM 27-52-021-2. 2 L 7 3 4F A3WE 2002020100013 20020201 00013 EU 2002 2 1 02FDEA00077 1 20020129 A 2750 CONTROL UNIT AIRBUS 300 A300F4605R 3930327 EU TE FLAPS MALFUNCTIONED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 680FE 794 DURING CLIMBOUT FLAPS WOULD NOT RETRACT. R&R NR 1 & 2 SFCC PER MM 27-51-18.4. 2 L 7 2 4F RT A35EU 2002020100014 20020201 00014 NM 2002 2 1 02FDEA00078 1 20020129 A 2750 MOTOR BOEING 727 727227 1384078 NM TE FLAPS LEAKING A FDEA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 25 482FE 21464 HYDRAULIC SYS "A" QUANTITY LOSS IN FLIGHT. R&R OUTBOARD FLAP HYDRAULIC DRIVE MOTOR PER MM 27-51-062-4. 2 L 7 3 4F A3WE 2002020500010 20020205 00010 NM 2002 2 5 02FDEA00079 1 20020128 A 5313 655623910 STRINGER BOEING 727 727277 138408S NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 STR 1 HAS A CRACK ON LT WEB AT BS 480. R&R STR. 2 L 7 3 4F RT A3WE 2002020500011 20020205 00011 NM 2002 2 5 02FDEA00080 1 20020128 A 5313 655623910 STRINGER BOEING 727 727277 138408S NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 BS 478, STR 2 RT, L FLANGE EDGE CRACKED AND BENT. R&R STR. 2 L 7 3 4F RT A3WE 2002020500012 20020205 00012 NM 2002 2 5 02FDEA00081 1 20020130 A 5531 RIB BOEING 727 727277 138408S NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 STR 5 LT IN VERTICAL STAB CRACKED AT NR 2 RIB FIN STA 6.37. R&R VERT STAB. 2 L 7 3 4F RT A3WE 2002020500013 20020205 00013 NM 2002 2 5 02FDEA00082 1 20020129 A 5532 SKIN BOEING 727 727277 138408S NM VERTICAL STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 DRILL START DAMAGE IN VERTICAL STAB SKIN STR 5 LT, NR 2 RIB. R&R SKIN. 2 L 7 3 4F RT A3WE 2002020100024 20020201 00024 NM 2002 2 1 2002UALA00071 1 20020119 A 5315 FLOORBEAM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 779UA 26941 STATION 246 FLOORBEAM CHORD CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002020100027 20020201 00027 NM 2002 2 1 2002UALA00124 1 20020119 A 5553 ATTACH FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 FUSELAGE VERTICAL STABILIZER RIGHT HAND REAR TERMINAL FITTING LUG CORRODED ON LUG FACES AT STATION 1085 - 1088 RBL 6 TO 10. MAJOR REPAIR ACCOMPLISHED. LUGS SPOT FACED. ROTO PEENED ALODINED PRIMED AND PAINTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020100028 20020201 00028 NM 2002 2 1 2002UALA00125 1 20020119 A 5553 ATTACH FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 FUSELAGE VERTICAL STABILIZER LEFT HAND AFT MAIN ATTACH LUG HAS RUST BETWEEN LUG FACE AND ATTACH "T" CHORD FITTING AT STA TION 1088 & LBL 10. MAJOR REPAIR ACCOMPLISHED. SPOT FACED LUG TO REMOVE DAMAGE. ROTO PEENED ALODINED PRIMED AND PAINT ED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002022100045 20020221 00045 NM 2002 2 21 2002UALA00127 1 20020119 A 2120 ODOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 308UA 23669 AIRCRAFT RETURNED TO FIELD DUE TO RUBBER SMELL IN CABIN. NO ROOT CAUSE WAS FOUND. INSPECTED WHEEL WELLS, CABIN SERVICE AND LIGHTING. ALSO, RAN BOTH ENGINES WITH PACKS ON AND ZERO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020600081 20020206 00081 NM 2002 2 6 2002UALA00128 1 20020120 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 193UA 26890 SEAT 53C EEL DAMAGED, INOP. REPLACED IN SEAT EEL STRIP. OPS CHECK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2002022100046 20020221 00046 NM 2002 2 21 2002UALA00131 1 20020120 A 2781 WARNING SYSTEM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 614UA 21875 CREW HEARD LOUD THUMPING ON LEFT SIDE OF AIRCRAFT, AND HAD L/E SLAT DISAGREE LIGHT ILLUMINATE. DIVERTED TO SLC. NUISAN CE EICAS MESSAGE GENERATED BY PROXIMITY SWITCH SYSTEM. THERE IS NO HISTORY OF SLAT POSITION PROBLEMS ON THIS AIRCRAFT. PERFORMED PSEU BITE CHECK ON ALL LEADING EDGE SLAT PROXIMITY SWITCHES PER APPLICABLE MAINTENANCE MANUAL AND ALL CHECKED OK. OPERATIONALLY CHECKED L/E SLATS PER APPLICABLE MAINTENANCE MANUAL AND ALL OPS CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E3NE 2002022800024 20020228 00024 NE 2002 2 28 2002UALA00132 2 20020121 A 7260 4A0300 CARBON SEAL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GEARBOX LEAKING A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 441UA 751 V10499 NR 1 ENGINE HAD INFLIGHT SHUTDOWN DUE TO LOSS OF OIL QUANTITY AND DECREASE IN OIL PRESSURE. AFTER SHUTDOWN ENGINE WINDM ILLED FOR 35 MINUTES, OIL TEMPERATURE 110-115, OIL PRESSURE 9.5 PSI AND OIL QUANTITY ZERO. INTERFACE BETWEEN FUEL PUMP AND MAIN ENGINE GEARBOX WAS FOUND TO BE LEAKING OIL. CARBON SEAL WAS REPLACED AND NO FURTHER LEAKS WERE OBSERVED DURING ENGINE GROUND RUN. 2 L 7 2 4F 4 F RT A28NM E40NE 2002022100047 20020221 00047 NM 2002 2 21 2002UALA00133 1 20020121 A 2160 SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E/E BAY DIRTY A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 325UA 23957 UNSCHEDULED LANDING DUE TO INDICATION OF INOPERATIVE EQUIPMENT COOLING FAN. NO FAULT FOUND. CLEANED THE EQUIPMENT COOL ING LOW FLOW SENSOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020100029 20020201 00029 NM 2002 2 1 2002UALA00134 1 20020124 A 5313 CREASE BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 926UA 26648 CABIN CREASE BEAM INNER CHORD OUTBOARD CLIP IS CRACKED AT BODY STATION 294 RBL 53 WL 208. MAJOR REPAIR ACCOMPLISHED.REP LACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020100030 20020201 00030 NM 2002 2 1 2002UALA00135 1 20020123 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 LOWER NOSE, LT SIDE BODY STATION 188 IS CRACKED AFT SIDE IN THE FRAME RADIUS JUST BELOW FLOOR LINE. MAJOR REPAIR ACC OMPLISHED. DOUBLER INSTALLED AT STATION 188 WL 207 AND EXTERNAL SKIN DOUBLER ON LEFT SIDE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020100031 20020201 00031 NM 2002 2 1 2002UALA00136 1 20020123 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 RT FUSELAGE FRAME AT STATION 188 CRACKED AT WL 208. MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED AT STATION 188 WL 208 AND EXTERNAL FUSELAGE SKIN DOUBLER INSTALLED ON RIGHT HAND SIDE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020100032 20020201 00032 NM 2002 2 1 2002UALA00137 1 20020123 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 CORROSION ON SKIN BASE DISTANCE MEASURING EQUIPMENT ANTENNA M763. MAJOR REPAIR ACCOMPLISHED INSTALLED REPAIR DOUBLER AT BODY STATION 548, BL 0. 2 L 7 2 4F 4 F RT A1NM E24NE 2002020100033 20020201 00033 NM 2002 2 1 2002UALA00138 1 20020120 A 2781 WARNING SYSTEM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LE SLATS ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 614UA 21875 EICAS MESSAGE LEADING EDGE SLAT DISAGREE DISPLAYED INTERMITTANTLY ALONG WITH CAUTION LIGHT ILLUMINATED. FLIGHT DIVERTE D TO SLC. 2 L 7 2 4F 4 F RT A1NM E3NE 2002020600087 20020206 00087 EU 2002 2 6 2002UALA00139 1 20020124 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 475UA 1495 DENT FOUND AT AIRCRAFT ARRIVAL. DENT LOCATED ABOUT 20 INCHES ABOVE AVIONICS EQUIPMENT AIR INLET AND 9 INCHES AFT OF FRA ME 20. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002020100034 20020201 00034 NM 2002 2 1 2002UALA00140 1 20020125 A 5321 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 STATION 1680 PRESSURE DECK UPPER SURFACE AT FORWARD EDGE HAS CORROSION BEYOND LIMIT 0 TO 24 LBL AT STRINGER 17 LT. MAJ OR REPAIR ACCOMPLISHED. REMOVED DAMAGE. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002030100012 20020301 00012 NM 2002 3 1 2002UALA00141 1 20020124 A 2721 024807002 MODULE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RUDDER TRIM FAULTY A UALA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 929UA 26652 UNSCHEDULED LANDING DUE TO A RUDDER TRIM IRREGULARITY. REPLACED RUDDER TRIM ACTUATOR, AND RUDDER TRIM CONTROL MODULE. CHECKED WIRING FROM D3116 TO D2932. ALL WIRES CHECKED GOOD. RUDDER TRIM MODULE WAS CONFIRMED BAD IN THE SHOP. THE SWI TCH HAD AN INTERNAL FAILURE CAUSING INTERMITTENT OPERATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020100035 20020201 00035 WP 2002 2 1 ABXA010683 1 20020108 A 5330 SKIN DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 MAIN ENTRY DOOR STAIR CUTOUT HAD CRACK AT LOWER AFT CORNER. REPAIRED LOWER AFT CORNER OF AIRSTAIR CUTOUT IAW DC-9 SRM 53 -94. 2 L 7 2 4F A6WE 2002020100036 20020201 00036 WP 2002 2 1 ABXA010685 1 20020109 A 5280 51175331 DOOR DOUG DC9 DC932F 3022067 WP MLG CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 INBOARD MAIN LANDING GEAR DOOR CRACKED JUST BELOW ACTUATOR ATTACH FITTING. REMOVED AND REPLACED DOOR IAW DC-9 SRM 51-30- 5 AND 51-30-7. REPAIRED INNER CRACKED SKIN IAW REA D952-42986. REINSTALLED DOOR ASSEMBLY IAW DC-9 MM 32-1-01. 2 L 7 2 4F A6WE 2002020100037 20020201 00037 WP 2002 2 1 ABXA010687 1 20020110 A 5511 99225793 SPAR CAP DOUG DC9 DC932F 3022067 WP HORIZONTAL STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 LEVEL 1 CORROSION INSIDE OF HORIZONTAL STABILIZER ON INSIDE OF FRONT SPAR, TOP CAP, BETWEEN TWO FASTENERS AT APPROXIMATE LY STATION XFS 163.3. REPAIRED HORIZONTAL STABILIZER FRONT SPAR TOP CAP IAW REA D955-43008MR. 2 L 7 2 4F A6WE 2002020100045 20020201 00045 NM 2002 2 1 SWAA020158 1 20020121 A 5310 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002020100046 20020201 00046 NM 2002 2 1 SWAA020160 1 20020121 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 384SW 26590 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED AT BS 520. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2002020100047 20020201 00047 NM 2002 2 1 SWAA020162 1 20020122 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED C4 CHECK, FOUND RT KEEL BEAM LOWER CHORD CORRODED BETWEEN BS 500C AND 500D, STR 28R. REPAIRED CHORD PE R SWA RA. 2 L 7 2 4F RT A16WE 2002020100048 20020201 00048 NM 2002 2 1 SWAA020163 1 20020123 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) AT BS 706, STR'S 2R, 3R, 2L AND 3L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002020100049 20020201 00049 2002 2 1 SWIA200210540 4 20020105 A 3425 COMPARATOR EMB 120 EMB120ER 3260203 SO NR 2 FAILED A SWIA O OTHER I FLT. ATTITUDE INST. CR CRUISE 1 NM 07 229SW 120305 F/O ADI WON'T DISPLAY A/C ATT TURNING GAUGES GYRO, COMP AND HDG FLAGS. REPLACED NR 2 AHC85 WITH SERVICEABLE UNIT. OPS CHECK GOOD ON TAXI. S/N OFF: 2731. 2 L 7 2 4T RT A31SO 2002020100050 20020201 00050 SO 2002 2 1 SWIA200210541 1 20020106 A 5610 SEAL EMB 120 EMB120ER 3260203 SO WINDSHIELD LOOSE A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 196SW 120151 UNUSUAL LOUD POPPING SOUND OVERHEAD. FOUND LOOSE PROSEAL ON TOP EDGE OF CAPTAIN'S WINDSHIELD. APPLIED SPEED TAPE. 2 L 7 2 4T RT A31SO 2002020100051 20020201 00051 2002 2 1 SWIA200210542 4 20020110 A 3417 ADC CNDAIR CL600 CL6002B19 1900309 EA NR 2 MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 408SW 7055 AFTER DEPARTURE FO PFD LOST ALTITUDE TAPE AND ALTIMETER SETTING AND VSI INDICATION. RED BOXES ALT AND VSI DISPLAYED. U NABLE TO RESET. SWITCHED TO ADC 1 TO REGAIN INDICATIONS. RETURNED TO SLC. PERFORMED AIR DATA SYSTEM FUNCTIONAL TEST. NO FAULTS FOUND ON NR 2 ADC. 2 L 7 2 4F RT A21EA 2002020100052 20020201 00052 EA 2002 2 1 SWIA200210543 1 20020105 A 4990 OIL COOLER CNDAIR CL600 CL6002B19 1900309 EA APU DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 499SW 7398 APU OIL TEMP CAUTION MSG. DIVERTED FROM SLC TO GJT. CLEANED THE OIL COOLER COOLING FINS. RAN THE APU FOR 30 MINS. OP S CHECK GOOD. 2 L 7 2 4F RT A21EA 2002020100053 20020201 00053 EA 2002 2 1 SWIA200210544 1 20020105 A 3097 WIRE CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYS CHAFED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 590SW 7077 ANTI-ICE DUCT MESSAGE INFLIGHT (RIGHT SIDE). RETURNED TO SLC. REMOVED RIGHT O/B LEADING EDGE. FOUND A CHAFED WIRE AT DUCT LEAK SENSOR. REPAIRED CHAFE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002020100054 20020201 00054 NM 2002 2 1 CALA0200058 1 20020130 A 5330 SKIN PANEL BOEING 737 7373T0 1384582 NM HS ATT. AREA WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND L/H FUSELAGE SKIN CUTOUT LOWER PANEL WORN WITH RIVET PULLING THROUGH AT HORIZONTAL STABILIZER ATTACH FI TTING. THE SKIN CUTOUT LOWER PANEL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002020100055 20020201 00055 NM 2002 2 1 CALA0200060 1 20020131 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 312-345 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 312-345, S22L. THE SKIN WAS REPAIRED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2002020100056 20020201 00056 SO 2002 2 1 SWIA200210545 1 20020105 A 3230 LANDING GEAR EMB 120 EMB120RT 3260202 SO NLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 200CD 120200 AFTER GEAR RETRACTION, BOTH RED AND GREEN A-SYSTEM NOSE LIGHTS REMAINED ILLUMINATED. PRESS TO TEST DISPLAYED ALL B-LIGH TS ON AND ONLY A-NOSE LIGHTS ON. ATTEMPTED TO CYCLE GEAR WITH NO RESPONSE. PERFORMED MANUAL ELECTRIC OVERRIDE QRH PROC EDURE SUCCESSFUL. REMOVED AND REPLACED A-HARNESS AND PROX SENSOR. CYCLED GEAR SEVERAL TIMES. OPS CHECKED GOOD. P/N O N 120-4125-001, S/N ON T99928. 2 L 7 2 4T RT A31SO 2002020100057 20020201 00057 SO 2002 2 1 SWIA200210546 1 20020105 A 2750 FLAP EMB 120 EMB120RT 3260202 SO WING MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 137H 120137 UPON SELECTING FLAPS TO 45 DEGREES, THE OUTBOARD FLAPS WENT TO 25 DEGREES ONLY. RECEIVED A FLAP DISAGREEMENT. FOLLOWED QRH PROCEDURE AGAIN, FLAP DISAGREEMENT. DIVERTED FROM SBP TO SMX. RESET FLAP ANNUNCIATOR. INSPECTED FLAPS, ROLLERS A ND TRACKS, FOUND TO BE OK. CLEANED FLAP TRACKS AND ROLLERS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002020100058 20020201 00058 2002 2 1 SWIA200210547 4 20020105 A 3425 COMPARATOR EMB 120 EMB120ER 3260203 SO NR 2 FAULTY A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 229SW 120305 DURING FLIGHT, ATT DISPLAY ON MAP CAME ON. A/P DISCONNECTED, GYRO AND COMPUTER FLAGS ON COPILOT'S ADI, HDG FLAG ON COPI LOT'S HSI. AFTER A/P DISCONNECT FLAGS WENT AWAY, BUT DURING TURNS F/O'S ATT IND STAYED STRAIGHT AND LVL. F/O COMMAND B ARS SHOW BELOW AIRPLANE SYMBOL. REPLACED NR 2 AHC85 WITH SERVICEABLE UNIT. OPS CHECK GOOD ON TAXI. S/N OFF: 2731. 2 L 7 2 4T RT A31SO 2002020100059 20020201 00059 SO 2002 2 1 SWIA200210548 1 20020107 A 5210 LOCK EMB 120 EMB120ER 3260203 SO PAX DOOR FROZEN A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 224SW 120294 MAIN CABIN DOOR WILL NOT OPEN SMOOTHLY. FOUND UPPER DOOR CENTERING PLATES TOO TIGHT. ADJUSTED AND FOUND AFT OVER CENTE R LOCK FROZEN. REMOVED AFT SHAFT, CLEANED AND LUBED, REINSTALLED SHAFT. OPS CHECK GOOD IAW 52-11-00. 2 L 7 2 4T RT A31SO 2002020100060 20020201 00060 EA 2002 2 1 SWIA200210549 1 20020108 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA LT SPOILER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 418SW 7446 LEFT SPOILERON FAULT CAUTION MESSAGE. REPLACED LEFT SPOILER OUTBOARD PCU IAW CL600 MM 27-62-01. SPOILERON OPS CHECK GO OD. PCU LEAK CHECK GOOD. S/N OFF: 9779. 2 L 7 2 4F RT A21EA 2002020100061 20020201 00061 2002 2 1 SWIA200210550 4 20020103 A 2210 6225798013 CONTROL PANEL EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA O OTHER I J FLT. ATTITUDE INST. WARNING INDICATION CR CRUISE 1 NM 07 268UE 4626 4626 120207 F/O'S COMMAND BARS STUCK AT 14 DEGREES AND A/P WILL NOT ENGAGE. DURING FLIGHT, ATTITUDE DISPLAY ON MAP, YELLOW PIT ON B OTH CAPTAIN'S AND FIRST OFFICER'S EADIS. FIRST OFFICERS DELTA SYMBOL DISPLAYED 5 DEGREES HIGHER THAN CAPTAIN'S. CAPTAI N'S DELTA SYMBOL DISPLAYED ACCURATE PITCH BUT COMMAND BARS WERE 3 DEGREES LOWER. DURING DESCENT, AUTOPILOT FAIL ON MAP, YAW DISCONNECT AND AP DISCONNECT ON BOTH CAPTAIN'S FCP. REMOVED AND REPLACED F/O'S FCP IAW MM 22-10-00. OPS CHECK GOO D ON A/P AND FLIGHT DIRECTOR. 2 L 7 2 4T RT A31SO 2002020100062 20020201 00062 SO 2002 2 1 C2XA02CL028 1 20020131 A 3350 20131A BATTERY EMB 135 EMB135ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27506 1840 48 145206 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHTS AT THE OVERWING EXITS WERE FOUND TO BE INOPERATIVE.MAINTENANCE REPLACED THE #3 EMERGENCY LIGHT BATTERY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002020100063 20020201 00063 EA 2002 2 1 SWIA200210551 1 20020111 A 3230 601R102371 SHAFT CNDAIR CL600 CL6002B19 1900309 EA RT MLG GALLED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 RIGHT MLG SIDE BRACE SHAFT FITTING IS GALLED AND CORRODED. REMOVED AND REPLACED RIGHT MLG SIDE BRACE SHAFT IAW 57-21-28 . OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002020100064 20020201 00064 SO 2002 2 1 SWIA200210552 1 20020114 A 3260 12043270001 CONTROL BOX EMB 120 EMB120ER 3260203 SO LANDING GEAR INTERMITTENT A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 188SW 4296 4296 120039 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOUND LANDING GEAR OVERNIGHT PINS INSTALLED IN GEAR. REMOVED GEAR PIN. GEAR WOULD RETRACT AND DEPLOY NORMALLY. FOUND GEAR TO HAVE INTERMITTENT INDICATION PROBLEM. REMOVED AND REPLACED LANDI NG GEAR CONTROL BOX AND RELAY. 2 L 7 2 4T RT A31SO 2002020100065 20020201 00065 SO 2002 2 1 C2XA02TY019 1 20020201 A 5343 14521680003 FITTING EMB 145 EMB145ER 3260211 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 TYS, During a scheduled 1C inspection, the forward left drag brace, frame side of the nose landing gear main brace strut bearing surface was found gouged. Maintenance blended the damage and performed dye penetrant inspection (no defects not ed) alodined, primed and panted I/A/W-GST-0348/02. Repair procedures are satisfactory, aircraft will be released upon co mplection of inspection. 2 L 7 2 4F RT T00011AT 2002020100066 20020201 00066 SO 2002 2 1 C2XA02IA017 1 20020130 A 3230 18190003 SOLENOID VALVE EMB 120 EMB120ER 3260203 SO INTERMITTENT A C2XA K NONE O OTHER AP APPROACH 1 SW 27 17728 9081 9081 120182 IAH - FLT 3680, Pilot reported that the landing gear would not exctend on the first attempt. The gear was eventually ext ended and the aircraft landed at IAH without incident. Maintenance removed and replaced the landing gear solenoid valve. The landing gear sytem operationally checked good and the aircraft was approved for return to service. 2 L 7 2 4T RT A31SO 2002020100067 20020201 00067 SO 2002 2 1 SWIA200210553 1 20020113 A 2530 CONNECTOR EMB 120 EMB120ER 3260203 SO GALLEY BURNED A SWIA O OTHER M OVER TEMP DE DESCENT 1 NM 07 565SW 120340 UPON DESCENT F/A'S GALLEY ELECTRICAL PANEL LOST LIGHTING, FUNCTIONING AND WAS HOT TO THE TOUCH. ALL 3 CREW MEMBERS SMEL LED SMOKE, BUT NO VISUAL. FOUND CANNON PLUG ON COFFEE POT BURNED. REPLACED COFFEE POT, OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002020100068 20020201 00068 WP 2002 2 1 ARWA20020115 1 20020129 A 7931 42D491C PRESSURE SWITCH DOUG DC8 DC863F 302198F WP A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 441J 45988 LOG PAGE 109685. DISCREPANCY: AFTER TAKE OFF ENGINE #3 OIL PRESS LIGHT CAME ON, OIL PRESS 50 Psi, PRESS 40 Psi WITH POWE R LEVER @ IDLE, OIL TEMP INCREASED TO 128 C ENGINE SHUT DOWN IAW AOM ABNORMAL PROCEDURE. ENGINE SHUT DOWN AT 2352Z. AIRC RAFT RETURNED TO KMIA AND PERFORMED OVERWEIGHT LANDING 279,000 Lbs. CORRECTIVE ACTION: REMOVED AND REPLACED DIFFERENTIAL PRESS SWITCH IAW MM 79-33-1 PERFORMED ENGINE RUN UP AND FOUND NORMAL IAW MM 71-00. ACCOMPLISHED OVERWEIGHT LANDING INSP ECTION IAW J/C 6372 NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002020100069 20020201 00069 WP 2002 2 1 ZW0A0201402 1 20020111 A 3350 7732 LAMP DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 966TW 53616 THE RED EGRESS LIGHT AT ROW 28 WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 3-23-01 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2002020100070 20020201 00070 WP 2002 2 1 ZW0A0201404 1 20020120 A 3350 58222 BATTERY PACK DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 961TW 53611 EMERGENCY LIGHTS ON OVERHEAD AT ROWS 28 & 29 ARE INOP. REPLACED BATTERY POWER SUPPLY AND OPS CHECK PER MM33-53-00. ---CL OSED--- 2 L 7 2 4F RT A6WE 2002020100071 20020201 00071 SO 2002 2 1 SWIA200210554 1 20020115 A 2752 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 188SW 4788 949 120039 FLAP DISAGREEMENT UPON RETRACTING FLAPS ON CLIMBOUT. PERFORMED QRH AND WORKED NORMAL FOR THE REMAINDER OF THE FLIGHT. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW 27-50-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002020100072 20020201 00072 2002 2 1 SWIA200210555 4 20020114 A 3425 COMPUTER EMB 120 EMB120ER 3260203 SO NR 2 FAULTY A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 232SW 120306 AFTER DEPARTURE FIRST OFFICER'S EHSI DISPLAY WENT BLANK. RETURNED TO LAX. REMOVED AND REPLACED NR 2 HPU74 WITH SERVICE ABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002020100073 20020201 00073 NM 2002 2 1 AWXA200200093 1 20020120 A 5330 654577892 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - MAJOR REPAIR - "C" - DURING C-16 CHECK 5/8" CRACK WAS FOUND ON SKIN AT THE R2 DOOR UPPER FUSELAGE HINGE CUTOUT BS 950. MAINTENANCE CUTOUT DAMAGED SECTION OF SKIN AT BS 950, FABRICATED REPAIR DOUBLER, TRIPLER, AND FILLER, AND INSTALLED REPAIR IAW B737-300 SRM 53-60-01, PG. 210-212. 2 L 7 2 4F RT A16WE 2002020100098 20020201 00098 NM 2002 2 1 AWXA200200092 1 20020119 A 5330 654577886 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - MAJOR REPAIR - "C" - DURING C-16 CHECK 1" CRACK WAS FOUND ON SKIN AT THE R2 DOOR LOWER FUSELAGE HINGE CUTOUT BS 95 0. MAINTENANCE CUTOUT DAMAGED SECTION OF SKIN AT BS 950, FABRICATED REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIR IAW B737-300 SRM 53-60-01, PG. 217-224. 2 L 7 2 4F RT A16WE 2002020700041 20020207 00041 NM 2002 2 7 F3LA200200029 1 20020131 A 5315 FLOORBEAM BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON TOP OF FLOORBEAM AT STA 294.5. REPLACED TOP CHORD OF FLOORBEAM AT ST A 294.5, LBL 28 TO RBL 65, PER SRM 53-10-9, 51-30-2, 51-10-1, 53-10-2 AND SOPM 20-41-02. 2 L 7 2 4U RT A16WE 2002020200001 20020202 00001 SO 2002 2 2 C2XA02TY020 1 20020202 A 3350 1317 BULB EMB 145 EMB145 3260210 SO CABIN BLOWN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 TYS, During a scheduled routine check the emergency light at seat 12A was found not working, Maintenance removed and rep laced the bulb I/A/W-EMB-145-AMM-33-50-00. operational checks good, aircraft released to service. 2 L 7 2 4F RT T00011AT 2002020200002 20020202 00002 SO 2002 2 2 C2XA02TY021 1 20020202 A 2731 14523458403 BRACKET EMB 145 EMB145ER 3260211 SO Zone 300 GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 TYS, During a scheduled 1C inspection a gouge was found on the outboard fitting of the left elevator spring tab. Mainten ance blended the damage, performed dye penetrant inspection (no defects noted) and restored the protective finish I/A/W- EMB-GST-0361/02, repair procedures were satisfactory and the aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002020200003 20020202 00003 NM 2002 2 2 PCAA0201023 1 20020129 A 3230 C03600491750S SPRING DHAV DHC8 DHC8102 2809003 NM RIGHT BROKEN A PCAA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 EA 13 809EX 15196 302 DURING A CHECK INSPECTION RIGHT MAIN LANDING GEAR UPLOCK HOOK FOUND TO HAVE ONE BROKEN RETRACTION SPRING. SPRING WAS REP LACED IN ACCORDANCE WITH MESSIER DOWTY COMPONENT MAINTENANCE MANUAL 32-30-21. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002020300001 20020203 00001 EU 2002 2 3 RAIA00201031 1 20020125 A 7900 3034508 OIL FILTER AEROSP ATR72 ATR72202 8680940 EU A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 722TE 220 5602- STL- CREW REPORTED SMOKE IN CABIN AND COCKPIT DURING TAXI. MAINTENANCE REMOVED AND REPLACED #1 ENGINE SCAVENGE OIL FILTER. INSPECTED MAIN OIL FILTER FOUND NO DEFECTS. PERFORMED GROUND RUN FOR 80 MINUTES - NO SMOKE - NO OIL WARNING LIG HTS - OIL QUANTITY STABLE. 2 H 7 2 4T RT A53EU 2002020300002 20020203 00002 GL 2002 2 3 RAIA00201037 3 20020131 A 6112 B5JFR36C1103DE PROPELLER JETAIR JETSTM JETSTM4101 1500501 EU MCAULY 5JFR36 B5JFR36C1103 GL INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 555HK 12589 3569 41072 951245 5596-STL- LEFT HAND PROPELLER HEAT FAILED DURING CLIMB. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND PROPELLER, LEAK A ND OPS CK OK. 2 L 7 2 4T RT A41NM 6 C P15NE 2002020300003 20020203 00003 SO 2002 2 3 RAIA00201038 1 20020116 A 5322 14522460015 GUSSET EMB 145 EMB145 3260210 SO CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING BLOCK CHECK FOUND CORROSION ON FLOOR SUPPORT AT STRINGER 18L ON EITHER SIDE OF FRAME 17. REMOVED AND REPL ACED FLOOR SUPPORT GUSSET AT STRINGER 18L FRAME 17 IAW SRM 51-40-02 2 L 7 2 4F RT T00011AT 2002020300004 20020203 00004 SO 2002 2 3 RAIA00201039 1 20020123 A 5330 14522460013 GUSSET EMB 145 EMB145 3260210 SO A RAIA L ABORTED APPROACH O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING BLOCK CK FOUND MODERATE CORROSION CENTER TOP CAP SKIN AT CENTER BEAM I/B OF SERVICE DOOR. REMOVED AND REP LACED CENTER TOP SKIN GUSSET IAW SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002020300005 20020203 00005 SO 2002 2 3 RAIA00201040 1 20020128 A 5322 14521725015 SILL EMB 145 EMB145 3260210 SO A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING BLOCK CHECK FOUND MODERATE CORROSION AN THE GALLEY TIE DOWN POINT JUST FORWARD OF SERVICE DOOR. REMOVED A ND REPLACED SERVICE DOOR FORWARD MEMBRANE SILL IAW SRM 53-21-10. 2 L 7 2 4F RT T00011AT 2002020300006 20020203 00006 SO 2002 2 3 RAIA00201041 1 20020122 A 5322 14521725015 SILL EMB 145 EMB145 3260210 SO A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING BLOCK CHECK FOUND MODERATE CORROSION AT GALLEY TIE DOWN POINT AFT OF SERVICE DOOR. REMOVED AND REPLACED R IGHT HAND SILL AFT OF SERVICE DOOR IAW EMB145 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002020300007 20020203 00007 SO 2002 2 3 RAIA00201042 1 20020125 A 5321 14522459003 SUPPORT BRACKET EMB 145 EMB145 3260210 SO A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING BLOCK CHECK FOUND MODERATE CORROSION AT FORWARD CENTER FLOOR BOARD ANGLE SUPPORT. REMOVED AND REPLACED AN GLE SUPPORT CENTER FLOOR BEAM IAW SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002020300008 20020203 00008 SO 2002 2 3 RAIA00201043 1 20020126 A 5320 14521721009 WEB EMB 145 EMB145 3260210 SO A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING BLOCK CHECK FOUND MODERATE CORROSION AT FORWARD DIGITAL WEB PLATE. REMOVED AND REPLACED FORWARD DIGITAL W EB, IAW SRM 53-21-10 FIG 203. 2 L 7 2 4F RT T00011AT 2002020300009 20020203 00009 SO 2002 2 3 RAIA00201044 1 20020123 A 5321 14521725001 SILL EMB 145 EMB145 3260210 SO A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING BLOCK CHECK FOUND MODERATE CORROSION ON FLOOR SUPPORTS AFT OF PAX DOOR. REMOVED AND REPLACED LEFT SILL AF T OF PAX DOOR, IAW SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002020400001 20020204 00001 WP 2002 2 4 0200229754 1 20020124 A 7100 103538754 EXCITER DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE RIGHT ENGINE A NWAA F ACTIVATE FIRE EXT. O OTHER TX TAXI/GRND HDL 1 GL 01 754NW 41135 144 47178 676231 DURING RIGHT ENGINE START, THE EGT WOULD NOT RISE. TAKEOFF WAS ABORTED. AFTER ENGINE RESTART, THE TOWER REPORTED SMOKE A ND FIRE IN THE RIGHT ENGINE TAILPIPE. CREW SHUT DOWN THE RIGHT ENGINE, DISCHARGED TWO FIRE BOTTLES, AND AN EMERGENCY PAS SENGER EVACUATION OF THE AIRCRAFT OCCURRED. MAINTENANCE INSPECTED THE RIGHT ENGINE FOR DAMAGE. NO DAMAGE WAS FOUND. RE PLACED THE RIGHT ENGINE FUEL PUMP, FUEL CONTROL, IGNITION EXCITER, AND TWO FIRE BOTTLES. ENGINE OPERATIONAL CHECK OK. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2002020400002 20020204 00002 WP 2002 2 4 0200239762 1 20020130 A 2780 COUPLING DOUG DC9 DC941 302207N WP LT WING SLATS MISALIGNED A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 762NW 47395 SLAT DISAGREEMENT LIGHT ILLUMINATED WITH A SLIGHT ROLLING TENDENCY TO THE LEFT ON APPROACH. REINSTALLED THE LEFT WING SL AT ANTI-ICE COUPLING BETWEEN NBR 1 AND NBR 2 SLATS. REPLACED THE LEFT NBR 1 SLAT INBOARD CUTOUT DOOR HINGES, TIGHTENED T HE RIGHT 'T' DUCT OUTBOARD RETAINER, AND REPLACED A SLAT CONTROL VALVE. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 2002020400003 20020204 00003 WP 2002 2 4 0200249962 1 20020121 A 5270 WARNING SYSTEM DOUG DC9 DC931 3022065 WP CARGO DOOR FALSE ACTIVATION A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 914RW 47362 ON TAKEOFF ROLL, THE AFT CARGO DOOR OPEN WARNING LIGHT ILLUMINATED AND FLASHED ON/OFF FOUR TIMES. CREW SAFELY ABORTED TH E TAKEOFF AT 110 KTS AND RETURNED TO THE GATE. MAINTENANCE INSPECTED THE DOOR AND LIGHT ASSEMBLY AND DID NOT FIND ANY PROBLEMS. DISCREPANCY WAS MEL'D UNTIL MSP SHIMMED THE DOOR SWITCH STRIKER PLATE. CLEARED MEL AND AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4F A6WE 2002020400004 20020204 00004 NM 2002 2 4 0200256624 1 20020130 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 624US 21706 DURING LINE CHECK, FOUND CABIN FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLIES IN ZONES B, C, D, AND E. OPERATIONAL CHECK OK. 2 L 7 4 4F A20WE 2002020400005 20020204 00005 EA 2002 2 4 02031627 1 20020131 A 7930 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA OIL SENSOR CONTAMINATED A VTZA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 EA 27 627BR 7233 DURING DESCENT OF THE FLIGHT FROM IAD TO JAX, THE CREW REPORTED A LEFT ENGINE OIL PRESSURE WARNING WITH AN ACCOMPANYING LOW OIL PRESSURE INDICATION. THE LEFT ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED AT JAX WITHOUT INCIDENT. MAINTENANC E PERSONNEL FOUND THE ELECTRICAL CONNECTORS FOR THE OIL PRESSURE SWITCH AND THE OIL PRESSURE TRANSDUCER OIL SOAKED. THE Y CLEANED THE CONNECTORS AND HAD THE FLIGHT CREW PERFORM GROUND ENGINE RUNS. THE OPERATIONAL CHECKS WERE SATISFACTORY A ND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002020400006 20020204 00006 WP 2002 2 4 ABXA010688 1 20020111 A 5313 59114329 LONGERON DOUG DC9 DC932F 3022067 WP CARGO BAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 LONGERON 2 LEFT CRACKED AT STATION 1076. REPLACED LONGERON SECTION IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002020400007 20020204 00007 WP 2002 2 4 ABXA010689 1 20020111 A 5313 59114329 LONGERON DOUG DC9 DC932F 3022067 WP CARGO BAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 LONGERON 2 RIGHT CRACKED AT STATION 1076. REPLACED CRACKED SECTION OF LONGERON IAW DC-9 SRM 53-11-4, 51-30-2 AND 51-30-5 . 2 L 7 2 4F A6WE 2002020400008 20020204 00008 WP 2002 2 4 ABXA010690 1 20020111 A 5313 59114279 LONGERON DOUG DC9 DC932F 3022067 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 LONGERON 17 LEFT AT STATION 965 WAS CRACKED. REPLACED LONGERON 17 LEFT FROM STATION 958 TO STATION 996 IAW DC-9 SRM 53-0 2. 2 L 7 2 4F A6WE 2002020400009 20020204 00009 WP 2002 2 4 ABXA010691 1 20020111 A 5313 59114267 LONGERON DOUG DC9 DC932F 3022067 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 LONGERON 13 LEFT AT STATION 965 WAS CRACKED. REPAIRED LONGERON 13 LEFT FROM STATION 956 TO STATION 996 IAW DC-9 SRM 53-0 2. 2 L 7 2 4F A6WE 2002020400010 20020204 00010 WP 2002 2 4 ABXA010692 1 20020112 A 5310 99218161 DOOR FRAME DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 UPPER CARGO DOOR, UPPER FORWARD CORNER STRUCTURE CRACKED INSIDE FUSELAGE. INSTALLED REPAIR DOUBLER ON UPPER CARGO DOOR, UPPER FORWARD CORNER DOOR PAN STRUCTURE IAW DC-9 SRM 51-30-5 AND 53-01. 2 L 7 2 4F A6WE 2002020400011 20020204 00011 WP 2002 2 4 ABXA010693 1 20020112 A 5310 99155101 FITTING DOUG DC9 DC932F 3022067 WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 KEEL FITTING IN LEFT WHEEL WELL, FORWARD OF INBOARD GEAR DOOR ACTUATOR CRACKED AT TOP CENTER AT WING ATTACH POINT. STOP DRILLED CRACK IAW DC-9 SRM 51-10-4. REPAIRED KEEL FITTING IAW DC-9 SRM 53-03. 2 L 7 2 4F A6WE 2002020400012 20020204 00012 WP 2002 2 4 ABXA010694 1 20020126 A 2750 5751152503 LINK DOUG DC8 DC863F 302198F WP RT TE FLAPS BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 RIGHT INBOARD FLAP DRIVE LINK BROKEN. REPLACED RIGHT STATION 98 FLAP DRIVE LINK ASSEMBLY IAW DC8 MM 27-51-04-3-0001. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2002020400013 20020204 00013 WP 2002 2 4 ABXA010695 1 20020131 A 3260 CONNECTOR DOUG DC9 DC932 3022066 WP MLG INDICATOR DAMAGED A ABXA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 23 988AX 47084 ON APPROACH IN ILN SELECTED GEAR DOWN. DID NOT GET RIGHT MAIN LANDING GEAR DOWN GREEN LIGHT. RECYCLED AND ACCOMPLISHED T HE GEAR HANDLE DOWN ABNORMAL CHECK LIST IN THE DC-9 OPS MANUAL. AIRCRAFT DID A GO-AROUND. FOUND AND REPAIRED BROKEN WIRE IN CONNECTOR PLUG. (PIN 5 IN RIGHT MAIN LANDING GEAR DOWNLOCK) IAW DC-9 WDM 32-60-01-2-0101. GEAR INDICATION OPS CHECKE D GOOD. 2 L 7 2 4F A6WE 2002020400014 20020204 00014 NE 2002 2 4 AEO2002F00000 2 20020116 A 7200 38421322 SHAFT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ENGINE BROKEN B JBXA K NONE O OTHER IN INSP/MAINT 1 SO 05 573ML 7227 ENGINE ARRIVED FOR REPAIR OF SEIZED ROTOR CONDITION. UPON DISASSEMBLY FOUND TURBINE ROTORSHAFT SEPARATED AT BASE OF TUR BINE ROTOR. THIS IS THE SECOND INSTANCE OF THIS CONDITION FOUND AT THIS REPAIR STATION. THE FAILURE WAS CONTAINED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002020400021 20020204 00021 NM 2002 2 4 AWXA200200075 1 20020106 A 5320 69407082 INTERCOSTAL BOEING 737 737317 138447P NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 YVR - MAJOR REPAIR - DURING C-13 CHECK A 8 INCH AREA OF CORROSION WAS FOUND ON WEB AT LOWER INTERCOASTAL AFT CARGO DOORW AY OPPOSITE OF FLOOR TRACK BS 727A TO BS 727B, STR 24L. MAINTENANCE REMOVED AND REPLACED LOWER INTERCOASTAL FLOOR TRACK AT BS 727A TO BS 727B, STR 24L IAW DWG 69-49708 SHT 1, AND 65-46592 SHT 7. 2 L 7 2 4F RT A16WE 2002020400022 20020204 00022 NM 2002 2 4 AWXA200200076 1 20020106 A 5315 65538444 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 DURING C-13 CHECK A 1/4 INCH CRACK WAS FOUND ON AFT CARGO DOORWAY FLOORBEAM AT BS 727E, STR 24R. MAINTENANCE REMOVED AND REPLACED FLOOR TRACK BETWEEN BS 727 TO BS 877 IAW DWG 65-46592, AND SRM 51-40-2, PG. 1. 2 L 7 2 4F RT A16WE 2002020400023 20020204 00023 NM 2002 2 4 AWXA200200077 1 20020124 A 3350 20131A BATTERY BOEING 737 73733A 1384673 NM ZONE 200 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 WHILE AT GATE GROUND POWER WAS DISCONNECTED FROM AIRCRAFT AND EMERGENCY LIGHTS ILLUMINATED FOR 10 MINUTES. (NOTED BY FLI GHT ATTENDANT) FLIGHT ATTENDANT ATTEMPTED TO TURN LIGHTS OFF BY TURNING ON THE GROUND POWER SERVICE BUS, BUT EMERGENCY L IGHTS WOULD NOT EXTINGUISH UNTIL GROUND POWER WAS RESTORED. BATTERIES WOULD REQUIRE A 16 HOUR CHARGE TO RESTORE VOLTAGE CAPACITY SO MAINTENANCE REPLACED ALL 9 BATTERY PACKS IAW T/C A1C33005. SYSTEM OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT A16WE 2002020400024 20020204 00024 NM 2002 2 4 AWXA200200078 1 20020124 A 3350 100865 POWER SUPPLY BOEING 737 7373G7 1384595 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 304AW 24011 AFT EMERGENCY EXIT LIGHTS FROM ROW 18 LT, ALL THE WAY AFT WILL NOT ILLUMINATE DURING TEST. MAINTENANCE TROUBLESHOT AND FOUND THE AFT POWER SUPPLY INOPERATIVE AT BS 947, REPLACED POWER SUPPLY IAW BMM 33-51-51, EMERGENCY EXIT LIGHTS OPERATI ONALLY CHECKED GOOD. 2 L 7 2 4F RT A16WE 2002020400025 20020204 00025 NM 2002 2 4 AWXA200200079 1 20020125 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 DURING INSPECTION, EMERGENCY AFT ESCAPE PATH LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE TROUBLESHOT AND REPLACED THE EMERGENCY ESCAPE PATH LIGHTING BATTERY PACK AT BS 827. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002020400026 20020204 00026 NM 2002 2 4 AWXA200200081 1 20020125 A 3397 BR964411 WIRE BOEING 737 73733A 1384673 NM ROW 19 CHAFED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 175AW 23634 DURING INSPECTION EMERGENCY ESCAPE PATH LIGHTS WERE FOUND INOPERATIVE FROM SEAT ROW 19 ALL THE WAY AFT ON LT SIDE OF CAB IN. MAINTENANCE TROUBLESHOT AND FOUND A CHAFED WIRE AT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY ON SEAT ROW 19 LT. REMOVED A ND REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002020400027 20020204 00027 NM 2002 2 4 AWXA200200082 1 20020125 A 3350 F100055000 LENS AIRBUS A319 A319132 3930340 NM ZONE 220 DISLODGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 EMERGENCY EXIT LIGHT LENS FELL OFF FORWARD BULKHEAD LIGHT ASSEMBLY. MAINTENANCE REMOVED AND REPLACED FORWARD BULKHEAD EM ERGENCY EXIT LIGHT ASSEMBLY IAW 33-51-13. 2 L 7 2 4F RT A28NM 2002020400028 20020204 00028 EU 2002 2 4 AWXA200200083 1 20020127 A 3350 321451 POWER SUPPLY AIRBUS 320 A320232 3930326 EU ZONE 221 FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 654AW 1050 DURING BC-02 CHECK FWD LT EMERGENCY POWER SUPPLY UNIT (EPSU) 10WL FAILED LOAD TEST, RECEIVED MESSAGE ON PROGRAM AND TEST PANEL. MAINTENANCE REMOVED AND REPLACED THE FWD LT EPSU 10WL IAW 33-51-38-401, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002020400029 20020204 00029 NM 2002 2 4 AWXA200200085 1 20020129 A 7931 ST104Z TRANSMITTER BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE READS LOW A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 182AW 22649 P708358B AT TAKEOFF FROM PHX ENROUTE TO SLC, NR 1 ENGINE OIL PRESSURE READ 26 PSI AT 80 KTS, ALL OTHER ENGINE INDICATIONS WERE NO RMAL, ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT AND REPLACED THE NR 1 ENGINE OIL TRANSMITTER. ENGI NE RUN OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 2002020400030 20020204 00030 NM 2002 2 4 AWXA200200086 1 20020107 A 5740 65C26602108 ATTACH FITTING BOEING 737 737317 138447P NM SLAT ACTUATOR DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 DURING C-13 CHECK DAMAGE WAS FOUND TO THE RT WING NR 5 SLAT ACTUATOR ATTACH RIB WS 189. MAINTENANCE DRESSED OUT DAMAGE T O NR 5 SLAT ACTUATOR ATTACH RIB, FABRICATED REPAIR ANGLE AND SHIMS, AND INSTALLED REPAIRS. SLAT REMOVED AND REINSTALLED . 2 L 7 2 4F RT A16WE 2002020400031 20020204 00031 NM 2002 2 4 AWXA200200087 1 20020113 A 5740 65C26602217 ATTACH FITTING BOEING 737 737317 138447P NM SLAT ACTUATOR CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 DURING C-13 CHECK DAMAGE WAS FOUND TO THE LT WING NR 2 L/E SLAT ACTUATOR ATTACH RIB WS 189. MAINTENANCE DRESSED OUT DAMA GE TO NR 2 SLAT ACTUATOR ATTACH RIB, FABRICATED REPAIR ANGLE AND SHIMS, AND INSTALLED REPAIRS. SLAT REMOVED AND REINSTA LLED. 2 L 7 2 4F RT A16WE 2002020400032 20020204 00032 NM 2002 2 4 AWXA200200088 1 20020129 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM SEAT 19 DISLODGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 FLIGHT CREW REPORTED EMERGENCY EXIT LIGHT HANGING DOWN AT ROW 19 LT. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY AT ROW 19 LT, OPERATIONAL CHECK WAS GOOD IAW T/C A1C33009. 2 L 7 2 4F RT A16WE 2002020400033 20020204 00033 NM 2002 2 4 AWXA200200090 1 20020130 A 2133 OUTFLOW VALVE AIRBUS A319 A319132 3930340 NM CABIN PRESSURE MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 822AW 1410 WHILE ENROUTE FROM PHX TO RNO AIRCRAFT EXPERIENCED A CABIN PRESSURE CONTROLLER (CPC) SYSTEM NR 1 FAULT AND A FLUCTUATION OF PLUS OR MINUS 2000 FEET PER MINUTE OPERATION IN MANUAL MODE. ON THE PREVIOUS FLIGHT CPC SYSTEM NR 2 WAS PLACED ON ME L 21-31-01 CONDITION 1 FOR AUTO CABIN PRESSURE CONTROLLER SYSTEM NR 2 INOPERATIVE, AIRCRAFT DIVERTED TO LAS FOR REPAIRS. IN LAS MAINTENANCE TROUBLESHOT AND REPLACED THE OUTFLOW VALVE AND CLEARED MEL 21-31-01 IAW T/C R2D21301, OPERATIONAL CH ECKOUT OF PRESSURIZATION SYSTEM WAS GOOD. 2 L 7 2 4F RT A28NM 2002020400034 20020204 00034 EU 2002 2 4 AWXA200200091 1 20020129 A 3320 ABS0201076 LIGHT AIRBUS 320 A320232 3930326 EU ROW 14 BURNED OUT A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 657AW 1083 WHILE ENROUTE FROM PHX TO LAX A FLIGHT ATTENDANT REPORTED A BURNING ODOR THAT SMELLED LIKE BURNING WIRES AT SEAT ROWS 14 OR 15. AT LAX MAINTENANCE OPENED THE PANELS ON BOTH SIDES OF ROW 14 AND 15 AND PERFORMED A DETAILED INSPECTION LOOKING FOR ANY ABNORMALITIES, NONE WERE NOTED WITH THE EXCEPTION OF A BURNED OUT LIGHT BULB AT SEAT STATION 14 LT, THE BULB WAS REPLACED AND THE PANELS WERE RESECURED. A DETAILED INSPECTION OF BOTH THE LT AND RT MAIN LANDING GEAR WHEEL WELLS WAS A LSO PERFORMED WITH NO DEFECTS NOTED. MAINTENANCE RAN BOTH ENGINES WITH BOTH AIR CONDITIONING PACKS ON TRYING TO DUPLICAT E THE BURNING SMELL BUT COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002020400035 20020204 00035 NM 2002 2 4 AWXA200200094 1 20020120 A 5241 6545871123 SKIN BOEING 737 7373G7 1384595 NM GALLEY DOOR BENT A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 DURING C-16 CHECK THE SKIN WAS FOUND BENT OUTWARD AT THE UPPER FORWARD CORNER OF THE FORWARD GALLEY SERVICE DOOR BS 296. 5. MAINTENANCE CUTOUT DAMAGED SECTION OF SKIN AT BS 296.5, FABRICATED REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIR. 2 L 7 2 4F RT A16WE 2002020400052 20020204 00052 NM 2002 2 4 02FDEA00084 1 20020131 A 2750 18157013 TRANSMITTER BOEING 727 727247 138408F NM LH OB FLAP INOPERATIVE A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 236FE 21330 02-35 REPEAT AFTER T/O HAD IND OF ASYMMETRICAL OUTBOARD FLAPS LOCKED OUT. R&R OUTBOARD POS TRANSMITTER PER MM 27-52-013 -4. 2 L 7 3 4F A3WE 2002020400053 20020204 00053 NM 2002 2 4 02FDEA00085 1 20020201 A 3230 656E08 ACCESSORY UNIT BOEING 727 727227 1384078 NM E&E COMPARTMENT FAILED A FDEA O OTHER O OTHER CL CLIMB 1 SO 25 496FE 21670 02-36 AFTER DEPART LG WOULD NOT RETRACT. R&R LAND GEAR ACCESSORY BOX PER MM 32-09-112-5. GEAR HAD ICE ON ARRIVAL & DEIC ED. 2 L 7 3 4F A3WE 2002020500014 20020205 00014 NM 2002 2 5 02FDEA00086 1 20020201 A 5330 SKIN BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 CORROSION ON INTERNAL SKIN BS 1160, STR 30. R&R SKIN. 2 L 7 3 4F RT A3WE 2002020400055 20020204 00055 SO 2002 2 4 C2XA02CL021 1 20020126 A 2120 ODOR EMB 145 EMB145LR 3260212 SO COCKPIT DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 15980 145202 CLE FLIGHT 3030 THE CREW REPORTED A FUEL SMELL IN THE COCKPIT WHEN THE APU WAS STARTED IN FLIGHT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE FOUND.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002020400056 20020204 00056 GL 2002 2 4 C2XA02CL027 2 20020129 A 7200 23070402 ENGINE EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL RIGHT PYLON FAILED A C2XA B A EMER. DESCENT UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 27 16510 3688 145251 CAE311393 CLE FLIGHT 3052 THE CREW REPORTED THE NR 2 ENGINE SHUT DOWN IN FLIGHT UNCOMMANDED. THEY REPORTED A LOUD BANG AND HIGH I TT. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE.OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002020400057 20020204 00057 SO 2002 2 4 C2XA02TY017 1 20020201 A 3030 PITOT TUBE EMB 145 EMB145ER 3260211 SO PITOT HEAT MISWIRED A C2XA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 27 14930 145011 DURING A SCHEDULED 1C INSPECTION, THE PITOT AND STATIC PORT HEATING CHECK FAILED STEP 29 OF TASK CARD 30-31-00-710-001-A OO, WHEN HEATING/PITOT 1 CIRCUIT BREAKER IS PULLED THE STATIC PORTS 1 AND 2 BECAME COOL INSTEAD OF 1 AND 4. MAINTENANCE REWIRED STATIC PORT HEATERS NR 2 AND 4, OPERATIONAL CHECKED GOOD. REPAIR PROCEDURES ARE SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLECTION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002020400058 20020204 00058 SO 2002 2 4 C2XA02TY018 1 20020201 A 5554 12040071001 FITTING EMB 145 EMB145ER 3260211 SO RUDDER DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 DURING A SCHEDULED 1C INSPECTION, THE NR 3 HINGE FITTING FROM TOP OF RUDDER 1, AFT EDGE HAS DAMAGE. MAINTENANCE BLENDED THE DAMAGE AND PERFORMED DYE PENETRANT INSPECTION (NO DEFECTS NOTED) ALODINED, PRIMED AND PANTED I/A/W-GST-0362/02. REPA IR PROCEDURES ARE SATISFACTORY, AIRCRAFT WILL BE RELEASED UPON COMPLECTION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002020400061 20020204 00061 SO 2002 2 4 SWIA200210556 1 20020105 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO ELEVATOR FAULTY A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 268UE 120207 AT 220 KTS IAS HAND FLYING VMC NON-ICING CONDITION AIRCRAFT LEVELED NOSE DOWN, TRIM AT 2.0 (NO MORE TRIM DOWN). EXCESSI VE FORWARD PRESSURE TO HOLD LEVEL FLIGHT. ONLY WAY TO HOLD ALT WAS WITH POWER REDUCTION. AIRCRAFT COULD NOT BE FLOWN A BOVE 210 KTS. UPON A/P DISCONNECT ON FINAL APP, A/C PITCHED UP AND REQUIRED TRIM DOWN DURING FLARE. ELEVATOR PRESSURE AND FEEL IS UNUSUALLY LIGHT. REMOVED AND REPLACED RIGHT AND LEFT ELEVATOR TRIM ACTUATORS WITH SERVICEABLE ACTUATORS IAW EMB120 MM 27-32-02. 2 L 7 2 4T RT A31SO 2002020400062 20020204 00062 2002 2 4 SWIA200210557 4 20020118 A 3418 CONTROL PANEL EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 268UE 120207 STALL WARNING MAP ILLUMINATED ON TAKEOFF. ABORTED TAKEOFF. LEFT STALL WARNING. INSTALLED SERVICEABLE TEST PANEL. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002020400063 20020204 00063 2002 2 4 SWIA200210558 4 20020115 A 3414 INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT DEFECTIVE A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 562SW 120336 HIGH SPEED VOICE WARNING DURING TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED NR 2 AIRSPEED INDICATOR. PERFORMED OPS CHECK. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002020400064 20020204 00064 SO 2002 2 4 SWIA200210559 1 20020115 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER K F J FLUID LOSS FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 235SW 5023 5023 120310 BLUE SYSTEM HYDRAULIC FAILURE UPON DEPLOYING 15 DEGREES FLAPS ON LANDING. INSPECTED AND FOUND BLOWN RIGHT NACELLE FLAP ACTUATOR. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002020400065 20020204 00065 EA 2002 2 4 SWIA200210561 1 20020113 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA A/C BAY MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 497SW 7482 LEFT PACK HIGH PRESSURE CAUTION MESSAGE IMMEDIATELY AFTER TAKEOFF. RAN ENGINES. FOUND PACK TO OPERATE NORMAL. 2 L 7 2 4F RT A21EA 2002020400066 20020204 00066 2002 2 4 SWIA200210562 4 20020115 A 2210 6229968001 DAMPER CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS FAILED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 409SW 5740 5740 7056 NR 1 YAW DAMPER WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPER IAW 22-20-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002020400067 20020204 00067 SO 2002 2 4 SWIA200210563 1 20020108 A 3010 DEICE SYSTEM EMB 120 EMB120ER 3260203 SO WING MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 295UX 120295 LEFT OUTBOARD WING DEICE BOOT INOP LIGHT IN ICING CONDITIONS. RETURNED TO SFO. RE-CHECKED INFLATION OF LEFT AND RIGHT OUTBOARD WING BOOTS. FOUND GOOD. SWAPPED LEFT AND RIGHT OUTBOARD WING BOOT PRESSURE SWITCHES FOR TROUBLESHOOTING. RAN ENGINES. OPERATIONAL CHECK OF DEICE SYSTEM GOOD. 2 L 7 2 4T RT A31SO 2002020400068 20020204 00068 SO 2002 2 4 SWIA200210564 1 20020116 A 2797 WIRE EMB 120 EMB120ER 3260203 SO FLIGHT CONTROL BROKEN A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 296SW 120325 ON TAKEOFF ROLL, CONTROL DISENGAGE MAP LIGHT ILLUMINATED. ABORTED TAKEOFF. REPAIRED BROKEN WIRE ON CONTROL DISENGAGE CONNECTOR 2P1421. OPS CHECK GOOD. PLACARD REMOVED. 2 L 7 2 4T RT A31SO 2002020400069 20020204 00069 SO 2002 2 4 SWIA200210565 1 20020116 A 3010 CONNECTOR EMB 120 EMB120ER 3260203 SO DEICE SYSTEM DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 291SW 120318 RIGHT OUTBOARD STAB AND VERTICAL STAB DEICE LIGHTS ILLUMINATED DURING CLIMBOUT. TRIED BOTH TIMER 1 AND TIMER 2 SEVERAL TIMES. RETURNED TO SEA. REMOVED RIGHT OUTBOARD PRESSURE SWITCH CANNON PLUG, CLEANED AND REINSTALLED. OPS CHECK GOOD O N GROUND. 2 L 7 2 4T RT A31SO 2002020400070 20020204 00070 EA 2002 2 4 SWIA200210567 1 20020117 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 405SW 7029 PRIOR TO FAF AT IDA, WHEN F/O CALLED FLAPS 8 RECEIVED A (FLAP FAIL) AMBER MESSAGE. CONSULTED QRH. FLAPS WERE STUCK AT 8 DEGREES. RETURNED TO SLC. LEFT BPSU FAILED BRAKE CHECK. REMOVED AND REPLACED LEFT BPSU. PERFORMED OPERATIONAL CHEC KS, NO FAULTS NOTED. REF MM 27-51-10. 2 L 7 2 4F RT A21EA 2002020400071 20020204 00071 SO 2002 2 4 SWIA200210568 1 20020117 A 2422 PC2511C INVERTER EMB 120 EMB120ER 3260203 SO NR 2 MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 223SW 4445 4445 120291 ON INITIAL TAKEOFF ROLL, INVERTER NR 2 INOP LIGHT CYCLES ON AND OFF TWICE WITH NO INDICATIONS OF AN INVERTER NR 2 FAILUR E. TAKEOFF WAS ABORTED. REPLACED NR 2 INVERTER WITH SERVICEABLE ASSEMBLY FOR TROUBLESHOOTING. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002020400072 20020204 00072 SO 2002 2 4 SWIA200210570 1 20020115 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO CABIN PRESSURE FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 223SW 120291 UPON ADVANCING POWER LEVERS FOR TAKEOFF, PRESSURIZATION VSI WENT TO 2000 FPM DOWN. ABORTED TAKEOFF AND RETURNED TO GATE . REPLACED ELECT. ALTITUDE PRESSURE CONTROLLER. PERFORMED OPS CHECK. OPS CHECK GOOD. S/N OFF: 153. 2 L 7 2 4T RT A31SO 2002020400073 20020204 00073 SO 2002 2 4 SWIA200210571 1 20020118 A 7697 WIRE EMB 120 EMB120ER 3260203 SO LT ENGINE CHAFED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 576SW 120345 FLIGHT IDLE UNLOCK LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. INSPECTED FLI GHT IDLE STOP WIRING AT LEFT ENGINE DECK. FOUND WIRE RUBBING ON ENGINE DECK. WIRE STILL SERVICEABLE AT THIS TIME. APP LIED ANTI-CHAFE AT RUBBING POINT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002020400074 20020204 00074 NM 2002 2 4 SWAA020198 1 20020126 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 645SW 28330 DURING SCHEDULED BC3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002020400075 20020204 00075 NM 2002 2 4 SWAA020200 1 20020126 A 3350 311500 LENS BOEING 737 7373Y0 1384671 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 8 DEF. SECURED LENS PE R MM. 2 L 7 2 4F RT A16WE 2002020400076 20020204 00076 NM 2002 2 4 SWAA020202 1 20020126 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED 3 INCHES LONG AT BS 727D + 2, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002020400077 20020204 00077 NM 2002 2 4 SWAA020203 1 20020126 A 5312 6516300 BULKHEAD BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 201 AND RBL 5, WL 188 AND RBL 1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002020400078 20020204 00078 NM 2002 2 4 SWAA020204 1 20020126 A 5312 6545409 PRESSURE PANEL BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 665, LBL31. REPAIRED WEB PER SWA TI. 2 L 7 2 4F RT A16WE 2002020400079 20020204 00079 NM 2002 2 4 SWAA020205 1 20020128 A 5330 589357 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED .25 INCHES LONG AT POINT C ON RT C-D WINDOW POST. REPAIRED SKI N PER SRM. 2 L 7 2 4F RT A16WE 2002020400080 20020204 00080 NM 2002 2 4 SWAA020206 1 20020128 A 5330 589358 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED .1 INCHES LONG AT POINT C ON LT C-D WINDOW POST. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002020400081 20020204 00081 NM 2002 2 4 SWAA020207 1 20020128 A 5240 6545871 DOOR FRAME BOEING 737 7373Y0 1384671 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED (3 EA) AT STOP CUT OUTS. REMOVED AND REPLACED DOOR PE R MM. 2 L 7 2 4F RT A16WE 2002020400082 20020204 00082 NM 2002 2 4 SWAA020208 1 20020127 A 5315 BAC1509 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 787 AND 847, RBL 8. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002020400083 20020204 00083 NM 2002 2 4 SWAA020209 1 20020125 A 5330 6545866 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 602SW 27953 DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM SKIN CRACKED ON BOTH LT AND RT SIDES AT BS 705. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002020400084 20020204 00084 NM 2002 2 4 SWAA020210 1 20020127 A 5610 5893543110 WINDOW BOEING 737 7373G7 1384595 NM COCKPIT CRACKED A SWAA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SW 07 690SW 23783 AIR TURNBACK, R-1 WINDOW SHATTERED AFTER T/O. REMOVED AND REPLACED WINDOW AND HEAT CONTROL UNIT PER MM. 2 L 7 2 4F RT A16WE 2002020400085 20020204 00085 NM 2002 2 4 SWAA020220 1 20020129 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D CHECK, FOUND STRINGER 5R CRACKED AT BS 1006. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2002020400086 20020204 00086 NM 2002 2 4 SWAA020222 1 20020130 A 5311 6546542 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED 1/2D CHECK, FOUND BS 663 FUSELAGE FRAME CRACKED AT STRINGERS 2L AND 2R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002020400087 20020204 00087 NM 2002 2 4 SWAA020223 1 20020127 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (3 INCHES LONG), BS 500C, STRINGER 15R. REPAIRED SKIN PER SWA RA . 2 L 7 2 4F RT A16WE 2002020400088 20020204 00088 NM 2002 2 4 SWAA020224 1 20020127 A 5330 6546574 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (1.9 INCHES LONG), BS 727E, STRINGER 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002020400089 20020204 00089 NM 2002 2 4 SWAA020226 1 20020129 A 3350 207330 CAP BOEING 737 7372H4 138448C NM CABIN FLOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED C4 CHECK, FOUND BOTH FWD AND AFT EEPLS END CAPS MISSING. INSTALLED BOTH END CAPS PER MM. 2 L 7 2 4F A16WE 2002020400090 20020204 00090 NM 2002 2 4 SWAA020227 1 20020130 A 3350 07912 LENS BOEING 737 7373A4 1384585 NM CABIN FLOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 EEPLS LENS COVERS MISSING AT ROWS 3, 17, AND 20. DEFERRED PER MEL. LATER AT TPA DURING RON, INSTALLED LENSES PER MM. 2 L 7 2 4F RT A16WE 2002020400091 20020204 00091 NM 2002 2 4 SWAA020228 1 20020130 A 5311 6545807 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE STUB FRAME CRACKED (.62 INCHES LONG) AT FWD SERVICE DOOR BELOW UPPER HINGE CUT OUT. REPAIRED FRAME PER SWA RA. 2 L 7 2 4F RT A16WE 2002020400092 20020204 00092 NM 2002 2 4 SWAA020214 1 20020128 A 3350 311500 LENS BOEING 737 7373Y0 1384671 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 6 ABC. SECURED LENS PE R MM. 2 L 7 2 4F RT A16WE 2002020400093 20020204 00093 NM 2002 2 4 SWAA020215 1 20020129 A 5310 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 960, STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002020400094 20020204 00094 NM 2002 2 4 SWAA020216 1 20020129 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR UPPER CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002020400095 20020204 00095 NM 2002 2 4 SWAA020218 1 20020129 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED BELOW FLOOR AT BS 578, STR 17R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002020400096 20020204 00096 NM 2002 2 4 SWAA020219 1 20020125 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) AT STR 10L, BS 370 TO BS 500B AND (4 EA) AT STR 4L, B S 390 TO BS 812. 2 L 7 2 4F A16WE 2002020400097 20020204 00097 WP 2002 2 4 CNMA200200001 1 20020130 A 3610 8986263 REGULATOR VALVE DOUG DC10 DC1030 3023501 WP INOPERATIVE A CNMA A H J UNSCHED LANDING DEACTIVATE SYST/CIRCUITS DUMP FUEL J M WARNING INDICATION OVER TEMP CL CLIMB 1 SW 07 540AX 46595 #3 PNEUMATIC SUPPLY PRESSURE READS ZERO WITH SUPPLY SELECTOR IN ANY MODE. COM PROCEDURES ACCOMPLISHED ON CLIMBOUT. #2 PN EUMATIC SUPPLY HI TEMP ILLUMINATED. TEMP GUAGE INDICATED RE LINE. 2 L 7 3 4F A22WE 2002020400098 20020204 00098 SO 2002 2 4 SWIA200210572 1 20020122 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAP MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 579SW 5141 5141 120347 AFTER TAKEOFF DURING FLAP RETRACTION, FLAP LIGHT ON MAP WITH DISAGREEMENT ON OUTBOARD PAIR. APPLIED QRH PROCEDURE, NO H ELP. RETURNED TO SLC. CLEANED GLYCOL FROM ACTUATOR CANNON PLUGS, REPLACED FLAP CONTROL UNIT AND REPLACED RIGHT OUTBOAR D FLAP ROLLERS (4). OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002020400099 20020204 00099 EA 2002 2 4 SWIA200210573 1 20020122 A 5610 601R3303310 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 493SW 7450 RIGHT WINDSHIELD CRACKED. REMOVED AND REPLACED RIGHT WINDSHIELD. PRESSURIZED AIRCRAFT. LEAK CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002020400100 20020204 00100 EA 2002 2 4 SWIA200210575 1 20020121 A 2131 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 497SW 7482 ON CLIMBOUT UNABLE TO PRESSURIZE. LEFT REMAINING PACK SHUTOFF UPON BLEED TRANSFER. RETURNED TO FIELD. OPERATED BOTH L T AND RT PACKS AND OPS CHECKED BOTH PRESSURIZATION CONTROLLERS. SYSTEM OPS CHECK GOOD. UNABLE TO DUPLICATE SQUAWK. 2 L 7 2 4F RT A21EA 2002020400101 20020204 00101 SO 2002 2 4 SWIA200210576 1 20020118 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 250YV 120250 RIGHT INBOARD FLAP WILL NOT RETRACT. INSPECTED RIGHT INBOARD FLAP. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. REMOVED AND REPLACED FCU. CYCLED FLAPS SEVERAL TIMES. OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2002020400102 20020204 00102 SO 2002 2 4 SWIA200210577 1 20020119 A 5350 TAIL CONE EMB 120 EMB120ER 3260203 SO FUSELAGE OUT OF POSITION A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 190SW 120050 CONTROL YOKE BINDS ABOUT HALFWAY THROUGH FORWARD AND AFT TRAVEL WITH ELEVATOR TRIM IN THE GREEN ARC. BIND IS LESS WITH ELEVATOR TRIM FULL FORWARD AND GOES AWAY COMPLETELY WITH TRIM FULL AFT. REPOSITIONED TAIL CONE TO PREVENT RUBBING ON EL EVATOR. OPS CHECK GOOD. NO FURTHER DEFECTS FOUND. 2 L 7 2 4T RT A31SO 2002020400103 20020204 00103 SO 2002 2 4 C2XA02CL031 1 20020203 A 5300 FIREWALL EMB 135 EMB135ER 3260203 SO AFT FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 DURING ROUTINE MAINTENANCE THE APU FIREWALL WAS FOUND CRACKED AT UPPER RIGHT CORNER OF FIREWALL.THE FIREWALL WAS REPAIRE D I/A/W EMBRAER GST-0401/02.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002020400104 20020204 00104 EA 2002 2 4 SWIA200210578 1 20020120 A 2432 100021101 CHARGER CNDAIR CL600 CL6002B19 1900309 EA E/E BAY DEFECTIVE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 437SW 763 763 7564 MAIN BATTERY CHARGER MESSAGE INFLIGHT. RETURNED TO FIELD. REMOVED AND REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002020400105 20020204 00105 SO 2002 2 4 SWIA200210579 1 20020118 A 2752 3430001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 250YV 13 13 120250 RIGHT INBOARD FLAP DROOPS. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. OPS CHECKED GOOD. NO LEAKS FOUND. 2 L 7 2 4T RT A31SO 2002021900047 20020219 00047 EA 2002 2 19 COMA0260076 1 20020105 A 2897 601R571351 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA LT FUEL TANK CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 987CA 9467 7199 WHILE WORKING DEFERRED MAINTENANCE ON LT FUEL QUANTITY SYSTEM, FOUND THE FUEL LEVEL PROBE WIRE HARNESS, BETWEEN NR 3 PRO BE AND CONNECTOR J3QB/P3QB, CHAFING ON FUEL BAFFLE P/N 601R62359-1. REPLACED WIRE HARNESS. 2 L 7 2 4F RT A21EA 2002020400106 20020204 00106 EA 2002 2 4 SWIA200210581 1 20020122 A 5610 1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 440SW 7589 CAPTAIN'S SIDE WINDOW SHATTERED ON TAXI OUT. REMOVED AND REPLACED LEFT WINDOW IAW 56-12-01. 2 L 7 2 4F RT A21EA 2002021900048 20020219 00048 EA 2002 2 19 COMA0260077 1 20020115 A 2897 601R571351 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA LT FUEL TANK CHAFED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 988CA 9234 7204 WHILE WORKING DEFERRED MAINTENANCE ON LT FUEL QUANTITY SYSTEM, FOUND THE FUEL LEVEL PROBE WIRE HARNESS, BETWEEN NR 3 PRO BE AND CONNECTOR J3QB/P3QB CHAFING ON FUEL BAFFLE P/N 601R62359-1. REPLACED THE WIRE HARNESS. 2 L 7 2 4F RT A21EA 2002020400107 20020204 00107 EA 2002 2 4 COMA0260078 1 20020131 A 3030 7858062 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 920CA 6154 7022 FLIGHT 5249 LEFT AOA HEAT MESSAGE AND LEFT STATIC HEAT MESSAGE.REPLACED THE ADSHC. 2 L 7 2 4F RT A21EA 2002020400110 20020204 00110 NM 2002 2 4 ABXA010696 1 20020131 A 7920 ST332T00432 SWITCH BOEING 767 767231 1385131 NM #1 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 GL 23 702AX 2291 22566 LEFT ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED. #1 ENGINE SHUTDOWN, EMERGENCY DECLARED, DIVERTED TO SLC. AFTER ENGINE SHUTDOWN, MESSAGE DISAPPEARED. REPLACED THE OIL PRESSURE SWITCH ON THE LEFT ENGINE. SYSTEM OPS CHECKED GOOD IAW BOEING MM. 2 L 7 2 4F RT A1NM 2002020400111 20020204 00111 EA 2002 2 4 02032649 1 20020201 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 1900309 EA CABIN FAILED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 649BR 7414 Emergency floor track lighting section inoperative. Maintenance personnel removed and replaced an emergency floor track lighting system lamp assembly. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002020400112 20020204 00112 EU 2002 2 4 02032305 1 20020201 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 305UE 41019 During preflight inspection, the crew reported that the emergency floor track lighting was inoperative. Maintenance per sonnel secured a loose connector for the emergency floor track lighting system. An operational check was satisfactory a nd the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002020400113 20020204 00113 EU 2002 2 4 02034301 1 20020203 A 3350 5521421 BATTERY PACK JETAIR JETSTM JETSTM4101 1500501 EU AFT CABIN DISCHARGED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 301UE 41012 During preflight inspection, the crew reported that the emergency floor track lighting was inoperative from seat row 7 a ft. Maintenance personnel removed and replaced the aft emergency lighting battery pack. An operational check was satis factory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002020400115 20020204 00115 WP 2002 2 4 CALA0200049 1 20020128 A 3350 FUSE DOUG DC9 DC982 3022082 WP BATTERY PACK INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10801 49127 THIRTEEN AFT SEAT MOUNTED EMERGENCY PATH LIGHTS WOULD NOT ILLUMINATE WHEN TESTED. THE AFT BATTERY PACK FUSE WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 2002020400116 20020204 00116 WP 2002 2 4 CALA0200050 1 20020128 A 3350 20131A BATTERY PACK DOUG DC9 DC982 3022082 WP EXIT SIGN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10801 49127 THE FORWARD OVERWING EMERGENCY EXIT DOOR SIGN FAILED DURATION TEST. THE BATTERY PACK WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-53-00. 2 L 7 2 4F A6WE 2002020400117 20020204 00117 NM 2002 2 4 PCAA0201017 1 20020117 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 830EX 155 DURING C-CHECK INSPECTION, CABIN INBOARD RIGHT SEAT RAIL FOUND HAVE EXCESSIVE CORROSION AT STATION X207. RIGHT INBOARD SEAT RAIL REPAIRED WITH A REPLACEMENT SPLICE AT STATION X207 IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-53-1102, RD8-53-2295 & RD8-53-3074. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002020400118 20020204 00118 WP 2002 2 4 CALA0200051 1 20020128 A 3350 20131A BATTERY PACK DOUG DC9 DC982 3022082 WP ROWS 9-12 INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10801 49127 THE OVERHEAD EMERGENCY LIGHTS AT ROWS 9-12 WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-53-00. 2 L 7 2 4F A6WE 2002020400119 20020204 00119 WP 2002 2 4 CALA0200052 1 20020128 A 3350 20131A BATTERY PACK DOUG DC9 DC982 3022082 WP ROWS 19-23 INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10801 49127 THE OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 19-23 FAILED DURATION TEST. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPE RATIONAL CHECKS WERE GOOD IAW MM 33-53-00. 2 L 7 2 4F A6WE 2002020400120 20020204 00120 NM 2002 2 4 CALA0200053 1 20020129 A 2530 8201110000A OVEN BOEING 737 737824 13844BZ NM FWD GALLEY INOPERATIVE A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 18223 1706 28932 SMOKE WAS REPORTED COMING FROM THE FORWARD GALLEY NR 2 OVEN WHILE ENROUTE FROM CLE TO RSW. THE OVEN WAS SWITCHED OFF AND GALLEY POWER WAS DISCONNECTED. THE AIRCRAFT WAS DIVERTED TO CVG WHERE IT LANDED WITHOUT INCIDENT. THE FORWARD GALLEY NR 2 OVEN AND CONTROLLER WERE REMOVED AND REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO SMOKE OBSERVED. 2 L 7 2 4F RT A16WE 2002020400121 20020204 00121 NM 2002 2 4 CALA0200057 1 20020129 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND FOUR 1/2 INCH CRACKS IN SEAT TRACK FRAME AT STA 727B. A STRAP REPAIR WAS INSTALLED AT EACH LOCATION IAW ECRA 5321-01122. 2 L 7 2 4F RT A16WE 2002020400122 20020204 00122 WP 2002 2 4 CALA0200059 1 20020130 A 2560 61020 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND THE FORWARD ENTRY I/B EMERGENCY FLASHLIGHT INOPERATIVE. THE FLASHLIGHT BATTERY WAS REPLACED. 2 L 7 2 4F A6WE 2002020400123 20020204 00123 EA 2002 2 4 COMA0260079 1 20020202 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 916CA 7014 FLIGHT 5957 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002020400124 20020204 00124 EA 2002 2 4 COMA0260080 1 20020202 A 7930 601509197 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 971CA 3918 7145 FLIGHT 5401 LEFT ENGINE LOW OIL PRESSURE WARNING.REPLACED THE OIL PRESSURE TRANSDUCER. 2 L 7 2 4F RT A21EA 2002020400125 20020204 00125 EA 2002 2 4 COMA0260081 1 20020202 A 3260 864202 SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF ADJ A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 739CA 7273 FLIGHT 5868 LANDING GEAR DISAGREE WARNING. NLG DID NOT RETRACT.ADJUSTED THE NLG CENTERED PROMIMITY SENSOR PS 14GA. 2 L 7 2 4F RT A21EA 2002020400126 20020204 00126 EA 2002 2 4 COMA0260082 1 20020203 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 403CA 7428 FLIGHT 5477 FLAPS FAILED DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002020400127 20020204 00127 WP 2002 2 4 DHL2002805022 1 20020102 A 5200 975106530 FITTING DOUG DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 46125 N/R 1994LT. AFT PAX DOOR UPPER INNER SECTION FITTING CRACKED 1" STA. 1600 2 L 7 4 4F RT 4A25 2002020400128 20020204 00128 WP 2002 2 4 DHL2002805023 1 20020102 A 5300 ANGLE DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R1841NLG W/W DOOR FRAME ANGLE @ STA -99 RT. , CRACKED 1" 2 L 7 4 4F RT 4A25 2002020400129 20020204 00129 WP 2002 2 4 DHL2002805024 1 20020101 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 805DH 75397 46125 N/R 1992RT. WING LEADING EDGE INNER RIB (FORMER) CRACKED 1" @ STA. XFS601.000 2 L 7 4 4F RT 4A25 2002020400133 20020204 00133 WP 2002 2 4 DHL2002805036 1 20020118 A 5753 47602680 ANGLE DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 LFT WING T/E FLAP LINK SUPPORT ANGLE CRACKED 1 IN AT XW 106.000 2 L 7 4 4F RT 4A25 2002020400134 20020204 00134 WP 2002 2 4 DHL2002805037 1 20020119 A 5730 5769960402 DOOR DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 R/H INBD SLOT DOOR UPPER SKIN SURFACE SHOWS A 1/2 IN CRACK BETWEEN STA XW 223.500 AND 293.793 2 L 7 4 4F RT 4A25 2002020400135 20020204 00135 WP 2002 2 4 DHL2002805040 1 20020125 A 3233 38875331 BRACKET DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 L/H MLG UP LOCK ACTUATER BRAKET CRACKED 2 L 7 4 4F RT 4A25 2002020400136 20020204 00136 WP 2002 2 4 DHL2002805044 1 20020119 A 5700 5769857613 ANGLE DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 LT WING Z ANGLE CRACKED 5 IN AT STA XW 485.000 2 L 7 4 4F RT 4A25 2002020400137 20020204 00137 NM 2002 2 4 P5CA0200630 1 20020122 A 3251 DL1020M1861 ACTUATOR BOEING 747 747122 1384872 NM NLG FAILED A P5CA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 23 853FT 19753 RUDDER PEDAL STEERING INOPERATIVE ON TAKEOFF ROLL. TILLER OK. TURNED BACK TO BLOCKS FOR MAINTENANCE. REMOVED AND REPL ACED RUDDER PEDAL STEERING ACTUATOR PER MM 32-51-07 PG 401 THROUGH 403. OPS NOW OK. 2 L 7 4 4F A20WE 2002020400139 20020204 00139 NM 2002 2 4 PCAA0201021 1 20020129 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DIRTY A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 814EX 318 BUF-FLIGHT 3600 CREW REPORTED CABIN EMERGENCY LIGHTS FLICKER ON AND OFF DURING FLIGHT. MAINTENANCE CLEANED CANNON PLUG ON EMERGENCY LIGHTS CONTROL BOX. SYSTEM OPERATES NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002020400140 20020204 00140 NM 2002 2 4 PCAA0201022 1 20020129 A 3350 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 833EX 282 DURING ROUTINE MAINTENANCE VISIT LEFT AFT FUSELAGE AND TWO CENTER OVERHEAD EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. BA TTERY PACK AT POSITION 300 REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002020400141 20020204 00141 NM 2002 2 4 PCAA0201025 1 20020124 A 5347 CARGO TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE DAMAGED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 829EX 146 DURING C-CHECK INSPECTION CARGO BAY RIGHT SEAT RAIL FOUND TO HAVE A HOLE APPROXIMATELY .8437 INCH FROM STEP UP IN BULKHE AD AT STATION 600. GOUGE 1.5 INCH AFT OF HOLE. GOUGE IS .030 INCH. SEAT RAIL SECTION REPLACED IN ACCORDANCE WITH DEHA VILAND STRUCTURAL REPAIR MANUAL AND REPAIR DRAWING RD8-53-4472. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002020400142 20020204 00142 NM 2002 2 4 PCAA0201026 1 20020124 A 5751 SKIN DHAV DHC8 DHC8102 2809003 NM AILERON DENTED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 829EX 146 DURING C-CHECK INSPECTION RIGHT AILERON RIGHT TOP SURFACE FOUND DENTED .304 INCH DEEP BY 2 INCHES. AILERON REPAIRED IN ACCORDANCE WITH SRM AND EO8-57-02-0084, AS APPROVED BY DERY-230219-CE. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002020400143 20020204 00143 NM 2002 2 4 QXEA0200080 1 20020126 A 3230 LANDING GEAR BOMBDR DHC8 DHC8401 NM NLG & MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 411QX 4055 YYC - ON TAKEOFF, AND GEAR SELECTED UP, GEAR DID NOT RETRACT AND LANDING GEAR PANEL SHOWED 3 GREEN LIGHTS, AND THE LANDI NG GEAR HANDLE HAD 3 RED LIGHTS. PERFORMED EMERGENCY/ABNORMAL CHECKLIST AND RETURNED TO FIELD. MAINTENANCE INSPECTED T HE PROXIMITY SWITCHES, DOOR SEALS, DOOR MECHANISMS, NOSE GEAR, AND BOTH LANDING GEAR ASSEMBLIES. AIRCRAFT WAS JACKED AN D THE LANDING GEAR WAS CYCLED SEVERAL TIMES. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002020400144 20020204 00144 EA 2002 2 4 QXEA0200081 1 20020128 A 2613 6007300 THERMOCOUPLE CNDAIR CL600 CL6002C10 1390015 EA NR 3 BRAKE FAULTY A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 604QX 10019 BOI-RECEIVED A GEAR BAY OVERHEAT WARNING WHILE AT 25,000 FEET. NR 3 BRAKE TEMP INDICATED HOT. FOLLOWED EMERGENCY PROCE DURES AND DESCENDED TO 21,000 FEET. WARNING WENT AWAY AND REOCCURRED 10 MINUTES LATER. REPEATED EMERGENCY PROCEDURES A ND LEFT LANDING GEAR DOWN. DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 3 BRAK E TEMP THERMOCOUPLE SENSOR. COMPLIED WITH SELF TEST. ALL NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002020400145 20020204 00145 EU 2002 2 4 QXEA0200082 1 20020124 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAULTY A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 498US 11181 SEA- GALLEY EMERGENCY EXIT SIGN INOPERATIVE IN ARM. REPLACED LAMP BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F RT A20EU 2002020400146 20020204 00146 EA 2002 2 4 QXEA0200083 1 20020130 A 2913 6619002 PUMP CNDAIR CL600 CL6002C10 1390015 EA HYDRAULIC SYS LEAKING A QXEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 600QX 683 10005 SEA - SYSTEM ONE HYDRAULIC LOW PRESS CAUTION LIGHT CAME ON AND NUMBER ONE HYDRAULIC SYSTEM QUANTITY SHOWS ZERO IN FLIGHT . CREW PERFORMED EMERGENCY/ABNORMAL CHECKLIST. FOUND LEFT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REPLACED THE NUMBER O NE HYDRAULIC PUMP. OPERATIONAL CHECK AND LEAK CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002020400147 20020204 00147 NM 2002 2 4 QXEA0200084 1 20020126 A 5210 HANDLE BOMBDR DHC8 DHC8401 NM PAX DOOR OUT OF ADJ A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 405QX 4047 SEA - MAIN CABIN DOOR CANNOT BE OPENED FROM THE OUTSIDE. MAINTENANCE ADJUSTED THE DOOR HANDLE IAW EA 6-52-129. OPERATI ONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002020400148 20020204 00148 EU 2002 2 4 RAIA00201029 1 20020124 A 2440 PANEL AEROSP ATR72 ATR72202 8680940 EU EXTERNAL POWER DAMAGED A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 722TE 220 5602-STL- DURING ENGINE START, HEARD LOUD BANG. SMOKE COMING FROM BEHIND F/O. SMELLED ELECTRICAL. MAINTENANCE REPAIRE D THE GROUND PANEL OF THE GPU RECEPTACLE, IAW ATR SRM. 2 H 7 2 4T RT A53EU 2002020400149 20020204 00149 EU 2002 2 4 RAIA00201035 1 20020130 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 560HK 41076 MX-STL- EMERGENCY PATH LIGHTS A ROW 7 & 8 INOP. RECONNECTED CONNECTOR, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002020400150 20020204 00150 EU 2002 2 4 RAIA00201036 1 20020130 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 561HK 41077 MX-STL- SOME ESCAPE PATH LIGHTS INOP. RESECURED EMERGENCY ESCAPE PATH LIGHT CONNECTOR, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002021900074 20020219 00074 NM 2002 2 19 SPAA0200049 1 20020124 A 3233 654491029 ACTUATOR BOEING 737 7372Y5 1384554 NM RT MLG LEAKING A SPAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 712S 23038 FLT 712 DEPARTED IGM AT 1900 HRS ZULU. AFTER TAKEOFF RIGHT LANDING GEAR IN TRANSIT LIGHT (RED) WOULD NOT EXTINGUISH. L ANDING GEAR EXTENDED AND VERIFIED LOCKED. AIRCRAFT RETURNED TO ORIGINATING AIRPORT. 2 L 7 2 4U RT A16WE 2002020400151 20020204 00151 NM 2002 2 4 SWAA020167 1 20020122 A 5310 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002020500015 20020205 00015 NM 2002 2 5 C1HA200281001 1 20020202 A 5610 WINDOW BOEING 727 7272S7 138407Z NM COCKPIT CRACKED A C1HA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 681CA 22020 ENROUTE AT FL290 WINDOW R2 FAILED OUTER PANE SPIDER WEBBED AND ARCED AND WHISTLED. REMOVED AND REPLACED R2 WINDOW, NO D EFECTS NOTED. OPS CHECK AND LEAK CHECKS NORMAL. A/C OKAY FOR CONTINUED SERVICE. 2 L 7 3 4F A3WE 2002020500016 20020205 00016 NM 2002 2 5 C1HA200282001 1 20020201 A 5313 STRINGER BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 STA. 560 FWD SIDE OF TOP ANGLE IS EXFOLIATED ON O/B SIDE OF STR 26 RT, ALSO HAS ONE CORRODED FASTENER THRU WEB. (C CHE CK FINDING) REPAIR APPROVED BY 8110. 2 L 7 3 4F A3WE 2002020500017 20020205 00017 NM 2002 2 5 C1HA200282002 1 20020201 A 5320 FLOOR SUPPORT BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 FLOOR SUPPORT CORRODED STA. 1070 LBL 22-44. (C CHECK FINDING) REPAIRED PER SRM 2 L 7 3 4F A3WE 2002020500018 20020205 00018 NM 2002 2 5 C1HA200282003 1 20020201 A 5313 STRINGER BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA O OTHER O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 AFT PIT STR 29 LT CORRODED AT STA. 950 A. (C CHECK FINDING) REPAIR APPROVED BY 8110. 2 L 7 3 4F A3WE 2002020500019 20020205 00019 NM 2002 2 5 C1HA200282004 1 20020201 A 5320 SPLICE BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED C C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 STA 480 SPLICE PLATE HAS CORROSION AT FWD END OF INTERCOSTAL BETWEEN STR 28 LT & RT. (C CHECK FINDING) REPAIR APPROVED B Y 8110 2 L 7 3 4F A3WE 2002020500020 20020205 00020 NM 2002 2 5 C1HA200282005 1 20020201 A 5543 TAB BOEING 727 7272S7 138407Z NM RUDDER DELAMINATED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 LOWER RUDDER TAB HAS DELAMINATED ON LT UPPER FWD CORNER. (C CHECK FINDING) REPAIR APPROVED BY 8110. 2 L 7 3 4F A3WE 2002020500021 20020205 00021 NM 2002 2 5 C1HA200282006 1 20020201 A 5300 SEAT TRACK BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 SEAT TRACK AT RBL 44 STA 344 TO STA 460 HAS CORROSION. (C CHECK FINDING) REPLACED SEAT TRACK SECTION PER SRM. 2 L 7 3 4F A3WE 2002020500022 20020205 00022 NM 2002 2 5 C1HA200282007 1 20020201 A 5347 SEAT TRACK BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 SEAT TRACK CHANNEL AT RBL 54 STA. 344 CORRODED (C CHECK FINDING) REPLACED SEAT TRACK SECTION PER SRM. 2 L 7 3 4F A3WE 2002020500023 20020205 00023 NM 2002 2 5 C1HA200282008 1 20020201 A 5730 PANEL BOEING 727 7272S7 138407Z NM RT WING CHAFED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 RT WING UPPER I/B PANEL FOR APU EXHAUST LOUVER IS CHAFING INTO AFT I/B CORNER OF RECESSED PAN. (CORROSION RELATED C CHEC K FINDING) PANEL REPLACED PER AMM. 2 L 7 3 4F A3WE 2002020500025 20020205 00025 NM 2002 2 5 C1HA200282009 1 20020201 A 5245 ACCESS DOOR BOEING 727 7272S7 138407Z NM AC BAY CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 CONDITIONED AIR GROUND CONNECT ACCESS DOOR HAS A BULGE IN SKIN AT HINGE POINT. (CORROSION RELATED C CHECK FINDING). DOOR REPLACED PER SRM. 2 L 7 3 4F A3WE 2002020500026 20020205 00026 NM 2002 2 5 C1HA200295002 1 20020130 A 2560 FLASHLIGHT BOEING 727 727290 138408W NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 295AS 22147 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY IN FLASHLIGHT. OPS CHECK OKAY. 2 L 7 3 4F A3WE 2002020500027 20020205 00027 SO 2002 2 5 C2XA02CL029 1 20020201 A 2530 1095 COFFEEMAKER EMB 145 EMB145LR 3260212 SO GALLEY FAILED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 17984 145246 THE CREW REPORTED A BURNING ELECTRICAL SMELL FROM THE COFFEE WARMER. MAINTENANCE REPLACED THE COFFEE WARMER.OPERATIONA L CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002020500028 20020205 00028 SO 2002 2 5 C2XA02CL030 1 20020202 A 2120 ODOR EMB 135 EMB135ER 3260203 SO CABIN DETECTED A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 19503 145176 THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN WHEN THE APU WAS STARTED ON THE GROUND. MAINTENANCE INSPECTED AND P ERFORMED OPERATIONAL CHECKS AND NO DEFECTS WERE NOTED.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002020500029 20020205 00029 SO 2002 2 5 C2XA02IA018 1 20020203 A 3260 MS3476L833S CONNECTOR EMB 120 EMB120ER 3260203 SO LT MLG CORRODED A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 17728 120182 CREW REPORTED THAT THE LEFT MAIN LANDING GEAR SYSTEM A GREEN LIGHT INTERMITTENTLY ILLUMINATES IN FLIGHT WITH THE GEAR RE TRACTED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND LIGHT CORROSION ON THE A SYSTEM PROXIMITY SWITCH CANNON PLUG. THE CORROSION WAS REMOVED, AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 2002020500031 20020205 00031 SO 2002 2 5 CHQ000102 1 20020131 A 3230 RELAY EMB 145 EMB145 3260210 SO MLG BURNED A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 11 269 145293 ELECTRICAL BURNING SMELL IN COCKPIT AND CABIN DURING FLIGHT, NO SMOKE PRESENT ALL SYSTEMS SEEMS NORMAL NO POPPED CIRCUIT BREAKERS UNABLE TO LOCATE SOURCE. UPON INSPECTION FOUND 3 RELAY SOCKETS WITH SIGNS OF OVERHEATING, R&R ALL 3 RELAYS A ND SOCKETS. 2 L 7 2 4F RT T00011AT 2002020500032 20020205 00032 EU 2002 2 5 CHQ000103 1 20020131 A 2612 WARNING LIGHT SAAB SF340 340B 7860101 EU LT ENGINE MALFUNCTIONED A CHQA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 19 019 LT ENGINE FIRE WARNING LIGHT STAYS ON AFTER ENGINE IS SHUT DOWN.WILL FILE AMENDMENT 2 L 7 2 4T RT A52EU 2002020500041 20020205 00041 NM 2002 2 5 DHL2002705001 1 20020202 A 2910 LINE BOEING 727 72722C 138400F NM NR 2 ENGINE LEAKING A DHLA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 705DH 19191 A SYS FAILURE 0,PRESSURE 0, QUANITY. REPLACED ENGINE DRIVEN PUMP PRESSURE FLEX LINE ON NR 2 ENGINE. LEAK AND OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002020500060 20020205 00060 NE 2002 2 5 S02271044 2 20020123 A 7310 FUEL LINE BOEING 747 747200F 1384866 NM PWA JT9 JT9D7R4G2 52054 NE NR 2 ENGINE CONTAMINATED W SAJF O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 03 24308 NR 2 ENG UNSCHEDULED THRUST LOSS IN FL 350 AFT IGN SW ON APPROX 1 MIN. ENG OPER RESUME NML. SINCE IN-FLT RESTART SUCCE SSFULLY, SUSPECT ENG FUEL SUPPLY SYS INTERRUPTED DUE TO WATER CONTAMINATION IN FUEL SYS. 2.IAW AMM FUEL PUMP FILTER INSP FOUND DIRTY AND RPLD, EVBC FUEL FILTER INSP NML AND RPLD. 3.IAW AMM CK EVBC PT3 & PS3 WATER TRAP, PS4 TUBE ON FCU, ALL COND NO DISCREPANCY FOUND, AND PFMED FUEL TANKS WATER DRAINING AND ENG RUN UP TEST NML. 2 L 7 4 4F 4 F RT A20WE E3NE 2002020500065 20020205 00065 SO 2002 2 5 2002F00089 1 20020113 A 2701 TRIM SWITCH EMB 145 EMB145LR 3260212 SO YOKE INOPERATIVE A MASA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SW 07 828MJ 145218 FLT 9513 - ON A MAINTENANCE FERRY FLIGHT MGM TO CLT, THE BACK UP TRIM SYSTEM WAS INOPERATIVE IN THE UP POSITION. RETURN ED TO THE FIELD FOR THE CAPTAIN AND F/O YOKE TRIM SWITCHES WERE INTERMITTENT. MAINTENANCE REMOVED AND REPLACED BOTH SWI TCHES. OP CHECKS GOOD. (M) 2 L 7 2 4T RT T00011AT 2002020500068 20020205 00068 NM 2002 2 5 SWAA020229 1 20020131 A 5312 6516300 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 10 TO LBL 12. REMOVED AND REPLACED WEB PER SWA ACO. 2 L 7 2 4F RT A16WE 2002020500069 20020205 00069 NM 2002 2 5 SWAA020230 1 20020130 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 890, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002020500070 20020205 00070 NM 2002 2 5 SWAA020231 1 20020131 A 2731 65C26384 TAB BOEING 737 7373Y0 1384671 NM LT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/4D CHECK, FOUND LT ELEVATOR TAB CRACKED AT NR 1 AND NR 3 HINGES. REMOVED AND REPLACED ELEVATOR TAB P ER MM. 2 L 7 2 4F RT A16WE 2002020500071 20020205 00071 NM 2002 2 5 SWAA020234 1 20020130 A 5313 65C27314 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND RELACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002020500072 20020205 00072 NM 2002 2 5 SWAA020236 1 20020131 A 5320 6545768 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, ABOVE STR 10R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002020500073 20020205 00073 NM 2002 2 5 SWAA020237 1 20020130 A 5313 65C27314 TIE CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED TIE CLIP PER SRM AND SWA TI. 2 L 7 2 4F RT A16WE 2002020500074 20020205 00074 NM 2002 2 5 SWAA020238 1 20020131 A 5320 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L AND 14L. REMOVED AND REPLACED SHEAR TIE PE R SRM. 2 L 7 2 4F RT A16WE 2002020500075 20020205 00075 NM 2002 2 5 SWAA020239 1 20020131 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) AT STR 8R, BS'S 380, 440, 827 AND 867. REPAIRED FRAMES P ER BFG ER. 2 L 7 2 4F RT A16WE 2002020500076 20020205 00076 NM 2002 2 5 SWAA020240 1 20020131 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) AT STR 8L, BS'S 440, 827, 867 AND 907. REPAIRED FRAMES P ER BFG ER. 2 L 7 2 4F RT A16WE 2002020500086 20020205 00086 NM 2002 2 5 A6WA200230001 1 20020101 A 3320 325310 BALLAST DORNER DO32 DO328100 2996000 NM CABIN DEFECTIVE A A6WA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 334PH 3012 ELECTRICAL BURNING SMELL AT SEAT 3D AND F. TURNED OFF CABIN SIDEWALL LIGHTS, SMELL DISSIPATED. MAINTENANCE REMOVED AND REPLACED BALLAST, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A45NM 2002020500090 20020205 00090 NM 2002 2 5 A6WA200230002 1 20020106 A 5330 SKIN DORNER DO32 DO328100 2996000 NM FUSELAGE CRACKED A A6WA K NONE O OTHER NR NOT REPORTED 1 GL 31 339PH 3015 LOWER FUSELAGE SKIN FOUND CRACKED AND CORRODED AT FRAME 14A BETWEEN STRINGERS 25 AND 26. THE DAMAGED AREA MEASURES /75 INCH BY .75 INCH. MAINTENANCE REMOVED DAMAGED AND INSTALLED EXTERNAL DOUBLER REPAIR IAW FAIRCHILD DORNIER REPAIR DESIGN APPROVAL SHEET RAS-328-53-1736 AND SERVICE PROBLEM REPORT MODOO33371. (M) 2 H 7 2 4T RT A45NM 2002020500091 20020205 00091 EA 2002 2 5 A6WA200240001 1 20020102 A 3260 PSEU CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 409AW 7447 ANTI-SKID IB AMBER CAS MESSAGE AND PARK BRAKE SOV AMBER CAS UPON GEAR RETRACTION. GEAR DID NOT RETRACT. MAINTENANCE RE MOVED AND REPLACED THE PSEU, OPERATED GEAR SEVERAL TIMES. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002020500092 20020205 00092 EA 2002 2 5 A6WA200240002 1 20020112 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 31 410AW 7490 APU AUTO SHUTDOWN IN FLIGHT, CREW RESTARTED INFLIGHT, STRONG FUEL SMELL IN CABIN AFTER APU BLEED AIR SELECTED ON TO FEED PACKS, FUEL ON TAIL OF AIRCRAFT ON GROUND. MAINTENANCE INSPECTED APU WITH APU RUNNING, NO FUEL LEAKS, CHECKED APU OIL LEVEL OK. OPERATED PACKS NO SMELL NOTED. (M) 2 L 7 2 4F RT A21EA 2002020500093 20020205 00093 EA 2002 2 5 A6WA200240003 1 20020112 A 3040 16591 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 404AW 7294 CAPTAINS SIDE WINDOW HEAT FAIL, RETURN TO DENVER. MAINTENANCE REMOVED AND REPLACED LEFT SIDE WINDSHIELD HEAT CONTROLLER . OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2002020500094 20020205 00094 EU 2002 2 5 A6WA200260001 1 20020114 A 2932 5066521 TRANSMITTER BAC 146 146200A 1500266 EU HYDRAULIC SYS LEAKING A A6WA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 31 156TR E2156 GREEN HYDRAULIC QUANTITY LOW INDICATION ILLUMINATED ON TAKEOFF. MAINTENANCE FOUND TRANSMITTER FOR PRESSURE INDICATION L EAKING. REMOVED AND REPLACED PRESSURE TRANSMITTER. (M) 2 H 7 4 4F A49EU 2002020500097 20020205 00097 SO 2002 2 5 C2XA02IA019 1 20020204 A 3350 1317 LAMP EMB 120 EMB120ER 3260203 SO FUSELAGE BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16731 120190 IAH - During scheduled maintenance the left forward exterior emergency light was found to be inoperative. Maintenance re moved and replaced the affected lamp, performed an operational check, and the aircraft was approved for return to servic e. 2 L 7 2 4T RT A31SO 2002020500098 20020205 00098 EU 2002 2 5 MALA020142 1 20020130 A 2460 A2043C PDU SAAB SF340 SF340A 7850100 EU DEFECTIVE A MALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 15 109XJ 340A109 A/C was originally on a Reposition Flight #422 from ABE-DTW. Enroute to DTW LH Main Buss dropped off line. Crew lost a ll Flight instruments on LH (Capt) side. Due to weather, Flight was diverted to FNT. Maintenance removed and replaced RH PDU PN A2043C, SN/on CM-10894, SN/offCL-773322. All checks good IAW SF340 MM Chap 24. Ground ran AC for 1 hour, no de fects noted. 2 L 7 2 4T RT A52EU 2002020500099 20020205 00099 NM 2002 2 5 SWAA020241 1 20020125 A 5311 6516301 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207 ON BOTH RT AND LT SIDES. REPAIRED FRAME PER SR M. 2 L 7 2 4F RT A16WE 2002020500100 20020205 00100 2002 2 5 SWAA020243 4 20020131 A 2565 6557463 BRACKET BOEING 737 7372T4 1384492 NM CABIN FLOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR BRACKET CORRODED. REMOVED AND R EPLACED GIRT BAR BRACKET PER MM. 2 L 7 2 4F A16WE 2002020500101 20020205 00101 NM 2002 2 5 SWAA020244 1 20020201 A 5312 6517582 WEB BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, WL 183.5 AND RBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F A16WE 2002020500102 20020205 00102 NM 2002 2 5 SWAA020246 1 20020130 A 5320 6551698 STIFFENER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D CHECK, FOUND STIFFENER CRACKED AT BS 291.5, WL 259 RT. REMOVED AND REPLACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2002020500103 20020205 00103 2002 2 5 SWAA020248 4 20020201 A 2565 65C168209 CLIP BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 709SW 27843 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINER CLIP LOOSE. SECURED CLIP PER MM. 2 L 7 2 4F RT A16WE 2002020500104 20020205 00104 NM 2002 2 5 SWAA020249 1 20020131 A 2910 6544561 ACTUATOR BOEING 737 7372H4 138448C NM RT WING LEAKING A SWAA D RETURN TO BLOCK J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 07 071SW 22358 DECLARED EMERGENCY, AIR TURNBACK, DURING CLIMB, LOST A HYD SYSTEM, ACCOMPLISHED APPROPIATE CK LIST AND RETURNED TO MSY. REMOVED AND REPLACED NR 6 SPOILER ACTUATOR PLUG PER MM. INSPECTION REMOVED AND REPLACED EDP CASE DRAIN FILTER AND MODU LAR PACKAGE FILTER'S ALSO REMOVED AND REPLACED 'A' SYSTEM RETURN FILTER PER MM. 2 L 7 2 4F A16WE 2002020500105 20020205 00105 NM 2002 2 5 SWAA020250 1 20020202 A 3230 65446916 MODULE BOEING 737 7373H4 1384600 NM NLG W/W ERRATIC A SWAA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 309SW 22948 LOWERED GEAR HANDLE AND NOSE GEAR DID NOT DROP. CYCLED HANDLE AND NOSE GEAR DROPPED. REMOVED AND REPLACED NOSE GEAR MO DULE PER MM. 2 L 7 2 4F RT A16WE 2002020500106 20020205 00106 NM 2002 2 5 SWAA020251 1 20020202 A 5320 6546529 SHEAR TIE BOEING 737 7372T4 1384492 NM FWD CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED 1/4D CHECK, FOUND BELTFRAME SHEAR TIE CORRODED AT BS 500, RBL 10.5. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2002020500107 20020205 00107 NM 2002 2 5 KPVA20021 1 20020103 A 2421 23088002B STARTER GEN DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE NR1 ENGINE INOPERATIVE A KPVA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 WP 13 806WP 405 357 ON CLIMBOUT WE NOTICED THE AIR DATA COMPUTER FAILED ALONG WITH NR1 DC GEN CAUTION LIGHT ILLUMINATED. WE EXCUTED PROCEDU RES IN ABNORMAL CHECKLIST, LIGHT EXTINGUISHED. 3 MINUTES LATER, LIGHT CAME BACK ON. WE TURNED OFF THE NR1 DC GEN SWITC H PER ABNORMAL CHECKLIST. WE REQUESTED RETURN TO AIRPORT WITH EMERGENCY EQUIPMENT STAND-BY. WE LANDED SAFELY AND RETUR NED TO TERMINAL WITHOUT INCIDENT. FOUND NEGATIVE TERMINAL ON DC GENERATOR, BROKEN. REMOVED AND REPLACED DC GENERATOR I AW MM. AFTER REPLACEMENT OF NR1 STARTER/GENERATOR, OPS TEST OF NR1 ADC GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2002020500108 20020205 00108 NM 2002 2 5 2002UALA00154 1 20020128 A 5311 FLANGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 AFT PIT FRAME INBOARD FLANGE TWO DENTS AT STATION 1400 AT STRINGER 25L AND 26L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR AC COMPLISHED. DAMAGE REMOVED. EXTERNAL DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020500109 20020205 00109 NM 2002 2 5 2002UALA00155 1 20020128 A 5311 FLANGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 AFT PIT FRAME INBOARD FLANGE DENT STATION 1420 AT STRINGER 26L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DAMA GE REMOVED. EXTERNAL DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020500110 20020205 00110 NM 2002 2 5 2002UALA00170 1 20020130 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 FORWARD PIT FRAME STATION 720 UPPER FLANGE UPPER SURFACE GOUGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED INTERNAL STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020500111 20020205 00111 NM 2002 2 5 2002UALA00174 1 20020131 A 5313 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 FOUND DAMAGED WEB IN AREA OF FUSELAGE DENT. BELOW DOOR 1 LEFT STATION 220 AT FLOOR LINE. MAJOR REPAIR ACCOMPLISHED. INS TALLED OF NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020500112 20020205 00112 NM 2002 2 5 2002UALA00185 1 20020201 A 5300 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 CABIN FLOOR INTERCOSTAL AT STATION 395 TO 418 RBL 56" STRINGER 17R HAD DEEP GOUGES. SUPPLEMENTAL DATA UPDATE MAJOR REPAI R ACCOMPLISHED. INSTALLED NEW INTERCOSTAL AND UPPER SURFACE JOGGLE FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020500113 20020205 00113 NM 2002 2 5 DHL2002715001 1 20020129 A 2612 POWER UNIT BOEING 727 727155C 138404Z NM FIRE DETECTION INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 715DH 19618 APU FIRE TEST WILL NOT TEST. REPLACED APU FIRE DETECTION POWER UNIT IAW B727 M/M 26-15-00, OP CHECK GOOD. 2 L 7 3 4F A3WE 2002020500114 20020205 00114 WP 2002 2 5 ABXA010697 1 20020121 A 5300 59203191 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 LONGERON 29 LEFT WAS CRACKED BETWEEN STATION 313 TO STATION 332. REPLACED LONGERON 29 LEFT BETWEEN STATION 313 TO STATIO N 332 IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002020500115 20020205 00115 WP 2002 2 5 ABXA010698 1 20020122 A 5300 591142351 SPLICE DOUG DC9 DC931 3022065 WP NOSE W/W CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 LONGERON SPLICE CRACKED F.S. 945 TO F.S. 965, LONGERON 22 LEFT. REPLACED SPLICE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002020500116 20020205 00116 WP 2002 2 5 ABXA010699 1 20020125 A 5300 59197079 LONGERON DOUG DC9 DC931 3022065 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 LONGERON 30 AT F.S. 870 WAS CORRODED AND CRACKED UNDERNEATH FLANGES. REPLACED LONGERON 30 STATION 862 - 879 IAW DC-9 SRM 53-02. INSTALLED FORWARD AND AFT SPLICES AT STATION 862 - 879 IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002020500117 20020205 00117 WP 2002 2 5 ABXA010700 1 20020125 A 5300 591970731 SKIN DOUG DC9 DC931 3022065 WP AFT CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 CORROSION ON SKIN UNDER LONGERON 30 AT FUSELAGE 870. REMOVED CORROSION IAW DC-9 SRM 53-01. CUT-OUT PORTION OF SKIN PLATI NG THAT WAS CORRODED BEYOND LIMITS AND REPAIRED IAW DC-9 SRM 53-04. 2 L 7 2 4F A6WE 2002020500136 20020205 00136 EU 2002 2 5 CA020109008 1 20020106 A 3242 BRAKE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE MLG OVERHEATED W C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 CA (CAN) SHORTLY AFTER POWER WAS APPLIED AT TAKEOFF, BOTH BRAKE TEMPERATURE INDICATIONS ON LEFT SIDE EXCEEDED 300 DEG.C, FLIGHT CREW REJECTED TAKEOFF. MAX BRAKE TEMP INDICATION ON LEFT SIDE WAS 610 DEG.C. BRAKES STARTED TO SMOKE. REJECTED TAKEOFF INSPECTION CARRIED OUT IAW AMM. INSPECTION REVEALED THAT GLYCOL CAUSED SMOKING. NO TECHNICAL FAULT FOUND. 2 L 7 2 4F 4 F RT A28NM E311NE 2002030500001 20020305 00001 NE 2002 3 5 CA020110010 2 20020109 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE NR 1 FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) NR 1 ENGINE LOST OIL PRESSURE AT 31,000 FT. PERFORMED IN-FLT SHUT-DOWN. DECLARED EMERGENCY AND LANDED. INSPE CTED ENGINE FOR LEAKS, SERVICING AND GROUND RUNS, NOTHING UNUSUAL FOUND. FERRIED TO CVG FOR FUTHER INVEST. NO ABNORMA LITIES NOTED DURING FERRY FLT. 2 L 7 2 4F 4 F RT A21EA E15NE 2002020500138 20020205 00138 NE 2002 2 5 CA020110012 2 20020109 A 7200 CARBON SEAL GE CF343B1 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE LEAKING W E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 872248 (CAN) AS CREW WAS CLIMBING THROUGH 27,000 FT, RECEIVED RT ENGINE OIL PRESSURE MESSAGE. CREW SHUT DOWN RT ENGINE AND CON TINUED ON TO ATL. ONCE IN ATL, MAINTENANCE FOUND THE ENGINE 6 QUARTS LOW OF OIL. EVENTUALLY, OIL LEAKAGE WAS FOUND IN T HE C-SUMP AREA. THE 6 O'CLOCK C-SUMP SCAVENGE TUBE WAS REMOVED AND THE O-RINGS WERE FOUND TO BE HARDENED AND FLAT. THE O-RINGS WERE REPLACED AND RUNS CARRIED OUT. OPS AND LEAK CHECKS WERE GOOD.IT SHOULD BE NOTED THAT DURING THE C-CHECK, TH E NR 7 CARBON SEAL WAS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002020500139 20020205 00139 EU 2002 2 5 CA020110013 1 20020108 A 3260 848401 SENSOR AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211TRENT77 NE NLG MALFUNCTIONED W O OTHER J WARNING INDICATION LD LANDING 1 CA (CAN) AFTER LANDING , THERE WAS AN ECAM MESSAGE; LANDING GEAR SYSTEM DISAGREE AND LANDING GEAR DOORS NOT CLOSED AND AFT ER 10 SECONDS; THERE WAS NOSE WHEEL STEERING FAULT. DOWNLOCK PROXIMITY SENSORS (POSITIONS 20GA1 & 20GA2 ) REPLACED AN D CHECKED SERVICEABLE PER M.M. 32-31-73. 2 L 7 2 4F 4 F RT A46NM E39NE 2002020500140 20020205 00140 EA 2002 2 5 CA020110014 1 20020101 A 5750 AILERON STBROS 601R130002 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AILERON FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 13967 SBRJ100 (CAN) DURING AILERON DEFLECTION TEST ON GROUND, THE PILOT FOUND THAT THERE WAS ONLY 15 DEG DEFLECTION. MAINTENANCE FOUN D THAT THE SEAL RETAINER ON THE WING TRAILING EDGE HAD CAUGHT WITH THE AILERONS LEADING EDGE AND INHIBITED AILERON FUNCT ION. THIS CAUSED STRUCTURAL DAMAGE TO THE WINGS TRAILING AND TO THE AILERONS LEADING EDGE. SEVERAL STRUCTURAL PARTS WER E REPLACED. AIRCRAFT RETURNED TO REVENUE SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002020500141 20020205 00141 EA 2002 2 5 CA020117004 1 20020115 A 7100 CF343B1 ENGINE GE CF343B1 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NACELLE FAILED W A UNSCHED LANDING E Y VIBRATION/BUFFET ENGINE STOPPAGE CL CLIMB 1 CA 629BR 872356 (CAN) AIRCRAFT DEPARTED WASHINGTON DULLES INTERNATIONAL AIRPORT ON FLIGHT 7187, THE FLIGHT CREW DETECTED A SEVERE VI BRATION AND RESULTANT ENGINE SHUTDOWN WITHOUT PILOT'S INPUT. THE AIRCRAFT RETURNED TO THE ORIGINATING AIRPORT AND DECLA RED AN EMERGENCY. ENGINE CHANGED WAS INITIATED AND THE AIRCRAFT RETURNED TO SERVICE - GEARBOX SUSPECTED. AWAITING TEARD OWN REPORT. ENGINE INSTALLED (TSN 0.0; CSN 0) 2 L 7 2 4F 4 F RT A21EA E15NE 2002020500142 20020205 00142 WP 2002 2 5 CA020117015 1 20020117 A 5230 116E100 GEARBOX LKHEED 10113853 LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE CARGO DOOR SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 193H1246 (CAN) C1A CARGO DOOR, AFT LIFT GEARBOX SHEARED FROM ATTACHMENT DURING OPENING. 2 L 7 3 4F 4 F A23WE E12EU 2002020500143 20020205 00143 NM 2002 2 5 CA020121002 1 20020106 A 2720 658D1003 ACTUATOR VICKERS BOEING 767 7673Y0 NM PWA 4060 PW4060 52119 NE RUDDER FAULTY W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) RUDDER TRIM 4.5 NOSE LT, THE AIRCRAFT STABILIZED IN CRUISE FOR 30 MINUTES.FOUND TO BE THE RUDDER TRIM ACTUATOR AT FAULT.REPLACED THE TRIM RUDDER ACTUATOR, OPERATIONAL CHECK CARRIED OUT AS PER MAINTENANCE MANUAL, FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002020500144 20020205 00144 NE 2002 2 5 CA020121005 2 20020101 A 7200 CFM565C4 ENGINE CFMINT CFM565C4 AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE NR 1 FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 741850 (CAN) ENGINE SHUT DOWN. WHILE IN CRUISE NR 1 ENGINE SURGED FOLLOWED BY GRADUAL INCREASE IN EGT AND FUEL FLOW. SHORTLY A FTER, ENGINE FILTER CLOG MESSAGE DISPLAYED AND THEN ENGINE LOW OIL PRESSURE.FOUND EVIDENCE OF NR 4 BEARING FAILURE. REP LACED ENGINE.RESULT OF FAILURE WILL BE FORWARDED IN THE FINAL REPORT. 2 L 7 4 4F 4 F RT A197 E37NE 2002020500145 20020205 00145 EA 2002 2 5 CA020121007 1 20020101 A 5270 52100033 HARNESS CNDAIR CL6002B19 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE PAX DOOR FAULTY W O OTHER N FALSE WARNING NR NOT REPORTED 1 CA 7097 (CAN) EICAS CAUTION MESSAGE FOR PASSENGER DOOR UNSAFE IN FLIGHT. AFTER TROUBLESHOOTING, NO FAULT FOUND, FLEET MANAGEM ENT REQUESTED TO REPLACE THE DOOR WIRE HARNESS. WIRE HARNESS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002020500191 20020205 00191 EU 2002 2 5 AUS20020001 1 20020101 A 2611 21562A SMOKE DETECTOR STBROS SD3 SD360 8100606 EU PWA PT6 PT6A67R 52043 NE HARTZL HCA6A HCA6A3 NE CARGO BAY FAULTY W O OTHER B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING CR CRUISE 1 AU S 2624 3675 (AUS) AFT BAGGAGE COMPARTMENT SMOKE DETECTOR ILLUMINATED. FIRE EXTINGUISHER DISCHARGED INTO COMPARTMENT. NO EVIDENCE OF FIRE. FURTHER INVESTIGATION FOUND THAT THE REAR BAGGAGE COMPARTMENT NR 2 SMOKE DETECTOR WAS OUT OF CALIBRATION RESULTI NG IN OVERSENSITIVE OPERATION. 2 H 7 2 4T 4 T A41EU E26NE 6 C P14NE 2002020500193 20020205 00193 EU 2002 2 5 AUS20020004 1 20020102 A 5511 332A1315001151 RIB AEROSP 332A131500 SNIAS AS332 AS332L 8680809 EU TMECA MAKILA MAKILA1A 60040 EU HORIZONTAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) HORIZONTAL STABILISER ROOT RIB ASSEMBLY CRACKED BEYOND LIMITS. 2 G 7 2 4U 4 U H4EU E12NE 2002020500194 20020205 00194 NE 2002 2 5 AUS20020005 2 20020104 A 7321 77333326 FUEL CONTROL PWA JT9D7R4E BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE LT ENGINE FAULTY W O OTHER E VIBRATION/BUFFET LD LANDING 1 AU S A2613 (AUS) LT ENGINE FUEL CONTROL UNIT SUSPECT FAULTY. 2 L 7 2 4F 4 F RT A1NM E3NE 2002020500195 20020205 00195 NM 2002 2 5 AUS20020007 1 20020107 A 2120 DUCT GE CFM563C BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C 13802 EU AIR CONDITIONING LEAKING W O OTHER J WARNING INDICATION CL CLIMB 1 AU S (AUS) LT AIR CONDITIONING SYSTEM LEAKING FROM DUCT JOINT. 2 L 7 2 4F 4 F RT A16WE E21EU 2002020500197 20020205 00197 NM 2002 2 5 AUS20020010 1 20020108 A 3230 BACH8AO6EE0250T LINE BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU MLG WORN W O OTHER K FLUID LOSS CL CLIMB 1 AU S (AUS) LT MAIN LANDING GEAR RETRACTION ACTUATOR UP LINE WORN AND LEAKING. 2 L 7 2 4F 4 F RT A16WE E21EU 2002020500203 20020205 00203 NM 2002 2 5 AUS20020034 1 20020118 A 2422 1A30001AHR INVERTER DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE AC POWER FAILED W O OTHER B G SMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE LD LANDING 1 AU S (AUS) INVERTER FAILED CAUSING FAILURE OF MISSION RADAR GIMBLE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002020500204 20020205 00204 EU 2002 2 5 AUS20020035 1 20020116 A 3211 FITTING BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE MLG ACTUATOR FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LANDING GEAR ASSIST ACTUATOR MOUNT BRACKET FAILED. DAMAGE CAUSED TO FUSELAGE. INVESTIGATION FOUND THAT THE EMERGEN CYSELECTOR LEVER WAS NOT FULLY MOVED TO THE FULL UP DETENTCAUSING THE LEVER TO MOVE TOWARDS THE DOWN POSITION WHILE THE GEAR WAS EXTENDING CAUSING BOTH HYDRAULIC SYSTEMS TO OPPOSE EACHOTHER. THE ASSISTER ACTUATOR MOUNTING BRACKET SHEARED RE SULTING IN THE ACTUATOR BEING FORCED INTO THE FRAME 29 FUSELAGE WEB AND RUPTURING THE SKIN. PERSONNEL/MAINTENANCE ERROR. INCORRECTOPERATION. 2 H 7 4 4F 4 F RT A49EU E6NE 2002020500206 20020205 00206 WP 2002 2 5 DHL2002801003 1 20020130 A 2612 CONNECTOR DOUG DC8 DC873F 302199F WP FIRE LOOP DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 NR 2 ENGINE FIRE LOOP-B WILL NOT TEST. INSPECTED AND CLEANED B-LOOP CONNECTORS IAW DC-8 MM 26-10-1, OP'S CHECK GOOD. C OULD NOT DUPLICATE ON GROUND. 2 L 7 4 4F RT 4A25 2002020500207 20020205 00207 WP 2002 2 5 ZW0A0200504 1 20020108 A 5240 BRACKET DOUG DC9 DC983 3022083 WP SERVICE DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT THE FWD SERVICE DOOR HAD A BRACKET BELOW LOWER HINGE ARM THAT WAS CRACKED. REPLACED FRAME PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2002020500208 20020205 00208 WP 2002 2 5 ZW0A0200509 1 20020110 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT IN AFT CABIN, LT FLOOR, FOUND CORROSION IN SHEET METAL MEMBRANE AT REAR CABIN FORMER RING, 1287 LT, LBL 42 INCHES. REMOVED CORROSION PER SPM 6-80-01. INSTALLED DOUBLER PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2002020500209 20020205 00209 NM 2002 2 5 KPVA20022 1 20020105 A 2435 23088002B STARTER GEN DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE NR1 ENGINE INOPERATIVE A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 807WP 375 23 (MX) LEFT STARTER GENERATOR B+ POLE LOOSE. REMOVE AND REPLACED LEFT STARTER GEN. IAW MM. OPERATION CHECK IAW MM. 2 H 7 2 4T 4 T RT A13NM E20NE 2002020500210 20020205 00210 NM 2002 2 5 KPVA20023 1 20020105 A 2435 23088002B STARTER GEN DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE NR1 ENGINE INOPERATIVE A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 807WP 482 023 (MX) RIGHT STARTER GENERATOR B+ POLE WORN AND LOOSE. LOCKNUT WOULD NOT LOCK DOWN. REMOVED AND REPLACED RIGHT STARTER GE NERATOR IAW MM. OPERATIONAL CHECK IAW MM. NO DEFECTS NOTED. 2 H 7 2 4T 4 T RT A13NM E20NE 2002020500220 20020205 00220 WP 2002 2 5 ZW0A0200601 1 20020111 A 5730 SKIN DOUG DC9 DC983 3022083 WP RT WING CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT ON THE RT WING LOWER SURFACE, CORROSION WAS FOUND AROUND THE FASTENER AT WING STATION 511, TR LOWER MID SPAR SKIN. ACCOMPLISHED UT INSPECTION PER NDT 51-00-03 AND FOUND 47 PERCENT MATERIAL LOSS. INSTALLED FILLER AND D OUBLER PER SRM 57-03, FIG 24A, SHEETS 1 THROUGH 6. 2 L 7 2 4F RT A6WE 2002020500221 20020205 00221 WP 2002 2 5 ZW0A0200602 1 20020111 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT CABIN FLOOR SUPPORT AT STA 864 HAD A CRACK AT LBL 10. REMOVED CRACKED SUPPORT AND REPLACED PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2002020500222 20020205 00222 WP 2002 2 5 ZW0A0200603 1 20020111 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND CORROSION ON FWD BOTTOM OF DOOR JAMB, LBL 57 AT STA 160. REPAIRED WEBBING PER SRM 53-01, FIG 2, AND REPAIRED ANGLE PER SRM 53-01, FIG 2. 2 L 7 2 4F RT A6WE 2002020500223 20020205 00223 NM 2002 2 5 ZW0A0200901 1 20020109 A 2121 FAN BOEING 757 757231 1384950 NM CABIN FAILED A ZW0A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 13 722TW 29385 SMOKE WAS REPORTED IN AIRCRAFT. FLIGHT RETURNED TO STL. CHANGED THE LT RECIRCULATION FAN 606772-3. ALSO ACCOMPLISHED PRECAUTIONARY CHECKS OF SYSTEM AND WIRING, RESULTS NEGATIVE. 2 L 7 2 4F RT A2NM 2002020500224 20020205 00224 NM 2002 2 5 ZW0A0200902 1 20020110 A 2121 FAN BOEING 757 757231 1384950 NM CABIN FAILED A ZW0A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 13 722TW 29385 IN CLIMB SMOKE APPEARED IN THE CABIN. FLIGHT RETURNED TO STL. CHANGED THE RT RECIRCULATION FAN, P/N 606772-3, AND BOTH RECIRC FILTERS, P/N P196555. ALSO ACCOMPLISHED CHECKS OF FAN CONNECTORS AND WIRING. PERFORMED TEST FLIGHT TO CONFIRM CORRECTIONS. 2 L 7 2 4F RT A2NM 2002020500225 20020205 00225 NM 2002 2 5 ZW0A0200903 1 20020114 A 2120 SMOKE BOEING 757 757231 1384950 NM CABIN DETECTED A ZW0A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 13 722TW 29385 SMOKE REPORTED IN CABIN RIGHT AFTER TAKEOFF. ACCOMPLISHED PACK BURN OUT, CHECKED L/E WING DUCTING, CHECKED MID CABIN BA LLAST WIRING AND RESULTS NEGATIVE. INDICATIONS CAUSED SUSPICION OF CONDENSATION. 2 L 7 2 4F RT A2NM 2002020500226 20020205 00226 WP 2002 2 5 ZW0A0200904 1 20020121 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 970TW 53620 THE EGRESS LIGHT WAS INOPERATIVE AT ROW 24 AND THE FWD OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE LAMP AT ROW 24, P/N 7732, AND THE BATTERIES, P/N 408822-101, FOR THE OVERWING LIGHTS. 2 L 7 2 4F RT A6WE 2002020500227 20020205 00227 NE 2002 2 5 ZW0A0200906 2 20020115 A 7230 1B715901 CARBON SEAL BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE NR 1 & 2 ENGINE FAILED A ZW0A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 13 722TW 29385 4948 JUST AFTER TAKEOFF SMOKE WAS REPORTED IN CABIN. FLIGHT RETURNED TO STL. FOUND THE NUMBER 2 AND 3 BEARING CARBON SEAL A SSEMBLY ON BOTH ENGINES HAD FAILED. THE AIRCRAFT WAS FERRIED TO ANOTHER STATION FOR REPLACEMENT OF THE CARBON SEAL ASSE MBLIES ON BOTH ENGINES. SERIAL NUMBER ON THE SECOND ENGINE WAS 4949, HOURS AND CYCLES THE SAME AS FIRST ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020500228 20020205 00228 NE 2002 2 5 ZW0A0200907 2 20020115 A 7230 1B715901 CARBON SEAL BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE RT ENGINE FAILED A ZW0A O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 13 720TW 30319 4946 INTO STL CREW REPORTED SMOKE IN THE CABIN. FOUND THE RT ENGINE NUMBER 2 AND 3 BEARING COMPARTMENT CARBON SEAL ASSEMBLY HAD FAILED. REPLACED THE ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020500229 20020205 00229 NE 2002 2 5 ZW0A0200908 2 20020119 A 7230 CARBON SEAL BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE LT ENGINE DETERIORATED A ZW0A O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 13 724TW 28488 4950 AN OIL SMELL WAS NOTICED INTO TPA. FOUND THE LT ENGINE NUMBER 2 AND 3 BEARING COMPARTMENT CARBON SEAL ASSEMBLY HAD DETE RIORATED. AIRCRAFT FERRIED TO ANOTHER STATION FOR REPLACEMENT OF THE SEAL ASSEMBLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020500231 20020205 00231 NM 2002 2 5 C1HA200297003 1 20020204 A 3350 BATTERY PACK BOEING 727 727270 138408P NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 697CA 23052 LEFT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AND BATTERY PACK FOR LT FWD OVERWING EXIT IAW 727 M/M 33-50-22, OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2002020500232 20020205 00232 EU 2002 2 5 DHL2002365001 1 20020201 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU MAIN CARGO BAY INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 365DH 149 SMOKE DETECTOR FOR THE MAIN DECK CARGO LEFT SIDE, ALL THE WAY AFT WILL NOT TEST. REMOVED AND REPLACED SMOKE DETECTOR IA W M/M 26-14-11, OPS CHECKED GOOD. 2 L 7 2 4F RT A35EU 2002020500233 20020205 00233 NM 2002 2 5 DHL2002707002 1 20020130 A 2612 SWITCH BOEING 727 72722 1384002 NM COCKPIT INOPERATIVE A DHLA K NONE L NO TEST NR NOT REPORTED 1 SO 01 707DH 18321 FIRE ALARM BELL DOES NOT WORK FOR ANY ALARM FUNCTION. REMOVED AND REPLACED THE S41 CUTOFF SWITCH WITH SERVICEABLE SWITC H, OPS CHECK GOOD IAW BOEING WM 26-11-01. 2 L 7 3 4F A3WE 2002020500234 20020205 00234 NM 2002 2 5 DHL2002708002 1 20020128 A 3350 LIGHT BOEING 727 72725 1384006 NM CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 708DH 18275 FWD ENTRY EMERGENCY EXIT LIGHT INOP IN TEST POSITION (ON POSITION). REMOVED AND REPLACED FWD ENTRY WAY EMERGENCY EXIT L IGHT ASSY IAW M/M 33-5-00. OPS CHECK SERVICEABLE. 2 L 7 3 4F A3WE 2002020500235 20020205 00235 NM 2002 2 5 DHL2002715002 1 20020202 A 2612 POWER SUPPLY BOEING 727 727155C 138404Z NM FIRE DETECTION INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 715DH 19618 APU FIRE DETECTION SYSTEM WILL NOT TEST. TROUBLESHOT SYSTEM, REMOVED AND REPLACED APU FIRE DETECT OPERATING POWER SUPPL Y. OPERATIONAL CHECK OF SYSTEM GOOD MM REF 26-15-00. 2 L 7 3 4F A3WE 2002020500236 20020205 00236 NM 2002 2 5 DHL2002727002 1 20020128 A 2612 CONNECTOR BOEING 727 727228 1384083 NM FIRE DETECTION DAMAGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 727DH 20204 NR 1 ENG FIRE WARNING WILL NOT TEST. REPINNED NR 1 ENG CANNON PLUG D-400P IAW B-727 WDM 26-11-01 PG 1 FIRE WARN SYS, OP S CHECKS GOOD. 2 L 7 3 4F RT A3WE 2002020500237 20020205 00237 NM 2002 2 5 DHL2002740001 1 20020131 A 3350 BATTERY BOEING 727 7272Q9 138448M NM COCKPIT DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 740DH 21930 RIGHT W/W LIGHT NEEDS CLEANING. EMERGENCY EXIT COCKPIT OVERHEAD LIGHT INOP. CLEANED RIGHT W/W LIGHT IAW MM 12-40-00. REMOVED AND REPLACED EMERGENCY EXIT BATTERY IAW MM 33-50-01, OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2002020500238 20020205 00238 NM 2002 2 5 DHL2002741002 1 20020201 A 3350 BATTERY BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 741DH 21931 EMERGENCY LIGHT FAILED TO ILLUMINATE WHEN TURNED ON. REMOVED AND REPLACED BATTERIES IN BOTH EMERGENCY LIGHTS, OPS CHECK GOOD IAW BMM CH 33-50-01. 2 L 7 2 4F A16WE 2002020500239 20020205 00239 WP 2002 2 5 DHL2002801004 1 20020202 A 2612 SWITCH DOUG DC8 DC873F 302199F WP FIRE DETECTION DEFECTIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 NR 2 ENG FIRE LOOP-B WILL NOT TEST. REPLACED SWITCH 51-7028 PER 20-50-1, OPS CHECK NORMAL PER M/M 26-10-00. 2 L 7 4 4F RT 4A25 2002020500240 20020205 00240 WP 2002 2 5 ZW0A0200502 1 20020110 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 912TW 49183 DURING CHECK-C MAINT FOUND CORROSION AT STA 1271, AFT FACE OF FORMER LONGERON 29L TO 29R. REPAIRED FORMER PER SRM 53-03 , FIG 2A. 2 L 7 2 4F A6WE 2002020500241 20020205 00241 WP 2002 2 5 ZW0A0200503 1 20020109 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT IN THE CABIN THE AFT FLOOR HAD CORROSION IN TRACK AT STA 1136 TO 1308, LBL 22. REMOVED AND REPLACE D TRACK. SPLICED TRACK PER SRM 53-05. 2 L 7 2 4F RT A6WE 2002020500242 20020205 00242 WP 2002 2 5 ZW0A0200505 1 20020108 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT THE FWD CABIN HAD CORROSION ON FLOOR MEMBRANE AT STA 198, RBL 9. REMOVED LIGHT CORROSION. CUT OUT BROKEN AREA. INSTALLED AND FILLED WITH TOP AND BOTTOM DOUBLER PER SRM 51-70-4, 51-10-3, 51-20-0, AND SPM 6-80-01. 2 L 7 2 4F RT A6WE 2002020500243 20020205 00243 WP 2002 2 5 ZW0A0200506 1 20020109 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT IN CABIN FOUND CORROSION AT STA 1125 TO 1127, MEMBRANE ON RT SIDE. REMOVED CORROSION PER SRM 51-10 -03 PAGE 27. REPAIRED AREA PER SRM 51-70-4 PAGE 4 AND 5. 2 L 7 2 4F RT A6WE 2002020500244 20020205 00244 WP 2002 2 5 ZW0A0200507 1 20020109 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT IN THE AFT CABIN FOUND CHAIR TRACK CORROSION AT STA 1205, LBL 44, AND STA 1262 LBL 46. REPAIRED CH AIR TRACK PER SRM 53-05, FIG 4, FROM STA 1183 THROUGH 1308. 2 L 7 2 4F RT A6WE 2002020500245 20020205 00245 WP 2002 2 5 ZW0A0200508 1 20020110 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOORBEAM CAP STA 1155, LBL 22 TO 44. REPLACED SUPPORT ASSEMBLY PER SPM 6 -70-01 AND SRM 51-30-5. 2 L 7 2 4F RT A6WE 2002020500246 20020205 00246 WP 2002 2 5 ZW0A0200510 1 20020110 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND CABIN FLOOR TO FUSELAGE MEMBRANE CORRODED AT APPROXIMATELY 6 INCHES FWD OF STA 636 THROUGH ST A 712, RIGHT SIDE. REMOVED CORROSION PER SPM 6-80-01. REPAIRED PER SRM 51-70-4 PAGE 6, STA 636 TO 680. 2 L 7 2 4F RT A6WE 2002020500247 20020205 00247 WP 2002 2 5 ZW0A0200511 1 20020108 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT ON FUSELAGE EXTERIOR, STA 1293, FOUND DENT BETWEEN LONGERON 16L AND 15L. ACCOMP INSP PER NDT 51-00 -03 AND NO CRACK. UT INSPECTION INDICATED 50 PERCENT MATERIAL LOSS. CUT OUT PLUG TO REMOVE DAMAGED AREA AND INSTALLED AN EXTERIOR AND INTERNAL DOUBLER SHIM AS REQUIRED PER SRM 53-04, FIG 38, PAGE 218. 2 L 7 2 4F RT A6WE 2002020500248 20020205 00248 WP 2002 2 5 ZW0A0200512 1 20020109 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT IN AFT CARGO COMPARTMENT FOUND CORROSION ON FLOOR TRACK BETWEEN STA 1136 THROUGH 1155 AT LONGERON 2 8R. REMOVED SURFACE CORROSION PER SPM 6-80-01. REMOVED AND REPLACED 2 ANGLES PER SRM 6-70-01. 2 L 7 2 4F RT A6WE 2002020500249 20020205 00249 WP 2002 2 5 ZW0A0200513 1 20020110 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT IN TAIL COMPT RT SIDE BETWEEN STA 1474 AND 1486 STRUCTURAL WEB WAS BROKEN OUTBOARD OF STAIR HYD ACT UATOR. INSTALLED NEW STANDARD STRUCTURAL WEB PER SPM 6-70-01 AND DOUGLAS DRAWING 9911946. 2 L 7 2 4F RT A6WE 2002020500250 20020205 00250 NM 2002 2 5 AWXA200200096 1 20020202 A 5330 2024T3050 SKIN AIRBUS A319 A319132 3930340 NM PUNCTURED A AWXA K NONE O OTHER TX TAXI/GRND HDL 1 WP 28 808AW 1088 TUS - GROUND DAMAGE - "C" - WHILE POSITIONING AIR-STAIR TRUCK TO R1 DOOR THE TRUCK STRUCK THE FUSELAGE PUNCTURING THE SK IN BELOW THE R1 DOOR 6" FWD OF FR 20, AND 4" BELOW STR 29. MAINTENANCE PERFORMED TEMPORARY REPAIR ER 25-5331-02033-ES1 A ND AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX. IN PHX MAINTENANCE CUTOUT THE DAMAGED AREA OF SKIN FABRICATED A DOUBLER , FILLER, AND SHIM, AND INSTALLED REPAIR IAW SRM 53-00-11 FIG. 209. 2 L 7 2 4F RT A28NM 2002020500251 20020205 00251 NM 2002 2 5 AWXA200200100 1 20020123 A 5230 6546921 TEE CHORD BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - MAJOR REPAIR - "C" - DURING C-16 CHECK A CRACK WAS FOUND ON THE VERTICAL LEG OF THE FORWARD CARGO DOOR LOWER OUTER TEE CHORD THE THIRD FASTENER HOLE FROM AFT END BS 485. MAINTENANCE CUTOUT DAMAGED SECTION OF CRACKED TEE CHORD AT BS 48 5, TRIMED NEW REPLACEMENT SECTION OF TEE CHORD, FABRICATED 3 EACH RADIUS FILLERS AND 2 EACH REPAIR ANGLES AND INSTALLED REPAIRS IAW AWA EO 52-31-04. 2 L 7 2 4F RT A16WE 2002020500252 20020205 00252 NM 2002 2 5 AWXA200200102 1 20020121 A 5330 50079452 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A CRACK WAS FOUND ON THE UPPER HINGE CUTOUT OF THE L1 DOOR AT UPPER CORNER BS 300. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED. FABRICATED AND INSTA LLED REPAIR DOUBLER IAW B737-200 SRM 52-00-3, FIG.6, PG 10 AND 10A. 2 L 7 2 4F RT A16WE 2002020500253 20020205 00253 NM 2002 2 5 AWXA200200103 1 20020123 A 5315 6545410152 WEB BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A CRACK WAS FOUND ON FLOOR BEAM WEB AT BS 714, RBL 25. MAINTENANCE REMOVED DAMAGED AREA OF WEB AT BS 714, RBL 25, FABRICATED REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW AWA ER 15-57 02-02033-GF1. 2 L 7 2 4F RT A16WE 2002020600010 20020206 00010 NM 2002 2 6 SABA020015 1 20020203 A 3350 1013075 BULB DHAV DHC8 DHC8102 2809003 NM CABIN BURNED OUT A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 882CC 168 Aircraft 882 on flight 2045. During pre-flight a red emergency floor light was found inoperative. Maintenance removed and replaced the bulb. System ops check good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002020600035 20020206 00035 EA 2002 2 6 2002F00102 1 20020102 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A MASA K NONE F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 07 27185 7185 FLT 6451 - PHX-COS - INBOUND TO COS, THE CREW REPORTED A FLAP FAIL CAUTION MESSAGE AND DECLARED AN EMERGENCY. THE MESSA GE APPEARED WITH THE FLAPS AT ZERO AND SELECTED DOWN. THE AIRCRAFT LANDED UNEVENTFULLY AND ON CALL MAINTENANCE PERFORME D PART A/B OF THE AD. NO FURTHER DEFECTS WERE NOTED AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002020600036 20020206 00036 SW 2002 2 6 2002F00096 1 20020103 A 3310 2719115007 PANEL SWRNGN SA227 SA227AC 8780603 SW COCKPIT MALFUNCTIONED A BSAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 05 158MC AC726B BIL - FLT 2551 - DURING CRUISE, THE COPILOT AVIONICS LIGHT PANEL GOT HOT AND STARTED TO SMOKE. LIGHTS WERE TURNED OFF A ND SMOKE STOPPED. CREW LANDED AT DESTINATION WITH NO FURTHER PROBLEMS. OVERLAY LIGHTED PANEL WIRING PROBLEM. FOUND CA RBON TRACING IN THE FIBERGLASS ON THE BACK OF THE PANEL BETWEEN THE NEGATIVE AND POSITIVE POWER STRIPS. THE POWER STRIP S WERE ALSO CORRODED. THE DAMAGE WAS ROUTED OUT, THEN AREA WAS REPAIRED. (M) 2 L 7 2 4T RT A8SW 2002020600038 20020206 00038 WP 2002 2 6 02FDEA00087 1 20020205 A 2910 1489951 SHUTOFF VALVE DOUG DC10 DC1010 3022110 WP HYDRAULIC SYS FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 399FE 48262 AFTER 80 KTS STABILIZER MOTION AURAL WARN ACCOMPANIED RED ANNUNCIATOR ON EAD. 2 L 7 3 4F A22WE 2002020600039 20020206 00039 NE 2002 2 6 02FDEA00088 2 20020205 A 7200 ENGINE DOUG DC10 DC1010F 3022111 WP GE CF6 CF650C2 30018 NE NR 3 MALFUNCTIONED A FDEA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 25 368FE 46606 AT CLIMB NR 3 ENG COUGHED AND ROLLED BACK N1 TO 35 PERCENT AND N2 50 PERCENT. EGT BEGAN TO RISE 800 DEG. SHUTDOWN ENG. 2 L 7 3 4F 4 F A22WE E23EA 2002020600040 20020206 00040 WP 2002 2 6 02FDEA00089 1 20020126 A 3241 60028703 CONTROL UNIT DOUG DC10 DC1030F 3023504 WP ANTI-SKID SYS FAILED A FDEA O OTHER G Z MULTIPLE FAILURE SIGNIFICANT FAILURE REPORT LD LANDING 1 SO 25 311FE 46871 DURING FLIGHT TEST BRAKE LAND ALL MAIN LANDING GEAR TIRES BLEW (10) EACH. REMOVED AND REPLACED ALL MLG WHEEL AND TIRE A SSY. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT PER AMM 32-45-01-2. 2 L 7 3 4F RT A22WE 2002020600067 20020206 00067 NM 2002 2 6 SWAA020254 1 20020203 A 5330 6545765 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 1.0 INCH LONG AT BS 500D, STR 12R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002020600068 20020206 00068 NM 2002 2 6 SWAA020255 1 20020203 A 5314 BAC1503 STIFFENER BOEING 737 7372T4 1384492 NM LT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663, LBL 57. REMOVED AND REPLACED STIFFENER PER SRM . 2 L 7 2 4F A16WE 2002020600069 20020206 00069 SW 2002 2 6 AUS20020006 1 20020107 A 2497 WIRE HARNESS SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL ELECTRICAL SYS BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 AU S (AUS) SMOKE IN COCKPIT. INVESTIGATION FOUND SUBSTANTIAL HEAT DAMAGE TO WIRING LOOMS IN RT PEDESTAL & UP TO RT INSTRUMENT PANEL. FAULTISOLATED TO RT AVIONICS BUSS LINK SHORT CCTING TO COPILOT'S AUDIO WIRING. RESULTANT HEAVY CURRENT CAUSED WI RES 103 TO JJ, 1C3 TO GND, 1C4 TO NN, 1C3 TO JJ, 104 TO MM, MK3 TO JJ & MIC4 TO KK TO MELT TO VARYING DEGS. WIRE 1C3 TO JJ FOUND TO HAVE MOST DAMAGE. AL L INSULATION HAD BEEN BURNT OFF CONDUCTOR. AS THESE WIRES WERE CONTAINED WITHIN A LOOM , 2NDARY WIRE DAMAGE RESULTED. DAMAGED SECTION OF LOOM WAS REMOVED & REPLACED. FURTHER 2ND ARY DAMAGE FOUND TO WIRE NO CPAAA TOPIN3, 1SA26 TO CBP EBF, TS-19 TO CBP-X, SATPHONE GND, XFR-5W-3. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002020600070 20020206 00070 NM 2002 2 6 SWAA020256 1 20020202 A 5320 6546529 SHEAR TIE BOEING 737 7372T4 1384492 NM E/E COMP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT BS 360, RBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2002020600071 20020206 00071 NM 2002 2 6 SWAA020258 1 20020202 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 745, ABOVE STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002020600072 20020206 00072 NM 2002 2 6 SWAA020259 1 20020202 A 5755 654645170AA SPOILER BOEING 737 7373A4 1384585 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED C2 CHECK, FOUND NR 6 SPOILER DELAMINATED ON TOP SIDE. REMOVED AND REPLACED NR 6 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2002020600073 20020206 00073 NM 2002 2 6 SWAA020260 1 20020202 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED 1.7 INCHES LONG AT BS 500D, STR 12L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002020600074 20020206 00074 2002 2 6 SWAA020261 4 20020202 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY LENGTH OUT OF ADJUST. ADJUSTED GIRT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002020600075 20020206 00075 NM 2002 2 6 SWAA020262 1 20020202 A 5230 6547952 DOOR BOEING 737 7373Y0 1384671 NM AFT CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR WEB AND FRAME CRACKED AT NR 2 FWD STOP FITTING. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 2002020600076 20020206 00076 NM 2002 2 6 SWAA020263 1 20020202 A 5312 6516300 WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 188 AND LBL 1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002020600077 20020206 00077 NM 2002 2 6 SWAA020264 1 20020203 A 5314 654624013 WEB BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING SCHEDULED C1 CHECK, FOUND NLG ACTUATOR SUPPORT BEAM WEB CRACKED AT FWD END. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002020600078 20020206 00078 NM 2002 2 6 SWAA020265 1 20020202 A 5312 6517583 WEB BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, WL 184 AND RBL 5.7. REPAIRED WEB PER SWA RA. 2 L 7 2 4F A16WE 2002020600079 20020206 00079 NM 2002 2 6 SWAA020266 1 20020202 A 5330 6545765 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 500, STR 27R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002020600080 20020206 00080 NM 2002 2 6 SWAA020268 1 20020204 A 5312 65458075 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR CUTOUT CRACKED BELOW UPPER HINGE ON FWD CENTER STUB FRAME. REPAIRED FRAME PER SWA RA. 2 L 7 2 4F RT A16WE 2002020600082 20020206 00082 NM 2002 2 6 AUS20020009 1 20020108 A 7830 LJ34179 BLOCKER DOOR RROYCE BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE THRUST REVERSER MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 1 ENGINE NR 10 BLOCKER DOOR AND ACTUATING ROD MISSING. DAMAGE TO ADJACENT AREA. 2 L 7 4 4F 4 F RT A20WE E30NE 2002020600083 20020206 00083 SW 2002 2 6 AUS20020011 1 20020106 A 2931 JL9154003 TRANSDUCER SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UHR WP MCAULY 4HFR34 4HFR34C652 NE HYDRAULIC SYS FAILED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AU S (AUS) HYDRAULIC SYSTEM PRESSURE TRANSDUCER LOCATED IN LT WHEEL WELL FAILED. LOSS OF HYDRAULIC FLUID. SHUTTLE VALVE REPLA CED. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002020600085 20020206 00085 NM 2002 2 6 AUS20020014 1 20020106 A 3260 WARNING SYSTEM DHAV DHC8 DHC8201 2809001 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE MLG FAULTY W D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 AU S (AUS) RT MAIN LANDING GEAR LIGHT AND WARNING HORN OPERATED DURING TAXI. INVESTIGATION OF THE WARNING SYSTEM COULD FIND N O DEFINITE CAUSEFOR THE DEFECT. PROXIMITY SENSOR WAS ON THE HIGH SIDE OF LIMITS AND WAS ADJUSTED TO THE LOWER LIMIT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002020600088 20020206 00088 NM 2002 2 6 AUS20020016 1 20020103 A 2821 AC9227F1740 FILTER BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL RT ENGINE CONTAMINATED W O OTHER J WARNING INDICATION TO TAKEOFF 1 AU S (AUS) RT ENGINE FUEL FILTER CONTAMINATED WITH LINT PARTICLES AND FINE METAL SWARF. FILTERS HAD NOT BEEN CHANGED SINCE TH E AIRCRAFT UNDERWENT STRUT MODS IN MAY 2001. 2 L 7 2 4F 4 F RT A1NM E23EA 2002020600089 20020206 00089 NM 2002 2 6 2002UALA00142 1 20020126 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 926UA 26648 STATION 178 BULKHEAD CRACKS AT BL 0, WL 187 LBL 5, WL 198 RBL 6, WL 201. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INS TALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020600090 20020206 00090 NM 2002 2 6 2002UALA00143 1 20020126 A 5230 STRUCTURE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO DOOR PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 930UA 26655 PUNCTURE .5 INCH, IN LOWER RIGHT CORNER OF FORWARD CARGO DOOR. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE, INSTALLED DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030100013 20020301 00013 NM 2002 3 1 2002UALA00144 1 20020125 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 118UA 28811 EEL AT SEAT 34 HJK INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2002020600091 20020206 00091 NM 2002 2 6 2002UALA00145 1 20020127 A 3234 CONTROL HANDLE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 105UA 26473 RETURNED TO THE FIELD DUE TO LANDING GEAR HANDLE WOULD NOT RAISE PAST LEVER LOCK AFTER TAKEOFF. NO EICAS MESSAGES APPEA RED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002030100014 20020301 00014 NM 2002 3 1 2002UALA00146 1 20020123 A 2910 AE1010745MO645 HYDRAULIC LINE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE HYDRAULIC SYS COLLAPSED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 187UA 26876 RIGHT WING GEAR WOULD NOT RETRACT AFTER TAKEOFF. CYCLED GEAR, NO HELP. WING GEAR DID NOT RETRACT DUE TO LOW SYSTEM 4 P RESSURE. NR 4 HYDRAULIC SYSTEM FOUND CONTAMINATED DUE TO EDP OVERHEAT CONDITION. OVERHEAT CONDITION BELIEVED DUE TO PA RTIALLY COLLAPSED EDP PRESSURE LINE. REPLACED EDP, ADP, ACMP, EDP SUPPLY LINE, PRESSURE LINE AND CASE DRAIN LINE. PRES SURE MODULE FILTERS, CASE DRAIN MODULE. FLUSHED SYSTEM NUMEROUS TIMES, AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2002020600092 20020206 00092 NM 2002 2 6 2002UALA00147 1 20020125 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 BODY STATION 1197+88 LBL 40-45 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002020600093 20020206 00093 NM 2002 2 6 2002UALA00148 1 20020125 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 BODY STATION 1197+110 LBL 40-45 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002020600094 20020206 00094 NM 2002 2 6 2002UALA00149 1 20020126 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 CABIN RIGHT HAND CREASE BEAM WEB BETWEEN STATION 996-1006 CORRODED. MAJOR REPAIR ACCOMPLISHED. CREASE BEAM WEB REPLACE D. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020600095 20020206 00095 NM 2002 2 6 2002UALA00150 1 20020125 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 CABIN FLOORBEAM CORRODED AFT UPPER FLANGE UPPER AND LOWER SURFACES STATION 377 LBL 58. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020600097 20020206 00097 NM 2002 2 6 2002UALA00151 1 20020126 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 CABIN FLOORBEAM HAS CORROSION AT STATION 324 RBL 41-68. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM BY SPLICING IN T -CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020600098 20020206 00098 NM 2002 2 6 AUS20020021 1 20020110 A 2720 69579005 SPRING 65C25465 BOEING 737 737 UTILSYS NM GE CFM56 CFM567B24 NE RUDDER CONTROL BROKEN W O OTHER F FLT CONT AFFECTED DE DESCENT 1 AU S 2617 (AUS) FEEL AND CENTERING UNIT INNER SPRING BROKEN. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002020600103 20020206 00103 NM 2002 2 6 2002UALA00152 1 20020126 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 CABIN FLOORBEAM HAS CORROSION STATION 310 RBL 39 TO 41 UPPER T-CAP. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM WITH ANGLE INSTALLED ON AFT FLANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020600104 20020206 00104 NM 2002 2 6 2002UALA00156 1 20020128 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 924UA 26645 FUSELAGE SKIN AT BODY STATION 845, STRINGER 21R TO 23R IS DENTED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPA IR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020600105 20020206 00105 NM 2002 2 6 2002UALA00157 1 20020128 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 924UA 26645 BODY STATION 188, WL 209 LEFT HAND SIDE FRAME IS CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FRAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020600106 20020206 00106 EU 2002 2 6 AUS20020029 1 20020116 A 2450 B345LS CONTACTOR BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE AC POWER OPEN W K NONE J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 AU S (AUS) AFTER TAKEOFF THE CREW REPORTED THAT SEVERAL SYSTEMS WARNINGS CAME ON. INVESTIGATION FOUND THE AUXILIARY CONTACTS WERE OPEN CIRCUITED ON BUS TIE CONTACTOR XD4. 2 H 7 4 4F 4 F A49EU E6NE 2002020600107 20020206 00107 NM 2002 2 6 2002UALA00158 1 20020128 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 924UA 26645 LEFT HAND LOWER FUSELAGE STATION 947, STRINGER 17L, SKIN IS DENTED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER RE PAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020600108 20020206 00108 NM 2002 2 6 2002UALA00160 1 20020129 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 EXTERNAL FUSELAGE SKIN DENT AT STATION 1010 STRINGER 12L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND INSTALLED REPA IR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020600109 20020206 00109 NM 2002 2 6 2002UALA00162 1 20020128 A 5320 ATTACH ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 MAJOR BS 246 RBL 70-72 WL 199.5 ANGLE ATTACHING TO BULKHEAD IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INS TALLED CHORD AND SPLICE ANGLES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002020600110 20020206 00110 NM 2002 2 6 2002UALA00163 1 20020128 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 MAJOR BS 1197+88 LBL 40-45 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002020600111 20020206 00111 NM 2002 2 6 2002UALA00164 1 20020128 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 MAJOR BS 344-348 STRINGER 20R RBL 82-83 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORB EAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2002020600112 20020206 00112 SO 2002 2 6 C2XA02TY023 1 20020206 A 5210 14533990403 ARM EMB 145 EMB145ER 3260211 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 TYS, During a scheduled 1C inspection, the upper rotation arm on the cabin door was found gouged. Maintenance blended th e damage, performed dye penetrant inspection (no defects noted) and restored protective finish. I/A/W-EMB-GST-0360/02, r epair procedures are satisfactory and aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002020600113 20020206 00113 NM 2002 2 6 2002UALA00165 1 20020127 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 FUSELAGE DENTED AFT OF THE NR 2 MAIN DOOR. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020600114 20020206 00114 SW 2002 2 6 AUS20020031 1 20020111 A 3230 LANDING GEAR SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP HARTZL HCB3T HCB3TN5 GL NOSE FAULTY W O OTHER O OTHER DE DESCENT 1 AU S (AUS) NOSE LANDING GEAR FAILED TO EXTEND. NLG EXTENDED AND LOCKED USING EMERGENCY FREE FALL SYSTEM. INVESTIGATION COULD FIND NO CAUSE FOR THE DEFECT. RETRACTION TESTS CARRIED OUT AND AIRCRAFT RETURNED TO SERVICE AND HAS OPERATED NORMALLY SI NCE. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P15EA 2002020600115 20020206 00115 SO 2002 2 6 C2XA02TY024 1 20020206 A 5520 14532475401 BELLCRANK EMB 145 EMB145ER 3260211 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 TYS, During a scheduled 1C inspection, the left elevator attach bellcrank was found gouged. Maintenance blended the dama ge, performed dye penetrant inspection (no defects noted) and restored protective finish. I/A/W-EMB-GST-0415/02, repair procedures are satisfactory and aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002020600116 20020206 00116 NM 2002 2 6 2002UALA00166 1 20020128 A 5314 KEELBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 MAJOR BS 794.5 STRINGER 39 RBL 9 LOWER KEELBEAM FASTENER HOLE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INST ALLED RETAINER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002020600117 20020206 00117 SO 2002 2 6 C2XA02TY026 1 20020206 A 5753 14568004005 TRACK EMB 145 EMB145ER 3260211 SO WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 TYS, During a scheduled 1C inspection, the right inboard flap track was found worn by roolers at normal flap degree stop s. Maintenance blended the worn areas, performed dye penetrant inspection (no defects noted, I/A/W-EMB-GST-0355/02, repa ir procedures are satisfactory and aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002020600118 20020206 00118 SO 2002 2 6 C2XA02TY027 1 20020206 A 5753 14568003003 TRACK EMB 145 EMB145ER 3260211 SO WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 TYS, During a scheduled 1C inspection, the right inboard flap, outbd track was found worn by roolers at normal flap degr ee stops. Maintenance blended the worn areas, performed dye penetrant inspection (no defects noted, I/A/W-EMB-GST-0355/0 2, repair procedures are satisfactory and aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002020600119 20020206 00119 SO 2002 2 6 C2XA02TY028 1 20020206 A 5753 14568254003 TRACK EMB 145 EMB145ER 3260211 SO WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 TYS, During a scheduled 1C inspection, the right outboard flap, inbd. track was found worn by roolers at normal flap deg ree stops. Maintenance blended the worn areas, performed dye penetrant inspection (no defects noted, I/A/W-EMB-GST-0355/ 02, repair procedures are satisfactory and aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002020600120 20020206 00120 SO 2002 2 6 C2XA02TY029 1 20020206 A 5753 14568253003 TRACK EMB 145 EMB145ER 3260211 SO WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 TYS, During a scheduled 1C inspection, the right outboard flap, outbd. track was found worn by roolers at normal flap de gree stops. Maintenance blended the worn areas, performed dye penetrant inspection (no defects noted, I/A/W-EMB-GST-0355 /02, repair procedures are satisfactory and aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002020600121 20020206 00121 NM 2002 2 6 AUS20020032 1 20020117 A 7732 241106000M101 CONTROL UNIT BOEING 747 747338 NM RROYCE RB211 RB211524D419 54555 NE VIBRATION SIGNAL FAULTY W O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED CR CRUISE 1 AU S 21433 (AUS) NR 2 ENGINE VIBRATION SIGNAL CONTROL UNIT SUSPECT FAULTY. 2 L 7 2 4F 4 F RT A20WE E12EU 2002020600123 20020206 00123 NM 2002 2 6 AUS20020036 1 20020116 A 5340 1114T40201 FITTING BOEING 767 767277 1385128 NM GE CF6 CF680A 30025 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) CENTER TANK LONGERON TO FORWARD FUSELAGE FITTINGS PNO 1114T4020-1 (LT) AND PN 1114T4020-3 (RT) CRACKED. FOUND DURI NG MAGNETIC PARTICLE INSPECTION. 2 L 7 2 4F 4 F RT A1NM E13NE 2002020600124 20020206 00124 SO 2002 2 6 COMA0210002 1 20020204 A 5280 12012347001 HANDLE EMB 120 EMB120RT 3260202 SO L/H MLG DEFECTIVE A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 269CA 120263 FLIGHT 5021 L/H MLG INDICATED INTRANSIT AFTER GEAR RETRACTION.REPLACED THE L/H INBD GEAR DOOR LATCH. 2 L 7 2 4T RT A31SO 2002022500053 20020225 00053 SO 2002 2 25 COMA0210003 1 20020201 A 3350 D366040001 BATTERY EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 264CA 18245 120256 FLIGHT 5044 EMERGENCY FLOOR PATH LIGHTS ARE INOP IN SEVERAL PLACES. REPLACED THE NR 2 EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 2002020600126 20020206 00126 EA 2002 2 6 COMA0260083 1 20020201 A 5530 600210617SB BUSHING CNDAIR CL600 CL6002B19 1900309 EA VERTICAL STAB SCORED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 952CA 14826 7092 THE R/H VERTICAL STABILIZER BUSHING WAS SCORED AT HORIZONTAL STABILIZER PIVOT POINT.REMOVED THE SCORED BUSHING. MACHINE D FLANGE OF NEW BUSHING P/N 600-21061-7S/B I/A/W WVAC EO 601R-55-2952.INSTALLED THE NEW BUSHING I/A/W CRJ AMM 20-26-00-9 10-803. REAMED THE BUSHING TO TOLERANCE I/A/W DRG 600-21029. 2 L 7 2 4F RT A21EA 2002020600127 20020206 00127 EA 2002 2 6 COMA0260084 1 20020204 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 403CA 3050 7428 FLIGHT 5518 FLAPS FAIL CAUTION MESSAGE.REPLACED THE LEFT BPSU. 2 L 7 2 4F RT A21EA 2002020600128 20020206 00128 EA 2002 2 6 COMA0260085 1 20020204 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 916CA 11512 7014 FLIGHT 5525 FLAPS FAIL CAUTION MESSAGE.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2002020600130 20020206 00130 NM 2002 2 6 2002UALA00167 1 20020128 A 5314 KEELBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 MAJOR BS 790 STRINGER 39 RBL 9 KEEL BEAM FASTENER HOLE IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLE D RETAINER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002020600131 20020206 00131 NM 2002 2 6 2002UALA00168 1 20020130 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 FORWARD PIT BILGE AREA BODY STATION 500 FRAME CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002020600132 20020206 00132 NM 2002 2 6 2002UALA00169 1 20020129 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 TOP CAP OF FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002022100048 20020221 00048 NM 2002 2 21 2002UALA00171 1 20020129 A 3610 32144887 SHUTOFF VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BLEED AIR SYS DEFECTIVE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 592UA 28143 RIGHT ENGINE BLEED OFF MSG PER CREW AND NO DUCT PRESSURE ON RIGHT SIDE AND LOST RIGHT PACK. PRSOV MANUAL HEX OVERRIDE N UT OUT OF OPEN DETENT AND SAFETY WIRE BROKEN. REPLACED PRSOV. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021300071 20020213 00071 2002 2 13 2002UALA00172 4 20020130 A 3460 4058650931 CDU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 648UA 25285 RT FMC OVERHEATED SHORTLY AFTER DEPARTURE. A HOT PLASTIC SMELL WAS VERY EVIDENT IN THE COCKPIT. CAPT ELECTED TO RETURN TO IAD. RT FMC HMCDU OVERHEATED, HOT PLASTIC SMELL WAS VERY EVIDENT IN THE COCKPIT. RT HMCDU BECAME INOPERATIVE AND WAS VERY HOT TO TOUCH. REPLACED THE RIGHT HMCDU. SHOP FINDINGS: BURNED TRACE ON THE I/O CARD A5. SHOP REPORTED PREVI OUS HMCDU'S WITH OVERHEATED CARD A5. 2 L 7 2 4F 4 F RT A1NM E24NE 2002020600133 20020206 00133 WP 2002 2 6 DHL2002804001 1 20020131 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CARGO BAY INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 804DH 46124 UPPER CARGO SMOKE DETECTOR ZONES 9 & 11 WILL NOT TEST. NR 7 MAIN DECK SMOKE DETECTOR SCREEN BRACKET BROKEN. RELAMPED N R 9 AND NR 11 SMOKE DET, OPS CHECK GOOD IAW DC-8 MM 26-10-6. REMOVED AND REPLACED NR 7 MAIN DECK SMOKE DET ASSY IAW DC- 8 MM 26-10-6. 2 L 7 4 4F RT 4A25 2002020600134 20020206 00134 WP 2002 2 6 DHL2002805029 1 20020114 A 5751 SKIN DOUG DC8 DC873F 302199F WP AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 LEFT WING INBOARD AILERON UPPER SKIN AT STA XW 563.000 CRACKED .5 INCH. 2 L 7 4 4F RT 4A25 2002020600135 20020206 00135 WP 2002 2 6 DHL2002805030 1 20020110 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 MAIN CARGO COMPT LT CUSP EXTRUSION TO FRAME JOINT FITTING .5 INCH CRACK, STA 1060. 2 L 7 4 4F RT 4A25 2002020600136 20020206 00136 WP 2002 2 6 DHL2002805031 1 20020119 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AFT CARGO COMPT PRESSURE BULKHEAD LINING SUPPORT ANGLE CRACKED 1 INCH AT STA 980.000 LBL 40. 2 L 7 4 4F RT 4A25 2002020600137 20020206 00137 WP 2002 2 6 DHL2002805032 1 20020109 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 MAIN CARGO COMPT BEAM TO INTERCOSTAL JOINT ANGLE CRACKED .5 INCH AT STA 680.000 LBL 23. 2 L 7 4 4F RT 4A25 2002020600138 20020206 00138 WP 2002 2 6 DHL2002805033 1 20020119 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 MAIN CARGO COMPT FRAME 3 INCH DENT AT STA 1580.000L-21R. 2 L 7 4 4F RT 4A25 2002020600139 20020206 00139 WP 2002 2 6 DHL2002805034 1 20020115 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AFT PRESS BULKHEAD .25 INCH CRACK ON ANGLE ATTACHED TO L-9R AT FS 1766.00. 2 L 7 4 4F RT 4A25 2002020600140 20020206 00140 WP 2002 2 6 DHL2002805035 1 20020118 A 2780 47701422 FITTING DOUG DC8 DC873F 302199F WP L/E SLOT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 LEFT WING OUTBOARD SLOT TORQUE TUBE FITTING CRACKED. 2 L 7 4 4F RT 4A25 2002020600141 20020206 00141 WP 2002 2 6 DHL2002805038 1 20020123 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 RIGHT MLG W/W FITTING ATTACHED TO LONGERON 24 HAS A 2 INCH CRACK AT STA 897.375. 2 L 7 4 4F RT 4A25 2002020600142 20020206 00142 WP 2002 2 6 DHL2002805039 1 20020123 A 5240 COVER DOUG DC8 DC873F 302199F WP SERVICE DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 FWD SERVICE DOOR CUSP EXTRUSION COVER FWD LOWER JAMB HAS A 0.250 INCH CRACK AT FS 160.00. 2 L 7 4 4F RT 4A25 2002020600143 20020206 00143 WP 2002 2 6 DHL2002805041 1 20020107 A 5320 CLIP DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 NLG W/W INTERCOSTAL TO PRESS BULKHEAD ATTACH CLIPS (2 EA) CRACKED 2 INCHES AT STA 131.000 RT. 2 L 7 4 4F RT 4A25 2002020600144 20020206 00144 WP 2002 2 6 DHL2002805042 1 20020120 A 5341 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 MAIN CARGO COMPT FUS AFT CTR SPAR FRAME TO WING ATTACH ANGLE CRACKED 1.5 INCH AT STA 798.000 RBL 48. 2 L 7 4 4F RT 4A25 2002020600145 20020206 00145 WP 2002 2 6 DHL2002805043 1 20020121 A 5341 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 MAIN CARGO COMPT FUS AFT CENTER SPAR FRAME TO WING ATTACH ANGLE CRACKED 2 INCHES AT STA 759.000, LBL 48. 2 L 7 4 4F RT 4A25 2002020600157 20020206 00157 EU 2002 2 6 AWXA200200104 1 20020203 A 5330 2024T3080 DOUBLER AIRBUS 320 A320231 3930325 EU DENTED A AWXA K NONE O OTHER TX TAXI/GRND HDL 1 WP 28 636AW 098 PHX - GROUND DAMAGE - "O" - DURING WALK AROUND DAMAGE TO THE FUSELAGE SKIN WAS FOUND JUST AFT OF THE RADOME ON BELLY OF AIRCRAFT AT FS 01. MAINTNENANCE PERFORMED HFEC INSPECTION ON OUTSIDE SKIN AND INTERNAL SURROUNDING STRUCTURE, NO DEFECTS WERE NOTED. TEMPORARY FASTENERS WERE INSTALLED AS PER AWA ER 26-5330-02036-SS2 SHT 2, PERMANENT FASTENERS MUST BE INSTA LLED WITHIN 2500 FLIGHT CYCLES. DOUBLER WAS FABRICATED FOR REPAIR AND DAMAGED AREA PLACED ON MONITOR, CONTROL # 220150. **SUPPLEMENTAL SDR WILL BE SUBMITTED UPON COMPLETION OF REPAIR. 2 L 7 2 4F RT A28NM 2002020600158 20020206 00158 EU 2002 2 6 AWXA200200107 1 20020205 A 3350 E0261CF20 CABLE AIRBUS 320 A320232 3930326 EU SEAT 24 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 653AW 1003 PHX - EEL - "C" - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHT AT ROW 24 L/H WAS FOUND INOPERATIVE. MAINTENANCE TROUBLE SHOT AND FOUND BROKEN WIRES AT SEAT ROW 24 L/H, REPAIRED BROKEN WIRES WITH SLICE. 2 L 7 2 4F RT A28NM 2002020700004 20020207 00004 NM 2002 2 7 SWAA020269 1 20020204 A 2560 10107451 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 391SW 27378 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LENS LOOSE ON CEILING PANEL AT ROW 3. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002020700005 20020207 00005 2002 2 7 SWAA020272 4 20020204 A 2565 6949956 CABLE BOEING 737 7373Q8 1384670 NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002020700006 20020207 00006 NM 2002 2 7 SWAA020273 1 20020205 A 5312 6546568 WEB BOEING 737 7375H4 138449D NM AFT CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D CHECK, FOUND WEB CORRO DED AT BS 1016, WL 208 & LBL 15 TO LBL 25. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002020700007 20020207 00007 NM 2002 2 7 SWAA020274 1 20020202 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002020700008 20020207 00008 NM 2002 2 7 SWAA020275 1 20020205 A 5312 6517583 WEB BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 182, WL 185 & RBL 5.7. REPAIRED WEB PER SWA RA. 2 L 7 2 4F A16WE 2002020700009 20020207 00009 NM 2002 2 7 SWAA020277 1 20020205 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 1.5 INCHES LONG AT BS 727D+10, STR 19R. REPAIRED SKIN PER SRM.. 2 L 7 2 4F RT A16WE 2002020700010 20020207 00010 NM 2002 2 7 SABA020017 1 20020206 A 3350 1013075 BULB DHAV DHC8 DHC8103 1386005 NM CABIN BURNED OUT A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 880CC 277 Aircraft 880 on flight 5025 from CLT to TLH. During preflight inspection one red floor emergency evac light was found i noperative. Maintence removed and replaced the bulb. System ops check good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002020700011 20020207 00011 NM 2002 2 7 02035407 1 20020204 A 2435 0160215 STARTER GEN DORNER DO32 DO328300 NM RT ENGINE FAILED A VTZA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 EA 27 407FJ DURING CRUISE FROM CHS TO LGA RT ENGINE VIBRATION ICON ILLUMINATED INDICATING VIBRATIONS >.2" UP TO 1.3" PER SECOND. FL IGHT CREW COMPLIED WITH QRH AND DIVERTED TO PHL. AN EMERGENCY WAS DECLARED WITH ATC AND A/C LANDED IN PHL WITHOUT FURTH ER INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED STARTER GENERATOR AND PERFORMED HIGH ENGINE RUNS, NO FURTHER DE FECTS NOTED AND ALL INDICATIONS WERE WITHIN LIMITS. AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A55NM 2002020700012 20020207 00012 NM 2002 2 7 200200173 1 20020206 A 5320 DOUBLER BOEING 747 747212B 1384886 NM MAIN ENTRY CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 482EV 20713 MAIN ENTRY DOOR NR 5 REVEAL DOUBLER CRACKING. THE REPAIR IS ACCOMPLISHED BY TRIMMING SECTIONS OF THE DOUBLERS OFF AND I NSTALLING REPLACEMENT SECTIONS USING SPLICE DOUBLERS PER ECRA 482-53-140-2. 2 L 7 4 4F A20WE 2002020700013 20020207 00013 NM 2002 2 7 200200174 1 20020206 A 5720 65B108644 FITTING BOEING 747 747212B 1384886 NM WING WORN B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 482EV 20713 THE REINSTALLATION OF THE FITTING REQUIRED THE SUBSTITUTION OF STRAIGHT SHANK FASTENERS IN LIEU OF THE TAPER SHANK FASTE NERS, ORIGINALLY USED THIS REPAIR IS APPROVED BY THE BOEING COMPANY PER ECRA 482-57-141-02. 2 L 7 4 4F A20WE 2002020700014 20020207 00014 NM 2002 2 7 200200175 1 20020206 A 5711 SPAR BOEING 747 747212B 1384886 NM WING CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 482EV 20713 CENTER WING REAR SPAR WEB CORROSION. THIS REPAIR IS ACCOMPLISHED BY BLENDING OUT CORROSION AREAS. SECTION OF THE SLOPI NG PRESSURE DECK ANGLE WHICH WAS REMOVED TO GAIN ACCESS TO CORRODED AREAS IS ALSO REPLACED. THIS IS ACCOMPLISHED USING TWO SPLICE ANGLES. THIS ECRA PROVIDES INSTRUCTIONS TO REINSTALL 3 OF THE REAR SPAR WEB STIFFENERS USING ALTERNATE FASTE NERS PER ECRA 482-57-142-2. 2 L 7 4 4F A20WE 2002030700065 20020307 00065 NM 2002 3 7 2002UALA00175 1 20020130 A 2410 AS1633A10H0160 RETURN LINE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 CSD LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 348UA 24252 UNSCHEDULED LANDING DUE TO NR 1 GENERATOR WENT OFF LINE. TROUBLESHOOTING ISOLATED THE SOURCE OF THE GENERATOR DROPPING OFF-LINE TO AN OIL LEAK OF THE NR 1 ENGINE GENERATOR CONSTANT SPEED DRIVE (CSD) OIL COOLING RETURN LINE. THE LINE WAS R EPLACED, AND THE CSD WAS SERVICED TO PROPER OIL LEVEL. MAINTENANCE ALSO VERIFIED THAT THE GENERATOR AND EXCITER LEADS W ERE PROPERLY TORQUED, AND THE ENGINE FIREWALL AND WING DISCONNECT FEEDER CONNECTORS SHOWED NO SIGNS OF ARCING OR PITTING / DAMAGE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021300075 20020213 00075 NM 2002 2 13 2002UALA00177 1 20020201 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 FORWARD BULKHEAD STATION 178 CENTER WEB CRACKED RBL 0.5 WL 186. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021300076 20020213 00076 NM 2002 2 13 2002UALA00178 1 20020201 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 FORWARD BULKHEAD STATION 178 LOWER RIGHT HAND ANTENNA MOUNT WEB CRACKED ON INBOARD SIDE LOWER FASTENER, AND INBOARD SIDE AT UPPER FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021300079 20020213 00079 NM 2002 2 13 2002UALA00179 1 20020201 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 FORWARD BULKHEAD STATION 178 WEB, LOWER LEFT HAND ANTENNA MOUNT 2 CRACKS ON INBOARD SIDE OF MOUNT. MAJOR REPAIR ACCOMPL ISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021300080 20020213 00080 NM 2002 2 13 2002UALA00180 1 20020201 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 EXTERNAL FUSELAGE STATION 1026 SKIN DENTED ON STRINGER 11L. MAJOR REPAIR ACCOMPLISHED. STRINGER SPLICE AND SKIN DOUBLE R INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040500049 20020405 00049 NE 2002 4 5 2002UALA00181 2 20020129 A 7230 52A129 BEARING BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT ENGINE WORN A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 794UA 3090 3090 26953 222013 AIRCRAFT EXPERIENCED A LOSS IN OIL QUANTITY IN THE RT ENGINE. DIVERTED TO YUL. OIL QUANTITY AT TOP OF DESCENT WAS ZERO WITH NORMAL TEMP/PRESSURE. ARRIVED WITH NO PROBLEMS. "ENG OIL FILTER R" BYPASS MESSAGE DISPLAYED AT TOP OF DESCENT; EN GINE CONTINUED TO OPERATE NORMALLY UNTIL DELIBERATELY SHUT DOWN ON THE GROUND. METAL WAS FOUND ON NR 3 BEARING MAGNETIC CHIP DETECTOR, ENGINE REMOVED. EXTENSIVE FRETTING WEAR BETWEEN NR 3 BEARING AND CARBON SEAL SEAT COMPONENTS, ESPECIALL Y INNER RACE AND REAR SEAL SEAT. OIL WETTING & COKING WAS FOUND IN THE HIGH PRESSURE TURBINE T1 DISK, INDICATING OIL LO SS THROUGH THIS AREA. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002030100015 20020301 00015 EU 2002 3 1 2002UALA00182 1 20020201 A 2120 ODOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 429UA 539 SMELL OF SMOKE IN CABIN. NO SMOKE VISIBLE. FLIGHT ATTENDANT SMELLED SMOKE IN THE CABIN. NO SMOKE WAS SEEN, SMELL WAS PUNGENT AND LOCATED JUST AFT OF 1ST CLASS. ACCOMPLISHED BITE CHECK OF THE TEMPERATURE CONTROL SYSTEM, CHECKED ALL FANS FOR OPERATION, CHECKED CABIN INTERCOMMUNICATION DATA SYSTEM FOR FAULTS, CHECKED ALL CABIN LIGHTS. NO FAULTS FOUND. CHE CKED THE ENVIRONMENTAL CONTROL SYSTEM (ECS) FOR CONTAMINATION, NONE FOUND. ACCOMPLISHED STAGE 2 CLEANING OF ECS SYSTEM , NO FURTHER REPORTS OF CABIN ODORS. 2 L 7 2 4F 4 F RT A28NM E40NE 2002030100016 20020301 00016 2002 3 1 2002UALA00183 4 20020131 A 2565 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR DEFECTIVE A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 829UA 1211 DURING EMERGENCY LIGHT TEST EXTERIOR LOAD AFT L MESSAGE WAS DISPLAYED. THE FAILURE MESSAGES INCLUDED COMM EMERGENCY R, EMERGENCY L, COMM AFT L, EXT LOADS AFT L. MOVED THE 2L SLIDE TO 2R TO ISOLATE THE PROBLEM. THEN REPLACED THE 2R SLIDE TO FIX THE PROBLEM AND ELIMINATE THE ERROR MESSAGES. 2 L 7 2 4F 4 F RT A28NM E40NE 2002030100018 20020301 00018 NM 2002 3 1 2002UALA00184 1 20020131 A 2530 E500175 CART BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY DEFECTIVE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 601UA 21862 BURNT ELECTRICAL ODOR FROM INSIDE GALLEY CART IN THE RIGHT SECTION OF THE AFT GALLEY REPORTED BY FLIGHT ATTENDANTS. BUR NT ODOR CAME FROM CART 404. CART REMOVED IN IND. POWERED UP ENTIRE GALLEY. CHECKED OPERATION OF ALL GALLEY COMPONENTS AND LIGHTS. CONFIRMED SMELL CAME FROM CART. NO OTHER DEFECTS WERE NOTED. THE PIGTAIL TO SUSPECT CART WAS REMOVED FRO M AIRCRAFT. 2 L 7 2 4F 4 F RT A1NM E3NE 2002020700015 20020207 00015 NM 2002 2 7 2002UALA00186 1 20020131 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 FORWARD CARGO COMP STATION 740 FUSE FRAME UPPER CAP GOUGED ABOVE STRINGER 28L LBL 12. MAJOR REPAIR ACCOMPLISHED. INSTA LLED UPPER CAP STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020700016 20020207 00016 NM 2002 2 7 2002UALA00187 1 20020131 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 AFT CABIN FLOORBEAM CAP AT BODY STATION 1540, LBL 3, RBL 12, EXCESSIVE MATERIAL LOSS AFTER BLEND. MAJOR REPAIR ACCOMPLI SHED. STRAP REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020700017 20020207 00017 NM 2002 2 7 2002UALA00188 1 20020131 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 AFT CAB, FLOORBEAM AT STATION 1640 BL 0, HAD EXCESSIVE MATERIAL REMOVED. MAJOR REPAIR ACCOMPLISHED. DOUBLE FLANGE REDU CED FASTENER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002020700018 20020207 00018 NM 2002 2 7 2002UALA00189 1 20020201 A 5320 PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 CABIN FLOOR DECK PLATE CORRODED STA 1681, RBL 12-24 WL 208. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021100022 20020211 00022 WP 2002 2 11 AT0200005 1 20020204 A 2730 NUT DOUG DC9 DC932 3022066 WP ELEVATOR BACKED OUT A ZZDA K NONE E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 SO 15 849AT 47484 AIRCRAFT ROTATED WITHOUT MUCH ELEVATOR INPUT. ON CLIMBOUT CREW FELT VIBRATION IN YOKE. AILERON TRIM OF 2.5 DEGREES LEF T AND 1 DEGREE LEFT, RUDDER WAS IMPUTED THROUGH LANDING. LANDING STABILIZATION TRIM WAS 2 DEGREES NOSE UP. FOUND RIGHT HAND ELEVATOR JAMMED IN UP POSITION DUE TO ELEVATOR HYDRAULIC BOOST CYLINDER ATTACH ROD NUT BACKED OFF AND ROD END JAMM ED ELEVATOR. REMOVED AND REPLACED ROD END RETAINER, NUT AND COTTER PIN. PERFORMED ELEVATOR POWER ON CHECK. 2 L 7 2 4F A6WE 2002020700019 20020207 00019 EU 2002 2 7 AWXA200200095 1 20020201 A 2612 D2612178000060 FIRE LOOP AIRBUS 320 A320231 3930325 EU NR 1 ENGINE CHAFED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 627AW 66 PHX - ABORTED T/O - FLT 0317 - C - WHILE PREPARING TO TAKEOFF FROM PHX EN ROUTE TO CMH WHEN THROTTLE WERE ADVANCED FLIGH T CREW RECEIVED A NR 1 ENGINE FIRE LOOP-A FAULT. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE TR OUBLESHOT AND FOUND CORE LOOP-A HARNESS CHAFED ALMOST ALL THE WAY THROUGH IN TWO PLACES APPROXIMATELY 6 INCHES FROM HIGH PRESSURE BLEED VALVE. REMOVED AND REPLACED CORE LOOP-A HARNESS IAW AMM 26-12-17-401, OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2002020700020 20020207 00020 NM 2002 2 7 AWXA200200097 1 20020202 A 5610 5893543109 WINDSHIELD BOEING 737 7373S3 1384711 NM COCKPIT CRACKED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 313AW 19401 23712 GEG - DIVERSION - FLT 592 - O - EN ROUTE FROM GEG TO PHX AT FL 330 CABIN PRESSURE DIFFERENTIAL OF 7.8 PSI CAPTAINS WINDS HIELD OUTER PANE SHATTERED. EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED SAFELY TO BOI. MAINTENANCE ARRIVED AT BOI FRO M PHX AND REPLACED THE CAPTAINS WINDSHIELD IAW T/C R1B56001. AS A PRECAUTION THE CAPTAINS NR 1 WINDOW HEAT CONTROL UNIT WAS ALSO REPLACED. WINDOW HEAT CONTROL UNIT, PACIFIC ELECTRO, P/N: 83000-05602, S/N: 2421. 2 L 7 2 4F RT A16WE 2002020700021 20020207 00021 NM 2002 2 7 AWXA200200101 1 20020121 A 5312 6545409245 PRESSURE PANEL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - MAJOR REPAIR - C - DURING C-16 CHECK A CRACK WAS FOUND ON THE LEFT MAIN WHEEL WELL UPPER PRESSURE DECK BS 665, LBL 33. MAINTENANCE TRIMMED OUT DAMAGED SECTION OF UPPER PRESSURE WEB AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED. FABRICATED DOUBLER, STIFFENER, AND FILLERS. INSTALLED REPAIR PARTS IAW AWA ER 03-5702-02032-GF3. 2 L 7 2 4F RT A16WE 2002020700022 20020207 00022 EU 2002 2 7 AWXA200200106 1 20020202 A 2560 MZ68742100 FLASHLIGHT AIRBUS 320 A320232 3930326 EU CABIN DEFECTIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 663AW 1419 PHX - EEL - C - FLASHLIGHT AT FORWARD FLIGHT ATTENDANT STATION HAS NO FLASHING RED CHARGE LIGHT. MAINTENANCE REMOVED AN D REPLACED WITH SERVICEABLE FLASHLIGHT. 2 L 7 2 4F RT A28NM 2002020700023 20020207 00023 SO 2002 2 7 C2XA02CL032 1 20020204 A 2530 CBC16707 RECEPTACLE EMB 145 EMB145ER 3260211 SO GALLEY BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14925 145004 CLE FLIGHT 3279 THE CREW REPORTED THE LEFT COFFEE POT WARMER DID NOT WORK AND HAD A BURNING SMELL WHEN TURNED ON. MAINT ENANCE INSPECTED AND REPLACED THE LT COFFEE POT WARMER RECEPTACLE CONNECTOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAF T WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002020700025 20020207 00025 SO 2002 2 7 C2XA02TY022 1 20020205 A 3222 11701402 AXLE EMB 145 EMB145ER 3260211 SO NLG GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 TYS DURING A SCHEDULED 1-C INSPECTION THE NLG AXLES HAD SOME SMALL GOUGES NOTED. A GST WAS ISSUED GST 0389/02 THAT STA TED BLEND AREA AND APPLY NDI AND IF NO CRACKS ARE FOUND, RESTORE PROTECTIVE FINISH. NO CRACKS WERE FOUND. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002020700026 20020207 00026 SO 2002 2 7 CHQ000110 1 20020130 A 3350 BATTERY EMB 145 EMB145 3260210 SO CABIN DISCHARGED A CHQA K NONE L NO TEST UK UNKNOWN 1 GL 11 265 145226 ALL EMERGENCY LIGHTS OFF OF NR 4 BATTERY INOP. REMOVED AND REPLACED EMERGENCY BATTERIES. 2 L 7 2 4F RT T00011AT 2002020700027 20020207 00027 EU 2002 2 7 CHQ000111 1 20020205 A 3150 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU COCKPIT ACTIVATED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 150 150 RETURNED TO FIELD FOR CONFIGURATION WARNING. 2 L 7 2 4T RT A52EU 2002020700028 20020207 00028 SO 2002 2 7 CHQ000112 1 20020206 A 5610 WINDSHIELD EMB 145 EMB145 3260210 SO COCKPIT DELAMINATED A CHQA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 270 145304 F/O'S WINDSHIELD DELAMINATING, AOG FOR WINDSHIELD. 2 L 7 2 4F RT T00011AT 2002020700029 20020207 00029 2002 2 7 DHL2002363001 4 20020205 A 3414 INDICATOR AIRBUS 300 A300B4203 3930306 EU COCKPIT FAULTY A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 363DH 85 AIRSPEED FLAG APPEARED DURING INITIAL TAKEOFF ROLL ON CAPTAINS SIDE. REJECTED TAKEOFF. TROUBLESHOT AIRSPEED IND IAW 34 -12-22. REMOVED AND REPLACED AIRSPEED IND, OPS CHECK GOOD IAW 34-12-22 AND 34-11-40. PITOT STATIC PRESSURE CHECK GOOD IAW AMM 34-11-40. 2 L 7 2 4F RT A35EU 2002020700030 20020207 00030 NM 2002 2 7 DHL2002745002 1 20020205 A 2612 LIGHT BOEING 727 727224 1384076 NM COCKPIT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 745DH 20665 NR 1 ENGINE FIRE WARNING WILL NOT TEST. REMOVED AND REPLACED FIRE WARNING TEST LIGHT BULBS IAW M/M 33-10-51, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002020700031 20020207 00031 NM 2002 2 7 DHL2002749001 1 20020205 A 2450 CONTROL PANEL BOEING 727 727200 138407E NM COCKPIT FAULTY A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 749DH 22013 TAKEOFF ROLL GEN NR 2 BUS TIE LIGHT ILLUMINATED. REJECTED TAKEOFF. ACCOMPLISHED ABNORMAL CHECKLIST, SYSTEM RETURNED TO NORMAL. MOVE THRUST LEVERS AND SAME CONDITION RETURNED. S/O AUX PANEL INDICATED GEN OVER - EXCITED SYSTEM NR 2. REMO VED AND REPLACED NR 2 GEN CONTROL PANEL AND RAN ALL THREE ENGINES. SYSTEM OPS CHECKED NORMAL IAW DHL MM 24-10-0. 2 L 7 3 4F RT A3WE 2002021100044 20020211 00044 WP 2002 2 11 DHL2002803005 1 20020206 A 2611 SMOKE DETECTOR DOUG DC8 DC873 302199C WP CARGO BAY FAULTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 803DH 46123 NR 9 SMOKE DETECTOR DOES NOT TEST PROPERLY, LIGHT ILLUMINATES BUT NOT EXTINGUISH. REMOVED AND REPLACED NR 9 SMOKE DETEC TOR ASSY AT MAIN CARGO COMPARTMENT GROUND OPS CK'D NORMAL IAW MM 26-10-5. 2 L 7 4 4F RT 4A25 2002020700035 20020207 00035 WP 2002 2 7 DHL2002806001 1 20020130 A 2611 LIGHT DOUG DC8 DC873F 302199F WP SMOKE DETECTOR INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806DH 46002 NR 1 SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED BEACON LAMP IN NR 1 SMOKE DETECTOR IAW MM 26-10-6, TESTED OPERA TION OK. 2 L 7 4 4F RT 4A25 2002020700036 20020207 00036 NM 2002 2 7 F3LA200200025 1 20020124 A 7830 ATTACH FITTING BOEING 737 7372Y5 1384554 NM THRUST REVERSER CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE BOTTOM OUTBOARD THRUST REVERSER ATTACH POINT DAMAGED AND CRACKED IN 2 PLACES. REPAIRED CRACKS AND DAMAGED AREA PER SRM 51-30-6. 2 L 7 2 4U RT A16WE 2002020700037 20020207 00037 NM 2002 2 7 F3LA200200026 1 20020125 A 7120 654685010 MOUNT BOEING 737 737228 13844AG NM NR 2 ENGINE WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED SEVERE MOVEMENT IN NR 2 ENGINE AT YOKE IN PYLON, INBOARD SIDE. REPLACED NR 2 ENGI NE MOUNT YOKE PER MM 54-41-11, 4C - J, PAGES 41 AND 402. 2 L 7 2 4F RT A16WE 2002020700039 20020207 00039 NM 2002 2 7 F3LA200200027 1 20020126 A 7120 MOUNT BOEING 737 737228 13844AG NM NR 2 ENGINE WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED EXCESSIVE PLAY IN NR 2 ENGINE YOKE TO WING MOUNT. REPLACED ENGINE MOUNT FITTINGS AND YOKE PER MM 54-51-41. 2 L 7 2 4F RT A16WE 2002020700042 20020207 00042 NM 2002 2 7 F3LA200200030 1 20020201 A 5311 BELTFRAME BOEING 737 7372Y5 1384554 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED BELT FRAME CORRODED AND CRACKED AT STA 807, BL 0. REPAIRED FRAME SHEAR TIE PER SR M 53-10-2. 2 L 7 2 4U RT A16WE 2002020700047 20020207 00047 NM 2002 2 7 CALA0200061 1 20020206 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 400 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND FUSELAGE SKIN DENTED FORWARD OF STA 400 BELOW S22R. A DOUBLER WAS INSTALLED IAW SRM 51-40-03. 2 L 7 2 4F RT A16WE 2002020700048 20020207 00048 NM 2002 2 7 CALA0200062 1 20020207 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 380-540 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 380-540. THE CORROSION WAS REMOVED IAW SRM 53-00-52. THE AREA AT STA 410 WAS BEYOND ALLOWABLE LIMITS. THE SEAT TRACK WAS REMOVED AND REPLACED FROM STA 380-480 IAW SRM 53-00-52. THE SEAT TR ACK WAS TREATED AND PRIMED FROM STA 380-540 IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2002020700049 20020207 00049 NM 2002 2 7 CALA0200063 1 20020206 A 2150 20405011 ACM BOEING 737 737524 1384721 NM R/H PACK LEAKING A CALA A D UNSCHED LANDING RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 14613 23343 27326 SMOKE AND FUMES ENTERED THE CABIN AFTER TAKEOFF FROM IAH. SOME ALARMS IN THE CABIN ACTIVATED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE R/H ACM TURBINE OIL SEAL BLOWN. THE R/H ACM AND COALESCER BAG WAS REMOVED AND REPLACED IAW MM 21-51-11 AND 21-51-41. THE LEFT PACK, AIR CONDITIONING DISTRIBUTION AREA, WHEEL WEL LS, AND TAIL AREA WERE INSPECTED WITH NO OTHER DISCREPANCIES NOTED. 2 L 7 2 4F RT A16WE 2002020700050 20020207 00050 NM 2002 2 7 CALA0200064 1 20020206 A 3233 273A12011 ACTUATOR BOEING 737 737824 13844BZ NM NLG INOPERATIVE A CALA A D UNSCHED LANDING RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 09 26210 12336 28770 THE NLG WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. THE FAILURE WAS ACCOMPANIED BY ILLUMINATION OF THE NLG UNSAFE LIGHT AN D VIBRATION FROM THE NOSE GEAR AREA. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NLG LOCK ACT UATOR AND LOCK MANIFOLD VALVE WERE REMOVED AND REPLACED IAW MM 32-33-21 AND 32-33-31. AN OPERATIONAL TEST WAS PERFORMED IAW MM 32-33-00 AND SYSTEM CHECKS WERE NORMAL. 2 L 7 2 4F RT A16WE 2002020700051 20020207 00051 EA 2002 2 7 HNAA0200010 1 20020130 A 2130 21178041 COMPUTER DHAV DHC8 DHC8311 1386006 EA CABIN PRESSURE FAULTY A HNAA I A CABIN DEPRESSURIZATION UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 326EN 17477 234 AFTER TAKEOFF, WITH PRESSURIZATION CONTROL ON AUTO, AIRCRAFT STARTED TO PRESSURIZE OUT OF CONTROL, SELECTED TO DUMP POSI TION. REPLACED PRESSURIZATION COMPUTER. 2 H 7 2 4T RT A13NM 2002020700052 20020207 00052 NE 2002 2 7 HNAA020009 2 20020129 A 7200 3038400 ENGINE DHAV DHC8 DHC8201 2809001 NM PWA PW120 PW123 NE NR 2 MAKING METAL A HNAA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 EA 07 988HA 11367 426 AT0002 WHILE SETTING CRUISE POWER NR 2 ENGINE BEGAN CLANKING AND POPPING. CREW SECURED NR 2 ENGINE AND RETURNED TO DEPARTURE F IELD. MAINTENANCE FOUND METAL CONTAMINATION IN THE OIL TANK. REPLACED NR 2 ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002020700053 20020207 00053 WP 2002 2 7 IXXAO200003O 1 20020129 A 3230 UPLOCK DOUG DC8 DC871F 302199D WP LANDING GEAR LACK OF LUBE A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 826BX 84202 2090 45998 EN ROUTE FROM MCI TO TOL, THE LANDING GEAR NOT LATCHED LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK. THE FLIGHT CREW CYCLED THE LANDING BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING . MAINTENANCE INSPECTED THE AIRCRAFT, CLEANED AND LUBRICATED THE GEAR UPLATCH MECHANISMS. MAINTENANCE PERFORMED A SUCC ESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002020700054 20020207 00054 EU 2002 2 7 MALA020128 1 20020114 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 DURING 4K-CHECK IN CWA, FWD LT CENTER AISLE SEAT TRACK LBL 18.3 FLANGE HAS CORROSION. MAINTENANCE REPLACED FWD SECTION OF SEAT RAIL FROM STA 297-349 ON LEFT CENTER AISLE IAW EO S53060. 2 L 7 2 4T RT A52EU 2002020700055 20020207 00055 EU 2002 2 7 MALA020129 1 20020112 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 DURING 4K-CHECK IN CWA, FWD PORTION OF RT CENTER AISLE SEAT TRACK FLANGE HAS CORROSION. MAINTENANCE COMPLETED SEAT TRAC K REPAIR IAW MAL EO S53060. 2 L 7 2 4T RT A52EU 2002020700056 20020207 00056 EU 2002 2 7 MALA020130 1 20020117 A 5411 FRAME SAAB SF340 340B 7860101 EU RT NACELLE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 DURING 4K-CHECK IN CWA, RIGHT O/B NACELLE CHAFE AT STA 197. MAINTENANCE REPAIRED CHAFE IAW MAL EO S54057 AND SAAB STATE MENT 340SDS003130. 2 L 7 2 4T RT A52EU 2002020700057 20020207 00057 EU 2002 2 7 MALA020132 1 20020116 A 5311 7253722001 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 DURING 4K-CHECK IN CWA, FRAME ANGLE FLANGES AT STA 258 ARE CORRODED. MAINTENANCE PERFORMED REPAIR OF FRAME ANGLE P/N 72 53722-001 AT STA 258, IAW EO S53102. 2 L 7 2 4T RT A52EU 2002020700058 20020207 00058 NM 2002 2 7 AWXA200200105 1 20020130 A 5330 65C35798 SKIN BOEING 737 73733A 1384673 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 LCQ - MAJOR REPAIR - "C" - DURING C-16 CHECK A 2" X 10" DENT WAS FOUND AT BS 907 R/H BETWEEN STR 21R AND 22R. MAINTENANC E CUTOUT DENTED AREA OF FUSELAGE SKIN AT BS 907 STR 21R & 22R; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS AT CUTOUT; FABRICATED FILLER AND DOUBLER AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG 223, PG. 314. 2 L 7 2 4F RT A16WE 2002020700059 20020207 00059 NM 2002 2 7 AWXA200200108 1 20020206 A 3350 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM SEAT ROW 3 BROKEN A AWXA A UNSCHED LANDING O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 PHX - EEL - "C" - DURING INSPECTION THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE AT SEAT ROW 3. MAINTENANCE TROUBLESHOT AND REPAIRED A BROKEN WIRE FOR SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 IAW BOEIN G STANDARD WIRING PRACTICES 20-30-12. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002020700060 20020207 00060 NM 2002 2 7 AWXA200200109 1 20020206 A 3350 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM SEAT ROW 23 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 PHX - EEL - "C" - DURING INSPECTION EMEGENCY ESCAPE PATH LIGHTING AT SEAT ROW 23 L/H WAS FOUND INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND WIRES BROKEN AT SEAT ROW 23 L/H, WIRES WERE REPAIRED IAW BOEING STANDARD WIRING PRACTICES 20-30-12 . OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM WAS GOOD. 2 L 7 2 4F RT A16WE 2002020700061 20020207 00061 NM 2002 2 7 AWXA200200110 1 20020207 A 3350 EO261CF20 CABLE AIRBUS A319 A319132 3930340 NM SEAT ROW 10 R/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 PHX - EEL - EMERGENCY ESCAPE PATH EXIT LIGHT WILL NOT ILLUMINATE AT SEAT ROW 10 R/H. MAINTENANCE REMOVED AND REPLACED EM ERGENCY ESCAPE PATH EXIT LIGHT HARNESS AT SEAT ROW 10 R/H IAW ESPM 20-53-20. 2 L 7 2 4F RT A28NM 2002020700062 20020207 00062 NM 2002 2 7 AWXA200200111 1 20020130 A 5330 6545767 SKIN BOEING 737 73733A 1384673 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 LCQ - MAJOR REPAIR - "C" - DURING C-16 CHECK A DENT WAS FOUND IN FUSELAGE SKIN AT FS 365, WL 209 L/H. MAINTENANCE CUTOUT DENTED AREA OF FUSELAGE SKIN AT FS 365, WL 209 L/H; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS FROM CUTOUT; FABRIC ATED A REPAIR DOUBLER AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG. 202, PG. 204-206. 2 L 7 2 4F RT A16WE 2002020700066 20020207 00066 EU 2002 2 7 MALA020135 1 20020118 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU LANDING GEAR DIRTY A MALA K NONE N FALSE WARNING CL CLIMB 1 GL 15 413XJ 340B413 DURING FLIGHT 3289, LANDING GEAR MOTOR IN-TRANSIT LIGHT CONTINUED TO RUN AFTER GEAR WAS SELECTED UP. NO INTERRUPTION IN FLIGHT. MAINTENANCE CLEANED CANNON PLUGS FOR OPERATIONS. RAISED AND LOWERED GEAR SELECT NUMEROUS TIMES, NO DEFECTS NO TED. MAINTENANCE FOUND CANNON PLUGS CONTAMINATED. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002020700067 20020207 00067 EU 2002 2 7 MALA020136 1 20020119 A 3411 PITOT LINE SAAB SF340 340B 7860101 EU PITOT/STATIC SYS CONTAMINATED A MALA K NONE J WARNING INDICATION CR CRUISE 1 GL 15 425XJ 340B425 DURING FLIGHT 2827 INFLIGHT CAPT'S AIRSPEED AND STANDBY AIRSPEED WENT TO ZERO. LANDED IN DTW WITHOUT INCIDENT. MAINTEN ANCE FOUND MOISTURE IN PITOT TRAPS, PURGED SYSTEM. CAPT'S AND STBY ASI OPS CHECK GOOD IAW SF340-MM CHAP 34. 2 L 7 2 4T RT A52EU 2002020700068 20020207 00068 EU 2002 2 7 MALA020138 1 20020123 A 3241 CONTROL BOX SAAB SF340 SF340A 7850100 EU ANTI-SKID SYS FAILED A MALA K NONE O OTHER TX TAXI/GRND HDL 1 GL 15 68XJ 340A068 DURING FLIGHT 2868 BRAKES FAILED BUF, WORKED AFTER PUMP SET TO OVERRIDE. NO INTERRUPTION OF FLIGHT. MAINTENANCE REPLAC ED ANTI-SKID CONTROL BOX PER TECH REP. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2002020700069 20020207 00069 EU 2002 2 7 MALA020141 1 20020129 A 3020 44730501 MODULE SAAB SF340 340B 7860101 EU ANTI-ICE SYS FAILED A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 416XJ 340B416 DURING FLIGHT 3317, RT INTAKE HEAT FAILED, INTAKE HEAT WAS CYCLING ON AND OFF AT ABOUT 14 SECOND INTERVALS. AC DIVERTED TO CWA, BECAUSE OF WEATHER CONDITIONS IN MSP. MAINTENANCE REMOVED AND REPLACED RT DEICE MODULE P/N 44730-501, SN/ON A0 0421, SN/OFF L248464. PERFORMED OPS CHECK OF RT INTAKE HEAT SYSTEM IAW 30-20-00, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002020700076 20020207 00076 EU 2002 2 7 USAASA02001 1 20020101 A 3350 32145510 BATTERY PACK AIRBUS A321 A321211 3930370 EU CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 168US 1447 LGA - FOUND VARIOUS EMERGENCY LIGHT POWER SUPPLIES INDICATING 'EXT LOAD'. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY U NITS. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002020700077 20020207 00077 EU 2002 2 7 USAASA02002 1 20020103 A 3350 321430 BATTERY AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 181UW 1531 LGA - THE EMERGENCY LIGHT SYSTEM TEST SHOWS FAULTS ON THE PROGRAMMING AND TEST PANEL. MAINTENANCE REPLACED EMERGENCY PO WER SUPPLY UNIT BATTERIES. (M) 2 L 7 2 4F RT A28NM 2002020700086 20020207 00086 EU 2002 2 7 MALA020147 1 20020131 A 3210 INTRANSIT LIGHT BAC 146 AVRO146RJ85A 1500097 EU A MALA K NONE J WARNING INDICATION NR NOT REPORTED 1 GL 15 533XJ E2367 During Flight 3410 on Gear retraction both Main Gear Intransit lights remain on. 2 H 7 4 4F RT A49EU 2002020700088 20020207 00088 EU 2002 2 7 QXEA0200091 1 20020202 A 5210 A26000705 DOOR FOKKER F28 F28MK4000 4990810 EU WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 39702 11169 PDX - MAIN CABIN DOOR IS HARD TO OPEN FROM OUTSIDE. REPLACED MAIN CABIN DOOR IAW THE FOKKER MAINTENANCE MANUAL. OPERATIO NAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002020700094 20020207 00094 NM 2002 2 7 USAASB02001 1 20020101 A 3397 WIRE BOEING 737 7374B7 1384702 NM CABIN PINCHED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 445US 24863 PIT - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 12 THROUGH 19, LEFT SIDE, INOPERATIVE. MAINTENAN CE FOUND WIRES FOR SEAT MOUNTED LIGHT AT ROW 14, LEFT SIDE, PINCHED. REPAIRED, INSULATED AND REROUTED WIRES. OPERATION AL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020700095 20020207 00095 SO 2002 2 7 C2XA02CL035 1 20020206 A 4900 4951048 CHECK VALVE EMB 145 EMB145ER 3260211 SO APU STICKING A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 16944 145045 CLE FLIGHT# 4065 THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN WHEN THE APU WAS STARTED.MAINTENANCE REPLACED THE AP U START FUEL CHECK VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002020800004 20020208 00004 NM 2002 2 8 HNAA0200011 1 20020206 A 5400 85410146105 ANGLE DHAV DHC8 DHC8102 2809003 NM CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 936HA 34771 145 #1 NACELLE HORSECOLLAR FRAME FWD ANGLE CRACKED. REPAIRED I.A.W. EO8-54-02-0173. 2 H 7 2 4T RT A13NM 2002020800005 20020208 00005 NM 2002 2 8 HNAA0200012 1 20020207 A 5400 85410146105 ANGLE DHAV DHC8 DHC8102 2809003 NM CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 906HA 44730 9 #1 NACELLE HORSECOLLAR FRAME FWD ANGLE CRACKED. REPAIRED ANGLE I.A.W. EO8-54-02-0177. 2 H 7 2 4T RT A13NM 2002020800007 20020208 00007 NM 2002 2 8 SWAA020280 1 20020205 A 3350 207377 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 603SW 27954 DURING SCHEDULED C3 CHECK, FOUND EEPLS LENS LOOSE AT ROW NR 2. REMOVED AND REPLACED EEPLS LENS PER MM. 2 L 7 2 4F RT A16WE 2002020800008 20020208 00008 NM 2002 2 8 SWAA020283 1 20020205 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 1011, STR 4 L. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2002020800009 20020208 00009 2002 2 8 SWAA020284 4 20020205 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 650SW 27720 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOLDER LOOSE. SECURED GIRT BAR HOLDER PER MM. 2 L 7 2 4F RT A16WE 2002020800010 20020208 00010 NM 2002 2 8 SWAA020285 1 20020205 A 5330 6545807 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002020800011 20020208 00011 NM 2002 2 8 SWAA020286 1 20020206 A 5312 6517583 WEB BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED .75 INCH LONG AT BS 180,WL 177 AND LBL 5.7. REPAIRED WEB P ER SRM. 2 L 7 2 4F A16WE 2002021100048 20020211 00048 NM 2002 2 11 F3LA200200031 1 20020204 A 3610 693866812 DUCT BOEING 737 7373Q8 1384670 NM PNEUMATIC SYS DAMAGED A F3LA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 318FL 2169 26293 AIR TURNBACK. FLIGHT CREW REPORTED RT WING/BODY OVERHEAT LIGHT ILLUMINATED AND AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACARD THE RT PACK INOPERATIVE PER MEL 21-2 AND SUBSEQUENTLY REPLACED DAMAGED DUCT (APPROX 1.5 INCH DIAMETER HOLE WITH CRACKS) UPSTREAM OF THE RT PRIMARY HEAT EXCHANGER. PERFORMED OPERATIONAL TEST AND SYSTEM CHECKED OKAY. 2 L 7 2 4F RT A16WE 2002020800012 20020208 00012 WP 2002 2 8 02FDEA00083 1 20020130 A 2910 1489951 SHUTOFF VALVE DOUG DC10 DC1010CF 3023502 WP HYDRAULIC SYS LEAKING A FDEA J A DUMP FUEL UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 25 056FE 47810 AFTER T/O NR 3 ELEV SHUTOFF VALVE LEAKING FLUID WHEN PRESS. REMOVED AND REPLACED ELEV SHUT OFF VALVE PER MM 29-12-23-2. 2 L 7 3 4F RT A22WE 2002020800013 20020208 00013 NM 2002 2 8 02FDEA00090 1 20020206 A 2910 O-RING BOEING 727 72725C 138400H NM HYDRAULIC SYS DAMAGED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 25 120FE 19356 LOST HYDRAULIC SYS-A QT & PRESS INSTANTLY. REMOVED AND REPLACED O-RING, SERVICED HYD SYS. 2 L 7 3 4F A3WE 2002020800014 20020208 00014 EU 2002 2 8 02FDEA00091 1 20020204 A 3610 CONTROLLER AIRBUS 310 A310222 3930315 EU BLEED AIR SYS MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 420FE 339 ON CLIMBOUT NR 2 BLEED FAULTED. REMOVED AND REPLACED PSC 2. 2 L 7 2 4F RT A35EU 2002020800015 20020208 00015 EU 2002 2 8 02FDEA00092 1 20020207 A 3230 LANDING GEAR AIRBUS 310 A310203 3930313 EU NLG & MLG MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 407FE 254 LANDING GEAR WOULD NOT RETRACT, EITHER SYSTEM. 2 L 7 2 4F RT A35EU 2002020800016 20020208 00016 NM 2002 2 8 200200176 1 20020207 A 5512 SKIN BOEING 747 747212B 1384886 NM HORIZ STAB CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 482EV 20713 LEFT HORIZ STAB UPPER SKIN STA 385 HOIST ATTACH POINT. THIS REPAIR IS ACCOMPLISHED USING AN EXTERNAL DOUBLER REPAIR. T HIS REPAIR IS APPROVED BY THE BOEING COMPANY PER ECRA 482-55-143-2. 2 L 7 4 4F A20WE 2002020800017 20020208 00017 NM 2002 2 8 200200177 1 20020207 A 5320 65B07992109 WEB BOEING 747 747212B 1384886 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 482EV 20713 CANTED WEB (P/N 65B07992-109) CORROSION, BODY STATION 1245, LBL 0.00-21.5. THIS REPAIR TO THE WEB WAS DONE BY TRIMMING OUT THE DAMAGED AREA AND INSTALLING FILLERS AND DOUBLERS PER ECRA 482-53-144-2. 2 L 7 4 4F A20WE 2002020800018 20020208 00018 NM 2002 2 8 200200178 1 20020207 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 482EV 20713 FRAME WEB CRACK, STA 1760 - STR 39L. THE CRACK LENGTH EXTENDS JUST BELOW THE FAILSAFE CHORD. THIS EXCEEDS THE 747 SRM REPAIR LIMITS. REPAIR OF THE FRAME IS ACCOMPLISHED BY USING THE 747 53-10-04 FIGURE 69. REPAIR WITH BOEING SPECIFIED C HANGES. THIS REPAIR IS AN AMOC TO THE FAA AD 86-18-01, PER ECRA 482-53-146-2. 2 L 7 4 4F A20WE 2002020800019 20020208 00019 NM 2002 2 8 200200179 1 20020207 A 5512 SKIN BOEING 747 747212B 1384886 NM HORIZ STAB CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 482EV 20713 LEFT HORIZONTAL STABILIZER UPPER SKIN CORROSION. THE REPAIR IS ACCOMPLISHED BY TRIMMING OUT CORRODED AREA OF SKIN THEN INSTALLING AN EXTERNAL DOUBLER SKIN REPAIR PER ECRA 482-55-148-2. 2 L 7 4 4F A20WE 2002020800020 20020208 00020 NM 2002 2 8 200200180 1 20020207 A 5320 65B07992110 WEB BOEING 747 747212B 1384886 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 482EV 20713 CANTED WEB (65B07992-110) CORROSION, BODY STATION 1245, RBL 0.00 - 33.9. THE REPAIR TO THE WEB TO ENSURE CRACK AND CORR OSION FREE CONDITIONS WAS DONE BY TRIMMING OUT THE DAMAGED AREAS AND INSTALLING FILLERS AND DOUBLERS PER ECRA 482-53-147 -2. 2 L 7 4 4F A20WE 2002020800023 20020208 00023 NM 2002 2 8 ABXA010701 1 20020204 A 3350 S106 BATTERY BOEING 767 767200 1385120 NM COCKPIT DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 790AX 23140 MAINTENANCE FOUND FLIGHT DECK EXIT LIGHT BATTERIES LOW. REPLACED BATTERIES IAW B767 MM 33-51-07. 2 L 7 2 4F RT A1NM 2002020800024 20020208 00024 WP 2002 2 8 ABXA010702 1 20020206 A 3350 TERMINAL DOUG DC9 DC932 3022066 WP CIRCUIT BREAKER LOOSE A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 903AX 47427 EMERGENCY EVACUATION PEANUT LIGHTS CAME ON AFTER ENGINE START AND ON AIRCRAFT POWER. NO ABNORMAL ANNUNCIATOR PANEL INDI CATIONS. FOUND LOOSE TERMINAL AT EMERGENCY LIGHT CIRCUIT BREAKER. TIGHTENED TERMINAL. OPS CHECKED GOOD IAW DC-9 MM 33 -50-00-00. 2 L 7 2 4F A6WE 2002020800025 20020208 00025 WP 2002 2 8 ABXA010703 1 20020206 A 3350 60030451 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 952AX 172 47615 EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED THE EMERGENCY EVACUATION LIGHTS BATTERY PACK IAW DC-9 MM 33-53-02. 2 L 7 2 4F A6WE 2002020800026 20020208 00026 2002 2 8 AWXA200200099 4 20020202 A 3460 FMC AIRBUS A319 A319132 3930340 NM E/E BAY OUT OF ADJUST A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 809AW 1111 BUR - ABORTED TAKEOFF - FLT 0536 - C - DURING TAKEOFF ROLL OUT OF BUR EN ROUTE TO PHX WHEN ADVANCING THROTTLE IN BLUE FL EX TEMPERATURE DROPPED OUT OF FMGC CAUSING THE MASTER CAUTION LIGHT TO ILLUMINATE AT APPROXIMATELY 40-50 KNOTS. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. AIRCRAFT WAS RECONFIGURED AND DEPARTED FOR SCHEDULED DESTINATION. 2 L 7 2 4F RT A28NM 2002021200138 20020212 00138 CE 2002 2 12 GLBA2002015 1 20020131 A 2435 23078019 STARTER GEN BEECH 1900 1900D 1154162 CE RT ENGINE INOPERATIVE A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 118GL 1061 UE118 DC LOAD METERS UNBALANCED 10 PERCENT RIGHT, LEFT 30 PERCENT. REPLACED RIGHT STARTER, GEN OPS CHECKED SYSTEM SATISFACTOR Y. 2 L 7 2 4T RT A24CE 2002020800029 20020208 00029 EU 2002 2 8 MALA020133 1 20020105 A 3620 SENSOR SAAB SF340 340B 7860101 EU PNEUMATIC SYS MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 407XJ 340B407 DURING FLIGHT RIGHT DUCT OVERTEMP CAUTION LIGHT CAME ON CLOSING RT BLEED VALVE. AIR RETURN TO DTW. PERFORMED QRH, TRIE D RESETTING IN BOTH AUTO AND MANUAL MODE BUT OVER TEMP CONTINUED. MAINTENANCE RE-DEFERRED AUTO PER MEL 21-60-2. MAINTE NANCE REPLACED TEMP SENSOR. MAINT CONTROL NOTIFIED VERIFIED OPS CHECK OF MANUAL TEMP CONTROL RT GOOD. 2 L 7 2 4T RT A52EU 2002020800030 20020208 00030 EU 2002 2 8 MALA020143 1 20020130 A 3260 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT ILLUMINATED A MALA K NONE J WARNING INDICATION CL CLIMB 1 GL 15 420XJ 340B420 AFTER TAKEOFF ON FLIGHT 3211, LANDING GEAR SELECTED UP RED INTRANSIT LIGHT REMAINS ON WITH HYDRAULIC PUMP RUNNING. MAIN TENANCE PERFORMED GEAR SWING SEVERAL TIMES, UNABLE TO DUPLICATE DISCREPANCY. GEAR SWING COMPLIED WITH IAW SA340 MM 32-3 0-06-5 PROCEDURE NR 2. 2 L 7 2 4T RT A52EU 2002020800031 20020208 00031 EU 2002 2 8 MALA020144 1 20020131 A 3020 NH24668169 DUCT SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 447XJ 340B447 DURING FLIGHT 2968, LT INTAKE HEAT CYCLES. LT INTAKE LIGHT ILLUMINATES W/MASTER CAUTION THEN EXTINGUISHES AFTER 5-15 SE CONDS. AIR RETURN TO DTW. MAINTENANCE T/S SYSTEM. FOUND CHIPS IN LOWER INTAKE DUCT HEATER MAT. ALL CHECKS GOOD. REM OVED AND REPLACED LT LOWER INLET DUCT ASSEMBLY P/N NH24668-169, SN/ON L169264, SN/OFF L291137. ALL CHECKS GOOD IAW CHAP 30 SF340 MM. 2 L 7 2 4T RT A52EU 2002020800032 20020208 00032 WP 2002 2 8 MWEA020057 1 20020123 A 5320 9923662502 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LONGERON 8 RIGHT, INTERCOSTAL AT STATION 292 HAS A CRACK BY A FASTENER. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002020800033 20020208 00033 WP 2002 2 8 MWEA020058 1 20020123 A 5320 99236693 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 SUBFLOOR REPAIR DOUBLER CRACKED AT STATION 160 AND CENTER OF FLOOR, FWD SIDE OF STATION 160 AS VIEWED FROM BELOW. FABRI CATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002020800034 20020208 00034 WP 2002 2 8 MWEA020060 1 20020123 A 5230 591015777 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 AFT CARGO DOOR INNER PAN HAS LIGHT CORROSION BETWEEN BEAMS NR 1 THROUGH NR 2 (FWD LEFT BOTTOM). MAINTENANCE FOUND CRACK IN LIP OF PAN. FABRICATED AND INSTALLED ANGLE REPAIR. 2 L 7 2 4F A6WE 2002021100049 20020211 00049 NM 2002 2 11 F3LA200200033 1 20020125 A 5320 694147322 INTERCOSTAL BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL CORRODED BETWEEN STA 500A AND 500B, STR 26-R. FABRICATED REPLACEMENT INTERCOSTAL AND INSTALLED PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2002020800035 20020208 00035 2002 2 8 MWEA020062 4 20020125 A 3456 4034240906 CONTROL PANEL DOUG DC9 DC981 3022081 WP COCKPIT DEFECTIVE A MWEA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 812ME 48006 FIRST OFFICERS VHF NAV FREQUENCY SELECT KNOB (BLACK) DOES NOT CHANGE FREQUENCIES AND IS LOOSE (PULLS OUT FROM PANEL). R EMOVED AND REPLACED FIRST OFFICERS NAV CONTROL PANEL IAW 34-32-03. 2 L 7 2 4F A6WE 2002020800036 20020208 00036 WP 2002 2 8 MWEA020063 1 20020130 A 5320 59364692 SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 CORROSION AT AFT CARGO DOOR JAMB CUTOUT AT LOWER FORWARD CORNER. FABRICATED AND INSTALLED CLIP AND SUPPORT. 2 L 7 2 4F A6WE 2002020800037 20020208 00037 WP 2002 2 8 MWEA020064 1 20020131 A 5754 59362843 HORN DOUG DC9 DC981 3022081 WP L/E SLAT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 LEFT INBOARD SLAT HORN HAS SPOT OF CORROSION BY A FASTENER. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002020800038 20020208 00038 WP 2002 2 8 MWEA020065 1 20020131 A 5754 59362843 HORN DOUG DC9 DC981 3022081 WP L/E SLAT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 LEFT INBOARD SLAT HORN HAS CORROSION AROUND SEVERAL FASTENER HOLES THAT ATTACH THE INBOARD GAP SEAL. FABRICATED AND INS TALLED DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2002020800039 20020208 00039 WP 2002 2 8 MWEA020066 1 20020131 A 5754 59362844 HORN DOUG DC9 DC981 3022081 WP L/E SLAT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 RIGHT SLAT HORN HAS SPOTS OF CORROSION BY FASTENERS (INBOARD). FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002020800040 20020208 00040 NE 2002 2 8 NACA20020003 2 20020124 A 7421 RHB32E SPARK PLUG DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 11 CYLINDER CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 2907F 394 533265 P33688 SHUTDOWN THE NR 1 ENGINE DUE TO RAPID CHT CLIMB AND DOUBLE SHORT NR 11 CYLINDER. REPLACED BOTH SPARK PLUGS. 2 L 7 4 4R 4 R A781 5E8 2002020800041 20020208 00041 NM 2002 2 8 P2EA2002M004 1 20020203 A 2612 FIRE DETECTOR BOEING 737 73725A 1384481 NM APU MALFUNCTIONED A P2EA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 CE 05 239TA 23789 PRIOR TO PUSH BACK, APU SHUT DOWN, LATER THE APU FIRE WARNING AND BELL ILLUMINATED. PERFORMED APU FIRE CHECK LIST PROCE DURES PULLED AND ROTATED HANDLE. PERFORMED AN APU FIRE INSPECTION AND FOUND NO EVIDENCE OF FIRE. PLACED THE APU, APU F IRE DETECTION AND THE APU SQUIB LIGHT ON MEL, DEACTIVATING THESE SYSTEMS. OPERATED APU FIRE TEST IN OVERHEAT AND FIRE M ODS NUMEROUS TIMES. APU AND FIRE DETECTION SYSTEM OPERATES NORMAL. 2 L 7 2 4F RT A16WE 2002020800043 20020208 00043 EU 2002 2 8 C2XA02IA 1 20020127 A 2422 559012A INVERTER AEROSP ATR42 ATR42320 8680930 EU FAILED A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 18814 103 IAH - FLT 3821 - Crew reported a burning smell and #1 inverter fault. Maintenance reset the #1 inverter, but could not d uplicate smoke smell in cockpit. Item re-occurred on next flt 3646 with same discrepancy. Maintenance removed and replac ed the #1 inverter. An operational check was performed and the aircraft was returned to service. 2 H 7 2 4T RT A53EU 2002021100029 20020211 00029 EU 2002 2 11 C2XA02IA020 1 20020203 A 2422 559012A INVERTER AEROSP ATR42 ATR42320 8680930 EU NR 1 FAILED A C2XA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION UK UNKNOWN 1 SW 27 18814 103 IAH - FLT 3821 - CREW REPORTED A BURNING SMELL AND NR 1 INVERTER FAULT. MAINTENANCE RESET THE NR 1 INVERTER, BUT COULD NOT DUPLICATE SMOKE SMELL IN COCKPIT. ITEM REOCCURRED ON NEXT FLT 3646 WITH SAME DISCREPANCY. MAINTENANCE REMOVED AND REPLACED THE NR 1 INVERTER. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2002020800044 20020208 00044 NM 2002 2 8 P5CA0200637 1 20020128 A 3350 S1356B37 LIGHT BOEING 747 747283B 1384867 NM CABIN INOPERATIVE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 921FT 21575 DURING A-CHECK FOUND MAIN CEILING EMERGENCY LIGHT INOP STATION 500. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM 33 -51-07. OPS CHECKED SATISFACTORY. 2 L 7 4 4F A20WE 2002020800045 20020208 00045 NE 2002 2 8 P5CA0200638 2 20020201 A 7230 COMPRESSOR BOEING 747 747122 1384872 NM PWA JT9 JT9D7 52054 NE NR 3 ENGINE FAILED A P5CA E A ENGINE SHUTDOWN UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 23 852FT 19757 685859 WHILE CLIMBING, NR 3 FAILED WITH LOUD BANG AND VIBRATION. EPR DECREASED RAPIDLY AND EGT INCREASED TO APPROX 910. PERFO RMED ENG FIRE/SEVERE DAMAGE CHECKLIST. SECURED ENGINE WITH ENGINE SHUTDOWN CHECKLIST. EMERGENCY DECLARED; DIVERTED TO SIN - CHANGI AIRPORT. APPARENT CAUSE OF FAILURE IS 8TH STAGE COMPRESSOR DAMAGE. 2 L 7 4 4F 4 F A20WE E20EA 2002020800046 20020208 00046 NM 2002 2 8 P5CA0200639 1 20020203 A 5230 LATCH BOEING 747 7472U3B 1384846 NM CARGO DOOR UNLOCKED A P5CA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 23 923FT 22769 AFTER TAKEOFF, MAIN DECK SIDE CARGO DOOR LIGHT ILLUMINATED. EMERGENCY DECLARED. 180,000 LBS OF FUEL WAS JETTISONED AND PRECAUTIONARY RETURN TO ICN WAS COMPLETED. WARNING LIGHTS REMAINED ILLUMINATED AT BLOCK IN. UPON INSPECTION, FOUND LA TCH IN THE UNLOCKED POSITION. INSIDE AND OUTSIDE MAIN DECK SIDE DOOR LATCH CHECKED NORMAL PER MM 52-71-00 PG 508. DOOR WARNING LIGHT SYS CHECK OK. 2 L 7 4 4F RT A20WE 2002020800047 20020208 00047 NM 2002 2 8 QXEA0200086 1 20020202 A 5270 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR STICKING A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 400QX 4030 EN ROUTE, AIRCRAFT WOULD NOT PRESSURIZE AND ALSO HAD A FWD CARGO DOOR CAUTION LIGHT. AIRCRAFT DIVERTED TO BOISE. MAINT ENANCE FOUND THE FORWARD CARGO DOOR PROXIMITY SENSOR STICKING. CLEANED AND LUBED SENSOR. OPERATIONAL CHECK IS GOOD. A IRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002020800048 20020208 00048 EA 2002 2 8 QXEA0200087 1 20020130 A 2612 474073 FIRE LOOP CNDAIR CL600 CL6002C10 1390015 EA RT ENGINE SHORTED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 610QX 63 10033 PDX - CREW RECEIVED A FIRE SYSTEM FAULT MESSAGE. MAINTENANCE FOUND A SHORT ON THE INBOARD LOOP OF THE RIGHT ENGINE. RE PLACED FIRE DETECTION RAIL ASSEMBLY. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002020800049 20020208 00049 NM 2002 2 8 QXEA0200088 1 20020128 A 5210 GUIDE DHAV DHC8 DHC8202 2809007 NM PAX DOOR DEFECTIVE A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 375PH 529 SEA - MAIN CABIN DOOR NEARLY IMPOSSIBLE TO OPEN. REPLACED PASSENGER DOOR HANDLE GUIDE STOP. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002020800050 20020208 00050 EA 2002 2 8 QXEA0200089 1 20020201 A 5210 STRIKER CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - THE FORWARD AND REAR MAIN CABIN DOOR STRIKERS ARE DENTED. REPAIRED DAMAGE AREAS IAW EA R-53-13 BY BLENDING AND PE RFORMING HFEC INSPECTION. 2 L 7 2 4F RT A21EA 2002020800051 20020208 00051 NM 2002 2 8 QXEA0200090 1 20020203 A 2620 SWITCH BOMBDR DHC8 DHC8401 NM EXTINGUISH SYS INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 412QX 4059 BOI - THE FORWARD FIRE BOTTLE DOES NOT ILLUMINATE ON TEST. TROUBLESHOT TO THE FORWARD HIGH PRESSURE BOTTLE PRESSURE SWI TCH. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002021100051 20020211 00051 NM 2002 2 11 F3LA200200035 1 20020125 A 5320 694147322 INTERCOSTAL BOEING 737 737228 13844AG NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT STA 440, STR 26-L. FABRICATED AND INSTALLED REPLACEMENT IN TERCOSTAL PER SRM 51-30-1. 2 L 7 2 4F RT A16WE 2002021100052 20020211 00052 NM 2002 2 11 F3LA200200036 1 20020125 A 5210 65C1612112 BRACKET BOEING 737 737228 13844AG NM L1 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED L-1 DOOR AFT GIRT BAR ATTACH BRACKET CORRODED. FABRICATED AND INSTALLED REPLACEME NT BRACKET PER BOWING DRAWING 65C16121. 2 L 7 2 4F RT A16WE 2002020800070 20020208 00070 NM 2002 2 8 USAASB02002 1 20020103 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 437US 24559 BWI - MAINTENANCE FOUND THE LAST TWO ROWS OF SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE BATTERY PACK CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020800071 20020208 00071 NM 2002 2 8 USAASB02004 1 20020106 A 3350 20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 415US 23883 PIT - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHT DIMS DURING OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM. MAI NTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY ASSEMBLY PER MM 33-50-04. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002020800072 20020208 00072 NE 2002 2 8 USAASB02006 2 20020108 A 7320 PMC BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING R F PARTIAL RPM/PWR LOSS FLT CONT AFFECTED CL CLIMB 1 EA 19 783AU 25022 722279 FLT 1276 - CLIMBOUT FROM RSW, PASSING 15,000 FEET, THE NR 2 ENGINE RPM ROLLED BACK ABOUT 5 PERCENT THEN RETURNED TO NORM AL. CREW DISENGAGED THE AUTOTHROTTLES BUT THROTTLE FLUCTUATIONS CONTINUED WITH GAINS AND LOSSES OF PLUS AND MINUS 5 PER CENT TO 10 PERCENT. AIRCRAFT YAWED AT THE SAME TIME. FLT DIVERTED AND LANDED WITHOUT INCIDENT. ENGINE PERFORMANCE APP EARED NORMAL ON APPROACH AND LANDING. NO EMERGENCY WAS DECLARED. MX RAN ENGINES AND FOUND MINOR FLUCTUATIONS WITH PMC' S ON. WITH PMC'S OFF, RT ENGINE STABILIZED. PERFORMED PMC CHECK WITH TESTER, TESTS PASSED. PERFORMED POWER ASSURANCE CHECK, SYSTEM CHECK NORMAL. COULD NOT DUPLICATE FAULT. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2002020800086 20020208 00086 NM 2002 2 8 AALA20020001 1 20020105 A 2913 849589 PUMP BOEING 737 737823 13844BZ NM NR 1 ENGINE LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 944AN 29535 SFO - FLT 1593 - EN ROUTE YUL-ORD, DURING CRUISE DETECTED HYDRAULIC PRESSURE DECREASE TO ZERO. LANDED SFO AND LANDED WI THOUT FURTHER INCIDENT. REPLACED LEFT HYDRAULIC PUMP. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2002020800087 20020208 00087 EU 2002 2 8 AALA20020005 1 20020110 A 2150 22058205 ACM FOKKER F28 F28MK0100 4990807 EU A/C BAY MALFUNCTIONED A AALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 1436A 11426 MSP - FLT 1482 - EN ROUTE MSP-ORD, SHORTLY BEFORE TAKEOFF DETECTED SMOKE IN COCKPIT. RETURNED MSP GATE WITHOUT FURTHER INCIDENT. REPLACED AIR CYCLE MACHINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002020800088 20020208 00088 NM 2002 2 8 AALA20020006 1 20020110 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 25 A/B INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHT CONNECTO R AT SEAT 25 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002020800089 20020208 00089 WP 2002 2 8 AALA20020007 1 20020110 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP R1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 403A 49314 PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002020800090 20020208 00090 WP 2002 2 8 AALA20020008 1 20020105 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 293AA 49305 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002020800091 20020208 00091 WP 2002 2 8 AALA20020009 1 20020106 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 291AA 49303 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRES AT SIDE WALL. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002020800092 20020208 00092 WP 2002 2 8 MWEA020114 1 20020206 A 5410 995815432 ANGLE DOUG DC9 DC932 3022066 WP RIGHT PYLON OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 RIGHT PYLON AFT SPAR ANGLE HAS OVERSIZE HOLE. -- FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2002020800093 20020208 00093 WP 2002 2 8 MWEA020115 1 20020206 A 5410 995815413 ANGLE DOUG DC9 DC932 3022066 WP RIGHT PYLON OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 RIGHT PYLON AFT SPAR UPPER ANGLE HAS OVERSIZE HOLES. -- FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2002020800094 20020208 00094 WP 2002 2 8 MWEA020117 1 20020206 A 5310 49191472 FITTING DOUG DC9 DC932 3022066 WP STATION 1038 OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 REMOVED FITTING THAT ATTACHES TO UPPER WEB AT FUSELAGE STATION 1038 LONGERON 15 RIGHT DUE TO OVERSIZED HOLES. -- FABRI CATED AND INSTALLED FITTING. 2 L 7 2 4F A6WE 2002020800095 20020208 00095 WP 2002 2 8 MWEA020118 1 20020206 A 5410 995815434 ANGLE DOUG DC9 DC932 3022066 WP RIGHT PYLON OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 RIGHT SPAR AFT UPPER ANGLE HAS OVERSIZED HOLES. -- FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2002020800096 20020208 00096 WP 2002 2 8 MWEA020119 1 20020206 A 5410 49198642 FITTING DOUG DC9 DC932 3022066 WP RIGHT PYLON OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 RIGHT PYLON FITTING HAS OVERSIZE HOLE. -- FABRICATED AND INSTALLED FITTING AND RADIUS BLOCKS. 2 L 7 2 4F A6WE 2002020800097 20020208 00097 WP 2002 2 8 MWEA020120 1 20020206 A 5410 995815412 ANGLE DOUG DC9 DC932 3022066 WP RIGHT PYLON OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 RIGHT PYLON AFT SPAR ANGLE HAS OVERSIZED FASTENER H0LE. -- FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2002020800098 20020208 00098 WP 2002 2 8 MWEA020123 1 20020206 A 5310 9958154 WEB DOUG DC9 DC932 3022066 WP STATION 1038 OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 REMOVED SECTION OF WEB AT STATION 1038 BETWEEN LONGERON 14 RIGHT AND 17 RIGHT. SPAR STRAP HOLES OVERSIZED. -- FABRICAT ED AND INSTALLED WEB SECTION AND WEB SPLICES. 2 L 7 2 4F A6WE 2002020800099 20020208 00099 WP 2002 2 8 MWEA020124 1 20020206 A 5310 9912246 WEB DOUG DC9 DC932 3022066 WP STATION 1038 OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 WEB AT 15 RIGHT BETWEEN STATION 1038 AND 1059 HAS OVERSIZED HOLES. -- FABRICATED AND INSTALLED SPLICE ANGLE. 2 L 7 2 4F A6WE 2002020800100 20020208 00100 2002 2 8 RAIA00202046 4 20020201 A 3420 7003360948 INDICATOR JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 565HK 3848 5 97093886 41082 5516-STL-BOTH AHRS FAILED DURING CLIMB. MAINTENANCE REMOVED AND REPLACED #1 AND #2 AHRS 2 L 7 2 4T RT A41NM 2002020800101 20020208 00101 NE 2002 2 8 RAIA00202048 2 20020206 A 7314 31057809 PUMP JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE FAILED A RAIA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 CE 03 560HK 11039 5074 41076 75090 5538-STL- LEFT ENGINE FAILED DURING CLIMB. MAINTENANCE REMOVED AND REPLACED THE #1 ENGINE FUEL PUMP, ENGINE AND PUMP OPS AND LK CK OK. 2 L 7 2 4T 4 T RT A41NM E18NE 2002021100003 20020211 00003 NM 2002 2 11 HNAA0200013 1 20020119 A 5310 853110031 SKIN PANEL DHAV DHC8 DHC8102 2809003 NM BOTTOM FUSELAGE CORRODED A HNAA O OTHER O OTHER IN INSP/MAINT 1 EA 07 927HA 35439 117 Skin corroded and cracked at station x182 and stringer 33. Replaced skin panel. 2 H 7 2 4T RT A13NM 2002021100014 20020211 00014 NM 2002 2 11 OZIA200243001 1 20020130 A 3260 7144002 PSEU DORNER DO32 DO328300 NM FAILED A OZIA A UNSCHED LANDING J G WARNING INDICATION MULTIPLE FAILURE CL CLIMB 1 CE 05 430Z 1377 3127 After takeoff, Pilot had multiple warning indications, "takeoff config, landing gear warning horn". Pilot elected to ret urn to airport. When elected to extend landing gear, the gear did not come down. Pilot used emergency landing gear exten sion procedures to land. After landing, maintenance found proximity switch unit and landing gear switch had failed. Remo ved and replaced proximity switch and gear switch. Performed retract checks and returned to service.Reference SDR Contro l #OZIA200243002 for Landing Gear Switch part information. 2 H 7 2 4T RT A55NM 2002021100020 20020211 00020 WP 2002 2 11 ABXA010704 1 20020206 A 3350 LIGHT DOUG DC9 DC932 3022066 WP COCKPIT LOOSE A ABXA K NONE O OTHER TO TAKEOFF 1 GL 23 903AX 47427 EMERGENCY EVACUATION LIGHTS FLICKER OCCASIONALLY DURING TAKEOFF ROLL AND LANDING ROLLOUT. FOUND THE CAPTAIN'S SIDE LAMP LOOSE. ADJUSTED/CLEANED THE CONTACTS AND REPLACED LAMPS. 2 L 7 2 4F A6WE 2002021100021 20020211 00021 NM 2002 2 11 OZIA200243002 1 20020130 A 3260 7178011 LEVER DORNER DO32 DO328300 NM FAILED A OZIA A UNSCHED LANDING J G WARNING INDICATION MULTIPLE FAILURE CL CLIMB 1 CE 05 430Z 3863 3127 After takeoff, Pilot had multiple warning indications, "takeoff config, landing gear warning horn". Pilot elected to ret urn to airport. When elected to extend landing gear, the gear did not come down. Pilot used emergency landing gear exten sion procedures to land. After landing, maintenance found proximity switch unit and landing gear switch had failed. Remo ved and replaced proximity switch and gear switch. Performed retract checks and returned to service.Reference SDR Contro l #OZIA200243001 for PSEU part information. 2 H 7 2 4T RT A55NM 2002021200111 20020212 00111 WP 2002 2 12 AT0200006 1 20020206 A 4920 38025611 APU DOUG DC9 DC932 3022066 WP APU BAY FAULTY A ZZDA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 15 847AT 47555 BOTH AFT LAVATORY SMOKE DETECTORS GOING OFF, OILY SMOKEY SMELL IN CABIN. REMOVED AND REPLACED AUXILIARY POWER UNIT. 2 L 7 2 4F A6WE 2002021100023 20020211 00023 EU 2002 2 11 AWXA200200098 1 20020203 A 4930 38828354 FLOW DIVIDER AIRBUS 320 A320232 3930326 EU APU LEAKING A AWXA K NONE K A FLUID LOSS FLAME/FIRE TX TAXI/GRND HDL 1 WP 28 657AW 5149 1083 CMH - APU TAILPIPE FIRE - S - WHILE AIRCRAFT WAS ON GROUND FOR RON AT CMH AUXILIARY POWER UNIT WAS PREMATURELY SHUTDOWN AND FLAMES WERE REPORTED COMING FROM THE TAILPIPE AREA, THERE WERE NO FIRE WARNINGS, EGT PROBLEMS, OR ECAM MESSAGES. MA INTENANCE PERFORMED A VISUAL INSPECTION OF THE APU COMPARTMENT, APU INLET, AND APU EXHAUST AREAS WITH NO ABNORMALITIES N OTED. SYSTEM WAS PLACED ON MEL. PHX MAINTENANCE TROUBLESHOT THE APU PER TSM 49-00-00-810-817, AND PERFORMED AN OPERATI ONAL TEST IAW AMM TASK 49-00-00-710-004; FUEL WAS OBSERVED DRIPPING FROM THE DRAIN MAST AND A FUEL FLOW DIVIDER WAS REPL ACED TO CORRECT THIS PROBLEM; OPERATIONAL TEST WAS REACCOMPLISHED AND CHECKED GOOD. 2 L 7 2 4F RT A28NM 2002041700125 20020417 00125 EU 2002 4 17 AWXA200200112 2 20020207 A 7200 ENGINE BOEING 737 7373S3 1384711 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 MALFUNCTIONED A AWXA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 WP 28 314AW 27655 23733 725146 ONT - DIVERSION - FLT 809 - EN ROUTE FROM PHX TO SFO AND AT CRUISING ALTITUDE A NR 2 ENGINE ROLLBACK OCCURRED. THE FLIG HT CREW DECLARED AN EMERGENCY AND THE AIRCRAFT DIVERTED TO ONT. AT FL 200 THE NR 2 ENGINE WAS RESTARTED AND OPERATED NO RMALLY FROM THIS TIME ON. THE EMERGENCY WAS CANCELED AND THE AIRCRAFT LANDED SAFELY AT ONT. MAIN ENGINE CONTROL S/N WY G35471 WAS NO FAULT FOUND BY VENDOR BENCH TEST. MAIN ENGINE FUEL PUMP, P/N 708600-5, S/N 17559 ALSO WAS NO FAULT FOUND BY VENDOR BENCH TEST, 4 EACH O-RINGS AND THE FUEL FILTER ELEMENT WERE REPLACED PRIOR TO RETURNING THE UNIT TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2002021100025 20020211 00025 SO 2002 2 11 C2XA02CL033 1 20020206 A 2120 ODOR EMB 145 EMB145LR 3260212 SO COCKPIT DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13955 145075 CLE FLIGHT 3260 THE CREW REPORTED A STRONG FUEL SMELL IN COCKPIT AFTER STARTING THE APU. MAINTENANCE INSPECTED AND PERF ORMED OPERATIONAL CHECKS OF THE APU. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002021100027 20020211 00027 SO 2002 2 11 C2XA02CL034 1 20020206 A 3350 602024 SIGN EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 17507 145215 CLE FLIGHT 3144 THE CREW REPORTED THE EXIT SIGN IN THE FORWARD CABIN DID NOT ILLUMINATE. MAINTENANCE REPLACED THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002021100031 20020211 00031 EU 2002 2 11 C2XA02IA021 1 20020207 A 3260 D228830001 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU NLG FAILED A C2XA K NONE N FALSE WARNING AP APPROACH 1 SW 27 97841 280 DURING APPROACH FLIGHT 3762, THE CREW NOTED THAT THE NOSE LANDING GEAR UNSAFE DOWNLOCK INDICATION IN FLIGHT ON THE FORWA RD PANEL, THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL. MAIN TENANCE REMOVED AND REPLACED THE LEFT AND RIGHT DOWNLOCK PROX SWITCHES. PERFORMED A OPERATIONAL CHECK OF THE LANDING GE AR SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002021100032 20020211 00032 EU 2002 2 11 C2XA02IA022 1 20020207 A 3260 D228830001 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU NLG FAILED A C2XA K NONE N FALSE WARNING AP APPROACH 1 SW 27 97841 280 DURING APPROACH FLIGHT 3762, THE CREW NOTED THAT THE NOSE LANDING GEAR UNSAFE DOWNLOCK INDICATION IN FLIGHT ON THE FORWA RD PANEL, THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL. MAINT ENANCE REMOVED AND REPLACED THE LEFT AND RIGHT DOWN LOCK PROX SWITCHES. PERFORMED A OPERATIONAL CHECK OF THE LANDING GE AR SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002021100034 20020211 00034 SO 2002 2 11 C2XA02TY025 1 20020206 A 5210 13533677401 BUSHING EMB 145 EMB145ER 3260211 SO PAX DOOR OUT OF POSITION A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 TYS, DURING A SCHEDULED 1C INSPECTION, THE MAIN CABIN DOOR HOLD OPEN LATCH BUSHING MIGRATING. MAINTENANCE REINSTALLED B USHING IAW-EMB-GST-1682/01, REPAIR PROCEDURES ARE SATISFACTORY AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTI ON. 2 L 7 2 4F RT T00011AT 2002021100036 20020211 00036 SO 2002 2 11 CHQ000113 1 20020207 A 2760 CONTROL UNIT EMB 145 EMB145 3260210 SO SPOILER FAILED A CHQA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 11 293 145500 SPOILER FAIL MESSAGE, E-2 REVERSER DISAGREE MESSAGE. REMOVED AND REPLACED BRAKE CONTROL UNIT AND OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2002021100041 20020211 00041 SO 2002 2 11 CHQ00097 1 20020120 A 2460 ELECTRICAL BOX EMB 145 EMB145 3260210 SO COCKPIT SHORTED A CHQA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 11 265SK 145226 PILOT REPORTS SMOKE IN COCKPIT FROM F/O'S RELAY BOX. 2 L 7 2 4F RT T00011AT 2002021100042 20020211 00042 SO 2002 2 11 CHQ00098 1 20020120 A 2460 ELECTRICAL BOX EMB 145 EMB145 3260210 SO COCKPIT SHORTED A CHQA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 11 265SK 145226 PILOT REPORTS SMOKE IN COCKPIT FROM F/O'S RELAY BOX. 2 L 7 2 4F RT T00011AT 2002021100043 20020211 00043 NM 2002 2 11 DHL2002724002 1 20020207 A 3310 PRINTED CKT BOAR BOEING 727 727228 1384083 NM COCKPIT MELTED A DHLA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 724DH 19862 DIMMING BOARD CIRCUIT DIRECTLY BEHIND AND BELOW GPS COMPUTER MELTED AND BURNT, CONNECTOR AT BOARD ALSO MELTED. REMOVED AND REPLACED PRINTED CIRCUIT CARD IAW B-727 M/M 33-15-11, OPERATIONAL CHECK SERVICEABLE. ALSO REPLACED CONNECTOR IAW B- 727 SWP 20-11-44. 2 L 7 3 4F RT A3WE 2002021100045 20020211 00045 WP 2002 2 11 DHL2002806002 1 20020208 A 3260 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT FAULTY A DHLA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 806DH 46002 RT MAIN GEAR DOWN GREEN LIGHT FAILS TO ILLUMINATE UNTIL A GO AROUND IUS ACCOMPLISHED AND REPEATED CYCLING OF THE GEAR. INSPECTED INDICATING GEAR DOWN AND FOUND FAULTY LAMP. RELAMPED AND OPS CHECK GOOD IAW 33-10-0. 2 L 7 4 4F RT 4A25 2002021100046 20020211 00046 NM 2002 2 11 HNAA0200018 1 20020206 A 2920 SM601BA20A1 CIRCUIT BREAKER DHAV DHC8 DHC8102 2809003 NM #1 NACELLE INOPERATIVE A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 938HA 152 While taxing to gate lost #1 standby hydraulic pump, lost toe brakes. Replaced RCCB, ops check good. 2 H 7 2 4T RT A13NM 2002021100047 20020211 00047 WP 2002 2 11 DJFA20020208 2 20020123 A 7200 ENGINE CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7313A 01518 WP NR 2 FAILED E DJFA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 EA 23 381CW 6500111 P87200C DURING DESCENT, THE AIRCRAFT SHOOK FOLLOWED BY A NR 2 ENGINE CHIP DETECTOR LIGHT ILLUMINATION. ENGINE WAS SHUT DOWN AND AN UNEVENTFUL LANDING WAS MADE. UPON VISUAL EXAMINATION, THERE WERE NO EXTERNAL OIL LEAKS, THE OIL RESERVOIR WAS FOUND FULL AND THE FAN WAS NOT ABLE TO BE TURNED BY HAND. THERE WAS NO VISIBLE SIGNS OF DAMAGE TO THE FAN. 2 L 7 2 4F 4 F A9NM E6WE 2002021100050 20020211 00050 NM 2002 2 11 F3LA200200034 1 20020125 A 5320 6545833153 FLOOR SUPPORT BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED FLOOR SUPPORT ANGLE CORRODED AT COCKPIT ENTRY AT STA 277. REPLACED FLOOR SUPPORT ANGLE PER EO 52-50-737-004. 2 L 7 2 4F RT A16WE 2002021100053 20020211 00053 NM 2002 2 11 F3LA200200037 1 20020125 A 5753 657192662 WEDGE BOEING 737 737228 13844AG NM T/E FLAP DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 2774 23007 DURING C-7 CHECK, INSPECTION REPORTED RT INBOARD HINGE FLAP DELAMINATED ON TRAILING EDGE. REPLACED RT INBOARD TRAILING EDGE OF HINGE FLAP PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 2002021100055 20020211 00055 EU 2002 2 11 MALA020148 1 20020131 A 3020 THERMISTER SAAB SF340 340B 7860101 EU INTAKE HEAT FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 447XJ 340B447 DURING FLIGHT 2968 LT ENGINE INTAKE HEAT (LT INTAKE) LIGHT CYCLES ABOUT EVERY 30 SECONDS TO A MINUTE IN FLIGHT. AS FLIG HT PROGRESSED LIGHT CAME ON EVERY 5 MINUTES. AIR RETURN TO DTW. MAINTENANCE CHECKED RES OF DUCTS, ALL GOOD, CHECKED R ES AT THERMISTOR FOUND J1 HIGH. SWAPPED J1 WITH J5. OPS CHECK GOOD IAW SF340 MM 3020. 2 L 7 2 4T RT A52EU 2002021100056 20020211 00056 EU 2002 2 11 MALA020149 1 20020201 A 7810 NC24668274 NOZZLE SAAB SF340 340B 7860101 EU LT ENGINE DEFECTIVE A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 447XJ 340B447 DURING CLIMBOUT OF FLIGHT 3102, LT INTAKE CYCLES, COMPLETED QRH. AIR RETURN TO DTW. MAINTENANCE FOUND CHAFED WIRE ON E XHAUST NOZZLE, INSTALLED SERVICEABLE EXHAUST NOZZLE P/N NC24668-274, S/N ON L290958, S/N OFF L291489. ALL CHECKS GOOD I AW 71-60-10. ALSO REPLACED AC GEN P/N 31342-003, S/N ON 496, S/N OFF Y0001, ALTHOUGH GEN WAS NO HELP. 2 L 7 2 4T RT A52EU 2002021100057 20020211 00057 EU 2002 2 11 MALA020150 1 20020203 A 5240 SERVICE DOOR SAAB SF340 340B 7860101 EU FUSELAGE OPEN A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 417XJ 340B417 DURING FLIGHT NR 3116, LOUD THUMPING NOISE HEARD INFLIGHT SHORTLY AFTER TAKEOFF. AIR RETURN TO DTW. FOUND LAV SERVICE DOOR OPEN, INSPECTED AREA AND NO DAMAGE NOTED. RESECURED DOOR, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2002021100058 20020211 00058 EU 2002 2 11 MALA020151 1 20020205 A 7931 TRANSDUCER SAAB SF340 340B 7860101 EU RT ENGINE FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 410XJ 340B410 DURING FLIGHT 2771, RT OIL PRESSURE DROPPED INTO RED AND GOT WARNING LIGHT. CREW DID NOT HAVE TO SHUTDOWN ENGINE ON FIN AL WITH ENGINE OIL PRESSURE IN RED. AIR RETURN TO CMI. MAINTENANCE REPLACED THE OIL PRESS TRANSDUCER. 2 L 7 2 4T RT A52EU 2002021100059 20020211 00059 WP 2002 2 11 MWEA020116 1 20020206 A 5411 995815421 SPAR DOUG DC9 DC932 3022066 WP RT PYLON DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 RIGHT PYLON AFT SPAR WEB UPPER HOLES OVERSIZED. FABRICATED AND INSTALLED SPAR WEB. 2 L 7 2 4F A6WE 2002021100060 20020211 00060 WP 2002 2 11 MWEA020121 1 20020206 A 5311 9912246103 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 AT STATION 1038, LONGERON 15 RIGHT INNER, OUTER FRAME CAP AND SHEAR TIE HAS 5 OVERSIZED HOLES. FABRICATED AND INSTALLED REPAIR BUSHINGS AND BUSHING RETAINING STRAPS. 2 L 7 2 4F A6WE 2002021100061 20020211 00061 NM 2002 2 11 P5CA0200640 1 20020207 A 2760 SWITCH BOEING 747 747249F 1384849 NM SPEED BRAKE OUT OF ADJUST A P5CA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 23 920FT 22237 TAKEOFF WARNING HORN WHEN POWER IS ADVANCED. ADJUSTED SPEED BRAKE DOWN SWITCH IAW 31-26-05. OPS CHECK NORMAL. 2 L 7 4 4F A20WE 2002021100062 20020211 00062 NM 2002 2 11 P5CA0200641 1 20020206 A 5321 FLOOR PANEL BOEING 747 74746NF 13848BT NM FUSELAGE PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 452PA 30810 MAIN DECK, STA 1920/2040 LEFT SIDE FLOOR PANEL DAMAGED (PUNCTURES). REMOVED AND REPLACED PER MM 53-00-50. 2 L 7 4 4F RT A20WE 2002021100063 20020211 00063 NM 2002 2 11 P5CA0200642 1 20020206 A 2550 GUIDE BOEING 747 74746NF 13848BT NM CARGO BAY DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 452PA 30810 AFT CARGO COMPT, STA 1820 SIDE GUIDE RAIL DAMAGED LT/SIDE. REPAIRED PER SRM 51-70-12 & MM 25-33-00. 2 L 7 4 4F RT A20WE 2002021100064 20020211 00064 NM 2002 2 11 P5CA0200643 1 20020206 A 2550 MC15562 LOCK BOEING 747 74746NF 13848BT NM CARGO BAY DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 452PA 30810 FWD CARGO COMPT AT STA 650 LOCK ASSY DAMAGED LEFT SIDE. REMOVED AND REPLACED PER MM 25-56-33. 2 L 7 4 4F RT A20WE 2002021100065 20020211 00065 NM 2002 2 11 P5CA0200645 1 20020207 A 5321 FLOORBOARD BOEING 747 74746NF 13848BT NM FUSELAGE PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 452PA 30810 MAIN DECK L/S FLOOR BOARD PUNCTURE BS 1720 LT SIDE. REPAIRED PER SRM 53-00-50. 2 L 7 4 4F RT A20WE 2002021100066 20020211 00066 NM 2002 2 11 P5CA0200646 1 20020207 A 5753 FAIRING BOEING 747 74746NF 13848BT NM T/E FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 452PA 30810 NR 7 CANOE ASSY, OUTBOARD SIDE AT MID POINT 2 INCH DELAMINATION. REPAIRED PER SRM 51-40-00. 2 L 7 4 4F RT A20WE 2002021100067 20020211 00067 NM 2002 2 11 PCAA0202027 1 20020207 A 3060 BRUSH BLOCK DHAV DHC8 DHC8102 2809003 NM RT PROPELLER DIRTY A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 814EX 318 BOS-FLIGHT 3937 CREW REPORTED EMERGENCY LIGHTS CYCLE ON AND OFF INTERMITTENTLY IN FLIGHT. MAINTENANCE CLEANED THE RIGHT PROPELLER BRUSH BLOCK, RAN AIRCRAFT AND FOUND NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002021100069 20020211 00069 NM 2002 2 11 SABA020016 1 20020204 A 3397 WIRE DHAV DHC8 DHC8103 1386005 NM CABIN BROKEN A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 801WP 086 AIRCRAFT 801 ON FLIGHT 5019 FROM CLT TO AGS. DURING PREFLIGHT THE LEFT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATI VE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE LIGHT ASSEMBLY. SYSTEM OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002021100071 20020211 00071 NM 2002 2 11 SWAA020182 1 20020125 A 3350 65C27093 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD SERVICE AND AFT ENTRYWAYS. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2002021100073 20020211 00073 NM 2002 2 11 SWAA020183 1 20020122 A 3350 6556633 LIGHT BOEING 737 7373L9 1384470 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 657SW 23331 DURING SCHEDULED C1 CHECK, FOUND CENTER CABIN CEILING EMERGENCY EXIT LIGHT INOP. RECONNECTED WIRING AND OPS CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 2002021100083 20020211 00083 NM 2002 2 11 CALA0200065 1 20020207 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 727B CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND A 1/2" CRACK IN R/H O/B SEAT TRACK AT STA 727B, RBL 45.57. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5321 -01123. 2 L 7 2 4F RT A16WE 2002021100084 20020211 00084 NM 2002 2 11 CALA0200067 1 20020208 A 5230 WEB BOEING 737 7373T0 1384582 NM C-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14320 23371 INSPECTION FOUND A 0.137" CRACK IN INTERIOR WEB AT HANDLE CUTOUT OF AFT BAGGAGE BIN DOOR. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01015. 2 L 7 2 4F RT A16WE 2002021100085 20020211 00085 NM 2002 2 11 SABA020018 1 20020208 A 3350 1013075 BULB DHAV DHC8 DHC8102 2809003 NM CABIN BURNED OUT A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 841PH 082 Aircraft 841 on flight 5027 from CLT to CVG. During preflight inspection the emergency floor lights had one bulb inop. No emergency procedures were involved. Maintenance removed and replaced the bulb. System ops checked good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002021100086 20020211 00086 EA 2002 2 11 COMA0260086 1 20020204 A 5300 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SO 01 427CA 7460 FLIGHT 9461 BIRDSTRIKE ON NOSE OF AIRCRAFT DURING T/O.C/W BIRDSTRIKE INSP - NO DAMAGE FOUND. 2 L 7 2 4F RT A21EA 2002021100087 20020211 00087 EA 2002 2 11 COMA0260087 1 20020128 A 2897 2261152 FUEL TANK CNDAIR CL600 CL6002B19 1900309 EA L/H DAMAGED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 918CA 19724 7018 WHEN L/H BOOST PUMP CANISTER WAS REMOVED FOR REPAIR, FOUND THE WIRING INSULATION PULLED BACK AND WIRE CONDUCTORS EXPOSED .REPLACED CANISTER. 2 L 7 2 4F RT A21EA 2002021100088 20020211 00088 2002 2 11 COMA0260088 4 20020205 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 932CA 7172 7038 FLIGHT 5045 STALL FAIL CAUTION MESSAGE.REPALCED THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 2002021100089 20020211 00089 2002 2 11 COMA0260089 4 20020201 A 3418 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 978CA 7158 FLIGHT 5996 - STICK SHAKER ACTIVATED AFTER T/O.RESET THE STALL COMPUTER - SYSTEM TEST SATISFACTORY. 2 L 7 2 4F RT A21EA 2002021100090 20020211 00090 2002 2 11 SWAA020193 4 20020128 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021100091 20020211 00091 2002 2 11 SWAA020194 4 20020126 A 2565 22D22900131 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F A16WE 2002021100092 20020211 00092 2002 2 11 SWAA020195 4 20020125 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 712SW 27846 DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021100093 20020211 00093 2002 2 11 SWAA020196 4 20020124 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 781WN 30601 DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021100094 20020211 00094 2002 2 11 SWAA020197 4 20020126 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 734SA 27866 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY LENGTH OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021100095 20020211 00095 NM 2002 2 11 SWAA020199 1 20020127 A 3350 900835A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP AT CENTER CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002021100096 20020211 00096 NM 2002 2 11 SWAA020201 1 20020128 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 739GB 29275 EEPLS LENS AND BULB MISSING AT ROW NR 1. REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002021100097 20020211 00097 2002 2 11 SWAA020211 4 20020125 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F A16WE 2002021100098 20020211 00098 2002 2 11 SWAA020212 4 20020126 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 743SW 29279 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021100099 20020211 00099 2002 2 11 SWAA020213 4 20020128 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021100100 20020211 00100 NM 2002 2 11 SWAA020217 1 20020129 A 5320 694036723 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EACH) AT BS 1138, STR 14L AND 16L. REMOVED AND REPLACE D STR TIE CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002021100101 20020211 00101 NM 2002 2 11 SWAA020221 1 20020130 A 3350 101114 LIGHT BOEING 737 7373H4 1384600 NM CABIN DEFECTIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED A1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT WEAK. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2002021100102 20020211 00102 NM 2002 2 11 SWAA020225 1 20020130 A 3350 300432 LIGHT BOEING 737 7372H4 138448C NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT NEAR AFT ENTRY DOOR INOP. RELAMPED PER MM. 2 L 7 2 4F A16WE 2002021100103 20020211 00103 2002 2 11 SWAA020232 4 20020131 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021100104 20020211 00104 NM 2002 2 11 SWAA020233 1 20020131 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 748SW 29800 EEPLS IN FWD CABIN INOP AND MISSING COVER. INSTALLED COVER AND REPAIRED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002021100105 20020211 00105 NM 2002 2 11 SWAA020235 1 20020130 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002021100106 20020211 00106 NM 2002 2 11 SWAA020242 1 20020202 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM SERVICE DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 771SA 27879 AFT SVC DOOR EMERGENCY EXIT LIGHT BRACKET BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002021100107 20020211 00107 NM 2002 2 11 SABA020014 1 20020203 A 3350 6104789 BATTERY DHAV DHC8 DHC8103 1386005 NM CABIN DISCHARGED A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 883 162 AIRCRAFT 883 ON FLIGHT 8681 CLT TO GSP. DURING PREFLIGHT BEFORE DEPARTURE TIME THE CABIN CEILING EMERGENCY LIGHT WERE F OUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERIES. SYSTEM OPS CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002021100108 20020211 00108 NM 2002 2 11 SWAA020169 1 20020122 A 2560 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 384SW 26590 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT SIGN DAMAGED AT FWD LAV AFT BULKHEAD. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2002021100109 20020211 00109 NM 2002 2 11 SWAA020180 1 20020125 A 5610 6531914 MECHANISM BOEING 737 7375H4 138449D NM COCKPIT OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D-CHECK, FOUND R2 COCKPIT WINDOW EMERGENCY RELEASE MECHANISM INOP. ADJUSTED R2 COCKPIT WINDOW RELEASE HANDLE MECHANISM PER MM. 2 L 7 2 4F RT A16WE 2002021100110 20020211 00110 NM 2002 2 11 SWAA020181 1 20020125 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED D-CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 15 DEF. REPAIRED WIRING PER MM. 2 L 7 2 4F RT A16WE 2002021100111 20020211 00111 2002 2 11 SWAA020187 4 20020125 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVACUATION SLIDE ATTACHED BRACKET CORRODED. REMOVED AND REPLACED BRACKET PER SRM. 2 L 7 2 4F RT A16WE 2002021100112 20020211 00112 NM 2002 2 11 SWAA020190 1 20020126 A 2822 8311001 PUMP BOEING 737 737317 138447P NM FUEL TANK FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 698SW 23176 NR 2 FUEL TANK FWD FUEL BOOST PUMP LOW PRESS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 FUEL TANK FWD BOOST PUMP AND LOW PRESS SWITCH PER MM. 2 L 7 2 4F RT A16WE 2002021100113 20020211 00113 2002 2 11 SWAA020191 4 20020127 A 2565 D31591 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 353SW 24889 FWD ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2002021100114 20020211 00114 NM 2002 2 11 02036408 1 20020205 A 3350 CONNECTOR DORNER DO32 DO328300 NM CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 408FJ DURING MAINTENANCE INSPECTION EMERGENCY ESCAPE FLOOR PATH LIGHT MIDDLE SECTION WAS OUT. MAINTENANCE PERSONNEL SECURED A LOOSE CONNECTOR FOR THE MID SECTION OF THE EMERGENCY FLOOR TRACK LIGHTING SYSTEM. AN OPERATIONAL CHECK WAS SATISFACTOR Y AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002021100116 20020211 00116 WP 2002 2 11 02FDEA00094 1 20020207 A 5230 63050007 DRIVE SHAFT DOUG DC10 DC1030 3023501 WP CARGO DOOR SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 CENTER CARGO DOOR LIFT ACT OUTPUT DRIVE SHAFT SHEARED, CAUSING DOOR TO FREE FALL AND IMPACT MAINTENANCE STAND. 2 L 7 3 4F A22WE 2002021100117 20020211 00117 EA 2002 2 11 02039648 1 20020208 A 3350 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA FAILED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 648BR 7406 During inspection, maintenance found the l/h aft overwing emergency exit light inoperative. Maintenance personnel remov ed and replaced the power supply. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002021100118 20020211 00118 NM 2002 2 11 CALA0200066 1 20020207 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND RT SUPPORT ANGLE CORRODED AROUND SCREW HOLE IN FORWARD CARGO COMPARTMENT AT STA 500A-500B. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51-40-02 AND 51-40-10. 2 L 7 2 4F RT A16WE 2002021100119 20020211 00119 SO 2002 2 11 CHQ000115 1 20020210 A 2611 SMOKE WARNING EMB 145 EMB145 3260210 SO COCKPIT ACTIVATED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 283SK 145424 AFTER TAKEOFF LAV SMOKE WARNING. 2 L 7 2 4F RT T00011AT 2002021100121 20020211 00121 NM 2002 2 11 AWXA200200114 1 20020123 A 5315 6545410152 WEB BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A 1/4" CRACK WAS FOUND ON FLOOR BEAM WEB BS 714, RBL 25. MAINTENANCE TRIMME D OUT DAMAGED SECTION OF FLOOR BEAM AT BS 714, RBL 25, FABRICATED A REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIRS IAW AWA ER 15-5702-02032-GF1 2 L 7 2 4F RT A16WE 2002021100122 20020211 00122 NM 2002 2 11 AWXA200200115 1 20020122 A 5210 654580023 SKIN BOEING 737 737277 1384570 NM GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A GOUGE WAS FOUND ON INNER SKIN AT FRAME TORQUE TUBE BOX OF THE L1 DOOR BS 305, STR 11-12, IN ADDITION TWO EXISTING REPAIRS WILL NEED TO BE INCORPORATED IN CORRECTIVE ACTION. MAINTENANCE REMOVED EXISTING REPAIRS FROM UPPER AND LOWER HINGE CUTOUT AND VERIFIED PREVIOUS TRIM OUT DID NOT EXCEED LIMITS DEFINED IN SRM 5 3-30-3 FIG 21 & 31 (TRIM OUT IS WITHIN LIMITS). CUTOUT GOUGED AREA OF SKIN AND PERFORMED HFEC INSPECTION TO VERIFY NO CR ACKS. FABRICATED AND INSTALLED A GAP COVER PER BOEING SERVICE BULLETIN 737-53-1074. FABRICATED REPAIR 2 EA. REPAIR DOUBL ERS AND 3 EA. FILLERS FOR UPPER AND LOWER L1 DOOR HINGE REPAIR AND INSTALLED REPAIR PARTS IAW AWA ER 15-5331-02039-ES2 2 L 7 2 4F RT A16WE 2002021100123 20020211 00123 NM 2002 2 11 AWXA200200116 1 20020130 A 5315 6545410554 TEE CHORD BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A 1.3" CRACK WAS FOUND ON INBOARD OF SEAT TRACK ON UPPER TEE CHORD OF LONGI TUDINAL BEAM BS 727B, RBL 44, WL 208. MAINTENANCE TRIMMED OUT CRACKED AREA OF CHORD AND PERFORMED HFEC INSPECTION TO VER IFY NO CRACKS, REMOVED EXISTING TIE STRAP, FABRICATED A NEW TIE STRAP AND INSTALLED REPAIR IAW AWA ER 15-5702-02038-GF1. 2 L 7 2 4F RT A16WE 2002021100124 20020211 00124 NM 2002 2 11 AWXA200200117 1 20020123 A 5414 65709471 SKIN BOEING 737 737277 1384570 NM GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A GOUGE .015 DEEP X 3" LONG WAS FOUND ON THE #1 ENGINE AFT PYLON INBOARD SI DE SKIN JUST AFT OF THE FLIPPER DOOR. MAINTENANCE REMOVED THE AFT INBOARD SKIN, FABRICATED NEW SKIN REPAIR DOUBLER AND I NSTALLED IAW AWA ER 15-5400-02036-TB1. 2 L 7 2 4F RT A16WE 2002021100125 20020211 00125 NM 2002 2 11 AWXA200200118 1 20020123 A 5414 65709471 SKIN BOEING 737 737277 1384570 NM GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 MCN - MAJOR REPAIR - "C" - DURING C-20 CHECK A GOUGE .009 TO .027 DEEP X 7" LONG WAS FOUND ON THE #1 ENGINE AFT PYLON IN BOARD SIDE SKIN JUST FORWARD OF THE FLIPPER DOOR. MAINTENANCE REMOVED THE CLOSEOUT DOUBLER BELOW MIDFLAP OUTBOARD ATTACH POINT ON INBOARD SIDE OF PYLON; TRIMMED OUT DAMAGED SKIN AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS; FABRICATED REPAIR SKIN AND SPLICE DOUBLER AND INSTALLED REPAIRS IAW AWA ER 15-5400-02036-TB2. 2 L 7 2 4F RT A16WE 2002022000022 20020220 00022 SO 2002 2 20 RAIA00202053 1 20020210 A 3250 3085701003 MANIFOLD EMB 145 EMB145LR 3260212 SO NLG STEERING FAULTY A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 811HK 8576 145256 5273- RIC- DURING TAXI HEARD BANGING SOUND COMING FROM FRONT OF AIRCRAFT. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLA CED THE STEERING HYDRAULIC MANIFOLD, LEAK AND OPS CHECK OK. 2 L 7 2 4T RT T00011AT 2002021100126 20020211 00126 SO 2002 2 11 RAIA00202049 1 20020203 A 3240 0132AEV1 SENSOR EMB 145 EMB145 3260210 SO MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 809HK 4933 145187 5318-PIT- RIGHT INBOARD BRAKE OVER TEMP INDICATION DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE RT INBOARD BRAKE TE MP SENSOR, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002021100127 20020211 00127 NE 2002 2 11 RAIA00202050 2 20020204 A 7320 31059006 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 560HK 8605 2621 41076 75090 5642-STL- LEFT ENGINE SLOW TO INCREASE TORQUE. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE FUEL CONTROL, LEAK AND O PS CK GOOD. 2 L 7 2 4T 4 T RT A41NM E18NE 2002021100128 20020211 00128 EU 2002 2 11 RAIA00202051 1 20020209 A 2435 23095002 STARTER GEN JETAIR JETSTM JETSTM4101 1500501 EU FAILED A RAIA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 03 571HK 9576 881 41090 5520-STL- LEFT GENERATOR FELL OFF LINE DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE LEFT STARTER GENERATOR, OPS CK OK. 2 L 7 2 4T RT A41NM 2002021100129 20020211 00129 EU 2002 2 11 RAIA00202052 1 20020209 A 7722 31050491 HARNESS JETAIR JETSTM JETSTM4101 1500501 EU A RAIA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 CE 03 554HK 41067 5385-BWI- LEFT ENGINE EGT FLUCTUATING AND UNRELIABLE DURING DECENT INTO RIC. SHUT DOWN ENGINE. MAINTENANCE INSPECTED THE EGT SYSTEM, FOUND BROKEN LEADS, AND REMOVED AND REPLACED THE EGT RAKE, OPS CK OK. 2 L 7 2 4T RT A41NM 2002021200009 20020212 00009 NM 2002 2 12 SWAA020287 1 20020206 A 5330 6545767 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND FUSLAGE SKIN CRACKED (4 EA) ABOVE STR 10R, BS'S 425, 434, 474 AND 494. REPAIRED S KIN PER SWA RA. 2 L 7 2 4F A16WE 2002021200010 20020212 00010 NM 2002 2 12 SWAA020288 1 20020206 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED .3 INCH LONG AT BS 470, WL 190 RT. REPAIRED SKIN PER SRM.. 2 L 7 2 4F RT A16WE 2002021200011 20020212 00011 NM 2002 2 12 SWAA020289 1 20020206 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED 1.0 INCH LONG AT BS 180, WL 184 AND RBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002021200012 20020212 00012 2002 2 12 SWAA020290 4 20020207 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED GIRT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002021200013 20020212 00013 NM 2002 2 12 SWAA020291 1 20020206 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED ON AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2002021200014 20020212 00014 NM 2002 2 12 SWAA020292 1 20020207 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 391SW 27378 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 219 TO 234, RBL 17.1. REMOVED AND REPLACED V ERTICAL BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2002021200015 20020212 00015 NM 2002 2 12 SWAA020293 1 20020205 A 5320 6546569 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR'S 2R AND 3R. REMOVED AND REPLACED SHEAR TIE P ER SRM. 2 L 7 2 4F RT A16WE 2002021200016 20020212 00016 NM 2002 2 12 SWAA020295 1 20020206 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING WALKAROUND INSPECTION, FOUND FUSLAGE SKIN CRACKED (3 EA) AT BS 740 AND STR 19L, BS 932 AND STR 22R, BS 973 AND ST R 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002021200029 20020212 00029 WP 2002 2 12 MWEA020081 1 20020208 A 5310 591415511 SKIN DOUG DC9 DC932 3022066 WP STATION 699 TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 STATION 699 TO 718 AT LONGERON 6 RIGHT, FUSELAGE SKIN (INTERNAL) HAS FOUR DIRLL START MARKS AND A GOUGE. -- FABRICATED AND INSTALLED SKIN REPAIRS. 2 L 7 2 4F A6WE 2002021200030 20020212 00030 WP 2002 2 12 MWEA020083 1 20020208 A 5330 59114272 SKIN DOUG DC9 DC932 3022066 WP STATION 990 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FUSELAGE SKIN IS CRACKED AT STATION 990 JUST BELOW LONGERON 14 RIGHT. -- FABRICATED AND INSTALLED REPAIR DOUBLER AND F ILLER. 2 L 7 2 4F A6WE 2002021200031 20020212 00031 WP 2002 2 12 MWEA020084 1 20020208 A 5330 59114271 SKIN DOUG DC9 DC932 3022066 WP STATION 990 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FUSELAGE SKIN IS CRACKED AT STATION 990 JUST BELOW LONGERON 14 LEFT. -- REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AN D FILLER. 2 L 7 2 4F A6WE 2002021200032 20020212 00032 WP 2002 2 12 MWEA020085 1 20020208 A 5310 9915558257 FORMER DOUG DC9 DC932 3022066 WP STATION 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD SIDE OF AFT PRESSURE BULKHEAD, FIRST FORMER UP FROM FLOOR, LEFT SIDE IS CRACKED AT OUTBOARD END IN RADIUS, STATI ON 996. -- FABRICATED AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 2002021200033 20020212 00033 WP 2002 2 12 MWEA020086 1 20020208 A 5310 9915558141 FORMER DOUG DC9 DC932 3022066 WP STATION 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD SIDE OF AFT PRESSURE BULKHEAD, THIRD FORMER UP FROM FLOOR, LEFT SIDE IS CRACKED IN RADIUS AT OUTBOARD END. STATI ON 996. -- FABRICATED AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 2002021200034 20020212 00034 WP 2002 2 12 MWEA020087 1 20020208 A 5310 9915558521 FORMER DOUG DC9 DC932 3022066 WP STATION 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD SIDE OF AFT PRESSURE BULKHEAD, FIRST FORMER UP FROM FLOOR ON RIGHT SIDE IS CRACKED IN RADIUS AT OUTBOARD END, ST ATION 996. -- FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2002021200035 20020212 00035 WP 2002 2 12 MWEA020088 1 20020208 A 5310 991558513 FORMER DOUG DC9 DC932 3022066 WP STATION 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD SIDE OF AFT PRESSURE BULKHEAD, THIRD FORMER UP FROM FLOOR ON RIGHT SIDE, IS CRACKED IN RADIUS AT OUTBOARD END. S TATION 996. -- FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2002021200036 20020212 00036 WP 2002 2 12 MWEA020093 1 20020208 A 5310 591141593 LONGERON DOUG DC9 DC932 3022066 WP STATION 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 STATION 699 LONGERON LEFT 3 CRACKED. -- FABRICATED AND INSTALLED HAT SECTION REPAIR SPLICE, FILLER, AND SPLICES. 2 L 7 2 4F A6WE 2002021200037 20020212 00037 WP 2002 2 12 MWEA020094 1 20020208 A 5310 591142221 LONGERON DOUG DC9 DC932 3022066 WP STATION 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 STATION 699 LONGERON 4 LEFT IS CRACKED. -- FABRICATED AND INSTALLED REPAIR SPLICE AND FILLER INSTALLED. 2 L 7 2 4F A6WE 2002021200038 20020212 00038 WP 2002 2 12 MWEA020095 1 20020208 A 5310 591141581 LONGERON DOUG DC9 DC932 3022066 WP STATION 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 STATION 699 LONGERON 5 LEFT IS CRACKED. -- FABRICATED AND INSTALLED LONGERON SECTION AND SPLICES. 2 L 7 2 4F A6WE 2002021200039 20020212 00039 WP 2002 2 12 MWEA020096 1 20020208 A 5310 591141581 LONGERON DOUG DC9 DC932 3022066 WP STATION 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 STATION 699 LONGERON 6 LEFT IS CRACKED. -- FABRICATED AND INSTALLED LONGERON RADIUS BLOCKS, TWO SPLICES, AND ONE LONGE RON FILLER. 2 L 7 2 4F A6WE 2002021200040 20020212 00040 WP 2002 2 12 MWEA020098 1 20020208 A 5310 99196161 FRAME DOUG DC9 DC932 3022066 WP STATION 680 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 STATION 680 FRAME HAS THREE OPEN HOLES BETWEEN LONGERON 17 LEFT AND 18 LEFT. -- FABRICATED AND INSTALLED FREEZE PLUG A ND RADIUS BLOCKS. 2 L 7 2 4F A6WE 2002021200041 20020212 00041 WP 2002 2 12 MWEA020099 1 20020208 A 5210 5934796521 TEE FITTING DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 CRACKED TEE FITTING ON PAX DOOR AT AFT END OF BEAM #3 (3RD FROM BOTTOM). -- REMOVED AND REPLACED TEE FITTING. 2 L 7 2 4F A6WE 2002021200042 20020212 00042 WP 2002 2 12 MWEA020102 1 20020208 A 5310 39203201 WEB DOUG DC9 DC932 3022066 WP RH MLG WELL CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD UPPER KEEL WEB TO SLANT PANEL ANGLE CRACKED. -- REMOVED AND REPLACED ANGLE FITTING. 2 L 7 2 4F A6WE 2002021200043 20020212 00043 WP 2002 2 12 MWEA020103 1 20020208 A 5310 99196151 FRAME DOUG DC9 DC932 3022066 WP STATION 658 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 STATION 658 FRAME HAS TWO HOLES IN INBOARD RADIUS OF FRAME BETWEEN LONGERON 17 LEFT AND 18 LEFT. -- FABRICATED AND INST ALLED RADIUS BLOCK AND CLIP. 2 L 7 2 4F A6WE 2002021200044 20020212 00044 WP 2002 2 12 MWEA020104 1 20020208 A 5310 995791917 FLOORBOARD DOUG DC9 DC932 3022066 WP STATION 965 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FLOORBOARD B11 IS DENTED AT THE FORWARD RIGHT CORNER. -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002021200045 20020212 00045 WP 2002 2 12 MWEA020107 1 20020208 A 5310 995791921 PANEL DOUG DC9 DC932 3022066 WP STATION 680 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 METALLIC FLOOR PANEL B8, HAS A FASTENER HOLE CRACKED AND ON THE SAME END THE OTHER CORNER IS CRACKED OFF WITH A BROKEN R IVET HEAD NEAR BY. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002021200046 20020212 00046 WP 2002 2 12 MWEA020125 1 20020208 A 5310 591140617 LONGERON DOUG DC9 DC932 3022066 WP STATION 160 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LONGERON 4 LEFT IS CRACKED AT STATION 160. -- FABRICATED AND INSTALLED LONGERON SECTIONS AND REPAIR SPLICES. 2 L 7 2 4F A6WE 2002021200047 20020212 00047 WP 2002 2 12 MWEA020068 1 20020206 A 5410 995815427 ANGLE DOUG DC9 DC932 3022066 WP RH PYLON OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 REMOVED RIGHT PYLON AFT SPAR WEB ANGLE TO FACILITATE OTHER MAINTENANCE. (UPPER FASTENER HOLE OVERSIZED.) -- FABRICATED AND INSTALLED "L" ANGLE ON NEW WEB. 2 L 7 2 4F A6WE 2002021200048 20020212 00048 WP 2002 2 12 MWEA020070 1 20020206 A 5410 995815419 ANGLE DOUG DC9 DC932 3022066 WP PYLON OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 PYLON WEB ANGLE HAS AN OVERSIZED HOLE. -- FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2002021200049 20020212 00049 WP 2002 2 12 MWEA020075 1 20020208 A 5230 4913644501 PAN DOUG DC9 DC932 3022066 WP FWD CARGO DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD CARGO DOOR INNER PAN IS DENTED FROM THE FORWARD DOOR HINGE. -- FABRICATED AND INSTALLED REPAIR DOUBLER. ALSO F OUND HINGE SUPPORT FITTING BOLT ATTACH HOLE AS OVERSIDED. REMOVED AND REPLACED HINGE SUPPORT FITTING. 2 L 7 2 4F A6WE 2002021200050 20020212 00050 WP 2002 2 12 MWEA020109 1 20020208 A 5310 39240271 FITTING DOUG DC9 DC932 3022066 WP STATION 604 UNSERVICEABLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 REMOVED FITTING FROM LEFT KEEL AREA AT STATION 604 TO FACILITATE OTHER MAINTENANCE. -- INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2002021200051 20020212 00051 WP 2002 2 12 MWEA020110 1 20020208 A 5310 591141851 SPLICE DOUG DC9 DC932 3022066 WP STATION 658 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 STRINGER SPLICE BETWEEN KEEL BEAM AND LONGERON 29 LEFT FUSELAGE STATION 658 ABD 667 HAS DOUBLE DRILLED HOLES. -- INSTA LLED NEW SPLICE. 2 L 7 2 4F A6WE 2002021200052 20020212 00052 WP 2002 2 12 MWEA020111 1 20020208 A 5310 99236621 INTERCOSTAL DOUG DC9 DC932 3022066 WP STATION 256 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 INTERCOSTAL AT LONGERON 7 RIGHT, FUSELAGE STATION 256, HAS A HOLE WHICH IS CRACKED ON THE AFT END. -- REMOVED AND REPL ACED INTERCOSTAL AND ANGLE. 2 L 7 2 4F A6WE 2002021200053 20020212 00053 WP 2002 2 12 MWEA020112 1 20020208 A 5410 49198641 FITTING DOUG DC9 DC932 3022066 WP STATION 1038 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FITTING IS CRACKED, LOCATED AT FUSELAGE STATION 1038 UPPER INBOARD CORNER. -- FABRICATED AND INSTALLED FITTING. 2 L 7 2 4F A6WE 2002021200066 20020212 00066 WP 2002 2 12 ARWA20020201 1 20020205 A 2760 H141008 SWITCH DOUG DC8 DC863F 302198F WP A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 441J 45988 LOG PAGE 107381. DISCREPANCY: TAKE OFF WARNING HORN SOUNDS WHEN POWER ADVANCED WITH FLAP SETTINGS 12, 18, AND 23 DEGREES FOR TAKE OFF. CORRECTIVE ACTION: REMOVED AND REPLACED RIGHT HAND SPOILER RELAY SWITCH IAW MM 27-63-1 OPERATIONAL CHECK NORMAL IAW MM 27-63-0. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002060300049 20020603 00049 WP 2002 6 3 ARWA20020202 1 20020204 A 5720 56449721 FITTING DOUG DC8 DC862 3021970 WP LT WING CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802BN 45909 DURING C-CHECK, LT WING NR 1 ALTERNATE FUEL TANK INTERIOR S-57 END FITTING WITH 1 INCH CRACK STA XRS 408.00. REMOVED AN D REPLACED STRINGER END FITTINGS IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 2002060300050 20020603 00050 WP 2002 6 3 ARWA20020203 1 20020204 A 5720 5644973502 FITTING DOUG DC8 DC862 3021970 WP RT WING CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802BN 45909 DURING C-CHECK, RIGHT WING NR 4 ALTERNATE FUEL TANK INTERIOR S-58 END FITTING WITH 1 INCH CRACK AT STA XRS 408.00. 2 L 7 4 4F 4A25 2002021200075 20020212 00075 NM 2002 2 12 SWAA020296 1 20020209 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM FUSELAGE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 641SW 27714 DURING SCHEDULED RON, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LOWER LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER M M. 2 L 7 2 4F RT A16WE 2002021200076 20020212 00076 2002 2 12 SWAA020297 4 20020206 A 2565 D31354 SLIDE BOEING 737 7373TO 138447G NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED GIRT ASSY PER MM . 2 L 7 2 4F RT A16WE 2002021200077 20020212 00077 2002 2 12 SWAA020299 4 20020208 A 2565 6556685 BRACKET BOEING 737 7372H4 138448C NM AFT SVC DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 AFT SVC DOOR EMERGENCY EVAC SLIDE DOOR RETAINING BRACKET BROKEN. REPAIRED BRACKET PER MM. 2 L 7 2 4F A16WE 2002021200078 20020212 00078 NM 2002 2 12 SWAA020300 1 20020208 A 5755 654645161A SPOILER BOEING 737 7372H4 138448C NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING WALK AROUND INSPECTION, FOUND NR 7 FLIGHT SPOILER DELAMINATED ON T/E. REMOVED AND REPLACED NR 7 FLIGHT SPOILER P ER MM. 2 L 7 2 4F A16WE 2002021200079 20020212 00079 2002 2 12 SWAA020301 4 20020208 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 600WN 27694 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021200080 20020212 00080 NM 2002 2 12 SWAA020303 1 20020209 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 603SW 27954 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 201, RBL 5.0 AND LBL 5.0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002021200081 20020212 00081 NM 2002 2 12 SWAA020304 1 20020208 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND HORIZONTAL WEBS CRACKED (2 EA) AT BS 180, WL 207, LBL 26.0 AND RBL 26.0. REMOVED AND REPLACED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2002021200082 20020212 00082 NM 2002 2 12 SWAA020305 1 20020208 A 5520 65C26384 TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND LT ELEVATOR TAB HINGE CUTOUTS DELAMINATED. REMOVED AND REPLACED ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002021200083 20020212 00083 NM 2002 2 12 SWAA020306 1 20020208 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED .125 INCH LONG AT BS 178, WL 234 AND RBL 10. REPAIRED WEB PE R SRM. 2 L 7 2 4F RT A16WE 2002021200084 20020212 00084 NM 2002 2 12 SWAA020307 1 20020207 A 5312 6517583 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED 1.0 INCH LONG AT BS 180, WL 184 AND RBL 17.1. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 2002021200085 20020212 00085 NM 2002 2 12 SWAA020308 1 20020208 A 3220 A5154B04 HOSE BOEING 737 7373Y0 1384671 NM NLG W/W FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 699SW 23826 DIVERSION, AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. F0UND LOCKING ACTUATOR FLEX HOSE FAILURE AT SWEDGE AREA. REMOVED AND REPLACED HOSE. OPS CK OK PER MM. 2 L 7 2 4F RT A16WE 2002021200086 20020212 00086 NM 2002 2 12 2002UALA00203 1 20020203 A 5321 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 CABIN FLOOR INTERCOSTAL AT STATION 332 RBL 4" TO 22" CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INST ALLED NEW U-CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021200087 20020212 00087 NM 2002 2 12 2002UALA00204 1 20020203 A 5321 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 CABIN FLOOR INTERCOSTAL AT STATION 332 RBL 25" TO 39" STRINGER 1 7R CORRODED ON UPPER SURFACE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW INTERCOSTAL U-CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021200088 20020212 00088 NM 2002 2 12 2002UALA00205 1 20020204 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 AFT PIT FRAME FLANGE DENT STATION 1440 AT STRINGER 26L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED DAMA GE AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021200089 20020212 00089 NM 2002 2 12 2002UALA00209 1 20020202 A 5315 BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 CABIN FLOOR STRUCTURE, INNER CREASE BEAM CHORD STATION 666 TO 755 HAD SEVERE CORROSION, ALSO INTERCOSTAL BELOW DOORWAY 2 L DRAIN GUTTER STATION 680 TO 700 LBL 62" AT STRINGER 17L (CREASE BEAM WAS ALSO AT 62" LBL AT STRINGER 17L) HAD SEVERE C ORROSION. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED INNER CREASE BEAM CHORD INSTALLED NEW PART AND I NSTALLED REPLACEMENT INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021200090 20020212 00090 NM 2002 2 12 2002UALA00211 1 20020203 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 EXTERNAL FUSELAGE SKIN STATION 359, STRINGER 3R, REQUIRED PERMANENT REPAIR. STRINGER 3R DAMAGED. SUPPLEMENTAL DATA UPDAT E MAJOR REPAIR ACCOMPLISHED. REPAIRED FUSELAGE SKIN AND STRINGER 3R WITH DOUBLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021200091 20020212 00091 NM 2002 2 12 2002UALA00212 1 20020203 A 5313 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 FUSELAGE BLIND FASTENER STATION 310 JUST BELOW STRINGER 2L REQUIRES PERMANENT REPAIR. SUPPLEMENTAL DATA UPDATE MAJOR REP AIR ACCOMPLISHED. REPLACED FASTENER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021200092 20020212 00092 NM 2002 2 12 2002UALA00216 1 20020203 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 FUSELAGE SKIN BLIND FASTENER INSTALLED STA. 333, STRINGER 2L. MAJOR REPAIR ACCOMPLISHED. INSTALLED SOLID FASTENER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021200093 20020212 00093 NM 2002 2 12 2002UALA00222 1 20020205 A 5315 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 AFT PIT, STATION 1420, ABOVE STRINGER 25L, FRAME DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FRAME DOUBL ER REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021200094 20020212 00094 NM 2002 2 12 2002UALA00224 1 20020204 A 5247 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 LEFT HAND APU DOOR HAS DAMAGE 38" FROM AFT END 3" FROM LOWER END RIVET IS PUSHING METAL AWAY FROM BUCKTAIL. MAJOR REPAI R ACCOMPLISHED. FLUSH REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021200095 20020212 00095 NM 2002 2 12 2002UALA00225 1 20020204 A 5315 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 CREASE BEAM BODY STATION 740 RBL 65 CORRODED. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR 2 L 7 2 4F 4 F RT A2NM E17NE 2002021200096 20020212 00096 NM 2002 2 12 2002UALA00226 1 20020204 A 5315 FLANGE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 BODY STATION 287 STRINGER 20R RBL 88.5 FLOORBEAM FLANGE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED F LOORBEAM FLANGE AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002021200097 20020212 00097 NM 2002 2 12 2002UALA00228 1 20020204 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 BODY STATION 266.5 BL 72 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SECTION AND SPLICE S. 2 L 7 2 4F 4 F RT A1NM E24NE 2002021200098 20020212 00098 NM 2002 2 12 2002UALA00230 1 20020204 A 5230 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 784UA 26951 BULK CARGO DOOR SKIN FORWARD EDGE AREA HAS DENT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002021200099 20020212 00099 NM 2002 2 12 2002UALA00231 1 20020205 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 CABIN FLOORBEAM CORRODED AT BODY STATION 852, LBL 53. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2002021200100 20020212 00100 NM 2002 2 12 2002UALA00233 1 20020206 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 FORWARD E & E ACCESS HOLE STATION 223.5 RBL 29" FRAME IS DAMAGED FROM FASTENER GOING THRU STAND-OFF ALSO HOLE CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021200101 20020212 00101 NM 2002 2 12 2002UALA00235 1 20020206 A 5320 CLIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 AFT PIT FRAME CLIP CORRODED STATION 1500 RBL17. MAJOR REPAIR ACCOMPLISHED. CLIP REMOVED AND CORROSION REMOVED FROM CLIP AND AFT LIP OF FRAME THEN CLIP REINSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021200102 20020212 00102 NM 2002 2 12 2002UALA00236 1 20020206 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 STATION 1681 STRINGER 17R FRAME CORRODED AT FLOOR Z ANGLE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR ON FRAM E. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021200103 20020212 00103 NM 2002 2 12 2002UALA00238 1 20020207 A 5313 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MISDRILLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FORWARD CARGO PIT STATION 654+88, INBD UPPER LEG OF STRINGER 31L HAS DOUBLE DRILLED HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPAIRED DAMAGE STRINGER SECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2002022100049 20020221 00049 NM 2002 2 21 2002UALA00239 1 20020207 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FORWARD PIT STATION 654+121 FRAME GOUGED OUT OF LIMITS AT STRINGER 31L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME. 2 L 7 2 4F 4 F RT A1NM E24NE 2002022100050 20020221 00050 NM 2002 2 21 2002UALA00240 1 20020207 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FORWARD PIT STATION 654+66 FRAME GOUGED OUT OF LIMITS AT STRINGER 32L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME. 2 L 7 2 4F 4 F RT A1NM E24NE 2002022100051 20020221 00051 NM 2002 2 21 2002UALA00241 1 20020207 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FORWARD PIT STATION 654+88, FRAME GOUGED OUT OF LIMITS AT STRINGER 31L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME. 2 L 7 2 4F 4 F RT A1NM E24NE 2002022100052 20020221 00052 NM 2002 2 21 2002UALA00242 1 20020207 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FORWARD PIT STATION 654+110, FRAME GOUGED OUT OF LIMITS AT STRINGER 31L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME. 2 L 7 2 4F 4 F RT A1NM E24NE 2002022100053 20020221 00053 NM 2002 2 21 2002UALA00243 1 20020207 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FUSELAGE SKIN CRACKED AT RIGHT HAND LOWER STAB CUTOUT STATION 1735 AT STRINGER 19R. MAJOR REPAIR ACCOMPLISHED. SKIN CR ACKED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002022100054 20020221 00054 NM 2002 2 21 2002UALA00244 1 20020207 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FUSELAGE LOWER SKIN CRACKED AT RIGHT HAND LOWER FORWARD STAB CUTOUT STATION 1740, STRINGER 19R. MAJOR REPAIR ACCOMPLISH ED. REPAIRED SKIN. 2 L 7 2 4F 4 F RT A1NM E24NE 2002022100055 20020221 00055 NM 2002 2 21 2002UALA00245 1 20020207 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FUSELAGE SKIN GOUGED OUT OF LIMITS AT LEFT HAND LOWER FORWARD STAB CUTOUT AT STATION 1735, STRINGER 19R. MAJOR REPAIR A CCOMPLISHED. REPAIRED SKIN. 2 L 7 2 4F 4 F RT A1NM E24NE 2002022100056 20020221 00056 NM 2002 2 21 2002UALA00246 1 20020207 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FUSELAGE LOWER SKIN GOUGED OUT OF LIMITS AT LEFT HAND STAB CUTOUT AT STATION 1740, STRINGER 19R. MAJOR REPAIR ACCOMPLIS HED. REPAIRED SKIN. 2 L 7 2 4F 4 F RT A1NM E24NE 2002021200109 20020212 00109 NM 2002 2 12 02039416 1 20020208 A 7921 30B316603 OIL COOLER DORNER DO32 DO328300 NM RT ENGINE DEFECTIVE A VTZA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 EA 27 416FJ DURING APPROACH INTO BOS CREW RECEIVED RT ENGINE AMBER OIL PRESSURE MESSAGE AND OIL PSI TURNED RED. CREW FOLLOWED QRH A ND PERFORMED A PRECAUTIONARY ENGINE SHUT DOWN. AN EMERGENCY WAS DECLARED WITH ATC AND FLIGHT LANDED WITHOUT FURTHER INC IDENTS. MAINTENANCE PERSONNEL REMOVED AND REPLACED RT FUEL/OIL HEAT EXCHANGER IAW 79-20-02. NO OIL LEAKAGE FOUND AND O PERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A55NM 2002021200110 20020212 00110 EU 2002 2 12 02FDEA00095 1 20020208 A 5270 SWITCH AIRBUS 300 A300F4605R 3930327 EU PAX DOOR FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 661FE 760 DURING CLIMB 7,000 FT RIGHT FWD CABIN DOOR NOT CLOSED WARNING ILLUM. REMOVED AND REPLACED DOOR WARNING SWITCH 8WS. 2 L 7 2 4F RT A35EU 2002021200112 20020212 00112 2002 2 12 AT0200007 4 20020207 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP R1 DOOR OUT OF POSITION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 825AT 47319 GIRT BAR WOULD NOT LATCH AT R1 DOOR. REPOSITIONED SLIDE AT R1 DOOR. 2 L 7 2 4F A6WE 2002021200115 20020212 00115 2002 2 12 AT0200008 4 20020210 A 2210 2589445933 ACTUATOR BOEING 717 717200 1383700 NM YAW DAMPENER MALFUNCTIONED A ZZDA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 15 946AT 55009 UNCOMMANDED SMALL RUDDER MOVEMENTS IN CHOPPY AIR. NOSE MADE SMALL YAW CHANGES, ACTED LIKE NO YAW DAMP ON. NO PROBLEM N OTED WHILE IN SMOOTH AIR. NEITHER AUTOPILOT ON. PROBLEM STOPPED WHEN RUDDER HYDRAULIC CONT TURNED OFF. REMOVED AND RE PLACED YAW DAMPENER ACTUATOR. 2 L 7 2 4F TR A6WE 2002021200121 20020212 00121 NM 2002 2 12 AWXA200200113 1 20020209 A 2910 BACH8C08NN0334 HYDRAULIC LINE BOEING 737 7373S3 1384711 NM LT MLG WW LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 316AW 23713 LAS - DIVERSION - FLT 0221 - C - EN ROUTE FROM SMF TO PHX DURING CLIMB THE A-SYSTEM HYDRAULIC PRESSURE CYCLED AND WENT T O ZERO ACCOMPANIED BY A FLIGHT CONTROL AND A-SYSTEM PRESSURE LIGHT. AIRCRAFT DIVERTED TO LAS WITHOUT FURTHER INCIDENT. IN LAS MAINTENANCE FOUND A-SYSTEM HYDRAULIC LINE LEAKING AT ACOUSTIC FILTER IN THE LT WHEEL WELL AND REPLACED THE LINE. ALSO REPLACED WAS THE ENGINE DRIVE HYDRAULIC PUMP, ELECTRIC DRIVEN HYDRAULIC PUMP, AND A-SYSTEM HYDRAULIC QUANTITY TRA NSMITTER IAW T/C'S R5M29002, R4R29001, R4M29002. A CONTAMINATION CHECK WAS ACCOMPLISHED IAW T/C F4M29002; OPERATIONAL A ND LEAK CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2002021200122 20020212 00122 SO 2002 2 12 C2XA02CL036 1 20020204 A 3350 66903 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17521 145378 CLE MAINTENANCE FOUND THE FORWARD AISLE PATH EMERGENCY LIGHT WAS INOPERATIVE. THE FORWARD EMERGENCY LIGHT STRIP WAS REP LACED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2002021200124 20020212 00124 SO 2002 2 12 C2XA02CL037 1 20020208 A 2120 ODOR EMB 145 EMB145ER 3260211 SO COCKPIT DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16944 145045 CLE FLIGHT 3015 THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN AND COCKPIT WHEN THE APU WAS STARTED. MAINTENANCE IN SPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002021200125 20020212 00125 NM 2002 2 12 DHL2002743001 1 20020210 A 2620 LIGHT BOEING 727 727225 1384077 NM COCKPIT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 743DH 22438 ENGINE NR 2 FIRE BOTTLE DISCHARGE BUTTON IS NOT ILLUMINATED BY FIRE HANDLE DURING TEST. ENG NR 1 DETECTOR CIRCUIT GROUN D LIGHT DOES NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED BULB IAW 727 MM 33-50-01, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002021200126 20020212 00126 NM 2002 2 12 DHL2002748001 1 20020208 A 3350 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 748DH 22440 ALL EMERGENCY EXIT LIGHTS INOP ON PREFLIGHT INSPECTION. RELAMPED EMERGENCY EXIT SIGNS AND REPLACED BATTERIES IAW MM 33- 50-01, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002021200128 20020212 00128 WP 2002 2 12 DHL2002806003 1 20020209 A 3260 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT WRONG PART A DHLA O OTHER W N INADEQUATE Q C FALSE WARNING AP APPROACH 1 SO 01 806DH 46002 LEFT MAIN GEAR LIGHT FAILED TO ILLUMINATE AFTER TWO CYCLES. LIGHT CAME ON AFTER PUSHING ON LIGHT COVER EXT POWER LIGHT OUT. FOUND INCORRECT LIGHT BULBS INSTALLED. REMOVED AND REPLACED LT MAIN GEAR LIGHT BULBS IAW DC-8 MM 33-10-0. LANDIN G GEAR POSITION INDICATION SYS OPS NORMAL IAW DC-8 MM 32-60-0. 2 L 7 4 4F RT 4A25 2002021200130 20020212 00130 NM 2002 2 12 F3LA200200032 1 20020127 A 5313 STRINGER BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 23007 DURING C-7 CHECK, BOLT MIGRATING OUT UNDER LT WING-TO-BODY FAIRING CHORD AT STA 685. REMOVED BROKEN BOLT AND FOUND CORR OSION INSIDE BOLT HOLE. OVERSIZED HOLE TO SECOND OVERSIZE OF ORIGINAL BOLT SIZE AND STILL FOUND INDICATION OF CORROSION . COMPLIED WITH INTERIM REPAIR PER EA 53-737-153 AT STR 18A-L, STA 663.75. INSTALLED SECOND OVERSIZE BOLT AND WASHER, FERRIED FOR REPAIR. REMOVED BOLT, BORE BRUSHED THE HOLE AND ALODINED HOLE. BORESCOPED HOLE FOR CORROSION. NO CORROSIO N NOTED. 2 L 7 2 4F RT A16WE 2002021200139 20020212 00139 CE 2002 2 12 GLBA2002016 1 20020207 A 2841 WARNING LIGHT BEECH 1900 1900D 1154162 CE COCKPIT ILLUMINATED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 228GL UE228 RIGHT COLLECTOR TANK LOW ANNUNCIATOR ILLUMINATED ON T/O. 2 L 7 2 4T RT A24CE 2002021200140 20020212 00140 CE 2002 2 12 GLBA2002017 1 20020207 A 3234 1013841377 CONTROL HANDLE BEECH 1900 1900D 1154162 CE COCKPIT INOPERATIVE A GLBA O OTHER J WARNING INDICATION AP APPROACH 1 NM 03 204GL 13397 UE204 LANDING GEAR WOULD NOT EXTEND ELECTRICALLY. REPLACED GEAR SELECT HANDLE, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002030400223 20020304 00223 2002 3 4 GLBA2002018 4 20020208 A 2562 ELT1104 ELT BEECH 1900 1900D 1154162 CE CABIN MALFUNCTIONED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 184UX 1641 UE184 ELT WOULD NOT SILENCE. REPLACE ELT, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002030400224 20020304 00224 CE 2002 3 4 GLBA2002019 1 20020210 A 2160 1143641407 PRINTED CKT BOAR BEECH 1900 1900D 1154162 CE CABIN TEMP FAULTY A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 251GL 1315 UE251 LEFT ENVIRONMENTAL FAILURE ON T/O. REPLACED PCB, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002021200142 20020212 00142 NM 2002 2 12 HNAA0200014 1 20020202 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 927HA 117 AT LEFT HAND EMERGENCY EXIT CORROSION FOUND ON FRAME AT STATION X366 AFT SIDE BELOW EMERGENCY EXIT. FRAME THICKNESS IS .040. DEPTH OF CORROSION AT EDGE OF FRAME IS .012. REPAIRED FRAME AREA IAW EO8-53-02-0141. BLEND OUT CORROSION, FABRIC ATED A REPAIR STRAP AND INSTALLED INSIDE OF FRAME INNER CHORD. 2 H 7 2 4T RT A13NM 2002021200143 20020212 00143 NM 2002 2 12 HNAA0200015 1 20020118 A 5320 GUSSET DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 927HA 117 FOUND CORROSION ON GUSSET AT STATION X354 STRINGER 21 RT. MFG NEW GUSSET AND INSTALLED. 2 H 7 2 4T RT A13NM 2002021200144 20020212 00144 NM 2002 2 12 HNAA0200016 1 20020118 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 927HA 117 RT INBOARD SEAT RAIL CORRODED BETWEEN STATION X182 TO X222. REMOVED AND REPLACED SEAT RAIL IN ACCORDANCE WITH RD8-53-30 74. 2 H 7 2 4T RT A13NM 2002021200145 20020212 00145 NM 2002 2 12 HNAA0200017 1 20020209 A 7910 OIL CAP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE LOOSE A HNAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 07 984HA 377 120586 NR 2 ENGINE LOSS OF OIL PRESSURE. SHUT DOWN NR 2 ENG AT 40 PSI. FOUND OIL AND CAP NOT SECURED COMPLIED WITH INSPECTION S IAW PWC MM 05-50-00 PG 11-13 ALSO CARD W79-01-21J AND W 79-20-04I. NO DISCREPANCIES NOTED. RESECURED OIL TANK CAP, S ERVICED ENGINE OIL, RUN UP AND LEAK CHECKS GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2002021200150 20020212 00150 EU 2002 2 12 UPS02137390 1 20020101 A 2560 GIRT BAR AIRBUS A300 A300F4622R 3930360 EU CABIN BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 139UP 0805 INSPECTION TYPE:N/A EMERGENCY SLIDE ON CABIN DOOR DISLODGED AND JAMS WHEN DOOR IS CLOSED. GIRT BAR IS BENT. SECURED GI RT BAR. POO-A010729 (ESCAPE SLIDE P/N D31023-101) REPLACED GIRT BAR AS PER AMM 52-10-30, STEP D6. TESTED RELEASE MECHA NISM AS PER AM 52-10-30. 2 L 7 2 4F RT A35EU 2002021200151 20020212 00151 EU 2002 2 12 UPS02137414 1 20020115 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU PAX DOOR WILL NOT TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 137UP 0810 INSPECTION TYPE:N/A EVAC SLIDE LIGHTS IN MAIN CABIN DOOR WILL NOT TEST. PERFORMED ADJUSTMENT TEST IAW MM 52-23-00 PG 50 1, NO FAULTS NOTED. 2 L 7 2 4F RT A35EU 2002021200152 20020212 00152 EU 2002 2 12 UPS02137423 1 20020115 A 2560 COVER AIRBUS A300 A300F4622R 3930360 EU COCKPIT LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 134UP 0818 INSPECTION TYPE:N/A CAPT ESCAPE ROPE COVER VELCRO LOOSE. SECURED VELCRO AND COVER. 2 L 7 2 4F RT A35EU 2002021200154 20020212 00154 EU 2002 2 12 UPS02137490 1 20020119 A 5210 DIAPHRAGM AIRBUS A300 A300F4622R 3930360 EU FWD DOOR PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 121UP 0806 INSPECTION TYPE:IN FWD DOOR EMERGENCY OPERATION CYLINDER SEALING DIAPHRAGM HAS BEEN PUNCTURED ITEM DEF M230237. INSTALL ED NEW DIAPHRAGM AND SERVICE DOOR DAMPER CYLINDER PER A300 MM CH 52-10-14. CHANGED O-RINGS AND SERVICED PER A300 MM 52- 10-14. THIS CLEARS M230237. 2 L 7 2 4F RT A35EU 2002021200156 20020212 00156 NM 2002 2 12 UPS02237389 1 20020103 A 3350 BATTERY BOEING 727 72730C 1384009 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:IN ENTRY DOOR EMERGENCY LIGHT INOP. INSTALLED NEW BATTERIES IN EMERGENCY EXIT LIGHT OVER ENTRY DOOR. O PS CHECK GOOD. 2 L 7 3 4F A3WE 2002021200157 20020212 00157 NM 2002 2 12 UPS02237393 1 20020105 A 3350 LENS BOEING 727 72730C 1384009 NM ENTRY DOOR LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:AS PLASTIC LENS FOR ENTRY DOOR EMERGENCY EXIT LIGHT FALLS OFF. REPLACED LIGHT LENS. 2 L 7 3 4F A3WE 2002021200159 20020212 00159 NM 2002 2 12 UPS02237399 1 20020107 A 3350 1000677 LIGHT BOEING 727 72727C 138400J NM L1 DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE:PFLT L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM 33-50-01, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2002021200160 20020212 00160 NM 2002 2 12 UPS02237405 1 20020102 A 3350 BATTERY BOEING 727 72762C 138402C NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:PFLT ON PREDEPARTURE CHECK, EMERGENCY EXIT LIGHT AT COCKPIT DOOR INOP. INSTALLED NEW BATTERIES AT COCKP IT DOOR EMERGENCY EXIT LIGHT ASSY, OPS CHECK NORMAL AS PER MM 33-50-1010. 2 L 7 3 4F A3WE 2002021200162 20020212 00162 NM 2002 2 12 UPS02237439 1 20020120 A 3350 LIGHT BOEING 727 72730C 1384009 NM COCKPIT NOT SEATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR IS DIM, RESEATED LIGHT ASSY. OPS CHECKS GOOD PER MM 33-50-1 01. 2 L 7 3 4F A3WE 2002021200166 20020212 00166 NM 2002 2 12 UPS02237448 1 20020112 A 5740 69139004 PIN BOEING 727 727185C 138406N NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI LEFT BS 740 TERMINAL PIN IS CORRODED IN AREA UNDERNEATH HEAD, AND PIN RETAINING BOLT HAS PITTING CO RROSION. LEFT BS 740 TERMINAL PIN AND RETAINING BOLT REPLACED IAW MM 57-41-04. 2 L 7 3 4F A3WE 2002021200171 20020212 00171 NM 2002 2 12 UPS02237460 1 20020102 A 5753 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 7 FLAP TRACK, PITTING CORROSION ON FWD SUPPORT LUG BORE LT LUG. BUSHING REMOVED AND CORROSION R EMOVED BY MACHINING. NDT COMPLIED WITH AND NDF. BUSHING FABRICATED, HEAT TREATED, CADPLATED, POST BAKED AND INSTALLED. 2 L 7 3 4F A3WE 2002021200172 20020212 00172 NM 2002 2 12 UPS02237461 1 20020102 A 5753 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 6 FLAP TRACK PITTING CORROSION ON FACE OF AUX SPAR PAD. CORROSION REMOVED BY MACHINING IAW OHM 57-40-01. NDT COMPLIED WITH NDF SOPM 20-20-01, FLAP PEENED IAW SOPM 20-10-03, STRESS RELIEVED IAW SOPM 20-10-02, CADPLA TED IAW SOPM20-42-10. 2 L 7 3 4F A3WE 2002021200173 20020212 00173 NM 2002 2 12 UPS02237462 1 20020102 A 5720 FITTING BOEING 727 727185C 138406N NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI RT WING NR 8 FLAP TRACK SUPPORT FITTING (WING FITTING) HAS PITTING CORROSION ON INBOARD FACE. CORR OSION REMOVED BY MACHINING, NDT COMPLIED WITH AND NDF. FLAP PEENED AND CADPLATED IAW OHM. 2 L 7 3 4F A3WE 2002021200177 20020212 00177 EA 2002 2 12 COMA0260090 1 20020210 A 4910 APU CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 932CA 7038 FLIGHT 5268 - SMOKE IN COCKPIT AFTER T/O.AIRCRAFT WAS DEICED WITH APU RUNNING. CLEANED ACM WATER SEPERATORS. 2 L 7 2 4F RT A21EA 2002021300113 20020213 00113 EA 2002 2 13 COMA0260091 1 20020206 A 2752 853D10017 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 916CA 6121 7014 FLIGHT 5872 FLAPS FAILED AT 45 DEGREES. REPLACED THE LT NR 3 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2002021200178 20020212 00178 NM 2002 2 12 UPS02237474 1 20020102 A 5753 BRACKET BOEING 727 727185C 138406N NM T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 4 FLAP TRACK CRACK IN FAIRING SUPPORT BRACKET FWD LT . BRACKET FABRICATED AND REPLACED IAW SRM. 2 L 7 3 4F A3WE 2002021200183 20020212 00183 SO 2002 2 12 C2XA02CL040 1 20020209 A 3350 CONNECTOR EMB 135 EMB135ER 3260203 SO CABIN LOOSE A C2XA O OTHER L NO TEST NR NOT REPORTED 1 SW 27 17507 145215 CLE FLIGHT# 3084 THE CREW REPORTED THE EMERGENCY LIGHT BELOW COCKPIT DOOR WAS INOPERATIVE.MAINTENANCE INSPECTED AND RESE CURED THE CONNECTOR ON THE LIGHT ASSEMBLY.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002021200184 20020212 00184 SO 2002 2 12 C2XA02CL041 1 20020209 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA O OTHER L NO TEST IN INSP/MAINT 1 SW 27 13968 145138 DURING 3A INSPECTION MAINTENANCE FOUND THE EMERGENCY LIGHT AT THE SERVICE DOOR WAS INOPERATIVE.MAINTENANCE INSPECTED AND TIGHTENED THE CONNECTOR ON THE EMERGENCY LIGHT.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002021200186 20020212 00186 WP 2002 2 12 G60A061 1 20020113 A 5754 NRB6221509 SKIN DOUG DC10 DC1030F 3023504 WP L/E SLAT DAMAGED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 609GC 46932 FATIGUE DAMAGE TO THE INNER SKIN OF THE NR 1 SLAT ON THE LEFT WING. MISSING MATERIAL HOLE SIZE IS APPROXIMATELY 8 INCHE S BY 11 INCHES WITH ONE AREA EXCEEDING THIS DIMENSION BY AN ADDITIONAL 2.5 INCHES BY 4 INCHES. THERE ARE 4 OBVIOUS FATI GUE CRACKS IN THE AREA. (M) 2 L 7 3 4F RT A22WE 2002021200187 20020212 00187 WP 2002 2 12 G6OA059 1 20020111 A 2730 ALH70111 BELLCRANK DOUG DC10 DC1030F 3023504 WP ELEVATOR WORN A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 605GC 47925 ELEVATOR CONTROL CHECK DOWNWARD MOVEMENT BINDING DURING NOSE DOWN MOVEMENT. FOUND BENT AND WORN BELLCRANK ASSEMBLIES ON LEFT INBOARD ELEVATOR ACTUATOR. REMOVED AND REPLACED BELLCRANK ASSEMBLY IAW MM 20-50-02. OPS CHECKS GOOD IAW MM 27-30 -00. (M) 2 L 7 3 4F RT A22WE 2002021200188 20020212 00188 WP 2002 2 12 G6OA060 1 20020111 A 2730 ALH70101 BRACKET DOUG DC10 DC1030F 3023504 WP ELEVATOR WORN A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 605GC 47925 FOUND ELEVATOR CONTROL CHECK DOWNWARD MOVEMENT BINDING DURING NOSE DOWN MOVEMENT. FOUND BENT AND WORN BRACKET ASSEMBLIE S ON LEFT INBOARD ELEVATOR. REMOVED AND REPLACED BRACKET ASSY IAW MM 20-50-02. OPS CHECKS GOOD IAW MM 27-30-00. (M) 2 L 7 3 4F RT A22WE 2002021200204 20020212 00204 NM 2002 2 12 UPS02237463 1 20020102 A 5753 FITTING BOEING 727 727185C 138406N NM FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 7 FLAP TRACK WING SUPPORT FITTING HAS PITTING CORROSION ON INBOARD FACE OF LUG. CORROSION REMOV ED, NDT COMPLIED WITH AND NDF. FLAP PEENED AND CADPLATED IAW OHM. 2 L 7 3 4F A3WE 2002021200205 20020212 00205 NM 2002 2 12 UPS02237466 1 20020107 A 5330 LAP JOINT BOEING 727 727185C 138406N NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI SURFACE CORROSION ON UPPER SKIN AT LAP JOINT BS 210 STR 24L IN LOWER NOSE COMPT. LAP JOINT DE-RIVE TED, CORROSION REMOVED, AREA OUTSIDE LIMITS CUT OUT, REPAIR PARTS FAB'D, HFEC C/W AND NDF, REPAIR INSTALLED IAW SRM 53-3 0-3 FIG 14 AND SRM 53-30-4 FIG 1. 2 L 7 3 4F A3WE 2002021200213 20020212 00213 NM 2002 2 12 UPS02237476 1 20020102 A 5753 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 1 FLAP TRACK HAS PITTING CORROSION ON LT FWD SUPPORT LUG OUTER FACE. CORROSION REMOVED BY MACHI NING IAW OHM 57-40-01. NDT COMPLIED WITH AND NDF IAW SOPM 20-20-01, FLAP PEENED IAW SOPM 20-10-03, STRESS RELIEVED IAW SOPM 20-10-02, CADPLATED IAW SOPM 20-42-10. 2 L 7 3 4F A3WE 2002021200214 20020212 00214 NM 2002 2 12 UPS02237477 1 20020103 A 5320 SUPPORT BOEING 727 727185C 138406N NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI SUPPORT TANG CRACKED ON DELTA BEAM BS 760 LT. CRACKED TANG TRIMMED FLUSH WITH DELTA BEAM LOWER CHO RD. HFEC CARRIED OUT NDF. REPAIR CARRIED OUT IAW SMRO EO 2001-057-011. 2 L 7 3 4F A3WE 2002021200215 20020212 00215 NM 2002 2 12 AWXA200200122 1 20020209 A 3350 BMS13311122 WIRE BOEING 757 7572S7 1384962 NM SEAT 3 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 PHX - EEL - "C" - DURING INSPECTION OF EMERGENCY LIGHTING SYSTEM EMERGENCY ESCAPE LIGHT ON SEAT ROW 3 L/H WAS FOUND INOP ERATIVE. MAINTENANCE FOUND BROKEN WIRE AT SEAT ROW 3 L/H AND REPAIRED BROKEN WIRE IAW BOEING SWP 20-30-12, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002021200216 20020212 00216 NM 2002 2 12 AWXA200200120 1 20020211 A 2830 L83A136021 DRAIN VALVE AIRBUS A319 A319132 3930340 NM ZONE 550 STUCK A AWXA A UNSCHED LANDING K P FLUID LOSS NO WARNING INDICATION TO TAKEOFF 1 WP 28 813AW 1223 PHX - AIR TURNBACK - FLT 689 - "C" - ON TAKEOFF FROM PHX ENROUTE TO EWR FUEL WAS SEEN STREAMING FROM THE L/H OUTBOARD WI NG FROM UNDERNEATH THE AILERON AS REPORTED BY AIRCRAFT FOLLOWING ON TAKEOFF, FUEL GAUGE ALSO INDICATED A 200 LB FUEL LOS S, AN EMERGENCY WAS DECLARED AND AIRCRAFT TURNED BACK TO PHX MAKING AN UNEVENTFUL LANDING. AT THE GATE WHEN MAINTENANCE ENTERED THE FLIGHT DECK THE MODE SELECT SWITCH WAS OBSERVED IN THE MANUAL POSITION. MAINTENANCE ALSO FOUND L/H WING OUTB OARD SUMP DRAIN NOT FULLY SEATED; RESEATED THE SUMP DRAIN VALVE AND INSPECTED FOR LEAKS, NO LEAKS WERE NOTED. 2 L 7 2 4F RT A28NM 2002021200217 20020212 00217 SO 2002 2 12 C2XA02IA025 1 20020210 A 3350 20131A BATTERY EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27523 145389 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS FAILED TO OPERATE. IAH- MAINTENANCE REMOVED and REPLAC EDTHE FORWARD BATTERY PACK, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE A IRCRAFT WAS APPEROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT TOOO11AT 2002021200218 20020212 00218 SO 2002 2 12 C2XA02IA026 1 20020208 A 3350 M610628023 RELAY EMB 120 EMB120ER 3260203 SO COCKPIT INOPERATIVE A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 27 57734 120199 IAH- DURING TAXI, FLIGHT 3585, THE EMERGENCY LIGHT (NOT ARMED LIGHT ON THE MAP)CAME ON WHEN THE SWITCH IS IN THE ARMED POSITION. IAH- MAINTENANCE REMOVED AND REPLACED RELAY K201, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SY STEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002021300036 20020213 00036 2002 2 13 ARWA20020204 4 20020212 A 3452 5222703011 TRANSPONDER DOUG DC8 DC863 302198A WP A ARWA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 19 345JW 46042 LOG PAGE 108434. DISCREPANCY: BOTH TRANSPONDERS MODE "C" ALTTITUDE REPORTING INOPERATIVE, C/B's RESET, NO HELP. AIRCRAFT RETURNED TO KMIA AND LANDED OVERWEIGHT UNEVENTFULL. CORRECTIVE ACTION: REMOVED AND REPLACED BOTH #1  ATC TRANSPONDER S IAW MM 34-53-0 ACCOMPLISHED TEST IAW FAR 43 APPENDIX"E" AND "F", PARAG "G" AND MM-34-53-0, ALL COVERS AND FLAGS REMOVE D AFTER TEST. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION "A" IAW ARROW AIR J/C 6372, NO DEFECTS NOTED. AIRCRFAT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002021300037 20020213 00037 CE 2002 2 13 00012 1 20020212 A 3260 WARNING SYSTEM LEAR 24 24 5170302 CE COCKPIT FALSE INDICATION E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 157TW 24157 LANDING GEAR UNSAFE LIGHT RETURNED TO DEPARTURE AIRPORT FOR MAINTENANCE. MAINTENANCE SWUNG GEAR, FOUND NO DISCREPANCIES . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4J A10CE 2002021300044 20020213 00044 2002 2 13 SWAA020309 4 20020209 A 2565 D31354 SLIDE BOEING 737 7373T0 1384582 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021300045 20020213 00045 2002 2 13 SWAA020310 4 20020209 A 2565 6557463 BRACKET BOEING 737 7373T0 1384582 NM FWD SVC DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY AFT BRACKET MISSING FASTENER. INSTALLED FA STENER PER MM. 2 L 7 2 4F RT A16WE 2002021300046 20020213 00046 NM 2002 2 13 SWAA020314 1 20020210 A 5330 6545409 WEB BOEING 737 7373A4 1384585 NM LT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 665, LBL 65. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002021300047 20020213 00047 NM 2002 2 13 SWAA020315 1 20020210 A 5240 6547952166 DOOR BOEING 737 7373T0 1384582 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR CRACKED .375 INCH ON FWD FRAME. REMOVED AND REPLACED DOOR PER MM. 2 L 7 2 4F RT A16WE 2002021300048 20020213 00048 2002 2 13 SWAA020316 4 20020210 A 2565 D31354 SLIDE BOEING 737 7373T0 1384582 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE ASSY PER M M. 2 L 7 2 4F RT A16WE 2002021300049 20020213 00049 NM 2002 2 13 SWAA020317 1 20020210 A 5330 589357 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 391SW 27378 DURING SCHEDULED 1/4D CHECK, FOUND LT WINDOW POST SKIN CRACKED BETWEEN NR 1 WINDOW UPPER OTBD CORNER AND NR 2 WINDOW UPP ER FWD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002021300050 20020213 00050 NM 2002 2 13 SWAA020318 1 20020211 A 5311 6545871 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT CORRODED AT BS 794, RBL 28 TO 47 AND WL 159 TO 169. REPAIRE D FRAME PER SRM AND BFG ER. 2 L 7 2 4F RT A16WE 2002021300051 20020213 00051 NM 2002 2 13 SWAA020319 1 20020211 A 5311 6546546 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (5 EA) AT STR 8L, BS'S 400, 440, 747, 867 AND 907. REPAIRED FRA MES PER BFG ER. 2 L 7 2 4F RT A16WE 2002021300052 20020213 00052 NM 2002 2 13 SWAA020320 1 20020211 A 5311 6546546 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) AT STR 8R, BS'S 380 AND 440. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2002021300073 20020213 00073 NM 2002 2 13 2002UALA00176 1 20020204 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 STATION 312 FLOORBEAM UPPER CHORD GOUGED FROM BL 0 TO LBL 10. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE AND STRAP INSTAL LED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021300083 20020213 00083 NM 2002 2 13 2002UALA00191 1 20020202 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CABIN UPPER LOBE FRAME CRACKED AT BODY STATION 867 AND STRINGER S9L. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FRAME DOU BLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021300084 20020213 00084 NM 2002 2 13 2002UALA00192 1 20020202 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CABIN UPPER LOBE FRAME CRACKED AT BODY STATION 887 AND STRINGER S9R. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FRAME REP AIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021300085 20020213 00085 NM 2002 2 13 2002UALA00193 1 20020202 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 RIGHT STRINGER 17 CREASE BEAM INNER CHORD HAS CORROSION ON UPPER SURFACE STATION 947-993. MAJOR REPAIR ACCOMPLISHED.REP LACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021300086 20020213 00086 NM 2002 2 13 2002UALA00194 1 20020202 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 MID CABIN RIGHT HAND FLOOR CHANNEL SUPPORT LOOSE AT STATION 616 AT INBOARD SEAT TRACK RIGHT HAND SIDE. MAJOR REPAIR ACC OMPLISHED. ACCOMPLISHED LONGITUDINAL FLOORBEAM ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021300087 20020213 00087 NM 2002 2 13 2002UALA00195 1 20020202 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 AFT LEFT HAND ENTRY DOOR LOWER SILL THRESHOLD Z-ANGLE CORRODED NUMEROUS AREAS FROM STATION 965 TO STATION 984 AROUND NUT PLATES ON UNDERSIDE. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021300089 20020213 00089 NM 2002 2 13 2002UALA00196 1 20020202 A 5320 ATTACH ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CABIN RIGHT HAND CREASE BEAM ATTACH L ANGLE BODY STATION 291 - BODY STATION 294 STRINGER 17R CRACKED, RBL 53. MAJOR REP AIR ACCOMPLISHED. L-ANGLE REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021300091 20020213 00091 NM 2002 2 13 2002UALA00197 1 20020202 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CABIN FLOOR WEB CRACKED AT STATION 996 JUST INBOARD OF RIGHT HAND Z-ANGLE. MAJOR REPAIR ACCOMPLISHED. WEB FABRICATED A ND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021300092 20020213 00092 NM 2002 2 13 2002UALA00198 1 20020202 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CABIN FLOORBEAM UPPER CAP HAS ELONGATED HOLE AND GOUGE AT STATION 987 RBL 45 INCHES. MAJOR REPAIR ACCOMPLISHED. INSTAL LED REPAIR STRAP, ANGLER AND FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030700067 20020307 00067 NM 2002 3 7 2002UALA00199 1 20020201 A 2782 5006397 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L/E SLAT FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 582UA 26702 LEADING EDGE SLAT DISAGREE MESSAGE DISPLAYED. THE NUMBER 6 LEADING EDGE SLAT ROTARY ACTUATOR FAILED AND CAUSED SOME BIN DING IN THE SLAT. THE BINDING WAS DETECTED BY THE FLAP/SLAT ELECTRONIC UNIT WHICH SUBSEQUENTLY SHUT DOWN THE SYSTEM AS FAILURE PROTECTION. THE NUMBER 6 SLAT ACTUATOR WAS REPLACED AND OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002030700069 20020307 00069 NM 2002 3 7 2002UALA00200 1 20020202 A 2782 5006397 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L/E SLAT FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 582UA 26702 LEADING EDGE SLAT DISAGREE MESSAGE DISPLAYED. THE NUMBER 6 LEADING EDGE SLAT ROTARY ACTUATOR FAILED AND CAUSED SOME BIN DING IN THE SLAT. THE BINDING WAS DETECTED BY THE FLAP/SLAT ELECTRONIC UNIT WHICH SUBSEQUENTLY SHUT DOWN THE SYSTEM AS FAILURE PROTECTION. THE NUMBER 6 SLAT ACTUATOR WAS REPLACED AND OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002030100020 20020301 00020 EU 2002 3 1 2002UALA00201 1 20020203 A 2421 766219 IDG AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT ENGINE OVERHEATED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 404UA 450 NR 1 INTEGRATED DRIVE GENERATOR DISCONNECTED AND UNABLE TO START AUXILIARY POWER UNIT. REPLACED NR 1 ENGINE INTEGRATED DRIVE GENERATOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2002021300095 20020213 00095 NM 2002 2 13 2002UALA00202 1 20020201 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 CABIN FLOORBEAM AT STATION 1640 RBL 51.5 AFT SIDE OF CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR . 2 L 7 2 4F 4 F RT A2NM E17NE 2002021300096 20020213 00096 NM 2002 2 13 2002UALA00206 1 20020204 A 5320 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 AFT CABIN DECK PLATE AT STATION 1680 AND RBL 25 CORRODED. MAJOR REPAIR ACCOMPLISHED. DECK PLATE REPAIR DOUBLER INSTALL ED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031400155 20020314 00155 NE 2002 3 14 2002UALA00207 2 20020202 A 7532 BLEED VALVE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE OUT OF RIG A UALA A UNSCHED LANDING R A PARTIAL RPM/PWR LOSS FLAME/FIRE CL CLIMB 1 WP 29 606UA 21867 707506 LEFT ENGINE COMPRESSOR STALL WITH EGT PEAKING AT 698 DEGREES. ATC REPORTED FLAMES FROM REAR OF ENGINE. RETURNED TO JFK . ACCOMPLISHED THE EVBC (ENGINE VANE & BLEED CONTROL) AND 3.0 BLEED TRIM. THE 3.0 BLEED WAS FOUND OUT OF TRIM. PROB LEMS WERE ENCOUNTERED WITH AIRCRAFT WIRING FOR THE TRIM EQUIPMENT, BUT WERE RESOLVED AND THE 3.0 BLEED WAS TRIMMED. 2 L 7 2 4F 4 F RT A1NM E3NE 2002021300097 20020213 00097 NM 2002 2 13 2002UALA00208 1 20020204 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 CABIN CREASE BEAM INNER CHORD BODY STATION 740 TO BODY STATION 757 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED CREAS E BEAM INNER CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021300098 20020213 00098 NM 2002 2 13 2002UALA00210 1 20020202 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 CABIN FLOOR SUPPORT BEAM FOR FWD GALLEY CORRODED UNDER GALLEY MOUNT AT BODY STATION 300 RBL 41 WL 208. MAJOR REPAIR ACC OMPLISHED. REPLACED FLOORBEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021300099 20020213 00099 NM 2002 2 13 2002UALA00213 1 20020202 A 7921 50G479 HEAT EXCHANGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 WP 29 648UA 25285 STATUS MSG LEFT ENGINE AIR OIL VALVE. SUITABLE EQUIPMENT MAY NOT BE AVAILABLE TO REPAIR ENGINE IN HAVANA. RETURNED TO MIA. REPLACED AIR-OIL HEAT EXCHANGER AND VALVE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002030100021 20020301 00021 EU 2002 3 1 2002UALA00214 1 20020204 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 435UA 613 SEATS 19, 21 LEFT EMERGENCY ESCAPE PATH LIGHTING INOPERABLE. REPLACED EMERGENCY LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2002021300102 20020213 00102 NM 2002 2 13 2002UALA00221 1 20020202 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 CABIN FLOORBEAM UPPER CAP HAS EXCESSIVE MATERIAL REMOVED AT STATION 365. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AN D ANGLE REPAIR ON FLOORBEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021300104 20020213 00104 NM 2002 2 13 2002UALA00223 1 20020205 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 CABIN CREASE BEAM BODY STATION 758 RBL 65 HAS EXCESSIVE MATERIAL LOSS AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. INS TALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021300105 20020213 00105 NM 2002 2 13 2002UALA00227 1 20020204 A 5310 DOOR FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 BODY STATION 266.5-286.5 RBL 86 DOOR CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED CHORD. 2 L 7 2 4F 4 F RT A1NM E24NE 2002021300108 20020213 00108 NM 2002 2 13 2002UALA00229 1 20020207 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 AFT PIT STA 1540 ABOVE STRINGER 25L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR ON FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021300109 20020213 00109 NM 2002 2 13 2002UALA00234 1 20020206 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 BODY STATION 640 BL 0 RBL 22 FLOORBEAM TOP SURFACE GOUGED. MAJOR REPAIR ACCOMPLISHED. CUT AWAY DAMAGED AREA AND INSTAL LED T-CAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021300110 20020213 00110 NM 2002 2 13 2002UALA00237 1 20020207 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 926UA 26648 LEFT HAND BODY STATION 188 FRAME CRACKED AT FLOOR LINE. MAJOR REPAIR ACCOMPLISHED. CRACK REPAIRED WITH ANGLE AND DOUBL ER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021300111 20020213 00111 EU 2002 2 13 C2XA02BT003 1 20020212 A 3397 WIRE AEROSP ATR42 ATR42320 8680930 EU PAX DOOR BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 86842 286 DURING LINE CHECK/WEEKLY INSPECTION MAINTENANCE FOUND PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. FOUND BROKEN WI RE TO EMERGENCY LIGHT REPAIRED AND OPS CHECKED EMERGENCY LIGHT GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2002021300112 20020213 00112 SO 2002 2 13 COMA0210004 1 20020209 A 5280 12012347001 LATCH EMB 120 EMB120RT 3260202 SO L/H MLG BROKEN A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 269CA 120263 FLIGHT 5021 L/H MLG, INBD GEAR DOOR, DOES NOT CLOSE AFTER GEAR RETRACTION.REPLACED THE DOOR LATCH. 2 L 7 2 4T RT A31SO 2002021300114 20020213 00114 EA 2002 2 13 COMA0260092 1 20020210 A 2751 601R930301 POTENTIOMETER CNDAIR CL600 CL6002B19 1900309 EA FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING N S FALSE WARNING AFFECT SYSTEMS CL CLIMB 1 SO 01 936CA 13660 7043 FLIGHT 5290 FLAP OVER SPEED WARNING AFTER T/O.REPLACED THE FLAP POSITION POT. 2 L 7 2 4F RT A21EA 2002021300116 20020213 00116 NM 2002 2 13 F3LA200200038 1 20020203 A 5753 SKIN BOEING 737 7372Y5 1384554 NM FOREFLAP DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED UPPER SURFACE OF LT OUTBOARD FOREFLAP DELAMINATED, STA 325. REPAIRED PER SRM 51-4 0-2 AND F9 MAINTENANCE FORM 5034-2. 2 L 7 2 4U RT A16WE 2002030500025 20020305 00025 CE 2002 3 5 GLBA2002020 1 20020211 A 2150 WARNING SYSTEM BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 226GL UE226 ABORTED TAKEOFF, LEFT ENVIRONMENTAL FAIL ILLUMINATED ON TAKEOFF ROLL. COULD NOT DUPLICATE FAULT, OPS CHECKED SYSTEM SAT ISFACTORY. 2 L 7 2 4T RT A24CE 2002021300117 20020213 00117 WP 2002 2 13 IXXA0200004O 1 20020207 A 3213 5777513501 STRUT DOUG DC8 DC871F 302199D WP LT MLG CRACKED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 826BX 84227 2115 45998 EN ROUTE FROM TOL TO BDL, THE LANDING GEAR AND DOOR UNSAFE WARNING LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. T HE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE UNSAFE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO TOL FOR AND UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE LEFT MAIN LANDING GEAR RETRACT PIN BO SS CRACK. MAINTENANCE REPLACED THE LEFT LANDING GEAR UPPER STRUT CYLINDER IN ACCORDANCE WITH THE MAINTENANCE MANUAL AND PERFORMED A SUCCEFUL OPERATIONAL CHECK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002021300118 20020213 00118 EU 2002 2 13 MALA020152 1 20020208 A 5410 SEAL SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING E-CHECK MAINTENANCE FOUND LT I/B NACELLE CHAFE IS OUT OF LIMITS IAW SAAB SRM 54-10-10. CAUSED BY LEADING EDGE FI LLET FAIRING SEAL. MAINTENANCE REPAIRED NACELLE DAMAGE IAW MAL EO 54053. 2 L 7 2 4T RT A52EU 2002021300119 20020213 00119 WP 2002 2 13 MWEA020069 1 20020206 A 5411 995815429 DOUBLER DOUG DC9 DC932 3022066 WP RT PYLON DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 RIGHT PYLON AFT SPAR WEB DOUBLER HAS OVERSIZED FASTENER HOLES. FABRICATED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 2002021300120 20020213 00120 WP 2002 2 13 MWEA020072 1 20020208 A 5230 591015777 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 AFT CARGO DOOR SKIN BY DOOR HANDLE HAS A CRACK. FABRICATED AND INSTALLED REPAIR SCUFF PLATE. 2 L 7 2 4F A6WE 2002021300121 20020213 00121 WP 2002 2 13 MWEA020073 1 20020208 A 5330 5911410175 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DENT IN FUSELAGE SKIN AT STATION 237 BELOW LONGERON 18 LEFT REQUIRES THE PANE REMOVED FOR EVALUATION. TRIMMED INTERNAL DOUBLER IAW TELEX MWX-ORD-02-00019H. INSTALLED REPAIR PLUG AND SHEAR TIE. INSTALLED FASTENERS IN SHEAR TIE IAW SRM 51- 30-5, 51-30-4, 51-30-2, MWX-ORD-02-00019H. 2 L 7 2 4F A6WE 2002021300122 20020213 00122 NM 2002 2 13 CALA0200068 1 20020212 A 5242 SKIN BOEING 737 7373T0 1384582 NM E&E DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND THE E&E DOOR DENTED AT R/H SIDE OF HANDLE. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203. 2 L 7 2 4F RT A16WE 2002021300134 20020213 00134 WP 2002 2 13 AALA20020023 1 20020103 A 5342 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND TWO HILOCK HEADS DISHED, ATTACH ANGLE CRACKED FROM HOLE TO HOLE PLUS .125 INCH FORWARD. INSTALLED VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE PER AARD 53-10-00-2. REPLACED 2 DISHED HILOCKS AND LEFT SIDE. (M) 2 L 7 2 4F A6WE 2002021300135 20020213 00135 WP 2002 2 13 AALA20020024 1 20020102 A 5342 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND 1 HI-LOCK DISHED, ATTACH ANGLE CRACKED FROM HOLE TO HOLE AND AFT PLUS 6 INCHES. REMOVED AND REPLACED CRACKE D HI-LOCK. INSTALLED DOUBLER PER AARD 53-10-00-2 ON RIGHT SIDE. (M) 2 L 7 2 4F A6WE 2002021300136 20020213 00136 WP 2002 2 13 AALA20020025 1 20020104 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND BOTTOM OF CUSP CORRODED AROUND LIGHTING HOLE. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER AARD 53. (M) 2 L 7 2 4F A6WE 2002021300137 20020213 00137 WP 2002 2 13 AALA20020026 1 20020104 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND DENT IN FORWARD CARGO DOOR CUTOUT UPPER CORNER. REPAIRED DENTED AREA PER ESO 80559. (M) 2 L 7 2 4F A6WE 2002021300138 20020213 00138 WP 2002 2 13 AALA20020027 1 20020104 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND GOUGE ON INNER SURFACE OF FUSELAGE SKIN STATION 260, BETWEEN LONGERON 24 AND LONGERON 25 RIGHT. INSTALLED R EPAIR PER SRM 53-04 FIG 38 SHEET 4. (M) 2 L 7 2 4F A6WE 2002021300139 20020213 00139 WP 2002 2 13 AALA20020028 1 20020107 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND CORROSION AROUND FAST HOLE. REMOVED AND REPLACED SEAT TRACK SECTION AT FACTORY BREAKS PER 53-05 FIG 4F SRM. (M) 2 L 7 2 4F A6WE 2002021300140 20020213 00140 WP 2002 2 13 AALA20020029 1 20020103 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND PREVIOUS REPAIR ON LEFT SIDE OF DORSAL FIN CRACKED AT INLET DUCT. STOP DRILLED AND INSTALLED DOUBLER PER SR M 53-30-00-02 AND SRM 53-01, FIG 2 SHEET 3. (M) 2 L 7 2 4F A6WE 2002021300148 20020213 00148 WP 2002 2 13 AALA20020038 1 20020111 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP ENTRY DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 237AA 49253 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002021300149 20020213 00149 NM 2002 2 13 AALA20020039 1 20020114 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AA 22327 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32H INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONNECTO RS AT SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002021300150 20020213 00150 NM 2002 2 13 AALA20020041 1 20020114 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 339AA 22336 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 33H INOPERATIVE. REPLACED CONNECTOR AN D PINS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002021300151 20020213 00151 NM 2002 2 13 AALA20020042 1 20020117 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 ORD - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT LIGHT COVER MISSING AND WIRES DISCONNECTED AT SET 7B. REPLACED EMERGENCY EXIT LIGHT COVER AND RECONNECTED WIRES TO SEAT 7B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002021300152 20020213 00152 NM 2002 2 13 AALA20020043 1 20020115 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 901AN 30258 MIA - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT LIGHT AT FIRST CLASS GALLEY MISSING. REPLACED EMERGENCY EXIT LIGHT A SSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002021400001 20020214 00001 NM 2002 2 14 0200296624 1 20020121 A 5414 SKIN BOEING 747 747251B 1384892 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 624US 21706 During "H" check found crack on NBR 3 pylon inboard skin lower left side at nacelle station 175. Repaired per EA 66-1873 14. 2 L 7 4 4F A20WE 2002021400002 20020214 00002 NM 2002 2 14 0200306308 1 20020123 A 5322 SUPPORT BOEING 747 747451 1384940 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 668US 24223 During "H" check found corrosion on support for main deck drain pan at BS 940 RBL 42. Repaired per EA 63-187821. 2 L 7 4 4F RT A20WE 2002021400003 20020214 00003 NM 2002 2 14 0200316308 1 20020122 A 5330 SKIN BOEING 747 747451 1384940 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 668US 24223 During "H" check found crack in fuselage skin at upper forward corner of aft cargo door cutout. Repaired per EA 63-18796 6 Rev C Section I. Established monitor inspection and will accomplish Section II at or prior to 21,009 cycles. Section I II of EA 63-187966 will be accomplished at or prior to 3000 cycles after accomplishment of Section II. 2 L 7 4 4F RT A20WE 2002021400027 20020214 00027 WP 2002 2 14 0200189762 1 20020203 A 3010 5919526507 DUCT DOUG DC9 DC941 302207N WP LT & RT WING MALFUNCTIONED A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 762NW 47395 SLAT DISAGREEMENT LIGHT ILLUMINATED UPON SLAT EXTENSION DURING APPROACH INTO MSP ACCOMPANIED WITH A ROLL TO THE LEFT. C OMPLIED WITH COM PROCEDURES AND AIRCRAFT LANDED SAFELY WITH SLATS RETRACTED. MAINTENANCE INITIALLY LUBRICATED THE 'T' D UCTS BUT HAVE SINCE ELECTED TO REPLACE BOTH 'T' DUCTS. ALSO, A COMPLETE INSPECTION OF THE SLAT OPERATION SYSTEM AND COM PONENTS HAS BEEN ACCOMPLISHED PER MOTR LOG. DUCT REPLACEMENT LOG HAS BEEN DEFERRED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002021400028 20020214 00028 WP 2002 2 14 ABXA010705 1 20020210 A 5753 BOLT DOUG DC8 DC863F 302198F WP T/E FLAP BROKEN A ABXA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 23 816AX 46093 ON APPROACH TO MIA, LOWERED FLAPS TO 23 DEGREES AT APPROXIMATELY 15 - 20 DEGREES, FLAPS HUNG UP ON INDICATION AND DISPLA YED A SLIGHT ASYMMETRY AND POPPED LOOSE WITH A BANGING EFFECT. TRAVEL OKAY TO 35 DEGREES. REPLACED BROKEN BOLT AND BEA RING SECURING ROLLER SUPPORT PLATE ASSEMBLY TO FLAP ROLLER HANGER ON RIGHT INBOARD FLAP SUPPORT TRACK. CYCLED FLAPS NUM EROUS TIMES, NO DEFECT NOTED. LUBRICATED FLAPS. 2 L 7 4 4F 4A25 2002021400029 20020214 00029 WP 2002 2 14 ABXA010706 1 20020210 A 3350 LIGHT DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 975AX 47512 EMERGENCY LAMP BY THE OVERHEAD FORWARD ATTENDANCE PANEL (THE AFT LAMP INOPERATIVE). REPOSITIONED CONTACT LEVEL POINT (D OOR CONTACT) AND RELAMPED IAW DC-9 AMM 33-55-00-4. 2 L 7 2 4F A6WE 2002021400030 20020214 00030 NM 2002 2 14 AWXA200200121 1 20020209 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 184AW 22651 PHX - EEL - C - DURING INSPECTION EMERGENCY EXIT LIGHT ON SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SEAT LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK C/W IAW T/C A1C33009. 2 L 7 2 4F RT A16WE 2002021400031 20020214 00031 EU 2002 2 14 AWXA200200124 1 20020211 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 WP 28 642AW 584 PHX - EEL - FLT 0794 - C - DURING TAXI TO RUNWAY AT IAH EN ROUTE TO PHX BOTH LT AND RT AFT DOOR EMERGENCY EXIT LIGHTS AN D AFT AISLE EMERGENCY ESCAPE PATH LIGHTS DID NOT ILLUMINATE. AIRCRAFT RETURNED TO GATE AND WAS LATER MAINTENANCE FERRIE D BACK TO PHX. IN PHX MAINTENANCE REPLACED CABIN EMERGENCY POWER SUPPLY UNIT 13WL AT ZONE 263, OPERATIONAL CHECK WAS GO OD. 2 L 7 2 4F RT A28NM 2002021400032 20020214 00032 SO 2002 2 14 C2XA02CL038 1 20020206 A 3234 7455501 CONTROL HANDLE EMB 145 EMB145 3260210 SO COCKPIT INTERMITTENT A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 14974 598 598 145161 CLE FLIGHT 3226 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE EICAS MESSAGE UPON GEAR RETRACTION. MAINTENANCE REPLACE D THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002021400033 20020214 00033 SO 2002 2 14 C2XA02CL039 1 20020208 A 2530 CBC16707 RECEPTACLE EMB 135 EMB135ER 3260203 SO GALLEY BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 17507 145215 CLE FLIGHT 3208 THE CREW REPORTED A BURNING SMELL AT THE COFFEE POT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 COFFEE POT RECEPTACLE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002021400034 20020214 00034 SO 2002 2 14 C2XA02CL042 1 20020209 A 7333 23052613 METER EMB 135 EMB135ER 3260203 SO NR 1 ENGINE INOPERATIVE A C2XA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 25504 2912 145186 CLE FLIGHT 3061 THE CREW REPORTED THE NR 1 FUEL FLOW INDICATOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 FUEL FLOW METER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002021400035 20020214 00035 SO 2002 2 14 C2XA02CL043 1 20020209 A 2150 8152402 ACM EMB 135 EMB135ER 3260203 SO A/C BAY SEIZED A C2XA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 25504 4868 3039 145186 THE CREW REPORTED A PACK 2 OVERLOAD EICAS MESSAGE. F/A REPORTED A BURNING SMELL IN CABIN. MAINTENANCE INSPECTED AND RE PLACED THE NR 2 AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002021400044 20020214 00044 SO 2002 2 14 C2XA02CL044 1 20020210 A 4930 CHECK VALVE EMB 135 EMB135LR 3260305 SO APU DIRTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 12519 145366 CLE THE CREW REPORTED ON APPROACH THE APU FAILED DURING START UP AND A FUEL SMELL WAS NOTED. ON THE GROUND THE APU DID START AND THE FUEL ODOR WAS PRESENT AGAIN. MAINTENANCE INSPECTED AND CLEANED THE APU COMBUSTER DRAIN CHECK VALVE. OPER ATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2002021400045 20020214 00045 SO 2002 2 14 C2XA02CL045 1 20020210 A 3320 7287501519 SOCKET EMB 135 EMB135ER 3260203 SO CABIN BURNED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 25504 145186 CLE FLIGHT 3443 THE CREW REPORTED A BURNING SMELL IN THE FRONT CABIN AREA. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FUR THER INCIDENT. MAINTENANCE INSPECTED AND FOUND A BURNT LIGHT SOCKET AT SEAT 2A. THE LIGHT FIXTURE WAS REPLACED AND OPE RATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002021400046 20020214 00046 SO 2002 2 14 C2XA02CL046 1 20020210 A 3397 WIRE EMB 145 EMB145ER 3260211 SO CABIN DAMAGED A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 14943 145040 CLE FLIGHT 3021 THE CREW REPORTED THE EMERGENCY LIGHTS WERE OUT AT ROWS 3-7. MAINTENANCE INSPECTED AND REPLACED THE EME RGENCY AISLE PATH LIGHT STRIP AT ROW 7. ALSO REPAIRED WIRING AT ROW 7 FOR THE LIGHT STRIP. MAINTENANCE ALSO REPLACED T HE EMERGENCY LIGHT BATTERY CHARGER. P/N 11-0049, S/N:11534 2 L 7 2 4F RT T00011AT 2002021400047 20020214 00047 EU 2002 2 14 C2XA02IA023 1 20020207 A 2120 ODOR AEROSP ATR42 ATR42320 8680930 EU COCKPIT DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 18814 103 IAH- THE CREW NOTED THAT A BURNING ODOR IN CABIN AND COCKPIT AFTER NR 2 ENGINE START UP AND AFTER NR 1 ENGINE SHUT DOWN . MAINTENANCE COULD NOT DUPLICATE ODOR ON GROUND, NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 H 7 2 4T RT A53EU 2002021400048 20020214 00048 NM 2002 2 14 ZW0A0201901 1 20020212 A 3350 65801003978970 CONNECTOR BOEING 757 7572Q8 1384972 NM DETACHED A ZW0A K NONE O OTHER UK UNKNOWN 1 CE 13 713TW 28173 DURING LAYOVER SERVICE, THE EGRESS LIGHTING STRIP FOUND INOP AT -D- LAVATORY DOOR. REPAIRED ELECTRICAL CONNECTION TO MAI N POWER SUPPLY FOR -D- LAV DOOR AND OPS CHECK NORMAL. CHECK-C 12/12/01. ---CLOSED--- 2 L 7 2 4F RT A2NM 2002021400049 20020214 00049 NM 2002 2 14 ZW0A0201902 1 20020212 A 3350 363674 LAMP BOEING 757 7572Q8 1384972 NM MISSING A ZW0A K NONE O OTHER UK UNKNOWN 1 CE 13 713TW 28173 DURING LAYOVER SERVICING, EGRESS LAMP MISSING AT FIRST CLASS SEAT - ROW 2L. INSTALLED MISSING LAMP, OPS CHECK NORMAL. CH ECK-C 12/12/01. ---CLOSED--- 2 L 7 2 4F RT A2NM 2002021400050 20020214 00050 SO 2002 2 14 C2XA02IA024 1 20020125 A 5315 14590141001 FLOORBEAM EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16963 7499 145116 IAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT HEAVE CORROSION ON THE LEFT HAND INBOARD FLOORBEAM AT FRAME 20 AT THE COMPOSITE FLOOR SUPPORT ATTACHMENT AREA. MAINTENANCE REPAIRED THE AREA, IAW EMB145 SRM 53-21-10, STEP NR 2 AND PAGE 204 , FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE UPON RELEASE FROM C-CHECK. 2 L 7 2 4F RT T00011AT 2002021400052 20020214 00052 EU 2002 2 14 MALA020153 1 20020209 A 3411 PITOT LINE SAAB SF340 340B 7860101 EU PITOT/STATIC SYS CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 435XJ 340B435 DURING FLIGHT 2985, RUDDER LIMITER LIGHT ILLUMINATED ALONG WITH ERRONEOUS READINGS FROM STANDBY AND F/O'S AIRSPEED INDIC ATORS. FLT CREW DECLARED EMERGENCY INTO MSP. HEAVY ICING CONDITIONS ENCOUNTERED THROUGHOUT FLIGHT. CXLD DUE TO WEATHE R. MAINTENANCE DRAINED AND PURGED NR 2 AND STBY PITOT SYSTEM WITH NITROGEN, NR 2 AND STBY PITOT SYSTEMS TEST GOOD IAW S F-340 MM CHAPTER 34, RUDDER LIMITER LIGHT ILLUMINATED BECAUSE OF STBY A/S SPLIT BETWEEN NR 1, RUDDER LIMITER TESTS GOOD. 2 L 7 2 4T RT A52EU 2002021400053 20020214 00053 EU 2002 2 14 MALA020154 1 20020209 A 2432 501122804 POWER SUPPLY SAAB SF340 SF340A 7850100 EU E/E BAY FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 76XJ 340A076 DURING FLIGHT NR 3299, EMERGENCY POWER OVERHEAD LIGHT ILLUMINATED. AIR RETURN TO DTW. MAINTENANCE REPLACED EMERGENCY P OWER PACK P/N 501-1228-04, SN/ON 8954, SN/OFF 8881. ALL CHECK GOOD. 2 L 7 2 4T RT A52EU 2002021400054 20020214 00054 WP 2002 2 14 MWEA020074 1 20020208 A 5411 995815441 STRAP DOUG DC9 DC932 3022066 WP LT PYLON SPAR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LEFT UPPER SPAR STRAP HAS CRACK INDICATION. MUST PERFORM MAGNETIC PARTICLE INSP IAW DC9 54A031 REV 8 FIG 3. REMOVED AN D REPLACED BN FASTENER AND CRACKED PYLON STRAP. 2 L 7 2 4F A6WE 2002021400055 20020214 00055 WP 2002 2 14 MWEA020077 1 20020208 A 5321 9910078871 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FLOORBOARD IS CHAFING ON SUBFLOOR BETWEEN AIRCRAFT CENTER LINE AND NR 2 SEAT TRACK STATION 200 TO 218. FABRICATED AND I NSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002021400056 20020214 00056 WP 2002 2 14 MWEA020078 1 20020208 A 5321 99100787 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FLOORBOARD IS CHAFING ON SUBFLOOR AT STATION 218 BETWEEN NR 3 AND 4 SEAT TRACKS. FABRICATED AND INSTALLED REPAIR DOUBLE R. 2 L 7 2 4F A6WE 2002021400057 20020214 00057 WP 2002 2 14 MWEA020079 1 20020208 A 5313 591140867 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 STATION 308 ON LONGERON 1 HAS A DEEP GOUGE FROM A STANDOFF. REMOVED AND REPLACED LONGERON SECTION AND SPLICES. 2 L 7 2 4F A6WE 2002021400058 20020214 00058 WP 2002 2 14 MWEA020080 1 20020208 A 5320 991556253 STIFFENER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 RIGHT UPPER VENTRAL DOOR CORNER STIFFENER BEAM ATTACH ANGLE IS CRACKED, LOCATED BETWEEN LONGERON 3 AND 4 RIGHT ON AFT PR ESSURE BULKHEAD FORWARD SIDE. REMOVED AND REPLACED STIFFENER. 2 L 7 2 4F A6WE 2002021400059 20020214 00059 WP 2002 2 14 MWEA020082 1 20020208 A 5311 3912237511 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 STATION 813 FRAME BELOW LONGERON 5 RIGHT HAS A DEEP GOUGE AND SOME SMALLER GOUGES. FABRICATED AND INSTALLED REPAIR FILL ER AND PLATE. 2 L 7 2 4F A6WE 2002021400060 20020214 00060 WP 2002 2 14 MWEA020089 1 20020208 A 5310 99577395 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FRAME STATION 945, SHEAR TIE HAS A CRACK LOCATED BETWEEN LONGERON 14 RIGHT AND 15 RIGHT. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2002021400061 20020214 00061 WP 2002 2 14 MWEA020091 1 20020208 A 5330 591142739 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FUSELAGE SKIN AFT OF FRAME STATION 945 HAS A CRACK LOCATED BETWEEN LONGERON 14 RIGHT AND 15 RIGHT. FABRICATED AND INSTA LLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002021400062 20020214 00062 WP 2002 2 14 MWEA020092 1 20020208 A 5310 991224316 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 SHEAR TIE AT BULKHEAD FRAME STATION 965 HAS A CRACK LOCATED BETWEEN LONGERON 16 RIGHT AND 17 RIGHT. FABRICATED AND INST ALLED SHEAR TIE. 2 L 7 2 4F A6WE 2002021400063 20020214 00063 WP 2002 2 14 MWEA020097 1 20020208 A 5320 5912995503 PAN DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 RIGHT AFT EMERGENCY EXIT DOOR JAMB IS GOUGED AT STATION 658 LONGERON 12 RIGHT. REMOVED AND REPLACED DOOR JAMB PAN. 2 L 7 2 4F A6WE 2002021400064 20020214 00064 WP 2002 2 14 MWEA020100 1 20020208 A 5320 9957727502 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 GOUGES ON TOP OF INTERCOSTAL AT STATION 726 ABOUT 10 INCHES RIGHT OF CENTER FLOOR SUPPORT CABIN AREA. FABRICATED AND IN STALLED DOUBLER STACK REPAIR. 2 L 7 2 4F A6WE 2002021400065 20020214 00065 WP 2002 2 14 MWEA020101 1 20020208 A 5320 9957727502 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 GOUGE ON TOP OF INTERCOSTAL AT STATION 708 ABOUT 10 INCHES RIGHT OF CENTER FLOOR SUPPORT CABIN AREA. FABRICATED AND INS TALLED DOUBLE ANGLE REPAIR. 2 L 7 2 4F A6WE 2002021400066 20020214 00066 WP 2002 2 14 MWEA020105 1 20020208 A 5712 991160916 RIB DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 RIGHT WING TANK -XRS 189 WING RIB LOWER CAP HAS LIGHT CORROSION ON UPPER INBOARD SURFACE FROM FORWARD SPAR TO STRINGER 1 9. BLENDED OUT AREA TO 1.0 INCH RADIUS IAW BAC TELEX MWX-ORD-02-00051H. 2 L 7 2 4F A6WE 2002021400067 20020214 00067 WP 2002 2 14 MWEA020106 1 20020208 A 5712 991160916 RIB DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 RIGHT WING TANK -XRS 189 WING RIB LOWER CAP HAS LIGHT CORROSION ON LOWER SURFACE FROM STRINGER 17 TO 13. BLENDED OUT AR EA TO 1.0 INCH RADIUS IAW DAC TELEX MWX-ORD-02-00051H. 2 L 7 2 4F A6WE 2002021400068 20020214 00068 WP 2002 2 14 MWEA020108 1 20020208 A 5712 5912070501 RIB DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LEFT WING FUEL TANK STATION XRS 164, RIB HAS LIGHT CORROSION IN AREA ON OUTBOARD SIDE FROM AFT SPAR TO STRINGER. COMPLI ED WITH PER BOEING TELEX MWX-ORD-02-00056H. 2 L 7 2 4F A6WE 2002021400069 20020214 00069 WP 2002 2 14 MWEA020113 1 20020208 A 5313 5911418101 STRINGER DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 CORROSION AND BARE METAL ON STRINGER AT STATION 604 TO 622. STRINGER IS LOCATED BETWEEN KEEL AND LONGERON 29 LEFT. REM OVED AND REPLACED HAT CHANNEL AND FASTENERS. 2 L 7 2 4F A6WE 2002021400070 20020214 00070 WP 2002 2 14 MWEA020126 1 20020212 A 5320 5956029223 SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 STATION 351 CEILING SUPPORT AT THE LEFT OUTBOARD END HAS CORROSION IN SEVERAL AREAS. FORMED AND INSTALLED NEW SUPPORT. 2 L 7 2 4F A6WE 2002021400071 20020214 00071 WP 2002 2 14 MWEA020127 1 20020212 A 5320 49125402 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 RIGHT LAV AREA HAS CRACKED FLOOR STRUT TO BULKHEAD FITTING LOCATED AT STATION 965 AND 3 FEET INBOARD OF LONGERON 18 RIGH T JUST BELOW FLOOR. REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 2002021400072 20020214 00072 NM 2002 2 14 P2EA2002M005 1 20020208 A 2731 FITTING BOEING 737 737230 1384401 NM ELEVATOR TAB LOOSE A P2EA K NONE E VIBRATION/BUFFET CR CRUISE 1 CE 05 124NJ 22122 AIRCRAFT VIBRATES AT 280 KIAS OR .73 MACH AND GREATER VIBRATION FELT ON COCKPIT FLOOR, CABIN FLOOR TO AFT GALLEY. INSPE CTED ELEVATOR AND ELEVATOR TAB AND FOUND THE LEFT HAND ELEVATOR TAB CONTROL ROD FITTING LOOSE. RETORQUED THE LEFT HAND ELEVATOR TAB CONTROL ROD FITTING PER BOEING MM 27-31-31. 2 L 7 2 4F RT A16WE 2002021400073 20020214 00073 WP 2002 2 14 AALA2002044 1 20020102 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND SEAT TRACK NR 3 HAS CORROSION AT STATION 1165 AND 1201. REPLACED NR 3 SEAT TRACK SECTION PER SRM 53-05. (M ) 2 L 7 2 4F A6WE 2002021400074 20020214 00074 WP 2002 2 14 AALA2002045 1 20020107 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND STATION 522 TO 530 RIGHT SIDE OF CARGO CUSP CORRODED AROUND FORWARD LIGHTNING HOLE OF BAY, BOTTOM SIDE OF CU SP. INSTALLED DOUBLER PER AARD 53-00-02. (M) 2 L 7 2 4F A6WE 2002021400075 20020214 00075 WP 2002 2 14 AALA2002046 1 20020111 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND CORNER STIFFENER CORRODED ON AFT SIDE OF STATION 1155 FRAME AT FORWARD LOWER CORNER OF CARGO DOOR WAY. REMO VED AND REPLACED CORNER STIFFENER ON AFT SIDE OF STATION 1155 FRAME AT FORWARD LOWER CORNER OF AFT CARGO DOOR WAY AS EPR SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2002021400077 20020214 00077 WP 2002 2 14 AALA2002048 1 20020102 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND HOLE IN SUBFLOOR UNDER CENTER FLIGHT COMPARTMENT FLOORBOARD, STATION 160 LBL 5 INCHES. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3. (M) 2 L 7 2 4F A6WE 2002021400078 20020214 00078 WP 2002 2 14 ABXA010713 1 20020129 A 5300 591359577 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 FUSELAGE FRAME STATION 1152 WAS CRACKED AT LONGERON 15 RIGHT. REPAIRED CRACKED SECTION OF FRAME AT STATION 1152 LONGERON 15 RIGHT IAW DC-9 SRM 53-03. 2 L 7 2 4F A6WE 2002021400079 20020214 00079 WP 2002 2 14 ABXA010714 1 20020129 A 5210 59100817 DOOR DOUG DC9 DC941 302207N WP EXT. FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 LEFT ENTRY DOOR LOWER AFT CORNER SKIN WAS CRACKED. REPAIRED ENTRY DOOR SKIN IAW DC-9 SRM 52-05. 2 L 7 2 4F A6WE 2002021400080 20020214 00080 WP 2002 2 14 ABXA010717 1 20020130 A 5313 59203192 LONGERON DOUG DC9 DC941 302207N WP FWD. CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 LONGERON 30 CRACKED AT LEFT FLANGE STATION 232 UNDER SPLICE. REPAIRED AREA IAW DC-9 REA D953-43229. 2 L 7 2 4F A6WE 2002021400081 20020214 00081 WP 2002 2 14 AALA2002049 1 20020104 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND CORROSION ON NR 6 SEAT TRACK. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK NR 6 FROM STATION 215-265 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002021400082 20020214 00082 WP 2002 2 14 AALA2002050 1 20020104 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND NR 6 SEAT TRACK HAS AREA OF CORROSION TOP SURFACE OF LUGS AND IN CHANNEL STATION 259. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK NR 6 FROM STATION 215-265 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002021400083 20020214 00083 WP 2002 2 14 AALA2002051 1 20020114 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND CORROSION ON AFT CARGO DOOR LOWER BEAM FROM STATION 1160-1193. INSTALLED FULL LENGTH DOUBLER NR 3 AS PER AA RD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2002021400084 20020214 00084 NM 2002 2 14 02FDEA00099 1 20020213 A 2613 SHIM BOEING 727 727227 1384078 NM STARTER DUCT BROKEN A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 481FE 21463 02-46 #1 ENG STRUT OVERHEAT LIGHT ILLUM ON CLBOUT. R&R SHIM ON STARTER DUCT. OPS CK GOOD. 2 L 7 3 4F A3WE 2002021400085 20020214 00085 EA 2002 2 14 COMA0260093 1 20020211 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA VERT STAB MALFUNCTIONED A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 927CA 6939 7031 FLIGHT 5368 CONFIG STAB WARNING DURING T/O.REPLACED THE STABILIZER TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 2002021400086 20020214 00086 EA 2002 2 14 COMA0260094 1 20020212 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 984CA 7171 FLIGHT 9872 FLAPS FAIL CAUTION MESSAGE.COULD NOT DUPLICATE, INTEROGATED FLAP COMPUTER, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2002021400088 20020214 00088 WP 2002 2 14 AALA2002053 1 20020109 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND LINE RUBBING ON 1431 CANT FRAME RIGHT SIDE INBOARD L15R. BLENDED OUT DAMAGED AREA, DYE CHECKED, FABRICATED AND INSTALLED DOUBLER PER 53-10-00-15. (M) 2 L 7 2 4F A6WE 2002021400089 20020214 00089 EA 2002 2 14 COMA0260095 1 20020212 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 403CA 7428 FLIGHT 5297 FLAPS FAILED AT 20 DEGREES DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002021400090 20020214 00090 WP 2002 2 14 AALA2002054 1 20020102 A 5310 BEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 589AA 53252 TUL - FOUND AFT CARGO DOOR BEAM HAS CORROSION FROM 1160 TO 1207. BLENDED OUT CORROSION PER ESO 80559. (M) 2 L 7 2 4F RT A6WE 2002021400091 20020214 00091 WP 2002 2 14 AALA2002055 1 20020109 A 5330 TRIPLER DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TUL - FOUND RIGHT MLG W/W CUT OUT, AFT OUTBOARD TRIPLER CRACKED. INSTALLED TRIPLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002021400105 20020214 00105 NM 2002 2 14 QXEA0200156 1 20020212 A 2420 DHC103024600C INVERTER DHAV DHC8 DHC8202 2809007 NM LEAKING A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 347PH * 7 480 SEA- PRIMARY INVERTER LEAKING COOLING OIL AND SMELLS LIKE FISH. REMOVED AND REPLACED PRIMARY INVERTER. OPERATIONAL CHECK S GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002021400115 20020214 00115 EU 2002 2 14 AWXA200200132 1 20020210 A 5315 D53112706200 SEAT TRACK AIRBUS 320 A320231 3930325 EU CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 271 YWG - MAJOR REPAIR - "C" - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SEAT TRACK Y765 R/H FR 16. MAINTENANC E REMOVED FLOOR SEAT TRACK Y765 R/H, FABRICATED NEW FLOOR SEAT TRACK AND INSTALLED REPAIR IAW DWG 53112782. 2 L 7 2 4F RT A28NM 2002021400116 20020214 00116 EU 2002 2 14 AWXA200200133 1 20020210 A 5315 D531112836 SEAT TRACK AIRBUS 320 A320231 3930325 EU CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 271 YWG - MAJOR REPAIR - "C" - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT SEAT TRACK Y254 L/H FR 20. MA INTENANCE REMOVED CORROSION FROM FLOOR SUPPORT SEAT TRACK AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 53-11-14. R EMOVED FLOOR SUPPORT SEAT TRACK Y254 L/H, FABRICATED NEW FLOOR SUPPORT SEAT TRACK AND INSTALLED REPAIR IAW DWG 53112836. 2 L 7 2 4F RT A28NM 2002021500001 20020215 00001 2002 2 15 SWAA020324 4 20020212 A 2565 D31591478 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOW A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 642WN 27715 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021500002 20020215 00002 NM 2002 2 15 SWAA020325 1 20020209 A 5530 BAC1514 TEE CHORD BOEING 737 7375H4 138449D NM VERTICAL FIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D CHECK, FOUND VERTICAL FIN LT TEE CHORD CRACKED AT RUDDER STA 13.33. REPAIRED TEE CHORD PER SRM. 2 L 7 2 4F RT A16WE 2002021500003 20020215 00003 NM 2002 2 15 SWAA020327 1 20020212 A 5312 6546529 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED (2 EA) AT STR 14R, BS'S 340 AND 360. REPAIRED SHEAR TIE PER SRM . 2 L 7 2 4F A16WE 2002021500004 20020215 00004 NM 2002 2 15 SWAA020329 1 20020212 A 5753 6546435 FLAP BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D CHECK, FOUND LT OTBD AFT T/E FLAP DELAMINATED AT AFT CORNER. REPAIRED T/E FLAP PER SRM. 2 L 7 2 4F RT A16WE 2002021500005 20020215 00005 NM 2002 2 15 SWAA020330 1 20020212 A 5312 6545409 WEB BOEING 737 7373H4 1384600 NM LT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESS WEB CRACKED IN CEILING AT BS 663, LBL 33. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002031500153 20020315 00153 NM 2002 3 15 SWAA020334 1 20020212 A 5610 5717623121 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 627SW 27935 DECLARED EMERGENCY, DIVERSION, L2 COCKPIT WINDOW CRACKED IN FLIGHT. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2002021500006 20020215 00006 WP 2002 2 15 0200279971 1 20020210 A 3010 5919526507 DUCT DOUG DC9 DC931 3022065 WP L/E SLAT BINDING A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 9335 47337 FLIGHT DIVERTED TO AN AIRPORT WITH A LONGER RUNWAY WHEN THE CREW DETERMINED THAT THE LEFT WING SLATS WOULD NOT EXTEND. THE AIRCRAFT DID ROLL TO THE LEFT AND THE SLAT DISAGREEMENT LIGHT DID ILLUMINATE. FOLLOWED COM PROCEDURES AND MADE AN U NEVENTFUL LANDING AT GRR AT 86,000 LBS AND 253 KTS. MAINTENANCE FOUND THE LEFT 'T' DUCT LOOSE AND BINDING. REPLACED TH E 'T' DUCT. LEAK AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002021500007 20020215 00007 NM 2002 2 15 0200286306 1 20020204 A 3350 SOCKET BOEING 747 747451 1384940 NM CABIN DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 666US 23821 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS ON THE RIGHT SIDE OF ZONE 'D' INOPERATIVE. REPAIRED SOCKET ASSEMBL Y. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002021500008 20020215 00008 EU 2002 2 15 02FDEA00096 1 20020212 A 2612 FIRE WARNING AIRBUS 300 A300F4605R 3930327 EU COCKPIT ACTIVATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 662FE 761 MAIN CARGO FIRE WARNING AFTER LIFTOFF. 2 L 7 2 4F RT A35EU 2002021500009 20020215 00009 WP 2002 2 15 02FDEA00097 1 20020212 A 3150 CONTROL BOX DOUG DC10 DC1010 3022110 WP COCKPIT FAULTY A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 375FE 46613 GREEN REVERSER THRUST LIGHT ILLUM AFTER APPLYING T/O POWER. REMOVED AND REPLACED MASTER WARNING CONTROL BOX PER DCN MM 33-15-01-2. OPS CHECK NORMAL. 2 L 7 3 4F A22WE 2002061900175 20020619 00175 WP 2002 6 19 02FDEA00098 1 20020213 A 7830 PDU DOUG DC10 DC1010 3022110 WP THRUST REVERSER FAULTY A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 375FE 46613 UPON TAKEOFF PWR THE GREEN REVERSER LIGHT FLICKERED THEN ILLUMINATED STEADY, IT W/N EXTINGUISHED UNTIL PWR REDUCED TO ID LE. SYS TO BAD DRIVE UNIT. REMOVED AND REPLACED PDU PER DC10-10 MM 78-31-01-2, OPS CHECK GOOD. 2 L 7 3 4F A22WE 2002021500012 20020215 00012 2002 2 15 371PA0001 4 20020207 A 2210 AUTOPILOT SYS BOEING 737 737306 NM COCKPIT MALFUNCTIONED A PIDA K NONE F FLT CONT AFFECTED DE DESCENT 1 SO 05 371PA 23543 AUTO PILOT EXCEEDING COMMANDED SPEEDS IN VNAV PATH, VNAV SPEED, AND LVL CHG. IT PERFORMS UNCOMMANDED LEVEL OFF AND CLIM BS DURING DESCENT (LVL CHG AND VNAV) AUTO THROTTLES NOT DRIVING CLOSED DURING LVL CHG (THIS IS AN INTERMITTENT PROBLEM). 2 L 7 2 4F RT A16NE 2002021500014 20020215 00014 NE 2002 2 15 ABXA010707 2 20020208 A 7321 71128726 FUEL CONTROL DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE FAILED A ABXA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 23 811AX 753 46113 671119 DURING DESCENT, THE NR 4 ENGINE FAILED TO ACCELERATE. EPR, EGT, RPM AND F/F DECAYED. OIL PRESSURE WAS NORMAL (WINDMILL ING). PERFORMED CHECKLIST - NO HELP. DURING LEVEL OFF WITH INCREASED AIRSPEED - NEGATIVE RELIGHT. PERFORMED ENGINE SH UTDOWN ACTIONS CHECKLIST. REPLACED PRESSURE RATIO BLEED CONTROL VALVE IAW DC-8 MM 75-31-1. REPLACED NR 4 ENGINE DRIVEN FUEL PUMP IAW DC-8 MM 73-10-02, NO HELP. ENGINE DRIVEN FUEL PUMP SAFTIED. INSTALLED FUEL CONTROL UNIT IAW DC-8 MM 73- 21-1. OPS AND LEAK CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 2002021500018 20020215 00018 WP 2002 2 15 ABXA010708 1 20020128 A 3231 3927498503 ROD END DOUG DC9 DC941 302207N WP RT MLG DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 RIGHT MAIN LANDING GEAR OUTBOARD DOOR LINKAGE ROD (FROM CRANK TO DOOR) CORRODED AT DOOR END. RIVET WAS CORRODED, RUST B LEEDING FROM ROD END, PLAY WHERE ROD END ATTACHES TO ROD. REPLACED DOOR ROD PANEL IAW DC-9 AMM. 2 L 7 2 4F A6WE 2002021500019 20020215 00019 WP 2002 2 15 ABXA010709 1 20020128 A 5320 49157601 FITTING DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 CRACK IN THE FORWARD SERVICE DOOR HOLD OPEN CUP. REPLACED THE FORWARD SERVICE DOOR HOLD OPEN CUP IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002021500020 20020215 00020 WP 2002 2 15 ABXA010710 1 20020128 A 5330 59134213 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 SKIN CRACKED AT LEFT REAR CUTOUT FOR LEFT AFT NOSE GEAR DOOR. REPAIRED IAW DC-9 SRM 53-01. INSTALLED ROD IAW DC-9 MM 2 0-16-0. 2 L 7 2 4F A6WE 2002021500021 20020215 00021 WP 2002 2 15 ABXA010711 1 20020128 A 5280 59107839 DOUBLER DOUG DC9 DC941 302207N WP LT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 REPAIR CRACKED ON FORWARD UPPER CORNER OF INBOARD GEAR DOOR. REPAIRED AREA IAW DC-9 SRM 52-05. REINSTALLED INBOARD MAI N LANDING GEAR DOOR IAW DC-9 MM 32-12-01. 2 L 7 2 4F A6WE 2002021500022 20020215 00022 WP 2002 2 15 ABXA010712 1 20020128 A 5330 5911412221 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 FORWARD LOWER CORNER CUTOUT HAD APPROXIMATELY .1250 INCH CRACK. REPAIRED DAMAGED AREA IAW DC-9 SRM 51-10-2. 2 L 7 2 4F A6WE 2002021500023 20020215 00023 WP 2002 2 15 ABXA010715 1 20020130 A 5320 991558250 STIFFENER DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 UPPER HORIZONTAL STIFFENER CRACKED ON OUTBOARD END FORWARD FACE OF AFT PRESSURE BULKHEAD RIGHT SIDE. REPAIRED STIFFENER IAW DC-9 SSRM K05159. 2 L 7 2 4F A6WE 2002021500024 20020215 00024 WP 2002 2 15 ABXA010716 1 20020130 A 5320 99105012 WEB DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 CUSP WEB CRACKED AT STATION 239 RBL 56. REPAIRED AREA IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002021500025 20020215 00025 WP 2002 2 15 ABXA010718 1 20020206 A 5712 99193014 BULKHEAD DOUG DC9 DC941 302207N WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 RIGHT WING LEADING EDGE BULKHEAD CRACKED AT LOWER FASTENER ON INBOARD SIDE OF NR 2 SLAT TRACK. REPAIRED AREA IAW DC-9 R EA D957-43261. 2 L 7 2 4F A6WE 2002021500026 20020215 00026 EA 2002 2 15 CA020104020 1 20020104 A 5711 75710099 SPAR CAP DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA HAMSTD 24PF 24PF305 GL LT WING CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 34913 34913 (CAN) DURING "C" CHECK AND CORROSION INSPECTION THE LT REAR SPAR CAP AND SPAR AREA ABOVE THE SPAR CAP WAS FOUND CHAFED. THE CHAFING WAS CAUSED BY SPIRAL WRAP WOUND AROUND A WIRE BUNDLE THAT RUNS ACROSS THE FACE OF THE REAR SPAR. 2 H 7 4 4T 4 T A20EA E4EA 6 C P1NE 2002021500028 20020215 00028 WP 2002 2 15 ABXA010719 1 20020212 A 3310 RHEOSTAT DOUG DC9 DC941 302207N WP COCKPIT MALFUNCTIONED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 967AX 47509 BURNING SMELL FROM FIRST OFFICER'S YOKE FOLLOWED BY MAP AND BRIEFCASE CIRCUIT BREAKER TRIPPING. REPLACED FIRST OFFICER' S BRIEFCASE RHEOSTAT IAW DC-9 AMM 33-10-00-2. 2 L 7 2 4F A6WE 2002021500031 20020215 00031 WP 2002 2 15 ABXA010720 1 20020213 A 3310 CLIP DOUG DC9 DC941 302207N WP COCKPIT DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 967AX 47509 SMOKE FROM FIRST OFFICER'S YOKE CLIPBOARD LIGHT. TRIPPED MAP AND BRIEFCASE LIGHT CIRCUIT BREAKER. REMOVED METAL CLIP F ROM FIRST OFFICER'S CLIPBOARD IAW DC-9 MM 33-10-00. 2 L 7 2 4F A6WE 2002021500032 20020215 00032 NM 2002 2 15 CA020107001 1 20020101 A 2913 570347 PUMP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 14356 10930 (CAN) AFTER TAKEOFF NR 2 ENGINE DRIVEN HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED, AIRCRAFT RETURNED TO DEPARTURE STATION FOR NORMAL LANDING. NR 2 EDP REPLACED, AIRCRAFT RETRURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002021500033 20020215 00033 NM 2002 2 15 CA020108001 1 20020107 A 3244 TIRE BOEING 657376140 BOEING 737 737204 1384458 NM PWA JT8 JT8D15 52051 NE MLG FAILED W A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CA BFG3564 (CAN) A/C ON TAKEOFF CLIMB RADIOED MAINT CONTROL THAT ATC REPORTED TIRE DEBRIS ON RWY AFTER THEIR DEPARTURE: CREW ALSO R EPORTED SEVERE WHEEL VIBRATION THROUGH AIRFRAME UPON ROTATION. A/C RETURNED ON SUSPICION OF TIRE FAILURE. FLY BY CONDU CTED WITH NO NOTABLE DAMAGE TO REPORT. CREW CARRIED OUT ABNORMAL 'BLOWN MAIN WHEEL & LANDED UNEVENTFULLY. CFR ON STAN DBY. MAINT INSPECTION REVEALED NR 4 MAIN WHEEL TIRE RETREAD & SIDEWALL PARTIALLY MISSING. MAIN WHEEL TIRE PRESSURE S TILL INTACT. MAINT ALSO NOTED TRAILING EDGE DAMAGE TO INBOARD FLAP. A/C REMOVED FROM SERVICE & IS CURRENTLY UNDER GOIN G REPAIR. 2 L 7 2 4F 4 F A16WE E2EA 2002021500042 20020215 00042 NM 2002 2 15 AWXA200200128 1 20020213 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 806AW 1056 PHX - EEL - C - DURING INSPECTION OF EMERGENCY LIGHT SYSTEM RT OVERWING EXIT LIGHTS DID NOT ILLUMINATE. MAINTENANCE REP LACED EMERGENCY POWER SUPPLY UNIT 12WL WITH BATTERY PACK IAW AMM 33-51-38-401. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002021500045 20020215 00045 EA 2002 2 15 CA020110005 1 20020107 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER CR CRUISE 1 CA (CAN) AIRCRAFT WAS ENROUTE TO GRR. CREW REPORTED CO-PILOT'S WINDSHIELD SHATTERED JUST BEFORE DESCENT AT 28,000 FEET. MA INTENANCE CREW REMOVED AND REPLACED CO-PILOT'S WINDSHIELD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500046 20020215 00046 EA 2002 2 15 CA020110006 1 20020107 A 5610 NP1393221 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER LD LANDING 1 CA 10382 (CAN) ON LANDING ROLL, THE LEFT SIDE WINDSHIELD SHATTERED. MAINTENANCE WAS SENT. THEY REMOVED AND REPLACED THE PILOT'S SIDE WINDOW. CHECKS CARRIED OUT AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500047 20020215 00047 SO 2002 2 15 C2XA02IA027 1 20020212 A 3260 MS3476L833S CONNECTOR EMB 120 EMB120ER 3260203 SO LT MLG DIRTY A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 17728 120182 IAH- DURING FLIGHT 3580 THE CREW NOTED THE LEFT MAIN GEAR SYSTEM A-GREEN LIGHT ILLUMINATED IN FLIGHT SEVERAL TIMES WITH GEAR UP. MAINTENANCE CLEANED THE LEFT MAIN SYSTEM-A CANNON PLUG, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYS TEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002021500048 20020215 00048 EU 2002 2 15 C2XA02IA028 1 20020211 A 3260 D229240003 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU NLG OUT OF ADJUST A C2XA K NONE N FALSE WARNING AP APPROACH 1 SW 27 97841 280 IAH- DURING FLIGHT 3798 THE CREW NOTED THAT NOSE GEAR UNSAFE LIGHT ON AFTER GEAR EXTENSION ON APPROACH, SYSTEM NR 1. S YSTEM NR 2 OK. MAINTENANCE ADJUSTED THE NOSE GEAR PRIMARY DOWNLOCK PROXIMITY SWITCH, PERFORMED A OPERATIONAL CHECK OF T HE LANDING GEAR SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002021500049 20020215 00049 NM 2002 2 15 CALA0200069 1 20020212 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 328-344, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT W AS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 2002021500050 20020215 00050 NM 2002 2 15 CALA0200070 1 20020212 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 294-312, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SR M 51-70-12. 2 L 7 2 4F RT A16WE 2002021500051 20020215 00051 SO 2002 2 15 CHQ000116 1 20020211 A 3240 WARNING SYSTEM EMB 145 EMB145 3260210 SO COCKPIT ACTIVATED A CHQA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 11 271 145305 OUTBOARD BRAKE FAIL MESSAGE ON EICAS. 2 L 7 2 4F RT T00011AT 2002021500052 20020215 00052 EA 2002 2 15 CA020110007 1 20020109 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) DURING CLIMB OUT, THE CO-PILOT'S WINDOW CRACKED. RIGHT SIDE WINDOW REPLACED AS PER AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500053 20020215 00053 EA 2002 2 15 CA020110008 1 20020109 A 5610 NP1393212 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W H DEACTIVATE SYST/CIRCUITS O OTHER DE DESCENT 1 CA 14422 (CAN) DESCENDING THROUGH 14,000 FT THERE WAS AN ELECTRICAL FLASH FOLLOWED BY THE F/O'S WINDSHIELD "CRACKING / SHATTERI NG". THE WINDSHIELD HEAT WAS ON AT THE TIME. R&R'D WINDSHIELD AND HEAT CONTROLLER ACCORDING TO AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500054 20020215 00054 NE 2002 2 15 CA020110009 2 20020109 A 7261 B-NUT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT ENGINE LOOSE W E A ENGINE SHUTDOWN UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 CA (CAN) LEFT ENGINE OIL TEMP PEAKED AT 175 DEG FOLLOWED BY LOW OIL PRESSURE AT 22-25 PSI. PERFORMED IN-FLIGHT SHUTDOWN. ENGINE HAD JUST BEEN INSTALLED DIRECTLY FROM GE OVERHAUL. FOUND OIL 3-4 QTS LOW. SENT MECHS TO ALB. MECHS FOUND OIL A LL OVER THE ENGINE AND COMING OUT THE TAILPIPE. THOUGHT TO BE LEAKING FROM 7 O'CLOCK 'B' SUMP STRUT. SENT GE MECHS TO T/S. FOUND A B-NUT BACKED OFF THREE TURNS. RE-SECURED BUT ON SUBSEQUENT ENGINE RUN, NO OIL PRESSURE INDICATED. SWAP PED TRANSDUCERS FROM RIGHT TO LT ENGINE, STILL NO READING. NO OTHER INFO AVAILABLE AT THIS TIME. THE LT ENGINE HAS BEEN CHANGED AND AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500055 20020215 00055 EU 2002 2 15 CHQ000117 1 20020211 A 2611 WARNING LIGHT SAAB SF340 SF340A 7850100 EU COCKPIT ILLUMINATED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 125 125 AVIONICS SMOKE LIGHT ON CLIMBOUT. 2 L 7 2 4T RT A52EU 2002021500056 20020215 00056 EA 2002 2 15 CA020110011 1 20020109 A 2913 PV304448 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYD SYSTEM LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) DURING FLIGHT THE CREW NOTED SYSTEM NR 2 LEVEL TO BE OWN TO 30 PERCENT. FLIGHT DIVERTED. MAINTENANCE DETERMINED THAT THE NR 2 EDP WAS LEAKING. NR 2 EDP WAS REMOVED AND REPLACED. SYSTEM WAS SERVICED. RUNS AND LEAK CHECKS CARRIED OUT. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500057 20020215 00057 EA 2002 2 15 CA020110015 1 20020110 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA 14524 (CAN) PILOTS LEFT SIDE WINDOW CRACKED IN CRUISE.REMOVED AND REPLACED LEFT SIDE WINDOW WITH SERVICEABLE UNIT IAW AMM 56-1 2-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500058 20020215 00058 WP 2002 2 15 CA020110016 1 20020107 A 3260 UPLOCK SENSOR LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE MLG OUT OF ADJUST W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) GEAR DOWN APPROACH YYZ, HAD THREE GREEN & RED DOOR LIGHT, FLIGHT ENGINEER LT GEAR OR DOOR LIGHT. FOLLOWED ABNORM AL PROCEDURE 03:18:03 (ALL LIGHTS WENT NORMAL ON SHORT FINAL). LT MAIN GEAR INBOARD UPLOCK SENSOR ADJUSTED I.A.W. M. M.32-61-07. 2 L 7 3 4F 4 F A23WE E12EU 2002021500059 20020215 00059 EA 2002 2 15 CA020110017 1 20020110 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERON FAILED W D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA (CAN) FLIGHT 5280 FROM AVP TO CVG ON TAXI OUT SPOILERON FAULT MSG ILLUMINATED AND UNCOMMANDED SPOILERON DEPLOYMENT. CB4C N CIRCUIT BREAKER POPPED IN AVIONICS BAY - SENT MECH & PARTS ON ROAD TRIP. SUBSTITUTED AIRCRAFT 7539. R&R'D LEFT SPOILER ON OUTBOARD PCU. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500060 20020215 00060 NM 2002 2 15 02FDEA00102 1 20020106 A 5320 INTERCOSTAL BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 522 INTERCOSTAL CRACKED AT BS 970 BETWEEN STR 26R AND 27R. R&R INTERCOSTAL PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002021500061 20020215 00061 NM 2002 2 15 02FDEA00105 1 20020104 A 2780 651622193 SLAT BOEING 727 727277 138408S NM LEFT WING CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 246 #4 LEAD EDGE SLAT HAS 3 CRACKED RIBS BETWEEN WS 383.5 AND 436.5. R&R SLAT PER MM 27-81-811-4. 2 L 7 3 4F RT A3WE 2002021500062 20020215 00062 NM 2002 2 15 02FDEA00106 1 20020104 A 5260 B275203601 STEP BOEING 727 727277 138408S NM FUSELAGE LOWER CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 258 CORROSION ON #5 AIRSTAIR STEP. R&R STEP PER SR 27-52-003 & SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002021500063 20020215 00063 NM 2002 2 15 02FDEA00107 1 20020106 A 5320 SHEAR TIE BOEING 727 727277 138408S NM FUSELAGE LOWER CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 408 CORROSION ON SHEAR TIE BS 720A BETWEEN STR 25R AND 26R. R&R SHEAR TIE PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002021500064 20020215 00064 NM 2002 2 15 02FDEA00108 1 20020106 A 5320 INTERCOSTAL BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 411 CRACKED INTERCOSTAL BS 540 TO 560 AT STR 25L. R&R INTERCOSTAL PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2002021500065 20020215 00065 NM 2002 2 15 02FDEA00109 1 20020106 A 5320 INTERCOSTAL BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 412 CRACKED INTERCOSTAL BS 550 AT STR 27L. R&R INTERCOSTAL PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2002021500066 20020215 00066 NM 2002 2 15 02FDEA00110 1 20020106 A 5347 SEAT TRACK BOEING 727 727277 138408S NM FUSELAGE TOP CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 414 SEAT TRACK #4 CRACKED AT BS 400. R&R TRACK PER SRM 53-10-5. 2 L 7 3 4F RT A3WE 2002021500067 20020215 00067 NM 2002 2 15 02FDEA00111 1 20020106 A 5322 ANGLE BOEING 727 727277 138408S NM FUSELAGE LOWER CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 424 WALL SUPPORT ANGLE CORRODED BS 1166 AT WL 178. R&R ANGLE PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002021500068 20020215 00068 NM 2002 2 15 02FDEA00113 1 20020108 A 5313 STRINGER BOEING 727 727277 138408S NM FUSELAGE LOWER CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 815 STR 28L CORRODED AT BS 540. R&R STRINGER PER SRM 51-10-3. 2 L 7 3 4F RT A3WE 2002021500069 20020215 00069 NM 2002 2 15 02FDEA00114 1 20020108 A 5322 ANGLE BOEING 727 727277 138408S NM FUSELAGE LOWER CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 848 BAGGAGE BIN WALL SUPPORT ANGLE CORRODED AT BS 720D BETWEEN STR 24L & 25L. R&R ANGLE PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002021500070 20020215 00070 NM 2002 2 15 02FDEA00115 1 20020108 A 5347 TRACK BOEING 727 727277 138408S NM FUSELAGE TOP CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 973 #7 CARGO TRACK CRACKED BETWEEN BS 690 AND 700. R&R TRACK PER SRM 53-10-5. 2 L 7 3 4F RT A3WE 2002021500071 20020215 00071 NM 2002 2 15 P2EA2002M006 1 20020210 A 4950 CLAMP BOEING 737 73725A 1384481 NM APU LOOSE A P2EA O OTHER J WARNING INDICATION CR CRUISE 1 CE 05 239TA 23789 APU FIRE LIGHT CAME ON IN FLIGHT. FIRE HANDLE PULLED AND FIRE BOTTLE DISCHARGED. LIGHT WENT OUT AFTER 10 MINUTES. FOU ND AN APU BLEED AIR DUCT WITH LOOSE CLAMP THAT WAS BLOWING ON THE FIRE DETECTION LOOP. TIGHTENED CLAMP, OPS CHECKS NORM AL. 2 L 7 2 4F RT A16WE 2002021500072 20020215 00072 GL 2002 2 15 CA020110019 2 20020107 A 7321 8061889 MEC AIRBUS 310 A310300 3930305 EU GE CF6 CF680C2* GL NR2 ENGINE FAILED W O OTHER J WARNING INDICATION DE DESCENT 1 CA (CAN) DURING TAKE OFF NR 2 ENGINE SPEED UP WAS SLOW ON APPROACH NR 2 ENGINE WAS 15 TO 20 PERCENT LOWER THAN NR 1 ENGINE AND THROTTLE LEVERS WERE EVEN. MAIN ENGINE CONTROL REPLACED. LEAK CHECK CARRIED OUT AND IDLE RUN CARRIED OUT, ALL PA RAMETERS CHECKED WITHIN LIMITS. 2 L 7 2 4F 4 F RT A35EU E23EA 2002021500074 20020215 00074 SO 2002 2 15 C2XA02CL048 1 20020213 A 3350 GE1317 BULB EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14939 145030 DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT LIGHT AT SEAT 12A WAS FOUND INOPERATIVE.MAINTENANCE REPLACED EMERGENCY EXI T LIGHT BULB.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002021500075 20020215 00075 WP 2002 2 15 P2EA2002M007 1 20020212 A 2130 CLAMP DOUG DC9 DC982 3022082 WP A/C BAY OUT OF POSITION A P2EA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 CE 05 130NJ 49222 AIRCRAFT BEGAN LOSING PRESSURIZATION AT FLIGHT LEVEL 240. CABIN ALTITUDE LIGHT ILLUMINATED, LOOKED UP AND LEFT PACK IND WENT TO 0 PSI. DESCENT WAS INITIATED TO 10,000 MSL. BEFORE ARRIVING TO 10,000 MSL CABIN MASKS DEPLOYED, FLOW LIGHT WA S ILLUMINATED. CHECK LIST WAS ACCOMPLISHED AND AIRCRAFT PRESSURE WAS REGULATED WITH MANUAL PRESSURIZATION CONTROL. AIR CRAFT WAS RETURNED TO MCI. CABIN WAS PRESSURIZING THROUGH 10,000 MSL. UPON INSPECTION, FOUND THE RIGHT HAND ACM WITH C LAMP OUT OF PLACE. RESECURED CLAMP IAW BOEING MM 20-00-00 AND OPS CHECK PRESSURIZATION SYSTEM IAW BOEING MM 21-30-0, OP S CHECKED NORMAL. 2 L 7 2 4F A6WE 2002021500076 20020215 00076 NM 2002 2 15 02FDEA00116 1 20020117 A 5230 SKIN BOEING 727 727277 138408S NM FUSELAGE TOP CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 1228 6 FASTENER HOLES CRACKED FOR MCD UPR HINGE ON FUSELAGE BETWEEN 480 & 620, STR 2L & 3L. R&R PER EO 7-5230-7-5000. 2 L 7 3 4F RT A3WE 2002021500077 20020215 00077 NM 2002 2 15 02FDEA00117 1 20020130 A 5530 65168036 TIE BOEING 727 727277 138408S NM STABILIZERS CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 1259 VERT STAB TENSION TIE FITTING RH AFT VERTICAL BOLT HOLE CORRODED. R&R TIE PER MM 55-30-051-4. 2 L 7 3 4F RT A3WE 2002021500078 20020215 00078 NM 2002 2 15 02FDEA00119 1 20020117 A 5320 INTERCOSTAL BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 1306 INTERCOSTAL CRACKED AT BS 950 AT STR 29R. R&R INTERCOSTAL PER SRM 51-20-1. 2 L 7 3 4F RT A3WE 2002021500079 20020215 00079 NM 2002 2 15 02FDEA00120 1 20020119 A 5320 INTERCOSTAL BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 1322 INTERCOSTAL CRACKED BETWEEN BS 720C AT STR 26L. R&R INTERCOSTAL PER SRM 51-20-1. 2 L 7 3 4F RT A3WE 2002021500080 20020215 00080 NM 2002 2 15 02FDEA00121 1 20020107 A 5313 STRINGER BOEING 727 727277 138408S NM FUSELAGE LOWER CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 813 STR 28R CORRODED AT BS 400 TO 500. R&R STR PER SRM 51-10-3. 2 L 7 3 4F RT A3WE 2002021500081 20020215 00081 NM 2002 2 15 02FDEA00122 1 20020107 A 5313 STRINGER BOEING 727 727277 138408S NM FUSELAGE LOWER CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 593 CORROSION ON STR 28R, BS 1065 TO 1070. R&R STRINGER PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 2002021500082 20020215 00082 NM 2002 2 15 02FDEA00123 1 20020107 A 3230 FITTING BOEING 727 727277 138408S NM LAND GEAR CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 600 SUPPORT FITTING FOR NOSE LG DOOR ACTUATOR RODS CORRODED. R&R FITING PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002021500083 20020215 00083 NM 2002 2 15 02FDEA00124 1 20020106 A 5311 BELTFRAME BOEING 727 727277 138408S NM FUSELAGE LOWER CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 592 CORROSION ON BELT FRAME BS 1050 BETWEEN STR 27R & 28R. R&R BELTFRAME PER SRM 53-10-4. 2 L 7 3 4F RT A3WE 2002021500084 20020215 00084 NM 2002 2 15 02FDEA00103 1 20020106 A 5320 STRINGER BOEING 727 727277 138408S NM FUSELAGE LOWER CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 507 CORROSION ON STR 29R AT BS 1168. R&R STRINGER PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 2002021500085 20020215 00085 NM 2002 2 15 02FDEA00112 1 20020106 A 5320 SHEAR TIE BOEING 727 727277 138408S NM FUSELAGE LOWER CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 N 507 SHEAR TIE CRACKED AT BS 1168, STR 29R. R&R SHEAR TIE PER SRM 53-10-4. 2 L 7 3 4F RT A3WE 2002021500086 20020215 00086 EA 2002 2 15 COMA0260096 1 20020211 A 3222 16124101 AXLE CNDAIR CL600 CL6002B19 1900309 EA NLG BLOWN A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 796CA 5647 7338 FLIGHT 5426 GEAR DISAGREE WARNING, NLG DID NOT RETRACT WHEN GEAR SELECTED UP.REPLACED THE NLG STRUT AXLE ASSY. 2 L 7 2 4F RT A21EA 2002021500087 20020215 00087 EA 2002 2 15 COMA0260097 1 20020213 A 3222 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 713CA 7245 FLIGHT 5557 GEAR DISAGREE WARNING, NLG DID NOT RETRACT.FOUND NLG FLAT - SERVICED NLG I/A/W M/M INSTRUCTIONS. 2 L 7 2 4F RT A21EA 2002021500088 20020215 00088 EA 2002 2 15 COMA0260098 1 20020213 A 2750 857SD100 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA L/H WING DRAGGING A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 916CA 7014 FLIGHT 5899 FLAPS FAILED AT 22 DEGREES DURING APPROACH.REPLACED THE #2 AND #3 FLEX DRIVE SHAFTS. 2 L 7 2 4F RT A21EA 2002021500089 20020215 00089 NM 2002 2 15 PCAA0202028 1 20020210 A 3350 SWITCH DHAV DHC8 DHC8102 2809003 NM CABIN FAULTY A PCAA K NONE O OTHER CR CRUISE 1 EA 13 814EX 318 PHL FLIGHT 3644 CREW REPORTED EMERGENCY LIGHTS CYCLE ON AND OFF DURING FLIGHT. MAINTENANCE INSPECTED FLIGHT ATTENDANTS EMERGENCY SWITCH, NO DEFECTS NOTED. ALSO INSPECTED RIGHT SECONDARY BUSS CANNON PLUGS, AND GROUND RAN AIRCRAFT WITH PROP ELLER HEAT ON WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. AS A FOLLOW UP DURING MAINTENANCE OVERNIGHT VISIT, FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH WAS REPLACED, WIRING AT SWITCH, CONTROL BOX AND COCKPIT SWITCH WERE INSPECTED. NO DEFECTS WERE FOUND. 2 H 7 2 4T RT A13NM 2002021500091 20020215 00091 NM 2002 2 15 QXEA0200092 1 20020206 A 2120 SMOKE DHAV DHC8 DHC8202 2809007 NM COCKPIT DETECTED A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 358PH 506 SEA - DURING DESCENT, SMOKE WAS OBSERVED IN CABIN AND COCKPIT. TURNING OFF THE NR 1 BLEED STOPPED THE SMOKE. MAINTENAN CE GROUND RAN AIRCRAFT AT 90 PERCENT TORQUE WITH THE BLEEDS ON, BLEED FLOW TO MAXIMUM AND THEN TO BLEEDS OFF, BLEED FLOW TO MAXIMUM AND AT VARIOUS OTHER POWER SETTINGS. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002021500092 20020215 00092 EA 2002 2 15 QXEA0200093 1 20020206 A 2820 B0305025A24 COUPLING CNDAIR CL600 CL6002C10 1390015 EA CENTER TANK FAILED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 606QX 825 10023 EUG - CREW RECEIVED FUEL EJECTOR CAUTION LIGHT AND FUEL IMBALANCE, RIGHT TANK LOW CAUTION MESSAGE AND CENTER TANK BEGAN TO TAKE ON FUEL. THE CENTER TANK HAD OVER 4500 LBS OF FUEL UPON LANDING. MAINTENANCE REPLACED THE FAILED RIGHT WIGGINS CLAMP AND RIGHT PRIMARY EJECTOR FUEL FEED TUBE IAW CRJ 700 MAINTENANCE MANUAL. LEAK CHECK IS GOOD. ALL RII ITEMS WERE COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002021500097 20020215 00097 EA 2002 2 15 CA020114004 1 20020110 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA (CAN) PILOTS RIGHT SIDE WINDOW CRACKED IN CRUISE. REMOVED AND REPLACED RIGHT SIDE WINDOW WITH SERVICEABLE UNIT IAW AM M 56-12-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500099 20020215 00099 EA 2002 2 15 CA020114007 1 20020108 A 2910 LINE DHAV DHC8 DHC8311 1386006 EA HYD SYSTEM CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 20751 (CAN) CHAFING DAMAGE FOUND ON LT & RT FLAP INBD TORQUE TUBES & HYD LINES.THIS PROBLEM WAS FOUND ON INSPECTION OF UPPER F USELAGE AREA BEHIND WING CENTRE SECTION LT & RT STA: YW42.000. 2 H 7 2 4T RT A13NM 2002021500109 20020215 00109 EA 2002 2 15 CA020117002 1 20020114 A 7120 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOUND CRACK ON THE ENGINE SUPPORT BEAM. ENGINE SUPPORT BEAM REPAIRED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500110 20020215 00110 EA 2002 2 15 CA020117003 1 20020115 A 5610 601R3303311 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA (CAN) PILOTS SIDE WINDOW CARACKED DURING CRUISE. WINDOW ASSEMBLY REPLACED IAW AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500111 20020215 00111 EA 2002 2 15 CA020117005 1 20020116 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) LEFT WINDSHIELD CRACKED DURING FLIGHT AT FL270. LEFT WINDSHIELD REPLACED PER AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500112 20020215 00112 EA 2002 2 15 CA020117006 1 20020116 A 7500 356124310 SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BLEED AIR SYS LEAKING W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA (CAN) CREW GOT L 14TH DUCT MESSAGE. MESSAGE WAS INTERMITTENT AT FIRST. EVENTUALLY, MESSAGE WENT TO STEADY STATE. CREW FO LLOWED QRH 6-2 THEN ABNORMAL 1-2. THEY LANDED AT THE NEAREST SUITABLE AIRPORT. MAINTENANCE WAS SENT. REPLACED THE LEFT LEAK SENSING ELEMENT IN THE LEFT PYLON. GROUND RUNS AND OPS CHECKS CARRIED OUT WITH NO DEFECTS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021500113 20020215 00113 WP 2002 2 15 CA020117007 1 20020111 A 5312 BULKHEAD LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACK FOUND ON PRESSURE BULKHEAD 1363 AT RBL 44.5 & WL 130. STIFFENERS SURROUNDING CRACK REMOVED FOR ACCESS IN ACC ORDANCE WITH S.R.M. 51-40-01. CRACK STOP DRILLED , 2 L 7 3 4F 4 F A23WE E12EU 2002021500114 20020215 00114 NM 2002 2 15 CALA0200072 1 20020214 A 5320 ANGLE BOEING 737 737524 1384721 NM STA 294-312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19636 26340 INSPECTION FOUND SUPPORT ANGLE CORRODED AT STA 294-312, LOCATED INLINE WITH RIGHT SIDE OF COCKPIT DOORWAY, RBL 12. THE S UPPORT ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002021500115 20020215 00115 2002 2 15 371PA0002 4 20020215 A 2210 LIMIT SWITCH BOEING 737 737306 NM A PIDA K NONE O OTHER DE DESCENT 1 SO 05 371PA 23543 Auto pilot kicks off line during descent, will not reset.C/A - Cleaned flap limit switch & performed DFCS Bite test. Op' s Cks OK. Ref 22-03-11. 2 L 7 2 4F RT A16NE 2002021500117 20020215 00117 2002 2 15 GTIA012166 4 20020101 A 2565 100503101 BOTTLE DOUG DC9 DC982 3022082 WP EVAC SLIDE LOW A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 DTW - AFT EVAC SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED AFT EVAC, SLIDE AS REQUIRED IAW MD80 MM 25-62-00. (M) 2 L 7 2 4F A6WE 2002021500120 20020215 00120 WP 2002 2 15 GTIA012169 1 20020113 A 3350 60030431 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 820NK 49126 MCO - FOUND SEVERAL OVERHEAD EMERGENCY LIGHTS INOPERATIVE MID CABIN. REPLACED EMERGENCY LIGHTS POWER SUPPLY AT ROW 17 R IGHT. OPS TEST OK IAW 33-53-00. (M) 2 L 7 2 4F A6WE 2002021500127 20020215 00127 NM 2002 2 15 AWXA200200138 1 20020129 A 5330 5007945264A SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 YVR - MAJOR REPAIR - "C" - DURING C-13 CHECK A CRACK WAS FOUND ON THE FWD ENTRY DOOR AT THE AFT FRAME CUTOUT ACCESS HOLE S OF THE 6TH AND 7TH STOP ADJUSTERS IN AN OUTWARD DIRECTION FROM HOLES TO THE EDGE OF THE FRAME SKIN. MAINTENANCE DRESSE D OUT CRACKS; PERFORMED A HFEC INSPECTION TO VERIFY CRACKS WERE CONTAINED; FABRICATED AND INSTALLED A DOUBLER IAW AWA ER 03-5210-02042-TB2. 2 L 7 2 4F RT A16WE 2002021500128 20020215 00128 NM 2002 2 15 AWXA200200139 1 20020129 A 5330 5007945264A SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 YVR - MAJOR REPAIR - "C" - DURING C-13 CHECK A CRACK WAS FOUND ON THE FWD ENTRY DOOR INNER SKIN ON THE AFT SIDE AT THE 7 TH ACCESS HOLE FOR THE STOP ADJUSTER, CRACK IS ON AN OUTWARD AND VERTICAL DIRECTION THROUGH A RIVET HOLE BS 344. MAINTEN ANCE DRESSED OUT CRACKS, PERFORMED A HFEC INSPECTION TO VERIFY CRACKS WERE CONTAINED, AND FABRICATED AND INSTALLED A DOU BLER IAW AWA ER 03-5210-02042-TB2. 2 L 7 2 4F RT A16WE 2002021500129 20020215 00129 NM 2002 2 15 AWXA200200141 1 20020127 A 5414 301A1070 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 YVR - MAJOR REPAIR - "C" - DURING C-13 CHECK A CRACK WAS FOUND AT CUTOUT OF THE #1 ENGINE PYLON TOP FWD PANEL 5727L. MAI NTENANCE PERFORMED HFEC INSPECTION AND VERIFIED THAT THE CRACK WAS CONTAINED BY THE FASTENER HOLE, THEN FABRICATED & INS TALLED A DOUBLER IAW DWG 311A1023, B737-300 SRM 51-10-02 PG.12, AND AWA ER 03-5433-00340-DL1. 2 L 7 2 4F RT A16WE 2002021500130 20020215 00130 NM 2002 2 15 AWXA200200143 1 20020121 A 5330 6545800 SKIN BOEING 737 7373G7 1384595 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 YVR - MAJOR REPAIR - "C" - DURING C-13 CHECK TWO SMALL DENTS WERE FOUND JUST ABOVE AND AFT OF THE FWD LAVATORY SERVICING DOOR BS 294. MAINTENANCE PERFORMED HFEC INSPECTION TO VERIFY DENTS WERE NOT CRACKED, NO CRACKS NOTED, FABRICATED AND IN STALLED REPAIR DOUBLER, FILLER, AND TRIPLER AS PER AWA ER 03-5311-01233-SS2E. 2 L 7 2 4F RT A16WE 2002021500131 20020215 00131 NM 2002 2 15 AWXA200200144 1 20020201 A 5330 6545769 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 YVR - MAJOR REPAIR - "C" - DURING C-13 CHECK A CRACK WAS FOUND ON THE AFT END SKIN OF THE EQUIPMENT COOLING AIR EXHAUST DUCT CUTOUT BS 373 . MAINTENANCE STOP DRILLED HOLE AND PERFORMED HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED, FABR ICATED SPACER RING AND EXTERNAL DOUBLER AND INSTALLED REPAIR PARTS IAW DWG 65C33930 AND AWA ER 03-5311-02040-KB1 2 L 7 2 4F RT A16WE 2002021600001 20020216 00001 SO 2002 2 16 C2XA02IA030 1 20020214 A 3350 2013A1 BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 WHILE PERFORMING A SERVICE CHECK THE MECHANIC NOTED THAT THE EMERGENCY LIGHT IN THE BACK ROW AND OVERWING DID NOT ILLUMI NATE. IAH- MAINTENANCE REMOVED AND REPLACED THE #4 EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY L IGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, 2 L 7 2 4T RT T00011AT 2002021600002 20020216 00002 EU 2002 2 16 C2XA02IA031 1 20020214 A 3610 S0003017000000 CLAMP AEROSP ATR42 ATR42320 8680930 EU #1 ENGINE BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 93840 210691510 271 IAH- DURING FLIGHT 3630 THE CREW NOTED THAT THE #1 ENGINE FIRE WARNING LIGHT ILLUMINATED DURING CLIMBOUT. THE CREW SHU T DOWN THE #1 ENGING,PULLED THE #1 ENGING FIRE BOTTLE HANDLE,DECLAIRED EMERGENCY, AND, RETURNED TO IAH WITHOUT INCIDENT. IAH- MAINTENANCE INSPECTED THE #1 ENGINE, AND FOUND NO EVIDENCE OF FIRE. THE FIRE INDICATION WAS CAUSED BY A BROKEN C LAMP AT THE HIGH PRESSURE VALVE. MAINTENANCE REMOVED AND REPLACED THE #1 ENGINE HIGH PRESSURE VALVE OUTLET DUCT,AND, TH REE ATTACHING CLAMPS,PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. 2 H 7 2 4T RT A53EU 2002021800001 20020218 00001 EU 2002 2 18 MALA020155 1 20020212 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E&E BAY MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 413XJ 340B413 ON CLIMBOUT DURING FLIGHT 2701, AVIONICS SMOKE LIGHT ILLUMINATED. WITH NO SMOKE OR FIRE PRESENT IN COCKPIT OR CABIN. AI R RETURN TO DTW. MAINTENANCE INSTALLED SERVICABLE AVIONICS RACK SMOKE DETECTOR PN 72-111211-000 SN/OFF A2501, SN/ON A51 49. ALL CHECK FOOD DONE IAW AMM. 2 L 7 2 4T RT A52EU 2002022000050 20020220 00050 NM 2002 2 20 F3LA200200039 1 20020203 A 5315 FLOORBEAM BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON TOP OF FLOORBEAM AT STA 294.5. REPLACED TOP CHORD OF 294.5 FLOORBEAM FROM LBL 28 TO RBL 65 PER SRM. 2 L 7 2 4U RT A16WE 2002022000051 20020220 00051 NM 2002 2 20 F3LA200200040 1 20020205 A 1430 NUT PLATE BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUT PLATE HOLE AT STA 727, BL 12R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPLACEMENT PARTS PER EO 51-00-737-001 AND SRM 51-40-4, FIGURE I, DETAIL 3. 2 L 7 2 4U RT A16WE 2002021800002 20020218 00002 EA 2002 2 18 SWIA200210645 1 20020203 A 2120 AIR FILTER CNDAIR CL600 CL6002B19 1900309 EA DISPLAY COOL A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 437SW 7564 DISPLAY COOL MESSAGE IN FLIGHT. COMPLIED WITH QRH PROCEDURE BUT DISPLAY COOL MESSAGE PERSISTED UNTIL GEAR DOWN. RETURN ED TO DFW.INSTALLED SERVICEABLE DISPLAY COOLING AIR FILTER IAW MM 21-21-15. 2 L 7 2 4F RT A21EA 2002021800005 20020218 00005 NM 2002 2 18 CA020131001 1 20020130 A 7120 84821CD524 NUT BOEING 65491811 BOEING 737 7372E3 NM PWA JT8 JT8D15 52051 NE 2ND SUPPORT MISSING W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA UK (CAN) SCHEDULED MAINTENANCE DURING REGULAR SCHEDULED OVERNIGHT MAINTENANCE; AD:99-26-07 (A)(2),INSPECTION OF NR 1 ENGINE AFT MOUNT CONE BOLT SECONDARY SUPPORT, WESTJET ENGINEER FOUND THE SECONDARY SUPPORT NUT, P/N:84821CD-524 MISSING. MAINT ENANCE REPLACED THE NUT, PER SB:737-71-1250 AND THE AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO REPORT. RE PEAT INSPECTION SCHEDULED WITHIN 300 CYCLES, PRIOR TO 30,160 C.OF AFT MOUNT CONE BOLT AND REPEAT INSPECTION SCHEDULED WI THIN 45 CYCLES, PRIOR TO 29,905 C. OF AFT CONE BOLT INDICATOR. 2 L 7 2 4F 4 F RT A16WE E2EA 2002021800006 20020218 00006 NE 2002 2 18 CA020201016 2 20020122 A 7200 6354600 CLAMP RROYCE RB211535E437 BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E437 54555 NE DUCT LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 30736 (CAN) DURING DEFECT INVESTIGATION, FOUND ON NR 1 ENGINE IN THE STRUT AREA, JUST BELOW THE REVERSE FLOW CHECK CONTROLLER , A CLAMP WITH BURNED RUBBER ON IT. PROCEEDED WITH AN AIR LEAK INVESTIGATION AND FOUND A LEAKING CLAMP. THE CLAMP WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 2002021800007 20020218 00007 EA 2002 2 18 CA020201022 1 20020117 A 5270 PROXIMITY SWITCH CNDAIR CL6002B19 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE PAX DOOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 7071 (CAN) OVERBOARD COOL MESSAGE ACCOMPANIED BY PASSENGER DOOR LATCH MESSAGE DURING CLIMB. FAULT ISOLATION GUIDE PROCEDURE PERFORMED BY FLIGHT CREW, OVERBOARD MESSAGE DISAPPEARED. PROXIMITY SWITCH PS2MB (DI 17) REPLACED. OPERATIONAL TEST OF DOOR WARNING SYSTEM AND AVIONIC COOLING SYSTEM PERFORMED AS PER AMM. ALL TESTS OK. AIRCRAFT SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021800008 20020218 00008 EU 2002 2 18 CA020204001 1 20020202 A 2910 AE7079101 HOSE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE HYD SYSTEM RUPTURED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) LOST HYDARULIC QUANTITY IN GREEN SYSTEM AND LOW PRESSURE WARNING ON ENGINE 1 HYDRAULIC SYSTEM(GREEN). CREW SWITCHE D OFF THE EDP AND PTU AT FIRST INDICATION OF FLUID LOSS AND USED THE EMERGENCY FREE FALL GEAR EXTENSION HANDLE. MAINTENA NCE FOUND A RUPTURED HOSE BETWEEN THE E.D.P. AND THE LOW PRESSURE SWITCH. THE GREEN RESEVOIR HAD 8 LTRS REMAINING AND FU RTHER CHECKS FOUND THAT NO OVERWEIGHT LANDING CHECKS WERE REQUIRED. THE AIRCRAFT WAS DISPATCHED UNDER MEL AND PARTS ORDE RED. 2 L 7 2 4F 4 F RT A28NM E311NE 2002021800009 20020218 00009 NM 2002 2 18 CA020205006 1 20020125 A 3246 2601913 TIE BOLT BENDIX 2604561 BOEING 727 727217 1384061 NM PWA JT8 JT8D17 52049 NE NR 3 WHEEL SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA BH0467B2032 (CAN) DURING AIRCRAFT WALK AROUND INSPECTION, FOUND NR 3 MAIN WHEEL ASSEMBLY WITH TWO SHEARED TIE BOLTS. NR 3 MAIN WHEE L ASSEMBLY REPLACED PER MAINTENANCE MANUAL 32-45-1. MAIN WHEEL ASSEMBLY TO BE SENT TO OVERHAUL FACILITY FOR INVESTIGATIO N AND TEAR DOWN REPORT FOR PROBABLE CAUSE. 2 L 7 3 4F 4 F RT A3WE E2EA 2002021800010 20020218 00010 NM 2002 2 18 CALA0200074 1 20020215 A 5210 BEARING BOEING 757 757224 1384958 NM L-1 DOOR BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14115 27557 THE L-1 DOOR WOULD ONLY OPEN ABOUT HALF WAY. MAINTENANCE FOUND CONTROL CAM ON HANDLE BOX WORN AND COCKING ROLLER CRANK B EARING BROKEN. BOTH PARTS WERE REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 52-11-13. 2 L 7 2 4F RT A2NM 2002021800011 20020218 00011 NM 2002 2 18 CALA0200075 1 20020215 A 5347 TRACK BOEING 737 7373T0 1384582 NM STA 280-294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND CABIN FLOOR R/H FORWARD GALLEY ATTACH TRACK CORRODED AT STA 280-294, RBL43. THE TRACK WAS REMOVED AND R EPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002021800012 20020218 00012 NM 2002 2 18 CALA0200079 1 20020217 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 927-947 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A 3" CRACK IN ANGLE AT STA 927-947, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-03. 2 L 7 2 4F RT A16WE 2002021800013 20020218 00013 NM 2002 2 18 CALA0200080 1 20020217 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES AT STA 967, LBL 50 TO RBL 50 AND AT RBL 18 TO LBL 18. A REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 202. 2 L 7 2 4F RT A16WE 2002021800014 20020218 00014 NM 2002 2 18 CALA0200081 1 20020218 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES AT STA 1016, RBL 37 TO LBL 37. THE FLOORBEAM WAS REMOVED AND R EPLACED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2002021800015 20020218 00015 NM 2002 2 18 UPS02237694 1 20020206 A 5210 FRAME BOEING 727 72731C 1384011 NM E & E DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C RH AFT FRAME ON E & E DOOR CRACKED FRAME REPLACED IAW DRAWING # 65-02163 2 L 7 3 4F A3WE 2002021800016 20020218 00016 EA 2002 2 18 COMA0260099 1 20020214 A 3220 750006000 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA L O ABORTED APPROACH OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 982CA 8077 7168 FLIGHT 5922 NLG DID NOT EXTEND WHEN GEAR SELECTED DOWN.REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002021800017 20020218 00017 EA 2002 2 18 COMA0260100 1 20020214 A 5270 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 809CA 7366 FLIGHT 5895 DOOR OUTER HANDLE CAUTION MESSAGE DURING T/O.COULD NOT DUPLICATE. DOOR OPERATION NORMAL, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2002021800018 20020218 00018 NM 2002 2 18 MWEA020131 1 20020218 A 2910 59369865001 RESERVOIR DOUG MD88 MD88 3023688 NM RIGHT LEAKING A MWEA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 31 601ME 49762 RIGHT HYDRAULIC QUANTITY DECREASING DURING TAKE-OFF AND CRUISE. -- REPLACED O'RINGS AT POPPET VALVE. 2 L 7 2 4F RT A6WE 2002021800019 20020218 00019 WP 2002 2 18 MWEA020132 1 20020218 A 5330 59114273 SKIN DOUG DC9 DC932 3022066 WP STATION 981 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 CRACK IN FUSELAGE SKIN AT LONGERON 16 LEFT AND APPROXIMATELY STATION 981. -- FABRICATED AND INSTALLED DOUBLER, FILLER, AND SHIMS. 2 L 7 2 4F A6WE 2002041700100 20020417 00100 EU 2002 4 17 AWXA200200145 1 20020125 A 5320 D5347209001100 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 271 YWG - MAJOR REPAIR - C - DURING C-08 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT Y1292 AT FR 66 RT. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW DWG D53472090, AND SRM 51-42-11. 2 L 7 2 4F RT A28NM 2002021800020 20020218 00020 NM 2002 2 18 AWXA200200147 1 20020207 A 5330 654577891 SKIN BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - MAJOR REPAIR - "C" - DURING C-10 CHECK A 5/16" CRACK WAS FOUND ON FUSELAGE SKIN AT UPPER R2 DOOR HINGE CUTOUT BS 9 52, HFEC INSPECTION AND 10X VISUAL CONFIRMED THE CRACK. MAINTENANCE CUTOUT DAMAGED AREA AND PERFORM HFEC INSPECTION TO V ERIFY CRACK WAS CONTAINED; FABRICATED REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIRS IAW B737-300 SRM 53-60-01, PG. 21 0-212. 2 L 7 2 4F RT A16WE 2002021800021 20020218 00021 NM 2002 2 18 AWXA200200148 1 20020207 A 5330 5007945265 SKIN BOEING 737 7373S3 1384711 NM DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - MAJOR REPAIR - "C" - DURING C-10 CHECK THE L1 DOOR FORWARD LOWER CORNER SKIN WAS FOUND DENTED BS 312, HFEC VERFIED NO CRACKS. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN, FARICATED A REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIRS IAW B7 37-300 SRM 52-00-01, PG 203-204. 2 L 7 2 4F RT A16WE 2002021800022 20020218 00022 NM 2002 2 18 AWXA200200150 1 20020217 A 3350 BMS13311122 WIRE BOEING 737 737301 1384611 NM SEAT ROW 3 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 PHX - EEL - "C" - EMERGENCY ESCAPE PATH SEAT LIGHT INOPERATIVE AT SEAT ROW 3 L/H. MAINTENANCE TROUBLESHOT AND FOUND WIRE S BROKEN TO EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 L/H, REPAIRED WIRES IAW BOEING SWP 20-30-12, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002021800023 20020218 00023 2002 2 18 RAIA00202060 4 20020214 A 3420 7003110901 INDICATOR JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 568HK 14046 879 41086 5578- STL- FO HORIZONTAL SITUATION INDICATOR WENT BLANK DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE FO ELECTRONIC FLIGHT INSTRUMENT SYSTEM INDICATOR. 2 L 7 2 4T RT A41NM 2002021900030 20020219 00030 WP 2002 2 19 02FDEA00126 1 20020218 A 5230 ADG7022503 BEAM DOUG DC10 DC1010 3022110 WP CARGO DOOR FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 390 46624 FWD CARGO DOOR BUNGEE BEAM SNAPPED DURING OPS. BUNGEE ACT VAPOR LOCKED. RUSTED WATER SPEWED FROM ACT SHRADER VALVE. R EMOVED AND REPLACED FWD CARGO DOOR BUNGEE BEAM AND BUNGEE ACT SNUBBER PER MM 52-31-07-2. 2 L 7 3 4F A22WE 2002021900002 20020219 00002 2002 2 19 SWAA020339 4 20020212 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 406WN 27894 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. . 2 L 7 2 4F RT A16WE 2002021900003 20020219 00003 NM 2002 2 19 SWAA020340 1 20020212 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10R, BS'S 500 AND 727B. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002021900004 20020219 00004 NM 2002 2 19 SWAA020341 1 20020212 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED 4.5 INCHES LONG AT BS 927, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002021900005 20020219 00005 NM 2002 2 19 SWAA020343 1 20020212 A 5315 BAC1509 FLOORBEAM BOEING 737 7373A4 1384585 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 767+5, RBL 3. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002021900006 20020219 00006 NM 2002 2 19 SWAA020344 1 20020212 A 5312 6516300 WEB BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (3 EA) AT BS 178, WL 207 AND LBL 5, WL 207 AND LBL 6.75, WL 217 AND RBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002021900007 20020219 00007 NM 2002 2 19 02021101 1 20020214 A 2781 WARNING SYSTEM BOEING 757 757236 1384971 NM COCKPIT ACTIVATED A N8TA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 19 521NA 25592 UPON FLAP RETRACTION LEADING EDGE LIGHT AND SLAT DISAGREE MESSAGE ILLUMINATE. LIGHT REMAINED ON DURING ACCOMPLISHMENT O F ABNORMAL CHECK LIST. TROUBLESHOOTING SYSTEM. 2 L 7 2 4F RT A2NM 2002021900008 20020219 00008 NM 2002 2 19 02021501 1 20020214 A 2781 WARNING SYSTEM BOEING 757 757236 1384971 NM COCKPIT ACTIVATED A N8TA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 19 521NA 25592 UPON FLAP RETRACTION LEADING EDGE LIGHT AND SLAT DISAGREE MESSAGE ILLUMINATE. LIGHT REMAINED ON DURING ACCOMPLISHMENT O F ABNORMAL CHECK LIST. TROUBLESHOOTING SYSTEM. 2 L 7 2 4F RT A2NM 2002021900009 20020219 00009 NM 2002 2 19 02FDEA00100 1 20020119 A 5320 FLOOR SUPPORT BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 COCKPIT FLOOR PANEL SUPPORT ANGLE CORRODED BS 266, LBL 10 TO 12, WL 207. REMOVED AND REPLACED ANGLE PER SRM 51-10-1. 2 L 7 3 4F RT A3WE 2002021900010 20020219 00010 NM 2002 2 19 02FDEA00101 1 20020106 A 5280 6521636160 SKIN BOEING 727 727277 138408S NM RT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 RT MLG WING DOOR SKIN CRACKED AT HINGE CUTOUT. REMOVED AND REPLACED DOOR PER EO 7-5280-7-4301. 2 L 7 3 4F RT A3WE 2002021900011 20020219 00011 NM 2002 2 19 02FDEA00104 1 20020103 A 5280 6521636159 DOOR BOEING 727 727277 138408S NM LT MLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 LT MLG STRUT DOOR CRACKED AT AFT HINGE CUTOUT. REMOVED AND REPLACED DOOR PER EO 7-5280-7-4301. 2 L 7 3 4F RT A3WE 2002021900012 20020219 00012 NM 2002 2 19 02FDEA00118 1 20020130 A 5530 65168036 FITTING BOEING 727 727277 138408S NM VERTICAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 VERT STAB TENSION TIE FITTING LT AFT VERTICAL BOLT HOLE CORRODED. REMOVED AND REPLACED TIE PER MM 55-30-051-4. 2 L 7 3 4F RT A3WE 2002021900013 20020219 00013 EU 2002 2 19 02FDEA00125 1 20020214 A 7932 INDICATOR AIRBUS 310 A310222 3930315 EU COCKPIT FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 448FE 260 AFTER T/O OIL QTY ON NR 1 ENG SHOW 2 QT ON BOTH ANALOG AND ECAM IND. REINSTALLED C/P AND HEAT SHIELD. REMOVED AND REPL ACED OIL QTY IND. TEST NORMAL PER 79-31-00-5-A. 2 L 7 2 4F RT A35EU 2002021900014 20020219 00014 2002 2 19 SWAA020347 4 20020214 A 2565 6556685 BRACKET BOEING 737 7373A4 1384585 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/4D CHECK, FOUND LOOSE FASTENER, AT AFT SVC DOOR EMERGENCY EVAC SLIDE ATTACH BRACKET. SECURED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2002021900015 20020219 00015 2002 2 19 SWAA020348 4 20020214 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD CABIN DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 626SW 27702 DURING SCHEDULED C3 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PE R MM. 2 L 7 2 4F RT A16WE 2002021900016 20020219 00016 2002 2 19 SWAA020350 4 20020213 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021900017 20020219 00017 2002 2 19 SWAA020351 4 20020213 A 2565 6567380 WINDOW BOEING 737 7373H4 1384600 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND VIEWING WINDOW CRACKED. REMOVED AND REPLAC ED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2002021900018 20020219 00018 NM 2002 2 19 SWAA020355 1 20020214 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES AT BS 500C, ABOVE STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002021900019 20020219 00019 NM 2002 2 19 SWAA020356 1 20020214 A 5314 149A7651 WEB BOEING 737 7377H4 1384404 NM MLG W/W'S CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 793SA 27888 DURING SCHEDULED SERVICE CHECK, FOUND AFT OTBD WEBS CRACKED IN BOTH LT AND RT MLG W/W, IN THE MID SECTION OF THE WEBS. REMOVED AND REPLACED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2002021900020 20020219 00020 2002 2 19 SWAA020360 4 20020215 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM 2 L 7 2 4F RT A16WE 2002021900021 20020219 00021 NM 2002 2 19 SWAA020362 1 20020216 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 789SW 29816 RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002021900022 20020219 00022 NM 2002 2 19 SWAA020363 1 20020215 A 3350 207377 LENS BOEING 737 7373A4 1384585 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED C2 CHECK, FOUND EEPLS LENS BROKEN IN AFT CABIN. REMOVED AND REPLACED EEPLS LENS PER MM. 2 L 7 2 4F RT A16WE 2002021900023 20020219 00023 2002 2 19 SWAA020365 4 20020215 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 789SW 29816 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021900024 20020219 00024 NM 2002 2 19 SWAA020367 1 20020214 A 5520 65C2574696A ELEVATOR BOEING 737 7373H4 1384600 NM RT HORIZ STAB DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 392SW 27379 DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR DELAMINATED. REMOVED AND REPLACED RT ELEVATOR PER MM. 2 L 7 2 4F RT A16WE 2002021900025 20020219 00025 NM 2002 2 19 SWAA020368 1 20020215 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 392SW 27379 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 767, LBL 6 AND LBL 10. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002021900026 20020219 00026 NM 2002 2 19 SWAA020369 1 20020215 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 21R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002021900027 20020219 00027 NM 2002 2 19 SWAA020372 1 20020217 A 5312 6517582 WEB BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, WL 227 AND RBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002021900028 20020219 00028 NM 2002 2 19 SWAA020373 1 20020215 A 5230 6546921528 DOOR BOEING 737 7372T4 1384492 NM FWD CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR LOWER FRAME AND ATTACH ANGLE CRACKED. REMOVED AND REPLACED CARGO DOOR P ER MM. 2 L 7 2 4F A16WE 2002021900029 20020219 00029 NM 2002 2 19 0200335507 1 20020205 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 507US 23196 DURING SCHEDULED MAINTENANCE THE ESCAPE PATH LIGHTING AT ROWS 15-22 WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER S UPPLY. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 2002030400050 20020304 00050 NM 2002 3 4 02FDEA00128 1 20020210 A 3211 NUT DOUG MD11 MD11F 3023600 NM LT & RT MLG LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 CLC LT & RT BOLTS LOOSE. REMOVED AND REPLACED TRUNNION NUTS PER CMM. 32-15-01. 2 L 7 3 4F RT A22WE 2002021900031 20020219 00031 SO 2002 2 19 C2XA02CL053 1 20020218 A 4920 164161100 CHECK VALVE EMB 145 EMB145ER 3260211 SO APU STICKING A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 16944 145045 CLE FLIGHT# 3157 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AND CABIN AFTER APU START.MAINTENANCE INSPECTED AN D STRAIGHTENED A KINKED DRAIN HOSE AND REPLACED THE COMBUSTOR DRAIN CHECK VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAF T WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002022800015 20020228 00015 NM 2002 2 28 02FDEA00129 1 20020217 A 5712 ARB2922924 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 RIGHT WING L/E COMPT RIB FOUND CRACKED AT STA XORS 694 APPROX 3 INCHES. REMOVED AND REPLACED RIB PER DWG ARB 2922. 2 L 7 3 4F RT A22WE 2002021900032 20020219 00032 WP 2002 2 19 02FDEA00130 1 20020131 A 5347 CARGO TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 303 46802 STA 959 UPPER CARGO SEAT TRACK HAS 10 INCH CRACK C/T RADIUS AT SPLICE X-27. 2 L 7 3 4F RT A22WE 2002021900033 20020219 00033 2002 2 19 AT0200009 4 20020206 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP L1 DOOR OUT OF POSITION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 L1 DOOR SLIDE FELL ONTO JET WAY. REINSTALLED SLIDE. 2 L 7 2 4F A6WE 2002021900034 20020219 00034 NM 2002 2 19 AT0200010 1 20020216 A 2120 ODOR BOEING 717 717200 1383700 NM CABIN DETECTED A ZZDA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 15 954AT 55016 SMOKE SMELL IN AFT CABIN. PERFORMED GVI AND SYSTEM CHECKS, AIRCRAFT SHOWS NO SIGN OF ORIGIN OF ODOR. 2 L 7 2 4F TR A6WE 2002021900035 20020219 00035 NM 2002 2 19 AWAX200200134 1 20020215 A 3350 20131A BATTERY BOEING 737 73733A 1384673 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 164AW 23625 LCQ - EEL - C - DURING C-16 CHECK CABIN EMERGENCY ESCAPE PATH LIGHTING AT SEAT ROWS 13-14 LT, 17 LT, AND 19 RT, WAS FOUN D INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AT BS 973, OPERATIONAL CHECK WAS GOOD IAW T/C A1C33005. 2 L 7 2 4F RT A16WE 2002021900036 20020219 00036 SO 2002 2 19 C2XA02CL054 1 20020218 A 4920 164161100 CHECK VALVE EMB 145 EMB145ER 3260211 SO APU STICKING A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 14939 145030 CLE FLIGHT# 3020 THE CREW REPORTED A STRONG FUEL SMELL WHEN THE APU WAS STARTED ON THE GROUND.MAINTENANCE INSPECTED AND REPLACED THE APU COMBUSTION DRAIN CHECK VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002021900037 20020219 00037 EU 2002 2 19 AWXA200200129 1 20020212 A 5320 D53472172203 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 271 YWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM Y1292 RT BETWEEN FR 66 AND FR 67. M AINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 51-74-00, PG 1. REMOVED FLOOR SUPPORT B EAM Y1292 RT, FABRICATED NEW FLOOR SUPPORT BEAM AND INSTALLED REPAIR IAW DWG 53472172. 2 L 7 2 4F RT A28NM 2002021900038 20020219 00038 EU 2002 2 19 AWXA200200130 1 20020210 A 5320 D53112821200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 271 YWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT BEAM Y254 LT BETWEEN FR 15 AND FR 21. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 53-11-14. REMOVED FLOOR SUPPOR T BEAM Y254 LT, FABRICATED NEW FLOOR SUPPORT BEAM AND INSTALLED REPAIR IAW DWG 53112821. 2 L 7 2 4F RT A28NM 2002021900039 20020219 00039 EU 2002 2 19 AWXA200200131 1 20020210 A 5320 D5311281400200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 271 YWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT BEAM Y1292 RT BETWEEN FR 15 AND FR 19. MAINTENANCE REMOVED FLOOR SUPPORT BEAM Y1292 RT, FABRICATED NEW FLOOR SUPPORT BEAM AND INSTALLED REPAIR IAW DWG 53112782. 2 L 7 2 4F RT A28NM 2002021900041 20020219 00041 NM 2002 2 19 AWXA200200137 1 20020201 A 5310 654797322 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 YVR - MAJOR REPAIR - C - DURING C-13 CHECK A 4 INCH CRACK WAS FOUND ON CREASE BEAM WEB RT BS 616 - 639. MAINTENANCE REM OVED DAMAGED CREASE BEAM WEB AND FITTED AND INSTALLED A NEW BEAM WEB IAW DWG 65-47973 AND SRM 51-40-2 PG 3. 2 L 7 2 4F RT A16WE 2002021900042 20020219 00042 NM 2002 2 19 AWXA200200140 1 20020130 A 5311 654653950 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 YVR - MAJOR REPAIR - C - DURING C-13 CHECK A CRACK WAS FOUND AT RT CABIN SIDEWALL FWD FRAME AT FLOORBEAM INTERSECTION BS 616. MAINTENANCE REMOVED DAMAGED SECTION OF INNER CHORD, FABRICATED A FILLER AND REPAIR ANGLE AND INSTALLED REPAIR PAR TS IAW AWA ER 03-5311-02035-TB2A. 2 L 7 2 4F RT A16WE 2002021900043 20020219 00043 NM 2002 2 19 AWXA200200142 1 20020131 A 5311 6546540 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 YVR - MAJOR REPAIR -C- DURING C-13 CHECK A CRACK WAS FOUND AT RT CABIN SIDEWALL FRAME FLOORBEAM INTERSECTION BS 639. MA INTENANCE REMOVED CRACKED INNER CHORD, FABRICATED NEW INNER CHORD AND REPAIR DOUBLER AND INSTALLED REPAIR PARTS IAW AWA ER 03-5362-02046-GF1. 2 L 7 2 4F RT A16WE 2002021900044 20020219 00044 EU 2002 2 19 AWXA200200146 1 20020207 A 5320 D534800204436 WEB AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 77 YVR - MAJOR REPAIR - C - DURING C-02 CHECK A CRACK WAS FOUND ON THE LT OUTBOARD WEB JUST BELOW THE AFT GALLEY FR 68-69. MAINTENANCE REMOVED CRACKED WEB, FABRICATED NEW WEB, AND INSTALLED REPAIR IAW SRM 51-72-00, AND SRM 53-41-14, PG 37 & 4 1. 2 L 7 2 4F RT A28NM 2002021900045 20020219 00045 NM 2002 2 19 AWXA200200149 1 20020216 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 PHX - EEL - C - DURING INSPECTION THE EMERGENCY EXIT LIGHT AT L-2 DOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE BATTERY PACK AT FOR L-2 DOOR EMERGENCY EXIT LIGHT IAW T/C A1C33005, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002021900046 20020219 00046 EA 2002 2 19 CA020110018 1 20020110 A 2433 TRU3502 TRANSFORMER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE COCKPIT FAILED W A UNSCHED LANDING H G ELECT. POWER LOSS-50 PC MULTIPLE FAILURE CL CLIMB 1 CA (CAN) DURING TAXI CHECK & UPON CHECKING THRUST REVERSER, PFD 1 & MFD 1 BLANKED OUT FOR 2 TO 3 SECONDS. STALL FAIL POS TED & FLAP HALFSPEED POSTED. RETURNED TO GATE. A/C POWERED DOWN & RESET PERFORMED. ALL MESSAGES DISAPPEARED. A/C RET URN TO SERVICE. AFTER TAKEOFF, WHILE SELECTING FLAP FROM 1 TO 0, PFD 2 & MFD 2 SHORTLY BLANKED & PFD 1 & MFD 1 BLANKE D FOR 1 MIN. STAB CH 2 INOPERATIVE. POSTED & UNABLE TO RESET. A/C DIVERTED BACK TO MUNICH. 3 JAN 02, MAINT WERE ABLE T O REPRODUCE SNAG ON GROUND. MAINT COULD HEAR MULTIPLE CLICKING FROM CONTACTOR IN LEFT CONSOLE. SINCE OTHER COMPONENT W ERE REPLACED BACK IN NOV FOR SIMILAR EVENT ON A/C, PCB FROM LEFT DCPC REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021900049 20020219 00049 WP 2002 2 19 DHL2002801005 1 20020212 A 2612 PIN DOUG DC8 DC873F 302199F WP FIRE DETECTION DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 NR 2 ENG FIRE SHORT TEST FAILED IN B-POSITION. PERFORMED FIRE TEST ON NR ENG, FOUND PIN L TO B HAVING HIGH RESISTANCE A FTER RESEATED CONNECTOR, CLEANED, STARTED TO CHECK NORMAL. 2 L 7 4 4F RT 4A25 2002021900050 20020219 00050 NM 2002 2 19 NACA20020004 1 20020212 A 7920 FITTING BOEING 727 72723 1384004 NM PWA JT8 JT8D NE NR 3 ENGINE LEAKING A NACA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 992AJ 19428 655097 ENGINE NR 3 SHUT DOWN AT 1850Z DUE TO LOSS OF OIL PRESSURE AND QUANTITY. RESEALED RESTRICTOR UNION AND TIGHTENED LINE A T TRANSMITTER T-FITTING, SERVICED ENGINE WITH OIL. OPS CHECK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2002021900051 20020219 00051 NM 2002 2 19 P5CA0200644 1 20020207 A 2550 CASTER BOEING 747 74746NF 13848BT NM MAIN CARGO BAY CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 452PA 30810 MAIN DECK CASTER ASSY AT BS 1900 R/S CRACKED. REPAIRED PER SRM 51-40-00. 2 L 7 4 4F RT A20WE 2002021900052 20020219 00052 NM 2002 2 19 P5CA0200647 1 20020207 A 2550 CASTER BOEING 747 74746NF 13848BT NM MAIN CARGO BAY CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 452PA 30810 RT MAIN DECK BS 1725 CASTER TRAY EXTRUSION CRACKED/DAMAGED. REPAIRED PER SRM 51-70-11 FIG 1 & PER MM 25-57-04. 2 L 7 4 4F RT A20WE 2002021900053 20020219 00053 NE 2002 2 19 QXEA0200152 2 20020212 A 7320 311489201 VALVE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 2 ENGINE FAILED A QXEA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 NM 09 358PH 9739 506 PDX - SMOKE IN CABIN VISIBLE FROM ROW 5 & 6. RINGING SOUND FROM LAVATORY SMOKE DETECTOR. NO VISIBLE FIRE. MAINTENANCE REPLACED THE NR 2 P2.5/P3 AIR PRESSURE SWITCHING VALVE. INSPECTED BOTH 6 & 7 BEARING SCAVENGE DRAIN LINES. NO DEFECTS NOTED. THE NR 1 & 2 ENGINE OIL LEVELS AT PROPER LEVEL. OPERATIONAL CHECK FLIGHT IS SATISFACTORY. 2 H 7 2 4T 4 T RT A13NM E20NE 2002030600032 20020306 00032 NM 2002 3 6 QXEA0200153 1 20020213 A 5270 SPRING BOMBDR DHC8 DHC8401 NM CARGO DOOR WEAK A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 402QX 4032 BOI - AIRCRAFT RETURNED TO FIELD AFTER RECEIVING AFT SERVICE DOOR WARNING. MAINTENANCE REPLACED DOOR HANDLE TARGET MOUN T SPRING. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002021900054 20020219 00054 EA 2002 2 19 CA020117008 1 20020117 A 3320 BC10065003 SOCKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN BURNED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) SHORTLY AFTER TAKEOFF FROM TOULOUSE, FRANCE, SMOKE APPEARED IN CABIN. SMOKE CAME FROM ROW 8DF FROM FINISHING PAN EL ABOVE RIGHT EMERGENCY EXIT. ELECTED TO RETURN TO TOULOUSE. SMOKE HOODS IN FORWARD AND AFT POSITION USED BY FLIGHT A TTENDANT. LANDING WEIGHT WAS 22601 KG AND VERTICAL SPEED WAS MAX 300 FEET/MIN.IN TOULOUSE: LAMP HOLDER ABOVE ROW 8DF F OUND BURNED. BALLAST UNIT B126 DISCONNECTED. SIDE WALL LIGHT AT ROW 8DF INOPERATIVE. - BOTH SMOKE HOODS REPLACED IN MUNI CH: LAMP HOLDER REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021900055 20020219 00055 EA 2002 2 19 CA020117009 1 20020117 A 5610 NP1393221 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) LEFT WINDOW CRACKED IN CLIMB. PERFORMED UNSCHEDULED LANDING. LEFT WINDOW REPLACED PER AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021900057 20020219 00057 NM 2002 2 19 SABA020022 1 20020216 A 3350 6L04789 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 Aircraft 883 on flight 5008 CLT to OAJ. During preflight inspection the emergency floor lights were found inoperative. Maintenance removed and replaced the floor emergency light batteries. System ops checked good. Aircraft returned to s ervice. 2 H 7 2 4T RT A13NM 2002021900058 20020219 00058 EA 2002 2 19 CA020117011 1 20020117 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) DURING CRUISE AT FL280 / IAS 280, THE RIGHT WINDOW CRACKED. RIGHT WINDOW REPLACED PER AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002021900059 20020219 00059 EA 2002 2 19 COMA0260102 1 20020215 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 917CA 7017 FLIGHT 6013 - CABIN DOOR WARNING.ADJUSTED DOOR INNER HANDLE. 2 L 7 2 4F RT A21EA 2002021900060 20020219 00060 EA 2002 2 19 COMA0260103 1 20020215 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 917CA 7017 FLIGHT 5547 - CABIN DOOR WARNING.C/W COMPLETE RIG PROCEDURE AND OPERATIONAL CHECK OF CABIN DOOR LATCH MECHANISM. 2 L 7 2 4F RT A21EA 2002021900061 20020219 00061 NM 2002 2 19 QXEA0200155 1 20020210 A 2120 ODOR DHAV DHC8 DHC8202 2809007 NM COCKPIT DETECTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 347PH 480 SEA- FISHLIKE SMELL IN THE COCKPIT. RAN AIRCRAFT FOR 15 MINUTES USING VARIOUS LOADS AND COMBINATIONS OF LOADS. ALL VOL TAGES NORMAL AND EVEN. COULD NOT DUPLICATE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2002021900062 20020219 00062 2002 2 19 QXEA0200157 4 20020213 A 2350 506011 CONTROL UNIT DHAV DHC8 DHC8202 2809007 NM CABIN FAULTY A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 367PH 511 PSC- FLIGHT ATTENDANT REPORTS ELECTRICAL SMELL IN FRONT OF CABIN. REMOVED AND REPLACED AUDIO REMOTE ELECTRONIC UNIT. O PERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002021900063 20020219 00063 EU 2002 2 19 RAIA00202054 1 20020211 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 561HK 41077 MX-STL- FLOOR ESCAPE PATH LIGHTS INOP. RECONNECTED EMERGENCY PATH LIGHTS AT SEAT 6A. 2 L 7 2 4T RT A41NM 2002021900064 20020219 00064 EU 2002 2 19 RAIA00202055 1 20020212 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 551HK 41040 MX-STL- EMERGENCY PATH LIGHTS INOP, LEFT AFT. RECONNECTED AFT EMERGENCY PATH LIGHT ELECTRICAL CONNECTION. 2 L 7 2 4T RT A41NM 2002021900065 20020219 00065 2002 2 19 COMA0260104 4 20020215 A 2350 536113 AUDIO PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 929CA 18420 7035 FLIGHT 5553 - PILOT TO COPILOT INTERCOM INTERMITTENT.REPLACED THE #1 ACP. 2 L 7 2 4F RT A21EA 2002021900066 20020219 00066 EU 2002 2 19 RAIA00202056 1 20020213 A 3350 LIGHT AEROSP ATR42 ATR42300 8680920 EU PAX DOOR NOT SEATED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 423TE 119 MX-STL- PAX DOOR EMERGENCY LIGHT INOP. RESEATED PAX DOOR EMERGENCY LIGHT BULB, OPS CHECK OK. 2 H 7 2 4T RT A53EU 2002021900067 20020219 00067 EU 2002 2 19 RAIA00202057 1 20020213 A 2840 WARNING SYSTEM AEROSP ATR42 ATR42300 8680920 EU COCKPIT MALFUNCTIONED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 424TE 124 BMI- LEFT FUEL CENTRAL ANNUNCIATOR PANEL LIGHT ILLUMINATED DURING TAXI. MAINTENANCE TROUBLESHOT AND DEFERRED IAW ATR ME L 28-21-1. 2 H 7 2 4T RT A53EU 2002021900068 20020219 00068 EU 2002 2 19 RAIA00202058 1 20020213 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 560HK 41076 MX-STL- EMERGENCY PATH LIGHTS INOP BETWEEN ROWS 8 & 9. RECONNECTED CONNECTOR IN PATH LIGHT TRACK, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002021900071 20020219 00071 EA 2002 2 19 CA020117013 1 20020117 A 2750 85350712001 TORQUE TUBE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE CENTER WING CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 20978 (CAN) CHAFING DAMAGE FOUND ON LT & RT FLAP INBD TORQUE TUBES & HYD LINES. THIS PROBLEM WAS FOUND ON INSPECTION OF UPPER FUSELAGE AREA BEHIND WING CENTRE SECTION LT & RT STA: YW42.000. 2 H 7 2 4T 4 T RT A13NM E20NE 2002021900073 20020219 00073 NM 2002 2 19 SABA020019 1 20020210 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 880CC 277 AIRCRAFT 880 ON FLIGHT 5054 FROM CLT TO PGV. DURING PREFLIGHT THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. NO EMERGENCY PROCEDURES WERE USED. MAINTENANCE REMOVED AND REPLACED THE BATTERY. BATTERY DID NOT FIX THE PROBLEM. MAINT ENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. SYSTEM OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002021900075 20020219 00075 NM 2002 2 19 SWAA020245 1 20020201 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE IN FWD CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002021900076 20020219 00076 NM 2002 2 19 SWAA020247 1 20020130 A 5320 6551698 SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002021900077 20020219 00077 NM 2002 2 19 SWAA020252 1 20020130 A 2560 6557463 LOCK BOEING 737 7373H4 1384600 NM GIRT FITTING DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED 1/2D CHECK, FOUND BOTH AFT DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKET LOCKS, WITH DAMAGED HARDWAR E ON FWD AND AFT LOCKS. REMOVED AND REPLACED HARDWARE PER MM. 2 L 7 2 4F RT A16WE 2002021900078 20020219 00078 NM 2002 2 19 SWAA020253 1 20020130 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED 1/2D CHECK, FOUND EEPLS INOP. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002021900079 20020219 00079 2002 2 19 SWAA020257 4 20020204 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM CABIN DOORS OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED C2 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2 L 7 2 4F A16WE 2002021900080 20020219 00080 NM 2002 2 19 SWAA020267 1 20020204 A 2910 65C26839 HYDRAULIC LINE BOEING 737 7373H4 1384600 NM RT MLG LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 307SW 22947 AIR TURNBACK, AFTER DEPARTURE LOSS A-SYSTEM HYD, ENG DRIVEN LOW PRESS LIGHT ILLUMINATED FOLLOWED BY SLOW DEPLETION OF B- SYSTEM TO BELOW 3/4 MARK. REMOVED AND REPLACED RT MLG ACTUATOR PRESS LINES AND CASE DRAIN FILTERS PER MM. 2 L 7 2 4F RT A16WE 2002021900081 20020219 00081 2002 2 19 SWAA020270 4 20020205 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 410WN 27897 FWD SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021900082 20020219 00082 2002 2 19 SWAA020271 4 20020204 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 601WN 27695 FWD SERVICE DOOR EMERGENCY EVAC SLIDE GIRT BAR DRAGGED AND PULLED SLIDE OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021900083 20020219 00083 NM 2002 2 19 2002UALA00254 1 20020209 A 5300 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 AFT CABIN BETWEEN STATION 1640 TO STA 1660, BL0, INTERCOSTAL NEEDS REMOVAL FOR ACCESS. MAJOR REPAIR ACCOMPLISHED. INTER COSTAL REMOVED AND REINSTALLED WITH NEW ANGLES AND SPACERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021900084 20020219 00084 NM 2002 2 19 2002UALA00255 1 20020210 A 5315 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 RIGHT HAND AFT CABIN STATION 1640 FLOOR BEAM WEB DAMAGED AT RBL 56, ALSO FLOOR BEAM CAP CORRODED AROUND FASTENER HOLES B ETWEEN RBL49-52. MAJOR REPAIR ACCOMPLISHED.INSTALLED ANGLE DOUBLER ON CAP AND WEB DOUBLERS ON INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021900085 20020219 00085 NM 2002 2 19 2002UALA00256 1 20020211 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 STATION 1280 ABOVE STRINGER 26R GOUGED AND HAS EXCESS MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR . 2 L 7 2 4F 4 F RT A2NM E17NE 2002021900086 20020219 00086 NM 2002 2 19 2002UALA00257 1 20020211 A 5313 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 STATION 1520 BETWEEN STRINGER 23R AND STRINGER 25R, EDGE OF FRAME DAMAGED AT RBL 36.5, 39.25, 41.5 AND 49 RESPECTIVELY. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021900087 20020219 00087 NM 2002 2 19 2002UALA00264 1 20020213 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 FUSE SKIN AT BODY STATION 760, BELOW STRINGER 16L, DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.SKIN DOUB LER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021900088 20020219 00088 NM 2002 2 19 2002UALA00265 1 20020212 A 5313 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 LEFT HAND CABIN WEB STATION 1640 JUST BELOW STRINGER 7L CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002021900089 20020219 00089 NM 2002 2 19 2002UALA00276 1 20020214 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 FUSELAGE BODY STATION 188 RIGHT HAND FRAME OUTBOARD SIDE CHORD CRACKED AT WL 208. MAJOR REPAIR ACCOMPLISHEDINSTALLED D OUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021900090 20020219 00090 NM 2002 2 19 SWAA020276 1 20020205 A 5320 6517583 STIFFENER BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL CHORD CRACKED 1.0 INCH LONG AT BS 178, WL 183 AND RBL 5.7. REMOVED AND REPL ACED CHORD PER SRM. 2 L 7 2 4F A16WE 2002021900091 20020219 00091 NM 2002 2 19 SWAA020278 1 20020206 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 788SA 30603 DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP IN AFT CABIN AND SEVERAL COVERS CRACKED. RELAMPED EEPLS AND REMOVED AND REP LACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002021900092 20020219 00092 NM 2002 2 19 SWAA020279 1 20020205 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 650SW 27720 DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT ROW NR 7. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002021900093 20020219 00093 2002 2 19 SWAA020281 4 20020206 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 410WN 27897 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021900094 20020219 00094 2002 2 19 SWAA020282 4 20020203 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 609SW 27929 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER AFTER LANDING. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021900095 20020219 00095 NM 2002 2 19 SWAA020294 1 20020206 A 3350 20131A BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 745SW 29491 DURING SCHEDULED RON, FOUND EMERGENCY EXIT LIGHT INOP AT AFT OVERHEAD BULLNOSE. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002021900096 20020219 00096 NM 2002 2 19 SWAA020298 1 20020205 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN MALFUNCTIONED A SWAA O OTHER O OTHER CL CLIMB 1 SW 07 727SW 27859 AFTER TAKEOFF, FWD ENTRY EMERGENCY EXIT LIGHT AND EEPLS AT ROW 1 ILLUMINATED. CYCLING LIGHT SW OFF AND ON HAD NO EFFECT . LIGHTS WENT OUT AFTER ABOUT 30 MINUTES. TESTED LIGHTS PER MM. NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 2002021900097 20020219 00097 2002 2 19 SWAA020302 4 20020208 A 2565 22022900131 SLIDE BOEING 737 7372K6 1364440 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED A2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021900098 20020219 00098 2002 2 19 SWAA020311 4 20020209 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 609SW 27929 DURING SCHEDULED CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002021900099 20020219 00099 NM 2002 2 19 SWAA020312 1 20020211 A 3350 7024091007 LIGHT BOEING 737 7373H4 1384600 NM ENTRY DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 627SW 27935 DURING SCHEDULED CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002021900101 20020219 00101 NM 2002 2 19 SWAA020313 1 20020211 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM ENTRY DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F A16WE 2002021900102 20020219 00102 NM 2002 2 19 SWAA020321 1 20020210 A 7603 315A1040 THROTTLE BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563B1US GL NR 2 ENGINE OBSTRUCTED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 611SW 27697 AIR TURNBACK, IN FLT ENGINE SHUTDOWN, DURING CLIMBOUT DISCOVERED THE NR 2 ENGINE THROTTLE WOULD NOT RETARD BELOW 88 PERC ENT N1, HAD TO SHUT ENGINE DOWN AND LAND SINGLE ENGINE. FOUND DEBRIS IN THE THROTTLE QUADRANT AT 6 O'CLOCK ENGINE POSIT ION. REMOVED DEBRIS, THROTTLES OPS NORMAL PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002021900103 20020219 00103 NM 2002 2 19 SWAA020322 1 20020211 A 2560 P2070001 FLASHLIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY FLASHLIGHTS INOP IN AFT CABIN. REMOVED AND REPLACED FLASHLIGHTS PER MM. 2 L 7 2 4F A16WE 2002021900104 20020219 00104 NM 2002 2 19 SWAA020323 1 20020212 A 3350 100885 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002021900105 20020219 00105 NM 2002 2 19 SWAA020326 1 20020212 A 5320 65C27314 STRINGER CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 11L, BS 767 AND 787. REMOVED AND REPLACED ST R CLIPS PER SRM. 2 L 7 2 4F A16WE 2002021900106 20020219 00106 NM 2002 2 19 SWAA020328 1 20020212 A 5320 6517583 STIFFENER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL CHORD CRACKED AT BS 178, WL 184 AND RBL 5.7. REPAIRED CHORD PER SRM. 2 L 7 2 4F A16WE 2002021900108 20020219 00108 NM 2002 2 19 SWAA020331 1 20020209 A 5754 65C26602223 SLAT BOEING 737 7375H4 138449D NM LT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D-CHECK, FOUND NR 2 L/E SLAT DISBONDED ON UPPER SURFACE OUTBOARD END OF T/E WEDGE. REMOVED AND REPLACE D NR 2 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2002021900109 20020219 00109 NM 2002 2 19 SWAA020332 1 20020210 A 5754 65C26686 SLAT BOEING 737 7375H4 138449D NM LT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D-CHECK, FOUND NR 3 L/E SLAT DISBONDED ON UPPER SURFACE AT THE T/E WEDGE ON INBOARD END AND OUTBOARD EN D. REPAIRED NR 3 L/E SLAT PER SRM. 2 L 7 2 4F RT A16WE 2002021900110 20020219 00110 NM 2002 2 19 SWAA020333 1 20020212 A 5314 6545866 KEELBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM SPLICE FITTING CORRODED AT BS 500D, FROM STR 28R TO 28L. REPAIRED KEEL BEA M PER SWA RA. 2 L 7 2 4F RT A16WE 2002021900111 20020219 00111 EA 2002 2 19 COMA0260105 1 20020215 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 455CA 107 7592 FLIGHT 5509 FLAPS FAILED DURING FLIGHT.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2002021900112 20020219 00112 EA 2002 2 19 COMA0260106 1 20020215 A 2750 860D10018ABC FCU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 403CA 1825 7428 FLIGHT 5363 FLAPS FAILED DURING APPROACH.REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2002021900113 20020219 00113 SO 2002 2 19 SWIA200210583 1 20020117 A 3234 12043270501 CONTROL BOX EMB 120 EMB120ER 3260203 SO LANDING GEAR MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 188SW 2167 2167 120039 AFTER TAKEOFF FROM JAC LANDING GEAR DID NOT RETRACT. HANDLE WENT UP BUT NO GEAR, HAD ALL LIGHTS - A & B, RED AND GREEN . SAME ON 2ND TRY PER MX CONTROL. RIGHT MAIN GEAR DOES NOT FULLY RETRACT ON FIRST TRY. CYCLED GEAR AND RETRACTION SUC CESSFUL. REMOVED AND REPLACED LANDING GEAR RELAY BOX IAW EMB MM 32-31-02. CYCLED GEAR SEVERAL TIMES. OPS CHECK GOOD. ADJUSTED RIGHT MLG ACTUATOR IAW 32-32-10. ALSO REPLACED LANDING GEAR RELAY BOX. S/N OFF: 120124, S/N ON 120230. 2 L 7 2 4T RT A31SO 2002021900119 20020219 00119 NM 2002 2 19 QXEA020294 1 20020216 A 3350 11521122 POWER SUPPLY GRIMES BOMBDR DHC8 DHC8401 NM CABIN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 179 100C0299 4055 SEA-AFT CABIN EMERGENCY LIGHTS EXTINGUSH 10 SECONDS AFTER TURNED ON. REMOVED AND REPLACED BOTH AFT EMERGENCY POWER SUPPL Y BATTERIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002021900120 20020219 00120 NM 2002 2 19 QXEA020295 1 20020216 A 3350 11521122 POWER SUPPLY BOMBDR DHC8 DHC8401 NM CABIN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 159 4055 SEA-LEFT HAND EXTERIOR EGRESS LIGHT IS INOP. REMOVED AND REPLACED POWER SUPPLY BATTERY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002021900123 20020219 00123 NM 2002 2 19 NOC2002F00000 1 20020206 A 2500 5A30863 SLIDE BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE DOOR ESCAP SLIDE INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 802NA 28587 SCHEDULED R1 DOOR SAMPLE SLIDE DEPLOYMENT UNSUCCESSFUL. R1 SLIDE DID NOT FULLY DEPLOY. INSPECTION FOUND SLIDE RESTRICT ED FROM FULLY DEPLOYING BY THE ESCAPE SLIDE STRAP. FURTHER INSPECTION FOUND EXCAPE SLIDE STRAP MISROUTED AND NOT SECURE D BEHIND SLIDE AS INDICATED IN INSTALLATION INSTRUCTIONS. DOOR SLIDES L1, L2 AND R2 REMOVED AS PRECAUTIONARY AND REINST ALLED TO INSURE SAME. QA REVIEW AND ACTION: 1)FLEET CAMPAIGN TO CHECK ALL DOOR SLIDES ON B737 FLEET. 2) QA BULLETIN T O BE ISSUED TO HIGHLIGHT ESCAPE SLIDE INSTALL AND STRAP LOCATION REQUIREMENT DURING ESCAPE SLIDE PACK AND COVER INSTALLA TION. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002021900140 20020219 00140 SO 2002 2 19 RAIA00202064 1 20020211 A 3243 39807 CONTROL VALVE EMB 145 EMB145LR 3260212 SO NOISY A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 811HK 3046 145256 5279-RIC-DURING TAXI HEARD NOISE FROM UNDER COCKPIT FLOOR. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE OUTBOARD BRAKE CONTROL VALVE, OPS AND LK CK OK. 2 L 7 2 4T RT T00011AT 2002021900141 20020219 00141 2002 2 19 RAIA00202066 4 20020218 A 2312 7510700806 RECEIVER JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 568HK 14081 514 41086 5535-STL- CREW REPORTED #1 COMM INOP. MAINTENANCE REMOVED AND REPLACED #1 COMM RECEIVER TRANSMITTER, OPS CK OK. 2 L 7 2 4T RT A41NM 2002021900142 20020219 00142 NM 2002 2 19 AWXA200200155 1 20020207 A 5330 507945265 SKIN BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - MAJOR REPAIR - "C" - DURING C-10 CHECK A 1/8" CRACK WAS FOUND AT THE R1 DOOR EXTERNAL SKIN UPPER HINGE CUTOUT LOWE R CORNER BS 307.25. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN, FABRICATED A REPAIR DOUBLER AND HINGE COVER, AND INSTALLED REPAIR PARTS IAW AWA EO 52-00-02, REV C. 2 L 7 2 4F RT A16WE 2002021900143 20020219 00143 NM 2002 2 19 AWXA200200156 1 20020219 A 3350 BMS13311122 WIRE BOEING 757 757225 1384959 NM SEAT ROW 12 L BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 PHX - EEL - "C" - DURING INSPECTION EMERGENCY EVACUATION LIGHT AT SEAT ROW 12 L/H DID NOT ILLUMINATE. MAINTENANCE TROUBL ESHOT AND FOUND A BROKEN WIRE AT SEAT ROW 12 L/H, REPAIRED WIRE IAW BOEING SWP 20-30-12. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002021900144 20020219 00144 NM 2002 2 19 AWXA200200151 1 20020218 A 3350 101114101 COVER BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 LAS - EEL - C - HORIZONTAL EMERGENCY EXIT COVER OVER SEAT ROW 10 LT IS BROKEN. MAINTENANCE REMOVED AND REPLACED THE HOR IZONTAL EMERGENCY EXIT LIGHT ASSEMBLY OVER SEAT ROW 10 LT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002021900145 20020219 00145 SO 2002 2 19 C2XA02CL047 1 20020212 A 2530 CBC16707 RECEPTACLE EMB 135 EMB135LR 3260305 SO GALLEY BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 28518 145334 CLE FLIGHT 3041 THE CREW REPORTED A BURNING SMELL COMING FROM THE COFFEE WARMERS. MAINTENANCE INSPECTED AND REPLACED TH E NR 2 COFFEE WARMER RECEPTACLE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2002021900146 20020219 00146 SO 2002 2 19 C2XA02CL049 1 20020214 A 3350 GE1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16954 145072 DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT LIGHT AT ROW 3 AND 12 WERE FOUND INOPERATIVE. MAINTENANCE REPLACED EMERGE NCY EXIT LIGHT BULB AT ROWS 3 AND 12. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002021900147 20020219 00147 SO 2002 2 19 C2XA02CL050 1 20020213 A 5270 14528237001 SWITCH EMB 145 EMB145ER 3260211 SO EMERGENCY EXIT LACK OF LUBE A C2XA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 27 14939 145030 DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT DOOR DID NOT INDICATE A OPEN MESSAGE ON THE EICAS WHEN THE D OOR WAS OPEN. MAINTENANCE INSPECTED AND FOUND THE MICROSWITCH ACTUATION PIN TO BE STICKING. THE PIN WAS LUBRICATED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002021900175 20020219 00175 NM 2002 2 19 QXEA0200094 1 20020207 A 3320 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN DEFECTIVE A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 354PH 498 GEG- FLIGHT ATTENDANT REPORTS SMOKE WAS COMING FROM AIRSTAIR DOOR LIGHT. RELAMPED LIGHT. OPERATIONAL CHECKS GOOD. AIRC RAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002021900176 20020219 00176 EU 2002 2 19 RAIA00202047 1 20020201 A 2612 FIRE LOOP AEROSP ATR72 ATR72202 8680940 EU LT ENGINE MALFUNCTIONED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 721TE 217 STL- LEFT ENGINE FIRE INDICATION. MAINTENANCE INSPECTED THE LEFT ENGINE AND FOUND NO EVIDENCE OF FIRE AND PLACED THE LE FT ENGINE FIRE LOOP-B ON DEFERRAL IAW MEL 26-12-1. 2 H 7 2 4T RT A53EU 2002021900177 20020219 00177 SO 2002 2 19 RAIA00202069 1 20020123 A 5320 14522460015 GUSSET EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL - DURING 8000 HOUR INSPECTION FOUND CORROSION ON FLOOR SUPPORT AT STRINGER 18L AT FRAME 17. REMOVED AND REPLACED FLOOR SUPPORT GUSSET AT STRINGER 18L FRAME 17 IAW SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002021900178 20020219 00178 SO 2002 2 19 RAIA00202070 1 20020123 A 5320 14521725001 SILL EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING 8000 HOUR INSPECTION FOUND CORROSION ON FLOOR SUPPORT AFT OF PAX DOOR. REMOVED AND REPLACED LEFT SILL IAW SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002021900179 20020219 00179 SO 2002 2 19 RAIA00202071 1 20020123 A 5320 14522459003 SUPPORT EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING 8000 HOUR INSPECTION FOUND CORROSION ON ANGLE SUPPORT FOR FORWARD CENTER FLOOR BOARD. REMOVED AND REPLACE D ANGLE SUPPORT AT FORWARD CENTER FLOOR BOARD IAW SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002021900180 20020219 00180 SO 2002 2 19 RAIA00202072 1 20020123 A 5320 14521725015 SILL EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING 8000 HOUR INSPECTION FOUND CORROSION AT TIE DOWN POINT FOR GALLEY FORWARD OF SERVICE DOOR. REMOVED AND RE PLACED SILL AT SERVICE DOOR, IAW SRM 53-21-10 AND 51-40-02. 2 L 7 2 4F RT T00011AT 2002021900181 20020219 00181 SO 2002 2 19 RAIA00202073 1 20020123 A 5320 14521725015 SILL EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING 8000 HOUR INSPECTION FOUND CORROSION ON THE GALLEY TIE DOWN POINT AFT OF THE SERVICE DOOR. REMOVED AND RE PLACED RIGHT HAND SILL AFT OF SERVICE DOOR, IAW SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002021900182 20020219 00182 SO 2002 2 19 RAIA00202074 1 20020123 A 5320 14521721009 WEB EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING 8000 HOUR INSPECTION FOUND CORROSION ON FORWARD DIGITAL WEB PLATE. REMOVED AND REPLACED FORWARD DIGITAL W EB, IAW SRM 53-21-10 2 L 7 2 4F RT T00011AT 2002021900183 20020219 00183 SO 2002 2 19 RAIA00202075 1 20020123 A 5320 14522460013 GUSSET EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL DURING 8000 HOUR INSPECTION FOUND CORROSION AT CENTER TOP CAP SKIN I/B OF SERVICE DOOR. REMOVED AND REPLACED CENT ER TOP CAP SKIN GUSSET, IAW SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002021900184 20020219 00184 SO 2002 2 19 C2XA02IA033 1 20020206 A 5300 14521725015 CREASE BEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 10967 145005 IAH- DURING "C" CHECK INSPECTION IT WAS NOTED THAT THE RIGHT CREASE BEAM BETWEEN FRAME 18 and 20 WAS CORRODED AROUND T HE NUT PLATES. IAH- MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE, WHEN RELEASED FROM "C" CHECK. 2 L 7 2 4F RT T00011AT 2002021900185 20020219 00185 SO 2002 2 19 C2XA02IA034 1 20020206 A 5300 14521725615 CREASE BEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 10967 145005 IAH- DURING "C" CHECK INSPECTION IT WAS NOTED THAT THE RIGHT CREASE BEAM BETWEEN FRAME 22 and 23 WAS CORRODED AROUND TH E NUT PLATES, IAH- MAINTENANCE REMOVED and REPLACED THE CREASE BEAM, AND, THE AIRCRAFT WAS APROVED FOR RETURN TO SERVI CE, WHEN RELEASED FROM "C" CHECK. 2 L 7 2 4F RT T00011AT 2002022000020 20020220 00020 NM 2002 2 20 C1HA200295003 1 20020215 A 3350 900542 BATTERY PACK BOEING 727 727290 138408W NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 Forward middle emergency exit light inoperative. Action Taken: Removed and replaced battery pack forward middle emerge ncy exit light. Ops check norma per 727 MM 33-50. 2 L 7 3 4F A3WE 2002022000021 20020220 00021 NE 2002 2 20 C1HA200297005 2 20020215 A 7260 780650 GEARBOX BOEING 727 727270 138408P NM PWA JT8 JT8D17 52049 NE A C1HA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 697CA 23052 688133 At 33,000 feet with cruise power set, engine #2 oil temp rose from 110 to 120 C, 2 seconds later oil quantity dropped fr om 4 gallons to .2 gallons. Oil pressure dropped from 50 PSI to 42 PSI. We brought the engine to idle, engine gauges s tabilized at .2 gallons, temp 110 C and pressure was 42 PSI. After bringing power back up to cruise oil pressure droppe d to 20 PSI. Ran the precautionary shutdown checklist. Engine windmilled for 28 minutes, oil qty stayed at 20 PSI. En gine gauges never exceeded limits. Action Taken: Removed and replaced gearbox assemly IAW JT8D MM 72-60. Performed le ak check and test and engine run IAW JT8D MM 72-00. No leaks noted. 2 L 7 3 4F 4 F RT A3WE E2EA 2002022000034 20020220 00034 SO 2002 2 20 C2XA02IA029 1 20020215 A 3260 12038594001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO COCKPIT DEFECTIVE A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 17728 120182 IAH- DURING FLIGHT 3916 THE CREW NOTED THAT THE LEFT MAIN SYSTEM -A- LANDING GEAR GREEN INDICATION LIGHT ILLUMINATES IN FLIGHT WITH THE GEAR HANDLE UP. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL, PERFORMED A OPERATIONAL CHE CK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002022000035 20020220 00035 SO 2002 2 20 C2XA02IA032 1 20020217 A 3230 12043270501 CONTROL BOX EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A C2XA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 27 17728 120182 IAH- DURING APPROACH FLIGHT 3989, THE CREW NOTED THE FOLLOWING, THE LANDING GEAR WOULD NOT COME DOWN. LEFT GEAR SYSTEM -A- LIGHT (GREEN) ON AND ALL OTHER RED LIGHTS ILLUMINATED (SYSTEM-B AND RIGHT AND NOSE SYSTEM-A). GEAR WAS CYCLED, BUT DID NOT COME DOWN UNTIL AFTER GO-AROUND IN A 30 DEGREE BANK. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL RELAY BOX, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002022000036 20020220 00036 SO 2002 2 20 C2XA02TY030 1 20020218 A 5320 14522459003 SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS DURING A SCHEDULED 1-C INSPECTION THE RAMP SUPPORT ON THE CENTER OMEGA BEAM BETWEEN FR'S 19 AND 20 HAS A AREA OF COR ROSION. MAINTENANCE REMOVED AND REPLACED THE RAMP SUPPORT IAW EMB 135/145 SRM 51-40-02. WORK WAS SATISFACTORY AND WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002022000037 20020220 00037 GL 2002 2 20 C2XA02TY031 2 20020218 A 7270 23061859 DUCT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 2 ENGINE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND BETWEEN THE OUTER BYPASS AND THE FAN CASE ON NR 2 ENGINE. MA INTENANCE CLEANED THE AFFECTED AREA, APPLIED A CHEMICAL COATING AND APPLIED CORROSION RESISTANT PAINT IAW EC7000-01001. WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2 L 7 2 4F 4 F RT TOOO11AT TE6CH 2002022000038 20020220 00038 SO 2002 2 20 C2XA02TY032 1 20020218 A 3397 78812 WIRE EMB 135 EMB135LR 3260305 SO CABIN BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS DURING A SCHEDULED 1-C INSPECTION A BROKEN WIRE WAS FOUND ON THE PROXIMITY LIGHT STRIP ON PANEL 251DF. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP IAW EMB 135/145 AMM 33-50-12. OPS CHECK GOOD AND WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002022000039 20020220 00039 NM 2002 2 20 CALA0200071 1 20020213 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND NUTS MILLED INTO KEEL BEAM JUST FORWARD OF BULKHEAD AT STA 727 LT SIDE. REPAIRED KEEL BEAM IAW ECRA 53 10-03740. 2 L 7 2 4F RT A16WE 2002022000040 20020220 00040 NM 2002 2 20 CALA0200073 1 20020215 A 3350 20121 POWER SUPPLY BOEING 767 767* NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 67157 30436 INSPECTION FOUND RT OVERWING EXIT DOOR EMERGENCY LIGHTS AND LAST THREE CENTER SEAT LIGHTS IN FIRST CLASS AISLE INOPERATI VE. THE POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-07 AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A1NM 2002022000041 20020220 00041 NM 2002 2 20 CALA0200076 1 20020216 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 947-967, LBL 18 AND RBL 18. THE FLOOR SUPPORTS WERE REMOVED AND REPLACE D IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002022000042 20020220 00042 NM 2002 2 20 CALA0200077 1 20020216 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 967-986, LBL 18 AND RBL 18. THE FLOOR SUPPORTS WERE REMOVED AND REPLACE D IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002022000043 20020220 00043 NM 2002 2 20 CALA0200078 1 20020216 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 951, LBL 14 TO LBL 16 AND AT LBL 18 TO LBL 24. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002022000044 20020220 00044 WP 2002 2 20 DHL2002806004 1 20020214 A 3260 DOWNLOCK SWITCH DOUG DC8 DC873F 302199F WP LT MLG CORRODED A DHLA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 806DH 46002 UPON EXTENSION OF LANDING GEAR, LEFT MAIN GEAR DID NOT ILLUMINATE. CYCLE GEAR ONCE, LIGHT CAME ON UPON GEAR EXTENSION. REMOVED AND REPLACED LT MAIN GEAR BULBS AND INSPECTED WIRING AT GEAR HANDLE AREA, RESECURED. FOUND CORROSION AT LT MAIN GEAR DOWNLOCK SWITCH. REMOVED AND REPLACED IAW MM 32-60-0. FURTHER TROUBLESHOOTING CONTINUED. FOUND PINS AT DOWNLOCK SWITCH CORRODED. FOUND TERMINAL STRIP CONNECTOR CORRODED FROM DOWNLOCK CONDUIT WIRES AND CONDUIT DAMAGED. REMOVED AND REPLACED CONDUIT, PINS AND CONNECTORS AT TERMINAL STRIP PER DACO M/M. 2 L 7 4 4F RT 4A25 2002022000049 20020220 00049 WP 2002 2 20 DHL2002807003 1 20020214 A 3297 WIRE DOUG DC8 DC873F 302199F WP COCKPIT DAMAGED A DHLA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 807DH 45990 WITH GEAR DOWN, NO LEFT MLG DOWN INDICATION. DURING CYCLING OF LANDING GEAR, THE LOWER NOSE GEAR LAMP ALSO FAILED BUT I LLUMINATED AGAIN ON TOUCHDOWN. NO GEAR UNSAFE LIGHT ASSOCIATED WITH FAILURE. FOUND WIRE FROM SWITCH S1-208 CONNECTOR P 1-1397 PIN L, GOING TO TERMINAL BLOCK S3-70 TERMINAL 2 OPEN, REPAIRED WIRE FROM CONNECTOR TO TERMINAL, CHECKED NORMAL IN DICATION. 2 L 7 4 4F RT 4A25 2002030400222 20020304 00222 NE 2002 3 4 FE5F200200001 2 20020216 A 7230 1B6507 BLADE BOEING 757 75727A NM PWA 2037 PW2037 NE RT ENGINE FRACTURED Z FE5F E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 03 CTEXT 5534 29608 728717 DURING CLIMBING THRU 12,000 FT, A BANG WAS HEARD FROM RT ENG AND THEN EPR DROPPED. IAW QRH, PILOT SHUT DOWN THE ENG AND TURNED BACK. BORESCOPE INSPECTION REVEALED ONE 7TH HPC BLADE UNDER-PLATFORM FRACTURED, THE ADJACENT BLADE CRACKED AND SUBSEQUENT STAGE DAMAGED. TAIL NUMBER B-27013 2 L 7 2 4F 4 F RT A2NM E17NE 2002022000053 20020220 00053 CE 2002 2 20 GLBA2002021 1 20020212 A 6123 5038912121 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE LEFT FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 247GL 986 UE247 AUTO FEATHER LIGHT ILLUMINATED INFLIGHT. REPLACED HIGH PRESSURE SWITCH, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002031200140 20020312 00140 WP 2002 3 12 IXXA0200005O 1 20020215 A 7110 D51B212003 COWLING DOUG DC8 DC871F 302199D WP NR 2 ENGINE DEPARTED A IXXA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SW 11 830BX 73103 2853 45973 EN ROUTE, SHORTLY AFTER TAKEOFF THE FLIGHT CREW HEARD AN ABNORMAL NOISE IN THE COCKPIT. THE FLIGHT CREW CYCLED THE LAND ING GEAR BUT THE NOISE WAS STILL PRESENT. THE FLIGHT RETURNED TO MCO FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE NUMBER TWO ENGINE FAN COWLINGS HAD DEPARTED THE AIRCRAFT. THE ENGINE FAN COWLS WERE REP LACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002022000054 20020220 00054 EU 2002 2 20 MALA020157 1 20020212 A 2450 52653025 CIRCUIT BREAKER BAC 146 AVRO146RJ85A 1500097 EU COCKPIT DEFECTIVE A MALA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 GL 15 503XJ E2310 DURING FLIGHT 3663 AC DEPARTED MSP. F/O'S EFIS DISPLAY WENT BLANK, LOST LT I/B FUEL PUMP, FLAP TRIM COMPENSATOR, RT COO LING FAN, PRESSURIZATION LT ON ONE CHANNEL AND NR 2 ADC. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED CB XD11 F OR AC NR 2 BUSS P/N 52653-025, FLO'S OPS CHECK GOOD IAW AVRO MM CHAP 24. 2 H 7 4 4F RT A49EU 2002022000055 20020220 00055 EU 2002 2 20 MALA020158 1 20020131 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 511XJ E2325 DURING C2-CHECK IN CVG, AC SUFFERED DENTS TO FUSELAGE LT SKIN AT FRAME 20. BETWEEN STRINGERS 14 &16 JUST AFT OF PREVIOU S REPAIR, DAMAGE REPAIRED IAW RIL HC536H9316, BARA/AVR 5747/02 DC AND EO A53071 DURING C-1/C-2 INTERVAL. 2 H 7 4 4F RT A49EU 2002022000056 20020220 00056 EU 2002 2 20 MALA020159 1 20020131 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 511XJ E2325 DURING C2-CHECK IN CVG, CORROSION DISCOVERED ON NR 1 SEAT RAIL TOP FLANGES AT FRAMES 18 & 20 THAT EXCEEDED SRM LIMITS. AC REWORKED (CORROSION REMOVED) AND APPROVED FOR RETURN TO SERVICE IAW BARA/AVR5752/02-DC. 2 H 7 4 4F RT A49EU 2002022000057 20020220 00057 EU 2002 2 20 MALA020160 1 20020206 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 511XJ E2325 DURING C-2 CHECK IN CVG, AC SUFFERED A DENT TO THE FUSELAGE SKIN (RT SIDE) AT FRAME 11, 18 INCHES BELOW THE C-SCREEN WIN DOW. DAMAGE REPAIRED IAW BARA/AVR/5764/02-DC, RIL HC537H9449 AND EO 53072 DURING C-CHECK INTERVAL. 2 H 7 4 4F RT A49EU 2002022000067 20020220 00067 EU 2002 2 20 MALA020161 1 20020208 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 511XJ E2325 DURING C2-CHECK IN CVG, CORROSION DISCOVERED ON NR 3 SEAT RAIL BETWEEN FRAMES 18 & 20 THAT EXCEEDED SRM LIMITS. SEAT RA IL REMOVED BETWEEN FRAMES 18 AND 20, REPLACED IAW SRM 53-00-32, BARA/AVR 5765/02-DC AND EO 53026 DURING C-CHECK INTERVAL . 2 H 7 4 4F RT A49EU 2002022000068 20020220 00068 EU 2002 2 20 MALA020162 1 20020208 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 511XJ E2325 DURING C2-CHECK IN CVG, CORROSION DISCOVERED ON NR 4 SEAT RAIL BETWEEN FRAMES 18 & 20 THAT EXCEEDED SRM LIMITS. SEAT RA IL REMOVED BETWEEN FRAMES 18 & 20 AND REPLACED IAW SRM 53-00-32, BARA/AVR/5765/02 DC AND EO 53026 DURING C-CHECK INTERVA L. 2 H 7 4 4F RT A49EU 2002022000070 20020220 00070 WP 2002 2 20 MWEA020128 1 20020214 A 2131 CONTROLLER DOUG DC9 DC932 3022066 WP CABIN PRESSURE FAILED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 CABIN PRESSURE CONTROL FAILED, SELECTED MANUAL. PERFORMED BIT CHECKS ON BOTH CONTROLLERS, BOTH SHOWED CONTROLLER FAILUR ES. CHECKED MANUAL OPS OF OUT FLOW VALVE, OPERATIONAL CHECKS GOOD. DEFERRED BOTH AUTO PRESS CONTROL SYSTEMS PER MEL 21 -24B. 2 L 7 2 4F A6WE 2002022000076 20020220 00076 NE 2002 2 20 RAIA00202077 2 20020219 A 7510 39702022 VALVE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 555HK 12869 41072 75075 5642-STL- LEFT ENGINE ANTI-ICE FAILED. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE ANTI-ICE VALVE. 2 L 7 2 4T 4 T RT A41NM E18NE 2002022000078 20020220 00078 NM 2002 2 20 CA020201001 1 20020121 A 2781 FE278001 INDICATOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA ELEVATOR TRIM FAILED W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA (CAN) DURING THE TAKEOFF ROLL ELEVATOR TRIM INDICATOR JUMPED TO THE FULL NOSE DOWN POSITION AND THE TAKEOFF WARNING HO RN SOUNDED. ABORTED TAKEOFF. FCECU RESET IAW REFERENCE INSTRUCTION LETTER (RIL) 84-27-004. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002022000079 20020220 00079 NM 2002 2 20 CA020201002 1 20020118 A 2450 67003008010 CONTROL PANEL DHAV DHC8 DHC8101 2809002 NM PWA PW121 PW121 52124 NE HAMSTD 14SF 14SF7 NE AC POWER FAILED W E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) DURING ENGINE START, FLIGHT CREW DETECTED ELECTRICAL BURNING ODOUR AFTER SELECTING BOTH ENGINE CONDITION LEVER FR OM FEATHER TO MIN. LEFT AC VM PHASE A, B, C AND RIGHT AC VM PHASE A, B, C ALL CIRCUIT BREAKERS POPPED. FLIGHT CREW THEN SHUT DOWN BOTH ENGINES AND DEPLANED PASSENGERS.MAINTENANCE FOUND AC POWER MONITOR PANEL WAS SOURCE OF ODOR. PANEL CONNEC TOR PINS X, Y AND Z WERE PUSHED BACK. PANEL INTERNAL PC BOARDS SHOWED EVIDENCE OF BURNING. AIRCRAFT SIDE CANON PLUG PINS Y AND Z WERE BURNT. CANON PLUG 2420-P1 REPLACED, AC POWER MONITOR PANEL REPLACED, AND 12 INCHES OF WIRES 20016B-22 AND 10016C-20 REPLACED DUE TO HEAT DAMAGE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002022000083 20020220 00083 NE 2002 2 20 CA020201011 2 20020127 A 7200 ENGINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE NR 1 FAILED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION AP APPROACH 1 CA (CAN) DURING FINAL APPROACH , FLAPS 33 DEGREES , 160KNOTS ON FLIGHT TSC 372 FROM YMX TO MCO THERE WAS A HIGH VIBRATION O N NR 1 ENGINE AT 3.8 UNITS ON CHANNELS A & B. THE AIRCRAFT LANDED SAFELY AND THE ENGINE VIBRATION DRILL WAS CARRIED OUT . THE BOROSCOPE CARRIED OUT AT MCO REVEALED THAT THE HP 4 COMPRESSOR WAS SATURATED IN OIL. THE AIRCRAFT WAS FERRIED BACK TO YMX ON A SPECIAL FLIGHT PERMIT TO HAVE THE ENGINE REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 2002022000085 20020220 00085 NM 2002 2 20 0200325530 1 20020210 A 3260 INDICATOR BOEING 757 757251 1384970 NM COCKPIT INOPERATIVE A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 530US 23845 UPON GEAR EXTENSION, THE LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. THE LANDING GEAR WAS CYCLED; NO CHANG E IN INDICATION. THE FLIGHT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN GEAR INDICATOR ASSEMBLY. SYSTEM TESTS WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 2002022000086 20020220 00086 NM 2002 2 20 0200345649 1 20020203 A 3397 WIRE BOEING 757 757251 1384970 NM CABIN DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 549US 26496 DURING SCHEDULED MAINTENANCE, THE ESCAPE PATH LIGHTING AT ROWS 25-30 WAS INOPERATIVE. MAINTENANCE REPAIRED DAMAGED TRAC K LIGHT WIRING AT ROW 29. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 2002022000088 20020220 00088 NM 2002 2 20 0200356613 1 20020208 A 3320 BALLAST BOEING 747 747251B 1384892 NM GALLEY MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 613US 20358 DURING FLIGHT, GALLEY NR 5 WORK LIGHT CONTROL BOX EMITTED SMOKE. PULLED CIRCUIT BREAKER AND SMOKE DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED BALLAST AND SOCKET INSIDE LIGHT CONTROL BOX. OPERATION AL CHECK GOOD. 2 L 7 4 4F A20WE 2002022000092 20020220 00092 NM 2002 2 20 0200362290 1 20020214 A 2910 CLAMP BOEING 727 727251 138408H NM HYDRAULIC SYS BROKEN A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 290US 21378 AFTER TAKEOFF, THE -A- SYSTEM HYDRAULIC QUANTITY WENT TO ZERO DURING FLAP RETRACTION. CREW FOLLOWED COM PROCEDURE AND V ERIFIED NO FLUID OR PRESSURE IN THE -A- SYSTEM. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLAC ED BROKEN CLAMP ON MAIN HYDRAULIC SYSTEM FILTER. MAINTENANCE FOLLOWED ALL FLUID LOSS MM PROCEDURES FOR MM 29-11-00, PG 1. ALL LEAK AND OPERATIONAL CHECKS OK. 2 L 7 3 4F A3WE 2002022000098 20020220 00098 NE 2002 2 20 02046333 2 20020215 A 7260 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE LT ENGINE CONTAMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 333UE 41101 DURING CLIMB OF THE FLIGHT FROM IAD TO EWR, THE CREW REPORTED THAT THE LEFT ENGINE OIL CONTAM LIGHT ILLUMINATED ON THE C AP PANEL. THE AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL INSPECTED AND FOUND ONE META L SLIVER ON THE LEFT ENGINE MAGNETIC CHIP DETECTOR. THE CHIP DETECTOR WAS CLEANED AND REINSTALLED, AN OIL SAMPLE WAS TA KEN FOR SOAP, AND ENGINE RUN OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A41NM E18NE 2002022000101 20020220 00101 EU 2002 2 20 02047328 1 20020216 A 2131 22260C020303A CONTROLLER JETAIR JETSTM JETSTM4101 1500501 EU CABIN PRESSURE FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 328UE 41083 DURING CLIMB OF THE FLIGHT FROM IAD TO JFK, THE CREW REPORTED THAT THE CABIN WOULD NOT PRESSURIZE IN MANUAL MODE. THE A UTOMATIC MODE WAS INOPERATIVE AND ON DMI. THE AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSON NEL REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETU RNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002022000103 20020220 00103 NM 2002 2 20 02FDEA00127 1 20020216 A 3260 SWITCH BOEING 727 727247 138408F NM NLG DOOR FAULTY A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 234FE 21328 ON GEAR RETRACTION NOSE GEAR DOOR LIGHT SYS ON DIMLY. REMOVED AND REPLACED NOSE GEAR DOOR WARNING SWITCHES PER MM 32-62 -011-4. 2 L 7 3 4F A3WE 2002022000104 20020220 00104 NM 2002 2 20 02FDEA00131 1 20020219 A 2781 G1133A1 INDICATOR BOEING 727 727227 1384078 NM COCKPIT MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 488FE 21491 AFTER DEPARTURE NR 5 LED WOULD NOT RETRACT. RAN RED TABS, NO RELIEF. REMOVED AND REPLACED SLAT-FLAP DISPLAY MODULE PRE CAUTION PER MM 27-82-031-4. 2 L 7 3 4F A3WE 2002022000108 20020220 00108 GL 2002 2 20 02042645 1 20020211 A 5610 601R3303310 WINDSHIELD BOMBDR BD700 BD7001A10 1390006 GL CRACKED A VTZA K NONE O OTHER CR CRUISE 1 EA 27 645BR 5077 7383 DISCREPANCY - FO'S WINDSHEILD CRACKED IN FLIGHT AT FL 370 - CABIN PRESSURE OK. CORRECTIVE ACTION - R&RD FO'S WINDSHEILD IAW MM CH 56-11-01 2 L 7 2 4F RT T00003NY 2002022000109 20020220 00109 2002 2 20 COMA0210005 4 20020217 A 2210 6225734002 SERVO EMB 120 EMB120RT 3260202 SO AVIONICS BINDING A COMA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SO 01 267CA 3879 120259 FLIGHT 5009 PILOT AND COPILOT RUDDER PEDALS BINDING.REPLACED THE RUDDER SERVO. 2 L 7 2 4T RT A31SO 2002022000110 20020220 00110 SO 2002 2 20 COMA0210006 1 20020216 A 3010 2957D513539 BOOT EMB 120 EMB120RT 3260202 SO VERT FIN PERFORATED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 01 268CA 120262 FLIGHT 5059 HORZ STAB AND VERT FIN DEICE FAILED.REPLACED THE VERT STABILIZER DEICE BOOT. 2 L 7 2 4T RT A31SO 2002022000111 20020220 00111 EA 2002 2 20 COMA0260107 1 20020216 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 716CA 12203 7250 FLIGHT 5324 GEAR DISAGREE AND NOSE DOOR WARNINGS WHEN LANDING GEA SELECTED DOWN.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002022000112 20020220 00112 EA 2002 2 20 COMA0260108 1 20020217 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 914CA 7012 FLIGHT 5675 FLAPS FAILED DURING LANDING.RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002022000113 20020220 00113 EA 2002 2 20 COMA0260109 1 20020218 A 3150 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 951CA 7091 FLIGHT 6080 CONFIG TRIM, CONFIG SPOILERON, AND CONFIG AILERON WARNINGS DURING T/O.COULD NOT DUPLICATED - INEROGATED MDC AND FOUND NO FAULT CODES. 2 L 7 2 4F RT A21EA 2002022000114 20020220 00114 EA 2002 2 20 COMA0260110 1 20020216 A 3230 7179015 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA INST PANEL MALFUNCTIONED A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 954CA 14734 7100 FLIGHT 5806 NLG DOORS OPENED IN FLIGHT - GEAR DISAGREE WARNING.REPLACED THE L/G CONTROL - SELECTOR ASSY. 2 L 7 2 4F RT A21EA 2002022000115 20020220 00115 NM 2002 2 20 SWAA020375 1 20020217 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1.75 INCHES LONG BETWEEN BS 787 AND 807, STR 27L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002022000116 20020220 00116 NM 2002 2 20 SWAA020376 1 20020217 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES LONG AT BS 888, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002022000117 20020220 00117 NM 2002 2 20 SWAA020377 1 20020216 A 3350 W13022222 WIRE BOEING 737 7373Q8 1384670 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 WITH ALL ELECT PWR REMOVED FROM A/C, EMERGENCY EXIT LIGHTS REMAINED ILLUMUNATED WITH LIGHT SWITCH IN OFF POS. FOUND WIR E LOOSE. SECURED WIRE PER MM. 2 L 7 2 4F RT A16WE 2002022000118 20020220 00118 2002 2 20 SWAA020378 4 20020217 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 FWD SVC DOOR EMERGENCY EVAC SLIDE NOT SECURED IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002022000119 20020220 00119 NM 2002 2 20 SWAA020380 1 20020217 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 392SW 27379 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED .25 INCH LONG AT BS 179, WL 227 AND LBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002022000120 20020220 00120 NM 2002 2 20 SWAA020381 1 20020216 A 5312 6517582 WEB BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED .25 INCH LONG AT BS 181.5, WL 182 AND RBL 17.1. REPAIRED W EB PER SRM. 2 L 7 2 4F RT A16WE 2002022000121 20020220 00121 NM 2002 2 20 UPS02237711 1 20020206 A 5700 654130116 CASTING BOEING 727 72731C 1384011 NM #5 FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C #5 FLAP TRACK ATTACH POINT ON LWR SURFACE OF WING, CORROSION EXIDENT IN AFT PAD, O/B HOLE. CORROSION SEEMS TO BE CONFINED TO BARREL NUT CASTING. REMOVED CASTING ON O/B OF #5 FLAP TRACK IAW SRM 51-30-02, CASTING RE PLA CED IAW BOEING DWGS 65-41301 AND 65-16216 AND SRM 51-30-02. 2 L 7 3 4F A3WE 2002022000122 20020220 00122 NM 2002 2 20 VNAA0202021 1 20020218 A 3200 ZCV1571 CHECK VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 438JS 13 3056 TWENTY MINUTES INTO THE FLIGHT, THE CREW RECEIVED A CAS MESSAGE STATING THE EMERGENCY PARKING BRAKE ACCUMULATOR PRESSURE WAS LOW. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND TURNED ON THE STAND BY PUMP TO MANUAL AND SET THE PARKING BRAKE FOR 10 SECONDS. THE LIGHT WENT OUT. AFTER ANOTHER TWENTY MINUTES THE CREW RECEIVED THE SAME INDICATION AND FLIGHT 4063 RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE HYDRUALIC CHECK VALVE IN ACCORDANCE WITH DORNIER MAINTENA NCE MANUAL 29-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002022000123 20020220 00123 NM 2002 2 20 VNAA0202019 1 20020214 A 3200 BRAKE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 440JS 3058 THE CREW REPORTED THAT THE FIRST OFFICER'S BRAKES WERE NOT RESPONDING CORRECTLY. MAINTENANCE INSPECTED AND BLED THE BRA KE WITH THE PILOT VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND T HE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002022000124 20020220 00124 NM 2002 2 20 VNAA0202015 1 20020213 A 7100 PW119B ENGINE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA E ENGINE SHUTDOWN O OTHER LD LANDING 1 GL 07 426JS 3038 AFTER BEING CLEAR FOR A VISUAL APPROACH, THE CREW REPORTED ENTERING AN AREA OF MODERATE TURBULENCE. THERE WAS A SINGLE JOLT, NOBODY SUSTAIN ANY SERIOUS INJURIES. THE LEFT HAND ENGINE WAS REPORTED TO SHUT DOWN DURING THE EVENT. WITHOUT SU FFICIENT TIME FOR A RESTART, FLIGHT 4096 LANDED WITHOUT ANY FURTHER INCIDENTS. THE AIRCRAFT WAS INSPECTED FOR DAMAGE, N ONE WAS FOUND. THE CREW PERFORMED POWER ASSURANCE RUNS WHICH CHECKED GOOD. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE PERFORMED AN AUTO FEATHER TEST AND POWER ASSURANCE RUNS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00- 00. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002030400166 20020304 00166 NM 2002 3 4 F3LA200200041 1 20020205 A 5320 BEAM BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED BEAM IN FWD BULKHEAD AT BL 20, WL 160, CORRODED AT NUT PLATE ATTACHMENT POINT FOR LWR DUCT SHROUD BRACKETS. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-40-4. 2 L 7 2 4U RT A16WE 2002022000137 20020220 00137 WP 2002 2 20 GTIA012218 1 20020117 A 5410 WEB DOUG DC9 DC932 3022066 WP NR 1 PYLON CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 FTW - NR 1 ENGINE PYLON LOWER SURFACE AFT HINGE PANEL OUTBOARD LOWER WEB CRACKED AT ANGLE. REMOVED WEB. FABRICATED NEW WEB. INSTALLED WEB. REMOVED DAMAGED SECTION OF ANGLE. FABRICATED REPAIR ANGLE AND DOUBLERS. INSTALLED REPAIR ANGLE AND DOUBLERS IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002022000138 20020220 00138 NM 2002 2 20 DL757020028 1 20020109 A 5330 146N34303 SKIN BOEING 757 757232 1384965 NM FS 1610, S-26L GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 FUSELAGE / SKIN / FS 1610 / STRG. 26L : DENT & GOUGE REPAIR THE FUSELAGE SKIN WAS DENTED AND GOUGED BY TOOLING AT FS 1610 JUST ABOVE THE STRINGER 26L SKIN LAP JOINT. THE DAMAGE WAS REMOVED WITH A 1" CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 382233-14, REV A. 2 L 7 2 4F RT A2NM 2002022000139 20020220 00139 NM 2002 2 20 DL757020037 1 20020111 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM FS 1680, S-17L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 FUSELAGE / SKIN / FS 1620-1720 / STRG. 14A-20L : SKIN REPLACEMENT THE FUSELAGE SKIN WAS FOUND WITH NUMEROUS DENTS AND GOUGES NEAR THE L4 DOOR OPENING. THE SKIN PANEL WAS REMOVED TO ELIMINATE ALL OF THE DAMAGE LOCATIONS. A NEW SKIN PANEL WAS INSTALLED PER ER/A 382226-14. 2 L 7 2 4F RT A2NM 2002022000140 20020220 00140 NM 2002 2 20 DLM11020040 1 20020111 A 3240 26094724 BRAKE DOUG MD11 MD11 3023602 NM NBR 8 POSITION UNSERVICEABLE A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 812DE DL265 48601 ON T/O ROLL NOTICEABLE PULL TO RIGHT. DURING CLIMBOUT CHECKED BRAKE TEMP NO. 8 READ 280 ALL OTHERS AT 60. 20 MINS INTO CLIMB TEMP BEGAN TO INCREASE RAPIDLY. TEMP DIFF LIGHT ALSO ILLUM MAX TEMP AT 475 DEG.__REMOVED AND REPLACED NBR 8 BRAKE ASSY. BLEED NBR 8 BRAKE DID ANTISKID RTS CHECK GOOD 2 L 7 3 4F RT A22WE 2002022000141 20020220 00141 NM 2002 2 20 DL76L020043 1 20020111 A 2110 211002469 HEAT EXCHANGER BOEING 767 767332 1382001 NM A/C BAY CRACKED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 178DN 25143 RTB..ON TAXI RT PACK INOP. RT DUCT LEAK EICAS MSG. FOUND RT HEAT EXCHANGER CRACKED LEAKING HOT AIR AND PRIMARY ALSO DAMA GED. DUE CREW DUTY TIME FLT CXLD. REPLACED RT HEAT EXCHANGER ASSY WITH PART SHIPPED FROM ATL. LEAK AND OPS CK OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2 L 7 2 4F RT A1NM 2002022000142 20020220 00142 NM 2002 2 20 DLM88020050 1 20020114 A 3040 NONE CONNECTOR DOUG MD88 MD88 3023688 NM WINDSHIELD LOOSE A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 921DL 49645 ON TAXIOUT SPARKS AT FO WINDSHIELD HEAT CONNECTOR BLOCK/ FOUND LOOSE SCREW AT WIRE L ON FO WINDSHIELD HEAT CONN BLOCK. CLEANED WINDSHIELD AND CONNECTOR MATING SURFACES. REINSTALLED CONN BLOCK. WINDSHIELD HEAT OPS NML. 2 L 7 2 4F RT A6WE 2002022000144 20020220 00144 NM 2002 2 20 DL767020053 1 20020115 A 3300 333201089 BATTERY BOEING 767 767232 1385132 NM MID CABIN DISCHARGED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 115DA 22227 MID LEFT AND RIGHT OVERHEAD EMERGENCY LIGHTS INOP REPLACED_BATTERY PACKS 2 L 7 2 4F RT A1NM 2002022000145 20020220 00145 NM 2002 2 20 DL777020067 1 20020119 A 2530 72077500 OVEN BOEING 777 777232 1385232 NM MID GALLEY UNSERVICEABLE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 863DA 29735 GALLEY FWD 2 DOOR CENTER OVEN OVERHEATS WHEN TURNED ON STRONG ELECT SMELL NOTICED BY FLT ATTEND. REPLACED OVEN IN MID GA LLEY POS 1 OPS CHECK GOOD MCO AND PLACARD REMOVED ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS 2 L 7 2 4F RT T00001SE 2002022000146 20020220 00146 NM 2002 2 20 DL738020073 1 20020119 A 3260 285A16003 SENSOR BOEING 737 737832 13844CF NM RIGHT GEAR WELL FAILED A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 387DA 30374 AIR RETURN TO SLC. AFTER LIFTOFF GOT PSEU LIGHT, AUTO THROTTLES DISENGAGED, TCAS INOP, FEEL DIFF PRESSURE, AND TAKEOFF WARNING HORN WHEN THROTTLES ADVANCED. REPEAT WRITE-UP OF PREVIOUS DAYS AIR RETURN. PSEU HAS A HARD FAULT OF THE SPOILE RS GROUND INTERLOCK SENSOR S1050. FAULT CODE 31-51001 GSBV CL FAULT. SUSPECT PROX SENSOR S1050. CA RPLD SENSOR, OP CKS NML 2 L 7 2 4F RT A16WE 2002022000147 20020220 00147 NM 2002 2 20 DL757020086 1 20020123 A 5330 146N37805 SKIN BOEING 757 757232 1384965 NM FS 1701, S-20L GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 FUSELAGE / SKIN / FS 1701 / STRG. 20L / SKIN LAP JOINT : GOUGE CUTOUT REPAIR THE LOWER SKIN OF THE STRINGER 20L SKIN LAP JOINT WAS GOUGED BY TOOLING AT FS 1701. THE DAMAGED AREA OF SKIN WAS TRIMMED OUT. THE SKIN LAP WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 382287-14, REV A. 2 L 7 2 4F RT A2NM 2002022000148 20020220 00148 NM 2002 2 20 DL757020090 1 20020124 A 2530 831620403M0DA OVEN BOEING 757 757232 1384965 NM AFT GALLEY UNSERVICEABLE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 663DN 24992 F/A REPORTED A BURNING SMELL IN THE BACK OF THE AIRCRAFT. THE AREA ABOVE THE OVENS. SHELF ABOVE THE OVENS WAS VERY HOT CUPS AND ACCES WERE REMOVED. CHECKED AFT LAVS AND OVERHAED LIGHT NO TROUBLE FOUND. CYCLED PACKS NO HELP. DECISION MADE TO DIVERT AIRCRAFT TO ATL._C/A REPLACED OVEN 2 L 7 2 4F RT A2NM 2002022000149 20020220 00149 NM 2002 2 20 DL757020102 1 20020126 A 5330 143N36504 SKIN BOEING 757 757232 1384965 NM FS 770, S-19R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 FUSELAGE / SKIN / FS 770-780 / STRG. 18R-19R : CORROSION CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND CORRODED AT SEVERAL NUTPLATE ATTACH HOLES FOR THE WING-TO-BODY FAIRING BETWEEN FS 770 & 780, ABOVE THE STRINGER 19R SKIN LAP JOINT. TWO AREAS OF CORROSION WERE REMOVED WITH 1" HOLES. THE AREA WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 382459- 14, REV A. 2 L 7 2 4F RT A2NM 2002022000150 20020220 00150 NM 2002 2 20 DL757020104 1 20020125 A 5330 146N36104 SKIN BOEING 757 757232 1384965 NM FS 1701, S-29L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 FUSELAGE / SKIN / FS 1701 / STRG. 29L : CRACKED HOLE REPAIR A SMALL CRACK WAS FOUND AT FASTENER HOLE DUE TO IMPROPER FASTENER INSTALLATION AT FS 1701 AND STRINGER 29L. THE CRACK WAS REMOVED WITH A .5" HOLE. THE HOLE WAS ADJACENT TO THE EDGE OF AN EXISTING INTERNAL REPAIR DOUBLER. TO REPAIR THE NEW DAMAGE, AN EXTERNAL ALUMINUM REPAIR DOUBLER WAS INSTALLED, OVERLAPPING THE EXISTING DOUBLER PER ER/A 382398-14, REV A. 2 L 7 2 4F RT A2NM 2002022000151 20020220 00151 NM 2002 2 20 DL757020105 1 20020125 A 5330 146N37806 SKIN BOEING 757 757232 1384965 NM FS 1630, S-25R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 FUSELAGE / SKIN / FS 1630 / STRG. 24R-26R : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS DENTED AND GOUGED AT FS 1630 BETWEEN STRINGERS 24R & 26R. THE DAMGE WAS REMOVED WITH A 7" X 2" CUTOUT AND A 5" X 2" CUTOUT. BOTH CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 382286-14, REV A. 2 L 7 2 4F RT A2NM 2002022000152 20020220 00152 NM 2002 2 20 DL733020121 1 20020201 A 5315 UNK WEB BOEING 737 737347 1384647 NM KEEL CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 THE KEEL BEAM LOWER SKIN PANEL WAS FOUND CRACKED IN SEVERAL PLACES_BETWEEN FS 661 AND FS 721. THE PANEL WAS REPLACED PER S/B 737-53-1104. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2002022000153 20020220 00153 NM 2002 2 20 DLM11020124 1 20020201 A 3230 ARK7550565 PIPE DOUG MD11 MD11 3023602 NM RIGHT GEAR UNSERVICEABLE A DALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 27 802DE 48473 AFTER TAKEOFF GEAR HANDLE WOULD NOT COME UP PUSHED HANDLE RELEASE BUTTON STILL WOULD NOT COME UP. FOUND RT MLG TRIM CYL HYD PIPE CRACKED AND HYD FUSE SET. REMOVED PIPE INSTALLED NEW LINE AND SAFTYWIRED HYD FUSE LEAK CHK GOOD CYCLED GEAR OPS NORMAL GOOD INDICATIONS. 2 L 7 3 4F RT A22WE 2002022000154 20020220 00154 NM 2002 2 20 DL757020153 1 20020207 A 5743 113N10706 SUPPORT FITTING BOEING 757 757232 1384965 NM RH WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 WING / RH MLG FWD TRUNNION SUPPORT FITTING : LUG CORROSION REPAIR WHILE ACCOMPLISHING INSPECTIONS OF THE RH WING MLG FWD TRUNNION FITTING FUSE PINS AND LUGS PER AD 2000-07-13, CORROSION WAS FOUND ON THE SURFACE OF THE LUGS AND THE LUG BORES. THE LUG BORES WERE OVERSIZED AND THE FACES MACHINED TO REMOVE THE DAMAGE. OVERSIZE BUSHINGS WERE INSTALLED TO RESTORE THE AREA PER ER/A 382408-14AD. 2 L 7 2 4F RT A2NM 2002022000155 20020220 00155 NM 2002 2 20 DLM88020157 1 20020208 A 3230 92748681 RELAY DOUG MD88 MD88 3023688 NM STA 110 UNSERVICEABLE A DALA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 979DL 53266 ON GEAR EXTENSION HAD ALL 3 UNSAFE RED LIGHTS AND GEAR DOOR OPEN LIGHT.PERFORMED LANDING GEAR UNSAFE GEAR HANDLE DOWN CK LIST.HYDRAULIC QTY AND PRESS NORMAL.LANDED WITH EMERGENCY GEAR EXTENSION HANDLE PULLED, THREE GREEN LIGHTS AND GEAR DOOR OPEN LIGHT ON. CA-T/S PER MM.BITE CK PSEU OK.JACKED A/C.CYCLED GEAR SEVERAL TIMES.ALL INDICATIONS NORMAL. REPLACED RELAY R2-28 PRECAUTIONARY.ALL CKS NORMAL. 2 L 7 2 4F RT A6WE 2002022000156 20020220 00156 NM 2002 2 20 DL757020165 1 20020210 A 2560 D30656132 SLIDE BOEING 757 757232 1384965 NM L4 DOOR DEPLOYED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 657DL 24419 AT GATE IN SJC OPERATIONS BLEW L4 DOOR SLIDE DURING NORMAL A/C SERVICE ON GND. THE SLIDE OPERATED NORMAL DUE TO IT BEING ARMED WHEN OPERATIONS OPENED DOOR..THIS OCCURED ON THE ORIGINATING LEG OF FLT 1432 10FEB IN SJC.. C/A MTC. REPL SLIDE PACK AND DOOR ASSIST BOTTLE IN SJC.. 2 L 7 2 4F RT A2NM 2002022000157 20020220 00157 NM 2002 2 20 DL72S020169 1 20020211 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM 2L DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 525DA 21585 EMERGENCY EXIT SIGN ABOVE 2L DOOR INOP. REPLACED BATTERY 2 L 7 3 4F A3WE 2002022000159 20020220 00159 NM 2002 2 20 DL757020183 1 20020212 A 5330 143N34713 SKIN BOEING 757 757232 1384965 NM FS 460, S-27R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 FUSELAGE / SKIN / FS 460 / STRG. 27R : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND GOUGED AT FS 460 BETWEEN STRINGERS 26R & 27R. THE GOUGE WAS REMOVED WITH A 3.4" X 2.9" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 382428-14, REV A. 2 L 7 2 4F RT A2NM 2002022000160 20020220 00160 NM 2002 2 20 DL757020184 1 20020212 A 5330 143N34713 SKIN BOEING 757 757232 1384965 NM FS 505, S-27L GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 FUSELAGE / SKIN / FS 499-515 / STRG. 26L-28L : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH SEVERAL GOUGES BETWEEN FS 499 & 515 AND BETWEEN STRINGERS 26L & 28L. THE GOUGES WERE REMOVED WITH A SINGLE 16.1" X 4.4" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 382448-14, REV A. 2 L 7 2 4F RT A2NM 2002022000161 20020220 00161 NM 2002 2 20 DL757020185 1 20020212 A 5330 141N34112 SKIN BOEING 757 757232 1384965 NM FS 310, S-5R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 FUSELAGE / SKIN / FS 310 / STRG. 4R-5R : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND GOUGED AT FS 310 BETWEEN STRINGERS 4R & 5R. THE GOUGE WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 382362-14, REV A. 2 L 7 2 4F RT A2NM 2002022000162 20020220 00162 NM 2002 2 20 DL757020186 1 20020212 A 5330 143N36504 SKIN BOEING 757 757232 1384965 NM FS 710, S-19R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 FUSELAGE / SKIN / FS 706 & 725 / STRG. 19R : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH A GOUGE IN THE UPPER SKIN AT STRINGER 19R AT FS 706 AND ANOTHER AT FS 725. THE GOUGES WERE REMOVED WITH 2 LOCAL CUTOUS TO THE UPPER SKIN AT THE LAP JOINT. THE CUTOUTS WERE REPAIRED WITH SEPERATE EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 382422-14, REV A. 2 L 7 2 4F RT A2NM 2002022000163 20020220 00163 NM 2002 2 20 DL72W020206 1 20020219 A 5300 6518636377 ANGLE BOEING 727 727247 138408F NM L/H WHEEL WELL CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 FOUND ON E-2 LETTER CK 1.25 INCH CRACK THRU ONE FASTENER HOLE TO FASTENER HOLE, AFT FLANGE OF VERTICAL ANGLE STA 870 TO KEEL BEEM. REPAIRED PER SRM 53-10-9D FIG 806D TIME LIMITED REPAIR 2 L 7 3 4F A3WE 2002022000164 20020220 00164 NM 2002 2 20 DL72W020207 1 20020219 A 5500 STRINGER BOEING 727 727247 138408F NM VERT STAB R/H CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 VERT. STAB R/H SIDE STRINGER CRACKED SIXTH FROM BOTTOM 3RD BAY DOWN REPAIR PER MM 55-30-000-8 2 L 7 3 4F A3WE 2002022000167 20020220 00167 NM 2002 2 20 AWXA200200159 1 20020207 A 5240 507945265 SKIN BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - MAJOR REPAIR - "C" - DURING C-10 CHECK A 1/4 CRACK WAS FOUND ON EXTERNAL SKIN OF R1 DOOR AT THE UPPER CORNER OF TH E LOWER HINGE CUTOUT 307.25. MAINTENANCE CUTOUT THE DAMAGED AREA OF SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY THE C RACK WAS CONTAINED. FABRICATED A REPAIR DOUBLER AND HINGE COVER AND INSTALLED REPAIRS IAW AWA EO 52-00-02, REV C. 2 L 7 2 4F RT A16WE 2002022000168 20020220 00168 NM 2002 2 20 AWXA200200160 1 20020213 A 5315 6546811 TEE CHORD BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - "C" - DURING C-13 CHECK CORROSION WAS FOUND ON FLOOR BEAM UPPER FLANGE BS 986, RBL 23 TO RBL 33. MA INTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; CUTOUT DAMAGED SECTION OF UPPER TEE CHORD AT BS 986, RBL 23 TO RBL 33; FABRICATED NEW SECTION OF UPPER TEE CHORD AND INSTALLED REPAIR IAW B737-300 SRM 53-00-51, PG 207-211. 2 L 7 2 4F RT A16WE 2002022100001 20020221 00001 SO 2002 2 21 C2XA02TY038 1 20020221 A 5315 14522460009 BEAM EMB 135 EMB135LR 3260305 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS, During a scheduled 1C inspection, corrosion was found on the forward center omega beam galley area. Maintenance rem oved corrosion and replaced affected rivits, alodined and primed. I/A/W-EMB-135/145-CPM-51-21-05 & 06. Repair procedure was satisfactory and aircraft will be released upon complection of inspection. 2 L 7 2 4F RT TOOO11AT 2002022100002 20020221 00002 SO 2002 2 21 C2XA02TY040 1 20020221 A 5320 14524131006 ANGLE EMB 135 EMB135LR 3260305 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS, During a scheduled 1C inspection, corrosion was found on the support angle at main door entrance below the threshol d strip. Maintenance removed and replaced the support angle. I/A/W-EMB-135/145-SRM-51-40-02. Repair procedure was satisf actory and aircraft will be released upon complection of inspection. 2 L 7 2 4F RT TOOO11AT 2002030700020 20020307 00020 NM 2002 3 7 02FDEA00133 1 20020216 A 5711 ARC74131 SPAR DOUG MD11 MD11F 3023600 NM LT WING BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 LT WING UPPER FIXED T/E PANEL BULGED AT BS XOR 674 (CTR OF NR 4 SPOILER). REMOVED AND REPLACED OUTER WING REAR SPAR/TRA ILING EDGE PER EA 1-5720-60680. 2 L 7 3 4F RT A22WE 2002022100003 20020221 00003 SO 2002 2 21 C2XA02TY041 1 20020221 A 5320 14522459003 SUPPORT EMB 135 EMB135LR 3260305 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS, During a scheduled 1C inspection, corrosion was found on the center omega beam ramp support between FR19-20. Mainte nance removed and replaced the ramp support. I/A/W-EMB-135/145-SRM-51-40-02. Repair procedure was satisfactory and aircr aft will be released upon complection of inspection. 2 L 7 2 4F RT TOOO11AT 2002022100004 20020221 00004 SO 2002 2 21 C2XA02TY042 1 20020221 A 5315 14521700007 BEAM EMB 135 EMB135LR 3260305 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS, During a scheduled 1C inspection, corrosion was found on the left omega beam ar FR20 under the carbon fiber beam. M aintenance cut out the damage, fabricated an external angle, plate and filler I/A/W-EMB-135/145-SRM-53-21-10 and reinsta lled the left ramp angle and "L" profile. I/A/W-EMB-135/145-SRM-51-40-02 and 53-21-10. Repair procedure was satisfactory and aircraft will be released upon complection of inspection. 2 L 7 2 4F RT TOOO11AT 2002022100005 20020221 00005 SO 2002 2 21 C2XA02TY043 1 20020221 A 5320 14521721005 PLATE EMB 135 EMB135LR 3260305 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS, During a scheduled 1C inspection, corrosion was found on the forward digital plate aft of cockpit door. Maintenance removed the corrosion by cutting out the center section and installed a new section, fabricated and installed doubler a nd shims. I/A/W-EMB-135/145-SRM-51-40-02 and CMP-51-21-04,05,06 and EC5320-01059. Repair procedure was satisfactory and aircraft will be released upon complection of inspection. 2 L 7 2 4F RT TOOO11AT 2002022100006 20020221 00006 WP 2002 2 21 2002F00106 1 20020129 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 812US 48092 IND - THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 1 THROUGH 3 AND ROWS 27 THROUGH 30, THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, AND THE TAILCONE EMERGENCY LIGHTS REMOTE RECEIVER WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT B ATTERIES FOR THE CEILING AND LOW LEVEL LIGHTS. REPLACED THE BATTERIES FOR THE TAILCONE REMOTE RECEIVER AND TWO OF THE C ONTROL TRANSMITTERS. REPLACED THE LOW LEVEL LIGHT ASSY AT SEAT ROW 11. (M) 2 L 7 2 4F A6WE 2002022100007 20020221 00007 WP 2002 2 21 2002F00107 1 20020129 A 3350 86210151 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 812US 48092 IND - THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 1 THROUGH 3 AND ROWS 27 THROUGH 30, THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, AND THE TAILCONE EMERGENCY LIGHTS REMOTE RECEIVER WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT B ATTERIES FOR THE CEILING AND LOW LEVEL LIGHTS. REPLACED THE BATTERIES FOR THE TAILCONE REMOTE RECEIVER AND TWO OF THE C ONTROL TRANSMITTERS. REPLACED THE LOW LEVEL LIGHT ASSEMBLY AT SEAT ROW 11. REF USAAD02003. 2 L 7 2 4F A6WE 2002022100008 20020221 00008 WP 2002 2 21 2002F00108 1 20020129 A 3350 9731045 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 812US 48092 IND - THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 1 THROUGH 3 AND ROWS 27 THROUGH 30, THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, AND THE TAILCONE EMERGENCY LIGHTS REMOTE RECEIVER WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT B ATTERIES FOR THE CEILING AND LOW LEVEL LIGHTS. REPLACED THE BATTERIES FOR THE TAILCONE REMOTE RECEIVER AND TWO OF THE C ONTROL TRANSMITTERS. REPLACED THE LOW LEVEL LIGHT ASSEMBLY AT SEAT ROW 11. REF USAAD02003. 2 L 7 2 4F A6WE 2002022100023 20020221 00023 NM 2002 2 21 USAABB02002 1 20020108 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN MALFUNCTIONED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625VJ 27246 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 ILLUMINATED. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002022100024 20020221 00024 NM 2002 2 21 USAABB02003 1 20020109 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 LAX - FOUND FLOOR EMERGENCY LIGHTS, LEFT SIDE FORWARD, INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTER IES. (M) 2 L 7 2 4F RT A1NM 2002022100025 20020221 00025 SO 2002 2 21 C2XA02CL056 1 20020220 A 3350 WIRE EMB 135 EMB135LR 3260305 SO CABIN BROKEN A C2XA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 27 14514 145303 CLE FLIGHT#3133 THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT ROW 9 WAS INOPERATIVE.MAINTENANCE INSPECTED AND REPAIRED A WIRE ON THE EMERGENCY AISLE PATH LIGHTING STRIP.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2002022100026 20020221 00026 NM 2002 2 21 USAABB02004 1 20020110 A 3350 CONNECTOR BOEING 767 7672B7 1385107 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 PHL - FOUND THE EMERGENCY EXIT LIGHTS INOPERATIVE IN THE FORWARD CABIN, LEFT SIDE. MAINTENANCE FOUND THE BATTERY PACK C ONNECTOR DETACHED AND SECURED IT. (M) 2 L 7 2 4F RT A1NM 2002022100028 20020221 00028 NM 2002 2 21 CALA0200083 1 20020220 A 5320 ANGLE BOEING 737 737524 1384721 NM STA 294-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19636 26340 INSPECTION FOUND Z-ANGLE IN L-I DOOR AREA CORRODED AT STA 294-360. THE Z-ANGLE WAS REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002022100031 20020221 00031 WP 2002 2 21 USAAD02003 1 20020129 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 91 812US 48092 IND - THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 1 THROUGH 3 AND ROWS 27 THROUGH 30, THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, AND THE TAILCONE EMERGENCY LIGHTS REMOTE RECEIVER WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT B ATTERIES FOR THE CEILING AND LOW LEVEL LIGHTS. REPLACED THE BATTERIES FOR THE TAILCONE REMOTE RECEIVER AND TWO OF THE C ONTROL TRANSMITTERS. REPLACED THE LOW LEVEL LIGHT ASSEMBLY AT SEAT ROW 11. (M) 2 L 7 2 4F A6WE 2002022100033 20020221 00033 EU 2002 2 21 USAAF02001 1 20020118 A 3350 6040681 BATTERY FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 889US 11358 GSO - THE FLOOR TRACK EMERGENCY LIGHTS BETWEEN SEAT ROWS 8 TO 12 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY L IGHT BATTERY SUPPLY. (M) 2 L 7 2 4F RT 2002022100034 20020221 00034 EU 2002 2 21 USAASA02003 1 20020107 A 3260 SENSOR AIRBUS 320 A320214 3930316 EU NLG DIRTY A USAA A UNSCHED LANDING N S FALSE WARNING AFFECT SYSTEMS CL CLIMB 1 EA 19 107US 1052 BDL - FLT 63 - EN ROUTE BDL-PHL - AS THE FLIGHT TOOK, RECEIVED THE ECAM WARNING 'SHOCK ABSORBER FAULT'. AS A RESULT, TH E LANDING GEAR WOULD NOT RETRACT. THE FLIGHT RETURNED TO BDL AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED THE NLG EXTEND SENSORS 24GA AND 25GA. THE SYSTEM WAS INSPECTED AND OPERATIONALLY CHECKED. NO FAULTS WERE FOUND. (M) 2 L 7 2 4F RT A28NM 2002022100035 20020221 00035 EU 2002 2 21 USAASA02004 1 20020107 A 3220 LANDING GEAR AIRBUS 320 A320214 3930316 EU NLG DEFECTIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 107US 1052 BDL - FLT 9201 - EN ROUTE BDL-PHL, RECEIVED AN ECAM WARNING FOR SHOCK ABSORBER FAULT. AS A RESULT, THE LANDING GEAR HAN DLE WOULD NOT GO INTO THE UP POSITION AND THE LANDING GEAR WOULD NOT RETRACT. THE FLIGHT RETURNED TO BDL AND LANDED WIT HOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR ASSEMBLY. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002022100036 20020221 00036 EU 2002 2 21 USAASA02005 1 20020108 A 2121 EVT3454H BLOWER AIRBUS A319 A319112 3930323 EU E/E BAY MALFUNCTIONED A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 748UW 1311 PHL - FLT 2249 - EN ROUTE PHL-PVD - DURING CLIMB-OUT, A STRONG, PUNGENT ODOR BECAME PRESENT IN BOTH THE COCKPIT AND CABI N, ACCOMPANIED BY A STRONG VIBRATION. THE VIBRATION STOPPED WHEN THE ECAM WARNING, 'BLOWER FAULT' ANNUNCIATED. THE FLI GHT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE EQUIPMENT BLOWER FAN. SYSTEM TESTS OK. ( M) 2 L 7 2 4F RT A28NM 2002022100037 20020221 00037 NM 2002 2 21 02FDEA00136 1 20020220 A 2750 SWITCH BOEING 727 727233 138408A NM FAULTY A FDEA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SO 25 274FE 22039 02-51 ON RETRACT OF FLAPS AMBER LED LIGHT ON. R&R #1 L/E FLAPS POSITION SWITCH PER IAW MM 27-82-001-4. OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2002022100038 20020221 00038 EU 2002 2 21 USAASA02006 1 20020111 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 700UW 7457 0885 TPA - THE EMERGENCY LIGHT TEST FAILED ON THE PROGRAMMING AND TEST PANEL. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT. (M) 2 L 7 2 4F RT A28NM 2002022100039 20020221 00039 EU 2002 2 21 USAASA02011 1 20020117 A 2120 ODOR AIRBUS A319 A319112 3930323 EU CABIN DETECTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 752US 1319 BOS - FLT 6402 - EN ROUTE DCA-BOS - DURING APPROACH TO BOS, NOTICED ELECTRICAL LIKE FUMES COMING FROM BOTH FORWARD AND R EAR GALLEY AREAS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE OPERATED ALL ELECTRICAL SYSTEM. ALSO, VISUALLY CHECKED RELAYS AND ELECTRICAL CONNECTIONS IN OVERHEAD GALLEY AREAS. NO FAULTS WERE FOUND. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2002022100040 20020221 00040 NM 2002 2 21 USAASB02007 1 20020111 A 2131 7638102 CONTROLLER BOEING 737 737301 1384611 NM CABIN PRESSURE MALFUNCTIONED A USAA B EMER. DESCENT O OTHER CR CRUISE 1 EA 19 340US 23237 ROC - FLT 202 - EN ROUTE FROM CLT TO ROC, THE AIRCRAFT EXPERIENCED A GRADUAL DEPRESSURIZATION AT FL370 AS CABIN ALTITUDE ROSE TO 10,500 FEET. QUICK REFERENCE HANDBOOK PROCEDURES WERE ACCOMPLISHED AND AFTER LEVELING OFF AT FL150, WITH CABIN UNDER CONTROL, PRESSURIZATION WAS SWITCHED TO STANDBY MODE AND OPERATED NORMALLY. FLIGHT CONTINUED ONTO CLT AND LANDED WITHOUT FURTHER INCIDENT. FLIGHT ATTENDANT REPORTED A POP SOUND IN THE VICINITY OF GALLEY DOOR AT LOWER ALTITUDE DURIN G APPROACH. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER (P/N 763810-2) A ND THE CABIN PRESSURE SELECTOR PANEL. OPERATIONAL TEST GOOD PER MM 21-31-00. (M) 2 L 7 2 4F RT A16WE 2002022100041 20020221 00041 WP 2002 2 21 ZW0A0202101 1 20020219 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 926TW 49356 DURING ROUTINE MAINTENANCE (LS), PARTIAL EGRESS LIGHT FAILURE BETWEEN ROWS 14-19. REMOVED AND REPLACED BATTERY PACK PER MM 33-59-00. OPERATIONAL CHECK PERFORMED NORMAL. CHECK-C 10/19/01 MCI. --CLOSED-- 2 L 7 2 4F A6WE 2002022100042 20020221 00042 NM 2002 2 21 USAASB02008 1 20020113 A 2130 7110025 CONTROL PANEL BOEING 737 7373B7 1384580 NM COCKPIT FAULTY A USAA B EMER. DESCENT O OTHER CR CRUISE 1 EA 19 390US 23312 DTW - FLT 765 - EN ROUTE TO DTW, CLIMBING TO FL350, CABIN ALTITUDE BEGAN CLIMBING APPROX 2,000 FPM. SWITCHED BOTH PACKS TO HIGH FLOW AND CABIN RETURNED TO NORMAL. SHORTLY THEREAFTER, CABIN BEGAN CLIMBING APPROX 700 FPM. WHEN CABIN ALTITUDE REACHED 8,000 FT, CREW SWITCHED TO STANDBY MODE AND REGAINED CABIN CONTROL. DESCENDED TO FL240 AND CABIN DESCENDED NORMA LLY. CABIN BEGAN SPIKING UP 1,000-2,000 FPM. DESCENDED TO FL180 AND CONTROLLED CABIN IN STANDBY MODE. FLT CONTINUED TO D TW WHERE THE FLT LANDED WITHOUT INCIDENT. DUCT PRESSURE WAS NORMAL AND CABIN PRESSURE HELD AT LOWER ALTITUDES, 16,000 FT AND BELOW. R&R CABIN PRESSURE SELECTOR PANEL (P/N 711002-5) AND CABIN PRESSURE CONTROLLER. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002022100043 20020221 00043 NM 2002 2 21 USAASB02013 1 20020117 A 5610 WINDSHIELD BOEING 737 7373B7 1384580 NM COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 383US 22956 CLT - FLT 1159 - EN ROUTE FROM ATL TO PHL, AT FL370, THE FIRST OFFICERS FORWARD WINDSHIELD CRACKED. CREW DESCENDED TO F L250 AND CONTACTED DISPATCH. ICING CONDITIONS IN PHL PROHIBITED FLIGHT TO CONTINUE TO DESTINATION. FLIGHT DIVERTED TO CLT FOR REPAIRS. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002022100057 20020221 00057 NM 2002 2 21 2002UALA00247 1 20020213 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 926UA 26648 FORWARD PIT BILGE FRAME AT STATION 440 RBL 23 HAS AREA .5 X .5 INCHES OF EXCESSIVE MATERIAL REMOVED ON WEB. MAJOR REPAI R ACCOMPLISH. REPAIR ANGLE INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002022100058 20020221 00058 NM 2002 2 21 2002UALA00248 1 20020209 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 AFT PRESSURE DOME RBL 20 BELOW WEB IS NICKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED RIVET AND PAINTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002031400156 20020314 00156 NE 2002 3 14 2002UALA00249 2 20020209 A 7230 1B0475 CARBON SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE WORN A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 593UA 11266 28144 726650 SMOKE FILLED AIRCRAFT IMMEDIATELY AFTER TAKEOFF. UPON DISASSEMBLY AT THE TURBINE SHOP, THE NR 2/3 CARBON SEAL WAS FOUND WORN. 2 L 7 2 4F 4 F RT A2NM E17NE 2002030100022 20020301 00022 EU 2002 3 1 2002UALA00250 1 20020209 A 2133 VFT300A1 OUTFLOW VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 409UA 462 RETURNED TO FIELD DUE TO CABIN PRESSURIZATION PROBLEM. UNABLE TO MAINTAIN CABIN PRESSURE IN AUTO OR MANUAL MODE. SKIN AIR OUTLET VALVE WAS DEACTIVATED AND SUBSEQUENTLY REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002031400157 20020314 00157 NE 2002 3 14 2002UALA00251 2 20020209 A 7230 1B0475 CARBON SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE WORN A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 593UA 11266 28144 726650 SMOKE FILLED AIRCRAFT IMMEDIATELY AFTER TAKEOFF. UPON DISASSEMBLY AT THE TURBINE SHOP, THE NR 3 BEARING AFT CARBON SEAL WAS FOUND WORN. 2 L 7 2 4F 4 F RT A2NM E17NE 2002022100059 20020221 00059 EU 2002 2 21 AWXA200200161 1 20020219 A 3350 9BG40450100 HOUSING AIRBUS 320 A320231 3930325 EU SEAT ROW 7 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 PHX - EEL - "C" - DURING INSPECTION EMERGENCY ESCAPE LIGHT WAS FOUND BROKEN AT SEAT ROW 7 L/H. MAINTENANCE REMOVED AND R EPLACED EMERGENCY ESCAPE LIGHT HOUSING AT SEAT ROW 7, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002022100060 20020221 00060 NM 2002 2 21 2002UALA00252 1 20020209 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 LEFT HAND EXTERNAL FUSELAGE HAS A 6 INCH VERTICAL DENT AT BODY STATION 760 BETWEEN STRINGER 15L TO 16L. MAJOR REPAIR AC COMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002022100061 20020221 00061 NM 2002 2 21 2002F00109 1 20020118 A 2163 1173T101 SENSOR BOEING 737 737230 1384401 NM A/C BAY MALFUNCTIONED A TSAA O OTHER O OTHER CL CLIMB 1 WP 13 818AL 22117 FLT 201 - HNL-LIH - AFTER TAKEOFF, NR 2 PACK TRIPPED. RESET AND TRIPPED AGAIN. RETURNED TO HNLG FOR UNEVENTFUL LANDING . REPLACED THE 365 TEMPERATURE SENSOR AND MODULATING VALVE. OPS CHECK, LEAK CHECK AND ENGINE RUN OK. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002022100062 20020221 00062 NM 2002 2 21 2002F00110 1 20020118 A 3610 39271611 VALVE BOEING 737 737230 1384401 NM A/C BAY MALFUNCTIONED A TSAA O OTHER O OTHER CL CLIMB 1 WP 13 818AL 22117 FLT 201 - HNL-LIH - AFTER TAKEOFF, NR 2 PACK TRIPPED. RESET AND TRIPPED AGAIN. RETURNED TO HNLG FOR UNEVENTFUL LANDING . REPLACED THE 365 TEMPERATURE SENSOR AND MODULATING VALVE. OPS CHECK, LEAK CHECK AND ENGINE RUN OK. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002022100063 20020221 00063 NM 2002 2 21 2002F00111 1 20020118 A 3610 39271611 VALVE BOEING 737 737230 1384401 NM A/C BAY MALFUNCTIONED A TSAA O OTHER O OTHER CL CLIMB 1 WP 13 818AL 22117 FLT 201 - HNL-LIH - AFTER TAKEOFF, NR 2 PACK TRIPPED. RESET AND TRIPPED AGAIN. RETURNED TO HNL FOR UNEVENTFUL LANDING. REPLACED THE 365 TEMPERATURE SENSOR AND MODULATING VALVE. OPS CHECK, LEAK CHECK AND ENGINE RUN OK. AIRCRAFT RETURNED TO SERVICE. REF TSAA0221021. (M) 2 L 7 2 4F RT A16WE 2002022100064 20020221 00064 NM 2002 2 21 TSAA0221021 1 20020118 A 2163 1173T101 SENSOR BOEING 737 737230 1384401 NM A/C BAY MALFUNCTIONED A TSAA O OTHER O OTHER CL CLIMB 1 WP 13 818AL 22117 FLT 201 - HNL-LIH - AFTER TAKEOFF, NR 2 PACK TRIPPED. RESET AND TRIPPED AGAIN. RETURNED TO HNL FOR UNEVENTFUL LANDING. REPLACED THE 365 TEMPERATURE SENSOR AND MODULATING VALVE. OPS CHECK, LEAK CHECK AND ENGINE RUN OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002022100068 20020221 00068 NM 2002 2 21 TSAA0253005 1 20020105 A 5330 65457701 SKIN BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 REPAIRED FUSELAGE SKIN CRACK AT BS 743 S-14L. TRIMMED OUT CRACK AND VERIFIED WITH HFEC, NO DEFECTS NOTED. FABRICATED, INSTALLED REPAIR DOUBLER IAW SRM 53-30-1 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002022100069 20020221 00069 NM 2002 2 21 TSAA0253006 1 20020101 A 5311 654657877 FRAME BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 24031 REMOVED CORROSION DAMAGE ON STRINGER 5R UPPER CHORD AT BS 1093. REMOVED FORWARD PORTION OF DAMAGED CHORD. FABRICATED R EPLACEMENT CHORD AND SPLICE ANGLES AND INSTALLED REPAIR PARTS PER FIGURE 1 IAW ECO 3259. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 2002022100070 20020221 00070 NM 2002 2 21 TSAA0253007 1 20020107 A 5330 65457901 SKIN BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 REPAIRED 1.25 INCH FUSELAGE SKIN CRACK AT BS 787 S-11L. TRIMMED OUT CRACK DAMAGE AND VERIFIED WITH HFEC, NO DEFECTS NOT ED. FABRICATED, INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-30-3 FIGURE 25. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002022100077 20020221 00077 NM 2002 2 21 S02232002 1 20020219 A 3200 LANDING GEAR BOEING 747 747209B NM PWA JT9 JT9D7A 52054 NE LH BODY L/G W SAJF O OTHER K FLUID LOSS CL CLIMB 1 WP 03 MHB209A 21843 B18255 1.HYD #1 QTY LOSS AFTER T/O, A/C LANDING WITH ALT FLAP AND GEAR EXTEND, #1 EDP DEPRESSURIZED WHEN HYD #1 QTY DROP PED. 2.GRD VISUAL CHECK, LH MAIN GEAR RETRACT ACTUATOR PISTON ROD BROKEN, AND WHEEL WELL VISUAL CHECK NO RELATED COMPONE NT DAMAGED.C/A:1.RPLD DEFECTIVE ACTUATOR. 2.ALL L/G UP LOCK RELEASE MECHANISM/ACTUATORS VISUAL CHECKED NORMAL PER AMM 32 -35-01. 3.HYD SYS CASE DRAIN FILTER AND DELTA PRESS IND VERIFIED FLUSH, HYD #1 QTY REPLENISHED. HYD SYS #1 CASE DRAIN FI LTER CK NML, #1 ENG EDP COND CK NML. 4.CYCLED BODY GEAR ACTUATOR 5 TIMES WITH AC PUMP AND #1 ENG R/U TEST SATISFACTORY. 5.PENDING FOR BOEING COMMENTS AND RECOMMENDATION. 2 L 7 4 4F 4 F RT A20WE E20EA 2002022200001 20020222 00001 SO 2002 2 22 C2XA02IA039 1 20020219 A 2100 8152403 ACM EMB 145 EMB145LR 3260212 SO AIR COND. BAY FROZEN A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14993 145289 IAH- DURING FLIGHT 3588 THE CREW NOTED THAT THE NUMBER 2 PACK ON IN FLIGHT PRODUCES BURNING SMELL AND SMOKE IN MAIN CAB IN. IAH- MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 AIR CYCLE MACHINE, PERFORMED A OPERATIONAL CHECK OF THE AIRCOND ITIONING SYSTEM, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002022200002 20020222 00002 SO 2002 2 22 C2XA02CL057 1 20020221 A 2761 3605401003 ACTUATOR EMB 145 EMB145LR 3260212 SO LEFT WING LEAKING A C2XA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 27 13908 1488 145465 CLE FLIGHT#3175 THE CREW REPORTED THE #2 HYDRAULIC SYSTEM LOW QUANITY WARNING ILLUMINATED DURING FLIGHT.THE AIRCRAFT LAN DED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE LEFT SPEED BRAKE ACTUATOR.OPERATIONAL CHECKS WERE GO OD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002022200003 20020222 00003 NM 2002 2 22 0200495528 1 20020216 A 2910 271N61192 LINE BOEING 757 757251 1384970 NM RT WHEEL WELL LEAKING A NWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 01 528US 23843 ON INITIAL CLIMB, CREW RECEIVED EICAS MESSAGE "L HYD QTY" AND "RSVR" LIGHT ON LEFT SYSTEM. QUANTITY WAS VERIFIED AS DECR EASING. LATER, "L HYD SYS PRESS" EICAS MESSAGE APPEARED AND CONFIRMED. CREW FOLLOWED ALL CHECKLISTS AND DECLARED AN EMER GENCY. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT GEAR ACTUATOR LINE LEAKING. REPL ACED THE LINE. LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 2002022200005 20020222 00005 NM 2002 2 22 SABA020008 1 20020119 A 3350 6104789 BATTERY DHAV DHC8 DHC8103 1386005 NM DISCHARGED A SABA O OTHER L NO TEST TX TAXI/GRND HDL 1 SO 33 801WP 086 Flight 5097 from CLT to PGV: During preflight, Aircrew found floor emergency lights out. Maintenance removed and replace d wiring harness for two foward lights and replaced emergency battery pack. System ops checked good. Aircraft returned t o service. 2 H 7 2 4T RT A13NM 2002030700039 20020307 00039 NM 2002 3 7 02FDEA00134 1 20020216 A 2782 BEARING DOUG MD11 MD11F 3023600 NM L/E SLAT OUT OF POSITION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 RT WING O/B SLAT DRIVE MECHANISM FWD BEARING MIGRATED. REMOVED AND REPLACED WING OUTBOARD SLAT DRIVE MECH PER EA 1-2780 -60721. 2 L 7 3 4F RT A22WE 2002022200006 20020222 00006 WP 2002 2 22 02FDEA00135 1 20020219 A 3020 ANTI-ICE VALVE DOUG DC10 DC1030 3023501 WP NR 1 COWLING FAULTY A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 305FE 47870 NR 1 ENGINE ANTI-ICE DISAGREE LIGHT ILLUM AFTER ANTI-ICE WAS ON. REMOVED AND REPLACED NOSE COWL A/I VALVE PER MM 30-20- 00. 2 L 7 3 4F A22WE 2002022200007 20020222 00007 WP 2002 2 22 02FDEA00137 1 20020220 A 5280 DOOR DOUG DC10 DC1030F 3023504 WP RT MLG CRACKED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 310FE 48299 ON GEAR RETRACT RT MLG IND UNSAFE ON BOTH PANELS. REMOVED AND REPLACED MAIN GEAR DOOR PER AMM 32-14-01-2. 2 L 7 3 4F RT A22WE 2002022200008 20020222 00008 NM 2002 2 22 2002UALA00253 1 20020208 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 STATION 1681 CABIN FLOORBEAM TOP CAP LOWER SURFACE CORRODED AT LBL 24 - LBL 32. MAJOR REPAIR ACCOMPLISHED. INSTALLED C AP STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002022200009 20020222 00009 NM 2002 2 22 2002UALA00258 1 20020211 A 5310 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 CABIN AFT SHEAR DECK UPPER SURFACE CORROSION WITH EXCESSIVE MATERIAL LOSS STATION 1680 TO 1682 LBL 10 TO LBL 41. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND TWO ANGLES INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002050200095 20020502 00095 NE 2002 5 2 2002UALA00259 2 20020131 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 8084 8084 26945 777027 ENG TORCHING ON START DURING GROUND MAINT TEST RUN. SEVERAL COMPOSITE PANELS LT WING T/E BOTTOM OF WING JUST AFT AND TO BOTH SIDES ON NR 1 ENG HAVE HEAT DAMAGE. FUEL METERING UNIT (FMU) WAS REPLACED, COULD NOT FIND FAULT WITH UNIT. FMU P ASSED AS-RECEIVED TEST. NOTHING UNUSUAL WAS FOUND, ALL PARTS AND ALL PACKINGS/RINGS WERE IN GOOD CONDITION WITH LITTLE OR NO WEAR. THE SEALING SURFACES OF THE FMU MPSOV AND ITS MATING SURFACE IN THE HOUSING HAD NO SIGNS OF DAMAGE OR EXCES SIVE WEAR. THE CAUSE OF TORCHING IS UNKNOWN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002022200010 20020222 00010 NM 2002 2 22 2002UALA00260 1 20020211 A 5512 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HORIZ STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 926UA 26648 LEFT HAND INBOARD SECTION OF HORIZONTAL STABILIZER LEADING EDGE 2 AREAS OF EXCESS MATERIAL LOSS MEASURED FROM INBOARD ED GE. 1ST DAMAGE 27 INCHES OUTBOARD. 2ND DAMAGE IS 32 INCHES OUTBOARD. MAJOR REPAIR ACCOMPLISHED. CUTOUT DAMAGE AND IN STALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002022200011 20020222 00011 NM 2002 2 22 2002UALA00261 1 20020211 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 926UA 26648 AFT CARGO PIT STATION 807 LBL 20 FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRAP DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002022200012 20020222 00012 NM 2002 2 22 2002UALA00262 1 20020211 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 EXTERNAL FUSELAGE SKIN HAS SHARP DENT - CREASE AT STATION 349 JUST ABOVE SKIN LAP STRINGER 19R. MAJOR REPAIR ACCOMPLISH ED. CUTOUT DAMAGE AND INSTALLED DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002022200013 20020222 00013 NM 2002 2 22 2002UALA00263 1 20020211 A 5320 CHANNEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 HAT CHANNEL AT STATION 324 RBL 344 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED HAT CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002022200014 20020222 00014 NM 2002 2 22 2002UALA00266 1 20020212 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 AFT CABIN STATION 1681 RBL 53 CORROSION BETWEEN FLOORBEAM CAP AND PRESSURE DECK. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLOORBEAM CAP SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002022200015 20020222 00015 NM 2002 2 22 2002UALA00267 1 20020212 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 CABIN FLOORBEAM AT STATION 324, RBL 41.60 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002022200016 20020222 00016 NM 2002 2 22 2002UALA00268 1 20020213 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 FUSELAGE BODY STATION 188 LEFT HAND FRAME OUTBOARD SIDE CHORD CRACKED AT WL 208. MAJOR REPAIR ACCOMPLISHED. DOUBLER RE PAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002022200017 20020222 00017 EA 2002 2 22 SWIA200210584 1 20020124 A 2751 860D10018 FCU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 438SW 607 607 7574 FLAPS FAIL CAUTION MESSAGE ILLUMINATED UPON SELECTING FLAPS TO 30 DEGREES. IAPS DEGRADED STATUS MESSAGE. REMOVE AND RE PLACE FECU. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2002022200018 20020222 00018 SO 2002 2 22 SWIA200210585 1 20020124 A 3150 COMPUTER EMB 120 EMB120RT 3260202 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 269UE 120194 AURAL TRIM INDICATION WITH TRIM IN THE GREEN ON THE TAKEOFF ROLL. RESET AURAL WARNING COMPUTER. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002022200019 20020222 00019 2002 2 22 SWIA200210586 4 20020124 A 3160 DISPLAY CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 427SW 7497 NR 1 PFD WENT BLANK INFLIGHT. COMPLIED WITH FAULT ISOLATION MANUAL. RESET ALL CB FOR DISPLAYS. NR 1 PFD OPERATIONAL. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2002022200020 20020222 00020 2002 2 22 SWIA200210587 4 20020127 A 3425 PIN EMB 120 EMB120ER 3260203 SO AHRS COMPUTER LOOSE A SWIA A UNSCHED LANDING I N FLT. ATTITUDE INST. FALSE WARNING CL CLIMB 1 NM 07 226SW 120296 DURING CLIMB, THE COMPUTER FLAGS FLICKERED INTERMITTENTLY (CAPT'S SIDE). DURING CRUISE THE CAPT'S ADI INDICATED 90 DEGR EES NOSE UP WITH BOTH FLAGS SHOWING AND THE AP DISCONNECTED FROM THE F/O'S SIDE. FOUND WIRE W001-0394024 LOCATED AT PLU G 0158 TO EXHIBIT INTERMITTENT CONTACT WITH AHRS COMPUTER. REMOVED AND REPLACED CONNECTOR PIN. SYSTEM OPS CHECKS GOOD IAW EMB MM CH 34-27. 2 L 7 2 4T RT A31SO 2002022200021 20020222 00021 SO 2002 2 22 SWIA200210588 1 20020125 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO CABIN PRESSURE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 187SW 120037 ON DEPARTURE, AIRCRAFT WOULD NOT PRESSURIZE AT ALL. MANUAL CONTROLLER WOULD NOT FUNCTION. RETURNED TO ELKO. REMOVED A ND REPLACED AUTO PRESSURIZATION CONTROLLER IAW EMB MM 21-30-01. AUTO PRESSURIZATION OPS CHECKS GOOD IAW EMB MM 21-30-00 . 2 L 7 2 4T RT A31SO 2002022200022 20020222 00022 SO 2002 2 22 SWIA200210590 1 20020126 A 2750 CONNECTOR EMB 120 EMB120ER 3260203 SO T/E FLAP CONTAMINATED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 214SW 120280 ON TAKEOFF, DURING FLAP RETRACTION, RECEIVED A FLAP DISAGREEMENT. FOLLOWED QRH AND FLAPS RETRACTED NORMALLY. COULD NOT DUPLICATE ON GROUND. INSPECTED FLAPS, TRACKS, ACTUATORS AND FOUND LEFT OUTBOARD FLAP CANNON PLUG WET. CLEANED AND RES ECURED. OPS CHECKS GOOD WITH NO DISCREPANCIES. 2 L 7 2 4T RT A31SO 2002022200023 20020222 00023 EA 2002 2 22 SWIA200210591 1 20020125 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 426SW 429 429 7468 SPOILERON FAULT STATUS MESSAGE. REMOVED AND REPLACED NR 1 SECU IAW 27-61-05. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002022200024 20020222 00024 EA 2002 2 22 SWIA200210593 1 20020125 A 3320 LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR INOPERATIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 587SW 7062 MAIN CABIN DOOR TOP BOARDING LIGHT INOP. REMOVED AND REPLACED DOOR BOARDING LIGHT. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002022200025 20020222 00025 2002 2 22 SWIA200210595 4 20020121 A 3417 8220372140 ADC CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 720SW 426 426 7297 AIR DATA COMPUTER ON FIRST OFFICER'S SIDE FAILED WHILE EN ROUTE. ONCE ON THE GROUND PROBLEM SEEMED TO CLEAR. SUSPECT M OISTURE IN THE PITOT STATIC SYSTEM. REMOVED AND REPLACED NR 2 ADC. OPS CHECKS GOOD IAW 34-13-00. 2 L 7 2 4F RT A21EA 2002022200026 20020222 00026 SO 2002 2 22 SWIA200210596 1 20020122 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO ENTRY DOOR LOOSE A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 186SW 120034 FORWARD DOOR WARNING LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. CYCLED DOOR AS PER MX CONTROL. DOOR LIGHT EX TINGUISHED. FORWARD DOOR WARNING LIGHT ON TAKEOFF ROLL. ABORTED TAKEOFF. INSPECTED FORWARD DOOR INDICATION SYSTEM. W ORKING NORMALLY, NO FAULTS NOTED. FOUND UPPER MICROSWITCH LOOSE. ADJUSTED SWITCH AND SECURED. OPS CHECK GOOD IAW MM 5 2-71-01. 2 L 7 2 4T RT A31SO 2002022200027 20020222 00027 SO 2002 2 22 SWIA200210598 1 20020128 A 3080 055201001 MONITOR EMB 120 EMB120ER 3260203 SO DEICE SYSTEM MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 199SW 120237 LEADING EDGE DEICE MIDDLE LEFT WING, INBOARD LEFT WING, INBOARD LEFT STAB AND INBOARD RIGHT STAB LIGHTS CAME ON IN FLIGH T. RETURNED TO SLC. REPLACED DEICE MONITOR. CYCLED WINGS AND ENGINE DEICERS 2 CYCLES ON EACH TIMER WITHOUT FAULT. P/ N ON 0552-01-001, S/N OFF 415. 2 L 7 2 4T RT A31SO 2002022200028 20020222 00028 NE 2002 2 22 SWIA200210599 2 20020117 A 7297 WIRE HARNESS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 224SW 120295 CLIMBING OUT OF GJT THROUGH 16,000 EXPERIENCED A TORQUE DROP FLUCTUATION ON LEFT ENGINE TO 30 PERCENT. EXPERIENCED CONT INUED TORQUE FLUCTUATIONS IN CLIMB THROUGH 19,000. RESET LEFT ENGINE EEC WITH NO CHANGE. RETURNED FOR PRECAUTIONARY LA NDING WITH CONTINUED TORQUE DROPS ON LEFT ENGINE. REPLACED LEFT ENGINE WIRING HARNESS. PERFORMED EXTENSIVE ENGINE RUNS IAW MM 71-00-00. OPS CHECK GOOD. NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2002022200029 20020222 00029 NE 2002 2 22 SWIA200210600 2 20020124 A 7297 WIRE HARNESS EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE LT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 196CA 120196 LEFT EEC FAILED ON TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE UPPER WIRE HARNESS IAW POWER PLANT BUILD UP MANUAL 71-00-00. OPS CHECKED IAW MM 71-00-00. ALL PARAMETERS GOOD. P/N ON 31159-11-01, S/N OFF AA9663. 2 L 7 2 4T 4 T RT A31SO E20NE 2002022200030 20020222 00030 SO 2002 2 22 SWIA200210601 1 20020126 A 3350 SIGN EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 567SW 120342 ROW 5 RIGHT SIDE EXIT SIGN NOT ILLUMINATED. REMOVED AND REPLACED ROW 5 RIGHT SIDE EXIT SIGN FIXTURE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002022200031 20020222 00031 2002 2 22 SWIA200210602 4 20020128 A 3445 COMPUTER EMB 120 EMB120ER 3260203 SO E/E BAY MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 566SW 120343 CAPTAIN'S SIDE RMI FLAG, FIRST OFFICER'S FD FLAG, NR 2 AHARS 26 VAC CB POPPED. REPLACED TCAS PROCESSOR WITH SERVICEABLE UNIT. ALSO REPLACED NR 1 INVERTER WITH SERVICEABLE UNIT. ALL CIRCUIT BREAKERS REMAINED SET THROUGH ALL SYSTEM OPERATI ONAL CHECKS. 2 L 7 2 4T RT A31SO 2002030400167 20020304 00167 NM 2002 3 4 F3LA200200042 1 20020219 A 3230 1030875 SOLENOID BOEING 737 737228 13844AG NM LANDING GEAR FAILED A F3LA O OTHER O OTHER CL CLIMB 1 NM 03 234TR 2884 23004 UPON TAKEOFF IN SLC, HAD TO PULL LANDING GEAR LEVER TRIGGER TO GET GEAR HANDLE UP. IN DEN, MADE LOW PASS BY DENVER TOWE R TO CONFIRM GEAR DOWN. NO GEAR INDICATION LIGHTS. RECYCLED HANDLE, ALL INDICATIONS NORMAL AND LANDED WITHOUT INCIDENT . REPLACED LANDING GEAR LEVER LOCK SOLENOID PER MM 32-31-31 AND REPLACED LANDING LIGHTS CIRCUIT BREAKER PER WDM 24-56-0 1. PERFORMED LANDING GEAR SWING PER MM 32-32-0, TELEFLEX CABLE RIG CHECK PER MM 27-26-51, AND MANUAL EXTENSION TEST PER MM 32-38-0. 2 L 7 2 4F RT A16WE 2002022200032 20020222 00032 SO 2002 2 22 SWIA200210604 1 20020129 A 3260 TARGET EMB 120 EMB120ER 3260203 SO RT MLG OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 214SW 120280 RIGHT GEAR LIGHTS RED A & B WOULD NOT EXTINGUISH WHEN GEAR RETRACTED. CYCLED 3 TIMES. INSPECTED RT MAIN GEAR. FOUND U PLOCK HOOK ADJUSTED OUT, PLUS ICE BUILD UP ON HOOK. ADJUSTED UPLOCK PROX TARGET. C/W GEAR SWING. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002022200033 20020222 00033 SO 2002 2 22 SWIA200210605 1 20020123 A 2131 22201T011400 CONTROLLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN PRESSURE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 584SW 5085 5085 120352 ON CLIMB THROUGH 16,000 FEET, ALT WARNING LIGHT CAME ON. QRH ACCOMPLISHED. MANUAL MODE WOULD NOT HOLD ALT LOW OR AUTO MODE. REMOVED AND REPLACED PRESSURIZATION AUTO CONTROLLER. OPS CHECKS GOOD. S/N ON 478, S/N OFF 437. 2 L 7 2 4T 4 T RT A31SO E20NE 2002022200034 20020222 00034 SO 2002 2 22 SWIA200210606 1 20020128 A 7714 SEDL0C29M INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 292SW 120319 DURING CLIMBOUT, NOTICED NH GAUGE FLUCTUATING RAPIDLY +/- 10 PERCENT. REDUCED POWER AND SELECTED NR 1 EEC TO MANUAL. N H GAUGE STILL FLUCTUATED. ALL OTHER ENGINE PARAMETERS NORMAL. INSTALLED NH SENSOR FOR TROUBLESHOOTING. DURING ENGINE RUNS NH/NL (LT) START FLUCTUATING AT GROUND IDLE. SWAPPED GAUGES. PROBLEM FOLLOWED. INSTALLED SERVICEABLE NH/NL GAUGE (LT). RAN ENGINES. OPS CHECK GOOD. P/N: SEDL-0C29M, S/N ON: 174A, S/N OFF: 180. 2 L 7 2 4T RT A31SO 2002022200035 20020222 00035 EA 2002 2 22 SWIA200210607 1 20020127 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN CONTAMINATED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 403SW 7028 FWD EMERGENCY TRACK LIGHTING ON FLOOR IS INOP. FOUND MOISTURE IN FLOOR TRACK LIGHTING STRIP PINS. REMOVED MOISTURE. O PS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002022200036 20020222 00036 SO 2002 2 22 SWIA200210608 1 20020128 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN SHORTED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 296SW 120325 FORWARD OF ROW 3, MOST OF THE EMERGENCY LIGHTS ARE INOP OR VERY DIM. FOUND FORWARD SECTION OF LIGHTS DIM AT PIN-H OF FO RWARD BATTERY ISOLATED TO WIRE W220-0316-24 AND REMOVED SHORT TO GROUND. ALSO FOUND COURTESY LIGHT AND OVERHEAD EMERGEN CY LIGHT POSITION SWITCHED. RESTORED TO ORIGINAL CONFIGURATION. GROUND CHECK NORMAL. 2 L 7 2 4T RT A31SO 2002022200037 20020222 00037 EA 2002 2 22 COMA0260111 1 20020219 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 926CA 7027 FLIGHT 5354 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT. 2 L 7 2 4F RT A21EA 2002022200038 20020222 00038 EA 2002 2 22 COMA0260112 1 20020219 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 984CA 7171 FLIGHT 5712 FLAPS FAILED DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002022200039 20020222 00039 EA 2002 2 22 COMA0260113 1 20020219 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 975CA 7150 FLIGHT 5032 NLG DID NOT EXTEND, GEAR DISAGREE WARNING. USED MANUAL EXTENSION SYSTEM.COULD NOT DUPLICATE - INSPECTED NLG AND FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 2002022200040 20020222 00040 EA 2002 2 22 SWIA200210609 1 20020130 A 3234 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 905SW 3785 3785 7437 MAIN GEAR WARNING ON LANDING. FOLLOWED EMERGENCY PROCEDURE AND MAIN GEAR DID NOT EXTEND. MANUALLY EXTENDED GEAR ON THI RD ATTEMPT. REMOVED AND REPLACED MAIN GEAR SELECTORS VALVE. GEAR SWINGS SATISFACTORY. LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002022200041 20020222 00041 SO 2002 2 22 SWIA200210610 1 20020130 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO LT MLG DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 586SW 120354 LEFT MAIN GEAR WOULD NOT RETRACT AFTER T/O. CYCLED TWICE, STILL NO RETRACTION. RETURNED TO AIRPORT. CONTACTED SGU MC. CLEANED DOWN & UP PROX SENSORS ON LT MLG. CYCLED MLG 8 CYCLES. CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002022200042 20020222 00042 NE 2002 2 22 SWIA200210611 2 20020130 A 7230 BLADE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE DAMAGED A SWIA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 NM 07 405SW 7029 ON TAKEOFF ROLL, LARGE VIBRATION/NOISE FELT THROUGHOUT AIRCRAFT FELT ON RUDDER PEDALS AND THRUST LEVERS. FOUND DAMAGE T O LEFT ENGINE NR 8 & 9 FAN BLADES. REMOVED AND REPLACED NR 8, 9, 22 & 23 LEFT ENGINE FAN BLADES WITH SERVICEABLE UNITS. PERFORMED RUN CHECKS. OPS CHECKS GOOD. NO VIBRATION NOTED. BLADE NR 8 P/N ON 6018T30P06, S/N OFF KGAJ0009. BLADE N R 9 P/N ON 6018T30P06, S/N OFF KGAR9905. BLADE NR 22 P/N ON 6018T3P06, S/N OFF KGAJ0051. BLADE NR 23 P/N ON 6018T3P06, S/N OFF KGAJ0384. 2 L 7 2 4F 4 F RT A21EA E15NE 2002022200043 20020222 00043 EA 2002 2 22 SWIA200210612 1 20020130 A 2613 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 594SW 7285 ABORTED TAKEOFF DUE TO WING OVERHEAT MSG. ACCOMPLISHED HIGH POWER ENG RUN WITH CREW ASSISTANCE. COULD NOT DUPLICATE. SYSTEM OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002022200044 20020222 00044 EA 2002 2 22 SWIA200210613 1 20020131 A 5610 HP13332002 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 594SW 7285 RT WINDSHIELD IS CRACKED. REMOVED AND REPLACED RIGHT WINDSHIELD. 2 L 7 2 4F RT A21EA 2002030700018 20020307 00018 NM 2002 3 7 02FDEA00132 1 20020216 A 5711 ARC74131 SPAR DOUG MD11 MD11F 3023600 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 LT WING UPPER FIXED T/E PANEL BULGE AT BS XOR 772.5 (O/B OF NR 5 SPOILER). REMOVED AND REPLACED OUTER WING REAR SPAR/TR AILING EDGE PER EA 1-5720-60680. 2 L 7 3 4F RT A22WE 2002022200045 20020222 00045 NE 2002 2 22 SWIA200210614 3 20020127 A 6140 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 212SW 120276 ON TAKEOFF ROLL, TAKEOFF AURAL WARNING AUTO FEATHER SOUNDED. AUTO FEATHER SWITCH IS ON POSITION. INSPECTED RELAY K0161 RECEPTACLE AND PERFORMED EXTENSIVE RUNS. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 6 C P11NE 2002022200046 20020222 00046 SO 2002 2 22 SWIA200210615 1 20020201 A 3297 WIRE HARNESS EMB 120 EMB120ER 3260203 SO RT MLG DEFECTIVE A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 214SW 120280 RT MAIN LANDING GEAR -A- DISAGREEMENT LIGHT ILLUMINATED DURING FLIGHT. ALL -B- LIGHTS FUNCTION NORMAL. REMOVED AND REP LACED -A- UPLOCK HARNESS WITH SERVICEABLE HARNESS. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002022200047 20020222 00047 NE 2002 2 22 SWIA200210617 2 20020130 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 VIBRATES A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 595SW 7292 NR 1 ENGINE FAN VIB IN YELLOW ARC SHORTLY AFTER TAKEOFF. ON ENGINE RUN UP, COULDN'T DUPLICATE PROBLEM. AT HIGH POWER S ETTINGS, VIB NEVER GOT ABOVE .3. INSPECTED FAN BLADES VISUALLY AND INSPECTION GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002022200048 20020222 00048 2002 2 22 ZW0A0202201 4 20020221 A 3414 HG280D80 COMPUTER DOUG MD80 MD83 3023681 NM NUMBER 1 A ZW0A A UNSCHED LANDING O OTHER CL CLIMB 1 CE 13 9413T 53188 THE CAPTAIN'S IAS INDICATOR FROZE AT 180 KNOTS ON CLIMB OUT. CREW MADE AN UNSCHEDULED LANDING AT MCI. REPLACED THE CAP TAIN'S AIR SPEED INDICATOR, PN 4057800-906, AND THE NUMBER 1 CADC. CHECK-C 7-29-01 STL. --CLOSED-- 2 L 7 2 4F RT 2002022200050 20020222 00050 WP 2002 2 22 MWEA020135 1 20020220 A 5310 5911402505 SKIN DOUG DC9 DC981 3022081 WP STATION 127 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FORWARD ENTRY DOOR HOLD OPEN HOOK SKIN DENTED. -- REPAIRED FORWARD ENTRY DOOR HOLD OPEN HOOK CUTOUT WITH INSTALL OF EX TERNAL DOUBLER. 2 L 7 2 4F A6WE 2002031500146 20020315 00146 NM 2002 3 15 SABA020025 1 20020220 A 3350 6104789 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 AIRCRAFT 883 ON FLIGHT 5019 FROM CLT TO AGS. DURING PREFLIGHT FLOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE AT ROW 1 AN D ROW 4. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 2002022200052 20020222 00052 2002 2 22 SWAA020393 4 20020219 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 625SW 27701 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002022200053 20020222 00053 NM 2002 2 22 SWAA020394 1 20020219 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 404WN 27892 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002022200054 20020222 00054 NM 2002 2 22 SWAA020395 1 20020219 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM FWD CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002022200055 20020222 00055 NM 2002 2 22 SWAA020397 1 20020219 A 5312 6517582 WEB BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED .25 INCH LONG AT BS 183, WL 233 AND LBL 17.1. REMOVED AND REPLACED VERTICAL BEAM WEB WEB PER SRM. 2 L 7 2 4F RT A16WE 2002022200056 20020222 00056 NM 2002 2 22 SWAA020398 1 20020220 A 2751 6938849 BOLT BOEING 737 7373H4 1384600 NM LT INBD T/E FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING WALK AROUND INSPECTION, FOUND LT INBD T/E FLAP EXTENDED 4 INCHES. REMOVED AND REPLACED BOLT FOR T/E INBD AFT FLA P LOAD ROLLERS PER MM. 2 L 7 2 4F RT A16WE 2002022200057 20020222 00057 NM 2002 2 22 SABA020026 1 20020220 A 3350 1013079 BULB DHAV DHC8 DHC8102 2809003 NM CABIN BURNED OUT A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 882CC 168 Aircraft 882 on flight 5008 from CLT to OAJ. During preflight an overhead emergency light was found inoperative. Maint enance removed and replaced the bulb. Ops check was good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002022200058 20020222 00058 EU 2002 2 22 RAIA00202079 1 20020220 A 2731 82363 ACTUATOR AEROSP ATR72 ATR72202 8680940 EU INOPERATIVE A RAIA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CE 03 721TE 22733 283 217 5553-STL ELEVATOR TRIM FAILED. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE RIGHT HAND ELEVATOR TRIM ACTUATOR, OPS CK OK. 2 H 7 2 4T RT A53EU 2002022200089 20020222 00089 SO 2002 2 22 SWIA200210616 1 20020201 A 3010 BOOT EMB 120 EMB120ER 3260203 SO LT WING DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 226SW 120296 DURING CLIMB OUT OF PDX, INBOARD LEFT WING DEICE LIGHT ILLUMINATED REPEATEDLY ON BOTH TIMERS. FOUND TWO SMALL HOLES ON INBOARD PORTION OF LEFT WING INBOARD BOOT. APPLIED PATCH. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002022500001 20020225 00001 WP 2002 2 25 ABXA010731 1 20020208 A 5230 39140251 FITTING DOUG DC9 DC931 3022065 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 AFT LOWER CARGO DOOR, #4 INTERCOSTAL BEAM, AFT END FITTING CRACKED. REPLACED END FITTING IAW DC-9 SRM 51-30-5 AND 51-30- 1. 2 L 7 2 4F A6WE 2002022500002 20020225 00002 WP 2002 2 25 ABXA010733 1 20020208 A 5313 591140617 LONGERON DOUG DC9 DC931 3022065 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 LONGERON 4 LEFT AT F.S. 200 WAS CRACKED. REPLACED LONGERON IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2002022500003 20020225 00003 WP 2002 2 25 ABXA010734 1 20020210 A 5711 5911306509 SPAR DOUG DC9 DC931 3022065 WP LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 LEFT UPPER FORWARD SPAR WAS CRACKED AT THE INBOARD LEADING EDGE ATTACH HOLE. REPAIRED SPAR IAW DC-9 REA D957-43288MR. 2 L 7 2 4F A6WE 2002022500004 20020225 00004 WP 2002 2 25 0200471235 1 20020216 A 7830 THRUST REVERSER DOUG DC10 DC1030 3023501 WP NR 1 ENGINE MALFUNCTIONED A NWAA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 GL 01 235NW 46915 DURING CLIMB, THE NR 1 THRUST REVERSER INTRANSIT LIGHT ILLUMINATED FOLLOWED BY A SEVERE AIRCRAFT YAW. THE CREW FOLLOWED COM PROCEDURE AND SHUT DOWN THE NR 1 ENGINE. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO IAD LANDING WITHOUT INCIDENT . MAINTENANCE PLACED THE NR 1 THRUST REVERSER ON MEL 78-1A. AN EXCESSIVE MANEUVER/OVERLOAD CHECK WAS COMPLETED PER AMM 05-51-02 WITH NO DAMAGE NOTED. 2 L 7 3 4F A22WE 2002022500005 20020225 00005 NM 2002 2 25 020048528 1 20020216 A 2910 HYDRAULIC SYSTEM BOEING 757 757251 1384970 NM LEFT MALFUNCTIONED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 528US 23843 DURING TAKEOFF ROLL AT 95 KNOTS, CREW RECEIVED LEFT ENGINE HYDRAULIC CAUTION LIGHT. CREW SUCCESSFULLY ABORTED TAKEOFF A T 110 KNOTS. DURING TAXI, CREW AGAIN RECEIVED THE SAME ENGINE HYDRAULIC LIGHT. MAINTENANCE INSPECTED THE HYDRAULIC SYS TEM AND FILTERS AND NOTED NO CONTAMINATION. SERVICED HYDRAULIC SYSTEM AND REPLACED FILTERS. RAN ENGINE AND CYCLED FLIG HT CONTROLS WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2002022500006 20020225 00006 WP 2002 2 25 0200429865 1 20020212 A 5720 SPAR DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 During Mck in ATL, corrosion was found above the inboard and outboard stud holes in the right wing rear spar upper cap a t station 267. Both holes were spot faced. Repaired per EA 98-185519. 2 L 7 2 4F RT A6WE 2002022500007 20020225 00007 WP 2002 2 25 0200439944 1 20020127 A 5755 SPOILER DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1309T 47316 During RON at ORD, a 1/2" crack was found in the lower skin of the L/H inbrd flight spoiler at station 206 hinge drive f itting. The crack emenated from the edge of the skin cutout to an adjacent fastener. Repaired per EA 99-85357. 2 L 7 2 4F A6WE 2002022500008 20020225 00008 WP 2002 2 25 0200449960 1 20020131 A 5310 BULKHEAD DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 During RON in CMH, a crack was found on the Apb radial stiffener at l 6 rhs. The crack runs from the outbrd edge of the stiffener to the outer most fastener hole. Repaired per EA 99-185524. 2 L 7 2 4F A6WE 2002022500009 20020225 00009 WP 2002 2 25 0200459981 1 20020204 A 5530 STABILIZER DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 994Z 47097 During overnight in MSP, a crack was found on the verticle stabilizer front spar left lower chord.Repaired per EA 99-187 946 2 L 7 2 4F A6WE 2002022500010 20020225 00010 WP 2002 2 25 0200469903 1 20020213 A 5310 PRESSURE PANEL DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 953N 47083 during Mck in ATL, cracks were found int the flight compartment horizontal pressure panel at station 105. RH x=35 1"long , RH X=25 1"long. Repaired per EA 99-185564. 2 L 7 2 4F A6WE 2002022500011 20020225 00011 WP 2002 2 25 0200379878 1 20020123 A 5310 BRACKET DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 787NC 48149 During M-ck in Atl, while working in the area of sta 69, the right and left brackets were found cracked. Repaired per EA 98-185475. 2 L 7 2 4F RT A6WE 2002022500012 20020225 00012 WP 2002 2 25 0200389873 1 20020129 A 5510 FITTING DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 5510 782NC During shop visit in ATl, corrosion damage was found on the LH side of the the Horizontal Stabilizer fitting 59180098-50 7. Fitting was removed and replaced. Repaired per EA 98-185483. 2 L 7 2 4F RT A6WE 2002022500013 20020225 00013 WP 2002 2 25 0200399870 1 20020207 A 5312 DOOR FRAME DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 779NC 48101 During Mck at Atl, the right hand Sta. 753 two small cracks were noted in the upper forward corner of the aft overwing e xit doorjamb. Repaired per EA. 98-185539. 2 L 7 2 4F RT A6WE 2002022500014 20020225 00014 WP 2002 2 25 0200409865 1 20020208 A 5720 SPAR DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 During Mck in ATL, 2 cracks were in the upper spar cap at STA 267. The cracks extend around the upper stud holes for the # 3 flap hinge fitting. Repaired per EA 98-185533. 2 L 7 2 4F RT A6WE 2002022500015 20020225 00015 WP 2002 2 25 0200419870 1 20020208 A 5530 FRAME DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 779NC 48101 During Mck in ATL, a crack was found in the area of the Verticle Access Cover, the crack was on the LH side of former P/ n 9911986-11. Repaired per EA.98-185563. 2 L 7 2 4F RT A6WE 2002031500147 20020315 00147 NM 2002 3 15 SABA020027 1 20020223 A 3350 6104789 BATTERY DHAV DHC8 DHC8103 1386005 NM CABIN DISCHARGED A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 801WP 086 AIRCRAFT 801 ON FLIGHT 8687 FROM GSP TO CLT. DURING PREFLIGHT FOUR FLOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. NO E MERGENCY PROCEDURES USED. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. SYSTEM OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002022500017 20020225 00017 NM 2002 2 25 2002UALA00269 1 20020213 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 326UA 23958 RIGHT HAND FORWARD FUSELAGE AT BODY STATION 328 - 344 AT STRINGER 19R - STRINGER 20R, PREVIOUS REPAIR INSTALLED WITH BLI ND FASTENERS. MAJOR REPAIR ACCOMPLISHED. REMOVED TEMPORARY REPAIR. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002022500018 20020225 00018 NM 2002 2 25 2002UALA00270 1 20020213 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 326UA 23958 RIGHT HAND LOWER FUSELAGE AT BODY STATION 460 - BODY STATION 480 BETWEEN STRINGER 26R - 27R, SKIN IN CREASED, BULGING AN D DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002022500019 20020225 00019 NM 2002 2 25 2002UALA00271 1 20020214 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 326UA 23958 OVERWING FRAME AT BODY STATION 616, LBL 65 ATTACH CHORD CRACKED OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED A ND INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002022500020 20020225 00020 NM 2002 2 25 2002UALA00272 1 20020213 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 326UA 23958 FORWARD PIT STATION 495 FLOOR WEB ANGLE HAS CRACK AT S-28R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW WE B ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002031500083 20020315 00083 NM 2002 3 15 2002UALA00273 1 20020213 A 2421 GENERATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE INOPERATIVE A UALA A UNSCHED LANDING H G ELECT. POWER LOSS-50 PC MULTIPLE FAILURE CR CRUISE 1 WP 29 579UA 26697 61932 DIVERTED DUE TO GENERATOR INOP AND APU FAILED TO START. NO EICAS STATUS MESSAGES FOR THE APU. NORMAL START ACCOMPLISHE D ON THE GROUND. 2 L 7 2 4F 4 F RT A2NM E17NE 2002022500021 20020225 00021 WP 2002 2 25 ABXA010721 1 20020215 A 3350 6012235 BATTERY DOUG DC8 DC863F 302198F WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 816AX 1096 46093 EMERGENCY EXIT LIGHTS INTERMITTENTLY INOPERATIVE WHEN POWER WAS REMOVED FROM AIRCRAFT. REPLACED EMERGENCY LIGHT BATTERY RACK ASSEMBLY. OPS CHECKED GOOD IAW DC-8 AMM 33-50-01-2-0001. 2 L 7 4 4F 4A25 2002022500022 20020225 00022 WP 2002 2 25 ABXA010722 1 20020125 A 5330 SR09501513 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 947AX 47004 CRACK INDICATION IN SKIN BETWEEN 2 FASTENERS, BETWEEN LONGERON 5 RIGHT AND LONGERON 6 RIGHT AT FS 996. INSTALLED PERMAN ENT REPAIR IAW DC-9 EA 53110005. 2 L 7 2 4F A6WE 2002022500023 20020225 00023 WP 2002 2 25 ABXA010723 1 20020130 A 5320 D0489835 WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 947AX 47004 CUSP WEB CRACKED BETWEEN FS 945 - 965, LONGERON 18 LEFT. REPAIRED AREA, DOUBLER INSTALLED ON CUSP WEB IAW DC-9 SRM 53-0 1. 2 L 7 2 4F A6WE 2002022500024 20020225 00024 WP 2002 2 25 ABXA010724 1 20020219 A 3230 LANDING GEAR DOUG DC8 DC863 302198A WP NLG OUT OF ADJUST A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 818AX 46075 NOSE LANDING GEAR FAILED UPLATCH CHECK AFTER TAKEOFF. RECYCLED THE LANDING GEAR AND TRIED AGAIN, IT ALSO FAILED ON THE SECOND ATTEMPT. BOTH TIMES IT SOUNDED LIKE THE NOSE GEAR CAME COMPLETELY OUT OF THE WHEEL WELL. PERFORMED ADJUSTMENT A ND TEST OF THE NOSE LANDING GEAR IAW DC-8 AMM 32-20-00-5-0-001. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2002051500029 20020515 00029 WP 2002 5 15 ARWA20020205 1 20020214 A 5711 5615058505N SPAR DOUG DC8 DC861 3021952 WP LT WING CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK, LEFT WING STA XW 60 AUXILIARY SPAR LUG WITH CRACK, ADJACENT TO MLG TRUNNION FITTING. REMOVED AND REPLAC ED AUXILIARY SPAR IAW DRAWING 5616128. 2 L 7 4 4F 4A25 2002022500025 20020225 00025 2002 2 25 AT0200011 4 20020219 A 2565 D29982255 SLIDE BOEING 717 717200 1383700 NM R1 DOOR DEFECTIVE A ZZDA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 954AT 55016 R1 DOOR SLIDE GIRTH BAR WAS NOT SECURED AFTER FLIGHT AND SLIDE WAS DEPLOYED BY CLEANERS WHEN R1 DOOR OPENED. SLIDE WAS REPLACED 2ND TIME DUE TO FIRST SLIDE FACE PLATE ROTATED AND BAD FROM STOCK. REMOVED AND REPLACED SLIDE. 2 L 7 2 4F TR A6WE 2002022500026 20020225 00026 NM 2002 2 25 AWXA200200152 1 20020218 A 3150 WARNING SYSTEM BOEING 737 73733A 1384673 NM COCKPIT MALFUNCTIONED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 174AW 23633 PHX - ABORTED TAKEOFF -C- WHEN PREPARING TO TAKEOFF FROM PHX EN ROUTE TO LGB THE CONFIGURATION WARNING HORN SOUNDED. TA KEOFF WAS ABORTED AND AIRCRAFT TAXIED OFF RUNWAY. FLIGHT CREW RESET FLIGHT CONTROLS; AIRCRAFT TAXIED BACK ON RUNWAY AND TOOK OFF WITHOUT INCIDENT. 2 L 7 2 4F RT A16WE 2002032900145 20020329 00145 NM 2002 3 29 AWXA200200153 1 20020218 A 2424 939D6855 ARMATURE BOEING 737 7373G7 1384595 NM GCU INTERMITTENT A AWXA K NONE H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 WP 28 160AW RH1075 23782 AT 28,000 FL CRUISE JUST PRIOR TO TOP OF DESCENT THE AIRCRAFT LOST ELECTRICAL POWER WITH ALL GAUGES AND INSTRUMENTS FLAG GED, POWER RETURNED AFTER 3 SECONDS AND AIRCRAFT LANDED UNEVENTFULLY IN PHX. MX COULD NOT DUPLICATE THE PROBLEM, TROUBL ESHOT FOR OPEN PHASE CONDITION REF AMM 24-21-00, AND SL-24-118. REMOVED AND REPLACED NR 1 GENERATOR CONTROL UNIT, REMOV ED AND REPLACED R4 BUS TRANSFER RELAY NR 2 AND R3 TRANSFER RELAY NR 1 IAW WDM 24-24-01. ENGINE RUN OPERATIONAL TEST WAS GOOD. VENDOR BENCH TEST CONFIRMED FAILURE OF GENERATOR CONTROL UNIT S/N RH1075 WITH TEST FAILURE OF THE BR DROPOUT CIR CUITS, K901 RELAY ARMATURE WAS REPLACED TO REPAIR THE UNIT. UNIT ALSO WAS UPGRADED WITH KIT MODS. 2 L 7 2 4F RT A16WE 2002022500027 20020225 00027 NM 2002 2 25 AWXA200200154 1 20020213 A 5311 65677758 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - MAJOR REPAIR - C - DURING C-10 CHECK A 1.375 INCH CRACK WAS FOUND ON FRAME SUPPORT AT BS 616, WL 202, RBL 65. MAI NTENANCE CUTOUT DAMAGED AREA OF CHORD AT BS 616, FABRICATED A STIFFENING ANGLE AND REPAIR FILLER, AND INSTALLED REPAIR P ARTS IAW AWA ER 03-5311-01143-001. 2 L 7 2 4F RT A16WE 2002030400168 20020304 00168 NM 2002 3 4 F3LA200200043 1 20020221 A 5310 SHEAR TIE BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CIRCUMFERENTIAL AT APPROX STA 350 BETWEEN STR 24-L AND 24-R CORRODED ON BOTH FWD A ND AFT SIDES. FABRICATED REPLACEMENT SHEAR TIE AND INSTALLED PER SRM 53-10-4, FIG 9, 51-30-2 AND SOPM 20-41-02. 2 L 7 2 4U RT A16WE 2002022500028 20020225 00028 NM 2002 2 25 HNAA0200021 1 20020222 A 3233 10500101 ACTUATOR DHAV DHC8 DHC8102 2809003 NM #2 NACELLE BROKEN A HNAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 07 906HA 44820 9 AFTER TAKE OFF, THE RIGHT MAIN GEAR AND NOSE GEAR DID NOT INDICATE RETRACTED, GEAR DOORS STAYED OPEN. FOUND THE ROD END BROKEN OFF OF THE RIGHT MAIN GEAR RETRACTION ACTUATOR. REPLACED RETRACTION ACTUATOR. 2 H 7 2 4T RT A13NM 2002030400169 20020304 00169 NM 2002 3 4 F3LA200200044 1 20020221 A 5315 FLOORBEAM BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED TOP OF FLOORBEAM CORRODED AT STA 1016, FROM CENTER TO 30 LBL. FABRICATED AND INST ALLED REPLACEMENT FLOORBEAM TOP CAP PER SRM 51-30-02. 2 L 7 2 4U RT A16WE 2002030400177 20020304 00177 NM 2002 3 4 F3LA200200046 1 20020221 A 5320 INTERCOSTAL BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 500A - 500B, STR 26-R CORRODED AT NUT PLATE HOLES. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-10-1 AND 51-20-1. 2 L 7 2 4U RT A16WE 2002022500029 20020225 00029 NM 2002 2 25 AWXA200200157 1 20020219 A 3610 2703500 DUCT BOEING 757 7572S7 1384962 NM RROYCE RB211 RB211* 54555 NE PNEUMATIC SYS DISCONNECTED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 903AW 23323 30555 PHX - AIR TURNBACK - FLT 0081 - O - ON TAKEOFF OUT OF PHX EN ROUTE TO BWI THE NR 1 ENGINE FIRE WARNING SYSTEM ACTIVATED WITH THE FIRE SWITCH HANDLE ILLUMINATING, A RED MASTER WARNING LIGHT, A RED FIRE LIGHT ON INSTRUMENT PANEL, A RED FUEL C ONTROL SWITCH, THE FIRE BELL SOUNDING, AND EICAS MESSAGE FOR FIRE/OVERHEAT NR 1 ENGINE. AUTO THROTTLES WERE SELECTED TO OFF AND THE THROTTLE LEVER RETURNED TO CLIMB; WITH THROTTLE LEVER IN CLIMB WARNING MESSAGES CLEARED. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY BACK AT PHX. WHEN MX EXAMINED THE NR 1 ENGINE THE HIGH PRESSURE DUCT WAS FOUND DISC ONNECTED, HEAT DAMAGE WAS NOTED TO THE PYLON, C-DUCTS, AND SURROUNDING AREA. 2 L 7 2 4F 4 F RT A2NM A12EU 2002030400178 20020304 00178 NM 2002 3 4 F3LA200200047 1 20020221 A 5320 INTERCOSTAL BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED INTERCOSTALS BETWEEN STA 787 AND 794, STR 16R TO 26R, CORRODED. FABRICATED AND IN STALLED REPLACEMENT INTERCOSTALS PER SRM 51-30-2. 2 L 7 2 4U RT A16WE 2002022500030 20020225 00030 NM 2002 2 25 AWXA200200158 1 20020219 A 3230 664700500A4D CONTROL UNIT AIRBUS A319 A319132 3930340 NM E/E BAY MALFUNCTIONED A AWXA O OTHER N FALSE WARNING DE DESCENT 1 WP 28 826AW 2102 1534 PHX - EMERGENCY LANDING - FLT 0652 - C - EN ROUTE FROM IAH TO PHX ON EXTENSION OF THE LANDING GEAR AN UNSAFE MLG (UNLOCK ) INDICATION APPEARED ON REMOTE INDICATOR, ECAM ALSO INDICATED UNSAFE CONDITION FOR LGCIU NR 1, LGCIU NR 2 INDICATION WA S OK WITH GREEN DOWN AND LOCKED. FLIGHT CREW DECLARED AN EMERGENCY AND FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES, AI RCRAFT LANDED SAFELY AT PHX. MAINTENANCE PERFORMED CFDS BITE CHECK THAT FAULTED PROXIMITY SENSOR 15GA, RESISTANCE CHECK OF THE SENSOR WAS GOOD, TARGET POSITION ALSO GOOD. REMOVED AND REPLACED LGCIU NR 1 PER AMM 32-31-71, OPERATIONAL AND B ITE CHECK WERE GOOD. 2 L 7 2 4F RT A28NM 2002022500031 20020225 00031 NM 2002 2 25 C1HA200294001 1 20020217 A 3350 POWER SUPPLY BOEING 727 727290 138408W NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294AS 22146 FORWARD SECTION OF FLOOR PROXIMITY LIGHTING INOPERATIVE. REMOVED AND REPLACED FORWARD FLOOR PROXIMITY BATTERY POWER SUP PLY PER MM 33-50-23. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2002022500032 20020225 00032 NM 2002 2 25 C1HA200295004 1 20020221 A 2760 SWITCH BOEING 727 727290 138408W NM SPEED BRAKE OUT OF ADJUST A C1HA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 295AS 22147 TAKEOFF WARNING HORN CAME ON WHEN POWER LEVER WAS ADVANCED. RESULTING IN ABORTED TAKEOFF ROLL. ADJUSTED SPEED BRAKE AU TO ARM SWITCH IAW MM 27-62-02. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002022500033 20020225 00033 SO 2002 2 25 C2XA02CL051 1 20020214 A 2120 ODOR EMB 145 EMB145ER 3260211 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16944 145045 CLE FLIGHT 3151 THE CREW REPORTED A FUEL ODOR IN THE CABIN DURING APU START. MAINTENANCE PERFORMED OPERATIONAL CHECKS G OOD. NO FUEL SMELL WAS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002022500034 20020225 00034 SO 2002 2 25 C2XA02CL055 1 20020219 A 4950 4950958 BLEED VALVE EMB 145 EMB145ER 3260211 SO APU WORN A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16944 145045 CLE FLIGHT 3040 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT WITH APU RUNNING WITH BLEEDS ON. MAINTENANCE INSPE CTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002022500035 20020225 00035 SO 2002 2 25 C2XA02CL058 1 20020221 A 2612 FIRE WARNING EMB 145 EMB145ER 3260211 SO COCKPIT MALFUNCTIONED A C2XA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 27 12934 145019 CLE FLIGHT 3234 THE CREW REPORTED A APU FIRE WARNING IN FLIGHT AFTER START. THE APU WAS SHUT DOWN AND THE FIRE BOTTLE W AS EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED APU AND FOUND NO EVIDENCE OF FIRE OR NO DEFECTS. THE APU WAS OPERATIONALLY CHECKED AND NO DEFECTS WERE FOUND. THE FIRE BOTTLE WAS REPLACED AND THE AIRC RAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002022500036 20020225 00036 WP 2002 2 25 ABXA010738 1 20020123 A 5740 57647172 FITTING DOUG DC8 DC861 3021952 WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 RIGHT WING AUX SPAR, LOWER "L" ANGLE, WAS CRACKED APPROXIMATELY 10 INCHES LONG AT XRS 47. REPLACED FITTING IAW DC-8 SRM 51-1-24, 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 2002022500037 20020225 00037 SO 2002 2 25 C2XA02IA036 1 20020218 A 5315 14522226003 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 10967 145005 IAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT THE CENTER FLOORBEAM GUSSET WAS CORRODED BETWEEN FRAMES 58 AND 60. MA INTENANCE REMOVED AND REPLACED THE CENTER FLOORBEAM GUSSET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, UPON REL EASE FROM C-CHECK. 2 L 7 2 4F RT T00011AT 2002022500038 20020225 00038 SO 2002 2 25 C2XA02IA037 1 20020218 A 5315 14526437001 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 10967 145005 IAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT THE RIGHT OUTBOARD FLOORBEAM DIGITAL RECESS WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM CAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, UPON RELEASE FROM C-CHECK. 2 L 7 2 4F RT T00011AT 2002022500039 20020225 00039 EU 2002 2 25 C2XA02IA038 1 20020220 A 3350 3011160 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14834 193 IAH- WHILE PERFORMING A LINE/WEEKLY CHECK IT WAS NOTED THAT THE GALLEY FLOOR LEVEL EXIT LIGHT FAILED TO ILLUMINATE. MAI NTENANCE REMOVED AND REPLACED THE GALLEY FLOOR LEVEL EXIT LIGHT, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002022500040 20020225 00040 SO 2002 2 25 C2XA02TY033 1 20020219 A 5523 14539190401 LEVER EMB 135 EMB135LR 3260305 SO ELEVATOR TAB GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS DURING A SCHEDULED 1-C INSPECTION THE LT SERVO TAB DOG BONE WAS FOUND WEARING AGAINST THE ELEVATOR SUPPORT BRACKET, WHICH REQUIRED A GST. ALL WORK WAS ACCOMPLISHED IAW GST-0522/02 AND WILL BE RELEASED UPON COMPLETION OF THE INSPECTION . 2 L 7 2 4F RT TOOO11AT 2002022500041 20020225 00041 SO 2002 2 25 C2XA02TY034 1 20020219 A 5523 14539190401 LEVER EMB 135 EMB135LR 3260305 SO ELEVATOR TAB GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS DURING A SCHEDULED 1-C INSPECTION THE RT SERVO TAB DOG BONE WAS FOUND WEARING INTO THE ELEVATOR SUPPORT BRACKET WHI CH REQUIRED A GST. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002022500042 20020225 00042 SO 2002 2 25 C2XA02TY035 1 20020220 A 5320 14524131005 ANGLE EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND ON THE SUPPORT ANGLE AT THE MAIN DOOR ENTRANCE BELOW THE THRE SHOLD. MAINTENANCE REMOVED AND REPLACED THE SUPPORT ANGLES, ALODINE AND PAINTED IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 1-C INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002022500043 20020225 00043 SO 2002 2 25 C2XA02BT004 1 20020222 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO PASSENGER CABIN FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14945 145049 EWR---CO3431, CREW REPORTED EMERGENCY LIGHTS INOPERATIVE (REAR SECTION ONLY)....MAINTENANCE REMOVED AND REPLACED AFT EME RGENCY LIGHT INVERTER IAW EMB145 AMM 33-50-11. OPS. CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002022500044 20020225 00044 SO 2002 2 25 C2XA02TY036 1 20020220 A 5552 ATTACH FITTING EMB 145 EMB145LR 3260212 SO ELEVATOR SEPARATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15985 145248 TYS, DURING A SCHEDULE INSPECTION THE LEFT ELEVATOR ATTACH FITTING WAS FOUND SEPARATING FROM THE HORIZONTAL STABILIZER O N THE LEFT SIDE. MAINTENANCE REMOVED AND REPLACED THE RIVETS WITH NEW OVERSIZED AND USING THE REMAINING RIVET PROTRUDIN G HEAD PART AS SHIM TO THE NEW ONE AS A PERMANENT REPAIR IAW-EMB-GST-0580/02. AIRCRAFT RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002030400180 20020304 00180 NM 2002 3 4 F3LA200200048 1 20020221 A 5320 ANGLE BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED FWD CARGO BAY AFT BULKHEAD SUPPORT ANGLE AT STA 520, STR 26-L TO 19-L, CORRODED. REPLACED ANGLE PER SRM 51-10-1. 2 L 7 2 4U RT A16WE 2002022500045 20020225 00045 SO 2002 2 25 C2XA02TY037 1 20020220 A 5315 14521721005 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS DURING A SCHEDULED 1-C INSPECTION THE FORWARD DIGITAL PLATE AFT OF THE COCKPIT DOOR WAS FOUND CORRODED. MAINTENANC E REMOVED THE CORROSION BY CUTTING OUT THE CENTER SECTION OF THE DIGITAL PLATE AND FAB. A NEW PART WITH A DOUBLER AND S HIM, ALODINE, PRIME AND PAINTED IAW EMB 135/145 SRM 51-40-02, CPM 51-21-04, 05, 06 AND EC 5320-01059. ALL WORK WAS ACCO MPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 1-C INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002022500046 20020225 00046 SO 2002 2 25 C2XA02TY039 1 20020221 A 5315 14521721005 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS, DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON THE FORWARD DIGITAL PLATE AFT OF COCKPIT DOOR. MAINTENANC E REMOVED CORROSION BY CUTTING OUT THE CENTER SECTION AND INSTALLING A NEW SECTION, FABRICATED AND INSTALLED DOUBLERS AN D SHIMS, ALODINED AND PRIMED IAW-EMB-135/145-SRM-51-40-02 & CMP-51-21-04, 05, 06 AND EC5320-01059. REPAIR PROCEDURE WAS SATISFACTORY AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002022500047 20020225 00047 SO 2002 2 25 C2XA02TY044 1 20020221 A 5330 SKIN EMB 135 EMB135LR 3260305 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS, DURING A SCHEDULED 1C INSPECTION, A DENT WAS FOUND ON THE FUSELAGE SKIN AFT OF FR24, BELOW STR 10R. MAINTENANCE RE CONTOURED DENT, PERFORMED DYE-PENATRENT INSPECTION (NO CRACKS NOTED) IAW-EMB-GST-0504/2. REPAIR PROCEDURE WAS SATISFAC TORY AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002022500048 20020225 00048 SO 2002 2 25 C2XA02TY045 1 20020222 A 3397 WIRE EMB 135 EMB135LR 3260305 SO CABIN BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS, DURING A SCHEDULED 1C INSPECTION A BROKEN WIRE WAS FOUND ON EMERGENCY LIGHT STRIP ON PANEL 251DE. MAINTENANCE REMO VED AND REPLACED THE EMERGENCY LIGHT STRIP IAW-EMB-135-AMM-33-50-12, OPERATIONAL CHECKED GOOD, AIRCRAFT RELEASED TO SERV ICE. 2 L 7 2 4F RT TOOO11AT 2002022500049 20020225 00049 NM 2002 2 25 CALA0200082 1 20020218 A 5551 ATTACH FITTING BOEING 737 737524 1384721 NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19636 26340 INSPECTION FOUND LT HORIZONTAL STABILIZER UPPER FORWARD ATTACH FITTING ON CENTER BOX LUG FACE CORRODED AROUND BUSHING FO RWARD LUG FACE. THE BUSHING WAS REMOVED AND AN OVERSIZED BUSHING WAS INSTALLED IAW CMM 55-10-06. 2 L 7 2 4F RT A16WE 2002022500050 20020225 00050 NM 2002 2 25 CALA0200084 1 20020220 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A 2 INCH CRACK IN AC BAY FLOOR SUPPORT AT STA 559, RBL 24, IN FORWARD BAGGAGE BIN. THE SUPPORT WAS REM OVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002022500051 20020225 00051 NM 2002 2 25 CG8A20020003 1 20020209 A 2612 100012703 CONTROL UNIT BOEING 727 727223 1384074 NM CARGO BAY MALFUNCTIONED A C8GA O OTHER N FALSE WARNING CR CRUISE 1 SO 15 898AA 22014 FLT 707 FROM DEN TO TOL. DURING CRUISE LEVEL, THE FORWARD LOWER CARGO COMPARTMENT FIRE LIGHT CAME ON. APPROPRIATE CHEC K LIST WERE ACCOMPLISHED AND FIRE WARNING LIGHT REMAINED ILLUMINATED. NOTIFIED ATC OF THE FIRE WARNING LIGHT AND LANDED WITHOUT INCIDENT. INSPECTED FORWARD CARGO PIT AND FOUND NO EVIDENCE OF FIRE. REPLACED FIRE DETECTION CENTRAL CONTROL UNIT AND BATTERY AND PERFORMED SYSTEM OPERATIONAL CHECK IAW SECURAPLANE ST3000 MANUAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2002022500052 20020225 00052 EU 2002 2 25 CHQ000119 1 20020220 A 2612 FIRE WARNING SAAB SF340 SF340A 7850100 EU LT ENGINE MALFUNCTIONED A CHQA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 11 95 095 LEFT ENGINE TAIL HOT LIGHT, ABORTED TAKEOFF. CLEANED CONNECTORS AND PERFORMED OPS CHECK OF FIRE DETECTION SYSTEM, NO FA ULTS FOUND. 2 L 7 2 4T RT A52EU 2002022500054 20020225 00054 EA 2002 2 25 02035638 1 20020204 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 638BR 7311 During maintenance inspection, it was discovered that the aft emergency flood light was inoperative. Maintenance person nel removed and replaced the lamp in the aft emergency flood light. An operational check was satisfactory and the aircr aft was returned to service. 2 L 7 2 4F RT A21EA 2002022500055 20020225 00055 EA 2002 2 25 02038631 1 20020207 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 631BR 7261 DURING MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE MAIN CABIN DOOR, LOWER, FORWARD, EMERGENCY LIGHT WAS INOPERATI VE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE MAIN CABIN DOOR , LOWER, FORWARD EMERGENCY LIGHT ASSY. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002030700041 20020307 00041 NM 2002 3 7 02FDEA00138 1 20020220 A 2497 D233900 WIRE HARNESS DOUG MD11 MD11F 3023600 NM NR 3 GENERATOR BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 NR 3 ENG GENERATOR FEEDER CABLE N117-1-00A (AL) NEAR TERMINAL STRIP S3-385R BROKEN. REMOVED AND REPLACED NR 3 ENG GEN FEEDER LINE CABLE AND CLAMPS PER MM 24-22-03-5. 2 L 7 3 4F RT A22WE 2002030700042 20020307 00042 NM 2002 3 7 02FDEA00141 1 20020224 A 2497 D233900 WIRE HARNESS DOUG MD11 MD11F 3023600 NM NR 1 GENERATOR BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 NR 1 ENG GENERATOR FEEDER CABLE N012-2-00B (AL) BROKEN NEAR LT WING ROOT FEED THROUGH. REMOVED AND REPLACED NR 1 ENG GE N FEEDER LINE CABLE AND CLAMPS PER MM 24-22-03-5. 2 L 7 3 4F RT A22WE 2002022500056 20020225 00056 2002 2 25 371PA0003 4 20020215 A 2210 AUTOPILOT SYS BOEING 737 737306 NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 371PA 23543 Autopilot disconnecting without commands 2 L 7 2 4F RT A16NE 2002030400184 20020304 00184 NM 2002 3 4 F3LA200200052 1 20020221 A 5315 FLOORBEAM BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED AFT FLOORBEAM AT STA 967 CORRODED ON TOP SURFACE. FABRICATED AND REPLACED FLOORBE AM CAP PER SRM 51-30-2. 2 L 7 2 4U RT A16WE 2002030400185 20020304 00185 NM 2002 3 4 F3LA200200053 1 20020221 A 5320 WEB BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED WEB AT STA 1016, STR 20-L, BEHIND L-2 DOOR. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-30-2 AND BOEING DRAWING 65-46812. 2 L 7 2 4U RT A16WE 2002022600047 20020226 00047 EA 2002 2 26 COMA0260114 1 20020225 A 5751 601R130002 SKIN CNDAIR CL600 CL6002B19 1900309 EA AILERON BUCKLED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 931CA 18207 7037 THE RT AILERON LOWER OUTBOARD SKIN WAS BUCKLED. REPAIRED THE BUCKLED SKIN IAW WVAC EO 601R-57-2984. 2 L 7 2 4F RT A21EA 2002030400165 20020304 00165 NM 2002 3 4 F3LA00200054 1 20020221 A 5315 FLOORBEAM BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY TRANSVERSE FLOORBEAM CORRODED AT STA 986 TO STA 1006, LBL 10. REPLAC ED DAMAGED TRANSVERSE FRAME TOP CAP PER SRM 51-30-2 AND 51-10-2. 2 L 7 2 4U RT A16WE 2002030400186 20020304 00186 NM 2002 3 4 F3LA200200055 1 20020221 A 7110 GUSSET BOEING 737 7372Y5 1384554 NM NR 1 COWLING WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE RT EXHAUST COWL INSIDE FLANGE ON BOTTOM OF THIRD RIB FROM FRONT WORN. REMOVED DAMAGED GUSSET FROM NR 1 ENGINE RT EXHAUST COWL. FABRICATED AND INSTALLED REPLACEMENT GUSSET PER SRM 51-21-171 AND 51-30-2. 2 L 7 2 4U RT A16WE 2002022500057 20020225 00057 NM 2002 2 25 CALA0200086 1 20020222 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 927 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND Z-ANGLE CORRODED AT L-2 DOOR JAMB, STA 927. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-05. 2 L 7 2 4F RT A16WE 2002022500058 20020225 00058 NM 2002 2 25 CALA0200088 1 20020222 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 500C CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A 1" CRACK IN STRINGER 16L AFT OF STA 500C. REPAIRED STRINGER IAW SRM 53-00-03, FIGURE 201. 2 L 7 2 4F RT A16WE 2002022500059 20020225 00059 NM 2002 2 25 CALA0200089 1 20020222 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 277 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND A 1/4" CRACK IN WEB AT STA 277, S14R. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002022500060 20020225 00060 NM 2002 2 25 CALA0200090 1 20020222 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 270 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A 1/2" CRACK IN WEB AT STA 270, S14R. A WEB INTERCOSTAL WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002022500061 20020225 00061 NM 2002 2 25 CALA0200094 1 20020224 A 5700 SKIN BOEING 737 7373T0 1384582 NM FLAP FAIRING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A 1/2" CRACK IN R/H WING #6 FLAP FAIRING LOWER SKIN WITH RIVETS PULLING THROUGH. A STIFFENER WAS INSTAL LED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2002022500062 20020225 00062 EA 2002 2 25 COMA0260101 1 20020218 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 729CA 7367 7265 TWO DENTS APPROX .077 AND .085 DEEP. THE DENTS ARE A SINGLE LINE EXTENDING FOR A COMBINED TOTAL OF 14 INCHES. REPAIRED IAW EA 10-5310-0047A. 2 L 7 2 4F RT A21EA 2002030400187 20020304 00187 NM 2002 3 4 F3LA200200056 1 20020221 A 5310 DOOR FRAME BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD DOOR FRAME AT STA 803, STR 24-R, CRACKED AND CORRODED. REPLACED AFT CARGO COMPARTMENT DOOR FRAME PER SRM 57-10-1 AND 51-30-2. 2 L 7 2 4U RT A16WE 2002022500063 20020225 00063 NM 2002 2 25 PCAA0202030 1 20020224 A 2120 PW120A ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT SMOKE A PCAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 820EX 25329 14 019 120912 LGA FLIGHT#3829. CREW REPORTED BURNING ODOR LIKE A DUCT OVERHEAT. DUCT TEMP 20 DEGREES. FLIGHT ATTENDANT REPORTED A LIGH T HAZE IN CABIN. LEFT ENGINE WAS REPLACED IN ACCORDANCE WITH ALLEGHENY AIRLINES JOB CARD# 008-7101-349. AIRCRAFT RETUENE D TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002030400189 20020304 00189 NM 2002 3 4 F3LA200200058 1 20020221 A 5320 INTERCOSTAL BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INTERCOSTAL CORRODED FROM STA 1006 TO STA 1016, BL 0. FABRICATED AND RE PLACED INTERCOSTAL PER SRM 53-10-2 AND 51-30-2. 2 L 7 2 4U RT A16WE 2002022500087 20020225 00087 2002 2 25 GTIA020003 4 20020110 A 2230 2587781901 DRIVE UNIT DOUG DC9 DC981 3022081 WP AUTOTHROTTLE SYS FAULTY A GTIA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 GL 23 819NK 48016 FLT 1225 - RSW - AUTOTHROTTLES INOPERATIVE, WOULD NOT ENGAGE FOR TAKEOFF, WOULD NOT STAY ENGAGED AT CRUISE. REMOVED AND REPLACED A/T SERVO DRIVE UNIT IAW MD80 MM 22-31-01. OPERATIONAL TEST, OPS OK, RAN RTS TEST ON STP, OPS OK IAW MD80 MM 22-01-05. (M) 2 L 7 2 4F A6WE 2002022500088 20020225 00088 WP 2002 2 25 GTIA020005 1 20020105 A 2760 5935212501 SWITCH DOUG DC9 DC981 3022081 WP SPOILER MALFUNCTIONED A GTIA O OTHER O OTHER LD LANDING 1 GL 23 805NK 48058 GROUND SPOILER DID NOT DEPLOY ON EITHER WING DURING LANDING. REMOVED AND REPLACED AUTO SPOILER SWITCHING UNIT. OPS CHE CK GOOD PER MD80 MM 27-62-09. (M) 2 L 7 2 4F A6WE 2002022500089 20020225 00089 WP 2002 2 25 GTIA020006 1 20020114 A 2410 697902E SWITCH DOUG DC9 DC982 3022082 WP RT CSD FAULTY A GTIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 817NK 49141 FLT 1504 - RSW - RETURN TO GATE, RIGHT CSD LOW OIL PSI LIGHT ON AT 80 KTS. RETURN TO GATE. REMOVED AND REPLACED RIGHT CSD LOW OIL PRESSURE SWITCH. OPS CHECKS GOOD IAW MD80 MM 24-10-01. (M) 2 L 7 2 4F A6WE 2002022500090 20020225 00090 WP 2002 2 25 GTIA020007 1 20020115 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 809NK 49503 DTW - FOUND EMERGENCY CABIN OVERHEAD LIGHT, 9 BURNED OUT WITH EMERGENCY POWER 2 EMERGENCY LIGHTS ON. REMOVED AND REPLAC ED BATTERY PACKS REF 33-53-00, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2002022500091 20020225 00091 WP 2002 2 25 GTIA020008 1 20020115 A 2560 LATCH DOUG DC9 DC983 3022083 WP R1 DOOR BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FLT 165 - PBI - FOUND SLIDE PACK R1 DOOR WILL NOT LATCH. REPAIRED BROKEN LATCH. SYSTEM OPERATES NORMALLY IAW MD80 MM 2 5-62-00, NO OTHER DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2002022500092 20020225 00092 WP 2002 2 25 GTIA020009 1 20020113 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 47113 DTW - FOUND OVERWING EXIT LIGHTS WILL NOT COME ON. REMOVED AND REPLACED BATTERY PACK SYSTEM, OPS CHECK GOOD PER DC9 MM 33-53-01. (M) 2 L 7 2 4F A6WE 2002022500093 20020225 00093 2002 2 25 GTIA020010 4 20020121 A 2210 4034238901 ACCELEROMETER DOUG DC9 DC982 3022082 WP AUTOPILOT SYS MALFUNCTIONED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 823NK 48020 DTW - WHILE LEVEL AT CRUISE THE 'YAW DAMP OFF' LIGHT ILLUMINATED FOR APPROX 5 MINUTES AND BOTH FMA'S SHOWED VERTICAL SPE ED AND NO AUTOLAND (PREV SHOWED ALT HOLD) THIS WAS ON DFGC NR 1, SWITCHED TO DFGC NR 2 AND PROBLEM REMAINED, AFTER SEVER AL MINUTES SWITCHED BACK TO DFGC NR 1 LIGHT STAYED ON UNTIL NOSE (YAW) TRIM WAS ADJUSTED SLIGHTLY LEFT AND RIGHT THIS AL L OCCURRED WHETHER AUTOPILOT WAS ON OR OFF NO ADVERSE YAW OF AIRCRAFT WAS EVER FELT QRH REF. REMOVED AND REPLACED DUAL LATERAL ACCELEROMETER PER MD80 MM 22-19-02. SYSTEM OPS CHECK (RTS) PER MD80 MM 22-01-05. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002022500094 20020225 00094 2002 2 25 GTIA020011 4 20020119 A 2210 4034242934 CONTROL PANEL DOUG MD80 MD83 3023681 NM COCKPIT FAULTY A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 822NK 49392 DTW - FLT 114 - FIVE MINUTES AFTER TAKEOFF ATTEMPTED TO ENGAGE AUTO PILOT NR 2 WOULD NOT ENGAGE. TRIED NR 1 IT WOULD NO T ENGAGE. COMPASSES AND ATTITUDE INDICATOR WERE CLOSELY MATCHED. AFTER SEVERAL ATTEMPTS TO ENGAGE AUTO PILOT NR 1 AND NR 2 AUTO PILOT NR 1 ENGAGED AND OPS NORMAL. AUTOPILOT NR 1 USED DTW TO PBI. FOUND CAPTAINS AUTO PILOT DISCOUNTED SWIT CH BAND AND FLIGHT GUIDANCE CONTROL PANEL BAD. REMOVED AND REPLACED CAPTAINS AUTO PILOT DISCOUNT SWITCH AND FLIGHT GUID ANCE CONTROL PANEL. SYSTEM OPS CHECK GOOD IAW MD80 MM 22-01-05 AND 22-01-04. (M) 2 L 7 2 4F RT 2002022500095 20020225 00095 WP 2002 2 25 GTIA020012 1 20020113 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 47113 DTW - FOUND OVERWING EXIT LIGHTS WILL NOT COME ON. REMOVED AND REPLACED BATTERY PACK SYSTEM. OPS CHECK GOOD PER MM 33- 53-01. (M) 2 L 7 2 4F A6WE 2002022500096 20020225 00096 WP 2002 2 25 GTIA020013 1 20020115 A 2560 LATCH DOUG DC9 DC983 3022083 WP SLIDE PACK BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 ACY - FOUND SLIDE PACK R1 WILL NOT LATCH. REPAIRED BROKEN LATCH SYSTEM OPERATES NORMALLY IAW MD-80 MM 25-62-00. NO OTH ER DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2002022500097 20020225 00097 NM 2002 2 25 AWXA200200163 1 20020223 A 2420 727792K IDG BOEING 757 7572S7 1384962 NM #2 ENGINE DEFECTIVE A AWXA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 WP 28 905AW 28773 23567 PHX - ELECTRICAL POWER LOSS - FLT 813 - "C" - WHILE CLIMBING OUT OF PHX ENROUTE TO SFO THE APU FAILED, AIRCRAFT ALREADY OPERATING ON MEL 24-00-1 CONDITION #1 FOR #2 ENGINE DRIVEN GENERATOR INOPERATIVE, AIRCRAFT TURNED BACK TO PHX AND LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE INTEGRATED DRIVE GENERATOR IAW T/C R5M24601, AND THE GENERATOR FIELD PANEL IAW B MM 31-10-00. MAINTENANCE ALSO FOUND A BENT PIN ON THE FIRE CONTROL MODULE CONNECTOR; REPAIRED THE PIN AND THE #2 ENGINE DRIVEN GENERATOR OPERATIONALLY CHECKED GOOD. THE APU INDICATED UNDERSPEED ON BITE AND WAS TROUBLESHOT IAW FAULT ISOLATIO N MANUAL 49-11-00, FIG 106, THE APU FUEL CONTROL UNIT WAS FOUND FAULTY AND REPLACED IAW T/C R6D49604. PART NAME; PANEL F 2 L 7 2 4F RT A2NM 2002022500098 20020225 00098 NM 2002 2 25 AWXA200200164 1 20020223 A 2923 AN9244D NUT BOEING 737 737301 1384611 NM STA 727 LOOSE A AWXA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 WP 28 325AW 23260 LAS - DIVERSION - FLT 771 - "C" - ENROUTE FROM PHX TO SMF "B" HYDRAULIC SYSTEM INDICATED QUANTITY LOSS OF 1/3 OF THE RES ERVIOR, A MAJOR DECREASE IN QUANTITY WAS NOTED WHEN LANDING GEAR AND FLAPS WERE IN MOTION, AFTER RETRACTION WAS COMPLETE FLUID QUANTITY LEVEL CAME BACK UP, AIRCRAFT DIVERTED SAFELY TO LAS. IN LAS WHEN MAINTENANCE ARRIVED AT THE AIRCRAFT FLU ID WAS FOUND LEAKING FROM A RETURN LINE COMING OFF THE STANDBY HYDRAULIC PUMP AT THE AFT BULKHEAD OF THE LEFT WHEEL WELL . MAINTENANCE TIGHTEN THE "B" NUT ON THE RETURN LINE, RESERVICED THE RESERVIOR, AND PERFORMED AN OPERATIONAL CHECK AND L EAK CHECK OF THE HYDRAULIC SYSTEM, ALL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2002022500099 20020225 00099 NM 2002 2 25 AWXA200200165 1 20020224 A 3040 558CA01Y1 CONTACTOR AIRBUS A319 A319132 3930340 NM FR 12 DEFECTIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 810AW 1116 PHX - AIR TURN BACK - FLT 126 - "C" - DURING CLIMB OUT OF PHX ENROUTE TO MKE BETWEEN FL360 AND FL370 RECEIVED WARNING ME SSAGE THAT R/H WINDSHIELD WINDOW HEAT WAS INOPERATIVE, AIRCRAFT TURNED BACK TO PHX AND LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOT SYSTEM AND REPLACED WINDOW HEAT COMPUTER #2 IAW AMM 30-42-34. EXAMINATION POST FLIGHT REPORT ALSO REVEALED E CAM WARNINGS AT SAME TIME OF WINDOW HEAT WARNINGS FOR NAV RA 2 FAULT, RECORDER FDIU FAULT, AND R/H ANTI-ICE WINDSHIELD, ALL HAD ASSOCIATED FAILURE MESSAGES. ALL SYSTEM USE THE PHASE B BUS #2 AND ALL HAVE CONTACTOR 9XU2 IN COMMON. REPLACED 9 XU2 3-POLE CONTACTOR IAW 24-22-55-401, OPERATIONAL CHECK OF SYSTEM WAS GOOD. PART NAME; WINDOW HEAT COMPUTER, MFG; SAGEM 2 L 7 2 4F RT A28NM 2002022500106 20020225 00106 2002 2 25 RAIA00202081 4 20020222 A 3425 70147000918 ADC EMB 145 EMB145 3260210 SO INOPERATIVE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 806HK 7490 3333 145112 5292-BGM- ON TAKE OFF ROLL GOT NUMEROUS WARNING MESSAGES: SPS, GPWS, AND #1 AHRS INOP. MAINTENANCE REMOVED AND REPLACED THE #1 AIR DATA COMPUTER, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002022500107 20020225 00107 SO 2002 2 25 RAIA00202082 1 20020223 A 3240 15851 PRESSURE SWITCH EMB 145 EMB145 3260210 SO FAILED A RAIA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CE 03 801HK 8289 145053 5270-PIT- TAKE OFF CONFIGURATION WARNING: "BRAKE". MAINTENANCE REMOVED AND REPLACED PARKING BRAKE PRESSURE SWITCH. 2 L 7 2 4F RT T00011AT 2002040100030 20020401 00030 NM 2002 4 1 02FDEA00142 1 20020223 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 CORROSION ON SKIN AND STRINGER AT BS 950D TO 950E, STR 28L. REMOVED AND REPLACED SKIN PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 2002022600001 20020226 00001 NM 2002 2 26 0200506624 1 20020103 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 624US 21706 DURING "H" CHECK FOUND CRACK IN UPPER DECK FLOORBEAM AT BS 300 RBL 64. REPAIRED PER EA 66-188018. 2 L 7 4 4F RT A20WE 2002022600002 20020226 00002 NM 2002 2 26 0200515505 1 20020204 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 505US 23194 DURING "H" CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 45. REPAIRED PER EA 55-188101. 2 L 7 2 4F RT A2NM 2002022600003 20020226 00003 NM 2002 2 26 0200525505 1 20020205 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 505US 23194 DURING "H" CHECK FOUND CRACK ON FLOORBEAM AT BS 700 LBL 25. REPAIRED PER EA 55-188102. 2 L 7 2 4F RT A2NM 2002022600004 20020226 00004 NM 2002 2 26 0200535505 1 20020213 A 5311 WEB BOEING 757 757251 1384970 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 505US 23194 During "H" check found crack on intercostal web at BS 660 STR 14 LT. Repaired per EA 55-188113. 2 L 7 2 4F RT A2NM 2002022600005 20020226 00005 NM 2002 2 26 02022501 1 20020210 A 5320 146N5246U6 FLOOR SUPPORT BOEING 757 757236 1384971 NM FUSELAGE CORRODED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 506N 31978 24771 DURING C-CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BS 1675, RBL 56, WL 208. CORROSION CLEANED UP, DETERMINED TO BEYOND ACCEPTABLE LIMITS. REPLACED FLOOR SUPPORT. 2 L 7 2 4F RT A2NM 2002022600006 20020226 00006 NM 2002 2 26 02022502 1 20020223 A 3610 51444138 DUCT BOEING 757 7572T7 1384914 NM RROYCE RB211 RB211535E4 54555 NE NR 1 ENGINE LEAKING A N8TA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 513NA 23895 30607 DURING CLIMB, PASSING THROUGH 8,000 FT MSL, LENG OVERHEAT EICAS MESSAGE CAME ON. SECURED BLEED VALVE, RETARDED THRUST; MESSAGE EXTINGUISHED. INVESTIGATION REVEALED HP6 DUCT LEAKING. REPLACED HP6 DUCT, LEAK CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2002022600007 20020226 00007 EU 2002 2 26 02FDEA00139 1 20020222 A 3230 D221270005 DAMPER AIRBUS 310 A310222 3930315 EU RT MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 450FE 162 UNABLE TO RAISE LANDING GEAR AFTER T/O. REMOVED AND REPLACED RT MLG BOGIE BEAM PITCH DAMPER PER MM 32-11-15-4 02 AND 12 -12-32-0 A/C NEEDS GEAR SWING JACKED AIRCRAFT PER MM 07-11-00-0. OPS CHECK NORMAL. 2 L 7 2 4F RT A35EU 2002022600008 20020226 00008 WP 2002 2 26 02FDEA00140 1 20020222 A 5754 SLAT DOUG DC10 DC1030F 3023504 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 303FE 46802 NR 1 SLAT RT WING CRACKED AT LIGHTNING HOLE AT I/B END AT XFS 145. REMOVED AND REPLACED DOUBLER PER SRM 57-00-01 VOL 1 FIG 4. 2 L 7 3 4F RT A22WE 2002022600009 20020226 00009 2002 2 26 372PA0001 4 20020223 A 3417 ADC BOEING 737 737306 NM E/E BAY MALFUNCTIONED A PIDA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 05 372PA 23546 DURING LEVEL OFF FROM CLIMB, FMC SYSTEMS SWITCHED CPU PAGE TO IAS LEGS PAGE. VNAV DISCONNECTED TO CWS PITCH AND LNAV DI SCONNECTED TO CWS ROLL. ROUTE DISAPPEARED FROM HSI. DURING APPROACH AP ENGAGED IN GS AND LOC, AUTOPILOT PITCHED UP RAD ICALLY AND SPEEDS DECREASED. AT DID NOT CONNECT. 2 L 7 2 4F RT A16NE 2002022600010 20020226 00010 2002 2 26 372PA0002 4 20020225 A 2213 CONTROL UNIT BOEING 737 737306 NM AUTOPILOT SYS FAULTY A PIDA K NONE O OTHER CL CLIMB 1 SO 05 372PA 23546 V-NAV ON AUTOPILOT WILL NOT ENGAGE IN CLIMB. EVENTUALLY WHEN IT DOES ENGAGE IT WILL DISCONNECT FOR NO APPARENT REASON. 2 L 7 2 4F RT A16NE 2002022600011 20020226 00011 WP 2002 2 26 ABXA010725 1 20020206 A 5320 5913093501 SUPPORT FITTING DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 TWO VERTICAL SUPPORTS CRACKED, EACH SIDE OF THE RUDDER TORQUE TUBE AREA. REPLACED THE VERTICAL SUPPORT BRACKETS, RIGHT AND LEFT SIDE IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002022600012 20020226 00012 WP 2002 2 26 ABXA010726 1 20020207 A 5730 59134383 PANEL DOUG DC9 DC931 3022065 WP LT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 LEFT WING, LOWER INBOARD BONDED PANEL HAD AREA OF DELAMINATION. REPLACED PANEL IAW DC-9 SRM 51-30-2 AND 51-30-1. SEAM SEALED PANEL IAW DC-9 SRM 51-20-6. 2 L 7 2 4F A6WE 2002022600013 20020226 00013 WP 2002 2 26 ABXA010727 1 20020207 A 5753 5910041510 VANE DOUG DC9 DC931 3022065 WP T/E FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 INBOARD FIXED VANE WAS DELAMINATED ON LOWER SKIN AT XRS 170. REPLACED FIXED VANE IAW DC-9 SRM 27-51-02-2-0002. 2 L 7 2 4F A6WE 2002022600014 20020226 00014 WP 2002 2 26 ABXA010728 1 20020207 A 5543 5910257501 TAB DOUG DC9 DC931 3022065 WP RUDDER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 RIGHT SIDE OF RUDDER TAB DELAMINATED. REPLACED RUDDER CONTROL TAB IAW DC-9 AMM 27-20-02-4-0001. 2 L 7 2 4F A6WE 2002022600015 20020226 00015 WP 2002 2 26 ABXA010729 1 20020208 A 5230 59101577 PAN DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 AFT LOWER CARGO DOOR, OUTER PAN BULGED AND CRACKED AROUND BLIND NUT ON LEADING EDGE. REPAIRED AREA IAW DC-9 SERVICE REW ORK DWG 5934142. 2 L 7 2 4F A6WE 2002022600016 20020226 00016 WP 2002 2 26 ABXA010730 1 20020208 A 5230 995766647 INTERCOSTAL DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 AFT LOWER CARGO DOOR, TEMPORARY REPAIR (STOP DRILL) ON INTERCOSTAL ON AFT SIDE OF LOWER DOOR STOP FITTING. REPLACED INT ERCOSTAL IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 2002022600017 20020226 00017 WP 2002 2 26 ABXA010732 1 20020208 A 5230 591015775 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 AFT LOWER CARGO DOOR, NR 3 INTERCOSTAL BEAM FORWARD END FITTING ANGLE CRACKED. REPLACED ANGLE IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2002022600018 20020226 00018 WP 2002 2 26 ABXA010735 1 20020211 A 5310 59174637 DOOR FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 AFT VENTRAL DOOR JAMB AT RBL 0 TO RBL 6, LOWER SECTION, CORRODED AND TWO POPPED RIVETS. REPAIRED AREA IAW DC-9 SRM 51-7 0-5. 2 L 7 2 4F A6WE 2002022600019 20020226 00019 WP 2002 2 26 ABXA010736 1 20020122 A 5320 37502571 SPLICE DOUG DC8 DC861 3021952 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 FORWARD CARGO AT FS 600 - 620, LONGERON 31 RIGHT, SPLICE FITTING WAS CRACKED, OUTBOARD SIDE. REPLACED FITTING IAW DC-8 SRM 51-1-24, 51-3-2 AND 51-1-20D. 2 L 7 4 4F 4A25 2002022600020 20020226 00020 WP 2002 2 26 ABXA010737 1 20020122 A 5320 37503301 SPLICE DOUG DC8 DC861 3021952 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 FORWARD CARGO AT FS 600 - 620, LONGERON 25 RIGHT, SPLICE FITTING WAS CRACKED. REPLACED FITTING IAW DC-8 SRM 51-3-2, 51- 1-20D AND 51-1-11. 2 L 7 4 4F 4A25 2002022600021 20020226 00021 WP 2002 2 26 ABXA010739 1 20020123 A 5720 57732542 FITTING DOUG DC8 DC861 3021952 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 RIGHT WING REAR SPAR, XRS 340, ACTUATOR ATTACH FITTING TO REAR SPAR WAS CRACKED. REPLACED FITTING IAW DC-8 DAC DWG 5773 254, MM 20-16-00, 20-14-00 AND 27-51-09. 2 L 7 4 4F 4A25 2002032900148 20020329 00148 EU 2002 3 29 AWXA200200162 1 20020222 A 2720 810A000005 SERVO AIRBUS 320 A320232 3930326 EU RUDDER FAILED A AWXA A UNSCHED LANDING E F J VIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 28 654AW 9957 1050 AT 26,500 FT 307 KTS ACFT STARTED VIBRATING. FLT CTL ECAM PAGE INDICATED ERRATIC & LOOSE RUDDER INPUTS BY AUTO PILOT, A CFT TURNED BACK. MX PERFORMED A RUDDER FREE PLAY CHK, RUDDER SERVO CONTROL, HINGE BEARING CHK, FLT AUGMENTATION COMPUTE R CHK & NO DEFECTS NOTED. REPLACED BUSHING AT BRACKET, RUDDER SERVO CONTROL, RUDDER CENTERING ROD SPRING, OPS CKS GOOD. FLT FOR RUDDER FOUND SATISFACTORY. VENDOR BENCH TEST OF RUDDER SERVO CTL CONFIRMED FAILURE OF UNIT FINDING SWIVEL BEA RINGS AT HOUSING & ROD END-EYE LOOSE, HYD LEAK FOUND AT END OF HOUSING & TOP OF GLAD, BUSHING FOUND WORN ON LEVER ARM. ALL AFFECTED ITEMS REPLACED. 2 L 7 2 4F RT A28NM 2002022600022 20020226 00022 SO 2002 2 26 C2XA02CL059 1 20020224 A 2530 CBC16707 RECEPTACLE EMB 145 EMB145LR 3260212 SO GALLEY BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14916 145415 CLE FLIGHT 3296 THE CREW REPORTED A BURNING SMELL FROM THE NR 1 COFFEE POT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 COFFEE POT RECEPTACLE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002022600023 20020226 00023 SO 2002 2 26 C2XA02IA035 1 20020213 A 4930 4501968D APU EMB 145 EMB145LR 3260212 SO APU BAY LEAKING A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 13955 145075 CLE- THE CREW NOTED THAT A STRONG FUEL ODOR OCCURRED WHEN STARTING THE APU. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL. MAINTENANCE REMOVED AND REPLACED THE APU. PERFORMED A OPERATIONAL CHECK OF THE APU, NO DEFECTS NOTED. THE AIRCRAFT WA S APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002022600024 20020226 00024 NM 2002 2 26 SWAA020409 1 20020222 A 2560 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE IN AFT CABIN. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002022600025 20020226 00025 NM 2002 2 26 SWAA020410 1 20020221 A 2560 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT FWD ENTRY LOWER LAV WALL. REMOVED AND REPLACED LE NS PER MM. 2 L 7 2 4F RT A16WE 2002022600026 20020226 00026 2002 2 26 SWAA020412 4 20020222 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 780SW 27885 FWD ENTRY DOOR EMERGENCY EVAC SLIDE DEPLOYED AT GATE. REMOVED AND REPLACED SLIDE AND CASE PER MM. 2 L 7 2 4F RT A16WE 2002022600027 20020226 00027 NM 2002 2 26 SWAA020413 1 20020223 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 728SW 27860 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED AT ROW'S 5, 11, 15 AND 20. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002022600028 20020226 00028 NM 2002 2 26 SWAA020414 1 20020222 A 5240 6552873 SKIN BOEING 737 7373A4 1384585 NM AFT ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA T1. 2 L 7 2 4F RT A16WE 2002022600029 20020226 00029 NM 2002 2 26 SWAA020415 1 20020223 A 5520 65C25745 ELEVATOR BOEING 737 7373H4 1384600 NM RH ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR DELAMINATED INBD OF T/E. REPAIRED ELEVATOR PER SRM. 2 L 7 2 4F RT A16WE 2002022600030 20020226 00030 NM 2002 2 26 SWAA020416 1 20020224 A 5320 BAC1490 STIFFENER BOEING 737 7373H4 1384600 NM FWD CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED D CHECK, FOUND STIFFENER CRACKED AT BS 328, WL 199 AND LBL 50. REMOVED AND REPLACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2002022600031 20020226 00031 NM 2002 2 26 SWAA020418 1 20020224 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 18L BETWEEN BS 779 AND BS 794, AND STR 20R BET WEEN BS 772 AND BS 785. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002022600032 20020226 00032 SO 2002 2 26 C2XA02IA040 1 20020222 A 2150 8152402 ACM EMB 145 EMB145ER 3260211 SO A/C BAY FAILED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 17928 145007 IAH- THE CREW NOTED WHITE SMOKE IN THE COCKPIT DURING PARKING WITH NR 1 ENGINE AND APU RUNNING, (NO WARNINGS). MAINTEN ANCE REMOVED AND REPLACED NR 1 ACM, PERFORMED A OPERATIONAL CHECK OF THE AIR CONDITIONING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002022600033 20020226 00033 2002 2 26 SWAA020400 4 20020220 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002022600034 20020226 00034 NM 2002 2 26 SWAA020403 1 20020221 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD CARGO COMPT DOOR CUTOUT AT BS 480 + 15', STR 22R. REPAI RED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002022600035 20020226 00035 NM 2002 2 26 SWAA020404 1 20020221 A 5241 6545871 FRAME BOEING 737 7373H4 1384600 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED ADJACENT TO STR 12R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002022600036 20020226 00036 NM 2002 2 26 SWAA020405 1 20020221 A 5230 6549889 FRAME BOEING 737 7373H4 1384600 NM FWD CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO COMPT DOOR FWD FRAME CRACKED. REPAIRED FRAME PER SB 737-52A1100. 2 L 7 2 4F RT A16WE 2002022600037 20020226 00037 NM 2002 2 26 SWAA020406 1 20020221 A 5241 6545871 SKIN BOEING 737 7373H4 1384600 NM AFT SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED 1/2D CHECK, FOUND AFT SVC DOOR OUTER SKIN CRACKED AT FWD EDGE ABOVE BOTTOM HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002022600038 20020226 00038 NM 2002 2 26 SWAA020407 1 20020221 A 5242 6557624 FRAME BOEING 737 7373H4 1384600 NM E/E BAY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED 1/2D CHECK, FOUND E/E BAY DOOR FRAME CRACKED. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002022600039 20020226 00039 NM 2002 2 26 SWAA020408 1 20020221 A 5310 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED 1/2D CHECK, FOUND E/E BAY FRAME CRACKED AT BS 328, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002022600040 20020226 00040 SO 2002 2 26 C2XA02IA041 1 20020222 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO LT MLG FAILED A C2XA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 SW 27 11539 145536 IAH- DURING FLIGHT 3628, ON APPROACH THE CREW NOTED THAT THE AIR/GND FAIL. THE CREW DECLARED EMERGENCY AND PERFORMED A EMERGENCY DESCENT WHILE ON APPROACH. AFTER LANDING IT WAS NOTED THAT THE SPOILER INOP, LEFT REVERSER INOP. MAINTENANC E REMOVED AND REPLACED THE NR 1 WEIGHT ON WHEELS PROX SWITCH, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002022600041 20020226 00041 NM 2002 2 26 CALA0200087 1 20020222 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 663.75, LBL 65. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002022600042 20020226 00042 NM 2002 2 26 CALA0200091 1 20020223 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND TWO FLOOR SUPPORTS CORRODED AT STA 986-1006. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-1 0-02. 2 L 7 2 4F RT A16WE 2002022600043 20020226 00043 NM 2002 2 26 CALA0200092 1 20020223 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A RT AND LT LAV FLOOR SUPPORT CORRODED AT STA 994, RBL 14 TO RBL 44, AND LBL 14 TO LBL 44. THE FLOOR S UPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002022600044 20020226 00044 NM 2002 2 26 CALA0200093 1 20020224 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1006-1016, LBL 7 AND RBL 7. THE FLOOR SUPPORTS WERE REMOVED AND REPLACE D IAW SRM 51-02-01. 2 L 7 2 4F RT A16WE 2002022600045 20020226 00045 NM 2002 2 26 CALA0200095 1 20020224 A 5753 COLLAR BOEING 737 7373T0 1384582 NM FLAP FAIRING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 FLAP FAIRING HORSE COLLAR. A NEW COLLAR WAS INSTALLED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2002022600046 20020226 00046 SO 2002 2 26 CHQ000120 1 20020222 A 2760 WARNING SYSTEM EMB 145 EMB145 3260210 SO COCKPIT MALFUNCTIONED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 375 145345 CREW REPORTS SPOILER FAIL MESSAGE ON EICAS, ABORTED TAKEOFF. SPOILER DEPLOYED, MESSAGE WENT OUT. ATTEMPTED ANOTHER TAK EOFF, NO PROBLEMS NOTED. 2 L 7 2 4F RT T00011AT 2002022600048 20020226 00048 EU 2002 2 26 CX7A194J 1 20020219 A 2613 1734362450 WARNING LIGHT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE HAMSTD 14RF 14RF19 NE COCKPIT FALSE INDICATION A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 303CE 340B194 RT TAIL PIPE HOT LIGHT ON T/O. NO TAIL WIND, ABORTED, REDUCED POWER, LIGHT WENT OUT. RAIN AND MOISTURE PREVAILED IN TH E AREA. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P11NE 2002022600049 20020226 00049 EU 2002 2 26 DHL2002366001 1 20020216 A 3040 CONVERTER AIRBUS 300 A300B4203 3930306 EU WINDSHIELD WIPER FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 366DH 249 CAPTS WIPER (WINDSHIELD) INOP. REMOVED AND REPLACED CAPTS WINDSHIELD WIPER MECH-CONVERTER IAW DHL A300 MM 30-41-12. 2 L 7 2 4F RT A35EU 2002022600050 20020226 00050 NM 2002 2 26 DHL2002721001 1 20020223 A 3040 WINDSHIELD WIPER BOEING 727 727228 1384083 NM WINDSHIELD OUT OF ADJUST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 721DH 19545 WINDSHIELD WIPER INOP. ADJUSTED WIPER TENSION PER 30-20-0, CHECKS GOOD. 2 L 7 3 4F RT A3WE 2002022600051 20020226 00051 NM 2002 2 26 DHL2002746003 1 20020221 A 2612 POWER UNIT BOEING 727 727224 1384076 NM APU FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 746DH 22252 APU WILL NOT FIRE TEST. REMOVED AND REPLACED APU OPERATING POWER UNIT, OP TEST OF FIRE TEST GOOD. 2 L 7 3 4F A3WE 2002022600052 20020226 00052 NM 2002 2 26 DHL2002746004 1 20020224 A 2440 WIRE BOEING 727 727224 1384076 NM EXTERNAL POWER LOOSE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 746DH 22252 DMI 8618 ENGINE FIRE WARNING SELF TEST INOP. FOUND LOOSE WIRE AT EXTERNAL POWER T/R C/B. SYSTEM CHECKS NORMAL IAW 24-4 0. 2 L 7 3 4F A3WE 2002022600053 20020226 00053 WP 2002 2 26 DHL2002801006 1 20020221 A 2612 FIRE DETECTOR DOUG DC8 DC873F 302199F WP NR 2 ENGINE FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 NR 2 ENG B-LOOP WON'T TEST. NR 2 ENG A-LOOP CHECKS GOOD. INSPECTED WIRING PER DC8 W/D 26-10-01, NO DEFECTS FOUND. REM OVED AND REPLACED NR 2 ENGINE FIRE DETECTOR UNIT IAW DACO MM 26-10-4. NR 2 FIRE WARNING TESTS GOOD. 2 L 7 4 4F RT 4A25 2002022600072 20020226 00072 NM 2002 2 26 DL72E020201 1 20020219 A 1430 65162221 BOLT BOEING 727 727247 138408F NM L/E SLAT BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 INSPECTION OF THE NR 3 LEADING EDGES SLAT ON THE LT WING PER AD BAC S/B 727-57-171 REVEALED A BROKEN BOLT COMMON TO THE DOWNSTOP FITTING ON THE OUTBOARD SLAT TRACK. THE ENTIRE SET OF SLATS ON THE LT WING WAS MODIFIED PER THE REQUIREMENTS O F THE S/B. THE WORK WAS DOCUMENTED PER ER/A 382632-14AD, REV A. 2 L 7 3 4F A3WE 2002022600073 20020226 00073 NM 2002 2 26 DL72L020031 1 20020110 A 5522 SKIN BOEING 727 727232 1384082 NM ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 FOUND ON B1 LETTER CHECK RT ELEVATOR LOWER SKIN IS CRACKED FWD OF TAB. REPAIRED PER B-727 DRD 55-20-3D FIG 4. 2 L 7 3 4F A3WE 2002022600074 20020226 00074 NM 2002 2 26 DL72L020032 1 20020109 A 5720 AND101341604 STIFFENER BOEING 727 727232 1384082 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 L/E SPAR STIFFENER CRACKED AT NR 7 SLAT I/B TRACK I/B SIDE. REPLACED STIFFENER PER M/M. 2 L 7 3 4F A3WE 2002022600075 20020226 00075 NM 2002 2 26 DL72L020035 1 20020110 A 5320 651751738 BEAM BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 INSPECTION OF THE RT VENTRAL STAIRWAY TORQUE BOX STRUCTURE PER AD 94-07-08 AND BAC S/B 727-53-0129 REVEALED TYPICAL CRAC KS IN THE FS 1263 AND 1273 HORIZONTAL BEAM CAPS. THE CRACKED MEMBERS WERE REMOVED AND NEW PARTS INSTALLED PER ER/A 3824 33-14AD. 2 L 7 3 4F A3WE 2002022600076 20020226 00076 NM 2002 2 26 DL72L020038 1 20020111 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION BETWEEN FS 1030 & 1050 AT STRINGER 28L. THE CORROSION WAS REMOVED WITH A 16 X 4 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH A DOUBLER PER ER/A 382438-14, REV A. 2 L 7 3 4F A3WE 2002022600077 20020226 00077 NM 2002 2 26 DL72L020127 1 20020201 A 2612 8928090400 CONTROLLER BOEING 727 727232 1384082 NM NR 1 ENGINE MALFUNCTIONED A DALA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 512DA 21314 090501 NR 1 ENG FIRE HANDLE ILLUMINATED AFTER LANDING. C/W EMERGENCY PROCEDURES AND LIGHT WENT OUT. THE LIGHT CAME BACK ON SE VERAL TIMES. REPLACED FIRE DETECTION CONTROLLER. 2 L 7 3 4F A3WE 2002022600078 20020226 00078 NE 2002 2 26 DL72L020154 2 20020208 A 7200 JT8D15AHK ENGINE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 FAILED A DALA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 512DA 74347 21314 687605 THROUGH CLIMB NR 2 ENGINE THUMPED, EPR WENT TO 0.00, EGT ROSE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002022600079 20020226 00079 NM 2002 2 26 DL72L020199 1 20020218 A 2120 ODOR BOEING 727 727232 1384082 NM COCKPIT DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 504DA 21306 IN FLIGHT NOTICED A FAINT ELECTRICAL SMELL. AFTER LANDING NOTICED DRAIN MAST C/B POPPED. NO SMELL WHEN MTC ARRIVED. O PENED C/B PANELS IN C/P ALL OK. RAN PACKS WITH ENGINES AND APU, ALL OK. REMOVED SEVERAL OVERHEAD PANELS AND TURNED ON ALL C/P LIGHTING, ALL OK. OPERATED DRAIN MAST HEATER APPROX 1 HR C/B STAYED IN. NO SMELL COULD BE DUPLICATED. 2 L 7 3 4F A3WE 2002022600080 20020226 00080 NM 2002 2 26 DL72S020051 1 20020115 A 2560 BATTERY PACK BOEING 727 727232 1384082 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 517DA 21433 MCO- AFT F/A FLASHLIGHT INOP. REPLACED BATTERY PACK AND TAMPER STRAP. 2 L 7 3 4F A3WE 2002022600081 20020226 00081 NM 2002 2 26 DL72S020069 1 20020119 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 518DA 21469 OVERWING EMERGENCY EXIT SIGN ILLUM, INOP SEAT LOC 22A. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 2002022600082 20020226 00082 NM 2002 2 26 DL72S020097 1 20020126 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 519DA 21470 FIRST CLASS EXIT LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2002022600083 20020226 00083 NM 2002 2 26 DL72S020114 1 20020131 A 3350 BATTERY PACK BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8890Z 21859 DURING S/C FOUND FWD LEFT DOOR OVERHEAD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED LIGHT ASSEMBLY AND BATTERY PACK. CHECKS GOOD. 2 L 7 3 4F RT A3WE 2002022600084 20020226 00084 NM 2002 2 26 DL72S020115 1 20020131 A 3350 90052 BATTERY PACK BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8875Z 21293 EMERGENCY LIGHT ABOVE SEAT 3B WOULD NOT COME ON. REPLACED BATTERY AND BATTERY RACK. 2 L 7 3 4F RT A3WE 2002022600085 20020226 00085 NM 2002 2 26 DL72S020116 1 20020131 A 3350 900835A BATTERY BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8875Z 21293 EMERGENCY LIGHTS ABOVE SEAT 3B WOULD NOT COME ON. REPLACED BATTERY. 2 L 7 3 4F RT A3WE 2002022600086 20020226 00086 NM 2002 2 26 DL72S020128 1 20020202 A 4920 APU BOEING 727 727225A 1384077 NM APU BAY LEAKING A DALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 8873Z 40351 21291 36433 AFTER TAKEOFF, SMOKE WAS NOTICED IN THE CABIN. REPLACED APU FOR LEAKING OIL. 2 L 7 3 4F RT A3WE 2002022600087 20020226 00087 NM 2002 2 26 DL72S020133 1 20020202 A 4920 656740214 APU BOEING 727 727232 1384082 NM APU BAY MALFUNCTIONED A DALA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 519DA 53326 21470 35826 ON APU SHUTDOWN FOUND APU EXHAUST FIRE OVER RIGHT WING COULD NOT PUT OUT HAD TO CALL FIRE DEPT TO PUT OUT FIRE. ALSO, F IRE BLISTERED WING TO FUSELAGE PANEL ABOVE APU EXHAUST ON FUSELAGE. FOUND APU BAD, REPLACED SAME. 2 L 7 3 4F A3WE 2002022600088 20020226 00088 NM 2002 2 26 DL72S020136 1 20020204 A 3350 LIGHT BOEING 727 727232 1384082 NM L1 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 533DA 22046 EMERGENCY EXIT SIGN AT L1 DOOR INOP. REPLACED LIGHTS ASSY AND BATTERIES, CHECKS OK. 2 L 7 3 4F A3WE 2002022600089 20020226 00089 NM 2002 2 26 DL72S020144 1 20020205 A 3350 POWER SUPPLY BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8890Z 21859 AFT SEAT ROWS EMERGENCY LIGHTS INOP. REPLACED EMERGENCY POWER SUPPLY M9027. 2 L 7 3 4F RT A3WE 2002022600090 20020226 00090 NM 2002 2 26 DL72S020149 1 20020207 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 531DA 21814 EMERGENCY LIGHT ABOVE SEAT 3B INOP. REPLACED BATTERY. 2 L 7 3 4F A3WE 2002022600091 20020226 00091 NM 2002 2 26 DL72S020163 1 20020209 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 ON LAYOVER FOUND EXTERIOR LIGHT FLASHING LEFT AFT FUSELAGE EMERGENCY LIGHT. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2002022600092 20020226 00092 NM 2002 2 26 DL72S020164 1 20020209 A 3350 1102831 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 519DA 21470 ON LAYOVER FOUND EMERGENCY LIGHT IN AFT STAIRWAY INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2002022600093 20020226 00093 NM 2002 2 26 DL72S020166 1 20020210 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 546DA 22677 ON L/O CHECK WHILE PERFORMING EMERGENCY LIGHT CHECK, CEILING MOUNTED LIGHT AT ROW 13 INOP. REPLACED BATTERIES IN LIGHT ASSEMBLY, OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 2002022600095 20020226 00095 NM 2002 2 26 DL72S020181 1 20020213 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 531DA 21814 DURING L/O FOUND 1ST CLASS OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY. 2 L 7 3 4F A3WE 2002022600096 20020226 00096 NM 2002 2 26 DL72S020195 1 20020216 A 3350 RPS1 POWER SUPPLY BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8891Z 21860 ON L/O FOUND FC EMERGENCY LIGHTS WOULD NOT TEST. REPLACED PWR SUPPLY. 2 L 7 3 4F RT A3WE 2002022600097 20020226 00097 WP 2002 2 26 MWEA020136 1 20020223 A 5310 39203122 FRAME DOUG DC9 DC932 3022066 WP STATION 718 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 RIGHT FUSELAGE FRAME AT STATION 718 IS CRACKED (REF WI 3673). -- INSTALLED 7075-T651.375 DOUBLER ON STATION 718 FRAME. REQUIRES DOUBLER INSTALLATION PER SERVICE BULLETIN 53-100. 2 L 7 2 4F A6WE 2002030400190 20020304 00190 NM 2002 3 4 F3LA200200059 1 20020224 A 3397 WIRE BOEING 737 737228 13844AG NM CABIN CHAFED A F3LA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 03 237TR 22 23007 DURING SERVICE CHECK, MAINTENANCE REPORTED L1 AND R1 DOOR EMERGENCY EXIT SIGNS AND FWD SECTION OF EMERGENCY FLOOR PATH L IGHTING INOPERATIVE. REPLACED POWER SUPPLY UNIT AND BATTERY PACK, WHICH DID NOT CORRECT PROBLEM. FERRIED AIRCRAFT TO D EN FOR REPAIR. FOUND CHAFED WIRING UNDER SEAT ROW 5 DEF, WHICH HAD CAUSED THE FUSE TO BLOW AT THE FWD EMERGENCY LIGHT B ATTERY CHARGER. REPAIRED WIRING AND SYSTEM CHECKED OKAY. 2 L 7 2 4F RT A16WE 2002022600102 20020226 00102 EA 2002 2 26 COMA0260115 1 20020225 A 5300 601R431143 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FS349 AT RBL27 INCORRECT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 931CA 17207 7037 THE INBOARD FLANGE OF A BRACKET ASSEMBLY HAS SHORT EDGE DISTANCE ON THE FASTENER COMMON WITH THE FLOOR BEAM AT FS349 RBL 27.FABRICATED AND INSTALLED A NEW BRACKET I/A/W WVAC EO 601R-53-2991. 2 L 7 2 4F RT A21EA 2002022600104 20020226 00104 EA 2002 2 26 COMA0260116 1 20020223 A 2410 IDG CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 01 959CA 7116 FLIGHT 5992 #2 GENERATOR FAILED DURING T/O.SERVICED THE R/H IDG TO PROPER OIL LEVEL. OPRATIONAL CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2002022600105 20020226 00105 EA 2002 2 26 COMA0260117 1 20020223 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 735CA 11685 7267 FLIGHT 5777 LT AND RT MLG WOULD NOT LOCK UP.REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2002022600108 20020226 00108 EA 2002 2 26 COMA0260118 1 20020223 A 2750 D3899926WB355N CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA R/H CONTAMINATED A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 978CA 7158 FLIGHT 5967 AILERON AND RUDDER TRIM WENT 80 DEGREES OUT OF TOLERANCE.REPLACED THE R/H FLAP POSITON TRANSMITTER WIRING CO NNECTOR. 2 L 7 2 4F RT A21EA 2002030400191 20020304 00191 NM 2002 3 4 F3LA200200060 1 20020222 A 5320 INTERCOSTAL BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED FLOOR INTERCOSTAL IN AFT GALLEY ENTRY CORRODED STA 957, BL 16L TO BL 42L. FABRICA TED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-10-2 AND 51-30-2. 2 L 7 2 4U RT A16WE 2002030400193 20020304 00193 NM 2002 3 4 F3LA200200061 1 20020222 A 5320 INTERCOSTAL BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 794, STR 27-R CORRODED. FABRICATED AND REPLACED INTERCOSTAL PE R SRM 51-30-2 AND 51-20-1. 2 L 7 2 4U RT A16WE 2002022600115 20020226 00115 WP 2002 2 26 CNMA200200002 1 20020221 A 3350 582223 POWER SUPPLY DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CNMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 540AX 46595 EMERGENCY EXIT LIGHT AT R4 DOOR CAME ON AFTER LANDING REMOVED AND REPLACED EMENGENCY LIGHT POWER SUPPLY OPS CHECKED PE R DC-10 MM 33-51 2 L 7 3 4F A22WE 2002022600116 20020226 00116 EU 2002 2 26 AWXA200200166 1 20020122 A 5320 D53112818 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 271 YWG - MAJOR REPAIR - "C" - DURING C-08 CHECK CORROSION WAS FOUND ON FORWARD AND AFT FLOOR SUPPORT IN FORWARD CABIN AT Y2 54, FR 15-19. MAINTENANCE CLEANED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER SRM 53-11-14; REMOVED CORRODED FLO OR SUPPORT; FABRICATED NEW FLOOR SUPPORT AND INSTALLED REPAIRS IAW DWG D53112818 AND SRM 51-42-11 PG.1, PARA 5. 2 L 7 2 4F RT A28NM 2002022600117 20020226 00117 EU 2002 2 26 AWXA200200167 1 20020125 A 5320 D53472089 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 271 YWG - MAJOR REPAIR - "C" - DURING C-08 CHECK CORROSION WAS FOUND AROUND SCREW HOLES ON FLOOR SUPPORT AT Y1162R, BETWEEN FR 68 & 69. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT Y1162R, BETWEEN FR 68 & 69; FABRICATED A NEW FLOOR SUPPORT AND INSTALLED REPAIRS IAW DWG D53472089. 2 L 7 2 4F RT A28NM 2002022600118 20020226 00118 NM 2002 2 26 AWXA200200168 1 20020211 A 5330 6552988 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - "C" - DURING C-13 CHECK A 1/8" CRACK WAS FOUND ON THE FUSELAGE SKIN OF THE L2 DOOR UPPER HINGE CUTO UT AT THE FWD EDGE BS 950. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN AND PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CON TAINED. FABRICATED REPAIR DOUBLER AND 2 EACH FILLERS AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01, PG 210-212. 2 L 7 2 4F RT A16WE 2002022600119 20020226 00119 NM 2002 2 26 AWXA200200169 1 20020212 A 5315 654681718 ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - "C" - DURING C-13 CHECK A 1/2" CRACK WAS FOUND ON SILL ANGLE AT BS 520, WL 208, RBL 64. MAINTENANCE REMOVED DAMAGED ANGLE AT BS 520, WL 208, RBL 64; FABRICATED A NEW ANGLE, SPLICE STRAP, AND SPLICE CHANNEL; AND INSTALLE D REPAIR PARTS IAW AWA ER 03-5300-02053-GF1. 2 L 7 2 4F RT A16WE 2002022600120 20020226 00120 NM 2002 2 26 AWXA200200174 1 20020208 A 5230 6547952134 FRAME BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24960 MCN - MAJOR REPAIR - "C" - DURING C-10 CHECK A CRACK WAS FOUND ON FWD LOWER CORNER OF AFT CARGO DOOR BS 795.5. MAINTENAN CE REMOVED & REPLACED FWD LOWER CORNER FRAME OF AFT CARGO DOOR IAW 737-300 SRM 51-40-02, PG. 38, 51-10-02, PG. 15-16, 51 -40-02, PG. 3, AND BOEING DWG #65-47952 2 L 7 2 4F RT A16WE 2002022600121 20020226 00121 NM 2002 2 26 AWXA200200175 1 20020211 A 5522 65C2574675 SKIN BOEING 737 7373S3 1384711 NM GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - MAJOR REPAIR - "C" - DURING C-10 CHECK A GOUGE WAS FOUND ON THE LOWER LEADING EDGE OF THE L/H ELEVATOR JUST INBOAR D OF THE #6 HINGE. MAINTENANCE REMOVED DAMAGE AREA AND APPLIED HONEYCOMB REPAIR PLY AT ELEVATOR STA 210.5 IAW B737-300 S RM 51-70-17, AND AWA ER 03-5521-02054-GF1. 2 L 7 2 4F RT A16WE 2002022600122 20020226 00122 NM 2002 2 26 AWXA200200176 1 20020216 A 5230 65917001053 FRAME BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - MAJOR REPAIR - "C" - DURING C-10 CHECK A CRACK WAS FOUND ON FWD UPPER CORNER OF AFT CARGO DOOR UNDER PULLY BRACKET AT BS 795.5. MAINTENANCE REMOVED & REPLACED FWD UPPER CORNER FRAME OF AFT CARGO DOOR IAW 737-300 SRM 51-40-02, PG. 38, 51-40-5, PG. 1-2, 51-40-02, PG. 3, AND BOEING DWG #65-47952 2 L 7 2 4F RT A16WE 2002022600123 20020226 00123 NM 2002 2 26 AWXA200200177 1 20020226 A 3350 BMS13311122 WIRE BOEING 737 7373S3 1384711 NM ZONE 200 CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 YVR - EEL - "C" - DURING C-15 CHECK EMERGENCY ESCAPE PATH LIGHTING MAIN WIRE HARNESS WAS FOUND DAMAGED AT SEVERAL PLACES . MAINTENANCE REPAIRED DAMAGED WIRING WITH ENVIRONMENTAL SPLICES IAW SWPM 20-30-12, PG 12, ITEM 6,B. FUNCTIONAL TEST OF ESCAPE PATH LIGHT TO BE ACCOMPLISHED IAW AWA T/C A1C33006. 2 L 7 2 4F RT A16WE 2002030400195 20020304 00195 NM 2002 3 4 F3LA200200063 1 20020222 A 5315 FLOORBEAM BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 986 CORRODED AT BOTTOM SURFACE AT FASTENERS THROUGH FLOORBOARDS. ALSO SHOWS EVIDENCE OF CORROSION ON TOP OF BEAM FROM BL 0 TO RBL 54 AS VIEWED FROM BELOW. REPLACED FLOORBEAM CAP AT ST A 986 PER SRM 53-10-9. 2 L 7 2 4U RT A16WE 2002030400194 20020304 00194 NM 2002 3 4 F3LA200200062 1 20020222 A 5320 INTERCOSTAL BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT STA 847, BL 16-R. FABRICATED AND INSTALLED REPLACEMEN T INTERCOSTAL PER BOEING DRAWING 65-47957, SRM 51-10-2 AND SRM 51-30-2. 2 L 7 2 4U RT A16WE 2002022600125 20020226 00125 NM 2002 2 26 TSAA0233030 1 20020205 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 4 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002022600130 20020226 00130 SO 2002 2 26 ASOA02013 1 20020103 A 5320 12046156001 BUTTSTRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 283AS 120236 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT BUTT STRAP BETWEEN FRAME 13 AND STATION 6653.1. MAIN TENANCE REMOVED THE CORRODED BUTT STRAP AND REPLACED IT WITH A NEW ONE IAW SRM 51-21-02. (M) 2 L 7 2 4T RT A31SO 2002022600131 20020226 00131 SO 2002 2 26 ASOA02014 1 20020103 A 5313 12026335014 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 283AS 120236 DURING C-CHECK INSPECTION IN BNA, STRINGER 21 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 9 AND 13. MAINTENANCE REMOV ED AND REPLACED THE CORRODED STRINGER IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002022600132 20020226 00132 SO 2002 2 26 ASOA02015 1 20020111 A 5713 12016085002 STRINGER EMB 120 EMB120RT 3260202 SO WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 257AS 120126 DURING HANGAR MAINTENANCE IN BNA, THE RIGHT MOST INBOARD FORWARD STRINGER WAS FOUND CRACKED IN TWO PLACES AT THE FUEL PA NEL JUST INBOARD OF THE NACELLE. MAINTENANCE REPAIRED THE CRACKED STRINGER IAW SRM 57-20-03. THE DAMAGED SECTION WAS C UT OUT AND A SPLICE WAS INSTALLED REFERENCING SRM 51-22-00. NO LEAKS WERE NOTED. (M) 2 L 7 2 4T RT A31SO 2002022600133 20020226 00133 SO 2002 2 26 ASOA02016 1 20020112 A 3350 D36804001 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 261AS 120141 FLT 4084 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTING BATTERY WAS FOUND BE INOPERATIVE, CAUSING THE EMERGEN CY FLOOR LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERIES IN THE NR 2 AND NR 3 POSITIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002022600134 20020226 00134 SO 2002 2 26 ASOA02017 1 20020113 A 3350 F02A250V1A FUSE EMB 120 EMB120RT 3260202 SO CABIN LOOSE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 281AS 120224 DURING A HANGAR INSPECTION IN TXK, THE AFT EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REINSERTED A LOOSE FUSE INTO THE BAYONET CONNECTOR ON THE AFT TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002022600135 20020226 00135 SO 2002 2 26 ASOA02018 1 20020113 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 281AS 120224 FLT 4903 - DURING GROUND INSPECTION IN DFW, THE EMERGENCY LIGHTS AT EXIT ROW 5 WERE FOUND TO BE INOPERATIVE. MAINTENANC E FOUND THE EMERGENCY BATTERY PACK AT ROW 5 BAD AND REPLACED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M ) 2 L 7 2 4T RT A31SO 2002022600136 20020226 00136 EA 2002 2 26 ASOA02019 1 20020113 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 866AS 7517 FLT 4669 - DURING GROUND INSPECTION IN ATL, THE LEFT MIDDLE OVERWING EMERGENCY EXIT LIGHT WAS FOUND BURNED OUT. MAINTEN ANCE REMOVED AND REPLACED THE LEFT MIDDLE OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERV ICE. (M) 2 L 7 2 4F RT A21EA 2002022600147 20020226 00147 NM 2002 2 26 2002F00114 1 20020105 A 5330 SKIN PANEL BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 359QS 19007 FOUND FUSELAGE SKIN PANEL CORRODED AT STATION 320 STRINGER 19R. (M) 2 L 7 3 4F A3WE 2002022600148 20020226 00148 NM 2002 2 26 2002F00115 1 20020105 A 5311 FRAME BOEING 727 72721 1384003 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 359QS 19007 FOUND LOWER END OF FRAME AND BRACKET AT STATION 312 RBL 40 EXFOLIATED. (M) 2 L 7 3 4F A3WE 2002022600149 20020226 00149 NM 2002 2 26 2002F00116 1 20020104 A 5754 WEDGE BOEING 727 72721 1384003 NM L/E FLAP DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 356QS 19258 FOUND RIGHT WING OUTBOARD FORWARD FLAP TRAILING EDGE WEDGE COMPOSITE HAS DELAMINATION AND APPROXIMATELY 75 PERCENT OF TH E SECTION OF WEDGE IS MISSING. (M) 2 L 7 3 4F A3WE 2002022700001 20020227 00001 NM 2002 2 27 CALA0200098 1 20020225 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 380-400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND A 2" CRACK IN SHEAR WEB UPON REMOVAL OF UPPER ANGLE AT STA 380-400, BL 0. THE WEB WAS REMOVED AND REPLA CED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002022700002 20020227 00002 NM 2002 2 27 CALA0200099 1 20020225 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND FLOORBEAM CORRODED ABOVE AND BELOW NUT CLIP HOLES AT STA 986, RBL 46 TO LBL 46. THE FLOORBEAM WAS REPAI RED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2002022700003 20020227 00003 NE 2002 2 27 NACA20020006 2 20020216 A 8530 356996 CYLINDER DOUG DC6 DC6B 3021712 WP PWA R2800 R2800* 52026 NE NR 4 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 AL 03 7919C 1621 1621 43554 P33313 SHUT DOWN NR 4 ENGINE AT 0735 ZULU DUE TO BACKFIRING. REPLACED NR 11 CYLINDER. 2 L 7 4 4R 4 R 6A4 5E8 2002022700004 20020227 00004 WP 2002 2 27 ARWA20020206 1 20020223 A 2161 CONTROLLER LKHEED 1011 1011385115 5265015 WP A/C BAY MALFUNCTIONED A ARWA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 19 308GB 193U1133 NR 1 PACK OVERHEAT, SMELLED SMOKE IN COCKPIT. RETURNED TO RAMP. RESET TEMPERATURE CONTROLLER NR 1 PACK, OPS CHECK NORM AL IAW MM 21-62-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A23WE 2002022700005 20020227 00005 NM 2002 2 27 AWXA200200170 1 20020213 A 5315 6549884 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - C - DURING C-13 CHECK CORROSION WAS FOUND ON FLOORBEAM UPPER FLANGE AT BS 967, RBL 46. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER B737-300 SRM 53-60-51 PG 107-110. REMOVED DAMAGED FLOORBEA M INTERCOSTAL AT BS 957 BETWEEN RBL 18-45; FABRICATED A NEW FLOORBEAM, SHIM AND REPAIR DOUBLER; AND INSTALLED REPAIR PAR TS IAW B737-300 SRM 53-60-51 PG 102-110, 51-40-02 PG 10-11, 51-21-21 PG 702. 2 L 7 2 4F RT A16WE 2002022700006 20020227 00006 NM 2002 2 27 AWXA200200171 1 20020128 A 5320 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 LCQ - MAJOR REPAIR - C - DURING C-16 CHECK .500 INCH CRACK WAS FOUND ON STRINGER TIE AT BS 639, STR 2R. MAINTENANCE REM OVED CRACKED STRINGER TIE, FABRICATED A NEW STRINGER TIE AND INSTALLED REPAIR IAW B737-300 SRM 51-40-2 PG 64 AND 51-40-5 PG 1-8. 2 L 7 2 4F RT A16WE 2002022700007 20020227 00007 NM 2002 2 27 AWXA200200172 1 20020128 A 5320 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 LCQ - MAJOR REPAIR - C - DURING C-16 CHECK .500 INCH CRACK WAS FOUND ON STRINGER TIE AT BS 639, STR 4R. MAINTENANCE REM OVED CRACKED STRINGER TIE, FABRICATED A NEW STRINGER TIE AND INSTALLED REPAIR IAW B737-300 SRM 51-40-2, PG 64 AND 51-40- 5 PG 1-8. 2 L 7 2 4F RT A16WE 2002022700008 20020227 00008 NM 2002 2 27 AWXA200200173 1 20020209 A 5320 694143714 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 LCQ - MAJOR REPAIR - C - DURING C-16 CHECK .500 INCH CRACK WAS FOUND ON STRINGER TIE AT BS 663.75, STR 11L. MAINTENANCE REMOVED CRACKED STRINGER TIE, FABRICATED A NEW STRINGER TIE AND INSTALLED REPAIR IAW B737-300 SRM 51-40-2 PG 1-4 & 64. 2 L 7 2 4F RT A16WE 2002022700009 20020227 00009 EU 2002 2 27 AWXA200200178 1 20020224 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 646AW 271 YWG - EEL -C- DURING C-08 CHECK EMERGENCY ESCAPE PATH LIGHTING AT ROWS 13, 17, 19, 24 WERE FOUND INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 13WL IAW AMM 33-51-38-401, OPERATIONAL CHECK PERFORMED IAW T/C F1C33 301. 2 L 7 2 4F RT A28NM 2002022700010 20020227 00010 WP 2002 2 27 MWEA020138 1 20020227 A 5310 9919621501 FRAME DOUG DC9 DC932 3022066 WP STATION 598 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 COMPLY WITH CARRY OVER #2682. FRAME AT FUSELAGE STATION 598 IS CRACKED BETWEEN TWO FASTNERS IN LOWER POCKET BELOW LEFT C USP LINE. -- REMOVED AND REPLACED FRAME AT STATION 598. 2 L 7 2 4F A6WE 2002022700011 20020227 00011 WP 2002 2 27 MWEA020141 1 20020227 A 5520 591041212 SKIN DOUG DC9 DC932 3022066 WP RH ELEVATOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 RIGHT ELEVATOR OUTBOARD UPPER SKIN DAMAGED. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002022700012 20020227 00012 EU 2002 2 27 AWXA200200181 1 20020208 A 5311 D533723232000 FRAME AIRBUS 320 A320231 3930325 EU FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 271 YWG - MAJOR REPAIR - C - DURING C-08 CHECK TOOLING HOLES AT FR 38-40 LT TO RT WERE FOUND TO BE OVERSIZED. COLD EXPANDED THE HOLES PER SRM 51-48-00, MAINTENANCE DRILLED HOLES TO APPLICABLE DIAMETER, COUNTERSUNK HOLES TO A MAXIMUM OF 0.4MM, INSTALLED FASTENERS NAS1241AD8, AND MILLED RIVET HEADS FLUSH. REPAIR PERFORMED IAW AWA ER 26-5310-02045-JS1, DEVIATION 5. 2 L 7 2 4F RT A28NM 2002022700013 20020227 00013 SO 2002 2 27 C2XA02IA042 1 20020225 A 3230 23092900401 UPLOCK EMB 145 EMB145 3260210 SO RT MLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16963 145116 IAH- ON CLIMBOUT THE CREW NOTED THAT THE LANDING GEAR LEVER DISAGREE/UP POSITION/RIGHT MAIN NOT FULLY RETRACTED (AIRBORN E). THE CREW DECLARED EMERGENCY AND RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE UPLOCK BOX IN THE RIGHT MAIN LANDING GEAR WHEEL WELL, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED AN D THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002022700014 20020227 00014 SO 2002 2 27 C2XA02TY046 1 20020227 A 5315 14521699001 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14516 145323 TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND UNDER FLOOR SUPPORT CROSS MEMBER AT FR 20 ON THE LEFT OMEGA B EAM. MAINTENANCE CUT OUT DAMAGE AREA, FAB DOUBLER, SHIM AND EXTERNAL ANGLE. INSTALL THE REPAIR PIECES AND PROFILE ANGL E IAW 135/145 SRM 53-21-10, 51-40-02, CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETIO N OF INSPECTION. 2 L 7 2 4F RT TOOO11AT 2002022700015 20020227 00015 EU 2002 2 27 CHQ000123 1 20020226 A 3150 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU COCKPIT ACTIVATED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 150 150 OAT LIGHT CONFIG WARNING AND TCAS FAIL AFTER TAKEOFF. 2 L 7 2 4T RT A52EU 2002022700016 20020227 00016 NM 2002 2 27 DHL2002746005 1 20020224 A 2612 FIRE WARNING BOEING 727 727224 1384076 NM COCKPIT WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 746DH 22252 ALL THREE ENGINE FIRE WARNINGS WILL NOT TEST PROPERLY. FOUND THAT FIRE WARNING WILL NOT WORK WITH A/C POWER CABLE CONNE CTED. ASSIGNED DMI 8618 PER MEL 24-14. PLACARD INSTALLED. 2 L 7 3 4F A3WE 2002022700017 20020227 00017 NM 2002 2 27 DL72S020200 1 20020218 A 3350 S106 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 532DA 22045 ON L/O, FOUND EMERGENCY CEILING LIGHTS AT ROW 26 INOP. REPLACED BATTERY PACK, CHECKS GOOD. 2 L 7 3 4F A3WE 2002022700018 20020227 00018 NM 2002 2 27 DL72S020202 1 20020216 A 5320 STIFFENER BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 INSPECTION OF THE WL 283 FASTENER HOLES ON THE RBL & LBL 17.8 BEAMS OF THE FS 1183 BULKHEAD REVEALED TOOLING DAMAGE IN T HE TWO RT HOLES AND A CRACK INDICATION IN THE LOWER LT HOLE. THE INSPECTION WAS ACCOMPLISHED PER AD 99-18-05 AND BAC S/ B 727-53-0210. THE TOOLING DAMAGE HOLES WERE REAMED TO CLEAN UP THE DAMAGE AND THE CRACKED HOLE OVERSIZED WITH AN INSUR ANCE CUT. LARGER DIA BOLTS WERE INSTALLED PER ER/A. 2 L 7 3 4F A3WE 2002022700019 20020227 00019 NM 2002 2 27 DL72S020211 1 20020219 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 542DA 22391 ON EMERGENCY LIGHT TEST FOR NR 4 S/C THE LIGHT ABOVE R1 DID NOT ILLUMINATE. REPLACED BATTERIES LIGHT, NOW CHECKS NORMAL . 2 L 7 3 4F A3WE 2002022700020 20020227 00020 NM 2002 2 27 DL72W020025 1 20020109 A 5743 BEAM BOEING 727 727247 138408F NM RT WING WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 291WA 22109 FOUND ON F-2 LETTER CHECK, WEAR AT RT MLG WALKING BEAM I/B END. REPAIRED PER MM 57-43 000-8. 2 L 7 3 4F A3WE 2002022700021 20020227 00021 NM 2002 2 27 DL72W020041 1 20020111 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 294WA 22112 MID FIRST CLASS CEILING EXIT SIGN IDENTIFIER BATTERY PACK INOP. REMOVED AND REPLACED SAME. CHECKS GOOD. 2 L 7 3 4F A3WE 2002022700022 20020227 00022 NM 2002 2 27 DL72W020078 1 20020121 A 3350 1000677 LIGHT BOEING 727 727247 138408F NM L1 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 290WA 22108 EMERGENCY EXIT OVERHEAD LIGHT ABOVE L1 PASSENGER DOOR INOP. REPLACED EMERGENCY EXIT LIGHT ASSY. OPN NORMAL. 2 L 7 3 4F A3WE 2002022700023 20020227 00023 NM 2002 2 27 DL72W020087 1 20020123 A 5311 651631232 FRAME BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 293WA 22111 THE INBOARD FRAME OF THE FS 294.5 BULKHEAD WAS FOUND CRACKED AT RBL 12.5 AND WL 181. THE CRACK WAS 1 INCH LONG AND WAS REMOVED BY ROUTING OUT THE FRAME FLANGE. THE CHORD WAS REPAIRED WITH AND ALUMINUM EXTRUDED REPAIR ANGLE INSTALLED PER E R/A 382496-14, REV A. 2 L 7 3 4F A3WE 2002022700024 20020227 00024 NM 2002 2 27 DL72W020126 1 20020201 A 3230 656021132 ACCESSORY UNIT BOEING 727 727247 138408F NM E/E BAY MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 290WA 22108 LANDING GEAR WOULD NOT RAISE AFTER TAKEOFF. GEAR REMAINED DOWN. REPLACED LANDING GEAR ACCESSORY UNIT. 2 L 7 3 4F A3WE 2002022700025 20020227 00025 NM 2002 2 27 DL72W020134 1 20020203 A 7931 ST104Z TRANSMITTER BOEING 727 727247 138408F NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE FAULTY A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 296WA 22533 700703 NR 3 OIL PRESSURE INDICATION DROPPED TO 32 PSI WHEN TAKEOFF POWER APPLIED. TAKEOFF ABORTED AT 70 KTS, GROSS WEIGHT 162. 0. BRAKE COOLING IN NORMAL RANGE. REPLACED NR 3 ENGINE OIL PRESSURE TRANSMITTER, LEAK CHECKS OK. PRESSURE CHECKS NORM AL ON ENGINE RUN. 2 L 7 3 4F 4 F A3WE E2EA 2002022700026 20020227 00026 NM 2002 2 27 DL72W020141 1 20020205 A 5522 SKIN BOEING 727 727247 138408F NM ELEVATOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 DURING ACCOMPLISHMENT OF EO 4-57713-3AD ON SUBJECT ELEVATOR, FASTENERS HOLES THAT ATTACH THE UPPER SKIN PNLS TO THE REAR SPAR WERE FOUND OVERSIZED. REPAIR PER ER/A 410467-14AD. 2 L 7 3 4F A3WE 2002022700027 20020227 00027 NM 2002 2 27 DL72W020156 1 20020207 A 7120 65187228 MOUNT BOEING 727 727247 138408F NM NR 3 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 HFEC BOLT HOLE INSPECTION OF THE FWD ENGINE MOUNT ON THE NR 3 PYLON PER AD 97-05-08 INDICATED CRACKS IN HOLES -C- AND -D - OF BAC S/B 727-54A0010. THE HOLES WERE OVERSIZED WITH A .0312 INCH ADDITIONAL INSURANCE CUT TO REMOVE ALL CRACKS. LA RGER DIAMETER FASTENERS WERE INSTALLED IN THE REWORKED HOLES PER ER/A 382517-14AD, REV A. 2 L 7 3 4F A3WE 2002022700028 20020227 00028 NM 2002 2 27 DL72W020161 1 20020208 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 294WA 22112 DURING L/O FOUND FIRST CLASS OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2002030400196 20020304 00196 NM 2002 3 4 F3LA200200064 1 20020223 A 5330 SKIN BOEING 737 7372Y5 1384554 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED FUSELAGE SKIN RUBBED BY BELT 2 INCHES BELOW L-1 DOOR TOP SPIGOT (INTERIOR). PERFO RMED EDDY CURRENT INSPECTION OF L-1 DOOR TOP SPIGOT INTERIOR BONDED DOUBLER AND FOUND 2 CRACKS. REPAIRED DAMAGED AREA P ER EA 53-737-160. 2 L 7 2 4U RT A16WE 2002022700029 20020227 00029 NM 2002 2 27 DL733020059 1 20020118 A 5410 311A11112 BEAM BOEING 737 737347 1384647 NM NR1 & 2 PYLON CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 CORROSION WAS FOUND ON THE CROWN BEAM LUG BORES OF THE NR 1 AND NR 2 PYLONS. THE BORES WERE OVERSIZED AND REPAIR BUSHIN GS INSTALLED. THE DAMAGE WAS FOUND DURING INSPECTION AT HMV. 2 L 7 2 4F RT A16WE 2002022700030 20020227 00030 NM 2002 2 27 DL733020061 1 20020118 A 7120 654685014 SUPPORT FITTING BOEING 737 737347 1384647 NM ENGINE MOUNT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 FWD ENGINE MOUNT SUPPORT FITTING WAS FOUND WITH OVERSIZED MOUNT HOLES. REPAIR PER ER/A 410878-14AD. 2 L 7 2 4F RT A16WE 2002022700031 20020227 00031 NM 2002 2 27 DL733020062 1 20020118 A 7120 654685010 SUPPORT FITTING BOEING 737 737347 1384647 NM ENGINE MOUNT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 FWD ENGINE MOUNT SUPPORT FITTING WAS FOUND WITH OVERSIZED MOUNT HOLES. REPAIR PER ER/A 410877-14AD. 2 L 7 2 4F RT A16WE 2002030400197 20020304 00197 NM 2002 3 4 F3LA200200065 1 20020223 A 5320 STRAP BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED STRAP ALONG THE BOTTOM OF PRODUCTION BREAK AT STA 1016, STR 23-L TO 23-R CORRODED. REPLACED STRAP PER SRM 51-30-2 AND BOEING DRAWING 65-46568. 2 L 7 2 4U RT A16WE 2002022700032 20020227 00032 NM 2002 2 27 DL733020122 1 20020201 A 5314 65621258 KEELBEAM BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 CORROSION WAS FOUND ON THE LOWER KEEL CHORD AT FS 727 AND STR 27R. ADDITIONALLY, SEVERAL WEAR LOCATIONS WERE FOUND BETW EEN FS 727 AND FS 715 AND A CRACK WAS FOUND ON THE AFT END OF THE PART AT FS 727A. THE CORROSION WAS BLENDED AND THE CR ACK WAS CUT OUT AND TWO REPAIR ANGLES WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2002022700033 20020227 00033 NM 2002 2 27 DL733020135 1 20020201 A 5230 6546921528 DOOR FRAME BOEING 737 737347 1384647 NM CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 FWD CARGO DOOR ARRIVED IN THE SHOP DUE TO CRACKING FOUND IN THE LOWER FWD AND AFT CORNER FRAMES AS WELL AS THE FWD AND A FT SECTIONS OF THE LWD STOP BEAM. REPAIR PER ER/A 410793-14AD. 2 L 7 2 4F RT A16WE 2002022700034 20020227 00034 NM 2002 2 27 DL733020187 1 20020214 A 3260 WARNING LIGHT BOEING 737 73735B 13844BM NM COCKPIT FALSE INDICATION A DALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 221DL 23970 ON APPROACH TO LANDING HAD UNSAFE GEAR INDICATION. NO GREEN LIGHTS AND ONLY NOSE GEAR RED UNSAFE. JACKED AIRCRAFT AND CYCLED GEAR. UNABLE TO DUPLICATE. 2 L 7 2 4F RT A16WE 2002030400198 20020304 00198 NM 2002 3 4 F3LA200200066 1 20020223 A 5320 WEB BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED WEB AT STA 996 TO STA 1016, RBL 40, NEXT TO R2 DOOR CORRODED. FABRICATED AND INST ALLED REPLACEMENT WEB PER SRM 51-30-2. 2 L 7 2 4U RT A16WE 2002022700035 20020227 00035 NM 2002 2 27 DL733020193 1 20020215 A 2121 65771 FAN BOEING 737 7373B7 1384580 NM E/E BAY MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 951WP 22951 WHILE SITTING AT GATE NOTICED SMOKE/SMELL IN AFT CABIN. GROUND PERSONNEL STATED SMOKE CAME FROM EQUIP COOLING FAN EXHAU ST. MTC INSPECTED ALL AREAS WHERE EQUIP COOL AIR DRAWN WITH NO ABNORMALITIES. RAN ENGINES AND ALL ASSOCIATED SYSTEMS, NO TROUBLE FOUND. PULLED BOTH NORMAL AND ALTERNATE FANS TO INSPECT. NO TROUBLE FOUND. 2 L 7 2 4F RT A16WE 2002022700036 20020227 00036 NM 2002 2 27 DL733020205 1 20020216 A 3350 20131A BATTERY BOEING 737 73735B 13844BM NM CABIN DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 225DL 25069 EMERGENCY EVACUATION LIGHTING DIM IN CABIN AISLE BETWEEN ROWS 11 AND 24. REPLACED BATTERY FOR CABIN LIGHTING SYSTEM. 2 L 7 2 4F RT A16WE 2002022700037 20020227 00037 NM 2002 2 27 DL738020026 1 20020109 A 2421 761574B IDG BOEING 737 737832 13844CF NM NR 2 ENGINE FAILED A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 375DA 29623 NR 2 SOURCE LIGHT AND DRIVE LIGHT ILLUMINATED SIMULTANEOUSLY. ACCOMPLISHED POM PROCEDURES BRING APU ON LINE AND DISCONN ECTED NR 2 DRIVE. FOUND NR 2 IDG LOST ALL OIL AND SHAFT SHEARED. REMOVED AND REPLACED SAME. 2 L 7 2 4F RT A16WE 2002030400199 20020304 00199 NM 2002 3 4 F3LA200200067 1 20020223 A 5320 INTERCOSTAL BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 986 TO STA 1006, RBL 3, CORRODED. FABRICATED AND INSTALLED REP LACEMENT INTERCOSTAL PER SRM 51-30-2 AND EA 53-737-158. 2 L 7 2 4U RT A16WE 2002030400200 20020304 00200 NM 2002 3 4 F3LA200200068 1 20020223 A 5315 FLOORBEAM BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED TOP SURFACE OF FLOORBEAM AT STA 986 CORRODED. REPLACED FLOORBEAM CAP PER SRM 53-1 0-9. 2 L 7 2 4U RT A16WE 2002022700038 20020227 00038 NE 2002 2 27 DL738020129 2 20020202 A 7230 CASE BOEING 737 737832 13844CF NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE CRACKED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 27 3760C 201 30816 88789 LOST OIL NR 1 ENGINE MADE OFF SCHEDULED LANDING AT ORD. FOUND ENGINE STATOR GENERATOR HOUSING CRACKED. REPLACED SAME, RAN ENGINE CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002022700039 20020227 00039 NM 2002 2 27 DL738020145 1 20020206 A 2530 720775000 OVEN BOEING 737 737832 13844CF NM GALLEY MALFUNCTIONED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 3762Y 30817 ACRID ODOR IN FWD CABIN SMOKE OBSERVED BY F/A. RETURN FOR LANDING. CHECKED LIGHTING AND FWD CABIN, ALL CHECK OK. FOUN D F/C OVEN SMELL AS IF OVERTEMPED. REPLACED OVEN. 2 L 7 2 4F RT A16WE 2002030400201 20020304 00201 NM 2002 3 4 F3LA200200069 1 20020223 A 5320 PANEL BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLOSING PANEL AROUND NUT PLATE AT STA 789, RBL 27 TO RBL 34. REPLACE D CLOSING PANEL PER SRM 51-10-1. 2 L 7 2 4U RT A16WE 2002030100026 20020301 00026 NM 2002 3 1 2002UALA00283 1 20020215 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 MAJOR BS 854 RBL 54 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2002030700074 20020307 00074 NM 2002 3 7 2002UALA00287 1 20020218 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 MID CABIN STA 663.73 STRINGER CLIP IS CRACKED AT STRINGER 10L. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER CLIP AT S TATION 663.73, STRINGER 10L. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030100028 20020301 00028 NM 2002 3 1 2002UALA00288 1 20020218 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 FUSELAGE STATION 297 STRINGER 2L HAS DEEP GOUGE ON STRINGER. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002030100029 20020301 00029 NM 2002 3 1 2002UALA00289 1 20020218 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 BODY STATION 852 RBL 34 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2002030100030 20020301 00030 NM 2002 3 1 2002UALA00290 1 20020218 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 BODY STATION 796 LBL 11 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2002030400202 20020304 00202 NM 2002 3 4 F3LA200200070 1 20020223 A 5320 PANEL BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLOSING PANEL AROUND NUT PLATES AT STA 789, RBL 39 TO RBL 46. REPLAC ED CLOSING PANEL PER SRM 51-10-1. 2 L 7 2 4U RT A16WE 2002022700040 20020227 00040 NM 2002 2 27 DL73K020029 1 20020108 A 2170 V1211 COALESCER BAG BOEING 737 737247 138448D NM A/C BAY DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 242WA 23516 WITH POWER APPLIED THERE WAS A SMELL LIKE BURNING RUBBER. SMELL DISSIPATED WITH POWER BACK, NO INDICATIONS. RAN BOTH E NGS TO T/O POWER WITH PACKS ON, ANTI-ICE ON. CHECKED AIR MIX DISTRIBUTION PLENUM IN FWD B/B, NO CRACKS. REPLACED BOTH WATER SEPARATOR BAGS, LEAK CHECKS OK. 2 L 7 2 4F A16WE 2002022700041 20020227 00041 NM 2002 2 27 DL73K020045 1 20020112 A 3350 BPS73 CHARGER BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 312DL 23084 EMERGENCY SEAT LIGHTS INOP AT SEAT ROWS 5 TO 9. REPLACED BATTERY CHARGER. 2 L 7 2 4F RT A16WE 2002022700042 20020227 00042 NM 2002 2 27 DL73K020047 1 20020113 A 2613 WARNING SYSTEM BOEING 737 737232 1384475 NM COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 311DL 23083 LEFT WING BODY OVERHEAT LIGHT ON IN FLT. DIVERTED TO MCO. REPAIRING OVERHEAT SYSTEM. TRIED CONTROLLER AND OVERHEAD PA NEL, NO HELP. RE-INSTALLED ORIGINAL. INSPECTED FOR LEAKS, NONE FOUND. INSPECTED LOOPS FROM NR 1 ENGINE TO AC PACK BAY CONNECTORS. CHECKED LOOPS WITH BREAKOUT BOX. ALL TEST OK. RAN AIRCRAFT AT TAKEOFF POWER. OPS CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2002022700043 20020227 00043 NM 2002 2 27 DL73K020099 1 20020126 A 3350 1317 LIGHT BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 305DL 23077 OVERHEAD EMERGENCY FLOODLIGHT INOP AT SEAT 04C. RELAMPED. 2 L 7 2 4F RT A16WE 2002022700044 20020227 00044 NM 2002 2 27 DL73K020118 1 20020130 A 5311 FRAME BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 INSPECTION OF THE FS 178 BULKHEAD PER AD 2000-05-29, REVEALED A CRACK IN THE LT SIDE CHORD NEAR WL 207. THE DAMAGED SEC TION OF CHORD WAS CUT OUT AND A NEW SECTION SPLICED IN. THE WORK WAS ACCOMPLISHED IN ACCORDANCE WITH BAC S/B 737-53A117 3 AND ER/A 382503-14AD. 2 L 7 2 4F A16WE 2002022700045 20020227 00045 NM 2002 2 27 DL73K020119 1 20020131 A 5330 6545767152 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312DL 23084 AN EXISTING DOUBLER REPAIR WAS FOUND FOR REPAIR OF CRACK CUTOUT BELOW THE STRINGER 19L LAP JOINT AT FS 500. THE REPAIR DOUBLER WAS REMOVED FOR INSTALLATION OF A BETTER FATIGUE DESIGN REPAIR. THE EXISTING CUTOUT AND FASTENER HOLES WERE INS PECTED TO ENSURE NO CRACKS. A MORE FATIGUE FRIENDLY DOUBLER AND TRIPLER REPAIR WAS INSTALLED PER ER/A 382511-14, REV A. 2 L 7 2 4F RT A16WE 2002022700046 20020227 00046 NM 2002 2 27 DL73K020147 1 20020206 A 3350 1317 LIGHT BOEING 737 737247 138448D NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 375DL 23602 EMERGENCY LIGHT OVERHEAD SEAT ROW 2 DEF INOP. REPLACED BULB. 2 L 7 2 4F A16WE 2002022700047 20020227 00047 NM 2002 2 27 DL73K020155 1 20020206 A 5311 FRAME BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 THE LT SIDE CHORD OF THE FS 178 BULKHEAD WAS FOUND CRACKED AT WL 195. THE FLOOR WEBS AT WL 207 WERE ALSO FOUND CRACKED . THE CHORD WAS REPAIRED WITH REPAIR ANGLES PER BAC S/B AND THE FLOOR WEBS WERE REPLACED PER THE S/B. THE WORK WAS DO CUMENTED PER ER/A 382559-14AD. 2 L 7 2 4F A16WE 2002022700048 20020227 00048 NM 2002 2 27 DL73K020182 1 20020213 A 3222 TORQUE LINK BOEING 737 737247 138448D NM NLG FAILED A DALA O OTHER E VIBRATION/BUFFET LD LANDING 1 SO 27 373DL 23520 AT 100 KTS LANDING ROLLOUT, NOSE WHEEL HAD SEVERE SHIMMY. REPLACED TORQUE LINK ASSY. 2 L 7 2 4F A16WE 2002022700049 20020227 00049 NM 2002 2 27 DL757020027 1 20020109 A 5315 146N51114 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 THE UPPER CAP OF THE FS 1681 PASSENGER FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION. TO REMOVE THE DAMAGE, THE E NTIRE UPPER CAP WAS TRIMMED OFF. A NEW CAP WAS FABRICATED FROM ALUMINUM EXTRUSION AND INSTALLED PER ER/A 382227-14, REV A. 2 L 7 2 4F RT A2NM 2002022700050 20020227 00050 NM 2002 2 27 DL757020065 1 20020118 A 3350 767 LIGHT BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 637DL 23760 FOUND ON WALK AROUND, LEFT FWD AND AFT OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP. 2 L 7 2 4F RT A2NM 2002022700051 20020227 00051 NM 2002 2 27 DL757020070 1 20020119 A 3350 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 651DL 24391 EMERGENCY PATH LIGHTS INOP AT 26DEF AND 2R DOOR. RELAMPED, CHECKS OK. 2 L 7 2 4F RT A2NM 2002030400203 20020304 00203 NM 2002 3 4 F3LA200200071 1 20020223 A 5320 FLOOR SUPPORT BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED FLOOR SUPPORT AT STA 957, LBL 16 TO LBL 42, CORRODED. FABRICATED AND INSTALLED RE PLACEMENT FLOOR SUPPORT PER SRM 53-10-2 AND 51-30-2. 2 L 7 2 4U RT A16WE 2002022700052 20020227 00052 NM 2002 2 27 DL757020071 1 20020120 A 2997 WIRE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 630DL 31654 22920 716581 LEFT ENGINE HYD MESSAGE AND OVERHEAD LIGHT CAME ON PRIOR TO T/O. REPAIRED SHIELDED WIRE 18 INCHES FROM CANNON PLUG IN L EFT ENGINE PYLON. INDICATION NOW NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002022700053 20020227 00053 NM 2002 2 27 DL757020079 1 20020122 A 3211 113N10703 TRUNNION BOEING 757 757232 1384965 NM LT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 INSPECTION OF THE MLG FUSE PINS AND ADJACENT LUG BORES PER AD 2000-07-13, REVEALED CORROSION IN THE FUSE PIN LUG BORES O F THE LT MLG FWD TRUNNION BEARING SUPPORT FITTING ASSEMBLY. CLEANUP OF THE CORROSION RENDERED THE FITTING UNACCEPTABLE FOR FURTHER SERVICE. A NEW FITTING ASSEMBLY WAS INSTALLED ON THE AIRCRAFT PER ER/A 382314-14AD. 2 L 7 2 4F RT A2NM 2002022700054 20020227 00054 NM 2002 2 27 DL757020088 1 20020123 A 5310 146N8512 DOOR FRAME BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 OUTER CHORD AND WEB SPLICE; LOWER SILL CHORD SUBSTITUTION THE LOWER SILL OF THE C2 DOOR OPENING WAS FOUND WITH SEVERAL A REAS OF CORROSION. THE OUTER CHORD AND WEB OF THE FS 1440 OPENING FRAME WERE CUT AND THE LOWER SECTION REMOVED TO ALLOW REPLACEMENT OF THE SILL. THE SILL WAS REPLACED, THE WEB SPLICED PER B757 SRM, AND THE CHORD SPLICED WITH 2 ALUMINUM RE PAIR ANGLES PER ER/A 382180-14, REV A. 2 L 7 2 4F RT A2NM 2002022700055 20020227 00055 NM 2002 2 27 DL757020091 1 20020124 A 3350 767 LIGHT BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 647DL 24218 FOUND ON WALKAROUND CHECK, R-1 DOOR; L-1 DOOR ; L-2 DOOR AND LEFT AFT OVERWING EXTERIOR EMERGENCY LIGHTS INOP. RELAMPED , ALL LIGHTS NOW OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 2002022700056 20020227 00056 NM 2002 2 27 DL757020120 1 20020201 A 5270 SENSOR BOEING 757 757232 1384965 NM L2 DOOR OUT OF ADJUST A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 633DL 23614 ABORTED TAKEOFF AT 99 KTS DUE TO ENTRY DOOR WARNING. ADJUSTED DOOR INDICATOR, CHECKS OK. 2 L 7 2 4F RT A2NM 2002022700057 20020227 00057 NM 2002 2 27 DL757020131 1 20020202 A 3350 3020445 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 650DL 24390 L-3 EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A2NM 2002022700058 20020227 00058 NM 2002 2 27 DL757020146 1 20020206 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 670DN 25331 FOUND ON LAYOVER LEFT OUTSIDE EMERGENCY LIGHT AFT OF WING INOP. REBULB, NO HELP. REPLACED PWR SUPPLY AND BATTERY PACK. ALL EMERGENCY LIGHTS, NOW OK. 2 L 7 2 4F RT A2NM 2002022700059 20020227 00059 NM 2002 2 27 DL757020162 1 20020209 A 3350 20131A BATTERY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 672DL 25977 ON L/O, FOUND F/C EMERGENCY SEAT ROW LIGHTS INOP. REPLACED BATTERY AND POWER SUPPLY. ALSO REPLACED LIGHT ASSY ON SEAT ROW 6C. 2 L 7 2 4F RT A2NM 2002022700060 20020227 00060 NM 2002 2 27 DL757020204 1 20020219 A 7910 O-RING BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE CUT A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 6704Z 47843 30396 716398 LEFT ENGINE LOW PRESS LIGHT ILLUM, LT ENG OIL QTY AT ZERO, PRESS STARTED TO DECREASE AND ENG SHUTDOWN ONCE OIL PRESS IN THE RED. MTC IN PROGRESS, NO DETAILS AS YET AS TO SOURCE OF OIL LOSS. MTC FOUND O-RING CUT ON MAIN OIL FILTER HOUSING. REPLACED SAME. ALSO OIL LINE WAS LEAKING AT FUEL/OIL HEAT EXCHANGER. TIGHTENED LINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002022700061 20020227 00061 NM 2002 2 27 DL75A020074 1 20020121 A 2932 CONNECTOR BOEING 757 757212 1384951 NM PRESSURE SWITCH NOT SEATED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 750AT 23126 LEFT HYD ELECT PUMP EICAS MSG CAME ON AND PRESS LIGHT IN THE LEFT HYD PUMP SWITCH ILLUMINATED. FOUND PUMP OPN NORMAL. RESEATED PRESSURE SWITCH PLUG. PUMP, LIGHT, AND MSG ALL CHECK OK. REPLACED OVERHEAD HYD CONTROL PANEL AND LEFT SYS HYD ELECT PUMP LOW PRESSURE SWITCH AS PRECAUTION. ALL CHECKS OK. 2 L 7 2 4F RT A2NM 2002022700062 20020227 00062 NM 2002 2 27 DL75A020192 1 20020215 A 5753 113N32523 FLAP BOEING 757 757212 1384951 NM LT WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752AT 23128 LEFT MAIN FLAP, LWR CHORD WAS FOUND CORRODED. REPAIR PER ER/A 410943-14. 2 L 7 2 4F RT A2NM 2002022700063 20020227 00063 NM 2002 2 27 DL764020075 1 20020121 A 3320 S283U00816 BALLAST BOEING 767 767432ER 1385134 NM LAVATORY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 838MH 29711 FWD IFE COOLING MESSAGE ILLUMINATED STATUS MSG. COULD BE RELATED TO SMOKE IN OBSERVED NEAR MID LAV BY F/A. FWD IFE COO LING MSG CAUSED BY IFE BEING TURNED OFF. SMOKE AT MID LAV CAUSED BY A BAD MIRROR LIGHT BALLAST M4 IN R2 LAV DISCONNECTE D LAV CAPPED CANNON PLUG. LOCKED OUT LAV AND FWD TO MCO PER MEL 38-30-01B. BALLAST P/N 335240080 NASI HNL. 2 L 7 2 4F RT A1NM 2002022700064 20020227 00064 NM 2002 2 27 DL764020081 1 20020116 A 5720 113T1660 PLATE BOEING 767 767432ER 1385134 NM LT WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 833MH 29706 FOUND ON PDC CHECK, LT WING CLOSURE PANEL FWD OF T/E FLAP HAS DAMAGED ATTACH POINTS AND FITTINGS. REPLACED DAMAGE C-CHA NNEL 1 EA TIED ROD AND 3 EA WIGGLE PLATES. 2 L 7 2 4F RT A1NM 2002022700065 20020227 00065 EA 2002 2 27 COMA0260119 1 20020227 A 5300 6003106819 FITTING CNDAIR CL600 CL6002B19 1900309 EA FS460 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 931CA 18207 7037 A FLOOR SUPPORT FITTING WAS CRACKED AT FS460 AND RBL9.REMOVED THE CRACKED FITTING AND INSTALLED A NEW FITTING P/N 600-31 068-19 I/A/W WVAC EO 601R-53-2988. 2 L 7 2 4F RT A21EA 2002022700066 20020227 00066 EA 2002 2 27 COMA0260120 1 20020226 A 5415 601370102 PYLON CNDAIR CL600 CL6002B19 1900309 EA EMPENNAGE CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 952CA 14966 7092 DURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY, DISCOVERED FRETTING/PITTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTIN G MOUNTING VIB.REPAIRED IN ACCORDANCE WITH REO 601R-54-50-036. 2 L 7 2 4F RT A21EA 2002030800015 20020308 00015 NM 2002 3 8 02FDEA00146 1 20020227 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 SKIN DENTED AT BS 1279 TO 1282, BETWEEN STR 20R & 21R. REMOVED AND REPLACED SKIN WITH DOUBLER PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 2002022700067 20020227 00067 NM 2002 2 27 02FDEA00147 1 20020215 A 5330 6554581 SKIN BOEING 727 727233 138408A NM CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 N 327 CORROSION ON SKIN & STRINGER AT BS 950D TO 950E, STR 28L (C53-113-01-(2)). ** S/D ** COMING 2 L 7 3 4F RT A3WE 2002030800016 20020308 00016 NM 2002 3 8 02FDEA00148 1 20020223 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 FRAME DENTED AT BS 420 BETWEEN STR 8L TO 9L. REMOVED AND REPLACED FRAME PER SRM 53-10-4 FIG 1. 2 L 7 3 4F RT A3WE 2002030800017 20020308 00017 NM 2002 3 8 02FDEA00149 1 20020225 A 5313 STRINGER BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 STR 25L CRACKED AT BS 560. REMOVED AND REPLACED STR PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 2002030800018 20020308 00018 NM 2002 3 8 02FDEA00150 1 20020216 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 FLOORBEAM AT BS 720A, RBL 48 - RBL 56, WL 208 CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 2002030800019 20020308 00019 NM 2002 3 8 02FDEA00151 1 20020219 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 CORROSION ON BS 950F FRAME ON LWR REPAIR ANGLE STR 30. REMOVED AND REPLACED ANGLE PER SRM 53-10-4. 2 L 7 3 4F RT A3WE 2002030100082 20020301 00082 EA 2002 3 1 COMA0260121 1 20020225 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 6295 7306 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 650EB. REPAIRED IAW 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002022700070 20020227 00070 WP 2002 2 27 ABXA010740 1 20020212 A 5310 3924028501N FITTING DOUG DC9 DC932 3022066 WP F.S. 604 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 LONGERON 28 RIGHT HAD CRACKED END FITTING AFT OF F.S. 604 "P" DOME. REPLACED END CAP IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002022700071 20020227 00071 WP 2002 2 27 ABXA010741 1 20020212 A 5310 99155744 INTERCOSTAL DOUG DC9 DC932 3022066 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 CRACK IN INTERCOSTAL LONGERON 27 LEFT, STATION 761. REPAIRED AREA IAW DC-9 DOUGLAS DWG 9915574. 2 L 7 2 4F A6WE 2002022700074 20020227 00074 NM 2002 2 27 TSAA0233028 1 20020125 A 3350 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST NR NOT REPORTED 1 WP 13 821AL 23155 REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACKS DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002022700075 20020227 00075 NM 2002 2 27 TSAA0253020 1 20020107 A 5330 65457701 SKIN BOEING 737 737209 13844AE NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 827AL 23913 FOUND FUSELAGE CRACK AT BS 940 S-21R. TRIMMED OUT DAMAGE AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED, INSTALLED FILLER AND DOUBLER IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002022700076 20020227 00076 NM 2002 2 27 TSAA0253022 1 20020114 A 5330 6545855502 SKIN BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 REPAIRED CRACK AT FS 965 (AFT ENTRY DOOR). CUTOUT AND REMOVED CRACK PORTION OF SKIN AROUND LOWER FORWARD AREA. PERFORM ED HFEC INSPECTION AROUND CUT OUT AREA NO DEFECTS NOTED. FABRICATED AND INSTALLED A REPAIR FILLER AND PLATE IAW SRM 53- 30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002022700077 20020227 00077 NM 2002 2 27 TSAA0255019 1 20020102 A 5542 65C258401 SKIN BOEING 737 737230 1384401 NM RUDDER DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 823AL 23154 COMPOSITE DAMAGE TO LEFT SIDE AT RUDDER STATION 86.59 TO STATION 66.59. REMOVED ALL CONTAMINATION AND WATER FROM DAMAGE D AREA. FABRICATED, CLEANED, AND INSTALLED HONEYCOMB REPLACEMENT CORE PLUG. REPAIRED IAW SRM 55-40-5 AND 51-40-14 REPA IR NR 3. (M) 2 L 7 2 4F RT A16WE 2002022700081 20020227 00081 NM 2002 2 27 TSAA0257031 1 20020108 A 5754 114A50303 SLAT BOEING 737 73725A 1384481 NM WING CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 REPAIRED CRACK AT NR 6 SLAT STATION 370.56. BLENDED OUT THE DAMAGED AREA IAW SRM 57-20-1, FIG 1, PAGE 1. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002022700086 20020227 00086 NM 2002 2 27 USAA020010 1 20020110 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND SKIN CRACKED .812 INCH LONG, FRAME POST SKIN OF CAPT L1 WINDOW UPPER OUTBOARD CORNER. INSTALLED DOUBLER PER EA 73010 AND SRM 53-10-01 FIG 210. (M) 2 L 7 2 4F RT A16WE 2002022700087 20020227 00087 NM 2002 2 27 USAA020011 1 20020110 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND STRINGER CRACKED 1.5 INCH, STRINGER 5L AT STATION 380. CUT OUT CRACKED SECTION, INSTALLED NEW STRINGER SECT ION AND DOUBLERS PER SRM 53-00-03. (M) 2 L 7 2 4F RT A16WE 2002022700088 20020227 00088 NM 2002 2 27 USAA020012 1 20020110 A 5320 654580730 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND ANGLE CRACKED .75 INCH, ANGLE SUPPORT FORWARD OF STATION 291.5 BETWEEN S12R-13R. REMOVED AND REPLACED SUPPO RT WITH IDENTICAL PART PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002022700089 20020227 00089 NM 2002 2 27 USAA020013 1 20020110 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND FRAME WEB CRACKED .75 INCH, AT STATION 277 S14R SUPPORT WEB. MANUFACTURED AND REPLACED WEB PER SRM 53-10-15 . (M) 2 L 7 2 4F RT A16WE 2002022700090 20020227 00090 NM 2002 2 27 USAA020014 1 20020110 A 5320 6545834525 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND INTERCOSTAL CRACKED .5 INCH, FORWARD TOP END OF INTERCOSTAL AT STATION 344, BL0. REMOVED AND REPLACED INTER COSTAL PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002022700091 20020227 00091 NM 2002 2 27 USAA020015 1 20020110 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 23312 PIT - FOUND FRAME CRACKED .5 INCH, CORNER FORWARD GALLEY DOOR STATION 296 BETWEEN S7R-8R. INSTALLED MANUAL DOUBLER PER SRM 51-70-11 AND EA 73057. (M) 2 L 7 2 4F RT A16WE 2002022700092 20020227 00092 NM 2002 2 27 USAA020016 1 20020110 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND SKIN CRACKED .5 INCH LONG, FRAME POST SKIN OF F/O'S R-1 WINDOW UPPER OUTBOARD CORNER. CUT OUT DAMAGED AREA INSTALLED FILLER AND DOUBLER PER SRM 53-10-01 FIG 210 SHEET 1. (M) 2 L 7 2 4F RT A16WE 2002022700093 20020227 00093 NM 2002 2 27 USAA020017 1 20020110 A 5311 50826162 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND FRAME CRACKED 2 INCHES, STATION 303.3 AT STR 4L UNDER BULKHEAD MOUNT FITTING. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2002022700094 20020227 00094 NM 2002 2 27 USAA020018 1 20020111 A 5310 DOOR FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND FRAME CRACKED 1 INCH, DOOR FRAME CUT OUT INTERIOR SKIN STATION 950 AT S11L. FABRICATED AND INSTALLED PER EA 73190 WITH TYPICAL REPAIR 53-30-07A. (M) 2 L 7 2 4F RT A16WE 2002022700095 20020227 00095 NM 2002 2 27 USAA020021 1 20020122 A 5311 654655072 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 782AU 31460 25021 PIT - FOUND FRAME CRACKED .25 INCH, FRAME 747 AT BAG BIN SUPPORT BETWEEN S8R AND S9R. DOUBLER INSTALLED PER TYPICAL REP AIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002022700096 20020227 00096 NM 2002 2 27 USAA020022 1 20020122 A 5311 6546529 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 782AU 31460 25021 PIT - FOUND FRAME CRACKED .125 INCH, FRAME 440 RT, BAG BIN SUPPORT BETWEEN S8R AND S9R. INSTALLED DOUBLER PER TYPICAL R EPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002022700097 20020227 00097 NM 2002 2 27 USAA020023 1 20020122 A 5311 654655072 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 782AU 31460 25021 PIT - FOUND FRAME CRACKED .25 INCH, FRAME 827 BAG BIN SUPPORT BETWEEN S8R AND S9R. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002022700098 20020227 00098 NM 2002 2 27 USAA020024 1 20020123 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 782AU 31460 25021 PIT - FOUND FRAME CRACKED .125 INCH, FRAME 380 BAG BIN SUPPORT BETWEEN S8R AND S9R. INSTALLED DOUBLER PER TYP REPAIR 53 -10-14. (M) 2 L 7 2 4F RT A16WE 2002022700099 20020227 00099 NM 2002 2 27 USAA020027 1 20020116 A 5522 65C25746132 SKIN BOEING 737 7374B7 1384702 NM ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 447US 31500 24874 PIT - FOUND ELEVATOR DELAMINATED .375 INCH, OUTER PLIES ON LOWER SKIN 75.5 FROM TIP 8 FROM L/E. REPAIRED PER SRM 55-20- 01 AND 51-70-17 .5 INCH PER PLY PER EA NR 73202. (M) 2 L 7 2 4F RT A16WE 2002022700102 20020227 00102 NM 2002 2 27 USAA020028 1 20020111 A 5410 SLEEVE BOEING 737 7374B7 1384702 NM NACELLE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 447US 24874 PIT - FOUND SLEEVE RIGHT WITH 3 INCH PUNCTURE, INNER AND OUTER SKIN AND HONEYCOMB CORE 6 INCH EDGE PANEL. COMPOSITE REP AIR IAW 54-30-70 FIG 201 AND SRM 51-70-17 PER EA 85845. (M) 2 L 7 2 4F RT A16WE 2002022700103 20020227 00103 NM 2002 2 27 USAA02008 1 20020109 A 5320 SPLICE BOEING 737 7374B7 1384702 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 447US 24874 PIT - FOUND STRINGER WITH 16 INCH SPLICE, FORWARD CARGO STRINGER 27R STATION 500E TO 500F. REPAIRED WITH 16 INCH SPLICE PER SRM 53-00-03 FIG 201. (M) 2 L 7 2 4F RT A16WE 2002022700106 20020227 00106 NM 2002 2 27 USAABB02010 1 20020128 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 628AU 27806 BDL - FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 13 DIM. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002022700107 20020227 00107 NM 2002 2 27 USAABB02011 1 20020130 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AU 27199 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 9. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002022700108 20020227 00108 WP 2002 2 27 USAAD02004 1 20020205 A 7932 WARNING SYSTEM DOUG DC9 DC982 3022082 WP COCKPIT FAULTY A USAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 830US 49443 FLL-CLT - FLT 482 - DURING CLIMB, THE RIGHT ENGINE OIL QUANTITY STARTED TO DROP. THE OIL PRESSURE WAS NORMAL WHEN THE C REW SHUT DOWN THE RIGHT ENGINE AND DIVERTED TO PB. THE FLIGHT LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME WAS 10 MINUT ES. MAINTENANCE CHECKED THE OIL QUANTITY AND FOUND TO BE FULL. THE RIGHT ENGINE OIL QUANTITY INDICATING SYSTEM WAS PLA CED ON MEL AND THE AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F A6WE 2002022700109 20020227 00109 WP 2002 2 27 USAAD02005 1 20020206 A 3350 MISC0639 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 826US 48026 IND - THE EXTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 2002022700110 20020227 00110 WP 2002 2 27 USAAD02006 1 20020206 A 3350 AD4002P BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 826US 48026 IND - THE AFT ACCESSORY CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2002022700111 20020227 00111 WP 2002 2 27 USAAD02007 1 20020206 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 826US 48026 IND - THE TAILCONE EMERGENCY LIGHT REMOTE RECEIVER WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT REMOTE REC EIVER BATTERY. (M) 2 L 7 2 4F A6WE 2002030400205 20020304 00205 NM 2002 3 4 F3LA200200073 1 20020223 A 5320 STRAP BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY FLOOR WEB STRAP CORRODED AT STA 1006 TO STA 1016. FABRICATED AND INS TALLED REPLACEMENT WEB STRAP PER SRM 51-30-2. 2 L 7 2 4U RT A16WE 2002030400206 20020304 00206 NM 2002 3 4 F3LA200200074 1 20020223 A 5321 FLOOR PANEL BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND EDGES OF AFT FLOOR PANEL IN FWD CARGO COMPARTMENT. REMOVED CORRO SION AROUND EDGES OF AFT FLOOR PANEL PER SRM 51-10-06. FABRICATED AND INSTALLED REPLACEMENT RETAINER STRAP PER SRM 51-1 0-01, 51-10-02 AND SOPM 20-41-02. 2 L 7 2 4U RT A16WE 2002030400207 20020304 00207 NM 2002 3 4 F3LA200200075 1 20020223 A 5315 FLOORBEAM BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 967 CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM CAP PER SRM 51-30-2. 2 L 7 2 4U RT A16WE 2002030400208 20020304 00208 NM 2002 3 4 F3LA200200076 1 20020223 A 5320 STIFFENER BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUT PLATE HOLE AT STA 727, RBL 12, VERTICAL STIFFENER. CUT OUT DAMAG ED AREA, FABRICATED REPLACEMENT PARTS AND INSTALLED PER EO 51-00-737-001 AND SRM 51-40-4. 2 L 7 2 4U RT A16WE 2002022800008 20020228 00008 SO 2002 2 28 C2XA02CL060 1 20020227 A 2133 2097K011100 OUTFLOW VALVE EMB 135 EMB135LR 3260305 SO AFT FUSELAGE FAILED A C2XA B EMER. DESCENT O OTHER CR CRUISE 1 SW 27 17513 3487 145292 CLE FLIGHT#3146 THE CREW REPORTED A TOTAL LOSS OF PRESSURIZATION IN FLIGHT.THE AIRCRAFT DESENDED TO 10000 FT.AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE ELECTOPNEUMATIC OUTFLOW VALVE.OPERATIONAL CHECKS WERE GO OD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2002022800009 20020228 00009 SO 2002 2 28 COMA0210007 1 20020223 A 3230 12038594001 CONTROL BOX EMB 120 EMB120RT 3260202 SO INST PANEL MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 259CA 20837 120252 FLIGHT 5061 LANDING GEAR DISAGREEMENT WARNING WHEN GEAR RETRACTED.REPLACED THE L/G CONTROL BOX. 2 L 7 2 4T RT A31SO 2002022800010 20020228 00010 SO 2002 2 28 COMA0210008 1 20020223 A 3230 12038594001 CONTROL BOX EMB 120 EMB120RT 3260202 SO INST PANEL MALFUNCTIONED A COMA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 259CA 26977 1 120252 FLIGHT 5018 L/H MLG DISAGREEMENT WARNING WHEN GEAR RETRACTED.REPLACED THE L/G CONTROL BOX. 2 L 7 2 4T RT A31SO 2002022800011 20020228 00011 EA 2002 2 28 COMA0260122 1 20020226 A 2750 601R9310591 BPSU CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 916CA 18484 7014 FLIGHT 5236 FLAPS FAILED DURING APPROACH.REPLACED THE L/H BPSU 2 L 7 2 4F RT A21EA 2002022800012 20020228 00012 EA 2002 2 28 COMA0260123 1 20020226 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 916CA 7014 FLIGHT 5235 FLAPS FAILED DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002022800013 20020228 00013 2002 2 28 02022701 4 20020225 A 2565 PIN BOEING 757 757256 NM EVAC SLIDE BINDING A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 542NA 1154 598 26245 WHILE OPENING LEFT OVERWING EXIT DURING C-CHECK THE SLIDE WAS INADVERTENTLY DEPLOYED DUE TO IMPROPER DE-ARMING PROCEDURE S. SLIDE DID NOT PROPERLY DEPLOY DUE TO RETAINING PIN NOT RELEASING. SLIDE ASSEMBLY SENT OUT FOR OVERHAUL. 2 L 7 2 4F RT A2NM 2002022800014 20020228 00014 EA 2002 2 28 COMA0260124 1 20020226 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 796CA 7338 FLIGHT 5872 GEAR DISAGREE WARNING - NLG DID NOT RETRACT.CLEANDED AND LUBED NLG - RETRACT CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2002022800016 20020228 00016 EU 2002 2 28 02FDEA00143 1 20020226 A 2170 COALESCER BAG AIRBUS 310 A310222 3930315 EU A/C BAY CONTAMINATED A FDEA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 25 448FE 260 ON FINAL ECAM WARN AVIONICS SMOKE AND M/DECK M/CARGO MID SMOKE DETECT. REMOVED AND REPLACED LT & RT COALESCER BAGS PER MM 21-51-16-3. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2002022800017 20020228 00017 EA 2002 2 28 COMA0260125 1 20020226 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 819CA 7415 FLIGHT 5202 SMOKE COMING FROM A/C VENTS AFTER T/O.COULD NOT DUPLICATED - INSPECTED A/C PACKS FOR OIL LEAKS - GROUND RAN ACFT AT HIGHT POWER - NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2002022800018 20020228 00018 EA 2002 2 28 COMA0260126 1 20020222 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 999CA 11295 7230 FLIGHT 5548 FLAPS FAILED AT 20 DEGREES.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2002022800019 20020228 00019 WP 2002 2 28 02FDEA00144 1 20020207 A 5230 63050007 DRIVE SHAFT DOUG DC10 DC1030 3023501 WP CARGO DOOR SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 CTR CARGO DOOR LIFT ACTUATOR OUTPUT DRIVE SHAFT SHEARED, CAUSING DOOR TO FREE FALL AND IMPACT MAINTENANCE STAND. REMOVE D AND REPLACED ACTUATOR CTR CARGO COMPARTMENT PER MM 52-32-01 & 52-32-07. 2 L 7 3 4F A22WE 2002022800020 20020228 00020 EU 2002 2 28 02FDEA00145 1 20020226 A 2170 COALESCER BAG AIRBUS 310 A310203 3930313 EU A/C BAY DIRTY A FDEA F ACTIVATE FIRE EXT. B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 25 430FE 394 MAIN DECK CARGO SMOKE WARNING ALERT LIGHT AND FUMES. CHECK A/C FOR SIGNS OF FIRE AND SMOKE ALL CLEAR. REMOVED AND REPL ACED COALESCER BAGS. ALL OK. 2 L 7 2 4F RT A35EU 2002022800021 20020228 00021 WP 2002 2 28 ABXA010747 1 20020213 A 5310 59114481 FRAME DOUG DC9 DC932 3022066 WP FWD. CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 FRAME WAS CORRODED AT STATION 332, FROM LONGERON 29 LEFT TO LONGERON 29 RIGHT. REPAIRED FRAME IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002022800022 20020228 00022 EU 2002 2 28 SABA020028 1 20020227 A 3240 AH084357 SHUTTLE VALVE BAG JETSTM JETSTM3201 1500217 EU LFT LDG GEAR INOPERATIVE A SABA K NONE O OTHER LD LANDING 1 SO 33 964AE 964 Aircraft 964 on flight 5215 GSP to RDU. During landing the left main gear brake failed. No emergency was declared. Ai rcraft completed the landing roll and taxied to the gate with no other problems. Maintenance from CLT removed and repla ced the left brake shuttle valve. Ops check was good. Aircraft returned to service. 2 L 7 2 4T RT A56EU 2002030800020 20020308 00020 NM 2002 3 8 02FDEA00152 1 20020216 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 CORROSION ON FLOORBEAM LOWER CHORD LBL 55 - RBL 55. REMOVED AND REPLACED FLOORBEAM. 2 L 7 3 4F RT A3WE 2002022800025 20020228 00025 NM 2002 2 28 CALA0200096 1 20020225 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR SUPPORT AT STA 578, BBL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IA W SRM 51-40-2. 2 L 7 2 4F RT A16WE 2002022800026 20020228 00026 NM 2002 2 28 CALA0200097 1 20020225 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND A 2 INCH CRACK IN UPPER CHORD ON FLOOR SUPPORT AT STA 380-400, BL 0. THE UPPER CHORD WAS REMOVED AND R EPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002022800027 20020228 00027 NM 2002 2 28 CALA0200100 1 20020226 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 947.5-967, RBL 17.5. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002022800028 20020228 00028 NM 2002 2 28 CALA0200101 1 20020226 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 951.5, RBL 8-16. A NEW FLOOR SUPPORT WAS INSTALLED IAW ECRA 5310-03585. 2 L 7 2 4F RT A16WE 2002022800029 20020228 00029 NM 2002 2 28 DL764020082 1 20020116 A 5720 113T1660 PLATE BOEING 767 767432ER 1385134 NM RT WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 838MH 29711 FOUND BY MTC, RT WING LOWER CLOSE OUT PANEL FOR T/E FLAP DAMAGED BETWEEN NR 7 AND 8 TRACK HOUSINGS. REPLACED 4 WIGGLER PLATES AND C-CHANNEL BETWEEN NR 7 AND NR 8 FLAP TRACK HOUSING AND INSTALLED CLOSURE PANEL. 2 L 7 2 4F RT A1NM 2002022800030 20020228 00030 NM 2002 2 28 DL764020094 1 20020125 A 3350 D71701100 BATTERY PACK BOEING 767 767432ER 1385134 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 832MH 29704 DURING PREDEPARTURE CHECK TO FLIGHT 1578 FOUND EMERGENCY ESCAPE PATH MARKING LIGHTS FROM ROW 17FG TO 22FG INOP. REPLACE D BATTERY PACK IN SIDEWALL AT 23FG. 2 L 7 2 4F RT A1NM 2002022800031 20020228 00031 NM 2002 2 28 DL764020101 1 20020126 A 3260 849704 PSEU BOEING 767 767432ER 1385134 NM E/E BAY FAULTY A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 839MH 29712 GEAR DISAGREE CAME ON AT CRUISE (FL 290) NOSE INDICATED UP, MAINS IN TRANSIT (INDICATED). SUSPECT SOFTWARE PROBLEM. PS EU BIT SHOWS CARD 005 AND TARGET 260 FAULTS. SWUNG GEAR SEVERAL TIMES WHILE OPERATING CABIN EQUIP TO TEST FOR EMI FAULT S, ALL CHECKS GOOD. REPLACED PSEU, CHECKED PA CABIN INTERPHONE AND CHIME, NO FAULTS OR MESSAGES, REPLACED S-260. ATTEM PTING TO INDUCE FAULT, RAN BOTH ENGINES WHILE OPERATING VARIOUS A/C SYS TO INCLUDE WINDOW HEAT, FLAPS, IFE, PA AT ALL ST ATIONS AND EXTERIOR LIGHTS. NO MSGS/S OF FAULTS NOTED. 2 L 7 2 4F RT A1NM 2002022800032 20020228 00032 EU 2002 2 28 01003310 1 20020103 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU LOOSE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 310UE 41028 During preflight inspection for flight from IAD to CRW, the crew reported that the emergency floor track lights at seat row 8 and 9 came on with the switch in the "armed" position. Maintenance personnel secured a loose connector for the em ergency floor track lighting system. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002022800033 20020228 00033 NM 2002 2 28 02044408 1 20020213 A 3350 POWER SUPPLY DORNER DO32 DO328300 NM A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 408FJ 3160 During preflight inspection, the crew reported that the emergency floor track lighting was inoperative from seat row 3 t o 6. Maintenance personnel removed and replaced the emergency exit lighting power supply. An operational check was sat isfactory and the aircraft was returned to service. 2 H 7 2 4T RT A55NM 2002022800034 20020228 00034 NM 2002 2 28 DL764020112 1 20020122 A 2781 PROXIMITY SENSOR BOEING 767 767432ER 1385134 NM L/E SLAT OUT OF ADJUST A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 839MH 29712 LEADING EDGE SLAT ASYMMETRY MESSAGE ON SLAT RETRACTION OUT OF ATL. NUMBER 2 SLAT PROX SENSOR OUT OF ADJUSTMENT. ADJUST ED PER BOEING S/L 767-SL-27-83. 2 L 7 2 4F RT A1NM 2002022800035 20020228 00035 NM 2002 2 28 DL764020172 1 20020210 A 1430 114T41457 BOLT BOEING 767 767432ER 1385134 NM L/E SLAT FAILED A DALA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 826MH 29697 L/E SLAT ASSY ON SHORT FINAL AS FLAPS WERE MOVED FROM 20 TO 30. FOUND NR 5 OUTBOARD LEADING EDGE AUX TRACK ROLLER MISSI NG AND BOLT BROKEN. LOWER ACCESS PANEL REMOVED AND PLACED IN FLOOR DECK SNSR TARGET IN SCREW BAG ATTACHED TO PANEL UA 1 03202. REPLACED AUX TRACK ROLLER AND BOLT PER MM. OPERATED FLAPS AND SLATS. ALL INDICATIONS NORMAL. REPLACED ACCESS PANEL. 2 L 7 2 4F RT A1NM 2002022800036 20020228 00036 NM 2002 2 28 DL764020188 1 20020214 A 3397 WIRE BOEING 767 767432ER 1385134 NM EXTERIOR BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 842MH 29715 EXTERIOR EMERGENCY LIGHT AT 2L INOP. WIRE BROKE OFF THE CONNECTOR TO THE BULB SOCKET. 2 L 7 2 4F RT A1NM 2002022800037 20020228 00037 NM 2002 2 28 DL767020168 1 20020210 A 2120 SMOKE BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE CABIN DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 115DA 50059 22227 580172 ON TAKEOFF ROLL, SMOKE AND FUMES THROUGHOUT CABIN. PERFORMED DUCT BURN OUT FOR BOTH PACKS AND BOTH ENGINES. NO EVIDENC E OF FUMES FROM PNEU SYS AFTER DUCT BURN OUT. CONTINUE TO MONITOR AIRCRAFT. 2 L 7 2 4F 4 F RT A1NM E13NE 2002022800038 20020228 00038 EU 2002 2 28 02058315 1 20020227 A 3397 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 315UE 41033 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE PERSO NNEL SECURED A LOOSE CONNECTOR. AN OPERATIONAL CHECK OF THE EMERGENCY FLOOR TRACK LIGHTING SYSTEM WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002022800039 20020228 00039 NE 2002 2 28 DL76G020066 2 20020119 A 7200 CF680C2B6 ENGINE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 2 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1501P 34263 695373 24983 695373 METAL FOUND ON CHIP DETECTOR,-A- -C- AND -D- SUMP CHIP DETECTORS. ATL MTC REPLACING ENGINE. UPON FURTHER EVALUATION FR OM ENGINE, SHOP NOW SUSPECT METAL IS CLEAN-UP MATERIAL. MTC FURTHER EVALUATING WITH T/O POWER PENALTY RUN. 2 L 7 2 4F 4 F RT A1NM E13NE 2002022800040 20020228 00040 NE 2002 2 28 DL76G020198 2 20020217 A 7200 ENGINE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 2 VIBRATION A DALA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 27 156DL 25354 695690 ON TAKEOFF ROLL, THE RIGHT ENGINE VIB INDICATED A 5.0 (LPT). TAKEOFF ABORTED AT 80 KNOTS INDICATED AIRSPEED. ALL OTHER ENGINE PARAMETERS ARE NORMAL. T/S PER FIM 71-05-00. CHIP DET CHECKED, CLEANED ACCEL CONNECTOR, LUBED FAN BLADES. PER FORMED VIBRATION SURVEY R/U PER PFHB. ALL VIBS WITHIN LIMITS. 2 L 7 2 4F 4 F RT A1NM E13NE 2002022800041 20020228 00041 NM 2002 2 28 DL76L020033 1 20020110 A 3350 BATTERY PACK BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 176DN 25061 LEFT SIDE CABIN EMERGENCY LIGHT MID CABIN INOP. REPLACED BATTERY PACK, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2002022800042 20020228 00042 NM 2002 2 28 DL76L020044 1 20020112 A 3350 CONNECTOR BOEING 767 767332 1382001 NM CABIN NOT SEATED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 178DN 25143 E-PATH LIGHTS INOP AT 22F, 27B, 30B, 34B AND 36B. RESEATED CONNECTORS, OPS OK. FOUND DURING LAYOVER CHECK. 2 L 7 2 4F RT A1NM 2002022800043 20020228 00043 NM 2002 2 28 DL76L020055 1 20020116 A 2121 6066223 FAN BOEING 767 767332 1382001 NM LEFT MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 175DN 24803 ODOR IN THE COCKPIT SMELLED LIKE HOT INSULATION, AT THE SAME TIME THE LEFT RECIRC FAN INOP LIGHT CAME ON WITH EICAS MSG. TURNED OFF LEFT RECIRC FAN AND SMELL WENT AWAY. T/S AS PER AMM FOUND LEFT RECIRC INOP AND RED RUBBER SEAL BETWEEN FIL TER AND FAN DAMAGED. PARTS NIS MUC FWD TO MCO AS PER MEL 21-25-01A. PLACARD INSTALLED. C/B R14 PULLED AND SECURED. 2 L 7 2 4F RT A1NM 2002022800044 20020228 00044 NM 2002 2 28 P5CA0200652 1 20020223 A 3240 141SM2T2 SWITCH BOEING 747 747122 1384872 NM #1 THROTTLE FAULTY A P5CA K NONE O OTHER LD LANDING 1 WP 23 852FT 19757 REF DMI 28874 / MEL 27-9 : AUTOSPOILER BRAKE DID NOT DEPLOY ON LANDING. TROUBLESHOT & FOUND THROTTLE SWITCH S860 AT FAUL T. REPLACED SAME & OPS CHKD OK PER MM 27-62-00. THIS CLEARS DMI 28874 / MEL 27-9. PLACARDS REMOVED. 2 L 7 4 4F A20WE 2002022800045 20020228 00045 NM 2002 2 28 P5CA0200656 1 20020227 A 3150 NONE WIRE BOEING 747 747122 1384872 NM SWITCH #334 BROKEN A P5CA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 23 853FT 19753 ON T/O ROLL, AS SOON AS POWER WAS ADVANCE, TAKE-OFF WARNING CAME ON. (ALL PARAMETERS NRML FOR T/O). RETURNED TO BLOCKS. FOUND BROKEN WIRE FOR SWITCH #334 POWER. REPAIRED WIRING BTWN LWR FIRE DISCONNECT & SWITCH S334 PER BMM CH 20. PERFORMED OPS TEST. CHKD GOOD FOR AURAL WARNING SYSTEM. HORIZONTAL STAB SYSTEM TEST OK ALSO. 2 L 7 4 4F A20WE 2002022800046 20020228 00046 NM 2002 2 28 DL76L020076 1 20020121 A 5730 PANEL BOEING 767 767332 1382001 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 191DN 28448 LEFT WING LOWER CLOSURE PANEL TRAILING EDGE CHANNEL AND FWD EDGE WIGGLE PLATES CRACKED AND DAMAGED. REPLACED PANELS. 2 L 7 2 4F RT A1NM 2002022800047 20020228 00047 NM 2002 2 28 DL76L020098 1 20020126 A 2120 ODOR BOEING 767 767332 1382001 NM CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 174DN 24802 ACRID SMELL INFLIGHT. A/C DIVERTED TO MANCHESTER. MANCHESTER MTC DID NOT FIND ANYTHING OBVIOUS. MTC WILL CONTINUE TO MONITOR AIRCRAFT. 2 L 7 2 4F RT A1NM 2002022800048 20020228 00048 NM 2002 2 28 DL76L020111 1 20020131 A 3213 AXLE BOEING 767 767332 1382001 NM RT MLG SHEARED A DALA K NONE Z SIGNIFICANT FAILURE REPORT TX TAXI/GRND HDL 1 SO 27 179DN 25144 RIGHT MLG OUTBOARD AFT REAR AXLE SHEARED DURING GROUND MOVEMENT TO WING OUT OF HANGAR. FAILURE WAS NOTICED BY TIRE TILT . REMOVAL OF TIRE AND BRAKE ASSY SHOWED COMPLETE SHEAR FAILURE OF AXLE UNDER BRAKE. REPLACED AXLE. 2 L 7 2 4F RT A1NM 2002022800049 20020228 00049 NE 2002 2 28 01058621 2 20020227 A 7200 6089T11G01 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE A VTZA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 27 631BR 11427 7186 872183 During cruise of the flight from CHS to IAD, the crew reported that the #1 engine oil pressure dropped to zero. The cre w performed QRH procedures to shut down the engine, and landed at IAD without incident. Maintenance personnel removed a nd replaced the #1 engine assy. 2 L 7 2 4F 4 F RT A21EA E15NE 2002030500039 20020305 00039 EU 2002 3 5 MALA020170 1 20020226 A 2520 2LA00746200 PSU SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 436XJ 340B436 FLIGHT RETURNED TO DTW AFTER SMOKE WAS NOTED IN THE CABIN. REPLACED RT PSU. 2 L 7 2 4T RT A52EU 2002022800050 20020228 00050 NM 2002 2 28 DL76L020143 1 20020204 A 3232 537213 ACTUATOR BOEING 767 767332 1382001 NM NLG DOOR FAULTY A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 187DN 27582 SHORTLY AFTER T/O NOTICED STATUS MESSAGE, LANDING GEAR MONITOR AT 346 KNOTS GEAR DOOR CAUTION LIGHT AND GEAR DISAGREE LI GHT ILLUMINATED. WHEN SLOWING BELOW 320 KNOTS BOTH LIGHTS EXTINGUISHED. INTERROGATED PSEU BOX FOUND CODE-408, 218, 219 , 217, 216, 214, 211, 209, 207, 206, 205, 204, 200, 199, 198, 257, 235 AND 234. PERFORMED TARGET TEST ON 234 AND 235, A LL CHECK'S NORMAL. CLEARED MESSAGES FROM STATUS PAGE. REPLACED LT AND RT NOSE GEAR DOOR OPERATING MECHANISM NR 2 RODS PER MM. NOSE GEAR SWING AND FINAL RIG OK PER MM. 2 L 7 2 4F RT A1NM 2002022800051 20020228 00051 NM 2002 2 28 DL76L020176 1 20020212 A 3350 RPS1 BATTERY PACK BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 199DN 28456 RIGHT OVERWING ESCAPE SQUIB WILL NOT TEST. REPLACED RIGHT OVERWING SLIDE BATTERY PACK. TEST OK. 2 L 7 2 4F RT A1NM 2002022800052 20020228 00052 NM 2002 2 28 DL76L020179 1 20020213 A 3350 CHARGER BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 187DN 27582 EMERGENCY BATTERY CHARGER INOP AFT LEFT CABIN. REMOVED AND REPLACED BATTERY CHARGER. CHECKS OK. 2 L 7 2 4F RT A1NM 2002022800053 20020228 00053 NM 2002 2 28 DL76L020203 1 20020218 A 3350 LIGHT BOEING 767 767332 1382001 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 188DN 27583 E-PATH LIGHTS 31AB BACK TO 31 FG INOP. REMOVED AND REPLACED BATTERY CHARGER, POPPED FUSE IMMEDIATELY. FOUND E-PATH LIG HT ASSY AT SEAT 32AB BAD. REMOVED AND REPLACED SAME, CHECKS OK. 2 L 7 2 4F RT A1NM 2002022800054 20020228 00054 NM 2002 2 28 DL76P020072 1 20020120 A 2421 75535913B IDG BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 27 1402A 25989 724687 AIR TURNBACK AT 17,000 LVL FLT RIGHT GENERATOR FAILED ALONG WITH AIRFRAME VIBRATION. APU GEN OPER OK. SERVICED RIGHT I DG, RAN ENGINE AND NO VIBRATIONS. NO HISTORY. CREW DID NOT DISCONNECT IDG. DISCONNECTED IDG AND FWD TO MCO/PLC PER ME L 24-00-01. 2 L 7 2 4F 4 F RT A1NM E24NE 2002022800055 20020228 00055 NM 2002 2 28 QXEA0200321 1 20020226 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM INOPERATIVE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 350PH 19753 570 488 PSC- LEFT HAND AFT EXTERIOR EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY. OPERAT IONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002022800056 20020228 00056 EU 2002 2 28 QXEA0200300 1 20020215 A 3350 6008905 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 7987 11161 PDX-TWO EMERGENCY LIGHTS IN CABIN CEILING REMAIN ILLUMINATED WITH POWER SELECTED OFF. REMOVED AND REPLACED LEFT HAND AFT OVERHEAD BIN EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002022800057 20020228 00057 NM 2002 2 28 QXEA0200302 1 20020221 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DEFECTIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 3094 494 PSC-AFT TWO RED FLOOR TRACK LIGHTS AT ROW 1DE INOPERATIVE. FOUND BATTERY AT POSITION PS6 TO HAVE LOW VOLTAGE. REPLACED B ATTERY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002022800058 20020228 00058 NM 2002 2 28 0200546729 1 20020114 A 5311 FRAME BOEING 747 747251F 1384898 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 During "L" check found crack in frame at BS 300 between STR 40L and 41L. Repaired per EA 67-165017. 2 L 7 4 4F A20WE 2002022800059 20020228 00059 NM 2002 2 28 0200556729 1 20020114 A 5312 WEB BOEING 747 747251F 1384898 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 During "L" check found crack in bulkhead web holes at BS 1480. Repaired per EA 67-162020. 2 L 7 4 4F A20WE 2002022800060 20020228 00060 NE 2002 2 28 DL76S020048 2 20020113 A 7310 GASKET BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 ENGINE LEAKING A DALA O OTHER K X FLUID LOSS ENGINE FLAMEOUT DE DESCENT 1 SO 27 133DN 41591 580364 24982 580364 LEFT ENGINE FAILED IN FLT ON DESCENT INTO MCO. POM PROCEDURES FOLLOWED, ONLY ABNORMAL INDICATION WAS HIGH FUEL FLOW, CO MPARED TO THE RIGHT ENGINE. ON ARRIVAL FOUND LEFT ENGINE IDG FUEL/OIL COOLER GASKET CUT AND LEAKING. REPLACED SAME. F ULL POWER RUN UP PER PFHB PERFORMED. LEAK CHECK OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2002022800062 20020228 00062 NM 2002 2 28 DL76S020060 1 20020118 A 2820 SWITCH BOEING 767 767332 1382001 NM COCKPIT MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 119DL 23278 DURING THE BOARDING OF FLIGHT 706 FROM SEA/ATL CREW REPORTED SMOKE IN THE COCKPIT. CAUSE OF SMOKE WAS FOUND TO BE THE R T AFT FUEL PUMP SWITCH IN P5 PANEL. REPLACED SWITCH ASSY, PART WAS REPLACED. 2 L 7 2 4F RT A1NM 2002022800063 20020228 00063 NM 2002 2 28 DL76S020096 1 20020125 A 3350 20131A BATTERY PACK BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 130DL 24080 DURING S/C FOUND FWD RIGHT CEILING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 2 4F RT A1NM 2002022800064 20020228 00064 NM 2002 2 28 DL777020106 1 20020128 A 2530 1105011 COFFEEMAKER BOEING 777 777232 1385232 NM GALLEY MALFUNCTIONED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 862DA 29734 GALLEY AFT COFFEEMAKER C/B POPPED AND SPARKS OBSERVED BY F/A. REPLACED COFFEEMAKER NUMBER 4 AT MID GALLEY. CHECKS GOOD . 2 L 7 2 4F RT T00001SE 2002022800065 20020228 00065 NE 2002 2 28 DL777020191 2 20020215 A 7230 COMPRESSOR BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 1 ENGINE DAMAGED A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 861DA 10571 29952 051149 NR 1 ENGINE ON THROTTLE UP FAILED TO ACCELERATE. BORESCOPED NR 1 ENGINE, FOUND COMPRESSOR DAMAGE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2002022800066 20020228 00066 NM 2002 2 28 DL78K020171 1 20020211 A 3350 767 LIGHT BOEING 737 737832 13844CF NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3731T 30775 LEFT EXTERIOR LOWER AFT EMERGENCY EGRESS LIGHT INOP. RELAMPED SAME PER AMM, OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 2002022800067 20020228 00067 NM 2002 2 28 DLM11020036 1 20020111 A 3244 320002319 TIRE DOUG MD11 MD11 3023602 NM RT MLG FLAT A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 808DE 48479 TIRE FAIL EICAS MESSAGE DURING CLIMB. TIRE PRESSURE ON RIGHT MAIN OUTSIDE AFT TIRE ZERO. TEMP INDICATIONS NORMAL. FOU ND NR 8 TIRE AT 0 PSI. REPLACED NR 8 WHEEL ASSY. ALSO REPLACED NR 7 WHEEL ASSY PRECAUTIONARY. 2 L 7 3 4F RT A22WE 2002022800068 20020228 00068 NM 2002 2 28 DLM11020054 1 20020114 A 5511 SPAR CAP DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 802DE 48473 AT HMV 2, CORROSION WAS FOUND WHILE INSPECTING HORIZONTAL STABILIZER UPPER SURFACE BARREL NUT BORES PER SI8-85288-12. C ORROSION WAS ON LT AND RT UPPER SKINS AS WELL AS FRONT AND REAR SPAR CAPS. REPAIRED PER ER/A 412285-14. 2 L 7 3 4F RT A22WE 2002022800069 20020228 00069 NM 2002 2 28 DLM11020084 1 20020123 A 2913 887673 PUMP DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 ENGINE CRACKED A DALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 809DE 48480 733740 NR 3 HYD SYSTEM FLUID LOSS. QTY CONTINUED TO DRAIN WITH HYD PUMPS OFF. FOUND NR 3 ENGINE RIGHT HYD PUMP HOUSING CRACKE D. REPLACED PUMP. 2 L 7 3 4F 4 F RT A22WE E24NE 2002022800070 20020228 00070 NM 2002 2 28 DLM11020085 1 20020122 A 2150 22054501 ACM DOUG MD11 MD11 3023602 NM A/C BAY CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 802DE 48473 AIRCRAFT DIVERTED TO PDX DUE TO SMOKE/FUMES IN COCKPIT. ISOLATED NR 3 PACK AS SOURCE OF ODOR. PERFORMED DUCT BURN OUT 21-53-00-7 AND DEFERRED NR 3 PACK. 2 L 7 3 4F RT A22WE 2002022800071 20020228 00071 NM 2002 2 28 DLM11020109 1 20020130 A 3350 6044113 BATTERY PACK DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 802DE 48473 EMERGENCY LIGHTS REMAIN ON AT ALL TIMES. REPLACED BATTERY PACK. 2 L 7 3 4F RT A22WE 2002022800072 20020228 00072 NM 2002 2 28 371PA0004 1 20020225 A 3350 20181A BATTERY PACK BOEING 737 737306 NM DISCHARGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 Emergency exit lights inop aft galley overhead and R2 door. R&R Battery pack. 2 L 7 2 4F RT A16NE 2002022800073 20020228 00073 NM 2002 2 28 DLM11020125 1 20020201 A 2612 WARNING SYSTEM DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE COCKPIT FALSE INDICATION A DALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 805DE 32828 48476 733731 NUMBER 3 ENGINE (RIGHT) FIRE INDICATION. FOLLOWED PROCEDURE. BOTH BOTTLES FIRED WITH LIGHT REMAINING ON. DIVERT TO KB OS. EXTERNAL INSPECTION SHOWED NO EVIDENCE OF FIRE ON THE GROUND, INSPECTED ENG AND NO EVIDENCE OF FIRE. HARD FAULT NU MBER 3 ENG FIRE DETECTOR T/S PER FIM FAULTED FDCU INTERNAL FAULT AND LOOP A FAULT. INSPECTED ALL LOOPS AND HARNESSES NT F RESISTANCE FROM FDCU OKAY, OHMED AT ALL LOOPS RESISTANCE WITHIN LIMITS. REPLACED FDCU OPS NORM, RTS GOOD VERIFIED IN NR 2 SPOT ITEM FOLLOWED REINSTALLED ORIG, ALL NOW TEST NORM. 2 L 7 3 4F 4 F RT A22WE E24NE 2002022800074 20020228 00074 NE 2002 2 28 DLM11020158 2 20020209 A 7230 COMPRESSOR DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 ENGINE STALLED A DALA O OTHER E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 802DE 25423 48473 733741 ON T/O, NR 3 ENGINE HAD COMP STALL, ENGINE PARAMETERS CHANGED SLIGHTLY AND RETURNED TO NORMAL, N1 N2 EGT ALL NORMAL AFTE R T/O EAD MSG ENGINE 3 FADEC. MAINT FOLLOWED POM PROC P23-107 23-108. REPLACED NR 3 ENGINE PER ROUTINE CARD DECK TRANS MITTAL 8T301. 2 L 7 3 4F 4 F RT A22WE E24NE 2002022800075 20020228 00075 NM 2002 2 28 DLM88020030 1 20020107 A 3610 VALVE DOUG MD88 MD88 3023688 NM A/C BAY MALFUNCTIONED A DALA H G B DEACTIVATE SYST/CIRCUITS O2 MASK DEPLOYED EMER. DESCENT B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 981DL 53268 DURING CLIMBOUT, FLIGHT ATTENDANT REPORTED HAZE AND SMOKE IN CABIN. AFT RT SMOKE DETECTOR SOUNDED. CREW S/O LEFT PACK. THE A/C DEPRESSURIZED. PASSENGER MASKS DEPLOYED. CREW PERFORMED EMERGENCY DESCENT AND SMOKE REMOVAL CHECK LIST. ODO R SMELLED LIKE PLASTIC MELTING. FOUND DUCT DISCONNECTED AT ACM DIS. REMOVED COALESCER ASSY FOUND BAGS MELTED. REPLACE D ASSY'S AND BAGS. FOUND CAPS INSTALLED ON BOTH LT AND RT AUG VALVES. REPLACED LT AND RT AUG VALVES. REPLACED O2 MASK S AND GEN. CONNECTED DUCT ON ACM DISCHARGE AND PERFORMED TEST 5, 6, 7 PER PFHB A/C SYS CKS OUT, BOTH PACKS OPS NORMAL. 2 L 7 2 4F RT A6WE 2002022800076 20020228 00076 NM 2002 2 28 DLM88020039 1 20020111 A 5270 TARGET DOUG MD88 MD88 3023688 NM CARGO DOOR OUT OF ADJUST A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 952DL 49883 AFTER T/O ROLL STARTED AFT CARGO LIGHT CAME ON. REJECTED T/O AT 30 KTS. ADJUSTED PROX TARGET. 2 L 7 2 4F RT A6WE 2002022800077 20020228 00077 NE 2002 2 28 DLM88020046 2 20020113 A 7314 766342 PUMP DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A DALA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 SO 27 914DL 49545 726053 RT ENGINE SHUT DOWN TWO MINUTES INTO CLIMB, EGT WENT TO ZERO, HAD F/F AND N1AND N2. SHUT ENGINE DOWN, WINDMILLED FOR 15 MIN WITH POSITIVE OIL PRESS. REPLACED FUEL PUMP. 2 L 7 2 4F 4 F RT A6WE E9NE 2002022800078 20020228 00078 NM 2002 2 28 DLM88020049 1 20020114 A 3222 HF2001 VALVE DOUG MD88 MD88 3023688 NM NLG STRUT LEAKING A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 915DE 53420 NOSE GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR HANDLE RAISED. T/S FOUND SCHRADER VALVE LEAKING. REPLACED S AME AND TESTED IAW M/M. 2 L 7 2 4F RT A6WE 2002022800079 20020228 00079 NM 2002 2 28 DLM88020056 1 20020116 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 904DL 49535 EMERGENCY SEAT EXIT LIGHTING INOP IN BACK HALF OF AIRCRAFT. 2 L 7 2 4F RT A6WE 2002022800080 20020228 00080 NM 2002 2 28 DLM88020063 1 20020118 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 952DL 49883 SEAT 21D EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT, CHECKS GOOD. 2 L 7 2 4F RT A6WE 2002030500041 20020305 00041 EU 2002 3 5 MALA020173 1 20020227 A 3260 WARNING SYSTEM SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 450XJ 340B450 LANDING GEAR INTRANSIT LIGHT STAYS ILLUMINATED AFTER RETRACTION. CLEANED NLG & MLG, CHECKED WOW SWITCHES AND CANNON PLU GS FOR DAMAGE. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002022800081 20020228 00081 NM 2002 2 28 DLM88020092 1 20020125 A 5730 585628115 SEAL DOUG MD88 MD88 3023688 NM T/E FLAP BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 THE LT WING LOWER SKIN WAS FOUND WORN AT APPROX XRS 108 AT THE WING REAR SPAR. DAMAGE CAUSED BY BENT FWD EDGE OF SEAL A NGLE (P/N 5856281-15) OF FLAP HINGE FAIRING. DAMAGE WAS BLENDED SMOOTH AND REWORKED PER ERA 412307-14, REV A. 2 L 7 2 4F RT A6WE 2002022800082 20020228 00082 NM 2002 2 28 DLM88020107 1 20020129 A 5330 59360049 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CORROSION DAMAGE FOUND IN FUSELAGE SKIN AT FS 636, L30. CORROSION WAS REMOVED AND REPAIRED PER ERA 412319-14. 2 L 7 2 4F RT A6WE 2002022800083 20020228 00083 NM 2002 2 28 DLM88020110 1 20020130 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 967DL 53116 FIRST CLASS EMERGENCY LIGHTS INOP. REPAIRED BROKEN WIRE UNDER SEAT 1C AND REPLACED POWER SUPPLY AND BATTERY PACK. 2 L 7 2 4F RT A6WE 2002022800084 20020228 00084 NM 2002 2 28 DLM88020113 1 20020131 A 3260 PROXIMITY SENSOR DOUG MD88 MD88 3023688 NM NLG OUT OF ADJUST A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 908DL 49539 NOSE GEAR UNSAFE LIGHT AFTER RETRACTION. CYCLED GEAR GOT THREE GREEN IN DOWN POSITION. RETRACTED AGAIN AND NOSE GEAR W OULD NOT RETRACT. SERVICED NOSE STRUT AND ADJUSTED PROX SENSOR. 2 L 7 2 4F RT A6WE 2002022800085 20020228 00085 NM 2002 2 28 DLM88020130 1 20020201 A 2197 WIRE HARNESS DOUG MD88 MD88 3023688 NM A/C BAY BURNED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 932DL 49719 RIGHT PACK FAN POPS C/B. FOUND WIRE HARNESS BURNED THROUGH AND ARCED AGAINST AIRCRAFT STRUCTURE APPROXIMATELY 12 INCHES ABOVE THE RIGHT PACK FAN CONNECTOR. 2 L 7 2 4F RT A6WE 2002022800086 20020228 00086 NM 2002 2 28 DLM88020137 1 20020204 A 2560 P20700030 FLASHLIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 995DL 53362 AFT CENTER JUMPSEAT FORWARD EMERGENCY USE ONLY FLASHLIGHT STRAP BROKEN AND REMOVED. FLASHLIGHT LED NOT BLINKING. REPLA CED EMERGENCY FLASHLIGHT AND INSTALLED NEW EMERGENCY USE ONLY STRAP. 2 L 7 2 4F RT A6WE 2002022800087 20020228 00087 NM 2002 2 28 DLM88020138 1 20020204 A 2560 P20700030 FLASHLIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 995DL 53362 AFT JUMPSEAT AFT EMERGENCY USE ONLY FLASHLIGHT STRAP BROKEN AND REMOVED. FLASHLIGHT LED BLINKING OUT OF LIMITS. REPLAC ED EMERGENCY FLASHLIGHT AND INSTALLED NEW EMERGENCY USE ONLY STRAP. 2 L 7 2 4F RT A6WE 2002022800088 20020228 00088 NM 2002 2 28 DLM88020139 1 20020204 A 2910 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM THRUST REVERSER LOOSE A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 918DL 49583 VALVE THERE WAS A SLOW LOSS OF HYDRAULIC FLUID OF THE LEFT SYSTEM QUANTITY EN ROUTE. LEFT HYDRAULIC SYSTEM QUANTITY SHOWED 3 QUARTS ON LANDING AND TAXI IN. TIGHTENED PRESSURE LINE FOR LT THRUST REVERSER AT CONTROL VALVE. 2 L 7 2 4F RT A6WE 2002030400087 20020304 00087 NE 2002 3 4 COMA0260127 2 20020227 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RIGHT FAILED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING E T VIBRATION/BUFFET ENGINE CASE PENETRATION CL CLIMB 1 SO 01 991CA 9121 7216 807496 FLIGHT 5266 - DURING CLIMBOUT OF ATW RECEIVED ABNORMAL VIBRATION FROM THE RIGHT ENGINE. CREW DECLARED AN EMERGENCY AND PERFORMED AN IFSD. REPLACED THE RIGHT ENGINE ASSY. 2 L 7 2 4F 4 F RT A21EA E15NE 2002022800089 20020228 00089 EA 2002 2 28 COMA0260128 1 20020226 A 3010 434419881 SWITCH CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 926CA 7027 FLIGHT 5837 WING ANTI-ICE CAUTION DURING T/O.REPLACED THE LT WING SUFFICIENT HEAT SWITCH. 2 L 7 2 4F RT A21EA 2002022800090 20020228 00090 EA 2002 2 28 COMA0260129 1 20020227 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 796CA 7338 FLIGHT 6009 - ONE CABIN EMERGENCY LIGHT IS INOP.REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2002022800091 20020228 00091 EA 2002 2 28 COMA0260130 1 20020227 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 933CA 7040 FLIGHT 5409 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.LUBRICATED DOOR LOCKING MECH. OPS CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2002022800092 20020228 00092 EA 2002 2 28 COMA0260131 1 20020227 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 443CA 7539 FLIGHT 551 FLAPS FAILED AT 17 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002022800093 20020228 00093 NM 2002 2 28 CALA0200103 1 20020227 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM STA 1006-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND L/H LAV O/B WEB INTERCOSTAL CORRODED AT STA 1006-1016. THE INTERCOSTAL WAS REPLACED IAW SRM 53-10-02. 2 L 7 2 4F RT A16WE 2002022800094 20020228 00094 NM 2002 2 28 CALA0200107 1 20020227 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 867 WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND UPPER FUSELAGE SKIN WORN AT STA 867, RBL 6. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 214. 2 L 7 2 4F RT A16WE 2002022800095 20020228 00095 NM 2002 2 28 CALA0200109 1 20020227 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 940-993 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND Z-ANGLE CORRODED AT L-2 DOOR, STA 940-993. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002022800096 20020228 00096 NM 2002 2 28 CALA0200111 1 20020228 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 270-294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND SEAT TRACK CORRODED AT STA 270-294.5, RBL 35. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND DRAWING # 69-40352. 2 L 7 2 4F RT A16WE 2002022800097 20020228 00097 SO 2002 2 28 2002F00137 1 20020104 A 3210 14571033007 CAP EMB 145 EMB145LR 3260212 SO LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE LEFT MAIN LANDING GEAR LOWER FORWARD AND AFT BEARING CAP S. MAINTENANCE REPLACED THE NOSE LANDING CAPS IAW EMB145 MM 32-10-01-000-801-A AND 32-10-01-400-801-A. REF SIMA2002023 10. (M) 2 L 7 2 4T RT T00011AT 2002022800098 20020228 00098 SO 2002 2 28 SIMA200201601 1 20020116 A 3240 0132AFU SENSOR EMB 145 EMB145LR 3260212 SO RT MLG FAULTY A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 648AE 145225 DSM - FLT 4112 - CREW REPORTED THE NR 3 BRAKE TEMPERATURE INDICATOR HAD ERRATIC READINGS AFTER TAKEOFF. CREW DECLARED A N EMERGENCY DUE TO POSSIBLE LOCKED WHEEL. AIRCRAFT WAS LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED, MAINTENANCE RE MOVED AND REPLACED THE NR 3 BRAKE TEMPERATURE SENSOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED T O SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002022800124 20020228 00124 SO 2002 2 28 C2XA02CL062 1 20020227 A 3350 20131A BATTERY EMB 135 EMB135ER 3260203 SO CABIN DISCHARGED A C2XA K NONE P NO WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 27506 7130 115 145206 CLE FLIGHT# 2977 THE CREW REPORTED THE AISLE PATH EMERGENCY LIGHTING WAS INOPERATIVE AT ROW 9.MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002022800141 20020228 00141 SO 2002 2 28 SIMA200202301 1 20020102 A 5320 14522461011 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 714BZ 145260 ABI - DURING MBV INSPECTION MAINTENANCE FOUND, THE AFT DIAMOND GUSSET TO BE CORRODED AT FRAME 20. MAINTENANCE REPLACED THE GUSSET IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002022800142 20020228 00142 SO 2002 2 28 SIMA200202302 1 20020102 A 5320 14526437001 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 714BZ 145260 ABI - DURING MBV INSPECTION MAINTENANCE FOUND, THE FORWARD DIAMOND GUSSET TO BE CORRODED AT FRAME 20. MAINTENANCE REPLA CED THE GUSSET IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002022800143 20020228 00143 SO 2002 2 28 SIMA200202304 1 20020102 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 714BZ 145260 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE FORWARD SERVICE DOOR SILL CORRODED AT THE FORWARD AND AFT NUTPLATES. MAINTENANCE REPAIRED THE FORWARD SERVICE DOOR SILL IAW EMB REPAIR STATEMENT NGST-0012/02 AND SRM 51-40-02. (M) 2 L 7 2 4F RT TOOO11AT 2002022800144 20020228 00144 SO 2002 2 28 SIMA200202305 1 20020102 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 714BZ 145260 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND THE CENTER BEAM GUSSET CORRODED. MAINTENANCE REPLACED THE CENTER BEAM GU SSET IAW EMB SRM 51-40-02, 51-40-06, 51-20-03, AND 51-40-04. (M) 2 L 7 2 4F RT T00011AT 2002022800145 20020228 00145 SO 2002 2 28 SIMA200202306 1 20020102 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 714BZ 145260 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 20. MAINTENANCE REPAIRED LEFT OMEG A BEAM IAW EMB REPAIR STATEMENT NGST-0012/02. (M) 2 L 7 2 4F RT TOOO11AT 2002022800146 20020228 00146 SO 2002 2 28 SIMA200202307 1 20020102 A 5320 BEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 714BZ 145260 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND THE GALLEY CENTER BEAM CORRODED BETWEEN FRAMES 18 AND 23. MAINTENANCE RE PAIRED THE GALLEY CENTER BEAM IAW EMB REPAIR STATEMENT NGST-0012/02. (M) 2 L 7 2 4F RT TOOO11AT 2002022800147 20020228 00147 SO 2002 2 28 SIMA200202308 1 20020104 A 3210 14571035412 CAP EMB 135 EMB135LR 3260305 SO LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 714BZ 145260 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND THE LEFT MLG BEARING CAP TO BE CORRODED. MAINTENANCE REPLACED THE MAIN L ANDING GEAR BEARING CAP IAW EMB MM 32-10-10-400-801A. (M) 2 L 7 2 4F RT TOOO11AT 2002030400210 20020304 00210 NM 2002 3 4 F3LA200200078 1 20020224 A 5311 FRAME BOEING 737 7372Y5 1384554 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED FRAME AT STA 82.7, RBL 10, CRACKED AT SHEAR TIE ATTACH FASTENERS IN AFT CARGO COMP ARTMENT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-4. 2 L 7 2 4U RT A16WE 2002030100001 20020301 00001 2002 3 1 SWAA020437 4 20020226 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY FRAYING AT ROD ENDS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002030100002 20020301 00002 NM 2002 3 1 SWAA020439 1 20020226 A 5320 6547977 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED D CHECK, FOUND WEBS CRACKED (2 EA) AT BS 195, WL 208, LBL 31 AND RBL 31. REMOVED AND REPLACED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2002030100003 20020301 00003 NM 2002 3 1 SWAA020440 1 20020226 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAMS CORRODED AT BS 847 AND LBL 8, BS 812 AND RBL 3, BS 847 AND LB L 3. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002030100004 20020301 00004 NM 2002 3 1 SWAA020441 1 20020225 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR LOWER AND UPPER HINGE CUTOUTS FUSELAGE SKIN CRACKED IN CORNER RADIUS. R EPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002030100005 20020301 00005 WP 2002 3 1 ABXA010744 1 20020213 A 5310 9922937501 FRAME DOUG DC9 DC932 3022066 WP AFT CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 HEAVY CORROSION ON UPPER CARGO FLOOR FRAME AT STATION 929 ABOVE TWO FASTENERS THAT HOLD THE AFT LOWER CARGO DOOR HOLD OP EN HOOK. REMOVED CORROSION AND INSTALLED REPAIR IAW DC-9 SRM 53-05. 2 L 7 2 4F A6WE 2002030100006 20020301 00006 WP 2002 3 1 ABXA010745 1 20020213 A 5310 99577395 SHEAR TIE DOUG DC9 DC932 3022066 WP AFT CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 HEAVY CORROSION ON FRAME SPLICE ANGLE ON AFT SIDE OF FRAME AT STATION 943, ABOVE LONGERON 29 LEFT. REPLACED SPLICE ANGLE IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002030100007 20020301 00007 WP 2002 3 1 ABXA010749 1 20020219 A 5700 99193014 RIB DOUG DC9 DC932 3022066 WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 RIGHT WING LEADING EDGE RIB (JUST INBOARD OF #2 SLAT TRACK) CRACKED AT THE LOWER ATTACH FASTENER. REPAIRED RIB IAW DC-9 REA D957-43342. 2 L 7 2 4F A6WE 2002030100008 20020301 00008 WP 2002 3 1 ABXA010750 1 20020212 A 5310 3915129501N FITTING DOUG DC9 DC932 3022066 WP F.S. 604 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 LONGERON 29 RIGHT HAD CRACKED END FITTING AFT OF F.S. 604 "P" DOME. REPLACED END CAP IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002030100009 20020301 00009 NM 2002 3 1 02043423 1 20020212 A 3244 TIRE DORNER DO32 DO328300 NM LT MLG BLOWN A VTZA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 27 423FJ BOTH LT MAIN TIRES BLEW ON TAKEOFF FROM GSP TO LGA, CREW CONTACTED DISPATCH AND ATC AND ARRANGEMENTS WERE MADE TO DIVERT TO IAD. A/C CONDUCTED A FLY-BY AND LANDED SAFELY WITHOUT FURTHER INCIDENTS, PASSENGERS WERE DEPLANED ON TAXI WAY. 2 H 7 2 4T RT A55NM 2002030100010 20020301 00010 EA 2002 3 1 02058631 1 20020227 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 631BR 7255 DURING CRUISE OF THE FLIGHT FROM SAV TO ORD THE CREW REPORTED THAT THE MAIN CABIN DOOR HANDLE STOW CAUTION WARNING ILLUM INATED MOMENTARILY THEN EXTINGUISHED FOLLOWED BY A MOMENTARY ILLUMINATION OF THE MAIN CABIN DOOR WARNING CAUTION. THE C REW FOLLOWED QRH PROCEDURES, DIVERTED TO IND, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL CLEANED THE MAIN CABIN DOOR HANDLE PROXIMITY SENSOR. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002030100011 20020301 00011 EU 2002 3 1 0379 1 20020226 A 3260 A123733M2B UPLOCK SWITCH AMD FALC20 20F5 2730105 EU NLG OUT OF ADJUST E ERYA K NONE N FALSE WARNING AP APPROACH 1 CE 07 892SB 379 NOSE GEAR DOOR LIGHT FOR TRANSIT WILL NOT EXTINGUISH IN GEAR UP OR DOWN SELECTION AND IS INTERMITTENT. NOSE GEAR UPLOCK AND NOSE GEAR DOOR ACTUATOR SWITCH STOPS WERE ADJUSTED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A7EU 2002030100019 20020301 00019 NE 2002 3 1 HEEA077700 1 20020125 A 7697 WIRE SKRSKY S76 S76A 8143006 NE ENGINE CONTROL BROKEN E HEEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 SW 03 5435V 760158 ON APPROACH TO LANDING THE NR 2 ENGINE WOULD NOT RESPOND WHEN COLLECTIVE PULLED. REPAIRED BROKEN WIRE AT BEEP MOTOR CONN ECTOR. 1 G 7 2 3U H1NE 2002030100023 20020301 00023 NM 2002 3 1 2002UALA00277 1 20020215 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 BODY STATION 178 BULKHEAD WEB IS CRACKED AT RBL 5 WL 198 AND WL 201. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLERS AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050200065 20020502 00065 NM 2002 5 2 2002UALA00278 1 20020215 A 2133 VFT300B00 OUTFLOW VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN PRESSURE FAULTY A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 841UA 1545 VENT SKIN VALVE FAULT ON TAKEOFF. AVIONICS SKIN AIR OUTLET VALVE ELECTRONIC CENTRALIZED AIRCRAFT MONITORING POSITION OS CILLATES BETWEEN AMBER AND CLOSED GREEN. REPLACED FAULTING SKIN AIR OUTLET VALVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2002030100024 20020301 00024 EU 2002 3 1 2002UALA00279 1 20020216 A 2934 C60AA0062 SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYDRAULIC SYS FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 403UA 442 DIVERTED TO MIA DUE TO HYDRAULIC QUANTITY LOSS INDICATION. CONFIRMED GREEN SYSTEM HYDRAULIC QUANTITY RESERVOIR FULL, NO EXTERNAL LEAKS NOTED. REPLACED LOW LEVEL SENSOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2002030100025 20020301 00025 NM 2002 3 1 2002UALA00280 1 20020218 A 5270 WARNING SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 834UA 1420 AFT CARGO DOOR ECAM DOOR PAGE INDICATIONS INOPERABLE. ON DEPARTURE ECAM DOORS, AFT CARGO CAME ON. 2 L 7 2 4F 4 F RT A28NM E40NE 2002030700071 20020307 00071 NM 2002 3 7 2002UALA00281 1 20020217 A 3231 SEQUENCE VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT MLG MALFUNCTIONED A UALA K NONE J WARNING INDICATION UK UNKNOWN 1 WP 29 775UA 26947 NO DOWNLOCK INDICATION FOR LEFT MAIN GEAR ON FIRST ATTEMPT. SECOND ATTEMPT NORMAL. PER CREW VERBAL FLAPS STEADY AT 20 DEGREES CREW OBSERVED GEAR PAGE WITH NO LOCK INDICATION PRIOR TO STATUS MESSAGES. ONCE GEAR STABLE IN UP POSITION, 2ND ATTEMPT NORMAL, 2 MILES FROM LANDING. BASED ON INDICATIONS IN FLIGHT IT APPEARED THE LT MLG DOOR WAS OPEN BUT THE LT GE AR DID NOT EXTEND. RT MLG AND NLG INDICATED DOWN AND LOCKED. AIRCRAFT WAS JACKED AND LANDING GEAR WAS CYCLED SEVERAL T IMES WITH NO DEFECTS OR ABNORMAL INDICATIONS NOTED. THE LT MLG DOOR OPERATED SEQUENCE VALVE WAS REPLACED AS PRECAUTIONA RY. AIRCRAFT HAS FLOWN SEVEN FLIGHTS AS OF THIS ENTRY WITH NO PROBLEMS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002030700073 20020307 00073 NM 2002 3 7 2002UALA00282 1 20020220 A 2497 1701766 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BACKUP GEN DAMAGED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 773UA 26929 CREW HAD AN EICAS MESSAGE BACK UP GEN RT CMC MESSAGE TO SAM INDICATED OIL PRESSURE LOW. FLIGHT RETURNING TO FIELD AND L ANDING OVERWEIGHT. THE RIGHT BACKUP GENERATOR (BUG) AND BACKUP GENERATOR CONVERTER WERE REPLACED. THE FINAL FIX WAS TO REPLACE THE BUG WIRE HARNESS PER AIRCRAFT AMIS HISTORY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002032700039 20020327 00039 NM 2002 3 27 2002UALA00285 1 20020216 A 2410 CSD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE LACK OF LUBE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 350UA 24301 UNSCHEDULED LANDING DUE TO CSD LOW OIL INDICATION. MAINTENANCE CREWS FOUND THE NR 2 CSD OIL QUANTITY LOW. THE NR 2 CSD WAS SERVICED TO ITS PROPER LEVEL AND THE NR 2 CSD MAGNETIC CHIP DETECTOR WAS CHECKED WITH NO MATERIAL FOUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030100027 20020301 00027 EU 2002 3 1 2002UALA00286 1 20020217 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 476UA 1508 DOOR 2L EMERGENCY EXIT LIGHT INOPERABLE. REINSTALLED POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2002030100031 20020301 00031 NE 2002 3 1 HEEA077701 2 20020125 A 7200 ENGINE SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE NACELLE LEAKING E HEEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 854PH 1282 3248 LEAKING FUEL OUT OF DRAIN WHEN ENGINE RUNNING. 1 G 7 1 3U 3 U H9EU E19EU 2002030100032 20020301 00032 NM 2002 3 1 2002UALA00291 1 20020218 A 5310 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 BODY STATION 1263 STRINGER 20R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002030100033 20020301 00033 NM 2002 3 1 SWAA020443 1 20020227 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 756SA 27872 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROW'S 9 AND 11. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002030100034 20020301 00034 2002 3 1 SWAA020444 4 20020226 A 2565 6557463 BRACKET BOEING 737 7375H4 138449D NM AFT ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FLOOR ATTACH BRACKET LOOSE. SECURED B RACKET PER MM. 2 L 7 2 4F RT A16WE 2002030100035 20020301 00035 2002 3 1 SWAA020445 4 20020226 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002030100036 20020301 00036 NM 2002 3 1 SWAA020446 1 20020227 A 2121 6454051 FAN BOEING 737 7373H4 1384600 NM A/C DIST. BAY OVERTEMP A SWAA O OTHER M OVER TEMP CR CRUISE 1 SW 07 343SW 24151 FLIGHT ATTENDANTS REPORTED BURNING ODOR IN CABIN, SMELL ALSO NOTED IN COCKPIT. REMOVED AND REPLACED AIR CONDITIONING RE CIRCULATION FAN PER MM. 2 L 7 2 4F RT A16WE 2002030100037 20020301 00037 NM 2002 3 1 SWAA020448 1 20020227 A 5520 65C26384 TAB BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002030100038 20020301 00038 NM 2002 3 1 SWAA020450 1 20020227 A 5520 BACB28AM07 BUSHING BOEING 737 7373H4 1384600 NM LT/RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED C3 CHECK, SWA SI 11111-55, BOTH LT AND RT ELEVATOR TAB FWD LOWER HANGER BUSHINGS WORN. REMOVED AND REP LACED TAB BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002031100045 20020311 00045 NM 2002 3 11 02FDEA00154 1 20020224 A 5315 BAC1518338 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION (C53-224-01,1) ON FLOORBEAM UPPER CHORD BS 560, LBL 50. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 8. 2 L 7 3 4F RT A3WE 2002030700043 20020307 00043 NM 2002 3 7 02FDEA00155 1 20020221 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION ON LOWER CHORD BS 1070 FLOORBEAM LBL 45, RBL 50, WL 200. REMOVED AND REPLACED FLOORBEAM PER SRM 51-30-2, 53-1 0-1 FIG 4 & 53-10-8 FIG 2. 2 L 7 3 4F RT A3WE 2002031400022 20020314 00022 NM 2002 3 14 02FDEA00157 1 20020226 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 BS 580, RBL 2, WL 156 FRAME INNER CHORD CRACKED. REMOVED AND REPLACED FRAME PER SRM 51-40-3, 51-20-001. 2 L 7 3 4F RT A3WE 2002031300043 20020313 00043 NM 2002 3 13 02FDEA00160 1 20020220 A 5310 SHEAR TIE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION ON SHEAR TIE BS 950F, RBL 7, WL 137. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-1, 53-10-4 FIG 15 & EA 7-53 10-62782. 2 L 7 3 4F RT A3WE 2002030700046 20020307 00046 NM 2002 3 7 02FDEA00161 1 20020220 A 5310 SHEAR TIE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION C53-113-01(2) ON SHEAR TIE BS 1130, LBL 8-10, WL 148. REMOVED AND REPLACED SHEAR TIE PER THE SRM. 2 L 7 3 4F RT A3WE 2002031300044 20020313 00044 NM 2002 3 13 02FDEA00163 1 20020220 A 5310 SHEAR TIE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION ON SHEAR TIE BS 970, RBL 8, WL 136. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-1, 53-10-4 FIG 5 & EA 7-5310 -62782. 2 L 7 3 4F RT A3WE 2002031300045 20020313 00045 NM 2002 3 13 02FDEA00164 1 20020220 A 5310 SHEAR TIE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION ON SHEAR TIE BS 970, LBL 8, WL 136. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-1, 53-10-4 FIG 15 & EA 7-531 0-62782. 2 L 7 3 4F RT A3WE 2002030700048 20020307 00048 NM 2002 3 7 02FDEA00165 1 20020220 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION ON LOWER SURFACE OF BS 344 FLOORBEAM. REMOVED AND REPLACED FLOORBEAM PER SRM 51-10-6, 53-10-8. 2 L 7 3 4F RT A3WE 2002031400023 20020314 00023 NM 2002 3 14 02FDEA00166 1 20020218 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MECHANICAL DAMAGE TO FRAME BS 804 BELOW STR 6L. REMOVED AND REPLACED FRAME PER SRM 53-10-4 FIG 1. 2 L 7 3 4F RT A3WE 2002030700049 20020307 00049 NM 2002 3 7 02FDEA00167 1 20020220 A 5310 SHEAR TIE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION C53-113-01(2) ON SHEAR TIE BS 1130, LBL 8-10, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-1, 53-10-4 , 51-10-2. 2 L 7 3 4F RT A3WE 2002030700050 20020307 00050 NM 2002 3 7 02FDEA00168 1 20020223 A 5315 BAC1518338 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FLOORBEAM UPPER CHORD ELONGATED HOLE BS 1030, LBL 18, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 8. 2 L 7 3 4F RT A3WE 2002030100039 20020301 00039 NM 2002 3 1 2002UALA00292 1 20020218 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 BODY STATION 852-855 LBL 30-34 FLOORBEAM CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM P ARTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002032500047 20020325 00047 NM 2002 3 25 2002UALA00293 1 20020217 A 2421 745329C IDG BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 667UA 29239 LEFT ENGINE GENERATOR LIGHT ILLUMINATED PRIOR TO ETOPS ENTRY POINT. DISCONNECTED GENERATOR AND STARTED APU. FLIGHT RET URNED TO SFO. REPLACED NR 1 INTEGRATED DRIVE GENERATOR, OPS CHECKED NORMAL. SHOP FINDINGS: METAL FOUND IN FILTER, HYD RAULIC LOG FAILURE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002030100040 20020301 00040 NM 2002 3 1 2002UALA00294 1 20020220 A 5315 FLOORBEAM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 205UA 28714 STATION 246 FLOORBEAM MID CHORD IS CRACKED IN CUTOUT RADIUS OF UPPER VERTICAL LEG AT LBL 38.5. MAJOR REPAIR ACCOMPLISHE D. MANUFACTURED AND INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002030100041 20020301 00041 NM 2002 3 1 2002UALA00295 1 20020221 A 5330 SKIN BOEING 777 777222 1385219 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 797UA 26924 RIGHT HAND EXT FUSELAGE SKIN CRACKED AT STATION 2276 (FWD OF HORIZ STAB FAIRING TRACK). MAJOR REPAIR ACCOMPLISHED. REP AIR AND EDDY CURRENT ACCOMPLISHED. 2 L 7 2 4F 4 F RT T0001SE E24NE 2002030100042 20020301 00042 NM 2002 3 1 2002UALA00297 1 20020221 A 5330 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 797UA 26924 LEFT HAND FUSELAGE SKIN CRACKED STATION 2276 (FWD OF HORIZ STAB FAIRING TRACK). MAJOR REPAIR ACCOMPLISHED. REPAIRED AN D EDDY CURRENT ACCOMPLISHED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002030100043 20020301 00043 NM 2002 3 1 2002UALA00298 1 20020219 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 EEL STRIP IN FRONT OF SEAT 1E NOT OPERATING. REPAIRED DAMAGED POWER FEED PER GNMM 2-0-15-5. OPERATIONALLY CHECKED NORM AL. 2 L 7 2 4F 4 F RT A1NM E24NE 2002030100047 20020301 00047 NM 2002 3 1 2002UALA00299 1 20020221 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 MAIN CABIN FLOORBEAM AT STATION 852, LBL 60, T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2002030100048 20020301 00048 WP 2002 3 1 35A501 2 20020226 A 7200 ENGINE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP LEFT MALFUNCTIONED E ERYA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 CE 07 326HG 6119 362 35A501 P89362 ENGINE START, TAXI, AND CLIMB UNEVENTFUL. CLIMB FROM 5000 FT TO 15000 FT, TURNED ON ANTI-ICE SYSTEMS, PRIOR TO ENTERING CLOUDS AT APPROX 6000 FT, LT ENGINE FLUCTUATED AND ROLLED BACK SHORTLY AFTER ENTERING CLOUDS. ENCOUNTERED ICING SHORTL Y AFTER ENTERING CLOUDS. TRIED TO CATCH ROLL BACK BY TURNING ON IGNITIONS WITH NO SUCCESS. SET UP FOR STARTER ASSISTED START. ENGINE CAME UP TO SPEED WITH A SLIGHT RUMBLE. UPON DISENGAGING STARTER, ENGINE ROLLED BACK AGAIN. SET UP FOR A FUEL COMPUTER OFF AIR START. AGAIN ENGINE CAME UP TO SPEED WITH A MORE NOTICEABLE RUMBLE. UPON DISENGAGING STARTER, E NGINE ROLLED BACK AGAIN. SECURED ENGINE AND RETURNED TO DEPARTURE AIRPORT. (362.7 HOURS SINCE LAST MPI) 2 L 7 2 4F 4 F A10CE E6WE 2002030100049 20020301 00049 SW 2002 3 1 HEEA077710 1 20020118 A 2435 206062200113 STARTER GEN BELL 407 407 1182206 SW ENGINE FAILED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 740PH 53435 NO STARTER ROTATION WITH VOLTAGE APPLIED. 1 G 7 1 3U O H2SW 2002030100050 20020301 00050 SW 2002 3 1 HEEA077711 1 20020118 A 2435 BRUSHES BELL 407 407 1182206 SW STATER GEN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 742PH 3284 97287 53461 BRUSHES WORN ON 300 HOUR INSPECTION. 1 G 7 1 3U O H2SW 2002030100051 20020301 00051 SW 2002 3 1 HEEA077713 1 20020118 A 6220 RETAINER BELL 206 206L3 1182108 SW SEAL LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 SEAL RETAINER SPINNING IN GRIP BORE DUE TO UNBONDING. 1 G 7 1 3U H2SW 2002030100052 20020301 00052 WP 2002 3 1 ABXA010742 1 20020213 A 5320 991015420 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 FRAME FOOT, WEB CRACKED AT FS 996, LONGERON 18 LEFT. REPLACED WEB IAW DC-9 SRM 53-11-3 AND 51-30-5. 2 L 7 2 4F A6WE 2002030100054 20020301 00054 SW 2002 3 1 HEEA077715 1 20020121 A 6330 406040056101 CASE 206040004107 BELL 206 206L3 1182108 SW TRANSMISSION CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21497 4489 B51694 51518 CRACK INDICATIONS ON WEBS OF TRANSMISSION. 1 G 7 1 3U H2SW 2002030100056 20020301 00056 WP 2002 3 1 ABXA010743 1 20020213 A 5320 99105035 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 CUSP WEB CRACKED BETWEEN FS 945 AND 965, LEFT SIDE. REPAIRED CRACKED AREA IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002030100059 20020301 00059 SW 2002 3 1 HEEA077727 1 20020122 A 6420 407012101111 HUB BELL 407 407 1182206 SW TAIL ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 1710 53159 TAIL ROTOR HUB HAS SEPARATED RUBBER. 1 G 7 1 3U O H2SW 2002030100060 20020301 00060 SW 2002 3 1 HEEA077728 1 20020125 A 7500 CLAMP BELL 412 412 1182202 SW TAIL ROTOR DAMAGED E HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 7128R 36007 IN CRUISE FLIGHT, THE BAGGAGE FIRE LIGHT ILLUMINATED. PRIOR TO LANDING LIGHT WENT OUT, BUT CAME BACK ON DURING COOL DO WN. REPAIRED CHAFED WIRE AT ADEL CLAMP IN TAIL ROTOR SERVO COMPARTMENT. 1 G 7 2 4U H4SW 2002030100061 20020301 00061 SW 2002 3 1 HEEA077729 1 20020125 A 2700 214001370103 ACTUATOR BELL 214 214ST 1182106 SW FLIGHT CONTROLS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 ACTUATOR WILL NOT ALLOW AARS PITCH CHANNEL TO COME ON LINE. 2 G 7 2 4U H10SW 2002030100062 20020301 00062 SW 2002 3 1 HEEA077730 1 20020125 A 6320 BEARING PHIPBH40701F BELL 407 407 1182206 SW COOLER BLOWER WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 402PH PHI0024 53159 OIL COOLER BLOWER HAS WORN BEARINGS. 1 G 7 1 3U O H2SW 2002030100067 20020301 00067 SW 2002 3 1 HEEA077736 1 20020128 A 7921 406360500101 OIL COOLER BELL 407 407 1182206 SW ENGINE CONTAMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 495PH 53397 METAL CONTAMINATION. 1 G 7 1 3U O H2SW 2002030100068 20020301 00068 SW 2002 3 1 HEEA077738 1 20020128 A 3212 407350302101 FLOAT BELL 407 407 1182206 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 496PH 53398 EMERGENCY FLOAT LEAKING. HOLE IN AFT LEFT BAG. 1 G 7 1 3U O H2SW 2002030100070 20020301 00070 NM 2002 3 1 ABXA010751 1 20020219 A 5753 113T13218 FITTING BOEING 767 767200 1385120 NM T/E FLAP DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 768AX 22786 WHILE PERFORMING AD 2002-01-15, THE RIGHT OUTBOARD, OUTBOARD 3-10 LINK, AFT FITTING, WILL NOT TAKE GREASE. REMOVED AND REPLACED THE FITTING IAW B767 MM 27-51-274. 2 L 7 2 4F RT A1NM 2002030100071 20020301 00071 NM 2002 3 1 ABXA010752 1 20020218 A 5753 113T13218 FITTING BOEING 767 767200 1385120 NM T/E FLAP DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 785AX 23018 RIGHT OUTBOARD FLAP, OUTBOARD 3-10 LINK, AFT FITTING, WOULD NOT TAKE GREASE WHILE PERFORMING AD 2002-01-15. REMOVED AND REPLACED FITTING IAW B767 MM 27-51-274. 2 L 7 2 4F RT A1NM 2002030100072 20020301 00072 NM 2002 3 1 ABXA010753 1 20020217 A 5753 113T13218 FITTING BOEING 767 767200 1385120 NM T/E FLAP DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 767AX 22785 RIGHT OUTBOARD FLAP, OUTBOARD 3-10 LINK, AFT FITTING, WOULD NOT TAKE GREASE WHILE PERFORMING AD 2002-01-15. REMOVED AND REPLACED FITTING IAW B767 MM 27-51-274. 2 L 7 2 4F RT A1NM 2002030100073 20020301 00073 SO 2002 3 1 C2XA02CL061 1 20020228 A 3234 14532170401 CONTROL HANDLE EMB 145 EMB145ER 3260211 SO COCKPIT FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 14943 9536 145040 CLE FLIGHT 3284 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT ON THE FIRST ATTEMPT AFTER TAKEOFF. THE CREW RECYC LED THE GEAR HANDLE AND THE GEAR DID RETRACT ON THE SECOND ATTEMPT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002030100074 20020301 00074 SO 2002 3 1 C2XA02IA043 1 20020227 A 3230 355022002 CONTROL UNIT EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 13949 145057 IAH- THE CREW NOTED AFTER TAKEOFF THAT THE NOSE GEAR DOOR HANGS AFTER RETRACTION, CLOSES AT 235 KTS. MAINTENANCE REMOVE D AND REPLACED THE LGEU, PERFORMED A OPERATIONAL CHECK OF LANDING GEAR SYSTEM. NO DEFECTS NOTED AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002030100075 20020301 00075 NM 2002 3 1 CALA0200102 1 20020227 A 3397 WIRE HARNESS BOEING 757 757224 1384958 NM CABIN DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND EMERGENCY LIGHTING WIRING HARNESS BETWEEN LT SEAT ROWS 12-22 CRUSHED AND DAMAGED IN SEVERAL PLACES. TH E WIRING HARNESS WAS REPAIRED IAW BSWPM CHAPTER 20-10-13. 2 L 7 2 4F RT A2NM 2002030100076 20020301 00076 NM 2002 3 1 CALA0200104 1 20020227 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 986.5-993.5, RBL 13-44. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW S RM 51-10-02. 2 L 7 2 4F RT A16WE 2002030100077 20020301 00077 NM 2002 3 1 CALA0200105 1 20020227 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND A 1 INCH CRACK IN UPPER CHORD ON WEB BETWEEN STA 500D AND 520, BL 0. THE CHORD WAS REMOVED AND REPLACE D IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002030100078 20020301 00078 NM 2002 3 1 CALA0200106 1 20020227 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND RT LAV WALL SUPPORT CORRODED AT STA 993.5, RBL 13-44. THE WALL SUPPORT WAS REMOVED AND REPLACED IAW SR M 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002030100079 20020301 00079 NM 2002 3 1 CALA0200108 1 20020227 A 5320 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND FLOOR H-STRAP CORRODED AT STA 1022-1026, LBL 3. A NEW H-STRAP WAS INSTALLED IAW SRM 51-10-2 AND 51-30- 3. 2 L 7 2 4F RT A16WE 2002030100080 20020301 00080 NM 2002 3 1 CALA0200110 1 20020227 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 986.5-1006, LBL 10-20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SR M 51-10-02. 2 L 7 2 4F RT A16WE 2002030100081 20020301 00081 SO 2002 3 1 CHQ000125 1 20020228 A 2760 CONTROL UNIT EMB 145 EMB145 3260210 SO SPOILER SYS MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 294 145497 SPOILER FAIL MESSAGE ON EICAS. REMOVED AND REPLACED SPOILER CONTROL UNIT, SPOILER SYSTEM TESTS GOOD AT THIS TIME. 2 L 7 2 4F RT T00011AT 2002030100083 20020301 00083 NM 2002 3 1 QXEA0200299 1 20020219 A 3350 6138001 BATTERY PACK BOMBDR DHC8 DHC8401 NM CABIN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 1508 4046 PDX-CEILING EMERGENCY LIGHT AT STA X33.50, FORWARD LEFT HAND EXTERIOR EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN SELECTED O N. INSTALLED NEW BATTERY PACKS IN FORWARD EMERGENCY LIGHT SYSTEM POWER SUPPLY UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002030100084 20020301 00084 SO 2002 3 1 RAIA00202083 1 20020226 A 3411 0851HU PITOT TUBE EMB 145 EMB145LR 3260212 SO INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 812HK 1670 145373 5251-PIT- CREW ALERTING SYSTEM MESSAGE "PITOT #1 INOP". MAINTENANCE REMOVED AND REPLACED THE #1 PITOT PROBE, OPS CK OK. 2 L 7 2 4T RT T00011AT 2002030100085 20020301 00085 EU 2002 3 1 RAIA00202084 1 20020226 A 2760 45150560 STALL WARNING AEROSP ATR42 ATR42300 8680920 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 421TE 4275 1968 102 5589-STL- DURING TAXI, ALPHA PROBE POPPED CIRCUIT BREAKER. MAINTENANCE REMOVED AND REPLACED THE ALPHA PROBE, OPS CK OK. 2 H 7 2 4T RT A53EU 2002030100086 20020301 00086 EU 2002 3 1 RAIA00202085 1 20020226 A 5610 NP1588011 WINDSHIELD AEROSP ATR42 ATR42300 8680920 EU CRACKED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 423TE 18270 119 5588-SGP- DURING CLIMB CAPTAINS WINDSHIELD CRACKED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD, IAW ATR MM 56-11-00. 2 H 7 2 4T RT A53EU 2002030400217 20020304 00217 NM 2002 3 4 F3LA200200085 1 20020224 A 5230 SKIN BOEING 737 73736E 138443A NM CARGO DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 315FL 3460 25159 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO DOOR INNER SKIN CRACKED AT LIGHTENING HOLE IN LOWER AFT CORNER. STOP DR ILLED CRACK AT LIGHTENING HOLE ON LOWER AFT CORNER OF AFT CARGO DOOR AND REPAIRED PER SRM 51-50-2 AND 51-70-13. 2 L 7 2 4F RT A16WE 2002030100087 20020301 00087 WP 2002 3 1 MWEA020148 1 20020301 A 5520 991848025 SKIN DOUG DC9 DC932 3022066 WP LH ELEVATOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 LEFT ELEVATOR LOWER SKIN DENTED AT APPROXIMATELY XE 184, APPROXIMATELY 2 INCHES BY 3/8 INCH .035 DEEP. -- FABRICATED A ND INSTALLED SKIN. 2 L 7 2 4F A6WE 2002030100088 20020301 00088 NM 2002 3 1 F3LA200200087 1 20020227 A 5320 ANGLE BOEING 737 7372Y5 1384554 NM STA. 727 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT PANEL ATTACH ANGLE AT STA. 727, RBL 21 TO RBL 2 5. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-30-2, 51-10-2 51-30-3 AND BOEING DRAWING 65-55726. 2 L 7 2 4U RT A16WE 2002030400219 20020304 00219 NM 2002 3 4 F3LA200200088 1 20020227 A 5320 BEAM BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED BEAM IN FWD BULKHEAD, AFT CARGO COMPARTMENT, CORRODED AT NUT PLATE ATTACHMENT POIN T FOR LOWER DUCT SHROUD BRACKETS AT LBL 20 AND WL 160. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 51-40-4. 2 L 7 2 4U RT A16WE 2002030100089 20020301 00089 EU 2002 3 1 USAABA02005 1 20020213 A 3350 32146220 POWER SUPPLY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 671UW 0323 PHL - THE EMERGENCY LIGHT EMERGENCY POWER SUPPLY UNITS 11WL, 13WL, AND 17WL FAILED TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNITS. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A46NM 2002030100090 20020301 00090 NM 2002 3 1 USAABB02012 1 20020205 A 3350 8621006 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 608AU 22204 MCO - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 9, 18, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002030400220 20020304 00220 NM 2002 3 4 F3LA200200089 1 20020227 A 2761 MOUNT BRACKET BOEING 737 7372Y5 1384554 NM SPOILER CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED LT WING REAR SPAR MOUNT TEE FOR NR 4 SPOILER OUTBOARD ACTUATOR MOUNT BRACKET CORRO DED. REPLACED BRACKET AND BUSHING PER SRM 51-30-5, BOEING OHM 20-50-03 AND BOEING SOPM 20-50-01. 2 L 7 2 4U RT A16WE 2002030100091 20020301 00091 NM 2002 3 1 USAABB02015 1 20020211 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002030100092 20020301 00092 WP 2002 3 1 USAAD02002 1 20020119 A 3230 LANDING GEAR DOUG DC9 DC982 3022082 WP NLG & MLG LACK OF LUBE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 830US 49443 CLT-MDT - FLT 910 - AFTER TAKEOFF, WHEN THE GEAR HANDLE WAS PLACED IN THE UP POSITION, THE RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. WHEN PLACING THE GEAR HANDLE DOWN, THE UNSAFE LIGHT EXTINGUISHED AND 3 GREEN LIGHTS ILLUMINATED. MAINTENANCE FOUND THE GEARS IN NEED OF LUBRICATION. LUBRICATED AND CYCLED THE LANDING GEARS. THE RIGHT MAIN GEAR UP P ROX. SENSOR WAS REPLACED PRECAUTIONARY. (M) 2 L 7 2 4F A6WE 2002030100096 20020301 00096 WP 2002 3 1 IXXA0200006S 1 20020107 A 5754 WING DOUG DC8 DC871F 302199D WP LEADING EDGE CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 823BX 83172 2873 46064 DURING ROUTINE C-CHECK INSPECTION A CRACK WAS DETECTED ON THE RIGHT WING CENTER LEADING EDGE FORWARD SIDE AT STATION WS4 85. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER EDP44-01. 2 L 7 4 4F RT 4A25 2002030100097 20020301 00097 WP 2002 3 1 USAAD02008 1 20020209 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 823US 49142 IND - THE FORWARD CEILING AND OVERWING EXIT SIGN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2002030100098 20020301 00098 WP 2002 3 1 USAAD02009 1 20020209 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 826US 48026 IND - TWO SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS AND THE TAILCONE EMERGENCY LIGHT REMOTE RECEIVER WERE INOPERATIVE. MA INTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2002030100099 20020301 00099 EU 2002 3 1 USAAF02003 1 20020212 A 2910 NAS161210 O-RING FOKKER F28 F28MK0100 4990807 EU HYDRAULIC SYS BROKEN A USAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 19 855US 11283 ORF-PHL - FLT 982 - DURING DESCENT, THE SYSTEM 1 HYDRAULIC LOW QUANTITY INDICATION ALERTED, FOLLOWED BY LOSS OF SYSTEM 1 HYDRAULICS. THE LANDING GEAR WAS LOWERED USING THE ALTERNATE PROCEDURE AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAIN TENANCE REPLACED A BROKEN O-RING ON THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP QUICK DISCONNECT. (M) 2 L 7 2 4F RT 2002030100100 20020301 00100 EU 2002 3 1 USAASA02007 1 20020111 A 3350 EO242A28A0 RELAY AIRBUS 320 A320214 3930316 EU CABIN FAILED A USAA K NONE O OTHER DE DESCENT 1 EA 19 103US 0861 LGA - THE EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WHEN PED SWITCH IS TURNED ON. MAINTENANCE REPLACED RELAY. OPERATIONA LLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2002030100101 20020301 00101 EU 2002 3 1 USAASA02010 1 20020117 A 3350 CONNECTOR AIRBUS A321 A321211 3930370 EU CABIN NOT SEATED A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 166US 1436 LGA - THE EMERGENCY LIGHT TEST GAVE EMERGENCY POWER SUPPLY UNIT 'INT LOAD' FAULTS FOR THE MID RIGHT AND LEFT, AND EXIT R IGHT AND LEFT POSITIONS. MAINTENANCE REMOVED AND REINSTALLED CANNON PLUGS ON SEVERAL EMERGENCY POWER SUPPLY UNITS. SYS TEM OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2002030100102 20020301 00102 EU 2002 3 1 USAASA02012 1 20020119 A 3350 Z040H0005110 DECODER AIRBUS A319 A319112 3930323 EU CABIN FAILED A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 726US 6928 1136 RDU - DURING THE EMERGENCY LIGHT TEST, RECEIVED 'EPSU COMM EMER R' MESSAGE. MAINTENANCE REPLACED A DECODER/ENCODER UNIT . OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002030100103 20020301 00103 EU 2002 3 1 USAASA02014 1 20020128 A 3350 321430 BATTERY PACK AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 753US 1326 DCA - THE EMERGENCY BATTERY LIGHTS FAILED TEST. MAINTENANCE REPLACED BATTERY PACK. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002030100104 20020301 00104 EU 2002 3 1 USAASA02015 1 20020201 A 3350 32145510 POWER SUPPLY AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 175US 1496 LAX - AN EMERGENCY POWER SUPPLY UNIT AT THE R-3 DOOR FAILED TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE R-3 DOOR. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002030100105 20020301 00105 2002 3 1 USAASA02016 4 20020201 A 2312 EVR750030100A TRANSCEIVER AIRBUS A319 A319112 3930323 EU E/E BAY MALFUNCTIONED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 751UW 1317 PVD - FLT 6422 - EN ROUTE DCA-BOS, DURING CRUISE, THE FLIGHT CREW HEARD STATIC SOUNDS COMING FROM THE VHF RADIOS. AFTER SWITCHING BACK TO VHF 1, THE CREW BEGAN TO SMELL SMOKE. THE FLIGHT CREW DONNED SMOKE MASKS. THE FLIGHT DIVERTED TO PV D, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 VHF TRANSCEIVER. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002030100106 20020301 00106 EU 2002 3 1 USAASA02017 1 20020203 A 3350 CONNECTOR AIRBUS A319 A319112 3930323 EU CABIN DIRTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 721UW 1095 DCA- RECEIVED, 'EPSU EXT LOAD AFT L', MESSAGE, WHEN PERFORMING THE EMERGENCY LIGHTS TEST. MAINTENANCE CLEANED AND RESEC URED THE AFT LEFT DOOR SLIDE CONNECTOR. SYSTEM BITE CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2002030100107 20020301 00107 EU 2002 3 1 USAASA02018 1 20020207 A 3350 321430 POWER SUPPLY AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 175US 1496 LGA - THE EMERGENCY LIGHTS TEST GAVE EMERGENCY POWER SUPPLY UNIT INTERNAL FAULTS FOR BOTH LEFT AND RIGHT, AND EXIT LEFT AND RIGHT POSITIONS. (M) 2 L 7 2 4F RT A28NM 2002030100108 20020301 00108 EU 2002 3 1 USAASA02019 1 20020209 A 3350 CONNECTOR AIRBUS A319 A319112 3930323 EU CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 714US 1046 RDU - THE LEFT FORWARD ESCAPE SLIDE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE RECONNECTED LOOSE PLUG BEHIND THE SLIDE ASSEMBLY. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002030100109 20020301 00109 NM 2002 3 1 USAASB02005 1 20020107 A 2910 693731768 MODULE BOEING 737 7373B7 1384580 NM COCKPIT FAILED A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 522AU 23857 BOS - FLT 960 - ON CLIMB-OUT FROM BOS, EN ROUTE TO PHL, CREW REPORTED SMOKE IN THE COCKPIT COMING FROM THE NR 1 HYDRAULI C PUMP SWITCH. CREW TURNED OFF THE ELECTRICAL NR 1 HYDRAULIC SWITCH AND SMOKE STOPPED. QUICK REF HANDBOOK PROCEDURES W ERE ACCOMPLISHED AND THE FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED BUT EMERGENCY EQUIPMENT WAS CALLED OUT. MAINTENANCE FOUND THE P5-8 OVERHEAD HYDRAULIC MODULE HAD FAILED. REMOVED AND REPLACED THE P5-8 OVERHEAD HYDRAULIC MODULE. RAN ENGINES AND SYSTEMS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002030100110 20020301 00110 NM 2002 3 1 USAASB02009 1 20020113 A 2120 ODOR BOEING 737 737401 1384701 NM CABIN DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 406US 23876 PHL - FLT 383 EN ROUTE FROM ROC TO PHL, CREW REPORTED FUMES AND A HOT SMELL IN THE AFT CABIN THAT WERE IRRITATING TO EYE S AND MAKING PEOPLE NAUSEOUS. CREW BEGAN PROCEDURES FOR FUMES IN THE CABIN BUT THE FLIGHT LANDED BEFORE COMPLETION. MA INTENANCE PERFORMED SATISFACTORY BITE CHECK OF TRIM AIR SYSTEM AND BOTH AIR CONDITION TEMPERATURE CONTROLLERS PER MM 21- 61-95. ALL CHECKS NORMAL WITH NO FAULTS NOTED. REMOVED AND REPLACED BOTH RECIRCULATION FAN FILTERS AS PRECAUTIONARY. (M) 2 L 7 2 4F RT A16WE 2002030100111 20020301 00111 NM 2002 3 1 USAASB02010 1 20020114 A 2120 ODOR BOEING 737 737301 1384611 NM CABIN DETECTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 584US 23743 PHL - FLT 735 - EN ROUTE FROM ROC TO PHL, FLIGHT ATTENDANTS REPORTED A STRONG SMELL OF EXHAUST FUMES IN THE REAR OF THE CABIN. FLIGHT LANDED AT PHL WITHOUT FURTHER INCIDENT. MAINTENANCE VISUALLY INSPECTED AIR CONDITIONING PACKS FOR LEAKS AND DEFECTS. NO LEAKS OR DEFECTS NOTED. PERFORMED ENGINE IDLE RUN ON BOTH ENGINES. NO FUMES NOTED. AIRCRAFT OK FOR S ERVICE. (M) 2 L 7 2 4F RT A16WE 2002030100112 20020301 00112 NM 2002 3 1 USAASB02011 1 20020115 A 3350 30043231 LIGHT BOEING 737 7373B7 1384580 NM EXTERIOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 528AU 24410 RDU - MAINTENANCE FOUND THE RIGHT EXTERIOR FUSELAGE EMERGENCY EXIT LIGHT, ADJACENT TO THE RIGHT INBOARD FLAP, INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE RIGHT EXTERIOR FUSELAGE EMERGENCY EXIT LIGHT SOCKET/ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002030100113 20020301 00113 NM 2002 3 1 USAASB02014 1 20020117 A 5610 5893543110 WINDSHIELD BOEING 737 737301 1384611 NM COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 574US 22772 23739 PIT - FLT 1433 - EN ROUTE FROM PIT TO ATL, FLYING OVER CRW, CREW REPORTED THAT THE FIRST OFFICERS WINDSHIELD HAD BROKEN. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002030100114 20020301 00114 NM 2002 3 1 F3LA200200091 1 20020227 A 5330 SKIN PANEL BOEING 737 7372Y5 1384554 NM STA. 326 DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED MISSED DRILLED RIVET HOLE IN FWD LT. CORNER OF AFT E&E DOOR CUTOUT AT STA. 326. F ABRICATED DOUBLER, TRIPLER AND FILLER PER EA 57-737-157. TREATED AND PRIMED REPAIR PARTS PER SOPM 20-41-02. INSTALLED FASTENERS PER 51-30-2. 2 L 7 2 4U RT A16WE 2002030100115 20020301 00115 NM 2002 3 1 F3LA200200092 1 20020227 A 5330 SKIN BOEING 737 7372Y5 1384554 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR CUTOUT CRACKED AT FWD LOWER CORNER OUTER SKIN APPROXIMATELY 1 INCH FROM RI VET TO DOOR CORNER. REPAIRED DAMAGE PER SRM 53-30-3. 2 L 7 2 4U RT A16WE 2002030100116 20020301 00116 SO 2002 3 1 ASOA02022 1 20020113 A 2560 25139915 COVER EMB 120 EMB120ER 3260203 SO CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 285AS 120265 FLT 4010 - DURING GROUND INSPECTION IN ATL, THE WHITE EMERGENCY EXIT SIGN BY SEAT 5C WAS MISSING THE PLASTIC COVER. MAI NTENANCE REPLACED THE EMERGENCY EXIT SIGN COVER. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002030100117 20020301 00117 SO 2002 3 1 ASOA020251 1 20020122 A 5320 12006157007 SILL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SILL WAS FOUND CORRODED FROM FRAMES 44 TO 47. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR SILL IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002030100118 20020301 00118 SO 2002 3 1 ASOA020258 1 20020124 A 5347 12015997003 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE RIGHT WALL SEAT TRACK, FORWARD SECTION, WAS FOUND WITH CORROSION BETWEEN FRAMES 16 AND 31. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK USING SRM 51-40-02, SRM 51-25-00, SRM 51-21-02, ASA E O 120-25-0007, AND THE MM 53-01-05 AS REF. (M) 2 L 7 2 4T RT A31SO 2002030100119 20020301 00119 EA 2002 3 1 ASOA02026 1 20020118 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 844AS 7317 FLT 4787 - DURING SCHEDULED INSPECTION IN XNA, THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE INOPERATIVE LEFT FORWARD EXTERIOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK F OR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002030100120 20020301 00120 EU 2002 3 1 ASOA02027 1 20020117 A 5311 FRAME AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 637AS 383 DURING C-CHECK INSPECTION IN BNA, A CRACK WAS DISCOVERED ON FRAME 26 AT THE BL 0. MAINTENANCE REPAIRED CRACK IN FRAME 2 6 IAW ASA EO 72-53-0125. THE EO REF S/B 72-53-1078 AND SRM CHAPTER 51. (M) 2 H 7 2 4T RT A53EU 2002030100121 20020301 00121 EU 2002 3 1 ASOA02028 1 20020118 A 5320 WEB AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 637AS 383 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE WEB AND UPPER FLANGE, AT FRAMES 36 AND 38, FROM THE RIGHT T O THE LEFT THRESHOLDS. MAINTENANCE REPAIRED THE CORROSION IAW ASA EO 72-53-0126. (M) 2 H 7 2 4T RT A53EU 2002030100122 20020301 00122 EU 2002 3 1 ASOA02029 1 20020118 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 637AS 383 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE UPPER FLANGE OF THE FLOORBEAM AT FRAMES 39 AND 40, LEFT TO RIGHT. MAINTENANCE REPAIRED THE CORROSION IAW ASA EO 72-53-0126. (M) 2 H 7 2 4T RT A53EU 2002030100123 20020301 00123 EU 2002 3 1 ASOA02030 1 20020118 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 637AS 383 DURING C-CHECK INSPECTION IN BNA, THE LOWER FLOOR SUPPORT FLANGE WAS FOUND TO BE CORRODED AROUND THE FASTENER HOLES, FRO M LEFT TO RIGHT, ON THE FLOORBEAM AT FRAME 41. MAINTENANCE REPAIRED THE CORROSION IAW ASA EO 72-53-0126. (M) 2 H 7 2 4T RT A53EU 2002030100124 20020301 00124 EU 2002 3 1 ASOA02031 1 20020118 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 637AS 383 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT INBOARD SEAT TRACK FRAME 23 TO 29. CORROSION WAS ALS O FOUND ON THE LEFT INBOARD SEAT TRACK FROM FRAME 13 TO 23. MAINTENANCE REPAIRED THE CORROSION IAW ASA EO 72-53-0126. (M) 2 H 7 2 4T RT A53EU 2002030100125 20020301 00125 SO 2002 3 1 ASOA02032 1 20020118 A 5320 12046158001 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 25 AND 30. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002030100126 20020301 00126 SO 2002 3 1 ASOA02033 1 20020118 A 5313 12005744013 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, STRINGER 19 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 13A AND 15A. MAINTENANCE REM OVED AND REPLACED THE CORRODED STRINGER IAW SRM 53-00-03 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002030100127 20020301 00127 SO 2002 3 1 ASOA02034 1 20020118 A 5320 12004149001 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD CROSS FRAME WAS FOUND TO BE CORRODED AT FRAME 26. MAINTENANCE REMO VED AND REPLACED THE CORRODED CROSS FRAME IAW SRM 51-30-01 AND 51-30-02. (M) 2 L 7 2 4T RT A31SO 2002030100128 20020301 00128 EA 2002 3 1 ASOA02035 1 20020119 A 2910 601R7528661 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS LEAKING A ASOA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 11 882AS 7503 FLT 4484 - WHILE DESCENDING THROUGH FL310, FROM DAL TO ATL, A 'HYD 1 LOW PRESS' MESSAGE WAS RECEIVED BY THE PILOT. THE HYDRAULIC QUANTITY SHOWED ZERO. THE PILOT SLOWED DOWN TO 250 KNOTS PER QRH PROCEDURES AND DECLARED AN EMERGENCY. AIRCR AFT LANDED SAFELY IN ATL. MAINTENANCE NOTED A TOTAL LOSS OF HYDRAULIC QUANTITY. MAINTENANCE REMOVED AND REPLACED THE N R 1 ENGINE DRIVEN HYDRAULIC PUMP DUE TO IT BEING RUN DRY FOR APPROX 37 MINUTES. MAINTENANCE ALSO REPLACED THE NR 1 HYDR AULIC PRESSURE TUBE WHICH WAS DETERMINED TO BE THE SITE OF THE LEAK. LEAK AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002030100129 20020301 00129 SO 2002 3 1 ASOA02036 1 20020120 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 282AS 120226 FLT 4159 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS AT ROW 5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE EMERGENCY LIGHTING POWER SUPPLY AT THE NR 2 POSITION, ROW 5. OPERATIONAL CHECKS GOOD. AIRCRAFT O K FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002030100130 20020301 00130 SO 2002 3 1 ASOA02037 1 20020118 A 5320 12004449001 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, A CROSS FRAME WAS FOUND CORRODED AT FRAME 23 BETWEEN THE RIGHT AND CENTER BUTT STRAPS. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS FRAME IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002030100131 20020301 00131 SO 2002 3 1 ASOA02038 1 20020118 A 5347 12015994003 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE FORWARD SECTION OF THE LEFT WALL SEAT TRACK WAS FOUND CORRODED BETWEEN FRAMES 17 A ND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002030100132 20020301 00132 SO 2002 3 1 ASOA02039 1 20020118 A 5347 12016000003 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 NM 01 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SEAT TRACK, FORWARD SECTION, WAS FOUND TO BE CORRODED BETWEEN FRAMES 1 6 AND 31. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002030100133 20020301 00133 SO 2002 3 1 ASOA02040 1 20020118 A 5347 12026863005 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 NM 01 638AS 120282 DURING C-CHECK INSPECTION IN BNA, FOUND CORROSION ON THE AFT SECTION OF THE LEFT WALL SEAT TRACK BETWEEN FRAMES 32 AND 3 9. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002030100134 20020301 00134 SO 2002 3 1 ASOA02041 1 20020118 A 5347 12015996005 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE RIGHT AFT SECTION OF WALL SEAT TRACK WAS FOUND CORRODED BETWEEN FRAMES 34 AND 38. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002030100135 20020301 00135 SO 2002 3 1 ASOA02042 1 20020118 A 5320 12006159001 SILL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT SILL PLATE BETWEEN FRAMES 38 AND 44. MAINTENANCE REM OVED AND REPLACED THE CORRODED SILL PLATE IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002030100136 20020301 00136 EA 2002 3 1 ASOA02043 1 20020122 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 861AS 7445 DURING A SCHEDULED INSPECTION IN XNA, THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE BURNED OUT LEFT FORWARD EXTERIOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE . (M) 2 L 7 2 4F RT A21EA 2002030100137 20020301 00137 EA 2002 3 1 ASOA02044 1 20020122 A 3260 864202 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A ASOA L ABORTED APPROACH J E WARNING INDICATION VIBRATION/BUFFET AP APPROACH 1 SO 11 846AS 7328 DURING APPROACH INTO ABY, THE NOSE GEAR FAILED TO EXTEND. THE CAPTAIN ABORTED THE INITIAL APPROACH. WHILE IN A HOLDING PATTERN, APPROXIMATELY 5 MINUTES AFTER BEING SELECTED DOWN, THE GEAR EXTENDED ON ITS OWN. EVEN WITH THE GEAR SAFE INDI CATIONS, A VIBRATIONS WAS STILL FELT COMING FROM THE NOSE AREA. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS MADE IN ABY. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR NR 2 DOWNLOCK PROXIMITY SENSOR. THE AIRCRAFT WAS JACKED, AND THE GEAR WAS SWUNG SEVERAL TIMES. SYSTEM OPERATIONAL CHECKS GOOD. NO DEFECTS WERE NOTED. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002030100138 20020301 00138 SO 2002 3 1 ASOA02046 1 20020122 A 5315 12005807007 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, FOUND CORROSION ON THE CENTER OMEGA BEAM BETWEEN FRAME STATION 5518-5533. MX REPAIRED THE CORRODED OMEGA BEAM IAW ASA EO120-53-0173. (M) 2 L 7 2 4T RT A31SO 2002030100139 20020301 00139 SO 2002 3 1 ASOA02047 1 20020122 A 5320 12004149002 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, ALL CROSSBEAMS AT FRAME 16 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACE D THE CORRODED CROSSBEAMS IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002030100140 20020301 00140 SO 2002 3 1 ASOA02048 1 20020122 A 5320 12004149001 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE LEFT CROSSBEAM AT FRAME 20 WAS FOUND CORRODED BETWEEN THE FLOOR SILL AND THE LEFT BUTT STRAP. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRM 51-40-02. M) 2 L 7 2 4T RT A31SO 2002030100141 20020301 00141 SO 2002 3 1 ASOA02049 1 20020122 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE CENTER BUTT STRAP AT FRAMES 13 TO 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED CENTER BUTT STRAP IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002030100142 20020301 00142 SO 2002 3 1 ASOA02050 1 20020122 A 5320 SILL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE SILL PLATE AT FRAME 13, RUNNING LEFT TO RIGHT, WAS CORRODED FROM THE CENTER TO THE RIGHT SIDE. MAINTENANCE CUT AWAY THE DAMAGED PORTION OF THE SILL PLATE. A NEW REPLACEMENT PART AND SPLICE PLATE WERE FABRICATED IAW SRM 51-10-02, SRM 51-21-05, AND SRM 51-21-06. MAINTENANCE INSTALLED THE SILL REPAIR IAW SRM 51-40-02. ( M) 2 L 7 2 4T RT A31SO 2002030100143 20020301 00143 SO 2002 3 1 ASOA02052 1 20020122 A 5347 12026864005 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE AFT, LEFT INBOARD SEAT TRACK, BETWEEN FRAMES 34 AND 40 WAS FOUND TO HAVE CORROSION . MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. A NEW SEAT TRACK WAS FABRICATED IAW SRM 5 1-25-00, 51-21-02, AND 51-20-05. (M) 2 L 7 2 4T RT A31SO 2002030100144 20020301 00144 SO 2002 3 1 ASOA02053 1 20020122 A 5313 12006173009 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON STRINGER 18 LEFT BETWEEN FRAME STATION 4214 AND 4992. MAINTENA NCE REMOVED AND REPLACED THE DAMAGED PART OF THE STRINGER IAW SRM 53-00-03, 51-25-00, AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002030400001 20020304 00001 NM 2002 3 4 EVA200201 1 20020301 A 7100 CF680C2B6 ENGINE BOEING 767 7673T7 1385201 NM GE CF6 CF680C2B6 30025 NE L ENGINE DAMAGED W QOCF A E UNSCHED LANDING ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 03 601EV 37926 25076 702536 1. During initial climb, Captain notice the L Engine N1 vibration indicationin on the EICAS is up to 3.3 and N2 up to 5. 0. All the rest parameters are normal.2. After 2 hours in cruise, "L ENG OIL FILTER" message appeared in the EICAS. Pilt o followed the QRH performed all the necessary action with no help. In-flight shut down the enine and aircraft diverted to BNE.3. On ground,maintenace check the Fan inlet area normal but found large oil in the tail pipe area and metal chips in the MCD. Removed all the oil filters and found B sump filter had many metal chips. Oil quantity drop to 12 QTS.4. Pe r MM replaced the L Engine and ground test normal. Aircraft return to service.5. Preliminary inspection report h 2 L 7 2 4F 4 F RT A1NM E13NE 2002030400002 20020304 00002 SW 2002 3 4 HEEA077743 1 20020128 A 6510 406040315111 BALANCE WEIGHT BELL 407 407 1182206 SW T/R SHAFT DEBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 2279 53400 TAIL ROTOR SHAFT WEIGHT UNBONDED. 1 G 7 1 3U O H2SW 2002030400003 20020304 00003 SW 2002 3 4 HEEA077744 1 20020128 A 6520 406040400119 GEARBOX BELL 407 407 1182206 SW TAIL ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 2281 53400 TAIL ROTOR GEARBOX SHAFT SPLINES PITTED. 1 G 7 1 3U O H2SW 2002030400004 20020304 00004 2002 3 4 HEEA077745 4 20020128 A 3120 M803B205VBATT CLOCK BELL 407 407 1182206 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 491PH 53386 CLOCK SELECT FUNCTION INOPERATIVE. 1 G 7 1 3U O H2SW 2002030400005 20020304 00005 SW 2002 3 4 HEEA077746 1 20020128 A 6730 BEARING BELL 407 407 1182206 SW CYCLIC SERVO WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 4948 HR425 53159 CYCLIC SERVO HAS A WORN BEARING. 1 G 7 1 3U O H2SW 2002030400006 20020304 00006 SW 2002 3 4 HEEA077748 1 20020128 A 6220 HUB BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 491PH 53386 SENDING IN FOR EVALUATION DUE TO CORROSION FOUND ON MAIN ROTOR HUB. 1 G 7 1 3U O H2SW 2002030400007 20020304 00007 2002 3 4 HEEA077749 4 20020128 A 3120 M803B205VBATT CLOCK BELL 407 407 1182206 SW COCKPIT MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 493PH 53393 CLOCK LIGHT SEGMENTS INTERMITTENT. 1 G 7 1 3U O H2SW 2002030400009 20020304 00009 SW 2002 3 4 HEEA077755 1 20020128 A 6730 206076062107 BEARING BELL 407 407 1182206 SW CYCLIC SERVO WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 493PH 2708 HR1175 53393 CYCLIC SERVO BEARING WEAR. 1 G 7 1 3U O H2SW 2002030400010 20020304 00010 SW 2002 3 4 HEEA077756 1 20020128 A 6320 407040006107 GEARBOX BELL 407 407 1182206 SW MAIN ROTOR MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 495PH 2568 53397 MAIN ROTOR GEARBOX MAKING METAL. 1 G 7 1 3U O H2SW 2002030400011 20020304 00011 SW 2002 3 4 HEEA077758 1 20020128 A 6520 406040400119 GEARBOX BELL 407 407 1182206 SW TAIL ROTOR VIBRATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 496PH 2154 53398 TAIL ROTOR GEARBOX PRODUCING HIGH FREQUENCY VIBRATION. 1 G 7 1 3U O H2SW 2002030400012 20020304 00012 SW 2002 3 4 HEEA077759 1 20020128 A 6510 407040302101 DRIVE SHAFT BELL 407 407 1182206 SW TAIL ROTOR PEELING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 7054 53003 TAIL ROTOR DRIVESHAFT PAINT PEELING. 1 G 7 1 3U O H2SW 2002030400014 20020304 00014 SW 2002 3 4 HEEA077761 1 20020128 A 6720 406012129101 PITCH LINK BELL 407 407 1182206 SW TAIL ROTOR WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 457PH 53147 TAIL ROTOR PITCH LINK HAS WORN BEARINGS. 1 G 7 1 3U O H2SW 2002030400015 20020304 00015 SW 2002 3 4 HEEA077762 1 20020128 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW MAIN ROTOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 494PH 53396 MAIN ROTOR MOUNT HAS CRACKED RUBBER. 1 G 7 1 3U O H2SW 2002030400017 20020304 00017 SW 2002 3 4 HEEA077764 1 20020128 A 6230 BUSHING BELL 407 407 1182206 SW LEVER WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 498PH 2031 A2608 53399 LEVER HAS WORN BUSHINGS. 1 G 7 1 3U O H2SW 2002030400018 20020304 00018 SW 2002 3 4 HEEA077765 1 20020128 A 2840 407362005103 SWITCH BELL 407 407 1182206 SW FUEL SYSTEM MALFUNCTIONED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 406PH 53198 LOW LEVEL LIGHT COMES ON WHEN WIRES TO SWITCH ARE MOVED. 1 G 7 1 3U O H2SW 2002030400019 20020304 00019 SW 2002 3 4 HEEA077766 1 20020128 A 3212 206050247138 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 722PH 53288 EMERGENCY FLOAT COVER WORN AND TORN. 1 G 7 1 3U O H2SW 2002030400020 20020304 00020 SW 2002 3 4 HEEA077767 1 20020128 A 3212 206050247132 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 722PH 53288 EMERGENCY FLOAT COVER WORN AND TORN. 1 G 7 1 3U O H2SW 2002030400021 20020304 00021 SW 2002 3 4 HEEA077768 1 20020128 A 3212 206050247131 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 722PH 53288 EMERGENCY FLOAT COVER WORN AND TORN. 1 G 7 1 3U O H2SW 2002030400022 20020304 00022 SW 2002 3 4 HEEA077769 1 20020128 A 2840 407362005103 SWITCH BELL 407 407 1182206 SW FUEL SYSTEM MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 741PH 53457 LOW LEVEL LIGHT STAYS ON ALL THE TIME. 1 G 7 1 3U O H2SW 2002030400023 20020304 00023 SW 2002 3 4 HEEA077770 1 20020128 A 6310 214040814105 SLEEVE BELL 407 407 1182206 SW FREEWHEEL UNIT LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 490PH 53378 FREEWHEEL UNIT SLEEVE SEAL LEAKING. 1 G 7 1 3U O H2SW 2002030400024 20020304 00024 SW 2002 3 4 HEEA077771 1 20020128 A 6300 407340339101 BEARING BELL 407 407 1182206 SW COOLER BLOWER ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 493PH 53393 COOLER BLOWER BEARING SOUNDS ROUGH AND GREASE TURNING BLACK. 1 G 7 1 3U O H2SW 2002030400025 20020304 00025 SW 2002 3 4 HEEA077772 1 20020128 A 6510 206061432118 INLET BELL 407 407 1182206 SW T/R OIL COOLER WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 53400 WORN. 1 G 7 1 3U O H2SW 2002030400026 20020304 00026 SW 2002 3 4 HEEA077776 1 20020128 A 3340 10648BH151 SWITCH BELL 407 407 1182206 SW MANUAL LIGHT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 407PH 53003 MANUAL LIGHT FLICKERS WHILE IN AUTO. 1 G 7 1 3U O H2SW 2002030400027 20020304 00027 2002 3 4 HEEA077777 4 20020128 A 2300 M880511104 SWITCH BELL 407 407 1182206 SW MICROPHONE STUCK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4999 53323 MICROPHONE SWITCH STUCK IN OPEN POSITION. 1 G 7 1 3U O H2SW 2002030400028 20020304 00028 SW 2002 3 4 HEEA077778 1 20020128 A 6300 20088P6D349 BOLT BELL 407 407 1182206 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 494PH 53396 MAIN ROTOR BOLT WORN AND RIDGED. 1 G 7 1 3U O H2SW 2002030400031 20020304 00031 2002 3 4 HEEA077783 4 20020130 A 3160 412074101101 TRANSDUCER BELL 407 407 1182206 SW FADEC FAULTY E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 495PH 53397 FAULTY TRANSDUCER PRODUCING A FADEC DEGRADE LIGHT. 1 G 7 1 3U O H2SW 2002030400032 20020304 00032 SW 2002 3 4 HEEA077784 1 20020130 A 2840 407362005103 SWITCH BELL 407 407 1182206 SW FUEL SYSTEM STUCK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 496PH 53398 SWITCH STICKS AT APPROXIMATELY 360 LBS. 1 G 7 1 3U O H2SW 2002030400034 20020304 00034 SW 2002 3 4 HEEA077789 1 20020130 A 2840 407362005103 SWITCH BELL 407 407 1182206 SW FUEL SYSTEM FAULTY E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 495PH 53397 FAULTY SWITCH CAUSING LOW LEVEL LIGHT. 1 G 7 1 3U O H2SW 2002030400036 20020304 00036 SW 2002 3 4 HEEA077791 1 20020130 A 6230 406310411101 BOOT BELL 407 407 1182206 SW MAIN ROTOR TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 53159 MAIN ROTOR BOOT IS TORN. 1 G 7 1 3U O H2SW 2002030400037 20020304 00037 2002 3 4 HEEA077793 4 20020130 A 2300 PM212302 SWITCH BELL 407 407 1182206 SW RADIO / ICS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 407PH 53003 RADIO / ICS WON'T KEY UP. FAULTY SWITCH. 1 G 7 1 3U O H2SW 2002030400038 20020304 00038 SW 2002 3 4 HEEA077794 1 20020130 A 6300 407310203101 MOUNT BELL 407 407 1182206 SW MAIN ROTOR DELAMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 MAIN ROTOR MOUNT DELAMINATED. 1 G 7 1 3U O H2SW 2002030400039 20020304 00039 SW 2002 3 4 HEEA077795 1 20020130 A 6710 406310405101 UNIVERSAL BELL 407 407 1182206 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 510PH 1632 53209 MAIN ROTOR UNIVERSAL WORN. 1 G 7 1 3U O H2SW 2002030400040 20020304 00040 SW 2002 3 4 HEEA077796 1 20020130 A 3340 01077006203 POWER SUPPLY BELL 407 407 1182206 SW STROBE LIGHT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 407PH 53003 STROBE LIGHT INOPERATIVE. FAULTY POWER SUPPLY. 1 G 7 1 3U O H2SW 2002030400041 20020304 00041 SW 2002 3 4 HEEA077797 1 20020130 A 7921 407062021101 DUCT BELL 407 407 1182206 SW COOLER BLOWER OUT OF ADJUST E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 53400 CAUSING OIL COOLER BLOWER HOUSING TO CRACK AT BEING OUT OF ALIGNMENT. 1 G 7 1 3U O H2SW 2002030400042 20020304 00042 SW 2002 3 4 HEEA077798 1 20020130 A 6510 206061432121 HOUSING BELL 407 407 1182206 SW COOLER BLOWER CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 53400 COOLER BLOWER HOUSING CRACKED AT NORMAL POSITION. 1 G 7 1 3U O H2SW 2002030400043 20020304 00043 SW 2002 3 4 HEEA077801 1 20020130 A 2800 206064263101 LINE BELL 407 407 1182206 SW FUEL SYSTEM BROKEN E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 407PH 53003 FUEL LINE BROKEN. 1 G 7 1 3U O H2SW 2002030400044 20020304 00044 SW 2002 3 4 HEEA077802 1 20020130 A 3212 206050247132 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406PH 53198 END COVER VELCRO WILL NOT HOLD. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFEREN CE: DMR#744642. 1 G 7 1 3U O H2SW 2002030400045 20020304 00045 SW 2002 3 4 HEEA077803 1 20020130 A 6300 206362002103 CAP BELL 407 407 1182206 SW M/R DRIVE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 406PH 53198 MAIN ROTOR DRIVE CAP LEAKS. 1 G 7 1 3U O H2SW 2002030400046 20020304 00046 SW 2002 3 4 HEEA077804 1 20020130 A 6420 406312100101 BEARING 407012101111 BELL 407 407 1182206 SW T/R HUB WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 53398 53400 TAIL ROTOR HUB BEARING IS WORN. 1 G 7 1 3U O H2SW 2002030400047 20020304 00047 WP 2002 3 4 0200569996 1 20020221 A 3040 TERMINAL DOUG DC9 DC931 3022065 WP COCKPIT DAMAGED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 8932E 47141 CREW REPORTED SMOKE IN COCKPIT. COMPLIED WITH COM PROCEDURES AND DONNED OXYGEN MASK. SMOKE ORIGINATED BEHIND OVERHEAD PANEL AND DISSIPATED SHORTLY AFTER THE WINDSHIELD HEAT WAS TURNED OFF SO IT LASTED ONLY 15 SECONDS. LANDING WAS UNEVENT FUL AND THE EMERGENCY WAS CANCELED AFTER TOUCHDOWN. MAINTENANCE FOUND THE LUGS AT TERMINAL STRIP S3-57 CHARRED WITH HEA T DAMAGE. REPLACED THE TERMINAL STRIP AND THE WINDSHIELD HEAT CONTROLLER. ALSO CHECKED THE WIRING RELATED TO THE SYSTE M. THE BATTERY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002030400048 20020304 00048 SW 2002 3 4 HEEA077806 1 20020130 A 7120 BEARING BELL 407 407 1182206 SW BIPOD MOUNT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 53159 ENGINE BIPOD MOUNT HAS BOTTOM BEARINGS WORN. 1 G 7 1 3U O H2SW 2002030400049 20020304 00049 SW 2002 3 4 HEEA077807 1 20020130 A 6510 206061432121 HOUSING BELL 407 407 1182206 SW COOLER BLOWER CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 53159 TAIL ROTOR COOLER BLOWER HOUSING CRACKED. 1 G 7 1 3U O H2SW 2002030700044 20020307 00044 NM 2002 3 7 02FDEA00156 1 20020228 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION C53-111-01(3) LWR SURFACE OF UPPER CHORD OF FLOORBEAM BS 1166, RBL 3, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 8. 2 L 7 3 4F RT A3WE 2002030400051 20020304 00051 NE 2002 3 4 02FDEA00158 2 20020227 A 7314 384300 PUMP BOEING 727 727200 138407E NM PWA JT8 JT8D17A 52049 NE NR 3 ENGINE FAILED A FDEA A UNSCHED LANDING X ENGINE FLAMEOUT TO TAKEOFF 1 SO 25 203FE 22925 NR 3 ENGINE QUIT ON TAKEOFF. REMOVED AND REPLACED ENGINE FUEL PUMP AND CONTROL UNIT PER 73-12-001-2, 73-21-000-4. CHEC K OK. 2 L 7 3 4F 4 F RT A3WE E2EA 2002030400052 20020304 00052 SW 2002 3 4 HEEA077805 1 20020130 A 6710 BEARING BELL 407 407 1182206 SW UNIVERSAL UNSTAKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 1018 RXFS5813 53400 MAIN ROTOR UNIVERSAL UNSTAKED BEARING. 1 G 7 1 3U O H2SW 2002030400054 20020304 00054 SW 2002 3 4 HEEA077809 1 20020130 A 6710 BEARING BELL 407 407 1182206 SW UNIVERSAL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 741PH 1309 RXFS5712 53457 MAIN ROTOR UNIVERSAL BEARING WORN. 1 G 7 1 3U O H2SW 2002030400055 20020304 00055 SW 2002 3 4 HEEA077810 1 20020130 A 6710 406310411101 BOOT BELL 407 407 1182206 SW MAIN ROTOR TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 496PH 53398 MAIN ROTOR BOOT TORN. 1 G 7 1 3U O H2SW 2002030700045 20020307 00045 NM 2002 3 7 02FDEA00159 1 20020220 A 5315 65317731 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION C53-224-08 ON BS 1176 CHORD LBL 36 TO LBL 65, WL 208. REMOVED AND REPLACED CHORD PER SRM 53-10-1, 51-30-2. 2 L 7 3 4F RT A3WE 2002030400056 20020304 00056 SW 2002 3 4 HEEA077811 1 20020130 A 6420 BEARING 407012101111 BELL 407 407 1182206 SW TAIL ROTOR HUB WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4999 53146 53323 TAIL ROTOR HUB HAS WORN BEARINGS. 1 G 7 1 3U O H2SW 2002030700047 20020307 00047 NM 2002 3 7 02FDEA00162 1 20020219 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION OF BELLY SKIN BS 965, LBL 8, WL 137. REMOVED AND REPLACED CORRODED SKIN PER SRM 53-30-3, 53-30-1. 2 L 7 3 4F RT A3WE 2002030400057 20020304 00057 SW 2002 3 4 HEEA077813 1 20020130 A 7921 406360500101 OIL COOLER BELL 407 407 1182206 SW ENGINE CONTAMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 495PH 53397 ENGINE OIL COOLER HAS METAL CONTAMINATION. 1 G 7 1 3U O H2SW 2002030400058 20020304 00058 NM 2002 3 4 02FDEA00169 1 20020216 A 2782 BEARING DOUG MD11 MD11F 3023600 NM L/E SLAT OUT OF POSITION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 RT WING O/B SLAT DRIVE MECHANISM FWD BEARING MIGRATED. 2 L 7 3 4F RT A22WE 2002030400059 20020304 00059 SW 2002 3 4 HEEA077815 1 20020130 A 2820 206064263101 TUBE BELL 407 407 1182206 SW FUEL SYSTEM BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 501PH 53401 FUEL TUBE IS BROKEN. 1 G 7 1 3U O H2SW 2002030400060 20020304 00060 SW 2002 3 4 HEEA077816 1 20020130 A 6300 407310203101 MOUNT BELL 407 407 1182206 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 492PH 53390 MAIN ROTOR MOUNT HAS WORN RUBBER. 1 G 7 1 3U O H2SW 2002030400061 20020304 00061 WP 2002 3 4 ABXA010746 1 20020213 A 5310 59144191 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 CRACK IN FORWARD ACCESSORY COMPARTMENT DOOR JAMB, APPROXIMATELY 1.5 INCH LONG, LOCATED ALONG THE UPPER AFT SIDE OF JAMB. REPAIRED DOOR JAMB IAW DC-9 SRM 51-10-3 AND 51-20. 2 L 7 2 4F A6WE 2002030400062 20020304 00062 SW 2002 3 4 HEEA077817 1 20020130 A 3212 206050247138 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 493PH 53393 VELCRO UNSEWN FROM EMERGENCY FLOAT COVER. 1 G 7 1 3U O H2SW 2002030400063 20020304 00063 WP 2002 3 4 ABXA010748 1 20020213 A 5320 991050129 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 CUSP WEB CRACKED (AFT WEB) AT FS 236, LONGERON 18 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002030400064 20020304 00064 SW 2002 3 4 HEEA077818 1 20020130 A 6420 406312100101 BEARING 407012101111 BELL 407 407 1182206 SW T/R HUB WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 496PH 1793 53396 53398 TAIL ROTOR HUB HAS WORN BEARINGS. 1 G 7 1 3U O H2SW 2002030400065 20020304 00065 WP 2002 3 4 ABXA010754 1 20020228 A 3260 WARNING SYSTEM DOUG DC9 DC932 3022066 WP COCKPIT MALFUNCTIONED A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 982AX 47317 ON INITIAL GEAR EXTENSION AT ILN, NOSE LANDING GEAR DID NOT INDICATE DOWN/LOCKED. SUBSEQUENTIAL RETRACT/EXTENSION CYCLE YIELDED NORMAL INDICATION. PERFORMED FUNCTIONAL CHECK IAW DC-9 MM 32-60-00-2-0101, NORMAL INDICATION AT THIS TIME. 2 L 7 2 4F A6WE 2002030400066 20020304 00066 SW 2002 3 4 HEEA077820 1 20020130 A 6320 204040760109 FILTER ELEMENT BELL 407 407 1182206 SW MAIN ROTOR OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 53159 FILTER ELEMENT FAILED, METAL IN OIL - SCRAPPED. 1 G 7 1 3U O H2SW 2002031100050 20020311 00050 NE 2002 3 11 ARWA20020207 2 20020226 A 7230 COMPRESSOR DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE STALLED A ARWA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 19 1808E 46105 671351 UPON COMMENCING T/O ROLL NR 2 ENGINE COMPRESSOR STALLED SPEED NIL WIND CALM. AIRCRAFT RETURNED TO THE RAMP. PERFORMED VISUAL INSPECTION OF NR 2 ENGINE IN ACCORDANCE WITH 71-00, OPS CHECKED FOUND NORMAL ON GROUND RUN UP. 2 L 7 4 4F 4 F 4A25 1E8 2002030400067 20020304 00067 SW 2002 3 4 HEEA077822 1 20020130 A 6320 204040760109 FILTER ELEMENT BELL 407 407 1182206 SW MAIN ROTOR OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 493PH 53393 FILTER ELEMENT FAILED, TRANSMISSION CHIP LIGHT ILLUMINATED. 1 G 7 1 3U O H2SW 2002031900078 20020319 00078 WP 2002 3 19 ARWA20020208 1 20020227 A 3310 TRANSFORMER DOUG DC8 DC862 3021970 WP COCKPIT FAULTY A ARWA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 19 810BN 45905 AFTER LANDING ROLL IN MGGT, HEAVY SMOKE WAS SEEN COMING OUT FROM BEHIND F/O'S INSTRUMENT PANEL. AREA WAS INSPECTED, FOU ND THE GLARESHIELD LIGHT BALLAST (B6) AT FAULT. REMOVED AND REPLACED BALLAST TRANSFORMER IAW MM 33-12-0, PERFORMED OPER ATIONAL CHECK IAW MM 33-12-0 FOUND NORMAL. 2 L 7 4 4F 4A25 2002030400068 20020304 00068 SW 2002 3 4 HEEA077824 1 20020130 A 8011 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE MALFUNCTIONED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 STARTER WILL NOT AUTOMATICALLY DISENGAGE AFTER ENGINE IS STARTED. 2 G 7 2 4U H10SW 2002030400069 20020304 00069 SW 2002 3 4 HEEA077825 1 20020207 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 STEP ACTUATOR HAS NO MOVEMENT WITH 24 V. GOING IN AND GOOD GROUND. 1 G 7 2 4U H4SW 2002030400070 20020304 00070 SW 2002 3 4 HEEA077826 1 20020207 A 2424 214175153105 VOLT REGULATOR BELL 214 214ST 1182106 SW ELECTRICAL SYS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 VOLTAGE DROPPING TO 20 VOLTS ON CROSS START, DUE TO MALFUNCTIONING VOLTAGE REGULATOR. 2 G 7 2 4U H10SW 2002030400071 20020304 00071 SW 2002 3 4 HEEA077827 1 20020208 A 6321 206340301103 BRAKE BELL 407 407 1182206 SW MAIN ROTOR LEAKING E HEEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 467PH 3152 53142 ROTOR BRAKE IS DAMAGED AND LEAKS. 1 G 7 1 3U O H2SW 2002030400072 20020304 00072 SW 2002 3 4 HEEA077828 1 20020208 A 6321 206340301103 BRAKE BELL 407 407 1182206 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 2074 53159 ROTOR BRAKE HAS EXCESSIVE HOUSING AND PISTON WEAR. 1 G 7 1 3U O H2SW 2002030400073 20020304 00073 EU 2002 3 4 AWXA200200182 1 20020301 A 2910 AE2463921G0181 HYDRAULIC LINE AIRBUS 320 A320231 3930325 EU NLG BURST A AWXA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 28 628AW 5306 67 ON FINAL TURN INTO PHX WHEN LANDING GEAR WAS EXTENDED ECAM INDICATED A LOSS OF GREEN SYSTEM HYDRAULIC PRESSURE. EMERGEN CY WAS DECLARED AND AIRCRAFT LANDED UNEVENTFULLY WITH ALTERNATE HYDRAULIC SYSTEM OPERATING NORMALLY. NOSE WHEEL STEERIN G INOPERATIVE AFTER LANDING AND AIRCRAFT REQUIRED TOW TO GATE. MAINTENANCE FOUND THE LT MAIN LANDING GEAR DOOR RETRACT ACTUATOR FLEX LINE HAD BURST. REMOVED AND REPLACED THE LT MAIN LANDING GEAR DOOR RETRACT FLEX LINE. MAINTENANCE ALSO F OLLOWED PROCEDURES FOR POSSIBLE PUMP CAVITATION AMM 29-00-00-280-006 AND REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYD RAULIC PUMP IAW AMM 29-13-51-401. 2 L 7 2 4F RT A28NM 2002030400074 20020304 00074 SW 2002 3 4 HEEA077829 1 20020208 A 6321 206340301103 BRAKE BELL 407 407 1182206 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 724PH 3200 53327 ROTOR BRAKE HAS EXCESSIVE HOUSING AND PISTON WEAR. 1 G 7 1 3U O H2SW 2002030400075 20020304 00075 SW 2002 3 4 HEEA077830 1 20020208 A 6321 206340301103 BRAKE BELL 407 407 1182206 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 457PH 2751 53147 ROTOR BRAKE EXCESSIVE HOUSING AND PISTON WEAR. 1 G 7 1 3U O H2SW 2002030400076 20020304 00076 SW 2002 3 4 HEEA077831 1 20020208 A 6310 406040500131 FREEWHEEL UNIT BELL 407 407 1182206 SW MAIN ROTOR MAKING METAL E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 495PH 256 53397 FREEWHEEL UNIT MAKING METAL CAUSING CHIP LIGHT TO ILLUMINATE. 1 G 7 1 3U O H2SW 2002030400077 20020304 00077 SW 2002 3 4 HEEA077836 1 20020208 A 6230 406010401117 SWASHPLATE BELL 407 407 1182206 SW MAIN ROTOR LEAKING E HEEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 740PH 960 53435 SWASHPLATE GREASE LEAKING FROM UPPER SEAL ON UNIBALL. 1 G 7 1 3U O H2SW 2002030400078 20020304 00078 SW 2002 3 4 HEEA077837 1 20020208 A 6220 BEARING BELL 407 407 1182206 SW M/R HUB ASSY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 490PH 2010 A416 53378 MAIN ROTOR HUB SHEAR BEARING FAILURE. 1 G 7 1 3U O H2SW 2002030400079 20020304 00079 NM 2002 3 4 AWXA200200183 1 20020228 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 189AW 22656 PHX - EEL - C - EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY E SCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD IAW T/C 18MO5002. 2 L 7 2 4F RT A16WE 2002030400080 20020304 00080 SW 2002 3 4 HEEA077838 1 20020208 A 2840 407375016103 SIGNAL COND UNIT BELL 407 407 1182206 SW FUEL QTY IND FAILED E HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 720PH 53277 SIGNAL CONDITION UNIT CAUSED FUEL QUANTITY INDICATOR TO BLANK OUT. 1 G 7 1 3U O H2SW 2002030400081 20020304 00081 NM 2002 3 4 AWXA200200184 1 20020227 A 3350 321430 BATTERY PACK AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 812AW 1178 SAN - EEL - C - DURING INSPECTION RT OVERWING EMERGENCY EXIT LIGHT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE BATTERY PACK AT RT OVERWING EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002030400082 20020304 00082 SW 2002 3 4 HEEA077840 1 20020208 A 6210 DOUBLER BELL 206 206L3 1182108 SW M/R BLADE SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 A4352 NR 2 LOWER DOUBLER SEPARATED APPROXIMATELY 4 1/2 INCHES LONG WHICH EXTENDS UNDERNEATH THE NR 3 FINGER. 1 G 7 1 3U H2SW 2002030400083 20020304 00083 NM 2002 3 4 CALA0200112 1 20020228 A 2530 8103060000 OVEN BOEING 737 7373T0 1384582 NM GALLEY MALFUNCTIONED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 59302 23353 A STRONG TOXIC ODOR WAS OBSERVED IN THE CABIN WHILE EN ROUTE FROM MSY TO EWR. THE CABIN CREW AND PASSENGERS COMPLAINED OF THE ODOR. THE FLIGHT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THAT A RELAY WIT HIN THE AFT GALLEY NR 1 OVEN HAD MELTED WHICH RESULTED IN THE TOXIC ODOR. THE OVEN WAS REMOVED AND REPLACED. THE OVEN AND CONTROLLER WILL BE SHIPPED TO ENGINEERING FOR ANALYSIS. 2 L 7 2 4F RT A16WE 2002030400084 20020304 00084 NM 2002 3 4 CALA0200113 1 20020228 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND LT WHEEL WELL WASHERS FRETTING INTO KEEL BEAM FROM STA 700-727. A REPAIR WAS INSTALLED IAW ECRA 5310-0 3740. 2 L 7 2 4F RT A16WE 2002030400085 20020304 00085 2002 3 4 HEEA077842 4 20020214 A 2200 214074303115 AMPLIFIER BELL 214 214ST 1182106 SW AUTOFLIGHT SYS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 PITCH LIGHT INOP. WON'T MONITOR TEST. AUTOFLIGHT AMPLIFIER FAILED. 2 G 7 2 4U H10SW 2002030400086 20020304 00086 SW 2002 3 4 HEEA077843 1 20020214 A 2913 214076334101 PUMP BELL 214 214ST 1182106 SW HYD SYSTEM FAILED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5748M 28102 DURING FLIGHT, UTILITY HYDRAULIC SYSTEM FAILED. MAINTENANCE FOUND UTILITY HYDRAULIC PUMP DELIVERY PRESSURE LOW. 2 G 7 2 4U H10SW 2002030400088 20020304 00088 SW 2002 3 4 HEEA077846 1 20020215 A 2435 BRUSHES BELL 407 407 1182206 SW STARTER GEN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 447PH 2837 2591 53114 STARTER GEN HAS WORN BRUSHES. 1 G 7 1 3U O H2SW 2002030400089 20020304 00089 SW 2002 3 4 HEEA077847 1 20020215 A 2435 BRUSHES BELL 407 407 1182206 SW STARTER GEN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 493PH 1895 99100 53393 STARTER GEN HAS WORN BRUSHES. 1 G 7 1 3U O H2SW 2003021000139 20030210 00139 NM 2003 2 10 DHL2002750001 1 20020227 A 4990 APU BOEING 727 7272M7 138407S NM APU BAY SMOKE A DHLA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 750DH 21951 HOSE / SMOKE IN COCKPIT AND IN UPPER CARGO AREA FROM LT PACK. DEFERRED PER MEL 21-14 DMI 8649 PLACARD INSTALLED ID 34 518. REF DMI 8649 HAZE / SMOKE IN COCKPIT AND IN UPPER CARGO AREA FROM LT PACK. CHECKED RT AMD LT COALESER BAGS, NO O IL EVIDENT, OPERATED PACKS WITH APU DUPLICATED PROBLEM. RAN ENGINES 1 & 3, OPERATED A/C PACKS SMOKE CLEARED. APU PRODU CING SMOKE, EVIDENCED BY HIGH OIL USAGE. LT PACK. 2 L 7 3 4F A3WE 2002030400090 20020304 00090 SW 2002 3 4 HEEA077849 1 20020215 A 6310 412040111105 CARBON SEAL BELL 412 412 1182202 SW MAIN ROTOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 MAIN ROTOR CARBON RING PART OF SEAL ASSY CRACKED. 1 G 7 2 4U H4SW 2002030400091 20020304 00091 WP 2002 3 4 DHL2002806005 1 20020227 A 3230 HOOK DOUG DC8 DC873F 302199F WP LANDING GEAR BROKEN A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 806DH 46002 AFTER TAKEOFF COULD NOT RAISE GEAR AND AIRCRAFT WOULD NOT TRANSITION TO FLIGHT MODE. FOUND HOOK ASSY BROKEN. REMOVED A ND REPLACED HOOK ASSY PER M/M 32-21-4, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2002030400092 20020304 00092 SW 2002 3 4 HEEA077853 1 20020218 A 8011 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE STUCK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 PILOT HAS TO DISENGAGE STARTER MANUALLY. HANGS UP. 2 G 7 2 4U H10SW 2002030400093 20020304 00093 NM 2002 3 4 DL76G020068 1 20020119 A 3150 4058650950 DISPLAY BOEING 767 767332 1382001 NM COCKPIT WRONG PART A DALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 SO 27 1603 29695 DIVERTED TO JFK DUE RIGHT FMS MCDU DISPLAY INCORRECT. FOUND LEFT MCDU WRONG P/N INSTALLED, REPLACED LEFT MCDU WITH P/N 341002530. GROUND TEST OK. 2 L 7 2 4F RT A1NM 2002030400094 20020304 00094 SW 2002 3 4 HEEA077854 1 20020218 A 6210 407015001117 EROSION SHIELD BELL 407 407 1182206 SW M/R BLADE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 3246 53003 MAIN ROTOR BLADE EROSION SHIELD WORN AND CORRODED. FILLER MISSING. NEED PAINTING. 1 G 7 1 3U O H2SW 2002030400095 20020304 00095 NM 2002 3 4 DLM11020178 1 20020213 A 2530 OVEN DOUG MD11 MD11 3023602 NM GALLEY DIRTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 810DE 48565 OVENS NR 305-306-327-328 HAD TO BE TURNED OFF DUE TO BILLOWING SMOKE. CLEANED PAPER AND DEBRIS FROM OVEN TRAYS. OVEN T RAYS REPLACED BY CATERER. OPERATED ALL OVENS FOR 35 MINUTES. ALL OVEN TEMPERATURE CONTROL AND TIMERS OPERATED NORMAL. OVENS NR 305-306-327-328 OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2002030400096 20020304 00096 NM 2002 3 4 DLM88020140 1 20020204 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 941DL 49814 EMERGENCY TRACK LIGHTING DAMAGED AT 34D. REPAIRED SAME. 2 L 7 2 4F RT A6WE 2002030400097 20020304 00097 2002 3 4 SWAA020452 4 20020227 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002030400098 20020304 00098 NM 2002 3 4 SWAA020453 1 20020227 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED 2.50 INCHES LONG AT BS 905, STR 25R. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F A16WE 2002030400099 20020304 00099 NM 2002 3 4 VNAA0202027 1 20020228 A 7900 O-RING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 471PS 3007 DURING CRUISE, THE CREW NOTICED A DROP IN OIL PRESSURE AND TEMPERATURE. THE CREW CALLED MAINTENANCE CONTROL, DECLARED A N EMERGENCY, AND SHUT DOWN THE #2 ENGINE. THE CREW THEN LANDED IN STL WITH NO FURTHER INCIDENTS. MAINTENANCE CONTROL S ENT MECHANICS FROM PIT TO STL. MAINTENANCE THEN INSPECTED AND FOUND AN O-RING ON THE OIL COOLER NOZZLE DEFORMED ALLOWIN G OIL TO DRAIN FROM THE ENGINE. MAINTENANCE REPLACED THE O-RING IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 79-00-00. OPERATIONAL AND LEAK CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002030400100 20020304 00100 2002 3 4 VNAA0202022 4 20020219 A 3140 7013348937 DAU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 427JS 1669 3039 WHILE EN ROUTE TO PHL, THE CREW RECEIVED A DOORS LIGHT ON THE RED WARNING PANEL. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO CREW. ONCE THE AIRCRAFT SLOWED TO 155 KNOTS AND DESCENDED DOWN TO 12,000 FEET THE INDICATION E XTINGUISHED. THE CREW CONTINUED TO CREW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTE NANCE REPLACED THE DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WER E PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002030400101 20020304 00101 NM 2002 3 4 DLM88020142 1 20020205 A 2910 P240002080240HH HYDRAULIC LINE DOUG MD88 MD88 3023688 NM HYDRAULIC SYS FAILED A DALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 909DE 00 53418 APPROX 20 MINUTES INTO FLIGHT WHILE CRUISING FL290 MASTER CAUTION ILLUMINATED W/L HYD PRESS LOW LIGHT ON. ANNUNCIATOR P ANEL HYDRAULIC PRESSURE WAS ZERO AND QTY WAS DOWN TO 2 QTS. RAN APPROPRIATE CHECKLISTS (SHUTTING OFF THE L ENG HYD PUMP ), PRESSURE STAYED AT ZERO AND QTY CAME BACK TO 7 QTS. CHECKED LT ENG PUMP CASE DRAIN FILTER DUE LOW HYD QTY. FILTER C HECKS NORMAL. REPLACED LT ENG PUMP CASE DRAIN FILTER. REPLACED LINES AT LT PRESS/CASE RETURN MOD. PRESSURE CHECKS GOOD LEAK CHECK GOOD. 2 L 7 2 4F RT A6WE 2002030400102 20020304 00102 2002 3 4 DLM88020148 4 20020207 A 2230 AUTOTHRUST SYS DOUG MD88 MD88 3023688 NM COCKPIT MALFUNCTIONED A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 925DL 49712 ON TAKEOFF ROLL ENGAGED THROTTLES DROVE TO T/O SETTING AND CLAMPED PRIOR TO 80 KNOTS. EPRS AND EPR SET MARKS STARTED TO ROLL BACK. DISCONTINUED T/O. DURING REVERSE THRUST AND TAXI BACK ENGINES LOOKED FINE. PERFORMED ENGINE TAKEOFF POWER RUN PER PFHB. ALL INDICATIONS NORMAL FOR NR 1 AND NR 2 ENGINE. TESTED AUTO THROTTLE SYSTEM, CHECKS OK. 2 L 7 2 4F RT A6WE 2002030400103 20020304 00103 NM 2002 3 4 DLM88020150 1 20020208 A 5320 WEB DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 954DL 49885 CUSP WEB DAMAGED AT STA 579. 2 L 7 2 4F RT A6WE 2002030400104 20020304 00104 NM 2002 3 4 DLM88020167 1 20020210 A 3350 BALLAST DOUG MD88 MD88 3023688 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 958DL 49977 EMERGENCY LIGHT B5-101 INOP. REPLACED BALLAST ASSY, CHECKS GOOD. 2 L 7 2 4F RT A6WE 2002030400105 20020304 00105 NM 2002 3 4 DLM88020174 1 20020212 A 5330 2953657501 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 DURING HMV-2 A DENT WAS NOTICED AT FS 89.050 BETWEEN L18R AND L19R. DENT WAS CUT OUT AND AN INTERNAL REPAIR INSTALLED P ER ERA 412359-14. 2 L 7 2 4F RT A6WE 2002030400106 20020304 00106 NM 2002 3 4 DLM88020175 1 20020212 A 5310 59360381 DOOR FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 DURING HMV-2, CORROSION ON THE C2 DOORWAY JAMB BEAM WAS NOTED AT THE DOOR STOP FITTING HOLES. ALSO, ALONG THE HORIZ FLA NGE OF THE BEAM. THERE WAS AN EXISTING SRM REPAIR WHICH WAS REMOVED. DAMAGE WAS REMOVED, CLEANED UP AND A REPAIR INSTA LLED PER ERA 412362-14, REV A. 2 L 7 2 4F RT A6WE 2002030400107 20020304 00107 NM 2002 3 4 DLM88020177 1 20020212 A 2120 ODOR DOUG MD88 MD88 3023688 NM CABIN DETECTED A DALA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 27 914DL 49545 LEFT AFT LAV SMOKE DETECTOR SOUNDED ON APPROACH FOLLOWED BY HOT SMELL FUMES IN CABIN AND COCKPIT. NO VISIBLE SMOKE AND SMELL DISSIPATED ON TAXI. CROSSFEEDS CLOSED, AIRFOIL ANTI ICE OFF, ENGINE ANTI ICE ON, APU OFF, LEFT TEMP CONTROL COLD, RIGHT TEMP CONTROL WARM. SMELL DESCRIBED AS PACK OVERHEAT. NO PACK TRIP. PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2002030400108 20020304 00108 NM 2002 3 4 DLM88020194 1 20020215 A 5320 THRESHOLD DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 929DL 49716 CORROSION ON C-1 LOWER THRESHOLD FWD OF AFT STOP. REPAIRED PER MD-80 DRD 53-05-D FIG 804. 2 L 7 2 4F RT A6WE 2002030400109 20020304 00109 NM 2002 3 4 DLM88020197 1 20020217 A 4990 SEAL DOUG MD88 MD88 3023688 NM APU BROKEN A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 922DL 9543 49646 P80332 SMOKE DETECTOR ACTIVATED IN LAV F/O SIDE ON T/O TO 8000 FT, THEN WHEN OUT, NO ENG / WING ICE ON CROSS FEEDS CLOSED. FOU ND APU OIL CAP SEAL BROKEN. REPLACED APU OIL CAP. REMOVED APU INLET PANEL AND CLEANED. PERFORMED STEPS 1-7 OF DUCT BU RN OUT. COMPLIED WITH DUCT BURN OUT OP 5088. 2 L 7 2 4F RT A6WE 2002030400110 20020304 00110 NM 2002 3 4 DLM88020208 1 20020219 A 3234 MS250081 SWITCH DOUG MD88 MD88 3023688 NM COCKPIT FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 905DL 49536 ALL THREE LANDING GEAR LIGHTS REMAINED ILLUM. RED WITH GEAR HANDLE UP, NORMAL INDICATION WITH GEAR HANDLE DOWN. GEAR C AME UP WITH GEAR HANDLE UP. REPLACED S1-89 (LEVER SWITCH) AND ACTUATOR PER M/M. 2 L 7 2 4F RT A6WE 2002030400111 20020304 00111 NM 2002 3 4 DLM88020209 1 20020219 A 2460 353448736 RELAY DOUG MD88 MD88 3023688 NM COCKPIT BURNED A DALA K NONE M OVER TEMP IN INSP/MAINT 1 SO 27 926DL 49713 RELAY R2-50 GROUND SERVICE BUS TIE WAS FOUND BURNT AND TERMINALS A2 AND B2 SHORTED. REPLACED SAME. 2 L 7 2 4F RT A6WE 2002030400112 20020304 00112 NM 2002 3 4 DLM90020100 1 20020126 A 2751 622EN149RB SWITCH DOUG MD90 MD9030 3023690 NM PYLON FLAP FAILED A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 905DA 53385 PYLON FLAP FAULT EOAP MESSAGE DURING TAKEOFF, RESULTING IN REJECTED TAKEOFF AT 110 KIAS. FOUND PYLON FLAP SWITCH S1-711 FAILED. REPLACED SAME PER MM. 2 L 7 2 4F RT A6WE 2002030500020 20020305 00020 NM 2002 3 5 F3LA200200093 1 20020228 A 5320 WEB BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON WEB AT STA 797 BETWEEN STR 22-R AND 24-R. REPLACED WEB PER SRM 51-30 -2 AND 51-10-1. 2 L 7 2 4U RT A16WE 2002030500021 20020305 00021 NM 2002 3 5 F3LA200200094 1 20020228 A 2550 PANEL BOEING 737 7372Y5 1384554 NM CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION AT SCREW HOLES ON TRANSITION PANEL AT STA 500-520. FABRICATED AND INSTA LLED REPLACEMENT TRANSITION PANEL PER SRM 51-21-41. 2 L 7 2 4U RT A16WE 2002030500022 20020305 00022 NM 2002 3 5 F3LA200200095 1 20020228 A 5320 THRESHOLD BOEING 737 7372Y5 1384554 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CRACK IN RADIUS UPPER SURFACE 28 INCHES FWD OF AFT EDGE OF WEB THRESHOLD C-2 DOOR AT STR 25-R, STA 794-847. REMOVED DAMAGED AREA AND INSTALLED DOUBLER AND FILLER ON WEB PER SRM 51-40-3. 2 L 7 2 4U RT A16WE 2002030500023 20020305 00023 NM 2002 3 5 F3LA200200096 1 20020228 A 5320 STIFFENER BOEING 737 7372Y5 1384554 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED STIFFENER ANGLE CRACKED AT STA 298 - STA 304. FABRICATED AND INSTALLED REPLACEMEN T CLIP PER SRM 51-10-2 AND 51-30-2. 2 L 7 2 4U RT A16WE 2002030400113 20020304 00113 NM 2002 3 4 DLM90020132 1 20020202 A 3350 RPS1 POWER SUPPLY DOUG MD90 MD9030 3023690 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 916DN 53396 FWD EMERGENCY TRACK LIGHTING INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A6WE 2002030400114 20020304 00114 NM 2002 3 4 DLM90020189 1 20020214 A 3350 SPLICE DOUG MD90 MD9030 3023690 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 916DN 53396 EMERGENCY LIGHTS IN FIRST CLASS INOP. FOUND BAD SPLICE AND REPLACED FUSES IN BATTERY PACK. 2 L 7 2 4F RT A6WE 2002030400117 20020304 00117 SW 2002 3 4 HEEA077855 1 20020218 A 6210 407015001117 EROSION SHIELD BELL 407 407 1182206 SW M/R BLADE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 3246 53003 EROSION SHIELD WORN AND CORRODED. FILLER MISSING. 1 G 7 1 3U O H2SW 2002030400119 20020304 00119 SW 2002 3 4 HEEA077856 1 20020218 A 6210 EROSION SHIELD BELL 407 407 1182206 SW M/R BLADE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 3935 53003 EROSION SHIELD WORN. CORRODED. FILLER MISSING. NEED PAINTING. 1 G 7 1 3U O H2SW 2002030400120 20020304 00120 SW 2002 3 4 HEEA077857 1 20020218 A 6210 407015001117 BLADE BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 3246 53003 EROSION SHIELD WORN. BLADE CORRODED. FILLER MISSING. NEED PAINTING. 1 G 7 1 3U O H2SW 2002030500024 20020305 00024 NM 2002 3 5 F3LA200200097 1 20020228 A 5320 WEB BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED VERTICAL WEB CORRODED FROM STA 352 TO STA 360. FABRICATED AND INSTALLED REPLACEME NT WEB PER SRM 51-20-01 AND 51-30-2. 2 L 7 2 4U RT A16WE 2002030500019 20020305 00019 EA 2002 3 5 COMA0260132 1 20020225 A 5320 601R31171 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 931CA 18207 7037 THE INTERCOSTAL FLANGE AT LBL 36 AND RBL 36 AND ANGLE AT LBL 27 ARE CRACKED FS 484. REMOVED CRACKED ANGLES AND FABRICAT ED NEW ANGLES, INSTALLED IAW WVAC EO 601R-53-2928. 2 L 7 2 4F RT A21EA 2002031800077 20020318 00077 NM 2002 3 18 373PA0001 1 20020303 A 3350 86210144 POWER SUPPLY BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 373PA 23749 LEFT AFT DOOR STROBE EMERGENCY LIGHT FAILED TO ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY. 2 L 7 2 4F RT A16WE 2002030400162 20020304 00162 2002 3 4 801DM0001 4 20020218 A 2230 TRANSDUCER BOEING 757 757200 1384950 NM A PIDA K NONE O OTHER DE DESCENT 1 SO 05 801DM 26240 Right autothrottle does not advance with left throttle after retarding to idle intermittently. Adjusted BVCU/PLH transdu cer. 2 L 7 2 4F RT A2NM 2002030400163 20020304 00163 SW 2002 3 4 HEEA077858 1 20020219 A 6310 406040516101 SHAFT 406040500131 BELL 407 407 1182206 SW FREEWHEEL UNIT LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 402PH A4001 53159 FREEWHEEL UNIT SHAFT LEAKING. 1 G 7 1 3U O H2SW 2002030400170 20020304 00170 WP 2002 3 4 ZW0A0202501 1 20020303 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 950U 49230 THE CABIN EGRESS LIGHTS WERE FLICKERING. REPLACED THE NUMBER 3 EGRESS BATTERY PACK. CHECK-C 10-24-2001 STL. --CLOSED-- - 2 L 7 2 4F A6WE 2002030400171 20020304 00171 SO 2002 3 4 CHQ000127 1 20020302 A 2611 SMOKE WARNING EMB 145 EMB145 3260210 SO COCKPIT FALSE ACTIVATION A CHQA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 271 145305 BAGGAGE SMOKE WARNING AFTER T/O. CREW BLEW FIRE EXTINGUISHERS, NO EVIDENCE OF FIRE. COULD NOT DUPLICATE SMOKE WARNING AND DETECTION SYSTEM, OPS CHECK GOOD. FERRIED A/C TO CMH FOR FIRE BOTTLES. 2 L 7 2 4F RT T00011AT 2002030400172 20020304 00172 SO 2002 3 4 CHQ000128 1 20020303 A 3010 ANTI-ICE SYSTEM EMB 145 EMB145 3260210 SO COCKPIT MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 262 145168 ICE CONDITION A/I INOP, W/A STAB A/I INOP EICAS MESSAGE AFTER T/O. RESET AIRCRAFT POWER, A/I TEST OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2002030400173 20020304 00173 2002 3 4 CHQ000200 4 20020220 A 3413 CONNECTOR SAAB SF340 SF340A 7850100 EU VSI DAMAGED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 125 125 RIGHT PROP OIL PRESSURE LOW, THEN VSI INOP. SERVICED RIGHT PROP GEARBOX OIL LEVEL, THEN REPAIRED VSI CONNECTION. 2 L 7 2 4T RT A52EU 2002030400174 20020304 00174 EA 2002 3 4 COMA0260133 1 20020227 A 5300 601R431143 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FS349 AND RBL27 MISDRILLED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 931CA 18207 7037 THE INBOARD FLANGE OF A BRACKET ASSEMBLY HAS SHORT EDGE DISTANCE WITH A HOLE COMMON TO THE FLOOR BEAM AT FS349 AND RBL27 .FABRICATED AND INSTALLED A NEW BRACKET I/A/W WVAC EO 601R-53-2991. 2 L 7 2 4F RT A21EA 2002030400175 20020304 00175 EA 2002 3 4 COMA0260134 1 20020227 A 5300 60094017374 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS280 AT RBL9 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 931CA 18207 7037 THE VERTICAL J STIFFENER AT FS280 RBL9 WAS CRACKED.REMOVED CRACKED J STIFFENER. FABRICATED AND INSTALLED A NEW J STIFFEN ER I/A/W WVAC EO 601R-53-2990. 2 L 7 2 4F RT A21EA 2002030400176 20020304 00176 NM 2002 3 4 F3LA200200045 1 20020221 A 2550 PANEL BOEING 737 7372Y5 1384554 NM CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED TRANSITION PANEL AT STA 520, STR 26-L, CORRODED AT NUT PLATE LOCATION. FABRICATED AND INSTALLED REPLACEMENT PANEL PER SRM 51-10-1. 2 L 7 2 4U RT A16WE 2002030400179 20020304 00179 EA 2002 3 4 COMA0260135 1 20020227 A 5300 601R31527XXX ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS310 TO FS349 MISDRILLED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 931CA 18207 7037 THE THRESHOLD SUPPORT ANGLE AT THE PASSENGER DOOR HAS SHORT EDGE DISTANCE ON THE UPPER FASTENER HOLES.FABRICATED AND INS TALLED A NEW ANGLE I/A/W WVAC EO 601R-53-2987A. 2 L 7 2 4F RT A21EA 2002030400181 20020304 00181 NM 2002 3 4 F3LA200200049 1 20020221 A 5320 MOUNT BRACKET BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CARGO NET ATTACH CLEAT MOUNT PLATE AT STA 847 ABOVE STR 22-L. FABRIC ATED AND INSTALLED NEW MOUNT PLATE PER SRM 51-10-2 AND 51-21-171. 2 L 7 2 4U RT A16WE 2002030400182 20020304 00182 NM 2002 3 4 F3LA200200050 1 20020221 A 5330 SKIN BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT, LOWER FWD CORNER, AT STA 790. REP AIRED DAMAGED SECTION PER SRM 53-30-3. 2 L 7 2 4U RT A16WE 2002030400183 20020304 00183 NM 2002 3 4 F3LA200200051 1 20020221 A 5320 SUPPORT BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY SUPPORT PARTITION FRAME CORRODED AT STA 998, 14 LBL. FABRICATED AND INSTALLED REPLACEMENT FRAME SUPPORT PER SRM 51-10-2. 2 L 7 2 4U RT A16WE 2002030400188 20020304 00188 NM 2002 3 4 F3LA200200057 1 20020221 A 5315 FLOORBEAM BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY TRANSVERSE BEAM CORRODED AT STA 1006 TO STA 1016, LBL 6. REPLACED TR ANSVERSE FRAME PER SRM 51-30-2. 2 L 7 2 4U RT A16WE 2002030400192 20020304 00192 NM 2002 3 4 02FDEA00171 1 20020302 A 2612 774001 SMOKE DETECTOR BOEING 727 727233 138408A NM MAIN CARGO #6 FAILED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 218FE 21101 02-57 MAIN CARGO SMOKE ALARM WENT ON. WENT OUT UPON EXECUTION PROC. OCCURRED WHEN ENG ANTI-ICE SECURED. RAN ALL THREE ENGINES PER JRH. NO DEFECTS NOTED. R&R #6 SMOKE DETECTOR PRECAUTIONARY. 2 L 7 3 4F RT A3WE 2002030700051 20020307 00051 NM 2002 3 7 02FDEA00176 1 20020304 A 5313 STRINGER BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER 15 LT CRACKED BS 720B+15. REMOVED AND REPLACED STRINGER PER SRM 53-10-3 FIG 5. 2 L 7 3 4F RT A3WE 2002030700053 20020307 00053 NM 2002 3 7 02FDEA00178 1 20020218 A 5320 INTERCOSTAL BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION C53-113-01(2) ON INTERCOSTAL WEB I/B AND O/B SIDES BS 1070-1090 RBL 2, WL 135-137. REMOVED AND REPLACED INTER COSTAL PER SRM 51-20-01, 51-10-3, 51-30-2. 2 L 7 3 4F RT A3WE 2002030400204 20020304 00204 NM 2002 3 4 F3LA200200072 1 20020223 A 5311 FRAME BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CHORD AT STA 352, STR 28L. REPLACED DAMAGED CHORD PER SRM 51-10-2 AN D SRM 51-30-2. 2 L 7 2 4U RT A16WE 2002030400209 20020304 00209 NM 2002 3 4 F3LA200200077 1 20020226 A 2131 7638102 CONTROLLER BOEING 737 73736E 138443A NM CABIN PRESSURE FAILED A F3LA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 314FL 3369 25256 AIR TURNBACK. FLIGHT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR STANDBY MODE DURING CLIMBOUT. REPLACED CAB IN PRESSURE CONTROLLER AND OUTFLOW VALVE, PERFORMED OPERATIONAL TEST AND SYSTEM CHECKED OKAY. 2 L 7 2 4F RT A16WE 2002030400211 20020304 00211 NM 2002 3 4 F3LA200200079 1 20020224 A 5311 BELTFRAME BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON BELT FRAME AT STA 827, RBL 10. REMOVED DAMAGE, FABRICATED AND INSTAL LED PER SRM 53-10-4. 2 L 7 2 4U RT A16WE 2002030400212 20020304 00212 NM 2002 3 4 F3LA200200080 1 20020224 A 5347 CARGO TRACK BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 315FL 3460 25159 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO BAY FLOOR TIE DOWN TRACK AT STA 859, RBL 13.8, CORRODED. SPLICED IN SEC TION OF AFT CARGO BAY FLOOR TIE DOWN TRACK PER SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002030400213 20020304 00213 NM 2002 3 4 F3LA200200081 1 20020224 A 2550 PANEL BOEING 737 73736E 138443A NM CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 315FL 3460 25159 DURING C-2 CHECK, INSPECTION REPORTED RT FLOOR TO SIDEWALL TRANSITION PANEL IN AFT CARGO COMPARTMENT CORRODED, STA 727 T O STA 767, STR 26R. FABRICATED AND INSTALLED REPLACEMENT TRANSITION ANGLE PER SRM 51-40-5 AND 51-30-2. 2 L 7 2 4F RT A16WE 2002030400214 20020304 00214 NM 2002 3 4 F3LA200200082 1 20020224 A 5320 CHANNEL BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 315FL 3460 25159 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR CHANNEL CORRODED AT STA 727, RBL 8.1. FABRICATED AND INSTALLED REPLACEMENT PART PER SRM 51-70-11 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002030400215 20020304 00215 NM 2002 3 4 F3LA200200083 1 20020224 A 5320 CHANNEL BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 315FL 3460 25159 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR CHANNEL CORRODED AT STA 859, LBL 3. REMOVED CORROSION AND DAMAGE, FABRICATED REPAIR ANGLE AND INSTALLED PER SOPM 20-41-02 AND SRM 53-60-53, 51-70-11, 51-10-11. 2 L 7 2 4F RT A16WE 2002030400216 20020304 00216 NM 2002 3 4 F3LA200200084 1 20020224 A 5320 ANGLE BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 315FL 3460 25159 DURING C-2 CHECK, INSPECTION REPORTED FLOOR ANGLES CORRODED IN AFT CARGO COMPARTMENT AT STA 787, STR 26R. REPLACED FLOO R STRAP BETWEEN STA 787 AND 867 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002030400218 20020304 00218 NM 2002 3 4 F3LA200200086 1 20020224 A 5347 CARGO TRACK BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 315FL 3460 25159 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR TIE DOWN CORRODED AT STA 859 AND STA 772, LBL 17.2. R EPLACED CORRODED AFT CARGO COMPARTMENT FLOOR TRACKS PER SRM 53-60-53. 2 L 7 2 4F RT A16WE 2002030400221 20020304 00221 NM 2002 3 4 F3LA200200090 1 20020227 A 7110 COWLING BOEING 737 7372Y5 1384554 NM NR 1 ENGINE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE LT OUTBOARD COWL TOP EDGE DAMAGED BETWEEN SECOND AND LAST HINGE. REMO VED DAMAGE PER SRM 51-40-3. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-2, 51-40-3 AND 51-30-2. 2 L 7 2 4U RT A16WE 2002030400225 20020304 00225 EU 2002 3 4 RAIA00203086 1 20020301 A 3010 13730897K FUSE JETAIR JETSTM JETSTM4101 1500501 EU A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 569HK 41088 5531-STL- CREW REPORTED ELEVATOR HORN DE-ICE FAILURE DURING CLIMB. MAINTENANCE REMOVED AND REPLACED A DEFECTIVE DE-ICE S YSTEM FUSE, OPS CK OK. 2 L 7 2 4T RT A41NM 2002030400226 20020304 00226 EU 2002 3 4 RAIA00203089 1 20020303 A 2731 C850176 STALL WARNING JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 555HK 12970 41072 5518-STL- LEFT "STALL" ANNUNCIATOR ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE LEFT STALL SENSOR, OPS CK OK. 2 L 7 2 4T RT A41NM 2002030500002 20020305 00002 WP 2002 3 5 ABXA010755 1 20020301 A 3260 7000010101ABX SWITCH DOUG DC9 DC932 3022066 WP NOSE DEFECTIVE A ABXA O OTHER O OTHER CL CLIMB 1 GL 23 982AX 47317 ON INITIAL GEAR EXTENSION AT ILN, NOSE GEAR DID NOT INDICATE DOWN/LOCKED. SUBSEQUENT RETRACTION/EXTENSION CYCLE YIELDED NORMAL INDICATION. REPLACED THE NOSE GEAR DOWN LOCK SWITCH IAW DC-9 MM 32-60-02. 2 L 7 2 4F A6WE 2002030500003 20020305 00003 WP 2002 3 5 MWEA020154 1 20020301 A 5310 99177013 INTERCOSTAL DOUG DC9 DC932 3022066 WP STATION 1168 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 AFT ACCESSORY, INTERCOSTAL BENT AND HAS AREAS OF BARE METAL BETWEEN CANTED FRAMES 1168 AND 1155. -- FABRICATED AND INS TALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2002030500004 20020305 00004 WP 2002 3 5 MWEA020155 1 20020301 A 5310 991966911 CLIP DOUG DC9 DC932 3022066 WP STATION 598 ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FRAME TO INTERCOSTAL ATTACH CLIP AT STATION 598 LEFT HAS ELONGATED HOLES. -- FABRICATED AND INSTALLED CLIP. 2 L 7 2 4F A6WE 2002030500005 20020305 00005 WP 2002 3 5 MWEA020156 1 20020301 A 5310 2913690501 CLIP DOUG DC9 DC932 3022066 WP STATION 598 ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FRAME TO SKIN ATTACH CLIP AT STATION 598 LEFT, UPPER FORWARD CORNER OF WINDOW RETAINER HAS ELONGATED HOLE. -- FABRICAT ED AND INSTALLED ATTACH CLIP. 2 L 7 2 4F A6WE 2002030500006 20020305 00006 WP 2002 3 5 MWEA020157 1 20020301 A 5415 991550030 CLIP DOUG DC9 DC932 3022066 WP RIGHT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 RIGHT PYLON SUPPORT CLIP AT UPPER REAR SPAR CAP IS CRACKED. -- FABRICATED AND INSTALLED CLIP. 2 L 7 2 4F A6WE 2002030500007 20020305 00007 NM 2002 3 5 SWAA020457 1 20020302 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 395SW 27689 DURING SCHEDULED A1 CHECK, FOUND EEPLS COVER MISSING AT ROW 22. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002030500008 20020305 00008 2002 3 5 SWAA020458 4 20020301 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD CABIN DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED C2 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT BAR ASSY'S OUT OF ADJUST. ADJUSTED SLIDE S PER MM. 2 L 7 2 4F RT A16WE 2002030500009 20020305 00009 NM 2002 3 5 SWAA020459 1 20020301 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED BC3 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT LT OVERWING EXIT. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002030500010 20020305 00010 NM 2002 3 5 SWAA020460 1 20020302 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 714CB 27848 EEPLS LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002030500011 20020305 00011 NM 2002 3 5 SWAA020464 1 20020228 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED BC1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE IN AFT CABIN. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002030500012 20020305 00012 NM 2002 3 5 SWAA020465 1 20020228 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED BC1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT LT OVERWING EXIT. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002030500013 20020305 00013 NM 2002 3 5 SWAA020466 1 20020301 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 5 INCHES LONG AT BS 927, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002030500014 20020305 00014 EU 2002 3 5 02034306 1 20020203 A 3350 SOCKET JETAIR JETSTM JETSTM4101 1500501 EU EXTERIOR DIRTY A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 306UE 41020 DURING INSPECTION IT WAS DISCOVERED THAT THE LT AFT EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNE L CLEANED THE LAMP SOCKET AND LAMP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002030500015 20020305 00015 EU 2002 3 5 02055316 1 20020224 A 3350 BATTERY PACK JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 316UE 41055 DURING INSPECTION IT WAS DISCOVERED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FORWARD, MID CABIN, AND AFT EMERGENCY EXIT LIGHT BATTERY PACKS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002030500016 20020305 00016 EA 2002 3 5 02056648 1 20020225 A 3350 FUSE CNDAIR CL600 CL6002B19 1900309 EA POWER SUPPLY BLOWN A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 648BR 7406 DURING INSPECTION IT WAS DISCOVERED THAT THE NR 1 EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED A ND REPLACED THE FUSE IN THE EMERGENCY EXIT LIGHTING POWER SUPPLY. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAF T WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002030500017 20020305 00017 EU 2002 3 5 02060321 1 20020301 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 321UE 41045 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. THE AIRCRAFT WA S FERRIED TO IAD FOR MAINTENANCE. MAINTENANCE PERSONNEL SECURED A LOOSE CONNECTOR FOR THE EMERGENCY FLOOR TRACK LIGHTIN G. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002030500018 20020305 00018 EU 2002 3 5 02062329 1 20020302 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 329UE 41097 DURING INSPECTION THE CENTER SECTION OF THE EMERGENCY FLOOR TRACK LIGHTING WAS DISCOVERED TO BE INOPERATIVE. MAINTENANC E PERSONNEL REMOVED AND REPLACED ONE RED STRIP LAMP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNE D TO SERVICE. 2 L 7 2 4T RT A41NM 2002030800021 20020308 00021 NM 2002 3 8 02FDEA00170 1 20020220 A 5315 BAC1596338 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 HOLE ON FLOORBEAM BS 720F UPPER CHORD LBL 54, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 8. 2 L 7 3 4F RT A3WE 2002031400025 20020314 00025 NM 2002 3 14 02FDEA00173 1 20020302 A 5312 6518745131 PRESSURE PANEL BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION ON PRESSURE CEILING LT MLG W/W UNDER DOUBLER BS 890, LBL 45, WL 196. REMOVED AND REPLACED WEB PER SRM 51-30-2 , 51-30-5. 2 L 7 3 4F RT A3WE 2002030800026 20020308 00026 NM 2002 3 8 02FDEA00174 1 20020302 A 5320 65863552 BEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION C53-224-05 ON LOWER CHORD OF STUB BEAM BS 783, RBL 64, WL 201. REMOVED AND REPLACED LOWER CHORD PER SRM 51-30 -5 & 51-30-2. 2 L 7 3 4F RT A3WE 2002031400027 20020314 00027 NM 2002 3 14 02FDEA00175 1 20020228 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FUSELAGE SKIN DENTED AT BS 362-370 BETWEEN STRS 2-3 R. REMOVED AND REPLACED SKIN PER SRM 53-30-3 & EA 7-5330-62783. 2 L 7 3 4F RT A3WE 2002030700054 20020307 00054 NM 2002 3 7 02FDEA00179 1 20020304 A 5320 SPLICE BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 DENT IN TOP FRAME SPLICE AT BS 500, RBL 29, WL 158 FWD CARGO BAY. REMOVED AND REPLACED FRAME SPLICE PER SRM 51-20-1, 51 -30-2. 2 L 7 3 4F RT A3WE 2002031300051 20020313 00051 CE 2002 3 13 GLBA2002022 1 20020217 A 2130 1143800595 SHUTOFF VALVE BEECH 1900 1900D 1154162 CE LEFT LEAKING A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 201GL 119 UE201 LEFT ENGINE TORQUE FLUCTUATION WITH CABIN BLEED FUNCTIONS. REPLACED PRSOV, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002030500026 20020305 00026 CE 2002 3 5 GLBA2002023 1 20020221 A 2752 TERMINAL BEECH 1900 1900D 1154162 CE T/E FLAP LOOSE A GLBA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 03 211GL UE211 FLAPS STUCK AT 17 PERCENT, FOUND LOOSE TERMINAL ON MOTOR RELAY. SECURED, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002030500027 20020305 00027 CE 2002 3 5 GLBA2002024 1 20020223 A 2460 1293640665 PRINTED CKT BOAR BEECH 1900 1900D 1154162 CE ELECTRICAL SYS FAULTY A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 228GL 238 UE228 BATTERY TIE OPENED INFLIGHT. REPLACED BUSS TIE PCB, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002030500028 20020305 00028 CE 2002 3 5 GLBA2002025 1 20020224 A 5610 10138402517 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT CRACKED A GLBA K NONE O OTHER DE DESCENT 1 NM 03 228GL 2936 UE228 CAPTAINS WINDSHIELD CRACKED ON DESCENT. REPLACED WINDSHIELD, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002030500029 20020305 00029 EA 2002 3 5 HNAA0200019 1 20020218 A 3246 314801 WHEEL DHAV DHC8 DHC8311 1386006 EA MLG DEPARTED A HNAA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 EA 07 329EN 18998 18998 290 AFTER TAKEOFF AT APPROXIMATELY 500 FEET, NUMBER 3 TIRE FELL OFF AIRCRAFT. AIRCRAFT RETURNED TO FIELD. REPLACED WHEEL A SSEMBLY AND FERRIED AIRCRAFT TO ORF WHERE THE LOWER PISTON AND AXLE WERE REPLACED AND NEW WHEEL ASSEMBLIES INSTALLED. 2 H 7 2 4T RT A13NM 2002030500030 20020305 00030 NM 2002 3 5 HNAA0200020 1 20020225 A 5415 85410273103 FITTING DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 933HA 134 DURING REPAIR OF THE NR 1 NACELLE HORSE COLLAR THE INTERNAL TOP MOUNT FITTING WAS FOUND CRACKED AT THE TOP AFT CORNER FR OM THE RADIUS TO THE EDGE OF THE ATTACH FLANGE. THE CRACK ENCIRCLES THE TOP RIVET OF THE AFT ATTACH FLANGE. REMOVED AN D REPLACED THE FITTING. 2 H 7 2 4T RT A13NM 2002030500031 20020305 00031 NM 2002 3 5 HNAA0200022 1 20020226 A 6120 78249050 PCU DHAV DHC8 DHC8102 2809003 NM NR 1 PROPELLER MALFUNCTIONED A HNAA K NONE R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 07 924HA 18362 516 105 DURING TAKEOFF AFTER V1 NR 1 PROP RPM DROPPED TO 1188 FOR 5 SECONDS. REPLACED PROP CONTROL UNIT. 2 H 7 2 4T RT A13NM 2002030500032 20020305 00032 EU 2002 3 5 MALA020163 1 20020210 A 3010 3D353301 SWITCH SAAB SF340 340B 7860101 EU DE-ICE SYS DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 436XJ 340B436 DURING FLIGHT 2836 TIMER LIGHT ILLUMINATES AFTER SECOND CYCLE OF STAB IN MANUAL MODE. AIR RETURN TO MSP. MAINTENANCE F OUND PSI SWITCH 62HP IN TAIL JUNK WOULD NOT CLOSE AT DECREASE PSI. REMOVED AND REPLACED PSI SWITCH. OPS CHECK GOOD PER MM 30-10-00. 2 L 7 2 4T RT A52EU 2002030500033 20020305 00033 NE 2002 3 5 MALA020164 2 20020216 A 7261 219379001 PUMP BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 4 ENGINE DEFECTIVE A MALA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 GL 15 509XJ E2321 DURING FLIGHT 3408 NR 4 ENGINE LOST OIL QUANTITY AND PSI DROPPING. SHUTDOWN ENGINE. MAINTENANCE REMOVED AND REPLACED N R 4 OIL PUMP IAW AMM 79-20-03. OPS CHECK GOOD. LEAK CHECK GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 2002030500034 20020305 00034 EU 2002 3 5 MALA020165 1 20020214 A 4950 APU BAC 146 AVRO146RJ85A 1500097 EU APU BAY CONTAMINATED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 503XJ E2310 WHILE IN CLT: AFTER SELECTING PACK 1 AND 2 ON WITH APU AIR THE CABIN STARTED TO FILL WITH SMOKE. MAINTENANCE PERFORMED PACK BURN PROCEDURE IAW SUNDSTRAND AMM 1.4.2.1. NO SMOKE NOTED AFTER PROCEDURE. 2 H 7 4 4F RT A49EU 2002030500035 20020305 00035 EU 2002 3 5 MALA020166 1 20020214 A 3230 UPLOCK BAC 146 AVRO146RJ85A 1500097 EU RT MLG LACK OF LUBE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 524XJ E2349 DURING FLIGHT 3460, RIGHT MAIN GEAR WILL NOT INDICATE UP AND LOCKED. AIR TURNBACK TO MSP. MAINTENANCE CLEANED AND LUBE D UP LOCKS, ADJUSTED GEAR DOOR IAW AMM 32-10-21. RAN GEAR UP AND DOWN SEVERAL TIMES. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2002030500036 20020305 00036 EU 2002 3 5 MALA020167 1 20020217 A 2750 AP14161005 CONTROL VALVE SAAB SF340 340B 7860101 EU T/E FLAP FAILED A MALA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 15 451XJ 340B451 ON APPROACH OF FLIGHT 3309, FLAPS FAILED TO EXTEND. QRH'D FLAP 0 LANDING. LANDED LONG RUNWAY WITH MINIMUM BRAKING. MA INTENANCE REMOVED AND REPLACED FLAP CONTROL VALVE IAW SF340MM 27-51-15-2. ALL IS GOOD. 2 L 7 2 4T RT A52EU 2002030500037 20020305 00037 NE 2002 3 5 MALA020168 2 20020219 A 7530 5056T88P01 SHUTOFF VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE BLEED AIR SYS FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 46XJ 340A046 DURING FLIGHT 3372, RT AIR VALVE LIGHT ILLUMINATED INFLIGHT WENT OUT AND CAME BACK ON AFTER 2 MINUTES. AIR RETURN TO MS P. MAINTENANCE REPLACED RT BLEED AIR SHUTOFF VALVE PER CTY-5 MM 75-00-00 OPS CHECK GOOD ON 20 MIN GROUND RUN PER MM 72- 00-00 AC RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2002031200139 20020312 00139 NM 2002 3 12 HNAA0200023 1 20020304 A 2611 PU90461S SMOKE DETECTOR DHAV DHC8 DHC8201 2809001 NM LAVATORY FALSE ACTIVATION A HNAA O OTHER N FALSE WARNING CR CRUISE 1 EA 07 983HA 6960 478 LAV SMOKE DETECTOR SOUNDED IN FLIGHT. MECHANIC IN TPA PERFORMED AN OPERATIONAL CHECK OF THE SMOKE DETECTOR, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2002030500038 20020305 00038 EU 2002 3 5 MALA020169 1 20020223 A 7933 4053T73P01 SENSOR SAAB SF340 340B 7860101 EU RT ENGINE DEFECTIVE A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 402XJ 340B402 DURING FLIGHT 2924, RT ENGINE PROP OIL TEMP HIGH. AIR RETURN TO DTW. MAINTENANCE REPLACED TEMP DETECTOR. 2 L 7 2 4T RT A52EU 2002030500040 20020305 00040 EU 2002 3 5 MALA020171 1 20020227 A 2750 FCU BAC 146 AVRO146RJ85A 1500097 EU T/E FLAP MALFUNCTIONED A MALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 15 524XJ E2349 AIR RETURN FLAPS STAYED AT 18 DEG WHEN SELECTED UP. RESET FLAP CONTROL UNIT. 2 H 7 4 4F RT A49EU 2002030500042 20020305 00042 EU 2002 3 5 MALA020175 1 20020302 A 3260 WARNING SYSTEM BAC 146 AVRO146RJ85A 1500097 EU COCKPIT MALFUNCTIONED A MALA O OTHER N FALSE WARNING UK UNKNOWN 1 GL 15 513XJ E2329 NO GEAR UP AND LOCKED INDICATION. GEAR CYCLED NUMEROUS TIMES, NO FAULTS. SATISFACTORY TEST FLIGHT COMPLETED. 2 H 7 4 4F RT A49EU 2002030500043 20020305 00043 EU 2002 3 5 MALA020176 1 20020302 A 7810 NF24668057 NOZZLE SAAB SF340 340B 7860101 EU RT ENGINE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 423XJ 340B423 RT INTAKE HEAT FAILED DURING FLIGHT. DIVERTED TO DTW. REMOVED AND REPLACED RT EXHAUST NOZZLE. 2 L 7 2 4T RT A52EU 2002030500044 20020305 00044 NE 2002 3 5 MWEA020129 2 20020215 A 7200 JT87B ENGINE DOUG DC9 DC915 3022036 WP PWA JT8 JT8D7B 52053 NE LEFT MALFUNCTIONED A MWEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 31 900ME 45841 654071 AT CRUISE ALT LEFT ENGINE MASTER CAUTION, LEFT ENGINE OIL PRESSURE LOW ANNUNCIATOR ON. LEFT ENGINE OIL PRESSURE IS ZERO . LEFT OIL TEMP IS 20 DEGREES CELSIUS AND QUANTITY IS 17-18 QUARTS. SHUT DOWN BY SELECTION. REMOVED AND REPLACED ENGI NE. 2 L 7 2 4F 4 F A6WE E2EA 2002030500045 20020305 00045 NM 2002 3 5 2002UALA00317 1 20020226 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 RIGHT HAND FUSELAGE SKIN HAS GOUGED AREA WHERE LOWER STAB FAIRING ATTACHES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMP LISHED. REPAIRED WITH DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002030500046 20020305 00046 NM 2002 3 5 2002UALA00318 1 20020226 A 5730 SPLICE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 RIGHT WING LE SKIN SPLICE CRACKED OUTBD #8 SLAT OUTBD. ROTARY ACTUATOR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISH ED. INSTALLED NEW SPLICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002030500047 20020305 00047 NM 2002 3 5 2002UALA00331 1 20020228 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 AFT PIT LEFT HAND SIDE FRAME DENTED AT STATION 1540, ABOVE STR 26L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED . 2 L 7 2 4F 4 F RT A2NM E17NE 2002030500048 20020305 00048 WP 2002 3 5 MWEA020133 1 20020220 A 5320 991014010 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 SUBFLOOR AT STATION 237 OUTBOARD OF NR 4 SEAT TRACK IS CRACKED. FABRICATED AND INSTALLED SUBFLOOR WEB. 2 L 7 2 4F A6WE 2002030500049 20020305 00049 WP 2002 3 5 MWEA020134 1 20020220 A 5321 9957807517 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 FLOORBOARD FUSELAGE STATION 237 TO 313 BETWEEN SEAT TRACK NR 1 AND NR 2 CRACK AT FORWARD END AND CORROSION ON FORWARD ED GE AROUND HOLES. FABRICATED AND INSTALLED FLOORBOARD REPAIR. 2 L 7 2 4F A6WE 2002030500050 20020305 00050 NM 2002 3 5 HNAA0200024 1 20020302 A 3242 83200502001 CABLE DHAV DHC8 DHC8102 2809003 NM L/H WING ROOT BROKEN A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 927HA 35550 117 During aircraft taxi from terminal to hanger by maintenance, there was a loss of right brake control. Subsequent inspect ion found broken cable at #1 brake valve. 2 H 7 2 4T RT A13NM 2002030500051 20020305 00051 WP 2002 3 5 MWEA020137 1 20020222 A 5311 9911500257 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LEFT HAND LOWER RADOME GUIDE PIN HAS A 1.5 INCH CRACK EMANATING FROM ITS HOLE OUTWARD TO A RIVET. REPAIRED PER SRM 53-0 1-00 FIGURE 2 SHEET 3, DOUBLER ON AFT SIDE OF FORMER. 2 L 7 2 4F A6WE 2002030500052 20020305 00052 WP 2002 3 5 MWEA020139 1 20020227 A 5415 991550032 CLIP DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 RIGHT PYLON SUPPORT CLIP AT LOWER REAR SPAR CAP IS CRACKED. FABRICATED AND INSTALLED CLIP. 2 L 7 2 4F A6WE 2002030500053 20020305 00053 WP 2002 3 5 MWEA020140 1 20020227 A 5347 59108205 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 CORROSION ON TOP SIDE OF NR 4 SEAT TRACK AT STATION 200 AND CORROSION ON BOTTOM OF UPPER FLANGE AROUND THREE FASTENER HO LES AT STATION 221 TO 230 OF NR 4 SEAT TRACK. REMOVED SEAT TRACK AT STATION 221 TO 230 AND INSTALLED SEAT TRACK REPLACE MENT AND SPLICE. 2 L 7 2 4F A6WE 2002030500054 20020305 00054 WP 2002 3 5 MWEA020142 1 20020226 A 3260 WARNING SYSTEM DOUG DC9 DC981 3022081 WP COCKPIT MALFUNCTIONED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 814ME 48010 NOSE GEAR UNSAFE LIGHT STAYED ON AFTER GOT THREE GREEN WITH GEAR HANDLE DOWN. INSPECTED NOSE GEAR AND DOORS FOR CONDITI ON AND SECURITY. JACKED AIRCRAFT NOSE AND PERFORMED MULTIPLE NOSE GEAR SWINGS. CHECKED STRUT EXTENSION AND LUBRICATED NOSE GEAR. CHECKED PROXIMITY SENSORS. FREE-FALL NOSE GEAR PERFORMED. MD80 MM 32-21-02, 32-20-00, AND 32-60-05. NO DEF ECTS NOTED AT THIS TIME. 2 L 7 2 4F A6WE 2002030500055 20020305 00055 WP 2002 3 5 MWEA020143 1 20020301 A 5320 59101371 MOUNT BRACKET DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 STATION 351 FLOORBEAM STRUT SIDEWALL MOUNT RIGHT SIDE IS GOUGED. FABRICATED AND INSTALLED MOUNT. 2 L 7 2 4F A6WE 2002030500056 20020305 00056 WP 2002 3 5 MWEA020144 1 20020301 A 5347 59108203 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 CORROSION ON NR 3 SEAT TRACK AT FROM 200 TO STATION 237. FABRICATED AND INSTALLED SEAT TRACK SECTION. 2 L 7 2 4F A6WE 2002030500057 20020305 00057 WP 2002 3 5 MWEA020145 1 20020301 A 5321 99578082 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 CORROSION ON CABIN FLOOR BOARD 31 AT STATION 237. FABRICATED AND INSTALLED SLICE REPAIR. 2 L 7 2 4F A6WE 2002030500058 20020305 00058 WP 2002 3 5 MWEA020146 1 20020301 A 5315 59101487 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 STATION 617 FLOORBEAM IS LOOSE JUST INBOARD OF THE NR 2 SEAT TRACK, SHOWS SIGNS OF CHAFING. REMOVED AND REPLACED FLOORB EAM. 2 L 7 2 4F A6WE 2002030500059 20020305 00059 WP 2002 3 5 MWEA020147 1 20020301 A 5311 995823811 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 LEFT LAV AREA HAS CRACK IN FRAME AT STATION 981 BETWEEN LONGERON 16 LEFT AND 15 LEFT. REMOVED AND REPLACED FRAME. 2 L 7 2 4F A6WE 2002030500060 20020305 00060 WP 2002 3 5 MWEA020149 1 20020301 A 5320 99577401 CLIP DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 KEEL BEAM AREA LEFT SIDE FRAME STATION 658 HAS A CRACKED END CLIP LOCATED AT LONGERON 27 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2002030500061 20020305 00061 WP 2002 3 5 MWEA020150 1 20020301 A 5321 9957807517 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 FLOORBOARD AT FUSELAGE STATION 288 BETWEEN NR 1 AND 2 SEAT TRACK HAS A SMALL PUNCTURE. FABRICATED AND INSTALLED FLOORBO ARD REPAIR. 2 L 7 2 4F A6WE 2002030500062 20020305 00062 WP 2002 3 5 02FDEA00181 1 20020223 A 2821 608473 PUMP DOUG DC10 DC1010F 3022111 WP FAULTY A FDEA H DEACTIVATE SYST/CIRCUITS J O WARNING INDICATION OTHER CL CLIMB 1 SO 25 368FE 46606 02-60 AFTER T/O #3 TANK AFT FUEL PUMP OWR CB POPPED, LIGHT ILLUM. R&R #3 AFT BOOST PUMP PER AMM 28-22-01-2. R&R PUMP H ARNESS. 2 L 7 3 4F A22WE 2002030500063 20020305 00063 WP 2002 3 5 MWEA020158 1 20020302 A 5415 99155007 STIFFENER DOUG DC9 DC914 3022034 WP LEFT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LEFT ENGINE PYLON AFT VERITCAL STIFFENER IS CRACKED LOCATED BETWEEN UPPER AND LOWER AFT PYLON SPARS. -- FABRICATED AND INSTALLED STIFFENER. 2 L 7 2 4F A6WE 2002030500064 20020305 00064 SO 2002 3 5 C2XA02CL063 1 20020304 A 3350 20131A BATTERY EMB 135 EMB135ER 3260203 SO CABIN DISCHARGED A C2XA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 27 27506 9516 30 145206 CLE FLIGHT#3251 THE CREW REPORTED THE EMERGENCY LIGHT STRIP AT SEAT ROW 8 WAS INOPERATIVE.MAINTENANCE REPLACED THE #3 EM ERGENCY LIGHT BATTERY PACK.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002030500065 20020305 00065 NM 2002 3 5 CA020205007 1 20020204 A 5513 6914410 HINGE PIN BOEING 727 727260 NM PWA JT8 JT8D17 52049 NE HORIZONTAL STAB CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION OF HORIZONTAL STABILIZER HINGE PINS, FOUND THE RT SIDE OUTER PIN THREADS AND THREAD RELIEF AREA CORRODED. THE OUTER AND INNER PINS WILL BE REPLACED PRIOR TO NEXT FLIGHT. 2 L 7 3 4F 4 F RT A3WE E2EA 2002030500066 20020305 00066 WP 2002 3 5 MWEA020151 1 20020301 A 5344 4918346507 HINGE FITTING DOUG DC9 DC932 3022066 WP VENTRAL DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 AFT VENTRAL DOOR JAMB, LOWER JAMB DOOR HINGE IS CRACKED. REMOVED AND REPLACED WITH FITTING. 2 L 7 2 4F A6WE 2002030500067 20020305 00067 EA 2002 3 5 COMA0260136 1 20020304 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 965CA 13460 7131 CRACK FOUND ON L/H LOWER WING PLANK AT PANEL 550BB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002030500068 20020305 00068 EA 2002 3 5 COMA0260137 1 20020304 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 965CA 13460 7131 CRACK FOUND ON L/H LOWER WING PLANK AT PANEL 550AB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002030500069 20020305 00069 NE 2002 3 5 NACA20020005 2 20020215 A 8530 356993 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 4 ENGINE CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 2907F 1775 1775 533265 CP450668 FEATHERED NR 4 ENGINE, BACKFIRING, WON'T TAKE A LEAN. REPLACED THE NR 18 CYLINDER. 2 L 7 4 4R 4 R A781 5E8 2002030500070 20020305 00070 NE 2002 3 5 NACA20020007 2 20020216 A 8530 356993 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 3 ENGINE CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 43872 2038 2038 533294 NK510186 FEATHERED NR 3 ENGINE DUE TO RAPID BACKFIRING. REMOVED AND REPLACED NR 4 CYLINDER ON THE NR 3 ENGINE. 2 L 7 4 4R 4 R A781 5E8 2002030500071 20020305 00071 EA 2002 3 5 COMA0260138 1 20020304 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 965CA 13460 7131 CRACK FOUND ON R/H LOWER WING PLANK AT PANEL 650 AB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002030500072 20020305 00072 EA 2002 3 5 COMA0260139 1 20020304 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 965CA 13460 7131 CRACK FOUND ON R/H LOWER WING PLANK AT PANEL 650BB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002030500073 20020305 00073 NE 2002 3 5 NACA20020008 2 20020221 A 7421 RHB32E SPARK PLUG DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 2 ENGINE SHORTED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 AL 03 43872 377 377 533294 P35404 PRECAUTIONARY SHUT DOWN NR 2 ENGINE, DUE TO DOUBLE SHORTED SECONDARY, NR 16 CYLINDER. REPLACED FRONT AND REAR SPARK PLU GS. 2 L 7 4 4R 4 R A781 5E8 2002030500074 20020305 00074 EA 2002 3 5 COMA0260140 1 20020304 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 965CA 13460 7131 CRACK FOUND ON R/H LOWER WING PLANK AT PANEL 650DB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002030500075 20020305 00075 NE 2002 3 5 P2EA2002M008 2 20020217 A 7220 INLET GUIDE VANE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 131NJ 49846 725357 ON INSPECTION OF THE NR 2 ENGINE INLET FOUND THE IGV AT 4 O'CLOCK WITH CRACK. UPON FURTHER INSPECTION FOUND THE NR 2 EN GINE BEARING HUB CRACKED. REPLACED THE NR 2 ENGINE INLET GUIDE VANE ASSY AND REPLACED THE NR 2 ENGINE BEARING HUB IAW 7 2-23-01 AND 72-23-02, OP'S CHECK NORMAL. 2 L 7 2 4F 4 F RT A6WE E9NE 2002030500076 20020305 00076 EA 2002 3 5 COMA0260141 1 20020301 A 2750 860D10018ABC FCU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 431CA 6452 7472 FLIGHT 5583 FLAPS FAIL MESSAGE DURING PUSH-BACK.REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2002030500077 20020305 00077 NM 2002 3 5 P2EA2002M009 1 20020217 A 7830 THRUST REVERSER BOEING 737 7372Q8 138448K NM NR 2 ENGINE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 121NJ 21735 ON WALK-AROUND FOUND THE NR 2 ENGINE THRUST REVERSER WITH CRACK ON THE RIGHT HAND SIDE. REPLACED THE NR 2 ENGINE THRUST REVERSER IAW MM 78-32-10, LEAK CHECK AND OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 2002030500078 20020305 00078 WP 2002 3 5 P2EA2002M010 1 20020224 A 2424 GCU DOUG DC9 DC981 3022081 WP LT ENGINE FAILED A P2EA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 05 814US 48094 LEFT GENERATOR FAILED ON TAKEOFF. LEFT GENERATOR FEEDER FAULT, LEFT AC BUS OFF, LEFT GENERATOR OFF. AC CROSSTIE LOCKOU T LIGHTS, LEFT SIDE LOCKED OUT (TRIM INOP ETC). LEFT GENERATOR WOULD NOT RESET ON FIRST TRY. DID RESET ON SECOND TRY. AC CROSSTIE LOCKOUT LIGHT REMAINED ON. REPLACED THE LEFT GCU PER MM 24-20-10, OP'S CHECKED GOOD. 2 L 7 2 4F A6WE 2002030500079 20020305 00079 EA 2002 3 5 COMA0260142 1 20020302 A 5300 VIBRATOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 01 443CA 7539 FLIGHT 5980 VERY LOUD NOISE AND VIBRATION FROM FORWARD HALF OF AIRCRAFT.COULD NOT DUPLICATE. INSPECTION OF AIRCRAFT FOU ND NO DEFECTS. 2 L 7 2 4F RT A21EA 2002030500080 20020305 00080 EA 2002 3 5 COMA0260143 1 20020302 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 713CA 11 7245 FLIGHT 5079 FLAPS FAIL MESSAGE AFTER T/O.REPLACED THE L/H BPSU. 2 L 7 2 4F RT A21EA 2002030500081 20020305 00081 EA 2002 3 5 COMA0260144 1 20020303 A 5210 1039669 LATCH CNDAIR CL600 CL6002B19 1900309 EA DOOR HANDLE BROKEN A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 779CA 7306 FLIGHT 5516 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.REPLACED THE OUTER HANDLE TRIGGER LATCH. 2 L 7 2 4F RT A21EA 2002030500082 20020305 00082 EA 2002 3 5 COMA0260145 1 20020303 A 2760 SPOILER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 937CA 7044 FLIGHT 5884 TAKE OFF CONFIG SPOILER WARNING.DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2002030500083 20020305 00083 NM 2002 3 5 QXEA0200095 1 20020204 A 7110 SKIN DHAV DHC8 DHC8202 2809007 NM NR 1 COWLING DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 PDX - DENT FOUND BETWEEN NR 1 LOWER COWL AND OIL COOLER. REPAIRED IAW RD 8-54-063. 2 H 7 2 4T RT A13NM 2002030500084 20020305 00084 NM 2002 3 5 QXEA0200096 1 20020119 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - CARGO DOOR SURROUND STRUCTURE UPPER FORWARD STOP IS GOUGED IN THREE PLACES. REPAIRED IAW DHC-8-200 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002030500085 20020305 00085 NM 2002 3 5 QXEA0200097 1 20020118 A 5320 STIFFENER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - CARGO DOOR SILL ANGLED PLATE SUPPORT STIFFENER AT AFT END IS CORRODED ON UNDER SIDE. REPAIRED IAW DHC-8 SRM 51-20 -16, SECTION C, 1-9. 2 H 7 2 4T RT A13NM 2002030500086 20020305 00086 NM 2002 3 5 QXEA0200098 1 20020118 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - CARGO DOOR LOWER SILL ANGLED PLATE CORRODED IN NUMEROUS PLACES BETWEEN STATION X580 AND X600. REPAIRED IAW DHC-8 SRM 51-20-16, SECTION C, 1-8 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002030500087 20020305 00087 NM 2002 3 5 QXEA0200099 1 20020118 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - CARGO DOOR LOWER SILL ANGLE PLATE HAS THREE SPOTS OF CORROSION AT STATION X568. REPAIRED IAW DHC-8 SRM 51-20-16, SECTION C, 1-9, SRM 51-20-36 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2002030500088 20020305 00088 NM 2002 3 5 QXEA0200100 1 20020118 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - CARGO DOOR SILL CORRODED AT STATION X558. REPAIRED IAW DHC-8 SRM 51-20-16, SECTION C, 1-9, SRM 51-20-36 AND SRM 5 1-20-51. 2 H 7 2 4T RT A13NM 2002030500089 20020305 00089 NM 2002 3 5 QXEA0200101 1 20020118 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM ICE SHIELD BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - BROKEN NUT PLATE FOR ICE SHIELD ON LT SIDE OF AIRCRAFT AT STATION X274.000 AND Z144.0. REPAIRED IAW DHC-8 SRM 51- 40-11. 2 H 7 2 4T RT A13NM 2002030500090 20020305 00090 NM 2002 3 5 QXEA0200102 1 20020117 A 5710 BEARING DHAV DHC8 DHC8202 2809007 NM AILERON ROUGH A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT AILERON OUTBOARD HINGE BEARING IS ROUGH. REPLACED BEARING IAW DHC-8 MM PSM 1-82-2, 20-21-52, TASK 20-21-52-390 -801. 2 H 7 2 4T RT A13NM 2002030500091 20020305 00091 NM 2002 3 5 QXEA0200103 1 20020117 A 5410 ANGLE DHAV DHC8 DHC8202 2809007 NM LT ENGINE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT EXHAUST FINGERNAIL HAS A CRACK ON THE INBOARD BARREL TO SIDE SKIN CLOSING ANGLE. REPAIRED IAW DHC-8 RD 8-54-24 0 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002030500092 20020305 00092 NM 2002 3 5 QXEA0200104 1 20020116 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - BRACKET CRACKED OUTBOARD TOP END OF INBOARD LEADING EDGE FLANGE AT STATION YW138.00. REPAIRED IAW DHC-8-200 SRM 5 1-40-00. 2 H 7 2 4T RT A13NM 2002030500093 20020305 00093 NM 2002 3 5 QXEA0200105 1 20020116 A 5720 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT WING FORWARD SPAR UPPER LEADING EDGE SUPPORT BRACKET IS CRACKED AT STATION YW139.00. REPAIRED IAW DHC-8-200 SR M 51-40-00. 2 H 7 2 4T RT A13NM 2002030500094 20020305 00094 NM 2002 3 5 QXEA0200106 1 20020117 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - BRACKET CHAFED OUTBOARD BOTTOM END OF INBOARD LEADING EDGE FLANGE AT STATION YW138.00. REPAIRED IAW DHC-8 SRM 51- 20-11 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002030500095 20020305 00095 NM 2002 3 5 QXEA0200107 1 20020117 A 3211 FITTING DHAV DHC8 DHC8202 2809007 NM LT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - NR 1 MLG H-MEMBER AT MLG ACTUATOR FITTING MOUNT HAS SLIGHT SURFACE FRETTING CORROSION BY MOUNT HOLES. REPAIRED IA W RD 8-54-1178. 2 H 7 2 4T RT A13NM 2002030500096 20020305 00096 NM 2002 3 5 CALA0200115 1 20020302 A 5754 SKIN BOEING 737 7373T0 1384582 NM #4 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A 4" CRACK IN #4 L/E SLAT PANEL AT O/B ACTUATOR. REPAIRED IAW SRM 57-43-01. 2 L 7 2 4F RT A16WE 2002030500097 20020305 00097 NM 2002 3 5 CALA0200117 1 20020302 A 5320 WEB BOEING 737 7373T0 1384582 NM C-1 DR JAMB WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND C-1 AFT DOOR JAMB LOWER WEB WORN AROUND EDGES. A NEW WEB WAS INSTALLED IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 2002030500098 20020305 00098 NM 2002 3 5 CALA0200118 1 20020304 A 5512 SKIN BOEING 737 7373T0 1384582 NM RH HOR STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A 3" CRACK IN R/H HORIZONTAL STABILIZER LOWER SKIN AT REAR SPAR JUST I/B OF #4 ELEVATOR HINGE. A PERMAN ENT REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01584. 2 L 7 2 4F RT A16WE 2002030500099 20020305 00099 NM 2002 3 5 CALA0200119 1 20020304 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-2 DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND C-2 DOOR SKIN DENTED, CENTERLINE 8 INCHES AFT OF LEADING EDGE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 5 2-00-01, FIGURE 203. 2 L 7 2 4F RT A16WE 2002030500100 20020305 00100 NM 2002 3 5 CALA0200121 1 20020301 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 340 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND FLOORBEAM CORRODED AT STA 340, RBL 12 TO LBL 12. THE CORRODED AREA OF FLOORBEAM WAS REMOVED AND A NEW S ECTION WAS INSTALLED IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 2002030500101 20020305 00101 NM 2002 3 5 QXEA0200108 1 20020117 A 5410 BARREL DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT FINGERNAIL HAS A TWO PRONG CRACK IN BARREL. REPAIRED IAW DHC-8 RD 8-54-240 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002030500102 20020305 00102 NM 2002 3 5 QXEA0200111 1 20020121 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT SIDE FUSELAGE SKIN HAS DENT AT STATION X511.000 AND Z103.00. REPAIRED IAW HORIZON AIR EA 2-53-364. 2 H 7 2 4T RT A13NM 2002030500103 20020305 00103 NM 2002 3 5 QXEA0200112 1 20020121 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - CORROSION ON BOTTOM SIDE OF PASSENGER DOOR THRESHOLD AROUND NUT PLATES. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002030500104 20020305 00104 NM 2002 3 5 QXEA0200113 1 20020121 A 5210 SKIN DHAV DHC8 DHC8202 2809007 NM PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - DENT IN MAIN CABIN DOOR OUT SHELL. REPAIRED IAW HORIZON AIR EA 2-52-119. 2 H 7 2 4T RT A13NM 2002030500105 20020305 00105 NM 2002 3 5 QXEA0200115 1 20020129 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - GOUGE IN RT BELLY SKIN AT STATION X213, JUST ABOVE TOP SEAM. REPAIRED IAW DHC-8 MM 20-34-11 AND HORIZON AIR EA 2- 53-368. 2 H 7 2 4T RT A13NM 2002030500106 20020305 00106 NM 2002 3 5 QXEA0200116 1 20020129 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - ATC ANTENNA AT STATION X252.700 WHERE ANTENNA MOUNTS TO FUSELAGE HAS CORROSION. REPAIRED IAW DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002030500107 20020305 00107 NM 2002 3 5 QXEA0200117 1 20020129 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT SIDE FUSELAGE EXTERIOR SKIN HAS 1.2 INCH LONG SCRAPE MARK AT STATION X480.500 AND Z119.00. REPAIRED IAW DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002030500108 20020305 00108 NM 2002 3 5 QXEA0200118 1 20020129 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - GOUGE IN RT BELLY SKIN AT STATION X202.17, JUST ABOVE LAP SEAM. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, PARAGRAP H 2.B AND HORIZON AIR EA 2-53-368. 2 H 7 2 4T RT A13NM 2002030500109 20020305 00109 NM 2002 3 5 QXEA0200119 1 20020129 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - .25 INCH GOUGE MARK ON LT SIDE OF EXTERIOR FUSELAGE SKIN 1.2 INCH BELOW STRINGER 23L AND STATION X265.000. REPAIR ED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2002030500110 20020305 00110 EU 2002 3 5 AWXA200200187 1 20020215 A 2742 D5598120100 FITTING AIRBUS 320 A320231 3930325 EU STA 35306 FR 74 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 55 YWG - MAJOR REPAIR - "C" - DURING C-02 INSPECTION CENTER JOINT FITTINGS FOR THE TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WERE FOUND WORN BEYOND DRAWING LIMITATIONS. L/H DIMENSIONS RANGE FROM 2.4746' TO 2.4751", R/H SIDE DIMENSIONS RANGE FRO M 2.6007" TO 2.6009". MAINTENANCE REMOVED AND REWORKED CENTER JOINT FITTING FIXED BEARING AND SLIDING BEARING PER AWA ER 26-5511-02060-ES2. 2 L 7 2 4F RT A28NM 2002030500111 20020305 00111 NM 2002 3 5 QXEA0200120 1 20020124 A 5720 FLANGE DHAV DHC8 DHC8202 2809007 NM WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - INBOARD BOTTOM LEADING EDGE FLANGE CHAFED AT YW57.00. REPAIRED IAW RD 8-57-811, DHC-8 SRM 51-20-16, PAGE 3 AND SR M 51-20-26. 2 H 7 2 4T RT A13NM 2002030500112 20020305 00112 NM 2002 3 5 QXEA0200121 1 20020125 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT INBOARD SEAT TRACK NR 8 HAS LIGHT CORROSION ON TOP OF RAILS BETWEEN STATION X498 AND X505. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-56. 2 H 7 2 4T RT A13NM 2002030500113 20020305 00113 NM 2002 3 5 QXEA0200122 1 20020129 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT EMERGENCY EXIT, ALL EIGHT DOOR STOPS HAVE .25 INCH GROOVE CHAFED ACROSS CENTER OF BEARING SURFACE. REPAIRED IA W RD8-53-126 AND DHC-8 SRM 51-20-16, PARAGRAPH D. 2 H 7 2 4T RT A13NM 2002030500114 20020305 00114 NM 2002 3 5 QXEA0200123 1 20020127 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT OUTBOARD SEAT TRACK HAS SCRATCHES AND LIGHT PITTING CORROSION INSIDE CHANNEL AT STATION X545.000. REPAIRED IAW RD 8-53-3644, STEP 4, PAGE 3. 2 H 7 2 4T RT A13NM 2002030500115 20020305 00115 NM 2002 3 5 QXEA0200124 1 20020127 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT OUTBOARD SEAT TRACK HAS TOP SURFACE CORROSION AT STATION X516.000. REPAIRED IAW RD 8-53-3644, STEP 4, PAGE 3. 2 H 7 2 4T RT A13NM 2002030500116 20020305 00116 NM 2002 3 5 QXEA0200125 1 20020127 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT OUTBOARD SEAT TRACK HAS PITTING CORROSION INSIDE CHANNEL AT STATION X456.500. REPAIRED IAW RD 8-53-1342, DHC-8 SRM 51-40-11 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002030500117 20020305 00117 NM 2002 3 5 QXEA0200126 1 20020125 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT INBOARD SEAT TRACK HAS PITTING CORROSION INSIDE CHANNEL AT STATION X377.000. REPAIRED IAW RD 8-53-1102, DHC-8 SRM 51-40-00, PAGE 4, TABLE A AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002030500118 20020305 00118 NM 2002 3 5 QXEA0200127 1 20020127 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT OUTBOARD SEAT TRACK HAS PITTING CORROSION INSIDE CHANNEL AT STATION X405.737. REPAIRED IAW RD 8-53-1352 AND DH C-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002030500119 20020305 00119 NM 2002 3 5 QXEA0200128 1 20020120 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - THERE IS CHAFING DAMAGE TO TOP EDGE OF BAGGAGE DOOR EXTERNAL SKIN. REPAIRED IAW DHC-8 SRM 51-40-11, SRM 51-20-26 AND RD 8-52-029. 2 H 7 2 4T RT A13NM 2002030500120 20020305 00120 NM 2002 3 5 QXEA0200129 1 20020122 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - TWO DENTS IN RT FORWARD FUSELAGE SKIN ABOVE PANEL 122AR, BETWEEN X123- X136 AT STRINGER 21. REPAIRED IAW HORIZON AIR EA 2-53-362. 2 H 7 2 4T RT A13NM 2002030500121 20020305 00121 NM 2002 3 5 QXEA0200130 1 20020121 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - DENT IN RT FUSELAGE SKIN BELOW ICE SHIELD, BETWEEN STATION X333 AND X312. REPAIRED IAW HORIZON AIR EA 2-53-363. 2 H 7 2 4T RT A13NM 2002031100171 20020311 00171 NM 2002 3 11 F3LA200200098 1 20020228 A 5320 CLIP BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLIP AT FWD FRAME, STA 360. FABRICATED AND INSTALLED CHANNEL TIE PER SRM 51-20-01 AND 51-30-2. 2 L 7 2 4U RT A16WE 2002030500122 20020305 00122 NM 2002 3 5 QXEA0200131 1 20020125 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - DENT IN LT REAR FUSELAGE SKIN, FORWARD OF FRAME NR 5 AT APPROXIMATELY Z129. REPAIRED IAW DHC-8-200 SRM 51-20-26, SRM 53-30-24 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002030500123 20020305 00123 NM 2002 3 5 QXEA0200132 1 20020125 A 5320 CLIP DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - FRAME CLIP AT X312.350, TYING SEAT TRACK TO FRAME DAMAGED AT INBOARD RIVET. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002030500124 20020305 00124 NM 2002 3 5 QXEA0200133 1 20020125 A 5320 CLIP DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - FRAME CLIP AT X291.400, TYING SEAT TRACK TO FRAME DAMAGED AT INBOARD RIVET. REPAIRED IAW DHC-8 SRM 51-40-11, PAGE 3. 2 H 7 2 4T RT A13NM 2002030500125 20020305 00125 NM 2002 3 5 QXEA0200134 1 20020123 A 3213 STRUT DHAV DHC8 DHC8202 2809007 NM RT MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT MAIN LANDING GEAR SHOCK STRUT HAS CHAFE MARK ON INBOARD RADIUS OF OUTBOARD LUG TOP END WHERE THE DRAG STRUT ATT ACHES. REPAIRED IAW CMM 32-10-01. 2 H 7 2 4T RT A13NM 2002030500126 20020305 00126 NM 2002 3 5 QXEA0200135 1 20020123 A 5312 BULKHEAD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - CHAFE DAMAGE ON FORWARD PRESSURE BULKHEAD AT STATION 110.300 AND Z84 IN TWO SPOTS. REPAIRED IAW DHC-8 SRM 51-20-1 1 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2002030500127 20020305 00127 NM 2002 3 5 QXEA0200136 1 20020122 A 5411 FRAME DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT NACELLE FRAME AT STATION 177.00 INBOARD SIDE OF NACELLE IS CHAFED ON FORWARD SIDE. REPAIRED IAW DHC-8 RD 8-54- 078. 2 H 7 2 4T RT A13NM 2002030500128 20020305 00128 NM 2002 3 5 QXEA0200137 1 20020122 A 2760 CONTROL CABLE DHAV DHC8 DHC8202 2809007 NM RT SPOILER WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT WING UPPER SPOILER CABLE WIRES WORN AT YW58.20. REPAIRED IAW DHC-8 MM 27-14-00, PAGE 505. 2 H 7 2 4T RT A13NM 2002030500129 20020305 00129 NM 2002 3 5 QXEA0200139 1 20020123 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT FUSELAGE EXTERIOR SKIN HAS A DENT AT STATION X291.400 AND Z153.00. REPAIRED IAW HORIZON AIR EA 2-53-365. 2 H 7 2 4T RT A13NM 2002030500130 20020305 00130 NM 2002 3 5 QXEA0200140 1 20020125 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT INBOARD SEAT TRACK HAS CORROSION INSIDE CHANNEL ALONG INBOARD EDGE AT STATION X485. REPAIRED IAW DHC-8 SRM 51- 20-16, RD 8-53-1399 AND SRM 51-20-56. 2 H 7 2 4T RT A13NM 2002030500131 20020305 00131 NM 2002 3 5 QXEA0200141 1 20020125 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT INBOARD NR 8 SEAT TRACK HAS CORROSION IN CHANNEL OUTBOARD CORNER AT STATION X471. REPAIRED IAW DHC-8 RD 8-53-1 339, SRM 51-20-16 AND SRM 51-20-56. 2 H 7 2 4T RT A13NM 2002030500132 20020305 00132 NM 2002 3 5 AWXA200200191 1 20020301 A 3350 BMS13311122 WIRE BOEING 737 737277 1384570 NM SEAT ROW 8,13 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22656 PHX - EEL - "C" - DURING INSPECTION OF THE EMERGENCY ESCAPE LIGHTING SYSTEM SEVERAL SEAT ROW LIGHTS WERE FOUND INOPERATI VE. MAINTENANCE SPLICED BROKEN WIRES AT SEAT ROWS 8 AND 13 AND RESECURED A PLUG AT SEAT ROW 1, OPERATIONAL CHECK OF EMER GENCY ESCAPE PATH LIGHTING CHECKED GOOD. 2 L 7 2 4F RT A16WE 2002030600001 20020306 00001 WP 2002 3 6 MWEA020130 1 20020216 A 3070 7274555 CIRCUIT BREAKER DOUG DC9 DC981 3022081 WP COCKPIT FAULTY A MWEA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 31 812ME 48006 SHORTLY AFTER TAKEOFF, NR 2 PFD AND NR 2 ND FAILED FOLLOWED BY SYMBOL GENERATOR NR 2 CB OPENING. FOUND PROBLEM CAUSED B Y INOP FORWARD DRAIN MAST HEATER. DRIED MOISTURE AND REPLACED SYMBOL GENERATOR. REPLACED FORWARD GALLEY MAST CIRCUIT B REAKER B1-509. 2 L 7 2 4F A6WE 2002031300109 20020313 00109 NM 2002 3 13 P2EA2002M011 1 20020301 A 5310 STRUCTURE BOEING 737 737230 1384401 NM FUSELAGE VIBRATION A P2EA K NONE E VIBRATION/BUFFET CR CRUISE 1 CE 05 122NJ 22120 DURING FLIGHT A FLIGHT ATTENDANT REPORTED VIBRATION AT THE AFT GALLEY FLOOR. VIBRATION STOPPED AND THEN STARTED AGAIN D URING FLIGHT. ALL SYSTEMS INDICATED NORMAL AND AIRCRAFT CONTINUED TO SCHEDULED DESTINATION AND LANDED WITH NO INCIDENT. AIRCRAFT WAS INSPECTED IAW SERVICE LETTER 737-5L-02-002-D. THE AFT LAV SERVICE DOOR WAS FOUND FAIRED INCORRECTLY. DOO R WAS SPEED TAPED AND AN EVALUATION FLIGHT WAS PERFORMED WITH NO DEFECTS NOTED THROUGHOUT FLIGHT. DOOR WAS REMOVED TO F OM AND PLACED ON CDL 52-40-03 CI C122906. VIBRATION OCCURRED AGAIN WITH DOOR REMOVED. INSTALLED DOOR IAW MM 38-30-0. 2 L 7 2 4F RT A16WE 2002030600002 20020306 00002 NM 2002 3 6 P5CA0200648 1 20020213 A 5246 65B1008295 SERVICE DOOR BOEING 747 74746NF 13848BT NM LT WING BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 451PA 30809 AT SCL ARRIVAL FOUND LT WING LT FUELING PANEL DOOR BROKEN. TRANSFERRED TO CDL 28876 AS PER CDL 57-31-1. CAUSE IS UNDER INVESTIGATION. REMOVED DOOR AND COVERED WITH HIGH SPEED TAPE. 2 L 7 4 4F RT A20WE 2002030600003 20020306 00003 NM 2002 3 6 P5CA0200649 1 20020220 A 1430 BACB30LJ10429 BOLT BOEING 747 747249F 1384849 NM LT MLG DOOR WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 WORN LT WING BODY GEAR, AREA 751; SUPPORT ROD BOLT WORN. REMOVED BOLTS/BUSHINGS AND CLEANED UP. REASSEMBLED IAW MM 32- 13-00 WITH LUBRICATION AND NEW WASHERS INSTALLED TO CORRECT ITEM. FOUND DOOR TO ROD BEARINGS AND BOLTS NOW WITHIN LIMIT S. OK FOR SERVICE. 2 L 7 4 4F A20WE 2002030600004 20020306 00004 NM 2002 3 6 P5CA0200650 1 20020220 A 5753 FLAP TRACK BOEING 747 747249F 1384849 NM T/E FLAP CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 LEVEL 1 CORROSION: FOUND LIGHT CORROSION, AREA 500, ON UPPER FLAP TRACKS AND CENTER TOGGLE ROLLERS ON NR 1, 2, 3 & 4 FL AP TRACKS. REMOVED CORROSION AND RETREATED IAW MM 27-51-22 & 27-51-23, PAGE 801. 2 L 7 4 4F A20WE 2002030600005 20020306 00005 NM 2002 3 6 P5CA0200651 1 20020220 A 5753 FLAP TRACK BOEING 747 747249F 1384849 NM T/E FLAP CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 FOUND LIGHT CORROSION, AREA 600, ON UPPER FLAP TRACKS AND CENTER TOGGLE ROLLERS ON NR 5, 6, 7 & 8 FLAP TRACKS. REMOVED CORROSION AND RETREATED IAW MM 27-51-22 & 27-51-23, PAGE 801. 2 L 7 4 4F A20WE 2002030600006 20020306 00006 NM 2002 3 6 ANCF200200004 1 20020222 A 2910 7936913691 LINE DOUG MD80 MD83 3023681 NM HYD SYSTEM BROKEN W ANCF O OTHER K FLUID LOSS DE DESCENT 1 SW 99 583AN 53183 DURING CLIMB TO BOGOTA, THE CREW NOTICED THAT THE RT HYDRAULIC QUANTITY DROPPED TO 4 QTS, WITH PUMP IN LOW AND OFF OPERA TION. THE SYSTEM WAS DEPRESSURIZED AND THE QUANTITY AUGMENTED TO 7 QTS. DURING CRUISE RH HYDRAULIC QUANTITY MAINTAINED I N 7 QTS, HOWEVER DURING DESCENT TO BOGOTA THE RH HYDRAULIC QUANTITY DROPPED TO 1 QTS, WITH AMBER LIGHT ON. PROCEDURE WAS ACCOMPLISHED. RT BRAKE TRANSMITTER PRESSURE LINE ASSEMBLY WERE REPLACED IAW AMM. 20-10-13 PAGE 201. OPERATIONAL TEST E XTENSION AND RETRACTION WAS PERFORMED SUCCESSFULLY IAW AMM. 32-30-00 PAGE 201. 2 L 7 2 4F RT 2002030600008 20020306 00008 NE 2002 3 6 AUS20020038 2 20020117 A 7200 1216669 BEARING AIRBUS 320 A320* EU CFMINT CFM56 CFM565A1 NE BALLSCREW ACT DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S 22010 (AUS) MASTER BALLSCREW ACTUATOR OUTPUT DRIVE LOWER BEARING BALLS MISSING AND BEARING COCKED ECCENTRICALLY. LIMITED INFOR MATION PROVIDED. 2 L 7 2 4F 4 F RT A46NM E29NE 2002030600009 20020306 00009 NM 2002 3 6 AUS20020039 1 20020121 A 2710 31701204 PCU BOEING 747 747338 NM RROYCE RB211 RB211524G19 NE AILERON CONTROL FAULTY W O OTHER F FLT CONT AFFECTED CL CLIMB 1 AU S 42575 (AUS) RT INBOARD AILERON POWER CONTROL UNIT (PCU) FAULTY. 2 L 7 2 4F 4 F RT A20WE E30NE 2002030600010 20020306 00010 NM 2002 3 6 P5CA0200653 1 20020226 A 5730 65B1162611 PANEL BOEING 747 7472U3B 1384846 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 CRACK LT WING REAR SPAR TO INBOARD AILERON TRAILING EDGE UPPER PANEL (573ST). PANEL ASSY REPLACED REF SRM 51-10-01. 2 L 7 4 4F RT A20WE 2002030600011 20020306 00011 NM 2002 3 6 AUS20020040 1 20020118 A 2720 4084042910 BOLT BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU PRESSURE VALVE MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RUDDER PRESSURE REDUCER VALVE PIVOT BOLT MISSING. 2 L 7 2 4F 4 F RT A16WE E21EU 2002030600012 20020306 00012 NM 2002 3 6 P5CA0200654 1 20020225 A 5730 PANEL BOEING 747 7472U3B 1384846 NM LT WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 DAMAGE LT WING UPPER PANEL STATION WS 440.62, ABOVE KRUEGER FLAPS 11/13. NO CRACK FOUND. REPAIR CARRIED OUT WITH REF T O SRM 51-40-09 & 51-40-15. 2 L 7 4 4F RT A20WE 2002030600013 20020306 00013 EU 2002 3 6 AUS20020042 1 20020118 A 2697 26210075 WIRE AIRBUS 320 A320* EU CFMINT CFM56 CFM565A1 NE FIRE WARNING WORN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 2 ENGINE FIRE WIRES CHAFED. WIRES PROVIDED AND INTERMITTENT GROUND TO WIRE. SUSPECT CAUSED BY EXCESSIVE LENGT H OF WIRE WHICH WAS INADEQUATELY SECURED ALLOWING WIRES TO CHAFE. 2 L 7 2 4F 4 F RT A46NM E29NE 2002031100173 20020311 00173 NM 2002 3 11 F3LA200200100 1 20020228 A 5320 ATTACH ANGLE BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SIDEWALL ATTACH ANGLE AT STA 947.5, STR 21R TO 24R. FABRICATED AND I NSTALLED REPLACEMENT ANGLE PER BOEING DRAWING 65-55726 AND SRM 51-40-3. 2 L 7 2 4U RT A16WE 2002031100174 20020311 00174 NM 2002 3 11 F3LA200200101 1 20020228 A 5320 ATTACH ANGLE BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SIDEWALL PANEL ATTACH ANGLE AT STA 727, LBL 21 TO LBL 25. 2 L 7 2 4U RT A16WE 2002030600014 20020306 00014 NM 2002 3 6 P5CA0200655 1 20020226 A 2700 DN8144DL PLUG BOEING 747 7472U3B 1384846 NM PDU MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 PDU NR 4 DRAIN PLUG MISSING. INSTALLED PLUG AND FILLED PDU IAW 12-13-12. PDU RAN OK. 2 L 7 4 4F RT A20WE 2002030600015 20020306 00015 CE 2002 3 6 AUS20020043 1 20020122 A 2750 MS276404 BEARING CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP HARTZL HCB3T HCB3TN5 GL TE FLAP FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT OUTBOARD FLAP INBOARD BELLCRANK BEARING HAD EXCESSIVE PLAY. SUSPECT CAUSED BY WATER INGRESS. 1 L 7 2 3T 4 T RT A28CE E4WE 6 C P15EA 2002030600016 20020306 00016 EU 2002 3 6 AUS20020045 1 20020119 A 2750 COMPUTER BAC 146 146200A 1500266 EU LYC ALF502 ALF502R3A 41580 NE TE FLAP SYSTEM FAULTY W O OTHER F FLT CONT AFFECTED LD LANDING 1 AU S (AUS) FLAP SYSTEM INOPERATIVE. NO CAUSE COULD BE FOUND AND INVESTIGATION IS CONTINUING. FLAP COMPUTER PNO 676801007 CHAN GED. 2 H 7 4 4F 4 F A49EU E6NE 2002030600017 20020306 00017 NM 2002 3 6 PCAA0202029 1 20020214 A 1430 85510031 FASTENER DHAV DHC8 DHC8102 2809003 NM RT GUST LOCK LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 836EX 297 DURING A CHECK INSPECTION RIGHT GUST LOCK PLATE FASTENERS ON ELEVATOR FOUND LOOSE. FASTENERS WERE REPLACED IN ACCORDANC E WITH DER CAS-AAL50. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031100175 20020311 00175 NM 2002 3 11 F3LA200200102 1 20020228 A 5320 WEB BOEING 737 7372Y5 1384554 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY FLOOR WEB CORRODED, STA 1016, AT DRAIN TO LBL 30. 2 L 7 2 4U RT A16WE 2002030600018 20020306 00018 NM 2002 3 6 PCAA0202031 1 20020301 A 2910 82970009325 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS CRACKED A PCAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 13 838EX 220 BWI- FLIGHT 3923. CREW REPORTED THAT NR 1 HYDRAULIC QUANTITY WAS READING ZERO AFTER TAKEOFF. AN EMERGENCY WAS DECLARED, AND PLANE LANDED SAFELY IN BWI WITH A LOSS OF BRAKES AND FLAPS. MAINTENANCE FOUND A CRACK IN A FLARE OF HYDRAULIC PRES SURE LINE AT NR 1 HYDRAULIC MANIFOLD. INTERIM FLEX LINE INSTALLED. ENGINE DRIVEN HYDRAULIC PUMP, AND CASE DRAIN FILTER AND HOUSING WERE REPLACED. HYDRAULIC SYSTEM BLED, AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002030600019 20020306 00019 SW 2002 3 6 PNSA020201 1 20020219 A 5220 DOUBLER SWRNGN SA227 SA227AC 8780603 SW EMERGENCY EXIT CORRODED A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 2719H AC713B FUSELAGE EMERGENCY EXIT STEEL DOUBLERS FOUND CORRODED DURING INSPECTION. X-RAY INSPECTION PERFORMED TO DETERMINE EXTENT OF DAMAGE AND AFT RT EXIT DOUBLER REQUIRED REPLACEMENT. OTHER TWO DOUBLERS STILL WITHIN SRM DAMAGE LIMITS. 2 L 7 2 4T RT A8SW 2002030600020 20020306 00020 SW 2002 3 6 PNSA020202 1 20020219 A 5220 DOUBLER SWRNGN SA227 SA227AC 8780603 SW EMERGENCY EXIT CORRODED A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 2708D AC709B DURING INSPECTION FOUND ALL THREE EMERGENCY EXIT WINDOW STEEL DOUBLERS CORRODED. X-RAY INSPECTION PERFORMED FOR DEPTH D ETERMINATION AND FOUND ALL THREE OUT OF SRM LIMITS. REPLACED ALL THREE DOUBLERS. 2 L 7 2 4T RT A8SW 2002030600021 20020306 00021 NM 2002 3 6 QXEA0200142 1 20020125 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT INBOARD NR 8 SEAT TRACK HAS CORROSION BELOW OUTBOARD LUG IN CHANNEL AT STATION X440. REPAIRED IAW DHC-8 RD 8-5 3-1339, SRM 51-20-16 AND SRM 51-20-56. 2 H 7 2 4T RT A13NM 2002030600022 20020306 00022 NM 2002 3 6 QXEA0200143 1 20020125 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT INBOARD NR 7 SEAT TRACK HAS PITTING CORROSION IN BOTTOM OF CHANNEL AND ON TOP RAILS BETWEEN STATION X281 AND X2 84. REPAIRED IAW DHC-8 RD 8-53-1339, RD 8-53-2295 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002030600023 20020306 00023 NM 2002 3 6 QXEA0200144 1 20020124 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT OUTBOARD NR 12 SEAT TRACK HAS WEAR MARK IN CENTER OF BOTTOM CHANNEL AT STATION X542. REPAIRED IAW DHC-8 RD 8-5 3-3644 AND SRM 51-20-56. 2 H 7 2 4T RT A13NM 2002030600024 20020306 00024 NM 2002 3 6 QXEA0200145 1 20020124 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT OUTBOARD NR 2 SEAT TRACK HAS SCRATCHES ON TOP RAILS BETWEEN STATION X526 AND X532. REPAIRED IAW DHC-8 RD 8-53- 3644 AND SRM 51-20-56. 2 H 7 2 4T RT A13NM 2002030600025 20020306 00025 NM 2002 3 6 QXEA0200146 1 20020124 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT OUTBOARD NR 12 SEAT TRACK HAS PITTING CORROSION IN BOTTOM OF CHANNEL AT STATION X518. REPAIRED IAW DHC-8 RD 8- 53-1644 AND SRM 51-20-56. 2 H 7 2 4T RT A13NM 2002030600026 20020306 00026 NM 2002 3 6 QXEA0200147 1 20020124 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT OUTBOARD NR 12 SEAT TRACK HAS LIGHT PITTING CORROSION IN BOTTOM OF CHANNEL FROM FORWARD END OF TRACK SECTION TO STATION X514. REPAIRED IAW DHC-8 RD 8-53-3644 AND SRM 51-20-56. 2 H 7 2 4T RT A13NM 2002030600027 20020306 00027 NM 2002 3 6 QXEA0200148 1 20020124 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT OUTBOARD NR 11 SEAT TRACK HAS PITTING CORROSION IN BOTTOM OF CHANNEL AND ON RAILS BETWEEN STATION X434 AND X439 . REPAIRED IAW DHC-8 RD 8-53-1342 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002030600028 20020306 00028 NM 2002 3 6 QXEA0200149 1 20020124 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RT OUTBOARD NR 10 SEAT TRACK HAS DEEP PITTING CORROSION IN BOTTOM OF CHANNEL AND LIGHT CORROSION ON TOP OF RAILS B ETWEEN STATION X373 AND X377. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002030600029 20020306 00029 NM 2002 3 6 QXEA0200150 1 20020123 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT INBOARD SEAT TRACK HAS PITTING CORROSION INSIDE CHANNEL AT STATION X597.000. REPAIRED IAW DHC-8 51-40-11 AND S RM 51-40-00. 2 H 7 2 4T RT A13NM 2002030600030 20020306 00030 NM 2002 3 6 QXEA0200151 1 20020123 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LT INBOARD SEAT TRACK HAS PITTING CORROSION INSIDE CHANNEL AT STATION X499.000. REPAIRED IAW DHC-8 SRM 51-31-01, SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002030600034 20020306 00034 EA 2002 3 6 QXEA0200154 1 20020208 A 5220 DOOR CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT LACK OF LUBE A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 609QX 10031 BOI - GALLEY/EMERGENCY DOOR DIFFICULT TO OPEN AND CLOSE. FLIGHT ATTENDANT NOT ABLE TO MOVE IT. MAINTENANCE CLEANED AND LUBED. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002030600035 20020306 00035 EU 2002 3 6 AUS20020053 2 20020124 A 7261 FILTER BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C 13802 EU ENGINE OIL BYPASSING W E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 AU S (AUS) RT ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2002030600037 20020306 00037 EU 2002 3 6 QXEA0200158 1 20020213 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - PANEL 72A APERTURE HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW F-28 SRM 51-10-04, PARAGRAPH 4, 57-12- 01, PAGE 9 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002030600038 20020306 00038 EU 2002 3 6 QXEA0200159 1 20020210 A 5713 STRINGER FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT WING STRINGER 2.222 IS CORRODED AT STATION 2350. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 4-5 AND SRM 51-10-04, PAGE 9. 2 L 7 2 4F RT A20EU 2002030600039 20020306 00039 NE 2002 3 6 AUS20020055 2 20020130 A 7200 ENGINE BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE NR 1 MAKING METAL W E A ENGINE SHUTDOWN UNSCHED LANDING R K J PARTIAL RPM/PWR LOSS FLUID LOSS WARNING INDICATION CR CRUISE 1 AU S (AUS) NR 1 ENGINE LOST POWER. OIL PRESSURE AND QUANTITY ALSO FELL. INVESTIGATION FOUND METAL IN THE SCAVENGE FILTER ON T HE GEARBOX AND MASTER CHIP DETECTORS. 2 L 7 4 4F 4 F RT A20WE E30NE 2002030600040 20020306 00040 EU 2002 3 6 QXEA0200160 1 20020209 A 5744 ATTACH FITTING FOKKER F28 F28MK4000 4990810 EU LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT WING STATION 8200 FLAP BEAM ATTACH FITTING ON REAR SPAR HAS TWO CHAFE MARKS ON BOTH LUGS OF FITTING. REPAIRED IAW HORIZON AIR EA 4-57-577 AND FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 2002030600041 20020306 00041 EU 2002 3 6 QXEA0200161 1 20020216 A 5320 DOUBLER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACKED REPAIR AT STATION 13815B AND STRINGER 2. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, SRM 51-31-01 AND SRM 5 1-11-04. 2 L 7 2 4F RT A20EU 2002030600042 20020306 00042 EU 2002 3 6 AUS20020057 1 20020124 A 3260 SENSOR AIRBUS 320 A320* EU CFMINT CFM56 CFM565A1 NE MLG CONTAMINATED W O OTHER N FALSE WARNING CL CLIMB 1 AU S (AUS) LANDING GEAR SENSORS CONTAMINATED WITH EXCESS GREASE CAUSING INCORRECT INDICATIONS. 2 L 7 2 4F 4 F RT A46NM E29NE 2002030600043 20020306 00043 EU 2002 3 6 QXEA0200162 1 20020211 A 5320 DOUBLER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACKED REPAIR DOUBLER AT FRAME 13815B ON RT SIDE OF STRINGER 73. REPAIRED IAW FOKKER SRM 51-10-05, PAGES 1-7, SR M 51-10-04 AND SRM 51-11-04, PAGE 5, TABLE 2. 2 L 7 2 4F RT A20EU 2002030600044 20020306 00044 EU 2002 3 6 AUS20020058 1 20020124 A 2697 63601199950 WIRE AGUSTA A109 A119 0261102 EU FIRE DETECTOR CHAFED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FIRE DETECTOR WIRING CHAFED IN INTAKE AREA ON LT SIDE OF ENGINE DECK. 1 G 7 2 3U H7EU 2002031100176 20020311 00176 NM 2002 3 11 F3LA200200103 1 20020228 A 7110 COWLING BOEING 737 7372Y5 1384554 NM NR 2 ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 118RW 3592 23040 DURING C-3 CHECK, INSPECTION REPORTED CRACK ON AFT LOWER CORNER OF NR 2 ENGINE OUTBOARD FIXED COWL NEXT TO FIRE SEAL. F ABRICATED AND INSTALLED REPAIR PER SRM 51-40-3 AND 51-30-2. 2 L 7 2 4U RT A16WE 2002030600046 20020306 00046 EU 2002 3 6 QXEA0200167 1 20020208 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - PANEL 73E HAS VERY LIGHT FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 57-01-01, PAGE 5. 2 L 7 2 4F RT A20EU 2002030600048 20020306 00048 EU 2002 3 6 QXEA0200168 1 20020209 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - PANEL 73G HAS VERY LIGHT FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9. 2 L 7 2 4F RT A20EU 2002030600049 20020306 00049 EU 2002 3 6 QXEA0200169 1 20020209 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - PANEL 73D HAS VERY LIGHT FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2002030600050 20020306 00050 EU 2002 3 6 QXEA0200170 1 20020208 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - PANEL 73C HAS VERY LIGHT FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5 AND SRM 51-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2002030600051 20020306 00051 EU 2002 3 6 QXEA0200171 1 20020208 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - PANEL 71A HAS FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002030600052 20020306 00052 EU 2002 3 6 QXEA0200172 1 20020208 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - PANEL 73A HAS FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002030600053 20020306 00053 NM 2002 3 6 AUS20020063 1 20020125 A 2163 213A64041 FILTER BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C 13802 EU CABIN TEMP CONTAMINATED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 AU S (AUS) CABIN INLET DUCT SENSOR FILTERS (2OFF) AND COCKPIT INLET DUCT SENSOR FILTER SUSPECT CONTAMINATED. 2 L 7 2 4F 4 F RT A16WE E21EU 2002030600054 20020306 00054 EU 2002 3 6 QXEA0200173 1 20020208 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - PANEL 73B HAS FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002030600055 20020306 00055 EU 2002 3 6 QXEA0200174 1 20020210 A 5730 FLANGE FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT WING FLANGE FOR PANEL 71A HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002030600056 20020306 00056 EU 2002 3 6 QXEA0200175 1 20020209 A 5730 FLANGE FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT WING FLANGE FOR PANEL 73A HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH 4C, SRM 57-12-01, PAGE 32 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002030600057 20020306 00057 EU 2002 3 6 QXEA0200176 1 20020209 A 5730 FLANGE FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT WING FLANGE FOR PANEL 73B HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5 AND SRM 51-10-4, PA GE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 2002030600058 20020306 00058 EU 2002 3 6 QXEA0200177 1 20020209 A 5713 STRINGER FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CORROSION ON LT WING STRINGER 2.36 AT STATION 6410. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5 AND SRM 51-10-4, PAG ES 8 AND 9. 2 L 7 2 4F RT A20EU 2002030600059 20020306 00059 EU 2002 3 6 QXEA0200178 1 20020209 A 5713 STRINGER FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CORROSION ON LT WING STRINGER 2.37 AT STATION 6410. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5 AND SRM 51-10-4, PAG ES 8 AND 9. 2 L 7 2 4F RT A20EU 2002030600060 20020306 00060 EU 2002 3 6 QXEA0200179 1 20020209 A 5713 STRINGER FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CORROSION ON LT WING STRINGER 2.38 AND STATION 6410. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5 AND SRM 51-10-4, PA GES 8 AND 9. 2 L 7 2 4F RT A20EU 2002030600061 20020306 00061 EU 2002 3 6 QXEA0200180 1 20020209 A 5730 FLANGE FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LIGHT FRETTING CORROSION ON WING FLANGE FOR PANEL 73C. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 2002030600062 20020306 00062 EU 2002 3 6 QXEA0200181 1 20020209 A 5730 FLANGE FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - MINOR FRETTING CORROSION AROUND ATTACH HOLES AT WING FLANGE FOR PANEL 73D. REPAIRED IAW FOKKER SRM 57-01-01 AND S RM 51-10-4, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 2002030600063 20020306 00063 EU 2002 3 6 QXEA0200182 1 20020209 A 5730 FLANGE FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - MINOR FRETTING CORROSION AROUND ATTACH HOLES, AT WING FLANGE FOR PANEL 73E. REPAIRED IAW FOKKER SRM 57-01-01, PAG E 5, PARAGRAPH 4C AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 2002030600064 20020306 00064 EU 2002 3 6 QXEA0200183 1 20020209 A 5730 FLANGE FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LIGHT FRETTING CORROSION AROUND ATTACH HOLES, AT WING FLANGE FOR PANEL 73F. REPAIRED IAW FOKKER SRM 57-01-01, PAG E 5, PARAGRAPH 4C, SRM 57-01-01, PARAGRAPH B(2)(A) AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002030600065 20020306 00065 EU 2002 3 6 QXEA0200184 1 20020209 A 5730 FLANGE FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LIGHT FRETTING CORROSION AROUND ATTACH HOLES, AT WING FLANGE FOR PANEL 73G. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 2002030600066 20020306 00066 EU 2002 3 6 QXEA0200185 1 20020209 A 5730 FLANGE FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LIGHT FRETTING CORROSION AROUND ATTACH HOLES AT WING FLANGE FOR PANEL 73H. REPAIRED IAW FOKKER SRM 87-01-01 AND S RM 51-10-4, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 2002030600067 20020306 00067 EU 2002 3 6 QXEA0200186 1 20020210 A 5713 STRINGER FOKKER F28 F28MK4000 4990810 EU LT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT WING STRINGER 2.9 GOUGED AT STATION 11130. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6, PARAGRAPH 5B(A). 2 L 7 2 4F RT A20EU 2002030600068 20020306 00068 EU 2002 3 6 QXEA0200187 1 20020210 A 5720 FITTING FOKKER F28 F28MK4000 4990810 EU LT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT WING LOWER STRINGER 2.9 END FITTING IS GOUGED AT STATION 11130. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 6, PARA GRAPH 5B(A). 2 L 7 2 4F RT A20EU 2002030600070 20020306 00070 WP 2002 3 6 IXXA0200007O 1 20020305 A 3260 WARNING LIGHT DOUG DC8 DC863F 302198F WP LANDING GEAR ILLUMINATED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 867BX 82149 1177 46049 ENROUTE FROM TOL TO LAX, AFTER THE LANDING GEAR WAS RETRACTED THE DOOR UNSAFE LIGHT REMAINED ILLUMINATED. THE FLIGHT CR EW CYCLED THE LANDING GEAR, PERFORMED A SUCCESSFUL GEAR UP LATCH CHECK, BUT THE WARNING INDICATION REMAINED THE SAME. TH E FLIGHT CONTINUED TO LAX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEAR DOOR WARNING ELECTRICAL SYST EM WITH NO DISCREPANCIES NOTED IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002030600072 20020306 00072 NM 2002 3 6 AUS20020067 1 20020126 A 2820 COUPLING BOEING 747 747338 NM RROYCE RB211 RB211524D419 54555 NE FUEL LINE MISRIGGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FUEL TRANSFER SYSTEM COUPLING INCORRECTLY ASSEMBLED. 2 L 7 2 4F 4 F RT A20WE E12EU 2002030600073 20020306 00073 EU 2002 3 6 AUS20020068 1 20020204 A 7603 C8222410 CONTROL CABLE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R375 R3754123F21 NE POWER LEVER BROKEN W A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 AU S (AUS) LT ENGINE POWER CONTROL CABLE BROKEN. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P17NE 2002030600074 20020306 00074 NM 2002 3 6 AUS20020069 1 20020130 A 5311 FRAME BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C 13802 EU FUSELAGE TORN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FORWARD AIRSTAIR SEQUENCING LEVER BENT. GUIDE BRACKET BENT AND FRAME TORN. 2 L 7 2 4F 4 F RT A16WE E21EU 2002030600078 20020306 00078 SO 2002 3 6 C2XA02IA044 1 20020227 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14953 145071 BNA - Maintenance found the left and right overwing emergency lights to be inoperative. Maintenance removed and replaced the #4 power supply. The system operationally checked good and the aircraft was approved for return to service. 2 L 7 2 4T RT T00011AT 2002030600079 20020306 00079 EU 2002 3 6 C2XA02IA045 1 20020227 A 3350 7012210 LAMP AEROSP ATR42 ATR42320 8680930 EU BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14830 184 IAH - Crew reported that the forward interior emergency exit light was inoperative. Maintenance removed and replaced the lamps in the exit light assembly and the aircraft was approved for return to service. 2 H 7 2 4T RT A53EU 2002030600080 20020306 00080 SO 2002 3 6 C2XA02IA046 1 20020302 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14920 145380 BNA - Crew reported that the aft ceiling emergency exit light was found to be inoperative. Maintenance removed and repla ced the #4 inverter and the aircraft was approved for return to service. 2 L 7 2 4T RT T00011AT 2002030600081 20020306 00081 EU 2002 3 6 AUS20020073 1 20020126 A 3510 2250413 VALVE BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE OXYGEN SYSTEM FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) OXYGEN BAROMETRIC VALVE ELECTRICAL CONNECTOR HAD DIFFERENT POLARISING KEYS TO THE AIRCRAFT ELECTRICAL CONNECTOR AN D COULDNOT BE FITTED. INVESTIGATION FOUND THAT THE INCORRECT CONNECTOR PN MS2464R14B15PN HAD BEEN FITTED DURING REPAIR I NSTEAD OF THE CORRECT PN MS24264R14B15P6X CONNECTOR. 2 H 7 4 4F 4 F RT A49EU E6NE 2002031400029 20020314 00029 NM 2002 3 14 02FDEA00183 1 20020218 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 DENT ON FRAME AT BS 950F BETWEEN STR 26L AND 27L. REMOVED AND REPLACED FRAME PER SRM 51-40-3 & EA 7-5310-62760. 2 L 7 3 4F RT A3WE 2002031400031 20020314 00031 NM 2002 3 14 02FDEA00184 1 20020306 A 5311 BAC14902763 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 DENT IN FRAME AT BS 560 BETWEEN STR 24L AND 25L. REMOVED AND REPLACED FRAME PER SRM 51-10-2, 51-20-151. 2 L 7 3 4F RT A3WE 2002031400035 20020314 00035 NM 2002 3 14 02FDEA00185 1 20020306 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FRAME DENTED AT BS 600 BETWEEN STR 24 & 25 LT. REMOVED AND REPLACED FRAME PER SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2002031400036 20020314 00036 NM 2002 3 14 02FDEA00186 1 20020220 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION ON TOP OF FLOORBEAM BS 1070, RBL 35-41, WL 208 PER SRM 53-10-1 FIG 4. REMOVED AND REPLACED FLOORBEAM PER EA 7 -5310-62765. 2 L 7 3 4F RT A3WE 2002030600082 20020306 00082 EA 2002 3 6 2002F00141 1 20020120 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77260 7286 FLT 6598 - CMH-DCA - HAD A LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED BULB. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002030600083 20020306 00083 SO 2002 3 6 C2XA02IA047 1 20020305 A 5315 14521721009 BEAM EMB 145 EMB145 3260210 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 7291 145131 IAH, During C-check inspection the floor beam top plate at frame 14 was found to be corroded beyond limits. Maintenance repaired the affected portion of floor beam utilizing a splice repair in accordance with EMB 145 SRM 53-21-10 2 L 7 2 4F RT T00011AT 2002030600084 20020306 00084 EU 2002 3 6 C2XA02IA048 1 20020305 A 3350 7012210 LAMP AEROSP ATR42 ATR42320 8680930 EU CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16824 166 IAH - Maintenance found the passenger door emergency light to be inoperative. Maintenance relamped the light assembly an d the emergency lighting system operationally checked good. The aircraft was the approved for return to service. 2 H 7 2 4T RT A53EU 2002030600085 20020306 00085 EU 2002 3 6 C2XA02IA049 1 20020305 A 3350 7012210 LAMP AEROSP ATR42 ATR42320 8680930 EU CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16824 166 IAH - Maintenance found the right side aft emergency light to be inoperative. Maintenance relamped the affected light as sembly. The lighting system operationally checked good and the aircraft was approved for return to service. 2 H 7 2 4T RT A53EU 2002030600086 20020306 00086 EA 2002 3 6 2002F00142 1 20020110 A 3222 16124101 AXLE CNDAIR CL600 CL6002B19 1900309 EA NLG DAMAGED A MASA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 77331 7331 FLT 5884 - RETURNED TO THE FIELD, AFTER ROTATION AND GEAR RETRACTION A LOUD RUMBLING WAS HEARD AND VIBRATION WAS FELT FR OM THE NOSE GEAR. MAINTENANCE REMOVED AND REPLACED THE NOSE WHEEL AXLE. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002030600087 20020306 00087 NM 2002 3 6 2002F00143 1 20020124 A 2121 4101054 FAN BOEING 757 757* NM E/E BAY MALFUNCTIONED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 552TZ 32586 DURING TAXI STATUS MESSAGE AFT EQUIP EXHAUST FAN 1, AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 AFT EQUIPMENT VENTILATION FAN IAW AMM 21-26-01. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 2002030600090 20020306 00090 NM 2002 3 6 BJNA020101 1 20020106 A 3350 CONNECTOR BOEING 737 737282 13844AT NM CABIN LOOSE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 FLOOR EMERGENCY LIGHTS FORWARD INOPERATIVE. INSPECTED FOUND LOOSE CONNECTION, REINSTALLED AND CLEANED OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002030600091 20020306 00091 NM 2002 3 6 BJNA020102 1 20020106 A 3350 900542 POWER SUPPLY BOEING 737 737282 13844AT NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 RIGHT AND LEFT EMERGENCY EXIT INTERIOR OVERWING LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND BATTERY POWER SUPPLY UNIT, OPS NORMAL IAW 33-51-41, AND 33-51-31. (M) 2 L 7 2 4F RT A16WE 2002030600092 20020306 00092 NM 2002 3 6 BJNA020103 1 20020106 A 3350 900835A BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 MID CABIN EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK NORMAL IAW 33-51-11. (M) 2 L 7 2 4F RT A16WE 2002030600093 20020306 00093 NM 2002 3 6 BJNA020104 1 20020116 A 3350 LIGHT BOEING 737 737282 13844AT NM CABIN CONTAMINATED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 FLOOR EMERGENCY LIGHTS AFT SECTION INOPERATIVE. REMOVED WATER FROM TRACK, DRIED AND RECONNECTED LAMP PER LOCTITE LUMINE SCENT SYSTEM MANUAL 33-50-01 PAGE 707, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002030600094 20020306 00094 NM 2002 3 6 BJNA020105 1 20020131 A 3350 6013211 POWER SUPPLY BOEING 737 737214 138446R NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 EMERGENCY EXIT LIGHTS FROM ROW 15 AFT INOPERATIVE, ALSO FLOOR LEVEL EXIT LIGHTS FOR BOTH AFT EXIT DOORS. REPLACED BATTE RY POWER SUPPLY UNDER SEAT ROW 16 ABC IAW BMM 33-51-11. (M) 2 L 7 2 4F A16WE 2002030600095 20020306 00095 NM 2002 3 6 BJNA020201 1 20020201 A 3350 6013211 POWER SUPPLY BOEING 737 737282 13844AT NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 FOUND LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY POWER SUPPLY IAW BMM 33-51-31, CHECKS NORMAL . (M) 2 L 7 2 4F RT A16WE 2002030600096 20020306 00096 NM 2002 3 6 GAIA02010OP 1 20020204 A 5330 SKIN BOEING 727 727287 1384020 NM FUSELAGE DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 DURING POST FLIGHT INSPECTION MAINTENANCE, FOUND DAMAGE TO THE FUSELAGE SKIN LOCATED AT STATION 610, STRINGER 19L WL 208 . MAINTENANCE REMOVED DAMAGED AREA, AND REPAIRED PER DRAWING P52-R01. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002030600097 20020306 00097 NM 2002 3 6 GAIA02012ST 1 20020206 A 5311 FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 DURING A CPCP INSPECTION DISCOVERED RIGHT WHEEL WELL TOP OUTBOARD BS 910 FRAME SHOWS CRACK TO BOTTOM INSIDE, 3 INCHES LO NG APPROX. ACCOMPLISHED BS 910 FRAME REPAIR IN THE RIGHT WHEEL WELL IAW WITH B727 SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 2002030600098 20020306 00098 NM 2002 3 6 GAIA02013ST 1 20020206 A 5314 KEELBEAM BOEING 727 727232 1384082 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 DURING A CPCP INSPECTION DISCOVERED LEFT WHEEL WELL BS 870 KEEL BEAM WEB SHOWS CRACK JUST FORWARD OF APU CUT OUT, 3 INCH LONG APPROX. ACCOMPLISHED BS 870 KEEL BEAM WEB REPAIR IN THE LEFT WHEEL WELL IAW B727 SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2002030600099 20020306 00099 NM 2002 3 6 GAIA02014ST 1 20020206 A 5314 KEELBEAM BOEING 727 727232 1384082 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 DURING A CPCP INSPECTION DISCOVERED RIGHT WHEEL WELL BS 870 AND KEEL BEAM FRAME ANGLE IS CRACKED, 1 INCH LONG APPROX. A CCOMPLISHED BS 870 AND KEEL BEAM FRAME ANGLE REPLACEMENT IN THE RIGHT WHEEL WELL IAW B727 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2002030600100 20020306 00100 NM 2002 3 6 GAIA02015ST 1 20020206 A 5310 SHEAR TIE BOEING 727 727232 1384082 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 DURING A CPCP INSPECTION DISCOVERED C3 DOOR AFT FRAME BS 1148 SHEAR TIE ABOVE STRINGER 23R IS CORRODED. ACCOMPLISHED BS 1148 SHEAR TIE REPLACEMENT ABOVE STRINGER 23R IAW B727 SRM 53-10-2 FIG 5. (M) 2 L 7 3 4F A3WE 2002030600101 20020306 00101 NM 2002 3 6 GAIA02016ST 1 20020206 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 DURING A CPCP INSPECTION DISCOVERED FORWARD CARGO COMPARTMENT STATION 540 STRINGER 23R CORROSION ON STRINGER. ACCOMPLIS HED STRINGER REPAIR AT BS 540 STRINGER 23R IAW B727 SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2002030600102 20020306 00102 NM 2002 3 6 GAIA02017ST 1 20020204 A 5311 FRAME BOEING 727 727243 138408D NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 579PE 21662 DURING INSPECTION, IT WAS DISCOVERED THAT A FUSELAGE FRAME WAS CRACKED AT STATION 580. ACCOMPLISHED FRAME REPAIR IAW B7 27 SRM 51-40-3. (M) 2 L 7 3 4F RT A3WE 2002030600103 20020306 00103 NM 2002 3 6 GAIA02018ST 1 20020208 A 5311 FRAME BOEING 727 727243 138408D NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 579PE 21662 DURING INSPECTION, IT WAS DISCOVERED THAT A FUSELAGE FRAME WAS CRACKED AT STATION 640. ACCOMPLISHED FRAME REPAIR IAW B7 27 SRM 51-40-3. (M) 2 L 7 3 4F RT A3WE 2002030600104 20020306 00104 EU 2002 3 6 QXEA0200188 1 20020210 A 5713 STRINGER FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - LT WING STRINGER 2.31 HAS TOOL MARK BECOMING CORRODED AT STATION 10990. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002030600105 20020306 00105 EU 2002 3 6 QXEA0200189 1 20020209 A 5730 FLANGE FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - ALODINE DETERIORATED ON LT WING FLANGE FOR PANELS 73E-73J, LIGHT CORROSION FILM FORMING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 2002030600106 20020306 00106 EU 2002 3 6 QXEA0200190 1 20020209 A 5730 FLANGE FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LIGHT FRETTING CORROSION ON FLANGE OF WING FOR PANEL 73J. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 2002030600107 20020306 00107 EU 2002 3 6 QXEA0200192 1 20020206 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - COCKPIT FLOOR CORROSION BELOW CAPTAINS OUTBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-04, SRM 53-01-01, PAGE 5 AND SRM 53-11-05 PAGE 8, ITEM 325. 2 L 7 2 4F RT A20EU 2002030600108 20020306 00108 EU 2002 3 6 QXEA0200193 1 20020206 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - COCKPIT FLOOR CORROSION UNDER CAPTAINS INBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, SRM 53-11-05 , PAGE 8, ITEM 325 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3C. 2 L 7 2 4F RT A20EU 2002030600109 20020306 00109 EU 2002 3 6 QXEA0200194 1 20020206 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - COCKPIT FLOOR CORROSION UNDER FIRST OFFICERS OUTBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-04-01, PAGE 5, SRM 5 3-11-05, PAGE 8, ITEM 325 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3C. 2 L 7 2 4F RT A20EU 2002030600110 20020306 00110 EU 2002 3 6 QXEA0200195 1 20020207 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - COCKPIT FLOOR CORROSION UNDER FIRST OFFICERS INBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, SRM 51 -10-04, PAGE 8, PARAGRAPH 9 AND HORIZON AIR EA 4-53-1554. 2 L 7 2 4F RT A20EU 2002030600111 20020306 00111 EU 2002 3 6 QXEA0200196 1 20020207 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - AFT DME ANTENNA MOUNT SURFACE ON FUSELAGE SKIN HAS CORROSION ON IT. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PAR AGRAPH 4C AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B (2). 2 L 7 2 4F RT A20EU 2002030600112 20020306 00112 EU 2002 3 6 QXEA0200197 1 20020208 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - UPPER ATC ANTENNA MOUNT SURFACE ON FUSELAGE SKIN HAS CORROSION ON IT. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002030600113 20020306 00113 EU 2002 3 6 QXEA0200198 1 20020209 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- NAV/COMM UPPER ANTENNA MOUNT SURFACE ON FUSELAGE SKIN HAS CORROSION ON IT. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002030600114 20020306 00114 EU 2002 3 6 QXEA0200199 1 20020208 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- VHF COMM FORWARD LOWER ANTENNA MOUNT SURFACE ON FUSELAGE SKIN HAS CORROSION ON IT. REPAIRED IAW FOKKER SRM 51-10-0 4 PAGE 9 PARA 4A AND 4B. 2 L 7 2 4F RT A20EU 2002030600115 20020306 00115 EU 2002 3 6 QXEA0200200 1 20020208 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- LOWER AIR TRAFFIC CONTROL ANTENNA MOUNT SKIN HAS CORROSION ON IT. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002030600116 20020306 00116 EU 2002 3 6 QXEA0200201 1 20020207 A 5320 SUPPORT BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED GILLINER SUPPORT BRACKET AND MISSING NUT PLATE AT FRAME 15635 OVER STRINGER 70. REPAIRED IAW FOKKER SRM 51 -11-4 PARA E AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030600117 20020306 00117 SO 2002 3 6 C2XA02IA051 1 20020305 A 3350 1317 LAMP EMB 120 EMB120ER 3260203 SO FUSELAGE BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 58733 120197 IAH - Maintenance found the right overwing emergency exit light to be inoperative. Maintenance removed and replaced the affected lamp, operationally checked the lighting system and approved the aircraft for return to service. 2 L 7 2 4T RT A31SO 2002030600118 20020306 00118 EU 2002 3 6 QXEA0200202 1 20020207 A 5542 DOUBLER FOKKER F28 F28MK4000 4990810 EU RUDDER CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- THE TOP EDGE OF THE BOTTOM SKIN PANEL ON THE RUDDER COVE HAS A TEMPORARY REPAIR STRIP INSTALLED ON THE INTERIOR BY THE GUSTLOCK HOUSING. THE STRUCTURE IS WORKING AND PRODUCING ALUMINUM OXIDE BUILDUP. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002030600119 20020306 00119 EU 2002 3 6 QXEA0200203 1 20020207 A 1430 RIVET FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- RIVET HEAD CRACKED ON TOP RIGHT HAND CORNER OF THE RUDDER COVE BOTTOM SKIN PANEL. REPAIRED IAW FOKKER SRM 51-31-01 . 2 L 7 2 4F RT A20EU 2002030600120 20020306 00120 EU 2002 3 6 QXEA0200204 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CORROSION BETWEEN STRINGER 74 AND STRINGER 1, ON FRAME CASTELLATION OF FRAME 15205. REPAIRED IAW FOKKER SRM 53-01- 01 PAGES 5-6 AND 51-10-04. 2 L 7 2 4F RT A20EU 2002030600121 20020306 00121 EU 2002 3 6 QXEA0200205 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CORROSION AT STRINGER 1 AND FRAME CASTELLATION FOR FRAME 15205. REPAIRED IAW FOKKER SRM 53-01-01 PAGES 5-6 AND 51- 10-4. 2 L 7 2 4F RT A20EU 2002030600122 20020306 00122 EU 2002 3 6 QXEA0200206 1 20020207 A 5320 DOUBLER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACK IN FRAME CLIP REPAIR DOUBLER AT FRAME 13815A AND STRINGER 2. REPAIRED IAW FOKKER SRM 51-10-05, 51-10-4 AND 5 1-31-01. 2 L 7 2 4F RT A20EU 2002030600123 20020306 00123 EU 2002 3 6 QXEA0200207 1 20020207 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION BETWEEN STRINGERS 1 AND 2 AT FRAME 13815A. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2, 53-02-13 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030600124 20020306 00124 EU 2002 3 6 QXEA0200208 1 20020207 A 5320 DOUBLER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED REPAIR DOUBLER AT FRAME 13815A AND STRINGER 73. REPAIRED IAW FOKKER SRM 51-10-05, 53-02-13, 51-10-4 AND 51 -31-01. 2 L 7 2 4F RT A20EU 2002030600125 20020306 00125 EU 2002 3 6 QXEA0200209 1 20020211 A 5320 DOUBLER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED REPAIR DOUBLER AT FRAME 13815B AND STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2, 51-10-04 PAGE 9, 51-20-00, 51-31-01, AND 51-11-04 PAGE 5. 2 L 7 2 4F RT A20EU 2002030600126 20020306 00126 EU 2002 3 6 QXEA0200210 1 20020211 A 5320 DOUBLER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED REPAIR DOUBLER AT FRAME 13815B AND STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2, 51-10-04 PAGE 9, 51-10-5 PAGES 1-7, 51-20-00, 51-31-01 AND 51-11-04. 2 L 7 2 4F RT A20EU 2002030600127 20020306 00127 EU 2002 3 6 QXEA0200211 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- RIGHT HAND INBOARD SEAT TRACK FROM FRAME 10346, FORWARD ABOUT THREE INCHES ON MATTING FLANGE THERE IS CORROSION. R EPAIRED IAW FOKKER SRM 53-01-01 PAGE 8, 53-40-01 PAGE 206 AND 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2002030600128 20020306 00128 EU 2002 3 6 QXEA0200212 1 20020206 A 5720 STRAP FOKKER F28 F28MK4000 4990810 EU LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- LT WING HAS CHAFE DAMAGE TO WING JOINT STRAP AT WS 1700, LOWER WING SURFACE. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 5 AND HORIZON AIR EA 4-57-575. 2 L 7 2 4F RT A20EU 2002030600129 20020306 00129 EU 2002 3 6 QXEA0200213 1 20020209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- RT INBOARD SEAT TRACK FROM FRAME 12405 INSIDE TUNNEL HAS PITTING CORROSION. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 206 AND 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2002030600130 20020306 00130 EU 2002 3 6 QXEA0200214 1 20020209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- RT INBOARD SEAT TRACK FROM FRAME 12875 FORWARD 8 INCHES INSIDE TUNNEL HAS CORROSION. REPAIRED IAW FOKKER SRM 53-40 -01 PAGE 206 AND 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2002030600131 20020306 00131 EU 2002 3 6 QXEA0200215 1 20020212 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- RT INBOARD SEAT TRACK AT FRAME 13345 FORWARD INBOARD FLANGE HAS PITTING CORROSION. REPAIRED IAW FOKKER SRM 53-40-0 1 PAGE 206 AND 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2002030600132 20020306 00132 EU 2002 3 6 QXEA0200216 1 20020209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- RT INBOARD SEAT TRACK AT FRAME 13815 FORWARD INSIDE TUNNEL HAS CORROSION. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 20 6 AND 51-10-04 PAGE 9. 2 L 7 2 4F RT A20EU 2002030600133 20020306 00133 EU 2002 3 6 QXEA0200217 1 20020209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- RT INBOARD SEAT TRACK AT FRAME 13815 AFT INSIDE LUGS HAVE CORROSION. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 8, 53-4 0-01 PAGE 206 AND 51-10-4 PAGE 9. 2 L 7 2 4F RT A20EU 2002030600134 20020306 00134 EU 2002 3 6 QXEA0200218 1 20020209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- RT INBOARD SEAT TRACK AT FRAME 13815B JUST FORWARD ABOUT 2.5 INCHES IN TUNNEL THERE IS CORROSION. REPAIRED IAW FOK KER SRM 53-01-01 PAGE 8, 53-40-01 PAGE 206 AND 51-10-4 PAGE 9. 2 L 7 2 4F RT A20EU 2002030600135 20020306 00135 WP 2002 3 6 MWEA020160 1 20020306 A 5310 99101407 WEB DOUG DC9 DC932 3022066 WP STATION 302 CANNING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 STATION 302 SUBFLOOR WEB LEFT SIDE IS OIL CANNING. -- FABRICATED AND INSTALLED SUBFLOOR WEB REPAIR. 2 L 7 2 4F A6WE 2002030600136 20020306 00136 WP 2002 3 6 MWEA020162 1 20020306 A 5750 995760015 ANGLE DOUG DC9 DC932 3022066 WP LEFT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING OUTBOARD FLAP HINGE FITTING OUTBOARD ATTACH ANGLE IS CRACKED. -- LOCATED, DRILLED AND DEBURRED RIB ANGLE. 2 L 7 2 4F A6WE 2002030600137 20020306 00137 WP 2002 3 6 MWEA020163 1 20020306 A 5750 99577737 FORMER DOUG DC9 DC932 3022066 WP A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 INBOARD FIXED VANE OUTBOARD STRUT L/E NOSE FORMER CRACKED. -- REMOVED AND REPLACED DOUBLER. 2 L 7 2 4F A6WE 2002030600138 20020306 00138 EU 2002 3 6 QXEA0200219 1 20020209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- RT INBOARD SEAT TRACK AT STATION 649.400 IN TUNNEL IS CORRODED. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 8, 53-40-01 PAGE 206 AND 51-10-4 PAGE 9. 2 L 7 2 4F RT A20EU 2002030700001 20020307 00001 NM 2002 3 7 AUS20020074 1 20020128 A 3250 HOSE BOEING 747 747338 NM NLG STEERING LEAKING W O OTHER K FLUID LOSS NR NOT REPORTED 1 AU S (AUS) LT BODY LANDING GEAR STEERING SYSTEM FLEXIBLE HYDRAULIC HOSE LEAKING. LOSS OF NR 1 HYDRAULIC SYSTEM FLUID. 2 L 7 2 4F RT A20WE 2002030700003 20020307 00003 NM 2002 3 7 AUS20020077 1 20020126 A 5610 5717623096 WINDOW BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C 13802 EU COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 AU S (AUS) RT NR 2 SLIDING WINDOW OUTER PANEL CRACKED. 2 L 7 2 4F 4 F RT A16WE E21EU 2002030700004 20020307 00004 NM 2002 3 7 AUS20020078 1 20020205 A 7720 285N0028 CARD BOEING 767 767300 1385204 NM RROYCE RB211 RB211524* NE ENGINE TEMP WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) LT TURBINE / STRUT OVERHEAT CARD M10425 WAS INCORRECT PART NUMBER. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART. 2 L 7 2 4F 4 F RT A1NM E12EU 2002030700011 20020307 00011 NM 2002 3 7 SWAA020484 1 20020305 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 7. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002030700012 20020307 00012 NM 2002 3 7 SWAA020485 1 20020304 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 628SW 27703 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2002030700013 20020307 00013 NM 2002 3 7 SWAA020487 1 20020303 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED 1/2 INCH LONG AT E/E COOLING EXHAUST CUTOUT. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2002030700014 20020307 00014 NM 2002 3 7 SWAA020488 1 20020304 A 5312 6517583 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 610WN 27696 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 182, WL 181 AND RBL 5.7. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002030700015 20020307 00015 NM 2002 3 7 SWAA020489 1 20020305 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR, UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002030700016 20020307 00016 NM 2002 3 7 SWAA020490 1 20020305 A 5241 6969854 FRAME BOEING 737 7373H4 1384600 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED (2 EA) AT NR 3 STOP FITTING CUTOUT AND LOWER END. REP AIRED FRAME PER SWA T1. 2 L 7 2 4F RT A16WE 2002030700017 20020307 00017 EU 2002 3 7 AWXA200200126 1 20020212 A 5330 2024T3070 DOUBLER AIRBUS 320 A320232 3930326 EU GOUGED A AWXA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 28 639AW 471 LAS - GROUND DAMAGE / MAJOR REPAIR - FLT 741 - "S" - WHILE POSITIONED AT GATE B23 IN LAS A BAGGAGE CART WAS BLOWN INTO T HE LOWER AFT FUSELAGE SKIN 6 O'CLOCK POSION CAUSING 4 EA. GOUGES BETWEEN FRAMES 60 - 61 AND STR 40 - 44 L/H. MAINTENANCE ACCOMPLISHED INTERIM REPAIRS AND INSPECTION IAW AWA ER 26-5300-02043-TB1 BY BLENDING DAMAGE, PERFORMING A VISUAL INSPEC TION, A NDT INSPECTION, AND A FASTENER INSPECTION; AIRCRAFT WAS MAINTENANCE FERRIED TO PHX FOR PERMANENT REPAIR. **SUPP* * AT PHX MAINTENANCE CUTOUT DAMAGED SECTION OF SKIN AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS. FABRICATED 2 EA R EPAIR DOUBLERS AND 1 EACH REPAIR FILLER AND INSTALLED REPAIR PARTS IAW AWA ER 26-5341-02044-TB1. 2 L 7 2 4F RT A28NM 2002030700019 20020307 00019 EA 2002 3 7 COMA0260146 1 20020304 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 916CA 4909 7014 FLIGHT 5687 FLAPS FAILED AT 20 DEGREES.REPLACED THE L/H INBD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2002030700021 20020307 00021 NM 2002 3 7 SWAA020471 1 20020303 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 2. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002030700022 20020307 00022 2002 3 7 SWAA020472 4 20020303 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002030700023 20020307 00023 2002 3 7 SWAA020473 4 20020225 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 751SW 29803 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002030700024 20020307 00024 NM 2002 3 7 SWAA020474 1 20020303 A 3350 101073 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 380SW 26587 EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002030700025 20020307 00025 NM 2002 3 7 SWAA020477 1 20020302 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10R, BS 500B AND BS 727. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002030700026 20020307 00026 NM 2002 3 7 SWAA020478 1 20020302 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10R, BS 727C, BS 727B AND BS 500B. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 2002030700027 20020307 00027 NM 2002 3 7 SWAA020480 1 20020302 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 770, LBL 7 AND LBL 17. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002030700028 20020307 00028 NM 2002 3 7 SWAA020481 1 20020303 A 5314 6545409 WEB BOEING 737 7373H4 1384600 NM LT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED 1/4D CHECK, FOUND WHEEL WELL CEILING PRESS WEB CRACKED AT BS 665, LBL 31. REPAIRED WEB PER SWA T1. 2 L 7 2 4F RT A16WE 2002030700029 20020307 00029 NM 2002 3 7 SWAA020482 1 20020228 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGERS CRACKED AT BS 530, STR 15R AND STR 15L. REPAIRED STR'S PER SRM. 2 L 7 2 4F A16WE 2002030700030 20020307 00030 NM 2002 3 7 SWAA020483 1 20020228 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, LT SIDE. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002030700031 20020307 00031 EA 2002 3 7 COMA0260147 1 20020305 A 2620 MS34762833SW CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 979CA 7159 FLIGHT 5838 CARGO FIRE BOTTLE LOW MESSAGE.REPAIRED WIRING CONNECTOR AT FIRE BOTTLE. 2 L 7 2 4F RT A21EA 2002030700032 20020307 00032 EA 2002 3 7 COMA0260148 1 20020304 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 868CA 7427 FLIGHT 5268 FLAPS FAILED AT 0 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002030700033 20020307 00033 EA 2002 3 7 COMA0260149 1 20020304 A 2760 SPOILER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 924CA 7026 FLIGHT 5409 SPOILER FAULT MESSAGE DURING T/O.RESET SYSTEM, NO FAULTS NOTED. 2 L 7 2 4F RT A21EA 2002030700034 20020307 00034 2002 3 7 HNAA0200025 4 20020306 A 3452 6226523205 CONTROL HEAD DHAV DHC8 DHC8201 2809001 NM BURNED A HNAA K NONE O OTHER LD LANDING 1 EA 07 989HA 11949 427 ON LANDING CREW REPORTED A STRONG BURNING SMELL IN THE COCKPIT. TRACED SMELL TO DUAL MODE S ATC CONTROL HEAD. REPLACED C ONTROL HEAD. 2 H 7 2 4T RT A13NM 2002030700035 20020307 00035 EA 2002 3 7 COMA0260150 1 20020304 A 2760 4916405 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 924CA 12283 7026 FLIGHT 5409 CONFIG SPOILERS WARNING DURING T/O.REPLACED THE #2 SECU. 2 L 7 2 4F RT A21EA 2002030700036 20020307 00036 EA 2002 3 7 COMA0260151 1 20020304 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 403CA 7428 FLIGHT 5406 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002030700037 20020307 00037 EA 2002 3 7 COMA0260152 1 20020304 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS AP APPROACH 1 SO 01 403CA 3263 7428 FLIGHT 5467 FLAPS FAILED AT 20 DEGREES.REPLACED THE R/H INBD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2002030700038 20020307 00038 EA 2002 3 7 COMA0260153 1 20020304 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 916CA 7014 FLIGHT 5602 FLAPS FAILED AT 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002030700040 20020307 00040 EA 2002 3 7 HNAA0200026 1 20020307 A 3246 314801 WHEEL DHAV DHC8 DHC8311 1386006 EA SEPARATED A HNAA K NONE D INFLIGHT SEPARATION LD LANDING 1 EA 07 328EN 14585 219 281 ON LANDING #1 MAIN WHEEL ASSY DEPARTED THE AIRCRAFT. REPLACED WHEEL ASSY. 2 H 7 2 4T RT A13NM 2002030700052 20020307 00052 WP 2002 3 7 P2EA2002M014 1 20020306 A 3350 110049 BATTERY PACK DOUG DC9 DC982 3022082 WP A P2EA K NONE L NO TEST IN INSP/MAINT 1 CE 05 130NJ 49222 AFT Galley Emergency Lights would not test during maintenance. Removed and replaced battery pack IAW MM 332-50-01 operat ional check normal. This is closing action for P2EA2002M014. REFLog Page 75325 2 L 7 2 4F A6WE 2002030700055 20020307 00055 WP 2002 3 7 02FDEA00180 1 20020302 A 2722 2025105003 ACTUATOR DOUG DC10 DC1010 3022110 WP RUDDER LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 397FE 46631 AT CRUISE NR 2 HYD QTY LEAKING. REMOVED AND REPLACED LOWER RUDDER ACTUATOR PER MM 27-23-01-4. 2 L 7 3 4F A22WE 2002030700056 20020307 00056 NM 2002 3 7 02FDEA00182 1 20020305 A 2132 INDICATOR BOEING 727 727173C 1384059 NM COCKPIT FAULTY A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 199FE 19509 A/C W/N PRESSURIZE, APPEARED LEFT PACK NOT SUPPLYING AIR TO A/C. RAN ENGS, PERFORMED AIR COND AND PRESSURIZATION OPS TE ST PER JET RUN HDBK CHAPTER 7 & 5A. PRESSURIZED IN AUTO AND MANUAL MODE. BOTH TEST CHECK NORM BOTH PACKS MAINTAIN AIR. 2 L 7 3 4F A3WE 2002030700057 20020307 00057 SW 2002 3 7 2002F00139 1 20020305 A 3340 000030279 LENS BELL 206 206L3 1182108 SW EXTERIOR CRACKED E EXJA O OTHER O OTHER NR NOT REPORTED 1 SO 07 521RC 64 GLASS COVER CONTINUES TO CRACK. 1 G 7 1 3U H2SW 2002030700058 20020307 00058 NM 2002 3 7 AUS20020089 1 20020208 A 2722 60130011 ACTUATOR BOEING 747 747338 NM RROYCE RB211 RB211524D419 54555 NE RUDDER FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S 28354 (AUS) RUDDER RATIO ACTUATOR FAULTY. 2 L 7 2 4F 4 F RT A20WE E12EU 2002030700060 20020307 00060 NM 2002 3 7 AUS20020093 1 20020208 A 2121 732591D COOLING FAN BOEING 767 767300 1385204 NM RROYCE RB211 RB211524* NE AIR DISTRIBUTION FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S 1459 (AUS) FORWARD EQUIPMENT COOLING FAN FAILED. 2 L 7 2 4F 4 F RT A1NM E12EU 2002030700061 20020307 00061 NM 2002 3 7 AUS20020094 1 20020210 A 2780 COUPLING BOEING 747 747238B 1384828 NM RROYCE RB211 RB211524D419 54555 NE SLATS SEPARATED W D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 AU S (AUS) NR 6 AND NR 7 LEADING EDGE FLAPS DISCONNECTED DUE TO THE OUTBOARD SPLINE COUPLING COMING ADRIFT. THERE WAS NO SIGN OF THE LOCKWIREOR ATTACHMENT SCREWS. 2 L 7 4 4F 4 F A20WE E12EU 2002030700063 20020307 00063 CE 2002 3 7 2002F00149 1 20020306 A 3231 NAS3544240 ROD END CESSNA 650 650 2076802 CE LT MLG DOOR BROKEN E K NONE O OTHER IN INSP/MAINT 1 EA 01 900FL 3291 6507049 WHILE PERFORMING A POST FLIGHT INSPECTION, THE LINKAGE ROD FOR THE LEFT MAIN LANDING GEAR UPPER DOOR WAS FOUND TO BE BRO KEN THROUGH AT THE THREADED ROD TO UPPER ROD SECTION. THE BREAK WAS CLEAN AND APPEARED TO BE AT THE LOCATION OF THE ROD END LOCK NUT. THE ROD END WAS REPLACED. 2 L 7 2 4F A9NM 2002031100178 20020311 00178 NM 2002 3 11 F3LA200200104 1 20020306 A 5321 FLOOR PANEL BOEING 737 7373S1 138447S NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3167 24856 DURING C-5 CHECK, INSPECTION REPORTED CRACK IN FWD CARGO COMPARTMENT FLOOR PANEL AT STA 490, STR 26R. 2 L 7 2 4F RT A16WE 2002030700066 20020307 00066 NM 2002 3 7 AUS20020097 1 20020212 A 3230 272U4200177 LINE BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE MLG CRACKED W O OTHER O OTHER NR NOT REPORTED 1 AU S (AUS) NOSE LANDING GEAR UP' HYDRAULIC LINE CRACKED AT STA 538 LOCATED IN THE FORWARD CARGO COMPARTMENT CEILING. CEILING , SIDEWALL, BILGE AREA AND INSULATION BLANKETS CONTAMINATED WITH HYDRAULIC FLUID. FUMES LEAKED INTO COCKPIT. 2 L 7 4 4F 4 F RT A20WE E30NE 2002030700070 20020307 00070 NM 2002 3 7 2002UALA00275 1 20020224 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 CABIN FUSELAGE FRAME WEB CRACKED AT FASTENER HOLE BODY STATION 887 AT STRINGER 9 LEFT. MAJOR REPAIR ACCOMPLISHED. INST ALLED CHANNEL AND FILLER FRAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030700072 20020307 00072 WP 2002 3 7 IXXA0200008O 1 20020306 A 3260 STRIKER DOUG DC8 DC863F 302198F WP GEAR DOOR WORN A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 867BX 82158 1186 46049 ENROUTE FROM BFI TO PDX, THE LANDING GEAR NOT LATCH LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK. THE FLIGHT CREW CYC LED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO PDX FOR AN UNEVENTFUL LANDING . MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE RIGHT MAIN GEAR DOOR SWITCH STRICER WORN. MAINTENANCE REPLACED T HE STRIKER AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETU RNED TO SERVICE. 2 L 7 4 4F 4A25 2002030700075 20020307 00075 NM 2002 3 7 2002UALA00301 1 20020225 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE BULGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 EXTERNAL FUSELAGE SKIN IS BULGED AT STATION 986 STRINGER 20L. DENT IS COMMON TO STRINGER AND TEAR STRAP. MAJOR REPAIR ACCOMPLISHED. SPLICE AND DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030700076 20020307 00076 NM 2002 3 7 AUS20020099 1 20020202 A 2731 83910081003 TRIM SCALE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ELEVATOR TAB MISINSTALLED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AU S (AUS) CONFIGURATION WARNING HORN SOUNDING FOR NO APPARENT REASON. INVESTIGATION FOUND THE ELEVATOR TRIM SCALE LOCATED IN THE FLIGHT DECK CENTRE CONSOLE TO BE THE CAUSE OF THE PROBLEM. THE ELEVATOR TRIM SCALE HAD BEEN REPLACED DURING INCOR PORATION OF SB8-39-07. INVESTIGATION FOUND THAT THE SERVICE BULLETIN WAS NOT APPLICABLETO THIS AIRCRAFT BUT THAT IT HAD BEEN CARRIED OUT DUE TO INCORRECT PAPERWORK. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002030700077 20020307 00077 NM 2002 3 7 2002UALA00302 1 20020224 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 BODY STATION 178 BULKHEAD CRACKED AT OUTBOARD SIDE OF LEFT HAND UPPER RADAR MOUNT. MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030700078 20020307 00078 NM 2002 3 7 2002UALA00303 1 20020224 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 RIGHT CREASE BEAM HAS CORROSION STATION 950 TO STATION 994 WL 208.1 RBL 44 TO RBL 57. MAJOR REPAIR ACCOMPLISHED. REPLA CED CORRODED ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030700079 20020307 00079 SW 2002 3 7 AUS20020101 1 20020212 A 7334 42D218 PRESSURE SWITCH BELL 412 412 1182202 SW PWA PT6T PT6T3 52045 EA FUEL SYSTEM CRACKED W O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 AU S (AUS) FUEL PRESSURE SWITCH FAULTY. FUEL LEAKING FROM SOLDERED JOINT ON PLUG FITTING LOCATED ON TOP OF SWITCH. 1 G 7 2 4U 4 U H4SW E22EA 2002030700080 20020307 00080 NM 2002 3 7 2002UALA00304 1 20020224 A 5320 THRESHOLD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 AFT PIT DOOR CUTOUT LOWER THRESHOLD WEB HAS NUMEROUS AREAS OF CORROSION FED-AFT END. MAJOR REPAIR ACCOMPLISHED. REPLAC ED THRESHOLD WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030700081 20020307 00081 GL 2002 3 7 AUS20020102 3 20020203 A 6111 PIN HARTZL HCC3YR1 NEWZE FU24 FU24954 6280102 WP LYC O720 IO720A1B 41546 EA HARTZL HCC3Y HCC3YR GL PROPELLER BLADE BROKEN W O OTHER O OTHER CR CRUISE 1 AU S (AUS) PROPELLER BLADE ACTUATING PIN BROKEN. 1 L 7 1 3O 3 O A9PC 1E15 5 C P25EA 2002032500049 20020325 00049 NM 2002 3 25 2002UALA00306 1 20020223 A 2120 ODOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN DETECTED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 213UA 30219 PER CREW, OIL SMELL IN CABIN DURING DESCENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002030700082 20020307 00082 GL 2002 3 7 AUS20020103 3 20020202 A 6111 PIN HARTZL HCC3YR1 NEWZE FU24 FU24954 6280102 WP LYC O720 IO720A1B 41546 EA HARTZL HCC3Y HCC3YR GL PROPELLER BLADE BROKEN W O OTHER O OTHER CL CLIMB 1 AU S 164 (AUS) PROPELLER BLADE PITCH ACTUATING PIN BROKEN. 1 L 7 1 3O 3 O A9PC 1E15 5 C P25EA 2002030700083 20020307 00083 NM 2002 3 7 2002UALA00307 1 20020223 A 2497 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE IDG DAMAGED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 773UA 2644 501 26929 FLIGHT DIVERTED TO LHR DUE TO EN ROUTE LOSS OF RIGHT GENERATOR. FLIGHT WAS RELEASED WITH INOPERATIVE BACK-UP GENERATOR. FLIGHT PLANNED TO LAND OVERWEIGHT. LANDED NORMAL WITH 98,200 LBS FOB. THE RIGHT GENERATOR CONTROL UNIT (GCU) AND INT EGRATED DRIVE GENERATOR (IDG) WERE REPLACED. THE FINAL FIX WAS TO REPLACE THE IDG WIRE HARNESS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002030700084 20020307 00084 NM 2002 3 7 2002UALA00308 1 20020218 A 3320 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BURNED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 128UA 30023 BURNING PLASTIC SMELL REPORTED BY F/A IN UPPER DECK DURING DESCENT. FOUND AND REPLACED LAMPS IN FSB-NS SIGNS IN UPPER D ECK THAT WERE BLACKENED-BURNT. 2 L 7 4 4F 4 F RT A20WE E24NE 2002030700085 20020307 00085 NM 2002 3 7 2002UALA00309 1 20020218 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY CEILING LIGHTS ON RIGHT HAND AISLE AT ROW 8, 24, 48, & 53 ARE INOP. THIS DISCREPANCY WAS FOUND DURING THE COU RSE OF A MAINTENANCE CHECK, (B-CK). RELAMPED CEILING LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2002030700086 20020307 00086 NM 2002 3 7 2002UALA00310 1 20020218 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY CEILING LIGHT AT UPPER DECK ROW 13 IS INOP. FOUND DURING MAINTENANCE CHECK, (B-CK). RELAMPED CEILING LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2002030700087 20020307 00087 EU 2002 3 7 QXEA0200163 1 20020207 A 5755 LINK FOKKER F28 F28MK4000 4990810 EU SPEED BRAKE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - SPEED BRAKE LT SUPPORT LINK HAS CHAFE DAMAGE AT LOWER END OF LOWER DIAGONAL FROM CONTACT WITH COMPOSITE TAIL CONE. REPAIRED IAW HORIZON AIR EA 4-53-1553. 2 L 7 2 4F RT A20EU 2002030700088 20020307 00088 EU 2002 3 7 QXEA0200164 1 20020208 A 5755 LINK FOKKER F28 F28MK4000 4990810 EU SPEED BRAKE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT SUPPORT LINK FOR LT SPEED BRAKE FLAP HAS CHAFE DAMAGE AT UPPER END OF DIAGONAL ARM. REPAIRED IAW HORIZON AIR E A 4-53-1556 AND FOKKER SRM 4-53-1556. 2 L 7 2 4F RT A20EU 2002030700089 20020307 00089 EU 2002 3 7 QXEA0200165 1 20020208 A 5755 LINK FOKKER F28 F28MK4000 4990810 EU SPEED BRAKE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - SPEED BRAKE RT SUPPORT LINK UPPER DIAGONAL IS CHAFED AT UPPER END FROM RUBBING COMPOSITE TAIL CONE. REPAIRED IAW HORIZON AIR EA 4-53-1557 AND FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002030700090 20020307 00090 EU 2002 3 7 QXEA0200166 1 20020208 A 5755 LINK FOKKER F28 F28MK4000 4990810 EU SPEED BRAKE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT SUPPORT LINK FOR SPEED BRAKE IS CHAFED AT BOTTOM END OF LOWER DIAGONAL FROM CONTACT WITH COMPOSITE TAIL CONE. REPAIRED IAW HORIZON AIR EA 4-53-1558 AND FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002030700091 20020307 00091 EU 2002 3 7 AUS20020105 1 20020215 A 5302 360A23002409 MOUNT AEROSP SA365 SA365C 8680667 EU TMECA ARRIEL ARRIEL1A 60030 NE TAIL BOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) TAIL ROTOR GEARBOX MOUNT CRACKED. CRACK EMANATES FROM A WELD AND PROGRESSED TO THE OUTER EDGE OF THE MOUNT PLATE. 1 G 7 2 3U 3 U H10EU E19EU 2002030700093 20020307 00093 NM 2002 3 7 AUS20020107 1 20020210 A 4997 WIRE BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE APU SYSTEM BURNED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) APU GENERATOR FEEDER CABLE BADLY BURNED. THE CABLE WAS ALSO LOOSE WITH INSULATION MISSING. 2 L 7 2 4F 4 F RT A1NM E3NE 2002030700094 20020307 00094 NE 2002 3 7 AUS20020108 2 20020212 A 7250 ST306611 NUT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE TURBINE SECTION UNAPPROVED PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) HIGH PRESSURE TURBINE WHEEL TO HIGH PRESSURE STUB SHAFT ATTACHMENT NUTS WERE INCORRECT PART NUMBER. THE NUTS FIT TED (ST3066-11) WERE NOT AN APPROVED ALTERNATE PART NUMBER. THE NUTSHAD BEEN FITTED AT THE LAST ENGINE HSI. PERSONNEL/MA INTENANCE ERROR. UNAPPROVED PART. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002030700095 20020307 00095 NM 2002 3 7 AUS20020109 1 20020205 A 2797 VARIOUS WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FLIGHT CONTROLS MISMANUFACTURED W O OTHER W F J INADEQUATE Q C FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 AU S (AUS ) SPOILER SYSTEM WIRING INCORRECT. MANUFACTURING ERROR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002030700097 20020307 00097 2002 3 7 AUS20020114 4 20020118 A 3457 14347010106 CDU BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502R5 41580 NE GPS FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 AU S (AUS) GNSX CDU FAILED. SMOKE IN COCKPIT. BURNING SMELL EMINATING FROM COCKPIT DISPLAY UNIT. 2 H 7 4 4F 4 F RT A49EU E6NE 2002030700098 20020307 00098 WP 2002 3 7 AUS20020115 1 20020118 A 6320 369A51983 BEARING HUGHES 369 369HS 4470728 WP ALLSN 250C 250C18 03011 GL M/R GEARBOX CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S 729 (AUS) MAIN TRANSMISSION BEARING INNER RACE SPLIT WITH HEAVY BRINNELLING EVIDENT. METAL CONTAMINATION OF TRANSMISSION OI L SYSTEM. 1 G 7 1 3U 3 U H3WE E4CE 2002030700099 20020307 00099 NM 2002 3 7 AUS20020116 1 20020211 A 5310 STRUCTURE BOEING 747 747238B 1384828 NM NLG WW CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT AND RT SIDES OF THE NOSE WHEEL WELL CRACKED IN NUMEROUS LOCATIONS. FOUND DURING INSPECTION IAW AD/B747/136 AND AD/B747/172. 2 L 7 4 4F A20WE 2002030700100 20020307 00100 NE 2002 3 7 AUS20020118 2 20020217 A 7200 ENGINE BOEING 747 747338 NM RROYCE RB211 RB211524D419 54555 NE NR 1 STALLED W O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 AU S (AUS) NR 1 ENGINE STALLED. VIBRATION FELT AND ENGINE PARAMETERS DIFFERENT FROM OTHER ENGINES. 2 L 7 2 4F 4 F RT A20WE E12EU 2002030700101 20020307 00101 NM 2002 3 7 AUS20020119 1 20020217 A 2424 734284 GCU BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL AC REGULATOR FAULTY W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 AU S (AUS) GENERATOR CONTROL UNIT (GCU) SUSPECT FAULTY. 2 L 7 2 4F 4 F RT A1NM E23EA 2002030700106 20020307 00106 NM 2002 3 7 AUS20020126 1 20020218 A 2722 654486112 PCU 1411503 BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C 13802 EU RUDDER ACTUATOR LEAKING W O OTHER K F J FLUID LOSS FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 AU S 12933 (AUS) RUDDER PCU LEAKING INTERNALLY. RUDDER STANDBY PCU ALSO LEAKING INTERNALLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2002030700107 20020307 00107 2002 3 7 AUS20020129 4 20020222 A 2565 BACW10P21TF WASHER BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL GIRT BAR MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ESCAPE SLIDE DEPLOYMENT BAR AFT LINK WASHER MISSING. FOUND DURING INSPECTION IAW AD/B767/163 AND FAA AD 2001-26-19 . 2 L 7 2 4F 4 F RT A1NM E23EA 2002030700108 20020307 00108 EU 2002 3 7 YENA200207 1 20020211 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU RT O/W EMCY EXIT INACTIVE A YENA O OTHER O OTHER DE DESCENT 1 EA 15 506JB 1235 Flt 66, JFK to RSW, Right overwing exit sign did not illuminate on gear extension and remained off at the gate.Removed a nd replaced right wing emergency light power supply per AMM 33-51-33, Ops check OK. 2 L 7 2 4F RT A28NM 2002030700109 20020307 00109 NM 2002 3 7 AUS20020131 1 20020220 A 7110 PANEL BOEING 747 747338 NM ENGINE COWLING DEBONDED W O OTHER E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 AU S (AUS) NR 1 ENGINE ICE IMPACT PANEL DISBONDED. 2 L 7 2 4F RT A20WE 2002030700111 20020307 00111 NM 2002 3 7 AUS20020135 1 20020221 A 2915 00377 RELIEF VALVE BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE HYD SYSTEM FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) HYDRAULIC PUMP PRESSURE RELIEF VALVE FAULTY. VALVE WAS BYPASSING FLUID. 2 L 7 2 4F 4 F RT A1NM E3NE 2002030700112 20020307 00112 EU 2002 3 7 QXEA0200220 1 20020206 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- RT INBOARD SEAT TRACK FROM FRAME 15635 TO FRAME 12405 HAS GOUGED LUGS. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 206. 2 L 7 2 4F RT A20EU 2002030700114 20020307 00114 EU 2002 3 7 QXEA0200221 1 20020208 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- EVIDENCE OF CORROSION UNDER NUT PLATES ON FRAME 5805 AT FOUR WAY SUPPORT BRACKET ABOVE STRINGER 74. REPAIRED IAW F OKKER SRM 51-10-04 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030700116 20020307 00116 EU 2002 3 7 QXEA0200222 1 20020207 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION AT FRAME 12875 AND STRINGER 46. REPAIRED IAW FOKKER SRM 51-10-04, 53-02-13 PAGE 4 AND 51-31-0 1. 2 L 7 2 4F RT A20EU 2002030700117 20020307 00117 EU 2002 3 7 QXEA0200223 1 20020207 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION AT FRAME 12875 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 AND 51-31-0 1. 2 L 7 2 4F RT A20EU 2002030700118 20020307 00118 NE 2002 3 7 AUS20020140 2 20020224 A 7230 13749 COMPRESSOR BOEING 747 747438 NM RROYCE RB211 RB211524* NE NR 3 ENGINE DAMAGED W O OTHER E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) NR 3 ENGINE HP COMPRESSOR FIFTH AND SIXTH STAGES DAMAGED BEYOND LIMITS. 2 L 7 4 4F 4 F RT A20WE E12EU 2002030700119 20020307 00119 EU 2002 3 7 QXEA0200224 1 20020207 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION AT FRAME 13345 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030700120 20020307 00120 EU 2002 3 7 QXEA0200225 1 20020207 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION AT FRAME 13345 AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030700121 20020307 00121 EU 2002 3 7 QXEA0200226 1 20020207 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION AT FRAME 13345 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 53-31-01. 2 L 7 2 4F RT A20EU 2002030700122 20020307 00122 EU 2002 3 7 QXEA0200227 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION AT FRAME 13815 AND STRINGER 17. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030700123 20020307 00123 EU 2002 3 7 QXEA0200228 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION AT FRAME 13815B AND STRINGER 49. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-4 PAGE 9 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030700125 20020307 00125 NM 2002 3 7 02FDEA00188 1 20020307 A 7932 1163P182 SWITCH BOEING 727 727233 138408A NM #2 ENGINE FAILED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 271FE 22036 02-63 #2 ENG LOW OIL PRESS FILTER BYPASS ILLUMINATED. #2 ENG SHUTDOWN. R&R LOW OIL PRESS SW PER MM 79-33-002-4. OPS CK OK. 2 L 7 3 4F RT A3WE 2002031400039 20020314 00039 NM 2002 3 14 02FDEA00189 1 20020306 A 5311 651632448 FRAME BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FRAME DOUBLER CRACKED BS 825, STR 8 LT & 9 LT. REMOVED AND REPLACED FRAME PER EA 7-5310-62774. 2 L 7 3 4F RT A3WE 2002030700126 20020307 00126 NM 2002 3 7 P5CA0200658 1 20020306 A 2780 AN502106 SCREW BOEING 747 7472U3B 1384846 NM L/H WING MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 L/H INBD L/E FLAPS ARE DEPLOYED BUT IND UP AT F/E'S PANEL & FWD IND. ON INSPECTION FOUND PDU DRIVE SHAFT DISCONNECTED, L OCKING SCREW MISSING & LOCKING SLEEVE MIGRATED FROM CONNECTION. RE-RIGGED & RE-ATTACHED DRIVE SHAFT IAW MM 27-81-02. OPS CHECK NORMAL. 2 L 7 4 4F RT A20WE 2002030700127 20020307 00127 NM 2002 3 7 P5CA0200659 1 20020306 A 2611 NONE SMOKE DETECTOR BOEING 747 74746NF 13848BT NM MAIN DECK CONTAMINATED A P5CA O OTHER J N WARNING INDICATION FALSE WARNING CR CRUISE 1 WP 23 450PA 30808 CENTER FIRE SENSORS ON MAIN DECK INDICATED FIRE 9 HRS INTO FLT. VISUAL INSPECTION REVEALED NO FIRE. CB'S PULLED TO SILEN CE ALARM FOR DURATION OF FLT & PERFORMED PERIODIC VISUAL FIRE INSPECTION. CLEANED & DRIED MAIN DECK SMOKE DETECTOR. (DET ECTOR CONTAMINATED DUE TO HORSE CHARTER). PERFORMED FIRE SENSOR BITE TEST. ALL PASSED. OK FOR CONTINUED SERVICE. 2 L 7 4 4F RT A20WE 2002030700128 20020307 00128 SW 2002 3 7 AUS20020143 1 20020211 A 2912 FILTER GULSTM G73 G73 3951802 SW PWA PT6 PT6A34 52043 EA HYDRAULIC SYS CRACKED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AU S (AUS) HYDRAULIC FILTER HOUSING CRACKED CIRCUMFERENTIALLY IN THREADED AREA. LOSS OF HYDRAULIC FLUID. VENT / DUMP VALVE AL SO FAULTY DUE TO A SPLIT O-RING SEAL. 1 H 7 2 3R 4 T A783 E4EA 2002030700131 20020307 00131 SO 2002 3 7 C2XA02CL066 1 20020307 A 3231 852701 PROXIMITY SWITCH EMB 145 EMB145ER 3260211 SO LEFT GEAR FAULTY A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 13936 145025 CLE FLIGHT#3848 THE CREW REPORTED THE LEFT MAIN GEAR DID NOT RETRACT AFTER TAKEOFF.THE AIRCRAFT LANDED WITHOUT FURTHER I NCIDENT.MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN GEAR UPLOCK PROXIMITY SWITCHES.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002030700132 20020307 00132 EU 2002 3 7 QXEA0200318 1 20020226 A 4990 APU FOKKER F28 F28MK4000 4990810 EU APU BAY LEAKING A QXEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 NM 09 499US 11182 YEG - AIRCRAFT RETURNED TO FIELD WHEN THE LAVATORY SMOKE DETECTOR SOUNDED. DURING INSPECTION OF APU AN EXTERNAL OIL LE AK WAS NOTED. MAINTENANCE INSPECTED THE ACM PACK CONDENSER SOCKS FOR OIL CONTAMINATION. NONE WAS NOTED. PRESSURIZED A ND RAN AIRCRAFT WITH PACKS AT FULL HOT FOR 20 MINUTES. NO SMOKE WAS NOTED AND SMOKE DETECTOR DID NOT SOUND. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002030700133 20020307 00133 NM 2002 3 7 QXEA0200319 1 20020226 A 5230 HANDLE BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR LACK OF LUBE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 408QX 4050 FORWARD BAGGAGE DOOR WARNING ILLUMINATED IN CLIMB. DIVERTED TO GEG. MAINTENANCE INTERROGATED FLIGHT HISTORY AND FOUND FORWARD BAGGAGE DOOR LOCK UNREADABLE. LUBED HANDLE AND OPERATED FORWARD BAGGAGE DOOR IAW AMM. OPERATIONAL CHECK IS GOO D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002030700134 20020307 00134 EU 2002 3 7 QXEA0200320 1 20020223 A 2810 9507305 FLOAT VALVE FOKKER F28 F28MK4000 4990810 EU FUEL SYSTEM MALFUNCTIONED A QXEA K NONE K P FLUID LOSS NO WARNING INDICATION CL CLIMB 1 NM 09 496US * * 11169 PDX- AIR TRAFFIC CONTROL ADVISED ON DEPARTURE FROM FRESNO THAT THREE SEPARATE CALLS WERE MADE, REPORTING THAT FUEL WAS V ENTING FROM THE AIRCRAFT. ALL INDICATIONS FROM THE COCKPIT WERE NORMAL THE ENTIRE FLIGHT. REMOVED AND REPLACED VENT FL OAT VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002030700135 20020307 00135 NM 2002 3 7 QXEA0200398 1 20020228 A 5270 SWITCH BOMBDR DHC8 DHC8401 NM CARGO DOOR LACK OF LUBE A QXEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 09 410QX 4053 MSO - FORWARD CARGO DOOR WARNING ILLUMINATED IN FLIGHT. AIRCRAFT WAS DIVERTED TO MSO. MAINTENANCE REMOVED FROST FROM S WITCH AND LUBRICATED. PERFORMED OPERATIONAL CHECK. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002030700136 20020307 00136 NM 2002 3 7 QXEA0200400 1 20020227 A 7797 WIRE HARNESS BOMBDR DHC8 DHC8401 NM NR 1 ENGINE DEFECTIVE A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 405QX 4047 GEG - NR 1 ITT INOP DIVERTED INTO GEG. INTERROGATED CDS AND FOUND FAULT CODES 738, 805. FOUND WIRING HARNESS DEFECTIVE . REPLACED NR 1 ENGINE FUEL ELECTRICAL WIRING HARNESS. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002030700137 20020307 00137 EU 2002 3 7 RAIA00202059 1 20020214 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR OUT OF ADJUST A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 558HK 41071 STL- BAGGAGE DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF. MAINTENANCE INSPECTED AND ADJUSTED BAGGAGE DOOR MICRO SWITC H, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002030700138 20020307 00138 EU 2002 3 7 RAIA00202061 1 20020215 A 5230 LATCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR LACK OF LUBE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 550HK 41039 STL- BAGGAGE DOOR UNSAFE LIGHT CAME ON DURING TAKEOFF ROLL. MAINTENANCE CLEANED AND LUBED DOOR LATCH MECHANISM, OPS CHE CK OK. 2 L 7 2 4T RT A41NM 2002030700139 20020307 00139 EU 2002 3 7 RAIA00202062 1 20020217 A 3397 WIRE JETAIR JETSTM JETSTM4101 1500501 EU CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 565HK 41082 MX - STL - ESCAPE PATH LIGHTS AT SEATS 1 & 2 INOP. REPAIRED EMERGENCY PATH LIGHT BROKEN WIRE AT SEAT 1A, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002030700140 20020307 00140 SO 2002 3 7 RAIA00202063 1 20020123 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 MX-STL- DURING 8000 HOUR INSPECTION FOUND CORROSION ON CENTER FUSELAGE OMEGA BEAM AT FRAME 20. REPAIRED OMEGA CENTER BEA M. 2 L 7 2 4F RT T00011AT 2002030700141 20020307 00141 EU 2002 3 7 RAIA00202065 1 20020215 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 574HK 41093 MX-STL- LEFT FORWARD SECTION OF EMERGENCY PATH LIGHTS INOP. RESECURED PATH LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT A41NM 2002030700142 20020307 00142 EU 2002 3 7 RAIA00202067 1 20020218 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 574HK 41093 MX-BMI- FORWARD SECTION OF EMERGENCY PATH LIGHTS INOP. RESECURED LOOSE CONNECTION AT EMERGENCY PATH LIGHTS, OPS CHECK O K. 2 L 7 2 4T RT A41NM 2002030700143 20020307 00143 SO 2002 3 7 RAIA00202068 1 20020218 A 2160 C1431232 CONTROL VALVE EMB 145 EMB145 3260210 SO A/C BAY FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 809HK 5349 145187 5324-PIT- CREW REPORTED NR 2 PAC OVERLOAD WARNING MESSAGE DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED DUAL TEMP CO NTROL VALVE, OP CHECK OK. 2 L 7 2 4F RT T00011AT 2002030700144 20020307 00144 EU 2002 3 7 RAIA00202076 1 20020219 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 552HK 41057 MX-STL- EMERGENCY ESCAPE PATH LIGHTS OUT ROW 1-3. RECONNECTED CONNECTOR ON ESCAPE PATH LIGHTS, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002030700145 20020307 00145 EU 2002 3 7 RAIA00202078 1 20020220 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 561HK 41077 MX-STL- EMERGENCY PATH LIGHTS INOP. SECURED LOOSE CONNECTOR AT EMERGENCY TRACK LIGHT. 2 L 7 2 4T RT A41NM 2002030700146 20020307 00146 EU 2002 3 7 RAIA00202080 1 20020221 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN NOT SEATED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 561HK 41077 MX-STL- EMERGENCY PATH LIGHTS ROW 3-5 INOP. RESEATED CONNECTOR AT EMERGENCY PATH LIGHTS. 2 L 7 2 4T RT A41NM 2002030700147 20020307 00147 SO 2002 3 7 RAIA00202086 1 20020227 A 2915 368960103 O-RING EMB 145 EMB145LR 3260212 SO RELIEF VALVE DAMAGED A RAIA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 03 812HK 145373 PIT- DURING DESCENT CREW ALERTING SYSTEM MESSAGE WITH MALFUNCTION DISPLAY MESSAGE HYD SYS NR 1 LOW. MAINTENANCE REMOVED AND REPLACED O-RING AT NR 1 HYD SYSTEM PRESSURE RELIEF VALVE, OPS AND LEAK CHECK OK. 2 L 7 2 4T RT T00011AT 2002030700148 20020307 00148 EU 2002 3 7 RAIA00203087 1 20020303 A 2120 INSULATION AEROSP ATR72 ATR72202 8680940 EU PAX AIR DUCT DETERIORATED A RAIA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 CE 03 723TE 283 STL- CENTRAL ANNUNCIATOR PANEL ELEC SMOKE ILLUMINATED. MAINTENANCE REPAIRED DETERIORATED INSULATION AT PAX AIR DISTRI BUTION DUCT, OPS CHECK OK. 2 H 7 2 4T RT A53EU 2002032700174 20020327 00174 EU 2002 3 27 RAIA00203088 1 20020303 A 2611 SMOKE WARNING AEROSP ATR72 ATR72202 8680940 EU COCKPIT FALSE ACTIVATION A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 723TE 283 5592-STL- ELEC SMOKE ANNUNCIATOR ILLUMINATED. MAINTENANCE TROUBLESHOT AND DEFERRED THE NR 2 BLEED SYSTEM. MAINTENANCE GROUND RAN RT BLEED AND PACK, OPS CHECK OK IAW MM 36-11-00. 2 H 7 2 4T RT A53EU 2002030700150 20020307 00150 NM 2002 3 7 SABA0200 1 20020228 A 3397 WIRE DHAV DHC8 DHC8103 1386005 NM CABIN OUT OF POSITION A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 801WP 086 AIRCRAFT 801 ON FLIGHT 8680 FROM CLT TO FAY. DURING PREFLIGHT INSPECTION THE CABIN FLOOR EMERGENCY WERE FOUND INOPERATI VE. MAINTENANCE REPOSITIONED WIRING. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002030700151 20020307 00151 EU 2002 3 7 SABA020020 1 20020214 A 3240 AH084357 SHUTTLE VALVE BAG JETSTM JETSTM3201 1500217 EU LT MLG LEAKING A SABA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 33 959A 959 AIRCRAFT 959 ON FLIGHT 5001 FROM HTS TO CLT. DURING TAXI OUT FOR DEPARTURE AT HTS THE LEFT BRAKE PRESSURE INDICATED ZER O AND THE LEFT BRAKE DID NOT RESPOND TO PEDAL INPUT. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO THE GATE WI TH NO OTHER PROBLEMS. MAINTENANCE FROM CLT TIGHTENED LOOSE WIRE ON THE BRAKE PRESSURE TRANSMITTER. THE LEFT BRAKE SHUT TLE VALVE WAS FOUND TO BE LEAKING. MAINTENANCE REMOVED AND REPLACED THE SHUTTLE VALVE. OPS CHECK WAS GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2002030700152 20020307 00152 EU 2002 3 7 2002F00151 1 20020125 A 5347 EPNE95300013023 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 545AT 8098 DURING CPCP2 AND 4 INSPECTIONS, CORROSION WAS FOUND ON 4 CABIN SEAT TRACKS, LEFT INBOARD MIDDLE, LEFT FLIGHT ATTENDANT, RIGHT MIDDLE INBOARD, RIGHT AFT INBOARD. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AE EO E2-53MR-115R1. THE AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002030700153 20020307 00153 EU 2002 3 7 2002F00152 1 20020125 A 5347 EPNE953000013014 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 545AT 545 DURING CPCP2 AND 4 INSPECTIONS, CORROSION WAS FOUND ON 4 CABIN SEAT TRACKS, LEFT INBOARD MIDDLE, LEFT FLIGHT ATTENDANT, RIGHT MIDDLE INBOARD, RIGHT AFT INBOARD. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AE EO E2-53MR-115R1. THE AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002030700154 20020307 00154 EU 2002 3 7 2002F00153 1 20020125 A 5347 EPNE95300013022 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 545AT 545 DURING CPCP2 AND 4 INSPECTIONS, CORROSION WAS FOUND ON 4 CABIN SEAT TRACKS, LEFT INBOARD MIDDLE, LEFT FLIGHT ATTENDANT, RIGHT MIDDLE INBOARD, RIGHT AFT INBOARD. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AE EO E2-53MR-115R1. THE AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002030700155 20020307 00155 EU 2002 3 7 SIMA200201701 1 20020115 A 5260 SUPPORT AEROSP ATR72 ATR72212 8680945 EU PAX STAIRS CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 DURING CPCP 2 INSPECTION, PASSENGER ENTRY STAIR, TREAD SUPPORTS WERE FOUND CORRODED. THE TREAD SUPPORTS (P/N S521764060 0001, S5217640620400) WERE REMOVED AND REPLACED IAW ATR72 SRM 51-21-42. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002030700156 20020307 00156 EU 2002 3 7 SIMA200201702 1 20020115 A 5311 S5357231120001 FRAME AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AT 274 DURING CPCP2 INSPECTION, FRAME 28D WAS FOUND TO BE CORRODED. THE FRAME WAS REMOVED AND REPLACED IAW ATR72 SRM 51-21-42. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002030700157 20020307 00157 SO 2002 3 7 SIMA200202309 1 20020104 A 3220 14524475001 CAP EMB 135 EMB135LR 3260305 SO NLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 714BZ 145260 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE NOSE LANDING GEAR BEARING CAPS. MAINTENANCE REPLACED TH E NOSE LANDING CAPS IAW EMB135 MM 32-20-01-400-001-A. (M) 2 L 7 2 4F RT TOOO11AT 2002030700158 20020307 00158 SO 2002 3 7 SIMA200202310 1 20020104 A 3210 14571033009 CAP EMB 145 EMB145LR 3260212 SO LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE LEFT MAIN LANDING GEAR LOWER FORWARD AND AFT BEARING CAP S. MAINTENANCE REPLACED THE CAPS IAW EMB145 MM 32-10-01-000-801-A AND 32-10-01-400-801-A. (M) 2 L 7 2 4T RT T00011AT 2002030700159 20020307 00159 SO 2002 3 7 SIMA200202311 1 20020104 A 3220 14524475001 CAP EMB 145 EMB145LR 3260212 SO NLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE NOSE LANDING GEAR RIGHT BEARING CAP. MAINTENANCE REPLAC ED THE NOSE LANDING BEARING CAP IAW EMB 145 MM 32-20-01-000-801-A AND 32-20-01-400-801-A. (M) 2 L 7 2 4T RT T00011AT 2002030700161 20020307 00161 EU 2002 3 7 SIMA200202803 1 20020125 A 5730 S5711232000000 FLANGE AEROSP ATR72 ATR72212A 8680902 EU WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 545AT 545 SAW - DURING CPCP 4 INSPECTION, FOUND CORROSION ON WING UPPER SURFACE FLANGES FOR WING ACCESS PANELS 522CT AND 521DT. T HE FLANGES WERE BLENDED TO REMOVE CORROSION IAW ATR72 SRM 57-14-12. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002030700162 20020307 00162 EU 2002 3 7 SIMA200202804 1 20020125 A 5320 EPNE95300013025 FITTING AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 545AT 545 DURING CPCP4 INSPECTION, FOUND CORROSION WAS FOUND ON LAVATORY WALL ATTACHMENT FEET. ATTACHMENT FEET WERE REMOVED AND R EPLACED IAW AE EO E2-53-MR-1151R. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002030700163 20020307 00163 EU 2002 3 7 SIMA200202805 1 20020125 A 5347 EPNE95300013014 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 545AT 545 DURING CPCP2 AND 4 INSPECTIONS, CORROSION WAS FOUND ON 4 CABIN SEAT TRACKS, LEFT INBOARD MIDDLE, LEFT FLIGHT ATTENDANT, RIGHT MIDDLE INBOARD, RIGHT AFT INBOARD. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AE EO E2-53MR-115R1. THE AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002030700164 20020307 00164 SO 2002 3 7 SIMA20020303 1 20020102 A 5320 14522459003 SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 714BZ 145260 ABI - DURING MBV INSPECTION MAINTENANCE FOUND, THE CENTER RAMP SUPPORT TO BE CORRODED BETWEEN FRAME 19 AND 20. MAINTENA NCE REPLACED THE CENTER RAMP SUPPORT IAW EMB 135 SRM 51-40-02, 51-20-03 AND 51-40-04. (M) 2 L 7 2 4F RT TOOO11AT 2002030700165 20020307 00165 EU 2002 3 7 SIMA200203201 1 20020131 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 341SB 340B341 PSP - FLT 3298 - EMERGENCY LIGHTS INOPERATIVE. RAI EMERGENCY POWER SUPPLY AT ROW 10BC IAW SAAB 340B AMM 33-50-10. PERF ORMED OPERATIONAL CHECK IAW SAAB 340B MM 33-50-00. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2002030700166 20020307 00166 EU 2002 3 7 QXEA0200229 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION AT FRAME 13815B AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030700167 20020307 00167 EU 2002 3 7 QXEA0200230 1 20020207 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030700168 20020307 00168 EU 2002 3 7 QXEA0200231 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030700169 20020307 00169 EU 2002 3 7 QXEA0200232 1 20020209 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 58. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-04-04 PAGE 9 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030700170 20020307 00170 EU 2002 3 7 QXEA0200233 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION ON FRAME 14755 AND STRINGER 59. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030700171 20020307 00171 EU 2002 3 7 QXEA0200234 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION ON FRAME 14755 AND STRINGER 60. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030700172 20020307 00172 EU 2002 3 7 QXEA0200235 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- CRACKED CASTELLATION ON FRAME 15205 AND STRINGER 60. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01. 2 L 7 2 4F RT A20EU 2002030700173 20020307 00173 NM 2002 3 7 QXEA0200292 1 20020216 A 3350 6050251 BATTERY BOMBDR DHC8 DHC8401 NM CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 411QX 4055 SEA- AFT CABIN EMERGENCY LIGHTS EXTINGUISH 10 SECONDS AFTER TURNED ON. REMOVED AND REPLACED BOTH AFT EMERGENCY POWER SU PPLY BATTERIES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002030700174 20020307 00174 NM 2002 3 7 QXEA0200293 1 20020217 A 5210 NUT BOMBDR DHC8 DHC8401 NM PAX DOOR LOOSE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 413QX 4060 SEA- ONCE MAIN CABIN DOOR IS UNLOCKED IT IS DIFFICULT TO PUSH OPEN AND OUT. TIGHTENED JAMB NUT ON ROD END. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2002030700175 20020307 00175 NM 2002 3 7 QXEA0200297 1 20020219 A 5280 SKIN BOMBDR DHC8 DHC8401 NM LT MLG DOOR PUNCTURED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 PDX - LEFT AFT GEAR DOOR ON THE LEFT NACELLE HAS A .5 INCH PUNCTURE IN OUTER SKIN COMPOSITE. REPAIRED GEAR DOOR IAW EA 6-52-130. 2 H 7 2 4T RT A13NM 2002030700176 20020307 00176 NM 2002 3 7 QXEA0200298 1 20020217 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 353PH 496 PDX- NR 2 EMERGENCY LIGHTING FLOOR TRACK WILL NOT ILLUMINATE. REPLACED DEFECTIVE LIGHTING TRACK. OPERATIONAL CHECK GOO D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002030700177 20020307 00177 EA 2002 3 7 QXEA0200301 1 20020223 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR OUT OF ADJUST A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 606QX 10023 BOI - AIRCRAFT RETURNED TO FIELD WHEN SERVICE DOOR CAUTION ILLUMINATED IN FLIGHT. MAINTENANCE ADJUSTED THE SERVICE DOOR PROXIMITY SENSOR IAW AMM 52-70-06. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002030700178 20020307 00178 NM 2002 3 7 QXEA0200303 1 20020225 A 5270 SENSOR BOMBDR DHC8 DHC8401 NM CARGO DOOR MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 401QX 4031 MSO - DEPARTING MSO TO SEA, IN CLIMB THROUGH 12,000 FT, THE FORWARD CARGO DOOR MASTER WARNING LIGHT ILLUMINATED. AIRCRA FT RETURNED TO FIELD. MAINTENANCE INSPECTED THE FORWARD CARGO DOOR. CYCLED DOOR HANDLE AND WARNING LIGHTS EXTINGUISHED . AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002030700179 20020307 00179 2002 3 7 QXEA0200317 4 20020225 A 6122 8210161E GOVERNOR DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE MALFUNCTIONED A QXEA A UNSCHED LANDING R F PARTIAL RPM/PWR LOSS FLT CONT AFFECTED CL CLIMB 1 NM 09 365PH 7230 3235 526 PDX - AT ROTATION NR 2 ENGINE ONLY INDICATED 980 RPM, WITH CONDITION LEVER AT MAX, FUEL FLOW WAS ALSO LOW. NOTICEABLE Y AW WITH UNEVEN POWER. RETURNED TO FIELD WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 PROP OVERSPEED GOVERNOR. OPERATIO NAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002030800003 20020308 00003 NM 2002 3 8 920WA0001 1 20020303 A 3350 1000679 BATTERY PACK BOEING 737 737236 1384476 NM A PIDA K NONE O OTHER UK UNKNOWN 1 SO 05 920WA 21791 Emergency exit light at left rear door inop. R&R battery pack. 2 L 7 2 4F RT A16WE 2002030800004 20020308 00004 NM 2002 3 8 SWAA020491 1 20020306 A 2612 W24209022 WIRE BOEING 737 7372H4 138448C NM COCKPIT DISCONNECTED A SWAA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 091SW 22963 FIRE WARNING BELL CUTOUT LIGHT FLICKERED IN FLIGHT. FOUND WIRE DISCONNECTED AT NR 1 FIRE WARNING BELL CUTOUT SWITCH, RE CONNECTED WIRE. OPS CK OK PER MM. 2 L 7 2 4F A16WE 2002030800005 20020308 00005 NM 2002 3 8 SWAA020493 1 20020306 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED 1/4D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2002030800006 20020308 00006 NM 2002 3 8 SWAA020494 1 20020305 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS 4, 11, 14, 15, 17, 18 AND 19. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002030800007 20020308 00007 NM 2002 3 8 SWAA020496 1 20020305 A 2731 65C26384 TAB BOEING 737 737317 138447P NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED SERVICE CHECK, FOUND RT ELEVATOR TAB HAS EXCESSIVE PLAY AT HINGE POINTS. REMOVED AND REPLACED RT ELEVA TOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002030800008 20020308 00008 NM 2002 3 8 SWAA020497 1 20020305 A 2731 65C26384 TAB BOEING 737 737317 138447P NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED SERVICE CHECK, FOUND LT ELEVATOR TAB HAS EXCESSIVE PLAY AT HINGE POINTS. REMOVED AND REPLACED LT ELEVA TOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002030800009 20020308 00009 NM 2002 3 8 SWAA020498 1 20020305 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002030800010 20020308 00010 NM 2002 3 8 SWAA020499 1 20020305 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED (2 EA) AT BS 360, BETWEEN STR 7L AND STR 8L AND BETWEEN STR 7R AN D STR 8R. REPAIRED FRAME PER BFG ER. 2 L 7 2 4F RT A16WE 2002030800011 20020308 00011 EU 2002 3 8 MALA020182 1 20020307 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU DEFECTIVE A MALA K NONE O OTHER TX TAXI/GRND HDL 1 GL 15 437XJ 340B437 During test of Emergency lighting System JC #335003, Maintenance found several lights Inop under no power conditions. F ound Power supply 20LN PN 3301-51 SN/2192 at fault. Removed and replaced Power Supply PN 3301-51, SN ON 1370, SN OFF 2 192. . 2 L 7 2 4T RT A52EU 2002030800012 20020308 00012 NM 2002 3 8 SABA020032 1 20020307 A 3232 864202 SWITCH DHAV DHC8 DHC8102 2809003 NM NSE WHEEL WELL FAILED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 882CC 168 Aircraft 882 on flihgt 5025 from CLT to TLH. After takeoff when the landing gear was retracted the nose gear door cauti on light remained on. The gear was extended and aircraft returned to CLT and landed with no other problems. No emergen cy was declared. Maintenance removed and replaced the nose gear door sensor switch. Aircraft was jacked and gear cycle d. System check was good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002030800014 20020308 00014 2002 3 8 372PA0003 4 20020307 A 2210 AUTOPILOT SYS BOEING 737 737306 NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 372PA 23546 V-nav disconnects in flight uncommanded will not engage. 2 L 7 2 4F RT A16NE 2002030800022 20020308 00022 NM 2002 3 8 CALA0200122 1 20020306 A 5711 SPAR CAP BOEING 737 7373T0 1384582 NM RW REAR SPAR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A 1/2" CRACK AT HOLE IN SPAR CAP AT R/H WING MLG BEAM ATTACH FITTING. REPAIRED IAW ECRA 5740-02000. THE ITEM WAS PLACED ON DIP TO PERFORM AN HFEC INSPECTION ON THE R/H WING REAR SPAR AT MLG BEAM ATTACH FITTING AT THE LOCATI ON REFERENCED IN ECRA 5740-02000. THE INSPECTION IS TO BE PERFORMED AT "C" CHECK INTERVALS OR AT 4500 FLIGHT CYCLES AND ANY CRACK FOUND MUST BE REPAIRED. 2 L 7 2 4F RT A16WE 2002030800023 20020308 00023 NM 2002 3 8 CALA0200123 1 20020306 A 2560 ACREM1A MEGAPHONE ACR BOEING 737 737924 13848A1 NM AFT FA STA INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 75410 30127 THE LANYARD ACTIVATED "WAILER" FUNCTION OF THE AFT FLIGHT ATTENDANT POWER MEGAPHONE WAS FOUND INOPERATIVE WHEN TESTED. T HE MEGAPHONE WAS REMOVED AND REPLACED. FUNCTIONAL CHECKS PER AMM TASK 25-64-00-710-801 WERE GOOD. 2 L 7 4 4F RT A16WE 2002030800024 20020308 00024 NM 2002 3 8 CALA0200124 1 20020307 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 1040 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A 1/2" CRACK IN WEB AT LIGHTENING HOLE AFT OF STA 1040 AND I/B OF TAIL COMPARTMENT ACCESS. A REPAIR WAS INSTALLED IAW ECRA 5320-01768. 2 L 7 2 4F RT A16WE 2002030800025 20020308 00025 NM 2002 3 8 CALA0200125 1 20020307 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A 1.25" CRACK IN C-2 DOOR INNER SKIN AT AFT LOWER CORNER. THE SKIN WAS REPAIRED IAW ECRA 5230-01650. 2 L 7 2 4F RT A16WE 2002030800027 20020308 00027 EU 2002 3 8 02FDEA00187 1 20020306 A 7830 PILOT VALVE AIRBUS 310 A310203 3930313 EU GE CF6 CF680A3 30025 NE NR 1 T/R FAULTY A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 407FE 254 585103 ON CLIMB AFTER GEAR RETRACTION NR 1 ENG REVERSE UNLOCK LIGHT CAME ON. REMOVED AND REPLACED NR 1 ENG DIRECTIONAL PILOT V ALVE AND PDU POS SWITCH MODULE PER MM 78-31-06-02-B, 78-32-09-04-B. 2 L 7 2 4F 4 F RT A35EU E13NE 2002030800028 20020308 00028 NM 2002 3 8 2002UALA00311 1 20020218 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY CEILING LIGHT AT RIGHT HAND AISLE BETWEEN LAV 102 AND CLOSET IS INOP. THIS DISCREPANCY WAS FOUND DURING THE C OURSE OF A MAINTENANCE CHECK, (B-CK). RELAMPED CEILING LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2002030800029 20020308 00029 NM 2002 3 8 2002UALA00312 1 20020218 A 3397 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 UPPER DECK STAIR PATHWAY LIGHTING (GOING FROM LOWER DECK TO UPPER DECK) ARE INOP AT 4TH AND 6TH FROM THE TOP POSITIONS. THIS DISCREPANCY WAS FOUND DURING THE COURSE OF A MAINTENANCE CHECK, (B-CK). REPAIRED OPEN HARNESS. 2 L 7 4 4F 4 F RT A20WE E24NE 2002030800030 20020308 00030 NM 2002 3 8 2002UALA00313 1 20020218 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY CEILING LIGHTS ON LEFT HAND AISLE AT ROW 24, 34 & 61 ARE INOP. THIS DISCREPANCY WAS FOUND DURING THE COURSE O F A MAINTENANCE CHECK, (B-CK). RELAMPED CEILING LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2002030800031 20020308 00031 NM 2002 3 8 2002UALA00314 1 20020218 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY EXIT LIGHT INOP AT UPPER DECK STAIR CEILING. THIS DISCREPANCY WAS FOUND DURING THE COURSE OF A MAINTENANCE CH ECK, (B-CK). RELAMPED WITH P/N 1317 AND TESTED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002030800032 20020308 00032 NM 2002 3 8 2002UALA00315 1 20020218 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY EXIT LIGHT INOP IN CENTER AFT UPPER DECK CEILING PANEL. THIS DISCREPANCY WAS FOUND DURING THE COURSE OF A MAI NTENANCE CHECK, (B-CK). RELAMPED WITH P/N 1317 AND TESTED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002031500089 20020315 00089 NE 2002 3 15 2002UALA00316 2 20020224 A 7530 ACTUATOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE OUT OF RIG A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 606UA 21867 707506 AFTER T/O PROIR TO POWER REDUCTION LT ENG SURGED 1.3 TO 1.9 EPR FOR 30 SECONDS, THROTTLES STEADY, ALL NORM UNTIL TOP OF CLIMB, AT LEVEL OFF, THROTTLES STEADY, SMALL SURGE 15 SECONDS, LATER IN CRUISE SMALL OSCILLATIONS IN EPR FRM 1.28 TO 1.3 0. DIVERTED TO ORD. THE 3.0 BLEED ACTUATOR WAS TRIMMED FOR A SIMILAR DISCREPANCY. DURING TRIM, A PROBLEM WAS ENCOUNTE RED WITH THE ACFT WIRING FOR THE TRIM EQUIP. THE 3.0 BLEED ACTUATOR WAS FOUND OUT OF TRIM AGAIN. THE EVBC WAS ALSO FOU ND OUT OF TRIM. AN EXTERNAL WIRE HARNESS WAS USED FOR TRIMMING, DUE TO CONCERNS OF THE RELIABILITY OF ACFT WIRING. BOT H COMPONENTS WERE TRIMMED. THE 3.0 BLEED ACTUATOR AND EVBC WERE REPLACED PRECAUTIONARY. 2 L 7 2 4F 4 F RT A1NM E3NE 2002030800034 20020308 00034 NM 2002 3 8 2002UALA00319 1 20020226 A 5320 CHANNEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 AFT PIT U-CHANNEL FITTING ATTACHED TO SKIN CORRODED BETWEEN BODY STATION 1395-1404, STRINGER 35R AND 36R. MAJOR REPAIR ACCOMPLISHED. REPLACED U-CHANNEL. 2 L 7 2 4F 4 F RT A1NM E24NE 2002030800035 20020308 00035 NM 2002 3 8 2002UALA00322 1 20020228 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 928UA 26651 FORWARD EXTERNAL SKIN AT NUMBER 2 VHF ANTENNA IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. ACCOMPLISHED DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030800037 20020308 00037 NM 2002 3 8 2002UALA00323 1 20020228 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 928UA 26651 STATION 188 FRAME AT STRINGER 17L IS CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030800038 20020308 00038 NM 2002 3 8 2002UALA00324 1 20020228 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 928UA 26651 FORWARD PIT CARGO DOOR OPENING AFT FRAME HAS A CRACK IN EDGE OF SKIN AT LOWER END ABOVE STRINGER 25R. MAJOR REPAIR ACCO MPLISHED. INSTALLED FILLER AND DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030800039 20020308 00039 NM 2002 3 8 2002UALA00325 1 20020228 A 5320 FLOOR SUPPORT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 928UA 26651 DOOR 2R FLOOR SUPPORT CORRODED AT STATION 340. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030800040 20020308 00040 NM 2002 3 8 2002UALA00326 1 20020228 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 928UA 26651 RIGHT HAND STATION 188 FRAME AT STRINGER 17R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002030800041 20020308 00041 NM 2002 3 8 2002UALA00327 1 20020226 A 3350 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 106UA 26474 FORWARD ASSEMBLY (RIGHT SIDE) EXTERIOR EMERGENCY LIGHT (FORWARD BULB) IS INOP. THIS DISCREPANCY WAS FOUND DURING THE CO URSE OF A MAINTENANCE CHECK, (B-CK). RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002030800042 20020308 00042 NM 2002 3 8 OZIA200241001 1 20020302 A 3246 AHA22273 BRAKE ASSY DORNER DO32 DO328300 NM #1 ON MLG FROZEN A OZIA K NONE O OTHER LD LANDING 1 CE 05 410Z 1194 3125 Pilot reported LH main wheel locked upon landing and ruined the tire. Upon removal of #1 wheel/tire assembly (MLG), brak e was found to be locked up/seized. Further inspection revealed brake frozen from residual slush/snow. 2 H 7 2 4T RT A55NM 2002030800043 20020308 00043 NM 2002 3 8 CA020201005 1 20020122 A 5610 17180003 WINDOW DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE COCKPIT FAILED W B EMER. DESCENT C D F.O.D. INFLIGHT SEPARATION CR CRUISE 1 CA (CAN) IN CRUISE AT FL240, PILOTS SIDE WINDOW OUTER PANE SHATTERED, DESCENT COMMENCED IMMEDIATELY. THE DEPARTING OUTER P LY OF THE CAPTAIN'S SIDE WINDOW IMPACTED THE LT PROP, NR 2 BLADE. ALSO THE INBOARD DEICE BOOT, INTAKE BOOT HAVE SMALL C UTS. PILOTS SIDE WINDOW AND LT PROP NR 2 BLADE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002030800044 20020308 00044 NM 2002 3 8 CA020201006 1 20020106 A 3230 465003 UPLOCK DHAV DHC8 DHC8* NM PWC 150 PW150A EA MLG WORN W O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 CA (CAN) DURING LDG DOWN SELECTION ONE MAIN GEAR WAS UNABLE TO EXTEND DOWN, EMERGENCY PROCEDURE USED, MAIN GEAR STILL UP, A LTERNATE EMERGENCY PROCEDURE USED, AIRCRAFT LANDED SAFELY - DUE TO NOSE GEAR'S HYDRAULIC POWER OFF, NO STEERING, AIRCRAF T PULLED TO HANGAR. INVESTIGATION FOUND DURING HANGAR TESTING THE R/H MLG FAILED TO EXTEND USING THE ALTERNATE EXTENSION METHOD. WEAR ON THE UP-LOCK HOOK WAS FOUND. UPLOCK HAD ABOUT 3700 CYCLES. NEW LT AND R/H UPLOCK ASSEMBLIES AND A NEW RT ROLLER WERE INSTALLED AND A TEST FLIGHT WAS CARRIED OUT SERVICEABLE.BOTH UPLOCKS S/N 0012/99 (R/H) & S/N 0002/99 (LT)UP LOCK P/N 46500-3ROLLER P/N 46152-1 2 H 7 2 4T 4 T RT A13NM E00062EN 2002030800045 20020308 00045 NM 2002 3 8 2002UALA00328 1 20020227 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN CONTAMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 ALL SEAT AISLE EEL LIGHTS INOP IN B-ZONE (BOTH SIDES). THIS DISCREPANCY WAS FOUND DURING THE COURSE OF A MAINTENANCE CH ECK, (B-CK). CLEANED WATER FROM SIDEWALL EEL LIGHTS CONNECTIONS AND REINSTALLED. OPS CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002030800046 20020308 00046 GL 2002 3 8 CA020206001 2 20020120 A 7230 23065593 COMPRESSOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) A ONE INCH LONG CRACK WAS DISCOVERED BY MAINTENANCE PERSONNEL DURING A SCHEDULED EVENT NR 5 INSPECTION. THE CRACK WAS FOUND ON THE UPPER HALF OF THE WELD ON THE RIGHT SIDE OF THE COMPRESSOR SCROLL ASSEMBLY. WHEN THE AIRCRAFT WAS GROUN D RUN AIR WAS FELT ESCAPING FROM THE CRACKED AREA. THE AIRCRAFT WAS THEN DECLARED GROUNDED BY THE BASE ENGINEER. THE COM PRESSOR ASSEMBLY WAS REMOVED AND SHIPPED TO STANDARD AERO LTD. FOR REPAIR. 1 G 7 1 3U 3 U O H2SW E1GL 2002030800047 20020308 00047 EU 2002 3 8 CA020206002 1 20020204 A 6320 4638302023 BEARING BOLKMS 105 BO105CBS 5626008 EU M/R GEARBOX SPALLED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) OUTER RACE AND TWO BALLS EXHIBIT SEVERE PEELING.TRUE INDICATION BY MAGNETIC PLUG.INTERNAL OIL PUMP FILTER CAPTU RED NUMEROUS METAL FRAGMENTS.BEARING CAGE SEVERLY WORN AND SPREAD THROUGH OUT THE TRANSMISSION AS POWDER. 1 G 7 2 3U NC H3EU 2002030800048 20020308 00048 NM 2002 3 8 2002UALA00329 1 20020225 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 OVERWING EMERGENCY ESCAPE LIGHTS THE FORWARD BULB IN THE MOST AFT ASSEMBLY ON THE RIGHT HAND SIDE IS INOP. THIS DISCREP ANCY WAS FOUND DURING THE COURSE OF A MAINTENANCE CHECK, (B-CK). RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002030800050 20020308 00050 GL 2002 3 8 CA020206004 2 20020116 A 7230 COMPRESSOR BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) ON CROSS-COUNTRY PATROL FLT PILOT NOTICED THAT HE HAD TO REFUEL A/C AT LOCATION FROM WHICH HE NORMALLY HAD SUFFI CIENT FUEL TO CONTINUE ON NEXT LEG. HE THEN NOTICED UNUSUALLY HIGH FUEL CONSUMPTION ON RETURN FLT TO HOME B ASE. PILOT H AD MANY HRS FLYING SAME A/C ON SAME ROUTE AND BECAME CONCERNED THAT FAULT. NO FUEL LEAK FOUND AND AFTER NORMAL TROUBLES HOOTING PROCEEDURES WERE CARRIED OUT IT DETERMINED THAT PROBLEM COULD HAVE DEVELOPED FROM ENGINE COMPRESSOR HAVING BEEN REPLACED ONLY 25.7 HRS PREVIOUS. ENGINE COULD ALSO NOT ACHIEVE SATISFACTORY POWER CHECK. COMPRESSOR ASSY REPL&ALL PARAME TERS RETURNED TO NORMAL. REMOVED COMPRESSOR FOR TESTING. 1 G 7 1 3U 3 U H2SW E1GL 2002030800051 20020308 00051 WP 2002 3 8 CA020206005 1 20020205 A 2610 356080765 FIRE DETECTOR CVAC 580 580 2422806 WP NR 2 ENGINE MALFUNCTIONED W F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA (CAN) NR 2 ENG ZONE 1 FIRE WARNING ILLUMINATED. ENGINE SECURED IAW ENG FIRE CHECK LIST. ONE FIRE BOTTLE DISCHARGED. AI RCRAFT DIVERTED TO MAINTENANCE BASE. 2 L 7 2 4T RT 2002040300102 20020403 00102 2002 4 3 2002UALA00330 4 20020301 A 3420 CIRCUIT CARD HONEYWELL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ADIRU FAILED A UALA J A DUMP FUEL UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 777UA 97100178 26916 DUMPED FUEL AND DIVERTED TO LHR WITH ADIRU INOP PRIOR TO RVSM/CLASS 2 AIRSPACE. EICAS STATUS MESSAGES AOA VANE, L STATI C ADM, L PITOT ADM AND ADIRU. ADIRU REPLACED AND SENT TO HONEYWELL FOR TEST AND REPAIR. PRELIMINARY FINDINGS SHOW FAIL URES ON A8 629 INTERFACE CARD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002030800054 20020308 00054 SW 2002 3 8 CA020208003 1 20020131 A 6210 2060101543 WASHER BELL 206011100021 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R HEAD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA JILM57064 (CAN) 2060101543 WASHER WAS USED ON A BLADE BOLT WITH A NAS1022A14 NUT. THE NUT IS A SMALLER NUT AND TENDS TO COVER O NLY 2/3 OF THE AREA OF THE WASHER. THE TORQUE REPETITIVE TORQUE CYCLES OVER TIME AND THE CUPPING OF THE WASHER CAUSED IT TO CRACK IN 3 PLACES AND BREAK. 1 G 7 1 3U 3 U H2SW E4CE 2002030800056 20020308 00056 EA 2002 3 8 CA020211002 1 20020201 A 5610 601R3303310 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W K NONE O OTHER TX TAXI/GRND HDL 1 CA (CAN) RT WINDSHIELD CRACKED DURING GROUND HANDLING. REMOVED AND REPLACED WINDSHIELD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002030800057 20020308 00057 EA 2002 3 8 SWIA200210594 1 20020124 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 410SW 7066 NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. CREW NOTED CHUNK OF ICE FELL FROM GEAR WHEN DOORS OPENED. PERFORMED NOSE GE AR RETRACTION TEST PER MM 32-30-00. NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A21EA 2002030800058 20020308 00058 EA 2002 3 8 CA020211005 1 20020201 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) DURING FLIGHT, IN CRUISE AT FL350, THE MIDDLE PLY OF THE LT WINDSHIELD CRACKED. PILOTS APPLIED QRH EMERGENCY PROCE DURE AND THE FLIGHT WAS DIVERTED. AIRCRAFT LANDED SAFELY. 2 L 7 2 4F 4 F RT A21EA E15NE 2002030800059 20020308 00059 EA 2002 3 8 CA020211006 1 20020201 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W K NONE O OTHER TX TAXI/GRND HDL 1 CA (CAN) CAPTAIN'S SIDE WINDOW CRACKED ON TAXI OUT. REMOVED AND REPLACED RT SIDE WINDOW IAW 56-12-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002030800060 20020308 00060 EA 2002 3 8 CA020211007 1 20020204 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN DETECTED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA (CAN) ON APPROACH, AFTER CREW STARTED APU AND SWITCHED BLEEDS, SMOKE TOILET MESSAGE CAME ON. SMOKE ALARM ALSO SOUNDED FOR SEVERAL MINUTES. F/A REPORTED HAZE FROM ROW 8 AFT. BY THE TIME THE CREW LANDED, HAZE HAD DISAPPEARED. LOCAL MAIN TENANCE INSPECTED THE BLEED LINES AND CHECKED SYSTEM. NO DUPLICATION OF PROBLEM. ON RETURN FLIGHT TO ATL, THE SAME ME SSAGE APPEARED AFTER APU STARTED AND BLEEDS SWITCHED. BLEEDS SWITCHED BACK TO ENGINES, AND MESSAGE EXTINGUISHED. MAIN TENANCE CHECKED THE COALESCER BAGS, ACM'S, GALLEY FAN, LAV FAN, SMOKE DETECTOR, LCV. NO SIGNS OF OIL OR OTHER LEAK AGE. ENGINE AND APU RUNS PERFORMED. DECISION MADE TO REPLACE APU. IT IS CURRENTLY ON MEL AND WILL BE REPLACED AS SOON 2 L 7 2 4F 4 F RT A21EA E15NE 2002030800061 20020308 00061 EA 2002 3 8 CA020211008 1 20020206 A 2822 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BOOST PUMP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 19724 (CAN) DURING THE NDT INSPECTION OF THE FUEL BOOST PUMP SCREW HOLES 3 CRACKS WERE FOUND. REPAIR IN ACCORDANCE WITH REO 601R-57-21-164. 2 L 7 2 4F 4 F RT A21EA E15NE 2002030800062 20020308 00062 EA 2002 3 8 CA020211009 1 20020207 A 5610 NP13932110 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) THE WINDSHIELD INSTALLED WAS A POST SERVICE BULLETIN WINDSHIELD. RT WINDSHIELD CORE PLY CRACKED IN CRUISE. CREW INITIATED DESCENT TO 10,000 FEET. (NO EMERGENCY DESCENT). AIRCRAFT LANDED IN BARCELONA, SPAIN AS SCHEDULED. REMOVED AN D REPLACED WINDSHIELD.AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002030800063 20020308 00063 EA 2002 3 8 CA020211010 1 20020208 A 3234 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MLG FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) LANDING GEAR WOULD NOT EXTEND FOR LANDING. HAD TO PERFORM EMERGENCY GEAR EXTENSION. AIRCRAFT DECLARED AN EMERGEN CY. UNEVENTFUL LANDING TOOK PLACE. MAINTENANCE REPLACED MAIN LANDING GEAR SELECTOR VALVE. OPS AND LEAKS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002030800064 20020308 00064 EA 2002 3 8 CA020211011 1 20020211 A 2710 6224404001 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AILERONS FAILED W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 CA 13785 (CAN) AP TRIM RWD CAUTION POSTED ON EICAS. DISCONNECTED AP AND FOUND AILERON SYSTEM JAMMED. OVERPOWERED SYSTEM ACC. CHEC KLIST AFTER SEVERAL ATTEMPTS. SUDDENLY SYSTEM GOT FREE AGAIN. VISUALLY INSPECTED AILERON SYSTEM CABLES AND PULLEYS FOR S IGN OF JAMMING NO FINDINGS. REPLACED AILERON SERVO ACTUATOR IAW AMM 22-11-21. PERFORMED OPS TEST SATISFACTORY. 2 L 7 2 4F 4 F RT A21EA E15NE 2002030800065 20020308 00065 EA 2002 3 8 CA020211012 2 20020130 A 7530 3029267 AIR FILTER PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA ENGINE FAILED W O OTHER R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) AFTER ENGINE START, ENGINE STABILIZE AT 52 PERCENT NG IDLE. SUDDENLY, WITHOUT MOVING ANY CONTROLS, NG WENT DOWN & STUCK AT 40 PERCENT. NG ON FCU MIN FUEL FLOW. WAS UNABLE TO HAVE CONTROL ON ENGINE. ONLY WAY TO REGAIN CONTROL ON E NGINE TO STOP IT & TO RESTART & AFTER THAT PROBLEM INTERMITTENT. AFTER INVESTIGATION, FOUND SMALL ROUND OF GLUE, LIKE PASTILLE IN P3 FILTER. ANY WAY TO TAKEOFF PASTILLE, SO WE THINK THAT IT WAS PART OF FILTER. SO, PASTILLE SOME TIME WEN T UP & OBSTRUCTED P3 LINE ON PT6'S, WHEN YOU LOOSE P3 AIR, YOU LOOSE YOUR CONTROL ON ENGINE & FCU GO TO HIS MIN FUEL FLO W SETTING. 1 L 7 2 3T 4 T A8EA E4EA 2002030800067 20020308 00067 NE 2002 3 8 CA020211014 2 20020113 A 7270 BR715DTA01601 BYPASS JACKET BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE COWL DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) A/C CAME IN FOR OVERNIGHT WITH NO MAINT PROBLEMS REPORTED. DURING OVERNIGHT SERVICE CHECK, DAMAGE NOTED ON BYPASS DUCT & CORE ENGINE. INITIAL INSPECTION FOUND DAMAGE IN BPD (BYPASS DUCT) AFT LOOKING FWD. AT 9 TO 2 O'CLOCK POS FROM BPD STATOR VANES TO END OF BPD. MOSTLY INNER BPD FIBRE GLASS LINER HAD BURNT AWAY, EXPOSING BPD HONEYCOMB SECTIONS. ALSO HE AVY DAMAGE TO UPPER SPLITTER FAIRING & WIRE BUNDLE DAMAGE. FURTHER T/S UNABLE TO LOCATE SOURCE OF FIRE: OPENED UP UPPER COWLING & INSP 5TH & 8TH STAGE BLEED DUCTS FOR DAMAGE, EVERYTHING FOUND IN GOOD ORDER. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002030800076 20020308 00076 EU 2002 3 8 CA020215005 1 20020129 A 5532 D5537002600400 STRUCTURE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE VERTICAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) VERTICAL STAB LEADING EDGE PANEL 322B1 CRACKED APPROXIMATELY 5 INCHES UP FROM LOWER EDGE. LT SIDE. THE DAMAGE IS W ITHIN REPAIR LIMITS WILL BE REPAIRED AS PER SRM 55-30-00, PA 200, OR REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2002030800078 20020308 00078 EU 2002 3 8 C2XA02IA052 1 20020301 A 3230 141FL01D3 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU NOSE GEAR MISALIGNED A C2XA O OTHER N FALSE WARNING AP APPROACH 1 SW 27 97841 280 IAH - Crew reported that on approach that the nose landing gear had an unlock indication that flashed 8 to 10 times with several lound bangs. Maintenance performed an inspection of the gear and did not find any defects. The problem reoccure d on flight 3604 on the same date. Maintenance adjusted the #1 nose landing gear proximity switch. The aircraft was then approved for return to service. 2 H 7 2 4T RT A53EU 2002030800079 20020308 00079 NM 2002 3 8 UPS02237796 1 20020207 A 5310 SKIN BOEING 727 72725C 138400H NM LT FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE:C LT FUSELAGE SKIN HAS CRACK STARTING AT FASTENER CUT OUT BS 254 STR 10L CRACK DOES NOT NEED STOP DR ILL IT RUNS FROM FASTENER HOLE TO EDGE OF SKIN, INSTALLED DOUBLER REPAIR AT LT FUSELAGE. BS 254 STR 10L AS PER B727 SRM 53-30-3 MATERIAL USED 2024-T3 .080 LOT NO 415602 P.O. #83112437 DIMENSION 9.5" X 3.5" 2 L 7 3 4F A3WE 2002030800080 20020308 00080 EA 2002 3 8 SWIA200210621 1 20020130 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 410SW 7066 GEAR DISAGREE ON TAKEOFF. NOSE GEAR WOULD NOT COME UP. INSPECTED NOSE GEAR TORQUE LINKS, PROX SWITCHES AND STEERING. NO DEFECTS NOTED. JACKED A/C NOSE, SWUNG NOSE LANDING GEAR WITH NO DEFECTS NOTED. GEAR OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002030800081 20020308 00081 SO 2002 3 8 SWIA200210622 1 20020201 A 3010 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO DEICE SYSTEM FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 294SW 120321 RIGHT INBOARD STAB DEICE BOOT FAILS BOTH TIMERS 1 & 2 DURING THE CLIMB. REPLACED RT INBOARD STAB PRESSURE SWITCH. RAN SYSTEM. BOOTS LEAK CHECK GOOD. SYSTEM OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002030800082 20020308 00082 SO 2002 3 8 SWIA200210624 1 20020204 A 7330 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 393SW 120330 EEC AURAL WARNING ON TAKEOFF ROLL. ABORTED PER SOP. INSPECTED BOTH EEC SYSTEMS. RAN AIRCRAFT. EEC'S OPERATED NORMALL Y AT VARIOUS POWER SETTINGS. NO DISCREPANCIES NOTED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002030800083 20020308 00083 2002 3 8 SWIA200210626 4 20020126 A 3415 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 188SW 120039 HIGH SPEED AURAL WARNING ACTIVATED AT 80 KTS ON TAKEOFF ROLL. OPERATED TEST PER MM 34-12-01. NO DISCREPANCIES NOTED ON GROUND. 2 L 7 2 4T RT A31SO 2002030800084 20020308 00084 GL 2002 3 8 CA020215009 1 20020204 A 5520 MS90354465 RIVET 100551005100 BOMBDR BD700 BD7001A10 1390006 GL RROYCE BR700 BR700710A220 09500 NE HORIZONTAL STAB JAMMED W A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CA (CAN) DURING A/C 20002 FLT 26, AM ELEVATOR BINDING EXPERIENCED BY CREW DURING HANDLING TESTS. AIRCREW TOOK NECESSARY P RECAUTIONS TO EVALUATE FLT CONTROL AVAILABILITY TO PERFORM SAFE LDG W/O HAVING TO DISCONNECT ELEVCCT. FOLLOWING AIR ASSE SSMENT, CREW PROCEEDED TO BURN OFF FUEL TO GET WITHIN MLW & CAME IN FOR SAFE & UNEVENTFUL LDG. A/C QUARANTINED BY QA UPO N ARRIVAL & THOROUGH INSP PERFORMED BY BFTC ENGINEERING AND QUALITY CNTL. INSP RESULTS REVEALED THAT PIECE OF BLIND RIVE T JAMMED BETWEEN GAIN CHANGER OUTPUT CNTL ROD CLEVIS&GAIN CHANGER OUTPUT FORK LEVER.THE BLIND RIVET REMVD&GAIN CHANGER O UTPUT FORK LEVER FOUND TO BE GOUGED AS RESULT OF FOULING. 2 L 7 2 4F 4 F RT T00003NY E00061EN 2002030800086 20020308 00086 SO 2002 3 8 SWIA200210629 1 20020205 A 2731 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO ELEVATOR TAB OUT OF ADJUST A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 226SW 120296 TAKEOFF TRIM SOUNDED ON TAKEOFF ROLL. ABORTED TAKEOFF. TRIM WAS SET PROPERLY WHEN WARNING SOUNDED. ADJUSTED LEFT AND RIGHT TRIM TAB PROX SWITCHES. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002030800087 20020308 00087 NM 2002 3 8 0200576623 1 20020303 A 2530 TERMINAL BOEING 747 747251B 1384892 NM GALLEY DOOR 2 BROKEN A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 623US 21705 DURING FLIGHT, A BURNING SMELL EMITTED FROM GALLEY DOOR 2. PULLED CIRCUIT BREAKERS FOR AFT COFFEEMAKER AND HOT PLATE AND SMELL DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED COFFEEMAKER AND HOT PLATE GROUND WIRE TERMINAL. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002030800088 20020308 00088 EA 2002 3 8 SWIA200210631 1 20020204 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 589SW 7072 FLAPS FAILED 20 DEGREES AFTER T/O. RETURNED TO FIELD. CHECKED FLAPS ALIGNMENT. NO TWIST. RESET CB 1-F4 & CB 2-F4. R AN FLAPS TO 45 DEGREES AND BACK TO 0 DEGREES. NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A21EA 2002030800089 20020308 00089 2002 3 8 SWIA200210640 4 20020208 A 2210 6229968001 DAMPER CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 NM 07 442SW 84 84 7609 NR 2 YAW DAMPER WON'T STAY ENGAGED. REMOVED AND REPLACED NR 2 YAW DAMPER. OPS CHECKS CAT II GOOD IAW 22-22-01. 2 L 7 2 4F RT A21EA 2002030800091 20020308 00091 SO 2002 3 8 SWIA200210618 1 20020201 A 2731 TRIM TAB EMB 120 EMB120ER 3260203 SO ELEVATOR OUT OF ADJUST A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 NM 07 187SW 120037 ON DESCENT INTO EKO, TRIM FAIL WARNING WENT OFF. AFTER A/P DISCONNECT, AIRCRAFT PITCHED UP AT 230 KTS WITH ELEVATOR TRI M AT FULL NOSE DOWN STOP. AIRCRAFT NOT UNDER NORMAL CONTROL UNTIL SLOWED BELOW 200 KTS. ADJUSTED RT ELEVATOR TRIM TAB AS REQUIRED TO RECEIVE TRIM EXPECTED. 2 L 7 2 4T RT A31SO 2002030800092 20020308 00092 SO 2002 3 8 SWIA200210619 1 20020131 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO CARGO DOOR OUT OF ADJUST A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 188SW 120039 CARGO DOOR LIGHT CAME ON DURING TAKEOFF (ABORTED). CARGO DOOR MICRO SWITCH FOUND TO BE OVER CENTERED. ADJUSTED SWITCH, OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002030800093 20020308 00093 2002 3 8 SWIA200210620 4 20020202 A 3444 6222855011 TRANSCEIVER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 406SW 4246 4246 7030 ON FINAL AT ABOUT 100 FT AGL, AIRCRAFT STARTED TO ROLL LEFT THEN RIGHT, THEN GROUND SPOILER DEPLOY CAUTION MESSAGE APPEA RED ON EICAS. AT TOUCHDOWN, GLD UNSAFE APPEARED ON EICAS. BOTH MESSAGES CLEARED AFTER ROLL OUT. REMOVED AND REPLACED NR 2 RADIO ALTIMETER TRANSCEIVER. OPS TESTS GOOD. AC RELEASED FOR CAT II OPERATION. S/N ON DBLG, S/N OFF 8755. 2 L 7 2 4F RT A21EA 2002030800094 20020308 00094 SO 2002 3 8 SWIA200210623 1 20020131 A 3150 80055711 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 234SW 3983 3983 120308 ON TAKEOFF WITH TRIM SET AT 50 PERCENT, GOT A TAKEOFF AURAL WARNING TRIM. ABORTED TAKEOFF. PERFORMED FUNCTIONAL TEST O F SENSORS. OPS CHECK GOOD. REPLACED AURAL WARNING UNIT. OPS CHECK GOOD. S/N ON 0045, S/N OFF 0225. 2 L 7 2 4T RT A31SO 2002030800095 20020308 00095 SO 2002 3 8 SWIA200210625 1 20020124 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PAX DOOR LOOSE A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 186SW 120034 FORWARD CABIN DOOR LIGHT ON TAKEOFF. ABORTED TAKEOFF. INSPECTED/RECYCLED DOOR. LIGHT DID NOT ILLUMINATE AGAIN. FOUND UPPER MICRO SWITCH LOOSE. ADJUSTED SWITCH AND SECURED. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002030800096 20020308 00096 SO 2002 3 8 SWIA200210627 1 20020130 A 2133 OUTFLOW VALVE EMB 120 EMB120ER 3260203 SO CABIN PRESSURE DIRTY A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 580SW 120348 AIRCRAFT WILL NOT PRESSURIZE, MANUAL OR AUTO. WARMED AIRPLANE, CLEANED OUTFLOW VALVES. TEST RUN AND OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2002030800097 20020308 00097 EA 2002 3 8 SWIA200210628 1 20020130 A 7603 GEARBOX CNDAIR CL600 CL6002B19 1900309 EA RT THROTTLE FAULTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 493SW 7450 RT REV CAUTION ICON ON N1 GAUGE IN FLIGHT WITH REV UNSAFE CAUTION MESSAGE AFTER LIFTOFF. REMOVED AND REPLACED RT ENGINE S THROTTLE GEAR BOX ASSEMBLY. 2 L 7 2 4F RT A21EA 2002030800098 20020308 00098 SO 2002 3 8 SWIA200210630 1 20020204 A 3260 UPLOCK SWITCH EMB 120 EMB120ER 3260203 SO RT MLG LOOSE A SWIA A UNSCHED LANDING N E FALSE WARNING VIBRATION/BUFFET CL CLIMB 1 NM 07 250YV 120250 RIGHT MAIN GEAR INTRANSIT LIGHT ON AND DOOR VIBRATION ON RIGHT MAIN GEAR. RETURNED TO FIELD. INSPECTED, FOUND LOOSE JA M-NUT ON RIGHT GEAR UPLOCK PLUNGER. ADJUSTED AND SECURED NUT. SWUNG GEAR NUMEROUS TIMES. ALL GEAR SWINGS SATISFACTORY . 2 L 7 2 4T RT A31SO 2002030800099 20020308 00099 NE 2002 3 8 SWIA200210632 3 20020202 A 6140 SELOC29DH INDICATOR EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE COCKPIT FAILED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 251YV 4417 4417 120251 RIGHT NP GAUGE FAILED DURING TAKEOFF ROLL. BOTH ANALOG AND DIGITAL. REMOVED AND REPLACED RT NP INDICATOR. OPS CHECK G OOD. P/N ON SEL-OC29DH, S/N ON 97C. 2 L 7 2 4T RT A31SO 6 C P11NE 2002030800100 20020308 00100 SO 2002 3 8 SWIA200210633 1 20020208 A 2750 3075001007 FCU EMB 120 EMB120RT 3260202 SO E/E BAY FAULTY A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 137H 120137 CREW REPORTS OUTBOARD FLAPS DO NOT RETRACT WITH ASSOCIATED DISAGREEMENT. REMOVED AND REPLACED FCU AND ANNUNCIATOR. OPS CHECK GOOD IAW MM 27-50-05 & 27-50-06. (FCU) S/N OFF 0255. (ANNUNCIATOR) P/N ON 306900-1017, S/N OFF 0142. 2 L 7 2 4T RT A31SO 2002030800101 20020308 00101 2002 3 8 SWIA200210634 4 20020207 A 3415 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 188SW 120039 TRIPLE CHIME HIGH SPEED WARNING ON TAKEOFF. ABORTED TAKEOFF. CHECKED BOTH AIRSPEED INDICATOR HIGH SPEED WARNINGS AND F OUND BOTH TO BE OPERATING AND NORMAL. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002030800102 20020308 00102 SO 2002 3 8 SWIA200210635 1 20020206 A 6123 RELAY EMB 120 EMB120ER 3260203 SO INDICATOR FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 212SW 120276 ABORTED TAKEOFF DUE TO AUTOFEATHER AURAL WARNING AND NO GREEN ARMED LIGHT. SUBSEQUENT RUN UP PRODUCED NO GREEN ARMED LI GHT. REF WDM 61-23-00 REPLACED RELAY K0161 - ARMED INDICATOR RELAY. OPS CHECKS PER MM 61-23-26. AUTOFEATHER SYSTEM TE ST WITH ENGINE RUNNING AND WITH ENGINE NOT RUNNING. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002030800103 20020308 00103 SO 2002 3 8 SWIA200210636 1 20020205 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO FUEL DOOR OUT OF ADJUST A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 583SW 120351 SERVICE DOOR LIGHT INTERMITTENT ON TAKEOFF ROLL. ADJUSTED FUEL SERVICE DOOR SWITCHES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002030800104 20020308 00104 2002 3 8 SWIA200210637 4 20020207 A 3425 COMPUTER EMB 120 EMB120ER 3260203 SO E/E BAY MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 289YV 120289 DURING CLIMBOUT, YELLOW HEADING FLAGS ON CAPTAIN'S EHSI, FIRST OFFICER'S EHSI AND MFD. ATTEMPTED RESET TO NO AVAIL. RE INITIALIZED AHRS AFTER SHUTDOWN. NO FLAGS DISPLAYED. REORIENTED AHRS NR 1 AND NR 2. SYSTEM OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002030800105 20020308 00105 EA 2002 3 8 SWIA200210639 1 20020207 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 438SW 7574 FLAPS FAIL CAUTION MESSAGE UPON FLAP RETRACTION. FLAPS STUCK AT 8 DEGREES. COMPLIED WITH AD98-20-01. NO EVIDENCE OF F LAP DAMAGE AT THIS TIME. PERFORMED MAINTENANCE CALLED OUT IN FECU IAW CRJ MM TASK 27-51-10-220-802, 27-51-10-830-801 AN D 27-54-00-710-801. CHECKED AND ADJUSTED RIGGING OF THE BPSU. OPERATIONAL CHECK GOOD AT THIS TIME. ADJUSTED LEFT BPSU . 2 L 7 2 4F RT A21EA 2002030800107 20020308 00107 NM 2002 3 8 2002F00157 1 20020115 A 5712 RIB BOEING 737 7372H4 138448C NM LT WING CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND LEFT WING STATION 453 HAS A CRACKED RIB AT THE FORWARD VENT STRINGER FORWARD ATTACH BOLT. (M) 2 L 7 2 4F A16WE 2002030800108 20020308 00108 NM 2002 3 8 2002F00158 1 20020118 A 5311 FRAME BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 FOUND LEFT STATION 294.5 STRINGER 4L, INSIDE COCKPIT, FRAME IS CRACKED. (M) 2 L 7 3 4F A3WE 2002030800110 20020308 00110 NM 2002 3 8 2002F00160 1 20020114 A 5510 WEB BOEING 737 7372H4 138448C NM HORIZ STAB CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND STATION 1125 W/L 250 SUBWEB UNDER HORIZONTAL STABILIZER SUPPORT FRAME, HAS SIX CRACKS EMANATING FROM THREE LIGHTEN ING HOLES IN THE SUB WEB. (M) 2 L 7 2 4F A16WE 2002030800126 20020308 00126 WP 2002 3 8 2002F00177 1 20020206 A 5320 S4929151 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 FOUND RIGHT FLOOR SUPPORT BEAM CORRODED AT STATION 1902 TO 1921. (M) 2 L 7 3 4F A22WE 2002030800127 20020308 00127 NM 2002 3 8 2002F00178 1 20020117 A 5330 SKIN BOEING 727 727222 1384073 NM FUSELAGE GOUGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 FOUND LEFT LOWER FUSELAGE SKIN IS GOUGED AT STATION 1200 STRINGER 19 AND 20L. (M) 2 L 7 3 4F A3WE 2002030800128 20020308 00128 WP 2002 3 8 2002F00179 1 20020206 A 5320 S2929348 SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 FOUND SUPPORT 'I' BEAM CORRODED AT STATION 1910. (M) 2 L 7 3 4F A22WE 2002030800129 20020308 00129 SO 2002 3 8 C2XA02IA055 1 20020220 A 5315 14522226003 GUSSET EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 7290 145131 IAH- DURING "C" CHECK THE LEFT FLOOR BEAM WAS CORRODED AT FR. 59 TO 61. IAH- MAINTENANCE REMOVED THE CORROSION BETWEEN FRAMES 59 to 61, DRILLED OUT THE CORRODED AREA AND INSTALLED #5 RIVET, TREATED PRIMED AND PAINTED THE AREA, AND. THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE AFTER RELEASE FROM "C" CHECK. 2 L 7 2 4F RT T00011AT 2002030900001 20020309 00001 SO 2002 3 9 C2XA02IA056 1 20020308 A 3350 AD2047 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 57734 120199 IAH- MAINTENANCE, WHILE INSPECTING THE ARICRAFT THE MECHANIC NOTED THAT THE LOWER CENTER EMERGENCY LIGHTS FAILED TO ILL UMINATE. IAH- MAINTENANCE REMOVED AMD REPLACED THE #2 (TWO) EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EM ERGENCY LIGHTIBG SYSTEM,NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002031200112 20020312 00112 EU 2002 3 12 C2XA02IA053 1 20020302 A 3260 D227011112 WIRE HARNESS AEROSP ATR42 ATR42320 8680930 EU LT MLG DEFECTIVE A C2XA K NONE N FALSE WARNING UK UNKNOWN 1 SW 27 97841 280 IAH - FLT 3601 - CREW REPORTED THAT THE NOSE LANDING GEAR HAD AN UNLOCK INDICATION. SYSTEM NR 1 FORWARD PANEL NOSE LAND ING GEAR UNSAFE DOWN CYCLES SAFE/UNSAFE ON GROUND DURING TURNS. MAINTENANCE REMOVED AND REPLACED SYSTEM NR 1 DOWN LOCK PROX SWITCH HARNESS, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. 2 H 7 2 4T RT A53EU 2002031100001 20020311 00001 EU 2002 3 11 CA020215012 1 20020206 A 6120 CU99 PCU BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU ROTOL R4304 R2124304 EU RT ENGINE SEIZED W C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA (CAN) TAKEOFF WAS ABORTED FROM YVP AFTER MIN TORQUE WAS NOT OBSERVED AND THE RT ENGINE PROCEEDED TO AUTO-FEATHER. ON RE MOVAL OF THE PCU IT WAS NOTICED THAT THE DRIVE GEAR HAD SEIZED AND SHEARED THE PCU DRIVE QUILL SHAFT. A SERVICEABLE PCU AND PCU QUILL SHAFT WAS INSTALLED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 3T 4 T A24EU A196 6 C P899 2002031100002 20020311 00002 EA 2002 3 11 CA020215014 2 20020213 A 7314 LW15473 PUMP PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA FUEL SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) OIL WAS FOUND LEAKING FROM RIGHT ENGINE DRAIN LINES. PUMP WAS REPLACED WITH NEW. 1 L 7 2 3O 3 O 1A10 1E4 2002031100003 20020311 00003 NM 2002 3 11 CA020218001 1 20020214 A 2780 CONTROL UNIT BOEING 737 737204 1384458 NM PWA JT8 JT8D15 52051 NE LE SLAT MALFUNCTIONED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA (CAN) AT FLAP EXTENSION FOR LANDING, NR 3 LEADING EDGE SLAT SHOWS YELLOW AT FLAP 1 WITH OVERHEAD PANEL CAUTION "LE FLAP INTRASIT" LIGHT STAYING YELLOW UNTIL FLAP 15 IS SELECTED. OCCURS IN FLT BUT SEEMS TO WORK FINE ON GROUND. "MAINT INSPECT ION FOUND NR 3 SLAT INBOARD SLAT TRACK UPPER ROLLER BOLT SEVERED & DAMAGE TO SLAT TRACK CUTOUT AREA. MAINT INST NEW BOLT ASSY (NEW BOLT,ROLLER, NUT & WASHER) LEADING EDGE WING DAMAGE TRIMMED OUT IN ACCORD WITH SRM 57-20-01 DETAIL 'E'. SLAT & FLAP SYS FUNCTION TESTED SERVICEABLE - ALL INDICATIONS NORMAL. A/C INSP&FOUND SAFE FOR FERRIED FLT TO YYC - COMMUNICA TIONS WITH BOEING FOUND REPAIR NOT CONFORMING TO SRM. 2 L 7 2 4F 4 F A16WE E2EA 2002031100005 20020311 00005 EA 2002 3 11 CA020220001 1 20020219 A 2910 AE7051911 LINE CNDAIR CL600 CL600* EA LYC ALF502 ALF502L2C NE HYD PRESSURE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) PIN HOLE DEVELOPED IN FLEX LINE PORTION OF HYDRAULIC PUMP PRESSURE LINE CAUSING DUMPING OF ALL HYD FLUID AND CAVIT ATION OF HYD PUMP (EDP), ASSOCIATED MASTER CAUTION LIGHT AND LOSS OF NR 2 HYD SYSTEM. PROBLEM OCCURED 5 MINUTES BEFORE LANDING. SMALL AMOUNT OF METAL SHOWED UP IN DRAIN FILTER, REQUIRING REPLACEMENT OF EDP AS WELL AS AFFECTED HYDRAULIC L INE. 2 L 7 2 4F 4 F RT A21EA E6NE 2002031100006 20020311 00006 WP 2002 3 11 CA020220006 1 20020212 A 5540 KSP6A BEARING GRUMAN 89C1024501 GRUMAN TS2 TS2ACALFORST 3951102 WP WRIGHT R1820 982C9HE2 67020 EA HAMSTD 43D 43D51 NE RUDDER WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE CARRYING OUT AN ANNUAL INSPECTION IT WAS NOTED THAT THE RUDDER SECTOR P/N 89C1024-501 HAD RAISED UP TO WHERE THE CABLE GUARD AND THE STOP WERE IN VERY CLOSE PROXIMITY TO ONE ANOTHER. IF THE SITUATION WENT UNDETECTED THERE IS A P OSIBILITY THAT THE RUDDER CONTROLS COULD BECOME JAMMED. WE WILL BE INSPECTING THE REST OF OUR FLEET TO DETERMINE IF THIS SITUATION EXISTS ON ANY OF OUR OTHER AIRCRAFT. THE RUDDER SECTOR WAS REMOVED FROM THE AIRCRAFT AND THE BEARING WAS REPL ACED WITH A SERVICEABLE UNIT. 2 H 7 2 4R 4 R A25WE E259 6 C P8879 2002031100007 20020311 00007 NE 2002 3 11 CA020220007 1 20020214 A 3213 7625002102103 CROSSOVER TUBE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 21169 (CAN) DURING A POST FLIGHT INSPECTION THE AME FOUND A CRACK ON THE MAIN LANDING GEAR CROSS TUBE WHEN REMOVED. THE CRACK WAS FOUND TO BE 360 DEGREES AROUND THE TUBE, ALLOWING SEPARATION OF THE ROD END. THE TUBE WAS REPLACED. 1 G 7 2 3U 3 U H1NE E1GL 2002031100010 20020311 00010 EA 2002 3 11 CA020220012 1 20020215 A 2133 62344 OUTFLOW VALVE CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A NE CABIN PRESS FAILED W A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 CA (CAN) OVERHAULED SECONDARY OUTFLOW VALVE FOR PRESSURIZATION SYSTEM WAS INSTALLED TO RECTIFY A POPPED CIRCUIT BREAKER. SY STEM GROUND RUN CARRIED OUT AND AIRCRAFT DEPARTED A FEW DAYS LATER. UPON REACHING FL 230 FT PNF NOTICED CABIN PRESSURIZA TION WAS AT MAX CABIN DIFFERENTIAL 8.8 POUNDS. THE CABIN ALTITUDE INDICATED SEA LEVEL "O". AIRCRAFT RETURNED TO POINT OF DEPARTURE. ANOTHER SECONDARY OUTFLOW VALVE INSTALLED AND GROUND CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A21AE E15NE 2002031100012 20020311 00012 EA 2002 3 11 CA020221003 1 20020205 A 2432 171BS1011 BATTERY CNDAIR CL601 CL6012A12 1900303 EA MAIN BURNED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) FOLLOWING FLIGHT DURING TAXI IN, PILOT REPORTED STRONG ELECTRICAL SMELL / SMOKE IN COCKPIT. EXTENSIVE T/S FOUND AMPS 500 BATTERY DIODE BURNED. NO FAIL INDICATION WAS REPORTED. 2 L 7 2 4F RT A21AE 2002031100014 20020311 00014 EA 2002 3 11 CA020221007 1 20020214 A 7603 2100140007 GEARBOX CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE THROTTLE FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) RT REV ICON ON N1 GUAGE AND REV UNSAFE CAUTION MESSAGE APPEARED AFTER TAKEOFF. RT ENGINE THROTTLE GEARBOX ASSEMBL Y REMOVED AND REPLACED. AIRCRAFT BACK IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002031100015 20020311 00015 EA 2002 3 11 CA020221011 1 20020219 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER DE DESCENT 1 CA (CAN) CREW REPORTED THE RIGHT WINDSHIELD CRACKED WHILE ON DESCENT. RIGHT WINDSHIELD REMOVED AND REPLACED IAW CRJ AMM 56 -11-01. THE WIDNSHIELD WAS PRE-SERVICE BULLETIN.AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002031100016 20020311 00016 EA 2002 3 11 CA020221014 1 20020219 A 3234 NUT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MLG SELECTOR LOOSE W O OTHER J WARNING INDICATION AP APPROACH 1 CA 14734 (CAN) ON APPROACH NOSE DOOR OPEN AT 250 KTS WITH NO INPUT TO GEAR HANDLE. NOSE GEAR SOUNDED LIKE IT CYCLED AND GEAR DISA GREE MESSAGE. ABORTED APPROACH. MANUAL EXTENSION PERFORMED. EMERGENCY DECLARED AND LANDED.DUPLICATED PROBLEM IN HANGAR O N JACKS.NLG DOOR WOULD OPEN / CLOSE INTERMITTENTLY. R&R'D PSEU AND GEAR SELECTOR HANDLE AS PRECAUTIONARY. THE PARTS REMO VAL REPORT FROM THE SPARES DEPT INDICATE THAT: "FOUND LOOSE NUT IN HOUSING OF THE LANDING GEAR CONTROL ASSEMBLY". 2 L 7 2 4F 4 F RT A21EA E15NE 2002031100017 20020311 00017 EA 2002 3 11 CA020221015 1 20020220 A 5730 601R100468 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 19497 (CAN) WHILE PERFORMING SCHEDULED MAINTENANCE, TASK CARD 002-57-510/610-603, A CRACK WAS FOUND ON ONE OF THE FUEL BOOST PUMP ACCESS SCREW HOLES. 2 L 7 2 4F 4 F RT A21EA E15NE 2002031100018 20020311 00018 EA 2002 3 11 CA020221016 1 20020220 A 5610 NP1393219 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) CLIMBING THROUGH 28,000 FEET AT ABOUT 290 KNOTS LEFT FRONT WINDSHIELD SHATTERED. DECLARED AN EMERGENCY AND DIVERTE D TO KNOXVILLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002031100019 20020311 00019 EA 2002 3 11 CA020222002 1 20020222 A 2731 9960013 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE STAB TRIM FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 13593 (CAN) AFTER TAKEOFF STAB TRIM CAUTION MESSAGE POSTED. RE-ENGAGEMENT NOT POSSIBLE. RETURNED TO BASE. LT STAB TRIM DISCONN ECT SWITCH SUSPECTED, CONFIRMED BY MDC. SWITCH REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002031100020 20020311 00020 SO 2002 3 11 CA020222003 1 20020216 A 3243 13450A VALVE EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA PARK BRAKE SYS LEAKING W K NONE W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 CA (CAN) 1) AN OVERHAULED PARKING BRAKE VALVE WAS INSTALLED TO REPLACE A UNIT "ROBBED" TO SERVICE ANOTHER AIRCRAFT. NOTE: AIRCRAFT HANGARED MORE THAN TWO (2) DAYS, THUS WARM FLUID AND SYSTEM. 2) OVERHAULED VALVE INSTALLED. 3) UPON FIRST PRESS URE TEST FOLLOWING INSTALLATION A "HEAVY LEAK" SPRUNG AT THE PISTON SHANK. NOTE: ONE MAY THINK "O" RING OR SEAL IS MISSI NG INSIDE. 4) UNIT REMOVED. RED TAGGED. PART IDENTIFIED FOR KEEPING AVAILABLE FOR 21 DAYS AS PER 24-0038 INSTRUCTIONS. 1 L 7 2 4T 4 T A21SO E4EA 2002031100021 20020311 00021 CE 2002 3 11 CA020222005 1 20020222 A 7920 3008786 SHAFT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE QUILL CONNECTION SHEARED W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) CREW REPORTED FLUXS ON RT ENGINE OIL PRESSURE DURING CLIMB. MANAGED TO STABILIZE TEMPORARILY WITH REDUCED POWER SE TTINGS. PRESSURE CONTINUED TO DROP BELOW 60PSI CAUSING INFLT SHUTDOWN PROCS TO BE CARRIED OUT. A/C RETURNED TO ST ATION FOR INVEST. MAINT FOUND EVIDENCE OF OIL LEAKAGE ON LOWER PORTION OF INNER WING AREA & RT MLG, ENGINE AREA DRY & OIL FR EE WITH EXCEPTION OF AFT COMPT WHICH SHOW SIGNS OF LEAKAGE. OIL COOLER SUSPECTED AT 1ST BUT RUNS IDENTIFIED EXCESS OIL E XITING L.P. FUEL PUMP DRAIN AREA. EXTERNAL SCAVENGE PUMP REMOVED & SHAFT CONNECTION FOR L.P. PUMP FOUND SHEARED DIRECTLY BEHIND QUILL ATTACHMENT AREA. SHEARED SHAFT ALLOWED OIL SEEP. PAST SHAFT & GARLOCK SEAL AREA INTO FUEL PUMP ATTACHMENT 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002031100030 20020311 00030 2002 3 11 SWAA020504 4 20020306 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET HAS A BROKEN RIVET. REMOVED AND R EPLACED RIVET PER SRM. 2 L 7 2 4F RT A16WE 2002031100031 20020311 00031 2002 3 11 SWAA020505 4 20020306 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 601WN 27695 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002031100032 20020311 00032 NM 2002 3 11 SWAA020506 1 20020307 A 2731 65C2638412M TAB BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED RON,(SI-11111-55) RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002031100033 20020311 00033 NM 2002 3 11 SWAA020507 1 20020307 A 5755 6573730 SPOILER BOEING 737 7373L9 1384470 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING WALK AROUND INSP, FOUND NR 6 SPOILER DELAMINATED. REMOVED AND REPLACED NR 6 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2002031100034 20020311 00034 NM 2002 3 11 SWAA020508 1 20020306 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER AFT CORNER OF FWD SVC DOOR CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002031100035 20020311 00035 NM 2002 3 11 SWAA020509 1 20020306 A 5753 6546435278 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 DURING SCHEDULED C2 CHECK, FOUND RT OTBD AFT FLAP DELAMINATED ON LOWER INBD CORNER, LOWER SURFACE. REMOVED AND REPLACED OTBD AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2002031100038 20020311 00038 WP 2002 3 11 0200589938 1 20020304 A 3397 WIRE DOUG DC9 DC931 3022065 WP COCKPIT SHORTED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 1798U 47369 AFTER LANDING AT IND, SIGNIFICANT SMOKE WAS COMING FROM GLARESHIELD ON EITHER SIDE OF THE ALTITUDE ALERTER. SMOKE STOPP ED AFTER THE PARKING CHECK WAS DONE AT THE GATE. MAINTENANCE INSPECTED BUT FOUND NO EVIDENCE OF SMOKE OR FIRE. THEN TW O FLIGHTS LATER ON NR 1289, 500 FT AGL ON FINAL APPROACH INTO MEM, 3 PILOTS SMELLED ELECTRICAL/OZONE ODOR. NO VISIBLE S MOKE THIS TIME AND SMELL DISSIPATED AFTER LANDING. MAINTENANCE FOUND A WIRE (218855) TO THE NOSE LANDING LIGHT SWITCH B ADLY BURNED AND SPLICED IN A NEW WIRE AND TERMINAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002031100039 20020311 00039 NM 2002 3 11 CA020228018 1 20020218 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8101 2809002 NM PWA 120 PW120 NE HAMSTD 14SF 14SF7 NE ENGINE LEAKING W E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CA (CAN) NR 2 OIL PRESSURE WARNING LIGHT ILLUMINATED WITH A DECAYING OIL PRESSURE INDICATION. ENGINE CONTROLS WERE MOVED TO FLIGHT IDLE AND THE PROPELLER FEATHERED. OIL PRESSURE CONTINUED TO REDUCE, AND CREW ELECTED TO SHUTDOWN NR 2 ENGINE. N R 2 ENGINE SHUTDOWN IN CRUISE DUE TO OIL PRESSURE LOSS. AIRCRAFT WAS 90 NM FROM PLANNED DESTINATION WHEN INCIDENT OCCURR ED.FLIGHT CREW ADVISED ATC OF A "PAN" CONDITION AND ELECTED TO CONTINUE TO BASE. INVESTIGATION FOUND THAT THE OIL LEAK W AS EMANATING FROM THE OIL COOLER ASSEMBLY. OIL COOLER WAS SUBSEQUENTLY REPLACED, AND THE AIRCRAFT RETURNED TO SERVICE.OI L COOLER ASSEMBLY IS TO BE RETURNED TO THE MANUFACTURER FOR TEST AND EVALUATION. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002031100040 20020311 00040 SW 2002 3 11 HEEA077859 1 20020219 A 6420 407312100101 BEARING 407012101111 BELL 407 407 1182206 SW T/R HUB WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 740PH 53436 53435 OUTPUT SHAFT SPLINES WORN AND CORRODED. 1 G 7 1 3U O H2SW 2002031100041 20020311 00041 SW 2002 3 11 HEEA077861 1 20020219 A 6420 406312100101 BEARING 407012101111 BELL 407 407 1182206 SW T/R HUB WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 457PH 53207 53147 T/R FEATHERING BEARINGS WORN. 1 G 7 1 3U O H2SW 2002031100042 20020311 00042 WP 2002 3 11 0200599154 1 20020226 A 3020 577957 DUCT DOUG DC9 DC914 3022034 WP PWA JT8 JT8D7 52053 NE RT ENGINE DAMAGED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8913E 7679 45830 654825 DURING CLIMBOUT, THE RIGHT ENGINE EXPERIENCED A FIRE WARNING INDICATION. CREW REDUCED RIGHT ENGINE THRUST TO IDLE SETTI NG AND LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGH T ENGINE FUEL HEAT ANTI-ICE DUCT. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2002031100043 20020311 00043 NE 2002 3 11 0200609617 2 20020302 A 7230 COMPRESSOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE ENGINE STALLED A NWAA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 617NW 47235 657496 DURING TAKEOFF ROLL AT 105 KTS, THE AIRCRAFT EXPERIENCED A COMPRESSOR STALL. CREW ABORTED TAKEOFF AND RETURNED TO THE G ATE. MAINTENANCE INSPECTED PS3 FILTERS AND SADDLE DUCTS ON BOTH ENGINES. NO DEBRIS WAS FOUND. BOTH ENGINES WERE OPERA TED TO TAKEOFF POWER WITH NO STALLS OCCURRING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2002031100044 20020311 00044 SW 2002 3 11 HEEA077862 1 20020219 A 6300 407040320101 SHAFT PHIPBH40701 BELL 407 407 1182206 SW COOLER BLOWER WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 720PH PHI0011 53277 OIL COOLER BLOWER HAS SPLINE WEAR. 1 G 7 1 3U O H2SW 2002031100046 20020311 00046 2002 3 11 P5CA0200660 4 20020307 A 3416 9650184601 COMPUTER BOEING 747 747122 1384872 NM E & E COMP. FAULTY A P5CA K NONE J N WARNING INDICATION FALSE WARNING CR CRUISE 1 WP 23 853FT 19753 WITH AUTO PILOT "A" OR "B" ENGAGED, ALTITUDE ALERT HORN & LIGHT CONTINUALLY CHIME IN LEVEL FLIGHT AFTER CLIMB TO FL 34.0 (WAS O.K. AT FL 32.0 & FL 33.0) REMOVED & REPLACED ALT ALERT WARNING COMPUTER IAW MM 31-16-00. OPS CHK GOOD. 2 L 7 4 4F A20WE 2002031100047 20020311 00047 EU 2002 3 11 02FDEA00190 1 20020306 A 7710 SENSOR AIRBUS 310 A310203 3930313 EU GE CF6 CF680A 30025 NE NR 1 ENGINE FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 442FE 353 585122 DURING CLIMB NR 1 ENGINE FLUCTUATED. REMOVED AND REPLACED NR 1 CIT SENSOR & T2 SENSOR PER 73-21-02-4, 73-23-07-4. ALL OK. 2 L 7 2 4F 4 F RT A35EU E13NE 2002032500050 20020325 00050 NM 2002 3 25 2002UALA00332 1 20020227 A 2910 BACC63CE2422S CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE HYD SYSTEM BURNED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 664UA 29236 SHORTLY AFTER TAKEOFF, EICAS DISPLAYED C-HYD PRI 1 WITH ASSOCIATED PRESS LIGHT ON CENTER ELEC 1 PUMP SWITCH. AIRCRAFT R ETURNED TO SFO. PUMP CONNECTOR FOUND BURNED. REPLACED PUMP PER MM 29-11-02, SERVICED HYD SYSTEM. REPLACED CONNECTOR D 482, OPS CHECKED AND LEAK CHECKED PER MM 29-11-02. CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2002031100048 20020311 00048 WP 2002 3 11 ABXA010757 1 20020304 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 954AX 47612 COCKPIT OVERHEAD EMERGENCY LIGHTS WOULD NOT TEST. REPLACED NICAD BATTERIES IN EMERGENCY LIGHTING BATTERY PACK IAW DC-9 MM 33-53-00-8. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002031100049 20020311 00049 NM 2002 3 11 ABXA010758 1 20020307 A 2840 HG1057AA07 COMPUTER BOEING 767 767281 1385109 NM FUEL SYSTEM DEFECTIVE A ABXA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 GL 23 773AX 2965 22788 DURING DESCENT, OBSERVED FUEL DISAGREE PROGRAM 2/2 AND VERIFIED FUEL IMBALANCE. LEFT FUEL QUANTITY LOWER THAN THE RIGHT BY APPROXIMATELY 1,400 LBS. ACCOMPLISHED THE QUICK REFERENCE HANDBOOK PROCEDURES AND SECURED THE LEFT ENGINE IAW THE Q RH. PERFORMED FIM PROCEDURE 34-61-00, FIG 106, SHEET 1. FUEL INDICATION CHECKED NORMAL. INSTALLED NEW FUEL QUANTITY P ROCESSOR IAW B767 MM 28-41-08-04 FOR PRECAUTIONARY PURPOSES. TRANSPOSED FMC'S FOR TROUBLESHOOTING. INSPECTED WINGS AND ENGINES FOR FUEL LEAKS. NONE FOUND. 2 L 7 2 4F RT A1NM 2002031800087 20020318 00087 2002 3 18 ARWA20020301 4 20020303 A 2312 VHF COMM DOUG DC8 DC862 3021970 WP COCKPIT MALFUNCTIONED A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 8968U 46069 RETURNED TO SVMI DUE TO TOTAL LOSS OF RADIO COMMUNICATION (VHF). AIRCRAFT LANDED UNEVENTFUL. CHECKED FOR SECURITY OF R ADIO AND RECEIVER PANELS, OPS CHECK OF VHF OK IAW MM 23-20-00. 2 L 7 4 4F 4A25 2002031100051 20020311 00051 SW 2002 3 11 HEEA077863 1 20020219 A 6310 406040516101 SHAFT 406040500127 BELL 407 407 1182206 SW FREEWHEEL UNIT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH A4539 53003 FREEWHEEL UNIT SHAFT HAS SPLINES WORN. 1 G 7 1 3U O H2SW 2002031800103 20020318 00103 NE 2002 3 18 ARWA20020302 2 20020305 A 7261 779606 RELIEF VALVE DOUG DC8 DC85F54 3021926 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE FAULTY A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 426FB 45667 DURING CLIMBOUT THROUGH 15,000 FT, NR 2 ENGINE OIL PRESSURE BEGAN FLUCTUATING, NR 2 OIL PRESSURE LIGHT ILLUMINATED. ACC OMPLISHED APPROPRIATE CHECK LISTS AND SHUT DOWN ENGINE AT 00:15Z, OIL WINDMILLED AT 12 PSI. AIRCRAFT RETURNED TO PTY AN D LANDED UNEVENTFUL. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE RELIEF VALVE IAW MM 79-20-5, OPS CHECK PER MM 79-20- 0, FOUND NORMAL. 2 L 7 4 4F 4 F RT 4A25 1E8 2002031100052 20020311 00052 SW 2002 3 11 HEEA077864 1 20020219 A 6310 214040841101 SEAL BELL 407 407 1182206 SW FREEWHEEL UNIT LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 8595X 53267 FREEWHEEL UNIT HAS A SEAL LEAKING. 1 G 7 1 3U O H2SW 2002031100053 20020311 00053 SW 2002 3 11 HEEA077865 1 20020219 A 6420 406012102109 YOKE 407012101111 BELL 407 407 1182206 SW T/R HUB DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 491PH T53069 53386 TAIL ROTOR YOKE HAS A CLICKING BEARING. 1 G 7 1 3U O H2SW 2002031100054 20020311 00054 SO 2002 3 11 LR7A02012 1 20020307 A 5230 FORMER LKHEED 382 382G 526414U SO FS 904 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC5303 FOUND AFT CARGO DOOR FS 904 FRAME RIB FORMER CRACKED AT LBL 10 AND LB L 30, WL 210.REPAIRED IAW SRM SMP 583 51-140-17. NR 0137. 2 H 7 4 4T A1SO 2002031100055 20020311 00055 SO 2002 3 11 LR7A02013 1 20020307 A 5312 BEAM LKHEED 382 382G 526414U SO FS 497 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC5303 FOUND RMLG WHEEL WELL FS 497 BOW BEAM CRACKED AT FS 497 UPPER FITTING , RBL 61, WL 200.REPAIRED IAW SRM SMP 583 53-40-14. NR 2051. 2 H 7 4 4T A1SO 2002031100056 20020311 00056 SO 2002 3 11 LR7A02015 1 20020307 A 5315 3896939 FITTING LKHEED 382 382G 526414U SO FS 577 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP53121 FOUND LH FS 577 BULKHEAD END FITTING CRACKED AT LBL 60, WL 142.REPL ACED FITTING IAW SRM SMP 583 51-10 PG 4. NR 2077. 2 H 7 4 4T A1SO 2002031100057 20020311 00057 SO 2002 3 11 LR7A02016 1 20020307 A 5320 3851882 FITTING LKHEED 382 382G 526414U SO FS 817E CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP5338 FOUND FS 817E RH GUSSET ANGLE FITTING CRACKED AT RBL 70, WL 200.REPL ACED FITTING IAW SRM SMP 583 51-10 PG 4. NR 2078. 2 H 7 4 4T A1SO 2002031100058 20020311 00058 SO 2002 3 11 LR7A02017 1 20020307 A 5230 BRACKET LKHEED 382 382G 526414U SO FS 809 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP53161 FOUND RAMP UNDERFLOOR FS 809 (RAMP STA 8) LINKAGE SUPPORT BRACKET C RACKED AT BL 0, WL 173.REPLACED BRACKET AND WEB IAW SRM SMP 583 51-10 PG 4. NR 2088. 2 H 7 4 4T A1SO 2002031100059 20020311 00059 SO 2002 3 11 LR7A02018 1 20020307 A 5315 38969310 FITTING LKHEED 382 382G 526414U SO FS 577 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP53121 FOUND RH FS 577 BULKHEAD END FITTING CRACKED AT RBL 60, WL 142.REPL ACED FITTING IAW SRM SMP 583 51-10 PG 4. NR 2089. 2 H 7 4 4T A1SO 2002031100060 20020311 00060 SO 2002 3 11 LR7A02019 1 20020307 A 5350 LONGERON LKHEED 382 382G 526414U SO FS 477 BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND LMLG WHEEL WELL LBL 85 LONGERON BROKEN AT FS 477, WL 200.REPAI RED IAW SRM SMP 583 53-40-42. NR 2094. 2 H 7 4 4T A1SO 2002031100061 20020311 00061 SO 2002 3 11 LR7A02020 1 20020307 A 5311 FRAME LKHEED 382 382G 526414U SO FS 928 & 940 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND FS 928 AND 940 STUB FRAMES CRACKED AT LBL 18, WL 285.REPAIRED IAW LAC MEA 382-53-02-013. NR 2130 2 H 7 4 4T A1SO 2002031100062 20020311 00062 SO 2002 3 11 LR7A02021 1 20020307 A 5315 3568597 CAP LKHEED 382 382G 526414U SO FS 577 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND FS 577 LOWER BEAM CAP CRACKED AT RBL 58, WL 138.REPAIRED IAW L AC MEA 382-53-02-011. NR 2134. 2 H 7 4 4T A1SO 2002031100063 20020311 00063 SO 2002 3 11 LR7A02025 1 20020307 A 5230 WEB LKHEED 382 382G 526414U SO FS 890 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC5303 FOUND FS 890 CARGO DOOR BULKHEAD WEB PUNCTURED AT RBL 22, WL 205.REPA IRED IAW SRM SMP 583 51-140-17. NR 2155 2 H 7 4 4T A1SO 2002031100064 20020311 00064 WP 2002 3 11 ARWA20020303 1 20020306 A 2760 FUSE DOUG DC8 DC863F 302198F WP SPOILER SYS BLOWN A ARWA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 19 441J 45988 IN CRUISE NR 1 MAIN & ALT TANK FUEL BOOST PUMPS POPPED C/B'S, WITH ASSOCIATED INDICATION OF NR 1 & 2 CSD TEMP INOP, NR 1 & 2 ENGINE OIL TEMP AND QTY INOP, GEAR LIGHTS INOP AND SPOILER PRESS ZERO, WITH OVERRIDE POSITION INOP. ALL OTHER C/B' S CHECK NORMAL AND NO POWER BUS FAILURE LIGHT. ABNORMAL CHECKLIST COMPLIED WITH, DIVERTED FROM GUA TO SAL WITHOUT INCID ENT. REMOVED AND REPLACED SPOILER PUMP FUSES, SPOILER CHECK NORMAL IAW MM 27-62-0. PERFORMED COMPLETE ELECTRICAL SYSTE M CHECK AND FOUND NORMAL IAW MM 24-20-0. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002031100065 20020311 00065 SW 2002 3 11 HEEA077866 1 20020219 A 6520 406040453101 SEAL PHI407123 BELL 407 407 1182206 SW TAIL ROTOR LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 407PH 53003 TAIL ROTOR INPUT SEAL LEAKING. 1 G 7 1 3U O H2SW 2002031800108 20020318 00108 NE 2002 3 18 ARWA20020304 2 20020306 A 7261 562021 HOUSING DOUG DC8 DC85F54 3021926 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE DAMAGED A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 426FB 45667 DURING CLIMBOUT THROUGH 16,000 FEET; NR 2 ENGINE OIL PRESSURE GAUGE BEGAN FLUCTUATING AT 180, AND NR 2 OIL PRESSURE LIGH T BEGAN FLICKERING, THEN WENT STEADY. ACCOMPLISHED APPROPRIATE ABNORMAL CHECKLISTS AND SHUTDOWN ENGINE AT 22:15 ENGINE OIL PRESSURE WINDMILLING AT 15 PSI. REMOVED AND REPLACED NR 2 ENGINE MAIN OIL FILTER HOUSING IAW P&W MM 72-00. PERFORM ED ENGINE RUN UP IAW MM 71-00, OPS CHECK GOOD. 2 L 7 4 4F 4 F RT 4A25 1E8 2002031100066 20020311 00066 SW 2002 3 11 HEEA077867 1 20020219 A 6310 406040516101 SHAFT 406040500127 BELL 407 407 1182206 SW FREEWHEEL UNIT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 490PH A4685 53378 FREEWHEEL UNIT INPUT SHAFT HAS EXCESSIVE SPLINE WEAR. 1 G 7 1 3U O H2SW 2002031100067 20020311 00067 NM 2002 3 11 QXEA0200414 1 20020308 A 5270 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 NM STICKING A QXEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 09 413QX 4060 YYC - AIRCRAFT RETURNED TO FIELD WHEN THE FORWARD BAGGAGE DOOR INDICATED OPEN AFTER AIRCRAFT ROTATION. MAINTENANCE INSPE CTED THE DOOR AND FOUND THE PROXIMITY SENSOR STICKING. CLEANED AND LUBED PROXIMITY SENSOR. OPERATIONAL CHECK WAS PERFORM ED AND THE DOOR INDICATION IS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031100068 20020311 00068 SW 2002 3 11 HEEA077868 1 20020219 A 6420 BEARING BELL 407 407 1182206 SW T/R HUB TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 501PH 53401 53401 TAIL ROTOR HAS A TORN FLAPPING BEARING. 1 G 7 1 3U O H2SW 2002031100069 20020311 00069 SW 2002 3 11 HEEA077869 1 20020219 A 6520 407040416101 SHAFT 406040400119 BELL 407 407 1182206 SW T/R GEARBOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 494PH 2172 A1077 53396 EXCESSIVE CORROSION ON OUTPUT SHAFT DRIVE SPLINES. 1 G 7 1 3U O H2SW 2002031100070 20020311 00070 NE 2002 3 11 ARWA20020305 2 20020306 A 7200 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 MALFUNCTIONED A ARWA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 19 441J 45988 WITH THROTTLE SET FOR MAX TAKEOFF NR 4 ENGINE GOT UP TO 1.70 EPR, N1-100, N2-100, AND THROTTLE FULL FORWARD. TAKEOFF AB ORTED AND RETURNED TO THE RAMP. 2 L 7 4 4F 4 F 4A25 1E8 2002031100071 20020311 00071 SW 2002 3 11 HEEA077870 1 20020219 A 6322 BEARING BELL 407 407 1182206 SW COOLER BLOWER ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 493PH 53393 FWD BEARING ROUGH AND MAKING NOISE. 1 G 7 1 3U O H2SW 2002031100074 20020311 00074 SW 2002 3 11 HEEA077872 1 20020219 A 6510 407340339101 BEARING 407040302101 BELL 407 407 1182206 SW T/R DRIVESHAFT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH A685 53159 TAIL ROTOR DRIVE SHAFT HAS ROUGH BEARINGS. SHAFT HAS MECHANICAL DAMAGE. 1 G 7 1 3U O H2SW 2002031100076 20020311 00076 SW 2002 3 11 HEEA077873 1 20020219 A 6420 406312100101 BEARING 407012101111 BELL 407 407 1182206 SW TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 720PH 53397 53277 TAIL ROTOR HUB HAS WORN FEATHERING BEARINGS. 1 G 7 1 3U O H2SW 2002031100077 20020311 00077 SW 2002 3 11 HEEA077874 1 20020219 A 6310 406040516101 SHAFT 406040500123 BELL 407 407 1182206 SW FREEWHEEL UNIT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4999 A3817 53323 FREEWHEEL UNIT SHAFT HAS SPLINES WORN. 1 G 7 1 3U O H2SW 2002031100079 20020311 00079 SW 2002 3 11 HEEA077875 1 20020219 A 6220 407010103101 PITCH HORN 407010100115 BELL 407 407 1182206 SW MAIN ROTOR HEAD CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 A282 MAIN ROTOR HEAD PITCH HORN HAS CORROSION. 1 G 7 1 3U O H2SW 2002031100080 20020311 00080 SW 2002 3 11 HEEA077876 1 20020219 A 6220 407310100103 DAMPER 407010100115 BELL 407 407 1182206 SW MAIN ROTOR HEAD CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 447PH A251 53114 MAIN ROTOR DAMPER CORRODED. 1 G 7 1 3U O H2SW 2002031100085 20020311 00085 WP 2002 3 11 AT0200020 1 20020130 A 5753 SKIN DOUG DC9 DC932 3022066 WP T/E FLAP CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 831AT 47674 INBOARD FLAP, INBOARD LEADING EDGE HAS DEEP CHAFING MARK ABOUT STA X CW 58 OF RIGHT WING. 2 L 7 2 4F A6WE 2002031100086 20020311 00086 WP 2002 3 11 AT0200021 1 20020122 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 831AT 47674 MAIN CABIN FLOOR SEAT TRACK HAS LIGHT CORROSION BETWEEN BS 237 AND BS 250 AT RBL 22 AND RBL 44, RBL 44 + 22 FROM STA 200 TO STA 410 AND REMOVED CABIN SEAT TRACK RBL 44 FROM STA 237 TO 331. 2 L 7 2 4F A6WE 2002031100087 20020311 00087 WP 2002 3 11 AT0200022 1 20020122 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 831AT 47674 MAIN CABIN FLOOR SEAT TRACK RBL 22 HAS SPOTS OF LIGHT CORROSION BS 470, BS 484, BS 515, BS 525, BS 545, BS 579, AND BS 6 05. 2 L 7 2 4F A6WE 2002031100092 20020311 00092 SW 2002 3 11 HEEA077879 1 20020219 A 6520 406040500119 SEAL BELL 407 407 1182206 SW XMSN SUPPORT LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 490PH 53378 TRANSMISSION SUPPORT SEAL LEAKING. 1 G 7 1 3U O H2SW 2002031100093 20020311 00093 SW 2002 3 11 HEEA077880 1 20020219 A 7714 222375022111 INDICATOR BELL 222 222 1182122 SW ENGINE NG STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 NEEDLE STICKS ON ZERO WHEN STARTING MOST OF THE TIME. 1 G 7 2 3U H9SW 2002031100094 20020311 00094 SW 2002 3 11 HEEA077881 1 20020219 A 2730 214001970111 ACTUATOR BELL 214 214ST 1182106 SW ELEVATORS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 ACTUATOR KICKS ELEVATORS OFF LINE. 2 G 7 2 4U H10SW 2002031100097 20020311 00097 WP 2002 3 11 AT0200028 1 20020303 A 3397 WIRE DOUG DC9 DC932 3022066 WP TAIL CONE BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 866AT 47168 DURING EMERGENCY LIGHTING CHECK OUT FOUND TAIL CONE EMERGENCY RELEASE HANDLE LIGHT INOP. FURTHER INVESTIGATION REVEALED POSITIVE WIRE CUT IN HALF 2 FEET FROM LIGHT. 2 L 7 2 4F A6WE 2002031100098 20020311 00098 EU 2002 3 11 HEEA077883 1 20020117 A 7170 0174078010 DRAIN VALVE SNIAS 350 AS350B 8680801 EU ENG START LEAKING E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 854PH 3248 START DRAIN VALVE LEAKING WHEN ENGINE RUNNING. 1 G 7 1 3U H9EU 2002031100099 20020311 00099 EU 2002 3 11 HEEA077885 1 20020208 A 2560 SCREW SNIAS 350 AS350B 8680801 EU INERTIA REEL MISSING E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 855PH 3351 INERTIA REEL HAS A SCREW MISSING. 1 G 7 1 3U H9EU 2002031100100 20020311 00100 EU 2002 3 11 HEEA077886 1 20020208 A 6220 350A31177000 PIN SNIAS 350 AS350B 8680801 EU M/R HEAD WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 855PH 3351 COATING WORN. 1 G 7 1 3U H9EU 2002031100101 20020311 00101 2002 3 11 HEEA077887 4 20020208 A 3120 B1894522282A CLOCK SNIAS 350 AS350B2 8680813 EU COCKPIT INTERMITTENT E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 40466 3004 CLOCK HAS INTERMITTENT OPERATION. 1 G 7 1 3U H9EU 2002031100103 20020311 00103 EU 2002 3 11 AWXA200200185 1 20020302 A 5210 FE174004 DAMPENER AIRBUS 320 A320231 3930325 EU L2 DOOR LEAKING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 55 YWG - DOOR SYSTEM - C - DURING C-02 CHECK DOOR ASSIST CYLINDER FOR THE L2 DOOR WAS FOUND TO HAVE NO DAMPENING ACTION. M AINTENANCE REMOVED, REPLACED AND RIGGED THE L2 DOOR DAMPER ASSIST CYLINDER IAW AMM 52-11-14-052, OPERATIONAL CHECK WAS G OOD. 2 L 7 2 4F RT A28NM 2002040100055 20020401 00055 NM 2002 4 1 AWXA200200186 1 20020302 A 2432 23013 CHARGER BOEING 737 737277 1384570 NM E/E BAY FAILED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 184AW 53987 22651 CLIMBOUT ELEC ODOR 7000 FT, NO SMOKE. TURNED BACK. PWR REDUCED, ODOR SUBSIDED. MX ENTERED COCKPIT, SMELL SIMILAR TO BU RNT RESISTOR. ALL C/B PNL LT & RT LOAD CNTL CENTER INSP FOR DAMAGE/ELEC ODOR, NONE FOUND. CIRCUIT CARDS IN P6 PNL INSP , M560 FOUND W/ OVERHEATED CAPACITOR FOR BATT CHARGER CIRCUIT. REPLACED CAPACITOR. RAN ENGS AT T/O PWR, OPERATING EQUI P FOR T/O, NO SMELL. MAIN BATT & BATT CHARGER REPLACED. MAIN BATT TESTED AT VENDOR, NO FAULT FOUND. CHARGER FAILED AU TO MODE TEST W/ LOW VOLT OUTPUT, TRANSISTOR Q9 FOUND DEFECT ON COMPT ASSY MODE CNTL CIRCUIT & REPLACED. 2 L 7 2 4F RT A16WE 2002031100107 20020311 00107 EU 2002 3 11 AWXA200200188 1 20020302 A 5210 FE174004 DAMPENER AIRBUS 320 A320231 3930325 EU R2 DOOR LEAKING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 55 YWG - DOOR SYSTEM - C - DURING C-02 CHECK DOOR ASSIST CYLINDER FOR THE R2 DOOR WAS FOUND TO HAVE NO DAMPENING ACTION. M AINTENANCE REMOVED, REPLACED, AND RIGGED THE R2 DOOR DAMPER ASSIST CYLINDER IAW AMM 52-11-14-052, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002031100108 20020311 00108 EU 2002 3 11 AWXA200200189 1 20020302 A 5210 FE174004 DAMPENER AIRBUS 320 A320231 3930325 EU L1 DOOR LEAKING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 55 YWG - DOOR SYSTEM - C - DURING C-02 CHECK DOOR ASSIST CYLINDER FOR THE L1 DOOR WAS FOUND TO HAVE NO DAMPENING ACTION. M AINTENANCE REMOVED, REPLACED, AND RIGGED THE L1 DOOR DAMPER ASSIST CYLINDER IAW AMM 52-11-14-052, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002031100109 20020311 00109 EU 2002 3 11 AWXA200200190 1 20020303 A 2910 B-NUT AIRBUS 320 A320231 3930325 EU HYDRAULIC SYS LOOSE A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 629AW 076 IAH - DIVERSION - FLT 555 - C - EN ROUTE FROM MIA TO LAS AT FL 350 ECAM MESSAGE FOR GREEN HYDRAULIC SYSTEM LOW PRESSURE INFLIGHT, POWER TRANSFER UNIT AND NR 1 ENGINE HYDRAULIC PUMP WERE TURNED OFF AND AIRCRAFT DIVERTED SAFELY INTO IAH. MAI NTENANCE FOUND 2 EACH B-NUTS LOOSE AT THE HYDRAULIC POWER TRANSFER UNIT. TIGHTENED B-NUTS, SERVICED THE SYSTEM, AND PER FORMED A LEAK CHECK. 2 L 7 2 4F RT A28NM 2002031100124 20020311 00124 SW 2002 3 11 ALG2002F00007 1 20020110 A 6510 407040303109 BEARING BELL 407 407 1182206 SW ALLSN 250B 250B* GL T/R DRIVESHAFT WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 1116H 580 53046 UPON RETURN TO BASE, PILOT FELT A MOMENTARY FLIGHT VIBRATION. ONCE ON THE GROUND MAINTENANCE WAS CALLED TO INVESTIGATE. SELF CENTERING BEARING/ HOUSINGS. GO TO FLOATING BEARING HOUSING. 1 G 7 1 3U 3 T O H2SW E10CE 2002031100125 20020311 00125 SW 2002 3 11 ALG2002F00009 1 20020119 A 6510 407340339101 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/R DRIVESHAFT FAILED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 587AL 81 53248 DURING PREVENTATIVE MAINTENANCE INSPECTION, BEARING FAILED COMPLETELY, PART SCRAPPED. 1 G 7 1 3U 3 U O H2SW E1GL 2002031100126 20020311 00126 SW 2002 3 11 ALG2002F00010 1 20020128 A 5302 206032308103 FRAME BELL 407 407 1182206 SW ALLSN 250C 250C20 03013 GL TAILBOOM CRACKED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 457AL 4864 53151 ROUTINE INSPECTION, UPPER SECTION OF FRAME CRACKED ABOVE RIGHT ATTACHMENT CASTING. PROBABLE CAUSE: RIGHT UPPER SHIM ON TAILBOOM (407-030-810-119) NOT BURNISHED AT EDGES. 1 G 7 1 3U 3 U O H2SW E4CE 2002031100127 20020311 00127 SW 2002 3 11 ALG2002F00011 1 20020125 A 6320 6893672 PINION GEAR ALLSN C47B BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX GALLED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 937AL 3190 53383 CAE847240 CHIP LIGHT LUMINATED, HAVING METAL IN OIL. UPON DISASSEMBLY OF GEARBOX, FOUND EXCESSIVE GALLING ON GEAR TEETH (PINION G EAR). EXCESSIVE GALLING ON PINION GEAR DUE TO IMPROPER GEAR MESHING AND EXCESSIVE LOAD TO TORQUE AREA. INSURE GEAR HAR DNESS AND PROPER MESHING OF GEAR TEETH. 1 G 7 1 3U 3 U O H2SW E1GL 2002031100128 20020311 00128 SW 2002 3 11 ALG2002F00012 1 20020125 A 6320 23066678 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL M/R GEARBOX IMPROPER PART B ALGR K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 937AL 3190 53383 CAE847270 UPON REPAIRS OF GEARBOX, BEARING RACE HAVING TWO SERIAL NUMBERS ETCHED ON RACE. TO PREVENT RECURRENCE: PROPER IDENTIFICA TION OF PART BEFORE LEAVING FACTORY. 1 G 7 1 3U 3 U O H2SW E1GL 2002031100129 20020311 00129 SW 2002 3 11 ALG2002F00013 1 20020204 A 2910 70061J175W216A HOSE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL HYD SYSTEM CRACKED B ALGR K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 457AL 53151 CAE847197 HYDRAULIC SYSTEM, DEFECT FOUND DURING UNSCHEDULED MAINTENANCE. SOCKET CRACKED. 1 G 7 1 3U 3 U O H2SW E1GL 2002031100130 20020311 00130 NM 2002 3 11 AWXA200200192 1 20020303 A 3350 BR964411 LIGHT BOEING 737 73733A 1384673 NM CABIN MISSING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 LCQ - EEL - C - DURING C-16 CHECK AT LCQ SEAT ROW 3 LT WAS FOUND TO HAVE 2 MISSING SEAT MOUNTED EMERGENCY ESCAPE PATH LI GHT ASSEMBLIES. MAINTENANCE INSTALLED 2 EACH EMERGENCY ESCAPE PATH LIGHT ASSEMBLIES ON SEAT ROW 3 LT PER EO 33-50-34, R EV A, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002031100131 20020311 00131 SW 2002 3 11 ALG2002F00014 1 20020124 A 6310 406040516101 SHAFT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TRANSMISSION WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 58236 4972 53069 CAE847085 INPUT SHAFT, DURING 2500 HOUR OVERHAUL, SPLINES WORN BELOW MINIMUM LIMITS. 1 G 7 1 3U 3 U O H2SW E1GL 2002031100132 20020311 00132 EU 2002 3 11 AWXA200200193 1 20020305 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU L2 DOOR DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 PHX - DOOR SYSTEM - C - L2 DOOR ASSIST BOTTLE LOW. MAINTENANCE SERVICED THE DOOR ASSIST BOTTLE IAW AMM 52-10-00-610-001 . 2 L 7 2 4F RT A28NM 2002031100133 20020311 00133 SW 2002 3 11 ALG2002F00015 1 20020120 A 6510 407340339101 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/R DRIVESHAFT WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 627AL 70 53284 DURING PREVENTATIVE MAINTENANCE INSPECTION, BEARINGS ROUGH AND WORN/ BEARINGS SCRAPPED. BEARINGS SHOULD BE MOUNTED IN S ELF-CENTERING HOUSING. 1 G 7 1 3U 3 U O H2SW E1GL 2002031100134 20020311 00134 SW 2002 3 11 ALG2002F00016 1 20020203 A 6220 407310101101 BEARING BELL 407 BELL 407 407 1182206 SW M/R HEAD SEPARATED A ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 697AL 1855 A398 53374 DURING INSPECTION AT FIELD BASE. ELASTOMER SEPARATION. 1 G 7 1 3U O H2SW 2002032000064 20020320 00064 2002 3 20 AWXA200200197 4 20020307 A 3425 H321BHM1 INDICATOR AIRBUS 320 A320231 3930325 EU COCKPIT FAILED A AWXA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 WP 28 634AW 12226 5424 091 LAS - DIVERSION - FLT 790 - "S" - DURING CRUISE STANDBY HORIZON INDICATOR FAILED, AIRCRAFT DIVERTED TO LAS. MAINTENANCE REPLACED STANDBY HORIZON INDICATOR AND PERFORMED AN OPERATIONAL CHECK IAW T/C 34-22-24-04. AIRCRAFT CONTINUED TO PDX WIT H OUT INCIDENT. BENCH TEST OF STANDBY HORIZON INDICATOR CONFIRMED FAILURE OF COMPONENT, THE FOLLOWING PARTS WERE REPLACE D; THE LAMP, A SCREW, A PIVOT, 3 EACH BEARINGS, AND A REDUCTION GEAR. REDUCTION GEAR, P/N; H140ADY10, BEARING, P/N; A118 6448. 2 L 7 2 4F RT A28NM 2002031100136 20020311 00136 NM 2002 3 11 C1HA200282010 1 20020302 A 3350 POWER SUPPLY BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 682CA 22019 FIXED INTERIOR EMERGENCY AREA LIGHTS AT AFT ENTRY INOP, 2 ROUND LIGHTS POINTING DOWN. REMOVED AND REPLACED BATTERY POWE R SUPPLY FOR AFT ENTRY IAW MM 33-50-71. EMERGENCY LIGHTS OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002031100137 20020311 00137 WP 2002 3 11 CHI2002F00000 1 20020118 A 6720 369A75058 BRACKET HUGHES 369 369D 4470706 WP ALLSN 250C 250C20 03013 GL TAIL ROTOR CRACKED B CHIR K NONE O OTHER IN INSP/MAINT 1 NM 09 502CH 14288 180252D LT TORQUE PEDAL BRACKET FAILED PRIOR TO ENG START ON GROUND. FAILED BRKT ASSY WAS SENT TO LOCAL LAB FOR FRACTOGRAPHIC EXAMINATION. -7 (RT) BRACKET FROM SAME HELICOPTER AND BOTH -8 AND -7 BRACKETS FROM SECOND HELICOPTER WERE REMOVED FOR V ISUAL AND NDT INSP. EVIDENCE OF FATIGUE CRACK IN A RADIUS AT UPR LT (PILOTS LT SIDE) MTG FLANGE. FATIGUE CRACKS INCREA SE TO A LENGTH OF APPROX. .1250 TO .1875 INCH PRIOR TO FINAL OVERLOAD, SUGGEST A HIGH CYCLIC STRESS MAGNITUDE AND A LOW NUMBER OF STRESS CYCLES TO FAILURE. 3 OF THE 4 MTG FLANGES HAD BROKEN OFF. CRACK THROUGH UPPER LT MTG FLANGE EXHIBITED . FRACTURE OCCURED AT AN INSIDE CORNER. THE TOTAL TIME OF THE SECOND HELI WAS 13,854. 1 G 7 1 3U 3 U H3WE E4CE 2002031100138 20020311 00138 WP 2002 3 11 CHI2002F00001 1 20020118 A 6720 369A75058 BRACKET HUGHES 369 369D 4470706 WP ALLSN 250C 250C20 03013 GL TAIL ROTOR CRACKED B CHIR K NONE O OTHER IN INSP/MAINT 1 NM 09 501CH 13854 170050D LEFT TORQUE PEDAL BRACKET FAILED PRIOR TO ENG START ON GROUND. FAILED BRACKET WAS SENT TO LOCAL LAB FOR FRACTOGRAPHIC EXAMINATION. -7 (RT) BRACKET FROM SAME HELICOPTER AND BOTH -8 AND -7 BRACKETS FROM SECOND HELICOPTER WERE REMOVED FOR V ISUAL AND NDT INSP. EVIDENCE OF FATIGUE CRACK IN A RADIUS AT UPR LT (PILOTS LT SIDE) MTG FLANGE. FATIGUE CRACKS INCREA SE TO A LENGTH OF APPROX. .1250 TO .1875 INCH PRIOR TO FINAL OVERLOAD, SUGGEST A HIGH CYCLIC STRESS MAGNITUDE AND A LOW NUMBER OF STRESS CYCLES TO FAILURE. 3 OF THE 4 MTG FLANGES HAD BORKEN OFF. CRACK THROUGH UPPER LT MOUNTING FLANGE EXH IBITED. FRACTURE OCCURRED AT AN INSIDE CORNER. THE TOTAL TIME OF THE SECOND HELICOPTER WAS 13,854. 1 G 7 1 3U 3 U H3WE E4CE 2002031100139 20020311 00139 EU 2002 3 11 HCM2002F00000 1 20020219 A 2150 0500521 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE EVAPORATOR FAILED A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 532BH 2494 4402 PILOT EXPERIENCED A RATTLING NOISE IN THE FORWARD PORTION OF THE CABIN DURING HIS SIGHTSEEING FLIGHT. THE PILOT ELECTED TO MAKE A PRECAUTIONARY LANDING, A MECHANIC WAS DISPATCHED TO THE SCENE AND DETERMINED THE PROBLEM TO BE A FAULTY FORWA RD AIR CONDITIONING BLOWER MOTOR. THE MAINTENANCE ITEM WAS DEFERRED IAW APPROVED MINIMUM EQUIPMENT LIST AND THE AIRCRAF T WAS FLOWN BACK TO BASE FOR REPAIR. PROBABLE CAUSE WILL BE DETERMINED AT OVERHAUL. INCREASED INSPECTIONS WILL PREVENT RECURRENCE. 1 G 7 1 3U 3 U NC H9EU E19EU 2002031100142 20020311 00142 SW 2002 3 11 PN12002F00001 1 20020207 A 2760 269A5497800 PULLEY HUGHES 269 269C1 8059504 SW LYC O360 HIO360* 41514 EA ELEVATORS LOOSE B PN1R K NONE O OTHER IN INSP/MAINT 1 EA 17 204HF 790 0109 DURING ROUTINE INSPECTION FOUND AFT LOWER PULLEY DRIVE BEARING WAS LOOSE ON THE SHAFT. SENT TO SAC FOR ELEVATOR. PRODU CT SUPPORT REPORTED THE AFT BEARING I.D. WAS OVERSIZED WHICH CAUSED THE LOOSENESS. THE AFT BEARING WAS REPLACED. 1 G 7 1 3O 3 O O 4H12 1E10 2002031100143 20020311 00143 EU 2002 3 11 S6G2002F00000 1 20020213 A 7921 1090401211 PIN AGUSTA A109 A109A2 0260120 EU ALLSN 250C 250C20B 03013 GL OIL COOLER SHEARED E S6GA K NONE O OTHER IN INSP/MAINT 1 GL 15 80NM 7327 CAE835751 DURING PREFLIGHT, PILOT FOUND NR1 ENGINE OIL COOLER FAN DRIVESHAFT DAMAGED. SHEAR BOLT BETWEEN NR1 ENGINE COUPLING ADAP TER AND DRIVE FAN ADAPTER FAILED ALLOWING DRIVE FAN ADAPTER TO MIGRATE AFT AND DISENGAGE SPLINES OF ENGINE PTO SHAFT. T HE OIL COOLER DIRVESHAFT STRUCK NR 6, NR 7 BEARING STRUT SUMP, DENTING IT AND CAUSING OIL LEAK, BROKE TURBINE COLLECTOR DRAIN FITTING AND BENT SHAFT. OIL COOLER FAN SPLINED DRIVESHAFT SHEARED AND OIL COOLER RIGHT MOUNT AREA CRACKED. FORWA RD THOMAS COUPLING SHREDDED. HARDWARE WAS INTACT OTHER THAN SHEAR BOLT, COTTER PIN WAS STILL IN PLACE IN SECTION OF BO LT THAT SHEARED OFF. REPLACED ALL DAMAGED PARTS. SHEAR BOLT SHOULD BE INSPECTED IN DETAIL AT EVERY SCHEDULED REMOVAL. 1 G 7 2 3U 3 U H7EU E4CE 2002031100144 20020311 00144 NM 2002 3 11 C1HA200285002 1 20020104 A 5753 FITTING BOEING 727 7272S7 138407Z NM T/E FLAP LOOSE A C1HA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 15 685CA 22492 AFTER DEPARTING, FELT VIBRATION THROUGH A/C. VISUALLY INSPECTED THROUGH L2 DOOR. O/B FLAP AILERON AND BALANCE TAB SEEN VIBRATING VIOLENTLY. FL 350-.81 .75 AND STILL VIBRATED, RECHECKED ON DESCENT THROUGH 15000, AND 250 KTS. SIGNIFICANTL Y REDUCED VIBRATION BUT STILL VISUALLY SEE TAB SHAKING. FOUND LT O/B AFT FLAP ECCENTRIC LOOSE. TIGHTENED AND ADJUSTED O/B ECCENTRICS IAW MM 27-51-12. CYCLED FLAPS, NO EXCESSIVE PLAY NOTED AS PREVIOUS TO ADJUSTMENT. 2 L 7 3 4F A3WE 2002031100145 20020311 00145 NE 2002 3 11 ULX2002F00000 2 20020205 A 7321 0164248850 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE LEAKING B ULXR K NONE K FLUID LOSS IN INSP/MAINT 1 WP 01 229LA 73 3317 9699 DURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, DIRECTLY UNDER THE ENGINE DECK DRAIN. FURTHER IN SPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FCU WAS NECESSARY TO CORRECT THIS PROBLEM. MF G HAS NOT OFFERED A CAUSE FOR THIS LEAK. 1 G 7 1 3U 3 U H9EU E19EU 2002031100146 20020311 00146 NM 2002 3 11 C1HA200294002 1 20020301 A 5610 58935722 WINDOW BOEING 727 727290 138408W NM COCKPIT CRACKED A C1HA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 294AS 22146 UPON CLIMBOUT, FOUND R4 COCKPIT WINDOW CRACKED. PERFORMED COM 2.56.3 PROCEDURE. SPOKE WITH MX AND RETURNED TO MSP. RE MOVED AND REPLACED NR 4 (FO'S SIDE) COCKPIT WINDOW IAW M/M 56-11-31. NO DEFECTS NOTED, OK FOR SERVICE. 2 L 7 3 4F A3WE 2002031100147 20020311 00147 NE 2002 3 11 ULX2002F00001 2 20020205 A 7321 0164248850 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE LEAKING B ULXR K NONE O OTHER IN INSP/MAINT 1 WP 01 221LA 3220 9674 DURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, DIRECTLY UNDER THE ENGINE DECK DRAIN. FURTHER IN SPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FUEL CONTROL UNIT WAS LEAKING FROM THE FUEL C ONTROL UNIT DRAIN. REPLACEMENT OF THE FCU WAS NECESSARY TO CORRECT THIS PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002031100148 20020311 00148 NE 2002 3 11 ULX2002F00002 2 20020205 A 7321 0164248850 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE LEAKING B ULXR K NONE K FLUID LOSS IN INSP/MAINT 1 WP 01 229LA 1388 3317 9699 DURING ROUTINE INSPECTION, A PUDDLE OF FUEL WAS NOTICED ON THE GROUND, DIRECTLY UNDER THE ENGINE DECK DRAIN. FURTHER IN SPECTION IDENTIFIED THE SOURCE OF THE LEAK AS THE FUEL CONTROL UNIT. THE FUEL CONTROL UNIT WAS LEAKING FROM THE FUEL CO NTROL UNIT DRAIN. REPLACEMENT OF THE FUEL CONTROL WAS NECESSARY TO CORRECT THIS PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002031100149 20020311 00149 SW 2002 3 11 WIP2002F00000 1 20020104 A 6510 407340339103 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR FAILED E K NONE O OTHER IN INSP/MAINT 1 WP 05 911FS 780 53424 MAIN ROTOR BEARING FAILIED. 1 G 7 1 3U 3 U O H2SW E1GL 2002031100150 20020311 00150 SO 2002 3 11 C2XA02CL065 1 20020305 A 3233 1300B000002 ACTUATOR EMB 145 EMB145LR 3260212 SO NLG LEAKING A C2XA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SW 27 13538 723 145527 CLE FLIGHT 3138 THE CREW REPORTED A VERY EXTREME VIBRATION FROM THE NOSE AREA WHILE THE GEAR WAS INTRANSIT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR ACTUATOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002031100151 20020311 00151 SW 2002 3 11 WIP2002F00001 1 20020125 A 7332 407362013101 SWITCH BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUEL PRESSURE FAILED E WIPA K NONE O OTHER IN INSP/MAINT 1 WP 05 911FS 802 53424 FUEL PRESS SWITCH FAILED, REMOVED AND REPLACED WITH NEW. 1 G 7 1 3U 3 U O H2SW E1GL 2002031100152 20020311 00152 SW 2002 3 11 WIP2002F00002 1 20020109 A 2910 407076018101 REDUCER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL HYD SYSTEM FAILED E WIPA K NONE O OTHER IN INSP/MAINT 1 WP 05 911FS 780 53424 REDUCER TUBE ASSEMBLY, REMOVED HYDRAULIC REDUCER AND TUBE ASSEMBLY, INSTALLED NEW REDUCER AND TUBE ASSEMBLY. 1 G 7 1 3U 3 U O H2SW E1GL 2002031100153 20020311 00153 SO 2002 3 11 C2XA02IA050 1 20020302 A 5315 14521700001 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 7291 145131 IAH - MAINTENANCE FOUND CORROSION OUT OF LIMITS ON THE FLOORBEAM AT FRAME 20. A SPLICE REPAIR WAS ACCOMPLISHED ON THE A FFECTED AREA OF FLOORBEAM IN ACCORDANCE WITH THE EMB SRM 53-21-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002031100154 20020311 00154 NM 2002 3 11 CALA0200114 1 20020301 A 5347 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND FORWARD CARGO RT TIE DOWN RAIL CORRODED AT BS 500B-500D. A NEW SECTION OF TIE DOWN RAIL WAS SPLICED IN IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002031100155 20020311 00155 NM 2002 3 11 CALA0200116 1 20020302 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND LT AFT UPPER SURFACE OF KEEL BEAM FLANGE HAD WORN HOLES ON UPPER SURFACE FROM PANEL ATTACH NUTS AT STA 719-727. REPAIRED IAW ECRA 5310-03740. 2 L 7 2 4F RT A16WE 2002031100156 20020311 00156 WP 2002 3 11 CALA0200120 1 20020303 A 2121 6054573 FAN DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 33817 31749 49371 SMOKE ENTERED THE CABIN WHILE AT CRUISE EN ROUTE TO TPA. THE RECIRCULATING FAN C/B'S ALSO POPPED. THE CABIN TEMP WAS L OWERED AND GALLEY POWER WAS REMOVED. THE SMOKE DISSIPATED AND THE AIRCRAFT LANDED SAFELY AT TPA. THE RECIRCULATING FAN WAS REMOVED AND REPLACED. 2 L 7 2 4F A6WE 2002031100157 20020311 00157 2002 3 11 CHQ000130 4 20020306 A 3423 COMPASS EMB 145 EMB145 3260210 SO COCKPIT OUT OF TOLERANCE A CHQA K NONE J WARNING INDICATION CL CLIMB 1 GL 11 271 145305 DURING CLIMBOUT RECEIVED AN AMBER HEADING MESSAGE ON BOTH PFD'S. PERFORMED COMPASS SWING AND FLUX DETECTOR TEST, OPS CH ECK GOOD. 2 L 7 2 4F RT T00011AT 2002031100158 20020311 00158 SO 2002 3 11 CHQ000131 1 20020307 A 3610 DUCT EMB 145 EMB145 3260210 SO CARGO BAY LEAKING A CHQA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 274 145344 BLEED LEAK IN CARGO BIN, FIRE BOTTLES DISCHARGED, AND OVERWEIGHT LANDING. 2 L 7 2 4F RT T00011AT 2002031100159 20020311 00159 EU 2002 3 11 DHL2002364500 1 20020216 A 5711 SPAR AIRBUS 300 A300B4203 3930306 EU LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 LEFT WING REAR SPAR BETWEEN RIB 19 AND 22 HAS LIGHT CORROSION ON AFT FACE SPAR. REMOVED CORROSION IAW A300SRM 51-40-11. 2 L 7 2 4F RT A35EU 2002031100160 20020311 00160 EU 2002 3 11 DHL2002364501 1 20020215 A 5320 CHANNEL AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 AFT CABIN FLOOR STRUCTURE AT FRAME STA 75 LT TO FRAME STA 75A LT 8 SQ INCH OF CORROSION ON CHANNEL CONNECTED TO THRESHOL D PAN. REMOVED CORROSION PER SRM 51-40-11. 2 L 7 2 4F RT A35EU 2002031100163 20020311 00163 EU 2002 3 11 DHL2002364502 1 20020220 A 5320 INTERCOSTAL AIRBUS 300 A300B4203 3930306 EU FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 INTERCOSTAL WEB AT FR STA 47 HAS 1 INCH CRACK THROUGH FASTENER HOLE LT. REPAIRED WEB IAW A300 SRM 51-41-20. 2 L 7 2 4F RT A35EU 2002031100166 20020311 00166 EU 2002 3 11 DHL2002364503 1 20020216 A 5730 SKIN AIRBUS 300 A300B4203 3930306 EU RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 TWO SQ INCHES OF LEVEL 1 CORROSION AT RIB 7A, TRAILING EDGE OF BOTTOM SKIN IN BOOSTER BAY RT WING. REMOVED CORROSION PE R SRM 51-40-11 A300. 2 L 7 2 4F RT A35EU 2002031100167 20020311 00167 SO 2002 3 11 C2XA02CL067 1 20020307 A 3234 355022002MOD3 CONTROL UNIT EMB 135 EMB135LR 3260305 SO COCKPIT INTERMITTENT A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 12519 145366 CLE FLIGHT# 3242 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE UPON GEAR RETRACTION.THE AIRCRAFT LANDED WITHOUT FURTHE R INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2002031100169 20020311 00169 SO 2002 3 11 C2XA02BT007 1 20020310 A 2530 CONNECTOR EMB 145 EMB145LR 3260212 SO DAMAGED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 16981 145208 EWR---CO3374, CREW REPORTED BURNING ODOR FROM COFFEE JUG AREA....MAINTENANCE REMOVED AND REPLACED CONNECTOR FOR COFFEE J UG IAW EMB145 WIRING MANUAL 25-31-50. OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002031500132 20020315 00132 EU 2002 3 15 DHL2002364504 1 20020218 A 5720 A5726021320300 BEAM AIRBUS 300 A300B4203 3930306 EU RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 RT OUTBOARD TOP SIDE AT WING TIP INSIDE OUTER COVER PLATE, THERE IS CORROSION. REMOVED WING TIP PER AMM 57-24-11 TO ACC ESS CORROSION, R&R NEW BEAM PER A300 SRM. 2 L 7 2 4F RT A35EU 2002031100170 20020311 00170 EU 2002 3 11 DHL2002366002 1 20020305 A 2510 SEAT BELT AIRBUS 300 A300B4203 3930306 EU COCKPIT WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 S/O LAP BELT WORN AND TSO UNREADABLE. REMOVED AND REPLACED S/O LAP BELT PER 25-11-13, CHECK GOOD. 2 L 7 2 4F RT A35EU 2002031100172 20020311 00172 NM 2002 3 11 375PA0001 1 20020310 A 3220 TIRE BOEING 737 7373Y0 1384671 NM A PIDA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 05 375PA 0878 23812 Right nose tire failed on take-off at V1 - seperation of tread. R&R both nose wheel/tire assy.'s Inspected A/C IAW MM.Fe rried A/C. R&R'd E&E door, nose prox sensor and associated wiring. 2 L 7 2 4F RT A16WE 2002031100177 20020311 00177 2002 3 11 C2XA02BT008 4 20020309 A 3425 7004544712 SYMBOL GENERATOR AEROSP ATR42 ATR42320 8680930 EU COCKPIT FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 86842 286 SYR---CO3549, CREW REPORTED CAPTAINS EFIS TUBES BOTH BLANK. STRONG PLASTIC BURN ODOR IN COCKPIT. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED #1 SYMBOL GENERATOR IAW ATR42 JIC 34-25-82. OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2002031100179 20020311 00179 SO 2002 3 11 C2XA02CL069 1 20020308 A 3350 1317 BULB EMB 145 EMB145ER 3260211 SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14942 145037 DURING ROUTINE MAINTENANCE CHECK MAINTENANCE FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE.MAINTEN ANCE REPLACED THE LEFT AND RIGHT OVERWING LIGHTS.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002031100180 20020311 00180 NM 2002 3 11 AWXA200200207 1 20020220 A 5311 6545775 SKIN BOEING 737 737277 1384570 NM IMPROPER A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 LCQ - MAJOR REPAIR - "C" - DURING C-14 CHECK TWO DOUBLER REPAIRS AT BS 727A TO BS 767 WERE FOUND TO BE TO CLOSE IN PROXI MITY. MAINTENANCE REMOVED SECTION OF FUSELAGE SKIN BETWEEN BS 727 TO BS 776.9, AND STR 20 TO 25 R/H, FABRICATED 2 EACH F ILLERS, DOUBLERS, AND TRIPLERS, AND NEW SECTION OF SKIN, AND INSTALLED REPAIR PARTS IAW AWA DWG AW5361001. 2 L 7 2 4F RT A16WE 2002031100181 20020311 00181 NM 2002 3 11 AWXA200200208 1 20020220 A 5315 BAC1520792 SEAT TRACK BOEING 737 737277 1384570 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 LCQ - MAJOR REPAIR - "C" - DURING C-14 CHECK CORROSION WAS FOUND ON SEAT TRACK AT BS 328, RBL 42. MAINTENANCE REMOVED CO RROSION BLENDED DAMAGED AREA, MATERAIL LOSS OUT OF LIMITS PER B737-200 SRM 51-20-2 PG.20. CUTOUT DAMAGED SECTION OF SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED REPAIR IAW B737-200 SRM 51-30-2, PG. 13 & 14. 2 L 7 2 4F RT A16WE 2002031100182 20020311 00182 SO 2002 3 11 C2XA02CL073 1 20020310 A 3350 78241REVE INVERTER EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA O OTHER L NO TEST UK UNKNOWN 1 SW 27 17507 145215 CLE FLIGHT#3098 THE CREW REPORTED THE EMERGENCY LIGHT BELOW THE COCKPIT DOOR WAS INOPERATIVE.MAINTENANCE REPLACED THE #1 EMERGENCY LIGHT INVERTER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002031100183 20020311 00183 EA 2002 3 11 SWIA200210642 1 20020208 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA O2 SERVICE OPEN A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 597SW 7293 STALL FAIL MESSAGE ONCE AIRBORNE. RETURNED TO SLC. FOUND O2 SERVICE DOOR OPEN. INSPECTED DOOR AND SECURED DOOR. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002031100184 20020311 00184 EA 2002 3 11 SWIA200210643 1 20020208 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 408SW 7055 TAKEOFF OUT OF SLC NOSE GEAR FAILED TO COME UP AND HAD GEAR DISAGREE MESSAGE. GEAR DOWN PER QRH. GEAR DISAGREE MESSAGE DISAPPEARED. RETURNED TO SLC. REPLACED NOSE LANDING GEAR DOOR SELECTOR VALVE AND A NLG SELECTOR VALVE IAW MM 32-22-20 & 32-33-10. LANDING GEAR FUNCTION CHECK & NWS CHECK GOOD. NO LEAKS NOTED. 2 L 7 2 4F RT A21EA 2002031100185 20020311 00185 SO 2002 3 11 SWIA200210644 1 20020209 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN DISCONNECTED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 232SW 120306 EMERGENCY POD LIGHT IN 6A IS INOP. FERRIED UNDER SPECIAL FLIGHT PERMIT FORM MOD TO SFO. FOUND BOTH WIRES NOT CONNECTED TO THE SOCKET ON OVERHEAD EMERGENCY LIGHT ASSEMBLY SEAT 6A. RECONNECTED WIRES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002031100186 20020311 00186 EA 2002 3 11 SWIA200210646 1 20020202 A 7931 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 498SW 7483 DURING FLIGHT OIL PRESSURE MESSAGE ILLUMINATED, ENGINE WAS SHUT DOWN PER QRH. DIVERTED TO IDA. INSPECTED RIGHT ENGINE FOR OIL LEAKAGE AND PROPER OIL SERVICE LEVEL. PERFORMED VISUAL OIL LEVEL INSPECTION OF AGB. RAN AIRCRAFT ON GROUND FOR APPROXIMATELY 1 HOUR. COULD NOT DUPLICATE. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2002031100187 20020311 00187 SO 2002 3 11 SWIA200210647 1 20020201 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO E/E BAY DOOR OUT OF ADJUST A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 270YV 120270 SERVICE DOOR LIGHT ILLUMINATES DURING POWER UP FOR TAKEOFF. ADJUSTED AVIONICS BAY SERVICE DOOR MICRO SWITCH. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002031100188 20020311 00188 EA 2002 3 11 SWIA200210648 1 20020202 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA OXYGEN SERVICE OPEN A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 429SW 7518 STALL FAIL MESSAGE AFTER TAKEOFF. RETURNED TO SLC. FOUND OXYGEN SERVICE DOOR OPEN, CLOSED DOOR. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002031100189 20020311 00189 2002 3 11 SWIA200210649 4 20020214 A 2210 CIRCUIT BOARD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AUTOPILOT SYS FAULTY A SWIA O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED CR CRUISE 1 NM 07 439SW 7578 AFTER EXCEEDING 250 KTS IAS, RUDDER FLUTTERED UNTIL AIRCRAFT WAS IN LANDING CONFIGURATION. REMOVED AND REPLACED LEFT (U PPER) LHP-4000 CARD IAW A/C MM 22-12-01. OPS CHECKED GOOD ON GROUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2002031100190 20020311 00190 2002 3 11 SWIA200210650 4 20020210 A 3418 STALL WARNING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FALSE ACTIVATION A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 439SW 7578 ON ROTATION RECEIVED STALL FAIL CAUTION MESSAGE. PERFORMED APPROPRIATE QRH PROCEDURE. RETURNED TO SLC. RESET STALL CO MPUTER CIRCUIT BREAKERS CBP-1 Q2 CBP-4 C7 AND CLEARED THE MEMORY. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002031100191 20020311 00191 SO 2002 3 11 SWIA200210651 1 20020115 A 5320 BRACKET EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 120290 FUSELAGE FRAME CRACKED BEHIND CAPTAIN'S DV WINDOW. REPLACED AFFECTED BRACKET IAW EMB120 SRM 51-10-02. 2 L 7 2 4T RT A31SO 2002031100192 20020311 00192 SO 2002 3 11 SWIA200210652 1 20020213 A 7714 3039242 SENSOR EMB 120 EMB120ER 3260203 SO LT ENGINE READS HIGH A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 393SW 120330 LEFT EEC IS INOP. HOOKED UP EEC BREAKOUT BOX, FOUND NH SENSOR READING HIGH. REMOVED AND REPLACED LEFT NH SENSOR WITH A SERVICEABLE UNIT. TRIMMED LEFT ENGINE. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME. 2 L 7 2 4T RT A31SO 2002031100193 20020311 00193 SO 2002 3 11 SWIA200210653 1 20020219 A 3010 29S70513532 BOOT EMB 120 EMB120ER 3260203 SO HORIZ STAB DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 199SW 120237 LEADING EDGE OUTBOARD RIGHT, LEFT AND VERTICAL STAB FAILURES ON BOTH DEICE TIMERS AT BOTH HIGH AND LOW POWER SETTINGS. OUTSIDE TEMP -6 DEGREES CELISUS AT 12,000 - 20,000 MSL. REMOVED AND REPLACED RIGHT HORIZONTAL DEICE BOOT IAW MM 30-10-0 0. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002031100194 20020311 00194 SO 2002 3 11 SWIA200210654 1 20020219 A 2731 SENSOR EMB 120 EMB120RT 3260202 SO ELEVATOR TAB CORRODED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 269UE 4956 4956 120194 TAKEOFF TRIM AURAL WARNING OCCURRED DURING INITIAL PART OF TAKEOFF ROLL. TRIM WAS SET IN THE MIDDLE OF THE GREEN BAND. INSPECTED WIRING AND CLEANED CORROSION AT ELEVATOR TRIM SENSORS. OPERATED SYSTEM, COULD NOT DUPLICATE. 2 L 7 2 4T RT A31SO 2002031100197 20020311 00197 2002 3 11 WRLA200202 4 20020209 A 3414 HG280D80 INDICATOR DOUG DC10 DC1030F 3023504 WP COCKPIT INOPERATIVE A WRLA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SO 11 304WL 47928 DURING TAKEOFF ROLL, CAPTAIN AIR SPEED INDICATOR REMAINED AT 0 KNOTS WITH NO FLAG INDICATED ON FIRST OFFICERS AIR SPEED INDICATED NORMAL. REJECTED TAKEOFF AT APPROXIMATELY 95 KNOTS. 2 L 7 3 4F RT A22WE 2002031100198 20020311 00198 2002 3 11 2002F00183 4 20020211 A 3130 A15802 FLIGHT RECORDER DOUG DC10 DC1010 3022110 WP CABIN FAULTY A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 FUNCTIONAL CHECK OF DIGITAL FLIGHT DATA RECORDER REVEALED FAILURE OF GMT CLOCK INPUT AND ATTITUDE REFERENCE INPUT. (M) 2 L 7 3 4F A22WE 2002031100199 20020311 00199 2002 3 11 2002F00184 4 20020211 A 3130 ED7429513 FLIGHT RECORDER DOUG DC10 DC1010 3022110 WP CABIN FAULTY A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 FUNCTIONAL CHECK OF DIGITAL FLIGHT DATA RECORDER REVEALED FAILURE OF GMT CLOCK INPUT AND ATTITUDE REFERENCE INPUT. (M) 2 L 7 3 4F A22WE 2002031100200 20020311 00200 NM 2002 3 11 2002F00185 1 20020208 A 2611 SMOKE DETECTOR BOEING 727 727222 1384073 NM CARGO BAY MALFUNCTIONED A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 7640U 19913 FOUND CARGO SMOKE DETECTOR LIGHT ILLUMINATED DURING CLIMB OUT FROM MDT. AIRCRAFT RETURNED TO MDT AND LANDED WITHOUT INC IDENT. NO EMERGENCY WAS DECLARED. (M) 2 L 7 3 4F A3WE 2002031100201 20020311 00201 WP 2002 3 11 2002F00186 1 20020206 A 5320 S2929169 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 FOUND FLOOR SUPPORT BEAM CORRODED AT STATION 1021 TO STATION 1887. (M) 2 L 7 3 4F A22WE 2002031100202 20020311 00202 WP 2002 3 11 2002F00187 1 20020206 A 5320 S2929169 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 FOUND J-SECTION FLOOR SUPPORT CORRODED AT STATION 1921. (M) 2 L 7 3 4F A22WE 2002031100203 20020311 00203 WP 2002 3 11 2002F00188 1 20020206 A 2520 DC1003040045 PLATE DOUG DC10 DC1010 3022110 WP F/A SEAT CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 AFT FLIGHT ATTENDANT SEAT BASE PLATE CORRODED AT STATION 1900. (M) 2 L 7 3 4F A22WE 2002031100204 20020311 00204 WP 2002 3 11 2002F00189 1 20020206 A 5320 S2929169 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 FOUND J SECTION SUPPORT CORRODED AT STATION 1887. (M) 2 L 7 3 4F A22WE 2002031100205 20020311 00205 WP 2002 3 11 2002F00190 1 20020206 A 5320 S4929151 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 FOUND FLOOR SUPPORT BEAM CORRODED AT STATION 1964. (M) 2 L 7 3 4F A22WE 2002031100206 20020311 00206 WP 2002 3 11 2002F00191 1 20020206 A 5320 S2929169 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 FOUND FLOOR SUPPORT J SECTION CORRODED AT STATION 1921. (M) 2 L 7 3 4F A22WE 2002031100207 20020311 00207 WP 2002 3 11 2002F00192 1 20020206 A 5320 S2929169 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 FOUND FLOOR SUPPORT BEAM CORRODED AT STATION 1902 TO STATION 1921. (M) 2 L 7 3 4F A22WE 2002031100208 20020311 00208 WP 2002 3 11 2002F00193 1 20020206 A 5320 S4929151 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 FOUND SUPPORT BEAM CORRODED AT STATION 1964 TO STATION 1902. (M) 2 L 7 3 4F A22WE 2002031100209 20020311 00209 NM 2002 3 11 2002F00194 1 20020116 A 5711 SPAR BOEING 737 7372H4 138448C NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 FOUND CORROSION ON RIGHT WING UPPER SPAR CHORD ALONG EDGE BETWEEN SPLICE PLATE AND CHORD STATION 663 OUTBOARD OF BBL 70. 85 APPROXIMATELY 3.5 INCHES LONG. (M) 2 L 7 2 4F A16WE 2002031100210 20020311 00210 NM 2002 3 11 2002F00195 1 20020114 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 54SW 21535 AFT CARGO COMPARTMENT DOOR JAMB FORWARD LOWER CORNER EXTERIOR SKIN HAS A ONE INCH CRACK AT FASTENER STATION 794. (M) 2 L 7 2 4F A16WE 2002031100216 20020311 00216 WP 2002 3 11 2002F00180 1 20020211 A 2913 414472 PUMP DOUG DC10 DC1010 3022110 WP HYDRAULIC SYS FAILED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 NR 1 AND NR 2 AUXILIARY HYDRAULIC PUMPS FAILED CHECKS. (M) 2 L 7 3 4F A22WE 2002031100217 20020311 00217 WP 2002 3 11 2002F00181 1 20020211 A 3350 08163000611 TRACK DOUG DC10 DC1010 3022110 WP CABIN DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 FOUND ESCAPE PATH FLOOR LIGHTING TRACK IS DAMAGED. (M) 2 L 7 3 4F A22WE 2002031100218 20020311 00218 2002 3 11 RAIA00203092 4 20020306 A 3417 7000700967 ADC JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 567HK 19 2 41085 5512-STL- CAPTAINS AIR DATA COMPUTER FAILED DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE #1 ADC, OPS CK OK. 2 L 7 2 4T RT A41NM 2002031100219 20020311 00219 NE 2002 3 11 RAIA00203093 2 20020308 A 7320 31055016 SENSING ELEMENT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE INOPERATIVE A RAIA E ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 CE 03 568HK 3091 41086 75073 5501-STL- LEFT ENGINE WILL NOT MAKE TARGET TORQUE. MAINTENANCE REMOVED AND REPLACED THE #1 ENGINE INLET TEMP SENSOR, OP CK OK 2 L 7 2 4T 4 T RT A41NM E18NE 2002031100220 20020311 00220 SO 2002 3 11 RAIA00203094 1 20020309 A 2730 0861DT5 VANE EMB 145 EMB145 3260210 SO INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 809HK 5435 145187 5270-PIT- CREW ALERT MESSAGE "AOA #1 INOP”. MAINTENANCE REMOVED AND REPLACED THE #1 ANGLE OF ATTACK VANE, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002031100221 20020311 00221 EU 2002 3 11 RAIA00203095 1 20020310 A 2841 7488822 GAUGE AEROSP ATR72 ATR72202 8680940 EU READS LOW A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 722TE 11849 1527 220 5540-STL - DURING CLIMB LOW FUEL QUANTITY CAUTION LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED FUEL QUANTITY GAUG E, OPS CK OK. 2 H 7 2 4T RT A53EU 2002031100222 20020311 00222 EU 2002 3 11 SIMA200203203 1 20020201 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN DISCONNECTED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 238AE 340B238 TYR - FLT 3872 - FOUND EMERGENCY LIGHT ABOVE F/A SEAT INOPERATIVE AND FORWARD FLOOR ESCAPE PATH LIGHT INOPERATIVE. FOUN D EMERGENCY BATTERY PACK CANNON PLUG DISCONNECTED, CONNECTED PACK OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2002031100223 20020311 00223 EU 2002 3 11 SIMA200203702 1 20020202 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST UK UNKNOWN 1 SW 21 499AT 499 MIA - FLT 5058 - EMERGENCY LIGHTS INOPERATIVE. RAI EMERGENCY BATTERY PACK AT 73WL. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2002031100224 20020311 00224 EU 2002 3 11 SIMA200203703 1 20020203 A 3350 MS274061 SWITCH SAAB SF340 340B 7860101 EU COCKPIT DEFECTIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 350CF 340B350 DFW - FLT 3818 - FOUND INTERIOR EMERGENCY LIGHTS CAN'T BE CONTROLLED FROM THE COCKPIT. REMOVED AND REPLACED COCKPIT EME RGENCY LIGHT SWITCH. (M) 2 L 7 2 4T RT A52EU 2002031100225 20020311 00225 EU 2002 3 11 SIMA200203704 1 20020204 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU COCKPIT LOOSE A SIMA O OTHER N FALSE WARNING LD LANDING 1 SW 21 386AE 340B386 LAX - FLT 3236 - FOUND RIGHT MLG GREEN INDICATION DID NOT COME ON WHEN GEAR WAS SELECTED DOWN. EMERGENCY WAS DECLARED A ND AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LOOSE CANNON PLUG 6GA AND RESECURED. (M) 2 L 7 2 4T RT A52EU 2002031100226 20020311 00226 EU 2002 3 11 SIMA200203705 1 20020203 A 3350 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST UK UNKNOWN 1 SW 21 541AT 541 MIA - FLT 5088 - FORWARD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. (M) 2 H 7 2 4T RT A53EU 2002031100227 20020311 00227 EU 2002 3 11 SIMA200203901 1 20020207 A 3350 AD3177 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEATS 10B AND 12B REMAIN ON WHEN SYSTEM TURNED OFF. RAI BATTERY PACK FOR FLOOR LIGHTING AT 10 AND 12B IAW SIC 33-50-00. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2002031100228 20020311 00228 EU 2002 3 11 SIMA200204204 1 20020130 A 5315 S53672409218 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 550LL 550 MBV - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION AROUND NUT PLATE HOLES ON FLOORBEAM 40. MAINTENANCE REPLACED F LOORBEAM 40 IAW ATR SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2002031100229 20020311 00229 EU 2002 3 11 SIMA200204205 1 20020130 A 5315 S53672407252 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 550LL 550 SAW - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION AROUND NUT PLATE HOLES ON FLOORBEAM 38. MAINTENANCE REPLACED F LOORBEAM 38 IAW ATR SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2002031100230 20020311 00230 EU 2002 3 11 SIMA200204206 1 20020130 A 5320 S5367800821601 SUPPORT AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 550LL 550 MBV - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE LEFT Z MEMBER INBOARD OF PASSENGER DOOR SPRING. MAINTEN ANCE REMOVED AND REPLACED THE Z-MEMBER IAW ATR SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 2002031100231 20020311 00231 EU 2002 3 11 SIMA200204207 1 20020130 A 5320 S5367800821602 SUPPORT AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 550LL 550 MBV - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE RIGHT Z-MEMBER JUST FORWARD OF SERVICE DOOR. MAINTENANC E REMOVED AND REPLACED THE Z-MEMBER IAW ATR SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 2002031100232 20020311 00232 EU 2002 3 11 SIMA200204208 1 20020130 A 5320 S5367129037202 BRACKET AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 550LL 550 SAW - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE PASSENGER DOOR SILL PLATE FORK AND AFT BRACKETS. MAINTE NANCE REMOVED AND REPLACED THE FORK (P/N S5367129034801) AND BRACKET IAW ATR SRM 51-25-04. (M) 2 H 7 2 4T RT A53EU 2002031100233 20020311 00233 NM 2002 3 11 C1HA200294004 1 20020211 A 3150 WARNING SYSTEM BOEING 727 727290 138408W NM COCKPIT MALFUNCTIONED A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 294AS 22146 ON FIRST TAKEOFF ATTEMPT, RECEIVED TAKEOFF WARNING HORN. BRAKES SET 1.4 EPR ALL ENGINES, FLAPS 15 DEGREES, APU OFF, STA B TRIM IN GREEN ARC, AND SPEED BRAKE STOWED. ON RUNWAY VERIFIED ALL POSSIBLE INPUTS. MOVED STAB TRIM REV AND FWD. THE HORN CONTINUED TO SOUND UNTIL REDUCED THRUST. MAX SPEED REACHED WAS 30 KTS. TAXIED CLEAR OF RUNWAY. RETESTED TAKEOFF WARNING HORN SYSTEM. THIS TIME IT FUNCTIONED PROPERLY. 2 L 7 3 4F A3WE 2002031100234 20020311 00234 NE 2002 3 11 C1HA200296010 2 20020219 A 7230 COMPRESSOR BOEING 727 727200 138407E NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE STALLED A C1HA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 15 696CA 22574 689989 AFTER STARTING TO APPLY T/O POWER WITH A CROSSWIND NR 2 ENGINE COMPRESSOR STALLED. INSPECTED NR 2 ENG INLET AND EXHAUST FOUND NO DAMAGE AS PER MM 71-00, OK FOR CONTINUED SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2002031100235 20020311 00235 GL 2002 3 11 C2XA02CL064 2 20020304 A 7250 TURBINE BLADES EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL NR 2 ENGINE DAMAGED A C2XA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SW 27 12957 9488 1486 145080 CAE310026 CLE FLIGHT 3303 THE CREW REPORTED ON APPROACH THE NR 2 ENGINE WOULD NOT RESPOND TO THRUST LEVER INPUT. AFTER ADVANCING LEVER RAPIDLY THE ITT SPIKED TO APPROX 800 DEGREES. THE CAPTAIN SHUT DOWN THE NR 2 ENGINE AS A PRECAUTION. THE AIRCRAF T LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND HIGH PRESSURE TURBINE BLADE DAMAGE TO 3 BLADES. THE DAMAGE WAS OUT OF LIMITS. THE ENGINE WAS REPLACED ALONG WITH THE TWO FADECS. OPERATIONAL CHECKS WERE GOOD. THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002031200114 20020312 00114 SO 2002 3 12 C2XA02TY047 1 20020311 A 5540 14525622003 ATTACH FITTING EMB 145 EMB145ER 3260211 SO RUDDER CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13929 145009 DURING A SCHEDULED 1-C INSPECTION THE LOWER RUDDER 1 STABILIZER ATTACH POINT HAS DISPLACED METAL ON RT SIDE NEAR BUSHING . 2 L 7 2 4F RT T00011AT 2002031200038 20020312 00038 EA 2002 3 12 HNAA0200030 1 20020308 A 3246 101481 NUT DHAV DHC8 DHC8311 1386006 EA #2 WHEEL ASSY DAMAGED A HNAA O OTHER O OTHER IN INSP/MAINT 1 EA 07 330EN 19471 274 DURRING WHEEL REMOVAL AND REPLACEMENT, #2 WHEEL ASSEMBLY AXEL NUT WAS FOUND DAMAGED. REPLACED NUT. 2 H 7 2 4T RT A13NM 2002031400041 20020314 00041 NM 2002 3 14 02FDEA00192 1 20020219 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FRAME IS DENTED AT BS 720A BETWEEN STR 24 AND 25 LT. REMOVED AND REPLACED FRAME PER SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2002031400045 20020314 00045 NM 2002 3 14 02FDEA00193 1 20020310 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FRAME HAS THREE DENTS AT BS 700 BETWEEN STR 22 & 25 LT. REMOVED AND REPLACED FRAME PER SRM 51-40-3 FIG 1 & EA 7-5310-62 779. 2 L 7 3 4F RT A3WE 2002031200042 20020312 00042 NM 2002 3 12 CALA0200126 1 20020308 A 5330 SKIN BOEING 737 7373T0 1384582 NM WINDOW POST CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND A 1" CRACK IN CAPTAIN'S WINDSHIELD O/B POST OUTER SKIN AT UPPER CORNER. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-01104. 2 L 7 2 4F RT A16WE 2002031200043 20020312 00043 NM 2002 3 12 CALA0200127 1 20020308 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND TWO INCH CRACKS AT THE EDGES OF THREE LIGHTENING HOLES IN C-2 DOOR INNER SKIN OVER CENTER BALANCE SPRIN GS. A 1" CRACK WAS FOUND AT THE EDGE OF A LIGHTENING HOLE IN C-2 DOOR INNER SKIN AT PULLEY ACCESS PANEL. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5230-01651 AND 5230-01652. 2 L 7 2 4F RT A16WE 2002031200044 20020312 00044 NM 2002 3 12 CALA0200128 1 20020311 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 494 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76354 23592 INSPECTION FOUND LOWER FUSELAGE SKIN BULGED AND CORRODED AT STA 494, S27R. A SKIN DOUBLER, TRIPLER, AND FILLER WERE INST ALLED IAW ECRA 5331-01108. 2 L 7 2 4F RT A16WE 2002031200048 20020312 00048 NM 2002 3 12 PCAA0202036 1 20020309 A 2720 82710038101 FITTING DHAV DHC8 DHC8102 2809003 NM LEFT CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 840EX 327 DURING ROUTINE MAINTENANCE VISIT, WHILE PERFORMING INSPECTION OF RUDDER ADJUSTMENT UPPER FITTING PER AD2002-01-25 LEFT F ITTING FOUND TO BE CRACKED. FITTING WAS REPLACED IN ACCORDANCE WITH DASH 8 MAINTENANCE MANUAL. AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2002031200052 20020312 00052 EU 2002 3 12 02070308 1 20020311 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 308 EMERGENCY TRACK LIGHTING INOP. RECONNECTED PLUG, CHECKED OK. 2 L 7 2 4T RT A41NM 2002031200075 20020312 00075 NM 2002 3 12 AWXA200200199 1 20020218 A 5315 6545410 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 YVR - MAJOR REPAIR - C - DURING C-15 CHECK OVERWING FLOORBEAM WAS FOUND CRACKED IN TWO PLACES AT BS 663. 2 L 7 2 4F RT A16WE 2002031200080 20020312 00080 NM 2002 3 12 AWXA200200200 1 20020218 A 5311 654653931 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 YVR - MAJOR REPAIR - C - DURING C-15 CHECK THE LT FUSELAGE FRAME INNER CHORD WAS FOUND CRACKED AT BS 616 JUST BELOW STR 17 LT. 2 L 7 2 4F RT A16WE 2002031200099 20020312 00099 NM 2002 3 12 AWXA200200201 1 20020218 A 5311 654653931 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 YVR - MAJOR REPAIR - C - DURING C-15 CHECK A CRACK WAS FOUND ON RT FUSELAGE FRAME INNER CHORD AT BS 616, STR 17 RT. 2 L 7 2 4F RT A16WE 2002031200100 20020312 00100 NM 2002 3 12 AWXA200200202 1 20020219 A 5315 6545410 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 YVR - MAJOR REPAIR - C - DURING C-15 CHECK DAMAGE WAS FOUND TO CLIP NUTS AT FLOORBEAM SCREW HOLES BS 540 TO BS 727, RLB 24, LBL 24. MAINTENANCE FOUND 5 HOLES BEYOND SERVICEABLE LIMITS. 2 L 7 2 4F RT A16WE 2002031200101 20020312 00101 NM 2002 3 12 AWXA200200203 1 20020219 A 5310 654797379 CREASE BEAM BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 YVR - MAJOR REPAIR - C - DURING C-15 CHECK A CRACK WAS FOUND ON CREASE BEAM ASSEMBLY INNER CHORD FRAME ATTACHMENT AT BS 616. 2 L 7 2 4F RT A16WE 2002031200102 20020312 00102 NM 2002 3 12 AWXA200200204 1 20020220 A 5743 6582764 BEAM BOEING 737 7373S3 1384711 NM RT MLG GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 YVR - MAJOR REPAIR - C - DURING C-15 CHECK THE RT MAIN LANDING GEAR ACTUATOR WALKING BEAM ATTACH BOLT WAS FOUND INSTALLE D BACKWARDS AND GOUGING INTO MAIN LANDING GEAR SUPPORT BEAM. 2 L 7 2 4F RT A16WE 2002031200103 20020312 00103 NM 2002 3 12 AWXA200200205 1 20020226 A 5320 65469212 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 YVR - MAJOR REPAIR - C - DURING C-15 CHECK A CRACK WAS FOUND ON THE FWD CARGO DOOR LOWER AREA MID INTERCOSTAL AT BEND RA DIUS. 2 L 7 2 4F RT A16WE 2002032000067 20020320 00067 EU 2002 3 20 AWXA200200206 1 20020308 A 2130 VFT300A1 VALVE AIRBUS 320 A320232 3930326 EU E/E BAY MALFUNCTIONED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 667AW 35332 3394 1710 CMH - ABORTED TAKEOFF - FLT 0287 - "O" - ON TAKEOFF ROLL OUT OF CMH ENROUTE TO PHX FLIGHT CREW RECEIVED AN AVIONIC VENT FAULT, TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. SKIN AIR VALVE REPLACED IAW AMM 21-26-53-401. THIS FAN HAD ONL Y BEEN INSTALLED FOR 6 DAYS. SDR IS STILL *OPEN* AND WILL BE UPDATED UPON RECEIPT BENCH TEST REPORT. 2 L 7 2 4F RT A28NM 2002031200104 20020312 00104 NM 2002 3 12 AWXA200200209 1 20020224 A 5315 BAC150310281 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 LCQ - MAJOR REPAIR - C - DURING C-14 CHECK CORROSION WAS FOUND ON FLOORBEAM AT BS 277. 2 L 7 2 4F RT A16WE 2002031200105 20020312 00105 NM 2002 3 12 C1HA200293002 1 20020310 A 5210 DOOR BOEING 727 727212 138407G NM L2 NOT CLOSED A C1HA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 GL 15 293AS 21348 AFTER DEPARTING F/E COULD NOT CONTROL CABIN PRESSURIZATION. F/A REPORTED LOUD NOISE WAS COMING FROM DOOR L-2. NO INDIC ATION OF L2 OPEN ON F/E PANEL. DIVERTED TO MCO AND MADE OVERWEIGHT LANDING. LANDING WAS SMOOTH. L2 DOOR FOUND TO BE I MPROPERLY CLOSED. DOOR WAS OPEN AND CLOSED PROPERLY, ALL SEALS IN GOOD CONDITION. PRESSURIZATION OPS CHECK IAW MM 21-0 0 PAGE 5. 2 L 7 3 4F A3WE 2002031200106 20020312 00106 NM 2002 3 12 C1HA200295006 1 20020303 A 7930 WARNING LIGHT BOEING 727 727290 138408W NM COCKPIT ILLUMINATED A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 295AS 22147 WITH INITIAL POWER SETTING OF 1.4 EPR HAD THE NR 1 ENGINE LOW OIL PRESSURE BYPASS LIGHT COME ON. REDUCED POWER AND CLEA RED THE RUNWAY. RAN CHECK LIST AND INITIATED TAKEOFF. 2 L 7 3 4F A3WE 2002031200107 20020312 00107 SO 2002 3 12 C2XA02BT005 1 20020311 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12921 145354 BTV---DURING RON MAINTENANCE, FOUND AFT EMERGENCY LIGHTING STRIP WIRES BROKEN. MAINTENANCE REMOVED AND REPLACED EMERGEN CY LIGHTING STRIP ON AFT PASSENGER CABIN FLOOR PANEL IAW EMB145 MM 33-50-12. OPS CHECKED, SYSTEM GOOD. 2 L 7 2 4T RT T00011AT 2002031200108 20020312 00108 SO 2002 3 12 C2XA02BT006 1 20020311 A 3230 23092900401 UPLOCK EMB 145 EMB145LR 3260212 SO NLG DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16951 145063 EWR---CO3536, CREW REPORTED NOSE LANDING GEAR DID NOT RETRACT ON TAKEOFF, CONFIRMED BY EICAS AND WIND NOISE. RECYCLED G EAR ONCE, NOSE GEAR SUCCESSFULLY RETRACTED ON SECOND ATTEMPT. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK BOX IAW EMB145 MM 32-33-07. OPS CHECKED, SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002031200109 20020312 00109 SO 2002 3 12 C2XA02CL068 1 20020308 A 3350 66368 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 29515 145309 CLE FLIGHT 3237 THE CREW REPORTED 1 SECTION OF EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY AISLE PATH LIGHTING SECTION. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT TOOO11AT 2002031200110 20020312 00110 SO 2002 3 12 C2XA02CL071 1 20020308 A 3234 CONNECTOR EMB 145 EMB145LR 3260212 SO COCKPIT DIRTY A C2XA O OTHER O OTHER CL CLIMB 1 SW 27 16954 145072 CLE FLIGHT 3262 THE CREW REPORTED THE LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION AFTER TAKEOFF. THE CREW USED THE DOWNLOCK RELEASE BUTTON AND THE GEAR RETRACTED. MAINTENANCE INSPECTED AND CLEANED THE GEAR LEVER CONNECTOR. OPERA TIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002031200111 20020312 00111 SO 2002 3 12 C2XA02CL074 1 20020310 A 2701 14531661402 YOKE EMB 145 EMB145LR 3260212 SO COCKPIT CRACKED A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 15986 145254 CLE FLIGHT 3265 THE CREW REPORTED THE FIRST OFFICERS, CONTROL YOKE IS CRACKED. MAINTENANCE REPLACED THE CONTROL YOKE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002031200113 20020312 00113 SO 2002 3 12 C2XA02IA054 1 20020219 A 5315 14522459003 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 7290 145131 IAH DURING C-CHECK INSPECTION IT WAS NOTED THAT CORROSION ON RIVET HEADS AND AROUND SCREW HOLES ON TOP OF FLOORBEAMS AT FRAME 20. 2 L 7 2 4F RT T00011AT 2002031200115 20020312 00115 NE 2002 3 12 CG8A20020004 2 20020305 A 7261 OIL FILTER BOEING 727 727223 1384074 NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE DIRTY A C8GA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 15 899AA 22015 700556 FLT 717 FROM ELP-TOL. DURING CRUISE LEVEL, THE NR 3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. FOLLOWED AOM PROCEDURES AND LIGHT REMAINED ILLUMINATED. PRECAUTIONARY SHUTDOWN ON NR 3 ENGINE ACCOMPLISHED, AIRCRAFT CONTINUE TO FI NAL DESTINATION AND LANDED WITHOUT INCIDENT. PERFORMED ENGINE TROUBLESHOOTING, INSTALLED NEW OIL FILTER, RAN AND LEAK C HECK ENGINE AND FOUND TO BE OK FOR RETURNED TO SERVICED IAW MM 72-00. 2 L 7 3 4F 4 F A3WE E2EA 2002031200116 20020312 00116 NE 2002 3 12 CHQ000132 3 20020307 A 6110 PROPELLER SAAB SF340 SF340A 7850100 EU ROTOL R354 R3544123F13 NE RT ENGINE VIBRATION A CHQA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 11 150 150 VIBRATION OF RT SIDE PROP MOST NOTICEABLE WHEN BRINGING PROP INTO AND OUT OF FEATHER IN FLIGHT, SEEMS WORSE AT HIGHER AI RSPEEDS RAN A/C. 2 L 7 2 4T RT A52EU 6 C P61GL 2002031200117 20020312 00117 SO 2002 3 12 CHQ000133 1 20020309 A 2750 FLAP EMB 145 EMB145 3260210 SO WING MALFUNCTIONED A CHQA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 11 262 262 AFTER TAKEOFF WHEN FLAPS SELECTED UP EICAS FLAP FAIL MESSAGE APPEARED UNABLE TO RAISE LOWER FLAPS. FLAPS REMAINED AT 0 DEGREES. 2 L 7 2 4F RT T00011AT 2002031200118 20020312 00118 NM 2002 3 12 DHL2002717001 1 20020307 A 2612 FIRE LOOP BOEING 727 72723 1384004 NM NR 3 ENGINE INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 717DH 19389 NR 3 ENG FIRE TEST INOP. REMOVED AND REPLACED NR 3 ENG FIRE LOOP IAW B727 OHM 71-02-01, OPS CHECKS SERVICEABLE. 2 L 7 3 4F A3WE 2002031200119 20020312 00119 WP 2002 3 12 DHL2002804002 1 20020308 A 2751 PANEL DOUG DC8 DC873F 302199F WP COCKPIT SHORTED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 804DH 46124 ON APPROACH CREW NOTICED SMOKE BILLOWING FROM THRUST LEVER CONSOLE. FOUND FLAP POSITION LIGHT PLATE CAUSING SHORT, REPL ACED SAME, OPS CHECKED NORMAL PER 33-13-0. PLACARDS REMOVED. 2 L 7 4 4F RT 4A25 2002031200120 20020312 00120 2002 3 12 SWAA020510 4 20020307 A 2565 6567380 CONTAINER BOEING 737 7373Y0 1384671 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 FWD ENTRY DOOR EMERGENCY EVAC SLIDE CONTAINER LOOSE. SECURED CONTAINER PER MM. 2 L 7 2 4F RT A16WE 2002031200121 20020312 00121 2002 3 12 SWAA020511 4 20020307 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR DISPLACED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 633SW 27936 FWD SVC DOOR EMERGENCY EVAC SLIDE DISPLACED FROM CASE WHEN DOOR CLOSED. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002031200122 20020312 00122 2002 3 12 SWAA020512 4 20020308 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR DISPLACED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 633SW 27936 FWD SVC DOOR EMERGENCY EVAC SLIDE DISPLACED FROM CASE WHEN DOOR CLOSED. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002031200123 20020312 00123 2002 3 12 SWAA020513 4 20020307 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM FWD ENTRY DOOR DISPLACED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002031200124 20020312 00124 NM 2002 3 12 SWAA020515 1 20020309 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM AFT CARGO WEAK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY EXIT LIGHT BATTERY VOLTAGE LOW. REMOVED AND REPLACED BATTERY PER MM . 2 L 7 2 4F A16WE 2002031200125 20020312 00125 NM 2002 3 12 SWAA020517 1 20020305 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 395SW 27689 EEPLS COVERS MISSING AT MID CABIN. INSTALLED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002031200126 20020312 00126 2002 3 12 SWAA020518 4 20020308 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 793SA 27888 AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR STRAP LOOSE. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002031200127 20020312 00127 2002 3 12 SWAA020520 4 20020308 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM BOTH FWD DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED C4 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT STRAP PLAY OUTS OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2 L 7 2 4F RT A16WE 2002031200128 20020312 00128 NM 2002 3 12 SWAA020522 1 20020310 A 5320 6545776 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 967, BETWEEN STR 6L AND 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002031200129 20020312 00129 NM 2002 3 12 SWAA020524 1 20020309 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 645SW 28330 DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 807, LBL 8. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002031200130 20020312 00130 NM 2002 3 12 SWAA020525 1 20020310 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 396SW 27690 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 185 AND LBL 1.0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002031200131 20020312 00131 NM 2002 3 12 SWAA020526 1 20020310 A 5753 6546435304 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED D CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED ON BOTH UPPER AND LOWER SKINS. REMOVED AND REPLACED RT OTBD AFT T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002031200132 20020312 00132 NM 2002 3 12 SWAA020529 1 20020310 A 5320 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FWD CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 646SW 28331 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 390, BL 0 AND WL 208.1. REMOVED AND REPLACED SHEAR TIE PER S RM. 2 L 7 2 4F RT A16WE 2002031200133 20020312 00133 NM 2002 3 12 SWAA020530 1 20020310 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, 1 INCH ABOVE STR 10L. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2002031200134 20020312 00134 NM 2002 3 12 SWAA020531 1 20020306 A 3246 L507949629 BEARING BOEING 737 7377H4 1384404 NM NLG WORN A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 796SW 27889 DURING TAXI INTO GATE, NOTED RT NLG WHEEL ASSY HAVING EXESSIVE PLAY. DISCOVERED RT NLG TIRE INNER BEARING AND RACE WORN . REMOVED AND REPLACED BOTH NLG TIRE/WHEEL ASSY'S, ALSO REMOVED AND REPLACED NLG AXEL ASSY DUE TO OVERHEAT. ALL WORK P ER MM. 2 L 7 2 4F RT A16WE 2002031200135 20020312 00135 NM 2002 3 12 F3LA200200106 1 20020301 A 2710 CARTRIDGE BOEING 737 7372L9 1384497 NM AILERON DEFECTIVE A F3LA K NONE F FLT CONT AFFECTED UK UNKNOWN 1 NM 03 270FL 419 22733 UPON ARRIVAL, FLIGHT CREW REPORTED AILERONS BECAME EXTREMELY TIGHT AND FELT AS IF IN MANUAL REVERSION. HYDRAULIC SYSTEM PRESSURES WERE BOTH NORMAL. RUDDER AND ELEVATOR FELT NORMAL. ACCOMPLISHED NORMAL LANDING. REPLACED AILERON SPRING CA RTRIDGE PER MM 27-11-0. CYCLED AILERONS SEVERAL TIMES AND FOUND NORMAL FORCES WERE REQUIRED TO OPERATE AILERONS. 2 L 7 2 4F RT A16WE 2002031200136 20020312 00136 CE 2002 3 12 GLBA2002026 1 20020301 A 2460 WARNING SYSTEM BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 NM 03 245GL UE245 LEFT GEN TIE ANNUNCIATOR ILLUMINATED IN-FLIGHT. COULD NOT DUPLICATE. 2 L 7 2 4T RT A24CE 2002031200137 20020312 00137 CE 2002 3 12 GLBA2002027 1 20020302 A 2752 1003840405 MOTOR BEECH 1900 1900D 1154162 CE T/E FLAP FAILED A GLBA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 03 169GL UE169 FLAPS STUCK AT 17 PERCENT. 2 L 7 2 4T RT A24CE 2002031200138 20020312 00138 CE 2002 3 12 GLBA2002028 1 20020302 A 7714 503890571 TACH GENERATOR BEECH 1900 1900D 1154162 CE LT ENGINE FLUCTUATES A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 204GL 1634 UE204 LEFT N1 INDICATOR FLUCTUATING. REPLACED TACH GEN, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002040300149 20020403 00149 CE 2002 4 3 GLBA2002029 1 20020302 A 2420 CONNECTOR BEECH 1900 1900D 1154162 CE LT GENERATOR LOOSE A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 245GL UE245 LEFT GENERATOR TIE ILLUMINATED ON T/O, RESECURED CONNECTOR PLUG & PCB OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2002040300150 20020403 00150 CE 2002 4 3 GLBA2002030 1 20020304 A 2750 SWITCH BEECH 1900 1900D 1154162 CE TE FLAPS OUT OF ADJUST A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 NM 03 208GL UE208 FLAPS STUCK AT 17 PERCENT, ADJUSTED FLAP SAFTEY SWITCH OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2002031200141 20020312 00141 WP 2002 3 12 IXXA0200009O 1 20020307 A 2750 CONNECTOR DOUG DC8 DC863F 302198F WP T/E FLAP CONTAMINATED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 867BX 82158 1186 46049 AFTER TAKEOFF FROM PDX, THE TAKEOFF WARNING HORN SOUNDED WHEN THE LANDING GEAR AND FLAPS WERE RETRACTED AND COULD NOT BE SILENCED. THE FLIGHT RETURNED TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE FLAP LIMIT SWITCH CONNECTOR CONTAMINATED. MAINTENANCE CLEANED THE CONNECTOR AND PERFORMED A SUCCESSFUL OPERATIONAL CHE CK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002031200142 20020312 00142 SO 2002 3 12 LR7A02014 1 20020307 A 7120 36001519 MOUNT LKHEED 382 382G 526414U SO NR 2 ENGINE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP53118 FOUND NR 2 ENGINE FS 517 OUTBOARD TRUSS MOUNT LUG CRACKED AT FWD DI AGONAL TUBE ATTACH HOLE, CWS 216L, WL 275. REPLACED TRUSS MOUNT IAW SRM SMP 583 51-10 PG 4. 2 H 7 4 4T A1SO 2002031200143 20020312 00143 SO 2002 3 12 LR7A02022 1 20020307 A 5320 37049910 CAP LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION FOUND FS 577 CHINE CAP CORRODED AT RBL 61, WL 146. REPLACED CHINE CAP FS 517 - 597 IAW S RM SMP 583 51-10 PG 4. 2 H 7 4 4T A1SO 2002031200144 20020312 00144 SO 2002 3 12 LR7A02023 1 20020307 A 5320 3704999 CAP LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION FOUND FS 577 CHINE CAP CORRODED AT LBL 62, WL 146. REPLACED CHINE CAP FS 517 - 597 IAW S RM SMP 583 51-10 PG 4. 2 H 7 4 4T A1SO 2002031200145 20020312 00145 SO 2002 3 12 LR7A02024 1 20020307 A 7120 36001619 MOUNT LKHEED 382 382G 526414U SO NR 2 ENGINE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2311 4590 DURING SCHEDULED C3 INSPECTION FOUND NR 2 ENGINE FS 517 INBOARD TRUSS MOUNT LUG CRACKED AT DIAGONAL TUBE ATTACH HOLE, CW S 179L, WL 275. REPLACED TRUSS MOUNT IAW SRM SMP 583 51-10, PG 4. 2 H 7 4 4T A1SO 2002031200146 20020312 00146 2002 3 12 COMA0260154 4 20020308 A 3418 SERVICE DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 719CA 7253 FLIGHT 5469 LOUD BUZZING NOISE AND STALL FAIL CAUTION PLUS IAS MESSAGE.FOUND 02 SERVICE DOOR OPEN - CLOSED DOOR. 2 L 7 2 4F RT A21EA 2002031200147 20020312 00147 EA 2002 3 12 COMA0260155 1 20020307 A 3230 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 735CA 7564 7267 FLIGHT 5650 GEAR DISAGREE MESSAGE.REPLACED THE MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002031200148 20020312 00148 EA 2002 3 12 COMA0260156 1 20020307 A 2750 7805013 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA INST PANEL MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS DE DESCENT 1 SO 01 938CA 8965 7046 FLIGHT 5719 FLAPS FAILED AT 8 DEGREES.REPLACED THE FLAP CONTROL LEVER. 2 L 7 2 4F RT A21EA 2002031200149 20020312 00149 EA 2002 3 12 COMA0260157 1 20020305 A 2750 860D10018AB FCU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 916CA 14975 7014 FLIGHT 5999 FLAPS FAILED AT 22 DEGREES.REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2002031300049 20020313 00049 EA 2002 3 13 COMA0260158 1 20020305 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 708CA 50 50 7235 FLIGHT 5075 FLAPS FAILED WARNING DURING TAXI. REPLACED THE RIGHT BPSU. 2 L 7 2 4F RT A21EA 2002031200150 20020312 00150 EA 2002 3 12 COMA0260159 1 20020305 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS CR CRUISE 1 SO 01 708CA 7235 FLIGHT 5073 FLAPS FAILED WARNING DURING FLIGHT.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002031200151 20020312 00151 EU 2002 3 12 MALA020177 1 20020307 A 3020 WARNING LIGHT SAAB SF340 SF340A 7850100 EU COCKPIT ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 46XJ 340A046 DURING FLIGHT 2827, RT INTAKE HEAT LIGHT ON. AC DIVERTED TO CVG. 2 L 7 2 4T RT A52EU 2002031200152 20020312 00152 EA 2002 3 12 COMA0260160 1 20020305 A 7830 1267587 POWER UNIT CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 815CA 8163 7397 FLIGHT 5786 R/H ENGINE REVERSE UNLOCKED DURING FLIGHT.REPLACED THE R/H ENGINE PDU 2 L 7 2 4F RT A21EA 2002031200153 20020312 00153 NE 2002 3 12 MALA020179 2 20020304 A 7260 CHIP DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE DIRTY A MALA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 412XJ 340B412 AFTER STARTING LT ENGINE CHIP DETECTOR LIGHT CAME ON. REMOVED AND CLEANED CHIP DETECTOR. NO CHIPS FOUND, RAN ENGINE NO DISCREPANCIES FOUND. 2 L 7 2 4T 4 T RT A52EU E8NE 2002031200154 20020312 00154 EA 2002 3 12 COMA0260161 1 20020305 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 915CA 19204 7013 FLIGHT 5359 GEAR DISAGREE WARNING, NLG SLOW TO EXTEND.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002031200155 20020312 00155 EU 2002 3 12 MALA020180 1 20020305 A 3243 AC67728 CONTROL VALVE BAC 146 AVRO146RJ85A 1500097 EU MLG DEFECTIVE A MALA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 15 521XJ E2346 BRAKES ARE GRABBING. MAINTENANCE REMOVED AND REPLACED GREEN & YELLOW BRAKE CONTROL VALVES. BLED BRAKES AND OPS CHECKED . 2 H 7 4 4F RT A49EU 2002031200156 20020312 00156 NE 2002 3 12 MALA020181 2 20020305 A 7321 6071T20P16 CONTROL UNIT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ENGINE MALFUNCTIONED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 457XJ 340B457 REPORTED SMOKE FROM RT AIRCRAFT VENTS IN CABIN ON ENGINE START. MAINTENANCE BORESCOPED POWER UNIT, FOUND NO EVIDENCE OF OVERTEMP OR OTHER DEFECTS. REMOVED DECU IAW GE MM 71-00-00. OPS & LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2002031200158 20020312 00158 EU 2002 3 12 MALA020183 1 20020204 A 5210 SEAL SAAB SF340 340B 7860101 EU PAX DOOR LACK OF LUBE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 408XJ 340B408 JUST AFTER TAKEOFF ON FLIGHT 3064, THE PAX DOOR HANDLE JARRED OPEN, AND THE MAIN CABIN DOOR LIGHT ILLUMINATED. CREW IMM EDIATELY CONTACTED MXC AND DISPATCH. AIR RETURN TO MSP. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PAX DOO R SEAL DRY/RUBBING. LUBED SEAL. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002031200159 20020312 00159 EU 2002 3 12 MALA020184 1 20020307 A 3020 NH2466816901 DUCT SAAB SF340 340B 7860101 EU LT ENGINE BURNED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 402XJ 340B402 AFTER TAKEOFF ON FLIGHT 175, LT INTAKE LIGHT ILLUMINATED IN FLIGHT. AIR RETURN TO MSP. LOWER DUCT IS BURNT. MAINTENAN CE REMOVED AND REPLACED LT LOWER INTAKE DUCT. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002031200160 20020312 00160 EU 2002 3 12 MALA020186 1 20020308 A 3030 WARNING SYSTEM BAC 146 AVRO146RJ85A 1500097 EU COCKPIT FALSE ACTIVATION A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 514XJ E2330 SHORTLY AFTER TAKEOFF ON FLIGHT 3547, CREW REPORTED THE Q-FEEL HEATER LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO DTW. M AINTENANCE RESET Q-FEEL C/B ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2002031200161 20020312 00161 EU 2002 3 12 MALA020187 1 20020308 A 3230 LANDING GEAR SAAB SF340 340B 7860101 EU NLG & MLG MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 449XJ 340B449 DURING FLIGHT 2972, COULD NOT GET GEAR TO RETRACT. 2 L 7 2 4T RT A52EU 2002031200162 20020312 00162 NE 2002 3 12 MALA020188 2 20020309 A 7261 SUMP SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE LEAKING A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 15 142XJ RIGHT ENGINE OIL PRESSURE LIGHT ILLUMINATED 2 TIMES DURING CLIMBOUT ON FLIGHT 3337, FLUCTUATED THROUGHOUT FLIGHT. AIR R ETURN TO MSP. MAINTENANCE ADDED 2.25 QTS TO RIGHT ENGINE, REPACKED C-SUMP AND STRUT TUBES IAW TASK CARD 7920-301, LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002031200163 20020312 00163 WP 2002 3 12 MWEA020153 1 20020301 A 5313 591022859 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 AFT ACCESSORY, LONGERON 22 LEFT HAS AREAS OF BARE METAL AND LIGHT CORROSION FROM CANTED FRAME 1121 TO SKIN SPLICE JUST F WD OF FUSELAGE STATION 1076. REMOVED AND REPLACED LONGERON SECTION. 2 L 7 2 4F A6WE 2002031200164 20020312 00164 WP 2002 3 12 MWEA020159 1 20020306 A 5320 99101403 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 CABIN SUBFLOOR HAS A CRACK IN THE WEB AT STATION 598 LEFT SIDE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002031200165 20020312 00165 WP 2002 3 12 MWEA020161 1 20020306 A 5320 99101403 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT CUSP MEMBRANE STATION 579 THROUGH 598 IS CRACKED IN SEVERAL LOCATIONS AND IS PUNCTURED. FABRICATED AND INSTALLED R EPAIR DOUBLER. 2 L 7 2 4F A6WE 2002031200166 20020312 00166 EA 2002 3 12 COMA0260162 1 20020311 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 14017 7123 CRACK FOUND ON RT LOWER WING PLANK AT 650GB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002031200167 20020312 00167 NE 2002 3 12 PCAA0202032 2 20020308 A 7260 PW120A ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RIGHT LEAKING A PCAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 13 834EX 18145 4793 285 121349 LGA- FLIGHT 3818. CREW REPORTED THAT AFTER TAKEOFF NR 2 OIL PRESSURE DROPPED TO ZERO WITH WARNING LIGHT. MAINTENANCE F OUND AC GENERATOR MOUNTING FLANGE LEAKING OIL. ENGINE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002031200168 20020312 00168 EA 2002 3 12 COMA0260163 1 20020311 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 14017 7123 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 640DB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002031200169 20020312 00169 EA 2002 3 12 SWIA200210695 1 20020225 A 5242 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NA AVIONICS BAY UNLATCHED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 907SW 7511 AFTER TAKEOFF THE CREW HEARD A "POP" AND THE AVIONICS BAY DOOR WARNING LIGHT ILLUMINATED. RETURNED TO BOI. FOUND AVIO NICS DOOR LATCH NOT SECURED. INSPECTED AND LATCHED AVIONICS BAY DOOR. NO DEFECTS FOUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2002031200170 20020312 00170 NM 2002 3 12 PCAA0202033 1 20020309 A 5610 07802 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM COCKPIT CRACKED A PCAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 13 809EX 12399 302 MDT-BOS. FLIGHT 3715. CREW REPORTED DURING CRUISE FLIGHT 20 MI FROM MDT OUTER LAYER OF CAPTAINS WINDSHIELD SHATTERED. AIRCRAFT RETURNED TO MDT FOR REPAIRS. MAINTENANCE REPLACED CAPTAINS WINDSHIELD IAW MM 56-10-11. OPERATIONAL CHECK GOOD . AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031200171 20020312 00171 EA 2002 3 12 COMA0260164 1 20020311 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 14017 7123 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 650DB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002031200172 20020312 00172 EA 2002 3 12 COMA0260165 1 20020311 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 14017 7123 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 650CB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002031200173 20020312 00173 EA 2002 3 12 COMA0260166 1 20020311 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 14017 7123 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 650BB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002031200174 20020312 00174 NM 2002 3 12 PCAA0202034 1 20020310 A 2731 TRIM TAB DHAV DHC8 DHC8102 2809003 NM ELEVATOR JAMMED A PCAA K NONE F FLT CONT AFFECTED CL CLIMB 1 EA 13 822EX 187 SYR-LGA FLIGHT 3863. CREW REPORTED ELEVATOR AND STANDBY TRIM JAMMED DURING TRANSITION FROM CLIMB TO LEVEL-OFF. MAINTEN ANCE INSPECTED BOTH ELEVATOR TRIM TABS. NO DEFECTS WERE NOTED. ELEVATOR TRIM AND STANDBY TRIM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031200175 20020312 00175 NM 2002 3 12 PCAA0202035 1 20020308 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT, EMERGENCY FLOOR PATH LIGHTING FOUND TO BE INOPERATIVE. FLOOR TRACK LIGHT STRIP WAS RE PLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031200176 20020312 00176 EA 2002 3 12 COMA0260167 1 20020311 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 14017 7123 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 650AB.REPAIRD I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002031200177 20020312 00177 EU 2002 3 12 Q2XEA0200343 1 20020215 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RIGHT WING STATION 5280, PANEL 82CE AFT ATTACH POINTS ON PANEL HAVE MOUNT BRACKET CHAFE ON ONE SIDE AND THE OTHER SIDE IS ELONGATED. REPAIRED IAW FOKKER SRM 57-61-04 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002031200178 20020312 00178 EU 2002 3 12 QXEA0200236 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - FUSELAGE CABIN FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGU RE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002031200179 20020312 00179 EU 2002 3 12 QXEA0200237 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - FUSELAGE CABIN FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 24. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGU RE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002031200180 20020312 00180 EU 2002 3 12 QXEA0200239 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - FUSELAGE CABIN FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 22. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGU RE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002031200181 20020312 00181 EA 2002 3 12 COMA0260168 1 20020311 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 14017 7123 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 640FB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002031200182 20020312 00182 EA 2002 3 12 COMA0260169 1 20020311 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 14017 7123 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 550EB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002031200183 20020312 00183 EU 2002 3 12 QXEA0200240 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - FUSELAGE CABIN FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGU RE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002031200184 20020312 00184 EU 2002 3 12 QXEA0200241 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - FUSELAGE CABIN FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGU RE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002031200185 20020312 00185 EU 2002 3 12 QXEA0200242 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - FUSELAGE CABIN FRAME 14755 CASTELLATION IS CRACKED AT STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGU RE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002031200186 20020312 00186 EA 2002 3 12 COMA0260170 1 20020311 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 14017 7123 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 550DB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002031200187 20020312 00187 EU 2002 3 12 QXEA0200243 1 20020207 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU EMERGENCY EXIT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT AFT OVERWING EMERGENCY EXIT DOOR OUTER SKIN HAS CHAFE AND STEP WEAR DAMAGE AT FORWARD LOWER CORNER. REPAIRED I AW FOKKER SRM 52-01-01, STEP E, AREA B AND FIGURE 1 ON PAGE 3. 2 L 7 2 4F RT A20EU 2002031200188 20020312 00188 EU 2002 3 12 QXEA0200244 1 20020207 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU EMERGENCY EXIT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT AFT OVERWING EMERGENCY EXIT DOOR OUTER SKIN EDGE HAS CHAFE AND STEP WEAR DAMAGE AT FORWARD UPPER CORNER. REPAI RED IAW FOKKER SRM 52-01-01, STEP E, AREA B AND FIGURE 1 ON PAGE 3. 2 L 7 2 4F RT A20EU 2002031200189 20020312 00189 EU 2002 3 12 AWXA200200198 1 20020307 A 5330 2024T3080 SKIN AIRBUS 320 A320231 3930325 EU DENTED A AWXA K NONE O OTHER TX TAXI/GRND HDL 1 WP 28 621AW 053 PHX - GROUND DAMAGE - "S" - WHILE AIRCRAFT WAS PARKED AT GATE A BAGGAGE CART WAS BLOWN INTO THE AIRCRAFT BY A GUST OF WI ND STRIKING THE AIRCRAFT JUST AFT OF THE AFT CARGO DOOR DAMAGING EXTERNAL SKIN AND FRAME FLANGE BETWEEN STR 37 R/H AND S TR 38 R/H, FR 30. **SUPP** MAINTENANCE REMOVED STRINGER TO FRAME CLIPS AT STR 37 R/H, AND STR 39 R/H, FR 30 TO FACILITAT E REPAIR OF SKIN. DAMAGED AREA OF SKIN WAS REMOVED AND DOUBLER WAS FABRICATED FROM 2024T3.080 AND INSTALLED IAW SRM 53-0 0-11, FIG. 201. STRINGERS WERE REINSTALLED TO FRAME CLIPS AT STR 37 R/H AND STR 39 R/H, FR 30 IAW SRM 51-42-00. 2 L 7 2 4F RT A28NM 2002031200190 20020312 00190 NM 2002 3 12 AWXA200200210 1 20020310 A 3350 BMS13311122 WIRE BOEING 737 737277 1384570 NM SEAT ROW 13L BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 PHX - EEL - "C" - EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 L/H INOPERATIVE. MAINTENANCE REPAIRED WIRE PULLED FROM SPLI CE AT SEAT ROW 13 L/H, FUNCTIONAL CHECK WAS GOOD IAW T/C A1C33006. 2 L 7 2 4F RT A16WE 2002031200191 20020312 00191 NM 2002 3 12 AWXA200200211 1 20020309 A 3350 BACC45FN10C5S CONNECTOR BOEING 737 7373S3 1384711 NM SEAT ROW 14L INCORRECT A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 YVR - EEL - "C" - DURING C-15 CHECK SEAT ROW 14 L/H WAS FOUND TO HAVE THE WRONG MATING CONNECTORS AT THE EMERGENCY LIGHT ING HARNESS JUNCTIONS. MAINTENANCE REMOVED AND REPLACED MATING CONNECTORS FOR EMERGENCY LIGHTING HARNESS AT SEAT ROW 14 L/H. FUNCTIONAL CHECK WAS GOOD IAW T/C A1C33006. 2 L 7 2 4F RT A16WE 2002031200192 20020312 00192 EU 2002 3 12 QXEA0200245 1 20020207 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU EMERGENCY EXIT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- RT AFT OVERWING EMERGENCY EXIT DOOR OUTER SKIN EDGE HAS CHAFE AND STEP WEAR AT AFT UPPER CORNER. REPAIRED IAW FOKK ER SRM 52-01-01, STEP E, AREA B AND FIGURE 1 ON PAGE 3. 2 L 7 2 4F RT A20EU 2002031200193 20020312 00193 EA 2002 3 12 COMA0260171 1 20020311 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 14017 7123 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 550BB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002031200194 20020312 00194 EU 2002 3 12 QXEA0200246 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD TRACK AT STATION 228.539 TOP EDGES AND LUGS HAVE CORROSION. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206 , FIGURE 205 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4C. 2 L 7 2 4F RT A20EU 2002031200195 20020312 00195 EU 2002 3 12 QXEA0200247 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 248.224 LUGS ARE CHAFED TO THE POINT OF DETERIORATION. REPAIRED IAW FOKKER MM 5 3-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 2002031200196 20020312 00196 EU 2002 3 12 QXEA0200248 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 267.909 THERE IS A 3 INCH AREA OF CORROSION IN CHANNEL. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4A AND SRM 51-10-4, PAGE 9, PARAGRAPH 4C. 2 L 7 2 4F RT A20EU 2002031200197 20020312 00197 EA 2002 3 12 COMA0260172 1 20020311 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 14017 7123 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 540FB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002031200198 20020312 00198 EU 2002 3 12 QXEA0200249 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 267.920 THERE IS A 3 INCH AREA IN THE CHANNEL HAS CORROSION. REPAIRED IAW FOKKE R SRM 53-01-01, PAGE 8, PARAGRAPH 4C, STEP 1 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4C. 2 L 7 2 4F RT A20EU 2002031200199 20020312 00199 2002 3 12 SWIA200210656 4 20020218 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO AUTOPILOT SYS DEFECTIVE A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 289YV 10 10 120289 AUTOPILOT WILL NOT HOLD ALTITUDE OR PITCH WITHIN ACCEPTABLE LIMITS. TRIED BOTH CAPT AND F/O CONTROLS WITH SAME RESULT. REMOVED AND REPLACED ELEVATOR SERVO. OPS CHECKED GOOD IAW MM 22-10-00. 2 L 7 2 4T RT A31SO 2002031200200 20020312 00200 EA 2002 3 12 COMA0260173 1 20020311 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 14017 7123 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 550CB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002031200201 20020312 00201 SO 2002 3 12 SWIA200210657 1 20020219 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 584SW 120352 ABORTED TAKEOFF DUE TO ERRONEOUS TRIM WARNING, ALTHOUGH TRIM WAS SET IN THE GREEN. PERFORMED TRIM WARNING FUNCTIONAL CH ECK IAW 27-32-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002031200202 20020312 00202 2002 3 12 SWIA200210658 4 20020218 A 3425 6229336400 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA NR 2 FAILED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 423SW 780 780 7456 COPILOT'S NR 2 AHARS BECAME INOPERATIVE INBOUND TO ICT, AT FD AND MAG FLAGS. REMOVED NR 2 AHARS COMPUTER AND REPLACED I T WITH A SERVICEABLE UNIT IAW CL600 MM 34-21-01. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002031200203 20020312 00203 SO 2002 3 12 SWIA200210659 1 20020216 A 3150 WARNING SYSTEM EMB 120 EMB120RT 3260202 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 269UE 120194 ABORTED 3 STATIC TAKEOFFS FOR T/O TRIM AURAL WARNING. TRIM SETTING WAS IN GREEN BAND 30 PERCENT TO 35 PERCENT. CYCLED TRIM WHEEL, THEN NORMAL TAKEOFF. TESTED TRIM AURAL WARNING AT VARIOUS SETTINGS. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002031200204 20020312 00204 EA 2002 3 12 SWIA200210660 1 20020218 A 5610 601R330331 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER DE DESCENT 1 NM 07 588SW 7069 LEFT OUTER WINDSHIELD SHATTERED DURING DESCENT. REMOVED AND REPLACED LEFT WINDSHIELD IAW 56-11-01. 2 L 7 2 4F RT A21EA 2002031200205 20020312 00205 SO 2002 3 12 SWIA200210661 1 20020220 A 2133 OUTFLOW VALVE EMB 120 EMB120ER 3260203 SO CABIN PRESSURE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 270YV 120270 AFTER TAKEOFF, CABIN CLIMBED AT GREATER THAN 2000 FPM. AFTER SWITCHING TO MANUAL MODE, THE PRESSURIZATION WAS CONTROLLA BLE. REPLACED PNEUMATIC OUTFLOW VALVE AND PRESSURE CONTROLLER. OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2002031200206 20020312 00206 EA 2002 3 12 SWIA200210662 1 20020216 A 2760 270003 PCU CNDAIR CL600 CL6002B19 1900309 EA RT SPOILERON MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 403SW 7028 RIGHT SPOILERON FAILS WHEN NR 3 HYDRAULIC IS TURNED ON BEFORE NR 2. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU I AW 27-63-00. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2002031200207 20020312 00207 EA 2002 3 12 COMA0260174 1 20020309 A 7110 22850583101 CLIP CNDAIR CL600 CL6002B19 1900309 EA LEFT ENG BROKEN A COMA O OTHER O OTHER CL CLIMB 1 SO 01 915CA 7013 FLIGHT 5910 LEFT ENGINE POWER LEVER JAMMED AT 92 DEGREES. POWER COULD BE INCREASED BUT COULD NOT BE DECREASED.FOUND CORE COWL SUPPORT ROD STOW BRACKET BROKEN WHICH ALLOWED THE SUPPORT ROD TO JAM THE FUEL CONTROL LINKAGE. REPLACED BRACKET. 2 L 7 2 4F RT A21EA 2002031200208 20020312 00208 NE 2002 3 12 SWIA200210663 2 20020214 A 7230 BLADE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 ENGINE BENT A SWIA O OTHER E VIBRATION/BUFFET CR CRUISE 1 NM 07 590SW 7077 WHILE INFLIGHT AT 35,000 FT FELT A THUMP, FOLLOWED BY A SLIGHT VIBRATION. ALL INDICATIONS NORMAL AND WITHIN PARAMETERS. ON DESCENT INTO SLC RIGHT NR 2 ENGINE VIBRATION INDICATION GRADUALLY INCREASED UP TO 2.5 BUT STILL WITHIN GREEN BAND O N GAUGE. ALL OTHER INDICATIONS NORMAL. ALL FAN BLADES ON RIGHT ENGINE REMOVED. FOUND SEVERAL FAN BLADES BENT ON RIGHT ENGINE. REINSTALLED ALL FAN BLADES IAW MM 72-00-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2002031200209 20020312 00209 SO 2002 3 12 SWIA200210664 1 20020225 A 3350 FUSE EMB 120 EMB120RT 3260202 SO PWA PW118 PW118B NE EMERGENCY LIGHT BLOWN A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 1117H 120117 RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FUSE AT FUSE HOLDER XF0016 IAW WM 20-00-00. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002031200210 20020312 00210 SO 2002 3 12 SWIA200210665 1 20020225 A 3397 WIRE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE CABIN BROKEN A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 1117H 120117 ROW 2BC EXIT SIGN INOP. REPAIRED BROKEN WIRE AT EXIT SIGN SEAT 2BC. 2 L 7 2 4T 4 T RT A31SO E20NE 2002031200211 20020312 00211 EA 2002 3 12 COMA0260175 1 20020309 A 3350 59465 CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 956CA 7105 FLIGHT 5010 EMERGENCY FLOOR PATH LIGHTING INOP.SECURED LOOSE WIRE CONNECTION AT ROW 11. 2 L 7 2 4F RT A21EA 2002031900109 20020319 00109 NM 2002 3 19 F3LA200200107 1 20020309 A 5230 R1792196 DOOR FRAME BOEING 737 7372L9 1384497 NM CARGO DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 50525 4384 22733 DURING AN OUTFLOW VALVE TEST WITH THE AIRCRAFT PRESSURIZED, MAINTENANCE REPORTED A LOUD POP IN THE AREA OF THE AFT CARGO DOOR AND FOUND A 5-INCH CRACK IN THE RADIUS OF THE DOOR FRAME OTBD OF THE LOWER FWD STOP FITTING AND CRACKS IN THE LOWE R DOOR BEAM OTBD CHORD AND WEB. REPLACED THE AFT CARGO DOOR. 2 L 7 2 4F RT A16WE 2002031200212 20020312 00212 SO 2002 3 12 SWIA200210667 1 20020212 A 2751 3069001005 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FAULTY A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 190SW 120050 FLAPS INOP - ALL CONTROL FAULT, DISAGREEMENT AND ASYMMETRY LIGHTS ON. COULD NOT CLEAR ANY OF THE FAULT LIGHTS. FLAP CO NTROL PANEL FLAP PORTION INDICATOR (ALL) INDICATED FLAPS UP WHEN FLAPS WERE 15 DEGREES, 25 DEGREES OR 45 DEGREES POSITIO N PHYSICALLY. CONDITION WAS INTERMITTENT ON TAXI BACK. REMOVED AND REPLACED FLAP CONTROL UNIT AND FLAP ANNUNCIATOR ASS EMBLY. OPS CHECK GOOD IAW 27-50-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2002031200213 20020312 00213 SO 2002 3 12 SWIA200210668 1 20020225 A 2751 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FAULTY A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 196SW 120151 DISAGREEMENT ON FLAP RETRACTION INBOARD PAIR. INBOARD FLAPS WOULD NOT RETRACT, INDICATED 10 DEGREES. RETURNED TO SLC. REMOVED AND REPLACED FLAP ANNUNCIATOR UNIT WITH SERVICEABLE UNIT IAW EMB 120 MM 27-51-01. RAN FLAPS, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002031200214 20020312 00214 SO 2002 3 12 SWIA200210669 1 20020128 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 232SW 120306 RIGHT SIDE UPPER SEAT TRACK HAS SIGN OF CORROSION AT SCREW HOLES AND NEEDS REPLACED. REMOVED AND REPLACED RIGHT SIDE UP PER SEAT TRACK WITH NEW AS REQUIRED IAW EMB120 MM 53-01-04. 2 L 7 2 4T 4 T RT A31SO E20NE 2002031200215 20020312 00215 SO 2002 3 12 SWIA200210670 1 20020128 A 5411 FRAME EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 232SW 120306 LEFT ENGINE FRAME NR 1 CRACKED. REPLACED LEFT FRAME NR 1 IAW SB 120-54-0035 REV 02. 2 L 7 2 4T 4 T RT A31SO E20NE 2002031200216 20020312 00216 SO 2002 3 12 SWIA200210671 1 20020128 A 5411 FRAME EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 232SW 120306 RIGHT ENGINE FRAME NR 1 CRACKED. REPLACED RIGHT FRAME NR 1 IAW SB 120-54-0036 REV 02. 2 L 7 2 4T 4 T RT A31SO E20NE 2002031200217 20020312 00217 SO 2002 3 12 SWIA200210672 1 20020217 A 2750 FCU EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 NM 07 269UE 120194 INBOARD FLAPS DID NOT RETRACT AFTER LANDING. REMOVED AND REPLACED FLAP CONTROL UNIT WITH SERVICEABLE. CYCLED FLAPS SEV ERAL TIMES. NO DISCREPANCIES NOTED. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002031200218 20020312 00218 SO 2002 3 12 SWIA200210673 1 20020223 A 5245 DOOR EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE A/C PACK DEPARTED A SWIA K NONE D P INFLIGHT SEPARATION NO WARNING INDICATION CR CRUISE 1 NM 07 269UE 120194 RIGHT AIR CONDITIONING PACK DOOR DEPARTED WHILE IN FLIGHT. REPLACED PACK DOOR IAW SRM 120 51-10-02. 2 L 7 2 4T 4 T RT A31SO E20NE 2002031200219 20020312 00219 SO 2002 3 12 SWIA200210674 1 20020217 A 7712 SIGNAL COND UNIT EMB 120 EMB120ER 3260203 SO LT ENGINE DEFECTIVE A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 235SW 120310 LEFT TORQUE GAUGE FLUCTUATES TO -0-, THEN WORKS AGAIN. REPLACED LEFT TORQUE SIGNAL CONDITIONER UNIT. PERFORMED POWER R UNS, ALL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002031200220 20020312 00220 NE 2002 3 12 SWIA200210675 2 20020225 A 7261 OIL SYSTEM EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NR 2 ENGINE LOW A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 199SW 120237 LOW OIL PRESSURE LIGHT ILLUMINATED FOR NR 2 ENGINE ON TAKEOFF ROLL. ABORTED TAKEOFF. ADDED 3 QUARTS TO NR 2 ENGINE. U PON INSPECTION NO OIL LEAKAGE FOUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2002031200221 20020312 00221 SO 2002 3 12 SWIA200210676 1 20020112 A 5320 CLIP EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 229SW 120305 FRAME 9 SKIN CLIP CRACKED ON COPILOT'S SIDE. 2 L 7 2 4T RT A31SO 2002031200222 20020312 00222 SO 2002 3 12 SWIA200210677 1 20020112 A 5410 WEB EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 229SW 120305 NACELLE WEB ON INBOARD RIGHT NACELLE CRACKED. INSTALLED NEW INBOARD FITTING AFT OF FRAME 13 AT NACELLE STATION 2425, SR M 51-10-02 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002031200223 20020312 00223 2002 3 12 SWIA200210678 4 20020223 A 2216 SERVO EMB 120 EMB120ER 3260203 SO AUTOPILOT SYS DAMAGED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 295SW 120322 ON PREFLIGHT, RUDDER HAS A BINDING FEEL WHEN LEFT RUDDER IS DEPRESSED. FOUND RUDDER TRIM SERVO DAMAGED. REPLACED RUDDE R TRIM SERVO WITH SERVICEABLE UNIT IAW MM 22-10-05. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002031200224 20020312 00224 EA 2002 3 12 SWIA200210679 1 20020216 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 438SW 7574 FLAP FAIL CAUTION MESSAGE ON SHORT FINAL. REMOVED AND REPLACED RIGHT FLAP BPSU IAW 27-51-00. RECHECKED RIGGING, OPS CH ECK GOOD. 2 L 7 2 4F RT A21EA 2002031200225 20020312 00225 EA 2002 3 12 SWIA200210680 1 20020211 A 2432 BATTERY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE E/E BAY DEFECTIVE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 498SW 7483 MAIN BATTERY CHARGER STATUS MESSAGE CAME ON AFTER TAKEOFF. RETURNED TO DFW. SWAPPED APU BATTERY CHARGER S/N 2248 AND M AIN BATTERY CHARGER S/N 1973 FOR TROUBLESHOOTING IAW MM 24-32-03. REMOVED AND REPLACED MAIN BATTERY IAW MM 24-32-01. O PS CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 2002031200226 20020312 00226 NM 2002 3 12 2002F00202 1 20020131 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437YV 437 DURING OVERNIGHT MAINTENANCE, DISCOVERED THAT SEVERAL EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED THE NR 2 POWER SU PPLY. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2002031200227 20020312 00227 EA 2002 3 12 2002F00203 1 20020126 A 2750 1104SD100501 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A MASA K NONE F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SW 07 27172 7172 FLT 6505 - FLAP FAIL MESSAGE DURING LANDING ROLLOUT IN PHL, WHEN FLAPS WERE RETRACTED. MAINTENANCE COMPLIED WITH PART A /B. MAINTENANCE REPLACED THE BPSU, AND THE OUTBOARD FLEX SHAFT. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031200228 20020312 00228 NM 2002 3 12 2002F00205 1 20020204 A 5711 65B392522 SPAR BOEING 747 7472F6B 1384807 NM RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 534MC 79566 21832 DURING CURRENT C-CHECK AT SIAC INSPECTION OF THE RT L/E NR 15 KRUEGER FLAP, A CRACK WAS DISCOVERED IN THE FRONT SPAR INB OARD END OF THE DEVICE (65B39252-2). (M) 2 L 7 4 4F A20WE 2002031200229 20020312 00229 NM 2002 3 12 2002F00206 1 20020130 A 2910 65174894061 B-NUT BOEING 727 727224 1384076 NM HYD SYSTEM LOOSE A FX7A H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 296SC 22449 DURING CRUISE, FLIGHT BOTH SYSTEMS B PUMPS LOW PRESSURE LIGHTS ILLUMINATED. AIRCRAFT DIVERTED TO SWA. ON THE GROUND TH EY TIGHTENED LOOSE B NUTS AT B PUMP NR 2 SERVICED SYSTEM AND OPS CHECK PER MM 29-12. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002031300013 20020313 00013 WP 2002 3 13 ZW0A0202901 1 20020309 A 3350 MISC0639 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 924TW 49100 DURING PREFLIGHT THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. THE AIRCRAFT WAS MAINTENANCE FERRIED TO STL WHERE THE POWER SUPPLY AT ROW 25 WAS REPLACED. CHECK-C 6-10-01 MCI. --CLOSED-- 2 L 7 2 4F A6WE 2002031300050 20020313 00050 EA 2002 3 13 COMA0260176 1 20020310 A 4930 M259882904 O-RING CNDAIR CL600 CL6002B19 1900309 EA APU DAMAGED A COMA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 984CA 7171 FLIGHT 5310 JET FUEL SMELL IN COCKPIT WITH LEFT A/C PACK OPERATING. REPLACED LEAKING O-RING ON APU FUEL CONTROL. 2 L 7 2 4F RT A21EA 2002031300023 20020313 00023 2002 3 13 COMA0260177 4 20020310 A 3418 45150340 SENSOR CNDAIR CL600 CL6002B19 1900309 EA #1 MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 981CA 14338 7163 FLIGHT 6013 STALL FAIL MESSAGE AFTER T/O.REPLACED THE #1 AOA SENSOR. 2 L 7 2 4F RT A21EA 2002031300024 20020313 00024 EA 2002 3 13 COMA0260178 1 20020311 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 735CA 7267 FLIGHT 5542 FLAPS FAILED AFTER LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002031300025 20020313 00025 EA 2002 3 13 COMA0260179 1 20020311 A 3350 362624 LAMP CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 811CA 7380 FLIGHT 5607 EMERGENCY LIGHTS AT ROW 6 INOP.REPLACED LIGHT STRIP. 2 L 7 2 4F RT A21EA 2002031300026 20020313 00026 EA 2002 3 13 COMA0260180 1 20020311 A 2420 BUSS CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 989CA 7215 FLIGHT 5624 AC ESS BUSS INOP MESSAGE.COULD NOT DUPLICATE. PERFORMED AC ELECTRICAL SYSTEM CHECK, NO FAULTS FOUND. 2 L 7 2 4F RT A21EA 2002031300027 20020313 00027 NM 2002 3 13 SWAA020532 1 20020310 A 3230 65C27360 LINK BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 640SW 27713 DURING SCHEDULED C1 CHECK, FOUND NLG LT AFT PUSH ROD ATTACH LINK CRACKED AT TRUNNION SIDE. REMOVED AND REPLACED ATTACH LINK PER MM. 2 L 7 2 4F RT A16WE 2002031300028 20020313 00028 2002 3 13 SWAA020535 4 20020311 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 795SW 30606 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002031300029 20020313 00029 NM 2002 3 13 SWAA020536 1 20020311 A 5311 BAC1506 FRAME BOEING 737 7373H4 1384600 NM RT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 680, WL 177 AND RBL 63. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002031300030 20020313 00030 NM 2002 3 13 SWAA020537 1 20020311 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 645SW 28330 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, LBL 5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2002031300031 20020313 00031 NM 2002 3 13 SWAA020539 1 20020311 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 DURING OUT OF SERVICE MAINTENANCE, FOUND FUSELAGE SKIN CRACKED 3 INCHES LONG AT BS 730 D, BELOW STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002031300032 20020313 00032 NM 2002 3 13 SABA020034 1 20020313 A 3350 1013075 BULB DHAV DHC8 DHC8102 2809003 NM LT FWD FUSALAGE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 813PH 032 ircraft 813 following flight 5057 ALH to CLT. during post flight inspection the left forward exterior emergency light w as found inoperative. Maintgenance removed and replaced the bulb. Ops check was good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002031300034 20020313 00034 EA 2002 3 13 COMA0260181 1 20020311 A 4900 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA APU FAILED A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 719CA 4706 7253 FLIGHT 5521 SMOKE IN COCKPIT AND CABIN.REPLACED THE APU. 2 L 7 2 4F RT A21EA 2002031300035 20020313 00035 EA 2002 3 13 COMA0260182 1 20020311 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 954CA 7100 FLIGHT 5447 FLAPS FAILED WHEN SELECTED TO 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 9-20-01. 2 L 7 2 4F RT A21EA 2002040100034 20020401 00034 NM 2002 4 1 02FDEA00191 1 20020310 A 5312 BULKHEAD BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 LEFT W/L BULKHEAD WEB IS CRACKED AT BS 870, LBL 61, WL 162. REMOVED AND REPLACED BULKHEAD WEB PER EA 7-5350-62780. 2 L 7 3 4F RT A3WE 2002031300046 20020313 00046 CE 2002 3 13 2002F00209 1 20020312 A 2150 26012672 DRIVE SHAFT CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE HARTZL HCB3T HCB3TN3 GL A/C UNIT WORN B S4WA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 07 95NA 3165 0666 PCEPC0556 BUA19725 DURING A 100 HOUR INSPECTION, LEAK WAS NOTED ON THE AIR CONDITIONING DRIVE UNIT. FURTHER INSPECTION REVEALED THE SPLINE S OF THE MALE END OF DRIVE WORN OVER 80 PERCENT. FURTHER INSPECTION REVEALED THE FEMALE END IN THE ENGINE WERE WORN THE SAME AMOUNT. 1 H 7 1 3T 3 T A37CE E4EA 6 C P15EA 2002031300047 20020313 00047 WP 2002 3 13 ABXA010760 1 20020311 A 2163 B7020 SENSOR DOUG DC9 DC941 302207N WP CABIN TEMP FAULTY A ABXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 975AX 1446 47512 AFTER TAKEOFF, AIRCRAFT DID NOT HOLD PRESSURE AND FORWARD CARGO DOOR LIGHT CAME ON AND OFF IN FLIGHT. REPLACED THE CABI N/FLIGHT RATE OF CHANGE/HIGH LIMIT TEMPERATURE SENSOR IAW DC-9 MM 21-61-03-2. 2 L 7 2 4F A6WE 2002031300048 20020313 00048 NM 2002 3 13 AWXA200200212 1 20020309 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 PHX - EEL - C - FLIGHT CREW REPORTED THAT EMERGENCY SEAT LIGHT AT SEAT ROW 22 LT WAS NOT SECURED TO SEAT. MAINTENANCE R EPLACED SEAT LIGHT ASSEMBLY AT SEAT ROW 22 LT, FUNCTIONAL CHECK WAS GOOD IAW T/C A1C33006. 2 L 7 2 4F RT A16WE 2002040300151 20020403 00151 CE 2002 4 3 GLBA2002031 1 20020310 A 7712 1303890023 TRANSMITTER BEECH 1900 1900D 1154162 CE TORQUE INDICATOR INTERMITTENT A GLBA O OTHER N FALSE WARNING CL CLIMB 1 NM 03 247GL 3406 UE247 RT TORQUE INDICATOR FAILED, REPLACED TRANSMITTER OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2002031300052 20020313 00052 WP 2002 3 13 NACA20020010 1 20020312 A 5210 SKIN DOUG DC6 DC6B 3021712 WP CRACKED CRACKED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 7919C 43554 PASSENGER DOOR SKIN BENT AND CRACKED AT BOTTOM EDGE. 2 L 7 4 4R 6A4 2002031300053 20020313 00053 NE 2002 3 13 NAFA20020001 2 20020311 A 7421 RHB32E SPARK PLUG DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE NR 2 ENGINE SHORTED I N32B E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 01 7780B 359 359 45372 P32927 PRECAUTIONARY SHUT DOWN NR 2 ENGINE, DUE TO BACKFIRING. NR 16 CYLINDER LEFT A LONG RESISTANCE PATTERN, RIGHT SHORTED SE CONDARY. INSPECTED THE NR 16 CYLINDER, REPLACED LEFT AND RIGHT SPARK PLUGS AND SHORT LEADS. 2 L 7 4 4R 4 R 6A3 5E8 2002031300054 20020313 00054 EU 2002 3 13 QXEA0200250 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 287.605 HAS A 3 INCH AREA IN THE CHANNEL THAT HAS CORROSION. 2 L 7 2 4F RT A20EU 2002031300055 20020313 00055 EU 2002 3 13 QXEA0200251 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 307.290 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300056 20020313 00056 EU 2002 3 13 QXEA0200252 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 307.277 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300057 20020313 00057 EU 2002 3 13 QXEA0200253 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 287.610 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300058 20020313 00058 EU 2002 3 13 QXEA0200254 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 326.971 TO STATION 326.959 IN THE CHANNEL THERE IS CORROSION. 2 L 7 2 4F RT A20EU 2002031300059 20020313 00059 EU 2002 3 13 QXEA0200255 1 20020209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 366.338 TO STATION 346.646 MOST INBOARD FLANGE HAS PITTING AND CORROSION. 2 L 7 2 4F RT A20EU 2002031300060 20020313 00060 EU 2002 3 13 QXEA0200256 1 20020209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 386.017 TO STATION 366.338 MOST INBOARD FLANGE HAS PITTING AND CORROSION. 2 L 7 2 4F RT A20EU 2002031300061 20020313 00061 EU 2002 3 13 QXEA0200257 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 326.955 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300065 20020313 00065 CE 2002 3 13 BSY2002F00001 1 20020108 A 3397 3538013243 SWITCH BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO COCKPIT FAILED E BSYA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 58TA TH596 249196R AIRCRAFT HAD ELECTRICAL SMELL IN COCKPIT. REMOVED AND REPLACED TAXI LIGHT SWITCH OPS CHECKS GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2002031300066 20020313 00066 EA 2002 3 13 BTH2002F00001 2 20020207 A 7414 BL68256013 MAGNETO PIPER PA32 PA32R300 7103213 SO LYC O540 IO540* 41532 EA RT SIDE INOPERATIVE A BTHA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 AL 01 75387 32R7680298 L2512448A MAGNETO RAN ROUGH ON RIGHT SIDE. DURING RUN, MAGNETO FOR INSPECTION OF PROBLEM FOUND HALF OF RIGHT SIDE GEAR DRIVE TEET H BROKEN OUT. 1 L 7 1 3O 3 O A3SO 1E4 2002031300067 20020313 00067 CE 2002 3 13 COOSDR02002 1 20020301 A 5751 6521766 STRUCTURE CESSNA 150 150L 2071826 CE PWA JT8 JT8D9 52048 NE AILERON DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 21634 15074549 LEFT WING, OUTBOARD AILERON TRAILING EDGE PN 6521766, DELAMINATED. 1 H 7 1 3O 4 F 3A19 E2EA 2002031300069 20020313 00069 EU 2002 3 13 QXEA0200258 1 20020209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 403.661 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300070 20020313 00070 EU 2002 3 13 QXEA0200259 1 20020209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 386.029 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300071 20020313 00071 EU 2002 3 13 QXEA0200260 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK FROM STATION 366.338 TO STATION 337.204 BOTH MATTING FLANGES FOR FLOOR BOARDS HAVE PITTING AND LIGHT CORROSION. 2 L 7 2 4F RT A20EU 2002031300072 20020313 00072 EU 2002 3 13 QXEA0200261 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 366.338 TOP LUGS ARE PITTED AND GOUGED. 2 L 7 2 4F RT A20EU 2002031300074 20020313 00074 EU 2002 3 13 QXEA0200262 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK BETWEEN STATION 386.023 AND STATION 366.338 MATTING FLANGES FOR FLOOR BOARDS ARE PITTED AND HAVE LIGHT CORROSION. 2 L 7 2 4F RT A20EU 2002031300075 20020313 00075 2002 3 13 DBC2002F00000 4 20020205 A 8300 721018 PUMP BEECH 100 B100 1152919 CE GARRTT TPE331 TPE3316252B 01514 WP ACCESSORY G/B FAILED E DBCA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 GL 13 36WH 1445 BE26 27054 WHILE ENROUTE, PILOT NOTED VIBRATION WITH VARYING INTENSITIES. PILOT RETURNED TO AIRPORT WITHOUT INCIDENT. TROUBLESHOT , SUSPECT SCAVENGE PUMP CAVITATION. BLED SCAVENGE SYSTEM PER MFG. SOAP SAMPLE TAKEN. AIRCRAFT GROUND RAN AND CHECKED FOR LEAKS. POST MAINTENANCE FLIGHT CHECK, OK. 1 L 7 2 4T 4 T A14CE E2WE 2002031300076 20020313 00076 EU 2002 3 13 QXEA0200263 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 403.661 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300077 20020313 00077 EU 2002 3 13 QXEA0200264 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 403.668 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300078 20020313 00078 EU 2002 3 13 QXEA0200265 1 20020209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 403.668 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300079 20020313 00079 EU 2002 3 13 QXEA0200266 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 403.656 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300080 20020313 00080 EU 2002 3 13 QXEA0200267 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 386.016 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300081 20020313 00081 EU 2002 3 13 QXEA0200268 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK FROM STATION 423.346 TO STATION 403.681 BOTH MATTING FLANGES ARE PITTED AND HAVE CORROSION. 2 L 7 2 4F RT A20EU 2002031300082 20020313 00082 EU 2002 3 13 QXEA0200269 1 20020209 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK FROM STATION 423.346 TO STATION 403.661 BOTH MATTING FLANGES ARE PITTED AND HAVE CORROSION. 2 L 7 2 4F RT A20EU 2002031300083 20020313 00083 CE 2002 3 13 DMV2002F00000 1 20020121 A 8010 680468T BEARING CESSNA 421 421B 2076014 CE CONT O520 GTSIO520H 17032 SO STARTER ADAPT FAILED E DMVA K NONE O OTHER IN INSP/MAINT 1 WP 05 81HR 608 421B0651 267111P STARTER ADAPTER HOUSING MAIN BEARING FAILURE, RESULTS IN EXCESSIVE PLAY TO REAR ENGINE GEAR ASSEMBLY ADVISE UPGRADING T O BETTER STYLE OF BEARING DESIGNED FOR BETTER LOADS. PROVIDE A 500 HOUR INSPECTION THAT MIGHT REQUIRE REMOVAL AND INSPE CTION OF BEARING TO PROVIDE BETTER SAFETY MARGIN. THIS UNIT HAD ALL UPDATES PRIOR TO FAILURE. HAVING A SPINNING VISCOU S DAMPENER MAY HAVE HAD SOMETHING TO DO WITH ADDED VIBRATION CAUSING BEARING FAILURE. 1 L 7 2 3O 3 O A7CE E7CE 2002031300084 20020313 00084 EU 2002 3 13 QXEA0200270 1 20020212 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - THREE DENTS, RT SIDE FUSELAGE, AFT OF RADOME OPENING, APPROXIMATELY WL 30.0 AND FRAME 1385. 2 L 7 2 4F RT A20EU 2002031300085 20020313 00085 CE 2002 3 13 EA42002F00000 1 20020102 A 3710 1H51 VALVE CESSNA 310 310Q 2074242 CE CONT O470 IO470* 17026 SO VACUUM SYSTEM BROKEN A EA4A K NONE O OTHER IN INSP/MAINT 1 SO 09 100CP 3950 310Q0219 RUBBER FLAPPER BROKE OFF AND BLOCKED VACUUM INLET FROM RIGHT VACUUM PUMP. THEN RIGHT ENGINE WAS OPERATED ALONE, BOTH F AIL INDICATORS WERE OUT AND VACUUM INDICATED (0)ZERO. WHEN LEFT ENGINE WAS OPERATED ALONE BOTH INDICATORS WERE IN AND V ACUUM INDICATED 5.0 ON GAUGE. 1 L 7 2 3O 3 O 3A10 E1CE 2002031300086 20020313 00086 EU 2002 3 13 QXEA0200271 1 20020210 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - DENT ON RT FUSELAGE, APPROXIMATELY FRAME 6802 AND WL 38. 2 L 7 2 4F RT A20EU 2002031300087 20020313 00087 EU 2002 3 13 QXEA0200272 1 20020210 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - PANEL 75E HAS TWO HOLES WITH MINOR DAMAGE WHERE SCREWS WERE REMOVED. 2 L 7 2 4F RT A20EU 2002031300088 20020313 00088 SO 2002 3 13 EEJ2002F00001 1 20020207 A 3251 9539400 CHANNEL PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360* 17025 SO NLG STEERING SYS INOPERATIVE E EEJA O OTHER E VIBRATION/BUFFET CL CLIMB 1 NM 07 81659 11141 348070143 ON TAKE OFF WHEN THE PILOT RETRACTED THE GEAR. HE HEAD A STRANGE NOISE FROM THE NOISE GEAR AREA. WHEN HE PUT THE GEAR HANDLE DOWN. THE NOSE GEAR EXTEND ABOUT 45 DEGREES. UPON INSPECTION AFTER LANDING THE TILLER BALL (95387-00) HAD COME OUT OF THE STEERING CHANNEL ASSEMBLY AND LOCKED UP ON THE SIDE OF THE GUIDE TRACK (95758-07). 1 L 7 2 3O 3 O A7SO E9CE 2002031300089 20020313 00089 EU 2002 3 13 QXEA0200273 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 619.409 AND FRAME 13815A THE LUGS ON TOP ARE GOUGED. 2 L 7 2 4F RT A20EU 2002031300090 20020313 00090 EU 2002 3 13 02067308 1 20020208 A 3350 DM21 CONNECTOR BAG JETSTM JETSTM4112 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 308UE 41023 During preflight inspection for the flight from IAD to CRW, the crew reported that the emergency floor track lighting wa s inoperative. Maintenance personnel secured an electrical connector for the emergency floor track lighting. An operat ional check was satisfactory and the aircraft was returned to service. 1 L 7 2 4T RT A196 2002031300091 20020313 00091 EU 2002 3 13 QXEA0200274 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 600.898 FORWARD OF FRAME 13815 GOUGES ON LUGS. 2 L 7 2 4F RT A20EU 2002031300092 20020313 00092 EU 2002 3 13 QXEA0200275 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 600.894 AFT OF FRAME 13345 TOP LUGS ARE GOUGED. 2 L 7 2 4F RT A20EU 2002031300093 20020313 00093 EU 2002 3 13 QXEA0200276 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 582.394 THERE ARE GOUGES ON LUGS. 2 L 7 2 4F RT A20EU 2002031300094 20020313 00094 EU 2002 3 13 QXEA0200277 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 488.740 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300095 20020313 00095 EU 2002 3 13 QXEA0200278 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 506.022 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300096 20020313 00096 EU 2002 3 13 QXEA0200279 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 506.028 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300097 20020313 00097 EU 2002 3 13 QXEA0200280 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 517.749 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300098 20020313 00098 EU 2002 3 13 QXEA0200281 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 525.713 TOP LUGS HAVE GOUGES. REPAIRED IAW FOKKER MM 53-40-01, PGE 206, FIGURE 205 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B AND 4C. 2 L 7 2 4F RT A20EU 2002031300099 20020313 00099 EU 2002 3 13 QXEA0200282 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 545.391 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300100 20020313 00100 EU 2002 3 13 QXEA0200283 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 563.892 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300101 20020313 00101 NM 2002 3 13 02FDEA00194 1 20020220 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CORROSION, BS 1050, RBL 27, WL 208 ON TOP OF FLOORBEAM. R&R FLOORBEAM PER SRM 53-10-1 FIG 4. 2 L 7 3 4F RT A3WE 2002031500071 20020315 00071 NM 2002 3 15 02FDEA00195 1 20020312 A 5311 651766445 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 TWO DENTED AREAS IN TOP OF FRAME AT BS 500, LBL 39-45, WL 162. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 3 4F RT A3WE 2002031500074 20020315 00074 NM 2002 3 15 02FDEA00196 1 20020312 A 5311 651716445 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 TWO DENTED AREAS IN TOP OF FRAME BS 520, LBL 39-48, WL 162. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 3 4F RT A3WE 2002031500076 20020315 00076 NM 2002 3 15 02FDEA00197 1 20020219 A 5311 FRAME BOEING 727 727233 138408A NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FRAME IS DENTED AT BS 720 BETWEEN STR 24 & 25 LT. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 3 4F RT A3WE 2002031300102 20020313 00102 SO 2002 3 13 C2XA02CL072 1 20020309 A 3260 852701 SWITCH EMB 135 EMB135ER 3260203 SO LEFT GEAR FAULTY A C2XA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 27 14505 4559 145192 CLE FLIGHT#4007 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE WARNING ON APPROACH TO CLEVELAND.THE AIRCRAFT LANDED WIT H A NOSE GEAR UNSAFE LIGHT.MAINTENANCE REPLACED THE NOSE GEAR DOWN LOCK PROXIMITY SWITCHES.OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.P/N LEFT SWITCH 8-527-01 S/N A10691 2 L 7 2 4F RT T00011AT 2002031300103 20020313 00103 SO 2002 3 13 C2XA02CL070 1 20020308 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14942 145037 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHTS WERE INOPERATIVE FROM ROW 12 TO ROW 19.MAINTENANCE REPLACED THE EMERGENC Y LIGHT DC/AC INVERTER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002031300104 20020313 00104 SO 2002 3 13 C2XA02IA058 1 20020309 A 3350 3025103 LIGHT EMB 145 EMB145 3260210 SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14974 145161 EWR - During scheduled maintenance the right over wing emergency light was found to be inoperative. Maintenance removed and replaced the emergency light, performed an operational check and approved the aircraft for return to service. 2 L 7 2 4F RT T00011AT 2002031300105 20020313 00105 SO 2002 3 13 C2XA02IA057 1 20020309 A 3350 1317 LAMP EMB 145 EMB145 3260210 SO LEFT FUSELAGE BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16963 145116 AGU - During scheduled maintenance the left overwing emergency light was found to be inoperative. Maintenance relamped t he light assembly, performed an operational check, and approved the aircraft for return to service. 2 L 7 2 4F RT T00011AT 2002031300106 20020313 00106 NM 2002 3 13 F3LA200200105 1 20020301 A 2722 U26B ACTUATOR BOEING 737 7373L9 1384470 NM RUDDER TRIM INOPERATIVE A F3LA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 03 313FL 1019 26442 BLOCK TURNBACK. FLIGHT CREW REPORTED RUDDER WOULD NOT CENTER AFTER START UP AND TAXI. REPLACED RUDDER TRIM ACTUATOR AN D CHECKED OKAY. 2 L 7 2 4F RT A16WE 2002031300107 20020313 00107 NE 2002 3 13 MWEA020164 2 20020307 A 7510 320115 SHUTOFF VALVE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE RT ENGINE FAULTY A MWEA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 31 302ME 47102 665298 RIGHT HAND ENGINE ANTI-ICE VALVE CAUTION LIGHT ON, WITH RIGHT HAND ENGINE ANTI-ICE SELECTED ON. REMOVED AND REPLACED RI GHT HAND ENGINE COWL VALVE. THE BAD VALVE REMOVED HAD TRIPPED THE CIRCUIT BREAKER. 2 L 7 2 4F 4 F A6WE E2EA 2002031300108 20020313 00108 NE 2002 3 13 NACA20020009 2 20020302 A 7230 CASE BOEING 727 72723 1384004 NM PWA JT8 JT8D NE NR 3 ENGINE CRACKED A NACA K NONE R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 992AJ 1891 19428 655097 NR 3 ENGINE HIGH N2, LOW N1, HIGH EGT, HIGH F/F AT CRUISE AND HIGHER POWER SETTINGS. SURGE BLEED VALVE MOUNT FAILURE, R EPLACED ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 2002031300110 20020313 00110 2002 3 13 P2EA2002M012 4 20020301 A 2565 HOUSING DOUG DC9 DC982 3022082 WP L1 DOOR LOOSE A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 130NJ 49222 L1 DOOR SLIDE HOUSING FOUND LOOSE AT GATE AFTER FLIGHT. RESECURED HOUSING IAW MM 25-60. 2 L 7 2 4F A6WE 2002031300111 20020313 00111 NM 2002 3 13 P2EA2002M013 1 20020306 A 2131 7638102 CONTROLLER BOEING 737 737230 1384401 NM CABIN PRESSURE FAILED A P2EA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 05 123NJ 22121 AIRCRAFT WOULD NOT PRESSURIZE ON CLIMBOUT. AIRCRAFT LANDED AND RETURNED TO BLOCKS WITH NO INCIDENT. REMOVED AND REPLAC ED PRESSURE CONTROLLER IAW MM 21-31-21. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2002031300112 20020313 00112 EU 2002 3 13 QXEA0200284 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 443.026 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300113 20020313 00113 WP 2002 3 13 P2EA2002M015 1 20020304 A 3246 26088911 BOLT DOUG DC9 DC983 3022083 WP RT MLG SHEARED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 131NJ 49846 NR 4 MAIN WHEEL MISSING LUG DURING WALK AROUND THROUGH FLIGHT, LUG SHEARED AT END OF SHANK. REMOVED AND REPLACED NR 4 M AIN WHEEL IAW MM 32-40-01. 2 L 7 2 4F RT A6WE 2002031300114 20020313 00114 NM 2002 3 13 P2EA2002M016 1 20020304 A 5510 HINGE FITTING BOEING 737 737230 1384401 NM HORIZ STAB VIBRATES A P2EA K NONE E VIBRATION/BUFFET CR CRUISE 1 CE 05 122NJ 22120 INTERMITTENT VIBRATION OBSERVED AROUND THE AFT GALLEY FLOOR AREA. REMOVED AND REPLACED THE NR 4 HINGE FITTING ON THE LT HORIZONTAL STAB IAW MM 27-31-13. NO VIBRATION NOTED TO THIS DATE. 2 L 7 2 4F RT A16WE 2002031300115 20020313 00115 NM 2002 3 13 P5CA0200657 1 20020226 A 3150 WARNING SYSTEM BOEING 747 747122 1384872 NM COCKPIT MALFUNCTIONED A P5CA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 23 853FT 19753 WHEN READY FOR T/O, TAKEOFF WARNING HORN SOUNDED. ALL T/O CONDITIONS SATISFACTORY. CYCLED ALL CONTROL SURFACES SEVERAL TIMES, CYCLED FLAPS FULL TRAVEL, EXERCISED HORIZONTAL STAB LIMIT SWITCHES, PERFORMED OPS CHECK. ALL OPS CHECKS NORMAL ON GROUND. 2 L 7 4 4F A20WE 2002031300116 20020313 00116 2002 3 13 P5CA0200661 4 20020307 A 3425 P2590623908 COMPUTER BOEING 747 747122 1384872 NM E/E BAY FAULTY A P5CA K NONE O OTHER CR CRUISE 1 WP 23 853FT 19753 INS SELECTED IN DUAL, CAPT'S FLT DIRECTOR HEAD FOLLOWS HEADING BUG. F/O'S SIDE OPS NORMAL. SWAP ROLL COMPUTERS A & B. GROUND OPS CHECK OK. 2 L 7 4 4F A20WE 2002031300117 20020313 00117 EU 2002 3 13 QXEA0200285 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 443.021 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031300131 20020313 00131 SO 2002 3 13 EWK2002F00000 2 20020206 A 7310 96324128121 LINE BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO FUEL PRESSURE CORRODED E EWKA K NONE O OTHER IN INSP/MAINT 1 SO 07 6652A 687 TH1045 DEEP CORROSION ON FUEL PRESSURE LINE AT CONJUNCTION OF FUEL LINE AND DEFROSTER HEAT DUCT. INSULATE FUEL LINE FROM HEAT DUCT. DANGER/POTENTIAL FOR FIRE. 1 L 7 2 3O 3 O 3A16 E5CE 2002031300132 20020313 00132 SO 2002 3 13 EWK2002F00001 2 20020206 A 7310 96324128121 LINE BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO FUEL SYSTEM CORRODED A EWKA K NONE O OTHER IN INSP/MAINT 1 SO 07 6652A 6872 TH1045 DEEP CORROSION ON FUEL PRESSURE LINE AT CONJUNCTION OF FUEL LINE AND DEFROSTER HEAT DUCT. INSULATE FUEL LINE FROM HEAT DUCT. DANGER: POTENTIAL FOR FIRE. 1 L 7 2 3O 3 O 3A16 E5CE 2002031300134 20020313 00134 SO 2002 3 13 FFS2002F00000 1 20020207 A 3222 409872 BRACKET PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA NLG ACTUATOR CRACKED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 4301C 20251 318353001 SUPPORT BRACKET FOR NOSE GEAR ACTUATOR CRACKED. 1 L 7 2 3O 3 O A20SO E14EA 2002031300135 20020313 00135 SO 2002 3 13 FFS2002F00001 1 20020208 A 3222 409872 SUPPORT BRACKET PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA NLG ACTUATOR CRACKED E FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 4112K 18826 318353006 CRACK IN RADIUS OF NOSE GEAR ACTUATOR ATTACH SUPPORT BRACKET. FOUND DURING INSPECTION. 1 L 7 2 3O 3 O A20SO E14EA 2002031300136 20020313 00136 SO 2002 3 13 FFS2002F00002 1 20020206 A 3222 409872 SUPPORT BRACKET PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA NLG ACTUATOR CRACKED E FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 7164D 22328 318052013 UPPER SUPPORT BRACKET FOR NOSE GEAR ACTUATOR WAS FOUND CRACKED AT RADIUSED CUT OUT. FOUND DURING INSPECTION. 1 L 7 2 3O 3 O A20SO E14EA 2002031300137 20020313 00137 SO 2002 3 13 FFS2002F00004 1 20020207 A 3222 409872 SUPPORT BRACKET PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA NLG ACTUATOR CRACKED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 200AK 27552 318052180 SUPPORT BRACKET FOR NOSE GEAR ACTUATOR CRACKED AT RADIUS OF CUT OUT THAT PROVIDES CLEARANCE FOR POWER PACK ACTUATING ARM . PART REPLACED WITH NEW PART. SUSPECT THIS FAILURE OCCURRED AS A RESULT OF CYCLIC STRESSED IMPOSED. 1 L 7 2 3O 3 O A20SO E14EA 2002031300138 20020313 00138 SO 2002 3 13 FFSA200201 1 20020206 A 3222 U09872 SUPPORT BRACKET PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA NLG ACTUATOR CRACKED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 7164D 22328 318052013 UPPER SUPPORT BRACKETT FOR NOSE GEAR ACTUATOR WAS FOUND CRACKED AT RADIUSED CUT OUT. FOUND DURING INSPECTION. 1 L 7 2 3O 3 O A20SO E14EA 2002031300139 20020313 00139 SO 2002 3 13 FFSA200202 1 20020208 A 3222 409872 SUPPORT BRACKET PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA NLG ACTUATOR CRACKED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 4112K 18826 318353006 CRACK IN RADIUS OF NOSE GEAR ACTUATOR ATTACH SUPPORT BRACKET, FOUND DURING INSPECTION. 1 L 7 2 3O 3 O A20SO E14EA 2002031300140 20020313 00140 EA 2002 3 13 FL84656 2 20020222 A 8530 LW19042 SEAT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA CYLINDER NR1 MISREPAIRED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 234CE 1173 318052203 L366161A INTAKE VALVE AND SEAT, CYLINDER NR 1 NOT SEALING. APPEARS THAT VALVE SEAT AND / OR VALVE WERE IMPROPERLY GROUND. THIS PATTERN IS NOT CONSISTANT AROUND CIRCUMFERENCE OF VALVE. ONE SECTION OF SEAT (APPROX .7500 INCH)APPEARS TO HAVE ON CON TACT WITH VALVE. 1 L 7 2 3O 3 O A20SO E14EA 2002031300141 20020313 00141 EU 2002 3 13 C2XA02IA061 1 20020312 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14822 5981 5981 163 During scheduled maintenance the cabin overhead emergency light was found to be inoperative. Maintenance removed and rep laced the emergency light battery pack for section 1 A/B, performed an operational check of the emergency lighting syste m, and approved the aircraft for return to service. 2 H 7 2 4T RT A53EU 2002031300142 20020313 00142 EA 2002 3 13 FL846561 2 20020222 A 8530 LW13622 VALVE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA CYLINDER 1 FAILED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 234CE 1173 318052203 INTAKE VALVE AND SEAT CYLINDER NR 1 NOT SEALING. APPEARS THAT VALVE SEAT AND/OR VALVE WERE IMPROPERLY GROUND. THIS PAT TERN IS NOT CONSISTANT AROUND CIRCUMFERENCE OF VALVE. ONE SECTION OF SEAT(APPROX .7500) APPEARS TO HAVE NO CONTACT WITH VALVE. 1 L 7 2 3O 3 O A20SO E14EA 2002031300143 20020313 00143 CE 2002 3 13 FPI2002F00001 1 20020130 A 3260 S19061 SWITCH CESSNA 210 T210N 2073456 CE CONT O550 IO550* SO MLG WARNING SYS INOPERATIVE E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 102CR 550 21064745 821013R SWITCH USED TO ACTUATE LANDING GEAR WARNING HORN. SWITCH MOUNTED TO THROTTLE CABLE. 1 H 7 1 3O 3 O 3A21 E3SO 2002031300145 20020313 00145 CE 2002 3 13 HP62002F00000 1 20020128 A 7810 88630031 VALVE BEECH 36 A36TC 1151603 CE ALLSN 250B 250B17C GL EXHAUST STACK BROKEN B HP6R K NONE O OTHER IN INSP/MAINT 1 NM 01 42LH 153 EA163 CAE880631 FLAPPER ASSEMBLY, HAS BROKEN AWAY FROM HINGE SHAFT AND WAS EJECTED OUT EXHAUST STACK. CAUSE IS THOUGHT TO BE VIBRATION (METAL FATIGUE). 1 L 7 1 3O 3 T 3A15 E10CE 2002031300146 20020313 00146 CE 2002 3 13 HYI2002F00000 1 20020225 A 2400 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO COCKPIT FAILED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 161TA 1540 402C0070 ON PREFLIGHT, AVIONICS MASTER SWITCH, FAILED. MAINTENANCE REPLACED THE SWITCH AND RETURNED THE AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2002031300147 20020313 00147 CE 2002 3 13 HYI2002F00001 1 20020225 A 3222 51420025 DRAG BRACE CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO NLG CRACKED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 402VN 2243 402C0488 AT REGULAR SCHEDULED INSPECTION, MECHANIC FOUND NOSE GEAR, DRAG BRACE CRACKED AT ACTUATOR ATTACH HOUSING. REMOVED AND R EPLACED DRAG BRACE AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2002031300150 20020313 00150 WP 2002 3 13 AT0200035 1 20020131 A 5310 5277722412000 LONGERON DOUG DC9 DC932 3022066 WP STATION 718 A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 LONG. 8R CRACKED AT STATION 718. CORRECTIVE ACTION: INSTALLED LONGERON REPAIR AT STATION 718 L-8R IN ACCORDAN CE WITH DC-9 SRM 53-02, FIGURE 18. MATERIAL USED LONGERON (SPLICE) P/N 52777922-4-12000, LONGERON P/N 7637813-3,LOT # 1 WOWGBH3, P.O. # : 2K16862. WEIGHT ADDED : .966 LBS. 2 L 7 2 4F A6WE 2002031300151 20020313 00151 SO 2002 3 13 IK82002F00000 1 20020202 A 7714 78368 DRIVE UNIT PIPER PA30 PA30 7103002 SO LYC O320 IO320B1A 41508 EA TACHOMETER SHEARED B IK8S K NONE O OTHER IN INSP/MAINT 1 SO 11 8808Y 2053 301965 L435455A WHEN CASE WAS REMOVED PN 78368 ON TACH DRIVE WAS FOUND TO BE SHEARED. IF ACCY CASE HAD NOT BEEN REMOVED AT THIS TIME, W E WOULD HAVE HAD A MAJOR FAILURE OF LT ENGINE. HALF OF THE ROLL PINS WERE SHEARED AND FLOATING INSIDE TACH RING ON END OF CAMSHAFT. NEW REPLACEMENT PART IS MADE OF STAINLESS STEEL, WITH SOLID PIN INSTALLED, INSTEAD OF COMMON ROLL PIN .1875 X 2.33 PIN. THIS SHOULD BE LOOKED AT TBO, IF THE OIL PUMP HAD NOT COME UP FOR INSPECTION THEN THIS WOULD HAVE NOT HAVE BEEN FOUND UNTIL ENGINE FAILURE. DUE TO A COMPLETE TOP 300 HOURS PREVIOUSLY, HAD DECIDED TO GO BEYOND TBO. OIL PUMP S AVED THE ENGINE. 1 L 7 2 3O 3 O A1EA 1E12 2002031300152 20020313 00152 SO 2002 3 13 ISP2002F00000 2 20020219 A 8520 SA648044B PISTON CESSNA 421 421C 2076016 CE CONT O520 GTSIO520L 17032 SO ENGINE FAILED E ISPA C ABORTED TAKEOFF R Y PARTIAL RPM/PWR LOSS ENGINE STOPPAGE TO TAKEOFF 1 CE 05 5560G 91 421C0250 272169R NR 2 PISTON FAILED AT TAKE OFF UNDER FULL POWER. 1 L 7 2 3O 3 O A7CE E7CE 2002031300153 20020313 00153 SO 2002 3 13 J8S2002F00000 1 20020102 A 7810 40B19850 CROSSOVER TUBE PIPER PA46 PA46350P 7104602 SO LYC O540 TIO540AE2A 41532 EA EXHAUST SPLIT B J8SR K NONE O OTHER IN INSP/MAINT 1 GL 11 555ES 2139 4622129 L938361A CROSSOVER PIPE BETWEEN LEFT AND RIGHT TURBOCHARGERS WAS SPLIT UNDER HEAT SHIELD. ALLOWING HOT EXHAUST TO BLOW ON FORWAR D SIDE OF FIREWALL. THE FIREWALL WAS NOT DAMAGED, BUT THE HEAT MELTED THE VINYL TRIM ON THE FORWARD SIDE OF THE NOSE BA GGAGE COMPARTMENT. THE HEAT SHIELD SHOULD BE REMOVED EACH 500 HOURS TO ALLOW FOR INSPECTION OF EXHAUST CROSSOVER PIPE. 1 L 7 1 3O 3 O RT A25SO E14EA 2002031300155 20020313 00155 CE 2002 3 13 LAT2002F00000 1 20020103 A 2435 23079004 STARTER GEN CESSNA 441 441 2076020 CE GARRTT TPE331 TPE331* 01514 WP ENGINE SHORTED D LATA K NONE O OTHER IN INSP/MAINT 1 AL 03 441SA 9 9 4410172 COWLING OF AIRCRAFT FOUND WITH EXCESSIVE CARBON CONTAMINATION. REMOVED STARTER GENERATOR. TEARDOWN REPORT REVEALED THE STARTER SHORTED. CAUSE UNKNOWN. 1 L 7 2 3T 3 T RT A28CE E2WE 2002031300156 20020313 00156 CE 2002 3 13 M672002F00000 1 20020131 A 2760 55170114 LINE CESSNA 500 550 2076604 CE PWA 530 PW530A NE SPOILERS CHAFED E M67A K NONE O OTHER IN INSP/MAINT 1 WP 11 45VM 450 5500918 DURING A ROUTINE INSPECTION. FOUND THAT THE LEFT SPEEDBRAKE RETRACT LINE HAD BEEN CHAFED NEARLY ALL THE WAY THRU BY THE CENTER FLAP BELLCRANK ROD ATTACH BOLT. RECOMMEND CLOSE INSPECTION OF TUBING FOR PROPER CLEARANCE. 1 L 7 2 4F 4 F A22CE E00053EN 2002031300157 20020313 00157 SO 2002 3 13 C2XA02CL075 1 20020313 A 3350 20131A BATTERY EMB 135 EMB135ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27506 1897 145206 DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT ROW LIGHTS ON BOTH SIDES WERE INOPERATIVE.MAINTENANCE REPLACED THE EMERGEN CY LIGHT BATTERY AND BATTERY CHARGER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. P/N FOR BATTERY CHARGER IS 11-0049 S/N 13118 2 L 7 2 4F RT T00011AT 2002031300158 20020313 00158 NM 2002 3 13 2002F00216 1 20020207 A 2910 651782114 MODULE BOEING 727 727231 1384079 NM HYD SYSTEM FAILED A FX7A O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 19 54348 21967 DURING APPROACH AIRCRAFT HAD FULL SYSTEM 'A' HYDRAULIC FAILURE. REMOVED AND REPLACED 'A' SYSTEM HYD MODULE PER MM 29-11- 61. REMOVED AND REPLACED CASE DRAIN FILTERS ON ENGINES 1/2 PER MM 29-11-41. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002031300159 20020313 00159 NM 2002 3 13 2002F00217 1 20020208 A 2913 371380 PUMP BOEING 727 727231 1384079 NM NR 1 ENGINE FAILED A FX7A H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 19 54348 21967 DURING CLIMB-OUT FROM MIAMI, LOW PRESSURE LIGHT ON NR 1 ENGINE 'A' SYSTEM HYDRAULIC PUMP ILLUMINATED, ACCOMPLISHED SUPPL EMENTARY PROCEDURE, UPON ARRIVAL TO CCS MAINTENANCE TROUBLESHOT AND FOUND THE NR 1 ENGINE HYDRAULIC PUMP TO BE DEFECTIVE . OPS CHECK NORMAL, NO LEAKS NOTED. (M) 2 L 7 3 4F A3WE 2002031300162 20020313 00162 SO 2002 3 13 2002F00220 1 20020214 A 3350 7287580505 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 826MJ 145214 ELM-PIT - AFT CABIN EMERGENCY FLOOR PROXIMITY LIGHTING STRIP INOPERATIVE. MAINTENANCE REPLACED PIGTAIL. OP CHECKS GOOD . THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002031300163 20020313 00163 EA 2002 3 13 2002F00221 1 20020205 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77181 7181 DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT THE NR 3 EMERGENCY CEILING LIGHT WAS INOPERATIVE. REPLACED BULB. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031300164 20020313 00164 SO 2002 3 13 2002F00222 1 20020127 A 2421 GENERATOR EMB 145 EMB145LR 3260212 SO NR 1 ENGINE MALFUNCTIONED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 825MJ 145179 FLT 5892 - PRIOR TO TAKEOFF THE CAPTAIN STARTED THE TAKEOFF ROLL WHEN A CHIME WAS HEARD. THE CAPTAIN NOTICED THE NR 3 G ENERATOR OFF BUS MSG. CAPTAIN ABORTED TAKEOFF AT 40 KIAS AND EXITED THE RUNWAY ONTO THE TAXIWAY. THE CAPTAIN RESET THE GENERATOR. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002031300165 20020313 00165 EA 2002 3 13 2002F00223 1 20020121 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27173 7173 WHILE PERFORMING SERVICE CHECK NOTICED, AFT CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED IAW 33-15-16. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002031300166 20020313 00166 EA 2002 3 13 2002F00100 1 20020105 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A MASA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 27185 7185 FLT 6071 - PHX-EUG - THE CREW DECLARED AN EMERGENCY DUE TO A FLAP FAIL CAUTION MESSAGE. THE AIRCRAFT RETURNED TO THE FI ELD WHERE MAINTENANCE WERE ABLE TO RESET THE FLAP SYSTEM AND COMPLIED WITH PART 'A' OF THE AD. (M) 2 L 7 2 4F RT A21EA 2002031300167 20020313 00167 NM 2002 3 13 2002F00133 1 20020110 A 3350 GE1619 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 DURING A ROUTINE LINE CHECK, THE CREW FOUND THE RIGHT AFT EMERGENCY EGRESS LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMO VED AND REPLACED THE BULB WITH NO FURTHER DEFECTS. (M) 2 H 7 2 4T RT A13NM 2002031300168 20020313 00168 EA 2002 3 13 2002F00134 1 20020109 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27318 7318 WHILE PERFORMING EXTERIOR LIGHT CHECK, THE CREW FOUND THE RIGHT EXTERIOR FORWARD EMERGENCY LIGHT INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE BULB AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2002031300169 20020313 00169 EA 2002 3 13 2002F00135 1 20020117 A 3350 20131A100865 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27173 7173 FLT 6507 - CMH-PHL - BEFORE DEPARTING THE GATE THE CREW NOTICED THAT THE FLOOR EMERGENCY PROX LIGHTS WENT INOPERATIVE ON ROWS 1 THROUGH 6. AIRCRAFT WAS SWAPPED FOR FURTHER TROUBLESHOOTING. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK A ND THE POWER SUPPLY. ALL LIGHTS OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002031300170 20020313 00170 EA 2002 3 13 2002F00138 1 20020121 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27173 7173 WHILE PERFORMING SERVICE CHECK NOTICE, AFT CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED IAW 33-15-16. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002031300171 20020313 00171 SO 2002 3 13 2002F00147 1 20020129 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A MASA K NONE N FALSE WARNING CL CLIMB 1 SW 07 832MJ 145310 FLT 5808 - CLT-JAN - LAVATORY SMOKE DETECTOR WARNING MESSAGE ILLUMINATED DURING CLIMB-OUT. MAINTENANCE INSPECTED SYSTEM , PERFORMED OPS CHECK AND COULD NOT DUPLICATE DISC. THE A/C WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002031300172 20020313 00172 EA 2002 3 13 2002F00155 1 20020128 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77331 7331 FLT 5769 - BHM-PHL - THREE CEILING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RELAMPED. OPS CHECK GOOD. THE AIRCRAFT W AS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031300173 20020313 00173 NM 2002 3 13 2002F00224 1 20020202 A 3350 900542 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 803MA 22434 BATTERY PACK AND BASE ASSEMBLY FAILED ON RIGHT SIDE OVERWING EXIT EMERGENCY LIGHT SYSTEM. REMOVED AND REPLACED BATTERY PACK AND BASE ASSY. OPS CHECK NORMAL ON GROUND IAW MM 33-50-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002031300174 20020313 00174 NM 2002 3 13 2002F00225 1 20020124 A 3150 32EN614 SWITCH BOEING 727 727225 1384077 NM WARNING SYS DAMAGED A MYWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 803MA 22434 ON TAKEOFF, WARNING HORN WENT OFF ABORTING TAKEOFF. TROUBLESHOT WARNING SYSTEM TO DAMAGED SWITCH AND CHAFED WIRES. REP LACED SWITCH AND REPAIRED DAMAGED WIRING. OPS CHECK FOUND NORMAL ON GROUND IAW MM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002031300175 20020313 00175 NM 2002 3 13 2002F00226 1 20020122 A 2150 39854011 VALVE BOEING 727 727225 1384077 NM A/C PACK DEFECTIVE A MYWA B A EMER. DESCENT UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 889MA 21854 FOUND AIRCRAFT COULD NOT PRESSURIZE ON ASCENT, RIGHT PACK VALVE INTERMITTENT. A/C DESCENDED TO 10,000 FT. PERFORMED AO M PROCEDURES A/C LANDED. REPLACED PACK VALVE, OPS CHECK NORMAL ON GROUND. AIRCRAFT RETURN TO SERVICE. (M) 2 L 7 3 4F A3WE 2002031300176 20020313 00176 NE 2002 3 13 2002F00227 2 20020125 A 7200 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 2 FAILED A MYWA E C ENGINE SHUTDOWN ABORTED TAKEOFF R T PARTIAL RPM/PWR LOSS ENGINE CASE PENETRATION TO TAKEOFF 1 SO 19 886MA 21855 700592 AFTER GOOD 1.4 EPR CHECK AND WITH MAX THRUST TAKEOFF POWER SET, LOUD BANG NOTICED WITH LOSS OF EPR ON NR 2 ENGINE WHILE ROLLING TO APPROX 40 KN. ABORTED TAKEOFF AND TAXIED BACK TO RAMP, WHILE TAXIING TO RAMP PRECAUTIONARY SHUT DOWN NR 2 EN GINE. FOUND TURBINE BLADES DAMAGED. PREPARED AIRCRAFT FOR FERRY FLIGHT TO MAINTENANCE HUB. REMOVED AND REPLACED NR 2 ENGINE IAW 71-00. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2002031300177 20020313 00177 NM 2002 3 13 2002F00228 1 20020118 A 3350 900835A POWER SUPPLY BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 802MA 22433 EXIT SIGN ABOVE 31 C-D INOPERATIVE. REPLACED POWER PACK AND OPS CHECK AS PER MM 33-50-00. AIRCRAFT RETURN TO SERVICE. (M) 2 L 7 3 4F A3WE 2002031300178 20020313 00178 NM 2002 3 13 2002F00229 1 20020118 A 3350 900835A POWER SUPPLY BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 802MA 22433 EXIT SIGN ON BOTH RIGHT OVERWING DOORS INOPERATIVE. REPLACED POWER PACK AND OPS CHECKED AS PER MM 33-50-00. RETURNED A IRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 2002031300179 20020313 00179 NM 2002 3 13 2002F00230 1 20020118 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN DISCONNECTED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 802MA 22433 EPL TRACK LIGHT INOPERATIVE, ROW 21 ABC. ORANGE LIGHTS. RECONNECTED STRIP AND OPS CHECK AS PER MM 33-50-00. AIRCRAFT RETURN TO SERVICE. (M) 2 L 7 3 4F A3WE 2002031300180 20020313 00180 EU 2002 3 13 USAABA02002 1 20020111 A 5210 FE256000 ROLLER AIRBUS 330 A330323 3930335 EU L4 DOOR WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 673UW 8015 0337 MAN - FLT 197 - THE L4 DOOR WOULD NOT OPEN. MAINTENANCE FOUND THE FORWARD LOCKING ROLLER BEHIND THE STRIKER PLATE. THE ROLLER WAS REPOSITIONED. SUBSEQUENTLY, THE ROLLER WAS REPLACED. (M) 2 L 7 2 4F RT A46NM 2002031300181 20020313 00181 SO 2002 3 13 C2XA02CL076 1 20020312 A 2720 SKIN EMB 135 EMB135LR 3260305 SO RUDDER II CRACKED A C2XA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 SW 27 17513 145292 DURING ROUTINE MAINTENANCE THE RUDDER II SKIN WAS FOUND CRACKED.THE CRACK WAS APROX.7 1/2 INCHES LONG AND APROX. 4 INCHE S FROM THE BOTTOM.THE CRACK WAS PERPENDICULAR TO THE TRAILING EDGE.MAINTENANCE REPAIRED THE RUDDER II SKIN I/A/W CONTINE NTAL EXPRESS EC5540-01015.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT TOOO11AT 2002031300183 20020313 00183 EU 2002 3 13 USAASA02013 1 20020119 A 2120 SMOKE AIRBUS A319 A319112 3930323 EU CABIN DETECTED A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 747UW 1301 CLT - FLT 53 - EN ROUTE CLT-JAX - AFTER TAKEOFF, THICK SMOKE FILLED THE CABIN, BUT NOT THE COCKPIT. FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIR CONDITIONING PACKS AND RAN THE ENGINES AT VARIOUS POWER SETTINGS. NO SMOKE WAS NOTED. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2002031300184 20020313 00184 NM 2002 3 13 USAASB02012 1 20020116 A 2741 65C255296 MODULE BOEING 737 7374B7 1384702 NM COCKPIT FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 448US 41242 24892 MSY - FLT 450 - AFTER TAKEOFF, CREW REPORTED FLAGS ON THE FLIGHT COMPUTER WITH ZERO AIRSPEED AND ALTITUDE TO FL500 ON TH E MODE CONTROL PANEL. THE MACH AIRSPEED AND TRIM INDICATIONS ALSO FAILED. THE FLIGHT RETURNED TO MSY AND LANDED WITHOU T FURTHER INCIDENT. MAINTENANCE REPLACED THE MODE CONTROL PANEL. THE FLIGHT TOOK OFF AND ENCOUNTERED THE SAME PROBLEM, RESULTING IN A SECOND RETURN TO FIELD AT MSY. MAINTENANCE R&R THE STABILIZER TRIM CONTROL COLUMN CUT OUT SWITCHING MODU LE. ALSO, REMOVED AND REPLACED BOTH A AND B FLIGHT CONTROL COMPUTERS AND AUTO PILOT STABILIZER TRIM SERVO. ACCOMPLISHE D SATISFACTORY FUNCTIONAL TEST OF FLIGHT CONTROL COMPUTERS, AUTO PILOT SYSTEM AND STABILIZER TRIM SERVO. (M) 2 L 7 2 4F RT A16WE 2002031300185 20020313 00185 NM 2002 3 13 2002F00104 1 20020114 A 3350 WIRE HARNESS BOEING 757 75723A 1384967 NM CABIN DAMAGED A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 757NA 24567 EMERGENCY ESCAPE PATH LIGHTING SEAT 27ABC INOPERATIVE. INVESTIGATION REVEALED WIRES BROKEN AND BURNED AT PLUG. REPLACE D WIRING HARNESS. (M) 2 L 7 2 4F RT A2NM 2002031300186 20020313 00186 EA 2002 3 13 2002F00112 1 20020130 A 3620 7546911 SENSOR CNDAIR CL600 CL6002B19 1900309 EA A/C BAY FAILED A ASOA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 11 857AS 7411 FLT 4531 - ON FINAL APPROACH INTO ATL, SHORTLY AFTER APU START UP, THE 'SMOKE TOILET' MESSAGE ILLUMINATED. THE CAPTAIN IMMEDIATELY SHUT DOWN THE APU AND TRANSFERRED THE BLEEDS BACK TO THE ENGINE. THE MESSAGE EXTINGUISHED. THE FLIGHT ATTE NDANT REPORTED A SLIGHT BUILD UP OF SMOKY HAZE IN THE CABIN THAT QUICKLY DISSIPATED ON LANDING. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT COALESCER SOCK AND DUCT TEMPERATURE SENSOR. OPERATIONAL CHECKS NORMA L. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031300187 20020313 00187 2002 3 13 2002F00132 4 20020121 A 3417 ADC BOEING 747 747230B 1384889 NM NR 1 FAULTY A Q2SA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 23 743SA 22671 IN CRZ WITH A/P AND AUTO THROTTLE ENGAGED A/C PITCHED UP WITH ALT HOLD DISENGAGED. BOTH F/D IS INOPERATIVE NR 1 AND 3 I NS LOST WIND AND G/S INFORMATION, ALL N1 IS INOPERATIVE. N1 LIMIT INOP TAT INOP TCAS INOP NR 1 MACH IND INOPERATIVE AND NR 1 ALTIMETER WENT TO STANDBY MOD. ALL SYSTEM CAME BACK TO NORMAL OPS AFTER 10-15 MINUTES SUSPECT NR 1 CADC. REMOVED AND REPLACED NR 1 CADC AS PER MM. OPS NORMAL AS PER MM 34-12-00. (M) 2 L 7 4 4F A20WE 2002031300188 20020313 00188 NM 2002 3 13 2002F00144 1 20020122 A 7711 FITTING BOEING 757 75723N 1384973 NM RT ENGINE LOOSE A AMTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 11 528AT 30887 DURING TAKEOFF, THE RIGHT ENGINE WOULD NOT REACH MAX TAKEOFF EPR WITH EEC AND LIMITER ON. ENGINE PARAMETERS NORMAL FOR LOW EPR TO WITH EEC AND ENGINE LIMITER OFF NOT CHECKED. MAINTENANCE PERFORMED AMM TEST 13 TAKEOFF POWER ON GROUND. COU LD NOT DUPLICATE ANY PROBLEMS. RIGHT ENGINE WILL REACH TAKEOFF EPR WITH EEC ON. EPR RAKES INSPECTED AND LOOSE PITOT FI TTINGS FOUND. (M) 2 L 7 2 4F RT A2NM 2002031300189 20020313 00189 NM 2002 3 13 2002F00145 1 20020122 A 2612 710127 FIRE LOOP BOEING 757 757* NM LT ENGINE FAULTY A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 553TZ 1052 32587 DURING CRUISE, EICAS STATUS MESSAGE LEFT ENGINE FIRE LP 2 DISPLAYED. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE D ETECTOR NR 3 FIRE OVERHEAT ELEMENT. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 2002031300190 20020313 00190 WP 2002 3 13 2002F00146 1 20020115 A 3320 100866103 TERMINAL BLOCK LKHEED 1011 10113853 5265020 WP CABIN MALFUNCTIONED A AMTA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE IN INSP/MAINT 1 GL 11 161AT 1219 DURING OPERATIONAL CHECK FOR MACH DISCREPANCY, FIRE WAS NOTICED AT LUMINAIRE TERMINAL BLOCK ABOVE SEATS 17 AND 18G. POW ER WAS SECURED AND NO OTHER DAMAGE VISIBLE. MAINTENANCE REMOVED AND REPLACED LUMINAIRE AND LUMINAIRE TERMINAL BLOCK ABO VE SEATS 17 AND 18G IAW MM 33-21-04. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A23WE 2002031300191 20020313 00191 NM 2002 3 13 2002F00154 1 20020125 A 2782 1U1110 ACTUATOR BOEING 727 727264 138408M NM L/E FLAP LEAKING A AMTA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 764AT 53038 22984 FLT 8001 - DURING CRUISE 'A' SYSTEM HYDRAULIC QUANTITY DECREASED TO ZERO, FOLLOWED BY NR 1 'A' SYSTEM PUMP LOW PRESSURE LIGHT. FLIGHT CREW FOLLOWED AOM PROCEDURE. AIRCRAFT LANDED AT MMUN WITHOUT INCIDENT. MAINTENANCE FOUND 'A' SYSTEM RES ERVOIR WITH 1 GALLON FLUID REMAINING, CASE DRAIN FILTERS REVEALED NO DEBRIS. THE NR 3 KRUEGER FLAP ACTUATOR WAS REMOVED AND REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002031300192 20020313 00192 NM 2002 3 13 AWXA200200216 1 20020224 A 5320 7075T6040 FLOOR SUPPORT BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 LCQ - MAJOR REPAIR - "C" - DURING C-14 CHECK CABIN FLOOR SUPPORT WAS CORRODED BEYOND LIMITS AT BS 279, LBL 28. MAINTENAN CE REMOVED CORRODED SECTION OF CABIN FLOOR SUPPORT AT BS 279, LBL 28, FSBRICATED NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW B737-200 SRM 51-30-2, PG. 32. 2 L 7 2 4F RT A16WE 2002031300193 20020313 00193 NM 2002 3 13 UPS02237479 1 20020102 A 5753 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 4 FLAP TRACK PITTING CORROSION ON FACE OF LANDING GEAR ATTACH PAD. LANDING GEAR ATTACH PAD MACH INED IAW OHM 57-40-01. TRACK REPLACED IAW MM 27-51-31. 2 L 7 3 4F A3WE 2002031300194 20020313 00194 NM 2002 3 13 UPS02237481 1 20020102 A 5753 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 4 FLAP TRACK PITTING CORROSION ON AUX SPAR PAD. CORROSION ON PAD REMOVED BY MACHINING IAW OHM 5 7-40-01. TRACK REPLACED IAW 27-51-31. 2 L 7 3 4F A3WE 2002031300195 20020313 00195 NM 2002 3 13 UPS02237482 1 20020102 A 5753 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 4 FLAP TRACK, PITTING CORROSION ON BORE OF HOLE C AND ON COUNTER BORE OF HOLE C. TRACKS REPLACE D. 2 L 7 3 4F A3WE 2002031300196 20020313 00196 NM 2002 3 13 UPS02237491 1 20020123 A 3510 LEVER BOEING 727 727172C 1384058 NM O2 REGULATOR INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:IN, F/O'S 02 DEMAND REGULATOR EMERGENCY LEVER INOP. REMOVED AND REPLACED F/O'S 02 REGULATOR AS REQUIRED OPS CHECK & LEAK CHECK GOOD. 2 L 7 3 4F A3WE 2002031300197 20020313 00197 NM 2002 3 13 UPS02237493 1 20020122 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE:IN EMERGENCY EXIT LIGHTS OVER MAIN ENTRY DOOR INOP. REMOVED AND REPLACED BATTERIES, OPS CHECKS NORMAL. 2 L 7 3 4F A3WE 2002031300198 20020313 00198 NM 2002 3 13 UPS02237499 1 20020102 A 5753 65192695 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 4 FLAP TRACK PITTING CORROSION ON BORE OF AFT LT HOLE ON MLG SUPPORT BEAM PAD. FLAP TRACK REPLA CED. 2 L 7 3 4F A3WE 2002031300199 20020313 00199 NM 2002 3 13 UPS02237500 1 20020102 A 5753 65192696 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 5 FLAP TRACK PITTING CORROSION ON AUX SPAR ATTACH PAD. TRACK REPLACED. 2 L 7 3 4F A3WE 2002031300200 20020313 00200 NM 2002 3 13 UPS02237501 1 20020102 A 5753 65192696 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+CI NR 5 FLAP TRACK PITTING CORROSION IN BORE AND COUTERBORE OF AFT RT HOLE ON FWD MOUNT PAD. TRACK RE PLACED IAW MM 27-51-31. 2 L 7 3 4F A3WE 2002031300201 20020313 00201 NM 2002 3 13 UPS02237502 1 20020102 A 5753 65196296 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 5 FLAP TRACK, PITTING CORROSION IN BORE AND COUNTER BORE OF AFT LT HOLE ON FWD PAD. TRACK REPLA CED IAW MM 27-51-31. 2 L 7 3 4F A3WE 2002031300202 20020313 00202 NM 2002 3 13 UPS02237503 1 20020103 A 5320 INTERCOSTAL BOEING 727 727185C 138406N NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI INTERCOSTAL BETWEEN FLOORBEAMS AT BS 320 RBL 55 APPROX IN THE E/E BAY IS CRACKED. 2 L 7 3 4F A3WE 2002031300204 20020313 00204 NM 2002 3 13 UPS02237507 1 20020123 A 3350 BATTERY BOEING 727 72727C 138400J NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERIES NOT CHARGED OVER MAIN ENTRY DOOR, PARTS ON F/E'S DESK LIGHT ASSY 10-0 067-9. INSTALLED NEW BATTERIES. 2 L 7 3 4F A3WE 2002031300207 20020313 00207 NM 2002 3 13 UPS02237512 1 20020102 A 5753 65192086 FLAP TRACK BOEING 727 727185C 138406N NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI NR 2 FLAP TRACK PITTING CORROSION ON FACE OF FWD MOUNT PAD. 2 L 7 3 4F A3WE 2002031300208 20020313 00208 NM 2002 3 13 UPS02237513 1 20020102 A 5347 SEAT TRACK BOEING 727 727185C 138406N NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI SURFACE CORROSION ON THE LWR SURFACE OF SEAT TRACK UPPER FLANGE AT BS 350 LBL 45. 2 L 7 3 4F A3WE 2002031300209 20020313 00209 NM 2002 3 13 UPS02237514 1 20020102 A 5310 DOOR FRAME BOEING 727 727185C 138406N NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI ON REMOVAL OF DAMAGED BRACKET, FWD LWR DOOR STOP FITTING FOUND DAMAGED AND DOOR CUTOUT FRAME CRACKE D AT LWR FWD FASTENER FITTING HOLE AFT CARGO DOOR CUTOUT FWD FRAME. 2 L 7 3 4F A3WE 2002031300210 20020313 00210 EU 2002 3 13 RAIA00203096 1 20020308 A 7931 311905701 VALVE AEROSP ATR72 ATR72202 8680940 EU MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 722TE 220 5592-STL - LOW OIL PRESSURE ANNUNCIATOR LIGHT ILLUMINATED DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE OIL PRESSURE PRIORITY VALVE, OPS AND LK CK OK. 2 H 7 2 4T RT A53EU 2002031300211 20020313 00211 EU 2002 3 13 RAIA00203097 1 20020308 A 3230 AIR864782 ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 572HK 1046 436 41091 5421-RIC- RED LIGHT IN GEAR HANDLE REMAINED ON AFTER GEAR RETRACTION. MAINTENANCE REMOVED, REPAIRED AND REINSTALLED THE NOSE LANDING GEAR RETRACT ACTUATOR, OPS AND LK CK OK. 2 L 7 2 4T RT A41NM 2002031300212 20020313 00212 GL 2002 3 13 RAIA00203098 2 20020309 A 7200 AE3007A ENGINE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL MALFUNCTIONED A RAIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 807HK 7324 145119 310126 5291-PIT- AT 40 KTS GOT WARNING "E2 ATTCS NO MARGIN". MAINTENANCE REMOVED AND REPLACED #2 ENGINE, OPS AND LK CK OK. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002031500128 20020315 00128 SO 2002 3 15 C2XA02TY048 1 20020214 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 TYS DURING A ROUTINE MAINTENANCE FOUND THE LEFT EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BULB A ND THE OPS CHECK WAS GOOD. AIRCRAFT RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002031400001 20020314 00001 EU 2002 3 14 C2XA02IA060 1 20020311 A 3230 D228830001 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU NOSE WHEEL WELL FAULTY A C2XA K NONE O OTHER AP APPROACH 1 SW 27 97841 280 IAH - Flt 3659 - Crew reported that on approach the nose gear unlock indication flashed on and off with a loud banging n oise heard. The aircraft landed at IAH without incident. Maintenance removed and replaced the proximity switch and the p roximity switch electronic unit. The aircraft was returned to service and the problem re-occurred on the same date, flig ht 3329. Maintenance performed an adjustment of the nose landing gear proximity switch and the aircraft was approved for return to service. 2 H 7 2 4T RT A53EU 2002031400006 20020314 00006 CE 2002 3 14 BSY2002F00002 1 20020225 A 7933 MS3106A12S3S CONNECTOR BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO OIL TEMP SENSOR FAILED D BSYA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 33DK TH372 AFTER TAKEOFF, LT ENGINE, OIL TEMPERATURE, SHOT UP TO RED LINE, RETURNED TO AIRPORT AFTER FEATHERING ENGINE. FOUND PIN PULLED OUT OF OIL TEMPERATURE CONNECTOR PLUG, INSTALLED NEW CONNECTOR PLUG, OPS CHECKS GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2002031400007 20020314 00007 CE 2002 3 14 BSY2002F00003 1 20020208 A 3260 SQUAT SWITCH BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO MLG FROZEN D BSYA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 696BD TH352 LANDING GEAR WOULD NOT GO UP. FOUND SQUAT SWITCH FROZEN. THAWED OUT SWITCH CLEANED AND LUBED CYCLED GEAR. OPS CHECK G OOD. 1 L 7 2 3O 3 O 3A16 E5CE 2002031400008 20020314 00008 CE 2002 3 14 BSY2002F00004 1 20020208 A 7714 963840593 TACH GENERATOR BEECH 58 58 1152740 CE CONT O520 IO520E 17032 SO LEFT INOPERATIVE D BSYA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 07 3703Q TH1189 LEFT TACH QUIT AFTER TAKE OFF, RETURNED TO AIRPORT. REMOVED AND REPLACED THE GENERATOR OPS CHECKS GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2002031400009 20020314 00009 CE 2002 3 14 BSY2002F00005 1 20020207 A 2140 FR81094 HEATER BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO COCKPIT FAILED D BSYA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 4AW TH450 PILOT NOTICED SMOKE IN COCKPIT, LANDED AT AIRPORT. MAINTENANCE INSPECTED AIRCRAFT FOUND NO ELECRTICAL PROBLEMS, TURNED ON HEATER AND CABIN FILLED WITH SMOKE. REMOVED AND REPLACED HEATER ASSY. 1 L 7 2 3O 3 O 3A16 E5CE 2002031400010 20020314 00010 CE 2002 3 14 GNB2002F00000 1 20020227 A 2140 722099 BLOWER MOTOR CESSNA 402 402C 207590R CE HEATER FAILED D GNBA O OTHER O OTHER NR NOT REPORTED 1 SW 01 525RH 86 402C0525 PILOT REPORTED HEATER QUIT WORKING. TROUBLESHOOT HEATER ASSEMBLY FOUND COMBUSTION AIR BLOWER MOTOR TURNING VERY SLOWLY . 1 L 7 2 3O A7CE 2002031400011 20020314 00011 CE 2002 3 14 KNFA611F 1 20020302 A 5630 52111312 WINDOW CESSNA 402 402A 207590M CE CONT O520 IO520* 17032 SO EMERGENCY EXIT DEPARTED D KNFA O OTHER D E INFLIGHT SEPARATION VIBRATION/BUFFET NR NOT REPORTED 1 WP 19 99AT 18753 402A0022 FLYING AT 7,000 FEET, EXPERIENCED SEVERE CLEAR AIR TURBULENCE. LOST 1,000 FEET WITHIN SECONDS AND HEARD A LOUD POP. LOOKED BACK AND NOTICED THE EMERGENCY EXIT WINDOW WAS GONE. 1 L 7 2 3O 3 O A7CE E5CE 2002031400012 20020314 00012 CE 2002 3 14 MHJ2002F00000 1 20020128 A 2824 476411 TRANSFER PUMP CESSNA 401 401 207590C CE CONT O520 GTSIO520C 17032 SO FUEL SYSTEM INOPERATIVE E MHJA K NONE O OTHER IN INSP/MAINT 1 SW 05 3208Q 4010008 TRANSFER PUMP, INOPERATIVE. 1 L 7 2 3O 3 O A7CE E7CE 2002031400013 20020314 00013 WP 2002 3 14 O9I2002F00000 2 20020218 A 7261 31020473 HOUSING GULSTM 690TP 690A 0141722 SW GARRTT TPE331 TPE331* 01514 WP OIL PRES PUMP CRACKED B O9IR A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 95JM 22 11289 P79574 DURING FLIGHT THE PILOT NOTICED THE RIGHT ENGINE OIL PRESSURE DROPPED ABOUT 30 PSI. THE AIRPLANE LANDED UNEVENTFULLY. THE ENGINE WAS DISASSEMBLED AND THE OIL PRESSURE PUMP HOUSING WAS FOUND CRACKED, RESULTING IN AN INTERNAL OIL LEAK REDUC ING ENGINE OIL PRESSURE, 22 HOURS PRIOR TO THIS EVENT THE SAME FAILURE HAPPENED ON THE SAME ENGINE. THE FIRST OIL PUMP FAILURE OCCURED AT 271.8 HOURS SINCE ENGINE OVERHAUL. THE SECOND OIL PRESSURE PUMP FAILURE OCCURED 22.0 HOURS LATER. T HE FAILED OIL PUMPS CONFIGURATION (PN 3103217-3). FOLLOWING THE SECOND OIL PRESSURE PUMP FAILURE, OIL PUMP WAS INSTALLE D (PN 897165-19). THE MANUFACTURER IS REPORTED TO BE ENGINEERING A REPLACEMENT OIL PUMP WITH INCREASED DURABILITY. 1 H 7 2 3T 3 T 2A4 E2WE 2002031400014 20020314 00014 2002 3 14 R2J2002F00000 4 20020213 A 3457 GA58 ANTENNA BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA GPS MISINSTALLED B R2JR K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 21 574GS BB429 DURING AAIP PHASE INSPECTION, FOUND UN-DOCUMENTED GPS INSTALLATION. FOUND ANTENNA MOUNTED IN PRESSURE VESSEL AREA WITH NO SEALING OR DOUBLER, COULD CAUSE VESSEL FAILURE. REPAIR OF FUSELAGE AND ALTERATION, INSTALLING ANTENNA, MADE USING AP PROVED DATA. ALWAYS DO A GOOD PAPERWORK CHECK WHEN DOING INSPECTION CHECK FOR UN-AIRWORTHY INSTALLATIONS. 1 L 7 2 4T 4 T A24CE E4EA 2002031400015 20020314 00015 CE 2002 3 14 R2J2002F00001 1 20020213 A 5320 9542001514 FLOOR SUPPORT BEECH 95 B95 1153404 CE CONT O470 IO470* 17026 SO CARGO BAY CORRODED B R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 111KF 3108 TC633 AT ANNUAL INSPECTION AFTER FINDING CRACKS IN AREA OF DOOR STEP, THE BAGGAGE FLOOR WAS COMPLETELY REMOVED. FOUND INSULAT ION ON UNDERSIDE OF FLOOR BOARD, HAD RETAINED SOME MOISTURE, CAUSING UNDER FLOOR STRUCTURE TO CORRODE. AIRCRAFT IS 1964 MODEL. SUGGEST A SERVICE BULLETIN TO CALL OUT FOR INSPECTION OF THIS AREA AND REMOVAL OF FIBERGLASS SOUND PROOFING. H AD TO REMOVE WHOLE PANEL TO NOTICE DAMAGE MOSTLY TO TOP OF CHANNELS, NEW PARTS INSTALLED. (PHOTO) 1 L 7 2 3O 3 O 3A16 E1CE 2002031400016 20020314 00016 EA 2002 3 14 02072635 1 20020213 A 3610 14403103 INSULATION CNDAIR CL600 CL6002B19 1900309 EA FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 635BR 7295 During cruise of the flight from SAV to ORD, the crew reported that the L/H engine 14th stage duct EICAS message illumin ated. The crew accomplished the QRH procedures and diverted to CAE where the aircraft was landed without incident. Mai ntenance personnel found that the insulation had failed on the L/H engine 14th stage bleed pylon duct. The duct was rem oved and replaced. Engine run operational checks were satisfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002031400017 20020314 00017 CE 2002 3 14 R2J2002F00002 1 20020212 A 5312 551104013 BULKHEAD CESSNA 500 500CESSNA 2076602 CE FUSELAGE CRACKED B R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 928RD 11590 5000204 WHILE TROUBLESHOOTING PRESSURIZATION PROBLEM FOUND CRACKING AT FASTENER ON FORWARD PRESSURE BULKHEAD BOX ASSEMBLY. REPA IR WAS COMPLETED USING APPROVED DATA. 4TH AIRCRAFT FOUND WITH CRACKING IN THIS AREA. PAY SPECIAL ATTENTION TO THIS ARE A ON OLDER 500 MODEL CITATIONS. 1 L 7 2 4F A22CE 2002031400018 20020314 00018 2002 3 14 R2J2002F00003 4 20020212 A 3457 ANTENNA CESSNA 500 500CESSNA 2076602 CE GPS MISINSTALLED B R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 928RD 5000204 DURING ACCEPTANCE INSPECTION, FOUND IMPROPER MOUNTING ON PRESSURE VESSEL OF GPS ANTENNA. NO DOUBLER OR SEALER INSTALLED , COULD CAUSE STRUCTURAL FAILURE. INSTALLATION UN-AIRWORTHY, REPAIRED DAMAGE AND REINSTALLED ANTENNA USING APPROVED DAT A. NO APPROVAL DATA FOUND FOR GPS INSTALLATION. DO A GOOD PAPERWORK INSPECTION WHERE PERFORMING ANY TYPE OF INSPECTION . (PHOTO) 1 L 7 2 4F A22CE 2002031400019 20020314 00019 CE 2002 3 14 R2J2002F00004 1 20020213 A 5720 CACB997435C SPLICE PLATE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA WING IMPROPER PART B R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 574GS 10000 BB429 DURING AAIP PHASE INSPECTION DISCOVERED IMPROPER PARTS HAD BEEN INSTALLED WHILE INSTALLING AVIADESIGN WING SPAR STRAP PE R STC SA 1602CE. STC HOLEDER WAS CONTACTED AND APPROVED PART, WHICH IS A SPECIAL ALLOY, WAS INSTALLED. FAA-PMA PART. SUGGEST CALLING THE STC HOLDER IF THERE IS ANY DOUBT NON-APPROVED PACTS HAVE BEEN INSTALLED. CHECK PAPERWORK CAREFULLY. 1 L 7 2 4T 4 T A24CE E4EA 2002031400020 20020314 00020 EU 2002 3 14 S4W2002F00000 1 20020131 A 3250 5322012134 ROD END PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE NLG STEERING SEPARATED A S4WR K NONE O OTHER IN INSP/MAINT 1 WP 07 308NA 2886 226 PCEPR0082 PILOT CALLED THE ON-CALL MECHANIC AND REPORTED THAT UPON LANDING AT AIRPORT, THE NOSE WHEEL STEERING DID NOT FEEL NORMAL . AFTER ENGINE SHUT DOWN THE PILOT LOOKED IN NOSE GEAR WELL AND FOUND THE NOSE WHEEL STEERING ROD AND EYELET HAD SEPARA TED FROM THE ROD END ASSEMBLY. THE MECHANIC REPLACED THE ROD END WITH SERVICEABLE PART AND FOUND NO OTHER DISCREPANCIES . THIS COULD HAVE RESULTED IN LOSS OF CONTROL OF THE AIRCRAFT ON LANDING/TAKEOFF/TAXI. PICTURES OF DEFECTIVE PART WILL BE EMAILED TO MFG FOR REVIEW 2/4/2002. 1 L 7 1 3T 4 T RT A78EU E26NE 2002031400021 20020314 00021 EU 2002 3 14 SDRS2002001 1 20020312 A 6220 L662C1014101 SUPPORT UROCOP EC135 EC135P1 8680990 EU MAIN ROTOR CRACKED E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 2034 0054 UPON REMOVAL OF MAIN ROTOR HUBCAP, ALL FOUR MOUNTING LUGS THAT ATTACH THE HUBCAP TO THE SUPPORT WERE FOUND TO BE CRACKED . ONE LUG WAS ALMOST READY TO DEPART THE SUPPORT. THIS SUPPORT P/N IS USED ON THE QUICK REMOVE HUBCAP. IT APPEARS THA T ALL FOUR ATTACH POINTS HAD FRETTING CORROSION. IN THE EVENT ALL FOUR ATTACH POINTS WOULD FAIL, THE HUBCAP WOULD DEPAR T THE AIRCRAFT. 1 G 7 2 3U O H88EU 2002031400024 20020314 00024 CE 2002 3 14 SIIA004K 1 20020311 A 5246 655230432 ACCESS DOOR CESSNA 500 550 2076604 CE RT NACELLE MISSING E SIIA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 WP 01 552SM 698 3 5500929 RIGHT ENGINE OIL ACCESS DOOR DISCOVERED MISSING ON POST-FLIGHT INSPECTION. IN-FLIGHT SEPARATION PROBABLY OCCURRED APPRO XIMATELY 2.5 HOURS INTO FLIGHT WHEN CREW NOTICED SLIGHT VIBRATION. WHEN QUERIED, CESSNA REPORTS PROBLEMS WITH SEPARATIO NS OF THESE ENGINE OIL ACCESS DOORS. 1 L 7 2 4F A22CE 2002031400047 20020314 00047 NM 2002 3 14 02FDEA00198 1 20020302 A 2710 AILERON DOUG MD11 MD11 3023602 NM WING MALFUNCTIONED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 590FE 48505 AFTER T/O RIB HAD DEFLECTED AILERON DISAGREE ALERT C/W RED TABS. MX DEF DEFLECTED AILERON SYS PER IAW MEL 27-2, PER MET HOD A AILERON RETRACTED UP. 2 L 7 3 4F RT A22WE 2002031400048 20020314 00048 CE 2002 3 14 TIM2002F00005 1 20020122 A 3010 503801391 DEICE SYSTEM BEECH 99 B99 1154004 CE PWA PT6 PT6A28 EA LEFT WING INOPERATIVE E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 99CA U127 DURING A WALK AROUND INSPECTION AND SUBSEQUENT OPERATIONAL CHECK, IT WAS DETERMINED THAT THE LEFT WING SURFACE DEICER WA S INOPERATIVE. A CLOSER INSPECTION REVEALED WEATHER CHECKING AROUND PREVIOUS BOOT PATCHES AND POSSIBLE WATER CONTAMINAT ION. REMOVED AND REPLACED BOOT IAW MM. DEICER APPEARED TO HAVE BEEN ON THE AIRCRAFT FOR SOME TIME. 1 L 7 2 3T 4 T A14CE E4EA 2002031400049 20020314 00049 CE 2002 3 14 TIM2002F00006 1 20020205 A 5520 1156100153 COLLAR BEECH 99 B99 1154004 CE PWA PT6 PT6A28 EA LT ELEVATOR CRACKED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 899CA 35565 U104 DURING AN INSPECTION OF THE ELEVATOR, IT WAS FOUND THAT THE OUTBOARD ELEVATOR COLLAR WAS CRACKED AT THE TAPER PIN. THE DEFECTIVE TORQUE TUBE WAS REPLACED AND THE NEW TUBE (SERVICEABLE) WAS RIGGED IAW MM. INSPECTION OF THE CRACKED COLLAR W AS INCONCLUSIVE AS TO WHETHER THE CRACK WAS CAUSED BY NORMAL WEAR OR POSSIBLE OVER TORQUING DUE TO THE AMOUNT OF PAINT I N THE AREA. 1 L 7 2 3T 4 T A14CE E4EA 2002032500046 20020325 00046 NM 2002 3 25 02FDEA00199 1 20020312 A 3220 BRACKET BOEING 727 727233 138408A NM NLG DAMAGED A FDEA O OTHER E VIBRATION/BUFFET LD LANDING 1 SO 25 268FE 21674 UPON LAND A/C SHIMMIED VIOLENTLY WITH NO NOSE WHEEL STEERING. REMOVED AND REPLACED BRACKET FROM LWR TORQUE LINK & BENT GRD SENSING ROD FROM UPPER TORQUE LINK. REPLACED BENT PISTON POS ROD & NOSE GEAR CABLE BRACKET PER MM 32-51-000-5. REM OVED AND REPLACED APEX PIN & MISSING BUSHING PER 32-51-000. 2 L 7 3 4F RT A3WE 2002031400050 20020314 00050 CE 2002 3 14 TIM2002F00007 1 20020131 A 3010 130936P8D0800 HOSE BEECH 99 C99 1154006 CE PWA PT6 PT6A36 52043 NE HORIZONTAL STAB CHAFED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 239AL 17612 U239 DURING THE INSPECTION OF THE SURFACE DEICE BOOT ON THE HORIZONTAL STABILIZER, IT WAS DETERMINED THE SUPPLY LINE WAS NOT PROVIDING ADEQUATE PRESSURE TO PROPERLY INFLATE THE DEICER. FURTHER INSPECTION REVEALED THE SYSTEM PRESSURE ADJUSTED. THE LINE HAD CHAFED DUE TO LACK OF PROPER SUPPORT FROM CLAMPS AND COULD HAVE BENEFITED FROM CHAFE SLEEVING OR THE LIKE. 1 L 7 2 3T 4 T A14CE E4EA 2002031400051 20020314 00051 NE 2002 3 14 TIM2002F00008 2 20020131 A 7510 5038017027 CHECK VALVE BEECH 99 C99 1154006 CE PWA PT6 PT6A36 52043 NE BLEED AIR SYS CORRODED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 239AL 17612 U239 DURING AN INSPECTION OF THE BLEED AIR SYSTEM, THE CHECK VALVES WERE FOUND TO BE INOPERATIVE DUE TO PARTS MISSING MOST LI KELY DUE TO AGE. THE CHECK VALVES WERE REPLACED WITH SERVICEABLE CHECK VALVES. IT MAY BE NECESSARY TO COMPLETELY DISAS SEMBLE BLEED AIR SYSTEM CHECK VALVES DURING DETAILED INSPECTIONS TO PREVENT ANY FURTHER MALFUNCTIONS. 1 L 7 2 3T 4 T A14CE E4EA 2002031400052 20020314 00052 SW 2002 3 14 TVM2002F00000 1 20020201 A 5711 SPAR BBAVIA 7 7ECA 21101NN SW LYC O235 O235* 41505 EA RT WING CRACKED B TVMR K NONE O OTHER IN INSP/MAINT 1 EA 05 6309N 3214 233 WHILE COMPLYING WITH AD, A LONGITUDINAL CRACK IN THE RIGHT FORWARD WOODEN WING SPAR APPROXIMATELY 30 INCHES LONG. 1 H 7 1 3O 3 O A759 E223 2002031400053 20020314 00053 GL 2002 3 14 TYW2002F00000 3 20020207 A 6111 R101525 BLADE WTHRLY 620 620B 9630605 CE PWA R985 R985AN1 52008 NE HARTZL HCB3R HCB3R304 GL PROPELLER FAILED A TYWG O OTHER D INFLIGHT SEPARATION AG AGRICULTURE 1 SW 13 90275 1015 1637 13769 EMA1094 11 INCHES SEPRATED FROM ONE PROPELLER BLADE DURING FLIGHT. AIRCRAFT WAS SPRAYING A CROP AND WAS IN A TURN WHEN BLADE TI P SEPARATED. 1 L 7 1 3R 3 R NC A26WE 5E1 5 C P28EA 2002031400054 20020314 00054 SO 2002 3 14 UC22002F00000 1 20020212 A 2700 62701113 CONTROL CABLE PIPER PA28 PA28181 7102807 SO LYC O360 O360A1D 41514 EA FWD STABILATOR FRAYED A UC2R K NONE O OTHER IN INSP/MAINT 1 GL 19 4145A 2453 2843150 FOUND RIGHT AND LEFT FORWARD STABILATOR CONTROL CABLES FRAYED AND WORN DURING A 100 HOUR INSPECTION. 1 L 7 1 3O 3 O 2A13 E286 2002031400055 20020314 00055 SO 2002 3 14 UC22002F00001 1 20020212 A 2700 62701114 CONTROL CABLE PIPER PA28 PA28181 7102807 SO LYC O360 O360A1D 41514 EA FWD STABILATOR WORN A UC2R K NONE O OTHER IN INSP/MAINT 1 GL 19 4145A 2453 2843150 FOUND RIGHT AND LEFT FORWARD STABILATOR CONTROL CABLES FRAYED AND WORN DURING A 100 HOUR INSPECTION. . 1 L 7 1 3O 3 O 2A13 E286 2002031400056 20020314 00056 SO 2002 3 14 UC22002F00002 1 20020212 A 2700 62701113 CONTROL CABLE PIPER PA28 PA28181 7102807 SO FWD STABILATR FRAYED A UC2R K NONE O OTHER IN INSP/MAINT 1 GL 19 4149C 2342 2843190 FOUND THE RIGHT AND LEFT FORWARD STABILATOR CONTROL CABLES FRAYED AND WORN DURING A 100 HOUR INSPECTION. 1 L 7 1 3O 2A13 2002031400057 20020314 00057 SO 2002 3 14 UC22002F00003 1 20020212 A 2700 62701114 CONTROL CABLE PIPER PA28 PA28181 7102807 SO FWD STABILATOR FRAYED A UC2R K NONE O OTHER IN INSP/MAINT 1 GL 19 4149C 2342 2843190 FOUND THE RIGHT AND LEFT FORWARD STABILATOR CONTROL CABLES FRAYED AND WORN DURING A 100 HOUR INSPECTION. 1 L 7 1 3O 2A13 2002031400058 20020314 00058 GL 2002 3 14 UF22002F00000 3 20020213 A 6114 HUB CESSNA 414 414 2075908 CE CONT O520 TSIO520* 17040 SO HARTZL HCC3Y PHCC3YF2 GL PROPELLER CRACKED B UF2R K NONE O OTHER IN INSP/MAINT 1 GL 15 4231C 5160 240 4140531 EB3209 CRACK IN PROPELLER HUB WAS FOUND DURING AN INSPECTION TO FIND A REASON FOR A GREASE LEAK COMING OUT OF THE PROP SPINNER. THE REAR HUB HALF WAS FOUND TO BE BROKEN IN TWO AROUND ONE BLADE SOCKET. ANY FURTHER OPERATION WOULD HAVE CAUSED A CO MPLETE BLADE SEPARATION. HUB WAS SENT TO MFG. FOR FURTHER EVALUATION. 1 L 7 2 3O 3 O RT A7CE E8CE 5 C P25EA 2002031400059 20020314 00059 SO 2002 3 14 UQM2002F00000 1 20020123 A 2140 37D77 HEATER PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA CABIN INOPERATIVE A UQMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 01 900TS 277405429 L10617 REMOVED HEATER FROM AIRCRAFT, 12 VOLT STYTEM AND FOUND (PN 45D70-1A) 24 VOLT. NO ENTRY IN THE AIRCRAFT LOG BOOK OF HEAT ER REPLACED. AFTER TALKING TO OVERHAUL SHOP, THEY ARE THE SAME HEATER EXCEPT ONE IS A 12 VOLT AND THE OTHER 24 VOLT ON THE COMPONENTS. HEATER WAS REPLACED WITH CORRECT UNIT FOR SERIAL NUMBER OF AIRCRAFT. PROBABLE CAUSE: FIELD OVERHAUL A ND TRYING TO MAKE A GOOD HEATER OUT OF SEVERAL JUNK HEATERS. 1 L 7 2 3O 3 O 1A10 1E4 2002031400060 20020314 00060 CE 2002 3 14 VJ32002F00005 1 20020129 A 3297 SM50D7 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MLG FAILED G VJ3R O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 8242T 202 CE1610 LANDING GEAR WOULD NOT COME DOWN, A SMALL TAP TO THE TOP OF THE RELAY, THE GEAR CYCLED DOWN NORMAL. RELAY WAS REMOVED A ND A NEW RELAY WAS INSTALLED. LANDING GEAR OPERATIONAL CHECKED NORMAL. RELAY SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002031400061 20020314 00061 CE 2002 3 14 VJ32002F00006 1 20020129 A 3230 9469 MOTOR BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MLG INOPERATIVE G VJ3R O OTHER O OTHER NR NOT REPORTED 1 WP 07 8242T 172 CE1610 820446R MOTOR SLOW TO RETRACT AND EXTEND GEAR. MOTOR VERY NOISEY. MOTOR SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002031400062 20020314 00062 CE 2002 3 14 VJ32002F00007 1 20020129 A 3297 SM50D7 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MLG INOPERATIVE G VJ3R O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 8252T 172 CE1545 820446R LANDING GEAR WAS SLOW TO COME UP AND TO EXTEND. REMOVE DYNAMIC RELAY AND INSTALLED NEW RELAY. CYCLED LANDING GEAR, OPE RATIONAL CHECKED NORMAL. RELAY SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002031400063 20020314 00063 CE 2002 3 14 VJ32002F00008 1 20020129 A 3297 SM50D7 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MLG INOPERATIVE G VJ3R O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 8240T 335 CE1542 825758R LANDING GEAR SELECTED SWITCH WAS PLACED IN THE DOWN POSITION, THE GEAR FAILED TO COME DOWN IN FLIGHT. A GEAR UP LANDING WAS MADE. INSPECTION OF THE LANDING GEAR SYSTEM AFTER THE ACCIDENT CHECKED NORMAL. INSPECTION OF THE DYNAMIC RELAY SH OWED ARCING ON THE CONTACTS. 1 L 7 1 3O 3 O 3A15 E5CE 2002031400064 20020314 00064 CE 2002 3 14 VJ32002F00009 1 20020212 A 3243 9638003425 MASTER CYLINDER BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO BRAKES MALFUNCTIONED A VJ3R O OTHER O OTHER NR NOT REPORTED 1 WP 07 8251C 40 CE1543 820396R POPPET VALVE IS STICKING AND THE BRAKE FAILED TO WORK. WHEN THIS HAPPENS THE PILOT MAY LOOSE CONTROL OF THE AIRCRAFT ON LANDING AND ROLL OUT. 1 L 7 1 3O 3 O 3A15 E5CE 2002031400065 20020314 00065 CE 2002 3 14 VJ32002F00010 1 20020227 A 3297 SM50D7 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MLG INOPERATIVE B VJ3R O OTHER O OTHER NR NOT REPORTED 1 WP 07 5609S 150 CE1454 825756R LANDING GEAR WOULD NOT COME DOWN, A SMALL TAP TO THE TOP OF THE RELAY THE GEAR CYCLED DOWN NORMAL. RELAY WAS REMOVED AN D A NEW RELAY WAS INSTALLED. LANDING GEAR OPERATIONAL CHECKED NORMAL. RELAY SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002031400066 20020314 00066 EA 2002 3 14 VJ32002F00011 2 20020227 A 7322 MA4SPA105217 CARBURETOR PIPER PA28 PA28181 7102807 SO LYC O360 O360A4M 41514 EA ENGINE LEAKING B VJ3R O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 07 4130W 2843204 RL3704036A FUEL LEAKING FROM BODY OF CARBURETOR WHEN ENGINE IS SHUT DOWN, MIXTURE VERY RICH. TOTAL TIME ON UNIT IS (0). CARBURETOR REMOVED FOR WARRANTY. OVERHAULED CARBURETOR INSTALLED, GROUND OPERATION CHECKED NORMAL. 1 L 7 1 3O 3 O 2A13 E286 2002031400067 20020314 00067 CE 2002 3 14 VJ32002F00012 1 20020227 A 3610 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO AIR SYSTEM INOPERATIVE B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 8242T 464 820462R LOW OUTPUT FROM PUMP TO AIRCRAFT, REMOVED PUMP AND INSTALLED NEW PUMP OPERATION WAS NORMAL. PUMP SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002031400068 20020314 00068 CE 2002 3 14 VJ32002F00013 1 20020227 A 2730 33524029 CONTROL CABLE BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO ELEVATOR FRAYED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 8251C 1805 CE1543 820396R ELEVATOR CABLE FRAYED. 1 L 7 1 3O 3 O 3A15 E5CE 2002031400069 20020314 00069 SO 2002 3 14 VOX2002F00000 1 20020104 A 8120 MKR0106 CONTROLLER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA WASTEGATE FAILED A VOXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 35164 1054 317952090 RL489461A AIRCRAFT ON CLIMB-OUT, PART FAILED, TURBO AND WASTEGATE SYSTEM LOST OIL PRESSURE, ENGINE LOST BOOST AND SUBSEQUENT POWER . ENGINE SHUT DOWN IN-FLIGHT, PRECAUTIONARY. 1 L 7 2 3O 3 O A20SO E14EA 2002031400070 20020314 00070 CE 2002 3 14 VXW2002F00000 1 20020206 A 3232 B543DD BEARING BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA MLG ACTUATOR FAILED E VXWA K NONE O OTHER IN INSP/MAINT 1 EA 21 12CF BB534 POST FLIGHT INSPECTION FOUND BOTH PIVOT BEARINGS ON LEFT MAIN LANDING GEAR ACTUATOR SHATTERED. UPON REMOVAL, BOTH BEARI NG OUTER RACES HAD BEEN BROKEN IN HALF AND BALLS FALLING DOWN TO WING SPAR. MISC PIECES ALSO LAYING ON SPAR, CONSIDERIN G THE FORCE REQUIRED TO SHATTER A BEARING RACE, THE ACTUATOR LEFT MAIN LANDING GEAR WAS REPLACED. ACTUATOR SHOWS NO EXT ERNAL SIGN OF DAMAGE EXCEPT THAT DOWN LOAD SPRING IS LOOSE FROM POSSIBLE OVER COMPRESSION. NO GEAR OR SHAFT BINDING, BU T REPLACED FOR SAFETY. 1 L 7 2 4T 4 T A24CE E4EA 2002031400071 20020314 00071 SO 2002 3 14 WVBA2002002 1 20020129 A 3211 CHANNEL PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA MLG WW CRACKED A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 59829 20347 317652081 DURING INSPECTION OF THE HYDRAULIC POWER PAK IT WAS DISCOVERED THAT THE CHANNEL THAT REINFORCERS THE NOSE WHEEL TUNNEL WHERE THE NOSE GEAR ACTUATOR ATTACHES HAD CRACKED ON THE FORWARD CUTOUT FOR THE HYDRAULIC POWER RELIEF VALVE THE CHANNEL WAS REMOVED AND INSPECTED WHERE IT WAS DISCOVERED THAT THE OUTBOARD BOLT HOLE FOR THE NOSE GEAR ACTUATOR BRACKET WAS E LONGATED AND CRACKED ON THE BOTTOM SIDE. THE PART WAS REMOVED AND REPLACED IT IS RECOMMENDED THAT THE NOSE GEAR ACTUATO R ATTACH BRACKET BOLTS BE CHECKED PERIODICLY FOR SECURITY DURING LANDING GEAR INSPECTIONS AS IT IS SUSPECTED THAT THE LO OSE BOLT CAUSED THE PART TO STRESS AND CRACK DURING GEAR OPERATIONS. 1 L 7 2 3O 3 O A20SO E14EA 2002031400072 20020314 00072 SO 2002 3 14 WVBA2002003 1 20020214 A 5343 409872 CHANNEL PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA MLG WW CRACKED A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 300ED 17414 317852008 DURING INSPECTION THIS AREA WAS LOOKED AT AFTER FINDING OTHER AIRCRAFT WITH THIS CHANNEL CRACKED THE PART WAS REMOVED AN D REPLACED. IT MAY BE THAT THE CUT OUT NOT BEING. DRESSED TO BELIEVE THE STRESS CAUSED THE PART TO FAIL AS EXTRA STRESS . IS INDUCED FROM THE NOSE GEAR ACTUATOR ATTACH BRACKETS 2 REAR BOLTS COMING THROUGH THE CHANNEL. THIS ALSO SEEMS TO B E FOUND ON AIRFRAMES OVER 35,000 HOURS. 1 L 7 2 3O 3 O A20SO E14EA 2002031400173 20020314 00173 NM 2002 3 14 200200181 1 20020313 A 5720 65B2285816 SUPPORT BOEING 747 747273C 1384896 NM LT WING BROKEN B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 471EV 84224 20651 LEFT WING LEADING EDGE LOWER FIXED FAIRING SUPPORT ROD WAS FOUND BROKE (SEPARATED). REPLACED SUPPORT ROD PER 747 MM 20- 51-01. 2 L 7 4 4F A20WE 2002031400073 20020314 00073 SO 2002 3 14 WVBA2002005 1 20020304 A 2820 VALVE PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA FUEL PRESSURE LEAKING E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 3527U 227 317952141 DURING SOME LINE MAINTENANCE, THE TECHNICIAN NOTICED FUEL STAIN FROM THE HEATER DRAIN. THE SOURCE WAS FOUND TO BE THE F UEL PRESSURE REGULATOR WHICH WAS LEAKING FROM THE LOWER PARTING SURFACE. THE UNIT WAS REMOVED AND REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 2002031400074 20020314 00074 SO 2002 3 14 ZKG2002F00000 1 20020121 A 5330 622375007 SKIN PIPER PA28 PA28180 7102808 SO LYC O360 O360A3A 41514 EA FUSELAGE CORRODED E ZKGA K NONE O OTHER IN INSP/MAINT 1 NE 05 7991W 282048 L761536A WHILE REPLACING WINDSHIELDS FOUND UNDER COVERING ON TOP OF INSTRUMENT PANEL. CORRISON ON SKIN FOR TOP OF INSTRUMENT PAN EL, LEFT SIDE. CORROSION WAS IN THE AREA OF THE GLUE. 1 L 7 1 3O 3 O 2A13 E286 2002031400174 20020314 00174 NM 2002 3 14 200200182 1 20020313 A 7810 NOZZLE BOEING 747 747273C 1384896 NM PWA JT9 JT9D7J 52054 NE NR 4 ENGINE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 471EV 20651 NR 4 ENGINE EXHAUST NOZZLE AT THE 2:00 POSITION, 4 INCHES FROM THE TRAILING EDGE HAS A 10 INCH CRACK IN THE OUTER SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER PER 747 SRM 54-30-03. 2 L 7 4 4F 4 F A20WE E20EA 2002031400175 20020314 00175 NM 2002 3 14 200200183 1 20020313 A 2550 65B621721 FITTING BOEING 747 747273C 1384896 NM CARGO BAY BROKEN B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 471EV 20651 FLOOR TRACK FITTING THAT HOLDS CARGO LOADING TRAY IN PLACE AT POSITION P2, WAS BROKEN AND WOULD NOT LOCK THE CARGO LOADI NG TRAY IN POSITION. INSTALLED NEW FLOOR TRACK FITTING PER 747 SOPM 20-50-01. 2 L 7 4 4F A20WE 2002031400075 20020314 00075 NM 2002 3 14 2002F00233 1 20020102 A 2782 SPRING BOEING 757 757236 1384971 NM SLAT ACTUATOR FAILED A PZ8M A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 07 521NA 25592 LE SLAT DISAGREE EICAS MESSAGE BETWEEN FLAPS 1 AND 0 ON RETRACTION. AIRCRAFT RETURNED TO DEPARTURE STATION. SLATS FOUN D TO BE BINDING, LUBED AND OPERATIONAL CHECK PER AMM. ON NEXT DEPARTURE DISCREPANCY REPEATED. AIRCRAFT RETURNED TO DEP ARTURE STATION. FURTHER INVESTIGATION REVEALED NR 1 AND NR 4 SLAT INBOARD ROTARY ACTUATOR SPRING POPPED, FSEU 1 FAULT C ODE 223 AND 310, FSEU 2 SLAT SYSTEM FAULT, FSEU 3 FAULT CODE 226. SLATS RELUBED, ADJUSTED RIGHT SLAT POSITION TRANSMITT ER, CLEARED FSEU FAULTS, OPERATIONAL CHECK OF SLAT SYSTEM AND PERFORMED BITE CHECKS OF FSEU'S. ACCOMPLISHED TEST FLIGHT , SYSTEMS FUNCTIONING PROPERLY. (M) 2 L 7 2 4F RT A2NM 2002031400076 20020314 00076 SO 2002 3 14 C2XA02BT010 1 20020313 A 3350 GE1317 BULB EMB 145 EMB145LR 3260212 SO CABIN FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14923 145318 BTV---DURING ROUTINE INSPECTION ON RON IN BTV, MAINTENANCE FOUND AFT UPPER AISLE EMERGENCY LIGHT TO BE INOPERATIVE....RE MOVED AND REPLACED LIGHT BULB IAW EMB145 MM 33-50-08. OPS.CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2002031400077 20020314 00077 WP 2002 3 14 ABXA010761 1 20020219 A 2730 3645797 SPRING DOUG DC8 DC863F 302198F WP ELEVATOR DEFECTIVE A ABXA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 23 816AX 465 46093 DURING TAXI, ELEVATOR FELT LIKE IT WAS BINDING AND COULD NOT GET A GOOD TEST. DID BLOCK TURNBACK. REPLACED THE ELEVATO R LOAD SPRING ASSEMBLY IAW DC-8 MM 27-30-04. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2002031400078 20020314 00078 WP 2002 3 14 AT0200019 1 20020122 A 5753 STUD DOUG DC9 DC932 3022066 WP T/E FLAP CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 831AT 47674 RIGHT WING FLAP HINGE LOWER OUTBOUND ATTACHMENT STUD AT X IN=33.148 SHOWS A CRACK INDICATION. 2 L 7 2 4F A6WE 2002031400079 20020314 00079 NM 2002 3 14 2002F00234 1 20020205 A 2530 CHILLER BOEING 757 757256 NM GALLEY SMOKE A N8TA H F A DEACTIVATE SYST/CIRCUITS ACTIVATE FIRE EXT. UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 19 508NA 26244 SMOKE IN CABIN FROM AFT GALLEY REFRIGERATOR. FLIGHT ATTENDANT PULLED ALL CIRCUIT BREAKERS FOR AFT GALLEY. SMOKE CONTRO LLED AND DISSIPATED. AN UNEVENTFUL, UNSCHEDULED LANDING ACCOMPLISHED. INVESTIGATION CONFIRMED CAUSE OF SMOKE TO BE CHI LLER IN AFT GALLEY (G4B). DEACTIVATED CHILLER BY PULLING AND COLLARING CHILLER CIRCUIT BREAKERS. (M) 2 L 7 2 4F RT A2NM 2002031400080 20020314 00080 2002 3 14 AT0200029 4 20020228 A 2565 SLIDE DOUG DC9 DC932 3022066 WP L1 DOOR OUT OF POSITION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 847AT 47555 FORWARD L1 DOOR CHUTE FELL OUT OF CONTAINER. REINSTALLED SLIDE REF 25-62. 2 L 7 2 4F A6WE 2002031400081 20020314 00081 NM 2002 3 14 2002F00235 1 20020105 A 2170 CONTROL VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AC PACK STUCK A UHLA E D ENGINE SHUTDOWN RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NE 03 816EX 329 SMOKE IN CABIN, STARTED NR 2 ENGINE AFTER START OF NR 1 ENGINE SMOKE IN CABIN AND COCKPIT UPON INSPECTION DISCOVERED DUC T TEMP 60 DEGREES CELSIUS AND OIL IN BLEED SYSTEM CAUSED BY SUSPECTED STUCK PACK TEMP CONTROL VALVE (FULL-HOT) DISCONNEC TED VALVE LINKAGE CYCLED VALVE. RECONNECTED LINKAGE OPS CHECKED GOOD FERRIED FLIGHT TO MDT MMB THERE THEY. REMOVED AND REPLACED CONTROL VALVE AND REPLACED NR 2 ENGINE.(M) 2 H 7 2 4T 4 T RT A13NM E20NE 2002031400082 20020314 00082 NM 2002 3 14 2002F00236 1 20020114 A 2721 682015 SWITCH DHAV DHC8 DHC8102 2809003 NM RUDDER TRIM INOPERATIVE A UHLA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NE 03 816EX 329 THE RUDDER TRIM IS INTERMITTENT MOVING NOSE RIGHT. PILOT WENT TO QRH. RETURNED TO TLN MAINTENANCE FOUND RUDDER TRIM SW ITCH TO BE MALFUNCTIONING. REMOVED AND REPLACED RUDDER TRIM SWITCH. PERFORMED TEST FLIGHT OPS CHECK GOOD. RESUMED FLI GHT SCHEDULED. (M) 2 H 7 2 4T RT A13NM 2002031400083 20020314 00083 WP 2002 3 14 AT0200032 1 20020202 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 FUSELAGE SKIN IS CRACKED AT THE FORWARD PASSENGER DOOR CUTOUT AT THE NR 1 AFT DOOR STOP. 2 L 7 2 4F A6WE 2002031400084 20020314 00084 EU 2002 3 14 2002F00237 1 20020120 A 3230 ATG130907 SWITCH SAAB SF340 SF340A 7850100 EU MLG CONTAMINATED A UHLA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 NE 03 158CQ 158 ON DEPARTURE FROM FROM TTN CREW NEEDED TO ABORT TAKEOFF DUE TO CONFIGURATION WARNING LIGHT. MOCC HAD CREW RESET SETTING S CYCLE FLAPS AND TRIMS STILL GOT WARNING MOCC HAD AIRCRAFT RETURN TO GATE MAINTENANCE CLEANED WOW SWITCHES AND CONNECTO R PLUGS. PERFORMED CONFIGURATION TEST, OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A52EU 2002031400085 20020314 00085 WP 2002 3 14 AT0200033 1 20020126 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 COMPLIED WITH AD PER SERVICE BULLETIN , X-RAY, AND CRACKS NOTED ON FILMS, AFT PRESSURE BULKHEAD 2 EA CRACKS UPPER RIGHT SIDE. 2 L 7 2 4F A6WE 2002031400086 20020314 00086 NM 2002 3 14 2002F00238 1 20020123 A 2913 PUMP DHAV DHC8 DHC8* NM HYD SYSTEM MALFUNCTIONED A UHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 03 810EX 308 NR 1 ENGINE HYDRAULIC PUMP FAILED SHORTLY AFTER TAKEOFF. STANDBY CAME ON. NR 1 SYSTEM WARNING LIGHTS CAME ON UNTIL STA NDBY BROUGHT UP PSI. NR 1 SYSTEM WAS OFF LINE APPROX 10 MINUTES THEN CAME BACK ON. AIRCRAFT RETURNED TO BED. NON EMER GENCY TO HAVE MECH CHECK IT OUT. AIRCRAFT WAS SERVICE BEFORE FLIGHT. MECH BLEED AND SERVICED NR 1 SYSTEM OPS CHECKED G OOD DISCREPANCY WAS SIGNED OF AND A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2002031400087 20020314 00087 EU 2002 3 14 2002F00239 1 20020224 A 5350 GASKET AIRBUS 320 A320233 3930329 EU FAIRING MISSING A U18F O OTHER O OTHER CL CLIMB 1 SO 23 463TA 1339 FLT TPU020 - UOI/GYE - DURING CLIMB, CABIN PERSONNEL DETECTED A NOISE AT THE PAX CABIN, NEAR THE EMERGNCY OVERWING EXIT DOORS. THE AIRCRAFT CONTINUE ITS FLIGHT TO GYE STATION. AFTER LANDING AT GYE STATION, TECHNICIANS PERFORMED INSPECTION OF THE AIRCRAFT, AND FOUND MISSING MATERIAL (ABOUT 25 INCHES OF MATERIAL LOST) ON A WING TO BODY FAIRING ON THE LEFT SI DE OF THE FUSELAGE. THE PANEL 151DT WAS REPLACED IAW AMM 53-35-11-400-001. THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2002031400088 20020314 00088 NM 2002 3 14 P5CA0200662 1 20020308 A 7810 TAILPIPE BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 689167 FOUND NR 1 ENGINE TAIL PIPE INNER SLEEVE, CRACK APPROX 1 INCH LONG AT 6 O'CLOCK POSITION AND APPROX 18 INCHES FROM FWD C ONE L/E. CRACK IS 6.5 INCH LONG FOUND ON OUTER SKIN OF EXHAUST CONE INNER BARREL. 2 L 7 4 4F 4 F A20WE E3NE 2002031400089 20020314 00089 NM 2002 3 14 2002F00240 1 20020212 A 2913 3508807 PUMP BOEING 757 757236 1384971 NM HYD SYSTEM FAILED A N8TA O OTHER J WARNING INDICATION CR CRUISE 1 WP 19 546NA 29945 DURING CRUISE, LT ENGINE HYD OVERHEAT EICAS MESSAGE CAME ON FOLLOWED BY LT HYD SYSTEM AND LOSS OF LT HYDRAULIC SYSTEM PR ESSURE. INVESTIGATION REVEALED LEFT ENGINE DRIVEN PUMP (EPD) FAILED. REPLACED PUMP. CASE DRAIN AND PRESSURE FILTERS F OR BOTH EDP AND ACMP. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2002031400090 20020314 00090 EU 2002 3 14 QXEA0200286 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 464.329 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031400091 20020314 00091 EU 2002 3 14 QXEA0200287 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 464.324 TOP LUGS HAVE GOUGES. 2 L 7 2 4F RT A20EU 2002031400092 20020314 00092 NM 2002 3 14 QXEA0200472 1 20020313 A 5270 HANDLE BOMBDR DHC8 DHC8401 NM DIRTY A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 405QX 4047 SEA - AICRAFT RETURNED TO FIELD WHEN FUSELAGE DOOR WARNING WAS RECIEVED FOR THE AFT BAGGAGE DOOR. MAINTENANCE INSPECTED AND FOUND THE DOOR HANDLE NOT STOWED. MAINTENANCE CLEANED AND LUBED THE MECHANISM, STOWED THE HANDLE AND PERFORMED OPERA TIONAL CHECK. OPERATIONAL CHECK IS GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031400093 20020314 00093 NM 2002 3 14 2002F00241 1 20020223 A 7500 51444138 DUCT BOEING 757 7572T7 1384914 NM LT ENGINE LEAKING A N8TA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 513NA 23895 DURING CLIMB, PASSING THROUGH 8,000 FT MSL, LT ENGINE OVERHEAT EICAS' MESSAFE CAME ON. SECURED BLEED VALVE, RETARDED TH RUST. MESSAGE EXTINGUISHED. INVESTIGATION REVEALED HP6 DUCT LEAKING. REPLACED HP6 DUCT, LEAK CHECKED GOOD. (M) 2 L 7 2 4F RT A2NM 2002031400094 20020314 00094 NM 2002 3 14 2002F00242 1 20020210 A 5320 146N5246U6 FLOOR SUPPORT BOEING 757 757236 1384971 NM FUSELAGE CORRODED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 506NA 24771 FOUND CORROSION ON FLOOR SUPPORT BS 1675, RBL 56, WL 208. CLEANED UP CORROSION, FOUND TO BE BEYOND ACCEPTABLE LIMITS PE R SRM 53-00-01. REMOVED AND REPLACED SUPPORT. (M) 2 L 7 2 4F RT A2NM 2002031400095 20020314 00095 NM 2002 3 14 2002F00243 1 20020209 A 3350 86210089 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 373PA 23749 EMERGENCY FLOOR PATH LIGHTING AT ROW 6 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW ALERT NR 7 11-4-01, TESTED OK . (M) 2 L 7 2 4F RT A16WE 2002031400096 20020314 00096 EU 2002 3 14 QXEA0200288 1 20020208 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT OUTBOARD SEAT TRACK AT STATION 443.024 LUGS ARE GOUGED. 2 L 7 2 4F RT A20EU 2002031400097 20020314 00097 EU 2002 3 14 QXEA0200289 1 20020201 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - THE FUSELAGE SKIN FOR THE AFT RADIO ALTIMETER ANTENNA MATTING SURFACE HAS CORROSION. REPAIRED IAW FOKKER SRM 51-1 0-4, PARAGRAPHA 4A. 2 L 7 2 4F RT A20EU 2002031400098 20020314 00098 EU 2002 3 14 QXEA0200290 1 20020201 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - THE FUSELAGE SKIN FOR THE FORWARD RADIO ALTIMETER ANTENNA MATTING SURFACE HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH A AND B. 2 L 7 2 4F RT A20EU 2002031400099 20020314 00099 EU 2002 3 14 QXEA0200291 1 20020201 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - THE SKIN UNDER MARKER BEACON ANTENNA MATTING SURFACE HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 PARAG RAPH 4A (1) AND 4B (1) (2). 2 L 7 2 4F RT A20EU 2002031400100 20020314 00100 EU 2002 3 14 QXEA0200304 1 20020214 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - SCRATCH ON BACK SIDE OF FRAME 16.2 TO LEFT SIDE OF CENTER LINE, NEAR TOP OF FRAME WEB. REPAIRED IAW FOKKER SRM 53 -01-01 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002031400101 20020314 00101 EU 2002 3 14 QXEA0200305 1 20020212 A 5320 BEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - HORIZONTAL BOX BEAM BETWEEN VERTICAL BEAMS BL425L AND BL425R, DENTED IN TOP SIDE, RT END ABOVE APU, FORWARD OF BLE ED AIR DUCT. REPAIRED IAW HORIZON AIR EA 4-53-1562. 2 L 7 2 4F RT A20EU 2002031400102 20020314 00102 EU 2002 3 14 QXEA0200306 1 20020214 A 5320 STIFFENER FOKKER F28 F28MK4000 4990810 EU FUSELAGE DEBONDED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - BONDED STIFFENER ON AFT SIDE OF REAR PRESSURE BULKHEAD, BETWEEN BEAM V AND VI, OUTBOARD OF BL425L IS DISBONDED FRO M BULKHEAD WEB. REPAIRED IAW HORIZON AIR EA 4-53-1559. 2 L 7 2 4F RT A20EU 2002031400103 20020314 00103 EU 2002 3 14 QXEA0200307 1 20020213 A 5542 FLANGE FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - THE FORWARD AND AFT FLANGES ON THE APERTURE FOR PANEL 57Y ON THE RUDDER ARE CRACKED OUT. REPAIRED IAW SRM 51-31-0 1. 2 L 7 2 4F RT A20EU 2002031400104 20020314 00104 EU 2002 3 14 QXEA0200308 1 20020217 A 5720 ATTACH FITTING FOKKER F28 F28MK4000 4990810 EU LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT WING FAIRING ATTACH STRUCTURE IS CRACKED ALONG THE FORWARD CIRCUMFERENCE OF PANEL 91J. 2 L 7 2 4F RT A20EU 2002031400105 20020314 00105 EU 2002 3 14 QXEA0200309 1 20020214 A 5553 ATTACH ANGLE FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - VISUAL CRACK INDICATION ON RT VERTICAL STAB TO FUSELAGE CONNECTION ANGLE AT INTERMEDIATE SPAR I AFT HI-LOK FORWARD SIDE. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1. 2 L 7 2 4F RT A20EU 2002031400106 20020314 00106 EU 2002 3 14 QXEA0200310 1 20020213 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK FROM FRAME 6305 FORWARD ALONG INSIDE CHANNEL HAS CORROSION. REPAIRED IAW FOKKER SRM 53-40-0 1. 2 L 7 2 4F RT A20EU 2002031400107 20020314 00107 EU 2002 3 14 QXEA0200311 1 20020214 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK FROM FRAME 12405 TO FRAME 9305B ON ATTACH POINTS, LUGS HAVE GOUGES. REPAIRED IAW FOKKER SR M. 2 L 7 2 4F RT A20EU 2002031400108 20020314 00108 EU 2002 3 14 QXEA0200312 1 20020213 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - GOUGE IN AFT CARGO DOOR APERTURE OF FORWARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-02, PAGES 8 AND 9. 2 L 7 2 4F RT A20EU 2002031400109 20020314 00109 EU 2002 3 14 QXEA0200313 1 20020214 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK AT FRAME 12875 FORWARD LUGS HAVE CORROSION. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002031400110 20020314 00110 EU 2002 3 14 QXEA0200314 1 20020214 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK FROM FRAME 12875 AFT ABOUT 8 INCHES, INSIDE TUNNEL THERE IS PITTING AND CORROSION. REPAIRE D IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002031400111 20020314 00111 NM 2002 3 14 QXEA0200473 1 20020312 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 350PH 6645 488 YVR-EMERGENCY LIGHTS WILL NOT EXTINGUSH. AIRCRAFT FERRIED TO PDX. PDX MAINTENANCE REMOVED AND REPLACED ESCAPE PATH POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031400112 20020314 00112 2002 3 14 2002F00245 4 20020128 A 2200 R10534182 LIMITER BOEING 737 7373Y0 1384671 NM AFCS DEFECTIVE A PIDA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 05 373PA 23749 ATL - AUTO PILOT WILL NOT ENGAGE. REMOVED AND REPLACED AILERON FORCE LIMITER AND OPERATION CHECKED NORMAL PER MM 22-11- 13. (M) 2 L 7 2 4F RT A16WE 2002031400113 20020314 00113 EU 2002 3 14 QXEA0200315 1 20020214 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - DENT .020 INCH DEEP BY 2 INCHES IN LENGTH, 14.5 INCHES AFT OF LEFT HAND FRAME 3050 AND 11 INCHES BELOW WINDOW FRAM E BASE. REPAIRED IAW FOKKER SRM 53-02-05, FIGURE 1, SRM 51-10-4 AND SRM 53-02-02. 2 L 7 2 4F RT A20EU 2002031400114 20020314 00114 NM 2002 3 14 2002UALA00341 1 20020302 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 FUSELAGE FRAME AT STATION 1420 JUST ABOVE STRINGER 26L DAMAGED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.DOUBL ER INSTALLED ON FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000018 20020320 00018 NM 2002 3 20 2002UALA00354 1 20020305 A 3246 BEA7300029685 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG FAILED A UALA O OTHER A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 537UA 25157 RIGHT NOSE WHEEL BEARING FAILED ON TAXI. SMOKE AND SMALL FLAME FROM WHEEL. RT NLG OUTBOARD BEARING FAILED. REPLACED N LG AXLE AND BOTH NLG WHEELS. PERFORMED NWS TEST. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031400115 20020314 00115 NM 2002 3 14 2002UALA00375 1 20020307 A 5315 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 CABIN FLOOR CREASE BEAM WEB UPPER SURFACE CORRODED AT OUTBOARD EDGE AROUND ATTACH FASTENERS AT THREE PLACES BETWEEN BODY STATION 960 AND BODY STATION 984, RBL 68.50 AND WL208. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000073 20020320 00073 NM 2002 3 20 2002UALA00390 1 20020308 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 CABIN DOOR 2 LEFT LOWER CREASE BEAM CORRODED, STATION 663-754 WATERLINE 208, STRINGER 17 LEFT. MAJOR REPAIR ACCOMPLISHE D. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000074 20020320 00074 NM 2002 3 20 2002UALA00391 1 20020308 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 STATION 602-604 STRINGER 16L DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031400116 20020314 00116 2002 3 14 2002F00246 4 20020127 A 2297 WIRE BOEING 737 737228 13844AG NM AFCS BROKEN A PIDA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 05 251TR 23792 DAL - AUTO PILOT B-CHANNEL ABRUPTLY PUSHES NOSE DOWN WHEN ENGAGED. REPAIRED BROKEN WIRE AT STATION 1080 DISCONNECT BRAC KET IAW WPM 20-10-13. OPERATION CHECKED NORMAL IAW MM 22-11-01. (M) 2 L 7 2 4F RT A16WE 2002031400117 20020314 00117 2002 3 14 2002F00247 4 20020127 A 2200 65528179 ACCESSORY UNIT BOEING 737 7373Y0 1384671 NM AFCS DEFECTIVE A PIDA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 05 373PA 23749 ATL - UNABLE TO ENGAGE EITHER A/B AUTO PILOT SYSTEM IN ANY MODE. REMOVED AND REPLACED AUTO PILOT ACCESSORY UNIT. PERFO RMED AFDS TEST BY CDU PER MM 22-11-01. (M) 2 L 7 2 4F RT A16WE 2002031400118 20020314 00118 EU 2002 3 14 QXEA0200316 1 20020214 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK GOUGES 9 INCHES FORWARD OF FRAME 11905. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002031400119 20020314 00119 2002 3 14 2002F00249 4 20020125 A 2200 65528179 ACCESSORY UNIT BOEING 737 7373Y0 1384671 NM AFCS MALFUNCTIONED A PIDA O OTHER O OTHER DE DESCENT 1 SO 05 373PA 23749 DURING DESCENT AUTOPILOT 'A' DISENGAGED, WITH AIRCRAFT IN TRIM. UNABLE TO ENGAGE EITHER A OR B AUTOPILOT IN ANY MODE. REPLACED AUTO-PILOT ACCY UNIT. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002031400120 20020314 00120 EU 2002 3 14 QXEA0200322 1 20020215 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACKED CASTELLATION ALONG TWO DIMPLES ON FORWARD SIDE OF FRAME 17565 AT STRINGER 54. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002031400121 20020314 00121 NM 2002 3 14 2002F00250 1 20020122 A 2750 25EN556 SWITCH BOEING 737 7372K5 138448X NM RT MLG WW DEFECTIVE A PIDA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 05 249TR 22598 INT - WHEN FLAPS SELECT FROM 1-5 UNITS AUTO PILOT KICKS OFF. REMOVED AND REPLACED FLAPS UP SWITCH AND RIGGED PER MM 27- 51-291. (M) 2 L 7 2 4F RT A16WE 2002031400122 20020314 00122 NM 2002 3 14 2002F00251 1 20020117 A 3350 20131A BATTERY PACK BOEING 757 757256 NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 810DM 26240 DAL - LEFT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED BATTERY PACK AND CHARGED BATTERY PACK. INSTALLED BATT ERY PACK, OPERATIONS CHECKED NORMAL. (M) 2 L 7 2 4F RT A2NM 2002031400123 20020314 00123 EU 2002 3 14 QXEA0200323 1 20020215 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CASTELLATION ON FORWARD SIDE OF FRAME 17565 AT STRINGER 20 IS CRACKED ADJACENT TO DIMPLE. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002031400124 20020314 00124 NM 2002 3 14 2002F00252 1 20020117 A 3350 767 LIGHT BOEING 757 757200 1384950 NM CABIN FAILED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 801DM 26240 DAL - RIGHT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP, OPERATIONAL CHECKED NORMAL. (M) 2 L 7 2 4F RT A2NM 2002031400125 20020314 00125 NM 2002 3 14 2002F00253 1 20020117 A 3350 LIGHT BOEING 757 757256 NM CABIN FAILED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 810DM 26240 DAL - L-1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP, OPERATIONS CHECKED NORMAL. (M) 2 L 7 2 4F RT A2NM 2002031400126 20020314 00126 NM 2002 3 14 2002F00254 1 20020117 A 3350 P2010046002 LIGHT BOEING 757 757200 1384950 NM CABIN FAILED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 801DM 26240 DAL - R-1 DOOR INTERIOR EMERGENCY RED PATH LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIVE CHECKED N ORMAL. (M) 2 L 7 2 4F RT A2NM 2002031400127 20020314 00127 EU 2002 3 14 QXEA0200324 1 20020218 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - DENT IN RADIUS OF CASTELLATION ON FRAME 16-2 OUTBOARD OF STRINGER 69. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031400128 20020314 00128 EU 2002 3 14 QXEA0200325 1 20020219 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - TWO DENTS IN CASTELLATION ON FRAME 16-2 OUTBOARD OF STRINGER 70. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031400130 20020314 00130 EU 2002 3 14 QXEA0200326 1 20020219 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACK NEXT TO LOWER RIVET OF CASTELLATION ON FRAME 16-2 OUTBOARD OF STRINGER 5. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031400135 20020314 00135 WP 2002 3 14 2002F00182 1 20020211 A 5400 732329287 WASHER DOUG DC10 DC1010 3022110 WP LEFT PYLON LOOSE A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 FOUND LEFT PYLON FORWARD SUPPORT LOWER PLUG NR 2 PLI WASHER ROTATES. (M) 2 L 7 3 4F A22WE 2002031400137 20020314 00137 NM 2002 3 14 2002F00207 1 20020207 A 3230 CONTROL UNIT AIRBUS A319 A319132 3930340 NM FAULTY A SOKF O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 23 474TA 1159 HAV - FLT 620 - DURING PUSH BACK, OF FLIGHT AT HAVANA STATION, THE CAPTAIN REPORTED, ON GROUND WITH ENGINES SHUTDOWN, EN GINE NR 2 HYDRAULIC YELLOW AND ELECTRICAL BLUE PUMPS FAULT LIGHT CAME ON AND OFF, ALSO EPR AND EGT NR 2 CAME ON AND OFF CONSTANTLY. LANDING GEAR SYSTEM DISAGREE. THE AIRCRAFT RETURNED TO THE GATE FOR MAINTENANCE. TECNICIANS AT HAVANA STA TION REMOVED AND REPLACED NR 2 LGCIU PERFORMED OPERATIONAL TEST PER MM 32-31-71, WITH SATISFACTORY RESULTS. NO OTHER FA ULTS WERE DETECTED. THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2002031400138 20020314 00138 NM 2002 3 14 2002F00208 1 20020201 A 2150 D198113 CONVERTER BOEING 757 75723N 1384973 NM A/C BAY FAILED A AMTA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 GL 11 520AT 13548 27976 DURING CRUISE, RIGHT PACK INOP LIGHT AND RIGHT PACK TEMP ON EICAS CAME ON. MAINTENANCE REPLACED NUMEROUS RIGHT PACK SYS TEM COMPONENTS. RIGHT PACK CATALYTIC CONVERTER FAILED INTERNALLY SENDING DEBRIS INTO PACK SYSTEM. (M) 2 L 7 2 4F RT A2NM 2002031400139 20020314 00139 NE 2002 3 14 2002F00210 2 20020124 A 7321 FFG022AC FUEL CONTROL BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAULTY A AMTA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 11 514AT 27971 DURING TAKEOFF FROM MDW, THE LEFT ENGINE DID NOT DEVELOP TAKEOFF POWER. ACHIEVED 1.53 EPR SHOULD HAVE HAD 1.73 EPR. TA KEOFF REJECTED AT 88 KNOTS. THE LEFT ENGINE FUEL FLOW GOVERNOR WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2002031400140 20020314 00140 WP 2002 3 14 2002F00211 1 20020204 A 5312 PRESSURE PANEL LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 186AT 193C1074 DURING C-CHECK, MAINTENANCE DISCOVERED CORROSION IN THE NLG WHEEL WELL WEB, ALONG LBL 22 BETWEEN FS 315 AND FS 334. (M) 2 L 7 3 4F A23WE 2002031400141 20020314 00141 NM 2002 3 14 2002F00212 1 20020128 A 7603 44111115 CONTROL CABLE BOEING 757 75723N 1384973 NM LT ENGINE DEFECTIVE A AMTA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 11 514AT 23434 27971 FLT 205, DURING TAKEOFF, DEPARTING SFO REJECTED THE TAKEOFF BECAUSE THE LEFT ENGINE WOULD NOT REACH TAKEOFF EPR WITH EEC AND ENGINE LIMITER ON. EEC LIMITER OFF NOT CHECKED. 1.72 EPR COMMANDED, 1.67 ACTUAL. AIRCRAFT RETURNED TO THE GATE A ND MAINTENANCE REMOVED AND REPLACED THE TELEFLEX CABLE CONTROL PER MM 76-11-10. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 2002031400142 20020314 00142 NM 2002 3 14 2002F00213 1 20020110 A 2530 OVEN BOEING 757 75723N 1384973 NM GALLEY DIRTY A AMTA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 515AT 27598 FLT 212, EN ROUTE TO MDW, HAD SMOKE IN THE CABIN AFTER OVEN NR 4 WAS TURNED ON AND HEATED. MAINTENANCE AT MDW CLEANED T HE OVEN AND REPLACED THE OVEN GLIDES. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 2002031400143 20020314 00143 EU 2002 3 14 QXEA0200327 1 20020218 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CASTELLATION DENTED ON FRAME 16-2 OUTBOARD OF STRINGER 68. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031400144 20020314 00144 EU 2002 3 14 QXEA0200328 1 20020215 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACKED CASTELLATION ON FRAME 32-2 AT STRINGER 12. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002031400145 20020314 00145 EU 2002 3 14 QXEA0200329 1 20020215 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CASTELLATION ON FRAME 32-2 CRACKED AT STRINGER 11. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002031400146 20020314 00146 EU 2002 3 14 QXEA0200331 1 20020215 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - TWO CRACKS AT RIVETS IN CASTELLATION ON FRAME 32-2 BETWEEN STRINGERS 3 AND 5. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002031400147 20020314 00147 EU 2002 3 14 QXEA0200339 1 20020219 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACK AT UPPER RIVET OF FRAME 41-2 CASTELLATION ON AFT SIDE ABOVE STRINGER 44. REPAIRED IAW FOKKER MM. 2 L 7 2 4F RT A20EU 2002031400148 20020314 00148 EA 2002 3 14 COMA0260183 1 20020313 A 5551 6002307014 FITTING CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 991CA 9124 7216 RH HORIZ STAB VISOR FITTING CRACKED.INSTALLED NEW SERVICEABLE FITTING.I/A/W REO 601R-55-11-016 AND SRM 51-42-06. 2 L 7 2 4F RT A21EA 2002031400149 20020314 00149 EA 2002 3 14 COMA0260184 1 20020313 A 5210 60031535 STRIKER CNDAIR CL600 CL6002B19 1900309 EA FS310 DENTED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 912CA 20338 7011 THE PREVIOUS PAX DOOR REPAIR STRAP ON THE SEAL STRIKER WAS DENTED.REMOVED THE DENTED STRAP AND FABRICATED AND INSTALLED A NEW STRAP I/A/W REO 601R-52-11-008 REV B, REPAIR A. 2 L 7 2 4F RT A21EA 2002031400150 20020314 00150 2002 3 14 VNAA0203013 4 20020309 A 3140 7013348937 DAU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 471PS 1175 3007 AFTER DEPARTING PIT PASSING THROUGH 7000 FEET, THE CAPTAIN REACHED UP TO TURN ON THE ICE PROTECTION AND THE ELEVATOR HOR N HEAT FAILED. DUE TO WEATHER ENROUTE, FLIGHT 4173 RETURNED TO PIT. MAINTENANCE INSPECTED, TROUBLESHOT, AND REPLACED T HE DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002031400151 20020314 00151 NE 2002 3 14 VNAA0203015 2 20020310 A 7300 FUEL FILTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 463PS 3087 THE FLIGHT WAS ENROUTE FROM PIT TO LEX AND THE CREW RECEIVED A FUEL FILTER BYPASS INDICATION. THE CREW FOLLOWED THE QUI CK REFERENCE HANDBOOK AND THEN CALLED MAINTENANCE CONTROL WHO HAD THE CREW DIVERT TO DAY FOR MAINTENANCE. MAINTENANCE I NSPECTED AND REPLACED THE FUEL FILTER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE P ERFORMED AND FLIGHT 4054 CONTINUED ON TO LEX. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002031400152 20020314 00152 NM 2002 3 14 VNAA0203016 1 20020311 A 3200 BRAKE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 424JS 3033 DURING TAKE OFF THE CREW RECEIVED A LEFT HAND INBOARD BRAKE OVERHEAT INDICATION AND ABORTED TAKE OFF. THE CREW CALLED M AINTENANCE CONTROL AND DEFFERRED THE BRAKE INDICATION. FLIGHT 4015 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002031400153 20020314 00153 NM 2002 3 14 VNAA0203009 1 20020308 A 3300 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE 9A FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 463PS 3087 THE CREW REPORTED THAT THE EXIT SIGN AT ROW 9A WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EXIT SIGN DUE TO A BROKEN WIRE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRA FT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002031400158 20020314 00158 NM 2002 3 14 UPS02237478 1 20020105 A 5320 FITTING BOEING 727 727185C 138406N NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI FRAME TO STRINGER CLEAT CORRODED AT BS 420 STR 18L IN THE E+E BAY. AREA OF CORROSION APPROX .75 IN CH BY .5 INCH AND EXTENDED THROUGH THE CLEAT. R&R IAW SRM. 2 L 7 3 4F A3WE 2002031400159 20020314 00159 NM 2002 3 14 UPS02237516 1 20020124 A 3350 COVER BOEING 727 72730C 1384009 NM CABIN LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:PFLT CABIN EXIT LIGHT COVER OVER CABIN DOOR IS LOOSE. CHECK SECURITY OF EXIT LIGHT ASSY PER MAINT PRACT ICES MM 33-50-01 AND INSTALLED LIGHT COVER, NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2002031400161 20020314 00161 NM 2002 3 14 UPS02237530 1 20020102 A 5410 WEB BOEING 727 727185C 138406N NM NR 2 NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI VERTICAL RT WEB CRACKED OVER ENGINE 2 HORIZONTAL FIREWALL AT BS 137 6 APPROX. WEB REPLACED IAW DWG 65-17555. 2 L 7 3 4F A3WE 2002031400162 20020314 00162 NM 2002 3 14 UPS02237531 1 20020102 A 5410 WEB BOEING 727 727185C 138406N NM NR 2 NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI VERTICAL LT WEB CRACKED OVER ENGINE NR 2 HORIZONTAL FIREWALL AT BS 1376 APPROX. WEB REPLACED IAW D WG 65-17555. 2 L 7 3 4F A3WE 2002031400163 20020314 00163 NM 2002 3 14 UPS02237532 1 20020106 A 5320 653414422 FITTING BOEING 727 727185C 138406N NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI EVIDENCE OF CORROSION ON SEAT TRACK SECTION BS 868 LBL 45.5, SEAT TRACK SUPPORT LINK. FITTING REMO VED SRM 51-30-02, NEW FITTING INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2002031400164 20020314 00164 NM 2002 3 14 UPS02237533 1 20020107 A 5315 FLOORBEAM BOEING 727 727185C 138406N NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI EXFOLIATION CORROSION ON THE UPPER CHORD FLANGE OF FLOORBEAM AT BS 480 LBL 25 TO 45. 2 L 7 3 4F A3WE 2002031400166 20020314 00166 NM 2002 3 14 UPS02237535 1 20020108 A 5320 FLOOR SUPPORT BOEING 727 727185C 138406N NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI FLOOR SUPPORT UNDER THIRD CREW MANS TABLE IS CRACKED AT ANCHOR NUT HOLE AND HAS NUMEROUS AREAS OF L IGHT SURFACE CORROSION, FLOOR SUPPORT IS LOCATED JUST AFT OF F/O O2 MASK STORAGE BOX. FLOOR SUPPORT Z-BRACKET LOCATED BETWEEN BS 258-277 LONGITUDINALLY AT RBL 44 APPROX. 2 L 7 3 4F A3WE 2002031400168 20020314 00168 NM 2002 3 14 UPS02237540 1 20020102 A 5720 SUPPORT BRACKET BOEING 727 727185C 138406N NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI SUPPORT BRACKET FOR LT FWD END OF NR 4 FLAP TRACK HAS PITTING CORROSION IN BORE OF HOLE. 2 L 7 3 4F A3WE 2002031400169 20020314 00169 NM 2002 3 14 UPS02237541 1 20020107 A 5753 65281073 CASTING BOEING 727 727185C 138406N NM T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI LT ELEPHANTS EAR FWD CASTING CRACKED ON MOUNT LUG. CASTING REPLACED IAW DWG NO65-26786. 2 L 7 3 4F A3WE 2002031400177 20020314 00177 EU 2002 3 14 QXEA0200332 1 20020215 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - FRAME 32-2 HAS CRACKED CASTELLATION AT BOTTOM RIVET AT STRINGER 70. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002031400178 20020314 00178 EU 2002 3 14 QXEA0200333 1 20020219 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CASTELLATION ON FRAME 50-2 AT STRINGER 9 HAS CRACK FROM LOWER RIVET. REPAIRED IAW FOKKER MM. 2 L 7 2 4F RT A20EU 2002031400179 20020314 00179 EU 2002 3 14 QXEA0200334 1 20020219 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CASTELLATION AT STRINGER 1 ON FRAME 50-2 IS CRACKED AT RIVET. REPAIRED IAW FOKKER MM. 2 L 7 2 4F RT A20EU 2002031400180 20020314 00180 EU 2002 3 14 QXEA0200335 1 20020217 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - AT STRINGER 31 ON AFT SIDE OF FRAME 61-2, CASTELLATION IS CRACKED. REPAIRED IAW FOKKER SRM AND MM. 2 L 7 2 4F RT A20EU 2002031400181 20020314 00181 EU 2002 3 14 QXEA0200336 1 20020216 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - THERE ARE TWO PARALLEL CRACKS IN CASTELLATION ON FORWARD SIDE OF FRAME 32-2. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031400182 20020314 00182 EU 2002 3 14 QXEA0200337 1 20020217 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACK IN RADIUS OF CASTELLATION AT STRINGER 22 ON FRAME 50-2. REPAIRED IAW FOKKER MM. 2 L 7 2 4F RT A20EU 2002031400183 20020314 00183 EU 2002 3 14 QXEA0200338 1 20020217 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACK PAST SECOND STOP DRILL IN LOWER END OF CASTELLATION ON AFT SIDE OF FRAME 50-2 AT STRINGER 46. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031400184 20020314 00184 EU 2002 3 14 QXEA0200340 1 20020215 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - FRAME 32-2 FORWARD SIDE CASTELLATION CRACKED AT STRINGER 61. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002031400185 20020314 00185 EU 2002 3 14 QXEA0200341 1 20020216 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - TWO PARALLEL CRACKS IN FRAME 32-2 CASTELLATION ON FORWARD SIDE AT STRINGER 52. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002031400186 20020314 00186 EU 2002 3 14 QXEA0200342 1 20020218 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACK IN RADIUS OF CASTELLATION REPAIR CLIP ON SIDE OF FRAME 61-2 AT STRINGER 42. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031400187 20020314 00187 EU 2002 3 14 QXEA0200344 1 20020219 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACK IN REAR PRESSURE BULKHEAD AT BEAM VI LOWER FLANGE RADIUS OUTBOARD OF BL 1050L. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002032600082 20020326 00082 NM 2002 3 26 QXEA0200409 1 20020301 A 2910 HYDRAULIC LINE BOMBDR DHC8 DHC8401 NM HYD SYSTEM RUPTURED A QXEA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 410QX 4053 BOI- NR 2 HYD QTY SLOWLY WENT TO ZERO IN FLT NR 2 HYD ISO VALVE CAUTION LIGHT ILLUM, NR 2 HYD PUMP CAUTION LIGHT THEN CA ME ON ALONG WITH RUD HYD CAUTION LIGHT. AFTER THE 3 CAUTION LIGHTS CAME ON, ELE PRESS LIGHT ILLUM. CHECK LIST WAS RAN AND ALTERNATE GEAR EXTENSION ACCOMPLISHED. A/C WAS STOPPED ON RUNWAY AND TOWED TO GATE. REMOVED AND REPLACED NR 2 PCU PRESS LINE AND NR 2 ENG DRIVEN HYD PUMP. REPLACED PTU, FLUSHED NR 2 HYD SYS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 2002031400188 20020314 00188 NM 2002 3 14 QXEA0200410 1 20020302 A 5270 SENSOR BOMBDR DHC8 DHC8401 NM CARGO DOOR DIRTY A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 413QX 4060 SEA- AIRCRAFT RETURNED TO FIELD. FORWARD BAGGAGE DOOR LIGHT ON INFLIGHT, PRESSURE NORMAL. CHECKED PSEU FOR FAULTS, NON E FOUND. CYCLED FORWARD BAGGAGE DOOR SEVERAL TIMES. NO DEFECTS NOTED. CLEANED AND LUBED FORWARD BAGGAGE DOOR PROXIMIT Y SENSORS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031400189 20020314 00189 EU 2002 3 14 QXEA0200411 1 20020302 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX- DENT IN FUSELAGE JUST FORWARD OF FORWARD BAGGAGE DOOR AND JUST AFT OF RIGHT HAND ACM EXHAUST. INSTALLED REPAIR IAW SRM. 2 L 7 2 4F RT A20EU 2002031400190 20020314 00190 WP 2002 3 14 ZW0A0201004 1 20020117 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C, THE CARGO COMPARTMENT LT TIE DOWN TRACK WAS CORRODED AT STA 1088 TO 1126. REPLACED TRACK PER SRM. 2 L 7 2 4F RT A6WE 2002031400191 20020314 00191 WP 2002 3 14 ZW0A0201005 1 20020117 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT, THE CABIN FLOOR SUPPORT, STA 200 TO 220, RBL 55 HAD CORROSION IN SEVERAL PLACES. REMOVED AND REPL ACED FLOOR SUPPORT PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2002031400192 20020314 00192 WP 2002 3 14 ZW0A0201006 1 20020117 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT IN THE FWD CABIN FOUND CORROSION UNDER FLOOR SUPPORTS AND AFT CORNER OF DOOR, STA 198 TO 204, BETWE EN RBL 52 AND RBL 59 WEB MEMBRANE. INSTALLED NEW MEMBRANE PER SRM 51-70-04. 2 L 7 2 4F RT A6WE 2002031400193 20020314 00193 WP 2002 3 14 ZW0A0201007 1 20020117 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND FWD CABIN FLOOR SUPPORT CORRODED AT STA 200 BETWEEN RBL 44 INCHES AND RBL 56 INCHES. INSTALL ED NEW FLOOR SUPPORT PER DRAWING 9957828. 2 L 7 2 4F RT A6WE 2002031400194 20020314 00194 WP 2002 3 14 ZW0A0201008 1 20020117 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT IN THE FWD CABIN FROM STA 160 TO 200, RBL 55, THE FLOOR SUPPORT WAS CORRODED IN SEVERAL LOCATIONS. 2 L 7 2 4F RT A6WE 2002031400195 20020314 00195 WP 2002 3 14 ZW0A0201009 1 20020118 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT, THE UNDER FLOOR MEMBRANE WAS CORRODED AT FWD GALLEY MOUNT FITTING, STA 160, RBL 45 TO 51. CUT OUT CORRODED SECTION AND REPLACED PER SRM 53-01 FIG 2. 2 L 7 2 4F RT A6WE 2002031400196 20020314 00196 WP 2002 3 14 ZW0A0201010 1 20020116 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT IN THE FWD CABIN FOUND HEAVY CORROSION ON FLOOR SUPPORT BEAM AT RBL 9 TO RBL 46, AT STATION 200. REPLACED FLOOR SUPPORT PER SRM 51-30-02. 2 L 7 2 4F RT A6WE 2002031400197 20020314 00197 WP 2002 3 14 ZW0A0201011 1 20020116 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FORMER AT STA 1308 HAD CORROSION AT LONGERON 30, ON THE AFT SIDE. REMOVED C ORRODED SECTION OF FRAME AND INSTALLED NEW PIECE WITH SPLICES PER SRM 53-03 FIG 2A. 2 L 7 2 4F RT A6WE 2002031400198 20020314 00198 WP 2002 3 14 ZW0A0201012 1 20020117 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT IN CABIN AT STA 1136 TO 1212, THE NUMBER 2 CHAIR TRACK HAD CORROSION AROUND FLOOR PANEL ATTACH HOLE S. REPAIRED SEAT TRACK PER SRM. 2 L 7 2 4F RT A6WE 2002031400199 20020314 00199 WP 2002 3 14 ZW0A0201013 1 20020118 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT IN THE FWD CABIN FOUND HEAVY CORROSION IN RT OUTBOARD CHAIR TRACK AT STA 217. REPLACED TRACK SECTI ON PER SRM 53-05-4F. 2 L 7 2 4F RT A6WE 2002031400200 20020314 00200 NM 2002 3 14 ZW0A0201101 1 20020118 A 3350 79785 LIGHT BOEING 767 76733AER 1385230 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 637TW 25403 THE EGRESS LIGHT STRIP WAS INOPERATIVE AT ROW 23L TO THE L4 CABIN DOOR, THE GALLEY BULKHEAD AND THE MID GALLEY. REPLACE D THE LIGHT STRIP AT EACH LOCATION. 2 L 7 2 4F RT A1NM 2002031400201 20020314 00201 NM 2002 3 14 ZW0A0201102 1 20020113 A 3350 767 LIGHT BOEING 767 7673Y0 NM EXTERIOR INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 640TW 25411 THE RT SIDE NUMBER 2 AND LT SIDE NUMBER 4 CABIN DOOR SLIDE LIGHTS WERE INOPERATIVE ON TEST. REPLACED THE LAMP AT BOTH L OCATIONS. 2 L 7 2 4F RT A1NM 2002031400202 20020314 00202 WP 2002 3 14 ZW0A0201103 1 20020121 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT FOUND CORROSION AT PANEL ATTACH HOLES IN LT TIE DOWN TRACK, STA 644 TO 787 AND IN TIE DOWN TRACK AB OVE LONGERON 27L. FOUND TRACK CORRODED BEYOND LIMITS. FABRICATED NEW TRACK AND INSTALLED REPAIR PER SRM. 2 L 7 2 4F RT A6WE 2002031500001 20020315 00001 NM 2002 3 15 HNAA0200031 1 20020313 A 7120 8DK1763001 STRUT DHAV DHC8 DHC8102 2809003 NM CRACKED A HNAA K NONE Z SIGNIFICANT FAILURE REPORT IN INSP/MAINT 1 EA 07 910HA 022 DURING ROUTINE INSPECTION FOUND #2 ENGINE AFT OUTBOARD ENGINE MOUNT VERTICAL STRUT CRACKED AT THE HORIZONTAL STRUT ATTAC H POINT. REPLACED VERTICAL STRUT. 2 H 7 2 4T RT A13NM 2002031500005 20020315 00005 EU 2002 3 15 2002F00267 1 20020206 A 2611 2TC61 SMOKE DETECTOR AIRBUS 320 A320231 3930325 EU CARGO BAY ACTIVATED A RYNA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 GCVYD 393 AFT CARGO AND LAVATORY SMOKE WARNING ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT FROM MSP TO MCO. (M) 2 L 7 2 4F RT A28NM 2002031500006 20020315 00006 WP 2002 3 15 2002F00268 1 20020219 A 2810 FUEL TANK DOUG DC10 DC1010 3022110 WP LT WING CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 BRACKETS INSIDE LEFT FUEL TANK CRACKED AT STATION 402 AND 403 STRINGERS 7, 36 AND 37. (M) 2 L 7 3 4F A22WE 2002031500007 20020315 00007 WP 2002 3 15 2002F00269 1 20020219 A 5751 BALANCE WEIGHT DOUG DC10 DC1010 3022110 WP LT AILERON CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 571RY 46645 BALANCE WEIGHTS ON LEFT OUTBOARD AILERON CORRODED. 2 L 7 3 4F A22WE 2002031500008 20020315 00008 NM 2002 3 15 2002F00270 1 20020129 A 3350 110049 BATTERY PACK BOEING 747 747132 1384882 NM CABIN DISCHARGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 FOUND A-CHECK, L5 AND R5 EMERGENCY LIGHT INOPERATIVE STATION 2280. BATTERY PACK REPLACED AND OPS CHECK PER MM. REF EIAA 2002003. (M) 2 L 7 4 4F A20WE 2002031500009 20020315 00009 CE 2002 3 15 2002F00271 1 20020223 A 5220 1294300452 DOOR BEECH 1900 1900D 1154162 CE EMERGENCY EXIT OUT OF RIG A AMWA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 07 139ZV UE139 FOUND DURING PREFLIGHT CHECK, THE RAMP AGENT FOUND THE HANDLE TO THE EMEGENCY EXIT DOOR NOT FLUSH, MAINTENANCE FOUND TH E DOOR TO BE OUT OF RIG, WAS FERRIED TO PFN FOR REPAIR WITH NO FURTHER INCIDENT. (M) 2 L 7 2 4T RT A24CE 2002031500010 20020315 00010 CE 2002 3 15 2002F00272 1 20020225 A 5220 1294300452 DOOR BEECH 1900 1900D 1154162 CE EMERGENCY EXIT OUT OF RIG A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 237YV UE237 DURING CREW CHANGE, THE ON COMING CREW FOR AIRCRAFT FOUND THE RIGHT FORWARD EMERGENCY EXIT DOOR NOT FLUSH WITH THE EXTER IOR OF THE AIRCRAFT. AIRCRAFT MAINTENANCE FOUND THE DOOR TO BE OUT OF RIG, AND ADJUSTED THE DOOR PER MAINTENANCE INSTRU CTION. RETURNED TO SERVICE WITH A ONE HOUR DELAY. (M) 2 L 7 2 4T RT A24CE 2002031500017 20020315 00017 NM 2002 3 15 A6WA200230003 1 20020126 A 2120 SMOKE DORNER DO32 DO328100 2996000 NM CABIN DETECTED A A6WA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 330MX 3067 LAVATORY SMOKE CAS MESSAGE, VISIBLE SMOKE, RETURNED TO GATE. MAINTENANCE RAN ENGINES WITH PAX ON FOR 15 MINUTES, NO SMO KE NOTED. (M) 2 H 7 2 4T RT A45NM 2002031500018 20020315 00018 EA 2002 3 15 A6WA200240004 1 20020204 A 3222 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA NLG DISCONNECTED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 405AW 7362 UPON DEPARTING OUT OF DENT, GEAR RETRACTION, GEAR DISAGREE WOW INPUT AND WOW OUTPUT MESSAGE MAINTENANCE FOUND NLG SCISSO RS (TORQUE LINKS) DISCONNECTED. UPPER TORQUE LINK DAMAGED. INSPECTED GEAR. REPAIRED DAMAGE TO SCISSOR. PERFORMED GEA R SWINGS. (M) 2 L 7 2 4F RT A21EA 2002031500026 20020315 00026 NM 2002 3 15 AALA20020040 1 20020111 A 3040 62400664 SENSOR BOEING 757 757223 1384957 NM COCKPIT DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 641AA 24599 PHX - FLT 612 - EN ROUTE SNA-DFW, DETECTED SMOKE IN CABIN AND COCKPIT. DIVERTED PHX AND LANDED WITHOUT FURTHER INCIDENT . REPLACED WINDOW HEAT SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002031500027 20020315 00027 WP 2002 3 15 AALA20020061 1 20020119 A 3600 5953625521 DUCT DOUG DC9 DC982 3022082 WP TAIL DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 474 49649 BOS - FLT 1229 - BOS-ORD - AFTER TAKEOFF, TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED. LANDED BOS WITHOUT INCIDENT. R EPLACED RUPTURED DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500028 20020315 00028 WP 2002 3 15 AALA20020062 1 20020119 A 2913 314195 PUMP DOUG DC9 DC982 3022082 WP NR 2 ENGINE DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 402A 49313 DFW-CMH - FLT 1122 - RIGHT ENGINE HYDRAULIC PUMP FAILURE. DURING CLIMB-OUT RETURNED AND LANDED DFW WITHOUT INCIDENT. R EPLACED RIGHT ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500029 20020315 00029 WP 2002 3 15 AALA20020063 1 20020118 A 2822 3980001 PUMP DOUG DC9 DC982 3022082 WP FUEL TANK DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 443AA 49469 ORD-ATL - FLT 419 - AFTER LEVELING OFF AT CRUISE ALTITUDE, FUEL NOT FEEDING FROM CENTER TANK. INLET FUEL LOW PRESSURE L IGHTS CAME ON WITH CENTER PUMPS ONLY ON. AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED FORWARD AND AFT FUEL PUMPS. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500030 20020315 00030 WP 2002 3 15 AALA20020067 1 20020122 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP SEAT 5 DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7536A 49990 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT TRACK LIGHTING AT SEAT 5E INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500031 20020315 00031 WP 2002 3 15 AALA20020068 1 20020122 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 558AA 53088 ORD - DURING OVERNIGHT MAINTENANCE EMERGENCY SEAT MOUNTED EXIT LIGHTING FORWARD OF OVERWING EXIT INOPERATIVE. COULD NOT DUPLICATE, SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500032 20020315 00032 WP 2002 3 15 AALA20020069 1 20020127 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7547A 53029 ORD - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT INOPERATIVE. REPAIRED OVERWING EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500033 20020315 00033 WP 2002 3 15 AALA20020070 1 20020126 A 3350 P4010049 CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 403A 49314 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD ENTRY LIGHT DIM. REPLACED FIRST CLASS BATTERY AND CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500034 20020315 00034 NM 2002 3 15 AALA20020076 1 20020118 A 2421 GENERATOR BOEING 767 767323 1385205 NM RIGHT INOPERATIVE A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 21 396AN 29603 BOS - FLT 147 - RT GENERATOR OFF LIGHT IN CRUISE. GENERATOR WOULD NOT RESET. REPLACED RIGHT GENERATOR PER MM. ACCOMPL ISHED REQUIRED TESTS. ALSO, REPLACED GCU PER MM. ALL CHECKS OK. (M) 2 L 7 2 4F RT A1NM 2002031500035 20020315 00035 NM 2002 3 15 AALA20020077 1 20020119 A 2460 CIRCUIT BOARD BOEING 777 777223 1385213 NM ELECTRICAL FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 759AN 32638 LHR - FLT 131 - ONE HOUR AND 20 MINUTES INTO FLIGHT RIGHT MAIN AC BUSS FAILED WITH THE FOLLOWING EICAS MSGS. BULK AFT C ARGO HEAT, ELMSP210 PANEL, RAT GEN HEAT, AIR GRNG R, RECIRCULATION FAN. DIVERTED TO LHR, DECLARED EMERGENCY, LANDING WE IGHT 452,00. TROUBLE SHOT AS PER FIM AND REPLACED ELEC UNIT CIRCUIT CARD M24403A3 AS PER MM 24-09-00-2. ALL MESSAGES C LEARED. ENGINE RUN COMPLETED WITH ELEC LOAD TRANSFER. ALL ELEC SYSTEM OPS AND INDICATOR NORMAL. (M) 2 L 7 2 4F RT T00001SE 2002031500036 20020315 00036 NM 2002 3 15 AALA20020078 1 20020119 A 2421 GEN3014 IDG BOEING 777 777223 1385213 NM RT ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 770AN 29578 JFK - FLT 132 - RIGHT GEN CONTROL TRIPPED. RESET, TRIPPED AGAIN. REPLACED RT ENG IDG PLUS ALL CHECKED. OPS CHECKED OK . (M) 2 L 7 2 4F RT T00001SE 2002031500037 20020315 00037 NM 2002 3 15 AALA20020081 1 20020124 A 2421 GEN5103 IDG BOEING 767 767223 1385123 NM RIGHT ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 322AA 22323 EICAS GEN DRIVE LIGHT AND ASSOCIATED RIGHT GEN CONTROL LIGHT ILLUMINATED WHILE CLIMBING TO FLIGHT LEVEL 370 GENERATOR DR IVE DISCONNECTED PER OP MANUAL. REMOVED AND REPLACED RIGHT IDG. NEEDS LEAK AND OPS CHECK AND DISCONNECT CHECK. OPS CH ECK AND LEAK CHECK OK. (M) 2 L 7 2 4F RT A1NM 2002031500038 20020315 00038 WP 2002 3 15 AALA20020083 1 20020128 A 5220 HANDLE DOUG DC9 DC982 3022082 WP TAIL CONE INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 492AA 49730 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE HANDLE RELEASE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED TAIL CONE HANDL E RELEASE EMERGENCY EXIT LIGHT ASSEMBLY AND ADJUSTED WIRE HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500039 20020315 00039 NM 2002 3 15 AALA20020084 1 20020127 A 3350 5736645 LIGHT BOEING 757 757223 1384957 NM OVERWING INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 614AA 24490 JFK - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002031500040 20020315 00040 NM 2002 3 15 AALA20020085 1 20020125 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 607AM 27058 DFW - DURING OVERNIGH MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 34D INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNECT OR AT SEAT 34D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002031500041 20020315 00041 2002 3 15 AALA20020086 4 20020124 A 3417 ADC AIRBUS 300 A300B4605R 3930308 EU COCKPIT FAILED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 25071 514 ATC 2 FAULTED CONTINUED AURAL WARNING UNTIL DESCENT. ACCOMPLISHED ATC BITE CHECK. ALL CHECKS NORMAL. ADC FAULT NR 1 S WITCHED TO 2. REPLACED NR 1 AIR DATA COMPUTER ACCOMPLISHED ADC BITE AND AFS TEST. ALL TEST PASSED. (M) 2 L 7 2 4F RT A35EU 2002031500042 20020315 00042 WP 2002 3 15 AALA20020087 1 20020115 A 5310 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - FOUND SHEAR TIE CRACKED. REPLACED SHEAR TIE PER SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2002031500043 20020315 00043 WP 2002 3 15 AALA20020088 1 20020115 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - FOUND CORROSION ON SEAT TRACK NR 6 STATION 218 TO 222. REPLACED SEAT TRACK STATION 218-304 PER SRM 53-05-00. (M) 2 L 7 2 4F RT A6WE 2002031500044 20020315 00044 WP 2002 3 15 AALA20020089 1 20020115 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - FOUND TWO SCRATCHES TWO FEET AFT OF FORWARD ENTRY DOOR ABOVE BLUE STRIPE. BLENDED, TREATED AND INSTALLED TWO ROW DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F RT A6WE 2002031500045 20020315 00045 WP 2002 3 15 AALA20020090 1 20020115 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - FOUND SCRATCHES IN SKIN AND DENT LEFT STATION 219 AT L10L. BLENDED, TREATED AND INSTALLED TWO ROW DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F RT A6WE 2002031500046 20020315 00046 WP 2002 3 15 AALA20020091 1 20020115 A 5310 WINDOW FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - FOUND FORWARD LOWER FORWARD CORNER OF WINDOW FRAME CRACKED ON RIGHT SIDE OF AC AT STATION 985. INSTALLED DOUBLER PER AARD 53-10-00-25. (M) 2 L 7 2 4F RT A6WE 2002031500047 20020315 00047 WP 2002 3 15 AALA20020092 1 20020117 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - FOUND STATION 1175 LOWER SIDE OF CUSP CORRODED, LEFT SIDE OF CABIN. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2002031500048 20020315 00048 WP 2002 3 15 AALA20020093 1 20020113 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - FOUND HEAVY CORROSION RIGHT CUSP PREVIOUSLY REPAIRED. INSTALLED NEW CUSP SHEET FROM STATION 598-712 RIGHT. (M) 2 L 7 2 4F RT A6WE 2002031500049 20020315 00049 WP 2002 3 15 AALA20020094 1 20020118 A 5320 BRACKET DOUG DC9 DC983 3022083 WP GIRT BAR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - AFT GALLEY SERVICE DOOR AREA CUSP UPPER SURFACE UNDER GIRT BAR ATTACH BRACKET INBOARD AND OUTBOARD HOLES IN CUSP H AS CORROSION AROUND THEM. INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2002031500050 20020315 00050 WP 2002 3 15 AALA20020096 1 20020116 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - FOUND SKIN GOUGED AT STATION 312 BETWEEN L21 AND L22 RIGHT SIDE. CUT 1 INCH HOLE TO REMOVE DAMAGE. INSTALLED DOU BLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F RT A6WE 2002031500051 20020315 00051 WP 2002 3 15 AALA20020097 1 20020113 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - FOUND LIGHT CORROSION RIGHT CUSP PREVIOUSLY REPAIRED. INSTALLED NEW CUSP SHEET FROM STATION 598-712 RIGHT. (M) 2 L 7 2 4F RT A6WE 2002031500052 20020315 00052 WP 2002 3 15 AALA20020098 1 20020114 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - FOUND DENT IN SKIN AND SKIN SCUFFED LEFT STATION 427 AT L20L. REWORKED SKIN AND INSTALLED DOUBLER PER SRM 53-04 F IG 38. (M) 2 L 7 2 4F RT A6WE 2002031500053 20020315 00053 WP 2002 3 15 AALA20020099 1 20020110 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1205-1210. ROUTED OUT CORRODED AREA, TREATED AND PRIMED. INSTALLED PLUG R EPAIR. (M) 2 L 7 2 4F RT A6WE 2002031500054 20020315 00054 WP 2002 3 15 AALA20020100 1 20020110 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSLEAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1233-1235. ROUTED OUT CORROSION BY ROUTER, TREATED AND PRIMED, INSTALLED P LUG REPAIR. (M) 2 L 7 2 4F RT A6WE 2002031500055 20020315 00055 WP 2002 3 15 AALA20020101 1 20020116 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 TUL - FOUND CORROSION ON CUSP SHEET RIGHT SIDE, STATION 712 TO 719. INSTALLED NEW FABRICATED DOUBLER PER AARD 53-00-00- 02. (M) 2 L 7 2 4F RT A6WE 2002031500056 20020315 00056 EU 2002 3 15 AALA20020105 1 20020131 A 2150 EGA1790501 A/C PACK FOKKER F28 F28MK0100 4990807 EU ACM BAY CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 1400H 11340 IAD - FLT 1097 - DURING TAKEOFF, EN ROUTE DCA-ORD, AIRCRAFT STARTED TO FILL WITH SMOKE. DIVERTED AND LANDED IAD WITHOUT INCIDENT. ACCOMPLISHED PACK BURNOUT OF RESIDUAL HYDRAULIC OIL THAT LEAKED FROM RIGHT PRESURE REGULATOR VALVE THE PREVI OUS DAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002031500057 20020315 00057 WP 2002 3 15 AALA20020106 1 20020131 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 555AN 53085 DFW - DURING OVERNIGHT MAINTENANCE, AFT HALF OF CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500058 20020315 00058 NM 2002 3 15 CALA0200130 1 20020314 A 5711 SPAR BOEING 737 7373T0 1384582 NM L/W UPPER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34315 23366 INSPECTION FOUND A 0.2" CRACK IN L/H WING UPPER SPAR AT #4 HOLE FROM THE I/B SIDE COMMOM TO THE SUPPORT FITTING. AN OVER SIZED BOLT WAS INSTALLED IAW ECRA 5743-01050. A DETAILED VISUAL INSPECTION OR HFEC INSPECTION WILL BE PERFORMED ON THE S PAR VERTICAL FLANGE BELOW AND ABOVE FOOTPRINT OF MLG FITTING IAW ECRA 5743-01050 EVERY 4500 CYCLES. 2 L 7 2 4F RT A16WE 2002031500059 20020315 00059 NM 2002 3 15 CALA0200131 1 20020315 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 685-706 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND A 1.125" CRACK IN WHEEL WELL CENTER KEEL EXTERIOR SKIN PANEL. THE CRACK WAS LOCATED ALONG R/H SIDE BETW EEN STA 685 AND 706. A DOUBLER WAS INSTALLED AND PAINTED IAW SRM 53-60-12, FIGURE 202. 2 L 7 2 4F RT A16WE 2002031500060 20020315 00060 2002 3 15 372PA0004 4 20020314 A 2210 AUTOPILOT SYS BOEING 737 737306 NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 372PA 23546 VNAV Disconnects in flight without command. Will not re-engage. All nav data lost. "Verify IRS position" message appears . CND. 2 L 7 2 4F RT A16NE 2002031500061 20020315 00061 EU 2002 3 15 02073330 1 20020214 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 330UE 41098 During preflight inspection, the crew reported that the forward section of the emergency floor track lighting was inoper ative. Maintenance personnel secured an electrical connector for the emergency floor track lighting system. An operati onal check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002031500062 20020315 00062 EU 2002 3 15 AALA20020107 1 20020131 A 2560 HORN AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 18066 509 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EVACUATION SIREN AT 2R DOOR WAS INOPERATIVE. REPLACED EMERGENCY EVACUATIO N SIREN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002031500063 20020315 00063 EA 2002 3 15 COMA0260185 1 20020313 A 2740 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 967CA 7134 FLIGHT 5651 STAB TRIM CAUTION MESSAGE DURING T/O.CLEANED CO PILOTS STAB RIM SWITCH. 2 L 7 2 4F RT A21EA 2002031500064 20020315 00064 WP 2002 3 15 AALA20020108 1 20020201 A 3350 P40110049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 225AA 49175 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEATS 18-21 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BAT TERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500065 20020315 00065 WP 2002 3 15 AALA20020109 1 20020203 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 553AA 53083 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 18-21 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATT ERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500066 20020315 00066 WP 2002 3 15 AALA20020110 1 20020203 A 2560 P2070003001 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 412AA 49323 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED FORWARD ENTRY EME RGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500067 20020315 00067 WP 2002 3 15 AALA20020111 1 20020131 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70504 49798 DFW - DURING OVERNIGHT MAINTENANCE, SEAT EMERGENCY PATH LIGHTING FRONT HALF OF AIRCRAFT INOPERATIVE. REPLACED NR 2 BATT ERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500069 20020315 00069 WP 2002 3 15 AALA20020112 1 20020131 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 555AN 53085 DFW - DURING OVERNIGHT MAINTENANCE, SEAT EMERGENCY PATH LIGHTING AFT HALF OF AIRCRAFT INOPERATIVE. REPLACED BATTERY PAC K. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500070 20020315 00070 NM 2002 3 15 AALA20020113 1 20020204 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 607AM 27058 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT 34D INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTO R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002031500072 20020315 00072 WP 2002 3 15 AALA20020114 1 20020205 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 483A 49676 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT AFT STAIRS SIDEWALL ON LEFT SIDE INOPERATIVE. REPAIRED LEF T SIDE EMERGENCY EXIT LIGHTS AT AFT STAIRS SIDEWALL WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500073 20020315 00073 WP 2002 3 15 AALA20020115 1 20020123 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND RIGHT CUSP STATION 1095 HAS HEAVY CORROSION AT LIGHTENING HOLE CUT OUT. INSTALLED DOUBLER PER AARD 53-00-00 -02. (M) 2 L 7 2 4F A6WE 2002031500075 20020315 00075 WP 2002 3 15 AALA20020116 1 20020125 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND DENT IN RIGHT FUSELAGE AFT OF CARGO DOOR STATION 446 REF ADL 0005. REMOVED DAMAGED SKIN AND INSTALLED REPAI R DOUBLR PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2002031500077 20020315 00077 WP 2002 3 15 AALA20020117 1 20020130 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND DENT WITH A GOUGE AT STATION 1302 L19R. INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 38 SHEET 24 1A INSTALLED SCUFF PLATE PER AARD 53-30-00-8. (M) 2 L 7 2 4F A6WE 2002031500078 20020315 00078 WP 2002 3 15 AALA20020118 1 20020124 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND SMALL CRACK FUSELAGE SKIN EXTENDING FROM FASTENER HOLE STATION 1380 9 INCH ABOVE LEFT ENGINE PYLON. STOP DR ILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3/ AARD 53-30-00-02. (M) 2 L 7 2 4F A6WE 2002031500079 20020315 00079 WP 2002 3 15 AALA20020119 1 20020125 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - BLEND OUT OF LIMITS ABOVE LONGERON 6R AT STATION 839. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 20. (M) 2 L 7 2 4F A6WE 2002031500080 20020315 00080 WP 2002 3 15 AALA20020120 1 20020122 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND GOUGES AT STATION 256 L28R AND L29R. BLENDED GOUGE AND INSTALLED DOUBLER PER SRM 53-04 VIEW E. (M) 2 L 7 2 4F A6WE 2002031500082 20020315 00082 WP 2002 3 15 AALA20020121 1 20020124 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND LEFT CUSP CORRODED STATION 275-278. REPAIRED WITH DOUBLER CUSP PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2002031500084 20020315 00084 WP 2002 3 15 AALA20020122 1 20020125 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND CUSP CORRODED AT STATION 1212 FRAME CUTOUT RIGHT CUSP. CUTOUT CORROSION. INSTALLED DOUBLER PER SRM 53-01 F IG 4. (M) 2 L 7 2 4F A6WE 2002031500085 20020315 00085 WP 2002 3 15 AALA20020123 1 20020112 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND SEAT TRACK NR 4 CORRODED STATION 237-239. INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2002031500086 20020315 00086 WP 2002 3 15 AALA20020124 1 20020128 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP CABIN FLOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND SUB FLOOR CORRODED AT STATION 200 RBL 4. CUT OUT DAMAGED AREA 1 INCH BY 2 INCH INSTALLED DOUBLER PER 53-00- 00-02 PAGE 1. (M) 2 L 7 2 4F A6WE 2002031500087 20020315 00087 NM 2002 3 15 02FDEA00200 1 20020313 A 2710 AILERON DOUG MD11 MD11F 3023600 NM ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 605FE 48514 02-67 AILERON DEFLECT DISAGREE ALERT CAME ON IN FLT. DIVERT TO RCTP DUE TO INCREASE FUEL BURN. ** S/D ** COMING 2 L 7 3 4F RT A22WE 2002031500088 20020315 00088 WP 2002 3 15 AALA20020125 1 20020124 A 5311 FRAME DOUG DC9 DC982 3022082 WP FS 465 CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND STATION 465 BELTFRAME WORN INTO ABOVE DUCT SUPPORT LONGERON 6L. BLENDED AREA AND INSTALLED DOUBLER PER AARD 53-10-00-14 FIG 1 SHEET 1. (M) 2 L 7 2 4F A6WE 2002031500090 20020315 00090 WP 2002 3 15 AALA20020126 1 20020129 A 5551 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FS 1463 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND VERTICAL STAB ATTACH ANGLE CRACKED AT TOP OF 1463 CANT FRAME. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PE R AARD 53-10-00-2. (M) 2 L 7 2 4F A6WE 2002031500091 20020315 00091 WP 2002 3 15 AALA20020127 1 20020130 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND WEAR GROOVE IN BELTFRAME RIGHT STATION 1418 AT L21R. BLENDED WEAR AND INSTALLED DOUBLER PER AARD 53-10-00-1 4. (M) 2 L 7 2 4F A6WE 2002050200066 20020502 00066 EU 2002 5 2 2002UALA00321 1 20020303 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 456UA 1128 LEFT HAND EXTERNAL FUSELAGE BLIND FASTENER HOLE AT STATION 1270 STRINGER 38L HAS CRACK INDICATION AT 6:00 POSITION VERIF IED WITH NONDESTRUCTIVE TESTING. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN DOUBLER. 2 L 7 2 4F 4 F RT A28NM E40NE 2002031500092 20020315 00092 WP 2002 3 15 AALA20020128 1 20020130 A 5753 FITTING DOUG DC9 DC982 3022082 WP TE FLAP WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND RIGHT INBOARD FLAP, OUTBOARD HINGE FITTING BEARING BORE WORN BEYOND LIMITS. OVERSIZED BORE TO 2.349 INCH, B USHED WITHE 17-4 PH BAR PER ESO 80559 DATED 1-29-02. (M) 2 L 7 2 4F A6WE 2002031500093 20020315 00093 NM 2002 3 15 2002UALA00333 1 20020302 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 FUSELAGE FRAME CRACKED AT STATION 188 RIGHT HAND AT WL 207. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL FUSELAGE SKI N DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002031500094 20020315 00094 WP 2002 3 15 AALA20020129 1 20020123 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND SHEAR TIE CRCKED IN RADIUS FRAME 1437 AFT SIDE JUST RIGHT OF LONGERON. REMOVED AND REPLACED SHEAR TIE PER S RM 51-01 FRAME 1437 RIGHT OF LONGERON 1. (M) 2 L 7 2 4F A6WE 2002031500095 20020315 00095 NM 2002 3 15 2002UALA00334 1 20020302 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 MID CABIN STRINGER 3R GOUGED ON INSIDE CHANNEL. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002031500096 20020315 00096 WP 2002 3 15 AALA20020130 1 20020125 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSLEAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND SEVERAL AREAS OF CORROSION ON NR 6 SEAT TRACK STATION 1031-1309. REPLACED NR 6 SEAT TRACK FROM STATION 1031 -1309 PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002031500097 20020315 00097 WP 2002 3 15 AALA20020131 1 20020123 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND CRACK ON FUSELAGE AT AFT HINGE CUT OUT FOR RIGHT NOSE GEAR STRUT DOOR. REMOVED CRACKED REPAIR DOUBLER AND I NSTALLED NEW SERVICEABLE DOUBLER PER SRM 53-05-00. (M) 2 L 7 2 4F A6WE 2002031500098 20020315 00098 WP 2002 3 15 AALA20020132 1 20020124 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 427AA 49339 TUL - FOUND DENT IN FUSELAGE SKIN 4 FEET AFT OF AFT CENTER CARGO DOOR. REMOVED DAMAGED AND INSTALLED DOUBLER PER SRM 53 -04 FIG 38 SHEET 23. (M) 2 L 7 2 4F A6WE 2002040300169 20020403 00169 NM 2002 4 3 2002UALA00335 1 20020301 A 3230 UPLOCK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LANDING GEAR MALFUNCTIONED A UALA K NONE J WARNING INDICATION AP APPROACH 1 WP 29 775UA 26947 AIRCRAFT GEAR MALFUNCTIONED ON APPROACH. CONFIRMED BY SAMC-LHR VIA PHONE APPROX 1 HOUR AFTER LANDING. NO CREW CONTACT. LANDED SAFELY AFTER GO-AROUND. FRA OPS HAD NO ADDITIONAL INFO. BASED ON INFO AVAILABLE THERE WAS A DELAY IN THE EXTE NSION OF THE LT MLG. THIS WAS SECOND OCCURRENCE IN TWO WEEKS ON SAME AIRCRAFT. AFTER EACH INCIDENT, THE AIRCRAFT WAS J ACKED AND GEAR WAS CYCLED WITH NO DEFECTS NOTED. THE DOOR OPERATED SEQUENCE VALVE WAS REPLACED AFTER FIRST INCIDENT AS A PRECAUTION. BOTH THE UPLOCK ACTUATOR AND DRAG BRACE OPERATED SEQUENCE VALVE WAS REPLACED AFTER THE SECOND INCIDENT. SUBSEQUENT TO SECOND INCIDENT AIRCRAFT HAS FLOWN TWENTY-THREE FLIGHTS AS OF THIS DATE WITH NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002031500099 20020315 00099 WP 2002 3 15 AALA20020134 1 20020204 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 423AA 49335 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT INOPERATIVE. REPLACED EMEREGNCY EXIT BATTERY. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002031500100 20020315 00100 NM 2002 3 15 AALA20020136 1 20020202 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 ORD - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHT AT AFT RIGHT CRWE BUNK INOPERATIVE. REPAIRED BROKEN WIRES TO EMERGENCY LIGHT AT AFT RIGHT CREW BUNK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002031500101 20020315 00101 NM 2002 3 15 AALA20020137 1 20020201 A 3350 S283T0143 BATTERY PACK BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS AT 7AB AND 1-8 INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002031500102 20020315 00102 NM 2002 3 15 2002UALA00337 1 20020303 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 FLOORBEAM T-CAP HAS CORROSION BODY STATION 1197, LBL 1 UNDER NUT PLATE. MAJOR REPAIR ACCOMPLISHED. REPAIRED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002031500103 20020315 00103 NM 2002 3 15 AALA20020140 1 20020203 A 2421 GEN5103 IDG BOEING 767 767323 1385205 NM LT GEN FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 389AA 27449 MIA - FLT 68 - LEFT GENERATOR OFF STATUS MESSAGE WITH ASSOCIATED LEFT GEN CONTINUED OFF LIGHT TRIED ONE RESET AND THE LI GHTS REMAINED ILLUMINATED. PREVIOUSLEY FACTED OUT AT MIA ON 2-3-02 LOG PAGE 6862243. REMOVED AND REPLACED LEFT ENGINE IDG PER MM. OPS CHECK AND LEAK CHECK NORMAL. (M) 2 L 7 2 4F RT A1NM 2002031500104 20020315 00104 2002 3 15 AALA20020141 4 20020205 A 3417 COM5107 ADC BOEING 767 767323 1385205 NM E/E COMP FAILED A AALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SW 21 370AA 25197 FRA - FLT 71 - AFTER TAKEOFF FIRST OFFICERS AIRSPEED AND ALTIMETER FAILED. SELECTING ADC TO ALTIMETER RESTORED INFORMAT ION. REPLACED F/O ADC PER MM 34-12-01-4. ALL CHECKS OK. (M) 2 L 7 2 4F RT A1NM 2002031500105 20020315 00105 NM 2002 3 15 2002UALA00339 1 20020303 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 FRAME DENTED IN FORWARD PIT STATION 580 STRINGER 23L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR ON FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031500106 20020315 00106 NM 2002 3 15 AALA20020143 1 20020130 A 3397 SWITCH BOEING 777 777223 1385213 NM CABIN CONTAMINATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 758AN 32637 EZE - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FLASH CONTINUOUSLY UNLESS TEST SWITCH IS HELD IN AT FLIGHT ATT ENDANTS STATION. REMOVED AND CLEANED DEBRIS FROM EMERGENCY LIGHTS TEST SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002031500107 20020315 00107 NM 2002 3 15 AALA20020144 1 20020210 A 3350 S283T0143 BATTERY PACK BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY ESCA PE PATH LIGHTS BATTERY PACK. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002031500108 20020315 00108 NM 2002 3 15 2002UALA00340 1 20020301 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 STATION 1681 TOP OF AFT PRESSURE DECK RBL 12 TO LBL 4 HAS AREAS OF CORROSION. MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTA LLED OVER PRESSURE DECK. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031500109 20020315 00109 WP 2002 3 15 AALA20020146 1 20020214 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 490AA 49683 TUL - FOUND EMERGENCY EXIT LIGHTS IN CEILING AT STATION 1298 AND STATION 1336 INOPERATIVE. INSTALLED SERVICEABLE BATTER Y PACK B5-27 AT STATION 1322R PER AMM 33-53-00-4, WORK ACCOMPLISHED ON E584135314. (M) 2 L 7 2 4F A6WE 2002031500110 20020315 00110 WP 2002 3 15 AALA20020662 1 20020104 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 429AA 49341 TUL - FOUND CORROSION AT AFT CARGO DOOR LOWER SILL FRAME, BETWEEN STATION 1155-1212. REMOVED AND REPLACED CARGO DOOR BE AM PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002031500111 20020315 00111 NM 2002 3 15 2002UALA00343 1 20020304 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 CABIN FLOORBEAM STATION 986 RBL 43 UPPER CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLOORBEAM UPPER CAP REP AIR ANGLE AND STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032500051 20020325 00051 NM 2002 3 25 2002UALA00344 1 20020301 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN CONTAMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 BOTH SIDES SEAT AISLE EEL LIGHTS INOP IN B-ZONE. CLEANED WATER FROM SIDEWALL EEL LIGHTS CONNECTIONS AND REINSTALLED. O PS CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032500052 20020325 00052 NM 2002 3 25 2002UALA00345 1 20020301 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 DOOR 2 LEFT EMERGENCY LIGHT ON UPPER BUSTLE IS INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002031500114 20020315 00114 NM 2002 3 15 2002UALA00346 1 20020301 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 ROW 22 LEFT SIDE EMERGENCY CEILING LIGHT IS INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002031900169 20020319 00169 NM 2002 3 19 2002UALA00347 1 20020301 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 SEAT 5A AFT EEL LIGHT ELEMENT INOP. REPAIRED EEL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002031500117 20020315 00117 NM 2002 3 15 ASAA0270001 1 20020106 A 5610 ROLLER BOEING 737 737790 13844CN NM COCKPIT WINDOW LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 626AS 3403 30793 ANC - DURING PREFLIGHT, THE FIRST OFFICERS SLIDING WINDOW HARD TO CLOSE. TIGHTENED FORWARD HINGE ROLLER ASSEMBLY. SLID ING WINDOW OPERATES NORMALLY. (M) 2 L 7 2 4F RT A16WE 2002031500118 20020315 00118 WP 2002 3 15 ABXA010762 1 20020312 A 2120 ODOR DOUG DC9 DC941 302207N WP CABIN DETECTED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 977AX 47513 THROUGH 10,000 FT, 10 - 15 SECONDS AFTER EXTENDING WING LANDING LIGHTS THERE WAS A VERY NOTICEABLE ELECTRICAL BURNING OD OR THAT LASTED 30 SECONDS TO 1 MIN, THEN DISSIPATED AND DID NOT RECUR. ALL ELECTRICAL INDICATIONS WERE NORMAL. EXTENDE D THE LIGHT AGAIN IN CHOCKS AFTER LANDING WITH NO ODOR. PERFORMED OPERATIONAL CHECK OF LT AND RT WING LANDING LIGHTS. INSPECTED LT AND RT WING LANDING LIGHT SWITCHES. INSPECTED WIRES FROM LANDING LIGHT SWITCHES TO BEHIND THE INSTRUMENT P ANEL AND ALL INTERIOR LIGHTING AND BALLASTS. CHECKED EMERGENCY INVERTER, LT & RT WING LANDING LIGHT ASSY. OPERATED WIN G LANDING LIGHTS AS WELL AS ALL OTHER EXTERIOR LIGHTS AND INTERIOR LIGHTS NUMEROUS TIMES. NO DEFECTS OR ODORS NOTED. 2 L 7 2 4F A6WE 2002031500119 20020315 00119 WP 2002 3 15 ASAA0280003 1 20020108 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 OAK - DURING C-CHECK, FOUND CORROSION AROUND FASTENERS ON LONGERON 30 FROM FUSELAGE STATION 1003 TO 1070 IN AFT CARGO BA Y. REMOVED DAMAGED SECTION. SPLICED IN NEW SECTION PER EA 5310-02049. (M) 2 L 7 2 4F RT A6WE 2002031500122 20020315 00122 EA 2002 3 15 ASOA02020 1 20020113 A 2613 356124310 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT ENGINE MALFUNCTIONED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 871AS 7537 873072 FLT 4579 - DURING CLIMB-OUT OF TOL, THE LEFT 14TH DUCT LIGHT ILLUMINATED ALONG WITH AN ASSOCIATED AURAL BLEED AIR DUCT M ESSAGE. THESE WARNINGS LASTED 1-2 SECONDS AND THEN WENT AWAY BUT CONTINUED TO INTERMITTENTLY REAPPEAR. AFTER THE PILOT HAD TRIED TO RETARD THE THRUST LEVER IN ORDER TO ELMINATE THE WARNINGS, THE WARNINGS APPEARED AND WOULD NOT STOP. THE CAPTAIN SECURED THE ENGINE AND DECLARED AN EMERGENCY. THE AIRCRAFT DIVERTED TO CVG FOR A SAFE LANDING. MAINTENANCE REM OVED AND REPLACED THE LEFT 14TH DUCT SENSING ELEMENT IN THE LEFT ENGINE PYLON. THE ENGINES WRE RAN FOR 30 MINUTES AND N O FAULTS APPEARED. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2002031500123 20020315 00123 EU 2002 3 15 AWXA200200213 1 20020312 A 5512 D5518313000401 SKIN AIRBUS 320 A320232 3930326 EU HORIZ STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 667AW 1710 DURING PREFLIGHT WALK AROUND A DENT WAS DISCOVERED ON THE LEADING EDGE OF THE OUTBOARD TIP ASSEMBLY OF THE LT TRIMABLE H ORIZONTAL STABILIZER. 2 L 7 2 4F RT A28NM 2002031500124 20020315 00124 NM 2002 3 15 AWXA200200214 1 20020224 A 5320 BAC14902760 INTERCOSTAL BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 LCQ - MAJOR REPAIR - C - DURING C-14 CHECK CORROSION AND A CRACK WAS FOUND ON THE UPPER INTERCOSTAL AT BS 346, LBL 10. 2 L 7 2 4F RT A16WE 2002031500125 20020315 00125 NM 2002 3 15 AWXA200200215 1 20020216 A 5320 6577488226 FLOOR SUPPORT BOEING 737 737277 1384570 NM FUSELAGE BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 LCQ - MAJOR REPAIR - C - DURING C-14 CHECK MAINTENANCE FOUND CORROSION AND A BROKEN SECTION OF CABIN FLOOR SUPPORT ANGLE AT BS 307, LBL 10 - LBL 20. 2 L 7 2 4F RT A16WE 2002031500126 20020315 00126 EU 2002 3 15 C2XA02BT009 1 20020312 A 3320 EO33601 SOCKET AEROSP ATR42 ATR42320 8680930 EU CABIN BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 86842 286 SYR/BTV -CO3551, CREW REPORTED STRONG ELECTRICAL SMELL IN COCKPIT, THEN DISSIPATED. MAINTENANCE DISPATCHED TO SYR, RAN ENGINES AT ALL POWER SETTINGS, CYCLED PACKS AND SMELL DISSIPATED. COULD NOT DUPLICATE PROBLEM. AIRCRAFT RELEASED FOR S ERVICE. DURING LINE CHECK IN BTV A STRONG ELECTRICAL BURNING SMELL WAS NOTED IN AFT CABIN AREA. BTV MAINTENANCE FOUND, REMOVED AND REPLACED BURNT LATERAL LIGHT SOCKET AT SEAT 9D IAW ATR42 STANDARD PRACTICES. OPS CHECKED SYSTEM GOOD. AIR CRAFT RELEASED FOR SERVICE. 2 H 7 2 4T RT A53EU 2002031500127 20020315 00127 SO 2002 3 15 C2XA02IA059 1 20020310 A 3230 23092900001 UPLOCK EMB 145 EMB145LR 3260212 SO NLG FAULTY A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 16951 9137 9137 145063 EWR - FLT 3536 - CREW REPORTED THAT THE NOSE LANDING GEAR DID NOT RETRACT WHEN THE GEAR HANDLE WAS SELECTED UP. THE CRE W RECYCLED THE GEAR HANDLE AND THE NOSE GEAR RETRACTED. THE AIRCRAFT LANDED AT EWR WITHOUT FURTHER INCIDENT WHERE MAINT ENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK BOX. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RE TURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002120300070 20021203 00070 EA 2002 12 3 ASOA02021 1 20020113 A 3246 5010572 BEARING CNDAIR CL600 CL6002B19 1900309 EA LT MLG SEIZED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 883AS 7504 POST FLIGHT INSP, CREW REPORTED, LT OUTBOARD TIRE ASSEMBLY MISSING. THE LANDING INTO HPN WAS SMOOTH WITH NO VIBRATIONS. THE ASSEMBLY WAS RECOVERED ON ATL AIRPORT PROPERTY. MAINTENANCE R&R THE MLG AXLE ASSEMBLY, LT OUTBOARD BRAKE ASSEMBLY , AND THE LT INBOARD AND OUTBOARD WHEEL ASSEMBLIES. PERFORMED A GEAR SWING AND INSP THE LT MLG PIVOT POINTS. NO DEFECT S NOTED. BASED ON THE TEAR DOWN ANALYSIS, IT WAS CONCLUDED THE POSSIBLE CAUSE WAS DUE TO A SECOND INNER BEARING SEAL BE ING TRAPPED BETWEEN THE WHEEL AND THE AXLE SPACER. THE INNER FACE OF THE METAL PORTION HAD IMPRESSIONS AND SURFACE DEFO RMATIONS THAT SUGGEST CONTACT BETWEEN THE SEAT AND THE BRAKE ATTACHMENT BOLTS. (M) 2 L 7 2 4F RT A21EA 2002031500129 20020315 00129 NM 2002 3 15 CALA0200129 1 20020313 A 3397 GROUND WIRE BOEING 737 7373T0 1384582 NM CABIN UNSECURE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 61304 23355 THE RIGHT WING EMERGENCY EXIT SIGN WOULD NOT TEST. MAINTENANCE FOUND LIGHT ASSEMBLY GROUND WIRE NOT SECURED TO GROUND S TUD. TIGHTENED LOCKING NUT AND OPERATION OF THE LIGHT CHECKED GOOD. 2 L 7 2 4F RT A16WE 2002031500130 20020315 00130 EU 2002 3 15 MALA020196 1 20020311 A 3230 801801 UPLOCK SENSOR BAC 146 AVRO146RJ85A 1500097 EU A MALA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 15 510XJ E2323 ON TAKEOFF OF FLIGHT #3550, LH GEAR RED INTRANSIT LIGHT STAYS ON AFTER GEAR RETRACTION. MAINTENANCE REMOVED AND REPLACE D LH GEAR UPLOCK SENSOR (GJ13) IAW AMM 32-60-17. PN ON AND OFF 8-018-01. OPS CHECKS GOOD. 2 H 7 4 4F RT A49EU 2002031500131 20020315 00131 SO 2002 3 15 CHQ000999 1 20020312 A 3320 SOCKET EMB 145 EMB145 3260210 SO CABIN SHORTED A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 11 273 145331 SMELL OF ELECTRICAL SMOKE IN THE AFT CABIN, TRACE AMOUNTS OF SMOKE COMING FROM ABOVE 17A. DEFERRED SIDEWALL LIGHTS, FIX TURE WAS SHORTING OUT. 2 L 7 2 4F RT T00011AT 2002031500133 20020315 00133 NM 2002 3 15 QXEA0200412 1 20020306 A 5610 17180003 WINDOW DHAV DHC8 DHC8202 2809007 NM COCKPIT BROKEN A QXEA A UNSCHED LANDING O OTHER UK UNKNOWN 1 NM 09 353PH 10561 496 PDX - AIRCRAFT RETURNED TO FIELD WHEN THE CAPTAINS SIDE WINDOW BECAME DELAMINATED AND BROKE IN FLIGHT. MAINTENANCE REPL ACED CAPTAINS SIDE WINDOW AND PERFORMED OPERATIONAL CHECK. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031500134 20020315 00134 SO 2002 3 15 ASOA02024 1 20020115 A 2150 311489201 VALVE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE A/C PACK INOPERATIVE A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 264AS 120165 FLT 4299 - DURING FLIGHT FROM ATL TO FLO, THE FLIGHT ATTENDANT REPORTED THERE WERE FUMES IN THE CABIN. THE PILOT TURNED OFF THE RIGHT PACK, BUT THAT DID NOT HELP. AIRCRAFT RETURNED TO ATL FOR A SAFE LANDING. MAINTENANCE REMOVED AND REPLA CED THE RIGHT ENGINE P2.5 SWITCHING VALVE. THIS VALVE BEING INOPERATIVE CAN ALLOW OIL FUMES TO FLOW INTO THE CABIN. OP ERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 2002031500135 20020315 00135 EU 2002 3 15 ASOA02025 1 20020115 A 5410 S541122000000 ACCESS PANEL AEROSP ATR72 ATR72 EU RT ENGINE BROKEN A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING D J INFLIGHT SEPARATION WARNING INDICATION CL CLIMB 1 SO 11 640AS 405 FLT 4318 - DURING CLIMB-OUT OF ATL, PASSING 500 FEET THE PILOT FELT A NOTICEABLE RHYTHMIC VIBRATION. AFTER PASSING 2000 FEET THE PILOT INCREASE THE AIRSPEED AND THE VIBRATION SUBSIDED. A PASSENGER RELAYED TO THE CREW THAT ONE OF THE ACCES S PANELS ON THE RIGHT ENGINE NACELLE WAS OPEN. THE DECISION WAS MADE TO RETURN TO ATL. AS THE AIRCRAFT TURNED A FIRE W ARNING WAS RECEIVED FOR THE RIGHT ENGINE. THE ENGIEN WAS SHUTDOWN PER QRH. AS THE PROPELLER FEATHERED THE FIRE WARNING STOPPED. AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY IN ATL. UPON POST FLIGHT INSPECTION THE CREW NOTED THE NA CELLE PANEL HAD COME OFF. MAINTENANCE WILL REPLACE THE MISSING RIGHT ENGINE NACELLE PANEL AND A BROKEN COWLING LATCH BR 2 H 7 2 4T RT 2002031500136 20020315 00136 SO 2002 3 15 ASOA02045 1 20020122 A 3397 M2275941249 WIRE EMB 120 EMB120RT 3260202 SO CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 269AS 120210 DURING GROUND INSPECTION IN ATL, THE AFT SECTION OF FLOOR LEVEL EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE TERMINAL UNDER SEAT 8A. THE BROKEN TERMINAL AND ASSOCIATED WIRE WERE REPAIRED BY MAINTENANCE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002031500137 20020315 00137 EA 2002 3 15 QXEA0200413 1 20020307 A 3234 533405 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A QXEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 09 604QX 487 10019 SJC - ON VFR APPROACH, THE LANDING GEAR HANDLE WAS LOWERED BUT THE GEAR INDICATED UP. THE APPROACH WAS ABORTED AND THE EMERGENCY/ABNORMAL CHECKLIST WAS RUN. THE GEAR WAS LOWERED USING THE MANUAL GEAR EXTENSION AND THE LANDING WAS NORMAL A ND UNEVENTFUL. MAINTENANCE REPLACED THE MAIN LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F RT A21EA 2002031500138 20020315 00138 EA 2002 3 15 QXEA0200453 1 20020308 A 2820 SWITCH CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FAULTY A QXEA K NONE J WARNING INDICATION CL CLIMB 1 NM 09 601QX 10009 PDX- ON CLIMBOUT HAD 230 POUNDS OF FUEL IN CENTER TANK WITH TRANSFER SYSTEM ACTIVE. FUEL LEVEL IN CENTER TANK DECREASED TO 90 POUNDS. LEFT HAND WING FUEL QUANTITY APPEARED TO INCREASE. BOOST PUMPS CYCLED ON AT FLIGHT LEVEL 410 AND REMAIN ED ON FOR SEVERAL MINUTES. THRUST LEVER POSITION (ADVANCING) HAD NO AFFECT. RIGHT HAND PRIMARY EJECTOR LIGHT FLASHED A MBER ONE TIME. MAINTENANCE REMOVED AND REPLACED RIGHT HAND BOOST PUMP SWITCH. OPERATIONAL CHECK IS GOOD. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002031500139 20020315 00139 EU 2002 3 15 QXEA0200454 1 20020307 A 4990 APU FOKKER F28 F28MK4000 4990810 EU APU BAY LEAKING A QXEA K NONE K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 498US 11181 SEA- SMELLED SMOKE IN THE CABIN WHEN BOARDING THE AIRCRAFT. LAVATORY SMOKE DETECTOR WENT OFF. UPON INSPECTION, FOUND A PU ALLOWING OIL INTO BLEED SYSTEM. COMPLIED WITH BLEED AIR SYSTEM CHECK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002031500140 20020315 00140 SO 2002 3 15 ASOA02055 1 20020124 A 5320 12005805003 STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 16 AND 21. MAINTENANCE REMOVE D AND REPLACED THE CORRODED SECTION OF BUTT STRAP IAW SRM 51-40-02 AND ASA EO 120-53-0173. (M) 2 L 7 2 4T RT A31SO 2002031500141 20020315 00141 SO 2002 3 15 ASOA02056 1 20020124 A 5347 12026865001 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE AFT RIGHT SEAT TRACK HAD CORROSION FROM FRAME 34 TO 40. MAINTENANCE REMOVED THE R IGHT AFT SEAT TRACK FROM FRAMES 34 TO 40 IAW SRM 51-40-02. A NEW TRACK WAS FABRICATED AND MADE READY FOR INSTALLATION I AW SRM 51-25-00 AND SRM 51-21-02. THE NEW SEAT TRACK WAS INSTALLED IAW THE MM 53-01-05. (M) 2 L 7 2 4T RT A31SO 2002031500142 20020315 00142 EA 2002 3 15 QXEA0200455 1 20020310 A 3260 895302 PSEU CNDAIR CL600 CL6002C10 1390015 EA LANDING GEAR MALFUNCTIONED A QXEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 NM 09 604QX 505 10019 BOI - GEAR DID NOT RETRACT DURING MISSED APPROACH. WHEN GEAR SELECTED UP THERE WAS AN IMMEDIATE GEAR DISAGREE WARNING M ESSAGE. THE GEAR INDICATORS SHOWED THREE GREEN AT ALL TIMES. COMPLIED WITH THE EMERGENCY CHECK LIST AND LANDED WITHOUT INCIDENT. REPLACED PSEU. PERFORMED OPERATIONAL TEST OF LANDING GEAR EXTENSION/RETRACTION. OPERATIONAL CHECK GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002031500143 20020315 00143 EU 2002 3 15 RAIA00203091 1 20020303 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 570HK 41089 5487-STL- EMERGENCY PATH LIGHTING OUT AT SEATS 3, 4, AND 5. RESECURED PATH LIGHT ELECTRICAL CONNECTION, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002031500144 20020315 00144 2002 3 15 SABA020021 4 20020214 A 2210 WARNING SYSTEM DHAV DHC8 DHC8102 2809003 NM AUTOPILOT SYS FALSE ACTIVATION A SABA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 33 882CC 168 AIRCRAFT 882 ON FLIGHT 5012 CLT TO TLH. AUTOPILOT DISENGAGE LIGHT STARTED BLINKING AND WOULD NOT STOP. AUTOPILOT SYSTE M WAS DEFERRED UNTIL AIRCRAFT RETURNED TO CLT. MAINTENANCE IN CLT PERFORMED A SELF TEST OF THE AUTOPILOT SYSTEM. SYSTE M TESTED NORMAL. NO PROBLEMS WERE FOUND IN THE AUTOPILOT SYSTEM.A 2 H 7 2 4T RT A13NM 2002031500145 20020315 00145 NM 2002 3 15 SABA020024 1 20020220 A 3350 SOCKET DHAV DHC8 DHC8102 2809003 NM EXTERIOR DIRTY A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 AIRCRAFT 883 ON FLIGHT 5057 TLH TO CLT. DURING PREFLIGHT THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. M AINTENANCE CLEANED THE RIGHT FORWARD EMERGENCY LIGHT SOCK, OPS CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031500148 20020315 00148 SO 2002 3 15 C2XA02CL077 1 20020315 A 2910 156221 SWITCH EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA B EMER. DESCENT K FLUID LOSS CR CRUISE 1 SW 27 14952 9087 145067 CLE FLIGHT#3232 THE CREW REPORTED #1 HYDRAULIC SYSTEM FAILED IN FLIGHT.THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE #1 HYDRAULIC SYSTEM PRESSURE SWITCH HAD CRACKED.THE SWITCH WAS REPLACED.OPO ERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002031500149 20020315 00149 EU 2002 3 15 SABA020029 1 20020228 A 3240 FITTING BAG JETSTM JETSTM3201 1500217 EU LT MLG LOOSE A SABA K NONE K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 33 964AE 964 AIRCRAFT 964 ON FLIGHT 5214 FROM LEX TO CLT. DURING LANDING AT CLT THE LEFT BRAKE FAILED. NO APPLIED BRAKE PRESSURE WA S INDICATED ON THE LEFT SIDE. NO EMERGENCY WAS DECLARED. AIRCRAFT CONTINUED THE LANDING ROLL-OUT AND TAXIED TO THE GAT E WITH NO OTHER PROBLEMS. MAINTENANCE SERVICED THE LEFT BRAKE MASTER CYLINDER AND TIGHTENED LEAKING FITTINGS ON BRAKE C ONTROL VALVE. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2002031500150 20020315 00150 NM 2002 3 15 SABA020030 1 20020228 A 3397 WIRE DHAV DHC8 DHC8103 1386005 NM CABIN OUT OF POSITION A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 801WP 086 AIRCRAFT 801 ON FLIGHT 8680 FROM CLT TO FAY. DURING PREFLIGHT INSPECTION THE CABIN FLOOR EMERGENCY WERE FOUND INOPERATI VE. MAINTENANCE REPOSITIONED WIRING. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031500151 20020315 00151 NM 2002 3 15 SABA020031 1 20020301 A 3350 1013075 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 841PH 082 AIRCRAFT 841 ON FLIGHT 5025 FROM CLT TO TLH. DURING PREFLIGHT FOR FIRST FLIGHT OF THE DAY, THE NR 2 OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB IN THE NR 2 OVERHEAD EMERGENCY LIGHT. SYSTEM OPS CHEC KED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031500152 20020315 00152 NM 2002 3 15 SABA020033 1 20020307 A 3231 54C546349 SEQUENCE VALVE DHAV DHC8 DHC8102 2809003 NM NLG MALFUNCTIONED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 882CC 168 AIRCRAFT 882 ON FLIGHT 5027 FROM CLT TO CVG. AFTER TAKEOFF WHEN THE LANDING GEAR WAS RETRACTED THE NOSE GEAR DOOR WARNI NG LIGHT REMAINED ON. THE GEAR WAS EXTENDED AND THE AIRCRAFT RETURNED TO CLT. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. NO EMERGENCY WAS DECLARED. MAINTENANCE ADJUSTED THE NOSE GEAR DOOR ACTUATING CABLE, AND REMOVED AND REPLACED THE NOSE GEAR HYDRAULIC SEQUENCING VALVE. AIRCRAFT WAS JACKED AND A GEAR RETRACTION CHECK AND ALTERNATE GEAR RELEASE CHECK AS RE QUIRED WITH THE CABLE ADJUSTMENT WAS PERFORMED. ALL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031500154 20020315 00154 NM 2002 3 15 SWAA020335 1 20020213 A 3350 610478 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002031500155 20020315 00155 2002 3 15 SWAA020336 4 20020213 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002031500156 20020315 00156 SO 2002 3 15 ASOA02057 1 20020124 A 5347 12015995003 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE LEFT FLOOR SEAT TRACK, FORWARD SECTION , WAS FOUND WITH CORROSION BETWEEN FRAMES 1 7 AND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK USING SRM 51-40-02, SRM 51-25-00, SRM 51-21-01, ASA EO 120-25-0007, AND THE MM 53-01-05 AS REF. (M) 2 L 7 2 4T RT A31SO 2002031500157 20020315 00157 SO 2002 3 15 ASOA02058 1 20020124 A 5347 12015997003 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 638AS 120282 DURING C-CHECK INSPECTION IN BNA, THE RIGHT WALL SEAT TRACK, FORWARD SECTION, WAS FOUND WITH CORROSION BETWEEN FRAMES 16 AND 31. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK USING SRM 51-40-02, SRM 51-25-00, SRM 51-21-02, ASA E O 120-25-0007, AND THE MM 53-01-05 AS REF. (M) 2 L 7 2 4T RT A31SO 2002031500158 20020315 00158 2002 3 15 SWAA020337 4 20020212 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 739GB 29275 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002031500159 20020315 00159 EA 2002 3 15 ASOA02059 1 20020125 A 3350 364911 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 864AS 7502 DURING HANGAR INSPECTION IN MCN, THE FORWARD FLOOR TRACK EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE INOPERATIVE FLOOR LIGHTING STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031500160 20020315 00160 EA 2002 3 15 ASOA02060 1 20020128 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FALSE ACTIVATION A ASOA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 854AS 7382 DURING CLIMB-OUT OF SDF, AT APPROXIMATELY 12,000 FEET, THE CAPTAIN RECEIVED A PAX DOOR LATCH CAUTION MESSAGE. AT THIS P OINT THE FLIGHT ATTENDANT PHYSICALLY VERIFIED THAT THE ALIGNMENT MARKS WERE IN THE CORRECT POSITION. THE CAPTAIN THEN R ECEIVED A PAX DOOR WARNING MESSAGE AND AN AURAL DOOR MESSAGE. WHEN THE FLIGHT ATTENDANT WENT TO VERIFY THE ALIGNMENT MA RKS AGAIN, IT WAS DISCOVERED THAT THE TOP TWO CAM LATCHES HAD MOVED AND WERE NO LONGER POSITIONED CORRECTLY. THE AIRCRA FT MADE AN EMEREGNCY DESCENT TO 10,000 FEET WHERE IT LEVELED OFF AND WAS DEPRESSURIZED. AIRCRAFT RETURNED TO SDF AND LA NDED SAFELY BUT OVERWEIGHT. MAINTENANCE PERFORMED AN OVERWEIGHT LANDING INSPECTION AND NO DEFECTS WERE NOTED. MAINTENA 2 L 7 2 4F RT A21EA 2002031500161 20020315 00161 NM 2002 3 15 SWAA020338 1 20020213 A 3350 ADD71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 727SW 27859 DURING SCHEDULED PM CHECK, FOUND EEPLS INOP ROWS 1 TO 4. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002031500162 20020315 00162 EU 2002 3 15 ASOA02061 1 20020127 A 3350 7012210 BULB AEROSP ATR72 ATR72212 8680945 EU CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 637AS 383 FLT 4100 - DURING TAXI INTO ATL, THE FLIGHT ATTENDANT REPORTED THAT THE EMERGENCY EXIT SIGN ABOVE THE AFT JUMPSEAT LIT I NTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE BULB AND CLEANED THE CONNECTIONS. OPERATIONAL CHECKS GOO D. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002031500163 20020315 00163 NM 2002 3 15 SWAA020342 1 20020212 A 2913 887477 PUMP BOEING 737 7373H4 1384600 NM HYD SYSTEM FAULTY A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 620SW 28036 AFTER 30 MIN IN FLT B-ELECTRIC HYD LOW PRESS LIGHT ILLUMINATED, WOULD NOT EXTINGUISH. FOUND B-PUMP WIRING BAD. REMOVED AND REPLACED PUMP PER MM. 2 L 7 2 4F RT A16WE 2002031500164 20020315 00164 SO 2002 3 15 ASOA02062 1 20020128 A 5753 12026501001 SUPPORT BRACKET EMB 120 EMB120RT 3260202 SO TE FLAPS CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 238AS 120053 DURING HANGAR MAINTENANCE IN TXK, THE LEFT FLAP SUPPORT BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLAC ED THE CRACKED FLAP SUPPORT BRACKET IAW SRM 57-50-07. (M) 2 L 7 2 4T RT A31SO 2002031500165 20020315 00165 EA 2002 3 15 ASOA02064 1 20020130 A 3350 487190 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 873AS 7549 DURING GROUND INSPECTION IN ATL, THE CAPTAIN REPORTED ONE SECTION OF FLOOR EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENA NCE CLEANED THE CONNECTORS TO THE INOPERATIVE SECTION OF EMERGENCY FLOOR LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT O K FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031500166 20020315 00166 EA 2002 3 15 ASOA02065 1 20020130 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA CABIN CONTAMINATED A ASOA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 11 857AS 7411 ON FINAL APPROACH INTO ATL, SHORTLY AFTER APU START UP, THE 'SMOKE TOILET' MESSAGE ILLUMINATED. THE CAPTAIN IMMEDIATELY SHUT DOWN THE APU AND TRANSFERRED THE BLEEDS BACK TO THE ENGINE. THE MESSAGE EXTINGUISHED. THE FLIGHT ATTENDANT REPOR TED A SLIGHT BUILD UP OF SMOKY HAZE IN THE CABIN THE QUICKLY DISSIPATED ON LANDING. AIRCRAFT LANDED SAFELY IN ATL. MAI NTENANCE REMOVED AND REPLACED THE LEFT COALESCER SOCK AND DUCT TEMPERATURE SENSOR. OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031500167 20020315 00167 EA 2002 3 15 ASOA02070 1 20020205 A 3230 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG WW MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 833AS 7246 FLT 4749 - ON FINAL APPROACH INTO DFW, THE NOSE GEAR EXTENDED NORMALLY, BUT THE MLG WOULD NOT. THE CAPTAIN PERFORMED AN EMERGENCY GEAR EXTENSION AND THE GEAR CAME DOWN AT THAT TIME AND ALL GEAR INDICATIONS SHOWED DOWN AND LOCKED. EMERGENC Y EQUIPMENT WAS REQUESTED AND THE AIRCRAFT HAD AN UNEVENTFUL LANDING IN DFW. MAINTENANCE REMOVED AND REPLACED THE MLG S ELECTOR VAVLE. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031500168 20020315 00168 NM 2002 3 15 SWAA020345 1 20020212 A 2780 65C26869 CONTROL VALVE BOEING 737 7377H4 1384404 NM L/E SLAT FAILED A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 709SW 27843 AIR TURNBACK, L/E SLATS WOULD NOT RETRACT AFTER T/O. REMOVED AND REPLACED AUTO SLAT CONTROL VALVE PER MM. 2 L 7 2 4F RT A16WE 2002031500169 20020315 00169 NM 2002 3 15 QXEA0200474 1 20020314 A 5210 HANDLE BOMBDR DHC8 DHC8401 NM DRY A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 405QX 4047 SEA-MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED INTERIOR HANDLE PIVOT. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031500170 20020315 00170 WP 2002 3 15 MWEA020167 1 20020315 A 5310 591143271 LONGERON DOUG DC9 DC932 3022066 WP STATION 1076 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LONGERON 2 RIGHT AT FUSELAGE STATION 1076 CRACKED AT END. -- REMOVED AND REPLACED WITH REPAIR, NEW LONGERON SPLICE. 2 L 7 2 4F A6WE 2002031500171 20020315 00171 NM 2002 3 15 UPS02237819 1 20020226 A 5310 STRINGER BOEING 727 72731C 1384011 NM STR 23L BS 740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:C WHILE CARRYING OUT SKIN SPLICE AT L/H BS 740 FITTING STR 23L FOUND T O BE CRACKED STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03 2 L 7 3 4F A3WE 2002031500172 20020315 00172 NM 2002 3 15 UPS02237872 1 20020225 A 5520 SUPPORT FITTING BOEING 727 72731C 1384011 NM ELEV STA 46.50 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:C LH ELEVATOR, STA 46.50, ACTUATOR ATTACH SUPPORT FITTING, CRACK BETWE EN THREE FASTENER HOLES LH EL EVATOR REPLACED. REF. NRC 450554. 2 L 7 3 4F A3WE 2002031500175 20020315 00175 NM 2002 3 15 UPS02237544 1 20020107 A 5753 ATTACH FITTING BOEING 727 727185C 138406N NM FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI ON REMOVAL OF NR 5 FLAP TRACK FWD ATTACH FITTING, PITTING CORROSION FOUND IN UPPER HOLE COMMON TO S PECIAL STUD ON TRUNNION SUPPORT FITTING. 2 L 7 3 4F A3WE 2002031500176 20020315 00176 NM 2002 3 15 UPS02237546 1 20020107 A 5320 SILL BOEING 727 727185C 138406N NM COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C EVIDENCE OF CORROSION ON R3 WINDOW SILL IN CONTROL CABIN (IE) LWR EXTRUDED ANGLE. 2 L 7 3 4F A3WE 2002031500178 20020315 00178 NM 2002 3 15 AWXA200200223 1 20020314 A 3350 BMS13311122 WIRE BOEING 757 7572G7 1384963 NM SEAT 19 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 PHX - EEL - "C" - EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT ROW 19 L/H. MAINTENANCE REPAIRED BROKEN WIRE ON SEAT 19 L/H, FUNCTIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002031500180 20020315 00180 NM 2002 3 15 UPS02237553 1 20020115 A 5720 65162271 CHANNEL BOEING 727 727185C 138406N NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI CHANNEL ON LT WING REAR SPAR O/B OF NR 1 SPOILER CRACKED. 2 L 7 3 4F A3WE 2002031500181 20020315 00181 NM 2002 3 15 UPS02237566 1 20020204 A 3350 LIGHT BOEING 727 72751C 1384015 NM CABIN DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE:N/A L1 DOOR EMERGENCY EXIT LIGHT COMES ON DIM AND GOES OUT IN LESS THAN A MINUTE. REMOVED AND REPLACED L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY SYSTEM, GROUND CHECKS GOOD. 2 L 7 3 4F A3WE 2002031500182 20020315 00182 NM 2002 3 15 UPS02237587 1 20020114 A 2550 6549398725 HOUSING BOEING 727 727185C 138406N NM CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:C+SI ON CLEANING OF 9G NET FITTINGS, FLOOR MOUNTED HOUSINGS X2 WERE FOUND TO BE CRACKED. HOUSING REPLAC ED IAW SRM 51-30-02 AND DWG 65-49366. 2 L 7 3 4F A3WE 2002031500183 20020315 00183 NM 2002 3 15 UPS02237588 1 20020208 A 3397 WIRE BOEING 727 727185C 138406N NM CABIN DAMAGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT ABOVE FORWARD ENTRY DOOR INOP. NO POWER TO PINS 1 AND 5 FOR CHARGING, CORRECT ED WIRING PER WDM 33-5 1-01. REPLACED BATTERIES PER MM 33-51-01 PAGE 201. 2 L 7 3 4F A3WE 2002031500184 20020315 00184 NM 2002 3 15 UPS02237609 1 20020212 A 2450 902F2425 CONTROL PANEL BOEING 727 72725C 138400H NM COCKPIT MALFUNCTIONED A IPXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 948UP 19357 INSPECTION TYPE:N/A AIR TURNBACK DUE TO SMOKE IN COCKPIT SMELLED SMOKE CLIMBING THROUGH 4000 FT THEN WENT AWAY UNTIL CRE W SAW SMOKE AND SMELLED HEAVY ELECTRICAL SMELL AFTER BLOCK IN WITH EXTERNAL POWER CONNECTED. INSPECTED BEHIND PANELS OF F/E PANEL. REMOVED AND REPLACED VOLTAGE REGULATOR, GENERATOR CONTROL PANEL, PERFORMED ADJ TEST PER MM 24-20-00, PERFOR MED HIGH POWER RUN. NO SMOKE, NO FAULTS. 2 L 7 3 4F A3WE 2002031500185 20020315 00185 NM 2002 3 15 UPS02237610 1 20020212 A 5270 SWITCH BOEING 727 72730C 1384009 NM MAIN CARGO DOOR OUT OF ADJUST A IPXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 917UP 19310 INSPECTION TYPE:N/A UPON LEVELING AT FLT LEVEL 280 AMBER MAIN CARGO DOOR LIGHT ILLUMINATED, FOLLOWED APPROPRIATE EMERGEN CY PROCEDURES. DESCENDED TO AIRCRAFT ALTITUDE 17,000, CABIN ALTITUDE 7,000. MAIN CARGO DOOR LIGHT WENT OUT. ADJ AFT M AIN CARGO DOOR MICROSWITCH IAW B727-100 M/M 52-70-01 PG 509. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2002031500186 20020315 00186 NM 2002 3 15 UPS02237691 1 20020215 A 3350 LIGHT BOEING 727 72730C 1384009 NM L1 DOOR UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:N/A L1 DOOR EMERGENCY EXIT LIGHT LENS COVER HANGING BY ONE END. FOUND FWD END OF EMERGENCY EXIT LIGHT A SSY NOT SECURED. SECURED LIGHT ASSY AND LENS. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002031500187 20020315 00187 NM 2002 3 15 UPS02237712 1 20020204 A 5320 SUPPORT BOEING 727 72731C 1384011 NM AFT AIRSTAIRS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, AFT AIRSTAIRS ACTUATOR FITTING SUPPORT ANGLE CRACKED IN AFT RT TORQUE BOX AT STA 1273. REPAIRED IAW EO B727-5310-1239. 2 L 7 3 4F A3WE 2002031500188 20020315 00188 EU 2002 3 15 UPS02237744 2 20020301 A 7200 TAY65154 ENGINE BOEING 727 72731C 1384011 NM RROYCE TAY TAY65154 EU NR 3 MALFUNCTIONED A IPXA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 SO 01 922UP 19231 81125 INSPECTION TYPE:N/A NR 3 ENGINE SHUT DOWN IN FLIGHT DUE TO LOW OIL PRESSURE (4 PSI). REPLACED ENGINE NR 3 IAW TC 1273 A ND TC 1276. ENGINE RUN SATISFACTORY. 2 L 7 3 4F 4 F A3WE E25NE 2002031500189 20020315 00189 NM 2002 3 15 UPS02237755 1 20020303 A 3350 1000679 LIGHT BOEING 727 72730C 1384009 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:IN FWD EXIT DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY. OP CHECK GOOD IAW MM 33-50-01. 2 L 7 3 4F A3WE 2002031500190 20020315 00190 NM 2002 3 15 UPS02237794 1 20020207 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CANNING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE:C RT FWD FUSELAGE SKIN HAS OIL CAN, PREVIOUSLY REWORKED BS 340 STR 19R. 2 L 7 3 4F A3WE 2002031500191 20020315 00191 NM 2002 3 15 UPS02237795 1 20020207 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE:C UPPER FUSELAGE SKIN HAS BULGE AT BUTT JOINT BS 521 STR 3L - 4R. 2 L 7 3 4F A3WE 2002031500192 20020315 00192 NM 2002 3 15 UPS02237797 1 20020207 A 5320 ANGLE BOEING 727 72725C 138400H NM FUSELAGE BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE:C LT AFT NOSE W/W DOOR CUTOUT HAS BULGE FASTENERS PULLING OFF BS 320 TO BS 350. REPLACED LEFT LOWER CHO RD ANGLE AT NWW AREA IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2002031500195 20020315 00195 NM 2002 3 15 UPS02437394 1 20020106 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:PFLT EMERGENCY LIGHT OVER UPPER DECK STAIRS INOP. RELAMPED, CHECKS GOOD. 2 L 7 4 4F A20WE 2002031500196 20020315 00196 NM 2002 3 15 UPS02437412 1 20020116 A 5714 ANGLE BOEING 747 747123F NM WING BOX CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:SP STA 1140 ON RT SIDE UNDERNEATH SECOND FLOOR PNL, I/B AND BENEATH DUCTING A 2 INCH CRACK WAS FOUND AND CORROSION ON CTR WING BOX. 2 L 7 4 4F A20WE 2002031500197 20020315 00197 NM 2002 3 15 UPS02437421 1 20020118 A 5314 KEELBEAM BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:SP, THREE CRACKS IN LT WHEEL WELL, LOWER KEEL BEAM AREA SURROUNDING STRUCTURE. REPAIRED AREA IAW SRM 53 -10-09 FIG 1. 2 L 7 4 4F A20WE 2002031500198 20020315 00198 NM 2002 3 15 UPS02437440 1 20020120 A 3350 LIGHT BOEING 747 747200 1384847 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 528UP INSPECTION TYPE:N/A EMERGENCY LIGHT IN CEILING NEAR FWD ENTRY DOOR INOP. RELAMPED, OPS CHECK OK. 2 L 7 4 4F RT A20WE 2002031500199 20020315 00199 NM 2002 3 15 UPS02437515 1 20020127 A 3350 LIGHT BOEING 747 747123 1384873 NM MAIN CARGO BAY INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:N/A EMERGENCY LIGHT MAIN CARGO CEILING FWD OF STAIRS INOP. RELAMPED MAIN CARGO CEILING LIGHT. 2 L 7 4 4F A20WE 2002031500200 20020315 00200 NM 2002 3 15 UPS02437552 1 20020131 A 3350 POWER SUPPLY BOEING 747 747123 1384873 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:PFLT EMERGENCY EXIT SIGN OVER CREW SERVICE DOOR INOP. REMOVED AND REPLACED POWER SUPPLY MODULE M312 IAW B747 MM 33-51-04, OPS CHECK GOOD. 2 L 7 4 4F A20WE 2002031500201 20020315 00201 NM 2002 3 15 UPS02437557 1 20020202 A 3350 BATTERY PACK BOEING 747 747121 1384871 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS OVER ESCAPE SLIDE DOOR INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY PER AM M 33-51-04. OPS CHECKS GOOD. 2 L 7 4 4F A20WE 2002031500202 20020315 00202 NM 2002 3 15 UPS02437558 1 20020203 A 3350 LIGHT BOEING 747 747200 1384847 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 528UP INSPECTION TYPE:N/A MAIN CABIN EMERGENCY LIGHT NEXT TO CREW LADDER INOP. REMOVED AND REPLACED BOTH BULBS, OPS CHECKS GO OD. 2 L 7 4 4F RT A20WE 2002031500203 20020315 00203 NM 2002 3 15 UPS02437561 1 20020128 A 5320 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C CRACK REVEALED ON LEFT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING AT HOLE NR 5 BY APPROX 0.030 IN LON G. 2 L 7 4 4F A20WE 2002031500204 20020315 00204 NM 2002 3 15 UPS02437562 1 20020128 A 5320 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C CRACK AND CORROSION REVEALED ON RIGHT BS 1480 BULKHEAD EXTENSION FITTING AT HOLE NR 9. 2 L 7 4 4F A20WE 2002031500205 20020315 00205 NM 2002 3 15 UPS02437563 1 20020124 A 2520 PANEL BOEING 747 747123 1384873 NM CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - R2 DOOR CUTOUT FWD LOWER REVEAL FOUND CRACKED. LOWER REVEAL REPAIRED AS PER SRM 53-10-04 FIG 84 . 2 L 7 4 4F A20WE 2002031500206 20020315 00206 NM 2002 3 15 UPS02437570 1 20020204 A 3350 LIGHT BOEING 747 747121 1384871 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:N/A EMERGENCY LIGHTS UNARMED ANNUNCIATOR WILL NOT ILLUMINATE. RELAMPED UNARMED ANNUNCIATOR LIGHT, OPS C HECK GOOD. 2 L 7 4 4F A20WE 2002031500207 20020315 00207 NM 2002 3 15 UPS02437571 1 20020124 A 5320 65B104212 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 1265 CANTED BULKHEAD BL 0 SPLICE FOUND CRACKED. SPLICE REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002031500208 20020315 00208 NM 2002 3 15 UPS02437572 1 20020125 A 5315 AMS490100401N FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 220 RBL 57 FLOORBEAM SURFACE CORRODED. FLOORBEAM UPPER CAP REPAIRED AS PER SRM 53-10-07 FIG 10. 2 L 7 4 4F A20WE 2002031500209 20020315 00209 NM 2002 3 15 UPS02437573 1 20020125 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 360 RBL 92 FLOORBEAM WEB CRACKED. BS 360 MOST RT O/B WEB REPAIRED AS PER SRM 53-10-07 FIG 11 . 2 L 7 4 4F A20WE 2002031500210 20020315 00210 NM 2002 3 15 UPS02437574 1 20020127 A 5310 SHEAR TIE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C FWD CARGO COMPT, S-43L TO S-44L BS 760 FLOORBEAM SHEAR TIE CORROSION CRACKED. SHEAR TIE REPAIRED AS P ER SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2002031500211 20020315 00211 NM 2002 3 15 UPS02437579 1 20020207 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:IN UPPER DECK EMERGENCY EXIT DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY LIGHT SIGN PER 33-51-02 , NO HELP. REMOVED AND REPLACED CEILING EMERGENCY LIGHT I/B OF SLIDE PER MM 33-51-07, OPS CHECK NORMAL. 2 L 7 4 4F A20WE 2002031500212 20020315 00212 NM 2002 3 15 UPS02437583 1 20020125 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 300 S-13AR FRAME FOUND CRACKED. M/D BS 300 FRAME REPAIRED AS PER RS 53-12-34717. 2 L 7 4 4F A20WE 2002031500213 20020315 00213 NM 2002 3 15 UPS02437584 1 20020207 A 5347 BAC15201566 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 500 RBL 97 SEAT TRACK FLANGE FOUND CORROSION DAMAGED. SEAT TRACK REPLACED AS PER SRM 51-10-0 1. 2 L 7 4 4F A20WE 2002031500214 20020315 00214 NM 2002 3 15 UPS02437597 1 20020129 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C, AFT BULK CARGO S-51R BS 2218 STRINGER CRACKED. STRINGER REPAIR SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002031500215 20020315 00215 NM 2002 3 15 UPS02437600 1 20020125 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 490 RBL 75 SEAT TRACK FLANGE CORRODED. SEAT TRACK REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002031500216 20020315 00216 NM 2002 3 15 UPS02437625 1 20020130 A 5320 SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C NLG W/W LT VERTICAL BEAM WEB MIDDLE AREA 1EA HORIZ SUPPORT ANGLE CRACKED AT STA 390 AREA (ACCESS FROM LT SIDE TUNNEL JUST AFT OF NLG CABLE AREA). SUPPORT ANGLE REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002031500217 20020315 00217 NM 2002 3 15 UPS02437626 1 20020129 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C AFT BULK CARGO, S-50R BS 2210 STRINGER CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002031500218 20020315 00218 NM 2002 3 15 UPS02437631 1 20020126 A 5320 65B07941125 ATTACH ANGLE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 260 LBL 8 AND NOSE WHEEL UPPER SURFACE STIFFENER ATTACH ANGLE CRACK. ATTACH ANGLES (2 EA) RE PLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002031500219 20020315 00219 NM 2002 3 15 UPS02437632 1 20020126 A 5320 65B07941125 ATTACH ANGLE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 260 LBL 10 & 22 NOSE WHEEL UPPER SURFACE STIFFENER ATTACH ANGLE CRACK. ATTACH ANGLES (2 EA) REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002031500220 20020315 00220 NM 2002 3 15 UPS02437633 1 20020126 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 380 S-22L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 85. 2 L 7 4 4F A20WE 2002031500221 20020315 00221 NM 2002 3 15 UPS02437634 1 20020126 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 360 S-18R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 85. 2 L 7 4 4F A20WE 2002031500222 20020315 00222 NM 2002 3 15 UPS02437635 1 20020126 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 1860 RBL 97 SEAT TRACK CROWN FOUND CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002031500223 20020315 00223 NM 2002 3 15 UPS02437636 1 20020126 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 1740 RBL 97 SEAT TRACK CROWN FOUND CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002031500224 20020315 00224 SO 2002 3 15 C2XA02IA062 1 20020312 A 4920 4501968D APU EMB 145 EMB145LR 3260212 SO TAIL LEAKING A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 14977 2768 145175 CLE- AFTER STARTING THE APU AT THE GATE THE CREW NOTED A FUEL SMELL IN THE CABIN. CLE- MAINTENANCE INSPECTED THE APU, AND, THE AIRCRAFT WAS RELEASED IAW MEL. BNA- MAINTENANCE REMOVED AND REPLACED THE APU,PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002031600001 20020316 00001 SO 2002 3 16 C2XA02TY049 1 20020316 A 5320 14522460015 GUSSET EMB 145 EMB145ER 3260211 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13929 145009 TYS, During a scheduled inspection the aft gusset was found corroded. Maintenance removed and replaced the aft gusset. I /A/W-EMB-SRM-51-40-02 and CMP-51-04-00. Repair procedures where satisfactory and the aircraft will be released upon comp lection of inspection. 2 L 7 2 4F RT T00011AT 2002031600002 20020316 00002 SO 2002 3 16 C2XA02TY050 1 20020316 A 5315 14521713003 BEAM EMB 145 EMB145ER 3260211 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13929 145009 TYS, During a scheduled inspection the center omega beam between FR18 and FR24 was found corroded. Maintenance removed a nd replaced the omega beam. I/A/W-EMB-SRM-51-40-02 and 51-21-02. Repair procedures where satisfactory and the aircraft w ill be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002031600003 20020316 00003 SO 2002 3 16 C2XA02TY051 1 20020316 A 2620 14531342403 TUBE EMB 145 EMB145ER 3260211 SO KINKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13929 145009 TYS, During a scheduled inspection the right APU fire extinguisher tube was found damaged. Maintenance removed and repla ced the tube. I/A/W-EMB145MM-20-10-03 and 26-23-05. Repair procedures where satisfactory and the aircraft will be releas ed upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002031600004 20020316 00004 SO 2002 3 16 C2XA02TY053 1 20020316 A 5320 14522459003 ANGLE EMB 145 EMB145ER 3260211 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13929 145009 TYS, During a scheduled inspection the ramp angle on center omega beam has corrosion. Maintenance removed and replaced t he ramp angle. I/A/W-EMB135/14SRM-51-40-02, 51-20-03, 51-40-06 and 51-40-02. Repair procedures where satisfactory and th e aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002031600005 20020316 00005 EU 2002 3 16 C2XA02IA063 1 20020315 A 3260 842503 PSEU AEROSP ATR42 ATR42320 8680930 EU 80 VU RIGHT SIDE INOPERATIVE A C2XA K NONE O OTHER LD LANDING 1 SW 27 14825 170 IAH- DURING FLIGHT 3804,LANDING THE CREW NOTED THAT THE NOSE LANDING GEAR INDICATION WAS FLICKERING. IAH- MAINTENANCE REMOVED AND REPLACED THE PROX SYSTEM ELECTRONICS UNIT,PERFORMED A SELF TEST OF THE NEW UNIT, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002031700001 20020317 00001 EU 2002 3 17 C2XA02IA064 1 20020315 A 3260 D228800001 CONNECTOR AEROSP ATR42 ATR42320 8680930 EU NLG LOOSE A C2XA K NONE J WARNING INDICATION LD LANDING 1 SW 27 97841 280 IAH- PRIOR TO LANDING THE FORWARD PANEL NOSE GEAR UNLOCK LIGHT INTERMITTENT AFTER GEAR EXTENSION, OVERHEAD PANEL OK. I AH- MAINTENANCE INSPECTED THE AIRCREFT, AND, RELEASED THE AIRCRAFT IAW MEL. IAH- MAINTENANCE RESECURED A CONNECTOR, A FTER FINDING THE CONNECTOR LOOSE, NO OTHER DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002031700002 20020317 00002 NE 2002 3 17 S02472004 2 20020227 A 7200 ENGINE PWA BOEING 747 747400 NM PWA 4056 PW4056 NE #1 ENG W SAJF E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 WP 03 727665 24309 B18271 DUE TO #1 ENG VIBRATION HIGH & EGT OVER LIMIT AFT 3 HRS DEPARTED FM BMM, #1ENG SHUT DOWN IN FLT & RETURN TO BKK.C /A:1.INITIAL INVESTIGATION:GROUND CHECK FOUND #4 BEARING PRESS TUBE BROKEN AT 7:00 CLOCK AND EDP PRESS OUTLET B-NUT LOOS EN. 2.INITAL ACTION:RPLD #1 ENG AND RUN UP TEST NORMAL IAW 71-00-02, HYD SYS CHECK AND RPLD FILTER IAW 29-11-23 RETURN F ILTER IAW 29-11-29 2 L 7 4 4F 4 F RT A20WE E24NE 2002031700003 20020317 00003 NM 2002 3 17 EVA200202 1 20020315 A 3320 F027WWBCAC LIGHT BOEING 747 74745E 1384947 NM BURNED W QOCF K NONE O OTHER DE DESCENT 1 WP 03 27141 1.DURING DES (ABOUT 7,000') C/PURSER SMELT SMOKE/OVHT WIRE(ELECT) AT R1 DR. SELECT UTILITY BUS OFF, DECLARE EMERGENCY LA NDING. UNEVENTFUL LANDING.2.ON GND CHECK FOUND 24/25 HK INDIRECT CEILING LIGHT FWD CONNECTOR DAMAGED.3.PER MM REPLACE TH E FLOUSCENT LIGHT AND LIGHT HOLDER. GROUND OPERATION CHECK NML.4.INSPECT THE A ZONE AREA INDIRECT CEILING LIGHT, ALL CON DITION NORMAL. 2 L 7 4 4F RT A20WE 2002031800003 20020318 00003 NM 2002 3 18 2002F00281 1 20020102 A 3411 PITOT TUBE BOEING 757 75723N 1384973 NM PITOT STATIC SYS MALFUNCTIONED A AMTA C D ABORTED TAKEOFF RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 11 514AT 27971 AFTER SELECTING MAXIMUM TAKEOFF POWER, LEFT THROTTLE RETARDED FROM 1.72 TO 1.60, TAKEOFF WAS REJECTED AT 75 KTS. REPLA CED PITOT TUBE ON PF RAKE ON THE NR 1 ENGINE, 9 O'CLOCK POSITION PER ENGINEERING REPAIR AUTHORIZATION 757-72T-4666 (TECH NICAL VARIANCE FROM ROLLS ROYCE). (M) 2 L 7 2 4F RT A2NM 2002031800010 20020318 00010 NM 2002 3 18 02FDEA00201 1 20020314 A 2997 WIRE BOEING 727 727233 138408A NM HYD SYSTEM CHAFED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 25 279FE 22346 HYD A-SYS OVERHEAT LIGHT CAME ON. BOTH PUMPS WERE OFF PER CK LIST. REPEAT WRITEUP. REMOVED AND REPLACED CHAFED WIRE W ITH TEFLON TAPE PER CHAPTER 20 STANDARD PRACTICES. 2 L 7 3 4F RT A3WE 2002032500053 20020325 00053 NM 2002 3 25 2002UALA00348 1 20020301 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 UPPER DECK EMERGENCY CEILING LIGHTS AT ROW S 13 & 17 INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032500054 20020325 00054 NM 2002 3 25 2002UALA00349 1 20020301 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 AFT EEL LIGHT IN CTR UPPER DECK CEILING PANEL INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032500055 20020325 00055 NM 2002 3 25 2002UALA00350 1 20020301 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 DOOR 1 RIGHT AND 4 RIGHT AFT DOOR SILL EEL LIGHTS INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032500056 20020325 00056 NM 2002 3 25 2002UALA00351 1 20020301 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 THE FOLLOWING EEL CEILING LIGHTS INOP ROW 39 RIGHT SIDE, ROW 23 RIGHT SIDE, ABOVE LAV 102. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000016 20020320 00016 NM 2002 3 20 2002UALA00352 1 20020303 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 191UA 26880 FIRST CLASS LEFT SIDE ALL EEL LIGHTS DO NOT COME ON. REPLACED BATTERY, OPS CHECK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000071 20020410 00071 NM 2002 4 10 2002UALA00353 1 20020305 A 5610 141T480014 WINDSHIELD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT CRACKED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 570UA 26678 ACRID SMELL AND SPARKS FROM RIGHT WINDSHIELD HEAT. RIGHT WINDSHIELD CRACKED. MOISTURE INGRESSION OF 1ST OFFICERS WINDS HIELD CAUSED ARCING OF THE HEATING ELEMENT. REPLACED WINDSHIELD ASSY AND WINDOW HEAT CONTROLLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031800012 20020318 00012 EU 2002 3 18 2002F00290 1 20020125 A 7810 L713M2054101 EJECTOR UROCOP EC135 EC135P1 8680990 EU EXHAUST SYS CRACKED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 135N 451 0086 EJECTOR ASSEMBLY CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M) 1 G 7 2 3U O H88EU 2002031800015 20020318 00015 NM 2002 3 18 2002UALA00355 1 20020305 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 STATION 1600, FLOORBEAM CAP RBL 5 TO LBL 18 HAS GOUGES IN AREA OF AFT CABIN. MAJOR REPAIR ACCOMPLISHED. FLOORBEAM DOUB LER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031800016 20020318 00016 NM 2002 3 18 2002UALA00356 1 20020305 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 CABIN CREASE BEAM INNER CHORD LOWER LEG, HAS EXCESSIVE MATERIAL LOSS AT FASTENER HOLE BODY STATION 753, LBL 65, WATERLIN E 208. MAJOR REPAIR ACCOMPLISHED. INNER CHORD REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000027 20020320 00027 NM 2002 3 20 2002UALA00357 1 20020303 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 SEAT 4E, 4F, 4J, & 5J AFT EEL ELEMENT IN SEAT IS INOP. REPLACED LIGHT ASSEMBLIES. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000029 20020320 00029 NM 2002 3 20 2002UALA00358 1 20020303 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EEL AT SEAT 52 ABC IS INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000030 20020320 00030 NM 2002 3 20 2002UALA00359 1 20020303 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EXTERIOR EMERGENCY LIGHT ON RIGHT SIDE 2ND FROM THE FRONT THE AFT BULB IS INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000033 20020320 00033 NM 2002 3 20 2002UALA00361 1 20020303 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 ALL STAIRCASE EEL LIGHTS ARE INOP. SECURED ELEC CONN AT THE TOP OF STAIRCASE. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000035 20020320 00035 NM 2002 3 20 2002UALA00362 1 20020303 A 3350 PIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CONNECTOR BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 AFT EEL LIGHT SEAT 4F IS INOP BECAUSE THE HARNESS THAT IT CONNECTS UP WITH HAS BROKEN PIN ON ITS CONNECTOR. REPAIRED AN D REINSTALLED CONNECTOR. TEST OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000037 20020320 00037 NM 2002 3 20 2002UALA00363 1 20020304 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 192UA 26881 EMERGENCY OVERWING LIGHT 1 EACH LAMP INOP AT RIGHT HAND WING AFT OF FORWARD MOST LIGHT ASSEMBLY. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000038 20020320 00038 NM 2002 3 20 2002UALA00364 1 20020304 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 192UA 26881 EMERGENCY LIGHT INOP LOCATED AT RIGHT FORWARD CLOSET. REPLACED BATTERY, OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000040 20020320 00040 NM 2002 3 20 2002UALA00365 1 20020304 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 192UA 26881 STAIRWAY EMERGENCY LIGHTS INOP. BAD CONNECTION SECURED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000041 20020320 00041 NM 2002 3 20 2002UALA00366 1 20020304 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 192UA 26881 EXTERIOR EMERGENCY LIGHT LEFT SIDE (2ND ASSEMBLY AFT) FORWARD BULB IS INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000045 20020320 00045 NM 2002 3 20 2002UALA00370 1 20020304 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 192UA 26881 AFT EEL LIGHT INOP ON SEAT 5E. SECURED EEL LIGHT ASSY. OPS CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002031800032 20020318 00032 EU 2002 3 18 2002F00310 1 20020112 A 6410 355A12004008 BLADE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR CRACKED B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 438AE 176 3402 TAIL ROTOR BLADE ASSEMBLY CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW, CORRECTED PROBLEM. (M) 1 G 7 1 3U H9EU 2002032000047 20020320 00047 NM 2002 3 20 2002UALA00371 1 20020304 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 192UA 26881 EMERGENCY AISLE LIGHT INOP AT SEATS 2J AFT POSN AND 3A AFT POSN. REPLACED BOTH AISLE EEL LIGHT ASSY, OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000048 20020320 00048 NM 2002 3 20 2002UALA00372 1 20020304 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 192UA 26881 EMERGENCY CEILING LIGHT INOP ABOVE SEATS 16 AND 17 UPPER DECK. REPLACED EMERGENCY BATTERY PACK. OPS TESTED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000049 20020320 00049 NM 2002 3 20 2002UALA00373 1 20020304 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 192UA 26881 EMERGENCY SLIDE LIGHTS INOP AT DR 2L, 4L AND 5R. REPLACED LAMP ASSY AT DOOR 5R AND RELAMP AT DOOR 2L AND 4L. OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000052 20020320 00052 NM 2002 3 20 2002UALA00374 1 20020304 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 192UA 26881 EMERGENCY AISLE LIGHT INOP FROM SEAT 6GH UP TO 8GH. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2002031800035 20020318 00035 NM 2002 3 18 2002UALA00376 1 20020306 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 CABIN AFT PRESSURE DECK HAS EXCESSIVE MATERIAL LOSS AT STATION 1681 RBL 12, STATION 1681 TO 1684 RBL 14 TO RBL 54, STATI ON 1688 RBL 50 AND STATION 1699 RBL 44. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031800040 20020318 00040 NM 2002 3 18 2002UALA00378 1 20020307 A 5751 RIB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE AILERON WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 AT NR 2 AILERON HINGE CASTING, INBOARD SUPPORT RIB LOWER FLANGE, IS WORN IN RADIUS. MAJOR REPAIR ACCOMPLISHED. MANUFAC TURED AND INSTALLED SUPPORT RIB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002031800042 20020318 00042 NM 2002 3 18 2002UALA00379 1 20020307 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 STRINGER 17R CRACKED AT STATION 178, HORIZONTAL FLANGE CRACKED FROM FORWARD HOLE TO INBOARD EDGE OF FLANGE. MAJOR REPAI R ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED REPLACEMENT TEE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002031800044 20020318 00044 NM 2002 3 18 CALA0200133 1 20020316 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 500C CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND A 1/8" CRACK IN STRINGER 16L AND 16R AT FASTENER AREA FWD OF LIGHT ASSEMBLY STA 500C AFT. A REPAIR DOUB LER WAS INSTALLED AT EACH LOCATION IAW SRM 53-00-03, FIGURE 201. 2 L 7 2 4F RT A16WE 2002031800045 20020318 00045 NM 2002 3 18 CALA0200134 1 20020317 A 5551 FITTING BOEING 737 7373T0 1384582 NM HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND TWO R/H FORWARD HORIZONTAL STABILIZER ATTACH FITTINGS HAD LOWER AFT AND FORWARD BUSHINGS CORRODED BETWE EN BUSHING AND LUG. AN OVERSIZED BUSHING WAS INSTALLED AT EACH LOCATION IAW CMM 55-10-10. 2 L 7 2 4F RT A16WE 2002031800046 20020318 00046 SO 2002 3 18 LR7A02026 1 20020314 A 5311 FRAME LKHEED 382 382G 526414U SO FS 792 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING LOG PAGE 08908 ITEM M2 ACCOMPLISHMENT (CARGO IMPACT DAMAGE REPAIR) FOUND SECONDARY DAMAGE RH FS 792 SIDE BULKHEAD FRAME CRACKED AT RLB 67, WL 171.REPAIRED IAW SRM SMP 583 53-50-14 AND LAC MEA 382-53-02-019. GMM133 ITEM M5. 2 H 7 4 4T A1SO 2002031800047 20020318 00047 NM 2002 3 18 2002UALA00380 1 20020307 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 STATION 188 RIGHT HAND FRAME WEB CRACKED AT WL 207. MAJOR REPAIR ACCOMPLISHED. INSTALLED WEB REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002031800048 20020318 00048 SO 2002 3 18 ASOA02072 1 20020206 A 5730 SKIN EMB 120 EMB120ER 3260203 SO WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 505AS 120279 DURING HANGAR MAINTENANCE IN MCN, THE PRESSURE REFUELING POINT WAS FOUND WITH A SKIN CRACK ON THE OUTBOARD AFT CORNER. MAINTENANCE REPAIRED THE CRACKED SKIN IAW ASA EO 120-57-0027. THIS EO REF SRM 51-00-00, EAC FAX 189-2 (DATED 6/5/92), A ND EAC FAX SST-562/97 (DATED 6/9/97). THIS EO OUTLINES WING SKIN PANEL REPAIRS FOR ALL EMB120 AIRCRAFT. LEAK CHECK GOO D. S/D - MAINTENANCE REPAIRED THE CRACKED SKIN IAW ASA EO 120-57-0027. THIS EO REF SRM 51-00-00, EAC FAX 189-92 (DATED 6/5/92), AND EAC FAX SST-562-97 (DATED 6/9/97) THIS EO OUTLINES WING SKIN PANEL REPAIRS FOR ALL EMB-120 AIRCRAFT. LEAK CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 2002031800049 20020318 00049 SO 2002 3 18 ASOA02073 1 20020206 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 505AS 120279 DURING HANGAR MAINTENANCE IN MCN, THE LEFT EXHAUST PIPE AFT ATTACH POINTS WERE FOUND WITH CRACKS ON THE SKIN. MAINTENAN CE REPAIRED THE SKIN CRACK BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER ON THE LEFT AFT INBOARD EXHAUST PIPE ATTA CH FITTING. THE DAMAGED AREA WAS REMOVED AND A FILLER DOUBLER WAS INSTALLED. ALL WORK WAS ACCOMPLISHED USING SRM 51-00 -00 AND 51-40-02 AS A REF. (M) 2 L 7 2 4T RT A31SO 2002031800050 20020318 00050 NM 2002 3 18 2002UALA00381 1 20020307 A 5320 CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 FUSELAGE STATION 663 STRINGER TO FRAME CLIP CRACKED AT 10L. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002031800051 20020318 00051 SO 2002 3 18 ASOA02074 1 20020206 A 7110 COWLING EMB 120 EMB120ER 3260203 SO LT ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 505AS 120279 DURING HANGAR MAINTENANCE IN MCN, THE LEFT ENGINE AFT COWL HAD CRACKS. MAINTENANCE REPAIRED DAMAGE TO THE LEFT ENGINE C OWL IAW SRM CHAPTER 51. CLEARANCE CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 2002031800052 20020318 00052 EU 2002 3 18 ASOA02075 1 20020206 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 641AS 387 DURING C-CHECK INSPECTION IN BNA, FOUND CORROSION ON THE ENTIRE LENGTH OF THE TOP FLANGE, FROM LEFT TO RIGHT, UPPER AND LOWER SURFACES AT FRAMES 36, 38, 39, AND 40. MAINTENANCE REPAIRED THE CORROSION IAW ASA EO 72-53-0128. S/D THIS EO REF FAA FROM 8110-3, REPORT NR 02-019, WHICH INCLUDES REPAIR SPECIFICATIONS FOR AIRCRAFT. (M) 2 H 7 2 4T RT 2002032000054 20020320 00054 NM 2002 3 20 2002UALA00382 1 20020305 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 191UA 26880 UPPER DECK EMERGENCY AISLE LIGHT DIM FROM SEAT 12AB THROUGH 14AB. CHARGED THE POWER PACK BATTERY, OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002031800053 20020318 00053 EU 2002 3 18 ASOA02076 1 20020206 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 641AS 387 DURING C-CHECK INSPECTION IN BNA, A CRACK WAS FOUND ON FRAME 26 AT THE BASE LINE. MAINTENANCE REPAIRED THE CRACK IAW AS A EO 72-53-0127. THIS EO REF SERVICE BULLETIN 72-53-1078 AND SRM CHAPTER 51. THIS EO ALSO INCLUDES REPAIR SPECIFICATIO NS FOR FRAME 26 CRACK REPAIR FOR A/C. (M) 2 H 7 2 4T RT 2002031800054 20020318 00054 EA 2002 3 18 ASOA02077 1 20020209 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA O OTHER O OTHER DE DESCENT 1 SO 11 858AS 4315 7417 FLT 4423 - DURNG DESCENT INTO OMA, THE FIRST OFFICERS WINDSHIELD CRACKED. NO EICAS MESSAGE WAS RECEIVED, BUT THE WINDSH IELD FELT COLD. THE CAPTAIN REPORTED ALL HEAT SWITCHES WERE IN THE CORRECT POSITIONS. AIRCRAFT LANDED SAFELY IN OMA. MAINTENANCE REMOVED AND REPLACED THE RIGHT WINDSHIELD. LEAK CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031800055 20020318 00055 NM 2002 3 18 2002UALA00383 1 20020305 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 191UA 26880 EXT EMERGENCY LIGHT (FWD ASSY) RT SIDE (FWD BULB) INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000056 20020320 00056 NM 2002 3 20 2002UALA00384 1 20020305 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 191UA 26880 EMERGENCY BUSTLE LIGHT INOP AT DR5L. REPLACED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2002031800056 20020318 00056 EA 2002 3 18 ASOA02078 1 20020209 A 3350 487191 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 864AS 7502 FLT 4236 - DURING GROUND INSPECTION IN DFW, THE CREW REPORTED THAT THE FORWARD FLOOR EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE CLEANED A DIRTY CONNECTOR ON THE FLOOR TRACK EMERGENCY LIGHTING. OPERATIONAL CHECKS NORMAL. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031800057 20020318 00057 SO 2002 3 18 ASOA02079 1 20020206 A 5313 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 281AS 120224 DURING C-CHECK INSPECTION IN BNA, THE STRINGER 19 (P/N 120-05744-013) LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 13A A ND 17. CORROSION WAS ALSO FOUND ON STRINGER 18 (P/N 120-06173-009) LEFT BETWEEN FRAMES 13A AND 15A. MAINTENANCE REMOVE D AND REPLACED THE CORRODED SECTION OF BOTH THE STRINGERS (P/N 120-05744-013, 120-06173-009) IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002031800058 20020318 00058 SO 2002 3 18 ASOA02080 1 20020206 A 5320 12027289001 STRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SW 21 281AS 120224 DURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS CORRODED BETWEEN FRAMES 13 AND 14. MAINTENANCE REMOVED AND RE PLACED THE CORRODED BUTT STRAP IAW SRM'S 51-40-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002032000057 20020320 00057 NM 2002 3 20 2002UALA00385 1 20020305 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN CONTAMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 191UA 26880 SEAT EEL LIGHTS INOP IN FRONT OF DOOR 3R AND IN FRONT OF LAV 111. CLEANED WATER FROM LIGHT STRIP CONNECTOR IN FRONT OF LAV 111. OPS CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2002031800059 20020318 00059 SO 2002 3 18 ASOA02081 1 20020206 A 5320 12046158603 STRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 281AS 120224 DURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP BETWEEN FRAMES 21 AND 26 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM'S 51-25-00, 51-21-05, 51-21-06 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002032000058 20020320 00058 NM 2002 3 20 2002UALA00386 1 20020305 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 191UA 26880 EXT EMERGENCY LIGHT (FWD ASSY) LT SIDE (AFT BULB) INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002031800060 20020318 00060 SO 2002 3 18 ASOA02082 1 20020206 A 5310 CROSSBEAM EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 EA 19 281AS 120224 DURING C-CHECK INSPECTION IN BNA, ALL CROSSBEAMS AT FRAME 16 WERE FOUND CORRODED. THE LEFT INBOARD AND RIGHT OUTBOARD C ROSSBEAMS WERE FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED THE CORROSION ON THE LEFT OUTBOARD AND RIGHT INBOARD CROS SBEAMS IAW CPM 51-14-00. THE CORROSION ON THE LEFT INBOARD AND RIGHT OUTBOARD CROSSBEAMS (P/N 120-04149-002, 120-06962- 001) WAS REPAIRED IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002031800061 20020318 00061 SO 2002 3 18 ASOA02083 1 20020206 A 5320 12006664006 SILL EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 281AS 120224 DURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SILL PLATE WAS CORRODED BETWEEN FRAMES 21 AND 26. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE USING SRM'S 51-25-00, 51-25-00, AND 51-40-02 AS REF. (M) 2 L 7 2 4T RT A31SO 2002032000060 20020320 00060 NM 2002 3 20 2002UALA00387 1 20020305 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 191UA 26880 EMERGENCY AISLE LIGHT INOP AT SEATS A1 THROUGH 5A. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2002031800062 20020318 00062 SO 2002 3 18 ASOA02084 1 20020206 A 5310 12004149002 CROSSBEAM EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 281AS 120224 DURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD CROSSBEAM AT FRAME 36 WAS FOUND CORRODED BEYOND LIMITS. MAINTENANC E REMOVED AND REPLACED THR RIGHT OUTBOARD CROSSBEAM IAW SRM 51-40-02 AND 51-22-00. (M) 2 L 7 2 4T RT A31SO 2002031800063 20020318 00063 SO 2002 3 18 ASOA02085 1 20020206 A 5310 12004149001 CROSSBEAM EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 281AS 120224 DURING C-CHECK INSPECTION IN BNA, THE LEFT INBOARD AND RIGHT OUTBOARD CROSSBEAMS AT FRAME 16 WERE CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH THE LEFT INBOARD AND RIGHT OUTBOARD CROSS BEAMS AT FRAME 16 IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002031800064 20020318 00064 EU 2002 3 18 DHL2002363002 1 20020202 A 5310 FITTING AIRBUS 300 A300B4203 3930306 EU FRAME 47 CRACKED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING INSPECTION OF FRAME 47 FITTING , FOUND CRACK, 19MM LONG BY 18MM DEEP IN UPPER RADIUS OF FITTING. REQUIRES REPEAT INSPECTION AT 200 LIGHT CYCLES PER AMOC, S/B 28215 AD 96-13-11 2 L 7 2 4F RT A35EU 2002031800065 20020318 00065 EU 2002 3 18 DHL2002364001 1 20020208 A 5310 FRAME AIRBUS 300 A300B4203 3930306 EU FRAME 47 CRACKED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 364DH 141 WHILE INSPECTION PER S/B 53-0246 LEFT UPPER FRAME 47 HAS CRACK 22MM LONG X 34MM DEEP. RIGHT UPPER FRAME 47 HAS CRACK 22M M LONG X 45 MM DEEP. CRACKS REQUIRE REINSPECTION AT 100 FC PER AMOC AD 96-13-11 2 L 7 2 4F RT A35EU 2002031800066 20020318 00066 EU 2002 3 18 DHL2002362002 1 20020108 A 5310 FITTING AIRBUS 300 A300B4203 3930306 EU FRAME 47 CRACKED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 362DH 84 WHILE INSPECTING FRAME 47, FOUND CRACK LEFT SIDE LENGTH 44MM, RT SIDE 22MM DEPTH 42MM. REQUIRES 200 FC REINSPECT. PERFO RMED CHAMFER TO CRUICIFORM FITTING RT AND LEFT SIDE PE S/B 53-0246 2 L 7 2 4F RT A35EU 2002031800067 20020318 00067 EU 2002 3 18 DHL2002366003 1 20020209 A 5310 FRAME AIRBUS 300 A300B4203 3930306 EU FRAME 47 CRACKED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 366DH 249 FRAME 47 INSPECTION FOUND CRACKED FRAME 22MM X 25MM IN UPPER RADIUS RT SIDE, L/H FRAME 47 CRACKED 11MM X 17MM IN UPPE R RADIUS. REQUIRES REPEAT INSPECTION 200 FC PER AMOC , S/B 53-0246 AND AD 96-13-11. 2 L 7 2 4F RT A35EU 2002032000069 20020320 00069 NM 2002 3 20 2002UALA00388 1 20020305 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 191UA 26880 EMERGENCY EXIT SIGN LIGHT INOP AT DR1L. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2002031800068 20020318 00068 SO 2002 3 18 ASOA02086 1 20020206 A 5320 12046963001 STRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 281AS 120224 DURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS CORRODED BETWEEN FRAMES 14 AND 21. MAINTENANCE REMOVED AND RE PLACED THE CORRODED BUTT STRAP IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002031800069 20020318 00069 SO 2002 3 18 ASOA02087 1 20020206 A 5347 SEAT TRACK EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 281AS 120224 DURING C-CHECK INSPECTION IN BNA, THE LEFT FLOOR SEAT TRACK, MID SECTION, WAS FOUND CORRODED BETWEEN FRAMES 22 AND 32. CORROSION WAS ALSO FOUND ON THE LEFT SEAT TRACK, FORWARD SECTION, BETWEEN FRAMES 17 AND 22 AS WELL AS THE AFT SECTION FR OM FRAME 32 AND 39. MAINTENANCE FABRICATED AND DRILLED NEW SEAT TRACKS IAW SRM 51-25-00. THE OLD SEAT TRACKS WERE REMO VED AND THE NEW ONES INSTALLED IAW SRM 53-01-05. (M) 2 L 7 2 4T RT A31SO 2002031800070 20020318 00070 SO 2002 3 18 ASOA02088 1 20020206 A 5347 SEAT TRACK EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 281AS 120224 DURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SEAT TRACK WAS FOUND CORRODED ON THE FORWARD SECTION BETWEEN FRAMES 15 AND 22 AND 31. MAINTENANCE FABRICATED AND DRILLED NEW SEAT TRACKS IAW SRM 51-25-00. THE OLD SEAT TRACKS WERE REMOVED AND THE NEW ONES INSTALLED IAW SRM 51-01-05. (M) 2 L 7 2 4T RT A31SO 2002032000071 20020320 00071 NM 2002 3 20 2002UALA00389 1 20020307 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 MID CABIN RIGHT HAND CREASE BEAM WEB EXFOLIATED BETWEEN STATION 940-944 STRINGER 17 RIGHT, WATERLINE 208. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031800071 20020318 00071 NE 2002 3 18 ASOA02089 2 20020211 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT VIBRATION A ASOA A UNSCHED LANDING E Y J VIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 11 852AS 7389 FLT 4563 - WHILE CLIMBING OUT OF FWA, AT 21,000 FEET, THE LEFT ENGINE N2 VIBRATION SPIKED APPROXIMATELY 2.6 MILS. THE F LIGHT ATTENDANT AND PASSENGERS REPORTED A LOUD NOISE FROM THE LEFT ENGINE. THE LEFT ENGINE SHUT ITSELF DOWN. THE CAPTA IN DECLARED AN EMERGENCY AND RETURNED TO FWA FOR AN OVERWEIGHT LANDING. MAINTENANCE PERFORMED THE OVERWEIGHT LANDING IN SPECTION. NO DEFECTS WERE NOTED. THE LEFT ENGINE WAS REMOVED AND REPLACED. THE MRR WILL REMAIN OPEN PENDING RESULTS O F ENGINE TEARDOWN. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2002031800072 20020318 00072 EA 2002 3 18 ASOA02090 1 20020212 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 827AS 7212 FLT 4505 - DURING SCHEDULED INSPECTION IN XNA, THE LEFT EXTERNAL AFT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031800073 20020318 00073 EA 2002 3 18 ASOA02091 1 20020212 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SW 21 836AS 7283 DURING GROUND INSPECTION IN DFW, THE AFT SECTION OF EMERGENCY FLOOR LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE INSPECT ED AND DISCOVERED WIRE DS29LY-1 NEEDED REPAIR. MAINTENANCE REPAIRED THE WIRE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FO R SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031800074 20020318 00074 EA 2002 3 18 ASOA02092 1 20020213 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 853AS 7374 DURING A SCHEDULED INSPECTION IN XNA, THE THIRD OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031800075 20020318 00075 SO 2002 3 18 ASOA02093 1 20020213 A 3350 3071BPE LIGHT EMB 120 EMB120RT 3260202 SO CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 269AS 120210 FLT 4346 - DURING GROUND INSPECTION IN ATL, THE CREW REPORTED THAT THE FORWARD SECTIONOF THE EMERGENCY FLOOR LIGHTING WA S INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BURNED OUT BULB. SYSTEM CHECKED GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002031800076 20020318 00076 SO 2002 3 18 ASOA02094 1 20020214 A 3350 31880 LIGHT EMB 120 EMB120ER 3260203 SO CABIN BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 285AS 120265 DURING SCHEDULED MAINTENANCE IN MCN, THE EMERGENCY DOOR EXIT LIGHT AT ROW 5 AND THE OVERHEAD BIN EMERGENCY LIGHTED EXIT SIGN AT ROW 8 WERE BOTH FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN ASSEMBLY (P/N 10-11 10-5) AT ROW 5. MAINTENANCE ALSO REPLACED A BROKEN WIRE TERMINAL (P/N 31880) ON THE EXIT SIGN AT ROW 8. (M) 2 L 7 2 4T RT A31SO 2002031800078 20020318 00078 SO 2002 3 18 ASOA02095 1 20020214 A 3230 922AAZYA6PZ722 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO LT MLG WW OUT OF ADJUST A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 500AS 120272 UPON TAKEOFF FROM TXK, THE CAPTAIN SELECTED THE LANDING GEAR HANDLE UP. THE RED A/B LIGHTS ON THE LEFT MAIN AND THE RED B LIGHT ON THE RIGHT MAIN GEAR WERE ILLUMINATED AND FAILED TO EXTINGUISH. THE TXK TOWER INFORMED THE CAPTAIN THAT THE LEFT MLG HAD FAILED TO RETRACT. THE CAPTAIN THEN ATTEMPTED TO RETRACT THE GEAR AGAIN BUT RECEIVED THE SAME RESULTS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO TXK FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED AND ADJUSTED THE SEQUENCE VALVES ON THE LEFT MLG DOORS. MX ALSO INSPECTED THE LEFT AND RIGHT GEAR UPLOCK PROXIMITY SWITCHES AND FOUN D THE RIGHT GEAR B UPLOCK PROXIMITY SWITCH OUT OF ADJUSTMENT. THE RIGHT GEAR B UPLOCK PROXIMITY SWITCH TARGET WERE ADJU 2 L 7 2 4T RT A31SO 2002031800079 20020318 00079 SO 2002 3 18 ASOA02096 1 20020212 A 5553 MS2113406018 ATTACH FITTING EMB 120 EMB120RT 3260202 SO VERTICAL STAB CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 281AS 120224 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE REAR FUSELAGE AT THE VERTICAL STABILIZER ATTACH POINTS. MA INTENANCE WILL REPAIR CORROSION AND REPLACED THE VERTICAL STABILIZER ATTACH BOLTS. THIS MRR WILL REMAIN OPEN UNTIL AN E O CAN BE WRITTEN AND THE WORK COMPLIED WITH. (M) 2 L 7 2 4T RT A31SO 2002031800080 20020318 00080 SO 2002 3 18 ASOA02096S 1 20020212 A 5553 MS2113406018 ATTACH FITTING EMB 120 EMB120RT 3260202 SO VERTICAL STAB CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 281AS 120224 DURNG C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE REAR FUSELAGE AT THE VERTICAL STABILIZER ATTACH POINTS. MAI NTENANCE WILL REPAIR CORROSION AND REPLACE THE VERTICAL STABILIZER ATTACH BOLTS IAW ASA EO 120-55-0045A. THIS EO REFERE NCES EAC FAX 02/039CS, DATED 2/12/02 AND EAC FAX 02/045CS, DATED 2/19/02. THIS EO OUTLINES REPAIR SPECIFICATIONS FOR BO LT REPLACEMENT DUE TO CORROSION ON AIRCRAFT. (M) 2 L 7 2 4T RT A31SO 2002031800081 20020318 00081 WP 2002 3 18 ABXA010763 1 20020313 A 3397 WIRE DOUG DC9 DC941 302207N WP COCKPIT SHORTED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 977AX 47513 WHILE ADJUSTING FIRST OFFICER'S OVERHEAD MAP LIGHT, SPARKING AND SMOKE CAME FROM BEHIND IT. MAP AND BRIEFCASE CIRCUIT B REAKER TRIPPED. FOUND WIRE L453A24 BEHIND THE FIRST OFFICER'S MAP LIGHT CHAFED THROUGH AND SHORTING TO GROUND. REPLACE D A FIVE INCH SECTION OF WIRE L453A24 FROM TERMINAL END BACK IAW DC-9 AMM 20-50-01-2. 2 L 7 2 4F A6WE 2002031800082 20020318 00082 EA 2002 3 18 ASOA02097 1 20020215 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 847AS 6425 7335 DURING FLIGHT FROM ATL, WHILE CLIMBING THROUGH 28,000 FEET AT APPROXIMATELY 290 KNOTS, THE LEFT FRONT WINDSHIELD SHATTER ED. AN EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED TO TYS AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE PILOT S WINDSHIELD. OPERATIONAL AND PRESSURIZATION CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031800083 20020318 00083 EA 2002 3 18 ASOA02098 1 20020215 A 3350 59257 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 864AS 7502 DURING A SCHEDULED INSPECTION IN XNA, THE GALLEY AND FORWARD ORANGE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE EMERGENCY LIGHTING INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031800084 20020318 00084 SO 2002 3 18 ASOA02099 1 20020215 A 5313 12016085002 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 262AS 120146 DURING HANGAR MAINTENANCE IN MCN, THE TENTH STRINGER ON THE RIGHT SIDE WAS FOUND CRACKED. MAINTENANCE REPAIRED THE CRAC KED STRINGER IAW SRM 57-20-01 AND SRM 51-20-02. (M) 2 L 7 2 4T RT A31SO 2002031800085 20020318 00085 SO 2002 3 18 ASOA02100 1 20020215 A 3350 D35504001 LIGHT EMB 120 EMB120RT 3260202 SO CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 273AS 120222 FLT 4349 - DURING GROUND INSPECTION IN ATL, THE LEFT AND RIGHT AFT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002031800086 20020318 00086 SO 2002 3 18 ASOA02101 1 20020217 A 3350 1317 LIGHT EMB 120 EMB120ER 3260203 SO CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 638AS 120282 DURING SCHEDULED INSPECTION IN MCN, THE FORWARD MOST WHITE FLOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE BURNED OUT BULB ON THE FLOOR EMERGENCY LIGHT TRACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002031800088 20020318 00088 EU 2002 3 18 ASOA02102 1 20020217 A 3350 POWER SUPPLY AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 631AS 382 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE AIRSTAIR DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE EMERGENCY LIGHTING POWER SUPPLY AT THE 62WL POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2002031800089 20020318 00089 SO 2002 3 18 ASOA02103 1 20020206 A 5320 12005803001 SILL EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 281AS 120224 DURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SILL PLATE WAS FOUND CORRODED BETWEEN FRAMES 13 AND 21. MAINTENANCE R EMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRM'S 51-40-02 AND 51-25-00. (M) 2 L 7 2 4T RT A31SO 2002031800090 20020318 00090 EA 2002 3 18 ASOA02104 1 20020219 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 867AS 7463 DURING A SCHEDULED INSPECTION IN XNA, THE THIRD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE THIRD EXTERIOR EMERGENCY LIGHT WHICH WAS BURNED OUT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031800091 20020318 00091 SO 2002 3 18 ASOA02105 1 20020219 A 3350 D36604001 SIGN EMB 120 EMB120RT 3260202 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 237AS 120051 DURING HANGAR CHECK IN TXK, BOTH AFT LEFT AND RIGHT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE NR 3 EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002031800092 20020318 00092 SO 2002 3 18 ASOA02106 1 20020219 A 3350 BATTERY PACK EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 265AS 120170 DURING HANGAR CHECK IN MCN, THE FORWARD FLOOR EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE AND THE NR 1 EMERGENCY LIGHT B ATTERY PACK WAS FOUND DEAD. MAINTENANCE SPLICED A BROKEN WIRE ON THE FORWARD FLOOR EMERGENCY LIGHT STRIP. MAINTENANCE ALSO REMOVED AND REPLACED THE DEAD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M ) 2 L 7 2 4T RT A31SO 2002031800093 20020318 00093 EA 2002 3 18 ASOA02108 1 20020221 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 840AS 7290 DURING HANGAR CHECK IN MCN, IN FLOOR EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE FROM ROW 6 TO ROW 8. MAINTENA NCE RESECURED THE LOOSE FLOOR EMERGENCY LIGHTING TRACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002031800094 20020318 00094 EU 2002 3 18 ASOA02109 1 20020223 A 3246 AHA1890 TIRE AEROSP ATR72 ATR72212 8680945 EU MLG DAMAGED A ASOA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 11 533AS 460 UPON LIFTOFF FROM MGM, THE CAPTAIN OBSERVED A STRONG VIBRATION FOR ABOUT 15-20 SECONDS. THE CAPTAIN DECLARED AN EMERGEN CY AND RETURNED TO MGM FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE DOORS, PANELS, DE-ICE BOOTS, AND LANDING GE AR AND FOUND NO DEFECTS. THE LEFT INBOARD TIRE WAS DISCOVERED TO HAVE A TEN INCH FLAT SPOT. MAINTENANCE REMOVED AND RE PLACED THE FLAT SPOTTED LEFT TIRE. (M) 2 H 7 2 4T RT A53EU 2002031800095 20020318 00095 EU 2002 3 18 ASOA02110 1 20020224 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 530AS 453 DURING A HANGAR INSPECTION IN MCN, THE AIRSTAIR DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002031800096 20020318 00096 SO 2002 3 18 ASOA022023 1 20020114 A 3350 1317 LIGHT EMB 120 EMB120ER 3260203 SO CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 505AS 120279 FLT 4283 - DURING GROUND INSPECTION IN ATL, ONE CEILING EMERGENCY LIGHT BULB WAS FOUND TO BE BURNED OUT. MAINTENANCE RE MOVED AND REPLACED THE BURNED OUT CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002031800097 20020318 00097 EA 2002 3 18 ASOA022107 1 20020220 A 2610 355924400 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE DEFECTIVE A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 826AS 7210 DURING CLIMB-OUT OF MCO, WITH THE GEAR UP THE CAPTAIN RECEIVED A 14TH STAGE DUCT WARNING ON THE LEFT ENGINE. AN EMERGEN CY WAS DECLARED AND AIRCRAFT RETURNED TO MCO AND LANDED SAFELY. MAINTENANCE FOUND THE ROOT CAUSE OF THIS OCCURRENCE TO BE A DEFECTIVE 14TH STAGE SENSING ELEMENT. MAINTENANCE REMOVED AND REPLACED THE SENSING ELEMENT. THE 14TH STAGE BLEED AIR DUCT WAS REPLACED DUE TO CHAFING DAMAGE CAUSED BY THE DEFECTIVE ELEMENT. THE 14TH STAGE ANTI-ICE CHECK VALVE AS WEL L AS THE VALVE COUPLING AND BOOT WERE REPLACED AS A PRECAUTION. (M) 2 L 7 2 4F RT A21EA 2002031800100 20020318 00100 NM 2002 3 18 EIA2002002 1 20020124 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 MZJ - FOUND FLOORBEAM UPPER RETURN FLANGE AT STATION 571, RBL 25, WAS FOUND BROKEN. REMOVED DAMAGED PORTION OF FLOORBEA M AND REPAIRED PER SRM CHAPTER 51. (M) 2 L 7 4 4F A20WE 2002031800101 20020318 00101 NM 2002 3 18 EIA2002003 1 20020129 A 3350 20131A LIGHT BOEING 747 747132 1384882 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481EV 19896 FOUND A-CHECK, L5 AND R5 EMERGENCY LIGHT INOPERATIVE STATION 2280. BATTERY PACK REPLACED AND OPS CHECK PER MM. (M) 2 L 7 4 4F A20WE 2002031800104 20020318 00104 2002 3 18 G60A065 4 20020202 A 3418 SENSOR DOUG DC10 DC1030F 3023504 WP STALL WARNING MALFUNCTIONED A G6OA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 27 607GC 46978 AFER TAKEOFF, STICK SHAKER STARTED AND THEN SLAT DISAGREE LIGHT CAME ON. RETURNED TO KMIA. REMOVED AND REPLACED AOA SE NSOR P/N 2568A13, PER MM 22-33-01 AND NR 1 AT/SC COMPUTER P/N 2593342976 PER MM 22-31-01. STALL WARNING TESTS GOOD. (M ) 2 L 7 3 4F RT A22WE 2002031800105 20020318 00105 NE 2002 3 18 G6OA064 2 20020201 A 7200 ENGINE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 3 FLAMED OUT A G6OA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 EA 27 604GC 47924 517763 NR 3 ENGINE FLAMED OUT AT CRUISE. AFTER TROUBLESHOOTING NR 3 ENGINE, REMOVED AND REPLACED NR 3 ENGINE FUEL FILTER ELEME NT PER MM 73-11-02. REMOVED AND REPLACED NR 3 FUEL PUMP PER MM 73-12-01. REMOVED AND REPLACED MEC UNIT ON NR 3 ENGINE PER MM 73-20-01. PERFORMED POWER ASSURANCE CHECK PER MM 71-06-00. NR 3 ENGINE CHECKS GOOD. (M) 2 L 7 3 4F 4 F RT A22WE E23EA 2002031800106 20020318 00106 NM 2002 3 18 GAIA02011OP 1 20020204 A 5414 72722000476 SKIN BOEING 727 727224 1384076 NM NACELLE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 69735 20664 DURING B-CHECK INSPECTION MAINTENANCE, FOUND A 2.5 INCH CRACK TO THE NR 3 ENGINE NOSE COWL SKIN LOCATED AT NAC STATION 7 7.5. MAINTENANCE REMOVED AND REPLACED THE NR 3 ENGINE NOSE COWL. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002031800107 20020318 00107 NM 2002 3 18 GAIA02019OP 1 20020223 A 2751 18129932 INDICATOR BOEING 727 727251 138408H NM COCKPIT STUCK A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 252US 19971 FLT 1801 - FWA-MCO - ON APPROACH TO MCO, THE OUTBOARD FLAPS ASYMMENTRIED LESS THAN 2 DEGREES. THE CREW DECLARED AN EMER GENCY AND THE AIRCRAFT LANDED AT MCO WITHOUT FURTHER DIFFICULTIES. FOUND THE OUTBOARD FLAP POSITION INDICATOR STICKING. REMOVED AND REPLACED THE OUTBOARD FLAP POSITIOIN INDICATOR. CYCLED FLAPS NUMEROUS TIMES AND OPERATIONLLY CHECKED GOOD . THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002032900101 20020329 00101 WP 2002 3 29 ARWA20020306 1 20020308 A 3310 BA170 TRANSFORMER DOUG DC8 DC862 3021970 WP COCKPIT MALFUNCTIONED A ARWA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 19 8969U 46070 SMOKE EMANATED MOMENTARILY FROM RT CORNER OF F/O GLARESHIELD (10 SEC), SMOKE STOPPED AS EMERGENCY CHECKLIST WAS INITIATE D. REMOVED AND REPLACED BALLAST TRANSFORMER AND REPLACED LAMPS IAW MM 33-12-0. 2 L 7 4 4F 4A25 2002031800109 20020318 00109 WP 2002 3 18 AT0200034 1 20020128 A 5620 WINDOW FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 CABIN WINDOW FRAME 33 RIGHT THIN SPOT, EXTERIOR RIM. 2 L 7 2 4F A6WE 2002031900095 20020319 00095 WP 2002 3 19 ARWA20020308 1 20020315 A 7711 C2918710005 INDICATOR DOUG DC8 DC85F54 3021926 WP COCKPIT STICKS A ARWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 426FB 45667 ABORTED TAKEOFF DUE TO ENGINE NR 4 MOMENTARY POWER LOSS, ALL ENGINE PARAMETERS NORMAL. RETURN TO RAMP. PERFORMED ENGIN E RUN-UP AND NOTICED EPR INDICATOR STICKING. REMOVED AND REPLACED EPR INDICATOR IAW MM 77-1-2 AND SYSTEMS OPS CHECKED N ORMAL IAW MM 71-0. 2 L 7 4 4F RT 4A25 2002031800111 20020318 00111 EA 2002 3 18 COMA0260186 1 20020313 A 5551 601R55310022 BUSHING CNDAIR CL600 CL6002B19 1900309 EA STABILIZER CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 991CA 9124 7216 HORIZONTAL STABILIZER ATTACH FITTING R.H. PIVOT PIN BUSHING LOOSE.REPLACED BUSHING I/A/W S.B. 601R-55-007 STEP 4 PAGE 51 THROUGH STEP 15 PAGE 64 AND REO 601R-55-31-036. 2 L 7 2 4F RT A21EA 2002031800112 20020318 00112 EU 2002 3 18 AWXA200200217 1 20020207 A 5320 D534800204436 WEB AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 55 YWG - MAJOR REPAIR - C - DURING C-02 CHECK A CRACK WAS FOUND ON LT OUTBOARD WEB BELOW THE AFT GALLEY, FR 68-69. 2 L 7 2 4F RT A28NM 2002031800113 20020318 00113 NM 2002 3 18 AWXA200200219 1 20020312 A 5220 PANEL BOEING 737 737317 138447P NM OVERWING EXIT OUT OF ADJUST A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - DURING C-13 CHECK LT OVERWING HATCH FAILED CLOSING REQUIREMENT FORCE CHECK. MAINTENANCE ADJUSTED SIDEWALL PANEL I AW BMM 52-21-00 PG 506. EMERGENCY EXIT CLOSING FORCE NOW WITHIN LIMITS PER BMM 52-21-00 PG 506. 2 L 7 2 4F RT A16WE 2002031800114 20020318 00114 NM 2002 3 18 AWXA200200220 1 20020312 A 5220 PANEL BOEING 737 737317 138447P NM OVERWING EXIT OUT OF ADJUST A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - DURING C-13 CHECK RT OVERWING HATCH FAILED CLOSING REQUIREMENT FORCE CHECK. MAINTENANCE ADJUSTED SIDEWALL PANEL I AW BMM 52-21-00 PG 506. RT EMERGENCY EXIT CLOSING FORCE NOW WITHIN LIMITS PER BMM 52-21-00 PG 506. 2 L 7 2 4F RT A16WE 2002031800115 20020318 00115 NM 2002 3 18 AWXA200200221 1 20020313 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 154AW 23776 PHX - EEL - C - EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 7 LT. MAINTENANCE REMOVED AND REPLACED SEAT LIGHT A SSEMBLY IAW T/C A1C33003, FUNCTIONAL CHECK WAS GOOD IAW T/C A1C33006. 2 L 7 2 4F RT A16WE 2002031800116 20020318 00116 NM 2002 3 18 AWXA200200222 1 20020314 A 3350 1010428 LIGHT BOEING 737 7373G7 1384595 NM CABIN DETACHED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 PHX - EEL - C - EMERGENCY EXIT LIGHT AT OVERHEAD BIN SEAT ROW 8 RT IS DETACHED FROM OVERHEAD BIN. MAINTENANCE REMOVED A ND REPLACED EMERGENCY LIGHT ASSEMBLY. 2 L 7 2 4F RT A16WE 2002031800117 20020318 00117 NM 2002 3 18 GAIA02021OP 1 20020228 A 2751 696R14S5S TRANSMITTER BOEING 727 727251 138408H NM TE FLAPS DAMAGED A GAIA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 252US 19971 FLT 715 - ELP-FWA - ON DESCENT, THE AIRCRAFT HAD OUTBOARD SPLIT FLAP IINDICATION. THE CERW USED THE ALTERNATE FLAP SYST EM TO LOWER THE FLAPS TO THEIR DESIRED SETTINGS PER THE CHECKLIST. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LAND ED IN FWA UNEVENTFUL. AFTER TROUBLE SHOOTING FOUND A PIN PUSHED BACK ON THE RIGHT OUTBOARD FLAP POSITION TRANSMITTER. RESET PIN AND CYCLED THE FLAPS SEVERAL TIMES AND FOUND TO OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 L 7 3 4F A3WE 2002031800118 20020318 00118 SO 2002 3 18 C2XA02RI002 1 20020315 A 3260 CONNECTOR EMB 135 EMB135LR 3260305 SO NLG LOOSE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 27523 145389 RIC-FLT 3000 CREW REPORTED THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE CREW RETURNED TO RIC WITHOUT FUR THER INCIDENT. MAINTENANCE FOUND BOTH NOSE LANDING GEAR UPLOCK AND DOWNLOCK PROXIMITY SWITCH HARNESS CANNON PLUGS NOT P ROPERLY SECURED. MAINTENANCE RESECURED BOTH CANNON PLUGS AND PERFORMED A SATISFACTORY SYSTEM OPERATIONAL TEST. THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002031800126 20020318 00126 SO 2002 3 18 C2XA02TY054 1 20020316 A 5315 14521721009 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13929 145009 TYS, DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL, AFT OF THE COCKPIT DOOR WAS FOUND CORRODED. 2 L 7 2 4F RT T00011AT 2002031800127 20020318 00127 WP 2002 3 18 GTIA012295 1 20020103 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND STATION 205 L15L, SHEAR TIE ON FORWARD END OF INTERCOSTAL IS CRACKED. REMOVED CRACKED INTERCOSTAL. FABRICA TED SHIM AND DOUBLER. INSTALLED SHIM AND DOUBLER IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002031800129 20020318 00129 NE 2002 3 18 MWEA020166 2 20020313 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE LEFT LEAKING A MWEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 216ME 47740 LEFT ENGINE OIL PRESSURE DECREASING, LEFT TEMPERATURE RISING INTO YELLOW ARCH 120 DEGREES CELSIUS. REDUCED POWER TO IDL E, OIL QUANTITY WENT TO ZERO, OIL PRESSURE LOW LIGHT CAME ON, OIL PRESSURE INDICATED 30 PSI. PERFORMED ENGINE SHUT DOWN PER QRH. MAINTENANCE REPLACED ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 2002031800130 20020318 00130 EA 2002 3 18 COMA0260187 1 20020318 A 5415 601370101 PYLON CNDAIR CL600 CL6002B19 1900309 EA EMPENNAGE CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 937CA 17486 7044 DURING REMOVAL OF THE LEFT ENGINE ASSEMBLY, DISCOVERED FRETTING CORROSION ON THE AFT ENGINE PYLON THRU FITTING MOUNTING RIB W.O. 41725.REPAIRED I/A/W REO 601R-54-50-036. 2 L 7 2 4F RT A21EA 2002031800133 20020318 00133 EU 2002 3 18 QXEA0200354 1 20020216 A 5553 ATTACH ANGLE FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT AND RT SIDES OF THE LOWER FLANGE AT THE VERTICAL STAB FROM SPAR TO FUSELAGE CONNECTION ANGLE HAS CRACKS. REPAI RED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002031800136 20020318 00136 EA 2002 3 18 ASOA02071 1 20020205 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 849AS 7347 FLT 4799 - DURING SCHEDULED INSPECTION IN XNA, THE RIGHT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVIC E. (M) 2 L 7 2 4F RT A21EA 2002031800138 20020318 00138 NM 2002 3 18 UPS02537894 1 20020315 A 5310 BEAM BOEING 757 75724APF 1384969 NM BS1200LBL47-62 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 406UP 23728 INSPECTION TYPE:MOD UPON REMOVAL OF FLOOR PANELS FOUND CORROSION ON UPPER FLANGE OF FLOOR BEAM AT BS 1200 LBL 47 TO LBL 62 WL 208 CORROSION TO BE OUT OF LIMITS FABRICATE REPAIR ANGLE AND ACCOMPLISH ERO 02-0295 2 L 7 2 4F RT A2NM 2002031800145 20020318 00145 WP 2002 3 18 GTIA012321 1 20020103 A 3520 OXYGEN MASK DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 47113 FTW - FOUND OXYGEN MASK DID NOT DROP IN AUTO. PERFORMED TROUBLE SHOOTING AND FOUND OXYGEN LEAK ON OXYGEN LINES. INSTAL LED PROPERLY OXYGEN LINES. OPS CHECK GOOD IAW DC9 MM 35-20-0. (M) 2 L 7 2 4F A6WE 2002031800147 20020318 00147 2002 3 18 0200811161 4 20020314 A 2330 PROJECTOR DOUG DC10 DC1040 3023508 WP A NWAA K NONE O OTHER CR CRUISE 1 GL 01 161US 46770 During cruise electrical odor noticed around door 3 area when overhead projector on. Flight continued to DTW and landed without incident. Maintenance replaced overhead projector.See Logpage 6991285.No previous history in last 30 days. 2 L 7 3 4F A22WE 2002031800150 20020318 00150 NM 2002 3 18 HALA0200015 1 20020128 A 3240 BRAKE BOEING 717 717200 1383700 NM MLG MALFUNCTIONED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 487HA 55132 FLT 281 - ITO - DRAGGING BRAKES. INSPECTED NR 3 WHEEL AXLE FOR DAMAGE. FOUND BLISTERING PAINT ON INNER AXLE AT 6:00 PO SITION. STRIPPIED PAINT AND FOUND EVIDENCE OF CADMIUM OVERHEAT (VEINING AND ROUGHNESS). REMOVED AND REPLACED RT MLG ST RUT PISTON PER MM 32-11-03. OPS CHECK AND SPIN CHECK GOOD. (M) 2 L 7 2 4F TR A6WE 2002031800151 20020318 00151 NM 2002 3 18 HALA0200034 1 20020125 A 3260 PROXIMITY SENSOR BOEING 717 717200 1383700 NM MLG MALFUNCTIONED A HALA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 481HA 55126 FLT 96 - RIGHT LANDING GEAR UNSAFE LIGHT ON WHEN GEAR IN THE UP POSITION. REPLACED RT MLG UPLATCH PROX SENSOR, D1-1058. RETURN TO SERVICE TEST AND GEAR RETRACTION CHECK OK PER BOEING 32-61-00. (M) 2 L 7 2 4F TR A6WE 2002031800152 20020318 00152 NM 2002 3 18 QXEA0200476 1 20020315 A 2610 3023143 DETECTOR DHAV DHC8 DHC8202 2809007 NM CABIN DEFECTIVE A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 360PH 21719 515 SEA-MASTER WARNING ILLUMINATED SEVERAL TIMES DURING FLIGHT. CREW MEMBERS IN CABIN CHECKED LAVATORY AND BAGGAGE AREA FOR SMOKE. NO SMOKE FOUND. MAINTENANCE REMOVED AND REPLACED #2 SMOKE DETECTOR IN BAGGAGE COMPARTMENT. OPERATIONAL CHECKS WER E GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002031800153 20020318 00153 WP 2002 3 18 ZW0A0203201 1 20020316 A 3350 60030431 BATTERY PACK DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9618A 53565 THE EGRESS LIGHTS ROW 21 THRU 26 WOULD NOT SHUT OFF. REPLACED THE BATTERY PACK. CHECK-C 11-9-01 MCI. --CLOSED-- 2 L 7 2 4F RT A6WE 2002031800154 20020318 00154 WP 2002 3 18 ABXA010769 1 20020307 A 5300 995821429 FRAME DOUG DC9 DC941 302207N WP AFT CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 978AX 47628 AFT LOWER CARGO FRAME AT F.S. 973, LONGERON 30, 29 LEFT AND 28 LEFT, HEAVILY CORRODED AND DOUBLE DRILLED HOLE. REPAIRED FUSELAGE FRAME IAW REA D953-43402-MR. 2 L 7 2 4F A6WE 2002031800155 20020318 00155 WP 2002 3 18 ABXA010770 1 20020228 A 5300 592480225 FRAME DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 978AX 47628 LONGERON 17 LEFT WAS CRACKED BEHIND FUSELAGE FRAMES AT STATION 256, 275, 408 AND 427. REPAIRED AREA IAW DC-9 SSRM K05864 . 2 L 7 2 4F A6WE 2002031800156 20020318 00156 WP 2002 3 18 ABXA010772 1 20020226 A 5100 99155547 ANGLE DOUG DC9 DC914 3022034 WP LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 OUTBOARD LOWER FASTENER HOLE ON ATTACH ANGLE CRACKED WHERE WING TO FUSELAGE FAIRING ATTACHES AT F.S. 585. REPLACED ANGLE IAW DC-9 SRM 51-30-1 AND DC-9 DWG 9915547. 2 L 7 2 4F A6WE 2002031800157 20020318 00157 WP 2002 3 18 ABXA010773 1 20020227 A 5220 49144131AX FITTING DOUG DC9 DC914 3022034 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 LEFT OVER WING EXIT DOOR PAN STIFFENER ANGLES ON OUTER PAN CRACKED 5 INCHES. REPLACED STOPS IAW DC-9 SRM 51-30-2 AND 51- 30-5. 2 L 7 2 4F A6WE 2002031800158 20020318 00158 WP 2002 3 18 ABXA010774 1 20020227 A 5311 505159 FRAME DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 AUXILIARY SUPPORT FRAME CRACKED IN AFT ACCESSORY COMPARTMENT FLOOR SUPPORT, FORWARD OF MAIN FRAME AT STATION 908. REPLAC ED FRAME IAW DC-9 SRM DWG 505159 AND DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 2002031800159 20020318 00159 WP 2002 3 18 ABXA010777 1 20020310 A 5310 3754473501 SPLICE DOUG DC8 DC861 3021952 WP AFT LWR CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 AFT LOWER CARGO COMPARTMENT, LONGERON SPLICE TIE CRACKED BETWEEN B.S. 1300 - 1320, LONGERON 31 LEFT. REPLACED SPLICE IAW DC-8 SRM 51-1-20D AND 51-3-2. 2 L 7 4 4F 4A25 2002031800160 20020318 00160 WP 2002 3 18 ABXA010764 1 20020315 A 3340 8906K1268 SWITCH DOUG DC9 DC941 302207N WP DEFECTIVE A ABXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 977AX 47513 WHEN THE LEFT LANDING LIGHT SWITCH WAS SELECTED TO EXTEND, COCKPIT FILLED WITH SMOKE. REPLACED THE LEFT LANDING LIGHT SW ITCH. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2002031800161 20020318 00161 WP 2002 3 18 ABXA010765 1 20020219 A 5300 591000644 PANEL DOUG DC9 DC941 302207N WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 978AX 47628 FITTING OUTBOARD OF CANTED KEEL PANEL AT STATION 603, RIGHT SIDE CRACKED. REPLACED FITTING IAW DC-9 MM. 2 L 7 2 4F A6WE 2002031800162 20020318 00162 WP 2002 3 18 ABXA010766 1 20020225 A 5313 59114063 SKIN DOUG DC9 DC941 302207N WP EXT. FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 978AX 47628 FOUND 2 CRACKS IN FUSELAGE SKIN AT UPPER AFT DOOR STOP HOLE FOR MAIN ENTRY DOOR. EACH CRACK IS APPROXIMATELY .350 INCHES LONG. REPAIRED CRACKED AREA OF FUSELAGE SKIN IAW E.A. 53100126-001. 2 L 7 2 4F A6WE 2002031800163 20020318 00163 SO 2002 3 18 C2XA02TY052 1 20020316 A 2620 14531342401 MANIFOLD EMB 145 EMB145ER 3260211 SO APU CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13929 145009 TYS, DURING A SCHEDULED INSPECTION THE APU FIRE EXTINGUISHER HEAD MANIFOLD WAS FOUND CHAFED AT B-NUT. MAINTENANCE REMOV ED AND REPLACED THE MANIFOLD IAW-EMB135/145MM-20-10-03 AND 26-23-05. REPAIR PROCEDURES WHERE SATISFACTORY AND THE AIRCR AFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002031800164 20020318 00164 WP 2002 3 18 DHL2002805045 1 20020314 A 5610 CAM DOUG DC8 DC873F 302199F WP SLIDING WINDOW OUT OF ADJUST A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 CAPTS SLIDING WINDOW WILL NOT OPEN. LUBED AND ADJUSTED CAM TO LOWER VERTICAL ADJUST IAW DC-8 MM 56-10-3, OPS NORMAL. 2 L 7 4 4F RT 4A25 2002031800165 20020318 00165 NM 2002 3 18 MWEA020165 1 20020310 A 7931 41800044 TRANSMITTER DOUG MD88 MD88 3023688 NM LT ENGINE FAULTY A MWEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 601ME 49762 AFTER ENGINE START THE LEFT ENGINE OIL PRESSURE WAS 56 PSI WITH THE OUTSIDE AIR TEMPERATURE -11 DEGREES FAHRENHEIT AND O IL TEMPERATURE WAS COLD. THE LEFT FUEL HEAT WAS CYCLED TO WARM OIL TEMPERATURE AND LEFT OIL PRESSURE REDUCED TO 54 PSI AS TAKEOFF POWER WAS APPLIED, THE LEFT OIL PRESSURE INCREASED TO 56 PSI (ABOVE LIMIT). REMOVED AND REPLACED THE OIL PRE SSURE TRANSMITTER. LEAK AND OPERATION CHECKS GOOD BY RUNNING NR 1 ENGINE, REFERENCE MAINTENANCE MANUAL 79-33-1. 2 L 7 2 4F RT A6WE 2002031800166 20020318 00166 WP 2002 3 18 MWEA020168 1 20020315 A 5313 591140113 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LONGERON 20 LEFT STATION 214 HAS DENT AND HAS CARRY OVER 5735. FABRICATED AND INSTALLED LONGERON SECTION. 2 L 7 2 4F A6WE 2002031800167 20020318 00167 WP 2002 3 18 MWEA020170 1 20020315 A 5311 995821429 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 STATION 897 FRAME AT LONGERON 29 RIGHT TO 30 HAS CORROSION ON THE LOWER SURFACE. FABRICATED AND INSTALLED CLIP, REPAIR DOUBLERS, AND SHIMS. 2 L 7 2 4F A6WE 2002031800168 20020318 00168 NM 2002 3 18 P5CA0200663 1 20020312 A 2810 408841 VALVE BOEING 747 747122 1384872 NM RESERVE TANK BINDING A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 23 852FT 19757 DURING REFUELING, NR 1 RESERVE VALVE FAILED TO OPEN AND UNABLE TO PUT FUEL INTO NR 1 RESERVE TANK. FOUND EXCESSIVE SHAF T BINDING THAT WOULD ONLY ALLOW PARTIAL OPENING OF THE VALVE. FUELED TANK, MANUALLY CLOSED VALVE. AFTER REFUELING, NR 2 MAIN TANK READ 38.0 & NR 3 MAIN TANK READ 36.6. DURING TAXI, FUEL QUANTITIES CHANGE WAS NOTED. NR 2 TANK READ 30.5 A ND NR 3 TANK READ 42.7. A/C RETURNED TO BLOCK. INSPECTED REFUEL VALVES AND RESET SWITCHES. REOPENED AND CLOSED NR 3 M AIN REFUEL VALVE. INSPECTED REFUEL MANIFOLD. FOUND ALL OK FOR SERVICE WITH NO FUEL MIGRATION. 2 L 7 4 4F A20WE 2002031800169 20020318 00169 EU 2002 3 18 QXEA0200346 1 20020218 A 5320 INTERCOSTAL FOKKER F28 F28MK4000 4990810 EU FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - INTERCOSTAL IMMEDIATELY ABOVE CUT OUT FOR PANEL 24A HAS BEEN SCRATCHED. REPAIRED IAW FOKER SRM. 2 L 7 2 4F RT A20EU 2002031800170 20020318 00170 EU 2002 3 18 QXEA0200347 1 20020214 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - REAR FUSELAGE SKIN CORRODED ON INSIDE OF FRAME 18075 BETWEEN STRINGERS 67 AND 69. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031800171 20020318 00171 EU 2002 3 18 QXEA0200348 1 20020215 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACKED CASTELLATION AT LOWER RIVET ON FRAME 17565 AT STRINGER 24. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031800172 20020318 00172 EU 2002 3 18 QXEA0200350 1 20020214 A 5553 ATTACH ANGLE FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT VERTICAL STAB TO FUSELAGE CONNECTION ANGLE AT INTERMEDIATE SPAR II, AFT HI-LOK FORWARD SIDE CRACKED. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031800173 20020318 00173 EU 2002 3 18 QXEA0200351 1 20020217 A 1430 RIVET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - TWO RIVETS BETWEEN FRAME 10775 AND 11300 HAVE SMALL CRACKS RADIATING ALONG THE LOWER CIRCUMFERENCE OF THE RIVET HE ADS. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13, PARAGRAPH 7 AND SRM 51-31-01 PAGE 13. 2 L 7 2 4F RT A20EU 2002031800174 20020318 00174 EU 2002 3 18 QXEA0200352 1 20020217 A 1430 RIVET FOKKER F28 F28MK4000 4990810 EU WING FAIRING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LEFT-HAND WING FAIRING -Z- PROFILE HAS FOUR RIVETS WITH SMALL CRACKS RADIATING FROM THE LOWER CIRCUMFERENCE OF THE HEAD BETWEEN FRAMES 10775 AND 10335. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13, PARAGRAPH 7. 2 L 7 2 4F RT A20EU 2002031800175 20020318 00175 EU 2002 3 18 QXEA0200353 1 20020214 A 5553 ATTACH ANGLE FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - VERTICAL STAB TO FUSELAGE LT CONNECTION ANGLE INTERMEDIATE SPAR I, TWO INDICATIONS OF CRACKS AT FORWARD HI-LOK AND ONE INDICATION OF A CRACK AT AFT SIDE OF AFT HI-LOK. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2. 2 L 7 2 4F RT A20EU 2002031800176 20020318 00176 EU 2002 3 18 QXEA0200355 1 20020215 A 5553 ATTACH ANGLE FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT SIDE OF THE VERTICAL STAB TO FUSELAGE CONNECTION ANGLE ON THE FORWARD FACE OF THE FRONT SPAR IS CRACKED IN THE RADIUS. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 2002031800177 20020318 00177 EU 2002 3 18 QXEA0200356 1 20020214 A 5532 SKIN PANEL FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - THREE CRACKS IN SKIN PANEL BENEATH THE LEADING EDGE OF THE RUDDER ON THE LT SIDE AT THE STIFFENER. REPAIRED IAW F OKKER SRM 53-02-05, PAGE 10, FIGURE 5 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002031800178 20020318 00178 EU 2002 3 18 QXEA0200357 1 20020216 A 5532 FLANGE FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - NUT PLATE FLANGE IS CRACKED AT TOP AFT CORNER OF APERTURE FOR PANEL 57P. REPAIRED IAW FOKKER SRM 55-02-05, PAGE 8 , FIGURE 4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002031800179 20020318 00179 EU 2002 3 18 QXEA0200358 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK AT FRAME 4610 FORWARD OF TRACK AFT ABOUT 4 INCHES ON INBOARD FLANGE HAS CORROSION. REPAIRED IAW FOKKER SRM 53-40-01. 2 L 7 2 4F RT A20EU 2002031800180 20020318 00180 EU 2002 3 18 QXEA0200359 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK AT FRAME 4610, FORWARD END OF TRACK, INBOARD FLANGE HAS CORROSION. REPAIRED IAW FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 2002031800181 20020318 00181 EU 2002 3 18 QXEA0200360 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK AFT OF FRAME 4900 ON OUTBOARD FLANGE THERE IS CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031800182 20020318 00182 EU 2002 3 18 QXEA0200361 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK FRAME 5305 TOP LUG AREA HAS CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031800183 20020318 00183 EU 2002 3 18 QXEA0200362 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK FRAME 5805 FORWARD 4 INCHES INSIDE THE CHANNEL HAS CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031800184 20020318 00184 EU 2002 3 18 QXEA0200363 1 20020218 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK FORWARD OF FRAME 5305 ON INBOARD FLANGE THERE IS PITTING AND CORROSION. REPAIRED IAW FOKKE R SRM. 2 L 7 2 4F RT A20EU 2002031800185 20020318 00185 EU 2002 3 18 QXEA0200364 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK FROM FRAME 6305 TO FRAME 4610 LUGS AT SEAT ATTACH POINTS HAVE GOUGES. REPAIRED IAW FOKKER M M. 2 L 7 2 4F RT A20EU 2002031800186 20020318 00186 EU 2002 3 18 QXEA0200365 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK FRAME 6805 AFT INSIDE CHANNEL THERE IS CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031800187 20020318 00187 EU 2002 3 18 QXEA0200366 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK FROM FRAME 7805 INSIDE THE CHANNEL HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031800188 20020318 00188 EU 2002 3 18 QXEA0200367 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK FROM FRAME 7805 FORWARD AND INSIDE THE CHANNEL HAS CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031800189 20020318 00189 EU 2002 3 18 RAIA00203090 1 20020303 A 7700 WARNING SYSTEM JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE COCKPIT FALSE ACTIVATION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 569HK 41088 75086 5484-STL- DURING TAKEOFF GOT LEFT ENGINE INTEGRATED ELECTRONIC CONTROL FAULT. MAINTENANCE CLEARED FAULT 20 AND GROUND R UN LEFT ENGINE, OPS CHECK GOOD. NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A41NM E18NE 2002031800190 20020318 00190 2002 3 18 SWAA020346 4 20020213 A 2565 63562101 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 772SW 27880 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002031800191 20020318 00191 NM 2002 3 18 SWAA020349 1 20020214 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHTS LOOSE AT ROWS 5 DEF AND 23 DEF. SECURED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2002031800192 20020318 00192 2002 3 18 SWAA020352 4 20020213 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002031800193 20020318 00193 NM 2002 3 18 SWAA020353 1 20020213 A 2560 100031 SIGN BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT SIGN LOOSE ABOVE ROW 20. SECURED EXIT SIGN PER MM. 2 L 7 2 4F A16WE 2002031800194 20020318 00194 2002 3 18 SWAA020354 4 20020214 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 654SW 28399 FWD SERVICE DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER INADVERTENTLY. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002031800195 20020318 00195 NM 2002 3 18 SWAA020357 1 20020214 A 3350 6104791 BATTERY BOEING 737 7372H4 138448C NM CARGO BAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED A2 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHTS INOP AT BOTH FWD CABIN DOORS. REMOVED AND REPLACED BATT ERY PER MM. 2 L 7 2 4F A16WE 2002031800196 20020318 00196 NM 2002 3 18 SWAA020358 1 20020214 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CARGO BAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED A2 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHTS INOP AT RT OVERWING AND AFT OF RT WING. REMOVED AND REP LACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002031800197 20020318 00197 NM 2002 3 18 SWAA020359 1 20020215 A 3350 7003661 BALLAST BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 709SW 27843 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB AND BALLAST PER MM. 2 L 7 2 4F RT A16WE 2002031800198 20020318 00198 2002 3 18 SWAA020361 4 20020216 A 2565 D31354 SLIDE BOEING 737 7372K6 1364440 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND LOW AND OUT OF VIEW. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002031800199 20020318 00199 NM 2002 3 18 SWAA020364 1 20020214 A 3350 610478 BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED D-CHECK, FOUND EMERGENCY EXIT LIGHTS BATTERY PACK M 1137 INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002031800200 20020318 00200 NM 2002 3 18 SWAA020366 1 20020217 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS LOOSE AT ROW 15. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002031800201 20020318 00201 NM 2002 3 18 SWAA020370 1 20020216 A 5311 96380 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 613SW 27931 DURING SCHEDULED SPECIAL VISIT, FOUND RT CHORD CRACKED AT BS 178, WL 207 AND RBL 34.5. REPAIRED CHORD PER SWA ACO. 2 L 7 2 4F RT A16WE 2002031800202 20020318 00202 NM 2002 3 18 SWAA020371 1 20020216 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 613SW 27931 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB HAS A HOLE AT BS 178, WL 183 AND RBL 17.1. REMOVED AND REPLACED WEB PER SWA ACO. 2 L 7 2 4F RT A16WE 2002031800203 20020318 00203 NM 2002 3 18 SWAA020374 1 20020216 A 3320 417A5500 BALLAST BOEING 737 7377H4 1384404 NM CABIN OVERHEATED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 789SW 29816 AIR TURNBACK, BURNING SMELL REPORTED IN CABIN. AFT GALLEY, RECIRC FAN AND GASPER FAN C/B PULLED, SMELL GOT STRONGER. F OUND SIDEWALL LIGHT BALLAST OVERHEATED AT ROW 17 ABC. REMOVED AND REPLACED SIDEWALL LIGHT BALLAST AT ROW 17 ABC PER MM. 2 L 7 2 4F RT A16WE 2002031800204 20020318 00204 NM 2002 3 18 SWAA020379 1 20020217 A 3350 6104789 BATTERY BOEING 737 7372H4 138448C NM CARGO BAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM . 2 L 7 2 4F A16WE 2002031800205 20020318 00205 NM 2002 3 18 SWAA020382 1 20020218 A 3260 TARGET BOEING 737 7373Q8 1384670 NM RT MLG OUT OF ADJUST A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 695SW 23506 AIR TURNBACK, DURING DEPARTURE GEAR HANDLE WOULD NOT GO TO UP POSITION. FOUND AIR SAFETY SENSOR TARGET GAP AND GROUND S POILER INTERLOCK CABLE OUT OF ADJUSTMENT. ADJUSTED TARGET GAP AND INTERLOCK CABLE PER MM. 2 L 7 2 4F RT A16WE 2002031800206 20020318 00206 NM 2002 3 18 SWAA020396 1 20020215 A 5320 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 294.5, STR 11L AND BS 907, STR 4L. REMOVED AND REPL ACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002031800207 20020318 00207 2002 3 18 SWAA020399 4 20020221 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED RON, FOUND AFT SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002031800208 20020318 00208 NM 2002 3 18 SWAA020401 1 20020220 A 3350 900835A BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED C4 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002031800209 20020318 00209 NM 2002 3 18 SWAA020402 1 20020220 A 5320 6517583 STIFFENER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL CHORD CRACKED .50 INCH LONG AT BS 178, WL 183 AND LBL 5.7. REPAIRED CHORD P ER SRM. 2 L 7 2 4F RT A16WE 2002031800210 20020318 00210 NM 2002 3 18 SWAA020411 1 20020222 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 380SW 26587 DURING SCHEDULED SERVICE CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHT INOP AFT OF AFT SERVICE DOOR. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002031800211 20020318 00211 NM 2002 3 18 SWAA020417 1 20020224 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002031800212 20020318 00212 NM 2002 3 18 SWAA020435 1 20020226 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 704SW 27838 EEPLS WIRES LOOSE AT ROW 9. REROUTED AND SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2002031800213 20020318 00213 NM 2002 3 18 AWXA200200224 1 20020317 A 5270 6943439501 BRACKET BOEING 737 7373G7 1384595 NM ZONE 105 LOOSE A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 306AW 24633 LAS - ABORTED TAKEOFF - FLT 8643 - "C" - ON TAKEOFF FROM LAS ENROUTE TO SFO AT 110 KTS THE L1 DOOR MASTER CAUTION LIGHT ILLUMINATED, TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. MAINTENANCE TROUBLESHOT L1 DOOR AND FOUND THE TARGET BRA CKET AND ROLLER NUT LOOSE, BRACKET AND NUT WERE ADJUSTED AND SECURED IAW BMM 52-11-00-501, DOOR SYSTEM WAS OPERATIONALLY TESTED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002031800214 20020318 00214 NM 2002 3 18 AWXA200200226 1 20020303 A 5314 659187911 PANEL BOEING 737 7373S3 1384711 NM BUCKLED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - "C" - DURING C-17 CHECK CENTER KEEL PANEL RIVETS WORKING ALONG ALL 4 SIDES, AND CENTER OF PANEL APP EARS TO BE WAVY. MAINTENANCE REMOVED CENTER KEEL PANEL, LEVELED AIRCRAFT, FABRICATED NEW CENTER KEEL PANEL, AND INSTALLE D REPAIR IAW AWA ER 03-5331-02071-TB2. 2 L 7 2 4F RT A16WE 2002031800215 20020318 00215 EU 2002 3 18 C2XA02IA065 1 20020318 A 3260 842503A PSEU AEROSP ATR42 ATR42320 8680930 EU 80 VU RACK RIGHT INOPERATIVE A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 14834 193 IAH- DURING FLIGHT 3889, THE CREW NOTED THAT THE LANDING GEAR SYSTEM #2(OVERHEAD) RIGHT MAIN INDICATES DOWN IN FLIGHT. IAH- MAINTENANCE REMOVED AND REPLACEDTHE PSEU, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM,VERIFIEDNORMAL GEAR INDICATION, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002031800216 20020318 00216 EU 2002 3 18 C2XA02IA066 1 20020317 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15816 105 IAH- WHILE PERFORMING A LINE CHECK INSPECTION THE MECHANIC NOTED THAT THE EMERGENCY LIGHTING DID NOT ILLUMINATE DURING TESTING. IAH- MAINTENANCE REMOVED AND REPLACED THE (10WL POSITION) EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002031800217 20020318 00217 EU 2002 3 18 C2XA02IA067 1 20020317 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15816 105 IAH- WHILE PERFORMING A LINE CHECK INSPECTION THE MECHANIC NOTED THAT THE EMERGENCY LIGHTING SYSTEM DID NOT ILLUMINATE DURING TESTING. IAH- MAINTENANCE REMOVED AND REPLACED THE (3WL POSITION) EMERGENCY BATTERY, PERFORMED A OPERATIONAL CH ECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, 2 H 7 2 4T RT A53EU 2002031800218 20020318 00218 EU 2002 3 18 C2XA02IA068 1 20020317 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15816 105 IAH- WHILE PERFORMING A LINE CHECK INSPECTION THE MECHANIC NOTED THAT THE EMERGENCY LIGHTING DID NOT ILLUMINATE DURING TESTING. IAH- MAINTENANCE REMOVED AND REPLACED THE (18 WL POSITION) EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK O F THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002031800219 20020318 00219 EU 2002 3 18 C2XA02IA069 1 20020317 A 3350 3011151 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15816 105 IAH- WHILE PERFORMING A LINE CHECK INSPECTION THE MECHANIC NOTED THAT THE EMERGENCY LIGHTING DID NOT ILLUMINATE DURING TESTING. IAH- MAINTENANCE REMOVED AND REPLACED THE (30WL POSITION) EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002031800220 20020318 00220 EU 2002 3 18 C2XA02IA070 1 20020317 A 3350 3011151 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15816 105 IAH- WHILE PERFORMING A LINE CHECK INSPECTION THE MECHANIC NOTED THAT THE EMERGENCY LIGHTING DID NOT ILLUMINATE DURING TESTING. IAH- MAINTENANCE REMOVED AND REPLACED THE (15 WL POSITION) EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK O F THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002031800221 20020318 00221 EU 2002 3 18 C2XA02IA071 1 20020317 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15816 105 IAH- WHILE PERFORMING A LINE CHECK INSPECTION THE MECHANIC NOTED THAT THE EMERGENCY LIGHTINGDID NOT ILLUMINATE DURING T ESTING. IAH- MAINTENANCE REMOVED AND REPLACED THE (15 WL POSITION)EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002031900001 20020319 00001 NM 2002 3 19 HALA0200035 1 20020125 A 3246 TIRE BOEING 717 717200 1383700 NM NLG VIBRATES A HALA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 WP 13 483HA 55128 KOA - FLT 157 - UNUSUAL SOUND HEARD FROM NOSE GEAR AREA DURING TAKEOFF ROLL. ABORTED TAKEOFF. RETURNED TO GATE. REPLA CED NOSE TIRES, SPIN/SECURITY CHECK OK. PER MM 32-42-21. TAXI CHECK OK. (M) 2 L 7 2 4F TR A6WE 2002031900003 20020319 00003 CE 2002 3 19 NSVA0203 1 20020103 A 2910 D10003606 LINE BEECH 1900 1900C 1154161 CE HYD SYSTEM CRACKED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 210CJ UC110 RKD - ON TAKEOFF ROLL OUT HYD LOW ANNUNCIATOR LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANC E AT RKD DECLARED THAT FLUID LEVEL WAS OK FOR 'M' ACTION AND HEF MAINTENANCE CONTROL DEFERRED IT IAW MEL 32-7 CAT 'C'. PILOT WROTE UP THAT THERE WAS FLUID ON THE NACELLE AFTER LANDING IN BHB. MAINTENANCE AT BHB DISCOVERED A LEAK IN THE RE TRACT LINE NEAR HYDRAULIC RES. AIRCRAFT REMOVED FROM SERVICE, SFP TO HYA WAS ISSUED. HYA MAINTNENANCE REMOVED AND REPL ACE DHYD LINE BY RES. LEAK AND OPS CHECK GOOD. (M) 2 L 7 2 4T RT A24CE 2002031900004 20020319 00004 EU 2002 3 19 NSVA0204 1 20020118 A 3213 13889 BEARING SAAB SF340 340B 7860101 EU NLG SEIZED A NSVA O OTHER O OTHER LD LANDING 1 EA 27 237MJ 340B237 ALB - NOSE TIRES FLAT JUST AFTER LANDING, TURNING ONTO TAXIWAY. MAINTENANCE FOUND LEFT INNER BEARING SEIZED ONTO AXLE. BEARING AND AXLE DESTROYED. (M) 2 L 7 2 4T RT A52EU 2002031900005 20020319 00005 EU 2002 3 19 NSVA0205 1 20020127 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A NSVA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 27 239CJ 340B239 ORF - PILOT SQUAWK, CARGO COMPARTMENT SMOKE DETECTOR ANNUNCIATOR ILLUMINATED IMMEDIATELY AFTER START UP. MAINTENANCE PI EDMONT ISOLATED PROBLEM TO DETECTOR AND/OR WEU. SFP ISSUED TO HEF. HEF MAINTENANCE REMOVED AND REPLACED AFT CARGO BAY SMOKE DETECTOR, FUNCTIONAL TEST OK. (M) 2 L 7 2 4T RT A52EU 2002031900006 20020319 00006 CE 2002 3 19 RU3A02001 1 20020116 A 2121 D001846 BLOWER BEECH 300 300BEECH 1152930 CE CABIN OVERHEATED A RU3A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 70 FF5 THE CREW REPORTED SMOKE SMELL IN FLIGHT. MOTOR REMOVED AND REPLACED. APPARENT CAUSE BLOWER MOTOR OVERHEATING. ENGINEE RING DEPARTMENT WILL RESEARCH MOTOR COOLING, AND WILL ISSUE APPROPRIATE TIEO. (M) 2 L 7 2 4T A24CE 2002031900007 20020319 00007 CE 2002 3 19 RU3A02002 1 20020207 A 7500 24540150 CLAMP LEAR 60 60LEAR 5170707 CE VALVE DUCT LOOSE A RU3A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 58 1792 057 AT APPROX 1604Z, DEPARTING RWY 13R WHILE CLIMBING THROUGH 9,000 FOR 25,000 FT, MCT POWER SELECTED, THE RIGHT ENGINE FIRE LIGHT ILLUMINATED. LEVEL OFF AT 22,000 FT INITIATED, ATC NOTIFIED. THE ENGINE FIRE LIGHT EXTINGUISHED, PRECAUTIONARY LANDING MADE AT BFI. NO FURTHER INDICATION OF AN ENGINE FIRE OBSERVED, THEREFORE, ENGINE WAS SHUTDOWN IN FLIGHT, CREW E LECTED TO BURN FUEL IN AN EFFORT TO AVOID OVERWEIGHT LANDING. AIRCRAFT REFERRED TO MAINTENANCE, CAUSE UNKNOWN AT THIS T IME. S/D - MAINTENANCE GROUND RAN ENGINE, FOUND BLEED AIR LEAK AT CLAMP HP AIR MIXING VALVE. LOOSENED CLAMP, INSPECTED AND RETORQUED. OPERATIONAL CHECK SATISFACTORY, NO LEAK DETECTED. (M) 2 L 7 2 4F RT A10CE 2002031900011 20020319 00011 SO 2002 3 19 SIMA200204210 1 20020126 A 5310 BEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AE 145276 ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED CORROS ION AND RETREATED SURFACE IAW EMB REPAIR STATEMENT GST 0332/02. (M) 2 L 7 2 4F RT T00011AT 2002031900012 20020319 00012 SO 2002 3 19 SIMA200204601 1 20020214 A 2560 P2070009120 CHARGER EMB 145 EMB145 3260210 SO FLASHLIGHT MELTED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 607AE 145064 ORD - FLT 4178 BURNING OR HOT INSULATOR ODOR IN THE VICINITY OF THE FA SEAT NOTED DURING DESCENT INTO ORD. AIRCRAFT LA NDED SAFELY NO FURTHER INCIDENTS NOTED. NO EMERGENCY REPORTED. NOTED F/A FLASHLIGHT HOLDER ASSEMBLY DEFORMED. RAI FLA SHLIGHT HOLDER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2002031900013 20020319 00013 EU 2002 3 19 SIMA200204901 1 20020218 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 284AE 340B284 LAX - FLT 3260 - CREW REPORTED THE EMERGENCY LIGHTS AT ROWS 4 AND 5 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLIES 20LN AND 21LN IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 L 7 2 4T RT A52EU 2002031900014 20020319 00014 SO 2002 3 19 SIMA200205103 1 20020220 A 3350 66361 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 639AE 145182 FLT 3570 - CRP - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS FROM ROW 12 AFT WERE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE FLOOR LIGHTING STRIP IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002031900015 20020319 00015 EU 2002 3 19 SIMA200205201 1 20020221 A 3350 CM1317 BULB SAAB SF340 340B 7860101 EU CABIN BURNED OUT A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 272AE 340B272 DFW - FLT 3877 - CREW REPORTED THE OVERHEAD CABIN EMERGENCY LIGHT AT SEAT 14A TO BE INOPERATIVE. LIGHT WAS DEFERRED AND AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE REPLACED BULB AT SEAT 14A. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002031900016 20020319 00016 EU 2002 3 19 SIMA200205301 1 20020222 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 211NE 340B211 SHV - CREW REPORTED THREE FLOOR PROXIMITY EMERGENCY LIGHTS AT ROW 6 AND 7 COME ON FOR 5 SECONDS AND THEN GO OUT. AIRCRA FT WAS INSPECTED AND FERRIED TO DFW FOR REPAIR. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT 22LN IAW SAAB MM. O PERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002031900017 20020319 00017 SO 2002 3 19 SIMA200205401 1 20020223 A 4900 APU EMB 135 EMB135LR 3260305 SO APU BAY FAILED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 731BE 145356 EWR - FLT 4587 - DURING TAXI OUT, CREW NOTED SMOKE IN CABIN AFTER APU FAIL AND SHUT DOWN. CREW RETURNED TO GATE AND PAS ENGERS WERE DEPLANED NORMALLY. NO FURTHER INCIDENTS WERE REPORTED. MAINTENANCE WAS SENT FROM LGA. AIRCRAFT WAS INSPEC TED AND APU WAS DEFERRED. (M) 2 L 7 2 4F RT T00011AT 2002031900018 20020319 00018 SO 2002 3 19 SIMA20204209 1 20020128 A 5320 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AE 145276 MBV - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE LEFT FLOOR SUPPORT IN CARGO BAY AT FRAME 71. MAINTENANC E REMOVED CORROSION AND RETREATED SURFACE IAW EMB REPAIR STATEMENT GST 0331/02. (M) 2 L 7 2 4F RT T00011AT 2002031900019 20020319 00019 NM 2002 3 19 TSAA0233044 1 20020214 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM PAX CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 39735 REPLACED NR 2 FLOOR PATH EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 2002031900020 20020319 00020 NM 2002 3 19 TSAA0251046 1 20020213 A 5310 65827741SP DOOR FRAME BOEING 737 7372S5C 1384499 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 REPAIRED .25 INCH CRACK AT MAIN CARGO DOOR FRAME EXTENDING FROM THE RIVET AT BS 390. CUTOUT AND CONFIRMED CRACK REMOVED USING HFEC METHOD. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-40-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900021 20020319 00021 NM 2002 3 19 0200776624 1 20020308 A 2433 241804 TRANSFORMER BOEING 747 747251B 1384892 NM ELECTRICAL SYS MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 GL 01 624US 21706 DURING DESCENT, A STRONG BURNING SMELL EMITTED IN THE FLIGHT DECK AND BEHIND DOOR 1L FOLLOWED BY A MASTER FIRE WARNING A ND BELL. PULLED ESSENTIAL TRANSFORMER RECTIFIER CIRCUIT BREAKER, DECLARED AN EMERGENCY, AND LANDED THE AIRCRAFT WITHOUT FURTHER INCIDENT. REPLACED THE TRANSFORMER RECTIFIER UNIT, FIRE DETECTION CONTROL ELECTRONICS MODULE WITH CARDS, MAIN AIRCRAFT BATTERY AND BATTERY CHARGER, A-13 CARD IN THE MASTER DIM AND TEST MODULE, AND REPAIRED THE MAIN BATTERY OVERHEA T TEMP SENSOR WIRE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002031900022 20020319 00022 NM 2002 3 19 TSAA0253023 1 20020124 A 5312 65163007 BULKHEAD BOEING 737 7372S5C 1384499 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 FOUND CRACK INDICATION FORWARD SIDE OF LEFT BULKHEAD 178 CENTER WEB LBL 10.0 WI234, ADJACENT TO RIVET HEAD. REMOVED CRA CK AND MAINTAINED A MINIMUM OF .038 INCH AT EACH CORNER OF THE CUTOUT. VERIFIED CRACK REMOVED USING HFEC. MADE AN INSU RANCE CUTOUT .004 INCHES LARGER WITH A MINIMUM RADIUS OF .038 INCH. FABRICATED AND INSTALLED .50 INCH 2024 T3 REPAIR DO UBLER IAW SRM 53-10-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900023 20020319 00023 NM 2002 3 19 TSAA0253034 1 20020108 A 5315 65C3453715 FLOORBEAM BOEING 737 73725A 1384481 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 FOUND CABIN INTERIOR LONGITUDINAL FLOORBEAM UPPER CHORD AND WEB CRACKED AT BS 663.75 BL 0. VERIFIED CRACK REMOVED USING HFEC. REPAIRED LONGITUDINAL FLOORBEAM IAW ECO 223R2 PART II, DEVIATION "C". AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900024 20020319 00024 NM 2002 3 19 TSAA0253035 1 20020108 A 5330 65C372771 SKIN BOEING 737 73725A 1384481 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 REPAIRED A 4 INCH CRACK ON THE FUSELAGE SKIN AT BS 727 JUST BELOW STRINGER 18 RT. VERIFEID CUTOUT USING HFEC. FABRICAT ED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3 PAGE 11 FIGURE 6. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900025 20020319 00025 NM 2002 3 19 TSAA0253036 1 20020108 A 5330 65C372771 SKIN BOEING 737 73725A 1384481 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 REPAIRED A 2.5 INCH CRACK ON THE FUSELAGE SKIN AT BS 727 JUST BELOW STRINGER 19 RT. VERIFIED CUTOUT USING HFEC. FABRIC ATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3 PAGE 11 FIGURE 6. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900026 20020319 00026 NM 2002 3 19 TSAA0253037 1 20020108 A 5522 65C2638428A SKIN BOEING 737 73725A 1384481 NM RT ELEVATOR DELAMINATED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 FOUND DELAMINATION ON LOWER SURFACE OF RIGHT ELEVATOR. TRIMMED OUT DAMAGED LAMINATION TO A SMOOTH SHAPE WITH ROUNDED CO RNERS. FABRICATED, CLEANED AND INSTALLED HONEYCOMB REPLACEMENT CORE PLUG. PREPARED AND APPLIED REPAIR PLIES. INSTALLE D HEATED BLANKET AND EVACUATED THE REPAIR REPAIR AREA MAINTAINING A VACCUM OF 22 INCHES OF MERCURY MINIMUM. REPAIR COMP LETED IAW SRM 51-40-12, REPAIR 14, FIGURE 22. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900027 20020319 00027 NM 2002 3 19 TSAA0253038 1 20020212 A 5330 6545855502 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 REPAIRED 2.5 INCH LONG SKIN CRACK AT FUSELAGE BS 937 STRINGER 26R. CONFIRMED 2.5 INCH REMOVED USING HFEC METHOD. THE R EPAIR CONSISTED OF CUTTING OUT THE SKIN CRACK AND FABRICATING A DOUBLER IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2002031900028 20020319 00028 NM 2002 3 19 TSAA0253040 1 20020108 A 5330 SKIN BOEING 737 73725A 1384481 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 BLENDED OUT CORROSION ON THE FUSELAGE SKIN AT BS 990 STRINGER 27L BY CUTTING STRINGER 27L IAW SRM 51-10-2. VERIFIED COR ROSION REMOVED, CLEANED AND TREATED IAW SRM 51-10-6. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-2 FIGURE 3. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900029 20020319 00029 NM 2002 3 19 TSAA0253041 1 20020108 A 5320 65C3453715 FLOOR SUPPORT BOEING 737 73725A 1384481 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 FOUND CABIN INTERIOR LONGITUTIONAL FLOOR SUPPORT UPPER CHORD AND WEB CRACKED AT BS 663.75 BL 0. VERIFIED CRACK REMOVED USING HFEC. REPAIRED LONGITIONAL FLOORBEAM IAW ECO 2223R2 PART II, DEVIATION 'C'. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900030 20020319 00030 NE 2002 3 19 0200786632 2 20020306 A 7230 COMPRESSOR BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 3 ENGINE STALLED A NWAA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 01 632US 23112 715186 DURING CLIMB AT APPROXIMATELY 5000 FEET, THE NR 3 ENGINE COMPRESSOR STALLED WITH THE LOW OIL PRESSURE WARNING AND A BRIE F FIRE WARNING INDICATION. THE ENGINE WAS SHUT DOWN. AFTER DUMPING FUEL, THE AIRCRAFT RETURNED TO MSP AND LANDED WITHO UT INCIDENT. THE ENGINE WAS REPLACED. OPERATIONAL CHECK GOOD. 2 L 7 4 4F 4 F A20WE E3NE 2002031900031 20020319 00031 NM 2002 3 19 TSAA0253042 1 20020209 A 5730 654549724 SKIN BOEING 737 737209 13844AE NM WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 827AL 23913 FOUND CORROSION ON LOWER SKIN SURFACE AT WS 435.5, WS 542, WS 567, WS 514.5, AND WS 461. CONFIRMED COMPLETE REMOVAL OF CORROSION WITH A 10X VISUAL INSPECTION. EVALUATED REMAINING WING SKIN THICKNESS AND FILLED DEPRESSIONS WITH BMS 5-95 SE ALANT REFERRING TO SRM 51-20-4 IAW ECO 3091. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900032 20020319 00032 NM 2002 3 19 TSAA0253043 1 20020209 A 5314 65306569 KEELBEAM BOEING 737 737209 13844AE NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 827AL 23913 FOUND CORROSION ON LOWER KEEL BEAM SURFACE AT BS 727. CUT OUT SKIN AREA AS REQUIRED TO ACCESS KEEL BEAM LOWER SURFACE. BLENDOUT KEEL BEAM LOWER CHORD SURFACE CORROSION. FABRICATED A FILLER FROM .71 TO .12 INCH 2024-T3. FABRICATED TWO DO UBLERS FROM .063 AND .080 INCH 2024-T3. ASSEMBLED REPAIR PARTS IAW ECO 1972 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 2002031900033 20020319 00033 NM 2002 3 19 TSAA0253047 1 20020218 A 5330 65457702 SKIN BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 REPAIRED 1.25 INCH FUSELAGE SKIN CRACK AT BS 727 STRINGER 15L. CONFIRMED CRACK REMOVED USING HFEC METHOD. FABRICATED A ND INSTALLED A .050 INCH DOUBLER IAW SRM 53030-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002031900034 20020319 00034 NM 2002 3 19 TSAA0255024 1 20020114 A 5551 ATTACH FITTING BOEING 737 7372M6C 1384708 NM HORIZONTAL STAB GOUGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 FOUND GOUGE MARKS ON LEFT HORIZONTAL STABILIZER CENTER SECTION LUG, UPPER FORWARD FITTING. REMOVED GOUGE / DAMAGED MATE RIAL TO A MINIMUM WIDTH OF .10 INCH AND RADIUS OF 1 INCH AND TAPERED. APPLIED A CHEMICAL CONVERSION COATING AND REFINIS HED THE REWORKED SURFACE IAW SRM 55-10-1 FIGURE 6, DETAIL II, VI, AND VII. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900035 20020319 00035 NM 2002 3 19 TSAA0255025 1 20020114 A 5511 65913631 SPAR BOEING 737 7372M6C 1384708 NM HORIZONTAL STAB NICKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 FOUND NICKS ON CENTER SECTION REAR SPAR UPPER FORWARD SIDE FITTING. REMOVED NICKS/DAMAGED MATERIAL TO A MAXIMUM OF .01 INCH AND TAPERED. APPLIED A CHEMICAL CONVERSION COATING AND REFINISHED THE REWORKED SURFACE IAW SRM 55-10-1 FIGURE 6, D ETAIL IX. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900036 20020319 00036 NM 2002 3 19 TSAA0257032 1 20020108 A 5754 114A50403 STRUCTURE BOEING 737 73725A 1384481 NM NR 5 SLAT CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 REPAIRED CRACK AT NR 5 SLAT STATION 195.53. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT L ENGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .050 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 P AGE 1 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900037 20020319 00037 NM 2002 3 19 TSAA0257033 1 20020108 A 5754 114A50403 STRUCTURE BOEING 737 73725A 1384481 NM NR 4 SLAT CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 REPAIRED CRACK AT NR 4 SLAT STATION 35.84. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LE NGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .50 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAG E 2 DETAIL II. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900038 20020319 00038 NM 2002 3 19 TSAA0257039 1 20020108 A 5754 STRUCTURE BOEING 737 73725A 1384481 NM NR 4 SLAT CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 REPAIRED CRACK AT NR 4 SLAT STATION 35.84. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LE NGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .50 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAG E 1 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002031900039 20020319 00039 NM 2002 3 19 UIEA02003 1 20020204 A 5415 65B17255 ATTACH FITTING BOEING 747 7472F6B 1384807 NM NR 4 PYLON SCORED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 534MC 79566 21832 DURING CURRENT C-CHECK AT SIAEC WHILE PERFORMING TERMINATING ACTION PER ATLAS AIR EO 4757A082, NR 4 PYLON LOWER WING DIA GONAL BRACE ATTACH FITTING, TAPER LOCATION INSTALLATION ' FOUND THE LAST THREE FASTENER HOLES SCORED. POSITIONS ARE ONE EACH AT INBOARD 2ND FROM NED, 1 EACH AT INBOARD AFT AND 1 EACH AT OUTBOARD AFT. REAMED HOLES TO .500. PERFORMED OPEN HOLE HFEC INSPECTION. NO FINDINGS. INSTALLED BACB30US8K32 FASTENERS IN LIEU OF TAPER LOCKS PER SRM 51-30. AMOC ISSUED TO SATISFY REQUIREMENTS PER AD 2001-13-06 ON FORM 8110-3. (M) 2 L 7 4 4F A20WE 2002031900040 20020319 00040 NM 2002 3 19 UIEA02004 1 20020204 A 5312 BULKHEAD BOEING 747 7472F6B 1384807 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 534MC 79566 21832 DURING CURRENT C-CHECK AT SIAEC INSPECTION OF BS 2484 UPPER BULKHEAD STRUCTURE DISCOVERED THE WEB CRACKED AT STRINGER 15 L LBL 45 WL 287.03. REMOVED STIFFENER 65B02571-153. TRIMMED OUT CRACK IN WEB AREA. DYE CHECKED AREA. NO FINDINGS. F ABRICATED REPAIR DOUBLER, FILLERS AND REPLACEMENT STIFFENER (65B02571-153) FROM DRAWING 65B02571. INSTALLED PER STANDAR D SRM 51-30 PRACTICES. (M) 2 L 7 4 4F A20WE 2002031900041 20020319 00041 NM 2002 3 19 UIEA02005 1 20020204 A 5340 FITTING BOEING 747 7472F6B 1384807 NM BULKHEAD CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 534MC 79566 21832 DURING CURRENT C-CHECK AT SIAEC WHILE PRFORMING INSPECTION AND REWORK OF THE RIGHT BS 1480 LONGERON AREA PER SB 747-53A2 390 FOUND NR 5 HOLE CORRODED AT BS 1480 RIGHT UPPER LONGERON BULKHEAD FITTING. REAMED HOLE TO .750 INCLUDING INSURANCE CUT. FABRICATED REPLACEMENT BUSHING. INSTALLED BUSHING AND FASTENERS PER ABOVE SB. POST MODIFICATION INSPECTION INTER VAL REDUCED TO 10,000 CYCLES AND REPEAT INSPECTION INTERVALS AT 2700 CYCLES THEREAFTER. AMOC ISSUED FOR REPAIR ON FORM 8110-3. (M) 2 L 7 4 4F A20WE 2002031900042 20020319 00042 NM 2002 3 19 UIEA02006 1 20020202 A 7500 CLAMP BOEING 747 7472D7B 1384803 NM NR 4 ENGINE LOOSE A UIEA O OTHER N FALSE WARNING CL CLIMB 1 EA 15 526MC 22337 LIM/MIA - NR 4 ENGINE FIRE LIGHT CAME ON CLIMBING THROUGH 20.0. BOTH A/B LOOPS WERE AT 9.0. FIRE SWITCH PULLED. FIRE BOTTLE WAS NOT FIRED. HYDRAULIC PUMP NR 4 IN SUPPLY OFF POSITION OR 1 PLUS 30 MINUTES. PERFORMED NACELLE OVERTEMPERATU RE INSPECTION ON NR 4 ENGINE. FOUND LOOSE CLAMP ON 8TH STAGE DUCT. SECURED AS REQUIRED. RAN NR 4 ENGINE. OPS CHECK N ORMAL IAW 71-00-00. (M) 2 L 7 4 4F RT A20WE 2002031900043 20020319 00043 NM 2002 3 19 UIEA02007 1 20020211 A 5711 SPAR BOEING 747 7472D7B 1384803 NM WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 527MC 22471 DURING CURRENT C-CHECK AT KLM/AMS, FOUND LEVEL 1 CORROSION ON THE L/W VERTICAL FLANGE OF THE LOWER FRONT SPAR CHORD BETW EEN ILES 630.72 AND 638 (INBOARD OF NR 2 PYLON). TAPER LOCK FASTENERS IN THE AFFECTED AREA WERE REMOVED. CORROSION BLE NDED AND FASTENER HOLES WERE REAMED AND SPOT FACED TO ENSURE A STRAIGHT HOLE AND FLAT CONTACT AREA. MATERIAL LOSS MEASU RED AT .150 INCH. AN OPEN HOLE HFEC, DYE CHECK AND SURFACE HFEC INSPECTION WAS PERFORMED TO INSURE NO CRACKS/CORROSION REMAINED. NO FINDINGS. AREA FLAP PEENED, ALODINED AND PRIME PAINTED. OVER-SIZED HI-LOCK FASTENERS INSTALLED WET WITH BMS 5-26 SEALANT. TANK SEALED. (M) 2 L 7 4 4F RT A20WE 2002031900044 20020319 00044 WP 2002 3 19 0200799882 1 20020305 A 3231 59164605509 CONTROL VALVE DOUG DC9 DC951 3022051 WP MLG FAULTY A NWAA K NONE P S NO WARNING INDICATION AFFECT SYSTEMS LD LANDING 1 GL 01 670MC 47659 MAIN LANDING GEAR DOORS WERE DAMAGED DURING LANDING AND TAXIING. GEAR DOOR OPEN LIGHT DID NOT ILLUMINATE UNTIL THE AIRC RAFT WAS ON THE GROUND. FLIGHT CREW STOPPED ON THE TAXIWAY UNTIL A GROUND CREW COULD INSPECT THE UNDER CARRIAGE. IT WA S DETERMINED THAT THERE WAS GEAR DOOR DAMAGE BUT OKAY TO TAXI. MAINTENANCE REPLACED THE MAIN GEAR DOOR, DOOR LATCH, TOR QUE TUBE, AND GEAR CONTROL VALVE WITH LINKAGE ALL ON THE LEFT SIDE. THE RIGHT SIDE HAD THE SEQUENCE DRIVE ARM REPLACED. PERFORMED BITE AND GEAR SWING CHECK. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002031900045 20020319 00045 NM 2002 3 19 UIEA02008 1 20020211 A 5310 STRUCTURE BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 05 527MC 80492 22471 DURING CURRENT C-CHECK AT KLM/AMS WHILE PERFORMING SB 747-53A2450, IAW AD 2001-16-02 AND HFEC OPEN HOLE INSPECTION REVEA LED CRACKS EMINATING FROM THE AFT STRAP ROW AT BS 2231, STRINGER 24R AND 25R. CUT OUT BLENDED CRACKS IN STRAP. HFEC IN SPECTED ROUTED AREAS AND ALL OPEN HOLES PER SRM 53-10-04 FIG 115. NO ADDITIONAL CRACKS FOUND. FILLERS AND REPAIR ALUMI NUM STRAPS FABRICATED AND INSTALLED IAW ABOVE SRM TEXT. REPAIR IS A TIME LIMITED REPAIR AND REQUIRES A REPETITIVE 3000 CYCLE INSPECTION. AD REQUIREMENTS NEVER TERMINATE. (M) 2 L 7 4 4F RT A20WE 2002031900046 20020319 00046 NM 2002 3 19 UIEA02009 1 20020211 A 5310 STRUCTURE BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 527MC 80492 22471 DURING CURRENT C-CHECK AT KLM/AMS WHILE PERFORMING SB 747-53A2450, IAW AD 2001-16-02 AND HFEC OPEN HOLE INSPECTION REVEA LED CRACKS EMINATING FROM THE AFT STRAP ROW AT BS 2231, STRINGER 25L. CUT OUT BLENDED CRACK IN STRAP. HFEC INSPECTED R OUTED AREA AND ALL OPEN HOLES PER SRM 53-10-04 FIG 115. NO ADDITIONAL CRACKS FOUND. FILLER AND REPAIR ALUMINUM STRAPS FABRICATED AND INSTALLED IAW ABOVE SRM TEXT. REPAIR IS A TIME LIMITED REPAIR AND REQUIRES A REPETITIVE 3000 CYCLE INSPE CTION. AD REQUIREMENTS NEVER TERMINATE. (M) 2 L 7 4 4F RT A20WE 2002031900047 20020319 00047 EU 2002 3 19 USAASA02020 1 20020214 A 3350 321430 BATTERY AIRBUS 320 A320214 3930316 EU PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 108UW 1061 BDL - AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED BATTERIES. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002031900048 20020319 00048 NM 2002 3 19 USAASB02015 1 20020118 A 2913 PUMP BOEING 737 7373B7 1384580 NM HYD SYSTEM LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 387US 22959 PIT - FLT 1158 - EN ROUTE FROM PBI TO PIT, AT FL370, CREW REPORTED THE SYSTEM B ELECTRIC HYDRAULIC PUMP LOW PRESSURE LIG HT ILLUMINATED. THEN, ON FINAL INTO PIT, SYSTEM B HYDRAULICS FAILED WITH FLAPS SET AT FIVE DEGREES. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MX REMOVED AND REPLACED A LEAKING B SYSTEM HYD RAULIC PRESSURE LINE AT MANIFOLD. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP (P/N 65075-06) PER MM 29-15-12 DUE TO FILTER CONTAMINATION. REMOVED AND REPLACED B SYSTEM ELECTRIC HYDRAULIC PUMP (P/N MPEV3-056-9A) AS PRECAUTIONARY . REMOVED AND REPLACED B SYSTEM RETURN AND CASE DRAIN FILTERS, FLUSHED SYSTEM AND REPLACED FILTERS AGAIN. SERVICED SYS 2 L 7 2 4F RT A16WE 2002031900049 20020319 00049 NM 2002 3 19 USAASB02016 1 20020118 A 3040 2057011 POTENTIOMETER BOEING 737 7373B7 1384580 NM WINDSHILD WIPER FAILED A USAA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 518AU 23704 CLT - FLT 289 - EN ROUTE FROM GSO TO MSY, UPON REACHING FL350, THE CABIN ALTITUDE WARNING HORN SOUNDED AS CABIN PRESSURI ZATION BECAME UNCONTROLLABLE. CREW ACCOMPLISHED AN EMERGENCY DESCENT AND AT FL090 CABIN PRESSURIZATION STABILIZED. CRE W MANUALLY DEPLOYED OXYGEN MASKS DURING EMERGENCY DESCENT AS PRESSURIZATION ASCENDED TO A MAXIMUM OF 12,000 FEET. FLIGH T DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED FUNCTIONAL CHECK OF THE PRESSURE CONTRO LLER PER MM 21-31-00. FOUND THE CAPTAINS ALTIMETER POTENTIOMETER WIPER FOR THE BAROMETRIC CORRECTION OUT OF LIMITS. RE MOVED AND REPLACED CAPTAINS ALTIMETER IN ASSOCIATION WITH MM 34-12-21. ACCOMPLISHED SATISFACTORY PRESSURIZATION CHECK O 2 L 7 2 4F RT A16WE 2002031900050 20020319 00050 NM 2002 3 19 USAASB02017 1 20020119 A 3610 1074922 REGULATOR BOEING 737 7373B7 1384580 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 393US 23315 BOS - FLT 926 - CLIMBING-OUT FROM PHL, EN ROUTE TO PWM AT FL250, THE NR 2 ENGINE BLEED TRIP LIGHT ILLUMINATED. CREW TRI ED TO RESET BLEED WITH NO HELP. WITH NR 2 BLEED INOPERATIVE, PRESSURIZATION WAS OK AT FL250 FOR 15 MINUTES, BUT THEN TH E CABIN PRESSURE BEGAN CLIMBING. FLIGHT DIVERTED TO BOS AND LANDED WITHOUT FURTHER INCIDENT. CREW REPORTED THEY WERE U NABLE TO CONTROL PRESSURIZATION UNTIL APPROX 6,000 FT. NO OXYGEN MASKS WERE DEPLOYED AND NO EMERGENCY WAS DECLARED. MX REMOVED AND REPLACED THE NR 2 ENGINE BLEED AIR REGULATOR. OPS CHECK GOOD PER MM 36-11-16. PERFORMED BLEED CONTROL SYS TEM OPERATIONAL CHECK PER MM 36-11-05, CABIN PRESSURE LEAKAGE CHECK PER MM 05-51-91 AND PRESSURE CONTROL SYSTEM OPS TEST 2 L 7 2 4F RT A16WE 2002031900051 20020319 00051 NM 2002 3 19 USAASB02018 1 20020119 A 5240 6523465 NUT BOEING 737 737301 1384611 NM SERVICE DOOR BROKEN A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 589US 23934 MKE - FLT 1242 - ON CLIMB-OUT FROM MKE, EN ROUTE TO CLT, THE AIRCRAFT WOULD PRESSURIZE. A LOUD AIR NOISE COULD ALSO BE HEARD FROM THE AFT RIGHT SERVICE DOOR AREA. FLIGHT RETURNED TO FIELD AT MKE AND LANDED WITHOUT FURTHER INCIDENT. NO EM ERGENCY WAS DECLARED. MAINTENANCE FOUND THE AFT RIGHT SERVICE DOOR SNUBBER JAM LOCK NUT BROKEN AND THE ROD END BACKED O UT FOUR TURNS. REPLACED LOCK, ADJUSTED SNUBBER, SAFTIED AND RERIGGED DOOR ASSEMBLY. DOOR OPERATIONAL CHECK NORMAL. (M ) 2 L 7 2 4F RT A16WE 2002031900052 20020319 00052 NM 2002 3 19 USAASB02019 1 20020124 A 3350 210310005 FUSE BOEING 737 7374B7 1384702 NM POWER SUPPLY FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 437US 24559 TPA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE AFT EMERGENCY LIGHT AT SEAT ROWS 24 AND 25 INOPERATIVE. MAINTENANCE FOUND THE 5 AMP FUSE BLOWN IN THE M1197 BATTERY POWER SUPPLY. REMOVED AND REPLACED FUSE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002031900053 20020319 00053 NM 2002 3 19 USAASB02020 1 20020124 A 3350 30043229 SOCKET BOEING 737 737301 1384611 NM EXTERIOR LIGHTS CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 23232 IND - MAINTENANCE FOUND THE LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS ON THE EXTERIOR FUSELAGE INOPERATIVE. MAINTENA NCE CLEANED BOTH AFT OVERWING EMERGENCY LIGHT SOCKETS AND RELAMPED BOTH BULBS (P/N 1619) PER MM. OPERATIONAL CHECK GOOD . (M) 2 L 7 2 4F RT A16WE 2002031900054 20020319 00054 NM 2002 3 19 USAASB02021 1 20020125 A 2150 655281050 A/C PACK BOEING 737 737301 1384611 NM A/C BAY FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 336US 23233 CLT - FLT 2434 - FLIGHT DEPARTED DCA WITH THE LEFT PACK ON MEL 21-1A. EN ROUTE TO CLT, AT FL240, THE CABIN ALTITUDE WAR NING HORN SOUNDED AS CABIN BEGAN CLIMBING RAPIDLY. CREW DESCENDED FLIGHT TO FL100 AND SWITCHED TO MANUAL PRESSURIZATION MODE TO CONTROL CABIN. FLIGHT CONTINUED ONTO CLT WHERE IT LANDED WITHOUT FURTHER INCIDENT. MX FOUND THE FWD OUTFLOW V ALVE MOTOR BAD AS VALVE WAS STUCK IN THE OPEN POSITION. REMOVED AND REPLACED VALVE (P/N 32-2684-007) PER MM 21-43-11. WHILE PERFORMING TEST, VALVE FAILED TO MOVE CLOSED WHEN USING THE RECIRCULATION FAN CIRCUIT. REMOVED AND REPLACED AIR C ONDITIONING ACCESSORY UNIT PER MM 21-51-06. VALVE WORKS/CHECKS GOOD WHEN USING RECIRCULATION FAN AND AFT OUTFLOW VALVE 2 L 7 2 4F RT A16WE 2002031900055 20020319 00055 NM 2002 3 19 USAASB02022 1 20020127 A 5270 189929 SWITCH BOEING 737 737301 1384611 NM PAX DOOR OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 588US 23933 PVD - FLT 2576 - AFTER TAKEOFF FROM PVD, EN ROUTE TO PIT, THE AFT LEFT ENTRY DOOR WARNING LIGHT ILLUMINATED. FLIGHT ATT ENDANT RESET THE DOOR HANDLE AND THE LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT PVD AND LANDED WITHOUT FURTHER INC IDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED AFT LEFT ENTRY DOOR LATCHES AND HANDLE OPERATION. FOUND VERY LITTLE HANDLE MOVEMENT TO ILLUMINATE DOOR OPEN LIGHT. ADJUSTED AFT LEFT ENTRY DOOR SWITCH. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002031900056 20020319 00056 NM 2002 3 19 USAASB02023 1 20020130 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM AFT CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 437US 24559 BOS - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS FOR THE AFT SEATS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002031900057 20020319 00057 NM 2002 3 19 USAASB02024 1 20020131 A 2170 V1211 COALESCER BAG BOEING 737 737301 1384611 NM PACK BAYS DIRTY A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 341US 23510 CLT - FLT 1081 - CREW REPORTED A MUSTY SMELL DURING CLIMB-OUT OF PHL BELOW 10,000 FEET AND AGAIN ON DESCENT INTO CLT BEL OW 10,000 FEET. NO SMELL WAS NOTED DURING OTHER FLIGHT PHASES. MAINTENANCE INSPECTED BOTH AIR CONDITIONING PACKS AND F OUND WATER SEPARATORS REMOVING MOISTURE NORMALLY. REMOVED AND REPLACED BOTH WATER SEPARATOR BAGS. OPERATIONAL CHECK GO OD. (M) 2 L 7 2 4F RT A16WE 2002031900058 20020319 00058 NM 2002 3 19 USAASB02025 1 20020131 A 5240 DOOR BOEING 737 7373B7 1384580 NM AFT SERVICE LEAKING A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 514AU 23700 ATL - FLT 2403 - ON CLIMB-OUT FROM ATL, EN ROUTE TO PHL, CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE IN ANY PRESSURI ZATION MODE. FLIGHT RETURNED TO FIELD AT ATL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENA NCE FOUND THE AFT RIGHT SERVICE DOOR NOT SEALING PROPERLY. (M) 2 L 7 2 4F RT A16WE 2002031900059 20020319 00059 NM 2002 3 19 USAASB02027 1 20020204 A 2612 FIRE DETECTOR BOEING 737 7374B7 1384702 NM CARGO BAY FALSE ACTIVATION A USAA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 EA 19 781AU 25020 DCA - FLT 855 - ON SHORT FINAL INTO DCA, FROM MSY, THE AIRCRAFT EXPERIENCED A PRESSURIZATION BUMP THAT DEPRESSURIZED THE CABIN. IMMEDIATELY AFTER THE DEPRESSURIZATION, THE CARGO FIRE LIGHT ILLUMINATED. CREW DISCHARGED THE FIRE BOTTLES AND THE FIRE LIGHT EXTINGUISHED. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED . MAINTENANCE INSPECTED ALL CARGO IN THE AFT CARGO BIN. NO EVIDENCE OF FIRE WAS NOTED. REMOVED AND REPLACED BOTH NR 1 AND NR 2 CARGO FIRE EXTINGUISHER BOTTLES (P/N 34200409-1) AND SQUIBS (P/N 3090852) PER MM 26-19-01. ALSO, REMOVED AND REPLACED LOWER DIVERTER VALVE SQUIB (P/N 3090394) PER MM 26-19-01. OPERATIONAL CHECK OF CARGO FIRE DETECTION SYSTEM NOR 2 L 7 2 4F RT A16WE 2002031900060 20020319 00060 NM 2002 3 19 USAASB02028 1 20020205 A 2611 PU90461R3 SMOKE DETECTOR BOEING 737 737401 1384701 NM FWD LAVATORY MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 413US 23882 CLT - FLT 417 - ON CLIMB-OUT FROM CLT, EN ROUTE TO SRQ, THE FLIGHT ATTENDANT REPORTED THE FORWARD LAVATORY SMOKE DETECTO R ALARM SOUNDING. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. CAP TAIN ADVISED AFTER LANDING THAT THERE WAS NO SMOKE OR FUMES PRESENT. MAINTENANCE REMOVED AND REPLACED THE FORWARD LAVAT ORY SMOKE DETECTOR UNIT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002031900061 20020319 00061 NM 2002 3 19 USAASB02029 1 20020206 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 576US 23741 PHL - MAINTENANCE FOUND THE FORWARD SERVICE DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FOR WARD RIGHT SIDE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002031900062 20020319 00062 WP 2002 3 19 WRLA200204 1 20020215 A 3610 AAM72411 DUCT DOUG DC10 DC1030 3023501 WP PNEUMATIC SYS RUPTURED A WRLA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 27 526MD 46998 EMERGENCY LANDING DUE TO MODERATE CABIN SMOKE/CARGO DECK. REMOVED AND REPLACED AFT LEFT SIDE DUCT ASSEMBLY, P/N AAM7241 -1, DUCT ASSY AFT WELDED. REMOVED AND REPLACED AFT LEFT SIDE DUCT ASSY AFT WELDED. LEFT SIDE AFT FUSELAGE PNEUMATIC DU CT ASSY. (M) 2 L 7 3 4F A22WE 2002031900065 20020319 00065 WP 2002 3 19 0200809923 1 20020306 A 2913 314195 DRAIN VALVE DOUG DC9 DC932 3022066 WP HYD PUMP BLOWN A NWAA H DEACTIVATE SYST/CIRCUITS K J B FLUID LOSS WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 01 927RC 47469 ON TOUCHDOWN AT LANDING, THE RIGHT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED AND THE RIGHT HYDRAULIC QUANTITY DROPPED TO ZERO. FLIGHT CLEARED THE RUNWAY AND TURNED OFF THE RIGHT ENGINE DRIVEN AND AUXILIARY HYDRAULIC PUMPS. DURING TAXI TO G ATE, SOME SMOKE ENTERED THE CABIN, PRESUMABLEY FROM HYDRAULIC FLUID LEAKING ONTO THE APU. NO EMERGENCY WAS DECLARED AND TAXI TO GATE WAS UNEVENTFUL. MAINTENANCE FOUND THE DRAIN MODULE FOR THE RIGHT ENGINE DPI ASSEMBLY BLOWN OFF. REPLACED BOTH CASE AND PRESSURE DRAIN FILTERS AND RIGHT ENGINE DRIVEN AND AUXILIARY HYDRAULIC PUMPS. LEAK AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002031900066 20020319 00066 EU 2002 3 19 02FDEA00202 1 20020316 A 7830 THRUST REVERSER AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 1 ENGINE MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 665FE 769 705229 DURING T/O N1 GOT NR 1 THRUST REVERSER PRESSURIZED ON LEFT ECAM REJECT AT LOW SPEED. PERFORMED FUNCTION CHECK CND. 2 L 7 2 4F 4 F RT A35EU E13NE 2002031900068 20020319 00068 WP 2002 3 19 ABXA010767 1 20020225 A 5730 5912156134 SKIN DOUG DC9 DC941 302207N WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 978AX 47628 INBOARD WING UPPER TRAILING EDGE UPPER SKIN WAS CRACKED ALONG THE TRAILING EDGE NEXT TO INBOARD SPOILER. REPAIRED TRAIL ING EDGE IAW DC-9 SRM 57-01. 2 L 7 2 4F A6WE 2002031900069 20020319 00069 WP 2002 3 19 ABXA010768 1 20020304 A 5320 39197481AX FITTING DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 978AX 47628 FLOORBEAM STATION 965, RIGHT END FITTING EXFOLIATED. REPLACED END FITTING IAW DC-9 SRM 1-30-5. 2 L 7 2 4F A6WE 2002031900071 20020319 00071 WP 2002 3 19 ABXA010771 1 20020225 A 5730 59127365 FINGER DOUBLER DOUG DC9 DC914 3022034 WP LT WING DEBONDED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 OUTBOARD REMOVABLE TRAILING EDGE LOWER SKIN FINGER DOUBLERS WERE DEBONDED. REPLACED UPPER/LOWER SKINS IAW REA D957-4337 9. 2 L 7 2 4F A6WE 2002031900074 20020319 00074 WP 2002 3 19 ABXA010775 1 20020228 A 5280 5910161116 SKIN DOUG DC9 DC914 3022034 WP RT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 RIGHT MAIN LANDING GEAR DOOR INNER SKIN CRACKED JUST AFT OF THE FORWARD HINGE FITTING. REPAIRED CRACKED AREA IAW DC-9 S RM 52-01. 2 L 7 2 4F A6WE 2002031900076 20020319 00076 WP 2002 3 19 ABXA010776 1 20020304 A 5720 39122141 STIFFENER DOUG DC9 DC914 3022034 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 OUTBOARD STATION 91.00, FRONT SPAR VERTICAL STIFFENER, UPPER PORTION WAS CRACKED. REPLACED STIFFENER IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002031900091 20020319 00091 WP 2002 3 19 ARWA20020307 1 20020313 A 2424 1085C VOLT REGULATOR DOUG DC8 DC85F54 3021926 WP ELECTRICAL SYS MALFUNCTIONED A ARWA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 19 426FB 45667 ON FINAL APPROACH SMOKE CAME FROM RT SIDE OF COCKPIT. REMOVED AND REPLACED NR 4 VOLTAGE REGULATOR (BURNT) IAW MM 29-5-1 1, OPS CHECKED NORMAL IAW MM 24-5-1. 2 L 7 4 4F RT 4A25 2002031900097 20020319 00097 WP 2002 3 19 AT0200036 1 20020318 A 3350 276005 FUSE DOUG DC9 DC932 3022066 WP POWER SUPPLY BLOWN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 819AT 47260 FORWARD EMERGENCY PATH LIGHTING WILL NOT ILLUMINATE ON THE FLOOR. INSTALLED FUSE ON FORWARD POWER SUPPLY FOR EMERGENCY PATH LIGHTING REF DC-9 MM 33-53 AND 33-00, OPS CHECK GOOD. 2 L 7 2 4F A6WE 2002031900100 20020319 00100 NM 2002 3 19 2002UALA00377 1 20020313 A 2121 6067723 FAN HONEYWELL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 569UA 26677 ACRID ODOR IN THE CABIN. SUPPLEMENTAL DATA UPDATE RIGHT RECIRCULATION FAN INOP. REPLACED RECIRCULATION FAN. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041000072 20020410 00072 NM 2002 4 10 2002UALA00396 1 20020309 A 2130 13050207 CONTROL PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT DAMAGED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 581UA 5173 26701 LANDING SELECT KNOB INOP. DOES NOT INDICATE ALTITUDE SELECTED. LANDING SELECTOR KNOB STRIPPED. REPLACED CABIN PRESSUR E CONTROL PANEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031900101 20020319 00101 NM 2002 3 19 2002UALA00405 1 20020308 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 BODY STATION 785 STRINGER 1-2 FUSELAGE SKIN IS GOUGED BODY STATION 785 LEFT HAND SIDE, STRINGER 1L-2L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2002031900102 20020319 00102 NM 2002 3 19 2002UALA00407 1 20020309 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 MID CABIN LEFT HAND SIDE, BODY STATION 1020 FUSELAGE FRAME CORRODED AT AFT OB AREA 3 INCHES ABOVE FLOOR LEVEL AND LWR IN BD SURFACE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. CHORD, SPLICE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031900103 20020319 00103 NM 2002 3 19 2002UALA00408 1 20020309 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 FORWARD CABIN FLOORBEAM STATION 310 LBL 18 HAS EXCESIVE MAT LOSS AFTER DAMAGE CLEAN UP. MAJOR REPAIR ACCOMPLISHED. INS TALLED ANGLE AND STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031900104 20020319 00104 NM 2002 3 19 2002UALA00409 1 20020310 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 AFT PIT FRAME STATION 1600 ABOVE STRINGER 26L IB CAP DENTED, SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031900105 20020319 00105 NM 2002 3 19 2002UALA00442 1 20020314 A 5330 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 780UA 26944 LH LOWER SEAL FAIRING SKIN CRACKED AFT OF STA 2268. MAJOR REPAIR ACCOMPLISHED. DAMAGED SKIN AREA REMOVED, FILLERS AND DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002031900106 20020319 00106 NM 2002 3 19 2002UALA00445 1 20020313 A 5315 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 CABIN BODY STATION 400 WL 208 RBL40, FLOORBEAM INTERCOSTAL TOP SURFACE DAMAGED FROM EXCESSIVE MATERIAL LOSS. SUPPLEMENTA L DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031900107 20020319 00107 NM 2002 3 19 2002UALA00446 1 20020313 A 5315 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 FORWARD CABIN RIGHT HAND CREASE BEAM BODY STATION 297-377, RBL 64 HAS EXCESSIVE MATERIAL LOSS ON INBOARD CHORD. SUPPLEME NTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032700062 20020327 00062 NM 2002 3 27 2002UALA00455 1 20020314 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 CABIN FLOOR INTERCOSTAL BETWEEN STATION 324.5 AND 345 HAD EXCESSIVE MATERIAL REMOVED DURING CORROSION CLEAN UP, 3 RBL AN D AT STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032700063 20020327 00063 NM 2002 3 27 2002UALA00456 1 20020315 A 5347 SEAT TRACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 STATION 695 RIGHT HAND INBOARD CABIN SEAT TRACK CORRODED AT SPLICE. MAJOR REPAIR ACCOMPLISHED. REPLACED TRACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2002031900108 20020319 00108 WP 2002 3 19 ABXA010778 1 20020227 A 5700 99193983 SUPPORT DOUG DC9 DC932F 3022067 WP LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 905AX 47147 VERTICAL SUPPORT FOR SLAT MECHANISM MOUNT HAD A CRACK AT LOWER INBOARD MOUNT BOLT. REPLACED VERTICAL SUPORT IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002041700126 20020417 00126 2002 4 17 AWXA200200225 4 20020315 A 3460 B546CCM0104 FMC AIRBUS 320 A320232 3930326 EU E/E BAY FAILED A AWXA A UNSCHED LANDING J F S WARNING INDICATION FLT CONT AFFECTED AFFECT SYSTEMS CL CLIMB 1 WP 28 605AW 2065 543 TAKEOFF FL 180 FMGC NR 1 & 2 FAILED DUMPING PRIMARY & SECONDARY FLT PLANS. AUTOPILOT WOULD NOT EXCEED 5 DEG TURN RATE, RADIO NAV HARD TUNED TO 109.9. VERTICAL RATE OF DESCENT AT TOUCHDOWN 100 FPM. R&R NR 1 & 2 FMGC. OPS CHECK, AUTO-LAND TEST GOOD & NAV DATA UPLOADED. VERIFICATION FLT FOR FMGC UNSATISFACTORY, NR 2 FMGC FAILED CLIMBING THROUGH FL 270, FMG C COULD NOT BE RESET. REPLACED NR 2 FMGC, OPS GOOD. 2ND VERIFICATION FLT SATISFACTORY. FMGC S/N 7600 CONFIRMED FAILUR E AT VENDOR, REPLACED A55 BOARD. FMGC S/N 0726, CONFIRMED FAILURE FAILING PARTS 8-1 & 9 OF FUNCTIONAL TEST, REPLACED A1 3 BOARD. FMGC S/N 6535 PASSED TEST, FAILED SOLDER INSPECTION, RESOLDERED A51 & A53 BOARDS. 2 L 7 2 4F RT A28NM 2002031900110 20020319 00110 NM 2002 3 19 AWXA200200227 1 20020305 A 5311 6546539 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - C - DURING C-17 CHECK A 1.2 INCH CRACK WAS FOUND IN FRAME BS 616 LT WL 200 AT THE FIRST FASTENER AB OVE CENTER WING. 2 L 7 2 4F RT A16WE 2002031900111 20020319 00111 NM 2002 3 19 AWXA200200228 1 20020316 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 326AW 23258 PHX - EEL - C - FLIGHT CREW REPORTED THAT EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT IS INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 8 LT, FUNCTIONAL TEST GOOD. 2 L 7 2 4F RT A16WE 2002031900113 20020319 00113 NM 2002 3 19 AWXA200200229 1 20020318 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 326AW 23258 AUS - EEL - C - EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 LT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY ESCAPE PATH L IGHT ASSEMBLY AT SEAT ROW 12 LT, FUNCTIONAL TEST GOOD. 2 L 7 2 4F RT A16WE 2002031900114 20020319 00114 SO 2002 3 19 C2XA02CL078 1 20020317 A 3350 110049 CHARGER EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14938 145029 DURING ROUTINE MAINTENANCE FOUND STRIPS 2 AND 3 OF THE EMERGENCY AISLE PATH LIGHTING, AND THE CABIN SERVICE DOOR EXTERIO R LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002031900116 20020319 00116 NM 2002 3 19 CALA0200132 1 20020315 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 23577 INSPECTION FOUND RT WHEEL WELL WASHERS FRETTING INTO KEEL BEAM FROM STA 663-727. REPAIRED IAW ECRA 5311-01115. 2 L 7 2 4F RT A16WE 2002031900117 20020319 00117 NM 2002 3 19 CALA0200135 1 20020317 A 5320 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND RT AFT LAV ANGLE STRAP CORRODED BETWEEN STA 986 AND 1006. A NEW ANGLE STRAP WAS INSTALLED IAW SRM 51-3 0-2. 2 L 7 2 4F RT A16WE 2002031900118 20020319 00118 NM 2002 3 19 CALA0200136 1 20020317 A 2760 A614463 VALVE BOEING 737 7373T0 1384582 NM GROUND SPOILER INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 77303 23354 THE LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION AFTER TAKEOFF FROM MSY. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO MSY WHERE IT LANDED SAFELY. MAINTENANCE FOUND THE GROUND SPOILER INTERLOCK VALVE AT FAULT. THE GROUND SPOILER INTERLOCK VALVE WAS REMOVED AND REPLACED AND SAFETY SENSORS WERE ADJUSTED IAW MM 27-62-61. THE GEA R WAS SWUNG SEVERAL TIMES AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2002031900119 20020319 00119 NM 2002 3 19 CALA0200137 1 20020318 A 5510 FITTING BOEING 737 737524 1384721 NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33637 27540 INSPECTION FOUND LT HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR UPPER FORWARD AND AFT LUGS CORRODED. OVERSIZED BUSH INGS WERE INSTALLED AT EACH LOCATION IAW CMM 55-10-06. 2 L 7 2 4F RT A16WE 2002031900120 20020319 00120 NM 2002 3 19 CALA0200138 1 20020318 A 5510 FITTING BOEING 737 737524 1384721 NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33637 27540 INSPECTION FOUND RT HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR UPPER FORWARD LUG CORRODED. AN OVERSIZED BUSHING WA S INSTALLED IAW MM 55-10-06. 2 L 7 2 4F RT A16WE 2002031900121 20020319 00121 EU 2002 3 19 DHL2002364002 1 20020316 A 2612 CONNECTOR AIRBUS 300 A300B4203 3930306 EU FIRE DETECTION DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 364DH 141 ENGINE NR 1 FIRE LOOP A FAILS TO TEST. FOUND NACELLE LOOP CONNECTOR DIRTY, (25WD-A) CLEANED & SECURED, OPS CHECKED GOOD PER MM 26-12-00. 2 L 7 2 4F RT A35EU 2002031900122 20020319 00122 NM 2002 3 19 DHL2002747001 1 20020316 A 3040 MOTOR BOEING 727 727224 1384076 NM WINDSHIELD WIPER FAILED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 747DH 22253 CAPTAINS WINDSHIELD WIPER INOPERATIVE WILL NOT OPERATE IN ANY SPEED FAILS TO PARK. REMOVED AND REPLACED CAPT WIPER MOTO R PER BMM 30-42-12. SYST OPS CHECKS NORMAL. 2 L 7 3 4F A3WE 2002040100131 20020401 00131 WP 2002 4 1 DHL2002801007 1 20020315 A 3340 LIGHT DOUG DC8 DC873F 302199F WP NLG BROKEN A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 801DH 46033 DURING T/O ROLL AT APPROX 100 KTS A LOUD BANG WAS HEARD FOLLOWED BY ILLUMINATION OF THE MASTER CAUTION LIGHT. TAKEOFF W AS REJECTED. PERFORMED VISUAL INSPECTION OF NLG AREA FOUND RT NLG LANDING LIGHT HAD FAILED AND SHATTERED CAUSING A LOUD BANG NOISE. PERFORMED ENG RUN W/CREW ELECTRICAL SYS CHECKED NORMAL, NO DEFECTS NOTED WITH MASTER. 2 L 7 4 4F RT 4A25 2002031900126 20020319 00126 NE 2002 3 19 MALA020193 2 20020311 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT ERRATIC A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 413XJ 340B413 DURING FLIGHT 2900, LT ENGINE AND TEMP SPIKES. LT ENGINE SHOWED ERRATIC INDICATIONS IN CRUISE. FLIGHT BROUGHT PL TO FL IGHT IDLE AND INDICATIONS AND AND NOISES STOPPED. A/C DIVERTED INTO FWA. MAINTENANCE BORESCOPED LT ENGINE AND THOROUGH LY INSPECTED ENGINE. NO DEFECTS NOTED GROUND RAN A/C AT POWER FOR 25 MINUTES AND AT CRUISE CONFIGURATIONS, NO ENGINE FL UCTUATION NOTED AT THIS TIME. PERFORMED ALL ENGINE AND GPA RUNS, A/C MAKES POWER AS REQUIRED. A/C TO BE RETURNED TO SE RVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2002031900128 20020319 00128 EU 2002 3 19 MALA020194 1 20020311 A 7712 TORQUE SENSOR SAAB SF340 340B 7860101 EU LT ENGINE FAULTY A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 420XJ 340B420 DURING FLIGHT 2771 LT TORQUE INDICATOR DROPPED TO ZERO INFLIGHT. MAINTENANCE COULD NOT DUPLICATE, REPLACED TORQUE SENSO R. 2 L 7 2 4T RT A52EU 2002031900130 20020319 00130 EU 2002 3 19 QXEA0200349 1 20020214 A 5530 BOSS FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - PIP PIN BOSS HAS STEP WEAR AT THE RT SIDE OF THE UPPER REMOVABLE FALSE RIB FOR PANEL 55F. REPAIRED IAW HORIZON AI R EA 4-55-301. 2 L 7 2 4F RT A20EU 2002031900132 20020319 00132 EU 2002 3 19 QXEA0200368 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK AT FRAME 9305B FORWARD TO FRAME 6805 INBOARD FLANGE HAS PITTING AND LIGHT CORROSION. REPAIR ED IAW FOKKER SRM AND MM. 2 L 7 2 4F RT A20EU 2002031900134 20020319 00134 EU 2002 3 19 QXEA0200369 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK AT FRAME 9305B FORWARD INSIDE CHANNEL HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031900135 20020319 00135 EU 2002 3 19 QXEA0200370 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK FROM FRAME 9305B TO FRAME 6805 LUGS AT SEAT TIE DOWN HAVE GOUGES. REPAIRED IAW FOKKER MM 53 -40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 2002031900137 20020319 00137 EU 2002 3 19 QXEA0200371 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK FROM FRAME 9305B TO FRAME 6805 LUGS HAVE GOUGES AT SEAT TIE DOWN. REPAIRED IAW FOKKER MM 5 3-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 2002031900138 20020319 00138 EU 2002 3 19 QXEA0200372 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK AT FRAME 8305 FORWARD OUTBOARD FLANGE HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031900139 20020319 00139 EU 2002 3 19 QXEA0200373 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK FROM FRAME 8805 ALONG OUTBOARD FLANGE HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031900141 20020319 00141 EU 2002 3 19 QXEA0200374 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK AT FRAME 9035A FORWARD ALONG INBOARD FLANGE HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031900142 20020319 00142 EU 2002 3 19 QXEA0200375 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK AT FRAME 9035A INBOARD FLANGE HAS CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031900143 20020319 00143 EU 2002 3 19 QXEA0200376 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK INBOARD FLANGE AROUND RECEPTACLE HOLE JUST FORWARD OF FRAME 9305B HAS CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031900144 20020319 00144 EU 2002 3 19 QXEA0200377 1 20020215 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CABIN FLOORBEAM ON LT SIDE IS DENTED ON LOWER FLANGE BETWEEN FRAMES 13815 AND 13815A. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031900149 20020319 00149 EU 2002 3 19 QXEA0200378 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK FRAME 9305B INSIDE CHANNEL THERE IS CORROSION. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002031900151 20020319 00151 EU 2002 3 19 QXEA0200379 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK FROM FRAME 12405 TO FRAME 9305B WHERE SEAT ATTACHES TO TRACK LUGS HAVE GOUGES. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002031900152 20020319 00152 EU 2002 3 19 QXEA0200380 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK FROM FRAME 12405 INSIDE TUNNEL THERE IS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031900153 20020319 00153 EU 2002 3 19 QXEA0200381 1 20020217 A 5720 ATTACH ANGLE FOKKER F28 F28MK4000 4990810 EU LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT WING LOWER WING-TO-FUSELAGE CONNECTION ANGLE FOR WING-TO-FUSELAGE FAIRING CONNECTION ANGLE IS CRACKED. REPAIRE D IAW FOKKER SRM 51-31-01, PAGE 13 AND SRM 51-31-02, PAGES 9-10, PARAGRAPHS 4B AND 4C. 2 L 7 2 4F RT A20EU 2002031900154 20020319 00154 EU 2002 3 19 QXEA0200382 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK AT FRAME 13815 AFT INSIDE TUNNEL HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031900155 20020319 00155 EU 2002 3 19 QXEA0200383 1 20020217 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK AT FRAME 13815 AFT OUTBOARD FLANGE THERE IS CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031900156 20020319 00156 EU 2002 3 19 QXEA0200384 1 20020217 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK AFT OF FRAME 13815A INSIDE CHANNEL HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031900157 20020319 00157 EU 2002 3 19 QXEA0200385 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK FORWARD OF FRAME 13815B INSIDE THE TUNNEL HAS PITTING AND CORROSION. REPAIRED IAW FOKKER S RM. 2 L 7 2 4F RT A20EU 2002031900158 20020319 00158 EU 2002 3 19 QXEA0200386 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK AT STATION 667.906 TO STATION 667.901 INSIDE TUNNEL HAS PITTING AND CORROSION. REPAIRED IA W FOKKER SRM. 2 L 7 2 4F RT A20EU 2002031900159 20020319 00159 2002 3 19 372PA0005 4 20020315 A 2210 AUTOPILOT SYS BOEING 737 737306 NM A PIDA O OTHER O OTHER DE DESCENT 1 SO 05 372PA 23546 V-Nav Disconnect in descent. A/T @ A/T limit. Aircraft abandoned path descent. Op's Ck's OK 2 L 7 2 4F RT A16NE 2002031900160 20020319 00160 EA 2002 3 19 COMA0260188 1 20020318 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 963CA 13459 7127 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 540EB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002032500077 20020325 00077 2002 3 25 372PA0006 4 20020315 A 2210 AUTOPILOT SYS BOEING 737 737306 NM COCKPIT MALFUNCTIONED A PIDA K NONE O OTHER CR CRUISE 1 SO 05 372PA 23546 AUTOPILOT & FD ON INTERSECTION OF LOC, AP TURNED OPPOSITE DIRECTION. CAPT WAS MASTER. CAPT'S INDICATIONS WERE WRONG. F/O INDICATIONS WERE CORRECT. OP'S CHECK OK. 2 L 7 2 4F RT A16NE 2002031900161 20020319 00161 EA 2002 3 19 COMA0260189 1 20020309 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 915CA 7013 FLIGHT 5295 GEAR DISAGREE WARING NLG SLOW TO EXTEND.COULD NOT DUPLICTE. RETRACT CHECKS WERE NORMAL. 2 L 7 2 4F RT A21EA 2002031900162 20020319 00162 EA 2002 3 19 COMA0260190 1 20020314 A 2720 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 01 455CA 1138 7592 FLIGHT 5819 RUDDER PULSED LEFT AND RIGHT DURING DECENT.REPLACED THE #1 AND #2 FCC. 2 L 7 2 4F RT A21EA 2002031900163 20020319 00163 EA 2002 3 19 COMA0260192 1 20020314 A 2740 70607 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 960CA 19953 7117 FLIGHT 5860 MACH TRIM/STAB TRIM CAUTION MESSAGE.REPLACED THE HSTCU. 2 L 7 2 4F RT A21EA 2002031900164 20020319 00164 2002 3 19 COMA0260193 4 20020314 A 3418 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 735CA 7267 FLIGHT 5529 STALL FAIL MESSAGE AFTER T/O.RESET THE STALL COMPUTER - SYSTEM CHECK NORMAL. 2 L 7 2 4F RT A21EA 2002031900165 20020319 00165 EA 2002 3 19 COMA0260194 1 20020315 A 3010 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 938CA 7046 FLIGHT 5294 LEFT WING ANTI ICE CAUTION MESSAGE DURING T/O.COULD NOT DUPLICATE. SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 2002031900166 20020319 00166 EA 2002 3 19 COMA0260195 1 20020315 A 2760 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 938CA 7046 FLIGHT 5294 CONFIG SPOILER WARNING DURING T/O.COULD NOT DUPLICATE SYSTEM OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A21EA 2002031900167 20020319 00167 EA 2002 3 19 COMA0260196 1 20020315 A 5270 840534 SWITCH CNDAIR CL600 CL6002B19 1900309 EA DOOR MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 01 716CA 7250 FLIGHT 5620 UNABLE TO PRESSURIZE CABIN AFTER T/O.REPLACED CABIN DOOR PROX SWITCH PS2M13. 2 L 7 2 4F RT A21EA 2002032500110 20020325 00110 2002 3 25 COMA0260191 4 20020314 A 2210 6229968001 DAMPER CNDAIR CL600 CL6002B19 1900309 EA RUDDER FAULTY A COMA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 455CA 2712 7592 FLIGHT 9468 YAW DAMPER NR 1 INOP MESSAGE. REPLACED YAW DAMPER NR 1. 2 L 7 2 4F RT A21EA 2002031900168 20020319 00168 WP 2002 3 19 MWEA020172 1 20020319 A 5750 99576007 ANGLE DOUG DC9 DC932 3022066 WP LEFT WING BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING OUTBOARD FLAP HINGE FITTING INBOARD ATTACH ANGLE IS BROKEN. -- LOCATED, DRILLED & DEBURRED INBOARD ATTACH AN GLE AND INBOARD RIB ANGLE AND INSTALLED. 2 L 7 2 4F A6WE 2002032500112 20020325 00112 NM 2002 3 25 F3LA200200108 1 20020314 A 5313 STRINGER BOEING 737 7373S1 138447S NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 3167 24856 DURING C-5 CHECK, INSPECTION REPORTED CRACK ON STRINGER 6L, STA 798. 2 L 7 2 4F RT A16WE 2002031900170 20020319 00170 EU 2002 3 19 QXEA0200394 1 20020214 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - DENT AFT OF LT FRAME 3050 AND 12 INCHES BELOW D-WINDOW FRAME BASE. REPAIRED IAW FOKKER SRM 53-02-05, FIGURE 1, SR M 53-02-02 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002031900171 20020319 00171 NM 2002 3 19 249TR0001 1 20020318 A 3350 BATTERY PACK BOEING 737 7372K5 138448X NM A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 Aft service door, aft entry door and fwd entry door emergency lights are inop. R&R battery pack/light assy. 2 L 7 2 4F RT A16WE 2002050900042 20020509 00042 NE 2002 5 9 ZW0A0203001 2 20020312 A 7250 775404 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT ENGINE FAILED A ZW0A A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 CE 13 905TW 49157 3223 A LOUD BANG WAS HEARD FROM THE RIGHT ENGINE AND THE ENGINE SHUT ITSELF DOWN. THE FLIGHT RETURNED TO AIRPORT AND THE ENGI NE WAS REPLACED. A FOURTH STAGE TURBINE BLADE HAD FAILED. 2 L 7 2 4F 4 F A6WE E9NE 2002031900172 20020319 00172 EU 2002 3 19 C2XA02IA072 1 20020318 A 3260 842503A PSEU AEROSP ATR42 ATR42320 8680930 EU 90 VU RACK FALSE INDICATION A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 14834 19704 19704 193 IAH - FLT 3695 - Crew reported that the number 2 gear system showed a down indication. The aircraft landed at IAH where mainetanance removed and replaced the proximity switch electronic unit. Gear swings were acvcomplished and the aircraft was approved for return to service. 2 H 7 2 4T RT A53EU 2002031900173 20020319 00173 WP 2002 3 19 0200619608 1 20020212 A 5280 DOOR DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608NW 47233 During H-ck in DHN, a crack was found in the inner skin of the LH MLG INBRD door, just aft of the actuator fitting. This EA 96-188201 provides instruction for the trim out of crack damage and installation of a larger internal doubler.Materi al .050" 7075-t6 2 L 7 2 4F A6WE 2002031900174 20020319 00174 WP 2002 3 19 0200629903 1 20020213 A 5310 PRESSURE PANEL DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 953N 47083 During M-ck in ATL, cracks were found in the flight compartment horizontal pressure panel at sta 105. The cracks are loc ated at RH x=35 1.0" and RH X=25 1.0". Repaired per EA 99-185564. 2 L 7 2 4F A6WE 2002031900175 20020319 00175 WP 2002 3 19 0200639903 1 20020222 A 5310 FRAME DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 953N 47083 During M ckin ATL, Sta 1076 frame was found cracked at longeron 15L. EA 99-185571 allows for repair for the frame. 2 L 7 2 4F A6WE 2002031900176 20020319 00176 WP 2002 3 19 0200649937 1 20020306 A 5310 SKIN DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 908H 47517 During stop over in STL while inspecting the fwd airstair door cutout, 2 cracks were found in the fuselage skin at the l ower aft corner. One crack is approx. .025" long and extends FWD from fastener hole. The second crack is .050" long and extends aft from the lower corner radius. Repaired per EA 99-185358. 2 L 7 2 4F A6WE 2002031900177 20020319 00177 WP 2002 3 19 0200659608 1 20020212 A 5230 DOOR FRAME DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608NW 47233 During Hck in DHN, crack damage was found in the radius underneath AFT Cargo doorstop number #2 and just inboard of the fastener location common to doorstop #2. Repaired per EA 96-188357. 2 L 7 2 4F A6WE 2002031900178 20020319 00178 WP 2002 3 19 0200669608 1 20020215 A 5330 DOUBLER DOUG DC9 DC941 302207N WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608NW 47233 During HCK in DHN, the ground power access door doubler was noted as being cracked at sta 94.5 LBL 41 forward lower corn er. The skin was not damaged. the Damaged area was trimmed out from the OEM doubler. Repaired per EA. 96-188359. 2 L 7 2 4F A6WE 2002031900179 20020319 00179 WP 2002 3 19 0200689608 1 20020220 A 5210 DOOR DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608NW 47233 While station in DHN for an H ck, a hole and crack were found in the fwd side of the door pan of the fwd entry door.Repa ired per EA 96-188361. 2 L 7 2 4F A6WE 2002031900180 20020319 00180 WP 2002 3 19 0200699865 1 20020212 A 5720 SPAR CAP DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 During MCK in ATL, corrosion was found above the inboard and outboard stud holes in the right wing rear spar upper cap a t station xrs 267. Repaired per EA 98-185519. 2 L 7 2 4F RT A6WE 2002031900181 20020319 00181 WP 2002 3 19 0200709865 1 20020218 A 5330 SKIN DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 During Mck in ATL, a .4" crack was found in the upper corner of the forward passenger door jamb. This was repaired per E A 98-185548. 2 L 7 2 4F RT A6WE 2002031900182 20020319 00182 WP 2002 3 19 0200719865 1 20020218 A 5310 LONGERON DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 During Mck in ATL, a crack was found in the 9911557-3 intercoastal that extends from station 148.5 to 160 at approximate ly z=44. The crack extended from the upper edge of the inbrd flange to the forward most lightning hole. repaired per EA 98-185566. 2 L 7 2 4F RT A6WE 2002031900183 20020319 00183 WP 2002 3 19 0200729871 1 20020219 A 5310 BRACKET DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 780NC 48102 During MCK in ATL, the left and right brackets 9957860-5/6 were found cracked. Repaired per EA 98-185579. 2 L 7 2 4F RT A6WE 2002031900184 20020319 00184 WP 2002 3 19 0200739865 1 20020220 A 5330 DOOR FRAME DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 During MCK in ATL a 3/8"long crack was found in the upper corner of the forward cargo door jamb. The crack was repaired per AMI-task and EA 98-185559. 2 L 7 2 4F RT A6WE 2002031900185 20020319 00185 WP 2002 3 19 0200742002 1 20020301 A 5410 RIB DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 During MCK in ATL, the aft end of the 99158159-57 lower cap of the pylon closing rib was completely severed by a crack. This EA 98-188392 provides the means for repair of the rib. 2 L 7 2 4F RT A6WE 2002031900186 20020319 00186 WP 2002 3 19 0200759865 1 20020303 A 5410 RIB DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 During MCK in ATL, the upper cap of the closing rib was found cracked at YN 146. The crack was stop drilled at 2 ends an d a repair angle was installed. Repaired per EA 98-188393. 2 L 7 2 4F RT A6WE 2002031900187 20020319 00187 WP 2002 3 19 0200769871 1 20020305 A 5310 WEB DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 780NC 48102 During MCK in ATL, the LHS and RHS indicator panel was found with .5" crack. EA 98-188387 provides repair for this. 2 L 7 2 4F RT A6WE 2002032500114 20020325 00114 NM 2002 3 25 F3LA200200109 1 20020314 A 5330 SKIN BOEING 737 73736E 138443A NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 314FL 3489 25256 DURING C-2 CHECK, INSPECTION REPORTED CRACKS IN SHEET METAL AFT OF FWD CARGO COMPARTMENT DOOR. FABRICATED AND INSTALLED REPAIR PER SRM 51-70-13. 2 L 7 2 4F RT A16WE 2002031900188 20020319 00188 NM 2002 3 19 P5CA00200666 1 20020318 A 5350 NONE SKIN BOEING 747 747122 1384872 NM TAIL/FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 CRACK FOUND IN BODY TAIL LOWER SKIN AT STATION 2280. CRACK CUT OUT, PACKER FITTED & NEW REPAIR DONE ON OUTER SKIN AS PER SRM 53-30-03. 2 L 7 4 4F A20WE 2002031900189 20020319 00189 NM 2002 3 19 P5CA0200667 1 20020318 A 5280 NONE PANEL BOEING 747 747122 1384872 NM RH MLG WING DOOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DELAMINATION FOUND ON RH MLG WING DOOR INBRD PANEL #723. DELAMINATED DOUBLER REPLACED REF SRM 51-40-05 2 L 7 4 4F A20WE 2002032000020 20020320 00020 NM 2002 3 20 02FDEA00204 1 20020319 A 2750 2061131 INDICATOR BOEING 727 727227 1384078 NM FLT DECK K FAILED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 483FE 21465 02-71 ASYMMETRICAL INBD FLAPS DUR RETRACT STOPPED BETWEEN 5 DEG & 2 DEG. R&R INBD FLAP IND PER MM 27-52-021-2. 2 L 7 3 4F A3WE 2002032000021 20020320 00021 NM 2002 3 20 02FDEA00205 1 20020316 A 2780 40173 SWITCH BOEING 727 727233 138408A NM #1 L/E FLAP FAILED A FDEA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 25 275FE 22040 02-72 #1 L/E FLAP W/N RETRACT ON TAKEOFF. R&R #1 L/E FLAP WARN SWITCH PER 27-82-001-4. R&R LINKAGE & MOUNT BRACKET PER 27-82-001-4. 2 L 7 3 4F RT A3WE 2002032000042 20020320 00042 NM 2002 3 20 2002UALA00367 1 20020308 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 EXTERNAL FUSELAGE SKIN IS DENTED AT STATION 937 STRINGER 20L + 9 INCHES. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000043 20020320 00043 NM 2002 3 20 2002UALA00369 1 20020304 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 192UA 26881 EEL LIGHT ON DOOR 4 LEFT DIM. SECURED CONNECTOR, OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000050 20020320 00050 NM 2002 3 20 PCAA0203037 1 20020319 A 2770 82740037101 SPRING DHAV DHC8 DHC8102 2809003 NM BROKEN A PCAA O OTHER O OTHER NR NOT REPORTED 1 EA 13 836EX 297 PHL-FLIGHT#3631. CREW REPORTED THAT THE GUST LOCK STICKS GOING ON OR OFF. MAINTENANCE REPLACED THE GUST LOCK SPRINGS IN ACCORDANCE WITH THE DEHAVILLAND MAINTENANC EMANUAL 27-70. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002032500117 20020325 00117 NM 2002 3 25 F3LA200200111 1 20020316 A 5313 STRINGER BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 314FL 3489 25256 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR STRINGER AT STA 793, RBL 3. FABRICATED AND INSTALLED REPAIR PE R SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002032000076 20020320 00076 NM 2002 3 20 2002UALA00392 1 20020308 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 FUSELAGE FRAME 727D UPPER FRAME FLANGE DENTED ABOVE STRINGER 24R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTAL LED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000078 20020320 00078 NM 2002 3 20 2002UALA00393 1 20020308 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 FUSELAGE FRAME AT STATION 827 UPPER FLANGE DENTED AT STRINGER 22L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTA LLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000081 20020320 00081 NM 2002 3 20 2002UALA00394 1 20020309 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 FUSELAGE STATION 188 FRAME OUTER CHORD CRACKED IN RADIUS AT WL 207 LEFT SIDE. MAJOR REPAIR ACCOMPLISHED. FABRICATED AN D INSTALLED WEB REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000083 20020320 00083 NM 2002 3 20 2002UALA00395 1 20020309 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE DENTED AT STATION 807 TO 837 AND STRINGER 24R TO STRINGER 27R. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLE R REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000084 20020320 00084 NM 2002 3 20 2002UALA00397 1 20020309 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 AFT CABIN STATION 947 LBL 5 AND LBL 15 HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM UPPE R CAP WITH SINGLE FLANGE BLEND OUT REPAIR. INSTALLED SINGLE REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000087 20020320 00087 NM 2002 3 20 2002UALA00398 1 20020310 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 CABIN BODY STATION 847 BETWEEN STRINGER 8R AND 9R FRAME IS CRACKED AT FASTENER HOLE FOR VENT BRACKET. MAJOR REPAIR ACCO MPLISHED. INSTALLED REPAIR CHANNEL (ANGLES) DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000088 20020320 00088 NM 2002 3 20 2002UALA00399 1 20020310 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 CABIN BODY STATION 827 FRAME BETWEEN STRINGER 8R AND STRINGER 9R, FRAME IS CRACKED AT FASTENER HOLE FOR VENT BRACKET (AF T SIDE). MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR CHANNEL (ANGLE) DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000090 20020320 00090 NM 2002 3 20 2002UALA00400 1 20020307 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 108UA 26903 EEL STRIP INOP IN FRONT OF LAV 104. SECURED LOOSE POWER STRIP CONNECTOR. OPS CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000091 20020320 00091 NM 2002 3 20 2002UALA00401 1 20020306 A 3350 SIGN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26876 EMERGENCY EXIT SIGN OVER RIGHT SIDE UPPER DECK DOOR IS INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000092 20020320 00092 NM 2002 3 20 2002UALA00402 1 20020306 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26876 OVERWING EMERGENCY EXIT LIGHTS ON THE LEFT HAND SIDE, THE 3RD AND 4TH ASSEMBLIES ARE INOP. REPLACED FUSE AND OPS CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000094 20020320 00094 NM 2002 3 20 2002UALA00403 1 20020309 A 5330 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 798UA 26928 LT FUSELAGE SKIN AT LOWER END OF HORIZ STAB BOX CUTOUT, BS 2268, SEAL FAIRING SKIN IS CRACKED. MAJOR REPAIR ACCOMPLISHE D. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002032000096 20020320 00096 NM 2002 3 20 2002UALA00404 1 20020309 A 5330 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 798UA 26928 RT FUSELAGE SKIN AT LOWER FWD END OF HORIZ STAB BOX CUTOUT, BS 2268, SEAL FAIRING SKIN IS CRACKED. MAJOR REPAIR ACCOMPL ISHED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002032000097 20020320 00097 NM 2002 3 20 2002UALA00406 1 20020311 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 ON AFT PRESS CABIN PRESSURE DECK DUE TO EXCESS MAT'L LOSS AT LBL 11 TO LBL 13 AMD STATION 1680 TO STATION 1683. MAJOR R EPAIR ACCOMPLISHED. REPAIRED WITH DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000098 20020320 00098 NM 2002 3 20 2002UALA00410 1 20020308 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 CABIN FLOORBEAM GOUGED, STATION 680 LBL 22, UPPER CAP OF CABIN FLOOR. MAJOR REPAIR ACCOMPLISHED. T-CAP REPAIR INSTALLE D. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000099 20020320 00099 NM 2002 3 20 2002UALA00411 1 20020309 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 CABIN FLOORBEAM MATERIAL REMOVED EXCEEDS LIMITS STATION 345 RBL 61. MAJOR REPAIR ACCOMPLISHED. TOP T-CAP SPLICED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000100 20020320 00100 NM 2002 3 20 2002UALA00412 1 20020309 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 AFT CABIN LEFT HAND CREASE BEAM INBOARD CHORD DUE TO CORROSION AT STATION 1584 AND LBL 64. MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVED AND REPAIRED SLICED IN WITH REINFORCING ANGLES AND FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000101 20020320 00101 NM 2002 3 20 2002UALA00413 1 20020309 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 RIGHT HAND CREASE BEAM INBOARD CHORD HAS CORROSION ON TOP AND BOTTOM AT STATION 755 TO STATION 780. MAJOR REPAIR ACCOMP LISHED. REPLACED DAMAGE CHORD SECTION AND INSTALLED SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000102 20020320 00102 NM 2002 3 20 2002UALA00414 1 20020309 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 CREASE BEAM I/B CHORD AT DOOR 2R IS CORRODED STATION 720 TO STATION 755. MAJOR REPAIR ACCOMPLISHED. I/B CHORD OF CREAS E REPLACED AND INSPECTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032700049 20020327 00049 NM 2002 3 27 2002UALA00415 1 20020312 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 AFT CARGO DOOR CUTOUT AFT EDGE DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032700054 20020327 00054 NM 2002 3 27 2002UALA00416 1 20020312 A 5230 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 AFT CARGO DOOR FORWARD EDGE STATION 794 HAS MATERIAL LOSS OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000103 20020320 00103 NM 2002 3 20 2002UALA00417 1 20020311 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 LEFT HAND BODY STATION 188 FRAME CRACKED AT WL 207. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000104 20020320 00104 NM 2002 3 20 2002UALA00418 1 20020311 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 FOUR INCHES AFT OF STATION 188 WL 207 LEFT HAND CHORD HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLE D REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000105 20020320 00105 NM 2002 3 20 2002UALA00419 1 20020311 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 930UA 26655 STATION 986.5 FLOORBEAM RBL 18 TO RBL 39 CORRODED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000106 20020320 00106 NM 2002 3 20 2002UALA00420 1 20020311 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 STRINGER CLIP CRACKED STATION 440 AT STATION 28L. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000107 20020320 00107 NM 2002 3 20 2002UALA00422 1 20020307 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 108UA 26903 EMERGENCY DOOR LIGHT FWD POSITION INOP AT DR1L. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000108 20020320 00108 NM 2002 3 20 2002UALA00423 1 20020307 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 108UA 26903 EEL CEILING LIGHT INOP AT SEAT 3J AND 6CD. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000112 20020320 00112 NM 2002 3 20 2002UALA00424 1 20020307 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 108UA 26903 AFT EEL LIGHT INOP ON SEAT 5A. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000113 20020320 00113 NM 2002 3 20 2002UALA00425 1 20020311 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 CABIN FLOOR UPPER T-CAP UPPER SURFACE CORRODED STATION 365 RBL 10 STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND L-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000114 20020320 00114 NM 2002 3 20 2002UALA00426 1 20020312 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 FLOORBEAM CORRODED, STATION 365 RBL 618. MAJOR REPAIR ACCOMPLISHED. ANGLE REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000115 20020320 00115 NM 2002 3 20 2002UALA00427 1 20020312 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 CABIN FLOORBEAM BODY STATION 310 RBL 39 IS CORRODED ON UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR STRA P AND NESTED ANGLE T-CAP ON FLOORBEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000116 20020320 00116 NM 2002 3 20 2002UALA00428 1 20020311 A 5753 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE T/E FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 LEFT MIDFLAP UPPER SKIN HAS WEAR DAMAGE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. INSTALLED BONDED METAL FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000117 20020320 00117 NM 2002 3 20 AWXA200200231 1 20020220 A 5315 BAC1520792 SEAT TRACK BOEING 737 737277 1384570 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 LCQ - MAJOR REPAIR - "C" DURING C-14 CHECK CORROSION WAS FOUND ON SEAT TRACK AT BS 328, RBL 42. MAINTENANCE REMOVED CORR OSION AND FOUND MATERIAL LOSS OUT OF LIMITS IAW B737-200 SRM 53-10-1, FIG 4, PG. 18. REMOVED DAMAGED SECTION OF SEAT TRA CK, FABRICATED NEW SECTION OF SEAT TRACK AND INSTALLED REPAIR IAW B737-200 SRM 51-30-2, PG. 13 & 14. 2 L 7 2 4F RT A16WE 2002032000118 20020320 00118 NM 2002 3 20 AWXA200200232 1 20020224 A 5320 7075T6040 FLOOR SUPPORT BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 LCQ - MAJOR REPAIR - "C" - DURING C-14 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 279, LBL 28. MAINTENANCE REMOVED DAMAGED SECTION OF FLOOR SUPPORT, FABRICATED NEW SECTION OF FLOOR SUPPORT, AND INSTALLED REPAIR IAW B737-200 SRM 51-30- 2, PG. 17 & 32. 2 L 7 2 4F RT A16WE 2002032000119 20020320 00119 NM 2002 3 20 AWXA200200233 1 20020220 A 5320 6577488226 FLOOR SUPPORT BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 LCQ - MAJOR REPAIR - "C" - DURING C-14 CHECK CORROSION WAS FOUND ON CABIN FLOOR SUPPORT ANGLE AT BS 307, LBL 10-20. MAIN TENANCE REMOVED DAMAGED FLOOR SUPPORT ANGLE AT BS 307, LBL 10-20, FABRICATED NEW FLOOR SUPPORT ANGLE, AND INSTALLED REPA IR IAW B737-200 SRM 51-30-2, PG. 14. 2 L 7 2 4F RT A16WE 2002032000120 20020320 00120 NM 2002 3 20 AWXA200200235 1 20020319 A 3350 BMS13311122 WIRE BOEING 737 737277 1384570 NM SEAT ROW 19 L/H. BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 PHX - EEL - "C" - DURING INSPECTION OF EMERGENCY ESCAPE PATH LIGHTING A BROKEN WIRE WAS FOUND AT SEAT ROW 19 L/H. MAINTE NANCE REPAIRED BROKEN WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H IAW SWP 20-30-12, OPERATIONAL CHECK WAS GO OD. 2 L 7 2 4F RT A16WE 2002032000121 20020320 00121 NM 2002 3 20 2002UALA00429 1 20020307 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT WEAK A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 108UA 26903 FLIGHT DECK EEL DIM. REMOVED LAMP 1308 AND REPLACED WITH LAMP 1317 PER MM 33-51-07. OPS CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000122 20020320 00122 2002 3 20 02FDEA00203 4 20020318 A 3441 6625136001 ANTENNA DOUG MD11 MD11F 3023600 NM FAILED A FDEA A J UNSCHED LANDING DUMP FUEL O OTHER CL CLIMB 1 SO 25 582FE 48420 02-70 BOTH WX RADARS FAILED AFTER T/O. R&R WX RADAR ANTENNA PER MM 34-41-07-4. 2 L 7 3 4F RT A22WE 2002032000130 20020320 00130 NM 2002 3 20 2002UALA00430 1 20020307 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 108UA 26903 UPPER DECK CEILING EEL INOP AT ROW 12 AND 15. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000132 20020320 00132 NM 2002 3 20 2002UALA00431 1 20020307 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 108UA 26903 EMERGENCY LIGHT AT MED NR 1 LT FWD SILL LIGHT IS OUT. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000134 20020320 00134 NM 2002 3 20 2002UALA00432 1 20020307 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 108UA 26903 EMERGENCY LIGHT AT MED NR 5 BUSTLE SLIDE LIGHT IN DIM. REPLACED EMERGENCY LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000135 20020320 00135 NM 2002 3 20 2002UALA00433 1 20020307 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 108UA 26903 EMERGENCY CEILING LIGHT INOP AT UPPER DECK ABOVE SEAT ROW 13 AND 17. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000137 20020320 00137 NM 2002 3 20 2002UALA00434 1 20020307 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 108UA 26903 EMERGENCY LIGHT ABOVE THE STAIRWAY INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000138 20020320 00138 NM 2002 3 20 2002UALA00435 1 20020307 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 108UA 26903 EEL THRESHOLD LIGHT INOP AT DOOR 2L, 3L, 5L, 1R. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032000139 20020320 00139 NM 2002 3 20 2002UALA00436 1 20020312 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 STATION 1681 RBL 49 FLOORBEAM HAS EXCESS MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER STRAP INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000140 20020320 00140 NM 2002 3 20 2002UALA00437 1 20020312 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 CABIN FLOOR INNER CREASE BEAM CHORD AT STATION 760 RBL 65 STRINGER 17R HAD EXCESSIVE MATERIAL REMOVED DURING CORROSION C LEAN UP. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLES AND STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000142 20020320 00142 NM 2002 3 20 2002UALA00438 1 20020312 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 547UA 25368 FLOOR EEL LIGHT STRIP AT SEAT 13 ABC WILL NOT ILLUMINATE. REPLACED FLOOR EEL LIGHT SEGMENT AT SEAT 13 ABC. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000145 20020320 00145 NM 2002 3 20 2002UALA00439 1 20020313 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 CABIN BODY STATION 867 FRAME, BETWEEN 8L & 9L FRAME IS CRACKED AT FASTENER HOLE FROM VENT BRACKET, AFT SIDE. MAJOR REPA IR ACCOMPLISHED. INSTALLED CHANNEL REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032000146 20020320 00146 NM 2002 3 20 2002UALA00441 1 20020313 A 5330 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 780UA 26944 RIGHT FUSELAGE SKIN CRACKED AT STAB FAIRING SLIDING SEAL ASSY. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002032000147 20020320 00147 NM 2002 3 20 2002UALA00443 1 20020313 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 BODY STATION 324 FLOORBEAM CAP RBL 55 CORRODED. MAJOR REPAIR ACCOMPLISHED. FLOORBEAM CAP DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032000149 20020320 00149 NM 2002 3 20 2002UALA00444 1 20020313 A 5347 SEAT TRACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 CABIN FLOOR SEAT TRACK SUPPORT BETWEEN STATION 365 TO 415 RBL 48 STRINGER 17R HAD EXCESSIVE MATERIAL REMOVED DURING CORR OSION CLEAN UP. MAJOR REPAIR ACCOMPLISHED. REMOVED COMPLETE SECTION OF SEAT TRACK SUPPORT AND INSTALLED NEW PART. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041000073 20020410 00073 NM 2002 4 10 2002UALA00447 1 20020313 A 2530 3510003201U2 COFFEEMAKER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY MALFUNCTIONED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 369UA 24538 UNSCHEDULED LANDING DUE TO BURNING ODOR. FORWARD COFFEEMAKER HEATING ELEMENT MALFUNCTIONED. REPLACED COFFEEMAKER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032700056 20020327 00056 NM 2002 3 27 2002UALA00448 1 20020314 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE BUCKLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 FORWARD PIT BODY FRAME IS BUCKLED AND MISDRILLED AT STATION 482B RBL 2 TO LBL 2. MAJOR REPAIR ACCOMPLISHED. MANUFACTUR ED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032700061 20020327 00061 NM 2002 3 27 2002UALA00449 1 20020314 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 DAMAGE FOUND ALONG FORWARD EDGE OF FORWARD CARGO DOOR CUT OUT AT BODY STATION 440 COMMON TO SKIN, DOUBLER AND BEARSTRAP. MAJOR REPAIR ACCOMPLISHED. EXTERNAL REPAIR DOUBLER, TRIPLER, QUADRUPLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040500028 20020405 00028 NM 2002 4 5 2002UALA00450 1 20020314 A 2751 INDICATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT OUT OF TOLERANCE A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 657UA 27112 EICAS MSG TRAILING EDGE FLAP DISAGREE DISPLAYED. EMERGENCY DECLARED. LANDING WAS UNEVENTFUL. TEMPORARY INTERRUPTION I N THE FLAP/SLAT ELECTRONICS UNIT (FSPM) CAUSED A DISAGREE INDICATION TO GENERATED ON EICAS DISPLAY. ONE TIME DISRUPTION OF SYSTEM. ACCOMPLISHED FSEU BITE TEST PER MM AND NO FAULTS FOUND. FLAP INDICATOR EXHIBITED A SPLIT IN THE FLAP INDIC ATION NEEDLES GREATER THAN ALLOWED. SUBJECT FLAP INDICATOR WAS REPLACED AND CHECKED PER APPLICABLE MM. FLAP SYSTEM WAS OPERATIONALLY CHECKED SEVERAL TIMES PER APPLICABLE MM. ALL OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040500029 20020405 00029 NM 2002 4 5 2002UALA00451 1 20020314 A 3350 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAULTY A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 642UA 25092 SMOKE SMELL AT DOOR 1L. FAULTY EMERGENCY EXIT LIGHT CHARGER AND BATTERY WERE REPLACED AT DOOR 1L. 2 L 7 2 4F 4 F RT A1NM E24NE 2002032700064 20020327 00064 NM 2002 3 27 2002UALA00457 1 20020314 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 AFT PIT FRAME UPPER CAP DENTED STATION 1400 AT STRINGER 26L. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECTION OF FRAM E. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032500119 20020325 00119 NM 2002 3 25 F3LA200200112 1 20020316 A 5313 STRINGER BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 314FL 3489 25256 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR STRINGER AT STA 793, LBL 3. FABRICATED AND INSTALLED REPAIR PE R SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002032500122 20020325 00122 NM 2002 3 25 F3LA200200113 1 20020316 A 5321 FLOOR PANEL BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 314FL 3489 25256 DURING C-2 CHECK, INSPECTION REPORTED JOINT BETWEEN PANELS 3 AND 4 IN AFT CARGO COMPARTMENT CORRODED. FABRICATED AND IN STALLED REPAIR PER SRM 53-60-53. 2 L 7 2 4F RT A16WE 2002032500123 20020325 00123 NM 2002 3 25 F3LA200200114 1 20020316 A 5321 FLOOR PANEL BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 314FL 3489 25256 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL NR 3 CORRODED. FABRICATED AND INSTALLED REPLACE MENT FLOOR PANEL PER SRM 51-20-01. 2 L 7 2 4F RT A16WE 2002032500124 20020325 00124 NM 2002 3 25 F3LA200200115 1 20020316 A 5320 STRAP BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 314FL 3489 25256 DURING C-2 CHECK, INSPECTION REPORTED SPLICE STRIP CORRODED BETWEEN FLOOR PANELS NR 1 AND NR 2 IN AFT CARGO COMPARTMENT. FABRICATED AND INSTALLED REPLACEMENT FLOOR JOINT STRAP PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002032100013 20020321 00013 NM 2002 3 21 DHL2002749003 1 20020320 A 5751 652176646 AILERON BOEING 727 727200 138407E NM DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 DURING A CHECK FOUND R/H O/B AILERON UPPER SURFACE WITH DELAMINATED UPPER O/B SKIN APPROX 4 1/2 X 8 IN. AREA OF TAB. 2 L 7 3 4F RT A3WE 2002032100021 20020321 00021 WP 2002 3 21 MWEA020174 1 20020319 A 5310 5956034514 SUPPORT DOUG DC9 DC932 3022066 WP STATION 980 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 STATION 980 BY LONGERON 27 RIGHT HAS A CRACKED SUPPORT. -- REMOVED AND REPLACED FLOOR SUPPORT. 2 L 7 2 4F A6WE 2002032100022 20020321 00022 WP 2002 3 21 MWEA020175 1 20020319 A 5310 5956034503 FITTING DOUG DC9 DC932 3022066 WP STATION 945 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 STATION 945 BETWEEN LONGERONS 28 LEFT AND 27 LEFT HAS A CORRODED SUPPORT FITTING. -- REMOVED AND REPLACED SUPPORT FITT ING. 2 L 7 2 4F A6WE 2002042900052 20020429 00052 NE 2002 4 29 CA020308012 2 20020130 A 7200 ENGINE CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A NE NR 2 FAILED W A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 CA (CAN) DURING FLIGHT INSPECTION OF ILS CLEARANCE ORBIT OF AIRFIELD IN SLIGHT BANK & 10-20 KTS TAILWIND NR 2 ENGINE SUDDEN LY SHUTDOWN. A/C RETURNED & LANDED. ENGINEER TOOK LOOK AT ENGINE NOTHING SEEN ABNORMAL. OIL SYS CHECKED BECAUSE OF PRE VIOUS EXPERIENCE WITH THESE ENGINE & NO FAULT FOUND WITH OIL SYS. FUEL SYS CHECKED WATER SAMPLE TAKING FROM FUEL TANKS & NO WATER FOUND. TALKING WITH ENGINE MFG THEY ADVISE US TO GO AND TRY TO START ENGINE. ENGINE STARTED WITH NO MALFUNCTI ON OBSERVED HIGH POWER RUN C/O ALL SYS RUNNING NORMAL. AT TIME A/C FLOWN BACK TO OTTAWA WHERE PROPER MAINT COULD BE CARR IED OUT. 2 L 7 2 4F 4 F RT A21AE E15NE 2002032700179 20020327 00179 NM 2002 3 27 SABA020035 1 20020319 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 880CC 277 DURING PREFLIGHT FOR FLIGHT 5027 IN CLT, TWO EMERGENCY LIGHTS WOULD NOT TEST AT ROW 1 & 8. MAINTENANCE REMOVED AND REPL ACED LIGHT BULBS. 2 H 7 2 4T RT A13NM 2002032100055 20020321 00055 NM 2002 3 21 SABA020036 1 20020319 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 881CC 294 During Pre-flight for flight 5025 from CLT to TLH, The foward overhead emergency light would not test. Maintenance remov ed and replaced the light Assembly. Systen OPS checked good and Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002032100060 20020321 00060 NM 2002 3 21 SWAA020578 1 20020317 A 3350 10107551 COVER BOEING 737 737301 1384611 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT COVER MISSING ON FWD LAV WALL OTBD OF F/A SEAT. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002032100061 20020321 00061 2002 3 21 SWAA020579 4 20020318 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 641SW 27714 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002032100062 20020321 00062 2002 3 21 SWAA020580 4 20020318 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399WN 27693 DURING SCHEDULED BC4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.. 2 L 7 2 4F RT A16WE 2002032100063 20020321 00063 NM 2002 3 21 SWAA020581 1 20020319 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 645SW 28330 EEPLS COVER LOOSE AT ROW NR 6. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2002032100064 20020321 00064 NM 2002 3 21 SWAA020582 1 20020319 A 3350 101073 LENS BOEING 737 7372K6 1364440 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 AFT SVC DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2002032100065 20020321 00065 2002 3 21 SWAA020573 4 20020318 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM BOTH AFT DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED C3 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDES DRAGGING WHEN CLOSING DOOR. ADJUSTED SLIDES PER MM. 2 L 7 2 4F A16WE 2002032100066 20020321 00066 2002 3 21 SWAA020574 4 20020318 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM BOTH AFT DOORS MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED C3 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE CABLES MISROUTED. REROUTED CABLES PER MM. 2 L 7 2 4F A16WE 2002032100067 20020321 00067 NM 2002 3 21 SWAA020575 1 20020314 A 5313 65C27314 TIE CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002032100068 20020321 00068 NM 2002 3 21 SWAA020577 1 20020318 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002032100069 20020321 00069 2002 3 21 SWAA020549 4 20020312 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 635SW 27708 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002032100070 20020321 00070 NM 2002 3 21 SWAA020550 1 20020312 A 3350 07912 COVER BOEING 737 7372H4 138448C NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER BROKEN BETWEEN ROWS 10 AND 11. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F A16WE 2002032100071 20020321 00071 NM 2002 3 21 SWAA020554 1 20020312 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED SPECIAL VISIT, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 10 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002032100072 20020321 00072 NM 2002 3 21 SWAA020555 1 20020313 A 5753 6546435334 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 396SW 27690 DURING SCHEDULED 1/4D CHECK, FOUND RT OTBD AFT FLAP DELAMINATED AT T/E. REMOVED AND REPLACED RT OTBD AFT FLAP PER MM.. 2 L 7 2 4F RT A16WE 2002032100073 20020321 00073 NM 2002 3 21 SWAA020556 1 20020314 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED C3 CHECK, FOUND FUSLAGE SKIN CRACKED AT AFT SVC DOOR ON LOWER HINGE CUT OUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002032100074 20020321 00074 NM 2002 3 21 SWAA020557 1 20020314 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND 9R, AT BS'S 360, 400, 827 AND 907. RE PAIRED FRAMES PER BFG ER AND SRM. 2 L 7 2 4F RT A16WE 2002032100075 20020321 00075 2002 3 21 SWAA020558 4 20020317 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 630WN 27705 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002032100076 20020321 00076 NM 2002 3 21 SWAA020562 1 20020317 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 935, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002032100077 20020321 00077 NM 2002 3 21 SWAA020563 1 20020315 A 5330 6545765 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED 3 INCHES AT BS 520D PLUS 13, ABOVE STR 10R. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2002032100078 20020321 00078 NM 2002 3 21 SWAA020564 1 20020314 A 5753 6545435237 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED C1 CHECK, FOUND LT OTBD T/E AFT FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2002032100079 20020321 00079 NM 2002 3 21 SWAA020565 1 20020316 A 5343 65C10300 BRACKET BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED A2 CHECK, FOUND NOSE GEAR ACTUATOR ATTACH BRACKET GUSSET CRACKED. REMOVED AND REPLACED BRACKET PER SRM . 2 L 7 2 4F RT A16WE 2002032100080 20020321 00080 NM 2002 3 21 SWAA020566 1 20020317 A 5330 6545768 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR HINGE CUTOUT BEAR STRAP CRACKED AT BS 303, WL 238.5 TO WL 258.5. REPAIRE D BEAR STRAP PER BFG ER. 2 L 7 2 4F RT A16WE 2002032100081 20020321 00081 NM 2002 3 21 SWAA020567 1 20020317 A 5330 6545774 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED D CHECK, FOUND AFT SVC DOOR CUTOUT BEAR STRAP CORRODED FROM BS 780 TO BS 796, STR 26R. REPAIRED BEAR S TRAP PER BFG ER. 2 L 7 2 4F RT A16WE 2002032100082 20020321 00082 NM 2002 3 21 SWAA020568 1 20020315 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10L, BS 360 AND BETWEEN BS 727A AND BS 727 B. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002032100083 20020321 00083 NM 2002 3 21 SWAA020569 1 20020315 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, BETWEEN STR'S 11L AND 13L. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2002032100084 20020321 00084 NM 2002 3 21 ANCF200200005 1 20020310 A 2420 CSD DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE RT ENGINE FAILED W ANCF D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 23 632CT 49632 725391 AFTER TAKE OFF ROLL DURING CLIMB. PRIOR TO CLIMB THRUST REDUCTION IN ANNUNCIATOR PANEL, RIGHT CSD OIL PRESSURE LOW AND R IGHT GENERATOR OFF APPEARS. WAS PERFORMED THE RESPECTED MALFUNCTIONS PROCEDURE AND CHECK LIST. THE CREW RETURNED TO EDR. THE RIGHT CSD WAS CHANGED. IAW AMM 24-10-01 PAGE 401, PERFORMED OPERATIONAL TEST WITH SATISFACTORY RESULTS. 2 L 7 2 4F 4 F RT E9NE 2002032100085 20020321 00085 NM 2002 3 21 CALA0200139 1 20020320 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND A 3" CRACK IN UPPER FUSELAGE SKIN AT STA 178, WL 243, LBL 1.5. THE CRACKED DOUBLER WAS REMOVED AND A NE W DOUBLER WAS INSTALLED IAW SOEING DRAWING #65-45800 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002032100086 20020321 00086 NM 2002 3 21 CALA0200140 1 20020321 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 887-947.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND L/H I/B SEAT TRACK CORRODED AT STA 887-947.5. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002032100087 20020321 00087 WP 2002 3 21 MWEA020182 1 20020319 A 5310 4912798507 CLIP DOUG DC9 DC932 3022066 WP STATION 945 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 AFT CARGO COMPARTMENT UNDERSIDE OF SHOVEL CLIP CORRODED AT STATION 945 LONGERON 26 RIGHT. -- REMOVED AND REPLACED SHOV EL CLIP. 2 L 7 2 4F A6WE 2002032100088 20020321 00088 WP 2002 3 21 MWEA020183 1 20020319 A 5310 3924050501 LONGERON DOUG DC9 DC932 3022066 WP STATION 552 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FORWARD PIT LONGERON 28 LEFT IS CRACKED UNDER SPLICE AT STATION 552 THROUGH 560. -- REMOVED LONGERON, POSITIONED AND D RILLED, REINSTALLED LONGERON. 2 L 7 2 4F A6WE 2002032100089 20020321 00089 CE 2002 3 21 CA020130007 1 20020119 A 5347 12139901 BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE SEAT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13437 (CAN) DURING THIRD INSPECTION WE FOUND EIGHT SEAT BRACKET CRACKED.THE CRACK WAS GENERATED FROM THE REAR THRU THE HOLE AD JACENT TO THE BEND. AFTER FLEET INVESTIGATION WE FOUND 34 BRACKET CRACKED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002032100094 20020321 00094 EA 2002 3 21 COMA0260197 1 20020317 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS DE DESCENT 1 SO 01 735CA 13244 187 7267 FLIGHT 5234 - FLAPS FIALED AT 0 DEGREES.REPLACED THE L/H BPSU. 2 L 7 2 4F RT A21EA 2002032100096 20020321 00096 EA 2002 3 21 COMA0260198 1 20020316 A 2750 860D10018AB FCU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS DE DESCENT 1 SO 01 735CA 14592 7267 FLIGHT 5436 FLAPS FIALED AT 0 DEGREES.REPLACED THE FECU 2 L 7 2 4F RT A21EA 2002032100099 20020321 00099 EA 2002 3 21 COMA0260199 1 20020316 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 409CA 7441 FLIGHT 5107 FWD FLOOR PATH EMERGENCY LIGHTS ARE INOP.CLEANED WIRING CONNECTION - SYSTEM OPS CHECK OK. 2 L 7 2 4F RT A21EA 2002032100100 20020321 00100 NM 2002 3 21 SABA020037 1 20020318 A 3350 6104789 BATTERY DHAV DHC8 DHC8103 1386005 NM POWER LOSS A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 801WP 086 During Pre-flight in Clt for flight 5027, The overhead emergency lights would not test. Maintenance removed and replaced the battery pack. System ops checked good and Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002032100101 20020321 00101 EA 2002 3 21 COMA0260201 1 20020317 A 3010 11513361 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 938CA 15661 7046 FLIGHT 5833 ANTI ICE DUCT WARNING.REPLACED THE TEMP CONTROLLER. 2 L 7 2 4F RT A21EA 2002032100103 20020321 00103 2002 3 21 RAIA00203099 4 20020317 A 3418 C850176 VANE JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 560HK 9663 823 41076 5576 STL- RIGHT STALL ANNUNCIATOR ILLUMINATED ON TAXI OUT. MAINTENANCE REMOVED AND REPLACED THE RIGHT STALL VANE, OPS CK OK. 2 L 7 2 4T RT A41NM 2002032100104 20020321 00104 SO 2002 3 21 RAIA00203100 1 20020317 A 3040 9001841 WINDSHIELD WIPER EMB 145 EMB145 3260210 SO DETERIORATED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 803HK 145077 5282-STL- CAPTAINS WINDSHIELD WIPER CAME OFF DURING TAXI. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD WIPER, OP S CK OK. 2 L 7 2 4F RT T00011AT 2002032100105 20020321 00105 NM 2002 3 21 AWXA200200236 1 20020320 A 3350 BMS13311122 WIRE BOEING 737 737301 1384611 NM SEAT ROW 4L BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 LAS - EEL - EMERGENCY ESCAPE PATH LIGHT HAS BROKEN WIRE AT EMERGENCY LIGHT ASSEMBLY ON SEAT 4 L/H. MAINTENANCE REPAIRED WIRE WITH BUTT SPLICE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 L/H, FUNCTIONAL TEST WAS GOOD IAW T/C A1C33006. 2 L 7 2 4F RT A16WE 2002032200007 20020322 00007 EA 2002 3 22 COMA0260200 1 20020316 A 2540 LAVATORY CNDAIR CL600 CL6002B19 1900309 EA A COMA H O DEACTIVATE SYST/CIRCUITS OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 983CA 7169 FLIGHT 5091 LAVATOR SMOKE WARNING - F/A CONFIRMED SMOKE PRESENT.COULD NOT DUPLICTE. CHECKED ALL LAV SYSTEM - NO SMOKE N OTED. 2 L 7 2 4F RT A21EA 2002032200016 20020322 00016 NM 2002 3 22 SABA020039 1 20020320 A 3350 10005511 BULB DHAV DHC8 DHC8102 2809003 NM CABIN A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 881CC 294 Aircraft 881 on flight 5027 from CLT to CVG. During preflight the forwaqrd emergency exit light was inoperative. Maint enance removed and replaced the bulbs. Ops check was good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002032200017 20020322 00017 EA 2002 3 22 COMA0260202 1 20020318 A 2150 601R5108623 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA INST PANEL MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 987CA 12508 7199 FLIGHT 5633 R/H AC PACK FAILED.REPLACED THE AC CONTROL PANEL. 2 L 7 2 4F RT A21EA 2002032200018 20020322 00018 EA 2002 3 22 COMA0260203 1 20020319 A 2720 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 918CA 7018 FLIGHT 5407 T/O CONFIG TRIM WARNING.FOUND AILERON TRIM OUT OF T/O RANGE - OPERATIONAL CHECK OF TRIM SYSTEM WAS NORMAL. 2 L 7 2 4F RT A21EA 2002032900107 20020329 00107 WP 2002 3 29 ARWA20020309 1 20020321 A 3230 56165545503 CYLINDER DOUG DC8 DC85F54 3021926 WP LT MLG LEAKING A ARWA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 426FB 45667 UPON CLEARING THE RUNWAY EXPERIENCED A TOTAL LOSS OF HYDRAULIC FLUID AND PRESSURE ALL CHECKLIST COMPLIED WITH. AIRBRAKE USED TO STOP AIRCRAFT WITHOUT INCIDENT. FOUND FWD LEFT BOGIE TRIM CYLINDER WITH HYDRAULIC LEAK. REMOVED AND REPLACED MLG FWD LEFT BOGIE TRIM CYLINDER IAW MM ALTERNATE INSTALLATION AND ADJUSTMENT PROCEDURE OF DC8 MM 32-11-3 (3). SERVICED AIR BRAKE BOTTLE AND HYDRAULIC RESERVOIR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002032200019 20020322 00019 EA 2002 3 22 COMA0260204 1 20020320 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 735CA 7267 FLIGHT 5150 EMERGENCY FLOOR LIGHTS, ROWS 2-6 ARE INOP.REMVOED MOISTURE FROM TRACK LIGHTING. 2 L 7 2 4F RT A21EA 2002032200020 20020322 00020 EA 2002 3 22 COMA0260205 1 20020320 A 3620 20035008067 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING M OVER TEMP CR CRUISE 1 SO 01 710CA 8621 7241 FLIGHT 5279 R/H 14TH STAGE BLEED AIR DUCT WARNING IFSD.REPLACED THE BLEED AIR CONTROL UNIT. 2 L 7 2 4F RT A21EA 2002032200021 20020322 00021 EA 2002 3 22 SWIA200210734 1 20020317 A 5244 SERVICE DOOR CNDAIR CL600 CL6002B19 1900309 EA OPEN A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 498SW 7483 LOUD SQUEAL INFLIGHT. RETURNED TO SLC. FOUND SERVICE PANEL DOOR OPEN. CLOSED DOOR. NO DAMAGE NOTED. OK FOR FURTHER FLIGHT. 2 L 7 2 4F RT A21EA 2002032200022 20020322 00022 NM 2002 3 22 C1HA200293003 1 20020322 A 3600 39608831 FLOW VALVE BOEING 727 727212 138407G NM INOPERATIVE A C1HA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 293AS 21348 During climbout, unable to pressurize cabin above 1 PSI diff. Action Taken: Removed and replaced right flow control va lve. Ops and leak check good on ground IAW MM 36-10-02. 2 L 7 3 4F A3WE 2002032200023 20020322 00023 SO 2002 3 22 C2XA02IA073 1 20020321 A 7932 4252070 GARLOCK SEAL EMB 145 EMB145 3260210 SO #1 ENGINE LEAKING A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 14972 145151 LCH- DURING FLIGHT 3788, THE CREW NOTED NUMBER 1 ENGINE LOW OIL QUANTITY AND PRESSURE, DECLAIRED EMERGENCY, AND DIVERTE D TO LCH, (ACTUAL DESTINATION WAS HSV). LCH- MAINTENANCE REMOVED AND REPLACED THE #3 GENERATOR GARLOCK SEAL, SERVICED THE ENGINE OIL SYSTEM,AND,PERFORMED A ENGINE RUN UP,NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4F RT T00011AT 2002032200024 20020322 00024 SO 2002 3 22 C2XA02IA074 1 20020318 A 4950 168401201 APU EMB 120 EMB120ER 3260203 SO TAIL OVERSERVICED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16718 120136 SHV- APU BLEED CAUSES SMOKE WHEN BOTH PACKS TURNED OFF. SHV- MAINTENANCE INSPECTED THE AIRCRAFT, AND, THE AIRCRAFT WA S RELEASED IAW MEL. IAH- MAINTENANCE REMOVED EXCESS OIL FORM APU TO OBTAIN THE PROPER SERVICE LEVEL,PERFORMED A OPERA TIONAL CHECK OF THE APU, AND APU BLEED SYSTENS,NO DEFECTS NOTED,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002032200025 20020322 00025 EU 2002 3 22 C2XA02IA075 1 20020319 A 3397 335018024 WIRE AEROSP ATR42 ATR42320 8680930 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 42836 200 IAH- WHILE PERFORMING A 1A CHECK INSPECTION IT WAS NOTED THAT THE EMERGENCY LIGHT BATTERY HAS LOW VOLTAGE. IAH-MAINTEN ANCE TROUBLESHOT THE SYSTEM AND FOUND THAT THERE WAS NO POWER TO THE EMERGENCY LIGHTS IN THE BATTERY MODE. MAINTENANCE REPAIRED A BROKEN WIRE TO 29WL PIN F AND G, AND PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFEC TS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002032200026 20020322 00026 SO 2002 3 22 C2XA02IA076 1 20020320 A 3397 W741803120 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12922 145338 EWR- DURING PERFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS BETWEEN ROWS 9 AND 12 FAILED TO ILLUMINATE. EWR- MAINTEN ANCE REPAIRED WIRE ON FLOOR PROXIMITY STRIP LIGHTS, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO D EFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002032300001 20020323 00001 SO 2002 3 23 C2XA02TY058 1 20020223 A 5320 73210301 FITTING EMB 145 EMB145ER 3260211 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13929 145009 TYS, During a scheduled inspection the aft galley inboard floor fitting was found corroded, Maintance removed and replac ed the fitting. I/A/W-C & D Aerospace VCMM-25-31-45. The replacement was satisfactory and the aircraft will be released upon complection of the inspection. 2 L 7 2 4F RT T00011AT 2002032400001 20020324 00001 EU 2002 3 24 C2XA02IA077 1 20020323 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14821 160 IAH- DURING POST FLIGHT INSPECTION THE CREW NOTED THAT THE EMERGENCY LIGHTING IN MID CABIN FLOOR INOP.. IAH- MAINTENA NCE REMOVED AND REPLACED THE POWER SUPPLY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DE FECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002032500001 20020325 00001 SO 2002 3 25 C2XA02TY059 1 20020324 A 2731 14522150401 BELLCRANK EMB 145 EMB145LR 3260212 SO CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16987 145261 TYS WHILE PERFORMING WITH EA-2730-01044 THE LEFT AND RIGHT ELEVATOR QUADRANT BELLCRANKS WERE FOUND CRACKED. MAINTENANCE R/R BOTH LEFT AND RIGHT BELLCRANKS. OPS CHECKS WERE GOOD AND WILL BE REL. UPON COMPLETION OF ALL MAINTENANCE. 2 L 7 2 4T RT T00011AT 2002032500057 20020325 00057 EU 2002 3 25 QXEA0200387 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK AT STATION 667.906 TO STATION 667.901 INSIDE LUGS THERE IS CORROSION. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002032500058 20020325 00058 EU 2002 3 25 QXEA0200388 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK AFT OF FRAME 14755 INSIDE TUNNEL THERE IS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM A ND MM. 2 L 7 2 4F RT A20EU 2002032500059 20020325 00059 EU 2002 3 25 QXEA0200389 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK FROM FRAME 15635 TO FRAME 12405 THE LUGS ARE GOUGED. REPAIRED IAW FOKKER MM AND SRM. 2 L 7 2 4F RT A20EU 2002032500060 20020325 00060 EU 2002 3 25 QXEA0200390 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK FORWARD OF FRAME 15635 CORROSION ON INSIDE LUGS. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 4C, STEP 1 AND SRM 51-10-04, PAGE 8. 2 L 7 2 4F RT A20EU 2002032500061 20020325 00061 EU 2002 3 25 QXEA0200391 1 20020218 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CORROSION EVIDENT UNDER NUT PLATE ON FRAME 7305 AT FOUR WAY FLOOR SUPPORT ABOVE STRINGER 74. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002032500062 20020325 00062 EU 2002 3 25 QXEA0200392 1 20020214 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU WINDOW BELT DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - DENT BELOW LT WINDOW FRAME BASE. REPAIRED IAW FOKKER SRM 53-02-05, FIGURE 1, SRM 51-10-4, 53-02-03 AND SRM 53-02- 02. 2 L 7 2 4F RT A20EU 2002032500063 20020325 00063 EU 2002 3 25 QXEA0200393 1 20020215 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - DENT ON LT FRAME 3050 BELOW WINDOW FRAME BASE. REPAIRED IAW FOKKER SRM 53-02-05. 2 L 7 2 4F RT A20EU 2002032500064 20020325 00064 EU 2002 3 25 QXEA0200395 1 20020216 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACK IN CLIP ON AFT SIDE OF FRAME 14175 10 INCHES LEFT OF CENTER LINE. REPAIRED IAW FOKKER SRM 51-11-4, PAGE 2, PARAGRAPH E, SRM 51-10-4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002061100101 20020611 00101 NM 2002 6 11 QXEA0200456 1 20020312 A 7810 VC1165 CLAMP DHAV DHC8 DHC8201 2809001 NM NR 2 ENGINE MISALIGNED A QXEA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 361PH 516 GEG - DURING TAXI NR 2 ENGINE FIRE WARNING SYSTEM ACTIVATED. STOPPED THE AIRCRAFT, PERFORMED FIRE ON THE GROUND PROCEDU RE. FIRE INDICATION CEASED AFTER ACTIVATING THE FORWARD EXTINGUISHER BOTTLE. MAINTENANCE INSPECTED AND FOUND THE TAILP IPE CLAMP ON THE ENGINE EXHAUST MISALIGNED. THE NR 2 NACELLE AND ENGINE WAS INSPECTED AND REPAIRED IAW DHC-8 MAINTENANC E MANUAL, DHC-8 STRUCTURAL REPAIR MANUAL, EA'S 2-54-120, -123, -124, -127, -128, -129, -130, AND 2-54-133. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002032700036 20020327 00036 NM 2002 3 27 02FDEA00207 1 20020320 A 2781 SWITCH BOEING 727 7272S2F 1384O81 NM L/E FLAP FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 217FE 22938 LEAD EDGE DEVICE NR 4 FAILED TO INDICATE UP ON FLAP RETRACTION AFTER T/O. REMOVED AND REPLACED NR 4 LEAD EDGE FLAP JUMP ER CABLE. REMOVED AND REPLACED L/E FLAP NR 4 SWITCH PER MM 27-82-001-4. 2 L 7 3 4F A3WE 2002032500066 20020325 00066 WP 2002 3 25 02FDEA00208 1 20020318 A 5753 BOLT DOUG DC10 DC1010 3022110 WP T/E FLAP BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 LEFT HAND OUTBOARD FLAP, OUTBOARD HINGE BOLT BROKEN. 2 L 7 3 4F A22WE 2002032500067 20020325 00067 WP 2002 3 25 2002F00321 1 20020303 A 5320 STIFFENER LKHEED 1011 10113851 5265010 WP FUSELAGE CRACKED G K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 70757 193C1078 MAIN FRAME VERTICAL STIFFENER ON FORWARD BULKHEAD OF LEFT ACM BAY IS CRACKED (LOWER STIFFENER) CRACK LENGTH 3.760 INCHES FS 315, BL 36L, WL 125. MAINTENANCE REPAIRED VERTICAL STIFFENER ON FORWARD BULKHEAD OF LEFT ACM BAY PER LOCKHEED SRM 5 3-11-00. 2 L 7 3 4F A23WE 2002032700065 20020327 00065 NM 2002 3 27 2002UALA00458 1 20020314 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 AFT PIT FRAME UPPER FLANGE HAS EXCESSIVE MAT LOSS AFTER BLENDOUT OF DAMAGE AND CORROSION, STATION 1320 BETWEEN STRINGER 28L AND 27L. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032700066 20020327 00066 NM 2002 3 27 2002UALA00460 1 20020314 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 BODY STATION 287 RBL 88 CHORD CORRODED AT CHORD LOCATED AT R-1 DOOR. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW CHORD. 2 L 7 2 4F 4 F RT A1NM E24NE 2002032700068 20020327 00068 NM 2002 3 27 2002UALA00461 1 20020314 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 BODY STATION 852 RBL 33 TRANSBEAM CORRODED ON UPPER CAP. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR SP LICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002032700069 20020327 00069 NM 2002 3 27 2002UALA00462 1 20020314 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 BODY STATION 800 LBL 11 TRANSBEAM UPPER CHORD IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED TRANSBE AM AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002032700180 20020327 00180 NM 2002 3 27 SABA020040 1 20020322 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 881CC 294 AIRCRAFT 881 ON FLIGHT 5190 FROM AGS TO CLT. DURING POST-FLIGHT INSPECTION IN CLT THE FLOOR LEVEL EMERGENCY LIGHT AT RO W 7 WAS FOUND INOPERATIVE. NO EMERGENCY WAS INVOLVED. MAINTENANCE REMOVED AND REPLACED THE BULB. OPS CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002032500079 20020325 00079 CE 2002 3 25 6500058 1 20020319 A 2432 407613 BATTERY CESSNA 650 650 2076802 CE E/E BAY SHORTED E ERYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 70DJ 6500058 ON CLIMBOUT FROM KPDK, NR 2 OVERHEAT LIGHT CAME ON. ALTITUDE WAS FL330, RAN BATTERY OVERHEAT CHECKLIST. BATTERY NR 2 T EMP CONTINUED TO CLIMB. DECLARED AN EMERGENCY AND RETURNED TO KPDK. BATTERY TEMP ON NR 2 BATTERY HELD AT 81 DEGREES CE LSIUS UNTIL LANDING. MAINTENANCE FOUND ONE CELL IN NR 2 BATTERY SHORTED. 2 L 7 2 4F A9NM 2002032500081 20020325 00081 WP 2002 3 25 ABXA010779 1 20020306 A 5711 3913070 SPAR DOUG DC9 DC932F 3022067 WP CENTER WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 905AX 47147 LEFT WHEEL WELL, JUST OUTBOARD OF STATION ZERO, CENTER TANK ON REAR SPAR, UPPER INBOARD CORNER, HAD A CRACK. REPAIRED A REA IAW DC-9 SRM 51-30-5 AND 57-09. 2 L 7 2 4F A6WE 2002032500083 20020325 00083 2002 3 25 375PA0002 4 20020323 A 2230 AUTOTHRUST SYS BOEING 737 7373Y0 1384671 NM MALFUNCTIONED A PIDA K NONE O OTHER TO TAKEOFF 1 SO 05 375PA 23812 AUTOTHROTTLES WOULD NOT ENGAGE FOR TAKE-OFF. DURING CLIMB AND CRUISE "A/T LIM" DISPLAYED 2 L 7 2 4F RT A16WE 2002032500084 20020325 00084 2002 3 25 375PA0003 4 20020323 A 2210 AUTOPILOT SYS BOEING 737 7373Y0 1384671 NM MALFUNCTIONED A PIDA K NONE O OTHER CR CRUISE 1 SO 05 375PA 23812 AUTOPILOT WOULD NOT INTERCEPT LOC AND ATTEMPTED TO CORRECT IN WRONG DIRECTION. 2 L 7 2 4F RT A16WE 2002032500089 20020325 00089 WP 2002 3 25 ABXA010780 1 20020315 A 2120 ODOR DOUG DC9 DC941 302207N WP COCKPIT DETECTED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 973AX 47511 NOTICED A BURNING SMELL IN THE COCKPIT, INTERMITTENT, NOT STRONG BUT NOTICEABLE. THE SOURCE WAS NEAR THE RIGHT CLEAR VI EW WINDOW HEAT SENSOR. INSPECTED WIRING AND TEMP. SENSOR AT FIRST OFFICER'S CLEAR VIEW WINDOW. CHECKED FORWARD ACCESS ORY COMPARTMENT AND E/E COMPARTMENT. NO DEFECTS OR SMELL NOTED. 2 L 7 2 4F A6WE 2002032500095 20020325 00095 NM 2002 3 25 AWXA200200230 1 20020307 A 5230 65C3836419 DOOR FRAME BOEING 737 7373S3 1384711 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - C - DURING C-17 CHECK A .125 INCH CRACK WAS FOUND ON THE VERTICAL LEG OF THE FORWARD CARGO DOOR LOW ER TEE CHORD IN THE THIRD FASTENER HOLE FROM AFT END OF BEAM BS 487. 2 L 7 2 4F RT A16WE 2002032500098 20020325 00098 NM 2002 3 25 AWXA200200234 1 20020220 A 5320 BAC14902760 INTERCOSTAL BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 LCQ - MAJOR REPAIR - C - DURING C-14 CHECK CABIN UPPER INTERCOSTAL WAS FOUND CRACKED AND CORRODED AT BS 346, LBL 10. 2 L 7 2 4F RT A16WE 2002032500100 20020325 00100 NM 2002 3 25 C1HA200281002 1 20020228 A 2131 7638101 CONTROLLER BOEING 727 7272S7 138407Z NM CABIN PRESSURE FAILED A C1HA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 681CA 22020 AT FL 310, CABIN BEGAN TO CLIMB SLOWLY, UNABLE TO MOVE CABIN AIR OUTFLOW VALVE IN AUTO, STBY, OR MAN AC/DC. DIVERTED TO DEN, LANDED UNEVENTFULLY. REMOVED AND REPLACED PRESS CONTROLLER IAW MM 21-31-00 AND PRESS SELECTOR PANEL IAW MM 21-31- 00, OPS CHECK NORMAL IAW MM 21-31-00. 2 L 7 3 4F A3WE 2002032500102 20020325 00102 NM 2002 3 25 C1HA200294005 1 20020318 A 3010 CLAMP BOEING 727 727290 138408W NM RT WING LOOSE A C1HA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 294AS 22146 DURING CLIMB WITH ENGINE/WING ANTI-ICE ON, RIGHT STRUT OVERHEAT LIGHT ILLUMINATED. COM PROCEDURE FOLLOWED, OVERHEAT LIG HT EXT AFTER CLOSING WING A/I. RETORQUED V-BAND CLAMP IN STRUT RT SIDE IAW 727 M/M 30-13-00. OPS AND LEAK CHECK. GOOD ON FULL POWER RUN. 2 L 7 3 4F A3WE 2002032500104 20020325 00104 SO 2002 3 25 C2XA02CL079 1 20020315 A 3230 LANDING GEAR EMB 135 EMB135LR 3260305 SO NLG & MLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 27 11526 145410 DAY FLIGHT 3316 CREW REPORTED THAT AFTER TAKEOFF, GOT THE LANDING GEAR LEVER DISAGREE WARNING, AND THE LANDING GEAR WO ULD NOT RETRACT. RETURNED TO DAY AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO TYS WHERE MAINTENANCE PERFORMED A LANDING GEAR RETRACTION CHECK, AND AN AIR GROUND OPERATIONAL CHECK. ALL OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WER E FOUND. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002032500108 20020325 00108 SO 2002 3 25 C2XA02TY055 1 20020319 A 2730 14522150401 BELLCRANK EMB 145 EMB145LR 3260212 SO ELEVATOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 TYS DURING A SCHEDULED EA INSPECTION EA 2730-01044 A CRACK WAS FOUND IN LEFT BELL CRANK ASSEMBLY. MAINTENANCE REMOVED A ND REPLACED THE QUADRANT IAW AMM 27-31-03. OPS CHECK WAS GOOD AND WILL BE RELEASED UPON COMPLETION OF ALL CHECKS. 2 L 7 2 4T RT T00011AT 2002032500109 20020325 00109 EU 2002 3 25 CHQ000135 1 20020320 A 3020 CONTROLLER SAAB SF340 SF340A 7850100 EU INTAKE HEAT FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 152 152 EN ROUTE RIGHT INTAKE HEAT LIGHT ILLUMINATED. PERFORMED CHECKLIST, LIGHT CAME ON AGAIN. REMOVED AND REPLACED THERMAL C ONTROLLER. 2 L 7 2 4T RT A52EU 2002032500111 20020325 00111 NM 2002 3 25 DHL2002726001 1 20020316 A 3040 WINDSHIELD WIPER BOEING 727 727228 1384083 NM RIGHT OUT OF ADJUST A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 726DH 20409 RIGHT WIPER DOES NOT FUNCTION. WINDSHIELD WIPER KNOB FELL OFF. REPLACED SET SCREWS IAW B727 M/M 30-42-01. RECLOCKED R IGHT WINDSHIELD WIPER IAW BMM 30-42-01, OPERATIONAL CHECK IS GOOD. 2 L 7 3 4F RT A3WE 2002032500115 20020325 00115 NM 2002 3 25 F3LA200200110 1 20020316 A 5320 PANEL BOEING 737 73736E 138443A NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 314FL 3489 25256 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD LOWER DOOR FRAME PANEL CRACKED. FABRICATED AND INSTALLE D REPLACEMENT PANEL AND DOUBLER PER SRM 51-40-2. 2 L 7 2 4F RT A16WE 2002040300152 20020403 00152 CE 2002 4 3 GLBA2002032 1 20020313 A 2120 1013810159 VALVE BEECH 1900 1900D 1154162 CE LEFT LEAKING A GLBA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 NM 03 151GL 8432 3699 UE151 LEFT AND RIGHT ENVIROMENTAL FAILURE AND LOSS OF PRESSURIZATION, REPLACED INSTRUMENT AIR VALVE 2 L 7 2 4T RT A24CE 2002032500126 20020325 00126 CE 2002 3 25 GLBA2002033 1 20020313 A 3213 114810000656 TORQUE LINK BEECH 1900 1900D 1154162 CE LT MLG DAMAGED A GLBA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 03 170GL 6027 UE170 LEFT MAIN TORQUE KNEE SEPARATED DURING TAXI. REPLACED, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2002040300153 20020403 00153 CE 2002 4 3 GLBA2002034 1 20020316 A 3213 571302 MOTOR BEECH 1900 1900D 1154162 CE HYD SYSTEM INOPERATIVE A GLBA O OTHER O OTHER AP APPROACH 1 NM 03 100UX 995 UE100 LANDING GEAR RELAY C/B POPPED, REPLACED HYDRAULIC MOTOR OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2002032500127 20020325 00127 CE 2002 3 25 GLBA2002035 1 20020312 A 2150 A/C PACK BEECH 1900 1900D 1154162 CE A/C BAY FAILED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 226GL UE226 LEFT ENVIRONMENTAL FAILURE ON T/O. 2 L 7 2 4T RT A24CE 2002032500128 20020325 00128 CE 2002 3 25 GLBA2002036 1 20020318 A 7997 WIRE BEECH 1900 1900D 1154162 CE OIL SYSTEM BROKEN A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 255GL UE255 OIL TEMP INDICATOR FAILED. REPAIRED BROKEN WIRE, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002040300154 20020403 00154 2002 4 3 GLBA2002037 4 20020318 A 3416 57024929412 ENCODER BEECH 1900 1900D 1154162 CE COCKPIT INACCURATE A GLBA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 03 184UX 1588 UE184 #2 ENCODER REPORTED HIGH BY ATC, REPLACED ENCODING ALTIMETER OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2002032500129 20020325 00129 2002 3 25 GLBA2002038 4 20020318 A 3416 ALTIMETER BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GLBA O OTHER O OTHER CR CRUISE 1 NM 03 184UX UE184 ALTIMETER SPLIT. COULD NOT DUPLICATE, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2002032500130 20020325 00130 CE 2002 3 25 GLBA2002039 1 20020319 A 2437 WARNING SYSTEM BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GLBA O OTHER N FALSE WARNING CR CRUISE 1 NM 03 249GL UE249 OVER FLEW MCK, BATT-TIE ANNUN, OPENED IN FLIGHT, WOULD NOT RESET. PERFORMED SELF TEST SEVERAL TIMES, NO FAULT FOUND. I NSPECTED AND CHECKED OKAY FOR SERVICE. 2 L 7 2 4T RT A24CE 2002032500131 20020325 00131 EU 2002 3 25 QXEA0200508 1 20020322 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 SEA-EXIT SIGN BULB INOPERATIVE. LOCATED ON FORWARD FACING PANEL BETWEEN ROW 8 AND 9. REPLACED EXIT SIGN CIRCUIT BOARD. O PERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002032500133 20020325 00133 NE 2002 3 25 MALA020197 2 20020305 A 7321 6071T20P17 CONTROL UNIT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE MALFUNCTIONED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 457XJ 340B457 WHEN STARTING RT ENGINE, AFTER STARTER CUT OUT, NG AND ITT KEPT ACCELERATING. WHEN NG REACHES 85 PERCENT WHITE SMOKE AP PREARS FROM VENTILATION SYSTEM. SMOKE IS FAIRLY DENSE WITH NO ODOR. MAINTENANCE BORESCOPED POWER UNIT, FOUND NO EVIDEN CE OF OVERTEMP OR OTHER DEFECTS. REMOVED AND REPLACED DECU IAW GE MM 71-00-00. REMOVED AND REPLACED HMU IAW GE MM 73-0 0-00, OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2002032500134 20020325 00134 EU 2002 3 25 MALA020198 1 20020317 A 3620 CONNECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A1 30030 NE BLEED AIR CONTAMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 106XJ 340A106 AFTER TAKEOFF ON FLIGHT 3026 ON CLIMBOUT IN ICING CONDITIONS THE RT AIR VALVE LIGHT ILLUMINATED. AIR RETURN TO MSP. MA INTENANCE FOUND OIL IN CANNON PLUG W3P7. CLEANED CANNON PLUG, PERFORMED OPS CHECKS IAW GE MM APPENDIX 7. OPS CHECK GOO D. 2 L 7 2 4T 4 T RT A52EU E8NE 2002032500135 20020325 00135 EU 2002 3 25 MALA020199 1 20020315 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 DURING E-CHECK FOUND DENT UNDER CARGO DOOR AFT OF STA 630. MAINTENANCE COMPLETED REPAIR IAW SAAB STATEMENT. 2 L 7 2 4T RT A52EU 2002032500136 20020325 00136 EU 2002 3 25 MALA020201 1 20020318 A 3620 CONNECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE BLEED AIR CONTAMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 106XJ 340A106 DURING FLIGHT 3163 AFTER TAKEOFF ON CLIMBOUT IN ICING CONDITIONS THE RIGHT AIR VALVE LIGHT ILLUMINATED. AIR RETURN TO M SP. MAINTENANCE FOUND OIL IN CANNON PLUG 23P7, CLEANED CANNON PLUG, PERFORMED OPS CHECKS IAW GE MM APPENDEX 7. OPS CHE CK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2002032500137 20020325 00137 WP 2002 3 25 P2EA2002M017 1 20020315 A 3411 FITTING DOUG DC9 DC982 3022082 WP PITOT/STATIC SYS DEFECTIVE A P2EA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 CE 05 141NJ 49932 ON CLIMBOUT NO AIR SPEED WAS INDICATED ON CAPTAINS INDICATOR. SWITCHED TO BOTH ON 1 AND BOTH ON 2 AND PROBLEM REMAINED. AIRCRAFT RETURNED TO GATE WITH NO INCIDENT. FOUND PITOT FITTING ON NR 1 AIR DATA COMPUTER DEFECTIVE. REMOVED AND REP LACED FITTING IAW MM CHAPTER 20. PERFORMED PITOT/STATIC CHECK IAW MM 34-11-00, NO DEFECTS NOTED. 2 L 7 2 4F A6WE 2002032500138 20020325 00138 NM 2002 3 25 P5CA0200664 1 20020317 A 5415 BACB30EK6A8C BOLT BOEING 747 747122 1384872 NM PWA JT9 JT9D7 52054 NE NR 1 PYLON SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 685982 ONE BOLT HEAD SHEARED OFF ON RT SIDE OF NR 1 ENGINE AFT MOUNT TO PYLON FITTING. REMOVED AND REPLACED TWO BOLTS ON RT SI DE FOR AFT MOUNT TO FITTING PER MM 54-41-02. 2 L 7 4 4F 4 F A20WE E20EA 2002032500139 20020325 00139 NM 2002 3 25 P5CA0200665 1 20020317 A 5412 FIREWALL BOEING 747 747122 1384872 NM NR 3 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 CRACK ON CLOSURE BULKHEAD FIREWALL, NR 3 PYLON UNDER SLOT SEAL AREA. CRACK RUNS VERTICALLY APPROX 5 INCHES THEN SPLITS TO INBOARD SIDE. REPAIR CARRIED OUT REF SRM 54-10-03. CRACK STOP DRILLED PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002032600003 20020326 00003 NM 2002 3 26 02FDEA00215 1 20020323 A 3260 LAMP BOEING 727 72721C 138400M NM INST PNL FAILED A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 143FE 19136 02-79 LEFT GEAR DOWN LIGHT INOP. RELAMPED GEAR INDICATOR. OK FOR SERVICE. 2 L 7 3 4F A3WE 2002032600004 20020326 00004 NM 2002 3 26 SWAA020596 1 20020321 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 647SW 27717 DURING SCHEDULED RON, FOUND EEPLS COVER CRACKED AT ROW NR 3. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002032600005 20020326 00005 NM 2002 3 26 SWAA020600 1 20020317 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002032600006 20020326 00006 NM 2002 3 26 SWAA020601 1 20020317 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002032600007 20020326 00007 NM 2002 3 26 SWAA020602 1 20020321 A 5210 6545871 DOOR FRAME BOEING 737 737301 1384611 NM FWD ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT AFT DOOR STOP CUTOUT NR 7 FROM TOP. REPAIRED FRAME P ER SRM. 2 L 7 2 4F RT A16WE 2002032600008 20020326 00008 NM 2002 3 26 SWAA020603 1 20020321 A 5315 BAC1509 FLOORBEAM BOEING 737 737301 1384611 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 727B, LBL 2 TO LBL 12. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002032600009 20020326 00009 NM 2002 3 26 SWAA020604 1 20020320 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002032600010 20020326 00010 NM 2002 3 26 SWAA020605 1 20020321 A 5311 6546569 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SKIN REPAIR, FOUND BELL FRAME CRACKED AT BS 907, STR 21R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2002032600011 20020326 00011 NM 2002 3 26 SWAA020592 1 20020320 A 5312 6517582 WEB BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 228 AND RBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002032600012 20020326 00012 NM 2002 3 26 SWAA020594 1 20020320 A 5312 6516300 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 234, LBL 12 AND WL 210, RBL 7.0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002032600013 20020326 00013 WP 2002 3 26 MWEA020187 1 20020322 A 5310 3913291503 SPLICE DOUG DC9 DC932 3022066 WP STATION 560 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LONGERON 28 LEFT SPLICE AT STATION 560 IS CRACKED OUT AFT HOLE. -- REMOVED LONGERON SPLICE FITTING. MATCH DRILLED FITT ING. FABRICATED AND INSTALLED SHIMS TO SPLICE AND INSTALLED SPLICE TO LONGERONS. 2 L 7 2 4F A6WE 2002032600023 20020326 00023 EU 2002 3 26 0200853217 1 20020322 A 5311 FRAME AIRBUS 320 A320211 3930320 EU CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 317US 197 During "M" check found corrosion on frame 68 above door sill. Repaired per EA 32-18934. 2 L 7 2 4F RT A28NM 2002032600034 20020326 00034 WP 2002 3 26 ABXA010784 1 20020315 A 5310 4646163501 FITTING DOUG DC8 DC861 3021952 WP FWD. LWR. CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 SPLICE FITTING CRACKED AT LONGERON 27 RIGHT, STATION 450, FORWARD LOWER CARGO. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F 4A25 2002032600035 20020326 00035 WP 2002 3 26 ABXA010785 1 20020316 A 5300 FITTING DOUG DC8 DC861 3021952 WP FWD. LWR. CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 FORWARD CARGO, F.S. 380 - 400, LONGERON 31 LEFT, SPLICE FITTING WAS CRACKED. REMOVED AND REPLACED FITTING AT STA. 390, L ONGERON 31 LEFT IAW DC-8 SRM 51-1-24 AND 51-1-20D. 2 L 7 4 4F 4A25 2002032600036 20020326 00036 WP 2002 3 26 ABXA010786 1 20020319 A 5300 TM5606549 SEAT TRACK DOUG DC8 DC861 3021952 WP FWD LWR CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 FORWARD CARGO AT F.S. 580 - 600, LEFT BUTT LINE 50, SEAT TRACK WAS CRACKED. REPLACED SEAT TRACK IAW DC-9 SRM 51-3-0, 51- 1-8 AND ZANTOP DWG. #86302. 2 L 7 4 4F 4A25 2002032600037 20020326 00037 WP 2002 3 26 ABXA010787 1 20020319 A 5300 FRAME DOUG DC8 DC861 3021952 WP FWD LWR CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 FORWARD CARGO AT F.S. 180, ABOVE LONGERON 36 FRAME, UPPER CHORD WAS CRACKED AND BENT. REPAIRED AREA IAW DC-8 SRM STD-531 0-002 AND SRM 51-1-8. 2 L 7 4 4F 4A25 2002032600038 20020326 00038 WP 2002 3 26 ABXA010788 1 20020319 A 5300 3754220503N FITTING DOUG DC8 DC861 3021952 WP FWD LWR CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 FORWARD CARGO AT F.S. 200 - 220, LONGERON 31 LEFT, SPLICE FITTING WAS CRACKED. REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 2002032600039 20020326 00039 WP 2002 3 26 ABXA010789 1 20020320 A 5300 SEAT TRACK DOUG DC8 DC861 3021952 WP FWD LWR CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 FORWARD CARGO AT F.S. 340 - 360, LEFT BUTT LINE 50, SEAT TRACK WAS CRACKED. REPLACED SEAT TRACK IAW DC-8 SRM 51-1-8, 51- 3-0, 51-1-21 AND ZANTOP DWG. #86302. 2 L 7 4 4F 4A25 2002032600040 20020326 00040 EU 2002 3 26 MALA020207 1 20020322 A 3230 D49412001 CONTROL BOX SAAB SF340 340B 7860101 EU DEFECTIVE A MALA K NONE J WARNING INDICATION CL CLIMB 1 GL 15 453XJ 340B453 UPON DEPARTURE FROM YNG ON FLIGHT #3397, GEAR WOULD NOT RETRACT INTO UPLOCKED POSITION. QRH FOLLOWED AND FLIGHT WAS MAD E TO DTW WITH THE GEAR DOWN. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL BOX, PN D494-12-001, SN/ON 632/03-97 . SN/OFF 677/08-98. PERFORMED OPS CHECKS IAW SAAB AMM CH. 32-01-05. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002032600041 20020326 00041 EA 2002 3 26 COMA0260206 1 20020322 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 2750 130 7238 FLIGHT 5295 FLAPS FAILED AT 20 DEGREES.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2002032600042 20020326 00042 EA 2002 3 26 COMA0260207 1 20020323 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 709CA 7238 FLIGHT 5820 FLAPS FAILED AT 0 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002032600043 20020326 00043 EA 2002 3 26 COMA0260208 1 20020322 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 959CA 7116 FLIGHT 5288 CABIN DOOR WARNING MESSAGE.COULD NOT DUPLICATE. FOUND DOOR AND WARNING SYSTEM TO OPERATE NORMALLY. 2 L 7 2 4F RT A21EA 2002032600044 20020326 00044 EA 2002 3 26 COMA0260209 1 20020324 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 818CA 7408 FLIGHT 5921 FLAPS FAILED AT 27 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002032600045 20020326 00045 EA 2002 3 26 COMA0260210 1 20020322 A 5210 601R383831 PIVOT CNDAIR CL600 CL6002B19 1900309 EA DOOR CORRODED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 959CA 7116 FLIGHT 5288 CABIN DOOR WARNING MESSAGE.REPLACED THE DOOR LATCH BELLCRANK ASSY. 2 L 7 2 4F RT A21EA 2002032600046 20020326 00046 WP 2002 3 26 02FDEA00209 1 20020319 A 2750 CONTROL VALVE DOUG DC10 DC1010 3022110 WP T/E FLAP FAULTY A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 370FE 46608 AFTER T/O 9L FLL FLAP TAPES REMAIN IN T/O POS WITH HANDLE 0 EX. REMOVED AND REPLACED INBOARD FLAP CONTROL VALVE PER MM 27-52-02-2. 2 L 7 3 4F A22WE 2002032600047 20020326 00047 WP 2002 3 26 02FDEA00210 1 20020319 A 3620 DETECTOR DOUG DC10 DC1010F 3022111 WP PNEUMATIC SYS INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 364FE 46600 ON CLIMBOUT NR 2 MANIFOLD FAIL ILLUM'D. NR 2 MANIFOLD FAIL DET LOOP INOP, DO NOT PRESS PNEU SYS NR 2 EXCEPT FOR ENG STA RT. 2 L 7 3 4F A22WE 2002032600048 20020326 00048 EA 2002 3 26 COMA0260211 1 20020322 A 3220 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 915CA 8429 7013 FLIGHT 5369 GEAR DISAGREE MESSAGE WHEN GEAR SELECTED DOWN.REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002032600049 20020326 00049 EU 2002 3 26 02FDEA00211 1 20020321 A 7920 LINE AIRBUS 310 A310203 3930313 EU GE CF6 CF680A3 30025 NE NR 1 ENGINE LOOSE A FDEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 414FE 400 585175 ON DEPART ECAM IND NR 1 ENG LOW OIL PRESS. ENG SHUTDOWN. SECURED AND SAFETIED LOSE OIL LINE. RESERVICED OIL AND REMOV ED AND REPLACED OIL FILTER. 2 L 7 2 4F 4 F RT A35EU E13NE 2002040100037 20020401 00037 NM 2002 4 1 02FDEA00212 1 20020219 A 5531 SPAR BOEING 727 727233 138408A NM VERTICAL STAB WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 VERT FIN MID SPAR AT FIN STA 230-231 WORN OUT OF LIMITS AT STR 7. REMOVED AND REPLACED MIDSPAR PER EA 7-5510-62791. 2 L 7 3 4F RT A3WE 2002040100038 20020401 00038 NM 2002 4 1 02FDEA00213 1 20020218 A 5531 65168165 SPAR BOEING 727 727233 138408A NM VERTICAL STAB WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 VERT FIN MID SPAR IS WORN OUT OF LIMITS AT STR 7. REMOVED AND REPLACED MID SPAR PER SRM 55-30-6 FIG 3. 2 L 7 3 4F RT A3WE 2002032600051 20020326 00051 NM 2002 3 26 02FDEA00214 1 20020322 A 2751 TRANSMITTER BOEING 727 727227 1384078 NM T/E FLAP FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 483FE 21465 AFTER T/O ON FLAP RETRACT INBOARD FLAPS STUCK AT 2 DEG. R&R BOTH LT & RT INBD FLAP TRANSMITTERS PER MM 27-52-002-4. SA FTIED FLAP ARM SWITCH & GPWS FLAP INHIBIT SWITCH. OK FOR SERVICE. 2 L 7 3 4F A3WE 2002040800009 20020408 00009 NE 2002 4 8 200200184 2 20020321 A 7250 FLANGE BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE ENGINE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 662291 CRACK FROM THE "R" FLANGE LIGHTNING HOLE TO THE FLANGE OUTER DIAMETER AT THE 12 O'CLOCK POSITION. RADIAL CRACK ( 1/2 IN CH LONG) FROM THE "R" FLANGE LIGHTNING HOLE TO THE CASE WALL BUT NOT TO THE FILLET RADIUS AT THE 12:30 O'CLOCK POSITION. CRACK FROM THE "R" FLANGE LIGHTNING HOLE TO THE FLANGE OUTER DIAMETER AT THE 10 O'CLOCK POSITION. CRACK FROM THE "R" F LANGE LIGHTNING HOLE TO THE FLANGE OUTER DIAMETER AT THE 3 O'CLOCK POSITION. WELDED PER EIA ECRA# 662291-72-044-1 AND 7 47 MM 72-53-02. 2 L 7 4 4F 4 F A20WE E20EA 2002032600053 20020326 00053 NE 2002 3 26 200200185 2 20020321 A 7250 FLANGE BOEING 747 747132 1384882 NM PWA JT9 JT9D7F 52054 NE CASE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 685755 CRACK FROM -R- FLANGE LIGHTENING HOLE TO THE OUTER FLANGE AT THE 6 O'CLOCK POSITION. WELDED PER EIA ECRA 685755-72-010- 1 AND 747 MM 72-53-02. 2 L 7 4 4F 4 F A20WE E20EA 2002032600054 20020326 00054 NM 2002 3 26 200200186 1 20020321 A 5320 FITTING BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 BS 2484, LEFT LOWER BULKHEAD SPLICE FITTING AT STRINGER 23, CRACKED FROM LOWER INBOARD FASTENER. REMOVED AND REPLACED F ITTING PER SERVICE BULLETIN 53-2162, FIGURE 2. 2 L 7 4 4F A20WE 2002032600055 20020326 00055 WP 2002 3 26 2002F00322 1 20020214 A 5313 STRINGER LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 70577 193C1078 MID FUSELAGE SECTION, MAIN EQUIPMENT SERVICE CENTER, STRINGER 30, FS 930 TO 983, BL 25 AFT SIDE OF BULKHEAD 943 LEVEL 2 CORROSION. MAINTENANCE REPAIRED IN ACCORDANCE WITH SRM 53-13-00. 2 L 7 3 4F A23WE 2002032600056 20020326 00056 WP 2002 3 26 2002F00323 1 20020305 A 5313 STRINGER LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 70757 193C1078 FORWARD FUSELAGE SECTION, STRINGER 30, FS 235 TO 297, BL 24 HAS LEVEL 2 CORROSION. MAINTENANCE REMOVED AND REPLACED STR INGER 30 AT STATION 235 - 297 IN ACCORDANCE WITH SRM 51-40-01. 2 L 7 3 4F A23WE 2002032600059 20020326 00059 NE 2002 3 26 2002F00324 2 20020305 A 7320 FFG052AC FUEL CONTROL BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE MALFUNCTIONED G C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 11 551TZ 1821 1821 32585 31797 WHEN SETTING MAX T/O POWER LEFT THROTTLE LAGS BEHIND RIGHT THROTTLE. ABOVE 100 KTS IAS LEFT EPR DECREASED .03 WITH THRO TTLE AT FORWARD STOP LIMIT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE FUEL FLOW GOVERNOR. 2 L 7 2 4F 4 F RT A2NM E12EU 2002032600060 20020326 00060 WP 2002 3 26 2002F00325 1 20020315 A 2120 ODOR LKHEED 1011 10113853 5265020 WP CABIN DETECTED G A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 161AT 1219 FLIGHT NUMBER 7162, FLIGHT CREW REPORTED BURNING SMELL AROUND L2 AREA. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE I NSPECTED GENERAL AREA BEHIND AND ABOVE CEILING PANELS L2 AREA, NO DEFECTS NOTED. ALL PAX SYSTEM OPERATIONAL, AIRCRAFT W AS RETURNED TO SERVICE. 2 L 7 3 4F A23WE 2002032600063 20020326 00063 2002 3 26 372PA0007 4 20020321 A 2210 AUTOPILOT SYS BOEING 737 737306 NM COCKPIT MALFUNCTIONED A PIDA K NONE O OTHER CR CRUISE 1 SO 05 372PA 23546 VNAV FAILED REPEATEDLY, AFTER T/O, CLIMB AND CRUISE. DEFAULTED TO TOGA, SPEED, AND PATH IS ABANDONED. 2 L 7 2 4F RT A16NE 2002032600064 20020326 00064 WP 2002 3 26 ABXA010782 1 20020320 A 3297 WIRE DOUG DC9 DC932 3022066 WP NLG BROKEN A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 982AX 47317 ON LANDING AT BDL, NO GREEN GEAR LIGHT. RECYCLED LANDING GEAR, THE GREEN LIGHT ILLUMINATED. REPAIRED BROKEN WIRES TO T HE NOSE GEAR UP LIMIT SWITCH CONNECTOR (P1-134) AND REPLACED THE UP LIMIT SWITCH AS A PRECAUTION. OPS CHECKED GOOD IAW DC9 MM 32-60-01-02. 2 L 7 2 4F A6WE 2002032600065 20020326 00065 WP 2002 3 26 AT0200037 1 20020320 A 2120 DUCT DOUG DC9 DC932 3022066 WP A/C BAY DAMAGED A ZZDA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 15 837AT 45774 OIL SMELL AND SMOKE DETECTOR GOING OFF. FOUND RIGHT PACK ACM DUCT BLOWN. REPAIRED HOLE IN DUCT. 2 L 7 2 4F A6WE 2002032600066 20020326 00066 NM 2002 3 26 AWXA200200237 1 20020310 A 5314 BAC15062002 KEELBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR -C- DURING C-17 CHECK CORROSION WAS FOUND ON KEEL BEAM CHORD AT BS 500 TO BS 520, LBL 6.5, WL 148.4. 2 L 7 2 4F RT A16WE 2002032600067 20020326 00067 NM 2002 3 26 AWXA200200239 1 20020312 A 5314 BAC15062002 KEELBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - C - DURING C-17 CHECK CORROSION WAS FOUND ON LOWER CHORD FROM BS 520 TO BS 525.5, WL 148.4, LBL 6.5 . 2 L 7 2 4F RT A16WE 2002032600068 20020326 00068 SO 2002 3 26 C2XA02BT011 1 20020320 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN DAMAGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12922 145338 CREW REPORTED EMERGENCY AISLE PATH LIGHTING INOPERATIVE. MAINTENANCE TROUBLESHOT SYSTEM AND REPAIR DAMAGED WIRING. OPS CHECKED SYSTEM GOOD. AIRCRAFT RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002032600069 20020326 00069 SO 2002 3 26 C2XA02IA078 1 20020324 A 3234 355022022 CONTROL UNIT EMB 145 EMB145 3260210 SO COCKPIT FAULTY A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 14972 145151 IAH- FLIGHT 4172, AFTER TAKEOFF, LD/AIR GROUND FAIL MESSAGE AND THRUST REV DISAGREE MESSAGE APPEARED EICAS AND, REMAINE D ON ENTIRE FLIGHT QRH'S COMPLETED. NO SPEED BRAKES INFLIGHT. NORMAL LANDING OCCURRED IN IAH. REMOVED AND REPLACED TH E LANDING GEAR ELECTRONIC UNIT, PERFORMED A OPERATIONAL CHECK IAW EMB145 M/M 32-32-01. NO DEFECTS NOTED AND THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002032600070 20020326 00070 SO 2002 3 26 C2XA02TY056 1 20020221 A 2730 14522150401 BELLCRANK EMB 145 EMB145 3260210 SO ELEVATOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15974 145159 TYS DURING A SCHEDULED EA-2730-01044 INSPECTION, THE RIGHT SIDE QUADRANT BELLCRANK WAS FOUND CRACKED. MAINTENANCE REM OVED AND REPLACED THE RIGHT BELL QUADRANT IAW EMB-145 MM 27-31-03. OPS CHECK WAS GOOD AND WILL BE RELEASED UPON COMPLET ION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002032600071 20020326 00071 SO 2002 3 26 C2XA02TY057 1 20020322 A 2730 14522150401 BELLCRANK EMB 145 EMB145 3260210 SO ELEVATOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13958 145085 TYS, DURING A SCHEDULED INSPECTION, THE RIGHT ELEVATOR QUADRANT BELL CRANK WAS FOUND CRACKED. MAINTENANCE REMOVED AND R EPLACED THE BELL CRANK IAW-EMB-145-AMM-27-31-03, OPERATIONAL CHECKED GOOD. AIRCRAFT WAS RELEASED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002032600072 20020326 00072 WP 2002 3 26 CALA0200141 1 20020319 A 2121 6054573 FAN DOUG DC9 DC982 3022082 WP A/C BAY OVERHEATED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 92874 35600 49122 THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL SMOKE ODOR APPARENTLY COMING FROM THE RIGHT AFT LAV AREA AFTER TAKEOFF FROM MIA. THE AIRCRAFT WAS RETURNED TO MIA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE CABIN AIR RECIRCULA TION FAN HAD OVERHEATED. THE CABIN RECIRCULATION FAN WAS REMOVED AND REPLACED IAW MM 21-20-12. OPERATIONAL CHECKS WERE GOOD WITH NO ODORS DETECTED. 2 L 7 2 4F A6WE 2002032600073 20020326 00073 NE 2002 3 26 CG8A20020005 2 20020321 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D15 52051 NE NR 2 VIBRATION A C8GA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 15 89427 21365 687407 FLT 202 FROM MPTO TO KMIA. DURING CRUISE LEVEL, AT FL310 THE NR 2 ENGINE EXPERIENCE VIBRATION THAT WAS FELT IN THE NR 2 THROTTLE. AT IDLE, THE NR 2 OIL PRESSURE REMAINED NORMAL UNTIL THE OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED. A PR ECAUTIONARY ENGINE SHUTDOWN PROCEDURE WAS INITIATED AND DESCENDED TO FL240 AND PROCEEDED TO FINAL DESTINATION AND LANDED WITHOUT ANY INCIDENT. PERFORMED ENGINE TROUBLESHOOTING, REMOVED/INSTALLED NEW OIL FILTER, RAN AND LEAK CHECK ENGINE AN D FOUND TO BE OK FOR RETURN TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002032600074 20020326 00074 NM 2002 3 26 F3LA200200116 1 20020321 A 5315 FLOORBEAM BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 314FL 3489 25256 DURING C-2 CHECK, INSPECTION REPORTED FLOORBEAM AT R-2 DOOR CORRODED. FABRICATED AND INSTALLED REPAIR PER SRM 53-60-51 AND 53-00-51 FIG 203. 2 L 7 2 4F RT A16WE 2002032600075 20020326 00075 2002 3 26 GLBA2002040 4 20020220 A 3454 6226137201 RECEIVER BEECH 1900 1900D 1154162 CE NR 2 FAILED A GLBA O OTHER O OTHER AP APPROACH 1 NM 03 254GL 519 UE254 NAV RADIO FAILED ON APPROACH. REPLACED NAV RADIO, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002032600076 20020326 00076 NM 2002 3 26 P5CA0200668 1 20020318 A 7930 21SN0471 SWITCH BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE NR 3 ENGINE FAULTY A P5CA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 23 921FT 21575 689185 OIL FILTER BYPASS LIGHT ON NR 3 ENGINE ILLUMINATED DURING CRUISE ON AIRWAY A450 EN ROUTE FROM GUM TO HNL AT 1715Z. NR 3 ENGINE SHUT DOWN IAW ABNORMAL PROCEDURE 6-15-10. LANDING WAS UNEVENTFUL. INSPECTION DETERMINED INTERNAL FAILURE IN PR ESSURE SWITCH AS CAUSE. REMOVED AND REPLACED OIL PRESS BYPASS SWITCH, REPLACED OIL FILTER AND INSPECTED MAG PLUGS. OPS CHECKED GOOD IAW MM 71-00-00. 2 L 7 4 4F 4 F A20WE E3NE 2002032600078 20020326 00078 EU 2002 3 26 QXEA0200396 1 20020218 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CORROSION UNDER NUT PLATES ON FRAME 6305 ON FOUR WAY FLOOR SUPPORT ABOVE STRINGER 74. REPAIRED IAW FOKKER MM 53-0 0-2, PAGES 601-602 AND SRM 51-31-04. 2 L 7 2 4F RT A20EU 2002032600079 20020326 00079 EU 2002 3 26 QXEA0200397 1 20020213 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT WING UPPER SURFACE AT STATION 9890, MINOR CHAFED AREA. REPAIRED IAW FOKKER SRM 53-01-01, SRM 51-10-4 AND SRM 5 1-30-03. 2 L 7 2 4F RT A20EU 2002032600080 20020326 00080 WP 2002 3 26 ABXA010790 1 20020315 A 5300 FITTING DOUG DC8 DC861 3021952 WP FWD LWR CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 FORWARD LOWER CARGO, STATION 272, FITTING WAS CRACKED FORWARD OF C1 DOOR. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1 -20D, 51-3-1 AND 51-1-24. 2 L 7 4 4F 4A25 2002032600081 20020326 00081 WP 2002 3 26 ABXA010792 1 20020310 A 5300 SEAT TRACK DOUG DC8 DC861 3021952 WP FWD LWR CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 FORWARD CARGO AT F.S. 580 - 600, AT LEFT BUTT LINE 55, SEAT TRACK WAS CRACKED. REMOVED AND REPLACED SEAT TRACK IAW DC-8 SRM 51-3-0, 51-1-24 AND 51-1-8. 2 L 7 4 4F 4A25 2002032600083 20020326 00083 EU 2002 3 26 QXEA0200415 1 20020220 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - TWO GOUGES AFT OF RT ACM LOWER MOUNT ON WALL SKIN. REPAIRED IAW HORIZON AIR EA 4-53-157 AND FOKKER SRM 51-30-01. 2 L 7 2 4F RT A20EU 2002032600084 20020326 00084 EU 2002 3 26 QXEA0200416 1 20020218 A 5210 DOOR FOKKER F28 F28MK4000 4990810 EU PAX DOOR STUCK A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - PASSENGER DOOR WILL NOT OPEN IN EMERGENCY MODE. REPAIRED IAW FOKKER SRM 52-10-05, PAGES 413-414, PARAGRAPH 6J, ST EPS 1-7 AND SRM 52-10-05, PAGES 414-415. 2 L 7 2 4F RT A20EU 2002032600085 20020326 00085 EU 2002 3 26 QXEA0200417 1 20020221 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CHAFE ON AFT CARGO DOOR APERTURE, AFT SIDE APPROXIMATELY 14 INCHES FROM LOWER CORNER. REPAIRED IAW FOKKER SRM 53- 01-01, PAGE 8, PARAGRAPH 3D AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B AND 4C. 2 L 7 2 4F RT A20EU 2002032600086 20020326 00086 EU 2002 3 26 QXEA0200418 1 20020216 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CORROSION UNDER NUT PLATES ON FRAME 9305 AT FOUR WAY FLOOR SUPPORT BETWEEN STRINGER 74 AND CENTER LINE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6, PARA 4B, SRM 51-31-01, PAGE 13, CHAPTER 7 AND SRM 51-30-02, PAGE 9-10. 2 L 7 2 4F RT A20EU 2002032600087 20020326 00087 EU 2002 3 26 QXEA0200419 1 20020216 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CORROSION UNDER NUT PLATES ON FRAME 9305B AT FOUR WAY FLOOR SUPPORT INBOARD OF STRINGER 74. REPAIRED IAW FOKKER S RM 51-31-01, PAGE 13, CHAPTER 7. 2 L 7 2 4F RT A20EU 2002032600088 20020326 00088 EU 2002 3 26 QXEA0200420 1 20020216 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - STRINGER 64 CORRODED AT FORWARD END, AFT OF FRAME 3820. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, SRM 53-01-01, P AGE 6, PARAGRAPH 3 (A) AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2002032600089 20020326 00089 EU 2002 3 26 QXEA0200421 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 525-709 TOP LUGS HAVE GOUGES. REPAIRED IAW FOKKER MM 53-40-01, PAGE 205, FIGURE 204. 2 L 7 2 4F RT A20EU 2002032600090 20020326 00090 EU 2002 3 26 QXEA0200422 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 506.028 TOP LUGS HAVE GOUGES. REPAIRED IAW FOKKER MM 53-40-01, PAGE 205, FIGURE 2 04. 2 L 7 2 4F RT A20EU 2002032600091 20020326 00091 EU 2002 3 26 QXEA0200423 1 20020302 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 488.740 THERE ARE GOUGES ON TOP LUGS AND FLANGE AT FRAME 10966. REPAIRED IAW FOK KER MM 53-40-01, PAGE 205, FIGURE 204 AND SRM 53-02-15, FIGURE 1. 2 L 7 2 4F RT A20EU 2002032600092 20020326 00092 EU 2002 3 26 QXEA0200424 1 20020302 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 488.738 HOLE FOR FLOORBOARD RECEPTACLE HAS CHAFING ON FLANGE. REPAIRED IAW FOKKE R MM 53-40-01, PAGE 206, FIGURE 306 AND SRM 53-02-15, FIGURE 1. 2 L 7 2 4F RT A20EU 2002032600093 20020326 00093 EU 2002 3 26 QXEA0200457 3 20020312 A 6140 WARNING SYSTEM BOMBDR DHC8 DHC8401 NM ROTOL R408 CR4086123F17 EU COCKPIT MALFUNCTIONED A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 408QX 4050 GEG - AUTO FEATHER FAILED TO ARM ON TAKEOFF. RETURNED TO GATE, PERFORMED AUTO FEATHER TEST. SYSTEM TEST NORMAL. NO DI SCREPANCIES NOTED. NO FAULT FOUND IN CDS SYSTEM INTERROGATION. NO PART REPLACED AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P17BO 2002032600094 20020326 00094 EU 2002 3 26 QXEA0200477 3 20020317 A 6140 WARNING SYSTEM BOMBDR DHC8 DHC8401 NM ROTOL R408 CR4086123F17 EU COCKPIT MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING UK UNKNOWN 1 NM 09 413QX 4060 SEA - RETURN TO GATE, AUTO FEATHER ARM LIGHT INOP. GROUND RAN AIRCRAFT AFTER DIAGNOSTICS OF MDC, NO DEFECTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P17BO 2002041800113 20020418 00113 NM 2002 4 18 QXEA0200478 1 20020317 A 6120 699018002 CONTROLLER BOMBDR DHC8 DHC8401 NM NR 1 PROPELLER MALFUNCTIONED A QXEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NM 09 412QX 233 233 4059 SMF - ON POWER REDUCTION RECEIVED NR 1 PEC LIGHT AND NR 1 PROP OVERSPEED. SHUTDOWN NR 1 ENGINE, LANDED WITHOUT INCIDENT . REMOVED AND REPLACED PEC, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002032600095 20020326 00095 NM 2002 3 26 QXEA0200479 1 20020314 A 3150 SWITCH DHAV DHC8 DHC8202 2809007 NM COCKPIT LACK OF LUBE A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 354PH 498 PDX - TAKEOFF WARNING HORN ACTIVATED ON TAKEOFF. ABORTED TAKEOFF, RAN CHECKLIST, TALKED TO MAINTENANCE CONTROL AND RAN TORQUE UP. DID NOT GET THE TAKEOFF WARNING HORN DURING CONFIGURATION CHECK. ATTEMPTED SECOND TAKEOFF AND RECEIVED TAKE OFF WARNING HORN. CLEANED AND LUBED SWITCHES UNDER PEDESTAL. GROUND RAN AIRCRAFT. OPERATIONAL CHECK GOOD. NO PARTS R EPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002032600096 20020326 00096 NM 2002 3 26 QXEA0200480 1 20020215 A 3250 WARNING SYSTEM BOMBDR DHC8 DHC8401 NM COCKPIT MALFUNCTIONED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 400QX 4032 SEA - UPON GEAR EXTENSION, NOSE STEERING CAUTION LIGHT ILLUMINATED. CYCLED NOSE STEERING SWITCH ACCORDING TO EMERGENCY CHECK LIST AND LIGHT WENT OUT. TAXIED AIRCRAFT AND OPERATED NOSE WHEEL STEERING SYSTEM. NO PARTS REPLACED. OPERATIONA L CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002032600097 20020326 00097 NM 2002 3 26 SWAA020436 1 20020226 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED C4 CHECK, FOUND LEFT LOWER OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002032600098 20020326 00098 2002 3 26 SWAA020438 4 20020226 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 AFT SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002032600099 20020326 00099 NM 2002 3 26 SWAA020442 1 20020226 A 5320 6551698 SPLICE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 5L. REPAIRED STR SPLICE PER SRM. 2 L 7 2 4F A16WE 2002032600122 20020326 00122 NM 2002 3 26 SWAA020447 1 20020226 A 2731 654516618 ROD END BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED C3 CHECK, SWA SI 11111-55, LT ELEVATOR, FOUND TAB PUSH ROD ENDS WORN. REMOVED AND REPLACED LT ELEVATOR ROD ENDS PER MM. 2 L 7 2 4F RT A16WE 2002032600123 20020326 00123 NM 2002 3 26 SWAA020449 1 20020226 A 3350 BR2013 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 EEPLS COVER MISSING AND WIRES EXPOSED AT LT OVERWING EMERGENCY EXIT. REMOVED AND REPLACED EEPLS LIGHT ASSY AND SECURED WIRES PER MM. 2 L 7 2 4F RT A16WE 2002032600124 20020326 00124 NM 2002 3 26 SWAA020451 1 20020228 A 2560 6557463 BRACKET BOEING 737 7377H4 1384404 NM FWD ENTRY OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 414WN 29820 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR WOULD NOT LATCH TO FLOOR BRACKETS. REPOSITIONED GIRT BAR BRACKETS PER MM. 2 L 7 2 4F RT A16WE 2002032600125 20020326 00125 2002 3 26 SWAA020454 4 20020227 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM CABIN DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED C2 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2 L 7 2 4F A16WE 2002032600126 20020326 00126 NM 2002 3 26 SWAA020455 1 20020228 A 5311 96380 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 609SW 27929 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OUTBOARD CHORDS CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CH ORDS PER SWA ACO. 2 L 7 2 4F RT A16WE 2002032600127 20020326 00127 2002 3 26 SWAA020456 4 20020227 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002032600128 20020326 00128 2002 3 26 SWAA020461 4 20020302 A 2565 61621469 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002032600129 20020326 00129 2002 3 26 SWAA020462 4 20020303 A 2565 22D22900131 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 FWD SVC DOOR EMERGENCY EVAC SLIDE HAS LOW PRESS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F A16WE 2002032600130 20020326 00130 NM 2002 3 26 SWAA020463 1 20020303 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 771SA 27879 EEPLS WIRES EXPOSED. SECURED WIRES PER MM. 2 L 7 2 4F RT A16WE 2002032600131 20020326 00131 NM 2002 3 26 SWAA020467 1 20020303 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 706SW 27840 DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT ROW NR 7. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002032600133 20020326 00133 NM 2002 3 26 UPS02237821 1 20020225 A 3211 LINK BOEING 727 72731C 1384011 NM LT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:C ON REMOVAL OF LT MLG TRUNNION LINK EXCESSIVE CORROSION WAS FOUND ON FWD SPLINED LOCKING SLEEVE. LT ML G TRUNNION LINK REPLACED IAW MM 32-11-01. 2 L 7 3 4F A3WE 2002032600134 20020326 00134 NM 2002 3 26 UPS02237822 1 20020225 A 5754 RIB BOEING 727 72731C 1384011 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:C LT WING, NR 3 SLAT, CRACK IN O/B RIB AT O/B TRACK, FWD TRACK ATTACH AREA. CRACK STOP DRILLED IAW SRM 51-10-1, REPAIR CARRIED OUT IAW SRM 57-50-3. 2 L 7 3 4F A3WE 2002032600137 20020326 00137 NM 2002 3 26 UPS02237869 1 20020221 A 5314 KEELBEAM BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:C CRACK FOUND IN KEEL BEAM WEB FWD OF APU CUTOUT. CRACK REPAIRED IAW SRM ADDENDUM EO B727-5330-1995-B U SING KIT P/N 65 -88832-2 AND BOEING DRG 65-88832 AND 65-22466. 2 L 7 3 4F A3WE 2002032600138 20020326 00138 NM 2002 3 26 UPS02237871 1 20020221 A 5320 FITTING BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:C LT BS 740 FITTING CRACKED IN 2 PLACES IN O/B FLANGE LOWER END. REPLACED LT FITTING IAW EO B727-5310-7 477-G. 2 L 7 3 4F A3WE 2002032600139 20020326 00139 NM 2002 3 26 UPS02237879 1 20020228 A 5320 FITTING BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:C CRACK AND CORROSION INDICATIONS FROM FASTENER HOLES AT BS 870L STR 13L TO STR 12L. 2 L 7 3 4F A3WE 2002032600141 20020326 00141 NM 2002 3 26 UPS02237913 1 20020320 A 3350 LIGHT BOEING 727 7272A1 138407F NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT AND OPS CHECK NORMAL IAW B727 MM 33-50-101. 2 L 7 3 4F A3WE 2002032600145 20020326 00145 NM 2002 3 26 UPS02437413 1 20020116 A 5714 STRUCTURE BOEING 747 747123 1384873 NM WING BOX CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:SP CENTER WING BOX UPPER SKIN HAS EXFOLIATION CORROSION APPROX 4 INCHES IN DIAMETER STA 1110, RBL 104. REPAIRED AREA IAW ENGINEERING FILE 747-57-20016. 2 L 7 4 4F A20WE 2002032600147 20020326 00147 NM 2002 3 26 UPS02437575 1 20020126 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 1780 RBL 95 SEAT TRACK CROWN FOUND CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002032600148 20020326 00148 NM 2002 3 26 UPS02437576 1 20020130 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - LBL 75 BS 2240-2280 FLOOR SUPPORT CORRODED. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2002032600149 20020326 00149 NM 2002 3 26 UPS02437577 1 20020131 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - LBL 11 BS 2240 FLOORBEAM WEB CORRODED (NEAR LWR CHORD). FLOORBEAM WEB REPLACED AS PER SRM 51-10 -01 PG 8. 2 L 7 4 4F A20WE 2002032600150 20020326 00150 NM 2002 3 26 UPS02437578 1 20020131 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - LBL 57 BS 2240 FLOORBEAM AFT SIDE WEB CORRODED (NEAR UPPER CHORD). FLOORBEAM WEB REPLACED AS PE R SRM 51-10-01, REFER NRC 7698. 2 L 7 4 4F A20WE 2002032600151 20020326 00151 NM 2002 3 26 UPS02437582 1 20020130 A 5347 BAC15201567 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - SEAT TRACK FOUND CORROSION AT BS 2225 RBL 75 AFTER FLOOR PANEL REMOVED. SEAT TRACK REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002032600153 20020326 00153 NM 2002 3 26 UPS02437586 1 20020129 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 2240 RBL 75 - RBL 33 FLOORBEAM WEB FOUND CORRODED. FLOORBEAM REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002032600154 20020326 00154 NM 2002 3 26 UPS02437592 1 20020130 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 218 RBL 45 SEAT TRACK FLANGE CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002032600155 20020326 00155 NM 2002 3 26 UPS02437593 1 20020126 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D BS 1900 RBL 97 SEAT TRACK CROWN CORROSION FOUND. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002032600157 20020326 00157 NM 2002 3 26 UPS02437594 1 20020129 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C AFT OF BULK CARGO - S49R BS 2218 STRINGER CORRODED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002032600160 20020326 00160 NM 2002 3 26 UPS02437595 1 20020204 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C BULK CARGO COMPT - BS 1980 RBL 45 - 50 LONG FLOOR SUPPORT FOUND CORROSION DAMAGE. FLOOR SUPPORT REPAI RED AS PER SRM 53-10-07 FIG 20. 2 L 7 4 4F A20WE 2002032600162 20020326 00162 NM 2002 3 26 UPS02437596 1 20020126 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C U/D - BS 340 LBL 10 - 20 FLOORBEAM SURFACE FOUND CORROSION. 2 L 7 4 4F A20WE 2002032600164 20020326 00164 NM 2002 3 26 UPS02437598 1 20020130 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - LBL 75 - 90 BS 2240 - 2280 FLOOR SUPPORT CORRODED. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 F IG 4. 2 L 7 4 4F A20WE 2002032600166 20020326 00166 NM 2002 3 26 UPS02437599 1 20020129 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 2196 RBL 11 SEAT TRACK CROWN FOUND CORRODED. BS 2190 - 2250 RBL 11 SEAT TRACK REPLACED PER S RM 51-10-01. 2 L 7 4 4F A20WE 2002032600169 20020326 00169 NM 2002 3 26 UPS02437601 1 20020125 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 260 - 280 LBL 33 SEAT TRACK FLANGE CORRODED. SEAT TRACK REPAIRED AS PER SRM 51-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002032600171 20020326 00171 NM 2002 3 26 UPS02437628 1 20020128 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C AFT CARGO COMPT - RBL 31-42 BS 1660 FLOORBEAM UPPER CHORD CORRODED. FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-41-04 FIG 2. 2 L 7 4 4F A20WE 2002032600173 20020326 00173 NM 2002 3 26 UPS02437629 1 20020128 A 5347 CARGO TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C AFT CARGO COMPT - RBL 25 BS 1870 TIE DOWN TRACK CORRODED DAMAGED. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 5. 2 L 7 4 4F A20WE 2002032600175 20020326 00175 NM 2002 3 26 UPS02437630 1 20020128 A 5347 CARGO TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C AFT CARGO COMPT - RBL 46 BS 1860 - 1900 TIE DOWN TRACK CORRODED. TIE DOWN TRACK REPAIRED AS PER SRM 5 3-10-05 FIG 5. 2 L 7 4 4F A20WE 2002032600177 20020326 00177 NM 2002 3 26 UPS02437637 1 20020126 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 1820 RBL 97 SEAT TRACK CROWN FOUND CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002032600179 20020326 00179 NM 2002 3 26 UPS02437638 1 20020127 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 360 S-22R FRAME FOUND CRACKED. M/D BS 360 FRAME REPAIRED AS PER SRM 53-10-04 FIG 85. 2 L 7 4 4F A20WE 2002032600181 20020326 00181 NM 2002 3 26 UPS02437639 1 20020128 A 5320 141U109212 CLIP BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C RT SIDE NOSE W/W ON BS 320 VERTICAL BEAM CLIP FOUND CRACK AT NR 5 CLIP (COUNT FROM TOP) AS MARKED. CL IP REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002032600185 20020326 00185 NM 2002 3 26 UPS02437640 1 20020128 A 5320 114U11076 WEB BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C RT SIDE W/W ON BS 300 VERTICAL BEAM WEB FOUND 1 EA INSULATION BLANKET STAND-OFF HOLE CRACKED AND JUST BETWEEN NR 1 & 2 STIFFENER. VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002032600187 20020326 00187 NM 2002 3 26 UPS02437641 1 20020128 A 5320 141U11073 WEB BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C LT SIDE NOSE W/W ON BS 320 VERTICAL BEAM WEB FOUND 1 EA INSULATION BLANKET STAND-OFF HOLE CRACKED, JUS T BETWEEN NR 4 & 5. VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002032600189 20020326 00189 NM 2002 3 26 UPS02437642 1 20020128 A 5320 141U11075 WEB BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C, LT SIDE NOSE W/W ON BS 380 VERT BEAM WEB FOUND 2 EA INSULATION STANDOFF HOLES CRACKED, 1 EA JUST BETW EEN 1 & 2 STIFFENER AND 1 EA JUST BETWEEN NR 5 STIFFENER AND 1 EA JUST BETWEEN NR 5 STIFFENER. VERT BEAM WEB REPLACED A S SRM 51-10-01. 2 L 7 4 4F A20WE 2002032600191 20020326 00191 NM 2002 3 26 UPS02437643 1 20020123 A 5230 SKIN BOEING 747 747123 1384873 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C AFT CARGO - CARGO DOOR FWD UPPER CORNER FOUND CRACKED AS MARKED. 2 L 7 4 4F A20WE 2002032600193 20020326 00193 NM 2002 3 26 UPS02437644 1 20020123 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C FX - SKIN SLIGHTLY BULGED UP AT BS 2200 S-32L & S-32R. APPROX SKIN REPAIRED PER SRM 53-30-03 FIG 1. 2 L 7 4 4F A20WE 2002032600197 20020326 00197 NM 2002 3 26 UPS02437645 1 20020203 A 5210 DOOR FRAME BOEING 747 747123 1384873 NM R1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - AFTER R1 DOOR INTERIOR HANDLE MECHANISM HOUSING REMOVED, THE DOOR CTR FRAME ACCESS HOLE CUTOUT F OUND CRACKED NEAR WINDOW AREA. FRAME WEB REPAIRED PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002032600200 20020326 00200 NM 2002 3 26 UPS02437646 1 20020128 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C RIGHT BLG W/W PRESSURE DECK O/B LWR SURFACE BETWEEN BS 1367 & 1372 AREA CORRODED AS MARKED. PRESSURE DECK BOND SKIN REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002032600201 20020326 00201 NM 2002 3 26 UPS02437647 1 20020120 A 5313 STRINGER BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 524UP INSPECTION TYPE:C AFT CARGO - STRINGER 51R FOUND CORRODED AT STA 1680. 2 L 7 4 4F RT A20WE 2002032600202 20020326 00202 NM 2002 3 26 UPS02437648 1 20020120 A 5313 STRINGER BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 524UP INSPECTION TYPE:C BULK CARGO - STA 2160 CORROSION FOUND AT STR 45L. 2 L 7 4 4F RT A20WE 2002032600203 20020326 00203 NM 2002 3 26 2002UALA00488 1 20020317 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 CABIN FLOORBEAM STATION 303, RBL 88 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM NEW SECTION WITH SPLICE A NGLES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002032600204 20020326 00204 NM 2002 3 26 2002UALA00497 1 20020315 A 5315 CHANNEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 CABIN FLOOR SUPPORT CHANNEL HAD EXCESSIVE CORROSION ON UPPER SURFACE BETWEEN STATION 310 AND 324 RBL 40" STRINGER 17R. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW OUTSIDE CENDER NEW CHANNEL INTERCOSTAL FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032600205 20020326 00205 NM 2002 3 26 2002UALA00519 1 20020320 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 BODY STATION 617 WL215 ZONE A, FWD DR2 LOWER AREA DAMAGED WITH 2 X 3 INCH PUNCTURE. MAJOR REPAIR ACCOMPLISHED.DOUBLER AND TRIPLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032600206 20020326 00206 NM 2002 3 26 UPS02437649 1 20020120 A 5313 STRINGER BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 524UP INSPECTION TYPE:C AFT CARGO - STRINGER 51L FOUND CORRODED AT STA 1685. 2 L 7 4 4F RT A20WE 2002032600207 20020326 00207 NM 2002 3 26 UPS02437658 1 20020211 A 5210 SKIN BOEING 747 747123 1384873 NM L3 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - DURING FINAL DOOR CLOSE UP L3 DOOR EXTERNAL SKIN CRACKED AT BS 1295 & 1305 WL 210 AREA 2 LOCATIO NS AS MARKED. DOOR SKIN REPAIRED AS PER SRM 52-10-02 FIG 9. 2 L 7 4 4F A20WE 2002032600208 20020326 00208 NM 2002 3 26 UPS02437659 1 20020124 A 5210 SKIN BOEING 747 747123 1384873 NM L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - L1 DOOR UPPER HINGE CUTOUT FOUND CRACKED AS MARKED. HINGE CUTOUT SKIN REPAIRED AS PER SB 747-52 -2144. 2 L 7 4 4F A20WE 2002032600209 20020326 00209 NM 2002 3 26 UPS02437660 1 20020130 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - FLOOR SUPPORT FOUND CORROSION AT BS 2240 RBL 75-85 AFTER FLOOR PANEL REMOVED. FLOORBEAM REPAIRE D AS PER SRM 51-40-04 FIG 2. 2 L 7 4 4F A20WE 2002032600210 20020326 00210 NM 2002 3 26 UPS02437661 1 20020124 A 5210 DOOR FRAME BOEING 747 747123 1384873 NM R4 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D R4 DOOR AFT FRAME LOWER CORNER FOUND CRACKED. DOOR AFT FRAME LOWER CORNER REPAIRED AS PER SRM 52- 10-02. 2 L 7 4 4F A20WE 2002032600211 20020326 00211 2002 3 26 SWAA020608 4 20020321 A 2565 6557463 BRACKET BOEING 737 7375H4 138449D NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE FLOOR GIRT BRACKET LOOSE. SECURED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2002032600212 20020326 00212 NM 2002 3 26 SWAA020613 1 20020324 A 5312 6516300 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 234, LBL 11 AND RBL 11. REPAIRED WEB PER S RM. 2 L 7 2 4F RT A16WE 2002032600213 20020326 00213 NM 2002 3 26 SWAA020615 1 20020322 A 5210 507945178 DOOR BOEING 737 737301 1384611 NM FWD ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT AFT DOOR STOP CUTOUT NR 6 FROM TOP. REMOVED AND REPL ACED DOOR PER MM. 2 L 7 2 4F RT A16WE 2002032600214 20020326 00214 NM 2002 3 26 SWAA020616 1 20020324 A 5320 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR'S 2R AND 3R. REMOVED AND REPLACED SHEAR TIE P ER SRM. 2 L 7 2 4F RT A16WE 2002032600215 20020326 00215 NM 2002 3 26 SWAA020617 1 20020324 A 5755 6573735 SPOILER BOEING 737 7373H4 1384600 NM RH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D CHECK, FOUND NR 5 T/E GRD SPOILER DELAMINATED ON UPPER SURFACE 3.75 INCHES AFT OF FWD END. REPAIRED NR 5 T/E SPOILER PER SRM. 2 L 7 2 4F RT A16WE 2002032600216 20020326 00216 NM 2002 3 26 SWAA020618 1 20020322 A 5330 6545768 SKIN BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 340LV 23738 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AFT OF E/E EXHAUST CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002032600217 20020326 00217 NM 2002 3 26 SWAA020619 1 20020322 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT 2.5 INCHES AT BS 940, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002032600218 20020326 00218 NM 2002 3 26 UPS02437662 1 20020125 A 2520 65B11751602 PANEL BOEING 747 747123 1384873 NM CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - R3 DOOR CUTOUT FWD LOWER CORNER REVEAL FOUND CRACKED. CORNER REVEAL REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002032600219 20020326 00219 WP 2002 3 26 AT0200041 1 20020321 A 2611 38025611 APU DOUG DC9 DC932 3022066 WP A ZZDA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 15 837AT 45774 AFTER TAKE OFF BOTH LAVATORY SMOKE DETECTORS ACTIVATED. WITH WHITE SMOKE IN AFT CABIN. CORRECTIVE ACTION: FOUND APU TO BE PRODUCING OIL INTO PACK SYSTEMS FROM INTERNAL LEAK. REMOVED AND REPLACED APU ASSY PER AMM 49-10, FUNCTI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 2002032600220 20020326 00220 NM 2002 3 26 UPS02437664 1 20020124 A 5720 65B01020375 STIFFENER BOEING 747 747123 1384873 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C L/W - L/E CAVITY FRONT SPAR 1 EA VERTICAL STIFFENER FOUND CRACKED AT LOWER END ABOUT 2 INCHES AT WS 38 2 JUST BEHIND NR 13 K/FLAP. STIFFENER IS REPAIRED AS PER HAECO RS R-57-21-34726. 2 L 7 4 4F A20WE 2002032600221 20020326 00221 NM 2002 3 26 UPS02437665 1 20020124 A 5730 PANEL BOEING 747 747123 1384873 NM LT WING BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C L/W - LOWER L/E PNL FOUND BULGED UP AT WS 1270 AFT OF NR 5 V/C FLAP. 2 L 7 4 4F A20WE 2002032600222 20020326 00222 NM 2002 3 26 UPS02437666 1 20020126 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 2350 S-51R STRINGER FOUND CRACKED. M/D BS 2350 S-51R CRACKED STRINGER REPAIRED AS PER SRM 53 -10-03 FIG 1. 2 L 7 4 4F A20WE 2002032600223 20020326 00223 EA 2002 3 26 02083650 1 20020224 A 2916 73011 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 650BR 7418 One half hour into the flight from GSP to ORD, the crew noted a hydraulic high temperature caution. Hydraulic temperatu re reached 200 degrees C. The crew followed the QRH procedures shutting down the L/H engine and returned to GSP where t he aircraft landed without incident. Maintenance personnel removed and replaced the #1 hydraulic system reservoir. Ope rational and leak checks were satisfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002032600224 20020326 00224 NM 2002 3 26 UPS02437667 1 20020125 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 360 S-23L FRAME FOUND CRACKED. SIDEWALL FRAME REPLACED AT BS 360 S-23L PER RS R53-12-3475. 2 L 7 4 4F A20WE 2002032600225 20020326 00225 NM 2002 3 26 UPS02437668 1 20020124 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C CRACK INDICATION REVEALED ON SKIN UNDERNEATH LT LOWER DRAG SPLICE FITTING AT BS 980 STR S-38L. CRACKE D F/X SKIN IN BS 980 S-38L REPAIRED AS PER SRM 53-30-03 FIG 60. 2 L 7 4 4F A20WE 2002032600226 20020326 00226 EA 2002 3 26 02070622 1 20020311 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA BROKEN A VTZA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 27 622 7187 Bird Strike on take-off shattering F/O's window. Open 2 L 7 2 4F RT A21EA 2002032600227 20020326 00227 NM 2002 3 26 UPS02437669 1 20020123 A 5320 WEB BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 1240 RBL 99 BELOW FLOOR WING CTR TANK SURFACE FOUND CORROSION. CORROSION REMOVED PER SRM 57- 30-01 FIG 1 & SHOT-PEENING CARRIED OUT AS PER BAC5884. 2 L 7 4 4F A20WE 2002032600228 20020326 00228 NM 2002 3 26 UPS02437670 1 20020126 A 5210 DOUBLER BOEING 747 747123 1384873 NM L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - L1 DOOR LOWER HINGE CUTOUT DOUBLER FOUND CRACKED. DOOR HINGE CUTOUT REPAIRED AS PER SB 747-52-2 144. 2 L 7 4 4F A20WE 2002032600229 20020326 00229 NM 2002 3 26 UPS02437671 1 20020129 A 5210 HINGE BOEING 747 747123 1384873 NM R1 DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - R1 DOOR HINGE UPPER DOUBLER FOUND NONSTANDARD REPAIR. DOOR UPPER HINGE CUTOUT REPAIRED AS PER S B 52-2144. 2 L 7 4 4F A20WE 2002032600230 20020326 00230 NM 2002 3 26 UPS02437672 1 20020203 A 5320 3398320101 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C CRACK FOUND AT BS 980 S-38R INTERNAL BATHTUB FITTING VERTICAL FLANGE 1 EA BOLT CRACK LENGTH .125 INCH APPROX RUNNING DOWNWARD. BS 980 RH S-38R BATHTUB FITTING REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002032600231 20020326 00231 NM 2002 3 26 UPS02437674 1 20020125 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 215 - 217 RBL 48 SEAT TRACK FLANGE CRACKED. SEAT TRACK REPAIRED SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002032600232 20020326 00232 NM 2002 3 26 2002F00327 1 20020202 A 3350 86210144 BATTERY PACK BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT IDENTIFIER ON SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED REMO TE ASSEMBLY BATTERY PACK AND EXIT IDENTIFIER ASSEMBLY, THEN EXIT IDENTIFIER OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2002032600233 20020326 00233 SO 2002 3 26 COMA0210009 1 20020324 A 7712 311197801 SENSOR EMB 120 EMB120RT 3260202 SO L/H MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 259CA 13689 120252 FLIGHT 5029 T6 WARING DURING T/O.REPLACED THE L/H ENGINE TORQUE. 2 L 7 2 4T RT A31SO 2002032600235 20020326 00235 EA 2002 3 26 COMA0260212 1 20020324 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 988CA 10443 7204 FLIGHT 5369 GEAR DISAGREE WARNING.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002032600236 20020326 00236 EA 2002 3 26 COMA0260213 1 20020325 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 984CA 7171 FLIGHT 5360 FLAPS FAILED AT 20 DEGREES DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002032600238 20020326 00238 NM 2002 3 26 ZW0A0203503 1 20020325 A 3350 20131ASMI BATTERY PACK BOEING 767 7673Q8 1385142 NM DISCHARGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 635TW 28132 EGRESS LIGHTING AT RH SIDE OF FIRST CLASS CABIN INOP. OVERHEAD EMERGENCY LIGHT AT SEAT 20H INOP. REPLACED BATTERY PACK T O EGRESS LIGHTING IN FIRST CLASS CABIN. RELAMPED OVERHEAD EMERGENCY LIGHT NEAR SEAT 20H.(LAMP PART #8074-1) LAST CHECK C 22FEB2001 LAX --CLOSED-- 2 L 7 2 4F RT A1NM 2002032600266 20020326 00266 NM 2002 3 26 AWXA200200246 1 20020317 A 3350 BMS13311122 WIRE BOEING 737 737317 138447P NM BS 960 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - EEL - "C" - DURING C-13 CHECK THE AFT CEILING EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE TROUBLESHOT A ND FOUND A BROKEN WIRE AT STA 960 EMERGENCY POWER BATTERY PACK CONNECTOR, WIRE WAS REPAIRED IAW BOEING SWPM 20-92-00 PG. 1 & 2, FUNCTIONAL TEST OF EMERGENCY EXIT SIGN WAS GOOD IAW T/C A1C33006. 2 L 7 2 4F RT A16WE 2002032600267 20020326 00267 2002 3 26 AWXA200200250 4 20020317 A 2565 60592101 RESERVOIR AIRBUS A319 A319132 3930340 NM ZONE 150 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 819AW 4552 1395 PHX - ESCAPE SLIDE - "C" - DURING P-09 INSPECTION THE R/H OVERWING ESCAPE SLIDE BOTTLE CABLE WAS FOUND BROKEN AT THE HOO K UP POINT. MAINTENANCE REMOVED AND REPLACED THE R/H OVERWING SLIDE BOTTLE ASSEMBLY AND RESERVOIR IAW AMM 25-62-46-800-0 01. 2 L 7 2 4F RT A28NM 2002032600274 20020326 00274 NM 2002 3 26 ASAA0140191 1 20020104 A 5315 65C339501 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 783AS 25114 PAE - DURING SI CHECK, FOUND CORROSION ON FLOORBEAM BS 986 AND RBL 32 AND WL 208. REPAIRED FLOORBEAM IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002032700001 20020327 00001 EU 2002 3 27 02FDEA00216 1 20020208 A 5311 FRAME AIRBUS 300 A300B4622R 3930312 EU CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 721FD 477 CRACK IN UPPER RADIUS RH. ** S/D ** COMING 2 L 7 2 4F RT A35EU 2002032700014 20020327 00014 WP 2002 3 27 ABXA010795 1 20020128 A 5400 THRUST LINK DOUG DC8 DC861 3021952 WP #2 PYLON CHAFED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 #2 PYLON THRUST LINK CHAFED ON BOTTOM SIDE FROM PNEUMATIC DUCT CLAMP (REF. EA 5403277MR) REPAIR OR REPLACEMENT PER CARD 8821016, STEP 02.A) REPAIRED AREA IAW DC-8 SRM 51-1-8, MM 71-00-00, SB 54-92 AND REA D854-40959MR. 2 L 7 4 4F 4A25 2002032700015 20020327 00015 WP 2002 3 27 ABXA010801 1 20020323 A 5400 57530652 FITTING DOUG DC8 DC861 3021952 WP #3 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 #3 PYLON V-BLOCK SUPPORT FITTING HAD A CRACK IN IT. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-3-0, 51-1-23 AND 56-3-0. 2 L 7 4 4F 4A25 2002032700030 20020327 00030 NE 2002 3 27 00013 2 20020326 A 7200 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE RIGHT FLAMED OUT E HAEA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 SW 05 221TW 221 245367 DURING CRUISE RT ENGINE FLAME-OUT AT FLT LVL 390, DESCENT TO FL 190. RELIGHT NORMAL, ALL INDICATIONS NORMAL, NO FURTHER PROBLEMS. 2 L 7 2 4F 4 F A7EU E7EA 2002050200090 20020502 00090 EU 2002 5 2 00014 1 20020326 A 3230 LANDING GEAR AMD FALC20 FALCON 2720302 EU NLG & MLG MALFUNCTIONED E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 204TW 204 GEAR FAILED TO RETRACT AFTER TAKEOFF IN YIP. RETURNED TO YIP FOR MAINTENANCE. MAINTENANCE PERFORMED SEVERAL GEAR SWING S, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A7EU 2002032700032 20020327 00032 WP 2002 3 27 0200679884 1 20020318 A 2780 SLAT DOUG DC9 DC951 3022051 WP WING MALFUNCTIONED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 GL 01 677MC 47756 WHILE ON APPROACH FOR LANDING AT MOT, CREW NOTICED THE SLAT DISAGREEMENT LIGHT ON AND THE AIRCRAFT ROLL TO THE RIGHT. F OLLOWED COM PROCEDURES. DUE TO INSUFFICIENT RUNWAY LENGTH FOR A NO SLAT LANDING AT MOT, THE CREW ELECTED TO DIVERT. CA PTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT AT MIB. MAINTENANCE INSPECTED ALL SLATS AND LUBED BOTH -T- DUCT S. THE AIRCRAFT RETURNED TO MSP FOR A MINIMUM WORKSCOPE MAINTENANCE ACTION. 2 L 7 2 4F RT A6WE 2002032700033 20020327 00033 NM 2002 3 27 0200826745 1 20020315 A 7830 WARNING SYSTEM BOEING 747 747222B 1384904 NM PWA JT9 JT9D7R4G2 52054 NE COCKPIT ACTIVATED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 645NW 2450 2450 23736 715230 DURING TAKEOFF ROLL, THE NR 4 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AT 100 KNOTS. M AINTENANCE INSPECTED THE THRUST REVERSER. OPERATIONAL CHECK SATISFACTORY. 2 L 7 4 4F 4 F RT A20WE E3NE 2002032700034 20020327 00034 NM 2002 3 27 0200836641 1 20020315 A 2530 DRAIN LINE BOEING 747 747212B 1384886 NM NR 3 GALLEY DIRTY A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 641NW 21941 DURING FLIGHT, SMOKE EMITTED FROM BEHIND NR 3 GALLEY COFFEEMAKER. TURNED OFF GALLEY POWER AND PULLED GALLEY CIRCUIT BRE AKERS, SMELL DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. CLEANED COFFEEMAKER DRAIN LINE AND REPLACED THE COFFEEMAKERS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002032800035 20020328 00035 NM 2002 3 28 0200846627 1 20020302 A 2120 ODOR BOEING 747 747251B 1384892 NM COCKPIT DETECTED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 627US 21709 DURING CRUISE, A SMOKE SMELL EMITTED IN THE FLIGHT DECK FOR A BRIEF MOMENT. ALL SYSTEMS CHECKED NORMAL AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. VISUALLY INSPECTED AND OPERATIONALLY CHECKED THE AIRCRAFT WITH N O FAULTS FOUND. 2 L 7 4 4F A20WE 2002032700035 20020327 00035 NM 2002 3 27 0200866624 1 20020319 A 5270 SENSOR BOEING 747 747251B 1384892 NM L1 DOOR MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 624US 21706 DURING CRUISE, A BURNING SMELL EMITTED AROUND DOOR 1L. PULLED ESSENTIAL TRANSFORMER RECTIFIER CIRCUIT BREAKER AND DEACT IVATED THE ESSENTIAL TRANSFORMER RECTIFIER, ESSENTIAL DC BUS, LEFT GALLEY POWER BUS, ENTERTAINMENT SYSTEM, GASPER FAN, A ND RECIRCULATION FAN. AIRCRAFT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED THE 1L CHIME SENSOR. OPERA TIONAL CHECK OK. 2 L 7 4 4F A20WE 2002032700037 20020327 00037 EU 2002 3 27 02FDEA00217 1 20020307 A 5311 FRAME AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 722FD 479 CRACK IN UPPER RADIUS RT FRAME. 2 L 7 2 4F RT A35EU 2002032700038 20020327 00038 WP 2002 3 27 2002F00328 1 20020320 A 2120 ODOR LKHEED 1011 10113853 5265020 WP CABIN DETECTED G AMTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 161AT 293A1219 FLIGHT 5027, DURING CRUISE AT FL 330, SENIOR FLIGHT ATTENDANT REPORTED UNIDENTIFIED FUMES AT REAR LEFT SIDE OF -A- ZONE. NO SMOKE VISIBLE. PASSENGER REPORTED SIMULTANEOUS LOSS OF AUDIO ENTERTAINMENT. THE AIRCRAFT LANDED AT YQX WITHOUT IN CIDENT. THE AIRCRAFT WAS FERRIED TO IND FOR MAINTENANCE. 2 L 7 3 4F A23WE 2002032700045 20020327 00045 NM 2002 3 27 2002UALA00305 1 20020226 A 2150 3964421 CONTROL VALVE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE A/C BAY FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 365UA 10727 24534 UNSCHEDULED LANDING DUE TO CABIN PRESSURIZATION PROBLEMS. DURING ONE-PACK OPERATION, THE RIGHT FLOW CONTROL VALVE (PACK VALVE) FAILED IN THE CLOSED POSITION. REPLACED RIGHT FLOW CONTROL VALVE (PACK VALVE) THEN PRESSURIZED AIRCRAFT, WHICH HELD PRESSURE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050200067 20020502 00067 EU 2002 5 2 2002UALA00368 1 20020320 A 5220 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY EXIT LOOSE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 412UA 465 LOWER ECAM MESSAGE HAD AMBER EXIT DOOR WARNING ON DOOR PAGE FOR RIGHT AFT OVERWING DOOR. PROBLEM WAS CAUSED BY MOVEMENT OF THE OVERWING EXIT HANDLE COVER FLAP. REMOVED OVERWING HATCH AND INSPECTED WITH NO FINDINGS. REINSTALLED DOOR AND S ECURED DOOR HANDLE COVER FLAP. 2 L 7 2 4F 4 F RT A28NM E40NE 2002032700050 20020327 00050 NM 2002 3 27 AWXA2002TESTC 1 20020202 A 5310 D533723392010 FRAME AIRBUS A319 A319132 3930340 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 0 0 271 TEST 2 L 7 2 4F RT A28NM 2002032700055 20020327 00055 NM 2002 3 27 AWXA2002TESTF 1 20020202 A 5310 D533723392010 FRAME AIRBUS A319 A319132 3930340 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 0 0 271 TEST 2 L 7 2 4F RT A28NM 2002032700057 20020327 00057 NM 2002 3 27 AWXA2002TESTJ 1 20020202 A 5310 D533723392010 FRAME AIRBUS A319 A319132 3930340 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 0 0 271 TEST 2 L 7 2 4F RT A28NM 2002032700058 20020327 00058 NM 2002 3 27 CALA0200150 1 20020325 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 727B CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND A 2" CRACK AT HI-LOCK HOLE IN R/H O/B SEAT TRACK, STA 727B. THE CRACKED AREA WAS REMOVED AND A REPAIR S TRAP AND FILLER WERE INSTALLED IAW ECRA 5311-01117. 2 L 7 2 4F RT A16WE 2002032700059 20020327 00059 WP 2002 3 27 ABXA010800 1 20020322 A 5400 5803958501 STRAP DOUG DC8 DC861 3021952 WP #1 PYLON CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 #1 PYLON "T" CAP STRAP HAD CORROSION AT WING STATION 485.00, LOWER SPAR CAP, FORWARD SPAR. REMOVED AND REPLACED THE FORW ARD SPAR STRAP, REMOVED AND REINSTALLED THE #1 PYLON "T" DOUBLER IAW DC-8 SRM 51-1-20D, 51-1-8. 2 L 7 4 4F 4A25 2002032700060 20020327 00060 NM 2002 3 27 AWXA2002TESTI 1 20020202 A 5310 D533723392010 FRAME AIRBUS A319 A319132 3930340 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 0 0 271 TEST 2 L 7 2 4F RT A28NM 2002032700067 20020327 00067 NM 2002 3 27 P2EA2002M018 1 20020324 A 3350 1000679 LIGHT BOEING 737 737230 1384401 NM A P2EA K NONE L NO TEST IN INSP/MAINT 1 CE 05 122NJ 22120 During operational check at scheduled inspection the R/H AFT Emergency Light was found defective. Removed and replaced L ight assembly IAW MM 33-51-81. This is closing action for P2EA2002M018. Reference VAM 037, dated 03/24/02 2 L 7 2 4F RT A16WE 2002032700071 20020327 00071 NM 2002 3 27 2002UALA00466 1 20020316 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 BODY STATION 887 FUSELAGE FRAME IS CRACKED BETWEEN STRINGER 8L AND STRINGER 9L AT UPPER FASTENER FOR VENT BRACKET. MAJ OR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032700072 20020327 00072 2002 3 27 2002F00319 4 20020318 A 8300 310045001 GEAR SHAFT PWA PT6A114A CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE HARTZL HCB3T HCB3TN3 GL EXCESS PLAY E S4WA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 07 95NA 3165 0666 PCEPC0556 BUA19725 DURING A 100 HOUR INSPECTION, LEAK WAS NOTED ON ACCESSORY DRIVE UNIT. FURTHER INSPECTION REVEALED THAT THE FEMALE SPLIN ES IN THE ENGINE WERE WORN TO APPROX 80 PERCENT, SAME AS THE MALE END. SUGGEST AN ON TIME INSPECTION TO DETERMINE AMOUN T OF WEAR SINCE THERE IS NO SET INSPECTION TIME TO CHECK THIS DRIVE. 1 H 7 1 3T 3 T A37CE E4EA 6 C P15EA 2002032700073 20020327 00073 EU 2002 3 27 2002F00320 1 20020301 A 5530 5553012149 STRUCTURE PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL VERTICAL STAB CRACKED E S4WA K NONE O OTHER IN INSP/MAINT 1 WP 07 562NA 2985 174 PCEPR0027 HJ967 DURING 100 HOUR INSPECTION 2 IDENTICAL CRACKS WERE NOTICED ON THE UPPER VERTICAL STABILIZER, DIRECTLY ABOVE THE RUDDER A ND MIGRATING FORWARD APPROXIMATELY 4.5 INCHES. AFTER CONTACTING MANUFACTURER, IT WAS SUGGESTED THAT THE BOTTOM FAIRING OF THE VERTICAL STAB WAS NOT MANUFACTURED WIDE ENOUGH AND THE SKINS HAD TO BE SQUEEZED FOR THE PROPER INSTALLATION OF TH E FAIRING. A REPAIR WAS APPROVED AND PERFORMED TO STRENGTHEN THE SKINS IN THAT AREA. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002032700074 20020327 00074 NM 2002 3 27 2002UALA00468 1 20020315 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 394UA 24669 JUST BELOW GROUND SERVICE ELECTRICAL PANEL, SKIN IS PUNCTURED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR, SHIM AND DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032700075 20020327 00075 NM 2002 3 27 2002UALA00469 1 20020318 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 FUSELAGE FRAME STATION 951 STRINGER 6R HOLE B IS ELONGATED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032700077 20020327 00077 SO 2002 3 27 C2XA02CL084 1 20020326 A 2430 30086011 GENERATOR EMB 135 EMB135ER 3260203 SO LEFT/RIGHT ENGIN CONTAMINATED A C2XA A B UNSCHED LANDING EMER. DESCENT J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 27 27512 145274 CLE FLIGHT# 3194 THE CREW REPORTED ALL 4 GENERATORS FELL OFF LINE AFTER GEAR RETRACTION.THE #4 GENERATOR DID COME BACK O NLINE. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND ALL FOUR G ENERATORS TO BE CONTAMINATED WITH GLYCOL AND SAND.ALL FOUR GENERATORS WERE REPLACED AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002032700078 20020327 00078 NM 2002 3 27 2002UALA00470 1 20020317 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 CABIN, BODY STATION 867 FRAME, BETWEEN STRINGER 8R AND 9R FRAME IS CRACKED AT FASTENER HOLE FOR VENT BRACKET. MAJOR REP AIR ACCOMPLISHED. INSTALLED REPAIR ANGLE (CHANNEL) NESTED ON INBOARD FRAME FLANGE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032700079 20020327 00079 NM 2002 3 27 2002UALA00471 1 20020317 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 STATION 178 BULKHEAD AFT SIDE WEB CRACKED RBL 5 WL 200. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032700080 20020327 00080 NM 2002 3 27 2002UALA00472 1 20020318 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 STATION 178 BULKHEAD WEB AFT SIDE CRACKED AT BL 0 WL 188. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032700081 20020327 00081 2002 3 27 SWAA020622 4 20020324 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 759GS 30544 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002032700082 20020327 00082 2002 3 27 SWAA020623 4 20020325 A 2565 6557463 BRACKET BOEING 737 7373G7 1384595 NM AFT SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE FWD FLOOR ATTACH BRACKET CRACKED. REMOVED AND REPL ACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2002032700083 20020327 00083 NM 2002 3 27 SWAA020626 1 20020325 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 740SW 29276 EEPLS COVER MISSING AT ROW NR 8. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002032700084 20020327 00084 2002 3 27 SWAA020627 4 20020325 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 622SW 27932 FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002032700085 20020327 00085 NM 2002 3 27 SWAA020629 1 20020324 A 5312 6516300 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND LBL 12. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002032700086 20020327 00086 NM 2002 3 27 SWAA020630 1 20020325 A 5312 6517582 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, WL 227 AND RBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002032700087 20020327 00087 NM 2002 3 27 SWAA020631 1 20020323 A 5312 6517582 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEBS CRACKED (2 EA) AT BS 180, RBL 17.1, WL 214 AND WL 224. REMOVED AND REPLACED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2002032700088 20020327 00088 NM 2002 3 27 SWAA020632 1 20020325 A 5312 6516300 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 218, LBL 11.5 AND WL 212.5, RBL 7.0. REPAI RED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002032700089 20020327 00089 NM 2002 3 27 SWAA020633 1 20020325 A 5313 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 967, BETWEEN STR'S 6L AND 7L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002032700090 20020327 00090 NM 2002 3 27 ZW0A0203601 1 20020326 A 3350 767 LAMP BOEING 757 7572Q8 1384972 NM BURNED OUT A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 710TW 28169 RIGHT FWD AND LEFT FWD EMERGENCY DOOR SLIDE LIGHTS INOP. RELAMPED RIGHT FWD AND LEFT FWD EMERGENCY SLIDE LIGHTS. LAST CH ECK C PERFORMED 14NOV2001 MCI --CLOSED-- 2 L 7 2 4F RT A2NM 2002032700091 20020327 00091 NM 2002 3 27 2002UALA00473 1 20020317 A 5315 FLOORBEAM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 770UA 26925 FOUND 2 EA APPROX 3.0 INCH CRACKS BOTH SIDES OF UPPER FLANGE ON FWD CARGO FLOORBEAM AT STA 676 UNDER THE RIGHT SIDE AUXI LIARY GUIDE. CRACK EXTENDS INTO UPPER FLANGE FILLET. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002032700092 20020327 00092 NM 2002 3 27 2002UALA00475 1 20020317 A 5320 GUIDE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 770UA 26925 AT STA 718 FLOORBEAM RT SIDE ROLLER TRACK GUIDE FOUND AFT OUTBOARD INTERCOSTAL ATTACH BRACKET TO FLOORBEAM CRACKED THROU GH AT PREVIOUS REPAIR. ALSO FOUND ROLLER GUIDE OUTBOARD ATTACH POINT ON PREVIOUS REPAIR NOT DRILLED THROUGH AND NO FAST ENER PRESENT. MAJOR REPAIR ACCOMPLISHED. DRILLED ROLLER GUIDE OUTBOARD ATTACH POINT AND INSTALLED FASTENER. NOTE: AT TACH BRACKET TO FLOORBEAM WAS NOT CRACKED THROUGH REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002032700100 20020327 00100 EA 2002 3 27 COMA0260214 1 20020325 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 967CA 13691 7134 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 640AB.REPAIRED I/A/W 601R57-21-030. 2 L 7 2 4F RT A21EA 2002032700101 20020327 00101 EA 2002 3 27 COMA0260215 1 20020325 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 967CA 13691 7134 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 540EB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002032700102 20020327 00102 EA 2002 3 27 COMA0260216 1 20020325 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 967CA 13691 7134 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 640FB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002032700103 20020327 00103 EA 2002 3 27 COMA0260217 1 20020325 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 967CA 13691 7134 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 640GB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002032700104 20020327 00104 EA 2002 3 27 COMA0260218 1 20020325 A 5730 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 967CA 13691 7134 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 540BB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002040500030 20020405 00030 NM 2002 4 5 2002UALA00478 1 20020314 A 3397 80181 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 EMERGENCY LIGHTS 2 EA AT SEAT 1E ARE INOP. WIRE HARNESS FAILED. REPLACED FAILED HARNESS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002040500031 20020405 00031 NE 2002 4 5 2002UALA00479 2 20020315 A 7532 8148902 ACTUATOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT ENGINE FAILED A UALA K NONE R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 WP 29 668UA 30024 724465 AT FL260 AFTER THROTTLES RETARDED TO IDLE FOR DESCENT EXPERIENCED AUDIBLE COMPRESSOR STALL WITH PULSING VIBRATION. LEFT ENGINE EEC C1 STATUS MESSAGE. SURGE WAS DETERMINED TO BE <1.25 EPR AND CAUSED BY A FAILED 2.5 BLEED ACTUATOR. ACCOMPL ISHED FORWARD THRUST SURGE INSPECTIONS, REPLACED THE 2.5 BLEED ACTUATOR AND PERFORMED OPERATIONAL CHECKS CONFIRMING REPA IR. 2 L 7 2 4F 4 F RT A1NM E24NE 2002032700105 20020327 00105 NM 2002 3 27 2002UALA00480 1 20020115 A 5730 PANEL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 773UA 26929 MISSING MATERIAL, 1 SQUARE INCH PER 12 SQUARE INCHES. LEFT WING L/E PANELS: 511AB, CB, EB, FB, GB, KB, MB. RIGHT WING L/E PANELS: 611CB, EB, FB, GB, MB. RIGHT STRUT AND ENG COWLS: 441BR. OTHER: 611LB, 511LB, 613AT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002032700106 20020327 00106 NM 2002 3 27 AWXA200200240 1 20020321 A 5210 60B1002617 CABLE BOEING 757 7572S7 1384962 NM L4 DOOR OUT OF ADJUST A AWXA K NONE O OTHER TX TAXI/GRND HDL 1 WP 28 906AW 23568 PHX - EMERGENCY ESCAPE SYS - POST FLT L4 DOOR DID NOT DEACTIVATE FROM EMERGENCY OPERATION WHEN CATERING OPENED THE DOOR FROM THE OUTSIDE. THE DOOR ASSIST RESERVOIR DISCHARGED PRIOR TO THE DOOR ROTATING OUT AND BOTH THE LOWER LINER PANEL AN D SLIDE COVER CAUGHT ON THE GATE AND WERE DAMAGED. SLIDE DID NOT DEPLOY. MX INSTALLED THE DOOR ASSIST RESERVOIR SAFETY PIN AND TROUBLESHOT L4 DOOR FINDING DOOR DISARM CABLE WAS OUT OF ADJUSTMENT. 2 L 7 2 4F RT A2NM 2002032700107 20020327 00107 EU 2002 3 27 CHQ000138 1 20020325 A 3320 SOCKET SAAB SF340 SF340A 7850100 EU CABIN SHORTED A CHQA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 95 095 PASSENGER WINDOW LIGHT ABOVE SEAT 8F ON RIGHT SIDE OF CABIN STARTED SMOKING AND SPARKING WHEN LIGHTS WERE TURNED ON. AF TER LANDING WINDOW LIGHT SWITCH WAS IMMEDIATELY TURNED OFF ALONG WITH ALL ELECTRICAL EQUIPMENT AND SMOKE STOPPED. FOUND WINDOW LIGHT ABOVE SEAT 8F SOCKET SHORTED OUT. 2 L 7 2 4T RT A52EU 2002040800044 20020408 00044 NM 2002 4 8 DHL2002741003 1 20020322 A 2612 1014A POWER UNIT BOEING 727 7272Q9 138448M NM FIRE DETECTOR DEFECTIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 741DH 2464 21931 ON SERVICE CHECK FOUND APU FIRE DETECTION WOULD NOT TEST. PLACED APU FIRE DETECTION ON DMI, CONTROL NR 8834, CAT C, PE R DHL MEL 26-11. C/W SP 26-11. 8834-APU FIRE DETECTION WILL NOT TEST. REMOVED AND REPLACED OPERATING POWER UNIT. PERFO RMED TEST IAW 26-15-00B727MM. OKAY . THIS CLEARS DMI 8834. 2 L 7 3 4F RT A3WE 2002032700108 20020327 00108 NM 2002 3 27 F3LA200200117 1 20020325 A 2550 PANEL BOEING 737 73736E 138443A NM CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 314FL 3489 25256 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TRANSITION PANEL AT STA 847 TO 867, LBL 24. FABRICATED AND INSTALLED REPLACEMENT TRANSITION PANEL PER SRM 53-60-53 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002032700109 20020327 00109 WP 2002 3 27 MWEA020173 1 20020319 A 3610 321417611 REGULATOR DOUG DC9 DC982 3022082 WP A/C BAY DEFECTIVE A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 808ME 48070 RIGHT AIRFOIL ICE PROTECTION TEMP HIGH LIGHT CAME ON DURING TAIL PORTION OF ICE PROTECTION CYCLE. FOLLOWED QRH AND GOT RIGHT AIR TEMPERATURE HIGH LIGHT. REMOVED AND REPLACED PNEUMATIC PILOT PRESSURE REGULATOR. REF MM 36-10-02 PER T/S CHE CKED DUCT TEMPS, FOUND TO BE HIGH. DUCT TEMPS WITHIN LIMITS AFTER PRESSURE REGULATOR CHANGE. 2 L 7 2 4F A6WE 2002032700111 20020327 00111 WP 2002 3 27 MWEA020176 1 20020319 A 5320 5956034509 SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 STATION 897 BETWEEN LONGERONS 27 LEFT AND 28 LEFT SUPPORT HAS CORROSION BY A FASTENER. WHILE REMOVING CORROSION, FOUND SUPPORT CRACK. REMOVED AND REPLACED SUPPORT. 2 L 7 2 4F A6WE 2002032700113 20020327 00113 WP 2002 3 27 MWEA020177 1 20020319 A 5311 995823817 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FORMER AT STATION 980 HAS AREA OF LIGHT CORROSION BETWEEN LONGERON 25 THROUGH LONGERON 26 LEFT. FABRICATED AND INSTALLE D FORMER AND SPLICES. 2 L 7 2 4F A6WE 2002032700114 20020327 00114 WP 2002 3 27 MWEA020178 1 20020319 A 5320 49127721 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 CUSP SPLICE FITTING AT STATION 229 LEFT SIDE HAS CORROSION. REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 2002032700115 20020327 00115 WP 2002 3 27 MWEA020179 1 20020319 A 5311 9912243105 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 STATION 965 FRAME HAS LIGHT CORROSION FROM LONGERON 25 LEFT TO 27 RIGHT AFT SIDE. REMOVED AND REPLACED SPLICE. 2 L 7 2 4F A6WE 2002032700117 20020327 00117 WP 2002 3 27 MWEA020180 1 20020319 A 5311 995821519 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 STATION 917 FRAME FORWARD SIDE HAS CORROSION FROM LONGERON 28 LEFT TO 29 RIGHT UNDER THE FLOOR SUPPORT. FABRICATED AND INSTALLED FRAME SECTION, REPAIR DOUBLERS, AND SUPPORT FITTING. 2 L 7 2 4F A6WE 2002032700127 20020327 00127 WP 2002 3 27 MWEA020181 1 20020319 A 5311 59114481 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 STATION 832 FRAME AFT SIDE HAS CORROSION BETWEEN LONGERONS 29 RIGHT TO 28 RIGHT. FABRICATED AND INSTALLED FRAME REPAIR SECTIONS. 2 L 7 2 4F A6WE 2002032700129 20020327 00129 WP 2002 3 27 MWEA020184 1 20020319 A 5311 995823837 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 STATION 980 FRAME UPPER -J- CHANNEL HAS AREAS OF LIGHT CORROSION BETWEEN LONGERON 29 LEFT THROUGH LONGERON 28 RIGHT. FA BRICATED AND INSTALLED REPAIR ANGLES, SPLICES AND FRAME SECTION. 2 L 7 2 4F A6WE 2002032700130 20020327 00130 WP 2002 3 27 MWEA020185 1 20020319 A 5313 3924809503 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FORWARD PIT, CORROSION ON LONGERON AT STATION 570 LONGERON 30. REMOVED AND REPLACED LONGERON. FABRICATED AND INSTALLED RADIUS STRAP. 2 L 7 2 4F A6WE 2002032700132 20020327 00132 NM 2002 3 27 PCAA0203038 1 20020321 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 DURING ROUTINE MAINTENANCE VISIT EMERGENCY LIGHTS WERE NOT ILLUMINATING PROPERLY. FORWARD CONNECTOR RESECURED ON RIGHT SIDE OF EMERGENCY LIGHT (FLOOR) STRIP. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002032700133 20020327 00133 EU 2002 3 27 QXEA0200504 1 20020319 A 3350 551800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 BOI- BOTH EXIT SIGNS AT MID CABIN POSITION HAVE BURNED OUT BULBS. REPLACED BOTH EXIT SIGNS. OPERATIONAL CHECK GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002032700149 20020327 00149 NM 2002 3 27 QXEA0200505 1 20020320 A 5270 WARNING SYSTEM BOMBDR DHC8 DHC8401 NM COCKPIT MALFUNCTIONED A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 400QX 4030 SEA - CREW ABORTED TAKEOFF WHEN THE FUSELAGE DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE INSPECTED ALL DOOR SWITCHES FO R CONDITION. NO DISCREPANCIES NOTED. THERE WERE NO CURRENT FAULTS STORED IN THE PSEU. AIRCRAFT WAS PRESSURIZED AND NO FAULTS WERE FOUND. LUBED THE DOOR HANDLE AND CYCLED. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002032700152 20020327 00152 SO 2002 3 27 CTU2002F00003 1 20020222 A 3110 587837 MASTER SWITCH PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360EB 17025 SO LT SIDE PANEL BROKEN B CTUR K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 21 3054K 347970102 307788 THE MASTER SWITCH IS DIVIDED INTO TWO SWITCHES THAT ARE COUPLED TOGETHER WITH A PLASTIC TAB. THE HALF OF THE SWITCH THA T CONTROLS THE ALTERNATOR FIELDS IS HIDDEN UNDER THE SIDE PANEL. WHEN THE TAB THAT COUPLES THE TWO TOGETHER BROKE, THE ALTERNATORS DROPPED OFF LINE. CAUSE OF THE MALFUNCTION IS MOST LIKELY, AGE. 1 L 7 2 3O 3 O A7SO E9CE 2002032700153 20020327 00153 CE 2002 3 27 CTU2002F00004 1 20020315 A 5610 10138402522 WINDSHIELD BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE COCKPIT CRACKED B CTUR K NONE O OTHER IN INSP/MAINT 1 GL 21 74RF BB1408 COPILOT WINDSCREEN INNER PANE FAILED AT 27,000 FEET IN LEVEL FLIGHT OUTSIDE AIR TEMPERATURE AT 32 DEGREES. WINDSHIELD ( PN 10138402522) (SN 97112H4959) WINDSHIELD INSTALL KIT (PN 101-50413) (SN 21851). 1 L 7 2 4T 4 T A24CE E4EA 2002032700155 20020327 00155 EU 2002 3 27 EGR2002F00002 1 20020303 A 6210 BLADE BOLKMS 117 BK117A3 5626015 EU MAIN ROTOR DAMAGED E EGRA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 17 526MB 7102 DURING MAIN ROTOR COAST DOWN, AFTER ENGINE SHUT DOWN ON THE HOSPITAL ROOF HELIPAD AT APPROX 40 PER CENT NR ONE MAIN ROT OR BLADE CONTACTED AND DAMAGED BOTH VERTICAL STABILIZER. THIS IS A DESIGN FLAW. IN HIGH AND GUSTY WINDS WITH LOW ROTOR SPEEDS, DURING START OR SHUT DOWN, THERE IS NOT ENOUGH CENTRIPETAL FORCE TO KEPT THE BLADES FROM FLAPPING EXCESSIVELY. THIS RESULTS IN THE MAIN ROTOR BLADES STRIKING ONE OR BOTH VERTICAL STABILIZERS. THE AIRCRAFT MANUFACTURERS FIX WAS TO INSTALL KNOCKOUT PLUGS IN THE LEADING EDGE OF THE VERTICAL STABILIZERS TO LESSEN THE SEVERITY AND COST OF THE REPAIR. ONE MAIN ROTOR BLADE REPLACED DUE TO TRAILING EDGE SEPARATION. BOTH VERTICAL STABILIZERS REMOVED FOR REPAIR. 1 G 7 2 3U H13EU 2002032700156 20020327 00156 GL 2002 3 27 EOO2002F00000 2 20020219 A 7230 CARBON SEAL HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL COMPRESSOR LEAKING B EOOR K NONE K FLUID LOSS IN INSP/MAINT 1 AL 03 C6PHC 1345 180257D DURING ANNUAL IT WAS NOTICED THAT THE NR1 CARBON SEAL WAS LEAKING. REMOVED AND SENT IN FOR REPAIR. 1 G 7 1 3U 3 U H3WE E4CE 2002032700157 20020327 00157 WP 2002 3 27 EOO2002F00001 1 20020219 A 7500 6856988 SEAT HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ANTI ICE VALVE MISSING B EOOR K NONE O OTHER IN INSP/MAINT 1 AL 03 CGPHC 180257D CAE833793 ON ANNUAL, FOUND THE ANTI-ICE POPPET SEAT MISSING. THE RETAINING SCREW HAD BACKED OUT. THERE WAS NO EVIDENCE THAT THE SCREW WAS STAKED AS IS REQUIRED. 1 G 7 1 3U 3 U H3WE E4CE 2002032700158 20020327 00158 GL 2002 3 27 EOO2002F00002 2 20020219 A 7250 A23038218 NOZZLE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL NR1 TURBINE CRACKED B EOOR K NONE O OTHER IN INSP/MAINT 1 AL 03 C6PHC 1462 180257D CAE838793 DURING ANNUAL INSPECTED THE NR 1 NOZZLE WAS FOUND TO BE BURNED AND CRACKED IN A (T) SHAPE AT THE 12:00 (APPROX) POSITION . THE ODD THING HERE IS ON THE ENGINE AS INSTALLED IN THE HELICOPTER THE NORMAL STARTING POINT FOR THIS KIND OF DAMAGE IS APPROX AT THE 3:00 POSITION. THIS IS A PMA NOZZLE. UNIT REMOVED AND SENT FOR REPAIR. 1 G 7 1 3U 3 U H3WE E4CE 2002032700159 20020327 00159 SO 2002 3 27 EVC2002F00000 2 20020311 A 8520 629340 CONNECTING ROD CESSNA 182 182H 2072718 CE CONT O470 O470* 17026 SO ENGINE BROKEN E EVCA K NONE O OTHER IN INSP/MAINT 1 CE 03 64AE 4213 18255970 1339977R NR 1 CONNECTING ROD BOTS BROKEN. 1 H 7 1 3O 3 O NT 3A13 E273 2002032700160 20020327 00160 CE 2002 3 27 EWO2002F00000 1 20020305 A 2750 55651945 SPROCKET CESSNA CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE FLAP DRIVE BROKEN B EW0R K NONE O OTHER IN INSP/MAINT 1 GL 25 92B 1801 5500471 LPCE71346 DURING PHASE 1 INSPECTION, FLAP MOTOR OPERATIONAL TEST, THE LEFT MOTOR WOULD NOT DRIVE FLAPS. THE FLAP DRIVE WAS INSPEC TED AND LEFT SPROCKET WAS FOUND BROKEN IN TWO. THIS CAUSED MOTOR TO BE INEFFECTIVE. NO BINDING OF FLAPS WAS FOUND. TH E SPROCKET WAS REPLACED WITH A NEW UNIT AND OPERATIONAL TEST WERE SATISFACTORY. 1 L 7 2 4F 4 F A22CE E1NE 2002032700161 20020327 00161 CE 2002 3 27 FPI2002F00002 1 20020104 A 8011 64208310 STARTER BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO ENGINE FAILED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 9098Q 278 TH109 299426R THE STARTER DRIVE FAILED TO ENGAGE OR EVEN ATTEMT TO TURN ENGINE AFTER BRINGING INTO HANGER AND WARMING UP IT STILL DID NOT ENGAGE. INSPECTED ENGINE OIL FILTER, NO CONTAMINATES FOUND. CHANGED STARTER DRIVE. OPS CHECK GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2002032700162 20020327 00162 CE 2002 3 27 FPI2002F00003 1 20020305 A 3233 98820152 ACTUATOR CESSNA 210 T210N 2073456 CE CONT O520 TSIO520* 17040 SO MLG BROKEN E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 4672Y 21063977 ACTUATOR PISTON SERVES AS A RACK WITH GEAR TEETH CUT INTO THE BOTTOM PART OF THE PISTON. THE RACK DRIVES A PINION GEAR ATTACHED TO THE GEAR LEG. THE RACK PISTON IS HELD IN ENGAGEMENT WITH THE PINION BY A HARDENED STEEL ROLLER ON TOP OF TH E RACK. THE ROLLER IS SUPPORTED BY TWO NEEDLE BEARINGS. AN ANNUAL INSPECTION IT WAS FOUND THAT THE ROLLER AND ITS BEAR INGS WERE ON THE FLOOR OF THE ACTUATOR COMPARTMENT. EVIDENTLY A HARD LANDING HAD BROKEN THE ACTUATOR HOUSING AT BOTH SI DES WITH NO ROLLER TO SUPPORT IT, THE RACK WAS BARELY ENGAGING THE PINION. RECOMMEND CLOSE INSPECTION OF ACTUATOR HOUS ING AT ROLLER BEARING AREA. 1 H 7 1 3O 3 O 3A21 E8CE 2002032700163 20020327 00163 CE 2002 3 27 HYI2002F00002 1 20020128 A 3700 IH59 MANIFOLD CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO VACUUM SYSTEM FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 780EA 1205 402C0257 CREW REPORTED THAT ON START, LEFT ENGINE DRIVEN VACUUM PUMP CAUSED BOTH VACUUM SOURCE FAILURE INDICATORS TO ENGAGE. MAI NTENANCE REMOVED AND REPLACED VACUUM MANIFOLD AND RELEASED THE AIRCRAFT BACK TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2002032700164 20020327 00164 CE 2002 3 27 HYI2002F00003 1 20020311 A 3110 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO LT SWITCH PANEL FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 812AN 402C0229 ON PREFLIGHT INSPECTION, AVIONICS MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2002032700165 20020327 00165 CE 2002 3 27 HYI2002F00004 1 20020219 A 3110 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO LT SWTCH PANEL FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 770CA 1157 402C0432 ON PREFLIGHT INSPECTION, AVIONICS SWITCH FAILED. MAINTENANCE REPLACED THE SWITCH AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2002032700166 20020327 00166 CE 2002 3 27 HYI2002F00005 1 20020311 A 3110 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO LT SWITCH PANEL FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 2748Y 1047 402C0248 AVIONIC MASTER SWITCH FAILED IN FLIGHT, CREW USED ALTERNATE MASTER (BACKUP). MAINTENANCE PLACE THE SWITCH AND RETURNED T HE SWITCH AND RETURNED THE AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2002032700170 20020327 00170 EU 2002 3 27 RAIA00203105 1 20020321 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 574HK 41093 MX-STL- FLOOR PATH LIGHTING INOP ROW 1 TO 3. RECONNECTED PATH LIGHTING STRIP. 2 L 7 2 4T RT A41NM 2002032700172 20020327 00172 2002 3 27 SABA020038 4 20020320 A 3425 7003360941 COMPUTER DHAV DHC8 DHC8102 2809003 NM NR 1 FAULTY A SABA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 33 881CC 294 AIRCRAFT 881 ON FLIGHT 5027 FROM CLT TO CVG. DURING CRUISE FLIGHT AFTER DEPARTURE FROM CLT THE NR 1 AHARS BECAME INOPER ATIVE. NO EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO CLT AND LANDED WITH NO OTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE NR 1 AHARS UNIT. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042200086 20020422 00086 EA 2002 4 22 QXEA0200506 1 20020320 A 4950 32912104 CONTROL VALVE CNDAIR CL600 CL6002C10 1390015 EA APU MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 601QX 10009 TUS - AIRCRAFT RETURNED TO FIELD WHEN CREW COULD NOT PRESSURIZE AIRCRAFT. MAINTENANCE FOUND THE LOAD CONTROL VALVE OF T HE APU WOULD NOT CLOSE. MAINTENANCE RECONNECTED APU LOAD CONTROL VALVE. STARTED APU AND PACKS WITH NO DISCREPANCIES NO TED ON LOAD CONTROL VALVE. ALSO PERFORMED GROUND RUN ON ENGINES WITH NO DISCREPANCIES NOTED. APU LOAD CONTROL VALVE CL OSED WITH APU SHUTDOWN. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002032700173 20020327 00173 EU 2002 3 27 QXEA0200507 1 20020322 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN DEFECTIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 BOI- DIM EXIT LIGHT MID CABIN FACING FORWARD. REPLACED EXIT SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4F RT A20EU 2002032700175 20020327 00175 EU 2002 3 27 RAIA00203101 1 20020317 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 550HK 41039 MX-STL- EMERGENCY PATH LIGHTS INOP. RESECURED PATH LIGHT CONNECTOR, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002032700176 20020327 00176 EU 2002 3 27 RAIA00203102 1 20020318 A 3397 WIRE JETAIR JETSTM JETSTM4101 1500501 EU CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 551HK 41040 MX-STL- EMERGENCY ESCAPE PATH LIGHTS INOP. REPAIRED BROKEN WIRE ON PATH LIGHTS, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002032700177 20020327 00177 EU 2002 3 27 RAIA00203103 1 20020318 A 3397 WIRE JETAIR JETSTM JETSTM4101 1500501 EU CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 565HK 41082 MX-STL- EMERGENCY PATH LIGHTS OUT AT ROWS 1-3. REPAIRED BROKEN WIRE AT PATH LIGHTS, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002032700178 20020327 00178 EU 2002 3 27 RAIA00203104 1 20020320 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 574HK 41093 MX-STL- EMERGENCY LIGHT OUT ROW 2. REMOVED AND REPLACED LAMP, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002032700181 20020327 00181 NM 2002 3 27 SWAA020468 1 20020303 A 2560 6949956 CABLE BOEING 737 7373H4 1384600 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE NOT SECURED. SECURED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002032700182 20020327 00182 NM 2002 3 27 ASAA0210047 1 20020131 A 3350 86210144 BATTERY PACK BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS ON SEAT PALLET 1-3 WOULD NOT EXTINGUISH. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY PACK, THEN LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2002032700183 20020327 00183 NM 2002 3 27 ASAA0210048 1 20020202 A 3350 8731002142 BATTERY PACK BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT IDENTIFIER ON SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED REMO TE ASSEMBLY BATTERY PACK AND EXIT IDENTIFIER ASSEMBLY, THEN EXIT IDENTIFIER OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2002032700184 20020327 00184 WP 2002 3 27 ASAA02280055 1 20020223 A 2560 3961896501 LANYARD DOUG DC9 DC983 3022083 WP SERVICE DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 SEA - FORWARD GALLEY DOOR LANYARD BETWEEN GIRT BAR AND SLIDE COVER BECAME DISCONNECTED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2002032700185 20020327 00185 NM 2002 3 27 ASAA0240021 1 20020219 A 3350 8100022605 LIGHT BOEING 737 737490 1384715 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 793AS 28888 PDX - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS INOPERATIVE AT ROW 10-12. REMOVED AND REPLACED LIGHT ASSEMBLY OPERATI ONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002032700186 20020327 00186 NM 2002 3 27 ASAA027002 1 20020216 A 3350 D71702001 POWER SUPPLY BOEING 737 737790 13844CN NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 622AS 30165 ANC - DURING PREFLIGHT CHECK, FOUND THE EMERGENCY TRACK LIGHTS INOPERATIVE AFT OF FIRST CLASS SEATS. REPLACED EMERGENCY POWER SUPPLY AT RIGHT OVERWING EXIT. SYSTEM THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2002032700187 20020327 00187 WP 2002 3 27 ASAA0280014 1 20020201 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 18802 5889 53449 SEA - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT. OP TESTED OK. (M) 2 L 7 2 4F RT A6WE 2002032700188 20020327 00188 WP 2002 3 27 ASAA0280015 1 20020203 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTS AT ROWS 13-21 WERE FOUND TO BE ILLUMINATED EVEN THOUGH POWER WAS T URNED OFF. LIGHTS WERE NOTICEABLY DIMMER THAN NORMAL. REPLACED ASSOCIATED POWER SUPPLIES (BATTERY PACK ASSEMBLIES), LI GHT BULBS (ADVANCED MICRO P/N 7732), AND FIVE CONNECTOR WIRING ASSEMBLIES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002032700189 20020327 00189 WP 2002 3 27 ASAA0280016 1 20020204 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 SEA - DURING LINE CHECK, MID-CABIN EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPAIRED BROKEN MODULE CO NNECTOR WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002032700190 20020327 00190 WP 2002 3 27 ASAA0280017 1 20020205 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 56929 7409 53018 SEA - DURING LINE CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT. OP TESTED OK. (M) 2 L 7 2 4F RT A6WE 2002032700191 20020327 00191 WP 2002 3 27 ASAA0280018 1 20020204 A 4930 FUEL LINE DOUG DC9 DC983 3022083 WP APU LEAKING A ASAA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 01 949AS 53022 FAI - INTERMITTENT FUEL ODOR IN COCKPIT AND CABIN NOTED DURING FLIGHT. RESECURED LOOSE FUEL LINE CONNECTION TO APU BURN ER. ALSO, TIGHTENED BURNER CAN CLAMP. RAN APU. NO FUEL ODOR WAS NOTED. (M) 2 L 7 2 4F RT A6WE 2002032700192 20020327 00192 WP 2002 3 27 ASAA0280020 1 20020207 A 5347 SR095301157003 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, FOUND CORROSION ON SEAT TRACK AT FUSELAGE STATIONS, 1118, 1152, AND 1160, AT BUTTOCK STATION X P LUS 54, AND WATERLINE 2-2. REPAIRED SEAT TRACK PER SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2002032700193 20020327 00193 WP 2002 3 27 ASAA0280021 1 20020207 A 5313 59327311 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 934AS 49235 OAK - DURING C-CHECK, FOUND CORROSION ON LONGERON 30 FROM FS 560 TO 579 IN MID CARGO COMPARTMENT. REMOVED CORROSION AND INSTALLED SPLICE ON LONGERON PER EA 5310-02056. (M) 2 L 7 2 4F A6WE 2002032700194 20020327 00194 WP 2002 3 27 ASAA0280022 1 20020207 A 5320 9930538U9 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, FOUND CORROSION ON FLOOR WEB BETWEEN FS 608 AND 693. EXTEND WAS DETERMINED TO BE BEYOND LIMITS. REPLACED CORRODED WEB PER SRM'S 51-10-04 AND 51-30-02. (M) 2 L 7 2 4F RT A6WE 2002032700195 20020327 00195 WP 2002 3 27 ASAA0280023 1 20020208 A 5313 5936051501 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 934AS 49235 OAK - DURING C-CHECK, FOUND CORROSION ON LONGERON 28L FROM FS 598-617 IN MID CARGO COMPARTMENT. REMOVED CORROSION AND I NSTALLED U-CHANNEL DOUBLER FROM FS 598-617 PER EA 5310-02060. (M) 2 L 7 2 4F A6WE 2002032700196 20020327 00196 WP 2002 3 27 ASAA0280024 1 20020208 A 2910 CONNECTOR DOUG DC9 DC983 3022083 WP HYD SYSTEM LOOSE A ASAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 01 949AS 53022 SEA - DURING FLIGHT, LEFT HYDRAULIC SYSTEM 'PRESS LOW' LIGHT ILLUMINATED AND PRESSURE FLUCTUATED BETWEEN 0 AND 100 PSI. LEFT SYSTEM AND THE POWER TRANSFER UNIT (PTU) WERE TURNED OFF. TIGHTENED LEAKING HYDRAULIC LINE CONNECTION TO THRUST R EVERSER CONTROL VALVE, AND REPLACED PTU DAMAGED BY OPERATION WITH LOW FLUID QUANTITY. SYSTEM CHECKED OK. (M) 2 L 7 2 4F RT A6WE 2002032700197 20020327 00197 WP 2002 3 27 ASAA0280026 1 20020208 A 5347 SR095301157001 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, FOUND CORROSION ON SEAT TRACK AT FUSELAGE STATION 1212-1296, BUTTOCK LINE PLUS 22. REPLACED SEA T TRACK PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2002032700198 20020327 00198 WP 2002 3 27 ASAA0280029 1 20020220 A 2560 3961896501 LANYARD DOUG DC9 DC983 3022083 WP SERVICE DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 LAX - LANYARD BETWEEN GIRT BAR AND SLIDE COVER BECAME DISCONNECTED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2002032700199 20020327 00199 WP 2002 3 27 ASAA0280031 1 20020212 A 5313 5936051501 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 934AS 49235 OAK - DURING C-CHECK, FOUND CORROSION ON LONGERON 28L FROM FS 617-636 IN MID CARGO COMPARTMENT. REMOVED CORROSION AND I NSTALLED U-CHANNEL DOUBLER FROM FS 617-636 PER EA 5310-02060. (M) 2 L 7 2 4F A6WE 2002032700200 20020327 00200 WP 2002 3 27 ASAA0280032 1 20020213 A 5310 5936038501 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 934AS 49235 OAK - DURING C-CHECK, FOUND CORROSION ON MID CARGO DOOR BEAM BETWEEN HORIZONTAL LEG OF REPAIR DOUBLER AT FORWARD AND AFT DOOR STOPS. INSTALLED REPAIR TAB ON BEAM PER EA 5310-02055. (M) 2 L 7 2 4F A6WE 2002032700201 20020327 00201 WP 2002 3 27 ASAA0280033 1 20020213 A 2560 3961899501 LANYARD DOUG DC9 DC983 3022083 WP L1 DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 SEA - DURING PREFLIGHT CHECK, L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM SLIDE COVER LATCH. REATTAC HED LANYARD BETWEEN GIRT BAR AND DOOR SLIDE COVER LATCH. (M) 2 L 7 2 4F RT A6WE 2002032700202 20020327 00202 WP 2002 3 27 ASAA0280034 1 20020214 A 5320 993053812 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, FOUND CORROSION ON OUTBOARD WEB FROM FS 522-541. REPLACED WEB SECTION FROM FS 503-600 PER SRM 5 1-30-02 AND 51-30-05. (M) 2 L 7 2 4F RT A6WE 2002032700203 20020327 00203 WP 2002 3 27 ASAA0280035 1 20020214 A 5310 59364423 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, AFT CARGO DOOR FRAME WEB WAS DETERMINED TO BE CRACKED AT LIGHTNING HOLE AT FS 1214, WL 16, AND B UTTOCK LINE 46. REPAIRED CRACK PER EA 5310-02059. (M) 2 L 7 2 4F RT A6WE 2002032700204 20020327 00204 WP 2002 3 27 ASAA0280036 1 20020217 A 5310 5912494501 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, FORWARD CARGO DOOR THRESHOLD LOWER BEAM WAS DETERMINED TO BE CORRODED AT FASTENER HOLES FROM FS 375-420. REMOVED CORROSION AND REPAIRED BEAM PER EA 53-10-02054. (M) 2 L 7 2 4F RT A6WE 2002032700205 20020327 00205 WP 2002 3 27 ASAA0280037 1 20020217 A 5330 59360331 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, FUSELAGE EXTERIOR SKIN WAS DETERMINED TO BE CORRODED AT CENTER OF LOWER LOBE, FS 1080, BETWEEN E NDS OF WING BODY FAIRING RUBSTRIPS. REMOVED CORROSION PER EA 5330-01566. (M) 2 L 7 2 4F RT A6WE 2002032700206 20020327 00206 WP 2002 3 27 ASAA0280038 1 20020217 A 5310 59360381 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, MID CARGO LOWER BEAM WAS DETERMINED TO BE CORRODED ON VERTICAL AND HORIZONTAL FACES FROM FS 636- 693 AND GOUGED FROM 655-689. REPAIRED DOOR BEAM PER EA 5310-02063. (M) 2 L 7 2 4F RT A6WE 2002032700207 20020327 00207 WP 2002 3 27 ASAA0280039 1 20020217 A 5310 59364423 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, AFT CARGO DOOR FRAME WEB WAS DETERMINED TO BE CRACKED AT LIGHTNING HOLE, FS STATION 1214. REPAI RED WEB CRACKS PER EA 531-02059. (M) 2 L 7 2 4F RT A6WE 2002032700208 20020327 00208 WP 2002 3 27 ASAA0280040 1 20020215 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - DURING PREFLIGHT CHECK, 1ST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. REPLACED DAMAG ED SECTION OF WIRING AND TWO LENS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002032700209 20020327 00209 WP 2002 3 27 ASAA0280041 1 20020216 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 17276 6233 53450 PAE - DURING LINE CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AS SEMBLY. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002032700210 20020327 00210 WP 2002 3 27 ASAA0280042 1 20020216 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 SEA - DURING PREFLIGHT CHECK, 1ST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. RECONNECTED WI RING BETWEEN MODULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002032700211 20020327 00211 WP 2002 3 27 ASAA0280043 1 20020216 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 SEA - DURING PREFLIGHT CHECK, FIRST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. RECONNECTED WIRING BETWEEN MODULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002032700212 20020327 00212 WP 2002 3 27 ASAA0280044 1 20020216 A 3350 1001191 BATTERY DOUG DC9 DC983 3022083 WP PORTABLE LIGHT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 20190 688 53074 OAK - PREFLIGHT CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT BATT ERY. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002032700213 20020327 00213 WP 2002 3 27 ASAA0280045 1 20020218 A 2560 3961899501 LANYARD DOUG DC9 DC982 3022082 WP R1 DOOR DETACHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 951AS 49111 PDX - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REPLACED LANYARD. (M) 2 L 7 2 4F A6WE 2002032700214 20020327 00214 WP 2002 3 27 ASAA0280046 1 20020219 A 5320 993061269 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, FOUND CORROSION ON FORWARD PASSENGER (L-1) DOOR WEB FS 1118, 1152, AND 1160. REPLACED WEB PER S RM 51-30-02 AND 51-30-05. (M) 2 L 7 2 4F RT A6WE 2002032700215 20020327 00215 WP 2002 3 27 ASAA0280047 1 20020219 A 5311 991960431 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OAK - DURING C-CHECK, FOUND CORROSION ON AFT SIDE OF CIRCUMFERENTIAL FRAME AT FS 1250 FROM LONGERON 29R-28L. (M) 2 L 7 2 4F RT A6WE 2002032700216 20020327 00216 WP 2002 3 27 ASAA0280048 1 20020220 A 5320 2912282 CHANNEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, FOUND CORROSION ON HAT CHANNEL AT FS 1106 AND 1155. REPLACED CHANNEL PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2002032700217 20020327 00217 WP 2002 3 27 ASAA0280049 1 20020220 A 5753 591921717 RETAINER DOUG DC9 DC983 3022083 WP T/E FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, FOUND LEFT OUTBOARD FLAP CENTER HINGE BEARING RETAINER HOLES AND SCREWS CORRODED. REPAIRED BEAR ING RETAINER AND REPLACED SCREWS PER EA 5750-01625. (M) 2 L 7 2 4F RT A6WE 2002032700218 20020327 00218 WP 2002 3 27 ASAA0280050 1 20020220 A 5753 591921810 HINGE FITTING DOUG DC9 DC983 3022083 WP T/E FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, FOUND RIGHT OUTBOARD FLAP CENTER HINGE SUPPORT ON WING REAR SPAR TO BE CORRODED IN TWO BEARINGS RETAINER HOLES. FASTENERS WERE ALSO CORRODED. REPAIRED BEARING RETAINER HOLES PER EA 5750-01625, AND REPLACE FASTENERS PER SRM 51-30. (M) 2 L 7 2 4F RT A6WE 2002032700219 20020327 00219 WP 2002 3 27 ASAA0280051 1 20020220 A 5753 59192189 HINGE FITTING DOUG DC9 DC983 3022083 WP T/E FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, FOUND LEFT OUTBOARD FLAP INBOARD HINGE BEARING RETAINER HOLES AND SCREWS CORRODED. REPAIRED BEA RING RETAINER HOLES PER EA 5750-01625, AND REPLACE FASTENERS PER SRM 51-30. (M) 2 L 7 2 4F RT A6WE 2002032800001 20020328 00001 NE 2002 3 28 EVA200203 2 20020319 A 7230 CF680C2D1F ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE W QOCF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 03 * 11155 48546 704273 CAPT REORTED :FIRE WARNING INTERMITTEM,ACRAS DOWNLINK MSG:NO.1 ENG N2 VIB 5.0,EGT 2022,A/C AIR RETURN TO ANC. MAINTENAN CE GOUND INSPECTION,1.FOUND NO.1 ENG TAIL PIPE BROKEN, N1 SIEZED, BIG CHIP FOUND AND TWO FIRE BOTTLES DISCHARGED. 2.NO.1 ENG LEVER ARM STG #5 BLADES BROKEN, 2 BLOW OUT DOOR OPENED AND PNEUM DUCT LINK B BROKEN. REPLACED NO.1 ENG AND FOUND AL L COND ARE NML. 2 L 7 3 4F 4 F RT A22WE E31N3 2002032800002 20020328 00002 NM 2002 3 28 DHL2002705543 1 20020327 A 5740 65413027 SUPPORT FITTING BOEING 727 72722C 138400F NM A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 UPON COMPLYING WITH VISUAL INSP OF LEFT WING, FOUND # 4 SPOILER ACTUATOR SUPPORT BRKT BOTTOM LEG CRACKED AND INBD AFT SP AR MOUNT ANGLE CRACKED AT LOWER END. 2 L 7 3 4F A3WE 2002032800006 20020328 00006 CE 2002 3 28 FPI2002F00004 1 20020111 A 5410 969800015 CHANNEL BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO RT NACELLE CRACKED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 9098Q TH109 UPPER U-CHANNEL ON ENGINE FIREWALL, BOTH LEFT AND RIGHT HAND ENGINE NACELLES. CRACK DEVELOPED WHERE ENGINE MOUNT BOLT R UNS THROUGH FIREWALL. PROBABLE CAUSE IS NORMAL ENGINE VIBRATION. 1 L 7 2 3O 3 O 3A16 E5CE 2002032800008 20020328 00008 CE 2002 3 28 L4Y2002F00000 1 20020311 A 3230 51227202 SUPPORT CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO RT MLG FWD PIVOT CRACKED E L4YA K NONE O OTHER IN INSP/MAINT 1 SW 19 2715T 14225 402C0214 CRACK FOUND DURING 100 HOUR INSPECTION. CAUSE WOULD BE HIGH TIME AIRCRAFT. ALL RIGGING WAS NORMAL. NO OTHER CAUSE COU LD BE FOUND. NOTE: HEAVYDUTY SUPPORTS ARE AVAILABLE AND ARE INSTALLED ON LATER MODEL AIRCRAFT. 1 L 7 2 3O 3 O A7CE E8CE 2002032800011 20020328 00011 CE 2002 3 28 ODAR018H 1 20020214 A 3230 50810323 TORQUE LINK BEECH 100 B100 1152919 CE GARRTT TPE331 TPE3316251M 01514 WP MLG BROKEN B ODAR K NONE O OTHER IN INSP/MAINT 1 EA 21 19DA BE87 RT MLG TORQUE KNEE FAILED AT UPPER PIVOT PIN. TORQUE KNEE WAS FOUND WITH SECTION MISSING ON INBOARD HALF AND BROKEN ON OUTBOARD SIDE. CRACKS WENT THROUGH GREASE FITTING HOLES IN BOTH CASES. GREASE FITTINGS WERE BOTH LOST. POSSIBLY CAUSE D BY EXCESSIVE SIDE LOAD. TORQUE KNEE WOULD BE STRONGER IF THERE WERE NO GREASE FITTINGS IN IT. PUT GREASE FITTINGS IN PIVOT PIN ENDS. 1 L 7 2 4T 4 T A14CE E2WE 2002032800012 20020328 00012 EU 2002 3 28 S9H2002F00000 1 20020303 A 2913 704A33690004 BELT SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE HYDRAULIC PUMP FAILED E S9HA K NONE O OTHER IN INSP/MAINT 1 WP 19 358NT 50 1016 AIRCRAFT IN FLIGHT EXPERIENCED HYDRAULIC LIGHT AND THEN HYDRAULIC FAILURE. AIRCRAFT SAFELY RETURNED TO AIRPORT AND LAND ED. FAILURE OF HYDRAULIC BELT AT THE JOINING SEAM WAS THE CAUSE OF FAILURE. 1 G 7 1 3U 3 U H9EU E19EU 2002032800014 20020328 00014 WP 2002 3 28 TCH2002F00000 2 20020307 A 7250 8675691 TURBINE WHEEL BEECH 100 B100 1152919 CE GARRTT TPE331 TPE3316252B 01514 WP ENGINE CRACKED D TCHA K NONE O OTHER IN INSP/MAINT 1 GL 03 949SW 1643 BE34 P27071 SEVENTY CRACKS FOUND IN TURBINE WHEEL AT RIVET HOLES. THIS IS A 5400 HOUR TBO ENGINE. A PREMATURE FAILURE. 1 L 7 2 4T 4 T A14CE E2WE 2002032800015 20020328 00015 WP 2002 3 28 TCH2002F00001 2 20020307 A 7250 86756911 TURBINE WHEEL BEECH 100 B100 1152919 CE GARRTT TPE331 TPE3316252B 01514 WP ENGINE CRACKED D TCHA K NONE O OTHER IN INSP/MAINT 1 GL 03 949SW 1643 1643 BE34 P27071 FOURTEEN CRACKS FOUND IN TURBINE WHEEL AT RIVET HOLES. THIS IS A 5400 HOUR TBO ENGINE. A PREMATURE FAILURE. 1 L 7 2 4T 4 T A14CE E2WE 2002032800016 20020328 00016 WP 2002 3 28 TCH2002F00002 2 20020307 A 7250 8682721 TURBINE WHEEL BEECH 100 B100 1152919 CE GARRTT TPE331 TPE3316252B 01514 WP ENGINE CRACKED D TCHA K NONE O OTHER IN INSP/MAINT 1 GL 19 949SW 6885 1643 BE34 P27071 SIXTEEN CRACKS AT RIVET HOLES IN TURBINE WHEEL. RIVET HOLES IN TURBINE WHEEL. THIS IS A 5400 HOUR TBO ENGINE. A PREMA TURE FAILURE. 1 L 7 2 4T 4 T A14CE E2WE 2002032800017 20020328 00017 WP 2002 3 28 TCH2002F00003 2 20020307 A 7250 8682721 TURBINE WHEEL BEECH 100 100BEECH 1152916 CE GARRTT TPE331 TPE3316252B 01514 WP ENGINE CRACKED D TCHA K NONE O OTHER IN INSP/MAINT 1 GL 19 949SW 6885 BE34 P27070 CRACKE AT RIVET HOLES IN TURBINE WHEEL. THIS IS A 5400 HOUR TBO ENGINE A PREMATURE FAILURE. 1 L 7 2 3T 4 T A14CE E2WE 2002032800018 20020328 00018 WP 2002 3 28 TCH2002F00004 2 20020307 A 7250 8686309 TURBINE WHEEL BEECH 100 B100 1152919 CE GARRTT TPE331 TPE3316252B 01514 WP ENGINE CRACKED D TCHA K NONE O OTHER IN INSP/MAINT 1 GL 19 949SW 6885 BE34 P27071 TOW CRACKS AT RIVET HOLES, AND DISK DAMAGE ON AFT SIDE. THIS ISA 5400 HOUR TBO ENGINE. A PREMATURE FAILURE. 1 L 7 2 4T 4 T A14CE E2WE 2002032800019 20020328 00019 WP 2002 3 28 TCH2002F00005 2 20020307 A 7250 8945286 STATOR BEECH 100 100BEECH 1152916 CE GARRTT TPE331 TPE3316252B 01514 WP ENGINE CRACKED D TCHA K NONE O OTHER IN INSP/MAINT 1 GL 19 949SW 1643 BE34 P27071 STATOR CRACKED BEYOND LIMITS. THIS IS A 5400 HOUR TBO ENGINE. A PREMATURE FAILURE. 1 L 7 2 3T 4 T A14CE E2WE 2002032800020 20020328 00020 WP 2002 3 28 TCH2002F00006 2 20020307 A 7250 8964509 STATOR BEECH 100 100BEECH 1152916 CE GARRTT TPE331 TPE3316252B 01514 WP ENGINE CRACKED D TCHA K NONE O OTHER IN INSP/MAINT 1 GL 19 949SW 6885 BE34 P27071 STATOR CRACK BEYOND LIMITS. THIS IS A 5400 HOUR TBO ENGINE. A PREMATUE FAILURE. 1 L 7 2 3T 4 T A14CE E2WE 2002032800021 20020328 00021 WP 2002 3 28 TCH2002F00007 2 20020307 A 7240 31017553 COMBUST CHAMBER BEECH 100 100BEECH 1152916 CE GARRTT TPE331 TPE3316252B 01514 WP ENGINE CRACKED D TCHA K NONE O OTHER IN INSP/MAINT 1 GL 19 949SW 1643 BE34 P27071 COMBUSTOR CRACKED. THIS IS A 5400 TBO ENGINE. A PREMATURE FAILURE. 1 L 7 2 3T 4 T A14CE E2WE 2002032800022 20020328 00022 WP 2002 3 28 TCH2002F00008 2 20020307 A 7240 31017553 COMBUST CHAMBER BEECH 100 100BEECH 1152916 CE GARRTT TPE331 TPE3316252B 01514 WP ENGINE CRACKED D TCHA K NONE O OTHER IN INSP/MAINT 1 GL 19 949SW 1643 BE34 P27071 COMBUSTOR CRACKED. THIS IS A 5400 TBO ENGINE. A PREMATURE FAILURE. 1 L 7 2 3T 4 T A14CE E2WE 2002032800023 20020328 00023 CE 2002 3 28 TIM2002F00011 1 20020129 A 2934 993641581 CIRCUIT BOARD BEECH 99 C99 1154006 CE PWA PT6 PT6* 52043 EA HYD SYSTEM BURNED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 216CS U216 PN 993641581, A PRINTED CIRCUIT BOARD ASSEMBLY INSTALLED IN A TIME DELAY ASSEMBLY. THE ASSEMBLY IS PART OF THE HYDRAULI C SYSTEM AND IS IN THE LOW LIQUID LEVEL SENSOR CIRCUIT. A CHECK OF THE ELECTRICAL SYSTEM FOUND NO DEFECTS IN THE SYSTEM . THE CAUSE OF THE MELT DOWN OF THE BOARD IS UNKNOWN. 1 L 7 2 3T 3 T A14CE E2NE 2002032800024 20020328 00024 SW 2002 3 28 UUM2002F00000 1 20020315 A 7120 5620003179 BEAM GULSTM 560 560 0141402 SW LYC O480 GO480B 41527 EA ENG MOUNT CRACKED D UUMR K NONE O OTHER IN INSP/MAINT 1 GL 07 2705B 6247 205 L86228 DURING AN ANNUAL INSPECTION, THE LEFT ENGINE, ENGINE MOUNT BEAM ASSEMBLY WAS FOUND CRACKED. THE CRACK WAS MIDWAY IN THE BEAM AND WAS 60-70 PERCENT OF THE WAY THROUGH THE BEAM. THERE WAS A CLAMP ON THE ENGINE DIRECTLY BEHIND THE CRACK, AND THE BEAM MAY HAVE BEEN SCRATCHED BY A TOOL OR BY THE CLAMP UPON INSTALLATION. (THIS WAS INDICATED ON THE RIGHT ENGINE, WHICH HAD THE CLAMP IN THE SAME PLACE, AND HAD A DEEP SCRATCH IN IT). ANOTHER FACTOR THAT CONTRIBUTED TO THE CRACK WAS THAT ALL THE RUBBER SHOCK MOUNTS ON THE ENGINE HAD SAGGED TO A POINT WHERE THE ENGINE WAS RESTING DIRECTLY ON THE BEAM, SO THERE WAS NO ISOLATION FROM ENGINE VIBRATION. 1 H 7 2 3O 3 O 6A1 E275 2002032800025 20020328 00025 CE 2002 3 28 VJ32002F00014 1 20020313 A 3230 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MLG INOPERATIVE B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 8251C 191 CE1543 LANDING GEAR WOULD NOT COME DOWN. RELAY WAS REMOVED AND A NEW RELAY WAS INSTALLED. LANDING GEAR OPERATIONAL CHECKED NO RMAL. RELAY SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002032800026 20020328 00026 CE 2002 3 28 VJ32002F00015 1 20020314 A 3230 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MLG INTERMITTENT B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 8242T 673 CE1610 LANDING GEAR WOULD NOT COME DOWN, RELAY INTERMITTENT IN OPERATION. NEW RELAY INSTALLED AND FUNCTIONAL OPERATION ON THE LANDING GEAR WAS PERFORMED CYCLING THE GEAR MANY TIMES, LANDING GEAR OPERATION CHECKED, NORMAL. 1 L 7 1 3O 3 O 3A15 E5CE 2002032800027 20020328 00027 SO 2002 3 28 VJ32002F00016 2 20020318 A 7320 10238901211 TRANSMITTER BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO FUEL FLOW FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 1568P 1 CE1298 AFTER ONE HOUR OF OPERATION THE FUEL FLOW TRANSMITTER FAILED. A NEW FUEL FLOW TRANSMITTER WAS INSTALLED AND OPERATION C HECK OF THE SYSTEM CHECKED NORMAL FUEL FLOW TRANSMITTER SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002032800028 20020328 00028 SO 2002 3 28 VJ32002F00017 1 20020318 A 2701 6827302 BUSHING PIPER PA34 PA34220T 7103420 SO RT CONTROL YOKE SEIZED B VJ3R O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 07 4123C 2031 3449042 THE CONTROLS LOCKED UP IN FLIGHT. THE PILOT WAS ABLE TO UNLOCK THE CONTROL IN FLIGHT WITH A JERK; AFTER THE CONTROLS W ERE FREE THE PILOT NOTICED THAT THE BUSING ON THE RIGHT CONTROL YOKE WAS FROZEN TO THE SHAFT OF THE CONTROL YOKE. SEE D ETAILS ATTRACTED FROM THE PARTS BOOK ITEM NR 20 (BUSHING PART NUMBER 68273-02). NEW BUSHING INSTALLED AND OPERATION OF THE FLIGHT CONTROL CHECKED NORMAL. 1 L 7 2 3O A7SO 2002032800032 20020328 00032 NE 2002 3 28 COMA0210010 2 20020326 A 7200 PW118 ENGINE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE R/H FAILED A COMA E ENGINE SHUTDOWN Y ENGINE STOPPAGE DE DESCENT 1 SO 01 264CA 21250 120256 115556 FLIGHT 5059 R/H ENGINE FAILED WITH NO WARNINGS. IFSD REPLACED ENGINE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002032800033 20020328 00033 EA 2002 3 28 COMA0260219 1 20020326 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS CL CLIMB 1 SO 01 940CA 7048 FLIGHT 5654 FLAPS FAILED AFTER T/O.COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2002042500099 20020425 00099 NM 2002 4 25 02FDEA00220 1 20020327 A 5522 SKIN DOUG MD11 MD11 3023602 NM ELEVATOR SEPARATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RIGHT O/B ELEVATOR UPPER SURFACE EXHIBITS COMPOSITE SCREEN MESH SEPARATION AT CRACKING PAINT. 2 L 7 3 4F RT A22WE 2002032800039 20020328 00039 NM 2002 3 28 2002UALA00492 1 20020317 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 CABIN STATION 850, LBL 33, TRANSBEAM UPPER CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED TRANSBEAM WITH NEW SEC TION AND SPLICE ANGLES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002032800041 20020328 00041 NM 2002 3 28 2002UALA00494 1 20020318 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 FORWARD CABIN FLOOR BODY STATION 365 RBL 15 TO RBL 48 T-CAP HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. RE PLACED T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032800042 20020328 00042 NM 2002 3 28 2002UALA00496 1 20020316 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 CABIN FLOORBEAM STA 310 RBL 40 HAS EXCESSIVE MATERIAL LOSS FROM CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. INSTALLE D TWO STRAPS REPAIRS ON EACH SIDE OF T-FLANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032800043 20020328 00043 NM 2002 3 28 2002UALA00499 1 20020316 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 CABIN FLOORBEAM UPPER FLANGE HAS CORROSION STATION 324 RBL 50 TO 60. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND AN GLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032800044 20020328 00044 NM 2002 3 28 2002UALA00500 1 20020316 A 2540 ODOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 587UA 26713 ELECTRICAL SMELL COMING FROM BOTH AFT LAVS. 2 L 7 2 4F 4 F RT A2NM E17NE 2002040500032 20020405 00032 NM 2002 4 5 2002UALA00501 1 20020315 A 2782 251N509114 PDU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L/E SLAT FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 WP 29 567UA 26673 LEADING EDGE DISAGREE EICAS MESSAGE AND LIGHT ILLUMINATED. FAILURE OF THE LEADING EDGE SLAT POWER DRIVE UNIT, (PDU), CA USED THE LEADING EDGE SLAT AND TRAILING EDGE FLAP SYSTEMS TO SHUTDOWN AND PRODUCE THE LEADING EDGE DISAGREE EICAS MESSAG E. REPLACED THE LEADING EDGE SLAT PDU AND OPERATIONALLY CHECKED THE SYSTEM GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002040500033 20020405 00033 NM 2002 4 5 2002UALA00502 1 20020318 A 2750 113W14511 BELLCRANK BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE T/E FLAP FRACTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 785UA 9353 26954 BELL CRANK FOUND FRACTURED ALONG WITH ADJACENT 113W1452-X PUSH ROD WITH ROD END FRACTURED. FOUND DAMAGED OVERWING FAIRI NG SPRT MLG BODY DOOR STOP STRUCTURE INSTL (49W4172-2,149W4175-1). MINOR DAMAGE (GOUGE TO INSIDE WALL OF I/B FLAP TRACK ON I/B FLAP). CLIP & ADJACENT RIB ON ADJACENT FAIRING DAMAGED. I/B LT FLAP WAS EXTENDED INTO GSE EQUIP CAUSING DAMAG E TO FLAP T/E & CANOE FAIRING. AT THIS TIME, UAL SUSPECTS THAT IMPACT TO FLAP CAUSED PARTIAL OR FULL FRACTURE OF BELL C RANK. ANOTHER OPERATOR REPORTED A FRACTURED BELL CRANK AND BROKEN FLAP, INBOARD TRACK. PARTS ARE BEING SENT TO UAL MET ALLURGIST TO DETERMINE MORE ABOUT HOW THE PARTS FRACTURED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002032800045 20020328 00045 NM 2002 3 28 2002UALA00503 1 20020318 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 STATION 925 STRINGER 24L INBOARD UPPER FLANGE GOUGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032800046 20020328 00046 NM 2002 3 28 2002UALA00504 1 20020318 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 EXTERNAL FUSELAGE SKIN REPAIR AT STATION 488 FORWARD PIT DOOR CUT OUT IS MISSING ROW OF FASTENERS BELOW SKIN LAP. MAJOR REPAIR ACCOMPLISHED. TRIPLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032800047 20020328 00047 NM 2002 3 28 2002UALA00505 1 20020318 A 5320 SILL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 AFT PIT DOOR CUTOUT LOWER AUXILIARY SILL BEAM WEB SECTION IS CRACKED AT BODY STATION 827-847, STRINGER 27R, WL 153-162. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB SECTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032800048 20020328 00048 NM 2002 3 28 2002UALA00506 1 20020318 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 FORWARD CABIN STATION 294.5 STRINGER 17R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032800049 20020328 00049 NM 2002 3 28 2002UALA00507 1 20020318 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 CABIN STATION 360 STRINGER 14L TAIL CRACKED AT FASTENER JUST FORWARD OF FRAME. MAJOR REPAIR ACCOMPLISHED. INSTALLED NE W U-CHANNEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032800050 20020328 00050 NM 2002 3 28 2002UALA00511 1 20020319 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 AFT CARGO PIT INTERCOSTAL WEB T-BODY STATION 807 TO 847, STRINGER 25R HAS CORROSION AND IS GOUGED AT LOWER FASTENER HOLE S. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002032800051 20020328 00051 NM 2002 3 28 2002UALA00513 1 20020320 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 CABIN, BODY STATION 887 FRAME, BETWEEN S8R & S9R, FRAME IS CRACKED AT FASTENER HOLE FOR VENT BRACKET. MAJOR REPAIR ACCO MPLISHED. INSTALLED REPAIR ANGLE-CHANNEL DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040500034 20020405 00034 NM 2002 4 5 2002UALA00514 1 20020319 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 SEATS 44A, B, C EEL LAMP INOP. REPLACED EEL STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002040500035 20020405 00035 NM 2002 4 5 2002UALA00515 1 20020319 A 3397 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 UPPER DECK EMERGENCY LIGHT ON STAIRCASE INOP. FOUND BROKEN CONNECTOR UNDER CARPET IN UPPER DECK. REPLACED BUS CABLE. ALL EMERGENCY LIGHTS OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002032800052 20020328 00052 NM 2002 3 28 2002UALA00516 1 20020320 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 AFT PIT FRAME AT 1480 3 INCHES BELOW STRINGER 26R UPPER FLANGE ON FRAME HAD WEAR MARK. MAJOR REPAIR ACCOMPLISHED. FABR ICATED A TWO PLY STRAP THAT WAS INSTALLED ON UNDERSIDE OF FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032800053 20020328 00053 NM 2002 3 28 2002UALA00517 1 20020320 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 BODY STATION 852 RBL 54-81 TRANSVERSE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR SPLICE S. 2 L 7 2 4F 4 F RT A1NM E24NE 2002032800054 20020328 00054 2002 3 28 801DM0002 4 20020323 A 3417 ADC BOEING 757 757200 1384950 NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 801DM 26240 Aircraft will not maintain selected speed in cruise. 2 L 7 2 4F RT A2NM 2002032800055 20020328 00055 NM 2002 3 28 2002UALA00518 1 20020320 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 BODY STATION 800-852 LBL 54.81 TRANSVERSE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR SP LICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040500036 20020405 00036 NM 2002 4 5 2002UALA00520 1 20020321 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 MAIN LANDING GEAR WHEEL WELL HORIZONTAL BULKHEAD WEB IS CRACKED BS 665, LBL 32 WL 202. MAJOR REPAIR ACCOMPLISHED. REPA IR DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040500037 20020405 00037 NM 2002 4 5 2002UALA00521 1 20020321 A 5220 COVER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE EMERGENCY EXIT OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 609UA 21870 LEFT WING EMERGENCY SLIDE DEPLOYED. THE AMT INVESTIGATED A VERBAL REPORT FROM THE INBOUND CREW THAT THE PLASTIC COVER H AD FALLEN OFF THE LEFT OVERWING DOOR RELEASE HANDLE. IT WAS DETERMINED THAT THE HANDLE GRIP WAS ROTATED 90 DEGREES FROM ITS CORRECT POSITION. THE AMT THOUGHT HE COULD TWIST THE HANDLE WITHOUT DISTURBING THE RELEASE HANDLE. HE HAD NOT DIS ARMED THE SYSTEM. THE SLIDE BLEW. 2 L 7 2 4F 4 F RT A1NM E3NE 2002040500038 20020405 00038 NM 2002 4 5 2002UALA00522 1 20020321 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 FUSELAGE SKIN AT STA 1426 LWR AFT END OF AFT PIT DOOR, DENTED WITHIN 10 INCHES OF DOOR CUTOUT STRINGER 25R-S7R. MAJOR R EPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002040500041 20020405 00041 NM 2002 4 5 2002UALA00523 1 20020321 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 STATION 1600 LEFT HAND STRINGER 20 HAS FUSELAGE DAMAGED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002032800056 20020328 00056 WP 2002 3 28 ABXA010781 1 20020318 A 3230 3755769509 BUSHING DOUG DC8 DC863F 302198F WP RT MLG DEFECTIVE A ABXA O OTHER O OTHER CL CLIMB 1 GL 23 815AX 46097 UNABLE TO RETRACT GEAR ON FIRST ATTEMPT. GROUND COOLING AND BLOWAWAY JET RETRACTED NORMALLY. REMOVED THE RIGHT MAIN LA NDING GEAR, REPLACED GEAR BUSHING IAW DC-8 MM. REINSTALLED RIGHT MAIN LANDING GEAR. SWING AND OPS CHECKED GOOD. REPLA CED BLOW AWAY JET SWITCH AND OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2002032800057 20020328 00057 WP 2002 3 28 ABXA010783 1 20020325 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 908AX 255 47008 DURING PREFLIGHT CHECK, FOUND THE EMERGENCY CABIN LIGHTS INOPERATIVE. REPLACED THE BATTERY POWER SUPPLY IAW DC-9 MM. O PS CHECKED GOOD. 2 L 7 2 4F A6WE 2002032800058 20020328 00058 WP 2002 3 28 ABXA010791 1 20020315 A 5720 STRAP DOUG DC8 DC861 3021952 WP WING SPAR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 T-CAP DOUBLER STRAP AT WS 485.00, FORWARD SPAR, LOWER CRACKED NR 4 ALT. REMOVED AND REPLACED DOUBLER STRAP IAW DC-8 SRM 51-1-20D, 51-1-24 AND DAC DWG 5803958. 2 L 7 4 4F 4A25 2002032800059 20020328 00059 WP 2002 3 28 ABXA010793 1 20020108 A 5313 STRINGER DOUG DC8 DC861 3021952 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 UPPER LEFT STRINGER 1 WAS CRACKED AT FS 1870, ABOVE BULKHEAD IN TAIL CONE FORWARD AREA. REPAIRED AREA IAW DC-8 SRM 51-1 -21, 51-1-20, 51-1-8, 53-2-0 AND REA D853-40948MR. 2 L 7 4 4F 4A25 2002032800060 20020328 00060 WP 2002 3 28 ABXA010796 1 20020121 A 5420 LINK DOUG DC8 DC861 3021952 WP NR 3 PYLON CHAFED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 NR 3 PYLON THRUST LINK CHAFED ON LOWER SIDE FROM PNEUMATIC DUCT CLAMP (REF EA AD 54-03277MR) FOR REPAIR OR REPLACEMENT P ER ABX CARD 8931015, STEP 02.A). REPAIRED AREA IAW DC-8 SB 54-92. 2 L 7 4 4F 4A25 2002032800061 20020328 00061 WP 2002 3 28 ABXA010797 1 20020205 A 5313 LONGERON DOUG DC8 DC861 3021952 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 RIGHT WHEEL WELL, LONGERON 24 RIGHT WAS CRACKED AND CORRODED AT STATION 980. REPAIRED AREA AND INSTALLED NEW DOUBLER AN D ANGLE IAW DC-8 SRM 51-1-21, 51-1-8, 51-1-20D AND REA D853-40964MR. 2 L 7 4 4F 4A25 2002032800062 20020328 00062 WP 2002 3 28 ABXA010798 1 20020130 A 5320 WEB DOUG DC8 DC861 3021952 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 FORWARD CARGO, AT FS 80, RIGHT CUSP AT LONGERON 21 RIGHT, ATTACH ANGLE WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-8 AND REA D853-40960MR. 2 L 7 4 4F 4A25 2002032800063 20020328 00063 WP 2002 3 28 ABXA010799 1 20020205 A 5313 LONGERON DOUG DC8 DC861 3021952 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 FORWARD ACCESSORY COMPARTMENT LONGERON 36 WAS CORRODED AT FS 662. REPAIRED AREA AND INSTALLED NEW REPAIR ANGLE IAW DC-8 SRM 53-2-0, 51-1-20D, 51-1-8 AND REA D853-40966MR. 2 L 7 4 4F 4A25 2002032800064 20020328 00064 WP 2002 3 28 ABXA010802 1 20020301 A 5313 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 FORWARD CARGO, STATION 300 - 320, LONGERON 35 LEFT, ATTACH ANGLE CRACKED. REPAIRED AREA AND INSTALLED NEW SECTION OF LO NGERON, NEW -Z- FITTINGS, SPLICES AND NEW WEB IAW DC-8 SRM 51-1-20D, 53-2-0, 51-1-8, 51-1-24 AND REA D853-43046MR. 2 L 7 4 4F 4A25 2002032800065 20020328 00065 WP 2002 3 28 MWEA020201 1 20020327 A 5241 991157912 CLIP DOUG DC9 DC981 3022081 WP FWD GALLEY DR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FORWARD GALLEY SERVICE DOOR BEAM #1 ATTACH CLIP TO DOOR PAN IS CRACKED, LOCATED ON BOTTOM AFT END. -- INSTALLED NEW CL IP. REPLACED 2 SHORT FASTENERS. 2 L 7 2 4F A6WE 2002032800066 20020328 00066 WP 2002 3 28 MWEA020204 1 20020327 A 5310 59360109 LONGERON DOUG DC9 DC981 3022081 WP STATION 1338 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 LONGERON 17 LEFT CHAFED AFT OF SHOVEL CLIP AT STATION 1338. -- REMOVED DAMAGED SECTION. FORMED REPAIR SPLICE AND FILLE R SECTION. INSTALLED LONGERON REPAIR SPLICE. 2 L 7 2 4F A6WE 2002032800067 20020328 00067 NM 2002 3 28 UPS02437663 1 20020125 A 5347 BAC15201890 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 423 LBL 10 SEAT TRACK FLANGE CORRODED. SEAT TRACK REPLACED PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002032800068 20020328 00068 NM 2002 3 28 UPS02437675 1 20020125 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C FX - STA 840 LBL 16-20 EXT SKIN FOUND BULGED. STA 840 LBL 16-20 EXT SKIN CORROSION REMOVED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2002032800069 20020328 00069 NM 2002 3 28 UPS02437676 1 20020124 A 5210 SKIN BOEING 747 747123 1384873 NM R1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - R1 DOOR LOWER HINGE CUTOUT FOUND CRACKED. DOOR HINGE CUTOUT SKIN REPAIRED SRM 52-10-02 FIG 12. 2 L 7 4 4F A20WE 2002032800070 20020328 00070 NM 2002 3 28 UPS02437677 1 20020125 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C AFT CARGO COMPT - BS 1700 - 1725 S-49L STRINGER FOUND CORRODED. 2 L 7 4 4F A20WE 2002032800071 20020328 00071 NM 2002 3 28 UPS02437678 1 20020128 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C AFT CARGO COMPT - BS 1560 S51R STRINGER CORRODED. 2 L 7 4 4F A20WE 2002032800072 20020328 00072 NM 2002 3 28 UPS02437679 1 20020129 A 5314 KEELBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C FX - KEEL BEAM ACCESS PANEL ANCHOR NUT SUPPORT FOUND CORROSION AT STA 1400 FROM LBL 8 TO RBL 8. FX BS 1400 BEAM REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002032800073 20020328 00073 NM 2002 3 28 UPS02437680 1 20020128 A 5320 141U11074 WEB BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C RT SIDE NOSE W/W ON BS 320 VERTICAL BEAM WEB FOUND 1 EA INSULATION BLANKET STAND OFF HOLE CRACKED AT J UST BETWEEN NR 1 AND 2 STIFFENER. VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002032800074 20020328 00074 NM 2002 3 28 UPS02437681 1 20020126 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 2350 S-51R STRINGER FOUND CRACKED. M/D BS 2350 S-51R CRACKED STRINGER REPAIRED AS PER SRM 53 -10-03 FIG 1. 2 L 7 4 4F A20WE 2002032800075 20020328 00075 NM 2002 3 28 UPS02437682 1 20020207 A 5320 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C DURING LT SIDE STA 1241 EXTERNAL LONGERON REMOVE, NR 13 BOLT (FROM FWD) FOUND BROKEN AND BOLT HOLE FOU ND CORROSION. BOLT HOLE CORROSION REMOVED, LONGERON SPLICE STRAP, B/H GORGING AND SKIN REAMED TO 0.875 INCH, HFEC INSPE CTION PERFORMED AS PER NTM PT 6 51-00-00 FIG 1. 2 L 7 4 4F A20WE 2002032800076 20020328 00076 NM 2002 3 28 UPS02437683 1 20020129 A 5313 LONGERON BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C RT WLG W/W OVERWING LOWER LONGERON FOUND EXFOLIATION CORROSION AT STA 1246-1249 RBL 125-127. CORROSIO N REMOVED AND SHOT-PEEN C/O AS PER SRM 51-10-01 & SOPM 20-10-03. 2 L 7 4 4F A20WE 2002032800077 20020328 00077 NM 2002 3 28 UPS02437684 1 20020129 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C LT WLG W/W STA 1241 B/H FOUND CORROSION AT WL 143 LBL 0-11. 2 L 7 4 4F A20WE 2002032800078 20020328 00078 NM 2002 3 28 UPS02437685 1 20020128 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C LEFT WLG W/W PRESSURE DECK WEB FOUND CORROSION CRACK AT STA 1319-1323 LBL 128-130. PATCH REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002032800079 20020328 00079 NM 2002 3 28 UPS02437686 1 20020125 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 380 S-24AL FRAME FOUND CRACKED. FRAME REPAIRED AS PER RS R53-12-34720. 2 L 7 4 4F A20WE 2002032800080 20020328 00080 NM 2002 3 28 UPS02437688 1 20020125 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C M/D - BS 380 S-24AR FRAME FOUND CRACKED. FRAME REPAIRED AS PER RS R53-12-34721. 2 L 7 4 4F A20WE 2002032800081 20020328 00081 NM 2002 3 28 UPS02437690 1 20020128 A 5320 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C CRACK REVEALED ON LT BS 1480 BULKHEAD HOLE NR 3 AT EXTENSION FITTING, SKIN, BULKHEAD CHORD AND OUTER C HORD SPLICE FITTING. LT BS 1480 BULKHEAD HOLE NR 3 EXTENSION FITTINGG REAMED TO 0.650 INCH, SKIN REAMED TO 0.687 INCH, BULKHEAD CHORD REAMED TO 0.625 INCH & OUTER CHORD SPLICE FITTING REAMED TO 0.687 INCH AS PER EO B747-5310-10732 & NDT CO NFIRMED NR 3 HOLE NO CRACK REVEAL. REPAIR BUSHING INSTALLED ON NR 3 HOLE AS PER SB 747-53A2390 R1 FIG 11. 2 L 7 4 4F A20WE 2002032800082 20020328 00082 EU 2002 3 28 MALA020209 1 20020320 A 2460 PDU SAAB SF340 SF340A 7850100 EU DEFECTIVE A MALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 119XJ 340A119 BEFORE TAKEOFF OF FLIGHT #3016, LEFT SIDE AVIONICS ARE LOST ANYTIME THE HYDRAULIC PUMP RUNS. RETURN TO GATE. MAINTENAN CE REPLACED LH PDU, ALL CHECKS GOOD. SEE CONTINUATION CARD #063144 AND MM 409 #080345 FOR DETAILS. 2 L 7 2 4T RT A52EU 2002032800083 20020328 00083 EU 2002 3 28 MALA020212 1 20020326 A 7600 PCU SAAB SF340 SF340A 7850100 EU A MALA K NONE S AFFECT SYSTEMS LD LANDING 1 GL 15 99XJ 340A099 DURING LANDING ROLLOUT OF FLIGHT #2917, LH ENGINE TORQUE "IN GROUND IDLE" WAS 20-25%. AC WANTED TO PULL RIGHT. POWER L EVERS WERE NOT IN FULL REVERSE. MAINTENANCE ADJUSTED LH AND RH PCU'S AS REQUIRED. IAW AMM 76-10-00-05. POWER LEVER SPLI T IN REVERSE CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002032800084 20020328 00084 EU 2002 3 28 MALA020215 1 20020327 A 1100 PLACARD SAAB SF340 SF340A 7850100 EU CABIN MISINSTALLED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 368XJ BINS THAT CONTAIN EMERGENCY EQUIPMENT MISMARKED. INSTALLED TEMP PLACARD FOR FIRE EXT/PBE/MED KIT. MAINTENANCE INSTALLE D PLACARDS. 2 L 7 2 4T RT A52EU 2002032800085 20020328 00085 NM 2002 3 28 UPS02437758 1 20020226 A 5320 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C RT BS 1480 HOLE 22 FOUND CRACKED AT BULKHEAD WEB SPLICE PLATE. PLS REFER ATTACHED SKETCH FOR DETAILS. RT BS 1480 BULKHEAD WEB SPLICE PLATE 22 HOLE OVERSIZED TO 0.500 INCH AND REPAIR BUSHING INSTALLED AS PER SB 747-5A2390 AND EO 747-5310-10732. 2 L 7 4 4F A20WE 2002032800086 20020328 00086 WP 2002 3 28 CALA0200151 1 20020327 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FS 769-786 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND INTERCOSTAL CORRODED IN MID CARGO COMPARTMENT AT FS 769-786 BETWEEN L27R AND 28R. THE INTERCOSTAL WAS R EMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2002032800087 20020328 00087 NM 2002 3 28 CALA0200152 1 20020327 A 5330 SKIN BOEING 737 737524 1384721 NM STA 1104 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33637 27540 INSPECTION FOUND FUSELAGE SKIN PANEL GOUGED AFT OF L/H HORIZONTAL STABILIZER FORWARD ATTACH FITTING AT STA 1104, WL 265. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5331-01110. 2 L 7 2 4F RT A16WE 2002032800088 20020328 00088 WP 2002 3 28 CALA0200153 1 20020327 A 5320 PAN DOUG DC9 DC982 3022082 WP STA 370-420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND PAN CORRODED AT FORWARD CARGO DOOR CUTOUT AREA, STA 370-420. THE CORROSION WAS BETWEEN SCUFF PLATE AND JAMB. THE PAN WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 44. 2 L 7 2 4F A6WE 2002032800089 20020328 00089 WP 2002 3 28 CALA0200154 1 20020327 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP STA 541 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND FORWARD BULKHEAD LOWER CENTER SUPPORT FRAME HAD CLIP-NUTS AND ATTACH HOLES CORRODED IN MID CARGO COMPAR TMENT AT STA 541. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4. 2 L 7 2 4F A6WE 2002032800090 20020328 00090 NM 2002 3 28 CALA0200155 1 20020328 A 3230 DIODE BOEING 737 7373T0 1384582 NM SOL, LEVER LCK FAULTY A CALA A D UNSCHED LANDING RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 09 70353 23591 THE LANDING GEAR TRIGGER LOCK OVERRIDE WAS REQUIRED TO RAISE THE GEAR AFTER TAKEOFF FROM EWR. IN ADDITION, THE "LAND GEA R LATCH AND PRESS WARNING" CIRCUIT BREAKER POPPED AND WOULD NOT RESET. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED SAFELY. MAINTENANCE FOUND THE M416 DIODE LOCATED AT THE LANDING GEAR LEVER LATCH SOLENOID INTERMITTENTLY BLEEDING THROUG H. THE M416 DIODE WAS REPLACED IAW STANDARD WIRING PRACTICES, WIRING DIAGRAM MANUAL 32-31-01, PAGE 901. AN OPERATIONAL C HECK PERFORMED IAW MM 32-31-31 WAS GOOD. 2 L 7 2 4F RT A16WE 2002032800091 20020328 00091 WP 2002 3 28 CALA0200156 1 20020327 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 1146 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1146, LBL 40. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTI ON WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4F, AND 51-10-3. 2 L 7 2 4F A6WE 2002032800092 20020328 00092 NM 2002 3 28 CALA0200157 1 20020328 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 796-847 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND AFT BAGGAGE BIN WEB AT DOORWAY CORRODED, STA 796-847. A NEW WEB WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002032800093 20020328 00093 WP 2002 3 28 MWEA020190 1 20020327 A 5310 99236874 INTERCOSTAL DOUG DC9 DC932 3022066 WP STATION 560 IMPROPER A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FORWARD PIT INTERCOASTAL LOCATED BETWEEN LONGERON 28 RIGHT AND 27 RIGHT AND FRAMES 560-579 HAS SEVERAL DIVETS IMPROPERLY BACKED. -- FABRICATED AND INSTALLED AFT FLANGE. FOUND CRACKS ON INTERCOSTAL LOWER ATTACH HOLES. FABRICATED AND INSTAL LED INTERCOSTAL . 2 L 7 2 4F A6WE 2002032800094 20020328 00094 WP 2002 3 28 MWEA020192 1 20020327 A 5310 39120752 FITTING DOUG DC9 DC932 3022066 WP STATION 218 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 REMOVED FLOOR BEAM END FITTING AT CUSP, STATION 218 LEFT SIDE TO FACILITATE OTHER MAINTENANCE. -- FITTING DAMAGED UPON REMOVAL. INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2002032800095 20020328 00095 WP 2002 3 28 MWEA020193 1 20020327 A 5310 995783811 FITTING DOUG DC9 DC932 3022066 WP STATION 207 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FITTINGS MISDRILLED AT STATION 207 (INTERCOSTAL ATTACH CLIP). -- FABRICATED AND INSTALLED NEW FITTING. LOCATED AND PRI MED AND INSTALLED PARTS. 2 L 7 2 4F A6WE 2002032800096 20020328 00096 WP 2002 3 28 MWEA020195 1 20020327 A 5310 29130441 GUSSET DOUG DC9 DC932 3022066 WP STATION 580 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 GUSSET AT STATION 580 IS CORRODED ON INTERCOSTAL. -- FABRICATED AND INSTALLED GUSSET. 2 L 7 2 4F A6WE 2002032800097 20020328 00097 WP 2002 3 28 MWEA020205 1 20020326 A 2932 1474253 VALVE DOUG DC9 DC981 3022081 WP WHEEL WELL LEAKING A MWEA A UNSCHED LANDING K FLUID LOSS DE DESCENT 1 GL 31 803ME 48029 TOTAL LOSS OF RIGHT HYDRAULIC PRESSURE AND FLUID QTY WHEN THE SWITCH WAS TURNED ON HIGH. -- MAINTENANCE WAS SENT TO RE MOVE AND REPLACE THE ENGINE HYDRAULIC PUMP, REMOVE AND REPLACE THE SPOILER SYSTEM VALVE, AND REMOVE THE LEFT GEAR DOOR D UE TO DAMAGE. 2 L 7 2 4F A6WE 2002032900001 20020329 00001 SO 2002 3 29 C2XA02IA081 1 20020325 A 4900 45011958B APU EMB 145 EMB145ER 3260211 SO TAIL LEAKING A C2XA K NONE O OTHER AP APPROACH 1 SW 27 17928 145007 DURING APPROACH FLIGHT 3649, THE CREW NOTED THAT THE APU FAILED ON APPROACH/STRONG FUEL ODOR IN CABIN AND COCKPIT. IAH- MAINTENANCE INSPECTED THE APU, AND, THE AIRCRAFT WAS RELEASED IAW MEL. IAH- MAINTENANCE REMOVED AND REPLACED THE APU, PERFORMED A OPERATINAL CHECK OF THE APU, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002032900002 20020329 00002 NM 2002 3 29 HNAA0200033 1 20020329 A 5311 85330073101 FRAME DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 916HA 072 DuringC-check found correded frame leg @X510 from STR30S to STR32S. The damage was repaired per EO8-53-02-0366. This EO replaces frame segment form existing factory splice at STR33 to STR29S. 2 H 7 2 4T RT A13NM 2002032900003 20020329 00003 NM 2002 3 29 2002F00344 1 20020206 A 5320 653535215 SPLICE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND TWO STRINGER SPLICES CRACKED .125 INCH AND .25 INCH LONG, COMING FROM RIVET HOLES, STATION 907 54L. INSTALL ED NEW SPLICE PER 51-40-02. REF USAA020059. (M) 2 L 7 2 4F RT A16WE 2002032900004 20020329 00004 NM 2002 3 29 2002F00345 1 20020206 A 5320 1123371 SPLICE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 23313 PIT - FOUND STRINGER SPLICE CRACKED .125 INCH AND .25 INCH LONG, COMING FROM RIVET HOLES, STATION 907 54R. INSTALLED SP LICE PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002032900005 20020329 00005 SW 2002 3 29 2002F00335 1 20020224 A 5230 H29497 LATCH SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR MISINSTALLED A BSAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 05 160MC AC733B MWH - FLT 6006 - CARGO DOOR WARNING LIGHT CAME ON DURING CRUISE FLIGHT. WHEN AIRCRAFT WAS DEPRESSURIZED THE LIGHT WENT OUT. CREW CONTINUED TO NEXT STATION AS IT WAS CLOSER. THE LOWER EDGE FORWARD CLICK-CLACK JAWS WERE NOT EXTENDING CORRE CTLY. THE LOWER EDGE AFT CLICK-CLACK EXTENSION WASN'T CORRECT. THE LOWER FORWARD CLICK-CLACK WAS REPLAED, BOTH THE FOR WARD AND AFT LOWER CLICK-CLACKS WERE ADJUSTED PER MM. TEST FLIGHT WAS COMPLETED WITH NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A8SW 2002032900006 20020329 00006 SW 2002 3 29 2002F00336 1 20020207 A 7931 2719153001 TRANSDUCER FRCHLD SA227 SA227DC 3377521 SW OIL PRESSURE FAILED A BSAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 05 853LS DC853B DURING CLIMB-OUT, THE CREW NOTICED THE LT OIL PERSSURE WAS BELOW THE LOWER REDLINE ON THE GAUGE. THE ANNUNCIATOR PANEL LOW OIL PRESSURE LIGHT WAS NOT ON, AND THE OIL TEMP WAS NORMAL. ALL OTHER ENGINE INDICATIONS WERE NORMAL. CREW RETURNE D TO STATION WITH NO FURTHER PROBLEMS. INDICATION PROBLEM. REPLACED OIL PRESSURE TRANSDUCER, CLEANED AND REINSTALLED S NUBBER. (M) 2 L 7 2 4T RT A18SW 2002032900007 20020329 00007 SW 2002 3 29 2002F00339 1 20020201 A 5230 LATCH SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR STUCK A BSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 27465 AC755B JUST AFTER TAKEOFF UPON ROTATION, THE CARGO DOOR WARNING LIGHT CAME ON. CREW DID A GO AROUND AND RETURNED TO STATION. STICKY HANDLE OR CLICK CLACKS, OR DOOR CLOSING PROCEDURES. CLEANED AND LUBED CLICK CLACKS. (M) 2 L 7 2 4T RT A8SW 2002032900008 20020329 00008 NM 2002 3 29 2002F00340 1 20020222 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 801EA 22432 DURING C-CHECK, FOUND PREVIOUS REPAIR CRACKED IN FORWARD CARGO COMPARTMENT STRINGER 25L STATION 541 LBL 32. (M) 2 L 7 3 4F A3WE 2002032900009 20020329 00009 EU 2002 3 29 2002F00341 1 20020308 A 2810 4L95160 DISK AIRBUS 320 A320233 3930329 EU FUEL CELL BROKEN A SOKF O OTHER O OTHER LD LANDING 1 SO 23 481TA 1500 SJO - FLT 660 - DURING THE FLIGHT, THE CAPTAIN REPORTED FUEL IMBALANCE INDICATION, THE AIRCRAFT RETURNED TO SJO STATION FOR MAINTENANCE. AFTER LANDING, MAINTENANCE PERSONNEL PERFORMED OVERWEIGHT LANDING INSPECTION IAW AMM 05-51-11, AND DIS CREPANCIES WERE NOT FOUND, THEN DURING TROUBLESHOOTING OF THE CENTER FUEL TANK WAS FOUND THE OVERPRESSURE DISK BROKEN, I T WAS REMOVED AND REPLACED REMOVED IAW AMM 28-22-27. OPS CHECK OF FUEL INDICATION WAS PERFORMED WITH SATIFACTORY RESULT S AND THE AIRCRAFT WAS RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2002032900010 20020329 00010 NM 2002 3 29 CALA0200158 1 20020328 A 5320 WEB BOEING 737 7373T0 1384582 NM BS 590 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34315 23366 INSPECTION FOUND FOUR 1/2" CRACKS AT AFT LOWER BOLT HOLES OF WEB AT SECONDARY HEAT EXCHANGER CUTOUT, BS 590, LBL 41(WING CENTER SECTION). REPAIRED IAW ECRA 5712-01003. 2 L 7 2 4F RT A16WE 2002032900011 20020329 00011 NM 2002 3 29 CALA0200159 1 20020328 A 5313 STRINGER BOEING 737 7373T0 1384582 NM APU COMPT. CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND APU COMPARTMENT STRINGER CORRODED AT CUTOUT JUST BELOW APU INLET. A NEW STRINGER WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002032900012 20020329 00012 2002 3 29 SWAA020642 4 20020327 A 2565 6556685 BRACKET BOEING 737 7373H4 1384600 NM AFT SVC DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 397SW 27691 DURING SCHEDULED 1/D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE MOUNTING BRACKET BROKEN. REMOVED AND REPLACED BRACK ET PER MM. 2 L 7 2 4F RT A16WE 2002032900013 20020329 00013 NM 2002 3 29 SWAA020643 1 20020326 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED C3 CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW NR 11 ABC. SECURED LENS PER M M. 2 L 7 2 4F RT A16WE 2002032900014 20020329 00014 NM 2002 3 29 SWAA020645 1 20020327 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 365SW 26576 EEPLS COVER MISSING AT MID CABIN. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002032900015 20020329 00015 2002 3 29 SWAA020646 4 20020327 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 792SW 27887 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002032900016 20020329 00016 NM 2002 3 29 SWAA020647 1 20020327 A 5315 BAC1509 FLOORBEAM BOEING 737 7373G7 1384595 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT RBL 3.0, BS 727D TO BS 847. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002032900017 20020329 00017 NM 2002 3 29 SWAA020650 1 20020327 A 2751 6546430122 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED SERVICE CHECK, FOUND RT T/E INBD FORE FLAP DELAMINATED. REMOVED AND REPLACED RT T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002032900018 20020329 00018 NM 2002 3 29 SWAA020651 1 20020326 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 951, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002032900019 20020329 00019 2002 3 29 SWAA020636 4 20020325 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 622SW 27932 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002032900020 20020329 00020 2002 3 29 SWAA020637 4 20020326 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM AFT SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED BC1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE FWD SUPPORT BRACKET CRACKED. REPAIRED BRACKET PER S RM. 2 L 7 2 4F RT A16WE 2002032900021 20020329 00021 NM 2002 3 29 SWAA020641 1 20020323 A 5330 654577572 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD LOWER CORNER OF AFT CARGO DOOR CUTOUT. REPAIRED SKIN PE R SWA RA. 2 L 7 2 4F RT A16WE 2002040100039 20020401 00039 WP 2002 4 1 02FDEA00218 1 20020326 A 2750 FLAP DOUG DC10 DC1030 3023501 WP LT WING MALFUNCTIONED A FDEA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 SO 25 308FE 48297 WRI 27-50-7942 WITH FLAPS SEL AT 50 DEG LEFT TAPE IND 45 DEG IN FLT ON GRD FLAP TAPE GO TO 50 DEG. REMOVED AND REPLACED O/B FLAP PER MM 27-50-02-4. 2 L 7 3 4F A22WE 2002032900026 20020329 00026 NM 2002 3 29 UPS02437703 1 20020126 A 5312 BULKHEAD BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C FWD CARGO COMPT - E/E COMPT BS 400 S-31R BULKHEAD WEB FOUND CRACKED. BULKHEAD WEB REPAIRED AS PER BOE ING DWG 65B00272. 2 L 7 4 4F A20WE 2002032900027 20020329 00027 NM 2002 3 29 UPS02437716 1 20020219 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:N/A 1 EMERGENCY LT INOP UPPER DECK. REMOVED AND REPLACED BULB, OPS CHECK GOOD. 2 L 7 4 4F A20WE 2002032900028 20020329 00028 NM 2002 3 29 UPS02437724 1 20020222 A 3350 LIGHT BOEING 747 747121 1384871 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:IN UPPER DECK EMERGENCY LIGHT OVER STAIRWAY INOP. RELAMPED, OPS CHECKED GOOD. 2 L 7 4 4F A20WE 2002032900029 20020329 00029 NM 2002 3 29 UPS02437726 1 20020225 A 3350 BATTERY BOEING 747 747123 1384873 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:PFLT CEILING EMERGENCY LIGHT ABOVE UPPER DECK EMERGENCY EXIT DOOR INOP. RECHARGED BATTERY, OPS CHECK GO OD. 2 L 7 4 4F A20WE 2002032900030 20020329 00030 NM 2002 3 29 UPS02437750 1 20020228 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 2180 S-25L STRINGER FOUND CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2. 2 L 7 4 4F A20WE 2002032900031 20020329 00031 NM 2002 3 29 UPS02437756 1 20020226 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 1660-1680 RBL 11 SEAT TRACK LIP FOUND WORN. SEAT TRACK REPAIRED AT M/D BS 1600-1680 RBL 11 A S PER SRM 53-10-05 FIG 14. 2 L 7 4 4F A20WE 2002032900032 20020329 00032 NM 2002 3 29 UPS02437757 1 20020227 A 5320 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C RIGHT BS 1480 RIGHT WEB 23 HOLE FOUND CRACK AT BULKHEAD WEB SPLICE FITTING. PLS REFER SKETCH FOR DETA ILS. RIGHT BS 1480 BULKHEAD WEB 23 HOLE OVERSIZED TO DIA 0.562 INCH AND REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 AND EO 747-510-10732. 2 L 7 4 4F A20WE 2002032900033 20020329 00033 NM 2002 3 29 UPS02437759 1 20020226 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C RT BS 1480 HOLE 2 FOUND CORROSION AT BULKHEAD CHORD. RT BS 1480 BULKHEAD CHORD 2 HOLE OVERSIZED TO 0. 625 INCH AND CRACK FREE AS PER SB 747-53A2390 AND EO 747-5310-10732. 2 L 7 4 4F A20WE 2002032900034 20020329 00034 NM 2002 3 29 UPS02437760 1 20020227 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C RT BS 1480 BULKHEAD WEB 13 FASTENER HOLE CRACK REVEALED APPROX 0.030 INCH IN LENGTH FOR DETAIL. RT BS 1480 BULKHEAD WEB 13 HOLE OVERSIZED TO 0.500 INCH AND REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 AND EO747-5310-107 32. 2 L 7 4 4F A20WE 2002032900035 20020329 00035 NM 2002 3 29 UPS02437761 1 20020226 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C RT BS 1480 HOLE 2 FOUND CRACKED AT FUSELAGE SKIN. RT BS 1480 FUSELAGE SKIN 2 HOLE OVERSIZED TO DIA 0. 625 INCH AND CRACK FREE AS PER SB 747-53A2390 AND EO 747-5310-10732. 2 L 7 4 4F A20WE 2002032900036 20020329 00036 NM 2002 3 29 UPS02437762 1 20020226 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C LT BS 1480 HOLE 19 FOUND CRACKED AT BULKHEAD WEB PNL. LT BS 1480 BULKHEAD WEB 19 HOLE OVERSIZED TO 0. 5500 INCH AND REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 AND EO 747-5310-10732. 2 L 7 4 4F A20WE 2002032900037 20020329 00037 NM 2002 3 29 UPS02437763 1 20020226 A 5320 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C RT BS 1480 HOLE 3 FOUND CRACKED AT LONGERON EXTENSION FITTING. RT BS 1480 LONGERON EXTENSION FITTING 3 HOLE OVERSIZED TO DIA 0.625 AND REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 AND EO 747-5310-10732. 2 L 7 4 4F A20WE 2002032900038 20020329 00038 NM 2002 3 29 UPS02437764 1 20020302 A 5320 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C RT BS 1480 HOLE 3 FOUND CRACK AT OUTER CHORD SPLICE FITTING. RT BS 1480 OUTER CHORD SPLICE FITTING 3 HOLE OVERSIZED TO DIA 0.625 AND CRACK FREE PER SB 747-53A2390 AND EO 5310-10732 REPAIR BUSHING INSTALLED AS PER SB 747-5 A2390. 2 L 7 4 4F A20WE 2002032900039 20020329 00039 NM 2002 3 29 UPS02437765 1 20020224 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C FWD CARGO COMPT - S760 S-44R STRINGER FOUND CRACKED. BS 740-770 STR 44R STRINGER REPAIRED AS PER SRM 53-10-01 FIG 1. 2 L 7 4 4F A20WE 2002032900040 20020329 00040 NM 2002 3 29 UPS02437777 1 20020225 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 2360-S-18R STRINGER FOUND CRACKED. STRINGER REPAIRED AS PER SRM 5-10-03 FIG 4. 2 L 7 4 4F A20WE 2002032900041 20020329 00041 NM 2002 3 29 UPS02437779 1 20020226 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 1700-1720 S-8L STR FOUND CRACKED. BS 1710-1740 STR 8L REPAIRED AS PER SRM 53-10-03 FIG 4. 2 L 7 4 4F A20WE 2002032900042 20020329 00042 NM 2002 3 29 UPS02437780 1 20020228 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 2270-7780 RBL 80 LONGITUDINAL FLOOR SUPPORT FOUND CORRODED. FLOOR SUPPORT CHANNEL REPAIRED A S PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2002032900043 20020329 00043 NM 2002 3 29 UPS02437781 1 20020226 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D- BS 850 RBL 11 SEAT TRACK O/B FLANGE LOWER FACE CORRODED. 2 L 7 4 4F A20WE 2002032900044 20020329 00044 NM 2002 3 29 UPS02437782 1 20020225 A 5347 TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 760-780 RBL 10, TIE DOWN TRACK FLANGE FOUND CORROSION CRACK AS MARKED. TIE DOWN TRACK REPAIR ED AS PER SRM 53-10-05 FIG 14. 2 L 7 4 4F A20WE 2002032900045 20020329 00045 NM 2002 3 29 UPS02437783 1 20020224 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C FWD CARGO COMPT BS 800 S-43R STRINGER FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 01. 2 L 7 4 4F A20WE 2002032900046 20020329 00046 NM 2002 3 29 UPS02437784 1 20020226 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 770 LBL 33 SEAT TRACK FLANGE CORROSION CRACK. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1. 2 L 7 4 4F A20WE 2002032900047 20020329 00047 NM 2002 3 29 UPS02437785 1 20020226 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 770 RBL 75 SEAT TRACK O/B FLANGE CORROSION FOUND. SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 1 A. 2 L 7 4 4F A20WE 2002032900048 20020329 00048 NM 2002 3 29 UPS02437786 1 20020225 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 960 LBL 97 SEAT TRACK CROWN CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05. 2 L 7 4 4F A20WE 2002032900049 20020329 00049 NM 2002 3 29 UPS02437787 1 20020226 A 5320 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 1700 LBL 70-73 FLOORBEAM LWR CHORD SPLICE FOUND CRACK. CRACKED SPLICE REPLACED AS PER SRM 51 -10-01. 2 L 7 4 4F A20WE 2002032900050 20020329 00050 NM 2002 3 29 UPS02437788 1 20020226 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 1600-1620 RBL 11 SEAT TRACK I/B FLANGE FOUND CORRODED. SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 4. 2 L 7 4 4F A20WE 2002032900051 20020329 00051 NM 2002 3 29 UPS02437789 1 20020228 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 2140 S25L FRAME FOUND CRACK. FRAME REPAIRED AS PER SRM 51-40-03 FIG 02. 2 L 7 4 4F A20WE 2002032900052 20020329 00052 NM 2002 3 29 UPS02437790 1 20020228 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 2160 S25L FRAME FOUND CRACK. FRAME REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2002032900053 20020329 00053 NM 2002 3 29 UPS02437791 1 20020226 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - UPPER LOBE CROWN STRINGER END CRACKED AT BS 1955 - 1960 S-5R. STRINGER REPAIRED AS PER SRM 53-1 0-03 FIG 6. 2 L 7 4 4F A20WE 2002032900054 20020329 00054 NM 2002 3 29 UPS02437792 1 20020226 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - UPPER LOBE CROWN STRINGER END CRACKED AT BS 1955-1960 S-6R. STRINGER REPAIRED AS PER SRM 53-10- 03 FIG 6. 2 L 7 4 4F A20WE 2002032900055 20020329 00055 NM 2002 3 29 UPS02437793 1 20020228 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 2180 S25L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2002032900056 20020329 00056 NM 2002 3 29 UPS02437798 1 20020302 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 1935 LBL 98 SEAT TRACK CROWN FOUND CORROSION. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1. 2 L 7 4 4F A20WE 2002032900057 20020329 00057 NM 2002 3 29 UPS02437799 1 20020228 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 2340- 2360 STRINGER S44R FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002032900058 20020329 00058 NM 2002 3 29 UPS02437800 1 20020224 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C FWD CARGO COMPT BS 760 RBL 55 FLOOR SUPPORT FOUND CORRODED. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-0 4 FIG 1. 2 L 7 4 4F A20WE 2002032900059 20020329 00059 NM 2002 3 29 UPS02437801 1 20020301 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C FWD CARGO COMPT BS 760 S40R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2002032900060 20020329 00060 NM 2002 3 29 UPS02437804 1 20020228 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C AFT CARGO COMPT - BS 1600 LBL 2 TO RBL 2 FLOORBEAM UPPER CHORD CHAFED. FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2. 2 L 7 4 4F A20WE 2002032900061 20020329 00061 NM 2002 3 29 UPS02437805 1 20020304 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 895 RBL 33 SEAT TRACK HEAVY CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002032900062 20020329 00062 NM 2002 3 29 UPS02437806 1 20020225 A 5320 65B091912 FITTING BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C FWD CARGO COMPT - BS 960 RBL 25 LOCK END FITTING CORROSION DAMAGE AT LOW FACE I/B. LOCK END FITTING R EPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002032900063 20020329 00063 NM 2002 3 29 UPS02437807 1 20020304 A 5347 CARGO TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C FWD CARGO COMPT - BS 960 RBL 25 TRACK FLANGE FOUND CORRODED AFTER END FITTING REMOVED. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-21 FIG 5. 2 L 7 4 4F A20WE 2002032900064 20020329 00064 NM 2002 3 29 UPS02437809 1 20020227 A 5320 CHANNEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 2313 LBL 7 - RBL 15 HAT SECTION FOUND CORRODED. HAT SECTION REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002032900065 20020329 00065 NM 2002 3 29 UPS02437810 1 20020228 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 1940-1990 LBL 118 FLOOR SUPPORT FOUND CORROSION. FLOOR SUPPORT CHANNEL REPLACED AS PER SRM 5 1-10-01. 2 L 7 4 4F A20WE 2002032900066 20020329 00066 NM 2002 3 29 UPS02437811 1 20020227 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C FWD CARGO COMPT BS 840 S39R STRINGER CORRODED (AROUND RIVET AREA). STRINGER REPAIRED AS PER SRM 53-10 -03 FIG 1. 2 L 7 4 4F A20WE 2002032900067 20020329 00067 NM 2002 3 29 UPS02437812 1 20020225 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 240 RBL 30 SEAT TRACK CROWN FOUND CRACKED DUE HANDLING. SEAT TRACK REPLACED SRM 51-10-01. 2 L 7 4 4F A20WE 2002032900068 20020329 00068 NM 2002 3 29 UPS02437813 1 20020228 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 2120 S25L FRAME FOUND CRACK. FRAME REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2002032900069 20020329 00069 NM 2002 3 29 UPS02437815 1 20020311 A 5220 SEAL BOEING 747 747123 1384873 NM EXIT DOOR LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:PFLT RIGHT EMERGENCY EXIT DOOR LEAKING WATER, WATER DRIPPING FROM CEILING ON MAIN DECK, COMING FROM DOOR . CLEANED AND INSPECTED SEAL, NO DEFECTS NOTED. 2 L 7 4 4F A20WE 2002032900070 20020329 00070 NM 2002 3 29 UPS02437825 1 20020226 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 1920-1940, STR 22R WINDOW FORGING AREA FOUND CORROSION. REPAIRED STRINGER PER SRM 51-40-04 F IG 3. 2 L 7 4 4F A20WE 2002032900071 20020329 00071 NM 2002 3 29 UPS02437828 1 20020225 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE SCRATCHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 1780, S17-24R, FRAME I/B CHORD SEVERAL SCRATCH MARK FOUND. SCRATCH MARK SMOOTHED OUT AS PER SRM. FRAME REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2002032900072 20020329 00072 NM 2002 3 29 UPS02437829 1 20020301 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C AFT CARGO COMPT - BS 1880, LBL 30 FLOORBEAM CORROSION CRACKED. REPAIR FLOORBEAM PER SRM 51-40-04. 2 L 7 4 4F A20WE 2002032900073 20020329 00073 NM 2002 3 29 UPS02437830 1 20020226 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 1800-1820, STR 22R WINDOW FORGING AREA FOUND CORROSION. STRINGER REPAIR PER SRM 51-40-04. 2 L 7 4 4F A20WE 2002032900074 20020329 00074 NM 2002 3 29 UPS02437831 1 20020227 A 5210 SKIN BOEING 747 747123 1384873 NM L1 DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - L1 DOOR UPPER HINGE DOUBLER FOUND NON-STANDARD REPAIR. L1 DOOR UPPER HINGE CUTOUT SKIN REPAIRED PER S/B747-52-2144. 2 L 7 4 4F A20WE 2002032900075 20020329 00075 NM 2002 3 29 2002F00326 1 20020317 A 3350 D71702001 POWER SUPPLY BOEING 737 73783N 13844HI NM CABIN DISCHARGED G K NONE O OTHER IN INSP/MAINT 1 GL 11 316TZ 313 313 32609 DURING EMERGENCY LIGHT TEST FOUND LEFT AFT OVERWING EXIT LIGHT AND LEFT GROUND LIGHT AND LEFT MID BULLNOSE WOULD NOT TUR N OFF. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY M1670 IN ACCORDANCE WITH M/M 33-51-06-960. 2 L 7 2 4F RT A16WE 2002032900076 20020329 00076 WP 2002 3 29 02FDEA00219 1 20020326 A 3610 PERISEAL DOUG DC10 DC1030F 3023504 WP PNEUMATIC SYS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 314FE 48312 AFTER T/O NR 3 PNEU MANIFOLD FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED PERISEALS PER SMP. 2 L 7 3 4F RT A22WE 2002032900082 20020329 00082 NM 2002 3 29 ASAA0210049 1 20020205 A 3350 883200312 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEAT PALLET 7-4 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002032900083 20020329 00083 NM 2002 3 29 ASAA0240013 1 20020205 A 3397 8100022602 WIRE BOEING 737 7374Q8 138447Q NM LIGHTS DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 756AS 25097 SEA - DURING SERVICE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 18-20. RECONNECTED WIRING AT ROW 18 OPS NO RMAL. (M) 2 L 7 2 4F RT A16WE 2002032900084 20020329 00084 WP 2002 3 29 ASAA0280019 1 20020207 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP MID CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 OAK - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTS CONTROLLED BY POWER SUPPLY B5-27 WERE FOUND TO BE INOPERATIVE. RE PAIRED CHAFED WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002032900085 20020329 00085 WP 2002 3 29 ASAA0280025 1 20020208 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP FWD PAX ENTRY INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 27453 4981 53019 SEA - DURING LINE CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPRERATIVE. REPLACED PORTABLE LIGHT. OP TESTED OK. (M_ 2 L 7 2 4F RT A6WE 2002032900086 20020329 00086 NM 2002 3 29 02FDEA00221 1 20020326 A 5753 BACB10A35DDH BEARING BOEING 727 727233 138408A NM T/E FLAP FAILED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 281FE 22348 FLAPS ARE DIFFICULT TO MOVE IN OR OUT OF 2 DEG. REMOVED AND REPLACED OUTBOARD FLAPS CONTROL VALVE SUPPORT BRACKET BEARI NGS. FLAPS CHECK OK PER MM 27-51-051-4. 2 L 7 3 4F RT A3WE 2002032900087 20020329 00087 WP 2002 3 29 ASAA0280027 1 20020208 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP FWD PAX ENTRY INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING LINE CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AS SEMBLY. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002032900088 20020329 00088 WP 2002 3 29 ASAA0280028 1 20020209 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP FWD CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 PDX - DURING LINE CHECK, FIRST CLASS EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED EMERGENCY T RACK LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002032900089 20020329 00089 WP 2002 3 29 ASAA0280030 1 20020208 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP FWD CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 PDX - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTS IN 1ST CLASS SECTION WERE FOUND TO BE INOPERATIVE. REPLACED DAMAGED SECTION OF WIRING. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002032900090 20020329 00090 NM 2002 3 29 ABXA010804 1 20020327 A 2120 ODOR BOEING 767 767281 1385109 NM CABIN DETECTED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 769AX 22787 AT TAKEOFF AND THROUGHOUT CLIMB, THERE WAS AN OIL SMELL COMING FROM THE ENVIRONMENTAL SYSTEM. RAN BOTH PACKS ON GROUND, NO SMELL NOTICED. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2002032900091 20020329 00091 2002 3 29 ASAA0280053 4 20020222 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 SEA - DURNIG PRE-FLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2002032900092 20020329 00092 WP 2002 3 29 ABXA010805 1 20020327 A 5610 TRACK DOUG DC9 DC931 3022065 WP COCKPIT WINDOW LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 COULD NOT OPEN CAPTAIN'S SLIDING WINDOW. LUBED TRACK AND LOCKING MECHANISM. CAPTAIN'S CLEARVIEW WINDOW OPS CHECKED GOO D. 2 L 7 2 4F A6WE 2002032900093 20020329 00093 WP 2002 3 29 ASAA0280056 1 20020224 A 5312 BULKHEAD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OAK - DURING C-CHECK, FOUND CRACK DAMAGE AT THE LEFT LOWER CORNER OF THE FORWARD BULKHEAD AT FS 110 SITUATED IN THE NLG WHEEL WELL. INSTALLED REPAIR DOUBLER PER EA 5310-02068. (M) 2 L 7 2 4F RT A6WE 2002032900094 20020329 00094 WP 2002 3 29 ASAA0280057 1 20020226 A 5313 S936027511 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OAK - DURING C-CHECK, FOUND LONGERON 29R IN AFT CARGO BAY TO HAVE CORROSION AROUND FASTENER HOLES AT FS 1022-1025. INST ALLED U-CHANNEL REPAIR PER EA 5310-012066. (M) 2 L 7 2 4F RT A6WE 2002032900095 20020329 00095 NM 2002 3 29 ASAA0290001 1 20020201 A 3397 CIRCUIT BREAKER BOEING 737 737* NM CABIN SIDEWALL FAILED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 01 305AS 30013 SEA - DURING PUSHBACK FROM GATE, LEFT SIDE FORE AND AFT EXTERNAL OVERWING EMERGENCY LIGHTS (WITHIN THE SINGLE LIGHT ASSE MBLY) ILLUMINATED, WITH A CORRESPONDING INDICATION ON COCKPIT ANNUNCIATOR PANEL. REPLACED ASSOCIATED POWER SUPPLY CIRCU IT BREAKER. LIGHTS THEN FUNCTIONED PROPERLY. (M) 2 L 7 2 4F RT A16WE 2002032900096 20020329 00096 SO 2002 3 29 ASOA02115 1 20020227 A 3350 F02A250V1A LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 505AS 120279 DURING HANGAR INSPECTION IN MCN, THE OVERHEAD EMERGENCY LIGHT AT ROW 2 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN INOPERATIVE FUSE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002032900097 20020329 00097 EU 2002 3 29 ASOA02116 1 20020228 A 3350 OL3042BPE BULB AEROSP ATR72 ATR72212 8680945 EU CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 636AS 375 DURING A HANGAR INSPECTION IN MCN, THE EMERGENCY EXIT LIGHTED SIGN BY THE AIRSTAIR DOOR WAS BURNED OUT. MAINTENANCE REM OVED AND REPLACED THE BURNED OUT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002032900098 20020329 00098 WP 2002 3 29 ABXA010806 1 20020225 A 5320 9755584508 FITTING DOUG DC8 DC863 302198A WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 DURING C-CHECK, THE FITTING (P/N 9755584-508) WAS DAMAGED. R&R IAW REA D853-43051-MR AND FAA FORM 8110-3. 2 L 7 4 4F 4A25 2002032900099 20020329 00099 WP 2002 3 29 HALA0200045 1 20020215 A 2710 ACTUATOR DOUG DC10 DC1010 3022110 WP AILERON FAILED A HALA D RETURN TO BLOCK F N FLT CONT AFFECTED FALSE WARNING TX TAXI/GRND HDL 1 WP 13 128AA 46984 FLT 932 - HNL - DURING TAXI, FOUND LEFT AILERON NOT SHOWING FULL DEFLECTION ON SPI. REMOVED LEFT OUTBOARD ACTUATOR PER MM 27-13-02. INSTALLED LEFT OUTBOARD ACTUATOR PER MM 27-13-02 STEP 3B. FINISHED STEP 15-20. LVDT NULLED AND A/P ROLL FOR LVDT CHECK OK PER MM. (M) 2 L 7 3 4F A22WE 2002032900100 20020329 00100 NM 2002 3 29 USAA020009 1 20020110 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 46642 23312 PIT - FOUND AFT BULKHEAD 4 INCHES BY 1 INCH TOTAL DIMENSION, STATION 1016 BL 00 FORWARD END OF LOWER PRESSURE BULKHEAD S TIFFENER. REMOVED DAMAGE, INSTALLED MANUFACTURED REPAIR PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2002032900102 20020329 00102 NM 2002 3 29 USAA020019 1 20020111 A 5313 693535214 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND STRINGER TIES WITH TWO CRACKS .25 INCH, FS 380 STRINGER NR 1L AND NR 2L. REPLACED WITH IDENTICAL P/N PER SR M 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002032900103 20020329 00103 NM 2002 3 29 USAA020054 1 20020129 A 7120 310A102016 MOUNT BOEING 747 747* NM ENGINE SCORED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 23383 PIT - FOUND ENGINE MOUNT SCORING AND LUG CHAMFER BEARING LUG. BLENDED TO DEPTH .051, UNIT MPI ACCOMPLISHED. ROTOPEENED BLENDED AREA PER EA 73271. (M) 2 L 7 4 4F RT A20WE 2002032900104 20020329 00104 NM 2002 3 29 USAA020055 1 20020121 A 5313 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND SKIN CHAFED .5 INCH BY .5 INCH BY .5 INCH BY .25 INCH, STATION B06 BETWEEN S12L-8L. INSTALLED DOUBLER PER E A 73245. (M) 2 L 7 2 4F RT A16WE 2002032900105 20020329 00105 NM 2002 3 29 USAA020056 1 20020121 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND FRAME CRACKED TWO PLACES .5 INCH AND .25 INCH IN LENGTH, FRAME 663.75 AT 5.3R. REPAIRED WITH ANGLE DOUBLER AND STRINGER SPLICE PER SRM 53-00-07 FIG 209. (M) 2 L 7 2 4F RT A16WE 2002032900106 20020329 00106 NM 2002 3 29 USAA020057 1 20020213 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 CLT - FOUND CRACKED FRAME, STRAP WITH SHEARED FASTENER, BS 639 AND STRAP ABOVE STRINGER 17R. INSTALLED MANUFACTURED WEB PER EA 73163. (M) 2 L 7 2 4F RT A16WE 2002032900108 20020329 00108 NM 2002 3 29 USAA020058 1 20020206 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND FRAME CRACKED .5 INCH, FS 767 BETWEEN S8R-S9R A/C DUCT BRACKET RIVET HOLE. INSTALLED PLUGS PER TYPICAL REPA IR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002032900109 20020329 00109 NM 2002 3 29 USAA020059 1 20020206 A 5320 1122424 SPLICE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 23313 PIT - FOUND TWO STRINGER SPLICES CRACKED .125 INCH AND .25 INCH LONG, COMING FROM RIVET HOLES, STATION 907 54L. INSTALL ED NEW SPLICE PER 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002032900110 20020329 00110 NM 2002 3 29 USAA020060 1 20020206 A 5310 DOOR FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND INTERIOR DOOR FRAME SKIN CRACKED 1 INCH, STATION 950 S11R INTERIOR DOOR FRAME SKIN FOR AFT SERVICE DOOR. IN STALLED STRAP PER SRM 53-30-07 AND EA 73190. (M) 2 L 7 2 4F RT A16WE 2002032900111 20020329 00111 NM 2002 3 29 USAA020061 1 20020206 A 5310 DOOR FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 23313 PIT - FOUND INTERIOR DOOR FRAME SKIN 1 INCH CRAC, STATION 950, S11L INTERIOR AFT ENTRY DOOR FORWARD DOOR FRAME. INSTALL ED DOUBLER PER EA 73190, T/R 53-30-07A. (M) 2 L 7 2 4F RT A16WE 2002032900112 20020329 00112 WP 2002 3 29 ARWA20020310 1 20020321 A 2910 HYDRAULIC LINE DOUG DC8 DC863F 302198F WP HYD SYSTEM LEAKING A ARWA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 441J 45988 WHEN READY TO TAXI, HYDRAULIC QUANTITY GAUGE INDICATED LOSS OF FLUID, HYDRAULIC PRESSURE GAUGE INDICATED LOSS OF PRESS. ACCOMPLISHED APPROPRIATE CHECKLIST, RETURNED TO RAMP. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE FROM NR 3 ENGINE HY DRAULIC PUMP, OPS CHECK AND LEAK CHECK NORMAL IAW MM 29-10-12. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002032900113 20020329 00113 NM 2002 3 29 USAA020062 1 20020206 A 5310 1122422 SPLICE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND STRINGER SPLICE CRACKED .125 INCH AND .25 INCH, COMING FROM RIVET HOLES, STATION 907 54R. INSTALLED SPLICE PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002032900114 20020329 00114 NM 2002 3 29 USAA020063 1 20020206 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND FRAME CRACKED .25 INCH, STATION 827 BETWEEN 58L AND 59L A/C DUCT BRACKET RIVET HOLE. MANUFACTURED AND INSTA LLED ANGLE PER T/R 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002032900115 20020329 00115 NM 2002 3 29 USAA020064 1 20020206 A 5320 CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND SUPPORT CLIP CRACKED .1875 INCH IN RADIUS, STATION 294.5 S-7L SUPPORT ATTACH TO AFT SIDE OF FRAME. INSTALLE D DOUBLER PER SRM 51-70-12. (M) 2 L 7 2 4F RT A16WE 2002032900116 20020329 00116 NM 2002 3 29 USAA020065 1 20020204 A 5310 69719477 WINDOW FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND WINDOW FRAME CRACKED .5 INCH, UPPER AFT CORNER OF COCKPIT WINDOW 1L FRAME. ROUTED CRACK, NDT'D AND INSTALLE D DOUBLER PER SRM 53-10-01. (M) 2 L 7 2 4F RT A16WE 2002032900117 20020329 00117 NM 2002 3 29 USAA020066 1 20020204 A 5310 69719478 WINDOW FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND WINDOW FRAME CRACKED .5 INCH, UPPER AFT CORNER OF COCKPIT WINDOW 1R FRAME. CRACK ROUTED, AND DOUBLER INSTAL LED AFTER NDT PER SRM 53-10-01. (M) 2 L 7 2 4F RT A16WE 2002032900118 20020329 00118 NM 2002 3 29 USAA020067 1 20020123 A 5710 65C3649221 BEAM BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND LEFT MLG BEAM SUPPORT WITH TWO CRACKS MERGED INTO ONE AT 1.5 INCH LONG, RT MLG BEAM SUPPORT FTG TOP FASTENER INBOARD OF BEAM. REPLACED FITTING PER BOEING SB 737-57-1216 REV 2 DATED 2/6/99. (M) 2 L 7 2 4F RT A16WE 2002032900119 20020329 00119 NM 2002 3 29 USAA020068 1 20020123 A 5740 65C3649221 FITTING BOEING 737 7373B7 1384580 NM WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 47034 23313 PIT - FOUND LEFT MLG BEAM SUPPORT FITTING 1 INCH LONG VERTICAL CRACK, TOP INBOARD FASTENER FROM BEAM PIN SLOT TO FTG EDG E. REPLACED FITTING PER BOEING SB 737-57-1216 REV 2 DATED 5/6/99 AND EA 73242. (M) 2 L 7 2 4F RT A16WE 2002032900120 20020329 00120 NM 2002 3 29 USAA020069 1 20020211 A 5320 1137848 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 782AU 31460 25021 PIT - FOUND RIGHT SKATE ANGLE WORN THROUGH ANGLE FRETTING, RIGHT SIDE VERTICAL FIN TO FUSELAGE SKATE ANGLE. PART REPLAC ED WITH IDENTICAL P/N TYPICAL REPAIR 53-20-05A. (M) 2 L 7 2 4F RT A16WE 2002032900121 20020329 00121 NM 2002 3 29 USAA020070 1 20020124 A 5310 DOUBLER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 392US 23314 PIT - FOUND DOUBLER CRACKED .5 INCHES AREA AND 1 INCH AREA BENT, LIP FOR A/C DOOR, STATION 490 BL 0. INSTALLED DOUBLER PER TR 53-30-05 AND EA 73180. (M) 2 L 7 2 4F RT A16WE 2002040300130 20020403 00130 WP 2002 4 3 ARWA20020311 1 20020324 A 7711 LINE DOUG DC8 DC862 3021970 WP PT 2 LEAKING A ARWA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 19 8969U 46070 DURING CLIMBOUT NR 1 ENGINE FAILED TO PRODUCE APPROPRIATE POWER ALL OTHER ENGINE PARAMETERS NORMAL, PROCEEDED WITH ABNO RMAL CHECKLIST AND LANDED WITH NO FURTHER INCIDENTS. PREFORMED EPR CHECK IAW MM 77-11-0, FOUND PT-2 LINE OBSTRUCTED AT INLET GUIDE VANE CASE. PERFORMED ENGINE RUN-UP IAW MM 71-00, ALL OTHER PARAMETERS CHECKED NORMAL. TRANSFERRED EPR INDIC ATION TO DMI 16369 PER MEL 77-1-2. CHECKED NR 1 ENGINE EPR. LINES FOR LEAK; FOUND PT2 LINE LEAKING. REMOVED AND REPL ACED PT2 RIGID LINE IAW MM 70-30-3 & MM 70-11-0. PERFORMED ENGINE RUN-UP, TAKE OFF POWER FOUND NORMAL IAW DC8 MM 71-00 CLEARED DMI 16369. 2 L 7 4 4F 4A25 2002032900122 20020329 00122 NM 2002 3 29 USAA020071 1 20020124 A 5320 WEB BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 392US 46617 23314 FOUND SUPPORTS AND WEB CORRODED 36 INCHES BY 3 INCHES AREA, STATION 300-340 MAIN ENTRY THRESHOLD. CORROSION LEVEL 2, TA SK NR C53-107-0. REMOVED AND REPLACED SUPPORTS AND WEB PER SRM 53-10-15. (M) 2 L 7 2 4F RT A16WE 2002032900123 20020329 00123 NM 2002 3 29 USAA020072 1 20020123 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 32053 24934 PIT - FOUND FRAME CRACKED .125 INCH, FRAME 867 BETWEEN S8R AND S9R. INSTALLED DOUBLER REPAIR PER TYPICAL REPAIR 53-10-1 4. (M) 2 L 7 2 4F RT A16WE 2002032900124 20020329 00124 NM 2002 3 29 AT0200038 1 20020319 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 972AT 55033 LOWER EMERGENCY EXIT SIGN AT AFT FLIGHT ATTENDANT STATION DOES NOT ILLUMINATE. OVERWING EMERGENCY EXIT LIGHTS INOP. RE MOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK ASSY AT FS 879R IAW B717 MM 33-51-03, OPS CHECK NORMAL. RESEATED CAN NON PLUG ON B5-125 BATTERY PACK, OPS CHECK GOOD PER B717 AMM 33-51. 2 L 7 2 4F TR A6WE 2002032900125 20020329 00125 NM 2002 3 29 USAA020074 1 20020215 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 45478 23318 CLT - FOUND SKIN CRACKED 2 INCHES, SKIN AT S19R, BS 753-755, SECTION 46. INSTALLED DOUBLER PER SRM 53-00-01, FIG 225 AN D STRINGER REPAIR CHANNEL PER 53-00-03 PAGE 213. (M) 2 L 7 2 4F RT A16WE 2002032900126 20020329 00126 NM 2002 3 29 USAA020075 1 20020213 A 5311 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 37141 23988 CLT - FOUND SKIN CRACKED 1.25 INCH CRACK, 3 INCH AFT OF FS 727E JUST BELOW S22L. INSTALLED DOUBLER PER BOEING SRM 53-00 -01, FIG 201. (M) 2 L 7 2 4F RT A16WE 2002032900128 20020329 00128 WP 2002 3 29 AT0200039 1 20020323 A 3397 WIRE DOUG DC9 DC932 3022066 WP TAIL CONE CUT A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 CONE HANDLE EMERGENCY PATH LIGHT AND FORWARD CATWALK, EMERGENCY PATH LIGHT WIRES WERE CUT OFF. REPAIRED WIRES L9045-20, L9054-20N, L9049-20 AND L9057-20N AT CONE HANDLE EMERGENCY PATH LIGHT AND FORWARD CATWALK EMERGENCY PATH LIGHT IAW WDM 33-51-03 AND MM 20-50-1. OPS CHECK NORMAL IAW MM 33-50. 2 L 7 2 4F A6WE 2002032900129 20020329 00129 NM 2002 3 29 USAA020081 1 20020123 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 32053 24934 PIT - FOUND FRAME CRACKED .5 INCH, FRAME STATION 867 BETWEEN S8L AND S9L. INSTALLED DOUBLER REPAIR PER TYPICAL REPAIR 5 3-10-14. (M) 2 L 7 2 4F RT A16WE 2002032900130 20020329 00130 2002 3 29 AT0200040 4 20020326 A 2565 13621228 SLIDE DOUG DC9 DC932 3022066 WP TAILCONE UNSERVICEABLE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 847AT 47555 DURING SERVICE CHECK FOUND TAIL CONE EVACUATION SLIDE PRESSURE LOW. REMOVED AND REPLACED EVACUATION SLIDE IAW DC9 MM 25 -62. 2 L 7 2 4F A6WE 2002032900131 20020329 00131 NM 2002 3 29 USAA020082 1 20020123 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 32053 24934 PIT - FOUND FRAME CRACKED .125 INCH, FRAME 747 BETWEEN S8L AND S9L. DOUBLER REPAIR INSTALLED PER TYPICAL REPAIR 53-10-1 4. (M) 2 L 7 2 4F RT A16WE 2002032900132 20020329 00132 WP 2002 3 29 AT0200042 1 20020326 A 2530 ODOR DOUG DC9 DC932 3022066 WP GALLEY DETECTED A ZZDA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 15 846AT 47226 STRONG ACIDIC SMELL FROM GALLEY AREA, COFFEE MAKER ON FORWARD SIDE OF AIRCRAFT RIGHT. TURNED GALLEY POWER OFF, SMELL DI SSIPATE. REMOVED ALL 3 COFFEE MAKERS AND INSPECTED WIRING TO EACH, NO DISCREPANCIES NOTED. INSPECTED ALL WIRING INSIDE FORWARD GALLEY, NO FAULTS NOTED, LEFT GALLEY POWER ON FOR EXTENDED PERIOD OF TIME AFTER THOROUGHLY CLEANING ENTIRE FORW ARD GALLEY, NO ACIDIC SMELL OR OTHER DISCREPANCIES NOTED. AIRCRAFT OKAY FOR SERVICE. 2 L 7 2 4F A6WE 2002032900135 20020329 00135 NM 2002 3 29 USAA020106 1 20020217 A 5320 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 392US 46617 23314 PIT - FOUND ANGLE CRACKED 2 INCHES, FORWARD OF STATION 345. REPLACED ANGLE PER SRM 31-70-12. (M) 2 L 7 2 4F RT A16WE 2002032900136 20020329 00136 NM 2002 3 29 USAA020107 1 20020217 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 392US 46617 23314 PIT - FOUND SKIN CRACKED 2.75 INCH, STATION 727E PLUS 3 INCHES AT S18R. INSTALLED DOUBLER PER SRM 53-00-01 AND 51-20-05 . (M) 2 L 7 2 4F RT A16WE 2002032900137 20020329 00137 NM 2002 3 29 USAA020108 1 20020217 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 392US 46617 23314 PIT - FOUND WEB BROKEN IN HALF, MAIN FRAME BROKE IN HALF STATION 639 FLOOR LEVEL. REMOVED AND REPLACED WEB PER EA 73114 . (M) 2 L 7 2 4F RT A16WE 2002032900138 20020329 00138 WP 2002 3 29 USAAD02010 1 20020219 A 3350 9721055 LIGHT DOUG DC9 DC981 3022081 WP PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 827US 48049 IND - SEVERAL SEAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2002032900139 20020329 00139 WP 2002 3 29 USAAD02011 1 20020222 A 3350 LIGHT DOUG DC9 DC981 3022081 WP FUSELAGE INOPERATIVE A USAA O OTHER O OTHER LD LANDING 1 EA 19 826US 48026 PIT - THE EMERGENCY LIGHT AT THE 1-R DOOR CAME ON LANDING. MAINTENANCE CHECK THE EMERGENCY LIGHT OPERATION, ALL CHECKED NORMAL. REPLACED THE EMERGENCY LIGHT BATTERY AS PRECAUTION. (M) 2 L 7 2 4F A6WE 2002032900140 20020329 00140 EU 2002 3 29 USAASA02022 1 20020215 A 3397 CONNECTOR AIRBUS A319 A319112 3930323 EU CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 727UW 1147 TPA - THE CABIN INTERCOMMUNICATION DATA SYSTEM DISPLAYED, "EPSU EXT LOAD AFT L", ATER THE EMERGENCY LIGHTS TEST WAS PERF ORMED. MAINTENANCE RESEATED THE SLIDE PACK LIGHTS CONNECTOR PLUG ON THE REAR SERVICE DOOR. EMERGENCY LIGHTS SYSTEM CHE CKS OK. (M) 2 L 7 2 4F RT A28NM 2002032900142 20020329 00142 NM 2002 3 29 USAASB02033 1 20020216 A 2133 327375 REGULATOR VALVE BOEING 737 7373B7 1384580 NM E/E COMPT FAILED A USAA B EMER. DESCENT O OTHER CR CRUISE 1 EA 19 518AU 293 23704 IND - FLT 866 - DURING CRUISE, EN ROUTE FROM CLT TO IND, CREW WAS UNABLE TO MAINTAIN CABIN PRESSURE IN AUTO MODE. CREW DESCENDED AIRCRAFT TO FL140 AND SWITCHED TO MANUAL PRESSURIZATION MODE TO KEEP CABIN WITHIN LIMITS. PASSENGERS WERE UNA WARE OF PRESSURIZATION PROBLEM. FLIGHT CONTINUED ONTO IND AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLAR ED. MAINTENANCE REMOVED AND REPLACED THE PRESSURE REGULATOR VALVE. PRESSURIZED AIRCRAFT. OPERATIONAL CHECK GOOD PER M M 21-58-31. (M) 2 L 7 2 4F RT A16WE 2002032900143 20020329 00143 NM 2002 3 29 USAASB02034 1 20020217 A 5210 69215961A SEAL BOEING 737 7373B7 1384580 NM FWD ENTRY DOOR LEAKING A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 518AU 23704 DAY - FLT 498 - EN ROUTE FROM PIT-MCI, AT FL280, THE CABIN STARTED CLIMBING AT 1,800 FEET PER MINUTE. AFTER DESCENDING TO FL140, CREW WAS ABLE TO GAIN CONTROL OF CABIN. FLIGHT DIVERTED TO DAY AND LANDED WITHOUT FURTHER INCIDENT. NO EMERG ENCY WAS DECLARED. CREW ALSO REPORTED A LOUD AIR LEAK AT THE FORWARD ENTRY DOOR. MAINTENANCE FOUND THE FORWARD ENTRY D OOR UPPER HINGE FLAP ROLL PIN FELL OUT. REINSTALLED PIN AND STAKED THE ENDS. INSTALLED TORQUE SEAL, RAN ENGINE AND PRE SURIZED AIRCRAFT. NO LEAKS NOTED. HOWEVER, THE FOLLOWING DAY, A LOUD SQUEAL/AIR LEAK WAS HEARD FROM THE FORWARD ENTRY DOOR DURING TAKEOFF AND AGAIN ON DESCENT AND LANDING. MAINTENANCE REMOVED AND REPLACED THE UPPER HINGE ARM COVER FLAP/S 2 L 7 2 4F RT A16WE 2002032900144 20020329 00144 NM 2002 3 29 USAASB02038 1 20020223 A 3260 189929 DOWNLOCK BOEING 737 7374B7 1384702 NM LT MLG OUT OF ADJUST A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 444US 24862 PBI - FLT 942 - ON PREPARATION FOR LANDING AT PBI, EN ROUTE FROM PIT, CRWE DID NOT RECEIVE A GREEN LIGHT FOR THE LEFT ML G WHEN GEAR WAS LOWERED. CREW CYCLED GEAR HANDLE BACK TO OFF AND THEN DOWN WITH NO HELP. CREW THEN CYCLED GEAR HANDLE TO UP AND THEN BACK DOWN AND RECEIVED GREEN LIGHT BUT THE RED INTRANSIT LIGHT REMAINED ILLUMINATED. FLIGHT LANDED WITHO UT FURTHER INCIDENT. MAINTENANCE FOUND RESISTANCE ON BLUE TO GROUND LEG OF LEFT MAIN LANDING GEAR S71 DOWNLOCK SENSOR O UT OF LIMITS. REMOVED AND REPLACED S71 SENSOR PER MM 32-61-31. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002032900146 20020329 00146 NM 2002 3 29 USAASB02039 1 20020223 A 3260 189929 SENSOR BOEING 737 7374B7 1384702 NM MLG INTERMITTENT A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 434US 24556 PHL - FLT 1186 - DURING CRUISE, EN ROUTE FROM PHL TO ALB, CREW REPORTED THE TAKEOFF WARNING HORN BEGAN SOUNDING AND COUL D NOT BE SILENCED. FLIGHT RETURNED TO FIELD AT PHL WITH NO EMERGENCY DECLARED. CREW REPORTED THE AUTO BRAKE WOULD NOT ARM AND THE SPEED BRAKE DID NOT DEPLOY ON LANDING. MAINTENANCE REMOVED AND REPLACED THE R280 RELAY. OPERATIONAL CHECK GOOD. HOWEVER, THE AIRCRAFT ENCOUNTERED THE SAME PROBLEM THE FOLLOWING DAY. ONLY DIFFERENCE WAS THAT THE SPEED BRAKE D ID DEPLOY ON LANDING AND THE CIRCUIT BREAKER TO THE AURAL WARNING WAS PULLED. MAINTENANCE FOUND THE S106 AIR SAFETY SEN SOR INTERMITTENT, INDICATING AIRCRAFT ON GROUND WHILE IN FLIGHT. REMOVED AND REPLACED S106 AIR SAFETY SENSOR PER MM 32- 2 L 7 2 4F RT A16WE 2002032900147 20020329 00147 NM 2002 3 29 USAASB02040 1 20020223 A 5610 5717623115 WINDOW BOEING 737 7373B7 1384580 NM COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 529AU 38798 24411 CLT - FLT 1145 - EN ROUTE FROM PHL-RSW, AT FL350, THE CAPTAINS SLIDING WINDOW OUTER PANE CRACKED. CREW ACCOMPLISHED QUI CK REF HANDBOOK PROCEDURES AND DUE TO THE ICING CONDITIONS IN FLORIDA, THE FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FUR THER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS SLIDING WINDOW AND AS A PRECAU TIONARY MEASURE, THEY REPLACED THE WINDOW HEAT CONTROLLER (P/N 231-2). OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002032900150 20020329 00150 SO 2002 3 29 SWIA200210655 1 20020209 A 6123 RELAY EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 289YV 120289 ON TAKEOFF ROLL AT APPROXIMATELY 70 KIAS, AUTO FEATHER AURAL WARNING AND TRIPLE CHIME. TAKEOFF WAS ABORTED. AUTO FEATH ER SWITCH WAS ON AND TRIM SET TO 28 PERCENT (MIDDLE OF GREEN BAND). PROP AUX FEATHER AND MANUAL FEATHER TESTS WERE NORM AL DURING TAXI. FUNCTION CHECKED PLA S0299 & S0300 POWER LEVER MICRO SWITCHES. REMOVED AND REPLACED RELAY K0161 ARM RE LAY. OPS CHECKED PER MEL 61-23-00. OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2002032900153 20020329 00153 SO 2002 3 29 SWIA200210666 1 20020225 A 2400 RELAY EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE ELECTRICAL SYS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 137H 120137 TEN MINUTES AFTER TAKEOFF, RIGHT TORQUE DROPPED TO ZERO AND POWER OFF AND APU LIGHT ILLUMINATED ON ANNUNCIATOR PANEL. A PU WAS OFF. RETURNED TO SBA. REPLACED RELAY K0397 WITH SERVICEABLE UNIT. RAN AIRCRAFT FOR 45 MINUTES. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2002032900157 20020329 00157 2002 3 29 SWIA200210682 4 20020208 A 2210 MODULE CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS DEFECTIVE A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 442SW 7609 NR 2 YAW DAMPER WILL NOT STAY ENGAGED. REPLACED LEFT AND RIGHT LIGHTNING/HIRF MODULES IAW CL600 MM 22-12-03. CAT II P/ N ON (LT) 822-0287-401, S/N OFF GR8M (RT), P/N ON 822-0332-401, S/N OFF GXTM. 2 L 7 2 4F RT A21EA 2002032900159 20020329 00159 EA 2002 3 29 SWIA200210683 1 20020228 A 4940 POTENTIOMETER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU MALFUNCTIONED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 913SW 7597 APU AUTO SHUTDOWN ON THE INITIATION OF TAKEOFF ROLL. ABORTED TAKEOFF AND TAXIED AIRCRAFT BACK TO THE GATE. FOUND APU D OOR POTENTIOMETER BAD. INSTALLED NEW POTENTIOMETER IAW 49-14-01. RIGGED DOOR AND RAN APU. ALL CHECKS OK AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 2002032900161 20020329 00161 EA 2002 3 29 SWIA200210684 1 20020228 A 2760 4916405 ECU CNDAIR CL600 CL6002B19 1900309 EA SPOILERON MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 426SW 3977 1120 7468 LEFT SPOILERON FAULT STATUS MESSAGE. INSTALLED SERVICEABLE SECU IN NR 2 POSITION IAW CRJ MM 27-61-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002032900166 20020329 00166 EA 2002 3 29 SWIA200210685 1 20020226 A 2761 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 426SW 7468 ON TAXI OUT SPOILERON FAULT STATUS MESSAGE CAME ON WITH THE LEFT SPOILERON INDICATING WHITE BOX/NOX. INSTALLED NEW PCU ON LEFT SPOILERON INBOARD POSITION IAW CRJ MM 27-62-01. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2002032900167 20020329 00167 NM 2002 3 29 COOSDR020041 1 20020301 A 5320 FLANGE BOEING 727 727231 1384079 NM LT AC EQUIP BAY CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 64347 21634 LEFT A/C EQUIPMENT BAY, FLANGE CRACKED. 2 L 7 3 4F A3WE 2002032900168 20020329 00168 NM 2002 3 29 COOSDR020042 1 20020301 A 4920 FLANGE BOEING 727 7272F9 138407D NM APU TURBINE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 APU TURBINE ASSEMBLY EXHAUST FLANGE CRACKED. 2 L 7 3 4F RT A3WE 2002032900169 20020329 00169 NM 2002 3 29 COOSDR02033 1 20020301 A 5330 SKIN BOEING 727 7272F9 138407D NM FUSELAGE CORRODED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 LOWER FUSELAGE SKIN BS 950F+10.0 INCHES, S-27R AND 28R, SKIN WITH CORROSION. 2 L 7 3 4F RT A3WE 2002032900170 20020329 00170 NE 2002 3 29 SWIA200210686 3 20020228 A 6140 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 393SW 120330 ABORTED TAKEOFF DUE TO AUTOFEATHER AURAL WARNING. STATIC TAKEOFF WAS ATTEMPTED WITH AUTOFEATHER ARMED AND THE POWER LEV ERS ADVANCED AS QUICKLY AS POSSIBLE. PERFORMED EXTENSIVE GROUND RUNS OF BOTH ENGINES WITH EEC'S ON AND OFF. COULD NOT DUPLICATE AUTOFEATHER AURAL WARNINGS. 2 L 7 2 4T RT A31SO 6 C P11NE 2002032900171 20020329 00171 NM 2002 3 29 COOSDR02034 1 20020301 A 5730 6521655 PANEL BOEING 727 7272F9 138407D NM RT WING DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 RIGHT WING, TRAILING EDGE PANEL (PN: 65-21655) DELAMINATED. 2 L 7 3 4F RT A3WE 2002032900172 20020329 00172 NM 2002 3 29 COOSDR02035 1 20020301 A 5730 6521657245 PANEL BOEING 727 7272F9 138407D NM LT WING DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 LEFT WING, TRAILING EDGE UPPER FIX PANEL (PN 65-21657-245) DELAMINATED. 2 L 7 3 4F RT A3WE 2002032900173 20020329 00173 EA 2002 3 29 SWIA200210687 1 20020227 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR NOT SEATED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 423SW 7456 PASSENGER DOOR STOW MESSAGE. RECYCLED DOOR BUT MESSAGE WILL NOT CLEAR. FOUND OUTER HANDLE NOT FULLY LATCHING. REMOVED PASSENGER DOOR OUTER HANDLE AND CLEANED HANDLE BOX OF BURRS. RESEALED AND REINSTALLED HANDLE. OPS CHECKED DOOR OPERAT ION SEVERAL TIMES. OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2002032900174 20020329 00174 NM 2002 3 29 COOSDR02036 1 20020301 A 5311 FRAME BOEING 727 7272F9 138407D NM FUSELAGE CORRODED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 MAIN LANDING GEAR WHEEL WELL, BS 950 CANTED BULKHEAD LOWER TEE CHORD CORRODED. 2 L 7 3 4F RT A3WE 2002032900175 20020329 00175 NM 2002 3 29 COOSDR02040 1 20020301 A 5730 6521655477 PANEL BOEING 727 7272F9 138407D NM LT WING T/E CORRODED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 LEFT WING, TRAILING EDGE UPPER FIX PANEL (PN 65-21655-477) CORRODED. 2 L 7 3 4F RT A3WE 2002032900176 20020329 00176 NM 2002 3 29 COOSDR02043 1 20020301 A 5314 FLANGE BOEING 727 7272F9 138407D NM KEEL BEAM CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 LOWER FUSELGAE - FROM BS 740 TO BS 742, RBL 5.0" KEEL BEAM INBOARD FLANGE CRACKED. 2 L 7 3 4F RT A3WE 2002032900177 20020329 00177 SO 2002 3 29 C2XA02CL086 1 20020328 A 2770 S0657 SWITCH EMB 145 EMB145LR 3260212 SO OUT OF ADJUST A C2XA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 27 16541 145542 EWR-STL FLIGHT#3543 THE CREW REPORTED A GUST LOCK LIGHT ILLUMINATED IN FLIGHT.THE AIRCRAFT DIVERTED INTO CLEVELAND AND L ANDED WITHOUT FURTHER INCIDENT.ON TOCHDOWN THE MESSAGE CLEARED.MAINTENANCE INSPECTED AND ADJUSTED THE LEFT SPRING CARTRI DGE POSITION MICROSWITCH FOR THE ELECTROMECHANICAL GUST LOCK SYSTEM.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEAS ED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002032900178 20020329 00178 WP 2002 3 29 COOSDR02044 1 20020301 A 5315 FLOORBEAM DOUG DC8 DC863 302198A WP FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 MAIN CARGO CABIN - STA Y=1600-FLOOR BEAM UPPER CHORD CRACKED. 2 L 7 4 4F 4A25 2002032900179 20020329 00179 WP 2002 3 29 COOSDR02045 1 20020301 A 5230 DOUBLER DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 SECTION 43 - CARGO DOOR DOUBLER CRACKED, AT STA Y=270.000, LONG 21L. 2 L 7 4 4F 4A25 2002032900180 20020329 00180 SO 2002 3 29 SWIA200210688 1 20020224 A 2750 3472001001 COMPUTER EMB 120 EMB120ER 3260203 SO T/E FLAP MALFUNCTIONED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 232SW 2851 1059 120306 WHEN SETTING FLAPS TO 15 DEGREES FOR TAKEOFF, FLAP/CONTROL FAULT ILLUMINATED AND WILL NOT RESET. REPLACED THE FLAP COMP UTER WITH A SERVICEABLE UNIT. OPS CHECK OF FLAP SYSTEM IS NORMAL. 2 L 7 2 4T RT A31SO 2002032900181 20020329 00181 SO 2002 3 29 SWIA200210689 1 20020218 A 5247 ACCESS PANEL EMB 120 EMB120ER 3260203 SO APU MISSING A SWIA K NONE P NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 584SW 120352 APU ACCESS PANEL MISSING UPON ARRIVAL AT SLC. INSTALLED SERVICEABLE PANEL ASSEMBLY AS NEEDED. P/N ON 145-33351-401. 2 L 7 2 4T RT A31SO 2002032900182 20020329 00182 EA 2002 3 29 SWIA200210690 1 20020226 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DEFECTIVE A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 423SW 7456 OUTER DOOR HANDLE HARD TO STOW. REMOVED AND REPLACED OUTER DOOR HANDLE IAW MM 52-11-03. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002032900183 20020329 00183 WP 2002 3 29 ARWA20020312 1 20020326 A 3260 801801 PROXIMITY SWITCH DOUG DC8 DC861 3021952 WP A ARWA O K OTHER NONE J WARNING INDICATION CR CRUISE 1 SO 19 29UA 46159 LOG PAGE # 108372. DISCREPANCY: GEAR NOT LATCHED, DOOR NOT LATCHED, LIGHTS ILLUMINATED. ON LEFT MAIN LANDING GEAR NO D OWN LIGHTS. CORRECTIVE ACTION: REMOVED AND INSTALLED LEFT MAIN GEAR PROXIMITY SWITCH SENSOR. ACCOMPLISHED ADJ & TEST P OSITION & WARNING SYSTEM IAW MM 32-60-0. ALL NORMAL. 2 L 7 4 4F 4A25 2002032900184 20020329 00184 EA 2002 3 29 SWIA200210691 1 20020222 A 2425 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 408SW 7055 ON TAKEOFF AT ABOUT 50 KTS, EXPERIENCED AN ACCESS BUS CAUTION MESSAGE AND ABORTED THE TAKEOFF. AFTER PULLING OFF THE RU NWAY, ALL SYSTEMS APPEARED NORMAL EXCEPT LEFT AND RIGHT AOA HEAT. POWERED DOWN AND POWERED UP AIRCRAFT AND ALL SYSTEMS SEEM NORMAL. DEPOWERED PLANE AND RESET. COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4F RT A21EA 2002032900185 20020329 00185 SO 2002 3 29 SWIA200210692 1 20020228 A 2731 SPLICE EMB 120 EMB120RT 3260202 SO ELEVATOR TRIM FAULTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 1117H 120117 ON TAKEOFF WITH TRIM SET IN THE GREEN BAND, RECEIVED A TAKEOFF TRIM AURAL WARNING. ABORTED THE TAKEOFF PER THE SOP AND TAXIED CLEAR. TESTED THE SYSTEM TWICE AND RECEIVED THE SAME WARNING. RETURNED TO THE GATE AND DEPOWERED THE AIRCRAFT. POWERED UP AND TESTED THE SYSTEM AGAIN AND IT TESTED OK. FOUND BAD SPLICE AT ELEVATOR TRIM RIGHT PROXIMITY SENSOR. RE PAIRED IAW MM 20-21-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002032900186 20020329 00186 SO 2002 3 29 SWIA200210693 1 20020227 A 3150 RELAY EMB 120 EMB120RT 3260202 SO COCKPIT FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 137H 120137 ON TAKEOFF ROLL, AMBER APU LIGHT AND AMBER POWER OFF LIGHT ILLUMINATED AND LEFT TORQUE GAUGE DROPPED TO ZERO. REPLACED RELAYS K129, K149, CB0266 AND WIRE W200-0214-24 WITH SERVICEABLE UNITS. RAN ENGINES. OPS CHECKS GOOD. NO DISCREPANCIE S NOTED AT THIS TIME. 2 L 7 2 4T RT A31SO 2002032900187 20020329 00187 SO 2002 3 29 SWIA200210694 1 20020227 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 196SW 120151 INBOARD FLAPS FAILED AT 5 DEGREES DOWN. CONTROL FAULT WILL NOT RESET. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW RII 27-307, OPS CHECK GOOD, NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2002032900189 20020329 00189 NM 2002 3 29 COOSDR010129 1 20020301 A 5753 65216351 SKIN BOEING 727 7272M7 138407S NM LT WING FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 LEFT WING OUTBOARD AFT FLAP UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900190 20020329 00190 NM 2002 3 29 COOSDR010130 1 20020301 A 5755 65178487 SKIN BOEING 727 7272M7 138407S NM NR 8 SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING SPOILER NR 8 UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900191 20020329 00191 NM 2002 3 29 COOSDR010131 1 20020301 A 5753 6524638188 SKIN BOEING 727 7272M7 138407S NM TE FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING OUTBOARD MID FLAP TRAILING EDGE UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900192 20020329 00192 NM 2002 3 29 COOSDR010132 1 20020301 A 5753 6521634147 SKIN BOEING 727 7272M7 138407S NM TE FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 LEFT WING INBOARD AAFT FLAP UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900193 20020329 00193 NM 2002 3 29 COOSDR010133 1 20020301 A 5753 6524691136 SKIN BOEING 727 7272M7 138407S NM RT IB MID FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING INBOARD MID FLAP TRAILING EDGE, UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900194 20020329 00194 NM 2002 3 29 COOSDR010134 1 20020301 A 5753 65216352 SKIN BOEING 727 7272M7 138407S NM RT OB AFT FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING OUTBOARD AFT FLAP, UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900195 20020329 00195 NM 2002 3 29 COOSDR010135 1 20020301 A 5753 6524638187 SKIN BOEING 727 7272M7 138407S NM LT OB MID FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 LEFT WING OUTBOARD MID FLAP TRAILING EDGE, UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900196 20020329 00196 NM 2002 3 29 COOSDR010136 1 20020301 A 5753 6524691135 SKIN BOEING 727 7272M7 138407S NM LT IB MID FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 LEFT WING INBOARD MID FLAP TRAILING EDGE UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002042400072 20020424 00072 NM 2002 4 24 SABA020041 1 20020329 A 3350 1005511 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 882CC 168 AIRCRAFT 882 ON FLIGHT 5114 FROM OAJ TO CLT. DURING PREFLIGHT INSPECTION AN OVERHEAD EMERGENCY LIGHT FAILED TO TEST. M AINTENANCE REMOVED AND REPLACED BULBS IN THE OVERHEAD EMERGENCY LIGHT. SYSTEM OPS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002032900197 20020329 00197 NM 2002 3 29 COOSDR010137 1 20020301 A 5751 652172634 SKIN BOEING 727 7272M7 138407S NM RT OB AILERON DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING OUTBOARD AILERON TAB UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900198 20020329 00198 NM 2002 3 29 COOSDR010138 1 20020301 A 5751 652173629 SKIN BOEING 727 7272M7 138407S NM LT IB AILERON DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 LEFT WING INBOARD AILERON TAB UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900199 20020329 00199 SO 2002 3 29 SWIA200210696 1 20020301 A 3350 CONNECTOR EMB 120 EMB120ER 3260203 SO COCKPIT LOOSE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 288SW 120316 EXIT SIGN ON FIRST OFFICER'S SIDE BULKHEAD DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE TESTED. FOUND LOOSE CONNECTION . SECURED CONNECTION. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002032900200 20020329 00200 NM 2002 3 29 COOSDR010139 1 20020301 A 5522 657239971K SKIN BOEING 727 7272M7 138407S NM RT ELEVATOR DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT ELEVATOR TAB UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900201 20020329 00201 NM 2002 3 29 COOSDR010140 1 20020301 A 5522 657279971K SKIN BOEING 727 7272M7 138407S NM ELEVATOR TAB DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 LEFT ELEVATOR TAB UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900202 20020329 00202 SO 2002 3 29 SWIA200210697 1 20020226 A 2751 3471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 580SW 5469 5469 120348 AFTER TAKEOFF, ATTEMPTED TO RAISE FLAPS AND RECEIVED A FLAP DISAGREEMENT ON THE OUTBOARD PAIR. RAN QRH PROCEDURE WITH N O CHANGE. RETURNED TO DEN. REMOVED AND REPLACED FLAP ANNUNCIATOR PANEL. CLEANED FLAP TRACKS AND CANNON PLUGS AND RAN SYSTEM DIAGNOSTICS. RAN FLAPS NUMEROUS TIMES. OPS CHECK GOOD IAW MM 27-00-00. 2 L 7 2 4T RT A31SO 2002032900203 20020329 00203 NM 2002 3 29 COOSDR010141 1 20020301 A 5751 652176601 SKIN BOEING 727 7272M7 138407S NM LT OB AILERON DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 LEFT WING OUTBOARD AILERON TAB UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900204 20020329 00204 NM 2002 3 29 COOSDR010142 1 20020301 A 5751 6521655 PANEL BOEING 727 7272M7 138407S NM RT WING DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING UPPER FIXED PANEL INNER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900205 20020329 00205 NM 2002 3 29 COOSDR010143 1 20020301 A 5280 6538217 SKIN BOEING 727 7272M7 138407S NM RT NLG DOOR DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT NOSE LANDING GEAR DOOR OUTER AND INNER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900206 20020329 00206 EA 2002 3 29 SWIA200210698 1 20020306 A 2742 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB FAILED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 435SW 7555 DURING INITIAL POWER UP IN FAT, STAB TRIM CH2 WOULD NOT ENGAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MCU IAW CRJ MM 27-42-01. OPS CHECK GOOD. AIRCRAFT OK FOR RETURN TO CAT II SERVICE. 2 L 7 2 4F RT A21EA 2002032900207 20020329 00207 NM 2002 3 29 UPS02237938 1 20020321 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 243.7 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE:C TWO CRACKS IN SECTION 41 R/H SKIN AT BS 243.7 AT WL 215.5 & WL 223.5 AREA REPAIRED IAW SRM 53-30-3 FIG. 3 2 L 7 3 4F A3WE 2002032900208 20020329 00208 NM 2002 3 29 COOSDR010144 1 20020301 A 5533 651749320 PANEL BOEING 727 7272M7 138407S NM VERTICAL STAB DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT VERTICAL STABILIZER ACCESS PANEL INNER AND OUTER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900209 20020329 00209 NM 2002 3 29 COOSDR010145 1 20020301 A 5753 65216341321 SKIN BOEING 727 7272M7 138407S NM TE FLAP DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING INBOARD AFT FLAP UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900210 20020329 00210 EA 2002 3 29 SWIA200210699 1 20020306 A 2741 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 426SW 3384 3384 7468 WHILE AT THE GATE, STAB TRIM PERFORMED UNCOMMANDED FULL NOSE UP TO FULL NOSE DOWN MOVEMENT. STAB CH2 INOP STATUS MESSAG E APPEARED. DISCONNECTED STAB TRIM. STAB TRIM REENGAGED SEVERAL TIMES ON ITS OWN. INSTALLED SERVICEABLE HSTCU. OPS C HECKS OF STAB/YAW SYSTEM IAW 27-41-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002032900211 20020329 00211 NM 2002 3 29 COOSDR010146 1 20020301 A 5330 655756023 SKIN BOEING 727 7272M7 138407S NM FAIRING INNER DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 LEFT WING TO BODY FAIRING INNER SKIN DELAMINAED. 2 L 7 3 4F A3WE 2002032900212 20020329 00212 NM 2002 3 29 COOSDR010147 1 20020301 A 5330 655851634 SKIN BOEING 727 7272M7 138407S NM FAIRING DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING TO BODY FAIRING INNER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900213 20020329 00213 NM 2002 3 29 COOSDR010148 1 20020301 A 5330 65609671 SKIN BOEING 727 7272M7 138407S NM FAIRING DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING TO BODY FAIRING INNER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900214 20020329 00214 EA 2002 3 29 SWIA200210700 1 20020306 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR JAMMED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 423SW 7456 MAIN CABIN DOOR JAMS IN CLOSED POSITION. REMOVED AND REPLACED PASSENGER DOOR OUTER HANDLE ASSEMBLY WITH NEW IAW CRJ MM 52-11-03. ADJUSTED PASSENGER DOOR WARNING SYSTEM IAW CRJ MM 52-70-03. OPERATED PASSENGER DOOR FROM INSIDE AND OUTSIDE OF AIRCRAFT. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002032900215 20020329 00215 NM 2002 3 29 COOSDR010149 1 20020301 A 5350 65255742 SKIN BOEING 727 7272M7 138407S NM FAIRING DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING TO BODY FAIRING SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900216 20020329 00216 NM 2002 3 29 COOSDR010150 1 20020301 A 5755 651734757A SKIN BOEING 727 7272M7 138407S NM RT WING SPOILER DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING SPOILER NR 11 UPPER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900217 20020329 00217 NM 2002 3 29 COOSDR010151 1 20020301 A 5755 651734757A SKIN BOEING 727 7272M7 138407S NM RT WING SPOILER DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING SPOILER NR 11 UPPER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900218 20020329 00218 NM 2002 3 29 COOSDR010152 1 20020301 A 5730 6519281246 SKIN BOEING 727 7272M7 138407S NM RT WING DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING ACCESS PANEL INNER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900219 20020329 00219 NM 2002 3 29 COOSDR010153 1 20020301 A 5730 6521657254 SKIN BOEING 727 7272M7 138407S NM LT WING DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 LEFT WING UPPER FIXED PANEL INNER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900220 20020329 00220 NM 2002 3 29 COOSDR010154 1 20020301 A 5350 656038614 SKIN BOEING 727 7272M7 138407S NM FAIRING DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 RIGHT WING TO BODY FAIRING OUTER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900221 20020329 00221 NM 2002 3 29 COOSDR010155 1 20020301 A 5730 6519281245 SKIN BOEING 727 7272M7 138407S NM LT WING DELAMINATED E EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 79751 21457 LEFT WING ACCESS PANEL OUTER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002032900222 20020329 00222 WP 2002 3 29 COOSDR020001 1 20020301 A 5315 97540242 FLOORBEAM DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 FRAME TO FLOORBEARM STRUT, CRACKED. 2 L 7 4 4F 4 F 4A25 1E8 2002032900223 20020329 00223 SO 2002 3 29 SWIA200210701 1 20020304 A 2910 O-RING EMB 120 EMB120ER 3260203 SO HYD SYSTEM LEAKING A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 227SW 120304 GREEN SYSTEM HYDRAULIC LOW LEVEL MAP LIGHT ILLUMINATED AT 22,000 FT WHILE EN ROUTE TO ACV. RESERVOIR PRESSURE WAS DECRE ASING AND ELECTRIC PUMP TURNED OFF. RETURNED TO SFO AND USED FREE FALL LANDING GEAR EXTENSION. REPLACED O-RING ON GREE N SYSTEM HYDRAULIC RESERVOIR TO HYDRAULIC BAY FORWARD BULKHEAD PRESSURE LINE FITTING AT RESERVOIR. RAN ENGINE, NO LEAKS NOTED. 2 L 7 2 4T RT A31SO 2002032900224 20020329 00224 WP 2002 3 29 COOSDR020006 1 20020301 A 5720 DOUBLER DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE BEAVER TAIL CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 LEFT LOWER WING EXTERNAL (BEAVER TAIL) DOUBLER WITH CORROSION. 2 L 7 4 4F 4 F 4A25 1E8 2002032900225 20020329 00225 WP 2002 3 29 COOSDR020007 1 20020301 A 5720 DOUBLER DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE BEAVER TAIL CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 RIGHT LOWER WING EXTERNAL (BEAVER TAIL) DOUBLER WITH CORROSION. 2 L 7 4 4F 4 F 4A25 1E8 2002032900226 20020329 00226 WP 2002 3 29 COOSDR020008 1 20020301 A 5311 FRAME DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE FUSELAGE CRACKED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 NOSE SECTION - WHEEL WELL FRAME CRACKED AT STA Y = 19,000 =X 23,000. 2 L 7 4 4F 4 F 4A25 1E8 2002032900227 20020329 00227 WP 2002 3 29 COOSDR020009 1 20020301 A 5311 FRAME DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE FUSELAGE CRACKED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 NOSE SECTION, WHEEL WELL FRAME CRACKED AT STA Y 19,000, -X 23,000. 2 L 7 4 4F 4 F 4A25 1E8 2002032900228 20020329 00228 SO 2002 3 29 SWIA200210702 1 20020306 A 3250 CONNECTOR EMB 120 EMB120ER 3260203 SO NLG STEERING CONTAMINATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 213SW 120277 ON TAKEOFF ROLL, AT APPROXIMATELY 100 KTS, THE STEERING INOP LIGHT ILLUMINATED ON THE MULTI-ALARM PANEL ALONG WITH A SIN GLE CHIME. TAKEOFF WAS ABORTED. CLEANED MOISTURE FROM NOSE STEERING CANNON PLUG ON NOSE GEAR. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002032900229 20020329 00229 NM 2002 3 29 COOSDR020026 1 20020301 A 5310 SHEAR TIE BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 LOWER FUSELAGE, STA 1050 BETWEEN STR 26L AND STR 27L SHEAR TIE CORRODED. 2 L 7 3 4F 4 F RT A3WE E2EA 2002032900230 20020329 00230 2002 3 29 SWIA200210703 4 20020306 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO RUDDER BINDING A SWIA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 NM 07 199SW 2470 2470 120237 LEFT RUDDER PEDAL BINDING. REMOVED AND REPLACED RUDDER AUTOPILOT SERVO IAW 27-31-00. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002032900231 20020329 00231 NM 2002 3 29 COOSDR020027 1 20020301 A 5320 SUPPORT BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 FWD C/C, STA 623, BETWEEN STR 25L AND STR 26L AND STA 560 BETWEEN STR 25R AND STR 26R NET TUBE SUPPORT. 2 L 7 3 4F 4 F RT A3WE E2EA 2002032900232 20020329 00232 NM 2002 3 29 COOSDR020028 1 20020301 A 5320 STRUCTURE BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 FORWARD C/C, STA 620, BETWEEN STR 23R AND STR 24R SUPPORT TEE CORRODED. 2 L 7 3 4F 4 F RT A3WE E2EA 2002032900233 20020329 00233 NM 2002 3 29 COOSDR02003 1 20020301 A 5754 6521631144 SKIN BOEING 727 727231 1384079 NM PWA JT8 JT8D9 52048 NE LE FLAP CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 64347 21634 RIGHT WING, OUTBOARD FORE FLAP PN 6521631144, SN BN78 LOWER SKIN CRACKED. 2 L 7 3 4F 4 F A3WE E2EA 2002032900234 20020329 00234 SO 2002 3 29 SWIA200210704 1 20020302 A 2731 12027883001 SUPPORT EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 THE ELEVATOR TRIM FORWARD QUADRANT IDLER SPROCKET SUPPORT HAS CHAIN TRACKS WORN IN IT. REMOVED DAMAGED SUPPORT AND INST ALLED NEW IAW EMB SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002032900235 20020329 00235 NM 2002 3 29 COOSDR02004 1 20020301 A 5754 6521631261 SKIN BOEING 727 727231 1384079 NM PWA JT8 JT8D9 52048 NE LE FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 64347 21634 LEFT WING, OUTBOARD FOR FLAP PN 6521631261, SN PN 418, LOWER AND UPPER SKIN DELAMINATED. 2 L 7 3 4F 4 F A3WE E2EA 2002032900236 20020329 00236 WP 2002 3 29 COOSDR02005 1 20020301 A 5751 5642831502 SKIN DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE RT AILERON DENTED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 RIGHT WING, INBOARD AILERON-CONTROL TAB (PN 5642831502, SN 60023311) LOWER AND UPPER SKIN WITH DENT. 2 L 7 4 4F 4 F 4A25 1E8 2002032900237 20020329 00237 WP 2002 3 29 COOSDR02010 1 20020301 A 5340 5711283516 FITTING DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE FUSELAGE CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 NET SUPPORT FITTING (PN 5711283516) CORRODED LOCATED AT AFT CARGO COMPARTMENT STA 1145 LONG 31R. 2 L 7 4 4F 4 F 4A25 1E8 2002032900238 20020329 00238 WP 2002 3 29 COOSDR02011 1 20020301 A 5315 FLOORBEAM DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE FUSELAGE CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 MAIN CARGO COMPARTMENT Y STA 1680, Z0, -X10, FLOOR BEAM WITH CORROSION. 2 L 7 4 4F 4 F 4A25 1E8 2002032900239 20020329 00239 WP 2002 3 29 COOSDR02012 1 20020308 A 5315 FLOORBEAM DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE FUSELAGE CRACKED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 MAIN CARGO COMPARTMENT. Y STA 1580, Z0, +49.0 AND +X56.0, FLOORBEAM UPPER CHORD WITH CRACK. 2 L 7 4 4F 4 F 4A25 1E8 2002032900240 20020329 00240 SO 2002 3 29 SWIA200210705 1 20020228 A 6120 78249046 PCU EMB 120 EMB120ER 3260203 SO LT PROP MALFUNCTIONED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 393SW 3737 2704 120330 NP AND TQ FLUCTUATE IN CLIMB AND ON APPROACH ON ENGINE NR 1. TQ 2 PERCENT, NP 0.8 PERCENT. INSTALLED SERVICEABLE LEFT PCU IAW MM 61-21-00. OPS CHECK GOOD. NO TORQUE FLUCTUATIONS OR LEAKS NOTED. 2 L 7 2 4T RT A31SO 2002032900241 20020329 00241 EA 2002 3 29 SWIA200210706 1 20020303 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 589SW 7072 SHORTLY AFTER TAKEOFF RECEIVED FLAPS FAIL CAUTION MESSAGE. CONSULTED QRH AND RETURNED TO MSP. COMPLIED WITH AD 98-20-0 1. RESET FLAP SYSTEM PER FIM 27-51-00. OPS CHECK NORMAL. 2 L 7 2 4F RT A21EA 2002032900242 20020329 00242 SO 2002 3 29 SWIA200210707 1 20020227 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 579SW 120347 EMERGENCY LIGHT AT SEAT 6A INOP. REPAIRED BROKEN GROUND WIRE IAW WIRING MANUAL 20-00-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002032900243 20020329 00243 SO 2002 3 29 SWIA200210708 1 20020226 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJUST A SWIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 229SW 120305 LEFT LANDING GEAR B RED LIGHT CAME ON INTERMITTENTLY. ADJUSTED B DOWNLOCK PROXIMITY SENSOR GAP. VERIFIED A AND B PROXI MITY SENSOR STRIKER PLATE ADJUSTMENT CHECKS GOOD. NO OTHER DEFECTS NOTED. OPS CHECK GOOD IAW 32-61-01. 2 L 7 2 4T RT A31SO 2002032900244 20020329 00244 SO 2002 3 29 SWIA200210709 1 20020301 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO CARGO DOOR OUT OF ADJUST A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 216SW 120285 ON TAKEOFF ROLL THE CARGO DOOR LIGHT ILLUMINATED ALONG WITH A TRIPLE CHIME WARNING. ABORTED TAKEOFF. ADJUSTED FORWARD MICROSWITCH IAW MM 52-72-02. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002032900245 20020329 00245 EA 2002 3 29 SWIA200210711 1 20020305 A 3310 SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT LOOSE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 720SW 7297 CAPTAIN'S SIDE POST MAP LIGHT WAS SPARKING WITH AN ASSOCIATED ELECTRICAL FIRE SMELL WHEN LIGHT WAS MANIPULATED. IF THE LIGHT CASING WAS NOT MOVED, NO NOTED ABNORMALITIES. FOUND SWITCH TO BE LOOSE AND TIGHTENED THE JAM NUT ON THE SWITCH TO RESTORE IT TO NORMAL OPERATION. 2 L 7 2 4F RT A21EA 2002032900246 20020329 00246 EA 2002 3 29 SWIA200210712 1 20020310 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT BROKEN A SWIA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED UK UNKNOWN 1 NM 07 594SW 7285 WIRES BROKEN OFF OF THE ROLL DISCONNECT SWITCH. REMOVED AND REPLACED ROLL DISCONNECT SWITCH IAW CRJ MM 27-12-10. OPS C HECK GOOD. 2 L 7 2 4F RT A21EA 2002032900247 20020329 00247 EA 2002 3 29 SWIA200210716 1 20020309 A 2421 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA NR 2 IDG LOW A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 426SW 7468 NR 2 GENERATOR DROPPED OFF LINE DURING THE TAKEOFF ROLL. ABORTED TAKEOFF. SERVICED NR 2 IDG IAW MM 12-13-24. RAN RIGH T ENGINE GENERATOR. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002032900248 20020329 00248 NM 2002 3 29 02032901 1 20020329 A 3350 FUSE BOEING 757 757236 1384971 NM BLOWN A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 547NA NA 29946 Cabin Emergency Lights row 7abc to 15abc INOP. Replaced battery pack fuse on L-2 door I.A.W. MM33-51-00, Ops. Check good 2 L 7 2 4F RT A2NM 2002040100001 20020401 00001 SO 2002 4 1 C2XA02IA082 1 20020330 A 3350 C36601100 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17728 15772 120182 IAH- WHILE PERFORMING MAINTENANCE TROUBLE SHOOTING, THE MECHANIC NOTED THAT THE #2 EMERGENCY BATTERY CHARGE WAS LOW. I AH- MAINTENANCE REMOVED AND REPLACED THE #2 EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002040100002 20020401 00002 WP 2002 4 1 COOSDR02013 1 20020301 A 5313 LONGERON DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE FUSELAGE CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 FORWARD CARGO COMPT. Y STA 570.0, LONGERON 31R WITH CORROSION. 2 L 7 4 4F 4 F 4A25 1E8 2002040100003 20020401 00003 NM 2002 4 1 COOSDR02014 1 20020301 A 5753 FITTING BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE MID FLAP CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 FITTING, LEFT WING, INBOARD MID-FLAP INBOARD FITTING FLAP CARRIAGE WITH CORROSION. 2 L 7 3 4F 4 F RT A3WE E2EA 2002040100004 20020401 00004 NM 2002 4 1 COOSDR02015 1 20020301 A 5753 FITTING BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE MID FLAP CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 RIGHT WING, OUTBOARD MID-FLAP, INBOARD/OUTBOARD FITTINGS FLAP CARRIAGE WITH CORROSION. 2 L 7 3 4F 4 F RT A3WE E2EA 2002040100006 20020401 00006 NM 2002 4 1 COOSDR02017 1 20020308 A 5753 FITTING BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE MID FLAP CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 FITTING, RIGHT WING, INBOARD MID-FLAP, OUTBOARD FITTING FLAP CARRIAGE WITH CORROSION. 2 L 7 3 4F 4 F RT A3WE E2EA 2002040100007 20020401 00007 NM 2002 4 1 COOSDR02018 1 20020301 A 5320 655615119 CLIP BOEING 727 7272F9 138407D NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 FRAME STA 373. STR 8 RT. AFT INTERCOSTAL CLIP CRACKED DUE TO FATIGUE. 2 L 7 3 4F RT A3WE 2002040100008 20020401 00008 NM 2002 4 1 COOSDR02019 1 20020301 A 5320 69219302 CLIP BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 FRAME STA 480 STR 7 LT 8 LT, CLIP CRACKED DUE TO INADEQUATE STRINGER RIVETING. 2 L 7 3 4F 4 F RT A3WE E2EA 2002040100009 20020401 00009 NM 2002 4 1 COOSDR02021 1 20020301 A 5320 69219302 CLIP BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 FRAME STA 480 STR 3 LT CLIP CRACKED DUE TO INADEQUATE STRINGER RIVETING. 2 L 7 3 4F 4 F RT A3WE E2EA 2002040100010 20020401 00010 NM 2002 4 1 COOSDR02022 1 20020301 A 5320 SKIN BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 SKIN LAP SPLICE-LOWER SKIN. LOWER FASTENER ROW WITH CRACK INDICATION AT S-4L, BS 446.750. 2 L 7 3 4F 4 F RT A3WE E2EA 2002040100011 20020401 00011 NM 2002 4 1 COOSDR02025 1 20020301 A 5740 65217098 FITTING BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE RT WING CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 RT WING, TRAINLING EDGE AT WS383.5, FITTING CORRODED. 2 L 7 3 4F 4 F RT A3WE E2EA 2002040100012 20020401 00012 NM 2002 4 1 COOSDR02029 1 20020301 A 5330 SKIN BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 FUSELAGE SKIN LAP SPLICE-LOWER SKIN, LOWER FASTENER ROW WITH CRACK INDICATION AT S-4L, BS 390.0. 2 L 7 3 4F 4 F RT A3WE E2EA 2002040100013 20020401 00013 NM 2002 4 1 COOSDR02030 1 20020301 A 5330 SKIN BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE LAP SPLICE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 SKIN LAP SPLICE-LOWER SKIN, LOWER FASTENER ROW WITH CRACK INDICATION AT S-4L, BS 412.0. 2 L 7 3 4F 4 F RT A3WE E2EA 2002040100014 20020401 00014 NM 2002 4 1 A6WA200230004 1 20020217 A 2121 COOLING FAN DORNER DO32 DO328100 2996000 NM LT A/C PACK INOPERATIVE A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 340LS 3040 LEFT PACK HEAT OVERHEATED AFTER LANDING AND SMOKE IN CABIN. MAINTENANCE RESET HX GROUND COOLING FAN C/B, OPS CHECK GOOD AT THIS TIME. 2 H 7 2 4T RT A45NM 2002040100015 20020401 00015 NM 2002 4 1 A6WA200230005 1 20020222 A 2730 43274 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE ELEVATOR SYS INOPERATIVE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 334PH 2635 3012 ON TAKE-OFF ROLL AT 80 KNOTS, ELEVATOR DISCONNECT CAS MESSAGE APPEARED. MAINTENANCE FOUND SWITCH ON DISCONNECT UNIT BAD . REMOVED AND REPLACED DISCONNECT UNIT. 2 H 7 2 4T 4 T RT A45NM E20NE 2002040100016 20020401 00016 EA 2002 4 1 A6WA200240005 1 20020209 A 2751 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 417AW 7610 FLAP FAIL IN FLIGHT, FOLLOWED QRH AND MECHANIC PROCEDURES, CAS MESSAGE WENT OUT. MAINTENANCE INTERROGATED FCU, RESET FC U, RAN FLAPS OP CHECK OK C/W AWAC SUPPLEMENT 98-18, AMM 27-50. 2 L 7 2 4F RT A21EA 2002040100017 20020401 00017 NM 2002 4 1 02FDEA00223 1 20020329 A 2780 651781822 ACTUATOR BOEING 727 7272D4 138407U NM SLAT FAILED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 25 288FE 21850 02-83 ON T/O FLAP RETRACTED FROM 5 DEG TO 2 DEG, #4 SLAT IND OUT. R&R #4 SLAT ACTUATOR PER MM 27-81-032-4. OK FOR SERVI CE. 2 L 7 3 4F A3WE 2002040100018 20020401 00018 EA 2002 4 1 A6WA200240007 1 20020214 A 2751 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 417AW 7610 FLAPS FAIL ON APPROACH AT ZERO. C/W QRH, RESET FLAP CONTROL NR 1 C/B PER MECHANIC CONTROL, FLAPS NOW RUN AT HALF SPEED - NORMAL LANDING. MAINTENANCE RESET FLAPS PER AWAC SUPPLEMENT 98-18 FLAPS OPERATE AT NORMAL SPEED. 2 L 7 2 4F RT A21EA 2002040100019 20020401 00019 EU 2002 4 1 A6WA200260002 1 20020205 A 2420 CONNECTOR BAC 146 146200A 1500266 EU LYC ALF502 ALF502* 41580 EA NR 1 GEN BUSS FAILED A A6WA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 GL 31 609AW 29895 E2070 ENROUTE, NR 1 GENERATOR FAILED, NO VOLTS OR HZ, NR 1 AC BUSS AND AC ESSENTIAL BUSS FELL OFF LINE. NR 4 GEN FELL OFF LIN E MOMENTARILY WITH AC NR 2 BUSS OFF LINE ALSO. RESET NR 4 GENERATOR BUT ONLY ABLE TO REGAIN AC NR 2 BUSS. STARTED APU , APU GENERATOR SHOWED VOLTS AND HZ BUT UNABLE TO POWER AC NR 1 BUSS OR ESSENTIAL BUSS. MAINTENANCE REMOVED AND REPLACE D PLUG CONNECTOR 1XB12R. 2 H 7 4 4F 4 F A49EU E6NE 2002040100020 20020401 00020 EU 2002 4 1 A6WA200260003 1 20020211 A 3246 AHA1489 WHEEL BAC 146 146200A 1500266 EU NR 3 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 183US 1341 176 E2043 RIGHT INBOARD MAIN WHEEL HAS PIECE MISSING FROM WHEEL ASSEMBLY. MAINTENANCE REMOVED AND REPLACED NR 3 MAIN WHEEL ASSEMB LY. 2 H 7 4 4F A49EU 2002040100022 20020401 00022 CE 2002 4 1 AMW2002F00001 1 20020227 A 7920 330997F120414 HOSE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ENGINE OIL LEAKING A AMWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CE 07 163YV UE163 ENROUTE, THE CREW NOTICED THAT THE OIL PRESSURE LOW LIGHT FLICKERED AND THE OIL PRESSURE INDICATED LOW. THE CREW REDUCE D POWER ON THE LEFT ENGINE AND LANDED WITHOUT INCIDENT. 2 L 7 2 4T 3 T RT A24CE E2NE 2002040100023 20020401 00023 CE 2002 4 1 AOQ2002F00000 1 20020115 A 3260 426EN98 SQUAT SWITCH LEAR 60 60LEAR 5170707 CE LT MLG FAILED E AOQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 11 1940 3436 002 ON TAKEOFF CLIMB, LANDING GEAR FAILED TO RETRACT, TRANSPONDER DID NOT REPORT, CABIN FAILED TO PRESSURIZE. INSPECTED AND FOUND DEFECTIVE LEFT MAIN GEAR SQUAT SWITCH. REMOVED LEFT SQUAT SWITCH AND INSTALLED A NEW UNIT IAW LEAR 60 MM. OPERA TIONAL CHECK, GOOD. UNEVENTFUL PRECAUTIONARY LANDING. 2 L 7 2 4F RT A10CE 2002040100025 20020401 00025 NE 2002 4 1 BAC2002F00000 2 20020213 A 7532 1H1068 BLEED VALVE LEAR 60 60LEAR 5170707 CE PWA 305 PW305 NE RIGHT STUCK A BACM A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 01 8271 066 LEFT AND RIGHT BLEED LIGHT ILLUMINATED AFTER TAKEOFF. EMERGENCY DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHO T SYSTEM AND FOUND RIGHT HAND BLEED AIR MIXING VALVE TO BE STUCK IN THE FULL OPEN POSITION CAUSING EXCESSIVE HIGH PRESSU RE BLEED AIR AND TEMPERATURE INTO CABIN AIR DUCTING. EXCESSIVE TEMPERATURES DETECTED BY TEMPERATURE SENSING LOOP LOCATE D NEXT TO BLEED AIR DUCTING. REMOVED AND REPLACED BLEED AIR MIXING VALVE. LEAK CHECK AND OPERATIONAL CHECK GOOD ON GRO UND AND DURING FLIGHT. 2 L 7 2 4F 4 F RT A10CE E35NE 2002040100026 20020401 00026 CE 2002 4 1 BSY2002F00000 1 20020108 A 3260 6838 BULB LEAR 35 35A 5170602 CE GARRTT TFE731 TPE7315A WP LT MLG INDICATOR BURNED OUT E BSYA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 07 800AW 149 P74483 MIR LEFT MAIN GEAR, NO DOWN AND LOCK INDICTATION. REMOVED AND REPLACED BULB, OPS CHECK GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2002040100027 20020401 00027 NE 2002 4 1 02088658 2 20020329 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT MALFUNCTIONED A VTZA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 27 658BR 7500 DURING CLIMB OF THE FLIGHT FROM IAD TO ALB, THE CREW NOTED THAT THE LT ENGINE VIBRATION INDICATOR WAS READING IN THE YEL LOW ARC. THE CREW COMPLIED WITH THE QRH, SHUT DOWN THE LT ENGINE, AND RETURNED TO IAD. MAINTENANCE PERSONNEL INSPECTED THE SPINNER, FAN BLADES AND PINS. PERFORMED ENGINE VIBRATION CHECKS. ALL SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002040100028 20020401 00028 CE 2002 4 1 CGH2002F00000 1 20020123 A 7921 723747 REGULATOR BEECH 300 300BEECH 1152930 CE RT OIL COOLER DEFECTIVE B CGHR A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 350CB 189 FL324 RIGHT ENGINE OIL TEMPERATURE INDICATION WENT TO RED LINE WHEN IN CRUISE CONFIGURATION. WHEN POWER WAS REDUCED, OIL TEMP ERATURE WENT INTO THE GREEN. THE OIL TEMPERATURE REGULATOR/PRESSURE RELIEF VALVE IS SUSPECTED TO BE STICKING AS THE INS TALLATION OF A NEW REGULATOR CURES THE PROBLEM. NOTE: THE EXACT SAME PROBLEM OCCURRED ON THIS AIRCRAFT, ON THE LEFT POS ITION, ON 12/06/2001 AT 110.7 HOURS, AIRCRAFT AND PART TOTAL TIME. 2 L 7 2 4T A24CE 2002040100029 20020401 00029 NM 2002 4 1 CW12002F00000 1 20020211 A 2120 721407 AIR DUCT AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE CABIN COLLAPSED B CW1R O OTHER O OTHER NR NOT REPORTED 1 EA 11 790M 4179 19 CREW REPORTED CABIN COULD NOT WARM UP IN AUTOMATIC MODE, INSPITE OF TEMPERATURE INCREASE ON POTENTIOMETER. UPON EXAMINA TION INSIDE OF DUCT PN 721-407 WAS FOUND TO HAVE INSULATION AND INTERIOR MESH COLLASPED RESTRICTING AIR FLOW. CAUSE OF COLLAPSE, UNKNOWN. THERE IS NO INSPECTION REQUIRED FOR THIS DUCT AND MATERIAL CONSTRUCTION SHOULD ALSO BE REVIEWED. 2 K 7 3 4F 4 F RT A50NM E44NE 2002040100032 20020401 00032 CE 2002 4 1 DBC2002F00001 1 20020314 A 2710 660821711 INDICATOR LEAR 35 31 5170530 CE GARRTT TFE731 TFE731* 01518 WP COCKPIT FAILED E DBCA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 350DS 2784 002 SHORTLEY AFTER TAKEOFF, PILOT NOTED THAT THE AILERON TRIM INDICATOR FAILED. PILOT RETURNED TO AIRPORT WITHOUT INCIDENT. T/S TO FAILED INDICATOR. REPLACED INDICATOR (PN 6608217-11) (SN 879) OFF, (SN 372) ON. OPS CHECKED OK. DBCA-122D 2 L 7 2 4F 4 F RT A10CE E6WE 2002040100033 20020401 00033 CE 2002 4 1 DRU2002F00000 1 20020306 A 7500 3034 HOSE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP BLEED AIR LEAKING E DRUA K NONE O OTHER IN INSP/MAINT 1 GL 25 43TJ 8694 121 74439C WHILE TROUBLESHOOTING THE BLEED AIR HEATING SYSTEM, WHICH WAS INOPERATIVE, SOME LEAK CHECK SOLUTION HAD GOTTEN ON HEATIN G SENSOR AND CONTROL HOSES. HOSES WERE LEAKING. REMOVED OLD SENSOR AND CONTROL HOSES, AND INSTALLED NEW HOSES. LEAK C HECK WAS GOOD, AND SYSTEM FUNCTIONAL CHECK WAS GOOD. HOSES USED IN THIS PORTION OF SYSTEM WERE 303-4 HIGH PRESSURE HOSE , DATE CODE WAS 3/76, MOST LIKELY ORIGINAL. VISUALLY HOSES LOOKED ACCEPTABLE, AND THE FLEXIBILITY WAS GOOD, BUT DUE TO HOSES AGE, HAD DETERIORATED, COULD NOT MAINTAIN PRESSURE EVEN AT LOW OPERATING PRESSURES OF THIS SYSTEM. SOME OF THE ORFICED (T) FITTINGS INSTALLED IN THE SYSTEM WERE CLOGGED. 2 L 7 2 4F 4 F A10CE E6WE 2002040100035 20020401 00035 CE 2002 4 1 DXT2002F00001 1 20020212 A 2720 MS356754 PIN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER PEDAL LOOSE E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 953QS 666 7500153 PIN THAT SECURES PILOTS INBOARD BRAKE PEDAL INBOARD PIN TO BRAKE ACTUATING ROD CLEVIS IS WORKING LOOSE. THE PIN WAS FOU ND PROTRUDING FROM CLEVIS. PIN LOOSE ENOUGH TO BE REMOVED BY HAND. RECOMMEND REPLACE PIN WITH LOCKING DEVICE. IE: A B OLT WITH CASTLE NUT OR ROLL PIN THAT CAN BE SAFTIED/OR HARDEN CLEVIS MATERIAL. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2002040100036 20020401 00036 SW 2002 4 1 EAT2002F00000 1 20020225 A 5610 2621126905 WINDSHIELD FRCHLD SA227 SA227CC 3377522 SW COCKPIT CRACKED B EATR O OTHER O OTHER NR NOT REPORTED 1 GL 09 592BA AC592 THE RIGHT COPILOTS HEATED WINDSHIELD CRACKED AT APPROX 20,000 FEET WITH THE AIRCRAFT PRESSURIZED TO APPROXIMATELY 4.5 PS I. THE WINDSHIELD IS SPIDER CRACKED ACROSS THE ENTIRE SURFACE. THE WINDSHIELD SHOWS NO EVIDENCE OF IMPACT CAUSING THE CRACKING. 2 L 7 2 4T RT A18SW 2002041500087 20020415 00087 NM 2002 4 15 02FDEA00222 1 20020327 A 5230 SKIN BOEING 727 727277 138408S NM CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 NR 2 CARGO DOOR OUTER SKIN HAS THREE LARGE DENTS FWD OF AFT EDGE 6 INCHES FROM BOTTOM. REMOVED AND REPLACED SKIN PER EA 75230-64035. 2 L 7 3 4F RT A3WE 2002040100040 20020401 00040 EU 2002 4 1 99V21902 1 20020329 A 7160 C42RDB502014 INLET HAWKER BAE125 BAE125700B 7450007 EU GARRTT TFE731 TFE7313R1H 29001 WP ENGINE CRACKED E UVCA K NONE O OTHER IN INSP/MAINT 1 CE 03 9999V 8838 1589 NA0308 P84355 ENGINE INLET INNER LINER CRACKED. FOUND DURING COMPLIANCE WITH RECOMMENDED SERVICE BULLETIN SB71-32. 2 L 7 2 4F 4 F RT A3EU E6WE 2002040100041 20020401 00041 NE 2002 4 1 ARWA20020313 2 20020327 A 7261 OIL SYSTEM DOUG DC8 DC85F54 3021926 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE FLUCTUATES A ARWA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 19 426FB 53280 10 45667 669269 AT 1140Z NR 2 ENGINE SHUTDOWN DUE FLUCTUATING OIL PRESSURE GAUGE AND LIGHT AND OIL QTY READING ZERO, NOTE OIL TEMP READI NG NORMAL 75 DEG. REMOVED AND REPLACED ENGINE. FUNCTIONAL TEST COMPLETED AND FOUND SATISFACTORY. ACFT RETURNED TO SER VICE. ENGINE (S/N 66929) SENT TO REPAIR FACILITY FOR TEARDOWN AND INSPECTION. AWAITING INSPECTIONS RESULTS. 2 L 7 4 4F 4 F RT 4A25 1E8 2002040100042 20020401 00042 WP 2002 4 1 ARWA20020314 1 20020322 A 2910 FLUID DOUG DC8 DC85F54 3021926 WP HYD SYSTEM LOW A ARWA O OTHER J WARNING INDICATION LD LANDING 1 SO 19 426FB 45667 UPON LANDING, HYDRAULIC PRESSURED DROPPED TO ZERO AFTER GEAR EXTENSION. ALL CHECKLIST ACCOMPLISHED. SERVICED HYDRAULIC IAW MM 12-4-0, NO LEAKS NOTED. 2 L 7 4 4F RT 4A25 2002040100043 20020401 00043 EA 2002 4 1 02088650 1 20020329 A 2910 719821 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA A VTZA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 27 650BR 7418 During cruise of the flight, the crew noted the #1 hydraulic temperature at greater than 178 degrees C. The crew follow ed the QRH procedures shutting down the #1 engine and returned to IAD where the aircraft landed without incident. Maint enance personnel removed and replaced the #1 hydraulic system temperature transducer. Operational checks were satisfact ory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002040100044 20020401 00044 CE 2002 4 1 EYK2002F00000 1 20020307 A 7920 30725911 TRANSFER TUBE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP RT ENGINE CRACKED B EYKR O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 17 84BA 2110 286 258313 P107191 ON APPROACH, THE RIGHT ENGINE OIL PRESSURE STARTED TO DROP. OIL TEMP WAS NORMAL. ENGINE WAS SHUT DOWN BY CREW WHEN OIL PRESSURE DROPPED TO 20PSI. TOUCHDOWN AND ROLL-OUT, UNEVENTFUL. INSPECTED, FOUND OIL TRANSFER TUBE CRACKED AT FLARE. REMOVED AND REPLACED TUBE (PN 307259-1). OIL SERVICED AND LEAK CHECKED CRACKED TUBE SHOWED NO SIGNS OF IMPROPER INSTALL ATION. 2 L 7 2 4F 4 F RT A3EU E6WE 2002040100045 20020401 00045 CE 2002 4 1 EYK2002F00001 1 20020307 A 7920 30725911 TRANSFER TUBE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP RT ENGINE CRACKED E EYKR O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 25 84BA 2110 258313 P107191 ON APPROACH PBI, THE RIGHT ENGINE OIL PRESSURE STARTED TO DROP, OIL TEMPERATURE WAS NORMAL. ENGINE WAS SHUTDOWN BY CREW WHEN OIL PRESSURE DROPPED TO 20 PSI. TOUCH DOWN AND ROLLOUT WAS UNEVENTFUL. MADE INVESTIGATION. FOUND OIL TRANSFER TU BE CRACKED AT FLARE. REMOVED AND REPLACED TUB (PN 3072591-1), OIL SERVICED AND LEAK CHECKED. CRACKED TUBE SHOWED NO SI GNS OF IMPROPER INSTALLATION. 2 L 7 2 4F 4 F RT A3EU E6WE 2002040100046 20020401 00046 CE 2002 4 1 EYK2002F00002 1 20020301 A 7920 30725911 TRANSFER TUBE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP RT ENGINE CRACKED E EYKR O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 25 84BA 2110 286 258313 ON APPROACH PBI, THE RIGHT ENGINE OIL PRESSURE STARTED TO DROP. OIL TEMPERATURE WAS NORMAL. ENGINE WAS SHUTDOWN BY CRE W WHEN OIL PRESSURE DROPPED TO 20 PSI. TOUCHDOWN AND ROLL OUT UNEVENTFUL. MADE INSPECTION, FOUND OIL TRANSFER TUBE CRA CKED AT FLARE. REMOVED AND REPLACED TUBE (PN 3072591-1). OIL SERVICED AND LEAK CHECKED, CRACKED TUBE SHOWED NO SIGNS O F IMPROPER INSTALLATION. 2 L 7 2 4F 4 F RT A3EU E6WE 2002040100047 20020401 00047 CE 2002 4 1 FFS2002F00003 1 20020204 A 5610 10138402517 WINDSHIELD BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA COCKPIT CRACKED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 575D UE24 PILOTS WINDSHIELD, FAILED IN CRUISE. 2 L 7 2 4T 3 T RT A24CE E2NE 2002040100048 20020401 00048 EU 2002 4 1 G1X2002F00000 1 20020128 A 5710 4AS9801310 BRACKET ISRAEL GALAXY GALAXY 4500307 EU POTENTIOMETER BENT B G1XR O OTHER O OTHER NR NOT REPORTED 1 SW 19 105GX 044 FDR POTENTIOMETER BRACKET INTERFERING WITH AILERON ACTUATOR AT FULL TRAVEL, BRACKET IS MOUNTED TOO FAR FORWARD DUE TO .1 250 SHIM USED BETWEEN AFT SPAR AND THE BRACKET. SHIM SHOULD BE REMOVED AND POTENTIOMETER ADJUSTED FOR NEW POSITION. SH IELD SHOULD ALSO BE REMOVED FROM BRACKET. 2 L 7 2 4F RT A53NM 2002040100049 20020401 00049 EU 2002 4 1 G1X2002F00001 1 20020128 A 2710 4AS9801310502 BRACKET ISRAEL GALAXY GALAXY 4500307 EU POTENTIOMETER BENT B G1XR O OTHER O OTHER NR NOT REPORTED 1 SW 19 105GX 044 FDR POTENTIOMETER BRACKET INTERFERING WITH AILERON ACTUATOR AT FULL TRAVEL, BRACKET IS MOUNTED TOO FAR FORWARD DUE TO .1 250 SHIM USED BETWEEN AFT SPAR AND THE BRACKET. SHIM SHOULD BE REMOVED AND POTENTIOMETER ADJUSTED FOR NEW POSITION. SH IELD SHOULD ALSO BE REMOVED FROM BRACKET. 2 L 7 2 4F RT A53NM 2002040100050 20020401 00050 EU 2002 4 1 G1X2002F00002 1 20020128 A 3240 5012889 CALIPER ISRAEL GALAXY GALAXY 4500307 EU BRAKES LEAKING A G1XR K NONE O OTHER IN INSP/MAINT 1 SW 19 408LM 25 036 SCRAPER SEALS FAILING. 3 AIRCRAFT, BRAKE ASSEMBLIES SO FAR. SCRAPER SUPPORTS PISTON GUIDE AND IS COMING UNSEATED. TH E GUIDE THEN SHIFTS IN THE BORE AND COCKS THE PISTON SIDEWAYS AND THE SEAL BECOMES INEFFECTIVE. WAITING ON ENGINEERING DISPOSITION FROM ABSC. 2 L 7 2 4F RT A53NM 2002040100051 20020401 00051 EU 2002 4 1 G1X2002F00003 1 20020128 A 3240 5012889 CALIPER ISRAEL GALAXY GALAXY 4500307 EU BRAKE ASSY LEAKING B G1XR K NONE O OTHER IN INSP/MAINT 1 SW 19 293GA 25 051 SCRAPER SEALS FAILING. 3 AIRCRAFT, S BRAKE ASSEMBLIES SO FAR. SCRAPER SUPPORTS PISTON GUIDE AND IS COMING UNSEATED. T HE GUIDE THEN SHIFTS IN THE BORE AND COCKS THE PISTON SIDEWAYS AND THE SEAL BECOMES INEFFECTIVE. WAITING ON ENGINEERING DISPOSITION FROM ABSC. RECOMMEND INSPECT AND REPLACE. 2 L 7 2 4F RT A53NM 2002040100053 20020401 00053 EU 2002 4 1 GJQ2002F00000 1 20020205 A 3260 GA597233 PROXIMITY SWITCH MESSIER AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE73140 29001 NE MLG SHORTED B GJQR K NONE L NO TEST IN INSP/MAINT 1 NM 01 26WP 183 H0451 312 BASE COMPUTER WILL NOT RESPOND TO INTERROGATION BY LAPTOP COMPUTER, INDICATION, MISSING FROM EIED. BASE CONTROL/MONITOR MENELCOS WERE TRIPPED RED, REPLACED DETECTION BOX ASSY. THAT INCLUDES 2 PROXIMITY SWITCHES LOCATED ON NOSE LANDING GEA R. 2 L 7 3 4F 4 F A46EU E1NM 2002040100054 20020401 00054 EU 2002 4 1 GJQ2002F00001 1 20020203 A 2497 F5014096513713 CONTROL BOX AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE73140 29001 NE GALLEY MISMANUFACTURED B GJQR K NONE O OTHER IN INSP/MAINT 1 NM 01 26WP 176 312 FLIGHT CREW HEARD RELAYS CHATTERING AND CLICKING IN THE GALLEY AND LAVATORY. LAV, WATER HEATER, OVERHEAD LAV LIGHT AND TOILET FLUSH HAD INTERMITTENT POWER. A THUMP ON BACK WALL ACTIVATED OR MADE INTERMITTENT. INSPECTION REVEALED AUX C/B BOX ASSEMBLY 700 JTA CONNECTOR ALMOST OFF. DISCOVERED WASHERS UNDER SCREW HEADS OF AUX C/B BOX PN F50-14096-513-713 PRE CLUDED 700 JTA CONNECTOR FROM LOCKING. REMOVED WASHERS AND REPLACED MALE AND FEMALE PORTIONS OF 700 JTA CONNECTOR DUE T O BURNED AREAS FROM ARCING. AIRCRAFT WAS DELIVERED NEW IN THIS CONDITION SO IT IS AN AIRCRAFT ASSEMBLY OR MANUFACTURING DEFECT. 2 L 7 3 4F 4 F A46EU E1NM 2002040100056 20020401 00056 NM 2002 4 1 QXEA0200528 1 20020327 A 5270 HANDLE BOMBDR DHC8 DHC8401 NM DIRTY A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 410QX 4053 BOI - AIRCRAFT RETURNED TO FIELD WHEN AT 20,000 FT THE FORWARD BAGGAGE DOOR WARNING LIGHT ILLUMINATED. THERE WAS NO LOSS IN PRESSURIZATION. MAINTENANCE FOUND THE HANDLE CENTER NOT LOCKED PROPERLY. CLEANED AND LUBED HANDLE. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002040100057 20020401 00057 NE 2002 4 1 GLA2002F00000 2 20020203 A 7200 BOLT AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE73121C NE ENGINE BACKED OUT E GLAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 401JW 46 P73217C TAKEOFF, AC WAS CLIMBING THROUGH WHEN NR1 ENG CHIP DETECTOR/LOW PRES WARNING LIGHT ILLUMINATED. ENG WAS SHUT DOWN AND S AFE SINGLE ENG LANDING WAS MADE. INVESTIGATION REVEALED NR1 ENGINE OIL PUMP HAD RUPTURED AND FAN ASSY WOULD NOT ROTATE. ENG WAS REMOVED AND SHIPPED FOR REPAIR. ENG FAN GEAR BOX DISASSEMBLY REVEALED ONE OF THE THREE BOLTS THAT RETAIN OIL NOZZLE TO SUPPORT AND ONE OF THREE BOLTS THAT RETAIN SUPPORT TO CARRIER ASSEMBLY HAD BACKED OUT OF THEIR THREADED HOLES. NO DAMAGE OF THREADED HOLES WAS NOTED. LOCKING WASHERS (TAB WASHERS) RETAIN BOLTS. THIS DEBRIS (BOLTS AND WASHERS) MI GRATED INTO GEAR TRAIN AREA AND ENGINE OIL PUMP. 2 L 7 2 4F 4 F A33EU E6WE 2002040100058 20020401 00058 NM 2002 4 1 HN62002F00000 1 20020114 A 5240 694122810 FITTING BOEING 737 7374K5 1384706 NM AFT DOOR FRAME CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 934NU 26043 27830 AFT ENTRY DOOR FRAMING LOWER FORWARD AND AFT STOP FITTING HAS CORROSION. CAUSE: UNKNOWN 2 L 7 2 4T RT A16WE 2002040100059 20020401 00059 NM 2002 4 1 HN62002F00001 1 20020114 A 5240 694122811 FITTING BOEING 737 7374K5 1384706 NM AFT DOOR FRAME CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 934NU 26043 27830 AFT ENTRY DOOR FRAMING LOWER FORWARD AND AFT STOP FITTING HAS CORROSION. 2 L 7 2 4T RT A16WE 2002040100060 20020401 00060 NM 2002 4 1 HN62002F00002 1 20020114 A 2730 STRUCTURE BOEING 737 7374K5 1384706 NM RT ELEVATOR TAB CRACKED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 934NU 26043 27830 RIGHT ELEVATOR TAB, INBOARD HINGE CUTOUT, CRACKED AT LOWER OUTBOARD END. 2 L 7 2 4T RT A16WE 2002040100061 20020401 00061 NM 2002 4 1 AWXA200200244 1 20020323 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 SNA - EEL - C - DURING 4-DAY INSPECTION EMERGENCY ESCAPE PATH SEAT LIGHT ON ROW 7 LT WAS FOUND BROKEN AND STRIPPED FROM WIRING. MAINTENANCE REPLACED EMERGENCY ESCAPE SEAT LIGHT ASSEMBLY ON SEAT ROW 7 LT PER EO 33-50-31, FUNCTIONAL CHECK WA S GOOD. 2 L 7 2 4F RT A16WE 2002040100062 20020401 00062 NM 2002 4 1 HN62002F00003 1 20020114 A 5311 FRAME BOEING 737 7374K5 1384706 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 934NU 27830 CORROSION ON FRAME AT BS 294, RBL 53, WL 208. 2 L 7 2 4T RT A16WE 2002040100063 20020401 00063 NM 2002 4 1 AWXA200200245 1 20020323 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 SNA - EEL - C - DURING 4-DAY INSPECTION EMERGENCY ESCAPE PATH SEAT LIGHT ON ROW 8 LT WAS FOUND PULLED FROM WIRING. MAIN TENANCE REPLACED DAMAGED EMERGENCY ESCAPE SEAT LIGHT ASSEMBLY ON SEAT ROW 8 LT PER EO 33-50-31, FUNCTIONAL CHECK WAS GOO D. 2 L 7 2 4F RT A16WE 2002040100064 20020401 00064 NM 2002 4 1 HN62002F00004 1 20020114 A 5240 69412289 FITTING BOEING 737 7374K5 1384706 NM DOOR FRAME CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 934NU 26043 27830 AFT GALLEY DOOR FRAMING LOWER FORWARD AND AFT STOP FITTINGS HAS CORROSION. 2 L 7 2 4T RT A16WE 2002040100065 20020401 00065 NM 2002 4 1 HN62002F00005 1 20020114 A 5347 CARGO TRACK BOEING 737 7374K5 1384706 NM CARGO BAY CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 934NU 26043 27830 CORROSION ON LEFT HAND CARGO TRACK BETWEEN BS 500F AND 500G, LBL18, WL 156. 2 L 7 2 4T RT A16WE 2002040100066 20020401 00066 NM 2002 4 1 HN62002F00006 1 20020114 A 5312 ANGLE BOEING 737 7374K5 1384706 NM BULKHEAD CORRODED B K NONE O OTHER IN INSP/MAINT 1 NM 01 934NU 26043 27830 CORROSION ON AFT BULKHEAD LOWER SUPPORT DP714C ANGLE, BS 947, LBL 17, TO RBL 15, WL 179. 2 L 7 2 4T RT A16WE 2002040100067 20020401 00067 NM 2002 4 1 AWXA200200247 1 20020301 A 5330 659187911 SKIN PANEL BOEING 737 737317 138447P NM FUSELAGE BUCKLED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - MAJOR REPAIR - C - DURING C-13 CHECK LOOSE CHERRY MAX RIVETS WERE FOUND ON ALL 4 SIDES OF CENTER KEEL PANEL, PANEL WAS ALSO BUCKLED AND DISTORTED. MAINTENANCE DRILLED OUT RIVETS, REMOVED PANEL, FABRICATED A NEW PANEL, AND INSTALLED R EPAIR IAW AWA ER 03-5331-02070-TB1. 2 L 7 2 4F RT A16WE 2002040100068 20020401 00068 NM 2002 4 1 AWXA200200248 1 20020325 A 2560 P4010021 BATTERY BOEING 757 7572G7 1384963 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 910AW 24523 PHX - EMERGENCY EQUIPMENT -C- DURING INSPECTION OF EMERGENCY EQUIPMENT THE AFT LT EMERGENCY FLASHLIGHT WAS FOUND INOPERA TIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES IAW GENERAL PRACTICES, REF MPPM 9-1,9. OPERATION AL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002040100069 20020401 00069 NM 2002 4 1 AWXA200200249 1 20020325 A 2560 P4010021 BATTERY BOEING 737 737277 1384570 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 188AW 22655 YVR - EMERGENCY EQUIPMENT - C - DURING C-14 CHECK INSPECTION OF EMERGENCY EQUIPMENT BOTH THE UPPER AND LOWER EMERGENCY F LASHLIGHT ON THE FORWARD WALL OF THE AFT LAV WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES FOR THE UPPER AND LOWER EMERGENCY FLASHLIGHTS ON THE FORWARD WALL OF THE AFT LAV IAW GENERAL PRACTICES, REF MPPM 9-1, 9. OPERA TIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002040100070 20020401 00070 NM 2002 4 1 HN62002F00007 1 20020114 A 5347 CARGO TRACK BOEING 737 7374K5 1384706 NM RT CARGO TRACK CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 934NU 26043 27830 CORROSION ON RIGHT HAND CARGO TRACK, FROM BS 500F TO BS 500G, RBL 14, WL 156. 2 L 7 2 4T RT A16WE 2002040100071 20020401 00071 WP 2002 4 1 DHL2002807501 1 20020324 A 5313 3779762501 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF. N/R 0980 MAIN CARGO COMPT. -- !" CRACK IN BATH TUB FITTING STA. 680 , L2RCORR.: REMOVED BATH TUB FITTING I/A/ W SRM 51-1-20D , PG. 21 CLEANED , TREATED , AND PRIMED AREA I/A/W SRM 51-1-8B. INSTALLED NEW FITTING I/A/W SRM 51-1-20D PG. 9 2 L 7 4 4F RT 4A25 2002040100072 20020401 00072 WP 2002 4 1 DHL2002807502 1 20020320 A 5514 ANGLE DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R2464 LH HORIZONTAL STAB. L/E- RIB ANGLE @ STA 153.750 WITH.50 CRACKCORR: REMOVED ANGLE I/A/W SRM 55-2-0 FIG. 2 - FABRICATED NEW ANGLE (LONG 516167570) I/A/W SRM 55-2-0 - CLEANED , TREATED , AND PRIMED I/A/W SRM 51-1-8B. IN STALLED NEW ANGLE I/A/W SRM 55-2-0 FIG 2 2 L 7 4 4F RT 4A25 2002040100073 20020401 00073 NM 2002 4 1 HN62002F00008 1 20020114 A 5312 STIFFENER BOEING 737 7374K5 1384706 NM BULKHEAD CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 934NU 27830 APU COMPARTMENT RIGHT SIDE BULKHEAD, APU TORQUE BOX LINER CUTOUT, VERTICAL STIFFENER CORRODED, BS1126, RBL 15. CAUSE: UNKNOWN 2 L 7 2 4T RT A16WE 2002040100074 20020401 00074 NM 2002 4 1 HN62002F00009 1 20020205 A 5410 BRACKET BOEING 757 75724APF 1384969 NM RT ENG PYLON WORN B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 407UP 17877 23729 HYDRAULIC LINE SUPPORT CLAMP BOLT IS LOOSE AND CHAFFING AGAINST FUEL LINE UNDER PANEL NR 611KT. CAUSE: WORN BRACKET. DISPOSITION:REPLACED FUEL LINE AND BRACKET. 2 L 7 2 4F RT A2NM 2002040100075 20020401 00075 NM 2002 4 1 HN62002F00011 1 20020114 A 5311 FRAME BOEING 737 7374K5 1384706 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 934NU 26043 27830 CORROSION FOUND ON FRAME IN AFT CARGO BAY AT BS 847, RBL19 BETWEEN STR25R AND 26R. 2 L 7 2 4T RT A16WE 2002040100076 20020401 00076 NM 2002 4 1 HN62002F00012 1 20020114 A 5752 SKIN BOEING 737 7374K5 1384706 NM RT AILERON TAB DELAMINATED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 934NU 26043 27830 RIGHT WING OUTBOARD AILERON TAB, OUTBOARD END IS DELAMINATED. 2 L 7 2 4T RT A16WE 2002040100077 20020401 00077 NM 2002 4 1 HN62002F00013 1 20020114 A 5311 FRAME BOEING 737 7374K5 1384706 NM FUSELAGE CORRODED B HN6R K NONE O OTHER IN INSP/MAINT 1 NM 01 934NU 26043 27830 BS 1088 BULKHEAD FORWARD SIDE, T-CHORD (FRAME) ON OUTBOARD SIDE OF APU DIFFUSER DUCT CUTOUT, HAS CORROSION. CAUSE: UN KNOWN. 2 L 7 2 4T RT A16WE 2002040100078 20020401 00078 CE 2002 4 1 IMJ2002F00000 1 20020124 A 3260 1EN1186 SWITCH CESSNA 500 560CESSNA 2076750 CE NLG ACTUATOR FAILED E IMJA K NONE O OTHER IN INSP/MAINT 1 EA 25 17LK 5600037 ON LANDING GEAR EXTENSION, THE GREEN NOSE LIGHT DID NOT ILLUMINATE INDICATING THAT THE NOSE GEAR WAS NOT DOWN AND LOCKED . FOUND HIGH ELECTRICAL RESISTANCE IN SWITCH ON NOSE GEAR ACTUATOR. OHM CHECK COULD BE ADDED TO THE PHASE 5 INSPECTION . A CHECK OF THE SWITCH ADJUSTMENT AND CONDITION OF THE ACTUATING BALL (BETWEEN THE SWITCH AND ACTUATING PISTON) COULD ALSO BE ADDED. 2 L 7 2 4F RT A22CE 2002040100079 20020401 00079 NE 2002 4 1 IY22002F00001 2 20020311 A 7200 ENGINE AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE73140 29001 NE NR 2 FAILED B IY2R A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 15 8550A 263 PILOT EXECUTED EMERGENCY PROCEDURES DUE TO SMOKE IN COCKPIT AND LOSS OF POWER ON NR 2 ENGINE. LANDED AT NEAREST AIRPORT WITHOUT FURTHER INCIDENT. NR 2 ENGINE EXPERIENCE SEVERAL COMPRESSOR STALLS DURING CLIMB OUT OF FL310. APPROXIMATELY 4 MINUTES LATER THE ENGINE DEEC (COMPUTER) WENT TO MANUAL MODE, PILOTS REDUCED POWER LEVER TO IDLE. UPON FURTHER INVESTI GATIONS THE NR 2 ENGINE FAN DOES NOT ROTATE FREELY, SUSPECT INTERNAL BEARING OR SEAL FAILURE. NR 2 ENGINE REQUIRES DISA SSEMBLY TO DETERMINE AND VALIDATE FAILED COMPONENT. NR 2 ENGINE INTERNAL CONTAINED FAILURE, UNKNOWN AT THIS TIME, ENGIN E REQUIRES ENGINE DISASSEMBLY TO DETERMINE AND VALIDATE FAILED COMPONENT. 2 L 7 3 4F 4 F A46EU E1NM 2002040100080 20020401 00080 NM 2002 4 1 AWXA200200252 1 20020326 A 3350 321454 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 36119 091 PHX - EEL - FLT 0472 - EMERGENCY EXIT SIGN AT RT OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 12WL IAW AMM 33-51-38-401. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002040100081 20020401 00081 CE 2002 4 1 JGV2002F00000 1 20020123 A 2133 66002073 CONNECTOR LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP OUTFLOW VALVE CRACKED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 987LP 670 PLASTIC CONNECTION THAT CONNECTS TO THE HOSE UNION CRACKED TO THE POINT THAT THE THREADED UNION WILL NOT STAY CONNECTED TO THE OUTFLOW VALVE. 2 L 7 2 4F 4 F A10CE E6WE 2002040100082 20020401 00082 NM 2002 4 1 AWXA200200253 1 20020327 A 3350 1012721 LIGHT AIRBUS A319 A319132 3930340 NM CABIN MISSING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 SNA - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 LT WAS FOUND MISSING. MAINTENANCE REPLACED EME RGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 12 LT, FUNCTIONAL CHECK WAS GOOD IAW A1C33006. 2 L 7 2 4F RT A28NM 2002040100083 20020401 00083 NM 2002 4 1 AWXA200200254 1 20020328 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN MISSING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 SNA - EEL - DURING 8-DAY INTERIOR CHECK EMERGENCY ESCAPE PATH LIGHT WAS FOUND MISSING FROM SEAT ROW 12 LT. MAINTENANCE INSTALLED A NEW EMERGENCY ESCAPE PATH LIGHT ASSEMBLY ON SEAT ROW 12 LT IAW T/C A1C33003, A1C33011, AND EO 33-50-33. OPE RATIONAL CHECK WAS GOOD IAW A1C33006. 2 L 7 2 4F RT A16WE 2002040100084 20020401 00084 SO 2002 4 1 C2XA02CL080 1 20020321 A 2120 ODOR EMB 135 EMB135ER 3260203 SO COCKPIT DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14505 145192 CLE FLIGHT 3000 THE CREW REPORTED SHORTLY AFTER TAKEOFF THERE WAS A LIGHT SMELL OF ELECTRICAL SMOKE AND BOTH TRANSPONDER S STOPPED WORKING. MAINTENANCE INSPECTED RELATED WIRING AND PERFORMED OPERATIONAL CHECKS OF THE SYSTEM. NO DEFECTS WER E FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002040100085 20020401 00085 CE 2002 4 1 JGV2002F00001 1 20020207 A 3411 DRAIN LINE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP PITOT TUBE LEAKING B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 365AT 917 258449 THE P1 DRAIN (LT FWD) AND THE P2 DRAIN (RT AFT OB) WERE FOUND TO LEAK IN EXCESS OF REQUIRED SPECS PER AIRCRAFT MM. THE P1 LEAKED SLIGHTLY LESS THAN 2 KTS AND THE P2 LEAKED MORE THAN 3 KTS PER MINUTE. LEAKS WERE TRACED TO THE P1 AND P2 DRA IN RESERVOIR. ON DISASSEMBLY OF DRAINS, PRC890 FOR DRAIN SEALANT IS NOT REFERENCED IN EITHER THE MM OR SB 34-3282 (DRAI N MODIFICATION). INSIDE OF THE DRAINS CONTAINED PRC 890. P1 DRAIN WAS CLEAR FOR DRAINAGE, P2 WAS BLOCKED WITH PRC890 AND WAS NOT DRAINABLE. P1 AND P2 DRAIN INSERTS WERE REMOVED AND NEW INSERTS INSTALLED PER SB. P1 AND P2 SYSTEMS WERE L EAK CHECKED TO 350 KTS WITH 0 KTS LEAKAGE FOR 2 MINUTES. STATIC SYSTEM LEAK CHECKED 100 FT PER MINUTE AT 25,000 FT. 2 L 7 2 4F 4 F RT A3EU E6WE 2002040100087 20020401 00087 SO 2002 4 1 C2XA02CL081 1 20020324 A 3350 7287103507 MODULE EMB 135 EMB135LR 3260305 SO CABIN FAULTY A C2XA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 27 15527 7 145413 CLE FLIGHT 3029 THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT GO OUT. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANC E REPLACED THE EMERGENCY LIGHT CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002040100089 20020401 00089 SO 2002 4 1 C2XA02CL082 1 20020325 A 3230 355022002MOD2 CONTROL UNIT EMB 145 EMB145LR 3260212 SO COCKPIT INTERMITTENT A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 14952 9385 145067 CLE FLIGHT 3296 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE ON THE EICAS AFTER GEAR RETRACTION. MAINTENANCE INSPECT ED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002040100090 20020401 00090 SW 2002 4 1 K7W2002F00000 1 20020128 A 3246 313571 WHEEL SWRNGN SA226 SA226TB 8780406 SW GARRTT TPE331 TPE331* 01514 WP MLG MISSING A K7WA K NONE O OTHER IN INSP/MAINT 1 GL 17 299EC 919 T410 INBOARD WHEEL ASSY OF LT MLG WAS MISSING. RETAINING NUTS AND WASHERS STILL IN PLACE AND SAFETIED. IB WHEEL BEARING WA S STILL ON AXLE, WITH NORMAL AMOUNT OF GREASE STILL ON IT. OB BEARING WAS GONE EXCEPT FOR INNER RING, BUT NO CAGE OR R OLLERS. AXLE AND BRAKE ASSY INSPECTED OK. OTHER MLG WHEELS WERE REMOVED, DISASSEMBLED, INSPECTED, AND REASSEMBLED WITH NEW TIRES INSTALLED. OTHER WHEELS SHOWED NO SIGNS OF WEAR OR DAMAGE. ALL BEARINGS WERE ADEQUATELY LUBRICATED, BUT DID REPLACE TWO BRGS AND CUPS DO TO NORMAL WEAR PATTERN. INSPECTION SHOWED OUTER BRG DISINTEGRATED AND INN WHEEL HALF HAD MULTIPLE CRACKS RADIATING FROM BRAKE DISC KEYWAYS. 2 L 7 2 4T 3 T RT A5SW E2WE 2002040100091 20020401 00091 CE 2002 4 1 KC82002F00000 1 20020213 A 2731 CONNECTOR LEAR 25 25D 5170514 CE GE CJ610 CJ6101 30006 NE PITCH TRIM LOOSE E KC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 95CK 248 PRIMARY PITCH TRIM WILL NOT PITCH UP. TIGHTENED LOOSE CONNECTOR PLUG AT TWO SPEED TRIM BOX AND RE-SAFTIED. FUNCTIONAL CHECK OF TRIM SYSTEM COMPLIED WITH PER MFG MM. 2 L 7 2 4J 4 J A10CE 1E16 2002040100092 20020401 00092 EU 2002 4 1 LS32002F00000 1 20020208 A 2910 723088365 LINE ISRAEL 1124 1124A 4500103 EU HYD SYSTEM CRACKED B LS3R K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 73CL 365 HYD FLUID LEAKING FROM FORWARD CABIN BELLY ANTENNA. FOUND GEAR UPLOCK LINE TO BE CRACKED IN BEND RADIUS UNDER CABIN FLO OR AT APPROX STA 66.45. AIRCRAFT TT: 5055.6 CYCLES 3384 2 M 7 2 4F A2SW 2002040100093 20020401 00093 NM 2002 4 1 P9R2002F00000 1 20020304 A 2910 2S5304 CHECK VALVE BOEING 727 727231 1384079 NM SYS A RESERVOIR CONTAMINATED A P9RA D RETURN TO BLOCK K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 11 54344 21631 ON TAXI OUT IN MSP CABIN AND COCKPIT FILLED WITH SMOKE. RETURNED TO GATE. REMOVED AND REPLACED NR 1 ENGINE SYSTEM. A CHECK VALVE IAW MM. CLEANED RESIDUAL FLUID OUT OF LINE FROM NR 1 ENGINE CHECK VALVE FOR SYSTEM A HEAD PRESSURE. REMOVE D AND REPLACED WATER SEPARATOR BAGS PER MM. RAN ENGINES AT POWER FOR SEVERAL MINUTES WITH PACKS ON AND OFF. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002040100094 20020401 00094 CE 2002 4 1 PAZ2002F00000 1 20020130 A 5730 652200472 SKIN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE WING CORRODED A PAZR K NONE O OTHER IN INSP/MAINT 1 CE 03 592M 3121 5600338 PERFORMED EDDY CURRENT INSPECTION OF WING PER REQUIREMENTS OF PHASE 5 INSPECTION. FOUND BOTH WINGS SEVERLY CORROEDE UND ER DEICE BOOTS. CORROSION EXTENDED COMPLETELY THROUGH RIGHT SKIN IN 6 LOCATIONS AND IN 1 LOCATION ON LEFT SKIN. CAUSED BY USE OF BODY FILLER UNDER WING BOOT. AWAITING ENGINEERING ORDER FOR REPAIR OR REPLACEMENT OF WING SKINS. 2 L 7 2 4F 4 F RT A22CE E25EA 2002040100095 20020401 00095 SO 2002 4 1 C2XA02CL085 1 20020326 A 4910 INLET EMB 145 EMB145 3260210 SO APU MISALIGNED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 12967 145133 CLE FLIGHT 3301 THE CREW REPORTED A GLYCOL SMELL AND SMOKE IN THE CABIN ON CLIMBOUT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND GLYCOL IN THE APU INLET AND THE INLET WAS MISALIG NED. THE GLYCOL WAS CLEANED UP AND THE INLET WAS ALIGNED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002040100096 20020401 00096 NM 2002 4 1 Q2S2002F00000 1 20020105 A 2420 21B731E GENERATOR BOEING 747 747230B 1384889 NM NR 3 FAILED A Q2SA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 GL 23 743SA 22671 AIR TURN BACK: AFTER T/O NR 3 GEN FIELD OFF ILLUMINATED ATTEMPTED TO RESET IAW CARRIER PROCEDURES AND FAILED CSD DISC PR OC ACCOMPLISHED. T/S SYS PER AMM FOUND NR 3 GCU FAULTY. REMOVED AND REPLACED GCU IAW AMM. OPS CHECK GOOD. 2 L 7 4 4F A20WE 2002040100097 20020401 00097 SO 2002 4 1 C2XA02IA079 1 20020324 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145 3260210 SO LT MLG DAMAGED A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 14972 145151 IAH- FLIGHT 4172, AFTER TAKEOFF LD/AIR GROUND FAIL MESSAGE AND THRUST REV DISAGREE MESSAGE APPEARED EICAS AND REMAINED ON ENTIRE FLIGHT QRH'S COMPLETED. NO SPEED BRAKES IN FLIGHT. NORMAL LANDING OCCURRED AT IAH. MAINTENANCE FOUND THAT T HE LEFT GEAR WEIGHT ON WHEELS PROX SWITCH FOR LEFT MLG STRUT CRACKED AND BENT. MAINTENANCE REMOVED AND REPLACED THE PRO X SWITCH ON LEFT MLG IAW EMB 145 M/M 32-63-01, NO OTHER DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002040100098 20020401 00098 SO 2002 4 1 C2XA02IA080 1 20020325 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13979 145181 IAH- THE CREW NOTED THAT FUMES IN THE CABIN, ISOLATED TO NR 2 PACK. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE N R 2 PACK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002040100099 20020401 00099 EU 2002 4 1 DHL2002364003 1 20020326 A 3040 WINDSHIELD WIPER AIRBUS 300 A300B4203 3930306 EU WINDSHIELD WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 COPILOTS WIPER BLADE HAS PARTIAL CONTACT WITH WINDSHIELD. REMOVED AND REPLACED COPILOTS WIPER BLADE IAW A300 MM 30-41-1 2. 2 L 7 2 4F RT A35EU 2002040100100 20020401 00100 NE 2002 4 1 SWIA200210710 3 20020301 A 6140 SELOC29DH INDICATOR EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE COCKPIT FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 215SW 873 873 120281 AFTER DEPARTURE LEFT NP NEEDLE WAS READING -0-. RETURNED TO SLC. REMOVED AND REPLACED NR 1 NP INDICATOR. OPS CHECK GO OD. 2 L 7 2 4T RT A31SO 6 C P11NE 2002040100101 20020401 00101 SO 2002 4 1 SWIA200210713 1 20020313 A 5210 ACTUATOR EMB 120 EMB120ER 3260203 SO PAX DOOR LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 214SW 120280 AT 1000 FT AGL AND 10 DEGREES BANK TO THE RIGHT (AFTER TAKEOFF), THE GREEN SYSTEM RESERVOIR LOW LEVEL LIGHT ILLUMINATED WITH HYD ON MAP. THE FLUID QUANTITY NEEDLE REGISTERED IN THE YELLOW ARC. THE LIGHTS EXTINGUISHED SOON AFTER WINGS LEVE LED AND THE FLUID QUANTITY NEEDLE STABILIZED JUST ABOVE THE YELLOW ARC FOR THE REMAINDER OF THE FLIGHT. THE GEAR WAS UP AND FLAPS AT 15 DEGREES WHEN AMBER LIGHTS FIRST ILLUMINATED. RETURNED TO DEN. FOUND THE FORWARD PASSENGER DOOR FORWAR D ACTUATOR LEAKING. REMOVED AND REPLACED WITH SERVICEABLE UNIT. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002040100102 20020401 00102 SO 2002 4 1 SWIA200210714 1 20020312 A 3080 DETECTOR EMB 120 EMB120ER 3260203 SO ICE PROTECTION MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 214SW 120280 ICE MONITOR FAILED INFLIGHT. RETURNED TO DEN. CYCLED CIRCUIT BREAKER. OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2002040100103 20020401 00103 SO 2002 4 1 SWIA200210715 1 20020308 A 2120 SMOKE EMB 120 EMB120ER 3260203 SO COCKPIT DETECTED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 579SW 120347 SMOKE IN THE COCKPIT, CENTER PILLAR AREA, NOT ASSOCIATED WITH THE FANS. RETURNED INSPECTED ALL EFDS, RADAR DISPLAYS, WI NDSHIELD HEAT WIRING, FMS AND ASSOCIATED WIRING. NO DEFECTS NOTED. PERFORMED MAINTENANCE TEST FLIGHT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002040100104 20020401 00104 SO 2002 4 1 SWIA200210718 1 20020309 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO FUEL DOOR LOOSE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 292SW 120319 SERVICE DOOR LIGHT ILLUMINATED PASSING 10,000 FT. RETURNED TO MFR. LIGHT EXTINGUISHED ON SHORT FINAL. FOUND BOTH MICR OSWITCHES ON REFUELING DOORS LOOSE. SECURED BOTH MICROSWITCH ASSEMBLIES AS NEEDED. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002040100105 20020401 00105 EA 2002 4 1 SWIA200210719 1 20020308 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 590SW 7077 CLIMBING THROUGH FL 240, THE RIGHT COCKPIT WINDOW SHATTERED. RETURNED TO ABQ. REMOVED AND REPLACED RIGHT SIDE WINDOW W ITH SERVICEABLE UNIT IAW MM 56-12-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002040100106 20020401 00106 EA 2002 4 1 SWIA200210720 1 20020306 A 2120 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA A/C BAY MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 498SW 7483 LEFT PACK OVER PRESSURIZED AND AUTO SHUTDOWN. FOLLOWED MEL PROCEDURES, COULD NOT RESET. RETURNED TO DFW. SWAPPED LEFT AND RIGHT PRSOV'S FROM SIDE TO SIDE. CHECKED SYSTEM FOR LEAKS. CHECKED SYSTEM PER MM 21-51-00, OPS CHECK GOOD. PERFO RMED INFLIGHT FUNCTION CHECK OF LEFT PACK FOR HIGH PRESSURE. FUNCTIONS NORMAL FOR SINGLE PACK OPERATION. 2 L 7 2 4F RT A21EA 2002040100107 20020401 00107 SO 2002 4 1 SWIA200210721 1 20020312 A 2731 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 268UE 120207 ABORTED TAKEOFF DUE TO TAKEOFF AURAL WARNING TAKEOFF OFF TRIM. TRIM WAS SET AT 25.7 UNITS, WELL WITHIN THE MIDDLE OF TH E GREEN BAND. REPLACED BOTH PROXIMITY SWITCHES IN ELEVATOR TRIM. PERFORMED OPS CHECK OF TRIM WARNING. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002040100108 20020401 00108 SO 2002 4 1 SWIA200210722 1 20020315 A 3010 SWITCH EMB 120 EMB120RT 3260202 SO LT WING BOOT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 593SW 120191 LEFT MIDDLE WING DEICE BOOT FAILS DURING CLIMBOUT AT HIGH POWER SETTINGS. RETURNED TO PDX. REPLACED 16 PSI SWITCH FOR LEFT MID WING BOOT PER MM 30-00-00. OPS CHECK OK. 2 L 7 2 4T RT A31SO 2002040100109 20020401 00109 SO 2002 4 1 SWIA200210723 1 20020315 A 2731 52991 ACTUATOR EMB 120 EMB120ER 3260203 SO ELEVATOR TAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 569SW 120344 CLIMBING TO FLIGHT LEVEL 200 AT APPROXIMATELY 18,000 FT, ELEVATOR TRIM WHEEL FROZE. UNABLE TO MOVE THE WHEEL UNTIL DESC ENDED BELOW APPROXIMATELY 12,000 FT BELOW THAT ALTITUDE THE TRIM FUNCTIONED NORMALLY. REMOVED AND REPLACED BOTH LEFT AN D RIGHT ELEVATOR TRIM TAB LINEAR ACTUATORS IAW MM 27-32-02. ADJUSTED TRIM TAB CABLE TENSIONS IAW MM 27-00-01. OPS CHEC K GOOD. 2 L 7 2 4T RT A31SO 2002040100110 20020401 00110 2002 4 1 SWIA200210724 4 20020315 A 3414 INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 295SW 120322 DURING TAKEOFF ROLL GOT A HIGH SPEED AURAL WARNING. ABORTED TAKEOFF. REPLACED CAPTAIN'S AIRSPEED INDICATOR. CHECKED P ITOT STATIC SYSTEM PER FAR 91-411 & PART 43 APPENDIX E. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002040100111 20020401 00111 NE 2002 4 1 SWIA200210725 2 20020314 A 7321 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LEFT DEFECTIVE A SWIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 197SW 120186 IN CLIMBOUT THROUGH FL20, THE LEFT POWER LEVER WOULD NOT RESPOND TO THROTTLE INPUT. SWITCHED THE LEFT EEC TO MANUAL AND THE ENGINE REQUIRED POWER. SELECTED MANUAL ON THE RIGHT ENGINE EEC AND RETURNED TO DEN. REMOVED AND REPLACED LEFT 14, 000 FT PRESSURE SWITCH IAW MM 73-23-01. OPS CHECK OF PRESSURE SWITCH GOOD AND ENGINE EEC OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002040100112 20020401 00112 SO 2002 4 1 SWIA200210726 1 20020313 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN LOOSE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 190SW 120050 EMERGENCY LIGHTS IN FLOOR TRACK WILL NOT ILLUMINATE. SECURED LOOSE WIRE AT CONNECTION BELOW FLOOR AT ROW 3. EMERGENCY LIGHTS, OPS CHECK OK. 2 L 7 2 4T RT A31SO 2002040100113 20020401 00113 SO 2002 4 1 SWIA200210727 1 20020216 A 2730 CONTROL CABLE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 190SW 120050 RIGHT OUTBOARD AFT ELEVATOR CABLE AND RIGHT AND LEFT AFT ELEVATOR TRIM CABLES SHOWING SIGNS OF WEAR AND CORROSION. REPL ACED RIGHT OUTBOARD AFT ELEVATOR CABLE AND RIGHT AND LEFT AFT ELEVATOR TRIM CABLES IAW EMB120 MM 27-00-01. 2 L 7 2 4T 4 T RT A31SO E20NE 2002040100114 20020401 00114 WP 2002 4 1 DHL2002807504 1 20020322 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 2047 RT. WING L/E UPPER INNER SECTION - RIB .250 CRACKED @ STA. XFS 722.500CORR: PERFORMED STOP DRILL I/ A/W SRM57-2-0 FIG. 2 - FABRICATED DOUBLER (2024T3 AL .063) I/A/W SRM57-2-0 - CLEANED, TREATED AND PRIMED I/A/W 51-1-8B - INSTALLED DOUBLER I/A/W SRM 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2002040100115 20020401 00115 SO 2002 4 1 SWIA200210728 1 20020216 A 2720 CONTROL CABLE EMB 120 EMB120ER 3260203 SO RUDDER CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 190SW 120050 LEFT RUDDER AFT OUTBOARD AND INBOARD CABLES SHOW SIGNS OF CORROSION. REPLACED LEFT RUDDER AFT OUTBOARD AND INBOARD CABL ES IAW EMB120 MM 27-00-01. 2 L 7 2 4T RT A31SO 2002040100116 20020401 00116 EA 2002 4 1 SWIA200210729 1 20020317 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 406SW 7030 EMERGENCY LIGHTS IN CABIN ARE OUT. REMOVED AND REPLACED EMERGENCY LIGHT POD LAMP AS NEEDED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002040100117 20020401 00117 EA 2002 4 1 SWIA200210731 1 20020316 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERON MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 NM 07 406SW 444 444 7030 AFTER LANDING OBSERVED SPOILERONS FAULT AND I/B GND SPLR FAULT. REMOVED AND REPLACED NR 2 SECU IAW 27-61-04. 2 L 7 2 4F RT A21EA 2002040100118 20020401 00118 SO 2002 4 1 SWIA200210733 1 20020316 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP LEAKING A SWIA A UNSCHED LANDING K F J FLUID LOSS FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 294SW 10 10 120321 FLAP DISAGREEMENT AND BLUE HYDRAULIC LOW PRESSURE, LOW LEVEL, AND MAIN PUMP LOW PRESSURE LIGHTS ILLUMINATED. RETURNED T O LAX. INSPECTION NOTED LEFT NACELLE FLAP ACTUATOR LEAKING. REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-00. OPS AND LEAK CHECKS GOOD. SERVICED BLUE SYSTEM HYDRAULIC RESERVOIR AS REQUIRED. RAN RELATED SYSTEMS WITH ELECTRIC AND ENGI NE DRIVEN PUMPS. ALL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002040100119 20020401 00119 EA 2002 4 1 SWIA200210736 1 20020316 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCONNECTED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 496SW 7473 FLOOR EMERGENCY LIGHTS ARE NOT WORKING. CONNECTED CANNON PLUG. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002040100120 20020401 00120 SO 2002 4 1 SWIA200210737 1 20020315 A 3010 CONTROL VALVE EMB 120 EMB120RT 3260202 SO DEICE SYSTEM MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 137H 120137 INBOARD LEFT AND RIGHT STABILIZER DEICE AND INBOARD LEFT AND RIGHT WING DEICE REPEATEDLY FAIL ON BOTH TIMERS. RETURNED TO PDX. REMOVED AND REPLACED EJECTOR FLOW CONTROL VALVE IAW MM 30-20-04. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002040100121 20020401 00121 WP 2002 4 1 DHL2002807505 1 20020322 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.; N/R 2048 RT. WING L/E UPPER INNER SECTION - RIB CRACKED .250 @ STA. XFS 741.250CORR: PERFORMED STOP DRILL I/A/W 57-2-0 - FABRICATED DOUBLER (2024T3 AL .063) I/A/W 57-2-0 FIG 2 - CLEANED , TREATED AND PRIMED I/A/W 51-1-8B - IN STALLED NEW DOUBLER I/A/W SRM 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2002040100122 20020401 00122 SO 2002 4 1 SWIA200210738 1 20020310 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PAX DOOR OUT OF ADJUST A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 298SW 120328 FORWARD DOOR RED LIGHT ON OVERHEAD PANEL CAME ON AT START OF TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO THE GATE. A DJUSTED MICROSWITCHES ON FORWARD DOOR AS NEEDED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002040100123 20020401 00123 EA 2002 4 1 SWIA200210739 1 20020314 A 2752 5332D1005 PDU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 437SW 26 26 7564 FLAP HALF SPEED STATUS MESSAGE ILLUMINATED AFTER EXTENDING FLAPS. REMOVED AND REPLACED LEFT PDU IAW CRJ MM 27-52-01. O PS CHECK OF HALF SPEED CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002040100124 20020401 00124 2002 4 1 SWIA200210740 4 20020319 A 2215 6225734002 CONTROL SERVO EMB 120 EMB120ER 3260203 SO AILERON STIFF A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 196SW 736 736 120151 AILERON CABLES ARE VERY STIFF. FOUND AILERON AUTOPILOT SERVO MOVEMENT STIFF. REPLACED SERVO IAW 22-10-05. AILERON AND AUTOPILOT OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002040100125 20020401 00125 SO 2002 4 1 SWIA200210741 1 20020319 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 296SW 120325 ON INITIAL TAKEOFF ROLL, TAKEOFF AUTO FEATHER AURAL WARNING WAS HEARD WITH AUTO FEATHER SWITCH ON. TAKEOFF WAS ABORTED. RETURNED TO THE GATE. PERFORMED SIMULATED TAKEOFF ENGINE RUNS. COULD NOT DUPLICATE. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002040800265 20020408 00265 EU 2002 4 8 DHL2002365002 1 20020327 A 3232 C23199103 ACTUATOR AIRBUS 300 A300B4203 3930306 EU NLG DOOR BYPASSING A DHLA O OTHER J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SO 01 365DH 149 UPON GEAR RETRACTION NOSE GEAR YELLOW LIGHTS ILLUMINATED ON BOTH FRONT S/O PANEL LIGHTS REMAIN LIT FOR 5 MIN SPEED WAS A PPROX 245 KTS WHEN PLANE STARTED VIBRATING. SLOWER TO 220 KTS RAISE GEAR HANDLE TO UP POSITION BOTH YELLOW LIGHTS WENT OUT MAINTAIN 270 KTS. FOUND R/S NOSE GEAR DOOR ACTUATOR BYPASSING FLUID REMOVED AND REPLACED R/S NOSE DOOR ACTUATOR AS PER MM 32-31-16, GROUND OPS NORMAL. 2 L 7 2 4F RT A35EU 2002040800266 20020408 00266 EU 2002 4 8 DHL2002365003 1 20020326 A 5270 NSA93203301 SWITCH AIRBUS 300 A300B4203 3930306 EU CARGO DOOR LOOSE A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 365DH 149 DOORS LIGHT ILLUMINATED ON MWP WITHOUT ANY DOORS LIGHTS ILLUMINATED ON THE ANNUNCIATOR PANEL. PRESSURIZATION WAS NORMAL . FOUND LOOSE SWITCH ON BULK CARGO DOOR, RESECURED. OP'S CHECK GOOD IAW MM 52-34-00. 2 L 7 2 4F RT A35EU 2002040800267 20020408 00267 EU 2002 4 8 DHL2002365004 1 20020327 A 5270 NSA93203301 LIMIT SWITCH AIRBUS 300 A300B4203 3930306 EU CARGO DOOR FAILED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 365DH 149 DOOR LIGHT ILLUMINATED ON MWP WITHOUT ANY DOOR LIGHT ILLUMINATED ON THE ANNUNCIATOR PANEL PRESSURIZATION WAS NORMAL. RE PLACED FORWARD LOWER CARGO DOOR LIMIT SWITCH 16WS. OPS CHECK GOOD AS PER A300 MM 52-71-00. 2 L 7 2 4F RT A35EU 2002040100126 20020401 00126 NM 2002 4 1 DHL2002708003 1 20020326 A 3040 TRANSMISSION BOEING 727 72725 1384006 NM WINDSHIELD WIPER FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 708DH 18275 CAPTAIN WINDSHIELD WIPER IS INOP. REMOVED AND REPLACED WINDSHIELD WIPER TRANSMISSION IAW B-M/M 30-42-11, OPS CHECK GOOD . 2 L 7 3 4F A3WE 2002040100127 20020401 00127 WP 2002 4 1 DHL2002807506 1 20020322 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.; N/R 2049 RT. WING L/E UPPER INNER SECTION - RIB CRACKED .250 @ STA. XFS 735.000CORR: STOP DRILLED CRACK I/A/ W SRM 57-2-0 FIG. 2 FABRICATED DOUBLER( 2024 T3 AL .063) I/A/W57-2-0 FIG 2. CLEANED , TREATED AND PRIMED I/A/W 51-1-8B . INSTALLED DOUBLER I/A/W 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2002040800042 20020408 00042 NM 2002 4 8 DHL2002724003 1 20020327 A 2621 80600011 BOTTLE BOEING 727 727228 1384083 NM APU FIRE EXTING DISCHARGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 1722 19862 APU FIRE BOTTLE PRESSURE INDICATES 50 PSI. APU DEFERRED, PLACARD INSTALLED. REF: DMI 8873 APU FIRE BOTTLE PRESSURE IN DICATES 50 PSI. REMOVED AND REPLACED APU FIRE BOTTLE. CHECKS GOOD. THIS CLEARS DMI 8873. PLACARD REMOVED. 2 L 7 3 4F RT A3WE 2002040100128 20020401 00128 NM 2002 4 1 DHL2002727003 1 20020328 A 5210 DOOR BOEING 727 727228 1384083 NM MAIN ENTRY JAMMED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 MAIN CABIN DOOR WILL NOT CLOSE. FREED JAMMED ENTRY DOOR AND OPERATED NORMALLY SEVERAL TIMES IAW M/M 52-00 INSPECTION RE VEALED NO DISCREPANCIES WITH DOOR. 2 L 7 3 4F RT A3WE 2002040100129 20020401 00129 NM 2002 4 1 DHL2002746006 1 20020326 A 2612 POWER UNIT BOEING 727 727224 1384076 NM APU DEFECTIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 746DH 22252 APU FIRE TEST WILL NOT TEST. REMOVED AND REPLACED APU FIRE DETECTION OPERATING POWER UNIT PER BMM 26-15-0, SYS OPS CHEC KS NORMAL. 2 L 7 3 4F A3WE 2002040100130 20020401 00130 NM 2002 4 1 DHL2002750002 1 20020326 A 3040 MOTOR BOEING 727 7272M7 138407S NM WINDSHIELD WIPER FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750DH 21951 LEFT WIPER INOP. REMOVED LEFT WIPER ARM AND WIPER MOTOR. REPLACED LT WIPER MOTOR IAW BMM 30-42-11. OPS AND RIG CHECKS GOOD. 2 L 7 3 4F A3WE 2002040100132 20020401 00132 WP 2002 4 1 DHL2002801008 1 20020326 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 FOUND 2 INCH CRACK LT FUSELAGE AT STA 1743 BETWEEN STR 16 & 17 ALSO FOUND A 1 INCH CRACK AT STA 1750 AT STR 15. PERFORM ED MAJOR REPAIR PER TYPICAL REPAIR CALLED IN SRM 53-2-1, ITEM 16-B-2. 2 L 7 4 4F RT 4A25 2002040100133 20020401 00133 WP 2002 4 1 DHL2002803033 1 20020316 A 5330 SKIN DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 A 1 INCH CRACK FOUND ON RT SIDE STA 1700.00 APPROX LONGERON 18. INSTALLED MINOR REPAIR STA 1700.00 LONGERON 18, RT SIDE FUESLAGE PER SRM 53-2-1 ITEM 16. 2 L 7 4 4F RT 4A25 2002040100134 20020401 00134 WP 2002 4 1 DHL2002805046 1 20020326 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 FOUND ON LT FUSELAGE AT STA 1743 BETWEEN STR 16 AND 17 A 1 INCH CRACK. 2 L 7 4 4F RT 4A25 2002040100135 20020401 00135 WP 2002 4 1 DHL2002806006 1 20020315 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 A 1.5 INCH CRACK FOUND ON RT SIDE, STA 1700.00 APPROX 18 LONGERON. INSTALLED REPAIR PER SRM 53-2-1 ITEM 16. 2 L 7 4 4F RT 4A25 2002040100136 20020401 00136 NM 2002 4 1 SWAA020469 1 20020303 A 3350 65C27093 LIGHT BOEING 737 7372K6 1364440 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002040100137 20020401 00137 NM 2002 4 1 SWAA020470 1 20020303 A 3350 6574550 LIGHT BOEING 737 7372T4 1384492 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F A16WE 2002040100138 20020401 00138 2002 4 1 SWAA020475 4 20020303 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002040100139 20020401 00139 2002 4 1 SWAA020476 4 20020226 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002040100140 20020401 00140 NM 2002 4 1 SWAA020479 1 20020303 A 5311 96380 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 610WN 27696 DURING SCHEDULED SPECIAL VISIT, FOUND LT BULKHEAD CHORD CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CHORD PER SWA A CO. 2 L 7 2 4F RT A16WE 2002040100141 20020401 00141 NM 2002 4 1 SWAA020486 1 20020305 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 623SW 27933 EEPLS DAMAGED AT ROWS 7, 8 AND 9. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2002040100142 20020401 00142 2002 4 1 SWAA020492 4 20020306 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED A2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002040100144 20020401 00144 NM 2002 4 1 SWAA020500 1 20020304 A 5330 6545871 BEAR STRAP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR BEAR STRAP CRACKED AT UPPER AND LOWER HINGE CUTOUTS. REPAIRED BEAR STRAP . 2 L 7 2 4F RT A16WE 2002040100145 20020401 00145 NE 2002 4 1 SWAA020501 2 20020305 A 7200 7B22G14 ENGINE BOEING 737 7377H4 1384404 NM GE CFM56 CFM56* 13802 NE NR 1 MALFUNCTIONED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 07 766SW 29806 876336 DECLARED EMERGENCY, INFLIGHT SHUTDOWN, AIR TURNBACK. DURING CLIMB POSSIBLE COMPRESSOR STALL OF NR 1 ENGINE, FOLLOWED BY SEVERE VIBRATION. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040100146 20020401 00146 NM 2002 4 1 SWAA020502 1 20020306 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT MID LOUNGE. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002040100147 20020401 00147 NM 2002 4 1 SWAA020503 1 20020306 A 3350 BR2013 CONNECTOR BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS INOP IN FWD CABIN. RECONNECTED CONNECTORS AT BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2002040100148 20020401 00148 2002 4 1 SWAA020514 4 20020308 A 2565 D31591478 SLIDE BOEING 737 7373Y0 1384671 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002040100150 20020401 00150 EA 2002 4 1 SH52002F00000 1 20020109 A 5310 600330363 SILL CNDAIR CL600 CL6002A12 1900304 EA GE CF34 CF34* NE WINDSHIELD CRACKED A SH5R K NONE O OTHER IN INSP/MAINT 1 NE 03 711SX 5955 3007 DURING SCHEDULED INSPECTION FOUND LOWER WINDSHIELD SILL CRACKED (PRIMARY STRUCTURE) ON LEFT AND RIGHT SIDE OF COCKPIT. BOTH CRACKS ARE AT FS 235.0 WL 110.5 AND RUN ALONG THE BASE OF A WEB LEFT CRACK IS 1.5 INCHES LONG, RIGHT IS 1.0 INCH LO NG. CRACKS IN THIS AREA ARE NOT REPAIRABLE PER FACTORY ENGINEERING. REMOVED AND REPLACED ONE PIECE WINDSHIELD LOWER SI LL. 2 L 7 2 4F 4 F RT A21EA E15NE 2002040100151 20020401 00151 NM 2002 4 1 UPS02237948 1 20020319 A 5310 WEB BOEING 727 72731C 1384011 NM BS 267 LH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE:C LH PRESSURE WEB CRACKED IN NWW @ BS 267 REPAIRED IAW SRM 51-40-02 FIG 1 2 L 7 3 4F A3WE 2002040100152 20020401 00152 NM 2002 4 1 UPS02237953 1 20020320 A 5210 STOP FITTING BOEING 727 72731C 1384011 NM FWD ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE:C TWO SUSPECT CRACKS ON LWR AFT ADJUSTABLE STOP FITTING ON FWD ENTRY D OOR DOOR STOP REPLACED IAW SM RO EO 2002-009-002 UPS ENGINEERING FILE NO B727-5210-16487-A 2 L 7 3 4F A3WE 2002040100153 20020401 00153 NM 2002 4 1 UPS02237954 1 20020321 A 2780 HINGE FITTING BOEING 727 72731C 1384011 NM #5 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE:C PITTING CORROSION ON I/B UPPER FLANGE OF #5 LE FLAP CENTER HINGE SUP PORT FITTING NEW HINGE FITTIN G KIT INSTALLED IAW SRM 51-30-02 2 L 7 3 4F A3WE 2002040100154 20020401 00154 CE 2002 4 1 TIM2002F00010 1 20020215 A 5410 1189100359 ANGLE BEECH 1900 1900 1154160 CE PWA PT6 PT6* 52043 EA NACELLE BROKEN E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 172GA UB11 ANGLE LOCATED ABOVE THE ICE DOOR HINGE. THIS ANGLE HOLDS THE LOWER FIRE SEAL BULK HEAD WHEN THIS ANGLE CRACKS, IT ALLOW S THE OUTSIDE COWL RIVETS TO WORK LOOSE, AND THIS CAUSES THE COWL SIDE SKIN TO CRACK. 2 L 7 2 4T 3 T RT A24CE E2NE 2002040100155 20020401 00155 WP 2002 4 1 UO22002F00003 2 20020116 A 7230 30720141 BLADE HONEYWELL LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP ENGINE FAILED B UO2R E ENGINE SHUTDOWN O OTHER NR NOT REPORTED 1 GL 19 531AJ 318040646 011 P74173 INFLIGHT SHUT DOWN CAUSED BY 3RD LPT BLADE FAILURE AT BLADE ROOT. MFG WORKING ON PROBLEM. 2 L 7 2 4F 4 F A10CE E6WE 2002040100156 20020401 00156 NM 2002 4 1 CALA0200160 1 20020329 A 5743 BUSHING BOEING 737 7373T0 1384582 NM OB ATT FTG. CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND THE L/H AND R/H MLG(WALKING BEAM) O/B ATTACH FITTING BUSHINGS CORRODED. THE CORROSION WAS REMOVED AND A NEW BUSHING WAS INSTALLED AT EACH LOCATION IAW ECRA 5741-01017. 2 L 7 2 4F RT A16WE 2002040100157 20020401 00157 EA 2002 4 1 COMA0260220 1 20020331 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 949CA 7080 FLIGHT 5472 CABIN DOOR WARNING.COULD NOT DUPLICATE OPERATIONAL CHECK OF DOOR NORMAL. NO FAULT CODES IN COMPUTER. 2 L 7 2 4F RT A21EA 2002040100158 20020401 00158 NE 2002 4 1 COMA0210011 2 20020331 A 7200 ENGINE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE A COMA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SO 01 259CA 120252 FLIGHT 5057 LT AND RT ENGINES T6 EXCEEDS 800 DEGREES C AT TAKE OFF POWER.C/W LT AND RT ENGINE COMPRESSOR WASH. 2 L 7 2 4T 4 T RT A31SO E20NE 2002040100159 20020401 00159 WP 2002 4 1 ZW0A0203701 1 20020327 A 4920 5910050 APU DOUG DC9 DC982 3022082 WP A ZW0A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 13 922TW 48013 SMOKE IN CABIN FROM AIR CONDITIONING. REMOVED AND REPLACED APU. LAST CHECK C PERFORMED 23AUG2001 MCI --CLOSED-- 2 L 7 2 4F A6WE 2002040100160 20020401 00160 EU 2002 4 1 02033001 1 20020330 A 3350 WIRE SNIAS SE313 SE3130 8680502 EU DISCONNECTED A N8TA O OTHER L NO TEST IN INSP/MAINT 1 WP 19 547 1374 Emergency lights in rows 7-13ABC did not come on when power dropped off-line. Found dis-connected wire under seat 13ABC; re-connected wire and ops checked ok as per M/M 33-51-1 1 G 7 1 3U 7H1 2002040100161 20020401 00161 NM 2002 4 1 AWXA200200257 1 20020330 A 3610 1828202 HEAT EXCHANGER BOEING 737 7373G7 1384595 NM CRACKED A AWXA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 WP 28 155AW 35679 924 23777 PHX - DIVERSION - FLT 0546 - WHILE ENROUTE FROM LAS TO DFW THE R/H WING TO BODY OVERHEAT LIGHT ILLUMINATED, AIRCRAFT DIV ERTED TO PHX. MAINTENANCE INSPECTED THE R/H PACK BAY AND FOUND 2 LOOSE/LEAKING CLAMPS. A FOLLOW UP (FUP) WAS ISSUED FOR A PNUEMATIC DUCT AND OVERHEAT INSPECTION TO BE ACCOMPLISHED (T/C'S 18M36003 & I8M36004). FOLLOW UP INSPECTION IDENTIFIED THE R/H PRIMARY HEAT EXCHANGER CRACKED, REPLACED PRIMARY HEAT EXCHANGER IAW T/C R2C21004, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002040100162 20020401 00162 NM 2002 4 1 AWXA200200260 1 20020321 A 5314 65918793 SKIN BOEING 737 73733A 1384673 NM BUCKLED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 0 0 23627 MCN - MAJOR REPAIR - DURING C-16 CHECK THE CENTER KEEL PANEL BETWEEN L/H AND R/H LANDING GEAR WHEEL WELL CUTOUTS ARE BUC KLED IN SEVERAL PLACES AND ALL FASTENERS ARE WORKING. MAINTENANCE REMOVED CENTER KEEL PANEL, FABRICATED A NEW PANEL, AND DOUBLERS FOR BS 690.75 & 706.58, INSTALLED REPAIR PARTS IAW AWA ER 03-5310-02085-JS1. 2 L 7 2 4F RT A16WE 2002040200002 20020402 00002 EU 2002 4 2 UO22002F00005 1 20020223 A 3500 4AS6900401501 TUBE ISRAEL GALAXY GALAXY 4500307 EU FLARE MISMANUFACTURED B UO2R K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 19 108GX 046 THIS TUBE CAME NEW WITH THE FLARE INSTALLED ON THE WRONG END FOR PROPER INSTALLATION. MFG HAS ISSUED DWG 30-1080269 TO ALTER THIS NEW PART. 2 L 7 2 4F RT A53NM 2002040200003 20020402 00003 WP 2002 4 2 UO22002F00006 2 20020308 A 7200 30756392 SEAL LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP NR4 RUNNER FAILED B UO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 326HG 1626 501 P89362 NR 4 SEAL RUNNER FAILED CAUSING DAMAGE TO ENGINE. MFG WORKING ON PROBLEM. 2 L 7 2 4F 4 F A10CE E6WE 2002040200004 20020402 00004 EA 2002 4 2 UWU2002F00000 1 20020301 A 2460 210D090BC RELAY CNDAIR CL600 CL6002B16 1900305 EA ELECTRICAL FAILED E UWUA K NONE O OTHER IN INSP/MAINT 1 NE 03 247WF 5369 AIRCRAFT ESS BUSS FILED, MESSAGE DISPLAYED ON ED NR 1, TROUBLESHOT PROBLEM TO AN INTERMITTENT AC ESS BUSS SENSE RELAY (K 1XD) IN JB 18. REPLACED RELAY (K1XD), OPS TEST AC ESS BUSS SYSTEM, NO FAULTS NOTED. NOTE: ESS BUSS DID NOT FAIL, SENSE RELAY FAILED GIVING AN INDICATION OF A FAILED ESS BUSS WAS ALWAYS POWERED. 2 L 7 2 4F RT A21EA 2002040200005 20020402 00005 EA 2002 4 2 UWU2002F00001 1 20020301 A 5210 600380035 ROD CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE DOOR SUPPORT BROKEN A UWUA K NONE O OTHER IN INSP/MAINT 1 NE 03 818TH 5046 MAIN ENTRANCE DOOR SUPPORT FOOT COLLAPSED. REPLACED MAIN DOOR ACTUATING ROD AND FOOT SUPPORT FOAM. OPS CHECKED MAIN DO OR NORMAL, NO FAULTS NOTED. NOTE: MAIN DOOR FOOT SUPPORT FOAM WAS MISSING CAUSING FOOT TO STICK IN POCKET, CAUSING ROD TO BREAK. 2 L 7 2 4F 4 F RT A21EA E15NE 2002040200010 20020402 00010 CE 2002 4 2 W1B2002F00000 1 20020207 A 3232 2327100029 ACTUATOR LEAR 35 31A 5170531 CE GARRTT TFE731 TFE731* 01518 WP MLG FAILED B WIBR O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 11 78PR 090 WITH LANDING GEAR SELECTED UP, HYDRAULIC PRESSURE LOW. BY PASSING FLUID IN LEFT MAIN GEAR ACTUATOR. THIS IS 3RD ACTUAT OR IN 1 YEARS TIME. 2 L 7 2 4F 4 F RT A10CE E6WE 2002040200011 20020402 00011 CE 2002 4 2 WIB2002F00000 1 20020313 A 2133 261950010 VALVE LEAR 35 31A 5170531 CE GARRTT TFE731 TFE731* 01518 WP EMERGENCY PRESS INOPERATIVE B WIBR K NONE O OTHER IN INSP/MAINT 1 SW 11 370SC 070 RIGHT EMERGENCY PRESSURIZATION VALVE WOULD NOT CLOSE AFTER ENGINE START, WAS INTERMITTENT PROBLEM. APPEARS THAT THE VAL VE HAS NO LUBRICATION AND STICKS. 2 L 7 2 4F 4 F RT A10CE E6WE 2002040200012 20020402 00012 NE 2002 4 2 WVE2002F00000 2 20020107 A 7200 31B41902 SOLENOID LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE LT ENGINE FAILED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 225FX 127 PCECA0064 LEFT ENGINE FAILED IN FLIGHT, ATTEMPTED RESTART, ENGINE TEMPERATURE HIGH AND VIBRATION CAUSED ABORT ATTEMPT. PROBABLE CAUSE: BOV SOLENOID AND/OR HMU FAILED. THE ENGINE WAS BORESCOPED WITH NO SIGNIFICANT FINDINGS. THE IGNITERS(2EA) PN31 B5168-01 SERIAL NUMBERS UNKNOWN AND RVDT PN 3AR-245 SN B0145 WERE ALSO CHANGED AS A PRECAUTIONARY MEASURE. THE AIRCRAFT FLEW TEST FLIGHT WITHOUT FURTHER INCIDENT. RECOMMEND THAT PARTS REMOVED, BE EXAMINED FOR POSSIBLE MALFUNCTIONS. 2 L 7 2 4F 4 F RT A10CE E35NE 2002040200013 20020402 00013 NE 2002 4 2 WVE2002F00001 2 20020107 A 7321 189111 HMU LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE LT ENGINE FAILED A WVER O OTHER O OTHER NR NOT REPORTED 1 EA 09 225FX 127 PCECA0064 LEFT ENGINE FAILED IN FLIGHT, ATTEMPTED RESTART, ENGINE TEMPERATURE HIGH AND VIBRATION CAUSED ABORT ATTEMPT. PROBABLE CAUSE: BOV SOLENOID AND/OR HMU FAILED. THE ENGINE WAS BORESCOPED WITH NO SIGNIFICANT FINDINGS. THE IGNITERS (2 EA) PN 31B5168-01 SERIAL NUMBERS UNKNOWN AND RVDT (PN 3AR245 SN B0145) WERE ALSO CHANGED AS A PRECAUTIONARY MEASURE. THE AIRCR AFT FLEW A TEST FLIGHT WITHOUT FURTHER INCIDENT. RECOMMEND THAT PARTS REMOVED, BE EXAMINED FOR POSSIBLE MALFUNCTIONS. 2 L 7 2 4F 4 F RT A10CE E35NE 2002040200014 20020402 00014 CE 2002 4 2 WVE2002F00002 1 20020218 A 3260 444EN2R SQUAT SWITCH LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312B WP RT MLG MISSING B WVER O OTHER O OTHER NR NOT REPORTED 1 EA 09 406FX 089 DURING OUT GOING INSPECTION FOUND ONE SET SCREW MISSING AND ONE SET SCREW LOOSE ON RIGHT MAIN LANDING GER OUT BOARD SQUA T SWITCH SWING ARM. PROBABLE CAUSE: THE SCREWS VIBRATED LOOSE. RECOMMEND THAT AN INSPECTION FOR LANDING GEAR SQUAT SWI TCH BE ADDED TO THE 300 HOUR INSPECTION; ALSO A STEP BE ADDED TO MM TO APPLY LOCTITE TO THE TWO SET SCREWS DURING INSTA LLATION. 2 L 7 2 4F 4 F RT T00008WI E6WE 2002040200015 20020402 00015 CE 2002 4 2 WVE2002F00003 1 20020304 A 2750 2300003152 CONTROL CABLE LEAR 60 60LEAR 5170707 CE PWA 305 PW305 NE TE FLAPS WORN E WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 220FX 108 DURING ROUTINE MAINTENANCE THE LEFT AND RIGHT FLAP CABLE (PN 2300003-152/155) ASSEMBLIES WERE FOUND WORN AND FRAYED AT WS 82 PULLEY SECTOR. A.C.T.T. 4174:52 A.C.T.C. 2945. PROBABLE CAUSE: FATIGUE OF CABLE AROUND A SMALL DIAMETER PULLEY . RECOMMENDATION: RECOMMEND A SPECIFIC FLAP CABLE INSPECTION CALL OUT BE ADDED TO ROUTINE MAINTENANCE AND/OR SPECIAL I NSPECTION CHECKS. 2 L 7 2 4F 4 F RT A10CE E35NE 2002040200016 20020402 00016 CE 2002 4 2 WVE2002F00004 1 20020304 A 2750 2300003155 CONTROL CABLE LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE TE FLAPS WORN E WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 227FX 4398 077 DURING ROUTINE MAINTENANCE THE LEFT AND RIGHT FLAP CABLE (PN 2300003-152/155) ASSEMBLIES WERE FOUND WORN AND FRAYED AT W S 82 PULLEY SECTOR. ACTT 4398:223 A.C.T.C. 3273. PROBABLE CAUSE: FATIGUE OF CABLE AROUND A SMALL DIAMETER PULLEY. R ECOMMENDATION: RECOMMEND A SPECIFIC FLAP CABLE INSPECTION CALL OUT BE ADDED TO ROUTINE MAINTENANCE AND/OR SPECIAL INSPE CTION CHECKS. 2 L 7 2 4F 4 F RT A10CE E35NE 2002040200018 20020402 00018 CE 2002 4 2 ZES2002F00000 1 20020131 A 3232 1EN18 SWITCH LEAR 35 31A 5170531 CE GARRTT TFE731 TFE7312B WP ACTUATOR INOPERATIVE E ZESA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 03 316AS 1622 150 PILOT REPORTED, NO DOWN AND LOCKED INDICATION ON THE RIGHT MAIN LANDING GEAR, LAMP TESTED OK. PERFORMED EMERGENCY GEAR EXTENSION IAW AFM. FOUND DEFECTIVE DOWN AND LOCK SWITCH ON THE RIGHT MAIN LANDING GEAR ACTUATOR, REPLACED WITH NEW. OP S CHECKED, OK. 2 L 7 2 4F 4 F RT A10CE E6WE 2002040200019 20020402 00019 CE 2002 4 2 ZES2002F00001 1 20020131 A 2435 23080003 STARTER GEN CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP RT ENGINE FAILED E ZESA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 EA 03 44M 742 6507043 PILOT REPORTED: WHILE IN FLIGHT FELT VIBRATION ON RIGHT ENGINE FOLLOWED BY RIGHT GENERAL LIGHT ON GLARESHIELD WARNING. PILOT DEVOTED TO NEAREST AIRPORT AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE STARTER GENERATOR, OPS CHECKED, OK 2 L 7 2 4F 4 F A9NM E6WE 2002040200020 20020402 00020 NM 2002 4 2 COOSDR02046 1 20020401 A 5753 652163586 SKIN BOEING 727 7272F9 138407D NM OB AFT FLAP DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 RIGHT WING, OUTBOARD AFT FLAP, SKIN DELAMINATED. 2 L 7 3 4F RT A3WE 2002040200021 20020402 00021 NM 2002 4 2 COOSDR02047 1 20020401 A 5753 652163492 SKIN BOEING 727 7272F9 138407D NM RT IB AFT FLAP DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 RIGHT WING, INBOARD AFT FLAP, SKIN DELAMINATED. 2 L 7 3 4F RT A3WE 2002040200022 20020402 00022 NM 2002 4 2 COOSDR02048 1 20020401 A 5753 652163475 SKIN BOEING 727 7272F9 138407D NM IB AFT FLAP DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 LEFT WING, INBOARD AFT FLAP, SKIN DELAMINATED. 2 L 7 3 4F RT A3WE 2002040200028 20020402 00028 CE 2002 4 2 QH52002F00000 1 20020221 A 7120 2651011 MOUNT LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP ENGINE CRACKED B QH5R K NONE O OTHER IN INSP/MAINT 1 NM 07 235MC 334 MOUNT HAS A .500 INCH CRACK AS MARKED ON PART. 2 L 7 2 4F 4 F A10CE E6WE 2002040200031 20020402 00031 EU 2002 4 2 T1I2002F00000 1 20020130 A 2910 ES133772 ADAPTER ISRAEL 1124 1124A 4500103 EU GARRTT TFE731 TFE731* 01518 WP HYD SYSTEM LOOSE A T1IR O OTHER W K J INADEQUATE Q C FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 19 439WW 439 HYDRAULIC SYSTEM FAILURE IN FLIGHT. ADAPTER WAS NOT TIGHTENED DURING MAINTENANCE PREVIOUS DAY. SAFETY WIRE LOOSE. PIL OT STATED SWITCH WAS CHANGED BY ANOTHER SHOP. 2 M 7 2 4F 4 F A2SW E6WE 2002040200034 20020402 00034 GL 2002 4 2 DXT2002F00000 2 20020128 A 7310 671600026 TUBE CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL FUSELAGE CHAFED A DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 987QS 2395 7500087 DURING ROUTINE INSPECTION RIGHT FUEL SUPPLY TUBE ASSEMBLY WAS FOUND TO BE NEARLY 100 PERCENT CHAFFED THROUGH BY THE RIGH T ELEVATOR CABLE JUST FORWARD OF THE RIGHT BATTERY. MAINTENANCE REMOVED AND REPLACED THE FUEL SUPPLY TUBE ASSEMBLY WITH A NEW ASSEMBLY. MAIN FUEL LINE ALMOST 100 PERCENT CHAFED THRU BY RT ELEVATOR CABLE FORWARD OF RT BATTERY. THIS ITEM DISCOVERED DURING INSPECTION. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2002040200035 20020402 00035 CE 2002 4 2 DXT2002F00002 1 20020215 A 2420 99144298 GENERATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL DC GENERATOR INOPERATIVE E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 964EJ 541 7500064 DC GENERATOR BEARING MESSAGE ILLUMINATED. COUNTERSUNK SCREW HOLES ENLONGATED ON MOUNTING SIDE FLANGE CAUSING WEAR ON GE NERATOR AND QD PAD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2002040200036 20020402 00036 CE 2002 4 2 TIM2002F00009 1 20020116 A 3222 908200111 BOLT BEECH 1900 1900 1154160 CE PWA PT6 PT6* 52043 EA NOSE STRUT CORRODED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 172GA UB11 BOLT PN 908200115, CONNECTING NOSE GEAR DRAG BRACE TO NOSE STRUT, AND BOLT PN 908200111 CONNECTING THE TWO DRAG BRACE HA LVES WAS FOUND WITH PITTING TYPE CORROSION. 2 L 7 2 4T 3 T RT A24CE E2NE 2002040200037 20020402 00037 WP 2002 4 2 0200911211 1 20020224 A 5510 STRINGER DOUG DC10 DC1030 3023501 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 211NW 46868 During "H" check found cracks on LH horizontal stabilizer outboard aft skin panel integral stringers, #1-7.5 inch crack at stations XE 77.100 and stringer #4-6.25 inch crack at station EX 77.100. Repaired per EA 12-162218. 2 L 7 3 4F A22WE 2002041200120 20020412 00120 SO 2002 4 12 C2XA02TY060 1 20020331 A 3350 276005MIN1 FUSE EMB 145 EMB145 3260210 SO POWER SUPPLY BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12957 145080 TYS DURING A ROUTINE CHECK, MAINTENANCE FOUND THE LEFT FORWARD FAIRING EXT EMERGENCY LIGHT INOP. MAINTENANCE REMOVED A ND REPLACED THE INVERTER FUSE AT THE NR 1 EMERGENCY POWER SUPPLY IAW EMB 145 AMM 30-50-50. OP'S CHECK WAS GOOD AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002041500119 20020415 00119 EU 2002 4 15 C2XA02IA083 1 20020329 A 2612 EL13201 DETECTOR AEROSP ATR42 ATR42320 8680930 EU E/E BAY MALFUNCTIONED A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 14825 170 DURING FLIGHT 3906 FROM IAH TO LIT THE CREW NOTED THAT THE NR 2 ENGINE/ LOOP -B- FAULT IN FLIGHT. MAINTENANCE REMOVED A ND REPLACED THE DETECTOR BOX, PERFORMED A OPERATIONAL CHECK OF THE ENGINE FIRE DETECTION SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002040200038 20020402 00038 EU 2002 4 2 CX7A194J1 1 20020329 A 2612 1734362450 SENSOR SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 303CE 340B194 RIGHT TAIL PIPE HOT LIGHT ON T/O. NO TAIL WIND, ABORTED, REDUCED POWER, LIGHT WENT OUT. RAIN AND MOISTURE PREVAILED IN THE AREA. 2 L 7 2 4T RT A52EU 2002040200039 20020402 00039 NM 2002 4 2 UPS02437687 1 20020131 A 5720 FITTING BOEING 747 747123 1384873 NM WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:C LT BS 1241 WING REAR SPAR UPPER SPLICE FITTING NR 3 HOLE FOUND CRACKED, PLS REFER ATTACH SKETCH. LT B S 1241 WING REAR SPAR UPPER SPLICE FITTING REPLACED AS PER UPS EO B747-5740-4366-E APPENDIX F, H AND I. 2 L 7 4 4F A20WE 2002040200040 20020402 00040 NM 2002 4 2 UPS02437826 1 20020301 A 5320 SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C FUSELAGE - BODY FAIRING SUPPORT FRAME WEB CORRODED AT BS 1540 RBL 20. FAIRING SUPPORT WEB REPAIRED SR M 53-50-04 FIG 1. 2 L 7 4 4F A20WE 2002040200041 20020402 00041 NM 2002 4 2 UPS02437832 1 20020226 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 1900-1920, BETWEEN S20R AND S22R WINDOW FORGING AREA FOUND CORROSION. STRINGER REPAIR AT BS 1900 - BS 1960 STR 20R AS PER SRM 51-40-04. 2 L 7 4 4F A20WE 2002040200042 20020402 00042 NM 2002 4 2 UPS02437833 1 20020224 A 5210 SKIN BOEING 747 747123 1384873 NM L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D : L1 DOOR LOWER HINGE ARM CUTOUT CRACK FOUND. CUTOUT SKIN REPAIRED AS PER S/B747-52-2144. 2 L 7 4 4F A20WE 2002040200043 20020402 00043 NM 2002 4 2 UPS02437834 1 20020305 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C AFT CARGO COMPT - AFTER BEAM UPPER CHORD REMOVED, BS 1820 S42L TO 43L FRAME FOUND HEAVY CORROSION. FR AME REPAIR AT AFT CARGO BS 1820 STR 42L-43L. 2 L 7 4 4F A20WE 2002040200044 20020402 00044 NM 2002 4 2 UPS02437835 1 20020222 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C UPS CUSTOMER REQUEST NEED TO REEVALUATE PREVIOUS REPAIR - PATCH ON FUSELAGE APPROXIMATELY S36 WING TO BODY FAIRING PANEL RT FWD. EXISTING INTERNAL PATCH REPAIRED BY REPLACEMENT PER SRM 53-30-03 FIG 1 INTERNAL SHEER TIE RE PAIRED AT BS 760 STR 37R TO S39R PER SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2002040200045 20020402 00045 NM 2002 4 2 UPS02437836 1 20020226 A 5230 WEB BOEING 747 747123 1384873 NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C AFT CARGO DOOR CLOSEOUT BEAM WEB CORRODED AT BS 1910 - 1915. AFT CARGO DOOR AFT LOWER WEB AT BS 1910 - 1905 REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002040200046 20020402 00046 NM 2002 4 2 UPS02437837 1 20020224 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C FWD CARGO COMPT - BS 840 S-40R STRINGER FOUND CORROSION CRACKED. STRINGER REPAIR AT FWD CARGO BS 830 - 850 STR 40R AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002040200047 20020402 00047 2002 4 2 UPS02537585 4 20020210 A 2210 6224717004 CONTROL PANEL BOEING 757 75724APF 1384969 NM COCKPIT FAILED A IPXA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 01 459UP 25480 INSPECTION TYPE:N/A ACFT AIR TURNBACK DO TO MULTIPLE FLT DIRECTOR AND AUTOPILOT REPORT- COMPLETE FAILURE OF THE MODE CON TROL PANEL. REPLACED MODE CONTROL PANEL IAW MM 22-1-02. 2 L 7 2 4F RT A2NM 2002040200049 20020402 00049 WP 2002 4 2 UPS02837388 1 20020102 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:IN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, LIGHTS OPS CHECKED OK. 2 L 7 4 4F RT 4A25 2002040200050 20020402 00050 WP 2002 4 2 UPS02837391 1 20020103 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:IN EMERGENCY LIGHTS WILL NOT TEST ON PREFLIGHT CHECK. REMOVED, REPLACED BATTERY PACK AND RELAY UNIT PER DC8 MM 33-50-01. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2002040200051 20020402 00051 WP 2002 4 2 UPS02837392 1 20020103 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS BATTERY INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01. O PS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2002040200058 20020402 00058 WP 2002 4 2 UPS02837403 1 20020104 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:LINE EXT FUSELAGE SKIN CRACKED AT STA 505 L27R. REPAIRED AREA IAW DC8 SRM 53-2-1 AND REO-G08474. 2 L 7 4 4F RT 4A25 2002040200059 20020402 00059 WP 2002 4 2 UPS02837404 1 20020104 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:LINE L27R CRACKED STA 505. REMOVED AND REPLACED DAMAGED SECTION OF LONGERON IAW DC8 SRM 53-2. 2 L 7 4 4F RT 4A25 2002040200060 20020402 00060 WP 2002 4 2 UPS02837406 1 20020114 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:N/A EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACK RELAY UNIT IAW MM 33-50-01, OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2002040200062 20020402 00062 WP 2002 4 2 UPS02837411 1 20020116 A 2611 CDU DOUG DC8 DC871F 302199D WP CARGO BAY MALFUNCTIONED A IPXA B EMER. DESCENT N FALSE WARNING NR NOT REPORTED 1 SO 01 744UP 45944 INSPECTION TYPE:N/A DIVERSION TO PIT LOWER FWD CARGO SMOKE WARNING IN FLIGHT. NOTE: MX STATED SYSTEM TESTED OK ON GROU ND. MX SMELLED CHEMICAL WHEN OPENING CARGO DOOR. HAZMAT TEAM ON SITE. PERFORMED TEST OF EACH FIRE DET PER MM 26-18-00 SYSTEM. COMPLETE BOW TS-1493 REV NO 998, T/S THE LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM. REMOVED AND REPLACED CDU GROUND OPS CHECKS GOOD PER MM 26-18-03. 2 L 7 4 4F RT 4A25 2002040200067 20020402 00067 WP 2002 4 2 UPS02837420 1 20020108 A 5320 ATTACH FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 AFT LOWER CARGO FS 1240 L35R INTERCOSTAL ATTACH FITTING IS CRACKED. 2 L 7 4 4F RT 4A25 2002040200068 20020402 00068 WP 2002 4 2 UPS02837422 1 20020116 A 3260 WARNING SYSTEM DOUG DC8 DC871F 302199D WP COCKPIT MALFUNCTIONED A IPXA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 01 744UP 45944 INSPECTION TYPE:N/A DURING FAULT ON NR 4 BUSS POWER FAIL LANDING GEAR FAULT ON EXTENSION THE GEAR HAD UNSAFE INDICATION ON ALL THREE GEARS AND GEAR WARNING HORN. PERFORMED LANDING GEAR CONTROL SYSTEM CHECK PER MM 32-31-00, NO FAULTS NOTED. SYSTEM CHECKS GOOD, OK TO CONTINUE. 2 L 7 4 4F RT 4A25 2002040200069 20020402 00069 WP 2002 4 2 UPS02837426 1 20020118 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1350 LONG 34R. CUT OUT CRACK, NDT VERIFIED NO CRACK AT CUT OUT AREA. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2002040200076 20020402 00076 WP 2002 4 2 UPS02837433 1 20020102 A 5320 3754220503 SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 200-220 LONG 31L SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED FITTING IAW 8110-3 APPROVED DH SK 702-811. 2 L 7 4 4F RT 4A25 2002040200078 20020402 00078 WP 2002 4 2 UPS02837435 1 20020110 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 1470 AT LONG 34R SKIN IS CRACKED. CUT OUT CRACKED SKIN, NDT VERIFIED NO CRACKS AT CUT OUT. FABR ICATED REPAIR AND INSTALLED IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2002040200080 20020402 00080 WP 2002 4 2 UPS02837437 1 20020105 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA -80 FLOORBEAM AND PRESSURE WEB ARE CORRODED BEYOND LIMITS AT LBL 47-59 APPROX. FABRICATED AND IN STALLED WEB AND FINGER DOUBLERS IAW SRO 8530026, FABRICATED AND INSTALLED FLOORBEAM SPLICE REPAIR IAW 8110-3 DH SK 702-9 53. 2 L 7 4 4F RT 4A25 2002040200082 20020402 00082 WP 2002 4 2 UPS02837441 1 20020101 A 5320 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C2, 3 AFT PIT FS 1050 L35L SPLICE FITTING CRACKED. 2 L 7 4 4F RT 4A25 2002040200083 20020402 00083 WP 2002 4 2 UPS02837442 1 20020106 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 AFT LOWER CARGO FS 1060 FRAME CAP CORRODED AT L36. FABBED ANGLE AND INSTALLED REPAIR IAW DC8 SRM 51 -1-16, 51-1-120D. 2 L 7 4 4F RT 4A25 2002040200084 20020402 00084 WP 2002 4 2 UPS02837443 1 20020110 A 5320 ATTACH FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C2, 3 FS 1240 L35L INTERCOSTAL ATTACH FITTING CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW FITTIN G IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040200086 20020402 00086 WP 2002 4 2 UPS02837452 1 20020122 A 5320 36431121 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STA 798 LBL 49 FLOORBEAM WEB ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE IAW DWG 3643112 AND SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 2002040200089 20020402 00089 NM 2002 4 2 SWAA020516 1 20020309 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIG HT ASSY DUE TO CRACK AND BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2002040200090 20020402 00090 NM 2002 4 2 SWAA020519 1 20020307 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2002040200091 20020402 00091 NM 2002 4 2 SWAA020521 1 20020307 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM SERVICE DOOR DEFECTIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT DIM. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002040200094 20020402 00094 NM 2002 4 2 VNAA0201001 1 20020101 A 2150 A/C PACK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A/C BAY MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 328JS 3030 AS THE CREW BEGAN TO APPLY POWER, THE CREW RECEIVED A RIGHT HAND PACK CAS MESSAGE AND ABORTED TAKEOFF. THE CREW FOLLOWE D THE QUICK REFERENCE HANDBOOK AND RESET THE SYSTEM. CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITHOUT ANY FURTH ER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200095 20020402 00095 2002 4 2 VNAA0201002 4 20020101 A 3160 DISPLAY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 461PS 3075 AFTER APPLYING POWER, THE NUMBER 4 AND NUMBER 5 MULTI FUNCTION DISPLAYS UNITS WENT BLANK. THE CREW ABORTED TAKEOFF AND DEPARTED THE RUNWAY. THE MULTI FUNCTION DISPLAY UNITS RETURNED AND WERE WORKING CORRECTLY. MAINTENANCE CONTROL ADVISED FLIGHT 4022 TO ATTEMPT ANOTHER TAKEOFF AND FLIGHT 4022 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200096 20020402 00096 NM 2002 4 2 VNAA0201005 1 20020106 A 3060 3E25152 BRUSH BLOCK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PROP FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 427JS 8175 3039 DURING THE FLIGHT, THE CREW RECEIVED A RIGHT HAND PROPELLER HEAT FAIL AND RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND REPLACED THE BRUSH BLOCK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200097 20020402 00097 NM 2002 4 2 VNAA0201006 1 20020106 A 2150 RELAY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A/C SYSTEM FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 431JS 3028 DURING FLIGHT THE CREW RECEIVED A RIGHT HAND PACK FAIL CAS MESSAGE AND RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND REPLACED THE 13 HB RELAY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200098 20020402 00098 NM 2002 4 2 VNAA0201008 1 20020106 A 3060 LEAD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PROP FRAYED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 460PS 3061 DURING CLIMB, THE CREW RECEIVED A RIGHT HAND PROPELLER FAIL MESSAGE AND RETURNED TO THE FIELD. MAINTENANCE INSPECTED AN D FOUND A FRAYED PROP DE-ICE LEAD AND REPAIRED IT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL T EST WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200099 20020402 00099 NM 2002 4 2 VNAA0201009 1 20020107 A 2421 ALTERNATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 424JS 3033 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ELECTRONIC CONTROL UNIT AND LEFT HAND ALTERNATOR FAIL CAS MESSAGE AND ABOR TED TAKEOFF. THE MESSAGE CLEARED AS FLIGHT 4019 CLEARED THE RUNWAY AND THE CREW CONTACTED MAINTENANCE CONTROL WHO ADVIS ED THE CREW TO ATTEMPT ANOTHER TAKEOFF ATTEMPT. FLIGHT 4019 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200100 20020402 00100 NE 2002 4 2 VNAA0201010 2 20020109 A 7321 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ECU DIRTY A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 424JS 3033 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ELECTRONIC CONTROL UNIT FAIL CAS MESSAGE AND ABORTED TAKEOFF. OUTSTATION MAINTENANCE CLEANED THE LEFT HAND ELECTRONIC CONTROL UNIT CANNON PLUG IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-0 0-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200101 20020402 00101 NE 2002 4 2 VNAA0201011 2 20020110 A 7321 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ECU DIRTY A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 424JS 3033 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ELECTRONIC CONTROL UNIT FAIL CAS MESSAGE AND ABORTED TAKEOFF. OUTSTATION MAINTENANCE CLEANED THE LEFT HAND ELECTRONIC CONTROL UNIT CANNON PLUG IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-0 0-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200102 20020402 00102 NM 2002 4 2 VNAA0201012 1 20020112 A 5610 SPSDO328311 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT CRACKED A VNAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 457PS 4310 3048 DURING CRUISE, FIRST OFFICER ADVISED THE RIGHT HAND WINDSHIELD CRACKED. LANDED AT THE FIRST SUITABLE AIRPORT. DID NOT DECLARE AN EMERGENCY. LANDED WITHOUT ANY INCIDENT. REPLACED THE RIGHT HAND WINDSHIELD IN ACCORDANCE WITH DORNIER MAINT ENANCE MANUAL 56-00-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200103 20020402 00103 NM 2002 4 2 VNAA0201013 1 20020113 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 436JS 15046 3052 THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMER GENCY BATTERY AT THE 4LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFO RMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200104 20020402 00104 SO 2002 4 2 C2XA02BT012 1 20020331 A 3350 NA CONNECTOR EMB 145 EMB145LR 3260212 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 13913 145438 BTV---DURING 1A INSPECTION, MAINTENANCE FOUND SERVICE DOOR EMERGENCY LIGHT TO BE INOPERATIVE.....FOUND ELECTRICAL PIN ON CONNECTOR J7198 TO BE PUSHED BACK. REPLACED (LOCKED) PIN INTO CONNECTOR IAW EMB145 MM 20-50-00. SERVICE DOOR EMERGENCY LIGHT OPS.CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2002040200105 20020402 00105 NM 2002 4 2 VNAA0201015 1 20020119 A 2430 1030200 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ELECTRICAL SYS FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 16685 3056 DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKEOFF. THE AIRCRAFT WAS THEN FERRIE D TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED THE HALL EFFECT SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 2 4-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200106 20020402 00106 NE 2002 4 2 VNAA0201016 2 20020120 A 7321 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 424JS 3033 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ELECTRONIC CONTROL UNIT FAIL MESSAGE AND ABORTED TAKEOFF. THE CREW FOLLOW ED THE QUICK REFERENCE HANDBOOK AND RESET THE SYSTEM. FLIGHT 4021 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPA RTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200107 20020402 00107 2002 4 2 VNAA0201017 4 20020121 A 3418 STICK SHAKER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 426JS 3038 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND SHAKER FAIL MESSAGE AND ABORTED TAKEOFF. THE MESSAGE CLEARED AND MAINTENA NCE CONTROL CLEARED FLIGHT 4050 FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4050 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200108 20020402 00108 2002 4 2 VNAA0201018 4 20020121 A 3160 DISPLAY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 442JS 3060 DURING TAKEOFF, THE CAPTAIN'S HEADING MODE ROLLED ON THE MULTI FUNCTION DISPLAY UNIT AND THE CREW ABORTED TAKEOFF. THE MULTI FUNCTION DISPLAY UNIT CLEARED ITSELF AND FLIGHT 4191 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4191 THEN DE PARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200109 20020402 00109 NM 2002 4 2 VNAA0201019 1 20020124 A 2810 40006 PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUEL SYSTEM FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 457PS 14304 3048 DURING TAKEOFF, THE FUEL QUANTITY FAILED AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE REFUELING PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED F OR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200110 20020402 00110 NM 2002 4 2 VNAA0201020 1 20020127 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 436JS 13807 3052 THE CREW REPORTED THAT THE FIRST STRIP OF EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED T HE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200111 20020402 00111 2002 4 2 VNAA0202001 4 20020201 A 3418 STICK SHAKER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 433JS 3047 DURING TAKEOFF, THE CREW RECEIVED A SHAKER AND PUSHER FAIL MESSAGE AND ABORTED TAKEOFF, THE MESSAGE CLEARED BY ITSELF. THERE WAS CONSIDERABLE WIND GUSTS. FLIGHT 4020 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INC IDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200112 20020402 00112 NM 2002 4 2 VNAA0202002 1 20020203 A 7712 311694201 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 431JS 10971 3028 AFTER THE TAKEOFF, THE LEFT HAND ENGINE LOST POWER. THEN THE ENGINE TORQUE SURGED TWICE. THE CREW DID DECLARE AN EMERG ENCY AND SHUT DOWN THE ENGINE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE TORQUE SENSOR IN ACCORDANCE W ITH DORNIER MAINTENANCE MANUAL 77-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040200113 20020402 00113 EU 2002 4 2 QXEA0200531 1 20020330 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX- LEFT HAND EMERGENCY DOOR LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECKS GOOD. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002040200114 20020402 00114 WP 2002 4 2 DHL2002807507 1 20020322 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 2050 RT. WING L/E UPPER INNER RIB .250 CRACK @ STA.XFS760.000 CORR: STOP DRILLED I/A/W 57-2-0 FIG. 2 FAB RICATED DOUBLER I/A/W 57-2-0 FIG 2 ( 2024T3 AL .063)CLEANED , TEATED , AND PRIMED DOUBLER I/A/W SRM 51-1-8B . INSTALLED DOUBLER ARM @RT. WING L/E UPPER INNER RIB @ STA. XFS760.000 I/A/W 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2002040200115 20020402 00115 WP 2002 4 2 DHL2002807509 1 20020322 A 5712 46554281501 TRACK DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: 1347 AFT CARGO COMPT. AFT DOOR -TRACK SUPPORT FITTING BROKENCORR: REPLACED TRACK SUPPORT FITTING OF "D" BELL Y DOOR / TIGHTENED BOLTS I/A/W 51-1-3 PG. 2A REFER TO N/R 2386 FOR OPS CK.NOTE: RII ITEM 2 L 7 4 4F RT 4A25 2002040200116 20020402 00116 WP 2002 4 2 IXXA0200011O 1 20020401 A 3260 TERMINAL DOUG DC8 DC862 3021970 WP GEAR DOOR LOOSE A IXXA O OTHER J WARNING INDICATION CR CRUISE 1 SW 11 41CX 72906 2828 46129 AFTER TAKEOFF FROM HIK, THE GEAR DOOR NOT LATCHED AND THE GEAR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO HIK FOR AN UNEV ENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED A LOOSE TERMINAL AT THE RIGHT HAND MAIN GEAR DOOR PROX IMITY SWITCH. MAINTENANCE TIGHTENED THE TERMINAL AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAI NTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002040200117 20020402 00117 WP 2002 4 2 IXXA0200012O 1 20020401 A 3260 MECHANISM DOUG DC8 DC862 3021970 WP GEAR STIFF A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 41CX 72907 2829 46129 AFTER TAKE OFF FROM HIK, THE LANDING GEAR NOT LATCHED LIGHT ILLUMINATED FOLLOWING LANDING GEAR RETRACTION. THE FLIGHT CR EW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO HIK FOR AN UNEVENTFUL LANDING. M AINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE LEFT MAIN LANDING GEAR UPLATCH MECHANISM LACKING LUBRICATION. MAINT ENANCE LUBRICATED THE UPLATCH MECHANISM AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002040200118 20020402 00118 NM 2002 4 2 2002UALA00524 1 20020322 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 FUSELAGE STRINGER 16 LH IS CRACKED AT BODY STATION 500C + 18 INCHES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHEDI NSTALLED NEW STRINGER AND SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040200119 20020402 00119 NM 2002 4 2 2002UALA00525 1 20020324 A 5313 CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 STRINGER CLIP AT STRINGER 14L BODY STATION 727A IS CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHEDREPLACED S TRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040200120 20020402 00120 NM 2002 4 2 2002UALA00526 1 20020324 A 5313 CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 STRINGER CLIP AT STRINGER 10L BODY STATION 727A IS CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHEDREPLACED S TRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040200121 20020402 00121 NM 2002 4 2 2002UALA00527 1 20020324 A 5313 CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 UPPER LOBE INTERNAL STRINGER CLIP AT STRINGER 5L BODY STATION 747 IS CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCO MPLISHEDREPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040200122 20020402 00122 NM 2002 4 2 2002UALA00528 1 20020324 A 5313 CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 STRINGER CLIP AT STRINGER 10L BODY STATION 787 CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHEDREPLACED STRIN GER CLIP 2 L 7 2 4F 4 F RT A16WE E2GL 2002041000074 20020410 00074 NM 2002 4 10 2002UALA00529 1 20020322 A 2910 271N611912 HYDRAULIC LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT MLG RUPTURED A UALA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 WP 29 559UA 26657 LOSS OF LEFT HYDRAULIC QUANTITY LEVEL DECREASED TO 1.8 WITH ASSOCIATED SYSTEM PRESSURE LIGHT ILLUMINATION. LEFT MAIN DO WNLOCK ACTUATOR HYDRAULIC LINE RUPTURED. REPLACED HYDRAULIC LINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002040200123 20020402 00123 NM 2002 4 2 2002UALA00530 1 20020324 A 5313 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 UPPER LOBE INTERNAL STRINGER CLIP CRACKED AT STRINGER 4R BODY STATION 727B. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOM PLISHEDREPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040200124 20020402 00124 NM 2002 4 2 2002UALA00531 1 20020324 A 5313 CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 STATION 380 S6L STRINGER CLIP CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHEDREPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040200125 20020402 00125 NM 2002 4 2 2002UALA00532 1 20020325 A 5313 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MISDRILLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 AFT STABILIZER COMPARTMENT STATION 1108 STRINGER 1R FORWARD FACE OF FRAME HAS MISDRILLED HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041000092 20020410 00092 NM 2002 4 10 2002UALA00533 1 20020325 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 AFT PIT FRAME UPPER SURFACE BODY STATION 727E STRINGER 25R TO STRINGER 26R HAS EXCESS MATERIAL LOSS. MAJOR REPAIR ACCOM PLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040200126 20020402 00126 NM 2002 4 2 2002UALA00538 1 20020322 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 AFT CABIN #4RH DOOR AFT LOWER FRAME HAS EXCESSIVE MATERIAL REMOVED JUST ABOVE FLOOR LEVEL BECAUSE OF CORROSION REMOVAL A T STATION 1681.5 RBL 60. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.FABRICATED AND INSTALLED INTERNAL REPAIR ANG LE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002040200127 20020402 00127 NM 2002 4 2 2002UALA00539 1 20020323 A 5500 173N2101913WT RUDDER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 38089 25019 PREVIOUS REPAIR DELAM ON RUDDER TRAILING EDGE RS 245.00 SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REMOVED DELAM REPAIR AND INSTALLED NEW REPAIR PLIES. 2 L 7 2 4F 4 F RT A2NM E17NE 2002040200128 20020402 00128 NM 2002 4 2 2002UALA00541 1 20020323 A 5315 CAP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 CABIN STATION 832, RBL 11, TRANSBEAM UPPER CAP IS CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED AND INSTALLED SPLICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040200129 20020402 00129 NM 2002 4 2 2002UALA00542 1 20020323 A 5315 CAP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 CABIN STAION 832-RBL 11, TRANSBEAM UPPER CAP IS CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED A ND INSTALLED WITH SPLICE BEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040200130 20020402 00130 NM 2002 4 2 2002UALA00543 1 20020323 A 5315 CLIP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 FLOOR BEAM ATTACH CLIP BROKEN STATION 434 LFT HAND, FORWARD PIT ABOVE STRINGER 33L. SUPPLEMENTAL DATA UPDATE MAJOR REPAI R ACCOMPLISHED. FABRICATED AND INSTALLED CLIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040200131 20020402 00131 NM 2002 4 2 2002UALA00544 1 20020323 A 5315 CLIP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 FLOOBEAM ATTACH CLIP BROKEN STATION 390LH, FORWARD PIT ABOVE STRINGER 33L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPL ISHED. FABRICATED AND INSTALLED NEW CLIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040200132 20020402 00132 NM 2002 4 2 2002UALA00546 1 20020323 A 5315 SPLICE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 STATION 880, RBL 54, TRANSBEAM OUTBOARD SPLICE GOUGED BEYOND LIMITS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR SPLICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040200133 20020402 00133 NM 2002 4 2 2002UALA00547 1 20020323 A 5315 SPLICE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 STATION 880, RBL 33, TRANSBEAM INBOARD SPLICE IS GUOGED BEYOND LIMITS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISH ED. FABRICATED AND INSTALLED SPLICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041000094 20020410 00094 NM 2002 4 10 2002UALA00552 1 20020322 A 3350 SIGN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 189UA 26878 EEL EXIT SIGN INOP ABOVE LAV 104. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000095 20020410 00095 NM 2002 4 10 2002UALA00553 1 20020322 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 189UA 26878 EEL LIGHT OVERHEAD AT ROWS 2A-2J INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000096 20020410 00096 NM 2002 4 10 2002UALA00554 1 20020322 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 189UA 26878 EEL LIGHT IN SEAT 4A (AFT LIGHT) INOP. REPLACED EEL STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000098 20020410 00098 NM 2002 4 10 2002UALA00556 1 20020322 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 CEILING EEL INOP AT DOOR 4 RIGHT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000099 20020410 00099 NM 2002 4 10 2002UALA00557 1 20020322 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 CEILING EEL INOP ABOVE SEAT 58C. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000101 20020410 00101 NM 2002 4 10 2002UALA00559 1 20020322 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 RIGHT FORWARD OVERWING EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000102 20020410 00102 NM 2002 4 10 2002UALA00560 1 20020322 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R3 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 DOOR 3R, DOOR LIGHT INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000104 20020410 00104 NM 2002 4 10 2002UALA00562 1 20020322 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 SEAT 4J - SEAT EEL STRIP LIGHT BROKEN OFF. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2002040200134 20020402 00134 NM 2002 4 2 2002UALA00564 1 20020327 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 931UA 26656 BODY STATION 178 WEB CRACKED AT WL 201 LBL 5 LOWER LT RADAR MOUNT INBOARD UPPER CORNER. MAJOR REPAIR ACCOMPLISHED, INST ALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041000105 20020410 00105 NM 2002 4 10 2002UALA00566 1 20020315 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 ON LEFT SIDE OF AIRCRAFT, THE SECOND ASSEMBLY BACK FROM THE FRONT, THE FORWARD BULB IS INOP ON THE OVERWING EEL. RELAMP ED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000106 20020410 00106 NM 2002 4 10 2002UALA00569 1 20020328 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 UPPER LOBE INTERIOR STRINGER CLIP CRACKED AT 14R AND 15R BODY STATION 727A. MAJOR REPAIR ACCOMPLISHED. REPLACED STRING ER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041000107 20020410 00107 NM 2002 4 10 2002UALA00571 1 20020327 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 CEILING EEL LIGHT IS INOP AT ROW 16. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000108 20020410 00108 NM 2002 4 10 2002UALA00572 1 20020327 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 AT SEAT 5A, AFT EEL LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000109 20020410 00109 NM 2002 4 10 2002UALA00573 1 20020327 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 AT DOOR 5 RIGHT HAND SIDE, THE FORWARD EEL SILL LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000110 20020410 00110 NM 2002 4 10 2002UALA00574 1 20020327 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 AT SEAT 5J, AFT EEL LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000111 20020410 00111 NM 2002 4 10 2002UALA00575 1 20020327 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 AT SEAT 3J, AFT EEL LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002040200135 20020402 00135 NM 2002 4 2 2002UALA00576 1 20020327 A 5320 FLOOR SUPPORT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 BODY STATION 790 LBL 12-14 FLOOR SUPPORT CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041000113 20020410 00113 NM 2002 4 10 2002UALA00580 1 20020328 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 931UA 26656 STATION 178 BULKHEAD WEB CRACKED AT WL 184 RBL 1 BEHIND LOC ANT SUPPORT. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041000115 20020410 00115 NM 2002 4 10 2002UALA00582 1 20020328 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 UPPER LOBE INT FUSE FRAME CRACKED AT FASTENER JUST ABOVE STRINGER 9L AND BODY STATION 787. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041000116 20020410 00116 NM 2002 4 10 2002UALA00583 1 20020328 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 UPPER LOBE INT STRINGER 2L HAS GOUGE JUST AFT OF BODY STATION 727. MAJOR REPAIR ACCOMPLISHED. REPLACED SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041000117 20020410 00117 NM 2002 4 10 2002UALA00584 1 20020328 A 5314 KEELBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 RIGHT HAND KEEL BEAM LOWER FLANGE UPPER SURFACE WEAR AREA AROUND FASTENER HOLE BODY STATION 700-727. MAJOR REPAIR ACCOM PLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040200136 20020402 00136 NM 2002 4 2 CALA0200164 1 20020401 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 1006-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016 IN AFT EQUIPMENT BAY. THE STRINGER WAS REMOVED AND REPL ACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002040200137 20020402 00137 EA 2002 4 2 COMA0260221 1 20020402 A 5310 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 964CA 13476 7129 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 550GB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002040200138 20020402 00138 EA 2002 4 2 COMA0260222 1 20020402 A 5310 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 964CA 13476 7129 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 550BB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002040200139 20020402 00139 EA 2002 4 2 COMA0260223 1 20020402 A 5310 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 964CA 13476 7129 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 640DB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002040200140 20020402 00140 EA 2002 4 2 COMA0260224 1 20020402 A 5310 601R10045 PLANK CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 964CA 13476 7129 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 610AB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002040200141 20020402 00141 NM 2002 4 2 SPAA0200050 1 20020324 A 5320 PANEL BOEING 737 7372T4 1384492 NM DELAMINATED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING PREFLIGHT, NOTED DELAMINATION ON LEFT WING UPPER SURFACE TRAILING EDGE FIXED PANEL. PANEL LOCATED BETWEEN AILERON AND #1 FLIGHT SPOILER PANEL 2 L 7 2 4F A16WE 2002040200142 20020402 00142 NM 2002 4 2 SPAA0200051 1 20020315 A 2700 654645258 PANEL BOEING 737 7372Y5 1384554 NM DELAMINATED A SPAA O OTHER O OTHER IN INSP/MAINT 1 WP 28 712S 23038 #5 SPOILER PANEL HAS AREAS OF DELAMINATION NOTED ON PREFLIGHT MAINTENANCE CHECK. 2 L 7 2 4U RT A16WE 2002042400080 20020424 00080 NM 2002 4 24 SPAA0200052 1 20020314 A 5753 PANEL BOEING 737 7372Y5 1384554 NM T/E FLAP DELAMINATED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 712S 23038 FOUND RT INBOARD TRAILING EDGE MIDFLAP WEDGE PANEL DELAMINATED. 2 L 7 2 4U RT A16WE 2002040800264 20020408 00264 EA 2002 4 8 COMA0260225 1 20020402 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 964CA 13476 7129 AREAS OF CORROSION NOTED ON LT AND RT FLOOR SUPPORT ANGLES BETWEEN FS 409.0+128 AND FS 559.0. REPAIRED IAW REO 601R-53- 41-079. 2 L 7 2 4F RT A21EA 2002040200143 20020402 00143 EA 2002 4 2 COMA0260226 1 20020402 A 5310 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FLOOR SUPPORT CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 964CA 13476 7129 65 FASTENERS REMOVED FROM LT AND RT FLOOR SUPPORT ANGLES BETWEEN FS 409.0+128 AND FS559.0.REPAIRED I/A/W REO 601R-53-41- 081. 2 L 7 2 4F RT A21EA 2002040200144 20020402 00144 NM 2002 4 2 AWXA200200269 1 20020310 A 5330 65C33756 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 0 0 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK 3 EACH .300" CRACKS WERE FOUND ON LOWER AFT RADIUS RIVET PATTERN OF R1 DOOR CUTOU T. MAINTENANCE CUTOUT CRACKED AREA OF SKIN, PERFORMED HFEC INSPECTION TO VERIFY CRACKS WERE CONTAINED, FABRICATED 2 EACH REPAIR DOUBLERS AND INSTALLED REPAIR PARTS AT R1 DOOR LOWER AFT CORNER IAW B737-300 SRM 53-10-01, FIG. 202, PG. 204-208 . 2 L 7 2 4F RT A16WE 2002040200145 20020402 00145 NM 2002 4 2 AWXA200200272 1 20020311 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATED CORROSION WAS FOUND ON AFT PIT FLOOR SUPPORT AT BS 860, LBL 12.5. MAIN TENANCE CLEANED CORROSION AND FOUND MATERAIL LOSS OUT OF LIMITS. FABRICATED AND INSTALLED 2 EACH REPAIR ANGLES IAW B737- 300 SRM 53-00-53, PG. 203, FIG. 201. 2 L 7 2 4F RT A16WE 2002040200146 20020402 00146 NM 2002 4 2 AWXA200200273 1 20020311 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON AFT CARGO PIT FLOOR SUPPORT NUT PLATE BS 860, RBL 2.5. MAI NTENANCE REMOVED NUT PLATE AND CORROSION AT BS 860, RBL 2.5. MATERAIL REMAINING .031, FABRICATED 2 EACH REPAIR ANGLES, H EAT TREATED, TRIMMED, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED ANGLES IAW B737-300 SRM 51-40-02, PG 1, 53-60-53 , PG 108, ASTM E797-95, 53-00-53, PG 201 AND 51-21-21, PG 703-705. 2 L 7 2 4F RT A16WE 2002040200147 20020402 00147 NM 2002 4 2 AWXA200200274 1 20020311 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON AFT CARGO PIT RT FLOOR SUPPORT BEAM BS 727D+6, RBL 7.5. MA INTENANCE REMOVED CORROSION AND MATERAIL REMAINING .039, FABRICATED 2 EACH REPAIR ANGLES FROM 7075-0.071, 7075-0-.081, H EAT TREATED IAW B737-300 SRM 53-00 FIG 201 SHT 1-3 & TPS-1003, TRIMMED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED AN GLES AT BS 727D+6, RBL 7.5 IAW B737-300 SRM 53-00-53 FIG 201, SHT 1-3. 2 L 7 2 4F RT A16WE 2002040300001 20020403 00001 NM 2002 4 3 SWAA020691 1 20020327 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 710SW 27844 EEPLS COVER MISSING AT ROW NR 9. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002040300002 20020403 00002 NM 2002 4 3 SWAA020694 1 20020401 A 5320 6546529 SHEAR TIE BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR'S 14L AND 15L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002040300003 20020403 00003 NM 2002 4 3 SWAA020695 1 20020401 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR'S 8R AND 9R. REPAIRED FRAME PER BFG ER.. 2 L 7 2 4F RT A16WE 2002040300004 20020403 00004 NM 2002 4 3 SWAA020696 1 20020401 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 774, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002040300005 20020403 00005 NM 2002 4 3 SWAA020697 1 20020401 A 5330 6545768 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 314, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002040300006 20020403 00006 NM 2002 4 3 SWAA020698 1 20020401 A 5330 6545774 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002040300007 20020403 00007 2002 4 3 SWAA020673 4 20020331 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002040300008 20020403 00008 NM 2002 4 3 SWAA020676 1 20020331 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) AT STR 8L, BS'S 380 AND 400. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2002040300009 20020403 00009 NM 2002 4 3 SWAA020677 1 20020331 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) AT STR 8R, BS'S 360, 400 AND 440. REPAIRED FRAMES PER BF G ER. 2 L 7 2 4F RT A16WE 2002040300010 20020403 00010 NM 2002 4 3 SWAA020678 1 20020331 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR'S 8R AND 9R, BS'S 787 AND 827. REPAIRED FRAM ES PER BFG ER. 2 L 7 2 4F RT A16WE 2002040300011 20020403 00011 NM 2002 4 3 SWAA020679 1 20020331 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR'S 8L AND 9L, BS'S 727D AND 787. REPAIRED FRA MES PER BFG ER. 2 L 7 2 4F RT A16WE 2002040300012 20020403 00012 NM 2002 4 3 SWAA020680 1 20020331 A 5330 6545768 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 4 INCHES AT BS 314, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002040300013 20020403 00013 NM 2002 4 3 SWAA020681 1 20020330 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED 3 INCHES AT BS 545, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002040300014 20020403 00014 NM 2002 4 3 SWAA020682 1 20020331 A 3350 20131A BATTERY BOEING 737 7373Q8 1384670 NM CABIN ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT WILL NOT STAY ILLUMINATED. REMOVED AND REPLACED BATTERY PE R MM. 2 L 7 2 4F RT A16WE 2002040300015 20020403 00015 NM 2002 4 3 SWAA020683 1 20020330 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002040300016 20020403 00016 NM 2002 4 3 SWAA020684 1 20020330 A 5330 65C33288 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED A2 CHECK, FOUND INTERCOSTAL CRACKED AT STR 10R, ONE INCH AFT OF FWD SVC DOOR. REPAIRED INTERCOSTAL PER SWA ACO. 2 L 7 2 4F RT A16WE 2002040300017 20020403 00017 NM 2002 4 3 SWAA020685 1 20020331 A 5210 6545871 FRAME BOEING 737 7373G7 1384595 NM FWD ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR AFT FRAME CRACKED AT 7TH FROM TOP STOP PIN FITTING. REPAIRED FRAME PE R SWA RA. 2 L 7 2 4F RT A16WE 2002040300018 20020403 00018 NM 2002 4 3 SWAA020686 1 20020331 A 5315 6546804 FLOORBEAM BOEING 737 7373G7 1384595 NM MID CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 663, BL-0. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002040300019 20020403 00019 2002 4 3 SWAA020654 4 20020327 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE, BOTH FWD AND AFT GIRT BAR BRACKETS CORRODED. REMOV ED AND REPLACED BRACKETS PER MM. 2 L 7 2 4F RT A16WE 2002040300020 20020403 00020 2002 4 3 SWAA020656 4 20020329 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 741SA 29277 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002040300021 20020403 00021 NM 2002 4 3 SWAA020657 1 20020328 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 713SW 27847 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002040300022 20020403 00022 NM 2002 4 3 SWAA020658 1 20020327 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 710SW 27844 EEPLS COVER MISSING AT ROW NR 9. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002040300023 20020403 00023 NM 2002 4 3 SWAA020660 1 20020330 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 502SW 24179 EEPLS COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2002040300024 20020403 00024 NM 2002 4 3 SWAA020661 1 20020329 A 3350 6042221 BATTERY BOEING 737 7373H4 1384600 NM CABIN ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED RON, FOUND BOTH FWD CABIN DOOR EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED AFTER SW IS TURNED OFF. REMOVE D AND REPLACED LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002040300025 20020403 00025 NM 2002 4 3 SWAA020663 1 20020328 A 5330 6545819122 SKIN BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED C1 CHECK, FOUND NLG W/W SKIN CRACKED AT AFT OTBD CORNER OF LT NOSE TIRE BRAKE PAD ATTACH POINT. REPAIR ED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2002040300026 20020403 00026 NM 2002 4 3 SWAA020664 1 20020328 A 5315 6545410 FLOORBEAM BOEING 737 7373G7 1384595 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED FROM BS 793 TO 825, LBL 3. REPAIRED FLOORBEAM PER SR M. 2 L 7 2 4F RT A16WE 2002040300027 20020403 00027 NM 2002 4 3 SWAA020667 1 20020330 A 5315 BAC1509 FLOORBEAM BOEING 737 7373G7 1384595 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED FROM BS 770 TO 846, LBL 8.0. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002040300028 20020403 00028 NM 2002 4 3 SWAA020669 1 20020328 A 5315 6545410 FLOORBEAM BOEING 737 7373G7 1384595 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED FROM BS 757 TO 947, RBL 12.0. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2002040300029 20020403 00029 NM 2002 4 3 SWAA020670 1 20020328 A 5241 6545871 FRAME BOEING 737 7373G7 1384595 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED AT CUTOUT FOR 4TH FROM TOP STOP PIN FITTING. REPAIRED FRAME PER SWA T1-152-003. 2 L 7 2 4F RT A16WE 2002040300030 20020403 00030 NM 2002 4 3 SWAA020671 1 20020328 A 5312 6516300 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND LBL 11.0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002040300031 20020403 00031 NM 2002 4 3 SWAA020672 1 20020328 A 5330 5898357 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/4D CHECK, FOUND CAPTIAN'S WINDOW POST SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002040300032 20020403 00032 NM 2002 4 3 SWAA020668 1 20020327 A 5312 6517582 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED (2 EA) AT BS 183, WL 183, LBL 17.1 AND RBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002040300033 20020403 00033 EA 2002 4 3 COMA0260227 1 20020402 A 5310 STRAP CNDAIR CL600 CL6002B19 1900309 EA FLOOR SUPPORT CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 964CA 13476 7129 TWO FLOOR SUPPORT STRAPS CORRODED TO THE POINT THAT REPLACEMENT IS REQUIRED.REPAIRED I/A/W REO 601R-53-41-080. 2 L 7 2 4F RT A21EA 2002040300034 20020403 00034 EU 2002 4 3 02091326 1 20020201 A 7600 745162407 CABLE JETAIR JETSTM JETSTM4101 1500501 EU A VTZA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CR CRUISE 1 EA 27 326UE 41064 During cruise of the flight from IAD to ROA, the crew noted that R/H engine throttle was stuck. The crew followed the Q RH procedures, returned to IAD, and shut down the R/H engine prior to the approach. Maintenance personnel removed and r eplaced the flex cable for the R/H engine power lever. Operational checks were satisfactory and the aircraft was return ed to service. 2 L 7 2 4T RT A41NM 2002040300035 20020403 00035 EA 2002 4 3 SWIA200210717 1 20020308 A 2740 STABILIZER CNDAIR CL600 CL6002B19 1900309 EA TAIL BINDING A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 406SW 7030 MACH TRIM AND STAB CH 1 INOP MESSAGES INFLIGHT. COULD NOT REENGAGE. RETURNED TO SLC. STAB PIVOT BOLTS BINDING - EXCES SIVE FORCE NEEDED TO MOVE STABILIZER. HORIZONTAL STABILIZER REMOVED FOR REPAIR/MAINT OF BUSHING AT MAIN PIVOTS. STABIL IZER - TEST, LUBRICATION, AND REWORK OF PIVOT PINS AND BUSHINGS PER SB. OPS CHECKS, FUNCTIONAL CHECKS AND LEAK CHECKS G OOD. REMOVED AND REPLACED THE HSTA AND MOTOR CONTROL UNIT IAW CRJ MM 27-42-01 AND 27-42-05. OPS CHECK GOOD. A/C IS OK FOR CAT II OPERATIONS. 2 L 7 2 4F RT A21EA 2002040300036 20020403 00036 NM 2002 4 3 SWAA020523 1 20020310 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002040300037 20020403 00037 NM 2002 4 3 SWAA020527 1 20020310 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM RT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED D-CHECK, FOUND RIGHT INBOARD AFT T/E FLAP DEBONDED 37 INCHES OUTBOARD OF INBOARD END. REPAIRED FLAP PE R SRM. 2 L 7 2 4F RT A16WE 2002040300038 20020403 00038 NM 2002 4 3 SWAA020528 1 20020310 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002040300039 20020403 00039 NM 2002 4 3 SWAA020533 1 20020311 A 5240 6523465 FITTING BOEING 737 7375H4 138449D NM R1 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 FWD SERVICE DOOR UPPER ATTACH CONTROL ARM FITTING BROKEN. REMOVED AND REPLACED CONTROL ARM FITTING PER MM. 2 L 7 2 4F RT A16WE 2002040300040 20020403 00040 2002 4 3 SWAA020534 4 20020311 A 2565 D313591 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 507SW 24184 FWD ENTRY DOOR EVACUATION SLIDE PRESS IND OUT OF LIMIT. REMOVED AND REPLACED EVACUATION SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2002040300041 20020403 00041 2002 4 3 SWAA020538 4 20020311 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 AFT SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002040300042 20020403 00042 NM 2002 4 3 SWAA020551 1 20020312 A 3350 BR2013 CONNECTOR BOEING 737 7377AD NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 798SW 28436 DURING SCHEDULED RON, FOUND EEPLS INOP BETWEEN ROWS 16 AND 20. SEATED EEPLS CONNECTOR AND OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2002040300043 20020403 00043 NM 2002 4 3 SWAA020552 1 20020313 A 2130 5416744 ACTUATOR BOEING 737 7373H4 1384600 NM A/C BAY FAILED A SWAA K NONE J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 368SW 26579 DURING T/O RT PACK WENT HOT, F/A REPORTED HOT SMELL, NO SMOKE. SMELL WENT AWAY AS CLIMB PROGRESSED. SMELL RETURNED AFT ER FLAPS EXTENDED FOR LANDING. REMOVED AND REPLACED RAM AIR DOOR ACTUATOR AND CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2002040300044 20020403 00044 2002 4 3 SWAA020553 4 20020313 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002040300045 20020403 00045 2002 4 3 SWAA020559 4 20020317 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002040300046 20020403 00046 NM 2002 4 3 SWAA020560 1 20020317 A 3350 1000679 LIGHT BOEING 737 7372K6 1364440 NM SERVICE DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED A2 CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002040300047 20020403 00047 2002 4 3 SWAA020561 4 20020315 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002040300048 20020403 00048 NM 2002 4 3 SWAA020570 1 20020316 A 5240 6555478 GATE BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR LOWER GATE CRACKED .500 INCH AT AFT EDGE. REPAIRED LOWER GATE ASSY PER SW A RA. 2 L 7 2 4F RT A16WE 2002040300049 20020403 00049 NM 2002 4 3 SWAA020571 1 20020317 A 3350 57771 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 751SW 29803 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LOOSE AT ROW NR 1. REMOVED AND REPLACED END CAP AND SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002040300050 20020403 00050 NM 2002 4 3 SWAA020572 1 20020314 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 646SW 28331 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE TO EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002040300051 20020403 00051 EA 2002 4 3 01091665 1 20020401 A 7110 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA NR 1 ENGINE OUT OF POSITION A VTZA E A ENGINE SHUTDOWN UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 EA 27 665BR 7534 DURING CRUISE OF THE FLIGHT, THE CREW NOTED THAT THE NR 1 ENGINE THRUST LEVER HAD JAMMED. THE CREW FOLLOWED THE QRH AND SHUT THE ENGINE DOWN PRIOR TO THE APPROACH. MAINTENANCE PERSONNEL FOUND THAT THE HOLD OPEN STRUT FOR THE NR 1 ENGINE U PPER CORE COWL HAD BECOME UNSECURED FROM THE STOWED POSITION AND WAS INTERFERING WITH THE THRUST LEVER LINKAGE. THE SUP PORT WAS STOWED, ENGINE RUN OPERATIONAL CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002040300052 20020403 00052 NM 2002 4 3 200200190 1 20020402 A 5711 SPAR BOEING 747 747121 1384871 NM CENTER WING CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 480EV 20348 REPAIR OF CORROSION ON WCS REAR SPAR WEB AT RBL 98.55. THE CORROSION WAS BLENDED PER B747 SRM 57-10-01. 2 L 7 4 4F A20WE 2002040300053 20020403 00053 NM 2002 4 3 200200191 1 20020402 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DENTED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 480EV 20348 EXTERIOR FUSELAGE STATION 2020 BETWEEN STR 44L TO 45L 12 INCH DENT. CUTOUT DAMAGED AREA, FABRICATED DOUBLER AND FILLERS PER B747 SRM. 2 L 7 4 4F A20WE 2002040300054 20020403 00054 NM 2002 4 3 200200192 1 20020402 A 5330 SKIN BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 SKIN CUTOUT AND CRACK DAMAGE AT BS 2210-2220, S35L-S37L. THE SUBJECT DAMAGE IS LOCATED COMMON TO BSB 747-53-2063 OUTFLO W VALVE CUTOUT REINFORCEMENT DOUBLER. REPAIR INSTALLED PER B747 SRM REPAIR PRACTICES. 2 L 7 4 4F A20WE 2002040300055 20020403 00055 NM 2002 4 3 200200193 1 20020402 A 5311 FRAME BOEING 747 747132 1384882 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 CORROSION AND SHORT EDGE MARGINS IN BS 340, 360 & 380 FRAME. CORROSION WAS FOUND IN THE HOLES COMMON TO THE FRAMES AND THE UPPER DECK FLOORBEAM UPPER CHORDS AT BS 340 & 360, LT & RT AND BS 360 RIGHT. THE HOLES WERE OVERSIZED TO REMOVE COR ROSION CAUSING A SHORT EDGE MARGIN BS 360 LEFT. 2 L 7 4 4F A20WE 2002040300056 20020403 00056 NM 2002 4 3 200200194 1 20020402 A 5720 SUPPORT BOEING 747 747132 1384882 NM WING DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 DAMAGED LOWER CHORD AND WEB OF TRAILING EDGE SUPPORT BEAM. TRIMMED OUT THE DAMAGE AREAS AND INSTALLED STRAPS, FILLERS A ND DOUBLERS PER ECRA 479-57-160-2. 2 L 7 4 4F A20WE 2002040300057 20020403 00057 NM 2002 4 3 P5CA0200669 1 20020330 A 5230 NONE SKIN BOEING 747 74746NF 13848BT NM LWR CARGO DOOR DENTED A P5CA K NONE O OTHER UK UNKNOWN 1 WP 23 451PA 30809 LOWER AFT EDGE SKIN OF AFT LWR CARGO DOOR DENTED IN BY CONTACT WITH GROUND EQUIPMENT. TRANSFERRED TO COI #451-013 PER MX CTRL (JOHN). NO FURTHER DISCREPANCIES NOTED. OK FOR CONTINUED SERVICE. COMPLETED REPAIR AT NEXT STATION (MIA) ON AFT CA RGO DOOR PER SRM 52-00-01, P 209. COI #451-013 CLEARED. 2 L 7 4 4F RT A20WE 2002040300058 20020403 00058 NM 2002 4 3 200200195 1 20020402 A 5711 SPAR BOEING 747 747132 1384882 NM CENTER WING CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 CORROSION ON BS 1241 WCS REAR SPAR WEB AT LBL 80. THE CORROSION WAS BLENDED PER SRM. 2 L 7 4 4F A20WE 2002040300059 20020403 00059 NM 2002 4 3 QXEA0200534 1 20020402 A 2840 FUEL DOOR BOMBDR DHC8 DHC8401 NM OPEN A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 401QX 4031 SEA - FUELING ON CAUTION LIGHT ILLUMINATED WHEN POWER WAS APPLIED FOR TAKE-OFF. TAKE-OFF WAS ABORTED. MAINTENANCE INSPEC TED THE AIRCRAFT AND FOUND THE OUTBOARD LATCH ON THE FUEL DOOR OPEN. THE LATCH WAS INSPECTED AND FOUND TO BE SERVICABLE AND WAS RESECURED. WARNING LIGHT WAS VERIFIED TO BE OUT AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002040300060 20020403 00060 NM 2002 4 3 200200196 1 20020402 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 CORROSION ON BS 400 FLOORBEAM AT RBL 70. SECTION OF FLOORBEAM UPPER AFT CHORD IS SPLICED IN FROM RBL 30 TO THE RT SIDE OF BODY PER ECRA 479-53-161-2. 2 L 7 4 4F A20WE 2002040300061 20020403 00061 NM 2002 4 3 200200197 1 20020403 A 5753 FITTING BOEING 747 747132 1384882 NM T/E FLAP GOUGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 GOUGE, NR 5 FLAP TRACK FWD FITTING, FAIL-SAFE BORE HOLE. THE GOUGE IS COMMON TO THE UPPER SURFACE OF THE BORE AT NEAR M IDPOINT. REPAIR IS ACCOMPLISHED BY LOCAL BLENDING. 2 L 7 4 4F A20WE 2002040300062 20020403 00062 NM 2002 4 3 200200198 1 20020403 A 5320 WEB BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 REPAIR OF CRACK IN SECTION 41 FLOOR WED AT BS 140, LBL 38. THE CRACKED SECTION IS REPAIRED BY TRIMMING AWAY THE DAMAGED PORTION OF WEB, AND SPLICING IN A NEW SECTION OF WEB WITH A REPAIR DOUBLER PER B747 SRM. 2 L 7 4 4F A20WE 2002040300063 20020403 00063 WP 2002 4 3 2002F00346 1 20020227 A 5310 SHEAR TIE LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION, FORWARD FUSELAGE SECTION, SHEAR TIE AT FS 297, RBL 8 TO 32 RIGHT WAS CORRODED, LEVEL 2 CORR OSION. MAINTENANCE REMOVED AND REPLACED SHEAR TIE IAW SRM 53-12-00 FIG 805. 2 L 7 3 4F A23WE 2002040300064 20020403 00064 NM 2002 4 3 SWAA020576 1 20020317 A 5610 5893543130 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 396SW 27690 AIR TURNBACK, F/O'S FRONT WINDOW SHATTERED AT FC 310. REMOVED AND REPLACED F/O'S FRONT WINDOW AND CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2002040300065 20020403 00065 NM 2002 4 3 SWAA020583 1 20020319 A 7931 APTE8A20007BARD SENSOR BOEING 737 7377H4 1384404 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A SWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 414WN 29820 888606 ABORTED TAKEOFF, NR 2 ENGINE WOULD NOT RESPOND TO THRUST LEVER MOVEMENT. REMOVED AND REPLACED OIL PRESS SENSOR PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040300066 20020403 00066 NM 2002 4 3 SWAA020584 1 20020318 A 5240 6552873 SERVICE DOOR BOEING 737 7373H4 1384600 NM AFT OUT OF RIG A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 395SW 27689 AIR TURNBACK, DURING CLIMB AIRCRAFT WOULD NOT PRESSURIZE. FOUND AFT SVC DOOR OUT OF RIG. RIGGED DOOR, OPS CHECK GOOD P ER MM. 2 L 7 2 4F RT A16WE 2002040300067 20020403 00067 2002 4 3 SWAA020585 4 20020319 A 2565 61624469 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 363SW 26574 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002040300068 20020403 00068 2002 4 3 SWAA020586 4 20020319 A 3418 861CAS3 VANE BOEING 737 7373H4 1384600 NM AOA BENT A SWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 339SW 24090 AIR TURNBACK, CAPT'S STALL WARNING CONTROL COLUMN ACTIVATED. FOUND AOA VANE BENT. REMOVED AND REPLACED AOA VANE PER MM . 2 L 7 2 4F RT A16WE 2002040300069 20020403 00069 NM 2002 4 3 SWAA020587 1 20020319 A 2913 887477 PUMP BOEING 737 7377H4 1384404 NM HYD SYSTEM FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 765SW 29805 AIR TURNBACK, A-SYSTEM, ELECTRIC HYD PUMP FAILURE. REMOVED AND REPLACED A-SYSTEM HYD PUMP AND CASE DRAIN FILTER PER MM. 2 L 7 2 4F RT A16WE 2002040300070 20020403 00070 NE 2002 4 3 UIA02001 2 20020228 A 7260 28B5278A BEARING DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE NR 2 ENGINE DAMAGED Z O OTHER J WARNING INDICATION CL CLIMB 1 TW 00 17921 7616 2076 53554 V20109 FLT 6182 FROM KNH TO TSA, PILOT REPORT R AC POWER FAULT SHOW ON EOAP AFTER LANDING MECHANIC CHECK FOUND BEARING DAMAGE O F ENGINE GEAR BOX, IAW AMM71-00-00. REPLACED NR 2 ENGINE IAE WOULD VERIFY THE ROOT CAUSE OF THE BEARING DAMAGE OF ENGIN E GEAR BOX. 2 L 7 2 4F 4 F RT A6WE A40NE 2002040300078 20020403 00078 WP 2002 4 3 UPS02837494 1 20020109 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 BANANA FITTING STA 1160 CRACKED INSIDE TORQUE BOX LONG 33R. PERFORMED HFEC IAW DOUGLAS IPM 06-10-01 -001 AND FOUND CRACK. REMOVED CRACKED BANANA FITTING. INSTALLED FITTING SUPPORT ANGLES AND END FITTING IAW DC8 SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 2002040300080 20020403 00080 WP 2002 4 3 UPS02837496 1 20020110 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 AFT PIT FS 1152 FITTING AT L31R L33R IS CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW BANANA F ITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040300086 20020403 00086 WP 2002 4 3 UPS02837518 1 20020115 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 LT LONG ATTACH FITTING HAS CORROSION. REMOVED DAMAGED FITTING AND INSTALLED NEW FITTING AND REPAIR IAW DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2002040300087 20020403 00087 WP 2002 4 3 UPS02837526 1 20020109 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 BANANA FITTING STA 1160 CRACKED INSIDE TORQUE BOX LONG 33R. 2 L 7 4 4F RT 4A25 2002040300088 20020403 00088 WP 2002 4 3 UPS02837527 1 20020110 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C23 AFT PIT FS 1152 FITTING AT L31R - L33R IS CRACKED. REMOVED CRACKED BANANA FITTING AND INSTALLED NEW BANANA FITTING. 2 L 7 4 4F RT 4A25 2002040300090 20020403 00090 WP 2002 4 3 UPS02837549 1 20020131 A 2560 CONTAINER DOUG DC8 DC871F 302199D WP CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:PFLT REF M231085 SLIDE ASSY OUT OF DOOR, BAR HOLDER BROKEN OFF OF CONTAINER. REMOVED AND REPLACED SLIDE EVAC CONTAINER. REINSTALLED SAME SLIDE ASSY INTO CONTAINER PER MM 25-60-01 3B, P/N ON & OFF-5750113-505, S/N ON-TAG645 594A. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2002040300091 20020403 00091 WP 2002 4 3 UPS02837554 1 20020201 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CABIN FALSE ACTIVATION A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:N/A AT ENGINE START ALL MAIN DECK SMOKE DET LIGHTS ILLUMINATED. PERFORMED ADJ TEST OF SMOKE DETECTOR SY S PER MM 26-10-05, SYS TEST NORMAL. 2 L 7 4 4F RT 4A25 2002040300092 20020403 00092 WP 2002 4 3 UPS02837559 1 20020131 A 2913 PUMP DOUG DC8 DC873F 302199F WP NR 2 & 3 ENGINE FAILED A IPXA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 880UP 46080 INSPECTION TYPE:N/A AFTER 2 HOURS IN FLIGHT LOST HYD QUANTITY TO STANDPIPE LEVEL, FOLLOWED EMERGENCY PROCEDURES, LANDING NORMAL FLAPS 23. REMOVED AND REPLACED NR 2 AND NR 3 ENGINE DRIVEN PUMPS AND ASSOCIATED FILTERS. 2 L 7 4 4F RT 4A25 2002040300093 20020403 00093 WP 2002 4 3 UPS02837564 1 20020204 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:N/A EMERGENCY LIGHTS DIM ON TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-01, T EST OK. 2 L 7 4 4F RT 4A25 2002040300094 20020403 00094 NM 2002 4 3 02FDEA00177 1 20020304 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 HOLES IN FLOORBEAM BS 1150, BL0, WL 208.1. R&R FLOORBEAM PER SRM 53-10-8 FIG 3. 2 L 7 3 4F RT A3WE 2002040300095 20020403 00095 NM 2002 4 3 02FDEA00224 1 20020331 A 5610 B275600102A WINDOW BOEING 727 727233 138408A NM COCKPIT LOOSE A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 221FE 20932 AFTER ROTATION F/O WINDOW POPPED AJAR WINDOW, OUT OF RIG. R/R R-2 SLIDING WINDOW PER MM 56-12-011-4. 2 L 7 3 4F RT A3WE 2002040300096 20020403 00096 NM 2002 4 3 200200188 1 20020401 A 5320 WEB BOEING 747 747121 1384871 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 480EV 20348 REPAIR OF CORROSION ON WCS CANTED WEB AT RBL 65. THE CORROSION WAS REMOVED BY TRIMMING AWAY THE DAMAGED SECTION OF WEB PER B747-51-10-01 GUIDELINES. THE WEB IS BEING REPAIRED BY INSTALLING REPAIR DOUBLERS. 2 L 7 4 4F A20WE 2002040300097 20020403 00097 NM 2002 4 3 200200189 1 20020401 A 5720 ANGLE BOEING 747 747121 1384871 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 480EV 20348 REPAIR OF CORROSION ON BS 1241 PRESSURE WEB ANGLE. THE CORROSION WAS REMOVED BY TRIMMING AWAY THE DAMAGED SECTION OF PRE SSURE WEB ANGLE AT APPROXIMATELY LBL 80 AND RBL 70. 2 L 7 4 4F A20WE 2002040300098 20020403 00098 2002 4 3 2002F00347 4 20020320 A 2330 110308010 ENCODER LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE G AMTA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 GL 11 161AT 62836 62836 293A1219 FLIGHT 5027, DURING CRUISE AT FL 330, SENIOR FLIGHT ATTENDANT REPORTED UNIDENTIFIED FUMES AT REAR LEFT SIDE OF "A" ZONE. NO SMOKE VISIBLE. PASSENGER REPORTED SIMULTANIOUS LOSS OF AUDIO ENTERTAINMENT. THE AIRCRAFT WAS FERRIED FROM YQX TO IND . MAINTENANCE AT IND REMOVED AND REPLACED THE MUX ENCODER BELOW SEAT 9D AND PERFORMED AN OPERATIONAL CHECK. 2 L 7 3 4F A23WE 2002040300099 20020403 00099 WP 2002 4 3 2002F00349 1 20020224 A 5311 FRAME LKHEED 1011 10113851 5265010 WP FUSELAGE CRACKED G K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION MAIN FRAME, SPLICE ANGLE AND STRAP FOR FS 328 FRAMES WHERE FOUND TO BE CRACKED. 3 CRACKS WER E DISCOVERED AND EACH CRACK WAS 2.00 INCHES IN LENGTH. MAINTENANCE FABRICATED SPLICE ANGLE AND STRAP FOR FS 328 AFT SIDE OF CHORD CTR. INSTALLED SPLICE ANGLE AND STRAP PER L-1011 SRM 51-40-01. 2 L 7 3 4F A23WE 2002040300100 20020403 00100 WP 2002 4 3 2002F00350 1 20020315 A 5320 SUPPORT LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED G K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION CABIN FLOORBEAM SUPPORT AT FS 1523, WL 195, RBL 83 HAD LEVEL 2 CORROSION. MAINTEANCE COMPLI ED WITH AMTA ERA L10-53R-4737 FS 1523 FLOORBEAM SUPPORT MODIFICAITON. 2 L 7 3 4F A23WE 2002040300101 20020403 00101 SW 2002 4 3 2002F00351 1 20020202 A 5230 HANDLE SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR STUCK A BSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 27465 AC755B FLT 1303 - HOT - JUST AFTER TAKEOFF UPON ROTATION, THE CARGO DOOR WARNING LIGHT CAME ON. CREW DID A GO AROUND AND RETUR NED TO STATION. STICKY HANDLE OR CLICK, OR DOOR CLOSING PROCEDURES. CLEANED AND LUBED CLICK CLACKS. (M) 2 L 7 2 4T RT A8SW 2002040300103 20020403 00103 SW 2002 4 3 2002F00352 1 20020130 A 5230 LATCH SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR STUCK A BSAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 NM 05 159MC AC728B CARGO DOOR LIGHT CAME ON DURING TAKEOFF ROLL AT APPROXIMATELY 50 KTS. CREW RETURNED TO GATE. STICKING DOOR HANDLE OR C LICK CLACKS. CLEANED AND LUBED CLICK CLACKS. (M) 2 L 7 2 4T RT A8SW 2002040300104 20020403 00104 SW 2002 4 3 2002F00353 1 20020129 A 5210 SEAL SWRNGN SA227 SA227AC 8780603 SW PAX DOOR DAMAGED A BSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 702M AC702 DEN - FLT 1314 - CABIN ALTITUDE WARNING LIGHT CAME ON ABOVE 10,000 FEET. CREW COULD NOT GET AIRCRAFT TO PRESSURIZE IN E ITHER AUTOMATIC OR MANUAL MODE. CREW RETURNED TO STATION. PASSENGER DOOR SEAL WAS DAMAGED. INITIALLY DEFERRED PRESSUR IZATION, THEN LATER REPLACED CABIN DOOR SEAL. (M) 2 L 7 2 4T RT A8SW 2002040300105 20020403 00105 SW 2002 4 3 2002F00354 1 20020122 A 2910 SS1009H000A441 LINE SWRNGN SA227 SA227AC 8780603 SW HYD SYSTEM RUPTURED A BSAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 05 160MC AC733B THE RT HYD PRESS LIGHT CAME ON DURING CRUISE AND THE LT HYD PRESS LIGHT CAME ON DURING DESCENT. THE FLAPS EXTENDED SLOW LY, CREW DECLARED EMERGENCY, USED THE GEAR EMERGENCY EXTEND SYS. LANDING WAS COMPLETED WITHOUT INCIDENT. RT ENG HYD PU MP PRESSURE LINE HAD FAILED. LINE WAS REPLACED. (M) 2 L 7 2 4T RT A8SW 2002040300107 20020403 00107 SW 2002 4 3 2002F00356 1 20020114 A 2900 LINE SWRNGN SA227 SA227AC 8780603 SW HYD SYSTEM LEAKING A BSAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 05 27465 AC755B DFW - FLT 1302 - ONE HUNDRED THIRTY MILES FROM ORGINATING STATION, AIRCRAFT LOST HYDRAULIC PRESSURE. CREW RETURNED TO S TATION AT MAX GEAR EXTENSION SPEED. GEAR WAS PUMPED DOWN USING EMERGENCY CHECKLIST. HYDRAULIC LEAK CAUSED LOSS OF HYDR AULIC FLUID LEADING TO LOSS OF HYDRAULIC PRESSURE. REPAIRED LINE BY SPLICING IN NEW SECTION PER MM. BOTH HYDRAULIC PUM PS CHANGED DUE TO EXCEEDING MM RESTRICION ON LENGTH OF TIME THE PUMPS CAN RUN WITHOUT FLUID. (M) 2 L 7 2 4T RT A8SW 2002040300109 20020403 00109 SW 2002 4 3 2002F00359 1 20020108 A 2150 20475546 ACM SWRNGN SA227 SA227AC 8780603 SW ACM BAY FAILED A BSAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 05 158MC 437 FCA - FLT 2582 - THE RIGHT BLEED AIR STARTED MAKING SMOKE IN THE CABIN. SUSPECTED RT ACM FAILED. INTERMIM REPORT INITI ALLY DEFERRED RT ACM. FOUND RT ACM SEIZED. REPLACED ACM. TEARDOWN REPORT STATED THE BEARING WERE DRY, WADDING WAS DRY , BUT THE WICK WAS NORMAL. THE TEARDOWN REPORT STATED IT WAS SUSPECTED THAT EITHER THE INITIAL AND SUBSEQUENT SERVICING WAS NOT DONE CORRECTLY. A MEMO ON THIS SUBJECT WAS ISSUED. THIS ISSUE WITH PERSONNEL INVOLVED. (M) 2 L 7 2 4T RT A8SW 2002040300122 20020403 00122 WP 2002 4 3 AALA20020165 1 20020220 A 2560 P2070003001 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7548A 53030 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED FORWARD ENTRY EME RGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040300123 20020403 00123 WP 2002 4 3 AALA20020166 1 20020220 A 2560 P2070003001 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 274AA 49271 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED FORWARD ENTRY EME RGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040300124 20020403 00124 WP 2002 4 3 AALA20020167 1 20020220 A 3350 BATTERY DOUG DC9 DC982 3022082 WP GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 283AA 49296 DFW - DURING OVERNIGHT MAINTENANCE, COCKPIT AND FORWARD ENTRANCE AND GALLEY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED COCKPIT AND FORWARD ENTRANCE AND GALLEY EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040300125 20020403 00125 NM 2002 4 3 AALA20020169 1 20020223 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - DURING OVERNIGHT MAINTENANCE, FOUND FIRST CLASS GALLEY WALL MOUNTED EMERGENCY LIGHT 1R INOPERATIVE. REPLACED WALL MOUNTED LIGHT ASSEMBLY AT 1R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002040300126 20020403 00126 WP 2002 4 3 AALA20020175 1 20020221 A 3350 P4010049 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 435AA 49453 DFW - DURING OVERNIGHT MAINTENANCE, EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EXTERIOR OVERWING EME RGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002040300127 20020403 00127 WP 2002 4 3 ABXA010810 1 20020318 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 FUSELAGE SKIN FLUSH REPAIR BULGING OUTWARD AND HAD RIVETS INSTALLED INTO RIVETS, STATION 379, BETWEEN LONGERON 2 - 3 RIG HT. REPAIRED AREA IAW DC-9 SRM 53-04. 2 L 7 2 4F A6WE 2002040300128 20020403 00128 WP 2002 4 3 ABXA010812 1 20020321 A 5320 59560654 PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 LEVEL I CORROSION UNDER 10 EACH LOWER FLOATING NUT PLATES ON LEFT SLANT PANEL. REMOVED AND REPLACED THE LEFT SLANT PANEL IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 2002040300129 20020403 00129 WP 2002 4 3 ABXA010813 1 20020321 A 5320 595606543 PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 LEVEL I CORROSION UNDER 8 EACH LOWER FLOATING NUT PLATES ON THE RIGHT SLANT PANEL. REMOVED AND REPLACED THE RIGHT SLANT PANEL IAW DC-9 SRM 51-30-2, 51-30-1 AND 51-20-0. 2 L 7 2 4F A6WE 2002040300131 20020403 00131 EA 2002 4 3 ASOA02117 1 20020228 A 3350 487190 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 828AS 4605 7213 FLT 4605 - DURING GROUND INSPECTION IN CAK, THE FLOOR PATH EMERGENCY LIGHTING JUST AFT OF THE WING EMERGENCY EXIT WAS IN OPERATIVE. MAINTENANCE FOUND THE ELECTRIC CABLE CONNECTING TO THE AFT MOST FLOOR LIGHT STRIP DAMAGED AND SHORTED. MAIN TENANCE REMOVED AND REPLACED THE FLOOR EMERGENCY LIGHTING WIRING PIG TAIL CONNECTOR AT ROW 12. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002040300132 20020403 00132 NM 2002 4 3 AWXA200200256 1 20020329 A 7722 AW71500042 WIRE HARNESS BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 ENGINE DEFECTIVE A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 328AW 23377 720388 AIR TURN BACK - FLT 0332 - AFTER T/O ENROUTE FROM OMA TO PHX, NR 2 ENGINE EGT FLUXUATED FULL SCALE FROM 0 TO 1250, RED LIGHT CAME ON AND DIGITS DISAPPEARED, FLUXUATED BACK TO 0 AND DIGITS DISAPPEARED AGAIN. IN LIGHT CHOP TO SMOOTH CONDIT IONS EGT GAUGE FAILED INTERMITTENTLY THROUGH OUT RETURN TO OMA, EGT DID NOT RESPOND TO THROTTLE MOVEMENT, NR 1 ENGINE O PERATED NORMALLY. NOTE: AIRCRAFT EXPERIENCED NR 2 ENGINE EGT OVERTEMP IN LIGHT TO MODERATE TURBULANCE (5 SECONDS) ON PRE VIOUS FLT INTO OMA (FLT 0512), MAINTENANCE REMOVED AND REPLACED 2 EACH WIRING HARNESSES IAW BMM 77-21-01-4 FOR THIS EVE NT. (FLT 0332) MAINTENANCE PERFORMED 70 PERCENT POWER RUN, NR 2 EGT WENT FROM NORMAL TO 1250 DEGREES C TO 0 DEGREES C A 2 L 7 2 4F 4 F RT A16WE E21EU 2002041200079 20020412 00079 2002 4 12 AWXA200200258 4 20020331 A 3416 4039892904 ALTIMETER BOEING 757 757225 1384959 NM COCKPIT DEFECTIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 907AW 7619 1123 22691 CMH - DIVERSION - FLT 0081 - EN ROUTE FROM PHX TO BWI FIRST OFFICERS ALTIMETER FLAG DISPLAYED, TURNING BAROMETRIC KNOB MOVES MB AND HG DRUMS BUT ALTIMETER NEEDLE DOES NOT MOVE. DUE TO WEATHER AHEAD DIVERTED TO CMH. MAINTENANCE REMOVED AN D REPLACED FIRST OFFICERS ALTIMETER IAW BMM 34-13-01-4 PG 1 & 2. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002040300133 20020403 00133 EU 2002 4 3 AWXA200200259 1 20020331 A 2910 2261024 O-RING AIRBUS 320 A320232 3930326 EU YELLOW HYD SYS LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 28 655AW 1075 PHX - EMERGENCY - FLT 0005 - YELLOW HYDRAULIC SYSTEM INDICATED LOW PRESSURE AND QUANTITY, MADE NORMAL LANDING, BUT BRAK ES OVERHEATED. INSPECTION OF HOT BRAKES. AFTER BRAKES INSPECTED TAXIED TO GATE, HYDRAULIC QUANTITY WHEN AIRCRAFT TAXIE D IN WAS "0". BELLY OF AIRCRAFT SOAKED WITH FLUID FROM W/W BACK. MAINTENANCE FOUND QUICK DISCONNECT FITTING LEAKING AT P OWER TRANSFER UNIT. REPLACED O-RING IN QUICK DISCONNECT FITTING, SERVICED YELLOW HYDRAULIC SYSTEM TO FULL AND PRESSURIZE D SYSTEM, NO LEAKS NOTED. 2 L 7 2 4F RT A28NM 2002040300134 20020403 00134 NM 2002 4 3 AWXA200200262 1 20020329 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 OAK - FLIGHT CREW REPORTED AFT CABIN EMERGENCY LT FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY FLASHLIGHT BA TTERIES. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002040300135 20020403 00135 NM 2002 4 3 AWXA200200263 1 20020330 A 5210 ACCUMULATOR AIRBUS A319 A319132 3930340 NM EMERGENCY OPEN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 830AW 1565 PHX - EMERGENCY EVACUATION EQUIPMENT - R2 DOOR EMERGENCY OPENEING ACCUMULATOR HAS LOW NITROGEN PRECHARGE. MAINTENANCE SE RVICED R2 DOOR EMERGENCY OPENING ACCUMULATOR WITH NITROGEN PER INSTALLED DOOR PLACARD. 2 L 7 2 4F RT A28NM 2002040300136 20020403 00136 NE 2002 4 3 BJNA020301 2 20020302 A 7200 ENGINE BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE NR 2 FAILED A BJNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 11 789TM 23046 SHUT DOWN NR 2 ENGINE DUE TO LOW OIL QUANTITY AND HIGH OIL TEMP. FOUND OIL EXITING THROUGH TAIL PIPE. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2002040300137 20020403 00137 NM 2002 4 3 C1HA200295007 1 20020324 A 3040 CONTROLLER BOEING 727 727290 138408W NM WINDSHIELD HEAT FAILED A C1HA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 295AS 22147 AFTER TURNING ON WINDOW HEAT, L2 BEGAN TO SMOKE AND THEN CRACKED. REMOVED AND REPLACED L2 WINDOW PER MM 56-12-11 AND R EMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER PER MM 30-41-42. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2002040300138 20020403 00138 NM 2002 4 3 C1HA200295008 1 20020328 A 3040 WIRE HARNESS BOEING 727 727290 138408W NM WINDSHIELD HEAT SHORTED A C1HA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 15 295AS 22147 DURING TAKEOFF ROLL, APPROXIMATELY 90 KTS, LOUD POP AND FLASH FROM UNDER L-3 WINDOW- ABORTED TAKEOFF, ELECTRICAL SHORT EVIDENT ON L-2 WINDOW HEAT CORD. REMOVED AND REPLACED L2 WINDOW IAW MM 56-12-11. WIRING HARNESS FOR WINDSHIELD HEAT ST OWED. 2 L 7 3 4F A3WE 2002040300139 20020403 00139 EU 2002 4 3 C2XA02SH0001 1 20020329 A 3246 L610549 BEARING AEROSP AEROSP ATR42 ATR42320 8680930 EU MLG WHEEL FAILED A C2XA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SW 27 14834 193 FLIGHT 3992, THE CREW REPORTED THAT THE NOSE GEAR HAD A BAD SHIMMY AFTER TOUCH DOWN AND DURING TAXI. MAINTENANCE INSPECT ED THE AIRCRAFT AND FOUND THAT THE NUMBER FOUR MAIN WHEEL ASSEMBLY HAD SHIFTED OUTBOARD. MAINTENANCE REMOVED AND REPLACE D THE RIGHT HAND MAIN LANDING GEAR SWINGING LEVER ASSY, NR 4 BRAKE ASSY, NR 3 & 4 MAIN WHEEL ASSY'S, AND THE AIRCRAFT WA S APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002040300140 20020403 00140 NM 2002 4 3 CALA0200161 1 20020329 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 887, S15R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202. 2 L 7 2 4F RT A16WE 2002040300141 20020403 00141 NM 2002 4 3 CALA0200162 1 20020329 A 5754 FASTENER BOEING 737 7373T0 1384582 NM NR 1 L/E SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34315 23366 INSPECTION FOUND NR 1 LEADING EDGE SLAT FASTENERS CRACKED ON LOWER SKIN. INSTALLED REPAIR IAW SRM 57-43-01. 2 L 7 2 4F RT A16WE 2002040300142 20020403 00142 WP 2002 4 3 DHL2002806007 1 20020327 A 2510 STRUCTURE DOUG DC8 DC873F 302199F WP ARM REST LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FIRST OFFICER'S RT ARM REST WILL NOT LATCH IN POSITION. TIGHTENED LOOSE HARDWARE, OPS CHECKS NORMAL PER DC-8 MM 25-11- 1 2 L 7 4 4F RT 4A25 2002040300143 20020403 00143 WP 2002 4 3 DHL2002806008 1 20020327 A 2611 BATTERY DOUG DC8 DC873F 302199F WP SMOKE DETECTOR DISCHARGED A DHLA O OTHER J WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 46002 LOWER SMOKE DETECTOR LIGHT ILLUMINATED. CODE AC15949 DISPLAYED. R&R SMOKE DETECTOR BATTERIES. SYSTEM OPS CHECKS GOOD PER SMM 26-15-0. 2 L 7 4 4F RT 4A25 2002040300144 20020403 00144 WP 2002 4 3 DHL2002807503 1 20020322 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 81797 45990 RT WING L/E UPPER INNER SKIN RIB CRACKED .250 AT STA. XFS 860.00. PERFORMED STOP DRILL, FABRICATED DOUBLERS, CLEANED , TREATED AND PRIMED. 2 L 7 4 4F RT 4A25 2002040300145 20020403 00145 CE 2002 4 3 DXTA200200193 1 20020320 A 3232 15257003 ACTUATOR CESSNA 650 650 2076802 CE MLG FAILED E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 792QS 2661 6507092 ON FINAL APPROACH, LEFT MAIN GEAR DOWN AND LOCKED LIGHT DIDN'T ILLUMINATE. CHECKED DOWN AND LOCKED LIGHTS, THE LIGHTS LI T WHEN TESTED. EMERGENCY DECLARED, AND AIRCRAFT LANDED SAFELY. 2 L 7 2 4F A9NM 2002040300146 20020403 00146 NM 2002 4 3 F3LA200200118 1 20020323 A 3350 LIGHT BOEING 737 7372P6 1C84609 NM CABIN INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 272 27 21613 MAINTENANCE REPORTED EMERGENCY PATH LIGHTING AT ROW 1 INOPERATIVE AND EXPOSED WIRES NEAR ROW 16. REPLACED AISLE PATH LI GHT SOCKET AND LENS AT ROW 1 AND REPAIRING WIRING AT ROW 16. SYSTEM CHECKED OKAY. 2 L 7 2 4F RT A16WE 2002040300147 20020403 00147 NM 2002 4 3 F3LA200200119 1 20020326 A 5320 ANGLE BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 314FL 3489 25256 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FWD CARGO COMPARTMENT AFT BULKHEAD LOWER TEE ANGLE. REPLACED TEE ANGL E PER MM 51-10-02 AND DRAWING 65-4931. 2 L 7 2 4F RT A16WE 2002040300155 20020403 00155 WP 2002 4 3 IXXA0200010O 1 20020322 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 85324 1151 45813 DURING A ROUTINE MAINTENANCE PREFLIGHT INSPECTION, A CRACK WAS DETECTED ON THE OUTER PLATING AT FUSELAGE STATION 25, LON GERON 33 RIGHT. THE REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION A REPAIR FILLER AND A EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH THE STRUCTURAL REPAIR MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002040300156 20020403 00156 SO 2002 4 3 SIMA200206201 1 20020302 A 3260 852701 PROXIMITY SWITCH EMB 135 EMB135LR 3260305 SO MLG FAILED A SIMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 21 700LE 145156 RDU - FLT 4879 - RIGHT MAIN GEAR UNSAFE INDICATION ON APPROACH INTO RDU. CREW PERFORMED CHECKLIST. GEAR STILL SHOWING UNSAFE. LANDED WITHOUT INCIDENT HAD GEARS PINNED BEFORE EXITING RUNWAY. RAI CHANNEL A PROX SWITCHES ON RIGHT AND LEFT MLG IAW AMM 32-61-02. EXTENSION/RETRACTION CHECK GOOD PER 32-32-00, S/N RT A11243/ LT A11215. (M) 2 L 7 2 4F RT T00011AT 2002040300157 20020403 00157 NM 2002 4 3 USAA020007 1 20020115 A 5347 SEAT TRACK BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 54705 22204 CLT - FOUND SEAT TRACK CORRODED .75 INCH BY 4 INCH AREA OF DEEP PITTING, STATION 1635-1640 LBL 24. CORROSION LEVEL 1. REMOVED OLD SEAT TRACK SECTION, FABRICATED NEW AND INSTALLED PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 2002040300158 20020403 00158 NM 2002 4 3 USAA020025 1 20020115 A 5320 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 PIT - FOUND FLOOR SUPPORT ANGLE CORRODED .5 INCH BY 4 INCH AREA, STATION 434 NEXT TO CREASE BEAM AFT LT FORWARD ENTRY DO OR. DEFECTIVE PART REPLACED WITH IDENTICAL P/N PER SRM 53-10-13 AND 51-10-02. (M) 2 L 7 2 4F RT A2NM 2002040300159 20020403 00159 NM 2002 4 3 USAA020038 1 20020107 A 5340 FITTING BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND FITTING CORRODED 1 INCH BY 1 INCH, LOWER FORWARD CARGO DOOR FRAME STATION 566. REMOVED AND REPLACED FITTING PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2002040300160 20020403 00160 NM 2002 4 3 USAA020039 1 20020109 A 5320 ANGLE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND UPPER CHORD SUPPORT ANGLE HAS 1 INCH DIAMETER CORROSION, STATION 1660 LBL 57. REMOVED AND REPLACED SUPPORT ANGLE. (M) 2 L 7 2 4F RT A2NM 2002040300161 20020403 00161 NM 2002 4 3 USAA020043 1 20020109 A 5320 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 22202 CLT - FOUND FLOOR SUPPORT ANGLE CORRODED 2 INCHES, STATION 434 TO 440 NEXT TO CREASE BEAM FORWARD ENTRY DOOR. REMOVED A ND REPLACED WITH NEW SUPPORT ANGLE PER SRM 53-10-13 AND 51-10-02. (M)55463 2 L 7 2 4F RT A2NM 2002040300162 20020403 00162 NM 2002 4 3 USAA020045 1 20020115 A 5410 FITTING BOEING 757 757225 1384959 NM NACELLE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 55157 22199 CLT - FOUND FITTING LUG/BORE WITH CORROSION. REWORKED LUG PER EA 85775. (M) 2 L 7 2 4F RT A2NM 2002040300163 20020403 00163 NM 2002 4 3 USAA020046 1 20020115 A 5410 FITTING BOEING 757 757225 1384959 NM NACELLE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 55157 22199 CLT - FOUND LUG/BORE CORRODED, INBOARD SIDE LOAD FITTING MOUNT LUG. REBORED/BLENDED/REWORK OF LUG/BUSHED PER EA 85775. (M) 2 L 7 2 4F RT A2NM 2002040300164 20020403 00164 NM 2002 4 3 USAA020048 1 20020130 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND STRINGER CORRODED 1 INCH BY .5 INCH, BS 560 STRINGER 28R. PERFORMED STRINGER SECTION REPAIR PER SRM 53-00-0 3 PER 208. (M) 2 L 7 2 4F RT A2NM 2002040300165 20020403 00165 NM 2002 4 3 USAA020077 1 20020214 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSLEAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 616AU 31377 27147 CLT - FOUND FLOORBEAM CORRODED 20 INCHES LONG, STATION 377 LBL 45 AT SEAT TRACK ATTACH. CORROSION LEVEL 1, TASK NR C53- 221-03. T/R 53-15-01 T-CAP FLOORBEAM REPAIR FROM LBL 51 TO LBL 13. (M) 2 L 7 2 4F RT A2NM 2002040300166 20020403 00166 NM 2002 4 3 USAA020078 1 20020214 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 616AU 31377 27147 CLT - FOUND FLOORBEAM CORRODED 20 INCHES LONG, STATION 377 LBL 25 AT SEAT TRACK ATTACH. CORROSION LEVEL 1, TASK NR C53- 221-03. T-CAP FLOORBEAM REPAIR FROM LBL 51 TO LBL 13 PER T/R 53-15-01. (M) 2 L 7 2 4F RT A2NM 2002040300167 20020403 00167 NM 2002 4 3 USAA020079 1 20020219 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 616AU 31377 27147 CLT - FOUND SEAT TRACK CORRODED 1 INCH BY 3 INCHES, STATION 377 LBL 45. CORROSION LEVEL 1, TASK NR C53-221-03. FABRICA TED AND INSTALLED SEAT TRACK SECTION LBL 45 BETWEEN STATION 377 AND 440 PER SRM 53-00-52. (M) 2 L 7 2 4F RT A2NM 2002040300168 20020403 00168 NM 2002 4 3 USAA020080 1 20020212 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 616AU 31377 27147 CLT - FOUND SEAT TRACK CORRODED 1 INCH BY 3 INCHES, STATION 377 LBL 25. CORROSION LEVEL 1, TASK NR C53-221-03. FABRICA TED AND INSTALLED SEAT TRACK SECTION LBL 25 BETWEEN STATION 377 AND 440 PER SRM 53-00-52. (M) 2 L 7 2 4F RT A2NM 2002040300170 20020403 00170 WP 2002 4 3 UPS02837565 1 20020204 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:N/A EMERGENCY LIGHT DIM. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW MM 33-50-01. 2 L 7 4 4F RT 4A25 2002040300171 20020403 00171 WP 2002 4 3 UPS02837567 1 20020131 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 LEFT WING CENTER L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 329. CUT OUT CORRODED AREA. FABR ICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 2002040300172 20020403 00172 WP 2002 4 3 UPS02837569 1 20020131 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN IS CRACKED AT DRAIN HOLE AT XFS 597.5. STOP DRILLED CRACK, NDT VERIFIED CRA CK IS TERMINATED, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5780-4087-B APPX C. 2 L 7 4 4F RT 4A25 2002040300173 20020403 00173 NM 2002 4 3 02040201 1 20020402 A 3350 BPS720121 POWER SUPPLY BOEING 757 75723A 1384967 NM R-2 DOOR INOPERATIVE A N8TA O OTHER L NO TEST IN INSP/MAINT 1 WP 19 542 26245 Emergency Path Lighting INOP; Replaced R2 door power supply for E-path lighting. Ops checked good as per M/M 33-51-1 2 L 7 2 4F RT A2NM 2002040300174 20020403 00174 WP 2002 4 3 IXXA0200013O 1 20020403 A 7720 CA11503 HARNESS DOUG DC8 DC871F 302199D WP ENGINE CRACKED A IXXA O OTHER M OVER TEMP CL CLIMB 1 SW 11 820BX 81502 1575 46065 AFTER TAKEOFF FROM TOL, THE FLIGHT CREW NOTICED AN ABNORMALLY HIGH ENGINE GAS TEMPERATURE INDICATION ON THE NUMBER FOUR ENGING. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURE AND THE ENGINE WAS SECURED AS PERCAUTIONARY MEASURE AND DISCHARGED ON E FIRE AGENT BOTTLE. THE FLIGHT RETURNED TO TOL FOR AN UNVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGING WITH NO EVEID ENCE OF A FIRE. FURTHER INSPECTION REVEALED THE RIGHT EGT HARNESS CRACKED. MAINTENANCE REPLACED THE EGT HARNESS AND FIRE AGENT BOTTLE. MAINTENANCE PERFORM A SUCCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE COMPANY ENGINE RUN HAND BOOK. T HE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002040300175 20020403 00175 NM 2002 4 3 DL72S020213 1 20020220 A 5300 FRAME BOEING 727 727232 1384082 NM RT W/W CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 FOUND ON F-2 LETTER CK 3/4 IN CRACK MLG UPLOCK FRAME SUPPORTSTRUCTURE AT STA 913 RIGHT W/W. REPAIRED PER MM 53-11-000-8. 2 L 7 3 4F A3WE 2002040300176 20020403 00176 NM 2002 4 3 DL757020214 1 20020220 A 3300 BULB BOEING 757 757232 1384965 NM EXTERIOR BURNED OUT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 666DN 25034 4L AND 4R DOOR EXTERIOR EMERG LITES OUT C/A RELAMPED 2 L 7 2 4F RT A2NM 2002040300177 20020403 00177 NM 2002 4 3 DLM88020224 1 20020223 A 3350 LIGHT DOUG MD88 MD88 3023688 NM TAIL CONE BROKEN A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 991DL 53343 WORKING L/O FOUND EMERGENCY LIGHTS IN TAIL CONE INOP. REPAIRED CONNECTOR - OPS NML. 2 L 7 2 4F RT A6WE 2002040300178 20020403 00178 NM 2002 4 3 DLM88020230 1 20020223 A 2710 59554191 LINK DOUG MD88 MD88 3023688 NM LEFT LOOSE A DALA K NONE F FLT CONT AFFECTED DE DESCENT 1 SO 27 978DL 53259 ON APPROACH AILERONS JAMMED -REPLACED THE LEFT AILERON I/B CRANK ASSY FOR EXCESSIVE PLAY 2 L 7 2 4F RT A6WE 2002040300179 20020403 00179 NM 2002 4 3 DL73K020239 1 20020227 A 5551 654648510 HINGE FITTING BOEING 737 737247 138448D NM LBL 21 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 377DL 23604 HORIZONATAL STABLIZER / LH / CENTER SECTION / HINGE FITTING:CORROSION REPAIR CORROSION WAS DETECTED ON THE HINGE FITTING OF THE LH HORIZ STABILIZER. THE CORROSION WAS REMOVED BY MACHINING THE BORE DIAMETERS OF THE FITTING TO A LARGER SIZE AND MACHINING THE FACE OF THE FITTING LUGS. LARGER DIAMETR BUSHINGS WERE INSTALLED IN THE OVERSIZE LUG BORES. THE WORK WAS ACCOMPLISHED PER ER/A 382668-14, REV B. 2 L 7 2 4F A16WE 2002040300180 20020403 00180 NM 2002 4 3 DLM88020241 1 20020301 A 5330 5911406 SKIN DOUG MD88 MD88 3023688 NM FS 228, S-17L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DE 53417 FUSELAGE / SKIN / FS 228 / STRG. 17L-18L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH 3 DENTS NEAR FS 228 BETWEEN STRINGERS 17L & 18L. THE DENTS WERE REMOVED WITH A SINGLE 10" X 10" CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 382691- 14, REV A. 2 L 7 2 4F RT A6WE 2002040300181 20020403 00181 NM 2002 4 3 DL76L020265 1 20020307 A 2120 6066223 FAN 6066223 BOEING 767 767332 1382001 NM LWR COMPARTMNENT INOPERATIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 177DN 127893 25122 IN CRUISE GOT STRONG SMOKE SMELL FOLLOWED BT RT RECIRC FAN EICAS MESSAGE.TURNED OFF BOTH RECIRC FANS AND SMOKE SMELL DISAPPATED. REMOVED AND REPLACED RIGHT RECIRC FAN PER AMM. CHECKS OK. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS 2 L 7 2 4F RT A1NM 2002040300182 20020403 00182 NM 2002 4 3 DL73K020268 1 20020307 A 2500 00 FLASHLIGHT BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 307DL 23079 IR - FWD EMERGENCY FLASHLIGHT INOP. CA - REPLACED FWD ATT EMERGENCY FLASHLIGHT. 2 L 7 2 4F RT A16WE 2002040300184 20020403 00184 NM 2002 4 3 DLM88020305 1 20020314 A 2760 UNKNOWN SWITCH DOUG MD88 MD88 3023688 NM PEDESTAL DIRTY A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 965DL 49984 CLEARED FOR T/O WHEN WE GOT AUTOBRK T/O WARNING.WE ABORTEDT/O AND CONTACTED ATL MCC.WE RTN TO GATE--NO SPEED NOTED- NE VER GOT ABOVE 20KTS. CLEANED RTO SWITCHES AT SPEEDBRAKE HANDLE.AURAL WARNING NO W CKS OK. 2 L 7 2 4F RT A6WE 2002040300185 20020403 00185 NM 2002 4 3 DL73K020332 1 20020318 A 5330 65516241 DOUBLER BOEING 737 737232 1384475 NM FS 970, S-27R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 308DL 23080 FUSELAGE / SKIN CUTOUT / FS 967-981 / STRG. 26R-27R : INTERNAL CUTOUT DOUBLER CORROSION THE INTERNAL SURROUND DOUBLER AROUND A FUSELAGE CUTOUT FOR A LAVATORY VENT WAS FOUND CORRODED BETWEEN FS 967 & 981 AND BETWEEN STRINGERS 26R & 27R. THE CORROSION WAS REMOVED WITH 6" X 6" CUTOUT TO THE INTERNAL DOUBLER. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 382767-14, REV B. 2 L 7 2 4F RT A16WE 2002040300186 20020403 00186 NM 2002 4 3 DL75A020348 1 20020320 A 5330 141N33121 SKIN BOEING 757 757212 1384951 NM FS 426, S-1 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752AT 23128 FUSELAGE / SKIN / FS 426 / STRG. 1-2R / TCAS ANTENNA CUTOUT CORROSION REPAIR CORROSION WAS FOUND AROUND THE TCAS ANTENNA CUTOUT AT FS 426 BETWEEN STRINGERS 1 AND 2R. THE EXISTING TCAS DOUBLER WAS REMOVED AND DISCARDED. THE CUTOUT WAS ENLARGER TO REMOVE THE CORROSION. THE NEW CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER ER/A 382746-14, REV. A. 2 L 7 2 4F RT A2NM 2002040300187 20020403 00187 NM 2002 4 3 DL75A020349 1 20020320 A 5330 143N36912 SKIN BOEING 757 757212 1384951 NM FS 676, S-23R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752AT 23128 FUSELAGE / SKIN / FS 676 / STRG. 23R : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS BADLY GOUGED BY A WORK STAND AT FS 676 NEAR STRINGER 23R. THE GOUGE WAS REMOVED WITH A 7.9" X 3" CUTOUT. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER AND INTERNAL ALUMINUM EDGE ROW DOUBLERS. THE REPAIR WAS ACCOMPLISHED PER ER/A 382725-14, REV A. 2 L 7 2 4F RT A2NM 2002040300188 20020403 00188 NM 2002 4 3 DL757020351 1 20020320 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM FS 1708, S-17L GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 FUSELAGE / SKIN / FS 1708 / STRG. 17L : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND GOUGED AT FS 1708 JUST BELOW STRINGER 17L. THE GOUGE WAS REMOVED WITH A CUTOUT TO THE SKIN. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER ER/A 382720-14, REV A. 2 L 7 2 4F RT A2NM 2002040300189 20020403 00189 NM 2002 4 3 DL75A020352 1 20020320 A 5330 143N35212 SKIN BOEING 757 757212 1384951 NM FS 900, S-28 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752AT 23128 FUSELAGE / SKIN / FS 900 / STRG. 28L-28R : CORROSION REPAIR THE FUSELAGE SKIN WAS FOUND BADLY CORRODED AT FS 900 AND BETWEEN STRINGERS 28L & 28R. THE SKIN WAS CUT AT FS 885 AND THE AFT SECTION REMOVED TO FS 900. A NEW SECTION OF SKIN WAS FABRICATED AND INSTALLED USING EXTERNAL AND INTERNAL ALUMINUM DOUBLERS TO SPLICE THE NEW SECTION. THE REPAIR WAS ACCOMPLISHED PER ER/A 382586-14, REV. A. 2 L 7 2 4F RT A2NM 2002040300190 20020403 00190 NM 2002 4 3 DL75A020353 1 20020320 A 5311 111N20012 BULKHEAD BOEING 757 757212 1384951 NM FS 900, S-28 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752AT 23128 FUSELAGE / BULKHEAD / FS 900 / STRG. 28L-28R / LOWER CHORD AND WEB : CORROSION REPAIR THE LOWER CHORD AND WEB OF THE FS 900 BULKHEAD WAS FOUND CORRODED BETWEEN STRINGERS 28L & 28R. THE DAMAGED SECTION OF WEB WAS CUTOUT AND THE LOWER CHORD WAS CUT AT STRINGER 28L & 28R. THE WEB CUTOUT WAS REPAIRED WITH 2 ALUMINUM REPAIR DOUBLERS. A NEW SECTION OF CHORD WAS SPLICED AT THE CUT LOCATION WITH STEEL REPAIR ANGLES. THE REPAIR WAS ACCOMPLISHED PER ER/A 382587-14, REV. A. 2 L 7 2 4F RT A2NM 2002040300191 20020403 00191 NM 2002 4 3 DL76G020357 1 20020321 A 2120 732591F FAN BOEING 767 7673P6 1385105 NM EQ COOLING EXH FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 1501P 24983 IMMEDIATLY AFTER T/O, F/AS CALLED TO REPORT SMOKE IN THE CABIN. SMOKE DETECTORS IN MID AND AFT LAVS ACTIVATED. SMOKE WAS VISIBLE WITH AN ELECTRICAL BURNING SMELL. FWD EQ EXH FAN EICAS MSG WITH STRONG ELECTRICAL SMELL IN FWD CABIN AREA. REMOVED AND REPLACED FWD EQUIP EXHAUST FAN PER M/M ETOPS CATEGORY 'B': DIVERSION OR TURNBACK 2 L 7 2 4F RT A1NM 2002040300192 20020403 00192 NM 2002 4 3 DL72S020373 1 20020326 A 5520 UNK SKIN BOEING 727 727225A 1384077 NM L/H ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 2 INCH CRACK R/H ELEVATOR LWR SKIN FWD OF TAB O/B BALANCE WEIGHT REPAIRED PER SRM 55-20-3D 2 L 7 3 4F RT A3WE 2002040300193 20020403 00193 NM 2002 4 3 DL73K020376 1 20020327 A 5700 WEDGE BOEING 737 737232 1384475 NM #5 SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 FOUND ON V1 LETTER CK AFT WEDGE DALAMINATED O/B END NUMBER 5 SLAT.__C/A REPLACED WEDGE ASSEMBLY 2 L 7 2 4F RT A16WE 2002040300194 20020403 00194 NM 2002 4 3 DL757020378 1 20020328 A 5330 146N37805 SKIN BOEING 757 757232 1384965 NM FS 1660, S-21L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 623DL 22913 FUSELAGE / SKIN / FS 1660 / STRG. 21L : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS STRUCK BY GROUND EQUIPMENT AT FS 1160 AND STRINGER 21L. THE DAMAGE WAS REMOVED WITH A 6" X 8" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 382800-14, REV B. 2 L 7 2 4F RT A2NM 2002040300195 20020403 00195 NM 2002 4 3 DL733020391 1 20020401 A 5410 311A11112 BEAM BOEING 737 737347 1384647 NM PYLONS CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304WA 23345 CORROSION WAS FOUND ON THE CROWN BEAM LUG BORES ON THE #1 AND #2 PYLONS. THE BORES WERE OVERSIZED TO REMOVE THE CORROSION AND REPAIR BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2002040300196 20020403 00196 NM 2002 4 3 UPS02537964 1 20020329 A 5340 CREASE BEAM BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 412UP 23852 INSPECTION TYPE:MOD CORROSION ON CREASE BEAM STA 585 - 685 RBL 62 REPAIRED CREASE BEAM PER SRM 51-4-02, 51-40-05 AND GOODRICH ER 02-03 41 2 L 7 2 4F RT A2NM 2002040300197 20020403 00197 NM 2002 4 3 UPS02537965 1 20020329 A 5340 CREASE BEAM BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 412UP 23852 INSPECTION TYPE:MOD CORROSION ON CREASE BEAM STA 875 RBL 61 REPAIRED PER SRM 51-40-02 AND GOODRICH ER 02-0342 2 L 7 2 4F RT A2NM 2002040300198 20020403 00198 WP 2002 4 3 ZW0A0203901 1 20020401 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP A ZW0A K NONE O OTHER CL CLIMB 1 CE 13 914TW 49185 DURING CLIMB AND DESCENT THE FIRST CLASS CABIN EGRESS LIGHTS ILLUMINATED. REPLACED THE POWER SUPPLY. CHECK-C 3-4-01 ST L. --CLOSED-- 2 L 7 2 4F A6WE 2002040300199 20020403 00199 NM 2002 4 3 QXEA0200536 1 20020402 A 5270 HANDLE BOMBDR DHC8 DHC8401 NM WORN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 405QX 4047 SEA - AIRCRAFT RETURNED TO FIELD WHEN AFT CARGO DOOR WARNING ILLLUMINATED. MAINTENANCE INSPECTED THE AFT CARGO DOOR AND FOUND THE HANDLE STANDOFFS WORN. HANDLE WAS REPLACED AND OPERATIONAL CHECK WAS PERFORMED. OPERATIONAL CHECK WAS GOOD. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002041500182 20020415 00182 NM 2002 4 15 F3LA200200121 1 20020402 A 5754 SKIN BOEING 737 7373L9 1384470 NM L/E SLAT CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 3415 24569 MAINTENANCE REPORTED SKIN CRACKED AT OUTBOARD END OF NR 6 SLAT. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 57-43 -01 FIG 206 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002040300200 20020403 00200 NM 2002 4 3 AWXA200200275 1 20020311 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM IN THE AFT CARGO COMPARTMENT AT BS 773, RBL 2.5. MAINTENANCE CLEANED CORROSION ON FLOOR SUPPORT BEAM AT FS 773, RBL 2.5 AND FOUND MATERIAL LOSS TO BE OUT OF LI MITS. FABRICATED 2 EACH REPAIR ANGLES, TREATED AND PRIMED ANGLES, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, FIG 201, SHT 201-203. 2 L 7 2 4F RT A16WE 2002040300201 20020403 00201 NM 2002 4 3 AWXA200200276 1 20020311 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AND NUTPLATE IN THE AFT CARGO COMPARTME NT AT BS 860, LBL 2.5. MAINTENANCE REMOVED THE NUTPLATE AND CLEANED CORROSION ON FLOOR SUPPORT BEAM AT FS 860, LBL 2.5 I AW 51-40-02 PG 1, 53-60-53, PG 108, .047 MATERIAL REMAING. FABRICATED 2 EACH REPAIR ANGLES, TREATED AND PRIMED ANGLES, A ND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, PG. 201, MM 51-21-21 PG. 705-705. 2 L 7 2 4F RT A16WE 2002040300202 20020403 00202 NM 2002 4 3 AWXA200200277 1 20020311 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT BEAM IN THE AFT CARGO COMPARTMEN T AT BS 860, RBL 7.5. MAINTENANCE FABRICATED 2 EACH REPAIR ANGLES, TREATED AND PRIMED ANGLES, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, FIG 201, PG. 201-203. 2 L 7 2 4F RT A16WE 2002040300203 20020403 00203 NM 2002 4 3 AWXA200200278 1 20020311 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AND NUTPLATES IN THE AFT AC RGO COMPARTMENT AT BS 860, LBL 7.5. MAINTENANCE FABRICATED 3 EACH REPAIR ANGLES, TREATED AND PRIMED, AND INSTALLED REPAI RS IAW B737-300 SRM 53-00-53, FIG 201, SHT 1-3. 2 L 7 2 4F RT A16WE 2002040300204 20020403 00204 NM 2002 4 3 AWXA200200279 1 20020311 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AND NUTPLATES IN THE AFT CARGO COMPARTM ENT AT BS 727D+6, LBL 7.5. MAINTENANCE REMOVED CORROSION IAW B737-300 SRM 51-10-2, PG. 24, FABRICATED 2 EACH REPAIR ANGL ES FROM 7075-0-.071, 7075-0-.080, HEAT TREATED TO 7075-T6, PRIMED, AND INSTALLED REPAIR PARTS AT BS 727D+6, LBL 7.5 IAW B737-300 SRM 53-00-53, FIG. 201, PG. 203. 2 L 7 2 4F RT A16WE 2002040300205 20020403 00205 NM 2002 4 3 AWXA200200280 1 20020403 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AND NUTPLATES IN THE AFT CARGO COMPARTM ENT AT BS 727+6, LBL 2.5. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS BEYOND LIMITS IAW B737 300 SRM 53-60-53, FIG 101, SHT 8. FABRICATED 2 EACH REPAIR ANGLES FROM 7075-0-.071, 7075-0-.081, HEAT TREATED AND PRIMED, AND INSTALLED R EPAIR PARTS AT BS 727+6, LBL 2.5 IAW B737-300 SRM 53-00-53, FIG. 201, PG. 203. 2 L 7 2 4F RT A16WE 2002040300206 20020403 00206 WP 2002 4 3 MWEA020207 1 20020402 A 5310 995578043 STIFFENER DOUG DC9 DC914 3022034 WP STATION 160 ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 VERTICAL STIFFENER IN FORWARD ELECTONIC POWER CENTER HAS ELONGATED HOLES. -- REPAIRED VERTICAL STIFFENER IAW SRM 53-01 FIGURE SHEET 4. 2 L 7 2 4F A6WE 2002040400002 20020404 00002 WP 2002 4 4 AALA20020172 1 20020222 A 3350 LIGHT DOUG DC9 DC982 3022082 WP TAIL STAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 221AA 49172 DFW - DURING OVERNIGHT MAINTENANCE, TAIL STAIRS EMERGENCY EXIT SIDE WALL LIGHTS INOPERATIVE. REPAIRED WIRES ON TAIL STA IRS EMERGENCY EXIT SIDE WALL LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400003 20020404 00003 EU 2002 4 4 AALA20020173 1 20020224 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1450A 11459 DFW - DURING OVERNIGHT MAINTNENANCE, EMERGENCY PATH LIGHTING AT FORWARD OVERWING EMERGENCY LATCH FLOOR LIGHTS INOPERATIV E. RESECURED EMERGENCY PATH LIGHTING AT FORWARD OVERWING EMERGENCY LATCH FLOOR LIGHTS CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002040400004 20020404 00004 EU 2002 4 4 AALA20020174 1 20020221 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1441A 11436 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH LIGHTING AT FIRST CLASS TO ROW 10 IN COACH INOPERATIVE. RESECURED EM ERGENCY PATH LIGHTING AT ROW 10 EMERGENCY LATCH FLOOR LIGHTS CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002040400005 20020404 00005 NM 2002 4 4 AALA20020196 1 20020221 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT PATH LIGHTING AT SEATS 20 AND 21 H, J, INOPERATIVE. REPLACED B ROKEN LIGHT ASSEMBLY AND BATTERY PACK FOR EMERGENCY EXIT PATH LIGHTING AT SEATS 20 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002040400006 20020404 00006 NM 2002 4 4 AALA20020197 1 20020226 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHT OUTSIDE OF R3 DOOR INOPERATIVE. REPLACED R3 SLIDE LIGHT ASSEM BLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002040400007 20020404 00007 EU 2002 4 4 AALA20020199 1 20020228 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80058 466 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONN ECTOR AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002040400008 20020404 00008 NM 2002 4 4 AALA20020200 1 20020226 A 5315 FLOORBEAM BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 691AA 25697 TUL - FOUND CORROSION ON FLOORBEAM MID SPAN. REPAIRED FLOORBEAM PER BOEING 757 SRM 53-00-51-2 AND 51-70-00. (M) 2 L 7 2 4F RT A2NM 2002040400009 20020404 00009 EU 2002 4 4 AALA20020202 1 20020301 A 3320 BALLAST AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 80057 465 MIA - FLT 915 - EN ROUTE MIA-BOG - DETECTED SMOKE IN CABIN. RETURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED BALLAST NR 5, 6, AND 7. PERFORMED INSPECTION OF AFT GALLEY OVERHEAD PANEL. NO DEFECTS NOTED. SYSTEM GROUND CHECKED N ORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002040400010 20020404 00010 NM 2002 4 4 AALA20020204 1 20020227 A 2432 AAP3274A CHARGER DOUG MD80 MD83 3023681 NM E/E BAY DEFECTIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 834RA 53124 OKC - FLT 9680 - AFTER TAKEOFF OKC, SHIP BATTERY CHARGER CIRCUIT BREAKER POPPED. RETURNED OKC AND LANDED WITHOUT INCIDE NT. REPLACED MAIN SHIP BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002040400011 20020404 00011 WP 2002 4 4 AALA20020205 1 20020302 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7547A 53029 ORD - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHTS CAME ON WITH POWER OFF. REPLACED EMERGENCY EXIT L IGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400012 20020404 00012 WP 2002 4 4 AALA20020206 1 20020303 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7514A 49891 TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM L2-639-694 AND 176-246 INOPERATIVE. REPLACED BATTERY. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400013 20020404 00013 WP 2002 4 4 AALA20020207 1 20020304 A 2560 P2070003001 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 467AA 49597 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED FORWARD ENTRY EME RGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400014 20020404 00014 WP 2002 4 4 AALA20020208 1 20020301 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AA 49289 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED CABIN EMERGENCY EXIT LIGHTS DIM IN ALL ROWS. REPLACED BOTH BATTERIES O N CENTER COACH MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400015 20020404 00015 WP 2002 4 4 AALA20020209 1 20020301 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AA 49289 DFW - DURING OVERNIGHT MAINTENANCE, ROWS 18-21 SEAT MOUNTED CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES FOR SEATS 18-21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400016 20020404 00016 WP 2002 4 4 AALA20020210 1 20020301 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AA 49289 DFW - DURING OVERNIGHT MAINTENANCE, ROWS 7/12 SEAT MOUNTED CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES FOR SEAT 7/12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400017 20020404 00017 NM 2002 4 4 AALA20020212 1 20020303 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 312AA 22315 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY PATH LIGHTING AT SEAT 28H INOPERATIVE. REMOVED AND REPLACED BROKEN CONNECTOR AT LOWER SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002040400018 20020404 00018 NM 2002 4 4 AALA20020213 1 20020302 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 394AN 29431 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH LIGHTING SYSTEM AT 2HJ INOPERATIVE. RESEATED CONNECTOR UNDER SEAT 2H J. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002040400019 20020404 00019 NM 2002 4 4 AALA20020214 1 20020301 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 383AN 26995 ORD - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY PATH LIGHTING AT 32HJ INOPERATIVE. REPAIRED BROKEN WIRE AND BATTERY PACK FOR EMERGENCY PATH LIGHTING AT SEAT 32HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002040400020 20020404 00020 NM 2002 4 4 AALA20020215 1 20020301 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 751AN 30798 DFW - DURING OVERNIGHT MAINTENANCE, FOUND RIGHT LOWER FORWARD EMERGENCY PATH LIGHTING ON G3 GALLEY WALL BROKEN. REPLACE D LIGHT ASSEMBLY AT G3 GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002040400021 20020404 00021 NM 2002 4 4 AALA20020219 1 20020220 A 2420 IDG BOEING 777 777223 1385213 NM RT GENERATOR FAILED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 791AN 30254 RIGHT GENERATOR WOULD NOT COME ON LINE AFTER ENGINE START. DEFERRED RIGHT IDG INOPERATIVE AS PER MEL 24-03 AUTH LGW2-18 2DC-A PLACARD INSTALLED MPM 24-03 ACCOMPLISHED, ENTERED IN MIC. REMOVED AND REPLACED RIGHT ENGINE IDG AS PER MM 24-11-0 1-4. ALL OPS AND LEAK CHECKS NORMAL. CLEARED MEL 24-03 AUGH 2-182DC-A CLEARED MIC SHEET. (M) 2 L 7 2 4F RT T00001SE 2002040400022 20020404 00022 WP 2002 4 4 AALA20020224 1 20020306 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 485AA 49678 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY SEAT MOUNTED EXIT LIGHTS FORWARD OF WINGS ARE DIM. REPLACED AFT EMERGENCY EXIT LIGHT BATTERY FOR FORWARD SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400023 20020404 00023 WP 2002 4 4 AALA20020225 1 20020304 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 452AA 49553 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT OVERWING EXIT SIGNS INOPERATIVE. REPLACED EMERGENCY EXIT L IGHT BATTERY AT OVERWING SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400024 20020404 00024 WP 2002 4 4 AALA20020226 1 20020306 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 493AA 49731 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN TAILCONE AREA INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT WIRES IN TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400025 20020404 00025 WP 2002 4 4 AALA20020227 1 20020306 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77421 49333 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CAT WALK SIDEWALL MARKERS INOPERATIVE. REPLACED EMERGENCY EXIT CAT W ALK SIDEWALL MARKERS WIRE SPLICES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400026 20020404 00026 NM 2002 4 4 AALA20020254 1 20020227 A 2420 IDG BOEING 777 777223 1385213 NM LT ENGINE FAILED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 798AN 30797 CLIMBING THROUGH FL180 ELEC AC BUS LT EICAS MESSAGE DISPLAYED. CHECKLIST PERFORMED AND APU WAS STARTED. APU POWERED LE FT MAIN A/C BUS ELEC GEN OFF LT EICAS MESSAGE REMAINED ON WITH FAILED LEFT IDG. REMOVED AND REPLACED IDG AT LEFT ENG IA W AMM 24-11-01. RUNUP ENGINE CHECKED OPS OK. SERVICED IDG. FOUND NO LEAKS. (M) 2 L 7 2 4F RT T00001SE 2002040400027 20020404 00027 NM 2002 4 4 AALA20020255 1 20020301 A 2420 IDG BOEING 767 767323 1385205 NM LT ENGINE FAILED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 385AM 27059 JFK - LEFT GENERATOR DRIVE LIGHT ILLUMINATED ON FINAL APPROACH TO JFK, LT GENERATOR DISCONNECTED PER FM VOL 1. RECONNEC TED AND SERVICED LEFT IDG AS PER MM PERFORMED GENERATOR DRIVE SYSTEM ADJUST/TEST AS PER 24-11-00-5. OPERATIONAL CHECK N ORMAL WITH NO FAULTS INDICATED. (M) 2 L 7 2 4F RT A1NM 2002040400028 20020404 00028 NM 2002 4 4 AALA20020256 1 20020305 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 JFK - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT ROW 44 INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHTING AT ROW 44. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002040400029 20020404 00029 NM 2002 4 4 AALA20020264 1 20020228 A 5330 SKIN BOEING 767 767323 1385205 NM FUSELAGE TORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 381AN 25450 AFW - FOUND FUSELAGE SKIN TORN AT FORWARD CARGO DOOR CUT OUT FORWARD LOWER CORNER. DAMAGE CUT OUT. FABRICATE FILLERS. FABRICATE DOUBLERS. ALODINED AND PRIME SURFACES. DOUBLER TO BE INSTALLED WET. REPLACE EXISTING FASTENERS. FILLERS T O BE ATTACHED TOGETHER WITH DOUBLE FLUSH RIVETS. (M) 2 L 7 2 4F RT A1NM 2002040400030 20020404 00030 NM 2002 4 4 AALA20020265 1 20020228 A 5753 STRUCTURE BOEING 767 767323 1385205 NM TE FLAP CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 358AA 24039 AFW - FOUND CORROSION IN 2 MOUNT HOLES FOR LEFT NR 4 INBOARD FLAP ATTACH BEAM HOLES OVERSIZED TO .6450. VISUALLY INSPEC T BORES TO ENSURE CORROSION REMOVAL. FABRICATED FREEZE PLUG FROM 7075-T6 TO ACHIEVE .001, INTERFERENCE FIT. ALODINE PL UGS INSTALL WET WITH BM5 5-95, REAM BORE HOLES TO ORIGINAL DIAMETERS MAINTAIN .060 WALL THICKNESS. INSTALL PRODUCTION T YPE WASHERS AT REWORK LOCATIONS INSTALL FLAP PER 767 AMM. (M) 2 L 7 2 4F RT A1NM 2002040400031 20020404 00031 NM 2002 4 4 AALA20020266 1 20020228 A 5753 STRUCTURE BOEING 767 767323 1385205 NM TE FLAPS CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 358AA 24039 AFW - FOUND CORROSION FOUND IN TWO MOUNT HOLES FOR RIGHT RN 5 INBOARD FLAP ATTACH BEAM. HOLES OVERSIZED TO REMOVE CORRO SION, FINK HOLE SIZE .6440. VISUALLY INSPECT BORES TO ENSURE COMPLETE CORROSION REMOVAL. FABRICATED FREEZE PLUGS FROM 7075-T6 TO ACHIEVE MIN .001 INCH INTERFERENCE FIT. ALODINE AND INSTALL WET WITH BMS 5-95. REAM BORE TO ORIGINAL HOLE D IAMETER MAINTAIN .060 WALL THICKNESS. INSTALLED PRODUCTION TYPE WASHERS AT THE REWORKED LOCATIONS INSTALL FLAP PER 767 AMM. (M) 2 L 7 2 4F RT A1NM 2002040400032 20020404 00032 NM 2002 4 4 AALA20020267 1 20020228 A 5753 FITTING BOEING 767 767323 1385205 NM TE FLAPS CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 358AA 24039 AFW - FOUND CORROSION IN HOLES OF FITTING. CLEANED OUT CORROSION FROM HOLES DIAMETER NOW .5440 AND .5340. VISUALLY INS PECT BORES TO ENSURE CORROSION REMOVAL. FABRICATED FREEZE PLUG FROM 7075-TL TO ACHIEVE .001 INCH INTERFERENCE. ALODINE AND INSTALL WET WITH BMS 5-95. BEAM BORE TO ORIGINAL HOLE DIAMETER MAINTAIN .050 INCH WALL THICKNESS. FABRICATED REPA IR WASHERS FROM .25 INCH THICK AND .90 INCH OLD TO BE USED IN LIEU OF EXISTING PROD WASHERS. INSTALL FLAP PER 767 AMM. (M) 2 L 7 2 4F RT A1NM 2002040400033 20020404 00033 NM 2002 4 4 AALA20020268 1 20020228 A 5753 STRUCTURE BOEING 767 767323 1385205 NM TE FLAPS CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 358AA 24039 AFW - FOUND CORROSION IN HOLES AT AFT ATTACH OF RIGHT FLAP 9-10 BEAM. HOLES CLEANED UP BEYOND DIAMETER LISTED IN AARD 2 7-50-00-01. VISUALLY INSPECT BORES TO ENSURE CORROSION REMOVAL. FABRICATED BUSHINGS OF A1-N1-BR TO ACHIEVE MIN .001 IN CH INTERFERENCE PIT, ALODINE AND INSTALLED WET W/BMS 5-95, REAM BORE BUSHING TO ORIGINAL HOLE DIAMETER. FABRICATED REPA IR WASHERS FROM .125 INCH THICK CRES WITH O/D OF .75, REFINISH REPAIR WASHER PER AARD 51-20-01-1. INSTALL WASHER IN PLA CE OF ORIGINAL WASHERS. INSTALL FLAP PER 767 AMM. (M) 2 L 7 2 4F RT A1NM 2002040400034 20020404 00034 WP 2002 4 4 AALA20020292 1 20020307 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND 1 INCH DENT ON FUSELAGE SKIN STATION 68 RIGHT SIDE OF A/C FORWARD OF LONGERON 21. REPAIRED PER SRM 53-01 F2 SHEET 3 AARD 53-30-00-02 INTERNAL 2 ROW DOUBLER. (M) 2 L 7 2 4F A6WE 2002040400035 20020404 00035 WP 2002 4 4 AALA20020293 1 20020308 A 2560 P2070003001 FLASHLIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 438AA 49456 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED FORWARD ENTRY EME RGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002040400036 20020404 00036 WP 2002 4 4 AALA20020294 1 20020308 A 3350 P40110049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 16545 53027 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEATS 20-31 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BA TTERIES FOR SEATS 20-31. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400037 20020404 00037 WP 2002 4 4 AALA20020295 1 20020310 A 3350 AAP3274A CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA O OTHER O OTHER CL CLIMB 1 SW 21 452AA 49553 ORD - FLT 1523 - DURING CLIMB-OUT ORD, EMERGENCY EXIT LIGHT BATTERY CHARGER LIGHT ILLUMINATED. RETURNED TO ORD AND LAND ED WITHOUT INCIDENT. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400038 20020404 00038 WP 2002 4 4 AALA20020297 1 20020311 A 2560 P2070003001 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 403A 49314 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED FORWARD ENTRY EME RGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400039 20020404 00039 WP 2002 4 4 AALA20020298 1 20020311 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 577AA 53154 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS IN SIDEWALL OF TAIL STAIRS INOPERATIVE. REPAIRED WIRE FOR EMERGENC Y LIGHTS IN SIDEWALL OF TAIL STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400040 20020404 00040 NM 2002 4 4 AALA20020299 1 20020309 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 303AA 22309 JFK - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHT SEAT 37B INOPERATIVE. RECONNECTED CONNECTOR AT SE AT 37B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002040400041 20020404 00041 WP 2002 4 4 AALA20020305 1 20020314 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 412AA 49323 TUL - FOUND CRACK IN CANT FRAME 1485 WEB UPPER LEFT CORNER. DOUBLER INSTALLED PER AARD 53-10-00-32. (M) 2 L 7 2 4F A6WE 2002040400042 20020404 00042 NM 2002 4 4 AALA20020306 1 20020309 A 2420 GEN3014 GENERATOR BOEING 777 777223 1385213 NM RIGHT FAILED A AALA K NONE H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SW 21 787AL 30010 JFK - LOST RIGHT GENERATOR DURING FLIGHT, LT WOULD NOT RESET. GENERATOR OFF LIGHT ILLUMINATED. ALL BACK-UP POWER SOURC ES WORKED NORMALLY. APU GENERATOR SUPPLIED AC POWER FOR REST OF FLIGHT. ELECTRICAL PAGE SHOWED NO POWER FROM THE RT GE NERATOR. REMOVED AND REPLACED RIGHT GENERATOR REQUIRES SERVICING. LEAKING AND OPS CHECK REF MM 24-11-01-4 SERVICED LEA K AND OPS CHECKED OK. (M) 2 L 7 2 4F RT T00001SE 2002040400043 20020404 00043 WP 2002 4 4 AALA20020307 1 20020321 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 205AA 49155 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 89 BROKEN. REPLACED EMERGENCY EXIT LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400044 20020404 00044 EU 2002 4 4 AALA20020308 1 20020313 A 7160 JR34968A SPINNER FOKKER F28 F28MK0100 4990807 EU NR 1 ENGINE DEFECTIVE A AALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 21 1470K 11506 DFW - FLT 457 - EN ROUTE MEM-DFW - EXCESSIVE VIBRATIONS NUMBER 1 AND 2 ENGINE IN ICY CONDITION, UNABLE TO CLEAR. DECLAR ED EMERGENCY, DIVERTED TO SHV, AND LANDED WITHOUT INCIDENT. REPLACED NR 1 AND 2 ENGINE LOW PRESSURE COMPRESSOR ROTATING FAIRING AND SPINNER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002040400045 20020404 00045 NM 2002 4 4 AALA20020310 1 20020313 A 3350 S283T0143 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 358AA 24039 LAX - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT PATH LIGHTING AT SEAT 2H INOPERATIVE. REPLACED BATTERY PACK AN D BATTERY CHARGER AT SEAT 2H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002040400046 20020404 00046 NM 2002 4 4 AALA20020311 1 20020313 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 371AA 25198 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT PATH LIGHTING AT SEATS 24H AND 29H INOPERATIVE. RESEATED LOOSE CONNECTORS AT SEATS 24H AND 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002040400047 20020404 00047 WP 2002 4 4 AALAA20020194 1 20020228 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 555AN 53085 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHTS AT ROWS 21-31 INOPERATIVE. RESEATED PUSH PIN AT AFT STAIRS EMERGENCY EXIT SIDEWALL LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040400048 20020404 00048 NM 2002 4 4 USAA020083 1 20020123 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 32053 24934 PIT - FOUND FRAME CRACKED .125 INCH, FS 907 BETWEEN S8L AND S9L. INSTALLED DOUBLER REPAIR PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002040400049 20020404 00049 NM 2002 4 4 USAA020084 1 20020228 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 32053 24934 CLT - FOUND FRAME CRACKED .125 INCH, FRAME 440R BETWEEN S8R AND S9R. INSTALLED DOUBLER REPAIR PER TYPICAL 53-10-14. (M ) 2 L 7 2 4F RT A16WE 2002040400050 20020404 00050 NM 2002 4 4 USAA020085 1 20020123 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 32053 24934 PIT - FOUND FRAME .125 INCH CRACK, FS 380 BETWEEN S8R AND S9R. INSTALLED DOUBLER REPAIR PER TYPICAL REPAIR 53-10-14. ( M) 2 L 7 2 4F RT A16WE 2002040400051 20020404 00051 NM 2002 4 4 USAA020086 1 20020113 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 32053 24934 PIT - FOUND FRAME .0625 INCH CRACK, FRAME 747 BETWEEN S8R AND S9R. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002040400052 20020404 00052 NM 2002 4 4 USAA020087 1 20020123 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 32053 24934 PIT - FOUND FRAME CRACKED .0625 INCH CRACK, FRAME 827 BETWEEN S8R AND S9R. INSTALLED DOUBLER REPAIR PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002040400053 20020404 00053 NM 2002 4 4 USAA020088 1 20020113 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 32053 24934 PIT - FOUND FRAME CRACKED .25 INCH, FS 787 BETWEEN S8L AND S9L. INSTALLED DOUBLER REPAIR PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002040400054 20020404 00054 NM 2002 4 4 USAA020089 1 20020120 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 32053 24934 PIT - FOUND FRAME CRACKED .25 INCH, FS 400 BETWEEN STRINGER S8L AND S9L. INSTALLED DOUBLER REPAIR PER TYPICAL REPAIR 53 -10-14. (M) 2 L 7 2 4F RT A16WE 2002040400055 20020404 00055 NM 2002 4 4 USAA020090 1 20020123 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 32053 24934 PIT - FOUND FLOORBEAM T-CAP CORRODED 50 INCHES BY 3 INCHES, FS 344 UPPER CHORD RBL 6 INCHES - LBLS 6 T-CAP. CORROSION L EVEL 1. REMOVED AND REPLACED T-CAP. (M) 2 L 7 2 4F RT A16WE 2002040400056 20020404 00056 NM 2002 4 4 USAA020091 1 20020223 A 5320 SCUPPER BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 32053 24934 PIT - FOUND CORROSION ON SCUPPER, 34 INCHES BY 3 INCHES, FORWARD SERVICE DOOR THRESHOLD BETWEEN STATION 312-344 RBL 56 I NCHES. CORROSION LEVEL 1. CLEANED CORROSION, PRIMED AND REINSTALLED SCUPPER PER SRM 53-10-07. (M) 2 L 7 2 4F RT A16WE 2002040400057 20020404 00057 NM 2002 4 4 USAA020092 1 20020121 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 32053 24934 PIT - FOUND FLOORBEAM SURFACE CORROSION 1 INCH BY 1 INCH AREA, FS 927 AT ATTACH POINTS FOR FLOORBOARDS. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED LEVEL 1 CORROSION PER SRM 53-0-51. (M) 2 L 7 2 4F RT A16WE 2002040400058 20020404 00058 NM 2002 4 4 USAA020093 1 20020202 A 5754 SKIN BOEING 737 7373B7 1384580 NM SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 42381 23860 PIT - FOUND NR 1 SLAT LOWER LEADING EDGE SKIN CRACKED 3.250 INCHES WIDE BY 17 INCH LONG DOUBLER, STA WBL 557-540 LOWER 4 E SKIN AT RIVET LINE. DOUBLER PREVIOUSLY INSTALLED PER SRM 57-43-01 FIG 206. (M) 2 L 7 2 4F RT A16WE 2002040400059 20020404 00059 NM 2002 4 4 USAA020094 1 20020202 A 5754 SKIN BOEING 737 7373B7 1384580 NM SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 42381 23860 PIT - FOUND NR 2 SLAT LOWER LEADING EDGE SKIN CRACKED 4 INCHES WIDE BY 28 INCHES LONG, STATION WBL 453 SLAT ACT ROD END. DOUBLER PREVIOUSLY INSTALLED PER SRM 57-43-01 FIG 206. (M) 2 L 7 2 4F RT A16WE 2002040400060 20020404 00060 NM 2002 4 4 USAA020095 1 20020202 A 5754 SKIN BOEING 737 7373B7 1384580 NM SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 42381 23860 PIT - FOUND NR 4 SLAT LOWER LEADING EDGE SKIN CRACKED 4 INCHES WIDE BY 54.5 INCH LONG DOUBLER, BETWEEN STATION WBL 254-3 04 LOWER L/E RIVET LINE. DOUBLER PREVIOUSLY INSTALLED PER SRM 57-43-01 FIG 206. (M) 2 L 7 2 4F RT A16WE 2002040400061 20020404 00061 NM 2002 4 4 USAA020096 1 20020202 A 5754 SKIN BOEING 737 7373B7 1384580 NM SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 42381 23860 PIT - FOUND NR 5 SLAT LOWER LEADING EDGE SKIN CRACKED 4 INCHES WIDE BY 30.5 INCH LONG DOUBLER, NR 5 SLAT LOWER RIVET LIN E STATION WBL 355-453. DOUBLER PREVIOUSLY INSTALLED PER SRM 57-43-01 FIG 206. (M) 2 L 7 2 4F RT A16WE 2002040400062 20020404 00062 NM 2002 4 4 USAA020097 1 20020202 A 5754 SKIN BOEING 737 7373B7 1384580 NM SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 42381 23860 PIT - FOUND NR 6 SLAT LOWER LEADING EDGE SKIN CRACKED 4 INCHES WIDE BY 17.5 INCH LONG DOUBLER, STATION WBL 531 NR 6 SLAT LOWER 4E SKIN AT RIVET LINE. DOUBLER PREVIOUSLY INSTALLED PER SRM 57-43-01 FIG 206. (M) 2 L 7 2 4F RT A16WE 2002040400063 20020404 00063 NM 2002 4 4 USAA020103 1 20020204 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 392US 46617 23314 PIT - FOUND FRAME CORRODED 6 INCHES BY .5 INCHES, RBL 8.10 BETWEEN STATION 727E AND 772. CORROSION LEVEL 1. REPAIRED P ER TYPICAL REPAIR 53-10-06B. (M) 2 L 7 2 4F RT A16WE 2002040400064 20020404 00064 NM 2002 4 4 USAABB02016 1 20020217 A 3040 141T480149 HEATER BOEING 757 757225 1384959 NM WINDSHIELD BURNED A USAA G A O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 605AU 865 22201 CLE - FL 741 - IN CRUISE AT FL310, CREW REPORTED THAT THE COCKPIT WAS FILLING UP WITH SMOKE. CREW DONNED THEIR OXYGEN MA SKS AND SMOKE GOGGLES AND PERFORMED AN EMERGENCY DESCENT. FLIGHT DIVERTED TO CLE AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE LOWER LEFT CORNER OF THE L1 WINDSHIELD ARCING AND SMOKING WITH THE WINDSHIELD HEAT ON. THE WINDSH IELD AND HEAT CONTROL WERE REPLACED. (M) 2 L 7 2 4F RT A2NM 2002040400065 20020404 00065 CE 2002 4 4 2002F00360 1 20020401 A 2750 50000084 CONTROL CABLE CESSNA 402 402B 207590P CE TE FLAPS BROKEN E H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED AP APPROACH 1 GL 27 3729C 10585 80 402B0589 WHILE ON APPROACH THE PILOT SELECTED HIS APPROACH FLAP SETTING OF 15 DEGREES. UPON DOING SO HE HEARD A BANG AND THE AIRC RAFT BEGAN A SLIGHT ROLL TO THE RIGHT. HE THEN RETRACTED THE FLAPS, WHICH CORRECTED THE SITUATION. HE CONTINUED HIS APPR OACH AND MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION, IT APPEARS THAT THE RIGHT HAND EXTEND CABLE FAILED AT A POINT A PPROXIMATELY TWO FEET RIGHT OF THE FLAP ACTUATOR, NEAR A PULLEY, CAUSING THE FLAPS TO RETRACT TO THE FULL UP POSITION. F ATIGUE MAY HAVE BEEN A CONTRIBUTING FACTOR TO THIS FAILURE. 1 L 7 2 3O A7CE 2002040400072 20020404 00072 NE 2002 4 4 VNAA0201014 2 20020114 A 7200 PW119B ENGINE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT FAILED A VNAA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 GL 07 438JS 16285 3056 DURING FLIGHT, THE LEFT HAND ENGINE SHUT DOWN. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO MDT. THE LEFT HAND PROPE LLER DID NOT FEATHER. OUT STATION MAINTENANCE INSPECTED THE AIRCRAFT AND TROUBLESHOT THE FUEL PUMP AND HYDRO MECHANICAL UNIT, THIS DID NOT CORRECT THE PROBLEM. DAY MAINTENANCE SENT MECHANICS AND AN ENGINE TO MDT. DAY MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND ENGINE IAW DORNIER MM 72-00-00. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. MAINTE NANCE THEN INSPECTED AND REPLACED FUSE 11KD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400074 20020404 00074 NM 2002 4 4 VNAA0202003 1 20020203 A 5210 STOP FITTING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DOOR OUT OF ADJUST A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 470PS 3006 JUST SOUTH OF CVG, THE CREW RECEIVED A RED WARNING PANEL MAIN CABIN DOOR INDICATION. THE CREW REFERENCED THE QUICK REFE RENCE HANDBOOK AND HEADED TOWARD CVG. WHILE DESCENDING THROUGH 16,000 FEET, THE INDICATION WENT OUT AND THE CREW WAS DI RECTED TO CONTINUE TO DAY. MAINTENANCE INSPECTED AND ADJUSTED THE DOOR STOPS IN ACCORDANCE WITH DORNIER MAINTENANCE MAN UAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400075 20020404 00075 2002 4 4 VNAA0202004 4 20020204 A 3418 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 433JS 3047 DURING TAKEOFF, THE CREW RECEIVED AN ANGLE OF ATTACK FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CREW CLEARED THE RUNWAY AND THE INDICATION CLEARED BY ITSELF. THERE WERE WINDY CONDITIONS AT THIS TIME. FLIGHT 4059 WAS CLEARED FOR ANOTHER TA KEOFF ATTEMPT. FLIGHT 4059 DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400076 20020404 00076 NM 2002 4 4 VNAA0202005 1 20020205 A 2150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 470PS 3006 DURING TAKEOFF THE CREW RECEIVED A LEFT HAND PACK FAIL MESSAGE AND ABORTED TAKEOFF. FLIGHT 4020 CLEARED THE RUNWAY AND THE MESSAGE CLEARED. MAINTENANCE CONTROL HAD THE CREW PERFORMED AN ENGINE RUN AND THE MESSAGE DID NOT APPEAR. FLIGHT 4 020 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400077 20020404 00077 NE 2002 4 4 VNAA0202006 2 20020205 A 7532 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 470PS 3006 DURING TAKEOFF THE CREW RECEIVED A LEFT HAND PACK FAIL MESSAGE AND ABORTED TAKEOFF FLIGHT 4020. THE CREW DEFERRED THE L EFT HAND HIGH PRESSURE BLEED VALVE WITH MAINTENANCE CONTROL AND FLIGHT 4020 DEPARTED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400078 20020404 00078 NM 2002 4 4 VNAA0202007 1 20020206 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 438JS 3056 DURING TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE CONTROL UNIT FAIL MESSAGE AND ABORTED TAKEOFF. THE MESSAGE CLEARED AS FLIGHT 4168 TAXIED ONTO THE TAXI WAY. THE CREW CALLED MAINTENANCE WHO SUGGESTED ANOTHER TAKEOFF ATTEMPT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002041000070 20020410 00070 NM 2002 4 10 02FDEA00226 1 20020328 A 5230 52FS13996 DOOR FRAME BOEING 727 727277 138408S NM CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 MAIN CARGO DOOR AFT SIDE FRAME DENTED ABOVE CENTERING GUIDE RAMP. REMOVED AND REPLACED FRAME PER EA 7-5230-64028. 2 L 7 3 4F RT A3WE 2002040400079 20020404 00079 2002 4 4 VNAA0202008 4 20020206 A 3140 701730011006 COMPUTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY FAULTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 2663 3056 DURING TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE CONTROL UNIT FAIL MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTE D AND REPLACED THE INTEGRATED AVIONICS COMPUTER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHE CKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400080 20020404 00080 NM 2002 4 4 VNAA0202009 1 20020208 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 431JS 3028 DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION MESSAGE AND ABORTED TAKEOFF. AFTER CLEARING THE RUNWAY, THE M ESSAGE CLEARED AND FLIGHT 4157 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4157 THEN DEPARTED WITH NO FURTHER INCID ENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400081 20020404 00081 2002 4 4 VNAA0202010 4 20020209 A 3140 7013348937 DAU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 328JS 1478 3030 DURING CLIMBOUT, THE CREW RECEIVED A NR 2 FAULT WARNING COMPUTER FAIL INDICATION AND RETURNED TO PIT. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAIN TENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400082 20020404 00082 NM 2002 4 4 VNAA0202011 1 20020209 A 3030 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 433JS 3047 DURING TAKEOFF, THE CREW RECEIVED A PITOT HEAT FAIL INDICATION AND ABORTED TAKEOFF. AS THE AIRCRAFT CLEARED THE RUNWAY THE INDICATION WENT OUT BY ITSELF. FLIGHT 4055 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4055 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400083 20020404 00083 NM 2002 4 4 VNAA0202012 1 20020210 A 5270 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FALSE ACTIVATION A VNAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 427JS 3039 WHILE IN CRUISE, THE CREW RECEIVED A MAIN CABIN DOOR OPEN INDICATION. THE CREW DIVERTED TO CLT AND THE INDICATION WENT OUT ON DESCENT. NO EMERGENCY WAS DECLARED AND FLIGHT 4120 LANDED WITH NO FURTHER INCIDENTS. OUTSTATION MAINTENANCE INS PECTED AND FOUND NO DISCREPANCIES. WHEN FLIGHT 4120 ARRIVED IN PIT WITH NO FURTHER INCIDENTS. MAINTENANCE COMPLIED WIT H AN OUTSTATION INSPECTION AND INSPECTED AND PERFORMED OPERATIONAL CHECKS WHICH WERE GOOD. THE AIRCRAFT WAS AGAIN RELEA SED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400084 20020404 00084 2002 4 4 VNAA0202013 4 20020210 A 3418 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 433JS 3047 DURING TAKEOFF, THE CREW RECEIVED A PUSHER FAIL CAS MESSAGE AND ABORTED TAKEOFF. AFTER EXITING THE RUNWAY THE MESSAGE C LEARED. FLIGHT 4021 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400085 20020404 00085 2002 4 4 VNAA0202016 4 20020214 A 3460 COMPUTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 3056 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL INDICATION AND ABORTED TAKEOFF. THE CREW WAS TAXIING TO THE GATE AND THE MESSAGE CLEARED BY ITSELF. MAINTENANCE CONTROL MEL'D THE FLIGHT GUIDANCE COMPUTER AND THE FLIGHT DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400086 20020404 00086 NE 2002 4 4 VNAA0202017 2 20020214 A 7310 FILTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE CLOGGED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 471PS 3007 EN ROUTE FROM SAT TO OKC, THE CREW RECEIVED A LEFT HAND HIGH PRESSURE FILTER BYPASS CAS MESSAGE AND RETURNED TO SAT. FA IRCHILD MAINTENANCE INSPECTED AND REPLACED THE HIGH PRESSURE FILTER AND THE HIGH PRESSURE BYPASS TEMPERATURE SENSOR IN A CCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400087 20020404 00087 NM 2002 4 4 VNAA0202018 1 20020214 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 431JS 12192 3028 THE CREW REPORTED THAT THE EMERGENCY FLOOR STRIP LIGHTING AT ROWS 3 AND 4 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 5 LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400088 20020404 00088 NE 2002 4 4 VNAA0202020 2 20020217 A 7532 4067B000003 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ENGINE MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 427JS 13946 3039 DURING TAKEOFF THE CREW RECEIVED A PACK FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE REPLACED THE HIGH PRESSURE BL EED VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WA S RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400089 20020404 00089 NM 2002 4 4 VNAA0202023 1 20020222 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 438JS 3056 THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL CAS MESSAGE AND ABORTED TAKEOFF. AS THE AIRCRAFT CLEARED THE RUNWAY T HE MESSAGE CLEARED. FLIGHT 4030 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4030 THEN DEPARTED WITH NO FURTHE R INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400090 20020404 00090 NM 2002 4 4 VNAA0202025 1 20020225 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 442JS 3060 DURING TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL INDICATION AND ABORTED TAKEOFF. AS THE AIRCRAFT CLEAR ED THE RUNWAY THE INDICATION EXTINGUISHED BY ITSELF AND FLIGHT 4075 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 407 5 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400091 20020404 00091 NM 2002 4 4 VNAA0202026 1 20020226 A 3240 AC69965 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PARK BRAKE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 438JS 2098 3056 DURING CLIMBOUT, THE CREW RECEIVED A EMERGENCY PARKING BRAKE ACCUMULATOR BRAKE CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND LANDED AT THE NEAREST SUITABLE AIRPORT. OUTSTATION MAINTENANCE INSPECTED AND SERVICED THE MAIN SYSTEM PRECHARGE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 12-00-00. THE AIRCRAFT WAS THEN FERRIED TO CAK WHERE MAI NTENANCE INSPECTED AND REPLACED THE EMERGENCY PARK BRAKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE COMPLETE AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400092 20020404 00092 2002 4 4 VNAA0203002 4 20020303 A 3418 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 433JS 3047 AT 80 KNOTS THE CREW RECEIVED A PUSHER-SHAKER FAIL CAS MESSAGE AND ABORTED TAKEOFF. AFTER EXITING THE RUNWAY THE MESSAG E CLEARED ITSELF. FLIGHT 4015 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400093 20020404 00093 NM 2002 4 4 VNAA0203003 1 20020304 A 2150 A/C PACK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 470PS 3006 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A LEFT HAND PACK FAIL MESSAGE AND ABORTED TAKEOFF. AFTER CLEARING THE RUNWAY , THE CREW RESET THE LEFT HAND PACK AND WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4179 THEN DEPARTED WITH NO FURT HER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400094 20020404 00094 NM 2002 4 4 VNAA0203005 1 20020305 A 2120 4068B00002 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A/C BAY FAILED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 463PS 7828 3087 WHILE SITTING AT THE GATE WITH THE APU RUNNING, THE CREW REPORTED A SMOKE SMELL IN THE CABIN. MAINTENANCE INSPECTED AND REPLACED THE PACK VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE COMPLETE AND T HE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400095 20020404 00095 NM 2002 4 4 VNAA0203007 1 20020308 A 2150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 470PS 3006 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND PACK FAIL MESSAGE AND ABORTED TAKEOFF. THE MESSAGE CLEARED AS FLIGHT 4147 EXITED THE RUNWAY AND FLIGHT 4147 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400096 20020404 00096 NE 2002 4 4 VNAA0203008 2 20020308 A 7532 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 470PS 3006 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND PACK FAIL MESSAGE AND ABORTED TAKEOFF. FLIGHT 4147 THEN RETURNED TO THE G ATE WHERE MAINTENANCE MEL'D THE LEFT HAND HIGH PRESSURE BLEED VALVE. FLIGHT 4147 THEN LEFT WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040400097 20020404 00097 WP 2002 4 4 UPS02837580 1 20020207 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:IN EMERGENCY LIGHTS FAILED PREFLIGHT CHECK. REPLACED LIGHT BATTERY PACK, OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2002040400098 20020404 00098 WP 2002 4 4 UPS02837602 1 20020206 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 STA 1753 CANTED FRAME HAS LONGERON 15L CRACKED. CUT OUT DAMAGED SECTION OF LONGERON, FABRICATED AND INSTALLED LONGERON REPAIR IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2002040400099 20020404 00099 WP 2002 4 4 UPS02837603 1 20020201 A 5514 56545017 STIFFENER DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 LEFT HORIZONTAL STAB L/E STIFFENER IS CRACKED AT XAR 0. REMOVED AND REPLACED STIFFENER IAW DWG 56545 01 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040400100 20020404 00100 WP 2002 4 4 UPS02837604 1 20020204 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 341.5. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATE D, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002040400101 20020404 00101 WP 2002 4 4 UPS02837605 1 20020131 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 STA 1580 FUSELAGE FRAME IS CRACKED AT LOWER END AT LONG 21L. REMOVED DAMAGED AREA, NDT VERIFIED NO C RACKS AROUND CUTOUT, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EO DC8-53A-011. 2 L 7 4 4F RT 4A25 2002040400102 20020404 00102 WP 2002 4 4 UPS02837606 1 20020204 A 5720 97532977 ATTACH ANGLE DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 LEFT WING CENTER L/E VERTICAL ATTACH ANGLE IS CRACKED AT LOWER END AT XS 520. REMOVED, FABRICATED AN D INSTALLED REPLACEMENT ANGLE IAW DWG 9753297 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040400103 20020404 00103 WP 2002 4 4 UPS02837611 1 20020211 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01. 2 L 7 4 4F RT 4A25 2002040400104 20020404 00104 WP 2002 4 4 UPS02837612 1 20020130 A 5230 PAN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 C PIT DOOR PAN CRACKED AT UPPER FWD CORNER NEAR GRAB HANDLE. REMOVED DOOR PAN SECTION P/N 57542060 - 17 & REPLACED IT WITH NEW DOOR PAN SECTION IAW 51-1-8, 51-3-0, 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2002040400105 20020404 00105 WP 2002 4 4 UPS02837613 1 20020130 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 REMOVED STEEL DOUBLER FROM L2 DOOR JAMB EXTERIOR UPPER L2 UPPER AFT CORNER. REPAIRED AREA IAW DC8 SR M 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2002040400106 20020404 00106 WP 2002 4 4 UPS02837614 1 20020127 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 AFT ACCY COMPT STA 1660 FLOORBEAM WEB IS CRACKED I/B OF PREVIOUS REPAIR AT RBL 37. 2 L 7 4 4F RT 4A25 2002040400107 20020404 00107 WP 2002 4 4 UPS02837615 1 20020126 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 REMOVED STEEL DOUBLER FROM L1 DOOR JAMB EXTERIOR UPPER FWD CORNER. REPAIRED AREA IAW REO G08505 AND UPS EO DC8-5330-15976-A. 2 L 7 4 4F RT 4A25 2002040400108 20020404 00108 WP 2002 4 4 UPS02837616 1 20020128 A 5230 PAN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 C PIT DOOR FRAME CRACKED AT UPPER AFT CORNER NEAR GRAB HANDLE. INSTALLED NEW DOOR PAN IAW DC8 SRM 51 -1-21, 51-3-0, 51-1-20D, 51-1-21A. 2 L 7 4 4F RT 4A25 2002040400109 20020404 00109 WP 2002 4 4 UPS02837617 1 20020129 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 AFT PIT CORROSION FS 1060 ON L35L AT FRAME INTERSECT, LONGERON SPLICE FITTING FOUND TO BE CRACKED. 2 L 7 4 4F RT 4A25 2002040400110 20020404 00110 WP 2002 4 4 UPS02837618 1 20020129 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 AFT ACCY COMPARTMENT FS 1660 LONG 32R END FITTING IS CORRODED. RECD LOCATED DRILLER FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 2002040400111 20020404 00111 WP 2002 4 4 UPS02837619 1 20020129 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 AFT ACCY COMPARTMENT FS 1660 LONG 32R IS CORRODED. 2 L 7 4 4F RT 4A25 2002041500067 20020415 00067 WP 2002 4 15 DHL2002807511 1 20020321 A 2752 57726925011 ACTUATOR DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 8206 45990 LEFT MID-WING FLAP ACTUATOR LINK CRACKED. REMOVED AND REPLACED LEFT MID WING FLAP ACTUATOR IAW MM 27-51-9 PG 401, OP'S AND LEAK CHECKS. 2 L 7 4 4F RT 4A25 2002040400112 20020404 00112 WP 2002 4 4 UPS02837620 1 20020130 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 L2 UPPER FWD DOOR JAMB CORNER CRACKED AT FASTENER HOLE. REPAIRED AREA IAW DC8 SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2002040400113 20020404 00113 WP 2002 4 4 UPS02837621 1 20020129 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 AFT PIT FS 1220 C3 DOOR JAMB SHROUD SUPPORT FITTING IS CORRODED. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002040400114 20020404 00114 WP 2002 4 4 UPS02837650 1 20020131 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 L35L HEAVILY CORRODED AT SPILCE FITTING, STA 1690. CUT OUT CORRODED SECTION OF LONG, FABRICATED AND INSTALLED LONGERON REPAIR IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2002040400115 20020404 00115 WP 2002 4 4 UPS02837651 1 20020204 A 5313 37735121 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 LONGERON 11R CRACKED AT R2 DOOR UPPER AFT CORNER. REMOVED CRACKED LONGERON SECTION FROM 1570 TO 1690 . INSTALLED REPLACEMENT SECTION IAW SRM 53-1-0, 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2002040400116 20020404 00116 WP 2002 4 4 UPS02837652 1 20020207 A 5720 5804006504U CLIP DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 RT WING CLIP CRACKED AT XW467 BETWEEN S62 AND S63. REMOVED AND REPLACED CLIP IAW SRM 51-1-20D AND DA C DWG 5804006. 2 L 7 4 4F RT 4A25 2002040400117 20020404 00117 WP 2002 4 4 UPS02837653 1 20020204 A 5711 DOUBLER DOUG DC8 DC871F 302199D WP LT WING BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 LT WING LOWER SPAR CAP DOUBLER BROKEN, PIECE MISSING AT XS520. REMOVED, FABRICATED AND REPLACED DOUB LER IAW SRM 57-2-1 FIG 14 A. 2 L 7 4 4F RT 4A25 2002040400118 20020404 00118 WP 2002 4 4 UPS02837654 1 20020201 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 X-RAY REVEALED ONE INCH CRACK AT R2 DOOR UPPER AFT DOUBLER STA 1660 LONG 11R. CUT OUT DAMAGE. NDT V ERIFIED ALL DAMAGE REMOVED. FABRICATED AND INSTALLED FILLER AND DOUBLERS PER SRM 53-1-0 FIG 16. 2 L 7 4 4F RT 4A25 2002040400119 20020404 00119 WP 2002 4 4 UPS02837655 1 20020201 A 5310 57510409 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 L2 LOWER AFT FRAME CRACKED AT STA 1660 NEAR 19L. REMOVED DAMAGED FRAME SECTION. FAB AND INSTALLED F RAME SECTION, FILLER AND DOUBLER PER DAC DWG 5751040, DC8-5310-11728 AND DC8-53A-011. 2 L 7 4 4F RT 4A25 2002040400120 20020404 00120 WP 2002 4 4 UPS02837656 1 20020206 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 LOWER FLANGE CRACKED ON LONG 15R, STA 1753. REMOVED CRACKED LONGERON SECTION. FABRICATED SPLICE AN D INSTALLED REPLACEMENT LONGERON SECTION PER 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2002040400121 20020404 00121 WP 2002 4 4 UPS02837657 1 20020214 A 3350 6012335 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER M/M 33-50-01. 2 L 7 4 4F RT 4A25 2002040400122 20020404 00122 WP 2002 4 4 UPS02837696 1 20020131 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 LEFT WING CENTER L/E UPPER SKIN IS CRACKED AND HAS INTERGRANULAR CORROSION BETWEEN XFS 341 TO XFS 366 .5. CUT OUT CRACKED AND CORRODED AREAS, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED DOUBLER AND FILLERS IAW SRM 5 7-2-1 FIG 38 AND UPS DC8-57-20040 AND DH SK 703-448. 2 L 7 4 4F RT 4A25 2002040400123 20020404 00123 WP 2002 4 4 UPS02837697 1 20020201 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 STA 118 LONG 36 IS CORRODED BEYOND LIMITS. REMOVED CORRODED LONGERON SECTION STA 100-130, FABRICATED AND INSTALLED LONGERON REPAIR IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2002040400124 20020404 00124 WP 2002 4 4 UPS02837698 1 20020130 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED BEYOND PREVIOUS REPAIR CUTOUT, AT STATION 25 BETWEEN LONG 10L TO 11L AT L-1 DOOR FWD UPPER CORNER OPENING. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW SRM 53-2-0 FIG 15. 2 L 7 4 4F RT 4A25 2002040400125 20020404 00125 WP 2002 4 4 UPS02837699 1 20020202 A 5320 3754473U1 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 STA 388 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 53- 1-0, 51-1-20D. 2 L 7 4 4F RT 4A25 2002040400126 20020404 00126 WP 2002 4 4 UPS02837701 1 20020205 A 5320 PAN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 STA 200 LONG 20R WEB AND DOOR PAN ARE CRACKED AT R-1 DOOR AFT LOWER CORNER. CUT OUT DAMAGE, NDT VERI FIED NO CRACKS. FABRICATED AND INSTALLED REPAIR DOUBLERS ON PAN AND WEB IAW SRM 53-2-0 FIG 23 AND DWG 5615700. 2 L 7 4 4F RT 4A25 2002040400127 20020404 00127 WP 2002 4 4 UPS02837702 1 20020216 A 3350 6012235 BATTERY DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:IN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY UNIT IAW MM 33-50-01, OPS OK. 2 L 7 4 4F RT 4A25 2002040400128 20020404 00128 WP 2002 4 4 UPS02837713 1 20020215 A 5330 561537275 FINGER DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:SP STA 1510 FINGER DOUBLER IS CORRODED BEYOND LIMITS BETWEEN LONG 22L TO 30L. REMOVED, FABRICATED AND R EPLACED DOUBLER IAW DWG 5615372 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002040400129 20020404 00129 WP 2002 4 4 UPS02837719 1 20020219 A 2450 CONTROL PANEL DOUG DC8 DC873F 302199F WP COCKPIT FAILED A IPXA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 01 801UP 46101 INSPECTION TYPE:N/A NR 2 BUS AND LT EMERGENCY BUS FAILED. CREW DECLARED EMERGENCY. LANDING UNEVENTFUL. T/S PER M/M 24 -20-00 REMOVED AND REPLACED NR 2 GENERATOR CONTROL PANEL AND PERFORMED ADJ/TEST PER 24-20-06, OPS CHECKS NORMAL. 2 L 7 4 4F RT 4A25 2002040400130 20020404 00130 WP 2002 4 4 UPS02837720 1 20020207 A 5720 5804006513 CLIP DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 LEFT WING NR 1 ALT TANK HAS 2 ATTACH CLIPS CRACKED AT O/B SKATE ANGLE AT XW485 BETWEEN STRINGER 62 & 63. REMOVED, FABRICATED ONE CLIP, REPLACED OTHER CLIP AND INSTALLED BOTH CLIPS IAW DWG 5804006 AND 5804007 AND SRM 51-1 -20D. 2 L 7 4 4F RT 4A25 2002040400131 20020404 00131 WP 2002 4 4 UPS02837721 1 20020201 A 5320 5641007501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 FRAME FITTING IS CRACKED AT STA 781 ON FWD SIDE ABOVE WING CENTER SECTION LBL 59. REMOVED, FABRICATE D AND REPLACED FITTING IAW DWG 5641007, 8110-3 APPROVED DH SK 703-641 AND DC8-53-20143A. 2 L 7 4 4F RT 4A25 2002040400132 20020404 00132 WP 2002 4 4 UPS02837722 1 20020131 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 STATION 1322 LONG 21L AT LBL 67 CUSP IS CORRODED BEYOND LIMITS. CUT OUT CUSP SECTION BETWEEN STA 125 0-1390, FABRICATED AND INSTALLED REPAIR SECTION OD CUSP IAW DWG J060296 AND SRM 53-2-5 FIG 15. 2 L 7 4 4F RT 4A25 2002040400133 20020404 00133 WP 2002 4 4 UPS02837723 1 20020206 A 5720 3704841501 FITTING DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C2 STRINGER FITTING CRACKED BETWEEN XRS 50 AND XRS 74 AT STRINGER 51 IN LEFT WING TANK. REMOVED AND REP LACED FITTING IAW DWG 3704841 AND SRM 51-1-20D, 51-1-20D, 51-1-23. 2 L 7 4 4F RT 4A25 2002040400134 20020404 00134 WP 2002 4 4 UPS02837727 1 20020224 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CREW DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:PFLT EMERGENCY LIGHT AT CREW DOOR INOP. REPLACED LAMP, OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2002040400135 20020404 00135 WP 2002 4 4 UPS02837728 1 20020225 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT'S BATTERY PACK, OPS CHECK GOOD IAW MM CHAPTER 33. 2 L 7 4 4F RT 4A25 2002040400136 20020404 00136 2002 4 4 UPS02837729 4 20020224 A 2565 FABRIC DOUG DC8 DC871F 302199D WP EVA SLIDE FRAYED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:PFLT EMERGENCY ESCAPE SLIDE GIRT BAR HAS FABRIC ATTACHMENT FRAYING. REMOVED AND REPLACED SLIDE. 2 L 7 4 4F RT 4A25 2002040400137 20020404 00137 WP 2002 4 4 UPS02837730 1 20020227 A 5330 FINGER DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:PFLT CORROSION UNDER FINGER DOUBLER AT STA 24 LONGERON 31R AT E/E COMPARTMENT. INSPECTED OUTER SKIN FOR CORROSION LOSS USING LOW FREQUENCY E/E PER NDT STANDARD PRACTICE MANUAL 06-10-02 PROCEDURE NR 2 LOSS OF SKIN INDICATED AT 10 PERCENT C/W EO DC8-5310-16320A INTERIM REPAIR FOR CORROSION AT FINGER DOUBLER. 2 L 7 4 4F RT 4A25 2002040400138 20020404 00138 WP 2002 4 4 UPS02837732 1 20020225 A 5320 975464660 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C INTERCOSTAL HAS HOLES IN RADIUS AT STA 1100-1120, L33R-L34R. FABRICATED REPLACEMENT INTERCOSTAL PER D AC DWG 9754949. INSTALLED IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040400139 20020404 00139 WP 2002 4 4 UPS02837733 1 20020225 A 5320 975494960 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C HOLES IN INTERCOSTAL BEND RADIUS AT STA 1100-1120 L33R TO L34R. FABRICATED REPLACEMENT INTERCOSTAL PE R DAC DWG 9754949. INSTALLED SAME PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040400140 20020404 00140 WP 2002 4 4 UPS02837734 1 20020221 A 5320 561032617 ATTACH ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C INTERCOSTAL ATTACH ANGLE CRACKED AT STA 600 RBL 12. REMOVED ANGLE, FABRICATED REPLACEMENT PER DAC DWG 5610326, INSTALLED PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002040400141 20020404 00141 WP 2002 4 4 UPS02837735 1 20020226 A 5313 57799163643032 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C L22R CORRODED BEYOND LIMITS. REMOVED L22R FROM STA 80 TO 130 IAW SRM 51-1-20D AND 51-1-21. INSTALLED LONGERON PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040400142 20020404 00142 WP 2002 4 4 UPS02837736 1 20020223 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C LOWER AFT CORNER OF R1 DOOR CUTOUT REQUIRES REPAIR IAW SRM 53-2-0 FIG 14. REMOVED EXISTING DOUBLER PE R SRM 51-1-20D. CUT OUT DAMAGE, NDT VERIFIED ALL DAMAGE REMOVED PER NDT SPM 06-10-01. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIG 14. 2 L 7 4 4F RT 4A25 2002040400143 20020404 00143 WP 2002 4 4 UPS02837737 1 20020225 A 5313 37585931 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C L35L CORRODED AND CRACKED AT STA 1270. REMOVED AND REPLACED DAMAGED LONGERON 35L FROM STA 1270 TO STA 1350 IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040400144 20020404 00144 WP 2002 4 4 UPS02837738 1 20020225 A 5313 37585931 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C L34L CRACKED AND CORRODED BEYOND LIMITS AT STA 1270. REMOVED L34L FROM STA 1270 TO STA 1350 PER SRM 5 1-1-20D. INSTALLED NEW LONGERON PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040400145 20020404 00145 WP 2002 4 4 UPS02837739 1 20020219 A 5320 5716454278 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C INTERCOSTAL CRACKED AT STA 1520 L33R. REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-20D. FOUND ATTACH ANG LE AND CLIP DAMAGED BEYOND LIMITS. INSTALLED PARTS PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040400146 20020404 00146 WP 2002 4 4 UPS02837741 1 20020224 A 5330 577991515 FINGER DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C FINGER DOUBLER CRACKED AT STA 1130 TO 1250 AT L31L. REMOVED DAMAGED FINGER DOUBLER FROM STA 1130 TO 1 250 IAW SRM 51-1-20 D. FABRICATED DOUBLER AND INSTALLED PER SRM 53-4-1 FIG 51. 2 L 7 4 4F RT 4A25 2002042400074 20020424 00074 EU 2002 4 24 SABA020043 1 20020403 A 7722 8974768 COMPENSATOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAULTY A SABA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 33 964AE 964 AIRCRAFT 964 ON FLIGHT 5152 FROM CLT TO LWB. DURING TAKEOFF ROLL BOTH ENGINES MADE ONLY 80 PERCENT TORQUE. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEMS. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE EGT COMPENSATOR FOR THE RIGHT ENGINE. MAINTENANCE ALSO ADJUSTED THE EGT COMPENSATOR FOR THE LEFT ENGIN E. GROUND AND OPS CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 2002040800043 20020408 00043 NM 2002 4 8 DHL2002740002 1 20020402 A 2612 FIRE DETECTOR BOEING 727 7272Q9 138448M NM APU BAY FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 740DH 21930 APU FIRE DETECTION FAILS TO TEST. DEFERRED, COMPLIED WITH PLACARD INSTALLED. 2 L 7 3 4F RT A3WE 2002040400147 20020404 00147 NM 2002 4 4 PCAA0204042 1 20020402 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM #2 INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 810EX 26120 308 DURING ROUTINE MAINTENANCE VISIT FIRST TWO AISLE EMERGENCY LIGHTS FOUND INOPERATIVE. BOTH LIGHT ASSEMBLIES WERE REPLACED DUE TO WIRING BEING CRUSHED. AFTER TROUBLESHOOTING FOUND PS2 POWER SUPPLY INOPERATIVE. PS2 POWER SUPPLY REPLACED. OPERA TIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002041600075 20020416 00075 NM 2002 4 16 PCAA0203039 1 20020327 A 2910 82940014105 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM LEAKING A PCAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 13 806EX 263 PHL-HPN FLIGHT 3668 AT 13,000 FEET IN CRUISE FLIGHT NR 1 HYDRAULIC SYSTEM FAILED. ROLL SPOILER INBOARD HYDRAULIC AND NR 1 HYDRAULIC ISOLATION LIGHTS ILLUMINATED. EMERGENCY DECLARED AND FLIGHT DIVERTED TO ISP. HYDRAULIC QUANTITY AT .5 QUA RT UPON LANDING. NORMAL BRAKES WERE INOPERATIVE. EMERGENCY BRAKES WORKED NORMALLY. MAINTENANCE INSTALLED A 36 INCH LO NG FLEXIBLE HYDRAULIC LINE. LEAK CHECK WAS GOOD IN ACCORDANCE WITH DEHAVILLAND DASH 8 MM 20-50-52. LEFT AND RIGHT HYDR AULIC SYSTEM SERVICED. SPOILER LINE LOCATED AT TOP CENTER FUSELAGE JUST AFT OF FORWARD WING SPAR. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002040400148 20020404 00148 NM 2002 4 4 ZW0A0204001 1 20020331 A 3350 CM387Q LAMP BOEING 757 757231 1384950 NM A ZW0A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 13 715TW 28483 THE LEFT AFT CABIN DOOR SLIDE LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 10-14-00 LAX. --CLOSED-- 2 L 7 2 4F RT A2NM 2002040400149 20020404 00149 WP 2002 4 4 DHL2002807512 1 20020323 A 2760 3654073 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 45990 ITEM: REF.: N/R 1243 #4 SPOILER SHOWS CRACKED FITTINGCORR.: R/R LH. SPOILER #4 FITTING I/A/W MM 27-61-1 PG. 202, 203 , 2 06- REFER TO N/R 2387 FOR OPS CHECK 2 L 7 4 4F RT 4A25 2002040400150 20020404 00150 WP 2002 4 4 DHL2002807513 1 20020322 A 5313 47723971 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 1440 AFT FUS. INTERIOR- FITTING CRACKED 2" @ STA. 1776.000 L17LCORR: REMOVED CRACKED FITTING I/A/W/ SRM5 1-1-20D , PG. 27 CLEANED TREATED & PRIMED AREA I/A/WSRM51-1-8B , INSTALLED NEW FITTING @ AFT FUS. INTERIOR (STA. 1776.0 00 , L17L) I/A/W SRM51-1-20D PG. 9 2 L 7 4 4F RT 4A25 2002040400151 20020404 00151 NM 2002 4 4 AWXA200200289 1 20020126 A 5315 654N02438 TRACK BOEING 757 7572S7 1384962 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 0 0 23322 GYR - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 398, RBL 45.0. MAINTENANCE REMOVED DAM AGED SECTION OF FLOOR SUPPORT BETWEEN BS 363 AND BS 415, RBL 45, FABRICATED NEW SECTION OF FLOOR SUPPORT AND INSTALLED R EPAIR IAW B757-200 SRM 51-40-0, AND SRM 53-10-51, PG. 1-6. 2 L 7 2 4F RT A2NM 2002040400152 20020404 00152 NM 2002 4 4 AWXA200200290 1 20020325 A 5311 65677758 FRAME BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 0 0 23627 MCN - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON R/H INBOARD ANGLE AT THE LOWER FASTENER HOLE ON THE FRAME AT BS 616, WL 199. MAINTENANCE REMOVED CRACKED AREA OF INNER CHORD AND PERFORMED HFEC INSPECTION TO VERIFY CRACK IS CONTAI NED. FABRICATED REPAIR ANGLE, FILLER, AND SHIM, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2002040400153 20020404 00153 NM 2002 4 4 AWXA200200293 1 20020310 A 5313 BAC1498162 STRINGER BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 0 0 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER IN THE AFT CARGO COMPARTMENT BS 1010, STR 27 R/H. MAINTENANCE REMOVED CORRODED STRINGER 27 R/H AT STA 1010, FABRICATED AND INSTALLED A NEW STRINGER IAW B737- 300 SRM 51-10-2, PG. 12, SRM 51-40-2, PG. 1, AND BMM 20-50-11, PG. 204. 2 L 7 2 4F RT A16WE 2002040400154 20020404 00154 NM 2002 4 4 AWXA200200295 1 20020311 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT AND NUTPLATES IN THE AFT CARGO PIT AT BS 773, LBL 2.5. MAINTENANCE REMOVED NUTPLATES AND CLEANED CORROSION, FABRICATED 2 EACH REPAIR ANGLES AND INSTALLED R EPAIR PARTS IAW B737-300 SRM 53-00-58, FIG. 201, PG. 203. 2 L 7 2 4F RT A16WE 2002041500183 20020415 00183 NM 2002 4 15 F3LA200200122 1 20020404 A 5414 FAIRING BOEING 737 73736E 138443A NM NR 1 ENGINE DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 314FL 3489 25256 DURING C-2 CHECK, INSPECTION REPORTED DELAMINATION ON TOP INSIDE DUCT OF NR 1 ENGINE INBOARD THRUST REVERSER MID STREAM FAIRING AND METAL MISSING. REMOVED DAMAGE, FABRICATED DOUBLER AND INSTALLED REPAIR PER EA 54-737-041 AND SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002040400155 20020404 00155 NM 2002 4 4 02040401 1 20020403 A 3350 FUSE BRUCE BOEING 757 757200 1384950 NM BLOWN A N8TA O OTHER L NO TEST IN INSP/MAINT 1 WP 19 547 NA 29946 Emergency Lights Rows 7-15ABC INOP. Replaced fuses Ops. Ck. Normal as per M/M 33-51-00 2 L 7 2 4F RT A2NM 2002040500001 20020405 00001 2002 4 5 0201096624 4 20020327 A 2565 4A30479 RESERVOIR 7A123857 BOEING 747 747251B 1384892 NM VALVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 624US 1538 G655 21706 WHILE FLAT FIRING THE DOOR SLIDE ASSEMBLY PRIOR TO OVERHAUL, THE RESERVOIR DELAYED THREE SECONDS AFTER THE MANUAL FIRING LANYARD WAS PULLED. OVERHAULED THE DOOR SLIDE. 2 L 7 4 4F A20WE 2002040500008 20020405 00008 NM 2002 4 5 SWAA020705 1 20020402 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED 4 INCHES AT BS 769, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002040500009 20020405 00009 NM 2002 4 5 SWAA020706 1 20020402 A 5320 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR 2R AND 3R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002040500010 20020405 00010 NM 2002 4 5 SWAA020707 1 20020402 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, BETWEEN STR 8R AND 9R. REPAIRED FRAME PER BFG ER. 2 L 7 2 4F RT A16WE 2002040500011 20020405 00011 NM 2002 4 5 SWAA020708 1 20020402 A 5315 BAC1509 FLOORBEAM BOEING 737 7373Y0 1384671 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 845, LBL 12. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002040500012 20020405 00012 NM 2002 4 5 SWAA020709 1 20020402 A 5320 6547977 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D CHECK, FOUND WEBS CRACKED (3 EA) AT BS 295 AT STR 12L, BS 295 AT STR 7L, BS 278 AT STR 14 R. REMOVED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2002040500013 20020405 00013 NM 2002 4 5 SWAA020712 1 20020402 A 3350 207377 LENS BOEING 737 7372T4 1384492 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LENS MISSING AT OVERWING EXIT. INSTALLED LENS PER MM. 2 L 7 2 4F A16WE 2002040500014 20020405 00014 NM 2002 4 5 SWAA020713 1 20020403 A 5313 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002040500015 20020405 00015 NM 2002 4 5 SWAA020714 1 20020403 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN CRACKS (2 EA) AT STR 10R, BS'S 430 AND 450. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002040500016 20020405 00016 NM 2002 4 5 SWAA020716 1 20020403 A 5314 6545409 WEB BOEING 737 7373Y0 1384671 NM LT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 33. REPAIRED WEB PER SWA RA. 2 L 7 2 4F RT A16WE 2002040500017 20020405 00017 NM 2002 4 5 VNAA0203033 1 20020321 A 2400 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 459PS 3070 DURING TAKE OFF, THE CREW RECEIVED A ECU FAIL CAS MESSAGE AND ABORTED TAKE OFF. THE AIRCRAFT CLEARED THE RUNWAY AND THE MESSAGE CLEARED BY ITSELF. THE CREW ATTEMPTED ANOTHER TAKE OFF AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040500018 20020405 00018 NE 2002 4 5 VNAA0203035 2 20020321 A 7300 1060003 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 459PS 16313 3070 DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL INDICATION AND ABORTED TAKE OFF. MAINTENANCE IN SPECTED AND REPLACED THE BUS POWER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHE CKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040500019 20020405 00019 NM 2002 4 5 VNAA0203040 1 20020325 A 2400 DTSP400L BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 437JS 11803 164 3055 ENROUTE FROM DCA TO BTV, THE NUMBER TWO BATTERY OVERHEATED. THE CREW CALLED DISPATCH AND DIVERTED TO IPT. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE NUMBER TWO BATTERY IN ACCORDANCE WITH DORNIER MAIN TENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040500020 20020405 00020 NM 2002 4 5 VNAA0203042 1 20020324 A 2700 FE255000 DAMPER 84282 DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 07 429JS 16120 221 151 3043 THIS IS AN AMENDMENT TO VNAA0203038. MAINTENANCE INSPECTED AND REPLACED THE RUDDER DAMPER AND LIMIT ACTUATOR IN ACCOR DANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. A FUNCTIONAL CHECK FLIGHT WAS PERFORMED AND THE AIRCRAFT WAS THEN RELEA SED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040500021 20020405 00021 NM 2002 4 5 VNAA0203044 1 20020328 A 7100 CONTACTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 07 429JS 3043 AFTER TAKE OFF THE CREW REPORTED THE RIGHT HAND ENGINE HAD A LOW POWER TORQUE SPILT AND RETURNED TO PIT. MAINTENANCE I NSPECTED AND REPAIRED A CONTACTOR ON THE TRIM SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. OPERATIONA L CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002040500022 20020405 00022 NM 2002 4 5 801DM0003 1 20020402 A 3350 3020413 LIGHT BOEING 757 757200 1384950 NM A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 801DM 26240 L1 door emergency slide light inop. R&R light assy. 2 L 7 2 4F RT A2NM 2002040500023 20020405 00023 NM 2002 4 5 200200209 1 20020403 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 SEAT TRACK STA 400 RT SIDE 70" SIDE FROM BUTTLINE 0 CORROSION. REMOVED AND REPLACED DAMAGED SEAT TRACK FRAME FS 370-410 RBL 70 APPROX PER B747 SRM 53-10-5 FIG 1A. 2 L 7 4 4F A20WE 2002040500024 20020405 00024 NM 2002 4 5 200200210 1 20020403 A 5310 SHEAR TIE BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 LOWER FRAME STIFFENER AT BS 2140 BETWEEN S-46 AND S-47 RIGHT IS CRACKED. REMOVED DAMAGED SHEAR TIE SECTION BS 2140 AND 46R - AND 44L PER B747 SRM 53-10-4 FIG 3A. FABRICATED AND INSTALLED SECTIONS AND REPAIR PARTS PER B747 SRM 51-30-02 AND 53-10-04 FIG 41. 2 L 7 4 4F A20WE 2002040500025 20020405 00025 NM 2002 4 5 200200211 1 20020403 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 MAIN DECK IN BETWEEN STA 440-460 RBL 66 HAS A CORRODED SEAT TRACK FLANGE. REMOVED AND REPLACED CORRODED SEAT TRACK FROM STA 332 RBL 45 TO STA 460 RBL 67 PER B747 SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002040500039 20020405 00039 SO 2002 4 5 C2XA02CL089 1 20020404 A 3350 110049 CHARGER EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13970 145146 DURING ROUTINE MAINTENANCE THE EXTERIOR OVERWING EMERGENCY LIGHTS WOULD NOT TEST.MAINTENANCE INSPECTED AND REPLACED THE #4 EMERGENCY BATTERY CHARGER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002040500040 20020405 00040 SO 2002 4 5 COMA0210012 1 20020402 A 3230 12038594001 CONTROL BOX EMB 120 EMB120RT 3260202 SO INST PANEL MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS CL CLIMB 1 SO 01 264CA 7 7 120256 FLIGHT 5070 LANDING GEAR CONTROL COULD NOT BE SELECTED TO THE UP POSITION.REPLACED THE L/G CONTROL HANDLE ASSY. 2 L 7 2 4T RT A31SO 2002040500042 20020405 00042 NM 2002 4 5 2002UALA00534 1 20020321 A 7930 21SN04404 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 557UA 26653 717979 RIGHT ENGINE OIL FILTER EICAS MSG AND RIGHT OIL FILTER STATUS MESSAGE APPEARED IN FLIGHT. EICAS MESSAGE EXTINGUISHED AF TER ONE MINUTE. OIL FILTER & BYPASS SWITCH REPLACED. OIL FILTER AND CHIP DETECTORS CHECKED CLEAN. OIL FILTER BYPASS S WITCH TESTED AND FOUND IT DREW EXCESSIVE CURRENT. SUSPECT A SHORT IN THE COIL. SWITCH SENT TO THE OEM FOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002040500043 20020405 00043 EA 2002 4 5 COMA0260228 1 20020401 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING E O VIBRATION/BUFFET OTHER CL CLIMB 1 SO 01 812CA 7381 FLIGHT 6152 LOUD SQUEALING AND VIBRATION FROM R/H SIDE OF COCKPIT.GROUND INTERFONE DOOR FOUND OPEN - SECURED DOOR CLOSED - NO DAMAGE TO AIRCRAFT. 2 L 7 2 4F RT A21EA 2002040500044 20020405 00044 EA 2002 4 5 COMA0260229 1 20020403 A 5210 601R31902318 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA PASSENGER DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 818CA 3994 7408 DURING COMPLIANCE OF C-CHECK TASK 52-840-100, THE PAX DOOR AFT LOWER INTERCOSTAL (VIEWED WITH THE DOOR OPEN), JUST BELOW THE BOTTOM BAYONET FITTING WAS FOUND CRACKED 3/8". THE INTERCOSTAL WAS REPLACED PER CRJ SRM STANDARD PRACTICES AND COM AIR ENGINEERING AUTHORIZATION #10-5210-00072. 2 L 7 2 4F RT A21EA 2002040500046 20020405 00046 EU 2002 4 5 2002F00364 1 20020321 A 2910 D2907019000200 MANIFOLD AIRBUS 320 A320233 3930329 EU HYD SYSTEM LEAKING A RJEF O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 23 454TA 789 AT THE ARRIVAL OF FLT 221, FLIGHT CREW REPORTED THE YELLOW RESERVOIR LOW LEVEL. ON GROUND TECHNICIANS FOUND A LEAK AT T HE PTU MANIFOLD. THE PTU MANIFOLD WAS REPLACED AS PER AIRCRAFT MM 29-13-15 AND OPERATIONAL TEST WAS PERFORMED IAW AIRCR AFT MM 29-23-00. RESULTS WERE SATISFACTORY, THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2002040500047 20020405 00047 NE 2002 4 5 2002F00365 2 20020325 A 7200 ENGINE AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 2 MALFUNCTIONED A SOKF O OTHER J WARNING INDICATION CL CLIMB 1 SO 23 472TA 1113 DURING CLIMB OF THE FLIGHT LR623, EGT ENGINE NR 2 WENT OUT OF LIMITS, AFTER THE CREW PERFORMED ALL NECESSARY CHECKLIST T HE AIRCRAFT WAS RETURNED TO TORONTO AIRPORT. AT TORONTO STATION, THE AIRCRAFT REMAINS ON GROUND FOR MAINTENANCE CHECKS AND FURTHER DISPOSITION. (M) 2 L 7 2 4F 4 F RT A28NM E40NE 2002040500048 20020405 00048 NM 2002 4 5 2002F00367 1 20020305 A 7603 FFG052AC THROTTLE BOEING 757 75733N 1384931 NM LT ENGINE INOPERATIVE A AMTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 11 551TZ 3683 32585 FLT 108, WHEN SETTING MAX TAKEOFF POWER LEFT THROTTLE LAGS BEHIND RIGHT THROTTLE. ABOVE 100 KTS IAS LEFT EPR DECREASED .03 WITH THROTTLE AT FORWARD STOP LIMIT. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE RE MOVED AND REPLACED THE FUEL FLOW GOVERNOR. (M) 2 L 7 2 4F RT A2NM 2002040500050 20020405 00050 WP 2002 4 5 2002F00369 1 20020228 A 2133 OUTFLOW VALVE LKHEED 1011 10113851 5265010 WP FUSELAGE STUCK A AMTA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 186AT 193C1074 ON DEPARTURE, CABIN FAULT LIGHT CAME ON AT 8,000 FEET CABIN ALTITUDE. FORWARD OUTFLOW VALVE STUCK AND HORN AT FULL OPEN , AFT WENT TO FULL CLOSED. AIRCRAFT RETURNED TO AIRPORT. MAINTENANCE REMOVED AND REPLACED THE PRESSURIZATION CONTROL P ANEL PER MM 21-31-01. PERFORMED ADJUSTMENT AND TEST PER 21-31-00. OP CHECK NORMAL. (M) 2 L 7 3 4F A23WE 2002040500051 20020405 00051 NM 2002 4 5 200200204 1 20020402 A 5720 STIFFENER BOEING 747 747132 1384882 NM LT WING CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 LEFT WING WS 1425 CRACKED STIFFENER ON REAR SPAR. REMOVED AND REPLACED STIFFENER ON REAR SPAR PER B747 SRM. 2 L 7 4 4F A20WE 2002040500052 20020405 00052 NM 2002 4 5 200200205 1 20020403 A 5720 STIFFENER BOEING 747 747132 1384882 NM LT WING CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 LEFT WING WS 1485 CRACKED STIFFENER ON REAR SPAR. REMOVED CRACKED STIFFENER AND INSTALLED NEW STIFFENER PER B747 SRM. 2 L 7 4 4F A20WE 2002040500054 20020405 00054 NM 2002 4 5 200200206 1 20020403 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 MAIN DECK AT STATION 1914-1940 AT LBL 11 HAS CORRODED SEAT TRACK. REMOVED AND REPLACED CORRODED SEAT TRACK IAW B747 SRM . 2 L 7 4 4F A20WE 2002040500055 20020405 00055 NM 2002 4 5 200200207 1 20020403 A 5311 FRAME BOEING 747 747132 1384882 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 EXFOLIATION CORROSION ON TOPSIDE OF WHALE BONE STRUCTURE FS 987 LBL 45-47 WHERE AIR CONDITIONING BAY SERVICE LIGHT BRACK ET MOUNTS TO WHALE BONE. REMOVED DAMAGED AREA PER SRM 51-40-04 FIG 2, FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2. 2 L 7 4 4F A20WE 2002040500056 20020405 00056 NM 2002 4 5 200200208 1 20020403 A 5320 SUPPORT BOEING 747 747132 1384882 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 UPPER DECK LAV THRESHOLD SUPPORT BEAM STA 440 - 460 HAS CORROSION. REMOVED THRESHOLD PER SRM 51-30-2, FABBED NEW U-CHAN NEL AND INSTALLED PER B747 SRM 51-30-2. 2 L 7 4 4F A20WE 2002040500057 20020405 00057 NE 2002 4 5 AALA20020257 2 20020304 A 7250 TURBINE WHEEL BOEING 767 767223 1385123 NM GE CF6 CF680A 30025 NE LT ENGINE SEIZED A AALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 21 319AA 22320 580337 LAX - FLT 76 - EN ROUTE LAX-DFW, ON ROTATION, LEFT ENGINE SHUTDOWN. ALL ENGINE INDICATIONS ZEROED AND FAN SEIZED. RETU RNED LAX LANDED WITHOUT INCIDENT. FOUND 860 ROTOR SEIZED. ACCOMPLISHED PYLON INSPECTION AND CHANGED LEFT ENGINE. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 2002041000093 20020410 00093 NM 2002 4 10 2002UALA00535 1 20020325 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 STATION 178 LEFT HAND VERTICAL SIDE CHORD CRACKED AT STRINGER 17. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050200068 20020502 00068 EU 2002 5 2 2002UALA00536 1 20020223 A 2621 34600017 FIRE BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO BAY UNSERVICEABLE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 475UA 2300 2300 1495 CREW REPORTS ECAM MESSAGE INDICATES A FIRE BOTTLE DISCHARGE. REPLACED CARGO FIRE BOTTLE DUE TO LOW PRESSURE INDICATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2002050200069 20020502 00069 EU 2002 5 2 2002UALA00537 1 20020322 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 418UA 485 DOOR ASSIST BOTTLE AT 2L LOW. SERVICED ASSIST BOTTLE PRESSURE TO 1750 PSI, CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2002040500058 20020405 00058 NM 2002 4 5 2002UALA00540 1 20020323 A 5312 BULKHEAD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 CABIN STATION 246, RBL 50, BULKHEAD WEB IS PUNCTURED. MAJOR REPAIR ACCOMPLISHED. REPAIRED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040500059 20020405 00059 NM 2002 4 5 2002UALA00545 1 20020323 A 5210 DOOR FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 L-2 DOOR CHORD HAS SEVERE CORROSION-EXFOLIATION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FILLER AND DOUBLE R. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040500060 20020405 00060 NM 2002 4 5 2002UALA00548 1 20020323 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 CHAFED LOWER SKIN AFT OF STATION 1725.5 ABOVE STRINGER 22 LT. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUB LER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040500061 20020405 00061 NM 2002 4 5 2002UALA00549 1 20020323 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 CHAFED LOWER SKIN AFT OF STATION 1725.5 ABOVE STRINGER 22 RT. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPA IR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040500062 20020405 00062 NM 2002 4 5 2002UALA00550 1 20020323 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 LEFT HAND FUSELAGE SKIN CHAFED AFT OF STATION 1809.5 AT STRINGER 17. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALL ED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040500063 20020405 00063 NM 2002 4 5 CALA0200169 1 20020403 A 5743 FITTING BOEING 737 7373T0 1384582 NM R/W AFT SPAR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND R/H MLG FITTING AFT SPAR CASTING HOLE AT FALSE SPAR O/B ATTACH PIN CORRODED. THE CORROSION WAS REMOVED IAW ECRA 5711-01038. 2 L 7 2 4F RT A16WE 2002040500064 20020405 00064 WP 2002 4 5 CALA0200170 1 20020404 A 5730 SKIN DOUG DC9 DC982 3022082 WP #1 FLAP VANE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND L/H WING #1 I/B FLAP VANE DENTED AND PUNCTURED. THE DAMAGED AREA OF SKIN WAS CUT OUT. FILLERS AND A DOU BLER WERE INSTALLED IAW SRM 57-03 AND 51-70-2. 2 L 7 2 4F A6WE 2002040500065 20020405 00065 WP 2002 4 5 CALA0200172 1 20020404 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 1098-1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND L/H I/B SEAT TRACK CORRODED FROM STA 1098-1174. THE SEAT TRACK WAS REMOVED AND A NEW SECTION OF TRACK W AS INSTALLED IAW SRM 51-30-1, 51-10-4, 51-10-3, 51-30-5, AND 53-05, FIGURE 4. 2 L 7 2 4F A6WE 2002040500066 20020405 00066 WP 2002 4 5 CALA0200174 1 20020404 A 5320 FITTING DOUG DC9 DC982 3022082 WP STA 155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND GALLEY SUPPORT FITTING CORRODED AT STA 155, RBL 10. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10- 04, 51-10-03, AND 51-30-2. 2 L 7 2 4F A6WE 2002040500067 20020405 00067 WP 2002 4 5 CALA0200175 1 20020404 A 5230 SKIN DOUG DC9 DC982 3022082 WP FWD CARGO DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND FORWARD EDGE OF FORWARD CARGO DOOR SKIN CRACKED AND BENT JUST ABOVE LOCK MECHANISM AND SEAL. THE CRACK MEASURED 0.4" LONG. THE EXISTING FASTENERS WERE REMOVED, THE CRACK WAS STOP DRILLED, AND A DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND 52-05, FIGURE 4. 2 L 7 2 4F A6WE 2002040500068 20020405 00068 WP 2002 4 5 CALA0200176 1 20020404 A 5753 SKIN DOUG DC9 DC982 3022082 WP R/W T/E FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND R/H WING I/B T/E FLAP PANEL #1613C SKIN NICKED AND GOUGED. THE SKIN WAS REMOVED AND REPLACED IAW SRM 51 -30-2 AND 51-10-3. 2 L 7 2 4F A6WE 2002040500069 20020405 00069 WP 2002 4 5 CALA0200177 1 20020404 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP STA 1485-1497 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND A 2" CRACK IN SUPPORT IN AFT ACCESSORY COMPARTMENT BETWEEN CANTED FRAMES STA 1485 AND 1497 AND BELOW LE FT AIRSTAIR TORQUE TUBE. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-30-1, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 2002040500070 20020405 00070 WP 2002 4 5 CALA0200179 1 20020404 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FS 1003 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND A 1.75" CRACK AT LOWER RADIUS OF LONGERON 20R EXTERNAL FITTING, FS 1003. THE CRACKED AREA WAS REMOVED I AW EA 9-5310-2-A0942 AND HFEC REVEALED NO FURTHER CRACKS IAW NTSPM 06-10-01. REPAIR PARTS WERE INSTALLED IAW EA 9-5310-- 2-A0942. 2 L 7 2 4F A6WE 2002040500071 20020405 00071 WP 2002 4 5 CALA0200180 1 20020404 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 237 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND MAIN DECK SEAT TRACK CORRODED AT STA 237, RBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30 -2. 2 L 7 2 4F A6WE 2002040500072 20020405 00072 NM 2002 4 5 AALA20020258 1 20020305 A 7830 SWITCH BOEING 767 767223 1385123 NM LT ENGINE FAILED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 323AA 22324 JFK - FLT 133 - EN ROUTE JFK-LAX - JUST AFTER TAKEOFF, LEFT ENGNE REVERSER UNLOCK LIGHT ILLUMINATED. NO ADVERSE YAW NOT ED. RETURNED JFK AND LANDED WITHOUT INCIDENT. REPLACED MICRO SWITCH PACK TO LEFT ENGINE REVERSER PER MM. ALL OPERATIO NAL CHECKS NORMAL. (M) 2 L 7 2 4F RT A1NM 2002040500073 20020405 00073 WP 2002 4 5 ASAA0280052 1 20020220 A 5230 S22418402 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K CHECK, FOUND MID CARGO BAY DOOR TO BE CRACKED AT INNER SKIN OF LIGHTENING HOLE AT LOWER SIDE NEAR INNER HANDLE MECHANISM. REPAIRED SKIN PER EA 5230-01162. (M) 2 L 7 2 4F RT A6WE 2002040500074 20020405 00074 SO 2002 4 5 SIMA200207201 1 20020306 A 5313 STRINGER EMB 145 EMB145 3260210 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AE 145068 ABI - DURING INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19R CHAFED. BLENDED CHAFE, FABRICATED TWO DOUBLERS ANGLE 1 4.5 INCH BY 1.5 INCH, .050 INCH THICK, AND FOUR SHIMS 4.5 INCH BY .75 INCH .080 INCH THICK IAW EMB 145 SRM 145/1142 REV 17 53-25-02, GST-0633/02, ETN EMB53-00-020 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002040500075 20020405 00075 SO 2002 4 5 SIMA200207202 1 20020306 A 5313 STRINGER EMB 145 EMB145 3260210 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AE 145068 DURING INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19L CHAFED. BLENDED CHAFE. FABRICATED TWO DOUBLER ANGLE 14.5 IN CH BY 1.5 INCH, .050 INCH AND FOUR SHIMS 4.5 INCH BY .75 INCH, .080 INCH THICK IAW EMB 145 (SRM 145/1142 REV 17) 53-24-0 2, GST-0633/02, ETN EM53-020 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002040500076 20020405 00076 SO 2002 4 5 SIMA200207203 1 20020220 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AE 145068 ABI - RIGHT SILL BETWEEN FRAME 23 AND 29 HAS CORROSION. BLENDED OUT, PERFORMED NDT AND TREATED IAW EMB GST-0623/02. (M ) 2 L 7 2 4F RT T00011AT 2002040500077 20020405 00077 SO 2002 4 5 SIMA200207204 1 20020220 A 5311 FRAME EMB 145 EMB145 3260210 SO CORRODED CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AE 145068 ABI - RIGHT HAT BEAM AT FRAME 22 HAS CORROSION. BLENDED AND NDT'D AND TREATED HAT BEAM AT FRAME 22 IAW EMB GST 0623/02. (M) 2 L 7 2 4F RT T00011AT 2002040500078 20020405 00078 SO 2002 4 5 SIMA200207205 1 20020220 A 5310 STRUCTURE EMB 145 EMB145 3260210 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AE 145068 ABI - GALLEY AREA AFT DIGITAL HAS CORROSION. BLENDED OUT, PERFORMED NDT, AND TREATED FOR CORROSION IAW EMB 145 CPM 51-2 1-03, 51-21-04, 51-21-05, 51-21-06. (M) 2 L 7 2 4F RT T00011AT 2002040500079 20020405 00079 SO 2002 4 5 SIMA200207206 1 20020220 A 5310 BEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AE 145068 ABI - FOUND LEFT OMEGA BEAM BETWEEN FRAME 24 AND 25 HAS CORROSION. BLENDED AND PERFORMED NDT INSPECTION AND TREATED FOR CORROSION IAW EMB GST 0623/02. (M) 2 L 7 2 4F RT T00011AT 2002040500080 20020405 00080 SO 2002 4 5 SIMA200207207 1 20020220 A 5310 BEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AE 145068 ABI - CENTER OMEGA BEAM BETWEEN FRAME 23 AND 25 HAS CORROSION. BLENDED, PERFORMED NDT AND TREATED FOR CORROSION IAW EMB GST-0623/02. (M) 2 L 7 2 4F RT T00011AT 2002040500081 20020405 00081 SO 2002 4 5 SIMA200207208 1 20020309 A 5310 STRUCTURE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AE 145055 ABI - DURING INSPECTION OF AIRCRAFT, FOUND THE FORWARD DIGITAL CORRODED. REMOVED CORROSION BY CUT OUT. FABRICATED A RE PLACEMENT STRAP 16.5 INCH BY 21.5 INC, TWO DOUBLERS 7 INCH BY 6 INCH AND S SHIM 16.5 INCH BY .75 INCH, .040 INCH IAW EMB 145 SRM 145/1142, REV 17, 53-21-10, GST 0714/02, ITEM H, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002040500082 20020405 00082 SO 2002 4 5 SIMA200207209 1 20020309 A 5320 14522459 SUPPORT EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AE 145287 ABI - CENTER BEAM RAMP AND SUPPORT CORRODED. INSTALLED NEW RAMP SUPPORT IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002040500083 20020405 00083 SO 2002 4 5 SIMA200207210 1 20020308 A 5320 14522461003 GUSSET EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AE 145287 ABI - FOUND CORROSION ON RIGHT GALLEY FORWARD DIAMOND GUSSETT. REPLACED GUSSETT IAW EMB 135 SRM 51-40-02, 51-40-06. (M ) 2 L 7 2 4F RT T00011AT 2002040500084 20020405 00084 SO 2002 4 5 SIMA200207211 1 20020310 A 7500 14531128401 DUCT EMB 145 EMB145 3260210 SO NR 1 ENGINE DAMAGED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 613AE 145081 TVC - FLT 4253 - ENGINE FIRE WARNING JUST AFTER CLIMB-OUT, THEN EXTINGUISHED. THE CREW SHUT DOWN NR 1 ENGINE, DECLARED EMERGENCY AND RETURNED TO TVC FOR MAINTENANCE, LANDED SAFELY. REPLACED BROKEN DUCT BETWEEN HIGHT STAGE VALVE AND ENGINE ANTI-ICE VALVE. (M) 2 L 7 2 4F RT T00011AT 2002040500085 20020405 00085 NM 2002 4 5 2002UALA00551 1 20020323 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 FUSE SKIN CHAFED, FORWARD SKIN, STATION 1725.5 AT STRINGER 22 RT. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041000097 20020410 00097 NM 2002 4 10 2002UALA00555 1 20020322 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 AFT SIDE WALL AISLE EEL INOP ON UPPER DECK STAIRWELL ENCLOSURE. SPLICED IN NEW POWER STRIP CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000100 20020410 00100 NM 2002 4 10 2002UALA00558 1 20020322 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 SEAT 4F, AFT EEL LIGHT INOP; SEAT 4J AFT EEL LIGHT BROKEN. REPLACED LIGHT ASSEMBLIES. 2 L 7 4 4F 4 F RT A20WE E24NE 2002040500086 20020405 00086 NE 2002 4 5 SIMA200207212 2 20020311 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO GE CFM56 CFM567B24 NE NR 1 SHUTDOWN A SIMA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 21 619AE 145101 TYS - FLT 3718 - NR 1 ENGINE AUTO SHUTDOWN CLIMBING 11,000 FEET. ENGINE SURGED THEN SHUTDOWN WITH SMELL IN CABIN OF BUR NING OIL. RAI, NR 1 ENGINE. (M) 2 L 7 2 4T 4 F RT T00011AT E00055EN 2002040500087 20020405 00087 SO 2002 4 5 SIMA200207301 1 20020312 A 5310 ALCLAD2024T3 STRUCTURE EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AE 145287 MBV - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON FORWARD DIGITAL. REMOVED CORROSION BY BLENDING OUT. FABRICATED A REPAIR DOUBLER 2 INCH BY 2.75 INCH, .040 INCH THICK IAW EMB GST-0800/02, ITEM 1, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002040500088 20020405 00088 SO 2002 4 5 SIMA200207303 1 20020312 A 5310 BEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AE 145287 ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FAB RICATED A DOUBLER ANGLE 18.5 INCH BY 3 INCH, AND FILLER 14 INCH BY 2.75 INCH, 050 INCH THICK, A PLATE 6.5 INCH BY 1 INCH .125 INCH THICK, AND TWO SHIMS 6 INCH BY 1 INCH AND 5.25 INCH BY 1 INCH .090 INCH THICK IAW EMB 145 (SRM 145/1142 CHAPT ER 53, REV 17) 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002040500089 20020405 00089 SO 2002 4 5 SIMA200207304 1 20020311 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 603AE 145055 ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY FLOOR SUPPORT AT FRAME 20 AND 23, BEYOND LIMITS. REMOVED AND INSTALLED NEW FLOOR SUPPORT IAW EMB145, SRM 145/1142, REV 17 51-40-01, 51-40-02, 51-40-04, CPM 51-21-04 51-21-05, G ST-0714/02, ITEM 12, SEP-0114/02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002040500090 20020405 00090 NM 2002 4 5 UIEA02011 1 20020308 A 2597 813617409 WIRE HARNESS BOEING 747 747271C 1384869 NM COCKPIT SEAT WORN A UIEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 537MC 22403 IN CRUISE MXP/JFK, F/E SEAT ELECTRICAL CHORD SPARKED WHEN SEAT WAS MOVED BACK MANUALLY. OPENED C/B. ODOR OF SMOKE WAS IN THE COCKPIT FOR ABOUT ONE MINUTE. INSPECTED F/E'S SEAT AND FOUND ELECTRICAL CHORD BROKEN. PULLED C/B AND REMOVED CH ORD. NO OTHER DEFECTS FOUND. TRANSFERRED TO DI PAGE 03877, ITEM M02-013 PER DDPG 25-12-1 "D". (M) 2 L 7 4 4F A20WE 2002040500091 20020405 00091 EU 2002 4 5 USAABA02007 1 20020314 A 3350 321430 BATTERY PACK AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 671UW 0323 PHL - EPSU IN POSITION 16WL FAILED TO TEST. MAINTENANCE REPLACED THE EPSU BATTERY PACK. (M) 2 L 7 2 4F RT A46NM 2002040500092 20020405 00092 NM 2002 4 5 USAABB02022 1 20020311 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 29. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002040500093 20020405 00093 NM 2002 4 5 USAABB02023 1 20020309 A 3350 SWITCH BOEING 757 7572B7 1384964 NM CABIN MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 PIT - FLOOR LEVEL EMERGENCY ILGHT AT ROW 26 WOULD NOT EXTINGUISH. MAINTENANCE CYCLED THE EMERGENCY LIGHT SWITCH. (M) 2 L 7 2 4F RT A2NM 2002040500094 20020405 00094 NM 2002 4 5 USAABB02025 1 20020313 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 CLT - FOUND RIGHT AISLE EMERGENCY LIGHTS FROM ROWS 13 TO 24 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHAR GER. (M) 2 L 7 2 4F RT A1NM 2002040500095 20020405 00095 NM 2002 4 5 USAABB02026 1 20020315 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002040500096 20020405 00096 NM 2002 4 5 USAABB02027 1 20020315 A 3350 267005 POWER SUPPLY BOEING 757 757225 1384959 NM L4 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 BDL - FOUND L4 DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED A FUSE IN THE POWER SUPPLY. (M) 2 L 7 2 4F RT A2NM 2002040500097 20020405 00097 WP 2002 4 5 USAAD02012 1 20020313 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 827US 48049 IND - SOME OF THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BA TTERIES. (M) 2 L 7 2 4F A6WE 2002041000103 20020410 00103 NM 2002 4 10 2002UALA00561 1 20020322 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 UPPER DECK EMERGENCY CEILING LIGHTS INOP AT ROWS 12, 13 AND 17. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002040500098 20020405 00098 NM 2002 4 5 2002UALA00563 1 20020325 A 5320 STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 FORWARD GALLEY FLOOR LOWER CUTOUT STRINGER 17R TEAR STRAP HAS EXCESSIVE BLENDOUT OF DAMAGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED OUTER SKIN DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002040500099 20020405 00099 EU 2002 4 5 USAASA02025 1 20020309 A 3350 D31516113 LIGHT AIRBUS A321 A321211 3930370 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 163US 1417 LGA - THE EMERGENCY LIGHT SYSTEM FAILED THE EMERGENCY LIGHT SYSTEM TEST. MAINTENANCE REPLACED THE RIGHT SIDE, FIRST POS ITION, EMERGENCY ESCAPE SLIDE. SYSTEM TESTS OK. (M) 2 L 7 2 4F RT A28NM 2002040500100 20020405 00100 EU 2002 4 5 USAASA02026 1 20020312 A 3350 32145410 LIGHT AIRBUS A319 A319112 3930323 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 717UW 1069 CLT - THE EMERGENCY LIGHT SYSTEM WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY IN THE MID CABI N. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002071600094 20020716 00094 NM 2002 7 16 WRLA2002206 1 20020313 A 2424 976J86217 GCU DOUG DC10 DC10 N/A-SDR NM NR 3 FAILED A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 107WA 46836 DURING TAXI OUT, NR 3 GENERATOR OFF LIGHT ILLUMINATED NR 3 GENERATOR WAS RESET PER FCOM. DURING CLIMB APPROXIMATELY 15, 000 FEET NR 3 GENERATOR VOLTS AND FREQUENCIES WENT TO ZERO. ATTEMPTED RESET NR 3 GENERATOR MAINTAINED VOLTS AND FREQUEN CIES, LOAD FOR SECOND THEN WENT TO ZERO. APU WAS USED TO POWER NR 1 AND 3 BUSES FOR SINGLE GENERATOR OPERATION. AIRCRA FT RETURNED TO CCS FOR GENERATOR REPAIRS NR 1 GENERATOR SYSTEM WAS ON DMI. RETURNED AND REPLACED NR 3 GENERATOR CONTROL UNIT PERFORMED ENGINE RUN UP AND SYSTEM OPS CHECKED. 2 L 7 3 4F RT A22WE 2002050200070 20020502 00070 EU 2002 5 2 2002UALA00565 1 20020326 A 2150 QB0639 FILTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E/E BAY CLOGGED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 458UA 1163 ABORTED TAKEOFF AT 73 KNOTS DUE TO AN AVIONICS COOLING FAN MESSAGE. FOUND AVIONICS COOLING SYSTEM FILTER CLOGGED. REPL ACED SAME. 2 L 7 2 4F 4 F RT A28NM E40NE 2002040500105 20020405 00105 EU 2002 4 5 BAQ2002F00001 1 20020320 A 6320 109040003109 GEARBOX AGUSTA A109 A109E 0260119 EU MAIN ROTOR MAKING METAL E BAQA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 03 109DK 102 11504 MAIN TRANSMISSION CHIP LIGHT ILLUMINATED IN FLIGHT. COMPLIED WITH SERVICEABILITY CHECK FOR MAIN TRANSMISSION. CHIP LIG HT ILLUMINATED AGAIN AFTER SECOND OIL CHANGE, DURING GROUND RUN. 1 G 7 2 3U RT H7EU 2002040500106 20020405 00106 NM 2002 4 5 2002UALA00567 1 20020326 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 FLOORBEAM T-CAP CORRODED UNDER NUT PLATE BODY STATION 153, LBL 10. MAJOR REPAIR ACCOMPLISHED. REPAIRED T-CAP WITH FABR ICATED NEW SECTION AND SPLICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040500107 20020405 00107 CE 2002 4 5 FPI2002F00005 1 20020109 A 5412 96980015 CHANNEL BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO FIREWALL CRACKED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 4626A 10163 TH39 UPPER U-CHANNEL ON ENGINE FIREWALL, CRACKS DEVELOPED WHERE ENGINE MOUNT BOLT RUNS THROUGH FIREWALL. PROBABLE CAUSE IS N ORMAL ENGINE VIBRATION. 1 L 7 2 3O 3 O 3A16 E5CE 2002040500108 20020405 00108 CE 2002 4 5 FPI2002F00006 1 20020109 A 5412 969800015 CHANNEL BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO NACELLE CRACKED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 80AC 9242 TH56 UPPER U-CHANNEL ON ENGINE FIREWALL. CRACKS DEVELOPED WHERE ENGINE MOUNT BOLT RUNS THROUGH FIREWALL. PROBABLE CAUSE IS NORMAL ENGINE VIBRATION. 1 L 7 2 3O 3 O 3A16 E5CE 2002040500109 20020405 00109 CE 2002 4 5 FPI2002F00007 1 20020315 A 2730 58524015 CONTROL CABLE BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO ELEVATOR FRAYED D FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 46US 12093 TH294 DURING A ROUTINE INSPECTION, THE ELEVATOR CONTROL CABLE WAS FRAYING IN THE AREA OF THE FORWARD LOWER CABLE PULLEY. 1 L 7 2 3O 3 O 3A16 E5CE 2002040500110 20020405 00110 CE 2002 4 5 FPI2002F00008 1 20020315 A 2730 58524015 CONTROL CABLE BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO ELEVATOR FRAYED D FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 950JP 15450 TH432 DURING A ROUTINE INSPECTION, THE ELEVATOR CONTROL CABLE WAS FRAYING IN THE AREA OF THE FORWARD LOWER CABLE PULLEY. 1 L 7 2 3O 3 O 3A16 E5CE 2002040500111 20020405 00111 SW 2002 4 5 MV52002F00001 1 20020318 A 2841 CMF12191 MONITOR GULSTM 690TP 690B 7630516 SW GARRTT TPE331 TPE331* 01514 WP FUEL QUANTITY FAILED B MV5R K NONE O OTHER IN INSP/MAINT 1 GL 11 690HT 204 11467 FUEL QUANTITY INDICATION -0- AT ALL TIMES. REPLACEMENT OF FUEL QUANTITY CONTROL MONITOR CORRECTED INDICATION PROBLEM. 1 H 7 2 3T 3 T 2A4 E2WE 2002040500112 20020405 00112 CE 2002 4 5 VJ32002F00018 1 20020326 A 3230 SM50D7 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MLG STUCK B VJ3R A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 07 8101C 244 CE1538 LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. AIRCRAFT WAS PLACED ON JACKS AND THE LANDING GEAR CYCLED IAW MM. INSPEC TION OF SYSTEM FOUND THAT THE DYNAMIC RELAY WOULD STICK IN THE DOWN POSITION. A NEW DYNAMIC RELAY WAS INSTALLED AND THE SYSTEM OPERATIONAL CHECKED NORMAL. 1 L 7 1 3O 3 O 3A15 E5CE 2002040500113 20020405 00113 CE 2002 4 5 VJ32002F00019 1 20020325 A 2822 64621216A2R PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO FUEL SYSTEM LEAKING B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 1570A 442 CE1333 INSPECTION OF THE FUEL PUMP FOUND OIL LEAKING FROM THE DRAIN PORT OF FUEL PUMP. IN FLIGHT THE ENGINE WAS ROUGH AT TIME. PUMP WAS REMOVED AND A NEW PUMP INSTALLED IAW MM. DEFECTIVE PUMP SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002040500114 20020405 00114 EA 2002 4 5 VNW2002F00000 2 20020401 A 8520 BOSS PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA IDL GEAR SHAFT FAILED A VNWA K NONE O OTHER IN INSP/MAINT 1 SO 15 59905 112 317652135 THE CRANKSHAFT IDLER GEAR SHAFT BOSS AT THE CRANKCASE AND THE CRANKSHAFT IDLER GEAR SHAFT BOSS AT THE ACCESSORY CASE FAI LED. RESULTING IN MEDAL IN OIL SCREEN AND OIL FILTER AND A LOSE IN OIL PRESSURE. IT IS BELIEVED THAT THE CRANKCASE BOS S FAILED FIRST. THIS IS THE SECOND TIME THIS FAILURE HAD OCCURED, THE FAILURES ON CRANKCASE WERE BOTH CERTIFIED BY A WE LL KNOWN REPAIR STATION. 1 L 7 2 3O 3 O A20SO E14EA 2002040500115 20020405 00115 CE 2002 4 5 WO56083 1 20020329 A 2731 SL60131 SHAFT CESSNA 208 208B 2073701 CE TRIM WHEEL BROKEN B O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 07 717BT 998 208B0863 THE ELEVATOR TRIM WHEEL SHAFT IN THE COCKPIT CONTROL QUADRANT WAS FOUND TO BE BROKEN. THE BREAK IN THE SHAFT WAS WHERE A MOUNTING/ALIGNING PLATE WAS WELDED TO THE SHAFT. THE TRIM WHEEL, WITH THE SPROCKETS AND END OF THE BROKEN SHAFT ASSY, FELL OFF RELEIVING TENSIONS FROM BOTH THE MANUAL ELEVTOR TRIM CABLES AND THE ELECTRIC TRIM CHAIN.THE SHAFT ASSY WAS REPL ACED WITH NEW AND THE TRIM SYSTEM WAS INSPECTED AND OPERATION WAS FOUND TO BE SATISFACTORY. 1 H 7 1 3T A37CE 2002040500116 20020405 00116 SO 2002 4 5 WVBA2002006 1 20020401 A 8120 LW12437 ADAPTER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA TURBOCHARGER CRACKED A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 27755 317852148 DURING INSPECTION EXHAUST STAIN WAS OBSERVED ON THE TURBOCHARGER MOUNT IN THE AREA WHERE THE TURBOCHARGER AND THE TRANSI TION MEET AND FACE THE TURBO MOUNT. THE TURBO WAS REMOVED AND A CRACK WAS FOUND IN THE DIVIDE WHICH CAUSED THE TRANSITI ON TO WARP AND LEAK EXHAUST GASES. THE PART WAS REMOVED AND REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 2002040500117 20020405 00117 NM 2002 4 5 2002UALA00568 1 20020326 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 LEFT NOSE TUNNEL AT BODY STATION 246, LBL 35, UPPER CHORD CRACKED AFT SIDE. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPA IR PARTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002050200071 20020502 00071 NE 2002 5 2 2002UALA00570 2 20020327 A 7297 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT ENGINE SHORTED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 420UA 489 NUMEROUS ECAM FAULT MESSAGES FROM THE NUMBER TWO ENGINE. FOUND NUMEROUS WIRES SHORTED IN THE RIGHT ENGINE OUTBOARD PYLO N AREA. AREA WAS CHECKED FOR DAMAGE AND NEW WIRES INSTALLED AS REQUIRED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002040500118 20020405 00118 NM 2002 4 5 2002UALA00577 1 20020327 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 BODY STATION 850-855 RBL 33 FLOORBEAM T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM T- CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002040500119 20020405 00119 WP 2002 4 5 DHL2002807514 1 20020324 A 5330 7075T6071 SKIN DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF. N/R 0669 FUS. EXT. CRACKED .75 @ STA 1730 - 1740 L17RCORR: REMOVED FASTNERS I/A/W SRM 51-1-21 PG.1 CLEANED ,T REATED & PRIMED AREA I/A/W SRM51-1-8B FABRICATED DOUBLER (7075T6,.O63) + FINGER DOUBLERS (7075T6 , .071) I/A/W SRM 53-2- 1 FIG. 7 CLEANED TREATED AND PRIMED THEM I/A/W/SRM 51-1-8B INSTALLED I/A/W SRM53-2-1-F7 + 51-1-21 P1 2 L 7 4 4F RT 4A25 2002040500120 20020405 00120 NM 2002 4 5 2002UALA00578 1 20020327 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 BODY STATION 1562 LBL 58 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS AND BEAM . 2 L 7 2 4F 4 F RT A1NM E24NE 2002041000112 20020410 00112 NM 2002 4 10 2002UALA00579 1 20020328 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 931UA 26656 CABIN FLOORBEAM STATION 986 RIGHT HAND OUTBOARD WAS CORRODED WITH EXCESSIVE MATERIAL REMOVED. MAJOR REPAIR ACCOMPLISHED . CUT OUT DAMAGE, INSTALLED REPAIR ANGLE AND FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041000114 20020410 00114 NM 2002 4 10 2002UALA00581 1 20020328 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE BUCKLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 LEFT HAND FUSELAGE FRAME AND SKIN BUCKLED AT STATION 927 BETWEEN STRINGER 19L & STRINGER 20L. MAJOR REPAIR ACCOMPLISHED . REMOVED DAMAGE AND INSTALLED EXTERNAL SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040500121 20020405 00121 2002 4 5 482DM32002 4 20020329 A 2312 1621B ANTENNA MTSBSI MU300 MU300 5780602 CE NR 1 COMM DEBONDED E UVCA K NONE O OTHER NR NOT REPORTED 1 CE 03 482DM 5886 A088SA NR 1 COMMUNICATION RADIO DIFFICULT TO UNDERSTAND WHEN IN VISUAL MOISTURE. FOUND LEFT SIDE OF LEADING EDGE OF ANTENNA DE BONDED. 2 H 7 2 4F RT A14SW 2002040500122 20020405 00122 2002 4 5 482DM32702 4 20020329 A 3455 6222362001 RECEIVER MTSBSI MU300 MU300 5780602 CE ADF SYSTEM UNRELIABLE E UVCA K NONE O OTHER CR CRUISE 1 CE 03 482DM 16 A088SA ADF INDICATOR INTERMITTENTLY WILL NOT LOCK ON SIGNAL, NEEDLE WOULD WANDER OFF STATION, THEN LOCK ON TO STATION. PILOT R EPORTED THAT IT WAS UNRELIABLE. 2 H 7 2 4F RT A14SW 2002040500123 20020405 00123 2002 4 5 482DM40102 4 20020401 A 3442 MI5852771 INDICATOR MTSBSI MU300 MU300 5780602 CE COCKPIT MALFUNCTIONED E UVCA K NONE O OTHER CR CRUISE 1 CE 03 482DM 20 A088SA RADAR INDICATOR HAS A GOOD TEST PATTERN BUT WILL NOT PAINT WEATHER AND/OR GROUND. 2 H 7 2 4F RT A14SW 2002040500124 20020405 00124 2002 4 5 700HH032902 4 20020401 A 2370 GA1000000 CVR BRAERO DH125 HS125700A 4230170 EU COCKPIT SHORTED E UVCA K NONE L NO TEST IN INSP/MAINT 1 CE 03 700HH 4647 NA0240 COCKPIT VOICE RECORDER CIRCUIT BREAKER TRIPPED DURING FUNCTIONAL TEST. UNABLE TO RESET. 2 L 7 2 4F A3EU 2002040500125 20020405 00125 2002 4 5 700HH40302 4 20020403 A 3418 SLZ9826 INDICATOR BRAERO DH125 HS125700A 4230170 EU COCKPIT FAULTY E UVCA K NONE O OTHER IN INSP/MAINT 1 CE 03 700HH 8746 NA0240 AOA INDICATOR NEEDLE WILL NOT FOLLOW AOA PROBE MOVEMENT THROUGH FULL RANGE OF TRAVEL. NEEDLE STAYS IN UPPER (RED ARC) O F INDICATOR. 2 L 7 2 4F A3EU 2002040500126 20020405 00126 WP 2002 4 5 AT0200043 1 20020404 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP LAV #2 BURNED A ZZDA K NONE O OTHER CR CRUISE 1 SO 15 823AT 47529 DURING CRUISE AN ELECTICAL SMELL WAS REPORTED IN AFT CABIN, SMELL DISIPATED BUT STILL PRESENT. CORRECTIV E ACTION: AFT RIGHT LAVATORY EMERGENCY BATTERY PACK OVERHEATED. REMOVED AND REPLACED BATTERY PACK. OPS CHECK O.K. IAW MM 33-00. 2 L 7 2 4F A6WE 2002040500127 20020405 00127 2002 4 5 GLBA2002043 4 20020329 A 2300 BW9001 SWITCH BEECH 1900 1900D 1154162 CE INOPERATIVE A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 170GL UE170 LEFT PUSH TO-TALK SWITCH FAILED REPLACED OPS CHECKED SATISFACTORY 2 L 7 2 4T RT A24CE 2002040500128 20020405 00128 NM 2002 4 5 AWXA200200298 1 20020315 A 5311 65465311 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 0 0 22655 YVR - MAJOR REPAIR - DURING C-14 CHECK A CRACK WAS FOUND ON THE FRAME INBOARD CHORD BETWEEN STR 21-22, FS 500 IN THE FOR WARD CARGO COMPARTMENT. MAINTENANCE REMOVED DAMAGED LOWER SECTION OF FRAME, FABRICATED A NEW LOWER SECTION OF FRAME AND SPLICE DOUBLER, AND INSTALLED REPAIR PARTS IAW B737-200 SRM 51-10-1, PG 8, DEG 65-46531-1, AND SRM 51-40-3, FIG.1, PG. 1 -6. 2 L 7 2 4F RT A16WE 2002040500129 20020405 00129 NM 2002 4 5 AWXA200200299 1 20020315 A 5311 654653031 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 0 0 22655 YVR - MAJOR REPAIR - DURING C-14 CHECK A 3" CRACK WAS FOUND COMING FROM THE ANCHOR NUT HOLE AT FS 460 L/H, STR 21 INBOAR D CHORD IN THE FORWARD CARGO COMPARTMENT. MAINTENANCE REMOVED DAMAGED LOWER SECTION OF FRAME, FABRICATED A NEW LOWER SE CTION OF FRAME AND SPLICE DOUBLER, AND INSTALLED REPAIR PARTS IAW B737-200 SRM 51-10-1, PG 8, AND SRM 51-40-3, FIG. 1, P G. 1-6. 2 L 7 2 4F RT A16WE 2002040500130 20020405 00130 NM 2002 4 5 AWXA200200301 1 20020315 A 5311 65479592 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 0 0 22655 YVR - MAJOR REPAIR - DURING C-14 CHECK A CRACK WAS FOUND ON THE AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME LOWER ST OP FITTING AT OUTBOARD LOWER CORNER. MAINTENANCE REMOVED T-EXTRUSION AND FRAME AT AFT CARGO COMPARTMENT DOOR CUTOUT FORW ARD FRAME LOWER STOP FITTING, FABRICATED A NEW T-EXTRUSION, FRAME, AND STRAP, AND INSTALLED REPAIR PARTS IAW B737-200 SR M 51-10-1, PG. 8, AND DWG 65-47959. 2 L 7 2 4F RT A16WE 2002040500131 20020405 00131 NM 2002 4 5 AWXA200200303 1 20020324 A 5330 6552988 SKIN BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 0 0 23627 MCN - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND EMANATING FROM EXTERNAL SKIN COUNTERSUNK FASTENER HOLE AT THE U PPER AFT CUTOUT OF THE L2 DOOR. MAINTENANCE STOP DRILLED CRACKS ON FIRST AND SECOND LAYER OF SKIN AND PERFORMED HFEC INS PECTION VERIFYING THE CRACKS WERE CONTAINED. FABRICATED INNER, MIDDLE, AND OUTER PATCH AND INSTALLED REPAIR PARTS IAW B 737-300 SRM 53-60-01, PG. 205-207 2 L 7 2 4F RT A16WE 2002040500132 20020405 00132 NM 2002 4 5 AWXA200200304 1 20020325 A 5230 654795220 TEE CHORD BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 0 0 23627 MCN - MAJOR REPAIR - DURING C-16 CHECK 2 CRACKS WERE FOUND ON THE AFT CARGO DOOR LOWER BEAM (TEE CHORD) FORWARD END AT 2 ND AND 3RD FASTENER HOLES ON VERTICAL LEG, CRACKS 1/8" AND 1/4" RESPECTIVELY. MAINTENANCE TRIMMED OUT FORWARD END OF TE E CHORD, FABRICATED A REPAIR DOUBLER AND FILLERS A, B, C, & D, AND INSTALLED REPAIR PARTS IAW EO 52-33-02. 2 L 7 2 4F RT A16WE 2002040500133 20020405 00133 EU 2002 4 5 AWXA200200305 1 20020320 A 5320 D5311281202 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 YWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON NUTPLATES AND FLOOR SUPPORT AT Y254L, BETWEEN FR 20 AND FR 21. MAINTENANCE REMOVED FLOOR SUPPORT BETWEEN FR 12 TO FR 24. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-72- 11, PG. 1 & 2. 2 L 7 2 4F RT A28NM 2002040500134 20020405 00134 NM 2002 4 5 200200212 1 20020404 A 5310 STIFFENER BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 LOWER FRAME STIFFENER AT BS 2160 BETWEEN S-49 AND S-50 LEFT IS CRACKED. FABRICATED AND INSTALLED SHEAR TIE, STRINGER CL IPS AND T CLIP SHEAR TIES PER B747 SRM. 2 L 7 4 4F A20WE 2002040500135 20020405 00135 NM 2002 4 5 200200213 1 20020404 A 5320 FLOOR SUPPORT BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 BULK PIT FLOOR SUPPORT AT BS 2160, ABOVE S-42 LEFT HAS A CRACK. REMOVED DAMAGED SECTION OF INTERCOSTAL AND PERFORMED SP LICE REPAIR PER B747 SRM 51-10-07 FIG 20 AND 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2002040500136 20020405 00136 NM 2002 4 5 200200214 1 20020404 A 5310 65B881915 FITTING BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 MED 3 LEFT DOOR STOP FITTING CRACKED (FLANGE ONE SIDE BROKEN OFF) INSTALLED NR 3 LT DOOR STOP FITTING AT STR 20 PER B747 SRM 51-30-02 & 51-10-01. REMOVED AND REPLACED LOCATED AND DRILLED FITTING PER B747 SRM 51-30-02, 51-10-01 & 51-30-05. 2 L 7 4 4F A20WE 2002040500137 20020405 00137 2002 4 5 99V40202 4 20020402 A 2310 6222631003 RADIO BRAERO DH125 HS125700A 4230170 EU COCKPIT FAILED E UVCA K NONE L NO TEST IN INSP/MAINT 1 CE 03 9999V NA0308 HF RADIO FAILED TO FUNCTION. 2 L 7 2 4F A3EU 2002040500138 20020405 00138 WP 2002 4 5 ZW0A0201104 1 20020121 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 IN THE ELECTRONIC COMPARTMENT FOUND CORROSION ON LONGERON 30 FROM STA 110 TO 130. REMOVED LONGERON 30 FROM STA 110 TO 1 30. INSTALLED REPAIR PER SRM 53-02, FIG 18, SHEET 1 PAGE 48. 2 L 7 2 4F RT A6WE 2002040500139 20020405 00139 WP 2002 4 5 ZW0A0201105 1 20020121 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT IN THE FWD CARGO COMPARTMENT FOUND CORROSION ON THE RT CARGO TIE DOWN TRACK, SEVERAL PLACES FROM ST A 427 TO 522. REPLACED DAMAGED AREA OF TIE DOWN TRACK PER SRM 53-05, FIG 4G, PAGE 10R. 2 L 7 2 4F RT A6WE 2002040500140 20020405 00140 NM 2002 4 5 ZW0A0201106 1 20020121 A 5330 SKIN BOEING 767 767300 1385204 NM FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 691LF 25137 DURING CHECK-C MAINT ON THE AFT FUSELAGE SKIN BELOW THE RT SIDE OF THE HORIZONTAL STABILIZER HAD A 8 IN BY 1 IN BY 0.050 GROOVE AND WEAR AREA ADJACENT TO THE AFT END OF THE AIRGATE FAIRING. CUT OUT DAMAGED AREA AND INSTALLED AN EXTERNAL DO UBLER PER SRM 53-80-01, FIG 203. 2 L 7 2 4F RT A1NM 2002040500141 20020405 00141 NM 2002 4 5 ZW0A0201107 1 20020122 A 5512 PANEL BOEING 767 767300 1385204 NM HORIZ STAB DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 691LF 25137 DURING CHECK-C MAINT FOUND DEEP GROOVE WORN AFT END OF THE HORIZONTAL STABILIZER LOWER FAIRING PANEL, LT SIDE, 8 IN BY 1 INCHES BY 0.050 DEEP. INSTALLED DOUBLER PER SRM 53-80-01. 2 L 7 2 4F RT A1NM 2002040500142 20020405 00142 WP 2002 4 5 ZW0A0201108 1 20020116 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT A CABIN FLOOR MEMBRANE PANEL HAD LIGHT CORROSION ON THREE AREAS, STA 160 TO 200, LBL 5 INCHES. REP LACED FLOOR MEMBRANE FROM STA 200 TO 160, LBL 9 INCHES TO RBL 32. INSTALLED PER SRM 51-30-02. 2 L 7 2 4F RT A6WE 2002040500143 20020405 00143 WP 2002 4 5 ZW0A0201109 1 20020116 A 5320 FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT STA 160 THE GALLEY FLOOR MOUNTS WERE CORRODED AT RBL 45 AND RBL 51. REMOVED CORRODED FITTINGS AND REPLACED WITH NEW PER SRM 51-01, PAGE 1 ITEM C. 2 L 7 2 4F RT A6WE 2002040500144 20020405 00144 WP 2002 4 5 ZW0A0201110 1 20020116 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT THE CUSP ANGLE AT STA 200, RBL 59, HAD CORROSION. INSTALLED NEW SECTION PER SRM 53-05, FIG 5. 2 L 7 2 4F RT A6WE 2002040500145 20020405 00145 WP 2002 4 5 ZW0A0201111 1 20020116 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND CRACK APPROXIMATELY 1.5 INCHES LONG AT FWD END OF CABIN FLOORBEAM APPROXIMATELY STA 1350, LBL 7. REMOVED AND REPLACED FLOORBEAM PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2002040500146 20020405 00146 WP 2002 4 5 ZW0A0201112 1 20020117 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND CORROSION ON LT CARGO TIE DOWN TRACK, STA 1136 TO 1212. REPLACED CORRODED TRACK FROM STA 112 6 TO 1221 PER SRM 53-05, FIG 46. 2 L 7 2 4F RT A6WE 2002040500147 20020405 00147 WP 2002 4 5 ZW0A0201113 1 20020118 A 5320 TIE CLIP DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT FOUR UPPER TIE CLIPS WERE CRACKED ON LOWER VENT AFT OF CANTED FORMER RING, STA 1463, LBL 19 INCHES TO LBL 32. FABRICATED 4 EACH TIE CLIPS PER SPM 6-70-01, PAGE 2 AND 3, AND DOUGLAS DRAWING 5920838. INSTALLED 4 EACH TI E CLIPS PER SPM 6-70-01, PAGE 3 AND DOUGLAS DRAWING 5920838, AND SRM 51-30-5. 2 L 7 2 4F RT A6WE 2002040500148 20020405 00148 NM 2002 4 5 ZW0A0201201 1 20020126 A 2120 ODOR BOEING 757 757231 1384950 NM CABIN DETECTED A ZW0A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 13 720TW 30319 IN CRUISE MID AND AFT LAVATORYS SMOKE DETECTOR SOUNDED FOLLOWED BY A HOT APPLIANCE SMELL, SOME SMOKE. CREW TURNED OFF V IDEO AND OPENED MID GALLEY CB'S AND ODOR DISAPPEARED. EXTENSIVE SEARCH FOUND NO MALFUNCTION. REOPENED MID GALLEY CB AN D PLACARD VIDEO SYSTEM INOPERATIVE PER MEL PRECAUTIONARY. 2 L 7 2 4F RT A2NM 2002040500149 20020405 00149 WP 2002 4 5 ZW0A0201301 1 20020128 A 5534 ATTACH ANGLE DOUG DC9 DC982 3022082 WP VERTICAL STAB CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 902TW 49153 DURING CHECK-C FWD LT DORSAL FIN ATTACH ANGLE, .5 INCH CRACK WAS FOUND ON UPPER LEG VERIFIED WITH EDDY CURRENT. INSTALL ED NEW ATTACH ANGLE PER SRM 51-30-02, 51-30-05, & MO 72R22 & ARA 17951. 2 L 7 2 4F A6WE 2002040500150 20020405 00150 WP 2002 4 5 ZW0A0201302 1 20020128 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT FRAME AT STA 1322, FOUND HEAVY CORROSION AT LONGERON 30 ON AFT SIDE. SPLICED IN NEW SECTION OF FRA ME PER SRM 53-03 FIGURE 2A. INSTALLED RIVETS IN BULKHEAD SUPPORT FRAME PER SRM 51-30-02. 2 L 7 2 4F RT A6WE 2002040500151 20020405 00151 WP 2002 4 5 ZW0A0201303 1 20020128 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT, RT SIDE AT STATION 1212 TO 1308, FOUND RT TIE DOWN TRACK CORRODED BEY OND LIMITS. INSTALLED NEW SECTION OF TRACK FROM STATION 1202 TO 1322, PER SPM 6-70-01 PAGES 1-3. 2 L 7 2 4F RT A6WE 2002040500152 20020405 00152 WP 2002 4 5 ZW0A0201304 1 20020128 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT LT SIDE, TIE DOWN TRACK FROM STATION 1220 TO 1308 IS CORRODED BEYOND L IMITS. NEW SECTION OF TRACK WAS INSTALLED PER SRM 51-30-01. 2 L 7 2 4F RT A6WE 2002040500153 20020405 00153 WP 2002 4 5 ZW0A0201305 1 20020126 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT AT STATION 1079 TO 1155 RT SIDE, TIE DOWN TRACK WAS FOUND CORRODED BEY OND LIMITS. NEW SECTION OF TRACK WAS INSTALLED FROM STATION 1079 TO 1155 PER SRM 53-05 PG 10. 2 L 7 2 4F RT A6WE 2002040500154 20020405 00154 WP 2002 4 5 ZW0A0201306 1 20020126 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT RT SIDE, TIE DOWN TRACK FROM STATION 1212 TO 1322 WAS FOUND CORRODED B EYOND LIMITS. NEW SECTION OF TRACK WAS INSTALLED FROM STATION 1212 TO 1322 PER SRM 51-30-02/05. 2 L 7 2 4F RT A6WE 2002040500155 20020405 00155 WP 2002 4 5 ZW0A0201401 1 20020121 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 966TW 53616 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 26 THROUGH 29. SECURED A LOOSE CONNECTION AT ROW 29. 2 L 7 2 4F RT A6WE 2002040500156 20020405 00156 WP 2002 4 5 ZW0A0201403 1 20020103 A 3350 58222 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 966TW 53616 THE CABIN EMERGENCY LIGHTS WERE INOPERATIVE FROM ROW 1 TO 20. REPLACED THE POWER SUPPLY, AND THE EMERGENCY SWITCH. 2 L 7 2 4F RT A6WE 2002040500157 20020405 00157 WP 2002 4 5 ZW0A0201601 1 20020207 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C FOUND CABIN STA 1338 LONGERON 18R, FRAME HAS CORROSION FROM FLOOR LEVEL TO 6 INCHES UP THE FWD SIDE. COR ROSION WAS REMOVED PER SPM 6-80-01. 2 L 7 2 4F A6WE 2002040700001 20020407 00001 EU 2002 4 7 RAIA00203108 1 20020327 A 2120 8323715 CONDENSER JETAIR JETSTM JETSTM4101 1500501 EU DIRTY A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 571HK 41090 5597-MSN-SMOKE IN COCKPIT ON CLIMB OUT, TOILET SMOKE CAP ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RIGHT ENVIRONMENT AL CONTROL SYSTEM CONDENSER, OPS CK OK. 2 L 7 2 4T RT A41NM 2002040700002 20020407 00002 SO 2002 4 7 RAIA00203109 1 20020327 A 8011 35059104 STARTER EMB 145 EMB145ER 3260211 SO FAILED A RAIA A UNSCHED LANDING O OTHER TX TAXI/GRND HDL 1 CE 03 808HK 5837 5837 145157 5316-PIT-RIGHT ENGINE WOULD NOT START. MAINTENANCE REMOVED AND REPLACED RIGHT STARTER, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002040700003 20020407 00003 WP 2002 4 7 DHL2002807516 1 20020323 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 2041 RT. WING OUTBD. L/EINNER SURFACE - RIB CRACKED .250 @ SAT. XFS 622.500CORR.; STOPPED DRILLED CRACK I/A/W SRM 57-2-0 FIG.2 FABRICATED RE-INFORCING ANGLE ( 2024-T3 AL , .063 ) I/A/W/ SRM57-2-0 FIG.2 CLEANED , TREATED AND PRIMED REINFORCING ANGLE I/A/W SRM 51-1-8B , INSTALLED REINFORCING ANGLE I/A/W SRM 57-2-0 FIG 2 2 L 7 4 4F RT 4A25 2002040700004 20020407 00004 WP 2002 4 7 DHL2002807518 1 20020322 A 5534 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 2540 VERTICAL STAB. L/E - INNER RIB CRACKED .500 @ ZFS108.000CORR.: STOP DRILLED CRACK IN VERTICAL STAB . L/E INNER - FABRICATED DOUBLER ( 2024 T3 AL .050)I/A/W SRM55-2-0 FIG. 2 , CLEANED , TREATED AND PRIMED I/A/W SRM 51-1- 8B , INSTALLED DOUBLER I/A/W SRM 55-2-0 FIG. 2 & SRM 51-1-21 PG. 1 2 L 7 4 4F RT 4A25 2002040700005 20020407 00005 NE 2002 4 7 RAIA00203110 2 20020328 A 7210 310430212 GEARBOX JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE DETERIORATED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 573HK 11301 2820 41092 76109 5508- STL- SHORTLY AFTER TAKE OFF RIGHT ENGINE INTEGRATED ELECTRONIC CONTROL WARNING WITH 10% TORQUE FLUCTUATION. MAINTE NANCE REMOVED AND REPLACED THE RIGHT ENGINE INTERMEDIATE GEAR BOX, OPS AND LK CK OK. 2 L 7 2 4T 4 T RT A41NM E18NE 2002040700006 20020407 00006 EU 2002 4 7 RAIA00203111 1 20020329 A 2613 51228801 OVERHEAT LOOP JETAIR JETSTM JETSTM4101 1500501 EU SHORTED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 573HK 41092 5529-STL- LEFT OVERHEAT LOOP LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE FIRE WIRE UNDER THE TAIL PIPE, OPS CK OK. 2 L 7 2 4T RT A41NM 2002040700007 20020407 00007 SO 2002 4 7 RAIA00204113 1 20020401 A 3242 0132AEV1 SENSOR EMB 145 EMB145 3260210 SO CORRODED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 803HK 5301 145077 5286-RIC- THE #4 BRAKE OVERHEAT LIGHT CAME ON DURING TAXI. MAINTENANCE REMOVED AND REPLACED CORRODED #4 BRAKE SENSOR, OP S CK OK. 2 L 7 2 4F RT T00011AT 2002040700008 20020407 00008 2002 4 7 RAIA00204114 4 20020402 A 3421 HG2010AC02 COMPUTER EMB 145 EMB145 3260210 SO INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 806HK 5749 203 145112 5277-DTW- DURING TAXI #2 AHRS FAILED. REMOVED AND REPLACED #2 AHRS UNIT, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002040700009 20020407 00009 EU 2002 4 7 RAIA00204115 1 20020402 A 7714 31055863 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 552HK 41057 5510-STL- RIGHT ENGINE INTEGRATED ELECTRONIC CONTROL LIGHT CAME ON DURING TAKE-OFF. MAINTENANCE REMOVED AND REPLACED THE RPM SPEED SENSOR, OPS CK OK. 2 L 7 2 4T RT A41NM 2002040800002 20020408 00002 NM 2002 4 8 0201055644 1 20020330 A 2120 ODOR BOEING 757 757251 1384970 NM CABIN DETECTED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 544US 26491 UPON ROTATION, A STRONG ACID ODOR BECAME EVIDENT IN COCKPIT. CABIN CREW ALSO NOTED THE SAME ODOR IN THE PASSENGER CABIN AREA. COCKPIT CREW DECLARED AN EMERGENCY AND MADE AN UNEVENTFUL OVERWEIGHT LANDING. MAINTENANCE PERFORMED MULTIPLE MAIN TENANCE CHECKS INCLUDING ENGINE RUN, PACK CHECKS, OIL CONTAMINANTS, AND OVEN CHECKS/REPLACEMENT WITH NO CONCLUSIVE DISCR EPANCIES. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2002040800003 20020408 00003 WP 2002 4 8 0201069997 1 20020321 A 2780 DUCT DOUG DC9 DC931 3022065 WP SLATS LACK OF LUBE A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 8933E 47142 UPON SLAT EXTENSION, THE AIRCRAFT ROLLED TO THE RIGHT AND THE BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE. CREW CYCLED SLA TS ONCE MORE WITH SAME RESULTS. FOLLOWED COM PROCEDURES AND LANDED UNEVENTFULLY WITHOUT SLATS AT FSD. MAINTENANCE INSPEC TED AND CHECKED THE SLATS, OPERATED USING EACH HYDRAULIC SYSTEM INDIVIDUALLY AND BOTH SLATS WORKED NORMALLY. LUBRICATED THE 'T' DUCTS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002040800004 20020408 00004 WP 2002 4 8 0201079763 1 20020330 A 2611 473597407 SMOKE DETECTOR DOUG DC9 DC951 3022051 WP CARGO BAY MALFUNCTIONED A NWAA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 GL 01 763NW 47708 DURING LANDING ROLL, THE MASTER WARNING LIGHT ILLUMINATED ALONG WITH THE FORWARD CARGO FIRE BELL AND CARGO SMOKE WARNING ANNUNCIATOR. COMPLIED WITH COM PROCEDURES BUT THE WARNING INDICATIONS REMAINED. CREW DISCHARGED THE CARGO FIRE SUPPRESS ION AGENT PER COM. LANDING WAS WITHOUT FURTHER INCIDENT AND THE FIRE INDICATIONS STAYED UNTIL ARRIVAL AT THE GATE. CFR R ESPONDED AND CLEARED THE CARGO HOLD. NO SIGNS OF FIRE OR SMOKE FOUND. MAINTENANCE REPLACED THE CARGO SMOKE DETECTORS AND THE NR 1 CARGO FIRE BOTTLE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002040800005 20020408 00005 WP 2002 4 8 0201089919 1 20020330 A 2150 LINE DOUG DC9 DC932 3022066 WP AUG VALVE LOOSE A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 941N 47450 WHILE CRUISING AT FL260 WITH ENGINE AND AIRFOIL ANTI-ICE ON, THE CABIN BEGAN A 500 FPM CLIMB. PACK SUPPLY PRESSURE INDIC ATED 25 PSI ON BOTH PACKS. TURNING OFF THE ANTI-ICE SYSTEM, RESETTING PACK TO MANUAL, AND CLOSING THE OUTFLOW VALVE DID NOT STOP THE PRESSURE LOSS. CREW DECLARED AN EMERGENCY DESCENT DOWN TO 10,000 FEET WHERE THEY WERE ABLE TO RECOVER THE C ABIN PRESSURIZATION. THE FLIGHT RETURNED TO ALTITUDE FL200 AND CONTINUED TO MSP WITHOUT INCURRING ANY INBOUND DELAYS. MA INTENANCE TIGHTENED LOOSE LINES AT THE LEFT AUGMENTATION VALVE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002040800006 20020408 00006 NM 2002 4 8 0201106626 1 20020402 A 2120 ODOR BOEING 747 747251B 1384892 NM COCKPIT DEFECTIVE A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 626US 21708 DURING FLIGHT, AN ELECTRICAL FUME EMITTED ON THE RIGHT SIDE OF ZONE 'D'. PULLED CIRCUIT BREAKER AND AIRCRAFT CONTINUED T O DESTINATION AND LANDED WITHOUT INCIDENT. VISUALLY INSPECTED AND OPERATIONALLY CHECKED ZONE 'D' WITH NO FAULTS FOUND. 2 L 7 4 4F A20WE 2002040800007 20020408 00007 NM 2002 4 8 02FDEA00225 1 20020329 A 2612 65249203 FIRE DETECTOR BOEING 727 727233 138408A NM NR 1 STRUT MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 277FE 22042 NR 1 STRUT OVERHEAT LIGHT CAME ON. REMOVED AND REPLACED FIRE DETECTION UNIT PER SMP 20-10-017, 28-14-011-5, 28-14-001-2 . 2 L 7 3 4F RT A3WE 2002040800008 20020408 00008 NM 2002 4 8 200200125 1 20020404 A 5340 65B11751601 FITTING BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 MED NR 3 LEFT FWD CORNER FITTING STA 1265 CRACKED AT LOWER END. INSTALLED MED NR 3 LT WD CORNER FITTING AT STA 1265 PER B747 SRM. REMOVED AND REPLACED LOCATED AND DRILLED FITTING PER B747 SRM. 2 L 7 4 4F A20WE 2002040800010 20020408 00010 NM 2002 4 8 200200199 1 20020403 A 5730 65B016262 SKIN BOEING 747 747132 1384882 NM WING CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 REPAIR FOR CORROSION ON LOWER IN SPAR SKIN PANEL AT FSS 1057. THE CORROSION WAS BLENDED AWAY WITH A 20:1 BLEND RATIO PER B747 SRM GUIDELINES AND HFEC INSPECTED TO ENSURE A CRACK FREE CONDITION. 2 L 7 4 4F A20WE 2002040800011 20020408 00011 NM 2002 4 8 200200200 1 20020403 A 5311 FRAME BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 FRAME AT BS 1940 STR WL125 IS CRACKED. (BETWEEN STR 37L AND 36L) INSTALLED NEW FRAME STA 1940 STR 34- 43L PER SRM 51-30- 2 SEALED PER 51-10-6. 2 L 7 4 4F A20WE 2002040800012 20020408 00012 NM 2002 4 8 200200201 1 20020403 A 5410 65B152419 PANEL BOEING 747 747132 1384882 NM NR 3 ENGINE DELAMINATED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 NR 3 ENGINE INTAKE NOSE COWL ACOUSTIC PANEL 5-6 OCLOCK FWD POSITION DELAMINATED. LOCATED AND DRILLED NEW ACOUSTIC PANEL , INSTALLED NEW ACOUSTIC PANEL. 2 L 7 4 4F A20WE 2002040800013 20020408 00013 NM 2002 4 8 200200202 1 20020403 A 5410 SEAL BOEING 747 747132 1384882 NM NACELLE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 REPAIR CRACKS IN LEFT AND RIGHT LOWER SLOT SEALS. THE LOWER SLOT SEALS ARE MADE FROM THE SAME MATERIAL AS THE UPPER SLO T SEALS BUT ARE NOT COVERED BY THE 747 SRM. THIS DOCUMENT ALLOWS WELDING OF THE LOWER SLOT SEAL ASSEMBLIES PROVIDED THE REPAIR IS NOT IN THE AREA OF THE HONEYCOMB SECTIONS. THE LOWER SLOT SEALS ARE SECONDARY STRUCTURE. 2 L 7 4 4F A20WE 2002040800014 20020408 00014 NM 2002 4 8 200200203 1 20020403 A 5410 STRUCTURE BOEING 747 747132 1384882 NM NR 3 PYLON DETERIORATED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 NR 3 PYLON LOWER SURFACE, JUST AHEAD OF THE AFT ENGINE MOUNT ON THE LEFT SIDE FIRESHIELD DETERIORATED. FABRICATED, AL ODINED, PRIMED AND INSTALLED PER B747 SRM. 2 L 7 4 4F A20WE 2002040800015 20020408 00015 NM 2002 4 8 200200231 1 20020405 A 5753 65B155351 BRACKET BOEING 747 747132 1384882 NM FLAP TRACK BROKEN B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 NR 6 FLAP TRACK TRANSMITTER POSITION CABLE PULLEY SUPPORT BRACKET LUG BROKEN OUTBOARD SIDE. REMOVED AND REPLACED SUPPO RT BRACKET ON NR 6 FLAP TRACK TRANSMITTER POSITION CABLE PULLEY BRACKET REF. B747 MM. 2 L 7 4 4F A20WE 2002040800016 20020408 00016 NM 2002 4 8 200200232 1 20020405 A 5551 ANGLE BOEING 747 747132 1384882 NM HORIZONTAL STAB CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 LT HORIZONTAL STAB INBOARD LEADING EDGE FAIRING HAS AN (L) ANGLE CRACKED 3RD RIB FROM INBOARD END. REMOVED (L) ANGLE CRA CKED, ORIGINAL MATERIAL 7075 PER CHEMICAL TEST 747 SRM 51-10-01 AND .030 PER CALIPER NR 99-0043 DUE DATE 04-02. FABRICAT ED (C) ANGLE FROM 7075-T6 .030 P.O.NR 221810 PER FLAT PATTERN LAYOUT 747 SRM 51-20-01 ALODINED AND PRIMED INSTALLED PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2002040800017 20020408 00017 NM 2002 4 8 200200233 1 20020405 A 5510 BALANCE WEIGHT BOEING 747 747132 1384882 NM HORIZONTAL STAB CHIPPED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 LEFT HAND HORIZONTAL STABILIZER ELEVATOR BALANCE WEIGHTS FROM STA. 206.8 - 331.8 HAS CHIPPED PAINT UPPER AND LOWER SURFA CES. REMOVED LOOSE AND FLAKING PAINT ON LEFT HORIZONAL STABILIZER BALANCE WEIGHTS AND PRIMED. 2 L 7 4 4F A20WE 2002040800018 20020408 00018 NM 2002 4 8 200200234 1 20020405 A 5312 BULKHEAD BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 BS1480 BULKHEAD AND SPLICE COMPONENT INSPECTION/ REPAIR/ MODIFICATION. THIS EO PERFORMS THE (PLAN B) INSPECTION AND MODI FICATION AS OUTLINED IN SB, INCLUDED ARE INSTRUCTIONS FOR INSPECTION, REPAIR AND MODIFICATION WORK ON THE SKIN, BULKHEAD AND COMPONENTS THAT CONNECT THE UPPER AND LOWER BULKHEAD AND OVERWING LONGERON AT BODY STATION 1480 ALSO INCLUDED ARE I NSTRUCTIONS FOR INSPECTION, REPAIR AND MODIFICATION WORK ON THE SKIN AND BULKHEAD WHERE STRINGER END FITTINGS AND SHEAR CLIP ARE ATTACHED TO THE BULKHEAD OUTER CHORD. PER E.O.53-747-1513-98 REV.F. 2 L 7 4 4F A20WE 2002040800019 20020408 00019 NE 2002 4 8 2002F00370 2 20020405 A 8530 116731 CYLINDER DOUG DC3 DC3C 3021457 WP PWA R1830 R183090D 52020 NE LT ENGINE SEPARATED E VLLA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 05 9923S 858 25964 BP436078 AT CRUISE POWER, LEFT ENGINE DEVELOPED A (SHAKE). ENGINE WAS SHUT DOWN AND AIRCRAFT DIVERTED. FOUND NR 4 CYLINDER LIFTED FROM ITS BASE. THE CYLINDER BARREL FAILURE ALSO CAUSED THE NR4 LINK ROD TO FAIL. 2 L 7 2 4R 4 R A669 5E4 2002040800020 20020408 00020 NM 2002 4 8 AWXA200200288 1 20020126 A 5315 AND101331202 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON FLOORBEAM TEE CAP AT BS 345, BL 0 TO LBL 23.0. MAINTENANCE CLE ANED CORROSION OFF FLOORBEAM AND FOUND MATERIAL REMAINING TO BE OUT OF LIMITS IAW B757-200 SRM 53-00-51. REMOVED DAMAGED SECTION OF FLOORBEAM FROM LBL 01 TO LBL 23, FABRICATED 2 EACH REPAIR ANGLES AND 1 EACH REPAIR FILLER AND INSTALLED REPA IR PARTS IAW B757-200 SRM 53-00-51, FIG 205, SHT 3, DETAIL I, PG. 218. 2 L 7 2 4F RT A2NM 2002040800021 20020408 00021 EU 2002 4 8 AWXA200200291 1 20020324 A 5347 D5311281520000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 MAJOR REPAIR - DURING C-8 CHECK CORROSION WAS FOUND ON OUTBOARD UPPER LIP OF SEAT TRACK NR2, 2 INCH AFT OF FR 20, Y 765 . MAINTENANCE REMOVED CORROSION AND CUTOUT DAMAGED SECTION OF SEAT TRACK, FABRICATED A REPAIR DOUBLER AND PLUG, AND INS TALLED REPAIR PARTS. 2 L 7 2 4F RT A28NM 2002040800022 20020408 00022 NM 2002 4 8 AWXA200200292 1 20020311 A 5315 6546811 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON THE TOP OF FLOORBEAM AT BS 986.5, LBL 58. MAINTENANCE CLEANED CO RROSION OFF FLOORBEAM AND FOUND MATERIAL LOSS EXCEEDING ALLOWABLE LIMITS. FABRICATED FLOORBEAM REPAIR STRAP AND INSTALL ED REPAIR PART AT BS 986.5, LBL 58. 2 L 7 2 4F RT A16WE 2002040800023 20020408 00023 NM 2002 4 8 AWXA200200294 1 20020311 A 5320 69434561 STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON THE RT FLOOR SUPPORT LOWER STRAP IN THE AFT CARGO COMPARTMENT AT BS 849, RBL 19. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED CORRODED STRAP AT RBL 1 9, BS 849, FABRICATED AND INSTALLED A NEW STRAP. 2 L 7 2 4F RT A16WE 2002040800024 20020408 00024 NM 2002 4 8 AWXA200200296 1 20020401 A 2560 P4010021 BATTERY BOEING 737 737277 1384570 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 186AW 22653 OAK - EMERGENCY EQUIPMENT - FORWARD EMERGENCY FLASHLIGHT INOPERATIVE (VERTICAL HANGING) NOT CHARGING. MAINTENANCE REPLAC ED EMERGENCY FLASHLIGHT BATTERIES. 2 L 7 2 4F RT A16WE 2002040800025 20020408 00025 NM 2002 4 8 C1HA200288001 1 20020322 A 5720 STRAP BOEING 727 7272S7 138407Z NM LT WING CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 688CA 22344 LEFT WING FIXED LEADING EDGE INNER STRAP IS CRACKED AT APPROX WS 226. REMOVED AND REPLACED STRAP, CUT STRAP INSTALL REP AIR. 2 L 7 3 4F A3WE 2002040800026 20020408 00026 NM 2002 4 8 C1HA200288002 1 20020322 A 5311 FRAME BOEING 727 7272S7 138407Z NM FUSELAGE GOUGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 688CA 22344 DENT WITH A GOUGE AT RIGHT NR 1 FRAME STA 188 AT 7:00 POS. BLENDED GOUGE IAW DOC PC-02-X062 AND 8110-3. VERIFIED NO CRACK EXIST. IAW B-727 NDT MAN. P1-6. TREATED AREA IAW B727 SRN 51-10-2. 2 L 7 3 4F A3WE 2002040800027 20020408 00027 NM 2002 4 8 C1HA200288003 1 20020322 A 5313 STRINGER BOEING 727 7272S7 138407Z NM CARGO BAY CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 688CA 22344 AFT CARGO PIT STA 950A, STRINGER 29L HAS CORROSION. REPAIRED STRINGER 29L FS 950B IAW AAR AIRCRAFT SERVICES SPEC AAR 022602. 8110-3 ATTACHED. 2 L 7 3 4F A3WE 2002040800028 20020408 00028 NM 2002 4 8 C1HA200288004 1 20020322 A 5720 STRAP BOEING 727 7272S7 138407Z NM RT WING CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 688CA 22344 RIGHT WING FIXED LEADING EDGE INNER STRAP IS CRACKED AT APPROX W.S. 226. REPAIRED INNER STRAP RIGHT WING AT WS 226. 2 L 7 3 4F A3WE 2002040800029 20020408 00029 NM 2002 4 8 C1HA200288005 1 20020322 A 5754 SLAT TRACK BOEING 727 7272S7 138407Z NM WING CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 688CA 22344 CUTOUT FOR NR 4 SLAT OUTBOARD TRACK IS CRACKED IN FIXED LEADING EDGE. STOP, DRILLED CRACK, REPAIRED. 2 L 7 3 4F A3WE 2002040800030 20020408 00030 NM 2002 4 8 C1HA200288006 1 20020322 A 5230 SEAL BOEING 727 7272S7 138407Z NM CARGO DOOR CHAFED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 688CA 22344 AFT PIT DOOR LOWER SEAL DEPRESSOR CHAFED ON OUTER EDGE. REMOVED LOWER DOOR SEAL DEPRESSOR'S (3EA), LOCATED AND DRILLED NEW SEAL DEPRESSORS (3EA). INSTALLED NEW SEAL DEPRESSORS (3 EA), PREPACKED LOWER DOOR SEAL AREA. 2 L 7 3 4F A3WE 2002040800031 20020408 00031 NM 2002 4 8 C1HA200288007 1 20020322 A 5313 STRINGER BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 688CA 22344 STRINGER 28L IS EXFOLIATED BETWEEN FA 1090 AND 1110. FABRICATED STRINGER REPAIR PARTS. INSTALLED STRINGER REPAIR, FAB RICATED SKIN REPAIR PARTS, INSTALL SKIN REPAIR. FABRICATED NEW STRINGER CLIP, INSTALLED. 2 L 7 3 4F A3WE 2002040800032 20020408 00032 NM 2002 4 8 C1HA200288008 1 20020322 A 5410 ANGLE BOEING 727 7272S7 138407Z NM NR 1 PYLON CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 688CA 22344 ANGLE IS CRACKED IN RADIUS INSIDE NR 1 PYLON AT APPROX FS 1160 IN ACCESS AREA FOR THROTTLE QUADRANT. REMOVED DAMAGED ANGLE, FABRICATED AND INSTALLED. 2 L 7 3 4F A3WE 2002040800033 20020408 00033 NM 2002 4 8 C1HA200288009 1 20020322 A 5410 ANGLE BOEING 727 7272S7 138407Z NM NR 1 PYLON CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 688CA 22344 NR1 PYLON LOWER FWD LEADING EDGE SUPPORT ANGLE IS CRACKED OUT AT A FASTENER HOLE. REMOVED DAMAGED ANGLE FABBED AND INST ALLED. 2 L 7 3 4F A3WE 2002040800034 20020408 00034 NM 2002 4 8 C1HA200288010 1 20020322 A 3222 BUSHING BOEING 727 7272S7 138407Z NM NLG ACTUATOR DAMAGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 688CA 22344 NOSE LANDING GEAR ATTACH LUGS FOR ACTUATOR FITTING HAS (1 EA) DAMAGED BUSHING ON THE INBOARD UPPER LUG AND (3 EA.) LOWER LUGS HAVE CORROSION ON FACES. REPAIR LUGS. 2 L 7 3 4F A3WE 2002040800035 20020408 00035 NM 2002 4 8 C1HA200288011 1 20020322 A 5340 FITTING BOEING 727 7272S7 138407Z NM FUSELAGE DAMAGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 688CA 22344 UPPER BEAM AT STA 1273 HAS PREVIOUS REPAIR CRACKED UNDER AIRSTAIRS ACTUATOR ATTACH FITTING, RIGHT SIDE OF VENTRAL THROUG H LIGHTNING HOLE. REPAIRED DAMAGE. 2 L 7 3 4F A3WE 2002040800036 20020408 00036 NM 2002 4 8 C1HA200296011 1 20020401 A 3350 BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 696CA 22574 EXTERIOR EMERGENCY LIGHT, AFT LEFT OVERWING NO ILLUMINATION AT SIDE PANEL. REMOVED AND REPLACED BATTERY PACK IN OVERHEA D CEILING PANEL OVER 27ABC WITH SERVICEABLE UNIT. OPERATIONAL CHECKS GOOD. 2 L 7 3 4F RT A3WE 2002040800037 20020408 00037 NM 2002 4 8 C1HA200296012 1 20020401 A 3350 BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 696CA 22574 EXTERIOR EMERGENCY LIGHT, LEFT AFT TRAILING EDGE NO ILLUMINATION. REMOVED AND REPLACED BATTERY PACK IN OVERHEAD CEILING AT 24ABC WITH SERVICEABLE UNIT. OPERATIONAL CHECKS GOOD. 2 L 7 3 4F RT A3WE 2002040800038 20020408 00038 SO 2002 4 8 C2XA02CL088 1 20020403 A 2120 ODOR EMB 135 EMB135LR 3260305 SO CABIN DETECTED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16525 145403 THE CREW REPORTED A STRONG ODOR OF FUEL IN CABIN WHEN THE APU WAS STARTED. MAINTENANCE INSPECTED AND PERFORMED OPERATIO NAL CHECKS OF THE APU. NO DEFECTS WERE FOUND.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002040800039 20020408 00039 WP 2002 4 8 CALA0200171 1 20020404 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND 1 INCH CRACKS AT FLOOR PANEL INSERTS, FS 1003. THE FLOOR PANEL WAS REPAIRED. 2 L 7 2 4F A6WE 2002040800040 20020408 00040 WP 2002 4 8 CALA0200173 1 20020404 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND FLOOR PANEL CORRODED AT STA 180, LBL 10 - RBL 55. THE CORRODED DOUBLER WAS REMOVED FROM THE WEB AND A R EPAIR DOUBLER WAS INSTALLED. 2 L 7 2 4F A6WE 2002040800041 20020408 00041 NM 2002 4 8 CALA0200178 1 20020404 A 5347 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND A 4 INCH CRACK AT ATTACH POINT OF RIGHT TIE DOWN TRACK, STA 747. A NEW SECTION OF TIE DOWN TRACK WAS SP LICED. 2 L 7 2 4F RT A16WE 2002040800045 20020408 00045 EU 2002 4 8 MALA020231 1 20020403 A 2610 006WS00 WEU SAAB SF340 SF340A 7850100 EU DEFECTIVE A MALA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 68XJ 340A068 DURING TAXI ON FLIGHT #2734, RH FIRE DETECT LIGHT ILLUMINATED ON TAXI. DECLARED EMERGENCY. ON TAXI INTO DTW RH FIRE T-H ANDLE ILLUMINATED AND MASTER WARNING SOUNDED. MEMORY ITEMS PERFORMED. T-HANDLE REMAINED ON AFTER FIREING BOTH BOTTLES. AFTER SHUTTING DOWN ENGINE AND HAVING CFR CHECKOUT RIGHT ENGINE, A/C WAS TOWED TO THE GATE AND LIGHT (T-HANDLE) ILLUMIN ATED INTERMITTANTLY. MAINTENANCE REPLACED WEU. PN ON/OFF 006WS00. SN ON 1390. RAN A/C THROUGH SEVERAL CONFIGURATIONS. ALL CHECKS GOOD AT THIS TIME. ALL IAW SAAB AMM 2 L 7 2 4T RT A52EU 2002040800119 20020408 00119 NM 2002 4 8 DHL2002741004 1 20020404 A 3260 PIN BOEING 727 7272Q9 138448M NM MLG FAILED A DHLA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 741DH 21931 WHEN LANDING GEAR EXTENDED, RED LANDING GEAR UNSAFE LIGHTS FAILED TO EXTINGUISH. CYCLED LANDING GEAR. ALL INDICATIONS NORMAL GEAR PINS INSTALLED TO FACILITATE OTHER MAINTENANCE OPS CHECK. LANDING GEAR EXTENTION AND RETRACTION INDICATIO NS, OPS CHECK. GOOD. REMOVED GEAR PINS AND STOWED. 2 L 7 3 4F RT A3WE 2002040800120 20020408 00120 WP 2002 4 8 DHL2002804003 1 20020404 A 2612 INDICATOR DOUG DC8 DC873F 302199F WP NR 1 ENGINE SHORTED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 804DH 46124 IN FLIGHT, NR 1 ENGINE SHORT CIRCUIT LIGHT CAME ON, FLICKERING WHEN ON (B) LOOP SWITCH TO (A) LOOP LIGHT EXTINGUISHED. PERFORMED OPS CHECK OF NR1 SHORT CIRCUIT SYSTEM. NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 2002040800125 20020408 00125 NM 2002 4 8 200200216 1 20020404 A 5320 65B11751602 FITTING BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 MED NR 3 RIGHT FWD CORNER FITTING CRACKED AT LOWER AFT END. INSTALLED NEW CORNER FITTING AT NR 3 RIGHT FWD AFT END STA 1265 PER B747 SRM 51-30-02 & 51-10-01. 2 L 7 4 4F A20WE 2002040800127 20020408 00127 NM 2002 4 8 200200217 1 20020404 A 5320 ANGLE BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 MAIN DECK AT STA 340, STR 26R FLOORBOARD SUPPORT ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, AND I NSTALLED REPAIR PARTS PER B747 SRM 51-40-04, 51-10-01, 51-30-05, 51-10-02 AND B747 SOPM 20-41-02. 2 L 7 4 4F A20WE 2002040800130 20020408 00130 NM 2002 4 8 200200218 1 20020404 A 5320 TIE CLIP BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 STRINGER TIE-CLIP DAMAGED -TWO SMALL CRACKS AT STA 1660 AND S-12 RIGHT. INSTALLED TIE-CLIP B747 SRM 51-30-02. 2 L 7 4 4F A20WE 2002040800132 20020408 00132 NM 2002 4 8 200200219 1 20020404 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 MAIN DECK AT STA 1000 RBL 33 HAS A CORRODED SEAT TRACK FLANGE I/B SIDE. REPAIRED PER SRM 53-10-5 FIG 1A. 2 L 7 4 4F A20WE 2002040800133 20020408 00133 NM 2002 4 8 200200220 1 20020404 A 5753 65B136971 ATTACH FITTING BOEING 747 747132 1384882 NM T/E FLAP CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 NR 3 FLAP TRACK ATTACHMENT FITTINGS BOTH INBOARD AND OUTBOARD CORRODED (PITTED). REMOVED AND REPLACED NR 3 TRACK ATTACH FITTINGS PER 747 MM 27-51-25. 2 L 7 4 4F A20WE 2002040800135 20020408 00135 WP 2002 4 8 ZW0A0201602 1 20020207 A 5314 KEELBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C IN LT WHEEL WELL, FOUND ANGLE CRACKED FWD OF HINGE CASTING AT KEEL BEAM. REMOVED AND REPLACED CRACKED AN GLE PER SPM 6-70-01. 2 L 7 2 4F A6WE 2002040800136 20020408 00136 WP 2002 4 8 ZW0A0201603 1 20020207 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 948TW 49575 DURING CHECK-C FOUND CORROSION ON HORIZONTAL ANGLE ATTACHED TO TRAPEZOIDAL PANEL RBL 58, 7 INCHES AFT OF CENTER SECTION UPPER SPAR CAP; JUST AFT OF LT MLG SIDE STRUT UPPER MOUNT, 9 INCHES BELOW PRESSURE DECK. REMOVED AND REPLACED ANGLE PER SRM 6-7-01 PG 3, AND BOEING DRAWING 5930516. 2 L 7 2 4F RT A6WE 2002040800137 20020408 00137 WP 2002 4 8 ZW0A0201701 1 20020208 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 971TW 53621 THE AFT LEFT AND RT OVERWING EMERGENCY OVERHEAD LIGHTS, AND THE ROW 13 EGRESS LIGHT, WERE INOPERATIVE. REPLACED THE BAT TERIES IN THE BATTERY PACK FOR THE OVERWING LIGHTS, AND THE LAMP P/N 7732 FOR THE EGRESS LIGHT. 2 L 7 2 4F RT A6WE 2002040800138 20020408 00138 NM 2002 4 8 ZW0A0201702 1 20020208 A 3350 BR9279106 LIGHT BOEING 717 717200 1383700 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 413TW 55080 THE EGRESS LIGHT AT ROW 19 WAS INOPERATIVE. REPLACED THE LIGHT ASSEMBLY. 2 L 7 2 4F TR A6WE 2002040800139 20020408 00139 WP 2002 4 8 ZW0A0201703 1 20020206 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 908TW 49169 DURING CHECK-C MAINTENANCE LONGERON 2R WAS FOUND CRACKED AT TAPERED END AFT OF STA 1418. A ONE INCH CRACK. REMOVED, FA BRICATED, AND INSTALLED LONGERON PER SRM 53-02, FIG 18 AND MD80 MM. 2 L 7 2 4F A6WE 2002040800140 20020408 00140 NM 2002 4 8 ZW0A0201801 1 20020211 A 3350 80751 LIGHT BOEING 767 76733AER 1385230 NM CABIN BROKEN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 637TW 25403 THE EGRESS LIGHT STRIP WAS BROKEN OFF AT SEAT 25A. REPLACED THE LIGHT ASSEMBLY. 2 L 7 2 4F RT A1NM 2002040800141 20020408 00141 WP 2002 4 8 ZW0A0201802 1 20020207 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT FOUND CORROSION ON THE LT TIE DOWN TRACK FROM STA 1003 TO 1231. INSTA LLED NEW TIE DOWN TRACK PER SPM 6-70-01-4B, AND SRM 51-30-01. 2 L 7 2 4F A6WE 2002040800142 20020408 00142 WP 2002 4 8 ZW0A0201803 1 20020207 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT FOUND CORROSION ON FLOOR TRACK AT STA 1211 TO 1320, RT TRACK. REPLACE D TRACK PER SPM 6-70-01-4B, AND SRM 51-30-01. 2 L 7 2 4F A6WE 2002040800143 20020408 00143 WP 2002 4 8 ZW0A0201804 1 20020207 A 5230 BRACKET DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT THE FORWARD CARGO COMPARTMENT DOOR HAD A SMALL BRACKET CRACKED LOCATED INSIDE THE SECOND LIGHTENING HOLE FROM THE AFT END, AT LOWER EDGE OF THE FWD CARGO COMPARTMENT DOOR. CONFIRMED WITH EDDY CURRENT. INSTALLED FITTIN G. 2 L 7 2 4F A6WE 2002040800144 20020408 00144 WP 2002 4 8 ZW0A0201805 1 20020212 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT THE AFT CABIN STA 1338, RBL 57, WEB HAD HEAVY CORROSION 6 INCHES BELOW FLOORBEAM RT LAV. INSTALLED FILLER DOUBLER PER SRM 51-70-4. 2 L 7 2 4F A6WE 2002040800145 20020408 00145 WP 2002 4 8 ZW0A0201806 1 20020212 A 5320 TIE CLIP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT THE AFT CABIN STA 1338 TIE CLIP HAD CORROSION AT RBL 57 AREA. INSTALLED NEW CLIP PER SPM 6-70-01. 2 L 7 2 4F A6WE 2002040800146 20020408 00146 WP 2002 4 8 ZW0A0201807 1 20020213 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT IN CARGO COMPT FOUND CORROSION ON TIE DOWN TRACK AT STA 785, RT SIDE. REPLACED TRACK WITH NEW AT S TA 693 TO 788 PER SPM 6-70-01. 2 L 7 2 4F A6WE 2002040800147 20020408 00147 WP 2002 4 8 ZW0A0202001 1 20020208 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT FOUND CORROSION IN RT FLOORBEAM BETWEEN STA 636 AND 693. REMOVED CORROSION PER SPM 6-80-01. INSTA LLED REPAIR ANGLE AND FILLER PER SRM 53-05, FIG 20A. 2 L 7 2 4F A6WE 2002040800148 20020408 00148 WP 2002 4 8 ZW0A0202002 1 20020208 A 5230 STOP FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT IN MID CARGO COMPT THE AFT BOTTOM DOOR STOP BRACKET, INSIDE THE DOOR, IS CRACKED ON AFT SIDE. REMO VED AND REPLACED CRACKED BRACKET AND REPLACED WITH NEW PER SRM 51-01, PAGE 1. 2 L 7 2 4F A6WE 2002040800149 20020408 00149 WP 2002 4 8 ZW0A0202003 1 20020210 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9304C 49530 DURING CHECK-C MAINT FOUND 8 INCH LONG GOUGE WITH SHARP EDGES IN FUSELAGE STA 323 BETWEEN LONGERON 17L AND 18L. INSTALL ED REPAIR PER SRM 53-04, FIG 38. 2 L 7 2 4F RT A6WE 2002040800150 20020408 00150 WP 2002 4 8 ZW0A0202004 1 20020213 A 5320 TIE CLIP DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 967TW 53617 DURING CHECK-C MAINT THE UPPER FWD CORNER OF THE RT VENT BOX STRUCTURAL TIE CLIP WAS BROKEN. FABRICATED NEW CLIP AND IN STALLED PER SRM 51-30-6 AND SPM 6-30-07. 2 L 7 2 4F RT A6WE 2002040800154 20020408 00154 NM 2002 4 8 200200221 1 20020404 A 5753 65B130961 ATTACH FITTING BOEING 747 747132 1384882 NM T/E FLAP CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 PITTING CORROSION ON NR 1 FLAP TRACK INBOARD ATTACH FITTING. REPLACED NR 1 TRACK INBOARD SIDE LOAD FITTING PER 747 MM 2 7-51-27. 2 L 7 4 4F A20WE 2002040800156 20020408 00156 NM 2002 4 8 200200222 1 20020404 A 5753 65B130971 ATTACH FITTING BOEING 747 747132 1384882 NM T/E FLAP CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 PITTING CORROSION ON NR 1 FLAP TRACK OUTBOARD ATTACH FITTING. REPLACED NR 1 TRACK OUTBOARD ATTACH (SIDELOAD) FITTING PE R 747 MM 27-51-27. 2 L 7 4 4F A20WE 2002040800158 20020408 00158 NM 2002 4 8 200200223 1 20020404 A 5753 65B136982 ATTACH FITTING BOEING 747 747132 1384882 NM T/E FLAP CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 PITTING CORROSION ON ATTACH FITTING BELOW BRONZE SHIM/SPACER ON NR 6 FLAP TRACK OUTBOARD ATTACH FITTING. REPLACED ATTAC H FITTING PER 747 MM 27-51-27. 2 L 7 4 4F A20WE 2002040800159 20020408 00159 NM 2002 4 8 200200224 1 20020404 A 5753 65B136972 ATTACH FITTING BOEING 747 747132 1384882 NM T/E FLAP CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 PITTING CORROSION ON ATTACH FITTING BELOW BRONZE SHIM/SPACER ON NR 6 FLAP TRACK INBOARD ATTACH FITTING. REMOVED AND REP LACED ATTACH FITTING WITH SHIM PER 747 MM 27-51-25. 2 L 7 4 4F A20WE 2002040800161 20020408 00161 NM 2002 4 8 200200225 1 20020404 A 5520 65B250451 BALANCE WEIGHT BOEING 747 747132 1384882 NM ELEVATOR CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 LEFT HAND HORIZONTAL STAB ELEVATOR WEIGHT APPROX STA 281.3 - 306.8 HAS CORROSION. REMOVED AND REPLACED LEFT HAND HORIZ STAB ELEVATOR WEIGHT AT STA 260-268 PER B747 OHM 55-20-21. 2 L 7 4 4F A20WE 2002040800162 20020408 00162 NM 2002 4 8 200200226 1 20020404 A 5720 SPACER BOEING 747 747132 1384882 NM WING CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 CORROSION ON SPACER TO FITTING AT NR 5 FLAP TRACK ON WALKING BEAM AFT ATTACH FITTING. REMOVED AND REINSTALLED FITTING A T NR 5 FLAP TRACK WITH NEW SHIM AND HARDWARE PER 747 20-51-01. 2 L 7 4 4F A20WE 2002040800163 20020408 00163 NM 2002 4 8 200200227 1 20020404 A 5312 63B1268223 FITTING BOEING 747 747132 1384882 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 STA 2484 LEFT LOWER BULKHEAD SPLICE FITTING AT S-23 CRACKED FROM LWR INBOARD FASTENER. REMOVED AND REPLACED FITTING PER SERVICE BULLETIN 53-2162 AND 05-0323 STEPS 5 & 6. 2 L 7 4 4F A20WE 2002040800164 20020408 00164 NM 2002 4 8 200200228 1 20020404 A 5753 65B229075 PIN BOEING 747 747132 1384882 NM FLAP TRACK CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 NR 1, 2, 3, 4, FLAP TRACK FWD FUSE PINS HAVE PITTING CORROSION ON INTERIOR OF PINS. REPLACED 1, 2, 3, 4 FLAP TRACK FWD FUSE PINS PER B747 MM CHAP 27-51-22, 25, 27. 2 L 7 4 4F A20WE 2002040800165 20020408 00165 NM 2002 4 8 200200229 1 20020405 A 5753 65B229051 PIN BOEING 747 747132 1384882 NM FLAP TRACK CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 NR 5, 6, 7, 8 FLAP TRACK FWD FUSE PINS HAVE PITTING CORROSION ON INTERIOR OF PINS. REPLACED NR 5, 6, 7, 8 FLAP TRACK FW D FUSE PINS PER 747 MM CHAP 27-51-27, 25, 22. 2 L 7 4 4F A20WE 2002040800166 20020408 00166 NM 2002 4 8 200200230 1 20020405 A 5753 MOUNT BOEING 747 747132 1384882 NM T/E FLAP CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 NR 8 FLAP TRACK I/B MOUNT HAS PITTING CORROSION ON FACE OF MOUNT AND BOLT HOLE. REPLACED NR 8 FLAP TRACK I/B SIDE LOAD FITTING PER B747 MM 27-51-27. 2 L 7 4 4F A20WE 2002040800167 20020408 00167 NM 2002 4 8 DHL2002715003 1 20020408 A 5310 BAC150529222 ANGLE BOEING 727 727155C 138404Z NM CRACKED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 On weekly visit "discrepancy" Frame at door latch fitting is cracked in radius at BS 500, 4l 200, below S-17L.1) Upon fu rther evaluation found attach angle "T" to frame cracked. Removed frame to skin attach "T" I.A.W. 727 S.R.M. 51-30-2. Fa bricated attach angle "T" using BAC 1505-29222 7075 T6 511 Dim approx 1"x 2" I.A.W. S.R.M. 53-10-2 fig. 3 and S.R.M. 53- 10-4 fig. 31. Alodined and primed I.A.W. 727 S.R.M. 51-10-2. Installed attach "T" to frame and skin I.A.W. 727 S.R.M. 51 -30-2.1) Upon further evaluation evatuation found attach "T" to frame cracked not frame.2) Removed cracked attach "T" I. A.W. 727 S.R.M. 51-30-2.3) Replaced attach "T" using BAC 1505-29222 7075 T 6511. Extrusion I.A.W. 727 S.R.M. 53- 2 L 7 3 4F A3WE 2002040800168 20020408 00168 NM 2002 4 8 3730002 1 20020405 A 3350 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 373PA 23749 THREE EMERGENCY EXIT FLOOR LIGHTS INOP. 2 L 7 2 4F RT A16WE 2002040800169 20020408 00169 NM 2002 4 8 373PA0002 1 20020405 A 3350 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 373PA 23749 THREE EMERGENCY EXIT FLOOR LIGHTS INOP. 2 L 7 2 4F RT A16WE 2002041500116 20020415 00116 WP 2002 4 15 ARWA20020401 1 20020402 A 3230 56165545503 CYLINDER DOUG DC8 DC863F 302198F WP RT MLG LEAKING A ARWA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 661AV 45969 AFTER LANDING, LOSS OF HYD PRESSURE WITH LOW PRESSURE LIGHT, AILERON & RUDDER POWER LIGHTS ON, QUANTITY NORMAL. ACFT WA S STOPPED ON THE TAXIWAY & TOWED TO THE RAMP. REMOVED AND REPLACED RIGHT HAND MLG BOGIE TRIM CYLINDER ASSY IAW MM 32-33 -1. LEAK CHECK ACCOMPLISHED, NO LEAKS NOTED. 2 L 7 4 4F 4A25 2002040800170 20020408 00170 NM 2002 4 8 SQ7A012002 1 20020206 A 5713 STRINGER BOEING 727 727251 138408H NM Zone 500 CRACKED A SQ7A O OTHER O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - during scheduled maintenance a crack was found in the L/H wing upper surface stringer @ WS 686.5, second stringer from aft.Repaired crack per Service bulletin 727-57A-159, figure 18. 2 L 7 3 4F A3WE 2002040800171 20020408 00171 NM 2002 4 8 AWXA200200261 1 20020329 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 PHX - EEL - EMERGENCY ESCAPE LIGHT ON SEAT ROW 7 LT DETACHED. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE LIGHT O N SEAT ROW 7 LT, FUNCTIONAL CHECK WAS GOOD IAW T/C A1C33006. 2 L 7 2 4F RT A16WE 2002040800172 20020408 00172 NM 2002 4 8 SQ7A022002 1 20020206 A 5320 ANGLE BOEING 727 727251 138408H NM BS480 CORRODED A SQ7A O OTHER O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - During scheduled maintenance the attach angle for the fwd cargo pit bulkhead attach angle @BS 480 was found corred ed.Removed & replaced the z section channel IAW SRM 51-10-1,para. 6 & SRM 51-30-2. 2 L 7 3 4F A3WE 2002041500184 20020415 00184 NM 2002 4 15 F3LA200200123 1 20020406 A 5320 INTERCOSTAL BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 3415 24569 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 344-360, BL 0, CRACKED ON TOP FLANGE FWD END AND HAS DAMAGE ON BOTTOM FLANGE. FABRICATED REPAIR PARTS PER SRM 51-70-11 AND INSTALLED REPAIR PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002040800173 20020408 00173 NM 2002 4 8 AWXA200200267 1 20020310 A 5330 65C27755 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .250 INCH CRACK WAS FOUND ON THE SKIN OF THE L2 DOOR CUTOUT AT BS 986.5, STR 8 LT. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW B737-300 SRM. 2 L 7 2 4F RT A16WE 2002040800174 20020408 00174 NM 2002 4 8 AWXA200200268 1 20020311 A 5311 654653949 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND ON CABIN SIDE WALL FRAME ATTACHED TO FLOORBEAM AT BS 6 16, LBL 66, WL 208, LOCATED JUST BELOW FLOOR LINE UNDER THE OVERWING EMERGENCY EXIT. MAINTENANCE REMOVED INNER CHORD, F ABRICATED NEW INNER CHORD AND INSTALLED REPAIR IAW B737-300, SRM 53-00-07 PG 101-104, AND DWG 65-46539. 2 L 7 2 4F RT A16WE 2002040800175 20020408 00175 NM 2002 4 8 AWXA200200270 1 20020311 A 5315 6545410 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK A CRACK WAS FOUND RUNNING FROM SEAT TRACK FLOORBEAM TEE CAP LOWER EDGE TO A FASTE NER HOLE ON INBOARD SIDE, BS 663.75, RBL 26. FABRICATED A REPAIR STRAP, SHIMS AND INSTALLED REPAIR PARTS IAW B737-300 S RM 51-40-02 PG 10 AND CP2-LCQ-02-00007H, PG 1 & 2. 2 L 7 2 4F RT A16WE 2002040800176 20020408 00176 NM 2002 4 8 AWXA200200271 1 20020321 A 5512 65C27494 SKIN BOEING 737 7373G7 1384595 NM HORIZ STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 LCQ - MAJOR REPAIR - DURING C-15 CHECK A DENT WAS FOUND ON RT HORIZONTAL STABILIZER AT STAB STA 144 MID SPAN. FABRICATE D A DOUBLER, FILLER AND INSTALLED REPAIR PARTS IAW B737-300 SRM. 2 L 7 2 4F RT A16WE 2002040800177 20020408 00177 EU 2002 4 8 AWXA200200281 1 20020321 A 5210 FE174003 DAMPER AIRBUS 320 A320231 3930325 EU R1 DOOR FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 30406 317 YWG - EMERGENCY EVACUATION - DURING C-08 CHECK THE R1 DOOR DAMPER WOULD NOT SNUB. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR DAMPER IAW AMM 52-11-14-401, PRESSURE CHECKED IAW AMM 52-11-14-210-056. 2 L 7 2 4F RT A28NM 2002040800178 20020408 00178 EU 2002 4 8 AWXA200200282 1 20020321 A 5210 FE174001 DAMPER AIRBUS 320 A320231 3930325 EU L1 DOOR FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 30406 317 YWG - EMERGENCY EVACUATION - DURING C-08 CHECK THE L1 DOOR DAMPER WOULD NOT SNUB. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR DAMPER IAW AMM 52-11-14-401, PRESSURE CHECKED IAW AMM 52-11-14-210-056. 2 L 7 2 4F RT A28NM 2002041900061 20020419 00061 NM 2002 4 19 AWXA200200283 1 20020402 A 3510 80130700 OXYGEN BOTTLE BOEING 737 7373G7 1384595 NM COCKPIT LEAKING A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 156AW 23778 PHX - AIR TURNBACK - FLT 0332 - EN ROUTE FROM PHX TO SJD WHILE CLIMBING TO CRUISE ALTITUDE FLIGHT CREW NOTICED CREW OXYG EN GAUGE READING BELOW 200 PSI, OXYGEN MASKS WERE CHECKED AND VERIFIED WITH NO PRESSURE, AIRCRAFT TURNED BACK TO PHX AND LANDED UNEVENTFULLY. MAINTENANCE VERIFIED OXYGEN GAUGE ON FLIGHT DECK AND AT CYLINDER BOTH INDICATED 0 PSI, REMOVED AN D REPLACED OXYGEN CYLINDER IAW T/C S8M35001. 2 L 7 2 4F RT A16WE 2002040800179 20020408 00179 NM 2002 4 8 AWXA200200284 1 20020323 A 5310 65566542 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - MAJOR REPAIR - DURING C-12 CHECK CORROSION WAS FOUND AROUND FASTENERS OF THE AFT CARGO COMPARTMENT DOOR CUTOUT FOR WARD JAMB WEB DOUBLER JUST FORWARD OF THE LOWER STOP FITTING. MAINTENANCE REMOVED THE DAMAGED WEB DOUBLER ON AFT CARGO COMPARTMENT DOOR CUTOUT FWD JAMB IAW B737-300 SRM 51-40-02, PG 38 & 42. FABRICATED A NEW WEB DOUBLER, AND INSTALLED REP AIR IAW B737-300 SRM 51-40-02, PG 26, 28, 39-41. 2 L 7 2 4F RT A16WE 2002040800180 20020408 00180 NM 2002 4 8 AWXA200200285 1 20020323 A 5310 65566542 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - MAJOR REPAIR - DURING C-12 CHECK TWO DENTS WERE FOUND ON THE AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD JAMB LOWER WEB DOUBLER. MAINTENANCE REMOVED THE DAMAGED WEB ON THE AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD JAMB LOWER WEB DOUBLE R IAW B737-300 SRM 51-40-02, PG 38 & 42. FABRICATED A NEW SECTION OF WEB, AND INSTALLED THE REPAIR IAW B737-300 SRM 51- 70-13, PG 1-5. 2 L 7 2 4F RT A16WE 2002040800181 20020408 00181 NM 2002 4 8 AWXA200200286 1 20020126 A 5315 141N51231 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 GYR - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AT BS 377, LBL 45 TO LBL 60. REMOVED D AMAGED SECTION OF FLOORBEAM, FABRICATED AND INSTALLED REPAIR IAW B757-200 SRM 53-10-51, AND SRM 51-21-1, FIG 203, PG 210 . 2 L 7 2 4F RT A2NM 2002040800182 20020408 00182 EA 2002 4 8 CA020315003 1 20020306 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE NOSE GEAR DOOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) GEAR DISAGREE LIGHT ON AFTER TAKEOFF FROM LAGUARDIA. NOSE GEAR AND DOOR REMAINED DOWN AND LOCKED. AIRCRAFT CONTINU E TO OTTAWA WITH GEAR DOWN. NOSE GEAR DOOR SELECTOR VALVE REPLACED. MAIN AND NOSE GEARS RETRACTION AND EXTENSION CARRIED OUT SEVERAL TIMES. NO FAULT FOUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2002040800183 20020408 00183 EU 2002 4 8 CA020315010 1 20020312 A 5320 FK26342 CLIP AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211TRENT77 NE FUEL LINE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING THE ENGINE INSPECTION , FOUND A BROKEN CLIP THAT WAS HOLDING A FUEL TUBE ASSY UNDER THE LP COMPRESSOR CAS E. NOW CAUSING CHAFING BETWEEN THE IDG AND THE UMMY FLOWMETER CONNECTOR. REFERENCE ; IPC 73-11-47 FIG 3 2 L 7 2 4F 4 F RT A46NM E39NE 2002040800184 20020408 00184 NM 2002 4 8 CA020328004 1 20020307 A 2133 60683221 OUTFLOW VALVE BOEING 767 7673S1 1385211 NM GE CF6 CF680C2B6F 30025 NE OUTFLOW VALVE FAILED W A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 CA (CAN) AFTER TAKEOFF, EICAS MESSAGE "CABIN ALT AUTO 1 APPEARED. AIRCRAFT DIVERTED TO LONDON (HEATHROW) LHR FOR FIX. O UTFLOW VALVE AND ACTUATOR REPLACED AS PER AMM 21-31-02. SYSTEM CHECKED SERVICEABLE.OUTFLOW VALVE -606832-21 ACTUATOR -2 022480-6 2 L 7 2 4F 4 F RT A1NM E13NE 2002040800186 20020408 00186 NM 2002 4 8 AWXA200200287 1 20020126 A 5315 BAC150510061 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 DURING C-08 CHECK CORROSION WAS FOUND ON TOP AND BOTTOM OF FLOORBEAM UPPER CHORD AT BS 365, BL 0 TO RBL 62.0. FABRICATE D NEW SECTION OF UPPER CHORD AND INSTALLED NEW CHORD. 2 L 7 2 4F RT A2NM 2002040800196 20020408 00196 NM 2002 4 8 AWXA200200297 1 20020317 A 5320 654657959 ANGLE BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 YVR - MAJOR REPAIR - DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON THE LOWER CHORD OF THE APU INLET TORQUE BOX CU TOUT AT SURFACE WHERE SHROUD SEAL MAKES CONTACT BS 1088+30. MAINTENANCE REMOVED AND REPLACED APU TORQUE BOX LOWER CHORD ANGLE AT BS 1088+30 IAW B737-200 SRM 51-10-1 PG 8, AND DWG 65-46579. 2 L 7 2 4F RT A16WE 2002040800207 20020408 00207 NM 2002 4 8 AWXA200200300 1 20020322 A 5320 6546579510 STIFFENER BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 YVR - MAJOR REPAIR - DURING C-14 CHECK CORROSION WAS FOUND ON APU TORQUE BOX FRAME APPROXIMATELY 3 INCHES FROM LOWER END AT BS 1113 RT SIDE. MAINTENANCE REMOVED STIFFENER ON APU TORQUE BOX FRAME, FABRICATED A NEW STIFFENER AND FILLER PLATE , AND INSTALLED IAW B737-200 SRM 51-10-1 PG 8 AND DWG 65-46579, SHT 4. 2 L 7 2 4F RT A16WE 2002040800211 20020408 00211 NM 2002 4 8 AWXA200200302 1 20020327 A 5320 6517688168 STIFFENER BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON INNER CHORD AT NUT PLATE HOLES OF UPPER AND LO WER SURFACE FROM BS 306 TO BS 328, ON LOWER SURFACE CORROSION WAS FOUND TO BE ON THE INNER CHORD STIFFENER (ANGLE). MAI NTENANCE REMOVED CORRODED STIFFENER AND INNER CHORD FROM BS 277 TO BS 360, FABRICATED A NEW STIFFENER AND INNER CHORD AN D INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PG 3, 4, & 10. 2 L 7 2 4F RT A16WE 2002040800213 20020408 00213 NM 2002 4 8 SABA020046 1 20020408 A 3350 10005511 BULB DHAV DHC8 DHC8103 1386005 NM CABIN BURNED OUT A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 880CC 277 Aircraft 880 on flight 5025 from CLT to TLH. During pre-flight inspection row 1 floor emergency light was found to have a bulb inoperative. Maintenance removed and replaced the bulb. Ops check was good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002040800214 20020408 00214 NM 2002 4 8 AWXA200200306 1 20020403 A 2560 DIN40863R62 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 826AW 1534 LAS - EMERGENCY EQUIPMENT - FORWARD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN FORWARD CABIN FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002040800215 20020408 00215 EU 2002 4 8 CX7A194J3 1 20020405 A 3230 AE7064588 HYDRAULIC LINE SAAB SF340 340B 7860101 EU BLEW OUT A CX7A O OTHER K FLUID LOSS CR CRUISE 1 GL 03 306CE 340B203 GOT A HYD LIGHT ON IN FLIGHT. MAIN PRESS GONE (0 PSI), EMER PRESS 2900 PSI, OUT/INBOARD 2900 BLEW BOLTS BECAUSE WE Weren ’t GETTING PRESS WITH HAND PUMP. LANDED FINE. NO NOSEWHEEL STEERING AFTER LANDING. HAD FLAPS FOR LANDING AND BREAK PRESS URE AFTERWARD. 2 L 7 2 4T RT A52EU 2002040800216 20020408 00216 NM 2002 4 8 UPS02237955 1 20020321 A 2780 HINGE FITTING BOEING 727 72731C 1384011 NM #5 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE:C PITTING CORROSION ON I/B UPPER FLANGE OF #5 LE FLAP CENTER HINGE SUP PORT FITTING NEW HINGE FITTIN G KIT INSTALLED IAW SRM 51-30-02 2 L 7 3 4F A3WE 2002040800217 20020408 00217 WP 2002 4 8 0200929970 1 20020326 A 5750 RIB DOUG DC9 DC931 3022065 WP CRACKED A NWAA O OTHER K FLUID LOSS IN INSP/MAINT 1 GL 01 9334 47247 During Overnight CK. in MSP the #5 leading edge rib was found cracked common to the lower most aft fastener hole . The c rack was .5" long. Repaired per EA 99-189349. 2 L 7 2 4F A6WE 2002040800218 20020408 00218 WP 2002 4 8 0200939610 1 20020312 A 5330 SKIN DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 610NW 47432 During Hck in DHN, crack damage was found at the fwd service door skin at the lower left corner area. Repaired per EA 96 -189244, 2 L 7 2 4F A6WE 2002040800219 20020408 00219 WP 2002 4 8 0200949602 1 20020327 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 602NW 47046 During Hck in ATL, the L/H wing spar revealed corrosion in the lower spar cap at the inbd and outbd attach holes for the flap hinge fitting. A .625 crack was found at the inboard hole. Repaired per EA 96-188409. 2 L 7 2 4F A6WE 2002040800220 20020408 00220 WP 2002 4 8 0200959870 1 20020311 A 5310 SKIN DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 779NC 48101 During Accomplishment of a Hck in ATL, a crack was found on the Aft Pressure Bulkhead skin on hte left side of the aircr aft just above the ventral door cutout. Repaired per EA 98-188225. 2 L 7 2 4F RT A6WE 2002040800221 20020408 00221 WP 2002 4 8 0200969871 1 20020311 A 5310 FRAME DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 780NC 48102 During "M" Check at ATL base a .5" crack was found on the station 389 L17R frame at the longeron to frame location. Repa ired per EA 98-188420. 2 L 7 2 4F RT A6WE 2002040800222 20020408 00222 WP 2002 4 8 0200979875 1 20020319 A 5310 FRAME DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 784NC 48109 During Mck in ATL the left side of the upper cusp sta 200 was found to be damaged by corrosion. Repaired per EA 98-18843 5. 2 L 7 2 4F RT A6WE 2002040800223 20020408 00223 WP 2002 4 8 0200989866 1 20020327 A 5310 LONGERON DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 775NC 47785 During MCK in ATL longeron 29L and #) were found with corrosion between stations 466 and 484. Repaired per EA 98-188429. 2 L 7 2 4F RT A6WE 2002040800224 20020408 00224 WP 2002 4 8 0200999866 1 20020328 A 5310 PRESSURE PANEL DOUG DC9 DC951 3022051 WP CRACKED A NWAA O OTHER K FLUID LOSS IN INSP/MAINT 1 GL 01 775NC 47785 During Mck in ATL a 2.0" crack was found in the flight compartment pressure panelat station 105 x=35. Repaired per EA 98 -188410. 2 L 7 2 4F RT A6WE 2002040800225 20020408 00225 WP 2002 4 8 0201009903 1 20020222 A 5310 FRAME DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 953N 47083 During Mck in ATL, Sta 1076 frame was found cracked at longeron 15L. Repaired per EA 99-185571. 2 L 7 2 4F A6WE 2002040800226 20020408 00226 WP 2002 4 8 0201019937 1 20020306 A 5310 SKIN DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 908H 47517 Aircraft inspection in STL revealed 2 cracks in the airstair door cut out. One crack was .25" and the other was .5". Rep aired per EA 99-185358. 2 L 7 2 4F A6WE 2002040800227 20020408 00227 WP 2002 4 8 0201029903 1 20020213 A 5310 PRESSURE PANEL DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 953N 47083 During Hck in ATL 2 cracks were found on the station 105 pressure panel, X=35rh (1.0") and x=25rh (1.0"). repaired per E A 99-185564. 2 L 7 2 4F A6WE 2002040800228 20020408 00228 WP 2002 4 8 02010399003 1 20020218 A 5310 LONGERON DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 953N 47083 During MCK in ATL, Longeron 23R was found cracked at sta 758. Repaired per EA 99-185561. 2 L 7 2 4F A6WE 2002040800229 20020408 00229 WP 2002 4 8 0201049954 1 20020220 A 5310 PRESSURE PANEL DOUG DC9 DC931 3022065 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 921RW 47164 During HCK in DHN, corrosion damage was found to the RH slant panel lower attach angle. Repaired per EA 99-188363. 2 L 7 2 4F A6WE 2002040800230 20020408 00230 SO 2002 4 8 C2XA02CL087 1 20020329 A 2120 SMOKE EMB 145 EMB145LR 3260212 SO COCKPIT DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 16918 145397 CLE FLIGHT 3738 THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSP ECTED AND FOUND NO DEFECTS. COULD NOT DUPLICATE. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002040800231 20020408 00231 SO 2002 4 8 C2XA02IA084 1 20020403 A 2120 ODOR EMB 145 EMB145LR 3260212 SO COCKPIT DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13903 145479 SDF- DURING ICE TEST THE CREW NOTED A STRONG SMELL OF SMOKE IN THE COCKPIT AND FORWARD CABIN. MAINTENANCE INSPECTED TH E AIRCRAFT AND THE AIRCRAFT WAS RELEASED IAW MEL. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE ICE DETECTION SYSTE M, NO SMOKE SMELL NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002040800232 20020408 00232 NM 2002 4 8 CALA0200163 1 20020401 A 5320 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69602 27315 INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR SUPPORT AT STA 540, RBL 1. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IA W SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002040800233 20020408 00233 NM 2002 4 8 CALA0200165 1 20020402 A 5320 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69602 27315 INSPECTION FOUND FOUR 1 INCH CRACKS IN CABIN FLOOR SUPPORT BETWEEN STA 482B AND 520, BL 0. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002040800234 20020408 00234 NM 2002 4 8 CALA0200166 1 20020402 A 5347 CARGO TRACK BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69602 27315 INSPECTION FOUND LT TIE DOWN TRACK IN AFT CARGO COMPARTMENT CORRODED AT STA 877-947. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002040800235 20020408 00235 WP 2002 4 8 CALA0200182 1 20020406 A 5730 SKIN DOUG DC9 DC982 3022082 WP FLAP VANE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND R/H I/B FLAP O/B VANE LOWER SKIN SURFACE DENTED. THE VANE WAS REMOVED, REPAIRED, AND REINSTALLED IAW SR M 51-30-1. 2 L 7 2 4F A6WE 2002040800236 20020408 00236 WP 2002 4 8 CALA0200183 1 20020406 A 5320 ANGLE DOUG DC9 DC982 3022082 WP L-2 DR JAMB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND L-2 DOOR LOWER FORWARD DOOR JAMB L-ANGLE CORRODED AT STA 1138, 18L. THE SCUFF PLATE WAS REMOVED TO GAIN ACCESS IAW SRM 51-30-1. THE L-2 DOOR WAS REMOVED IAW MM 52-42-00. THE ANGLE AND FITTING WERE REMOVED AND A NEW ANGLE AN D SPLICE WAS INSTALLED IAW EA 9-5310-2-A0945. INSTALLED SCUFF PLATE IAW SRM 51-30-1. THE L-2 DOOR WAS INSTALLED AND RIG GED IAW MM 52-42-00. 2 L 7 2 4F A6WE 2002040800237 20020408 00237 WP 2002 4 8 CALA0200184 1 20020406 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP STA 120 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND UPPER CAP(ANGLE) OF FLOORBEAM CORRODED IN E&E COMPARTMENT OVERHEAD AT STA 120, RBL 15 TO RBL 30. THE AN GLE WAS REMOVED AND A NEW ANGLE AND REPAIR SPLICES WERE INSTALLED IAW SRM 51-10-4. 2 L 7 2 4F A6WE 2002040800238 20020408 00238 WP 2002 4 8 CALA0200185 1 20020406 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CO-PILOT SEAT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND L/H AND R/H FORWARD UPPER CO-PILOT'S SEAT TRACKS CORRODED AND WORN. THE SEAT TRACKS WERE REMOVED AND RE PAIRS WERE INSTALLED IAW SRM 51-30-2, 51-10-3, AND 53-05, FIGURE 92. 2 L 7 2 4F A6WE 2002040800239 20020408 00239 WP 2002 4 8 CALA0200186 1 20020406 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP PILOT SEAT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND R/H AND L/H FORWARD UPPER PILOT'S SEAT TRACKS CORRODED AND WORN. THE SEAT TRACKS WERE REMOVED AND REPAI RS WERE INSTALLED IAW SRM 51-30-2, 51-10-3, AND 53-05, FIGURE 92. 2 L 7 2 4F A6WE 2002040800240 20020408 00240 WP 2002 4 8 CALA0200187 1 20020406 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 110-120 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND SEAT TRACK CORRODED AT STA 110-120, RBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 2002040800241 20020408 00241 WP 2002 4 8 CALA0200188 1 20020406 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 120-148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND CAPTAIN'S I/B SEAT TRACK CORRODED AT STA 120-148, LBL 15. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRA CK WAS INSTALLED IAW SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2002040800242 20020408 00242 WP 2002 4 8 CALA0200189 1 20020406 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 110-120 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND COCKPIT SEAT TRACK CORRODED AT STA 110-120, RBL 15. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51- 30-01. 2 L 7 2 4F A6WE 2002040800243 20020408 00243 EA 2002 4 8 COMA0260231 1 20020404 A 5300 601R3200439 BEAM CNDAIR CL600 CL6002B19 1900309 EA FS333 ELONGATED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 938CA 17458 7046 THE FOUR FASTENER HOLES AT FS 333 AND RBL9 THAT ARE COMMON TO THE FLOORBEAM AND THE TRANSVERSE BEAM ARE ELONGATED.THE DA MAGED AREA WAS CUT OUT AND REPAIR PARTS WERE FABRICATED AND INSTALLED I/A/W WVAC EO 601R-53-3097C. 2 L 7 2 4F RT A21EA 2002040800244 20020408 00244 EA 2002 4 8 COMA0260232 1 20020404 A 5300 6003401717 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FS280 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 938CA 17458 7046 THE FLOOR MEMBER AT FS 280.0 WAS CRACKED 3/4" TO THE RIGHT OF THE FLOOR SUPPORT AT RBL9.TRIMMED OUT THE DAMAGED AREA AND FABRICATED AND INSTALLED REPAIR PARTS I/A/W WVAC EO 601R-53-3098A. 2 L 7 2 4F RT A21EA 2002040800245 20020408 00245 EA 2002 4 8 COMA0260233 1 20020404 A 2750 FCU CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 431CA 7472 FLIGHT 5471 FLAPS FAIL MESSAGE.ADJUSTED THE FECU POTENTIOMETERS. 2 L 7 2 4F RT A21EA 2002041500062 20020415 00062 EA 2002 4 15 COMA0260230 1 20020408 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 13593 7132 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 540CB. REPAIRED IAW 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002040800246 20020408 00246 WP 2002 4 8 DHL2002807521 1 20020326 A 5712 FORMER DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.; N/R 1897 LT. WING L/E FORMER CRACKED .250 @ STA. XFS695.000CORR: STOP DRILLED CRACK I/A/W SRM 57-2-0 FIG.2 - FABRICATED REINFORCING ANGLE( 2024 T3 .063)I/A/W SRM 57-2-0 FIG. 2 - CLEANED TREATED , AND PRIMED ANGLE I/A/W SRM 51-1- 8B - INSTALLED REINFORCING ANGLE I/A/W SRM 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2002040800247 20020408 00247 NM 2002 4 8 2PEA2002V0017 1 20020218 A 5753 BOEING BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -During Q1+Q2 inspection.-RIGHT WING FORE FLAP EXISTING REPAIR FROM WBL227 TO 254 FOUND WITH GOUGE.-Doubler of existing repair replaced IAW SRM 51-10-1, Fig 1, between WBL250 to WBL254, repair accomplished IAW SRM 57-50-4, Fig 1.Note: See A eroman W/O No. 2002-90/1, VAM100 No.055, SDA No. 239SDA002. 2 L 7 2 4F RT A16WE 2002040800248 20020408 00248 NM 2002 4 8 P2EA2002V0019 1 20020215 A 5753 BOEING BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -During Q1+Q2 inspection.-RH WING FORE FLAP AT WSL 479 LOWER SURFACE WITH SEVERAL GOUGES.-R-H wing Fore flap repaired IA W SRM 57-40-4, Fig 1.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0160, SDA No. 239SDA009. 2 L 7 2 4F RT A16WE 2002040800249 20020408 00249 NM 2002 4 8 P2EA2002V0020 1 20020309 A 5330 SKIN BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -During Q1+Q2 inspection.-IMPROPER REPAIR LOCATED AT BS 1000 STR 14L.-Existing repair replaced IAW E.O. No.B737HC53-022/ 02, Dated March 15, 2002, approved with FAA 8110-3 form submited by P.C.LeBar.Note: See Aeroman W/O No. 2002-90/1, VAM10 0 No.0715, SDA No. 239SDA021. 2 L 7 2 4F RT A16WE 2002040800250 20020408 00250 NM 2002 4 8 P2EA2002V0021 1 20020221 A 5330 SKIN BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -During Q1+Q2 inspection.-IMPROPER REPAIR LOCATED AT BS 259 STR 19L.-Existing repair replaced IAW E.O. No.B737HC53-023/0 2, Dated March 15, 2002, approved with FAA 8110-3 form submited by B.R.Frakes.Note: See Aeroman W/O No. 2002-90/1, VAM10 0 No.0714, SDA No. 239SDA022. 2 L 7 2 4F RT A16WE 2002040800251 20020408 00251 NM 2002 4 8 P2EA2002V0022 1 20020220 A 5533 FITTING BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -During Q1+Q2 inspection.-VERTICAL STABILIZER SUPPORT FITTING WITH CRACK AT REAR SPAR CAVITY FIN STA 90.3.-Rudder suppor t fitting repaired IAW E.O. No. B737HC55-007/02, DATED Feb 15, 2002 approved with FAA 8110-3 form, submited by Robert Ma nashi, (DERT-710167-SW).Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0506, SDA No. 239SDA025. 2 L 7 2 4F RT A16WE 2002040800252 20020408 00252 NM 2002 4 8 P2EA2002V0023 1 20020220 A 5752 BOEING BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -During Q1+Q2 inspection.-RH WING AILERON TAB BROKEN NEAR INBD AND OUTBD CENTER HINGE ASSEMBLY.-Repaired cracks IAW E.O. No. B737HC57-012/02, DATED March 08, 2002 approved with FAA 8110-3 form, submited by Robert Manashi, (DERT-710167-SW).N ote: See Aeroman W/O No. 2002-90/1, VAM100 No.0599, SDA No. 239SDA027. 2 L 7 2 4F RT A16WE 2002040800253 20020408 00253 NM 2002 4 8 P2EA2002V0024 1 20020220 A 5753 BOEING BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -During Q1+Q2 inspection.-L-H WING IMB. FORE FLAP WITH UPPER SKIN DELAMINATED.-Repaired IAW E.O. No. B737HC57-006/02, DA TED Feb 27, 2002 approved with FAA 8110-3 form, submited by Robert Manashi, (DERT-710167-SW).Note: See Aeroman W/O No. 2 002-90/1, VAM100 No.0577, SDA No. 239SDA028. 2 L 7 2 4F RT A16WE 2002040800254 20020408 00254 NM 2002 4 8 P2EA2002V0011 1 20020218 A 5311 FRAME BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -During Q1+Q2 inspection.-BS 460 AT STR 26LH FRAME WITH CRACK.-Frame repaired IAW SRM 51-40-3, Fig 1.Note: See Aeroman W /O No. 2002-90/1, VAM100 No.073, SDA No. 239SDA004. 2 L 7 2 4F RT A16WE 2002040800255 20020408 00255 NM 2002 4 8 P2EA2002V0026 1 20020303 A 5532 BOEING BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -DURING Q1 AND Q2 INSPECTION:-RUDDER STA 85 SKIN WITH DENT-REPAIRED IAW EO B737HC57-051/02. APPROVED 8110-3 DTD 03-06-02 BY FAA DER ROBERT MANASHI (DERT-71067-SW)-NOTE: SEE AEROMAN W/O No. 2002-90/1, VAM100 0579, SDA 239SDA030 2 L 7 2 4F RT A16WE 2002040800256 20020408 00256 NM 2002 4 8 P2EA2002V0030 1 20020219 A 5310 SEAT TRACK BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -DURING Q1 AND Q2 INSPECTION:-PAX CABIN BS 380 AND RBL 45.5 SEAT TRACK WITH CORROSION -SEAT TRACK REPAIRED IAW SRM 53-10 -5 FIG. 2-NOTE: SEE AEROMAN W/O No. 2002-90/1, VAM100 0583, SDA 239SDA097 2 L 7 2 4F RT A16WE 2002040800257 20020408 00257 NM 2002 4 8 P2EA2002V0031 1 20020214 A 5242 SKIN BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1 AND Q2 INSPECTION:-E/E COMPARTMENT DOOR WITH NICK ON SKIN EDGES STA 325.18-NICK REPAIRED IAW SRM 737-200 52-00 -3 FIG.5-NOTE: SEE AEROMAN W/O No. 2002-90/1, VAM100 0012, SDA 239SDA112 2 L 7 2 4F RT A16WE 2002040800258 20020408 00258 NM 2002 4 8 P2EA2002V0012 1 20020218 A 5311 FRAME BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -During Q1+Q2 inspection.-BS 420 AT STR 26LH FRAME WITH CRACK.-Frame upper flange repaired IAW SRM 51-40-3, Fig1.Note: S ee Aeroman W/O No. 2002-90/1, VAM100 No.076, SDA No. 239SDA005. 2 L 7 2 4F RT A16WE 2002040800259 20020408 00259 NM 2002 4 8 P2EA2002V0014 1 20020219 A 5311 FRAME BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -During Q1+Q2 inspection.-FWD CARGO COMPARTMENT AT BS 492.4 ATR 24R FRAME WITH CRACK.-Frame repaired IAW SRM 51-40-3, Fi g 1.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.314, SDA No. 239SDA017. 2 L 7 2 4F RT A16WE 2002040800260 20020408 00260 NM 2002 4 8 P2EA2002V0015 1 20020218 A 5311 STRINGER BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -During Q1+Q2 inspection.-INTERNAL FUSELAGE STR 16R WITH CRACK BTW BS 520 AND SCANNING LIGHT BASE.-Scaqnning ligth base at Str 16R-H repaired IAW E.O. No. B737MC53-18/02 & S/B 737-53-1145.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0321, SDA No. 239SDA018. 2 L 7 2 4F RT A16WE 2002040800261 20020408 00261 NM 2002 4 8 P2EA2002V0016 1 20020218 A 5313 STRINGER BOEING 737 73725A 1384481 NM A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 -During Q1+Q2 inspection.-INTERNAL FUSELAGE STR 16L WITH CRACK BTW BS 520 AND SCANNING LIGHT BASE.-Scaqnning ligth base at Str 16L-H repaired IAW E.O. No. B737MC53-18/02 & S/B 737-53-1145.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0322, SDA No. 239SDA019. 2 L 7 2 4F RT A16WE 2002040800262 20020408 00262 NM 2002 4 8 CALA0200167 1 20020403 A 5347 CARGO TRACK BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69602 27315 INSPECTION FOUND RT TIE DOWN TRACK IN FRONT OF AFT CARGO THRESHOLD CORRODED AT STA 767-870. A NEW TRACK SECTION WAS INS TALLED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002040800263 20020408 00263 NE 2002 4 8 CALA0200168 2 20020402 A 7200 CFM563B1 ENGINE BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE NR 2 LEAKING A CALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 14320 39440 23371 721426 SMOKE ENTERED THE COCKPIT AND CABIN AFTER TAKEOFF FROM ORD. ISOLATING THE PACKS DID NOT HELP. THE AIRCRAFT WAS RETURNE D TO ORD WHERE IT LANDED WITHOUT INCIDENT. A BORESCOPE OF THE NR 2 ENGINE HPC SECOND STAGE FOUND THE AREA WET WITH OIL. THE VSV WAS ALSO FOUND TO BE WET WITH OIL. A NR 2 ENGINE CHANGE WILL BE PERFORMED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002040800268 20020408 00268 NM 2002 4 8 DHL2002708004 1 20020330 A 3350 LIGHT BOEING 727 72725 1384006 NM COCKPIT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 708DH 18275 COCKPIT EMERGENCY LIGHTS DO NOT ILLUMINATE IN TEST. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT, OPS CK NORMAL IA W B727 MM 33-50-1. 2 L 7 3 4F A3WE 2002040800269 20020408 00269 WP 2002 4 8 DHL2002804004 1 20020404 A 3230 UPLOCK DOUG DC8 DC873F 302199F WP RT MLG LACK OF LUBE A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 804DH 46124 DURING CLIMBOUT AFTER GEAR RETRACTION DOOR NOT LATCHED LIGHT ILLUMINATED AND RIGHT DOOR UNSAFE LIGHT ON S/O PANEL ILLUMI NATED TOO. ABNORMAL PROCEDURE WAS PERFORMED LANDING GEAR WAS CYCLED AND UPLOCK CHECK PERFORMED FIVE TIMES SPEED WAS KEP T WITHIN LIMITATIONS. CONTACTED FLIGHT CONTROL WHO DIVERTED US TO MIAMI. CLEANED AND LUBED RT GEAR DOOR MECHANISM UPLO CK CLEANED PROX SWITCH, OPS CHECK NORMAL PER M/M 32-60-0. 2 L 7 4 4F RT 4A25 2002040800270 20020408 00270 WP 2002 4 8 DHL2002807508 1 20020322 A 5712 FORMER DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 81797 45990 RIGHT WING L/E - FORMER WITH .250 CRACK IN IT AT STA XFS822.000. STOP DRILLED CRACK IAW 57-2-0 FIG 2, FABRICATED AND IN STALLED DOUBLER IAW 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002040800271 20020408 00271 WP 2002 4 8 DHL2002807510 1 20020322 A 5320 4641324N SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 81797 45990 AFT ACCY COMPT INTERIOR - SPLICE FITTING 2 INCH CRACK AT STA 1690.000 TO 1700.00 L24L. REMOVED CRACKED FITTING AND INST ALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2002040800272 20020408 00272 WP 2002 4 8 GTIA020036 1 20020211 A 3150 WARNING SYSTEM DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A GTIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 23 800NK 49144 FLT 1657 - DTW - GOT TAKEOFF WARNING DURING TAKEOFF ROLE. RETURNED TO GATE. PERFORMED TAKEOFF WARNING TEST OPS CHECKS GOOD IAW MD80 MM 27-00-0. (M) 2 L 7 2 4F A6WE 2002040800273 20020408 00273 WP 2002 4 8 GTIA020126 1 20020224 A 2611 SMOKE DETECTOR DOUG DC9 DC981 3022081 WP LAVATORY FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 810NK 48015 DTW - FOUND LEFT AFT LAVATORY SMOKE DETECTOR TEST PANEL FAILED. OPS CHECK. REMOVED AND REPLACED LEFT AFT SMOKE DETECTO R. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002040800274 20020408 00274 WP 2002 4 8 UPS02837742 1 20020224 A 5320 975494985 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C LONGERON SUPPORT T-ANGLE HEAVILY CORRODED AT STA 1250 BETWEEN L33R AND L34R. REMOVED CORRODED ANGLE P ER SRM 51-1-21. FABBRICATED REPLACEMENT AND INSTALLED PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040800275 20020408 00275 WP 2002 4 8 UPS02837743 1 20020224 A 5313 37585931 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C L34R CRACKED AT STA 1350. REMOVED DAMAGED LONGERON FROM STA 1290 TO STA 1350 PER SRM 51-1-20D. INSTA LLED REPLACEMENT LONGERON IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002040800276 20020408 00276 WP 2002 4 8 UPS02837745 1 20020220 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C STEEL DOUBLER AT UPPER FWD CORNER OF R1 DOOR DOES NOT CONFORM TO SRM. CUT OUT CRACKED AREA. FABRICAT ED AND INSTALLED REPAIR PARTS PER SRM 53-2-0 FIG 14. 2 L 7 4 4F RT 4A25 2002040800277 20020408 00277 WP 2002 4 8 UPS02837746 1 20020225 A 5330 57799157 FINGER DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C FINGER DOUBLER CORRODED BEYOND LIMITS AT STA 1350 L31L TO L31R. FABRICATED AND INSTALLED DOUBLER PER SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2002040800278 20020408 00278 WP 2002 4 8 UPS02837747 1 20020222 A 5313 5758874 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C L7R CRACKED AT STA 520. REMOVED L7R FROM STA 510 TO STA 530 PER SRM 53-2-2 FIG 4C. FABRICATED LONGER ON AND INSTALLED PER SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2002040800279 20020408 00279 WP 2002 4 8 UPS02837748 1 20020224 A 5330 5779915 FINGER DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C FINGER DOUBLER CRACKED AT STA 1329 L31R. FABRICATED AND INSTALLED DOUBLER PER SRM 51-1-21 AND 51-1-20 D. 2 L 7 4 4F RT 4A25 2002040800280 20020408 00280 WP 2002 4 8 ZW0A0202005 1 20020213 A 5230 BRACKET DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT IN THE MID CARGO COMPARTMENT, THE AFT BOTTOM DOOR STOP BRACKET WAS CRACKED INSIDE THE DOOR, ON THE FWD FACE. REMOVED AND REPLACED CRACKED BRACKET WITH NEW PER SRM 51-01, AND SPM 6-70-01. 2 L 7 2 4F A6WE 2002040800281 20020408 00281 WP 2002 4 8 ZW0A0202006 1 20020213 A 5230 BRACKET DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT THE MID CARGO DOOR BOTTOM INBOARD BRACKET WAS CRACKED, LOWER SIDE FOR AFT BOTTOM DOOR STOP. FABRIC ATED NEW BRACKET AND INSTALLED. 2 L 7 2 4F A6WE 2002040800282 20020408 00282 WP 2002 4 8 ZW0A0202202 1 20020221 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9621A 53592 THE FORWARD OVERWING EMERGENCY EXIT LIGHTS, EGRESS LIGHTS AT ROW 17 TO 20, AND FIVE OTHER INDIVIDUAL EGRESS LIGHTS, WERE INOPERATIVE. REPLACED THE BATTERY PACK (P/N 5822-2) FOR THE EMERGENCY LIGHTS, REPLACED THE WIRE HARNESS (P/N 0105606-0 03SMI) BETWEEN ROW 17 AND 18 AND INSTALLED FIVE LAMPS (P/N 7732) THAT HAD FALLEN OUT. 2 L 7 2 4F RT A6WE 2002040800283 20020408 00283 WP 2002 4 8 ZW0A0202203 1 20020215 A 5320 TIE CLIP DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 967TW 53617 DURING CHECK-C MAINT THE LT SIDE VENT BOX UPPER FORWARD STRUCTURAL TIE CLIP WAS FOUND BROKEN. 2 L 7 2 4F RT A6WE 2002040800284 20020408 00284 NM 2002 4 8 ZW0A0202301 1 20020224 A 3350 LIGHT BOEING 767 7673Q8 1385142 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 634TW 28132 THE EGRESS LIGHTS WERE INOPERATIVE ON LEFT SIDE OF CABIN, ROW 4 AND FORWARD. REPAIRED FEEDER CABLE AT ROW 4 USING PINS AND REPLACED ROW 4 LIGHT ASSY. 2 L 7 2 4F RT A1NM 2002040800285 20020408 00285 WP 2002 4 8 ZW0A0202401 1 20020225 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C FOUND LT AFT LAV AT STA 1338 TO 1350, STRINGER 18L TO 17L, LBL 50 TO 56, THE FLOORBEAM FRAME AT FUSELAGE SKIN AREA, WEB HAD CORROSION. REMOVED CORROSION PER SRM 51-10-3. REPLACED DAMAGED WEB SECTION PER 51-70-4. INSTALLED NEW CHORD FITTING. 2 L 7 2 4F A6WE 2002040800286 20020408 00286 WP 2002 4 8 ZW0A0202402 1 20020220 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT THE LEFT SIDE MOST FORWARD CABIN DOOR JAMB, 2 ANGLES HAD CORROSION AT STA 180 TO 200. FABRICATED A ND INSTALLED PER SRM 1-10-02, 1-10-03, 51-30-02, 51-14-01, AND SPM 6-10-01. 2 L 7 2 4F A6WE 2002040800287 20020408 00287 WP 2002 4 8 ZW0A0202403 1 20020222 A 5320 BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 967TW 53617 DURING CHECK-C FOUND AFT ACCY COMPARTMENT BRACKET CRACKED ABOVE RT VENT BOX FWD OF RUDDER TRIM DRUM. DOUBLER FABRICATED PER SRM 53-01, FIG 3 AND 4, PAGE 18. 2 L 7 2 4F RT A6WE 2002040800288 20020408 00288 WP 2002 4 8 ZW0A0202404 1 20020225 A 5320 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 941AS 49925 DURING CHECK-C MAINT FOUND A SUPPORT BRACKET CRACKED, 8 INCHES BELOW THE FLOOR TRACK AT STA 845, LBL 22 INCHES. REPLACE D SUPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 2002040800289 20020408 00289 NM 2002 4 8 AWXA200200315 1 20020324 A 5330 6545800732 SKIN BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 0 0 23627 MCN - MAJOR REPAIR - DURING C-16 CHECK A 3/16" CRACK WAS FOUND ON THE EXTERNAL FUSELAGE SKIN AT THE LOWER AFT CUTOUT OF THE L1 DOOR, BS 338, CONFIRMED BY HFEC. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC INSPECTION, CRACK CONTAINED. F ABRICATED A -26 REPAIR DOUBLER AND -7 REPAIR STRAP AND INSTALLED REPAIR PARTS IAW AWA ER 03-5311-02092-JS1. 2 L 7 2 4F RT A16WE 2002040800290 20020408 00290 NM 2002 4 8 AWXA200200316 1 20020325 A 5310 6545409245 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 0 0 24710 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1 1/2" CRACK WAS FOUND PRESSURE WEB AT BS 664, LBL 34. MAINTENANCE TRIMMED OUT DAMAGED AREA AND REMOVED 2 EACH ATTACH ANGLES, PERFORMED HFEC INSPECTION VERIFYING CRACK WAS CONTAINED, FABRICATED A -6 STIFFNER, -8 DOUBLER, AND -9, -10, -11 FILLERS, AND INSTALLED REPAIR AND ATTACHING PARTS IAW B737-300 SRM -53-60-51, PG. 214-222, FIG. 203. 2 L 7 2 4F RT A16WE 2002040800291 20020408 00291 NM 2002 4 8 AWXA200200317 1 20020405 A 3350 BMS13311122 WIRE BOEING 757 7572S7 1384962 NM SEAT ROW 18 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 0 0 23322 PHX - EEL - DURING INSPECTION SEAT ROW 18 L/H EMERGENCY EXIT PATH LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED LIGH T BULB, DID NOT CORRECT THE PROBLEM, FOUND BROKEN WIRE AT SEAT ROW 18 L/H, REPAIRED BROKEN WIRE PER BOEING SWP 20, OPERA TIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002040900001 20020409 00001 2002 4 9 SWAA020717 4 20020403 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM FWD CABIN DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED C1 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PE R MM. 2 L 7 2 4F RT A16WE 2002040900002 20020409 00002 2002 4 9 SWAA020718 4 20020403 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM AFT ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002040900003 20020409 00003 NM 2002 4 9 SWAA020722 1 20020404 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT END OF EQUIPTMENT COOLING EXHAUST HOLE, BS 378.5 AT LBL 3.5 . REPAIRED SKIN PER BFG ER. 2 L 7 2 4F RT A16WE 2002040900025 20020409 00025 EU 2002 4 9 02095303 1 20020405 A 3397 WIRE JETAIR JETSTM JETSTM4101 1500501 EU CABIN BROKEN A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 303UE 41015 DURING PREFLIGHT INSPECTION, THE CREW NOTED THAT THE AFT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REPAIRED A BROKEN WIRE. AN OPERATIONAL CHECK OF THE EMERGENCY EXIT LIGHT SYSTEM WAS SATISFACTORY AND THE AIRCRAFT WAS R ETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002041000129 20020410 00129 NM 2002 4 10 2002UALA00596 1 20020329 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 931UA 26656 BODY STATION 178 WEB CRACKED AT WL 313 LBL 6.5 UPPER LEFT HAND RADAR MOUNT UPPER OUTBOARD CORNER. MAJOR REPAIR ACCOMPLI SHED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041000130 20020410 00130 NM 2002 4 10 2002UALA00597 1 20020329 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 UPPER LOBE INT FUSELAGE FRAME CRACKED AT FASTENER JUST ABOVE STRINGER 9L AT BODY STATION 847. MAJOR REPAIR ACCOMPLISHED . ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041000131 20020410 00131 NM 2002 4 10 2002UALA00598 1 20020330 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 UPPER LOBE INT FUSELAGE FRAME CRACKED AT FASTENER JUST ABOVE STRINGER 9L AT BODY STATION 887. MAJOR REPAIR ACCOMPLISHED . INSTALLED ANGLE AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041100059 20020411 00059 NM 2002 4 11 2002UALA00599 1 20020330 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 FORWARD GALLEY DOOR CUTOUT FORWARD FRAME STATION 296 CRACKED THROUGH FASTENER HOLE IN INBOARD FLANGE TO RADIUS AT FLOOR LEVEL. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041100060 20020411 00060 NM 2002 4 11 2002UALA00600 1 20020331 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 EXTERNAL FUSELAGE STATION 430 AT STRINGER 22 RIGHT STRINGER IS DENTED BEHIND EXTERIOR SKIN. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE REPAIR AND EXTERNAL DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041100061 20020411 00061 NM 2002 4 11 2002UALA00601 1 20020331 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 EXTERNAL FUSELAGE SKIN DENTED AT STATION 430 STRINGER 20R. MAJOR REPAIR ACCOMPLISHED. EXTERNAL DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041100062 20020411 00062 NM 2002 4 11 2002UALA00602 1 20020330 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT CARGO COMPARTMENT CIRCUMFERENTIAL FRAME AT BODY STATION 1520 LBL 16 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIR ST RAP INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002040900026 20020409 00026 NM 2002 4 9 2002UALA00606 1 20020402 A 5312 DOME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 931UA 26656 AFT PRESSURE BULKHEAD (DOME) DAMAGED BY TOOLING AT RH SIDE JUST BELOW FLOOR, WL 207, BS 1018. MAJOR REPAIR ACCOMPLISHED . DRILL START WAS DRILLED THROUGH THE WEB AND RIVET INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041100070 20020411 00070 NM 2002 4 11 2002UALA00611 1 20020401 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 MID CABIN FLOOR BODY STATION 960-984 RBL 65-72 CREASE BEAM UPPER EXCESSIVE MATERIAL LOSS DUE TO CORROSION REMOVAL. MAJO R REPAIR ACCOMPLISHED. CREASE BEAM WEB REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041100071 20020411 00071 NM 2002 4 11 2002UALA00613 1 20020401 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT CARGO COMP STATION 1480 FUSE FRAME ABOVE STRINGER 22R HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP RE PAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041100072 20020411 00072 NM 2002 4 11 2002UALA00614 1 20020401 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT PIT FRAME STATION 1420 DENTED ABOVE STRINGER 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041100076 20020411 00076 NM 2002 4 11 2002UALA00618 1 20020401 A 5320 INTERCOSTAL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 BODY STATION 1284 RBL 17 INTERCOSTAL CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041100079 20020411 00079 NM 2002 4 11 2002UALA00623 1 20020403 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 AFT CABIN FLOOR SUPPORT IS CORRODED FROM STA 947.5 TO 987.5, RIGHT BL 50. MAJOR REPAIR ACCOMPLISHED. REPLACED Z ANGLE ON CREASE BEAM STA 910 TO 1000, RIGHT BL 50 WL 208. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041100089 20020411 00089 NM 2002 4 11 2002UALA00629 1 20020403 A 5310 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT CABIN DECK PLATE HAS EXCESSIVE MATERIAL LOSS AT STATION 1681 RBL 9.5-RBL 14. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041100096 20020411 00096 NM 2002 4 11 2002UALA00639 1 20020405 A 5210 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 26945 NR 4L PASSENGER DOOR EXTERIOR SKIN DENTED AT EDGE AT LOWER AFT CORNER OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. ROUTED OUT CRACK AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002040900027 20020409 00027 NM 2002 4 9 200200241 1 20020408 A 5330 SKIN BOEING 747 747132 1384882 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 LAP SEAM AT STA 930 TO 950 STR 8 LEFT HAS SURFACE CORROSION AND SKIN EXFOLIATED. OPENED LAP, REMOVED CORROSION, REPAIRE D AREA AND CLOSED LAP PER B747 SRM. 2 L 7 4 4F A20WE 2002040900028 20020409 00028 NM 2002 4 9 2002UALA00588 1 20020326 A 2421 HARNESS BOEING 747 747422 1384935 NM PWA 4090 PW4090 52119 NE NO 3 ENG CHAFED A UALA A H J UNSCHED LANDING DEACTIVATE SYST/CIRCUITS DUMP FUEL J WARNING INDICATION CR CRUISE 1 WP 29 197UA 0 0 26901 727691 GOT MULTIPLE ELECTRICAL PROBLEMS IE. FLASHING LIGHTS INTERMITTENT PFD'S LOSS OF ALL 3 AUTO PILOTS, AUTO THROTTLES ETC. EMERGENCY DECLARED, DUMPED FUEL AND DIVERTED TO HNL. SUPPLEMENTAL DATA UPDATE ACFT LOST AC & DC BUS 3 WHEN THE NO. 3 INT EGRATED DRIVE GENERATOR (IDG) EXPERIENCED AN OVER FREQUENCY CONDITION RESULTING IN ITS AUTOMATIC ISOLATION FROM AC BUS 3 . AC BUS 3 REMAINED ISOLATED WHEN THE NO. 3 BUS TIE BREAKER DID NOT CLOSE AUTOMATICALLY LEAVING NO 3 AC & DC BUSES DEAD . CREW WAS SUCCESSFUL IN MANUALLY RESTORING POWER TO BUS USING ESTABLISHED PROCEDURE.. CAUSE OF PROBLEM WAS FOUND TO BE CHAFED ENGINE HARNESS WIRING. IDG "EXCITER" WIRING INTERMITTENTLY SHORTING TO AN ADJACENT SUPPORT BRACKET, CAUSING I 2 L 7 4 4F 4 F RT A20WE E46NE 2002040900029 20020409 00029 NM 2002 4 9 200200242 1 20020408 A 5310 SHEAR TIE BOEING 747 747132 1384882 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 CORROSION FOUND ON SHEAR TIE AT BOTTOM OF FRAME AT STA 2200 AT LEFT OUTFLOW VALVE. REMOVED OLD SHEAR TIE FABRICATED NEW AND INSTALLED AS PER B747 SRM 51-30-02, SRM 51-20-01 AND SRM 51-30-05. 2 L 7 4 4F A20WE 2002040900030 20020409 00030 NM 2002 4 9 200200243 1 20020408 A 5720 65B116143 SUPPORT FITTING BOEING 747 747132 1384882 NM LT WING CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 479EV 19898 LEFT WING WBL 235, UPPER TRAILING EDGE PANEL SUPPORT TEE CRACKED ABOVE NR 4 FLAP TRACK. REMOVED CRACKED SUPPORT FITTING AND INSTALLED NEW FITTING PER B747 SRM 51-30-02, 51-30-05, 51-30-04 AND SOPM 20-41-02. 2 L 7 4 4F A20WE 2002040900031 20020409 00031 WP 2002 4 9 2002807519 1 20020322 A 5531 RIB DOUG DC8 DC873F 302199F WP VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 81797 45990 VERT STAB L/E INNER RIB CRACKED .500 AT ZFS 108.00. STOP DRILLED CRACK IN VERT STAB L/E INNER RIB AT STA ZFS 108.000 IA W SRM 55-2-0 FIG 2. FABRICATED AND INSTALLED DOUBLER IAW SRM 55-2-0 FIG 2 & 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002040900032 20020409 00032 NM 2002 4 9 PCAA0204044 1 20020401 A 5610 NP15790112 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM COCKPIT CRACKED A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 849EX 14117 337 CREW REPORTED CO-PILOTS WINDSHIELD IS CRACKED. MAINTENANCE REPLACED FIRST OFFICERS WINDSHIELD. OPERATIONAL AND LEAK CHEC K GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002040900033 20020409 00033 NM 2002 4 9 AWXA200200255 1 20020327 A 3350 BR964411 LIGHT BOEING 757 7572S7 1384962 NM CABIN MISSING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 AMS - EEL - DURING C-08 CHECK SEAT ROW 6 LT WAS FOUND TO HAVE A MISSING EMERGENCY ESCAPE PATH LIGHT. MAINTENANCE INSTAL LED 1 WHITE EMERGENCY ESCAPE PATH LIGHT AT ROW 6, OPS CHECK GOOD REF MM 33-51-00 PG 501. 2 L 7 2 4F RT A2NM 2002040900034 20020409 00034 NE 2002 4 9 AWXA200200265 2 20020401 A 7261 SEAL AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 ENGINE LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 629AW 1824 076 PHX - AIR TURNBACK - FLT 0001 - ON CLIMBOUT FROM PHX EN ROUTE TO ORD LT ENGINE OIL PRESSURE INDICATED 300 PSI, AIRCRAFT TURNED BACK TO PHX. MAINTENANCE TROUBLESHOT THE HIGH OIL PRESSURE INDICATION PER AWA ER 26-7920-02091-KL1, THE DIFFEREN TIAL PRESSURE TRANSDUCER WAS REPLACED FOR TROUBLESHOOTING BUT THE READINGS REMAINED THE SAME AS ORIGINAL TRANSDUCER. A SMALL LEAK WAS NOTED AT THE LT ENGINE DE-OILER OUTLET AND A CARBON SEAL WAS REPLACED TO STOP THE LEAK. AS A PRECAUTIONA RY MEASURE THE LT ENGINE NR 4 SCAVENGE VALVE WAS REPLACED IAW AMM 79-23-51-401. OIL PRESSURE WITHIN LIMITS PER AMM 71-0 0-00-991-155A. 2 L 7 2 4F 4 F RT A28NM E311NE 2002042500063 20020425 00063 EU 2002 4 25 AWXA200200307 1 20020406 A 2934 C60AA0062 SENSOR AIRBUS 320 A320231 3930325 EU HYD SYSTEM FAILED A AWXA O OTHER N FALSE WARNING LD LANDING 1 WP 28 635AW 38766 092 EN ROUTE FROM PHX A WARNING FOR GREEN HYD SYS LOW LEVEL APPEARED ON ECAM. FLT CREW REQUESTED EMERGENCY EQUIP STANDBY AT LANDING, ACFT LANDED WITHOUT EVENT. MX REPLACED THE GREEN HYD SYS LOW LEVEL SENSOR. REPLACED WAS THE GREEN HYD SYS DR AIN VALVE, AND THE QTY TRANSMITTER GAUGE. LEAK & OPERATIONAL CHECKS WERE GOOD. VENDOR BENCH TEST & DISASSEMBLY OF LOW L EVEL SWITCH S/N 203 FAILED LEAKAGE AND INSULATION TEST FINDING SKYDROL SATURATION DAMAGE TO THE CONNECTOR AND DRIPSTICK. CONNECTOR, DRIPSTICK, AND CONNECTOR SCREWS WERE ALL REPLACED. SWITCH WAS REPAIRED AND MODIFIED BUILD STANDARD. 2 L 7 2 4F RT A28NM 2002040900035 20020409 00035 WP 2002 4 9 AALA20020149 1 20020214 A 3350 LIGHT DOUG DC9 DC982 3022082 WP EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 458AA 49563 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED RIGHT EXTERIOR OVERWI NG EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040900036 20020409 00036 WP 2002 4 9 AALA20020150 1 20020214 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 TUL - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-671, L2-694 INOPERATIVE. REPLACED EMERGENCY EXIT BAT TERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040900037 20020409 00037 WP 2002 4 9 AALA20020151 1 20020214 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-152, L2-155, L2-175, L2-160 INOPERATIVE. REPLACED EMERGENC Y EXIT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040900038 20020409 00038 WP 2002 4 9 AALA20020152 1 20020214 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-700, L2-701, L2-702, L2-703, AND L2-704 INOPERATIVE. REPLA CED EMERGENCY EXIT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040900039 20020409 00039 WP 2002 4 9 AALA20020157 1 20020217 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 435AA 49453 SEA - DURING OVERNIGHT MAINTENANCE, LEFT AND RIGHT OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED LEFT AND RIGHT OVERWING EMERGENCY EVACUATION LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002040900040 20020409 00040 WP 2002 4 9 AALA20020158 1 20020218 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 510AM 49804 RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH LIGHTING IN VENTRAL STAIRS AFT SIDEWALL INOPERATIVE. REPLACED EMERGE NCY PATH LIGHTING ASSEMBLY IN VENTRAL STAIRS AFT SIDEWALL, SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040900041 20020409 00041 WP 2002 4 9 AALA20020164 1 20020219 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 289AA 49301 AUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT CABIN INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTE RY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002040900042 20020409 00042 NM 2002 4 9 GTIA020021 1 20020204 A 2612 CONTROL UNIT DOUG MD80 MD83 3023681 NM FIRE DETECTION MALFUNCTIONED A GTIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 23 822NK 49392 FLT 1570 - MYR - DURING TAKEOFF AT APPROX 70 KTS, SMOKE DETECTOR LOOP ANNUNCIATOR ILLUMINATED. TAKEOFF ABORTED RIGHT EN GINE LOOP B LIGHT ON. RETURN TO MAINTENANCE. PERFORMED LEAK CHECK OF ALL RIGHT ENGINE BLEED DUCTS, ALSO PERFORMED VISU AL INSPECTION OF RIGHT ENGINE FIRE DETECTOR LOOP AND CONNECTORS. FOUND NO LEAKS OR DEFECTS. REMOVED AND REPLACED RIGHT ENGINE FIRE DETECTOR AMP CONTROL UNIT IAW MD80 MM 26-10-03. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F RT 2002040900043 20020409 00043 WP 2002 4 9 GTIA020094 1 20020217 A 7711 B-NUT DOUG DC9 DC982 3022082 WP NR 1 ENGINE LOOSE A GTIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 23 823NK 48020 DTW - FLT 902 - NR 1 ENGINE 1.23 EPR MAX-ENGINE HEAT ON LOW SPEED ABORT RETURN TO GATE. REMOVED AND REPLACED LEFT EPR X MITTER NO HELP, FOUND LOOSE 'B' NUT ON PIT FLEX LINE ON PYLON, TIGHTEN SAME SYSTEM OPS CHECK OK PER 77-11-02. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 2002040900044 20020409 00044 WP 2002 4 9 GTIA020127 1 20020104 A 7120 BOLT DOUG DC9 DC982 3022082 WP ENGINE MOUNT MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND NR 2 ENGINE FORWARD MOUNT CONE BOLT THROUGH BOLT HAS MISSING ALIGNED BOLT ON ANTI-ROTATION ASSY. REMOVED AN D REPLACED TOP FORWARD CONE BOLT PER MD80 MM 71-20-01. (M) 2 L 7 2 4F A6WE 2002040900045 20020409 00045 WP 2002 4 9 GTIA020128 1 20020222 A 3397 GROUND WIRE DOUG DC9 DC981 3022081 WP CABIN DISCONNECTED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 805NK 48058 FLL - FOUND EMERGENCY EXIT LIGHTS ABOVE L2 DOOR INOPERATIVE. CONNECTED GROUND WIRES FOR EMERGENCY EXIT LIGHTS ABOVE L-2 DOOR. OPS CHECK NORMAL IAW MD-80 MM 33-50-00. (M) 2 L 7 2 4F A6WE 2002040900046 20020409 00046 WP 2002 4 9 GTIA020130 1 20020219 A 7160 LINER DOUG DC9 DC981 3022081 WP NR 1 ENGINE SEPARATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 DTW - FOUND NR 1 ENGINE INLET 6 O'CLOCK POSITION DYNAROHR ACOUSTIC LINER PULLING AWAY. REPAIRED INLET NOSE COWL IAW MD- 80 MM 54-04. (M) 2 L 7 2 4F A6WE 2002040900047 20020409 00047 WP 2002 4 9 GTIA020132 1 20020227 A 2760 LINKAGE DOUG DC9 DC982 3022082 WP SPOILER OUT OF ADJUST A GTIA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 23 603CA 49508 SJU - FLT 770 - SPOILER AURAL WARNING SOUNDED IN T/O CONFIGURATION WHEN THROTTLE ADVANCED, FLAPS 11, SPOILER DISARMED. ADJUSTED PUSHROD LINKAGE ON SPOILER ACTUATION SWITCH IAW MD80 MM 27-60-00. OPS CHECK OK, TAKEOFF AND LANDING MODES NORM AL. (M) 2 L 7 2 4F A6WE 2002040900048 20020409 00048 SO 2002 4 9 C2XA02CL094 1 20020408 A 3350 1317 BULB EMB 135 EMB135ER 3260203 SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27512 145274 DURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY LIGHT.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002040900049 20020409 00049 2002 4 9 GTIA020133 4 20020228 A 2230 RELAY DOUG DC9 DC981 3022081 WP AUTOTHROTTLE SYS FAILED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 810NK 48015 FLT 953 - AFTER TAKEOFF FAST SLOW SPEED FLAG APPEARED ON BOTH CAPTAIN'S AND FO HSI. AUTO THROTTLES DISENGAGED AND WOULD NOT RE-ENGAGE DURING THE FLIGHT A/T DISENGAGE AT ALTITUDE CAPTURE AND AUTO THROTTLES WENT INTO SPEED SEL MODE. REMOVED AND REPLACED RELAY R2-6 IAW MD80 MM 20-50-00. OPS CHECK NORMAL IAW MD80 MM 34-24-00. (M) 2 L 7 2 4F A6WE 2002040900050 20020409 00050 WP 2002 4 9 GTIA020134 1 20020228 A 2760 SPOILER DOUG DC9 DC982 3022082 WP WING MALFUNCTIONED A GTIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 23 603CA 49508 SJU - FLT 770 - ABORTED TAKEOFF, SPOILER CAAWS SOUNDED DURING TAKEOFF ROLL AT 80 KTS, ABORTED TAKEOFF. DEACTIVATED AUTO GROUND SPOILER ACTUATOR AND PLACED INFLIGHT MODE. DISCONNECTED LEFT AND RIGHT GROUND SPOILER CONTROL VALVES, VERIFIED OPERATION OF FLIGHT SPOILERS WHILE GROUND SPOILERS REMAIN RETRACTED. RECONNECTED AND OPS CHECK LT AND RT INBOARD AND OU TBOARD SPOILERS FOUND AUTO GROUND SPOILER ACT EXTENDED. RETRACTED AUTO GROUND SPOILER ACTUATOR SPEED BRAKE AND SPOILERS OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2002040900054 20020409 00054 2002 4 9 GTIA020139 4 20020301 A 3414 INDICATOR DOUG DC9 DC981 3022081 WP COCKPIT MALFUNCTIONED A GTIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 23 805NK 48058 TPA - FLT 638 - DURING TAKEOFF, CAPTAINS AIRSPEED JUMPED TO 110 KNOTS WITH NO FLAGS, F/O'S LESS THAN 80 KIAS. ABORTED A T 80 KNOTS BRAKE TEMP 180 DEGREE. PERFORMED TEST ON CAPTAINS AIRSPEED INDICATOR PER MM 34-13-01 PAGE 203. TESTS GOOD. PERFORMED PITOT TEST ON CAPTAINS AIRSPEED INDICATOR PER MM 34-13-02. TESTS GOOD. (M) 2 L 7 2 4F A6WE 2002040900055 20020409 00055 2002 4 9 GTIA020140 4 20020301 A 2210 4034242934 CONTROL PANEL DOUG DC9 DC981 3022081 WP COCKPIT FAULTY A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 805NK 48058 FLL - FLT 461 - A/P WOULD NOT ENGAGE IN FLIGHT (1 OR 2). REMOVED AND REPLACED GUIDANCE CONTROL PANEL. PERFORMED RTS ON BOTH DFGS COMPUTERS. BOTH SYSTEM. OPS CHECK GOOD IAW MD80 MM 22-01-05. (M) 2 L 7 2 4F A6WE 2002040900056 20020409 00056 2002 4 9 GTIA020141 4 20020302 A 3460 4034241973 COMPUTER DOUG DC9 DC981 3022081 WP COCKPIT FAILED A GTIA O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 819NK 48016 RSW - NR 1 DFGS WENT INOPERATIVE ON SHORT FINAL. NR 2 DFGS WORKS OK. REMOVED AND REPLACED NR 1 DIGITAL FLIGHT GUIDANCE COMPUTER AS REQUIRED IAW MD80 MM CH 22-01-05. PERFORMED RETURN TO SERVICE TEST. RTS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002040900065 20020409 00065 WP 2002 4 9 GTIA020150 1 20020103 A 7120 ISOLATOR DOUG DC9 DC982 3022082 WP ENGINE MOUNT OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - RIGHT ENGINE FORWARD LOWER VIBRATION ISOLATOR ROTATION IND MARKS ARE MISMATCHED. REMOVED RIGHT ENGINE FORWARD LOW ER VIBRATION ISOLATOR IAW MD80 MM 71-20-02. INSTALLED RIGHT LOWER VIBRATION ISOLATOR. (M) 2 L 7 2 4F A6WE 2002040900066 20020409 00066 WP 2002 4 9 GTIA020151 1 20020103 A 7120 ISOLATOR DOUG DC9 DC982 3022082 WP ENGINE MOUNT OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FOUND LEFT ENGINE FORWARD LOWER VIBRATION ISOLATOR ROTATION MARKS ARE MISMATCHED. REMOVED LEFT LOWER VIBRATION ISOLATOR . INSTALLED LOWER LEFT VIBRATION ISOLATOR IAW MD80 MM 71-20-02. (M) 2 L 7 2 4F A6WE 2002040900071 20020409 00071 EU 2002 4 9 YENA200201 1 20020108 A 3260 SENSOR AIRBUS 320 A320232 3930326 EU NLG OUT OF ADJUST A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 505JB 1173 AFTER TAKEOFF LANDING GEAR FAILED TO RETRACT, L/G SHOCK ABSORBER FAULT, AIR RETURN TO JFK, OVERWEIGHT LANDING APPROX 160 ,000 LBS AT 3-400 FPM. ON INSPECTION FOUND FOD (UNSERVICEABLE TAXI LAMP) IN AREA OF SCISSORS LINK CAUSING TARGET FOR EX TENSION TO FAIL, REMOVED FOD, PERFORMED EXTENSION AND RETRACTION TEST PER AMM TASK 32-31-00-501, NLG FAILED TO RETRACT, INSPECTED NOSE STRUT ASSY, FOUND PROX SENSORS 24GA AND 25GA OUT OF ADJUSTMENT. ADJUSTED, OPS CHECK PROX SENSORS. PERFO RMED RETRACTION TEST, OPS CHECK OK. 2 L 7 2 4F RT A28NM 2002040900072 20020409 00072 EU 2002 4 9 YENA200202 1 20020124 A 2520 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU CABIN CONTAMINATED A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 519JB 1398 FLT 107, IAD TO FLL, IN FLIGHT TV C/B'S POPPED. RESET ONCE, GOT SMOKE AND WIRE SMELL AROUND ROWS 14 AND 15 DEF. PULLED C/B'S AND TURNED TV'S OFF. INSPECTED ROWS 14 AND 15 LIVE TV COMPONENTS. NO DAMAGE NOTED, REPLACED SEB AT ROWS 15DEF A ND SEAT TO SEAT CABLE BETWEEN ROWS 15 TO 14 IAW LIVE TV MM 23-39-00, OPS CHECK OK. ENGINEERING AND MANUFACTURER INVESTI GATION FOUND FAILURE OF SEB (SEAT ELECTRONIC BOX) DUE TO MOISTURE CONTAMINATION. 2 L 7 2 4F RT A28NM 2002040900073 20020409 00073 2002 4 9 YENA200205 4 20020226 A 2565 D30665105 SLIDE AIRBUS 320 A320232 3930326 EU R2 DOOR UNSERVICEABLE A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 509JB 6174 1989 1270 R2 DOOR EMERGENCY SLIDE INDICATED LOW PRESSURE. REMOVED AND REPLACED R2 DOOR SLIDE IAW AMM CHAP 25-62-44. 2 L 7 2 4F RT A28NM 2002041100086 20020411 00086 NM 2002 4 11 02FDEA00233 1 20020325 A 5241 WEB BOEING 727 727277 138408S NM GALLEY DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 FWD GALLEY DOOR INTERNAL WEB ABOVE CENTER PRESSURE PANEL UPPER SURFACE OF WEB HAS CORROSION. REMOVED AND REPLACED WEB P ER SRM 51-20-1, 51-10-1. 2 L 7 3 4F RT A3WE 2002040900074 20020409 00074 NM 2002 4 9 02FDEA00235 1 20020408 A 5330 SKIN BOEING 727 727277 138408S NM WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 N 279 FASTENERS AROUND DRAIN HOLE 11" ABOVE LH AFT NLG DOOR WORN. ** S/D ** COMING 2 L 7 3 4F RT A3WE 2002041700079 20020417 00079 NM 2002 4 17 02FDEA00236 1 20020405 A 5310 SHEAR TIE BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FRAME TO SKIN SHEAR TIE CRACKED AT BS 990, L29L. REMOVED AND REPLACED PARTS FOR SHEAR TIE PER SRM 51-10-4 FIG 13. 2 L 7 3 4F A3WE 2002040900084 20020409 00084 WP 2002 4 9 ABXA010815 1 20020401 A 5300 5614272503 CONTROL COLUMN DOUG DC9 DC931 3022065 WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 CAPTAIN'S CONTROL COLUMN SHOWED CRACK INDICATIOIN AND WAS BLENDED BEYOND LIMITS. REPLACED CAPTAIN'S CONTROL COLUMN IAW D C-9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 2002040900085 20020409 00085 EA 2002 4 9 COMA0260234 1 20020405 A 2720 6229820008 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 712CA 3081 7244 FLIGHT 5635 UNCOMMANDED RUDDER OSCILLATIONS.REPLACED THE #2 DCU. 2 L 7 2 4F RT A21EA 2002040900086 20020409 00086 EA 2002 4 9 COMA0260235 1 20020405 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 710CA 4057 7241 FLIGHT 5297 FLAPS FAILED AT 0 DEGREES.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2002040900087 20020409 00087 EA 2002 4 9 COMA0260236 1 20020405 A 7830 1267587 POWER UNIT CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 987CA 10096 7199 FLIGHT 5931 R/H THRUST REVERSER UNLOCKED MESSAGE DURING T/O.REPLACED THE PDU. 2 L 7 2 4F RT A21EA 2002040900088 20020409 00088 EA 2002 4 9 COMA0260238 1 20020406 A 2750 853D10012 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA R/H BINDING A COMA O OTHER S AFFECT SYSTEMS DE DESCENT 1 SO 01 713CA 8531 7245 FLIGHT 5234 FLAPS FAILED MESSAGE. R/H OUTBD FLAP IS TWISTED.REPLACED R/H OUTBD FLAP ACTUATORS, 2 L 7 2 4F RT A21EA 2002041500063 20020415 00063 EA 2002 4 15 COMA0260237 1 20020405 A 2752 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 713CA 13862 7245 FLIGHT 5393 FLAPS FAIL MESSAGE. REPLACED THE LT INBOARD FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 2002040900089 20020409 00089 2002 4 9 GLBA2002045 4 20020406 A 3400 066306200 ALTIMETER BEECH 1900 1900D 1154162 CE #1 INACCURATE A GLBA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 NM 03 202GL 1060 UE202 CAPTAINS ALTIMETER ALTITUDE INDICATION OFF, REPLACED ALTIMETER OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2002040900090 20020409 00090 2002 4 9 GLBA2002047 4 20020407 A 3400 ALTIMETER BEECH 1900 1900D 1154162 CE #1 INACCURATE A GLBA O OTHER I FLT. ATTITUDE INST. CR CRUISE 1 NM 03 100UX 990 UE100 CAPTAINS ALTIMETER INDICATION OFF, REPLACED ALTIMETER OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2002040900091 20020409 00091 EU 2002 4 9 QXEA0200542 1 20020404 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 494US * 500 11167 PDX- AFT WING/BELLY FAIRING EVACUATION LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002040900092 20020409 00092 WP 2002 4 9 MWEA020210 1 20020408 A 5321 995792713 PANEL DOUG DC9 DC932 3022066 WP STATION 598 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 REMOVED CABIN FLOOR PANEL B-5 TO FACILITATE OTHER MAINTENANCE. -- FORWARD END OF PANEL IS DAMAGED. FABRICATED NEW SKI N AND REINSTALLED CABIN FLOOR PANEL. 2 L 7 2 4F A6WE 2002040900093 20020409 00093 WP 2002 4 9 MWEA020211 1 20020408 A 5313 591142397 LONGERON DOUG DC9 DC932 3022066 WP STATION 945 BLOWN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 AFT CARGO COMPARTMENT HAS A LONGERON BLOWN OUT IN THE CENTER OF LONGERON 23 LEFT AT STATION 945. -- FABRICATED AND INS TALLED STRAP. 2 L 7 2 4F A6WE 2002040900094 20020409 00094 WP 2002 4 9 MWEA020212 1 20020408 A 5320 59145581 DOUBLER DOUG DC9 DC932 3022066 WP STATION 965 BLOWN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 AFT CARGO COMPARTMENT DOUBLER AROUND THE SUGAR SCOOP IS BLOWN OUT ON THE BOTTOM AFT AREA AT STATION 965 ABOVE LONGERON 2 2 LEFT. -- REMOVED DOUBLER. DRILLED UP AND TRIMMED DOUBLER TO FIT IAW SRM 51-10-4 DAC DRAWING 5914558. INSTALLED DOUBL ER. 2 L 7 2 4F A6WE 2002040900095 20020409 00095 WP 2002 4 9 MWEA020213 1 20020408 A 5230 99576644 INTERCOSTAL DOUG DC9 DC932 3022066 WP FWD CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FORWARD CARGO DOOR, INTERCOSTAL CRACKED, LOWER AFT AREA OF DOOR. -- REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F A6WE 2002040900096 20020409 00096 WP 2002 4 9 MWEA020219 1 20020408 A 5320 99124533 WEB DOUG DC9 DC932 3022066 WP FWD CARGO DOOR MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FORWARD CARGO DOOR JAMB WEB AND FRAME AT 427 HAS A DOUBLE DRILLED HOLE BETWEEN LONGERON 29 RIGHT AND LONGERON 28 RIGHT. -- FABRICATED AND INSTALLED REPAIR STRAP AND WEB REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002040900097 20020409 00097 WP 2002 4 9 MWEA020221 1 20020408 A 5320 99115243 FORMER DOUG DC9 DC932 3022066 WP STATION 237 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FORMER AT STATION 237 LONGERON 18 LEFT TO 17 LEFT IS CRACKED. -- FABRICATED AND INSTALLED SHIM TO ACHIEVE EDGE DISTANC E. 2 L 7 2 4F A6WE 2002040900098 20020409 00098 WP 2002 4 9 MWEA020223 1 20020408 A 5320 591015891 WEB DOUG DC9 DC932 3022066 WP AFT CARGO DOOR OUT OF TOLERANCE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 REMOVAL AFT CARGO DOOR JAMB LOWER INNER WEB TO FACILITATE OTHER MAINTENANCE. -- OLD WEB FOUND OUT OF LIMITS. INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2002040900100 20020409 00100 NM 2002 4 9 AWXA200200325 1 20020331 A 5313 BAC1498157 STRINGER BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 0 0 24710 MCN - MAJOR REPAIR - DURING C-12 CHECK A CRACK WAS FOUND ON STRINGER 16 ON CABIN L/H SIDE AT BS 500C+5, JUST FORWARD OF LIGHT. MAINTENANCE REMOVED DAMAGED END OF STR 16, FABRICATED A REPAIR CHANNEL AND SHIM, AND INSTALLED REPAIR PARTS IAW A WA ER 03-5312-02092-SS4. 2 L 7 2 4F RT A16WE 2002040900101 20020409 00101 NM 2002 4 9 AWXA200200326 1 20020331 A 5313 BAC1498157 STRINGER BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 0 0 24710 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/2" CRACK WAS FOUND ON STRINGER 16 ON CABIN L/H SIDE AT BS 500C+16", JUST AFT OF LIGHT. MAINTENANCE REMOVED DAMAGED END OF STR 16, FABRICATED A REPAIR CHANNEL AND SHIM, AND INSTALLED REPAIR PARTS IA W AWA ER 03-5312-02092-SS4. 2 L 7 2 4F RT A16WE 2002040900102 20020409 00102 NM 2002 4 9 AWXA200200327 1 20020404 A 3350 172160 CONNECTOR BOEING 737 73733A 1384673 NM BS 627.5 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 0 0 23627 MCN - EEL - DURING C-16 CHECK THE R/H OVERWING HATCH LOWER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE R/H OVERWING HATCH LOWER EMERGENCY EXIT LIGHT CONNECTOR IAW BOEING SWPM 20-42-01, PG. 1-6, OPERATION AL CHECK WAS GOOD IAW T/C A1C33006. 2 L 7 2 4F RT A16WE 2002040900103 20020409 00103 2002 4 9 RAIA00204116 4 20020402 A 2340 ACP2531 AUDIO PANEL AEROSP ATR42 ATR42300 8680920 EU INOPERATIVE A RAIA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 03 424TE 5452 66 124 5522-STL- #1 COMM INOP, INTERCOM SCRATCHY. MAINTENANCE REMOVER AND REPLACED ACM AUDIO PANEL, OPS CK OK. 2 H 7 2 4T RT A53EU 2002040900104 20020409 00104 SO 2002 4 9 RAIA00204117 1 20020403 A 3250 3085701003 MANIFOLD EMB 145 EMB145 3260210 SO NOISY A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 805HK 6816 145096 5302-STL- NOSE WHEEL STEERING MAKES NOISE. MAINTENANCE REMOVED AND REPLACED THE STEERING MANIFOLD, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002041000001 20020410 00001 NM 2002 4 10 AUS20020261 1 20020318 A 2780 256A22257 PIPE BOEING 737 737* NM GE CFM56 CFM567B24 NE SLATS WRONG PART W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) HYDRAULIC PIPES AND BRACKETS LOCATED IN AREA OF NR 8 LEADING EDGE WERE INCORRECT PARTS. PIPE WORN THROUGH BY STRU CTURE WHEN SLATS RETRACTED. UNAPPROVED PART. MANUFACTURING ERROR. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002041000004 20020410 00004 NM 2002 4 10 CA020308010 1 20020129 A 5532 657094728 PANEL BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE RT WING SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FLAPS EXTENDED FOR SERVICE CHECK INSPECTION. UPON RETRACTION RT CLOSURE PANEL AT INBOARD FLAPS HUNG UP AT 10 UNITS .FOUND RT INBOARD CLOSURE PANEL SHEARED CAUSING FLAPS TO JAM. CLOSURE PANEL REMOVED. AIRCRAFT OPERATED PER CDL 57-52-01 . AIRCRAFT FERRIED FOR SCRAPPING PROCESS. OPERATIONAL LIFE ENDED AT DESTINATION. 2 L 7 2 4F 4 F A16WE E2EA 2002041000008 20020410 00008 EA 2002 4 10 CA020311005 1 20020308 A 5524 C2TE67 HINGE PIN C2TE1A DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE ELEVATOR LOOSE W A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CA (CAN) PILOT REPORTED ELEVATOR STICKING IN FLIGHT AND RETURNED TO POINT OF DEPARTURE. UPON INSPECTION IT WAS FOUND THAT L T ELEVATOR TRIM TAB HINGE PIN HAD WORKED OUT AND WAS RUBBING AGAINST TAILCONE. HINGE PIN WAS PUSHED BACK IN AND LOCKWIRE D. AIRCRAFT WAS THEN RETURNED TO SERVICE. 1 H 7 1 3R 3 R A806 5E1 2002041000018 20020410 00018 EU 2002 4 10 CA020315004 1 20020225 A 2910 AE2463921J0227 LINE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE HYD SYSTEM LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CA (CAN) AIRCRAFT HAD A COMPLETE LOSS OF GREEN HYDRAULIC SYSTEM FLUID AND PRESSURE IN FLIGHT OVER WASHINGTON STATE. FLIGHT DIVERTED TO VANCOUVER. PTU GREEN PRESSURE FLEX LINE FOUND LEAKING. FLEX LINE REPLACED AND SYSTEM LEAK CHECKED SERVICEABL E. 2 L 7 2 4F 4 F RT A28NM E29NE 2002041000022 20020410 00022 NM 2002 4 10 CA020315008 1 20020302 A 5610 141T480150 WINDSHIELD BOEING 767 767333 1385301 NM PWA 4060 PW4060 52119 NE COCKPIT FAILED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 93092H7352 (CAN) FIRST OFFICER WINDSHIELD SHATTERED IN FLIGHT, AIRCRAFT RETURNED TO HEATHROW. REPLACED WINDSHIELD AND HEAT CONTRO LLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041000025 20020410 00025 NE 2002 4 10 CA020315012 2 20020314 A 7297 CONNECTOR AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211TRENT77 NE NR 2 ENGINE CONTAMINATED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) IN CRUISE FROM MANCHESTER NR 2 ENGINE PARAMETERS FLUCTUATED & TGT PEGGED VERY HIGH, THE THROTTLE RETARDED, SAME F LUX, ENGINE PUT ON N1 MODE, PARAMETERS STABILIZED EXCEPT FOR TGT. THROTTLE ADVANCED & ALL PARAMETERS STARTED TO FLUCTUAT E AGAIN&TGT FLUCTUATED FROM 400 TO 1000 DEGS C, THROTTLE RETARDED&TGT STAYED SAME & ECAM INDICATED ENGINE SHUTDOWN, WHIC H LED TO IFSD. MAINT FOUND CONNECTOR CONTAMINATED & CLEANED IT & REPLACED EEC FOR PRECAUTIONARY MEASURES. EEC & FADEC T EST C/OUT SERVICEABLE IAW MM TASK 73-21-00-710-812 & 813. MAINT ALSO VISUALLY INSP ALL NR 2 ENGINE PYLON ELECT. CONNECTI ONS FOR CONDITION AND SECURITY IAW MM 70-50-02-902-801 2 L 7 2 4F 4 F RT A46NM E39NE 2002041000035 20020410 00035 WP 2002 4 10 UPS02837623 1 20020212 A 5755 RIB DOUG DC8 DC871F 302199D WP SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 TRAILING EDGE RIB ON O/B END IS CRACKED BY CUT-OUT FOR BOLT ACCESS. REMOVED CRACKED WEB IAW DC8 SRM 51-1-24 & REMOVED SPOILER ATTACH IAW DC8 SRM 51-1-20 D & 51-1-21 LOCATED & DRILLED NEW SPOILER ATTACH FITTING IAW DC8 SR M 51-1-24 INSTALLED NEW WEB T/E INTERCOSTAL, CLOSING INTERCOSTAL. 2 L 7 4 4F RT 4A25 2002041000036 20020410 00036 WP 2002 4 10 UPS02837709 1 20020212 A 5755 WEB DOUG DC8 DC871F 302199D WP SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 TRAILING EDGE RIB ON O/B END IS CRACKED BY CUT OUT FOR BOLT ACCESS. REMOVED CRACKED WEB IAW DC8 SRM 51-1-20D & 51-1-21. LOCATED AND DRILLED NEW WEB IAW DC8 SRM 51-1-24. REMOVED SPOILER ATTACH FITTING IAW DC8 SRM 51-1-2 0D, 51-1-21. LOCATED DRILLED NEW SPOILER ATTACH FITTING IAW 51-1-24, INSTALLED. 2 L 7 4 4F RT 4A25 2002041000037 20020410 00037 WP 2002 4 10 UPS02837751 1 20020220 A 5320 3755862505 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED O/B AT L28L STA 1180. REMOVED CRACKED Z-FITTING. INSTALLED FITTING AND SPLICES IAW DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2002041000038 20020410 00038 WP 2002 4 10 UPS02837754 1 20020303 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:N/A, A/C FAILS STANDBY POWER CHECK (NO EMERGENCY LIGHTS). REPLACED EMERGENCY BATTERY PACK, EMERGENCY LI GHTS OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2002041000039 20020410 00039 WP 2002 4 10 UPS02837768 1 20020222 A 5310 5750985 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C CRACK DETECTED BY XRAY AT UPPER AFT CORNER OF L2 DOOR FRAME APPROX STA 1657. REMOVED DOUBLERS PER SRM 51-1-21 AND 51-1-20D. LOCATED AND REMOVED CRACKED FILLER BETWEEN SKIN AND DOUBLER. NDT C/W PER SPM 06-10-01.00 1 NO C RACKS NOTED ON SKIN OR DOUBLER. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-2-0 FIG 18 & DWG 4751734-1. 2 L 7 4 4F RT 4A25 2002041000040 20020410 00040 WP 2002 4 10 UPS02837770 1 20020226 A 5313 S25972423 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C LOWER FUSELAGE SKIN BULGING AT L36, STA 380 TO 400. REMOVED SPLICE FITTING AT L36, STA 380 TO 400. R EMOVED CORROSION ON L36 PER SRM 51-1-8. NO CORROSION FOUND ON SKIN. NDT REVEALED CRACK ON L36 FROM STA 390-394. FABRI CATED AND INSTALLED REPLACEMENT LONGERON SECTION PER SRM 53-4-1 FIG 28. INSTALLED NEW SPLICE FITTING. 2 L 7 4 4F RT 4A25 2002041000041 20020410 00041 WP 2002 4 10 UPS02837774 1 20020220 A 5320 3755843501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED O/B OF L35R STA 1180. REMOVED CRACKED FITTING, FABBED SPLICES FOR F ITTING REPAIR AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, 53-2-0 NOTE 17. 2 L 7 4 4F RT 4A25 2002041000042 20020410 00042 WP 2002 4 10 UPS02837775 1 20020226 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED I/B OF L34R AT STA 1200. INSTALLED NEW FITTING AND SPLICES IAW DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2002041000043 20020410 00043 WP 2002 4 10 UPS02837802 1 20020308 A 2910 HYDRAULIC LINE DOUG DC8 DC871F 302199D WP HYD SYSTEM FAILED A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 705UP 45949 INSPECTION TYPE:N/A, HYD FAILURE IN FLIGHT. EMERGENCY DECLARED. ON CLIMBOUT LOSS OF HYDRAULIC FLUID DOWN TO AUX QUANTI TY POSITION. R&R MS ON AILERON RETURN LINE I/B RT WING BEHIND O/B FALSE PANEL. RAN NR 2 & 3 ENG, ALL SYS RAN AND NO LE AKS NOTED. REMOVED AND REPLACED NR 2 ENG HYD PUMP, REMOVED AND REPLACED HYD FILTER PUMP CASE DRAIN. BLEED AIR FROM SYS TEM PUMP PRESS CHECK OK. 2 L 7 4 4F RT 4A25 2002041000044 20020410 00044 2002 4 10 UPS02M37560 4 20020204 A 2565 60289117 SLIDE DOUG MD11 MD11F 3023600 NM ENTRY DOOR DEPARTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP INSPECTION TYPE:N/A RT FWD ENTRY DOOR ESCAPE SLIDE DEPLOYED. REMOVED AND REPLACED R1 EVACUATION SLIDE/RAFT ASSY IAW MM 25-61-01. 2 L 7 3 4F RT A22WE 2002041000045 20020410 00045 NM 2002 4 10 VNAA0203001 1 20020302 A 3010 001B552A1512000 HEATER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ELEVATOR FAILED A VNAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 440JS 643 3058 OVER RIC, THE CAPTAIN CONTACTED MAINTENANCE CONTROL WITH A ELEVATOR HORN HEAT PROBLEM. FLIGHT 4005 DIVERTED TO PIT WHER E MAINTENANCE REPLACED THE ELEVATOR HORN HEAT MAT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 55-00-00. OPERATIONAL C HECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002041000046 20020410 00046 NM 2002 4 10 VTZA02043408 1 20020211 A 3350 BATTERY PACK DORNER DO32 DO328300 NM CABIN DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 408FJ DURING MAINTENANCE INSPECTION EMERGENCY ESCAPE FLOOR PATH LIGHT WAS OUT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BATTERY PACK AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002041000047 20020410 00047 NM 2002 4 10 VTZA02043427 1 20020211 A 3350 BATTERY PACK DORNER DO32 DO328300 NM CABIN DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 427FJ DURING MAINTENANCE INSPECTION EMERGENCY ESCAPE FLOOR PATH LIGHT WAS OUT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BATTERY PACK AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002041000048 20020410 00048 NM 2002 4 10 VTZA02060408 1 20020301 A 3350 PANEL DORNER DO32 DO328300 NM CABIN FAULTY A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 408FJ DURING INSPECTION, EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE 33VE PANEL. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002041000049 20020410 00049 EU 2002 4 10 VTZA02063307 1 20020304 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU EXTERIOR DEFECTIVE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 307UE 41021 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT FORWARD EXTERIOR EMERGENCY EXIT LIGHT WAS DIM. MAINTENANCE P ERSONNEL REMOVED AND REPLACED THE LAMP IN THE RT FORWARD EXTERIOR EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISF ACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002041000050 20020410 00050 EA 2002 4 10 VTZA02064657 1 20020305 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 657BR 7491 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT A SECTION OF THE EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MA INTENANCE PERSONNEL REMOVED AND REPLACED AN EMERGENCY FLOOR TRACK LIGHTING LAMP STRIP. AN OPERATIONAL CHECK WAS SATISFA CTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002041000051 20020410 00051 EA 2002 4 10 VTZA02076647 1 20020317 A 2611 SMOKE WARNING CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FALSE ACTIVATION A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 647BR DURING INITIAL CLIMB OF FLT 7187, CREW RECEIVED A SMOKE - TOILET WARNING. AIRCRAFT PERFORMED AN AIR-RETURN TO DEPARTURE STATION, LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED A/C WITH NO EVIDENCE OF SMOKE OR FIRE. PERFORMED OPS CHECK O F LAV SMOKE DETECTOR. NO FAULTS NOTED. RAN A/C WITH PACKS ON FULL HEAT IN BOTH AUTO & MANUAL. UNABLE TO DUPLICATE FAU LT. A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002041000052 20020410 00052 EU 2002 4 10 XEA0200238 1 20020205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - FUSELAGE CABIN FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 23. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGU RE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002041000053 20020410 00053 EU 2002 4 10 XNOA01034 1 20020208 A 3260 SWITCH AIRBUS 300 A300B4203 3930306 EU NLG LOOSE A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 473AS 203 ON TAKEOFF GEAR WOULD NOT RETRACT. PERFORMED CHECK LIST. WOULD NOT RETRACT. OVERWEIGHT LANDING NOT FACTOR. CLEANED A ND RESECURED NOSE GEAR CENTERING SWITCH. C/P OPS CHECK NORMAL ON GEAR SWING IAW A300 MM 32-30-00. 2 L 7 2 4F RT A35EU 2002041000054 20020410 00054 2002 4 10 XNOA01036 4 20020208 A 2350 CONTROL UNIT AIRBUS 300 A300B4203 3930306 EU E/E BAY MALFUNCTIONED A XN0A A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 23 224KW 073 POSSIBLE STUCK MIC ON NR 1 COM & NR 2 MIC INTERMITTENTLY WILL NOT TRANSMIT. CLEANED AND RE-RACKED AUDIO INTEGRATING UNI T. OPS CHECKS GOOD IAW A300 MM 23-21-00. 2 L 7 2 4F RT A35EU 2002041000055 20020410 00055 EU 2002 4 10 XNOA01037 1 20020209 A 3230 DAMPER AIRBUS 300 A300B4203 3930306 EU LANDING GEAR LOW A XN0A O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 473AS 203 THREE TRIES TO GET GEAR RETRACTED OUT OF DENVER. INSPECTED LANDING GEAR. FOUND PITCH DAMPERS NITROGEN CHARGE LOW ALL 4. SERVICED PITCH DAMPERS IAW A300 MM 12-12-32. RECHECKED PRESS AFTER 48 HRS. NO DEFECTS NOTED. LUBED LANDING GEAR IAW A300 MM 12-22-32. REMOVED AND REPLACED LANDING GEAR NORMAL CONTROL MICROSWITCH UNIT AND PERFORMED TEST IAW A300 MM 32- 31-11. SYS OPS CHECKED GOOD. NO DEFECTS NOTED. CLEANED PROXIMITY SWITCHES IAW A300 MM 32-00. 2 L 7 2 4F RT A35EU 2002041000056 20020410 00056 EU 2002 4 10 XNOA01038 1 20020222 A 2710 CONNECTOR AIRBUS 300 A300B4203 3930306 EU AILERON LOOSE A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 474AS 219 AFTER TAKEOFF LT LO SPEED AILERON INDICATION SHOWS NOT DISCONNECTED. CONNECTED LOOSE CONNECTOR AT LT LO SPEED AILERON D ISCONNECT ACTUATOR. OPS CHECKS GOOD ON GROUND AND FLT MODE, IAW A300 MM 27-11-00. 2 L 7 2 4F RT A35EU 2002041000057 20020410 00057 2002 4 10 YENA200203 4 20020215 A 2330 ODOR AIRBUS 320 A320232 3930326 EU CABIN DETECTED A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 533JB 1652 FLT 58, PBI TO JFK, IN FLIGHT, ELECTRICAL ODOR COMING FROM SEAT ROW 24ABC, PULLED LIVE TV CB'S. REMOVED AND REPLACED 24 B SEB IAW LIVE TV MM 23-39-00 PRECAUTIONARY, OPS CHECK OK. 2 L 7 2 4F RT A28NM 2002041000058 20020410 00058 NM 2002 4 10 ZW0A0201202 1 20020126 A 4920 380029816 APU BOEING 757 757231 1384950 NM APU BAY MALFUNCTIONED A ZW0A K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 13 720TW 30319 HEAVY OILY SMELL REPORTED FROM THE LEFT AIR CONDITIONING SYSTEM ON TAKEOFF AND DESCENT BELOW 5000 FEET. ACCOMPLISHED CH ECKS AND RESULTS NEGATIVE. RECIRCULATION SYSTEM FILTERS WERE CLEAN. ACCOMPLISHED PACK BURN OUT. AIRCRAFT FERRIED TO S TL FOR FURTHER WORK. REMOVED AND REPLACED APU. 2 L 7 2 4F RT A2NM 2002041000059 20020410 00059 WP 2002 4 10 ZW0A0201501 1 20020203 A 2120 SMOKE DOUG DC9 DC982 3022082 WP COCKPIT DETECTED A ZW0A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 13 940AS 49825 IN DESCENT ENGINE ANTI-ICE WAS TURNED ON AND CREW NOTICED SOME HAZE. TURNED OFF ENGINE ANTI-ICE AND HAZE DISSIPATED. A CCOMPLISHED NUMEROUS PRECAUTIONARY CHECKS AND NO PROBLEM FOUND. CHANGED THE WATER SEPARATORS AND ACCOMPLISHED A PACK BU RN OUT. 2 L 7 2 4F A6WE 2002041000060 20020410 00060 WP 2002 4 10 ZW0A0202204 1 20020214 A 3211 TRUNNION DOUG DC9 DC982 3022082 WP LT MLG CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT IN THE LT WHEEL WELL, FOUND CRACK IN LT GEAR SUPPORT CASTING ABOVE THE LT INBOARD FLAP TRACK, AND A BOVE THE LT FLAP BUSS CABLE BRACKET. REPAIRED GEAR SUPPORT CASTING PER ARA 18090. 2 L 7 2 4F A6WE 2002041000061 20020410 00061 NM 2002 4 10 AWXA200200308 1 20020406 A 2932 501310000 PRESSURE SWITCH AIRBUS A319 A319132 3930340 NM NR 1 ENGINE CRACKED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 805AW 1049 LAX - ABORTED TAKEOFF - FLT 0694 - AT APPROXIMATELY 60 KTS ON TAKEOFF ROLL OUT OF LAX BOUND FOR CMH RECEIVED GREEN HYDRA ULIC SYSTEM NR 1 ENGINE PUMP LOW PRESSURE INDICATION, T/O WAS REJECTED AND AIRCRAFT RETURNED TO GATE. AT GATE MAINTENAN CE FOUND THE NR 1 ENGINE HYDRAULIC PRESSURE SWITCH CRACKED, THE SWITCH WAS REMOVED AND REPLACED IAW AMM 29-11-17-000-010 , OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002041000063 20020410 00063 EU 2002 4 10 AWXA200200309 1 20020306 A 5310 D53480020343 PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 YWG - MAJOR REPAIR - DURING C-08 CHECK A 6 INCH CRACK WAS FOUND ON THE RT AFT SIDE OF THE R2 DOOR SHEAR PLATE. MAINTENA NCE REMOVED SHEAR PLATE, FABRICATED A NEW SHEAR PLATE AND INSTALLED REPAIR IAW SRM 51-42-11 PG 1, SRM 51-72-11 PG 1 & 2. 2 L 7 2 4F RT A28NM 2002041000064 20020410 00064 EU 2002 4 10 AWXA200200310 1 20020306 A 5310 D53480020342 PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 YWG - MAJOR REPAIR - DURING C-08 CHECK A 2 INCH CRACK WAS FOUND ON THE LT AFT L2 DOOR SHEAR PLATE. MAINTENANCE REMOVED SHEAR PLATE, FABRICATED A NEW SHEAR PLATE AND INSTALLED REPAIR IAW SRM 51-42-11 PG 1 AND SRM 51-72-11 PG 1 & 2. 2 L 7 2 4F RT A28NM 2002041000067 20020410 00067 EU 2002 4 10 AWXA200200311 1 20020304 A 5347 D53472209203 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 YWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON RECESSED NUT HOLE OF SEAT RAIL AT FR 64, Y765. MAINTENANC E REMOVED SEAT RAIL AT FR 64, Y765 RT, FABRICATED A NEW SEAT RAIL, AND INSTALLED REPAIR IAW SRM 51-72-11 PG 1 & 2 AND SR M 51-42-11 PG 1. 2 L 7 2 4F RT A28NM 2002041000069 20020410 00069 EU 2002 4 10 AWXA200200312 1 20020304 A 5347 D53472190205 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 YWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND AT RECESSED NUT HOLES ON SEAT RAIL Y1292 RT, FR 64 TO FR 66. MAINTENANCE REMOVED SEAT RAIL Y1292 RT BETWEEN FR 64 AND FR 66, FABRICATED A NEW SEAT RAIL AND INSTALLED REPAIR IAW SRM 51-72-11 PG 1 & 2, AND SRM 51-42-11, PG 1. 2 L 7 2 4F RT A28NM 2002041000075 20020410 00075 2002 4 10 SABA020048 4 20020408 A 2210 7003975 CONTROLLER DHAV DHC8 DHC8103 1386005 NM FWD FUSALAGE FAILED A SABA K NONE O OTHER CR CRUISE 1 SO 33 882CC 168 Aircraft 883 on flight 5078 from OAJ to CLT. During cruise flight the autopilot and both yaw-damp became inoperative. Flight continued to CLT with no other problems and no emergency declared. Maintenance removed and replaced the flight g uidance controller. System ops checked good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002041000076 20020410 00076 NM 2002 4 10 SWAA020739 1 20020406 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 727D AT STR 19R, BS 749 AT STR 18R, BS 745 AT S TR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002041000077 20020410 00077 NM 2002 4 10 SWAA020740 1 20020406 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 905, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002041000078 20020410 00078 NM 2002 4 10 SWAA020741 1 20020408 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED RON, ON WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10L, BS 670 AND BS 680. REPAI RED SKIN PER SWA RA. 2 L 7 2 4F A16WE 2002041000079 20020410 00079 NM 2002 4 10 SWAA020742 1 20020408 A 5320 6517684 DOUBLER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR CUTOUT DOUBLER CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED DO UBLER PER SRM. 2 L 7 2 4F RT A16WE 2002041000080 20020410 00080 NM 2002 4 10 SWAA020743 1 20020408 A 5311 6545871 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR FWD CUTOUT FRAME VERTICAL WEB CRACKED AT BS 303.9, STR 16R. REMOVED A ND REPLACED VERTICAL WEB PER SRM. 2 L 7 2 4F RT A16WE 2002041000081 20020410 00081 NM 2002 4 10 SWAA020744 1 20020408 A 5311 6546569 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME AND SHEAR TIE CRACKED AT BS 967, BETWEEN STR 5L AND 7L. REPAIRED FRAME A ND SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002041000082 20020410 00082 NM 2002 4 10 SWAA020745 1 20020408 A 5753 65C26602 WEDGE BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D CHECK, FOUND NR 3 L/E SLAT INBD T/E WEDGE DELAMINATED. REPAIRED NR 3 L/E SLAT WEDGE PER SRM. 2 L 7 2 4F RT A16WE 2002041000083 20020410 00083 NM 2002 4 10 SWAA020746 1 20020408 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 500B, STR 10R. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2002041000084 20020410 00084 NM 2002 4 10 SWAA020747 1 20020408 A 2910 AS116080290 HOSE BOEING 737 7373Q8 1384670 NM RT MLG W/W LEAKING A SWAA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 663SW 23256 AIR TURNBACK, B HYD SYSTEM, FLUID LEAK NOTICED INFLIGHT AND RETURNED TO PHX. REMOVED AND REPLACED B HYD SYSTEM FLEX HOS E FROM B HYD PUMP TO ACOUSTIC FILTER PER MM. 2 L 7 2 4F RT A16WE 2002041000085 20020410 00085 2002 4 10 SWAA020724 4 20020404 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002041000086 20020410 00086 2002 4 10 SWAA020725 4 20020405 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002041000087 20020410 00087 NM 2002 4 10 SWAA020726 1 20020405 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 404WN 27892 EEPLS COVER MISSING AT MID CABIN. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002041000088 20020410 00088 NM 2002 4 10 SWAA020727 1 20020407 A 3350 65C27093 LIGHT BOEING 737 7372K6 1364440 NM AFT ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 AFT ENTRY DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002041000089 20020410 00089 NM 2002 4 10 SWAA020731 1 20020407 A 5313 BAC1493 STIFFENER BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED 1/2D CHECK, FOUND STIFFENER CORRODED AT BS 1088, RBL 30 ABOVE APU INTAKE CUTOUT. REPAIRED STIFFENER PE R SRM. 2 L 7 2 4F RT A16WE 2002041000090 20020410 00090 NM 2002 4 10 SWAA020733 1 20020405 A 5210 6545871 DOOR FRAME BOEING 737 7373Y0 1384671 NM FWD ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR AFT FRAME CRACKED (3 EA) AT NR 3, NR 4 AND NR 5 STOP FITTINGS FROM BOT TOM. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002041000091 20020410 00091 NM 2002 4 10 SWAA020734 1 20020406 A 5312 6517582 WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, WL 227 AT LBL 17.1. REMOVED AND REPLACED WEB PE R SRM. 2 L 7 2 4F RT A16WE 2002053000049 20020530 00049 NM 2002 5 30 2002UALA00585 1 20020331 A 2822 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL SYSTEM FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 545UA 25323 RIGHT FORWARD FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED. REPLACED THE RIGHT FORWARD FUEL BOOST PUMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041000118 20020410 00118 NM 2002 4 10 2002UALA00586 1 20020326 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 AT DOOR 5 RIGHT HAND SIDE THE FORWARD EEL SILL LIGHT IS INOP. REPLACED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000119 20020410 00119 NM 2002 4 10 2002UALA00587 1 20020327 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 AT LAV 110 EEL LIGHT INOP. STAPLED POWER STRIP AND OPS TESTED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000120 20020410 00120 NM 2002 4 10 2002UALA00589 1 20020329 A 3320 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 CEILING EEL LIGHT AT ROW 17 IS INOPERATIVE. REPLACED BATTERY PACK IN CEILING. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000121 20020410 00121 NM 2002 4 10 2002UALA00590 1 20020329 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 FORWARD SIDE OF LAV 117 EEL LIGHT INOPERATIVE. REPLACED EEL STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000122 20020410 00122 NM 2002 4 10 2002UALA00591 1 20020329 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 CEILING EEL AT ROW 2 IS INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000123 20020410 00123 NM 2002 4 10 2002UALA00592 1 20020329 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 FORWARD SEAT EEL AT SEAT 2J IS INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000124 20020410 00124 NM 2002 4 10 2002UALA00593 1 20020329 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 BOTH SEAT EEL AT SEAT 1A IS INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000125 20020410 00125 NM 2002 4 10 2002UALA00594 1 20020329 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 AFT SEAT EEL AT SEAT 5F IS INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041000142 20020410 00142 SO 2002 4 10 COMA0210013 1 20020407 A 2150 9799901 VALVE EMB 120 EMB120RT 3260202 SO L/H MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 463CA 29563 120267 FLIGHT 5069 CABIN VERY HOT A/C SYSTEM NOT WORKING.REPLACED THE L/H TEMP CONTROL VALVE. 2 L 7 2 4T RT A31SO 2002041000143 20020410 00143 EA 2002 4 10 COMA0260239 1 20020406 A 2710 AILERON CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 952CA 7092 FLIGHT 6066 AILERON CONFIG WARNING DURING T/O.COULD NOT DUPLICATE. INSPECTED AILERON SYSTEM - NO ABNORMALTY FOUND. 2 L 7 2 4F RT A21EA 2002041000144 20020410 00144 NM 2002 4 10 UPS02437978 1 20020325 A 5220 FRAME BOEING 747 747212B 1384886 NM R1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C M/D - R1 DOOR FWD LOWER CORNER FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 52-10-02 FIG 10. 2 L 7 4 4F A20WE 2002041000145 20020410 00145 NM 2002 4 10 UPS02437981 1 20020328 A 5310 141U109212 CLIP BOEING 747 747212B 1384886 NM NOSE W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C NOSE WHEEL WELL VERTICAL BEAM WEB WEB R/H BS 320 #2 SHEAR TIE CLIP (COUNT FROM TOP) CRACK FOUND AT FAS TENER AS MARKED. NWW VERTICAL BEAM WEB RH BS 320 #2 SHEAR TIE CLIP (COUNT FROM TOP) REPLACED AS PER SRM 51-10-01 & I NSTALLED AS PER BOEING DWG 624U0005. 2 L 7 4 4F A20WE 2002041000146 20020410 00146 NM 2002 4 10 UPS02437985 1 20020327 A 5310 65B280813 ANGLE BOEING 747 747212B 1384886 NM NOSE W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C NLG W/W PRESSURE DECK LH CORNER LONG. ANGLE FOUND CRACKED AT BS 321 LBL 32 AS MARKED. NLG W/W PRES SURE DECK LH ANGLE REPLACE AS PER EO B747-5310-0574 DWG 624U0005 ST 3. 2 L 7 4 4F A20WE 2002041000147 20020410 00147 NM 2002 4 10 UPS02437988 1 20020325 A 5310 WEB BOEING 747 747212B 1384886 NM R2 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C M/D - R2 DOOR FWD CUTOUT REVEAL FOUND CRACKED. M/D R2 DOOR FWD CUTOUT REVEAL REPAIRED AS PER HX RS #R-53-20-34755. 2 L 7 4 4F A20WE 2002041000148 20020410 00148 NM 2002 4 10 UPS02437989 1 20020325 A 5310 WEB BOEING 747 747212B 1384886 NM L2 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C M/D - L2 DOOR FWD CUTOUT REVEAL FOUND CRACKED. M/D L2 DOOR FWD CUTOUT REVEAL REPAIRED AS PER RS #R -53-20-34755. 2 L 7 4 4F A20WE 2002041000149 20020410 00149 NM 2002 4 10 UPS02437990 1 20020326 A 3220 ANGLE BOEING 747 747212B 1384886 NM NLG W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C NLG W/W - CRACK SUSPECTED AT PRESSURE DECK RH LONGI. SUPPORT ANGLE STA 307 & STA 320 AS MARKED. NL G W/W CEILING R/H UPPER O/B ANGLE REPLACED AS PER EO B747-5310-0574. 2 L 7 4 4F A20WE 2002041000150 20020410 00150 NM 2002 4 10 UPS02437999 1 20020325 A 5310 WEB BOEING 747 747212B 1384886 NM R5 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C M/D - R5 DOOR FWD CUTOUT UPP SPLICE WEB FOUND CRACKED. REPAIR DOUBLER INSTALLED AS PER SRM 53-10-0 4 FIG.91. 2 L 7 4 4F A20WE 2002041000151 20020410 00151 NM 2002 4 10 UPS02438001 1 20020325 A 5330 65B38600382 TIE CLIP BOEING 747 747212B 1384886 NM FWD CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C FWD CARGO COMPT BS 560 S-33L STRINGER TIE CLIP CRACKED. TIE CLIP REPLACED AS PER SRM 51-10-01 P.8. 2 L 7 4 4F A20WE 2002041000152 20020410 00152 NM 2002 4 10 UPS02438002 1 20020325 A 5310 STRINGER BOEING 747 747212B 1384886 NM MAIN DECK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C M/D - BS 856 S25R STRINGER END FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG.1. 2 L 7 4 4F A20WE 2002041000153 20020410 00153 NM 2002 4 10 UPS02438009 1 20020324 A 5710 FITTING BOEING 747 747212B 1384886 NM BS 1241 R/H CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C FX - R/H BS 1241 WING CENTER SECTION REAR SPAR WEB AFT SURFACE BULKHEAD FITTING FOUND COR BETWEEN FAST ENER #2 AND #9. R/H BS 1241 WING CENTER SECTION REAR SPARE WEB AFT FACE BULKHEAD FTG BETWEEN FASTENER #2 & #9 CORROS ION REMOVED AS PER UPS EO B747-5710-11129. 2 L 7 4 4F A20WE 2002041000154 20020410 00154 SO 2002 4 10 C2XA02CL098 1 20020408 A 5210 AN313A BOLT EMB 145 EMB145ER 3260211 SO CABIN DOOR LOOSE A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 15948 145056 CLE FLIGHT#3157 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN.MAINTENANCE INSPECTED AND TIGHTENED THE INNE R DOOR HANDLE ASSEMBLY BOLT.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002041000155 20020410 00155 EA 2002 4 10 COMA0260240 1 20020407 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 868CA 7427 FLIGHT 5083 FLAPS FAILED AT 30 DEGREES DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002041000156 20020410 00156 EA 2002 4 10 COMA0260241 1 20020408 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 938CA 7046 FLIGHT 5204 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.COULD NOT DUPLICATE. OPERATED PASSENGER DOOR AND FOUND NO ABNORMALI TIES. 2 L 7 2 4F RT A21EA 2002041000157 20020410 00157 WP 2002 4 10 DHL2002807522 1 20020323 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.; N/R 2042 RT. WING L/E UPPER INNER SKIN - RIB CRACKED .250 @ SAT. XFS628.75OCORR: STOP DRILLED CRACK I/A/W S RM 57-2-0 , FIG. 2 - FABRICATED REINFORCING ANGL ( 2024 T3 AL .063) I/A/W 57-2-0 FIG. 2 CLEANED , TREATED ,A ND PRIMED I /A/W SRM 51-1-8B . INSTALLED REINFORCING ANGLE I/A/W 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2002041000158 20020410 00158 WP 2002 4 10 DHL2002807523 1 20020326 A 5330 SKIN DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 1443 FUS. EXT. SKIN CRACKED .500 STA 1748CORR.: REMOVED FASTNERS I/A/W SRM 51-1-21 PG.1 - CUT OUT DAMAGE D AREA I/A/W SRM 53-2-1 PG. 99-100 -FABRICATED FILLER (7075T6 .063) + FINGER DOUBLERS (7075T6 .040 + DOUBLER (7075T6 .07 1) I/A/W SRM53-2-1 PG. 99-100 - CLEANED , TREATED , PRIMED I/A/W SRM 51-1-8B - INSTALLED FILLER , FINGER DOUBLERS AND DO UBLER I/A/W SRM 53-2-1PG. 99-100 , 51-1-21 & 51-1-20D PG.9 2 L 7 4 4F RT 4A25 2002041000159 20020410 00159 WP 2002 4 10 DHL2002807524 1 20020328 A 5330 3779762501 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: N/R 0541 MAIN CARGO COMPARTMENT - 2" CRACK ON BATHTUB FITTING STA. 670.000 -680.000 , L9RCORR: REMOVED BATHTUB FI TTING I/A/W SRM 51-1-20DPG. 21 - CLEANED , TREATED , AND PRIMED AREA IAWSRM 51-1-8B - INSTALLED NEW FITTING IAW SRM 51- 1-20D PG. 9 2 L 7 4 4F RT 4A25 2002041700085 20020417 00085 NM 2002 4 17 02FDEA00242 1 20020409 A 5320 6587260 FITTING BOEING 727 727277 138408S NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 BS 1185, LBL 24, WL 292 BULKHEAD TO SPAR FITTING CRACKED AT FWD HORZ FASTENER HOLE. REMOVED AND REPLACED FITTING PER SR M & MM. 2 L 7 3 4F RT A3WE 2002041000160 20020410 00160 EU 2002 4 10 02FDEA00241 1 20020410 A 5530 A55471611000400 FITTING AIRBUS 310 A310203 3930313 EU CORRODED A FDEA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SO 25 410FE 356 #1 RUDDER HINGE FITTING HAS CORROSION AT LWR HINGE PIN ATTACH. R&R FITTING. 2 L 7 2 4F RT A35EU 2002041000161 20020410 00161 NM 2002 4 10 02FDEA00240 1 20020409 A 5330 FRAME BOEING 727 727225 1384077 NM CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 N 852 CRACKED FRAME AT FASTENER HOLE AT BS 540, RBL 3, WL 155. ** S/D ** COMING 2 L 7 3 4F A3WE 2002042200140 20020422 00140 NM 2002 4 22 QXEA0200546 1 20020409 A 6123 83910321021 CONTROLLER DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS FAULTY A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 355PH 500 PDX - ABORTED TAKEOFF, AUTO FEATHER DID NOT ARM. REPLACED AUTO FEATHER CONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002041000162 20020410 00162 WP 2002 4 10 AT0200046 1 20020408 A 2130 71145730016 DUCT DOUG DC9 DC932 3022066 WP TAIL COMPARTMENT TORN A ZZDA K NONE O OTHER CR CRUISE 1 SO 15 819AT 47260 AIRCRAFT WOULD NOT MAINTAIN CABIN ALTITUDE/PRESSURE IN AUTOMATIC OR MANUAL MADE AT FL290. A/C DESCENDED LOWER TO ENABL E MANUAL PRESURIZATION; THUS NORMAL/OPTIMUM CABIN ALT/PRESSURE FOR CREW AND PASSENGERS. ALL MASKS FELL. CO RRECTIVE ACTION: REMOVED AND REPLACED RIGHT PRESSURE VALVE DUCT; FORWARD RELIEF VALVE, AND RIGHT AIR CYCLE MACH INE. 2 L 7 2 4F A6WE 2002041000163 20020410 00163 NM 2002 4 10 P5CA0200670 1 20020409 A 2530 NONE INVERTER BOEING 747 747122 1384872 NM GALLEY FAILED A P5CA H DEACTIVATE SYST/CIRCUITS O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 WHEN MICROWAVE WAS TURNED ON, GALLEY INVERTER FAILED & SMELLED ELECTRICAL FUMES. REMOVED CANNON PLUG FROM GALLEY STATIC INVERTER. NO POWER TO GALLEY. TRANSFERED TO O.I.L. #61919 PER MX CTRL DAVID. 2 L 7 4 4F A20WE 2002041000164 20020410 00164 NM 2002 4 10 AWXA200200329 1 20020329 A 5315 654541041 WEB BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 0 0 23627 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON THE CABIN FLOOR BEAM UPPER TEE CHORD AND WEB AT BS 660, L BL 0.07. MAINTENANCE REMOVED DAMAGED AREA OF WEB AT BS 660, LBL 0.07, FABRICATED 2 EACH REPAIR ANGLES, 3 EACH STRAPS, 2 EACH SPLICE PLATES, 2 EACH FILLERS, AND 1 EACH CHORD ANGLE & WEB, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5717-02098-KB 1. 2 L 7 2 4F RT A16WE 2002041000165 20020410 00165 NM 2002 4 10 AWXA200200331 1 20020129 A 5313 BAC1498203 STRINGER BOEING 757 7572S7 1384962 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 0 0 23322 GYR - MAJOR REPAIR - DURING C-08 CHECK A 3/8" CRACK WAS FOUND AT FASTENER HOLE ON STRINGER 15 L/H, BS 590. MAINTENANCE C UTOUT DAMAGED AREA OF STRINGER, FABRICATED 2 EACH REPAIR ANGLES & CHANNELS, AND 1 EACH SHIM & FILLER, AND INSTALLED REPA IRS IAW SRM 53-00-03, FIG 201, PG. 201-209. 2 L 7 2 4F RT A2NM 2002041100021 20020411 00021 NM 2002 4 11 CA020402005 1 20020402 A 2131 7638102 CONTROLLER BOEING 727 727200 138407E NM PWA JT8 JT8D17 52049 NE CABIN PRESSURE FAILED W G O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 CA (CAN) FLT 146 AFTER DEPARTURE, CABIN ALTITUDE WARNING HORN SOUNDED. CREW EXECUTED CABIN ALTITUDE WARNING / RADID DEPRES SURIZATION CHECKLIST & CABIN PRESSURE STABILIZED AT 12,000 FT. AIRCRAFT DESCENDED TO 26,000 FT, FLT ATTENDENTS DONNED PO RTABLE OXYGEN MASKS & CHECKED ON PASSENGERS. ONCE A/C AT 26,000 FT CREW SWITCHED PRESSURE CONTOLLER TO STANDBY AND THE C ABIN SLOWLY DESCENDED TO 10,000 FT. A/C CONTINUED ON & LANDED W/O FURTHER INCIDENT. MAINT PERFORMED A/C PRESSURIZATION TEST IN ACCORD WITH MM & ELECTED TO CHANGE CABIN PRESSURE CONTROLLER. SYS GROUND CHECKED SERVICEABLE. A/C RETURNED TO S ERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2002041100033 20020411 00033 WP 2002 4 11 COOSDR02049 1 20020401 A 5280 CHANNEL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE MLG DOOR CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69803 49229 LEFT MAIN LANDING GEAR INBOARD DOOR FORWARD Z CHANNEL CRACKED. 2 L 7 2 4F 4 F A6WE E2EA 2002041100034 20020411 00034 WP 2002 4 11 COOSDR02050 1 20020401 A 5315 FLOORBEAM DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE FUSELAGE CORRODED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 MAIN CARGO COMPONENT, STA 1680, Z0, +X7 INCHES AND X 15 INCHES, FLOOR BEAM UPPER CHORD CORRODED. 2 L 7 4 4F 4 F 4A25 1E8 2002041100035 20020411 00035 WP 2002 4 11 COOSDR02051 1 20020401 A 5311 FRAME DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE FUSELAGE CORRODED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 950R 45903 AFT CARGO COMPONENT STA 1600 BETWEEN LONG 34 LEFT AND 34 RIGHT FRAME, CORRODED. 2 L 7 4 4F 4 F 4A25 1E8 2002041100036 20020411 00036 WP 2002 4 11 COOSDR02052 1 20020401 A 5230 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE CARGO DOOR CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69803 49229 FORWARD C/C DOOR, LOWER FORWARD CORNER, OUTER SKIN CRACKED. 2 L 7 2 4F 4 F A6WE E2EA 2002041100037 20020411 00037 WP 2002 4 11 COOSDR02053 1 20020401 A 5310 5936469U1 ANGLE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D9 52048 NE CARGO DOORWAY CORRODED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 813US 48093 MID CARGO DOOR CUTOUT, STA 693 BETWEEN LONGERON 26R AND LONG. 28R, ANGLE PN: 5936469U1 CORRODED. 2 L 7 2 4F 4 F A6WE E2EA 2002041100038 20020411 00038 NM 2002 4 11 COOSDR02054 1 20020401 A 5753 652163585 SKIN BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE LT TE FLAP DEBONDED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 LEFT WING, OUTBOARD AFT FLAP DEBONDED. 2 L 7 3 4F 4 F RT A3WE E2EA 2002041100039 20020411 00039 NM 2002 4 11 COOSDR02055 1 20020401 A 5753 6521630174 SKIN BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE RT TE FLAP DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 199AJ 21426 RIGHT WING, INBOARD FORE FLAP UPPER AND LOWER SKIN DELAMINATION. 2 L 7 3 4F 4 F RT A3WE E2EA 2002041100040 20020411 00040 WP 2002 4 11 COOSDR02056 1 20020401 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69803 49229 FUSELAGE, TAIL AREA, CANTED STA 1492, X 17 INCHES, Z 2 INCHES STIFFENER CRACKED. 2 L 7 2 4F 4 F A6WE E2EA 2002041100041 20020411 00041 WP 2002 4 11 COOSDR02057 1 20020401 A 5230 FITTING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69803 49229 AFT CARGO COMPARTMENT DOOR, LOWER SIDE, STA 1196 FITTING CRACKED. 2 L 7 2 4F 4 F A6WE E2EA 2002041100042 20020411 00042 CE 2002 4 11 EPD2002F00000 1 20020318 A 5610 10138402517 WINDSHIELD BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE COCKPIT CRACKED W EPDA K NONE O OTHER IN INSP/MAINT 1 NM 02 149SR 1486 BB1572 PCEPJ009261 COCKPIT WINDSHIELD INNER PANEL CRACKED AT ALTITUDE. OUTER PANEL REMAINED INTACT. WINDSHIELD HEAT WAS ON. NO STRIKES N OTED. 1 L 7 2 4T 4 T A24CE E4EA 2002041100055 20020411 00055 SW 2002 4 11 C1Y2002F00000 1 20020226 A 2140 SHUTOFF VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL CABIN HEATER FAILED B C1YM K NONE O OTHER IN INSP/MAINT 1 CE 01 407LG 695 53143 CABIN HEATER SHUTOFF VALVE (PN ES26185-1) WOULD CONTINUALLY TRIP THE CIRCUIT BREAKER. INSTALLED NEW VALVE. HEATER OPER ATION BACK TO NORMAL. 1 G 7 1 3U 3 U O H2SW E1GL 2002041100056 20020411 00056 CE 2002 4 11 CTU2002F00005 1 20020329 A 2121 EM6039 BLOWER BEECH 90 C90 1152913 CE PWA PT6 PT6A60A 52043 NE VENTILATION SYS FAILED B CTUR O OTHER O OTHER NR NOT REPORTED 1 GL 21 911ND 1408 LJ774 VENTILATION BLOWER ASSEMBLY FAILED IN FLIGHT, FILLING COCKPIT AND CABIN WITH SMOKE. 1 L 7 2 3T 4 T 3A20 E4EA 2002041100057 20020411 00057 EA 2002 4 11 02099632 1 20020209 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 632BR 7268 DURING CRUISE OF THE FLIGHT FROM PVD TO IAD, THE CREW NOTED THAT THE PASSENGER DOOR OUTER HANDLE EICAS MESSAGE HAD DISPL AYED. THE FLIGHT DIVERTED TO BDL AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL INSPECTED THE DOOR MECHANISM AND I NDICATION SYSTEM. OPERATIONAL CHECKS COULD NOT DUPLICATE THE MALFUNCTION. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002041100058 20020411 00058 EA 2002 4 11 02099646 1 20020209 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 646BR 7379 DURING CRUISE OF THE FLIGHT FROM CHS TO ORD, THE CREW NOTED THAT THE PASSENGER DOOR OUTER HANDLE EICAS MESSAGE HAD DISPL AYED. THE FLIGHT DIVERTED TO CAE AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL CLEANED THE PASSENGER DOOR PROXIMI TY SENSOR. OPERATIONAL AND PRESSURIZATION CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002041100063 20020411 00063 NM 2002 4 11 2002UALA00603 1 20020329 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 BODY STATION 832 RBL II TRANSBEAM UPPER CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041100064 20020411 00064 NM 2002 4 11 2002UALA00604 1 20020329 A 5312 BULKHEAD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 BODY STATION 246 RBL 50 BULKHEAD WEB IS PUNCTURED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041100065 20020411 00065 NM 2002 4 11 2002UALA00605 1 20020329 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 FORWARD NOSE COMP STATION 231.25 RBL 4 FRAME UPPER CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041100066 20020411 00066 NM 2002 4 11 2002UALA00607 1 20020402 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 RT LOWER FUSELAGE, STA 392 THROUGH 400, AT STRINGER 20R, FUSELAGE SKIN HAS 7 INCH DENT. MAJOR REPAIR ACCOMPLISHED. DOU BLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041100067 20020411 00067 NM 2002 4 11 2002UALA00608 1 20020401 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 CABIN FLOOR STATION 660-680 LEFT HAND SIDE CREASE BEAM INNER CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED INNER CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041100068 20020411 00068 NM 2002 4 11 2002UALA00609 1 20020401 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 CABIN FLOORBEAM BODY STATION 640 LBL 4 TO LBL 17 HAS EXCESSIVE MATERIAL REMOVED DUE TO GOUGE IN CENTER O/B BEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND NESTED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041100069 20020411 00069 NM 2002 4 11 2002UALA00610 1 20020401 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 CABIN FLOORBEAM BODY STATION 440 UPPER SURFACE HAS EXCESSIVE MATERIAL LOSS DUE TO REMOVAL OF CORROSION AT RBL 4 TO RBL 5 .5. MAJOR REPAIR ACCOMPLISHED. STRAP REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041100073 20020411 00073 NM 2002 4 11 2002UALA00615 1 20020402 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 BODY STATION 852-870 LBL 55 FLOORBEAM T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041100074 20020411 00074 NM 2002 4 11 2002UALA00616 1 20020401 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 BODY STATION 1197+88 LBL 40-41 FLOORBEAM UPPER CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED UPP ER CHORD T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041100075 20020411 00075 NM 2002 4 11 2002UALA00617 1 20020401 A 5411 SPAR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PLYON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 NR 1 ENGINE PYLON UPPER SPAR WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041100077 20020411 00077 NM 2002 4 11 2002UALA00619 1 20020401 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 BODY STATION 790 RBL 12-14 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SPLICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041100078 20020411 00078 NM 2002 4 11 2002UALA00620 1 20020402 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 931UA 26656 STA 188 FRAME ON LT SIDE IS CRACKED IN RADIUS AT WL 207. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041100080 20020411 00080 NM 2002 4 11 2002UALA00624 1 20020402 A 5310 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT CABIN DECK PLATE CORRODED AT STA 1681 RBL 22.5 TO RBL 52. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041100081 20020411 00081 NM 2002 4 11 2002UALA00625 1 20020403 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 CABIN FUSELAGE FRAME INBOARD CORD HAS A CRACK AT BOTTOM END BODY STATION 616 WL 216 RBL 64.5. MAJOR REPAIR ACCOMPLISHED . INSTALLED REINFORCING ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041100082 20020411 00082 NM 2002 4 11 2002UALA00626 1 20020403 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 AFT SIDE OF BODY STATION 188 FRAME CRACKED AT WL 207 LEFT HAND SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPA IR ON FRAME, AND DOUBLER TO SKIN. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041100083 20020411 00083 NM 2002 4 11 2002UALA00627 1 20020403 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 AFT SIDE OF BODY STATION 188 FRAME CRACKED AT WL 207 RIGHT HAND SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REP AIR ON FRAME, AND DOUBLER TO SKIN. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041100084 20020411 00084 NM 2002 4 11 2002UALA00628 1 20020328 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 UPPER LOBE INTERNAL FUSELAGE FRAME CRACKED AT FASTENER JUST ABOVE STRINGER 9L AT BODY STATION 867. MAJOR REPAIR ACCOMPL ISHED. INSTALLED CHANNEL REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041100085 20020411 00085 WP 2002 4 11 ZW0A0202502 1 20020227 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 941AS 49925 DURING CHECK-C MAINT CABIN SEAT TRACK HAD CORROSION IN LT FLANGE OF TRACK, LBL 44.5 INCHES, BETWEEN STA 1117 AND 1174. INSTALLED NEW SECTION OF TRACK FROM STA 1108 TO 1222 PER SPM 6-70-01, PAGE 3. SPLICED PER SRM 53-05, FIG 4F. 2 L 7 2 4F A6WE 2002041100087 20020411 00087 EU 2002 4 11 02FDEA00238 1 20020407 A 5210 SKIN AIRBUS 310 A310222 3930315 EU PAX DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 LT MAIN ENTRY DOOR EXTERIOR HANDLE CUTOUT CORRODED AT HORIZ WEB & AFT VERTICAL WEB. 2 L 7 2 4F RT A35EU 2002041100088 20020411 00088 NM 2002 4 11 02FDEA00239 1 20020328 A 5753 STOP FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 LT INBOARD FLAP VANE SPRING CARTRIDGE STOP ASSY BROKEN FROM STOP FASTENER HOLES. DISCONNECTED CARTRIDGE. 2 L 7 3 4F RT A22WE 2002042600098 20020426 00098 NM 2002 4 26 02FDEA00243 1 20020409 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 207FE 22929 SKIN LAP AT STR 19R, BS 720E IS CHAFED. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 14. 2 L 7 3 4F A3WE 2002042600099 20020426 00099 NM 2002 4 26 02FDEA00244 1 20020404 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 207FE 22929 SKIN LAP AT STR 19L, BS 720E IS CHAFED. REMOVED AND REPLACED SKIN PER SRM 53-30-3. 2 L 7 3 4F A3WE 2002041800117 20020418 00117 NM 2002 4 18 2002UALA00630 1 20020323 A 5532 146T06002 PANEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE VERTICAL STAB MISSING A UALA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 WP 29 655UA 25393 ON ARRIVAL FOUND DORSAL FIN PANEL MISSING. THE DORSAL FIN PANEL WAS REPLACED. THE FUSELAGE SKIN IN THE AREA OF THE DOR SAL FIN WAS VISUALLY AND HFEC INSPECTED TO ENSURE THAT NO DAMAGE TO THE FUSELAGE SKIN OCCURRED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041100090 20020411 00090 NM 2002 4 11 2002UALA00631 1 20020331 A 4920 4500381 TURBINE WHEEL HAMLTN 62T47C1 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 390UA 912097 24665 APU HAD A COMPLETE FAILURE AFTER NORMAL START. COMPRESSOR CASE SPLIT. FOUND TURBINE WHEEL FAILED. REPLACED APU AND MU FFLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041800118 20020418 00118 NM 2002 4 18 2002UALA00632 1 20020404 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 STATION 400 ABOVE STRINGER 9L INNER FRAME FLANGE IS CRACKED AT RAIL SUPPORT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041800119 20020418 00119 NM 2002 4 18 2002UALA00633 1 20020404 A 3350 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 SEAT EEL AT ROWS 32-34, SEATS A, B, C IS INOP. REPLACED POWER SUPPLY UNIT. OP CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041800124 20020418 00124 NM 2002 4 18 2002UALA00634 1 20020404 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 AFT EEL ON SEAT 4J INOP. REPLACED EEL LAMP. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041800125 20020418 00125 NM 2002 4 18 2002UALA00635 1 20020404 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 FORWARD SIDE OF GALLEY 415, THE EEL STRIP IS INOP. RELAMPED, OP CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041800126 20020418 00126 NM 2002 4 18 2002UALA00636 1 20020404 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 SEAT EEL AT SEATS 55 A, B, C IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041800127 20020418 00127 NM 2002 4 18 2002UALA00637 1 20020404 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 AT NUMBER 3 MED ON THE LEFT SIDE, THE AFT EXIT SIGN IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041800138 20020418 00138 NM 2002 4 18 2002UALA00638 1 20020404 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 SEAT EEL AT SEATS 37 A, B, C IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041100109 20020411 00109 NM 2002 4 11 AALA20020065 1 20020122 A 3350 CONNECTOR BOEING 737 737823 13844BZ NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 916AN 29517 TUL - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LGIHT ON SEAT 9D INOPERATIVE. RESEATED PIN ON LIGHT SOC KET CONNECTOR TO SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2002041100110 20020411 00110 NM 2002 4 11 AALA20020104 1 20020128 A 5330 SKIN BOEING 737 737823 13844BZ NM FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 915AN 29516 TUL - FOUND GOUGE IN FUSELAGE SKIN ON AFT EDGE OF AFT CARGO DOOR CUTOUT ABOVE SKIN LAP. BLENDED DAMAGED AREA AND FINISH ED REPAIR PER ESO 61000 DATED 1-15-02. (M) 2 L 7 2 4F RT A16WE 2002041100111 20020411 00111 WP 2002 4 11 AALA20020153 1 20020214 A 2170 COALESCER BAG DOUG DC9 DC982 3022082 WP ACM CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 285AA 49297 DFW - FLT 515 - EN ROUTE DFW-COS, SHORTLY AFTER TAKEOFF, HEAVY SMOKE WAS REPORTED IN CABIN. EMERGENCY DECLARED, RETURNE D DFW AND LANDED WITHOUT INCIDENT. ACCOMPLISHED PACK BURN OUT. NO SMOKE OR ODORS NOTED. PRECAUTIONARY REPLACED COALES CER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002041100112 20020411 00112 WP 2002 4 11 AALA20020154 1 20020215 A 2120 ODOR DOUG DC9 DC982 3022082 WP CABIN DETECTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 285AA 49297 DFW - FLT 641 - EN ROUTE DFW-YYC, SHORTLY AFTER TAKEOFF, SMOKE WAS REPORTED IN CABIN. EMERGENCY DECLARED, RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT PACK PRIMARY AND SECONDARY HEAT EXCHANGER. REPLACED APU, AND ACCOMPLISHED PACK BURN OUT. NO SMOKE OR ODORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002041100113 20020411 00113 WP 2002 4 11 AALA20020155 1 20020215 A 2560 P2070003001 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 559AA 53089 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED FORWARD ENTRY EME RGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002041100114 20020411 00114 WP 2002 4 11 AALA20020156 1 20020215 A 2560 P2070003001 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 216AA 49167 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED FORWARD ENTRY EME RGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002041100115 20020411 00115 WP 2002 4 11 AALA20020163 1 20020220 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 471AA 49601 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS IN FORWARD ENTRANCE AND GALLEY AREA ARE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY AND CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002041100116 20020411 00116 NM 2002 4 11 AALA20020170 1 20020224 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 869AA 21374 DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT SEAT TRACK LIGHTING SYSTEM ROW 6 THROUGH 16 INOPERATIVE. RECON NECTED EMERGENCY EXIT SEAT TRACK LIGHTING CONNECTOR AT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2002041100117 20020411 00117 NM 2002 4 11 AALA20020171 1 20020222 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 906AN 29508 LAX - DURING OVERNIGHT MAINTENANCE FOUND OVERHEAD EMERGENCY LIGHT 14EF INOPERATIVE. REPLACED LIGHT SOCKET AT SEAT 14EF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2002041100118 20020411 00118 NM 2002 4 11 DL72E020269 1 20020305 A 7120 MOUNT BOEING 727 727247 138408F NM NR 3 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2829W 21481 DURING INSPECTIONS OF THE FORWARD ENGINE MOUNT SUPPORT FITTING ON THE NR 3 ENGINE PYLON PER AD 97-05-08, A CRACK INDICAT ION WAS NOTED IN HOLE C AS REFERENCED IN BAC S/B 727-54A0010. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK WITH AN ADDITI ONAL INSURANCE CUT. ACCOMPLISHED PER FED-EX S/B 2000-5410A01 AND ER/A 382703-14AD. 2 L 7 3 4F A3WE 2002041100119 20020411 00119 WP 2002 4 11 AALA20020177 1 20020222 A 2530 OVEN DOUG DC9 DC982 3022082 WP FWD GALLEY ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 7537A 49991 DFW - FLT 353 - EN ROUTE LGA-ORD, AT 31,000 FEET NR 1 FLIGHT ATTENDANT REPORTED SMOKE AND FUMES COMING FROM CEILING NEAR FORWARD GALLEY. SHUTOFF GALLEY POWER, RE-CIRCULATION FAN PASSENGER PHONES AND POWER PORTS FOR SEATS, RAN SMOKE REMOVAL PROCEDURES. FUMES WERE REDUCED BUT WOULD NOT GO AWAY SMELLED LIKE BURNING ELECTRICAL OR PLASTIC. LANDED BUF WITHOUT I NCIDENT. REPLACED FORWARD GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002041100120 20020411 00120 WP 2002 4 11 AALA20020192 1 20020227 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 510AM 49804 DFW - DURING OVERNIGHT MAINTENANCE, AFT GALLEY OVERHEAD EMERGENCY PATH LIGHTING AND ROW 28-30 EMERGENCY EXIT LIGHTS INOP ERATIVE. RESEATED EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002041100121 20020411 00121 NM 2002 4 11 AALA20020193 1 20020228 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 623AA 24581 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH LIGHTS FROM ROW 17 TO REAR OF AIRCRAFT INOPERATIVE. REPLACED EMERGEN CY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002041100122 20020411 00122 WP 2002 4 11 AALA20020203 1 20020301 A 2822 O-RING DOUG DC9 DC982 3022082 WP LEFT WING LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 278AA 49294 RDU - FLT 1858 - EN ROUTE PBI-LGA, FUEL LEAK COMING FROM BOOST PUMP COVER DURING FLIGHT. DIVERTED AND LANDED RDU WITHOU T INCIDENT. REPLACED AND SECURED O-RING AT LEFT WING FUEL PROBE FIRST OUTBOARD FROM HEATER BLANKET. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002041100123 20020411 00123 NM 2002 4 11 DL72E020366 1 20020323 A 3350 900542 BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 21481 AFT EMERGENCY EXIT SIGN INOP. REPLACED BATTERY RACK AND LIGHT ASSY. 2 L 7 3 4F A3WE 2002041100124 20020411 00124 WP 2002 4 11 AALA20020317 1 20020316 A 4990 LINE DOUG DC9 DC982 3022082 WP APU OIL SYSTEM LEAKING A AALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 44503 49797 DFW - FLT 1954 - AFTER TAKEOFF DFW, RETURNED TO DFW DUE TO SMOKE AND BURNING RUBBER SMELL IN CABIN. LANDED DFW OVERWEIG HT WITHOUT INCIDENT. TIGHTENED APU OIL COOLER LINE. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002041100125 20020411 00125 NM 2002 4 11 DL72L020320 1 20020317 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 512DA 21314 FOUND LEFT OVERWING EMERGENCY LIGHT NOT ILLUMINATING. REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY. 2 L 7 3 4F A3WE 2002041100126 20020411 00126 NM 2002 4 11 AALA20020319 1 20020317 A 3397 WIRE BOEING 767 767223 1385123 NM FWD GALLEY DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 303AA 22309 LAX - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002041100127 20020411 00127 NM 2002 4 11 AALA20020321 1 20020317 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 36G INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT WIR E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002041100128 20020411 00128 NM 2002 4 11 AALA20020322 1 20020317 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 36C INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT WIR E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002041100129 20020411 00129 NM 2002 4 11 AALA20020323 1 20020313 A 3350 SIGN BOEING 777 777223 1385213 NM GALLEY EXIT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT GALLEY BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002041100138 20020411 00138 NM 2002 4 11 DL72L020321 1 20020317 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 512DA 21314 FOUND EMERGENCY LIGHT AT CENTER AISLE OVERHEAD NEXT TO OVERWING EXITS INOP DURING LAYOVER CHECK. REPLACED BATTERY ASSY, OP CHECK GOOD. 2 L 7 3 4F A3WE 2002041100139 20020411 00139 NM 2002 4 11 DL757020294 1 20020311 A 3620 WARNING SYSTEM BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 634DL 23615 716448 LEFT ENGINE HIGH STAGE LIGHT ON TAKEOFF ROLL. ABORT AT 100 KTS. PERFORMED HIGH EMER STOP/ RTO INSP PER AMM 05-51-14-2. NO DEFECTS FOUND. LOCKED HPPRSOV PER MEL 36-11-02. REMOVED, CAPPED & SECURED CANNON PLUG PER SAME. FWD TO MCO/PLC P ER MEL 36-11-02. CLSD/ SECURED COWLS. 2 L 7 2 4F 4 F RT A2NM E17NE 2002042200142 20020422 00142 NM 2002 4 22 QXEA0200551 1 20020410 A 7712 311835404 TSCU DHAV DHC8 DHC8202 2809007 NM ENGINE FAULTY A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 355PH 4418 500 SEA - ABORTED TAKEOFF, AUTO FEATHER FAILED TO ARM. REPLACED BOTH ENGINE TSCU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2002041100140 20020411 00140 NM 2002 4 11 DL757020296 1 20020311 A 2782 NUT BOEING 757 757232 1384965 NM L/E SLAT LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 RT AND LT WINGS L/E ROTARY ACTUATORS, TORQUE TUBE SPLINE RETAINING NUTS LOOSE. TORQUED RETAINING NUTS AS PER M/M 27-81- 18-4. 2 L 7 2 4F RT A2NM 2002041100141 20020411 00141 NM 2002 4 11 DL757020297 1 20020114 A 5320 114N33108402 SPLICE BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 WHILE REPLACING LOOSE SEALER AT THE FUSELAGE STATION 900 SPLICE CORROSION WAS FOUND. THE CORROSION EXTENDED FROM STR 16 R TO STR 13R ON THE STA 900 SPLICE STRAP. THE SPLICE STRAP WAS REMOVED AND REPLACED DUE TO THE CORROSION BEING OUT OF LIMITS. 2 L 7 2 4F RT A2NM 2002041100142 20020411 00142 NM 2002 4 11 DL757020331 1 20020318 A 3397 WIRE BOEING 757 757232 1384965 NM CABIN PULLED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 633DL 23614 EMERGENCY LIGHT AT SEAT 6CD INOP. FOUND SEAT WIRING HARNESS CONNECTOR WIRE PULLED OUT. REPLACED HARNESS. 2 L 7 2 4F RT A2NM 2002041100143 20020411 00143 NM 2002 4 11 DL757020355 1 20020321 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 621DL 22911 R4 DOOR EXT EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY AND BATTERY. OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002041100144 20020411 00144 NE 2002 4 11 DL757020361 2 20020322 A 7261 GARLOCK SEAL BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 641DL 36686 23995 716541 LEFT ENG OIL QTY DECREASING DURING FLIGHT. DECREASED TO -0- ON APPROACH. REPLACED NUMBER 5 BEARING COVER GARLOCK SEAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041100145 20020411 00145 NM 2002 4 11 DL757020369 1 20020325 A 3330 MS25306222 SWITCH BOEING 757 757232 1384965 NM CARGO BAY FAULTY A DALA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE IN INSP/MAINT 1 SO 27 632DL 23613 ON L/O CHECK, AFT CARGO LIGHT SWITCH CAUGHT ON FIRE. REPLACED SWITCH. 2 L 7 2 4F RT A2NM 2002041100146 20020411 00146 NM 2002 4 11 DL757020381 1 20020328 A 3350 SPLICE BOEING 757 757232 1384965 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 654DL 24394 EMERGENCY LIGHTS FROM SEAT 20 TO 26 GO FROM OUT TO ALMOST BRIGHT. FOUND BAD SPLICE AT SEAT 20 DEF. REPAIRED SPLICE AND RELAMPED, CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002041100147 20020411 00147 2002 4 11 DL757020394 4 20020401 A 2565 D30655133 SLIDE BOEING 757 757232 1384965 NM L2 DOOR FAILED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 697DL 30318 ON ARRIVAL L2 DOOR WAS NOT DISARMED AND DOOR WAS OPENED. DOOR ASSIST BOTTLE FIRED AND SLIDE PACK REMAINED UNINFLATED. PINNED BOTTLE AND REMOVED SLIDE PACK ASSY 715913. REPLACED SLIDE AND DOOR EMERGENCY POWER RESERVOIR PER M/M 393247. 2 L 7 2 4F RT A2NM 2002041100148 20020411 00148 NM 2002 4 11 DL757020395 1 20020302 A 5755 113N55045 SPOILER BOEING 757 757232 1384965 NM WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 SPOILER WAS FOUND WITH ELONGATED HOLE IN THE OUTBOARD VERTICAL FLANGE COMMON TO THE SPAR. REPAIR PER ER/A 411144-14 AND NORDAM EWO E0037096. 2 L 7 2 4F RT A2NM 2002041100149 20020411 00149 EA 2002 4 11 COMA0260242 1 20020410 A 5300 BEAM CNDAIR CL600 CL6002B19 1900309 EA FS623.00 TO 640. CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 957CA 14975 7109 LEFT ENGINE SUPPORT BEAM CRACKED.PERFORMED REPAIR TO LEFT ENGINE SUPPORT BEAM I/A/W BOMBARDIER REO 601R-53-61-366 REVC. 2 L 7 2 4F RT A21EA 2002041100150 20020411 00150 NM 2002 4 11 DL75A020334 1 20020318 A 5310 143N85121 DOOR FRAME BOEING 757 757212 1384951 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752AT 23128 C1 DOOR OPENING LOWER CHORD CORRODED, THE FS 620 OPENING FRAME OUTER CHORD AND WEB WERE CUT AND THE LOWER SECTIONS REMOV ED TO ALLOW ACCESS TO THE CHORD. AFTER REPLACEMENT OF THE CHORD, THE LOWER SECTION OF FRAME CHORD AND WEB WERE REINSTAL LED AND SPLICE WITH REPAIR ANGLES AND A DOUBLER PER ER/A 382597-14, REV A. 2 L 7 2 4F RT A2NM 2002041100151 20020411 00151 EA 2002 4 11 COMA0260243 1 20020410 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA FS623.00 TO 640. CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 957CA 14975 7109 RIGHT ENGINE SUPPORT BEAM CRACKED.PERFORMED REPAIR TO RIGHT ENGINE SUPPORT BEAM I/A/W BOMBARDIER REO 601R-53-61-366 REV C. 2 L 7 2 4F RT A21EA 2002041100152 20020411 00152 NM 2002 4 11 DL75A020335 1 20020318 A 5315 146N509116 FLOORBEAM BOEING 757 757212 1384951 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752AT 23128 THE UPPER CAP OF THE FS 1681 FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION. THE UPPER CAP WAS TRIMMED OFF TO REMO VE ALL AREAS OF CORROSION. A NEW CAP WAS FABRICATED AND INSTALLED PER ER/A 382554-14, REV A. 2 L 7 2 4F RT A2NM 2002041100153 20020411 00153 NM 2002 4 11 DL75A020336 1 20020316 A 3211 113N10704 TRUNNION BOEING 757 757212 1384951 NM RT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752AT 23128 INSPECTION OF THE RT MLG FWD TRUNNION SUPPORT FITTING FUSE PINS PER AD 2000-07-13 REVEALED CORROSION IN THE FUSE PIN LUG BORES OF THE FITTING. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG BORES AND INSTALLING OVERSIZED BUSHINGS. THE RE PAIR WAS ACCOMPLISHED PER ER/A 382613-14. 2 L 7 2 4F RT A2NM 2002041100154 20020411 00154 NM 2002 4 11 DL75A020347 1 20020320 A 5330 146N33054 SKIN BOEING 757 757212 1384951 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752AT 23128 THE FUSELAGE SKIN AND UNDERLYING BEAR STRAP WERE FOUND WITH AREAS OF CORROSION NEAR THE C2 DOOR CUTOUT AT FS 1440 AND ST RINGERS 25R-26R. THE CORROSION WAS REMOVED FROM THE BEAR STRAP AND ANOTHER IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH EXTERNAL DOUBLERS PER ER/A 382594-14, REV A. 2 L 7 2 4F RT A2NM 2002041100155 20020411 00155 NM 2002 4 11 DL764020222 1 20020223 A 1430 A10210D BOLT BOEING 767 767424ER 1385270 NM L/E SLAT SHEARED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 837MH 29710 AFTER EXTENDING FLAPS ON PUSHBACK HAD L/E SLAT ASYMMETRY MSG. FOUND TARGET MISSING DUE TO SLAT BOLT FAILED AND ROLLER M ISSING. FLEET HISTORY ITEM. 2 L 7 2 4F RT A1NM 2002041100156 20020411 00156 NM 2002 4 11 DL764020223 1 20020222 A 3610 7929305 COOLER BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 2 ENGINE FAILED A DALA O OTHER M OVER TEMP NR NOT REPORTED 1 SO 27 830MH 29701 706163 FOUND METAL IN OZONE CONVERTER. METAL CONTAMINATION A RESULT FROM A FAILED/MELTED ENGINE PNEUMATIC PRECOOLER, 767-400 F LEET HISTORY. REMOVED RT ENG RT CORE COWL. REMOVED PRECOOLER. INSTALLED PRECOOLER PER MM. INSTALLED CORE COWL, LEAK CHECK GOOD. ALSO REPLACED RIGHT ENGINE PRESSURE REGULATING VALVE. 2 L 7 2 4F 4 F RT A1NM E23EA 2002041100157 20020411 00157 NM 2002 4 11 DL764020247 1 20020301 A 2710 2832001007 ACTUATOR BOEING 767 767432ER 1385134 NM AILERON CRACKED A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 833MH 29706 ON LAYOVER, FOUND LT OUTBOARD AILERON ACTUATOR CRACKED. REPLACED SAME. 2 L 7 2 4F RT A1NM 2002041100158 20020411 00158 NM 2002 4 11 DL764020280 1 20020308 A 1430 114T41457 BOLT BOEING 767 767432ER 1385134 NM L/E SLAT SHEARED A DALA O OTHER N FALSE WARNING LD LANDING 1 SO 27 831MH 29702 L/E SLAT ASYMMETRY ILLUMINATED ON LANDING ROLLOUT. FOUND TARGET MISSING FROM NR 4 SLAT. FLEET PROBLEM. BOLT SHEARED, BEARING AND TARGET LOST. INSTALLED TARGET, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2002041100159 20020411 00159 GL 2002 4 11 DL764020283 2 20020308 A 7230 COMPRESSOR BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 1 ENGINE DAMAGED A DALA K NONE E VIBRATION/BUFFET AP APPROACH 1 SO 27 828MH 4507 4507 29699 706120 LT ENG N2 VIBES READING HIGH AT CRUISE DESCENT AND TAXI 3.2 TO 4.4. REPLACED LT ENG CRF ACCEL PER MM. RAN ENG PER PFHB . AT IDLE N2 VIBE RANGED FROM 1.6 TO 3.0 AT 95 PERCENT N1. N2 VIBES AT 2.2. REMOVED BORO TURNING PLUG AND PLUGS B3-2 AND B2-2. CLOSED COWLINGS. CHECKED MAIN ENG OIL CHIP DET, NO DEBRIS. C/W PBS4000 VIB SURVEY, FAN HI. BORESCOPED HRT CK/D OK. BORESCOPED HPC. FOUND 13 AND 14TH STAGE BLADES DAMAGED. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E23EA 2002041100160 20020411 00160 NM 2002 4 11 DL764020302 1 20020313 A 2750 N012300000 CIRCUIT CARD BOEING 767 767432ER 1385134 NM T/E FLAP FAULTY A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 829MH 29700 ON T/O FLL FLAP RETRACT GOT T/E FLAP DISAGREE BETWEEN 5 AND 15 DEG WITH ALT PROC FLAPS/SLATS WOULD NOT COME UP. RAN FLA PS OUT TO 20 DEG THEN AFTER 3 ATTEMPTS AND 40 MINS FLAPS RETRACTED. INSPECTED AND FOUND NO DAMAGE TO LE/TE FLAPS. REPL ACED CARD M11291 ADU CONTROL. RAN FLAP/SLAT BOTH ELEC/HYD SEVERAL TIMES, NO TROUBLE FOUND. T/S PER FIM. 2 L 7 2 4F RT A1NM 2002041100161 20020411 00161 2002 4 11 DL764020311 4 20020315 A 3425 H341CBM INDICATOR BOEING 767 767432ER 1385134 NM COCKPIT FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 838MH 29711 STANDBY GYRO FAILED. REPLACED STANDBY ADI, CHECKS NORMAL. 2 L 7 2 4F RT A1NM 2002041100162 20020411 00162 NM 2002 4 11 DL764020313 1 20020315 A 2782 271040006 ACTUATOR BOEING 767 767432ER 1385134 NM L/E SLAT MALFUNCTIONED A DALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 839MH 29712 RECEIVED ACARS FOR A FLAP DISAGREE ON CLIMBOUT FROM HNL, QRHB FOLLOWED AND WILL CONTINUE TO LAX. ON APPROACH IN LAX, FL APS/SLATS EXTENDED, FLAPS OK BUT HAD NO INDICATION THAT THE LEADING EDGE HAD EXTENDED. CREW CALLED FAA FOR EMERGENCY EQ UIPMENT. NORMAL LANDING. THE CAPTAIN TOLD MTC UPON ARRIVAL VISUAL INSPECTION SHOWS THE L/E WERE DOWN. MTC IN PROGRESS . LAX MTC T/S PER FIM AND FOUND THE NR 7 ROTARY ACT TRIPPED. RESET AND OPS OK. REPLACE ALTERNATE IN/BD SLAT DRIVE MOT OR PER M/M ALL. CHECKS GOOD. 2 L 7 2 4F RT A1NM 2002041100163 20020411 00163 2002 4 11 DL764020314 4 20020315 A 2310 8220987003 COUPLER BOEING 767 767432ER 1385134 NM E/E BAY DEFECTIVE A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 843MH 29716 AIRBORNE UNABLE XMIT ON EITHER HF. RADIO. HAD A VALID OK ON THE GROUND BEFORE DEPARTURE. TRIED NEW HF XCVRS, NO HELP. REPLACED LEFT AND RIGHT HF COUPLERS. BOTH SYSTEMS TEST GOOD. 2 L 7 2 4F RT A1NM 2002041100164 20020411 00164 NM 2002 4 11 DL764020329 1 20020318 A 2752 256T63102 ACTUATOR BOEING 767 767432ER 1385134 NM T/E FLAP MALFUNCTIONED A DALA K NONE F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 829MH 29700 AFTER T/O FLAP RETRACTION, T/E FLAP DISAGREE EICAS MSG. RAISED FLAPS USING ATLN SYS. FOUND NR 6 ROTARY ACTUATOR TRIPPE D. CYCLED FLAPS SEVERAL TIMES, OPN NORMAL. REPLACED NR 6 FLAP ROTARY ACTUATOR PER AMM, CHECK NORMAL. 2 L 7 2 4F RT A1NM 2002041100165 20020411 00165 NM 2002 4 11 DL764020360 1 20020322 A 2782 PDU BOEING 767 767432ER 1385134 NM L/E SLAT FAULTY A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 825MH 29696 ALTERNATE SLAT INBOARD ELECTRIC ACTUATOR POPPED C/B. REPLACED SLAT PDU INBD ELECT MOTOR. OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2002041100166 20020411 00166 NM 2002 4 11 DL764020363 1 20020323 A 4900 38850273 DUCT BOEING 767 767432ER 1385134 NM APU LEAKING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 835MH 29708 FOUND 3 WAY DUCT CRACKED. REPLACED DUCT. LEAK CHECKS NORMAL. 2 L 7 2 4F RT A1NM 2002041100167 20020411 00167 NM 2002 4 11 DL764020364 1 20020323 A 4950 38850273 DUCT BOEING 767 767432ER 1385134 NM APU CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 829MH 4260 29700 P1007 APU PNEUMATIC T-DUCT FOUND CRACKED. FLEET PROBLEM. REMOVED AND REPLACED DUCT. LEAK CHECKS NORMAL. 2 L 7 2 4F RT A1NM 2002041100168 20020411 00168 NM 2002 4 11 DL76G020233 1 20020226 A 2530 811150417 COFFEEMAKER BOEING 767 767324 1385203 NM GALLEY MALFUNCTIONED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 394DL 27394 DURING CRUISE A BURNING ELECTRICAL SMELL IN FORWARD GALLEY FAULT TRACED TO NUMBER 1 COFFEEMAKER. REMOVED SAME, CB PULLE D AND COLLARED NIS LGW FWD TO MCO AND PLACARD PER MEL. CB PULL FOR COFFEEMAKER 2 AS PRECAUTION. 2 L 7 2 4F RT A1NM 2002041100169 20020411 00169 NM 2002 4 11 DL76G020260 1 20020303 A 2530 ODOR BOEING 767 7673P6 1385105 NM CABIN DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1501P 24983 FLIGHT ATTENDANTS REPORTED ELECTRICAL SMOKE/FIRE SMELL AT 2R DOOR. TURNED OFF 2R LIGHTS, SMELL DISSIPATED. CHECKED ELE CTRICAL SYS IN AREA, CK LIGHTS AND GALLEY APPLIANCES. 2 L 7 2 4F RT A1NM 2002041100170 20020411 00170 NM 2002 4 11 DL76G020261 1 20020303 A 2560 BATTERY BOEING 767 767332 1382001 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1608 30573 FWD MID ATT SEAT FLASHLIGHT INOP. REPLACED BATTERY, OPS NORMAL. 2 L 7 2 4F RT A1NM 2002041100171 20020411 00171 NM 2002 4 11 DL76G020275 1 20020308 A 2620 LINE BOEING 767 7673P6 1385105 NM LINE CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 DURING HMV IT WAS FOUND THAT A C-2 CARGO COMPARTMENT FIRE EXTINGUISHER DISCHARGE LINE WAS CHAFING ON APU AIR SUPPLY DUCT . REPLACED LINE. 2 L 7 2 4F RT A1NM 2002041100172 20020411 00172 NM 2002 4 11 DL76G020301 1 20020313 A 2560 333101582 BATTERY PACK BOEING 767 7673P6 1385105 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 152DL 29831 24984 OVERWING EMERGENCY ESCAPE SYS SQUIB TEST 1 FAILED ON LEFT SIDE. TEST 2 FAILED ON RIGHT SIDE. REPLACED EMERGENCY BATTER IES M961 AND M962 PER M/M. ALL SQUIB, TESTS OK. 2 L 7 2 4F RT A1NM 2002041100173 20020411 00173 NM 2002 4 11 DL76G020317 1 20020316 A 2160 3987505 CONTROL VALVE BOEING 767 767332 1382001 NM AIR CONDITIONING FAULTY A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 1605 30198 LT PACK TEMP OFF MULTIPLE TIMES BUT ALWAYS RESET. LT AND RT TEMP CONTROL VALVES FAULTED. REPLACED BOTH VALVES. 2 L 7 2 4F RT A1NM 2002041100174 20020411 00174 NM 2002 4 11 DL76G020371 1 20020325 A 3350 CHARGER BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1613B 32776 EMERGENCY LIGHTS AT SEATS 10GF - 11GF INOP. REPLACED BATTERY CHARGER M1209, OPS NORMAL. 2 L 7 2 4F RT A1NM 2002041100175 20020411 00175 NM 2002 4 11 DL76G020372 1 20020325 A 4950 ODOR BOEING 767 7673P6 1385105 NM CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 154DL 17858 25241 P1542 RAN APU FOR 10 HRS FROM MADRID. AFTER LANDING SELECTED APU BLEED TO OPERATE BOTH PACKS. CABIN FILLED WITH THIN HAZE AN D FLT ATT REPORT ELECTRICAL ODOR. RAN APU PNEU SYS, RAN BOTH PACKS WITH AND WITHOUT RECIRC FAN AND NO HAZE OR ODORS FOU ND. APU PNEU SYS, OPS OK. 2 L 7 2 4F RT A1NM 2002041100176 20020411 00176 NM 2002 4 11 DL76L020240 1 20020228 A 2720 285T0014104 MODULE BOEING 767 767332 1382001 NM E/E BAY MALFUNCTIONED A DALA K NONE F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 186DN 27962 YELLOW RUDDER RATIO CAUTION MESSAGE ILLUMINATED TWICE MOMENTARILY. NOTICED SLIGHT YAWING MOVEMENT ON CLIMBOUT BUT NOTHI NG IN CRUISE. NO FAULTS LATCHED ON RUDDER RATIO MODULES OR SAM MODULES. NO ECS FAULTS. REPLACED RT RUDDER RATIO CHANG ER MODULE PER MM. ALL TEST OK. 2 L 7 2 4F RT A1NM 2002041100177 20020411 00177 NM 2002 4 11 DL76L020245 1 20020301 A 7921 COOLER BOEING 767 767332 1382001 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE DEFECTIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 181DN 30384 25986 727524 ON CLIMB REPORTED ENG OIL TEMP HIGH. CONFIRMED NOT A INDICATION PROBLEM. MTC IN WORK. OIL FILTER/CHIP DETECTOR CLEAN. NO EEC FAULTS. T/S PER FIM NO FAULTS. REPLACED AIR/OIL COOLER AND VALVE. ALSO REPLACED FUEL/OIL COOLER BY PASS VALV E. 2 L 7 2 4F 4 F RT A1NM E46NE 2002041100178 20020411 00178 NM 2002 4 11 DL76L020286 1 20020310 A 2150 62594610 CONTROLLER BOEING 767 767332 1382001 NM E/E BAY MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 186DN 27962 AFTER APPROX 30 MINUTES OF FLIGHT RIGHT PACK TRIPPED OFF. CREW ATTEMPTED RESET AND PACK TRIPPED OFF AGAIN. PERFORMED B ITE ON PACK TEMP CONTROLLER AND NO FAULTS. REPLACED PACK TEMP CONTROLLER DUE TO SHOP HISTORY ON PREV ACFT. ALSO REPLAC ED FLOW CONTROL SOV AS A PRECAUTION. 2 L 7 2 4F RT A1NM 2002041100179 20020411 00179 NE 2002 4 11 DL76L020306 2 20020312 A 7230 BLADE BOEING 767 767332 1382001 NM PWA 4090 PW4090 52119 NE NR 2 ENGINE DAMAGED A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 173DN 26436 724719 24800 724719 JFK MTC FOUND SURGE MESSAGE ON EICAS. MTC THEN BORESCOPED ENGINE FOUND COMPRESSOR BLADE DAMAGE. REPLACED RT ENGINE PER TRANSMITTAL 1T149. 2 L 7 2 4F 4 F RT A1NM E46NE 2002041100180 20020411 00180 NE 2002 4 11 DL76L020315 2 20020316 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 SURGES A DALA K NONE J WARNING INDICATION TO TAKEOFF 1 SO 27 176DN 8739 25061 727893 UPON ARRIVAL ATL LEFT ENG SURGE DET MTC MESSAGE FOUND. EDR SURGE REPORT CONFIRMED SURGE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041700103 20020417 00103 EU 2002 4 17 QXEA02002539 1 20020402 A 4920 38075412 APU FOKKER F28 F28MK4000 4990810 EU APU BAY MALFUNCTIONED A QXEA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION UK UNKNOWN 1 NM 09 492US 1033 11159 BIL- WHEN ENTERING AIRCRAFT IT WAS FULL OF SMOKE AND THE LAVATORY SMOKE ALARM WAS GOING OFF. APU WAS RUNNING, BOTH DUCT TEMPS IN GREEN ARC. REPLACED APU. GROUND RAN APU, NO LEAKS NOTED. ALL INDICATION NORMAL DURING RUN. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A20EU 2002041100182 20020411 00182 NM 2002 4 11 CALA0200190 1 20020408 A 5414 SKIN BOEING 737 7373T0 1384582 NM L/H PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND A 1/4" CRACK IN UPPER PYLON SKIN PANEL #5727L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED I AW ECRA 5430-01230, REV. B. 2 L 7 2 4F RT A16WE 2002041100183 20020411 00183 NM 2002 4 11 CALA0200194 1 20020410 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 727D-827 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND STRINGER 26L CORRODED IN AFT BAGGAGE BIN AT BS 727D-827. THE CORRODED SECTION OF STRINGER WAS REMOVED A ND REPAIR SPLICES WERE INSTALLED IAW ECRA 5311-01119. 2 L 7 2 4F RT A16WE 2002041100184 20020411 00184 SO 2002 4 11 C2XA02TY071 1 20020411 A 2731 14522150401 BELLCRANK EMB 145 EMB145LR 3260212 SO EMPENAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 TYS, During a scheduled EA2730-01044 inspection of the elevator control system, the right hand rear mechanism quadrant b ellcrank was found cracked. Maintenance removed and replaced the bellcrank. I/A/W-EMB-145-MM-27-31-01. Operational check ed good, aircraft released to service. 2 L 7 2 4T RT T00011AT 2002041100185 20020411 00185 EA 2002 4 11 SWIA200210772 1 20020406 A 2120 FILTER CNDAIR CL600 CL6002B19 1900309 EA DISPLAY COOLING DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 410SW 7066 ''DISPLAY COOL'' CAUTION MESSAGE DURING FLIGHT. MESSAGE PERSISTED AFTER 1ST STEP PER QRH. MESSAGE WENT AWAY AFTER SWIT CHING TO STBY. RETURNED TO SLC. REMOVED AND REPLACED THE DISPLAY FILTER AS REQUIRED. OPS CHECK GOOD. PN 196305. 2 L 7 2 4F RT A21EA 2002041200018 20020412 00018 WP 2002 4 12 GTIA020190 1 20020103 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND AFT PIT STATION 1334 L18L-L18R CORROSION ON FRAME WEB, STIFFENERS, UPPER/LOWER FLANGES (AFT SIDE OF FRAME). ONE VERTICAL STIFFENER OUT OF LIMITS. FABRICATED DRILLED AND LOCATED NEW STIFFENER. INSTALLED NEW STIFFENER PER SRM M D80 51-30-2. (M) 2 L 7 2 4F A6WE 2002041200019 20020412 00019 WP 2002 4 12 GTIA020191 1 20020108 A 5310 STRUCTURE DOUG DC9 DC982 3022082 WP LAVATORY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FORWARD LAVATORY HAS CORROSION AT LOWER FLOOR, INSIDE TRASH CAN AREA CORROSION FOUND AFTER TRASH CAN REMOVAL. MATERIAL OUT OF LIMITS. FABRICATED PART. INSTALLED PART IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002041200020 20020412 00020 WP 2002 4 12 GTIA020192 1 20020108 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - PAX CABIN FLOORBOARDS TWO DELAMINATED AT AFT GALLEY SERVICE DOOR THRESHOLD. REMOVED DELAMINATED FLOORBOARDS. REP AIRED PAX CABIN FLOORBOARDS. INSTALLED FLOORBOARDS AT AFT GALLEY SERVICE DOOR THRESHOLD. (M) 2 L 7 2 4F A6WE 2002041200021 20020412 00021 WP 2002 4 12 GTIA020198 1 20020104 A 5320 WEB DOUG DC9 DC982 3022082 WP EMERGENCY EXIT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - RIGHT, LEFT OUTBOARD CUSP WEB AT EMERGENCY EXIT CRACKED IN SEVERAL PLACES. REMOVED DAMAGED AREA. FABRICATED DOUB LER AND FILLER RIGHT SIDE. FABRICATED DOUBLER AND FILLER LEFT SIDE. INSTALLED LEFT AND RIGHT DOUBLERS AND FILLERS IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002041200027 20020412 00027 WP 2002 4 12 GTIA020206 1 20020121 A 5755 STRUCTURE DOUG DC9 DC982 3022082 WP SPOILER WARPED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND LEFT WING, OUTBOARD FLIGHT SPOILER WARP/DELAMINATED. REMOVED LEFT OUTBOARD SPOILER. INSTALLED LEFT OUTBOAR D FLIGHT SPOILER. (M) 2 L 7 2 4F A6WE 2002041200034 20020412 00034 2002 4 12 GTIA020213 4 20020305 A 3418 VANE DOUG DC9 DC981 3022081 WP AOA SYSTEM FAILED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 810NK 48015 DTW - FLT 1258 - AUTOTHROTTLE WORKED UNTIL REACHING CRUISE AT 29,000 THEN WENT OFF LINE COULD NOT RE-ENGAGE. REMOVED AN D REPLACED RIGHT AOA VANE PER MD80 MM 34-19-01, SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002041200035 20020412 00035 NM 2002 4 12 GTIA020214 1 20020302 A 2720 LINKAGE DOUG MD80 MD83 3023681 NM RUDDER LACK OF LUBE A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 822NK 49392 RSW - FLT 1525A - FOUND RUDDER TRAVEL UNRESTRICTED LIGHT DID NOT COME ON UNTIL AIRCRAFT TOUCHED DOWN. SPEED ON FINAL WA S 104 K. LUBRICATED BEARINGS IN CONTROL LINKAGES AND ADJUSTED RIGGING ON RUDDER THROW LIMITER SYSTEM. ALL WORK IAW MD8 0 MM 27-20-00. (M) 2 L 7 2 4F RT 2002041200036 20020412 00036 WP 2002 4 12 GTIA020215 1 20020109 A 7110 COWLING DOUG DC9 DC982 3022082 WP RT ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - RT ENGNE NOSE COWL ACCOUSTIC LINING HAS APPROX 48 FASTENERS PULLED THROUGH, RIGHT ENGINE NOSE COWL ACCOUSTIC LININ G HAS BAD REPAIR AT 6 O'CLOCK POSITION. RT ENGINE NOSE COWL ACCOUSTIC LINING HAS THREE BAD REPAIRS FROM 12-10 O'CLOCK P OSITIONS. RIGHT ENGINE NOSE COWL L/E HAS ERROSION AND PITTING. REMOVED NR 2 ENGINE NOSE COWL TO SEND OSV, REINSTALL AFTER SERVICE. INSTALLED SERVICEABLE NR 2 NOSE COWL. (M) 2 L 7 2 4F A6WE 2002041200037 20020412 00037 WP 2002 4 12 GTIA020216 1 20020110 A 7110 COWLING DOUG DC9 DC982 3022082 WP LT ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FTW - FOUND P/N 11-N-00304 LEFT ENGINE NOSE COWL ACCOUSTIC LINER IS FASTENERS AT 3 O'CLOCK POSITION AND 1 FASTENER AT 9 O'CLOCK ARE PULLED THROUGH. P/N 11-N-00316, REMOVE NR 1 ENGINE NOSE COWL TO SEND OSV, REINSTALL AFTER SERVICE. INSTALL ED SERVICEABLE NOSE COWL. (M) 2 L 7 2 4F A6WE 2002041200038 20020412 00038 WP 2002 4 12 GTIA020217 1 20020309 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP COCKPIT DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 603CA 49508 DTW - FOUND EMERGENCY LIGHTS IN COCKPIT AND ENTRY WAY WILL NOT SHUT OFF. BATTERY PACK STUCK IN ARM. REMOVED AND REPLAC ED BATTERY PACK. OPS CHECK GOOD IAW 33-53-01. (M) 2 L 7 2 4F A6WE 2002041200039 20020412 00039 WP 2002 4 12 GTIA020218 1 20020309 A 2761 CONTROL ARM DOUG DC9 DC982 3022082 WP SPOILER ACTUATOR OUT OF RIG A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 603CA 49508 TPA - FOUND AUTO SPOILER DO NOT USE LIGHT ON AFTER TAKEOFF. RE-POSITIONED CONTROL ARM ON AUTO SPOILER ACTUATOR IAW MD80 MM 27-62-05. OPS CHECK GOOD. COULD NOT DUPLICATE. (M) 2 L 7 2 4F A6WE 2002041200040 20020412 00040 WP 2002 4 12 GTIA020219 1 20020309 A 5310 LATCH DOUG DC9 DC982 3022082 WP GIRT BAR BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 ACY - FLT 1304 - LATCH HOLDING GIRT BAR TO R1 DOOR IS BROKEN. FOUND BRACKET FOR GIRT BAR LATCH LOOSE RE-SECURED BRACKET IAW MM 25-62-00, OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2002041200041 20020412 00041 2002 4 12 GTIA020220 4 20020308 A 2213 25866865 COMPUTER DOUG DC9 DC932 3022066 WP PITCH AXIS MALFUNCTIONED A GTIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 23 12536 47113 FLT 8011 - ACY - ON STABILIZED DESCENT AUTOPILOT SUDDENLY PITCHED DOWN THEN PITCHED UP. REMOVED AND REPLACED PITCH AXIS COMPUTER IAW MM 27-13-1, OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2002041200042 20020412 00042 2002 4 12 GTIA020221 4 20020308 A 3497 CIRCUIT BREAKER DOUG DC9 DC981 3022081 WP NAV TRANSFORMER FAILED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FLL - NAV INST XFMR L C/B-F16 TRIPPED CAUSED 1, ALT WINDOWS TO GO BLANK 2 ART TO FIRE 3, NO AUTO THROTTLE. FOUND NR 1 N AV INST TRANSFORMER C/B WEAK NO HOLDING. REMOVED AND REPLACED THE 2A C/B IAW MM 31-15-01. OP CHECK NORMAL. PERFORMED OPERATIONAL CHECK OF AUTOTHROTTLE SYSTEM IAW MM 22-30-00 NORMAL. NO FAULT INDICATION FOR ART SYSTEM IAW 73-20-00. CHEC K NORMAL. (M) 2 L 7 2 4F A6WE 2002041200043 20020412 00043 2002 4 12 GTIA020222 4 20020305 A 3418 VANE DOUG DC9 DC981 3022081 WP AOA SYSTEM DAMAGED A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 810NK 48015 DTW - FLT 1258 - AUTOTHROTTLE WORKED IN UNTIL REACHING CRUISE AT 29,000 THEN WENT OFF LINE COULD NOT RE-ENGAGE. REMOVED AND REPLACED RIGHT AOA VANE PER MD80 MM 34-19-01, SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002041200044 20020412 00044 WP 2002 4 12 GTIA020223 1 20020125 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 603CA 49508 FTW - FOUND RIGHT OUTBOARD SEAT TRACK HAS GOUGES AT STATIONS 655, 687, 716. REMOVED GOUGES AT STATION 716. REMOVED TRA CK SECTION FROM 702-722. LOCATED AND DRILLED AND COUNTERSINKING. INSTALLED SEAT TRACK AND SPLICE IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002041200045 20020412 00045 WP 2002 4 12 GTIA020224 1 20020312 A 2760 59369715503 CONTROL VALVE DOUG DC9 DC983 3022083 WP SPOILERS FAILED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 DTW - FOUND INBOARD SPOILERS ON BOTH WINGS DO NOT DEPLOY ON GROUND. REMOVED AND REPLACED RIGHT GROUND SPOILER CONTROL V ALVE PER MD80 MM 27-62-04, SYSTEM OP CHECK AND LEAK CHECKED GOOD. (M) 2 L 7 2 4F RT A6WE 2002041200046 20020412 00046 WP 2002 4 12 GTIA020225 1 20020205 A 3350 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DEFECTIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 807NK 49777 FTW - FOUND NUMEROUS OVERHEAD EMERGENCY LIGHTS BURNED OUT IN PAX CABIN. REMOVED DEFECTIVE BATTERY PACKS AT SEAT 5 RIGHT AND 20 RIGHT. TROUBLESHOT SYSTEM AND FOUND BATTERIES IN NEED OF CHARGE REF MD80 WDM 33-51-12. (M) 2 L 7 2 4F RT A6WE 2002041200047 20020412 00047 WP 2002 4 12 GTIA020226 1 20020204 A 2560 BATTERY DOUG DC9 DC987 3022087 WP FLASHLIGHT DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 807NK 49777 FTW - FOUND FOUR EMERGENCY CABIN FLASH LIGHT REQUIRE NEW BATTERIES. REPLACED BATTERIES 94) IAW MD80 MM 25-60-00. (M) 2 L 7 2 4F RT A6WE 2002041200048 20020412 00048 WP 2002 4 12 GTIA020227 1 20020312 A 3350 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 810NK 48015 ACY - FOUND RIGHT AFT OVERWING EMERGENCY DOOR EXIT LIGHT AND LEFT AFT OVERWING EMERGENCY DOOR EXIT LIGHT INOPERATIVE. R EMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY OVER SEAT 23D OPERATION CHECK NORMAL IAW MM 33-53-00. (M) 2 L 7 2 4F A6WE 2002041200049 20020412 00049 WP 2002 4 12 GTIA020229 1 20020314 A 3222 STRUT DOUG DC9 DC983 3022083 WP NLG DISCHARGED A GTIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 825NK 53012 DTW - FLT 906 - AIRCRAFT NOSE WHEEL WOULD NOT TURN ON TAXI OUT. RETURN TO GATE. SERVICED NOSE LANDING GEAR STRUT AS RE QUIRED IAW MD80 MM CH 12-21-04. NOSE WHEEL STEERING OPS CHECK GOOD IAW MD80 MM 32-50-00. (M) 2 L 7 2 4F RT A6WE 2002041200050 20020412 00050 2002 4 12 GTIA020230 4 20020314 A 2565 LANYARD DOUG DC9 DC983 3022083 WP ESCAPE SLIDE DETACHED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 MYR - FLT 557 - FORWARD GALLEY ESCAPE SLIDE LANYARD IS OFF. REINSTALLED LANYARD ON FORWARD GALLEY ESCAPE SLIDE IAW MD80 MM 25-62-00. NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2002041200052 20020412 00052 NE 2002 4 12 ALG2002F00008 1 20020225 A 2611 30231R7B SMOKE DETECTOR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL CARGO BAY FAILED E ALGA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 03 717AL 760221 CAE890539S ON ENGINE START, FOUND BAGGAGE COMPARTMENT SMOKE DETECTOR FAILED TEST. 1 G 7 2 3U 3 U H1NE E1GL 2002041200053 20020412 00053 SW 2002 4 12 ALG2002F00018 1 20020318 A 6310 406040580103 SPRAG CLUTCH BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FREEWHEEL UNIT WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 607AL 53264 CAE847048 DURING OVERHAUL FOUND, CAGE SLOTS WORN BEYOND MAX. LIMIT, 1 EACH SPRAG BREAKING DOWN ON INNER CAM FACE. TO PREVENT RECU RRENCE: STRONGER ALLOY. 1 G 7 1 3U 3 U O H2SW E1GL 2002041200054 20020412 00054 SW 2002 4 12 ALG2002F00019 1 20020318 A 6310 SPLINE ADAPTER BELL 407 BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FREEWHEEL UNIT WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 607AL 3556 A4722 53264 CAE847048 DURING OVERHAUL, FOUND SPLINE WEAR BELOW MIN. 1 G 7 1 3U 3 U O H2SW E1GL 2002041200055 20020412 00055 SW 2002 4 12 ALG2002F00020 1 20020319 A 6310 406040516101 SHAFT BELL 407 BELL 407 407 1182206 SW ALLSN 250C 250C20 03013 GL FREEWHEEL UNIT WORN E ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 847AL 4153 1672 A4073 53150 DURING REPAIR, FOUND SPLINE WEAR BELOW MIN. LIMIT. 1 G 7 1 3U 3 U O H2SW E4CE 2002041200056 20020412 00056 SW 2002 4 12 ALG2002F00021 1 20020204 A 3213 407050202101 CROSSTUBE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MLG CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 477AL 3690 53203 DURING DAILY INSPECTION, FOUND PITTING CORROSION ON CROSSTUBE .2500 INCH DEEP .5000 INCH ROUND. SCRAPPED CROSSTUBE. PR OBABLE CAUSE IS WATER ENTRAPMENT. ALMOST UNDETECTABLE WITH ALL PARTS INSTALLED. 1 G 7 1 3U 3 U O H2SW E1GL 2002041200057 20020412 00057 SW 2002 4 12 ALG2002F00022 1 20020204 A 3213 407050201115 CROSSTUBE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MLG CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 477AL 5567 53203 DAILY SERVICE CHECK, FOUND PITTING CORROSION ON CROSSTUBE AT STRAP ATTACH POINT. PROBABLE CAUSE IS WATER ENTRAPMENT. S CRAP CROSSTUBE. 1 G 7 1 3U 3 U O H2SW E1GL 2002041200058 20020412 00058 SW 2002 4 12 ALG2002F00023 1 20020221 A 3213 407050202101 CROSSTUBE BELL 407 407 1182206 SW MLG CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 437AL 5298 53141 DAILY SERVICE CHECK, FOUND HEAVY PITTING CORROSION UNDER WEAR PADS. SCRAPPED CROSSTUBE. PROBABLE CAUSE IS WATER ENTRAP MENT. EXTENT OF CORROSION ALMOST UNDETECTABLE WITH ALL PARTS INSTALLED. RECOMMEND INSPECTION BE DONE WITH CROSSTUBE RE MOVED FROM AIRCRAFT AND WEAR PADS REMOVED. INSPECTION SHOULD BE ON TIME SPECIFIC INTERVALS. 1 G 7 1 3U O H2SW 2002041200059 20020412 00059 GL 2002 4 12 ALG2002F00024 2 20020217 A 7250 23053299 TURBINE WHEEL BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 587AL 53248 TURBINE WAS RECEIVED IN SHOP FOR LOW POWER. FOUND AFTER REMOVAL OF COMBUSTION SECTION FOUND SULPHADATION ON 1ST STAGE W HEEL. 1 G 7 1 3U 3 U O H2SW E1GL 2002041200060 20020412 00060 SW 2002 4 12 ALG2002F00025 1 20020217 A 5530 206020113222 SPACER BELL 407 407 1182206 SW VERT STABILIZER SPINNING B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 567AL 4480 53246 REMOVING STABILIZER FROM AIRCRAFT AND NOTED SPACER SPINNING. WHILE STARTING TO REPAIR SPACER, BUBBLED PAINT WAS NOTED BY TIP CAP AND ON TRAILING EDGE CAPS. SPACER SPINNING IN HONEYCOMB, THE SPACER IS MANUFACTURED SMOOTH WITH NO SERATION S TO PREVENT SPINNING. WHEN TRAILING EDGE CAPS WERE REMOVED ARCING DAMAGE WAS NOTED 4 INCHES DOWN FROM TIP. CABLE ASSE MBLY, ANTI-COLLISION LIGHT HAD CHAFED INSIDE CAPS AND CAPS SHOWED EVIDENCE OF ARCING. 1 G 7 1 3U O H2SW 2002041200061 20020412 00061 SW 2002 4 12 ALG2002F00026 1 20020227 A 6310 406040516101 SHAFT BELL 407 407 1182206 SW FREEWHEEL UNIT WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 567AL 2199 2199 53246 DURING NORMAL OVERHAUL, FOUND SPLINE WORN BELOW MINIMUM. 1 G 7 1 3U O H2SW 2002041200062 20020412 00062 SW 2002 4 12 LS12002F00000 1 20020402 A 5313 20603181449 LONGERON BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUSELAGE CORRODED B LS1R K NONE O OTHER IN INSP/MAINT 1 EA 13 49718 7815 1917 DURING STRUCTUAL REPAIR OF ENGINE DECK. CORROSION WAS NOTICED ON THE RIGHT LONGERON RUNNING ALONG THE RIGHT SIDE OF THE ENGINE PAN. IT WAS NOTICED THAT RED DYE PENETRANT WAS COVERING THE AREA OF CORROSION . SOMEONE AT A PRIOR DATE HAD IN SPECTED THE AREA AND DID NOT CLEAN THE PENETRANT OFF WELL. THIS WE THINK CAUSED THE CORROSION OF THE LONGERON. THE LON GERON WAS OUT AT LIMITS SO IT WAS REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 2002041200063 20020412 00063 CE 2002 4 12 181421 1 20020409 A 3260 INDICATOR BEECH 58 58 1152740 CE MLG MALFUNCTIONED E DEBA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CE 03 18142 TH1270 PILOT REPORTED NO GEAR DOWN AND LOCKED INDICATION WAS OBSERVED ON PREPARATION FOR LANDING. CYCLED THE GEAR WITH NO CHAN GE IN THE INDICATION. AFTER A SAFE, NORMAL LANDING AND SHUTDOWN, HE TURNED THE MASTER BACK ON AND THE GEAR INDICATION W AS NORMAL. THE AIRCRAFT WAS JACKED UP AND A RETRACTION CHECK PERFORMED. NO FAULTS WERE FOUND. AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 1 L 7 2 3O 3A16 2002041200067 20020412 00067 CE 2002 4 12 H792002F00000 1 20020323 A 5551 12326231 BRACKET CESSNA 210 T210N 2073456 CE CONT O520 TSIO520* 17040 SO HORIZONTAL STAB CRACKED A H79A K NONE O OTHER IN INSP/MAINT 1 EA 11 155RR 2882 21063286 DURING ANNUAL INSPECTION NOTICED CRACKS IN THE LEFT AFT HORIZONTAL STABILIZER ATTACH BRACKET. IF BRACKET IS CRACKED, RE PLACE WITH IMPROVED BRACKET. 1 H 7 1 3O 3 O 3A21 E8CE 2002041200068 20020412 00068 EA 2002 4 12 WVBA2002007 2 20020404 A 8530 SL54002 CYLINDER HEAD PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE CRACKED E WVBA O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 01 42WP 198 318252038 RL604561A PILOT REPORTED HIGH CYLINDER HEAD TEMPERATURE AND RETURNED TO BASE. TECHNICIANS DISCOVERED A CRACK COMING OUT OF SPARK PLUG HOLE AN REMOVED INTERCYLINDER BAFFLING WHERE IT WAS FOUND TO RUN FROM SPARK PLUG HOLE TO FIRST COOLING FIN OF STEEL BARREL. THIS WHICH IS NR 6 POSITION WHICH EXPLAINS HIGH TEMPS. THERE APPEARS TO BE MACHINE MARKS IN AREA THAT ALLOWS INTAKE PUSH ROD TUBE TO PASS THROUGH THE COOLING FINS. THIS COULD NOT BE DETERMINED TO BE A CONTRIBUTING FACTOR. THE ASSEMBLY WAS REMOVED AND REPLACED. IN INSPECTION OF PUSHROD TUBE CUT-OUT AREA OF THE CYLINDER FINS (AS DISCUSSED ABOVE) IT IS NOTED THE CUT INTO THE MEAT OF THE CYLINDER HEAD WAS LEFT WITH A VERY SHARP EDGE. NO CHAMFER FOR STRESS RELIEF. 1 L 7 2 3O 3 O A20SO E14EA 2002042400086 20020424 00086 NM 2002 4 24 02FDEA00229 1 20020404 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 207FE 22929 FRAME CRACKED AT BS 1050, STR 26L. REMOVED AND REPLACED FRAME PER EA. 7-5310-63836. 2 L 7 3 4F A3WE 2002062000011 20020620 00011 NE 2002 6 20 02FDEA00231 2 20020406 A 7230 COMPRESSOR AIRBUS 310 A310 EU PWA JT9 JT9D7R4E1 52054 NE NR 1 ENGINE STALLED A FDEA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 25 419FE 345 SEVERAL COMPRESSOR STALLS ON NR 1 ENGINE FL350. NO OTHER PARAMETERS NOTED. BLED ENG AND SLOWLY BROUGHT POWER BACK IN. REMOVED AND REPLACED NR 1 ENGINE AFTER NUMEROUS PARTS REPLACED. 2 L 7 2 4F 4 F RT A35EU E3NE 2002042400087 20020424 00087 NM 2002 4 24 02FDEA00232 1 20020407 A 5311 FRAME BOEING 727 7272S2F 1384O81 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 207FE 22929 FRAME CRACKED AT BS 1130, STR 26R. REMOVED AND REPLACED FRAME PER SRM 51-40-3 FIG 1 & EA 7-5310-63837. 2 L 7 3 4F A3WE 2002041200069 20020412 00069 NM 2002 4 12 02FDEA00234 1 20020406 A 5242 SKIN BOEING 727 727277 138408S NM PWA JT8 JT8D NE E/E BAY DOOR CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 MAIN E/E BAY DOOR SKIN IS CHAFED AT LEFT AFT EDGE. R&R SKIN PER SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002041700086 20020417 00086 NM 2002 4 17 02FDEA00245 1 20020411 A 2611 SMOKE DETECTOR BOEING 727 727233 138408A NM CARGO BAY FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 283FE 22350 ON CLIMB LWR FWD CARGO SMOKE WARNING LIGHT AND BELL CAME ON. REMOVED AND REPLACED NR 1 & 2 FWD LWR CARGO COMP FIRE SUPP RESSION BOTTLES PER MM 26-17-014-2. INSTALL NEW FIRE EXTINGUISHER. REMOVED AND REPLACED 4 FWD CARGO COMP SMOKE DETECTI ON UNITS. 2 L 7 3 4F RT A3WE 2002050600090 20020506 00090 NM 2002 5 6 02FDEA00246 1 20020408 A 5532 FLANGE BOEING 727 7272S2F 1384O81 NM VERTICAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 207FE 22929 VERTICAL FIN MATING SURFACE FOR PANEL 9602 CORRODED (C55-391-30). REMOVED AND REPLACED FLANGE PER EA 7-5510-64063. 2 L 7 3 4F A3WE 2002041800139 20020418 00139 NM 2002 4 18 2002UALA00640 1 20020404 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 CABIN FLOORBEAM AT STATION 365 RBL 43 HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. EXCESSIVE MATERIAL WAS R EMOVED AND A STRAP REPAIR APPLIED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041800140 20020418 00140 NM 2002 4 18 2002UALA00641 1 20020404 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 CABIN FLOOR SUPPORT AT STATION 365 RBL 45 HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. FILLER AND DOUBLER I NSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041800141 20020418 00141 NM 2002 4 18 2002UALA00642 1 20020405 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 LEFT HAND CREASE BEAM WEB AT BODY STATION 1020-1023 HAS EXCESSIVE MATERIAL LOSS AFTER REMOVAL OF CORROSION. MAJOR REPAI R ACCOMPLISHED. CREASE BEAM WEB REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041800142 20020418 00142 NM 2002 4 18 2002UALA00643 1 20020405 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 LEFT HAND CREASE BEAM WEB AT BODY STATION 1020-1023 HAS EXCESSIVE MATERIAL LOSS AFTER REMOVAL OF CORROSION. MAJOR REPAI R ACCOMPLISHED. CREASE BEAM WEB REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041800143 20020418 00143 NM 2002 4 18 2002UALA00644 1 20020404 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 FUSELAGE SKIN AT RIGHT HAND AFT HORIZ SEAL IS CHAFED. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIRED WITH DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041800144 20020418 00144 NM 2002 4 18 2002UALA00645 1 20020404 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 BODY STATION 1809 LEFT HAND FUSELAGE SKIN CHAFED UNDER LOWER BANANA FAIRING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041200070 20020412 00070 2002 4 12 482DM40802 4 20020408 A 3442 MI5852221 TRANSCEIVER MTSBSI MU300 MU300 5780602 CE WX RADAR FAULTY E UVCA K NONE O OTHER NR NOT REPORTED 1 CE 03 482DM A088SA RADAR INDICATOR COMES ON THE GOES OUT WITHIN 10 MINUTES. REMOVE AND REPLACE RADAR R/T. 2 H 7 2 4F RT A14SW 2002041200071 20020412 00071 NE 2002 4 12 6049040502 2 20020405 A 7200 ENGINE LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE LEFT MALFUNCTIONED E J7SA E ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP LD LANDING 1 SW 05 126CX 3184 26 049 PCE305219 ON LANDING AND AFTER T/R DEPLOYMENT, SIC NOTICED LOP WARNING LIGHT, AND NO FUEL FLOW TO LT ENG. PERFORMED SHUTDOWN OF E NGINE ON ROLLOUT. MAINTENANCE INSPECTED OVERSPEED SHUTOFF VALVE, WHICH SHOWED TO BE ACTIVATED. INTERROGATION OF THE ED S FOUND T4.5 OPERATION HAD EXCEEDED 903.5 DEGREES CELSIUS IN TEMPERATURE. ENGINE WAS REMOVED AND SHIPPED TO PRATT & WHI TNEY FOR INVESTIGATION OF OVER TEMP OPERATION. 2 L 7 2 4F 4 F RT A10CE E35NE 2002041200072 20020412 00072 WP 2002 4 12 ABXA010814 1 20020402 A 5320 591013053 FITTING DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 NR 6 TEE CRACKED APPROXIMATELY 1 INCH LONG AT LONGERON 14. REPLACED THE NR 6 TEE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002041200073 20020412 00073 WP 2002 4 12 ABXA010816 1 20020404 A 5610 ROD DOUG DC9 DC932 3022066 WP WINDOW OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. FOUND UPPER HOOK NOT CLEARING TO ALLOW WINDOW TO OPEN. ADJUSTED UPPER ROD W INDOW IAW DC-9 MM, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002041200074 20020412 00074 WP 2002 4 12 ABXA010817 1 20020402 A 2740 591096231 JACKSCREW DOUG DC9 DC932 3022066 WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 VISUAL INSPECTION OF THE JACKSCREW ASSEMBLY THREADED AREA SHOWED PITTING ALONG TOP FLANGE OF THREADS. REPLACED THE JACK SCREW ASSEMBLY IAW DC-9 MM 27-40-01-4-001. 2 L 7 2 4F A6WE 2002041200075 20020412 00075 WP 2002 4 12 ABXA010818 1 20020410 A 3260 DOWNLOCK SWITCH DOUG DC8 DC863 302198A WP NLG MALFUNCTIONED A ABXA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 GL 23 823AX 46122 UPON LANDING, LANDING GEAR EXTENSION, THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. CHANGED BOTH BULBS, NO HELP . RECYCLED GEAR, NO HELP. RECYCLED GEAR A SECOND TIME AND GREEN LIGHT ILLUMINATED. INSPECTED NOSE LANDING GEAR, NO DE FECTS NOTED. REMOVED AND REPLACED THE NOSE LANDING GEAR DOWNLOCK POSITION SWITCH IAW DC-8 MM 32-60-00-2. CYCLED NOSE L ANDING GEAR 3 TIMES. NOSE LANDING GEAR EXTENSION, RETRACTION AND INDICATION OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2002041200076 20020412 00076 WP 2002 4 12 AT0200044 1 20020404 A 3230 CYLINDER DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A ZZDA K NONE J WARNING INDICATION CL CLIMB 1 SO 15 832AT 47451 NOSE GEAR INDICATED NO RETRACTION AFTER TAKEOFF. REMOVED AND REPLACED NOSE LANDING GEAR CYLINDER, OPS AND LEAK CHECK GO OD IAW DC-9 MM 32-3-6. 2 L 7 2 4F A6WE 2002041200077 20020412 00077 WP 2002 4 12 AT0200045 1 20020405 A 3230 ROD END DOUG DC9 DC932 3022066 WP NLG OUT OF ADJUST A ZZDA K NONE J WARNING INDICATION CL CLIMB 1 SO 15 832AT 47451 AFTER TAKEOFF NOSE LANDING GEAR FAILED TO RETRACT. ADJUSTED NOSE LANDING GEAR RETRACT CYLINDER ROD END AND PERFORMED LA NDING GEAR SYSTEM RETRACT AND EXTENSION TEST PER DC9 MM 32-32-6 AND 32-30-0. ALL INDICATIONS AND OPERATIONS NORMAL. 2 L 7 2 4F A6WE 2002041200078 20020412 00078 WP 2002 4 12 AT0200047 1 20020409 A 3232 ACTUATOR DOUG DC9 DC932 3022066 WP NLG DOOR STICKING A ZZDA K NONE J WARNING INDICATION CL CLIMB 1 SO 15 866AT 47168 FORWARD NOSE GEAR DOOR REMAINED OPEN ON DEPARTURE/BURNED DOWN FUEL, RETURNED TO BASE. FOUND NOSE GEAR DOOR MANUAL ACTUA TOR STICKING, LUBED ACTUATOR AND MANUALLY OPERATION PERFORMED GOOD, AIRCRAFT GOOD TO CONTINUE IAW M/M 32-00 AND 12-90. 2 L 7 2 4F A6WE 2002041200080 20020412 00080 EU 2002 4 12 AWXA200200313 1 20020314 A 5712 D57252580002 RIB AIRBUS 320 A320231 3930325 EU LT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 YWG - MAJOR REPAIR - DURING C-08 CHECK A CRACK WAS FOUND ON LT WING GEAR SUPPORT RIB 5, HOLE NR 82. MAINTENANCE OVERSIZ ED HOLE TO AND INSTALLED NEW FASTENER IAW AWA ER 26-5721-02093-TB2. 2 L 7 2 4F RT A28NM 2002041200081 20020412 00081 NM 2002 4 12 AWXA200200318 1 20020407 A 3350 20121 CHARGER BOEING 757 7572S7 1384962 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 903AW 23323 PHX - EEL - EMERGENCY ESCAPE PATH LIGHT (BULLNOSE) BETWEEN SEAT ROWS 7 AND 8 LT ARE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED BATTERY PACK CHARGER AT STA 375 REF MM 33-51-07, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002041200082 20020412 00082 EU 2002 4 12 AWXA200200320 1 20020312 A 5320 D53480043201 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 YWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON THE R2 DOOR SILL AT FR 68. MAINTENANCE FABRICATED AND INS TALLED REPAIR IAW SRM. 2 L 7 2 4F RT A28NM 2002041200083 20020412 00083 EU 2002 4 12 AWXA200200321 1 20020312 A 5320 D53480043200 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 YWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON THE L2 DOOR SILL AT FR 68. MAINTENANCE FABRICATED AND IN STALLED REPAIR IAW SRM. 2 L 7 2 4F RT A28NM 2002041200084 20020412 00084 NM 2002 4 12 DL72S020226 1 20020224 A 3350 1061783201 LIGHT BOEING 727 727225A 1384077 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8875Z 21293 OVERHEAD EMERGENCY LIGHT IN CEILING, SEAT 25 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY. 2 L 7 3 4F RT A3WE 2002041200085 20020412 00085 NM 2002 4 12 DL72S020231 1 20020222 A 5532 65174633 SKIN BOEING 727 727232 1384082 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 A .9375 INCH CRACK WAS FOUND FROM FASTENER HOLE AT THE STRINGER 7L SKIN SPLICE TO THE EDGE OF THE SKIN. THE CRACK WAS V ERIFIED TO BE CONTAINED IN THE FASTENER HOLE THROUGH HFEC INSPECTION. THE CRACKED AREA WAS REPAIRED WITH AN EXTERNAL TI TANIUM DOUBLER. 2 L 7 3 4F A3WE 2002041200086 20020412 00086 NE 2002 4 12 DL72S020246 2 20020302 A 7230 JT8D15AHK COMPRESSOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE STALLED A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 546DA 70552 22677 695201 ON TAKEOFF NR 3 COMPRESSOR STALLED. AIRSPEED PLUS 130 ENG HEAT WAS ON USING AT 35 PWR WINDS 330/20 GUSTING TO 28. PERF ORMED ENGINE COMPRESSOR STALL CHECK INSPECTION. NO DEFECTS FOUND AND ENGINE TAKEOFF POWER RAN NORMAL. AIRCRAFT, OKAY F OR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002041200087 20020412 00087 NM 2002 4 12 DL72S020258 1 20020305 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 519DA 21470 FORWARD AISLE EMERGENCY SIGN INOPERATIVE. REPLACED BATTERY PACK AND RACK ASSEMBLY PER MM, OPS GOOD. 2 L 7 3 4F A3WE 2002041200088 20020412 00088 NM 2002 4 12 DL72S020290 1 20020310 A 3350 900542 CHARGER BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 544DA 22493 LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER. 2 L 7 3 4F A3WE 2002041200089 20020412 00089 NM 2002 4 12 DL72S020308 1 20020315 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 523DA 21583 EMERGENCY LIGHTS OUT, ROWS 12 - 19. REPAIRED BROKEN WIRE. 2 L 7 3 4F A3WE 2002041200090 20020412 00090 NM 2002 4 12 DL72S020325 1 20020318 A 5753 SKIN BOEING 727 727225A 1384077 NM T/E FLAP DEBONDED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 RIGHT OUTBOARD MIDFLAP TRAILING EDGE BONDED. ASSEMBLY WAS FOUND WITH TYPICAL LOWER SKIN TO CORE DEBONDING. 2 L 7 3 4F RT A3WE 2002041200091 20020412 00091 NM 2002 4 12 DL72S020338 1 20020319 A 2150 32194211 VALVE BOEING 727 727232 1384082 NM AIR CONDITIONING MALFUNCTIONED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 522DA 21582 PACKS OVERHEATED ON TAXI OUT. RETURNED TO GATE. HAZE IN CABIN. FOUND RIGHT PACK FREEZING UP, REPLACED 35 DEGREE CONT ROLLER AND VALVE. 2 L 7 3 4F A3WE 2002041200092 20020412 00092 NM 2002 4 12 DL72S020370 1 20020325 A 3350 900542 CHARGER BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 544DA 22493 LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY, OPERATION NORMAL. 2 L 7 3 4F A3WE 2002041200093 20020412 00093 NM 2002 4 12 DL72S020374 1 20020326 A 5720 STIFFENER BOEING 727 727225A 1384077 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 OUTBOARD SPAR STIFFENER CRACKED NR 4 SLAT INBOARD TRACK. REPLACED SPAR STIFFENER. 2 L 7 3 4F RT A3WE 2002041200094 20020412 00094 NM 2002 4 12 DL72S020384 1 20020330 A 2621 4739243 BOTTLE BOEING 727 727225A 1384077 NM CARGO BAY INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8875Z 21293 NR 1 CARGO FIRE BOTTLE SQUIBS DO NOT TEST. REPLACED NR 1 CARGO FIRE BOTTLE, TEST OK. 2 L 7 3 4F RT A3WE 2002041200095 20020412 00095 NM 2002 4 12 DL72W020248 1 20020302 A 3350 900542 BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 291WA 22109 AFT AISLE EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2002041200096 20020412 00096 NE 2002 4 12 DL72W020255 2 20020304 A 7200 JT8D15HHK ENGINE BOEING 727 727247 138408F NM PWA JT8 JT8D15A 52051 NE NR 2 FIRE A DALA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN A J FLAME/FIRE WARNING INDICATION DE DESCENT 1 SO 27 295WA 74766 687475 22532 687475 NUMBER 2 ENGINE FIRE IN FLIGHT. FIRE HANDLES PULLED, BOTTLES DISCHARGED. REPLACED ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 2002041200097 20020412 00097 NM 2002 4 12 DL72W020267 1 20020307 A 3350 S106 BATTERY PACK BOEING 727 727247 138408F NM COCKPIT DISCHARGED A DALA K NONE L NO TEST CR CRUISE 1 SO 27 293WA 22111 COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2002041200098 20020412 00098 NM 2002 4 12 AWXA200200314 1 20020325 A 5320 6517688131 SILL BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON INNER CHORD AT THE L1 DOOR THRESHOLD BETWEEN B S 328 AND BS 340 AT THE DOME NUT LOCATION. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLE, SPLICE PLATE AND STIFFENE R IAW B737-300 SRM 51-40-02 PG 3-4, 10-11. 2 L 7 2 4F RT A16WE 2002041200099 20020412 00099 NM 2002 4 12 AWXA200200322 1 20020327 A 5315 65498835 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - MAJOR REPAIR - DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOORBEAM AT BS 947.5, LB L 13-17. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW B737-300 SRM 53-00-51 PG 212, 215 AND SRM 51-20-01 PG 1. 2 L 7 2 4F RT A16WE 2002041200100 20020412 00100 NM 2002 4 12 AWXA200200323 1 20020327 A 5315 65498835 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - MAJOR REPAIR - DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOORBEAM AT BS 947.5, LB L 2-4. MAINTENANCE FABRICATED AND INSTALLED REPAIR STRAP IAW B737-300 SRM 53-00-51, PG 212-215. 2 L 7 2 4F RT A16WE 2002041200101 20020412 00101 EU 2002 4 12 AWXA200200328 1 20020305 A 5512 D55181513001 FLANGE AIRBUS 320 A320231 3930325 EU HORIZ STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 YWG - MAJOR REPAIR - DURING C-08 CHECK A CRACK WAS FOUND ON THE RT HORIZONTAL STABILIZER L/E 3 FROM OUTBOARD END ON LOWE R L/E PANEL MATING SURFACE. MAINTENANCE REMOVED DAMAGED AREA AT STAB STA 6009, RIB 14, FABRICATED AND INSTALLED REPAIR PARTS IAW AWA ER 26-5513-02095-ES4. 2 L 7 2 4F RT A28NM 2002041200102 20020412 00102 NM 2002 4 12 AWXA200200330 1 20020329 A 5315 6545410104 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON THE CABIN FLOORBEAM UPPER TEE CHORD AND WEB AT BS 660 , LBL 0.07. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS IAW AWA ER 03-5717-02098-KB1. 2 L 7 2 4F RT A16WE 2002041700127 20020417 00127 NM 2002 4 17 AWXA200200332 1 20020408 A 3350 RER60F10ROR RESISTOR BOEING 737 7373Y0 1384671 NM COCKPIT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 334AW 23747 PHX - EEL - FLOOD LIGHT BEHIND CAPTAINS SEAT DID NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. MAINTENANCE TROUBLESHOT AN D FOUND THE TERMINAL AND STUD BROKEN OFF OF THE R340 RESISTOR AT CEILING ABOVE FLIGHT DECK. MAINTENANCE REPLACED RESIST OR R340, OPERATIONAL CHECK OF EMERGENCY FLOOD LIGHT WAS GOOD. 2 L 7 2 4F RT A16WE 2002041200103 20020412 00103 WP 2002 4 12 CALA0200195 1 20020411 A 5280 SKIN DOUG DC9 DC982 3022082 WP R/H MLG DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND A 1/2" CRACK IN THE R/H MLG I/B DOOR SKIN AT LOWER FORWARD EDGE. THE DOOR SKIN WAS REPAIRED IAW EA 9-52 81-2-A0941 AND ECRA 5281-01020. 2 L 7 2 4F A6WE 2002041200104 20020412 00104 NM 2002 4 12 CALA0200196 1 20020411 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 360. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2002041200105 20020412 00105 NM 2002 4 12 CALA0200197 1 20020412 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 303.9 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND A 4" CRACK IN WEB AT STA 303.9, STRINGER 4L. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2002041200106 20020412 00106 NM 2002 4 12 AWXA200200333 1 20020409 A 3350 PIN BOEING 737 7373G7 1384595 NM CONNECTOR BACKED OUT A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 306AW 24633 PHX - EEL - DURING INSPECTION EMERGENCY PATHWAY LIGHTS AT SEAT ROWS 12 AND 13 LT WERE FOUND INOPERATIVE. MAINTENANCE TR OUBLESHOT SYSTEM AND FOUND PIN NR 1 ON CONNECTOR D9032J RECESSED, REINSERTED PIN, VERIFIED IT WAS LOCKED AND SECURED, AN D PERFORMED FUNCTIONAL TEST, TESTED GOOD. 2 L 7 2 4F RT A16WE 2002041200107 20020412 00107 NM 2002 4 12 AWXA200200334 1 20020410 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 PHX - EEL - CABIN CREW REPORTED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT WAS DETACHED FROM SEAT. MAINTENANCE REPLA CED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT, FUNCTIONAL CHECK WAS GOOD IAW A1C33006. 2 L 7 2 4F RT A16WE 2002041200108 20020412 00108 NM 2002 4 12 AWXA200200335 1 20020329 A 5753 65C344835 CARRIAGE BOEING 737 7373G7 1384595 NM T/E FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - MAJOR REPAIR - DURING C-12 CHECK CORROSION WAS FOUND ON THE LT OUTBOARD MIDFLAP, INBOARD NR 2 CARRIAGE SPINDLE AT THE BUSHED HOLE. MAINTENANCE REPLACED THE LT OUTBOARD MIDFLAP CARRIAGE IAW BMM 27-51-34 PG 408. 2 L 7 2 4F RT A16WE 2002041200109 20020412 00109 NM 2002 4 12 C1HA200294006 1 20020410 A 7920 FILTER BOEING 727 727290 138408W NM NR 3 ENGINE DIRTY A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 294AS 22146 DURING TAKEOFF ROLL AT APPROX 60 KTS, NR 3 ENGINE LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACE D NR 3 ENGINE MAIN OIL FILTER PER MM 79-31-60. 2 L 7 3 4F A3WE 2002041200110 20020412 00110 SO 2002 4 12 C2XA02CL090 1 20020405 A 3260 WARNING SYSTEM EMB 135 EMB135LR 3260305 SO COCKPIT FAULTY A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 17513 145292 CLE FLIGHT 3078 THE CREW REPORTED A LANDING GEAR WARNING AFTER TAKEOFF. THE WARNING WOULD NOT CANCEL. MAINTENANCE INSP ECTED AND REPLACED THE AURAL WARNING UNIT. OPERATIONAL CHECKS WERE GOOD. MAINTENANCE ALSO PERFORMED CONTINUITY CHECK O F WIRES W001-0843-24 AND W001-0845-24. OPERATIONAL CHECKS OF LANDING GEAR ELECTRONIC UNIT. THE AIRCRAFT WAS RELEASED F OR SERVICE. 2 L 7 2 4F RT T00011AT 2002041200111 20020412 00111 SO 2002 4 12 C2XA02CL091 1 20020405 A 2750 3631101007 LEVER EMB 135 EMB135LR 3260305 SO COCKPIT FAULTY A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 17513 127 145292 CLE FLIGHT NR 3052 THE CREW REPORTED UPON GEAR RETRACTION RECEIVED A LANDING GEAR WARNING AND THE WARNING WOULD NOT CANC EL UNTIL THE GEAR WAS EXTENDED. MAINTENANCE INSPECTED AND REPLACED THE FLAP SELECTOR LEVER. OPERATIONAL CHECKS WERE GO OD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002041200112 20020412 00112 SO 2002 4 12 C2XA02CL092 1 20020407 A 2120 ODOR EMB 135 EMB135ER 3260203 SO CABIN DETECTED A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 27512 145274 CLE FLIGHT 3193 THE CREW REPORTED NR 2 PACK HAD A BURNING SMELL. THE SMELL WENT AWAY AFTER THE PACK WAS TURNED OFF. MA INTENANCE INSPECTED NR 2 PACK AND PERFORMED SYSTEM CHECKS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVIC E. 2 L 7 2 4F RT T00011AT 2002041200113 20020412 00113 SO 2002 4 12 C2XA02CL093 1 20020408 A 2150 8152915 SWITCH EMB 135 EMB135ER 3260203 SO A/C BAY INOPERATIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 27512 145274 CLE FLIGHT 4141 THE CREW REPORTED A SMOKE SMELL WHEN IN ICE CONDITIONS AND WHEN THE ICE TEST WAS DONE. MAINTENANCE INSP ECTED AND REPLACED NR 2 PACK SETDOWN SWITCH. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002041200114 20020412 00114 SO 2002 4 12 C2XA02CL095 1 20020407 A 4930 ODOR EMB 145 EMB145 3260210 SO CABIN DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13956 145078 CLE FLIGHT 4005 THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN AFTER APU START. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE APU. NO FUEL SMELL WAS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002041200115 20020412 00115 SO 2002 4 12 C2XA02CL096 1 20020402 A 3350 74441 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14945 145049 CLE FLIGHT 3021 THE CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE FLIGHT ATTENDANT JUMP SEAT WAS INOPERATIVE. MAINTE NANCE REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002041200116 20020412 00116 EU 2002 4 12 C2XA02IA085 1 20020405 A 3260 C24589002 UPLOCK SENSOR AEROSP ATR42 ATR42320 8680930 EU NLG MALFUNCTIONED A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 14828 179 FLIGHT 3985 FROM SHV TO IAH THE NOSE WHEEL GEAR SHOWS UNLOCK ON BOTH SYSTEMS 1 AND 2 AFTER RETRACTION. AIRCRAFT WAS FLO WN WITH THE LANDING GEAR DOWN. MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK BOX, ADJUSTED THE NLG DOORS. PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002041200117 20020412 00117 NM 2002 4 12 QXEA0200627 1 20020410 A 3350 6138001 BATTERY PACK BOMBDR DHC8 DHC8401 NM CABIN DEFECTIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 1961 4055 PDX-EMERGENCY LIGHTS INOPERATIVE AT AFT EXIT LOCATOR SIGN AND AFT AISLE CEILING POSITIONS. REMOVED AND REPLACED 3 POWER SUPPLY BATTERY PACKS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002041200118 20020412 00118 SO 2002 4 12 C2XA02IA086 1 20020407 A 3230 12038594001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A C2XA K NONE J WARNING INDICATION DE DESCENT 1 SW 27 58733 120197 FLIGHT 3583 IAH TO VCT -A- INDICATION CB POPPED FOR LANDING GEAR. RESET UNSUCCESSFUL, QRH UNSUCCESSFUL. RECYCLED GEAR, IT WOULD NOT COME UP OR DOWN, B SYSTEM INDICATES DOWN AND LOCKED, THE AIRCRAFT LANDED AT VCT WITHOUT INCIDENT. MAINTEN ANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL MODULE, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002041200119 20020412 00119 SO 2002 4 12 C2XA02IA087 1 20020407 A 2540 SMOKE EMB 145 EMB145LR 3260212 SO LAVATORY DETECTED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13978 145180 AMA- FLIGHT 3808 ON TAKEOFF THE CREW NOTED SMOKE IN THE LAV AND RETURNED TO AMA WITHOUT INCIDENT. MAINTENANCE PERFORME D A OPERATIONAL CHECK OF THE LAV FIRE DETECTION SYSTEM AND CHECKED THE LAV FOR SMOKE, NO DEFECTS NOTED. COULD NOT DUPLI CATE THE PROBLEM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002041200121 20020412 00121 NM 2002 4 12 UPS02438020 1 20020323 A 5330 SKIN BOEING 747 747212B 1384886 NM NLG W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C FX - FUSELAGE EXTERNAL SKIN IS CRACKED AROUND RIVET HEAD AT BS 400 STR 44R - STR 45R (NLG W/WELL RH AF T CORNER CUTOUT). NLG W/W R/H AFT CORNER CUTOUT FX EXTERNAL SKIN REPAIRED AS PER UPS EO B747-5330-3520E AND SRM 51-3 0-02 AND DWG 141U1099 AT BS 400 STR 44R - STR 45R. 2 L 7 4 4F A20WE 2002041200122 20020412 00122 NM 2002 4 12 UPS02438026 1 20020325 A 5410 FRAME BOEING 747 747212B 1384886 NM NO.3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C NO.3 PYLON - REAR ENG MOUNT FTG UPPER FRAME FOUND CRACK AT O/B AFT PORTION AS MARKED. REPAIR CARRI ED OUT IAW REPAIR SCHEME INSTRUCTION REFER R-54-53-34756 FOR MATERIAL HEAT TREATMENT REFER TO COMPONENT WORK PROCESS CAR D CONTROL SEQUENCE NO.SQYJ016-090 CLASSIFIED MAJOR REPAIR. 2 L 7 4 4F A20WE 2002041200123 20020412 00123 NM 2002 4 12 UPS02438027 1 20020325 A 5410 FRAME BOEING 747 747212B 1384886 NM NO.3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C NO.3 PYLON - REAR ENG MOUNT FTG UPPER FRAME FOUND CRACK AT O/B FWD AREA AS MARKED. REPAIR CARRIED OUT IAW REPAIR SCHEME INSTRUCTIONS REFER R-54-53-34756 FOR MAT HT REFER TO CWPS CONTROL SEQUENCE NO.SQYJ016-090 CLASSIFI ED MAJOR REPAIR. 2 L 7 4 4F A20WE 2002041200124 20020412 00124 NM 2002 4 12 SWAA020748 1 20020408 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 771SA 27879 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002041200125 20020412 00125 NM 2002 4 12 SWAA020751 1 20020409 A 5311 6546536 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BETWEEN STR 19L AND 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002041200126 20020412 00126 NM 2002 4 12 SWAA020753 1 20020405 A 5312 6517582 WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 183, WL 233 AT RBL 17.1. REMOVED AND REPLACED WEB PE R SRM. 2 L 7 2 4F RT A16WE 2002041200127 20020412 00127 NM 2002 4 12 SWAA020755 1 20020409 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 395SW 27689 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 230 AT RBL 17.1. REMOVED AND REPLACED WEB PE R SRM. 2 L 7 2 4F RT A16WE 2002041200128 20020412 00128 NM 2002 4 12 SWAA020756 1 20020408 A 5230 65C36183 SKIN BOEING 737 7372H4 138448C NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 AFT CARGO DOOR CRACKED AT AFT UPPER CORNER OF HANDLE CUTOUT. REPAIRED DOOR PER SWA RA. 2 L 7 2 4F A16WE 2002041200129 20020412 00129 EA 2002 4 12 COMA0260244 1 20020410 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 969CA 18958 7141 FLIGHT 5354 NOSE L/G DOOR DISAGREE MESSAGE DURING APPROACH.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002041200130 20020412 00130 NE 2002 4 12 COMA0260245 2 20020410 A 7421 4096T38910 IGNITER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE L/H INOPERATIVE A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 952CA 7092 FLIGHT 5877 LEFT ENGINE IGNITION STATUS MESSAGE.REPALCED THE ENGINE IGNITERS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002041200131 20020412 00131 EA 2002 4 12 COMA0260246 1 20020410 A 2750 PAINT CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 01 713CA 7245 FLIGHT 5012 AIRCRAFT ROLLS RIGHT WHEN FLAPS EXTENDED.SANDED ROUGH PAINT ON R/H OUTBD FLAP. 2 L 7 2 4F RT A21EA 2002042400079 20020424 00079 NM 2002 4 24 SABA020050 1 20020411 A 3242 2146655 BRAKE DHAV DHC8 DHC8103 1386005 NM RT MLG WORN A SABA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 33 880CC 277 AIRCRAFT 880 ON FLIGHT 5008 FROM CLT TO OAJ. DURING TAXI OUT THE RIGHT BRAKES VIBRATED AND GRABBED. AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBD AND OTBD BRAKES. OPS CHECK WAS GOO D. AIRCRAFT RETURNED SERVICE. 2 H 7 2 4T RT A13NM 2002051400045 20020514 00045 WP 2002 5 14 ARWA20020315 1 20020327 A 2410 688228 CLUTCH DOUG DC8 DC85F54 3021926 WP PWA JT3D JT3D3B 52039 NE CSD FAILED A ARWA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 426FB 45667 669269 NR 2 ENGINE SHUTDOWN DUE FLUCTUATING OIL PRESSURE GAUGE AND LIGHT AND OIL QTY READING ZERO, NOTE OIL TEMP READING NORMAL 75 DEG. REMOVED AND REPLACED ENGINE. FUNCTIONAL TEST COMPLETED AND FOUND SATISFACTORY. ACFT RETURNED TO SERVICE. EN GINE SENT TO REPAIR FACILITY FOR TEARDOWN & INSPECTION. INSPECTIONS RESULTS, UPON QEC REMOVAL IT WAS DETERMINED THAT A FAILURE OF THE CSD DISCONNECT CLUTCH ASSEMBLY WAS THE CAUSE FOR THE COMPLETE OIL LOSS. 2 L 7 4 4F 4 F RT 4A25 1E8 2002041200132 20020412 00132 WP 2002 4 12 DHL2002807525 1 20020328 A 5313 3979762501 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF>: N/R 0541 MAIN CARGO COMPARTMENT - 2" CRACK ON BATHTUB FITTING (STA. 670-680 L9R)CORR: REMOVED BATHTUB FITTIN G IAW SRM51-1-20D PG. 21 - CLEANED TREATED & PRIMED AREA IAW SRM 51-1-8B - INSTALLED NEW BATHTUB FITTING IAW SRM 51-1-2 0D PG.9 2 L 7 4 4F RT 4A25 2002041200133 20020412 00133 2002 4 12 RAIA00204119 4 20020408 A 3420 7003360948 COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 573HK 2654 41092 5484-STL-DURING TAXI GOT ROLL COMPUTER ERROR ON RIGHT SIDE. MAINTENANCE REMOVER AND REPLACED RIGHT AHARS COMPUTER. 2 L 7 2 4T RT A41NM 2002041200134 20020412 00134 EU 2002 4 12 RAIA00204120 1 20020409 A 2700 C850176 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU INACCURATE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 560HK 4908 4159 41076 5502-STL- LEFT STALL WARNING DURING TAXI. MAINTENANCE REMOVED AND REPLACED LEFT AOA SENSOR. 2 L 7 2 4T RT A41NM 2002041200135 20020412 00135 EU 2002 4 12 RAIA00204121 1 20020409 A 3350 1317 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 558HK 41071 MX-STL- RIGHT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED RIGHT EMERGENCY EXIT LIGHT BULB. 2 L 7 2 4T RT A41NM 2002041300001 20020413 00001 SO 2002 4 13 C2XA02IA089 1 20020408 A 7931 1593732 HOSE EMB 120 EMB120ER 3260203 SO OIL COOLER PUNCTURED A C2XA O OTHER K FLUID LOSS AP APPROACH 1 SW 27 16731 120190 BPT- DURING FLIGHT 3636 APPROACH, THE CREW NOTED THAT THE #2 ENGINE OIL PRESSURE INDICATED LOW IN FLIGHT. THE PILOT FE ATHERED THE #2 PROP, AND LANDED WITHOUT INCIDENT. BPT- MAINTENANCE REMOVED AND REPLACED THE #2 ENGINE OIL COOLER INLET HOSE, SERVICED THE #2 ENGINE OIL, PERFORMED ENGINE RUN AND LEAK CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002041400001 20020414 00001 WP 2002 4 14 DHL2002807526 1 20020323 A 5313 4641324N FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 1128 AFT ACCY COMP. INTERIOR - BATHTUB FITTING CRACKED 2" @ STA. 1690-1700 , L26RCORR: REMOVED CRACKED F ITTING IAW SRM 51-1-20D PG. 21 CLEANED , TREATED AND PRIMED AREA IAW SRM 51-1-8B . INSTALLED NEW FITTING IAW SRM 51-1-20 D PG.9 2 L 7 4 4F RT 4A25 2002041400002 20020414 00002 WP 2002 4 14 DHL2002807527 1 20020323 A 2760 3654073 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 1243 #4 SPOLIER SHOWS CRACKED FITTINGCORR: REPLACED LH. SPOILER #4 FITTING IAW MM 27-61-1 PG. 202, 203 , 206 REFER TO N/R 2387 FOR OPS CHECK 2 L 7 4 4F RT 4A25 2002041500001 20020415 00001 EU 2002 4 15 C2XA02IA090 1 20020414 A 3260 5000VS SPLICE AEROSP ATR42 ATR42320 8680930 EU RT.MLG. W/W BROKEN A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 16824 166 IAH- DURING FLIGHT 3899 THE CREW NOTED THAT THE RIGHT MAIN GEAR UNLOCK LIGHT ON SYSTEM #2 ILLUMINATED IN FLIGHT, IAH- MAINTENANCE REPAIRED SPLICE 5000VS,PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR, NO DEFECTS NOTED, AND, THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002062000006 20020620 00006 NE 2002 6 20 02FDEA00230 2 20020405 A 7530 REGULATOR AIRBUS 310 A310 EU PWA JT9 JT9D7 52054 NE NR 1 ENGINE FAULTY A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 447FE 251 715438 ON TAKEOFF THROTTLE WERE 2 KNOB WIDTHS APART. NR 1 ENG W/N REACH FULL CLIMB PWR. DURING DESCENT NR 1 ENG IDG ADVISORY ILLUMINATED & TEMP REACHED 144 DEG. REMOVED AND REPLACED PRESS REGULATOR & SHUTOFF VALVE. TRIMMED HEATSHIELD, LEAK CHE CK GOOD. 2 L 7 2 4F 4 F RT A35EU E20EA 2002041500002 20020415 00002 NM 2002 4 15 02FDEA00277 1 20020405 A 4900 1014A APU BOEING 727 727233 138408A NM APU BAY FIRE A FDEA F ACTIVATE FIRE EXT. F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 283FE 22350 02-86 DURING CLIMBOUT, FIRE IN APU. SHUTDOWN APU. REMOVED AND REPLACED APU, FIRE OVERHEAT DETECTOR, FIRE BOTTLE AND S QUIB ASSEMBLY. 2 L 7 3 4F RT A3WE 2002041500003 20020415 00003 SO 2002 4 15 C2XA02CL097 1 20020409 A 3230 7455501 LEVER EMB 135 EMB135LR 3260305 SO MLG CONTROL FAILED A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 12519 2329 145366 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE AFTER TAKEOFF. MAINTENANCE REPLACED THE LANDING GEAR LEVER ASSE MBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002041500004 20020415 00004 SO 2002 4 15 CHQ000140 1 20020407 A 7500 O-RING EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL BLEED AIR LEAKING A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 265SK 145226 NR1 BLEED LEAK ON EICAS---REMOVED AND REPLACED, LEAKING O-RING. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002041500005 20020415 00005 SO 2002 4 15 CHQ000141 1 20020407 A 7500 CLAMP EMB 145 EMB145 3260210 SO BLEED AIR LEAKING A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 265 145226 BLEED 1 LEAK ON EICAS----REMOVED AND REPLACED BLEED CLAMP NEAR PACK 1. 2 L 7 2 4F RT T00011AT 2002041500006 20020415 00006 NM 2002 4 15 DHL2002715004 1 20020410 A 5230 65931151 FITTING BOEING 727 727155C 138404Z NM CARGO DOOR LATCH CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 REPLACE MAIN CARGO DOOR LATCH FITTING. GAINED ACCESS TO MCD LATCH SUPPORT FITTING AT B.S. 580 THROUGH FWD. CARGO PIT LT SIDEWALL/ CEILING AND MAIN CABIN. REMOVED AND REPLACED MCD LATCH SUPPORT FITTING AT BS 580. ADJUSTED LATCH FITTING AN D OPS CHECKED. OPENED FWD. PIT UPPER LT SIDEWALL AND CEILING PANEL BS 500 TO 520 AND FLOORBOARD IN CABIN FOR ACCESS. D RILLED AND LOCATED ALL HOLES IN NEW FITTING AND REINSTALLED DOME NUT CHANNELS. REMOVED LT BALLMAT IN CABIN FOR ACCESS. O.K. TO INSTALL FLOOR BOARD REMOVED. O.K. TO INSTALL LT BALLMAT IN CABIN. 2 L 7 3 4F A3WE 2002041500007 20020415 00007 NM 2002 4 15 DL72S020216 1 20020221 A 5754 SPAR BOEING 727 727232 1384082 NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 FOUND ON A2 LETTER CHECK, NR 7 SLAT FWD SPAR AND RIB CRACKED AT ACTUATOR ROD END. REPAIRED PER MM 57-54-000-8. 2 L 7 3 4F A3WE 2002041500008 20020415 00008 NM 2002 4 15 DL72S020344 1 20020320 A 2133 OUTFLOW VALVE BOEING 727 727232 1384082 NM RT PACK MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 543DA 22392 DURING CLIMBOUT FROM ATL, CABIN ALT CONT TO CLIMB AT 400 FT / MIN TO APPROX 9800 FT. A DESCENT WAS INITIATED AT 27000 F T TO AN ALTITUDE OF 16000 FT WHERE PRESSURIZATION COULD BE MAINTAINED. CARGO VALVE INDICATOR CLOSED THE ENTIRE FLIGHT. CHANGES TO BLEED SOURCES HAD NO EFFECT. PRIMARY OUTFLOW VALVE INDICATOR CLOSED ENTIRE FLIGHT ALSO. REPLACED VALVE, CH ECKS GOOD. 2 L 7 3 4F A3WE 2002041500009 20020415 00009 NM 2002 4 15 DL72S020359 1 20020322 A 3270 65579293 PIN BOEING 727 727232 1384082 NM TAIL SKID SHEARED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 520DA 21471 AFTER TAKEOFF, CREW REPORTED TAIL SKID LIGHT ON DIVERTED. UPON INSPECTION, FOUND RIVETS SHEARED FROM BOTTOM OF ENERGY ABSORBER AND TAIL SKID DOOR HANGING FROM HINGES. NO EVIDENCE OF TAIL STRIKE ON TAIL SKID PAD. REPLACED ENERGY ABSORBER AND ADJUSTED DOOR ASSEMBLY, OP CHECKS OK. AIRCRAFT OK FOR SERVICE. 2 L 7 3 4F A3WE 2002041500010 20020415 00010 NM 2002 4 15 DL72S020367 1 20020224 A 3150 AUDIO PANEL BOEING 727 727232 1384082 NM EQUIPMENT CENTER INOPERATIVE A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 515DA 21431 REJECTED TAKEOFF AT 110 KNOTS DUE TO COCKPIT BELL/CHIME THAT SOUNDED TWICE DURING TAKEOFF ROLL. CHIME SOUNDED LIKE FLIG HT ATTENTION CALL CHIME. REMOVED AND REPLACED AUDIO ASSEMBLY UNIT, OPERATIONAL CHECK NORMAL. ALSO CLEANED CONTACTS ON FORWARD FLIGHT ATTENTION PANEL CAPONENTS CALL SWITCH. 2 L 7 3 4F A3WE 2002041500011 20020415 00011 NM 2002 4 15 DL72W020318 1 20020317 A 3250 COLLAR BOEING 727 727247 138408F NM STEERING UNIT LACK OF LUBE A DALA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 27 295WA 22532 VERY LITTLE RESPONSE TO RIGHT RUDDER MOVEMENT ON TAKEOFF ROLL. TAKEOFF DISCONTINUED AT TAXI SPEED. LUBED STEERING COL LAR, CYCLED STEERING THRU SEVERAL TIMES, MOVEMENT CHECKS GOOD WITH RUDDER PEDALS AND STEERING TILLER. 2 L 7 3 4F A3WE 2002041500012 20020415 00012 NM 2002 4 15 DL72W020365 1 20020323 A 3350 BATTERY PACK BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 293WA 22111 CABIN CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OP CHECKS NORMAL. 2 L 7 3 4F A3WE 2002041500013 20020415 00013 NM 2002 4 15 DL733020227 1 20020224 A 3350 POWER SUPPLY BOEING 737 737347 1384647 NM AFT CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3301 23181 L2 DOOR AND AFT AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A16WE 2002041500014 20020415 00014 NM 2002 4 15 DL733020250 1 20020303 A 2560 MEGAPHONE BOEING 737 737330 13844BJ NM AFT CABIN INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 241DL 23833 AFT CABIN MEGAPHONE INOPERATIVE. INSTALLED NEW BATTERIES, MEGAPHONE STILL INOPERATIVE. REPLACED MEGAPHONE. 2 L 7 2 4F RT A16WE 2002041500015 20020415 00015 NM 2002 4 15 DL733020272 1 20020307 A 3397 WIRE BOEING 737 737347 1384647 NM CABIN SHORTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 305WA 23346 SPARKS COMING FROM SIDEWALL AT SEAT 1A. FOUND WIRING TO SIDEWALL LIGHTING SHORTED TO INSULATION HOLD DOWN CLAMP. REPIN NED CONNECTOR TO LIGHT, OP CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2002041500016 20020415 00016 NM 2002 4 15 DL733020273 1 20020308 A 5553 ATTACH FITTING BOEING 737 737347 1384647 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302WA 23182 THE VERTICAL STABILIZER ATTACH LUGS AND THE FUSELAGE CLEVIS LUGS WERE FOUND TO BE CORRODED DURING AN INSPECTION. THE LU G BORES WERE OVERSIZED AND THE FACES SPOTFACED TO REMOVE THE CORROSION AND OVERSIZED BUSHINGS WERE INSTALLED. 2 L 7 2 4F RT A16WE 2002041500017 20020415 00017 NM 2002 4 15 DL733020307 1 20020314 A 2930 ACTUATOR BOEING 737 737347 1384647 NM RT MLG WW LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 3301 23181 NR 1 ENGINE LOW PRESSURE HYDRAULIC (A) SYSTEM LIGHT ILLUMINATED WITH ASSOCIATED A SYSTEM QUANTITY DECREASED TO ZERO. FO LLOWED POM PROCEDURE NO OTHER INDICATION. MADE UNEVENTFUL LANDING. REPLACED O-RING AND FITTING ON A SYSTEM AILERON AUT OPILOT CONTROL ACTUATOR. LEAK CHECK OK. ALSO REPLACED CASE DRAIN FILTERS AND PERFORMED LEAK CHECK. 2 L 7 2 4F RT A16WE 2002041500018 20020415 00018 NM 2002 4 15 DL733020337 1 20020316 A 5415 ATTACH FITTING BOEING 737 737347 1384647 NM NR 2 PYLON WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307WA 23440 A BEARING WAS FOUND MIGRATED FROM THE LUG BORE OF THE AFT FITTING ON THE NR 2 PYLON CROWN BEAM. AFTER REMOVAL OF THE BE ARING LIGHT GOUGES WERE FOUND IN THE LUG BORE. THE LUG WAS REAMED TO A LARGER DIAMETER, A STEEL REPAIR BUSHING INSTALLE D, AND A NEW BEARING INSTALLED. THE WORK WAS ACCOMPLISHED PER ER/A 382769-14. 2 L 7 2 4F RT A16WE 2002041500019 20020415 00019 NM 2002 4 15 DL733020358 1 20020322 A 5755 SKIN BOEING 737 737347 1384647 NM SPOILER DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304WA 23345 UPPER SKIN OF THE OUTBOARD SPOILER WAS FOUND DELAMINATED IN TWO AREAS. REPAIR PER ER/A 411104-14 NORDAM EWO E0037119 RE V I/R. 2 L 7 2 4F RT A16WE 2002041500020 20020415 00020 NM 2002 4 15 DL733020386 1 20020331 A 3150 RELAY BOEING 737 737330 13844BJ NM CENTRAL WARNING INTERMITTENT A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 241DL 23833 TAKEOFF WARNING HORN CAME ON WHEN ADVANCING POWER FOR TAKEOFF. REPEAT WRITEUP. SYSTEM REPLACED R274 PARK AND SQUAT REL AY DUE TO INTERMITTENT OPERATION. TAKEOFF WARNING TEST NORMAL. 2 L 7 2 4F RT A16WE 2002041500021 20020415 00021 NM 2002 4 15 DL733020387 1 20020331 A 3150 CONNECTOR BOEING 737 737330 13844BJ NM RT MLG WW MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 241DL 23833 TAKEOFF WARNING HORN CAME ON UPON ADVANCING POWER FOR TAKEOFF. ALL INDICATIONS NORMAL FOR TAKEOFF EXCEPT HORN. RESEAT ED CONNECTOR PLUGS 4514P AND 5983P, TAKEOFF WARNING TEST NORMAL. 2 L 7 2 4F RT A16WE 2002041500022 20020415 00022 NM 2002 4 15 DL738020237 1 20020226 A 3350 D70701100 BATTERY PACK BOEING 737 737832 13844CF NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3761R 29628 EMERGENCY LIGHT BATTERY RIGHT SIDE FIRST CLASS INOPERATIVE FOR FORWARD EMERGENCY LIGHT OVER RIGHT WING. REPLACED BATTER Y PACK. 2 L 7 2 4F RT A16WE 2002041500023 20020415 00023 NM 2002 4 15 DL738020298 1 20020312 A 2760 UNK SWITCH BOEING 737 737832 13844CF NM SPEED BRAKE INTERMITTENT A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 3739P 30541 TAKEOFF CONFIGURATION ON TAKEOFF ROLL WHILE SETTING TAKEOFF POWER. DISCONTINUED TAKEOFF AT 10 KTS AND RETURNED TO GATE. TROUBLESHOT SYSTEM FOUND SPEED BRAKE SWITCH INTERMITTENT. REPOSITIONED AND CLEANED SPEED BRAKE SWITCH, OPS CHECK NORM AL PER FIM. 2 L 7 2 4F RT A16WE 2002041500024 20020415 00024 NM 2002 4 15 DL738020356 1 20020321 A 3340 767 BULB BOEING 737 737832 13844CF NM EXTERIOR BURNED OUT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3769L 30822 R1 AND R2 EMERGENCY LIGHT EXTERIOR LIGHT BULBS INOPERATIVE. REPLACED LAMP. 2 L 7 2 4F RT A16WE 2002041500025 20020415 00025 NM 2002 4 15 DL738020362 1 20020322 A 2933 MODULE BOEING 737 737832 13844CF NM COCKPIT SHORTED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 393DA 30377 ON CLIMBOUT THROUGH LANDING, RETURN AND TAXI MASTER CAUTION WITH FLIGHT CONTROL ANNUNCIATION ILLUMINATED REPEATEDLY. FO UND STANDBY HYDRAULIC SYSTEM LOW, QUALITY LIGHT CAUSING MASTER CAUTION. CHECKED WIRING AND RESEATED CONNECTOR D46020 A ND REPLACED L4 MODULE IN LOW QUALITY LIGHT ASSEMBLY SYSTEM NOW CHECKS NORMAL OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2002041500026 20020415 00026 NM 2002 4 15 DL738020388 1 20020331 A 2750 SENSOR BOEING 737 737832 13844CF NM TE FLAPS INOPERATIVE A DALA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 27 390DA 30536 AFTER SELECTING FLAP SETTING 2 DEGREES AT AIRSPEED 210 KNOTS THE FLAPS SPLIT ASYMMETRICALLY. THE RIGHT TRAILING EDGE FL AP WAS AT 1.75 DEGREES AND THE LEFT TRAILING EDGE FLAP INDICATED 1.3 DEGREES. PROCEDURE FOLLOWED IAW QR HANDBOOK. LAN DING ACCOMPLISHED NORMAL 130000 LBS, BRAKES APPLIED AT 153 KNOTS. NO PROBLEMS. T/S PER FIM NO EXISTING FAULTS. FAULT HISTORY SHOWED TR FLAP SENSOR DIS. RAN FLAPS UP AND DOWN SERVERAL TIMES NO FAULT INSPECTED FLAP DRIVE NO VISUAL DEFECTS NOTED PER FIM AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2002041500027 20020415 00027 2002 4 15 DL73K020229 4 20020224 A 3410 COMPUTER BOEING 737 737232 1384475 NM NR 1 FAILED A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 306DL 23078 ON TAKEOFF ROLL, CAPTAINS AIR DATA COMPUTER FAILED. ASSOC FLAGS APPEARED. ABORTED TAKEOFF AT 100 KNOTS AND RETURNED TO GATE. REPLACED NR 1 ADC PER MM TEST OK IND NOW NORMAL. ABORTED TAKEOFF INSPECTION C/W. 2 L 7 2 4F RT A16WE 2002041500028 20020415 00028 NM 2002 4 15 DL73K020234 1 20020226 A 2611 SMOKE DETECTOR BOEING 737 737247 138448D NM LAVATORY INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 244WA 23518 FORWARD LAVATORY SMOKE DETECTOR INOPERATIVE. REPLACED FORWARD LAVATORY SMOKE DETECTOR. 2 L 7 2 4F A16WE 2002041500029 20020415 00029 NM 2002 4 15 DL73K020235 1 20020227 A 7110 724705838 BULLET BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE ENG INTAKE SEPARATED A DALA C ABORTED TAKEOFF D C INFLIGHT SEPARATION F.O.D. TO TAKEOFF 1 SO 27 375DL 23602 709150 ON TAKEOFF ROLL, A LOUD THUD WAS HEARD AND AIRCRAFT PULLED SLIGHTLY TO THE LEFT. TAKEOFF WAS ABORTED. ENGINE PARAMETER S WERE NORMAL. UPON INSPECTION FOUND NR 1 ENGINE NOSE BULLET MOUNTING STUDS HAD PULLED FROM N1 TACH GEARBOX AND BULLET BECAME DISLODGED IN THE INLET OF ENGINE. NO DAMAGE WAS FOUND OTHER THAN TO THE BULLET ITSELF. ALL PARTS WERE ACCOUNTED FOR AND NO FURTHER DAMAGE TO THE ENGINE WAS FOUND DURING INSPECTION. N1 TACH GEARBOX AND NOSE BULLET IN NUMBER 1 ENGIN E WERE REPLACED. ENGINE POWER RUN WAS ACCOMPLISHED PER PFHB AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2002041500030 20020415 00030 NM 2002 4 15 DL73K020242 1 20020301 A 2420 CSD BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 ENG GEN INOPERATIVE A DALA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SO 27 315DL 23087 717146 NR 2 ENGINE GENERATOR TRIPPED OFF ON TAKEOFF WOULD NOT RESET. REPLACED RIGHT CSD AND GENERATOR PER MM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002041500031 20020415 00031 NM 2002 4 15 DL73K020251 1 20020304 A 5230 FRAME BOEING 737 737232 1384475 NM CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 FORWARD CARGO DOOR WAS FOUND WITH CRACKED LOWER FOWARD AND AFT CORNER FRAMES, FORWARD AND AFT LOWER STOP BEAMS. REPAIRE D. 2 L 7 2 4F RT A16WE 2002041500032 20020415 00032 NM 2002 4 15 DL73K020264 1 20020307 A 5230 FRAME BOEING 737 737232 1384475 NM CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 FORWARD CARGO DOOR FOUND WITH CRACKED LOWER FORWARD AND AFT CORNER FRAMES AND FORWARD AND AFT SECTIONS OF THE LOWER STOP BEAM. REPAIR PER ER/A 410632-14AD. 2 L 7 2 4F RT A16WE 2002041500033 20020415 00033 NM 2002 4 15 DL73K020271 1 20020307 A 5312 BULKHEAD BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 INSPECTION OF THE FS 178 BULKHEAD PER AD 2000-05-29 REVEALED A SMALL CRACK IN THE LEFT SIDE CHORD AT WL 207 AND ANOTHER AT WL 195. THE LT CHORD WAS CUT AT WL 212 AND A NEW LOWER SECTION INSTALLED PER THE REQUIREMENTS OF BAC S/B 737-53A1173 . THE WORK WAS DOCUMENTED PER ER/A 382698-14AD. 2 L 7 2 4F RT A16WE 2002041500034 20020415 00034 NM 2002 4 15 DL73K020287 1 20020310 A 3350 FUSE BOEING 737 737247 138448D NM CABIN BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 245WA 23519 FOUND FORWARD EMERGENCY LIGHTS FROM ROWS 1 THRU 4 INOPERATIVE. REMOVED AND REPLACED FUSE IN EMERGENCY BATTERY PACK LOCA TED AT STA 400 (IN EMERGENCY RAFT BAY). EMERGENCY LAMPS, NOW OPS NORMAL. 2 L 7 2 4F A16WE 2002041500035 20020415 00035 NM 2002 4 15 DL73K020299 1 20020311 A 5315 6545410513 FLOORBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 CENTER WING / LONGITUDINAL OVERWING FLOORBEAM / BL 24.82 / FS 678 : CHORD AND WEB CRACK REPAIR INSPECTION OF THE LBL & R BL 24.82 LONGITUDINAL FLOORBEAMS PER AD 2001-17-18 REVEALED TYPICAL CRACKS IN THE BEAM WEB, WEB DOUBLER, AND UPPER CHO RD AT FS 678 AT THE AILERON CONTROL QUADRANT CUTOUT. THE CRACKS ARE TYPICAL OF BAC S/B 737-57-1139. THE UPPER CHORDS A ND WEB DOUBLERS WERE REPLACED. THE WEB CRACKS WERE ROUTED OUT AND REPAIRED WITH AN ALUMINUM DOUBLER. THE WORK WAS DONE PER ER/A 382700-14AD. 2 L 7 2 4F RT A16WE 2002041500036 20020415 00036 NE 2002 4 15 DL73K020326 2 20020318 A 7250 JT8D15AHK ENGINE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 FAILED A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 27 305DL 41741 23077 709178 PASSING THROUGH 10,000 FT ON DEPARTURE, HAD LOUD BANG FROM NR 1 ENGINE. ENGINE RPM DECREASED RAPIDLY AND TEMPERATURE WE NT TO MAX INDICATED ON GAUGE. SHUT DOWN ENGINE AND RETURNED TO AIRPORT. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002041500037 20020415 00037 NE 2002 4 15 DL73K020341 2 20020320 A 7261 GARLOCK SEAL BOEING 737 737232 1384475 NM PWA JT8 JT8D* NE NR 2 ENGINE LEAKING A DALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 312DL 70354 695348 23084 695348 NR 2 ENGINE OIL QUANTITY INDICATOR SLOWLY DROPPED TO 0.0 OIL PSI. OIL TEMPERATURE REMAINED WITHIN THE NORMAL OPERATING LIMITS. OIL PRESSURE, LOW YELLOW ARC AND FLICKERING OIL FILTER BYPASS LIGHT. ENGINE SHUTDOWN. FOUND STARTER GARLOC K SEAL LEAKING. REPLACED SAME. LEAK CK GOOD 2 L 7 2 4F 4 F RT A16WE E2EA 2002041500038 20020415 00038 NM 2002 4 15 DL73K020379 1 20020328 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 FUSELAGE / AFT GALLEY DOOR CUTOUT / LOWER HINGE CUTOUT : CRACK REPAIR THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR C UTOUT (R2) WAS FOUND WITH A .5 INCH CRACK IN THE SKIN ASSY AND UNDERLYING BEARSTRAP. THE CRACK WAS REMOVED WITH A CU TOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS AND A STRUCTURAL FILLER. THE WORK WAS ACCOMPLISHED PER ER/A 382827- 14, REV A. 2 L 7 2 4F RT A16WE 2002041500039 20020415 00039 NM 2002 4 15 DL757020243 1 20020301 A 4900 425404 CHARGER BOEING 757 757232 1384965 NM APU BATTERY INOPERATIVE A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 667DN 11096 P2440 25035 P2440 VISIBLE SMOKE AND ELECTRIC SMELL IN CABIN AROUND ROW 42 ON GROUND, DURING BOARDING. FOUND APU BATTERY HOT WITH SOME SM ELL COMING FROM COOLING VENTS. REPLACED APU BATTERY AND CHARGER PER MM CIRCULATED AIR THROUGH CABIN WITH PACKS. NO SMELL OR SMOKE. 2 L 7 2 4F RT A2NM 2002041500040 20020415 00040 NM 2002 4 15 DL757020244 1 20020301 A 3397 WIRE BOEING 757 757232 1384965 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 666DN 25034 EMERGENCY EVACUATION LIGHTING. SEAT 3C, LIGHT INOPERATIVE. C/A FOUND WIRE BROKEN. REPAIRED SAME. 2 L 7 2 4F RT A2NM 2002041500041 20020415 00041 NM 2002 4 15 DL757020252 1 20020302 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 635DL 23762 FUSELAGE / SKIN / FS 1680-1710 / STRG. 18L-21L : SKIN CUTOUT REPAIR. AN EXISTING SKIN REPAIR WAS REMOVED TO ALLOW FOR INSTALLATION OF A BETTER FATIGUE DESIGN REPAIR. THE PREVIOUS REPAIR CUTOUT WAS ENLARGED TO REMOVE THE PREVIOUS REPAIR FASTENER HOLES. THE CUTOUT MEASURED 22 INCHES X 25 INCHES AND WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/ A 382661-14, REV A. 2 L 7 2 4F RT A2NM 2002041500042 20020415 00042 CE 2002 4 15 IKM2002F00000 1 20020318 A 3250 80071702 COMPUTER LEAR 25 25B 5170511 CE GE CJ610 CJ610* 30006 NE NLG STEERING INOPERATIVE E IKMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 118MB 118 STEERING COMPUTER. OPERATIONAL CHECK SHOWED THE NOSE WHEEL WOULD TURN PAST STEERING LIMIT. REPAIRED COMPUTER FIXED TH IS PROBLEM. AFTER INCIDENT, NOSE WHEEL WITH NO POWER COULD TURN LEFT BUT WAS MECHANICALLY STOPPED FROM TURNING RIGHT. NOSE WHEEL STEERING WOULD TURN NOSE WHEEL STEERING WOULD TURN NOSE WHEEL PAST STOPS-ALL THE WAY AROUND-360 DEGREES. GE AR WELL SHOWS SIGNS OF NOSE TIRE NOT BEING STRAIGHT. STRUT STILL INFLATED. 2 L 7 2 4J 4 J A10CE 1E16 2002041500043 20020415 00043 WP 2002 4 15 0201129754 1 20020408 A 2130 DOOR SEAL DOUG DC9 DC941 302207N WP AFT PRESS BLKHD MISSING A NWAA B EMER. DESCENT J O WARNING INDICATION OTHER CR CRUISE 1 GL 01 754NW 47178 CRUISING AT 24,000 FEET WITH WING AND ENGINE ANTI-ICE ON, THE CABIN BEGAN CLIMBING UNCONTROLLABLY. CREW FOLLOWED COM PRO CEDURES AND PERFORMED AN EMERGENCY DESCENT. FLIGHT ATTENDANT REPORTED A LOUD SQUEAL IN THE AFT SECTION OF THE CABIN. FLI GHT CONTINUED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A SEAL FROM THE VACUUM RELIEF DOOR ON THE AF T PRESSURE BULKHEAD MISSING AND REPLACED IT. PRESSURE TESTS OF THE AIRCRAFT CHECKED GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002041500044 20020415 00044 WP 2002 4 15 AALA20020159 1 20020216 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 DFW - FOUND TWO LARGE DENTS WITH CREASES, STATION 427 TO 439, ABOVE AND BELOW BOTH SIDES OF LONGERON 24L. CUT OUT DAMAG E ON UPPER FORWARD DENT, COLD WORKED AND DYE CHECKED LOWER AFT DENT, INSTALLED PLUG AND INTERNAL FINGER DOUBLER PER SRM 53-04, FIGURE 38, SHEET 24. (M) 2 L 7 2 4F A6WE 2002041500045 20020415 00045 WP 2002 4 15 AALA20020160 1 20020216 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 DFW - FOUND DEEP DENT WITH GOUGE, STATION 351, BELOW LONGERON 27L. CUTOUT DAMAGED AREA, PLUGGED AND INSTALLED INTERNAL FINGER DOUBLER PER SRM 53-04-00, FIGURE 38, SHEET 24. (M) 2 L 7 2 4F A6WE 2002041500046 20020415 00046 WP 2002 4 15 AALA20020161 1 20020216 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 DFW - FOUND STATION 281 OUTBOARD OF LONGERON 26L, OUTER SKIN GOUGED. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER SR M 53-04. (M) 2 L 7 2 4F A6WE 2002041500047 20020415 00047 WP 2002 4 15 AALA20020162 1 20020216 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 DFW - FOUND AIRCRAFT FUSELAGE DAMAGE, LEFT SIDE OF FUSELAGE, STATION 278 TO 398 LONGERON 21L TO 26L. CUT OUT DAMAGED SK IN AND STRUCTURE. REPAIRED SKIN PER SRM 53-04, REPAIRED FRAMES PER SRM 53-03 (Z FRAME) 53-10-00-17 (J ANGLE). REPAIRED FORMERS (SHEAR TIES) PER SRM 53-03 FIG 6 AND 7 AND REPAIRED LONGERONS, NEW SPLICED IN SECTIONS PER SRM 53-02 INCH (FLUS H SKIN PANEL REPAIR). INCORPORATED ESO'S 80559 DATED 2/15/2002 80559 DATED 2-5-2002, ESO 80559 DATED 2/5/2002. (M) 2 L 7 2 4F A6WE 2002041500048 20020415 00048 WP 2002 4 15 AALA20020179 1 20020220 A 5312 PRESSURE PANEL DOUG DC9 DC982 3022082 WP NLG WW DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7514A 49891 TUL - FOUND STEERING CYLINDER CONTACTED RIGHT NOSE W/W SIDE WALL DUE TO TOW BAR OVER STEER. INSTALLED DOUBLER REPAIR PE R ESO 80559 DATED 1-31-02. (M) 2 L 7 2 4F A6WE 2002041500049 20020415 00049 WP 2002 4 15 AALA20020180 1 20020212 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND CORROSION ON CUSP STATION 1219. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002041500050 20020415 00050 WP 2002 4 15 AALA20020181 1 20020214 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND FORWARD CARGO DOOR, CUT OUT CORRODED AT LOWER END OF CUT OUT AT BEAM FROM STATION 390 TO 412. SPLICED IN NE W SECTION OF DOOR JAMB PAN PER SRM 53-05 FIG 44. (M) 2 L 7 2 4F A6WE 2002041500051 20020415 00051 WP 2002 4 15 AALA20020182 1 20020211 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND CORROSION ON NR 6 SEAT TRACK FORWARD END, STATION 215 AROUND FIRST FLOORBOARD SUPPORT FASTENER HOLE OUTBOARD SIDE. INSTALLED NEW SECTION OF NR 6 SEAT TRACK AND SPLICE PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002041500052 20020415 00052 WP 2002 4 15 AALA20020183 1 20020208 A 5310 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND AFT CARGO DOOR CUTOUT FORWARD LOWER CHORD ATTACH ANGLE CORRODED. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002041500053 20020415 00053 WP 2002 4 15 AALA20020184 1 20020207 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND CORROSION ON NR 1 SEAT TRACK AROUND LUG HOLE. INSTALLED SEAT TRACK LUG REPAIR SRM 53-05-00 FIG 4A. (M) 2 L 7 2 4F A6WE 2002041500054 20020415 00054 WP 2002 4 15 AALA20020185 1 20020213 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND CORROSION ON CUSP AROUND RIVETS STATION 1150R. REMOVED CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01 PA GE 18. (M) 2 L 7 2 4F A6WE 2002041500055 20020415 00055 SO 2002 4 15 C2XA02TY068 1 20020409 A 5315 14532636A FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 TYS DURING A SCHEDULED 1C/2C INSPECTION THE LEFT OMEGA BEAM HAS CORROSION IN THE GALLEY AREA. MAINTENANCE FABRICATED A ND INSTALLED REPAIR IAW EMB135/145 SRM 53-21-10. 2 L 7 2 4F RT T00011AT 2002041500056 20020415 00056 SO 2002 4 15 C2XA02TY069 1 20020408 A 5330 12020333049 SKIN EMB 145 EMB145 3260210 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 TYS DURING A SCHEDULED 1C/2C INSPECTION A GOUGE WAS FOUND IN THE CARGO DOOR CUTOUT SKIN. 2 L 7 2 4F RT T00011AT 2002041500057 20020415 00057 SO 2002 4 15 C2XA02TY070 1 20020410 A 5315 14525422001 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 TYS DURING A SCHEDULED 1C/2C INSPECTION, THERE WAS EVIDENCE OF CORROSION IN THE LEFT AND RIGHT SIDES OF THE CARGO COMPA RTMENT FLOORBEAMS AT THE BULKHEAD AREA. MAINTENANCE REMOVED AND REPLACED THE LT AND RT FORWARD FLOORBEAMS IAW 135/145 S RM 51-40-02-03 AND 51-40-06. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF ALL MAINTENANCE. 2 L 7 2 4F RT T00011AT 2002041500058 20020415 00058 NM 2002 4 15 CALA0200181 1 20020405 A 5347 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND AFT BAGGAGE BIN LT TIE DOWN TRACK CORRODED AT STA 727C-947. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-53, FIGURE 202. 2 L 7 2 4F RT A16WE 2002041500059 20020415 00059 WP 2002 4 15 CALA0200191 1 20020409 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND FLOOR WEB CORRODED AT FS 120-133, LBL 28 TO RBL 84. THE O/B PILOT SEAT TRACK WAS REMOVED IAW SRM 51-30 -1. THE FLOOR SUPPORT AND WEB WERE REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 2002041500060 20020415 00060 NM 2002 4 15 CALA0200192 1 20020409 A 5711 SPAR BOEING 737 7373T0 1384582 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND A .125 INCH CRACK IN RT WING REAR SPAR UPPER CHORD AT MLG BEAM ATTACH FITTING. THE CRACKED AREA WAS RE MOVED AND A FREEZE PLUG WAS INSTALLED. 2 L 7 2 4F RT A16WE 2002041500061 20020415 00061 NM 2002 4 15 CALA0200193 1 20020409 A 3221 TRUNNION BOEING 737 7373T0 1384582 NM NLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND NLG LT AND RT MAIN TRUNNION SUPPORT FITTING BEARING SEATS CORRODED. THE CORROSION WAS REMOVED, THE ARE AS WERE REWORKED AND BUSHINGS WERE INSTALLED AT EACH LOCATION IAW ECRA 5343-01006 REV A. 2 L 7 2 4F RT A16WE 2002041500064 20020415 00064 EU 2002 4 15 CX7A194J2 1 20020408 A 2613 1734362450 WARNING SYSTEM SAAB SF340 340B 7860101 EU COCKPIT FALSE ACTIVATION A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 311CE 340B214 ON TAKEOFF ROLL TAIL PIPE HOT LIGHT ILLUMINATED. ABORTED TAKEOFF. LIGHT WENT OFF WHEN A/C RETURNED TO THE GATE. 2 L 7 2 4T RT A52EU 2002041500065 20020415 00065 EU 2002 4 15 CX7A194J4 1 20020408 A 2613 1734362450 WARNING SYSTEM SAAB SF340 340B 7860101 EU COCKPIT FALSE ACTIVATION A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 305CE 340B202 ON TAKEOFF ROLL TAIL PIPE HOT LIGHT ILLUMINATED. ABORTED TAKEOFF. LIGHT WENT OUT WHEN A/C RETURNED TO THE GATE. 2 L 7 2 4T RT A52EU 2002041500066 20020415 00066 WP 2002 4 15 DHL2002806009 1 20020406 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 A 1 INCH CRACK ON RT SIDE, STA 1755, BETWEEN LONGERON 10 & 11, MAJOR REPAIR. INSTALLED MAJOR REPAIR AFT RT FUSE SKIN PE R SRM 53-2-1 ITEM 16-2. 2 L 7 4 4F RT 4A25 2002041500068 20020415 00068 WP 2002 4 15 DHL2002807515 1 20020323 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 81797 45990 FUS EXT - CRACK OF 2 INCHES BETWEEN L14L & L15L , FROM STA 1745.000 TO 1755.000. FABRICATED AND INSTALLED DOUBLER, FILL ER, AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002041500069 20020415 00069 WP 2002 4 15 DHL2002807517 1 20020323 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 81797 45990 RIGHT WING OUTBOARD L/E UPPER INNER SURFACE - RIB CRACKED .250 AT STA 660.000. STOP DRILLED CRACK IAW SRM 57-2-0 FIG 2, FABRICATED AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002041500070 20020415 00070 WP 2002 4 15 DHL2002807519 1 20020322 A 5531 RIB DOUG DC8 DC873F 302199F WP VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 81797 45990 VERT STAB L/E - INNER RIB CRACKED .500 AT ZFS 108.000. STOP DRILLED CRACK IAW SRM 55-2-0 FIG 2. FABRICATED AND INSTALL ED DOUBLER IAW SRM 55-2-0 FIG 2 & SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002041500071 20020415 00071 WP 2002 4 15 DHL2002807520 1 20020326 A 5712 FORMER DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 81797 45990 RIGHT WING L/E FORMER CRACKED .500 AT STA XFS835.000. STOP DRILLED FORMER IAW 57-2-0 FIG 2. FABRICATED AND INSTALLED R EINFORCING ANGLE IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002041500072 20020415 00072 NM 2002 4 15 DL76L020390 1 20020331 A 3350 LIGHT BOEING 767 767332 1382001 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 195DN 28452 NUMEROUS EMERGENCY EXIT LIGHTS INOP IN COACH SEATS. FOUND OPEN FUSE IN PWR SUPPLY M9009. REPLACED FUSE. FOUND LIGHT A SSY SHORTED AT 33F. REPLACED LIGHT ASSY. FOUND PWR SUPPLY M9 INOP. REPLACED PWR SUPPLY PER M/M. ALL LIGHTS, NOW CHEC K OK. 2 L 7 2 4F RT A1NM 2002041500073 20020415 00073 NM 2002 4 15 DL76P020385 1 20020330 A 3350 BPS73 BATTERY PACK BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1402A 25989 LT SIDE EXT EMERGENCY LIGHTS INOP. REPLACED M738 BATTERY RACK. 2 L 7 2 4F RT A1NM 2002041500074 20020415 00074 NM 2002 4 15 DL76S020215 1 20020220 A 2421 241080105 IDG BOEING 767 767332 1382001 NM LT ENGINE FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 136DL 23146 BOTH GENS FAILED AT 1500 FT AFTER TAKEOFF FOR ABOUT 10 SEC/RT GEN CAME BACK ON LINE. LEFT GEN REMAINED FAILED. CK'D OI L LEVEL ON RT IDG FOR CORRECT SERVICING, ALL GOOD. RAN RT ENG, RT IDG CKS GOOD. REPLACED LT ENG IDG PER M/M. RAN LT E NG, IDG OPS AND LEAK CKS GOOD. 2 L 7 2 4F RT A1NM 2002041500075 20020415 00075 NM 2002 4 15 DL76S020219 1 20020222 A 3350 767GE LIGHT BOEING 767 767332 1382001 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 132DN 24981 TWO EMERGENCY LIGHTS INOP ON LEFT SIDE OF A/C AND ONE ON RIGHT SIDE, L-4, AFT OF LEFT WING AND FWD OF R-4. RELAMPED LIG HTS. 2 L 7 2 4F RT A1NM 2002041500076 20020415 00076 NM 2002 4 15 DL76S020257 1 20020304 A 5754 BEAM BOEING 767 767332 1382001 NM L/E SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 119DL 23278 NR 5 LEADING EDGE SLAT NOSE BEAM WAS FOUND DAMAGED AT STA 439. REPAIR PER ER/A 402159-14. 2 L 7 2 4F RT A1NM 2002041500077 20020415 00077 NM 2002 4 15 DL76S020312 1 20020315 A 3350 1265 LIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 123DN 23437 SVC CHECK FOUND EMERGENCY OVERHEAD LIGHT AT ROW 17 LT SIDE INOP. REPLACED EMERGENCY LIGHT ASSY AT ROW 17 LT SIDE, CHECK S OK. 2 L 7 2 4F RT A1NM 2002041500078 20020415 00078 NM 2002 4 15 DL76S020323 1 20020318 A 5753 SKIN BOEING 767 767332 1382001 NM T/E FLAP DEBONDED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 116DL 23275 WING INBOARD AFT FLAP WAS FOUND WITH THE UPPER SKIN DISBONDED AT THE INBOARD END. REPAIR PER ER/A 411072-14. 2 L 7 2 4F RT A1NM 2002041500079 20020415 00079 NM 2002 4 15 DL76S020324 1 20020318 A 5755 FLANGE BOEING 767 767332 1382001 NM SPOILER DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 116DL 23275 THE OUTBOARD SPOILER WAS FOUND WITH DELAMINATION ON THE SPAR UPPER FLANGE. REPAIR PER ER/A 411065-14. 2 L 7 2 4F RT A1NM 2002041500080 20020415 00080 NM 2002 4 15 DL76S020368 1 20020324 A 2780 301201561 DUCT BOEING 767 767332 1382001 NM RT WING DAMAGED A DALA K NONE F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 127DL 24077 L/E SLAT ASYM MESSAGE AND LEADING EDGE LIGHT ON AFTER LANDING WHILE BRINGING FLAPS UP. REPLACED TAI DUCT AND TORQUE TUB E. REPAIRED SLAT PANELS. 2 L 7 2 4F RT A1NM 2002041500081 20020415 00081 NM 2002 4 15 DL777020210 1 20020220 A 2120 ODOR BOEING 777 777232 1385232 NM CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 860DA 29951 CREW REPORTS FOUL SMELL IN THE AIR CONDITIONING SYSTEM AT LOW ALTITUDES. REMOVED WATER SEPARATOR ON LEFT PACK, SEPARATO R CLEAN. CLEANED RESIDUE IN OUTLET OF COMPRESSOR REHEATER, RAN PACKS WITH APU AIR AND WITH ENGINES AT PWR. NO ODOR NOT ED AT THIS TIME. 2 L 7 2 4F RT T00001SE 2002041500082 20020415 00082 2002 4 15 DL777020327 4 20020318 A 2330 CONNECTOR BOEING 777 777232 1385232 NM CABIN BURNED A DALA K NONE M OVER TEMP IN INSP/MAINT 1 SO 27 865DA 29737 ROCKWELL FOUND BURNT CONNECTOR AT VIDEO SCREEN SEAT 30G. DISCONNECTED SDU TO AVU CABLE FWD TO MCO. 2 L 7 2 4F RT T00001SE 2002041500083 20020415 00083 NM 2002 4 15 DLM11020228 1 20020224 A 2450 13206263 RECEPTACLE DOUG MD11 MD11 3023602 NM R1 DOOR BURNED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 811DE 48566 FOUND CIRCUIT BREAKER UTILITY OUTLET OPEN. RESET RESULTED IN CRACKLING NOISE AND SMOKE BY R-1 DOOR. FOUND R-1 SERVICE OUTLET BURNT. USED FOR VACUUM CLEANERS. REPLACED THE OUTLET. VISUALLY INSPECTED THE OTHER AIRCRAFT OUTLETS R5-1122, R 5-1124 AND R5-1125, NO DEFECTS NOTED. 2 L 7 3 4F RT A22WE 2002041500084 20020415 00084 NM 2002 4 15 DLM11020253 1 20020221 A 5330 NGA6313515 SKIN DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 804DE 48475 AT OVERHAUL, DAMAGE WAS FOUND TO THE EXISTING REPAIR DOUBLERS AT STA 1937 AND 1959 AT THE AFT LAV EXHAUST PORTS. REPAIR ED PER ER/A 360655-14 REV C. 2 L 7 3 4F RT A22WE 2002041500085 20020415 00085 NE 2002 4 15 00015 2 20020411 A 7200 ENGINE LEAR 25 25B 5170511 CE GE CJ610 CJ6106 30006 NE RIGHT FLAMED OUT E HAEA B EMER. DESCENT X ENGINE FLAMEOUT CL CLIMB 1 SW 05 666TW 116 251210A MODERATE TURBULENCE CLIMB FLAME-OUT RT ENGINE. DESCENT NORMAL RESTART. 2 L 7 2 4J 4 J A10CE 1E16 2002041500086 20020415 00086 WP 2002 4 15 AALA20020186 1 20020212 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND CORROSION ON CUSP STATION 1212. REMOVED CORROSION, CUT OUT DAMAGE AND INSTALLED DOUBLER PER 53-01. (M) 2 L 7 2 4F A6WE 2002041500088 20020415 00088 WP 2002 4 15 AALA20020187 1 20020208 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND GOUGE IN CUSP AT STATION 199, 25 RBL. FABRICATED AND INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002041500089 20020415 00089 WP 2002 4 15 AALA20020188 1 20020211 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND VERTICAL ANGLE CRACKED AT TOP AND BOTTOM FASTENER ON FORWARD SIDE OF AFT PRESSURE BULKHEAD ABOVE DOOR CUTOUT . REMOVED AND REPLACED ANGLE PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002041500090 20020415 00090 WP 2002 4 15 AALA20020189 1 20020215 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND DENTS AND GOUGES IN FUSELAGE SKIN STATION 218 TO STATION 256 BETWEEN LONGERON 18L TO LONGERON 20L. INSTALLE D PERMANENT REPAIR DOUBLERS STATION 214 TO STATION 262, LONGERON 16L TO LONGERON 21L PER SRM 53-04 FIG 12B SHEET 34 AND AARD 53-30-00-0. (M) 2 L 7 2 4F A6WE 2002041500091 20020415 00091 WP 2002 4 15 AALA20020190 1 20020227 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND HOLE ELONGATED OUT OF LIMITS IN AFT CARGO DOOR JAMB BEAM AT AFT DOOR STOP HOLE APPROX STATION 1193. INSTALL ED DOUBLER PER AARD 53-10-00-8. (M) 2 L 7 2 4F A6WE 2002050600091 20020506 00091 NM 2002 5 6 02FDEA00247 1 20020412 A 5741 65870197 PIN BOEING 727 7272S2F 1384O81 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 207FE 22929 RT WING REAR TERMINAL PIN AT BS 870 HAS RUST AROUND BASE OF PIN. REMOVED AND REPLACED PIN. 2 L 7 3 4F A3WE 2002041500092 20020415 00092 WP 2002 4 15 AALA20020191 1 20020214 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FS 1338 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND CORROSION ON FLOORBEAM AT STATION 1338 LBL 40 AND LBL 47. CUT OUT CORROSION, INSTALLED REPAIR ANGLE AND SPA CERS PER SRM 53-05-00 FIG 20A AND AARD 51-60-00-05. (M) 2 L 7 2 4F A6WE 2002041500093 20020415 00093 WP 2002 4 15 AALA20020222 1 20020204 A 5313 STRINGER DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7527A 49919 TUL - FOUND STRINGER 25R DAMAGED STATION 1060. BLENDED DAMAGED AREA, INSTALLED REPAIR STRAP PER ESO 80559 DATED 1-31-02 . (M) 2 L 7 2 4F A6WE 2002041500094 20020415 00094 NM 2002 4 15 200200244 1 20020412 A 5753 65B1704711 ATTACH FITTING BOEING 747 747SR46 1384816 NM T/E FLAP BROKEN B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 477EV 20784 LEFT HAND INBOARD FORE FLAP, INBOARD DRIVE LINK ATTACH FITTING WAS BROKE COMPLETELY THROUGH. REPLACED ATTACH FITTING IN ACCORDANCE WITH SRM 57-30-02. 2 L 7 4 4F RT A20WE 2002041500095 20020415 00095 SO 2002 4 15 ASOA02135 1 20020227 A 5313 12005744011 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SW 21 286AS 120268 DURING C-CHECK INSPECTION IN BNA, STRINGER 20 LEFT WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 19. MAINTENANCE RE MOVED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-25-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002041500096 20020415 00096 SO 2002 4 15 ASOA02136 1 20020227 A 5310 CROSSBEAM EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 286AS 120268 DURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD CROSSBEAM WAS CORRODED AT FRAME 20. CORROSION WAS ALSO FOUND ON TH E LEFT OUTBOARD CROSS BEAM (P/N 120-14243-001) AT FRAME 15. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAMS IA W SRMS 51-21-04, 51-21-05, 51-25-00, AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002041500097 20020415 00097 EA 2002 4 15 ASOA02137 1 20020305 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SW 21 827AS 7212 FLT 4505 - DURING GROUND INSPECTION IN XNA, THE NR 2 CABIN CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED THE BURNED OUT CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVIC E. (M) 2 L 7 2 4F RT A21EA 2002041500098 20020415 00098 EA 2002 4 15 ASOA02138 1 20020306 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SW 21 877AS 434 7579 DURING GROUND INSPECTION IN ATL, THE CAPTAIN REPORTED LARGE CRACKS RUNNING THROUGH THE LEFT SIDE WINDOW. MAINTENANCE RE MOVED AND REPLACED THE CRACKED LEFT SIDE WINDOW. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002041500099 20020415 00099 WP 2002 4 15 2002F00371 1 20020225 A 5311 FRAME LKHEED 1011 10113851 5265010 WP FUSELAGE CRACKED G K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION MAIN FRAME CHORD FS 315 WAS FOUND CRACKED AT RBL 22. CRACK WAS 1 INCH IN LENGTH. MAINTENAN CE COMPLIED WITH ER/A L10-53R-4740, ER/A L10-53R-4733, AND SRM 51-40-01 FOR REPAIR. 2 L 7 3 4F A23WE 2002041500100 20020415 00100 SO 2002 4 15 ASOA02139 1 20020306 A 3350 3071BPE BULB EMB 120 EMB120RT 3260202 SO CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SW 21 280AS 120231 FLT 4903 - DURING GROUND INSPECTION IN DFW, THE CREW REPORTED THAT THE RED FLOOR EMERGENCY LIGHT NEAR THE AIRSTAIR DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT FLOOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKS NORMAL . AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002041500101 20020415 00101 SO 2002 4 15 ASOA02140 1 20020307 A 3350 3071BPE BULB EMB 120 EMB120ER 3260203 SO CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SW 21 261AS 120141 DURING A HANGAR INSPECTION IN TXK, THE LOWER AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNT OUT EMERGENCY EXIT LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002041500102 20020415 00102 SO 2002 4 15 ASOA02141 1 20020307 A 3350 1317 BULB EMB 120 EMB120ER 3260203 SO CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 501AS 120273 FLT 4945 - DURING GROUND INSPECTION IN ATL, THE LEFT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE BURNED OUT EXTERIOR EMERGENCY LIGHT BULB (P/N 1317). MAINTENANCE ALSO FOUND A LOOSE WIRE CONNECT ION (P/N M22759209) THAT WAS REPAIRED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002041500103 20020415 00103 EA 2002 4 15 ASOA02142 1 20020308 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 863AS 7487 FLT 4787 - DURING A SCHEDULED INSPECTION IN XNA, THE LEFT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE BURNED OUT EXTERIOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. ( M) 2 L 7 2 4F RT A21EA 2002041500104 20020415 00104 EA 2002 4 15 ASOA02143 1 20020308 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 840AS 7290 DURING GROUND INSPECTION IN ATL, THE CREW REPORTED THAT THE EMERGENCY FLOOR LEVEL STRIP LIGHTING WAS LOOSE AND SOME WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BROKEN LUMINESCENT STRIP LIGHTING (P/N 5872-8) AND REMOVED AND REPLAC ED THE ENTIRE COVER STRIP (P/N 362624). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002041500105 20020415 00105 SO 2002 4 15 ASOA02144 1 20020309 A 3350 3071BPE BULB EMB 120 EMB120ER 3260203 SO CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 267AS 120198 DURING HANGAR INSPECTION IN MCN, THE FLOOR EMERGENCY LIGHT WAS INOPERATIVE AT ROW THREE. MAINTENANCE REMOVED AND REPLAC ED THE BURNED OUT FLOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002041500106 20020415 00106 SO 2002 4 15 ASOA02145 1 20020309 A 3397 12021299001 WIRE EMB 120 EMB120RT 3260202 SO FUSELAGE MISINSTALLED A ASOA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 11 260AS 120132 FLT 4224 - DURING GROUND INSPECTION IN ATL, THE AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE ON THE LEFT AND RIGHT SIDES. MAINTENANCE FOUND THE RIGHT SIDE LIGHT WIRED INCORRECTLY. MAINTENANCE REWIRED THE EMERGENCY LIGHT. OPERATIONA L CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002041500107 20020415 00107 WP 2002 4 15 GTIA020231 1 20020313 A 3350 CONTROL PANEL DOUG DC9 DC981 3022081 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 819NK 48016 DTW - FOUND LIGHT ABOVE AFT TAIL SLIDE INOPERATIVE. REPAIRED GROUND BAR AFT OVERHEAD PANEL EMEGENCY LIGHT, OPS CHECK NO RMAL IAW MD 80 MM 33-50-00. (M) 2 L 7 2 4F A6WE 2002041500108 20020415 00108 WP 2002 4 15 GTIA020232 1 20020313 A 2611 SMOKE DETECTOR DOUG DC9 DC981 3022081 WP LAVATORY FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 SW 21 819NK 48016 DTW - FOUND AFT RIGHT LAVATORY SMOKE DETECTOR FAILS TO TEST. CLEANED CANNON PLUG, OPS CHECK NORMAL IAW MD80 MM 26-10-00 . (M) 2 L 7 2 4F A6WE 2002041500109 20020415 00109 2002 4 15 2002F00372 4 20020401 A 3160 4058650930 CDU BOEING 757 75723N 1384973 NM COCKPIT MALFUNCTIONED G K NONE O OTHER CR CRUISE 1 GL 11 518AT 20719 20719 27974 FLIGHT NUMBER 8026, DURING CRUISE CAPTAINS CDU LOCKED UP THEN WENT BLANK FOR APPROXIMATELY 15 MINUTES AND THEN CAME BACK ON LINE ON ITS OWN ACCORD AND OPERATED NORMALLY FOR REMAINDER OF FLIGHT. MAINTENANCE TESTED THE CAPTAINS CDU, ALL TEST NORMAL. THE CAPTAINS AND FIRST OFFICERS CDU'S WERE SWAPPED FOR TROUBLESHOOTING. R&R OF CDU'S IN ACCORDANCE WITH 34-60 -101. 2 L 7 2 4F RT A2NM 2002041500110 20020415 00110 WP 2002 4 15 GTIA020234 1 20020316 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 803NK 48087 FLL - FOUND AFT EMERGENCY LIGHT OVER L-2 DOOR INOPERATIVE. SECURED DISCONNECTED GROUND WIRE IN OVERHEAD. OPS CHECK NOR MAL IAW MD80 MM 33-50-00. (M) 2 L 7 2 4F A6WE 2002041500111 20020415 00111 NM 2002 4 15 SABA020051 1 20020411 A 3350 10005511 BULB DHAV DHC8 DHC8103 1386005 NM CABIN BURNED OUT A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 882CC 168 Aircraft 882 on flight 5025 from CLT to TLH. During preflight inspection the floor emergency light at row 5 burned out. Maintenance removed and replaced the bulb. Ops check was good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002041500112 20020415 00112 WP 2002 4 15 GTIA020235 1 20020316 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 SW 21 803NK 48087 FLL - FOUND L-1 DOOR AND R-1 DOOR EMERGENCY LIGHT EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERIES IN EMERGENCY LIGHT B ATTERY PACK ON DROP CEILING BETWEEN FORWARD LAVATORY, OPS CHECK NORMAL IAW MD80 MM 33-50-00. (M) 2 L 7 2 4F A6WE 2002041500113 20020415 00113 WP 2002 4 15 GTIA020236 1 20020316 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 803NK 48087 ORD - DURING PREFLIGHT, COULD NOT GET CABIN EMERGENCY LIGHTS TO TEST. REMOVED AND REPLACED FORWARD EMERGENCY BATTERY PO WER SUPPLY. OPS CHECKED IAW MM 33-51-00. OPS NORMAL. (M) 2 L 7 2 4F A6WE 2002041500114 20020415 00114 NE 2002 4 15 2002F00373 2 20020409 A 7320 FFG052AC GOVERNOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535* NE RT ENGINE MALFUNCTIONED G K NONE J WARNING INDICATION CR CRUISE 1 GL 11 551TZ 2129 2129 32585 31798 FLIGHT 537, DURING CRUISE RIGHT EEC + LIMITER INOP, LIGHT ILLUMINATED. EICAS MSG ENG EEC AND RT ENG LIMITER DISPLAYED. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE FUEL FLOW GOVERNOR, REFERENCE MM 73-21-01, COMPLIED WITH TEST 1, 2, 9, 10 OF MM 71-00-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002041500115 20020415 00115 NM 2002 4 15 2002F00374 1 20020315 A 2421 727792K IDG BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FAILED G K NONE J WARNING INDICATION CR CRUISE 1 GL 11 519AT 16365 16365 27975 31511 FLIGHT NUMBER 273, DURING CRUISE EICAS MSG R GEN OFF DISPLAYED, R GEN OFF LIGHT ILLUMINATED. GENERATOR RESET DID NOT CO RRECT CONDITION, EICAS MSG AC BUS OFF REMAINED DISPLAYED. MAINTENANCE REMOVED AND REPLACED THE RIGHT IDG PER MM 57-24-0 1, PAGE 1-14. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002041500117 20020415 00117 NM 2002 4 15 AWXA200200336 1 20020330 A 5753 654648120 SPINDLE BOEING 737 7373G7 1384595 NM T/E FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CORROSION FLAP SYSTEM - DURING C12 CHECK CORROSION WAS FOUND ON THE NR 7 FLAP TRACK CARRIAGE SPINDLE AT SLEEVE THR OUGH BOLT AREA. MAINTENANCE REMOVED AND REPLACED THE NR 7 FLAP TRACK CARRIAGE SPINDLE ASSEMBLY IAW AWA T/C C3R57024. 2 L 7 2 4F RT A16WE 2002041700129 20020417 00129 NE 2002 4 17 AWXA200200337 2 20020412 A 7510 324425 ANTI-ICE VALVE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 ENGINE CLOSED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 631AW 35664 11835 077 YKM - DIVERSION - EN ROUTE FROM PHX TO SEA LT ENGINE ANTI-ICE VALVE CLOSED, ECAM WARNING OCCURRED AFTER SELECTION OF ANT I-ICE TO ON. TRIED VARIOUS POWER SETTINGS UP TO FULL CLIMB POWER TO OPEN THE ANTI-ICE VALVE, ATTEMPTS WERE UNSUCCESSFUL , DUE TO ICING CONDITIONS DIVERTED TO YKM. THE ANTI-ICE VALVE WAS REPLACED IAW AMM 30-21-51-401, OPERATIONAL CHECK WAS GOOD AND MEL 30-21-01, COND NR 2 WAS CLEARED. 2 L 7 2 4F 4 F RT A28NM E311NE 2002041500118 20020415 00118 GL 2002 4 15 C2XA02CL099 2 20020411 A 7313 3035060 NOZZLE EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL NR 2 ENGINE COKED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 27512 145274 CAE311437 CLE FLIGHT 3085 THE CREW REPORTED A STRONG BURNING ODOR DURING ICE TEST AND WHEN NR 2 PACK IS ON. MAINTENANCE REPLACED THE NR 2 ENGINE FUEL NOZZLES. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002061300169 20020613 00169 SO 2002 6 13 C2XA02TY072 1 20020414 A 7120 14529426001 YOKE EMB 145 EMB145LR 3260212 SO LT PYLON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16954 145072 TYS, DURING A SCHEDULE ENGINE CHANGE ON THE LEFT ENGINE, THE FORWARD MOUNT YOKE, UPPER AFT ATTACHMENT BOLT HOLE WAS FOUN D OVERSIZED, THE HAT BUSHING MOVES FREELY AND ROCKS WHILE IN POSITION. MAINTENANCE APPLIED AS700 SEALANT TO THE BUSHING AND REINSTALLED. EMBRAER AUTHORIZES TO FLY FOR 400 FLIGHT CYCLES TILL A PERMANENT DISPOSITION CAN BE SENT IAW-EMB-GST- 1198/02. AN APPROVED REPAIR WAS OBTAINED, WHICH WILL REWORK THE AFFECTED YOKE IAW-EC5420-01035. 2 L 7 2 4T RT T00011AT 2002041500120 20020415 00120 NM 2002 4 15 DHL2002743003 1 20020410 A 2612 FIRE DETECTOR BOEING 727 727225 1384077 NM NR 1 ENGINE MALFUNCTIONED A DHLA K NONE L NO TEST UK UNKNOWN 1 SO 01 743DH 22438 NR 1 DET CIRCUIT GRD LIGHT DOES NOT ILLUM W/ FIRE TEST. BOOT STRAPPED NEW FIRE LOOP NR 1 ENG, NO HELP. SWAPPED OPERATI NG PWR UNIT, NO HELP. SWAPPED R604 & R605, NO HELP. INSPECTED ENG WIRING, NO DEFECTS. R&R FIRE & OVERHEAT DET ACCY UN IT, NO HELP. ORIG ACCY UNIT REINSTALLED DMI REMAINS OPEN. RAN ENG FIRE TEST ON GROUND. SYS OPS CHECKS NORM, PLACARD R EMOVED. 2 L 7 3 4F A3WE 2002041500121 20020415 00121 WP 2002 4 15 DHL2002802001 1 20020410 A 2611 SMOKE DETECTOR DOUG DC8 DC873 302199C WP CARGO BAY INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802DH 46076 UPPER CARGO NR 1 SMOKE DETECTOR WON'T TEST. RELAMPED NR 1 SMOKE DETECTOR, TEST CHECKS OK AS PER MM 26-26 AS NEEDED. 2 L 7 4 4F RT 4A25 2002041500122 20020415 00122 CE 2002 4 15 DJFA0127 1 20020228 A 3010 1283840545 CONTACTOR BEECH MU300 400A 1155402 CE ANTI-ICE SYS FAILED E DJFA K NONE J WARNING INDICATION NR NOT REPORTED 1 EA 23 495CW RK5 HORIZONTAL STAB ANTI-ICE INOPERATIVE. HORIZONTAL STAB ICE FAIL WARNING LIGHT COMES ON IMMEDIATELY WHEN HORIZONTAL STAB ANTI-ICE IS TURNED ON. RECYCLED CIRCUIT BREAKERS AND SWITCHES NUMEROUS TIMES. GROUND CHECKS OK. NUMEROUS FAILURES (73 ) OF THIS PART ON OUR FLEET OF 26 BEECHJETS WITHIN THE LAST YEAR. 2 H 7 2 4F RT A16SW 2002041500123 20020415 00123 NM 2002 4 15 DL777020249 1 20020303 A 3350 873605 POWER SUPPLY BOEING 777 777232 1385232 NM E/E BAY FAULTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 865DA C532 29737 STRONG BURNING SMELL IN CABIN, INFLIGHT. EMERGENCY DECLARED INTO ATL. REMOVED AND REPLACED POWER SUPPLY. UNIT SENT TO MANUFACTURER FOR ANALYSIS. SUSPECT FOREIGN RESIDUE MAY HAVE CONTRIBUTED TO THE FAILURE. 2 L 7 2 4F RT T00001SE 2002041500124 20020415 00124 NM 2002 4 15 DLM11020254 1 20020304 A 2530 72077500 OVEN DOUG MD11 MD11 3023602 NM GALLEY MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 802DE 48473 MID GALLEY OVENS OVERHEAT AND CAUSE SURROUNDING PANELS TO WARM BEYOND TOUCH SLIGHT BURNING SMELL REPORTED BY F/A. REMOV ED AND REPLACED OVEN NR 2 MID GALLEY, OPS GOOD. 2 L 7 3 4F RT A22WE 2002041500125 20020415 00125 NM 2002 4 15 DLM11020256 1 20020304 A 2560 BATTERY DOUG MD11 MD11 3023602 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 808DE 48479 EMERGENCY FLASHLIGHT AT 4R INBOARD BATTERY LOW. REMOVED AND REPLACED FLASHLIGHT AND BATTERY, OPS NORMAL. 2 L 7 3 4F RT A22WE 2002041500126 20020415 00126 NM 2002 4 15 DLM11020262 1 20020226 A 5514 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 804DE 48475 CORROSION WAS FOUND IN THE BORES OF THE UPPER SURFACE BARREL NUT HOLES AT 49 LOCATIONS ON THE HORIZONTAL STABILIZER. RE PAIRED PER ER/A 412361-14. 2 L 7 3 4F RT A22WE 2002041500127 20020415 00127 NM 2002 4 15 DLM11020288 1 20020310 A 8012 77553815 START VALVE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 804DE 48475 723955 ATB FOR NUMBER 3 ENG START VALVE LIGHT FLICKERING DURING FLIGHT. REPLACED NR 3 START VALVE AND PRESSURE SWITCH. 2 L 7 3 4F 4 F RT A22WE E24NE 2002041500128 20020415 00128 NM 2002 4 15 DLM11020291 1 20020309 A 3830 FLUSH MOTOR DOUG MD11 MD11 3023602 NM LAVATORY FAULTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 804DE 48475 LAV SMOKE WARNING ILLUMINATED. FLT ATTN FOUND NO SMOKE BUT ODOR L4 LAV. FOUND L4 TOILET VALVE MOTOR SMOKING. REPLACED TOILET ASSY. 2 L 7 3 4F RT A22WE 2002041500129 20020415 00129 NM 2002 4 15 DLM11020330 1 20020315 A 5220 23962368 RELIEF VALVE DOUG MD11 MD11 3023602 NM EMERGENCY EXIT OPEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 803DE 48474 ON TRIP CHECK, FOUND L1 DOOR EMERGENCY EXIT N2 RESERVOIR PRESSURE READING 0 PSI. FOUND PRESSURE RELIEF VALVE OPEN. REP LACED PRESS RELIEF VALVE PER M/M. CHARGED N2 PRESSURE AND PRESSURE CHECKS OKAY PER M/M. 2 L 7 3 4F RT A22WE 2002041500130 20020415 00130 NM 2002 4 15 DLM11020389 1 20020331 A 2497 WIRE HARNESS DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 2 ENGINE CHAFED A DALA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 27 809DE 17668 48480 723923 AT FL330 NR 2 ENGINE FIRE WARNING SOUNDED. PULLED T-HANDLE. DECLARED AN EMERGENCY AND DIVERTED TO CLT. NO EVIDENCE OF FIRE FOUND. FOUND CHAFED IDG FEEDER CABLE ONTO FIRE LOOP WHICH ARCED AND DAMAGED FIRE DETECTOR CONTROL UNIT. REPLACED FDCU, LOOP, AND FEEDER HARNESS. 2 L 7 3 4F 4 F RT A22WE E24NE 2002041500131 20020415 00131 NM 2002 4 15 DLM11020392 1 20020331 A 2612 FIRE WARNING DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE COCKPIT ACTIVATED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 809DE 48480 723923 ON GROUND AFTER DIVERTING TO CLT FOR NR 2 ENG FIRE WARNING, R1 DOOR SLIDE INFLATED INTO CABIN. INCIDENT UNDER INVESTIGA TION BY NTSB. 2 L 7 3 4F 4 F RT A22WE E24NE 2002041500133 20020415 00133 NM 2002 4 15 DLM88020212 1 20020218 A 2450 HDX9F011 RELAY DOUG MD88 MD88 3023688 NM EPC PANEL BURNED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 926DL 49713 FOUND R2-50 AC GND SERVICE TIE RELAY BURNED AND DAMAGED, TERMINALS AT A2 AND B2 DAMAGED. REPLACED WIRE NB X226A10A. IN STALLED NEW TERMINAL ENDS AT A2 AND B2 AND REPLACED C/B B1-241. 2 L 7 2 4F RT A6WE 2002041500134 20020415 00134 NM 2002 4 15 DLM88020217 1 20020221 A 2420 3101363901 TRANSFORMER DOUG MD88 MD88 3023688 NM COCKPIT SHORTED A DALA A UNSCHED LANDING J G WARNING INDICATION MULTIPLE FAILURE CL CLIMB 1 SO 27 901DL 49532 STALL IND FAILURE ILLUMINATED ON AOP, RT ENG OIL PRESSURE, HYDRAULIC QTY AND RT FLAP IND LOST SIGNAL. REPLACED POWER TR ANSFORMER. 2 L 7 2 4F RT A6WE 2002041500135 20020415 00135 NM 2002 4 15 DLM88020218 1 20020222 A 3211 5935376501 PIN DOUG MD88 MD88 3023688 NM LT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 DURING INSPECTION OF THE MLG AT HMV THE LT MLG FWD TRUNNION ATTACH PIN WAS FOUND TO HAVE CORROSION CAUSING LOOSENESS IN THE ATTACH POINT. 2 L 7 2 4F RT A6WE 2002041500136 20020415 00136 2002 4 15 SWAA020758 4 20020409 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691WN 23781 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002041500137 20020415 00137 NM 2002 4 15 SWAA020759 1 20020409 A 3350 311500 LENS BOEING 737 7373G7 1384595 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691WN 23781 DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW NR 20 DEF. SECURED LENS PER M M. 2 L 7 2 4F RT A16WE 2002041500138 20020415 00138 NM 2002 4 15 SWAA020761 1 20020409 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D PLUS 4, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002041500139 20020415 00139 NM 2002 4 15 SWAA020763 1 20020409 A 5311 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 440, BETWEEN STR 4R AND 12R. REMOVED AND REPLACED SHEAR T IE PER SRM. 2 L 7 2 4F RT A16WE 2002041500140 20020415 00140 NM 2002 4 15 SWAA020764 1 20020410 A 3230 6968730 VALVE BOEING 737 737317 138447P NM MLG W/W DAMAGED A SWAA D A RETURN TO BLOCK UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 693SW 23174 AIR TURNBACK, AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. FOUND INNER STRUT SUPPORT VALVE DAMAGED, WOULD NOT LET STRU T FULLY EXTEND AND ACTUATE AIR SENSOR. REPACKED INNER STRUT AND REMOVED AND REPLACED SUPPORT VALVE PER MM. 2 L 7 2 4F RT A16WE 2002041500141 20020415 00141 NM 2002 4 15 DLM88020225 1 20020224 A 3070 2120565 HEATER DOUG MD88 MD88 3023688 NM LAVATORY SHORTED A DALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 949DL 49880 SMOKE REPORTED ON APPROACH TO ATL IN AFT LT LAV. FOUND AFT LT LAV WATERLINE HEATER SHORTED CAUSING TEFLON TAPE TO MELT. REPLACED HEATER. 2 L 7 2 4F RT A6WE 2002041500142 20020415 00142 NM 2002 4 15 DLM88020259 1 20020305 A 3397 WIRE DOUG MD88 MD88 3023688 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 919DL 49584 EMERGENCY TRACK LIGHTING AT ROW 30 INOP. REPAIRED BROKEN WIRING, OPERATIONAL CHECKS OK. 2 L 7 2 4F RT A6WE 2002041500143 20020415 00143 NM 2002 4 15 DLM88020279 1 20020309 A 2910 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM LOOSE A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 971DL 53214 RETURNED ACFT TO GATE DUE TO SMOKE INSIDE CABIN AND COCKPIT. FOUND LOOSE HYDRAULIC LINE ON THRUST REVERSER CONTROL VALV E. TIGHTENED SAME, PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2002041500144 20020415 00144 NM 2002 4 15 DLM88020304 1 20020313 A 1430 MS21059L3 NUT DOUG MD88 MD88 3023688 NM R1 THRESHOLD DAMAGED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 930DL 49717 DOOR 1R GIRT BAR ATTACH FITTING COULD NOT BE SECURED. FOUND NUTS DAMAGED. REPLACED SAME. 2 L 7 2 4F RT A6WE 2002041500145 20020415 00145 NM 2002 4 15 DLM88020310 1 20020315 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN SHORTED A DALA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 27 912DL 49543 AFTER PUSH BACK EMERGENCY LIGHTS IN F/C FAIL TO COMES ON. REPLACED FUSE IN F/C BATT PACK BETWEEN WINDOWS 7 AND 8, FOUND SHORT IN LIGHT ASSY FOR SEAT 4DC. REPLACED SAME, CHECKS GOOD. 2 L 7 2 4F RT A6WE 2002041500146 20020415 00146 2002 4 15 SWAA020768 4 20020410 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002041500147 20020415 00147 NM 2002 4 15 SWAA020771 1 20020411 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 395SW 27689 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL WEB CRACKED AT BS 178, WL 180 AT RBL 5.7. REPAIRED WEB PER CASCADE AEROSPAC E ERO. 2 L 7 2 4F RT A16WE 2002041500148 20020415 00148 NM 2002 4 15 SWAA020772 1 20020411 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002041500149 20020415 00149 NM 2002 4 15 SWAA020774 1 20020410 A 5230 6545871 FRAME BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD OUTER FRAME CRACKED. REMOVED AND REPLACED DOOR PER MM. 2 L 7 2 4F RT A16WE 2002041500150 20020415 00150 NM 2002 4 15 SWAA020775 1 20020411 A 3220 65C2803419 SENSOR BOEING 737 7373TO 138447G NM NLG OUT OF ADJUST A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 697SW 23838 NOSE GEAR RED LIGHT DID NOT EXTINGUISH ON TAKEOFF. RECYCLE HANDLE, NO HELP. PULLED AND RESET AIR/GRD RELAY CB AND LIGH T WENT OUT. ADJUSTED NOSE GEAR LOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2002041500151 20020415 00151 NM 2002 4 15 DLM88020316 1 20020316 A 2120 ODOR DOUG MD88 MD88 3023688 NM CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 915DL 49546 ON CLIMBOUT OF PWM CREW NOTICED ODOR THAT RESEMBLED CAR EXHAUST IN CABIN. ENG AT 1.77 EPR BOTH PACKS ON. CREW REPORT T HAT SMELL WAS NOT ACRID LIKE ELECTRICAL. A/C WAS BEING FERRIED TO ATL. T/S PER OPN 5088 PNEUMATIC DISTRIBUTION CABIN S MOKE/ODOR FIG 5 AND FIG 7, NO TROUBLE FOUND AND NO SMOKE OR ODOR NOTED. PER OPN 5088 PERFORMED DUCT BURNOUT OPN 5089 A/ C OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2002041500152 20020415 00152 NM 2002 4 15 DLM88020322 1 20020318 A 5321 9952521 FLOOR PANEL DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 DURING HMV THE 9952521-12, -71, AND -84 FLOOR PANELS WERE FOUND DAMAGED. REPAIR PER ER/A 411064-14. 2 L 7 2 4F RT A6WE 2002041500153 20020415 00153 NM 2002 4 15 P2EA2000V0003 1 20020219 A 5315 FLOORBEAM BOEING 737 73725A 1384481 NM FUSELAGE CORRODED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 344 BTW LBL 14 AND LBL 21. FLOORBEAM REPAIRED I AW SRM 53-10-9, FIG 5. 2 L 7 2 4F RT A16WE 2002041500154 20020415 00154 NM 2002 4 15 P2EA2000V0008 1 20020219 A 5315 FLOORBEAM BOEING 737 73725A 1384481 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1+Q2 INSPECTION, AFT GALLEY AREA BS 1016 LBL 33 FLOORBEAM WITH CORROSION. FLOORBEAM REPAIRED IAW EO B737MC53-01 9/02, BOEING SL 737-SL-53-036 AND DWG NR 65C37528, 65C37472. 2 L 7 2 4F RT A16WE 2002041500155 20020415 00155 2002 4 15 P2EA2002M019 4 20020403 A 3460 COMPUTER DOUG DC9 DC987 3022087 WP COCKPIT MALFUNCTIONED A P2EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 136NJ 49413 NR 1 & NR 2 FLT GUIDANCE COMPUTER WENT BLANK DURING FLIGHT. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO INCIDENT. PER FORMED RETURN TO SERVICE TEST ON BOTH DIGITAL FLIGHT GUIDANCE COMPUTER IAW MM 22-01-05. OPERATIONAL CHECKED GOOD. 2 L 7 2 4F RT A6WE 2002041500156 20020415 00156 WP 2002 4 15 P2EA2002M020 1 20020405 A 5270 TARGET DOUG DC9 DC987 3022087 WP CARGO DOOR OUT OF ADJUST A P2EA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 05 132NJ 49780 AFTER TAKEOFF THE FORWARD CARGO DOOR OPEN LIGHT ILLUMINATED. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO INCIDENT. AD JUSTED DOOR SENSOR TARGET IAW MM 53-31-00. OPERATIONAL NORMAL. 2 L 7 2 4F RT A6WE 2002041500157 20020415 00157 WP 2002 4 15 P2EA2002M021 1 20020405 A 2742 95906 ACTUATOR DOUG DC9 DC982 3022082 WP HORIZ STAB MALFUNCTIONED A P2EA K NONE F FLT CONT AFFECTED AP APPROACH 1 CE 05 135NJ 49440 ON FINAL APPROACH INTO LAX BOTH PRIMARY AND ALTERNATE STAB TRIM FAILED TO WORK. AFTER THREE MINUTES BOTH RESUMED WORKIN G. REMOVED AND REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR IAW MM 27-40-01. 2 L 7 2 4F A6WE 2002041500158 20020415 00158 WP 2002 4 15 P2EA2002M022 1 20020409 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 135NJ 49440 EMERGENCY POWER CHECK DOES NOT HAVE PROPER VOLTS AND AMPS. REMOVED AND REPLACED EMERGENCY POWER BATTERYS IAW MM 24-30-0 1, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002041500159 20020415 00159 NM 2002 4 15 P2EA2002V0001 1 20020219 A 5315 FLOORBEAM BOEING 737 73725A 1384481 NM FUSELAGE SCRATCHED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1+Q2 INSPECTION, PAX CABIN AT BS 380 BETWEEN RBL 24.5 AND RBL 45.5 FLOORBEAM UPPER CHORD WITH SCRATCH. SCRATCH REPAIRED IAW SRM 53-10-9 FIG 1. 2 L 7 2 4F RT A16WE 2002041500160 20020415 00160 NM 2002 4 15 P2EA2002V0002 1 20020219 A 5315 FLOORBEAM BOEING 737 73725A 1384481 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1+Q2 INSPECTION, PAX CABIN FLOORBEAM UPPER CHORD WITH CORROSION AT BS 947.5 BETWEEN LBL 5 AND RBL 5. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 2. 2 L 7 2 4F RT A16WE 2002041500161 20020415 00161 NM 2002 4 15 P2EA2002V0004 1 20020218 A 5315 FLOORBEAM BOEING 737 73725A 1384481 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 328 AND LBL 28. FLOORBEAM REPAIRED IAW SRM 53-1 0-9 FIG 6. 2 L 7 2 4F RT A16WE 2002041500162 20020415 00162 NM 2002 4 15 P2EA2002V0005 1 20020218 A 5315 FLOORBEAM BOEING 737 73725A 1384481 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 312 AND LBL 8. FLOORBEAM REPAIRED IAW SRM 53-10 -9 FIG 5. 2 L 7 2 4F RT A16WE 2002041500163 20020415 00163 NM 2002 4 15 P2EA2002V0006 1 20020218 A 5315 FLOORBEAM BOEING 737 73725A 1384481 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 294.5 BL 0. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 5. 2 L 7 2 4F RT A16WE 2002041500164 20020415 00164 NM 2002 4 15 P2EA2002V0007 1 20020219 A 5315 FLOORBEAM BOEING 737 73725A 1384481 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1+Q2 INSPECTION, PAX CABIN BS 294.5 FLOORBEAM UPPER CHORD LWR SURFACE WITH CORROSION RBL 24. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 6. 2 L 7 2 4F RT A16WE 2002041500165 20020415 00165 NM 2002 4 15 P2EA2002V0009 1 20020219 A 5315 FLOORBEAM BOEING 737 73725A 1384481 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1+Q2 INSPECTION, PAX CABIN RBL 12 BS 360 FLOORBEAM WITH CORROSION. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 1. 2 L 7 2 4F RT A16WE 2002041500166 20020415 00166 NE 2002 4 15 DLM88020342 2 20020320 A 7530 LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE LOOSE A DALA O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 SO 27 961DL 4092 49980 031100 ON APPROACH APPROX 1500 AGL JUST INSIDE THE OUTER MARKER NR 1 ENG ROLLED BACK TO APPROX 40 PERCENT. PACK TRIPPED. SELE CTED CONTINUOUS IGNITION. ADVANCED THROTTLES AND ENGINE RECOVERED. FOUND PS4 LINE AT PRBC LOOSE, TIGHTENED AND RESAFET IED SAME, RAN ENG PER PFHB, ALL INDICATIONS AND ENG PARAMETERS NORMAL. UNABLE TO DUPLICATE. ENG OK FOR SERVICE. 2 L 7 2 4F 4 F RT A6WE E9NE 2002041500167 20020415 00167 WP 2002 4 15 MWEA020225 1 20020412 A 5720 49192851 CLIP DOUG DC9 DC932 3022066 WP STATION XRS 69 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING TANK STATION XRS 69 RIB ATTACH CLIP IS CRACKED AT STRINGER #2. -- REMOVED AND REPLACED CLIP. 2 L 7 2 4F A6WE 2002041500168 20020415 00168 WP 2002 4 15 MWEA020237 1 20020412 A 5712 4911499510 CLIP DOUG DC9 DC932 3022066 WP STATION XRS 69 INADEQUATE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 REMOVED ATTACH FITTING AT BULKHEAD XRS 69, BETWEEN STRINGER 21 THROUGH 22 RIGHT WING TO FACILITATE OTHER MAINTENANCE. - - NEW CLIP NEEDED DUE TO BUILD UP OF REPAIR ON STRINGER. FABRICATED AND INSTALLED CLIP. 2 L 7 2 4F A6WE 2002041500169 20020415 00169 WP 2002 4 15 MWEA020238 1 20020412 A 5720 4912012505 CLIP DOUG DC9 DC932 3022066 WP STATION XRS 69 INADEQUATE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING RIB ATTACH CLIP AT BULKHEAD 69 BETWEEN STRINGERS 22 AND 23 TO FACILITATE OTHER MAINTENANCE. -- REMOVED AND R EPLACED CLIP. REPLACEMENT OF CLIP WAS REQUIRED DUE TO REPAIR IN AREA. 2 L 7 2 4F A6WE 2002041500170 20020415 00170 WP 2002 4 15 MWEA020248 1 20020412 A 5720 4911308504 CLIP DOUG DC9 DC932 3022066 WP STATION XRS 91 INADEQUATE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 STATION XRS 91, STRINGER 21, STRINGER TO BULKHEAD ATTACH CLIP REMOVED TO FACILITATE OTHER MAINTENANCE. -- REMOVED AND REPLACED CLIP. NEW CLIP NEEDED DUE TO BUILD UP OF REPAIR. 2 L 7 2 4F A6WE 2002041500171 20020415 00171 WP 2002 4 15 MWEA020249 1 20020412 A 5320 9955780673 ANGLE DOUG DC9 DC932 3022066 WP STATION 157 GROUNDED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 ANGLE FORWARD INBOARD CORNER IS GROUND OFF. LOCATED IN THE EPC PANEL. -- REMOVED AND REPLACED ANGLE. 2 L 7 2 4F A6WE 2002041500172 20020415 00172 WP 2002 4 15 MWEA020254 1 20020415 A 5412 9912243200 SHEAR TIE DOUG DC9 DC982 3022082 WP STATION 1369 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 RIGHT PYLON BULKHEAD STATION 1369 SHEAR TIE IS CRACKED LOCATED BETWEEN LONGERONS 13 RIGHT AND 14 RIGHT. -- FABRICATED AND INSTALLED SHEAR TIE REPAIR PARTS. 2 L 7 2 4F A6WE 2002041500173 20020415 00173 WP 2002 4 15 MWEA020255 1 20020415 A 5312 593643625 LONGERON DOUG DC9 DC982 3022082 WP STATION 1309 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 LONGERON 8 RIGHT IS CRACKED JUST ABOVE HYLOCK AT STATION 1309 MARKED WITH RED ARROW POINTING TO HYLOCK. -- FABRICATED AND INSTALLED LONGERON REPAIR PARTS. 2 L 7 2 4F A6WE 2002041500174 20020415 00174 WP 2002 4 15 MWEA020250 1 20020412 A 5711 5919153529 CAP DOUG DC9 DC932 3022066 WP STATION 380 INADEQUATE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 COMPLY WITH CARRY OVER 2681. LOWER CAP REPAIR, LEFT WING, AT STATION 380 REQUIRES REMOVING TEMPORARY REPAIR AND INSTALLA TION OF PERMANENT REPAIR. -- FABRICATED AND INSTALLED FILLERS AND REPAIR ANGLES. 2 L 7 2 4F A6WE 2002041500175 20020415 00175 NM 2002 4 15 DLM88020333 1 20020319 A 3260 SWITCH DOUG MD88 MD88 3023688 NM RT MLG FAULTY A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 993DL 53345 GEAR DOOR OPEN LIGHT REMAINS ON WITH LANDING GEAR IN UP OR DOWN POSITION. IN DOWN POSITION 3 GREEN LIGHTS ILLUMINATE. IN UP POSITION ALL GEAR LIGHTS EXTINGUISHED. APPROX BOX FAULTS SENSOR RT GEAR DOOR-FAIL 20. REPLACED D1-29R MAIN GEAR DOOR SW PER M/M, RT GEAR DOOR INDICATION CHECK GOOD PER MM. 2 L 7 2 4F RT A6WE 2002041500176 20020415 00176 NM 2002 4 15 DLM88020345 1 20020221 A 5321 9952521 FLOOR PANEL DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 FUSELAGE CABIN FLOOR PANEL WAS FOUND DELAMINATED AND CRACKED. REPAIR PER ER/A 411006-14. 2 L 7 2 4F RT A6WE 2002041500177 20020415 00177 NM 2002 4 15 DLM88020354 1 20020321 A 4990 LINE DOUG MD88 MD88 3023688 NM A/C BAY LOOSE A DALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 937DL 49810 ON TAKEOFF SMOKE AND FUMES IN CABIN. ALL LAV SMOKE DETECTORS WENT OFF. RAN ENGS PER MCC, NO SMOKE. C/W OPNS 5088 AND 5089 ALL CHECK GOOD. FOUND LOOSE OIL SUPPLY LINE NEAR APU OIL COOLER. SECURED SAME. 2 L 7 2 4F RT A6WE 2002041500178 20020415 00178 NM 2002 4 15 DLM88020377 1 20020327 A 2150 20495062 ACM DOUG MD88 MD88 3023688 NM A/C BAY FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 968DL 53161 RUBBER SMELL REPORTED BY PAX AND FLT ATTENDANTS SHORTLY AFTER T/O. CLEARED QUICKLY, TOWER REPORTED NO RUBBER ON RUNWAY. REMOVED AND REPLACED LEFT ACM PER MM, LEAK AND OPS CHECKS GOOD. 2 L 7 2 4F RT A6WE 2002041500179 20020415 00179 NM 2002 4 15 DLM88020380 1 20020328 A 2740 575600015 SENSOR DOUG MD88 MD88 3023688 NM HORIZ STAB FAILED A DALA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SO 27 935DL 49722 PRIMARY TRIM RAN AWAY NOSE UP. AIRCRAFT RETURN TO B-13. REPLACED STAB MOTION SENSOR C/W ADJ/TEST PER MM 27-40-04-5 AND 27-40-02-2 AND VISUALLY INSPECTED STAB JACKSCREW, NTF. 2 L 7 2 4F RT A6WE 2002041500180 20020415 00180 NM 2002 4 15 DLM88020396 1 20020402 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 973DL 53241 EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE DURING TEST. REPLACED BATTERY PACK POWER SUPPLY AND BATTERIES. 2 L 7 2 4F RT A6WE 2002041500181 20020415 00181 2002 4 15 F3LA200200120 4 20020401 A 2330 RDAX730801 VIDEO UNIT BOEING 737 7373L9 1384470 NM CABIN SHORTED A F3LA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 313FL 26442 FLIGHT CREW REPORTED ENTERTAINMENT TAPE RECORDER SMOKING EN ROUTE TO DEN. DIVERTED TO SLC AND LANDED WITHOUT INCIDENT. ISOLATED ELECTRICAL SHORT IN TAPE PLAYER. PULLED AND COLLARED CIRCUIT BREAKER E7 ON P6-1 PANEL. REMOVED TAPE PLAYER F ROM WALL ABOVE FWD FLIGHT ATTENDANT SEAT AND SECURED CANNON PLUG TO WALL WITH TAPE. DEACTIVATED AND REMOVED TAPE REPROD UCER PER EA 23-737-021. 2 L 7 2 4F RT A16WE 2002041500185 20020415 00185 NM 2002 4 15 F3LA200200124 1 20020405 A 5230 CROSSBEAM BOEING 737 7373L9 1384470 NM CARGO DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 3415 24569 DURING C-4 CHECK, INSPECTION REPORTED C-1 DOOR LOWER CROSSBEAM WEB CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTAL LED DOUBLER REPAIR PER SRM 51-70-13. 2 L 7 2 4F RT A16WE 2002052000136 20020520 00136 CE 2002 5 20 GLBA2002044 1 20020402 A 7722 1303800415 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 179GL 15004 UE179 RIGHT ITT INDICATOR FAILED ON CLIMBOUT. REPLACED INDICATOR. 2 L 7 2 4T RT A24CE 2002041500186 20020415 00186 CE 2002 4 15 GLBA2002046 1 20020406 A 2150 WARNING SYSTEM BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 150GL UE150 RIGHT ENVIRONMENTAL FAIL ILLUMINATED. COULD NOT DUPLICATE FAULT. 2 L 7 2 4T RT A24CE 2002041500187 20020415 00187 SO 2002 4 15 LR7A02027 1 20020328 A 5523 33265891 HORN LKHEED 382 382G 526414U SO ELEVATOR TAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 609 4763 DURING SCHEDULED B3 INSPECTION, FOUND LT ELEVATOR TRIM TAB INBOARD AFT HORN BRACKET CRACKED AT HSS 99, FS 1153, WL 277. REPLACED HORN ASSY IAW SMP 581 91-00. OPERATIONAL CHECK AND RIGGING COMPLIED WITH IAW SMP 581 27-31 PG 218 AND 201. 2 H 7 4 4T A1SO 2002041500188 20020415 00188 SO 2002 4 15 LR7A02028 1 20020329 A 2170 1858486 COALESCER BAG LKHEED 382 382G 526414U SO A/C BAY DIRTY A LR7A K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 AL 03 402LC 408 4698 FLIGHT CREW REPORTED FLIGHT DECK AIR CONDITIONING SYSTEM GIVES OFF AN OILY SMELL TO FLIGHT STATION ON GROUND. REPLACED FLIGHT STATION WATER SEPARATOR COALESCER IAW SMP 581 CH 21A-50. OPS CHECK NORMAL. 2 H 7 4 4T A1SO 2002041500189 20020415 00189 WP 2002 4 15 MWEA020186 1 20020322 A 5753 995757822 PANEL DOUG DC9 DC932 3022066 WP T/E FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LEFT FLAP TRAILING EDGE PANEL NR 3 HAS MODERATE TO HEAVY CORROSION AROUND FINGER DOUBLERS IN SEVERAL BAYS. FINGER DOUBL ERS LOOSE IN SEVERAL AREAS. FABRICATED AND INSTALLED LOWER AND UPPER PANELS. 2 L 7 2 4F A6WE 2002041500190 20020415 00190 WP 2002 4 15 MWEA020188 1 20020327 A 5320 5956034535 BRACKET DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 CORROSION ON ANGLE BRACKET FOR FLOOR SUPPORT AT STATION 367 RIGHT SIDE. REMOVED AND REPLACED BRACKET. 2 L 7 2 4F A6WE 2002041500191 20020415 00191 WP 2002 4 15 MWEA020191 1 20020327 A 5320 99100789 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 CORROSION ON CELING IN E&E BAY FROM STATION 200 TO 218 JUST BELOW THE CUSP LINE NEAR LONGERON 18 LEFT. REMOVED DAMAGED SECTION OF UPPER CUSP ANGLE. FABRICATED AND FORMED -3 REPAIR SPLICE. INSTALLED CUSP ANGLE AND SPLICE. 2 L 7 2 4F A6WE 2002041500192 20020415 00192 WP 2002 4 15 MWEA020194 1 20020327 A 5542 5910256501 PANEL DOUG DC9 DC932 3022066 WP RUDDER DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 DENT DAMAGE ON RUDDER LEADING EDGE STRUCTURE AT STATION ZR70 RIGHT SIDE. MEASURES APPROX 4 INCHES IN LENGTH. FABRICATE D AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2002041500193 20020415 00193 WP 2002 4 15 MWEA020196 1 20020327 A 5753 59304961 VANE DOUG DC9 DC981 3022081 WP T/E FLAP DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 LEFT WING OUTBOARD FLAP, INBOARD FIXED VANE HAS A 2 INCH BY 2 INCH AREA OF DELAMINATION 4 INCHES INBOARD OF OUTBOARD UPP ER EDGE. REMOVED AND REPLACED CORE. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002041500194 20020415 00194 WP 2002 4 15 MWEA020197 1 20020327 A 5522 591041281 TIP CAP DOUG DC9 DC981 3022081 WP ELEVATOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 RIGHT ELEVATOR TIP END HAS SEVERAL ELONGATED HOLES. FABRICATED AND INSTALLED TIP END. 2 L 7 2 4F A6WE 2002041500195 20020415 00195 WP 2002 4 15 MWEA020198 1 20020327 A 5753 59304961 VANE DOUG DC9 DC981 3022081 WP T/E FLAP DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 LEFT WING OUTBOARD FLAP, INBOARD FIXED VANE HAS A 2 INCH BY 2 INCH AREA OF DELAMINATION 12 INCH INBOARD OF OUTBOARD LOWE R EDGE. FABRICATED AND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F A6WE 2002041500196 20020415 00196 WP 2002 4 15 MWEA020199 1 20020327 A 5753 59304762 SKIN DOUG DC9 DC981 3022081 WP T/E FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 RIGHT FLAP HAS A CRACK FROM A SCREW HOLE, 3RD FLAP TRAILING EDGE REMOVABLE SECTION OUT FROM THE FUSELAGE. THE CRACK IS ON THE TOP BACK SIDE. FABRICATED AND INSTALLED PLUG AND DOUBLER. 2 L 7 2 4F A6WE 2002041500197 20020415 00197 WP 2002 4 15 MWEA020200 1 20020327 A 5753 59304952 VANE DOUG DC9 DC981 3022081 WP T/E FLAP DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 TWO SPOTS OF DELAMINATION ON THE RIGHT WING, FIXED FLAP VANE (NR 2 FROM FUSELAGE) ON TOP AFT SIDE. APPLIED COLD BOND RE PAIR. 2 L 7 2 4F A6WE 2002041500198 20020415 00198 WP 2002 4 15 MWEA020202 1 20020327 A 5241 59131841 PAN DOUG DC9 DC981 3022081 WP GALLEY DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FORWARD GALLEY SERVICE DOOR PAN HAS TWO GOUGE MARKS LOCATED ON BOTTOM CENTER BY TWO RIVNUTS, WHICH APPEAR TO HAVE STRIPE D THREADS. DRILLED AND PLUGGED HOLES PER TELEX-MWX-ORD-02-00130H. 2 L 7 2 4F A6WE 2002041500199 20020415 00199 WP 2002 4 15 MWEA020203 1 20020327 A 5320 99115173 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 STATION 180 INTERCOSTAL HAS TWO DAMAGED FASTENER HOLES AT A GUSSET 40 INCHES RIGHT OF THE AIRCRAFT CENTERLINE. FABRICAT ED AND INSTALLED STACKED ANGLE REPAIR. 2 L 7 2 4F A6WE 2002041500200 20020415 00200 WP 2002 4 15 MWEA020206 1 20020329 A 5330 591140216 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 FUSELAGE SKIN DAMAGE WHERE PAX DOOR HOLD OPEN HOOK LATCHES. INSTALLED EXTERNAL DOUBLER. 2 L 7 2 4F A6WE 2002041500201 20020415 00201 WP 2002 4 15 MWEA020208 1 20020404 A 3260 D126 UPLOCK SWITCH DOUG DC9 DC981 3022081 WP MLG MALFUNCTIONED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 803ME 48029 MAIN GEAR INDICATOR UNSAFE LIGHT ILLUMINATED AFTER RETRACTION. REPLACED MAIN LANDING GEAR UPLOCK SWITCH D1-26 AND CONNE CTOR P1-1151 IAW WDM 32-61-00 AND STANDARD WIRING PRACTICES. ADJUSTED WEIGHT ON WHEELS CONDUIT ADD CLAMPS. 2 L 7 2 4F A6WE 2002041500202 20020415 00202 2002 4 15 MWEA020209 4 20020407 A 3431 CONNECTOR DOUG DC9 DC932 3022066 WP NAV ANTENNA DIRTY A MWEA A UNSCHED LANDING I FLT. ATTITUDE INST. AP APPROACH 1 GL 31 602ME 48133 LOCALIZER FLAGS ON BOTH NAV 1 AND NAV 2 FROM TWO DIFFERENT APPROACHES WITH TWO DIFFERENT FREQUENCYS. DISCONNECTED NR 1 AND 2 NAV ANTENNAS AND CLEANED. PERFORMED OPS CHECK OF FLIGHT DIRECTOR SYSTEM WITH LOCAL FREQUENCY AND WITH NAV TESTER. SYSTEM OPERATIONS CHECK GOOD PER MM 34-25-0. 2 L 7 2 4F A6WE 2002041500203 20020415 00203 WP 2002 4 15 MWEA020214 1 20020408 A 5512 59106257 SKIN DOUG DC9 DC932 3022066 WP HORIZ STAB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LEFT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AROUND SOME OF THE WRAP AROUND SCREWS (CENTER SECTION INBOARD AREA ). THERE WAS PREVIOUS BLEND OUT ALREADY IN THIS AREA. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002041500204 20020415 00204 WP 2002 4 15 MWEA020215 1 20020408 A 5512 59106257 SKIN DOUG DC9 DC932 3022066 WP HORIZ STAB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AROUND SOME OF THE WRAP AROUND SCREWS (CENTER SECTION INBOARD ARE A). THERE WAS PREVIOUS BLEND-OUT ALREADY IN THIS AREA. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002041500205 20020415 00205 WP 2002 4 15 MWEA020216 1 20020408 A 5330 59114013 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FUSELAGE CLASS III DOUBLER NEEDS UPGRADE AT STATION 218 LONGERON 25 LEFT. REMOVED DOUBLER, VERIFIED AS NO CRACKS IN SKI N. INSTALLED DOUBLER. REPAIR PLACED ON WATCH ITEM 6712 FOR REINSPECTION PER SRM 53-04 FIGURE 12B. 2 L 7 2 4F A6WE 2002041500206 20020415 00206 WP 2002 4 15 MWEA020217 1 20020408 A 5320 9955780681 ANGLE DOUG DC9 DC932 3022066 WP STATION 160 BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 CORROSION ON LOWER LEG FORWARD SIDE OF ELECTRONIC POWER CENTER PANEL SUPPORT FROM COCKPIT DOOR JAMB TO BANANA PANEL. FO UND ANGLE CRACKED OFF. REMOVED AND REPLACED ANGLE. 2 L 7 2 4F A6WE 2002041500207 20020415 00207 WP 2002 4 15 MWEA020222 1 20020408 A 5534 591218835 ANGLE DOUG DC9 DC932 3022066 WP VERTICAL STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 VERTICAL STABILIZER LEADING EDGE TAIL TO FUSELAGE DORSAL INTERNAL ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE BRACKET. 2 L 7 2 4F A6WE 2002041500208 20020415 00208 WP 2002 4 15 MWEA020224 1 20020408 A 5753 5910134151 SKIN DOUG DC9 DC932 3022066 WP T/E FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 LEFT FLAP LOWER SKIN HAS A SMALL AREA OF CORROSION ABOUT 20 INCHES OUTBOARD OF INBOARD FLAP HINGE. FABRICATED AND INSTA LLED REPAIR SKIN AND DOUBLERS. 2 L 7 2 4F A6WE 2002041500209 20020415 00209 NM 2002 4 15 DLM88020343 1 20020320 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG LOW A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 905DE 53410 NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO CLT. INSPECTED NOSE LANDING GEAR AND DOORS, NO DAMAGE OR FOREIGN OBJE CTS FOUND. NOSE GEAR OLEO FLAT ON ARRIVAL. SERVICED STRUT PER OPN 4703, SWUNG NOSE LANDING GEAR PER MM 07-11-00-2. GE AR RETRACTION AND INDICATION NORMAL. 2 L 7 2 4F RT A6WE 2002041500210 20020415 00210 WP 2002 4 15 2002F00376 1 20020228 A 2133 OUTFLOW VALVE LKHEED 1011 10113851 5265010 WP CABIN PRESSURE STUCK A AMTA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 186AT 193C1074 ON DEPARTURE FROM LAX, CABIN FAULT LIGHT CAME ON AT 8,000 FEET CABIN ALTITUDE. FORWARD OUTFLOW VALVE STUCK AND HORN AT FULL OPEN, AFT WENT TO FULL CLOSED. AIRCRAFT MADE EMERGENCY DESCENT AND LANDED WITHOUT INCIDENT. (M) 2 L 7 3 4F A23WE 2002041500211 20020415 00211 2002 4 15 2002F00377 4 20020301 A 3460 FMC BOEING 757 75733N 1384931 NM E/E BAY FAULTY A AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 554TZ 32588 WHILE EN ROUTE, FL370, SMOOTH AIR, AIRSPEED ORANGE BUG SLOWED TO 220 KT, THEN RETURNED TO NORMAL SPEED FOLLOWED BY AUTOP ILOT AND AUTOTHROTTLE DISCONNECT. AUTOPILOT RECONNECTED OK, AUTOTHROTTLE DIFFICULT TO RECONNECT. MAINTENANCE REPLACED LEFT FMC. (M) 2 L 7 2 4F RT A2NM 2002041500212 20020415 00212 WP 2002 4 15 2002F00379 1 20020201 A 5315 FLOORBEAM LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 186AT 193C1074 DURING SCHEDULED INSPECTION LEVEL 2 CORROSION, FOUND IN FLOORBEAM AT FS 901 BETWEEN LBL 74.5 TO 55.5. MAINTENANCE REPAI RED CORROSION IAW ATA ERA L10-53R-4686. (M) 2 L 7 3 4F A23WE 2002041500213 20020415 00213 EU 2002 4 15 AWXA200200339 1 20020413 A 3320 325060 BALLAST AIRBUS 320 A320231 3930325 EU SEAT ROW 19 L/H INOPERATIVE A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 626AW 0 0 65 ABQ - DIVERSION - FLT 0081 - WHILE ENROUTE FROM PHX TO BWI FLIGHT CREW RECEIVED MULTIPLE REPORTS (6+) OF AN INTENSE ELEC TRICAL BURNING SMELL IN THE CABIN CENTERED AROUND SEAT ROWS 15-18, SMELL PERSISTED FOR 5-7 MINUTES, PASSENGER ENTERTAINM ENT SYSTEM WAS DEACTIVATED, AND AIRCRAFT DIVERTED TO ABQ. MAINTENANCE INSPECTED THE PASSENGER SERVICE UNIT, CABIN LIGHTI NG BALLASTS, AND SEAT ELECTRICAL BOXES IN AND AROUND SEAT ROWS 15-18. BOTH PACKS WERE OPERATED USING APU AND ENGINE BLEE D AIR, PASSENGER ENTERTAINMENT SYSTEM WAS ALSO OPERATED, NO BURNING SMELL OR ODOR WAS NOTED. MAINTENANCE FOUND A BAD BAL LAST FOR CABIN LIGHTING AT SEAT ROW 19. PROBLEM WAS DEFFERED PLACED ON MEL 33-20-01, CONDITION 1, CABIN SIDEWALL LIGHT I 2 L 7 2 4F RT A28NM 2002041500214 20020415 00214 NM 2002 4 15 AWXA200200342 1 20020331 A 5313 BAC1498139 STRINGER BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 0 0 24710 MCN - MAJOR REPAIR - DURING C-12 CHECK A CRACK WAS FOUND ON STRINGER 16 ON CABIN R/H SIDE AT BS 500C+5, JUST FORWARD OF LIGHT. MAINTENANCE REMOVED DAMAGED END OF STR 16, FABRICATED A REPAIR CHANNEL, AND INSTALLED REPAIR IAW AWA ER 03-5314-0 2102-ES1. 2 L 7 2 4F RT A16WE 2002041600001 20020416 00001 SO 2002 4 16 C2XA02IA091 1 20020414 A 3350 SP9035 SPLICE EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16918 145397 IAH- DURING PERFLIGHT THE CREW NOTED THAT THE FRONT SECTION OF EMERGENCY LIGHTS NOT WORKING. IAH- MAINTENANCE RESECUR ED A LOOSE CONNECTOR AT THE FORWARD SECTION OF EMERGENCY LIGHTS, PERFORMED A OPERATIONAL CHECK OF THE EMERFENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCREFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002041600002 20020416 00002 WP 2002 4 16 CALA0200198 1 20020413 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP STA 1307 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND A 1" CRACK IN SKIN TO FRAME SHEAR TIE AT STA 1307, LONGERON 15R LAV BULKHEAD. THE #2 ENGINE WAS REMOVED FOR ACCESS. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-10-04 AND 51-30-5. THE #2 ENGINE WAS REINSTALLED. 2 L 7 2 4F A6WE 2002041600003 20020416 00003 WP 2002 4 16 CALA0200199 1 20020412 A 5320 FITTING DOUG DC9 DC982 3022082 WP STA 200-216 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND GALLEY FITTING CORRODED AT STA 200-216, RBL 22, UPON REMOVAL OF SUBFLOOR WEB. THE FITTING WAS REMOVED A ND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 2002041600004 20020416 00004 WP 2002 4 16 CALA0200200 1 20020413 A 5313 LONGERON DOUG DC9 DC982 3022082 WP STA 1287 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND LONGERON 29R CORRODED AT STA 1287. THE CORRODED AREA OF LONGERON WAS REMOVED AND A NEW SECTION AND SPLI CES WERE INSTALLED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 2002041600005 20020416 00005 WP 2002 4 16 CALA0200201 1 20020413 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FS 769-786 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND INTERCOSTAL CORRODED IN MID CARGO AREA BETWEEN FS 769 AND 786, L27L-L28L. THE INTERCOSTAL WAS REMOVED A ND A NEW PART WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4. 2 L 7 2 4F A6WE 2002041600006 20020416 00006 WP 2002 4 16 CALA0200203 1 20020413 A 5330 SKIN DOUG DC9 DC982 3022082 WP VENTRAL STAIR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND VENTRAL STAIRS EXTERNAL SKIN DENTED. THE SKIN WAS REPAIRED IAW SRM 52-01, FIGURE 1 AND 51-10-3. 2 L 7 2 4F A6WE 2002041600008 20020416 00008 WP 2002 4 16 ABXA010826 1 20020403 A 5310 9957739121 ANGLE DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 ANGLE CRACKED ON AFT SIDE OF FRAME AT STATION 1021, BETWEEN LONGERON 15 LEFT AND LONGERON 16 LEFT. REPLACED ANGLE IAW DC -9 SRM 53-03. 2 L 7 2 4F A6WE 2002041600009 20020416 00009 WP 2002 4 16 ABXA010821 1 20020401 A 5310 59134213 SKIN DOUG DC9 DC941 302207N WP EXT. FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 SKIN CRACKED AT RIGHT AFT NOSE GEAR DOOR AFT CUT-OUT. REPAIRED AREA IAW DC-9 SRM 53-05. 2 L 7 2 4F A6WE 2002041600010 20020416 00010 SO 2002 4 16 C2XA02RI003 1 20020415 A 3260 852701 PROXIMITY SENSOR EMB 145 EMB145 3260210 SO CRACKED A C2XA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 13964 145123 ORF Flt#3483-Crew reported Air/Ground circiut breaker A29 popped. Maintenance found the # 2 Wieght on Wheels proximity s ensor cracked.Maintenance removed and replaced the # 2 Weight on Wheels proximity sensor and performed a satisfactory sy stem operational test. The aircraft was approved for return to service. 2 L 7 2 4F RT T00011AT 2002041600011 20020416 00011 WP 2002 4 16 2002F00381 1 20020214 A 5320 SPLICE LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED G K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION LEVEL 2 CORROSION FOUND ON MOUNT PAD FOR NOSE LANDING GEAR RIGHT FORWARD GEAR DOOR FORWARD H INGE ATTACH BRACKET TO AIRFRAME, AFT SIDE FS 318 TO 355, RBL 22. MAINTENANCE REPAIRED LONGERON SPLICE IN ACCORDANCE WIT H ER/A L10-53R-4712. 2 L 7 3 4F A23WE 2002041600012 20020416 00012 WP 2002 4 16 2002F00382 1 20020215 A 5522 SKIN LKHEED 1011 10113851 5265010 WP ELEVATOR CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION LEVEL 2 CORROSION FOUND ON LEFT ELEVATOR LOWER SURFACE FROM ES 180 TO ES 451. MAINTENANCE R EMOVED AND REPLACED THE LEFT ELEVATOR IN ACCORDANCE WITH MM 27-31-03. 2 L 7 3 4F A23WE 2002041600013 20020416 00013 WP 2002 4 16 2002F00383 1 20020218 A 5320 FLOOR SUPPORT LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED G K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION LEVEL 2 CORROSION WAS FOUND AT CABIN FLOOR SUPPORT, LOWER GALLEY, LOWER T-CAP ABOVE LEFT ELE VATOR DOOR FS 901, WL 190, RBL 55 TO LBL 38. MAINTENANCE REPAIRED AREA IN ACCORDANCE WITH ER/A L10-53R-4724. 2 L 7 3 4F A23WE 2002041600014 20020416 00014 WP 2002 4 16 2002F00384 1 20020218 A 5710 TORQUE BOX LKHEED 1011 10113851 5265010 WP LT WING CRACKED G K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION A 2 INCH CRACK WAS FOUND AT THE LEFT MAIN LANDING GEAR TORQUE BOX AFT WEB WALL, LOWER INBOAR D CORNER. MAINTENANCE INSTALLED ANGLE AND WEB PER SRM 51-40-01, FS 1284, WSL 319, LBL 222. 2 L 7 3 4F A23WE 2002041600015 20020416 00015 WP 2002 4 16 2002F00385 1 20020218 A 5315 FLOORBEAM LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED G K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION FOUND LEVEL 2 CORROSION AT CABIN FLOOR SUPPORT, FLOORBEAM AT FS 865, LBL 34, RBL 39 AS VIEWE D FROM LOWER GALLEY. MAINTENANCE REPAIRED AREA PER ER/A L10-53R-4727. 2 L 7 3 4F A23WE 2002041600016 20020416 00016 NE 2002 4 16 2002F00386 2 20020411 A 7320 FFG052AC GOVERNOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535* NE RT ENGINE FAULTY G C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 11 555TZ 381 381 32589 31851 FLIGHT NUMBER 925, DURING TAKEOFF RIGHT ENGINE WOULD NOT REACH TAKEOFF THRUST, MAX EPR 1.70 AND N1 LOW WITH THRUST LEVER FULL FORWARD. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE FUEL FLOW GOVERNOR. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002041600017 20020416 00017 EU 2002 4 16 MALA020202 1 20020323 A 3510 89506050 CYLINDER SAAB SF340 SF340A 7850100 EU COCKPIT LEAKING A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 590XJ DURING CLIMBOUT OF FLIGHT 3064, O2 PRESSURE WENT BELOW 800 PSI ON CLIMBOUT. CONTINUED TO DECREASE TO 600 PSI WHEN TURNE D O2 VALVE OFF, THEN IT STEADIED AND STAY AT 600 PSI. AIR RETURN TO MSP. MAINTENANCE NOTED AUDIBLE O2 LEAK AT PRESSURE REGULATOR/MANIFOLD AREA. REPLACED OXYGEN CYLINDER AND MANIFOLD ASSEMBLY PER AMM 35-11-05-2. LEAK CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002041600018 20020416 00018 EU 2002 4 16 MALA020204 1 20020321 A 2611 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT ILLUMINATED A MALA F ACTIVATE FIRE EXT. B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 451XJ 340B451 WHILE ON THE RAMP THE CARGO SMOKE INDICATOR ILLUMINATED THEN WENT OUT. CREW WENT THROUGH THE MEMORY ITEMS AND BLEW BOTH EXTINGUISHERS UPON VERIFICATION OF SMOKE BY A RAMP AGENT. MAINTENANCE REMOVED AND REPLACED BOTH FIRE BOTTLES. ALSO RE PLACED FRONT SMOKE DETECTOR BECAUSE OF BROKEN SMOKE SCREEN COVER IAW 26-13-10. 2 L 7 2 4T RT A52EU 2002041600019 20020416 00019 EU 2002 4 16 MALA020205 1 20020322 A 3260 SWITCH SAAB SF340 SF340A 7850100 EU LANDING GEAR DIRTY A MALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 15 48XJ ON APPROACH OF FLIGHT 3072, CREW REPORTED THE CONFIG LIGHT ILLUMINATED ON APPROACH AT 1500 FT AGL/ WITH FLAPS 20 PERCENT THE CONFIG WARNING ILLUMINATED CREW HAD 3 GREEN LIGHTS ON GEAR FLAPS INDICATED 20 DEGREES. CREW DID A GO AROUND (ABORT ED APPROACH), TRIED AGAIN NO PROBLEMS. MAINTENANCE CLEANED AND LUBED WOW SWITCHES AND CANNON PLUGS, PERFORMED CONFIG FU NCTIONAL TEST IAW 31-350-00-5. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002041600020 20020416 00020 EU 2002 4 16 MALA020206 1 20020322 A 5350 SKIN SAAB SF340 340B 7860101 EU TAILCONE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 DENT IN LT TAIL CONE AREA STA 803, .042 DEEP. MAINTENANCE REPAIRED DENT IAW EO S53117. 2 L 7 2 4T RT A52EU 2002041600021 20020416 00021 EU 2002 4 16 MALA020208 1 20020325 A 3230 UPLOCK BAC 146 AVRO146RJ85A 1500097 EU LT MLG DIRTY A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 511XJ E2325 DURING FLIGHT 3586, LT MAIN GEAR WOULD NOT COME UP, AND INTRANSIT LIGHT REMAINED ON. AIR RETURN TO DTW. MAINTENANCE CL EANED AND REMOVED DEBRIS FROM LANDING GEAR BAY AREA AND UPLOCKS, PERFORMED RETRACTION AND EXTENSION TESTS PER AVRO AMM, ALL CHECKS GOOD AT THIS TIME. 2 H 7 4 4F RT A49EU 2002041600022 20020416 00022 EU 2002 4 16 MALA020210 1 20020324 A 3350 COVER SAAB SF340 340B 7860101 EU CABIN LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 BEFORE FLIGHT 3058 PAX DOOR EMERGENCY LIGHT COVER WAS LOOSE/BROKEN. EMERGENCY EXIT SIGN FALLS OFF AGAIN. MAINTENANCE S ECURED EXIT COVER AS NOTED. 2 L 7 2 4T RT A52EU 2002041600023 20020416 00023 EU 2002 4 16 MALA020211 1 20020326 A 3350 SIGN SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 445XJ 340B445 BEFORE FLIGHT 2548, EMERGENCY EXIT SIGN BY MAIN DOOR INOP. MAINTENANCE SECURED EXIT COVER AS NOTED. 2 L 7 2 4T RT A52EU 2002041600024 20020416 00024 EU 2002 4 16 MALA020213 1 20020326 A 3350 SIGN SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE L NO TEST NR NOT REPORTED 1 GL 15 421XJ 340B421 VERTICAL EXIT SIGN 6A DOES NOT ILLUMINATE. MAINTENANCE REPOSITION WIRE CONNECTOR AND RESECURED EXIT SIGN. COMPLETED SE VERAL OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002041600025 20020416 00025 EU 2002 4 16 MALA020216 1 20020327 A 2750 HP14161005 CONTROL VALVE SAAB SF340 340B 7860101 EU T/E FLAP FAILED A MALA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 15 438XJ 340B438 ON APPROACH OF FLIGHT 3250 INTO MQT, FLAPS WOULD NOT COME DOWN, VERY LITTLE BRAKING WAS USED DURING ROLLOUT. MAINTENANC E REMOVED AND REPLACED FLAP CONTROL VALVE AND REMOVED AND REPLACED FLAP CONTROLLER. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2002041600026 20020416 00026 NE 2002 4 16 MALA020217 2 20020329 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 76XJ 340A076 AFTER TAKEOFF ON FLIGHT 3338, RT ENGINE TORQUE AND ITT FLUCTUATING. AIR TURNBACK TO DTW. MAINTENANCE REMOVED AND REPLA CED RT ENG IAW MM 409 152513 FOR FURTHER DETAIL. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002041600027 20020416 00027 NE 2002 4 16 MALA020218 2 20020329 A 7261 SCREEN SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE DIRTY A MALA K NONE J WARNING INDICATION NR NOT REPORTED 1 GL 15 142XJ DURING FLIGHT 2944, RT ENGINE OIL PRESSURE FLUCTUATES. MAINTENANCE REMOVED AND CLEANED B-SUMP SCREEN AND LINE FOUND CAR BON BUILD. REINSTALLED SCREEN AND LINE, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002041600028 20020416 00028 EU 2002 4 16 MALA020219 1 20020329 A 3411 PITOT LINE SAAB SF340 340B 7860101 EU RIGHT CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 438XJ 340B438 DURING FLIGHT 3058, RT PITOT SYSTEM INDICATIONS ERRATIC. AIR RETURN TO DTW. MAINTENANCE REMOVED WATER FROM RT PITOT SY STEM, ALL CHECK GOOD IAW SAAB MM CHAP 34. 2 L 7 2 4T RT A52EU 2002041600029 20020416 00029 SO 2002 4 16 COMA0210014 1 20020413 A 5720 12024373002 BRACKET EMB 120 EMB120RT 3260202 SO FWD RIGHT WINGBO CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 22858 120264 DUIRNG A 2,000 FLIGHT CYCLE INSPECTION, THE FUEL SHUT-OFF SUPPORT BRACKET (P/N 120-24373-002) ON THE RIGHT WING BOX FORW ARD SIDE AFT OF FRAME 10 WAS FOUND TO BE CRACKED.THE CRACKED BRACKET (P/N 120-24373-002) WAS REMOVED FROM THE AIRCRAFT, REPAIRED AND RE-INSTALLED. WORK WAS ACCOMPLISHED IN ACCORDANCE WITH EMB 120 SRM 514-70-05 AND AERODESIGN REPORT #4249-1, REV IR DATED 4-13-02. 2 L 7 2 4T RT A31SO 2002041600030 20020416 00030 WP 2002 4 16 MWEA020252 1 20020414 A 5320 9955780671 ANGLE DOUG DC9 DC932 3022066 WP STATION 155 OUT OF TOLERANCE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 ANGLE IS NOT OF CORRECT THICKNESS. SHOULD BE .063 AND IS CURRENTLY MADE FROM .040. STATION 155, EPC PANEL. -- REMOVED ANGLE. DRILLED UP ANGLE AND INSTALLED. 2 L 7 2 4F A6WE 2002041600031 20020416 00031 WP 2002 4 16 MWEA020251 1 20020414 A 5320 9955780677 ANGLE DOUG DC9 DC932 3022066 WP STATION 155 OUT OF TOLERANCE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 ANGLE IS MADE FROM TOO THIN OF MATERIAL. ANGLE IS CURRENTLY .063 AND SHOULD BE MADE FROM .071 THICK STOCK MATERIAL. STAT ION 155, EPC PANEL LOCATION. -- REMOVED ANGLE. DRILLED UP ANGLE AND INSTALLED. 2 L 7 2 4F A6WE 2002041600032 20020416 00032 SO 2002 4 16 COMA0210015 1 20020412 A 5310 12034416001 BRACKET EMB 120 EMB120RT 3260202 SO FRAME9/STA 3010. CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 264CA 23448 120256 DURING AN E-10 PART A INSPECTION THE FUSELAGE SKIN SUPPORT BRACKET (P/N 120-34416-001) ON THE LEFT SIDE JUST BELOW THE P ILOTS WINDSHIELD SIDE POST AT FRAME 9 WAS FOUND TO BE CRACKED.THE CRACKED BRACKET (P/N 120-34416-001) WAS REMOVED FROM T HE AIRCRAFT AND A SERVICEABLE BRACKET WAS INSTALLED. WORK WAS ACCOMPLISHED IN ACCORDANCE WITH AERODESIGN REPORT #660-1, IR DATED 2-16-93. 2 L 7 2 4T RT A31SO 2002041600033 20020416 00033 2002 4 16 VNAA0204007 4 20020413 A 3100 LAMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 441JS 3059 AFTER SELECTING GEAR DOWN, THE CREW RECEIVED NO NOSE GEAR DOWN AND LOCK INDICATION. A LAMP TEST THEN INDICATED THAT THE RE WAS A BURNED OUT LIGHT. AS A PRECAUTION, THE CREW DECLARED AN EMERGENCY AND REQUESTED A FLY BY FROM ATC. THE TOWER CONFIRMED THAT THE GEAR WAS DOWN. FLIGHT 4117 THEN LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND REPLACE D THE LAMP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL TEST WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002041600034 20020416 00034 2002 4 16 VNAA0204008 4 20020413 A 2300 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 459PS 3070 WHILE ENROUTE, THE CREW CALLED MAINTENANCE CONTROL AND STATED THE FIRST OFFICER'S MICROPHONE'S PUSH TO TALK SWITCH WAS N OT WORKING. FLIGHT 4169 DIVERTED TO CAK WHO HAD THE PART IN STOCK. MAINTENANCE THEN INSPECTED AND REPLACED THE SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 23-00-00. OPERATIONAL CHECKS WERE PERFOMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002041600035 20020416 00035 EA 2002 4 16 COMA0260249 1 20020413 A 3230 46193 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 708CA 10482 7235 FLIGHT 5899 LANDING GEAR DISAGREE MESSAGE DURING APPROACH.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002041600036 20020416 00036 EU 2002 4 16 MALA020220 1 20020330 A 3020 NH24668165 DUCT SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 407XJ 340B407 DURING FLIGHT 2800, RT INTAKE LIGHT ILLUMINATED INFLIGHT, WITH ELECTRICAL SMELL IN FLIGHT DECK. FLT CREW DECLARED EMERG ENCY INTO MEM. AFTER DEPARTING MEMPHIS ABOUT 20 MINUTES OUT, THE F/O NOTICED A STRONG ELECTRICAL SMELL IN THE COCKPIT. DONNED 02, RETURNED TO MEM. MAINTENANCE REPLACED RIGHT ENGINE LOWER DUCT P/N NH 24668-165, SN/ON L169286S, SN/OFF L155 017 IAW AMM 71-60-04. RAN ENGINE, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002041600037 20020416 00037 NE 2002 4 16 MALA020221 2 20020330 A 7200 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 4 MALFUNCTIONED A MALA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 GL 15 504XJ E2311 AFTER TAKEOFF ON FLIGHT 3460, THE NR 4 ENGINE FLAME-OUT AND RETURNED TO FAR. AIR TURNBACK TO FAR. MAINTENANCE DETERMIN ED NR 4 ENGINE DIFFICULT TO ROTATE/SIEZED. REFERENCE FOLLOWING DISC/CA'S 14, 15, 16, 17, 18, 19 AND 20 FOR TROUBLESHOOT ING. AC TO BE FERRIED TO MSP, TASK CARD THREE ENGINE FERRY. INSPECTED AC AND FOUND SAFE FOR FERRY FROM FAR TO MSP WITH NR 4 ENGINE INOP. 2 H 7 4 4F 4 F RT A49EU E6NE 2002041600038 20020416 00038 NE 2002 4 16 MALA020222 2 20020330 A 7532 BLEED BAND BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 1 ENGINE MALFUNCTIONED A MALA O OTHER M OVER TEMP CL CLIMB 1 GL 15 507XJ E2316 NR 1 ENGINE EGT TEMP LIMITED TO 600 DEGREES, SLIGHTLY HIGHER THAN NORMAL AFTER TAKEOFF. LANDED IN MSP, NO INCIDENTS. M AINTENANCE DOWNLOADED FDR FOUND ENGINE TO HAVE OVERTEMPED. BORESCOPED NR 1 ENGINE REPLACED NR 1 BLEED BAND AND PERFORME D TAKEOFF POWER ASSURANCE. ALL CHECKS GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 2002041600039 20020416 00039 EU 2002 4 16 MALA020223 1 20020331 A 3020 SWITCH SAAB SF340 340B 7860101 EU COCKPIT DEFECTIVE A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 454XJ 340B454 DURING FLIGHT 3177, LT INTAKE HEAT CYCLING. AIR TURNBACK TO DTW. MAINTENANCE FOUND LT SWITCH ON PANEL BAD. REMOVED AN D REPLACED LT SWITCH. RAN A/C, OPS CHECK GOOD. ALL DONE IAW AMM 20-30. 2 L 7 2 4T RT A52EU 2002041600040 20020416 00040 EU 2002 4 16 MALA020224 1 20020330 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 413XJ 340B413 LT REAR FUSELAGE SKIN HAS A DENT AT STA 620, 2 INCHES LONG, 1.75 INCH WIDE, .040 INCH DEEP. COMPLIED WITH EA01-01159. NO DEFECTS NOTED. REQUIRES PERMANENT REPAIR WITHIN 800 FLT HOURS. MAINTENANCE REPAIRED IAW EO S53119. 2 L 7 2 4T RT A52EU 2002041600041 20020416 00041 EU 2002 4 16 MALA020226 1 20020318 A 5534 ANGLE BAC 146 AVRO146RJ85A 1500097 EU VERTICAL STAB CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 534XJ E2370 DURING C-CHECK IN CVG, CRACK ON RT SIDE OF LOWER VERTICAL STABILIZER, LOCATED AT STAB TO FUSELAGE CLOSING ANGLE. REPAIR ED IN ACCORDANCE WITH BAE FAX BARA/AVR/5825/02-DC, RIL HC550H9004 ISS 3 AND EO A55013. 2 H 7 4 4F RT A49EU 2002041600042 20020416 00042 EU 2002 4 16 MALA020227 1 20020322 A 5753 SKIN BAC 146 AVRO146RJ85A 1500097 EU T/E FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 534XJ E2370 DURING C-CHECK IN CVG, THE LT O/B FLAP TAB SUFFERED CHAFE DAMAGE TO THE UPPER SKIN BETWEEN RIBS 11 & 12. DAMAGE REPAIRE D IN ACCORDANCE WITH SRM 57-55-11 201 FIG 204 AND EO A57038. 2 H 7 4 4F RT A49EU 2002041600043 20020416 00043 EU 2002 4 16 MALA020228 1 20020328 A 2612 WEU SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FIRE WARNING MALFUNCTIONED A MALA K NONE N FALSE WARNING DE DESCENT 1 GL 15 112XJ ON DESCENT INTO MSP, RT ENGINE FIRE ILLUMINATED WITH FIRE BELL FOR 1-2 SECONDS. NO MASTER CAUTION OR T-HANDLE LIGHT. M AINTENANCE PERFORMED OPS CHECK OF FIRE DETECTION SYSTEM IAW AMM 25-1-00-2 PARA 2A, OPS CHECK GOOD. PERFORMED VIS INSPEC TION OF RT NACELLE FIRE LOOP, NO DISCREPANCIES NOTED. REPLACED WEU IAW 31-50-05-4, ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2002041600044 20020416 00044 EU 2002 4 16 MALA020229 1 20020402 A 2421 31342003 GENERATOR SAAB SF340 340B 7860101 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 414XJ 340B414 DURING FLIGHT 3006, AC DEPARTED DTW, RT AC GENERATOR FAILED. DUE TO CURRENT CONDITIONS AND DTW AIR TO GROUND RADAR DOWN . PILOT RETURNED TO DTW. MAINTENANCE REMOVED AND REPLACED RIGHT HAND GCU AND GEN AC, GCU P/N 51634-002, S/N 92027 IAW SF340 AMM. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2002041600045 20020416 00045 EU 2002 4 16 MALA020230 1 20020402 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE L NO TEST NR NOT REPORTED 1 GL 15 421XJ 340B421 F/A'S EMERGENCY LIGHT ARM LIGHT BURNT OUT. MAINTENANCE RELAMPED, ALL CHECKS GOOD IAW SMM CHAPTER 33. 2 L 7 2 4T RT A52EU 2002041600046 20020416 00046 EU 2002 4 16 MALA020232 1 20020404 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN OUT OF POSITION A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 412XJ 340B412 EMERGENCY FLOOR TRACK LIGHTING AT ROWS 2 AND 3 STICKS OUT ON LEFT SIDE. MAINTENANCE RESECURED EMERGENCY FLOOR TRACK LIG HTING AT ROWS 2 AND 3. ALL SECURITY CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2002041600047 20020416 00047 EU 2002 4 16 MALA020233 1 20020405 A 3350 SOCKET SAAB SF340 340B 7860101 EU PSU BROKEN A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 424XJ 340B424 EMERGENCY LIGHT SOCKET AT SEAT 10A IS BROKEN. MAINTENANCE REMOVED PSU PANEL AND INSTALLED SERVICEABLE PSU PANEL P/N 2LA 007466-07 IAW SAAB AMM 20-10-00. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002041600048 20020416 00048 EU 2002 4 16 MALA020234 1 20020206 A 5330 SKIN SAAB SF340 SF340A 7850100 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369XJ FOUND DENT IN RT FUSELAGE FWD ICE SHIELD BELOW SL161.8 FWD OF STA 319. MAINTENANCE REPAIRED DENT ON RT FUSELAGE IAW MAL EO S53005. REPLACED ICE SHIELD IAW SRM 53-70-10. 2 L 7 2 4T RT A52EU 2002041600049 20020416 00049 NE 2002 4 16 MALA020235 2 20020406 A 7200 GECT75B ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT MALFUNCTIONED A MALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 GL 15 430XJ 340B430 DURING FLIGHT 3247 FROM MQT, LT ENGINE SHUTDOWN AFTER TAKEOFF. AIR RETURN TO MQT. MAINTENANCE WENT UP TO REMOVE AND SE ND DFDR FOR DOWNLOAD. REMOVED AND REPLACED LT ENGINE. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2002041600050 20020416 00050 EU 2002 4 16 MALA020236 1 20020407 A 7603 5308212 CONTROLLER SAAB SF340 SF340A 7850100 EU ENGINE CONTROL STICKING A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 48XJ AFTER TAKEOFF ON FLIGHT 2801, F1 STOP OPEN LIGHT. QUADRANT F1 STOP MECHANISM STICKING. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED CONTROL QUADRANT. 2 L 7 2 4T RT A52EU 2002041600051 20020416 00051 EU 2002 4 16 MALA020237 1 20020407 A 6123 638005001 PUMP SAAB SF340 SF340A 7850100 EU LT PROP FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 367XJ ON FLIGHT 2837 LEFT ENGINE OIL PRESSURE LIGHT ILLUMINATED INFLIGHT. LEFT PROP OIL PRESSURE WAS LOW. COMPLIED WITH QRH ALL OTHER ENGINE T-PROP PARAMETERS OK. FLIGHT DIVERTED TO EAU. FLIGHT LANDED WITHOUT PROBLEMS. MAINTENANCE REPLACED F EATHERING PUMP IAW SAAB AMM 61-20-01. OPS CHECKED OK. 2 L 7 2 4T RT A52EU 2002041600052 20020416 00052 NM 2002 4 16 QXEA0200634 1 20020412 A 5270 HANDLE BOMBDR DHC8 DHC8401 NM DIRTY A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 412QX 4059 SEA - AIRCRAFT RETURNED TO FIELD WHEN DURING CLIMB THE FUSELAGE DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE INSPECTED TH E AIRCRAFT AND FOUND THE FORWARD BAGGAGE DOOR HANDLE NOT PROPERLY STOWED. THE DOOR HANDLE WAS CLEANED, LUBED, AND PROPER LY STOWED. THE DOOR WAS OPERATED WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042500091 20020425 00091 NM 2002 4 25 QXEA0200635 1 20020415 A 5230 HANDLE BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR UNSECURE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 401QX 4031 AIRCRAFT RETURNED TO FIELD WHEN ON CLIMBOUT THE FUSELAGE DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE INSPECTED THE AIRC RAFT AND FOUND THE FORWARD BAGGAGE DOOR HANDLE NOT SECURED. HANDLE WAS SECURED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002041600053 20020416 00053 EU 2002 4 16 MALA020238 1 20020407 A 3020 CONNECTOR SAAB SF340 SF340A 7850100 EU LT INTAKE HEAT CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 115XJ DURING FLIGHT 2816 LT INTAKE HEAT FAILED IN ICING CONDITIONS. AIR RETURN TO MSP. MAINTENANCE OHMED CHECK OF THERMISTOR S GOOD. CLEANED MOISTURE FROM CANNON PLUGS ON SHOEBOX SIDE AND AT THE BULKHEAD FWD OF SHOEBOX. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002041600054 20020416 00054 EU 2002 4 16 MALA020239 1 20020407 A 3020 44730501 MODULE SAAB SF340 SF340A 7850100 EU DEICE SYSTEM FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 115XJ DURING FLIGHT 3271 LEFT ENGINE INTAKE CAUTION LIGHT CYCLING ON AND OFF AT 30 SECOND INTERVALS. AIR RETURN TO MSP. MAIN TENANCE REMOVED AND REPLACED LEFT DEICE MODULE PER AMM 30-20-00, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002041600055 20020416 00055 EU 2002 4 16 MALA020240 1 20020407 A 3397 WIRE SAAB SF340 340B 7860101 EU CABIN BROKEN A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 411XJ 340B411 DURING WALKAROUND OF AC 411 IN CWA, NOTED EMERGENCY LIGHT 44LN NOT WORKING. FOUND BROKEN WIRES WHERE WIRES ATTACH TO TH E STRIP. MAINTENANCE REMOVED AND REPLACED FLOOR PATH EMERGENCY LIGHT 44LN, P/N 6690-2 IAW SF340 AMM 33-50-20-4. 2 L 7 2 4T RT A52EU 2002041600056 20020416 00056 NE 2002 4 16 MALA020241 2 20020409 A 7261 SEAL SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE DEFECTIVE A MALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 15 428XJ 340B428 DURING FLIGHT 2775 LT ENGINE OIL PRESSURE FLUCTUATION ALONG WITH CWP LIGHT CAME ON INFLIGHT. LT PROP OR PSI AND TEMP WE RE OK. NO SIGNS OF OIL LEAKS NOTED FROM CABIN WINDOW. ENGINE SHUTDOWN IN FLIGHT. QRH COMPLETE. MAINTENANCE PERFORMED ALL PROPER MAINT PROCEDURES. REPLACEMENT OF LEFT GENERATOR BB AXIS SEAL AND COMPLETED EO 71073 FROM GE, ALL PROCEDURES COMPLIED WITH. LEAK AND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2002041600057 20020416 00057 WP 2002 4 16 CALA0200204 1 20020415 A 3350 WIRE DOUG DC9 DC982 3022082 WP EMER LT CONN DISCONNECTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE AT SEAT 14R AND 15R. TROUBLESHOOTING FOUND CONNECTOR AT 15R HAD A PUSHED P IN. THE PIN WAS RESEATED IAW MM 20-50-01. SEAT 14R HAD GROUND WIRE PULLED FROM CONNECTOR SPLICE. THE GROUND WIRE AT CONN ECTOR WAS RESEATED IAW MM 20-50-01. OPERATIONAL CHECKS WERE GOOD IAW MM 33-53-00. 2 L 7 2 4F A6WE 2002041600058 20020416 00058 NM 2002 4 16 CALA0200206 1 20020415 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 1006-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-02 . 2 L 7 2 4F RT A16WE 2002041600059 20020416 00059 EU 2002 4 16 MALA020242 1 20020409 A 3230 7232000631 SWITCH SAAB SF340 340B 7860101 EU LANDING GEAR DEFECTIVE A MALA K NONE P NO WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 365XJ IN ATW FOUND GEAR DOORS HANGING OPEN. EXPLOSIVE BOLTS BLOWN. LT AND RT MAIN GEAR DOORS FOUND TO BE DOWN ON POST FLIGHT . MAINTENANCE REMOVED AND REPLACED SWITCH 5GB P/N 7232000-631 AND MAIN, EMERGENCY I/B AND O/B BRAKE ACCUMILATORS COMPLE TED REQUIRED OPS AND FUNCTION CHECKS. OPS AND LEAK CHECKS GOOD IAW SAAB AMM. 2 L 7 2 4T RT A52EU 2002041600060 20020416 00060 NE 2002 4 16 NACA20020011 2 20020324 A 8530 356993 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 4 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 2907F 1871 1871 533265 CP450668 NR 4 ENGINE FEATHERED AT 0507Z, (BACKFIRING AND RUNNING ROUGH). REPLACED NR 16 CYLINDER. 2 L 7 4 4R 4 R A781 5E8 2002041600061 20020416 00061 NE 2002 4 16 NACA20020012 2 20020326 A 8530 356994 CYLINDER DOUG DC6 C118A 3021710 WP PWA R2800 R2800* 52026 NE NR 3 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 AL 03 1377K 385 385 44596 P33192 FEATHERED THE NR 3 ENGINE DUE TO RUNNING ROUGH. REPLACED THE NR 7 CYLINDER. 2 L 7 4 4R 4 R 6A3 5E8 2002041600062 20020416 00062 NE 2002 4 16 NACA20020013 2 20020402 A 7421 URHB32E SPARK PLUG DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 3 ENGINE DAMAGED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 779TA 336 45529 36210 NR 3 ENGINE NR 4 CYLINDER DOUBLE SHORTED SECONDARY, BACKFIRING. REPLACED BOTH RIGHT AND LEFT SPARK PLUGS. 2 L 7 4 4R 4 R A781 5E8 2002041600063 20020416 00063 WP 2002 4 16 NACA20020014 1 20020321 A 5210 DOOR FRAME DOUG DC6 DC6 3021702 WP PAX DOOR CRACKED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 43872 533294 PASSENGER DOOR, FORWARD FRAME, CRACKED 16 INCHES ABOVE LOWER CORNER OF THE DOOR. REMOVED DAMAGED AREA, FABBED AND INSTA LLED A FILLER. FABBED AND INSTALLED A SHIM AND A DOUBLER. 2 L 7 4 4R A781 2002041600064 20020416 00064 WP 2002 4 16 NAFA20020002 1 20020313 A 5720 CAP DOUG DC6 DC6A 3021706 WP RT WING CRACKED I N32B K NONE O OTHER IN INSP/MAINT 1 AL 01 7780B 45372 RIGHT WING NR 23 STRINGER CAP CRACKED AT STA 325. FABRICATED AND INSTALLED 2 DOUBLERS PER DRAWING NAC2002-02. 2 L 7 4 4R 6A3 2002041600065 20020416 00065 WP 2002 4 16 NAFA20020003 1 20020313 A 5330 SKIN DOUG DC6 DC6A 3021706 WP FUSELAGE CRACKED I N32B K NONE O OTHER IN INSP/MAINT 1 AL 01 7780B 45372 TOP OF FUSELAGE STA 640, LAP SEAM CORRODED AND SKIN CRACKED BETWEEN L-4 AND L5. REMOVED CORRODED AND DAMAGED AREA. FAB RICATED AND INSTALLED FILLER AND DOUBLER PER NAC DRAWING NAC011 REV 32. 2 L 7 4 4R 6A3 2002041600066 20020416 00066 NM 2002 4 16 P2EA2002V0010 1 20020217 A 5315 FLOORBEAM BOEING 737 73725A 1384481 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1+Q2 INSPECTION, LONGITUDINAL FLOORBEAM AT BL 0, BS 663 UPPER CHORD CRACKED. LONGITUDINAL FLOORBEAM REPAIRED IA W EO B737MC57-010/02, S/B 737-57-1210. 2 L 7 2 4F RT A16WE 2002041600067 20020416 00067 NM 2002 4 16 P2EA2002V0013 1 20020219 A 5311 FRAME BOEING 737 73725A 1384481 NM FUSELAGE BENT A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1+ Q2 INSPECTION, FWD CARGO COMPARTMENT BS 420 STR 24L FRAME BENT. FRAME REPAIRED IAW SRM 51-40-3 FIG 1. 2 L 7 2 4F RT A16WE 2002041600068 20020416 00068 NM 2002 4 16 P2EA2002V0025 1 20020220 A 5751 AILERON BOEING 737 73725A 1384481 NM RT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 RIGHT WING AILERON DELAMINATED BETWEEN WBL 417 AND WBL 446. REPAIRED IAW EO B737HC57-007/02 APPROVED 8110-3 FORM BY FAA . 2 L 7 2 4F RT A16WE 2002041600069 20020416 00069 NM 2002 4 16 P2EA2002V0027 1 20020220 A 5751 SPAR BOEING 737 73725A 1384481 NM AILERON DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1 AND Q2 INSPECTION, LT WING AILERON FRONT SPAR LOWER CHORD WITH DELAMINATION SPOTS BETWEEN WBL 417.250 AND WBL 251.8. REPAIRED IAW EO B737HC57-008/02 APPROVED BY 8110-3 FORM BY FAA. 2 L 7 2 4F RT A16WE 2002041600070 20020416 00070 NM 2002 4 16 P2EA2002V0028 1 20020220 A 5313 STRINGER BOEING 737 73725A 1384481 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1 AND Q2 INSPECTION, BETWEEN BS 967 AND BS 986.5 STR 23L WITH CORROSION. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1. 2 L 7 2 4F RT A16WE 2002041600071 20020416 00071 NM 2002 4 16 P2EA2002V0029 1 20020220 A 5514 BEAM BOEING 737 73725A 1384481 NM HORIZ STAB CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1 AND Q2 INSPECTION, RT HORIZONTAL STABILIZER LWR AREA T/E BEAM WITH CORROSION BETWEEN ELEV STA 94.07 AND ELEV S TA 100. RT HORIZONTAL STABILIZER LWR AREA T/E BEAM REPAIRED IAW SRM 55-107 FIG 1. 2 L 7 2 4F RT A16WE 2002041600072 20020416 00072 NM 2002 4 16 P2EA2002V0032 1 20020406 A 7910 LINK BOEING 737 73725A 1384481 NM PWA JT8 JT8D17 52049 NE OIL SYSTEM LOOSE A P2EA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CE 05 239TA 23789 DURING EVALUATION FLIGHT AFTER Q1 AND Q2 INSPECTION, NR 1 ENGINE OIL QUANTITY STARTED DECREASING AFTER TAKEOFF, ENGINE N R 1 SHUTDOWN UPON TOUCHDOWN WITH 0.750 GALS. PRESSURE LINK TIGHTENED AT OIL FILTER BYPASS SW IAW MM 20-50-11 PAGE 211, ENGINE OIL SERVICED IAW MM 12-13-11, LEAK CHECK IAW 71-09-11. 2 L 7 2 4F 4 F RT A16WE E2EA 2002041600073 20020416 00073 NM 2002 4 16 P2EA2002V018 1 20020219 A 5320 ANGLE BOEING 737 73725A 1384481 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 DURING Q1+Q2 INSPECTION, MAIN PASSENGER CABIN FLOOR AREA AT STA 520 FLOOR ANGLE CRACKED. FLOOR ANGLE REPAIRED IAW SRM 5 1-40-4 FIG 1 DETAIL 5. 2 L 7 2 4F RT A16WE 2002041600074 20020416 00074 NE 2002 4 16 P5CA0200671 2 20020410 A 7250 SEAL BOEING 747 7472U3B 1384846 NM PWA JT9 JT9D7Q 52054 NE NR 4 ENGINE BURNED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 923FT 22769 702445 NR 4 ENGINE 1ST STAGE TURBINE OUTER AIR SEAL HAS 2 INCH BURN THROUGH. ENGINE TO BE REMOVED FROM SERVICE IN 60 HRS PER M M 72-00-00, PAGE 680N, TABLE 6. 2 L 7 4 4F 4 F RT A20WE E3NE 2002041600076 20020416 00076 NM 2002 4 16 PCAA0204040 1 20020401 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN CRUSHED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 844EX 339 DURING ROUTINE MAINTENANCE VISIT FOUND EMERGENCY LIGHTS ON FLOOR THIRD AND FORTH LIGHTS BACK WERE INOPERATIVE. LAMP ASS EMBLIES WERE REPLACED DUE TO WIRES BEING CRUSHED. ALL OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002041600077 20020416 00077 NM 2002 4 16 PCAA0204041 1 20020331 A 3350 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN FAULTY A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 817EX 191 DURING ROUTINE MAINTENANCE VISIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. EMERGENCY LIGHT CONTROL BOX REPLACED IN ACCOR DANCE WITH DEHAVILLAND DASH 8 MM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002041700144 20020417 00144 EA 2002 4 17 COMA0260248 1 20020412 A 2750 860D10018AB FCU CNDAIR CL600 CL6002B19 1900309 EA E/E BAY MALFUNCTIONED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 926CA 6485 7027 FLIGHT 5903 FLAPS FAIL MESSAGE WHILE A/C AT GATE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2002041600078 20020416 00078 NM 2002 4 16 PCAA0204043 1 20020408 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 840EX 327 DURING ROUTINE MAINTENANCE VISIT FIRST TWO EMERGENCY LIGHTS WERE FOUND INOPERATIVE. EMERGENCY LIGHT BATTERY AT POSITION 500 WAS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002041600079 20020416 00079 NM 2002 4 16 PCAA0204045 1 20020410 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT LEFT SIDE OF CABIN EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. FORWARD AND AFT PLUG CONN ECTORS ON LEFT SIDE OF CABIN EMERGENCY LIGHT STRIPS WERE RESECURED. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH DEHAVILLA ND DASH 8 MAINTENANCE MANUAL 33-51-30. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002041600080 20020416 00080 NM 2002 4 16 QXEA01200497 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - PITTING IN RT INBOARD SEAT TRACK FROM STATION 184.0 TO 187.0. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAPH F, STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002081500032 20020815 00032 2002 8 15 249TR0002 4 20020807 A 2230 COMPUTER BOEING 737 7372K5 138448X NM AUTOTHRUST SYS FAULTY A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 A/T FAILS BITE TEST AND GOES COMPLETELY INOP AT TIMES. REMOVED AND REPLACED A/T COMPUTER, OPS NORMAL PER BITE TEST MM 2 2-31-01. 2 L 7 2 4F RT A16WE 2002041600081 20020416 00081 2002 4 16 249TR0003 4 20020408 A 2230 AUTOTHRUST SYS BOEING 737 7372K5 138448X NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 249TR 22598 Autothrottles inop. 2 L 7 2 4F RT A16WE 2002041600082 20020416 00082 EA 2002 4 16 COMA0260247 1 20020415 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RIGHT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 709CA 7238 WHILE AIRCRAFT WAS AT HANGAR FOR OVERNIGHT, MAINTENANCE NOTICED EVIDENCE OF A LIGHTNING STRIKE ON RIGHT WING LOWER SKIN TOWARD TIP AT W.S.401.COMPLIED WITH LIGHTNING STRIKE INSPECTION PER CHECKLIST AND PERFORMED TEMPORARY REPAIR PER BOMBAR DIER REO 601R-57-31-364. OK FOR RETURN TO SERVICE. 2 L 7 2 4F RT A21EA 2002041600083 20020416 00083 2002 4 16 250TR0001 4 20020409 A 2220 959960714945 RECEIVER BOEING 737 7372K5 138448X NM A PIDA K NONE O OTHER CL CLIMB 1 SO 05 250TR 22597 MCP panel @ 7000`, engage PDC A/S bug goes to 310K. Speed mode would not engage. When flaps select to 5 auto pilots kick off, would not re-engage. R&R both radio altimeters. 2 L 7 2 4F RT A16WE 2002042200107 20020422 00107 2002 4 22 250TR0002 4 20020412 A 2230 SWITCH BOEING 737 7372K5 138448X NM AUTOTHRUST SYS OUT OF ADJUST A PIDA K NONE O OTHER CR CRUISE 1 SO 05 250TR 22597 AUTO THROTTLES WILL SET TAKEOFF AND CLIMB POWER BUT WILL NOT RETARD THROTTLES TO MAINTAIN SPEED. DURING CRUISE PDC SPEE D IS THE ONLY MODE THAT WORKS. MCP SPEED MODE WILL NOT WORK IN ANY REGIME. ADJUSTED AUTO THROTTLE SWITCH. OP'S CHECKS OK. 2 L 7 2 4F RT A16WE 2002041700145 20020417 00145 EA 2002 4 17 COMA0260250 1 20020415 A 5320 6003603031 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 739CA 7917 7273 LT FS 718.00 DOUBLER IS CRACKED. REMOVED CRACKED DOUBLER LT FS 718.00 AND INSTALLED NEW DOUBLER IAW CANADAIR REO 601R-5 3-61-193. 2 L 7 2 4F RT A21EA 2002041600084 20020416 00084 EA 2002 4 16 COMA0260251 1 20020415 A 5300 600360302432 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FS718.00 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 739CA 7917 7273 R/H F.S. 718.00 FRAME AND DOUBLER ARE CRACKED.REMOVED CRACKED FRAME AND DOUBLER R/H F.S. 718.00 AND INSTALLED NEW FRAME AND DOUBLER I/A/W CANADAIR REO 601R-53-61-193. 2 L 7 2 4F RT A21EA 2002041600085 20020416 00085 CE 2002 4 16 JJB2002F00000 1 20020322 A 3020 1189100569 LINK BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA SHOCK LINK ASSY DISCHARGED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 835CA 2834 VE400 DURING ROUTINE INSPECTION, FOUND LEFT ENGINE ANTI-ICE VANE DOOR SHOCK LINKS MISSING PARTS AND DOOR DISCONNECTED. NOTE: DOWEL PINS FELL OUTOF SPRING RETAINER. 2 L 7 2 4T 3 T RT A24CE E2NE 2002041600086 20020416 00086 NM 2002 4 16 C8GA20020006 1 20020416 A 2710 414001410 ROD END BOEING 727 7272A1 138407F NM GEAR WELL BROKEN A C8GA D RETURN TO BLOCK F FLT CONT AFFECTED CL CLIMB 1 SO 15 89427 55095 21365 Flight DAE001 from MIA to PTY. After takeoff during climb, crew could not keep aircraft level. Applied 5 units of trim and left rudder required to maintain level flight. Aircraft returned to MIA and landed without further incident. Upon landing found 2 right hand spoilers remained extended caused by broken spoiler cable rod end at the rigging beam. Repla ced rod end, ops check good. Aircraft returned to service. 2 L 7 3 4F A3WE 2002041600087 20020416 00087 NM 2002 4 16 AWXA200200343 1 20020415 A 3350 BMS13311122 WIRE BOEING 737 737301 1384611 NM SEAT ROW 17 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 0 0 23260 PHX - EEL - FLIGHT CREW REPORTED EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 17 L/H. MAINTENANCE REPAIRED BROKEN WIRE AT SEAT ROW 17 L/H, FUNCTIONAL CHECK GOOD IAW T/C A1C33006. 2 L 7 2 4F RT A16WE 2002041600088 20020416 00088 NM 2002 4 16 AWXA200200344 1 20020413 A 3350 E0261CF20 CABLE AIRBUS A319 A319132 3930340 NM SEAT ROW 12 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 0 0 1049 PHX - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY ESCAPE PATH SEAT LIGHT AT SEAT ROW 12 L/H, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 2002041700001 20020417 00001 NM 2002 4 17 SWAA020777 1 20020412 A 3350 207377 LENS BOEING 737 7372T4 1384492 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 EEPLS LENS MISSING AT MID CABIN. INSTALLED LENS PER MM. 2 L 7 2 4F A16WE 2002041700002 20020417 00002 NM 2002 4 17 SWAA020780 1 20020411 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 715SW 27849 DURING SCHEDULED C2 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002041700003 20020417 00003 NM 2002 4 17 SWAA020782 1 20020413 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, 2 INCHES BELOW STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002041700004 20020417 00004 NM 2002 4 17 SWAA020784 1 20020412 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 0 22942 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 727D + 4, BELOW STR 19R AND BS 910, STR 22R. R EPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002041700005 20020417 00005 NM 2002 4 17 SWAA020786 1 20020414 A 5312 6516300 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED (3 EA) AT BS 178, RBL 7.0, WL 201, WL 213 AND WL 211. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002041700006 20020417 00006 NM 2002 4 17 SWAA020787 1 20020412 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 0 26571 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (5 EA) BETWEEN STR 7L AND 8L, BS'S 380, 400, 827, 867 AND 907.. REPAIRED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2002041700007 20020417 00007 NM 2002 4 17 SWAA020788 1 20020412 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (8 EA) BETWEEN STR 7R AND 8R, BS'S 500, 480, 440, 400, 787, 827, 867 AND 907. REPAIRED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2002041700008 20020417 00008 NM 2002 4 17 2002F00378 1 20020226 A 3600 10746016 PILOT VALVE BOEING 757 75723N 1384973 NM LT ENGINE PYLON INOPERATIVE A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 528AT 30887 DURNG TAXI, LEFT DUCT PRESSURE FLUCTUATES. AIRCRAFT RETURNED TO GATES. MAINTENANCE REPLACED THE HIGH STAGE PILOT. (M) 2 L 7 2 4F RT A2NM 2002041700009 20020417 00009 NM 2002 4 17 2002F00380 1 20020219 A 3600 32143042 SHUTOFF VALVE BOEING 757 75723N 1384973 NM LT ENG PYLON INOPERATIVE A AMTA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 GL 11 519AT 16094 27975 DURING CRUISE EICAS MESSAGE LEFT ENGINE HIGH STAGE DISPLAYED, L HIGH STAGE LGT ILLUMINATED, DUCT PRESSURE NORMAL. AIRCR AFT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED HPSOV PER MM 36-11-07. (M) 2 L 7 2 4F RT A2NM 2002041700010 20020417 00010 NE 2002 4 17 2002F00391 2 20020219 A 7230 COMPRESSOR WHEEL BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE OUT OF BALANCE A AMTA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 11 517AT 27973 DURING CLIMB ENGINE VIB HIGH READ 2.6, ENGINE INDICATIONS NORMAL. VIB RETURNED BELOW 2.5 WITH THRUST LEVER RETARDED. A IRCRAFT RETURNED TO THE AIRPORT AND MAINTENANCE PERFORMED RIGHT ENGINE FAN BALANCE, REF MM 71-00-00 ADJ/TEST, TEST NR 7. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2002041700011 20020417 00011 NM 2002 4 17 2002F00392 1 20020219 A 2730 162005102 COMPUTER BOEING 757 75723N 1384973 NM ELEVATOR FEEL MALFUNCTIONED A AMTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 517AT 19861 27973 DURING CRUISE STATUS MESSAGE 'ELEV FEEL'. AIRCRAFT MADE UNSCHEDULED LANDING AND LANDED WITHOUT INCIDENT. MAINTENANCE R EMOVED AND REPLACED THE ELEVATOR FEEL COMPUTER. (M) 2 L 7 2 4F RT A2NM 2002041700012 20020417 00012 NM 2002 4 17 2002F00393 1 20020212 A 7830 LJ70533 CLUTCH BOEING 757 75723N 1384973 NM LT ENGINE T/R MALFUNCTIONED A AMTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 11 514AT 27971 DURING CRUISE, LEFT AND RIGHT THRUST LEVERS DIFFICULT TO MOVE. MAINTENANCE REMOVED AND REPLACED THE AUTOTHROTTLE CLUTCH PACK. REMOVED AND REPLACED LEFT ENGINE OUTBOARD FEEDBACK ACTUATOR IAW MM 78-34-06. (M) 2 L 7 2 4F RT A2NM 2002041700013 20020417 00013 WP 2002 4 17 2002F00394 1 20020217 A 5210 SWITCH LKHEED 1011 1011385115 5265015 WP PAX DOOR FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 198AT 193B1111 DURING SCHEDULED MAINTENANCE, THE 2L DOOR WOULD NOT OPERATE ELECTRICALLY. DOOR OPERATED MECHANICALLY AND IN EMERGENCY. MAINTENANCE REMOVED AND REPLACED THE 2L DOOR SWITCH IAW L1011 MM 52-12-19. (M) 2 L 7 3 4F A23WE 2002041700014 20020417 00014 WP 2002 4 17 2002F00395 1 20020214 A 5320 FLOOR SUPPORT LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION THE CABIN FLOOR SUPPORT FS 1521, RBL 48.5-74.5 WAS FOUND TO HAVE LEVEL 2 CORROSION. MAINTEN ANCE REPAIRED THE FLOOR SUPPORT AT FS 1521, RBL 48.5-74.5 IAW THE L1011 STRUCTURAL REPAIR MANUAL, 53-21-00, FIG 815. (M ) 2 L 7 3 4F A23WE 2002041700015 20020417 00015 NE 2002 4 17 2002F00396 2 20020219 A 7321 3TL3212A SWITCH BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT INOPERATIVE A AMTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 11 522AT 12196 29330 UPON SHUTDOWN OF NR 2 ENGINE, EXCESSIVE SMOKE COMING OUT OF INLET AND EXHAUST AREAS. MAINTENANCE FOUND FUEL CONTROL SWI TCH FAILED INTERNALLY. SWITCH WAS KEEPING POWER ON THE 'VALVE OPEN' CONTACTS AT ALL TIMES CAUSING ENGINE VALVE TO CYCLE OPEN AND CLOSE. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2002041700016 20020417 00016 NM 2002 4 17 2002F00397 1 20020308 A 2931 65178494061 LINE BOEING 727 727224 1384076 NM HYD INDICATOR FAILED A FX7A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 296SC 22449 DURING CLIMB-OUT, HYDRAULIC SYSTEM "B" LOSS THE PRESSURE INDICATION, INDICATION SHOWED 0. HYDRAULIC QUANTITY SHOWED 1.8 US GALLONS, AND BOTH 'B' SYSTEM LOW PRESSURE LIGHTS ILLUMINATED, PERFORMED EMERGENCY/ABNORMAL CHECKLIST A/C DIVERTED FR OM SWA TO SVMI. THE AIRCRAFT LANDED WITHOUT ACCIDENT. FOUND HYDRAULIC LEAK IN HYDRAULIC SERVICING PORT. REMOVED AND R EPLACED DAMAGED LINE IAW MM 20-10-05. SERVICED HYDRAULIC SERVICING PORT, REMOVED AND REPLACED DAMAGED LINE IAW MM 20-10 -05. SERVICED HYDRAULIC QTY IAW M 12-12. OPS CHECKED GOOD. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002041700017 20020417 00017 GL 2002 4 17 2002F00398 1 20020319 A 5754 65B392081 HINGE BOEING 747 747300 GL KRUGER FLAP WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 24837 41942 24837 DURING CURRENT D-CHECK AT SIAEC, FOUND L/W NR 11, 12 AND 13 L/E KRUGER FLAP HINGE FITTING ASSEMBLIES WITHWORN AND ELONGA TED BORE HOLES. REAMED HOLES. PERFORMED DYE CHECK TO ENSURE CORROSION AND CRACK FREE CONDITION. NO DEFECTS FOUND. FAB RICATED AND INSTALLED SPLIT-BUSHINGS. REINSTALLED L/E DEVICES WITH NEW BEARINGS AND HARDWARE. OPERATIONAL CHECKS NORMA L. (M) 2 L 7 4 4F RT A20WE 2002041700018 20020417 00018 NM 2002 4 17 2002F00400 1 20020327 A 5610 58935558 WINDOW BOEING 727 727251 138408H NM COCKPIT CRACKED A FX7A A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 266US 19985 R2 WINDOW OUTER PANEL CRACKED A/C DIVERTED TO KMIA FROM KMCO EN ROUTE TO CCS. REMOVED AND REPLACED R2 WINDOW PER MM 56- 12-11 A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002041700019 20020417 00019 NM 2002 4 17 2002F00401 1 20020308 A 2910 65174894061 LINE BOEING 727 727224 1384076 NM HYD SYSTEM DAMAGED A FX7A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 296SC 22449 DURING CLIMB-OUT OF SWA, HYDRAULIC SYSTEM B PRESSURE LOSS IND SHOWED 0 QTY ABNORMAL CHECKLIST FOLLOWED A/C DIVERTED TO S VMI, LANDED WITH NO INCIDENT. FOUND HYD LINE IN SERVICE PORT DAMAGED. REMOVED AND REPLACED LINE PER MM 20-10-05 SERVIC ED HYD QTY LEAK AND OPS CHECKED GOOD A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002041700020 20020417 00020 NM 2002 4 17 2002F00402 1 20020323 A 2781 80173 SWITCH BOEING 727 727224 1384076 NM SLAT INDICTOR WORN A FX7A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 19 79750 22452 ON TAXI-OUT WITH FLAPS 15 F/E AUX PANEL SHOWED NR 4 LE DEVICE NOT DOWN AND LOCKED A/C RETURNED TO GATE. REMOVED AND REP LACED NR 4 L/E DEVICE SWITCH PER MM 27-82-31. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002041700021 20020417 00021 2002 4 17 2002F00403 4 20020322 A 3421 1068951 INVERTER BOEING 727 727251 138408H NM ATTITUDE IND MALFUNCTIONED A FX7A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 266US 19985 ON PUSHBACK, POWER FLAG ON STANDBY ATTITUDE INDICTOR RERACKED STATIC INVERTER AND CLEANED CONNECTOR. OPS CHECKED NORMAL PER MM 34-25. A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002041700022 20020417 00022 NM 2002 4 17 2002F00404 1 20020304 A 2131 CONNECTOR BOEING 727 727225 1384077 NM CABIN PRESSURE DAMAGED A MYWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 804MA 22435 ON TAKEOFF FROM MIA, WHEN PASSING 17500 AUTO PRESSURIZATION FAILED TO STANDBY. SELECTED MANUAL DC. CONTINUED CLIMB TO FL330, AT 330 UNABLE TO CONTROL CABIN WITH OUTFLOW VALVES FULL CLOSED AND CARGO HEAT OUTFLOW VALVE CLOSED. CABIN CONTIN UED TO CLIMB AT 150 FT PER MINUTE. ENGINE BLEED PRESSURE NORMAL. RETURNED TO MIA. TROUBLESHOT SYSTEM AND FOUND PIN OP EN BETWEEN PIN 29 PRESSURE CONTROLLER AND PIN 55 ELECTRONIC CONTROLLER, FOUND MISSING IN CONNECTOR D4904. REMOVED AND R EPLACED CONNECTOR D4904P AND 4904J. OPERATION CHECK NORMAL IAW 21-31-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002041700027 20020417 00027 WP 2002 4 17 IXXA0200014O 1 20020415 A 3260 BRACKET DOUG DC8 DC871 302199A WP GEAR LOOSE A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 829BX 94922 623 45994 AFTER TAKE OFF FROM ANC, THE LANDING GEAR UPLATCH CHECK FAILED AND THE LANDING GEAR UNSAFE LIGHT ILLUMINATED. THE CREW C YCLED THE GEAR SEVERAL TIMES BEFORE THE UPLATCH CHECK PASSED AND THE LANDING GEAR UNSAFE LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO SEA FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE LEFT MAIN GEAR UP LIMI T SWITCH MOUNTING BRACKET LOOSE. MAINTENANCE TIGHTENED THE BRACKET AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK IN ACCOR DANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002041700028 20020417 00028 NM 2002 4 17 ASAA0210005 1 20020108 A 5330 6545767578 SKIN PANEL BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 416, STRINGER 16L CREASED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002041700029 20020417 00029 NM 2002 4 17 ASAA0210006 1 20020108 A 5330 65458001121 SKIN PANEL BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 259-360, STRINGER 28R-29R DAMAGED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002041700030 20020417 00030 NM 2002 4 17 ASAA0210007 1 20020108 A 5315 65549056 FLOORBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 400, STRINGER 17L CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002041700031 20020417 00031 NM 2002 4 17 ASAA0240004 1 20020103 A 5330 65C35768 SKIN BOEING 737 737490 1384715 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 799AS 29270 PAE - DURING C-CHECK, FOUND EXTERNAL SKIN GOUGED AT BS 494 AND STRINGER 21-22. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2002041700032 20020417 00032 NM 2002 4 17 ASAA0240006 1 20020118 A 5230 6547952358 SKIN BOEING 737 7374Q8 138447Q NM CARGO DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 783AS 25114 PAE - AFT CARGO DOOR INTERNAL SKIN IS CORRODED AT SNAP ADJACENT TO DOOR STOP PIN FITTING. REPAIRED IAW ASA EA. (M) 2 L 7 2 4F RT A16WE 2002041700033 20020417 00033 NM 2002 4 17 ASAA0240007 1 20020118 A 5230 6547952358 SKIN BOEING 737 7374Q8 138447Q NM CARGO DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 783AS 25114 PAE - AFT CARGO DOOR INTERNAL SKIN IS CORRODED AT SNAP AT AFT LOWE CORNER. REPAIRED IAW ASA EA. (M) 2 L 7 2 4F RT A16WE 2002041700034 20020417 00034 2002 4 17 ASAA0280011 4 20020123 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 SEA - DURING DISARMING OF R-1 SLIDE (IE UNCLIPPING AND STOWING GIRT BAR), LANYARD BETWEEN GIRT BAR AND SLIDE COVER BECAM E DISCONNECTED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2002041700035 20020417 00035 WP 2002 4 17 ASAA0280013 1 20020127 A 5311 S27779307003 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 PAE - DURING 30K-CHECK, FOUND CORROSION ON AFT SIDE OF FRAME AT FUSELAGE STATION 1250 BETWEEN LONGERON 30 AND 29R. REPA IRED FRAME PER SRM 53-03, FIG 2A. (M) 2 L 7 2 4F RT A6WE 2002041700036 20020417 00036 NE 2002 4 17 BJNA020302 2 20020314 A 7200 ENGINE BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE NR 2 STALLED A BJNA D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 11 789TM 23046 709435 ENGINE NR 2, COMPRESSOR STALL ABOVE IDLE. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2002041700037 20020417 00037 NE 2002 4 17 BJNA020303 2 20020319 A 7200 848101 TURBINE WHEEL BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE NR 2 ENGINE DAMAGED A BJNA C ABORTED TAKEOFF C R J F.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 11 344TM 34055 23044 709406 ON TAKEOFF ROLL, HEARD SEVERAL LOUD BANGS WITH A LOSS OF POWER ON NR 2 ENGINE. ABORTED TAKEOFF. REMOVED AND REPLACE TH E C-1 DISK, DUE TO FOD. ENGINE BORESCOPED, FOUND DAMAGE TO C-1 DISK. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2002041700038 20020417 00038 NM 2002 4 17 BJNA020304 1 20020322 A 3350 6013211 POWER SUPPLY BOEING 737 737282 13844AT NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 LEFT OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY PER BMM 33-51-31, GROUND CHECKS NORMAL, PER BMM 33-51-11. (M) 2 L 7 2 4F RT A16WE 2002041700039 20020417 00039 NE 2002 4 17 GAIA02027OP 2 20020320 A 7200 ENGINE BOEING 727 727223 1384074 NM PWA JT8 JT8D7B 52053 NE NR 2 STALLED A GAIA E A ENGINE SHUTDOWN UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 07 6833 20186 6533657B FLT 2713 - MCO-FWA - DURING CRUISE AT 31,000 FEET. THE NR 2 ENGINE COMPRESSOR STALLED. THE CREW SHUT DOWN NR 2 ENGINE AND DECLARED AN EMERGENCY. THE FLIGHT DIVERTED TO JAX AND THE LANDING WAS UNEVENTFUL. (M) 2 L 7 3 4F 4 F A3WE E2EA 2002041700040 20020417 00040 WP 2002 4 17 GTIA020253 1 20020328 A 2731 95906 ACTUATOR DOUG DC9 DC983 3022083 WP NOSE TRIM FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 824NK 53015 MYR - PRIMARY TRIM NOSE DOWN INTERMITTENT ON GROUND. REMOVED AND REPLACED PRIMARY TRIM MOTOR PER MD80 MM 27-40-01, OPER ATIONAL TEST OF PRIMARY TRIM MOTOR. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2002041700041 20020417 00041 2002 4 17 GTIA020254 4 20020328 A 2211 CONTROLLER DOUG DC9 DC983 3022083 WP AUTOPILOT MALFUNCTIONED A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 602CA 49415 FLL - FLT 1083 - NR 2 AUTOPILOT VERY JERKY IN LEVEL FLIGHT, YOKE MOVES BACK AND FORTH IN SHORT CHOPPY MOVEMENTS. STP RT S CHECK SHOWED 4 FAULTS A/P, F/D, A/T, S/V, Y/D. REMOVED AND REPLACED NR 2 DFGC. OPS CHECK NORMAL IAW MM 22-01-05. RT S CHECK INDICATES 'GO' NO FAULTS. (M) 2 L 7 2 4F RT A6WE 2002041700042 20020417 00042 WP 2002 4 17 GTIA020256 1 20020326 A 7160 LINER DOUG DC9 DC981 3022081 WP NR 2 ENGINE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 DTW - NR 2 ENGINE DIFFUSER OUTER FAN DUCT SECTION SOUND ABSORBING LINER DELAMINATED APPROX 40 SQUARE INCHES AT APPROX 7 O'CLOCK POSITION. REMOVED AND REPLACED NR 2 ENGINE AND TRIM TO-217A POWER IAW MD80 MM 71-00-00 AND SPIRIT CARD NR 191, 192 AND 193. (M) 2 L 7 2 4F A6WE 2002041700043 20020417 00043 WP 2002 4 17 GTIA020257 1 20020330 A 2700 95906 SWITCH DOUG DC9 DC983 3022083 WP TRIM INOPERATIVE A GTIA O OTHER O OTHER LD LANDING 1 GL 23 824NK 53015 DTW - FLT 56 - PRIMARY TRIM ON F/O SIDES STOP WORKING ON APPROACH INTO DTW HANDLES WERE USED AFTER LANDING, LEFT AND RIG HT ELECTRIC TRIM SWITCH AND HANDLES MANUAL TRIM INOPERATIVE. REMOVED AND REPLACED PRIMARY TRIM MOTOR. OPS CHECK GOOD I AW MD80 MM 27-40-01. (M) 2 L 7 2 4F RT A6WE 2002041700044 20020417 00044 WP 2002 4 17 GTIA020258 1 20020331 A 7120 K22199SA31 ISOLATION MOUNT DOUG DC9 DC983 3022083 WP ENGINE MOUNT WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 DTW - NR 2 FORWARD LOWER VIBRATION ISOLATOR REGS CHANGE DUE TO SLIP MARK OUT OF LIMITS. REMOVED AND REPLACED NR 2 ENGIN E FORWARD LOWER VIBRATION ISOLATOR IAW MD80 MM 71-20-02. INSTALLATION CHECKS GOOD WITH NO FURTHER DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 2002041700045 20020417 00045 WP 2002 4 17 GTIA020259 1 20020331 A 7120 K22199SA31 ISOLATION MOUNT DOUG DC9 DC983 3022083 WP ENGINE MOUNT WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 DTW - NR 2 ENGINE FORWARD UPPER VIBRATION ISOLATOR REGS CHANGE DUE TO METAL FLAKING OFF OF INNER RACE. REMOVED AND REPL ACED NR 2 ENGINE FORWARD UPPER VIBRATION ISOLATOR IAW MD80 MM 71-20-02. INSTALLATION CHECKS GOOD WITH NO FURTHER DEFECT S NOTED AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 2002041700046 20020417 00046 WP 2002 4 17 GTIA020260 1 20020331 A 7120 K22199SA32 ISOLATION MOUNT DOUG DC9 DC983 3022083 WP ENGINE MOUNT WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 DTW - NR 2 ENGINE AFT VIBRATION ISOLATOR REGS CHANGE DUE TO SCRATCHES ON INNER FACE. REMOVED AND REPLACED NR 2 ENGINE A FT VIBRATION ISOLATOR IAW MD80 MM 71-20-02. INSTALLATION CHECKS GOOD WITH NO FURTHER DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 2002041700047 20020417 00047 WP 2002 4 17 GTIA020261 1 20020331 A 3350 60030451 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 802NK 53168 MCO - AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY IAW M 33-53-00. LIGHTS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2002041700048 20020417 00048 NE 2002 4 17 GTIA020262 2 20020330 A 7200 FAN BLADE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D15 52051 NE NR 1 ENGINE DAMAGED A GTIA K NONE C F.O.D. IN INSP/MAINT 1 GL 23 805NK 48058 FLL - NR 1 ENGINE HAS FOD. FOUND THREE BLADES OUT OF LIMITS. REPLACED 3 AT SET OF C-1 BLADES IAW PWA JT8D FM P/N 77312 8 723302. PERTINENT DETAILS ARE ON FILE UNDER W/O 3198. (M) 2 L 7 2 4F 4 F A6WE E2EA 2002041700049 20020417 00049 2002 4 17 GTIA020263 4 20020331 A 2297 WIRE DOUG DC9 DC983 3022083 WP AUTOPILOT CHAFED A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 808NK 49504 ORD - AUTOPILOT AND AUTOTHROTTLES KICKED OFF AT 240. TAIL KICKED TO ONE SIDE TURNED OFF YAW DAMPER AND HAND FLEW AIRCRA FT. PERFORMED SYSTEM TROUBLESHOOTING AND SERVO/SENSOR OPERATION IAW MD80 MM 22-01-03. NOTED 2 CHAFED WIRE ON LUG NR 2 TERMINAL S-30-5. BUT SPLICED WIRES IAW MD80 MM 22-50-01. PERFORMED RTS CHECK IAW MD80 MM 22-01-05. NO FAULTS ERRORS D ETECTED SYSTEM OPERATION NORMAL AT THIS TIM. (M) 2 L 7 2 4F RT A6WE 2002041700050 20020417 00050 NE 2002 4 17 GTIA020264 2 20020331 A 7250 TURBINE BLADES DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 725388 DTW - NR 2 ENGINE REQUIRES BORESCOPE FOUND C-1 BLADE DAMAGED AND BORESCOPE REVEALED DAMAGED 7TH STAGE BLADES OUT OF LIMI TS. REMOVED AND REPLACED ENGINE. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002041700051 20020417 00051 WP 2002 4 17 GTIA020267 1 20020331 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAIL BAY LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FLL - EMERGENCY LIGHT INOPERATIVE IN TAIL COMPARTMENT. CEILING PANEL BETWEEN FLOURSCENT LIGHTS. SECURE WIRES AT SOCKET OF EMERGENCY LIGHT IN TAIL COMPARTMENT CEILING BETWEEN FLOUR. LIGHTS AND RELAMPED OPS CHECK OK IAW MM 33-50-00. (M) 2 L 7 2 4F A6WE 2002041700052 20020417 00052 WP 2002 4 17 GTIA020268 1 20020329 A 2742 ACTUATOR DOUG DC9 DC983 3022083 WP TRIM FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 809NK 49503 LGA - PREFLIGHT, FOUND PRIMARY STAB TRIM WOULD NOT OPERATE NORMALLY FROM THE SUITCASE HANDLES, MOTOR THERMALLY CUTS OUT AFTER ONLY SHORT USAGE 5-10 SECONDS FROM YOLK SWITCHES. FOUND 'B' PHASE C/B BAD REMOVED AND REPLACED 'B' PHASE C/B, OPS CHECK NORMAL PER A/C MM 27-40-00, AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A6WE 2002041700053 20020417 00053 WP 2002 4 17 GTIA020270 1 20020331 A 5270 STRIKER DOUG DC9 DC983 3022083 WP CARGO DOOR OUT OF ADJUST A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 809NK 49503 SJU - FLT 774 - AFT CARGO DOOR LIGHT ON AFTER TAKEOFF, RTB SJU, LIGHT OUT AFTER LANDING. ADJUSTED STRIKER PLATE FOR AFT CARGO DOOR PROX SWITCH IAW MD80 MM 52-70-02. FUNCTIONS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2002041700054 20020417 00054 WP 2002 4 17 GTIA020271 1 20020402 A 3260 CONNECTOR DOUG DC9 DC983 3022083 WP MLG INDICATION CONTAMINATED A GTIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 16892 49391 DTW - FLT 906 - CLIMBING OUT AT 14,000 FEET GEAR DOOR OPEN LIGHT CAME ON AND LEFT MAIN GEAR LIGHT CAME ON. HYDRAULIC PU MP TO HI, DOOR LIGHT WENT OUT. RECYCLED GEAR, LEFT GEAR UNSAFE LIGHT STAYED ON. DOOR LIGHT OUT WITH HYDRAULIC AT HIGH, LANDED AT DTW AT 139,000 LBS. FOLLOW QRH PROCEDURES. PERFORMED ADJUSTMENT/TEST OF LANDING GEAR POSITION AND WARNING I NDICATION SYSTEM PER MD80 MM 32-60-00 PAGE 201. PERFORMED PROXIMITY SWITCH ELECTRONICS UNIT BIT CHECK PER MD80 MM 32-60 -04. VERIFIED LEFT MAIN LANDING UP AND LATCHED PROXIMITY SENSOR AIR GAP TO BE CORRECT AND LEFT MAIN GEAR DOOR PROXIMITY SWITCH AIR GAP TO BE CORRECT. ALL OPS CHECK NORMALLY WITH NO DEFECTS NOTED. CLEANED MOISTURE FROM LEFT MLG DOOR UP AN 2 L 7 2 4F RT A6WE 2002041700055 20020417 00055 WP 2002 4 17 GTIA020274 1 20020401 A 3241 426071 CONTROL BOX DOUG DC9 DC983 3022083 WP ANTI SKID SYSTEM MALFUNCTIONED A GTIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 814NK 49619 DTW - FLT 909 - AT 80 KIAS ON TAKEOFF WHEEL NOT TURNING LIGHT CAME ON ABORTED TAKEOFF. REMOVED AND REPLACED ANTI-SKID C ONTROL BOX. BITE TEST AND SYSTEM CHECK OK IAW MD80 MM 32-43-00. (M) 2 L 7 2 4F RT A6WE 2002041700057 20020417 00057 EU 2002 4 17 SIMA200200701 1 20020107 A 3350 74449 SIGN SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 396AE 340B396 GGG - FLT 3504 - CREW REPORTED THE EMERGENCY EXIT SIGN FOR THE LEFT OVERWING EXIT TO BE INOPERATIVE. AIRCRAFT WAS FERRI ED TO DFW FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002041700058 20020417 00058 EU 2002 4 17 SIMA200200702 1 20020107 A 3330 3716 BALLAST AEROSP ATR42 ATR42300 8680920 EU CARGO BAY MALFUNCTIONED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 242AT 242 MHH - FLT 5017 - ON APPROACH INTO MHH CREW DETECTED WHAT APPEARED TO BE ELECTRICAL SMELL. AFTER DEBOARDING AT THE GATE CREW NOTED THAT THE OVERHEAD LIGHT IN THE FORWARD CARGO WAS HOT AND THE SMELL WAS COMING FROM THE LIGHT. LIGHT WAS PUT ON MEL AT THIS TIME. MAINTENANCE REMOVED AND REPLACED THE BALLAST UNIT FOR THE FORWARD CARGO LIGHT IAW ATR MM. OPERATIO NAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002041700059 20020417 00059 EU 2002 4 17 SIMA200207403 1 20020315 A 3350 LH6151 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 420AT 420 MIA - FLT 4958 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 6AB TO BE INOPERATIVE. MAINTENANCE REPLACED THE SOCKET AT SEAT 6AB. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002041700060 20020417 00060 NM 2002 4 17 TSAA0251094 1 20020226 A 5511 6573794 RIB BOEING 737 7372X6C 1384552 NM HORIZONTAL STAB CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CRACKS ON VARIOUS SUPPORT RIBS LISTED FROM INBOARD TO OUTBOARD NR 2, 3, 4, 5, 6, 7, AND 8. CUT AND REMOVED PORTIONS OF FORMED SECTIONS. FABRICATED REPAIR PARTS FROM .040 AND .050 INCH THI CK 2024 T3. ASSEMBLED THE REPAIR PARTS AND DRILLED HOLES, REMOVED ALL SHARP EDGES TO .015 R TO .030 R. APPLIED ALODINE D COATING AND PRIMER. INSTALLED REPAIR PARTS IAW SRM 51-40-3 FIGURE 1 SHEET 1-6 AND SRM 51-30-2 PAGE 2. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002041700061 20020417 00061 NM 2002 4 17 TSAA0251095 1 20020226 A 5313 65C33547 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 DAMAGED STRINGER BETWEEN FS 1040 AND FS 1064 STRINGER 27L. REMOVED DAMAGED SECTION IAW SRM 51-40-3 FIGURE 1. FABRICATE D REPAIR DOUBLER USING .040 INCH THICK 2024 T3 IAW SRM 51-20-1 PAGES 10A TO 22. PROTECTED MATERIAL USING AN IRIDITE SOL UTION APPLICATION IAW SRM 51-20-2 PAGE 7. PRIMED AND INSTALLED REPAIR PARTS IAW SRM 51-40-3. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 2002041700062 20020417 00062 NM 2002 4 17 TSAA0251096 1 20020329 A 5312 6545819 BULKHEAD BOEING 737 737230 1384401 NM NLG WW CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 FOUND CRACK ON UPPER BULKHEAD IN THE NOSE WHEEL WELL. TRIMMED OUT CRACK ENSURING A .50 INCH MINIMUM RADIUS. VERIFIED C RACK REMOVED USING HFEC METHOD AND MADE A .040 INCH INSURANCE CUT. FABRICATED A FILLER FROM .050 INCH, A DOUBLER FROM . 063 INCH AND TWO TAPPERED FILLERS AS SHOWN IN FIGURE 1 WITH A 50:1 TAPER RATION FROM 2024-T3 CLAD SHEET. INSTALLED ALL REPAIR PARTS IAW FIGURE 1. VERIFIED 8110-3 RECEIVED FROM BOEING. REPAIR COMPLETED IAW ECO 3194. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002041700063 20020417 00063 2002 4 17 USAABB02034 4 20020319 A 2565 GIRT BAR BOEING 757 757225 1384959 NM ESCAPE SLIDE DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 600AU 22192 CLT - GIRT BAR ENGAGEMENT LIGHT DID NOT ILLUMINATE WITH SLIDE ARMING LEVER IN THE ARMED POSITION (L1 DOOR). MAINTENANCE REINSTALLED THE GIRT BAR. (M) 2 L 7 2 4F RT A2NM 2002041700064 20020417 00064 WP 2002 4 17 USAAD02013 1 20020218 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 822US 49139 PIT - THE SEAT MOUNTED AND TAILCONE EMERGENCY LIGHT BATTERIES INDICATED LOW. MAINTENANCE REPLACED THE EMERGENCY LIGHT B ATTERIES. (M) 2 L 7 2 4F A6WE 2002041700065 20020417 00065 WP 2002 4 17 USAAD02014 1 20020319 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 800US 48034 PIT - THE SEAT MOUNTED AND TAILCONE EMERGENCY LIGHT BATTERIES INDICATED LOW. MAINTENANCE REPLACED THE EMERGENCY LIGHT B ATTERIES. (M) 2 L 7 2 4F A6WE 2002041700066 20020417 00066 WP 2002 4 17 USAAD02015 1 20020319 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 812US 48092 IND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2002041700067 20020417 00067 WP 2002 4 17 USAAD02016 1 20020319 A 3350 BATTERY DOUG DC9 DC981 3022081 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 811US 48043 PIT - THE DOOR EXIT AND NUMEROUS FLOOR LEVEL EMERGENCY LIGHTS WILL NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT B ATTERIES. (M) 2 L 7 2 4F A6WE 2002050600092 20020506 00092 NM 2002 5 6 02FDEA00252 1 20020410 A 5320 A6A709417 STANCHION DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 EXFOLIATION CORROSION ON FWD CARGO COMPT VERTICAL BEAM SUPPORT (U-CHANNEL) AT X=-8 IN. REMOVED AND REPLACED STANCHION P ER DWG A6A7094. 2 L 7 3 4F RT A22WE 2002041700072 20020417 00072 EU 2002 4 17 02FDEA00251 1 20020407 A 5210 A5211100420201 FITTING AIRBUS 310 A310222 3930315 EU #1 LEFT DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 L/MAIN ENTRY DOOR EXTERIOR HANDLE CUTOUT CORRODED AT HORZ WEB & AFT VERT WEB. R&R FITTINGS PER SRM 51-72-10 & REFITTED DOOR HANDLES & LIFT RODS. 2 L 7 2 4F RT A35EU 2002050600093 20020506 00093 NM 2002 5 6 02FDEA00253 1 20020410 A 5320 A6A70949 STANCHION DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 EXFOLIATION CORROSION ON FWD CARGO COMPT AFT BULKHEAD VERT BEAM SUPPORT (U-CHANNEL) AT X=+ 8 IN. REMOVED AND REPLACED S TANCHION PER DWG A6A7094. 2 L 7 3 4F RT A22WE 2002050600094 20020506 00094 NM 2002 5 6 02FDEA00254 1 20020410 A 5320 A6A710947 STANCHION DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 INTERGRANULAR CORROSION ON FWD CARGO COMPT AFT BULKHEAD VERT BEAM SUPPORT (U-CHANNEL) AT X=+ 29 IN. REMOVED AND REPLACE D STANCHION PER DWG A6A7094. 2 L 7 3 4F RT A22WE 2002050600095 20020506 00095 NM 2002 5 6 02FDEA00255 1 20020410 A 5320 A6A70945 STANCHION DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 EXFOLIATION CORROSION ON FWD CARGO COMP AFT BULKHEAD VERT BEAM SUPPORT (U-CHANNEL) AT X =+ 56 IN. REMOVED AND REPLACED STANCHION PER DWG A6A7094. 2 L 7 3 4F RT A22WE 2002042400090 20020424 00090 NM 2002 4 24 02FDEA00257 1 20020407 A 5311 6516314 FRAME BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 CORROSION (C53-224-01) AND TOOLING DAMAGE ON FRAME I/B FLANGE BS 372, WL 212, RBL 64. REMOVED AND REPLACED FRAME PER SR M 51-4-3. 2 L 7 3 4F A3WE 2002042400092 20020424 00092 NM 2002 4 24 02FDEA00258 1 20020413 A 5741 65870197 PIN BOEING 727 727225 1384077 NM WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 CORROSION AT FLANGE BASE OF TERMINAL PIN. REMOVED AND REPLACED PIN PER 75C012-00. 2 L 7 3 4F A3WE 2002042400093 20020424 00093 NM 2002 4 24 02FDEA00259 1 20020413 A 5741 6483365 PIN BOEING 727 727225 1384077 NM WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 CORROSION AT FLANGE BASE OF TERMINAL PIN. REMOVED AND REPLACED PIN PER 75C011-00. 2 L 7 3 4F A3WE 2002050900069 20020509 00069 NM 2002 5 9 02FDEA00260 1 20020416 A 5313 STRINGER BOEING 727 727225 1384077 NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 N 1101 STRINGER 7 LT MID SPAR IS CHAFED 4 INCHES IN FRONT OF SLIDING SEAL. R&R STRINGER PER E.A. 7-5530-54204. 2 L 7 3 4F A3WE 2002050200091 20020502 00091 CE 2002 5 2 00016 1 20020412 A 3260 WARNING LIGHT LEAR 24 24D 5170311 CE COCKPIT FALSE INDICATION E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 277TW 277 NOSE GEAR UNSAFE LIGHT AFTER TAKEOFF, RETURN TO DEPARTURE AIRPORT, THREE GREEN DOWN AND LOCKED. AIRCRAFT TO BE FERRIED BACK TO ADS, GEAR DOWN AND LOCKED FOR MAINTENANCE. MAINTENANCE JACKED AND CYCLED GEAR 10 TIMES WITH ALL OP'S NORMAL. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4J A10CE 2002041700074 20020417 00074 WP 2002 4 17 0201119925 1 20020407 A 3246 95608924 WHEEL DOUG DC9 DC932 3022066 WP LT MLG FAILED A NWAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 925US 47472 THE LEFT OUTBOARD ANTI-SKID LIGHT ILLUMINATED DURING TAKEOFF ROLL AT FAR. CLIMBOUT AND GEAR RETRACTION WERE NORMAL. LA NDING WAS UNEVENTFUL AT MSP BUT CREW THOUGHT THE AIRCRAFT WAS A LITTLE HARD TO TAXI. SUSPECTED A FLAT TIRE OR A DRAGGIN G BRAKE. NO TIRE WAS FLAT AND INSPECTION REVEALED THE WHEEL HUB HAD FAILED. HUBCAP AND BEARINGS WERE FOUND ON THE TAXI WAY AT FAR. MAINTENANCE REPLACED THE DAMAGED WHEEL, NR 1 BRAKE, AND NR 1 ANTI-SKID TRANSDUCER. ALL FUNCTIONAL CHECKS W ERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002041700075 20020417 00075 2002 4 17 0201139981 4 20020404 A 2565 13621228 SLIDE DOUG DC9 DC931 3022065 WP TAILCONE FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 994Z 47097 GROUND SERVICE AGENT DROPPED THE TAIL CONE WHILE TRYING TO GAIN ENTRY INTO THE AIRCRAFT. THE EVACUATION SLIDE DID NOT D EPLOY WHEN THE TAIL CONE DROPPED. MAINTENANCE REPLACED THE TAIL CONE. DROPPED CHECK TESTED THE TAIL CONE AND SLIDE ASS EMBLY AND THE SLIDE DID DEPLOY ON TEST. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002041700076 20020417 00076 NM 2002 4 17 0201146304 1 20020405 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 664US 23819 DURING LINE CHECK, FOUND THE RIGHT FIRST CLASS FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED WIRES. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002041700077 20020417 00077 WP 2002 4 17 0201159880 1 20020404 A 7897 WIRE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE RT T/R DAMAGED A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 675MC 47651 688777 DURING TAKEOFF ROLL AT 116 KNOTS, THE RIGHT ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND R ETURNED TO THE GATE. MAINTENANCE REPAIRED DAMAGED WIRES AND REPLACED THE CANNON PLUG FOR THE RIGHT ENGINE THRUST REVERS ER LATCH SWITCH. ENGINE OPERATIONALLY CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2002041700078 20020417 00078 EA 2002 4 17 02100650 1 20020410 A 2910 13E415 HEAT EXCHANGER CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM DEFECTIVE A VTZA E A ENGINE SHUTDOWN UNSCHED LANDING J M WARNING INDICATION OVER TEMP CR CRUISE 1 EA 27 650BR 7418 DURING CRUISE OF THE FLIGHT FROM ORD TO JAX, THE NR 1 HYDRAULIC SYSTEM INDICATED AN OVERHEAT. THE CREW FOLLOWED THE QRH PROCEDURES, SHUT DOWN THE NR 1 ENGINE AND DIVERTED TO IND WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REMO VED AND REPLACED THE HYDRAULIC HEAT EXCHANGER AND HEAT EXCHANGER POWER RELAY. A MAINTENANCE ACCEPTANCE FLIGHT WAS SATIS FACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. RELAY P/N M83536-6-025M. 2 L 7 2 4F RT A21EA 2002041700080 20020417 00080 NE 2002 4 17 02FDEA00237 2 20020408 A 7321 FUEL CONTROL AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E 52054 NE NR 1 ENGINE FAULTY A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 447FE 251 ON TAKEOFF THROTTLES WERE 2 KNOB WIDTH APART ON CLIMB NR 1 ENG W/N REACH FULL PWR. DURING DESCENT NR 1 IDG ADVISORY ILL UM AND TEMP REACHED 144 DEG. REMOVED AND REPLACED PRSOV DIFFUSER CASE LINER REWORKED. REMOVED AND REPLACED AIR HEAT EX CHANGER SOV VALVE. 2 L 7 2 4F 4 F RT A35EU E3NE 2002042600100 20020426 00100 NM 2002 4 26 02FDEA00261 1 20020414 A 5320 WEB BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 HOLES IN WEB AT BS 372 TO 415, RBL 65 TO 70, WL 208. REMOVED AND REPLACED WEB PER SRM 51-30-2, 53-10-1, 51-10-3, 51-10- 2, 51-20-1. 2 L 7 3 4F A3WE 2002042400096 20020424 00096 NM 2002 4 24 02FDEA00263 1 20020415 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 HOLES IN FLOORBEAM AT BS 420, RBL 60-65, WL 208. REMOVED AND REPLACED FLOORBEAM PER EA 7-5335-54192. 2 L 7 3 4F A3WE 2002042400098 20020424 00098 NM 2002 4 24 02FDEA00264 1 20020415 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 HOLE UPPER FWD FLANGE OF FLOORBEAM BS 480, RBL 49, WL 208. REMOVED AND REPLACED FLOORBEAM PER EA 7-5335-54192 & SRM 53- 10-8 FIG 3. 2 L 7 3 4F A3WE 2002042400099 20020424 00099 NM 2002 4 24 02FDEA00265 1 20020415 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 HOLES IN FLOORBEAM AT BS 380, RBL 60-65, WL 208. REMOVED AND REPLACED FLOORBEAM PER EA 7-5335-54192 & SRM 53-10-8 FIG 3 . 2 L 7 3 4F A3WE 2002042400104 20020424 00104 NM 2002 4 24 02FDEA00266 1 20020415 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 HOLES IN FLOORBEAM AT BS 400, RBL 60-65, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 3 & EA 7-5335-54192 . 2 L 7 3 4F A3WE 2002041700087 20020417 00087 NM 2002 4 17 200200245 1 20020412 A 7830 65B9751312 VANE BOEING 747 747SR46 1384816 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 477EV 20784 LEFT HAND NR 4 CASCADE VANE WAS CRACKED AT AFT ATTACH AREA. REPLACED CASCADE VANE IN ACCORDANCE WITH B747 M/M 78-31-07. 2 L 7 4 4F 4 F RT A20WE E20EA 2002041700089 20020417 00089 WP 2002 4 17 2002F00375 1 20020214 A 5312 PRESSURE PANEL LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION LEVEL 2 CORROSION ON NOSE LANDING GEAR WHEEL WELL TOP PANEL AT FS 369, RBL 22, AFT RIGHT OUT BOARD CORNER OF FORWARD WHEEL WELL PANEL FOUND. MAINTENANCE REPAIRED THE CORRODED AREA IN ACCORDANCE WITH ER/A L10-53R- 4717. 2 L 7 3 4F A23WE 2002041700090 20020417 00090 2002 4 17 2002F00387 4 20020411 A 3425 INDICATOR BOEING 757 75733N 1384931 NM COCKPIT FAILED G AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 558TZ 32592 FLIGHT NUMBER 596, DURING CRUISE ADIRU INERTIAL FUNCTION FAILED, FIRST OFFICERS ARTIFICIAL HORIZON FAILED. 2 L 7 2 4F RT A2NM 2002041700092 20020417 00092 WP 2002 4 17 ABXA010820 1 20020401 A 5730 59195721 PANEL DOUG DC9 DC941 302207N WP LT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 PANEL 1502 HAD 2 EACH AREAS OF DELAMINATION AND 1 SPOT OF LEVEL 1 CORROSION ON EXTERIOR SURFACE. REPLACED THE BUTE DOOR IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002041700093 20020417 00093 WP 2002 4 17 ABXA010822 1 20020401 A 5330 5910228183 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 CRACK IN FUSELAGE EXTERIOR SKIN AT STATION 1222, LONGERON 15 RIGHT. REPAIRED CRACK IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002041700094 20020417 00094 WP 2002 4 17 ABXA010823 1 20020403 A 5320 992345352 ANGLE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 CRACKED ANGLE AT STATION 775, RIGHT UPPER WHEEL WELL AT LONGERON 20. REPLACED ANGLE AND REPAIRED AREA IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002041700095 20020417 00095 WP 2002 4 17 ABXA010824 1 20020403 A 5320 49113831 FITTING DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 FRAME FOOT FITTING CORRODED AT FS 927 LEFT. REPLACED FRAME FOOT IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2002041700096 20020417 00096 WP 2002 4 17 ABXA010825 1 20020403 A 5320 49113831 FITTING DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 FRAME FOOT FITTING CORRODED AT STATION 946 LEFT. REPLACED FRAME FOOT IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2002041700098 20020417 00098 WP 2002 4 17 ABXA010827 1 20020403 A 5320 49113832 FITTING DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 FRAME FOOT FITTING AT STATION 927 RIGHT WAS CORRODED. REPLACED FRAME FOOT IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2002041700099 20020417 00099 WP 2002 4 17 ABXA010828 1 20020409 A 5320 D0489835 WEB DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 CUSP WEB BTN, FS 1021-1041, LEFT SIDE WAS CRACKED (2 PLACES) EACH COMING OUT OF A LIGHTENING HOLE. REPAIRED DAMAGED CUS P WEB IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002060700034 20020607 00034 NM 2002 6 7 AWXA200200338 1 20020413 A 3260 6552811109 ACCESSORY UNIT BOEING 737 737277 1384570 NM E/E BAY FAILED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 178AW 4008 4008 22645 AFTER RETRACTION OF THE LANDING GEAR THE RT MLG WARNING LIGHT REMAINED ILLUM, ACFT RETURNED. LIGHT EXTINGUISHED AFTER T HROTTLES WERE ADVANCED AT THE BOTTOM OF DESCEND. MX TROUBLESHOT AND REPLACED THE LANDING GEAR ACCESSORY UNIT, AND THE R T LANDING GEAR PROXIMITY SENSOR SWITCH, OPS TEST GOOD. VENDOR BENCH TEST OF LANDING GEAR ACCESSORY UNIT CONFIRMED FAILU RE WITH UNIT FAILING TEST FOR PROXIMITY SWITCH. TEARDOWN FINDING FOUND PROXIMITY SWITCHES L3, L8, L13, AND L16 OUT OF C ALIBRATION. THE SWITCHES WERE CALIBRATED, AND TEARDOWN ALSO NOTED RESISTORS WERE REPLACED (NO PART NUMBERS). 2 L 7 2 4F RT A16WE 2002041700101 20020417 00101 NM 2002 4 17 AWXA200200340 1 20020413 A 5270 FPTN404781R0003 PROXIMITY SWITCH AIRBUS A319 A319132 3930340 NM AVIONICS DOOR OUT OF ADJUST A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 802AW 924 PHX - AIR TURNBACK - FLT 0590 - WHILE CLIMBING OUT OF PHX EN ROUTE TO MCI AT 10,000 FEET ECAM INDICATED THE RT AFT AVION ICS DOOR WAS OPEN. AIRCRAFT TURNED BACK AND LANDED SAFELY AT PHX. MAINTENANCE VERIFIED THE DOOR WAS CLOSED. ADJUSTED THE GAP ON THE RT AFT AVIONICS DOOR PROXIMITY SWITCH, OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2002052000099 20020520 00099 NM 2002 5 20 AWXA200200341 1 20020414 A 2433 08020325 RECTIFIER BOEING 737 7373Y0 1384671 NM E/E BAY FAULTY A AWXA A UNSCHED LANDING J B G WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE CR CRUISE 1 WP 28 334AW 23747 DURING CRUISE NR 2 AFT FUEL PUMP LOW PRESSURE LIGHT AND FIRST OFFICERS PITOT STATIC 1 AUX P/S ILLUMINATED . NR 2 TRANSF ORMER RECTIFIER CIRCUIT BREAKER POPPED FOLLOWED BY A STRONG ELECTRICAL BURNING SMELL. AN EMERGENCY WAS DECLARED AND AIR CRAFT DIVERTED TO ABQ. DURING FINAL APPROACH AFTER DISCONNECTING AUTOPILOT; THE ELECTRICAL STABILIZER TRIM FAILED, AND STANDBY ALTIMETER, AIR SPEED INDICATOR & VIBRATION CIRCUIT BREAKERS POPPED. MX TROUBLESHOT, FOUND A BURNED SPOT WITH BU RNT ELECTRICAL ODOR ON NR 2 TRANSFORMER RECTIFIER. REPLACED NR 2 TRANSFORMER RECTIFIER. OPERATIONAL CHECKS PERFORMED O N STANDBY ALTIMETER, FUEL PUMP, HORIZONTAL STABILIZER TRIM CONTROL SYSTEM AND PITOT STATIC. ALL CHECKS GOOD. 2 L 7 2 4F RT A16WE 2002041700102 20020417 00102 NM 2002 4 17 C1HA200292004 1 20020412 A 5210 DOOR BOEING 727 727212 138407G NM L1 NOT CLOSED A C1HA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 15 292AS 21458 FORWARD L1 DOOR EXCESSIVE NOISE ON DEPARTURE. ALL LIGHT INDICATIONS ON ANNUNCIATOR PANEL NORMAL. FOUND L1 DOOR NOT COM PLETELY CLOSED. OPS CHECKED DOOR SEVERAL TIMES AND INSPECTED ALL SEALS. ALL LIGHT INDICATIONS WERE NORMAL. SEALS WERE NORMAL. ALL CHECKS GOOD, OK FOR CONTINUED SERVICE. 2 L 7 3 4F A3WE 2002041700104 20020417 00104 EU 2002 4 17 QXEA0200425 1 20020302 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 481.800 THERE IS AN AREA ABOUT 5 INCHES LONG WITH MANY GOUGES ON THE LUGS. REPAI RED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205 AND SRM 53-02-15, FIGURE 1. 2 L 7 2 4F RT A20EU 2002041700105 20020417 00105 EU 2002 4 17 QXEA0200426 1 20020302 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 464.328 TOP LUGS HAVE GOUGES. REPAIRED IAW FOKKER SRM 53-02-15, FIGURE 1 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002041700106 20020417 00106 EU 2002 4 17 QXEA0200427 1 20020302 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 443.024 ON FLANGE WHERE TRACKS BUTT UP THERE IS CHAFING. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205 AND SRM 53-02-15, FIGURE 1. 2 L 7 2 4F RT A20EU 2002041700107 20020417 00107 EU 2002 4 17 QXEA0200428 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK AT STATION 191.929 MOST FORWARD END OF TRACK HAS CORROSION ON LUGS. ALSO, IN CHANNEL AND ON FLANGES. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 4C, SRM 51-10-4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002041700108 20020417 00108 EU 2002 4 17 QXEA0200429 1 20020220 A 5310 DOOR FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CHAFE ON AFT CARGO DOOR APERTURE LOWER AFT CORNER. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3, PARAGRAPH 3D AND HOR IZON AIR EA 4-53-1570. 2 L 7 2 4F RT A20EU 2002041700109 20020417 00109 EU 2002 4 17 QXEA0200430 1 20020222 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK FROM FRAME 9305 FORWARD 9 X 2 INCHES LONG INSIDE CHANNEL HAS PITTING AND CORROSION. REPAIRE D IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 4C AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002041700110 20020417 00110 EU 2002 4 17 QXEA0200431 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT INBOARD SEAT TRACK FROM FRAME 8805 FORWARD ABOUT 7 X 6 INCHES LONG INSIDE CHANNEL THERE IS CORROSION. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 4C, STEP1. 2 L 7 2 4F RT A20EU 2002041700111 20020417 00111 EU 2002 4 17 QXEA0200432 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK AT FRAME 6305 FORWARD ABOUT 5 INCHES LONG ON INBOARD FLANGE THERE IS CORROSION. REPAIRED I AW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 4C, STEP 1. 2 L 7 2 4F RT A20EU 2002041700112 20020417 00112 EU 2002 4 17 QXEA0200433 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CORROSION ON RT OUTBOARD SEAT TRACK AT FRAME 5805 FORWARD ABOUT 5.5 X 3 INCHES LONG ON INBOARD FLANGE. REPAIRED I AW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 2002041700113 20020417 00113 EU 2002 4 17 QXEA0200434 1 20020222 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CORROSION ON RT OUTBOARD SEAT TRACK FORWARD OF FRAME 5305 ABOUT 10 INCHES TO FRAME 4610 OUTBOARD FLANGE. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002041700114 20020417 00114 EU 2002 4 17 QXEA0200435 1 20020222 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CORROSION ON RT OUTBOARD SEAT TRACK AFT OF FRAME 4610 ON INBOARD FLANGE. REPAIRED IAW FOKKER MM PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 2002041700115 20020417 00115 EU 2002 4 17 QXEA0200436 1 20020222 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CORROSION ON RT INBOARD SEAT TRACK FORWARD OF FRAME 4900 ABOUT 2 X 3 INCHES LONG ON OUTBOARD FLANGE. REPAIRED IAW FOKKER MM PAGE 206, FIGURE 205 AND SRM 53-01-01, PAGE 8, PARAGRAPH 4C. 2 L 7 2 4F RT A20EU 2002041700116 20020417 00116 EU 2002 4 17 QXEA0200437 1 20020306 A 5534 ANGLE FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACK ON VERTICAL STAB TO FUSELAGE LT CONNECTION ANGLE INTERMEDIATE SPAR II. REPAIRED IAW FOKKER SRM 55-31-00, PA GE 2 AND SRM 51-31-04. 2 L 7 2 4F RT A20EU 2002041700117 20020417 00117 EU 2002 4 17 QXEA0200438 1 20020215 A 2730 CONTROL CABLE FOKKER F28 F28MK4000 4990810 EU ELEVATOR BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD ELEVATOR CABLE AT PULLEY CLUSTER BELOW HORIZONTAL STABILIZER ACTUATOR HAS BROKEN WIRES. REPAIRED IAW F OKKER SRM 27-31-00, PAGES 201 AND 502, STEPS 1-3 A (1)-(8). 2 L 7 2 4F RT A20EU 2002041700118 20020417 00118 EU 2002 4 17 QXEA0200439 1 20020219 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - DENT IN AFT FUSELAGE SKIN AFT OF FRAME 41-2 BETWEEN STRINGER 3 AND 5. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 9, P ARAGRAPH 6C AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002041700123 20020417 00123 NM 2002 4 17 02FDEA00228 1 20020404 A 5310 FRAME BOEING 727 727225 1384077 NM CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 N 321 DRILL START IN BS 700 FRAME BETWEEN STR 24 & 35 R. ** S/D ** R&R FRAME PER SRM 51-40-03. 2 L 7 3 4F A3WE 2002041700124 20020417 00124 NM 2002 4 17 SABA020052 1 20020417 A 3250 1306 BULB DHAV DHC8 DHC8103 1386005 NM CABIN BURNED OUT A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 882CC 168 Aircraft 882 on flight 5025 from CLT to TLH. During preflight inspection in CLT a floor emergency light bulb was found inoperative. Maintenance removed and replaced the bulb. System ops checked good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002041700128 20020417 00128 WP 2002 4 17 COOSDR020069 1 20020401 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CABIN CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 FORWARD CARGO COMPARTMENT, AT Y STA 100, 120, 140, 160, 180, 200, 220, 240, 260, 360, 380, 400, 418, 460, 480, 520, 540, 580, 600, 620, BETWEEN LONG 29 LEFT TO 29 RIGHT, TITANIUM FLOOR SUPPORT ANGLES CRACKED. 2 L 7 4 4F RT 4A25 2002041700130 20020417 00130 WP 2002 4 17 COOSDR02058 1 20020401 A 5320 5952803515 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP STA 1231 CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 813US 48093 AFT CARGO COMPARTMENT, AT STA 1231 BETWEEN LONGERON 28L AND LONGERON 29L, TITANIUM FLOOR SUPPORT ANGLE (PN 5952803-515) CRACKED. 2 L 7 2 4F A6WE 2002041700131 20020417 00131 WP 2002 4 17 COOSDR02059 1 20020401 A 5320 5952803521 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 813US 48093 AFT CARGO COMPARTMENT, AT STA 1287 BETWEEN LONGERON 29L AND LONG 30, TITANIUM FLOOR SUPPORT ANGLE (5952803-521) CRACKED. 2 L 7 2 4F A6WE 2002041700132 20020417 00132 WP 2002 4 17 COOSDR02060 1 20020401 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 813US 48093 LOWER FUSELAGE - YSTA 237.0 AND YSTA 332.0 LONGERON 17 LEFT WITH CRACK. 2 L 7 2 4F A6WE 2002041700133 20020417 00133 WP 2002 4 17 COOSDR02061 1 20020401 A 5730 9936835505 PANEL DOUG DC9 DC981 3022081 WP LT WING DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 813US 48093 LEFT WING, INNER TRAILING EDGE LOWER PANEL (PN 9936835) DELAMINATED. 2 L 7 2 4F A6WE 2002041900065 20020419 00065 NM 2002 4 19 F3LA200200125 1 20020415 A 5230 DOOR FRAME BOEING 737 7373L9 1384470 NM CARGO DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 3415 24569 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT DOOR FRAME WEB FROM STR 23-R TO 25-R. FABRICAT ED AND INSTALLED REPLACEMENT WEB PER SRM 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A16WE 2002041900062 20020419 00062 EU 2002 4 19 DHL2002364005 1 20020416 A 2611 FSD200500 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN FALSE ACTIVATION A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 364DH 141 AFT MAIN CABIN SMOKE DETECTOR LIGHT ON. REMOVED AND REPLACED NR 6 SMOKE DETECTOR IAW MM 26-14-11. 2 L 7 2 4F RT A35EU 2002041700134 20020417 00134 WP 2002 4 17 COOSDR02062 1 20020401 A 5753 5930496501J4 SKIN DOUG DC9 DC981 3022081 WP TE FLAP DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 813US 48093 LEFT WING OUTBOARD FLAP, NR 2 VANE FLAP, UPPER SKIN DELAMINATED. 2 L 7 2 4F A6WE 2002041700135 20020417 00135 WP 2002 4 17 COOSDR02063 1 20020401 A 5753 5910042507AB1 SKIN DOUG DC9 DC981 3022081 WP TE FLAP DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 813US 48093 LEFT WING, OUTBOARD FLAP, CENTER VANE FLAP (PN 5910042-507AB1) DELAMINATED. 2 L 7 2 4F A6WE 2002041700136 20020417 00136 NM 2002 4 17 C1HA200294007 1 20020403 A 3244 TIRE BOEING 727 727290 138408W NM LT MLG FAILED A C1HA K NONE O OTHER LD LANDING 1 GL 15 294AS 22146 AFTER LANDING AND SLOWING TO APPROX 80 KNOTS, THE LEFT MAIN TIRE SEEMED TO HAVE BLOWN. THIS WAS CONFIRMED BY TOWER. EM ERGENCY PERSONNEL CONFIRMED LEFT OUTBOARD TIRE WAS NOT PRESENT AND THE LEFT INBOARD TIRE DEFLATED SHORTLY AFTERWARD. RE MOVED AND REPLACED NR 1AND 2 MLG TIRE ASSY'S PER MM 32-45-01. REMOVED AND REPLACED NR 1 MAIN BRAKE ASSY IAW MM 32-41-32 . REMOVED AND REPLACED NR 2 BRAKE ASSY IAW MM 32-41-32. REMOVED AND REPLACED NR 1 BRAKE FLEX LINES AS PER MM 32-00. P ERFORMED ADJ AND TEST OP'S. CHECK NORMAL. NO DEFECTS AT THIS TIME. REMOVED AND REPLACED O-RING AND BACK-UP RINGS ON N R 1 BRAKE SHUTTLE VALVE. OPS CHECK GOOD, NO LEAKS PER MM 32-44. 2 L 7 3 4F A3WE 2002041700137 20020417 00137 WP 2002 4 17 COOSDR02070 1 20020401 A 5720 5919572508 DOOR DOUG DC9 DC981 3022081 WP RT WING CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 813US 48093 RIGHT WING, TRAILING EDGE, XW 156.583, BUTTE DOOR (PN 5919572-509) SN 1202 CRACKED. 2 L 7 2 4F A6WE 2002041700138 20020417 00138 NM 2002 4 17 C1HA200296013 1 20020411 A 7711 LG14C14 TRANSMITTER BOEING 727 7272J4 1384006 NM NR 2 FAILED A C1HA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 15 696CA 22574 ONE TAKEOFF ROLL, NR 2 EPR GAUGE INOPERATIVE. ABORTED TAKEOFF. TROUBLESHOT SYSTEM AND REMOVED AND REPLACED NR 2 EPR TR ANSMITTER. ENGINE RUN UP TO MAX. TRIM AND OPERATIONAL CHECKS GOOD. 2 L 7 3 4F RT A3WE 2002041700139 20020417 00139 WP 2002 4 17 COOSDR02071 1 20020401 A 5320 4646163501 SPLICE DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT CARGO COMPARTMENT, BETWEEN STA 1340 AND STA 1360 AT LONG, 28L LEVEL, LONGERON SPLICE (PN 4646163501) CORRODED. 2 L 7 4 4F RT 4A25 2002041900097 20020419 00097 NM 2002 4 19 F3LA200200126 1 20020415 A 5230 STRAP BOEING 737 7373L9 1384470 NM CARGO DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 3415 24569 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT DOOR FRAME UNDER UPPER FLANGE AT NUT PLATES AT STA 794, STR 25-R. REPLACED CORRODED RADIUS STRAP FROM STR 17R TO 27R PER SRM 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A16WE 2002041700140 20020417 00140 SO 2002 4 17 C2XA02BT013 1 20020415 A 3230 355022002 CONTROL UNIT EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13997 145298 EWR---CO3541, AIRCRAFT AIR RETURN TO EWR. CREW REPORTED, WHEN LANDING GEAR BROUGHT TO RETRACT, RECEIVED ON EICAS LG/LEV ER DISAGREE MESSAGE, ALSO LEFT MAIN ON EICAS WAS RED CROSS HATCHED(INDICATION), NOSE AND RIGHT MAIN RED DOWN INDICATION. MAINTENANCE TROUBLESHOT PROBLEM AND REMOVED AND REPLACED LGEU IAW REFERENCE EMB 145 MM 32-32-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002041700141 20020417 00141 WP 2002 4 17 CALA0200202 1 20020413 A 3397 WIRE DOUG DC9 DC982 3022082 WP L2 DOOR BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND L-2 DOOR EXIT LIGHT INOPERATIVE. CHECKED WIRING AT AFT DROP CEILING AND FOUND POWER WIRE BROKEN AT WIR E CONDUIT. THE POWER WIRE WAS RESPLICED. NO GROUND WIRE WAS FOUND GOING TO SIGN. CONNECTED GROUND WIRE AND OPERATIONA L CHECKS WERE GOOD IAW WDM 33-51-14. 2 L 7 2 4F A6WE 2002041700142 20020417 00142 WP 2002 4 17 CALA0200205 1 20020415 A 3350 RPS1B CHARGER DOUG DC9 DC982 3022082 WP CABIN FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 18835 49439 THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 5-12 WERE FOUND INOPERATIVE DURING S CHECK INSPECTION. TROUBLESHOOTING IAW WD M 33-51-14 FOUND THE BATTERY CHARGER AT FAULT. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 2002041700143 20020417 00143 SO 2002 4 17 CHQ000143 1 20020412 A 3320 LIGHT EMB 145 EMB145 3260210 SO CABIN DEFECTIVE A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 280 145381 SIDEWALL LIGHT AT SEAT 1A STARTED SMOKING WHEN TURNED ON, SMELL OF SMOKE WAS OBVIOUS IN THE CABIN. REMOVED AND REPLACED SIDEWALL LIGHT SEAT 1A TURNED ON SIDEWALL LIGHT SW (F/A ATT PANEL) AND PLACED SHED BUS IN OVRD TO TEST SIDEWALL LIGHT A T SEAT 1A WORKS PROPERLY, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2002041700146 20020417 00146 EU 2002 4 17 DHL2002365005 1 20020413 A 5270 SWITCH AIRBUS 300 A300B4203 3930306 EU CARGO DOOR DIRTY A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 365DH 149 DOORS MWP LIGHT AND CHIMED, PERFORMED ABNORMAL PROCEDURES. NO OTHER IRREGULARITIES. CLEANED CONTACTS OF SWITCH BULK PI T DOOR, OPS CHECK OK ACCORDING TO M/M 52-32-1. 2 L 7 2 4F RT A35EU 2002041700147 20020417 00147 EU 2002 4 17 DHL2002365006 1 20020413 A 5270 SWITCH AIRBUS 300 A300B4203 3930306 EU L1 DOOR INTERMITTENT A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 365DH 149 DURING CRUISE FLT, DOORS ON MWP ILLUMINATED WITH SSC. COMPLETED ABNORMAL NO OTHER INDICATIONS. FOUND SWITCH 7WS ON L1 ENTRY DOOR INTERMITTENT. REPLACED SWITCH, OPS CHECK GOOD PER MM 52-71-11. 2 L 7 2 4F RT A35EU 2002041700148 20020417 00148 2002 4 17 COMA0260252 4 20020413 A 3440 6229302003 RADAR CNDAIR CL600 CL6002B19 1900309 EA NOSE CONE MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 951CA 8905 7091 FLIGHT 5463 RADAR FAULT MESSAGE.REPLACED RTA-844 2 L 7 2 4F RT A21EA 2002041900066 20020419 00066 NM 2002 4 19 F3LA200200127 1 20020411 A 2550 PANEL BOEING 737 7373L9 1384470 NM CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 3415 24569 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT RT TRANSITION PANEL FROM STA 767 TO 727. FABRI CATED AND INSTALLED REPLACEMENT PANEL PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002041700149 20020417 00149 EA 2002 4 17 COMA0260253 1 20020414 A 3350 59465 CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 447CA 7552 FLIGHT 5504 FORWARD 1/3 OF EMERGENCY FLOOR PATH LIGHTING IS INOP.REPLACED FLOOR LIGHTING CONNECTOR CABLE. 2 L 7 2 4F RT A21EA 2002041900099 20020419 00099 NM 2002 4 19 F3LA200200128 1 20020411 A 1430 NUT PLATE BOEING 737 7373L9 1384470 NM FLOORBEAM CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 3415 24569 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON NUT PLATES OF FLOORBEAM AT STA 344, LBL 10. REPAIRED DAMAGE PER SRM 53-00-51. 2 L 7 2 4F RT A16WE 2002041700150 20020417 00150 NM 2002 4 17 2002UALA00661 1 20020409 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 LH EXTERIOR SKIN STA 2205 FORWARD AND BELOW #5 LH MED SKIN HAD SHARP DEN MARK SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCO MPLISHED. CUT OUT DAMAGE, REMOVED EXISTING FASTENERS, INSTALLED DOUBLER. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041700151 20020417 00151 NM 2002 4 17 2002UALA00666 1 20020410 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EEL LIGHT MISSING AT 49C. SUPPLEMENTAL DATA UPDATE REPLACED EEL STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041700152 20020417 00152 NM 2002 4 17 2002UALA00667 1 20020410 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EEL LIGHT INOP AT 4A AFT. SUPPLEMENTAL DATA UPDATE REPLACED EEL STRIP 2 L 7 4 4F 4 F RT A20WE E24NE 2002041700153 20020417 00153 NM 2002 4 17 2002UALA00668 1 20020410 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT INOP, DOOR 4L FORWARD SILL SUPPLEMENTAL DATA UPDATE RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2002041700154 20020417 00154 NM 2002 4 17 2002UALA00669 1 20020410 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT INOP. 13B CEILING AND 17B CEILING. SUPPLEMENTAL DATA UPDATE RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2002041700155 20020417 00155 NM 2002 4 17 2002UALA00670 1 20020410 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT INOP, CEILING ADJACENT LAV 100. SUPPLEMENTAL DATA UPDATE RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2002042400117 20020424 00117 NM 2002 4 24 2002UALA00676 1 20020410 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 BS 287, RBL 14 - LBL 10, FLOORBEAM GOUGED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SECTION AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041700156 20020417 00156 NM 2002 4 17 2002UALA00678 1 20020411 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 FLOORBEAM AT STATION 365 RBL18 MATERIAL LOSS BEYOND 10 PERCENT LIMIT FORWARD EDGE. MAJOR REPAIR ACCOMPLISHEDFILLER INST ALLED AND TWO EACH ANGLES NESTED UNDER FLOORBEAM CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041700157 20020417 00157 NM 2002 4 17 2002UALA00679 1 20020411 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 FORWARD CABIN FLOORBEAM AT STATION 297 RBL 40 CORRODED. MAJOR REPAIR ACCOMPLISHED DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041700158 20020417 00158 NM 2002 4 17 DHL2002708005 1 20020415 A 2612 POWER SUPPLY BOEING 727 72725 1384006 NM FIRE DETECTION NOT SEATED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 708DH 18275 APU FIRE DETECT SYS WILL NOT TEST. RESEATED APU FIRE WARNING POWER SUPPLY. OPS GOOD IAW MM 26-15-0. 2 L 7 3 4F A3WE 2002041900100 20020419 00100 NM 2002 4 19 F3LA200200129 1 20020411 A 5320 STRAP BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 3415 24569 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOORBOARD TIE DOWN STRAP CORRODED AROUND SCREW HOLES. REPA IRED DAMAGE PER SRM 51-10-2, 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002041900102 20020419 00102 NM 2002 4 19 F3LA200200130 1 20020415 A 2550 PANEL BOEING 737 7373L9 1384470 NM CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 3415 24569 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT RT TRANSITION PANEL CORRODED FROM STA 767 TO STA 787. REPLA CED TRANSITION PANEL PER SRM 51-40-02 AND 51-30-01. 2 L 7 2 4F RT A16WE 2002041700159 20020417 00159 EA 2002 4 17 COMA0260254 1 20020414 A 2150 NH1033230350 COUPLING CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP DISCONNECTED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 957CA 7109 FLIGHT 5427 AIRCRAFT PRESSURIZATION FAILED ABOVE 8000RECONNECTED AIRCRAFT SUPPLY DUCTS THAT CAME DISCONNECTED AT WATER S EPERATORS. 2 L 7 2 4F RT A21EA 2002041700160 20020417 00160 EA 2002 4 17 COMA0260255 1 20020414 A 2750 860D10018AB FCU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 926CA 6485 7027 FLIGHT 5797 FLAPS FAIL MESSAGE, FLAPS STUCK AT 20 DEGREES.REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2002041700161 20020417 00161 EA 2002 4 17 COMA0260256 1 20020414 A 2910 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS CL CLIMB 1 SO 01 924CA 19916 7026 FLIGHT 5928 GEAR DISAGREE WARNING DURING EXTENSION AND RETRACTION.REPLACED THE SYSTEM 3 HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A21EA 2002041700162 20020417 00162 NM 2002 4 17 02040701 1 20020414 A 3397 WIRE BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E4 54555 NE SHORTED A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 506 24771 Emergency Interior light at seat 5D INOP. T/S identified wire shorted to ground. Repaired short, replaced fuse, ops chec k good as per m/m 33-51-11 2 L 7 2 4F 4 F RT A2NM E12EU 2002041700163 20020417 00163 EA 2002 4 17 COMA0260257 1 20020415 A 3150 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 971CA 7145 FLIGHT 5848 T/O CONFIG WARNING - T/O ABORTED.COULD NOT DUPLICATE ALL SYSTEMS CHECK NORMAL. 2 L 7 2 4F RT A21EA 2002041700164 20020417 00164 EA 2002 4 17 COMA0260258 1 20020415 A 3230 750006000 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS CL CLIMB 1 SO 01 708CA 9246 7235 FLIGHT 5890 GEAR DISAGREE WARNING.COULD NOT DUPLICATE. REPLACED THE NLG SELECTOR VALVE FOR TROUBLE SHOOTING. 2 L 7 2 4F RT A21EA 2002041700165 20020417 00165 NM 2002 4 17 DHL2002745003 1 20020412 A 2612 CONNECTOR BOEING 727 727224 1384076 NM NR 3 ENGINE CONTAMINATED A DHLA K NONE N FALSE WARNING CR CRUISE 1 SO 01 745DH 20665 NR 3 ENGINE DETECTOR FIRE CIRCUIT GRD LIGHT ILLUMINATED DURING CRUISE. DURING DESCENT WITH THRUST LEVERS IDLE THE LIGHT WENT OUT. WHEN PARKED THE LIGHT ILLUMINATED. FOUND AFT LOOP CONNECTOR ON NR 3 ENG OIL SOAKED. ELECTRICAL CONNECTOR C LEANED. FIRE DETECTION SYST FUNCTIONED PER MM 26-11-00 WITH NO FAULTS. 2 L 7 3 4F A3WE 2002041700166 20020417 00166 NM 2002 4 17 DHL2002745004 1 20020413 A 2612 CLAMP BOEING 727 727224 1384076 NM FIRE LOOP OUT OF POSITION A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 745DH 20665 NR 3 ENG DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. REPOSITIONED INSULATING CLAMP AT RAM AIR DUCT ON NR 3 ENGINE LOWER FIRE SENSOR. OPS NORMAL. TEST OK. 2 L 7 3 4F A3WE 2002041700167 20020417 00167 WP 2002 4 17 DHL2002801009 1 20020416 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING PREFLIGHT BATTERY CHECK. CHARGE BATTERY PACK AND OPS CHECKED OK M/M 25-60- 0. 2 L 7 4 4F RT 4A25 2002041700168 20020417 00168 WP 2002 4 17 DHL2002803006 1 20020414 A 3260 PROXIMITY SWITCH DOUG DC8 DC873 302199C WP RT MLG DOOR FAILED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 803DH 46123 DOOR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. RIGHT MAIN GEAR DOOR ILLUMINATED. PERFORMED ABNORMAL PROCEDU RE, DOOR LIGHT STAYED ON. LIGHT EXTINGUISHED ON DESCENT. REPLACED RT DOOR PROX SWITCH IAW M/M 32-60-0, OPS CHECK NORMA L ON GROUND. 2 L 7 4 4F RT 4A25 2002052000137 20020520 00137 CE 2002 5 20 GLBA2002048 1 20020411 A 2150 12938000111 SENSOR BEECH 1900 1900D 1154162 CE A/C BAY FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 151GL 16247 UE151 LEFT & RIGHT ENVIRONMENTAL FAILURE. REPLACED TEMP SENSOR. 2 L 7 2 4T RT A24CE 2002041700169 20020417 00169 EA 2002 4 17 COMA0260259 1 20020416 A 2710 601R130002 HINGE FITTING CNDAIR CL600 CL6002B19 1900309 EA WING STA 343 OVERSIZED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 739CA 7917 7273 THE R/H AILERON HAS A SLIGHTLY OVERSIZE HOLE IN THE INBOARD HINGE FITTING AT STA 343.FABRICATED AN OVERSIZE BUSHING I/A/ W WVAC EO 601R-57-3130 AND INSTALLED BUSHING I/A/W CRJ AMM 20-26-00910-803. 2 L 7 2 4F RT A21EA 2002041700170 20020417 00170 2002 4 17 GLBA2002050 4 20020413 A 3416 06603062008 ALTIMETER BEECH 1900 1900D 1154162 CE COCKPIT INOPERATIVE A GLBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 03 150GL 514 UE150 NR 1 ALTIMETER FAILED DURING TAXI. REPLACED, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2002041700171 20020417 00171 NM 2002 4 17 UPS02238036 1 20020404 A 5310 FLANGE BOEING 727 72731C 1384011 NM BS 1183 BLKD WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C BS 1183 BULKHEAD THE AFT FLANGE OF HOIZ. STIFFENER P/N 65-16350-240 IS WORN AT LBL 32 APPROX DUE CHAFF ING OFF HYDRAULIC PIPE FLANGE REPAIRED IAW SMRO EO 2002-015-001 UPS ENGINEERING FILE NO. 727-53-20048 2 L 7 3 4F A3WE 2002041700172 20020417 00172 NM 2002 4 17 UPS02238037 1 20020405 A 2780 WEB BOEING 727 72731C 1384011 NM #4 SLAT RIB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C SUSPECT CRACK #4 SLAT RIB I/B OF ACTUATOR ROD END CARRIED OUT WEB REPAIR IAW SRM 51-40-2 2 L 7 3 4F A3WE 2002041700173 20020417 00173 NM 2002 4 17 UPS02238048 1 20020403 A 5520 SKIN BOEING 727 72731C 1384011 NM ELEV. STA 130 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C R/H ELEVATOR SUSPECT CRACK IN ELEVATOR BEADED SKIN ELEV. STA. 130 AP PROX. REPAIR CARRIED OUT IAW SRM 51-30-2, 55-20-3, 51-40-5, 51-80-7 2 L 7 3 4F A3WE 2002041700174 20020417 00174 2002 4 17 GLBA2002051 4 20020414 A 3416 066306200 ALTIMETER BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 219GL 60 UE219 CAPTAINS ALTIMETER FLAGGED. REPLACED, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2002043000094 20020430 00094 SO 2002 4 30 LR7A02029 1 20020411 A 3350 44910 LIGHT LKHEED 382 382G 526414U SO COCKPIT INOPERATIVE A LR7A K NONE L NO TEST IN INSP/MAINT 1 AL 03 405LC 5025 DURING SCHEDULED A CHECK FLIGHT DECK LOWER EMERGENCY LIGHT FAILED FUNCTIONAL CHECK. REPLACED LIGHT ASSY. OPS CHECK GOO D IAW SMP 581 33-50. 2 H 7 4 4T A1SO 2002041700175 20020417 00175 EU 2002 4 17 MALA020243 1 20020411 A 3412 102CP2AF PROBE SAAB SF340 SF340A 7850100 EU TAT INOPERATIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 370XJ 300 SEVERAL MINUTES AFTER TAKEOFF ON FLIGHT 3076, THE OAT ANNUNCIATOR ILLUMINATED. RAN QRH, BUT OAT WAS STILL INOP. AIR RE TURN TO DTW. MAINTENANCE REMOVED AND REPLACED TAT PROBE. ALL CHECKS GOOD IAW SF 340 MM CHS 30, 34. 2 L 7 2 4T RT A52EU 2002041700176 20020417 00176 WP 2002 4 17 IXXA0200015O 1 20020416 A 3260 WARNING LIGHT DOUG DC8 DC871 302199A WP LANDING GEAR ILLUMINATED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 829BX 84929 630 45994 AFTER TAKE OFF FROM ANC, THE LANDING GEAR UPLATCH CHECK FAILED AND THE LANDING GEAR UNSAFE LIGHT ILLUMINATED. THE CREW C YCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO SEA FOR AN UNEVENTFUL LANDING. MAIN TENANCE INSPECTED THE AIRCRAFT AND VERIFIED THE GEAR DOOR LATCHES IN FLIGHT POSITION AND VERIFIED THE GEAR AND DOOR LIGH TS OPERATIVE. THE AIRCRAFT IS REMOVED FROM SERVICE AND FURTHER INVESTIGATION CONTINUES AT THIS TIME. ADDITIONAL INFORMAT ION WILL FOLLOW AS REPAIRS ARE ACCOMPLISHED. 2 L 7 4 4F 4A25 2002041700177 20020417 00177 WP 2002 4 17 MWEA020226 1 20020412 A 5713 5911280501 STRINGER DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING TANK STRINGER NR 22 HAS FASTENERS ON FORWARD AND AFT SIDE WITH LIGHT CORROSION AND BARE METAL ON TOP SIDE, LOC ATED BETWEEN STATION XRS 69 AND 91. FABRICATED AND INSTALLED REPAIR STRAP AND FILLER. 2 L 7 2 4F A6WE 2002041700178 20020417 00178 WP 2002 4 17 MWEA020227 1 20020412 A 5713 59112801 STRINGER DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING TANK STRINGER 21 HAS A SPOT OF LIGHT CORROSION ON FORWARD SIDE AT 4TH FASTENER INBOARD STATION XRS 91. FABRIC ATED AND INSTALLED REPAIR SPLICES AND REPLACEMENT STRINGER. 2 L 7 2 4F A6WE 2002041700179 20020417 00179 WP 2002 4 17 MWEA020229 1 20020412 A 5720 4911499529 CLIP DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING TANK STATION XRS 69 RIB ATTACH CLIP HAS LIGHT CORROSION ON OUTBOARD SIDE, LOCATED BETWEEN STRINGER 19 AND 20. REMOVED AND REPLACED CLIP. 2 L 7 2 4F A6WE 2002041700180 20020417 00180 WP 2002 4 17 COOSDR02072 1 20020401 A 5230 5936715501 DOOR DOUG DC9 DC981 3022081 WP CARGO DOOR DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 813US 48093 FORWARD CARGO COMPARTMENT BARRIER DOOR DELAMINATED. 2 L 7 2 4F A6WE 2002041700181 20020417 00181 WP 2002 4 17 MWEA020230 1 20020412 A 5713 591127981 STRINGER DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING TANK STRINGER 18 HAS FASTENERS ON FORWARD END AFT SIDE WITH LIGHT CORROSION AND SPOTS OF CORROSION JUST INBOAR D OF STATION XRS 91, FASTENERS ARE BETWEEN STATION XRS 69 AND 91. FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2002041700182 20020417 00182 WP 2002 4 17 COOSDR02073 1 20020401 A 5200 5926003403 SKIN DOUG DC9 DC981 3022081 WP BARRIER DOOR DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 813US 48093 MID CARGO COMPARTMENT BARRIER DOOR DELAMINATED. 2 L 7 2 4F A6WE 2002041700183 20020417 00183 WP 2002 4 17 MWEA020231 1 20020412 A 5720 4911499509 CLIP DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING TANK, RIB ATTACH CLIP OUTBOARD SIDE AT STATION XRS 69 ON BOTTOM END HAS LIGHT CORROSION, LOCATED BETWEEN STRIN GER 18 AND 19. REMOVED AND REPLACED CLIP. 2 L 7 2 4F A6WE 2002041700184 20020417 00184 WP 2002 4 17 COOSDR02075 1 20020401 A 5753 5930495503 SKIN DOUG DC9 DC981 3022081 WP TE FLAP DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 813US 48093 LEFT WING OUTBOARD FLAP, INBOARD FLAP VANE DELAMINATED. 2 L 7 2 4F A6WE 2002041700185 20020417 00185 WP 2002 4 17 MWEA020232 1 20020412 A 5720 4911499509 CLIP DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING TANK STATION XRS 69 RIB ATTACH CLIP HAS LIGHT CORROSION ON OUTBOARD SIDE, LOCATED BETWEEN STRINGERS NR 20 AND 21. REMOVED AND REPLACED CLIP. 2 L 7 2 4F A6WE 2002041700186 20020417 00186 WP 2002 4 17 COOSDR02076 1 20020401 A 5350 5936195401 TAIL CONE DOUG DC9 DC981 3022081 WP FUSELAGE DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 813US 48093 FUSELAGE TAIL CONE WITH DELAMINATION AT THE OUTER SURFACE. 2 L 7 2 4F A6WE 2002041700187 20020417 00187 WP 2002 4 17 MWEA020233 1 20020412 A 5713 591923683 STRINGER DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING TANK STRINGER 16 HAS SPOTS OF LIGHT CORROSION AND CORRODED FASTENERS ON AFT SIDE BETWEEN STATION XRS 69 AND 91 . REMOVED ANGLE, HOLES IN WING SKIN ARE DAMAGED. OVERSIZED HOLES AS REQUIRED TO CLEAN UP DAMAGE. INSTALLED REPLACEMEN T ANGLE. RECEIVED APPROVAL FOR REPAIR AND GENERATED WATCH ITEM. 2 L 7 2 4F A6WE 2002041700188 20020417 00188 WP 2002 4 17 COOSDR02077 1 20020401 A 5510 57148377 RUB STRIP DOUG DC8 DC873F 302199F WP HORIZONTAL STAB WORN W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 FUSELAGE TAIL SECTION, HORIZONTAL STABILIZER FIXED FAIRINGS (RUB PLATES) WITH WEAR IN SEVERAL PLACES. 2 L 7 4 4F RT 4A25 2002041700189 20020417 00189 WP 2002 4 17 COOSDR02078 1 20020401 A 5755 5910055524 SKIN DOUG DC9 DC982 3022082 WP SPOILER DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69803 49229 RIGHT WING, OUTBOARD FLIGHT SPOILER UPPER SURFACES DELAMINATED. 2 L 7 2 4F A6WE 2002041700190 20020417 00190 WP 2002 4 17 MWEA020234 1 20020412 A 5713 59192371 STRINGER DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING TANK STRINGER NR 12 HAS SPOTS OF LIGHT CORROSION JUST OUTBOARD OF STATION XRS 91 AND FASTENERS ON FORWARD AND AFT SIDE WITH CORROSION BETWEEN STATION XRS 91 AND 111. REMOVED FASTENERS. REMOVED CORROSION. BLENDED CORROSION FOUND ON STRINGER FORWARD FLANGE. INSTALLED REMOVED FASTENERS. 2 L 7 2 4F A6WE 2002041700191 20020417 00191 WP 2002 4 17 MWEA020235 1 20020412 A 5713 5911280502 STRINGER DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 RIGHT WING TANK STRINGER NR 22 HAS LIGHT CORROSION ON FORWARD SIDE JUST INBOARD AND OUTBOARD OF STATION XRS 69. REMOVED AND REPLACED STRINGER SECTIONS. FABRICATED AND INSTALLED SPLICE PIECES. 2 L 7 2 4F A6WE 2002041700192 20020417 00192 WP 2002 4 17 COOSDR02079 1 20020401 A 5755 5910055523 SKIN DOUG DC9 DC982 3022082 WP SPOILER DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69803 49229 RIGHT WING, INBOARD GROUND SPOILER (PN 5910055523) SKIN SURFACES DELAMINATED. 2 L 7 2 4F A6WE 2002041700193 20020417 00193 WP 2002 4 17 COOSDR02080 1 20020401 A 5753 5030495501 VANE DOUG DC9 DC982 3022082 WP TE FLAP DELAMINATED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69803 49229 LEFT WING, INBOARD FLAP NR2 VANE FLAP (PN 5930495-501) WITH DELAMINATION. 2 L 7 2 4F A6WE 2002041700197 20020417 00197 WP 2002 4 17 AALA20020220 1 20020205 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7527A 49919 TUL - FOUND DENT IN FUSE STATION 237 L18 AND L19 DENT IS .110 DEEP 2 BY 5 INCH CLASS 3 REPAIR INSTALLED AT 12686 CYCLES 5270025. REMOVED CLASS 3 'TEMP' REPAIR AND INSTALLED CLASS 1 PERMANENT REPAIR PER MD80 SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 2002041700198 20020417 00198 WP 2002 4 17 AALA20020221 1 20020204 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7527A 49919 TUL - FOUND CORROSION IN NR 4 SEAT TIE-DOWN TRACK AT STATION 237. REMOVED CORRODED TRACK SECTION. SPLICED IN NEW TRACK SECTION, STATION 200 TO 265, PER SRM 53-05-00. (M) 2 L 7 2 4F A6WE 2002041700199 20020417 00199 WP 2002 4 17 AALA20020223 1 20020209 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7527A 49919 TUL - FOUND AFT CARGO DOOR OPENING STATION 1155-1211 BEAM CORRODED. REPLACED LONGITUDINAL BEAMS AT STRIGNER 28R FROM ST ATION 1117 TO 1250. 2 L 7 2 4F A6WE 2002041700200 20020417 00200 WP 2002 4 17 AALA20020228 1 20020222 A 5347 GALLEY TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 TUL - FOUND G2 GALLEY MOUNT CORRODED. REMOVED AND REPLACED MOUNT PER AARD INTRODUCTION AND SRM 51-10-4. (M) 2 L 7 2 4F A6WE 2002041700201 20020417 00201 WP 2002 4 17 AALA20020229 1 20020222 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 TUL - FOUND WEB GOUGED AT STATION 1380. INSTALLED DOUBLER PER SRM 51-70-04. (M) 2 L 7 2 4F A6WE 2002041700202 20020417 00202 WP 2002 4 17 AALA20020230 1 20020221 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSLEAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 TUL - FOUND NR 4 SEAT TRACK INBOARD FLOORBOARD SUPPORT FLANGE HAS CORROSION FROM STATION 210 TO 248. INSTALLED SEAT TRA CK SECTION STATION 200 TO 274 PER SRM 53-05 FIG 4F SHEET 2. (M) 2 L 7 2 4F A6WE 2002041700203 20020417 00203 WP 2002 4 17 AALA20020231 1 20020221 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 TUL - FOUND WEAR ON SEAT TRACK NR 3 AT STATION 300 OUT OF LIMITS. INSTALLED PLUG IN SEAT TRACK NR 3 AT STATION 300 PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2002041700204 20020417 00204 WP 2002 4 17 AALA20020232 1 20020221 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 TUL - FOUND CRACK IN RIGHT CUSP AT STATION 1297 BETWEEN SEAT TRACKS. PER AARD 53-00-00-02 INSTALLED TRIPLER. (M) 2 L 7 2 4F A6WE 2002041700205 20020417 00205 WP 2002 4 17 AALA20020233 1 20020222 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 TUL - FOUND RIGHT CUSP CORRODED AT STATION 1201 TO 1204. INSTALLED DOUBLER PER AARD 53-00. (M) 2 L 7 2 4F A6WE 2002041700206 20020417 00206 WP 2002 4 17 AALA20020234 1 20020214 A 5610 WINDOW DOUG DC9 DC982 3022082 WP CABIN CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND LOWER FORWARD CORNER OF WINDOW PANEL CRACKED AT STATION 1175, RIGHT SIDE. DOUBLER INSTALLED PER 53-10-00-25 . (M) 2 L 7 2 4F A6WE 2002041700207 20020417 00207 WP 2002 4 17 AALA20020235 1 20020215 A 5610 WINDOW DOUG DC9 DC982 3022082 WP CABIN CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND UPPER RIGHT CORNER OF WINDOW PANEL CRACKED AT STATION 1021, RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-10-00 -25. (M) 2 L 7 2 4F A6WE 2002041700208 20020417 00208 WP 2002 4 17 AALA20020236 1 20020220 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND RIGHT SIDE BELT FRAME IS CRACKED JUST BELOW AIRSTAIR ACT AT MOUNT BRACKET. REPAIRED PER AARD 53-10-00-33 PA GE 1, 2, 3. (M) 2 L 7 2 4F A6WE 2002041700209 20020417 00209 WP 2002 4 17 AALA20020237 1 20020221 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 TUL - FOUND FRAME IS CRACKED AT GALLEY SUPPORT CHANNEL ATTACH ANGLE, FORWARD SIDE OF FRAME 1174 AT LONGERON 6L. INSTALL ED DOUBLER ON FRAME 1174 AT LONGERON 6L PER AARD/OH 53-10-00-30 PAGE 2. (M) 2 L 7 2 4F A6WE 2002041700210 20020417 00210 WP 2002 4 17 AALA20020238 1 20020215 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND CORROSION ON NR 1 SEAT TRACK BETWEEN STATION 1174 AND STATION 1309. INSTALLED NEW NR 1 SEAT TRACK BETWEEN S TATION 1174 TO STATION 1309. (M) 2 L 7 2 4F A6WE 2002041700211 20020417 00211 NM 2002 4 17 159PL0001 1 20020415 A 3350 2187D LIGHT BOEING 737 737242 1384477 NM A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Emer floor lighting bulb at row 8 broken. R&R bulb. 2 L 7 2 4F A16WE 2002041900123 20020419 00123 NM 2002 4 19 F3LA200200131 1 20020411 A 5330 SKIN BOEING 737 73736E 138443A NM FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 3461 25263 DURING C-2 CHECK, INSPECTION REPORTED DENT IN FWD FUSELAGE UNDER C-1 DOOR AT STA 450, BETWEEN STR 27R AND 26-R. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 53-00-01 FIG 210, 53-01-01 FIG 210 AND SOPM 20-40-02. 2 L 7 2 4F RT A16WE 2002041700212 20020417 00212 SO 2002 4 17 C2XA02CL100 1 20020416 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 14998 145302 CLE FLIGHT#3132 THE CREW REPORTED THE EMERGENCY EXIT LIGHT IN THE CABIN WAS INOPERATIVE.THE LIGHT WAS AT THE OVERWING EX IT.MAINTENANCE RESECURED THE LIGHT STRIP CONNECTOR AT ROW 11.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002041700213 20020417 00213 WP 2002 4 17 MWEA020240 1 20020412 A 5720 4911499529 CLIP DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING TANK STATION XRS 111 BETWEEN STRINGER 20 AND 21 HAS LIGHT CORROSION ON INBOARD SIDE. REMOVED AND REPLACED CLI P. 2 L 7 2 4F A6WE 2002041700214 20020417 00214 WP 2002 4 17 MWEA020242 1 20020412 A 5713 5911279504 STRINGER DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 RIGHT WING STRINGER NR 20 HAS LIGHT CORROSION 10 INCHES INBOARD OF STATION 69. FABRICATED AND INSTALLED REPAIR STRAP AN D FILLER. 2 L 7 2 4F A6WE 2002041700215 20020417 00215 EU 2002 4 17 QXEA0200442 1 20020221 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CASTELLATION ON AFT SIDE OF FRAME 50-2 CRACKED AT BOTH ENDS IN RADIUS BETWEEN STRINGERS 25 AND 26. REPAIRED IAW F OKKER MM 53-10-05, PAGE 601 AND SRM 53-02-13, PAGE 5, FIGURE 13. 2 L 7 2 4F RT A20EU 2002041700216 20020417 00216 2002 4 17 MWEA020262 4 20020417 A 2350 488T MICROPHONE DOUG DC9 DC932 3022066 WP COCKPIT DIRTY A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 202ME 47672 COMMUNICATIONS INTERMITTENT. -- FOUND CAPTAIN'S AND FIRST OFFICER'S MICROPHONE JACKS DIRTY. REMOVED AND REPLACED BOTH MICROPHONE JACKS IAW MM 20-50-01. 2 L 7 2 4F A6WE 2002041800001 20020418 00001 WP 2002 4 18 AALA20020239 1 20020226 A 5210 SKIN DOUG DC9 DC982 3022082 WP PAX DOOR CANNING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND OUTER SKIN OIL CANNING AT BOTTOM OF DOOR. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER ESO 80172. (M) 2 L 7 2 4F A6WE 2002041800002 20020418 00002 WP 2002 4 18 AALA20020240 1 20020225 A 5330 PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND FORWARD CARGO AREA LOWER PANEL HAS CORROSION UNDER LOWER FLANGE, ON DOOR BEAM. INSTALLED NEW LOWER PAND AND SPLICES AT LOWER FORWARD CARGO DOOR CUTOUT PER SRM 53-05, FIG 44. REPLACED FORWARD CARGO DOOR LOWER BEAM PER SRM 51-01 PAGE 1 STATION 370-426. (M) 2 L 7 2 4F A6WE 2002041800003 20020418 00003 WP 2002 4 18 AALA20020241 1 20020226 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND DAMAGE TO OUTER SKIN AT HOLD OPEN HOOK. INSTALLED DOUBLER TO DAMAGED AREA PER SRM 52-05-00. (M) 2 L 7 2 4F A6WE 2002041800004 20020418 00004 WP 2002 4 18 AALA20020243 1 20020219 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND LEFT CUSP CRACKED IN TWO PLACES BETWEEN STATION 218-237 (E58 NR 4173738). INSTALLED NEW SECTION OF CUSP LEF T SIDE BETWEEN STATION 218-237 PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002041800005 20020418 00005 WP 2002 4 18 AALA20020244 1 20020225 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSLEAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND APPROX STATION 47 ABOVE FORWARD NLG DOOR LEFT SIDE FUSELAGE SKIN IS CREASED JUST FORWARD OF FRAME. INSTALLE D DOUBLER PER AARD 53-30-00-02 AND SRM 53-01 FIG 2 SHEET 3. (M) 2 L 7 2 4F A6WE 2002041800006 20020418 00006 WP 2002 4 18 AALA20020245 1 20020225 A 5330 SKIN DOUG DC9 DC982 3022082 WP AIRSTAIR DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND LARGE DENT IN LOWER RT AFT SIDE OF AFT AIRSTAIR SKIN. INSTALLED DOUBLER PER SRM 52-01 FIG 2 SHEET 3. (M) 2 L 7 2 4F A6WE 2002041800007 20020418 00007 WP 2002 4 18 AALA20020246 1 20020228 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND CUSP LINE WEB CORRODED 20 INCHES INBOARD OF SERVICE DOOR JAMB AT STATION 200 AND FORWARD ALONG JAMB TO STATI ON 180. INSTALLED NEW SECTION OF CUSP BETWEEN STATION 160 TO STATION 200 PE SRM 53-15. (M) 2 L 7 2 4F A6WE 2002041800008 20020418 00008 WP 2002 4 18 AALA20020247 1 20020226 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND CUSP LINE WEB CORRODED UNDER AND OUTBOARD OF NR 5 SEAT TRACK. INSTALLED NEW SECTION OF CUSP UNDER SEAT TRAC K NR 5 FROM STATION 200 TO 218 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002041800009 20020418 00009 WP 2002 4 18 AALA20020248 1 20020227 A 5320 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND STATION 1401 TWO HAVE WEAR MARKS ON TOP OF BELL FRAME. INSTALLED DOUBLER PER AARD 53-10-00-14. (M) 2 L 7 2 4F A6WE 2002041800010 20020418 00010 WP 2002 4 18 AALA20020249 1 20020228 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 TUL - FOUND DENT AT FORWARD UPPER SIDE OF MID CARGO DOOR FRAME. PERFORMED REPAIR PER ESO 80559 2/21/02. (M) 2 L 7 2 4F A6WE 2002041800011 20020418 00011 WP 2002 4 18 AALA20020250 1 20020228 A 5340 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 469AA 49599 TUL - FOUND RIGHT STAB TO FUSELAGE ATTACH ANGLE CRACKED BETWEEN FASTENERS AT AFT END. REPAIRED BY INSTALLATION OF A REP AIR DOUBLER PER MD80 AARD 53-10-00-2. (M) 2 L 7 2 4F A6WE 2002041800012 20020418 00012 WP 2002 4 18 AALA20020251 1 20020227 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSLEAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 TUL - FOUND CORROSION ON VERTICAL AND HORIZONTAL LEGS OF AFT CARGO DOOR BEAM STATION 1155 TO STATION 1212. INSTALLED DO UBLER REPAIR ON AFT CARGO DOOR BEAM PER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2002041800013 20020418 00013 WP 2002 4 18 AALA20020269 1 20020227 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND CORROSION ON UNDERSIDE OF LEFT CUSP, STATION 619-627. INSTALLED DOUBLER PER AARD 53-00-00-02 AND SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2002041800015 20020418 00015 WP 2002 4 18 AALA20020271 1 20020226 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND CORROSION ON SEAT TRACK. REPLACED SEAT TRACK NR 1 FROM STATION 1174 TO 1309 PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 2002041800016 20020418 00016 WP 2002 4 18 AALA20020272 1 20020304 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND SEAT TRACK NR 2 CORRODED STATION 1199-1203. CORRODED SECTION OF NR 2 TRACK REMOVED NEW SECTION OF SEAT TRAC K INSTALLED STATION 1033-1309 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002041800017 20020418 00017 WP 2002 4 18 AALA20020273 1 20020304 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND CORROSION ON NR 1 SEAT TRACK STATION 1025. CORRODED SECTION OF NR 1 SEAT TRACK REMOVED. NEW SEAT TRACK INS TALLED STATION 936-1033 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002041800018 20020418 00018 WP 2002 4 18 AALA20020278 1 20020301 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND MID CARGO TIE DOWN TRACK GOUGED, STATION 598. REMOVED AND REPLACED WITH NEW CARGO TIE DOWN TRACK SRM 51-01 FIG 2-4. (M) 2 L 7 2 4F A6WE 2002041800019 20020418 00019 WP 2002 4 18 AALA20020279 1 20020226 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND METAL FIR BOARD/CUSP SHEET HAS DENT STATION 200-205, JUST INBOARD OF NR 2 SEAT TRACK. INSTALLED DOUBLER AAR D 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002041800020 20020418 00020 WP 2002 4 18 AALA20020280 1 20020226 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND INTERIM REPAIR ON CUSP CRACK PROPAGATING FROM LIGHTENING HOLE BETWEEN STATION 1193-1212 OUTBOARD OF NR 1 SEA T TRACK. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2002041800021 20020418 00021 WP 2002 4 18 AALA20020281 1 20020305 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND LEFT CUSP MEMBRANE BETWEEN STATIN 1079-1098 HAS CORROSION. REMOVED AND REPLACED CORRODED CUSP MEMBRANE BETW EEN STATION 1079-1098 PER SRM 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002041800022 20020418 00022 WP 2002 4 18 AALA20020282 1 20020305 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND LEFT CUSP MEMBRANE BETWEEN STATIN 1022-1079 CORRODED BOTTOM SIDE AROUND LIGHTENING HOLE. REMOVED AND REPLAC ED CORRODED CUSP MEMBRANE BETWEEN STATION 1022-1079 PER SRM 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002041800023 20020418 00023 WP 2002 4 18 AALA20020283 1 20020227 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND CORROSION ON UNDERSIDE OF LEFT CUSP STATION 678. INSTALLED DOUBLER PER AARD 53-00-00-02 AND SRM 53-01 FIG 4 . (M) 2 L 7 2 4F A6WE 2002041800024 20020418 00024 WP 2002 4 18 AALA20020285 1 20020227 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND CORROSION ON UNDERSIDE OF LEFT CUSP, STATION 522-541. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 2002041800025 20020418 00025 WP 2002 4 18 AALA20020286 1 20020225 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND CRACK IN LONGERON 4 LT STATION 160. CUT OUT CRACKED, INSTALLED NEW LONGERON SECTION AND SPLICE PER SRM 53-0 3 FIG 18, SAT 1, 4, 5, 6. (M) 2 L 7 2 4F A6WE 2002041800026 20020418 00026 WP 2002 4 18 AALA20020287 1 20020305 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND FRAME DENTED STATION 408 ABOVE LONGERON 27L. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-01-17. (M ) 2 L 7 2 4F A6WE 2002041800027 20020418 00027 WP 2002 4 18 AALA20020288 1 20020225 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND LOWER SIDE OF BELT FRAME HAS 2 GOUGES STATION 465 BELOW LONGERON 6 LEFT. INSTALLED DOUBLER PER AARD 53-10-0 0-14. (M) 2 L 7 2 4F A6WE 2002041800028 20020418 00028 WP 2002 4 18 AALA20020289 1 20020222 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND WORN SPOT ON BELL FRAME LONGERON 6L STATION 693. INSTALLED DOBLER PER AARD 53-10-00-14. (M) 2 L 7 2 4F A6WE 2002041800029 20020418 00029 WP 2002 4 18 AALA20020290 1 20020222 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - FOUND WORN AREA ON BOTTOM SIDE OF BELT FRAME STATION 522 BELOW LONGERON 6 RIGHT. INSTALLED J ANGLE PER AARD 53-10 -00-14. (M) 2 L 7 2 4F A6WE 2002041800030 20020418 00030 NM 2002 4 18 EIA2002009 1 20020202 A 5320 STIFFENER BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 MZJ-EAC - FOUND STATION 1241, BL 0, T-STIFFENER HAS CORRODED FASTENER HOLE ON RIGHT SIDE, SECOND FROM TOP. REPAIRED PER ECRA 482-57-142-2. (M) 2 L 7 4 4F A20WE 2002041800031 20020418 00031 NM 2002 4 18 EIAA2002010 1 20020202 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 MZJ-EAC - FOUND CORROSION ON INSIDE AND OUTSIDE OF OUTBOARD FLANGE OF STRINGER 2L, JUST ABOVE STATION 1560 FRAME,MAIN DE CK, UPPER LOBE. REPAIRED STRINGER SECTION WITH FABRICATED PARTS PER SRM 53-10-03, 51-10-02 AND 51-30-02. (M) 2 L 7 4 4F A20WE 2002041800032 20020418 00032 NM 2002 4 18 EIAA2002011 1 20020202 A 5320 WEB BOEING 747 747212B 1384886 NM LT MLG WW CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 SW 21 482EV 20713 MZJ-EAC - FOUND LEFT WHEEL WELL STATION 1241, LBL 2, WAS FOUND TO HAVE CORROSION ON OUTSIDE OF CENTER TANK WEB AROUND SC AVENGE PUMP OPENING. REPAIRED PER ECRA 482-57-142-2. (M) 2 L 7 4 4F A20WE 2002041800033 20020418 00033 NM 2002 4 18 EIAA2002012 1 20020202 A 5711 SPAR BOEING 747 747212B 1384886 NM LT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 MZJ-EAC - FOUND STATION 1241 REAR SPAR WEB, LEFT SIDE WAS FOUND TO HAVE 2 LOCATIONS OF CORROSION BEHIND FITTING. CORROS ION REMOVED AND REPAIRED PER SB 747-57-2263 R2, EO 57-747-1544-99A AND ECRA 482-57-141-2. (M) 2 L 7 4 4F A20WE 2002041800040 20020418 00040 EU 2002 4 18 SIMA200204201 1 20020211 A 3350 3013017 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 541AT 541 MIA - MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEATS 1A, 3A, 4A, 6A, AND 7A TO BE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE EMERGENCY LIGHT POWER SUPPLY UNIT IAW ATR MM. OPERATIONAL CHECK WA S GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002041800041 20020418 00041 EU 2002 4 18 SIMA200204203 1 20020130 A 5315 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 550LL 550 SAW - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION AROUND NUT PLATE HOLES ON FLOORBEAM 36. MAINTENANCE REPLACED F LOORBEAM 36 IAW ATR SRM 51-25-01 AND 51-15-03. (M) 2 H 7 2 4T RT A53EU 2002041800042 20020418 00042 EU 2002 4 18 SIMA200204602 1 20020215 A 3350 3013000 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 541AT 541 MIA - FLT 4999 - FORWARD LEFT EMERGENCY EXIT LIGHTS INOPERATIVE. RAI EMERGENCY POWER SUPPLY AT 43WL. (M) 2 H 7 2 4T RT A53EU 2002041800043 20020418 00043 EU 2002 4 18 SIMA200205101 1 20020218 A 5347 53375001214 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 550LL 550 SAW - DURING CPCP4 INSPECTION, CORROSION WAS FOUND ON THE FOLLOWING SEAT TRACKS, LEFT FORWARD OUTBOARD, LEFT AFT OUTBOAR D, AND LEFT AFT INBOARD. THE SEAT TRACKS WERE REMOVED AND REPLACED (P/N S53375001214, S53678001244-245, S53678001246) I AW WITH AE EO E2-53MR-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002041800044 20020418 00044 EU 2002 4 18 SIMA200205102 1 20020218 A 5315 S53672408254 FLOORBEAM AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 550LL 550 SAW - DURING CPCP4 INSPECTION, CORROSION WAS FOUND ON FLOORBEAM 39. THE FLOORBEAM WAS REMOVED AND REPLACED IAW ATR 72 S RM 51-25-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002081400158 20020814 00158 NE 2002 8 14 SIMA200207402 2 20020315 A 7320 32448716 HMU AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE NR 2 ENGINE FAULTY A SIMA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 SW 21 440AM 14653 440 DURING CLIMB-OUT, THE NR 2 ENGINE TQ FLUCTUATED UP TO 117 PERCENT. ALL OTHER PARAMETERS FOLLOWED THE TQ. THE CREW COUL D NOT CONTROL THE TQ SO ENGINE WAS SHUT DOWN IN FLIGHT. EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO AIRPORT SAF ELY WITH NO OTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE EEC, HMU, AND THE FUEL PUMP IAW ATR MM. OPE RATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2002041800045 20020418 00045 EU 2002 4 18 SIMA200207701 1 20020318 A 3350 301120 LIGHT AEROSP ATR72 ATR72212 8680945 EU PAX DOOR INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 322AC 320 MIA - FLT 4975 - CREW REPORTED THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE LIGHT ASSEMBLY IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002041800046 20020418 00046 SW 2002 4 18 ALG2002F00027 1 20020318 A 6320 23071895 GEAR ALLSN C47B BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX GALLED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 847AL 820 CAG47261 53150 CAE847121 UPON DISASSEMBLY AND INSPECTION OF GEARBOX BEARINGS AND GEARS. FOUND ROUGH SURFACE AT GEAR TEETH EDGE NEAR RADIUS OF TM GEAR, CAUSING GALLING ON PINION GEAR AND METAL CONTAMINATION. ASSURE PROPER MACHINE AND MESHING OF GEAR TEETH AT FACTO RY. 1 G 7 1 3U 3 U O H2SW E1GL 2002041800047 20020418 00047 SW 2002 4 18 ALG2002F00028 1 20020324 A 7160 206064819159 COWLING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL AIR INLET COWL CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 427AL 6737 53107 REBUILD. EXCESSIVE CORROSION, CRACKING AND WEAR ON COWLING AND INTAKE SHELF. 1 G 7 1 3U 3 U O H2SW E1GL 2002041800048 20020418 00048 SW 2002 4 18 ALG2002F00029 1 20020311 A 7160 206064819159 COWLING BELL 407 407 1182206 SW AIR INLET COWL CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 587AL 53248 REBUILD. EXCESSIVE CORROSION, CRACKING AND WEAR ON COWLING AND INTAKE SHELF. 1 G 7 1 3U O H2SW 2002041800049 20020418 00049 SW 2002 4 18 ALG2002F00030 1 20020327 A 6320 6898785 GEAR 206L3 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL M/R GEARBOX ROUGH B K NONE O OTHER IN INSP/MAINT 1 SW 03 355AL 623 CAG95020 51444 CAE890701 UPON VISUAL INSPECTION OF PARTS. T/M GEAR HAS ROUGH GEAR TEETH EDGES AT RADIUS CAUSING LIGHT GALLING ON PINION GEAR. P TO GEAR ALSO HAS ROUGH EDGES AT RADIUS. ASSURE PROPER MATERIAL, MACHINING AND MESHING OF GEAR TEETH AT FACTORY. 1 G 7 1 3U 3 U H2SW E1GL 2002041800050 20020418 00050 SW 2002 4 18 ALG2002F00031 1 20020324 A 6320 6893672 PINION GEAR ALLSN C47B BELL 407 407 1182206 SW M/R GEARBOX SPALLED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 537AL CAG47257 53230 UPON INSPECTION OF PART. SPALLING AND GALLING GEAR TEETH DUE TO ROUGH EDGES ON T/M GEAR TEETH. (PN 6893673 SN NN144757) TT 1878.2. 1 G 7 1 3U O H2SW 2002041800051 20020418 00051 SW 2002 4 18 ALG2002F00032 1 20020325 A 6320 6893673 GEAR C47B BELL 407 407 1182206 SW M/R GEARBOX DAMAGED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 537AL 1878 CAG47257 53230 UPON INSPECTION OF PARTS, FOUND ROUGH GEAR TEETH EDGES AT RADIUS, CAUSING DMAGE TO MATING GEAR TEETH. THIS IS DUE TO IM PROPER MACHING AT RADIUS. 1 G 7 1 3U O H2SW 2002041800052 20020418 00052 SW 2002 4 18 ALG2002F00033 1 20020302 A 6520 407040416101 SHAFT BELL 407 407 1182206 SW T/R GEARBOX WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 687AL 1247 53366 DURING REPAIR FOR LEAKING OUTPUT SEAL, FOUND SPLINES ON OUTPUT SHAFT WORN BELOW LIMITS, READING 1.3025, MIN 1.3035 (SHAF T SPLINES SOFTER METAL THAN TRUNNION SPLINES.) 1 G 7 1 3U O H2SW 2002041800053 20020418 00053 SW 2002 4 18 ALG2002F00034 1 20020321 A 6310 23073520 SHAFT BELL 206 206L1 1182107 SW SPUR ADAPTER WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 27545 744 45234 ENGINE MAKING METAL. WORN AFT SPLINES BELOW SPECS. 1 G 7 1 3U H2SW 2002041800054 20020418 00054 SW 2002 4 18 LSI2002F00000 1 20020204 A 2821 30325725 FILTER BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA ENGINE FUEL FAILED E LS1R K NONE O OTHER IN INSP/MAINT 1 EA 13 8530B 30702 17273 DURING MAINTENANCE OF THE ENGINE FUEL CONTROL AIR SUPPLY SYSTEM, THE P3 WAS REMOVED FOR INSPECTION AND FOUND TO BE IN TW O PIECES. THE METAL END CAPS ARE NORMALLY WELDED TO METAL SCREEN. THIS PMA FILTER WAS BONDED TOGETHER. THE BOND MATER IAL WAS SO BRITTLE FROM THE HEAT, IT JUST CRUMPLED OFF THE FILTER. PART REMOVED AND REPLACED. 1 G 7 1 4U 4 U H4SW E22EA 2002041800055 20020418 00055 2002 4 18 SDRO2002003 4 20020315 A 2211 41600298100 CONTROL HEAD UROCOP EC135 EC135P1 8680990 EU AUTOPILOT SYS FAILED E R7MA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 NM 07 135N 334 0086 PILOT REPORTED THAT 10 MINUTES INTO CRUISE FLIGHT DURING NORMAL CROSS CHECK HE NOTICED HEADING WAS STARTING TO DRIFT. P ILOT WAS UNABLE TO RESELECT AUTO PILOT HEADING. AUTO PILOT HAD FAILED. CONTROL HEAD STILL INDICATED THE AUTO PILOT WAS ENGAGED. DID NOT RECEIVE A DECOUPLE OR AUTO PILOT CAUTION ON CDS OR AP TRIM WARNING. ALL INDICATIONS WERE THAT THE AUT O PILOT WAS FUNCTIONING. CAUSE OF FAILURE WAS AN INTERNAL RESISTOR IN THE CONTROL HEAD (AMPS 2100) HAD DISLODGED AND WA S ROLLING FREE INSIDE OF THE UNIT. 1 G 7 2 3U O H88EU 2002041800072 20020418 00072 WP 2002 4 18 MWEA020236 1 20020412 A 5720 4912532505 CLIP DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 REMOVED LEFT WING RIB ATTACH CLIP BETWEEN STRINGERS 17 AND 18 AT STATION XRS 91 TO FACILITATE OTHER MAINTENANCE. CORROS ION FOUND ON CLIP. INSTALLED REPLACEMENT CLIP. 2 L 7 2 4F A6WE 2002041800073 20020418 00073 WP 2002 4 18 MWEA020239 1 20020412 A 5720 4911499529 CLIP DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING TANK STATION XRS 111, BOTTOM CLIP BETWEEN STRINGER 19 AND 20 HAS LIGHT CORROSION ON INBOARD SIDE. REMOVED AND REPLACED CLIP. 2 L 7 2 4F A6WE 2002041800074 20020418 00074 WP 2002 4 18 MWEA020241 1 20020412 A 5720 4911499581 CLIP DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING STATION 111 STRINGER 20 THROUGH 21 OUTBOARD CLIP REMOVED TO FACILITATE OTHER MAINTENANCE. REMOVED AND REPLACE D CLIP. 2 L 7 2 4F A6WE 2002041800075 20020418 00075 WP 2002 4 18 MWEA020243 1 20020412 A 5713 5911279504 STRINGER DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 STRINGER NR 20 IN RIGHT WING HAS LIGHT CORROSION 9 INCHES OUTBOARD OF STATION XRS 69. FABRICATED AND INSTALLED REPAIR S TRAP AND FILLER. 2 L 7 2 4F A6WE 2002041800076 20020418 00076 WP 2002 4 18 MWEA020244 1 20020412 A 5713 5911279502 STRINGER DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 RIGHT WING STRINGER 19 HAS LIGHT CORROSION 9 INCHES INBOARD OF STATION XRS 69. FABRICATED AND INSTALLED REPAIR STRAP. 2 L 7 2 4F A6WE 2002041800077 20020418 00077 WP 2002 4 18 MWEA020245 1 20020412 A 5720 4911499510 CLIP DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 RIGHT WING STATION XRS 69 CLIP BETWEEN STRINGER 20 TO 21 HAS LIGHT CORROSION. REMOVED AND REPLACED CLIP. 2 L 7 2 4F A6WE 2002041800078 20020418 00078 WP 2002 4 18 MWEA020246 1 20020412 A 5720 4911499582 CLIP DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 RIGHT WING STATION XRS 69 CLIP BETWEEN STRINGER 18 TO 19 HAS LIGHT CORROSION. REMOVED AND REPLACED CLIP. 2 L 7 2 4F A6WE 2002041800079 20020418 00079 WP 2002 4 18 MWEA020247 1 20020412 A 5713 59112802 STRINGER DOUG DC9 DC932 3022066 WP RT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 RIGHT WING STRINGER 21 HAS CORROSION PRESENT ON FORWARD LOWER LEG FROM XRS 69 THROUGH 91. FOUND CRACKS ON STRINGER. RE MOVED AND REPLACED SECTION OF STRINGER. INSTALLED REPAIR SPLICES. 2 L 7 2 4F A6WE 2002041800080 20020418 00080 WP 2002 4 18 MWEA020253 1 20020415 A 5230 3926046503N STOP FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FORWARD CORGO COMPARTMENT DOOR HAS A CRACKED STOP FITTING ANGLE (FORWARD BOTTOM STOP-DOOR INTERIOR). REMOVED AND REPLAC ED NEW FITTING. 2 L 7 2 4F A6WE 2002041800081 20020418 00081 WP 2002 4 18 MWEA020256 1 20020415 A 5310 9957828503 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 GALLEY DOOR JAMB LOWER FORWARD AND AFT CORNER AREAS HAVE ANGLES WITH CORROSION. FABRICATED AND INSTALLED GALLEY DOOR LO WER JAMB TO THRESHOLD. 2 L 7 2 4F A6WE 2002041800082 20020418 00082 2002 4 18 MWEA020258 4 20020411 A 3415 WARNING SYSTEM DOUG DC9 DC932 3022066 WP COCKPIT OUT OF ADJUST A MWEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 216ME 47740 OVERSPEED WARNING SOUNDED. REJECTED TAKEOFF AT LESS THAN 20 KTS. DEFERRED OVERSPEED WARNING. PERFORMED ADJUSTMENT/TES T OF OVERSPEED WARNING SYSTEM. REF MM 34-10-5. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 2002041800083 20020418 00083 2002 4 18 MWEA020259 4 20020412 A 3415 B070610003 SENSOR DOUG DC9 DC932 3022066 WP OVERSPEED SYS FAULTY A MWEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 216ME 47740 THE OVERSPEED WARNING WENT OFF. REJECTED TAKEOFF. REMOVED AND REPLACED OVERSPEED SENSOR, OPS CHECK OK. 2 L 7 2 4F A6WE 2002041800084 20020418 00084 NE 2002 4 18 NACA20020015 2 20020413 A 8530 356994 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE NR 1 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 99330 725 725 43576 P31669 FEATHERED THE NR 1 ENGINE AT 2318Z DUE TO RUNNING ROUGH AND BACKFIRING. REMOVED AND REPLACED THE NR 13 CYLINDER ON THE NR 1 ENGINE. 2 L 7 4 4R 4 R 6A3 5E8 2002041800085 20020418 00085 WP 2002 4 18 P2EA2002M024 1 20020414 A 3610 DUCT DOUG DC9 DC981 3022081 WP A/C BAY CLOGGED A P2EA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 814US 48094 TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED AFTER TAKEOFF OUT OF LAX. INSPECTED TAIL COMPARTMENT, FOUND THE LEFT HAND SENSOR OFF AND THE DUCT TO CHECK VALVE CLOGGED WITH DEBRIS. SECURED THE LEFT HAND SENSOR AND CLEANED DUCT. OPS CHECKED , ALL PARAMETERS NORMAL PER ENGINE RUN AND MM 36-20-02. 2 L 7 2 4F A6WE 2002041800086 20020418 00086 NM 2002 4 18 PCAA0204046 1 20020412 A 2597 WIRE DHAV DHC8 DHC8102 2809003 NM GALLEY CHAFED A PCAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 13 805EX 228 LGA-FLIGHT 3862. IN FLIGHT, FLIGHT ATTENDANT NOTICED A HOT SMELL COMING FROM THE GALLEY AREA (SPECIFICALLY THE HOT JUGS ). PULLED THE HOT JUG CIRCUIT BREAKER AND THE SMELL WENT AWAY. MAINTENANCE INSPECTED THE RECEPTACLES AND WIRING. DISC OVERED THAT THE NR 2 HOT JUG HAD CHAFED WIRES. CIRCUIT BREAKER WAS PULLED AND BANDED AND DEFERRAL ISSUED. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002041800087 20020418 00087 NM 2002 4 18 PCAA0204047 1 20020412 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 830EX 155 DURING ROUTINE MAINTENANCE VISIT A CRACK WAS DISCOVERED IN AFT EQUIPMENT BAY (APU AREA) AT FRAME NR 4 RIGHT SIDE. CRACK WAS REPAIRED IN NR 4 FRAME IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING. REPAIR FABRICATED AND INSTALLED PER RD8-55-1 99. EDDY CURRENT INSPECTION FOR ADDITIONAL CRACKS COMPLETED AND NO CRACKS WERE FOUND. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002041800088 20020418 00088 EU 2002 4 18 QXEA0200440 1 20020221 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACK IN FRAME 50-2 ATTACH FLANGE AT CUTOUT FOR STRINGER 26. REPAIRED IAW FOKKER MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2002041800089 20020418 00089 EU 2002 4 18 QXEA0200441 1 20020224 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - FOUR CRACKS IN CUTOUT OF CASTELLATION ON BACKSIDE OF FRAME 41-2 ABOVE STRINGER 29. REPAIRED IAW FOKKER SRM 53-02- 13, PAGE 8. 2 L 7 2 4F RT A20EU 2002041800090 20020418 00090 EU 2002 4 18 QXEA0200443 1 20020221 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACKED CASTELLATION BELOW STRINGER 25 ON AFT SIDE OF FRAME 50-2. REPAIRED IAW FOKKER MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 2002041800091 20020418 00091 EU 2002 4 18 QXEA0200444 1 20020220 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - DENT IN AFT FUSELAGE SKIN AFT OF FRAME 41-2 BETWEEN STRINGER 3 AND 5. REPAIRED IAW SRM 53-02-02, PAGE 2, FIGURE 1 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002041800092 20020418 00092 EU 2002 4 18 QXEA0200445 1 20020222 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACK IN REAR PRESSURE BULKHEAD AT BEAM 6 LOWER FLANGE. REPAIRED IAW HORIZON AIR EA 4-53-1564/A. 2 L 7 2 4F RT A20EU 2002041800093 20020418 00093 EU 2002 4 18 QXEA0200446 1 20020221 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - LT INBOARD SEAT TRACK, INBOARD FLANGE HAS CHAFE FROM FLOORBOARD JUST FORWARD OF CAMLOCK RECEPTACLE AT FRAME 14755. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 2002041800094 20020418 00094 EU 2002 4 18 QXEA0200447 1 20020222 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACKED NESTING ANGLE IN FLOOR SUPPORT ON OUTBOARD SIDE OF INBOARD SEAT TRACK, JUST AFT OF FRAME 8770. REPAIRED I AW FOKKER SRM 53-15-05, PAGE 60, FIGURE 16, SRM 53-02-18, PAGE 3, FIGURE 1 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002041800095 20020418 00095 EU 2002 4 18 QXEA0200448 1 20020222 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACKED NESTING ANGLE IN FLOOR SUPPORT ON INBOARD SIDE OF OUTBOARD SEAT TRACK, JUST AFT OF FRAME 8770. REPAIRED I AW FOKKER SRM 53-02-18, PAGE 3, FIGURE 1, SRM 53-15-02, PAGE 32, FIGURE 11 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002041800096 20020418 00096 EU 2002 4 18 QXEA0200449 1 20020221 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - PROFILE AND SKIN CHAFED AT RIGHT WING TO FUSELAGE FAIRING BY PANEL 92N. REPAIRED IAW FOKKER SRM 51-00-00. 2 L 7 2 4F RT A20EU 2002041800097 20020418 00097 EU 2002 4 18 QXEA0200450 1 20020222 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT CEILING AT FRAME 13815A AND 13815B, STRINGER 42 HAS SMALL CRACK GOING FROM HOLE IN STRINGER FOR INSULATION TO H OLD IN PLACE. REPAIRED IAW FOKKER SRM 51-10-4, SRM 53-02-01, PAGE 8, FIGURE 6 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002041800098 20020418 00098 EU 2002 4 18 QXEA0200451 1 20020216 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT OUTBOARD SEAT TRACK FROM FRAME 8805 FORWARD ABOUT 12 INCHES INBOARD FLANGE HAS PITTING AND CORROSION. REPAIRED IAW HORIZON AIR EA 4-53-1569. 2 L 7 2 4F RT A20EU 2002041800099 20020418 00099 EU 2002 4 18 QXEA0200452 1 20020223 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - RT SIDE EXTERIOR EMPENNAGE SKIN HAS A DENT BELOW V-STAB CONNECTION ANGLE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3 AND HORIZON AIR EA 4-53-1572. 2 L 7 2 4F RT A20EU 2002041800100 20020418 00100 EU 2002 4 18 QXEA0200458 1 20020222 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CRACK IN DOUBLER SKIN BETWEEN RIVETS ABOVE LT MAIN LANDING GEAR STRUT. REPAIRED IAW HORIZON AIR EA 4-57-578. 2 L 7 2 4F RT A20EU 2002041800101 20020418 00101 EU 2002 4 18 QXEA0200459 1 20020220 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - CORROSION ON FRAME 6805 ABOVE STRINGER 1 AT THE NUT PLATES. REPAIRED IAW FOKKER MM 53-00-2, PAGE 601, FIGURE 2, S TEPS 1-4 AND MM 53-00-2, PAGES 601-603, FIGURE 2, STEPS 5 AND 6. 2 L 7 2 4F RT A20EU 2002041800102 20020418 00102 NM 2002 4 18 QXEA0200460 1 20020307 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - FUSELAGE SKIN IS DENTED OUT AT X477.0 AND Z100.0. REPAIRED IAW DHC-8 RD 8-53-2181. 2 H 7 2 4T RT A13NM 2002041800103 20020418 00103 NM 2002 4 18 QXEA0200461 1 20020307 A 5730 SEAL DHAV DHC8 DHC8202 2809007 NM LT WING FAIRING DETERIORATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - LT WING ROOT FAIRING HAS DETERIORATED FILLET SEAL AND LOOSE RIVET AT X427.0 AND Z152.0. REPAIRED IAW 51-40-11. 2 H 7 2 4T RT A13NM 2002041800104 20020418 00104 NM 2002 4 18 QXEA0200462 1 20020301 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - CHAFE DAMAGE, TOP OF RT OUTBOARD FLAP, 18 INCHES FROM TRAILING EDGE OF FLAP, YW173.0. REPAIRED IAW RD 8-57-1734 A ND RD 8-57-1549. 2 H 7 2 4T RT A13NM 2002041800105 20020418 00105 NM 2002 4 18 QXEA0200463 1 20020228 A 5310 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - STRUCTURE IS DAMAGED AT TOP AFT DOOR STOP. REPAIRED IAW RD 8-53-5461 AND DHC-8 SRM 51-20-26 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2002041800106 20020418 00106 NM 2002 4 18 QXEA0200464 1 20020228 A 5230 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - CARGO DOOR STRUCTURE AT TOP FORWARD DOOR STOP IS DAMAGED. REPAIRED IAW RD 8-53-5461 AND DHC-8 SRM 51-20-26, SRM 5 1-20-51. 2 H 7 2 4T RT A13NM 2002041800107 20020418 00107 NM 2002 4 18 QXEA0200465 1 20020305 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - TURTLE BACK AREA FORWARD OF FRONT SPAR, BRACKET THAT SUPPORTS INBOARD END OF LT BLACK BLEED AIR DUCT IS CRACKED AT YW17.55L. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002041800108 20020418 00108 NM 2002 4 18 QXEA0200466 1 20020301 A 5420 BRACKET DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX- LEFT HAND NACELLE LOWER FINGERNAIL DECK SUPPORT BRACKETS ARE CRACKED AT TWO LOCATIONS. REPAIRED IAW DHC-8 RD 8-54- 310. 2 H 7 2 4T RT A13NM 2002041800109 20020418 00109 NM 2002 4 18 QXEA0200467 1 20020305 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX- TURTLE BACK AREA FORWARD OF FRONT SPARS BOTTOM BRACKET THAT SUPPORTS INBOARD END OF RT BLACK BLEED AIR DUCT IS CRAC KED. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002041800110 20020418 00110 NM 2002 4 18 QXEA0200468 1 20020301 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX- TURTLE BACK AREA FORWARD OF FRONT SPAR WEB JUST FORWARD OF CENTER BLEED AIR T-DUCT IS CHAFED THROUGH. REPAIRED IAW DHC-8 RD 8-53-5437. 2 H 7 2 4T RT A13NM 2002041800111 20020418 00111 NM 2002 4 18 QXEA0200469 1 20020305 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - LT WING NR 4 FLAP TRACK INBOARD FLAT SIDE ON TOP ROLLER HAS PITTING ON BEAM. REPAIRED IAW HORIZON AIR EA 2-57-151 . 2 H 7 2 4T RT A13NM 2002041800112 20020418 00112 NM 2002 4 18 QXEA0200470 1 20020228 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - AFT BELLY SKIN HAS OUTWARD DENT 12 INCHES LEFT OF CENTERLINE AND 4 INCHES FORWARD OF STATION 531.500. REPAIRED IA W RD 8-53-2181, PAGE 3, ITEM 1. 2 H 7 2 4T RT A13NM 2002041800114 20020418 00114 NM 2002 4 18 QXEA0200481 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - WEAR IN RT INBOARD SEAT TRACK FROM STATION 515.75 TO 518.25. REPAIRED IAW DHC-8 SRM 51-20-36, PARAGRAPH F, STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002041800115 20020418 00115 NM 2002 4 18 QXEA0200482 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - GOUGE IN LT INBOARD SEAT TRACK AT STATION 541.0. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAPH F, STEPS 1 AN D 2. 2 H 7 2 4T RT A13NM 2002041800116 20020418 00116 NM 2002 4 18 QXEA0200483 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GROOVED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - GROVES WORN INTO LT INBOARD SEAT TRACK FROM STATION 502.0 TO 516.75. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PAR AGRAPH F, STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002062000012 20020620 00012 EU 2002 6 20 02FDEA00250 1 20020411 A 7711 LINE AIRBUS 310 A310 EU NR 1 ENGINE KINKED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 447FE 251 NR 1 THROTTLE SPLIT 12 DEG TA MORE THAN NR 2, NR 1 NACELLE TEMP 35-45 DEG HOTTER THAN NR 2. REMOVED AND REPLACED PT2/TT 2 SENSOR AND THE TT2 SENSOR. REMOVED AND REPLACED KINKED PT7 LINE AND RESEALED 1, 2, 3, 12, 13, 14 AND 16 FUEL NOZZLE P AD AIR LEAKS ALL ON NR 1 ENGINE. 2 L 7 2 4F RT A35EU 2002042400088 20020424 00088 NM 2002 4 24 02FDEA00256 1 20020413 A 5315 BAC1518338 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND HOLES IN FLOORBEAM BS 440, RBL 60-65, WL 208. REMOVED AND REPLACED FLOORBEAM PER EA 7-5335-54192 & SRM 53-10-8 FI G 3. 2 L 7 3 4F A3WE 2002042400095 20020424 00095 NM 2002 4 24 02FDEA00262 1 20020415 A 5315 FLOORBEAM BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 207FE 22929 CORROSION ON LWR LONG FLOORBEAM UNDER NUT PLATES FROM BS 1030 TO 1160, WL 200, LBL 2-RBL 2. REMOVED AND REPLACED FLOORB EAM PER SRM 51-30-5, 51-20-1, 51-30-2 & BAC 1506-1706. 2 L 7 3 4F A3WE 2002041800120 20020418 00120 EA 2002 4 18 COMA0260262 1 20020416 A 5270 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 959CA 7116 FLIGHT 5904 AVIONICS BAY DOOR CAUTION MESSAGE.DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2002041800121 20020418 00121 EA 2002 4 18 COMA0260263 1 20020416 A 2721 601R5122623 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT BROKEN A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 809CA 7366 FLIGHT 5674 RUDDER TRIM CONTROL IS BROKEN.REPLACED TRIM CONTROL PANEL. 2 L 7 2 4F RT A21EA 2002041800122 20020418 00122 NM 2002 4 18 QXEA0200638 1 20020416 A 3260 BRACKET BOMBDR DHC8 DHC8401 NM BROKEN A QXEA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 09 413QX 4060 HLN - NOSE LANDING GEAR DOORS REMAIN OPEN AFTER EXTENSION WITH 3 GREEN DOWN LOCKED LIGHTS. ALTERNATE GEAR EXTENSION LIGH TS SHOW 2 MAIN GEAR DOWN AND LOCKED AND NO NOSE GEAR DOWN AND LOCKED LIGHT. REPLACED RIGHT-HAND NOSE GEAR DOWN LOCK SENS OR BRACKET. COMPLIED WITH RIGGING OF PROX SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002041800123 20020418 00123 EA 2002 4 18 COMA0260264 1 20020416 A 3150 WEU CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 427CA 7460 FLIGHT 5910 T/O ABORTED AT 95 KTS.C/W RTO INSPECTION 2 L 7 2 4F RT A21EA 2002041800128 20020418 00128 2002 4 18 SWAA020796 4 20020415 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 365SW 26576 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002041800129 20020418 00129 NM 2002 4 18 SWAA020799 1 20020416 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 606SW 27926 LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002041800130 20020418 00130 NM 2002 4 18 SWAA020800 1 20020416 A 5330 6545776 SKIN BOEING 737 7372K6 1364440 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 937, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002041800131 20020418 00131 NM 2002 4 18 SWAA020801 1 20020415 A 5313 6935365 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L AND 15L. REMOVED AND REPLACED SHEAR TIE PE R SRM. 2 L 7 2 4F RT A16WE 2002041800132 20020418 00132 NM 2002 4 18 SWAA020803 1 20020415 A 7720 D3302 CONNECTOR BOEING 737 7373H4 1384600 NM NR 1 ENG ERRATIC A SWAA D E RETURN TO BLOCK ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 SW 07 394SW 27380 AIR TURNBACK, ENG SHUTDOWN, DECLARED EMERGENCY ON TAKEOFF NR 1 ENG EGT INDICATED 1290 DEGREES, COULD NOT STABILIZE ENG, SHUT ENG DOWN. DISCREPANCY WAS DETERMINNED TO BE AN INDICATION PROBLEM. REMOVED AND REPLACED ENG EGT WIRE CONNECTOR PE R MM. 2 L 7 2 4F RT A16WE 2002041800133 20020418 00133 NM 2002 4 18 SWAA020791 1 20020415 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL WEB CRACKED AT BS 178, WL 220 AT RBL 17.1. REMOVED AND REPLACED VERTICAL WEB PER SRM. 2 L 7 2 4F RT A16WE 2002041800134 20020418 00134 NM 2002 4 18 SWAA020792 1 20020415 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002041800135 20020418 00135 NM 2002 4 18 SWAA020794 1 20020415 A 5313 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE'S CRACKED (2 EA) AT BS 360, ABOVE AND BELOW STR 14L. REMOVED AND REPLAC ED SHEAR TIE'S PER SRM. 2 L 7 2 4F RT A16WE 2002041800136 20020418 00136 EU 2002 4 18 CX7A194J5 1 20020416 A 2910 AE7064588 HYDRAULIC LINE SAAB SF340 340B 7860101 EU HYD SYSTEM FAILED A CX7A B A EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 03 307CE 340B204 HYD FLUID LOST. MAIN PRESSURE WENT TO ZERO. HYD LIGHT ILLUMINATED. EMER LANDING GEAR EXTENSION PER CHECK LIST. LANDED WI THOUT INCIDENT. 2 L 7 2 4T RT A52EU 2002041800137 20020418 00137 EA 2002 4 18 SWIA200210780 1 20020415 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA RIGHT SIDE BROKEN A SWIA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 NM 07 597SW 7293 RIGHT SIDE WINDSHIELD SHATTERED INFLIGHT. DIVERTED TO CPR. REMOVED AND REPLACED FIRST OFFICER'S WINDSHIELD IAW MM 56-1 1-01. OPS AND LEAK CHECK GOOD. PN ON NP139321-10 SN OFF 99147H8942. 2 L 7 2 4F RT A21EA 2002041800145 20020418 00145 NM 2002 4 18 2002UALA00646 1 20020405 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 AFT CABIN STATION 947 FLOORBEAM RBL 24 TO RBL 47 HAD CORROSION ON UPPER CAP WITH EXCESSIVE MATERIAL REMOVED DURING CORRO SION REMOVAL. MAJOR REPAIR ACCOMPLISHED. INSTALLED 2 REPAIR ANGLES. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041800146 20020418 00146 NM 2002 4 18 2002UALA00647 1 20020406 A 5720 STIFFENER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE WINGROOT CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 931UA 26656 NR 1 FUEL TANK AT WINGROOT, 20 INCHES AFT OF FORWARD SPAR, LOWER STIFFENER HAS DEEP WEAR ON UPPER SURFACE OF LOWER FLANG E DUE TO CHAFING OF FUEL LINE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041800147 20020418 00147 NM 2002 4 18 2002UALA00648 1 20020406 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 CABIN STATION 294.5 FRAME HAS EXCESSIVE MATERIAL LOSS AT STRINGER 10L CUTOUT. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041800148 20020418 00148 NM 2002 4 18 2002UALA00649 1 20020408 A 5330 BEAR STRAP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 931UA 26656 AFT CARGO DOOR CUTOUT AFT EDGE BEAR STRAP HAS TWO AREAS OF EXCESSIVE MATERIAL LOSS DUE TO DAMAGE BLEND OUT. MAJOR REPAI R ACCOMPLISHED. INSTALLED DOUBLER TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041800149 20020418 00149 NM 2002 4 18 2002UALA00650 1 20020407 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 FORWARD PIT FRAME LOWER CHORD AT BODY STATION 500 LEFT HAND IS DENTED BETWEEN STRINGER 29L AND 30L. MAJOR REPAIR ACCOMP LISHED. FABRICATED AND REPLACED FRAME CHORD. 2 L 7 2 4F 4 F RT A1NM E24NE 2002041800150 20020418 00150 NM 2002 4 18 2002UALA00651 1 20020407 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 CABIN FLOOR BEAM UPPER CHORD STATION 1640 LBL 56 HAS EXCESSIVE MATERIAL REMOVED. MAJOR REPAIR ACCOMPLISHED. FLOORBEAM UPPER CHORD AFT FLANGE REPAIRED AND STRAP INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041800151 20020418 00151 NM 2002 4 18 2002UALA00652 1 20020407 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 FORWARD PIT STATION 684, RBL 16, FLOOR SUPPORT ANGLE CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT ANGLE . 2 L 7 2 4F 4 F RT A2NM E17NE 2002041800152 20020418 00152 NM 2002 4 18 2002UALA00653 1 20020408 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 931UA 26656 AFT CABIN FLOORBEAM AT STATION 946 RBL 20 HAS EXCESSIVE MATERIAL LOSS DUE TO CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISH ED. INSTALLED REINFORCEMENT ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041800153 20020418 00153 NM 2002 4 18 2002UALA00654 1 20020408 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 AFT PIT FRAME DENTED STATION 727B AT STRINGER 25L. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCEMENT ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041800154 20020418 00154 NM 2002 4 18 2002UALA00655 1 20020408 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 LEFT HAND FORWARD CABIN, STRINGER 10L CRACKED AT STATION 297. MAJOR REPAIR ACCOMPLISHED. REPLACED WITH NEW STRINGER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041800155 20020418 00155 NM 2002 4 18 2002UALA00656 1 20020409 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 STATION 787 FRAME HAS DENT ON TOP FLANGE BETWEEN STRINGER 23R AND 24R. MAJOR REPAIR ACCOMPLISHED. EXTENDED A SPLICE PL ATE AND INSTALLED FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050200072 20020502 00072 NM 2002 5 2 2002UALA00657 1 20020408 A 3350 FUSE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE POWER PACK BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 834UA 1420 SEATS 12C, 13C, 16C, 17C & 20C ESCAPE PATH LIGHTING INOPERATIVE. REPLACED FUSE ON POWER PACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2002041800156 20020418 00156 NM 2002 4 18 2002UALA00658 1 20020409 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 CABIN FLOORBEAM HAD CORROSION MATERIAL REMOVED EXCEEDS LIMITS, STATION 345 RBL 52 UPPER FLANGE AFT SIDE. MAJOR REPAIR A CCOMPLISHED. UPPER CAP REPAIRED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041800157 20020418 00157 NM 2002 4 18 373PA0003 1 20020416 A 3350 LIGHT BOEING 737 7373Y0 1384671 NM A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 Three emergency floor exit lights inop. R&R light assy.'s 2 L 7 2 4F RT A16WE 2002041800158 20020418 00158 NM 2002 4 18 SABA020053 1 20020418 A 3350 1306 BULB DHAV DHC8 DHC8103 1386005 NM CABIN BURNED OUT A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 881CC 294 Aircraft 881 on flight 5012 from CLT to TLH. During preflight inspection the floor emergency light at row 8 would not t est. Maintenance removed and replaced the bulb. Ops check was good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002041800159 20020418 00159 NM 2002 4 18 CALA0200210 1 20020416 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM STA 986.5-1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND AFT O/B CHANNEL OF WEB CORRODED AT STA 986.5-1006, LBL 38. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002041800160 20020418 00160 NM 2002 4 18 CALA0200211 1 20020416 A 5320 MOUNT BOEING 737 7373T0 1384582 NM STA 1012 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND AFT O/B LAV MOUNT CORRODED AT STA 1012, LBL 38. THE LAV MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-02 . 2 L 7 2 4F RT A16WE 2002041800161 20020418 00161 NM 2002 4 18 CALA0200212 1 20020417 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 500C CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND A 1/2" CRACK IN STRINGER 16L JUST FORWARD OF WING ILLUMINATION LIGHT HOUSING AT STA 500C. A NEW STRINGE R WAS INSTALLED IAW SRM 53-30-03 AND 53-00-03. 2 L 7 2 4F RT A16WE 2002041800162 20020418 00162 WP 2002 4 18 CALA0200213 1 20020417 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FS 218-256 SPLIT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND CHANNEL ON BACK OF MAIN CABIN DECK FLOOR PANEL AT FS 218-256, RBL 44-58, COMING LOOSE AND PANEL WAS SPL ITTING AT THE END. THE PANEL AND CHANNEL WERE REPAIRED IAW SRM 51-70-2 AND 51-20-1. 2 L 7 2 4F A6WE 2002041800163 20020418 00163 WP 2002 4 18 CALA0200214 1 20020417 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 1510 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND FUSELAGE SKIN GOUGED UNDER R/H RAIN GUTTER AT FS 1510. THE GUTTER WAS REMOVED AND A DOUBLER WAS INSTALL ED IAW SRM 51-10-2, 51-30-2, AND 51-20-1. 2 L 7 2 4F A6WE 2002041800164 20020418 00164 NM 2002 4 18 CALA0200215 1 20020417 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND CENTER STRINGER ON LOWER FLOOR SIDE OF AFT PRESSURE BULKHEAD AT STA 1016 CORRODED ON LOWER END. THE STR INGER WAS REPAIRED IAW SRM 51-70-11, PAGE 1-6. 2 L 7 2 4F RT A16WE 2002041800165 20020418 00165 NM 2002 4 18 2002UALA00682 1 20020408 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 172UA 24363 EEL LIGHTS INOP, ROW 22 TO 26, RIGHT SIDE. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041800166 20020418 00166 NM 2002 4 18 02FDEA00248 1 20020416 A 3230 656021123 ACCESSORY UNIT BOEING 727 727233 138408A NM E&E COMPARTMENT FAILED A FDEA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 25 283FE 22350 02-92 LAND GEAR W/N RETRACT AFTER TAKEOFF, LG LATCH CIRCUIT BREAKER POPPED AND WOULD NOT RESET. R&R LG ACCESSORY UNIT P ER MM 32-09-121. OPS CK NORM. 2 L 7 3 4F RT A3WE 2002041800167 20020418 00167 CE 2002 4 18 GLBA2002052 1 20020415 A 7700 503890571 TACH GENERATOR BEECH 1900 1900D 1154162 CE LEFT N1 INTERMITTENT A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 249GL 296 UE249 LEFT N1 FLUXUATION, REPLACED TAC GEN OPS CHECKED SATISFACTORY 2 L 7 2 4T RT A24CE 2002041900014 20020419 00014 SW 2002 4 19 AC2A0000337 1 20020219 A 2120 RING ASSEMBLY BELL 430 430 1182150 SW ALLSN 250C 250C* GL GASPER LOOSE E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CV 1158 49072 GUIDE RINGS SNAP LOOSE PREVENTING PROPER OPERATION. SPRING RING LOSES TENSION PREVENTING PROPER OPERATION. REMOVE AND REPLACED. 1 G 7 2 3U 3 U RT H9SW E4CE 2002041900016 20020419 00016 SW 2002 4 19 AC2A0000339 1 20020407 A 6220 BEARING BELL 430 430 1182150 SW ALLSN 250C 250C* GL P/C LINK FAILED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CH 49037 REPLACED BEARINGS IN P/C LINKS. 1 G 7 2 3U 3 U RT H9SW E4CE 2002041900019 20020419 00019 SW 2002 4 19 AC2A0000342 1 20020221 A 2520 222020742133 CUSHION BELL 430 430 1182150 SW ALLSN 250C 250C* GL PAX SEAT BROKEN E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CV 488 49072 ENERGY ABSORBING MATERIAL BROKEN. REPLACED WITH NEW SERVICEABLE SEAT. 1 G 7 2 3U 3 U RT H9SW E4CE 2002041900020 20020419 00020 2002 4 19 AC2A0000343 4 20020313 A 3421 430375002107 DISPLAY BELL 430 430 1182150 SW ALLSN 250C 250C* GL COCKPIT FAILED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CH 995 49037 HSI SCREEN BLANK. HSI CIRCUIT BREAKER POPPED. REPLACED WITH NEW EFIS AND IT CORRECTED PROBLEM. 1 G 7 2 3U 3 U RT H9SW E4CE 2002041900021 20020419 00021 SW 2002 4 19 AC2A0000344 1 20020319 A 2497 D38999 CONNECTOR BELL 430 430 1182150 SW ELECTRICAL BROKEN E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CT 27 49089 CONNECTOR P16, PIN (G) LOCK BROKEN. REPACED CONNECTOR AND IT CORRECTED PROBLEM. 1 G 7 2 3U RT H9SW 2002041900022 20020419 00022 SW 2002 4 19 AC2A0000345 1 20020319 A 2797 D38999 CONNECTOR BELL 430 430 1182150 SW ELECTRICAL INOPERATIVE E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CT 49089 REMOVED AND REPLACED CONNECTOR. 1 G 7 2 3U RT H9SW 2002041900023 20020419 00023 NE 2002 4 19 CW12002F00001 1 20020401 A 5400 7630207593102 CABLE SKRSKY S76 S76B 8143007 NE PWA PT6 PT6* 52043 EA COWLING BROKEN B CW1R K NONE O OTHER IN INSP/MAINT 1 EA 11 780P 760359 UPON CLOSING THE LEFT TOP ENGINE COWLING, WHEN THE CABLE WAS ACTUATED TO CLOSE THE COWLING THE END ENGAGING PIN BROKE. THE COWLING WAS NOT SECURED PROPERLY. THE COWLING CABLE BROKE AT THE THREADED END WHERE THE ENGAGEMENT PIN SCREWS ON. 1 G 7 2 4U 3 T H1NE E2NE 2002041900028 20020419 00028 CE 2002 4 19 KNF2002F00000 1 20020327 A 3246 800X6 TIRE CESSNA 207 T207A 2073614 CE CONT O520 TSIO520* 17040 SO RT MLG FAILED E KNFA K NONE O OTHER IN INSP/MAINT 1 WP 19 3156X 20700376 RIGHT MAIN TIRE BLEW OUT ON LANDING. TIRE HAD SURFACE TREAD AND WAS NOT WORN. A FLAT SPOT WAS NOTED WHERE THE BLOWOUT OCCURED. BRAKES WERE APPLIED BEFORE AIRCRAFT TOUCHED DOWN. PILOT NEEDS TO KEEP FEET OFF THE BRAKES UNTIL THE AIRCRAFT HAS LANDED. 1 H 7 1 3O 3 O A16CE E8CE 2002041900029 20020419 00029 CE 2002 4 19 PAZ2002F00001 1 20020402 A 2822 57181061 WIRE CESSNA 441 441 2076020 CE RT BOOST PUMP CHAFED B PAZR K NONE O OTHER IN INSP/MAINT 1 CE 03 441CJ 7403 4410117 FOUND WIRING TO RIGHT AUXILIARY BOOST PUMP CHAFING ON BOOST PUMP HOUSING AND DAMAGING THE INSULATION OF THE WIRING. FAB RICATE A SHEATH FOR THE WIRE BUNDLE TO PROTECT IT FROM CHAFFING DAMAGE. 1 L 7 2 3T RT A28CE 2002041900033 20020419 00033 NM 2002 4 19 DHL2002743004 1 20020418 A 3150 SWITCH BOEING 727 727225 1384077 NM A DHLA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 743DH 22438 1) ON T/O CREW EXPERIENCED A TAKEOFF WARNING HORN. RESET AIRCRAFT CONFIG ATTEMPTED ANOTHER T/O SAME HORN. RETURNED TO CV G RAMP.2) R/R UPPER TAKEOFF, TAKEOFF WARNING SWITCH ON STABILIZER, OPS CHECKS SERVICABLE IAW B-727 M/M 31-26-00. 2 L 7 3 4F A3WE 2002042400108 20020424 00108 NM 2002 4 24 2002UALA00659 1 20020408 A 2920 27802227 RAM AIR TURB BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE HYD SYSTEM FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 799UA 17867 26926 DURING OPERATIONAL TEST OF THE RAM AIR TURBINE DURING ROUTINE MAINTENANCE CHECK, THE RAM AIR TURBINE (RAT) FAILED TO PRO DUCE THE REQUIRED VOLTAGE. FAILURE OF THE RAM AIR TURBINE GENERATOR. THE RAM AIR TURBINE ASSEMBLY, WHICH INCLUDES THE GENERATOR, WAS REPLACED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002041900034 20020419 00034 NM 2002 4 19 2002UALA00662 1 20020408 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 172UA 24363 EEL LIGHTS INOP F-C SEATS 1J AND 4J, AFT LIGHTS. REPLACED LIGHT ASSEMBLIES. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900035 20020419 00035 NM 2002 4 19 2002UALA00663 1 20020410 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 AFT PIT FLOOR SUPPORT STATION 1340 TO STATION 1440 RBL 3 IS CRACKED AND CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041900036 20020419 00036 NM 2002 4 19 2002UALA00664 1 20020410 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 EXTERIOR FUSELAGE DENTED AT BS 800, STR 25R, RBL 64. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER AND F ILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041900037 20020419 00037 NM 2002 4 19 2002UALA00665 1 20020410 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 RIGHT HAND CABIN BODY STATION 520 STRINGER 16R2 FRAME CHORD PUNCTURED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTA LLED NEW ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041900038 20020419 00038 NM 2002 4 19 2002UALA00671 1 20020410 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 AFT PIT FRAME LT SIDE AT STA 1520 ABOVE STRINGER 26L IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED TRIPLER REPAIR TO FRAME AT STA 1520, STRINGER 26L. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041900039 20020419 00039 NM 2002 4 19 2002UALA00672 1 20020410 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 CAB FLOOR CREASE BEAM INNER CHORD UPPER FLANGE BETWEEN STATION 1580 TO 1600, RBL 44, IS CORRODED. MAJOR REPAIR ACCOMPLI SHED. DOUBLER REPAIR WAS PERFORMED ON CREASE BEAM AT STATION 1580 TO 1600, RBL 44. 2 L 7 2 4F 4 F RT A2NM E17NE 2002041900040 20020419 00040 NM 2002 4 19 2002UALA00673 1 20020411 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 CABIN CREASE BEAM INBOARD CHORD VERTICAL LEG CORRODED STATION 900 TO 1040, LBL 64. MAJOR REPAIR ACCOMPLISHED. INSTALLE D DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002042400112 20020424 00112 NM 2002 4 24 2002UALA00674 1 20020410 A 5320 BEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 STA 852-856 LBL 33 TRANSBEAM UPPER FLANGE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SECTION AND SP LICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002042400114 20020424 00114 NM 2002 4 24 2002UALA00675 1 20020410 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 STA 830 LBL 11 UPPER CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SECTION AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002042400118 20020424 00118 NM 2002 4 24 2002UALA00677 1 20020411 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 933UA 26659 LEFT HAND UPPER FUSELAGE SKIN BELOW CABIN WINDOW AT STATION 390 WAS BLENDED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002041900041 20020419 00041 NM 2002 4 19 2002UALA00680 1 20020410 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 775UA 26947 EMERGENCY EEL LIGHT INOP AT SEAT ROWS NR 1E AND NR 2F. REPLACED EEL STRIPS AT 1E & 2F. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002041900042 20020419 00042 NM 2002 4 19 2002UALA00681 1 20020408 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 172UA 24363 EMERGENCY LIGHT INOP. AFT GALLEY LEFT WALL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900043 20020419 00043 NM 2002 4 19 CALA0200216 1 20020418 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND FLOORBEAM T-CAP CORRODED AT FASTENER HOLES, STA 344. REPAIRED IAW SRM 51-10-51. 2 L 7 2 4F RT A16WE 2002041900044 20020419 00044 NM 2002 4 19 CALA0200217 1 20020418 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 559-578 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND A 3" CRACK IN WEB AT R/H SIDEWALL FLOOR BETWEEN STA 559 AND 578. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002041900045 20020419 00045 WP 2002 4 19 CALA0200218 1 20020419 A 5313 LONGERON DOUG DC9 DC983 3022083 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 49525 INSPECTION FOUND A 1.25" CRACK IN LONGERON 2L AFT OF BELTFRAME STA 1418. THE CRACKED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION AND SPLICE WERE INSTALLED IAW SRM 53-02, FIGURE 17. 2 L 7 2 4F RT A6WE 2002041900046 20020419 00046 NM 2002 4 19 2002UALA00683 1 20020408 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 172UA 24363 EMERGENCY LIGHTS DIM, DOOR 3 RT EXIT AND EELS 32 TO 34 RIGHT SIDE. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900047 20020419 00047 NM 2002 4 19 2002UALA00684 1 20020408 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 172UA 24363 EEL LIGHT INOP, 4E AFT. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900048 20020419 00048 NM 2002 4 19 2002UALA00685 1 20020408 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 172UA 24363 EMERGENCY LIGHT INOP, DOOR 2 LEFT FORWARD SILL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900049 20020419 00049 NM 2002 4 19 2002UALA00686 1 20020411 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EEL LIGHT BROKEN, 5F AFT. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900050 20020419 00050 NM 2002 4 19 2002UALA00687 1 20020411 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 OUTSIDE EMERGENCY LIGHT INOP, AFT LEFT HAND BULB. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900051 20020419 00051 NM 2002 4 19 2002UALA00688 1 20020411 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EEL STRIP AT SEATS 49ABC INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900052 20020419 00052 NM 2002 4 19 2002UALA00689 1 20020411 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 CEILING EEL INOP ON CENTER AFT UPPER DECK DROP DOWN PANEL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900053 20020419 00053 NM 2002 4 19 2002UALA00690 1 20020409 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 RIGHT WING OVERWING EMERGENCY EXIT LIGHTS INOP AT 4 POSITIONS. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900054 20020419 00054 NM 2002 4 19 2002UALA00691 1 20020409 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EEL LIGHT INOP, 7ABC AFT. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900055 20020419 00055 NM 2002 4 19 2002UALA00692 1 20020409 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY LIGHTS INOP, DOOR 3 RIGHT SILL AND OVER DOOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900056 20020419 00056 NM 2002 4 19 2002UALA00693 1 20020409 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EEL LIGHT INOP 34C. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900057 20020419 00057 NM 2002 4 19 2002UALA00694 1 20020409 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY LIGHT INOP, CEILING 32C. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900058 20020419 00058 NM 2002 4 19 2002UALA00695 1 20020409 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY LIGHT INOP, OVER DOOR 5 LEFT. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900059 20020419 00059 NM 2002 4 19 2002UALA00696 1 20020409 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 OVERHEAD EMERGENCY LIGHT ROW 16 INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002041900060 20020419 00060 NM 2002 4 19 ABXA010819 1 20020412 A 3234 257T110320 MODULE BOEING 767 767231 1385131 NM COCKPIT MALFUNCTIONED A ABXA O OTHER J WARNING INDICATION DE DESCENT 1 GL 23 707AX 384 22570 EICAS MESSAGE GEAR DISAGREE DISPLAYED AND GEAR AMBER LIGHT ILLUMINATED WITH GREEN DOWN LIGHTS ILLUMINATING. ACCOMPLISHE D ABNORMAL PROCEDURE. ON FINAL, GPWS GAVE TOO LOUD GEAR WARNING. ACCOMPLISHED GO AROUND. WHEN GEAR EXTENDED AGAIN, IN DICATIONS WERE NORMAL. REMOVED AND REPLACED THE LANDING GEAR LEVER MODULE IAW B767 AMM 32-31-01-4. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2002041900063 20020419 00063 NM 2002 4 19 DHL2002715005 1 20020413 A 2612 69295671 WARNING HORN BOEING 727 727155C 138404Z NM NLG WW FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 715DH 19618 DURING APU FIRE WARNING TEST, FIRE BELL AND FIRE WARNING HORN FAIL SOUND. REMOVED AND REPLACED FIRE WARNING HORN IN NOS E WHEEL WELL IAW MM 26-11-00. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002041900064 20020419 00064 WP 2002 4 19 DHL2002802002 1 20020323 A 5320 STRUCTURE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 DURING INSPECTION FOUND A CRACK AT FUSELAGE STA 1760 1.25 INCH IN LENGTH. INSTALLED REPAIR PER SRM 53-2-1 ITEM 16. 2 L 7 4 4F RT 4A25 2002041900067 20020419 00067 NM 2002 4 19 EIA2002005 1 20020130 A 5714 SPAR BOEING 747 747212B 1384886 NM CENTER WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 MZJ - FOUND CORROSION ON REAR SPAR WEB OF WING CENTER SECTION BS 1241 BULKHEAD FITTING. CORROSION REMOVED AND WORK ACCO MPLISHED PER SB 747-57-2263/EO 57--747-1544-99 (A). 2 L 7 4 4F A20WE 2002041900068 20020419 00068 NM 2002 4 19 EIA2002006 1 20020202 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 MZJ - FOUND C-CHECK, FOUND 6 INCH CRACK IN FRAME AT STATION 1760 BELOW AND INBOARD OF STRINGER 39L TIE CLIP. FABRICATED AND INSTALLED CLIP, STRAP AND DOUBLER PER ECRA 482-53-146-2. (M) 2 L 7 4 4F A20WE 2002041900069 20020419 00069 NM 2002 4 19 02FDEA00267 1 20020417 A 3260 UPLOCK SWITCH BOEING 727 7272S2F 1384O81 NM NLG FAULTY A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 206FE 22928 NOSE GEAR RED LIGHT ILLUM WITH GEAR HANDLE IN UP POS. REMOVED AND REPLACED NOSE GEAR LOCK SW PER MM 32-61-071-4. CLEAN ED GEAR HANDLE CONTACT PRECAUTIONARY. 2 L 7 3 4F A3WE 2002041900070 20020419 00070 NM 2002 4 19 EIA2002007 1 20020202 A 5310 STRUCTURE BOEING 747 747212B 1384886 NM APU BAY CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 MZJ - FOUND EXFOLIATION CORROSION AT STATION 1241 RBL 2, UNDER DOUBLER FOR APU SHROUD LINE. REPAIRED CORROSION AREA PER ECRA 482-53-147-2. (M) 2 L 7 4 4F A20WE 2002041900071 20020419 00071 NM 2002 4 19 EIA2002016 1 20020202 A 5320 WEB BOEING 747 747212B 1384886 NM LT MLG WW CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 MZJ-EAC - DURING C-CHECK, FOUND CORROSION ON THE LEFT WHEEL WELL CANTED WEB. REPAIRED PER ECRA 482-53-144-2. (M) 2 L 7 4 4F A20WE 2002041900072 20020419 00072 NM 2002 4 19 02FDEA00268 1 20020417 A 3310 RHEOSTAT DOUG MD11 MD11F 3023600 NM COCKPIT FAULTY A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 623FE 48794 AT CR SMELLED HOT INSULATION ODOR. DISCOVERED POPPED C/B FOR OVERHEAD SWITCH PANEL. MX FOUND OVERHEAD LIGHT RHEOSTAT T RANSFORMER TO BE PRIMARY CAUSE OF ODOR. 2 L 7 3 4F RT A22WE 2002041900073 20020419 00073 NM 2002 4 19 EIA2002018 1 20020202 A 5714 STRUCTURE BOEING 747 747212B 1384886 NM CENTER WING TANK CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 MZJ-EAC - FOUND CORROSION AT STATION 1238, RBL 2, ON CENTER WING TANK SKIN. REPAIRED PER ECRA 482-57-149-2. (M) 2 L 7 4 4F A20WE 2002041900074 20020419 00074 NM 2002 4 19 02FDEA00269 1 20020418 A 2613 DETECTOR BOEING 727 7272S2F 1384O81 NM OVERHEAT SYS MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 208FE 22930 LWR AFT BODY OVERHEAT LIGHT ILLUMINATED IN FLT. REMOVED AND REPLACED FIRE DETECTION PER MM 20-10-017-2. 2 L 7 3 4F A3WE 2002041900075 20020419 00075 NM 2002 4 19 EIAA2002008 1 20020202 A 5320 WEB BOEING 747 747212B 1384886 NM LT MLG WW CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 MZJ-EAC - LEFT WHEEL WELL, STATION 1241, LBL 19, HAS AREA OF EXFOLIATION CORROSION ON WEB. REPAIRED PER ECRA 482-57-142 -2. (M) 2 L 7 4 4F A20WE 2002050700065 20020507 00065 NM 2002 5 7 02FDEA00270 1 20020415 A 5315 FLOORBEAM BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 207FE 22929 CORROSION ON LWR LONG FLOORBEAM UNDER NUT PLATES FROM BS 1030 TO 1060, WL 200, LBL 2 TO RBL 2. *S/D* REMOVED AND REPLA CED FLOORBEAM PER SRM 51-30-5, 51-20-1 & 51-30-2. 2 L 7 3 4F A3WE 2002041900076 20020419 00076 NM 2002 4 19 EIAA2002013 1 20020202 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 MZJ-EAC - FOUND TWO CRACK DURING HFEC INSPECTION ON FRAME STRAP AT STATION 2231 BETWEEN STRINGERS 24L AND 25L. REPAIRED PER ECRA 482-53-140-2. (M) 2 L 7 4 4F A20WE 2002041900077 20020419 00077 NM 2002 4 19 EIAA2002014 1 20020202 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 SW 21 482EV 20713 MZJ-EAC - FOUND CRACK DURING HFEC INSPECTION ON FRAME STRAP AT STATION 2231 BETWEEN STRINGERS 24R AND 25R. REPAIRED PER ECRA 482-53-140-2. (M) 2 L 7 4 4F A20WE 2002041900078 20020419 00078 NM 2002 4 19 EIAA2002015 1 20020202 A 5312 BULKHEAD BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 MZJ-EAC - DURING C-CHECK, FOUND EXFOLIATION CORROSION AT STATION 1241 BULKHEAD, RBL 46, RBL 60 AND INBOARD OF FORK FITTI NG ALONG UPPER CHORD WEB IN THE RIGHT WING GEAR WHEEL WELL. REPAIRED PER ECRA 482-57-142-2 AND SRM 57-10-1. (M) 2 L 7 4 4F A20WE 2002041900079 20020419 00079 NM 2002 4 19 EIAA2002017 1 20020202 A 5312 PRESSURE PANEL BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 MZJ-EAC - FOUND CORROSION AT STATION 1245, RBL 34 ON CANTED PRESSURE DECK. REPAIRED PER ECRA 482-53-147-2. (M) 2 L 7 4 4F A20WE 2002041900080 20020419 00080 EU 2002 4 19 DHL2002367003 1 20020418 A 2611 FSD200500 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU DEFECTIVE A DHLA O OTHER N FALSE WARNING IN INSP/MAINT 1 SO 01 367DH 265 1. LEFT CABIN SMOKE DETECTOR ILLUMINATED ON GROUND WITH AURAL AND VISUAL WARNING ON MWP DURING PREFLIGHT. 2. R&R LEFT CA BIN SMOKE DETECTOR ASSY AS PER MM 26-11-00 GROUND OPS NORMAL. 2 L 7 2 4F RT A35EU 2002041900081 20020419 00081 EU 2002 4 19 DHL2002364007 1 20020416 A 2611 FSD200500 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA K NONE N FALSE WARNING UK UNKNOWN 1 SO 01 364DH 141 AFT MAIN CABIN SMOKE DETECTOR LIGHT ON. REMOVED & REPLACED NR 6 R SMOKE DETECTOR IAW MM 26-14-11. 2 L 7 2 4F RT A35EU 2002041900082 20020419 00082 EU 2002 4 19 DHL2002363003 1 20020416 A 2613 3500813 CONTROL UNIT AIRBUS 300 A300B4203 3930306 EU A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 363DH 85 1. MANIFOLD FAULT DETECT LOOPS RH SELECT B TEST FAILS. 2. DEFERRED PER MEL 36-12-03. CONTROL #9034 ASSIGNED. 3. REPLACE D #2 OVERHEAT DETECTION CONTROL UNIT IAW M/M 26-16-11. OPS CK GOOD. THIS CLEARS DMI 9034. 2 L 7 2 4F RT A35EU 2002041900083 20020419 00083 CE 2002 4 19 2002F00408 1 20020417 A 2140 CONNECTOR LEAR 35 35A 5170602 CE DEFOG BLOWER MELTED E K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 17 66NJ 11982 000205 296 CONNECTOR ON AUX DEFOG BLOWER MELTED AND INSULATION ON WIRE AT CONNECTOR MELTED. THIS DEFOG BLOWER WAS INSTALLED UNDER STC SA1482SO REV B. THIS IS THE 4TH BLOWER ASSY WHERE THE CONNECTOR HAS MELTED. MANUFACTURED BY FLIGHT ENGINEERING AND DEVELOPMENT. 2 L 7 2 4F A10CE 2002041900084 20020419 00084 2002 4 19 AT0200048 4 20020410 A 2565 SLIDE DOUG DC9 DC932 3022066 WP R1 DOOR OUT OF POSITION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 R1 DOOR SLIDE OFF. REINSTALLED R1 DOOR SLIDE PACK. 2 L 7 2 4F A6WE 2002041900085 20020419 00085 WP 2002 4 19 MEX2002046 1 20020221 A 3241 392492 CONTROL VALVE DOUG DC9 DC987 3022087 WP MLG ANTI-SKID FAILED A ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 214AM 7627 110 49585 HMO-LAS - WHEN LANDING GEAR GOT DOWN, ANTI-SKID IGHTS TURNED ON. AS CONSEQUENCE OF SPARE PARTS MISSING, AN AIRCRAFT CHA NGE TOOK PLACE. LEFT ANTI-SKID DUAL CONTROL VALVE WAS REPLACED IAW MM 32-43-02, TESTS WERE PERFORMED OK. 2 L 7 2 4F RT A6WE 2002041900086 20020419 00086 SO 2002 4 19 C2XA02BT014 1 20020417 A 3350 66361 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16918 145397 BTV---CO3218, DURING SERVICE/ROUTINE INSPECTION FOUND EMERGENCY AISLE PATH LIGHTING AT ROWS THREE AND FOUR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLOOR STRIP LIGHT AT ROWS THREE AND FOUR IAW EMB145 AMM 33-50-12. OPS CHECK ED GOOD. 2 L 7 2 4T RT T00011AT 2002041900087 20020419 00087 SO 2002 4 19 C2XA02BT015 1 20020417 A 3350 B6245305 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19966 145131 BTV---CO3389, DURING ROUTINE INSPECTION MAINTENANCE FOUND THE EMERGENCY LIGHT IN THE SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT ASSEMBLY IAW EMB145 MM 33-50-09. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2002041900088 20020419 00088 NM 2002 4 19 CALA0200208 1 20020416 A 5320 SPLICE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND A 1 INCH CRACK IN STRINGER SPLICE AT STA 907, S4L. A NEW SPLICE WAS INSTALLED IAW SRM 51-40-00. 2 L 7 2 4F RT A16WE 2002041900089 20020419 00089 WP 2002 4 19 MEX2002047 1 20020222 A 2781 SWITCH DOUG DC9 DC983 3022083 WP SLAT POSITION FAILED A ASMF H DEACTIVATE SYST/CIRCUITS N FALSE WARNING TX TAXI/GRND HDL 1 SW 23 838AM 49397 FLT 411 - MIA-CUN - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF LIGHT DISAGREE SLAT TURNED ON. ON REVISION IT WAS F OUND STALL FAILURE LIGHT, TURN ON TOO. PERFORMED BITE TO BOTH COMPUTERS, FAIL ON VANE NR 1, CONNECTOR WAS CLEANED, AND A BITE TO PROXIMITY SWITCH WAS PERFORMED. DURING TRANSIT CHECK IN CUN THERE WAS TROUBLES WITH WING/TAIL ANTI-ICE RUPTOR . THERE WAS A SHORT-CIRCUIT IN THE WIRE BUNDLE NEAR THE VENTRAL STAIR. AGAIN AIRCRAFT RETURNED BY LIGHT DISAGREE SLAT TURNED ON. IT WAS REPLACED SWITCH SLAT POSITION S1-467 IAW MM 27-80-07. (M) 2 L 7 2 4F RT A6WE 2002041900090 20020419 00090 NM 2002 4 19 2002316001 1 20020419 A 2550 119100 PDU BOEING 767 767300 1385204 NM Zone 200 INOPERATIVE A FWTA O OTHER O OTHER IN INSP/MAINT 1 SO 19 316LA Inoperative cargo loading power drive units Since 1-12-02 thru 4-6-02 FWTA has experienced 23 failures of these units. T hese units are new as the aircraft has a TAT 1502 and TAC 478Failed units have part numbers of 19100-1 and 19100-3. Unit s removed for inop, broken brackets, will not run, frozen, and no power. 2 L 7 2 4F RT A1NM 2002041900091 20020419 00091 NM 2002 4 19 CALA0200209 1 20020416 A 5551 FITTING BOEING 737 7373T0 1384582 NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND RT HORIZONTAL STABILIZER FORWARD UPPER LUG CORRODED. THE CORROSION WAS REMOVED FROM LUG IAW SRM 55-10- 10. 2 L 7 2 4F RT A16WE 2002041900092 20020419 00092 EA 2002 4 19 COMA0260260 1 20020417 A 5720 601R10045 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 783CA 6473 7315 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 540AB. REPAIRED IAW 601R-57-21-030 AND REO 601R-57-21-183. 2 L 7 2 4F RT A21EA 2002041900093 20020419 00093 EA 2002 4 19 COMA0260261 1 20020417 A 5720 601R10045 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 783CA 6473 7315 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 540CB. REPAIRED IAW 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002041900094 20020419 00094 NM 2002 4 19 DHL2002747002 1 20020418 A 7920 O-RING BOEING 727 727224 1384076 NM OIL FILTER CAP DAMAGED A DHLA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 747DH 22253 NR 3 OIL QUANTITY SLOWLY DECREASING, WORKED ABNORMAL PROCEDURE. QUANTITY FELL BELOW 0 GALLONS, LOW OIL PRESSURE LIGHT I LLUMINATED AND OIL PRESSURE GAUGE WENT TO 0 PSI. PERFORMED IN FLIGHT ENGINE SHUTDOWN PROCEDURE. FOUND MAIN OIL FILTER CAP LEAKING. REMOVED AND REPLACED O-RING, LEAK CK GOOD IAW MM 20-10-11, 79-20-0 & JHR 5.2 2 L 7 3 4F A3WE 2002041900095 20020419 00095 WP 2002 4 19 MEX2002048 1 20020222 A 2420 947F9463 GCU DOUG DC9 DC987 3022087 WP AC GENERATOR FAILED A ASMF O OTHER H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 SW 23 803ML 7894 49726 FLT 603 - DFW-MEX - AC CROSS TIE LIGHT TURN OFF, THERE WAS NOT A CROSS FEED AND APU O/S. CIRCUIT BREAKER OF GCU, GENERA TION AND INTERCHANGE WAS RESET AND AIRCRAFT WAS DISPATCHED BY MEL WITH APU O/S. DURING TRANSIT CHECK IN MEX IT WAS REPL ACED THE GCU OF THE APU, HOWEVER CROSSFEED WAS NOT POSSIBLE. REPORT DEFERRED BY MEL 24-3 CAT 'C'. LATER WAS REPLACED T HE BCU IAW MM 24-20-05. AT RON MEX 22/23 SEVERAL TESTS WERE PERFORMED IAW 24-20-08 AND 24-20-07. (M) 2 L 7 2 4F RT A6WE 2002041900096 20020419 00096 WP 2002 4 19 DHL2002802003 1 20020412 A 5330 SKIN DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 FOUND CRACK 1.5 INCH BETWEEN STRINGER 17 AND 18 AT STA 1740 ABOVE TAB, FRONT SPAR, RT SIDE OF A/C. INSTALLED REPAIR PER SRM 53-2-1 ITEM 16-2. 2 L 7 4 4F RT 4A25 2002041900098 20020419 00098 2002 4 19 MEX2002051 4 20020225 A 2200 4034241972 CONTROL UNIT DOUG DC9 DC987 3022087 WP E/E COMPT FAILED A ASMF B EMER. DESCENT J G WARNING INDICATION MULTIPLE FAILURE CR CRUISE 1 SW 23 803ML 61522 3028 49726 FLT 608 - MEX-DFW - AIRCRAFT STOPPED OVER IN MTY AS CONSEQUENCES OF AUTOMATIC THROTTLES, AUTO PILOT AND FLIGHT DIRECTORS FAIL, REPORTS ARE DEFERRABLES, HOWEVER PILOT ASKED THEIR CORRECTION. BOTH DFGC WERE REPLACED IAW MM 22-01-01. (M) 2 L 7 2 4F RT A6WE 2002041900101 20020419 00101 2002 4 19 MEX2002053 4 20020226 A 3421 4034241973 CONTROLLER DOUG DC9 DC987 3022087 WP E/E COMPT FAILED A ASMF O OTHER G MULTIPLE FAILURE CR CRUISE 1 SW 23 803ML 6102 6102 49726 FLT 584 - CUN-MEX - DURING FLIGHT THERE WAS 25 DEGREE DIFFERENCE IN HDG RDI OF PILOT AND ALSO ATS 1, AUTO PILOT AND FMA O;S, BOTH DFGC CONFIRMED FAIL IN ATT 1 AND 2, HDG 1 AND 2 AND COMPASS CONTROLLER 1 AND 2. THERE WAS AN INFORMATION LOS T IN DFGC 2. BOTH C/B OF AHRS WERE RESET, AND AIRCRAFT WAS DISPATCHED. DURING FLIGHT, CREW REPORTED THE FAIL AGAIN. A T RON MEX 26/27 THE AHRU 1, DFGC 2 AND COMPASS CONTROLLER 2 WERE REPLACED IAW 34-21-10, 22-01-01 AND 34-21-13. AN RTS W AS PERFORMED, COMPUTERS OK IAW MM 22-01-05. (M) 2 L 7 2 4F RT A6WE 2002041900103 20020419 00103 NM 2002 4 19 MEX2002055 1 20020203 A 3350 LIGHT DOUG MD80 MD83 3023681 NM CABIN INOPERATIVE A ASMF K NONE L NO TEST IN INSP/MAINT 1 SW 23 861LF 49826 FLT 112 - GDL-TIJ - DURING PREFLIGHT TESTS, AN EMERGENCY LIGHTS FAIL WAS DETECTED. THE FRONT EMERGENCY PACKAGE WAS CHAN GED, HOWEVER APPEARED A TROUBLE WITH THE LIGHT EMERGENCY CONTROL. THE WIRE BUNDLE WAS REVISED AND A SHORT CIRCUIT WAS F OUND IN BREAKER OF DC BUS FEED EMERGENCY, IT WAS REPLACED, TESTS OK. AS CONSEQUENCE OF LOST OF LIGHT EMERGENCY CONTROL THE MOST OF EMERGENCY PACKAGE BATTERIES WERE CHANGED. AT MEX RON 3/04 EMERGENCY LIGHTS SYSTEM WAS REVISED IAW 33-53-00, EVERYTHING WAS OK. (M) 2 L 7 2 4F RT 2002041900104 20020419 00104 NM 2002 4 19 USAA020112 1 20020321 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 563AU 46744 23551 TPA - FOUND SKIN WITH WORN AREA, FUSELAGE CROWN STATION 1000, DORSAL FIN CONTACT. INSTALLED DOUBLER AND TRIPLER PER EA 86014A. (M) 2 L 7 2 4F RT A16WE 2002041900105 20020419 00105 NM 2002 4 19 USAA020113 1 20020321 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 563AU 46744 23551 TPA - FOUND SKIN CRACKED 2 FT BY 3 FT DOUBLER INSTALLED, CROWN SKIN DIRECTLY BELOW DORSAL FIN SEAL STATION 1000. INSTAL LED NEW DOUBLER PER WORK INSTRUCTIONS OF EA AND ENG USING DOUBLER AND TRIPLER PER EA 67346B. (M) 2 L 7 2 4F RT A16WE 2002041900106 20020419 00106 NM 2002 4 19 USAA020114 1 20020303 A 5743 FITTING BOEING 737 7374B7 1384702 NM LT MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 443US 31548 24842 PIT - FOUND SPAR FITTING CRACKED .125 INCH, LEFT AFT MAIN GEAR SPAR FITTING AT 2ND BOLT HOLE OUTBOARD. REPLACED FITTING PER TR 57-40-13, SB 737-57-1216 REV 2, EA 73435. 2 L 7 2 4F RT A16WE 2002041900107 20020419 00107 NM 2002 4 19 USAA020115 1 20020310 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 443US 31548 24842 PIT - FOUND SKIN CORRODED 1 INCH BY 8 INCHES, 1 INCH BY 6 INCHES, 1 INCH BY 10 INCHES, INNER LIP OF CARGO DOOR THRESHOLD . CORROSION LEVEL 1. REMOVED CORROSION PER SRM 53-00-01 PAGE 102/103 AND 53-60-01. (M) 2 L 7 2 4F RT A16WE 2002041900108 20020419 00108 NM 2002 4 19 USAA020116 1 20020309 A 5512 SKIN BOEING 737 737301 1384611 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 45802 23232 PIT - FOUND SKIN CRACKED 1.75 INCHES LONG, LEFT HORIZ STABILIZER LOWER SIDE STATION 99.07 AND 66.54. CUT OUT DAMAGE, HF EC AREA, INSTALLED FILLER AND DOUBLER PER TR 55-10-07 REV A. (M) 2 L 7 2 4F RT A16WE 2002041900109 20020419 00109 NM 2002 4 19 USAA020117 1 20020308 A 5542 SKIN BOEING 737 7374B7 1384702 NM RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 778AU 24980 PIT - FOUND RUDDER DELAMINATED .5 INCH BY .5 INCH AND 1 INCH BY .050 INCH, 2 AREAS LEFT AND RIGHT SIDE STATION 0.00. 20 0-230 DEGREE F WET LAYUP PER SRM 51-70-17 AND EA 73419. (M) 2 L 7 2 4F RT A16WE 2002041900110 20020419 00110 NM 2002 4 19 USAA020126 1 20020304 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 23860 PIT - FOUND FITTING CRACKED 1 INCH, FOR FUSELAGE FRAME STATION 616 BETWEEN S17R. INSTALLED REPAIR DOUBLER AND FILLER PE R TR 53-62-01. (M) 2 L 7 2 4F RT A16WE 2002041900111 20020419 00111 NM 2002 4 19 USAA020127 1 20020403 A 1430 FASTENER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 23860 PIT - FOUND FASTENER CRACKED 1.5 INCH, STATION 616 1ST FASTENER ON INNER CHORD ANGLE. REPAIR DOUBLER AND FILLER INSTALL ED PER TR 62-01. (M) 2 L 7 2 4F RT A16WE 2002041900112 20020419 00112 NM 2002 4 19 USAA020128 1 20020304 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 23860 PIT - FOUND FRAME CRACKED .25 INCH, BS 827R AND S10R RIVET HOLD AT VENT/OUTBOARD BIN ATTACH FITTING. INSTALLED DOUBLER PER T/R 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002041900113 20020419 00113 NM 2002 4 19 USAA020129 1 20020304 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 23860 PIT - FOUND FRAME CRACKED .25 INCH, BS 877 AND S10R RIVET HOLE AT VENT/OVERHEAD BIN SPT ATTACH. INSTALLED DOUBLER PER T R 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002041900114 20020419 00114 NM 2002 4 19 USAA020130 1 20020208 A 5315 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 42381 23860 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH DIAMETER, STATION 772 CARGO FLOOR SUPPORT RBL 5, 8, 13, LBL 5, 8, 13. DOUBLER INSTALLED PER TR 53-10-06B. (M) 2 L 7 2 4F RT A16WE 2002041900115 20020419 00115 EU 2002 4 19 USAABA02008 1 20020323 A 2120 ODOR AIRBUS 330 A330323 3930335 EU CABIN DETECTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 678US 0388 SJU - ELECTRICAL SMELL REPORTED COMING FROM SEATS 1GH. MAINTENANCE SECURED POWER TO THE SEATS. (M) 2 L 7 2 4F RT A46NM 2002041900116 20020419 00116 NM 2002 4 19 USAABB02033 1 20020319 A 3350 CHARGER BOEING 767 767201 1385125 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 646US 23898 PHL - FOUND THE AFT THREE EXTERIOR EMERGENCY LIGHTS ON THE RIGHT SIDE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHA RGER. (M) 2 L 7 2 4F RT A1NM 2002041900117 20020419 00117 2002 4 19 USAASA02028 4 20020314 A 2330 RDAX443110 VIDEO UNIT AIRBUS A319 A319112 3930323 EU PAX CABIN FAILED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 736US 1209 SAN - FLT 85 - EN ROUTE PIT-SAN, THE LEFT SIDE CABIN VIDEO SYSTEM BECAME INOPERATIVE WHEN THE CIRCUIT BREAKER IN THE OVE RHEAD FORWARD GALLEY AREA POPPED. AFTER THE CIRCUIT BREAKER WAS RESET, IT POPPED AGAIN AND WAS FOLLOWED BY AN ELECTRICA L ODOR. THE CIRCUIT BREAKER WAS LEFT OPEN, AND THE MAIN CONTROL CIRCUIT BREAKER WAS OPENED AS A FURTHER PRECAUTION. TH E ELECTRICAL ODOR DISSIPATED, AND THE FLIGHT CONTINUED, LANDING IN SAN WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE SEAT ELECTRONIC BOX AND CABLE SHORTED. REPLACED THE SEAT ELECTRONIC BOX AND CABLE. SYSTEM OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2002041900118 20020419 00118 EU 2002 4 19 USAASA02029 1 20020319 A 3350 321430 POWER SUPPLY AIRBUS 320 A320214 3930316 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 105UW 0868 BOS - THE FORWARD LEFT EMERGENCY POWER SUPPLY UNIT FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERIES. SYSTEM TESTS OK. (M) 2 L 7 2 4F RT A28NM 2002041900119 20020419 00119 EU 2002 4 19 USAASA02030 1 20020324 A 3350 POWER SUPPLY AIRBUS A319 A319112 3930323 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 770UW 1393 PHL - THE FORWARD AIRCRAFT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE LEFT FORWARD EMERGENCY POW ER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002041900120 20020419 00120 EU 2002 4 19 USAASA02031 1 20020327 A 2121 EVT3454H BLOWER AIRBUS A319 A319112 3930323 EU AVIONICS BAY OVERHEATED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 756US 2038 1340 DCA - FLT 6529 - EN ROUTE BOS-DCA - A VIBRATING NOISE WAS HEARD FROM UNDER THE COCKPIT. AN ELECTRICAL ODOR WAS THEN NOT ICED, FOLLOWED BY A VENT "BLOWER FAULT". THE VENTILATION BLOWER WAS PUT INTO OVER-RIDE, AND THE ELECTRICAL ODOR WENT AW AY. FLIGHT LANDED IN DCA WITHOUT INCIDENT. MAINTENANCE REPLACED THE AVIONICS FAN. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2002041900121 20020419 00121 2002 4 19 WRLA200207 4 20020318 A 3457 GPS DOUG DC10 DC1030 3023501 WP COCKPIT FAILED A WRLA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 EA 27 14075 46922 AIRCRAFT RETURNED TO FRANKFORT DUE TO GPS NAVIGATIONAL ERROR. RESET GPS (ALL THREE UNITS) BY SWAPPING NAVIGATIONAL DATA , TO EXPIRED DATA BASE AND BACK TO ACTUAL NAVIGATIONAL DATA BASE. ALL FUNCTIONS BACK TO NORMAL. DATA BASE RELOADED. ( M) 2 L 7 3 4F A22WE 2002041900122 20020419 00122 NM 2002 4 19 WRLA200208 1 20020317 A 2612 FIRE LOOP DOUG MD11 MD11 3023602 NM NR 1 ENGINE MALFUNCTIONED A WRLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 272WA 48437 ABORTED TAKEOFF DUE TO NR 1 ENGINE FIRE DETECTOR LIGHT, FDCU FAUTL 'PYLON FIRE DETECTOR ASSEMBLY B' LOOP B FAULT. (M) 2 L 7 3 4F RT A22WE 2002041900124 20020419 00124 CE 2002 4 19 GLBA2002049 1 20020411 A 3040 503800704 CONVERTER BEECH 1900 1900D 1154162 CE WINDSHIELD WIPER FAILED A GLBA O OTHER O OTHER TO TAKEOFF 1 NM 03 151GL 16247 UE151 RIGHT WINDSHIELD WIPER FAILED. REPLACED CONVERTER, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2002041900125 20020419 00125 SO 2002 4 19 LR7A020230 1 20020415 A 5320 ATTACH FITTING LKHEED 382 382G 526414U SO FUSELAGE BROKEN A LR7A K NONE J WARNING INDICATION DE DESCENT 1 AL 03 402LC 510 4698 FLIGHT CREW REPORTED MASTER DOOR WARNING LIGHT AND RAMP WARNING LIGHT ON DURING DESCENT INTO ETAR. INVESTIGATION REVEAL ED RT FS 858 SLOPING LONGERON STRUT ATTACH LUG CRACKED AND BROKEN AT RBL 61, WL 190. INSPECTED FOR SECONDARY DAMAGE, NO NE NOTED. AIRCRAFT MAINTENANCE FERRIED UNPRESSURIZED TO ESGC FOR REPAIR. AT EGSC REPLACED FS 858 RT STRUT AND REPAIRED LONGERON LUG IAW SRM SMP 583 53-50-26. 2 H 7 4 4T A1SO 2002041900126 20020419 00126 NE 2002 4 19 MALA020245 2 20020416 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LEFT MALFUNCTIONED A MALA C ABORTED TAKEOFF Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 GL 15 114XJ 340A114 DURING LANDING OF FLIGHT 2825 ON ROLLOUT, LT ENGINE FAILED ON LANDING ROLLOUT WHILE TURNING ON TO THE TAXIWAY. ENGINE S HUTDOWN. MAINTENANCE PERFORMED LT ENGINE INSPECTION PER GE MM 72-00-00 PG 111. BORESCOPE INSPECTION, INLET VG ACTUATIO N, POWER RUNS, NO DISCREPANCIES NOTED. 2 L 7 2 4T 4 T RT A52EU E8NE 2002041900127 20020419 00127 EU 2002 4 19 MALA020246 1 20020411 A 3020 THERMISTER SAAB SF340 340B 7860101 EU RT ENGINE FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 439XJ 340B439 DURING FLIGHT 3045, RT INTAKE LIGHT ILLUMINATED INFLIGHT QRH COMPLETED. AIR RETURN TO MSP. MAINTENANCE SWAPPED UNDER T EMP THERMISTOR TO SPARE J4. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002041900128 20020419 00128 EU 2002 4 19 MALA020247 1 20020416 A 3297 AIR130902 WIRE HARNESS SAAB SF340 340B 7860101 EU LT MLG FAULTY A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 456XJ 340B456 DURING FLIGHT 2814, LT MAIN GEAR DOWN LOCKED GREEN LIGHT REMAINED ILLUMINATED AFTER GEAR HANDLE SELECTED UP AND GEAR INT RANSIT LIGHT EXTINGUISHED. AIR RETURN TO MEM. MAINTENANCE REPLACED HARNESS ASSEMBLY DOWNLOCK ACTUATOR P/N AIR 130902 I AW AMM 32-60-05. AFTER GEAR SWINGS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002041900129 20020419 00129 EU 2002 4 19 MALA020248 1 20020415 A 7930 CONNECTOR BAC 146 AVRO146RJ85A 1500097 EU OIL SYSTEM DEFECTIVE A MALA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 GL 15 534XJ E2370 ON APPROACH OF FLIGHT 3653, NR 4 ENGINE OIL PRESSURE DROP TO ZERO. LOW OIL PRESSURE LIGHT REMAIN OUT. AFTER LANDING PI LOT SHUTDOWN ENGINE. LIGHT CAME ON AND INDICATED PRESSURE PEGGED OUT. MAINTENANCE REPLACED P1 CONNECTOR AT 442-00-00. 2 H 7 4 4F RT A49EU 2002041900130 20020419 00130 2002 4 19 MWEA020260 4 20020414 A 3415 SWITCH DOUG DC9 DC932 3022066 WP COCKPIT FAULTY A MWEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 216ME 47740 AT 90 KNOTS, THE OVERSPEED WARNING WENT OFF. REMOVED AND REPLACED CAPTAIN'S OVERSPEED WARNING SWITCH. 2 L 7 2 4F A6WE 2002041900131 20020419 00131 2002 4 19 MWEA020261 4 20020415 A 3422 2587794 FLUX DETECTOR DOUG DC9 DC981 3022081 WP LEFT FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 812ME 48006 INFLIGHT HEADING AND NO AUTO LAND ANNUNCIATORS CAME ON FMA. STANDBY COMPASS INDICATES 52 DEGREES, NUMBER RMI 052 DEGREE S, NUMBER 2 RMI 044 DEGREES, NUMBER 1 ND 044 DEGREES, NUMBER 2 ND 052 DEGREES, CAPTS GPS 43 DEGREES, AND F/O'S GPS 052 D EGREES. CONFIRMED NR 1 SYSTEM DRIFTS WITHIN 5 MINUTES OF ATTAINING HEADING. REMOVED AND REPLACED LEFT FLUX VALVE REF M M 34-21-06. OPS CHECK GOOD. 2 L 7 2 4F A6WE 2002041900132 20020419 00132 WP 2002 4 19 P2EA2002M025 1 20020417 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 140NJ 49931 ON WALK AROUND FOUND SKIN DAMAGE (GOUGE) ON FUSELAGE OUTER SKIN AT BS 256 BETWEEN STR 17 AND 18L. INSTALLED EXTERNAL DO UBLER PER SRM 53-04 FIG 12B. 2 L 7 2 4F A6WE 2002041900133 20020419 00133 NM 2002 4 19 QXEA0200484 1 20020310 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - WEAR FROM SEAT IN RT INBOARD SEAT TRACK AT STATION 272.75. REPAIRED IAW HORIZON AIR EA 2-53-372. 2 H 7 2 4T RT A13NM 2002041900134 20020419 00134 NM 2002 4 19 QXEA0200485 1 20020310 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - PITTING IN RT INBOARD SEAT TRACK AT STATION 273.0. REPAIRED IAW HORIZON AIR EA 2-53-372. 2 H 7 2 4T RT A13NM 2002041900135 20020419 00135 NM 2002 4 19 QXEA0200486 1 20020309 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - FRETTING CORROSION AT MOST INBOARD BOLT HOLE, BOTTOM SPAR CAP, LT WING AT STATION YW57.0. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAPH F, STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002041900136 20020419 00136 NM 2002 4 19 QXEA0200487 1 20020309 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - WARE ON TOP OF NR 4 FLAP TRACK FOR RT OUTBOARD FLAP, 10 INCHES AFT OF TRAILING EDGE OF BOTTOM OF WING SKIN. REPAI RED IAW HORIZON AIR EA 2-57-152. 2 H 7 2 4T RT A13NM 2002041900137 20020419 00137 NM 2002 4 19 QXEA0200488 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - SCRATCH IN RT OUTBOARD SEAT TRACK AT STATION 277.5. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAPH F, STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002041900138 20020419 00138 NM 2002 4 19 QXEA0200489 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - PITTING IN RT OUTBOARD SEAT TRACK FROM STATION 280.25 TO 282.0. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAP H F, STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002041900139 20020419 00139 NM 2002 4 19 QXEA0200490 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - GOUGE IN RT OUTBOARD SEAT TRACK AT STATION 310.75. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAPH F, STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002081300108 20020813 00108 NM 2002 8 13 UPS02238068 1 20020418 A 5330 DOUBLER BOEING 727 727180C 138406G NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE:C DOUBLER ON LEFT FWD WHEEL WELL PANEL IS PULLING LOOSE, AND IS CORRODED AT LOWER FASTENER. REMOVED AND REPLACED DOUBLER PER B727 SRM 51-30-2 ON LEFT FWD WHEEL WELL BELOW APU EXTINGUISHER BLOW OUT DISC. 2 L 7 3 4F A3WE 2002041900140 20020419 00140 NM 2002 4 19 ZW0A0204501 1 20020415 A 3350 80741 LAMP BOEING 767 76733AER 1385230 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 637TW 25403 THE EGRESS LIGHT AT SEAT 17B WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 2-9-01 LAX. --CLOSED-- 2 L 7 2 4F RT A1NM 2002041900141 20020419 00141 NM 2002 4 19 AWXA200200345 1 20020324 A 5330 6545871132 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 0 0 24710 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/4" CRACK WAS FOUND AT THE AFT UPPER CORNER OF THE LOWER HINGE CUTOUT ON THE R 1 DOOR EXTERNAL SKIN. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED. F ABRICATED REPAIR DOUBLER AND INSTALLED REPAIR AT AFT UPPER CORNER OF THE LOWER HINGE CUTOUT ON THE R1 DOOR IAW AWA ER 03 -5240-02099-TB2. 2 L 7 2 4F RT A16WE 2002041900142 20020419 00142 2002 4 19 AWXA200200349 4 20020414 A 2230 JX58 SWITCH BOEING 737 737277 1384570 NM #2 THROTTLE LVR BROKEN A AWXA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 WP 28 178AW 0 0 22645 PHX - ABORTED TAKEOFF - FLT 0627 - ON TAKEOFF OUT OF PHX EN ROUTE TO OAK WITH AUTO THROTTLES ARMED (GREEN LIGHT ILLUMINA TED) AUTO THROTTLES WOULD NOT MOVE WHEN TOGA BUTTON PUSHED. AUTO THROTTLE DID NOT DISCONNECT. AFTER MANUAL SETTING OF TA KEOFF THRUST AND PUSHING EPR BUTTON FOR CLIMB THRUST, ALL AUTO THROTTLES OPERATED NORMALLY. THRUST LEVERS ARE VERY CLOSE LY SPACED WITH NO STAGGER AT ANY SETTING. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE DEFERRED PROBLEM BY PLACING ON MEL 22-17, COND. #1, R/H TOGA SWITH INOPERATIVE. ON 04/18/2002 MEL WAS CLEARED WHEN MAINTENANCE REPLACED A BROKEN T OGA SWITCH ARM, OPERATIONAL CHECK WAS GOOD IAW BMM 22-11-01, PG. 519, STEP 17. 2 L 7 2 4F RT A16WE 2002041900143 20020419 00143 NM 2002 4 19 AWXA200200351 1 20020418 A 3350 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM SEAT ROW 16 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 0 0 24712 LAS - EEL - EMERGENCY ESCAPE LIGHT AT SEAT ROW 16 L/H IS INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND A BROKEN WIRE AT SPLICE AT SEAT ROW 16 L/H, REPLACED SPLICE IAW SWPM, OERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002041900144 20020419 00144 NM 2002 4 19 QXEA0200640 1 20020403 A 3350 82210031009 FLASHER BOMBDR DHC8 DHC8401 NM CABIN INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 SEA-CABIN OVERHEAD RED LIGHT DOES NOT ILLUMINATE WHEN EMERGENCY SWITCH LIGHT IS PUSHED FROM EITHER ARCDU OR FLIGHT ATTEN DANT POSITION. REMOVED AND REPLACED FLASHER UNIT. SELECTED EMERGENCY ON FLIGHT ATTENDANT POSITION AND ARCDU. BOTH POSITI ONS WORK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042300118 20020423 00118 NM 2002 4 23 DHL2002705005 1 20020419 A 5312 BULKHEAD BOEING 727 72722C 138400F NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 WHILE PERFORMING INSPECTION FOUND BS 870 BULKHEAD WEB CRACKED APPROX 2 INCHES RBL 60, WL 200 AS VIEWED FROM RT MLG W/W A BOVE SPOILER MIXER. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 3 4F A3WE 2002042300119 20020423 00119 NM 2002 4 23 DHL2002705006 1 20020419 A 5312 BULKHEAD BOEING 727 72722C 138400F NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 PER CUSTOMER REQUEST, REPAIR CRACKS 2 EACH ON BS 870 BULKHEAD WL 200 AT RBL 45. CUT OUT DAMAGED SECTION OF BULKHEAD, FA BRICATED AND INSTALLED DOUBLER AND FILLERS IAW B-727 SRM 53-10-9 FIG 4. 2 L 7 3 4F A3WE 2002042100001 20020421 00001 WP 2002 4 21 DHL2002807533 1 20020404 A 5313 37502711N FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF. N/R 1698 MAIN CARGO COMPT. - L1 SPLICE FITTING SHOWS 2 EACH CRACKS 7" @ STA. 1040-1060CORR: R&R SPLICE FITTIN G IAW SRM 51-1-20D PG. 9 2 L 7 4 4F RT 4A25 2002042100002 20020421 00002 WP 2002 4 21 DHL2002807529 1 20020328 A 5712 RIB DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 2045 RT. WING L/E UPPER SKIN INNER SECTION - RIB CRACKED .250 @ STA XFS 672.500CORR.: STOP DRILLED CRAC K IAW SRM 57-2-0 FIG. 2 FABRICATED DOUBLER (2024T3 AL .060) IAW SRM 57-2-0 FIG.2 , CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B , INSTALLED DOUBLER IAW SRM 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2002042100003 20020421 00003 WP 2002 4 21 DHL2002807530 1 20020404 A 5313 37798742 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 0542 MAIN CARGO COMPARTMENT- 1" CRACK ON BATHTUB FITTING, STA. 670-680 L6LCORR.; REMOVED DAMAGED BATHTUB FITTING IAW SRM51-1-20D PG. 21 , CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B INSTALLED NEW FITTING IAW SRM 51-1-20D PG .9 2 L 7 4 4F RT 4A25 2002042100004 20020421 00004 WP 2002 4 21 DHL2002807531 1 20020404 A 5313 37798742 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 0979 MAIN CARGO COMPT-1" CRACK IN FITTING STA. 749.000-759.000 , L13R.CORR> REMOVED DAMAGED FITTING STA. 749.000-759.000 , L13R IAW SRM 51-1-20D , PG. 21 CLEANED ,TREATED AND PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW FITTING IAW SRM 51-1-20D PG. 9 2 L 7 4 4F RT 4A25 2002042100005 20020421 00005 WP 2002 4 21 DHL2002807532 1 20020330 A 5310 SKIN DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 0070 AFT PAX DOOR AFT UPPER CORNER CRACKED 1.5" AT STA. 1660.000, L10LCORR.; CUT OUT DAMAGED AREA IAW SR M53-2-0 FIG.18 SHEET 3 , FABRICATED FILLER 7075T6.125 IAW SRM53-2-0 FIG. 18, SHEET 3 , CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B - INSTALLED FILLER AND DOUBLER & TRIPLER IAW SRM53-2-0 FIG.18 SHEET 3, SRM51-1-21 PG. 1, SRM 51-1-20D PG. 9 , SRM 51-1-15 PG.1 2 L 7 4 4F RT 4A25 2002042100006 20020421 00006 WP 2002 4 21 DHL2002807534 1 20020404 A 5313 97540242 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM REF. N/R 1580 FWD CARGO PIT- FRAME BEAM ATTACH FITTING CRACKED 1" @ STA. 340CORR: R&R DAMAGED FITTING IAW SRM 51-3- 0 PG.1 2 L 7 4 4F RT 4A25 2002042100007 20020421 00007 WP 2002 4 21 DHL2002807535 1 20020404 A 5712 5769857614 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM REF.: N/R 2507 RT WING- CENTER L/E INTERIOR - FITTING WITH 2.5 INCH CRACK IN IT , STA. XW456.250CORR: R&R FITTING I AW SRM 51-1-20D PG. 9 2 L 7 4 4F RT 4A25 2002042100008 20020421 00008 WP 2002 4 21 DHL2002807536 1 20020402 A 5313 ANGLE DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM REF. N/R 0287 FWD. CARGO COMPT. - RH TUNNEL - FRAME ATTACH ANGLE FLANGE CRACKED 2" @ STA. 200.000 , L26RCORR: REMOV ED DAMAGED FRAME ATTACH ANGLE AT STA. 200.000 L26R IAW SRM51-1-20D PG. 21-FABRICATED NEW ANGLE(2024T3.063)-CLEANED , TRE ATED,PRIMED IAW SRM51-1-8B-INSTALLED NEW ANGLE IAW SRM53-2-0 FIG. 1B , SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002042100009 20020421 00009 WP 2002 4 21 DHL2002807537 1 20020403 A 2730 DOUBLER DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM REF. N/R 2059 RH ELEVATOR- INNER DOUBLER FROM ACCESS PANEL 51C @ STA.XE 221.000 , .5 CRACK IN IT.CORR.; REMOVED CRA CKED DOUBLER IAW SRM55-2-0 FIG. 2 FABRICATED DOUBLER(2024T3.020) IAW SRM55-2-0 FIG. 2 CLEANED , TREATED , PRIMED IAW SRM 51-1-8B INSTALLED NEW DOUBLER IAW SRM55-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2002042100010 20020421 00010 EU 2002 4 21 RAIA00204124 1 20020401 A 7710 31055863 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 552HK 7648 41057 5640-STL - RIGHT ENGINE DID NOT MAKE TORQUE. MAINTENANCE TROUBLE SHOT AND FOUND THAT RIGHT ENGINE WOULD MAKE TORQUE WITH TORQUE AND TEMPERATURE LIMITING SYSTEM SELECTED “OFF”, AND DEFERRED THE TTL SYSTEM PER MEL 76-2. LATER CLEARED DMI, REM OVING AND REPLACING THE RIGHT ENGINE RPM TRANSDUCER. 2 L 7 2 4T RT A41NM 2002042100011 20020421 00011 EU 2002 4 21 RAIA00204125 1 20020413 A 3243 320511 VALVE JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA K NONE J WARNING INDICATION LD LANDING 1 CE 03 571HK 12714 41090 5578-SPI- ANTI-SKID LIGHT ILLUMINATED DURING ROLLOUT. MAINTENANCE DEFERRED THE ANTI-SKID SYSTEM PER J41-MEL 32-6. LATER CLEARED DMI, REMOVING AND REPLACING THE BRAKE CONTROL VALVE. 2 L 7 2 4T RT A41NM 2002042100012 20020421 00012 SO 2002 4 21 RAIA00204126 1 20020415 A 8011 35059105 STARTER EMB 145 EMB145 3260210 SO FROZEN A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 803HK 5678 4372 145077 5252-MSN- RIGHT ENGINE NO ROTATION DURING START ATTEMPT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE AIR-TURBINE S TARTER. 2 L 7 2 4F RT T00011AT 2002042100013 20020421 00013 2002 4 21 RAIA00204127 4 20020417 A 2211 7003938907 COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU A RAIA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 03 565HK 12654 3634 41082 5616-STL - SPARKS AND SMOKE IN COCKPIT COMING FROM AREA OF FLIGHT DIRECTOR. MAINTENANCE REMOVED AND REPLACED DEFECTIVE A UTOPILOT COMPUTER. 2 L 7 2 4T RT A41NM 2002042100014 20020421 00014 WP 2002 4 21 DHL2002807539 1 20020404 A 5200 SKIN DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM REF. N/R 2099 M/C DOOR FRAME UPPER INNER SKIN CRACKED 2.5" @ STA. 170.000CORR. CUT OUT DAMAGED AREA IAW SRM52-2-3 F IG. 10A FABRICATED FILLER & DOUBLER IAW SRM 52-2-3 FIG 10A CLEANED , TREATED, PRIMED IAW SRM 51-1-8B INSTALLED DOUBLER I AW SRM 52-2-3 FIG 10A 2 L 7 4 4F RT 4A25 2002042100015 20020421 00015 WP 2002 4 21 DHL2002807540 1 20020404 A 5200 SKIN DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM REF. N/R 2098 M/C DOOR FRAME UPPER INNER SKIN CRACKED 4" @ STA. 200.000CORR. CUT OUT DAMAGED AREA IAW SRM52-2-3 FIG . 10A FABRICATED FILLER & DOUBLER IAW SRM 52-2-3 FIG 10A CLEANED , TREATED, PRIMED IAW SRM 51-1-8B INSTALLED DOUBLER IAW SRM 52-2-3 FIG 10A 2 L 7 4 4F RT 4A25 2002042100016 20020421 00016 SO 2002 4 21 C2XA02IA094 1 20020419 A 2150 8152402 ACM EMB 145 EMB145ER 3260211 SO A/C BAY INOPERATIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13936 145025 IAH- PACK #1 GIVES SMOKE WHEN OPERATING ON APU BLEED. IAH- MAINTENANCE INSPECTED THE AIRCRAFT AND RELEASED IAW MEL. IAH- MAINTENANCE REMOVED AND REPLACED THE #1 ACM. PERFORMED A OPERATIONAL CHECK AND A LEAK CHECK, NO DEFECTS NOTED, AN D, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002042200001 20020422 00001 NM 2002 4 22 ASAA0140189 1 20020104 A 5320 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 783AS 25114 PAE - DURING SI CHECK, FOUND FORWARD GALLEY CUT OUT MOPSILL IS CORRODED FROM BS 290 LBL 52 TO BS 344 RBL 61, AND WL 208. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002042200002 20020422 00002 NM 2002 4 22 ASAA0140190 1 20020104 A 5340 654580733 ATTACH ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 783AS 25114 PAE - DURING SI CHECK, FOUND SKIN TO INTERCOSTAL ATTACH ANGLE IS CRACKED AT BS 290 RBL 55 AND WL 254. REMOVED AND REPLA CED ANGLE IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002042200003 20020422 00003 2002 4 22 ASAA0210001 4 20020106 A 2565 24C292592 CABLE BOEING 737 737290C 138448V NM ESCAPE SLIDE OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING MAINTENANCE CHECK, FOUND GIRT BAR DIFFICULT TO ARM AND DISARM. ADJUSTED CABLE AND LATCH ASSEMBLY THEN GIRT BAR ARMED NORMALLY. (M) 2 L 7 2 4F A16WE 2002042200004 20020422 00004 NM 2002 4 22 ASAA0210002 1 20020106 A 5315 65549131 FLOORBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM FLANGE AT BS 947, WATERLINE 207 CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002042200005 20020422 00005 NM 2002 4 22 ASAA0210003 1 20020106 A 5315 65548932 FLOORBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 420, LBL 51.5-53 CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002042200006 20020422 00006 NM 2002 4 22 ASAA0210004 1 20020107 A 5330 6545770 SKIN BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 727, STRINGER 14L WITH OVERSIZED HOLES. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002042200007 20020422 00007 NM 2002 4 22 ASAA0210008 1 20020108 A 5312 6546568518 BULKHEAD BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING SCHEDULED MAINTENANCE, FOUND AFT PRESSURE BULKHEAD AT BS 1016, RBL 1 CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002042200008 20020422 00008 NM 2002 4 22 ASAA0210009 1 20020108 A 5754 6546422282 SKIN BOEING 737 737298C 1384490 NM NR 5 SLAT WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT WING STATION 447-474 ON NR 5 SLAT WORN. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002042200009 20020422 00009 NM 2002 4 22 ASAA0210011 1 20020108 A 5330 65C357986 SKIN BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND CONTOUR OF SKIN PANEL AT BODY STATION 218-219, RIGHT BUTTOCK LINE 38 DAMAGED. REP AIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002042200010 20020422 00010 NM 2002 4 22 ASAA0210012 1 20020108 A 5315 655490510 FLOORBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 480, STRINGER 17L CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002042200011 20020422 00011 NM 2002 4 22 ASAA0210013 1 20020108 A 5315 65548944 FLOORBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 787, RIGHT BUTTOCK LINE 27 CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002042200012 20020422 00012 NM 2002 4 22 ASAA0210014 1 20020108 A 5311 65465477 FRAME BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BODY STATION 727, RIGHT BUTTOCK LINE 12, RIGHT BUTTOCK LINE 14 CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002042200013 20020422 00013 NM 2002 4 22 ASAA0210022 1 20020108 A 5730 6562203501 SKIN BOEING 737 737298C 1384490 NM CENTER WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURIGN SCHEDULED C-CHECK, FOUND WING SKIN PANEL AT BS 562-578, LEFT BUTTOCK LINE 52 CORRODED. REPAIRED PER EA. ( M) 2 L 7 2 4F RT A16WE 2002042200014 20020422 00014 NM 2002 4 22 ASAA0210035 1 20020111 A 5320 655496049 STRAP BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND SPLICE STRAP AT BS 360, STRINGER 25R-28R WITH ELONGATED HOLES. REPAIRED SPLICE ST RAP PER EA. (M) 2 L 7 2 4F RT A16WE 2002042200015 20020422 00015 NM 2002 4 22 ASAA0210036 1 20020111 A 5340 69333727 FITTING BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND TERMINAL FITTINGS AT BS 259, STRINGER 26R WITH OVERSIZED HOLES. REMOVED AND REPLA CED TERMINAL FITTINGS PER SRM. (M) 2 L 7 2 4F RT A16WE 2002042200016 20020422 00016 NM 2002 4 22 ASAA0210037 1 20020111 A 5315 6554907501 FLOORBEAM BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 727B, RIGHT BUTTOCK LINE 45 CRACKED. REPAIRED FLOORBEAM PER EA. (M) 2 L 7 2 4F RT A16WE 2002042200017 20020422 00017 NM 2002 4 22 ASAA0210038 1 20020111 A 5315 6554906501 FLOORBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 500A, LEFT BUTTOCK LINE 8, LEFT BUTTOCK LINE 24 CORRODED. REPAIRE D FLOORBEAM PER EA. (M) 2 L 7 2 4F RT A16WE 2002042200018 20020422 00018 NM 2002 4 22 ASAA0210045 1 20020126 A 5210 GUIDE BOEING 737 737290C 138448V NM PAX DOOR BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, FOUND L1 DOOR GUIDE ARM ASSEMBLY BROKEN. REMOVED AND REPLACED GUIDE ARM ASSEMBLY, THEN DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2002042200019 20020422 00019 NM 2002 4 22 ASAA0210046 1 20020128 A 3350 86210144 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS ON SEAT PALLET 7-4 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY PACK, THEN DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2002042200020 20020422 00020 NM 2002 4 22 ASAA024010 1 20020130 A 5320 MOUNT BOEING 737 7374Q8 138447Q NM ANTENNA CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 773AS 25106 PAE - FOUND CORROSION ON MOUNTING AREA AROUND MAKER BEACON ANTENNA AT BS 628, WL 148.5, BL 00. REPAIRED IAW ENGINEERING AUTHORIZATION. (M) 2 L 7 2 4F RT A16WE 2002042200021 20020422 00021 2002 4 22 MEX2002057 4 20020307 A 3160 SYMBOL GENERATOR DOUG DC9 DC987 3022087 WP INSTRUMENT PANEL FAILED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 204AM 3233 49404 FLT 190 - MEX-TIJ - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF FAIL IN THE RIGHT INSTRUMENTS PANEL. THERE WAS NO I NDICATION IN FPD AND ND FIRST OFFICER SIDE, EFIS WAS SELECTED IN 1 AND THE FAIL WAS CORRECTED HOWEVER FAIL APPEARED AGAI N WHEN EFIS WAS SWAPPED, AIRCRAFT WAS CHANGED. SYMBOL GENERATOR WAS CHECKED, AND AHRS 2 CONFIRMED FAIL UNIT WAS REPLACE D, TEST OK. (M) 2 L 7 2 4F RT A6WE 2002042200022 20020422 00022 2002 4 22 MEX2002059 4 20020307 A 3418 COMPUTER DOUG MD88 MD88 3023688 NM STALL WARNING FAILED A ASMF O OTHER O OTHER NR NOT REPORTED 1 SW 23 168PL 53174 FLT 601 - ATL-MEX - THERE WAS A FAIL IN THE STALL WARNING COMPUTERS IAW MM 34-19-00. AT RON MEX 07/08 TESTS WERE PERFOR MED IAW MM 34-19-00. (M) 2 L 7 2 4F RT A6WE 2002042200023 20020422 00023 NE 2002 4 22 MEX2002060 2 20020308 A 7321 FUEL CONTROL DOUG DC9 DC987 3022087 WP PWA JT15 JT15D4 52112 NE ENGINE FAILED A ASMF O OTHER O OTHER CR CRUISE 1 SW 23 214AM 49585 FLT 419 - MEX-VSA - PILOT REPORTED A MISALIGNMENT OF MORE THAN .5 INCH BETWEEN THROTTLE LEVERS. ROD END OF FCU WAS REPL ACED AND RIGGING AND OPERATIONAL TEST TRIM, WERE PERFORMED IAW MM 71-00-01. (M) 2 L 7 2 4F 4 F RT A6WE E1NE 2002042200024 20020422 00024 NM 2002 4 22 MEX2002067 1 20020303 A 2130 1305026 PANEL BOEING 757 7572Q8 1384972 NM COCKPIT FAILED A ASMF O OTHER G MULTIPLE FAILURE DE DESCENT 1 SW 23 806AM 26273 FLT 941 - MTY-MEX - CABIN CREW REPORTED OTU OF SERVICE THE LANDING ALTITUDE SELECTOR, AS CONSEQUENCE OF SPARE PARTS MISS ING IN MTY, MEX SENT SUCH PARTS IN FLT 944. AT ARRIVING, THE SELECTOR PANEL WAS SWAPPED, TEST OK, IAW MM 21-31-01. AT RON MEX 13/14 TESTS WERE PERFORMED OK. THE SPARE PARTS WRE INSTALLED TO THE AIRCRAFT, TESTS OK IAW MM 21-31-01. (M) 2 L 7 2 4F RT A2NM 2002042200025 20020422 00025 NM 2002 4 22 MEX2002071 1 20020315 A 2720 37723745503 SHUTOFF VALVE DOUG MD88 MD88 3023688 NM RUDDER CRACKED A ASMF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 23 161PL 49764 FLT 227 - CJS-MEX - CABIN CREW REPORTED A LOST OF 2 QUARTS OF HYDRAULIC FLUID DURING FLIGHT. VALVE ASSEMBLY RUDDER SHUT OFF WAS FOUND WITH A HOUSING CRACK. AS CONSEQUENCES OF SPARE PARTS MISSING, SUCH VALVE WAS SENT IN FLIGHT 220. VALVE A S REPLACED IAW MM 27-20-09, TESTS OK. (M) 2 L 7 2 4F RT A6WE 2002042200026 20020422 00026 NM 2002 4 22 MEX2002073 1 20020308 A 2824 VALVE DOUG MD88 MD88 3023688 NM FUEL SYSTEM MALFUNCTIONED A ASMF O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 23 161PL 49764 FLT 103 - MEX-CEN - DURING TRANSIT CHECK PILOT REPORTED THAT LEFT FUEL TANK DECREASED THE FUEL QTY UNTIL 3,900 LBS AND T HE RIGHT FUEL TANK INCREASED TO 6,500 LBS, WITH CROSS FEED OFF AND RIGHT AFT PUMP ON IN BOTH SYSTEMS. VALVE WAS CHECKED , SEVERAL CYCLES WERE PERFORMED TO THE CROSS FEED VALVE IN CABIN, WORKING OK. AIRCRAFT WAS DISPATCHED TO FLIGHT OK. AT RON, MEX 18/19 THE CROSS FEED VALVE WAS ADJUSTED IAW MM 28-20-12, TESTS OK. (M) 2 L 7 2 4F RT A6WE 2002042200027 20020422 00027 WP 2002 4 22 MEX2002077 1 20020321 A 2781 4952287503 SWITCH DOUG DC9 DC983 3022083 WP SLATS FAILED A ASMF O OTHER N H FALSE WARNING ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 23 838AM 49397 FLT 6426 - MEX-MTY - CABIN CREW REPORTED THAT SLAT AND SIF LIGHT WAS TURN ON AT ANY SELECTION/POSITION FLAP. IT WAS DET ECTED A TROUBLE WITH THE SWITCH S1-467. SUCH SWITCH WAS REPLACED IAW MM 27-81-02, TESTS OK. AT RON, MEX 21/22 SEVERAL TESTS WERE PERFORMED, OK. (M) 2 L 7 2 4F RT A6WE 2002042200028 20020422 00028 NM 2002 4 22 MEX2002078 1 20020322 A 2913 AS66411LS666 PUMP DOUG MD88 MD88 3023688 NM HYD SYSTEM FAILED A ASMF O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 23 158PL 49761 FLT 219 - CJS-MTY - DURING TRANSIT CHECK, AT ENGINE STARTING, THE LEFT HYDRAULIC PUMP INDICATED A CERO PRESSURE. BOTH C IRCUIT BREAKERS WERE RESET AND TROUBL REMAINED. HYDRAULIC PUMPS WERE SWAPPED, TESTS OK. IN MTY, THE LEFT HYDRAULIC PUM P WAS REPLACED IAW MM 29-10-05. AT RON MEX 23/24, THE PERFORMANCE TO BOTH PUMPS WERE VERIFIED DURING ENGINE RUNNING, EV ERYTHING OK IAW MM 29-10-05. (M) 2 L 7 2 4F RT A6WE 2002042200029 20020422 00029 2002 4 22 MEX2002079 4 20020322 A 2312 6226831022 PANEL DOUG MD88 MD88 3023688 NM VHF COMMS FAILED A ASMF H DEACTIVATE SYST/CIRCUITS O OTHER TX TAXI/GRND HDL 1 SW 23 158PL 5023 5023 49761 FLT 273 - GDL-CJS - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCES OF COMMUNICATION LACK WITH VHF 1 IN ANY FREQUENCY. BO TH TX/RX VHF WERE SWAPPED, NO RESULTS. FREQUENCY SELECTOR PANEL WERE REPLACED IAW MM 23-30-02, TESTS OK. (M) 2 L 7 2 4F RT A6WE 2002042200030 20020422 00030 WP 2002 4 22 MEX2002081 1 20020322 A 2932 SWITCH DOUG DC9 DC987 3022087 WP HYD SYSTEM FAILED A ASMF O OTHER K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SW 23 753RA 49587 FLT 434 - LAP-PHX - DURING TRANSIT CHECK AN HYDRAULIC LEAK WAS DETECTED IN THE LOWER PART OF THE REAR ACCESSORIES COMPAR TMENT. THE RIGHT SYSTEM WAS EMPTY. THE RIGHT SYSTM WAS RECHARGED WITH 6 QUARTS TO FIND SUCH LEAK. LEAK WAS DETECTED W AS IN A PIPE LINE OF THE RUDDER SHUTOFF VALVE. THE PIPE LINE WAS REPLACED. AT ENGINE STARTING CAPTAIN REPORTED RT HYD PRESS LOW LIGHT WAS TURNED ON, AIRCRAFT WAS DISPATCHED BY MEL 29-5 CAT 'C'. AT MTY, THE HYDRAULIC PRESSURE SWITCH WAS R EPLACED. (M) 2 L 7 2 4F RT A6WE 2002042200031 20020422 00031 NE 2002 4 22 MEX2002083 2 20020324 A 7321 76960615 FUEL CONTROL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 158PL 23148 6985 49761 FLT 575 - MEX-CUN - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCES OF NOT ACCELERATION OF THE LEFT ENGINE. WITHOUT TURN OFF ENGINES THE WATER TRAP WAS DRAINED AND THE THROTTLE CHAMBER WAS LUBRICATED. IS NECESSARY AN AIRCRAFT CHANGE TO MAKE AN FCU REPLACEMENT. AT MEX HANGAR, THE FCU OF THE ENGINE 1 WAS REPLACED, THROTTLE TESTS WERE PERFORMED IAW MM 73-20-01 , OK. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002042200032 20020422 00032 WP 2002 4 22 MEX2002084 1 20020325 A 3412 92743642 RELAY DOUG DC9 DC987 3022087 WP COCKPIT FAILED A ASMF D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 205AM 49405 FLT 608 - MEX-DFW - AIRCRAFT RETURNED TO SOUTH POSITION AS CONSEQUENCES OF OVERHEATING OF THE RAT PROBE AND A FAIL FLAG WAS APPEARED. DURING THE CHECKING SYSTEM IT WAS FOUND ALSO THAT THE TAKEOFF ALARM DID NOT WORK. IT WAS DETECTED A TROU BLE WITH THE RELAY R2-5, SUCH RELAY WAS REPLACED, IT WAS PERFORMED SEVERAL TESTS TO RAT PROBE AND TAKEOFF ALARM, OK MM 3 4-00-01. (M) 2 L 7 2 4F RT A6WE 2002042200037 20020422 00037 NE 2002 4 22 KBMA111999 2 20020208 A 7261 1742510 FILTER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE FILTER CLOGGED E KBMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 115SH 3250 3141 FILTER, BYPASS BUTTON PASSED. REMOVED FILTER AND REPLACED WITH NEW. 1 G 7 1 3U 3 U H9EU E19EU 2002042200040 20020422 00040 2002 4 22 KBMA112004 4 20020216 A 3422 103002201 GYRO SNIAS 350 AS350BA 8680817 EU COCKPIT SPINNING E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 18 2300 DIRECTIONAL GYRO, SPINS IN FLIGHT. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2002042200041 20020422 00041 EU 2002 4 22 KBMA112009 1 20020305 A 7722 56265220 GAUGE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE T4 INTERMITTENT E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 2300 T4 GAUGE, IRRATIC READING, REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002042200043 20020422 00043 EU 2002 4 22 KBMA112012 1 20020119 A 6420 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 345SH 1101 3345 BEARINGS WORN BEYOND LIMIT. REPLACED WITH NEW BEARINGS. 1 G 7 1 3U 3 U H9EU E19EU 2002042200044 20020422 00044 EU 2002 4 22 KBMA113788 1 20020215 A 7714 TACHOMETER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 169 2300 TACH REPORTED INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002042200045 20020422 00045 EU 2002 4 22 KBMA113796 1 20020317 A 2932 MA12401 PRESSURE SWITCH SNIAS 350 AS350B1 8680811 EU HYD SYSTEM FAILED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 5799 2009 PRESSURE SWITCH, LIGHT WOULD NOT GO OUT. REPLACED WITH NEW SWITCH. 1 G 7 1 3U H9EU 2002042200046 20020422 00046 EU 2002 4 22 KBMA113797 1 20020317 A 7170 0174078010 DRAIN VALVE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE ENG START LEAKING E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 270SH 8796 1864 START DRAIN VALVE WAS LEAKING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U 3 U NC H9EU E19EU 2002042200047 20020422 00047 EU 2002 4 22 KBMA113798 1 20020320 A 7334 642792002 TRANSMITTER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE FUEL PRESSURE INOPERATIVE E KBMA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 19 313LV 999 3296 NO PSI INDICATION WITH POSITIVE FUEL FLOW. REMOVED AND REPLACED WITH NEW TRANSMITTER. 1 G 7 1 3U 3 U H9EU E19EU 2002042200048 20020422 00048 EU 2002 4 22 KBMA113799 1 20020326 A 2110 59008 COMPRESSOR SNIAS 350 AS350BA 8680817 EU AIR CONDITIONER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 181 2300 AIR CONDITIONER INOPERATIVE. COMPRESSOR INOPERATIVE, REPLACED WITH SERVICEABLE COMPRESSOR. 1 G 7 1 3U NC H9EU 2002042200049 20020422 00049 SW 2002 4 22 KBMA113800 1 20020324 A 2842 EA470B3588 PROBE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUEL QTY IND INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 73DP 12177 2513 FUEL GAUGE REPORTED INOPERATIVE. REPLACED WITH NEW FUEL PROBE TANK UNIT. 1 G 7 1 3U 3 U H2SW E4CE 2002042200050 20020422 00050 EU 2002 4 22 KBMA113801 1 20020329 A 2150 060018 BELT SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE AIR CONDITIONER BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 15 2300 AIR CONDITIONER BELT BROKE OFF. REPLACED WITH NEW. 1 G 7 1 3U 3 U NC H9EU E19EU 2002042200051 20020422 00051 2002 4 22 KBMA113802 4 20020330 A 2300 064105430 RADIO SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT MALFUNCTIONED E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 2273A 4194 2273 RADIO KNOB STICKS AND SKIPS FREQUENCIES. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2002042200052 20020422 00052 2002 4 22 KBMA113803 4 20020402 A 3452 KT76A TRANSPONDER SNIAS 350 AS350BA 8680817 EU COCKPIT INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 1188P 205 2347 TRANSPONDER NOT GIVING REPLY LIGHT OR IDENTY. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2002042200053 20020422 00053 SW 2002 4 22 KBMA113804 1 20020402 A 7720 1244440 GAUGE BELL 206 206B 1181511 SW ALLSN 250C 250C* GL TOT INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 188TV 10079 2704 TOT GAUGE IS INOPERATIVE. REPLACED WITH SERVICEABLE GAUGE 1 G 7 1 3U 3 U H2SW E4CE 2002042200054 20020422 00054 2002 4 22 KBMA113857 4 20020323 A 3422 DSQ20 SWITCH SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE DIR GYRO INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 345SH 1264 3345 DIRECTIONAL GYRO SWITCH WILL NOT STAY IN. REPLACED WITH NEW DSQ SWITCH. 1 G 7 1 3U 3 U H9EU E19EU 2002042200055 20020422 00055 SW 2002 4 22 KBMA113858 1 20020321 A 6710 206062721113 ACTUATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R CONTROL INOPERATIVE E KBMA O OTHER L NO TEST NR NOT REPORTED 1 WP 19 73DP 1800 2513 LINEAR ACTUATOR, UNABLE TO ADJUST N2/NR. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U H2SW E4CE 2002042200056 20020422 00056 NE 2002 4 22 AOQ2002F00001 2 20020214 A 7200 TFE73131C ENGINE AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE73131C 01518 NE NR 3 FAILED B AOQA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 EA 11 929ML 8958 92 P76418 AFTER LANDING, THE FLIGHT CREW NOTED THAT THE NR 3 ENGINE OIL WARNING LIGHT ILLUMINATED. OIL PRESSURE INDICATED 25 PSI. UPON POST FLIGHT INSPECTION, CREW NOTICED OIL LEAKING FROM THE NR 3 ENGINE COWLING AND OIL FILTER BYPASS BUTTON WAS PO PPED. AIRFRAME TT 9153.0 HOURS. NR 3 ENGINE TT 8958.2 HOURS NR3 ENGINE CYCLES 6436. AIRCRAFT WAS INSPECTED BY MAINTENA NCE AND SUSPECTED AN INTERNAL FAILURE. LOANER ENGINE WAS INSTALLED IN THE NR 3 POSITION. ORIGINAL NR 3 ENGINE WAS SENT TO MFG FOR TEARDOWN INSPECTION. 2 L 7 3 4F 4 F A46EU E6WE 2002042200057 20020422 00057 EU 2002 4 22 AXI2002F00000 1 20020315 A 2435 36B50419G1 SHAFT AMD FALCON FALCON20 2730103 EU GARRTT TFE731 TFE7312B WP STARTER GEN FAILED E AX1R K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 25 1881Q 414 STARTER GENERATOR SPLINE SHAFT INSTALLED IN STARTER GENERATOR SHEARED AT THE BASE OF THE INTERNAL SPLINE AFTER ABOUT 25 START CYCLES. IT IS OUR OPINION THAT THE HOLE, WHICH IS DRILLED AND TAPE TO ACCEPT THE RETAINING SCREW IS BEING DRILLED TO DEEP AND IS THE CAUSE OF THE SHAFT FAILURES. 2 L 7 2 4F 4 F RT A7EU E6WE 2002042200058 20020422 00058 EU 2002 4 22 AXI2002F00001 1 20020315 A 4940 368510419G1 SHAFT AMD FALCON FALCON20 2730103 EU GARRTT TFE731 TFE7312B WP APU START/GEN BROKEN E AX1R O OTHER O OTHER NR NOT REPORTED 1 EA 25 1881Q 414 GENERAL ELECTRIC STARTER GENERATOR (PN 2CM308C3) WAS INSTALLED ON OUR APU ON 10/30/01 WITH A NEW SPLINE SHAFT SHEARED AT THE BASE OF THE INTERNAL SPLINE AFTER ABOUT 50 START CYCLES. IT IS OUR OPINION THAT THE HOLE, WHICH IS DRILLED AND TAP ED TO ACCEPT THE RETAINING SCREW IS BEING DRILLED TO DEEP AND IS THE CAUSE OF THE SHAFT FAILURES. 2 L 7 2 4F 4 F RT A7EU E6WE 2002042200059 20020422 00059 EU 2002 4 22 AXI2002F00002 1 20020315 A 4940 36B510419G1 SHAFT AMD FALCON FALCON20 2730103 EU GARRTT TFE731 TFE7312B WP APU STARTER/GEN BROKEN E AX1R K NONE O OTHER IN INSP/MAINT 1 EA 25 1881Q 414 STARTER GENERATOR SPLINE SHAFT (PN 36B50419G1) INSTALLED IN STARTER GENERATOR (PN 2CM308C3) SHEARED AT THE BASE OF THE I NTERNAL SPLINE AFTER ABOUT 30 START CYCLES. IT IS OUR OPINION THAT THE HOLE, WHICH IS DRILLED AND TAPED TO ACCEPT THE R ETAINING SCREW IS BEING DRILLED TO DEEP AND IS THE CAUSE OF THE SHAFT FAILURES. 2 L 7 2 4F 4 F RT A7EU E6WE 2002042200060 20020422 00060 EU 2002 4 22 02109329 1 20020419 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 329UE 41097 During preflight inspection, the crew noted that a section of the emergency floor track lighting was inoperative. Maint enance personnel secured a loose connector for the emergency floor track lights. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002042200061 20020422 00061 EU 2002 4 22 02110324 1 20020420 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 324UE 41017 During preflight inspection, the crew noted that a section of the emergency floor track lighting was inoperative. Maint enance personnel secured a loose connector for the emergency floor track lighting. An operational check was satisfactor y and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002042200062 20020422 00062 EU 2002 4 22 02111311 1 20020421 A 3350 8545K15T33T SWITCH JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER CR CRUISE 1 EA 27 311UE 41029 During cruise, the crew noted that the emergency exit lights illuminated with the switch in the armed position. Mainten ance personnel removed and replaced the flight deck emergency lights switch. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002042200063 20020422 00063 2002 4 22 B2P2002F00000 4 20020329 A 6113 C792 BEARING RACE HARTZL BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE PROPELLER BROKEN B B2PR K NONE O OTHER IN INSP/MAINT 1 SO 17 48544 15540 2736 HJ310 UE183 HJ310 CUSTOMER REMOVED PROPELLER FROM SERVICE DUE TO EXCESSIVE BLADE PLAY AND GREASE LEAKING FROM BLADE SOCKETS. UPON DISASSE MBLY, IT WAS NOTED THAT THE BEARING RACES ON BLADES (SN 2579 AND 2583) HAD FAILED COMPLETELY AND WERE IN MANY PIECES. P OSSIBLE CAUSE COULD BE THAT THE BEARING SPLITS IN THE RACES WERE IMPROPERLY INDEXED AT THE HUB PARTING LINE. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002042200064 20020422 00064 NE 2002 4 22 B2P2002F00001 3 20020329 A 6114 C792 BEARING RACE HARTZL BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE PROPELLER BROKEN B B2PR K NONE O OTHER IN INSP/MAINT 1 SO 17 48544 15540 2736 HJ310 UE183 HJ310 CUSTOMER REMOVED PROPELLER FROM SERVICE DUE TO EXCESSIVE BLADE PLAY AND GREASE LEAKING FROM BLADE SOCKETS. UPON DISASSE MBLY IT WAS NOTED THAT THE BEARING RACES ON BLADES (SN 2579 AND 2583 HAD FAILED COMPLETELY AND WERE IN MANY PIECES. POS SIBLE CAUSE COULD BE THAT THE BEARING SPLITS IN THE RACES WERE IMPROPERLY INDEXED AT THE HUB PARTING LINE. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002042200065 20020422 00065 NE 2002 4 22 B2P2002F00002 3 20020329 A 6114 B70192 SCREW HARTZL BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE PROPELLER BROKEN B B2PR K NONE K FLUID LOSS IN INSP/MAINT 1 SO 17 48544 15540 2736 HJ310 UE183 CUSTOMER REMOVED PROPELLER FROM SERVICE DUE TO EXCESSIVE BLADE PLAY AND GREASE LEAKAGE FROM BLADE SOCKETS. PROPELLER WA S DISASSEMBLED AND INSPECTED. UPON FURTHER INVESTIGATION, THE PRELOAD PLATE SCREWS WERE SEVERELY WORN AND ONE WAS BROKE N IN TWO PIECES. LOSS OF BLADE PRELOAD HAD CAUSED THE BLADES TO HAVE TOO MUCH END PLAY BEYOND ALLOWABLE LIMITS CAUSING EXCESSIVE DAMAGE TO THE BEARING RACES AND HUB ASSEMBLY. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002042200066 20020422 00066 NM 2002 4 22 BTV2002F00000 1 20020305 A 5246 LATCH AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE FUEL DOOR FAILED B BTVR O OTHER K FLUID LOSS NR NOT REPORTED 1 GL 23 635E 106 REFUELING DOOR CAME OFF IN FLIGHT, STRIKING RIGHT HORIZONTAL STABILIZER. DOOR LATCH FAILURE. 2 K 7 3 4F 4 F RT A50NM E44NE 2002042200067 20020422 00067 CE 2002 4 22 DBC2002F00002 1 20020410 A 7332 10038901823 PRESSURE SWITCH BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60 52043 NE FUEL SYSTEM FAILED E DBCA O OTHER N FALSE WARNING CL CLIMB 1 GL 13 1250 7336 FA88 SHORTLY AFTER TAKEOFF, PILOT NOTED LOW PRESSURE FUEL LIGHT ILLUMINATED. PILOT LANDED WITHOUT INCIDENT. TROUBLESHOT TO FAILED FUEL PRESSURE SWITCH. REMOVED (PN 100-398018-23 SN 12948) AND REPLACED WITH NEW UNIT. OPERATIONS CHECKED, OK. 2 L 7 2 4T 4 T A24CE E4EA 2002042200068 20020422 00068 CE 2002 4 22 ECA2002F00000 1 20020401 A 5210 SEAL LEAR 25 25 5170506 CE GE CJ610 CJ6101 30006 NE CABIN DOOR TORN E ECAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 11 25EC 25026 CABIN ALTITUDE REACHED 10,000 FT MAX., AIRFLOW WAS APPLIED AND CABIN WAS RESTORED. DECENT FOLLOWED WITH FLOW ON UNTIL 1 500 FT PRIOR TO LANDING. REQUIRED MAX AIRFLOW TO MAINTAIN CABIN PRESSURE. MAINTENANCE PERFORMED GROUND TEST OF CABIN P RESSURIZATION SYSTEM, OPERATED NORMALLY BUT EXCESSIVE AIR LEAK WAS FOUND COMING FROM AROUND CABIN DOOR SEAL FORWARD SIDE . A VISUAL INSPECTION SHOWED A 1.5 INCH TEAR IN THE SEAL. SEAL IS TO BE REPLACED BEFORE ANY FURTHER TROUBLSHOOTING TAK ES PLACE. 2 L 7 2 4J 4 J A10CE 1E16 2002042200069 20020422 00069 CE 2002 4 22 FCP2002F00000 1 20020218 A 5520 263150713 FRAME LEAR 35 35A 5170602 CE ELEVATOR WORN B FCPR K NONE O OTHER IN INSP/MAINT 1 NM 09 184TS 8564 35A08 MAINTENANCE DISCOVERED WHILE TROUBLESHOOTING PITCH TRIM DISCREPANCY. ELEVATOR PITCH SPRING FRAME ASSEMBLY (PN 2631507-1 3). DURING INSPECTION OF SPRING AND FRAME ASSEMBLY, UPPER ATTACH POINT FOR SPRING WAS FOUND WORN BEYOND LIMITS. SPRING ATTACH BOLT WAS WORN THROUGH BUSHING AND AT LEAST 50 PER CENT INTO FRAME ASSEMBLY. THIS AIRCRAFT IS 13 MONTHS OUT OF A 12 YEAR INSPECTION. 2 L 7 2 4F A10CE 2002042200070 20020422 00070 CE 2002 4 22 KOS2002F00000 1 20020401 A 2432 4076 BATTERY LEAR 35 35A 5170602 CE MULTIPLE CELL INOPERATIVE E K0SA K NONE L NO TEST IN INSP/MAINT 1 NE 01 498JR 2351 498 BATTERY INOPERATIVE. 2 L 7 2 4F A10CE 2002042200071 20020422 00071 CE 2002 4 22 KOS2002F00001 1 20020401 A 7332 1G1344 PRESSURE SWITCH LEAR 35 35A 5170602 CE FUEL SYSTEM INOPERATIVE E K0SA K NONE O OTHER IN INSP/MAINT 1 NE 01 498JR 7008 498 FUEL PRESSURE SWITCH, INOPERATIVE. 2 L 7 2 4F A10CE 2002042200072 20020422 00072 CE 2002 4 22 WVE2002F00005 1 20020326 A 7500 156CA3213A336 COUPLING LEAR 60 60LEAR 5170707 CE TAILCONE FAILED B WVER A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 09 221FX 111 PILOT REPORTED DUCT OVERHEAT CAUTION DURING SECOND FLIGHT AFTER 1200/2400 HOUR AND 3000 CYCLE INSPECTION AT 25,000 FT. SUBSEQUENTLY REPORTED GENERATOR AND INVERTER FAIL. DECLARED IFE AND RETURNED TO AIRFIELD. UPON INSPECTION BY MAINTENAN CE, THE AFT TAILCONE BLEED AIR DUCT COUPLING WAS FOUND TO BE DISCONNECTED. THE SEALS ON THIS COUPLING WERE CHANGED DURI NG THE SCHEDULED INSPECTION. CAUSE AND CORRECTIVE ACTION REMAINS UNDER INVESTIGATION AT THIS TIME. 2 L 7 2 4F RT A10CE 2002042200073 20020422 00073 NE 2002 4 22 WVE2002F00006 2 20020326 A 7261 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 LACK OF LUBE B WVER E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 09 27318 7318 PILOT REPORTED INFLIGHT NR1 ENGINE SHUTDOWN DUE TO LOSS OF OIL PRESSURE DURING FLIGHT AFTER C1/C2 INSPECTION. DECLARED IFE AND DIVERTED. UPON INSPECTION BY MAINTENANCE, THE NR1 ENGINE REQUIRED FIVE QUARTS OF OIL. CAUSE AND CORRECTIVE ACT ION REMAINS UNDER INVESTIGATION AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 2002042200074 20020422 00074 CE 2002 4 22 ZKG2002F00001 1 20020311 A 3600 1143800025 COOLER BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE RT ENGINE CRACKED B ZKGR K NONE O OTHER IN INSP/MAINT 1 NE 05 550CJ UC50 PRECOOLER CRACKED ON RIGHT ENGINE INBOARD AFT. THIS IS THE 2ND AC WITH THE SAME TROUBLE IN LESS THAN ONE WEEK. 2 L 7 2 4T 4 T RT A24CE E4EA 2002042200075 20020422 00075 NM 2002 4 22 QXEA0200491 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - PITTING IN RT OUTBOARD SEAT TRACK FROM STATION 339.75 TO 342.0. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAP H F, STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002042200076 20020422 00076 NM 2002 4 22 QXEA0200492 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - PITTING IN RT OUTBOARD SEAT TRACK AT STATION 374.0. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAPH F, STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002042200077 20020422 00077 NM 2002 4 22 QXEA0200493 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - PITTING IN RT OUTBOARD SEAT TRACK AT STATION 470.25. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042200078 20020422 00078 NM 2002 4 22 QXEA0200494 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - PITTING IN RT OUTBOARD SEAT TRACK AT STATION 516.5. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAPH F, STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002042200079 20020422 00079 NM 2002 4 22 QXEA0200495 1 20020309 A 5534 WEB DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - LT REAR FUSELAGE AT VERTICAL STAB IS CRACKED AT WEB. REPAIRED IAW RD 8-55-199. 2 H 7 2 4T RT A13NM 2002042200080 20020422 00080 NM 2002 4 22 QXEA0200496 1 20020310 A 5534 WEB DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - RT REAR FUSELAGE AT VERTICAL STAB IS CRACKED AT WEB AT STRINGER 45. REPAIRED IAW RD 8-55-199. 2 H 7 2 4T RT A13NM 2002042200081 20020422 00081 NM 2002 4 22 QXEA0200498 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - CHAFE IN RT INBOARD SEAT TRACK AT STATION 196.0. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAPH F, STEPS 1 AN D 2. 2 H 7 2 4T RT A13NM 2002042200082 20020422 00082 NM 2002 4 22 QXEA0200499 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - PITTING IN RT INBOARD SEAT TRACK AT STATION 239.25. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAPH F, STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002042200083 20020422 00083 NM 2002 4 22 QXEA0200500 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - PITTING IN RT INBOARD SEAT TRACK AT STATION 244.5 TO 249.25. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAPH F , STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002042200084 20020422 00084 NM 2002 4 22 QXEA0200501 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - PITTING IN RT INBOARD SEAT TRACK AT STATION 262.5. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAPH F, STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002042200085 20020422 00085 NM 2002 4 22 QXEA0200502 1 20020309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - PITTING AND GROVE INSIDE RT INBOARD SEAT TRACK CHANNEL AT STATION 267.25. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6 , PARAGRAPH F, STEPS 1 AND 2. 2 H 7 2 4T RT A13NM 2002042200087 20020422 00087 NM 2002 4 22 QXEA0200509 1 20020321 A 5330 SKIN BOMBDR DHC8 DHC8401 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 2174 4031 PDX - THERE IS A GOUGE IN THE FUSELAGE SKIN 18.5 INCHES BELOW THE FORWARD CARGO DOOR AND 13.5 INCHES AFT OF THE LAVATORY SERVICE DOOR. 2 H 7 2 4T RT A13NM 2002042200088 20020422 00088 NM 2002 4 22 QXEA0200510 1 20020323 A 3080 WARNING SYSTEM BOMBDR DHC8 DHC8402 NM COCKPIT FALSE ACTIVATION A QXEA K NONE N FALSE WARNING DE DESCENT 1 NM 09 408QX 4050 SEA- DEICE CAUTION LIGHT ON DURING DESCENT. EMERGENCY PROCEDURES COMPLIED WITH, NOTED NORMAL DEICE PRESSURE ON BOTH SID ES AND ALL LIGHTS FOR DEICE BOOTS ON ICE PROTECTION PANEL ILLUMINATED. GROUND RAN AIRCRAFT WITH DEICE PRESSURE NORMAL I N FAST/SLOW OR MANUAL. COULD NOT DUPLICATE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042200089 20020422 00089 EU 2002 4 22 QXEA0200511 1 20020322 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 PDX- RIGHT ARROW OF FORWARD EMERGENCY EXIT SIGN DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE TURNED ON. REMOVED AND RE PLACED FORWARD EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002042200090 20020422 00090 NM 2002 4 22 QXEA0200512 1 20020314 A 2710 ROD END DHAV DHC8 DHC8202 2809007 NM AILERON BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - RT AILERON POSITION SYNCHRO PUSH PULL ROD END BROKEN OFF. REPLACED SYNCHRO PUSH PULL ROD. 2 H 7 2 4T RT A13NM 2002042200091 20020422 00091 NM 2002 4 22 QXEA0200513 1 20020316 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - DENT 6 INCHES BELOW FORWARD CORNER OF BAGGAGE DOOR. REPAIRED IAW HORIZON AIR EA 2-53-375. 2 H 7 2 4T RT A13NM 2002042200092 20020422 00092 NM 2002 4 22 QXEA0200514 1 20020320 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - DENT ON FUSELAGE SKIN BELOW MAIN CABIN DOOR. REPAIRED IAW HORIZON AIR EA 2-53-376 AND DHC-8 200 SRM 51-20-26. 2 H 7 2 4T RT A13NM 2002042200093 20020422 00093 NM 2002 4 22 QXEA0200516 1 20020317 A 5751 SKIN DHAV DHC8 DHC8202 2809007 NM AILERON CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - CRACK AT YW409.7 ON THE LT AILERON TRAILING EDGE INBOARD HINGE CUTOUT. REPAIRED IAW HORIZON AIR EA 2-57-153. 2 H 7 2 4T RT A13NM 2002042200094 20020422 00094 NM 2002 4 22 QXEA0200517 1 20020319 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - DENT IN CARGO DOOR LOWER THRESHOLD. REPAIRED IAW HORIZON AIR EA 2-53-375. 2 H 7 2 4T RT A13NM 2002042200095 20020422 00095 NM 2002 4 22 QXEA0200519 1 20020320 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - DENT 6 INCHES BELOW CORNER OF BAGGAGE DOOR. REPAIRED IAW HORIZON AIR EA 2-53-375. 2 H 7 2 4T RT A13NM 2002042200096 20020422 00096 NM 2002 4 22 QXEA0200520 1 20020127 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 831PH 328 CKB - LAMP SOCKET DS21 HAS BROKEN WIRES ON EMERGENCY LIGHTING FLOOR STRIP ON FLOOR PANEL 143CZ. REPAIRED IAW DASH 8 MM 33-53-01, PAGE 3/4, FIGURE 1, SHEET 2. 2 H 7 2 4T RT A13NM 2002042200097 20020422 00097 NM 2002 4 22 QXEA0200521 1 20020114 A 3350 SPLICE DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 831PH 328 CKB - DIODE SPLICE FOR EMERGENCY TRACK LIGHTING AT FLOOR PANEL 143CZ IS DAMAGED. REPAIRED IAW DHC-8 AMM 33-51-00, PAGE 201-202, SECTION 2. 2 H 7 2 4T RT A13NM 2002042200098 20020422 00098 NM 2002 4 22 QXEA0200523 1 20020314 A 5751 AILERON DHAV DHC8 DHC8102 2809003 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 831PH 328 CKB - RT AILERON HAS COMPOSITE DAMAGE OUTBOARD TRAILING EDGE. REPAIRED IAW HORIZON AIR EA 9-57-578-A-. 2 H 7 2 4T RT A13NM 2002042200099 20020422 00099 EU 2002 4 22 QXEA0200524 1 20020325 A 2611 SMOKE DETECTOR FOKKER F28 F28MK4000 4990810 EU LAVATORY ACTIVATED A QXEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 09 499US 11182 PDX - AIRCRAFT RETURNED TO FIELD WHEN LAVATORY SMOKE DETECTOR SOUNDED. AIRCRAFT DOWN FOR MAINTENANCE. 2 L 7 2 4F RT A20EU 2002042200100 20020422 00100 EA 2002 4 22 QXEA0200525 1 20020328 A 2121 GG670950225 FAN CNDAIR CL600 CL6002C10 1390015 EA CABIN MALFUNCTIONED A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 605QX 10022 SEA- AFTER DEPARTURE, AN ACRID ODOR WAS REPORTED FROM CABIN. RECIRCULATING FAN CIRCUIT BREAKER WAS FOUND TO BE POPPED. TURNED RECIRCULATING FAN OFF, ODOR WENT AWAY. MAINTENANCE REPLACED THE NR 2 RECIRCULATION FAN, OPERATIONAL CHECK WAS G OOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002042200101 20020422 00101 NM 2002 4 22 QXEA0200526 1 20020327 A 5270 SENSOR BOMBDR DHC8 DHC8402 NM CARGO DOOR DIRTY A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 405QX 4047 SEA- AFT BAGGAGE DOOR WARNING LIGHT ILLUMINATED AT TAKEOFF AND REMAINED ON MORE THAN OFF DURING BRIEF UNPRESSURIZED FLIG HT. AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. INTERROGATED PSEU FOR FAULT CODES AND INSPECTED SENSOR. FOUND SENSOR FACE AND TARGET TO BE DIRTY. CLEANED AND LUBED. GROUND RAN, NO FAULT INDICATIONS OR WARNINGS NOTED. OPERATIONAL CHEC KS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042200102 20020422 00102 NM 2002 4 22 QXEA0200527 1 20020327 A 5270 SENSOR BOMBDR DHC8 DHC8402 NM CARGO DOOR FAULTY A QXEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 09 405QX 4047 SEA- CARGO DOOR LIGHT FLICKERS ON INTERMITTENTLY WITH CHIME AND DOOR LIGHTS DURING FLIGHT. AIRCRAFT RETURNED TO FIELD W ITHOUT INCIDENT. REMOVED AND REPLACED AFT BAGGAGE DOOR PROXIMITY SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2002042200103 20020422 00103 NM 2002 4 22 QXEA0200529 1 20020330 A 5270 401020101 PROXIMITY SWITCH BOMBDR DHC8 DHC8401 NM EMERGENCY EXIT FAULTY A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 401QX 4031 PDX - WHILE CLIMBING THROUGH 9,000 - 10,000 FT, CREW RECEIVED A DOOR WARNING FOR THE TYPE 2/3 EMERGENCY EXIT. AIRCRAFT RETURNED TO FIELD. DOOR WARNING WENT GREEN WHILE PASSING THROUGH 6,000 FT. MAINTENANCE INSPECTED AIRCRAFT AND REPLACED THE FORWARD EMERGENCY DOOR PROXIMITY SWITCH. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042200104 20020422 00104 2002 4 22 QXEA0200530 4 20020328 A 3425 7003360941 COMPUTER DHAV DHC8 DHC8201 2809001 NM COCKPIT FAULTY A QXEA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 NM 09 369PH 2609 513 PDX- FIRST OFFICER'S FLIGHT INSTRUMENTS INDICATED INCORRECTLY AND COMPASS CARD DID NOT WORK. AIRCRAFT DIVERTED TO PDX W ITHOUT INCIDENT. REMOVED AND REPLACED NR 2 AHRS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042200105 20020422 00105 CE 2002 4 22 00017 1 20020419 A 3260 SQUAT SWITCH LEAR 25 25 5170506 CE MLG OUT OF ADJUST E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 525TW 011 AIRCRAFT DEPARTED YIP, SELECTED GEAR UP, MAIN GEAR DOOR RED LIGHTS STAYED ON. RETURNED TO DEPARTURE AIRPORT. MAINTENAN CE FOUND RT SQUAT SWITCH OUT OF ADJUSTMENT, ADJUSTED SWITCH AND PERFORMED GEAR SWINGS, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4J A10CE 2002042200106 20020422 00106 EU 2002 4 22 00018 1 20020419 A 3230 A24239107 UPLOCK AMD FALC20 FALCON 2720302 EU LT MLG FAILED E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 295TW 5 AIRCRAFT DEPARTED ADS, GEAR DOORS RED LIGHTS STAYED ON, RETURNED TO DEPARTURE AIRPORT. MAINTENANCE REPLACED LT MAIN GEA R UPLOCK, PERFORMED GEAR SWINGS, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A7EU 2002042200108 20020422 00108 CE 2002 4 22 81TJ41802 1 20020405 A 5414 45A344206 SKIN BEECH MU300 400A 1155402 CE RT PYLON CRACKED E UVCA K NONE O OTHER IN INSP/MAINT 1 CE 03 81TJ 2067 RK14 RIGHT UPPER MIDDLE ENGINE PYLON SKIN DUE TO CRACKING AT LOCATION OF PRE-EXISTING REPAIR OF HOLE AND CRACK IN SKIN. 2 H 7 2 4F RT A16SW 2002042200109 20020422 00109 CE 2002 4 22 81TJ41902 1 20020405 A 5414 45A34412002 SKIN BEECH MU300 400A 1155402 CE RT PYLON CHAFED E UVCA K NONE O OTHER IN INSP/MAINT 1 CE 03 81TJ 2067 RK14 LEADING EDGE SKIN PANEL OF RIGHT PYLON HAS CHAFED HOLE FROM CONTACT WITH COWLING. 2 H 7 2 4F RT A16SW 2002042200110 20020422 00110 CE 2002 4 22 81TJ42002 1 20020405 A 5330 SKIN BEECH MU300 400A 1155402 CE FUSELAGE CHAFED E UVCA K NONE O OTHER IN INSP/MAINT 1 CE 03 81TJ 2067 RK14 FUSELAGE BELLY SKIN CHAFED JUST AFT OF NOSE LANDING GEAR AREA. 2 H 7 2 4F RT A16SW 2002042200111 20020422 00111 2002 4 22 99V41702 4 20020417 A 3442 7007700803 RADAR BRAERO DH125 HS125700A 4230170 EU COCKPIT MALFUNCTIONED E UVCA K NONE O OTHER CR CRUISE 1 CE 03 9999V 1 2571550308 THIRD FAILURE OF RADAR INDICATORS NR 1. AFTER 1 HOUR OF FLIGHT, IMAGES WOULD GET FUZZY. AFTER 2 HOURS THIS UNIT WENT T OTALLY BLANK. AFTER 30 MINUTES OF FLIGHT UNIT IMAGE WOULD STROBE. BLANK SCREEN TO IMAGE TO BLANK SCREEN. UNITS NR 2 & 3 REPAIRED UNITS FROM HONEYWELL. 2 L 7 2 4F A3EU 2002042200112 20020422 00112 NM 2002 4 22 C1HA200294008 1 20020419 A 3350 900835A BATTERY PACK BOEING 727 727290 138408W NM INOPERATIVE A C1HA K NONE L NO TEST UK UNKNOWN 1 GL 15 294AS 4 22146 Left side upper over wing emergency lights don't illuminate. Removed and replaced battery pack charger and battery pack IAW MM. Ops checks good. 2 L 7 3 4F A3WE 2002042200113 20020422 00113 NM 2002 4 22 C1HA200297006 1 20020421 A 3350 200131A BATTERY PACK BOEING 727 727270 138408P NM INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 697CA 23052 Upon inspection found forward emergency track lighting to be inoperative. Removed and replaced battery pack, operational checks good. 2 L 7 3 4F RT A3WE 2002042200114 20020422 00114 WP 2002 4 22 ARWA20020402 1 20020414 A 7711 8DJ174LWMI INDICATOR LKHEED 1011 1011385115 5265015 WP COCKPIT FAULTY A ARWA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 19 307GB 193U1131 ABORTED TAKEOFF AT 110 KTS, DUE TO NR 2 ENGINE EPR NOT AT TO POWER (1.2 EPR). REMOVED AND REPLACED NR 2 EPR INDICATOR I AW 77-11-00.` 2 L 7 3 4F A23WE 2002042200115 20020422 00115 NM 2002 4 22 AWXA200200346 1 20020325 A 5320 69374112 TIE CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - MAJOR REPAIR - DURING C-12 CHECK A .5 INCH CRACK WAS FOUND ON THE STRINGER TIE OF THE 2ND STRINGER FROM THE FLOOR JUST FORWARD OF THE R1 DOOR AT FS 294.5. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02 PG 2-4, 10 & 11. 2 L 7 2 4F RT A16WE 2002042200116 20020422 00116 EU 2002 4 22 AWXA200200347 1 20020306 A 5320 D53118221200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 YWG - MAJOR REPAIR - DURING C-8 CHECK CORROSION WAS FOUND IN 7 PLACES ON FLOOR SUPPORT RAIL AT Y254, FR 16 TO FR 20, INC LUDING THE SPLICE REPAIR. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM 51-72-11 PG 1 & 2. 2 L 7 2 4F RT A28NM 2002042200117 20020422 00117 EU 2002 4 22 AWXA200200348 1 20020306 A 5320 D53472189202 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 YWG - MAJOR REPAIR - DURING C-8 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AT Y1292 RT, FR 68 TO FR 69. MAINTENANC E FABRICATED AND INSTALLED REPAIR IAW SRM 51-42-11 PG 1, PARA 5. 2 L 7 2 4F RT A28NM 2002042200118 20020422 00118 NM 2002 4 22 AWXA200200350 1 20020411 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN LOOSE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 PHX - EEL - EMERGENCY EXIT LIGHTING AT SEAT ROW 7 LT HAS COME LOOSE FROM ITS MOUNT. MAINTENANCE REPLACED LIGHT ASSEMBLY AT SEAT ROW 7 LT, FUNCTIONAL CHECK WAS GOOD IAW T/C A1C33006. 2 L 7 2 4F RT A16WE 2002042200119 20020422 00119 NM 2002 4 22 AWXA200200352 1 20020419 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 PHX - EEL - VERTICAL EMERGENCY EXIT LIGHTS ABOVE THE L2 AND R2 DOORS ARE INOPERATIVE. MAINTENANCE TROUBLESHOT AND REPLA CED DEPLEATED BATTERY PACK AT M1051 IN OVERHEAD AFT GALLEY, OPERATIONAL CHECK OF LIGHTING SYSTEM WAS GOOD. 2 L 7 2 4F RT A16WE 2002042200120 20020422 00120 SO 2002 4 22 C2XA02IA093 1 20020420 A 3260 2050500101 CONNECTOR EMB 120 EMB120ER 3260203 SO LT MLG DIRTY A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 16718 120136 IAH- LEFT MAIN GEAR SYSTEM A DISAGREEMENT. CLEANED AND RESECURED CANNON PLUG ON LEFT HAND MLG FOR SYSTEM A, PERFORMED AN OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002042200121 20020422 00121 NM 2002 4 22 C7WA20020000 1 20020410 A 5320 651986219 BEAM BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING A SCHEDULED MAINTENANCE VISIT, FOUND LEVEL II CORROSION ON LT NLG MID CHORD AS VIEWED FROM INSIDE AT BS 300.00-31 5.00, LBL 20 WL 170 INBOARD OF LT NLG TRUNNION. REMOVED AND REPLACED MID CHORD IAW B-727 SRM 51-30-2. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 3 4F A3WE 2002042200122 20020422 00122 NM 2002 4 22 C7WA200200001 1 20020410 A 5320 651986219 BEAM BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING A SCHEDULED MAINTENANCE VISIT, FOUND LEVEL II CORROSION ON LT NLG MID CHORD AS VIEWED FROM INSIDE AT BS 300.00-31 5.00, LBL 20 WL 170 INBOARD OF LT NLG TRUNNION. REMOVED AND REPLACED MID CHORD IAW B-727 SRM 51-30-2. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 3 4F A3WE 2002042200123 20020422 00123 EU 2002 4 22 DHL2002364006 1 20020417 A 3260 MODULE AIRBUS 300 A300B4203 3930306 EU LANDING GEAR MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 364DH 141 UPON GEAR RETRACTION UNABLE TO RAISE GEAR. RAN ABNORMAL. SWITCHED FROM LEVER LOCK POSITION 1 TO 2 GEAR RETRACTED NORMA LLY. RESEATED PROXIMITY DETECTOR MODULE AND PERFORMED OPS CHECK ON BOTH SYS 1 & 2 CHECKED OK FOR SERVICE PER M/M 32-61- 12. 2 L 7 2 4F RT A35EU 2002042200124 20020422 00124 SO 2002 4 22 C2XA02CL103 1 20020421 A 4900 4950958 VALVE EMB 135 EMB135LR 3260305 SO APU LEAKING A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 28518 2931 145334 CLE FLIGHT#3316 THE CREW REPORTED A STRONG FUEL SMELL IN THE AIRCRAFT WHEN THE APU IS STARTED.MAINTENANCE REPLACED THE A PU AIRBLEED VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002042200125 20020422 00125 NM 2002 4 22 DHL2002705003 1 20020418 A 5320 FITTING BOEING 727 72722C 138400F NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 DURING INSPECTION FOUND STA 880 WL 198 RBL 62 SMALL FRAME & ATTACH FITTING HAS CORROSION. REMOVED ATTACH ANGLE STA 880 WL 198 RBL 62 FROM FRAME. REMOVED CORROSION FROM FRAME, WITHIN LIMITS. FABRICATED NEW ATTACH ANGLE P/N 60-8892. INSTA LLED NEW ATTACH ANGLE TO FRAME STA 880. 2 L 7 3 4F A3WE 2002042200126 20020422 00126 NM 2002 4 22 DHL2002741005 1 20020416 A 2150 RELAY BOEING 727 7272Q9 138448M NM LT A/C PACK FAILED A DHLA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 01 741DH 21931 ON SHORT FINAL, BURNING SMELL FROM A/C DUCTS, 20 SEC LATER LT PACK TRIP OFF LIGHT ILLUMINATED. SHUT LT PACK OFF, LT BLE ED OFF AND LANDED. LEFT OFF ON TAXI IN AND RAN ABNORMAL PROCEDURE. DID NOT TRY TO REESTABLISH PACK OPS. COOLING FAN A IR INLET COOLING DOOR. REMOVED AND REPLACED RELAY R-596 (LT PACK COOLING DOOR RELAY) OPS CHECKS GOOD ON GRND AT EWR IAW 727 M/M 21-51-00. 2 L 7 3 4F RT A3WE 2002042200127 20020422 00127 NM 2002 4 22 QXEA0200518 1 20020319 A 2520 VENT DHAV DHC8 DHC8202 2809007 NM CABIN MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - NEED VENT GRILL FOR NR 3 SEAT TRACK. REPAIRED IAW DASH 8 SRM 51-40-11 AND 51-40-00. 2 H 7 2 4T RT A13NM 2002042200128 20020422 00128 NM 2002 4 22 QXEA0200522 1 20020114 A 7110 PLATE DHAV DHC8 DHC8102 2809003 NM RT COWLING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 831PH 328 PDX - BUTT PLATES ON RT LOWER COWL ALIGNMENT HOLES ON INBOARD AND OUTBOARD SIDES ARE ELONGATED AND OUT OF LIMITS. REPAI RED IAW DHC-8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002042200129 20020422 00129 NM 2002 4 22 QXEA0200532 1 20020322 A 5415 TRUSS BOMBDR DHC8 DHC8401 NM NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 412QX 4059 SMF- INBOARD AND OUTBOARD AFT DIAGONAL TRUSS SHOWS SIGNS OF HEAT DAMAGE. REPAIRED IAW HORIZON AIR EA 6-54-60. 2 H 7 2 4T RT A13NM 2002042200130 20020422 00130 EA 2002 4 22 QXEA0200535 1 20020402 A 2840 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ACTIVATED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 601QX 10009 TUS - COMPLIED WITH EMERGENCY CHECKLIST WHEN FUEL TRANSFERRING PROBLEM OCCURRED. LEFT AND RIGHT BOOST PUMP ADVISORY'S I LLUMINATED AND CENTER TANK JET TRANSFER PUMPS WERE ON. LEFT TANK SHOWED INCREASE AND RIGHT TANK SHOWED NO INCREASE. RE CEIVED 800 LBS IMBALANCE WITH ASSOCIATED CAUTION LIGHTS. AIRCRAFT DOWN FOR MAINTENANCE. 2 L 7 2 4F RT A21EA 2002042200131 20020422 00131 NM 2002 4 22 QXEA0200537 1 20020331 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8201 2809001 NM LAVATORY FALSE ACTIVATION A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 359PH 514 PDX- LAVATORY SMOKE DETECTOR ALARM SOUNDED. REMOVED AND REPLACED SMOKE DETECTOR, OPERATIONAL CHECKS GOOD. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042200132 20020422 00132 NM 2002 4 22 QXEA0200538 1 20020401 A 3350 6104781 POWER SUPPLY BOMBDR DHC8 DHC8401 NM CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 409QX 4051 SEA- AFT PASSENGER AND SERVICE DOORS, EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 4 EMERGENCY LIGHT POWER SUPPLY AND BOTH BATTERIES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042200133 20020422 00133 NM 2002 4 22 QXEA0200540 1 20020403 A 6123 POST DHAV DHC8 DHC8201 2809001 NM AUTOFEATHER SYS OUT OF ADJUST A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 368PH 512 MFR - ABORTED TAKEOFF AUTO FEATHER ARM FUNCTION INOP. ADJUSTED POST AND PERFORMED AUTO FEATHER OPERATIONAL CHECK. OPER ATION CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042200134 20020422 00134 NM 2002 4 22 QXEA0200541 1 20020405 A 6123 CONNECTOR DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS LOOSE A QXEA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 NM 09 355PH 500 PDX - ABORTED TAKEOFF. DURING TAKEOFF ROLL WITH POWER LEVERS SET, NO AUTO FEATHER ARM LIGHT ILLUMINATED. FOUND CONNECT OR AT AUTO FEATHER CONTROLLER LOOSE. REMOVED CONNECTOR AND CHECKED NR 1 AND 2 POWER LEVER A, F POTENTIOMETERS. RIGS CH ECKED NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042200135 20020422 00135 EU 2002 4 22 QXEA0200543 1 20020407 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 PDX- FORWARD EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR HAS SEVERAL LIGHT BULBS INOPERATIVE. REMOVED AND REPLACED FORWARD E MERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002042200136 20020422 00136 EU 2002 4 22 QXEA0200544 1 20020404 A 5312 PRESSURE PANEL FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 PDX - CRACK WAS FOUND IN LEFT SIDE OF NOSE LANDING GEAR BAY SIDEWALL JUST FORWARD OF STATION 3050. MAINTENANCE FABRICAT ED AND INSTALLED A DOUBLER AND SHIM IAW F-28 STRUCTURAL REPAIR MANUAL, 53-02-18. 2 L 7 2 4F RT A20EU 2002042200137 20020422 00137 EU 2002 4 22 QXEA0200545 1 20020404 A 1430 RIVET FOKKER F28 F28MK4000 4990810 EU WING SHEARED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 PDX - FOUND TWO RIVETS SHEARED OFF ON CENTER WING TO FUSELAGE CLOSING ANGLE ON RIGHT SIDE OF A/C. ONE RIVET WAS 7 INCHE S FORWARD OF FRAME 10790, AND ONE RIVET 18 INCHES AFT OF FRAME 10790. MAINTENANCE REMOVED THE DAMAGED CHERRY RIVETS AND INSTALLED CHERRY RIVET IAW F-28 STRUCTURAL REPAIR MANUAL 51-31-05. 2 L 7 2 4F RT A20EU 2002042200138 20020422 00138 SO 2002 4 22 COMA0210016 1 20020418 A 5240 DOOR EMB 120 EMB120RT 3260202 SO A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 267CA 120259 FLIGHT 5061 SERVICE DOOR WARNING DURING T/O.CLOSED AND LATCHED SERVICE DOOR. 2 L 7 2 4T RT A31SO 2002042200139 20020422 00139 EA 2002 4 22 COMA0260265 1 20020413 A 2910 PV304448 PUMP CNDAIR CL600 CL6002B19 1900309 EA LEFT LEAKING A COMA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 786CA 10101 7333 FLIGHT 6040 HYDRAULIC SYSTEM #1 QUANTITY DROPPED TO 25%.REPLACED THE #1 ENGINE HYD PUMP. 2 L 7 2 4F RT A21EA 2002042200141 20020422 00141 2002 4 22 QXEA0200550 4 20020410 A 3425 7003360941 COMPUTER DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 361PH * 3173 516 PDX- AFTER TAKEOFF FIRST OFFICER'S ATTITUDE AND HEADING FAIL. CAPTAIN'S RMI FAIL. RETURNED TO FIELD. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 AHRS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042200143 20020422 00143 NM 2002 4 22 QXEA0200552 1 20020329 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - RIGHT WING NR 5 FLAP TRACK HAS PITTING ON INBOARD SIDEWALL. REPAIRED IAW HORIZON EA 2-57-156. 2 H 7 2 4T RT A13NM 2002042200144 20020422 00144 NM 2002 4 22 QXEA0200553 1 20020327 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - RT OUTBOARD SEAT TRACK X424 HAS CORROSION PITS IN CHANNEL. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002042200145 20020422 00145 NM 2002 4 22 CALA0200219 1 20020419 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND FLOORBEAM UPPER T CAP CORRODED AT FASTENER HOLES, STA 294.5, LBL 20 TO RBL 58. REPAIRED IAW SRM 53-10-5 1. 2 L 7 2 4F RT A16WE 2002042200146 20020422 00146 WP 2002 4 22 CALA0200221 1 20020419 A 5315 BULKHEAD DOUG DC9 DC982 3022082 WP FS 120 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND BULKHEAD CORRODED FORWARD OF FIRST OFFICER'S I/B SEAT TRACK AT FS 120, LBL 30 TO RBL 58. THE BULKHEAD W AS REPAIRED IAW SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 2002042200147 20020422 00147 WP 2002 4 22 CALA0200222 1 20020420 A 5313 LONGERON DOUG DC9 DC983 3022083 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 49525 INSPECTION FOUND A 1.125" CRACK IN LONGERON 2R AFT OF BELTFRAME STA 1418. THE CRACKED SECTION OF LONGERON WAS CUT OUT AN D A NEW SECTION OF LONGERON AND SPLICE WERE INSTALLED IAW SRM 53-02, FIGURE 17. 2 L 7 2 4F RT A6WE 2002042200148 20020422 00148 NM 2002 4 22 CALA0200223 1 20020420 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND CABIN FLOORBEAM UPPER CAP CORRODED AT STA 312. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2002042200149 20020422 00149 WP 2002 4 22 CALA0200225 1 20020420 A 5311 BELTFRAME DOUG DC9 DC983 3022083 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 49525 INSPECTION FOUND A 1/4" CRACK IN BELTFRAME UPPER FLANGE AT ATTACH POINT WITH LONGERON 2L AT STA 1418. REPAIRED IAW SRM 5 3-03. 2 L 7 2 4F RT A6WE 2002042200150 20020422 00150 NM 2002 4 22 CALA0200227 1 20020421 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 847-907 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND R/H SEAT TRACK HAD PITTING CORROSION AT STA 847-907. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WA S INSTALLED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2002042200151 20020422 00151 NM 2002 4 22 CALA0200229 1 20020421 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM STA 727D+5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNELS CORRODED AT STA 727D+5", RBL 8 AND LBL 8. REPAIR ANGLES WERE INS TALLED AT EACH LOCATION IAW ECRA 5320-01603. 2 L 7 2 4F RT A16WE 2002042200152 20020422 00152 NM 2002 4 22 CALA0200230 1 20020421 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM STA 727D+5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNEL CORRODED AT STA 727D+5" RBL 3. A REPAIR ANGLE WAS INSTALLED IAW E CRA 5320-01603. 2 L 7 2 4F RT A16WE 2002042200153 20020422 00153 NM 2002 4 22 CALA0200231 1 20020421 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM STA 794 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND CHANNEL CORRODED IN AFT BAGGAGE BIN AT STA 794, RBL 8. REPAIRED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002042200154 20020422 00154 NM 2002 4 22 CALA0200232 1 20020421 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM STA 794 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNELS CORRODED AT STA 794, LBL 3 AND RBL 3. CHANNEL BEAM REPAIRS WERE INSTALLED AT EACH LOCATION IAW SRM 53-00-53, FIGURE 201. 2 L 7 2 4F RT A16WE 2002042200155 20020422 00155 WP 2002 4 22 DHL2002802005 1 20020418 A 2611 CONNECTOR DOUG DC8 DC873 302199C WP A DHLA O OTHER J L WARNING INDICATION NO TEST IN INSP/MAINT 1 SO 01 802DH 46076 1) #2 ENG LOOP B WILL NOT TEST, IN EITHER SHORT CIRCUIT OR FIRE WARNING.2) REPLACED CONNECTOR ON RIGHT SIDE OF FAN LOO P "B" ; OPS CHECKS GOOD PERDC-8 M/M 26-10-1. 2 L 7 4 4F RT 4A25 2002042200156 20020422 00156 NM 2002 4 22 AWXA200200355 1 20020327 A 5313 65468778 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 0 0 24710 MCN - MAJOR REPAIR - DURING C-12 CHECK A CRACK WAS FOUND ON THE AFT END OF STR 18 R/H, BS 727. MAINTENANCE TRIMMED OUT C RACK IN STR 18 SHEAR WEB, PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED, FABRICATED SHEAR WEB FILLER, -12 GUSS ET, -194 RADIUS FILLER, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5312-02109-GF1. 2 L 7 2 4F RT A16WE 2002042300001 20020423 00001 SO 2002 4 23 ASOA02118 1 20020301 A 3350 BATTERY PACK EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 273AS 23733 120222 FLT 4265 - DURING GROUND INSPECTION IN ATL, THE CREW DISCOVERED THE LAST FIVE FLOOR EMERGENCY LIGHT WERE INOPERATIVE. M AINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK AT ROWS 7C. OPERATIONAL CHECKS GOOD. AIRCRAFT OK F OR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002042300002 20020423 00002 SO 2002 4 23 ASOA02119 1 20020301 A 3350 BATTERY EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 260AS 23627 120132 FLT 4822 - DURING GROUND INSPECTION IN DFW, THE MIDDLE SECTION OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY. OPERATIONAL CHECKS NORMAL. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002042300003 20020423 00003 SO 2002 4 23 ASOA02122 1 20020303 A 2150 22045402 A/C PACK EMB 120 EMB120RT 3260202 SO CABIN CONTAMINATED A ASOA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 269AS 120210 DURING CRUISE FLIGHT, THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. AT THIS TIME THERE WAS NO SMOKE BUT A SLIGHT O DOR IN THE COCKPIT. COMPLETED THE FUSELAGE FIRE/SMOKE CHECKLIST, NO SIGN OF INCREASE OR DECREASE IN THE CABIN SMOKE. AN EMERGENCY WAS DECLARED AND DIVERTED TO FSM. LANDED WITHOUT INCIDENT. AT NO TIME WAS THERE ANY INDICATION OF FIRE. THE SMOKE IN THE CABIN DISSIPATED WHEN DOOR WAS OPENED. INSPECTED THE RT PACK AND FOUND OIL ON THE PACK. THERE WAS NO EVIDENCE OF OIL INSIDE THE RT PACK HEAT EXCHANGER OR THE RT ENGINE BLEED LINE. THE RT ENGINE OIL LEVEL WAS FOUND TO BE NORMAL. REMOVED AND REPLACED THE RIGHT ACM. OPS AND LEAK CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2002042300004 20020423 00004 SO 2002 4 23 ASOA02123 1 20020227 A 5313 12005744013 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 286AS 120268 DURING C-CHECK INSPECTION IN BNA, STRINGER 19 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 13 AND 15A. CORROSION WAS AL SO FOUND ON THE SAME STRINGER BETWEEN FRAMES 16 AND 18A. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 'S 51-40-00, 51-25-00, AND 51-21-00. (M) 2 L 7 2 4T RT A31SO 2002042300005 20020423 00005 SO 2002 4 23 ASOA02124 1 20020227 A 5313 12005744002 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 286AS 120268 DURING C-CHECK INSPCTION IN BNA, STRINGER 18 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND 15. MAINTENANCE REMOV ED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-40-02, 51-25-00, AND 51-21-02. (M) 2 L 7 2 4T RT A31SO 2002042300006 20020423 00006 SO 2002 4 23 ASOA02125 1 20020227 A 5313 12005722013 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 286AS 120268 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS DISCOVERED ON STRINGER 17 LEFT BETWEEN FRAMES 18 AND 20. MAINTENANCE RE MOVED AND REPLACED THE CORRODED STRIGNER IAW SRM 51-40-00. (M) 2 L 7 2 4T RT A31SO 2002042300007 20020423 00007 SO 2002 4 23 ASOA02126 1 20020227 A 5313 12005744011 STRINGER EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 286AS 120268 DURING C-CHECK INSPECTION IN BNA, STRINGER 20 LEFT HAD CORROSION BETWEEN FRAMES 18 AND 19. MAINTENANCE REMOVED AND REPL ACED THE CORRODED STRINGER IAW SRM'S 51-25-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002042300008 20020423 00008 SO 2002 4 23 ASOA02127 1 20020227 A 5310 12009846001 CROSSBEAM EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 286AS 120268 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT OUTBOARD CROSSBEAM AT FRAME 16. CORROSION WAS ALSO FO UND ON THE LEFT INBOARD CROSS BEAM AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAMS IAW SRM'S 51-4 0-05, 51-40-02, AND 51-25-00. (M) 2 L 7 2 4T RT A31SO 2002042300009 20020423 00009 SO 2002 4 23 ASOA02128 1 20020227 A 5310 12008896001 CROSSBEAM EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 286AS 120268 DURING C-CHECK INSPECTION IN BNA, THE RIGHT INBOARD CROSSBEAM HAD CORROSION AT FRAME 16. THE RIGHT OUTBOARD CROSSBEAM A LSO HAD CORROSION AT FRAME 18. MAINTENANCE REMOVED AND REPLACED CORRODED CROSSBEAMS IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002042300010 20020423 00010 SO 2002 4 23 ASOA02129 1 20020227 A 5310 12005805003 BUTT STRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 286AS 120268 DURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 16 AND 21. MAINTENANCE REMOVE D AND REPLACED THE CORRODED BUTT STRAP IAW SRMS 51-40-02, 51-25-00, 51-21-02 AND 51-21-00. (M) 2 L 7 2 4T RT A31SO 2002042300011 20020423 00011 SO 2002 4 23 ASOA02130 1 20020227 A 5310 12046963001 BUTT STRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 286AS 120268 DURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 15 AND 21 AND ALSO FROM FRAME 21 TO FRAME 25. MAINTENANCE REMOVED AND REPLACED THE TWO CORRODED SECTIONS OF BUTT STRAP IAW SRM 51-25-00, 51-21-00, AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002042300012 20020423 00012 SO 2002 4 23 ASOA02131 1 20020227 A 5320 12005803001 SILL EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 286AS 120268 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL PLATE BETWEEN FRAMES 13 AND 21. MAINTENAN CE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRMS 51-25-00, 51-21-04, AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002042300013 20020423 00013 EA 2002 4 23 ASOA02132 1 20020303 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 11 837AS 7271 FLT 4468 - DURING APPROACH INTO YYZ, THE CAPTAIN RECEIVED A FLAP FAIL MESSAGE WHEN FLAPS WERE SET TO 8 DEGREES LEFT AND RIGHT. AIRCRAFT WAS AT 7000 FEET AND 200 KKNOTS. AS THE AIRCRAFT SLOWED TO 190 KNOTS THE FLAPS WERE STUCK AT ZERO DEGR EES LT AND RT. AN EMERGENCY WAS DECLARED AND A ZERO FLAP LANDING WAS ACCOMPLISHED INTO YYZ WITHOUT FURTHER INCIDENT. M AINTENANCE VISUALLY INSPECTED THE FLAPS AND NO DEFECTS WERE NOTED. THE CIRCUIT BREAKERS WERE CYCLED AND THE FLAP SYSTEM WAS RAN ALSO WITH NO DEFECTS NOTED. ALL WORK WAS COMPLETED IAW ASA EO 600-27-0004A WHICH ENCOMPASSES AD98-20-01. (M) 2 L 7 2 4F RT A21EA 2002042300014 20020423 00014 EA 2002 4 23 ASOA02133 1 20020303 A 2750 855D1009 SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT WING INOPERATIVE A ASOA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 11 837AS 3086 7271 FLT 4469 - AFTER TAKEOFF FROM YYZ, THE CAPTAIN RECEIVED A FLAP FAIL MESSAGE WHEN FLAPS WERE SELECTED TO 8 DEGREES LT AND RT. THE CAPTAIN ATTEMPTED TO RETRACT THE FLAPS TO ZERO DEGREES WITH NO RESULTS. AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED AND LANDED SAFELY IN YYZ. MAINTENANCE INTERROGATED THE FLAP ELECTRONIC CONTROL UNIT AND FOUND A FLAGGED RIGHT FLAP BRAKE AND POSITION SENSOR UNIT. MAINTENANCE REMOVED AND REPLACED THE RIGHT BPSU AND RIGGED IT. THE FLAPS WERE THE N CYCLED NUMEROUS TIMES WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002042300015 20020423 00015 EA 2002 4 23 ASOA02134 1 20020304 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 11 841AS 7300 FLT 4736 - UPON TAKEOFF FROM ATL, RETRACTION OF THE FLAPS CAUSED A FLAP FAIL CAUTION MESSAGE TO APPEAR. THE CAPTAIN RAN THE FLAP FAIL CHECKLIST. AN EMERGENCY WAS DECLARED, AND FIRE EQUIPMENT WAS REQUESTED AS A PRECAUTION. AIRCRAFT PERFOR MED A ZERO FLAP LANDING IN ICT, WHICH WAS THE ORIGINAL DESTINATION, WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE FLA P SYSTEM. OPERATIONAL CHECK OF THE FLAP SYSTEM GOOD WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. ALL WORKS WA S PERFORMED IAW AD 98-20-01. (M) 2 L 7 2 4F RT A21EA 2002042300016 20020423 00016 SO 2002 4 23 ASOA02220 1 20020301 A 3350 BATTERY EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 232AS 120036 FLT 4824 - DURING GROUND INSPECTION IN TUL, THE CAPTAIN REPORTED THAT THE FORWARD SECTION OF CABIN FLOOR EMERGENCY LIGHT S WOULD NOT TEST. MAINTENANCE CHARGED THE EMERGENY LIGHT BATTERY FOR 15 MINUTES THEN RETESTED THE EMERGENCY LIGHTS. OP ERATIONAL TEST OF LIGHTS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002042300017 20020423 00017 SO 2002 4 23 ASOA02221 1 20020303 A 2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO CARGO BAY MALFUNCTIONED A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 266AS 120188 FLT 4144 - AFTER TAKEOFF FROM VLD, AT ABOUT 300 FEET THE CAPTAIN RECEIVED A TRIPLE CHIM AND SMOKE AURAL WARNING, BUT NO RED LIGHTS ASSOCIATED WITH SMOKE IN THE CARGO BIN WERE ILLUMINATED. FIRE EQUIPMENT WAS REQUESTED TO MEET THE AIRCRAFT. AIRCRAFT RETURNED TO VLD FOR AN UNEVENTFUL LANDING. THE FIRE DEPARTMENT INSPECTED THE CARGO COMPARTMENT AND FOUND NO S IGNS OF SMOKE OR THE SMELL OF SMOKE, HEAT, OR FIRE. MAINTENANCE RESET AND CLEANED THE COCKPIT SMOKE DETECTOR AND RESET THE SMOKE DETECTOR CIRCUIT BREAKER. OPERATIONAL CHECKS OF THE SMOKE DETECTOR SYSTEM WERE GOOD. NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2002042300018 20020423 00018 SO 2002 4 23 SIMA200206504 1 20020206 A 5311 12010732001 FRAME EMB 145 EMB145 3260210 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AE 145069 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND GOUGE AT BOTTOM FRAME 81 BEYOND SRM LIMITS. REMOVED DAMAGED FRAME. INSTALLED NEW FRAME IAW EMB 145 (SRM145/1142, REV 16) 51-20-03, 51-40-02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002042300019 20020423 00019 SO 2002 4 23 SIMA200206505 1 20020207 A 5330 SKIN EMB 145 EMB145 3260210 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AE 145069 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, REQUIRES PERMANENT REPAIR OF DENT LEFT FUSELAGE BETWEEN FRAMES 19 AND 20, S TRINGERS 15L AND 16L. REMOVED DENT BY CUT OUT. PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER 8 INCH BY 6.75 INCH, .063 INCH THICK, AND A FILLER 1.5 INCH BY 1.8125 INCH, .032 INCH THIC K. WORK DONE IAW EMB GST-0432/02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002042300020 20020423 00020 SO 2002 4 23 SIMA200206506 1 20020215 A 5310 BEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AE 145069 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 20 WHICH EXCEEDED SRM L IMITS. COMPLETELY REMOVED CORROSION BY CUT OUT. FABRICATED .050 INCH, A DOUBLER ANGLE 18 INCH BY 3.75 INCH AND FILLER 12.1125 INCH BY 3.5 INCH BY 1.125 INCH, A 6.5 INCH BY 1.125 INCH PLATE .125 INCH THICK, AND TWO SHIMS 5.5 INCH BY 1.125 INCH .090 INCH THICK. WORK DONE IAW EMB 145 (SRM 145/1142 CHAPTER 53 REV 17, 53-21-10, PARA 2 AND STANDARD SRM PRACTICE S. (M) 2 L 7 2 4F RT T00011AT 2002042300021 20020423 00021 SO 2002 4 23 SIMA200206510 1 20020212 A 5310 STRUCTURE EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 607AE 145064 ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON FORWARD DIGITAL BEYOND SRM LIMITS AFT BLENDING. PERFORME D AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER 4.3 INCH BY 2.1 INCH .040 I NCH THICK. REPAIR DONE IAW EMB GST-0488/02, EMB145 SRM145/1142, REV 16 51-40-02, 51-40-04, 51-40-06, CPM 51-21-04, 51-2 1-05 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002042300022 20020423 00022 SO 2002 4 23 SIMA200206511 1 20020205 A 5313 STRINGER EMB 145 EMB145 3260210 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AE 145069 ABI - DURING IN IMBV INSPECTION OF AICRAFT, STRINGER 19R WAS FOUND TO BE CHAFED BY THE AFT BELLY FAIRING AT HYDRAULIC BA Y WALL. BLENDED CHAFED AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA WITH NO DEFECTS NOTED. APPLIED ALODINE AND EPOXY PRIMER TO THE BLENDED AREA. FABRICATED A REPAIR DOUBLER 14.8 INCH BY 1.4 INCH, .063 INCH THICK, AND TWO SHIMS 4.5 INCH BY .7 INCH, .080 INCH THICK. WORK DONE IAW EMBGST-0409/02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002042300023 20020423 00023 SO 2002 4 23 SIMA200206512 1 20020306 A 5610 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT FAILED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 655AE 145452 ORD - FLT 4286 - AFTER TAKEOFF WHEN CREW SELECTED WINDSHIELD HEAT ON THE WINDSHIELD STARTED TO BUBBLE AND THEN SHATTERED . CREW DECLARED AN EMERGENCY AND RETURNED TO ORD WITH NO OTHER INCIDENTS. (M) 2 L 7 2 4T RT T00011AT 2002042300028 20020423 00028 CE 2002 4 23 A852002F00000 1 20020415 A 3710 13695 VALVE CESSNA 177 177B 2073708 CE LYC O360 O360* 41514 EA STANDBY VACUUM FAILED B A85A K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 09 20300 17702656 VALVE WAS REPLACED WAS WITH IN SERIAL NUMBERS TO BE RE-USED IN MOD TO SVS V SYSTEM TO COMPLY WITH ALTERNATE METHOD OF CO MPLAIANCE TO AD. VALVE WAS FOUND TO HAVE FAILED INT HE OPEN POSITION ON BACK UP SIDE. 1 H 7 1 3O 3 O A13CE E286 2002042300029 20020423 00029 EA 2002 4 23 BSY2002F00007 2 20020408 A 7321 469153 ROD END PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA RIGHT ENGINE WORN D BSYA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 40978 318152199 148768A MIR. ON TAKEOFF, RIGHT ENGINE HAD ERRATIC FUEL FLOW. RETURNED TO AIRPORT. REPLACED WORN ROD END ON FIRE WALL SHUTOFF AND RERIGGED. OPS CHECKED GOOD. 1 L 7 2 3O 3 O A20SO E14EA 2002042300030 20020423 00030 CE 2002 4 23 BSY2002F00008 1 20020408 A 3230 0843400117 BELLCRANK CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MLG GEARBOX BROKEN D BSYA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 3700G 310R0899 270867R GOING INTO AIRPORT, HAD NO NOSE GEAR DOWN LIGHT. ROCKED AIRCRAFT, GEAR THEN SHOWED DOWN AND LOCK. LANDED, NO PROBLEMS. FOUND BELLCRANK BROKEN ON GEARBOX, REMOVED AND REPLACED BELLCRANK, CHECKED RIGGING. OPS CHECKED GOOD. 1 L 7 2 3O 3 O 3A10 E5CE 2002042300047 20020423 00047 CE 2002 4 23 FGQ2002F00000 1 20020329 A 3246 265F864 BALANCE WEIGHT BEECH 200 200BEECH 1152920 CE NOSE TIRE DISLODGED B FGQA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SO 01 715JH 100 BB1345 BALANCE PATCH INSIDE TUBELESS TIRE CAME LOOSE AND SEVERE VIBRATION NOTED DURING NOSEWHEEL SPIN DOWN AFTER RETRACTION. 1 L 7 2 4T A24CE 2002042300048 20020423 00048 CE 2002 4 23 GMZ2002F00000 1 20020401 A 2910 S123630070 HOSE CESSNA 337 T337F 2075724 CE CONT O360 TSIO360* 17025 SO NLG ACTUATOR FAILED B GMZ2 K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 01 1723M 8 33701323 NOSE GEAR WILL NOT EXTEND. NEW HOSES FABRICATED 8 HOURS BEFORE, MALFUNCTIONED. RETEST HOSE, REMOVED AND CHECKED FOR RE STRICTIONS. RESTRICTION EVIDENT. REMOVED ORIFICE AND FILTER AT FIREWALL. FOUND RUBBER TRAPPED ORIFICE (UPSTREAM) AND RUBBER AND METAL PARTICLES TRAPPED IN FILTER DISC. RUBBER PARTICLES FROM HOSE FABRICATION OR RUBBER PIECES AT HOSE RESTR ICTION ON RETRACT HOSE WHICH BROKE LOOSE AND RESTRICTED FLOW AT ORIFICE NOT ALLOWING GEAR TO EXTEND. MORE CARE IN FABRI CATING HOSE AND FLUSHING, AFTER NEW HOSE INSTALLATION. 1 H 7 2 3O 3 O A6CE E9CE 2002042300049 20020423 00049 GL 2002 4 23 HEF2002F00000 2 20020327 A 7321 2537739 SLEEVE HUGHES 369 369E 4470707 WP ALLSN 250C 250C20B 03013 GL FUEL CONTROL ERRATIC A HEFR K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 21 911RP 1359 526E SLEEVE BROKEN AT GLUE JOINT. CAUSED ERRATIC FUEL CONTROL. 1 G 7 1 3U 3 U H3WE E4CE 2002042300050 20020423 00050 EU 2002 4 23 S4W2002F00001 1 20020410 A 3251 5322012134 ROD CAP PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE NOSE STEERING SEPARATED B S4WR K NONE O OTHER IN INSP/MAINT 1 WP 07 317NA 3032 223 ON 100 HOUR INSPECTION THE ROD END BEARING ON THE NOSE GEAR STEERING ORING WAS FOUND TO BE MIGRATING OUT OF THE ROD END ASSEMBLY. IF ROD END WAS NOT REPLACED AND THE BEARING MIGRATED ALL THE WAY OUT OF THE ROD END THEN STEERING CONTROL WOU LD BE LOST. THIS COULD BE POSSIBLY PREVENTED BY A SB FROM MFG, IMPLEMENTING A LARGE AREA WASHER ON THE BOTTOM OF THE RO D END OR AN EQUIVALENT FIX, THIS WOULD PREVENT THE BEARING FROM MIGRATING ALL THE WAY OUT OF THE ORING ROD END AND LOSIN G CONTROL OF NOSE WHEEL STEERING. THIS DISCREPANCY IS A RESULT OF NORMAL OPERATIONS, NOT A RESULT OF TOWING OR UNUSUAL OPERATIONS. 1 L 7 1 3T 4 T RT A78EU E26NE 2002042300051 20020423 00051 CE 2002 4 23 VJ32002F00021 1 20020409 A 3230 SM50D7 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MLG STUCK B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 1556A 118 CE1318 820455R LANDING GEAR FAILED TO EXTEND IN FLIGHT, GEAR WAS HAND CRANKED DOWN AND A SAFE LANDING WAS MADE. AIRCRAFT WAS PLACED ON JACKS AND THE LANDING GEAR CYCLED IAW MM. THE RELAY CONTROL WOULD STICK THREE OUT OF FOUR TIMES WHEN THE GEAR WAS CYCL ED. RELAY WAS REMOVED AND REPLACED WITH NEW. LANDING GEAR OPERATIONAL CHECK OF THE SYSTEM WAS MADE. LANDING GEAR CHEC KED NORMAL. PART SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002042300052 20020423 00052 CE 2002 4 23 WC72002F00000 1 20020401 A 2810 VALVE CESSNA 500 550 2076604 CE FUEL CELL STUCK B WC7R K NONE O OTHER IN INSP/MAINT 1 GL 25 91B 5500194 DURING A PREFLIGHT INSPECTION, WHILE DRAINING THE FUEL SUMP ON THE RIGHT WITN, THE DARIN VALVE BECAME STUCK IN THE OPEN POSITION. THE TOPPED OF WING WAS PROFUSELY DRAINING ON THE HANGER FLOOR. AFTER THE AIRCRAFT WAS DEFUELED AND THE DRAIN VALVE REMOVED. IT WAS DISCOVERED THAT A SMALL PLASTIC TUBE, POSSIBLY A PRIST NOZZLE, HAD WORKED ITS WAY THOUGH THE WIN G AND INTO THE DRAIN PREVENTING IT FROM CLOSING. 1 L 7 2 4F A22CE 2002042600140 20020426 00140 NM 2002 4 26 DLM88020399 1 20020403 A 3350 60030451 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DL 49543 FWD AUX EXIT LIGHTS FAILED TO OPERATE DURING LAYOVER CHECK. REPLACED POWER SUPPLY B5-103, OPS NORMAL. 2 L 7 2 4F RT A6WE 2002042600142 20020426 00142 NM 2002 4 26 DLM88020404 1 20020404 A 3350 41B004AD073 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 930DL 49717 AFT OVERWING OVERHEAD EMERGENCY LIGHTS INOP. REPLACED BATTERIES. 2 L 7 2 4F RT A6WE 2002042300056 20020423 00056 NM 2002 4 23 DLM11020407 1 20020403 A 5330 AGA73811 SKIN DOUG MD11 MD11 3023602 NM FS 1960, S-44L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 811DE 48566 FUSELAGE / SKIN / FS 1959-1964 / STRG. 43L-45L : DENT REPAIR THE FUSELAGE SKIN NEAR THE LOWER AFT CORNER OF THE AFT CARGO DOOR OPENING WAS BADLY DENTED BY GROUND EQUIPMENT. HFEC INSPECTION OF THE DENT REVEALED A SMALL CRACK. THE DENT WAS REMOVED WITH A 3" X 5.5" CUTOUT THROUGH THE SKIN AND UNDERLYING DOUBLER. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS INSTALLED PER ER/A 382873-14, REV B. 2 L 7 3 4F RT A22WE 2002042500073 20020425 00073 NM 2002 4 25 DL72S020426 1 20020411 A 5754 ANGLE BOEING 727 727232 1384082 NM L/E SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 A .375 INCH CRACK AT LWR SLAT COVE SKIN ATTACH ANGLE BELOW NR 6 SLAT TAI DUCT. REPAIRED PER M/M 57-54-000-8. 2 L 7 3 4F A3WE 2002042500087 20020425 00087 NM 2002 4 25 DL757020430 1 20020412 A 5330 141N33313 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 644DL 23998 THE FUSELAGE SKIN WAS FOUND WITH TWO GOUGES BETWEEN FS 410 & 420 AND BETWEEN STRINGERS 15L & 16L. THE GOUGES WERE REMOV ED WITH 2 CUTOUTS. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 382919-14. 2 L 7 2 4F RT A2NM 2002042600149 20020426 00149 NM 2002 4 26 DLM88020448 1 20020417 A 2910 AN8158 REDUCER DOUG MD88 MD88 3023688 NM NR 1 ENGINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 971DL 53214 LEFT HYD WENT TO ZERO LEFT HYD PRESS FAIL. LEFT REVERSER CONTROL VALVE LEAKING AT LOWER OUTBOARD B/NUT. REPLACED REDUC ER AND O-RING, RESECURED HYD LINE. NO FLUID CONTAMINATION IN APU INLET. CLEANED TAIL COMPT OF RESIDUAL FULID, LEAK CHE CKS GOOD. 2 L 7 2 4F RT A6WE 2002042500117 20020425 00117 NM 2002 4 25 DL757020451 1 20020416 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 THE FUSELAGE SKIN WAS FOUND GOUGED AT FS 460 BETWEEN STRINGERS 16L & 17L. THE GOUGE WAS REMOVED AND REPAIRED WITH EXTER NAL DOUBLERS PER ER/A 382910-14. 2 L 7 2 4F RT A2NM 2002042500119 20020425 00119 NM 2002 4 25 DL757020453 1 20020417 A 5310 146N871163 DOOR FRAME BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 644DL 23998 THE OUTER CHORD OF THE FS 1640 FRAME AT THE AFT GALLEY DOOR OPENING WAS FOUND GOUGED. TO FACILITATE REPAIR, THE DAMAGED SECTION OF FRAME WAS CUT AND REMOVED. A NEW SECTION WAS INSTALLED AND SPLICED WITH REPAIR CHANNELS PER ER/A 382808-14, REV A. 2 L 7 2 4F RT A2NM 2002042500122 20020425 00122 NM 2002 4 25 DL757020454 1 20020417 A 5330 146N35317 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 644DL 23998 THE FUSELAGE SKIN AT AN ANTENNA CUTOUT NEAR FS 1510 BETWEEN STRINGERS 28R & 29R WAS FOUND CORRODED. THE SKIN WAS CUTOUT TO REMOVE ALL DAMAGE. THE CUTOUT WAS REPAIRED PER ER/A 382820-14, REV A. 2 L 7 2 4F RT A2NM 2002042300057 20020423 00057 NM 2002 4 23 DL757020458 1 20020419 A 5220 D30655123 SLIDE BOEING 757 757232 1384965 NM 2R DOOR DEPLOYED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 639DL 23993 SLIDE DEPLOYED BY CABIN SERVICE_C/A REPLACED SLIDE 2 L 7 2 4F RT A2NM 2002042600154 20020426 00154 NM 2002 4 26 DLM88020462 1 20020421 A 2120 CLAMP DOUG MD88 MD88 3023688 NM A/C BAY LOOSE A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 928DL 49715 PASSING THROUGH 14000 FEET ON CLIMBOUT TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON. HIGH PRESSURE BLEED TURNED OFF, NO HEL P. RAN ABNORMAL CHECKLIST AND LIGHT WENT OUT AFTER TURNING OFF THE LEFT PACK. FOUND CLAMP LOOSE AND LEAKING DOWNSTREAM OF LEFT TEMP CONTROL VALVE. TIGHTENED SAME AND TIGHTENED OTHER CLAMPS IN AREA PRECAUTIONARY. 2 L 7 2 4F RT A6WE 2002042300058 20020423 00058 NM 2002 4 23 QXEA0200554 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X270 HAS LIGHT PITTING ON TOP FLANGE. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042300059 20020423 00059 NM 2002 4 23 QXEA0200555 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X300 TO X302 HAS LIGHT CORROSION PITS ON TOP FLANGE. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042300060 20020423 00060 NM 2002 4 23 QXEA0200556 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X315 TO X318 HAS LIGHT CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042300061 20020423 00061 NM 2002 4 23 QXEA0200557 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X342 HAS LIGHT CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042300062 20020423 00062 NM 2002 4 23 QXEA0200558 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X375 HAS LIGHT CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042300063 20020423 00063 NM 2002 4 23 QXEA0200559 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X390 TO X393 HAS LIGHT CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042300064 20020423 00064 NM 2002 4 23 QXEA0200560 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X404 TO X407 HAS LIGHT CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042300065 20020423 00065 NM 2002 4 23 QXEA0200561 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X421 TO X428 HAS LIGHT CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042300066 20020423 00066 NM 2002 4 23 QXEA0200562 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X467 HAS LIGHT CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042300067 20020423 00067 NM 2002 4 23 QXEA0200563 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X484 HAS LIGHT CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042300068 20020423 00068 NM 2002 4 23 QXEA0200564 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X489 HAS LIGHT CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042300069 20020423 00069 NM 2002 4 23 QXEA0200565 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X500 HAS LIGHT CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042300070 20020423 00070 NM 2002 4 23 QXEA0200566 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X532 HAS LIGHT CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-3644. 2 H 7 2 4T RT A13NM 2002042300071 20020423 00071 NM 2002 4 23 QXEA0200567 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT OUTBOARD SEAT TRACK X542 TO X545 HAS LIGHT CORROSION ON TOP FLANGE. REPAIRED IAW RD 8-53-3644. 2 H 7 2 4T RT A13NM 2002042300072 20020423 00072 NM 2002 4 23 QXEA0200568 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - RT INBOARD SEAT TRACK X545 INBOARD HOLE IS GOUGED. REPAIRED IAW RD 8-53-784. 2 H 7 2 4T RT A13NM 2002042300073 20020423 00073 NM 2002 4 23 QXEA0200569 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - RT INBOARD SEAT TRACK X505 TO 515 THERE ARE PITS IN THE CHANNEL SCRATCHES. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002042300074 20020423 00074 NM 2002 4 23 QXEA0200570 1 20020320 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LEADING EDGE PANEL 611AR OUTBOARD UPPER OUTBOARD NUT PLATE BRACKET APPEARS TO BE CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 4, TABLE 4. 2 H 7 2 4T RT A13NM 2002042300075 20020423 00075 NM 2002 4 23 QXEA0200571 1 20020320 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LEADING EDGE PANEL 611AR OUTBOARD LOWER NUT PLATE BRACKET APPEARS TO BE CRACKED. REPAIRED IAW DHC-8-200 SRM 51-40 -00. 2 H 7 2 4T RT A13NM 2002042300076 20020423 00076 NM 2002 4 23 QXEA0200572 1 20020322 A 5330 DOUBLER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LOWER TCAS ANTENNA MOUNT DOUBLER ON FUSELAGE CORRODED. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, PARAGRAPH B1 AND SRM 53-00-16. 2 H 7 2 4T RT A13NM 2002042300077 20020423 00077 NM 2002 4 23 QXEA0200573 1 20020321 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - CARGO DOOR SURROUND STRUCTURE HAS GOUGE ON DOOR SILL AT FORWARD STOP FITTING. REPAIRED IAW RD 8-53-5461. 2 H 7 2 4T RT A13NM 2002042300078 20020423 00078 NM 2002 4 23 QXEA0200574 1 20020321 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - CARGO DOOR SURROUND STRUCTURE HAS GOUGE ON DOOR SILL AT AFT STOP FITTING. REPAIRED IAW RD 8-53-5461. 2 H 7 2 4T RT A13NM 2002042300079 20020423 00079 NM 2002 4 23 QXEA0200575 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT INBOARD SEAT TRACK X500 THERE ARE CORROSION PITS ON TOP FLANGE AND IN CHANNEL. REPAIRED IAW RD 8-53-1339, STEP 5. 2 H 7 2 4T RT A13NM 2002042300080 20020423 00080 NM 2002 4 23 QXEA0200576 1 20020320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LT INBOARD SEAT TRACK X520 HAS CORROSION PITS IN CHANNEL. REPAIRED IAW RD 8-53-1339, STEP5. 2 H 7 2 4T RT A13NM 2002042300081 20020423 00081 NM 2002 4 23 QXEA0200577 1 20020320 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LEADING EDGE PANEL 511AL OUTBOARD UPPER NUT PLATE BRACKET APPEARS TO BE CRACKED IN RADIUS BEHIND NUT PLATE. REPAI RED IAW DHC-8-200 SRM 51-40-00, PAGE 4 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002042300082 20020423 00082 NM 2002 4 23 QXEA0200578 1 20020320 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LEADING EDGE PANEL 511AL OUTBOARD NUT PLATE BRACKET APPEARS TO BE CRACKED IN RADIUS BEHIND NUT PLATE. REPAIRED IA W DHC-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002042300083 20020423 00083 WP 2002 4 23 0201169922 1 20020415 A 2150 20495055 ACM DOUG DC9 DC932 3022066 WP A/C BAY DAMAGED A NWAA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 GL 01 945N 47664 CREW WAS UNABLE TO COOL THE CABIN DOWN WITH AIR CONDITIONING PRIOR TO DEPARTURE. THEN, DURING CLIMBOUT, CABIN DISPLAYED NONSTANDARD CLIMB PROFILE. VERY SLOW CLIMB TO ABOUT 17,000 FEET AND AS MAX DIFFERENTIAL WAS OBTAINED CABIN CONTINUED T O CLIMB AT 1000 FPM. AT FL310, THE CABIN PRESSURE WARNING LIGHT ILLUMINATED. CREW DECLARED AN EMERGENCY AND STARTED A RAPID DESCENT TO 10,000 FEET WHERE THE EMERGENCY WAS CANCELLED. FLIGHT CONTINUED TO A NORMAL LANDING AT MSP. MAINTENAN CE REPLACED THE RIGHT AIR CYCLE MACHINE AND THE RIGHT WATER SEPARATOR BAGS. BITE OF THE PRESSURIZATION SYSTEM CHECKED N ORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002042300084 20020423 00084 WP 2002 4 23 0201179859 1 20020414 A 2160 32185831 CONTROL VALVE DOUG DC9 DC951 3022051 WP A/C BAY FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 768 47729 DURING CLIMBOUT, THE CABIN FILLED WITH SMOKE AND THE RIGHT PACK DUCT TEMP WAS INDICATING ABOUT 150 DEGREES. CREW DECLAR ED AN EMERGENCY AND RETURNED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT TEMP CONTROL VA LVE AND THE CABIN TEMPERATURE CONTROL AMPLIFIER. REPLACED THE WATER SEPARATOR BAGS AND DID A HIGH POWER RUN TO CLEAR AN Y RESIDUAL OIL. A CONFIRMED SOURCE OF THE SMOKE WAS NEVER IDENTIFIED. THE AIRCRAFT HAS BEEN CLEARED FOR RETURN TO SERV ICE. 2 L 7 2 4F RT A6WE 2002042300085 20020423 00085 EU 2002 4 23 USAASA02034 1 20020405 A 3350 30665105 SLIDE RAFT AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE ESCAPE SLIDERAFT FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 104UW 8827 19 0863 THE EMERGENCY LIGHT TEST GENERATED AND (EPSU EXT LOAD AFT L) MESSAGE. MAINTENANCE REPLACE THE LEFT AFT ESCAPE SLIDE. E MERGENCY LIGHT TESTS OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2002042300086 20020423 00086 WP 2002 4 23 0201189152 1 20020418 A 2520 INSULATION DOUG DC9 DC914 3022034 WP CABIN OUT OF POSITION A NWAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 8911E 45825 JUST PRIOR TO THE FLIGHT LEVELING OFF AT FL290, THE CABIN PRESSURE WARNING LIGHT ILLUMINATED. CABIN ALTITUDE WAS 10,500 FEET WITH THE DIFFERENTIAL AT 5 PSI. CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FEET AND RETURNED TO DTW. NO MENTI ON OF COM COMPLIANCE OR IF THE MANUAL CONTROL FUNCTIONED AT ALL. CREW DID STATE THAT PACK INDICATIONS WERE NORMAL, OUTF LOW VALVE INDICATED FULL CLOSED, AND THAT THE FLIGHT ATTENDANTS REPORTED A HIGHER THAN NORMAL NOISE LEVEL NEAR THE REAR JUMPSEAT. LANDING AT DTW WAS WITHOUT INCIDENT. MAINTENANCE REMOVED THE AFT PRESSURE PLUG DOOR AND FOUND AN INSULATION BLANKET UNDER THE DOOR SEAL LIP. RE-ATTACHED THE BLANKET. PRESSURE CHECKS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002042300087 20020423 00087 WP 2002 4 23 0201199995 1 20020418 A 2780 DUCT DOUG DC9 DC931 3022065 WP L/E SLAT RATCHETING A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 8978E 47327 DURING APPROACH FOR LANDING INTO GRR, THE SLAT DISAGREEMENT LIGHT REMAINED ILLUMINATED AND THE AIRCRAFT ROLLED TO THE LE FT. FLIGHT CREW COMPLIED WITH COM PROCEDURES AND ACCOMPLISHED AN UNEVENTFUL NO SLAT LANDING AT GRR. CONTRACT MAINTENAN CE COULD NOT FIND ANY ABNORMALITIES AND COULD NOT DUPLICATE THE PROBLEM. ALL CHECKS WERE NORMAL. THE AIRCRAFT WAS CLEA RED FOR FERRY FLIGHT AND PROBLEM REPEATED ON APPROACH INTO DTW. DTW MAINTENANCE NOTED A SLIGHT RATCHETING ON THE RIGHT T-DUCT DURING OPERATION. THE T-DUCT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002042300088 20020423 00088 EU 2002 4 23 USAASA02033 1 20020401 A 3350 LIGHT AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE WIRE DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 713UW 1040 THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE AT THE LEFT SIDE ROW 4 SEATS. MAINTENANCE RECONNECTED THE WIRING UNDERNEATH THE SEAT. OPERATIONALLY CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2002042300089 20020423 00089 NM 2002 4 23 0201206743 1 20020410 A 2920 HYDRAULIC LINE BOEING 747 747249F 1384849 NM HYD SYSTEM LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 GL 01 643NW 22245 DURING FLIGHT, LOST HYDRAULIC FLUID IN THE NR 2 HYDRAULIC SYSTEM. PERFORMED COM PROCEDURES AND THE AIRCRAFT CONTINUED T O DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE HYDRAULIC RETURN LINE AT THE RIGHT INBOARD AILERON POWER CONTRO L UNIT. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002042300090 20020423 00090 NM 2002 4 23 0201216301 1 20020418 A 3040 SWITCH BOEING 747 747451 1384940 NM COCKPIT MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 661US 23719 DURING FLIGHT, THE CAPTAIN'S WINDOW ARCED AND SMOKED. TURNED OFF WINDOW HEAT AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPAIRED WIRE AND INSULATED TERMINAL ON WINDOW 2L OVERHEAT SWITCH. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002042300091 20020423 00091 NM 2002 4 23 0201226311 1 20020418 A 2121 FAN BOEING 747 747451 1384940 NM E/E BAY FAILED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 671US 26477 DURING FLIGHT, AN ELECTRICAL BURNING SMELL EMITTED IN THE AREA OF DOOR 1R. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE EQUIPMENT COOLING EXHAUST FAN. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002042300092 20020423 00092 NM 2002 4 23 0201236311 1 20020416 A 2530 OVEN BOEING 747 747451 1384940 NM GALLEY MALFUNCTIONED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 671US 25477 DURING FLIGHT, AN ELECTRICAL BURNING SMELL EMITTED IN THE AREA OF DOOR 1R. THE SMELL DISSIPATED DURING DESCENT AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED OVENS 1-24 AND 1-25. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002042300093 20020423 00093 EU 2002 4 23 USAASA02032 1 20020331 A 3350 32145410 PSEU AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE PASSENGER CABIN FAULTY A USAA K NONE O OTHER NR NOT REPORTED 1 EA 19 764US 4041 1369 THE CENTER AISLE EMERGENCY LIGHTS BLINK ON AND OFF. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2002042300094 20020423 00094 WP 2002 4 23 AT0200049 1 20020418 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DAMAGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 823AT 47529 AFT ESCAPE SLIDE EMERGENCY LIGHT DOES NOT ILLUMINATE (FOUND B5-28 BATTERY PACK NICAD BATTERY BLEW UP). REMOVED AND REPL ACED B5-28 BATTERY PACK AND NICAD BATTERY. OPS CHECK GOOD IAW DC-9 MM 33-53. 2 L 7 2 4F A6WE 2002042300095 20020423 00095 NM 2002 4 23 AWXA200200353 1 20020420 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 308AW 24710 PHX - EEL - EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WILL NOT ILLUMINATE. MAINTENANCE REPLACED EMERGENCY ESCAPE PA TH LIGHT ASSEMBLY AT SEAT ROW 19 LT, FUNCTIONAL CHECK WAS GOOD IAW A1C33006. 2 L 7 2 4F RT A16WE 2002042300096 20020423 00096 NM 2002 4 23 AWXA200200354 1 20020420 A 2560 P4010021 BATTERY BOEING 737 7373B7 1384580 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 332AW 23384 PHX - EMERGENCY EQUIPMENT - EMERGENCY FLASHLIGHT IN AFT GALLEY HAS LOW BATTERY VOLTAGE. MAINTENANCE REPLACED BATTERIES IN THE EMERGENCY FLASHLIGHT IN AFT GALLEY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002042300097 20020423 00097 SO 2002 4 23 C2XA02CL101 1 20020419 A 2530 CBC16707 RECEPTACLE EMB 135 EMB135LR 3260305 SO GALLEY BURNED A C2XA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 17513 145292 CLE FLIGHT 2955 THE FLIGHT ATTENDANT REPORTED A SMOKE SMELL IN THE GALLEY IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT COFFEE WARMER AND THE CONNECTOR RECEPTACLE. OPERATIONAL CHECKS WERE GOOD. COFFEE WARMER (P/N 1095A). 2 L 7 2 4F RT T00011AT 2002042300098 20020423 00098 SO 2002 4 23 C2XA02CL102 1 20020420 A 3350 66369 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16502 145166 CLE MAINTENANCE FOUND THE CABIN EMERGENCY AISLE LIGHT INOPERATIVE DURING ROUTINE MAINTENANCE. MAINTENANCE REPLACED THE EMERGENCY AISLE LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002042300099 20020423 00099 NM 2002 4 23 CALA0200220 1 20020419 A 5720 SUPPORT BOEING 737 737824 13844BZ NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12218 28778 INSPECTION FOUND RT WING UPPER PANEL SUPPORT DIRECTLY BEHIND NR 2 ENGINE EXHAUST T/E OF WING CRACKED THROUGH. THE SUPPO RT WAS REMOVED AND REPLACED IAW SRM 51-40. 2 L 7 2 4F RT A16WE 2002042300100 20020423 00100 NM 2002 4 23 CALA0200224 1 20020420 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 294-312, RBL 15. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-1 0-02. 2 L 7 2 4F RT A16WE 2002042300101 20020423 00101 NM 2002 4 23 CALA0200226 1 20020421 A 3350 20121 CHARGER BOEING 757 757224 1384958 NM CABIN FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 26123 28966 INSPECTION FOUND R-2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERAT IONAL CHECKS WERE GOOD IAW FIM 33-51-00. 2 L 7 2 4F RT A2NM 2002042300102 20020423 00102 NM 2002 4 23 CALA0200228 1 20020421 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNEL CORRODED AT STA 727D+5, LBL 12. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5320-01603. 2 L 7 2 4F RT A16WE 2002042300103 20020423 00103 EU 2002 4 23 USAASA02036 1 20020410 A 3350 32145410 P-LEAD AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE PASSENGER CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 700UW 3594 0885 AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. 2 L 7 2 4F 4 F RT A28NM E2GL 2002042300104 20020423 00104 NM 2002 4 23 CALA0200234 1 20020422 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 727-767 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND L/H O/B SEAT TRACK HAD PITTING CORROSION AT STA 727-767. A SEAT TRACK REPAIR WAS INSTALLED IAW SRM 53-0 0-52, FIGURE 204. 2 L 7 2 4F RT A16WE 2002042300105 20020423 00105 NM 2002 4 23 CALA0200235 1 20020422 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 947 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND A 3/4" CRACK IN FUSELAGE SKIN FORWARD OF L-2 DOOR FUSELAGE TORQUE TUBE ACCESS PANEL AT STA 947 BETWEEN STRINGER 10 AND 11L. THE CRACKED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-60-01. 2 L 7 2 4F RT A16WE 2002042300106 20020423 00106 CE 2002 4 23 GLBA2002055 1 20020420 A 2800 3038472 FLOW DIVIDER BEECH 1900 1900D 1154162 CE RIGHT LEAKING A GLBA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 NM 03 251GL 670 UE251 FUEL ODOR IN COCKPIT ON TAXI, INSPECTED FOUND RIGHT FUEL FLOW DIVIDER LEAKING, REPLACED OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2002042300107 20020423 00107 EU 2002 4 23 USAABA02010 1 20020417 A 3350 321430 PSEU AIRBUS 330 A330323 3930335 EU L1,R2 DOORS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 672UW 0333 FOUND EPSU FAILED AT DOORS L1 AND 2R. MAINTENANCE REPLACED BOTH EPSU. 2 L 7 2 4F RT A46NM 2002050200074 20020502 00074 NM 2002 5 2 2002UALA00708 1 20020415 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 CABIN FLOORBEAM STATION 1640 DAMAGED AND CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002050200075 20020502 00075 NM 2002 5 2 2002UALA00709 1 20020412 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 AFT CARGO PIT FRAME STATION 1280 LBL 23 IS GOUGED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND INSTALLED TWO REPAIR STRAPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2002042300108 20020423 00108 NM 2002 4 23 2002UALA00710 1 20020412 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT PIT FRAME BODY STATION 1620 ABOVE STRINGER 26R EDGE DAMAGED FROM DRILL START. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.DOUBLER REPAIR APPLIED TO WEB AND INBD CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002050200077 20020502 00077 NM 2002 5 2 2002UALA00723 1 20020416 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 CABIN FLOORBEAM UPPER CAP HAD CORROSION ON UNDER SIDE AT STATION 365 AT APPROX RBL 36 STRINGER 17R. MAJOR REPAIR ACCOMP LISHED. REMOVED PORTION OF UPPER T-CAP AND USED SPLICE REPAIR IN INSTALLING NEW UPPER T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002050200078 20020502 00078 NM 2002 5 2 2002UALA00724 1 20020416 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 AFT PIT STATION 1638, LT CREASE BEAM, OUTER CHORD ANGLE CORRODED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002042300109 20020423 00109 NM 2002 4 23 2002UALA00731 1 20020418 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 AFT PIT STATIO 1400 BETWEENS TATION 25L AND 26L FRAME IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002042300110 20020423 00110 NM 2002 4 23 2002UALA00732 1 20020419 A 5315 THRESHOLD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 AFT CARGO PIT THRESHOLD LOWER BEAM PREVIOUS REPAIR HAD SEVERE EXFOLIATION CORROSION AT REPAIR ANGLE AND BOTH SPLICE PLA TES STATION 1436 TO STATION 1383. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. INSTALLED FILLER SECTION AND TWO EA REPAIR ANGLES. 2 L 7 2 4F 4 F RT A2NM E17NE 2002042300111 20020423 00111 NM 2002 4 23 2002UALA00733 1 20020418 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 THREE EACH DENTS IN SKIN AT STATION 406, STRINGER 36R ARE OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPAIR D OUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002042300112 20020423 00112 NM 2002 4 23 2002UALA00735 1 20020418 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 FWD CARGO DOOR, FWD FRAME IS CRACKED AROUND S152 SENSOR BRACKET. MAJOR REPAIR ACCOMPLISHED. REPAIRED FORWARD DOOR FRAME . 2 L 7 2 4F 4 F RT A1NM E24NE 2002042300113 20020423 00113 NM 2002 4 23 2002UALA00736 1 20020418 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT CARGO, FUSE SKIN CORRODED BODY STATION 1197+117, ADJACENT TO STRINGER 37L, INTERNAL SKIN. MAJOR REPAIR ACCOMPLISHED . FABRICATED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002042300114 20020423 00114 NM 2002 4 23 2002UALA00738 1 20020418 A 5313 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 FWD PIT, BODY STATION 406 RIGHT HAND, SHEAR TIE BETWEEN STRINGER 36R AND STRINGER 35R, REQUIRES FABRICATION FOR SKIN REP AIR. MAJOR REPAIR ACCOMPLISHED. FABRICATED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002042300115 20020423 00115 NM 2002 4 23 2002UALA00739 1 20020418 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 RIGHT HAND FUSE SKIN STATION 1820, REAR EDGE OF H-STAB TO FUSE FAIRING SKIN HAS DEPTH CHAFFING FROM FAIRING. MAJOR REPA IR ACCOMPLISHED. FABRICATED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002042300116 20020423 00116 2002 4 23 DHL2002363004 4 20020418 A 2230 AUTOTHRUST SYS AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 01 363DH 85 DURING T/O THE AUTO THROTTLE PULLED THE THRUST LEVERS BACK. REJECTED AT 70 KTS. CKD WIRING BETWEEN N1 SENSORS ON BOTH ENGINES AND N1 LIMIT COMPUTER, PERFORMED WIRE PULL CK BEHIND N1 COMPUTER. CKD TERMINALS BLOCK 81VT 18 & 19 NO DEFECTS. PERFORMED OPS CHECK OF PREVIOUSLY CHANGED NR 2 ENG N1 SENSOR, GROUND RAN BOTH ENGS T/O MAX & FLEX WITH A/T CONTROLLING SEVERAL TIMES. REACHED AND HELD TARGET SEVERAL TIMES IAW 22-31-00 & 31-42-00. 2 L 7 2 4F RT A35EU 2002042300117 20020423 00117 NM 2002 4 23 DHL2002705004 1 20020418 A 5320 SUPPORT BOEING 727 72722C 138400F NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 DURING DROP IN CHECK STA 870 WL 186 RBL 42, SUPPORT ANGLE HAS CORROSION BEHIND SPOILER MIXER. CUT OUT CORROSION ON SUPP ORT ANGLE. FABRICATED AND INSTALLED REPAIR. 2 L 7 3 4F A3WE 2002042300120 20020423 00120 NM 2002 4 23 DHL2002727004 1 20020420 A 3350 BATTERY PACK BOEING 727 727228 1384083 NM CABIN NOT SEATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 MAIN ENTRY DOOR EMERGENCY EXIT LIGHT DIM. RESEATED BATTERY PACK IN EXIT LIGHT ASSY. OPS CHECKS NORMAL IAW B727 M/M CH 33-50. 2 L 7 3 4F RT A3WE 2002042300121 20020423 00121 WP 2002 4 23 DHL2002802004 1 20020418 A 2612 CONNECTOR DOUG DC8 DC873 302199C WP FIRE LOOP DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802DH 46076 ENGINE COMP FIRE DET LOOP-B ON ENG NR 2 DOES NOT TEST. CLEANED AND RESECURED NR 2 ENG B-LOOP CONNECTOR AT MEC FAN LOOP AREA IAW M/M 26-10-1, OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2002042300122 20020423 00122 WP 2002 4 23 DHL2002807538 1 20020326 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 81797 45990 MID-SHIP ACCY COMPT - INTERCOSTAL WITH CRACK IN IT AT STA 660 - 680, L25R. REMOVED DAMAGED INTERCOSTAL IAW SRM 53-2-0 F IG 1B. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2002042300123 20020423 00123 EU 2002 4 23 MALA020249 1 20020409 A 5280 DOOR BAC 146 AVRO146RJ85A 1500097 EU RT MLG CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 535XJ E2371 DURING C1 CHECK, CHAFE MARKS ON RT GEAR RT DOOR (MLG) LOWER FORWARD. MAINTENANCE REPAIRED IAW LOWER FWD CORNER REPAIRED IAW BAE FAX BARA/AVR/1006/02-CV. 2 H 7 4 4F RT A49EU 2002042300124 20020423 00124 EU 2002 4 23 MALA020250 1 20020409 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 535XJ E2371 WHILE INSPECTING AC 535, OUT OF CVG, MAINTENANCE REPAIRED DENT IN FUSELAGE AND ASSOCIATED DAMAGE AT FRAMES 9, 10 & 11 IA W REPAIR OF FUSELAGE DENT AND ASSOCIATED DAMAGE AT FRAMES 9, 10 AND 11 IAW EO A53078. 2 H 7 4 4F RT A49EU 2002042300125 20020423 00125 EU 2002 4 23 MALA020251 1 20020409 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 535XJ E2371 WHILE IN C-CHECK, IN CVG, REPAIR OF FUSELAGE DENT AT FRAME 4 IAW EO A53077. 2 H 7 4 4F RT A49EU 2002042300126 20020423 00126 EU 2002 4 23 MALA020252 1 20020413 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 441XJ 340B441 DURING 4K-CHECK IN CWA, LT FUSELAGE DENTED BETWEEN 355, AND 359.5, JUST BELOW FUSELAGE DOUBLER, REPAIRED IAW EO 53009. 2 L 7 2 4T RT A52EU 2002042300127 20020423 00127 EU 2002 4 23 MALA020253 1 20020414 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 441XJ 340B441 WHILE IN CWA, FOR 4K-CHECK, LT CENTER AISLE SEAT TRACK FWD PORTION HAS CORROSION. MAINTENANCE REPLACED A 32 INCH SECTIO N OF THE SEAT TRACK STARTING AT 297.0 GOING AFT IAW EO 53060. 2 L 7 2 4T RT A52EU 2002042300128 20020423 00128 EU 2002 4 23 MALA020254 1 20020414 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 441XJ 340B441 DURING 4K INSPECTION IN CWA, MAINTENANCE FOUND TOP FRAME FLANGE AND ANGLE AT STA 258 CORRODED. MAINTENANCE REPAIRED IAW EO 53102. 2 L 7 2 4T RT A52EU 2002042300129 20020423 00129 EU 2002 4 23 MALA020255 1 20020413 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 441XJ 340B441 DURING 4K INSPECTION RT FUSELAGE DENTS BETWEEN STA 356 TO 339. MAINTENANCE REPAIRED RT FUSELAGE DENTS BETWEEN STA 356 T O 339 SL1617 & SL1618. REPAIRED IAW EO 53005. 2 L 7 2 4T RT A52EU 2002042300130 20020423 00130 EU 2002 4 23 MALA020256 1 20020418 A 7933 4053T73P01 SENSOR SAAB SF340 SF340A 7850100 EU RT ENGINE FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 362XJ DURING FLIGHT 2845, RT PROP OIL TEMP FLUCTUATES INFLIGHT. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED PGB OIL TEMP SENSOR, IAW AMM 79-30-10. OPS CHECKS AND LEAK CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002042900076 20020429 00076 EU 2002 4 29 MALA020257 1 20020418 A 7603 CONTROLLER SAAB SF340 340B 7860101 EU LT ENGINE FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 367XJ DURING FLIGHT 2822, FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED AFTER T/O. AIR RETURN TO DTW. MAINTENANCE RESET F1 STOP, O K CHECK NOT GOOD AT THIS TIME. WITH POWER LEVERS OFF, LT POWER LEVER GOES BELOW F1. MAINTENANCE REMOVED AND REPLACED C ONTROL QUADRANT. ALL GROUND RUNS CHECK OK. 2 L 7 2 4T RT A52EU 2002042300131 20020423 00131 2002 4 23 MALA020258 4 20020418 A 2561 LIFE VEST BAC 146 AVRO146RJ85A 1500097 EU CABIN UNSECURE A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 515XJ E2333 ON FLIGHT 3525, SEAT 3B/C LIFE VESTS NEED TO BE SECURED UNDER SEAT. MAINTENANCE RESECURED SEATS, ALL CHECKS GOOD AT THI S TIME. 2 H 7 4 4F RT A49EU 2002042300132 20020423 00132 NM 2002 4 23 PCAA0204048 1 20020418 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DISCONNECTED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT LEFT AFT FLOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. LIGHT CONNECTION FOUND UNPLUGG ED. CONNECTION PLUGGED IN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042300133 20020423 00133 NM 2002 4 23 DHL2002753001 1 20020423 A 2611 100064901 SMOKE DETECTOR BOEING 727 727223 1384074 NM A DHLA K NONE L NO TEST UK UNKNOWN 1 SO 01 712AA 22468 1) LOWER CARGO SMOKE DETECTION SYS INOP.2) DEFERED IAW MEL REF 26-19 CTRL#9097 ASSIGNED CAT C PLACARD INSTALLED.3) REF D MI 9097, LOWER CARGO SMOKE DETECTION SYSTEM INOP.4) FOUND AFT DETECTOR AT FAULT. R&R AFT SDU IAW DHL M/M SUPP 26-16-01. PERF ADJ AND TEST OF SMOKE DETECTOR SYSTEM IAW DHL M/M SUPP 26-16-01. THIS CLEARS DMI 9097. PLACARD REMOVED. 2 L 7 3 4F A3WE 2002042300134 20020423 00134 WP 2002 4 23 MWEA020267 1 20020423 A 5330 591142485 SKIN DOUG DC9 DC932 3022066 WP STATION 948 TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 AFT PIT SKIN HAS TOOLING DAMAGE @ FS 948 ABOVE LONGERON 26 RIGHT. -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002042300135 20020423 00135 WP 2002 4 23 IXXA0200018O 1 20020418 A 7100 COWLING DOUG DC8 DC871 302199A WP #1 ENGINE DAMAGED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 829BX 81552 1625 45994 DURING A ROUTINE MAINTENANCE PREFLIGHT IN TER, MINOR EVIDENCE OF DAMAGE TO #1 ENGINE OUTBOARD COWLING. MAINTENANCE INSPE CTED THE ENGINE IN ACCORDANCE WITH AN APPROVED DER ENGINEERING DIRECTIVE EDQ11-1. NO ADDITIONAL DAMAGE WAS NOTICED AND T HE ENGINE PERFORMANCE WAS NORMAL. REPLACED THE COWLINGS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002042300136 20020423 00136 EU 2002 4 23 RAIA00204130 1 20020419 A 2613 51228801 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU CHAFED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 567HK 41085 5639-STL - RIGHT OVERHEAT WARNING CAME ON DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVER HEAT SENSOR WIRE. 2 L 7 2 4T RT A41NM 2002042300137 20020423 00137 GL 2002 4 23 RAIA00204131 3 20020419 A 6110 C5JFR36C1104D PROPELLER JETAIR JETSTM JETSTM4101 1500501 EU MCAULY 5JFR C5JFR36C1104 GL VIBRATES A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 560HK 12777 4070 41076 950662 5645-STL - CREW REPORTED RIGHT ENGINE VIBRATION. MAINTENANCE REMOVED AND REPLACED RIGHT PROPELLER ASSEMBLY. 2 L 7 2 4T RT A41NM 5 C P15NE 2002042300138 20020423 00138 SO 2002 4 23 RAIA00204132 1 20020421 A 3040 90024252 CONTROLLER EMB 145 EMB145ER 3260211 SO INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 808HK 5790 4184 145157 5258-PIT- BOTH WINDSHIELD WIPERS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED WINDSHIELD WIPER CONTROLLER. 2 L 7 2 4F RT T00011AT 2002042400001 20020424 00001 EA 2002 4 24 A6WA200240008 1 20020320 A 2752 853D10017 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION CR CRUISE 1 GL 31 421ZW 7346 FLAPS FAIL AT 14 DEGREES IN FLIGHT, COMPLIED WITH QRH AFTER LANDING, LEFT OUTBOARD FLAP IS TWISTED. REMOVED AND REPLACE D NR 3 LEFT FLAP ACTUATOR. (M) 2 L 7 2 4F RT A21EA 2002042400002 20020424 00002 EA 2002 4 24 A6WA200240009 1 20020322 A 2150 SWITCH CNDAIR CL600 CL6002B19 1900309 EA ROTORY COOL FAILED A A6WA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 31 401AW 7280 DISPLAY COOL MESSAGE IN FLIGHT MAINTENANCE REMOVED AND REPLACED DISPLAY COOL ROTARY SWITCH. OPERATIONAL CHECK GOOD. (M ) 2 L 7 2 4F RT A21EA 2002042400003 20020424 00003 NM 2002 4 24 ASAA0210053 1 20020214 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROWS 7 AND 8 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AT ROWS7 AND 8, THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002042400004 20020424 00004 NM 2002 4 24 ASAA0210056 1 20020305 A 3350 86210144 BATTERY BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 19 AND 20 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002042400005 20020424 00005 NM 2002 4 24 ASAA0240024 1 20020226 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 764AS 25101 PDX - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS INOPERATIVE AT ROW 20. RECONNECTED LOOSE WIRES OPERATIONAL CHECK NORM AL. (M) 2 L 7 2 4F RT A16WE 2002042400006 20020424 00006 NM 2002 4 24 ASAA0240028 1 20020307 A 3397 WIRE BOEING 737 7374Q8 138447Q NM ROW 12-15 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 PDX - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 12-15 INOPERATIVE. RECONNECTED WIRES, OPERATIONS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2002042400007 20020424 00007 WP 2002 4 24 ASAA0280059 1 20020301 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP FWD CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 LAS - DURING PREFLIGHT CHECK, 1ST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. RECONNECTED WI RING BETWEEN MODULES AT ROW 2. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002042400008 20020424 00008 WP 2002 4 24 ASAA0280060 1 20020301 A 3397 0105606 WIRE DOUG DC9 DC982 3022082 WP FWD CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 PDX - DURING PREFLIGHT CHECK, 1ST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. REPAIRED BROKE N WIRING BETWEEN MODULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002042400009 20020424 00009 WP 2002 4 24 ASAA0280061 1 20020302 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP FWD CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE IN FIRST CLASS CABIN. REPLACED ASSOCIAT ED BATTERY POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002042400010 20020424 00010 WP 2002 4 24 ASAA0280062 1 20020304 A 3350 1001191 BATTERY DOUG DC9 DC983 3022083 WP FWD PAX ENTRY DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 40498 849 53063 OAK - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT. OP TESTED OK. (M) 2 L 7 2 4F RT A6WE 2002042400011 20020424 00011 NM 2002 4 24 RIVA020308 1 20020308 A 5514 BEAM BOEING 727 7272J0 138407E NM HORIZONTAL STAB CORRODED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 MQY - FOUND RIGHT HORIZONTAL STAB UPPER TRAILING EDGE BEAM AT REAR SPAR STATION 151.81 HAS CORROSION. FOUND TO BE OUT O F LIMITS IAW B727 SRM 55=10-1, FIG 1. REMOVED AND REPLACED TRAILING EDGE BEAM IAW B727 SRM 51-30-5 AND B727SRM 51-30-2. PART REPLACED WITH IDENTICAL PART NR. NO WEIGHT CHANGE. (M) 2 L 7 3 4F RT A3WE 2002042400012 20020424 00012 NM 2002 4 24 RIVA0203081 1 20020308 A 5521 RIB BOEING 727 7272J0 138407E NM RT ELEVATOR PUNCTURED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 MQY - FOUND RIGHT ELEVATOR UPPER SKIN STATION 173 LOWER RIB PUNCTURED 3 PLACES. FABRICATED REPAIR DOUBLER IAW B727 SRM 55-20-3. TREATED AND PRIMED IAW B727 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-30-2. APPRECIABLE WEIGHT ADDED BY THI S REPAIR .120 LB AT STATION 173. CALCULATION IAW B727 SRM 51-80-7, PAGES 1 AND SHOWS REPAIR MOMENT REQUIRES NO ADDITION AL OF REBALANCE WEIGHTS. (M) 2 L 7 3 4F RT A3WE 2002042400013 20020424 00013 NM 2002 4 24 RIVA020308A 1 20020308 A 5754 SKIN BOEING 727 7272J0 138407E NM LE FLAP BROKEN A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 MQY - FOUND LEFT WING INBOARD FLAP INBOARD END OF FORE FLAP UPPER SURFACE SKIN IS WORN AND HAS PIECES BROKEN OFF WS 220. REMOVED DAMAGED SECTION. FABRICATED FILLER DOUBLER AND INSTALLED PER EO NR 01-298 WITH APPROVED 8110-3. APPRECIABLE WEIGHT ADDED BY THIS REPAIR .200 LB AT WS 200. (M) 2 L 7 3 4F RT A3WE 2002042400014 20020424 00014 NM 2002 4 24 RIVA020308B 1 20020308 A 5310 DOOR FRAME BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 MQY - FOUND R-1 DOOR LOWER FORWARD CORNER WEB CRACKED 2.5 INCHES LENGTH STATION 380, STRINGER 17R. CUT OUT DAMAGED SECT ION. FABRICATED NEW SECTION AND SPLICES AND INSTALLED PER EO NR 01-298 WITH APPROVED 8110-3. APPRECIABLE WEIGHT ADDED BY THIS REPAIR IS .680 STATION 380. (M) 2 L 7 3 4F RT A3WE 2002042400015 20020424 00015 NM 2002 4 24 RIVA020308C 1 20020308 A 5310 DOOR FRAME BOEING 727 7272J0 138407E NM FUSELAGE CORRODED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 MQY - FOUND R-1 DOOR AFT JAMB HAS CORROSION AT UPPER CAM FITTING STATION 420. CUT OUT DAMAGED AREA. FABRICATED FILLER/ REPAIR ANGLE AND INSTALLED PER EO NR 01-298 WITH APPROVED 8110-3. APPRECIABLE WEIGHT ADDED BY THIS REPAIR IS .55 LB STA TION 420. (M) 2 L 7 3 4F RT A3WE 2002042400016 20020424 00016 NM 2002 4 24 RIVA020308E 1 20020308 A 5315 FLOORBEAM BOEING 727 7272J0 138407E NM FUSELAGE CORRODED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 MQY - FOUND FLOORBEAM CORRODED AT STATION 1110 FROM LBL 45 INCHES TO RBL 20 INCHES HAS BEEN BLENDED TO LIMITS IAW B727 S RM 53-10-1, FIG 4. CORROSION STILL EXISTS IN AREA. REMOVED AND REPLACED UPPER T-CHORD AT STATION 1110 LBL 69 TO RBL 34 .5 IAW B727 SRM 53-10-8, 51-10-2 AND EO NR 01-298 WITH APPROVED 8110-3. APPRECIABLE WEIGHT ADDED BY THIS REPAIR IS .480 LB AT STATION 1110. (M) 2 L 7 3 4F RT A3WE 2002042400017 20020424 00017 NM 2002 4 24 RIVA020308F 1 20020308 A 5315 FLOORBEAM BOEING 727 7272J0 138407E NM FUSELAGE CORRODED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 MQY - FOUND STATION 344 FLOORBEAM CORROSION REMOVED TO MAX LIMITS PER SRM. CORROSION STILL EXISTS RBL 25 INCHES - LBL 2 5 INCHES. REMOVED DAMAGED SECTION AND REPLACED WITH NEW T-CAP AND SPLICES IAW B727 SRM 53-10-8, 51-30-2 AND 51-10-2. N EW REPLACEMENTS PARTS USED. NO CHANGE IN WEIGHT. (M) 2 L 7 3 4F RT A3WE 2002042400018 20020424 00018 NM 2002 4 24 RIVA020308G 1 20020308 A 5315 FLOORBEAM BOEING 727 7272J0 138407E NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 FOUND STATION 380 FLOORBEAM CORROSION. REMOVED TO MAX LIMITS PER SRM. CORROSION STILL EXISTS RBL 13 INCHES - 33 INCHES RBL. REMOVED EXISTING REPAIR T-CAP. FABRICATED NEW SECTION AND INSTALLED IAW B727 SRM 53-10-8, FIG 3 AND 51-10-2, 51- 30-2. NEW REPLACEMENT PARTS USED. NO CHANGE IN WEIGHT. (M) 2 L 7 3 4F RT A3WE 2002042400019 20020424 00019 NM 2002 4 24 RIVA020308H 1 20020308 A 5315 FLOORBEAM BOEING 727 7272J0 138407E NM FUSELAGE CORRODED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 MQY - FOUND STATION 400 FLOORBEAM CORROSION REMOVED TO MAX LIMITS PER SRM. CORROSION STILL EXISTS LBL 18 INCH - RBL 15 I NCH. REMOVED AND INSTALLED REPAIR SECTION T-EXTRUSION IAW B727 SRM 53-10-8, FIG 3 AND 51-10-2. NEW REPLACEMENT PARTS U SED. NO CHANGE IN WEIGHT. (M) 2 L 7 3 4F RT A3WE 2002042400020 20020424 00020 NM 2002 4 24 RIVA020308J 1 20020308 A 5315 FLOORBEAM BOEING 727 7272J0 138407E NM FUSELAGE CORRODED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 MQY - FOUND FLOORBEAM STATION 420 RBL 3 INCH CORROSION BLEND TO LIMITS IAW B727 SRM 53-10-1, FIG 4 CORROSION STILL EXIST S. CUT OUT CORRODED AREA PER B727 SRM 53-10-8, FIG 8. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-10-8, FIG 8. APPRECIABLE WEIGHT ADDED BY THIS REPAIR .92 LB AT STATION 420. (M) 2 L 7 3 4F RT A3WE 2002042400021 20020424 00021 NM 2002 4 24 RIVA020308K 1 20020308 A 5315 FLOORBEAM BOEING 727 7272J0 138407E NM FUSELAGE CORRODED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 MQY - FOUND FLOORBEAM STATION 328 UPPER FLANGE CORRODED BEYOND LIMITS LBL 30 INCHES AND RBL 13 INCHES UPPER AND LOWER SU RFACES. REMOVED DAMAGED SECTION IAW B727 SRM 53-10-8. FABRICATED REPAIR SECTION AND SPLICES IAW B727 SRM 53-10-8. TRE ATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 53-10-8. APPRECIABLE WEIGHT ADDED BY THIS REPAIR 1.57 LBLS AT STA 328. (M) 2 L 7 3 4F RT A3WE 2002042400022 20020424 00022 NM 2002 4 24 RIVA020308L 1 20020308 A 5753 SKIN BOEING 727 7272J0 138407E NM TE FLAPS DAMAGED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 MQY - FOUND LEFT OUTBOARD FORE FLAP TRAILING EDGE DAMAGE APPROX 2 INCH BY 5 INCH AT WS 491. CUT OUT DAMAGED AREA. FILL ED VOID AREA. FABRICATED UPPER AND LOWER SKIN DOUBLERS. TREATED PRIMED PER EO NR 01-298 WITH APPROVED 8110-3. APPRECI ABLE WEIGHT ADDED BY THIS REPAIR .200 LB AT WS 491. (M) 2 L 7 3 4F RT A3WE 2002042400023 20020424 00023 NM 2002 4 24 RIVA020308M 1 20020308 A 5310 DOOR FRAME BOEING 737 737300 1384610 NM CARGO BAY CRACKED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 362PA 21106 MQY - NR 3 CARGO DOOR STATION1090 FRAME HAS CRACK BETWEEN STRINGERS 26R AND 27R. ROUTED OUT CRACK. FABRICATED REPAIR A NGLES AND FILLERS. TREATED AND PRIMED AND INSTALLED REPAIR ANGLES AND FILLERS PER BOEING REPAIR SKETCH TEK MQY 02-0001F WITH 8110-3, DATED 01/17/02. (M) 2 L 7 2 4F RT A16WE 2002042400024 20020424 00024 NM 2002 4 24 TSAA0221093 1 20020310 A 2131 7638102 CONTROLLER BOEING 737 737230 1384401 NM CABIN PRESSURE FAILED A TSAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 WP 13 820AL 22138 FLT 66 - HNL-OGG - PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED AT 14,000 FT AND STANDBY LIGHT CAME ON. SWITCHED TO STAND BY MODE. CABIN RATE STARTED CLIMBING AND DESCENDING AT 4,000 FPM. SWITCHED TO MANUAL DC THEN AC MODE AND STILL UNABLE TO CONTROL PRESSURIZATION. DECLARED AN EMERGENCY AND DESCENDED TO 5400 FEET AND UNABLE TO CONTROL PRESSURE. UNEVENTFUL LANDING IN OGG. AIRCRAFT FERRIED TO HNL. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. GROUND CHECKED OK PER MM 21 -31-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002042400025 20020424 00025 NM 2002 4 24 TSAA0251084 1 20020226 A 5310 6545766 WINDOW FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10R ON WINDOW NR 26 RIGHT LOWER FORWARD HOLE NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE T RIMMED AREA. FABRICATED FILLER 1 AND DOUBLER FROM .063 INCH THICK 2024-T3. FABRICATED FILLER 2 AND TRIPLER FROM .050 I NCH THICK 2024-T3 MATERIAL IAW FIGURES 1, 2, 3, AND 4. INSTALLED REPAIR PARTS SB 737-53A1176R6 FOR S10 AND S14 IAW ECO 3250 DEVIATION J. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002042400026 20020424 00026 NM 2002 4 24 TSAA0251085 1 20020226 A 5310 6545766 WINDOW FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S-10R AND S14R ON WINDOW NR 26 RIGHT UPPER AFT HOLES NR 9 AND NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECT ED EDGE OF THE TRIMMED AREAS. FABRICATED FILLER 1 AND DOUBLER FROM .063 INCH THICK 2024-T3. FABRICATED FILLER 2 AND TR IPLER FROM .050 INCH THICK 2024-T3 MATERIAL IAW FIGURES 1, 2, 3 AND 4. INSTALLED REPAIR PARTS SB 737-53A1176R6 FOR S10 AND S14 IAW ECO 3250 DEVIATION J. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002042400027 20020424 00027 NM 2002 4 24 TSAA0251086 1 20020226 A 5310 6545766 WINDOW FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S-10R BS 867 PLUS 10 ON WIN DOW NR 29 RIGHT UPPER AFT HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED ED GE OF THE TRIMMED AREAS. FABRICATED FILLER 1 FROM .032 INCH THICK 2024-T3 AND DOUBLER FROM .063 INCH THICK 2024-T3. FA BRICATED FILLER 2 AND TRIPLER FROM .050 INCH THICK 2024-T3 MATERIAL IAW FIGURES 1, 2 AND 3. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION K. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002042400028 20020424 00028 NM 2002 4 24 TSAA0251087 1 20020226 A 5310 6545766 WINDOW FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PEFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S-14R BS 420 ONWINDOW NR 4 R IGHT LOWER AFT CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE O F THE TRIMMED AREAS. FABRICATED FILLER 1 AND DOUBLER FROM .032 INCH THICK 2024-T3. FABRICATED FILLER 2 AND TRIPLER FRO M .050 INCH THICK 2024-T3 MATERIAL IAW FIGURES 1, 2, 3, AND 4. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION G. AIRCRA FT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002042400029 20020424 00029 NM 2002 4 24 TSAA0251088 1 20020226 A 5310 6545766 WINDOW FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 NE 05 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 5 RIGHT UPPER FOR WARD CORNER HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIM MED AREAS. FABRICATED FILLER 1 AND DOUBLER FROM .032 INCH THICK 2024-T3. FABRICATED FILLER 2 AND TRIPLER FROM .050 INC H THICK 2024-T3 MATERIAL IAW FIGURES 1, 2, 3 AND 4. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002042400030 20020424 00030 NM 2002 4 24 TSAA0251089 1 20020226 A 5310 6545766 WINDOW FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 6 RIGHT UPPER FOR WARD CORNER HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIM MED AREAS. FABRICATED FILLER 1 AND DOUBLER FROM .032 INCH THICK 2024-T3. FABRICATED FILLER 2 AND TRIPLER FROM .050 INC H THICK 2024-T3 MATERIAL IAW FIGURES 1, 2, 3 AND 4. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002042400031 20020424 00031 NM 2002 4 24 TSAA0251090 1 20020226 A 5310 6545766 WINDOW FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATION ON WINDOW NR 8 RIGHT UPPER FORW ARD CORNER HOLE NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLER 1 AND DOUBLER FROM .032 INCH THICK 2024-T3. FABRICATED FILLER 2 AND TRIPLER FROM .050 INCH THICK 2024-T3 MATERIAL IAW FIGURES 1, 2, 3 AND 4. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002042400032 20020424 00032 NM 2002 4 24 TSAA0251091 1 20020226 A 5313 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 FOUND CRACKES ON STRINGER 6L AND 7L FORWARD LAV SIDEWALL AREA. TRIMMED OUT DAMAGED PORTIONS OF INTERCOSTAL IAW SRM 51-4 0-3 FIGURE 1. VERIFIED NO FURTHER CRACKS USING HFEC METHODS AROUND THE TRIMMED OUT AREA. FABRICATED AND INSTALLED REPA IR PARTS IAW SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002042400033 20020424 00033 NM 2002 4 24 TSAA0252092 1 20020327 A 5210 GUIDE BOEING 737 7372X6C 1384552 NM PAX DOOR OUT OF ADJUST A TSAA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 13 816AL 23122 FLT 46 - HNL-ITO - FORWARD ENTRY DOOR LIGHT CAME ON DURING THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT R ETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE ADJUSTED THE ROLLER GUIDE SERRATED PLATES AND GUIDE ARM. OPE RATIONAL CHECKS WERE GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002042400039 20020424 00039 CE 2002 4 24 ECA2002F00001 1 20020401 A 5210 24112808634 SEAL LEAR 25 25 5170506 CE GE CJ610 CJ6101 30006 NE PAX DOOR TORN A ECAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 11 25EC 25026 CABIN ALTITUDE REACHED 10,000 FT MAXIMUM AIRFLOW WAS APPLIED AND CABIN WAS RESTORED. DECENT FOLLOWED WITH FLOW ON UNTIL 1500 FT PRIOR TO LANDING. REQUIRED MAX AIRFLOW TO MAINTAIN CABIN PRESSURE. MAINTENANCE PERFORMED GROUND TEST OF CABIN PRESSURIZATION SYSTEM, OPERATED NORMALLY BUT EXCESSIVE AIR LEAK WAS FOUND COMING FROM AROUND CABIN DOOR SEAL FORWARD SI DE. A VISUAL INSPECTION SHOWED A 1.5 INCH TEAR IN THE SEAL. SEAL REPLACEMENT CURED PROBLEM. GROUND CHECKS NORMAL IAW MM. 2 L 7 2 4J 4 J A10CE 1E16 2002042400040 20020424 00040 CE 2002 4 24 IKM2002F00001 1 20020405 A 3246 954399 WHEEL LEAR 25 25D 5170514 CE GE CJ610 CJ6108 30006 NE MLG CRACKED B IKMA K NONE O OTHER IN INSP/MAINT 1 NM 07 347JV 347 WHEEL, CRACKED, BEAD SEAL AREA. 2 L 7 2 4J 4 J A10CE 1E16 2002042400041 20020424 00041 NM 2002 4 24 PB82002F00000 1 20020318 A 2597 WIRE HARNESS ISRAEL 1125 1125 NM GARRTT TFE731 TFE731* 01518 WP GALLEY BURNED B PB8R K NONE O OTHER IN INSP/MAINT 1 SO 17 60AJ 3851 071 AIRCRAFT CAME IN WITH ELECTRICAL PROBLEMS. REMOVED FORWARD GALLEY. AT TOP OF GALLEY (FORWARD SIDE-AFT OF ENTRY DOOR CU T-OUT) FOUND NUMEROUS BURNED/ CRUSHED WIRES IN A 1 INCH WIRE HARNESS. SUSPECT GALLEY INSTALLATION CRUSHED WIRE HARNESS. 2 L 7 2 4F 4 F RT A16NM E6WE 2002042400042 20020424 00042 CE 2002 4 24 QH52002F00001 1 20020406 A 3246 9544207 WHEEL LEAR 25 25B 5170511 CE GE CJ610 CJ6101 30006 NE MLG CRACKED B QH5R K NONE O OTHER IN INSP/MAINT 1 NM 07 118MB 118 WHEEL CRACKED AT BOLT HOLES. 2 L 7 2 4J 4 J A10CE 1E16 2002042400043 20020424 00043 EU 2002 4 24 USAABA02009 1 20020405 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU EPSU DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 673UW 0337 EPSU 11 WL FAILED BATTERY CAPACITY TEST. MAINTENANCE REPLACED THE EPSU. 2 L 7 2 4F RT A46NM 2002042400044 20020424 00044 NM 2002 4 24 USAABB02044 1 20020413 A 3397 WIRE BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 650US 23902 FOUND FLOOR EMERGENCY LIGHTING INOPERATIVE, RIGHT SIDE IN FIRST CLASS. MAINTENANCE REPAIRED FAULTY WIRING. 2 L 7 2 4F 4 F RT A1NM E13NE 2002042400045 20020424 00045 NM 2002 4 24 USAABB02045 1 20020413 A 3350 20121 CHARGER BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 650US 23902 FOUND LIFT OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. 2 L 7 2 4F 4 F RT A1NM E13NE 2002042400046 20020424 00046 EU 2002 4 24 USAASA02027 1 20020314 A 3350 32145410 PSEU AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 717UW 10 1069 RECEIVED AN LEFT INT LOAD EPSU FAULT DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE LEFT EMERGENCY EXIT ROW. OPERATIONALLY CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2002042400047 20020424 00047 EU 2002 4 24 USAASA02035 1 20020409 A 3397 WIRE AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 703UW 0904 AN EMERGENCY LIGHT WAS INOPERATIVE AT SEAT 9D. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONALLY CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2002042400048 20020424 00048 WP 2002 4 24 WIB2002F00001 2 20020329 A 7321 307080011 FUEL CONTROL LEAR 35 31A 5170531 CE GARRTT TFE731 TFE731* 01518 WP LT ENGINE INOPERATIVE D WIBR K NONE L NO TEST IN INSP/MAINT 1 SW 11 370SC 4772 070 99227 FCU - SLOW TO START, NO POWER LEVER AUTHORITY IN MANUAL MODE. 2 L 7 2 4F 4 F RT A10CE E6WE 2002042400049 20020424 00049 SW 2002 4 24 XR52002F00000 1 20020412 A 7700 56140008 INDICATOR AIRTRC AT500 AT502B 0390307 SW PWA PT6 PT6* 52043 EA ITT SHORTED D XR5R O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 91262 43 502B0640 IN FLIGHT, PILOT REPORTED THAT CIRCUIT BREAKER (POPPED) OUT. HE RESET THE BREAKER AND SPARKS CAME OUT OF THE ITT GAUGE. THE MARK ON THE INSTRUMENT CASE INDICATE THAT A SHORT OCCURRED INSIDE AND GROUNDED TO THE INSTRUMENT PANEL, CAUSING TH E SPARKS. 1 L 7 1 3T 3 T NC A17SW E2NE 2002042400053 20020424 00053 NM 2002 4 24 QXEA0200579 1 20020322 A 5220 SHAFT DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - ESCAPE HATCH LATCHING LEVER SHAFT HAS LIGHT SURFACE CORROSION. REPAIRED IAW DHC-8 SRM 51-20-26, PAGE 7. 2 H 7 2 4T RT A13NM 2002042400054 20020424 00054 NM 2002 4 24 QXEA0200580 1 20020324 A 5720 WEB DHAV DHC8 DHC8202 2809007 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LIGHTENING HOLE CRACKED BOTTOM SIDE, RIGHT TRAILING EDGE, BELOW AND OUTBOARD OF RIGHT OUTBOARD ROLL SPOILER CENTER HINGE. REPAIRED IAW DHC-8 SRM 51-10-21. 2 H 7 2 4T RT A13NM 2002042400055 20020424 00055 EU 2002 4 24 QXEA0200626 1 20020410 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 PDX- FORWARD CABIN EXIT SIGN LIGHTS INOPERATIVE. REMOVED AND REPLACED FORWARD CABIN EXIT SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002061100102 20020611 00102 EU 2002 6 11 QXEA0200628 1 20020413 A 2742 1110039AAA5 ACTUATOR FOKKER F28 F28MK4000 4990810 EU HORIZ STAB LEAKING A QXEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 496US 32709 4445 11169 PDX - EN ROUTE FROM YEG TO SEA, THE UTILITY AND FLIGHT CONTROL HYDRAULIC QUANTITY DROPPED TO ZERO. AIRCRAFT DIVERTED TO PDX. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE HORIZONTAL STABILIZER ACTUATOR LEAKING FLUID AND REPLACED SAME. OPERATIONAL CHECK AND LEAK CHECKS ARE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002042400056 20020424 00056 EU 2002 4 24 QXEA0200629 1 20020412 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 11169 SEA-AFT FACING PORTION OF OVERHEAD EXIT SIGN ROW 9 INOPERATIVE. REPLACED OVERHEAD EXIT SIGN AT ROW 9. OPERATIONAL CHEC K GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002042400057 20020424 00057 NM 2002 4 24 QXEA0200630 1 20020413 A 3610 311325301 VALVE DHAV DHC8 DHC8202 2809007 NM PNEUMATIC SYS MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 348PH 484 SEA- HAZE IN CABIN AND COCKPIT AFTER START UP. CLEARED SHORTLY AFTER. APPEARS TO BE DURING START UP OF NR 1 ENGINE. R EMOVED AND REPLACED SWITCHING VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042400058 20020424 00058 NM 2002 4 24 QXEA0200632 1 20020407 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 356PH 49 49 502 SEA- MASTER WARNING AND SMOKE LIGHTS CAME ON IN FLIGHT FOR ABOUT FIVE SECONDS. REMOVED AND REPLACED FORWARD AND AFT BAG GAGE PIT SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042400059 20020424 00059 NM 2002 4 24 QXEA0200633 1 20020412 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 366PH 7217 4208 510 PDX- INTERMITTENT SMOKE WARNING LIGHT CAME ON NUMEROUS TIMES THROUGHOUT FLIGHT. REMOVED AND REPLACED FORWARD AND AFT BA GGAGE SMOKE DETECTORS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042400060 20020424 00060 EA 2002 4 24 QXEA0200639 1 20020413 A 1430 RIVET CNDAIR CL600 CL6002C10 1390015 EA FLAP VANE MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 609QX 10031 PDX - RIGHT OUTBOARD FLAP VANE LEADING EDGE HAS 3 LOOSE RIVETS AND ONE RIVET MISSING. MAINTENANCE REMOVED THE 3 LOOSE R IVETS AND INSTALLED 3 CHERRY MAX RIVETS AND INSTALLED 1 CHERRY MAX RIVET FOR THE ONE RIVET THAT WAS MISSING IAW CRJ SRM 51-42-13. 2 L 7 2 4F RT A21EA 2002042400061 20020424 00061 NM 2002 4 24 QXEA0200642 1 20020420 A 2910 DRAIN LINE BOMBDR DHC8 DHC8401 NM HYD SYSTEM LEAKING A QXEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 403QX 4037 BOI - AIRCRAFT MADE AN UNSCHEDULED LANDING WHEN THE NR 1 HYDRAULIC ISOLATION VALVE/ROLL SPOILER HYDRAULIC LIGHTS ILLUMIN ATED IN FLIGHT. NR 1 HYDRAULIC QUANTITY WAS OBSERVED AT 25 PERCENT AND FALLING. HYDRAULIC QUANTITY WAS NEAR 0 AT TOUCH DOWN. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 1 CASE DRAIN LINE AFT OF THE FIREWALL IAW -400 MAINTENANCE MANUAL 29-00-00. OPERATIONAL CHECK AND LEAK CHECK WERE GOOD. ROLL SPOILERS OPERATIONAL CHECK WAS NORMAL. NO FURTHER DISCREPANCIES NOTED. AIRCRAFT OK FOR CONTINUED SERVICE. 2 H 7 2 4T RT A13NM 2002042400062 20020424 00062 WP 2002 4 24 0201249611 1 20020405 A 5310 PRESSURE PANEL DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611NA 47435 During an Hck in ATl, three cracks were found in the flight compartment pressure panel at station 105. The cracks are lo cated at x=25 1.5" long x=35 2.3" long and x=-35 2.4" long. Repaired per EA 96-188455. 2 L 7 2 4F A6WE 2002042400063 20020424 00063 WP 2002 4 24 0201269611 1 20020408 A 5310 PRESSURE PANEL DOUG DC9 DC932 3022066 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611NA 47435 During Hck at ATL, corrosion was found on the APB WEB at L26R. The corrosion was found within Blue Print tolerance. Repa ired per EA 96-188478. 2 L 7 2 4F A6WE 2002042400064 20020424 00064 WP 2002 4 24 0201299866 1 20020408 A 5310 DOUBLER DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 775NC 47785 During Mck in ATL, a crack was discovered in the APB doubler. This EA provides inspection criteria and limits for crack. EA 98-188427 2 L 7 2 4F RT A6WE 2002042400065 20020424 00065 WP 2002 4 24 0201309151 1 20020411 A 5230 DOOR DOUG DC9 DC914 3022034 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8909E 45770 During shop visit in ATL, the 2 aft cargo door assy webs were found cracked at aft end. Repaired per EA 99-189648. 2 L 7 2 4F A6WE 2002042400066 20020424 00066 EA 2002 4 24 QXEA0200643 1 20020418 A 2842 SENSE LINE CNDAIR CL600 CL6002C10 1390015 EA FUEL TANK BROKEN A QXEA K NONE J WARNING INDICATION DE DESCENT 1 NM 09 608QX 10026 FAT-RIGHT MAIN EJECTOR CAUTION MESSAGE AT 22,000 FEET DESCENDING, TANK AT 80 POUNDS INCREASED TO 220 POUNDS THEN DECREAS ED TO 70 POUNDS. BOTH BOOST PUMPS WERE OPERATING. REMOVED FUEL PANEL 611AB, FOUND PRIMARY EJECTOR SENSOR LINE BROKEN A T B-NUT. REMOVED AND REPLACED SENSOR LINE WITH NEW. CLOSED PANEL 611AB. GROUND RAN BOTH ENGINES. OPERATIONAL CHECK G OOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002042400067 20020424 00067 NM 2002 4 24 QXEA0200644 1 20020418 A 3350 6138001 POWER SUPPLY BOMBDR DHC8 DHC8401 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 401QX 4031 PDX- CEILING AISLE EMERGENCY LIGHT AT STATION 340.25 IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT NUMBER 3. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042400068 20020424 00068 EU 2002 4 24 RAIA00203107 1 20020327 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 550HK 41039 MX-STL - LEFT FORWARD EMERGENCY LIGHTS INOP. SECURED LOOSE CONNECTOR, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002042400069 20020424 00069 EU 2002 4 24 RAIA00203112 1 20020331 A 3350 LIGHT AEROSP ATR72 ATR72202 8680940 EU CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 723TE 283 MX-STL- FLOOR PATH LIGHTS OUT AT 6AB AND 11AB. REMOVED AND REPLACED LIGHT BULBS IN EMERGENCY TRACK LIGHT AT 6AB AND 11A B. 2 H 7 2 4T RT A53EU 2002042400070 20020424 00070 EU 2002 4 24 RAIA00204123 1 20020410 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 556HK 41073 MX-STL- EMERGENCY PATH LIGHTS OUT AT ROW 3 & 4. RECONNECTED PATH LIGHT ELECTRICAL CONNECTOR. 2 L 7 2 4T RT A41NM 2002042400071 20020424 00071 EU 2002 4 24 RAIAOO203106 1 20020325 A 3350 CONNECTOR AEROSP ATR42 ATR42300 8680920 EU CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 423TE 119 MX-STL- EMERGENCY EXIT LIGHT OUT ON DOOR. CLEANED ELECTRICAL CONNECTION ON PAX DOOR EMERGENCY LIGHT. 2 H 7 2 4T RT A53EU 2002042400073 20020424 00073 NM 2002 4 24 SABA020042 1 20020402 A 7697 WIRE DHAV DHC8 DHC8102 2809003 NM COCKPIT DAMAGED A SABA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 33 882CC 168 AIRCRAFT 882 ON FLIGHT 5025 FROM CLT TO TLH. DURING THE TAKEOFF ROLL THE TAKEOFF WARNING HORN SOUNDED. AIRCRAFT ABORTE D THE TAKEOFF AND RETURNED TO THE GATE IN CLT WITH NO OTHER PROBLEMS. NO EMERGENCY WAS DECLARED. MAINTENANCE REPAIRED DAMAGED WIRING AND CANNON PLUG AT POWER LEVER SWITCH. SYSTEM OPS CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042400075 20020424 00075 NM 2002 4 24 SABA020044 1 20020404 A 3350 SOCKET DHAV DHC8 DHC8103 1386005 NM CABIN DAMAGED A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 801WP 086 AIRCRAFT 801 ON FLIGHT 5019 FROM AGS TO CLT. DURING POST-FLIGHT INSPECTION THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOU ND INOPERATIVE. NO EMERGENCY PROCEDURES WERE USED. MAINTENANCE REPAIRED THE LIGHT SOCKET. OPS CHECK WAS GOOD. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042400076 20020424 00076 2002 4 24 SABA020045 4 20020403 A 2210 DAMPENER DHAV DHC8 DHC8103 1386005 NM AUTOPILOT SYS MALFUNCTIONED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 801WP 086 AIRCRAFT 801 ON FLIGHT 5097 FROM CLT TO PGV. AFTER TAKEOFF THE RIGHT CHANNEL OF THE YAW DAMP SYSTEM FAILED. THE YAW DA MP SYSTEM FAILED TO TRANSFER FROM THE RIGHT CHANNEL TO THE LEFT CHANNEL. THE AIRCRAFT RETURNED TO CLT AND LANDED WITH N O OTHER PROBLEMS. NO EMERGENCY WAS DECLARED. MAINTENANCE PERFORMED AN AUTOMATIC FLIGHT CONTROL SYSTEM CHECK OF THE LEF T AND RIGHT YAW DAMP SYSTEMS PER DHAV MAINTENANCE MANUAL. SYSTEM CHECK WAS GOOD. NO TROUBLE WAS FOUND IN THE LEFT OR R IGHT SYSTEM. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042400077 20020424 00077 2002 4 24 SABA020047 4 20020407 A 3425 7003360941 COMPUTER DHAV DHC8 DHC8103 1386005 NM NR 2 FAILED A SABA C ABORTED TAKEOFF I FLT. ATTITUDE INST. TO TAKEOFF 1 SO 33 881CC 294 AIRCRAFT 881 ON FLIGHT 5027 FROM CLT TO CVG. ON TAKEOFF ROLL THE NUMBER 2 ATTITUDE INDICATOR FAILED. THE TAKEOFF WAS A BORTED AND AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEMS. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND RE PLACED THE NUMBER 2 AHRU COMPUTER. OPS CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042400078 20020424 00078 NM 2002 4 24 SABA020049 1 20020411 A 3350 1005511 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 AIRCRAFT 883 ON FLIGHT 5232 FROM CLT TO CVG. DURING PREFLIGHT FLOOR EMERGENCY LIGHT AT ROW 4 WAS INOPERATIVE. ALSO ONE OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULBS. OPS CHECK WAS GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042400081 20020424 00081 EA 2002 4 24 COMA0260266 1 20020420 A 5311 600360302324 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FS718.0 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 735CA 7862 7267 THE L/H AND R/H FRAME AND AFT DOUBLER AT FS718.0 WERE CRACKED BETWEEN STR10 AND 12.REPAIRED THE CRACKED FRAMES AND DOUBL ERS I/A/W CANADAIR REO 601R-53-91-193 REV A. 2 L 7 2 4F RT A21EA 2002042400082 20020424 00082 EA 2002 4 24 COMA0260267 1 20020421 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING W O INADEQUATE Q C OTHER CL CLIMB 1 SO 01 786CA 7333 FLIGHT 5045 AIRCRAFT MADE UNSCHEDULED LANDING DUE TO EXT. SERVICE PANEL OPEN.INSPECTED AREA, FOUND NO DEFECTS, SECURED P ANEL. 2 L 7 2 4F RT A21EA 2002042400083 20020424 00083 EA 2002 4 24 COMA0260268 1 20020419 A 2710 AILERON CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 988CA 7204 FLIGHT 5375 ABORTED T/O DUE TO AILERON CONFIG WARNING.COULD NOT DUPLICATE. AILERON TRIM AND RIGGING FOUND SATISFACTORY. 2 L 7 2 4F RT A21EA 2002042400084 20020424 00084 EA 2002 4 24 COMA0260269 1 20020420 A 2760 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 804CA 7352 FLIGHT 5541 GROUND SPOILER FAULT MESSAGE DURING T/O.COULD NOT DUPLICATE. RESET SECU AND SYSTEM TEST WAS SATISFACTORY. 2 L 7 2 4F RT A21EA 2002042400085 20020424 00085 2002 4 24 00019 4 20020422 A 3422 25883023 GYRO AMD FALCON FALCON20 2730103 EU COCKPIT FAILED E HAEA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 699TW 050 NR 1 HSI AND 32 HSI NOT MOVING AFTER DEPARTURE, RETURN TO ADS. REMOVED AND REPLACED PILOTS DIRECTIONAL GYRO OPERATIONAL CHECK GOOD ON GROUND TEST. RETURN AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A7EU 2002042400089 20020424 00089 EA 2002 4 24 COMA0260270 1 20020420 A 8010 8989308 START VALVE CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 436CA 2664 7482 FLIGHT 5705 ENGINE START STATUS MESSAGE DURING T/O.REPLACED THE R/H ENGINE START VALVE. 2 L 7 2 4F RT A21EA 2002042400091 20020424 00091 EA 2002 4 24 COMA0260271 1 20020421 A 2420 V210D090BC RELAY CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 01 821CA 7420 FLIGHT 5964 ESS BUSS CAUTION MESSAGE.REPLACED THE RELAY K1XD. 2 L 7 2 4F RT A21EA 2002042400094 20020424 00094 EA 2002 4 24 COMA0260272 1 20020420 A 3350 64643 CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 931CA 7037 FLIGHT 5791 EMERGENCY FLOOR PATH LIGHTING OUT ROWS 1 TO 4.REPLACED FLOOR LIGHTS CABLE ASSY ROW 1 TO 4. 2 L 7 2 4F RT A21EA 2002042400097 20020424 00097 2002 4 24 COMA0260273 4 20020422 A 2220 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 431CA 7472 FLIGHT 5356 YAW DAMPNER #1 INOP WARNING DURING T/O.RESET IAPS SYSTEM - YAW DAMP SYTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 2002042400100 20020424 00100 NM 2002 4 24 2002F00409 1 20020221 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM ROW 20 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROW 20 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER AT ROW 20, THEN LIGHTS OPERATED NORMAL. REF ASAA0210054. (M) 2 L 7 2 4F RT A16WE 2002042400101 20020424 00101 NM 2002 4 24 2002F00410 1 20020212 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM AFT CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING TRANSMITTERS NOT TRANSMITTING. REMOVED AND REPLACE D FORWARD TRANSMITTER AND BATTERY FOR AFT TRANSMITTER, THEN TRANSMITTERS OPERATED NORMAL. REF ASAA0210052. (M) 2 L 7 2 4F RT A16WE 2002042400102 20020424 00102 NM 2002 4 24 2002F00411 1 20020214 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE PUNCTURED A RYNA K NONE O OTHER IN INSP/MAINT 1 NM 01 801EA 22432 AT C-CHECK, FOUND SKIN PUNCTURED AT L1 DOOR CUTOUT, FORWARD UPPER BETWEEN SECOND AND THIRD DOOR STOP. (M) 2 L 7 3 4F A3WE 2002042400103 20020424 00103 NM 2002 4 24 2002F00412 1 20020216 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 801EA 22432 AT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOORBEAM CORRODED AT STATION 536 LBL2. (M) 2 L 7 3 4F A3WE 2002042400105 20020424 00105 NM 2002 4 24 ASAA0210010 1 20020108 A 5311 65C357986 FRAME BOEING 737 737298C 1384490 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 218-219, RIGHT BUTTOCK LINE 38 GOUGED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002042400106 20020424 00106 NM 2002 4 24 ASAA0210018 1 20020108 A 5311 654581986 FRAME BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 227-295, RIGHT BUTTOCK LINE 18 WITH OVERSIZED HOLES. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002042400107 20020424 00107 NM 2002 4 24 ASAA0210019 1 20020108 A 5310 65C314278 CROSSBEAM BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND CARGO DOOR CROSSBEAM AT BS 444, WATERLINE 60 CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002042400109 20020424 00109 NM 2002 4 24 ASAA0210050 1 20020206 A 5311 6546549 FRAME BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 PAE - DURING SCHEDULED C-CHECK,F OUND AFT CARGO BAY FRAME AT BS 767, RIGHT BUTTOCK LINE 9 CORRODED. REMOVED DAMAGE AND REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002042400110 20020424 00110 NM 2002 4 24 ASAA0210051 1 20020208 A 5314 6551637160 KEELBEAM BOEING 737 737210C 1384459 NM CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM FLANGE AT BS 679, RIGHT BUTTOCK LINE 7 RIGHT BUTTOCK LINE 9 WITH A DOUBL ER DRILLED HOLE. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2002042400111 20020424 00111 NM 2002 4 24 ASAA0210052 1 20020212 A 3350 BATTERY BOEING 737 737298C 1384490 NM FWD CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING TRANSMITTERS NOT TRANSMITTING. REMOVED AND REPLACE D FORWARD TRANSMITTER AND BATTERY FOR AFT TRANSMITTER, THEN TRANSMITTERS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002042400113 20020424 00113 NM 2002 4 24 ASAA0210054 1 20020221 A 3350 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROW 20 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER AT ROW 20, THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002042400115 20020424 00115 NM 2002 4 24 ASAA0210055 1 20020225 A 5220 65566321 DOOR BOEING 737 737290C 138448V NM EMERGENCY EXIT JAMMED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, FOUND AFT AIRSTAIR/EMERGENCY EXIT L2 DOOR WOULD NOT OPEN. FOUND WIRE STUCK IN AIRSTAIR HINGE. REMOVED AND REPAIRED WIRE, AIRSTAIR THEN OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002042400116 20020424 00116 NM 2002 4 24 ASAA0240020 1 20020214 A 5313 6549886152 STRINGER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 PAE - DURING C-CHECK, FOUND CORROSION AT BS 520 STRINGER 27R AND WL 148.5 FORWARD CARGO BAY. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002042600128 20020426 00128 EA 2002 4 26 COMA0260274 1 20020422 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 420CA 2940 7451 FLIGHT 5468 GEAR DISAGREE WHEN GEAR LOWERED AT 200 KTS. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002042400119 20020424 00119 NM 2002 4 24 2002UALA00700 1 20020413 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 933UA 26659 LEFT HAND UPPER FUSELAGE SKIN BELOW CABIN WINDOW AT STATION 410 WAS BLENDED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042600102 20020426 00102 NM 2002 4 26 02FDEA00275 1 20020420 A 5311 651766445 FRAME BOEING 727 727225 1384077 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 DENTS IN FRAME BS 580, STR 22 - 23 LT. REMOVED AND REPLACED FRAME PER SRM 51-30-2. 2 L 7 3 4F A3WE 2002042600105 20020426 00105 NM 2002 4 26 02FDEA00279 1 20020418 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FRAME GOUGED AT BS 620, STR 6R. REMOVED AND REPLACED FRAME PER SRM 53-10-4. 2 L 7 3 4F A3WE 2002042400120 20020424 00120 NM 2002 4 24 2002UALA00701 1 20020413 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 933UA 26659 LEFT HAND FUSELAGE AFT OF ENTRY DOOR 2L GOUGED AT TWO AREAS. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. INSTALLED DOU BLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042400121 20020424 00121 NM 2002 4 24 2002UALA00702 1 20020413 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 AFT PIT FRAME STATION 727E BLENDED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAP INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042400122 20020424 00122 NM 2002 4 24 2002UALA00703 1 20020413 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 STATION 727C FRAME AT STRINGER 19L BLENDED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAP INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042400123 20020424 00123 NM 2002 4 24 2002UALA00704 1 20020414 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 933UA 26659 CABIN STATION 616 FRAME CHORD WEB IS CRACKED JUST BELOW STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FILLER A ND ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042400124 20020424 00124 NM 2002 4 24 2002UALA00705 1 20020414 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 LOWER FUSELAGE SKIN AT FORWARD CARGO DOOR CUTOUT, LOWER FORWARD CORNER HAS 30 PERCENT MATERIAL LOSS AFTER BLENDING. MAJ OR REPAIR ACCOMPLISHED. EXTERNAL DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051500139 20020515 00139 EU 2002 5 15 2002UALA00706 1 20020412 A 5270 HANDLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO DOOR UNSECURE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 417UA 483 CARGO (FORWARD) DOOR ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE SHOWED OPEN PASSING 10,000 FEET. AIRCRAFT RETUR NED TO FIELD. HANDLE WAS STOWED AND LIGHT EXTINGUISHED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002050200073 20020502 00073 NM 2002 5 2 2002UALA00707 1 20020413 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT PIT FUSELAGE FRAME INNER FLANGE DENTS STATION 1380 STRINGER 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPA IR ON FLANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002042400125 20020424 00125 NM 2002 4 24 2002UALA00711 1 20020415 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 933UA 26659 LEFT HAND FUSELAGE SKIN SURFACE AT BS420, TWO AREAS HAVE EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042400126 20020424 00126 NM 2002 4 24 2002UALA00712 1 20020415 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 933UA 26659 LOWER FUSELAGE SKIN IS DENTED BELOW FORWARD PIT DOOR CUTOUT FORWARD CORNER. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBL ER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042400127 20020424 00127 NM 2002 4 24 2002UALA00713 1 20020415 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 933UA 26659 LEFT HAND SIDE BS 188 CHORD AT STRINGER 17L CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED CHORD DOUBLER AND SKIN DOUBL ER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042400128 20020424 00128 NM 2002 4 24 2002UALA00714 1 20020415 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 AFT CARGO PIT FRAME STATION 727E, STR 25L-26L, LBL 14 HAS DEEP GOUGE. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042400129 20020424 00129 NM 2002 4 24 2002UALA00715 1 20020415 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 STATION 727B STRINGER 19L ON INBOARD FLANGE HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBL ER AND STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042400130 20020424 00130 NM 2002 4 24 2002UALA00716 1 20020415 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 AFT PIT LEFT HAND FRAME STATION 727D GOUGED ON FORWARD SIDE AT RADIUS, BETWEEN STRINGER 19L AND 20L. MAJOR REPAIR ACCOM PLISHED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042400131 20020424 00131 NM 2002 4 24 2002UALA00717 1 20020415 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 LOWER EXTERIOR FUSELAGE SKIN AT FORWARD CARGO DOOR LOWER AFT CUTOUT CORNER HAS EXCESS MATERIAL LOSS. MAJOR REPAIR ACCOM PLISHED. ACCOMPLISHED DOUBLER AND STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050200076 20020502 00076 NM 2002 5 2 2002UALA00718 1 20020415 A 5320 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 AFT CABIN DECKPLATE CORRODED STATION 1690 TO 1694 RBL 50. MAJOR REPAIR ACCOMPLISHED. REPAIRED DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002050900060 20020509 00060 NM 2002 5 9 2002UALA00719 1 20020416 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EEL LIGHT INOP, 3A AFT. REPLACED EEL STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002050900061 20020509 00061 NM 2002 5 9 2002UALA00720 1 20020416 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 OUTSIDE EMERGENCY INOP, 3RD DOWN, FWD BULB. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002050900062 20020509 00062 NM 2002 5 9 2002UALA00721 1 20020416 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY CEILING LIGHT INOP, ROW 16. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002050900063 20020509 00063 NM 2002 5 9 2002UALA00722 1 20020416 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 OVERSTAIRS EMERGENCY LIGHT, LOWER BULB INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002042400132 20020424 00132 NM 2002 4 24 2002UALA00725 1 20020417 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 CABIN FRAME AT STATION 847 STRINGER 9R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050900064 20020509 00064 NE 2002 5 9 2002UALA00726 2 20020221 A 7230 COMPRESSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 ENGINE FAULTY A UALA J A DUMP FUEL UNSCHED LANDING E A Y VIBRATION/BUFFET FLAME/FIRE ENGINE STOPPAGE CL CLIMB 1 WP 29 107UA 19360 19360 26900 727668 NR 3 ENGINE SURGED 3 TIMES DURING TAKEOFF WITH FLAMES PER CREW. CREW WRITE UP DURING T/O LAX NR 3 ENGINE VIBRATED WITH LOUD 3 TIME POPS. ENGINE EXPERIENCED A GROUP 3 SURGE (EXCESSIVE BLADE TIP CLEARANCES IN HPC REAR STAGES). ENGINE WAS R EMOVED FOR COMPRESSOR REFURBISHMENT. 2 L 7 4 4F 4 F RT A20WE E24NE 2002042400133 20020424 00133 NM 2002 4 24 2002UALA00727 1 20020418 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 CABIN FRAME STATION 847 CRACKED AT STRINGER 9L RIVET. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042400134 20020424 00134 NM 2002 4 24 2002UALA00728 1 20020418 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSLEAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 CABIN STATION 867 STRINGER 9L FRAME IS CRACKED AT RIVET. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042400135 20020424 00135 NM 2002 4 24 2002UALA00729 1 20020418 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 CABIN STATION 887 STRINGER 9R FRAME IS CRACKED AT RIVET. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002042400136 20020424 00136 NM 2002 4 24 2002UALA00734 1 20020418 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 MAIN CABIN STATION 852 LBL 55, TRANSBEAM T-CAP UPPER CHORD CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICAT ED REPAIR SECTION AND INSTALLED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002042400137 20020424 00137 NM 2002 4 24 2002UALA00737 1 20020418 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 MAIN CABIN STATION 852, RBL 55, TRANSBEAM UPPER CHORD CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED RE PAIR SECTION AND INSTALLED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002042400138 20020424 00138 WP 2002 4 24 ZW0A0204603 1 20020423 A 3350 7732 LAMP DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 THE EGRESS LIGHT WAS INOPERATIVE AT SEAT ROW 14D. REPLACED THE LAMP. CHECK-C 6-19-01 MCI. --CLOSED-- 2 L 7 2 4F RT A6WE 2002042400139 20020424 00139 WP 2002 4 24 MWEA020270 1 20020423 A 5315 39258121 FITTING DOUG DC9 DC982 3022082 WP STATION 927 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 CRACKED VERTICAL FLOOR BEAM SUPPORT ANGLE ATTACH FITTING AT STATION 927, 44 INCHES TO THE LEFT OF CENTER. -- REMOVED A ND INSTALLED NEW FITTINGS. 2 L 7 2 4F A6WE 2002042400140 20020424 00140 WP 2002 4 24 MWEA020271 1 20020423 A 5315 3936668507 FITTING DOUG DC9 DC982 3022082 WP STATION 731 BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 CENTER CARGO AY FLOOR BEAM AT STATION 731 HAS A BROKEN FITTING AT AIRCRAFT CENTER LINE. -- REMOVED AND REPLACED FITTIN G. 2 L 7 2 4F A6WE 2002042400141 20020424 00141 WP 2002 4 24 ABXA010830 1 20020318 A 5300 575499227 LONGERON DOUG DC8 DC861 3021952 WP FWD. LWR. CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 FORWARD ACCESSORY COMPARTMENT AT F.S. 640 - 660, LONGERON 31 RIGHT, WAS CRACKED. FABBED REPAIR STRAP AND REPAIRED AREA I AW DC-8 SRM 53-2-0, 53-4-1, 51-1-20D AND REA D853-43068MR. 2 L 7 4 4F 4A25 2002042400142 20020424 00142 WP 2002 4 24 ABXA010831 1 20020329 A 5700 56429401 DOUBLER DOUG DC8 DC861 3021952 WP LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LEFT WING 505F PANEL HAD 10 EACH CRACK INDICATIONS AT FASTENER HOLES. REPAIRED AREA IAW REA D857-43069MR. 2 L 7 4 4F 4A25 2002042400143 20020424 00143 WP 2002 4 24 ABXA010832 1 20020328 A 5300 3755822512N FITTING DOUG DC8 DC861 3021952 WP FWD LWR. CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 SURFACE CORROSION FOUND IN CARGO DOOR TORQUE BOX AT STA. 345, LONGERON 35 RIGHT, LOWER CARGO COMPARTMENT. REPLACED 'Z' F ITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-24, REA D853-43-83MR AND REA D853-43076MR. 2 L 7 4 4F 4A25 2002042400144 20020424 00144 WP 2002 4 24 ABXA010833 1 20020327 A 5300 97549453 DOUBLER DOUG DC8 DC861 3021952 WP AFT LWR CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 AFT CARGO, LONGERON 32 RIGHT, B/S 1200, WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-21 AND REA D853-43071MR. 2 L 7 4 4F 4A25 2002042400145 20020424 00145 WP 2002 4 24 ABXA010834 1 20020312 A 5700 30602321 SPAR CAP DOUG DC8 DC861 3021952 WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 RIGHT WING, FORWARD LOWER SPAR CAP HAD 9 EACH FASTENERS HOLES SHOWING CRACK INDICATIONS. REPAIRED DAMAGED HOLES IAW REA D857-43058. 2 L 7 4 4F 4A25 2002042400146 20020424 00146 NM 2002 4 24 UPS02438085 1 20020422 A 7100 ENGINE BOEING 747 747200 1384847 NM ENGINE #3 A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 521UP 21944 INSPECTION TYPE:N/A SHORTLY AFTER DECENT, SMOKE CAME INTO COCPIT FROM UNDETERMINED SOURC E. ENTERED FROM VENTS WITH ALL SYSTEMS OPERATING NORMALLY. PER DISCUSSION W/FLT CREW, SMOKE TO BE VERY LIGHT & OF OILY NATURE T/S PER M/M 71-00-44. FOUND #3 ENG N2 GRN & FLT IDLE LOW. TRIMMED ENG PER M/M 71-00-11 TRIM CHARTS. GRN IDLE INCR 12 CLICKS.FLT IDLE INCR 12 CLICKS.RPLC 1 & 3 COALESOR BAGS CLEANED #2 PER MM21-51-05 OPS ALL ENG AND A/C PACKS CHECKED OK. OK FOR SERVICE 2 L 7 4 4F RT A20WE 2002042900008 20020429 00008 NM 2002 4 29 F3LA200200132 1 20020419 A 5315 FLOORBEAM BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 3461 25263 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM TRACK TIE IN AFT CARGO COMPARTMENT, STA 772, RBL 13.80. RE MOVED CORRODED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002042400147 20020424 00147 WP 2002 4 24 AT0200050 1 20020423 A 2611 38025611 APU DOUG DC9 DC932 3022066 WP LEAKING A ZZDA K NONE O OTHER TO TAKEOFF 1 SO 15 840AT 47523 AFTER TAKE OFF AFT FLIGHT ATTENDANT REPORTED BOTH AFT LAVATORY SMOKE SOUNDED AND A LIGHT SMOKE COULD BE SEEN; STRONG ODO R. CORRECTIVE ACTION: REMOVED AND REPLACED APU AND CHANGED COELESOR BAG RAN ENGINES OPS CHECK AC SYS TEM NO ODOR COMING FROM AC SYSTEM. 2 L 7 2 4F A6WE 2002042400148 20020424 00148 NM 2002 4 24 AWXA200200361 1 20020406 A 5313 140N20044 FRAME BOEING 757 7572G7 1384963 NM CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 0 0 24233 GYR - MAJOR REPAIR - DURING C-11 CHECK MAIN FRAME WAS FOUND CHAFED BEYOND LIMITS AT BS 1280, STR 14R TO STR 12R. MAINTEN ANCE REMOVED DAMAGED SECTION OF FRAME, FABRICATED REPAIR FRAME SPLICE ANGLES, TREATED, PRIMED AND INSTALLED IAW B757-200 SRM 53-00-07, FIG 201, SHEET 1-3. 2 L 7 2 4F RT A2NM 2002042400149 20020424 00149 NM 2002 4 24 02042401 1 20020424 A 3350 BULB BOEING 757 757236 1384971 NM CABIN ROW 24 A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 545 29944 Emergency Light out, at row 24. Re-lamped as per M/M 33-51-11; Operational Check good. 2 L 7 2 4F RT A2NM 2002042400150 20020424 00150 2002 4 24 02042402 4 20020424 A 2565 D31393110 SLIDE BOEING 757 757256 NM RROYCE RB211 RB211535E4 54555 NE BINDING A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 508 9746 26244 Right Wing escape slide failed to deploy for flight attendant training purposesl The metal bar that the lacing goes thro ugh caught on the lip of the slide compartment preventing the slide from deployiing completely. Cause of interference as yet undetermined but suspected at this time to be normal settling of fabric product over time. Replacement overwing esc ape slide installed. 2 L 7 2 4F 4 F RT A2NM E12EU 2002042500001 20020425 00001 NM 2002 4 25 SWAA020819 1 20020418 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 743SW 29279 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 8. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002042500002 20020425 00002 NM 2002 4 25 SWAA020820 1 20020419 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 710SW 27844 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 11. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002042500003 20020425 00003 NM 2002 4 25 SWAA020821 1 20020420 A 2731 65C2638416M TAB BOEING 737 7373G7 1384595 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED A2 CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TA B PER MM. 2 L 7 2 4F RT A16WE 2002042500004 20020425 00004 NM 2002 4 25 SWAA020822 1 20020419 A 2560 A170033 STRAP BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 615SW 27698 EMERGENCY FLASH LIGHT STRAP BROKEN AT AFT F/A STATION. REMOVED AND REPLACED STRAP PER MM. 2 L 7 2 4F RT A16WE 2002042500005 20020425 00005 NM 2002 4 25 SWAA020823 1 20020415 A 5330 6545819 SKIN BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED SPECIAL VISIT, FOUND NLG W/W SKIN CRACKED AT LT FWD OF NLG DOOR BELL CRANK. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2002042500006 20020425 00006 NM 2002 4 25 SWAA020824 1 20020419 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 743SW 29279 DURING SCHEDULED C4 CHECK, SWA SI 11075-55, FOUND RT ELEVATOR TAB NR 2 HINGE WORN. REMOVED AND REPLACED NR 2 HINGE BUSH ING PER MM. 2 L 7 2 4F RT A16WE 2002042500007 20020425 00007 NM 2002 4 25 SWAA020825 1 20020419 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 743SW 29279 DURING SCHEDULED C4 CHECK, SWA SI 11075-55, FOUND LT ELEVATOR TAB NR 3 AND NR 4 HINGES WORN. REMOVED AND REPLACED TAB B USHINGS PER MM. 2 L 7 2 4F RT A16WE 2002042500008 20020425 00008 NM 2002 4 25 SWAA020826 1 20020418 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED (2 EA) AT BS 179, WL 227, RBL 17.1 AND LBL 17.1. REPAIR ED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002042500009 20020425 00009 NM 2002 4 25 SWAA020810 1 20020418 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002042500010 20020425 00010 NM 2002 4 25 SWAA020811 1 20020417 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 730, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002042500011 20020425 00011 NM 2002 4 25 SWAA020812 1 20020417 A 5754 65C26603102 SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED C4 CHECK, FOUND NR 4 L/E SLAT T/E WEDGE DELAMINATED ON INBD EDGE. REMOVED AND REPLACED NR 4 L/E SLAT P ER MM. 2 L 7 2 4F RT A16WE 2002042500012 20020425 00012 NM 2002 4 25 SWAA020815 1 20020417 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002042500013 20020425 00013 NM 2002 4 25 SWAA020816 1 20020417 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 15L, BS'S 390 AND 395. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002042500014 20020425 00014 NM 2002 4 25 SWAA020817 1 20020417 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002042500015 20020425 00015 2002 4 25 SWAA020805 4 20020417 A 2565 6557463 BRACKET BOEING 737 7373T0 1384582 NM FWD SVC DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK BRACKET CORRODED. REMOVED AND RE PLACED HOOK BRACKET PER SRM 2 L 7 2 4F RT A16WE 2002042500016 20020425 00016 NM 2002 4 25 SWAA020806 1 20020416 A 5312 6516300 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 213 AT LBL 5.0 AND WL 195 AT RBL 21. RE PAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002042500017 20020425 00017 NM 2002 4 25 VNAA0204018 1 20020419 A 2400 GENERATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 425JS 3037 AFTER DEPARTING SDF, THE LEFT HAND GENERATOR FAILED. THE CAPTAIN RESET THE GENERATOR TWICE AND BOTH TIMES THE GENERATOR WOULD FAIL. FLIGHT 4145 THEN RETURNED TO SDF. OUTSTATION MAINTENANCE INSPECTED AND SWAPPED GENERATOR CONTROL UNITS FR OM SIDE TO SIDE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002042500018 20020425 00018 NM 2002 4 25 VNAA0204019 1 20020420 A 3300 321473 POWER SUPPLY 321430 DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 457PS 4532 10525 3048 THE AIRCRAFT HAD THE EMERGENCY BATTERY CHANGED PRIOR TO FLIGHT 4189. HOWEVER, ON THE TAXI FROM THE GATE THE EMERGENCY L IGHTING AT ROWS 3 AND 4 DIDN'T ILLUMINATE. THE FLIGHT RETURNED TO THE GATE WHERE MAINTENANCE CHANGED THE POWER SUPPLY I N ACCORDANCE WITH MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERV ICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002042500019 20020425 00019 NM 2002 4 25 VNAA0204014 1 20020419 A 2400 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 424JS 3033 DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL CAS MESSAGE AND ABORTED TAKE OFF. AS THE AIRCRA FT CLEARED THE RUNWAY THE MESSAGE EXTINGUISHED BY ITSELF AND FLIGHT 4073 WAS CLEARED FOR ANOTHER TAKE OFF ATTEMPT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002042500020 20020425 00020 NE 2002 4 25 VNAA0204015 2 20020419 A 7300 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 424JS 3033 DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL CAS MESSAGE AND ABORTED TAKE OFF. MAINTENANCE I NSPECTED AND CLEANED THE INTERCOMP BLEED VALVE AND ENGINE CONTROL UNIT CANNON PLUGS IN ACCORDANCE WITH DORNIER MAINTENAN CE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002042500021 20020425 00021 NM 2002 4 25 VNAA0204010 1 20020414 A 3200 BRAKE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 440JS 3058 THE CREW REPORTED THAT THE FIRST OFFICER'S BRAKES WERE NOT FUNCTIONING. MAINTENANCE INSPECTED AND SERVICED THE FIRST OF FICER'S LEFT HAND BRAKE PEDAL MASTER CYLINDER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECK S WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002042500022 20020425 00022 NM 2002 4 25 ASAA0240027 1 20020305 A 2897 6937335129 MODULE BOEING 737 737490 1384715 NM FUEL SYSTEM BURNED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 791AS 28886 SEA - AFTER TAKEOFF AT SEVERAL HUNDRED FEET, NR 1 FUEL TANK FORWARD PUMP LIGHT ILLUMINATED IN CONJUNCTION WITH A 'POP' FOLLOWED BY SMOKE IN THE COCKPIT AND AN ELECTRICAL SMELL. RETURNED TO FIELD AND LANDED UNEVENTFULLY. FOUND SHORT CIRCU IT BETWEEN OPEN AND CLOSED WIRE OF NR 1 ENGINE SHUTOFF VALVE AND THE 115 VOLT AC RETRACT WIRE FOR THE OUTBOARD LANDING L IGHT. REMOVED AND REPLACED FUEL SYSTEM MODULE ASSEMBLY. OPERATIONAL CHECKED NORMAL IAW MM. (M) 2 L 7 2 4F RT A16WE 2002042500023 20020425 00023 2002 4 25 ASAA0280058 4 20020228 A 2565 3961896501 LANYARD DOUG DC9 DC982 3022082 WP ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 SEA - FORWARD PASSENGER ENTRY L-1 DOOR EMERGENCY SLIDE LANYARD DISCONNECTED. REATTACHED LANYARD. (M) 2 L 7 2 4F A6WE 2002042500024 20020425 00024 2002 4 25 ASAA0280063 4 20020305 A 2565 3961896501 LANYARD DOUG DC9 DC982 3022082 WP ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 SEA - LEFT AFT GALLEY DOOR EMERGENCY SLIDE LANYARD DISCONNECTED. REATTACHED LANYARD. (M) 2 L 7 2 4F A6WE 2002042500025 20020425 00025 WP 2002 4 25 ASAA0280064 1 20020307 A 5610 59644202 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT DISLODGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 36691 53022 SEA - DURING PREFLIGHT CHECK, THE FIRST OFFICERS SLIDING CLEARVIEW WINDOW OPEN/CLOSE MECHANICAL ARM BECAME DETACHED. RE INSTALLED MECHANICAL ARM. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002042500026 20020425 00026 WP 2002 4 25 ASAA0280065 1 20020307 A 5610 PIN DOUG DC9 DC983 3022083 WP WINDOW MISSING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 35538 53063 PDX - DURING PREFLIGHT CHECK, THE CAPTAINS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. REINSTALLED PIN IN WINDOW HING E LINKAGE. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002042500027 20020425 00027 2002 4 25 ASAA0280073 4 20020317 A 2565 3961899501 LANYARD DOUG DC9 DC982 3022082 WP ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M) 2 L 7 2 4F A6WE 2002042500028 20020425 00028 2002 4 25 ASAA0280074 4 20020318 A 2565 3961899501 LANYARD DOUG DC9 DC982 3022082 WP ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 934AS 49235 ANC - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M) 2 L 7 2 4F A6WE 2002042500029 20020425 00029 WP 2002 4 25 ASAA0280075 1 20020320 A 2133 20219742 OUTFLOW VALVE DOUG DC9 DC983 3022083 WP AFT FUSELAGE FAILED A ASAA B EMER. DESCENT O OTHER CR CRUISE 1 NM 01 976AS 53452 EN ROUTE TO SEA FLT 748, AUTO CABIN PRESSURE CONTROL MALFUNCTIONED, WITH CREW PERFORMING EMERGENCY DESCENT FROM 28,000 F EET ALTITUDE TO 10,000. REPLACED OUTFLOW VALVE MOTOR/ACTUATOR ASSEMBLY. SYSTEM THEM OP CHECK OK. (M) 2 L 7 2 4F RT A6WE 2002042500030 20020425 00030 WP 2002 4 25 ASAA0280076 1 20020319 A 5311 991960563 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON TOP OF FRAME IN AFT CARGO BAY. INSTALLED NEW FRAME PER SRM 53-03, FIG 2A. ( M) 2 L 7 2 4F RT A6WE 2002042500031 20020425 00031 WP 2002 4 25 ASAA0280077 1 20020319 A 5321 993061221 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K CHECK, FOUND CORROSION ON FLOOR WEB IN PAX CABIN. INSTALLED NEW WEB PER SRM 53-01 AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002042500032 20020425 00032 WP 2002 4 25 ASAA0280078 1 20020319 A 5321 993053865N FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON FLOOR WEB AT FS 235-313. INSTALLED NEW WEB PER SRM 51-30-2 AND SRM 52-30-1. (M) 2 L 7 2 4F RT A6WE 2002042500033 20020425 00033 WP 2002 4 25 ASAA0280079 1 20020319 A 5321 993061215 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON FLOOR WEB AT FS 1250-1271. TRIMMED CORRODED AREA AND INSTALLED REPAIR DOUBLE R PER SRM 51-70-4 AND SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002042500034 20020425 00034 WP 2002 4 25 ASAA0280080 1 20020319 A 5347 SR095301157003 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K CHECK, FOUND CORROSION ON SEAT TRACK AT FS 1174. CUT OUT CORRODED AREA AND SPLICED IN NEW SECTION PER SRM 53-05 FIG 4. (M) 2 L 7 2 4F RT A6WE 2002042500035 20020425 00035 WP 2002 4 25 ASAA0280081 1 20020319 A 5320 DWG9910151 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K CHECK, FOUND CORROSION ON WEB AT FS 828-845. CUT OUT CORRODED AREA AND INSTALLED REPAIR DOUBLER PER SR M 51-70-4. (M) 2 L 7 2 4F RT A6WE 2002042500036 20020425 00036 WP 2002 4 25 ASAA0280082 1 20020319 A 5320 9930538 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K CHECK, FOUND WEB CRACKED AT FASTENER HOLE AT FS 314. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2002042500037 20020425 00037 WP 2002 4 25 ASAA0280083 1 20020319 A 5320 993053812 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K CHECK, FOUND CUSP WEB CORRODED AT FS 560-579. REPLACED WEB PER SRM 51-30-2, -1, 2, AND -5. (M) 2 L 7 2 4F RT A6WE 2002042500038 20020425 00038 WP 2002 4 25 ASAA0280084 1 20020319 A 5320 993053877 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K CHECK, FOUND WEB CORRODED AT FS 693-712. REPLACED WEB PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002042500039 20020425 00039 WP 2002 4 25 ASAA0280085 1 20020319 A 5320 99305388N WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K CHECK, FOUND WEB CORRODED AT FS 731-750. REPLACED WEB PER SRM 51-30-2, 51-10-4, AND 51-30-6. (M) 2 L 7 2 4F RT A6WE 2002042500040 20020425 00040 WP 2002 4 25 ASAA0280086 1 20020319 A 5347 SR095301157003 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K CHECK, FOUND CORROSION ON SEAT TRACK AT FS 235-239. CUT OUT CORRODED LENGTH OF TRACK AND INSTALLED REP LACEMENT SECTION PER SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2002042500041 20020425 00041 WP 2002 4 25 ASAA0280087 1 20020319 A 5320 9930538U9 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K CHECK, FOUND CORROSION ON WEB AT FS 674-693. REPLACED WEB PER SRM 51-30-2 AND 51-10-4. (M) 2 L 7 2 4F RT A6WE 2002042500042 20020425 00042 WP 2002 4 25 ASAA0280088 1 20020319 A 5755 59545913 FITTING DOUG DC9 DC983 3022083 WP SPOILER CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K CHECK, FOUND LEFT WING OUTBOARD FLIGHT SPOILER CENTER HINGE FITTING CORRODED. REPLACED SPOILER HINGE F ITTING PER CMM 27-61-10. (M) 2 L 7 2 4F RT A6WE 2002042500043 20020425 00043 WP 2002 4 25 ASAA0280089 1 20020319 A 5755 59545913 FITTING DOUG DC9 DC983 3022083 WP SPOILER CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND LEFT WING INBOARD FLIGHT SPOILER CENTER HINGE FITTING CORRODED. REPLACED SPOILER HINGE FI TTING PER CMM 27-61-10. (M) 2 L 7 2 4F RT A6WE 2002042500044 20020425 00044 WP 2002 4 25 ASAA0280090 1 20020319 A 5755 59545913 FITTING DOUG DC9 DC983 3022083 WP SPOILER CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND LEFT WING GROUND SPOILER CENTER HINGE FITTING CORRODED. REPLACED SPOILER HINGE FITTING PE R CMM 27-61-10. (M) 2 L 7 2 4F RT A6WE 2002042500045 20020425 00045 WP 2002 4 25 ASAA0280091 1 20020319 A 5755 59545913 FITTING DOUG DC9 DC983 3022083 WP SPOILER CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND RIGHT WING GROUND SPOILER CENTER HINGE FITTING CORRODED. REPLACED SPOILER HINGE FITTING P ER CMM 27-61-10. (M) 2 L 7 2 4F RT A6WE 2002042500046 20020425 00046 WP 2002 4 25 ASAA0280092 1 20020319 A 5755 59545913 FITTING DOUG DC9 DC983 3022083 WP SPOILER CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K CHECK, FOUND RIGHT WING INBOARD FLIGHT SPOILER CENTER HINGE FITTING CORRODED. REPLACED SPOILER HINGE F ITTING PER CMM 27-61-10. (M) 2 L 7 2 4F RT A6WE 2002042500047 20020425 00047 WP 2002 4 25 ASAA0280093 1 20020319 A 5755 59545913 FITTING DOUG DC9 DC983 3022083 WP SPOILER CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND RIGHT WING OUTBOARD FLIGHT SPOILER CENTER HINGE FITTING CORRODED. REPLACED SPOILER HINGE FITTING PER CMM 27-61-10. (M) 2 L 7 2 4F RT A6WE 2002042500048 20020425 00048 WP 2002 4 25 ASAA0280094 1 20020319 A 5320 993053811 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND WEB CORRODED AT FS 522-541. REPLACED WEB PER SRM 51-30-02 AND 51-10-4. (M) 2 L 7 2 4F RT A6WE 2002042500049 20020425 00049 WP 2002 4 25 ASAA0280095 1 20020319 A 5347 SR095301157003 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND SEAT TRACK GOUGED AT FS 547. REMOVED SEAT TRACK SECTION FROM FS 531-550. SPLICED IN NEW SECTION. (M) 2 L 7 2 4F RT A6WE 2002042500050 20020425 00050 WP 2002 4 25 ASAA0280096 1 20020319 A 5320 99367184 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K CHECK, FOUND CORROSION ON UPPER SURFACE OF INTERCOSTAL IN AFT CARGO BAY AT FS 1309-1322. REPLACED INTE RCOSTAL PER SRM 51-30-5 AND 41-30-2. (M) 2 L 7 2 4F RT A6WE 2002042500051 20020425 00051 2002 4 25 WRLA200205 4 20020201 A 3414 2594466905 INDICATOR DOUG DC10 DC1030F 3023504 WP COCKPIT INOPERATIVE A WRLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 304WL 47928 DURING TAKEOFF ROLL CAPTAIN AIRSPEED WOULD NOT INDICATE ANY AIRSPEED. NO CADC FLAG WERE SHOWING. FIRST OFFICERS AND AU X AIRSPEED INDICATORS WERE READ 100 KNOTS PRIOR TO REJECTING THE TAKEOFF. REPLACED CAPTAINS AIR SPEED INDICATOR PART NR 2594466-905 S/N ON 30505552 S/N OFF 80071397. PERFORMED PITOT CHECK OPERATION NORMAL. REPLACED CAPTAINS AIR SPEED IND ICATOR. (M) 2 L 7 3 4F RT A22WE 2002042500064 20020425 00064 NM 2002 4 25 AWXA200200356 1 20020422 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 184AW 22651 PHX - EEL - EMERGENCY ESCAPE PATH SEAT LIGHTS ON ALL SEATS EXCEPT LAST FIVE ROWS AND EMERGENCY EXIT LIGHTS AT L1 AND L2 DOOR ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED 2 EACH EMERGENCY LIGHTING BATTERY PACKS UNDER SEATS AT ROWS 3 AN D 11 LT IAW BMM 33-51-18-1, TR 033-018W, OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 2002042500065 20020425 00065 NM 2002 4 25 C1HA200282011 1 20020421 A 5270 WARNING SYSTEM BOEING 727 7272S7 138407Z NM COCKPIT ACTIVATED A C1HA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 682CA 22019 AMBER AIRSTAIR ANNUNCIATOR ILLUMINATED INFLIGHT. VISUAL INSPECTION FROM AFT ENTRY REVEALED DAYLIGHT FROM RIGHT AFT STAI R. DIVERTED TO ORD AND DUMPED FUEL. UPON ARRIVAL FOUND AIRSTAIR IN UP AND LOCKED POSITION. CHECKED OPERATIONS OF AIRS TAIRS PER MM. INSPECTED DOOR ROLLERS, LOCKS AND SWITCHES. ALL CHECKS NORMAL WITH STAIR IN UP AND LOCKED POSITION. NO DAYLIGHT VISIBLE. AIRCRAFT OK FOR SERVICE. 2 L 7 3 4F A3WE 2002051000075 20020510 00075 SO 2002 5 10 C2XA02BT016 1 20020419 A 2530 CONNECTOR EMB 145 EMB145LR 3260212 SO GALLEY DIRTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 11548 145565 CREW REPORTED STRONG SMELL OF ELECTRICAL BURNING FORWARD CABIN/FORWARD GALLEY. MAINTENANCE INSPECTED AND FOUND BURNT CO FFEE POT CONNECTOR. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT ARRIVED IN MAINTENANCE BASE, MAINTENANCE CLEANED COFFEE POT CONNECTOR AND OPS CHECKED COFFEE POT GOOD. 2 L 7 2 4T RT T00011AT 2002042500066 20020425 00066 WP 2002 4 25 CALA0200233 1 20020422 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 49525 INSPECTION FOUND TWO .5 INCH CRACKS IN WEB DOUBLER AT AFT SIDE OF AFT CARGO DOOR JAMB AT STA 1212 ABOVE LONGERONS 27R-28 R. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5310-03742. 2 L 7 2 4F RT A6WE 2002042500067 20020425 00067 NM 2002 4 25 DHL2002715006 1 20020423 A 3150 WARNING SYSTEM BOEING 727 727155C 138404Z NM COCKPIT ACTIVATED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 715DH 19618 TAKEOFF REJECTED FOR AURAL WARNING HORN. CYCLED FLAPS AND SPEED BRAKE, VERIFIED MOVEMENT OF FLT CONTROL SURFACES. PERF ORMED AURAL OPERATIONAL CHECKOUT IAW 31-26-0. OP CHECK GOOD. 2 L 7 3 4F A3WE 2002042500068 20020425 00068 NM 2002 4 25 DL72L020420 1 20020408 A 3350 900542 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 504DA 21306 FOUND AFT EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY RACK. 2 L 7 3 4F A3WE 2002042500069 20020425 00069 NM 2002 4 25 DL72S020398 1 20020403 A 5720 STIFFENER BOEING 727 727232 1384082 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 NR 7 SLAT I/B TRACK I/B SPAR STIFFENER CRACKED. REPLACING STIFFENER PER M/M 57-20-021-8. 2 L 7 3 4F A3WE 2002042500070 20020425 00070 NM 2002 4 25 DL72S020401 1 20020403 A 5755 CASTING BOEING 727 727232 1384082 NM SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 NR 7 SPOILER LWR CASTING REPAIR CRACKED AT LWR WING ATTACH. REPAIRED PER MM 57-20-022-8. 2 L 7 3 4F A3WE 2002042500071 20020425 00071 CE 2002 4 25 DKB2002F00000 1 20020311 A 2750 2660001105 CABLE CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA TE FLAP BROKEN A DKBA K NONE O OTHER IN INSP/MAINT 1 SO 09 699BA 2997 208B0833 RIGHT FLAP CABLE THAT ATTACHES TO THE OUTBOARD END OF FLAP, FOUND WITH BROKEN STRANDS, WHERE THE CABLE IS SWAGED TO THE TERMINAL THAT CONNECTS TO THE FLAP. 1 H 7 1 3T 3 T A37CE E2NE 2002042900009 20020429 00009 NM 2002 4 29 F3LA200200133 1 20020424 A 5320 655289416 FLOOR SUPPORT BOEING 737 73736E 138443A NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 3461 25263 DURING C-2 CHECK, INSPECTION REPORTED CRACK IN A/C DISTRIBUTION BAY FLOOR SUPPORT RT OF CENTER AT STA 540. REMOVED DAMA GED FLOOR SUPPORT. INSTALLED NEW SUPPORT AND FLOOR PANELS PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002042500072 20020425 00072 NM 2002 4 25 DL72S020422 1 20020409 A 7120 MOUNT BOEING 727 727232 1384082 NM NR 3 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 INSPECTION OF THE FWD ENGINE MOUNT SUPPORT FITTING ON THE NR 3 ENGINE PYLON PER AD 97-05-08 REVEALED A CRACK IN HOLE LOC ATION -D-. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND AN ADDITIONAL INSURANCE CUT TAKEN. THE REWORK WAS ACCOMPLISH ED PER FED EX S/B 2000-5410A01 AND ER/A 382909-14AD. 2 L 7 3 4F A3WE 2002042500074 20020425 00074 NM 2002 4 25 DL72S020459 1 20020419 A 5754 RIB BOEING 727 727225A 1384077 NM L/E SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 L/E NOSE RIB ON NR 5 SLAT I/B SIDE OF ACTUATOR ROD END IS CRACKED. REPAIRED PER M/M 57-54-000-8 AND ERA 382989-14. 2 L 7 3 4F RT A3WE 2002042500075 20020425 00075 NM 2002 4 25 DL72S020460 1 20020421 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 526DA 21586 OVERHEAD EMERGENCY EXIT SIGN IN CENTER AISLE BY FWD GALLEY INOP. REPLACED BATTERY PACK, OPS NORMAL. 2 L 7 3 4F A3WE 2002042500076 20020425 00076 NM 2002 4 25 DL72S020464 1 20020421 A 3350 900542 CHARGER BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 519DA 21470 FOUND AFT OVERHEAD EMERGENCY LIGHT INOP FWD OF AIRSTAIR DOOR. REMOVED AND REPLACED BATTERY PACK CHARGING RACK. CHECKS GOOD. 2 L 7 3 4F A3WE 2002042500077 20020425 00077 NM 2002 4 25 DL72S020465 1 20020421 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 526DA 21586 CENTER AISLE EMERGENCY EXIT SIGN OVERHEAD AT ROW 21 INOP. REPLACED BATTERY PACK, OPS NORMAL. 2 L 7 3 4F A3WE 2002042500078 20020425 00078 NM 2002 4 25 DL72S020473 1 20020422 A 3350 900542 CHARGER BOEING 727 727225A 1384077 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8890Z 21859 FOUND AFT OVERHEAD EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGING RACK. CHECKS GOOD. 2 L 7 3 4F RT A3WE 2002042500079 20020425 00079 NM 2002 4 25 DL72W020427 1 20020411 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 293WA 22111 FWD BULLNOSE EMERGENCY LIGHT INOP. FOUND BATTERY PACK BAD, REPLACED SAME. 2 L 7 3 4F A3WE 2002042500080 20020425 00080 NM 2002 4 25 DL733020423 1 20020410 A 5755 SKIN BOEING 737 737347 1384647 NM SPOILER DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 OUTBOARD SPOILER UPPER SKIN WAS FOUND DELAMINATED. REPAIR PER ER/A 411175-14 AND NORDAM EWO E0037508 REV I/R. 2 L 7 2 4F RT A16WE 2002042500081 20020425 00081 NM 2002 4 25 DL733020424 1 20020410 A 3397 WIRE BOEING 737 737347 1384647 NM CABIN DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3301 23181 EMERGENCY EXIT LIGHT ON SEAT 12D INOP. FOUND WIRES PULLED FROM CONNECTOR. REWIRED CONNECTOR, LIGHT OPNS NORMAL. 2 L 7 2 4F RT A16WE 2002042500082 20020425 00082 NM 2002 4 25 DL738020408 1 20020405 A 2550 255140567 RESTRAINT BOEING 737 737832 13844CF NM CARGO BAY WORN A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 394DA 30562 TAKEOFF ABORTED FOR MASTER CAUTION/AFT CARGO DOOR WARNING LIGHT. ABORT OCCURRED AT 90 KTS GW 148000/OAT 24C. REPLACED AFT CARGO PIT REAR NET RT SIDE AND FLOOR ANCHOR AFT LOWER FOR NET ACCT WORN/AFT CARGO LIGHT, OPS NORMAL. 2 L 7 2 4F RT A16WE 2002042500083 20020425 00083 NM 2002 4 25 DL738020429 1 20020411 A 2750 285A12001 FSEU BOEING 737 737832 13844CF NM E/E BAY MALFUNCTIONED A DALA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 390DA 30536 TRAILING EDGE FLAPS EXTENDED AT 240 KTS TO FIVE DEGREES, FLAPS STOPPED AT MID POSITION BETWEEN UP AND 1. T/S-READ FSEU BITE, NO FAULTS. REPLACED FSEU PER M/M, NO FAULTS. INSPECTED FLAPS AND FLAPS OPERATE NORMALLY. OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2002042500084 20020425 00084 NM 2002 4 25 DL73K020432 1 20020411 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR (R2) CUTOUT WAS FOUND WITH A .5 INCH TYPICAL CRACK IN THE BONDED SKIN ASSY . THE CRACK WAS REMOVED. THE SKIN WAS REPAIRED WITH AN EXTERNAL DOUBLER INSTALLED PER ER/A 382883-14 REV A. 2 L 7 2 4F A16WE 2002042500085 20020425 00085 NM 2002 4 25 DL757020400 1 20020327 A 5410 311N315113 FITTING BOEING 757 757232 1384965 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 DURING INSPECTION THE NR 1 PYLON STRUT ATTACH MIDSPAR FITTING INBOARD FITTING OUTBOARD LUG A CRACK INDICATION WAS NOTED. THE LUG WAS OVERSIZED TO REMOVE CRACK INDICATION. REPAIRED PER ER/A 389368-14, REV A. 2 L 7 2 4F RT A2NM 2002042500086 20020425 00086 NE 2002 4 25 DL757020415 2 20020406 A 7200 FIRE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE DETECTED A DALA O OTHER P B A NO WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 624DL 40536 22914 716315 DURING ENGINE START ON RT ENG, FLT ATT REPORTED A FIRE ON THE RIGHT ENG. REPORTED SMOKE AND FLAMES OUT THE RIGHT TAIL P IPE. SMOKE IN CABIN. ENG FUEL WAS CUT OFF, MOTORED FOR 30 SECS AND STARTER WAS TURNED OFF. NO COCKPIT INDICATION OF E NG FIRE. OPEN ENG VERIFIED SVA AND 2.5 BLEED FULL OPEN. REPLACED NR 1 AND NR 2 IGNITORS AS PRECAUTION. INSPECTED INLE T AND EXHAUST, NO TROUBLE FOUND. RAN ENG WITH PACKS, NO TROUBLE FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 2002042500088 20020425 00088 NE 2002 4 25 DL757020438 2 20020413 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 DAMAGED A DALA A UNSCHED LANDING A Y FLAME/FIRE ENGINE STOPPAGE CL CLIMB 1 SO 27 610DL 51086 22817 716308 ON TAKEOFF AT 140 KNTS AND 800 FT LEFT ENGINE LOST POWER DURING GEAR RETRACTION. ENGINE CONTINUED TO ROLLBACK AND SHUTD OWN. SURGE AND FLAME FROM INLET REPORTED BY PASSENGERS. CONTRACT MTC REPORTS METAL PARTICLES IN TAILPIPE. ENGINE WILL REQUIRE REPLACEMENT IN BNA. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002042500089 20020425 00089 NM 2002 4 25 DL757020439 1 20020414 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 658DL 24420 FOUND ON LAYOVER SEVERAL EMERGENCY LIGHTS INOP IN AFT LEFT CABIN. REPLACED M737 POWER SUPPLY. NOW CHECKS OKAY. 2 L 7 2 4F RT A2NM 2002042500090 20020425 00090 WP 2002 4 25 IXXA0200025O 1 20020417 A 2923 57155A PUMP DOUG DC8 DC871 302199A WP HYD SYSTEM LEAKING A IXXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 11 829BX 84933 634 45994 EN ROUTE FROM SEA TO ANC, THE FLT CREW NOTICED A DECLINE IN THE MAIN HYD SYS QUANTITY. THE FLT CREW NOTICED WHILE FOLLO WING COMPANY PROCEDURES THE HORIZONTAL STABILIZER ALTERNATE TRIM INOPERATIVE. THE FLT CONTINUED TO ANC FOR AN UNEVENTFU L LANDING. MX INSPECTED THE ACFT WHICH REVEALED THE STANDBY RUDDER PUMP LEAKING. MX REPLACED THE STANDBY RUDDER PUMP I N ACCORDANCE WITH THE MM. MX FOUND THE ALTERNATE STABILIZER ELECTRICAL TRIM MOTOR ELECTRICAL CONNECTOR CONTAMINATED WIT H MOISTURE. MX CLEANED THE ELECTRICAL CONNECTOR AND PERFORMED A SUCCESSFUL OPS CHECK. THE ACFT WAS RETURNED TO SERVICE . 2 L 7 4 4F 4A25 2002042500092 20020425 00092 NM 2002 4 25 QXEA0200637 1 20020415 A 2120 ODOR DHAV DHC8 DHC8202 2809007 NM COCKPIT DETECTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 375PH 529 PDX- FISHY ODOR IN COCKPIT. CHECKED INVERTERS, NO DEFECTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAF T RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042500093 20020425 00093 2002 4 25 00020 4 20020423 A 3422 25883023 GYRO AMD FALC20 FALCON 2720302 EU COCKPIT FAILED E HAEA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 977TW 13 HSI AND RMI COPILOT SIDE OF AIRCRAFT WOULD NOT MOVE, RETURN TO DEPARTURE AIRPORT. REMOVED AND REPLACED NR 2 DIRECTIONAL GYRO, OP'S CHECK GOOD ON GROUND. RETURN AIRCRAFT TO SERVICE. 2 L 7 2 4F A7EU 2002042500094 20020425 00094 CE 2002 4 25 00021 1 20020423 A 1430 COTTER PIN LEAR 24 24D 5170311 CE GE CJ610 CJ6106 30006 NE THROTTLE OUT OF POSITION E HAEA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 05 266TW 266 PILOT REPORTED STUCK THROTTLE, FOUND COTTER PIN CATCHING QUADRANT. REPAIRED COTTER PIN , OP'S CHECK GOOD. RETURN AIRCR AFT TO SERVICE. 2 L 7 2 4J 4 J A10CE 1E16 2002042500095 20020425 00095 WP 2002 4 25 0201259611 1 20020408 A 5730 SKIN DOUG DC9 DC932 3022066 WP LT WING CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611NA 47435 DURING HCK IN ATL, CORROSION WAS FOUND ON THE LEADING EDGE OF LT WING. DAMAGE WAS TRIMMED OUT AND REPAIR WAS ACCOMPLISH ED PER EA 96-188468. 2 L 7 2 4F A6WE 2002042500096 20020425 00096 WP 2002 4 25 0201279611 1 20020411 A 5320 STIFFENER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611NA 47435 DURING AN HCK IN ATL, ONE .60 INCH LONG CRACK WAS FOUND IN THE STA 756 BULKHEAD. THE CRACK IS LOCATED IN THE UPPER END OF THE VERTICAL STIFFENER AT X=22. THIS EA 96-188473 PROVIDES REPAIR INSTRUCTIONS FOR THIS CRACK. 2 L 7 2 4F A6WE 2002042500098 20020425 00098 WP 2002 4 25 0201289611 1 20020411 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611NA 47435 DURING CHK IN ATL, THE FORWARD UPPER CORNER OF THE CARGO DOOR JAMB WAS FOUND CRACKED .0625. THE REPAIRS WERE MADE IAW E A 96-188479. 2 L 7 2 4F A6WE 2002042500100 20020425 00100 NM 2002 4 25 02FDEA00227 1 20020405 A 2612 FIRE WARNING BOEING 727 727233 138408A NM COCKPIT FALSE ACTIVATION A FDEA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 25 283FE 22350 DURING CLIMBOUT FIRE IND ON APU. APU MASTER SWITCH OFF AND IND SHOW NORMAL SHUTDOWN. REMOVED AND REPLACED APU FIRE AND OVERHEAT DET SYS PER PRECAUTIONARY MM 26-15-003-4. 2 L 7 3 4F RT A3WE 2002042500101 20020425 00101 CE 2002 4 25 HYI2002F00010 1 20020408 A 3110 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO LT SWITCH PANEL FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 83PB 1301 402C0350 AVIONICS MASTER SWITCH FAILED DURING TAXI. MAINTENANCE REMOVED AND REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2002042500102 20020425 00102 NE 2002 4 25 02FDEA00249 2 20020412 A 7321 MEC DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE OUT OF RIG A FDEA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 25 319FE 47820 455125 ON TAKEOFF NR 3 ENG W/N ATTAIN MAX PWR. ADJUSTED NR 3 ENG MEC 1/2 TURN UPTRIM, RAN ALL ENG PER JRH CHAPTER 5 AND ACCOMP LISHED MAX. ALL ENGINES OPERATING OKAY. 2 L 7 3 4F 4 F RT A22WE E23EA 2002042500103 20020425 00103 CE 2002 4 25 HYI2002F00011 1 20020322 A 3110 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO LT SWITCH PANEL INOPERATIVE E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 406GA 1310 402C0329 ON PREFLIGHT, CREW REPORTED AVIONICS MASTER SWITCH, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SWITCH AND RETURN ED THE AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2002042500104 20020425 00104 WP 2002 4 25 02FDEA00271 1 20020420 A 5610 WINDOW DOUG DC10 DC1010 3022110 WP COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 550FE 46521 CAPT'S WINDSCREEN OUTER PANEL SHATTERED. REMOVED AND REPLACED CAPT'S L1 WINDOW PER MM 56-11-00-2. 2 L 7 3 4F A22WE 2002042500105 20020425 00105 NE 2002 4 25 PG92002F00000 2 20020318 A 7200 ARRIEL1D1 ENGINE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE NACELLE FAILED A PG9A A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 19 170PA 1747 2637 9433 ENGINE CHIP LIGHT ILLUMINATED DURING PART 135 FLIGHT. PILOT MADE PRECAUTIONARY LANDING ON IMPROVED PRIVATE HELIPAD. ME CHANIC DISPATCHED TO SIDE. FOUND EXCESSIVE METAL SLIVERS ON ALL ENGINE OIL SYSTEM MAGNETIC AND INDICATOR CHIP DETECTORS . AIRCRAFT GROUNDED FROM FURTHER FLIGHT. AIRCRAFT TRUCKED BACK TO BASE, AND ENGINE WAS REMOVED. 1 G 7 1 3U 3 U H9EU E19EU 2002042500106 20020425 00106 NM 2002 4 25 02FDEA00272 1 20020423 A 2781 SWITCH BOEING 727 7272S2F 1384O81 NM L/E FLAP FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 216FE 22937 L/E FLAP NR 5 IND INTRANSIT LIGHT ON FWD INSTRUMENT PANEL AND AUX PANEL. REMOVED AND REPLACED FLAP POS SW FOR NR 5 KRUE GER FLAP PER MM 27-82-001-4. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002050200060 20020502 00060 NM 2002 5 2 02FDEA00273 1 20020423 A 2910 HYDRAULIC LINE BOEING 727 7272D4 138407U NM HYD SYSTEM FAILED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 287FE 21849 HYDRAULIC A SYSTEM FAILURE DURING GEAR RETRACT FLUID QTY DEPLETED TO ZERO, EXCEEDED HYD FLUID S/O VALVE LIMITATION. REM OVED AND REPLACED LINE, CHECKED ALL A-SYS. LEAK CHECK GOOD. 2 L 7 3 4F A3WE 2002042600101 20020426 00101 NM 2002 4 26 02FDEA00274 1 20020420 A 5754 STRUCTURE BOEING 727 727225 1384077 NM L/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 NR 5 K-FLAP OUTBOARD LWR BONDING JUMPER UPPER ATTACH POINT IS CORRODED. REMOVED AND REPLACED FLAP PER DWG SR 27-97-010. 2 L 7 3 4F A3WE 2002042600103 20020426 00103 NM 2002 4 26 02FDEA00276 1 20020419 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 204FE 22926 CREASE IN SKIN BS 1065, STR 19R - 20R. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 2002042600104 20020426 00104 NM 2002 4 26 02FDEA00278 1 20020417 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 CORROSION ON UPPER FLANGE OF FLOORBEAM BS 312, LBL 3-19. REMOVED AND REPLACED FLOORBEAM PER DWG SR 27-53-017A. 2 L 7 3 4F A3WE 2002042600106 20020426 00106 NM 2002 4 26 02FDEA00280 1 20020414 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 HOLES IN FLOORBEAM AT BS 400, RBL 60-65, WL 208. REMOVED AND REPLACED FLOORBEAM PER EA 7-5335-54192 & SRM 53-10-8 FIG 3 . 2 L 7 3 4F A3WE 2002050700066 20020507 00066 NM 2002 5 7 02FDEA00281 1 20020418 A 3230 FITTING DOUG MD11 MD11F 3023600 NM RT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 RT MLG RETRACT ACTUATOR FITTING FOUND CORRODED ON LOWER BOLT HOLES. REMOVED AND REPLACED ACTUATOR FITTING PER SRM 51-31 -01 VOL 11. 2 L 7 3 4F RT A22WE 2002050700067 20020507 00067 NM 2002 5 7 02FDEA00282 1 20020419 A 3230 FITTING DOUG MD11 MD11F 3023600 NM LT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 LT MLG RETRACT ACTUATOR FITTING FOUND PITTING CORROSION ON UPPER FWD BOLT HOLE. REMOVED AND REPLACED ACTUATOR FITTING P ER SRM 51-31-01 VOL 11. 2 L 7 3 4F RT A22WE 2002050700068 20020507 00068 NM 2002 5 7 02FDEA00283 1 20020417 A 3230 FITTING DOUG MD11 MD11F 3023600 NM LT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 LT MLG RETRACT ACTUATOR FITTING FOUND BOTH LOWER MOUNTING BOLT HOLES CORRODED (PITTING CORROSION). REMOVED AND REPLACED ACTUATOR FITTING PER SRM 51-31-01 VOL 11. 2 L 7 3 4F RT A22WE 2002050700105 20020507 00105 NM 2002 5 7 02FDEA00284 1 20020420 A 5314 KEELBEAM BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 204FE 22926 CORROSION (C53-113-01, 02) ON O/B FLANGE OF KEEL BEAM BS 950B - 950D, RBL 8. REMOVED FLANGE PER EA 7-5310-64072. 2 L 7 3 4F A3WE 2002042500107 20020425 00107 NM 2002 4 25 P5CA0200672 1 20020424 A 2421 NONE BEARING BOEING 747 747249F 1384849 NM #2 APU GENERATOR FAILED A P5CA F ACTIVATE FIRE EXT. J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 23 920FT 22237 #2 APU GENERATOR BEARING FAILURE LIGHT ILLUMINATED & GRND CREW REPORTED SMOKE EMANATING FROM APU. FIRE HANDLE PULLED & B OTTLE DISCHARGED AS A PRECAUTION. VISUAL INSPECTION OF APU COMPARTMENT BY MX & F/E SHOWED DAMAGE ONLY TO THE #2 GENERATO R. NO FIRE OR DAMAGE TO OTHER COMPONENTS OR STRUCTURES. DEACTIVATED APU & DEFERRED PER MEL 49-01, DMI #29098. MX XTL LGB NOTIFIED & PLACARDS INSTALLED. 2 L 7 4 4F A20WE 2002042500108 20020425 00108 SW 2002 4 25 XVI2002F00000 1 20020411 A 5302 2050308167S FRAME BELL BELL 204 UH1H 1181407 SW LYC T53 T53L13B 41549 NE TAILBOOM CRACKED B XVIR K NONE O OTHER IN INSP/MAINT 1 NM 01 114DR ABD04421 6600792 X-RAY INSPECTION REVEALED A CRACK IN THE FRAME FLANGE APPROXIMATELY .1250 INCH LONG CONTAINED BY ADJACENT FASTENER HOLE. THE CRACK IS LOCTED IN THE 3 OCLOCK POSITION, LOOKING FORWARD ON THE FRAME. 1 G 7 1 4U 4 U EXPA1G71 E17EA 2002042500109 20020425 00109 WP 2002 4 25 ABXA010829 1 20020422 A 2910 SEAL DOUG DC8 DC863 302198A WP CONTROL VALVE BLOWN A ABXA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 817AX 45928 ON CLIMBOUT, HYDRAULIC QUANTITY DROPPED TO STANDPIPE. EMERGENCY DECLARED. FOUND SLOT CONTROL VALVE MOUNT BOLT SEAL BLO WN. REPLACED SEAL. SLOT SYSTEM OPS AND LEAK CHECKED GOOD IAW DC-8 MM. 2 L 7 4 4F 4A25 2002042500110 20020425 00110 WP 2002 4 25 AT0200051 1 20020423 A 3350 41BO04AD073 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 831AT 47674 AFT ACCESSORY COMPARTMENT EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REMOVED AND REPLACED BATTERIES IN APPLICABLE BATTERY P ACKS, OPS CHECK GOOD. 2 L 7 2 4F A6WE 2002042500111 20020425 00111 NM 2002 4 25 AWXA200200357 1 20020423 A 2560 P4010021 BATTERY BOEING 737 737277 1384570 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 180AW 22647 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED LOWER FLASHLIGHT IN AFT CABIN IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES IN THE AFT CABIN LOWER FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002042500112 20020425 00112 NM 2002 4 25 AWXA200200358 1 20020423 A 3350 BR964411 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 322AW 25400 TUS - EEL - EMERGENCY ESCAPE PATH LIGHT SEAT ROW 14 LT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAP E PATH LIGHT RECEPTACLE AT SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD PER T/C A1C33006. 2 L 7 2 4F RT A16WE 2002042500113 20020425 00113 EU 2002 4 25 AWXA200200359 1 20020423 A 3320 325060 BALLAST AIRBUS 320 A320231 3930325 EU CABIN FAULTY A AWXA K NONE O OTHER CR CRUISE 1 WP 28 626AW 65 PHX - BURNING SMELL - FLT 0467 - DURING FLIGHT, FLIGHT CREW NOTICED A BURNING SMELL SIMILAR TO HOT WIRES AT SEAT ROW 13 LT. MAINTENANCE TROUBLESHOT AND FOUND A BAD CEILING LIGHT BALLAST AT SEAT ROW 13 LT. REPLACED BALLAST IAW AMM 33-21-11 -401, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002042500114 20020425 00114 NM 2002 4 25 AWXA200200360 1 20020408 A 5310 146N559057 CREASE BEAM BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 GYR - MAJOR REPAIR - DURING C-11 CHECK EXFOLIATION CORROSION WAS FOUND ON THE RT CREASE BEAM AT BS 1597, RBL 61.0. MAIN TENANCE CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-12 FIG 1, SHEET 1-6. 2 L 7 2 4F RT A2NM 2002042500115 20020425 00115 SO 2002 4 25 C2XA02CL104 1 20020423 A 2530 1095A30 CONNECTOR EMB 135 EMB135LR 3260305 SO COFFEEMAKER MELTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 28518 145334 CLE FLIGHT 3149 THE CREW REPORTED A BURNING RUBBER SMELL WHEN THE APU WAS STARTED. INSPECTED AND FOUND THE SMELL WAS OR IGINATED FROM A MELTING CONNECTOR ON THE COFFEE HOT JUG. THE COFFEE HOT JUG WAS REPLACED. OPERATIONAL CHECKS WERE GOOD . 2 L 7 2 4F RT T00011AT 2002042500116 20020425 00116 NM 2002 4 25 DL757020441 1 20020415 A 2913 3508807 PUMP BOEING 757 757232 1384965 NM LT ENGINE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 669DN 25142 LEFT HYD ENGINE PUMP ADVISORY MSG AND LT ENGINE ON APPROX 5 MINUTES AFTER TAKEOFF. REPLACED LEFT ENGINE EDP AND MAIN SU PPLY LINE PER M/M, CHECKS OK. 2 L 7 2 4F RT A2NM 2002042500118 20020425 00118 NM 2002 4 25 2002F00414 1 20020216 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 CE 07 801EA 22432 AT C-CHECK FOUND FORWARD CARGO COMPARTMENT FLOORBEAM CORRODED AT STATION 536 RBL 2. (M) 2 L 7 3 4F A3WE 2002042500120 20020425 00120 NM 2002 4 25 2002F00415 1 20020307 A 2621 BOTTLE BOEING 737 7372H4 138448C NM APU EXTINGUISHER DISCHARGED A RYNA F ACTIVATE FIRE EXT. M OVER TEMP CR CRUISE 1 CE 07 29SW 21340 IN FLIGHT, GOT APU OVERHEAT INDICATION. DISCHARGED APU FIRE BOTTLE. AIRCRAFT LANDED WITHOUT INCIDENT. NO EVIDENCE OF FIRE FOUND AFTER APU INSPECTION. (M) 2 L 7 2 4F A16WE 2002042500121 20020425 00121 2002 4 25 2002F00416 4 20020315 A 2397 870012 CIRCUIT BREAKER BOEING 737 7372H4 138448C NM COCKPIT SHORTED A RYNA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 07 29SW 21340 IN FLIGHT, CREW NOTICED CIRCUIT BREAKER POPPED AND ELECTRICAL SMOKE IN COCKPIT. AIRCRAFT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4F A16WE 2002042500123 20020425 00123 SW 2002 4 25 2002F00417 1 20020207 A 7700 2719153001 TRANSDUCER FRCHLD SA227 SA227DC 3377521 SW OIL PRESSURE FAILED A BSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 853LS DC853B DURING CLIMB-OUT, THE CREW NOTICED THE LEFT OIL PRESSURE WAS BELOW THE LOWER REDLINE ON THE GAUGE. THE ANNUNCIATOR PANE L LOW OIL PESSURE LIGHT WAS NOT ON, AND THE OIL TEMP WAS NORMAL. ALL OTHER ENGINE INDICATIONS WERE NORMAL. CREW RETURN ED TO STATION WITH NO FURTHER PROBLEMS. REPLACED OIL PRESSURE TRANSDUCER, CLEANED AND REINSTALLED SNUBBER. (M) 2 L 7 2 4T RT A18SW 2002042500124 20020425 00124 SW 2002 4 25 2002F00418 1 20020131 A 5270 HANDLE SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR STUCK A BSAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NM 05 159MC AC728B CARGO DOOR LIGHT CAME ON DURING TAKEOFF ROLL AT APPROXIMATELY 50 KTS. CREW RETURNED TO GATE. STICKING DOOR HANDLE OR C LICK CLACKS. CLEANED AND LUBED CLICK CLACKS. (M) 2 L 7 2 4T RT A8SW 2002042500125 20020425 00125 2002 4 25 DL757020456 4 20020419 A 2565 654N001041 BOTTLE BOEING 757 757232 1384965 NM CARGO BAY INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 632DL 23613 EMERGENCY ESCAPE TEST 2 BOTTLE PRESSURE INOP ON RIGHT SIDE. REPLACED BOTTLE ASSY PER M/M, TESTS GOOD. 2 L 7 2 4F RT A2NM 2002042500126 20020425 00126 SW 2002 4 25 2002F00419 1 20020129 A 5210 2724089009 DOOR SEAL SWRNGN SA227 SA227AC 8780603 SW PASSENGER DOOR FAILED A BSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 702M AC702 CABIN ALTITUDE WARNING LIGHT CAME ON ABOVE 10,000 FEET. CREW GOT AIRCRAFT TO PRESSURIZE IN EITHER AUTOMATIC OR MANUAL M ODE. CREW RETURNED TO STATION. PASSENGER DOOR SEAL WAS DAMAGED. INITIALLY DEFERRED PRESSURIZATION, THEN LATER REPLACE D CABIN DOOR SEAL. (M) 2 L 7 2 4T RT A8SW 2002042500127 20020425 00127 NM 2002 4 25 DL757020457 1 20020419 A 2910 CLAMP BOEING 757 757232 1384965 NM HYD SYSTEM FAILED A DALA E ENGINE SHUTDOWN K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 607DL 22814 FUEL SUPPLY LINE CHAFED THROUGH IN LEFT ENG STRUT. CHAFING CAUSED BY FAILED HYD TUBE CLAMP/BRACKET ABOVE FUEL LINE. RE PLACED FUEL LINE AND LEAK CHECKED. REPAIRED CLAMP PER ER/A 382986-14. 2 L 7 2 4F RT A2NM 2002042500128 20020425 00128 SW 2002 4 25 2002F00420 1 20020114 A 2910 2781032135 LINE SWRNGN SA227 SA227AC 8780603 SW HYD SYSTEM LEAKING A BSAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 05 27465 AC755B 130 MILES FROM ORIGINATING STATION, AIRCRAFT LOST HYDRAULIC PRESSURE. CREW RETURNED TO STATION AT MAX GEAR EXTENSION SP EED. GEAR WAS PUMPED DOWN USING EMERGENCY CHECKLIST. HYDRAULIC LEAK CAUSED LOSS OF HYDRAULIC FLUID LEADING TO LOSS OF HYDRAULIC PRESSURE. REPAIRED LINE BY SPLICING IN NEW SECTION PER MM. BOTH HYDRAULIC PUMPS CHANGED DUE TO EXCEEDING MM RESTRICTION ON LENGTH OF TIME THE PUMPS CAN RUN WITHOUT FLUID. (M) 2 L 7 2 4T RT A8SW 2002042500130 20020425 00130 EA 2002 4 25 2002F00422 1 20020304 A 2913 AE2460010H0264 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAILED A MASA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 593ML FLT 3322 - SLC-SJC - DIVERTED TO DEN WHEN THE NR 2 HYD SYSTEM PRESSURE WENT TO ZERO. MAINTENANCE REPLACED THE HIGH PRES SURE LINE FROM THE PUMP THROUGH PYLON AND THE PUMP. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002042500131 20020425 00131 NM 2002 4 25 DL757020466 1 20020421 A 3397 WIRE BOEING 757 757232 1384965 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 666DN 25034 EMERGENCY LIGHTS INOP AT R4 AND L4 EXTERIOR EGRESS, 45DEF OVERHEAD AND BOTH AFT RIGHT LAV MODULE. FOUND BROKEN WIRE BET WEEN SEAT ROWS 44 AND 45DEF. REPAIRED WIRE, ALL EMERGENCY LIGHTS NOW CHECK NORMAL. 2 L 7 2 4F RT A2NM 2002042500132 20020425 00132 NM 2002 4 25 DL757020467 1 20020419 A 5320 SILL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 CORROSION WAS FOUND ON THE OUTER CHORD OF THE LOWER SILL BEAM OF THE C1 DOOR OPENING. 2 L 7 2 4F RT A2NM 2002042500133 20020425 00133 NM 2002 4 25 DL757020468 1 20020419 A 5330 141N33314 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 A LONG GOUGE WAS FOUND IN THE FUSELAGE SKIN BETWEEN FS 390 & 435 AND BETWEEN STRINGERS 14L & 15L. THE GOUGE WAS CUTOUT . THE CUTOUT WAS REPAIRED PER ER/A 382877-14, REV A. 2 L 7 2 4F RT A2NM 2002042500134 20020425 00134 NM 2002 4 25 DL757020469 1 20020419 A 5330 143N36504 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 644DL 23998 CORROSION WAS FOUND IN THE FUSELAGE SKIN AT A FAIRING NUT PLATE ATTACH LOCATION NEAR FS 780 AND STRINGER 18R. THE CUTOU T WAS REPAIRED PER ER/A 382916-14, REV A. 2 L 7 2 4F RT A2NM 2002042500135 20020425 00135 NM 2002 4 25 DL757020471 1 20020422 A 3244 B757N TIRE BOEING 757 757232 1384965 NM RT NLG SEPARATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 605DL 22812 ON L/O, FOUND RT NLG TREAD SEPARATED. REPLACED RT NLG WHEEL ASSY PER M/M. 2 L 7 2 4F RT A2NM 2002042500136 20020425 00136 NE 2002 4 25 HNAA0200035 2 20020421 A 7200 310450001 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE SHUTDOWN A HNAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 07 928HA 19054 10010 120 121320 IN CRUISE FLIGHT THE #2 ENGINE OIL PRESSURE DROPPED BELOW 40 PSI. CREW SHUT DOWN ENGINE. ON THE GROUND IT WAS FOUND THAT THE ENGINE, NACELLE AND GEAR WERE COVERED WITH OIL AND THAT THE PROP WOULD NOT TURN. REPLACED #2 ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002042500137 20020425 00137 NM 2002 4 25 DL757020472 1 20020422 A 3350 BR9279108 SIGN BOEING 757 757232 1384965 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 663DN 24992 ON L/O, FOUND AFT LT EMERGENCY EXIT SIGN DAMAGED. REMOVED BROKEN PARTS AND INSTALLED NEW LIGHT ASSY. 2 L 7 2 4F RT A2NM 2002042500138 20020425 00138 2002 4 25 DL764020417 4 20020408 A 3425 H341CBM INDICATOR BOEING 767 767432ER 1385134 NM COCKPIT FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 829MH 29700 STANDBY ATTITUDE INDICATOR WILL NOT STAY ERECT. REPLACED INDICATOR. 2 L 7 2 4F RT A1NM 2002042500139 20020425 00139 NE 2002 4 25 HNAA020034 2 20020423 A 7200 310450001 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEAKING A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 07 923HA 26614 8290 099 120875 CREW REPORTED SMOKE IN THE COCKPIT DURING DESCENT TO LAND. ON THE GROUND, OIL WAS FOUND LEAKING FROM THE INTAKE OF #1 EN GINE. REPLACED #1 ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002042500140 20020425 00140 NM 2002 4 25 HNAA0200027 1 20020311 A 5310 SKIN DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 933HA 134 During 40K inspection corrosion was found on the interior of the A/C in the center of a bay between frames 202 and 222 a nd between stringers 32 left and right. The corroded area was cut out and a doubler installed per EO8-53-02-0228. 2 H 7 2 4T RT A13NM 2002042500141 20020425 00141 NM 2002 4 25 HNAA0200028 1 20020311 A 5347 85320490135 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 933HA 134 During 40K inspection the right hand inboard seat rail was found to be corroded at fastener holes for the lav. and galle y. The damaged portion of the seat track was removed and a new section spliced in per RD8-53-3074. 2 H 7 2 4T RT A13NM 2002042500142 20020425 00142 NM 2002 4 25 HNAA0200029 1 20020311 A 5313 85320056103 STRINGER DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 933HA 134 During 40K inspection corrosion was found along the length of stringer 31S. The stringer was changed along with several tension fittings and frame legs along the length of stringer 31S. 2 H 7 2 4T RT A13NM 2002042500143 20020425 00143 NM 2002 4 25 DL764020463 1 20020421 A 3350 CONNECTOR BOEING 767 767432ER 1385134 NM CABIN DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 832MH 29704 EMERGENCY PATH LIGHTING INOP BETWEEN SEATS 25FG AND 32FG. FOUND CONNECTOR DISCONNECTED AT SEAT 25FG. RECONNECTED PLUG OPERATION NOW NORMAL. ITEM FOUND ON ETOPS PREDEPARTURE CHECK. 2 L 7 2 4F RT A1NM 2002042500144 20020425 00144 WP 2002 4 25 ABXA010835 1 20020418 A 5310 FITTING DOUG DC8 DC861 3021952 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 FUSELAGE STATION 1168, RIGHT SIDE UPPER CUSP LINE CORNER CASTING FROM CUSP EXTRUSION TO STATION 1168 VERTICAL SUPPORT, H AD A CRACK INDICATION FROM BOLT HEAD TO EDGE OF PART, INBOARD SIDE. REPLACED FITTING AND REPAIRED AREA IAW DC-8 SRM 51-3 -2, 51-1-20D AND 51-1-21D. 2 L 7 4 4F 4A25 2002042500145 20020425 00145 WP 2002 4 25 ABXA010836 1 20020418 A 5300 FITTING DOUG DC8 DC861 3021952 WP FWD LWR CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 FORWARD CARGO AT F.S. 330, 'T' BOLT LATCH ATTACH FITTING WAS CORRODED BETWEEN LONGERON 33 RIGHT. REMOVED AND REPLACED BA CKUP FITTING IAW DC-8 MM. 2 L 7 4 4F 4A25 2002042500146 20020425 00146 WP 2002 4 25 ABXA010837 1 20020418 A 5300 3755822502N FITTING DOUG DC8 DC861 3021952 WP FWD LWR CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 FORWARD CARGO AT F.S. 350, BETWEEN LONGERON 36 - 35 LEFT, 'Z' FITTING WAS CRACKED. REPLACED 'Z' FITTING AND REPAIRED ARE A IAW DC-8 SRM 51-1-8, 51-1-20D, 51-3-2 AND 53-2-0. 2 L 7 4 4F 4A25 2002042500147 20020425 00147 WP 2002 4 25 ABXA010838 1 20020418 A 5300 SPAR CAP DOUG DC8 DC861 3021952 WP RT WHEEL WELL CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 F.S. 857, BUTT LINE 54 RIGHT, 16" BELOW THE RIGHT MAIN LANDING GEAR WHEEL WELL CEILING, FORWARD BULKHEAD SKIN WAS CORROD ED. FABRICATED REPAIR DOUBLER AND SHIM IAW REA D857-43109MR. INSTALLED PARTS AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1 -20D AND REA D857-43109MR. 2 L 7 4 4F 4A25 2002042500148 20020425 00148 WP 2002 4 25 ABXA010839 1 20020418 A 5700 975301899 ATTACH ANGLE DOUG DC8 DC861 3021952 WP #1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 #1 ENGINE PYLON FOOTSTOOL WAS CRACKED AT THE '6'O-CLOCK POSITION, CENTER BOLT AND NEXT BOLT OUTBOARD. REPAIRED AREA IAW D854-43106MR. 2 L 7 4 4F 4A25 2002042500149 20020425 00149 WP 2002 4 25 ABXA010840 1 20020418 A 5300 5616306 RIB DOUG DC8 DC861 3021952 WP RT WHEEL WELL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 F.S. 870, RIGHT WHEEL WELL, LOWER OUTBOARD RIB REPAIR WAS CRACKED. FABBED AND INSTALLED NEW REPAIR, AND REPAIRED AREA IA W DC-8 SRM 51-1-8, 53-2-0, 51-1-20D AND ABX DWG 5616306. 2 L 7 4 4F 4A25 2002042500150 20020425 00150 WP 2002 4 25 ABXA010841 1 20020406 A 2710 57630901 FITTING DOUG DC8 DC861 3021952 WP LT I/B AILERON BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 LEFT INBOARD AILERON, INBOARD HINGE FITTING WAS BROKEN. INSTALLED NEW FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-21A, 5 1-3-0, 51-1-21, 51-1-24 AND 51-1-20D. 2 L 7 4 4F 4A25 2002042500151 20020425 00151 WP 2002 4 25 ABXA010842 1 20020403 A 5300 FITTING DOUG DC8 DC861 3021952 WP A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 RIGHT LOWER CUSP AT F.S. 6700, LONGERON 20 RIGHT, HAD POPPED RIVET HEADS FROM CORROSION BULGE. CUTOUT DAMAGED AREA AND I NSTALLED NEW DOUBLER AND FILLER, AND REPAIRED AREA IAW DC-8 SRM 51-3-0, 53-2-0, 51-1-20D, 53-3-1 AND 51-1-8. 2 L 7 4 4F 4A25 2002042500152 20020425 00152 WP 2002 4 25 ABXA010843 1 20020421 A 5700 56429401 DOUBLER DOUG DC8 DC861 3021952 WP LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 LEFT WING PANEL LAND 505F, UPPER SURFACE, 3 EACH FASTENER HOLES CRACKED. REPAIRED AREA IAW REA D857-43118MR. 2 L 7 4 4F 4A25 2002042500153 20020425 00153 WP 2002 4 25 ABXA010844 1 20020421 A 5700 56429402 DOUBLER DOUG DC8 DC861 3021952 WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 RIGHT WING 505F PANEL LAND NUT CHANNEL REMOVED, SEALANT REMOVED, AND HOLES POLISHED TO FACILITATE NDT INSPECTION. REPAIR ED AREA IAW DC-8 SRM 51-1-20D AND REA D857-43117MR. 2 L 7 4 4F 4A25 2002042500154 20020425 00154 NM 2002 4 25 ABXA010845 1 20020424 A 5510 FITTING BOEING 767 767200 1385120 NM LT. HORIZ. STAB. CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 LEFT HORIZONTAL, LOWER HORIZONTAL STABILIZER FITTINGS HAD 3 EACH FORWARD FASTENER HOLES CRACKED. REPAIRED AREA IAW B767 SRM 51-40-05 AND REA B766-43116MR. 2 L 7 2 4F RT A1NM 2002042500155 20020425 00155 NM 2002 4 25 ABXA010846 1 20020424 A 5510 FITTING BOEING 767 767200 1385120 NM LT. HORIZ. STAB. CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 LEFT UPPER HORIZONTAL STABILIZER FITTING HAD 2 EACH FORWARD FASTENER HOLES CRACKED. REPAIRED AREA IAW B767 SRM 57-40 AND REA B655-43116MR. 2 L 7 2 4F RT A1NM 2002042500156 20020425 00156 NM 2002 4 25 ABXA010847 1 20020424 A 5510 FITTING BOEING 767 767200 1385120 NM RT. HORIZ. STAB. CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 RIGHT UPPER HORIZONTAL STABILIZER FITTING HAD INBOARD FORWARD FASTENER HOLE CRACKED. REPAIRED AREA IAW B767 REA B655-431 16MR. 2 L 7 2 4F RT A1NM 2002042500157 20020425 00157 NM 2002 4 25 CALA0200236 1 20020423 A 5311 BELTFRAME BOEING 737 7373T0 1384582 NM STA 616 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND A 1/4" CRACK IN L/H BELTFRAME ANGLE AT STA 616 JUST ABOVE CENTER TANK. THE CRACKED AREA WAS TRIMMED OUT . AN ANGLE DOUBLER AND FILLER WERE INSTALLED ON FRAME IAW ECRA 5311-01121. 2 L 7 2 4F RT A16WE 2002042500158 20020425 00158 WP 2002 4 25 CALA0200237 1 20020424 A 5320 CHANNEL DOUG DC9 DC983 3022083 WP MBB DR JAMB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 49525 INSPECTION FOUND MAIN BAGGAGE BIN LOWER DOOR JAMB Z-CHANNEL CORRODED AROUND HI SHEARS. THE CHANNEL WAS REPLACED IAW SRM 53-05, FIGURE 63 AND DRAWING #5930481. 2 L 7 2 4F RT A6WE 2002042500159 20020425 00159 WP 2002 4 25 CALA0200238 1 20020424 A 5330 SKIN DOUG DC9 DC982 3022082 WP STA 232 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND TWO DENTS IN THE FUSELAGE SKIN AT STA 232, LONGERON 17R. THE DENTS WERE REMOVED AND A DOUBLER WAS INSTA LLED IAW SRM 53-04, FIGURE 38, 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 2002042500160 20020425 00160 NM 2002 4 25 CALA0200239 1 20020425 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 767-847 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND CORROSION UNDER FLANGE OF VERTICAL THRESHOLD WEB AT AFT BAGGAGE BIN DOORWAY FROM STA 767-847. THE WEB W AS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2002042500161 20020425 00161 NM 2002 4 25 CALA0200240 1 20020425 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 500C + 5" CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND A 1" CRACK IN STRINGER 16R AND 16L AT STA 500C + 5". THE CRACKED AREA OF EACH STRINGER WAS REMOVED AND REPAIRS WERE INSTALLED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2002042500162 20020425 00162 EA 2002 4 25 COMA0260275 1 20020424 A 5311 600360302331 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FS718.0 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 982CA 11621 7168 THE L/H SIDE 718.0 FRAME AND DOUBLER WERE CRACKED BETWEEN STINGERS 10 AND 11.REPAIRED THE CRACKED FRAME AND REPLACED THE DOUBLER I/A/W REO 601R-53-61-193 REV A AND WVAC EO 601R-53-3158. 2 L 7 2 4F RT A21EA 2002042600159 20020426 00159 NM 2002 4 26 F3LA200200134 1 20020425 A 5320 SILL BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 3415 24569 DURING C-4 CHECK, INSPECTION REPORTED FLOOR ANGLE CORRODED AT L1 ENTRY THRESHOLD, STA 312 TO 344. REMOVED L1 MOP SILL P ER SRM 53-10-15. INSTALLED NEW MOP SILL PER SRM 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A16WE 2002042500163 20020425 00163 EA 2002 4 25 COMA0260276 1 20020423 A 4910 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP FAILED A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 986CA 4855 7174 FLIGHT 5432 SMOKE IN COCKPIT DURING BOARDING, APU AUTO-SHUTDOWN.DETERMINED APU TO BE SOURCE OF SMOKE - SECURED APU AND D EFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2002042500164 20020425 00164 EA 2002 4 25 COMA0260277 1 20020423 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 984CA 7171 FLIGHT 5801 FLAPS FAILED WHEN SELECTED UP AFTER LANDING.RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002042500165 20020425 00165 NM 2002 4 25 AWXA200200362 1 20020424 A 5311 6517684107 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 0 0 22646 YVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND ON FRAME AT BS 303.9, STR 16 L/H. MAINTENANCE REMOVED DAMAGED A REA, FABRICATED A FILLER AND 2 EACH REPAIR DOUBLERS, AND INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-2, FIG. 1, PG. 1. 2 L 7 2 4F RT A16WE 2002042500166 20020425 00166 SO 2002 4 25 C2XA02TY073 1 20020425 A 5320 14521721005 STRAP EMB 145 EMB145 3260210 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS, During a schedule inspection, corrosion was found on the forward digital at frames 15,16 and 17. Maintenance cut ou t the damage, fabricated doublers and shims and installed I.A.W.-EMB-135/145-SRM-53-20-10, 51-21-04, CMP-51-21-04 and 05 . The repair was satisfactory and aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002042600001 20020426 00001 NM 2002 4 26 GAIA02028OP 1 20020321 A 3350 1000679 LIGHT BOEING 727 727251 138408H NM COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 279US 21158 DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. REMOVED AND R EPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY IN THE COCKPIT. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002042600002 20020426 00002 CE 2002 4 26 NSVA0209 1 20020325 A 2120 ODOR BEECH 1900 1900C 1154161 CE CABIN DETECTED A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 27 210CJ UC110 BOS - FAINT SMELL OF OIL COMING FROM ENVIRONMENTAL SYSTEM. MAINTENANCE INSPECTED LT AND RT ENGINE INTAKES FOR OIL RESID UE, OIL FOR PROPER LEVEL AND DUCT OUTLETS FOR RESIDUE, NONE FOUND. SFP ISSUED TO HYA. MAINTENANCE INSPECTED ACM FOR OI L LEAKS, NO DEFECTS NOTED. PERFORMED COMP WASH, RAN ENGINES AT VARIOUS POWER SETTNIGS, COULD NOT DUPLICATE (CND). AIRC RAFT RELEASED FROM MAINTENANCE. (M) 2 L 7 2 4T RT A24CE 2002042600003 20020426 00003 NE 2002 4 26 SIMA200201001 2 20020110 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT MALFUNCTIONED A SIMA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION DE DESCENT 1 SW 21 393AE 340B393 DFW - FLT 3826 - ON DESCENT, LEFT ENGINE TQ WENT TO MAX, GOT OVERTEMP LIGHT. CREW SHUT LEFT ENGINE DOWN. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2002042600004 20020426 00004 EU 2002 4 26 SIMA200204211 1 20020211 A 2911 4018502 ACCUMULATOR SAAB SF340 340B 7860101 EU HYDRAULIC BAY FAILED A SIMA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 234AE 340B234 SPS - FLT 3635 - CREW REPORTED THE MAIN HYDRAULIC ACCUMULATOR PRESSURE WENT TO ZERO IN FLIGHT. LANDING GEAR WAS PUMPED DOWN AFTER GETTING NO RESPONSE FROM HYDRAULIC OVERRIDE. EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY IN SPS. MAINTENANCE REMOVED AND REPLACED THE MAIN HYDRAULIC PUMP IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002042600005 20020426 00005 EU 2002 4 26 SIMA200206203 1 20020303 A 3260 DOWNLOCK SWITCH SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 256AE 340B256 JFK - FLT 4852 - DURING CLIMB THROUGH LIGHT TURBULENCE THE NOSE LANDING GEAR (NLG) GREEN INDICATION CAME ON. AFTER RUNNI NG THE CHECKLIST AND CYCLING THE GEAR THE NLG GREEN LIGHT DID NOT EXTINGUISH. CAPTAIN ELECTED TO DECLARE EMERGENCY AND BLOW THE GEAR DOWN. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE AND CLEANED THE UPLOCK AND DOWNLOCKS I AW SAAB MM OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. SEPARATOR BOLTS FOR THE MAIN GEAR WERE REPL ACED ALSO PRIOR TO RETURN TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002042600006 20020426 00006 EU 2002 4 26 SIMA200207401 1 20020313 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 320AE 340B320 GROUND CREW REPORTED A FEW EMERGENCY LIGHTS WERE INOPERATIVE, ISSUED FERRY PERMIT TO LAX FOR REPAIRS. RAI POWER SUPPLIE S AT 20LN AND 22LN IAW SAAB AMM 33-50, S/N ON 20LN-17323, S/N ON 22LN-1726. (M) 2 L 7 2 4T RT A52EU 2002042600007 20020426 00007 EU 2002 4 26 SIMA200207901 1 20020319 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 358RZ 340B358 DURING A SCHEDULED STRUCTURE INSPECTION, FOUND A CRACK ON FRAME 677. REMOVED CRACK BY CUT OUT. FABRICATED A DOUBLER AN GLE 2.875 INCH BY 10.25 AND A FILLER .75 INCH BY 3.4375 INCH .040 INCH THICK. REPAIR DONE IAW SAAB REPAIR STATEMENT 340 SDS003429 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002042600008 20020426 00008 EU 2002 4 26 SIMA200208101 1 20020322 A 3350 6013211 BATTERY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 280AE 340B280 SAN - FLT 3360 - CREW REPORTED THAT ALL EMERGENCY LIGHTS WOULD NOT TEST. CONTRACT MAINTENANCE INSPECTED AIRCRAFT WHICH WAS THEN FERRIED TO SFP FOR REPAIR. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT POWER SUPPLY UNITS (S/N 17381, 18335, 17649, 19522, 19068) IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002042600009 20020426 00009 NM 2002 4 26 USAA020119 1 20020305 A 5512 SKIN BOEING 737 7373B7 1384580 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 42381 23860 PIT - FOUND SKIN CRACKED 1.75 INCH, RIGHT HORIZ LOWER SKIN AT STATION 125. INSTALLED REPAIR PER TR 55-10-07 REV A, SRM 55-10-01 FIG 204. (M) 2 L 7 2 4F RT A16WE 2002042600010 20020426 00010 NM 2002 4 26 USAA020120 1 20020304 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 42381 23860 PIT - FOUND INTERCOSTAL CRACKED .75 INCH, BS 360-380 LBL 12. INSTALLED CAP PER SRM 53-30-51. (M) 2 L 7 2 4F RT A16WE 2002042600011 20020426 00011 NM 2002 4 26 USAAABB02036 1 20020326 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM ROW 18 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 605AU 22201 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002042600012 20020426 00012 NM 2002 4 26 USAABB02028 1 20020316 A 3350 BATTERY BOEING 757 7572B7 1384964 NM L1 DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 614AU 27145 BDL - FOUND L1 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002042600013 20020426 00013 NM 2002 4 26 USAABB02029 1 20020319 A 3350 20131A BATTERY PACK BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 22199 LAX - FOUND AFT EMERGENCY LIGHT BATTERY PACK INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT A2NM 2002042600014 20020426 00014 NM 2002 4 26 USAABB02030 1 20020320 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AU 27199 BDL - FOUND LOW LEVEL EMERGENCY LIGHTS AT ROWS 22 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002042600015 20020426 00015 NM 2002 4 26 USAABB02031 1 20020320 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM ROW 6 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AU 27199 BDL - FOUND LOW LEVEL EMERGENCY LIGHT AT ROW 6 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002042600016 20020426 00016 NM 2002 4 26 USAABB02032 1 20020320 A 3350 SIGN BOEING 757 7572B7 1384964 NM R1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AU 27199 BDL - FOUND EXIT IDENTIFIER AT R1 DOOR INOPERATIVE. MAINTENANCE REPLACED THE EXIT IDENTIFIER ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002042600017 20020426 00017 NM 2002 4 26 USAABB02035 1 20020322 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 626AU 27303 LAX - FOUND ALL FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE, ROWS 1, 4, 6, 9, 13, 18, 23, 26, 29 AND 33. MAINTENANCE REPLA CED ALL TEN BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002042600018 20020426 00018 NM 2002 4 26 USAABB02037 1 20020326 A 3350 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 605AU 22201 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002042600019 20020426 00019 NM 2002 4 26 USAABB02038 1 20020325 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM ROW 13 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 PIT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002042600020 20020426 00020 NM 2002 4 26 USAASB02050 1 20020313 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 587US 23932 SYR - MAINTENANCE REPORTED THE CABIN CENTER OVERHEAD EMERGENCY LIGHT AND THE LEFT OVERWING EMERGENCY EVACUATION LIGHT IN OPERATIVE. MAINTNANCE REMOVED AND REPLACED THE CABIN CENTER OVERHEAD BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002042600021 20020426 00021 NM 2002 4 26 USAASB02051 1 20020315 A 3350 BATTERY PACK BOEING 737 737401 1384701 NM MID CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 405US 23885 DCA - MAINTENANCE REPORTED THE RIGHT OVERWING EMERGENCY HATCH EXIT SIGN AND RELATED LIGHTS INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE BATTERY SUPPLY FROM BATTERY PACK M1479. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002042600022 20020426 00022 NM 2002 4 26 USAASB02052 1 20020317 A 2120 ODOR BOEING 737 7374B7 1384702 NM CABIN DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 777AU 24979 DCA - FLT 716 - EN ROUTE FROM PIT-DCA, FLIGHT ATTENDANT REPORTED AN ELECTRICAL SMELL IN TH AFT CABIN AREA. FLIGHT LANDE D WITHOUT FURTHER INCIDENT. MAINTENANCE RAN PACKS AND CHECKED AIR CONDITION BAY FOR LEAKS. ALL CHECKS GOOD. NO SMELL DETECTED. PIT - FLT 1524 - ON THE VERY NEXT FLIGHT, EN ROUTE FROM DCA-PIT, AN ELECTRICAL TYPE OF ODOR WAS AGAIN REPORTE D FROM THE AFT CABIN. NO SMOKE WAS PRESENT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RAN ENGINES AND AIR C ONDITION PACKS WITH CABIN LIGHTING TURNED ON. CYCLED LAVATORY PUMPS, COFFEE MAKERS AND GALLEY ELECTRICS. NO ODOR DETEC TED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002042600023 20020426 00023 NM 2002 4 26 USAASB02053 1 20020318 A 3350 BATTERY PACK BOEING 737 7374B7 1384702 NM FWD CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 437US 24559 LGA - MAINTENANCE REPORTED THE FORWARD SERVICE DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK M1160. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002042600024 20020426 00024 NM 2002 4 26 USAASB02054 1 20020318 A 3350 CHARGER BOEING 737 7374B7 1384702 NM AFT CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 437US 24559 LGA - MAINTENANCE REPORTED THE AFT ENTRY DOOR EMERGENCY ESCAPE SLIDE LIGHT AND THE FLOOR PROXIMITY LIGHTS ON SEAT ROWS 2 4 AND 25 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BLOWN FUSE IN THE AFTER LEFT BATTERY CHARGER ASSEMBLY M1197 AN D INSPECTED WIRES AT SEAT ROWS 24 AND 25. NO DEFECTS WTH WIRES NOTED. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. (M) 2 L 7 2 4F RT A16WE 2002042600025 20020426 00025 NM 2002 4 26 USAASB02055 1 20020318 A 3350 1012721 LIGHT BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 376US 22955 IND - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 6ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET ASSEMBLY AT SEAT ROW 6 ABC. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002042600026 20020426 00026 NM 2002 4 26 USAASB02056 1 20020318 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM FWD CABIN CRACKED A USAA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 19 376US 22955 PHL - MAINTENANCE REPORTED AN OVERHEAD EMERGENCY LIGHT BATTERY PACK, FOR LOW LEVEL LIGHTING, WAS LEAKING FROM CEILING IN TO OVERHEAD COMPARTMENT ABOVE SEAT ROW 1C. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002042600027 20020426 00027 NM 2002 4 26 USAASB02057 1 20020319 A 2913 6507506 PUMP BOEING 737 737301 1384611 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 586US 38058 23931 CLT - FLT 9228 - DURING CLIMB-OUT FROM TPA, EN ROUTE TO CLT, CAPTAIN REPORTED THE HYDRAULIC MASTER CAUTION ILGHTS ILLUMI NATING INTERMITTENTLY. CAPTAIN OBSERVED 'A' SYSTEM HYDRAULIC QUANTITY AT REFILL. A SHORT TIEM LATER, 'A' SYSTEM HYDRAU LIC PRESSURE FLUCTUATED FROM 3,211 PSI TO 3,500 PSI. PRESSURE LIGHT FOR 'A' SYSTEM HYDRAULIC ENGINE DRIVEN PUMP THEN IL LUMINATED. HYDRAULIC QUANTITY FOR 'A' SYSTEM HAD DROPPED TO ONE-QUARTER CAPACITY. CAPTAIN REQUESTED EMERGENCY EQUIPMEN T ON STANDBY AS A PRECAUTION. NO EMERGENCY WAS DECLARED. FLIGHT LANDED AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE F OUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING AND THE INPUT SHAFT SHEARED. (M) 2 L 7 2 4F RT A16WE 2002042600028 20020426 00028 NM 2002 4 26 USAASB02058 1 20020321 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM MID CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 506AU 23381 LGA - MAINTENANCE REPORTED THE EMERGENCY PATH LIGHTING INOPERATIVE AT SEAT ROW 12 LEFT AND SEAT ROWS 10, 16, 18 AND 20 R IGHT. ALSO, THE OVERWING EMERGENCY LIGHTS ARE DIM AND EXTINGUISH WITHIN 30 SECONDS OF OPERATION. MAINTENANCE REMOVED A ND REPLACED THE M1136 BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002042600029 20020426 00029 NM 2002 4 26 USAASB02062 1 20020324 A 3350 30043229 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 517AU 23703 IND - MAINTENANCE REPORTED THE EXTERIOR EMERGENCY LIGHT AT THE AFT LEFT SERVICE DOOR INOPERTIVE. MAINTENANCE CLEANED TH E CONTACTS IN THE LIGHT SOCKET. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002042600030 20020426 00030 NM 2002 4 26 USAASB02064 1 20020326 A 2133 OUTFLOW VALVE BOEING 737 7373B7 1384580 NM CABIN PRESSURE FAILED A USAA B A EMER. DESCENT UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 518AU 23695 23704 PIT - FLIGHT 1963 - AFTER DEPARTURE FROM DAY, CLIMBING THROUGH FL190, A LOUD BANG WAS HEARD BY THE FLIGHT CREW. AN AIR N OISE WAS ALSO HEARD IN THE FORWARD CABIN AND THE FLOOR IN THE FIRST CLASS STARTED TO VIBRATE. CREW NOTICED THE CABIN AL TITUDE STARTED TO CLIMB AT 2,000 FEET PER MINUTE BUT THEN STABILIZED AFTER DESCENT TO 10,000 FEET. FLIGHT DIVERTED TO P IT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FORWARD CARGO DOOR ASSEMBLY. ALSO, REMOVED AND REPLACED THE AFT OUTFLOW VALVE FOR FAILING TROUBLESHOOTING RESISTANCE TEST. OPERATION AL TEST OF VALVE GOOD. PRESSURIZED AIRCRAFT SEVERAL TIMES. LEAK CHECK AND PRESSURIZATION CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002042600035 20020426 00035 2002 4 26 SWAA020827 4 20020420 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002042600036 20020426 00036 NM 2002 4 26 SWAA020828 1 20020420 A 3350 101114 LENS BOEING 737 7373Q8 1384670 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED BC3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2002042600037 20020426 00037 2002 4 26 SWAA020829 4 20020422 A 2565 6556685 BRACKET BOEING 737 7373H4 1384600 NM FWD CABIN DOORS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED C1 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKET FASTENERS LOOSE. REMO VED AND REPLACED BRACKET FASTENERS PER SRM. 2 L 7 2 4F RT A16WE 2002042600038 20020426 00038 NM 2002 4 26 SWAA020830 1 20020421 A 2731 BACB28AM07 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 365SW 26576 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ALL ELEVA TOR TAB HINGE BUSHINGS. 2 L 7 2 4F RT A16WE 2002042600039 20020426 00039 NM 2002 4 26 SWAA020831 1 20020421 A 2731 BACB28AM07 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 365SW 26576 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHINGS PER MM 2 L 7 2 4F RT A16WE 2002042600040 20020426 00040 NM 2002 4 26 SWAA020833 1 20020421 A 5753 6546435 FLAP BOEING 737 7373T0 1384582 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED 1/2D CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED JUST OTBD OF NR 7 CANOE FAIRING. REMOVED AND REPLAC ED AFT T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002042600041 20020426 00041 NM 2002 4 26 SWAA020834 1 20020421 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 19R, BS'S 745, AND 727E PLUS 12 AND PLUS 4. REPAIR ED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002042600042 20020426 00042 NM 2002 4 26 SWAA020835 1 20020420 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 508SW 24185 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002042600043 20020426 00043 NM 2002 4 26 SWAA020836 1 20020422 A 2781 6938185 ROD END BOEING 737 7373H4 1384600 NM LT WING BROKEN A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 07 374SW 26582 ABORTED TAKEOFF, DURING TAKEOFF THE L/E FLAP TRANSIT LIGHT AND THE NR 1 KRUGER FLAP TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 KRUGER FLAP TAILGATE ACTUATING ROD END PER MM. 2 L 7 2 4F RT A16WE 2002042600044 20020426 00044 NM 2002 4 26 SWAA020838 1 20020417 A 5230 6969854 DOOR FRAME BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR FRAME CRACKED (2 EA) AT FWD INBD LOWER STOP AREA AND FWD INBD PULLY BRAC KET. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002042600045 20020426 00045 NM 2002 4 26 SWAA020839 1 20020422 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 714CB 27848 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS WITH GAPS AND WIRES EXPOSED. INSTALLED AND REPOSITIONED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002042600046 20020426 00046 2002 4 26 SWAA020840 4 20020422 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002042600047 20020426 00047 NM 2002 4 26 SWAA020843 1 20020422 A 5754 65C26686 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED C2 CHECK, FOUND NR 1 L/E SLAT CRACKED (2 EA), 12 INCHES OTBD OF OTBD ACTUATOR STOP. REPAIRED L/E SLAT PER SRM. 2 L 7 2 4F RT A16WE 2002042600048 20020426 00048 NM 2002 4 26 SWAA020844 1 20020423 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D PLUS 17, WL 204L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002042600049 20020426 00049 NM 2002 4 26 SWAA020846 1 20020419 A 5230 6547952 FRAME BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED SPECIAL VISIT, FOUND AFT CARGO DOOR FRAME CRACKED (2 EA) AT FWD INBD LOWER STOP AREA AND FWD INBD PULLE Y BRACKET. REMOVED AND REPLACED CARGO DOOR PER SWA ACO AND SWA RA. 2 L 7 2 4F RT A16WE 2002042600050 20020426 00050 NM 2002 4 26 SWAA020847 1 20020422 A 2910 6544761 PCU BOEING 737 7373H4 1384600 NM LT MLG W/W LEAKING A SWAA B EMER. DESCENT J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 07 388SW 26591 DECLARED EMERGENCY, DURING FLIGHT A HYD SYSTEM QTY DROPPED TO ONE-QUARTER WITH ASSOCIATED LOW PRESS LIGHT ILLUMINATED. TIGHTENED BOTTOM FLEX LINE ON AILERON PCU PER MM 2 L 7 2 4F RT A16WE 2002042600051 20020426 00051 NM 2002 4 26 SWAA020848 1 20020420 A 5312 6517583 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SPECIAL VISIT, FOUND WEB CRACKED AT BS 182, WL 190 AT RBL 5.7. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002042600052 20020426 00052 NM 2002 4 26 SWAA020853 1 20020424 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, ABOVE STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002042600053 20020426 00053 NM 2002 4 26 SWAA020855 1 20020423 A 5523 65C2638416M TAB BOEING 737 7373H4 1384600 NM RT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399WN 27693 DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 4 HINGE. REMOVED AND REPLACED RT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002042600054 20020426 00054 NM 2002 4 26 SWAA020856 1 20020423 A 5312 6547978 WEB BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED (2 EA) AT BS 636, WL 208, LBL 67 AND RBL 67. REPAIRED WEB PER S RM. 2 L 7 2 4F RT A16WE 2002042600055 20020426 00055 NM 2002 4 26 SWAA020858 1 20020424 A 5330 6545768 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 296, STR 10L. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2002042600056 20020426 00056 NM 2002 4 26 SWAA020859 1 20020423 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM ELEVATORS WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 774SW 27882 DURING SCHEDULED C2 CHECK, SI 11038-55, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 4 HINGE BUSHINGS ON LT AND RT TABS PER MM. 2 L 7 2 4F RT A16WE 2002042600057 20020426 00057 NM 2002 4 26 SWAA020861 1 20020424 A 2731 BACB28AM07 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED A2 CHECK,SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED TAB NR 1 HINGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002042600059 20020426 00059 EA 2002 4 26 CA020328006 1 20020311 A 2750 8551009 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AT 180 KIAS AND HAVING BEEN AT FLAP 8 FOR 2-3 MINUTES. CREW SELECTED FLAP 20 AND IMMEDIATELY "FLAP FAIL" CAUTION M ESSAGE ILLUMINATED. FLIGHT CONTROL PAGE SHOWED LEFT FLAP 8 AND RIGHT FLAP 10. TOUCH DOWN SPEED APPROXIMATELY 175 IAS. LE FT BPSU AND LEFT NR 5 FLEX SHAFT CHANGED. FECU POTS ADJUSTED. SYSTEM TORQUE CHECKED AND RIGGING CARRIED OUT AS PER AIRCR AFT MAINTENANCE MANUAL. SYSTEM CONSIDERED SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002042600061 20020426 00061 EA 2002 4 26 CA020412004 1 20020409 A 3310 SWITCH 2LA00516320 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT LOOSE W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) CAPTAIN'S SIDE POST MAP LIGHT WAS SPARKING WITH AN ASSOCIATED ELECTRICAL FIRE SMELL WHEN LIGHT WAS MANIPULATED. I F LIGHT CASING WAS NOT MOVED, NO NOTED ABNORMALTIES. FOUND SWITCH TO BE LOOSE AND TIGHTENED THE JAM NUT ON THE SWITCH T O RESTORE IT TO NORMAL OPERATION. AIRCRAFT BACK IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002042600062 20020426 00062 EA 2002 4 26 CA020412005 1 20020409 A 4990 38004883 APU HONEYWELL 38004883 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU BAY LEAKING W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA P115C (CAN) ON CLIMB OUT, SMOKE NOTED IN CABIN. APU FAULT AND APU OIL PRESS CAUTION MESSAGES POSTED. AN EMERGENCY WAS DECLAR ED AND THE AIRCRAFT RETURNED TO WHERE AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE FOUND AN APU EXTERNAL OIL LEAK - EXACT LOCATION NOT KNOWN AT THIS STAGE. THE APU WAS REPLACED. AIR CYCLE MACHINE, PRECOOLER, HEAT EXCHANGER, WATER SEPARA TOR AND DUCTS HAE BEEN REMOVED FROM BOTH PACKS, CLEANED AND REFITTED. AIRCRAFT BACK IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002042600063 20020426 00063 EA 2002 4 26 CA020412007 1 20020409 A 5610 NP1393215 WINDSHIELD PPG NP1393215 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 98005H4076 (CAN) CREW REPORTED THE LT WINDSHIELD SHATTERED AT THE GATE. THE LT WINDSHIELD WAS REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002042600064 20020426 00064 EU 2002 4 26 CA020416001 1 20020406 A 3320 BA08006281 BALLAST SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE CABIN FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA (CAN) ON APPROACH FLIGHT ATTENDANT NOTED THAT SMOKE WAS EMITTED FROM THE LIGHTING IN THE AREA OF SEAT 5A. THE COCKPIT CR EW WAS ADVISED AND REPORTED THAT CIRCUIT BREAKER F24 HAD POPPED IN THE COCKPIT. THE SMOKE DISIPATED AT THE LIGHT AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DETERMINED THAT A BALLAST FOR THE LIGHTING AT 5A HAD FAILED RESUL TING IN THE SMOKE AND CAUSING THE CB TO POP. THE BALLAST WAS REPLACED AND THE WIRING INSPECTED. A WIRE WAS REPAIRED AT C ONNECTOR 113VP AND THE LIGHTING TESTED. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002042900073 20020429 00073 NM 2002 4 29 DHL2002726504 1 20020415 A 5312 PRESSURE PANEL BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, RT NLG W/W FWD BULKHEAD LOWER I/B CORNER HAS 4 INCH CRACK. CUT OUT CRACKED WEB & INSTALLED A WEB REPAIR DOUBLER. CUT OUT CRACKED SECTION OF LOWER EXTRUSION ANGLE & INSTALLED AN EXTRUSION ANGLE REPAIR. 2 L 7 3 4F RT A3WE 2002042600066 20020426 00066 NM 2002 4 26 DL764020470 1 20020421 A 1430 114T41457 BOLT BOEING 767 767432ER 1385134 NM L/E SLAT SHEARED A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 830MH 29701 L/E ASSY WHEN FLAPS LOWERED FOR LANDING. FOUND OUTBOARD NR 4 SLAT TARGET DAMAGED. ALSO FOUND SENSOR DAMAGED. REPLACED L/E SENSOR S279, TARGET BOLT AND ROLLER. ALL CHECKS GOOD. 2 L 7 2 4F RT A1NM 2002042600067 20020426 00067 NM 2002 4 26 DL764020474 1 20020422 A 2910 272T3100498 HYDRAULIC LINE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 2 ENGINE BROKEN A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 831MH 29702 706165 ON LAYOVER, NR 2 ENGINE CASE DRAIN HYD FILTER MODULE LINE LEAKING. FOUND LINE BROKEN BEND REF IPC 29-11-75-14 ITEM 357. REPLACED SAME. 2 L 7 2 4F 4 F RT A1NM E23EA 2002042600068 20020426 00068 NM 2002 4 26 DL767020442 1 20020416 A 2930 367027020 MONITOR BOEING 767 767232 1385132 NM HYD SYSTEM FAULTY A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 113DA 22225 AFTER T/O, RIGHT HYD QTY WENT TO ZERO, ATB. FOUND RIGHT HYD QTY IND INOP. NO ASSOCIATED LOW PRESS LIGHTS REPLACED MONI TOR AND TRANSMITTER PER M/M, OP CHECKED NORMAL. REMOVED MCO/PLA. 2 L 7 2 4F RT A1NM 2002042600069 20020426 00069 NM 2002 4 26 DL767020443 1 20020416 A 3350 1000677 LIGHT BOEING 767 767232 1385132 NM COCKPIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 103DA 22215 COCKPIT PORTABLE EMERGENCY LIGHT WILL NOT ILLUM. REPLACED SAME. 2 L 7 2 4F RT A1NM 2002042600070 20020426 00070 NM 2002 4 26 DL76L020397 1 20020330 A 3260 849704 PSEU BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 193DN 28450 CONFIG LIGHT AND WARNING HORN WOULD NOT SILENCE. DIVERTED TO LGW. PSEU FAILED. REPLACED AND CHECKS GOOD. 2 L 7 2 4F RT A1NM 2002042600071 20020426 00071 NM 2002 4 26 DL76S020406 1 20020404 A 5330 148T31113 SKIN BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 124DE 23438 WHILE ACCOMPLISHING THE FS 1809.5 BULKHEAD OUTER CHORD MOD PER BAC S/B 767-53-0078 AND AD 2001-09-13, A CRACK WAS FOUND IN THE SKIN COMMON TO A FASTENER HOLE FOR THE OUTER CHORD ON THE LT SIDE. THE HOLE WAS OVERSIZED IN THE SKIN ASSY ONLY AND A BUSHING INSTALLED. THE WORK WAS ACCOMPLISHED PER ER/A 382872-14, REV A. 2 L 7 2 4F RT A1NM 2002042600072 20020426 00072 WP 2002 4 26 DHL2002802006 1 20020424 A 2612 CONNECTOR DOUG DC8 DC873 302199C WP A DHLA K NONE J L WARNING INDICATION NO TEST IN INSP/MAINT 1 SO 01 802DH 46076 1) #2 ENG SYSTEM "B" FIRE LOOP WILL NOT TEST.2) DEFERRED PER DHL MEL 26-2-3 CONTROL #9112 S.P 26-2 COMPILED WITH. R.L EVY 8616.3) REF W/O # 600005727 T/S #2 ENG B-LOOP FIRE DETREF DMI 9112 #2 ENG FIRE LOOP WONT TEST4) REMOVED AND INSPEC TED ALL FIRE LOOP CONNECTIONS ON NO.2 ENG. REINSTALLED ALL CONNECTORS. FIRE LOOPS TEST GOOD IAW MM 26-10-0. THIS CLOSES W/O 600005727 2 L 7 4 4F RT 4A25 2002042600075 20020426 00075 NM 2002 4 26 DL76S020434 1 20020413 A 2750 FLAP BOEING 767 767332 1382001 NM WING MALFUNCTIONED A DALA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 137DL 25306 ON APPROACH TRAILING EDGE FLAP DISAGREE EICAS WITH T/E FLAP. SHUT DOWN STATUS MSG LANDED WITH FLAPS AT 23 DEG. T/S PER FIM 27-51-00 FIG 114B. SYS TEST NORMAL. MSG CLEARED, NO FAULTS. 2 L 7 2 4F RT A1NM 2002042600076 20020426 00076 NM 2002 4 26 UPS02237936 1 20020319 A 5310 WINDOW POST BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE:C SUSPECT CRACKS ON COCKPIT LT F/N WINDOW POST AT POINT F (2 OFF). F/N WINDOW POST REPAIRED IAW EO B727 -5310-0012 & SMRO EO 2002-009-00 1. 2 L 7 3 4F A3WE 2002042600077 20020426 00077 NM 2002 4 26 UPS02237937 1 20020322 A 5754 SKIN BOEING 727 72731C 1384011 NM L/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE:C NR 4 L/E FLAP ANTI-ICE SKIN ON PANEL O/B OF ACTUATOR ATTACH POINT CRACKED ON LWR O/B RIVET. REPAIR CA RRIED OUT AS REQUIRED IAW UPS EO B727-5750-3082. 2 L 7 3 4F A3WE 2002042600078 20020426 00078 NM 2002 4 26 UPS02237940 1 20020319 A 5260 WEB BOEING 727 72731C 1384011 NM AFT AIRSTAIRS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE:C TORQUE BOX WEB IN AFT AIRSTAIRS AREA HAS A CRACK ON A LIGHTENING HOLE LT SIDE AT BS 1263. CRACK TRIMM ED OUT IAW SRM 51-40-2. REPAIR CARRIED OUT IAW SRM 51-40-2. 2 L 7 3 4F A3WE 2002042600079 20020426 00079 NM 2002 4 26 UPS02237941 1 20020319 A 5260 WEB BOEING 727 72731C 1384011 NM AFT AIRSTAIRS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE:C TORQUE BOX WEB IN AFT AIRSTAIRS AREA HAS A CRACK AT THE LIGHTENING HOLE, RT SIDE AT BS 1283. CRACK TR IMMED OUT IAW SRM 51-40-2 REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2002042600080 20020426 00080 NM 2002 4 26 UPS02237947 1 20020321 A 7120 MOUNT BOEING 727 72731C 1384011 NM NR 1 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE:C NR 1 PYLON FWD CRANE BEAM, CORROSION IN BORE OF BOTH LARGE HOLES AT FWD ENGINE MOUNT ATTACH POINT. RE PAIR OF NR 1 ENG MOUNT FITTING ASSY ACCOMPLISHED IAW EO BB727-5440- 11592-A. 2 L 7 3 4F A3WE 2002042600081 20020426 00081 NM 2002 4 26 UPS02237949 1 20020320 A 5312 PRESSURE PANEL BOEING 727 72731C 1384011 NM FUSELAGE LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE:C AIR LEAK FROM LT PRESSURE WEB IN NWW AT BS 290. REPAIRED IAW SRM 51-40-02 FIG 1. 2 L 7 3 4F A3WE 2002042600082 20020426 00082 NM 2002 4 26 UPS02237952 1 20020321 A 7120 MOUNT BOEING 727 72731C 1384011 NM NR 1 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE:C NR 1 PYLON, FWD CRANE BEAM, CORROSION IN BORE OF BOTH LARGE HOLES AT FWD ENGINE MOUNT ATTACH POINT. R EPAIR OF NR 1 ENG MOUNT FITTING ASSY ACCOMPLISHED IAW UPS EO B727-54 40-11592-A. 2 L 7 3 4F A3WE 2002042600083 20020426 00083 NM 2002 4 26 UPS02238038 1 20020409 A 3211 TRUNNION BOEING 727 72731C 1384011 NM LT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C LT MLG TRUNNION LINK FWD TRUNNION CORRODED. LT MLG TRUNNION LINK REPLACED IAW MM 32-11-01. 2 L 7 3 4F A3WE 2002042600084 20020426 00084 NM 2002 4 26 UPS02238047 1 20020403 A 5754 FLAP BOEING 727 72731C 1384011 NM WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C NR 5 L/E FLAP HAS CRACK AT I/B LOWER BONDING WIRE ATTACH POINT (BULLNOSE). REPAIR CARRIED OUT IAW SMR O EO 2002-015-002 UPS ENGINEERING FILE 727-57-20052. 2 L 7 3 4F A3WE 2002042600085 20020426 00085 NM 2002 4 26 UPS02437839 1 20020225 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 1980-2000 S22L STRINGER FOUND CORROSION. REPAIRED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002042600086 20020426 00086 NM 2002 4 26 UPS02437840 1 20020225 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 2060-2080 S22L STRINGER FOUND CORROSION. REPAIRED AS PER SRM 51-10-02. 2 L 7 4 4F A20WE 2002042600087 20020426 00087 NM 2002 4 26 UPS02437841 1 20020225 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 2160-2180 STR S22L STRINGER FOUND CORROSION. REPAIRED AS PER SRM 51-40-04 FIG 3. 2 L 7 4 4F A20WE 2002042600088 20020426 00088 NM 2002 4 26 UPS02437842 1 20020225 A 5313 654U662449 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C BULK CARGO COMPT - BS 1960 S49R STRINGER FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 8. STRINGER SPLICE REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002042600089 20020426 00089 NM 2002 4 26 UPS02437843 1 20020226 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 980 RBL 65 FLOORBEAM FOUND CRACK. FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 12. 2 L 7 4 4F A20WE 2002042600090 20020426 00090 NM 2002 4 26 UPS02437844 1 20020226 A 5320 65B046561 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - UPPER LOBE CROWN STRINGER SPLICE FITTING CORROSION CRACKING FOUND AT BS 1737 S-2R. REPLACED STR SPLICE BS 1740 S2R AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002042600091 20020426 00091 NM 2002 4 26 UPS02437846 1 20020227 A 5347 BAC152018907178T SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - BS 1980-2020 LBL 11 SEAT TRACK O/B FLANGE FOUND CORROSION. TRACK REPLACED AS PER SRM 53-10-05 F IG 14. 2 L 7 4 4F A20WE 2002042600092 20020426 00092 NM 2002 4 26 UPS02437847 1 20020227 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C AFT CARGO - STRINGER END FOUND CRACKED AT BS 1740 STR 42R. AFT CARGO COMPT BS 1700 STR 43R REPAIRED P ER HX RS 53-61-34732. 2 L 7 4 4F A20WE 2002042600093 20020426 00093 NM 2002 4 26 UPS02437861 1 20020228 A 5320 70757600631N FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C AFT CARGO COMPT - BS 1879-1880 S-48L FLOOR SUPPORT WEB CORRODED. REPLACED FLOOR SUPPORT WEB AS PER SR M 51-10-01. 2 L 7 4 4F A20WE 2002042600094 20020426 00094 NM 2002 4 26 UPS02437862 1 20020228 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C AFT CARGO - BS 1820 LBL 47 FLOORBEAM FOUND CORR CRACK AS MARK. FLOORBEAM REPAIR AT BS 1820 LBL 47 MOS T O/B AS PER SRM 51-40-04. 2 L 7 4 4F A20WE 2002042600095 20020426 00095 NM 2002 4 26 UPS02437863 1 20020228 A 5315 70757600711N FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C AFT CARGO COMPT - BS 1880 S48L FLOORBEAM UPPER CHORD SUPPORT PAD CORRODED. FLOORBEAM UPPER CHORD SUPP ORT PAD REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002042600096 20020426 00096 NM 2002 4 26 UPS02437864 1 20020301 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - AFTER WINDOW FORGING REMOVED FOUND SURROUND FX SKIN CORRODED. REPAIR SKIN AT BS 2120-2140 STR 2 0R - STR 22R AS PER RS R53-61-34742. 2 L 7 4 4F A20WE 2002042600097 20020426 00097 NM 2002 4 26 UPS02437865 1 20020301 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D - AFTER WINDOW FORGING REMOVED FOUND SURROUND FX SKIN CORRODED. REPAIR SKIN AT BS 1960 - 1980 STR 20R - STR 22R AS PER RS R53-61-347 42. 2 L 7 4 4F A20WE 2002043000071 20020430 00071 EU 2002 4 30 00022 1 20020425 A 5230 STRUCTURE AMD FALC20 FALCON 2720302 EU CARGO DOOR DAMAGED E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 158TW 158 CARGO DOOR LIGHT ILLUMINATED, DESCENT TO 10,000 MSL BLEED AIR OFF DOOR LIGHT WENT OUT. RETURNED TO DEPARTURE AIRPORT. AIRCRAFT FERRY FLIGHT TO ADS FOR MAINTENANCE. FOUND AND STRAIGHTENED TWO LOCALIZED IMPACTS ON THE LOWER DOOR EDGE, REPA IRED IN ACCORDANCE WITH SRM 51-10-11, VISUALLY INSPECTED HINGE AND LOCKS, OPS CK GOOD. 2 L 7 2 4F A7EU 2002050900003 20020509 00003 WP 2002 5 9 02FDEA00285 1 20020424 A 1430 BOLT DOUG DC10 DC10* WP FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 RIGHT I/B FLAP O/B HINGE FWD BRACKET O/B H-11 BOLT CORRODED. R&R BOLTS PER EA 8-5750-60625. 2 L 7 3 4F A22WE 2002050200061 20020502 00061 NM 2002 5 2 02FDEA00286 1 20020424 A 2780 69186361 LINK BOEING 727 727233 138408A NM L/E FLAP BINDING A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 269FE 21675 ON TAKEOFF LEAD EDGE W/N RAISE WHEN MOVING FLAP HANDLE FROM 5 DEG TO 2 DEG. REMOVED AND REPLACED LINK ASSY PER MM 27-51 -051-4. OPS CHECK NORMAL. 2 L 7 3 4F RT A3WE 2002042600108 20020426 00108 NM 2002 4 26 AWXA200200363 1 20020424 A 3350 LENS BOEING 737 7373Y0 1384671 NM CABIN LOOSE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 334AW 23747 LAS - EEL - FLIGHT CREW REPORTED THAT THE LT OVERWING EMERGENCY EXIT LIGHT LENS WILL NOT STAY IN PLACE. MAINTENANCE REP LACED THE LT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002042600109 20020426 00109 NM 2002 4 26 CALA0200241 1 20020425 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 867-887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND STRINGER 22L CORRODED AT STA 867-887. A REPAIR STRINGER WAS INSTALLED IAW SRM 53-00-03, PAGE 201 AND 20 4. 2 L 7 2 4F RT A16WE 2002042600110 20020426 00110 NM 2002 4 26 CALA0200242 1 20020425 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 793-847 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND AFT CARGO DOOR CUTOUT THRESHOLD WEB CORRODED AT STA 793-847. THE WEB WAS REMOVED AND REPLACED IAW SRM 5 1-10-2. 2 L 7 2 4F RT A16WE 2002042600111 20020426 00111 WP 2002 4 26 CALA0200243 1 20020426 A 3222 TORQUE LINK DOUG DC9 DC982 3022082 WP NLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 17100 49580 INSPECTION FOUND A 1.5" CRACK IN NLG UPPER TORQUE LINK. THE UPPER TORQUE LINK WAS REMOVED AND REPLACED IAW MM 32-21-04. 2 L 7 2 4F A6WE 2002042600113 20020426 00113 2002 4 26 AWXA200200364 4 20020423 A 3417 501FAD11 ADC BOEING 737 737375 13844BN NM E/E BAY FAILED A AWXA C ABORTED TAKEOFF J S WARNING INDICATION AFFECT SYSTEMS TO TAKEOFF 1 WP 28 336AW 25334 7014 23707 ONT - ABORTED TAKEOFF - FLT 0775 - ON TAKEOFF ROLL AT 95 KTS, FUEL LOAD 98,000 LBS AIRSPEED, ALTIMETER, VSI, AND GPWS FA ILED. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT AND REPLACED THE NR 1 AIR DATA COMPUTER (ADC) IAW BMM 34-12-11. ADC OPERATIONAL TEST AND PITOT STATIC LEAK CHECK WAS GOOD IAW T/C A1B34027. 2 L 7 2 4F RT A16WE 2002042600114 20020426 00114 2002 4 26 SWIA200210742 4 20020320 A 2210 6229968001 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA YAW DAMPER MALFUNCTIONED A SWIA O OTHER E VIBRATION/BUFFET CR CRUISE 1 NM 07 594SW 148 148 7285 AT AIRSPEEDS ABOVE 290 KIAS THERE IS A VIBRATION IN THE RUDDER PEDALS. ALSO NOTICED A VIBRATION 2 MINUTES AFTER SHUTDOW N ON THE GROUND. REPLACED NR 1 YAW DAMPER ACTUATOR IAW MM 22-22-01. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002042600116 20020426 00116 EA 2002 4 26 SWIA200210743 1 20020319 A 2721 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE COCKPIT FAULTY A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 591SW 7079 DURING TAXI IN, RUDDER TRIM WENT FULL NOSE RIGHT. UNABLE TO RETURN TRIM TO TAKEOFF POSITION. INSTALLED SERVICEABLE RUD DER/AILERON TRIM PANEL. RUDDER TRIM CHECKS GOOD IAW 27-22-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2002042600117 20020426 00117 SO 2002 4 26 SWIA200210744 1 20020320 A 2797 WIRE EMB 120 EMB120RT 3260202 SO T/E FLAP CHAFED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 593SW 120191 AFTER ENGINE START, CONTROL FAULT FLAP AND ADV SWS ILLUMINATED AND WOULD NOT RESET. INSPECTED RIGHT INBOARD WIRE BUNDLE FROM P1756 TO P0366 AND FOUND WIRES CHAFING INTO W602-0007-22. REPAIRED WIRE AND RECONNECTED. OPS CHECKED FLAPS 20 TI MES. NO DEFECTS NOTED. OPS CHECK GOOD ON GROUND. 2 L 7 2 4T RT A31SO 2002042600118 20020426 00118 SO 2002 4 26 SWIA200210745 1 20020320 A 6123 RELAY EMB 120 EMB120RT 3260202 SO PWA PW118 PW118B NE AUTO FEATHER FAULTY A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 137H 120137 ON ROTATION AT SJC RECEIVED AN AURAL WARNING TAKEOFF AUTO FEATHER. ABORTED TAKEOFF. FOUND K0161 RELAY TO BE SLOW. INS TALLED NEW RELAY AND OPERATED SYSTEM. OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2002042600119 20020426 00119 2002 4 26 SWIA200210746 4 20020323 A 3444 9650686001 COMPUTER EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 223SW 5129 5129 120291 AFTER TAKEOFF RECEIVED CONTROL SINK, TERRAIN AND CONTINUOUS PULL UP WARNINGS UNTIL 50 FT AGL. RETURNED TO FAT. REPLAC ED GPWS COMPUTER. OPS CHECK GOOD IAW MM 34-44-00. 2 L 7 2 4T RT A31SO 2002042600121 20020426 00121 SO 2002 4 26 SWIA200210747 1 20020323 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE E/E BAY DOOR OUT OF ADJUST A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 189SW 120048 SERVICE DOOR LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. ADJUSTED AVIONICS BAY DOOR MICROSWITCH. OPS CHECK G OOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002042600122 20020426 00122 EA 2002 4 26 SWIA200210748 1 20020321 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILER MALFUNCTIONED A SWIA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 NM 07 426SW 181 181 7468 RECEIVED SPOILERON FAULT STATUS MESSAGE. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT INBOARD SPOILERON PCU WITH SERVICE ABLE UNIT IAW MM 27-62-01. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002042600125 20020426 00125 NE 2002 4 26 SWIA200210750 2 20020317 A 7261 SEAL EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE DEFECTIVE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 199SW 120237 ON TAKEOFF RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING. OIL PRESSURE RETURNED BACK IN THE GREEN ARC AND FLUCTUATED BET WEEN 60 & 50 PSID. OIL PRESSURE DROPPED BACK OFF AGAIN WITH ASSOCIATED WARNINGS. OIL PRESSURE STABILIZED AT 63 PSID ON DOWNWIND RETURNING TO RENO. COMPLIED WITH INSPECTION OF CHIP DETECTOR AND INSPECTION OF OIL FILTERS. FOUND BAD SEAL O N OIL PUMP PICK UP TUBE. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY. OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002042600126 20020426 00126 SO 2002 4 26 C2XA02CL105 1 20020424 A 2530 CBC16707 RECEPTACLE EMB 135 EMB135ER 3260203 SO GALLEY BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 16502 145166 CLE FLIGHT 3180 THE CREW REPORTED ELECTRICAL SMELL COMING FROM THE COFFEE WARMERS. MAINTENANCE INSPECTED AND REPLACED B OTH LEFT AND RIGHT COFFEE WARMER RECEPTACLES. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002042600127 20020426 00127 SO 2002 4 26 CHQ000148 1 20020424 A 2611 SMOKE DETECTOR EMB 145 EMB145 3260210 SO LAVATORY ACTIVATED A CHQA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 289 P3370233 LAV SMOKE WARNING. 2 L 7 2 4F RT T00011AT 2002042600129 20020426 00129 NM 2002 4 26 DHL2002726500 1 20020414 A 7120 65234651 ATTACH FITTING BOEING 727 727228 1384083 NM NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, NR 2 ENGINE LT UPPER ENGINE MOUNT FITTING ATTACH ANGLE FITTING INSIDE (PANEL 5201) HAS A 3 INCH LONG CRA CK. REMOVED AND REPLACED ATTACH FITTING IAW B-727 SRM 51-30-2. REMOVED AND REPLACED LT UPPER SUPPORT CHORD. REMOVED N R 2 ENGINE LT UPPER ENGINE SUPPORT STRUCTURE AND CRACKED ATTACHED ANGLE FITTING IAW B-727 SRM 51-30-2. INSTALLED NEW CH ORD ANGLE (P/N 65-23465-3) AND NR 2 ENGINE SUPPORT STRUCTURE LT UPPER SIDE IAW B-727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002042600130 20020426 00130 NM 2002 4 26 DHL2002726501 1 20020416 A 5210 SKIN BOEING 727 727228 1384083 NM C1 DOOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, DENT ON C-1 DOOR SKIN AT BS 590, STR 20 R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER IAW B-727 SRM 51- 30-2. 2 L 7 3 4F RT A3WE 2002042600131 20020426 00131 NM 2002 4 26 DHL2002726502 1 20020418 A 7110 PLATE BOEING 727 727228 1384083 NM NR 1 COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, NR 1 ENGINE LOWER COWL NR 5 O/B U-BOLT COVER PLATE IS CRACKED. REMOVED COVER PLATE. FABRICATED AND INS TALLED NEW PLATE IAW B-727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002042600132 20020426 00132 NM 2002 4 26 DHL2002726503 1 20020418 A 7110 SKIN BOEING 727 727228 1384083 NM NR 1 COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, NR 1 ENGINE UPPER COWL SKIN IS CRACKED AT NR 3 LATCH. FABRICATED AND INSTALLED DOUBLER IAW B-727 SRM 51 -30-2. 2 L 7 3 4F RT A3WE 2002042600133 20020426 00133 NM 2002 4 26 DHL2002727005 1 20020424 A 2612 POWER UNIT BOEING 727 727228 1384083 NM FIRE WARNING MALFUNCTIONED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 727DH 20204 APU FIRE WARNING DOES NOT TEST. RERACKED APU FIRE DETECTION OPERATING POWER UNIT, OP'S CHECKED GOOD IAW B-MM 26-15-0. 2 L 7 3 4F RT A3WE 2002042600134 20020426 00134 NM 2002 4 26 DL76S020409 1 20020405 A 1430 BOLT BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE FUEL PUMP LOOSE A DALA O OTHER K F FLUID LOSS FLT CONT AFFECTED CR CRUISE 1 SO 27 139DL 32767 25984 580384 PILOT REPORT, SUSPECTED FUEL LEAK RIGHT ENGINE FUEL FLOW NORMAL IN FLIGHT -5700PPH, NO VISUAL LEAKAGE NOTED REQ'D REBALA NCING 3 TIME IN FLIGHT. FOUND BOLTS LOOSE ON FUEL PUMP TO MEC TUBE AT MEC. REPLACED GASKETS AND RETORQUED BOLTS (P/N 7 31203193) GASKET TUBE (P/N 9378M10G07). 2 L 7 2 4F 4 F RT A1NM E13NE 2002042600135 20020426 00135 NM 2002 4 26 DL76S020446 1 20020417 A 2421 IDG BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 ENGINE LACK OF LUBE A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 127DL 40692 24077 580356 LT GEN DRIVE EICAS MESSAGE ILLUMINATED WHEN TAKEOFF POWER APPLIED. LIGHT WENT OUT WHEN THROTTLES RETURNED TO IDLE. TAK EOFF ABORTED BELOW 80 KTS. SERVICED IDG, RAN NR 1 ENG, PUT GEN ONLINE, LOADED GEN TO .67 PERCENT VOLTS AND FREQS CHECK NORMAL. OIL TEMP NORMAL. OPN NORMAL, LEAK CHECK OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2002042600136 20020426 00136 NM 2002 4 26 DLM11020405 1 20020405 A 2530 72077500 OVEN DOUG MD11 MD11 3023602 NM GALLEY FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 801DE 48472 WATER LEAKING OVER FWD GALLEY. F/O`S SIDE STRONG SMELL OF HOT INSULATION OR ELECTRICAL WIRES. INSPECTED AND FOUND 1 OV EN BAD. REPLACED SAME. 2 L 7 3 4F RT A22WE 2002042600137 20020426 00137 NM 2002 4 26 DLM11020418 1 20020408 A 3310 LIGHT DOUG MD11 MD11 3023602 NM REST MODULE DEFECTIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 804DE 48475 CREW REST MODULE READING LIGHT IN BOTTOM BUNK BEGAN TO SMOKE AND WAS TURNED OFF. REPLACED READING LIGHT BULB. 2 L 7 3 4F RT A22WE 2002042600138 20020426 00138 NM 2002 4 26 DLM11020428 1 20020412 A 5330 NGA6313515 SKIN DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 812DE 48601 CORROSION ON FUSELAGE SKIN AT LAVATORY VACUUM WASTE AIR EXHAUST, FS 1937 & 1959, FOUND DURING HMV. CORROSION BLENDED. INSTALLED DOUBLERS PER ER/A 412865-14, REV NEW. 2 L 7 3 4F RT A22WE 2002042600139 20020426 00139 NM 2002 4 26 DLM11020450 1 20020416 A 5713 ARB75342 STRINGER DOUG MD11 MD11 3023602 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 812DE 48601 A CRACK WAS FOUND IN AT WS 826.5 STR 34 IN THE LOWER SKIN STRINGER. THE CRACK WAS APPROX 6 INCHES IN LENGTH RUNNING IN THE RADIUS OF THE STRINGER. REPAIRED ER/A 412871-14. 2 L 7 3 4F RT A22WE 2002042600141 20020426 00141 NM 2002 4 26 DLM88020403 1 20020404 A 2913 623337 PUMP DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAULTY A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 977DL 53258 718150 IN FLIGHT RIGHT HYD PRESS LOW LIGHT ILLUM AND RT PRESS INDICATED ZERO. QUANTITY INDICATED 19 QTS. FOLLOWED POM PROCEDU RES AND RESTORED HYD PRESS. NORMAL INDICATIONS FOR THE REST OF FLIGHT. REPLACED RT ENGINE HYD PUMP PER M/M. LEAK CHEC K AND TEST NORMAL. 2 L 7 2 4F 4 F RT A6WE E9NE 2002042600143 20020426 00143 NE 2002 4 26 DLM88020413 2 20020406 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 MAKING METAL A DALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 924DL 31666 49711 718180 RT ENG OIL STRAINER CLOG LIGHT ILLUMINATED SHORTLY AFTER T/O. IAW POM PROCEDURES RETARDED THE THROTTLE. THE STRAINER M ESSAGE STAYED ON SO THE ENGINE WAS SHUTDOWN. RETURNED TO DFW. FOUND METAL IN OIL FILTER AND ON MCD. REPLACED FILTER A ND CLEANED MCD. RAN ENG AND REINSPECTED MCD AND FILTER PER M/M 72-00-02-1 FIGURE 113A. FOUND METAL ON MCD. CHANGED EN GINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2002042600144 20020426 00144 NM 2002 4 26 DLM88020416 1 20020405 A 5330 5920323249 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 DURING HMV-2 DENTS WERE FOUND IN THE FUSELAGE SKIN FROM FS 275 TO 330 AT APPROX L20R. REPAIRED PER ERA 413006-14. 2 L 7 2 4F RT A6WE 2002042600145 20020426 00145 NM 2002 4 26 DLM88020419 1 20020408 A 2170 17101912 CHECK VALVE DOUG MD88 MD88 3023688 NM A/C BAY STICKING A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 951DL 49882 AFTER T/O FROM CVG, PASSING THROUGH APPROX 11K AFT FLT ATT REPORTED ABNORMALLY HIGH PITCHED NOISE COMING FROM TAIL CONE AREA AND REPORTED FLUID LEAKING FROM O/H TAIL CONE. RETURNED TO CVG. CYCLED BOTH PACKS WITH NO EFFECT ON NOISE, NOISE STOPPED DESCENDING THROUGH 7K. REPLACED LT & RT WATER SEPARATOR BAGS, FOUND BOTH DRAIN SCREENS ON WATER BAG HOUSING CLO GGED. CLEANED SAME, FOUND RT WATER BAG HOUSING CHECK VALVE STICKING. REPLACED SAME, SYS CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2002042600146 20020426 00146 NM 2002 4 26 DLM88020435 1 20020411 A 3222 5920602513 CYLINDER DOUG MD88 MD88 3023688 NM NLG FAULTY A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 977DL 53258 NOSE GEAR WOULD NOT RETRACT ON T/O NOR DURING CHECKLIST. REPLACED NOSE GEAR PISTON AND INNER CYLINDER. 2 L 7 2 4F RT A6WE 2002042600147 20020426 00147 NM 2002 4 26 DLM88020445 1 20020417 A 3233 59370365507 ACTUATOR DOUG MD88 MD88 3023688 NM LT MLG LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 905DL 49536 AFTER GEAR RETRACTION ON T/O LEFT MAIN GEAR RED LIGHT REMAINED ON. POM ABNORMAL PROCEDURES FOLLOWED UNTIL GEAR DOWN WIT H 3 GREEN LIGHTS. GEAR WAS LEFT DOWN AND RETURNED TO ATL. FOUND LT GEAR RETRACT ACTUATOR LEAKING. REMOVED AND REPLACE D SAME. OP CHECKS GOOD. 2 L 7 2 4F RT A6WE 2002042600148 20020426 00148 NE 2002 4 26 DLM88020447 2 20020416 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 DAMAGED A DALA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SO 27 910DL 29748 49541 725835 ACFT RTO DUE NR 2 ENGINE OVERTEMP. ACFT RETURNED TO GATE. SUBSEQUENT BORESCOPE CONFIRMED 7 STAGE FAILURE. REPLACED EN GINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2002042600150 20020426 00150 NM 2002 4 26 DLM88020449 1 20020418 A 2170 COALESCER BAG DOUG MD88 MD88 3023688 NM A/C BAY CONTAMINATED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 917DE 49958 AFT RT SMOKE DETECTOR SOUNDED ON TAXI OUT. FUMES/HAZE REPORTED NEAR WING AREA. APU, LEFT ENGINE, AND BOTH PACKS WERE O PERATING. RETURNED TO GATE. ODOR PRESENT WITH LEFT PACK ONLY. INPS APU INLET, CKS OK. INSPECTED LT PACK, OIL CLEAN A ND ROTATES FREELY. INSPECTED DUCTS, NO CONTAMINATION FOUND. REPLACED SOILED WATER SEPARATOR BAG LEFT SIDE, RAN A/ PACK PER OPN 5088 WITH APU AND E. 2 L 7 2 4F RT A6WE 2002042600151 20020426 00151 EA 2002 4 26 COMA0260278 1 20020425 A 5311 601360012330 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS640.0 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 915CA 20229 7013 FOUND CRACKED FRAME AND FRAME DOUBLER AT R/H SIDE FS 640.0 AT STRINGER 12, WL 120.REPAIRED CRACKED FRAME AND REPLACED CR ACKED DOUBLER I/A/W REO 601R-53-61-487. 2 L 7 2 4F RT A21EA 2002042600152 20020426 00152 EA 2002 4 26 COMA0260279 1 20020425 A 5330 60135004419 SKIN CNDAIR CL600 CL6002B19 1900309 EA FS640.0 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 915CA 20229 7013 FOUND CRACKED FUSELAGE SKIN DOUBLER AT R/H SIDE FS640.0 T STRINGER 12, WL 120.CUT AWAY CRACKED PORTION OF DOUBLER AND FA BRICATED AND INSTALLED REPAIR PARTS I/A/W REO 601R-53-61-500. 2 L 7 2 4F RT A21EA 2002050200062 20020502 00062 2002 5 2 02FDEA00289 4 20020425 A 3416 ALTIMETER BOEING 727 72722 1384002 NM COCKPIT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 151FE 19147 CAPT'S ALTIMETER GOT OFF FLAG ON CLIMBOUT, ALSO GOT OFF FLAG IN ALTITUDE ALERT BOX, WHEN OFF FLAG SHOWING, ALTIMETER DID N'T MOVE. REMOVED AND REPLACED CAPT'S ALTIMETER PER MM 34-12-011-5. 2 L 7 3 4F A3WE 2002042600153 20020426 00153 NM 2002 4 26 DLM88020455 1 20020417 A 3260 833703 PROXIMITY SWITCH DOUG MD88 MD88 3023688 NM NLG OUT OF ADJUST A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 926DL 49713 AFTER T/O AND GEAR RETRACTION, NOSE GEAR UNSAFE INDICATION. EXTENDED GEAR ALL GREEN. RETRACTED GEAR, NOSE GEAR DIDN'T RETRACT FOR SEVERAL MINUTES. EXTENDED GEAR AGAIN AND ALL GREEN. ADJ D1-31 NOSE GEAR UP POSITION PROX SW PER M/M. SWUN G NOSE GEAR SEVERAL TIMES, OPERATION AND INDICATION NORMAL. 2 L 7 2 4F RT A6WE 2002042600155 20020426 00155 NM 2002 4 26 DLM90020412 1 20020405 A 3350 LIGHT DOUG MD90 MD9030 3023690 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 ONE CLEAR EMERGENCY FLOOR TRACK LIGHT WAS MISSING. REPLACED COVER, OPS NORMAL. 2 L 7 2 4F RT A6WE 2002042600157 20020426 00157 NM 2002 4 26 0201356311 1 20020418 A 2610 COFFEEMAKER BOEING 747 747451 1384940 NM NBR 1 GALLEY BURNED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 671US 26477 (BOM) DURING FLIGHT, AN ELECTRICAL BURNING SMELL EMITTED FROM THE FIRST CLASS GALLEY. TURNED OFF OVEN AND COFFEEMAKERS A ND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE COFFEEMAKERS AND THERMOSTATS IN THE NBR 1 AND NBR 2 POSITIONS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002042600158 20020426 00158 NM 2002 4 26 UPS02438088 1 20020422 A 5410 65B931298 WEB BOEING 747 747200 1384847 NM #3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C #3 PYLON REAR ENGINE MOUNT B/H FOUND CRACKED AT AFT WEB FROM EDGE TO 3RD FASTENER HOLE. REFER ATTACH S KETCH FOR DETAILS. B/HEAD WEB CRACKED AREA REPAIRED AS PER RS 54-53-34781 AND UPS EO B747-5410-16695-A. 2 L 7 4 4F RT A20WE 2002042600160 20020426 00160 EA 2002 4 26 COMA0260280 1 20020424 A 2760 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 818CA 7408 FLIGHT 5898 TAKE-OFF CONFIG SPOILER MESSAGE DURING T/O.COULD NOT DUPLICATE RESET SECU, SYSTEM OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A21EA 2002042600161 20020426 00161 EA 2002 4 26 COMA0260281 1 20020425 A 3230 HYDRAULIC SYSTEM CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 982CA 7168 FLIGHT 5620 GEAR DISAGREE WARNING WHEN SELECTED UP.SERVICED AND BLED AIR FROM #3 HYDRAULIC SYSTEM, RETRACT CHECKS WERE N ORMAL. 2 L 7 2 4F RT A21EA 2002042600162 20020426 00162 EA 2002 4 26 COMA0260282 1 20020423 A 7930 WIRE CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 712CA 7244 FLIGHT 5966 LEFT ENGINE OIL PRESSURE WARNING.REPAIRED CHAFED WIRE AT OIL PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 2002042600163 20020426 00163 EU 2002 4 26 AWXA200200367 1 20020417 A 5347 D53112782200 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 605AW 543 YWG - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND FROM FR 16 TO FR 20, Y-1292 RT ON FLOOR SUPPORT SEAT TRACK. M AINTENANCE REMOVED CORRODED FLOOR SUPPORT SEAT TRACK FROM FR 16 TO FR 24, FABRICATED A NEW FLOOR SUPPORT SEAT TRACK PER DWG D53112782, AND INSTALLED REPAIR IAW A320 SRM 51-42-11, PG.1, PARA. 1 - 2A, 2 L 7 2 4F RT A28NM 2002042600164 20020426 00164 NM 2002 4 26 AWXA200200369 1 20020426 A 5311 140N20044 FRAME BOEING 757 7572G7 1384963 NM CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 0 0 24233 GYR - MAJOR REPAIR - DURING C-11 CHECK A CHAFED FRAME WAS FOUND AT BS 1280 BETWEEN STR 11-14 L/H. MAINTENANCE REMOVED DA MAGED SECTION OF FRAME, FABRICATED NEW FRAME SPLICE ANGLES, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-07, FIG. 201, SHEET 1-3. 2 L 7 2 4F RT A2NM 2002042600165 20020426 00165 NM 2002 4 26 AWXA200200371 1 20020404 A 5531 174N12014 RIB BOEING 757 7572G7 1384963 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 0 0 24233 GYR - MAJOR REPAIR - DURING C-11 CHECK A CRACK WAS FOUND ON THE VERTICAL STAB TOP LEADING EDGE SUPPORT WEB (RIB), L/H AN D R/H SIDES AT FSS 417.169. MAINTENANCE REMOVED DAMAGED RIB, FABRICATED AND INSTALLED A NEW RIB IAW B757-200 SRM 51-40-0 1, PG. 1. 2 L 7 2 4F RT A2NM 2002042600166 20020426 00166 EA 2002 4 26 SWIA200210800 1 20020422 A 5242 ACCESS DOOR CNDAIR CL600 CL6002B19 1900309 EA EXT POWER OPEN A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 418SW 7446 RETURNED TO AIRPORT AFTER TAKEOFF DUE TO EXT POWER ACCESS PANEL LEFT OPEN BY COS RAMPERS. INSPECTED EXT POWER ACCESS DO OR. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2002042900001 20020429 00001 SO 2002 4 29 C2XA02IA096 1 20020428 A 3350 7281000501 MODULE EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15973 145159 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS FAILED TO ARM. IAH- MAINTENANCE REMOVED AND REPLACED T HE CABIN CONTROL MODULE FOR LIGHTS, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AN D, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002042900002 20020429 00002 NM 2002 4 29 SWAA020865 1 20020425 A 5311 6546529 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 334, STR 22L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002042900003 20020429 00003 NM 2002 4 29 SWAA020866 1 20020425 A 5312 6547978 WEB BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 777, LBL 67 AT WL 208. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002042900004 20020429 00004 NM 2002 4 29 SWAA020867 1 20020424 A 2731 BACB28AM07 BUSHING BOEING 737 737317 138447P NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED C4 CHECK, FOUND LT ELEVATOR TAB HAS EXCESSIVE AXIAL PLAY. REMOVED AND REPLACED TAB HINGE BUSHING PER M M. 2 L 7 2 4F RT A16WE 2002042900005 20020429 00005 NM 2002 4 29 SWAA020868 1 20020425 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727A, ABOVE STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002042900006 20020429 00006 NM 2002 4 29 SWAA020869 1 20020424 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, BELOW STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002042900007 20020429 00007 NM 2002 4 29 DLM90020414 1 20020406 A 2913 623337 PUMP DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 901DA 53381 020074 AT CRUISE EOAP-LT HYD PRESS LO-ILLUMINATED. L/R HTD QTY OK. COULD NOT RESTORE L HYD PRESS PER POM. FOUND METAL CHUNKS IN LT ENG HYD PUMP. REMOVED AND REPLACED LT ENG HYD PUMP PER MM. REPLACED LT EDP CASE DRAIN / PRESS FILTERS. REPLACE D L SYS RETURN FILTERS. FLUSHED SYS. RAN LT ENG / EDP. CHECKED EDP CASE DRAIN/ PRESS FILTERS. NO METAL FOUND. REPLA CED EDP CASE DRAIN. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A6WE E40NE 2002042900010 20020429 00010 NM 2002 4 29 F3LA200200135 1 20020425 A 5320 SILL BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 3461 25263 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON L-2 THRESHOLD MOP SILL BETWEEN STA 951 AND 986.5. PERFORMED A TYPICA L FORM SECTION REPAIR PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2002042900011 20020429 00011 EU 2002 4 29 MALA020260 1 20020422 A 2560 P10021 BATTERY BAC 146 AVRO146RJ85A 1500097 EU FLASHLIGHT INOPERATIVE A MALA K NONE L NO TEST NR NOT REPORTED 1 GL 15 507XJ E2316 ON FLIGHT 3592 THE F/A'S AFT EMERGENCY FLASHLIGHT BATTERY DEAD. MAINTENANCE REPLACED BATTERY IN AFT F/A EMERGENCY LIGHT . OPS CHECK GOOD, REINSTALLED STRAP. 2 H 7 4 4F RT A49EU 2002042900012 20020429 00012 WP 2002 4 29 MWEA020263 1 20020315 A 5330 5911400515 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 AIRCRAFT NOSE SKIN CREASED ON RIGHT SIDE AT STATION 87, 10 INCHES BELOW CUSP, AFT OF AOA VANE. FABRICATED AND INSTALLED FLUSH SKIN PANEL REPAIR. 2 L 7 2 4F A6WE 2002042900013 20020429 00013 WP 2002 4 29 MWEA020264 1 20020315 A 5320 99100736 ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 RIGHT NOS SUPPORT ANGLE HAS A DENT AT STATION 87, 10 INCHES BELOW CUSP AFT OF AOA VANE. REMOVED AND REPLACED SUPPORT AN GLE. 2 L 7 2 4F A6WE 2002042900014 20020429 00014 WP 2002 4 29 MWEA020265 1 20020420 A 2720 59140665561 POWERPACK DOUG DC9 DC982 3022082 WP RUDDER FAULTY A MWEA K NONE F FLT CONT AFFECTED CR CRUISE 1 GL 31 809ME 48071 PRIOR TO DESCENT FROM FL370, THE RUDDER PEDAL AUTHORITY DEGRADED TO THE POINT OF REQUIRING SIGNIFICANT RUDDER PEDAL DISP LACEMENT TO YAW THE AIRCRAFT. THE RUDDER TRIM WOULD MOVE, BUT REQUIRED EXCESSIVE FORCE. THE CONDITIONS CONTINUED UNTIL PASSING 15,000 FT IN THE DESCENT. BOTH RUDDER AND TRIM RETURNED TO NORMAL AND RUDDER LIMITER OPERATES NORMAL. REMOVED AND REPLACED RUDDER POWER PACK IAW MD80 AMM 27-20-8-4. PERFORMED ADJ/TEST OF 27-20-8-4 STEPS 4A1-19, COMPLETED ADJ/TES T OF 27-20-8-4 STEPS 20 & 21. OPERATION OK AT THIS TIME. 2 L 7 2 4F A6WE 2002042900015 20020429 00015 WP 2002 4 29 MWEA020266 1 20020422 A 2530 ODOR DOUG DC9 DC932 3022066 WP GALLEY DETECTED A MWEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 31 216ME 47740 CREW REPORTED STRONG CHEMICAL SMELL IN FORWARD GALLEY AREA OF AIRCRAFT. CLEANED CARPETING, REMOVED AND REPLACED WATER S OCKS, VERIFIED APU SERVICING. OPERATED BOTH ENGINES AND APU. PRESSURIZED AIR CONDITIONING SYSTEM AND PRESSURIZATION SY STEM. NO SMELLS NOTED. 2 L 7 2 4F A6WE 2002042900016 20020429 00016 WP 2002 4 29 MWEA020268 1 20020423 A 5753 9935962502 SKIN DOUG DC9 DC982 3022082 WP T/E FLAP DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 RIGHT INBOARD FLAP LOWER SKIN PITTED IN SEVERAL AREAS AT STATION XW 50. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002042900017 20020429 00017 WP 2002 4 29 MWEA020269 1 20020423 A 5320 ME2513513 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 GALLEY STRUCTURE MOUNT BEAM HAS CORROSION AT STATION 1185 BEAM IS LOCATED BETWEEN FLOORBEAMS STATION 1174 AND 1193. FAB RICATED AND INSTALLED BEAM SECTION. 2 L 7 2 4F A6WE 2002042900018 20020429 00018 WP 2002 4 29 MWEA020272 1 20020423 A 5210 99557523 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 PASSENGER DOOR HAS LIGHT CORROSION ON AFT END OF BEAM NR 1. FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2002042900019 20020429 00019 WP 2002 4 29 MWEA020273 1 20020423 A 5321 99365841 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FLOORBOARD BETWEEN SEAT TRACKS NR 3 AND 4 HAS SEVERAL GOUGES BETWEEN STATION 1145 TO 1260. FABRICATED AND INSTALLED FLO ORBOARD. 2 L 7 2 4F A6WE 2002042900020 20020429 00020 WP 2002 4 29 MWEA020274 1 20020423 A 5321 99365831 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FLOORBOARD D4 IS DENTED ABOUT 8 INCHES FORWARD OF THE AFT END. FABRICATED AND INSTALLED FLOORBOARD. 2 L 7 2 4F A6WE 2002042900021 20020429 00021 NE 2002 4 29 P2EA2002M027 2 20020422 A 7230 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE DAMAGED A P2EA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 05 141NJ 49932 725675 DURING CLIMBOUT AROUND 9,000 FEET AT NORMAL EPR CLIMB LIMIT. THE LEFT ENGINE DEVELOPED STRONG SURGES. RETURN TO LAX WI TH ENGINE AT IDLE. PERFORMED BORESCOPE OF THE NR 1 (LEFT) ENGINE. FOUND NUMEROUS 13TH STAGE BLADES DAMAGED BEYOND LIMI TS. PER MM 72-00-00. R&R NR 1 ENGINE. 2 L 7 2 4F 4 F A6WE E9NE 2002042900022 20020429 00022 NM 2002 4 29 SABA020054 1 20020427 A 3350 1306 BULB DHAV DHC8 DHC8103 1386005 NM CABIN BURNED OUT A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 882CC 168 Aircraft 882 on flight 5204 from CLT to PGV. During preflight inspection the floor emergency evacuation light at row 3 woas found inoperative. Maintenance removed and replaced the bulb. Ops check was good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002042900023 20020429 00023 NM 2002 4 29 PCAA0204049 1 20020422 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN OUT OF POSITION A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 811AW 201 DURING ROUTINE MAINTENANCE VISIT FORWARD EMERGENCY FLOOR LIGHTING FOUND INOPERATIVE. WIRE FOUND PULLED OUT OF SOCKET. SOCKET ASSEMBLY REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042900024 20020429 00024 NM 2002 4 29 PCAA0204050 1 20020420 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DISCONNECTED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 809EX 302 DURING ROUTINE MAINTENANCE VISIT CENTER AISLE EMERGENCY LIGHT ON CEILING FOUND INOPERATIVE. CANNON PLUG FOUND TO BE DIS CONNECTED IN CEILING. CANNON PLUG RESECURED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042900025 20020429 00025 NM 2002 4 29 QXEA0200581 1 20020324 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM VHF ANTENNA UNSERVICEABLE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - NR 1 VHF UPPER ANTENNA, TWO FORWARD NUT PLATES HAVE SPINNING NUTS. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002042900026 20020429 00026 NM 2002 4 29 QXEA0200582 1 20020323 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - GOUGE IN CARGO DOOR SKIN 15 INCHES FROM FORWARD END AND 5.75 INCHES FROM TOP OF DOOR. REPAIRED IAW DHC-8 SRM 51-2 0-11, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002042900027 20020429 00027 NM 2002 4 29 QXEA0200583 1 20020323 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - ANGLE CORRODED AT NUT PLATE UNDERSIDE X600 Y6L Z100. REPAIRED IAW DHC-8 SRM 51-20-11, SRM 51-20-16 AND SRM 51-20- 36. 2 H 7 2 4T RT A13NM 2002042900028 20020429 00028 NM 2002 4 29 QXEA0200584 1 20020323 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - UNDERSIDE STRUCTURE HAS LIGHT CORROSION AT FOUR NUT PLACES, X582 Y11L, X584 Y11L, X582 Y13L AND X582 Y15L. REPAIR ED IAW DHC-8 SRM 51-20-11, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002042900029 20020429 00029 NM 2002 4 29 QXEA0200585 1 20020323 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- UNDERSIDE STRUCTURE CORRODED AT NUT PLATE X592, Z100 & Y10L. REPAIRED IAW DHC-8 SRM 51-00-06, 51-00-04, 51-20-11, 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2002042900030 20020429 00030 NM 2002 4 29 QXEA0200586 1 20020323 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- UNDERSIDE OF ANGLE CORRODED AT A NUT PLATE AT X600, Z100 AND Y21L. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-11, 51-2 0-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2002042900031 20020429 00031 NM 2002 4 29 QXEA0200587 1 20020323 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX-UNDERSIDE OF SKIN CORRODED AT NUT PLATE AT X600, Y27R AND Z100. REPAIRED IAW DHC-8 SRM 51-00-06, 51-00-04, 51-20-16 , 51-20-36 AND 51-20-11. 2 H 7 2 4T RT A13NM 2002042900032 20020429 00032 NM 2002 4 29 QXEA0200588 1 20020329 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- CARGO DOOR THRESHOLD FROM X545 TO X600, 20 EACH NUT PLATES AND NUT PLATE HOLES ARE CORRODED ON UNDER SIDE. REPAIRE D IAW DHC-8 SRM 51-20-11, 51-40-11 AND 20-21-16. 2 H 7 2 4T RT A13NM 2002042900033 20020429 00033 NM 2002 4 29 QXEA0200589 1 20020331 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- RT OUTBOARD SEAT TRACK AT STATION X540 TO X545 HAS LIGHT PITTING CORROSION ON TOP OF FLANGES. REPAIRED IAW DHC-8 S RM 51-00-06 RD 8-53-3644. 2 H 7 2 4T RT A13NM 2002042900034 20020429 00034 NM 2002 4 29 QXEA0200590 1 20020331 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- RT OUTBOARD SEAT TRACK AT X468 HAS CORROSION PITS ON TOP FLANGE. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042900035 20020429 00035 NM 2002 4 29 QXEA0200591 1 20020409 A 3397 WIRE DHAV DHC8 DHC8202 2809007 NM CABIN FAULTY A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 358PH 506 PDX- FORWARD MOST 6 INCH SECTION OF EMERGENCY TRACK LIGHTING ON PANEL 133BZ WILL NOT ILLUMINATE. REPINNED WIRING IN TRA CK LIGHTING RECEPTACLE. 2 H 7 2 4T RT A13NM 2002042900036 20020429 00036 NM 2002 4 29 QXEA0200592 1 20020407 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- LT INBOARD SEAT TRACK X217 HAS TOP FLANGE PITTING. REPAIRED IAW DHC-8 SRM 21-40-11 AND 51-40-00. 2 H 7 2 4T RT A13NM 2002042900037 20020429 00037 NM 2002 4 29 QXEA0200594 1 20020403 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- UPPER FLANGE OF REAR WING SPAR HAS LIGHT FRETTING CORROSION AT STATION X426.9. REPAIRED IAW DHC-8 RD 8-57-1434. 2 H 7 2 4T RT A13NM 2002042900038 20020429 00038 NM 2002 4 29 QXEA0200596 1 20020402 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- UPPER FLANGE OF WING REAR SPAR HAS LIGHT FRETTING CORROSION AT STATION X426.9. REPAIRED IAW DHC-8 RD 8-57-1434. 2 H 7 2 4T RT A13NM 2002042900039 20020429 00039 NM 2002 4 29 QXEA0200597 1 20020408 A 5420 WEB DHAV DHC8 DHC8202 2809007 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- RT NACELLE WEB IS CRACKED AT UPPER FASTENER WHERE REFUEL/DEFUEL BRACKET ATTACHES TO WEB. REPAIRED IAW HORIZON AIR EA 2-54-135. 2 H 7 2 4T RT A13NM 2002042900040 20020429 00040 NM 2002 4 29 QXEA0200599 1 20020403 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- DENT IN FUSELAGE RIGHT HAND SIDE UNDER SECOND FROM LAST PASSENGER WINDOW AT STATION X488.5 AND X510 AND STRINGER 18 AND 19. REPAIRED IAW HORIZON AIR EA 2-53-385. 2 H 7 2 4T RT A13NM 2002042900041 20020429 00041 NM 2002 4 29 QXEA0200600 1 20020409 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- FLOOR PANEL 143BZ HAS EMERGENCY LIGHTING CRACKED. REPAIRED IAW DHC-8 SRM 33-51-11. 2 H 7 2 4T RT A13NM 2002042900042 20020429 00042 NM 2002 4 29 QXEA0200601 1 20020331 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- AREA OF CORROSION ON RIGHT HAND OUTBOARD SEAT TRACK AT STATION 490.0. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53- 1342. 2 H 7 2 4T RT A13NM 2002042900043 20020429 00043 SO 2002 4 29 SWIA200210752 1 20020217 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 233SW 120307 LEFT FRAME 9 IS CRACKED FORWARD OF THE DIRECT VISION WINDOW POST. REPAIRED CRACK BY COMPLIANCE WITH SB 120-53-0073. 2 L 7 2 4T RT A31SO 2002042900044 20020429 00044 EA 2002 4 29 SWIA200210753 1 20020318 A 2721 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA RUDDER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 405SW 7029 RUDDER TRIM SWITCH OPERATES RUDDER TRIM TO THE LEFT ONLY. REPLACED RUDDER AND AILERON TRIM CONTROL PER 27-12-10. OPS C HECK GOOD. 2 L 7 2 4F RT A21EA 2002042900045 20020429 00045 SO 2002 4 29 SWIA200210754 1 20020322 A 2752 3203001005 ACTUATOR EMB 120 EMB120RT 3260202 SO T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 593SW 2747 1058 120191 FLAP CONTROL FAULT ILLUMINATED DURING CRUISE WITH FLAP SELECTOR IN UP POSITION. ANNUNCIATOR PANEL SHOWED SECOND SEGMENT S ONLY OF INBOARD LEFT AND RIGHT FLAPS ILLUMINATED. QRH PROCEDURE WOULD NOT CORRECT FAULT. INSTALLED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-07. INSTALLED RIGHT INBOARD FLAP ACTUATOR IAW MM 27-50-07. OPS CHECKED IAW 27-50-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002042900046 20020429 00046 SO 2002 4 29 SWIA200210756 1 20020324 A 2750 FCU EMB 120 EMB120ER 3260203 SO T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION UK UNKNOWN 1 NM 07 224SW 120294 FLAP CONTROL FAULT, INBOARD FLAPS STUCK. REPLACED FCU WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002042900048 20020429 00048 SO 2002 4 29 SWIA200210758 1 20020327 A 2133 20916010800 OUTFLOW VALVE EMB 120 EMB120ER 3260203 SO CABIN PRESSURE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 579SW 120347 AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. REMOVED AND REPLACED ELECTRO PNEUMATIC OUTFLOW VALVE. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002042900049 20020429 00049 2002 4 29 SWIA200210759 4 20020327 A 2312 CONTROL BOX EMB 120 EMB120ER 3260203 SO COMM SYSTEM FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 251YV 120251 COMMUNICATIONS FREQUENCY SWITCH FAILED AFTER DEPARTURE. DIVERTED BACK TO FAT. REMOVED AND REPLACED COMM-1 CONTROL BOX WITH SERVICEABLE UNIT. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002042900050 20020429 00050 SO 2002 4 29 SWIA200210760 1 20020327 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 220SW 120288 EMERGENCY LIGHTS AT ROW 6 AND FLOOR LIGHTING AT ROWS 3, 4 & 5 ARE INOPERATIVE. REPLACED CENTER BATTERY PACK PER 33-50-0 0. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002042900051 20020429 00051 SO 2002 4 29 SWIA200210761 1 20020327 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 284YV 120284 ABORTED TAKEOFF DUE TO TRIM AURAL WARNING. TRIM WAS IN THE GREEN RANGE AT 38 DEGREES CG. CHECKED TRIM WARNING SYSTEM. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002042900054 20020429 00054 2002 4 29 SWIA200210763 4 20020328 A 3452 TRANSPONDER EMB 120 EMB120ER 3260203 SO E/E BAY MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 271YV 120271 AFTER TAKEOFF, TRANSPONDER NR 1 REPORTED DIAG WITH NO ASSOCIATED NUMBER. ATC REPORTED NO ALTITUDE READOUT. SWITCHED TO NR 2 TRANSPONDER AND HAD NO REPLY LIGHT OR ALT INFORMATION AS REPORTED BY ATC. RETURNED TO PDX. RERACKED NR 1 TDR94 T RANSPONDER. INSPECTED CONNECTIONS. NO DEFECTS NOTED. OPS CHECKED NR 1 TRANSPONDER OK. REMOVED NR 2 TDR94 AND CAD62 A ND CLEANED CONNECTIONS. OPS CHECKED SYSTEM. SYSTEM TESTS GOOD. 2 L 7 2 4T RT A31SO 2002042900055 20020429 00055 SO 2002 4 29 SWIA200210764 1 20020329 A 2912 FILTER EMB 120 EMB120ER 3260203 SO HYD SYSTEM DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 295UX 120295 GREEN HYDRAULIC FILTER LIGHT ILLUMINATED ON TAKEOFF. ALL SYSTEM INDICATORS NORMAL. RETURNED TO SFO. INSTALLED NEW HYD RAULIC RETURN FILTER ON GREEN SYSTEM. PRESSURIZED SYSTEM. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002042900056 20020429 00056 SO 2002 4 29 SWIA200210765 1 20020329 A 3350 D36604001 BATTERY EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 196CA 120196 FORWARD FLOOR EMERGENCY LIGHTS ARE OUT. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-02. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002042900057 20020429 00057 EA 2002 4 29 SWIA200210766 1 20020401 A 4990 PRESSURE SWITCH CNDAIR CL600 CL6002B19 1900309 EA APU DIRTY A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 903SW 7425 APU OIL PRESSURE MESSAGE IN FLIGHT. DIVERTED TO FAT. CHANGED OIL AND FILTER AND CLEANED PRESSURE SWITCH. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2002042900058 20020429 00058 NE 2002 4 29 SWIA200210767 2 20020401 A 7321 EEC EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 293SW 120320 RIGHT EEC FAILURE ON TAKEOFF, ABORTED TAKEOFF. REMOVED AND INSTALLED SERVICEABLE RIGHT EEC IAW MM 73-22-00. REPLACED R IGHT ENGINE NP SENSOR WITH SERVICEABLE UNIT. LEAK CHECK ON ENGINE NP SENSOR CHECKS GOOD. NO LEAKS NOTED AT THIS TIME. RAN RIGHT ENGINE, EEC OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002042900059 20020429 00059 NM 2002 4 29 0201365643 1 20020402 A 5410 TORQUE BOX BOEING 757 757251 1384970 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 543US 26490 During "H" check found crack in outboard side of pylon lower torque box upper aft corner at access panel 433AL. Repaired per EA 56-189401. 2 L 7 2 4F RT A2NM 2002042900060 20020429 00060 NM 2002 4 29 CALA0200247 1 20020427 A 5540 65C2584160 RUDDER BOEING 737 7373T0 1384582 NM TAIL SECTION CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 40033 23358 WHILE AIRCRAFT WAS IN HOLD FOR PAINT JOB AT VENDOR FACILITY THE RUDDER SUSTAINED DAMAGE. INSPECTION FOUND THAT THE RUDDE R LOWER WEB HAD AN 8" CRACK WITH A HOLE AND SHORTER CRACKS EMANATING FROM IT. THE LEFT LOWER SKIN OF RUDDER HAD TWO CRAC KS IN SAME AREA. THE RUDDER WAS REMOVED AND REPLACED IAW MM 27-21-11, PAGE 401-403. A TEST FLIGHT WAS CONDUCTED AND OPER ATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 2002042900061 20020429 00061 WP 2002 4 29 0201319609 1 20020418 A 2150 39271411 SHUTOFF VALVE DOUG DC9 DC932 3022066 WP A/C BAY FAILED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 609NW 47234 MASTER WARNING AND CABIN PRESSURE LIGHTS ILLUMINATED AT FL350. AIRFOIL AND ENGINE ANTI-ICE WERE SELECTED ON. CABIN ALT ITUDE WAS 10,000 FEET AND CLIMBING AT 1200 FPM. CREW PERFORMED AND EMERGENCY DESCENT AND SHUT OFF THE AIRFOIL ANTI-ICE AND THE PNEUMATIC CROSSFEED VALVE. CABIN REACHED 12,500 FEET BUT THE MASKS DID NOT DEPLOY. CABIN STARTED TO RECOVER DU RING THE DESCENT AND THE CONTROLLER SEEMED TO HAVE OPERATED NORMALLY ALL THE WAY TO LANDING. LANDING AT MSP WAS UNEVENT FUL. MAINTENANCE FOUND THE RIGHT PACK PRESSURE SHUTOFF VALVE NOT ALLOWING ENOUGH FLOW THROUGH THE RIGHT PACK FLOW CONTR OL VALVE AND REPLACED THE RIGHT PRESSURE SHUTOFF VALVE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002042900062 20020429 00062 WP 2002 4 29 0201329961 1 20020424 A 2131 10256861 CONTROLLER DOUG DC9 DC931 3022065 WP CABIN PRESSURE MALFUNCTIONED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 994Z 47097 AIRCRAFT WAS CRUISING AT FL330 WHEN THE CABIN PRESSURE ANNUNCIATOR LIGHT ILLUMINATED AND CABIN ALTITUDE WAS APPROACHING 10,000 FEET. WING ANTI-ICE AND ENGINE ANTI-ICE WERE BOTH ON AT THE TIME AND TURNING THEM OFF DID NOT HELP TO REGAIN CAB IN PRESSURE. CREW DECLARED AN EMERGENCY AND DESCENDED TO 10,000 FEET WHERE THE SYSTEM WAS ABLE TO RECOVER. LANDING AT ATL WAS WITHOUT INCIDENT AND MAINTENANCE REPLACED THE PRESSURE CONTROLLER AND THE PRESSURE AMPLIFIER AFTER CHECKING FOR LEAKS. NO LEAKS WERE FOUND AND MASKS DID NOT DEPLOY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002042900063 20020429 00063 WP 2002 4 29 0201331242 1 20020423 A 2910 HYDRAULIC LINE DOUG DC10 DC1030 3023501 WP NR 3 SYSTEM LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 242NW 47845 DURING CRUISE FROM HNL-KIX, THE ELEVATOR OFF LIGHT ILLUMINATED. COMPLIED WITH COM PROCEDURE AND CONTINUED TO DESTINATIO N. UPON GEAR EXTENSION, THE NR 3 SYSTEM QUANTITY WENT TO ZERO. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDR AULIC LINE TO RIGHT SPOILER DRIVE ACTUATOR LEAKING. REPLACED THE PACKINGS IN FITTING. LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 2002050200093 20020502 00093 NM 2002 5 2 02FDEA00287 1 20020425 A 7110 FRAME BOEING 727 7272S2F 1384O81 NM COWLING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 207FE 22929 RIB STRIP AT BS 1352 IS WORN THROUGH IN SEVERAL PLACES, OVER ENTIRE LT & RT SIDES. REMOVED AND REPLACED CHORD PER SRM 5 1-30-2, 53-10-1, 51-30-5. 2 L 7 3 4F A3WE 2002050200063 20020502 00063 NM 2002 5 2 02FDEA00290 1 20020425 A 2910 HYDRAULIC LINE BOEING 727 72722 1384002 NM HYD SYSTEM LEAKING A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 169FE 18866 HYDRAULIC A-QTY TO ZERO IN FLT. REMOVED AND REPLACED NR 1 ENG A-SYSTEM HYDRAULIC PRESS LINE. REMOVED AND REPLACED 1 & 2 ENGINE HYD PUMP CASE DRAIN FILTERS PER MM 29-11-041-2. 2 L 7 3 4F A3WE 2002042900064 20020429 00064 NM 2002 4 29 2002F00423 1 20020415 A 2160 3987505 CONTROL VALVE BOEING 757 75723N 1384973 NM A/C BAY MALFUNCTIONED G AMTA K NONE J WARNING INDICATION AP APPROACH 1 GL 11 516AT 23867 23867 27972 FLIGHT 217, LEFT PACK TEMP EICAS & LEFT PACK INOP LIGHT CAME ON DURING APPROACH. ON & OFF 3 TIMES, CAME ON DURING TAXI IN. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK TEMP CONTROL VALVE. 2 L 7 2 4F RT A2NM 2002042900065 20020429 00065 EU 2002 4 29 AWXA200200365 1 20020424 A 3320 325060 BALLAST AIRBUS 320 A320231 3930325 EU CABIN DEFECTIVE A AWXA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 621AW 053 PHX - BURNING SMELL - FLT 0652 - FLIGHT ATTENDANTS NOTICED AN ELECTRICAL BURNING SMELL AT MID CABIN NEAR OVERWING AREA. MAINTENANCE DISCOVERED AND REPLACED A BAD CABIN SIDEWALL LIGHTING BALLAST AT SEAT ROW 7 RT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002042900066 20020429 00066 NM 2002 4 29 AWXA200200366 1 20020425 A 3350 20121 CHARGER BOEING 757 7572G7 1384963 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 910AW 24523 PHX - EEL - DURING INSPECTION 3 EACH AFT EMERGENCY LIGHTS WERE FOUND INOPERATIVE; RT AFT BULLNOSE, AND THE R4 DOOR SLIDE LIGHT. MAINTENANCE REPLACED BATTERY CHARGER AND BATTERY PACK M736 PER T/C A1C33607, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002042900067 20020429 00067 NM 2002 4 29 AWXA200200368 1 20020408 A 5313 651960337 STRINGER BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 YVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND AT FORWARD CABIN LT INBOARD SIDE BS 360-380, STR 17 LT WEB AND STR 17 LT CHORD. MAINTENANCE REMOVED DAMAGED WEB AND OUTER CHORD BETWEEN BS 360 AND BS 380, FABRICATED A NEW WEB AND OU TER CHORD, AND INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-4, FIG 1, PG 16 AND SRM 51-10-1, PG 8 DWG 65-19603. 2 L 7 2 4F RT A16WE 2002042900068 20020429 00068 NM 2002 4 29 AWXA200200370 1 20020406 A 5320 146N83262 FLOOR SUPPORT BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 GYR - MAJOR REPAIR - DURING C11 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBOARD SUPPORT ANGLE (INNER CHORD) AT BS 1350, RBL 64. MAINTENANCE REMOVED INNER CHORD FROM BS 1290 TO BS 1405 RT, FABRICATED NEW INNER CHORD, AND INSTALLED REPAIR P ARTS IAW DWG 146N8326, AND SRM 51-40-01 PG 1. 2 L 7 2 4F RT A2NM 2002042900069 20020429 00069 NM 2002 4 29 AWXA200200372 1 20020404 A 5330 146N36009 DOUBLER BOEING 757 7572G7 1384963 NM FUSELAGE WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 GYR - MAJOR REPAIR - DURING C-11 CHECK THE INTERNAL DOUBLER FOR THE AFT POTABLE WATER SERVICE PANEL LATCH WAS FOUND WORN BEYOND LIMITS. MAINTENANCE REMOVED FLOORBOARD BS 1510-1640, REMOVED CLIPS AT BS 1640, AND 1660, STR 29 RT TO 29 LT, RE MOVED POTABLE WATER SERVICE DOOR INTERNAL DOUBLER AT BS 1640-1660, STR 29 RT TO 29 LT, FABRICATED DOUBLER AND INSTALLED REPAIR PART AND REINSTALLED FLOORBOARD AND CLIPS PER DWG 146N3600, AND SRM 51-10-02. 2 L 7 2 4F RT A2NM 2002042900070 20020429 00070 SO 2002 4 29 C2XA02IA095 1 20020424 A 3350 P890S CONNECTOR EMB 145 EMB145 3260210 SO COCKPIT DIRTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15973 145159 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHT NOT ARMED INTERMITTENT ON EICAS. MAINTENANCE CLEANED TH E CANNON PLUG ON THE CABIN LIGHT CONTROL UNIT, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002042900071 20020429 00071 SO 2002 4 29 C2XA02IA097 1 20020428 A 2120 SMOKE EMB 120 EMB120ER 3260203 SO COCKPIT DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16718 120136 VCT- DURING POST FLIGHT THE CREW NOTED THAT SMOKE WAS PRESENT IN THE COCKPIT WITH THE APU RUNNING. THE AIRCRAFT WAS RE LEASED FOR FLIGHT. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE APU AND AIR CONDITIONING SYSTEMS, COULD NOT DUPLICA TE THE PROBLEM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002042900072 20020429 00072 NM 2002 4 29 QXEA0200708 1 20020423 A 3350 1640518 CONNECTOR DHAV DHC8 DHC8202 2809007 NM CABIN LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX-EMERGENCY EXIT SIGN NEXT TO LEFT HAND OVERWING EXIT IS INOPERATIVE. REMOVED AND REPLACED LOOSE CONNECTOR PIN AT LEFT HAND OVERWING EMERGENCY EXIT CONNECTOR PLUG. EMERGENCY LIGHT OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002042900074 20020429 00074 NM 2002 4 29 DHL2002726505 1 20020418 A 5330 SKIN BOEING 727 727228 1384083 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, EXTERNAL FUSELAGE REPAIR AT BS 1223, STR 21R IS INSTALLED WITH BLIND FASTENERS. REMOVED REPAIR IAW B-72 7 SRM 51-30-2. FABRICATED AND INSTALLED NEW DOUBLER IAW B-727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002042900075 20020429 00075 NM 2002 4 29 DHL2002753002 1 20020426 A 3350 BATTERY BOEING 727 727223 1384074 NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 712AA 22468 EMERGENCY LIGHT OVER L1 DOOR INOP. REMOVED AND REPLACED BATTERIES IN EMERGENCY LIGHT OVER L1 DOOR, GROUND OP CHECK GOOD IAW MM REF 33-50-71. 2 L 7 3 4F A3WE 2002042900077 20020429 00077 NE 2002 4 29 P2EA2002M028 2 20020225 A 7532 BLEED VALVE BOEING 737 737230 1384401 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE LACK OF LUBE A P2EA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 05 123NJ 22121 NR 2 ENGINE COMPRESSOR STALLED AS THE THROTTLES WERE ADVANCED FOR TAKEOFF. LUBED THE NR 2 ENGINE BLEED VALVES IAW AMM 7 5-31-0. RAN ENGINE, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 2002042900078 20020429 00078 NM 2002 4 29 QXEA0200593 1 20020404 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- REFERENCE HORIZON AIR EA 2-57-158 RIGHT HAND FRONT SPAR UPPER FLANGE DAMAGE. 2 H 7 2 4T RT A13NM 2002042900079 20020429 00079 NM 2002 4 29 QXEA0200598 1 20020405 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- MAIN CABIN FLOOR HAS RIVET HOLE AT FRAME X355.950 THAT HOLDS NR 4 SEAT TRACK IS DIMPLED AND CRACKED. REPAIRED IAW HORIZON AIR EA 2-53-379. 2 H 7 2 4T RT A13NM 2002042900080 20020429 00080 NM 2002 4 29 QXEA0200602 1 20020331 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS CORROSION AND TOOLING DAMAGE ON TOP TRACK SURFACE FROM STATION 498.5 TO 500.5. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042900081 20020429 00081 NM 2002 4 29 QXEA0200603 1 20020331 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- RT OUTBOARD SEAT TRACK HAS CORROSION ON TOP TRACK SURFACE AT STATION 486.5 TO 488.5. REPAIRED IAW DHC-8 SRM 51-00- 06 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042900082 20020429 00082 NM 2002 4 29 QXEA0200604 1 20020325 A 5320 STRAP DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- FRAME REINFORCING STRAP HAS THREE MINOR CHAFES AT STATION X636.0 BETWEEN STRINGERS 21-23 RIGHT HAND. 2 H 7 2 4T RT A13NM 2002042900083 20020429 00083 NM 2002 4 29 QXEA0200605 1 20020323 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- CORROSION ON FRAME 653.35 29 INCHES LEFT OF AIRCRAFT CENTER LINE UNDER CARGO PIT FLOOR. REPAIRED IAW DHC-8 SRM 51- 20-11 AND 51-20-16. 2 H 7 2 4T RT A13NM 2002042900084 20020429 00084 NM 2002 4 29 QXEA0200606 1 20020323 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- CORROSION ON FRAME 653.35 28 INCHES RIGHT OF CENTER LINE UNDER CARGO PIT FLOOR. REPAIRED IAW DHC-8 SRM 51-20-11 AN D 51-20-16. 2 H 7 2 4T RT A13NM 2002042900085 20020429 00085 NM 2002 4 29 QXEA0200607 1 20020323 A 5320 TIE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- CORROSION ON FRAME TIE, ON FRAME 653.35 TO STRINGER 22. REPAIRED IAW DHC-8 SRM 51-20-11 AND 51-20-16. 2 H 7 2 4T RT A13NM 2002042900086 20020429 00086 NM 2002 4 29 QXEA0200608 1 20020323 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- MAIN CABIN DOOR THRESHOLD ANGLE TOP SIDE HAS DEEP PITTING IN RADIUS. REPAIRED IAW DHC-8 SRM 51-20-16, 51-20-36, 51 -40-11 AND 51-40-00. 2 H 7 2 4T RT A13NM 2002042900087 20020429 00087 NM 2002 4 29 QXEA0200609 1 20020323 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- VERTICAL STABILIZER SKIN HAS 1 SMOKING RIVET AT AFT APR LOCATION JUST BELOW ACCESS PANEL 322DL OPENINGS. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002042900088 20020429 00088 WP 2002 4 29 ABXA010849 1 20020415 A 5310 59114003 DOUBLER DOUG DC9 DC932 3022066 WP EXT. FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 LOWER FUSELAGE SKIN WAS CRACKED AT THE LEFT AFT NOSE GEAR DOOR ATTACHING CUTOUT. INSTALLED REPAIR DOUBLER AT THE AFT NOS E GEAR DOOR CUTOUT AREA IAW DC-9 SRM 53-05. 2 L 7 2 4F A6WE 2002042900089 20020429 00089 WP 2002 4 29 ABXA010850 1 20020415 A 5530 591214130 ANGLE DOUG DC9 DC932 3022066 WP VERT. STAB. CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 RIGHT VERTICAL STABILIZER ATTACH ANGLE WAS CRACKED ON THE AFT END. REPAIRED AREA IAW DC-9 SRM 53-05. 2 L 7 2 4F A6WE 2002042900090 20020429 00090 WP 2002 4 29 ABXA010851 1 20020413 A 5700 4925721502 FITTING DOUG DC9 DC932 3022066 WP REAR SPAR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 CRACK IN FITTING COMMON TO REAR SPAR, JUST BELOW THE INBOARD SPOILER/TORSION BAR. REPLACED STIFFENER AND REPAIRED AREA I AW DC-9 SRM. 2 L 7 2 4F A6WE 2002042900091 20020429 00091 WP 2002 4 29 ABXA010852 1 20020416 A 5700 99193017 RIB DOUG DC9 DC932 3022066 WP LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 LEFT WING LEADING EDGE RIB AT THE #2 SLAT TRACK, INBOARD RIB WAS CRACKED. REPAIRED RIB IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002042900092 20020429 00092 WP 2002 4 29 ABXA010853 1 20020416 A 5700 3920511508 SUPPORT DOUG DC9 DC932 3022066 WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 RIGHT WING SLAT CONTROL PULLEY BRACKET SUPPORT WAS CRACKED. INSTALLED NEW PULLEY BRACKET IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002042900093 20020429 00093 WP 2002 4 29 ABXA010854 1 20020416 A 5310 5956034538 SUPPORT DOUG DC9 DC932 3022066 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 INTERCOSTAL ATTACH FITTING AT STATION 994 BETWEEN LONGERON 27 - 28 RIGHT WAS CRACKED AND CORRODED AROUND LOWER NUTPLATE. REPLACED INTERCOSTAL ATTACH FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002042900094 20020429 00094 WP 2002 4 29 ABXA010855 1 20020416 A 5310 591142547 LONGERON DOUG DC9 DC932 3022066 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 LONGERON 28 RIGHT AT STATION 990 WAS CRACKED FROM EXFOLIATION CORROSION. REPLACED LONGERON 28 RIGHT AT STATION 990 IAW D C-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002042900095 20020429 00095 WP 2002 4 29 ABXA010856 1 20020416 A 5310 595803441 FITTING DOUG DC9 DC932 3022066 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 INTERCOSTAL ATTACH FITTING AT STATION 994 BETWEEN LONGERON 27 - 28 LEFT WAS CRACKED. REPLACED INTERCOSTAL ATTACH FITTING IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002042900096 20020429 00096 NM 2002 4 29 QXEA0200610 1 20020323 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- VERTICAL STABILIZER SKIN HAS 5 SMOKING RIVETS AT AFT SPAR JUST BELOW ACCESS PANEL 322HR OPENING. REPAIRED IAW DHC- 8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002042900097 20020429 00097 NM 2002 4 29 02042901 1 20020427 A 3350 UNKNOWN LIGHT BOEING 757 75723A 1384967 NM SEAT 16C A N8TA K NONE O OTHER UK UNKNOWN 1 WP 19 757NA 24567 Seat 16C Emergency Light INOP. Deferred I.A.W. MEL 33-51-03 Situation 1 Category C Authorization Number 57-0233. Removed and Replaced Light Assembly; Light Assembly had been ripped from seat. 2 L 7 2 4F RT A2NM 2002042900098 20020429 00098 NM 2002 4 29 QXEA0200611 1 20020325 A 5544 RUB STRIP DHAV DHC8 DHC8202 2809007 NM RUDDER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- FORE RUDDER TOP RUB STRIP HAS CHAFE WEAR. REPAIRED IAW DHC-8 SRM 51-20-36, 51-40-11 AND 20-21-50. 2 H 7 2 4T RT A13NM 2002042900099 20020429 00099 NM 2002 4 29 QXEA0200614 1 20020405 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- SEAT TRACK NR 7 RT FORWARD INBOARD ATTACH POINT IN FRAME 270.5 HAS RIVET HOLE DAMAGE. REPAIRED IAW DHC-8 SRM 51-40 -11 AND HORIZON AIR EA 2-53-381. 2 H 7 2 4T RT A13NM 2002042900100 20020429 00100 NM 2002 4 29 QXEA0200615 1 20020402 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- UPPER FLANGE OF REAR WING SPAR IS CHAFED AND POSSIBLE FRETTING CORROSION. REPAIRED IAW DHC-8 SRM 51-20-11 AND RD 8 -57-1434. 2 H 7 2 4T RT A13NM 2002042900101 20020429 00101 NM 2002 4 29 QXEA0200616 1 20020402 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- UPPER FLANGE OF FORWARD WING SPAR HAS CHAFE DAMAGE AT FRAME 38.4/LBL 52.0 TO RBL 52.0. REPAIRED IAW DHC-8 RD 8-57- 1441. 2 H 7 2 4T RT A13NM 2002042900102 20020429 00102 NM 2002 4 29 QXEA0200618 1 20020323 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- MAIN CABIN DOOR THRESHOLD ANGLE TOP AND BOTTOM IS CORRODED AT 7 EACH NUT PLATE HOLES. REPAIRED IAW DHC-8 SRM 51-20 -16, 51-20-36 AND CPM 4-25-4-26. 2 H 7 2 4T RT A13NM 2002042900103 20020429 00103 NM 2002 4 29 QXEA0200619 1 20020403 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- RT INBOARD SEAT TRACK X189 HAS CORROSION PITS ON TOP RAIL. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-53-2295. 2 H 7 2 4T RT A13NM 2002042900104 20020429 00104 NM 2002 4 29 QXEA0200620 1 20020407 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- LT INBOARD SEAT RAIL X217 HAS PITTING CORROSION ON TOP FLANGE. REPAIRED IAW DHC-8 SRM 51-40-00, 51-40-11 RD 8-53-2 295, 8-53-4473 AND 8-53-1102. 2 H 7 2 4T RT A13NM 2002042900105 20020429 00105 NM 2002 4 29 QXEA0200622 1 20020402 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- GOUGES ON TOP OF RIGHT WING FORWARD SPAR AROUND TOP OUTBOARD SCREW HOLES. REPAIRED IAW HORIZON AIR EA 2-57-158. 2 H 7 2 4T RT A13NM 2002042900106 20020429 00106 NM 2002 4 29 QXEA0200623 1 20020402 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- SCRATCH AND FRETTING CORROSION ON RIGHT WING FORWARD SPAR AROUND SCREW HOLE FOR RIGHT LEADING EDGE 611 AT TOP INBOA RD NEXT TO FUSELAGE. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-57-158. 2 H 7 2 4T RT A13NM 2002042900107 20020429 00107 NM 2002 4 29 QXEA0200624 1 20020403 A 3230 FITTING DHAV DHC8 DHC8202 2809007 NM LT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- FRETTING AT LEFT MAIN GEAR RETRACTION ACTUATOR FITTING ATTACH POINT IN FORWARD WHEEL WELL AT LOWER TWO BOLT POINTS. REPAIRED IAW DHC-8 RD 8-54-1178 AND HORIZON AIR EA 2-54-125. 2 H 7 2 4T RT A13NM 2002042900108 20020429 00108 NM 2002 4 29 QXEA0200625 1 20020327 A 3220 ARM DHAV DHC8 DHC8202 2809007 NM NLG GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- GOUGES ON FACE OF TRAILING ARM ON NOSE LANDING GEAR. REPAIRED IAW DHC-8 SRM 32-20-01 AND RD 8-32-289. 2 H 7 2 4T RT A13NM 2002042900109 20020429 00109 NM 2002 4 29 QXEA0200645 1 20020420 A 2751 INDICATOR DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTIONED A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 347PH 480 PDX - AIRCRAFT ABORTED TAKEOFF WHEN THE TAKEOFF WARNING HORN SOUNDED. THE FLAP LEVER WAS SET AT 5 DEGREES AND THE INDIC ATOR SHOWED 0 DEGREES. CREW PULLED AND RESET THE FLAP INDICATOR CIRCUIT BREAKERS AS DIRECTED BY MAINTENANCE CONTROL AND IAW QX GMM 4-1-0, PAGE 7. THE FLAP INDICATION AND OPERATION RETURNED TO NORMAL. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A13NM 2002042900110 20020429 00110 EA 2002 4 29 QXEA0200650 1 20020418 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - SHALLOW GOUGES NOTED JUST FORWARD OF THE MAIN CABIN DOOR OPENING, MIDWAY ALONG THE LENGTH. HFEC INSPECTED THE GOU GED AREAS AND NO CRACKS WERE NOTED. THE REPAIR WAS COMPLETED IAW EA R-53-33. 2 L 7 2 4F RT A21EA 2002042900111 20020429 00111 NM 2002 4 29 QXEA0200651 1 20020415 A 5420 ANGLE DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- CLOSING ANGLE CRACKED AT LT ENGINE FIREWALL INBOARD FORWARD SIDE. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002042900112 20020429 00112 NM 2002 4 29 QXEA0200652 1 20020414 A 5347 CARGO TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- BAGGAGE COMPARTMENT FLOOR AFT RT SEAT TRACK NR 9 HAS CORROSION INSIDE CHANNEL. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-4936. 2 H 7 2 4T RT A13NM 2002042900113 20020429 00113 NM 2002 4 29 QXEA0200653 1 20020414 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- PANEL MATTING SURFACES THROUGHOUT FORWARD SPAR ARE GOUGED AND SCRATCHED ON FORWARD TURTLE BACK AREA. REPAIRED IAW DHC-8 SRM 51-20-36, 51-20-16 AND RD 8-57-1441. 2 H 7 2 4T RT A13NM 2002042900114 20020429 00114 NM 2002 4 29 QXEA0200654 1 20020416 A 5413 STRINGER DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- LT NACELLE FINGERNAIL DECK FORE AND AFT LOWER STRINGERS ARE CRACKED. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002071200183 20020712 00183 NM 2002 7 12 QXEA0200655 1 20020417 A 5320 CLIP DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- CRACKED CLIP ON REAR FUSELAGE FRAME 4 AND STRINGER 4L. REPAIRED IAW DHC-8 RD 8-55-199. 2 H 7 2 4T RT A13NM 2002042900115 20020429 00115 NM 2002 4 29 QXEA0200656 1 20020417 A 5320 CLIP DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- CRACKED CLIP AT REAR FUSELAGE FRAME 4 AND STRINGER 4R. REPAIRED IAW DHC-8 RD 8-55-199. 2 H 7 2 4T RT A13NM 2002042900116 20020429 00116 NM 2002 4 29 QXEA0200657 1 20020417 A 5544 RUB STRIP DHAV DHC8 DHC8202 2809007 NM RUDDER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- FORE RUDDER RUB STRIP CHAFED. REPAIRED IAW DHC-8 SRM 51-20-51, 51-40-11 AND HORIZON AIR EA 2-55-65. 2 H 7 2 4T RT A13NM 2002042900117 20020429 00117 NM 2002 4 29 QXEA0200658 1 20020419 A 5320 WEB DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- WEB IS GOUGED AND DENTED AT CENTER MOUNT FOR ISOLATION VALVE LEFT HAND YW01.500 FORWARD SPAR. REPAIRED IAW DHC-8 R D 8-53-5437. 2 H 7 2 4T RT A13NM 2002042900118 20020429 00118 NM 2002 4 29 QXEA0200659 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- WEAR IN RT INBOARD SEAT TRACK FROM X472.0 TO 483.5. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002042900119 20020429 00119 NM 2002 4 29 QXEA0200660 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- WEAR INSIDE AND ON TOP OF RT INBOARD SEAT TRACK FROM X507.5 TO X518.5. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53- 3644. 2 H 7 2 4T RT A13NM 2002042900120 20020429 00120 WP 2002 4 29 MWEA020291 1 20020425 A 5210 39158521 SUPPORT DOUG DC9 DC914 3022034 WP PAX DOOR ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 INTERCOSTAL SUPPORT WAS REMOVED TO FACILITATE OTHER MAINTENANCE AND WAS FOUND TO HAVE ELONGATED HOLES AFTER REMOVAL. -- REPLACED WITH NEW SUPPORT. 2 L 7 2 4F A6WE 2002042900121 20020429 00121 WP 2002 4 29 MWEA020292 1 20020425 A 5210 99557563 BEAM DOUG DC9 DC914 3022034 WP PAX DOOR ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 REMOVED DAMAGED INTERCOSTAL AND SUPPORT AND FOUND PAX DOOR BEAM #5 TO HAVE AN ELONGATED HOLE. -- FABRICATED AND INSTAL LED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002042900122 20020429 00122 WP 2002 4 29 MWEA020294 1 20020411 A 5313 3924809501 LONGERON DOUG DC9 DC932 3022066 WP STATION 570 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FORWARD PIT LONGERON 29 RIGHT IS CRACKED AT STATION 570-578. -- REMOVED, MATCH DRILLED LONGERON AS REQUIRED PER DWG # 5910068, AND INSTALLED. 2 L 7 2 4F A6WE 2002042900123 20020429 00123 WP 2002 4 29 MWEA020297 1 20020423 A 5330 5920323187 SKIN DOUG DC9 DC981 3022081 WP STATION 229 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 NUMEROUS AREAS OF DAMAGE BETWEEN STATION 229 AND 255 FROM LONGERON 20 RIGHT TO LONGERON 26 RIGHT. -- SPLICED IN SECTIO N OF SKIN FLUSH REPAIR IAW SRM 53-04 FIGURE 12C. 2 L 7 2 4F A6WE 2002042900124 20020429 00124 WP 2002 4 29 MWEA020281 1 20020426 A 5320 5932658196 BRACKET DOUG DC9 DC982 3022082 WP STATION 886 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 INTERCOSTAL BRACKET AT STATION 886 LONGERON 16 IAW SRM 51-30-5. REMOVED TO FACILITATE OTHER MAINTENANCE. -- BRACKET HA S A GOUGE AT VERTICAL LEG. FABRICATED AND INSTALLED TEE CLIP. 2 L 7 2 4F A6WE 2002042900125 20020429 00125 WP 2002 4 29 MWEA020283 1 20020426 A 5320 99196715 INTERCOSTAL DOUG DC9 DC982 3022082 WP STATION 886 UNSERVICEABLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 REMOVE INTERCOSTAL AT RIGHT LONGERON 17 BETWEEN STATION 886 TO STATION 906 TO FACILITATE OTHER MAINTENANCE. -- FABRICA TED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2002042900126 20020429 00126 WP 2002 4 29 MWEA020284 1 20020426 A 5311 9923406504 FRAME DOUG DC9 DC982 3022082 WP STATION 886 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FRAME 886 IS CRACKED ON RIGHT SIDE AT FLOOR LEVEL. -- REMOVED AND REPLACED LOWER SECTION OF FRAME. FABRICATED AND INST ALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 2002042900127 20020429 00127 WP 2002 4 29 MWEA020288 1 20020426 A 5320 5932658198 CLIP DOUG DC9 DC982 3022082 WP STATION 905 UNSERVICEABLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 REMOVE CLIP AT STATION 905 ON FORWARD SIDE OF FRAME AT LONGERON 17 RIGHT TO FACILITATE OTHER MAINTENANCE. -- FABRICATE D AND INSTALLED TEE CLIP. 2 L 7 2 4F A6WE 2002042900128 20020429 00128 WP 2002 4 29 MWEA020289 1 20020426 A 5320 5932658192 CLIP DOUG DC9 DC982 3022082 WP STATION 886 UNSERVICEABLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 REMOVE CLIP AFT OF FRAME 886 AT LONGERON 17 RIGHT TO FACILITATE OTHER MAINTENANCE. -- FABRICATED AND INSTALLED TEE CLI P. 2 L 7 2 4F A6WE 2002042900129 20020429 00129 EU 2002 4 29 MALA020259 1 20020428 A 3020 M61069002 RELAY SAAB SF340 340B 7860101 EU A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 367XJ dURING fLIGHT #3182 THE LH INTAKE HEAT LIGHT ILLUMINATED AFTER DEPARTURE. AIR RETURN TO MSP. MAINTENANCE REMOVED AND R EPLACED POWER RELAY 37HE PN M6106-9-002. IAW AMM 30-20-10-4. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002042900130 20020429 00130 EU 2002 4 29 MALA020261 1 20020423 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A MALA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 15 446XJ 340B446 THE CARGO SMOKE LIGHT ILLUMINATED ACCOMPANIED BY THE TRIPLE CHIME DURING ENGINE START. MAINTENANCE REMOVED AND REPLACED CARGO AFT SMOKE DETECTOR PN CGAB1201-01 SN/OFF 764, IAW AMM 26-13-15. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002042900131 20020429 00131 EU 2002 4 29 MALA020262 1 20020425 A 2610 WG9220 WIRE SAAB SF340 SF340A 7850100 EU A MALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 15 112XJ DURING POST FLIGHT ON FLIGHT #3055, RH ENGINE FIRE INDICATION. MAINTENANCE FERRIED AC FROM TVC TO DTW TROUBLESHOOTING O F RH ENGINE FIRE DETECTION SYSTEM PROBLEM. MAINTENANCE FOUND AND REPAIRED SHORT IN WIRE WG92-20. ALL CHECKS GOOD AT TH IS TIME. ALL IAW SF340 MM. SEE 409 # 087254 FOR DETAILS. 2 L 7 2 4T RT A52EU 2002042900132 20020429 00132 NM 2002 4 29 AWXA200200375 1 20020416 A 5230 6546921183 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 0 0 24711 MCN - MAJOR REPAIR - DURING C-13 CHECK A 7/8" CRACK WAS FOUND ON THE FORWARD CARGO DOOR LOWER BEAM AT LOWER FASTENER HOL E ON TEE, CONFIRMED BY HFEC INSPECTION. MAINTENANCE TRIMMED OUT CROSSBEAM WEB AFT END, FABRICATED CROSSBEAM WEB FILLER, AND INSTALLED REPAIR PARTS IAW EO 52-31-04. 2 L 7 2 4F RT A16WE 2002042900133 20020429 00133 NM 2002 4 29 AWXA200200376 1 20020424 A 5313 69532071 CLIP BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 0 0 23780 MCN - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON THE FRAME TO STRINGER CLIP, STR 11 R/H, BS 663.75. MAINTENAN CE REMOVED DAMAGED STRINGER CLIP AT STR 11 R/H, BS 663.75, FABRICATED A NEW STRINGER CLIP, TREATED AND INSTALLED IAW DWG 69-53207, AND B737-300 SRM 51-40-02, PG 10. 2 L 7 2 4F RT A16WE 2002042900134 20020429 00134 NM 2002 4 29 AWXA200200377 1 20020424 A 5313 69532071 CLIP BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 0 0 23780 MCN - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON STRINGER CLIP AT STR 4 R/H, BS 663.75. MAINTENANCE REMAOVED DAMAGED STRINGER CLIP AT STR 4 R/H, BS 663.75, FABRICATED A NEW STRINGER CLIP, TREATED AND INSTALLED REPAIR IAW DWG 69-5 3207, AND B737-300 SRM 51-40-02, PG. 10-11. 2 L 7 2 4F RT A16WE 2002042900135 20020429 00135 SO 2002 4 29 LR7A02031 1 20020429 A 5512 SKIN LKHEED 382 382G 526414U SO HSS 188 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 559 4698 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB0503 FOUND FS 1091 LH UPPER HORIZONTAL STAB SKIN CRACKED AT HSS 188, WL 28 5.REPAIRED IAW SRM SMP 583 55-20-06. NR 0057. 2 H 7 4 4T A1SO 2002042900136 20020429 00136 SO 2002 4 29 LR7A02032 1 20020429 A 5320 3751672 BRACKET LKHEED 382 382G 526414U SO FS 204 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 559 4698 DURING SCHEDULED B2 INSPECTION PER JOB CARD HSP5396 FOUND CREW ENTRANCE LONGERON BRACKET CRACKED AT FS 204, LBL 70, WL 1 90.REPLACED BRACKET IAW DWG 375167 AND SRM SMP 583 51-10. NR 0064. 2 H 7 4 4T A1SO 2002043000021 20020430 00021 NM 2002 4 30 QXEA0200661 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- WEAR IN RT INBOARD SEAT TRACK AT X545.0. REPAIRED IAW DHC-8 SRM 51-10-4. 2 H 7 2 4T RT A13NM 2002043000022 20020430 00022 NM 2002 4 30 QXEA0200662 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- WEAR IN LT INBOARD SEAT TRACK AT X545.0. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-4936. 2 H 7 2 4T RT A13NM 2002043000023 20020430 00023 NM 2002 4 30 QXEA0200663 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- PITTING INSIDE OF RIGHT HAND OUTBOARD SEAT TRACK AT X467.0. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002043000024 20020430 00024 NM 2002 4 30 QXEA0200664 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- PITTING ON RT OUTBOARD SEAT TRACK AT X265.0. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002043000025 20020430 00025 NM 2002 4 30 QXEA0200665 1 20020415 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- LT ENGINE FIREWALL INBOARD APPROXIMATELY MIDWAY DOWN HAS A ONE INCH CRACK. REPAIRED IAW DHC-8 RD 8-54-806. 2 H 7 2 4T RT A13NM 2002043000026 20020430 00026 NM 2002 4 30 QXEA0200666 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- CORROSION ON LT OUTBOARD SEAT TRACK FROM X542.5 TO 545.0. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-3644. 2 H 7 2 4T RT A13NM 2002043000027 20020430 00027 NM 2002 4 30 QXEA0200667 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- WEAR ON LT INBOARD SEAT TRACK AT X530.5. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-4936. 2 H 7 2 4T RT A13NM 2002043000028 20020430 00028 NM 2002 4 30 QXEA0200668 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- WEAR IN LT INBOARD SEAT TRACK FROM X338.75 TO X343.25. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002043000029 20020430 00029 NM 2002 4 30 QXEA0200672 1 20020419 A 3241 WARNING SYSTEM DHAV DHC8 DHC8202 2809007 NM ANTISKID SYS MALFUNCTIONED A QXEA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 345PH 476 SEA- OUTBOARD ANTI-SKID CAUTION LIGHT ILLUMINATED AFTER TAKING IT OUT OF START/FEATHER FOR TAXI. AFTER COMPLETING EMERG ENCY CHECKLIST, RECYCLED ANTI-SKID. INBOARD ANTI-SKID ILLUMINATED AND OUTBOARD EXTINGUISHED. RAN ENGINES. PERFORMED A NTI-SKID SYSTEM SELF TEST. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2002043000030 20020430 00030 NM 2002 4 30 QXEA0200701 1 20020417 A 7110 SUPPORT BRACKET BOMBDR DHC8 DHC8401 NM NR 1 COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX- NR 1 LOWER COWL HAS A CRACK AT FIRE DECK SUPPORT BRACKET. REPAIRED IAW DHC-8 400 RD 8/4-71-016-117. 2 H 7 2 4T RT A13NM 2002043000031 20020430 00031 NM 2002 4 30 QXEA0200702 1 20020418 A 7110 SUPPORT BRACKET BOMBDR DHC8 DHC8401 NM NR 2 COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX- NR 2 ENGINE COWL HAS CRACKED FIRE DECK SUPPORT BRACKET. REPAIRED IAW DHC-8 400 RD 8/4-71-016-117. 2 H 7 2 4T RT A13NM 2002043000032 20020430 00032 NM 2002 4 30 QXEA0200703 1 20020420 A 2751 INDICATOR DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTIONED A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 347PH 480 PDX- ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN. FLAP LEVER SET AT 5 DEGREES, INDICATOR AT 0 DEGREES. PULLED AND RESE T LEFT AND RIGHT FLAP INDICATOR CIRCUIT BREAKERS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 2002043000033 20020430 00033 EA 2002 4 30 QXEA0200704 1 20020424 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 601QX 1393 1393 10009 PDX- EMERGENCY LIGHT BATTERY PACKS DISCHARGED. REMOVED AND REPLACED 1, 2, 3 AND 4 BATTERY PACKS. OPERATIONAL CHECKS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002043000034 20020430 00034 NM 2002 4 30 QXEA0200705 1 20020423 A 7110 SUPPORT BRACKET BOMBDR DHC8 DHC8401 NM NR 2 COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - NR 2 ENGINE COWL, AFT CONE SUPPORT BRACKET CRACKED. REPAIRED BRACKET IAW RD 8-71-016. 2 H 7 2 4T RT A13NM 2002043000035 20020430 00035 NM 2002 4 30 QXEA0200706 1 20020425 A 2910 HYDRAULIC SYSTEM BOMBDR DHC8 DHC8401 NM NR 1 CONTAMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 405QX 4047 SEA - BEFORE START, THE NR 1 HYDRAULIC QUANTITY READ 100 PERCENT. AFTER START, QUANTITY DROPPED TO 50 PERCENT. ALSO AF TER START, THE STANDBY PRESSURE FLUCTUATED. MAINTENANCE BLED THE NR 1 HYDRAULIC SYSTEM IAW Q400 29-10-00 AND SERVICED T HE SYSTEM IAW 12-10-29. HYDRAULIC SYSTEM OPERATES NORMALLY AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002043000036 20020430 00036 NM 2002 4 30 QXEA0200707 1 20020426 A 2720 WARNING SYSTEM BOMBDR DHC8 DHC8401 NM COCKPIT MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 405QX 4047 SEA - PITCH TRIM AND NR 2 RUDDER HYDRAULIC CAUTION LIGHT ILLUMINATED ON TAXI. MAINTENANCE PERFORMED THE FAULT ISOLATION PROCEDURE PER 27-20-00-810-805. NO FAULTS WERE PRESENT. DH8-400-SL-27-003 WAS PERFORMED. NO FAULTS NOTED. CAUTION L IGHTS EXTINGUISHED PER PROCEDURE. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002043000037 20020430 00037 EU 2002 4 30 RAIA00204128 1 20020416 A 7931 WARNING SYSTEM JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE COCKPIT MALFUNCTIONED A RAIA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 572HK 41091 76107 EWR - RIGHT ENGINE OIL PRESSURE WARNING DURING TAXI AFTER LANDING, FEATHERED NR 2 PROP. MAINTENANCE INSPECTED, FOUND OI L QUANTITY OK. PERFORMED ENGINE GROUND RUN AND DECELERATION CHECK, NO DEFECTS NOTED. ENGINE OPS CK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A41NM E18NE 2002043000038 20020430 00038 NE 2002 4 30 RAIA00204129 2 20020417 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LEFT FLAMED OUT A RAIA K NONE X ENGINE FLAMEOUT LD LANDING 1 CE 03 562HK 41078 75109 BWI - LEFT ENGINE FLAMED OUT ON LANDING GOING INTO REVERSE. MAINTENANCE INSPECTED AND DETERMINED THAT NR 1 ENGINE FLAME D OUT DURING DECELERATION. ADJUSTED NR 1 ENGINE DECELERATION, OPS CHECK OK. 2 L 7 2 4T 4 T RT A41NM E18NE 2002043000039 20020430 00039 EU 2002 4 30 RAIA00204133 1 20020422 A 2730 PITCH CONTROL AEROSP ATR72 ATR72202 8680940 EU ELEVATOR DISCONNECTED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 721TE 217 STL - ELEVATOR PITCH DISCONNECT DURING TAXI. MAINTENANCE RESET ELEVATOR PITCH DISCONNECT IAW ATR MM 27-31-42. 2 H 7 2 4T RT A53EU 2002043000040 20020430 00040 2002 4 30 SWAA020588 4 20020320 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 608SW 27928 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002043000041 20020430 00041 2002 4 30 SWAA020589 4 20020320 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 608SW 27928 DURING SCHEDULED BC3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002043000042 20020430 00042 NM 2002 4 30 SWAA020590 1 20020319 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 501SW 24178 DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE AT ROW NR 12. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002043000043 20020430 00043 NM 2002 4 30 SWAA020591 1 20020319 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 608SW 27928 DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM CRACKED 2 INCHES LONG AT BS 700. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2002043000044 20020430 00044 NM 2002 4 30 SWAA020593 1 20020320 A 5320 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIPS CRACKED AT BS 400, STR 28L AND STR 28R. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002043000045 20020430 00045 2002 4 30 SWAA020595 4 20020321 A 2565 LANYARD BOEING 737 7373H4 1384600 NM EVAC SLIDE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LANYARD CHAIN BROKEN. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002043000046 20020430 00046 2002 4 30 SWAA020597 4 20020321 A 2565 61620468 CHAIN BOEING 737 7373T5 1384608 NM EVAC SLIDE CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE RELEASE CHAIN CHAFED. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002043000047 20020430 00047 NM 2002 4 30 SWAA020598 1 20020321 A 3350 57771 CAP BOEING 737 7373T5 1384608 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP CRACKED. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2002043000048 20020430 00048 NM 2002 4 30 SWAA020599 1 20020321 A 3350 1013073 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 EEPLS INOP AT ROW NR 3. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2002043000049 20020430 00049 2002 4 30 SWAA020606 4 20020324 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002043000050 20020430 00050 NM 2002 4 30 SWAA020607 1 20020323 A 3350 65C34691 LIGHT BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT LOOSE AT ROW 7 ABC. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002043000051 20020430 00051 2002 4 30 SWAA020609 4 20020323 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002043000052 20020430 00052 2002 4 30 SWAA020610 4 20020322 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002043000053 20020430 00053 NM 2002 4 30 SWAA020611 1 20020322 A 5314 6545866 KEELBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 501SW 24178 DURING SCHEDULED C2 CHECK, FOUND KEEL BEAM CORRODED AT BS 482. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2002043000054 20020430 00054 NM 2002 4 30 SWAA020612 1 20020324 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (3 EA) AT STR 8L, BS 380, 400 AND 500A. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002043000055 20020430 00055 NM 2002 4 30 SWAA020614 1 20020324 A 5320 6517582 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL WEBS CRACKED (2 EA) AT BS 179, WL 227 AND LBL 17.1 AND BS 183, WL 230 AND LB L 17.1. REPAIRED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2002043000056 20020430 00056 NM 2002 4 30 SWAA020620 1 20020323 A 3231 6546205 LINK BOEING 737 7372T4 1384492 NM NLG DOOR BROKEN A SWAA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 130SW 22699 RT NOSE GEAR DOOR CAME OPEN DURING FLT. REMOVED AND REPLACED RT NOSE GEAR DOOR LINK PER MM. 2 L 7 2 4F A16WE 2002043000057 20020430 00057 NM 2002 4 30 SWAA020621 1 20020324 A 2612 33600011 FIRE LOOP BOEING 737 7372H4 138448C NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAULTY A SWAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SW 07 093SW 22965 687784 DECLARED EMERGENCY, IN FLT ENGINE SHUTDOWN, NR 1 ENGINE FIRE WARNING ILLUMINATED DURING DESCENT. DISCHARGED BOTH FIRE B OTTLES, LIGHT WENT OUT. BELL AND LIGHT REMAINED INTERMITTENT. REMOVED AND REPLACED BOTH NR 1 FIRE DETECTION LOOPS AND BOTH FIRE BOTTLES PER MM. 2 L 7 2 4F 4 F A16WE E2GL 2002043000058 20020430 00058 2002 4 30 SWAA020624 4 20020325 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT CABIN DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2 L 7 2 4F A16WE 2002043000059 20020430 00059 NM 2002 4 30 SWAA020625 1 20020325 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 793SA 27888 ONE EEPLS INOP. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002043000060 20020430 00060 2002 4 30 SWAA020628 4 20020322 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002043000061 20020430 00061 NM 2002 4 30 SWAA020872 1 20020423 A 5314 BAC1503 STIFFENER BOEING 737 7375H4 138449D NM LT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663, WL 190 AT LBL 54. REMOVED AND REPLACED STIFFEN ER PER SRM. 2 L 7 2 4F RT A16WE 2002043000062 20020430 00062 NM 2002 4 30 SWAA020873 1 20020422 A 5312 6516300 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AT RBL 9.0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002043000063 20020430 00063 NM 2002 4 30 SWAA020874 1 20020426 A 2731 65C25798 HINGE BOEING 737 7373L9 1384470 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SCHEDULED C2 CHECK, FOUND EXCESSIVE AXIAL PLAY AT RT AND LT ELEVATOR TABS. REMOVED AND REPLACED NR 1 TAB HINGES PER MM. 2 L 7 2 4F RT A16WE 2002043000064 20020430 00064 NM 2002 4 30 SWAA020875 1 20020426 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 367SW 26578 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 190 AT OBL. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002043000065 20020430 00065 NM 2002 4 30 SWAA020876 1 20020424 A 5523 65C2638415M TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED A1 CHECK, FOUND LT ELEVATOR TAB INBD CONTROL ROD ATTACH POINT CRACKED. REMOVED AND REPLACED LT ELEVAT OR TAB PER MM. 2 L 7 2 4F RT A16WE 2002043000066 20020430 00066 NM 2002 4 30 SWAA020877 1 20020425 A 5330 65458197 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED C2 CHECK, FOUND NLG W/W UPPER LT PANEL OPENING CRACKED AT AFT INBD CORNER. MX FERRY TO DAL FOR REPAIR. REPAIRED WEB PER SWA RA AND SWA T1. 2 L 7 2 4F RT A16WE 2002043000067 20020430 00067 2002 4 30 SWAA020878 4 20020426 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 736SA 27868 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002043000068 20020430 00068 NM 2002 4 30 SWAA020879 1 20020427 A 5312 6516300 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 199 AT RBL 7. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002043000069 20020430 00069 NM 2002 4 30 SWAA020880 1 20020427 A 5330 589357 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED 1/2D CHECK, FOUND CAPT'S WINDOW POST SKIN CRACKED AT LOWER RADIUS. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002043000070 20020430 00070 NM 2002 4 30 SWAA020881 1 20020427 A 2731 BACB28AM07 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED PM CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB B USHINGS PER MM. 2 L 7 2 4F RT A16WE 2002050200092 20020502 00092 CE 2002 5 2 00023 1 20020428 A 2740 727423 CIRCUIT BREAKER LEAR 24 24E 5170316 CE COCKPIT WEAK E HAEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 05 330TW 330 PILOT REPORTED NO NORMAL PITCH TRIM AFTER DEPARTURE, USED EMERGENCY PITCH TRIM TO RETURN TO DEPARTURE AIRPORT. MAINTENA NCE FOUND WEAK CIRCUIT BREAKER. REMOVED AND REPLACED CIRCUIT BREAKER, OP'S CHECK GOOD AT THIS TIME. 2 L 7 2 4J A10CE 2002043000072 20020430 00072 NM 2002 4 30 0201345532 1 20020418 A 3260 WARNING SYSTEM BOEING 757 757251 1384970 NM COCKPIT FALSE ACTIVATION A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 532US 24263 AFTER TAKEOFF WHEN RETRACTING GEAR, CREW RECEIVED LEFT MAIN GEAR DISAGREE AND GEAR DOOR MESSAGE. CREW CYCLED GEAR AND S AME INDICATION REMAINED. FLIGHT RETURNED TO DTW AND COMPLETED AN UNEVENTFUL LANDING. DTW MAINTENANCE PERFORMED OPERATI ONAL CHECK PER MM AND COMPLETED 12 NORMAL GEAR SWINGS. MAINTENANCE CALLED AIRCRAFT OK FOR SERVICE. NWA MAINTENANCE CON TROL FOLLOWED UP THIS EVENT WITH LOG TO CHANGE GEAR SEQUENCE VALVE AND THE GEAR DOWNLOCK ACTUATOR AS A PRECAUTIONARY MEA SURE. 2 L 7 2 4F RT A2NM 2002043000073 20020430 00073 EA 2002 4 30 02116631 1 20020426 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 631BR 7261 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTS BETWEEN SEAT ROWS 2 AND 5 WERE INOP ERATIVE. MAINTENANCE PERSONNEL SECURED A LOOSE CONNECTOR IN THE EMERGENCY FLOOR TRACK LIGHTING SYSTEM. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002043000074 20020430 00074 EU 2002 4 30 02118333 1 20020428 A 3397 WIRE JETAIR JETSTM JETSTM4101 1500501 EU CABIN BROKEN A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 333UE 41101 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT AT THE PASSENGER ENTRY DOOR WAS INOPERATIVE . MAINTENANCE PERSONNEL REPAIRED A BROKEN WIRE. AN OPERATIONAL CHECK OF THE EMERGENCY EXIT LIGHTING SYSTEM WAS SATISFA CTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002043000075 20020430 00075 EA 2002 4 30 02119623 1 20020429 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 623BR 7192 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT AFT FUSELAGE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENAN CE PERSONNEL REMOVED AND REPLACED THE LAMP. AN OPERATIONAL CHECK OF THE EMERGENCY EXIT LIGHTING SYSTEM WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002050800054 20020508 00054 WP 2002 5 8 02FDEA00295 1 20020425 A 5230 6300500007 ACTUATOR DOUG DC10 DC1030 3023501 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315 48318 PERFORMED HFEC INSPECTION, FOUND AFT LWR CARGO DOOR ACTUATOR SHAFT SPLINES HAS CRACK IND. REMOVED AND REPLACED ACTUATOR PER 52-33-01-02. 2 L 7 3 4F A22WE 2002050700106 20020507 00106 WP 2002 5 7 02FDEA00296 1 20020425 A 5230 630500007 ACTUATOR DOUG DC10 DC1030 3023501 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315 48318 PERFORMED HFEC INSPECTION FOUND FWD LWR CARGO DOOR ACTUATOR OUTPUT SHAFT SPLINES HAS CRACK INDICATION. REMOVED AND REPL ACED ACTUATOR PER MM 52-31-01. 2 L 7 3 4F A22WE 2002043000076 20020430 00076 NM 2002 4 30 AWXA200200373 1 20020427 A 3350 6104789 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 182AW 22649 LAS - EEL - EXTERIOR OVERWING EMERGENCY LIGHT FOR RT ESCAPE HATCH INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002043000077 20020430 00077 EU 2002 4 30 AWXA200200374 1 20020427 A 3350 ABS0374A24 TERMINAL AIRBUS 320 A320232 3930326 EU CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 655AW 1075 PHX - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT WAS FOUND INOPERATIVE. MAINTENANCE TROUBLESH OT AND FOUND A BROKEN TERMINAL AT SEAT LIGHT ASSEMBLY. REPLACED BROKEN TERMINAL AT SEAT ROW 4 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002043000078 20020430 00078 2002 4 30 AWXA200200378 4 20020423 A 2565 65C1990141 LATCH BOEING 737 7373G7 1384595 NM EVAC SLIDE OUT OF ADJUST A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 158AW 23780 MCN - EMERGENCY EVACUATION - DURING C-16 CHECK THE L2 DOOR EMERGENCY ESCAPE SLIDE LATCH ASSEMBLY FAILED FUNCTIONAL TEST. MAINTENANCE TROUBLESHOT AND FOUND THE EMERGENCY ESCAPE SLIDE LATCH BRACKET OUT OF ADJUSTMENT; ADJUSTED LATCH BRACKET P ER BMM 25-61-35, PG 209. OPERATIONAL CHECK WAS GOOD IAW EO-25-61-23, PG 1, 6, & 15 AND BMM 25-61-35, PG 209. 2 L 7 2 4F RT A16WE 2002043000079 20020430 00079 EU 2002 4 30 AWXA200200379 1 20020428 A 3610 7850027 COMPUTER AIRBUS 320 A320231 3930325 EU PNEUMATIC SYS FAULTY A AWXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 28 629AW 9600 076 EN ROUTE FLT CREW RECEIVED ECAM MESSAGE FOR NR 2 ENG BLEED FAULT TEMP AT 70 C AND 70 PSI; DUE TO ICING CONDITIONS AT IND , ACFT TURNED BACK TO PHX. MX TROUBLESHOT & REPLACED NR 2 BLEED MONITORING COMPUTER, BITE CHECK GOOD, NR 2 ENG PRESSURE TRANSDUCER REPLACED. TWO FLTS EARLY SAME PROBLEM OCCURRED; CFDS PREFLIGHT REPORT DISPLAYED FAILURE MSG 36-11-53 OVPRES S-V 5HA2, SOURCE BMC NR 2, THIS INDICATED NR 2 ENG OVERPRESSURE VALVE WAS BAD. MX REPLACED VALVE & PERFORMED AN ENG RUN OPERATIONAL CHECK, CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002043000080 20020430 00080 NM 2002 4 30 C1HA200285003 1 20020404 A 5320 SUPPORT BOEING 727 7272S7 138407Z NM FUSELAGE CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 685CA 22492 LOWER FLOORBEAM SUPPORT IS CRACKED IN 2 AREAS AT STA 300 AND 320 30 INCHES FROM CENTER LINE UNDER FWD LAV. REMOVED AND REPLACED SPLICE PLATE ON FWD END IAW SRM 51-40-2. 2 L 7 3 4F A3WE 2002043000081 20020430 00081 NM 2002 4 30 C1HA200285004 1 20020405 A 5313 STRINGER BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 685CA 22492 AFT PIT S29L BETWEEN STA 970 & 990 HAS CORROSION. REMOVED CORROSION IAW 727 SRM 51-10-6. INSTALLED REPAIR STRIP IAW EO AAR 0409-02 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2002043000082 20020430 00082 NM 2002 4 30 C1HA200285005 1 20020404 A 5347 SEAT TRACK BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 685CA 22492 SEAT TRACK RBL 24 STA 1100-1130 HAS CORROSION TOP & BOTTOM. SEAT TRACK REPLACED. 2 L 7 3 4F A3WE 2002043000083 20020430 00083 NM 2002 4 30 C1HA200285006 1 20020403 A 5320 SUPPORT BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 685CA 22492 SUPPORT FRAME AT STA 344 15 INCHES FROM CENTER LINE IS CORRODED ON TOP AND BOTTOM. REPAIRED SUPPORT STA 344 IAW EO AAR0 410-02 DOC N PC-02-X106. 2 L 7 3 4F A3WE 2002043000084 20020430 00084 NM 2002 4 30 C1HA200285007 1 20020403 A 5320 FLOOR SUPPORT BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 685CA 22492 AFT LAV RT STA 1130 FLOOR SUPPORT HAS CORROSION RBL 3L. REMOVED DAMAGED CHANNEL IAW 51-30-2. FABRICATED NEW HAT CHANNE L IAW 51-20-1, 51-30-2, 51-10-2. INSTALLED NEW HAT CHANNEL IAW 51-30-2. 2 L 7 3 4F A3WE 2002043000085 20020430 00085 NM 2002 4 30 C1HA200285008 1 20020403 A 2540 LAVATORY BOEING 727 7272S7 138407Z NM CABIN CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 685CA 22492 AFT LAV RT RBL 27-48 HAS CORROSION STA 1150. BLENDED CORROSION IAW SRM 53-10-1, OUT OF LIMITS IAW 51-10-1. FABRICATED REPAIR IAW 51-40-2, 51-10-2, INSTALLED REPAIR IAW SRM 51-30-2, 51-20-4. 2 L 7 3 4F A3WE 2002043000086 20020430 00086 NM 2002 4 30 C1HA200285009 1 20020403 A 5320 CHANNEL BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 685CA 22492 LEFT AFT LAV LBL 30 STA 1128 HAS CORROSION ON METAL STRIP. FABBED NEW CHANNEL IAW SRM 51-30-6, 51-30-8, INSTALLED NEW C HANNEL IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2002043000087 20020430 00087 EU 2002 4 30 C2XA02SH002 1 20020419 A 3397 204 WIRE AEROSP ATR42 ATR42320 8680930 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16824 166 IAH - FLIGHT 3679, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT TWO AISLE PATH EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULBS, AND REPAIRED TWO BROKEN SOLDER JOINTS ON THE LIGHT STRIP WIRING. OPERATIONAL CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002043000088 20020430 00088 NM 2002 4 30 CALA0200244 1 20020426 A 5347 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND RT TIE DOWN RAIL CORRODED ON UPPER SIDE FRONT IN AFT BAGGAGE BIN AT STA 807-840. A NEW TIE DOWN RAIL W AS INSTALLED IAW SRM 53-00-53, PAGE 204-205. 2 L 7 2 4F RT A16WE 2002043000089 20020430 00089 NM 2002 4 30 CALA0200246 1 20020426 A 5711 SPAR BOEING 737 7373T0 1384582 NM LT&RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND THE RT AND LT WING REAR SPARS HAD A 0.050 INCH CRACK INDICATION AT HOLE AT MLG BEAM ATTACH FITTINGS. 2 L 7 2 4F RT A16WE 2002050900065 20020509 00065 NM 2002 5 9 2002UALA00749 1 20020421 A 5712 RIB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 LT WING TRAILING EDGE WBL 445.95 RIB LOWER TEE CHORD 65B08150-99 HAS A CRACK IN THE VERTICAL FLANGE BETWEEN 2 FASTENERS. DAMAGE CAN BE VIEWED FROM OUTBOARD END OF INBOARD FLAPWELL BELOW 65B07818 MIDFLAP DEFLECTOR RAMP. MAJOR REPAIR WAS AC COMPLISHED ON THE LEFT HAND WING TRAILING EDGE RIB LOWER TEE CHORD. 2 L 7 4 4F 4 F RT A20WE E24NE 2002043000090 20020430 00090 NM 2002 4 30 2002UALA00755 1 20020424 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 STATION 740 BEL0W FORWARD PIT FUSE FRAME HAS DAMAGE FROM TELESCOPING LOADER JACKSCREW. MAJOR REPAIR ACCOMPLISHED. INSTA LLED DOUBLER AND STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002043000091 20020430 00091 NM 2002 4 30 2002UALA00761 1 20020425 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 FORWARD PIT STATION 760 BEL0W FUSELAGE FRAME DAMAGED FROM LOADER JACKSCREW. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002043000092 20020430 00092 WP 2002 4 30 CALA0200248 1 20020427 A 3350 60030451 CHARGER DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 938MC 49525 INSPECTION FOUND SECTION OF EMERGENCY LIGHTS NEAR AFT LAV INOPERATIVE. THE CHARGER WAS REPLACED IN AFT LAV IAW CHAPTER 20 AND MM 33-53-00. OPERATIONAL CHECKS WERE GOOD IAW MM 33-53-00. 2 L 7 2 4F RT A6WE 2002043000093 20020430 00093 NM 2002 4 30 CALA0200249 1 20020427 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND UPPER SURFACE OF FUSELAGE KEEL BEAM RIGHT AND LEFT LOWER ANGLES HAD WASHERS WEARING INTO THE ANGLES AT STA 710-727. THE KEEL BEAM ANGLES WERE REPLACED IAW ECRA 5310-03740. 2 L 7 2 4F RT A16WE 2002043000095 20020430 00095 SO 2002 4 30 LR7A02030 1 20020415 A 5320 ATTACH FITTING LKHEED 382 382G 526414U SO FUSELAGE BROKEN A LR7A K NONE J WARNING INDICATION DE DESCENT 1 AL 03 402LC 510 4698 FLIGHT CREW REPORTED MASTER DOOR WARNING LIGHT AND RAMP WARNING LIGHT ON DURING DESCENT INTO ETAR. INVESTIGATION REVEAL ED RT FS 858 SLOPING LONGERON STRUT ATTACH LUG CRACKED AND BROKEN AT RBL 61, WL 190. INSPECTED FOR SECONDARY DAMAGE, NO NE NOTED. AIRCRAFT MAINTENANCE FERRIED UNPRESSURIZED TO ESGC FOR REPAIR. AT EGSC REPLACED FS 858 RT STRUT AND REPAIRED LONGERON LUG IAW SRM SMP 583 53-50-26. 2 H 7 4 4T A1SO 2002043000096 20020430 00096 WP 2002 4 30 MWEA020275 1 20020426 A 3350 BR9279109 SIGN DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 808ME 48070 AFT CABIN DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED AFT CABIN DOOR EMERGENCY EXIT SIGN IAW MM 33-53-01. 2 L 7 2 4F A6WE 2002043000097 20020430 00097 WP 2002 4 30 MWEA020276 1 20020426 A 5320 991015117 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 CUSP BETWEEN STATION 864 AND 886, RIGHT SIDE IS DENTED. FABRICATED AND INSTALLED CUSP. 2 L 7 2 4F A6WE 2002043000098 20020430 00098 WP 2002 4 30 MWEA020278 1 20020426 A 5320 995821268 STIFFENER DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 STIFFENER IN RIGHT MAIN LANDING GEAR WELL IS CHAFED, LOCATED IN MIDDLE OF AFT WALL. FABRICATED AND INSTALLED STIFFENER. 2 L 7 2 4F A6WE 2002043000099 20020430 00099 WP 2002 4 30 MWEA020279 1 20020426 A 5230 59101419 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FORWARD CARGO DOOR, INNER PAN HAS A CRACK ON FORWARD END AT HOLD OPEN LATCH GUIDE. FABRICATED AND INSTALLED PAN REPAIR. 2 L 7 2 4F A6WE 2002043000100 20020430 00100 WP 2002 4 30 MWEA020280 1 20020426 A 5220 5912995504 DOOR FRAME DOUG DC9 DC982 3022082 WP EXIT DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 RIGHT AFT OVERWING EXIT DOOR JAMB HAS SOME GOUGES AT TOP DOOR LATCH AREA. REMOVED UPPER SEAL DEPRESSOR, TRIMMED, AND RE INSTALLED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002043000101 20020430 00101 WP 2002 4 30 MWEA020282 1 20020226 A 5321 995791921 FLOORBOARD DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 CABIN FLOORBOARD B-8 HAS DAMAGE TO THE FORWARD EDGE. FABRICATED AND INSTALLED SKIN AND HAT CHANNELS. 2 L 7 2 4F A6WE 2002043000102 20020430 00102 WP 2002 4 30 MWEA020285 1 20020426 A 5312 9958212269 PRESSURE PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 RIGHT MAIN LANDING WELL AFT WALL IS CHAFED MIDWAY UP AND MIDWAY ACROSS WALL. FABRICATED AND INSTALLED REPAIR DOUBLER AN D FILLER. 2 L 7 2 4F A6WE 2002043000103 20020430 00103 WP 2002 4 30 MWEA020290 1 20020425 A 5210 ARM DOUG DC9 DC914 3022034 WP PAX DOOR FAILED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 PASSENGER DOOR HAS STRUCTURAL DAMAGE (CRACK) TO INTERCOSTAL LOCATED WHERE CRANK ARM PASSES THROUGH. DAMAGED CAUSED BY C RANK ARM FAILURE. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F A6WE 2002043000104 20020430 00104 WP 2002 4 30 MWEA020293 1 20020413 A 5753 995800011 SPAR DOUG DC9 DC932 3022066 WP T/E FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LEFT WING FLAP TRAILING EDGE SPAR WEB HAS A SMALL CRACK ORIGINATING FROM FASTENER HOLE AT STATION. CUT AND REMOVED DAMA GED WEB AREA AND REMOVED REMAINING PORTION OF DOUBLER. LOCATED, DRILLED AND DEBURRED DOUBLER AND INSTALLED. 2 L 7 2 4F A6WE 2002043000105 20020430 00105 WP 2002 4 30 MWEA020295 1 20020411 A 5330 59197073 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 REPLACE AFT CARGO PIT BELLY SKIN SECTION LONGERON 28 LEFT TO 28 RIGHT STATION 803 THROUGH 996 TO COMPLY WITH CARRY OVER NR 2201. REMOVED AND REPLACED SKIN. 2 L 7 2 4F A6WE 2002043000106 20020430 00106 WP 2002 4 30 MWEA020296 1 20020411 A 5320 49209341 SUPPORT BRACKET DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FORWARD PIT LEFT AUX TANK STRUT UPPER SUPPORT BRACKET HAS EXFOLIATION AROUND A FASTENER STATION 545 LONGERON 24 LEFT. R EMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 2002043000107 20020430 00107 2002 4 30 MWEA020298 4 20020428 A 3160 4055900906 SYMBOL GENERATOR DOUG DC9 DC981 3022081 WP COCKPIT FAILED A MWEA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 812ME 48006 THE FIRST OFFICER'S PRIMARY FLIGHT DISPLAY WENT BLANK. RESET CIRCUIT BREAKER FOR SYMBOL GENERATOR NR 2 (WITH MX DIRECTI ON). PROBLEM REMAINED. REMOVED AND REPLACED NR 2 SYMBOL GENERATOR. SYSTEM OPERATIONAL CHECK OK. REF MD80 MM CHAPTER 34. 2 L 7 2 4F A6WE 2002043000108 20020430 00108 NM 2002 4 30 PCAA0204051 1 20020428 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DISCONNECTED A PCAA K NONE L NO TEST NR NOT REPORTED 1 EA 13 820EX 019 PHL- FLIGHT 3657 CREW REPORTED EMERGENCY FLOOR LIGHTING AFT SECTION LEFT SIDE AISLE INOPERATIVE AND WIRING LOOSE. MAINT ENANCE RE-ATTACHED LEFT AFT SIDE EMERGENCY LIGHT PLUG. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002043000109 20020430 00109 NM 2002 4 30 SWAA020634 1 20020325 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) AT BS 277 AND STR 11L, BS 360 AND STR 8R, BS 400 AND STR 1 , BS 500C AND STR 16R. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002043000110 20020430 00110 NE 2002 4 30 SWAA020635 2 20020325 A 7200 JT8D9AHK ENGINE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9 52048 NE NR 1 FLAMED OUT A SWAA B EMER. DESCENT X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 07 090SW 22905 687858 INFLIGHT SHUT DOWN, DECLARED EMERGENCY, NR 1 ENGINE FLAMED OUT DURING CLIMB, NO N2 INDICATION. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2002043000111 20020430 00111 2002 4 30 SWAA020638 4 20020326 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 629SW 27704 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002043000112 20020430 00112 NM 2002 4 30 SWAA020639 1 20020324 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002043000113 20020430 00113 NM 2002 4 30 SWAA020640 1 20020326 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, WL 208 AND LBL 25.5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2002043000114 20020430 00114 NM 2002 4 30 SWAA020644 1 20020327 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 717SA 27851 EEPLS LOOSE. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002043000115 20020430 00115 NM 2002 4 30 SWAA020648 1 20020327 A 5311 96380 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OUTBOARD BULKHEAD CHORDS CRACKED AT BS 178, WL 207. REMOVED AND RE PLACED CHORDS PER SWA ACO. 2 L 7 2 4F RT A16WE 2002043000116 20020430 00116 NM 2002 4 30 SWAA020649 1 20020325 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED STR CLIP PER MM. 2 L 7 2 4F RT A16WE 2002043000117 20020430 00117 NM 2002 4 30 SWAA020652 1 20020327 A 2910 280205 FUSE BOEING 737 7377AD NM HYD SYSTEM DEFECTIVE A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 798SW 28436 AIR TURNBACK, DURING CLIMB L/E DEVICES WOULD NOT RETRACT. UPON LANDING DEVICES WOULD NOT FULLY EXTEND. REMOVED AND REP LACED EXTEND AND RETRACT HYD FUSES PER MM. 2 L 7 2 4F RT A16WE 2002043000118 20020430 00118 2002 4 30 SWAA020653 4 20020327 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 398SW 27692 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002043000119 20020430 00119 2002 4 30 SWAA020655 4 20020327 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT CABIN DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED C2 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2 L 7 2 4F A16WE 2002043000120 20020430 00120 NM 2002 4 30 SWAA020659 1 20020329 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 EEPLS LOOSE BETWEEN ROW 15 AND 16. SECURED EEPLS PER MM. 2 L 7 2 4F A16WE 2002043000121 20020430 00121 NM 2002 4 30 SWAA020662 1 20020330 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 500A, STR 10R AND BS 500D, STR 8R. REMOVED AND REPL ACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002043000122 20020430 00122 NM 2002 4 30 SWAA020665 1 20020330 A 5320 694036723 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138, STR 13L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002043000123 20020430 00123 NM 2002 4 30 SWAA020666 1 20020330 A 5311 96380 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/2D CHECK, FOUND RT OUTBOARD SIDE CHORD CRACKED AT BS 178, WL 207 AND RBL 26. REMOVED AND REPLACED CH ORD PER SRM. 2 L 7 2 4F RT A16WE 2002043000124 20020430 00124 NM 2002 4 30 SWAA020674 1 20020331 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 4R, BS 727B AND 727C. REMOVED AND REPLACED STR CLI PS PER SRM. 2 L 7 2 4F RT A16WE 2002043000125 20020430 00125 NM 2002 4 30 SWAA020675 1 20020331 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 500C, STR 10R AND BS 700, STR 3R. REMOVED AND REPLA CED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002043000126 20020430 00126 NM 2002 4 30 SWAA020687 1 20020331 A 7720 D3302 CONNECTOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 374SW 26582 723135 AIR TURNBACK, DURING CLIMB NR 2 ENGINE EGT WENT TO 1250 AND OVER TEMP LIGHT ILLUMINATED. REMOVED AND REPLACED ELECT DIS CONNECT D3302 PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002043000127 20020430 00127 NM 2002 4 30 SWAA020688 1 20020330 A 2782 65445519 ACTUATOR BOEING 737 7373H4 1384600 NM L/E FLAP FAILED A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 07 396SW 27690 DIVERSION, AT FL 350 L/E FLAP TRANSIT LIGHT ILLUMINATED, NR 2 L/E FLAP LIGHT ON OVERHEAD ILLUMINATED. REMOVED AND REPLA CED NR 2 L/E FLAP ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2002043000128 20020430 00128 NM 2002 4 30 SWAA020689 1 20020331 A 2433 0802032501 TRU BOEING 737 7373Y0 1384671 NM COCKPIT MALFUNCTIONED A SWAA B A EMER. DESCENT UNSCHED LANDING M B J OVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 07 664WN 23495 DECLARED EMERGENCY, DIVERSION, NR 2 TRANSFORMER RECTIFIER UNIT CB POPPED, FUMES IN CABIN AND FLT DECK, USED FLT DECK 02. REMOVED AND REPLACED TRANSFORMER RECTIFIER UNIT PER MM. 2 L 7 2 4F RT A16WE 2002043000129 20020430 00129 NM 2002 4 30 SWAA020690 1 20020329 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 EEPLS LOOSE. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002043000130 20020430 00130 NM 2002 4 30 DHL2002726506 1 20020418 A 5410 NA COWLING BOEING 727 727228 1384083 NM CRACKED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 During C Check "discrepancy" as follows, #3 engine upper cowling gouged/chaffed on the #12 rib O/B section.Corrective ac tion as follows,Cut-out damaged area on #3 engine cowl upper #12 rib I.A.W. B-727 SRM 54-10-2. Fabricated repair from 70 75-T6 .050 P.O.# 9911388 size 2 3/8" X 6" I.A.W. B-727 SRM 54-10-3. Alodined and primed part I.A.W. B-727- SRM 51-10-2. Installed doubler angle I.A.W. B-727 SRM 51-30-2.1) Clean area #3 engine upper cowl on the #12 rib out of limits I.A.W. B-727 SRM 51-10-6, cut .005 area damage. Dim. 5/8" X 1/4" I.A.W. B-727 SRM 51-40-3 and 54-10-2 fig. #2.2) Fabricated rep air angle Mat. 7075-T6 .050 P.O.# 9911388 size 2 3/8" X 6" I.A.W. B-727 SRM 54-10-3.3) Alodined and primed 2 L 7 3 4F RT A3WE 2002043000131 20020430 00131 EA 2002 4 30 COMA0260285 1 20020426 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 978CA 7158 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.COULD NOT DUPLICATE. OPERATIONAL CHECK OF DOOR AND WARNING SYSTEM WAS SATISFACTO RY. 2 L 7 2 4F RT A21EA 2002043000132 20020430 00132 EA 2002 4 30 COMA0260286 1 20020428 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 956CA 7105 FLAPS FAILED AT 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002043000133 20020430 00133 EA 2002 4 30 COMA0260289 1 20020428 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 915CA 7013 FLAPS FAIL MESSAGE AFTER LANDING.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002043000134 20020430 00134 NM 2002 4 30 AWXA200200381 1 20020422 A 5330 6518420 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 0 0 23780 MCN - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON THE CAPTAINS WINDSHIELD OUTBOARD FRAME UPPER CORNER, CONFIRM ED BY HFEC INSPECTION. MAINTENANCE CUTOUT THE CRACK AT CAPTIANS WINDSHIELD OUTBOARD FRAME UPPER CORNER AND CRACKED SECTI ON OF GUSSET, PERFORMED HFEC INSPECTION TO VERIFY THE CRACKS WERE CONTAINED. FABRICATED A REPAIR DOUBLER AND FILLER, AN D INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01, PG. 231-234. PART NAME; GUSSET, MFG; BOEING, P/N; 65-55074, COND; CR ACKED, LENGTH; 0.750, LOC; SAME AS SKIN. 2 L 7 2 4F RT A16WE 2002043000135 20020430 00135 NM 2002 4 30 SWAA020699 1 20020401 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT STR 10R, BS 500 AND 500B. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002043000136 20020430 00136 NM 2002 4 30 CALA0200250 1 20020429 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 380 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND A 1/2" CRACK IN FUSELAGE SKIN AT TWO SCREW HOLES AFT OF C/L OF AIRCRAFT STA 380. A DOUBLER WAS INSTALLE D IAW ECRA 5330-02849. 2 L 7 2 4F RT A16WE 2002043000137 20020430 00137 NM 2002 4 30 CALA0200254 1 20020429 A 5414 SKIN BOEING 737 7373T0 1384582 NM #2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND A 1/2" CRACK IN #2 ENGINE UPPER PYLON SKIN AT ACCESS PANEL 5827R. THE CRACK WAS STOP DRILLED AND A DOUB LER WAS INSTALLED IAW ECRA 5430-01230. 2 L 7 2 4F RT A16WE 2002050100021 20020501 00021 NM 2002 5 1 SWAA020692 1 20020401 A 3350 AD20131A BATTERY BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED RON, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002050100022 20020501 00022 NM 2002 5 1 SWAA020693 1 20020401 A 5320 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 578, STR 10L. REMOVED AND REPLACED TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002050100023 20020501 00023 NM 2002 5 1 SWAA020700 1 20020401 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002050600135 20020506 00135 NM 2002 5 6 DHL2002726511 1 20020417 A 5312 PRESSURE PANEL BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, NOSE WHEEL WELL L/SIDE WALL PANEL CRACKED BS 280 AND UPPER CHORD ANGLE SEEN FROM INSIDE (NDT VERIFIED). FABRICATED AND INSTALLED REPAIR PARTS IAW B-727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002050100024 20020501 00024 NM 2002 5 1 SWAA020701 1 20020401 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED STR TIE CLIP PER SRM . 2 L 7 2 4F RT A16WE 2002050100025 20020501 00025 NM 2002 5 1 SWAA020702 1 20020401 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 500D, STR 19R. REMOVED AND REPLACED STR TIE CLIP PER SR M. 2 L 7 2 4F RT A16WE 2002050100026 20020501 00026 NM 2002 5 1 SWAA020703 1 20020401 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASS Y PER MM. 2 L 7 2 4F A16WE 2002050100027 20020501 00027 2002 5 1 SWAA020704 4 20020402 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002050100028 20020501 00028 NM 2002 5 1 SWAA020710 1 20020402 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (5 EA) AT BS 500D AT STR 4L, BS 616 AT STR 5R, BS 663 AT STR 10L, BS 639 AT STR 4L, BS 907 AT STR 8L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002050100029 20020501 00029 NM 2002 5 1 SWAA020711 1 20020402 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002050100030 20020501 00030 NM 2002 5 1 SWAA020715 1 20020402 A 5240 6545871523 DOOR FRAME BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT AFT LOWER STOP CUTOUT. REMOVED AND REPLACED DOOR PER MM. 2 L 7 2 4F RT A16WE 2002050100031 20020501 00031 NM 2002 5 1 SWAA020719 1 20020403 A 3397 WIRE BOEING 737 7373H4 1384600 NM COCKPIT BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D-CHECK, FOUND COCKPIT EMERGENCY FLOOD LIGHT INOP. REPAIRED BROKEN WIRE PER MM. 2 L 7 2 4F RT A16WE 2002050100032 20020501 00032 NM 2002 5 1 SWAA020720 1 20020404 A 2560 P2070001 FLASHLIGHT BOEING 737 737317 138447P NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 698SW 23176 EMERGENCY FLASHLIGHT INOP IN AFT CABIN TOP POSITION. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2002050100033 20020501 00033 NM 2002 5 1 SWAA020721 1 20020403 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002050100034 20020501 00034 NM 2002 5 1 SWAA020723 1 20020403 A 3240 715775 VALVE BOEING 737 7372H4 138448C NM LT MLG ERRATIC A SWAA K NONE O OTHER LD LANDING 1 SW 07 074SW 22674 INTERMITTENT BRAKE ACTION LT SIDE ON TOUCHDOWN AND TAXI, LT BRAKES ENGAGE AND RELEASE WITH ASSOCIATED A/C PULL. REMOVED AND REPLACED NR 1 AND NR 2 BRAKE HYD DISCONNECT VALVES AND REMOVED AND REPLACED NR 1 AND NR 2 MLG BRAKE ASSY'S PER MM. 2 L 7 2 4F A16WE 2002050100035 20020501 00035 2002 5 1 SWAA020728 4 20020406 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002050100036 20020501 00036 NM 2002 5 1 SWAA020729 1 20020405 A 5311 96380 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 612SW 27930 DURING SCHEDULED SPECIAL VISIT, FOUND LT OUTBOARD CHORD CRACKED AT BS 178, WL 207 AT LBL 26.0. REMOVED AND REPLACED CHO RD PER SRM. 2 L 7 2 4F RT A16WE 2002050100037 20020501 00037 NM 2002 5 1 SWAA020730 1 20020407 A 5553 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED D-CHECK, FOUND VERTICAL FIN REAR SPAR LT AND RT CLEVIS LUGS CORRODED. REPAIRED LUGS AND INSTALLED BUSH INGS PER BFG ER. 2 L 7 2 4F RT A16WE 2002050100038 20020501 00038 2002 5 1 SWAA020732 4 20020405 A 3418 861CAS3 SENSOR BOEING 737 7373H4 1384600 NM AOA BROKEN A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 610WN 27696 AIR TURNBACK, DURING ROTATION AT ABOUT 10 DEGREES NOSE UP BOTH STICK SHAKERS ACTIVATED, A/C FLEW NORMAL. FOUND AOA SENS OR BROKEN. REMOVED AND REPLACED AOA SENSOR PER MM. 2 L 7 2 4F RT A16WE 2002050100039 20020501 00039 NM 2002 5 1 SWAA020735 1 20020406 A 2730 65C2546518 FEEL UNIT BOEING 737 7375H4 138449D NM ELEVATOR FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 510SW 24187 ELEVATOR FEEL FORCE IS LOW, IT TAKES MUCH LESS FORCE THAN NORMAL TO ROTATE OR FLARE THE A/C. REMOVED AND REPLACED ELEVA TOR FEEL AND CENTERING UNIT PER MM. 2 L 7 2 4F RT A16WE 2002050100040 20020501 00040 NM 2002 5 1 SWAA020736 1 20020407 A 3350 6104789 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002050100041 20020501 00041 NM 2002 5 1 SWAA020737 1 20020408 A 3350 7003661 BALLAST BOEING 737 7377H4 1384404 NM CABIN DEFECTIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 785SW 30602 DURING SCHEDULED A2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM. 2 L 7 2 4F RT A16WE 2002050100042 20020501 00042 2002 5 1 SWAA020738 4 20020406 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 645SW 28330 DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLID E PER MM. 2 L 7 2 4F RT A16WE 2002050100043 20020501 00043 NM 2002 5 1 SWAA020749 1 20020409 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT ASSY DAMAGED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002050100044 20020501 00044 2002 5 1 SWAA020750 4 20020408 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002050100045 20020501 00045 NM 2002 5 1 SWAA020752 1 20020408 A 3350 BCREF4146 LIGHT BOEING 737 7373Y0 1384671 NM COCKPIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT NOT ARMED LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002050100046 20020501 00046 NM 2002 5 1 SWAA020754 1 20020409 A 5311 96380 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 605SW 27956 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OUTBOARD CHORDS CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CH ORDS PER SWA ACO. 2 L 7 2 4F RT A16WE 2002050100047 20020501 00047 NM 2002 5 1 SWAA020757 1 20020409 A 3350 57771 CAP BOEING 737 7373L9 1384470 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS END CAP LOOSE AT AFT CABIN. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 2002050100048 20020501 00048 2002 5 1 SWAA020760 4 20020410 A 2565 D31354418 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 367SW 26578 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002050100049 20020501 00049 NM 2002 5 1 SWAA020762 1 20020410 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 908, STR 4R AND 10R. REMOVED AND REPLACED S TR SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2002050100050 20020501 00050 NM 2002 5 1 SWAA020765 1 20020411 A 3350 6104789 BATTERY BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BAT TERY PER MM. 2 L 7 2 4F RT A16WE 2002050100051 20020501 00051 NM 2002 5 1 SWAA020766 1 20020411 A 3350 6042221 BATTERY BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS (2 EA) AFT CABIN INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002050100052 20020501 00052 NM 2002 5 1 SWAA020767 1 20020411 A 3350 100885 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 395SW 27689 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS INOP AT ROW NR 22 AND AFT. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002050100053 20020501 00053 2002 5 1 SWAA020769 4 20020411 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 652SW 27722 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002050100054 20020501 00054 NM 2002 5 1 SWAA020770 1 20020411 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 614SW 28033 OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW NR 20 DEF. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002050100055 20020501 00055 NM 2002 5 1 SWAA020773 1 20020411 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4R. REMOVED AND REPLACED STR SPLICE PER SR M. 2 L 7 2 4F RT A16WE 2002050100056 20020501 00056 2002 5 1 SWAA020776 4 20020412 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 622SW 27932 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002050100057 20020501 00057 2002 5 1 SWAA020778 4 20020412 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002050100058 20020501 00058 NM 2002 5 1 SWAA020779 1 20020412 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002050100059 20020501 00059 NM 2002 5 1 SWAA020781 1 20020413 A 3350 6104789 BATTERY BOEING 737 7372T4 1384492 NM CARGO BAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AT RT FWD OF AFT CARGO DOOR. REMOVED AND REPLA CED BATTERY PER MM. 2 L 7 2 4F A16WE 2002050100060 20020501 00060 NM 2002 5 1 SWAA020783 1 20020413 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2002050100061 20020501 00061 NM 2002 5 1 SWAA020785 1 20020412 A 5730 6573720 SKIN BOEING 737 7372H4 138448C NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED 1/4D CHECK, FOUND RT WING UPPER SURFACE CRACKED ABOVE REAR SPAR AT WS 237. REPAIRED WING UPPER SURFACE PER SRM AND SWA T1. 2 L 7 2 4F A16WE 2002050100062 20020501 00062 NM 2002 5 1 SWAA020789 1 20020414 A 2130 327375 CHECK VALVE BOEING 737 7373H4 1384600 NM E/E BAY FAILED A SWAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SW 07 333SW 23697 AIR TURNBACK, NO PRESSURIZATION AFTER TAKEOFF, CONFIGURED FOR SINGLE PACK OPS. REMOVED AND REPLACED AFT CARGO DOOR SEAL AND REMOVED AND REPLACED EQUIP COOLING PRESSURIZATION CHECK VALVE PER MM. 2 L 7 2 4F RT A16WE 2002050100063 20020501 00063 NM 2002 5 1 SWAA020790 1 20020413 A 3230 M986 PRINTED CKT BOAR BOEING 737 7373H4 1384600 NM E/E BAY FAULTY A SWAA K NONE N FALSE WARNING CL CLIMB 1 SW 07 321SW 23342 SELECTED GEAR TO UP POSITION, POSITION LIGHTS WENT OUT, SELECTED GEAR TO OFF POSITION, MLG LT AND RT LIGHTS WERE BOTH RE D AND GREEN. TRIED AGAIN WITH SAME RESULTS, ON THIRD TRY ALL INDICATIONS NORMAL. REMOVED AND REPLACED LANDING GEAR PRI NTED CIRCUIT CARD PER MM. 2 L 7 2 4F RT A16WE 2002050100064 20020501 00064 NM 2002 5 1 SWAA020793 1 20020415 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 501SW 24178 EEPLS BROKEN AT MID CABIN. REMOVED AND REPLACED EEPLS SECTION PER MM. 2 L 7 2 4F RT A16WE 2002050100065 20020501 00065 NM 2002 5 1 SWAA020795 1 20020413 A 5753 6546435335 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED C3 CHECK, FOUND LT T/E OUTBOARD AFT FLAP DELAMINATED NEAR OUTBOARD END, UPPER AND LOWER SURFACES. REMO VED AND REPLACED T/E OUTBOARD AFT FLAP PER MM, ROUTED FLAP TO SHOP FOR REPAIR. REPAIRED FLAP PER SWA RA. 2 L 7 2 4F RT A16WE 2002050100067 20020501 00067 2002 5 1 SWIA200210768 4 20020331 A 2210 AUTOPILOT SYS EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 218SW 120287 JUST AFTER ROTATION, TRIPLE CHIME AUTOPILOT WITH ASSOCIATED AUTOPILOT FAIL RED MAP INDICATION AND TRIPLE CHIME TRIM FAIL WITH ASSOCIATED TRIM FAIL MAP LIGHT. RAN QRH, RETURNED TO PSP. COMMAND BARS ON CAPTAIN'S SIDE STUCK 15 DEGREES DOWN A ND 30 DEGREES RIGHT. OPS CHECK GOOD AT THIS TIME. COULD NOT DUPLICATE AUTOPILOT PROBLEM. 2 L 7 2 4T RT A31SO 2002050100068 20020501 00068 SO 2002 5 1 SWIA200210769 1 20020402 A 2740 PROXIMITY SENSOR EMB 120 EMB120RT 3260202 SO HORIZ STAB FAULTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 1117H 120117 THE TAKEOFF TRIM AURAL WARNING SOUNDED ON TAKEOFF ROLL, TRIM WAS SET WELL WITHIN THE GREEN BAND. ABORTED TAKEOFF. REPL ACED LEFT HORIZONTAL TRIM PROXIMITY SENSOR AND REPAIRED GROUND WIRE FOR PROXIMITY SENSORS. TRIM WARNING OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002050100070 20020501 00070 NE 2002 5 1 SWIA200210770 2 20020402 A 7261 OIL SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE LOW A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 298SW 120328 AFTER TAKEOFF, AT ABOUT 1500 AGL, THE LEFT ENGINE OIL AURAL WARNING CAME ON. CONCURRENTLY HEARD RCCB'S CLICKING AND THE OIL NEEDLE FLUCTUATED. RETURNED TO DEN. ADDED 4 QUARTS OF OIL AND COMPLIED WITH ST72-344. NO DEFECTS NOTED. LEAK CH ECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002050100081 20020501 00081 SO 2002 5 1 SWIA200210771 1 20020408 A 3241 CONNECTOR EMB 120 EMB120ER 3260203 SO ANTISKID SYS DIRTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 251YV 120251 ANTISKID INOP MESSAGE ON LEFT SIDE ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF. CLEANED CANNON PLUGS AT ANTISKID HARNESS AND SWAPPED RIGHT SIDE TRANSDUCERS INBOARD TO OUTBOARD TRANSDUCERS. GROUND OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002050100082 20020501 00082 EA 2002 5 1 SWIA200210773 1 20020406 A 2913 PV304448 PUMP CNDAIR CL600 CL6002B19 1900309 EA NR 2 ENGINE FAILED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 423SW 6107 1964 7456 NR 2 HYDRAULIC ENGINE DRIVEN PUMP INOP. AT FL 350 RECEIVED RT ENGINE LOW OIL PRESSURE WARNING. OIL PRESSURE WENT 15-25 PSI, THE OIL TEMP WAS NORMAL. ELECTED TO SHUT RIGHT ENGINE DOWN INFLIGHT. DIVERTED TO CDC. REMOVED HYDRAULIC PUMP PL UG AND INSTALLED HYDRAULIC PUMP WITH SERVICEABLE UNIT IAW MM 29-11-01. RAN ENGINE RIGHT SIDE FOR OPS AND LEAK CHECK. S ERVICED ENGINE OIL. CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002050100083 20020501 00083 NE 2002 5 1 SWIA200210774 2 20020405 A 7314 PUMP EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A SWIA O OTHER O OTHER TO TAKEOFF 1 NM 07 268UE 120207 RIGHT ENGINE SLUGGISH IN ACCELERATION. T6 WAS ABOUT 820 DEGREES USING TORQUE SETTINGS SUPPLIED ON THE RELEASE. REMOVED AND REPLACED RIGHT ENGINE FUEL PUMP AND HMU IAW MM 73-21-00. RUN CHECKS AND LEAK CHECKS GOOD. HMU: P/N: 786390-10, S/N OFF: F1829. 2 L 7 2 4T 4 T RT A31SO E20NE 2002050100084 20020501 00084 SO 2002 5 1 SWIA200210775 1 20020404 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA A UNSCHED LANDING K F J FLUID LOSS FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 291SW 120318 UPON FLAP EXTENSION TO 15 DEGREES ON APPROACH TO OXR, BLUE SYSTEM HYDRAULIC FAILURE OCCURRED. FOLLOWED QRH. RETURNED T O LAX. REPLACED RIGHT NACELLE FLAP ACTUATOR PER MM 27-50-00. REPLACED RIGHT ENGINE HYDRAULIC PUMP. RUNUP AND OPS CHEC K AND LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2002050100085 20020501 00085 SO 2002 5 1 SWIA200210776 1 20020405 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 294SW 4767 4767 120321 FRONT HALF OF EMERGENCY LIGHTS ON FLOOR AND CEILING WILL NOT TEST OR TURN ON. REPLACED FORWARD EMERGENCY EXIT LIGHT BAT TERY PACK. 2 L 7 2 4T RT A31SO 2002050100086 20020501 00086 SO 2002 5 1 SWIA200210777 1 20020403 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 271YV 120271 DURING TAKEOFF ROLL, RECEIVED A HIGH SPEED TRIPLE CHIME AND AURAL WARNING. ABORTED TAKEOFF. CYCLED CIRCUIT BREAKER. G ROUND OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002050100087 20020501 00087 SO 2002 5 1 SWIA200210778 1 20020404 A 5230 DOOR SEAL EMB 120 EMB120ER 3260203 SO CARGO DOOR LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 562SW 120336 ON CLIMBOUT LOST CABIN PRESSURIZATION FOR ABOUT 1 MINUTE, THEN THE SYSTEM BEGAN WORKING NORMALLY AGAIN IN MANUAL AND AUT O MODE. RETURNED TO LAX. SECURED CARGO DOOR SEAL. PRESSURIZED AIRCRAFT TO 7 PSID. OPS CHECK GOOD. NO DISCREPANCIES NOTED. 2 L 7 2 4T RT A31SO 2002050100088 20020501 00088 SO 2002 5 1 SWIA200210779 1 20020324 A 5210 FRAME EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 217SW 120286 INTERGRANULAR CORROSION FOUND IN FORWARD TOP INTERNAL AREA ACCESS HOLE ON PASSENGER DOOR. REMOVED AND REPLACED THE CORR ODED FRAME IAW EMB SRM 51-40-02 AND 51-00-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2002050100089 20020501 00089 SO 2002 5 1 SWIA200210781 1 20020408 A 6123 RELAY EMB 120 EMB120ER 3260203 SO AUTOFEATHER SYS FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 268UE 120207 ON THE TAKEOFF ROLL, RECEIVED A TAKEOFF AUTO FEATHER WARNING WITH THE AUTO FEATHER SWITCH IN THE ON POSITION (IT HAD TES TED NORMALLY ON TAXI OUT). TAKEOFF WAS ABORTED AND AUTO FEATHER SYSTEM WAS TESTED AGAIN ON TAXI BACK. TESTED NORMALLY AGAIN. ON SECOND TAKEOFF ATTEMPT, DID A STATIC TAKEOFF AND AGAIN GOT AN AURAL WARNING. THERE WAS NO AUTO FEATHER ARMED LIGHT WITH TAKEOFF POWER LEVERS FORWARD. REPLACED SWITCH S023 AND RELAY K0161. RAN AIRCRAFT AUTO FEATHER SYSTEM, TEST AND ARMS GOOD. 2 L 7 2 4T RT A31SO 2002050100090 20020501 00090 SO 2002 5 1 SWIA200210782 1 20020405 A 7714 SEDLOC29M INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 295SW 5297 5297 120322 NR 1 ENGINE NH GAUGE (ANALOG & DIGITAL), INOP DURING FLIGHT. NL WAS OK. RETURNED TO PDX. LEFT ANALOG AND DIGITAL PORT ION OF NH GAUGE READ EITHER -0- OR ERRATIC. NL WORKS FINE. REPLACED WIRE HARNESS 3115911-01 ON LEFT ENGINE. RAN ENGIN ES FOR OPS CHECK. OPS CHECK GOOD PER MM 77-00-00. REMOVED AND REPLACED LEFT NH/NL INDICATOR IAW M/M 77-00-00. RAN EN GINES AT HIGH POWER SETTINGS FOR 15 MINUTES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002050100091 20020501 00091 EA 2002 5 1 SWIA200210783 1 20020415 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FALSE ACTIVATION A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 587SW 7062 AT APPROXIMATELY 10,000 FEET, THE PASSENGER DOOR MESSAGE CAME ON. PERFORMED QRH PROCEDURES AND RETURNED TO SLC. PRESSU RIZED AIRCRAFT TO 4.0 DELTA P. FOUND DOOR INDICATOR TO FUNCTION NORMALLY. CHECKED FAULTS IN PSEU. CLEARED FAULTS. CY CLED PASSENGER DOOR SEVERAL TIMES. NO FAULTS NOTED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002050100097 20020501 00097 SO 2002 5 1 SWIA200210784 1 20020413 A 2752 3082001007 ACTUATOR EMB 120 EMB120RT 3260202 SO T/E FLAP LEAKING A SWIA A UNSCHED LANDING K F J FLUID LOSS FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 1110J 3223 1107 120110 TEN MINUTES AFTER TAKEOFF, THE RIGHT SIDE HYDRAULIC RESERVOIR LOW LEVEL LIGHT ILLUMINATED, FOLLOWED SHORTLY BY THE RIGHT SIDE MAIN PUMP LOW PRESSURE LIGHT. RETURNED TO LAX AFTER COMPLETING QRH PROCEDURES. RIGHT HYDRAULIC PUMP OUT OF FLUID APPROX 15 MINUTES. INSTALLED SERVICEABLE LEFT HYDRAULIC FLAP ACTUATOR IAW EMB MM 27-50-00. INSTALLED NEW HYDRAULIC PU MP. RAN ENGINE, NO LEAKS NOTED. CYCLED FLAPS, OPS CHECK GOOD. CHECKED ACTUATOR, NO LEAKS NOTED. ALL OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002050100101 20020501 00101 SO 2002 5 1 SWIA200210785 1 20020414 A 3010 38E966A RELIEF VALVE EMB 120 EMB120ER 3260203 SO LEFT MALFUNCTIONED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 296SW 9990 9990 120325 ON CLIMBOUT, DUCT LEAK LIGHT ILLUMINATED AND WOULD NOT GO OUT. ENGINE SHUT DOWN. RETURNED TO PDX. REMOVED AND REPLACE D LEFT BLEED PRESSURE RELIEF VALVE IAW MM 30-10-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002050100102 20020501 00102 SO 2002 5 1 SWIA200210786 1 20020411 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PAX DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 NM 07 232SW 120306 FORWARD DOOR LIGHT ILLUMINATED ON TAKEOFF. RETURNED TO MRY. ADJUSTED FORWARD DOOR LOWER MICROSWITCH. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002050100103 20020501 00103 EA 2002 5 1 SWIA200210787 1 20020409 A 1430 SCREW CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LOOSE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 403SW 7028 RECEIVED A SERVICE DOOR CAUTION MESSAGE DURING CLIMBOUT. FOLLOWED QRH AND RETURNED TO LAX. FOUND THE 4 SCREWS HOLDING THE SERVICE DOOR INNER HANDLE TO BE LOOSE. TIGHTENED THE SCREWS AND CHECKED THE GAP FOR THE SERVICE DOOR PROXIMITY SWIT CH. ALL CHECKS GOOD AT THIS TIME. SERVICE DOOR INDICATION IS GOOD. 2 L 7 2 4F RT A21EA 2002050100104 20020501 00104 EA 2002 5 1 SWIA200210788 1 20020411 A 5297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 416SW 7089 RECEIVED PASSENGER DOOR WARNING MESSAGE ON CLIMBOUT. RAN QRH AND RETURNED SLC. REMOVED AND REPLACED DOOR WARNING WIRIN G HARNESS, REF SB 601R-52-099 AND TESTED IAW MM 52-11-04. OPS GOOD. 2 L 7 2 4F RT A21EA 2002050100105 20020501 00105 SO 2002 5 1 SWIA200210789 1 20020416 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT 3260202 SO T/E FLAP FAILED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 137H 538 538 120137 DURING TAXI FLAPS WOULD NOT SET TO 15 DEGREES. RECEIVED A CONTROL FAULT MESSAGE FOR THE OUTBOARD FLAPS. INSTALLED SERV ICEABLE OUTBOARD FLAP ACTUATOR (RIGHT) IAW MM 27-50-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002050100106 20020501 00106 EA 2002 5 1 SWIA200210790 1 20020415 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DIRTY A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 407SW 7034 EMERGENCY EXIT (RED) LIGHTS, EXIT ROW 8 ON THE FLOOR, ARE INOP. CLEANED CONNECTIONS TO FLOOR EMERGENCY LIGHTING, OPS CH ECKS GOOD. 2 L 7 2 4F RT A21EA 2002050100107 20020501 00107 SO 2002 5 1 SWIA200210791 1 20020416 A 3320 RECEPTACLE EMB 120 EMB120ER 3260203 SO CABIN MELTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 197SW 120186 SMOKE SMELL IN CABIN. FOUND A LIGHT RECEPTACLE MELTED. REPLACED LIGHT RECEPTACLE AT SEAT 5A. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002050100108 20020501 00108 SO 2002 5 1 SWIA200210792 1 20020417 A 2740 CONNECTOR EMB 120 EMB120ER 3260203 SO STAB TRIM CORRODED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 196SW 120151 ABORTED TAKEOFF FOR TRIM AURAL WARNING. TRIM WAS SET AT 35. FOUND THREE VERY LOOSE AND CORRODED CONNECTIONS ON THE LEF T TRIM PROXIMITY SENSOR. REPLACED ALL WITH ENVIRONMENTAL SPLICES. OPERATED TRIM SEVERAL TIMES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002050100109 20020501 00109 SO 2002 5 1 SWIA200210793 1 20020419 A 3350 SPLICE EMB 120 EMB120ER 3260203 SO CABIN DAMAGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 227SW 120304 EMERGENCY EXIT SIGN OVER ROW 9 IS INOP. INSPECTED AND REPAIRED BUTT SPLICE. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002050100110 20020501 00110 SO 2002 5 1 SWIA200210797 1 20020414 A 5240 DOOR EMB 120 EMB120ER 3260203 SO SERVICE DOOR LACK OF LUBE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 585SW 120353 SERVICE LIGHT ILLUMINATED 3 MINUTES AFTER TAKEOFF. RETURNED TO SLC. CLEANED AND LUBED ALL SERVICE DOORS. OPS CHECKS G OOD IAW MM 52-73-03. 2 L 7 2 4T RT A31SO 2002050100111 20020501 00111 NE 2002 5 1 SWIA200210798 2 20020415 A 7321 RELAY EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 301YV 120301 RIGHT EEC FAILED. ABORTED TAKEOFF. REPLACED RIGHT ENGINE REVERSION RELAY. ALL OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002050100112 20020501 00112 EA 2002 5 1 SWIA200210799 1 20020417 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE THROTTLE LOCKOUT OUT OF ADJUST A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 432SW 7548 DURING CLIMBOUT RECEIVED LEFT THRUST REVERSER UNLOCKED MESSAGE. FOLLOWED QRH AND RETURNED TO GSO. ADJUSTED THROTTLE LO CKOUT MICROSWITCH IAW CRJ MM 78-30-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002050100113 20020501 00113 2002 5 1 SWIA200210801 4 20020421 A 2210 6229968001 DAMPER CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS FAULTY A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 496SW 1581 1581 7473 YAW DAMPER NR 1 WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPER IAW 22-22-00. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002050100114 20020501 00114 SO 2002 5 1 SWIA200210802 1 20020420 A 2797 WIRE EMB 120 EMB120ER 3260203 SO PWA 119 PW119B NE FLAP ACTUATOR BROKEN A SWIA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 NM 07 220SW 120288 FLAP CONTROL FAULT ON FLAP INDICATOR PANEL AND FLAP/ADVANCED STALL WARNING ON MAP. ABORTED TAKEOFF. REPAIRED BROKEN WI RE AT NR 8 PIN ON LEFT OUTBOARD ACTUATOR. OPERATED FLAPS. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002050100115 20020501 00115 EA 2002 5 1 SWIA200210803 1 20020421 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE SPOILER MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 499SW 2569 2569 7398 RECEIVED SPOILERON FAULT STATUS MESSAGE ON TAXI OUT. REMOVED AND REPLACED RIGHT SPOILERON INBOARD PCU PER 27-62-01. OP S AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002050100116 20020501 00116 EU 2002 5 1 QXEA0200732 1 20020429 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 11159 BOI-BOTH MID CABIN EXIT SIGNS HAVE LAMPS INOPERATIVE. REPLACED BOTH EXIT SIGNS. OPERATIONAL CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002050100118 20020501 00118 2002 5 1 C2XA02CL106 4 20020316 A 2216 AN46A BOLT EMB 135 EMB135ER 3260203 SO FUSELAGE LOOSE A C2XA K NONE F FLT CONT AFFECTED LD LANDING 1 SW 27 17507 145215 CLE FLIGHT #3273 THE CREW REPORTED THE CONTROL COLUMN DID NOT MOVE FULL AFT ON LANDING ROLL.THE CONTROL MOVED HALFWAY.MA INTENANCE INSPECTED AND FOUND THE AILERON SERVO ATTACH HARDWARE WAS LOOSE AND HINDERING THE ELEVATOR BELLCRANK FROM FULL TRAVEL.THE HARDWARE WAS TIGHTENED AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002050100119 20020501 00119 NM 2002 5 1 AWXA200200387 1 20020430 A 3350 BMS13311122 WIRE BOEING 737 7373Q8 1384670 NM SEAT ROW 3 L/H BROKEN A AWXA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 28 327AW 0 0 23507 PHX -EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED B ROKEN WIRE AT SEAT ROW 3 L/H, OPERATIONAL CHECK GOOD IAW T/C A1C33006. 2 L 7 2 4F RT A16WE 2002050100120 20020501 00120 EU 2002 5 1 AWXA200200388 1 20020417 A 5315 D53112729200 SEAT TRACK AIRBUS 320 A320232 3930326 EU CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 605AW 0 0 543 YWG - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FRAME (SEAT TRACK) AT Y254 R/H, FROM FR 16-20. MAINTENANCE REMOVED SEAT TRACK FROM FR 16-20, Y254 R/H PER DWG 053112729, FABRICATED NEW SEAT TRACK AND INSTALLED REPAI R IAW A320 SRM 51-44-21, PG. 6 2 L 7 2 4F RT A28NM 2002050200001 20020502 00001 EU 2002 5 2 C2XA02IA098 1 20020428 A 3260 D228830001 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU NLG STRUT INOPERATIVE A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 97841 280 IAH- DURING FLIGHT 3600 THE CREW NOTED THAT NOSE LANDING GEAR ON #1 SYSTEM SWITCHED FROM LOCKED TO UNLOCKED IN FLIGHT, ON GROUND WAS DOING SAME THING, BUT WITH LOUD BANGING, AND, #2 HYDRAULIC SYSTEM LOOSING 1,000 PSI. IAH- MAINTENANCE RE MOVED AND REPLACED THE RIGHT HAND NLG PROXIMITY SWITCH REF. ATR 42 JIC 32-61-00, AND, THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 H 7 2 4T RT A53EU 2002050200002 20020502 00002 EU 2002 5 2 C2XA02IA099 1 20020428 A 3260 D61306 BRACKET AEROSP ATR42 ATR42320 8680930 EU NLG STRUT BENT A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 97841 280 IAH- DURING FLIGHT 3581 THE CREW NOTED THAT THE #1 SYSTEM NOSE LANDING GEAR UNLOCKED LIGHT STAYS ON. IAH- MAINTENANCE INSPECTED THE NLG, AND, RELEASED THE AIRCRAFT IAW MEL. IAH- MAINTENANCE REMOVED and REPLACED THE PROX SWITCH BRACKET, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002050200003 20020502 00003 NM 2002 5 2 UPS02238102 1 20020420 A 5310 SEAT TRACK BOEING 727 727180C 138406G NM BS 500 R/H O/B CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C CORROSION FOUND ON SEAT TRACK O/B FLANGE AT BS 500 AT R/H O/B SEAT T RACK SEAT TRACK REPAIRED IAW SRM 53-10-5 2 L 7 3 4F A3WE 2002050200004 20020502 00004 NM 2002 5 2 UPS02238103 1 20020418 A 5330 SKIN BOEING 727 727180C 138406G NM BS 310 S8L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C SUSPECT CRACK IN FUSELAGE SKIN BS 310 S8 L/H AT FWD ENTRY DOOR FWD D OOR CUT OUT REPAIR CARRIED OU T IAW UPS EO B727-5340-1460 2 L 7 3 4F A3WE 2002050200057 20020502 00057 NM 2002 5 2 ANCF200200007 1 20020413 A 2910 LINE BOEING 767 767383 1385214 NM PWA 4060 PW4060 52119 NE HYD SYSTEM LEAKING W ANCF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 23 984AN 24357 DURING FLIGHT RT HYDRAULIC QUANTITY DECREASED FROM 1.03 TO ZERO, QUANTITY STABLE WITH EDP DEPRESSURIZED AND AC PUMP OFF. RT HYDRAULIC QUANTITY READS ZERO. DURING MAINTENANCE INSPECTION WAS FOUND HYDRAULIC LEAK FROM RT AC PUMP PRESSURE. LIN E., ADJUSTED PRESSURE LINE IAW AMM 20-10-09 PAG 401, CHECKED HYDRAULIC SYSTEM BY LEAKS WITH ENGINE RUN UP. NO EVIDENCE O F LEAK WAS FOUND IAW AMM 29-11-00. 2 L 7 2 4F 4 F RT A1NM E24NE 2002050200058 20020502 00058 WP 2002 5 2 0201329981 1 20020424 A 2131 10256861 CONTROLLER DOUG DC9 DC931 3022065 WP CABIN PRESSURE MALFUNCTIONED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 994Z 47097 AIRCRAFT WAS CRUISING AT FL330 WHEN THE CABIN PRESSURE ANNUNCIATOR LIGHT ILLUMINATED AND CABIN ALTITUDE WAS APPROACHING 10,000 FEET. WING ANTI-ICE AND ENGINE ANTI-ICE WERE BOTH ON AT THE TIME AND TURNING THEM OFF DID NOT HELP TO REGAIN CAB IN PRESSURE. CREW DECLARED AN EMERGENCY AND DESCENDED TO 10,000 FEET WHERE THE SYSTEM WAS ABLE TO RECOVER. LANDING AT ATL WAS WITHOUT INCIDENT AND MAINTENANCE REPLACED THE PRESSURE CONTROLLER AND THE PRESSURE AMPLIFIER AFTER CHECKING FOR LEAKS. NO LEAKS WERE FOUND AND MASKS DID NOT DEPLOY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002050200059 20020502 00059 EA 2002 5 2 02119663 1 20020429 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A VTZA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 27 663BR 7527 AFTER TAKEOFF, THE CREW REPORTED THAT THE FLAPS HAD STUCK AT 20 DEGREES AND WOULD NOT RETRACT. THE CREW FOLLOWED THE QR H PROCEDURES, RETURNED TO CAE, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL PERFORMED EXTENSIVE TESTS OF THE FLAP SYSTEM AND FECU, CYCLING THE FLAPS SEVERAL TIMES FROM ZERO TO 45, AND FROM ZERO TO 45 IN INCREMENTS BUT WERE UNABLE TO DUPLICATE ANY MALFUNCTION. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002050700123 20020507 00123 NM 2002 5 7 02FDEA00298 1 20020427 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 204FE 22926 FUSELAGE SKIN IS WORN AT RT RAIN GUTTER AT BS 1342. REMOVED AND REPLACED SKIN PER SRM 53-10-1, 51-20-1, 54-30-3, 51-10- 2. 2 L 7 3 4F A3WE 2002050700125 20020507 00125 NM 2002 5 7 02FDEA00299 1 20020427 A 5330 65C25331 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 204FE 22926 GOUGE IN SKIN AT BS 588, STR 22L. REMOVED AND REPLACED SKIN PER SRM 53-30-1. 2 L 7 3 4F A3WE 2002050700126 20020507 00126 NM 2002 5 7 02FDEA00300 1 20020427 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 204FE 22926 CREASE IN SKIN AT BS 1105, STR 19R. REMOVED AND REPLACED SKIN PER SRM 53-30-3. 2 L 7 3 4F A3WE 2002050900050 20020509 00050 NM 2002 5 9 02FDEA00301 1 20020427 A 5320 STRAP BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 204FE 22926 CORROSION ON STRAP AT BS 870 BULKHEAD, LBL 60 18 INCHES I/B OF TERMINAL FITTING. REMOVED AND REPLACED STRAP PER EA 7-53 10-64069. 2 L 7 3 4F A3WE 2002050700128 20020507 00128 NM 2002 5 7 02FDEA00302 1 20020417 A 5330 6572702 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 204FE 22926 SKIN BULGED AT BS 975, STR 28R. REMOVED AND REPLACED SKIN PER SRM 53-30-3. 2 L 7 3 4F A3WE 2002050900051 20020509 00051 NM 2002 5 9 02FDEA00303 1 20020430 A 3230 MOUNT BOEING 727 7272S2F 1384O81 NM NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 204FE 22926 NOSE GEAR DOWN LOCK ACTUATOR MOUNT IS CRACKED. REMOVED AND REPLACED ACTUATOR PER SRM 51-30-2. 2 L 7 3 4F A3WE 2002050200064 20020502 00064 CE 2002 5 2 2002F00429 1 20020430 A 1430 50452112 BOLT CESSNA 402 402B 207590P CE NLG BROKEN E A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 27 402SS 402B0562 UPON REACHING DESTINATION THE PILOT SELECTED GEAR DOWN AND THERE WAS NO GREEN LIGHT FOR THE NOSE GEAR. THE GEAR WAS CYC LED AND MANUAL EXTENSION TRIED TO NO AVAIL. RETURNED TO HOME BASE AND MANEUVERED THE AIRCRAFT IN AN ATTEMPT TO SWING TH E GEAR OVER CENTER, WHICH AFTER SEVERAL ATTEMPTS SUCCEEDED AND GOT A GREEN GEAR SAFE LIGHT. UPON INSPECTION IT WAS DISC OVERED THAT THE NOSE LANDING GEAR FORK BOLT HAD BROKEN. EXAMINATION OF THE BOLT SHOWS NO SIGNS OF PRE-EXISTING DAMAGE. 1 L 7 2 3O A7CE 2002050200079 20020502 00079 NM 2002 5 2 2002UALA00740 1 20020419 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 STATION 867 FRAME IS CRACKED AT STRINGER 9R RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050200080 20020502 00080 NM 2002 5 2 2002UALA00741 1 20020419 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 CREASE BEAM WEB CORRODED 3 AREAS STATION 620 - 640 RIGHT HAND SIDE. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER 17R C REASE BEAM WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050200081 20020502 00081 NM 2002 5 2 2002UALA00742 1 20020419 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 RIGHT HAND STUB FRAME STATION 294 STRINGER 17R WL 208 CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER . 2 L 7 2 4F 4 F RT A16WE E2GL 2002050200082 20020502 00082 NM 2002 5 2 2002UALA00744 1 20020420 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 LEFT HAND BODY STATION 188 STRINGER 17L IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050200083 20020502 00083 NM 2002 5 2 2002UALA00745 1 20020420 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 LEFT HAND CABIN STATION 727C TO 727D STRINGER 17 WL 208 CREASE BEAM WEB CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050200084 20020502 00084 NM 2002 5 2 2002UALA00746 1 20020421 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 STRINGER 17R CREASE BEAM HAS CORROSION FROM STATION 294 TO 328 RBL 58 INBOARD ANGLE. MAJOR REPAIR ACCOMPLISHED. REPLAC ED SECTION OF CREASE BEAM INBOARD CHORD ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050200085 20020502 00085 NM 2002 5 2 2002UALA00747 1 20020421 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 RIGHT HAND CABIN STATION 727B TO 727C STRINGER 17R WL 208 CREASE BEAM WEB CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACE D CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050200086 20020502 00086 NM 2002 5 2 2002UALA00748 1 20020421 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 FLOORBEAM AT BODY STATION 335 RBL 16 TO RBL 24 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050200087 20020502 00087 NM 2002 5 2 2002UALA00750 1 20020423 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 EXTERNAL FUSELAGE AT KEEL BEAM STATION 698 LBL 4 LOWER SKIN CRACKED. MAJOR REPAIR ACCOMPLISHED. EXTERNAL DOUBLER INSTA LLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002052900068 20020529 00068 2002 5 29 2002UALA00751 4 20020423 A 2565 101651303 PIPE BFGOODRICH 101651303 BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EVAC SLIDE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 DOOR 1R SLIDE-RAFT DEPLOYED AFTER PARKING AT GATE. SLIDE FELL ONTO JETWAY PREVENTING FULL DEPLOYMENT. THE FLIGHT ATTEN DANT ROTATED DOOR HANDLE RATHER THAN ARM/DISARM LEVER CAUSING INADVERTENT DEPLOYMENT. SLIDE DEPLOYED, BUT DID NOT INFLA TE. FURTHER INVESTIGATION FOUND THE HOSE/PIPE CONNECTION FROM THE BOTTLE TO THE ASPIRATORS HAD BROKEN/SNAPPED. UNITED' S METALLURGIST INSPECTED BROKEN PIPE AND DETERMINED THAT AN IMPACT OF UNKNOWN ORIGIN WAS DELIVERED TO THE ALUMINUM FITTI NG AT THE TIME OF DEPLOYMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 2002050200089 20020502 00089 NM 2002 5 2 CALA0200255 1 20020502 A 5743 654949118 FITTING BOEING 737 7373T0 1384582 NM R/H MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 R/H MLG FITTING INNER BUSHING CORROSION ON THE BOSS. REPAIRED FITTING HOLE AND INSTALLED OVER SIZE BUSHING PER ECRA 57 11-01039. 2 L 7 2 4F RT A16WE 2002050200094 20020502 00094 NM 2002 5 2 02FDEA00288 1 20020422 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 207FE 22929 AFT CARGO DOOR CUTOUT SKIN AT UPPER FWD CORNER IS CHAFED. REMOVED AND REPLACED SKIN PER EA 7-5310-63844. 2 L 7 3 4F A3WE 2002050700122 20020507 00122 NM 2002 5 7 02FDEA00297 1 20020427 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 204FE 22926 DENT ON SKIN LAP BS 595, STR 19L. REMOVED AND REPLACED SKIN PER SRM 53-30-1, 53-30-3, 51-10-2, 51-20-4. 2 L 7 3 4F A3WE 2002050900066 20020509 00066 EU 2002 5 9 2002UALA00752 1 20020423 A 2133 VFT300A1 OUTFLOW VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 416UA 479 AIRCRAFT UNABLE TO MAINTAIN PRESSURE. VALVE REPLACED ALONG WITH THE AVIONICS COMPUTER. 2 L 7 2 4F 4 F RT A28NM E40NE 2002050200096 20020502 00096 NM 2002 5 2 2002UALA00753 1 20020424 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 934UA 26662 EXTERNAL FUSELAGE DENTED AT APPROXIMATELY STATION 410 BETWEEN STRINGER 25R AND 26R. DENT IS WITHIN 10 INCHES OF CUTOUT AND WITHIN 3 INCHES OF SKIN SPLICE. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002050900067 20020509 00067 2002 5 9 2002UALA00754 4 20020423 A 2330 7002086001 PROJECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN MALFUNCTIONED A UALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 29 673UA 29241 ON APPROACH TO SFO AT FL080 F/A NOTICED SMOKE COMING FROM FIRST CLASS PROJECTOR. F/A DISCHARGED FIRE EXTINGUISHER. REP LACED VIDEO PROJECTOR, TESTS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2002052900072 20020529 00072 NE 2002 5 29 2002UALA00756 2 20020424 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 ENGINE DETERIORATED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 666UA 12254 12254 29238 727815 AT APPROX 300 AGL NR 2 ENGINE HAD A COMPRESSOR SURGE, MAX EGT 638F. ENGINE EXPERIENCED A GROUP 3 SURGE. SURGE IS CAUSE D BY EXCESSIVE BLADE TIP CLEARANCES IN THE HPC REAR STAGES. PERFORMED TEST-21 AND ENGINE FAILED. ENGINE WAS REMOVED FO R SHOP REWORK. AD 2001-25-11 ALREADY IN EFFECT FOR FLEET DETERIORATION MANAGEMENT. FINAL FIX PENDING. 2 L 7 2 4F 4 F RT A1NM E24NE 2002050200097 20020502 00097 NM 2002 5 2 2002UALA00757 1 20020425 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 934UA 26662 CABIN STATION 987 FLOORBEAM CAP CORROSION REMOVAL BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. ACCOMPLIS HED SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002052900083 20020529 00083 NM 2002 5 29 2002UALA00758 1 20020425 A 2612 G718505 PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAULTY A UALA K NONE N FALSE WARNING LD LANDING 1 WP 29 381UA 24656 LANDED UNDER AMBER ALERT DUE TO CARGO FIRE LIGHT ILLUMINATED ON FINAL APPROACH. MAINTENANCE REMOVED AND REPLACED THE CA RGO DETECTION PANEL, BOTH FIRE BOTTLES, METERING VALVE, DIVERTER VALVE, LINE FILTERS, PERFORMED INSPECTION OF THE CARGO COMPARTMENT DISCHARGE NOZZLES AND THE SMOKE DETECTORS. AFTER INSTALLATION OF SERVICEABLE EQUIPMENT, CARGO COMPARTMENT F IRE DETECTION AND SUPPRESSION SYSTEM WAS TESTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051500140 20020515 00140 NE 2002 5 15 2002UALA00759 2 20020309 A 7230 COMPRESSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 ENGINE FAILED A UALA J A DUMP FUEL UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 117UA 13772 13772 28810 727856 STALL ON TAKEOFF CONFIRMED NR 1 ENGINE POSITION 3 LOUD BANGS. WINDS 2820 TO 40 SFOLM-EMC LANZA PER CREW VERBAL 3 BANGS AT 300 FEET AGL EPR 1.51 V2 184 APRX 190 KNOTS NO ENGINE PARAMETER CHANGES NOTED AT TIME OF STALL OR AFTER ALL ENGINES R AN NORMAL. ENGINE EXPERIENCED A GROUP 3 SURGE. SURGE IS CAUSED BY EXCESSIVE BLADE TIP CLEARANCES IN THE HPC REAR STAGE S. ENGINE WAS REMOVED AND PERFORMED TEST-21 AND FAILED. THE COMPRESSOR WILL BE OVERHAULED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002050900068 20020509 00068 NM 2002 5 9 2002UALA00760 1 20020426 A 5313 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 FORWARD CARGO PIT STRINGER 34L HAS A 2 INCH CRACK AT STATION 390. MAJOR REPAIR ACCOMPLISHED. INSTALLED U-CHANNEL. 2 L 7 2 4F 4 F RT A1NM E24NE 2002050200098 20020502 00098 NM 2002 5 2 2002UALA00762 1 20020425 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 FORWARD PIT STATION 780 BELOW FUSELAGE FRAME UPPER CAP HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALL ED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000053 20020530 00053 NM 2002 5 30 2002UALA00763 1 20020425 A 2721 PCU BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RUDDER MALFUNCTIONED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 29 609UA 21870 IN CRUISE THE RUDDER TRIM FROZE. ATTEMPTS TO TROUBLESHOOT WITH THE CAPTAIN WERE UNSUCCESSFUL. DIVERTED TO ORD. NO EME RGENCY DECLARED. REPLACED CENTER PCU, REPLACED RUDDER TRIM MODULE AND RUDDER TRIM POSITION INDICATOR, REPLACED RUDDER T RIM ACTUATOR. REPAIRED SEVERAL BENT PINS ON CONNECTOR D5300J. ADJUSTED AND TESTED RUDDER PER MM 27-21-00. REPLACED CE NTER PCU. ACCOMPLISHED REPLACEMENT OF THE RUDDER FEEL CENTERING & TRIM MECHANISM IAW MM 27-21-10 PAGE 214. 2 L 7 2 4F 4 F RT A1NM E3NE 2002050200100 20020502 00100 WP 2002 5 2 ABXA010858 1 20020114 A 5730 SKIN DOUG DC8 DC863F 302198F WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE SKIN HAD CRACK WITH STOP HOLES AT XLS 710, OUTBOARD SIDE OF NR 4 ENGINE. INSTALLED DOUBLER REPA IR IAW DC-8 SRM 57-2-1. 2 L 7 4 4F 4A25 2002050200101 20020502 00101 WP 2002 5 2 ABXA010859 1 20020121 A 5320 ATTACH ANGLE DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT MAIN WHEEL WELL INSIDE KEEL BEAM, STATION 910, VERTICAL ATTACH ANGLE, LOWER END CRACKED WITH STOP DRILL HOLE. INST ALLED REPAIR ANGLES IAW REA D853-41947. 2 L 7 4 4F 4A25 2002050200102 20020502 00102 WP 2002 5 2 ABXA010860 1 20020103 A 5730 SKIN DOUG DC8 DC863F 302198F WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE LOWER SKIN, JUST OUTBOARD OF THE NR 1 PYLON HAD 4 EACH CRACKS AT STATION XRS 525. INSTALLED DOUB LER REPAIR AND REPAIRED AREA IAW DC-8 SRM 57-2-1 AND 51-1-8. 2 L 7 4 4F 4A25 2002050200104 20020502 00104 WP 2002 5 2 ABXA010862 1 20020115 A 5310 DOOR FRAME DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT FORWARD ENTRY DOOR MADE A BINDING NOISE WHEN MOVED FROM FULL OPEN POSITION. FOUND SNUBBER SUPPORT WEB CRACKED. CU T OUT DAMAGED SECTION OF FRAME AND INSTALLED NEW SPLICE AT BOTH ENDS IAW REA D853-41451MR. 2 L 7 4 4F 4A25 2002050200105 20020502 00105 NM 2002 5 2 ABXA010864 1 20020428 A 5711 SPAR BOEING 767 767200 1385120 NM RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 RIGHT WING FRONT SPAR OUTBOARD HOLES, HOLE NR 12, FROM TOP HAD A CRACK INDICATION WITH NDT. REAMED HOLE SIZE TO .387, N O CRACKS FOUND IAW B767 NDT MANUAL PT6 51-00-19. INSTALLED OVERSIZED FASTENERS IAW REA B657-43120MR. 2 L 7 2 4F RT A1NM 2002050200106 20020502 00106 NM 2002 5 2 ABXA010865 1 20020428 A 5711 SPAR BOEING 767 767200 1385120 NM RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 RIGHT WING, FRONT SPAR, OUTBOARD HOLES, HOLE NR 4 FROM TOP, HAD A CRACK INDICATION WITH NDT. REAMED HOLE SIZE TO .387, NO CRACKS FOUND IAW B767 NDT MANUAL PT6 51-00-19. INSTALLED OVERSIZED FASTENERS IAW REA B657-43120MR. 2 L 7 2 4F RT A1NM 2002050200107 20020502 00107 NM 2002 5 2 ABXA010866 1 20020428 A 5711 SPAR BOEING 767 767200 1385120 NM RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 RIGHT WING, FRONT SPAR, OUTBOARD HOLES, HOLE NR 10 FROM TOP, HAD A CRACK INDICATION WITH NDT. REAMED HOLE SIZE TO .387, NO CRACKS FOUND IAW B767 NDT MANUAL PT6 51-00-19. INSTALLED OVERSIZED FASTENERS IAW REA B657-43120MR. 2 L 7 2 4F RT A1NM 2002050200108 20020502 00108 NM 2002 5 2 02FDEA00306 1 20020328 A 5230 52FX13996 FRAME BOEING 727 727277 138408S NM DENTED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 N 697 MAIN CARGO DOOR AFT SIDE FRAME DENTED ABOVE CENTERING GUIDE RAMP. ** S/D ** COMING 2 L 7 3 4F RT A3WE 2002050200109 20020502 00109 WP 2002 5 2 AT0200055 1 20020429 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 OVERWING EMERGENCY LIGHTS STAY ON WHEN BATTERY SWITCH IS OFF. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY. 2 L 7 2 4F A6WE 2002050200110 20020502 00110 NM 2002 5 2 AWXA200200380 1 20020429 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 660AW 7213 1234 ATL - EEL - DURING INSPECTION EMERGENCY POWER SUPPLY UNIT 12WL WAS FOUND INOPERATIVE. MAINTENANCE REPLACED EMERGENCY PO WER SUPPLY UNIT 12WL IAW AMM 33-51-38-401, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002050200111 20020502 00111 NM 2002 5 2 AWXA200200382 1 20020424 A 5320 6623574 CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON GUSSET CLIP STRINGER 12 LT, BS 706. MAINTENANCE REMOVED GUS SET CLIP FROM STR 12 LT AT BS 706, FABRICATED AND INSTALLED NEW CLIP IAW DWG 66-23574, AND B737-300 SRM 51-40-02, PG 2-3 . 2 L 7 2 4F RT A16WE 2002061000041 20020610 00041 NM 2002 6 10 AWXA200200383 1 20020429 A 3610 342B030000 FILTER AIRBUS A319 A319132 3930340 NM THERMOSTAT CONTAMINATED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 802AW 12938 924 ON CLIMBOUT, CREW RECEIVED ECAM MESSAGE FOR NR 1 ENG BLEED FAULT; BLEED TEMP REACHED 280 DEG & CROSSFEED VALVE OPENED; A CFT RETURNED. MX REPLACED FAN AIR THERMOSTAT & OPERATIONALLY CHECKED OUT SYS BY RUNNING ENG FOR AN EXTENDED PERIOD OF T IME AT POWER, CHECKED GOOD. SYS PREVIOUSLY PLACED ON MEL 36-11-04 COND. NR 1 FAN AIR VALVE INOPERATIVE FOR SIMILAR EVE NT THAT OCCURRED ON 04/28/2002. NR 1 ENGINE FAN AIR VALVE WAS REPLACED. VENDOR BENCH CHECK OF FAN AIR VALVE, NO FAULT FOUND. VENDOR TEARDOWN OF TEMP CONTROL THERMOSTAT CONFIRMED FAILURE. THERMOSTAT FILTER CONTAMINATED & BLOCKED BY POLLU TION. FILTER WAS CLEANED, AND PACKING (S602-6X1) AND PRESSURE REDUCING CLAPPER GUIDE REPLACED. 2 L 7 2 4F RT A28NM 2002050200112 20020502 00112 EU 2002 5 2 AWXA200200384 1 20020417 A 5315 D53472193200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 605AW 543 YWG - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND FLOORBEAM AT Y765 RT, FR 67-68. MAINTENANCE REMO VED CORRODED FLOORBEAM FROM FR 67-70, Y765 RT, FABRICATED AND INSTALLED A NEW FLOORBEAM IAW A320 SRM 53-41-14, FIG 8 PG 34B. 2 L 7 2 4F RT A28NM 2002050200113 20020502 00113 NM 2002 5 2 DL757020480 1 20020423 A 5330 146N3700149 SKIN BOEING 757 757232 1384965 NM FS 1715, S-16L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 FUSELAGE / SKIN / FS 1715.5 / STRG. 15L-17L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH 2 DENTS NEAR FS 1715.5 BETWEEN STRINGERS 15L & 17L. THE DENTS WERE REMOVED WITH CUTOUTS IN THE SKIN. THE 2 CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER PER ER/A 412647-14, REV A. 2 L 7 2 4F RT A2NM 2002050200114 20020502 00114 2002 5 2 DLM11020487 4 20020428 A 2310 MV10 MEGAPHONE DOUG MD11 MD11 3023602 NM AFT FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 807DE 48478 AFT CABIN MEGAPHONE WILL NOT TEST. REPLACED MEGAPHONE. 2 L 7 3 4F RT A22WE 2002050200115 20020502 00115 NM 2002 5 2 DL73K020492 1 20020427 A 5330 SKIN BOEING 737 737232 1384475 NM FS 747, S-18R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 323DL 23095 FUSELAGE / SKIN / FS 747 / STRG. 18R : CRACK REPAIR THE FUSELAGE SKIN WAS FOUND WITH A 2" LONG CRACK AT THE EDGE OF THE BONDED "WAFFLE" DOUBLER AT STRINGER 18R AND FS 747. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383028-14. 2 L 7 2 4F RT A16WE 2002050200116 20020502 00116 2002 5 2 DL767020496 4 20020501 A 2300 6226831001 PANEL BOEING 767 767232 1385132 NM NBR 1 UNRELIABLE A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 103DA 22215 CAPTAINS VHF FREQUENCY SELECT PANEL LEFT DISPLAY 4TH DIGIT CHANGED_WITHOUT INPUT. 118.97 SWITCHED BACK AND FORTH TO 118 .17 CA RPLD PANEL, OP CKS GD. 2 L 7 2 4F RT A1NM 2002050200117 20020502 00117 EU 2002 5 2 AWXA200200385 1 20020416 A 5315 D53472195202 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 605AW 543 YWG - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND FLOOR SUPPORT RAIL BEAM AT Y765 RT, FR 68. MAINT ENANCE REMOVED CORRODED FLOOR SUPPORT RAIL BEAM FROM FR 66-70, Y765 RT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT RAI L BEAM IAW A320 SRM 53-42-11, PG 1 PARA 2 (A). 2 L 7 2 4F RT A28NM 2002050200118 20020502 00118 WP 2002 5 2 ABXA010867 1 20020404 A 5340 ANGLE DOUG DC8 DC861 3021952 WP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 AFT PRESSURE BULKHEAD FORWARD SIDE ANGLE WAS CRACKED AT LONGERON 2 RIGHT, APPROXIMATELY 2 INCHES IN LENGTH. INSTALLED AN GLES AND REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8 AND 51-1-11. 2 L 7 4 4F 4A25 2002050200119 20020502 00119 WP 2002 5 2 ABXA010868 1 20020409 A 2700 FITTING DOUG DC8 DC861 3021952 WP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 LEFT WING STATION 340, FLAP SUPPORT FITTING WAS CRACKED. REMOVED AND REPLACED THE LEFT WING STATION 340 FLAP SUPPORT FIT TING IAW DC-8 MM 20-14-00 AND 20-16-00. REMOVED AND REPLACED THE LEFT WING STATION 340 FLAP ACTUATOR CYLINDER AND OPS C HECKED GOOD IAW DC-8 MM 27-51-09. 2 L 7 4 4F 4A25 2002050200120 20020502 00120 2002 5 2 AWXA200200386 4 20020423 A 2565 65C1990141 LATCH BOEING 737 7373G7 1384595 NM L1 DOOR OUT OF ADJUST A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - EMERGENCY EVACUATION - DURING C-16 CHECK THE L1 DOOR EMERGENCY ESCAPE SLIDE LATCH ASSEMBLY FAILED FUNCTIONAL TEST. MAINTENANCE TROUBLESHOT AND FOUND THE EMERGENCY ESCAPE SLIDE LATCH BRACKET OUT OF ADJUSTMENT; ADJUSTED LATCH BRACKET A ND PERFORMED OPERATIONAL CHECK IAW BMM 25-61-35, PG 208. 2 L 7 2 4F RT A16WE 2002050200121 20020502 00121 WP 2002 5 2 CALA0200251 1 20020429 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR PAN AT FORWARD AND AFT SIDE. THE CRACK WAS LOCATED AT RADIUS BELO W LATCH. THE CRACKS WERE STOP DRILLED IAW SRM 52-05, FIGURE 26A. REPAIR ANGLES WERE INSTALLED AT EACH LOCATION IAW SRM 52-05, FIGURE 26A. 2 L 7 2 4F A6WE 2002050200122 20020502 00122 WP 2002 5 2 CALA0200252 1 20020429 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND A CREASE IN FUSELAGE SKIN AT STA 420 AND 446 BETWEEN STRINGER 22L AND 23L. THE CREASED AREAS WERE CUT OUT IAW SRM 53-04, FIGURE 38. A DOUBLER, FILLER, AND FINGER DOUBLER WERE INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGU RE 38. 2 L 7 2 4F A6WE 2002050200123 20020502 00123 WP 2002 5 2 CALA0200253 1 20020429 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND A CREASE IN FUSELAGE SKIN AT STA 218 BETWEEN STRINGER 16R AND 17R. THE CREASED AREA WAS REMOVED IAW SR M 53-04, FIGURE 38. A DOUBLER WAS INSTALLED IAW SRM 51-10-04 AND 53-04, FIGURE 38. 2 L 7 2 4F A6WE 2002050200124 20020502 00124 EA 2002 5 2 COMA0260283 1 20020429 A 5297 601R578951 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 805CA 7354 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. REPLACED THE DOOR WIRE HARNESS. 2 L 7 2 4F RT A21EA 2002050200125 20020502 00125 NM 2002 5 2 DHL2002753003 1 20020501 A 5610 5893543129 WINDSHIELD BOEING 727 727223 1384074 NM A DHLA A D UNSCHED LANDING RETURN TO BLOCK O OTHER CL CLIMB 1 SO 01 712AA 22468 1) PASSING FL 280 8PSI CAPT L1 WINDOW SHATTERED. COMPLETED ABNORMAL PROCEDURES AND RETURNED TO EWR2) R & R L1 (PILOT) WI NDOW IAW DHL 727A M/M 56-11-11 WINDOW LEAK CHECKS GOOD ON GROUND AT EWR 2 L 7 3 4F A3WE 2002050200126 20020502 00126 EA 2002 5 2 COMA0260291 1 20020429 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 975CA 13416 7150 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 650GB.REPAIRED IAW 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002050200127 20020502 00127 EA 2002 5 2 COMA0260294 1 20020429 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA 209.040 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 973CA 13330 7146 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 550CB.REPAIRED IAW 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002050200128 20020502 00128 WP 2002 5 2 MWEA020299 1 20020429 A 5320 591142343 DOUBLER DOUG DC9 DC932 3022066 WP STATION 908 WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 LAVATORY SERVICE PANEL 2 UPPER LATCHES WORN THRU DOUBLERS. -- REPAIRED BY INSTALLING DOUBLER PER IAW TELEX MWX-ORD-02- 002-00249H DATED APRIL 18 2002. 2 L 7 2 4F A6WE 2002050200129 20020502 00129 WP 2002 5 2 MWEA020300 1 20020419 A 5320 991224375N GUSSET DOUG DC9 DC932 3022066 WP STATION 965 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FRAME TO STRUT GUSSET, LEFT SIDE AT STATION 965 CORRODED. -- REMOVED AND REPLACED GUSSET. 2 L 7 2 4F A6WE 2002050200130 20020502 00130 WP 2002 5 2 MWEA020301 1 20020429 A 5320 991224371 SHEAR TIE DOUG DC9 DC932 3022066 WP STATION 965 ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 SHEAR TIE AT STATION 965 BETWEEN LONGERON 20 LEFT AND LONGERON 128 LEFT HAS OBLONG HOLE COMMON TO SKIN. -- REMOVED AND REPLACED UPPER SECTION OF SHEAR TIE. 2 L 7 2 4F A6WE 2002050200131 20020502 00131 WP 2002 5 2 MWEA020302 1 20020429 A 5311 SR0953005725 FRAME DOUG DC9 DC932 3022066 WP STATION 965 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FRAME AT 965 IS CORRODED BETWEEN LONGERON 22 AND 23 LEFT. -- REMOVED AND REPLACED FRAME SECTION. 2 L 7 2 4F A6WE 2002050200132 20020502 00132 WP 2002 5 2 MWEA020303 1 20020429 A 5313 591142351 LONGERON DOUG DC9 DC932 3022066 WP STATION 956 UNSERVICEABLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 LONGERON 22 LEFT CUT AT STATION 956 AND AFT SECTION REMOVED TO FACILITATE OTHER MAINTENANCE. -- SPLICED SEGMENT OF LON GERON 22 LEFT AT STATION 956 AND AFT SECTION IAW SRM 53-02 FIG 18. 2 L 7 2 4F A6WE 2002050200133 20020502 00133 WP 2002 5 2 MWEA020305 1 20020429 A 5320 59145581 DOUBLER DOUG DC9 DC932 3022066 WP STATION 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 SUGAR SCOOP ATTACH RING DOUBLER CORRODED ON AFT END AT 2 SPOTS. -- REMOVED ATTACH RING DOUBLER. LOCATED AND INSTALLED NEW DOUBLER IAW SRM 51-30. 2 L 7 2 4F A6WE 2002050200134 20020502 00134 WP 2002 5 2 MWEA020308 1 20020429 A 5320 991224361 SHEAR TIE DOUG DC9 DC932 3022066 WP STATION 965 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 DAMAGED LOWER SECTION OF SHEAR TIE AT STATION 965 LEFT HAND DURING THE REMOVAL OF SHEAR TIE TO FACILITATE OTHER MAINTENA NCE. -- INSTALLED WITH NEW LOWER SECTION OF SHEAR TIE AT STATION 965 LEFT HAND IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2002050200135 20020502 00135 NM 2002 5 2 AWXA200200393 1 20020410 A 5313 654576738 STRINGER BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 0 0 22646 YVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND COMING FROM A RIVET HOLE ON STRINGER 15 L/H, FS 540. MAINTENANC E CUT OUT CRACKED SECTION OF STRINGER 15 L/H, FS 540, FORWARD OF AFT END; FABRICATED A REPAIR SPLICE AND INSTALLED REPAI R IAW AWA ER 15-5361-02113-TB3. 2 L 7 2 4F RT A16WE 2002050200136 20020502 00136 NM 2002 5 2 AWXA200200394 1 20020410 A 5210 6545849 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 0 0 22646 YVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND ON THE L2 DOOR LOWER HINGE CUTOUT BS 948, STR 14 L/H. MAINTENAN CE ROUTED OUT CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS PRESENT; FABRICATED A REPAIR DOUBLER AND INSTALL ED REPAIR IAW AWA ER 15-5210-02120-SS6, AND DWG 65C34390. 2 L 7 2 4F RT A16WE 2002050200137 20020502 00137 NM 2002 5 2 AWXA200200396 1 20020412 A 5311 654795946 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 0 0 22646 YVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND JUST ABOVE THE LOWEST DOOR STOP ON THE OUTER CHORD OF FORWARD F RAME OF AFT CARGO DOORWAY. MAINTENANCE REMOVED DAMAGED SECTION OF FRAME, FABRICATED NEW SECTION OF FRAME AND A FILLER, AND INSTALLED REPAIR PARTS PER B737-200 SRM 51-10-1, PG. 8, AND DWG 65-47959. 2 L 7 2 4F RT A16WE 2002050200138 20020502 00138 NM 2002 5 2 AWXA200200397 1 20020410 A 5311 65458088 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 0 0 22646 YVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND ON FRAME AT BS 294.5, STR 2 R/H. MAINTENANCE TRIMMED OUT CRACK ON FRAME AT BS 294.5, STR 2 R/H, FABRICATED 2 EA. REPAIR ANGLES, A FILLER, AND 2 EA. TIE CLIPS AND INSTALLED REPAIR PART S IAW AWA ER 15-5312-02120-SS7. 2 L 7 2 4F RT A16WE 2002050200139 20020502 00139 NM 2002 5 2 AWXA200200398 1 20020410 A 5330 6545767 SKIN PANEL BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 0 0 22646 YVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND ON FUSELAGE SKIN BS 520 STR 16 L/H. MAINTENANCE CUTOUT CRACKED AREA OF SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED. FABRICATED A REPAIR PLATE AND INSTALLED REPA IR PER B737-200 SRM 53-30-3, FIG. 1, PG. 2B. 2 L 7 2 4F RT A16WE 2002050200140 20020502 00140 NM 2002 5 2 AWXA200200399 1 20020410 A 5330 6546881 SKIN PANEL BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 0 0 22646 YVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND ON FUSELAGE EXTERNAL SKIN AT AUXILIARY POWER UNIT DISCHARGE DIS C (RED) ATTACH RIVET. MAINTENANCE CUTOUT CRACK AND PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED, FABRICATED A SMALL REPAIR DOUBLER, AND INSTALLED REPAIR PART IAW B737-200 SRM 53-30-3, FIG.43, PG. 175. 2 L 7 2 4F RT A16WE 2002050200141 20020502 00141 NM 2002 5 2 AWXA200200400 1 20020408 A 5311 65499534 FRAME BOEING 737 737277 1384570 NM WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 0 0 22646 YVR - MAJOR REPAIR - DURING C-20 CHECK THE R/H MAIN LANDING GEAR UPLOCK BUSHING FITTINGS WERE FOUND WORN BEYOND LIMITS, BS 685. MAINTENANCE REMOVED BUSHINGS AT BS 685 & 695, FOUND CORROSION IN BUSHING BORE BS 685, MACHINED TO REMOVED CORROS ION, FABRICATED 2 EA. REPAIR SLEEVES, INSTALLED SLEEVES AND FLAP PEENED PER SOPM 2010-03, INSTALLED NEW BUSHINGS. REPAIR PERFORMED IAW AWA ER 15-5364-02115-TB3. 2 L 7 2 4F RT A16WE 2002050200142 20020502 00142 NM 2002 5 2 S02279011 1 20020327 A 7900 POWERPLANT BOEING 747 747209B NM PWA JT9 JT9D7Q 52054 NE # 2 ENG W SAJF O OTHER O OTHER IN INSP/MAINT 1 WP 03 LD6340 22446 B18753 1.DURING O/N CHECK FOUND #2 ENG OIL SYS CONTAMINATED BY FUEL. 2.CHECK OIL TANK HAVE STRONG FUEL SMELL.C/A:1.RPLD FUEL/OIL COOLER IAW MM 79-21-01. 2.PERFORM M.C.D AND OIL FILTER CHECK NML, OIL FILTER RPLD. 3.PERFORM OIL SYS. FLUSH. EN G RUN UP CHECK NML. 2 L 7 4 4F 4 F RT A20WE E3NE 2002050300001 20020503 00001 NM 2002 5 3 S02856012 1 20020424 A 5600 SLIDING WINDOW BOEING 737 737800* NM CFMINT CFM567 CFM567B22 13802 NE W SAJF C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 03 29104 B18607 DURING T/O ROLLING AIRFLOW NOISE WAS HEARD FROM RH SLIDING WINDOW. WHEN SPEED REACH ABOUT 100KTS, CAPT DECIDED TO ABORT T/O ABOUT 120KTS.C/A:1.CREW CHKED THE WINDOW AT TAXI WAY AND REQUESTED MAINT. TO CHK BRAKE COND. 2.MAINT VISUALLY CHKED BRAKES AND HIGH ENERGY STOP/HEAT DAMAGE COND CHKED PER 737-800 AMM 05-51-07. THE RESULT WAS NML COND. 3.BOTH SLID E WINDOW CHKED. THE COND WAS NML. 4.CREW CONTINUED THE FLT. WHEN AIRPLANE ARRIVED THE, CREW REPORTED EVERYTHING WAS NML. 5.NO ANY PART, COMPONENT, ASSEMBLY AND STRUCTURE HAS IN SERVICE DIFFICULTY. 6.PREVENTIVE ACTION:IT IS NOT MECHANISM CAU SE, NO FURTHER ACTION IS REQUIRE. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002050300002 20020503 00002 NM 2002 5 3 ANCF200200008 1 20020425 A 5610 WINDOW BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT CRACKED W ANCF A UNSCHED LANDING O OTHER CL CLIMB 1 SO 23 321LF 24357 DURING CLIMB AFTER 15000 FT, A LOUD BANG WAS HEARED IN THE COCKPIT THE BANG WAS PRODUCED BECAUSE THE WINDOW CRACKED IN THE UPPER AND LOWER RIGHT HAND CORNER. WAS ACCOMPLISHED INSPECTION CHECK IAW AMM 56-11-00 PAGE 607 AND NO FOUND CRAC K, WAS FOUND DELAMINATION BETWEEN LIMITS IAW AMM 56-11-00, THE WINDOW 3R HEAT WAS DESACTIVATED AND DEFERRED TO DMI 208 M EL 30-41-1-2 CAT C. 2 L 7 2 4F 4 F RT A2NM E12EU 2002050300003 20020503 00003 NM 2002 5 3 ANCF200200009 1 20020426 A 2497 WIRE BOEING 767 767259 1385136 NM PWA 4056 PW4056 NE PRESSURE SWITCH CHAFED W ANCF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 986AN 24835 DURING FLIGHT EICAS MESSAGE RT GEN DRIVE DISPLAYED, GENERATOR DRIVE LIGHT ILLUMINATED. GENERATOR DRIVE DISCONNECTED. RECONNECTED RT GENERATOR AND PERFORMED OIL SERVICE, ADDITIONALLY PERFORMED BITE TO BPCU, RT OIL PRESSURE SWITCH WAS SHO WN, CHECKED WIRING AND FOUND CHAFED ON THE CONNECTOR D10964 PIN 9, IT WAS REPAIRED IAW AMM 24-11-21. 2 L 7 2 4F 4 F RT A1NM E24NE 2002050300013 20020503 00013 NM 2002 5 3 VNAA0204021 1 20020424 A 2400 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 425JS 3037 DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND F OUND A DISCONNECTED WIRE ON THE 1VE PANEL. MAINTENANCE CONNECTED THE WIRE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002050300014 20020503 00014 NM 2002 5 3 VNAA0204025 1 20020429 A 2400 8160121 GENERATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 459PS 3070 DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKE OFF. THE CREW RESET THE GENERAT OR AND IT CONTINUED TO WORK DURING THE TAXI BACK TO THE GATE. MAINTENANCE CONTROL HAD OUTSTATION MAINTENANCE INSPECT TH E RIGHT HAND GENERATOR AND THEN PERFORM POWER RUNS WITH THE CREW IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00 . THERE WERE NO DEFECTS NOTED THROUGHOUT THE INSPECTION. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002050300015 20020503 00015 NM 2002 5 3 VNAA0204026 1 20020429 A 2400 8160121 GENERATOR 1060003 DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 459PS 13694 285 1028 3070 DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND GENERATOR AND BUS POWER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. O PERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002050300016 20020503 00016 NM 2002 5 3 VNAA0204024 1 20020427 A 2800 311794904A FLOW DIVIDER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA O OTHER K FLUID LOSS CL CLIMB 1 GL 07 459PS 6871 3070 SHORTLY AFTER TAKE OFF, THE CREW HAD A POWER SPLIT AND THE LEFT HAND ENGINE FUEL SHOWED 500 POUNDS PER HOUR MORE THAN T HE RIGHT HAND. THE CREW NOTICED A FLUID OFF THE LEFT HAND ENGINE, DECLARED AN EMERGENCY, AND RETURNED TO PWM WITH NO FU RTHER INCIDENTS. PIT MAINTENANCE WAS DISPATCHED AND INSPECTED AND REPLACED THE FLOW DIVIDER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002050300052 20020503 00052 EA 2002 5 3 COMA0260284 1 20020429 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 786CA 7333 FLAP FAIL CAUTION MESSAGE. RESET THE FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002050300053 20020503 00053 EA 2002 5 3 COMA0260287 1 20020428 A 2750 860D10018AB FCU CNDAIR CL600 CL6002B19 1900309 EA E/E BAY MALFUNCTIONED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 956CA 12673 7105 FLAPS FAIL MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2002050300054 20020503 00054 EA 2002 5 3 COMA0260288 1 20020428 A 3350 6464 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 716CA 7250 EMERGENCY FLOOR PATH LIGHTS ROW 1 TO 5 ARE INOP. REPLACED THE NR 2 FLOOR LIGHT STRIP. 2 L 7 2 4F RT A21EA 2002050300055 20020503 00055 EA 2002 5 3 COMA0260290 1 20020426 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A COMA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 431CA 2307 7472 FLAPS FAILED AT 20 DEGREES. REPLACED THE FLAP PDU. 2 L 7 2 4F RT A21EA 2002050300056 20020503 00056 NM 2002 5 3 DHL2002726508 1 20020422 A 5230 655714039 ANGLE BOEING 727 727228 1384083 NM CARGO DOOR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C CHECK, C-1 CARGO DOOR INTERIOR STRUCTURE, 10 ANGLE HAS SEVERE EXFOLIATION CORROSION. REMOVED ANGLE FROM C-1 DO OR INTERIOR STRUCTURE AND REPLACED IAW B-727 SRM 51-40-4. REMOVED ANGLE FROM C-1 DOOR INTERNAL STRUCTURE IAW B-727 SRM 51-30-2. REPLACED ANGLE ON C-1 DOOR INTERNAL STRUCTURE IAW B-727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002050300057 20020503 00057 NM 2002 5 3 DHL2002726509 1 20020415 A 5260 SKIN BOEING 727 727228 1384083 NM VENTRAL STAIRS DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, VENTRAL STAIRS ASSY STA 1315 TO 1335, AFT EXT SKIN HAS 3 DENTS. FABRICATED AND INSTALLED DOUBLER REPAIR S. 2 L 7 3 4F RT A3WE 2002050300058 20020503 00058 NM 2002 5 3 DHL2002726512 1 20020425 A 5313 STRINGER BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, STRINGER 27R AT BS 710 HAS CORROSION. CUT OUT DAMAGED AREA IAW B-727 SRM 53-10-3 FIG 1. FABRICATED AND INSTALLED NEW STRINGER SECTIONS IAW SRM 53-10-2 FIG 9 SHEET 1. 2 L 7 3 4F RT A3WE 2002050300059 20020503 00059 NM 2002 5 3 DHL2002726513 1 20020416 A 5712 RIB BOEING 727 727228 1384083 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, RT WING FIXED L/E RIB HAS A CRACK AT WS 572. CUT OUT DAMAGED AREA IAW B-727 SRM 51-40-3. FABRICATED AN D INSTALLED REPAIR IAW B-727 SRM 51-30-2 AND 51-40-3. 2 L 7 3 4F RT A3WE 2002050300060 20020503 00060 NM 2002 5 3 DHL2002743005 1 20020501 A 2612 CONNECTOR BOEING 727 727225 1384077 NM COCKPIT DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 743DH 22438 ENGINE NR 1 FIRE HANDLE DOES NOT ILLUMINATE WITH TEST. CLEANED ELECT CONNECTOR NR 1 ENGINE, OPS CHECK OK IAW B727 M/M 2 6-11-01. 2 L 7 3 4F A3WE 2002050300061 20020503 00061 WP 2002 5 3 P2EA2002M030 1 20020430 A 7931 PRESSURE SWITCH DOUG DC9 DC982 3022082 WP OIL SYSTEM FAULTY A P2EA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 05 140NJ 49931 AT CRUISE ALTITUDE IN ROUTE FROM LAX TO MCI THE NR 2 ENGINE OIL STRAINER LIGHT FLICKERED. AIRCRAFT DIVERTED TO LAS AND LANDED WITH NO INCIDENT. REMOVED AND REPLACED NR 2 ENGINE OIL STRAINER FILTER IAW MM 79-20-01. DEFERRED INDICATION SYS TEM. REMOVED AND REPLACED DIFFERENTIAL PRESSURE SWITCH AND OPERATIONAL CHECKED IAW MM 79-35-01. 2 L 7 2 4F A6WE 2002050300062 20020503 00062 NM 2002 5 3 QXEA0200621 1 20020403 A 5320 FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX- RIGHT WING TO FUSELAGE JOINT BATHTUB FITTING AT FRONT SPAR HAS SCRIBE MARKS. REPAIRED IAW HORIZON AIR EA 2-53-382. 2 H 7 2 4T RT A13NM 2002050300063 20020503 00063 NM 2002 5 3 QXEA0200669 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- SCRATCH INSIDE LT INBOARD SEAT TRACK X328.25. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002050300064 20020503 00064 NM 2002 5 3 QXEA0200670 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- WEAR INSIDE LT INBOARD SEAT TRACK FROM X285.0 TO 296.5. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002050300065 20020503 00065 NM 2002 5 3 QXEA0200673 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- WEAR IN LT INBOARD SEAT TRACK FROM X278.5 TO X283.0. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002050300066 20020503 00066 NM 2002 5 3 QXEA0200674 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- WEAR IN LT INBOARD SEAT TRACK FROM X266.0 TO X270.5. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002050300067 20020503 00067 NM 2002 5 3 QXEA0200675 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- CORROSION ON LT INBOARD SEAT TRACK AT STATION X222.0. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-4698. 2 H 7 2 4T RT A13NM 2002050300068 20020503 00068 NM 2002 5 3 QXEA0200676 1 20020414 A 5320 WEB DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- CORROSION ON WEB CLOSET AT X222 ATTACHED TO LEFT HAND INBOARD SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8- 53-4698. 2 H 7 2 4T RT A13NM 2002050300069 20020503 00069 NM 2002 5 3 QXEA0200677 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- CORROSION ON LEFT HAND INBOARD SEAT TRACK FROM X208.75 TO 212.75. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-4698. 2 H 7 2 4T RT A13NM 2002050300070 20020503 00070 NM 2002 5 3 QXEA0200678 1 20020418 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- DENT IN BELLY SKIN 1.5 INCHES RIGHT OF CENTER LINE, LOCATED 2 INCHES FORWARD OF FRAME 136.800. REPAIRED IAW HORIZO N AIR EA 2-53-388. 2 H 7 2 4T RT A13NM 2002050300071 20020503 00071 NM 2002 5 3 QXEA0200679 1 20020416 A 5410 TAIL CONE DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- RIGHT NACELLE TAIL CONE AFT SIDE HAS CHAFING ON INBOARD SIDE BY NUT PLATES. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002050300072 20020503 00072 NM 2002 5 3 QXEA0200680 1 20020420 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM LT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- THERE IS A DEEP SCRATCH ON UPPER SKIN AT STATION YW199.00 ON LT WING. REPAIRED IAW DHC-8 SRM 51-20-11 AND 51-20-56 . 2 H 7 2 4T RT A13NM 2002050300073 20020503 00073 NM 2002 5 3 QXEA0200681 1 20020411 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- THERE IS A DEEP SCRATCH ON LEADING EDGE MATTING SURFACE OF LT WING FORWARD SPAR UPPER LIP FROM YW171.000 TO YW202.0 00. REPAIRED IAW RD 8-57-1119. 2 H 7 2 4T RT A13NM 2002050300074 20020503 00074 NM 2002 5 3 QXEA0200682 1 20020413 A 5730 FLANGE DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- GOUGE IN RIGHT HAND WING LEADING EDGE TOP FLANGE AT YW207.00. REPAIRED IAW DHC-8 SRM 51-20-36 AND RD 8-57-1675. 2 H 7 2 4T RT A13NM 2002050300075 20020503 00075 NM 2002 5 3 QXEA0200683 1 20020413 A 5730 FLANGE DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- GOUGES AROUND NUT PLATE ON RT WING LEADING EDGE TOP FLANGE AT YW285.00. REPAIRED IAW DHC-8 SRM 51-20-36 AND RD 8-5 7-1675. 2 H 7 2 4T RT A13NM 2002050300076 20020503 00076 NM 2002 5 3 QXEA0200684 1 20020412 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- SCRATCHES AND TOOLING MARKS ON BACK SIDE OF APERTURE FOR PANEL 623AT AT YW161.50. REPAIRED IAW DHC-8 SRM 51-20-11 AND 20-32-012. 2 H 7 2 4T RT A13NM 2002050300077 20020503 00077 NM 2002 5 3 QXEA0200685 1 20020419 A 5330 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- DAMAGED COUNTERSINK HOLE ON AFT UPPER PANEL FASTENER HOLE FORWARD RIGHT HAND FUSELAGE SKIN ADJACENT TO PANEL 122AR. REPAIRED IAW DHC-8 RD 8-53-4317. 2 H 7 2 4T RT A13NM 2002050300078 20020503 00078 NM 2002 5 3 QXEA0200686 1 20020414 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- WEAR IN LT OUTBOARD SEAT TRACK FROM X277.5 TO X282.0. REPAIRED IAW DHC-8 SRM 51-10-4 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002050300079 20020503 00079 NM 2002 5 3 QXEA0200688 1 20020418 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- DENT IN FUSLAGE SKIN 1.5 INCHES AFT OF CENTERLINE. REPAIRED IAW HORIZON AIR EA 2-53-388. 2 H 7 2 4T RT A13NM 2002050300080 20020503 00080 NM 2002 5 3 QXEA0200689 1 20020418 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- PANEL 524 AT SECOND RIB FROM OUTBOARD HAS CHAFE DAMAGE AT FUEL WIGGINGS FITTING. REPAIRED IAW HORIZON AIR EA 2-57- 161. 2 H 7 2 4T RT A13NM 2002050300081 20020503 00081 NM 2002 5 3 QXEA0200690 1 20020415 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- PANEL 524BT HAS FRETTING CORROSION ON OUTBOARD FLANGE. REPAIRED IAW DHC-8 SRM 51-20-16 AND RD 57-320. 2 H 7 2 4T RT A13NM 2002050300082 20020503 00082 NM 2002 5 3 QXEA0200691 1 20020415 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- PANEL 524BT HAS FRETTING CORROSION ON OUTBOARD FLANGE. REPAIRED IAW DHC-8 SRM 51-20-16 AND RD 8-57-320. 2 H 7 2 4T RT A13NM 2002050300083 20020503 00083 NM 2002 5 3 QXEA0200692 1 20020415 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- PANEL 524CT HAS FRETTING CORROSION ON OUTBOARD FLANGE. REPAIRED IAW DHC-8 SRM 51-20-16 AND RD 8-57-320. 2 H 7 2 4T RT A13NM 2002050300084 20020503 00084 NM 2002 5 3 QXEA0200694 1 20020414 A 2572 FRAME DHAV DHC8 DHC8202 2809007 NM AVIONICS RACK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- FORWARD LT UNDERFLOOR OF PASSENGER CABIN HAS CORROSION ON TOP FRAME OF AVIONICS RACK, ALSO ON NUT PLATES. REPAIRED IAW DHC-8 SRM 51-40-11, 51-20-11 AND 51-20-36. 2 H 7 2 4T RT A13NM 2002050300085 20020503 00085 NM 2002 5 3 QXEA0200695 1 20020414 A 2572 FRAME DHAV DHC8 DHC8202 2809007 NM AVIONICS RACK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- FORWARD LT UNDERFLOOR OF PASSENGER CABIN HAS CORROSION ON TOP FRAME FOR AVIONICS RACK AT STATION 201.150. REPAIRED IAW DHC-8 SRM 51-20-36 AND 51-20-11. 2 H 7 2 4T RT A13NM 2002050300086 20020503 00086 NM 2002 5 3 QXEA0200696 1 20020414 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- LT CABIN UNDERFLOOR HAS CORROSION AT FRAME 302.400 AND STRINGER 25 ON FLOOR SKIN. REPAIRED IAW DHC-8 SRM 51-20-36 AND 51-20-11. 2 H 7 2 4T RT A13NM 2002050300087 20020503 00087 NM 2002 5 3 QXEA0200697 1 20020415 A 5420 MECHANISM DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- RT WHEEL WELL AFT DOOR MECHANISM IS CHAFED. REPAIRED IAW DHC-8 RD 8-54-1052. 2 H 7 2 4T RT A13NM 2002050300088 20020503 00088 NM 2002 5 3 QXEA0200699 1 20020415 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- CARGO DOOR BOTTOM RIVET HEADS ARE DAMAGED NEXT TO LOWER RUBBER BUMPER, AND NEXT TO LOWER DOOR STOP MOUNT. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002050300089 20020503 00089 NM 2002 5 3 QXEA0200700 1 20020416 A 5410 TAIL CONE DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- RIGHT NACELLE INSIDE TAIL CONE THERE IS CHAFING TO THE UNDERSIDE OF DECK. REPAIRED IAW DHC-8 RD 8-54-097. 2 H 7 2 4T RT A13NM 2002050300090 20020503 00090 NM 2002 5 3 QXEA0200709 1 20020417 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- CARGO DOOR, LOWER EDGE OF SKIN AT FORWARD DOOR STOP IS BENT. REPAIRED IAW HORIZON AIR EA 2-52-125. 2 H 7 2 4T RT A13NM 2002050300091 20020503 00091 NM 2002 5 3 QXEA0200710 1 20020416 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- CARGO DOOR EXTERNAL SKIN, TOP FORWARD AREA HAS CHAFE DAMAGE. REPAIRED IAW DHC-8 SRM 52-20-16, SRM 51-20-11, PG 3 & 6, SRM 51-20-16, PG 2-4, SRM 51-20-36 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2002050300093 20020503 00093 NM 2002 5 3 DHL2002726510 1 20020415 A 5312 PRESSURE PANEL BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, NOSE WHEEL WELL LEFT SIDEWALL BULKHEAD BS 243, WL 150 CRACK INDICATION ABOUT 2.5 INCH LONG. NDT VERIFIE D. CUT-OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW B-727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002050300097 20020503 00097 2002 5 3 QXEA0200698 4 20020415 A 3445 PLATE DHAV DHC8 DHC8202 2809007 NM TCAS ANTENNA CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- THE BASE PLATE HAS CORROSION ON THE AFT TCAS ANTENNA. REPAIRED IAW DHC-8 SRM 20-32-02 AND 53-00-16. 2 H 7 2 4T RT A13NM 2002050300099 20020503 00099 NM 2002 5 3 QXEA0200711 1 20020411 A 7110 ANGLE DHAV DHC8 DHC8202 2809007 NM NR 1 COWLING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- NR 1 ENGINE COWL LOWER DECK, AFT EDGE ANGLE CHAFED ALONG ENTIRE LENGTH. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002050300100 20020503 00100 NM 2002 5 3 QXEA0200712 1 20020411 A 7110 COWLING DHAV DHC8 DHC8202 2809007 NM NR 1 ENGINE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- NR 1 ENGINE COWL, LOWER DECK RIGHT HAND CORNER IS CHAFED ALONG AFT EDGE. REPAIRED IAW DHC-8 SRM 51-20-11 PG 4. 2 H 7 2 4T RT A13NM 2002050300101 20020503 00101 NM 2002 5 3 QXEA0200713 1 20020412 A 7110 PAD DHAV DHC8 DHC8202 2809007 NM NR 1 COWLING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- NR 1 ENGINE LOWER COWL BOTH CHAFE PADS AT TOP FORWARD LATCHES ARE CHAFED. REPAIRED IAW DHC-8 RD 8-71-018 AND DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002050300102 20020503 00102 NM 2002 5 3 QXEA0200714 1 20020419 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX-LOWER RT INBOARD WING SPAR IS HEAVILY CHAFED AND TEFLON PAINT IS MISSING. REPAIRED IAW DHC-8 RD8-57-811 AND SRM 51- 20-26. 2 H 7 2 4T RT A13NM 2002050300104 20020503 00104 NM 2002 5 3 QXEA0200715 1 20020420 A 2770 BRACKET DHAV DHC8 DHC8202 2809007 NM GUST LOCK LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- ELEVATOR GUST LOCK BRACKETS, BOTH ARE LOOSE AND SMOKING. REPAIRED IAW DHC-8 RD 8-55-112, SRM 27-32-11, PG 402, 403 AND SRM 27-70-11, PG 401. 2 H 7 2 4T RT A13NM 2002050300108 20020503 00108 NM 2002 5 3 QXEA0200716 1 20020423 A 5420 BRACKET DHAV DHC8 DHC8202 2809007 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- RIGHT NACELLE, INSIDE TAIL CONE REFUEL/DEFUEL VALVE MOUNT BRACKET IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 28-25-11. 2 H 7 2 4T RT A13NM 2002050300109 20020503 00109 NM 2002 5 3 QXEA0200717 1 20020423 A 5320 SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- ATTACH POINT HOLE FOR NR 7 SEAT TRACK AT STATION X370.80 SUPPORT BEAM IS OVERSIZED. REPAIRED IAW HORIZON AIR EA 2- 53-389. 2 H 7 2 4T RT A13NM 2002050300110 20020503 00110 NM 2002 5 3 QXEA0200718 1 20020423 A 5320 SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- ATTACH POINT HOLE FOR NR 7 SEAT TRACK AT STATION X354.25 SUPPORT BEAM IS OVERSIZED. REPAIRED IAW HORIZON AIR EA 2- 53-389. 2 H 7 2 4T RT A13NM 2002050300111 20020503 00111 NM 2002 5 3 QXEA0200719 1 20020423 A 5320 SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- ATTACH POINT FOR NR 7 SEAT TRACK AT STATION X333.30 SUPPORT BEAM IS OVERSIZED. REPAIRED IAW HORIZON AIR EA 2-53-38 9. 2 H 7 2 4T RT A13NM 2002050300112 20020503 00112 NM 2002 5 3 QXEA0200720 1 20020423 A 5320 SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- ATTACH POINT HOLE FOR NR 7 SEAT TRACK AT STATION X312.35 SUPPORT BEAM IS OVERSIZED. REPAIRED IAW HORIZON AIR EA 2- 53-389. 2 H 7 2 4T RT A13NM 2002050300113 20020503 00113 NM 2002 5 3 QXEA0200721 1 20020423 A 5320 SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- ATTACH POINT HOLE FOR NR 7 SEAT TRACK AT STATION X291.40 SUPPORT BEAM IS OVERSIZED. REPAIRED IAW HORIZON AIR EA 2- 53-389. 2 H 7 2 4T RT A13NM 2002050300115 20020503 00115 NM 2002 5 3 QXEA0200722 1 20020423 A 5320 SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- ATTACH POINT HOLE FOR NR 7 SEAT TRACK AT STATION X290.50 SUPPORT BEAM IS OVERSIZED. REPAIRED IAW HORIZON AIR EA 2- 53-389. 2 H 7 2 4T RT A13NM 2002050300116 20020503 00116 NM 2002 5 3 QXEA0200723 1 20020423 A 5320 SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- ATTACH POINT HOLE FOR NR 7 SEAT TRACK AT STATION X252.70 SUPPORT BEAM IS OVERSIZED. REPAIRED IAW HORIZON AIR EA 2- 53-389. 2 H 7 2 4T RT A13NM 2002050300117 20020503 00117 NM 2002 5 3 QXEA0200724 1 20020423 A 5320 SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- ATTACH POINT HOLE FOR NR 7 SEAT TRACK AT STATION X240.5 SUPPORT BEAM IS OVERSIZED. REPAIRED IAW HORIZON AIR EA 2-5 3-389. 2 H 7 2 4T RT A13NM 2002050300118 20020503 00118 NM 2002 5 3 QXEA0200725 1 20020423 A 5320 SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- ATTACH POINT HOLE FOR NR 7 SEAT TRACK AT STATION X222.70 SUPPORT BEAM IS OVERSIZED. REPAIRED IAW HORIZON AIR EA 2- 53-389. 2 H 7 2 4T RT A13NM 2002050300119 20020503 00119 NM 2002 5 3 QXEA0200726 1 20020423 A 5320 SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- ATTACH POINT HOLE FOR NR 7 SEAT TRACK AT STATION X202.72 SUPPORT BEAM IS OVERSIZED. REPAIRED IAW HORIZON AIR EA 2- 53-389. 2 H 7 2 4T RT A13NM 2002050300121 20020503 00121 NM 2002 5 3 QXEA0200727 1 20020413 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- PANEL 511AL OUTBOARD UPPER NUT PLATE BRACKET APPEARS TO BE CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002050300123 20020503 00123 NM 2002 5 3 QXEA0200728 1 20020413 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- PANEL 511AL OUTBOARD LOWER NUT PLATE BRACKET APPEARS TO BE CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002050300124 20020503 00124 NM 2002 5 3 QXEA0200729 1 20020423 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- NR 7 SEAT TRACK HAS INTERGRANULAR CORROSION IN SEVERAL PLATES. REPAIRED IAW DHC-8 RD8-53-1102, SRM 20-09-06, PG 20 1 AND HORIZON AIR EA 2-53-389. 2 H 7 2 4T RT A13NM 2002050300125 20020503 00125 2002 5 3 QXEA0200730 4 20020420 A 3445 ANTENNA DHAV DHC8 DHC8202 2809007 NM TCAS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- LOWER TCAS ANTENNA HAS CORROSION AT AIRCRAFT SIDE. REPAIRED IAW DHC-8 SRM 53-00-16 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002050300126 20020503 00126 NM 2002 5 3 QXEA0200731 1 20020422 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX- STRUCTURE IS GOUGED. ADJACENT TO HORIZONTAL ATTACH HI-LOKS AT FORWARD END OF NEW NR 7 SEAT TRACK. REPAIRED IAW DH C-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002050300127 20020503 00127 EA 2002 5 3 QXEA0200733 1 20020428 A 2121 GG670950225 FAN CNDAIR CL600 CL6002C10 1390015 EA CABIN MALFUNCTIONED A QXEA K NONE J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 603QX 951 951 10011 BOI- RECIRCULATION FAN FAULT (WHITE). CIRCUIT BREAKER A2 POPPED AND HOT PLASTIC SMELL. REMOVED AND REPLACED RECIRCULAT ION FAN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002050300128 20020503 00128 NM 2002 5 3 SABA020055 1 20020429 A 3350 101307150 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 841PH 082 AIRCRAFT 841 ON FLIGHT 5012 FROM CLT TO TLH. DURING INSPECTION PRIOR TO DEPARTURE MAINTENANCE FOUND FLOOR EMERGENCY LIG HT AT ROW 6 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPS CHECK WAS GOOD. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2002050300129 20020503 00129 EU 2002 5 3 SDRO2002004 1 20020418 A 2822 1176415103 PUMP BOLKMS 117 BK117A3 5626015 EU FUEL SYSTEM LEAKING E R7MA K NONE K FLUID LOSS LD LANDING 1 NM 07 117NY 10 7110 UPON LANDING, CREW SMELLED FUEL ODOR. FOUND FUEL POURING FROM FUEL PUMP ACCESS PANEL ON BOTTOM OF FUSELAGE. 1 G 7 2 3U H13EU 2002050300130 20020503 00130 2002 5 3 SWAA020797 4 20020415 A 2565 D31354 SLIDE BOEING 737 7372K6 1364440 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002050300131 20020503 00131 NM 2002 5 3 SWAA020798 1 20020415 A 3350 BR2013 LIGHT BOEING 737 7372K6 1364440 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE IN AFT CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002050300132 20020503 00132 NM 2002 5 3 SWAA020802 1 20020416 A 7797 332A1023 WIRE BOEING 737 7373H4 1384600 NM NR 2 ENGINE CHAFED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 608SW 27928 AIR TURNBACK, DURING CLIMB NR 2 ENG EGT INDICATION WARNING, LIGHT ILLUMINATED. FOUND CHROMMEL EGT WIRE CHAFING NEAR PYL ON DISCONNECT. REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 2002050300133 20020503 00133 NM 2002 5 3 SWAA020804 1 20020412 A 2530 41600019 COFFEEMAKER BOEING 737 7373H4 1384600 NM GALLEY OVERHEATED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 653SW 28398 BURNING, SMOKE SMELL COMING FROM AFT GALLEY. REMOVED AND REPLACED AFT RT COFFEEMAKER PER MM. 2 L 7 2 4F RT A16WE 2002050300134 20020503 00134 NM 2002 5 3 SWAA020807 1 20020418 A 3350 6104781 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002050300135 20020503 00135 2002 5 3 SWAA020808 4 20020417 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER INADVERTENTLY. RE INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002050300136 20020503 00136 2002 5 3 SWAA020809 4 20020418 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 602SW 27953 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. RE INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002050300137 20020503 00137 NM 2002 5 3 SWAA020813 1 20020418 A 2731 6545166 ROD END BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED RON, SWA SI 11111-55, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED B OTH LT AND RT ELEVATOR TAB OUTBOARD ROD END ASSY'S PER MM. 2 L 7 2 4F RT A16WE 2002050300138 20020503 00138 NM 2002 5 3 SWAA020814 1 20020417 A 2731 6545166 ROD END BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 615SW 27698 DURING SCHEDULED PM CHECK, SWA SI 11111-55, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY INSPECTION. REMOVED AND REPLA CED BOTH LT AND RT ELEVATOR TAB OUTBOARD ROD END ASSY'S PER MM. 2 L 7 2 4F RT A16WE 2002050300139 20020503 00139 NM 2002 5 3 PCAA0205053 1 20020502 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM 300 INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 834EX 8370 8370 285 DURING ROUTINE MAINTENANCE VISIT LEFT EXTERIOR AFT EMERGENCY LIGHT FOUND INOPERATIVE. BULB, HARNESS, BATTERY AND 2 BATTE RY LIGHT POWER SUPPLIES WERE REPLACED. OPERATIONAL CHECK GOOD.AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002050300140 20020503 00140 NM 2002 5 3 02050301 1 20020501 A 3350 LIGHT BOEING 757 757236 1384971 NM CABIN INOPERATIVE A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 522NA 25133 EMERGENCY LIGHT FOR SEAT 22 A/B/C INOP. REMOVED AND REPLACED E-PATH LIGHT AT 22 A/B/C AS PER M/M 33-51-11; OPS CHECK GOO D. 2 L 7 2 4F RT A2NM 2002050300142 20020503 00142 NM 2002 5 3 UPS02238111 1 20020422 A 5330 SKIN BOEING 727 727180C 138406G NM BS479STR26R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C CORROSION FOUND AT LAP SKINS BS 479 STRINGER 26R FASTENERS REMOVED IAW SRM51-30-02, UPUPER SKIN CU T OUT BETWEEN BS 47 2-485, NDT NDF, REPAIR PARTS FABRICATED IAW AND INSATLLED IAW EO B72 7-5330-16775. 2 L 7 3 4F A3WE 2002050300143 20020503 00143 NM 2002 5 3 UPS02438116 1 20020503 A 5310 STRINGER BOEING 747 747200 1384847 NM STA 1148 25L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:N/A CORROSION STA 1148 STRINGER 25L TO 26L ***MRR FILED AS OPEN**** 2 L 7 4 4F RT A20WE 2002050300144 20020503 00144 WP 2002 5 3 DHL2002806010 1 20020502 A 2900 HYDRAULIC LINE DOUG DC8 DC873F 302199F WP A DHLA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 01 806DH 46002 1) PRIOR TO TAKEOFF, LOSS OF HYDRAULIC FLUID LEAD TO DECISION TO RETURN TO THE RAMP. DURING TAXI BACK QUANTITY FELL TO EMERGENCY LEVEL AND HYDAULIC SYSTEM AND BRAKE PRESSURES BEGAN DECREASING. STPPED TAXI AND SET BRAKES FOR TOW IN2) FOUN D HOLE IN T/R PUMP SUPPLY LINE. REPLACED LINE PER DACO 70 M/M 78-36-2. SERVICED T/R RES. PER DACO 70 M/M 78-36-2 AND MAIN RES. PER DACO M/M 12-30-1. OP AND LEAK CHECKS GOOD. 2 L 7 4 4F RT 4A25 2002050300145 20020503 00145 WP 2002 5 3 DHL2002807541 1 20020406 A 5730 SKIN DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM REF.: N/R 0694 RT. WING T/E SKIN CRACKED 1/4 INCK , STA. XW795.000 - 761.694CORR: REMOVED CRACKED SKIN IAW SRM57-2- 1 FIG. 25 FABRICATED SKIN ( 2024T3 .032) IAW SRM57-2-1 FIG.2S CLEANED, TREATED AND PRIMED IAW SRM51-1-8B , INSTALLED T/E SKIN IAW SRM57-2-1 FIG. 2S 2 L 7 4 4F RT 4A25 2002050300146 20020503 00146 NM 2002 5 3 02FDEA00307 1 20020503 A 2780 FLAP BOEING 727 727233 138408A NM FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 258FE 20940 02-108 RIGHT INBD LEADING EDGE FLAP #5 FAILED TO RETRACT WHEN FLAPS 2 WAS SELECTED. ** S/D ** COMING 2 L 7 3 4F RT A3WE 2002050300147 20020503 00147 WP 2002 5 3 DHL2002807542 1 20020409 A 5313 FRAME DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: 0952 MAIN CARGO COMPT- 2" CRACK ON FRAME STA. 1580.000 , L21RCORR: REMOVED FASTNERS IAW SRM 51-11-20D PG. 21 CUT OUT DAMAGED AREA IAW SRM53-2-0 FIG.2 , CLEANED , TREATED AND PRIMED IAW SRM51-1-8B INSTALLED FRAME SPLICE IAW SRM 5 3-2-0 FIG2 2 L 7 4 4F RT 4A25 2002050300148 20020503 00148 WP 2002 5 3 DHL2002807543 1 20020410 A 2720 36194393 SUPPORT DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 2200 RUDDER- # 4 RUDDER SUPPORT FROM REAR SPAR CRACKEDCORR: REPLACED # 4 RUDDER SUPPORT ( REAR SPAR ) IA W OHM 27-20-1, PG. 1-2 REFER TO N/R 2387 FOR OP'S CHECK 2 L 7 4 4F RT 4A25 2002050300149 20020503 00149 EA 2002 5 3 SWIA200210816 1 20020424 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA FIRST OFFICER'S CRACKED A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 588SW 7069 RIGHT WINDSCREEN CRACKED WHILE ON THE GROUND. REPLACED FIRST OFFICER'S WINDSHIELD IAW 56-11-01. OPS CHECK GOOD. PN ON 601R33033-14 SN OFF 95032H2520. 2 L 7 2 4F RT A21EA 2002050300150 20020503 00150 WP 2002 5 3 DHL2002807544 1 20020407 A 2710 5705334501 AILERON DOUG DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 1756 LT. WING INBD AILERON UPPER SKIN CRACKED 1/2" @ STA. XW563.000CORR.: PERFORMED MAJOR REPAIR IAW E.O . DHL020320 , ED2861 , EO SEMANS 2002262. TRIMMED OUT CRACKED SKIN IAW EO DHL020320,ED2861,EO SEMANS 2002262. CLEANED , TREATED , PRIMED AREA IAW SRM51-1-8B FABRICATED NEW SKIN (2024T3AL.050) AND A FILLER (2024T3.025) CLEANED , TREATED , PR IMED IAW SRM51-1-8B. INSTALLED NEW SKIN, ANGLE & STRAP & FILLERIAW EODHL020320,ED2861,EO SEMANS 200262. 2 L 7 4 4F RT 4A25 2002050300151 20020503 00151 WP 2002 5 3 DHL2002807545 1 20020416 A 2710 5705334501 AILERON DOUG DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 1754 LT. INBD. AILERON L/E UPPER SKIN CRACKED .250 @ STA. XA508.000CORR: PERFORMED MAJOR REPAIR IAW DHL EO020422, ED2893 , EO SEMANS 2002287 2 L 7 4 4F RT 4A25 2002050300152 20020503 00152 WP 2002 5 3 DHL2002807546 1 20020402 A 5313 3779659501 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 0976 MAIN CARGO COMPARTMENT - 3" CRACK IN BATHTUB FITTING (STA. 847.000-857.125,L6L) CORR: REMOVED CRACK ED BATHTUB FITTING IAW SRM51-1-20D , PG. 21, CLEANED TREATED PRIMED AND PAINTED AREA IAW SRM51-1-8B , INSTALLED NEW BATH TUB FITTING IAW SRM 51-1-20D PG.9 2 L 7 4 4F RT 4A25 2002050300153 20020503 00153 WP 2002 5 3 DHL2002807547 1 20020410 A 5313 FRAME DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 0950 MAIN CARGO COMPT.- 1" CRACK ON FRAME @ STA. 1580.000 L21LCORR: REMOVED FASTNERS IAW SRM 51-11-21 FI G. 2 FABRICATED FRAME SPLICE (7075T6.071) IAW SRM53-2-0 FIG. 2 CLEANED , TREATED , PRIMED IAW SRM 51-1-8B INSTALLED FRAM E SPLICE IAW 53-2-0 FIG. 2 SRM51-1-21 2 L 7 4 4F RT 4A25 2002050300154 20020503 00154 WP 2002 5 3 DHL2002807548 1 20020415 A 5313 3779659501 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM; ref.: N/R 0974 MAIN CARGO COMPT- 1 1/2" CRACK IN BATHTUB FITTING(STA. 847.000-857.125)L2RCORR: REMOVED CRACKED BAT HTUB FITTING IAW SRM51-1-20D PG. 21 CLEANED , TREATED , PRIMED SRM 51-1-8B , INSTALLED NEW BATHTUB FITTING IAW SRM 51-1- 20D pg 9 2 L 7 4 4F RT 4A25 2002050300155 20020503 00155 WP 2002 5 3 DHL2002807549 1 20020416 A 5313 3779659501 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R MAIN CARGO COMPT.- 2" CRACK IN BATHTUB FITTING STA. 847.000-857.125, L3LCORR.: REMOVED DAMAGED BATHTUB F ITTING IAW SRM 51-1-20D PG. 21 CLEANED , TREATED& PRIMED AREAIAW SRM51-1-8B INSTALLED NEW FITTING IAW SRM 51-1-20D PG. 9 2 L 7 4 4F RT 4A25 2002050300156 20020503 00156 WP 2002 5 3 DHL2002807550 1 20020415 A 5313 3779659501 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 0977 MAIN CARGO COMPT.- 3" CRACKIN BATHTUB FITTING (STA.847.000-857.125)L7LCORR.: REMOVED DAMAGED FITTIN G IAW SRM 51-1-20D PG. 21 CLEANED , TREATED , PRIMED IAW SRM 51-1-8B INSTALLED NEW FITTING IAW SRM 51-1-20D PG. 9 2 L 7 4 4F RT 4A25 2002050400001 20020504 00001 WP 2002 5 4 DHL2002807552 1 20020415 A 5313 FRAME DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R2003 MAIN CARGO COMPT.- FRAME CRACKED 3" @ STA.220.00 , L20R-L21RCORR: REMOVED FASTNERS IAW SRM51-1-20D P G. 21 SHEETS1,2,6 , FABRICATED NEW FRAME SEGMENT(7075T651) IAW SRM 53-2-0 FIG. 2 SHEET 1,2,6, DWG8530008, EA SEMANS20023 01, FABRICATED SPLICE DOUBLER(7075T6) IAW SRM53-2-0 FIG. 2SHEETS 1,2,6 CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B , IN STALLED NEW FRAME SEGMENTS AND SPLICE DOUBLER IAW SRM 53-2-0 FIG. 2 SHEETS 1,2,6 SRM51-1-20D PG.9 2 L 7 4 4F RT 4A25 2002050400002 20020504 00002 WP 2002 5 4 DHL2002807553 1 20020416 A 5313 FRAME DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 2004 MAIN CARGO COMPT-FRAME FLANGE CRACKED 2.5" @ STA. 260.000 L20R-L21RCORR: REMOVED FASTNERS IAW SRM51 -1-20D PG. 21 CUT OUT FRAME AREA DETERIORATED IAW SRM53-2-0 FIG.2 SHEET 1,2,6, DWG. SR0530008. FABRICATED FRAME SEGEMENT S (7075T651) IAW SRM53-2-0 FIG.2 SHEET 1,2,6 CLEANED, TREATED AND PRIMEDSEGMENT AND DOUBLER IAW SRM51-1-8B. INSTALLED FR AME SEGMENT AND SPLICE DOUBLER IAW SRM 53-2-0 FIG. 2 SHEETS 1,2,6 AND SRM 51-1-20D PG.9 2 L 7 4 4F RT 4A25 2002051300043 20020513 00043 NM 2002 5 13 DHL2002726516 1 20020417 A 5313 STRINGER BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, CABIN BS 720B STR 15 L IS CRACKED FWD OF WING LIGHT. FABRICATED NEW ANGLE CHANNEL AND DOUBLER IAW 53-10 -3 FIG 5. INSTALLED NEW ANGLE CHANNEL IAW B-727 SRM 51-30-2 SRM 53-10-3 FIG 5. PRESSURE CHECK GOOD IAW B-727 21-30-0. 2 L 7 3 4F RT A3WE 2002050400003 20020504 00003 WP 2002 5 4 DHL2002807554 1 20020413 A 2750 74593712 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: REF.: N/R 1124 RT. WING FLAP ACTUATOR (LWR) ATTACH FITTING CRACKED 1" @ STA. 339.000CORR: R/R RH FLAP ACTUATOR LOW ER ATTCH FITTING IAW OHM27-28-8 PG. 3 REFER TO N/R 2387 FOR OP'S CHECK 2 L 7 4 4F RT 4A25 2002050400004 20020504 00004 WP 2002 5 4 DHL2002807555 1 20020417 A 5312 47504261 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM: N/R 2197 AFT ACCY COMPT- PRESSURE BULKHEAD FITTING CRACKED BTWN. L36 -L35L, STA.683.548REMOVED DAMAGED FITTING IAW SRM51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM51-1-8B INSTALLED NEW FITTING IAW 51-1-21 PG.1 2 L 7 4 4F RT 4A25 2002050400005 20020504 00005 WP 2002 5 4 DHL2002807556 1 20020417 A 5720 36514451 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 81797 45990 ITEM REF.: N/R 1758 LH WING T/E FITTING HAS A 2" CRACK, XRS410.000REMOVED DAMAGED FITTING AT STA. XRS 410.000 IAW SRM51- 3-0 PG.1 CLEANED , TREATED AND PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW FITTING IAW SRM51-3-0 PG1 2 L 7 4 4F RT 4A25 2002050500001 20020505 00001 SO 2002 5 5 C2XA02TY076 1 20020505 A 5312 14523220401 BULKHEAD EMB 145 EMB145 3260210 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS, During a schedule inspection the forward pressure bulkhead was found gouged under the windshield wiper moter. Maint enance blended out the damage, performed dye penetrant inspection, alodined and primed I/A/W-EMB-135/145-CPM-51-21-04,51 -21-05 and GST-1423/02. The repair procedure was satisfactory and the aircraft will be released upon complection of insp ection. 2 L 7 2 4F RT T00011AT 2002050600003 20020506 00003 NM 2002 5 6 SWAA020908 1 20020501 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 715SW 27849 EEPLS COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002050600004 20020506 00004 NM 2002 5 6 SWAA020909 1 20020428 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 405WN 27893 EEPLS COVER BROKEN AT OVERWING EXIT. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002050600005 20020506 00005 2002 5 6 SWAA020912 4 20020501 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F A16WE 2002050600006 20020506 00006 NM 2002 5 6 SWAA020915 1 20020501 A 3233 65446104 ACTUATOR BOEING 737 7375H4 138449D NM NLG MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 527SW 26569 DIVERSION, AFTER T/O NLG WOULD NOT RETRACT, CYCLED THE GEAR TWICE AND NLG RETRACTED. ALL GEAR EXTENDED NORMALLY FOR LAN DING. REMOVED AND REPLACED NLG ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2002050600007 20020506 00007 NM 2002 5 6 SWAA020916 1 20020430 A 5512 65C25727 SKIN BOEING 737 7375H4 138449D NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED C4 CHECK, FOUND HORIZ STAB SKIN CRACKED AT STA 108 OF THE STAB REAR SPAR. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002050600008 20020506 00008 NM 2002 5 6 SWAA020917 1 20020501 A 5312 6516300 BULKHEAD BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 213, LBL 7 AND LBL 5.0. REPAIRED WEB PE R SRM. 2 L 7 2 4F RT A16WE 2002050600009 20020506 00009 NM 2002 5 6 SWAA020918 1 20020430 A 5320 AND10133 WEB BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A VNAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED SPECIAL VISIT, FOUND HORIZONTAL WEBS CRACKED (2 EA) AT BS 180, WL 207, RBL 25.0 AND LBL 25.0. REPAIRED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2002050600038 20020506 00038 WP 2002 5 6 COOSDR 02102 1 20020401 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 STA 1690 BETWEEN LONGERON 21L AND LONG. 23L FRAME ANGLE CORRODED. 2 L 7 4 4F RT 4A25 2002050600039 20020506 00039 WP 2002 5 6 COOSDR020064 1 20020401 A 5340 3755843501 FITTING DOUG DC8 DC873F 302199F WP LWR FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT CARGO COMPARTMENT, FITTING CRACKED, LOCATED AT STA Y =1200 BETWEEN LONG 34R AND LONG 35R. 2 L 7 4 4F RT 4A25 2002050600040 20020506 00040 WP 2002 5 6 COOSDR020065 1 20020401 A 5340 3755842505 FITTING DOUG DC8 DC873F 302199F WP LWR FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT CARGO COMPARTMENT, FITTING CRACKED, LOCATED AT STA Y=1200 BETWEEN LONG 27L AND LONG 28L. 2 L 7 4 4F RT 4A25 2002050600041 20020506 00041 WP 2002 5 6 COOSDR020091 1 20020401 A 5340 37584982 FITTING DOUG DC8 DC873F 302199F WP LWR FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT CARGO COMPARTMENT, FITTING, LOCATED AT STA Y=1240 AT LONG 35R. 2 L 7 4 4F RT 4A25 2002050600042 20020506 00042 WP 2002 5 6 COOSDR020092 1 20020401 A 5340 4758514517 FITTING DOUG DC8 DC873F 302199F WP LWR FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT CARGO COMPARTMENT, FITTING, LOCATED AT STA Y= 1140 BETWEEN LONG 33R AND 34R. 2 L 7 4 4F RT 4A25 2002050600043 20020506 00043 WP 2002 5 6 COOSDR020093 1 20020401 A 5340 37540472 FITTING DOUG DC8 DC873F 302199F WP LWR FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT CARGO COMPARTMENT, FITTING, LOCATED AT STA Y=1227 BETWEEN LONG 21R AND 22R. 2 L 7 4 4F RT 4A25 2002050600044 20020506 00044 WP 2002 5 6 COOSDR020096 1 20020401 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT CARGO COMPARTMENT BETWEEN STA Y 1340 INCH TO STA Y1360 INCH LONG 36 CRACKED. 2 L 7 4 4F RT 4A25 2002050600045 20020506 00045 WP 2002 5 6 COOSDR020097 1 20020401 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT CARGO COMPARTMENT, BETWEEN STA Y1340 TO STA Y1360 LONG 35 RIGHT, CRACKED. 2 L 7 4 4F RT 4A25 2002050600046 20020506 00046 WP 2002 5 6 COOSDR020098 1 20020401 A 5313 3619434503 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT LOWER CARGO COMPARTMENT BETWEEN STA Y1480 TO STA Y1500 LONGERON SPLICE 32 RIGHT, CORRODED. 2 L 7 4 4F RT 4A25 2002050600047 20020506 00047 WP 2002 5 6 COOSDR020099 1 20020401 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 MAIN CARGO CABIN, FLOORBEAM LOWER CHORD ON STA Y857 BETWEEN +X60 TO -X60, CORRODED. 2 L 7 4 4F RT 4A25 2002050600048 20020506 00048 WP 2002 5 6 COOSDR020100 1 20020401 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 MAIN CARGO CABIN, FLOORBEAM LOWER CHORD ON STA Y980 BETWEEN +X45 TO -X25 CORRODED. 2 L 7 4 4F RT 4A25 2002050600049 20020506 00049 WP 2002 5 6 COOSDR02090 1 20020401 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT CARGO COMPARTMENT, STA Y:1354, LONGERON 30R CRACKED. 2 L 7 4 4F RT 4A25 2002050600050 20020506 00050 WP 2002 5 6 COOSDR02094 1 20020401 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 FWD CARGO COMPARTMENT, STA Y: 387, LONGERON 31 LT, CRACKED. 2 L 7 4 4F RT 4A25 2002050600051 20020506 00051 WP 2002 5 6 DHL2002805047 1 20020504 A 2500 BELT DOUG DC8 DC873F 302199F WP A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 1) F/O SEAT BELT NO TSO2) REMOVED AND REPLACED SEAT BELT PER M/M 25-10-0 2 L 7 4 4F RT 4A25 2002052000115 20020520 00115 WP 2002 5 20 DHL2002807004 1 20020503 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP NR 4 WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807DH 45990 NR 4 SMOKE DETECTOR DOES NOT TEST. RELAMPED NR 4 SMOKE DETECTOR IAW MM 26-10-5, OPS CHECK GOOD ON PRESS TO TEST. 2 L 7 4 4F RT 4A25 2002052000116 20020520 00116 WP 2002 5 20 DHL2002807005 1 20020504 A 2611 302314 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP NR 4 WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807DH 45990 NR 4 SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED NR 4 SMOKE DETECTOR, SYS TEST OK IAW 26-10-5. 2 L 7 4 4F RT 4A25 2002050600053 20020506 00053 NM 2002 5 6 SABA020057 1 20020504 A 3350 101307150 BULB DHAV DHC8 DHC8102 2809003 NM CABIN BURNED OUT A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 881CC 294 Aircraft 881 on flight 5027 from CLT to CVG. During preflight check a floor emergency light was found inoperative. Mai ntenance removed and replaced the bulb. Ops check was good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002050600060 20020506 00060 2002 5 6 SWAA020818 4 20020418 A 2565 61620468 SLIDE BOEING 737 7373Y0 1384671 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLID E PER MM. 2 L 7 2 4F RT A16WE 2002050600061 20020506 00061 NM 2002 5 6 SWAA020832 1 20020421 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 520 AT STR 16L AND BS 663 AT STR 10L. REMOVED AN D REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002050600062 20020506 00062 NM 2002 5 6 SWAA020837 1 20020421 A 2133 7110033 OUTFLOW VALVE BOEING 737 7372H4 138448C NM CABIN PRESSURE FAILED A SWAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 082SW 22731 DECLARED EMERGENCY, AIR TURNBACK. DURING CLIMB ALTITUDE HORN SOUNDED, CABIN CLIMBING 1000 FPM. STBY NO HELP, WORKED IN MANUAL. REMOVED AND REPLACED AFT OUTFLOW VALVE PER MM. 2 L 7 2 4F A16WE 2002050600063 20020506 00063 2002 5 6 SWAA020841 4 20020422 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT CABIN DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED C3 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2 L 7 2 4F A16WE 2002050600064 20020506 00064 NM 2002 5 6 SWAA020842 1 20020423 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED A1 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002050600065 20020506 00065 NM 2002 5 6 SWAA020845 1 20020422 A 2121 6454051 FAN BOEING 737 7373Q8 1384670 NM A/C BAY OVERTEMP A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 687SW 23388 ODOR DETECTED IN CABIN WHILE ON APPROACH TO MCI. REMOVED AND REPLACED RECIRCULATION FAN PER MM. 2 L 7 2 4F RT A16WE 2002050600066 20020506 00066 NM 2002 5 6 SWAA020849 1 20020419 A 5311 96380 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OUTBOARD CHORDS CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CH ORDS PER SWA ACO. 2 L 7 2 4F RT A16WE 2002050600067 20020506 00067 NM 2002 5 6 SWAA020850 1 20020419 A 5320 6517583 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL CHORD CRACKED AT BS 178, WL 184 AT LBL 5.7. REPAIRED CHORD PER SWA T1. 2 L 7 2 4F RT A16WE 2002050600068 20020506 00068 2002 5 6 SWAA020851 4 20020424 A 2565 D31354418 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002050600069 20020506 00069 NM 2002 5 6 SWAA020852 1 20020424 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 501SW 24178 EEPLS DAMAGED AT ROW 13. REMOVED AND REPLACED EEPLS AT ROW 13 PER MM. 2 L 7 2 4F RT A16WE 2002050600070 20020506 00070 NM 2002 5 6 SWAA020854 1 20020424 A 5320 6517583 STIFFENER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAMS CRACKED (2 EA) AT BS 180, LBL 5.7 AT WL 153 AND RBL 17.1 AT WL 230. R EPAIRED VERTICAL BEAMS PER SRM. 2 L 7 2 4F RT A16WE 2002050600071 20020506 00071 NM 2002 5 6 SWAA020857 1 20020422 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002050600072 20020506 00072 NM 2002 5 6 SWAA020860 1 20020423 A 5753 6546481 CARRIAGE BOEING 737 7372H4 138448C NM T/E FLAP CRACKED A SWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 07 074SW 22674 A/C HAS A LEFT ROLL TENDENCY AFTER FLAPS ARE LOWERED BEYOND 5 DEGREES. POSITION INDICATORS AND OVERHEAD INDICATE NORMAL . FOUND BOTH LT T/E FLAP NR 1 AND NR 2 CARRIAGE SPINDLES CRACKED. REMOVED AND REPLACED NR 1 AND NR 2 LT FLAP CARRIAGE ASSY'S PER MM. 2 L 7 2 4F A16WE 2002050600073 20020506 00073 NM 2002 5 6 SWAA020862 1 20020424 A 2731 6545166 ROD END BOEING 737 7373H4 1384600 NM ELEVATOR TAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED A2 CHECK, FOUND BOTH LT AND RT ELEVATOR TAB ROD ENDS CORRODED INBOARD AND OUTBOARD. REMOVED AND REPLAC ED ALL ELEVATOR TAB ROD ENDS PER MM. 2 L 7 2 4F RT A16WE 2002050600074 20020506 00074 2002 5 6 SWAA020863 4 20020425 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002050600075 20020506 00075 NM 2002 5 6 SWAA020864 1 20020422 A 5311 6516301 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED D-CHECK, FOUND LOWER CHORD CRACKED AT BS 188, WL 209 RT. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2002050600076 20020506 00076 NM 2002 5 6 SWAA020870 1 20020425 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT ROW 11. RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2002050600077 20020506 00077 2002 5 6 SWAA020871 4 20020426 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002050600078 20020506 00078 NM 2002 5 6 SWAA020882 1 20020426 A 2731 654516618 ROD END BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C4 CHECK, FOUND BOTH LT AND RT ELEVATOR TAB PUSH ROD ENDS WORN. REMOVED AND REPLACED TAB ROD ENDS PER MM. 2 L 7 2 4F RT A16WE 2002050600079 20020506 00079 SO 2002 5 6 SWIA200210796 1 20020417 A 3020 211117183 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO RT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 580SW 120348 RIGHT ENGINE AIR INLET DEICE BOOT FAILED IN FLIGHT AT FL240, -19 DEGREES C, 36 MINUTES AFTER DEPARTURE. RETURNED TO SLC . LEAK CHECKED RIGHT INLET DEICE SYSTEM FROM EJECTOR VALVE TO BOOTS AND FOUND NO LEAKS. REMOVED AND REPLACED RIGHT INL ET BOOT PRESSURE SWITCH. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002050600080 20020506 00080 SO 2002 5 6 SWIA200210805 1 20020418 A 5610 1513111 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 215SW 120281 AT 26,000 MSL, THE CAPTAIN'S WINDSHIELD CRACKED. REMOVED AND REPLACED THE LEFT WINDSHIELD. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002050600081 20020506 00081 EA 2002 5 6 SWIA200210806 1 20020419 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 439SW 1364 1364 7578 SPOILERON FAULT FOR RIGHT WING. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU IAW MM 27-62-01. OPS CHECK AND LEAK CHECK GOOD. REMOVED AND REPLACED SECU NR 1 WITH SERVICEABLE UNIT IAW 27-61-05. OPS CHECK GOOD. SECU P/N: 49-164-05, S/N OFF: 01374. 2 L 7 2 4F RT A21EA 2002050600082 20020506 00082 NE 2002 5 6 SWIA200210808 2 20020422 A 7321 CONNECTOR EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE LT & RT EEC DIRTY A SWIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 269UE 120194 WHILE IN POSITION FOR TAKEOFF, RECEIVED AN AURAL WARNING ENGINE CONTROLS AND MOMENTARY RED EEC LIGHT. CLEANED P1 CONNEC TOR OF LEFT AND RIGHT EEC'S. PERFORMED ENGINE RUNS. NO DISCREPANCIES FOUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2002050600083 20020506 00083 WP 2002 5 6 U2RB040202 1 20020402 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76322 46088 DURING CPCP 18 MONTH INSPECTION, AFT ACCESSORY COMPARTMENT INTERIOR. DETECTED LEVEL 2 CORROSION OF UPPER TEE OF FORWARD FLANGE OF FLOORBEAM 11.5 INCHES INBOARD OF RIGHT FUSELAGE CUSP LINE 1.75 INCHES LONG. 2 L 7 4 4F 4A25 2002050600084 20020506 00084 NM 2002 5 6 UPS02238090 1 20020424 A 3350 BATTERY BOEING 727 72725C 138400H NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHTS WILL NOT COME ON. REPLACED BATTERIES, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2002050600085 20020506 00085 NM 2002 5 6 UPS02238094 1 20020422 A 5754 SKIN BOEING 727 727180C 138406G NM KRUEGER FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C NR 3 KRUEGER FLAP ANTI ICE SKIN CRACKED 14 INCHES FROM I/B END. INSPECTED IAW NDTM PT 6 51-00-00 FIG 4, REPAIR CARRIED OUT IAW UPS EO B727-5750-3082-D. 2 L 7 3 4F A3WE 2002050600086 20020506 00086 NE 2002 5 6 00024 2 20020501 A 7200 ENGINE LEAR 24 24D 5170311 CE GE CJ610 CJ6106 30006 NE RIGHT FLAMED OUT E HAEA B EMER. DESCENT X ENGINE FLAMEOUT CL CLIMB 1 SW 05 324TW 24324 251710A ROUTE JVL TO GKY ATTEMPTED TO CLIMB OVER WEATHER FL430 TO FL450 TO TOP THUNDERSTORM RT ENGINE FLAME-OUT. DESCENDED TO F L250 PERFORMED AIR START, ALL OPERATION NORMAL. CONTINUED TO FINAL DESTINATION ADS. MAINTENANCE TO CK ENGINE WILL UPDA TE REPORT. MAINTENANCE COMPLIED WITH FLAME-OUT INSPECTION IN ACCORDANCE WITH GE SEI-186, NO DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4J 4 J A10CE 1E16 2002050600087 20020506 00087 WP 2002 5 6 0201379619 1 20020430 A 2910 FITTING DOUG DC9 DC932 3022066 WP HYD SYSTEM LOOSE A NWAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 01 619NW 47518 PRIOR TO EITHER LANDING GEAR EXTENSION OR FLAP EXTENSION DURING APPROACH INTO DTW, THE RT HYDRAULIC SYSTEM FAILED. QUAN TITY DROPPED TO BELOW 3 QTS AND PRESSURE WENT TO ZERO. COMPLIED WITH COM AND EXTENDED GEAR PER LEFT SYSTEM PROCEDURE. GEAR EXTENDED NORMALLY AND INDICATED ALL 3 GREEN WITH DOORS CLOSED. LANDING WAS UNEVENTFUL AT DTW. CREW DECLARED AN EM ERGENCY PRIOR TO LANDING. MAINTENANCE FOUND A FITTING ON THE RIGHT SIDE PRESSURE FOR GEAR UPLOCK LEAKING. TIGHTENED FI TTING. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002050600088 20020506 00088 WP 2002 5 6 CALA2000258 1 20020506 A 5320 9912243237 SHEAR TIE DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 F/S 1309 BETWEEN LONGERON 41L AND 15L SHEAR TIE IS CRACKED 12 INCHES. REMOVED OUTER CHORD, DOUBLER AND SHEAR TIE IAW SRM 51-10-4 AND SRM 51-31-1. INSTALLED NEW SHEAR TIE IAW 51-10-4 AND 51-30-5. INSTALLED CHORD, DOUBLER AND STIFFNER IAW SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2002050600089 20020506 00089 WP 2002 5 6 CALA2000259 1 20020506 A 5320 9912243238 SHEAR TIE DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 F/S 1309 BETWEEN LONGERON 14R AND 15R SHEAR TIE IS CRACKED 12 INCHES. REMOVED OUTER CHORD DOUBLER AND SHEAR TIE IAW SRM 51-30-4 AND 51-30-5. INSTALLLED SHEAR TIE, OUTER CHORD, DOUBLER AND STIFFER IAW SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2002050600100 20020506 00100 NM 2002 5 6 02FDEA00305 1 20020502 A 2613 SENSE LINE BOEING 727 727200 138407E NM OVERHEAT SYS OUT OF POSITION A FDEA O OTHER N FALSE WARNING DE DESCENT 1 SO 25 208FE 22930 DURING DESCENT THE LOWER AFT BODY OVERHEAT LIGHT CAME ON FOR APPROX 2 SECONDS THEN WENT OUT. THIS OCCURRED ONLY 1 TIME AND THE SYSTEM TESTED NORMALLY. ALL OTHER AIRCRAFT SYSTEMS/INDICATIONS NORMAL. INSPECTED AND FOUND SENSE LINE AT STATI ON 1243 LT SIDE OF AFT STAIR WELL TOUCHING BLEED AIR SUPPLY LINE. REPOSITIONED LINE WITH NEW CLAMPS OPERATIONALLY CHECK GOOD. ALL WORK DONE IAW B727MM 26-14-00, OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2002050600101 20020506 00101 WP 2002 5 6 2002F00430 1 20020312 A 5315 FLOORBEAM LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 70757 193C1078 DURING SCHEDULED INSPECTION LEVEL 2 CORROSION DISCOVERED ON CABIN FLOORBEAM UPPER CAP, FS 901, WL 200, LBL 115 TO RBL 14 . MAINTENANCE REPAIRED THE FLOORBEAM IN ACCORDANCE WITH LOCKHEED SRM 53-21-00, FIGURE 815. 2 L 7 3 4F A23WE 2002050600102 20020506 00102 WP 2002 5 6 2002F00431 1 20020330 A 5312 BULKHEAD LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION LEVEL 2 CORROSION DISCOVERED ON BULKHEAD LOWER WEB AT FS 315, LBL 18 TO RBL 18. MAINTENANCE REPLACED THE LOWER WEB IN ACCORDANCE WITH LOCKHEED SRM 51-40-01. 2 L 7 3 4F A23WE 2002050600103 20020506 00103 CE 2002 5 6 2002FA0000548 1 20020401 A 2823 1216608200 SELECTOR SWITCH CESSNA 207 207 2073602 CE CONT O520 IO520* 17032 SO FUEL SYSTEM FAILED B VDQC K NONE O OTHER IN INSP/MAINT 1 AL 03 91190 6100 20700109 SECOND FUEL SELECTOR VALVE SHAFT IN 13, 403.4 HOURS. 1 H 7 1 3O 3 O A16CE E5CE 2002050600104 20020506 00104 WP 2002 5 6 2002F00432 1 20020319 A 5330 DOUBLER LKHEED 1011 10113851 5265010 WP FUSELAGE CRACKED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION A 3 INCH CRACK WAS DISCOVERED AT FESC INTERNAL SKIN DOUBLER. MAINTENANCE REPAIRED THE DOUBL ER IN ACCORDANCE WITH AMTA ER/A L10-53R-4728 FS 315 TO 335, LBL 10 TO LBL 21. 2 L 7 3 4F A23WE 2002050600105 20020506 00105 WP 2002 5 6 2002F00433 1 20020324 A 5720 CHANNEL LKHEED 1011 10113851 5265010 WP LT WING CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 188AT 193C1078 DURING SCHEDULED INSPECTION THE LEFT MAIN LANDING GEAR TORQUE BOX LOWER AFT BATHTUB FITTING CHANNEL WAS CORRODED (LEVEL 2). MAINTENANCE REMOVED AND REPLACED THE FITTING CHANNEL IN ACCORDANCE WITH LOCKHEED SRM 51-40-01, FS 1230, WS 319 LEFT . 2 L 7 3 4F A23WE 2002050600106 20020506 00106 CE 2002 5 6 2002F00434 1 20020501 A 7910 M832481117 O-RING CESSNA 650 650 2076802 CE GARRTT TPE731 TFE7313C WP LT ENGINE DEFECTIVE E E B ENGINE SHUTDOWN EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 717JM 6500138 P87397 LT ENGINE HAD A LOSS OF OIL PRESSURE, SHUT DOWN LT ENGINE. LANDED IN MCO. CESSNA SERVICE CENTER TROUBLESHOT PROBLEM TO BAD O-RING ON LT ENGINE OIL CAP (OUTBOARD). REMOVED AND REPLACED O-RING. 2 L 7 2 4F 4 F A9NM E6WE 2002050600107 20020506 00107 WP 2002 5 6 2002F00435 1 20020107 A 5312 BULKHEAD LKHEED 1011 10113853 5265020 WP FUSELAGE CRACKED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 293A1238 DURING SCHEDULED INSPECTION BULKHEAD WEB FASTENER HOLE AT FS 1363, RBL 90 TO RBL 91 TO HAVE 0.020 INCH CRACK. MAINTENAN CE REMOVED AND REPLACED THE BULKHEAD WEB IN ACCORDANCE WITH LOCKHEED SRM 51-10-01. 2 L 7 3 4F A23WE 2002050600108 20020506 00108 WP 2002 5 6 2002F00436 1 20020107 A 5312 BULKHEAD LKHEED 1011 10113853 5265020 WP FUSELAGE CRACKED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 293A1238 DURING SCHEDULED INSPECTION BULKHEAD WEB FASTENER HOLE AT FS 1363, LBL 91 FOUND TO HAVE 0.063 INCH CRACK. MAINTENANCE R EMOVED AND REPLACED THE BULKHEAD WEB IN ACCORDANCE WITH LOCKHEED SRM 51-10-01. 2 L 7 3 4F A23WE 2002050600109 20020506 00109 WP 2002 5 6 2002F00437 1 20020104 A 5312 BULKHEAD LKHEED 1011 10113853 5265020 WP FUSELAGE CRACKED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 293A1238 DURING SCHEDULED INSPECTION BULKHEAD INNER SKIN FASTENER HOLE AT FS 1363, STRINGER 21 RIGHT TO 22 RIGHT, RBL 90 FOUND TO HAVE 0.250 INCH CRACK. MAINTENANCE REPAIRED THE AREA IN ACCORDANCE WITH LOCKHEED SRM 53-11-00, FIGURE 826. 2 L 7 3 4F A23WE 2002050600111 20020506 00111 NM 2002 5 6 2002F00438 1 20020428 A 3020 7646B000 VALVE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE INOPERATIVE G AMTA K NONE J WARNING INDICATION CL CLIMB 1 GL 11 555TZ 556 556 32589 31851 FLIGHT 926, DURING CLIMB RECEIVED EICAS MSG RT ANTI-ICE DISPLAYED WHEN SWITCH IS POSITIONED TO OFF POSITION VALVE LIGHT IN RT ENGINE TAI SWITCH LIGHT ILLUMINATED WITH TAI SELECTED OFF. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE TAI VAL VE IN ACCORDANCE WITH MM 30-21-03-4. SYSTEM OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E12EU 2002050600114 20020506 00114 WP 2002 5 6 ABXA010869 1 20020406 A 5310 DOOR FRAME DOUG DC8 DC861 3021952 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 AFT PASSENGER DOOR CUTOUT LOWER FORWARD CORNER SHOWED CRACK INDICATION ON THE FIRST FASTENER COMMON TO THE LOWER DOOR PA N. INSTALLED REPAIR FILLER, DOUBLER, TRIPLER, AND REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-20B AND 51-1-21. 2 L 7 4 4F 4A25 2002050600121 20020506 00121 WP 2002 5 6 ABXA010870 1 20020430 A 5610 ACCESS PANEL DOUG DC9 DC932F 3022067 WP WINDOW RELEASE MISSING A ABXA K NONE O OTHER CL CLIMB 1 GL 23 904AX 47040 AFTER TAKEOFF, LOUD WINDSTREAM NOISE FROM THE CAPTAIN'S SIDE OF AIRCRAFT. AIRCRAFT WOULD NOT PRESSURIZE. REINSTALLED T HE CAPTAIN'S EMERGENCY WINDOW RELEASE ACCESS PANEL. PRESSURIZATION OPS CHECKED NORMAL IAW DC-9 MM. 2 L 7 2 4F A6WE 2002050600122 20020506 00122 NM 2002 5 6 AWXA200200389 1 20020409 A 5315 146N51116 FLOORBEAM BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 GYR - MAJOR REPAIR - DURING C-11 CHECK EXFOLIATION CORROSION FOUND ON UPPER HORIZONTAL FLANGE AT BS 1681. NUMEROUS ARE AS OF CORROSION FROM LBL 50 - RBL 53. MAINTENANCE CUT OUT CORROSION AND INSTALLED REPAIR PARTS PER AWA ER 19-5360-0211 9-JS1. 2 L 7 2 4F RT A2NM 2002050600123 20020506 00123 NM 2002 5 6 AWXA200200390 1 20020408 A 5320 146N53183 WEB BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 GYR - MAJOR REPAIR - DURING C-11 CHECK CORROSION WAS FOUND ON AFT GALLEY FLOOR WEB IN MULTIPLE AREAS BETWEEN BS 1681 TO 1720, LBL 56 TO RBL 56. MAINTENANCE REMOVED CORRODED AFT GALLEY FLOOR WEB BETWEEN BS 1681 TO 1720, LBL 56 TO RBL 56, FA BRICATED AND INSTALLED REPAIR PER DWG 146N5318. 2 L 7 2 4F RT A2NM 2002050600124 20020506 00124 NM 2002 5 6 AWXA200200391 1 20020501 A 4920 38002784 APU AIRBUS A319 A319132 3930340 NM APU BAY LEAKING A AWXA K NONE K A FLUID LOSS FLAME/FIRE IN INSP/MAINT 1 WP 28 806AW 10537 1056 PHX - TAILPIPE FIRE - WHEN AUXILIARY POWER UNIT (APU) WAS SHUTDOWN AN APU TAILPIPE FIRE WAS NOTICED FROM THE GROUND. MA INTENANCE REMOVED AND REPLACED THE APU IAW T/C R6D49301, LEAK AND OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002050600125 20020506 00125 NM 2002 5 6 AWXA200200392 1 20020408 A 5311 651630086 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 YVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND ON PRESSURE BULKHEAD CHORD BS 178 AT THE LT SIDE 12.5 INCHES BE LOW WL 208. MAINTENANCE REMOVED DAMAGED CHORD AT LT SIDE BS 178, WL 196; FABRICATED NEW CHORD AND INSTALLED REPAIR IAW B737-200 SRM 51-10-1, PG 8, AND DWG 65-16300. 2 L 7 2 4F RT A16WE 2002050600126 20020506 00126 NM 2002 5 6 AWXA200200395 1 20020408 A 5230 6547952166 CROSSBEAM BOEING 737 737277 1384570 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 YVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND ON THE AFT CARGO DOOR LOWER AFT CROSS BEAM. MAINTENANCE REMOVE D EXISTING T-CHORD AND FILLER, FABRICATED AND INSTALLED REPAIR PARTS IAW BSB 737-52A1079, AND AWA ER 15-5233-02116-GF1. 2 L 7 2 4F RT A16WE 2002050600127 20020506 00127 SO 2002 5 6 C2XA02BT018 1 20020430 A 2120 SMOKE EMB 145 EMB145ER 3260211 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 13935 145022 CREW REPORTED, DECLARED EMERGENCY FOR SMOKE IN CABIN, SEEMED TO BE COMING FROM NR 2 PACK. MAINTENANCE RAN NR 2 PACK IAW EMB145 MM 21-51-00, NO SMOKE DETECTED. REPEATED PROCESS SEVERAL TIMES, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4F RT T00011AT 2002050600128 20020506 00128 WP 2002 5 6 CALA0200256 1 20020501 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 CUSP WEB IS CRACKED AND CORRODED AT STA 218 L18R RBL 56. CUT OUT CORRODED AREA IAW SRM 53-01, FIG 4. FABRICATED NEW DO UBLER IAW SRM 55-14-2 AND 53-01, FIG 4. INSTALLED DOUBLER IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2002050600129 20020506 00129 EA 2002 5 6 COMA0260292 1 20020430 A 5270 840534 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 967CA 7134 OVERBOARD COOL AND INBOARD COOL CAUTION MESSAGE. REPLACED CABIN DOOR SWITCH PS1MB. 2 L 7 2 4F RT A21EA 2002050600130 20020506 00130 EA 2002 5 6 COMA0260293 1 20020430 A 3397 64643 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 984CA 7171 EMERGENCY FLOOR PATH LIGHTING IS INOP ROWS 1-5. REPLACED FLOOR LIGHTS CABLE ASSEMBLY. 2 L 7 2 4F RT A21EA 2002050600131 20020506 00131 EA 2002 5 6 COMA0260295 1 20020429 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 13330 7146 CORROSION FOUND ON FLOOR SUPPORT ANGLES LT & RT SIDE. REPAIRED FLOOR ANGLES IAW REO 601R-53-41-083. 2 L 7 2 4F RT A21EA 2002050600132 20020506 00132 NM 2002 5 6 DHL2002707003 1 20020430 A 3230 ACCESSORY UNIT BOEING 727 72722 1384002 NM E/E BAY MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 707DH 18321 AFTER GEAR RETRACTION MOVED GEAR HANDLE TO OFF, GEAR DOOR LIGHT FORWARD PANEL AND RIGHT MAIN GEAR DOOR LIGHT S/O PANEL I LLUMINATED. MOVED GEAR HANDLE TO UP, LIGHTS OUT, HANDLE TO OFF, LIGHTS OUT NORMAL OPS. ACCOMPLISHED POWER OFF RERACK O F LDG ACCY UNIT, CLEANED BENCH PLUG. CYCLED DOORS W/ GEAR HANDLE. ALL NORMAL PER MM 32-00. 2 L 7 3 4F A3WE 2002050600133 20020506 00133 SO 2002 5 6 C2XA02CL109 1 20020504 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13989 145271 DURING ROUTINE MAINTENANCE THE EXTERIOR EMERGENCY LIGHT AT THE LEFT WING WAS FOUND INOPERATIVE.MAINTENANCE REPLACED THE BULB ON THE EXTERIOR EMERGENCY LIGHT ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002050600136 20020506 00136 SO 2002 5 6 SWIA200210795 1 20020416 A 3020 EJECTOR VALVE EMB 120 EMB120ER 3260203 SO LT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 296SW 120325 LEFT ENGINE AIR INLET INOP INFLIGHT. RETURNED TO SFO. UPDATE: LEFT ENGINE AIR INLET REPORTED INOP BY CREW ON FLIGHT T O PDX. INSTALLED SERVICEABLE PRESSURE SWITCH ON LEFT ENGINE INLET. OPS CHECK GOOD. REMOVED AND REPLACED LEFT ENGINE E JECTOR VALVE IAW 30-20-04. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002050600137 20020506 00137 2002 5 6 SWIA200210804 4 20020414 A 3425 COMPUTER EMB 120 EMB120ER 3260203 SO NR 2 FAULTY A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 190SW 120050 FIRST OFFICER'S EHSI TURNED 30-40 DEGREES RIGHT WHILE CLIMBING STRAIGHT OUT. FIRST OFFICER'S RMI HEADING INFORMATION MA TCHES CAPTAIN'S EHSI, RMI AND MAGNETIC COMPASS. RESET FIRST OFFICER'S HEADING BY SWITCHING FIRST OFFICER'S COMPASS COMP ENSATOR MOMENTARILY TO DG MODE. NO ASSOCIATED FLAGS OR WARNINGS. REPLACED NR 2 AHRS COMPUTER AND PERFORMED ORIENTATION . OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002050600138 20020506 00138 NM 2002 5 6 UPS02238096 1 20020426 A 3350 RACK BOEING 727 72751C 1384015 NM COCKPIT LOOSE A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 903UP 18945 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ILLUMINATED SEVERAL TIMES DURING FLIGHT. FLIGHT DECK EMERGENCY LIGHT MOUNTING RACK TIGHTENED, EMERGENCY LIGHTING CHECK SERV PER MM 33-50-67. 2 L 7 3 4F A3WE 2002050600139 20020506 00139 NM 2002 5 6 PCAA0205054 1 20020504 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM LW1 INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 844EX 17745 15632 339 DURING ROUTINE MAINTENANCE VISIT 2 RED FLOOR EMERGENCY LIGHTS FOUND INOPERATIVE AT ROW 1. AFTER LIGHTS WERE RELAMPED, IT WAS DISCOVERED THAT THERE WAS NO POWER THROUGH WIRING. EMERGENCY LIGHT POWER SUPPLY AND BATTERY WERE REPLACED. OPERATIO NAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002062100017 20020621 00017 EU 2002 6 21 UPS02238098 2 20020430 A 7200 ENGINE BOEING 727 727172C 1384058 NM RROYCE TAY TAY65154 EU NR 1 FAILED A IPXA E ENGINE SHUTDOWN O OTHER NR NOT REPORTED 1 SO 01 916UP 19808 INSPECTION TYPE:N/A ATB NR 1 ENGINE OIL PRESSURE LOSS (ENGINE SHUT DOWN) NR 1 ENG CHANGE REF BOEING 727 MAINTENANCE FUNC TION TASK CARD 1273. ENGINE CHANGE COMPLETED IAW TC 1273. 2 L 7 3 4F 4 F A3WE E25NE 2002050600140 20020506 00140 NM 2002 5 6 UPS02437866 1 20020301 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C M/D AFTER WINDOW FORGING REMOVED FOUND SURROUND FX SKIN CORRODED. REPAIR WINDOW FORGING ATT SKIN DOUB LER AT BS 2060-2080 STR 20L - STR 22L AS PER RS R53-61-34742. 2 L 7 4 4F A20WE 2002050600141 20020506 00141 NM 2002 5 6 UPS02437867 1 20020301 A 5347 BAC15201682717 CARGO TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C AFT CARGO COMPT - BS 1577 RBL 25 TIE DOWN TRACK VERTICAL ATTACHMENT CORRODED. TIE DOWN TRACK REPLACED AT BS 1500 - BS 1590 RBL 25 AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002050600142 20020506 00142 NM 2002 5 6 UPS02437868 1 20020227 A 5320 WEB BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C RT BLG W/W BS 1394 O/B WEB UPPER O/B FILLET AREA FOUND CORROSION ADJACENT PRESSURE DECK AREA AS MARK. WEB REPAIRED AS PER 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2002050600143 20020506 00143 NM 2002 5 6 UPS02437870 1 20020226 A 5330 DOUBLER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C FX - LT STA 1960 STR 26 SKIN ATT DOUBLER FOUND CRACKED. EXTERNAL DOUBLER REPAIRED AS PER RS R53-61-34 730. 2 L 7 4 4F A20WE 2002050600144 20020506 00144 NM 2002 5 6 UPS02437880 1 20020224 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C AFT CARGO DOOR CUTOUT FWD UPPER CORNER FOUND FASTENER HOLE CRACKED APPROX .125 INCH AT SKIN BS 1810 TO 1820, WL 190 TO 195. AFT CARGO DOOR FWD UPPER CUTOUT CORNER REPAIRED AS PER SRM 53-30-03 FIG 62. 2 L 7 4 4F A20WE 2002050600145 20020506 00145 NM 2002 5 6 UPS02437881 1 20020226 A 5320 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C FX - RT SIDE TUNNEL STA 300 NOSE WHEEL WELL VERTICAL BEAM WEB ATTACH CHORD FOUND CRACKED AT LOWER AREA FWD FACE AS MARKED. FX RT SIDE TUNNEL STA 300 NOSE WHEEL WELL VERTICAL BEAM WEB ATTACH CHORD REPAIRED AS PER SRM 51-40 -04 FIG 1. 2 L 7 4 4F A20WE 2002050600146 20020506 00146 EA 2002 5 6 COMA0260298 1 20020503 A 5300 601R311711517 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FS464,RBL36,LBL3 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 932CA 18588 7038 THE UNDER FLOOR SUPPORT INTERCOSTALS HAD CRACKED ATTACH FLANGES AT FS484, RBL36 AND LBL36.CUT OFF THE CRACKED FLANGE, FA BRICATED AND INSTALLED A REPAIR ANGLE I/A/W WVAC EO 601R-53-3181. 2 L 7 2 4F RT A21EA 2002050600149 20020506 00149 EA 2002 5 6 COMA0260299 1 20020503 A 5300 POST CNDAIR CL600 CL6002B19 1900309 EA FS559,RBL9 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 932CA 18588 7038 THE BOTTOM FLANGE OF VERTICAL POST WAS CRACKED AT FS559 AT RBL9.REMOVED THE CRACKED FLANGE AND FABRICATED AND INSTALLED A REPAIR ANGLE I/A/W REO 601R-53-41-057. 2 L 7 2 4F RT A21EA 2002050600151 20020506 00151 EA 2002 5 6 COMA0260300 1 20020503 A 5300 6003106819 FITTING CNDAIR CL600 CL6002B19 1900309 EA FS460 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 932CA 18588 7038 THE FLOOR SUPPORT FITTING AT FS460, RBL9 WAS CRACKED.REMOVED THE CRACKED FITTING AND INSTALLED A NEW FITTING I/A/W WVAC EO 601R-53-3182. 2 L 7 2 4F RT A21EA 2002050600152 20020506 00152 EA 2002 5 6 COMA0260301 1 20020502 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 430CA 7461 FLIGHT 5150 EMERGENCY FLOOR LIGHT INOP.REPOSITIONED FWD FLOOR LIGHT, OPERATIONAL CHECK O.K. 2 L 7 2 4F RT A21EA 2002050600153 20020506 00153 NM 2002 5 6 C1HA200281004 1 20020503 A 3350 900542 POWER SUPPLY BOEING 727 7272S7 138407Z NM INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 681CA 9 22020 Left hand aft overwing emergency exit light inoperative. Removed and replaced power supply per MM. Ground tests normal. 2 L 7 3 4F A3WE 2002050600154 20020506 00154 NM 2002 5 6 C1HA200281003 1 20020502 A 3350 900035A BATTERY BOEING 727 7272S7 138407Z NM INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 681CA 22020 Left hand overwing aft emergency exit light inoperative. Removed and replaced emergency light battery IAW MM. Operationa lly checks good at this time. 2 L 7 3 4F A3WE 2002060700166 20020607 00166 NM 2002 6 7 UPS02238118 1 20020502 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:N/A CORROSION STA 1148 STRINGER 25L TO 26L. REMOVED CORRODED SKIN AND INTERNAL DOUBLER REPAIRED PER EO B727-5330 -16790-A 2 L 7 3 4F A3WE 2002050600155 20020506 00155 WP 2002 5 6 P2EA2002M032 1 20020506 A 8000 38334211 STARTER DOUG DC9 DC981 3022081 WP A P2EA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 05 814US 48094 #2 Engine would not start. #2 Engine would not cross-bleed start. Removed and replaced #2 Engine Started IAW MM 80-10-01 . Operational check normal. This is closing action for SDR P2EA2002M032. Reference log page 122431. 2 L 7 2 4F A6WE 2002050600156 20020506 00156 NM 2002 5 6 AWXA200200405 1 20020504 A 3350 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM SEAT ROW 22 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 0 0 23776 PHX - EEL - DURING INSPECTION EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 22 L/H. MAINTENANCE REPAIRED BROKEN WIRE AT SEAT ROW 22, OPERATIONAL CHECK WAS GOOD PER AWA T/C A1C33006. 2 L 7 2 4F RT A16WE 2002050600157 20020506 00157 EU 2002 5 6 AWXA200200408 1 20020422 A 5520 D55982510201 FITTING AIRBUS 320 A320232 3930326 EU CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 605AW 0 0 543 YWG - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON THE R/H ELEVATOR OUTBOARD AFT SERVO ACTUATOR ATTACH FITTIN G INBOARD LUG BORE EDGE. MAINTENANCE BLENDED OUT CORROSION AT INBOARD LUG BORE EDGE, REAMED THE LUG BORE TO 1.0374", PER FORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST, FABRICATED A REPAIR SLEEVE BUSHING, AND INSTALLED REPAIR SLEEVE BUSHIN G IAW AWA ER 26-5526-02122-TB3. 2 L 7 2 4F RT A28NM 2002050700004 20020507 00004 CE 2002 5 7 FEG2002F00000 1 20020220 A 7930 1023200019 LINE BEECH 58 58P 1152744 CE CONT O520 TSIO520* 17040 SO WING L/E CHAFED A WUXA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 153Z 5116 TJ322 ENGINE OIL FOUND LEAKING FROM WING ROOT/FUSELAGE JUNCTION AT LEADING EDGE. LEADING EDGE REMOVED. FOUND ALUMINUM OIL PR ESSURE GAUGE LINE CHAFFED THROUGH FROM CONTACT WITH INBOARD RIB OF 102-100026-602 LEADING EDGE FAIRING ASSEMBLY. RECOMM END INSPECTING OIL PRESSURE GAUGE LINE AT INBOARD END WHERE IT ATTACHES TO BULKHEAD FITTING AT FUSELAGE FOR EVIDENCE OF CONTACT WITH ADJACENT STRUCTURE. 1 L 7 2 3O 3 O A23CE E8CE 2002050700005 20020507 00005 SO 2002 5 7 MHJ2002F00001 2 20020218 A 8530 646657 CYLINDER CESSNA 401 401A 207590D CE CONT O520 TSIO520F 17040 SO ENGINE BROKEN E MHJA K NONE O OTHER IN INSP/MAINT 1 SW 05 217BA 1331 401A0118 515604 NR 2 CYLINDER ON LEFT ENGINE HAD A SMALL PIECE MISSING FROM AROUND EXHAUST VALVE AREA. ENGINE HAS BEEN REMOVED FROM SER VICE FOR OVERHAUL. 1 L 7 2 3O 3 O A7CE E8CE 2002050700006 20020507 00006 SO 2002 5 7 MHJ2002F00002 2 20020218 A 8530 646657 CYLINDER CESSNA 401 401 207590C CE CONT O520 IO520E 17032 SO ENGINE SEPARATED E MHJA K NONE O OTHER IN INSP/MAINT 1 SW 05 401PW 130 4010269 182946R NR 4 CYLINDER FOUND SEPERATED FROM CRANKCASE, CAUSE UNKNOWN. ENGINE REMOVED FROM AIRCRAFT AND SENT TO OVERHAUL FACILITY . 1 L 7 2 3O 3 O A7CE E5CE 2002050700007 20020507 00007 EA 2002 5 7 PJM2002F00000 1 20020410 A 7332 CLIP DHAV DHC2 DHC2* 2800108 EA PWA R985 R985AN14BM1 52008 NE FUEL PRESS IND MISINSTALLED E PJMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 05 64393 111 845 18206 PILOT REPORTED ERRATIC FUEL PRESSURE INDICATION DURING FLIGHT. AIRCRAFT ARRIVED AT MAINTENANCE BASE WHERE INSPECTION OF THE FUEL PUMP REVEALED FUEL SEEPING FROM PRESSURE RELIEF DIAPHRAGM VENT. UPON REMOVAL OF THE DIAPHRAGM, IT WAS NOTED T HAT THE DIAPHRAGM RETAINING NUT WAS LOOSE DUE TO IMPROPER ENGAGEMENT OF THE LOCKING CLIP. DUE TO THE LOOSENESS OF THE R ETAINING NUT, FUEL WAS ALLOWED TO LEAK PAST THE DIAPHRAGM CRUSH GASKET, FLOODING THE AMBIENT SIDE OF THE DIAPHRAGM. THI S ACTION PREVENTED THE RELIEF MECHANISM TO PROPERLY REGULATE THE FUEL PRESSURE. IT IS IMPORTANT TO REMOVE ANY FUEL PUMP OF THIS TYPE FROM SERVICE IF THERE IS ANY SIGN OF LEAKAGE FROM THE VENT AREA. 1 H 7 1 3R 3 R A806 5E1 2002050700008 20020507 00008 CE 2002 5 7 VJ32002F00022 1 20020418 A 3610 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO AIR PRESSURE INOPERATIVE B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 5599P 422 CE1344 852760R NO INSTRUMENT AIR PRESSURE AT 1000 RPM, SYSTEM CHECKED AND FOUND THE AIR PUMP HAD NO OUTPUT. PUMP WAS REMOVED AND A NE W PUMP INSTALLED. GROUND RUN OF THE AIRCRAFT SYSTEM CHECKED NORMAL. 1 L 7 1 3O 3 O 3A15 E5CE 2002050700009 20020507 00009 SO 2002 5 7 WVBA2002008 1 20020425 A 5343 409872 CHANNEL PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA NLG CRACKED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 05 4082T 17028 17028 318152089 DURING INSPECTION, THIS AREA WAS LOOKED AT AFTER FINDING OTHER AIRCRAFT WITH THIS CHANNEL CRACKED THE PART WAS REMOVED A ND REPLACED. IT MAY BE THAT THE CUT OUT NOT BEING DRESSED TO RELIEVE THE STRESS CAUSED THE PART TO FAIL AS EXTRA STRESS IS INDUCED FROM THE NOSE GEAR ACTUATOR ATTACH BRACKETS , 2 REAR BOLTS COMING THROUGH THE CHANNEL. THE OUTBOARD ACTUATO R ATTACH HOLE WAS CRACKED FROM THE HOLE TO THE EDGE OF THE CHANNEL. 1 L 7 2 3O 3 O A20SO E14EA 2002050700010 20020507 00010 CE 2002 5 7 YE92002F00000 1 20020326 A 2120 10138001313 A/C PACK BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE CABIN PRESSURE MALFUNCTIONED E YE9A A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 09 87SA BB1089 PILOT NOTICED CABIN CLIMBING AT A HIGHER THAN NORMAL RATE. AIRCRAFT RETURNED TO AIRPORT AND LOCAL MAINTENANCE DETERMINE D. FLOW PACK NEEDED TO BE CHANGED. BOTH FLOW PACKS WERE CHANGED. ALL OPERATIONAL TEST ARE GOOD AT THIS TIME, PRESSURIZ ATION, NORMAL. 1 L 7 2 4T 4 T A24CE E4EA 2002050700011 20020507 00011 CE 2002 5 7 YE92002F00001 1 20020411 A 3230 SWITCH BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE LAND GEAR DEFECTIVE E YE9A O OTHER J WARNING INDICATION CL CLIMB 1 EA 09 87SA BB1089 LANDING GEAR WAS RETRACTED AFTER TAKEOFF AND LANDING GEAR SEEMED SLUGGISH. LOCAL MAINTENANCE DETERMINED DEFECTIVE GEAR SWITCH. NEW GEAR SWITCH WAS INSTALLED AND TESTED. LANDING GEAR IS OPERATIONAL AT THIS TIME. 1 L 7 2 4T 4 T A24CE E4EA 2002050700015 20020507 00015 NE 2002 5 7 ZYW2002F00003 2 20020306 A 7320 0164248860 FUEL CONTROL AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE LEAKING E ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365WM 415 6429 FCU, FUEL LEAKING FROM DRAIN WITH AIRCRAFT BOOST PUMPS ENERGIZED AND ENGINE STATIC. REMOVED AND REPLACED FUEL CONTROL U NIT. 1 G 7 2 3U 3 U RT H10EU E19EU 2002050700016 20020507 00016 EU 2002 5 7 ZYW2002F00004 1 20020306 A 6730 14860011 ACTUATOR AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1 60030 NE STOP ACTUATOR INOPERATIVE E ZYWA K NONE L NO TEST NR NOT REPORTED 1 GL 09 365WM 9 6429 ACTUATOR, INOPERATIVE. REMOVED AND REPLACED ACTUATOR. 1 G 7 2 3U 3 U RT H10EU E19EU 2002050700017 20020507 00017 NE 2002 5 7 ZYW2002F00005 2 20020211 A 7320 0174078010 DRAIN VALVE AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1 60030 NE FUEL CONTROL LEAKING E ZYWA K NONE L NO TEST IN INSP/MAINT 1 GL 09 365WM 3309 6429 START DRAIN VALVE, FUEL LEAKING FROM AUXILARY VALVE OPENING. REMOVED AND REPLACED VALVE. 1 G 7 2 3U 3 U RT H10EU E19EU 2002050700018 20020507 00018 EU 2002 5 7 ZYW2002F00006 1 20020219 A 5260 14860011 ACTUATOR AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1 60030 NE AIR STAIR INOPERATIVE E ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365WM 3402 6429 ACTUATOR, INOPERATIVE. REMOVED AND REPLACED ACTUATOR. 1 G 7 2 3U 3 U RT H10EU E19EU 2002050700019 20020507 00019 EU 2002 5 7 ZYW2002F00007 1 20020128 A 5260 14860011 ACTUATOR AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1 60030 NE STEP INOPERATIVE E ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365WM 6429 ACTUATOR TRIPS CIRCUIT BREAKER WHEN ACTIVATED. REMOVED AND REPLACED ACTUATOR. 1 G 7 2 3U 3 U RT H10EU E19EU 2002050700020 20020507 00020 NM 2002 5 7 2002F00442 1 20020226 A 5315 FLOORBEAM BOEING 727 727225A 1384077 NM FUSLEAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 810EA 22432 AT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOORBEAM CORRODED AT STATION 536 LBL 13. (M) 2 L 7 3 4F RT A3WE 2002050700021 20020507 00021 NM 2002 5 7 2002F00444 1 20020215 A 2120 2040751 ACM BOEING 727 727225 1384077 NM CABIN PRESSURE INOPERATIVE A MYWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 887MA 21857 ON ASCENT FROM AUS AIRCRAFT WILL NOT PRESURIZE WITH ONE PACK. ACCOMPLISHED AOM PROCEDURE 2-E-23, NO HELP. RETURN TO AU S. REMOVED AND REPLACED RT AIR CYCLE MACHINE IAW MM 21-51-11. SYSTEM OPS CHECK GOOD. AIRCRAFT RETURNED TO REVENUE SER VICE. (M) 2 L 7 3 4F A3WE 2002051700070 20020517 00070 NM 2002 5 17 DHL2002726518 1 20020417 A 5344 HINGE BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, MAIN CARGO DOOR HINGE (UPPER FUSELAGE SIDE) IS CRACKED, 2ND LOBE FROM AFT. VERIFIED BY HFEC. REMOVED C RACKED UPPER HINGE IAW B-727 SRM 51-30-2. INSTALLED NEW HINGE FOR MCD IAW PEMCO DWG 52-487-1. 2 L 7 3 4F RT A3WE 2002050700022 20020507 00022 2002 5 7 2002F00445 4 20020409 A 3442 20709430104 DISPLAY BOEING 747 747230B 1384889 NM RADAR SYSTEM SMOKE A Q2SA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 23 743SA 22671 DURING FLIGHT, SMOKE STARTED TO COME OUT OF THE FIRST OFFICERS RADAR DISPLAYED. THE RADAR DISPLAY WAS TURNED OFF AND TH E SMOKE STOPPED. REMOVED AND REPLACED FIRST OFFICERS RADAR INDICATOR AND INSPECTED THE SURROUNDING RACK AND CONNECTORS FOR DAMAGE. NO DISCREPANCIES NOTED IAW AMM 34-43-00. (M) 2 L 7 4 4F A20WE 2002050700023 20020507 00023 NM 2002 5 7 2002F00446 1 20020223 A 2120 CLAMP BOEING 727 727276 138408R NM FLOW CONTROL LOOSE A FX7A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 908PG 20951 DURING CRUISE, FLT LEVEL 310, AFT BODY OVERHEAT LIGHT ILLUMINATED. SHUT OFF PACK PER ABNORMAL CHECKLIST, BUT AIRCRAFT WO ULD NOT HOLD CABIN PRESSURIZATION WITH ONE PACK AIRCRAFT RETURNED TO SVMC NO FUEL WAS DUMPED. FOUND LOOSE CLAMP ON FLOW CONTROL VALVE TIGHTENED AND OPS CHECK PER 36-00 AND 71-00. CHECKS GOOD ALSO FOUND LOOSE SEAL AT FORWARD CARGO DOOR REP OSITIONED AND PRESSURIZED A/C PER MM 21-31-01 TO 3.5 PSI A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002050700024 20020507 00024 NM 2002 5 7 2002F00447 1 20020216 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE GOUGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 801EA 22432 AT C-CHECK, FOUND GOUGE ON FUSELAGE SKIN AT STATION 1343. (M) 2 L 7 3 4F A3WE 2002050700025 20020507 00025 NM 2002 5 7 2002F00448 1 20020126 A 5320 FLOOR SUPPORT BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 AT C-CHECK, FOUND AFT PIT FLOOR SUPPORT CORROSION AT STATION 1163-1166 LBL 4. (M) 2 L 7 3 4F A3WE 2002050700026 20020507 00026 NM 2002 5 7 2002F00449 1 20020222 A 3230 658702228 TRUNNION BOEING 727 727222 1384073 NM RT MLG CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 AT C-CHECK, FOUND RIGHT MLG TRUNNION SUPPORT FITTING CRACKED. (M) 2 L 7 3 4F A3WE 2002050700027 20020507 00027 NM 2002 5 7 2002F00450 1 20020318 A 5321 WEB BOEING 727 727225 1384077 NM CARGO FLOOR CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND AFT PIT SHEAR FLOOR WEB CORRODED AT STATION 1183 RBL 18. (M) 2 L 7 3 4F A3WE 2002050700028 20020507 00028 NM 2002 5 7 2002F00451 1 20020319 A 5210 SKIN BOEING 727 727225 1384077 NM PAX DOOR CHAFED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND L-1 DOOR INTERIOR SKIN CHAFED BETWEEN THE CENTER STOPS ON THE AFT EDGE. (M) 2 L 7 3 4F A3WE 2002050700029 20020507 00029 NM 2002 5 7 2002F00452 1 20020320 A 5320 PANEL BOEING 727 727225 1384077 NM CARGO BAY CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND CORROSION AND CRACK IN THE FORWARD PIT AT THE RIGHT TRANSITION PANEL TOP SIDE FROM STATION 480-560. ( M) 2 L 7 3 4F A3WE 2002050700030 20020507 00030 NM 2002 5 7 2002F00453 1 20020320 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND CRACK SIX INCHES LONG AT LOWER LEFT Z-FRAME IN FORWARD CARGO PIT STATION 480 LBL 32. (M) 2 L 7 3 4F A3WE 2002050700031 20020507 00031 WP 2002 5 7 CALA2000457 1 20020506 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 AFT PIT, F/S 1212 LONGERON 30 SHEAR TIE HAS 3 INCHES OF CORROSION. REMOVED SHEAR TIE IAW SRM 51-30-2. INSTALLED NEW SHEA R TIE IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2002050700032 20020507 00032 NM 2002 5 7 2002F00454 1 20020321 A 5320 SUPPORT BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND FORWARD CARGO SUPPORT CORROSION AT STATION 536. (M) 2 L 7 3 4F A3WE 2002050700033 20020507 00033 NM 2002 5 7 2002F00455 1 20020322 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE WORN A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND SEAT TRACK WORN OUT OF LIMITS AT STATION 852-868. (M) 2 L 7 3 4F A3WE 2002050700034 20020507 00034 NM 2002 5 7 2002F00456 1 20020222 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE WORN A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND SEAT TRACK WORN OUT OF LIMITS AT STATION 700D TO STATION 720E LBL 44. (M) 2 L 7 3 4F A3WE 2002050700035 20020507 00035 NM 2002 5 7 UPS02437882 1 20020301 A 5312 BULKHEAD BOEING 747 747123 1384873 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:C EMP - BS 2360 APB AFT FACE AT 11 O/C POSITION RADIAL LAP FOUND 1 REPAIR WHICH CANNOT CATEGORIZED AS DE TAIL I TO V REPAIR AS PER EO B747-5310-10823-I. THE EXISTING DOUBLER WAS REMOVED, AREA INSPECTED AND A FASTENER LOCATIO N WAS FOUND WITH A DENTED MARK ON AFT WEB AREA, REPAIRED AS PER HX RS R-53-83-34744, UPS EO B747-5310-16417-A. 2 L 7 4 4F A20WE 2002050700036 20020507 00036 NM 2002 5 7 UPS02437890 1 20020316 A 3350 LIGHT BOEING 747 747200 1384847 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 528UP 1 INSPECTION TYPE:PFLT UPPER DECK EMERGENCY EXIT LIGHT AT ROW 1 INOP. RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 4 4F RT A20WE 2002050700037 20020507 00037 NM 2002 5 7 UPS02437916 1 20020322 A 2612 CIRCUIT CARD BOEING 747 747200 1384847 NM FIRE DETECTION LOOSE A IPXA K NONE N FALSE WARNING CL CLIMB 1 SO 01 522UP 21936 INSPECTION TYPE:N/A DURING CLIMB NR 3 ENG FIRE DETECT FAULT LIGHT ILLUMINATED CHANNEL A NEEDLE WAVERED IN RED/ORANGE BAN D. STABLE IN GREEN BAND ONCE POWER REDUCED. SELECTED CHANNEL B ONLY. NR 3 ENG FIRE DETECTOR -A- INOP. REF M23 4208. RESEATED THE A-3/A-7 WARNING AND CONTROL CARDS IAW MM 26-10-0 0, CHECKS GOOD. 2 L 7 4 4F RT A20WE 2002050700038 20020507 00038 NM 2002 5 7 UPS02437920 1 20020325 A 3350 BATTERY PACK BOEING 747 747123 1384873 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:PFLT OVERHEAD EMERGENCY LIGHT ADJACENT TO SMOKE EVACUATION HOLE WILL NOT STAY ILLUMINATED WHEN POWER IS LOST AND EMERGENCY LIGHTS ARMED. REMOVED AND REPLACED BATTERY PACK ASSY IAW M/M 33-51-00. OPS CHECK OK. 2 L 7 4 4F A20WE 2002050700039 20020507 00039 NM 2002 5 7 UPS02437921 1 20020325 A 3350 BATTERY PACK BOEING 747 747123 1384873 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT AFT OF DOOR L-5 IS INOP (CEILING LOCATION). REMOVED AND REPLACED BATTERY PACK ASSY IAW MM 33-51-00, OPS CHECK OK. 2 L 7 4 4F A20WE 2002050700040 20020507 00040 NM 2002 5 7 UPS02437922 1 20020323 A 3350 LIGHT BOEING 747 747123 1384873 NM MAIN CARGO DECK INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:PFLT 2 EMERGENCY LIGHTS OUT ON MAIN CARGO DECK CEILING. ONLY 2 LIGHT ASSY ARE REQUIRED PER MM 33-51-00 PAGE 501. BOTH LIGHT ASSY OPS CHECK GOOD AT THIS TIME. 2 L 7 4 4F A20WE 2002050700041 20020507 00041 NM 2002 5 7 UPS02437924 1 20020322 A 3350 BATTERY PACK BOEING 747 747121 1384871 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:PFLT EMERGENCY LIGHTS ABOVE STAIRS INOP. REPLACED BATTERY PACK, EMERGENCY LIGHTS CHECK GOOD. 2 L 7 4 4F A20WE 2002050700042 20020507 00042 NM 2002 5 7 UPS02437929 1 20020325 A 3350 BATTERY PACK BOEING 747 747123 1384873 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT OVER UPPER DECK STAIRS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMB LY AND BATTERY PACK OPS CHECK GOOD. 2 L 7 4 4F A20WE 2002050700043 20020507 00043 NM 2002 5 7 UPS02437957 1 20020401 A 3211 TRUNNION BOEING 747 747123 1384873 NM RT MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:N/A RT MLG TRUNNION CRACKED. GEAR REPLACED BY BOEING AOG UNDER REPAIR AGREEMENT. 2 L 7 4 4F A20WE 2002050700044 20020507 00044 NM 2002 5 7 UPS02437979 1 20020327 A 5320 65B140581 SUPPORT BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C FX - KEEL BEAM BOX UNDER FAIRING SUPPORT LOWER SURFACE FOUND SURFACE CORROSION AT BS 1465 RBL 16 TO LB L 16. FAIRING SUPPORT REPLACED IAW SEM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002050700045 20020507 00045 NM 2002 5 7 UPS02437980 1 20020327 A 5320 65B140633 CHANNEL BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C FX - KEEL BEAM BOX UNDER FAIRING SUPPORT LOWER SURFACE FOUND SURFACE CORROSION AT BS 1438 TO BS 1465 R BL 16 TO LBL 16. CHANNEL REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002050700046 20020507 00046 NM 2002 5 7 UPS02437982 1 20020328 A 5310 141U109211 SHEAR TIE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C NOSE WHEEL WELL VERTICAL BEAM WEB BS 300 LT NR 3 & 4 SHEAR TIE CLIP (COUNT FROM TOP) FOUND CRACK AT FA STENER. NWW VERTICAL BEAM WEB LT BS 300 NR 3 & 4 SHEAR TIE CLIP (COUNT FROM TOP) REPLACED AS PER SRM 51-10-01 AND INSTA LLED AS PER BOEING DWG 624U0005. 2 L 7 4 4F A20WE 2002050700047 20020507 00047 NM 2002 5 7 UPS02437983 1 20020328 A 5310 141U109212 SHEAR TIE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C NOSE WHEEL WELL VERTICAL BEAM WEB RT BS 300 NR 2 AND 4 SHEAR TIE CLIP (COUNT FROM TOP) CRACK FOUND AT FASTENER. NWW VERTICAL BEAM WEB RT BS 300 NR 2 AND 4 SHEAR TIE CLIP REPLACED (COUNT FROM TOP) REPLACED AS PER SRM 51-10 -01 AND INSTALLED AS PER BOEING DWG 624U0005. 2 L 7 4 4F A20WE 2002050700048 20020507 00048 NM 2002 5 7 UPS02437984 1 20020328 A 5310 141U109211 SHEAR TIE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C NOSE WHEEL WELL VERTICAL BEAM WEB BS 320 LT NR 3 SHEAR TIE CLIP (COUNT FROM TOP) FOUND CRACK AT FASTEN ER. NWW VERTICAL BEAM WEB LT BS 320 NR 3 SHEAR TIE CLIP (COUNT FROM TOP) REPLACED AS PER SRM 51-10-01 AND INSTALLED AS PER BOEING DWG 624U0005. 2 L 7 4 4F A20WE 2002050700049 20020507 00049 NM 2002 5 7 UPS02437986 1 20020328 A 5310 141U109211 SHEAR TIE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C NOSE WHEEL WELL VERTICAL BEAM WEB BS 280 LT NR 4 SHEAR TIE CLIP (COUNT FROM TOP) FOUND CRACK AT FASTEN ER. NWW VERTICAL BEAM WEB LT BS 280 NR 4 SHEAR TIE CLIP (COUNT FROM TOP) REPLACED AS PER SRM 51-10-01 & BOEING DWG 624U 0005. 2 L 7 4 4F A20WE 2002050700050 20020507 00050 NM 2002 5 7 UPS02437987 1 20020328 A 5310 141U109211 SHEAR TIE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C NOSE WHEEL WELL VERTICAL BEAM WEB RT BS 280 NR 3 AND NR 4 SHEAR TIE CLIP (COUNT FROM TOP) CRACK FOUND AT FASTENER. NWW VERTICAL BEAM WEB RT BS 280 NR 3 AND 4 SHEAR TIE CLIP (COUNT FROM TOP) REPLACED AS PER SRM 51-10-01 & INSTALLED AS PER BOEING DWG 624U0005. 2 L 7 4 4F A20WE 2002050700051 20020507 00051 NM 2002 5 7 UPS02437991 1 20020323 A 5280 BEAM BOEING 747 747212B 1384886 NM LT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C LEFT MLG INBOARD W/W DOOR INBOARD CHANNEL FWD CORNER AREA CRACKED AS MARKED. LEFT MLG INBOARD W/W DOO R INBOARD BEAM REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002050700052 20020507 00052 NM 2002 5 7 UPS02438004 1 20020325 A 5210 65B135915 GATE BOEING 747 747212B 1384886 NM L1 DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C M/D - L1 DOOR LOWER GATE FOUND PITTING CORROSION. LOWER GATE ASSY CHANGED AS PER MM 52-11-00. 2 L 7 4 4F A20WE 2002050700053 20020507 00053 NM 2002 5 7 UPS02438011 1 20020409 A 3350 POWER SUPPLY BOEING 747 747212B 1384886 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:IN UPPER DECK AFT EMERGENCY LIGHT INOP. REMOVED SIDEWALL AND BOTH LIGHTS. REMOVED POWER SUPPLY, NO HEL P. FOUND POWER SUPPLY TO BE BAD FROM STOCK. REMOVED AND REPLACED POWER SUPPLY IN STA 650 AND INSTALLED SIDEWALL & LIGH T ASSY, SYS CHECKS NORMAL IAW 33-50-00. 2 L 7 4 4F A20WE 2002050700054 20020507 00054 NM 2002 5 7 UPS02438013 1 20020408 A 5420 STRAP BOEING 747 747200 1384847 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 528UP 24071 INSPECTION TYPE:C-2 CRACKS REVEALED ON THE FASTENER HOLE OF THE STRAP IN NR 3 PYLON REAR ENGINE MOUNT BULKHEAD. SKIN RE PAIRED AS PER HX RS R54-53-34766 AND UPS EA B747-5410-16563-A FOR DETAILS. 2 L 7 4 4F RT A20WE 2002050700055 20020507 00055 NM 2002 5 7 UPS02438014 1 20020406 A 5412 BULKHEAD BOEING 747 747200 1384847 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 528UP 24071 INSPECTION TYPE:C-2 NR 3 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD FOUND CRACKED AT FWD & AFT FRAME WEB. BULKHEAD CHORD REPAIRED AS PER HX RS R54-53-34766 FOR DETAIL UPS EA B747-5410-16563-A. 2 L 7 4 4F RT A20WE 2002050700056 20020507 00056 NM 2002 5 7 UPS02438018 1 20020327 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C LT MLG W/W STA 1480 LBL 65 STR 42L WL 122 LONGERON FITTING AND ATT PLATE FOUND CORROSION (AFT OF O/B T RUNNION SUPPORT FITTING). 2 L 7 4 4F A20WE 2002050700057 20020507 00057 NM 2002 5 7 UPS02438025 1 20020326 A 5312 141U10878 PRESSURE PANEL BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C PRESSURE PAN AT BS 400 CRACK INDICATION FOUND AT 1 EA FASTENER APPROX .75 INCH LENGTH. CRACKED PRESSU RE PAN AT BS 400 REPLACED AS PER DWG 624U0005 SHT 9. 2 L 7 4 4F A20WE 2002050700058 20020507 00058 NM 2002 5 7 UPS02438028 1 20020324 A 5412 65B903117 BULKHEAD BOEING 747 747212B 1384886 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C NR 4 PYLON AFT TORQUE BULKHEAD FOUND 3 FASTENER HOLES CRACK AT CHORD AREA. REPAIR CARRIED OUT AS PER RS-54-53-34764 INSTRUCTIONS. 2 L 7 4 4F A20WE 2002050700059 20020507 00059 NM 2002 5 7 UPS02438029 1 20020324 A 5412 65B903117 BULKHEAD BOEING 747 747212B 1384886 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:C NR 1 PYLON AFT TORQUE BULKHEAD FOUND 3 FASTENER HOLES CRACK AT CHORD AREA. REPAIR CARRIED OUT AS PER RS R-54-53-34764 INSTRUCTION. 2 L 7 4 4F A20WE 2002050700060 20020507 00060 NM 2002 5 7 UPS02438032 1 20020411 A 3350 LIGHT BOEING 747 747123 1384873 NM MAIN CARGO BAY INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:PFLT MAIN DECK CARGO AFT EMERGENCY EXIT LIGHT IN CEILING INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGH T ASSY AS PER MM 33-51-07, OPS CHECK OK. 2 L 7 4 4F A20WE 2002050700061 20020507 00061 NM 2002 5 7 UPS02438033 1 20020413 A 3350 LIGHT BOEING 747 747121 1384871 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:PFLT SEVERAL EMERGENCY BACKGROUND LIGHTS ABOVE CENTER INSTRUMENT PANEL INOP. RELAMPED SEVERAL EMERGENCY BACKGROUND LIGHTS ABOVE INSTRUMENT PANEL IAW GMM 3-6-9. OPS CHECK GOOD. 2 L 7 4 4F A20WE 2002050700062 20020507 00062 NM 2002 5 7 UPS02438046 1 20020415 A 5411 FRAME BOEING 747 747123 1384873 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: NR 3 PYLON INTERNAL FRAME FOUND CRACKED JUST O/B OF PYLON VALVE AREA. FRAME REPAIRED AS PER SRM 51-40- 03 FIG 2. 2 L 7 4 4F A20WE 2002050700063 20020507 00063 NM 2002 5 7 UPS02438051 1 20020413 A 5314 KEELBEAM BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:PFLT KEEL BEAM CORROSION. REPAIRED IAW EO B747-5310-16631. 2 L 7 4 4F A20WE 2002050700064 20020507 00064 NM 2002 5 7 UPS02438065 1 20020417 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE: FOUND NUMEROUS BURNT AND PITTED FASTENERS ON RT SIDE OF FUSELAGE AT STA 140 AT ABOUT 4 O'CLOCK TO 6 O'C LOCK POSITION COUNTING AFT TO STA 2240. REMOVED DAMAGED FASTENERS PER 53-30-03, EDDIE CURRENT INSPECTION FOUND 3 SMALL CRACKS AT 3 SEPARATE FASTENERS. 2 L 7 4 4F A20WE 2002050700103 20020507 00103 NM 2002 5 7 2002F00457 1 20020322 A 5320 SUPPORT BOEING 727 727225 1384077 NM CARGO BAY CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND CORROSION ON FORWARD CARGO SUPPORT AT STATION 644. (M) 2 L 7 3 4F A3WE 2002050700104 20020507 00104 NM 2002 5 7 2002F00427 1 20020226 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 801EA 22432 AT C-CHECK, FOUND FLOORBEAM CORRODED IN FORWARD CARGO COMPARTMENT AT STATION 536 RBL 13. (M) 2 L 7 3 4F A3WE 2002050700109 20020507 00109 CE 2002 5 7 CA020417001 1 20020415 A 5610 10138402518 WINDSHIELD BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) DURING CLIMBOUT FROM YYC THE CO PLIOTS WINDSHIELD CRACKED. AIRCRAFT WAS LEVELED OFF AND RETURNED TO AIRPORT. THE O UTER PLY OF WINDSHIELD WAS CRACKED WITH NO APPARENT REASON SUCH AS IMPACT. THE WINDSHIELD WAS REPLACED AND THE OLD SENT FOR INVESTIGATION. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002050700110 20020507 00110 CE 2002 5 7 CA020419002 1 20020321 A 7620 77GB408R4A18 RELAY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE ENGINE CONTROLS CORRODED W K NONE L NO TEST TX TAXI/GRND HDL 1 CA 13729 13729 (CAN) DURING PREFLIGHT CHECK PILOT PULLED THE LT FIRE HANDLE TO CHECK THE SHUTTOFF VALVE OPERATION, WHEN HE PUSH BACK TH E HANDLE THE VALVE STAYED CLOSED. SEVERAL TRIES WERE NECESSARY TO OPEN THE VALVE. DURING TROUBLESHOOTING, THE PROBLEM DI D NOT REOCCUR BUT AFTER INVESTIGATION FOUND THAT THE RELAY CONTACT AND THE WIRE TERMINAL WAS CORRODED AND CONTACT A3 WAS FOUND BEARLY ATTACHED. RELAY, WIRE AND TERMINAL WAS REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002050700115 20020507 00115 EA 2002 5 7 CA020502006 1 20020329 A 5230 601350821 SPRING CNDAIR CL6002B19 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE CARGO DOOR LATCH FAILED W O OTHER N FALSE WARNING CL CLIMB 1 CA 7095 (CAN) CARGO DOOR OPEN INDICATION ON EICAS DURING CLIMB, NO PRESSURIZATION FAULTS. FLIGHT CREW ELECTED TO TURN BACK. FOU ND TO BE THE DOOR LATCH MECHANISM AT FAULT. REPLACED ON SPRING SPACER AND PIN AFFECTED. SPRING MPN 601-35082-1SPACER P/ N NAS43DD4-18PIN P/N MS 16562-38 2 L 7 2 4F 4 F RT A21EA E15NE 2002050700117 20020507 00117 2002 5 7 CA020502009 4 20020403 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE STALL WARNING FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) STALL FAIL CAUTION MESSAGE SHORTLY AFTER TAKEOFF, QRH PROCEDURE APPLIED WITHOUT SUCCESS - MESSAGE DID NOT CLEAR. FOUND TO BE THE STALL PROTECT COMPUTER AT FAULT. REPLACED COMPUTER, SYSTEM CHECK SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002050700118 20020507 00118 NE 2002 5 7 CA020502010 2 20020317 A 7200 300U411020 ENGINE BOEING 767 7673Y0 NM PWA 4060 PW4060 52119 NE NACELLE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) ENGINE SURGE/STALL IN FLIGHT, ENGINE SHUTDOWN, AIRCRAFT RETURNED TO STATION. REPLACED ACCESSORIES WITHOUT SUCCESS . REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002050700119 20020507 00119 NM 2002 5 7 CA020502011 1 20020325 A 2730 2827001011 ACTUATOR BOEING 767 767375 1385217 NM GE CF6 CF680C2B6F 30025 NE RT ELEVATOR LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CA (CAN) CENTRE SYSTEM HYDRAULIC QUANTITY MESSAGE ON EICAS ON TOP OF DESCENT. QUANTITY CONTINUED TO DROP SLOWLY DURING DES CENT AND FLAP/GEAR EXTENSION FOUND TO BE A LEAK FROM THE INBOARD RT ELEVATOR POWER CONTROL ACTUATOR (PCA). REPLACED ACTU ATOR. 2 L 7 2 4F 4 F RT A1NM E13NE 2002050700120 20020507 00120 NM 2002 5 7 CA020502016 1 20020408 A 2710 550030019 ACTUATOR BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE LT AILERONS FAILED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 CA (CAN) AILERON LOCKOUT MESSAGE ON EICAS. REPLACED LEFT OUTBOARD LOCKOUT ACTUATOR. 2 L 7 2 4F 4 F RT A1NM E3NE 2002050700124 20020507 00124 NE 2002 5 7 A6WA200230006 2 20020321 A 7200 ENGINE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE LEFT SMOKE A A6WA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 339PH 3015 EXCESSIVE SMOKE FROM LEFT ENGINE DURING SHUTDOWN MAINTENANCE INSPECTED ENGINE FOR ANY VISABLE FLUID LEAKS, NONE FOUND. CREW RAN ENGINE IN FEATHER AND LOW PITCH SHUTDOWN ENGINE NO SMOKE OF ANY KIND NOTED. (M) 2 H 7 2 4T 4 T RT A45NM E20NE 2002050700127 20020507 00127 NM 2002 5 7 ASAA0210015 1 20020108 A 5315 6554960507 FLOORBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 360, STRINGER 17L-17R CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002050700129 20020507 00129 NM 2002 5 7 ASAA0210016 1 20020108 A 5315 65548932 FLOORBEAM BOEING 737 737298C 1384490 NM FUSLEAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 420, LEFT BUTTOCK LINE 2, LEFT BUTTOCK LINE 54 CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002061000044 20020610 00044 NM 2002 6 10 AWXA200200401 1 20020502 A 4930 FUEL CONTROL BOEING 757 757225 1384959 NM APU FAILED A AWXA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 28 907AW 22691 APU SHUTDOWN IN CRUISE; NR 2 ENGINE GENERATOR WAS ALREADY ON MEL 24-00-1, COND NR 1 (RT ENGINE DRIVEN GENERATOR INOPERAT IVE, ACFT DIVERTED TO CMH. MX TROUBLESHOT & FOUND AN INTERMITTENT GROUND TERMINAL -N- AND FOUND PIN -D- LOOSE ON NR 2 E NG IDG TERMINAL CANNON PLUG. MX REPLACED GROUND PIN -D- ON CONNECTOR D101G PER CHAP 20. OPS CHECK GOOD. APU INLET PRE SSURE SENSOR -P2- REPLACED AND APU FUEL CONTROL UNIT WAS ALSO REPLACED PER AWA T/C R6D49604 TO CORRECT THE APU AUTO SHUT DOWN PROBLEM. VENDOR BENCH TEST AND TEAR DOWN OF APU FUEL CONTROL UNIT CONFIRMED FAILURE, UNIT WAS FOUND TO HAVE ERRODE D BUSHINGS DUE TO BLOWN OIL SEAL PACKING. REPLACED SEAL, SLEEVES. UNIT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2002050700130 20020507 00130 NM 2002 5 7 ASAA0210017 1 20020108 A 5330 654850011 SKIN BOEING 737 737298C 1384490 NM FUSLEAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 360, STRINGER 27L-27R WITH OVERSIZED HOLES. REPAIRED PER EA. (M ) 2 L 7 2 4F RT A16WE 2002050700131 20020507 00131 NM 2002 5 7 AWXA200200402 1 20020502 A 3350 LIGHT BOEING 737 737375 13844BN NM EXTERIOR INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 336AW 23707 LAS- EEL R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT IAW BMM 33-50-00. FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002050700132 20020507 00132 SO 2002 5 7 C2XA02CL107 1 20020502 A 4980 4503825 LINER EMB 145 EMB145 3260210 SO APU MISSING A C2XA K NONE J WARNING INDICATION LD LANDING 1 SW 27 13965 145125 CLE FLIGHT 3595 THE CREW REPORTED ON LANDING RECEIVED A APU FIRE INDICATION. THE APU WAS SHUT DOWN AND THE INDICATION C LEARED. MAINTENANCE INSPECTED AND FOUND THE EXHAUST SILENCER LINER ASSEMBLY WAS MISSING. THE EXHAUST SILENCER ASSEMBLY WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. MAINTENANCE PERFORMED APU FIRE INDICATION INSPECTION. NO DEFECTS WERE FOUND. 2 L 7 2 4F RT T00011AT 2002050700133 20020507 00133 EU 2002 5 7 C2XA02IA100 1 20020501 A 3230 S3218000100067 LANDING GEAR AEROSP ATR42 ATR42320 8680930 EU MLG MALFUNCTIONED A C2XA K NONE O OTHER CL CLIMB 1 SW 27 14821 160 BPT- DURING FLIGHT 3640 FROM IAH TO BPT, THE CREW NOTED THAT THE LANDING GEAR WAS HAVING PROBLEMS RETRACTING, STICKING, MAKING LOUD BANGING NOISES, AND, TAKING EXCESSIVE TIME TO RETRACT. MAINTENANCE SERVICED BOTH MLG FREE FALL ASSISTERS, CLEANED AND LUBED NOSE WHEEL UPLOCK BOX. PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. 2 H 7 2 4T RT A53EU 2002050700134 20020507 00134 EU 2002 5 7 C2XA02IA101 1 20020501 A 3230 C245890002 UPLOCK AEROSP ATR42 ATR42320 8680930 EU NLG LACK OF LUBE A C2XA K NONE O OTHER CL CLIMB 1 SW 27 14821 160 BPT- DURING FLIGHT 3640 FROM IAH TO BPT, THE CREW NOTED THAT THE LANDING GEAR WAS HAVING PROBLEMS RETRACTING, STICKING, MAKING LOUD BANGING NOISES AND TAKING EXCESSIVE TIME TO RETRACT. MAINTENANCE SERVICED BOTH FREE FALL ASSISTERS, CLEANE D AND LUBED THE NOSE LANDING GEAR UPLOCK BOX. PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTE D. 2 H 7 2 4T RT A53EU 2002050700135 20020507 00135 NE 2002 5 7 C2XA02IA102 3 20020505 A 6111 SFA13M1ROA BLADE AEROSP ATR42 ATR42320 8680930 EU HAMSTD 14SF 14SF5 NE NR 1 PROP WORN A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 27 97841 280 IAH- FLIGHT 3797, DURING TAKEOFF THE CREW NOTED THAT THE NR 1 ENGINE HAD A VIBRATION. THE AIRCRAFT DID AN AIR RETURN, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 BLADE, NR 1 PROPELLER ASSEMBLY (DUE TO A WORN PIN/ROLLER ASSEMBLY). PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 6 C P7NE 2002050700136 20020507 00136 EA 2002 5 7 COMA0260296 1 20020430 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 729CA 7265 GROUND LIFT DUMP WARNING DURING T/O. OPERATIONAL CHECK OF SYSTEM WAS NORMAL. 2 L 7 2 4F RT A21EA 2002050700137 20020507 00137 EA 2002 5 7 COMA0260297 1 20020430 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 915CA 3540 7013 GEAR DISAGREE WARNING DURING GEAR EXTENSION. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002050700138 20020507 00138 SO 2002 5 7 C2XA02TY080 1 20020507 A 5510 1452139003 HINGE FITTING EMB 145 EMB145 3260210 SO WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS DURING A SCHEDULED 1C/2C INSPECTION THE HORIZ. STAB HINGE PIN LOCKING BRACKETS ON THE LT. AND RT. SIDE HAD WEAR ST EPS IN THEM. MAINT. BLENDED THE WEAR STRIPS,PERFORMED NDT INSPECTION,ALLODINED,PRIMED AND PAINTED IAW WITH GST#1391/02-E MB 135/145 CPM 51-21-04,05.06. ALL WORK WAS ACCOMPLISH AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002050700139 20020507 00139 EU 2002 5 7 DHL2002366004 1 20020503 A 2750 LIMITER AIRBUS 300 A300B4203 3930306 EU T/E FLAP MALFUNCTIONED A DHLA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 01 366DH 249 ON SELECTING FLAPS 8 DEGREES, FLAPS JAMMED AT ABOUT 0 DEGREES, SLATS WERE 16 DEGREES. COMPLETED ABNORMAL PROC FOR JAMME D FLAPS & LANDED. FOUND FLAPS OVERTRAVELED TO UP POSITION. DISCONNECTED TORQUE LIMITER RIG FLAP TO UP POSITION. RECON NECTED TORQUE LIMITER. RUN FLAPS OPERATE NORMAL MM 27-50-00. 2 L 7 2 4F RT A35EU 2002050700140 20020507 00140 NM 2002 5 7 DHL2002726514 1 20020417 A 5320 PANEL BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, NLG WW LT SIDEWALL PANEL IS CRACKED BS 290 WL 198 APPROX UNDERNEATH FITTING SUPPORT DOOR ACTUATOR 2 PLAC ES CRACKED (NDT CONFIRMED). ROUTED OUT CRACKED AREA. NDT INSP AROUND ROUTED OUT AREA PER NDT MANUAL, NO CRACKS NOTED. FABRICATED DOUBLER AND INSTALLED IAW B-727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002050700141 20020507 00141 NM 2002 5 7 UPS02438066 1 20020418 A 3350 POWER SUPPLY BOEING 747 747212B 1384886 NM CABIN DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:PFLT EMERGENCY EXIT SIGN ABOVE UPPER DECK ESCAPE SLIDE DOOR INOP. LIGHT COMES ON AND THEN GOES OUT QUIC KLY. REMOVED AND REPLACED POWER PACK PER AMM 33-51-04, OPS CHECK GOOD. 2 L 7 4 4F A20WE 2002050700142 20020507 00142 NM 2002 5 7 UPS02438067 1 20020419 A 2612 FIRE WARNING BOEING 747 747212B 1384886 NM COCKPIT FALSE ACTIVATION A IPXA K NONE N FALSE WARNING CR CRUISE 1 SO 01 525UP 21939 INSPECTION TYPE:N/A DURING CRUISE AT FL270, ALL FIRE WARNING/DET LIGHTS ILLUMINATED MOMENTARILY AND FIRE BELL ALSO RANG MOMENTARILY. THE FIELD OFF AND GEN OPEN LIGHT ON NUMBER 1 GEN WERE ILLUMINATED. REFER TO ITEM 2 AND T/S FOUND THAT FIR E WARNING/DET LIGHT WERE CAUSED BY SWITCHING ELECTRIC POWER TRANSFER. FIRE WARNING OPERATIONAL TEST OK PER AMM 26-11-00 P501, AMM 26-15-00 P501 AND AMM 26-17-00 P501. 2 L 7 4 4F A20WE 2002050700143 20020507 00143 NM 2002 5 7 UPS02438069 1 20020416 A 5320 65091911 ATTACH FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:MX FWD LOWER CARGO COMPT POS 5 AFT RT O/B VERTICAL RESTRAINT ATTACH STRUCTURE APPEARS CRACKED AT FWD I/B BOLT HOLE. VERIFIED CRACK WITH HEFC. INSTALLED NEW SUPPORT FITTING IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2002050700144 20020507 00144 NM 2002 5 7 UPS02438070 1 20020416 A 5320 65B091914 ATTACH FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:MX FWD LOWER CARGO COMPARTMENT AFT END VERTICAL RESTRAINT ATTACH STRUCTURE IS CRACKED ON LOWER LEG OF FR AME. LOCATED ON 2ND FROM RIGHT ATTACH STRUCTURE. INSTALLED NEW VR ATTACH FITTING IAW 51-30-02. 2 L 7 4 4F A20WE 2002050700145 20020507 00145 NM 2002 5 7 UPS02438071 1 20020416 A 5320 65091912 ATTACH FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:MX FWD LOWER CARGO COMPARTMENT AFT END VERTICAL RESTRAINT ATTACH STRUCTURE LOCATED FAR LEFT SIDE IS CRAC KED ON I/B UPPER LEG OF FRAME BOTTOM SIDE. REMOVED CRACKED RESTRAINT FITTING IAW SRM 51-30-02. INSTALLED NEW RESTRAINT FITTING IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2002050700146 20020507 00146 NM 2002 5 7 UPS02438072 1 20020416 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:MX FWD LOWER CARGO COMPARTMENT AFT END VERTICAL RESTRAINT ATTACH STRUCTURE O/B LEFT SIDE HAS LARGE AMOUN T OF CORROSION ON SEAT TRACK. SEAT TRACK IS ALSO CRACKED. REMOVED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-10-05 FIG 5 . FABBED NEW SECTION OF SEAT TRACK IAW 53-10-05. FABBED REPAIR ANGLES IAW SRM 51-10-01. INSTALLED NEW TRACK AND REPAI R ANGLES. 2 L 7 4 4F A20WE 2002050700147 20020507 00147 NM 2002 5 7 UPS02438073 1 20020418 A 5420 STRAP BOEING 747 747121 1384871 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:N/A NR 3 PYLON REAR ENG, MOUNT BULKHEAD FRAME STRAP CRACKED AT I/B AREA JUST ABOVE AFT LOWER SPAR. REPA IR CUTOUT AS PER SRM 54-10-03 FIG 18, 54-30-03 FIG 35 & 54-30-03 FIG 36. 2 L 7 4 4F A20WE 2002050700148 20020507 00148 NM 2002 5 7 UPS02438074 1 20020418 A 5412 FIREWALL BOEING 747 747121 1384871 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: NR 2 PYLON LOWER FIREWALL WEB O/B POSN CRACKED AT NAC 221.9 REAR ENGINE MOUNT BULKHEAD AREA. NR 2 PYLO N LOWER FIREWALL WEB REPAIRED AS PER SRM 54-10-03 FIG 2. 2 L 7 4 4F A20WE 2002050700149 20020507 00149 NM 2002 5 7 UPS02438075 1 20020419 A 3350 POWER SUPPLY BOEING 747 747200 1384847 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:N/A 2 EMERGENCY LIGHTS ABOVE CREW SERVICE DOOR INOP. REMOVED AND REPLACED CREW SERVICE DOOR POWER SUPPL Y MODULE IAW B747 MM 33-51-04, OPS CHECKS GOOD. 2 L 7 4 4F RT A20WE 2002050700150 20020507 00150 NM 2002 5 7 UPS02438076 1 20020419 A 3350 CONNECTOR BOEING 747 747200 1384847 NM COCKPIT DIRTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:N/A CREW SERVICE DOOR EMERGENCY EXIT SIGN INOP. OPS CHECK AFTER CLEANING CANNON PLUG NO DEFECTS NOTED P ER MM 33-51-04. 2 L 7 4 4F RT A20WE 2002050700151 20020507 00151 NM 2002 5 7 UPS02438077 1 20020419 A 3350 LIGHT BOEING 747 747200 1384847 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:N/A CREW SERVICE DOOR CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED CEILING EMERGENCY LIGHT IAW B7 47 MM 33-51-07, OPS CHECKS GOOD. 2 L 7 4 4F RT A20WE 2002050700152 20020507 00152 NE 2002 5 7 UPS02438086 2 20020416 A 7200 ENGINE BOEING 747 747256B 1384865 NM PWA JT9 JT9D* NE NR 1 MALFUNCTIONED A IPXA K NONE A FLAME/FIRE NR NOT REPORTED 1 SO 01 528UP INSPECTION TYPE:N/A NR 1 ENG TAIL PIPE FIRE AFTER START LEVER CUTOFF (ABOUT 15 SECONDS) ON ENG WAN 668162. REMOVED AND INSTALLED ENGINE. 2 L 7 4 4F 4 F RT A20WE E20EA 2002050700153 20020507 00153 NE 2002 5 7 UPS02438087 2 20020421 A 7311 811945 HEAT EXCHANGER BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE DEFECTIVE A IPXA E ENGINE SHUTDOWN M OVER TEMP CR CRUISE 1 SO 01 675UP 20390 P662709CN INSPECTION TYPE:N/A ENG NR 2 OIL TEMP CLIMBED INTO YELLOW RANGE THEN HIT RED RADIAL 8 MIN LATER. EXECUTED PRECAUTIONARY INFLIGHT SHUTDOWN AT 08H53Z. REMOVED AND REPLACED FUEL HEATER VALVE AND FUEL /OIL COOLER. ENG RUN AT EPR 1.18 FOR 32 MIN OIL TEMP 70 DEGREES C. ALL CHECKS OK. 2 L 7 4 4F 4 F A20WE E20EA 2002050700154 20020507 00154 NM 2002 5 7 UPS02537808 1 20020309 A 7830 ACTUATOR BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE THRUST REVERSER LEAKING A IPXA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 01 416UP 23903 717928 INSPECTION TYPE:N/A UPON LANDING AT OMA CABIN SMOKE WHEN REVERSE INITIATED (NOTE: ONLY RT PACK ON DURING LANDING). INS PECTED A/C FOR LEAKS. FOUND UPPER I/B TR ACT LEAKING REPLACED RT UPPER I/B ACTUATOR. RAN PACK, OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002050700155 20020507 00155 NM 2002 5 7 UPS02537928 1 20020304 A 5347 HFAB53SEA009 SEAT TRACK BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 406UP 23728 INSPECTION TYPE:MOD UPON REMOVAL OF BALLMAT, FOUND CORROSION IN SEAT TRACK AT BS 614, LBL 45, WL 208. REMOVED AND REPLA CED SEAT TRACK FROM BS 440 TO 680, LBL 45 PER SRM 51-40-02 AND SRM 53-00-52. 2 L 7 2 4F RT A2NM 2002050700156 20020507 00156 NM 2002 5 7 UPS02537963 1 20020323 A 5315 BAC14902865 FLOORBEAM BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 452UP 25473 INSPECTION TYPE:MOD FLOORBEAM CORRODED STA 1200 TOP SURFACE LBL 25 - 45. 2 L 7 2 4F RT A2NM 2002050700157 20020507 00157 NM 2002 5 7 UPS02538012 1 20020409 A 5610 141T480013 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE:IN PILOT REPORT L1 WINDOW CRACKED. REMOVED AND REPLACED L1 WINDOW IAW MM 56-11-04-4. 2 L 7 2 4F RT A2NM 2002050700158 20020507 00158 NM 2002 5 7 UPS02538021 1 20020411 A 5610 SEAL BOEING 757 75724APF 1384969 NM COCKPIT WINDOW LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 427UP 25458 INSPECTION TYPE:N/A L2 WINDOW LEAKING. REMOVED AND REPLACED L2 WINDOW FRAME SEAL WITH REF TO MM 56-11-53-4, OPS AND LEA K CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002050700159 20020507 00159 NM 2002 5 7 UPS02637857 1 20020313 A 5330 SKIN BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 313UP 27764 INSPECTION TYPE:PNT CRACK IN LOWER FUSELAGE SKIN APPROX 1.125 INCH AT BS 786 STRINGER 38R. 2 L 7 2 4F RT A1NM 2002050700160 20020507 00160 WP 2002 5 7 UPS02837816 1 20020311 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS BATTERY DEAD. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY SYSTEM, OPS C HECKS NORMAL PER MM 33-50-01. 2 L 7 4 4F RT 4A25 2002050700161 20020507 00161 WP 2002 5 7 UPS02837817 1 20020224 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C1 SHEAR TIE BROKEN AT STA 1140 BETWEEN LONG 34L TO 35L. REMOVED, FABRICATED, AND REPLACED SHEAR TIE SE CTION IAW SRM 53-4-1, 51-1-20D, 53-1-0. 2 L 7 4 4F RT 4A25 2002050700162 20020507 00162 WP 2002 5 7 UPS02837824 1 20020301 A 5753 WEB DOUG DC8 DC871F 302199D WP T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C23 LT WING I/B FLAP I/B END CLOSEOUT WEB IS CRACKED AND HAS LOOSE FASTENERS. REMOVED AND REPLACED WEB IAW REO G08529. 2 L 7 4 4F RT 4A25 2002050700163 20020507 00163 WP 2002 5 7 UPS02837850 1 20020221 A 5220 3755862 FITTING DOUG DC8 DC871F 302199D WP EMERGENCY EXIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C RT AFT OVERWING EMERGENCY DOOR AFT FRAME ATTACH ANGLE CRACKED. REMOVED DAMAGED FITTING PER SRM 51-1-2 0D. INSTALLED PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002050700164 20020507 00164 WP 2002 5 7 UPS02837851 1 20020228 A 5210 DWG5755530 STRUCTURE DOUG DC8 DC871F 302199D WP L2 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C LT AFT ENTRY DOOR STRUCTURE CRACKED AT LOWER HINGE CUTOUT. STOP DRILLED CRACK PER SRM 52-2-0 FIG 6. NDT VERIFIED CRACK TERM PER SPM 06-10-01.001. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 52-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002050700165 20020507 00165 WP 2002 5 7 UPS02837852 1 20020222 A 5310 SRO8530021 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C R2 DOOR FRAME UPPER AFT CORNER CRACKED NEAR STA 1655, L11. REPAIRED PER DHSK707-642. 2 L 7 4 4F RT 4A25 2002050700166 20020507 00166 SO 2002 5 7 C2XA02SH003 1 20020419 A 2700 14573604005 SPRING EMB 145 EMB145ER 3260211 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 SHV - DURING C-CHECK INSPECTION, THE RIGHT HAND INBOARD AND OUTBOARD FLAP LOWER SHROUD SPRINGS WERE FOUND TO BE CORRODED . MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPRINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002051300040 20020513 00040 SO 2002 5 13 C2XA02SH004 1 20020419 A 2750 14573604005 SPRING EMB 145 EMB145ER 3260211 SO T/E FLAP CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 SHV - DURING C-CHECK INSPECTION, THE LEFT HAND INBOARD AND OUTBOARD LOWER FLAP SHROUD SPRINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPRINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002050700167 20020507 00167 NM 2002 5 7 SWAA020920 1 20020502 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 649SW 27719 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKETS CORRODED. REMOVED AND R EPLACED ATTACH BRACKETS PER SRM. 2 L 7 2 4F RT A16WE 2002050700168 20020507 00168 NM 2002 5 7 SWAA020923 1 20020502 A 5311 6516301 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188 AT WL 210 LT. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002050700169 20020507 00169 NM 2002 5 7 SWAA020926 1 20020501 A 2780 65C26797 FITTING BOEING 737 7372H4 138448C NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 NR 5 L/E SLAT ACTUATOR MOUNT FITTING CRACKED. REMOVED AND REPLACED FITTING PER MM. 2 L 7 2 4F A16WE 2002050700170 20020507 00170 NM 2002 5 7 SWAA020927 1 20020502 A 5330 6546882 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (5 EA) AT STR 2R, BS'S 1099, 1111, 1113, 1115 AND 1116.5. REPA IRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002050700171 20020507 00171 NM 2002 5 7 SWAA020928 1 20020502 A 5330 6546882 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1065, STR 3R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002050700172 20020507 00172 NM 2002 5 7 SWAA020929 1 20020504 A 3350 207377 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 362SW 26573 EEPLS RED LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002050700173 20020507 00173 NM 2002 5 7 SWAA020935 1 20020504 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 780SW 27885 EEPLS COVER LOOSE. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002050700174 20020507 00174 2002 5 7 SWAA020938 4 20020503 A 2565 6557463 BRACKET BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 740SW 29276 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2002050700175 20020507 00175 NM 2002 5 7 SWAA020940 1 20020504 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 21R. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F A16WE 2002050700176 20020507 00176 NM 2002 5 7 SWAA020941 1 20020503 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10R, BS'S 500A, 500C AND 500D. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2002050700177 20020507 00177 NM 2002 5 7 SWAA020942 1 20020505 A 5330 6545765 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 520, STR 27L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002050700178 20020507 00178 NM 2002 5 7 SWAA020943 1 20020504 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 6, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002050700179 20020507 00179 NM 2002 5 7 SWAA020944 1 20020504 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002050700180 20020507 00180 NM 2002 5 7 SWAA020945 1 20020505 A 5753 6546435185 FLAP BOEING 737 7372H4 138448C NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4D CHECK, FOUND LT OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT OTBD T/E AFT FLAP PER MM. 2 L 7 2 4F A16WE 2002050700181 20020507 00181 NM 2002 5 7 SWAA020947 1 20020505 A 5754 65C26686 SLAT BOEING 737 7372H4 138448C NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4D CHECK, FOUND NR 4 L/E SLAT DELAMINATED AT UPPER INBD CORNER. REPAIRED L/E SLAT PER SRM. 2 L 7 2 4F A16WE 2002050700182 20020507 00182 NM 2002 5 7 VNAA0205002 1 20020502 A 5200 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 461PS 3075 AFTER DEPARTURE FROM DAY, THE CREW RECEIVED A LEFT HAND EMERGENCY DOOR OPEN INDICATION. FLIGHT 9412 THEN RETURNED TO DA Y. MAINTENANCE INSPECTED AND ADJUSTED THE EMERGENCY DOOR PROXIMITY SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002050700183 20020507 00183 NE 2002 5 7 COMA0210017 2 20020503 A 7200 ENGINE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE A COMA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SO 01 268CA 120262 FLIGHT 5075 T6 WARNING DURING T/O.COMPLIED WITH COMPRESSOR WASH, ENGINE PERFORMANCE RUNS WERE WITHIN LIMITS. 2 L 7 2 4T 4 T RT A31SO E20NE 2002050700184 20020507 00184 SO 2002 5 7 COMA0210018 1 20020503 A 3350 10130115 SIGN EMB 120 EMB120RT 3260202 SO CABIN BROKEN A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 267CA 120259 FLIGHT 5021 EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN.REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 2002050700185 20020507 00185 EA 2002 5 7 COMA0260302 1 20020504 A 2450 BUSS TIE CNDAIR CL600 CL6002B19 1900309 EA A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 451CA 7562 FLIGHT 5117 AUTO XFER FAIL MESSAGE.RESET A/C BUSS 1 - MESSAGE CLEARED. 2 L 7 2 4F RT A21EA 2002050700186 20020507 00186 EA 2002 5 7 COMA0260303 1 20020504 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS DE DESCENT 1 SO 01 811CA 7380 FLIGHT 5570 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002050700188 20020507 00188 NM 2002 5 7 QXEA0200736 1 20020502 A 3350 6138001 BATTERY PACK BOMBDR DHC8 DHC8401 1390041 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 405QX 1827 4047 SEA-AFT EMERGENCY LIGHTS TURN OFF AFTER 10 SECONDS WITH SWITCH IN ON POSITION. REMOVED AND REPLACED EMERGENCY LIGTH BAT TERY PACKS AT STATIONS 692. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002050700189 20020507 00189 WP 2002 5 7 MWEA020320 1 20020504 A 5320 J0600923N WEB DOUG DC9 DC932 3022066 WP VENTRAL DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 VENTRAL DOOR CORNER JAMB WEB IS CRACKED 3/8 INCH OUT OF RELIEF HOLE ON FORWARD SIDE, UPPER LEFT CORNER. -- INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002050700190 20020507 00190 WP 2002 5 7 MWEA020321 1 20020505 A 2597 50226 OVEN DOUG DC9 DC914 3022034 WP GALLEY SHORTED A MWEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 31 500ME 45711 F/A REPORTED SEEING AN ORANGE FLASH ABOVE AND BEHIND GALLEY OVEN. -- NWA MTC INSPECTED LEFT AND RIGHT OVENS. FOUND OVE N GROUND WIRE SHORTED. PULLED AND COLLARD LEFT AND RIGHT OVEN CIRCUIT BREAKERS. DEFERRED OVENS PER MEL 25-12. REMOVED AN D REPLACED OVENS DMI CLEARED PLACARD REMOVED. CIRCUIT BREAKERS RESET. OPS CHECK GOOD. 2 L 7 2 4F A6WE 2002050700191 20020507 00191 SO 2002 5 7 C2XA02SH006 1 20020416 A 5300 12024428001 COWLING EMB 145 EMB145ER 3260211 SO APU COWLING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 SHV - DURING C-CHECK INSPECTION, THE LOWER RIGHT HAND APU COWLING MOUNT OPENING WAS FOUNDS TO BE CRACKED. MAINTENANCE ST OP DRILLED THE CRACK, AND INSTALLED A REPAIR DOUBLER ON THE AFFECTED AREA IN ACCORDANCE WITH EMB-145 SRM 51-40-02, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002050700192 20020507 00192 SO 2002 5 7 C2XA02TY084 1 20020507 A 5300 14520552001 SKIN EMB 145 EMB145 3260210 SO FUSELAGE NICKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS During a scheduled inspection the #1 right hand passenger window frame was found to be damaged (nicked). Maintena nce accomplished a blend out repair which included a NDT inspection IAW EMB GST#1392/02, EMB-145 M.M. 56-20-00, CPM 51-2 1-04, 51-21-05 and 51-21-06. The repair was found to be satisfactory, the aircraft will be released upon completion of i nspection. 2 L 7 2 4F RT T00011AT 2002050700193 20020507 00193 SO 2002 5 7 C2XA02TY085 1 20020507 A 5300 14520553001 SKIN EMB 145 EMB145 3260210 SO FUSELAGE NICKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS During a scheduled inspection the L/H #1 passenger window frame was found to be nicked. Maintenance accomplished a blend out repair which included a NDT inspection IAW EMB GST#1393/02, EMB-145 M.M. 56-20-00, CPM 51-21-04, 51-21-05, a nd 51-21-06. The repair was found to be satisfactory, the aircraft will be released upon completion of inspection. 2 L 7 2 4F RT T00011AT 2002050800001 20020508 00001 EU 2002 5 8 MALA020266 1 20020503 A 5420 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU A MALA O OTHER H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 GL 15 442XJ 340B442 DURING COMPLETION OF TASK CARD #335003, BATTERY PACK POWER SUPPLY 24LN FAILED TEST. MAINTENANCE REPLACED POWER SUPPLY P N 3301-51, SN/OFF 1311 SN/ON 2192. IAW SAAB AMM 33-50-10 2 L 7 2 4T RT A52EU 2002050800002 20020508 00002 NM 2002 5 8 ASAA0210020 1 20020108 A 5311 65C314272 FRAME BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 444, WATERLINE 156 CRACKED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002050800003 20020508 00003 NM 2002 5 8 ASAA0210021 1 20020108 A 5330 655496047 DOUBLER BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND DOUBLER AT BS 360, STRINGER 11R-13R CUT. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002050800004 20020508 00004 NM 2002 5 8 ASAA0210026 1 20020109 A 5330 65458352 BEAR STRAP BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND BEAR STRAP AT BS 260, RBL 18 WITH AN OVERSIZED HOLE. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002050800005 20020508 00005 NM 2002 5 8 ASAA0210028 1 20020109 A 5260 656096310 LATCH BOEING 737 737298C 1384490 NM AIRSTAIR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND AIRSTAIR LATCH MECHANISM BASE PLATE ASSEMBLY AT BS 987, LEFT BUTTOCK LINE 50 CORRO DED. REMOVED AND REPLACED AIRSTAIR LATCH MECHANISM BASE PLATE ASSEMBLY PER SRM. (M) 2 L 7 2 4F RT A16WE 2002050800006 20020508 00006 NM 2002 5 8 ASAA0210029 1 20020109 A 5330 65C32358 SKIN PANEL BOEING 737 737298C 1384490 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 360, STRINGER 19R DENTED. REPAIRED SKIN PANEL PER EA. (M) 2 L 7 2 4F RT A16WE 2002050800007 20020508 00007 NM 2002 5 8 ASAA0210030 1 20020109 A 5330 6545804147 DOUBLER BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND DOUBLER AT BS 260, RBL 18 WITH AN OVERSIZED HOLE. REPAIRED DOUBLER PER EA. (M) 2 L 7 2 4F RT A16WE 2002050800008 20020508 00008 NM 2002 5 8 ASAA0210031 1 20020109 A 5315 65549059 FLOORBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 460, LBL 20 LBL 39 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2 L 7 2 4F RT A16WE 2002050800009 20020508 00009 NM 2002 5 8 ASAA0210032 1 20020109 A 5315 65548932 FLOORBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 420, RBL 2, RBL 23 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2 L 7 2 4F RT A16WE 2002050800010 20020508 00010 NM 2002 5 8 ASAA0210033 1 20020109 A 5311 6554967 FRAME BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT BS 706-727B, RBL 45 CORRODED. REPAIRED CHORD PER EA. (M) 2 L 7 2 4F RT A16WE 2002050800011 20020508 00011 NM 2002 5 8 ASAA0210034 1 20020109 A 5315 6554906501 FLOORBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 500A, LBL 52 CORRODED. REPAIRED CHORD PER EA. (M) 2 L 7 2 4F RT A16WE 2002050800012 20020508 00012 EU 2002 5 8 SIMA200209433 1 20020404 A 2120 ODOR SAAB SF340 340B 7860101 EU COCKPIT DETECTED A SIMA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 211NE 340B211 SHV - FLT 3471 - CREW REPORTED SHARP ELECTRICAL/SMOKE SMELL IN COCKPIT AFTER ARRIVAL AND TAXI TO THE GATE. AVIONICS MAS TER SMOKE WARNING ILLUMINATED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. PERFORMED GROUND WITH ALL SYSTEMS ON AND F OUND NO DEFECT AT THIS TIME. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002050800013 20020508 00013 EU 2002 5 8 SIMA200209701 1 20020407 A 2612 51533172 LOOP SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A SIMA K NONE N FALSE WARNING DE DESCENT 1 SW 21 174AE 340B174 DFW - FLT 3826 - CREW REPORTED A LEFT HAND BLEED LEAK DURING FLIGHT. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE TO FLAP DETECTION LOOP IAW SAAB MM. OPERATIONAL CHECK WAS GOO D AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002050800014 20020508 00014 EU 2002 5 8 SIMA200210001 1 20020404 A 5315 FLOORBEAM SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AE 340B348 DURING AN HMBV INSPECTION OF AIRCRAFT, FOUND GALLEY FLOOR FRAME 272 CORRODED. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, A FILLER, AND A SHIM. WORK DONE IAW SAAB 340 SRM 53-70-30 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002050800015 20020508 00015 EU 2002 5 8 SIMA200210002 1 20020402 A 5347 7253799383 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AE 340B348 DURING AN HMBV INSPECTION OF AIRCRAFT, FOUND CABIN SEAT TRACK 18.3L FORWARD NEAR KICK PLATE CORRODED BEYOND SRM LIMITS. REMOVED SECTION OF CORRODED SEAT TRACK. INSTALLED IAW SAAB 340 SRM AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002050800016 20020508 00016 SO 2002 5 8 SIMA200210201 1 20020407 A 5311 12010732001 FRAME EMB 145 EMB145 3260210 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - DURING INSPECTION OF AIRCRAFT, FOUND FRAME 81 CHAFED. REPLACED CHAFED FRAME IAW EMB 145 SRM 51-20-03, 51-40-03, A ND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002050800017 20020508 00017 SO 2002 5 8 SIMA200210202 1 20020407 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIGHT SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING. FABRI CATED AND INSTALLED DOUBLER IAW EMB GST-1140/02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002050800018 20020508 00018 SO 2002 5 8 SIMA200210203 1 20020405 A 5315 1452171300 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY CENTER BEAM. REPLACED GALLEY CENTER BEAM IAW EMB 145 EMB SRM 1 45 51-40-02, GST-1128/02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002050800019 20020508 00019 EU 2002 5 8 SIMA200210204 1 20020408 A 5315 FLOORBEAM SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AE 340B348 ABI - DURING INSPECTION OF AIRCRAFT, FOUND PREVIOUSLY REPAIRED GALLEY FLOOR FRAME 258 CORRODED. FABRICATED AND REPLACED DOUBLER, FILLER, AND TWO TRIPLERS IAW SAAB 340 SRM 53-70-30 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002050800020 20020508 00020 EU 2002 5 8 SIMA200210205 1 20020408 A 5311 7253813485 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AE 340B348 ABI - DURING INSPECTION OF AIRCRAFT, FOUND TWO DENTS ON CARGO FRAME 677. REFORMED FRAME. PERFORMED A NDT INSPECTION OF THE FRAME AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER ANGLE. INSTALLED NEW FRAME IAW SAAB 340 REPAIR ST ATEMENT 340SDS003569, PARA 9, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002050800021 20020508 00021 EU 2002 5 8 SIMA200210206 1 20020408 A 5414 FAIRING SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AE 340B348 DURING INSPECTION OF AIRCRAFT, FOUND RIGHT INBOARD NACELLE FILLET FAIRING CHAFED. BLENDED OUT CHAFE. FABRICATED AND IN STALLED DOUBLER IAW SAAB 340 SRM 54-10-10 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002050800022 20020508 00022 NM 2002 5 8 TSAA0251067 1 20020226 A 5315 65C28106 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 FOUND CORROSION ON THE EXISTING UPPER FLANGE FLOORBEAM REPAIR AT STATION 1016, WL 208 BBI 0 TO LBL 15. FABRICATED AND I NSTALLED REPAIR PARTS IAW SRM 53-10-9 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800023 20020508 00023 NM 2002 5 8 TSAA0251068 1 20020226 A 5314 6545866688 KEELBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 FOUND CORROSION ON THE KEEL BEAM LOWER CHORD. CONFIRMED CORROSION REMOVED AND NO EVIDENCE OF CRACKS USING HFEC METHOD. REPAIR COMPLETED IAW ECO 3269. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800024 20020508 00024 NM 2002 5 8 TSAA0251069 1 20020226 A 5314 6545866688 KEELBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 FOUND CORROSION ON THE KEEL BEAM ON RIGHT LOWER FLANGE IN RIGHT AC BAY AT STATION 557 TO STATION 567, STATION 584 AND ST ATION 608. BLENDOUT THE CORROSION THEN FLAT PEENED IAW SOPM CHAPTER 20-10-03. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800025 20020508 00025 NM 2002 5 8 TSAA0251074 1 20020226 A 5320 65C28106 FLOOR SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 IDENTIFIED CORROSION ON FLOOR SUPPORT DIAGONAL LEFT BETWEEN STATION 1006 AND STATION 1016 LBL 5. REMOVED CORROSION IAW SRM 53-10-1 DETAIL I, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800026 20020508 00026 NM 2002 5 8 TSAA0251075 1 20020226 A 5330 6545766 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 10 RT AT BS 500B PLUS 10 UPPER FORWARD CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS AND DOUBLERS. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION G. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800027 20020508 00027 NM 2002 5 8 TSAA0251076 1 20020226 A 5330 6545766 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10, BS 420 0 PLUS 10 AND BS 500 PLUS 10 ON WINDOW NR 1 RIGHT LOWER AFT CORNER. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS AND DOUBLERS. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION G. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800028 20020508 00028 NM 2002 5 8 TSAA0251077 1 20020226 A 5330 6545766 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10 ON WIND OW NR 1 RIGHT UPPER FORWARD CORNER HOLE NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE T RIMMED AREAS. FABRICATED FILLERS AND DOUBLERS. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800029 20020508 00029 NM 2002 5 8 TSAA0251078 1 20020226 A 5330 6545766 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10 ON WIND OW NR 2 RIGHT UPPER FORWARD CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AR EAS. FABRICATED FILLERS AND DOUBLERS. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800030 20020508 00030 NM 2002 5 8 TSAA0251079 1 20020226 A 5330 6545771 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S14L BS 727 PLUS 10 ON WIND OW NR 20 LEFT LOWER FORWARD HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. F ABRICATED FILLERS, QUADRUPLER, DOUBLER AND TRIPLER IAW B 737-53A1177. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION F-R 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800031 20020508 00031 NM 2002 5 8 TSAA0251080 1 20020226 A 5330 6545771 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10L BS 827 PLUS 10 ON WIND OW NR 24 LEFT UPPER AFT HOLES NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED ARE AS. FABRICATED FILLERS, DOUBLER AND TRIPLER. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION E. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4F RT A16WE 2002050800032 20020508 00032 NM 2002 5 8 TSAA0251081 1 20020226 A 5330 6545771 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS BETWEEN S10L BS 767 PLUS 10 AN D BS 827 PLUS 10 ON WINDOW NR 25 LEFT UPPER AFT HOLES NR 10. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS, DOUBLER AND TRIPLER. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION E. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800033 20020508 00033 NM 2002 5 8 TSAA0251082 1 20020226 A 5330 6545766 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10R AND S14R ON WINDOW NR 24 RT UPPER AFT HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FI LLERS, DOUBLER AND TRIPLER. INSTALLED REPAIR PARTS SB 737-53A1176R6 AND S10 AND S14 IAW ECO 3250 DEVIATION J. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800034 20020508 00034 NM 2002 5 8 TSAA0251106 1 20020412 A 5315 6545410 FLOORBEAM BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 FOUND A CRACK AT FUSELAGE STATION 665 FLOORBEAM BL 0 ON THE UPPER CHORD. FABRICATED AND INSTALLED REINFORCING DOUBLER, STIFFENERS, FILLERS, SPLICE PLATE AND ANGLE. REPAIR COMPLETED IAW ECO 2223 R1 PART II DEVIATION D. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800035 20020508 00035 NM 2002 5 8 TSAA0253105 1 20020406 A 5330 6545800 SKIN BOEING 737 7372M6C 1384708 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 FOUND 3 INCH CRACK ON THE FUSELAGE SKIN AT BS 887 ALONG STRINGER 24R. CUT OUT DAMAGED PORTION OF SKIN. VERIFIED CRACK REMOVED USING HFEC. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800036 20020508 00036 NM 2002 5 8 TSAA0253112 1 20020412 A 5313 65C25709 STRINGER BOEING 737 737230 1384401 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 FOUND EXFOLIATION CORROSION ON STRINGER 27L AT BS 967. REMOVED THE DAMAGED SECTION OF THE STRINGER. FABRICATED AND INS TALLED ALL REPAIR PARTS IAW SRM 53-10-3 PAGE 10. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800037 20020508 00037 NM 2002 5 8 TSAA0255063 1 20020226 A 5531 65737881 SPAR BOEING 737 7372X6C 1384552 NM VERTICAL STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 FOUND CORROSION ON LEFT REAR SPAR CHORD 6 INCHES UP FROM VERTICAL STABILIZER ATTACH LUG. BLENDED OUT THE CORROSION AND INSTALLED TAPERED FILLERS. REPAIR ACCOMPLISHED IAW ECO 2509. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800038 20020508 00038 NM 2002 5 8 TSAA0255064 1 20020226 A 5531 65737881 SPAR BOEING 737 7372X6C 1384552 NM VERTICAL STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 FOUND CORROSION ON LEFT REAR SPAR CHORD 46 INCHES UP FROM VERTICAL STABILIZER FIN BETWEEN STATION 99.5 AND 108.7 ATTACH LUG. BLENDED OUT THE CORROSION AND INSTALLED TAPERED FILLERS. REPAIR ACCOMPLISHED IAW ECO 2509. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050800039 20020508 00039 WP 2002 5 8 UPS02837853 1 20020309 A 5320 3755843 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C BATHTUB FITTING CRACKED, STA 1200 L34R-L35R. REMOVED AND REPLACED FITTING PER SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002050800040 20020508 00040 NM 2002 5 8 USAA020121 1 20020304 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 42381 23860 PIT - FOUND INTERCOSTAL CAP CRACKED 1 INCH, BS 500-520. INSTALLED FABRICATED INTERCOSTAL PER SRM 53-30-51 AND SRM 51-10 -02. (M) 2 L 7 2 4F RT A16WE 2002050800041 20020508 00041 CE 2002 5 8 00025 1 20020503 A 3260 LIGHT LEAR 24 24B 5170306 CE COCKPIT LOOSE E HAEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 05 233TW 24B221 AIRCRAFT ON APPROACH TO ORH SELECTED GEAR DOWN, NO RT MAIN GREEN LIGHT, ALL OTHER INDICATIONS NORMAL. FLYBY THE TOWER, TOWER INDICATED GEAR APPEARED DOWN, NORMAL LANDING. MAINTENANCE FOUND BULB LOOSE IN SOCKET AND RESET, CHECKED WITH TEST SWITCH GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4J A10CE 2002050800042 20020508 00042 2002 5 8 0126417 4 20020503 A 2210 7015327901 CONTROL PANEL DORNER DO32 DO328300 NM COCKPIT MALFUNCTIONED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 417FJ AFTER TAKEOFF FROM CAE TO CVG, CREW NOTICE ELECTRICAL SMELL COMING FROM THE GP300 AUTO PILOT PANEL. AN EMERGENCY WAS DE CLARED WITH ATC; FLIGHT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL REMOV ED AND REPLACED THE GP300 AUTO PILOT PANEL AND AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A55NM 2002050800043 20020508 00043 NM 2002 5 8 0126429 1 20020503 A 2120 ODOR DORNER DO32 DO328300 NM COCKPIT DETECTED A VTZA A UNSCHED LANDING B G SMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE CR CRUISE 1 EA 27 429FJ DURING CRUISE FROM GSO TO LGA A/C DIVERTED INTO ACY DUE TO ELECTRICAL SMELL IN THE FLIGHT DECK AND PFD'S WENT BLANK. AN EMERGENCY WAS DECLARED WITH ATC AND AIRCRAFT LANDED IN ACY WITHOUT ANY FURTHER INCIDENT. 2 H 7 2 4T RT A55NM 2002050800044 20020508 00044 NM 2002 5 8 ASAA0210027 1 20020109 A 5714 6562203501 WEB BOEING 737 737298C 1384490 NM CENTER WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING SCHEDULED C-CHECK, FOUND WING CENTER SECTION UPPER SKIN AT BS 565-569, LEFT BUTTOCK LINE 53 CORRODED. REPA IRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002050800045 20020508 00045 GL 2002 5 8 02126629 1 20020505 A 3350 CONNECTOR BOMBDR BD700 BD7001A10 1390006 GL CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 629BR EMERGENCY FLOOR TRACK LIGHTS AT ROLL 10/CD WERE FOUND TO BE INOPERATIVE DURING INSPECTION. MAINTENANCE PERSONNEL SECURE D AN ELECTRICAL CONNECTOR FOR THE EMERGENCY FLOOR TRACK LIGHTING. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAF T WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00003NY 2002050800046 20020508 00046 NM 2002 5 8 2002UALA00765 1 20020426 A 2840 CONTROL UNIT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 521UA 24891 FUEL CONFIGURATION LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE THE CAUSE WAS A COMBINATION OF A LEAK IN THE RIGHT ENGINE DRY BAY AND A DEFECTIVE RIGHT MAIN TANK FUEL FILL VALVE CONTROL UNIT. THE PRIMARY CAUSE OF IMBALANCE CAN BE ATTRIBUTED TO THE FUEL FILL VALVE CONTROL UNIT WHICH WAS STUCK IN THE OPEN POSITION. AN OPEN FUEL FILL VALVE CONTROL UNIT TOGETHER WITH A FULL LOAD OF FUEL IN A CLIMB WOULD TRANSFER FUEL BACK INTO THE FUELING MANIFOLD WHERE IT WOULD DRAIN INTO THE C ENTER TANK. 2 L 7 2 4F 4 F RT A2NM E17NE 2002050800047 20020508 00047 NM 2002 5 8 2002UALA00786 1 20020428 A 5315 FLANGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 AFT PIT FRAME FLANGE AFT SIDE LIP WORN, 2 EACH AREAS FROM FASTENERS STA 1520 BETWEEN STRINGER 22R AND 23R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.L-ANGLE DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002050800048 20020508 00048 NM 2002 5 8 2002UALA00790 1 20020430 A 5315 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 MID CABIN CREASE BEAM HAS EXCESSIVE MATERIAL LOSS AT BODY STATION 1408 RBL71. MAJOR REPAIR ACCOMPLISHED.REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002050800049 20020508 00049 NM 2002 5 8 2002UALA00794 1 20020430 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 FORWARD PIT CENTER LINE CIRCUMFERENTIAL FRAME STATION 800 HAS LOADER JACK-SCREW DAMAGE. SUPPLEMENTAL DATA UPDATE MAJOR R EPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR ON FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2002050800050 20020508 00050 NM 2002 5 8 2002UALA00795 1 20020430 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 AFT PIT FRAME AT STATION 1470 STRINGER 25L IS DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBL ER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002050800051 20020508 00051 SO 2002 5 8 LR7A02034 1 20020507 A 5330 SKIN LKHEED 382 382G 526414U SO FS 317 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 554 4606 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB0502 FOUND FS 317 BELLY SKIN CRACKED AT RBL 18 AND LBL 18, WL 127.REPAIRED IAW SRM SMP 583 51-140-12. NR 0019. 2 H 7 4 4T A1SO 2002050800052 20020508 00052 SO 2002 5 8 LR7A02035 1 20020507 A 5230 ANGLE LKHEED 382 382G 526414U SO FS 1020 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 554 4606 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB0505 FOUND CARGO DOOR 2 EA. CRACKED ANGLES AT FS 1020, WL 256, BL0 & RBL 1 0.REPAIRED IAW SRM SMP 583 51-140-19. NR 0021. 2 H 7 4 4T A1SO 2002050800053 20020508 00053 WP 2002 5 8 MWEA020322 1 20020508 A 5311 5911448503 FRAME DOUG DC9 DC932 3022066 WP STATION 775 UNSERVICEABLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 CUT AND REMOVED FRAME STATION 775 AT LONGERONS 27 LEFT THROUGH 27 RIGHT TO FACILITATE OTHER MAINTENANCE. -- CUT SHEAR TIE, REMOVED FRAME TO INTERCOSTAL CLIPS TO FACILITATE OTHER MAINTENANCE. LOCATED AND DRILLED NEW FRAME SECTION. FABRICAT ED PLATE. LOCATED AND DRILLED FRAME SPLICES. INSTALLED FRAME, SPLICES, AND SHIMS. 2 L 7 2 4F A6WE 2002050800055 20020508 00055 NM 2002 5 8 02FDEA00308 1 20020506 A 2781 POSITION SWITCH BOEING 727 727200 138407E NM L/E FLAP FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 258FE 20940 RIGHT INBOARD LEADING EDGE FLAP NR 5 FAILED TO RETRACT WHEN FLAPS 2 SELECTED. REMOVED AND REPLACED NR 5 LEADING EDGE FL AP POSITION SWITCH PER MM 27-80-001-4. OPS CHECK NORMAL. 2 L 7 3 4F RT A3WE 2002050800056 20020508 00056 2002 5 8 GTIA020242 4 20020322 A 2210 CONTROLLER DOUG DC9 DC932 3022066 WP AUTOPILOT SYS FAULTY A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 12536 47113 ACY - FLT 8012 - A/P WILL NOT STAY ENGAGED. REMOVED AND REPLACED AUTOMATIC PILOT CONTROLLER. OPERATIONAL CHECK NORMAL IAW DC9 MM 22-10-2. (M) 2 L 7 2 4F A6WE 2002050800057 20020508 00057 WP 2002 5 8 GTIA020243 1 20020323 A 3350 60030431 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 603CA 49508 FLL - FLT 1258 - PREFLIGHT CHECK, EMERGENCY LIGHTS FAIL TO COME ON WITH SWITCH IN ON POSITION. REMOVED AND REPLACED FOR WARD CABIN EMERGENCY LIGHT POWER PACK. OPS CHECK GOOD IAW MM 33-60-00. OPS NORMAL. (M) 2 L 7 2 4F A6WE 2002050800058 20020508 00058 WP 2002 5 8 GTIA020244 1 20020322 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 802NK 53168 FLL - EMERGENCY LIGHTS AT EMERGENCY EXIT AFT ON LEFT AND RIGHT SIDES ROW 22AC AND 22DEF ARE INOPERATIVE. REMOVED AND RE PLACED BATTERIES IN THE CONT. UNIT FOR LT AND RIGHT AFT EMERGENCY EXIT ROW OVERHEAD LIGHTS. OPS CHECK GOOD IAW MM 33-5 0-00. (M) 2 L 7 2 4F RT A6WE 2002050800059 20020508 00059 2002 5 8 GTIA020245 4 20020322 A 2215 4034237915 SERVO DOUG DC9 DC983 3022083 WP AUTOPILOT SYS FAILED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 808NK 49504 FLT 386 - DTW - AUTOPILOT WILL NOT STAY ENGAGED, TRIPS OFF EVERY 2-3 MINUTES, DFGS NR 1 OR NR 2, ALT TRIM OK. FOUND ELE VATOR POWER SERVO FAIL IN FLIGHT FAULT REVIEW. REMOVED AND REPLACED ELEVATOR SERVO IAW MM 21-12-01, PERFORMED AUTO PILO T CHECK AND RTS. OPS CHECK GOOD IAW MM 22-10-00 AND 22-01-01. (M) 2 L 7 2 4F RT A6WE 2002050800060 20020508 00060 WP 2002 5 8 GTIA020246 1 20020317 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 816NK 49140 FLL - AISLE OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 6, 7 AND 8. REMOVED AND REPLACED BATTERIES FOR ASSOCIATED LIG HTS. OPS CHECK GOOD IAW MM 33-50-00. (M) 2 L 7 2 4F A6WE 2002050800061 20020508 00061 WP 2002 5 8 GTIA020247 1 20020323 A 3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083 WP LT MLG DIRTY A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 16892 49391 DTW - FOUND AFTER DEPARTURE DURING GEAR RETRACTION, GOT A RED UNSAFE LIGHT ON THE LEFT MAIN. RECYCLED THE GEAR AND HAD NORMAL INDICATIONS. CLEAN PROXIMITY SENSORS, OPS CHECKED GOOD IAW MD80 MM 32-60-05. (M) 2 L 7 2 4F RT A6WE 2002050800062 20020508 00062 WP 2002 5 8 GTIA020248 1 20020323 A 2741 SWITCH DOUG DC9 DC983 3022083 WP STAB TRIM FAULTY A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 16892 49391 DTW - FLT 909 - ALTERNATE TRIM MOTO TRIMS WHEN RIGHT SWITCH IS MOVED. LEFT SWITCH IN CENTER POSITION, RIGHT SWITCH ALON E WILL MOVE TRIM IN BOTH DIRECTIONS. REMOVED AND REPLACED ALT TRIM BRAKE RELEASE SWITCH AND ALT TRIM SWITCH. SYSTEM OP S CHECK GOOD IAW MM 27-40-00. (M) 2 L 7 2 4F RT A6WE 2002050800063 20020508 00063 WP 2002 5 8 GTIA020249 1 20020322 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 16892 49391 DTW - SAFETY GLOW FLOOR PATH LIGHTING HAS NO BREAKS AT LEFT OVERWING EXITS. REPOSITIONED SAFETY GLOW FLOOR PATH LIGHTIN G AT LEFT OVERWING EXITS IAW SPIRIT AIRLINES ENGINEERING DRAWING NR SG-DC9 REVISION F. (M) 2 L 7 2 4F RT A6WE 2002050800064 20020508 00064 NM 2002 5 8 GTIA020250 1 20020327 A 2720 LIMITER DOUG MD80 MD83 3023681 NM RUDDER LACK OF LUBE A GTIA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 23 822NK 49392 FLT 198 - ACY - RUDDER TRAVEL UNRESTRICTED LIGHT DID NOT COME ON DURING FINAL APPROACH UNTIL SLOWING TO BELOW 150 KIAS. CLEANED RUDDER PITOT DRAIN SUMP AND LUBRICATED RUDDER LIMITER SYSTEM IAW MD80 27-20-00. NO DEFECTS NOTED. CLEANED PRO XIMITY SENSOR IAW 27-20-06. (M) 2 L 7 2 4F RT 2002050800065 20020508 00065 WP 2002 5 8 GTIA020252 1 20020323 A 3350 SOCKET DOUG DC9 DC983 3022083 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 809NK 49503 LGA - FLT 774 - FOUND EMERGENCY LIGHT IN FORWARD OVERHEAD INOPERATIVE. FOUND SOCKET LOOSE. RESECURED SOCKET AND RELAMP ED. OPS CHECK NORMAL IAW MM 33-50-00. (M) 2 L 7 2 4F RT A6WE 2002050800066 20020508 00066 WP 2002 5 8 DHL2002807557 1 20020316 A 5510 37024963 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 DURING C CHECK FOUND L/H HORIZTAL STABILIZER ATTACH FITTING OF UPPER FAIRING,FWD PART CRACKED 5 IN.REMOVED DAMAGED FITTI NG PER SRM 51-3-0 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-3-0 PG 1 2 L 7 4 4F RT 4A25 2002050800067 20020508 00067 WP 2002 5 8 DHL2002807558 1 20020312 A 5740 3651809IN FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 DURING C CHECK, FOUND L/H INBD FLAP WELL FITTING WITH CRACK IN IT AT STA XW 70.000.REMOVED DAMAGED FITTING AT STA. 70.00 0 PER SRM 51-3-0 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2002050800068 20020508 00068 WP 2002 5 8 DHL2002807559 1 20020417 A 5320 3779762US01 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 MAIN CARGO COMPARTMENT-2 IN CRACK ON BATHTUB FITTING AT STA 670.000-680.000 L-41.REMOVED DAMAGED FITTING PER SRM 51-1-20 D PG 21.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW BATHTUB FITTING PER SRM 51-1-20D PG1. 2 L 7 4 4F RT 4A25 2002050800069 20020508 00069 WP 2002 5 8 DHL2002807560 1 20020414 A 5730 5770409501 DOUBLER DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 LFT WINGCTR L/E SHOWS INTERNAL DOUBLER CRACKED 12 IN XFS 422.750.REMOVED DAMAGED DOUBLER PER SRM 51-3-0 PG 1.CLEANED TRE ATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW DOUBLER PER SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2002050800070 20020508 00070 WP 2002 5 8 DHL2002807561 1 20020419 A 5740 36449242 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 LT WING REAR SPAR AUX INTERIOR SHOWS A CRACKED FITTING 2 IN AT STA XW 80.000.REMOVED CRACKED FITTING PER SRM 51-3-0 PG 1 .FABRICATED NEW FITTING (7075-T651).CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-3-0 PG1 2 L 7 4 4F RT 4A25 2002050800071 20020508 00071 WP 2002 5 8 DHL2002807562 1 20020415 A 5320 37558201 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 MAIN CARGO COMPT. FITTING CRACKED 2 IN AT STA 420.000L-10-R.REMOVED DAMAGED FITTING PER SRM 51-1-20D.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.FABRICATED NEW FITTING (7075.T651)PER ATM P0111359, DWNG 3755820,SEMAM 2D02300.CLEANED TREATED A ND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002050800072 20020508 00072 WP 2002 5 8 DHL2002807563 1 20020417 A 5730 36520232 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 RT WING T/E LOWER SKIN FITTING CRACKED 2 IN AT XRS 351.000.REMOVED DAMAGED FITTING PER SRM 51-1-21 PG1.CLEANED TERATED A ND PRIMED AREA PER SRM 51-1-8B.FABRICATED NEW FITTING (7075.T651) PER ATM PO111340,DWG 3652023,EA200298.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-21 PG1 2 L 7 4 4F RT 4A25 2002050800073 20020508 00073 WP 2002 5 8 DHL2002807567 1 20020418 A 5300 4772397U1 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AFT FUESLAGE INTERIOR FITTING CRACKED 2 IN AT STA 1776.000 L-17 R.REMOVED CRACKED FITTING PER SRM 51-1-20D PG 21.CLEANED TERATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20 PG 9 2 L 7 4 4F RT 4A25 2002050800074 20020508 00074 WP 2002 5 8 DHL2002807568 1 20020416 A 5320 3779658501 FITTING DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 MAIN CARGO COMPARTMENT 2 IN CRACK IN BATHTUB FITTING STA 847.000-857.000REMOVED DAMAGED BATHTUB FITTING PER SRM 51-1-20 D PG 21.FABRICATED NEW FITTING (7075-T651)PER ATM PO 111423,DWG 3779658.EA SEMAN 2002312.CLEANED TREATED AND PRIMED PER SRM 51-1-8BINSTALLED NEW FITTING PER SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002050800075 20020508 00075 WP 2002 5 8 DHL2002807569 1 20020418 A 5300 51616757 LONGERON DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AFT FUESLAGE INTERIOR LONG 17R CRACKED AT STA 776.000.REMOVED CRACKED LONGERON PER SRM 51-120D PG 21.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW LONGERON PER SRM 51-120D PG 9. 2 L 7 4 4F RT 4A25 2002050800076 20020508 00076 2002 5 8 GTIA020273 4 20020330 A 3417 2587400436 ADC DOUG DC9 DC932 3022066 WP E/E BAY FAULTY A GTIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 23 12536 47113 FLT 616 - ACY - AUTO PILOT PITCH CONTROL PORPOISES DURING CLIMB AND DESCENTS AND WILL NOT HOLD ALTITUDE ALL OTHER FUNCTI ONS OK FLT 616. REMOVED AND REPLACED AIR DATA COMPUTER PERFORMED PITOT STATIC LEAK CHECK. GROUND CHECK OK AT THIS TIME . (M) 2 L 7 2 4F A6WE 2002050800077 20020508 00077 WP 2002 5 8 GTIA020275 1 20020401 A 2740 92747813 RELAY DOUG DC9 DC983 3022083 WP STAB TRIM FAILED A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 824NK 53015 FLT 9824 - FOUND CAPTAINS YOKE TRIM SWITCH INTERMITTENT. F/O'S YOKE AND SUIT CASE HANDLES OK. REMOVED AND REPLACED PRI MARY LONGITUDINAL TRIM BRAKE CONTROL RELAYS (UP TRIM R20-18 AND DOWN TRIM R20-17. (M) 2 L 7 2 4F RT A6WE 2002050800078 20020508 00078 WP 2002 5 8 GTIA020276 1 20020402 A 2740 920710296 RELAY DOUG DC9 DC983 3022083 WP STAB TRIM FAILED A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 824NK 53015 DTW - PRIMARY TRIM NOSE DOWN INOPERATIVE FROM YOKE TRIM SWITCHES. REPLACED DOWN TRIM RELAY OP'S CHECKED GOOD IAW MD80 M M 27-40-01. (M) 2 L 7 2 4F RT A6WE 2002050800079 20020508 00079 WP 2002 5 8 GTIA020277 1 20020430 A 5280 DOOR DOUG DC9 DC983 3022083 WP LT MLG OUT OF ADJUST A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 16892 49391 FLT 909 - LGA - LEFT MAIN GEAR INDICATES UNLOCK WITH DOOR LIGHT OUT. COMPLIED WITH QRH PROCEDURES. ADJUSTED LEFT MLG F LYAWAY DOOR. (M) 2 L 7 2 4F RT A6WE 2002050800080 20020508 00080 WP 2002 5 8 GTIA020278 1 20020407 A 3260 UPLOCK SWITCH DOUG DC9 DC983 3022083 WP RT MLG DIRTY A GTIA O OTHER O OTHER AP APPROACH 1 GL 23 602CA 49415 FLL - FLT 779 - SPOILERS WOULD NOT COME UP INTO ARMED POSITION ONCE GEAR DOWN, POSSIBLE PROBLEM WITH GROUND SHIFT MECHAN ISM. CLEANED GREASE AND DIRT FROM RT MLG UPLOCK SWITCH. ARMED SPOILER HANDLE. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2002050800081 20020508 00081 WP 2002 5 8 GTIA020279 1 20020405 A 2740 95906 MOTOR DOUG DC9 DC982 3022082 WP STAB TRIM FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 817NK 49141 DTW - FLT 503 - PRIMARY TRIM MOTOR WILL NOT TRIM. REMOVED AND REPLACED PRIMARY TRIM MOTOR. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 2002050800082 20020508 00082 2002 5 8 GTIA020281 4 20020409 A 2230 2588533901 AMPLIFIER DOUG DC9 DC982 3022082 WP COCKPIT FAILED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 803NK 48087 DTW - FLT 56 - AUTO THROTTLE WILL NOT ENGAGE. FOUND NR 1 INSTRUMENT AMP BAD. REMOVED AND REPLACED NR 1 INSTRUMENT AMP. (M) 2 L 7 2 4F A6WE 2002050800083 20020508 00083 WP 2002 5 8 GTIA020282 1 20020407 A 1420 TERMINAL DOUG DC9 DC981 3022081 WP TAIL CONE BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 811NK 48017 FLL - TAIL CONE UPPER CENTER EMERGENCY LIGHT INOPERATIVE. REPLACED BROKEN WIRE TERMINALS REF MM 20-50-01. OPS CHECK OK . (M) 2 L 7 2 4F A6WE 2002050800084 20020508 00084 WP 2002 5 8 GTIA020283 1 20020326 A 5730 SKIN DOUG DC9 DC982 3022082 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 DTW - FOUND CRACK IN RIGHT WING LEADING EDGE APPROX 2 INCHES IN LENGTH BETWEEN SLAT 0 AND 1. REPAIRED CRACK IN RIGHT WI NG LEADING EDGE BETWEEN SLAT 0 AND 1. (M) 2 L 7 2 4F A6WE 2002050800085 20020508 00085 WP 2002 5 8 GTIA020284 1 20020408 A 5270 834003 PROXIMITY SWITCH DOUG DC9 DC982 3022082 WP CARGO DOOR FAULTY A GTIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 23 800NK 49144 FLT 503 - MCO - ON TAKEOFF ROLL APPROXIMATELY 80 KTS FORWARD DOOR CARGO LIGHT CAME ON PERFORMED LOW SPEED ABORT LIGHT WE NT OFF CLEARING RUNWAY. REMOVED AND REPLACED PROXIMITY SWITCH. ADJUSTED DOOR TARGET. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002051700072 20020517 00072 NM 2002 5 17 DHL2002726520 1 20020501 A 5754 SKIN BOEING 727 727228 1384083 NM L/E SLAT DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, NR 5 LEADING EDGE SLAT HAS A DENT AT SLAT AT STA 355. CUT OUT DENTED SECTION OF SLAT SKIN IAW B-727 SRM 57-50-1 FIG 1, FABRICATED REPAIR PARTS IAW B-727 SRM 57-50-3 FIG 1, AND INSTALLED DOUBLER AND FILLER REPAIR ON NR 5 LEA DING EDGE SLAT IAW B-727 SRM 57-50-3 FIG 1. 2 L 7 3 4F RT A3WE 2002050800086 20020508 00086 NM 2002 5 8 USAA020020 1 20020104 A 5510 6549873501 HINGE FITTING BOEING 737 7374B7 1384702 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 447US 31500 24874 PIT - FOUND SCATTERED CORROSION ON HINGE SUPPORT FITTING 2 SQUARE INCHES, NR 6 HORIZONTAL STABILIZER TO ELEVATOR FITTING , LEFT HINGE SUPPORT FITTING. CORROSION LEVEL 1. REMOVED AND REPLACED WITH IDENTICAL PART PER BOEING DWG 65-33570. (M ) 2 L 7 2 4F RT A16WE 2002050800087 20020508 00087 NM 2002 5 8 USAA020029 1 20020127 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND FRAME DENTED .5 INCH BY .5 INCH, STATION 660 S23L. INSTALLED DOUBLER PER EA 85865A/SRM 53-00-07 FIG 201. ( M) 2 L 7 2 4F RT A2NM 2002050800088 20020508 00088 NM 2002 5 8 USAA020030 1 20020103 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND SKIN DENTED 1 INCH, STATION 500-520 BETWEEN S25R PLUS S26R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 208. (M ) 2 L 7 2 4F RT A2NM 2002050800089 20020508 00089 NM 2002 5 8 USAA020031 1 20020103 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55453 22202 CLT - FOUND C4 SKIN DENTED 6 INCHES BY 9 INCHES, FS 590-600 BETWEEN S29L AND S29R. INSTALLED DOUBLER PER EA 67990A. (M ) 2 L 7 2 4F RT A2NM 2002050800090 20020508 00090 NM 2002 5 8 USAA020032 1 20020107 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND FRAME DENTED 2 INCHES BY 3 INCHES, STATION 560 BETWEEN S25L-S24L. FABRICATED AND INSTALLED NEW FRAME PER EA 85865A. (M) 2 L 7 2 4F RT A2NM 2002050800091 20020508 00091 NM 2002 5 8 USAA020033 1 20020107 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND FRAME DENTED, STATION 600 BETWEEN S25L-24L. CUT OUT DAMAGE, FABRICATED, DOUBLER AND FILLER, AND THEN INSTAL LED PER EA 85865A. (M) 2 L 7 2 4F RT A2NM 2002050800092 20020508 00092 NM 2002 5 8 USAA020034 1 20020107 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND FRAME DENTED 2 INCHES BY 2 INCHES, STATION 580 BETWEEN S25L-S23L. CUT OUT DAMAGE, FABRICATED DOUBLER AND FI LLER AND INSTALLED PER EA 85865A. (M) 2 L 7 2 4F RT A2NM 2002050800093 20020508 00093 NM 2002 5 8 USAA020035 1 20020107 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND FRAME AND DOUBLER DENTED .5 INCH BY .75 INCH, STATION 620 AT S25L. INSTALLED REPAIR FRAME DOUBLER AND FILLE R PER EA 85865A. (M) 2 L 7 2 4F RT A2NM 2002050800094 20020508 00094 NM 2002 5 8 USAA020036 1 20020113 A 5310 CREASE BEAM BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND WEB CRACKED 4 INCHES, CREASE BEAM WEB BS 1044 AND S176. REPLACED WEB PER SRM 51-10-20. (M) 2 L 7 2 4F RT A2NM 2002050800095 20020508 00095 NM 2002 5 8 USAA020037 1 20020109 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND FLOORBEAM CORRODED 1.5 INCHES, STATION 1661 LBL 4. INSTALLED T-CAP REPAIR AND FILLER ON FLOORBEAM PER SRM 5 3-00-51. (M) 2 L 7 2 4F RT A2NM 2002050800096 20020508 00096 NM 2002 5 8 USAA020040 1 20020112 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 54705 22204 CLT - FOUND FRAME WEB CRACKED 2.5 INCH BY 1.5 INCHES, BS 1440, WL 150, RBL 33. INSTALLED DOUBLER PER EA 85844. (M) 2 L 7 2 4F RT A2NM 2002050800097 20020508 00097 NM 2002 5 8 USAA020041 1 20020112 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND INTERCOSTAL CRACKED 1 INCH, BL 0 BETWEEN STATION 780 AND 800 AT FLOOR LEVEL. REPLACED CRACKED UPPER FLANGE OF INTERCOSTAL PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2002050800098 20020508 00098 NM 2002 5 8 USAA020042 1 20020114 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 22202 CLT - FOUND FRAME WITH IMPROPER PREVIOUS REPAIR, STATION 1116 FRAME FORWARD SIDE AT S10L. TRIM AND FILLED AREA PER EA 8 5855. (M) 2 L 7 2 4F RT A2NM 2002050800099 20020508 00099 NM 2002 5 8 USAA020044 1 20020110 A 5310 DOOR FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 55707 22205 CLT - FOUND WEB AND CHORD CRACKED 3 INCHES, STATION 1380, FORWARD FRAME OF AFT CARGO DOOR CUTOUT. SPLICED IN WEB SECTIO N AND REPLACED CHORD PER EA85820 AND EA 85824. (M) 2 L 7 2 4F RT A2NM 2002050800100 20020508 00100 NM 2002 5 8 USAA020047 1 20020124 A 5412 BULKHEAD BOEING 757 757225 1384959 NM PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND PYLON MID BULKHEAD WITH .125 INCH CRACK, OUTBOARD SIDE MID BULKHEAD, BOTTOM HOLE. FABRICATED DOUBLER AND SH IMS, VERIFY NO OTHER CRACKS, INSTALLED PE EA 63980A. (M) 2 L 7 2 4F RT A2NM 2002050800101 20020508 00101 WP 2002 5 8 CALA2000261 1 20020507 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 AFT PIT F/S 1146 TO 1155 BETWEEN LONGERON 30 & 29R INTERCOSTAL CORROSION 10 INCHES LONG. REMOVED INTERCOSTAL IAW SRM 51- 30-2 AND 51-30-5. REPLACED INTERCOSTAL IAW SRM 51-30-2 & 51-30-5. 2 L 7 2 4F A6WE 2002050800102 20020508 00102 WP 2002 5 8 CALA2000262 1 20020507 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 CAPTAINS UPPER AND LOWER SEAT TRACKS WORN, REPAIRED AND REINSTALLED TRACKS IAW SRM 51-30-1 & 53-40-01. 2 L 7 2 4F A6WE 2002050800103 20020508 00103 WP 2002 5 8 CALA2000263 1 20020507 A 5330 SKIN DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 RIGHT FORWARD FUSELAGE SKIN HAS 2" CREASE BETWEEN LONGERON 25 & LONGERON 26 AT APPROXIMATELY F/S 141. CUT OUT DAMAGE IAW SRM53-04 FIG 38, SHEET 34. INSTALLED REPAIR PARTS IAW SRM 53-04 FIG 38, SHEET 34. 2 L 7 2 4F A6WE 2002050800104 20020508 00104 WP 2002 5 8 CALA2000264 1 20020507 A 5330 SKIN DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 ONE INCH DENT AT F/S 237, 17L-18L. REF. NON ROUTINE 4684047, REPAIRED DENT AT STA 229 PER ECRA 5330-03055. 2 L 7 2 4F A6WE 2002050800105 20020508 00105 WP 2002 5 8 CALA2000265 1 20020507 A 5320 602204418 SEAT TRACK DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 CABIN FLOOR SEAT TRACK RBL 24 F/S 984 AND 1003 HAS SURFACE CORROSION. REMOVED SEAT RACK FROM STA 789-1032 RBL24 IAW SRM 51-30-5 AND INSTALLED NEW TRACK IAW SRM 53-05. 2 L 7 2 4F A6WE 2002050800106 20020508 00106 NM 2002 5 8 CALA2000266 1 20020507 A 5755 654646165A SPOILER BOEING 737 7373T0 1384582 NM A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 #3 SPOILER DENTED AND CRACKED .75X.75 INCHES JUST FWD AND OB OF ACTUATOR ATTACH POINT. INSTALLED DOUBLER PER SRM 57-70-0 1, FIG 204. 2 L 7 2 4F RT A16WE 2002052000110 20020520 00110 NM 2002 5 20 DHL2002726522 1 20020415 A 5320 651758866 SUPPORT BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, COCKPIT FLOOR STA 265 LBL 3, PANEL IN FLOOR BULGED WITH PULLING RIVETS AT I/B END OF F/E SEAT TRACK. RE MOVED AND REPLACED F/E SEAT TRACK SUPPORT IAW B-727 SRM 51-30-5/ 51-30-8/ 51-30-2. BULGING FOUND TO BE CORROSION OF F/E SEAT TRACK SUPPORT. CORRODED SECTION WAS OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. 2 L 7 3 4F RT A3WE 2002050900001 20020509 00001 EU 2002 5 9 MALA020273 1 20020501 A 5320 NR FLANGE SAAB SF340 340B 7860101 EU A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 DURING 4K-CHECK IN CWA, UPPER FLANGE OF BOTTOM FRAME AT STA 258 HAS CORROSION. MAINTENANCE COMPLETED PREAIR IAW EO #5310 8. RELEASE DATE 5/7/2002. 2 L 7 2 4T RT A52EU 2002050900002 20020509 00002 EU 2002 5 9 MALA020274 1 20020501 A 5320 NR SEAT TRACK SAAB SF340 340B 7860101 EU A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 DURING 4K-CHECK IN CWA, SEAT TRACK LBL 18.3 HAS CORROSION FROM STA 638-686.MAINTENANCE REPLACED SEAT TRACK IAW EO #53060 . A/C RELEASE DATE 5/7/2002. 2 L 7 2 4T RT A52EU 2002050900004 20020509 00004 SO 2002 5 9 SIMA200201801 1 20020118 A 3350 20131A POWER SUPPLY EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 704PG 145174 RDU - FLT 4612 - SEVERAL EMERGENCY INTERIOR LIGHTS ARE INOPERATIVE. REPLACED NR 2 BATTERY SUPPLY, OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2002050900005 20020509 00005 SO 2002 5 9 SIMA200206501 1 20020209 A 5320 14525480003 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AE 145069 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CARGO DOOR CUTOUT CENTER SILL BEAM CORRODED. REMOVED CORRODED SILL B EAM. INSTALLED NEW SILL BEAM IAW EMB 145 SRM 145/1142, REV 16, 51-40-02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002050900006 20020509 00006 SO 2002 5 9 SIMA200206502 1 20020214 A 5315 145217130005 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AE 145069 ABI - DURING AN IMBV INSPECTION OF THE AIRCRAFT, THE CENTER FLOORBEAM IN THE GALLEY AREA WAS FOUND TO BE CORRODED BEYOND SRM LIMIT AT FRAMES 20, 22 AND 23. REMOVED ENTIRE CENTER GALLEY FLOORBEAM. INSTALLED NEW FLOORBEAM IAW EMB 145 SRM, 1 45/1142 (REV 17) 51-20-01, 51-40-02, 51-40-04 AND EMB GST 0459/02. (M) 2 L 7 2 4F RT T00011AT 2002050900007 20020509 00007 SO 2002 5 9 SIMA200206503 1 20020212 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AE 145069 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIGHT GALLEY FLOORBEAM AT FRAME 22. BLENDED CHAFED AREA . PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER IAW EMB GST 0467 /02, ITEM 2 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002050900008 20020509 00008 SO 2002 5 9 SIMA200206507 1 20020122 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 715AE 145262 ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. FABRICATED A DOUBLER, F ILLER, PLATE, AND TWO SHIMS. WORK DONE IAW EMB 145 SRM 145/1172 REV 16, 53-21-10 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002050900009 20020509 00009 WP 2002 5 9 UPS02837854 1 20020222 A 5330 561561465 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C LOWER FUSE SKIN PILLOWED AT STA 80 L21R. FOUND L22R AND FINGER DOUBLER CORRODED BEYOND LIMITS. REMOV ED DOUBLER SECTION FROM STA 70-80. FABRICATED REPLACEMENT AND INSTALLED PER SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2002050900010 20020509 00010 WP 2002 5 9 UPS02837855 1 20020225 A 5313 94585063 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C L34R CORRODED BEYOND LIMITS AT STA 1220. REPAIRED PER DHSK 707-819 AND SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2002050900011 20020509 00011 WP 2002 5 9 UPS02837858 1 20020221 A 5330 57503223N1 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C CORROSION FOUND ON INTERIOR OF BELLY SKIN, 1050-1350, L31L TO L31R. REMOVED AND REPLACED AFT BELLY SK IN AND C-PIT DOOR INTERNAL DOUBLER PER SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2002050900012 20020509 00012 WP 2002 5 9 UPS02837859 1 20020303 A 5720 37048411 SPLICE DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C STRINGER 51 SPLICE CRACKED APPROX 12 INCHES OUTBOARD OF XRS 74, NR 3 ALT TANK, RT WING, FIRST STRINGER FWD OF REAR SPAR CAP. REMOVED AND REPLACED STRINGER 51 SPLICE PER SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2002050900013 20020509 00013 WP 2002 5 9 UPS02837860 1 20020303 A 5720 37048411 SPLICE DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C STRINGER 51 SPLICE FITTING CRACKED APPROX 10 INCHES OUTBOARD OF XRS74, LT WING. REMOVED AND REPLACED SPLICE FITTING PER SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2002050900014 20020509 00014 WP 2002 5 9 UPS02837873 1 20020306 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 REPAIR AT STA 280 FWD LOWER CORNER OF A PIT DOOR CUTOUT IS A CATEGORY D PER EO DC8-5330-12800 AND SKI N IS CRACKED BETWEEN LONG 31R AND 32R. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-2-0 FIG 22. 2 L 7 4 4F RT 4A25 2002050900015 20020509 00015 WP 2002 5 9 UPS02837874 1 20020301 A 5313 37585931 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 BELLY SKIN BULGING APPROX 2 FT FWD TO THE RIGHT OF THE VHF ANTENNA, NO CORROSION FOUND. REMOVED FAST ENER TO INSPECT AND REPLACED WITH BLIND. FOUND LONG 36 CORRODED BEYOND LIMITS STA 1260-1350. REMOVED AND REPLACED LONG ERON SECTION IAW DWG 3758593, AND SRM 53-1-0, 51-1-20D. 2 L 7 4 4F RT 4A25 2002050900016 20020509 00016 WP 2002 5 9 UPS02837875 1 20020304 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 SKIN CRACKED STA 160 LONG 10R-11R. REMOVED EXISTING, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS. A T CUTOUT, FABRICATED AND INSTALLED REPAIR FILLER, AND DOUBLERS IAW SRM 53-2-0 FIG 14. 2 L 7 4 4F RT 4A25 2002050900017 20020509 00017 WP 2002 5 9 UPS02837878 1 20020306 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 L1 DOOR UPPER FWD PAN IS CRACKED IN CORNER, STA 25 LONG 10L. CUT OUT CRACK, NDT VERIFIED NO CRACK. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1D. 2 L 7 4 4F RT 4A25 2002050900018 20020509 00018 WP 2002 5 9 UPS02837884 1 20020301 A 5753 WEB DOUG DC8 DC871F 302199D WP FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C23 RG I/B FLAP CLOSEOUT WEB CRACKED AROUND BEADED AREA. REMOVED AND REPLACED IAW REO G08529. 2 L 7 4 4F RT 4A25 2002050900019 20020509 00019 WP 2002 5 9 UPS02837885 1 20020220 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C23 AFT PIT LT TUNNEL CORR ON BOTTOM OF CABIN FLOORBEAM UPPER FWD FLANGE AT STA 1240 LBL 62. REMOVED CO RROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED AND INSTALLED IAW DC8 SRM. 2 L 7 4 4F RT 4A25 2002050900020 20020509 00020 NM 2002 5 9 USAA020049 1 20020103 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND FRAME CRACKED 3 INCHES, STATION 1380 AT LOWER STOP FITTING AFT CARGO DOOR FRAME. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A2NM 2002050900021 20020509 00021 NM 2002 5 9 USAA020050 1 20020108 A 5320 140N2001PE57 TIE CLIP BOEING 757 757225 1384959 NM FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND TIE CLIP GOUGED. REMOVED AND REPLACED TIE CLIP. (M) 2 L 7 2 4F RT A2NM 2002050900022 20020509 00022 NM 2002 5 9 USAA020051 1 20020114 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND SKIN DENTED 1 INCH BY .250 INCH, STATION 570 STRINGER 17L. TRIM DAMAGE OUT, FABRICATED DOUBLER AND INSTALLE D PER EA 85846. (M) 2 L 7 2 4F RT A2NM 2002050900023 20020509 00023 NM 2002 5 9 USAA020052 1 20020105 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND SKIN DENTED 17 INCHES BY 13 INCHES, BS 1681 AT STRINGER S20L. INSTALLED REPAIR DOUBLER, TRIPLER, AND FILLER PER EA 68028D. (M) 2 L 7 2 4F RT A2NM 2002050900024 20020509 00024 NM 2002 5 9 USAA020053 1 20020114 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 55463 22202 CLT - FOUND SKIN CREASED 20 INCHES BY 1.5 INCHES BY .052 INCH, STATION 1695.68, S14R TO S17R. REMOVED DAMAGE, INSTALLED DOUBLER, TRIPLER AND FILLER PER EA 85889. (M) 2 L 7 2 4F RT A2NM 2002050900025 20020509 00025 NM 2002 5 9 USAA020073 1 20020225 A 7110 LJ38066 ACOUSTIC PANEL BOEING 757 757225 1384959 NM COWLING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 53442 22192 PIT - FOUND NOSE COWLING CRACKED/DISBONDED 4 FT BY 2 FT, LOWER ACOUSTICAL PANEL NOSE COWL 4 TO 8 O'CLOCK. DEFECTIVE PAR T REPLACED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A2NM 2002050900026 20020509 00026 NM 2002 5 9 USAA020122 1 20020222 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 42381 23860 PIT - FOUND SKIN WITH TWO 3 INCH CRACKS, STATION 680 AND 700, CENTER KEEL AREA. FABRICATED PART INSTALLED PER EA 73445. (M) 2 L 7 2 4F RT A16WE 2002050900027 20020509 00027 NM 2002 5 9 USAA020123 1 20020215 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 42381 23860 PIT - FOUND SKIN AND INNER DOUBLER CRACKED .5 INCH, AFT ENTRY DOOR UPPER HINGE CUT OUT. DOUBLER INSTALLED PER SRM 53-60 -01, FIG 205. (M) 2 L 7 2 4F RT A16WE 2002050900028 20020509 00028 NM 2002 5 9 USAA020124 1 20020304 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 42381 23860 PIT - FOUND SKIN CRACKED .25 INCH, BOTTOM LAYER .5 INCH AND BENT, BELOW LOWER HINGE OF AFT ENTRY DOOR. REPAIRED PER 53- 00-01 WITHIN ALLOWABLE LIMITS. (M) 2 L 7 2 4F RT A16WE 2002050900029 20020509 00029 NM 2002 5 9 USAA020125 1 20020304 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 42381 23860 PIT - FOUND STRINGER CRACKED .5 INCH, STATION 787, S25L STRINGER TO FRAME CUP. INSTALLED NEW STRINGER TIE PER SRM 53-60 -53 AND 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002050900030 20020509 00030 EU 2002 5 9 USAABA02006 1 20020305 A 3350 32146220 POWER SUPPLY AIRBUS 330 A330323 3930335 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 670UW 0315 PHL - EPSU'S 15WL AND 16WL FAILED TESTING. MAINTENANCE REPLACED THE EPSU'S. (M) 2 L 7 2 4F RT A46NM 2002050900033 20020509 00033 NM 2002 5 9 USAABB02013 1 20020131 A 3230 LINK BOEING 757 7572B7 1384964 NM NOSE GEAR W/W BROKEN A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 631AU 27809 CLT - FLT 171 - AFTER TAKEOFF FROM CLT, CREW RECEIVED THE E/M 'GEAR DOORS' AND THE 'DOORS' LIGHT ILLUMINATED WHEN THE GE AR WAS RETRACTED. CREW EXTENDED THE GEAR AND LIGHT REMAINED ON. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCI DENT. MAINTENANCE REPLACED THE NOSE GEAR SEQUENCING VALVE LINK. (M) 2 L 7 2 4F RT A2NM 2002050900034 20020509 00034 WP 2002 5 9 ZW0A0202503 1 20020228 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 941AS 49925 DURING CHECK-C MAINT FOUND CORROSION IN LONGITUDINAL FLOOR SUPPORT FROM STA 160 TO 196, LBL 45. REPLACED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-02. 2 L 7 2 4F A6WE 2002050900035 20020509 00035 WP 2002 5 9 ZW0A0202601 1 20020305 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 110HM 49787 DURING CHECK-C MAINT LONGERON 2R HAD A CRACK JUST AFT OF STA 1429. SPLICED IN NEW LONGERON PER SRM 53-02, FIG 18. 2 L 7 2 4F RT A6WE 2002050900036 20020509 00036 WP 2002 5 9 ZW0A0202602 1 20020304 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 110HM 49787 DURING CHECK-C MAINT LONGERON 2L WAS CRACKED JUST AFT OF STA 1429. SPLICED IN NEW LONGERON PER SRM 53-02, FIG 18. 2 L 7 2 4F RT A6WE 2002050900037 20020509 00037 WP 2002 5 9 ZW0A0202603 1 20020301 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 941AS 49925 DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT STA 195, LBL 14. REMOVED CORROSION ON MEMBRANE PER SRM 53-01, PAGE 6, AND SPM 6-80-01, PAGES 1, 2, AND 3. REMOVED FLOOR SUPPORT AND FABRICATED NEW PER SPM 6-70-01, PAGES 1, 2, AND 3. I NSTALLED FLOOR SUPPORT PER SRM 51-30-05, PAGE 1. 2 L 7 2 4F A6WE 2002050900038 20020509 00038 WP 2002 5 9 ZW0A0202604 1 20020301 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 967TW 53617 DURING CHECK-C MAINTENANCE FOUND CORROSION FROM LONGERON 29L TO 29R, STA 160 TO 218. REPLACED SKIN FROM STA 110 TO 229 , STRINGER 26L TO 26R, PER SPM. 2 L 7 2 4F RT A6WE 2002050900039 20020509 00039 WP 2002 5 9 ZW0A0202605 1 20020228 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 967TW 53617 DURING CHECK-C MAINT THE FWD CARGO COMPT BELLY SKIN HAD CORROSION AT STA 218 TO 229, LONGERON 29L TO 29R. INSTALLED NEW SKIN PER DRAWING 5911401. 2 L 7 2 4F RT A6WE 2002050900040 20020509 00040 WP 2002 5 9 ZW0A0202701 1 20020305 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 941AS 49925 DURING CHECK-C MAINTENANCE FOUND CORROSION IN LATERAL FLOOR SUPPORT, STATION 181, FROM RBL 9 TO RBL 42. INSTALLED LATE RAL SUPPORT AFTER FABRICATION AT STA 181, FROM RBL 9 TO RBL 42, PER SPM 6-70-01. 2 L 7 2 4F A6WE 2002050900041 20020509 00041 NM 2002 5 9 ZW0A0202801 1 20020309 A 3350 BATTERY DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9630A 53561 DURING PREFLIGHT THE FIRST CLASS EGRESS LIGHTS FLASHED DURING TEST. THEY DID NOT REMAIN ON. REPLACED THE BATTERIES IN T HE POWER SUPPLY. 2 L 7 2 4F RT 2002050900043 20020509 00043 WP 2002 5 9 CALA2000268 1 20020509 A 5347 602500376 SEAT TRACK DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 SEAT TRACK AT F/S 390 RH O/B IS HEAVILY CORRODED APPROXIMATELY 4"X19'. REMOVED AND REINSTALLED AIR GRILL F/S 200-484 RH O/B IAW SRM 51-30-1. REMOVED AND REINSTALLED FLOOR PANELS F/S 256-465 RH O/B IAW SRM 51-30-1. INSTALLED NEW SEAT TRACK, SPLICE, & FITTING IAW SRM 53-05 FIG 4, SRM 51-30-01 & 51-30-05. 2 L 7 2 4F A6WE 2002050900044 20020509 00044 WP 2002 5 9 CALA2000269 1 20020509 A 5313 SHEAR TIE DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 AFT PIT F/S 1193 LONGERON 30 SHEAR TIE IS CORRODED 0.5 INCHES. REMOVED AND REINSTALLED NEW SHEAR TIE IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2002050900045 20020509 00045 WP 2002 5 9 CALA2000270 1 20020509 A 5320 WEB DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 CUSP WEB L/S AFT OF L-2 DOOR IS CORRODED 20"X38". REMOVED WEB IAW SRM 53-01. INSTALLED WEB IAW SRM 51-30-2 & 51-30-5, 53 -01 FIG 1. 2 L 7 2 4F A6WE 2002050900046 20020509 00046 SO 2002 5 9 000155 1 20020426 A 3350 BATTERY EMB 145 EMB145 3260210 SO CABIN DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 277 277 NR 1 AND 2 EMERGENCY LIGHT BATTERIES DEAD. INSTALLED NR 1 AND 2 EMERGENCY LIGHT BATTERIES. 2 L 7 2 4F RT T00011AT 2002050900047 20020509 00047 SO 2002 5 9 000156 1 20020426 A 3350 BATTERY EMB 145 EMB145 3260210 SO CABIN DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 277 277 NR 3 AND 4 EMERGENCY LIGHT BATTERIES DEAD. INSTALLED NR 3 AND 4 EMERGENCY LIGHT BATTERIES 2 L 7 2 4F RT T00011AT 2002050900048 20020509 00048 2002 5 9 000999 4 20020506 A 3160 COMPUTER SAAB SF340 SF340A 7850100 EU COCKPIT MALFUNCTIONED A CHQA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 35 035 BOTH CAPTAINS DISPLAYS WENT BLANK. MX REMOVED AND REPLACED DPU. 2 L 7 2 4T RT A52EU 2002050900049 20020509 00049 EU 2002 5 9 02127320 1 20020507 A 3350 BATTERY JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 320UE 41043 EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE DURING INSPECTION. MAINTENANCE PERSONNEL REMOVED AND REPLACED FWD EMERGENCY BATTERY AND AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 L 7 2 4T RT A41NM 2002050900052 20020509 00052 NM 2002 5 9 02FDEA00309 1 20020506 A 3230 RELAY DOUG MD11 MD11F 3023600 NM COCKPIT FAILED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 616FE 48747 ON APPROACH PRIMARY & SECONDARY GEAR IND UNSAFE (RED). REMOVED AND REPLACED GEAR HANDLE INTERLOCK RELAY-3 FOR PRIMARY G EAR POS IND SYS PER MM 32-31-00. RESET ALTERNATE GEAR EXTENSION LEVER PER MM 32-32-00. 2 L 7 3 4F RT A22WE 2002050900053 20020509 00053 NM 2002 5 9 02FDEA00310 1 20020506 A 2750 TORQUE TUBE BOEING 727 727200 138407E NM T/E FLAP DISCONNECTED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 489FE 21492 ON DEPARTURE OUTBOARD FLAPS WENT ASYMMETRIC WITH ONE NEEDLE IND. RECONNECTED TORQUE TUBE PER MM 27-51-00-5. OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2002050900054 20020509 00054 NM 2002 5 9 02FDEA00311 1 20020506 A 3260 WARNING SYSTEM BOEING 727 727200 138407E NM COCKPIT FALSE ACTIVATION A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 491FE 21529 AFTER GEAR RETRACT, GEAR HANDLE IN UP POSITION, R/GEAR RED WARN LIGHT REMAIN ON. PERFORMED TEST OF R/GEAR UPLOCK IND PE R MM 32-61-081-4. OPS CHECK NORMAL. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2002062000013 20020620 00013 NE 2002 6 20 02FDEA00312 2 20020504 A 7532 BLEED VALVE AIRBUS 310 A310 EU PWA JT9 JT9D7 52054 NE NR 2 ENGINE MALFUNCTIONED A FDEA B A EMER. DESCENT UNSCHED LANDING R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CR CRUISE 1 SO 25 456FE 318 716109 CRUISE IN WX AT 350 MACH 80 A/I ON, EXPERIENCED ENGINE COMPRESSOR STALL ON NR 2 ENGINE. REMOVED EVBC. 2 L 7 2 4F 4 F RT A35EU E20EA 2002051400046 20020514 00046 NE 2002 5 14 02FDEA00314 2 20020507 A 7250 TURBINE BOEING 727 727100 1384036 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE DAMAGED A FDEA A UNSCHED LANDING K R E FLUID LOSS PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CL CLIMB 1 SO 25 120FE 19356 NR 2 ENGINE COMPRESSOR STALLED EXCESSIVE VIBRATION. INTAKE HAD NO APPARENT DAMAGE, EXHAUST SHOWED THE TURBINE BLADES HA D DAMAGE AND POOLS OF OIL. REMOVED AND REPLACED NR 2 ENGINE. OK FOR SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2002051400047 20020514 00047 NM 2002 5 14 02FDEA00315 1 20020507 A 2797 WIRE BOEING 727 72721C 138400M NM ELEVATOR DAMAGED A FDEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 25 144FE 19137 DURING TAXI ELEVATOR FEEL DIFFERENTIAL LIGHT CAME ON. LOW PRESS LIGHT C/B ON. HYD A & B FILTERS CHECK GOOD. PITOT TUB ES ON TAIL WERE CLEAN. SPLICED IN NEW SECTION OF WIRE PER SMP, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2002051400048 20020514 00048 NM 2002 5 14 02FDEA00316 1 20020507 A 2613 SENSING ELEMENT BOEING 727 727200 138407E NM NR 1 ENGINE FAULTY A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 243FE 21480 IN CRUISE NR 1 ENGINE OVERHEAT FLICKERED ON/OFF. REDUCED PWR AND COMPLETED ENG STRUT OVERHEAT CHECKLIST. LIGHT REMAINE D OUT. THEN FLICKERED AND CAME ON. SHUTDOWN NR 1 ON TAXI IN. REMOVED AND REPLACED OVERHEAT SENSING ELEMENT, BOOT & CL AMP ON DUCT. 2 L 7 3 4F RT A3WE 2002052300140 20020523 00140 NM 2002 5 23 02FDEA00317 1 20020507 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 N 329 FRAME DENTED AT BS 950F BETWEEN STR 26 & 25 LT. R&R FRAME IAW SRM 51-40-03 FIG 1. 2 L 7 3 4F RT A3WE 2002052900005 20020529 00005 NM 2002 5 29 02FDEA00318 1 20020507 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 FRAME DENTED AT BS 970 BETWEEN STR 25 & 26 LT. REMOVED AND REPLACED FRAME PER SRM 51-40-3 & EA 7-5310-64087. 2 L 7 3 4F RT A3WE 2002052300141 20020523 00141 NM 2002 5 23 02FDEA00319 1 20020507 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 N 653 FRAME DENTED AT BS 990 AT STR 26 LT. R&R FRAME PER SRM 51-40-3 & 51-10-2. 2 L 7 3 4F RT A3WE 2002050900055 20020509 00055 WP 2002 5 9 200200246 1 20020507 A 5310 99216961 DOOR FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 941F 47193 REPAIRED CRACK IN UPPER FWD CORNER OF MAIN CARGO DOOR BY REMOVING TEMPORARY REPAIR, TRIMMING OUT THE CRACK, FABRICATING FILLER AND REINSTALLING EXISTING REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002050900056 20020509 00056 WP 2002 5 9 200200247 1 20020507 A 5230 59101575 PAN DOUG DC9 DC933F 302207A WP CARGO DOOR CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 941F 47193 REPAIRED CRACKED INNER AND OUTER PANS OF AFT CARGO DOOR AT STOP NR 3 BY STOP-DRILLING CRACKS, PERFORMED HFEC TO VERIFY D AMAGE CONTAINMENT AND INSTALLED DOUBLERS PER DC-9 SRM 52-05 FIG 50 TO INNER PAN AND DC-9 SRM 52-03 FIG 8 SHEET 1 TO OUTE R PAN. 2 L 7 2 4F A6WE 2002050900057 20020509 00057 NM 2002 5 9 2002F00440 1 20020501 A 5210 MECHANISM BOEING 757 75723N 1384973 NM L1 DOOR OUT OF ADJUST G AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 520AT 27976 FLIGHT 073, AFTER PUSHBACK DOOR 1L ARM LIGHT EXTINGUISHED, CLOSER INSPECTION REVEALED DOOR SLIDE WAS NOT ARMED. AIRCRAF T RETURNED TO THE GATE AND MAINTENANCE PERFORMED ADJUSTMENT AND TEST FOR THE 1L DOOR EMERGENCY MECHANISM PER M/M 25-66-1 1-2. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2002050900058 20020509 00058 2002 5 9 2002F00441 4 20020502 A 2564 7435PS8 ASPIRATOR BOEING 737 73783N 13844HI NM LIFE RAFT OPEN G K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 DURING PARTIAL DITCH DEMONSTRATION A 46 MAN LIFE RAFT WAS ACCIDENTLY DEPLOYED. BOTH RINGS ON THE RAFT INFLATED AND THEN THE BOTTOM RING DEFLATED. UPON INSPECTION THE ASPIRATOR FOR THE BOTTOM RING WAS FOUND TO BE PARTIALLY OPEN. THE RAFT HAD BEEN OVERHAULED ON 03/02. 2 L 7 2 4F RT A16WE 2002050900071 20020509 00071 WP 2002 5 9 MWEA020319 1 20020506 A 2711 CV524 VALVE DOUG DC9 DC932 3022066 WP WHEEL WELL CLOGGED A MWEA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 31 206ME 47791 AILERON SERVO INDICATOR SHOWED FULL DEFLECTION. DISCONNECTED AUTO PILOT AND THE AIRCRAFT STARTED TO TURN TO THE LEFT. FO UND WATER DRAINING IN LEFT GEAR AREA AND ICE ON CABLES AT THE LEFT TRAPEZOID PANEL. FOUND DEBRIS IN DRAIN HOSE THAT CAUS ED THE CHECK VALVE TO STICK IN THE CLOSED POSITION SO WATER COULD NOT DRAIN FROM ABOVE TRAILING EDGE SLANT PANEL. -- R EMOVED AND REPLACED CHECK VALVE. REMOVED OLD SEALANT AND CLEANED WIRES OF SEALANT. REMOVED FEED THRU GROMMET. INSTALLED FEED THRU GROMMET AND RESEALED AS REQUIRED. REMOVED AND REPLACED LEFT AND RIGHT DRAIN VALVES. REMOVED AND REPLACED LEFT AND RIGHT SLANT PANELS SEALS. 2 L 7 2 4F A6WE 2002050900072 20020509 00072 GL 2002 5 9 USAASB02045 2 20020308 A 7200 ENGINE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B1US GL NR 1 OVERTEMP A USAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 383US 22956 MCI - FLT 1821 - AFTER TAKEOFF FROM MCI, AT APPROXIMATELY 600 FEET, THE WINDSHEAR WARNING SOUNDED. CREW APPLIED FIREWAL L THRUST FOR APPROXIMATELY 2 TO 3 SECONDS AND REPORTED THE NR 1 ENGINE EGT ROSE TO JUST ABOVE THE 940 DEGREE LIMIT. CRE W ELECTED TO RETURN TO FIELD AT MCI. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 1 ENGINE EGT EXCURSION TO BE WITHIN AREA 'A'. CONSULTED WITH MAINTENANCE CONTROL AND DETERMINED EGT EXCURSION TO BE N1 OVERSHOOT. INSPECTED IN ASSO CIATION WITH MM 72-00-00 AND COMPLIED WITH OVERTEMP INSPECTION. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2002050900073 20020509 00073 NM 2002 5 9 USAASB02046 1 20020309 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 437US 24559 PHL - MAINTENANCE REPORTED THE EMERGENCY LIGHTS, AT THE TWO AFT SEAT ROWS, INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE AFT LEFT BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002050900074 20020509 00074 NM 2002 5 9 USAASB02047 1 20020310 A 2751 2061141 INDICATOR BOEING 737 737401 1384701 NM COCKPIT FAULTY A USAA L A ABORTED APPROACH UNSCHED LANDING N FALSE WARNING AP APPROACH 1 EA 19 407US 8384 23877 BDL - FLT 482 - ON SHORT FINAL TO ALB, WHEN FLAPS WERE SELECTED TO 10 UNITS, CAPTAIN RECEIVED A FLAP INDICATOR NEEDLE SP LIT AND ASSOCIATED LEADING EDGE DEVICE AMBER LIGHT. LANDING WAS ABORTED AT ALB AND CAPTAIN REQUESTED ATC TO LAND AT BDL FOR LONGER RUNWAYS. CAPTAIN DECLARED AN EMERGENCY AS THE FLIGHT DIVERTED AND LANDED UNEVENTFUL AT BDL WITH FLAPS AT 5 UNITS. CAPTAIN REPORTED THAT NO ROLL PROBLEMS WERE ENCOUNTERED. MAINTENANCE PERFORMED VISUAL INSPECTION OF TRAILING ED GE FLAPS. NO DEFECTS NOTED. REMOVED AND REPLACED FLAP POSITION INDICATOR PER MM AND LUBRICATED FLAP JACKSCREW BALLNUT RESERVOIRS PER JOB CARD. OPERATED FLAPS SEVERAL TIMES WITH NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A16WE 2002050900075 20020509 00075 EU 2002 5 9 RAIA00204134 1 20020417 A 7312 10718 FUEL HEATER AEROSP ATR42 ATR42300 8680920 EU MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 424TE 19239 8376 124 5546-STL- DURING CLIMB LEFT FUEL HEATER INDICATED IN THE RED. MAINTENANCE INSPECTED AND PLACED ON DEFERRAL. LATER CLEARE D DEFERRAL BY REMOVING AND REPLACING THE FUEL HEATER. 2 H 7 2 4T RT A53EU 2002050900076 20020509 00076 EU 2002 5 9 RAIA00204135 1 20020417 A 3350 167006 LAMP AEROSP ATR42 ATR42300 8680920 EU BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 426TE 228 MX-STL- ESCAPE PATH LIGHTING HAS TWO BULBS INOP. MAINTENANCE PLACED ON DEFERRAL AND LATER CLEARED THE DEFERRAL BY REMOVI NG AND REPLACING THE DEFECTIVE LAMPS. 2 H 7 2 4T RT A53EU 2002050900077 20020509 00077 SO 2002 5 9 RAIA00204136 1 20020424 A 2700 0861DT5 VANE EMB 145 EMB145 3260210 SO INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 809HK 300 145187 5251-RIC- ADVISORY SYSTEM REPORTED STALL PROTECTION SYSTEM INOP. MAINTENANCE REMOVED AND REPLACED THE #1 AOA VANE. 2 L 7 2 4F RT T00011AT 2002050900078 20020509 00078 EU 2002 5 9 RAIA00204137 1 20020424 A 3010 3D351906 EJECTOR VALVE JETAIR JETSTM JETSTM4101 1500501 EU DEFECTIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 569HK 12694 41088 5585-STL- AIRFRAME DEICE FAULT INDICATION CCT-1 AUTO AND MANUAL. MAINTENANCE REMOVED AND REPLACED HR-7 CCT-1 EJECTOR FLO W VALVE. 2 L 7 2 4T RT A41NM 2002050900079 20020509 00079 NM 2002 5 9 USAASB02048 1 20020310 A 2751 1061141 INDICATOR BOEING 737 737401 1384701 NM COCKPIT FAULTY A USAA O OTHER F FLT CONT AFFECTED DE DESCENT 1 EA 19 424US 23991 BOS - FLT 1507 - ON DESCENT INTO BOS, CAPTAIN ADVISED THAT THE FLAPS WOULD NOT COME DOWN WHEN SELECTED. CREW WAS ADVISE D BY MAINTENANCE IN BOS TO CHECK CIRCUIT BREAKER FOR FLAP INDICATOR AND RESET. SLATS BEGAN TO DEPLOY ASYMMETRICALLY AND WERE THEN RETRACTED. AN EMERGENCY WAS DECLARED WITH ATC AND THE ALTERNATE ELECTRIC FLAP EXTENSION WAS USED. FLIGHT LA NDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE WITH EMERGENCY TRUCK ESCORT. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR. RAN FLAPS UP AND DOWN SEVERAL TIMES. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002050900080 20020509 00080 NM 2002 5 9 USAASB02049 1 20020312 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 445US 24863 LGA - MAINTENANCE REPORTED THE EMERGENCY LIGHTS INOPERATIVE AT THE AFT SERVICE DOOR IDENTIFIER AND ESCAPE SLIDE LIGHT TH E FLOOR PROXIMITY LIGHTING AT SEAT ROWS 24 AND 25 AND THE BULL NOSE LIGHT AT SEAT ROW 22 RIGHT. MAINTENANCE REMOVED AND REPLACED THE M1137 BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002050900081 20020509 00081 NM 2002 5 9 USAASB02060 1 20020323 A 2432 279202 CHARGER BOEING 737 7373B7 1384580 NM E/E BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 524AU 23859 BUF - FLT 1605 - EN ROUTE FROM PHL-YYZ, CAPTAIN REPORTED HE HAD LOST BOTH IRU'S AND THAT THE DC FAIL LIGHT WAS ILLUMINAT ED INDICATING A BATTERY CHARGER PROBLEM. FLIGHT DIVERTED TO BUF AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE BATTERY CHARGER INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER. ALSO, REMOVED AND REPLACED BATTERY DUE TO VOLTAGE READING LOW. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002050900082 20020509 00082 NM 2002 5 9 TSAA0233054 1 20020218 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED FORWARD SERVICE DOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A16WE 2002050900083 20020509 00083 NM 2002 5 9 TSAA0233055 1 20020303 A 3350 1000679 LIGHT BOEING 737 737282C 13844AU NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050900084 20020509 00084 NM 2002 5 9 TSAA0251049 1 20020221 A 5310 65505601 DOOR FRAME BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 FOUND EXFOLIATION CORROSION ON FORWARD SERVICE DOOR CHORD AT FRAME BS 294. REMOVED CORROSION BY CUTTING AWAY DAMAGED AR EA. FABRICATED REPAIR ANGLE AND DOUBLER. INSTALLED REPAIR PARTS IAW SRM 51-40-3, FIGURE 4. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 3 4F RT A3WE 2002050900085 20020509 00085 NM 2002 5 9 TSAA0251050 1 20020220 A 5320 651580778 ANGLE BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 CRACKED ANGLE ON FLOOR AT FRAME BS 294.5 RIGHT FLOOR LINE ALONG STRINGER 17R. REMOVED CRACKED ANGLE ON FLOOR AT FRAME B S 294.5 RIGHT FLOORLINE. REPLACED ANGLE PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002050900086 20020509 00086 NM 2002 5 9 TSAA0251051 1 20020220 A 5310 65505601 DOOR FRAME BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 FORWARD SERVICE DOOR CUTOUT, FORWARD FRAME CRACKED AT FRAME BS 294.5, STRINGER 15R. FABRICATED A REPAIR DOUBLER, FILLER AND A REPAIR ANGLE. INSTALLED ALL REPAIR PARTS IAW FIGURE 1 OF ECO 3272. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002050900087 20020509 00087 NM 2002 5 9 TSAA0251053 1 20020221 A 5240 6515580779 WEB BOEING 727 7272Q9 138448M NM SERVICE DOOR CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 FOUND EXFOLIATION CORROSION ON FORWARD SERVICE DOOR WEB AT BS 294. REMOVED CORROSION BY CUTTING AWAY DAMAGED AREA. FAB RICATED REPAIR WEB DOUBLER. INSTALLED REPAIR PARTS IAW SRM 51-40-2, FIGURE 4. (M) 2 L 7 3 4F RT A3WE 2002050900088 20020509 00088 NM 2002 5 9 TSAA0251057 1 20020221 A 5314 6574447 KEELBEAM BOEING 737 737209 13844AE NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 827AL 23913 DURING HEAVY CHECK, FOUND CORROSION ON LEFT KEEL BEAM LOWER CHORD AT BS 727 STRINGER 27L. THE CORROSION WAS TRIMMED OUT PER SRM. FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR PARTS USING SRM 51-30-2. VERIFIED APPROVAL RECEIVED AND COM PLETED REPAIR IAW ECO 1972. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050900089 20020509 00089 NM 2002 5 9 TSAA0253048 1 20020207 A 5347 65465271 SEAT TRACK BOEING 737 7372S5C 1384499 NM FUSELAGE DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 CUT AND REMOVED THE DAMAGED PORTION OF THE TRACK AT BS 420 TO 480. FABRICATED NEW SEAT TRACK. INSTALLED THE REPAIR PAR TS IAW SRM 53-10-5, FIGURE 7. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002050900090 20020509 00090 NM 2002 5 9 TSAA0257052 1 20020225 A 5754 HINGE FITTING BOEING 727 7272Q9 138448M NM KRUEGER FLAP DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 REMOVED DAMAGED KRUEGER FLAP PER MM 57-56-42 DUE TO ELONGATED HINGE FITTING HOLES. REMOVED AND REPLACED KRUEGER FLAP WI TH A LOWER PART NR IAW ECO 3273. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002051000014 20020510 00014 NM 2002 5 10 AUS20020309 1 20020402 A 2160 7787272 CONTROL VALVE DHAV DHC8 DHC8315 2809010 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE CABIN TEMP FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 AU S (AUS) NR 1 AIR CONDITIONING PACK TEMPERATURE CONTROL VALVE FAULTY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002051000015 20020510 00015 NM 2002 5 10 SABA020058 1 20020509 A 3350 1306 BULB DHAV DHC8 DHC8102 2809003 NM CABIN BURNED OUT A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 841PH 082 Ailrcraft 841 on flight 5032 PGV to CLT. During post-flight inspection at CLT a floor emergency light was found intermi ttently inoperative. Maintenance removed and replaced the bulb. Ops check was good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002053000057 20020530 00057 NM 2002 5 30 2002UALA00764 1 20020428 A 7931 8D1415 PRESSURE SWITCH BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE DEFECTIVE A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 607UA 21868 707522 LEFT ENGINE OIL FILTER EICAS CAUTION ILLUMINATED ON CLIMBOUT. REPLACED ENGINE MAIN OIL PRESS DIFFERENTIAL SWITCH PER MM . 2 L 7 2 4F 4 F RT A1NM E3NE 2002053000061 20020530 00061 NE 2002 5 30 2002UALA00766 2 20020428 A 7230 6A5994 RUB STRIP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE DEBONDED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 411UA 16855 5171 464 V10218 NR 2 ENGINE EXPERIENCED A MAJOR COMPRESSOR STALL. THE THROTTLE WAS RETARDED TO IDLE SPEED. REPLACED ENGINE. CORRECTIV E ACTION FOR MAJOR CAUSE IS INCORPORATION OF UPGRADED HIGH PRESSURE COMPRESSOR (HPC) RUBSTRIP MATERIAL THAT IS MUCH MORE RESISTANT TO DISBONDING. 2 L 7 2 4F 4 F RT A28NM E40NE 2002051000016 20020510 00016 NM 2002 5 10 2002UALA00771 1 20020427 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 935UA 26663 LEFT HAND FUSELAGE AT APPROXIMATELY STATION 360 AND STRINGER 16L HAS GOUGE AND DENT. MAJOR REPAIR ACCOMPLISHED. INSTAL LED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051000017 20020510 00017 NM 2002 5 10 2002UALA00772 1 20020427 A 5620 WINDOW FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 934UA 26662 LEFT HAND NR 5 CABIN WINDOW FRAME LOWER AFT CORNER INBOARD EDGE HAS EXCESSIVE MATERIAL LOSS IN SEAL CONTACT AREA DUE TO CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED EXTERNAL LOWER HALF DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002052900088 20020529 00088 NM 2002 5 29 2002UALA00773 1 20020427 A 2450 BACC18AE35 CIRCUIT BREAKER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 341UA 24245 DIVERTED TO DEN DUE TO LOSS OF GENERATOR. THE AIRCRAFT WAS DIVERTED TO DENVER WITHOUT INCIDENT. AMT CREW ISOLATED CAUS E OF FAILURE DUE TO NR 2 TRANSFER BUS NORMAL CIRCUIT BREAKER (C821) AS BAD. THE CIRCUIT BREAKER WAS REPLACED, AND THE A IRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002052900091 20020529 00091 NM 2002 5 29 2002UALA00774 1 20020426 A 2450 BACC18AE35 CIRCUIT BREAKER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 306UA 23667 DIVERTED TO DEN DUE TO ELECTRICAL PROBLEMS. CREW REPORTED NR 2 TRANSFER BUS CIRCUIT BREAKER (C821) POPPED IN CRUISE & I N SMOOTH AIR. REPORTED LOSING FIRST OFFICER'S INSTRUMENTS INCLUDING EADI AND EHSI. THE AIRCRAFT WAS DIVERTED TO DEN WI THOUT INCIDENT. AMT CREWS COULD NOT ISOLATE CAUSE OF FAILURE / DUPLICATE PROBLEM. THE CIRCUIT BREAKER WAS REPLACED AS PRECAUTIONARY, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051000018 20020510 00018 NM 2002 5 10 2002UALA00775 1 20020428 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 935UA 26663 STATION 178 BULKHEAD CRACKED AT RBL 517 INBOARD SIDE LOWER ANTENNA. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051000019 20020510 00019 2002 5 10 2002UALA00776 4 20020428 A 2330 7002086001 PROJECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 672UA 8103 30027 FIRST CLASS PROJECTOR FAILED EMITTING SMOKE AND FUMES INTO PASSENGER COMPARTMENT. REPLACED FIRST CLASS PROJECTOR, SYSTE M TEST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2002051000020 20020510 00020 NM 2002 5 10 2002UALA00777 1 20020424 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY CEILING LIGHT INOP AT ROW 13 CENTER AISLE. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002051000021 20020510 00021 NM 2002 5 10 2002UALA00778 1 20020424 A 3350 GUARD BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L1 DOOR MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT LIGHT SWITCH AT DOOR 1 LEFT IS MISSING THE GUARD. REPLACED GUARD. 2 L 7 4 4F 4 F RT A20WE E24NE 2002051000022 20020510 00022 NM 2002 5 10 2002UALA00779 1 20020424 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EEL STRIPS INOP AT ROWS 37HJK AND 53HJK. REPLACED EEL STRIP ASSY ON ROWS 37HJK AND 53HJK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002051000023 20020510 00023 NM 2002 5 10 2002UALA00780 1 20020424 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 ALL RIGHT SIDE A-ZONE EEL STRIPS INOP. REPAIRED EEL STRIP AT SEAT 4J. 2 L 7 4 4F 4 F RT A20WE E24NE 2002051500141 20020515 00141 NM 2002 5 15 2002UALA00781 1 20020430 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EEL LIGHTS INOP FIRST CLASS ENTIRE LEFT HAND SIDE FROM SEAT 1A THRU 5A. REPAIRED SHORTED EEL WIRING AT SEAT 2A. 2 L 7 4 4F 4 F RT A20WE E24NE 2002051000024 20020510 00024 NM 2002 5 10 2002UALA00782 1 20020424 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EEL STRIPS INOP AT DOOR 1 LEFT FORWARD OF CLOSET AND AFT GALLEY WALL RIGHT AISLE. RESECURED CONNECTOR, OP CHECKED OK. RELAMPED AT AFT GALLEY. 2 L 7 4 4F 4 F RT A20WE E24NE 2002051000025 20020510 00025 NM 2002 5 10 2002UALA00783 1 20020426 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 594UA 28145 EMERGENCY FLOOR LIGHTING INOP BEGINNING ROW 27 GOING AFT. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051000026 20020510 00026 WP 2002 5 10 CALA2000271 1 20020509 A 2560 3961899501 LANYARD DOUG DC9 DC982 3022082 WP A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 69826 49486 AFT GALLEY SLIDE LANYARD IMPROPERLY INSTALLED AT PREVIOUS STATION BY A CREWMEMBER. REPORTED BY FLIGHT ATTENDANT. REINSTA LLED LANYARD PER 25-62-00. 2 L 7 2 4F A6WE 2002051000027 20020510 00027 WP 2002 5 10 CALA2000272 1 20020509 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 FWD ENTRY THRESHOLD PLATE SUPPORT HAS CORROSION FROM STA 160-180 LBL-24L, 2"X24". REMOVED AND REPLACED THRESHOLD PLATE SUPPORT IAW SRM 51-10-03 2 L 7 2 4F A6WE 2002051000028 20020510 00028 NM 2002 5 10 2002UALA00784 1 20020427 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 CABIN FLOORBEAM CORRODED AT BODY STATION 345, RBL 36. MAJOR REPAIR ACCOMPLISHED. DAMAGED AREA CUT OUT RBL 34.5 - 37 FO RWARD FLANGE ONLY. NESTED DOUBLE ANGLE AND STRAP APPLIED TO FLOORBEAM, RBL 31-41. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051000029 20020510 00029 NM 2002 5 10 2002UALA00785 1 20020428 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 CABIN FLOORBEAM IS CORRODED AT STA 1640, RBL 50 TO RBL 60. MAJOR REPAIR ACCOMPLISHED. SPLICED IN A NEW FLOORBEAM CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051000030 20020510 00030 NM 2002 5 10 ABXA010871 1 20020504 A 3350 38931002 BATTERY BOEING 767 767231 1385131 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 707AX 22570 DURING MAINTENANCE INSPECTION, FOUND FLIGHT DECK REMOVABLE EMERGENCY EXIT SIGN BATTERIES LOW. REPLACED BATTERIES IAW B7 67 MM 33-51-01. 2 L 7 2 4F RT A1NM 2002051000031 20020510 00031 SO 2002 5 10 COMA0210019 1 20020508 A 3240 21585 BRAKE ASSY EMB 120 EMB120RT 3260202 SO L/H MLG FAILED A COMA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 259CA 26630 120252 FLIGHT 5042 ANTI-SKID WARNING DURING T/O ROLL.REPLACED THE L/H INBD BRAKE ASSY. 2 L 7 2 4T RT A31SO 2002051000032 20020510 00032 NM 2002 5 10 AWXA200200406 1 20020504 A 3350 233T321030 CONTROL PANEL BOEING 757 757225 1384959 NM COCKPIT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 913AW 14596 14596 22207 PHX -EEL - UNARMED LIGHT ON CAPTAINS EMERGENCY LIGHT CONTROL PANEL IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS EMERGENCY LIGHT CONTROL PANEL IAW BMM 33-51-08-401, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002051000033 20020510 00033 NM 2002 5 10 AWXA200200407 1 20020424 A 5230 BAC1505101353 DOOR FRAME BOEING 737 7373G7 1384595 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-16 CHECK A .0625 INCH CRACK WAS FOUND COMING FROM THE FASTENER HOLE AT FWD END OF LOWER T- CHORD VERTICAL LEG OF THE FORWARD CARGO DOOR, CONFIRMED BY HFEC INSPECTION. MAINTENANCE CUTOUT DAMAGED SECTION OF T-CHO RD AT BS 443, FABRICATED NEW SECTION OF T-CHORD, 2 DOUBLER ANGLES, 1 RADIUS FILLER, AND INSTALLED REPAIR PARTS IAW EO 52 -31-04. 2 L 7 2 4F RT A16WE 2002051000034 20020510 00034 NM 2002 5 10 AWXA200200409 1 20020505 A 3260 189915 PROXIMITY SENSOR BOEING 737 7373G7 1384595 NM LT MLG OUT OF ADJUST A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 302AW 24009 PHX - AIR TURNBACK - FLT - 0590 - AFTER TAKEOFF FROM PHX EN ROUTE TO MCI WHEN LANDING GEAR WAS RETRACTED THE LT MAIN LAN DING GEAR UNSAFE LIGHT ILLUMINATED. RETURNED TO PHX AND LANDED SAFELY. MAINTENANCE TROUBLESHOT AND REPLACED THE LT MAI N LANDING GEAR UPLOCK SENSOR/CONNECTOR IAW BMM 32-61-21-4, SENSOR ADJUSTED IAW BMM 32-61-21-5, OPERATIONAL CHECK WAS GOO D IAW BMM 32-61-00 PG 501-504. 2 L 7 2 4F RT A16WE 2002051000035 20020510 00035 NM 2002 5 10 AWXA200200410 1 20020428 A 2560 P4010021 BATTERY BOEING 737 737277 1384570 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 179AW 22646 YVR - EMERGENCY EQUIPMENT - DURING C-20 CHECK TEST OF THE EMERGENCY FLASHLIGHT LOCATED ON AFT WALL OF FWD LAV (LOWER) FO UND BATTERIES DEPLETED. MAINTENANCE REPLACED FLASHLIGHT BATTERIES, FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002051000036 20020510 00036 NM 2002 5 10 AWXA200200411 1 20020419 A 5330 6545774575 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CANNING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 GYR - MAJOR REPAIR - DENT / OIL CANNING ON SKIN DUE TO PREVIOUS REPAIR AND SKIN FATIGUE, BS 770, STRINGERS 24-25 LT, JUS T AFT OF DOUBLER. MAINTENANCE REMOVED SKIN PANEL FROM BS 727-908, STRINGERS 20-25 LT, PERFORMED HFEC INSPECTION OF UPPE R AND LOWER SPLICE FASTENER HOLES, NO CRACKS. FABRICATED NEW SKIN PANEL, STRINGER, AND STRINGER SPLICES, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5360-02120-SS1. 2 L 7 2 4F RT A16WE 2002051000037 20020510 00037 SO 2002 5 10 C2XA02SH005 1 20020501 A 3397 WIRE EMB 145 EMB145ER 3260211 SO CABIN BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 SHV - DURING C-CHECK INSPECTION, THE NUMBER THREE EMERGENCY LIGHT STRIP WAS FOUND TO HAVE BROKEN WIRES. 2 L 7 2 4F RT T00011AT 2002051000038 20020510 00038 SO 2002 5 10 C2XA02TY077 1 20020506 A 2620 14526968403 LINE EMB 145 EMB145 3260210 SO EXTINGUISH SYS CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS, DURING A SCHEDULED INSPECTION THE FIRE EXTINGUISHING DISCHARGE LINE WAS FOUND CHAFED ON THE LEFT ENGINE. MAINTENAN CE REMOVED AND REPLACED THE LINE IAW EMB-145-AMM-26-21-06. 2 L 7 2 4F RT T00011AT 2002051000039 20020510 00039 SO 2002 5 10 C2XA02TY078 1 20020507 A 5320 14522461003 DOUBLER EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS DURING A SCHEDULED 1C/2C INSPECTION, THE OMEGA BEAM DOUBLERS AT FRAMES 20 AND 22 WERE FOUND CORRODED. MAINTENANCE FABRICATED A NEW OMEGA BEAM DOUBLER'S AND REPLACED IAW EMB 145-SRM-53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE REL EASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002051000040 20020510 00040 SO 2002 5 10 C2XA02TY079 1 20020507 A 3210 14571035407 CAP EMB 145 EMB145 3260210 SO MLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS DURING A SCHEDULED 1C/2C INSPECTION, BOTH LT AND RT BEARING CAPS HAD CORROSION ON THE MLG. MAINTENANCE REMOVED AN D REPLACED BOTH FWD AND AFT LOWER BEARING CAPS IAW AMM 32-10-01, WHICH WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETI ON OF ALL C-CHECK INSPECTION. 2 L 7 2 4F RT T00011AT 2002051000041 20020510 00041 SO 2002 5 10 C2XA02TY081 1 20020507 A 7110 14576631621 STRUCTURE EMB 145 EMB145 3260210 SO NR 1 COWLING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS DURING A 1C/2C INSPECTION, THE NR 1 LOWER COWLING AFT EDGE MEMBER WAS CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER. ALL WORK WAS ACCOMPLISHED IAW EMB 135/145 SRM 51-20-03, CPM 51-21-04-05-06 AND SRM 51-40-02. ALL WOR K WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002051000042 20020510 00042 SO 2002 5 10 C2XA02TY082 1 20020507 A 5210 12021065001 STRUCTURE EMB 145 EMB145 3260210 SO PAX DOOR DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS DURING A SCHEDULED 1C-2C INSPECTION THE PAX DOOR LOWER AFT CORNER WAS DENTED. DENT MEASUREMENT'S WERE 1.25 INCH L BY .1875 INCH. MAINTENANCE RESTORED THE PROFILE, INSPECTED FOR CRACKS, NONE NOTED. ALL WORK WAS ACCOMPLISH AND WILL B E RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002051000043 20020510 00043 SO 2002 5 10 C2XA02TY083 1 20020507 A 5330 14524125003 SKIN EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS DURING A SCHEDULED INSPECTION THE SERVICE DOOR CUTOUT SKIN WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENA NCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB GST 1395/02, EMB145 CPM 51-21-04, 51-21-05 AND 51-21-06, THE REPAIR WAS SATI SFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002051000044 20020510 00044 NM 2002 5 10 CALA2000257 1 20020503 A 5320 656134 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 CORROSION ON L-ANGLE AT STA 500D, STRINGER 26L F/B/B. REMOVED AND REPLACED ANGLE REF SRM 51-70-12. 2 L 7 2 4F RT A16WE 2002051000045 20020510 00045 NM 2002 5 10 USAABB02014 1 20020205 A 3610 312N53217 DUCT BOEING 757 7572B7 1384964 NM BLEED AIR LEAKING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 624AU 27245 LAX - FLT 46 - CREW RECEIVED THE LEFT ENGINE 'OVHT' LIGHT AFTER TAKEOFF FROM LAX. FLIGHT RETURNED TO LAX AND LANDED WIT HOUT FURTHER INCIDENT. MAINTENANCE PERFORMED FIM PROCEDURES 26-11-00 AND RAN THE LEFT ENGINE FOR FIVE MINUTES. NO FAUL TS WERE FOUND AND THE PROBLEM COULD NOT BE DUPLICATED. AIRCRAFT RELEASED FOR SERVICE. SUBSEQUENTLY, MAINTENANCE FOUND THE HP-6 DUCT LEAKING AND REPLACED IT. (M) 2 L 7 2 4F RT A2NM 2002051000046 20020510 00046 NM 2002 5 10 USAABB02017 1 20020228 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 613AU 27144 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 29. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002051000047 20020510 00047 EA 2002 5 10 COMA0260304 1 20020507 A 3240 428853 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 920CA 4472 7022 FLIGHT 5527 ANTI SKID MESSAGE DURING T/O.REPALCED ANTI-SKID CONTROL. 2 L 7 2 4F RT A21EA 2002051000048 20020510 00048 NM 2002 5 10 USAABB02018 1 20020303 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 624AU 27245 BOS - FOUND LOW LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002051000049 20020510 00049 NM 2002 5 10 USAABB02019 1 20020228 A 2120 ODOR BOEING 767 7672B7 1385107 NM CABIN DETECTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 656US 26847 CLT - FLT 1522 - DURING THE LAST TWENTY MINUTES OF THE FLIGHT, A RUBBER SMELL WAS REPORTED IN THE AREA OF ROW 11. MAINT ENANCE INSPECTED THE AIRCRAFT AND COULD FIND NO DEFECTS. (M) 2 L 7 2 4F RT A1NM 2002051000050 20020510 00050 NM 2002 5 10 USAABB02020 1 20020306 A 3350 37067001 BATTERY BOEING 767 7672B7 1385107 NM COCKPIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 651US 24764 LAX - FLIGHT STATION EMERGENCY EXIT LIGHT WOULD NOT TEST. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A1NM 2002051000052 20020510 00052 NM 2002 5 10 USAABB02021 1 20020307 A 3397 WIRE BOEING 767 7672B7 1385107 NM CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 CLT - FOUND AISLE EMERGENCY LIGHTS ON RIGHT SIDE OF CABIN INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A SHORTED WIRE. (M) 2 L 7 2 4F RT A1NM 2002051000053 20020510 00053 2002 5 10 USAABB02024 4 20020311 A 2565 CONNECTOR BOEING 767 7672B7 1385107 NM CABIN DIRTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 652US 24765 MUC - RIGHT OVERWING ESCAPE SLIDE SQUIB FAILED TEST. MAINTENANCE CLEANED THE RIGHT BATTERY PACK CONNECTOR. (M) 2 L 7 2 4F RT A1NM 2002051000054 20020510 00054 EU 2002 5 10 USAASA02021 1 20020215 A 3230 LANDING GEAR AIRBUS A319 A319112 3930323 EU NLG MALFUNCTIONED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 704US 0922 PIT - FLT 2153 - EN ROUTE PIT-MSP, THE NOSE LANDING GEAR FAILED TO EXTEND ON APPROACH TO MSP. THE LANDING GEAR WAS CYCL ED AND WAS EXTENDED ONCE MORE. THE LANDING GEAR EXTENDED OK ON THE SECOND ATTEMPT. FLIGHT LANDED WITHOUT FURTHER INCID ENT. MAINTENANCE TESTED SYSTEM. CLEANED AND CHECKED CLEARANCES OF PROXIMITY SENSORS. SYSTEM BITE CHECK ON THE LANDING GEAR CONTROL AND INTERFACE UNIT WAS PERFORMED. NO FAULTS WERE FOUND. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2002051000055 20020510 00055 EU 2002 5 10 USAASA02023 1 20020217 A 3260 ABS012110 PROXIMITY SENSOR AIRBUS A319 A319112 3930323 EU NLG FAULTY A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 704US 0922 PIT - FLT 1686 - EN ROUTE DFW-PIT, ON APPROACH TO PIT, WHEN THE LANDING GEAR WAS EXTENDED, RECEIVED 'L/G DOORS NOT CLOSE D' AND 'L/G SYSTEM DISAGREE' MESSAGES. THE NOSE GEAR DID NOT INDICATE GREEN. THE LANDING GEAR WAS RECYCLED AND THE GEA R EXTENDED ON THE SECOND ATTEMPT. MAINTENANCE REPLACED THE NOSE LANDING GEAR DOWNLOCK SYSTEM NR 1 PROXIMITY SENSOR (FIN 18GA). SYSTEM FUNCTIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002051000056 20020510 00056 EU 2002 5 10 USAASA02024 1 20020301 A 3350 321430 BATTERY AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 179UW 1521 LGA - THE FORWARD, RIGHT, EMERGENCY POWER SUPPLY UNIT BATTERY FAILED DURING THE OPERATIONAL TEST. MAINTENANCE REMOVED A ND REPLACED THE BATTERY IN THE FORWARD RIGHT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002051000057 20020510 00057 NM 2002 5 10 USAASB02031 1 20020213 A 3350 20131A POWER SUPPLY BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 425US 23992 DCA - MAINTENANCE REPORTED THE RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1479 B ATTERY SUPPLY PACK AT STATION 598R. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002051000058 20020510 00058 NM 2002 5 10 USAASB02032 1 20020215 A 3350 20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 405US 23885 ERW - MAINTENANCE REPORTED THE LEFT AFT OVERWING EMERGENCY LIGHT, THE EMERGENCY LIGHTS AT SEAT ROWS 10 AND 11 AND THE OV ERHEAD EMERGENCY LIGHTS AT SEAT ROWS 8 AND 9 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MID CABIN OVERHEAD EMERG ENCY BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002051000059 20020510 00059 NM 2002 5 10 USAASB02035 1 20020217 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 512AU 23595 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 14L INOPERATIVE. MAINTENANCE REPAIRED WIRING FOR THE EMERGEN CY LIGHT AT SEAT ROW 14L. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002051000060 20020510 00060 NM 2002 5 10 USAASB02036 1 20020218 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 527AU 23862 PHL - MAINTENANCE REPORTED THE MID CABIN CEILING EMERGENCY EXIT LIGHT, RIGHT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002051000061 20020510 00061 NM 2002 5 10 USAASB02037 1 20020221 A 3397 WIRE BOEING 737 737401 1384701 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 412US 23881 IND - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 10 ABC INOPERATIVE. MAINTENANCE FOUND WIRES FROM THE SEAT TR ACK BROKEN. SPLICED WIRES FROM SEAT TRACK TO CONNECTOR UNDER SEAT ROW 10ABC. OPS CHECK OF ALL EMERGENCY LIGHTS GOOD. (M) 2 L 7 2 4F RT A16WE 2002051000062 20020510 00062 NM 2002 5 10 USAASB02041 1 20020302 A 2120 ODOR BOEING 737 7373B7 1384580 NM CABIN DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 511AU 23594 PHL - FLT 370 - ON CLIMB-OUT FROM PWM, EN ROUTE TO PHL, FLIGHT ATTENDANTS REPORTED A SULFUR SMELL WHICH DISSIPATED. ON DESCENT INTO PHL, AT THE END OF THE FLIGHT, THE SMELL RETURNED. SMELL WAS REPORTED TO BE COMING FROM THE MID CABIN, ARO UND ROW 14. CAPTAIN DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT WITH THE SMELL DISSIPATING AGAIN. AIRCRAFT TAXIIED TO THE GATE. MAINTENANCE PERFORMED VISUAL INSPECTION OF EXTERIOR AND INTERIOR OF AIRCRAFT. INSPECTED CABIN LIG HTING AND COFFEE MAKERS. NO DEFECTS OR SMELL NOTED. RAN ENGINES AND PRESSURIZED AIRCRAFT. NO LEAKS OR SMELL NOTED. A IRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002051000063 20020510 00063 NM 2002 5 10 USAASB02042 1 20020302 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 529AU 24411 CLT - MAINTENANCE REPORTED THE OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD IN ASSOCIATION WITH MM 33-51-51. (M) 2 L 7 2 4F RT A16WE 2002051000064 20020510 00064 NM 2002 5 10 USAASB02043 1 20020303 A 3350 20121 CHARGER BOEING 737 737401 1384701 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 422US 23989 LGA - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 6 ABC THROUGH 9 ABC INOPERATIVE AND THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLIES IN THE CEIL ING AT CENTER AISLE ADJACENT TO SEAT ROW 12 AND AT BATTERY POSITION 4 STATION 598. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002051000065 20020510 00065 NM 2002 5 10 USAASB02044 1 20020307 A 3350 1012721 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 371US 22950 PHL - MAINTENANCE REPORTED THE FLOOR LEVEL EMERGENCY LIGHT AT SEAT ROW 5 ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE LIGHT ASSEMBLY AT SEAT ROW 5 ABC. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002051000076 20020510 00076 SO 2002 5 10 C2XA02BT017 1 20020420 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 15983 145239 CREW REPORTED ELECTRICAL BURNING SMELL NOTICED ON APPROACH. MAINTENANCE INSPECTED THE ELECTRICAL SYSTEM IAW EMB145 MM C HAPTER 20-00-00. COULD NOT DUPLICATE THE SMELL. INSPECTION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002051000077 20020510 00077 SO 2002 5 10 C2XA02CL108 1 20020505 A 3350 744412 SIGN EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 14939 145030 CLE FLIGHT 3223 THE CREW REPORTED THE EXIT LIGHT SIGN ON THE RIGHT SIDE BULKHEAD WOULD NOT ILLUMINATE. MAINTENANCE INSP ECTED AND REPLACED THE EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002051000078 20020510 00078 SO 2002 5 10 C2XA02TY088 1 20020510 A 5322 14521718003 ANGLE EMB 145 EMB145 3260210 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS DURING A SCHEDULED 1C/2C INSPECTION THE LEFT AFT AISLE RAMP ANGLE AT FR. 20 WAS CORRODED. MAINTENANCE REMOVED AND F AB.A NEW ANGLE AND SHIM AND INSTALL ,ALLODINE,PRIMED AND PAINTED IAW EMB51-30-01 AND 51-21-04,05,06. ALL WORK WAS ACCOMP LISH AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002051000108 20020510 00108 WP 2002 5 10 DHL2002801010 1 20020508 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 801DH 46033 1) ¥2 ENGINE FIRE WARNING CAME ON ERRATICALLY AND INTERMITTENTLY WHEN ON "B" LOOP. NORMAL INDICATION WHEN ON "A" LOO P2) CHECKED ¥2 ENGINE FIRE WARNING SYSTEM R&R "B" CORE LOOP CONNECTOR P1-8059 IAW WD.26-01-01.TESTED OPERATION O F BOTH LOOPS FOUND OK 2 L 7 4 4F RT 4A25 2002051000109 20020510 00109 EU 2002 5 10 MALA020275 1 20020509 A 7930 TRANSDUCER SAAB SF340 340B 7860101 EU A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 410XJ 340B410 DURING FLIGHT #3356 RH ENG OIL PRESS FLUX IN FLIGHT AT ALL POWER SETTINGS BETWEEN 70 PSI AND 120 PSI. AIR RETURN TO DTW . MAINTENANCE INSPECTED CANNON PLUG AT GAUGE AND PRESS XDUCER, CHECKS GOOD. MAINTENANCE CLEANED PRESSURE REF. TUBE. RE MOVED AND REPLACED RH ENG OIL PRESS. TRANSDUCER.GROUND RAN A/C FOR 30 MIN. NO FLUX NOTED. LEAK CHK GOOD. 2 L 7 2 4T RT A52EU 2002051000110 20020510 00110 EU 2002 5 10 QXEA0200796 1 20020509 A 2130 39253021 VALVE FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 499US * 7758 11182 BOI- CLIMBING THROUGH 25,000 FEET CABIN PRESSURIZATION WAS CLIMBING 8,000 FEET. LEVELED OFF AT 26,000 FEET, CABIN PRESSU RE CONTINUED TO CLIMB TO 10,000. (AIRFOIL ANTI-ICE WAS ON AND WING TEMPERATURE WAS IN YELLOWAND BACK-UP VALVE WAS CLOSED ).AIRCRAFT RETURNED TO FEILD WITH OUT INCIDENT.ON DECENT TO BOI TURNED AIRFOIL OFF, BACK-UP VALVE OPENED AND PRESSURE RE TURNED TO 55 PSI.REMOVED AND REPLACED #1 BACK-UP VALVE AND #2 MAIN VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002051000111 20020510 00111 NM 2002 5 10 AALA20020058 1 20020117 A 2530 46700017 COFFEEMAKER BOEING 777 777223 1385213 NM GALLEY FAULTY A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 785AN 30005 LGW - FLT 0050 - EN ROUTE DFW-LGW - MAIN CABIN COFFEE MAKER 19 ON LEFT SIDE SMOKES. LANDED LGW WITHOUT INCIDENT. REPLA CED MAIN CABIN COFFEE MAKER 19. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002051000112 20020510 00112 2002 5 10 AALA20020168 4 20020223 A 2565 62772216 SLIDE BOEING 777 777223 1385213 NM R2 DOOR FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 LHR - FLT 87 - PRIOR TO DEPARTURE R-2 DOOR SLIDE INADVERTENTLY DEPLOYED WHEN OPENING DOOR FROM OUTSIDE. SLIDE FAILED TO INFLATE DUE TO LOW PRESSURE. REPLACED SLIDE ASSEMBLY AND RESERVOIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002051000113 20020510 00113 NM 2002 5 10 AALA20020263 1 20020225 A 5754 SKIN BOEING 777 777223 1385213 NM L/E SLAT DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 784AN 29588 AFW - FOUND DENT AT NR 6 SLAT TOP TRAILING EDGE JUST INBOARD OF OUTBOARD SLAT TRACK. CORRECTED PER MRB 777-030. (M) 2 L 7 2 4F RT T00001SE 2002051000114 20020510 00114 2002 5 10 AALA20020326 4 20020320 A 2565 62774415 BOTTLE BOEING 777 777223 1385213 NM EVAC SLIDE LOW A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 ORD - DURING OVERNIGHT MAINTENANCE, FOUND LOW BOTTLE FOR L4 DOOR EMERGENCY EXIT SLIDE. REPLACED SLIDE ASSEMBLY WITH SER VICEABLE UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002051000115 20020510 00115 2002 5 10 AALA20020328 4 20020320 A 2565 62774415 BOTTLE BOEING 777 777223 1385213 NM EVAC SLIDE LOW A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 ORD - DURING OVERNIGHT MAINTENANCE, FOUND LOW BOTTLE FOR L4 DOOR EMERGENCY EXIT SLIDE. REPLACED SLIDE ASSEMBLY WITH SER VICEABLE UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002051000116 20020510 00116 EU 2002 5 10 AALA20020329 1 20020320 A 5230 DOOR FRAME FOKKER F28 F28MK0100 4990807 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1432A 11417 TUL - FOUND MID CARGO AFT DOOR FRAME CORRODED. FABRICATED DOUBLER AND INSTALLED PER ESO 51000 DATED 14 MAR 02. (M) 2 L 7 2 4F RT 2002051000117 20020510 00117 WP 2002 5 10 AALA20020374 1 20020401 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 423AA 49335 AUS - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051000118 20020510 00118 WP 2002 5 10 AALA20020376 1 20020402 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 554AA 53084 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING ASSEMBLY AT 11D DIM. REPLACED EMERGENCY EXIT PATH LIGH TING ASSEMBLY AT 11D DIM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051000119 20020510 00119 NM 2002 5 10 AALA20020379 1 20020331 A 2131 S210T160113 CONTROLLER BOEING 767 767223 1385123 NM CABIN PRESSURE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 339AA 22336 JFK - FLT 15 - EN ROUTE JFK-LAX - SHORTLY AFTER TAKEOFF EICAS MESSAGE INDICATED NO NR 1 AND 2 CABIN ALTIMETER INDICATION . MANUAL MODE ALLOWED LIMITED VALVE CONTROL. RETURNED TO JFK AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 AUTO PRESSURE CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002051000120 20020510 00120 WP 2002 5 10 AALA20020423 1 20020402 A 3350 LIGHT DOUG DC9 DC982 3022082 WP A/C BAY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 450AA 49476 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT MARKER IN TAIL COMPARTMENT BROKEN. REPLACED EMERGENCY EXI T PATH LIGHT MARKER IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051000121 20020510 00121 WP 2002 5 10 AALA20020424 1 20020404 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7550 53032 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY AFT LOWER OVERWING EXIT LIGHT DIM. REPLACED EMERGENCY AFT LOWER OVERWING EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051000122 20020510 00122 WP 2002 5 10 AALA20020425 1 20020404 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7550 53032 PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AFT SEAT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT AFT SEAT LIGHT B ATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051000123 20020510 00123 WP 2002 5 10 AALA20020426 1 20020408 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7550 53032 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS SEAT 20 TO END OF AIRCRAFT INOPERATIVE. REPLACED EMERGEN CY EXIT SEAT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051000124 20020510 00124 WP 2002 5 10 AALA20020427 1 20020407 A 3350 P4010049 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 436AA 49454 ORD - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD HALF OF CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY E XIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002051000125 20020510 00125 WP 2002 5 10 AALA20020428 1 20020406 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 285AA 49297 ORD - DURING OVERNIGHT MAINTENANCE, AFT SECTION EMERGENCY EXIT LIGHTS FORWARD OF AFT DOOR INOPERATIVE. RESECURED EMERGE NCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051000126 20020510 00126 NM 2002 5 10 AALA20020430 1 20020322 A 5753 SUPPORT BOEING 767 767323 1385205 NM T/E FLAP CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AA 26996 AFW - FOUND CORROSION IN MOUNT HOLE FORWARD OUTBOARD LEFT INBOARD FLAP SUPPORT BEAM. VISUALLY INSPECT BORE TO ENSURE CO MPLETE CORROSION REMOVAL. FABRICATE FREEZE FIT PLUG TO ACHIEVE A MIN .001 INCH INTERFERENCE FIT. (M) 2 L 7 2 4F RT A1NM 2002051000127 20020510 00127 GL 2002 5 10 RAIA00204138 2 20020426 A 7310 23061825 FUEL FILTER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CLOGGED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 812HK 145373 311666 5299-STL- LEFT ENGINE FUEL IMPENDING BYPASS MESSAGE. MAINTENANCE REMOVED AND REPLACED FUEL FILTER. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002051000128 20020510 00128 EU 2002 5 10 RAIA00205139 1 20020501 A 3030 E0308028C0 RELAY AEROSP ATR42 ATR42300 8680920 EU A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 424TE 124 5554-STL- FIRST OFFICER PITOT FAULT LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RELAY 33DA. 2 H 7 2 4T RT A53EU 2002051000129 20020510 00129 2002 5 10 RAIA00205142 4 20020502 A 3425 7003974606 COMPUTER AEROSP ATR72 ATR72202 8680940 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 722TE 16423 10529 220 5550-STL- FLIGHT DIRECTOR FAILED. MAINTENANCE REMOVED AND REPLACED AFCS COMPUTER. 2 H 7 2 4T RT A53EU 2002051000130 20020510 00130 EU 2002 5 10 RAIA00205143 1 20020506 A 7722 30738451 LEAD JETAIR JETSTM JETSTM4101 1500501 EU BROKEN A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 564HK 41081 5387-EWR- RECEIVED RIGHT ENGINE INTEGRATED ELECTRONIC CONTROL FAULT INDICATION. MAINTENANCE REMOVED AND REPLACED THE THE RMOCOUPLE LEAD. 2 L 7 2 4T RT A41NM 2002051000131 20020510 00131 EU 2002 5 10 RAIA00205144 1 20020506 A 3240 E032401 SWITCH AEROSP ATR72 ATR72202 8680940 EU INTERMITTENT A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 721TE 217 5592-STL- PARKING BRAKE LIGHT INTERMITTENT. MAINTENANCE REMOVED AND REPLACED PARKING BRAKE MICRO SWITCH. 2 H 7 2 4T RT A53EU 2002051000132 20020510 00132 NM 2002 5 10 02051002 1 20020510 A 3397 WIRE BOEING 757 757200 1384950 NM A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 542NA 26245 EMERGENCY FLOOR LIGHTS INOP ROWS 7 TO 15 ABC. T/S FOUND BROKEN CONTACT WIRE. REPAIRED WIRE AS PER M/M 33-51-00; OPS CHE CK GOOD. 2 L 7 2 4F RT A2NM 2002051100001 20020511 00001 SO 2002 5 11 C2XA02TY090 1 20020511 A 5320 14522466011 PLATE EMB 145 EMB145 3260210 SO GALLEY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS, During a scheduled inspection, minor corrosion was found on tha aft digital plate at frames 16 and 17. Maintenance removed the corrosion and replaced the corroded rivits. I/A/W-EMB-145-SRM-51-10-02, 51-40-02 and 51-21-04/05 & 06. The r epair was satisfactory and the aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002051300008 20020513 00008 SW 2002 5 13 CA020313001 1 20020313 A 5711 SPAR BBAVIA 7 7GCBC 1220601 SW LYC O320 O320A2B 41508 EA LT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LT WING SPAR CRACKS WERE FOUND. THE FRONT SPAR WAS CRACKED FROM THE STRUT ATTACHMENT OUTBOARD. THE REAR SPAR HAD A SEVERE COMMPRESSION CRACK STARTING 3 FEET FROM WINGTIP, PROGRESSING OUTBOARD. 1 H 7 1 3O 3 O NC A759 E274 2002051300038 20020513 00038 WP 2002 5 13 2002F00471 1 20020405 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 466AA 49596 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED FIRST OVERHEAD EMER GENCY EXIT LIGHT CONTACTS ON BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051300039 20020513 00039 SO 2002 5 13 C2XA02RI004 1 20020506 A 3222 1170C000001 STRUT EMB 145 EMB145 3260210 SO NLG FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13965 145125 RIC FLT 3576-CREW REPORTED AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO RIC WITHOUT FURTHER INCIDENT. MAINT ENANCE FOUND THE NOSE LANDING GEAR CENTERING UNIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR S TRUT ASSEMBLY, AND PERFORMED A SATISFACTORY SYSTEM OPERATIONAL TEST. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002051300041 20020513 00041 NM 2002 5 13 DHL2002715007 1 20020503 A 2612 POWER UNIT BOEING 727 727155C 138404Z NM APU FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 715DH 19618 APU FIRE WARNING BELL IN COCKPIT INOP, HORN IN NOSE WHEEL WELL WORKS NORMALLY. REMOVED APU FIRE DETECTION POWER UNIT AN D CLEANED CONTACTS. REINSTALLED POWER UNIT. OPS CHECK GOOD IAW MM 26-15-00. 2 L 7 3 4F A3WE 2002051300042 20020513 00042 NM 2002 5 13 DHL2002726515 1 20020420 A 5523 TAB BOEING 727 727228 1384083 NM ELEVATOR PUNCTURED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, LT AND ELEVATOR CONTROL TAB SHOW PUNCTURED HOLE TOP SIDE STA 73.0 APPROX. CUT OUT PUNCTURED AREA ON LT ELEVATOR TAB, IAW B-727 SRM 55-20-1 FIG 1 AND 51-40-10 FIG 2. INSTALLED REPAIR IAW B-727 SRM 51-40-10 FIG 2. OPS CHECK GOOD IAW B-727 MM 27-30-0. 2 L 7 3 4F RT A3WE 2002051300044 20020513 00044 NM 2002 5 13 DHL2002726517 1 20020423 A 5315 FLOORBEAM BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C CHECK, BS 930 FLOORBEAM IS EXFOLIATED ON THE AFT SIDE OF THE BEAM AT THE INTERSECTION WITH THE BS 930 LT FORGIN G LBL 62, WL 203. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-10-2 FIG 8 SHEET 3 DETAIL III. FABRICA TED REPAIR PART IAW AVITAS DWG FASI-021D-1. INSTALLED REPAIR IAW AVITAS DWG FASI-021D-1. 2 L 7 3 4F RT A3WE 2002051300045 20020513 00045 NM 2002 5 13 DHL2002743006 1 20020503 A 2612 PIN BOEING 727 727225 1384077 NM CONNECTOR SHORTED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 743DH 22438 ON PREDEPARTURE CHECK NR 1 ENGINE FIRE TEST POPPED C/B. FOUND PIN SHORTED NR 1 ENGINE FIRE LOOP CONNECTOR D1504 REF: W/ D 26-11-00. REPLACED PIN PER M/M 20-11-0. OPS CHECKS GOOD PER M/M 26-11-001. 2 L 7 3 4F A3WE 2002051300046 20020513 00046 NM 2002 5 13 DHL2002747003 1 20020501 A 2612 69295671 WARNING HORN BOEING 727 727224 1384076 NM NLG WW INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 747DH 22253 DURING APU FIRE TEST THERE IS NO AURAL HORN SOUND IN NOSE WHEEL WELL. REMOVED & REPLACED APU AURAL WARNING HORN IAW DHL WPM 20-30-12. OPS CHECK OK IAW DHL MM 26-15-0. 2 L 7 3 4F A3WE 2002051300047 20020513 00047 NM 2002 5 13 DL72S020493 1 20020429 A 5753 652497862 WEDGE BOEING 727 727232 1384082 NM WING DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 OUTBOARD MIDFLAP TRAILING EDGE DELAMINATION. REPAIRED PER ER/A 417248-14. 2 L 7 3 4F A3WE 2002051300048 20020513 00048 NM 2002 5 13 DL72W020488 1 20020428 A 3350 S106 BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 293WA 22111 ON L/O FOUND CENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 29. REPLACED BATTERIES, OPS NORMAL. 2 L 7 3 4F A3WE 2002051300049 20020513 00049 NM 2002 5 13 DL72W020491 1 20020429 A 3350 900835A BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 296WA 22533 RT OVERWING EXIT SIGN EMERGENCY LIGHTS INOP. REPLACED BATTERY, CKS OK. 2 L 7 3 4F A3WE 2002051300050 20020513 00050 NM 2002 5 13 DL733020486 1 20020427 A 3350 0201924001 LIGHT BOEING 737 737301 1384611 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948WP 23259 L2 DOOR EMERGENCY EXIT IDENT NEAR FLOOR DAMAGED. REPLACED BASE, OP CKS GOOD. 2 L 7 2 4F RT A16WE 2002051300051 20020513 00051 NM 2002 5 13 DL738020489 1 20020429 A 2530 50459 OVEN BOEING 737 737832 13844CF NM GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 3740C 30800 F/A REPORTS ODOR IN CABIN, NO VISIBLE SMOKE PRESENT. ISOLATED GALLEY PWR, ODOR DISPERSED. PERFORMED T/S JIC 5088 ALSO F/A SUSPECTED FIRST CLASS OVEN. REPLACED OVEN AND OPERATE ALL CHECKS GOOD. 2 L 7 2 4F RT A16WE 2002051300052 20020513 00052 NM 2002 5 13 DL73K020478 1 20020424 A 5753 CARRIAGE BOEING 737 737232 1384475 NM T/E FLAP SEPARATED A DALA O OTHER F FLT CONT AFFECTED LD LANDING 1 SO 27 315DL 23087 RUDDER TRIM EXCESSIVE DURING ALL PHASES OF FLIGHT. REQUIRES 1.5 UNITS OF RUDDER TRIM. OUT OF TRIM ROLL TENDENCY INCREA SED ON APPROACH WITH EACH SUCCESSIVE FLAP EXTENSION. IE 3 UNITS OF RUDDER TRIM REQUIRED AT FLAPS 15. CONDUCTED 15 UNI T FLAP LANDING FOR CONDITION. FOUND LT OUTBOARD FLAP INBOARD TRACK CARRIAGE SEPARATED AT SHANK TO THRUST BEARING. REPL ACED SAME. 2 L 7 2 4F RT A16WE 2002051300053 20020513 00053 2002 5 13 DL757020481 4 20020425 A 2330 RDAV2132 MONITOR BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 616DL 22823 FAINT SMELL OF BURNT/ELECTRICAL ON FINAL AND ON TAXI IN. FOUND FIRST CLASS VIDEO MONITOR FAILED. MONITOR SMELLED AND S HOWED EVIDENCE OF ELECTRICAL DISTRESS. REPLACED MONITOR. 2 L 7 2 4F RT A2NM 2002051300054 20020513 00054 2002 5 13 DL757020482 4 20020425 A 2565 80330033 RESERVOIR BOEING 757 757232 1384965 NM R1 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 684DA 27104 R1 DOOR HAD PARTIAL SLIDE DEPLOYMENT/ INSPECTED SLIDE NOT ACTIVATED. REINSTALLED SLIDE BACK ON DOOR PER MM. FOUND EMER GENCY POWER RESERVOIR EMPTY. INSTALLED AND RIGGED NEW RESERVOIR PER MM. 2 L 7 2 4F RT A2NM 2002051300055 20020513 00055 SO 2002 5 13 SIMA200206508 1 20020214 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 145275 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, CORROSION WAS FOUND ON FORWARD DIGITAL STATION 163 AND BL 0.0 THAT WAS BEYO ND SRM LIMITS. FABRICATED REPAIR DOUBLER, WORK DONE IAW EMB GST-0508/02, EMB145 SRM 145/1142, REV 17, STANDARD PRACTICE S AND CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002051300056 20020513 00056 SO 2002 5 13 SIMA200206509 1 20020214 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 145275 ABI - DURING AN MBV INSPECTION OF AIRCRAFT, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 20 WHICH EXCEEDED SRM LI MITS. FABRICATED DOUBLER ANGLE, A FILLER, AND PLATE. WORK DONE IAW EMB 145 SRM 145/1142 CHAPTER 53 REV 17 53-21-10 PARA 2 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002051300057 20020513 00057 SO 2002 5 13 SIMA200206702 1 20020123 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 604DG 145058 DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE FORWARD DIGITAL. REMOVED CORROSION BY BLENDING OUT. FABRICATED A REPAIR DOUBLER IAW EMB GST-0149/02, ITEM 2 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002051300058 20020513 00058 SO 2002 5 13 SIMA200206703 1 20020124 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 604DG 145058 ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY AREA SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLEN DING OUT. FABRICATED A REPAIR DOUBLER IAW EMB GST-0149/02 ITEM 1 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002051300059 20020513 00059 SO 2002 5 13 SIMA200206704 1 20020129 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 604DG 145058 ABI - DURING INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19L CHAFED BETWEEN FRAMES 52 AND 53. FABRICATED AND INSTAL LED A TEMPORARY DOUBLER ANGLE AND TWO SHIMS IAW EMB GST-0154/02 PERMANENT REPAIR BY NEXT C-CHECK IAW GST-0289/02. (M) 2 L 7 2 4T RT T00011AT 2002051300060 20020513 00060 SO 2002 5 13 SIMA200206705 1 20020129 A 5313 STRINGER EMB 145 EMB145 3260210 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 607AE 145064 ABI - DURING INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19R CHAFED BETWEEN FRAME 52 AND 53. FABRICATED AND INSTALL ED A TEMPORARY DOUBLER AND TWO SHIMS IAW EMB GST-0154/02 PERMANENT REPAIR BY NEXT C-CHECK IAW GST-0289/02. (M) 2 L 7 2 4F RT T00011AT 2002051300061 20020513 00061 SO 2002 5 13 SIMA200206706 1 20020112 A 5320 DOUBLER EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 607AE 145064 ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED PREVIO US REPAIR AND CORROSION BY CUT OUT. FABRICATED AND INSTALLED A DOUBLER ANGLE AND FILLER. A PLATE AND TWO SHIMS IAW EMB 145 SRM 145/1142 CHAPTER 53 REV 16, 53-21-10 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002051300062 20020513 00062 SO 2002 5 13 SIMA200206707 1 20020123 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 607AE 145064 ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY FLOORBEAM 3 INCH AFT OF FRAME 22. REMOVED CORROSION BY BLENDING OUT. FABRICATED AND INSTALLED U-CHANNEL DOUBLER IAW EMB GST-0130A/02 ITEM 6, AND STANDARD SRM PRACTICES. ( M) 2 L 7 2 4F RT T00011AT 2002051300063 20020513 00063 SO 2002 5 13 SIMA200206708 1 20020124 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 607AE 145064 ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY CENTER FLOORBEAM AT FRAME 20. REMOVED CORROSION BY B LENDING OUT. FABRICATED AND INSTALLED A 'U' CHANNEL DOUBLER IAW EMB GST-0130A/02 ITEM 6, GST-0276/02 AND STANDARD SRM P RACTICES. (M) 2 L 7 2 4F RT T00011AT 2002051300064 20020513 00064 SO 2002 5 13 SIMA200206709 1 20020122 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 706AE 145064 ABI - DURING INSPECTION OF AIRCRAFT, FOUND STRINGER 19R CHAFED IN HYDRAULIC BAY. REMOVED CHAFED BY BLENDING IAW EMB GST -0093/02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002051300065 20020513 00065 SO 2002 5 13 SIMA200206710 1 20020122 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 706AE 145064 DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON CARGO DOOR CENTER SILL BEAM. REMOVED AND REPLACED WITH NEW BEAM IAW E MB145 SRM 145/1142, REV 16 51-20-01, 51-40-02, 51-40-04, CPM 51-21-04, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002051300066 20020513 00066 SO 2002 5 13 SIMA200206901 1 20020310 A 2612 FIRE WARNING EMB 145 EMB145 3260210 SO COCKPIT ACTIVATED A SIMA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 21 613AE 145081 TVC - FLT 4253 - CREW REPORTED, A E1 FIRE WARNING JUST AFTER CLIMB-OUT AND THEN IT WENT OUT. THE CREW DECLARED AN EMERG ENCY AND SHUTDOWN THE ENGINE. THE AIRCRAFT WAS RETURNED TO TVC AND LANDED WITH NO FURTHER INCIDENTS. (M) 2 L 7 2 4F RT T00011AT 2002051300067 20020513 00067 SO 2002 5 13 SIMA200207001 1 20020224 A 5320 DOUBLER EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AE 145068 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION, PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20. REMOV ED PREVIOUS REPAIR, CORROSION LIMITED TO PREV REPAIR. FABRICATED A DOUBLER ANGLE AND FILLER. A PLATE AND TWO SHIMS. W ORK DONE IAW EMB 145 SRM 145/1142 CHAPTER 53 REV 16, 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002051300068 20020513 00068 SO 2002 5 13 SIMA200207002 1 20020301 A 5320 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AE 145055 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, THE PREVIOUS REPAIR AND THE LEFT OMEGA BEAM AT FRAME 20 WERE FOUND TO BE CO RRODED BEYOND SRM LIMITS. REMOVED PREV REPAIR AND CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, FILLER, A PLATE, A ND TWO SHIMS. WORK DONE IAW EMB145 SRM, SRM 145/1142 CHAPTER 53 REV 17, 53-21-10 PAGE 201, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002051300069 20020513 00069 SO 2002 5 13 SIMA200207004 1 20020305 A 5320 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AE 145055 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND LEFT BEAM CHAFED BETWEEN FRAMES 20 AND 24. BLENDED CHAFE. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A 'Z' PROFILE REPAIR DOUBLER. (M) 2 L 7 2 4T RT T00011AT 2002051300070 20020513 00070 SO 2002 5 13 SIMA200207005 1 20020306 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AE 145055 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND LOWER CARGO DOOR CENTER SILL BEAM CORRODED. REMOVED CORRODED SILL BE AM. INSTALLED SILL BEAM IN CARGO DOOR IAW EMB 145 SRM 145/1142, REV 17 51-20-01, 51-40-00, 51-40-02, 51-40-04, CPM 51-2 1-04, 51-21-05, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002051300071 20020513 00071 SO 2002 5 13 SIMA200207006 1 20020307 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AE 145055 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING OUT. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER. WORK DONE IAW EMB GST 0714/02, ITEM 6 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002051300072 20020513 00072 SO 2002 5 13 SIMA200207007 1 20020308 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AE 145055 DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19R UNDER AFT BELLY PANEL GOUGED. BLENDED GOUGE. PERFOR MED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED TWO DOUBLER ANGLES, AND FOUR SHIMS. WORK DONE IAW EMB GST 0700/02, ETN-EM-53-020 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002051300073 20020513 00073 SO 2002 5 13 SIMA200207008 1 20020308 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AE 145068 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY AREA FORWARD DIGITAL. PERFORMED AN NDT INSPE CTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPLACEMENT STRAP, TWO DOUBLERS AND A SHIM. WORK DONE I AW EMB 145 SRM 145/1142, REV 17, 53-21-10, GST-0623/02, ITEM 1, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002051300074 20020513 00074 SO 2002 5 13 SIMA200207009 1 20020302 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AE 145068 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY CENTER HAT BEAM. REMOVED CORRODED GALLEY CEN TER HAT BEAM. INSTALLED NEW HAT BEAM IAW EMB 145 SRM/1142, REV 17, 51-20-03, 51-40-02, GST-0623/02, ITEM 7 SEP 0114/02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002051300075 20020513 00075 2002 5 13 SIMA200207702 4 20020318 A 3460 710700083407 COMPUTER EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A SIMA B EMER. DESCENT S AFFECT SYSTEMS CL CLIMB 1 SW 21 643AE 145200 OKC - FLT 3602 - CREW REPORTED AT APPROXIMATELY 4000 FT FIRST OFFICER LOST HEADING AND ATTITUDE FOLLOWED BY THE CAPTAIN LOSING HIS HEADING AND ATTITUDE. EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY. DURING RETURN TO FIELD CAPTAIN SIDE CAME BACK ON LINE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS INTEGRATED AVIONICS COMPUTER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002051300076 20020513 00076 SO 2002 5 13 SIMA200207908 1 20020302 A 3350 7824I INVERTER EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST NR NOT REPORTED 1 SW 21 704PG 145174 FLT 4501 - BOS - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 INVERTER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2002051300077 20020513 00077 NE 2002 5 13 SIMA200208811 2 20020327 A 7261 312169001 SHAFT SEAL AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 2 ENGINE FAILED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 141AE 141 DURING CLIMB ABOVE 700 MSL NR 2 OIL PRESSURE LIGHT CAME ON. PRESSURE SHOWED FLUCTUATIONS BETWEEN 30-60 PSI. LARGE FLUC TUATIONS EXECUTED PRECAUTIONARY SHUTDOWN AND RETURN TO MCO. LANDING UNEVENTFUL. INFLIGHT EMERGENCY DECLARED. REPLACED PROP SHAFT SEAL. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2002051300078 20020513 00078 SO 2002 5 13 SIMA200210712 1 20020410 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIGHT OMEGA BEAM BETWEEN FRAMES 23 AND 25. REMOVED CORR OSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DO UBLER. REPAIR DONE IAW EMBRAER GST-1140/02 DAMAGE NR 13, GST-1169/02, ITEM 2 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002051300079 20020513 00079 EA 2002 5 13 SWIA200210807 1 20020422 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG LOW A SWIA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 NM 07 437SW 7564 INBOARD GROUND SPOILERS DEPLOYED DURING TAKEOFF RUN WHILE THRUST LEVERS WERE BEING ADVANCED. SERVICED NOSE GEAR STRUT IAW CRJ MM 12-12-32. PERFORMED GROUND TAXI. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002051300080 20020513 00080 NE 2002 5 13 UPS02438093 2 20020428 A 7530 RESISTOR BOEING 747 747200 1384847 NM PWA JT9 JT9D7A 52054 NE COCKPIT BLOWN A IPXA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 521UP 21944 INSPECTION TYPE:N/A SMOKE IN THE C/P ON TOP OF DESCENT. COULD NOT LOCATE SOURCE. DID NOT SMELL ELECTRICAL. COMPLETED C/P SMOKE/FUME EVACUATION CHECKLIST. SMOKE WAS MODERATE TO HEAVY FROM GLARESHIELD-AREA THROUGH WHOLE UPPER DECK. ADJU STED NR 1 & 4 ENG N2 GROUND IDLE PER MM 71-00-00. NR 2 ENG NR 2 IP BLEED VALVE ACOUSTICAL ATTENUATOR BLOWN THROUGH, REM OVED AND REPLACED SAME NR 1 ENG RUN REQ FOR LEAK CHECK AND IGN VERIFICATION RUN NR 1 ENGINE, NO LEAK NOTED. NR 2 ENG RU N REQUIRED FOR LEAK CHECK. RAN NR 2 ENGINE, NO LEAK NOTED. 2 L 7 4 4F 4 F RT A20WE E20EA 2002051300081 20020513 00081 NE 2002 5 13 UPS02637961 2 20020327 A 7230 LINKAGE BOEING 767 76734AF 1385212 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE BROKEN A IPXA K NONE E VIBRATION/BUFFET CL CLIMB 1 SO 01 331UP 27757 INSPECTION TYPE:ETOP COMPRESSOR STALL ON T/O AFTER V1. ALL ENGINE INDICATIONS NORMAL UNTIL IDLE POWER DESCENT. THEN NU MBER 2 ENGINE VIBRATION SHOWED 4.4 - 4.8 UNITS. FOUND 5TH STAGE VSV LEVER ARM BROKEN OFF AT APPROX 7 O'CLOCK POSITION. REMOVED AND REPLACED RT ENGINE PER TC 6002 AND 6001 REF ENG OPS CHECKS AND LEAK CHECK NORMAL. PN OFF CF6- 80C2B6F609, SN OFF 704924. AC DOWNGRADED TO NON-ETOPS DUE TO RT ENGINE CHANGE. 2 L 7 2 4F 4 F RT A1NM E13NE 2002051300084 20020513 00084 NE 2002 5 13 00026 2 20020510 A 7200 ENGINE LEAR 24 24D 5170311 CE GE CJ610 CJ6106 30006 NE LEFT FLAMED OUT E HAEA B EMER. DESCENT X ENGINE FLAMEOUT CR CRUISE 1 SW 05 266TW 266 240M228 AIRCRAFT EN ROUTE FROM MDW TO MCI AT FL450 CRUISE ENCOUNTERED TURBULENCE LT ENGINE FLAME OUT. REQUESTED LOWER FOR RELIG HT, RELIGHT NORMAL, ALL INDICATIONS NORMAL. CONTINUED FLIGHT, ENGINE INSPECTED ON GROUND, NOTHING FOUND. 2 L 7 2 4J 4 J A10CE 1E16 2002051300086 20020513 00086 NM 2002 5 13 C1HA200296014 1 20020510 A 3350 900542 POWER SUPPLY BOEING 727 7272J4 1384006 NM INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 696CA 22574 LH aft exterior emergency light inoperative. Removed and replaced power supply IAW MM. Operationally checks good. 2 L 7 3 4F RT A3WE 2002051300088 20020513 00088 WP 2002 5 13 0201389752 1 20020507 A 2120 BOOT DOUG DC9 DC941 302207N WP A/C BAY TORN A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 752NW 47116 WHILE CRUISING AT FL240, THE AIRCRAFT EXPERIENCED A LOSS OF CABIN PRESSURIZATION. WING AND ENGINE ANTI-ICE PROTECTION W ERE ON. COMPLIED WITH COM PROCEDURES WITH NO HELP. CREW ACCOMPLISHED AN EMERGENCY DESCENT TO 10,000 FEET AND CONTINUED TO DESTINATION. RIGHT AIR CONDITION SUPPLY HIGH AND AIRFOIL ICE PROTECTION PRESSURE ABNORMAL ANNUNCIATORS DID ILLUMINA TE ON FINAL APPROACH. LANDING WAS UNEVENTFUL AT OMA. MAINTENANCE FOUND THE RAM AIR DUCTING AFT OF THE HEAT EXCHANGER W ORN THROUGH, THE RIGHT SIDE FLEXIBLE BOOT FROM THE -Y- DUCT WAS TORN. BOOT WAS REPLACED AND SOME WORN WIRES FROM THE CA NNON PLUG ON THE RIGHT ACM WERE REPAIRED. STINGER CHECK OK. 2 L 7 2 4F A6WE 2002051300090 20020513 00090 WP 2002 5 13 0201399944 1 20020504 A 3010 5919526508 DUCT DOUG DC9 DC931 3022065 WP L/E SLAT BINDING A NWAA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 1309T 47316 DURING APPROACH FOR LANDING WHEN SLATS EXTENDED, THE SLAT DISAGREEMENT LIGHT ILLUMINATED AND THE AIRCRAFT ROLLED. FOLLO WED COM PROCEDURES AND THE FLIGHT ATTENDANT VERIFIED THE RIGHT SLAT DID NOT DEPLOY. FLAP ONLY LANDING AT MSP WAS UNEVEN TFUL. MAINTENANCE DISCOVERED THAT THE SLAT WOULD NOT FALL OUT OF RIGHT WING AND IT APPEARED TO BE HANGING UP ON THE T-D UCT. REPLACED THE RIGHT T-DUCT AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002051300091 20020513 00091 WP 2002 5 13 0201409754 1 20020408 A 3510 15830AB HOSE DOUG DC9 DC941 302207N WP COCKPIT NOT SEATED A NWAA B EMER. DESCENT O OTHER DE DESCENT 1 GL 01 754NW 47178 WHILE CRUISING AT ALTITUDE, THE AIRCRAFT HAD A LOSS OF PRESSURIZATION AND INITIATED AN EMERGENCY DESCENT TO 10,000 FEET. DURING DESCENT, COM REQUIRED THE CREW TO BE ON OXYGEN. THE CAPTAIN'S MASK WOULD NOT SUPPLY OXYGEN DURING THE EMERGENC Y DESCENT. THE TEST FEATURE WAS ALSO INOPERATIVE. THE MASK DID FUNCTION NORMALLY AFTER THE AIRCRAFT RECOVERED FROM THE DESCENT AND CONTINUED TO UNTIL LANDING. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT AT DFW WHERE MAINTENANCE RESEATED T HE OXYGEN SUPPLY HOSE TO THE CAPTAIN'S MASK. FUNCTIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002052900030 20020529 00030 NM 2002 5 29 0201413137 1 20020504 A 2761 PIN AIRBUS A319 A319114 3930350 NM SPOILER ACTUATOR MISSING A NWAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 01 337NB 01685 PILOT REPORTED LOSS OF HYDRAULIC FLUID IN THE GREEN HYDRAULIC SYSTEM DURING CLIMBOUT. SWITCHED POWER TRANSFER UNIT TO O FF AND GREEN SYSTEM ENGINE 1 PUMP TO OFF. COMPLETED GRAVITY GEAR EXTENSION AND LANDED IN MSP UNEVENTFULLY. FOUND OUTBO ARD SWIVEL GLAND IN RIGHT WING NR 5 SPOILER ACTUATOR LEAKING DUE TO RETAINING PIN MISSING. REPLACED THE ACTUATOR 32-276 0-9-0002. RETURNED LANDING GEAR EXTENSION SYSTEM TO NORMAL MODE AFTER GRAVITY EXTENSION. LEAK AND OPERATIONAL CHECK GO OD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002051300093 20020513 00093 2002 5 13 0201423204 4 20020504 A 3441 PG1152AC03 MODULE AIRBUS 320 A320211 3930320 EU COCKPIT FAULTY A NWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 01 304US 5039 5039 00040 DURING TAKEOFF ROLL, THE FIRST OFFICER'S AIRSPEED INDICATION NEVER EXCEEDED 45 KNOTS. ABORTED TAKEOFF AT 105 KNOTS. RE PLACED THE LEFT NR 1 AIR DATA MODULE AND NR 2 AIR DATA INERTIAL REFERENCE UNIT. LEAK AND FUNCTIONAL CHECK OF ALTITUDE, AIRSPEED AND AIR DATA SYSTEM OK. AFS AND LAND III TEST OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002051300094 20020513 00094 2002 5 13 0201433224 4 20020505 A 3441 PG1152AC03 MODULE AIRBUS 320 A320211 3930320 EU COCKPIT FAULTY A NWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 01 324US 33308 33308 00273 CAPTAIN'S AIRSPEED INDICATION WAS AT 40 KNOTS WHEN THE FIRST OFFICER'S WAS 80 KNOTS. ABORTED TAKEOFF AT 105 KNOTS AND T AXIED TO GATE. CLEARED CAPTAIN'S PITOT LINE. REPLACED NR 1 PITOT PROBE, LEFT AIR DATA MODULE, AND NR 1 AIR DATA INERTI AL REFERENCE UNIT. LEAK AND FUNCTIONAL TEST OF ALTITUDE, AIRSPEED, AND AIR DATA SYSTEM CHECKED OK. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F RT A28NM 2002051700059 20020517 00059 WP 2002 5 17 CALA2000274 1 20020511 A 5320 2932222 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 CENTER FLOOR PANEL SUPPORT AT STA 218, RBL 3 IS CORRODED. REPLACED SUPPORT IAW SRM 51-10-02. 2 L 7 2 4F A6WE 2002051700061 20020517 00061 WP 2002 5 17 CALA2000276 1 20020511 A 5320 3932140 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 FWD ENTRY CENTER FLOOR PANEL SCF01 H RT SIDE SUPPORT IS CORRODED 40 INCHES, STA 148-200. INSTALLED REPLACEMENT FLOOR SU PPORT IAW SRM 51-40-00. 2 L 7 2 4F A6WE 2002051700062 20020517 00062 WP 2002 5 17 CALA2000277 1 20020511 A 5320 3932140 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 FWD ENTRY CENTER FLOOR PANEL SCF01 H LT SIDE SUPPORT IS CORRODED FROM STA 160-200. REPLACED FLOOR SUPPORT IAW SRM 51-40 -00. 2 L 7 2 4F A6WE 2002051700064 20020517 00064 WP 2002 5 17 CALA2000279 1 20020511 A 5260 39366777 ACTUATOR DOUG DC9 DC982 3022082 WP VENTRAL STAIRS CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 AFT VENTRAL STAIRS ACTUATOR LOWER TUBE, RT, IS CORRODED 2 INCHES. REPLACED RT LOWER STRUT ON VENTRAL STAIRS AND PERFORM ED ADJUSTMENT AND TEST IAW MM 52-63-00. 2 L 7 2 4F A6WE 2002051700065 20020517 00065 WP 2002 5 17 CALA2000280 1 20020512 A 5347 95301157003 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 RIGHT O/B SEAT TRACK PITTED UNDER G-2 GALLEY AT APPROXIMATELY STA 208. REPLACED O/B SECTION OF SEAT TRACK IAW SRM 53-05 , FIG 4F. 2 L 7 2 4F A6WE 2002051700066 20020517 00066 WP 2002 5 17 CALA2000281 1 20020513 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 TAIL COMPARTMENT STA 1418 AT LONGERON 15R FRAME HAS DEEP CHAFE. INSTALLED REPAIR AND SHIMS IAW SRM 51-30-2, 51-30-5, 53 -03, FIG 4. 2 L 7 2 4F A6WE 2002051700067 20020517 00067 WP 2002 5 17 CALA2000282 1 20020513 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 MID CARGO DOOR, OUTER SKIN HAS A SHARP DENT. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-2, 52-05, FIG 1. 2 L 7 2 4F A6WE 2002051300095 20020513 00095 WP 2002 5 13 CALA2000283 1 20020513 A 5330 SKIN DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 SKIN DAMAGED AFT OF PITOT TUBE AT STA 76 R/S FWD OF COCKPIT WINDOW 3"X4". INSTALLED CLASS II REPAIR IAW SRM 53-04 FIG 1 2B. 2 L 7 2 4F A6WE 2002051300096 20020513 00096 NM 2002 5 13 0201442288 1 20020504 A 2910 HYDRAULIC LINE BOEING 727 727251 138408H NM HYD SYSTEM FAILED A NWAA K NONE K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 01 288US 21376 APPROACHING TOP OF DESCENT INTO DTW, BOTH -B- PUMP LOW PRESSURE LIGHTS ILLUMINATED. -A- SYSTEM SHOWED 2.5 GALLONS, -B- SYSTEM QUANTITY SHOWED 1.7 GALLONS. -B- SYSTEM PRESSURE FELL TO ZERO AFTER SOME FLUCTUATIONS. COMPLIED WITH COM PROCE DURE FOR FLUID LOSS AND DECLARED AN EMERGENCY. FLIGHT MADE AN UNEVENTFUL LANDING IN DTW. DTW MAINTENANCE FOUND -B- PUM P PRESSURE LINE HAD FAILED AND REPLACED SAME. REPLACED NR 2 -B- PUMP AND SERVICED. ALL LEAK AND OPERATIONAL CHECKS OK. 2 L 7 3 4F A3WE 2002051300098 20020513 00098 NM 2002 5 13 0201456305 1 20020501 A 2120 ODOR BOEING 747 747451 1384940 NM CABIN DETECTED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 666US 23821 DURING CRUISE, AN INTENSE BURNING SMELL EMITTED IN THE AREA OF DOOR 5L. TURNED OFF RECIRCULATION FANS AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. VISUALLY INSPECTED AREA WITH NO DEFECTS NOTED. 2 L 7 4 4F RT A20WE 2002051300099 20020513 00099 NE 2002 5 13 0201461244 2 20020506 A 7200 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 MAKING METAL A NWAA J A DUMP FUEL UNSCHED LANDING R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CL CLIMB 1 GL 01 244NW 48316 517844 DURING CLIMB AT 10,000 FEET, NR 3 ENGINE COMPRESSOR STALLED AND FLAMED OUT. FLIGHT CREW DID NOT ATTEMPT ENGINE RESTART. APPROXIMATELY 65,000 LBS OF FUEL WAS DUMPED. FLIGHT CREW RETURNED TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LA NDING. MAINTENANCE FOUND METAL IN THE TAILPIPE. REPLACED THE NR 3 ENGINE. 2 L 7 3 4F 4 F A22WE E23EA 2002051300100 20020513 00100 NE 2002 5 13 0201471242 2 20020429 A 7200 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 FLAMED OUT A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 GL 01 242NW 47845 455283 DURING CRUISE FLIGHT AT 36,000 FEET THE NR 3 ENGINE ROLLED BACK APPROXIMATELY 20 PERCENT. THRUST LEVER INPUT HAD NO EFF ECT ON ENGINE RPM AND 30 SECONDS AFTER INITIAL ROLLBACK THE NR 3 ENGINE FLAMED OUT. FLIGHT CREW WAS UNABLE TO RESTART T HE NR 3 ENGINE. FLIGHT CREW RETURNED TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE REPLACED TH E NR 3 ENGINE. 2 L 7 3 4F 4 F A22WE E23EA 2002051300101 20020513 00101 2002 5 13 02051001 4 20020509 A 3442 RADAR BOEING 757 75728A 1384976 NM COCKPIT FAILED A N8TA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 523NA 30043 RADAR FAILED DURING CLIMB. MSG RT AND WINDSHEAR SYS, ALSO STATUS MSG WXR SYS CYCLED C/B'S, UNABLE TO RESET. AIRCRAFT R ETURNED TO BASE, AN UNEVENTFUL LANDING WAS ACCOMPLISHED. 2 L 7 2 4F RT A2NM 2002051300102 20020513 00102 NE 2002 5 13 02126429 2 20020506 A 7200 ENGINE DORNER DO32 DO328300 NM PWA 306 PW306B NE RIGHT VIBRATION A VTZA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 27 429FJ DURING CRUISE FROM BOS TO CAE CREW EXPERIENCED EXCESSIVE RT ENGINE VIBRATION. AN EMERGENCY WAS DECLARED WITH ATC AND FL IGHT DIVERTED TO IAD. FLIGHT LANDED IN IAD WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACE RT ENGI NE, MAF FLIGHT WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 F RT A55NM E35NE 2002051300104 20020513 00104 EU 2002 5 13 02127305 1 20020507 A 3350 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY EXIT OUT OF ADJUST A VTZA K NONE O OTHER AP APPROACH 1 EA 27 305UE 305UE EMERGENCY EXIT LIGHT ILLUMINATED ON SHORT FINAL. MAINTENANCE ADJUSTED EMERGENCY DOOR MICROSWITCH. OP'S CHECK OK. 2 L 7 2 4T RT A41NM 2002051300106 20020513 00106 2002 5 13 249TR0004 4 20020505 A 2210 AUTOPILOT SYS BOEING 737 7372K5 138448X NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 249TR 22598 Auto pilot in B mode shakes aircraft while engaged. Bite ck OK. 2 L 7 2 4F RT A16WE 2002051300111 20020513 00111 2002 5 13 PCAA0205056 4 20020512 A 2297 82210040001 CIRCUIT CARD DHAV DHC8 DHC8102 2809003 NM COCKPIT BURNED A PCAA K NONE A FLAME/FIRE LD LANDING 1 EA 13 820EX 019 FLIGHT# 3581 BUF-BDL. CREW REPORTED FIRE AND SMOKE FROM FLIGHT TAXI SWITCH. MAINTENANCE FOUND AUTOPILOT DISENGAGE CIRCUI T CARD BURNT DUE TO FAULTY RESISTOR. AUTOPILOT DISCONNECT CIRCUIT BOARD REPLACED. OPERATIONAL CHECK GOOD. WIRING IN SURR OUNDING AREA INSPECTED. NO DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002051300112 20020513 00112 NM 2002 5 13 SABA020059 1 20020513 A 3350 1306 BULB DHAV DHC8 DHC8102 2809003 NM CABIN BURNED OUT A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 Aircraft 883 on flight 5190 from AGS to CLT. during turn-around inspection after arrival in CLT a bulb in the floor eme rgency lights would not test. Maintenance removed and replaced the bulb. Ops check was good. Aircraft returned to ser vice. 2 H 7 2 4T RT A13NM 2002051300113 20020513 00113 WP 2002 5 13 ZW0A02049101 1 20020511 A 4920 5910050 APU DOUG DC9 DC982 3022082 WP A ZW0A K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 13 956U 49701 BURNING SMELL IN CABIN DURING CRUISE CAUSED BY INGESTION OF SKYDROL INTO APU. REMOVED AND REPLACED APU. LAST CHECK C PER FORMED IN STL 09/08/01 -- CLOSED-- 2 L 7 2 4F A6WE 2002051300114 20020513 00114 NM 2002 5 13 02051301 1 20020510 A 2612 2156204A SMOKE DETECTOR BOEING 757 75728A 1384976 NM AFT CARGO COMP. A N8TA F ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 WP 19 517NA 24260 At FL350, Aft Cargo Fire Light illuminated, first fire extinguisher discharged, light extinguished, on approach second f ire extinguisher was discharged. Investigation revealed No sign of Heat or Fire; Light bulbs in smoke detectors burnt ou t. re-lamped smoke detectors, system checks ok per M/M 26-23-00 Investigation ongoing. 2 L 7 2 4F RT A2NM 2002051300115 20020513 00115 NM 2002 5 13 02051302 1 20020511 A 3350 LAMP BRUCE BOEING 757 75728A 1384976 NM FWD CABIN ROW 8 BURNED OUT A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 523NA 30043 Aft Red Emergency light, for seat 8ABC INOP. Re-lamped light at 8ABC per M/M 33-13-00; Ops Check Good. 2 L 7 2 4F RT A2NM 2002051300116 20020513 00116 NM 2002 5 13 QXEA0200798 1 20020512 A 2420 DH103024600CS INVERTER DHAV DHC8 DHC8202 2809007 NM COCKPIT DEFECTIVE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 350PH 11403 488 SEA-STRONG ODOR IN COCKPIT. REMOVED AND REPLACED INVERTER. C/W QX MTC 9340002 HGS SYSTEM RTS TEST. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002051300117 20020513 00117 EU 2002 5 13 02129303 1 20020509 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 303UE EMERGENCY FLOOR LIGHTING INOP BETWEEN ROWS 8-10. RECONNECTED FLOOR TRACK LIGHTING CONNECTOR. OP'S CHECKED OK. 2 L 7 2 4T RT A41NM 2002062500136 20020625 00136 NM 2002 6 25 UPS02438211 1 20020513 A 5347 SEAT TRACK BOEING 747 747256B 1384865 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 528UP 24071 INSPECTION TYPE:N/A F/O SEAT TRACK IS CRACKED AND BENT IN TWO PLACES. REMOVED AND REPLACED F/O RT SEAT TRACK, OPS CHECK S GOOD IAW MM 25-11-01. 2 L 7 4 4F RT A20WE 2002051300118 20020513 00118 EA 2002 5 13 COMA0260305 1 20020509 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA L/H CRACKED A COMA O OTHER O OTHER DE DESCENT 1 SO 01 779CA 6845 7306 FLIGHT 5728 PILOTS WINDSHIELD CRACKED.REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2002051300119 20020513 00119 EA 2002 5 13 COMA0260306 1 20020508 A 2710 600911775 BELLCRANK CNDAIR CL600 CL6002B19 1900309 EA WING CENTER DIRTY A COMA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 01 937CA 7044 FLIGHT 5296 AILERON CONTROLS LOCKED UP, MINIMUM CONTROL AVIABLE. COULD NOT DUPLICATE PROBLEM ON GROUND - BOTH THE LT AN D RT AILERON AFT CONTROL CABLE QUADRANTS WERE REPLACED AS THE MOST PROBABLE CAUSE OF DISCREPANCY. 2 L 7 2 4F RT A21EA 2002051300120 20020513 00120 EA 2002 5 13 COMA0260307 1 20020508 A 2710 600911775 BELLCRANK CNDAIR CL600 CL6002B19 1900309 EA WING CENTER DIRTY A COMA B EMER. DESCENT F FLT CONT AFFECTED CR CRUISE 1 SO 01 977CA 7157 FLIGHT 5261 - A/P TRIM LWD CAUTION MESSAGE. AILERON CONTROLS LOCKED UP.COULD NOT DUPLICATE PROBLEM ON GROUND - AILERON A FT BELLCRANK ASSY WERE DETERMINED TO BE MOST PROBABLE CAUSE AND WERE REPLACED. 2 L 7 2 4F RT A21EA 2002051300121 20020513 00121 EA 2002 5 13 COMA0260308 1 20020508 A 2710 600911775 BELLCRANK CNDAIR CL600 CL6002B19 1900309 EA WING CENTER DIRTY A COMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 709CA 7238 FLIGHT 5883 A/P TRIM LWD CAUTION MESSAGE. AILERONS VERY STIFF.COULD NOT DUPLICATE PROBLEM ON GROUND - AILERON AFT BELLCR ANK ASSY WERE DETERMINED TO BE MOST PROBABLE CAUSE AND WERE REPLACED. 2 L 7 2 4F RT A21EA 2002051300123 20020513 00123 2002 5 13 N249TR0004 4 20020505 A 2210 AUTOPILOT SYS BOEING 737 7372K5 138448X NM A PIDA K NONE O OTHER AP APPROACH 1 SO 05 249TR 22598 Capt. Flt director during App. while on "B" channel turns itself off. Bite test OK. 2 L 7 2 4F RT A16WE 2002051300124 20020513 00124 2002 5 13 N249TR0005 4 20020505 A 2210 AUTOPILOT SYS BOEING 737 7372K5 138448X NM A PIDA K NONE O OTHER AP APPROACH 1 SO 05 249TR 22598 Capt. Flt director during App. while on "B" channel turns itself off. Bite test OK. 2 L 7 2 4F RT A16WE 2002051300125 20020513 00125 NM 2002 5 13 N371PA0005 1 20020508 A 3350 58674 INVERTER BOEING 737 737306 NM A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 371PA 23543 Aft floor emergency exit pros. lights Inop. R & R inverter. Ops check OK 2 L 7 2 4F RT A16NE 2002051300126 20020513 00126 2002 5 13 N250TR0003 4 20020505 A 2230 AUTOTHRUST SYS BOEING 737 7372K5 138448X NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 250TR 22597 Auto Throttles Inop. 2 L 7 2 4F RT A16WE 2002051300127 20020513 00127 NM 2002 5 13 AWXA200200416 1 20020511 A 3350 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM SEAT ROW 5 L/H SHORTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 0 0 23778 LAS - EEL - EMERGENCY ESCAPE PATH LIGHTING IS DIM AND INOPERATIVE AT SEAT ROWS 5-9. MAINTENANCE REPLACED THE EMERGENCY LIGHTING BATTERY PACK IN OVERHEAD PANEL 10 L/H PER T/C A1C33005, AND REPLACED THE BATTERY CHARGER IAW BMM 33-51-51-962-0 16. MAINTENANCE ALSO REPAIRED A SHORTED WIRE FOUND AT SEAT ROW 5 L/H. EMERGENCY ESCAPE PATH LIGHTING SYSTEM OPERATIONALL Y CHECKED GOOD. PART NAME: BATTERY CHARGER, MFG; RADIANT ILLUMINATION, P/N; 2012-1 LOC; ZONE 107. PART NAME; BATTERY, M FG; RADIANT ILLUMINATION, P/N; 2013-1A, LOC; ZONE 107, COND; LOW VOLTAGE. 2 L 7 2 4F RT A16WE 2002051300128 20020513 00128 NM 2002 5 13 AWXA200200417 1 20020423 A 5330 6552988 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 0 0 23780 MCN - MAJOR REPAIR - DURING C-16 CHECK HFEC INSPECTION FOUND A CRACK AT THE L2 DOOR UPPER HINGE CUTOUT BS 948.5. MAINTEN ANCE REMOVED DAMAGED AREA OF INNER WEB AT FWD SIDE OF L2 DOOR BS 948, FABRICATED 2 EA. FILLERS AND 1 EA. REPAIR DOUBLER, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01, PG. 210-212. 2 L 7 2 4F RT A16WE 2002051300129 20020513 00129 NM 2002 5 13 AWXA200200418 1 20020507 A 5313 6545767512 STRINGER BOEING 737 7373Q8 1384670 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 0 0 23507 MCN - MAJOR REPAIR - DURING C-15 CHECK A CRACK WAS FOUND ON STRINGER 16 R/H JUST AFT OF OVERWING LIGHT AT BS 500C+16. MA INTENANCE CUTOUT THE DAMAGED AREA OF STRINGER 16 R/H, AT BS 500C+16, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR CHANNEL, FILLER, AND RADIUS FILLER, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2002051300130 20020513 00130 NM 2002 5 13 AWXA200200419 1 20020507 A 5313 66235744 CLIP BOEING 737 7373Q8 1384670 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 0 0 23507 MCN - MAJOR REPAIR - DURING C-15 CHECK A CRACK WAS FOUND ON STRINGER CLIP ON THE AFT SIDE OF FRAME AT BS 706, STR 12 R/H . MAINTENANCE REMOVED AND REPLACED CLIP AT BS 706, STR 12 R/H IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002051300131 20020513 00131 NM 2002 5 13 AWXA200200421 1 20020510 A 3350 210013 SWITCH BOEING 757 7572G7 1384963 NM BS 1638 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 0 0 24233 GYR - EEL - DURING C-11 CHECK THE L4 DOOR EMERGENCY LIGHTING TEST SWITCH WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLA CED THE EMERGENCY LIGHT TEST SWITCH AT THE L4 DOOR IAW WDM 33-51-15, PG . 1. EMERGENCY LIGHT TEST WAS GOOD IAW BMM 33-51 -00, PG. 502. 2 L 7 2 4F RT A2NM 2002051400022 20020514 00022 EA 2002 5 14 CA020502024 1 20020426 A 2820 CC670622471 LINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE FUEL SYSTEM BROKEN W O OTHER J WARNING INDICATION DE DESCENT 1 CA (CAN) CREW EXPERIENCED A RT MAIN EJECTOR (C) MESSAGE AT 22,000 FEET DESCENDING. THEY REPORTED THE CENTRE TANK WAS AT 80 LBS AND IT INCREASED TO 220 LBS, THEN DECREASING TO 70 LBS PRIOR TO LANDING. BOTH BOOST PUMPS WERE OPERATING AT ALL TIM ES.MAINTENANCE FOUND THE R PRIMARY EJECTOR SWITCH SENSE LINE WAS BROKEN AT THE "B" NUT (LINE BROKE INSIDE FERRULE). THE AFFECTED LINE WAS REPLACED.AIRCRAFT BACK IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002051400029 20020514 00029 NM 2002 5 14 S02271013 1 20020508 A 7920 LINE BOEING 747 747209B NM PWA JT9 JT9D7R4G2 52054 NE NR 4 ENGINE LEAKING W SAJF O OTHER M J OVER TEMP WARNING INDICATION DE DESCENT 1 WP 03 22299 B18752 AFT 2 & 1/2 HRS FLT, NR 4 ENG OIL PRESSURE WARNING LT ILLUMINATED WITH OIL PRESSURE INDICATION AT 30 PSI, OIL QTY INDICATION 1/2. AFTER CHANGING THRUST SETTING, OIL PRESSURE INDICATION CONTINUOUSLY DECREASE TO 20 PSI, OIL QTY GRADUA LLY DECREASE TO 1/16, OIL TEMP INCREASE TO 110 DEGREE C. BEFORE DESCENT, RECYCLE OIL QTY & PRESSURE C/BS, OIL PRESSURE D ECREASE TO "0" PSI UNTIL LANDING. TOTAL AROUND 30 MINS. C/A:GRD INSP ON NR 4 ENGINE FOUND ONE TUBE OF OIL PRESSURE TRAN SMITTER BROKEN, IAW MM 72-00-00 CONFIG 3 P682H(4) IF OIL PRESSURE WAS SHUT OFF OR INTERRUPTED FOR MORE THAN 10 SECONDS A T RPM IN EXCESS OF WINDMILL RPM. ENG MUST BE REMOVED FOR BEARING INSP. 2 L 7 4 4F 4 F RT A20WE E3NE 2002051400034 20020514 00034 CE 2002 5 14 2002F00458 1 20020509 A 3260 S21121 DOWNLOCK SWITCH CESSNA 340 340A 2076405 CE MLG BROKEN B BIGA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 04 118BH 340A0003 LT MLG DOWN LIGHT FAILED TO ILLUMINATE ON APPROACH. EMERGENCY GEAR SYSTEM ACTIVATED. AIRCRAFT LANDED SAFELY AT MAIN BA SE. FOUND LT MLG DOWNLOCK SWITCH ACTUATOR BROKEN. 1 L 7 2 3O 3A25 2002051400035 20020514 00035 SW 2002 5 14 2002F00459 1 20020509 A 6720 HOUSING BELL 206 206L1 1182107 SW ALLSN 250C 250C30 03013 GL PITCHCHANGE LINK CRACKED G UP8A K NONE O OTHER IN INSP/MAINT 1 SW 09 10814 45415 CAE897508 DURING INSPECTION FOUND TAIL ROTOR PITCH CHANGE LINK OUTBOARD BEARING HOUSING CRACKED. CRACK PROPAGATED FROM ROLL STAKE AREA OF ONE SIDE OF BEARING THROUGH OUTBOARD END OF PITCH CHANGE LINK TO THE OTHER SIDE AT OPPOSITE ROLL STAKE AREA. S USPECTED CAUSES ARE BEARING BORE LINE REAM FRACTIONALLY TOO SMALL AND/OR CORROSION IN AREA OF ROLL STAKE. 1 G 7 1 3U 3 U H2SW E1GL 2002051400043 20020514 00043 EA 2002 5 14 ASO2002F00002 1 20020421 A 5300 BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE SUPPORT BEAM CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 850AS 7355 DURING (C) CHECK, INSPECTION WHILE COMPLYING WITH VISUAL INSPECTION OF THE ENGINE SUPPORT BEAMS, THE LEFT SIDE WAS FOUN D TO HAVE A CRACK. MAINTENANCE PERFORMED A TEMPORARY REPAIR. THIS REPAIR IS VALID FOR UP TO ONE YEAR FROM DATE OF INCO RPORATION. 2 L 7 2 4F 4 F RT A21EA E15NE 2002053100117 20020531 00117 NM 2002 5 31 02FDEA00321 1 20020509 A 5314 KEELBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CORROSION ON KEEL BEAM AT BS 950E+9, WL 139, LBL 6. 2 L 7 3 4F RT A3WE 2002061900191 20020619 00191 NM 2002 6 19 02FDEA00322 1 20020509 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 HOLES IN FRAME AT BS 870, STR 9 RT. REMOVED AND REPLACED FRAME PER EA 7-5310-64105. 2 L 7 3 4F RT A3WE 2002051400050 20020514 00050 2002 5 14 2002F00472 4 20020502 A 2564 7435PS8 ASPIRATOR BOEING 737 73783N 13844HI NM LIFE RAFT FAILED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 20068 TL476 30640 DURING PARTIAL DITCH DEMONSTRATION A 46 MAN LIFE RAFT WAS ACCIDENTLY DEPLOYED. BOTH RINGS ON THE RAFT INFLATED AND THEN THE BOTTOM RING DEFLATED. UPON INSPECTION THE ASPIRATOR FOR THE BOTTOM RING WAS FOUND TO BE PARTIALLY OPEN. THE RAFT HAD BEEN OVERHAULED ON 03/02. 2 L 7 2 4F RT A16WE 2002051400051 20020514 00051 WP 2002 5 14 2002F00473 1 20020503 A 3240 M835369024 RELAY LKHEED 1011 10113853 5265020 WP BRAKE SYSTEM FAULTY G AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 164AT 59588 59588 293A1238 FLIGHT NUMBER 5028, DURING TAXI WITH HYDRAULIC SYSTEM-B OFF, BRAKE PRESSURE DROPS RAPIDLY WHEN BRAKES APPLIED. MAINTENA NCE REMOVED AND REPLACED NORMAL RELAY NR 1 3343-K3 PER FIM 32-48-00, FIG 103, BLOCK 12 AND MM 32-40-02. PRESSURE DECAY WITHIN LIMITS PER MM 32-48-00, FIG 4. 2 L 7 3 4F A23WE 2002051400054 20020514 00054 WP 2002 5 14 UPS02837886 1 20020220 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED O/B OF L34R AT STA 1180. REMOVED CRACK Z-FITTING, LOCATED AND DRILL ED NEW FITTING AND SPLICES IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 53-2-0 AND 51-120D. 2 L 7 4 4F RT 4A25 2002051400055 20020514 00055 WP 2002 5 14 UPS02837887 1 20020221 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C23 L2 DOOR CORNER UPPER AFT SHOWS CRACK INDICATION IN REPAIR AREA GOING TO FASTENER HOLE. REMOVED EXIS TING DOUBLERS, ROUTED OUT CRACK, FABBED AND INSTALLED REPAIR DOUBLERS IAW DC8 SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2002051400056 20020514 00056 WP 2002 5 14 UPS02837888 1 20020221 A 5512 SKIN PANEL DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C23 LT HORIZONTAL STAB UPPER O/B FWD SKIN PANEL CRACKED AT 2ND BOLT IN AFT DIRECTION. REMOVED AND REPLA CED HORIZ STAB PLANK IAW DAC SB55-16 AND DAC DWG SRO 8 550001. 2 L 7 4 4F RT 4A25 2002051400057 20020514 00057 WP 2002 5 14 UPS02837889 1 20020228 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C23 AFT PIT FS 1200 ZEE FITTING AT L34R - L33R IS CORRODED. REMOVED CORRODED ANGLE LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED ZEE FITTING REPAIR ANGLE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002051400058 20020514 00058 WP 2002 5 14 UPS02837891 1 20020223 A 5330 SN08530001 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C L1 DOOR UPPER FWD CORNER, AND UPPER AFT CORNER REPAIRS DO NOT CONFORM TO EO DC8-5330-12073F. REPAIRED PER UPS EO DC8-5330-16381-A, DHSK707-694. 2 L 7 4 4F RT 4A25 2002051400059 20020514 00059 WP 2002 5 14 UPS02837892 1 20020218 A 5330 5779936 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C REMOVE STEEL DOUBLER AT L2 DOOR, LWR FWD CORNER & INSTALL APPROVED REPAIR PER SRM. REPAIRED PER UPS E O DC8-5330-16382-A. 2 L 7 4 4F RT 4A25 2002051400060 20020514 00060 WP 2002 5 14 UPS02837893 1 20020221 A 5320 J0602969 WEB DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C LT CUSP REPAIR DOES NOT CONFORM TO SRM AT LT STA 1328. REMOVED AND REPLACED LT CUSP EXTRUSION FROM ST A 1190 TO STA 1370 PER SRM 53-2-5 FIG 15. 2 L 7 4 4F RT 4A25 2002051400061 20020514 00061 WP 2002 5 14 UPS02837895 1 20020306 A 5320 47732951N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 MAIN CARGO DOOR JAMB NR 7 LATCH SPOOL FITTING HAS LOWER JAMB FITTINGS FWD AND AFT OF LATCH SPOOL FITT ING HAVE INTERGRANULAR CORROSION AT STA 280 LONG 21L. REMOVED AND REPLACED FITTINGS IAW DWG 4773295 AND SRM 51-3-0, 51- 1-20D. 2 L 7 4 4F RT 4A25 2002051400062 20020514 00062 WP 2002 5 14 UPS02837896 1 20020308 A 5320 3755841501N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 STA 1200 BATHTUB FITTING IS CRACKED BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 37558 41 AND SRM 51-1-20D, 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002051400063 20020514 00063 WP 2002 5 14 UPS02837897 1 20020308 A 5320 3755843501N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 STA 1220 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 37558 43 AND SRM 53-2-0 FIG 2D, 51-1-20D. 2 L 7 4 4F RT 4A25 2002051400064 20020514 00064 WP 2002 5 14 UPS02837899 1 20020306 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 REPAIR AT STA 1440, UPPER AFT CORNER D-PIT DOOR IS A CATEGORY D PER EO DC8-5330-12800, AND SKIN IS CR ACKED AT LONG 22R APPROX. REMOVED EXISTING REPAIR, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS. AT CUTOUT, FABRICATED AND INSTALLED DOUBLER TRIPLER AND FILLER IAW SRM 53-2-0 FIG 21. 2 L 7 4 4F RT 4A25 2002051400066 20020514 00066 WP 2002 5 14 UPS02837900 1 20020306 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 L-1 LOWER AFT CORNER DOUBLER AND TRIPLER DOES NOT CONFORM TO SRM 53 -2-0 FIG 15 AND SRO8530021, AND S KIN IS CRACKED AT STA 60 BETWEEN LONG 20L AND 21L. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED A ND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15. 2 L 7 4 4F RT 4A25 2002051400067 20020514 00067 WP 2002 5 14 UPS02837901 1 20020303 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 LT WING T/E UPPER RIB IS CRACKED AT XRS 247. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABR ICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002051400068 20020514 00068 WP 2002 5 14 UPS02837902 1 20020301 A 5730 DOUBLER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C23 MOULD-LINE DOUBLER AT NR 1 PYLON HAS PREVIOUSLY INSTALLED REPAIR DOUBLER ON THE I/B SIDE THATS CRACK ED AT FASTENER HOLE. REMOVED DOUBLER, PERFORMED HFEC AND BOLT HAVE HFEC IAW NDT SPM 06-10.001 AND 06-10.003. CRACKS PR ESENT IN 5 EA HOLES, FABBED REPAIR BUSHINGS IAW REO G08542. INSTALLED BUSHINGS IAW REO G08542 & DC8 SRM 51-1-25. FABBE D WASHER, INSTALLED RIVET THROUGH BUSHING & WASHER IAW REO G08542 & SRM 51-1-21. PERFORMED HFEC, NO CRACKS NOTED. 2 L 7 4 4F RT 4A25 2002051400069 20020514 00069 WP 2002 5 14 UPS02837903 1 20020319 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:N/A CREW REPORTED EMERGENCY EXIT LIGHT INOP. RELAMPED BULB TO EMERGENCY EXIT LIGHT, OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2002051400070 20020514 00070 WP 2002 5 14 UPS02837904 1 20020306 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 L2 DOOR JAMB LOWER FWD CORNER SKIN IS CRACKED BETWEEN LONG 20L AND 21L STA 1620. CUT OUT CRACKED ARE A, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2002051400071 20020514 00071 WP 2002 5 14 UPS02837905 1 20020305 A 5320 47516431 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 STA 822 LONG 12R FRAME FITTING IS CRACKED AT EMERGENCY EXIT FRAME, AFT FITTING. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4751643 AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2002051400072 20020514 00072 WP 2002 5 14 UPS02837906 1 20020304 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 FUSELAGE SKIN CRACKED AT L-1 DOOR FWD UPPER CORNER STA 25 BETWEEN LONG 10L-11L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15. 2 L 7 4 4F RT 4A25 2002051400073 20020514 00073 WP 2002 5 14 UPS02837907 1 20020301 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 FUSELAGE SKIN IS CRACKED AT L-2 DOOR LOWER AFT CORNER STA 1660 BETWEEN LONG 20L-21L. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2002051400074 20020514 00074 WP 2002 5 14 UPS02837908 1 20020308 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 STA 1650 LONG 35L LONGERON AND END FITTINGS ARE CORRODED BEYOND LIMITS. REMOVED END FITTINGS, AND LO NG 35L BETWEEN STA 1650-1680, FABRICATED AND REPLACED LONGERON SECTION AND END FITTINGS IAW DWG 3647110, AND SRM 51-1-20 D, 51-3-0. 2 L 7 4 4F RT 4A25 2002051400075 20020514 00075 WP 2002 5 14 UPS02837909 1 20020304 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 822.5. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATE D. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002051400076 20020514 00076 WP 2002 5 14 UPS02837911 1 20020307 A 5320 5616306171 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 STA 960 T-FITTING BETWEEN MAIN LANDING GEAR DOORS IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5 616306, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002051400077 20020514 00077 WP 2002 5 14 UPS02837912 1 20020321 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CARGO BAY CONTAMINATED A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 852UP 46052 INSPECTION TYPE:N/A LOWER CARGO SMOKE LIGHT ILLUMINATED ON TAKEOFF. WARNING INDICATED SECTION C. AIR TURNBACK. INSPEC TED PIT 33 DETECTORS, FOUND WATER INTRUSION ON ALL DETECTOR UNITS. DRIED ALL DETECTORS AND DEFERRED SYSTEM. OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2002051400078 20020514 00078 WP 2002 5 14 UPS02837914 1 20020306 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 LT MID GALLEY DOOR LOWER FWD CORNER CUTOUT SKIN IS CRACKED AT STA 1306 BETWEEN LONG 20L AND 21L. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2- 0 FIG 15A. 2 L 7 4 4F RT 4A25 2002051400079 20020514 00079 WP 2002 5 14 UPS02837915 1 20020304 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 R-2 DOOR UPPER AFT CORNER FUSELAGE SKIN, INTERNAL DOUBLER, AND LONG 11R ARE CRACKED AT STA 1654 AND L ONG 11R. CUT OUT CRACKED AREA ON SKIN AND INTERNAL DOUBLER, STOPDRILLED CRACK ON LONG 11R. NDT VERIFIED NO CRACKS AT S TOPDRILL AND CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, FILLER, AND STRAP IAW DC8-5330-16410-A, AND 8110-3 APPR OVED DH SK 706-504. 2 L 7 4 4F RT 4A25 2002061000054 20020610 00054 EU 2002 6 10 AWXA200200404 1 20020504 A 2133 VFT300B00 VALVE AIRBUS 320 A320231 3930325 EU CABIN PRESSURE MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 631AW 236 077 LAX - AIR TURNBACK - FLT 0315 - AFTER TAKEOFF FROM LAX EN ROUTE TO PHX RECEIVED VENT SKIN VALVE AND VENT AVIONICS SYSTEM FAULT ON ECAM, NO CABIN PRESSURE, TURNED BACK TO LAX. MAINTENANCE AT LAX ISSUED MEL 21-26-04, COND. NR 1 (EXTRACT VAL VE INOPERATIVE); THIS MEL DEACTIVATES THE MAIN FLAP IN THE CLOSED POSITION AND THE INTERNAL FLAP IN THE OPEN POSITION AL LOWING THE AIRCRAFT TO PRESSURIZE. AIRCRAFT CONTINUED TO PHX. MAINTENANCE REMOVED AND REPLACED THE SKIN AIR VALVE (EXT RACT) IAW AMM 21-26-53-000-001. VENDOR BENCH TEST OF SKIN AIR VALVE S/N 2772 WAS NO FAULT FOUND, UNIT WAS NOT DISASSEMB LED AND INSPECTED. 2 L 7 2 4F RT A28NM 2002051400080 20020514 00080 NM 2002 5 14 0201456306 1 20020501 A 2120 ODOR BOEING 747 747451 1384940 NM CABIN DETECTED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 666US 23821 DURING CRUISE, AN INTENSE BURNING SMELL EMITTED IN THE AREA OF DOOR 5L. TURNED OFF RECIRCULATION FANS AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. VISUALLY INSPECTED AREA WITH NO DEFECTS NOTED. 2 L 7 4 4F RT A20WE 2002051400081 20020514 00081 NM 2002 5 14 02FDEA00323 1 20020511 A 5270 WARNING SYSTEM BOEING 727 727200 138407E NM COCKPIT FALSE ACTIVATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 212FE 22934 AFT AIRSTAIR LIGHT ON S/O PANEL ON AFTER TAKEOFF. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B. AIRSTAIR UP UPON ARRI VAL. INSPECTED SYSTEM, HANDLE IN CORRECT LOCK POSITION. CYCLED AIRSTAIR ALL INDICATIONS NORMAL AT THIS TIME. MACH SH OWS NO HISTORY FOR LAST 60 DAYS. PER MEL - LOWER AFT AIRSTAIR CONTROL STATION RED NOT LOCKED WARNING LIGHT OPS NORMALLY . DURING AIRSTAIR OPERATION & EXTINGUISHES WHEN AIRSTAIR IS LOCKED UP. CYCLED AIRSTAIRS SEVERAL TIMES ALL FUNCTIONS OF AIRSTAIRS OP CHECKS GOOD AS PER AMM 52-62-001-0, DEBRIEFED INCOMING FLIGHT CREW INDICATIONS WERE NORMAL. 2 L 7 3 4F RT A3WE 2002051400082 20020514 00082 NM 2002 5 14 02FDEA00325 1 20020511 A 5243 655623514 DOOR BOEING 727 727200 138407E NM HYD SERVICE DAMAGED A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 267FE 21673 ON ARRIVAL INTO LAS FOUND HYD SERVICE DOOR TORN ABOUT 3/4 OFF. NO RESTRICTION HYD SERVICE DOOR MISSING (ON 2 CYCLE EA). FABRICATED AND INSTALLED TEMP REPAIR PER EA 7-5320. REMOVED AND REPLACED HYD ACCESS DOOR PER 12-30-000, OK FOR SERVIC E. 2 L 7 3 4F RT A3WE 2002051400083 20020514 00083 NM 2002 5 14 200200250 1 20020510 A 5753 STRINGER BOEING 747 747273C 1384896 NM T/E FLAP GOUGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 470EV 20653 FOUR GOUGES WERE FOUND COMMON TO THE PRODUCTION STRINGER ON VARIABLE CAMBER FLAP NR 21 ON THE RIGHT WING. THIS DISCREPA NCY WAS CORRECTED BY TRIMMING OUT THE DAMAGED AREAS AND INSTALLING AN ANGLE DOUBLER PER EIA ECRA 470-57-150-2. 2 L 7 4 4F A20WE 2002051400084 20020514 00084 NM 2002 5 14 2002UALA00820 1 20020503 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 BODY STATION 1809.5 RT EXTERNAL FUSELAGE SKIN HAS EXCESSIVE CHAFING WEAR. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INS TALLEDREPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002051400085 20020514 00085 NM 2002 5 14 2002UALA00822 1 20020504 A 5330 SPLICE PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 AFT PIT FRAME SPLICE PLATE AT STATION 1520 STRINGER 25R WAS BLENDED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED.SPLICE PLA TE WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400086 20020514 00086 NM 2002 5 14 2002UALA00823 1 20020504 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 AIRCRAFT FRAME IN AFT PIT DENTED, STATION 1420 BETWEEN STRINGER 25 AND STRINGER 26L. MAJOR REPAIR ACCOMPLISHED.REMOVED DAMAGE, INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400087 20020514 00087 NM 2002 5 14 2002UALA00824 1 20020504 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 CABIN FLOOR SUPPORT ANGLE CORRODED AT STATION 736, RBL 68, WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM ANG LE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400088 20020514 00088 NM 2002 5 14 2002UALA00827 1 20020505 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 LEFT HAND EXTERIOR FUSELAGE SKIN BODY STATION 610, 8" BELOW 17L STRINGER IS DENTED. MAJOR REPAIR ACCOMPLISHED.REMOVED D AMAGE AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400089 20020514 00089 NM 2002 5 14 2002UALA00828 1 20020505 A 5300 SEAT TRACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 LH OB SEAT TRACK CRACKED AT OB FASTENER HOLE STATION 1200. MAJOR REPAIR ACCOMPLISHED.SPLICED IN NEW SEAT TRACK SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400090 20020514 00090 NM 2002 5 14 2002UALA00837 1 20020508 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 AFT PIT FRAME CORRODED, STATION 1480 RBL 27 STRINGER 27 UNDERNEATH RT Z ANGLE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400091 20020514 00091 NM 2002 5 14 2002UALA00838 1 20020507 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 BODY STATION 1809.5 LT EXT FUSE SKIN HAS EXCESSIVE CHAFFING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002051400092 20020514 00092 NM 2002 5 14 2002UALA00839 1 20020507 A 5313 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 BODY STATION 348 STRINGER 20R RBL 84 TOP OF FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLO ORBEAM SECTION AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002053000082 20020530 00082 NM 2002 5 30 2002UALA00843 1 20020508 A 5313 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 STATION 358 STRINGER 3 RT IS PUNCTURED, LIGHTNING STRIKE DAMAGE. MAJOR REPAIR ACCOMPLISHED. STRINGER REPAIRED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002051400093 20020514 00093 NM 2002 5 14 2002UALA00844 1 20020508 A 5313 SPLICE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 FUSELAGE STRINGER SPLICE STRINGER 27R STATION 1486 CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400094 20020514 00094 NM 2002 5 14 2002UALA00846 1 20020509 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 AFT PIT FRAME BENT ABOVE STRINGER 25LH STATION 1460. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.INSTALLED FRAME CAP WEB CUTOUT INTERNAL AND EXTERNAL DOUBLER AND TRIPPLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400095 20020514 00095 NM 2002 5 14 2002UALA00847 1 20020509 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 AFT PIT FRAME AT STATION 1200 STRINGER 30 TOP FLANGE HAS EXCESSIVE MATERIAL LOSS FROM CORROSION REMOVAL. SUPPLEMENTAL DA TA UPDATE MAJOR REPAIR ACCOMPLISHED.INSTALLED FRAME CAP REPAIR STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400096 20020514 00096 NM 2002 5 14 2002UALA00850 1 20020509 A 5315 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 CABIN FLOOR INTERCOSTAL AT STATION 357 RBL 25" STRINGER 17R IS CRACKED OUT AROUND NUTPLATE HOLE. MAJOR REPAIR ACCOMPLIS HED.INSTALLED NEW U- CHANNEL INTERCOSTAL BETWEEN STATION 345 AND 365. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400097 20020514 00097 NM 2002 5 14 2002UALA00851 1 20020509 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 FORWARD CABIN STRINGER 2R IS GOUGED AT STATION 460. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW SECTION WITH SPLICE AT 470 STATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400098 20020514 00098 NM 2002 5 14 2002UALA00852 1 20020509 A 5315 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 AFT PIT FRAME STATION 1500 RBL 15 CORRODED. MAJOR REPAIR ACCOMPLISHED.REPAIR DOUBLER INSTALLED ON FRAME 1500. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400099 20020514 00099 NM 2002 5 14 200200251 1 20020510 A 5711 65B116148 SPAR BOEING 747 747273C 1384896 NM RT WING CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 470EV 20653 A CRACK WAS FOUND COMMON TO THE UPPER CHORD OF THE RIGHT WING TRAILING EDGE AUXILIARY SPAR AT WBL 425. THIS DISCREPANCY WAS REPAIRED BY REMOVING THE DAMAGED SECTION OF CHORD AND SPLICING IN A NEW SECTION OF CHORD WITH REPAIR ANGLES PER EIA ECRA 470-57-141-02. 2 L 7 4 4F A20WE 2002051400100 20020514 00100 NM 2002 5 14 200200252 1 20020510 A 5320 65B154583 FITTING BOEING 747 747273C 1384896 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 470EV 20653 THE BS 1480 FLOOR SUPPORT FITTING FLANGE WAS FOUND CRACKED COMMON TO THE DIAGONAL BRACE. THE FITTING WAS REPAIRED BY MA CHINING THE CRACKED FLANGE PER BOEING SRM GUIDELINES, DYE PENETRANT INSPECTING THE MACHINED FLANGE AND MACHING AND INSTA LLING A NEW FLANGE PER EIA ECRA 470-53-149-2. 2 L 7 4 4F A20WE 2002051400101 20020514 00101 NM 2002 5 14 200200257 1 20020510 A 5330 65B0700310 SKIN BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 470EV 20653 A DAMAGED SKIN REPAIR WAS FOUND COMMON TO THE FUSELAGE SKIN AT BS 1760, STR 33R. THE DAMAGED SKIN WAS REMOVED AND AN EX ISTING BLEND WAS FOUND COMMON TO THE 1760 CHORD. THE DAMAGED SKIN REPAIR WAS REMOVED AND THE SUBJECT SKIN PANEL WAS REP AIRED. A REPLACEMENT SECTION OF SKIN AND BONDED DOUBLER WAS SPLICED IN WITH REPAIR DOUBLERS. 2 L 7 4 4F A20WE 2002051400102 20020514 00102 NM 2002 5 14 200200258 1 20020510 A 5315 65B07936599 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 470EV 20653 CORROSION WAS FOUND ON THE BS 400 FLOORBEAM UPPER FORWARD CHORD AT RBL 35. ALSO AN EXISTING REPAIR WAS FOUND COMMON TO THE FORWARD UPPER CHORD AT RBL 40. THE CORROSION WAS REMOVED BY TRIMMING AWAY THE HORIZONTAL FLANGE OF THE CHORD. THE EXISTING REPAIR WAS REMOVED FROM THE AIRCRAFT. THE FORWARD UPPER CHORD WAS REPAIRED BY CUTTING THE CHORD AT RBL 60 TO L BL 60 AND SPLICING IN A NEW SECTION OF CHORD PER EIA ECRA 470-53-134-2. 2 L 7 4 4F A20WE 2002051400103 20020514 00103 NM 2002 5 14 200200259 1 20020510 A 5315 65B10929518 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 470EV 20653 CORROSION WAS FOUND ON THE BS 380 FLOORBEAM UPPER CHORD LBL 9 TO LBL 28. THE FLOORBEAM WAS REPAIRED BY REMOVING THE DAM AGED SECTION OF UPPER CHORD AND SPLICING IN A NEW SECTION BETWEEN LBL 28 AND LBL 9.2 PER BOEING DRAWING 14100044 SHEET 4 AND ECRA 470-53-133-2. 2 L 7 4 4F A20WE 2002051400104 20020514 00104 NM 2002 5 14 200200260 1 20020510 A 5330 65B070009 SKIN BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 470EV 20653 DAMAGE WAS FOUND IN THE FUSELAGE SKIN AT THE FORWARD EDGE OF THE BULK CARGO DOOR CUTOUT AT STA 1983, STR 36R TO STR 39R. THE SKIN IS IN FACT AN ASSEMBLY CONSISTING OF SKIN/DOUBLER/TRIPLER WHICH WERE DAMAGED AND A QUADRUPLER WHICH WAS NOT. THE DAMAGED SECTION WAS REMOVED AND EXTERNAL DOUBLERS INSTALLED. 2 L 7 4 4F A20WE 2002051400105 20020514 00105 NM 2002 5 14 200200261 1 20020510 A 5320 WEB BOEING 747 747273C 1384896 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 470EV 20653 CORROSION WAS FOUND ON THE WING CENTER SECTION CANTED WEB AT RBL 65. THE CORROSION WAS REMOVED BY TRIMMING AWAY THE DAM AGED SECTION OF WEB. THE WEB WAS REPAIRED BY INSTALLING REPAIR DOUBLER PER EIA ECRA 470-53-129-2. 2 L 7 4 4F A20WE 2002051400106 20020514 00106 NM 2002 5 14 200200262 1 20020510 A 5330 65B041092 SKIN BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 470EV 20653 A GOUGE WAS FOUND NEAR THE EDGE OF THE FUSELAGE SKIN AT BS 670 BELOW STR 38R AT THE AFT EDGE OF THE FORWARD CARGO DOOR C UTOUT. THE SKIN IS AN ASSEMBLY CONSISTING OF THE SKIN AND A DOUBLER. THE DAMAGE IS CONFINED TO THE SKIN ONLY. THE DAM AGE WAS TRIMMED OUT, A HFEC INSPECTION PERFORMED, AN EXTERNAL DOUBLER INSTALLED PER EIA ECRA 470-53-120-2. 2 L 7 4 4F A20WE 2002051400107 20020514 00107 NM 2002 5 14 200200263 1 20020510 A 5753 65B170641 FLAP TRACK BOEING 747 747273C 1384896 NM T/E FLAP DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 470EV 20653 CORROSION AND THREAD DAMAGE WERE FOUND COMMON TO FORWARD BOLT HOLE LOCATIONS (4 EA INBOARD AND OUTBOARD SIDES) OF NR 4 T RAILING EDGE FLAP TRACK. THREAD DAMAGE WAS COMMON TO THE FAIL-SAFE BAR OUTBOARD HOLE NR 3. THE CORROSION AND THREAD DA MAGE WERE REMOVED AND THE BOLT HOLES WERE REWORKED PER BOEING SERVICE BULLETIN 747-57-2256 AND EIA ECRA 470-57-125-2. 2 L 7 4 4F A20WE 2002051400108 20020514 00108 NE 2002 5 14 2002F00465 2 20020503 A 7421 CH34743 IGNITER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FAILED G AMTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 11 553TZ 2044 2044 32587 31808 FLIGHT NUMBER 539, AFTER PUSHBACK FROM GATE THE RIGHT ENGINE FAILED TO START. AIRCRAFT RETURNED TO THE GATE. MAINTENAN CE REMOVED AND REPLACED THE NR 1 AND 2 IGNITOR PLUGS IN ACCORDANCE WITH M/M 74-21-02-04. THE AIRCRAFT WAS RETURNED TO S ERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002051400109 20020514 00109 NM 2002 5 14 2002F00466 1 20020506 A 4940 106170756D EXCITER BOEING 757 75723N 1384973 NM APU FAILED G AMTA K NONE O OTHER CR CRUISE 1 GL 11 519AT 16914 16914 27975 FLIGHT NUMBER 126, DURING CRUISE APU FAILED TO START DURING INFLIGHT START VERIFICATION (5 ATTEMPTS). MAINTENANCE TROUB LESHOT PER FIM 49-11-00 TO FAULTY EXCITER UNIT. REMOVED AND REPLACED IGNITION EXCITER IN ACCORDANCE WITH MM 49-41-03. APU OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002051400110 20020514 00110 NM 2002 5 14 2002F00467 1 20020507 A 2613 WARNING SYSTEM BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT FALSE ACTIVATION G AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 521AT 24368 30688 FLIGHT NUMBER 669, DURING CRUISE RIGHT ENGINE OVERHEAT EICAS MESSAGE AND LIGHT/AURAL WARNING AT FL 370. FLIGHT CREW PER FORMED CHECKLIST, SHUT OFF BLEED VALVE AND BROUGHT POWER TO IDLE THRUST. LIGHT AND EICAS MESSAGE WENT AWAY 30 SECONDS L ATER. MAINTENANCE RAN ENGINE AT 1.7 EPR FOR TWENTY MINUTES, NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002051400111 20020514 00111 NM 2002 5 14 2002F00468 1 20020430 A 2612 FIRE LOOP BOEING 757 75733N 1384931 NM NR 1 ENGINE FAULTY G AMTA K NONE N FALSE WARNING CR CRUISE 1 GL 11 554TZ 32588 FLIGHT NUMBER 925, DURING CRUISE THE LEFT ENGINE FIRE LP NR 1 STATUS MESSAGE DISPLAYED. MAINTENANCE REMOVED AND REPLACE D THE NR 1 FIRE LOOP DET PER MM 26-11-01-04. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002051400112 20020514 00112 NM 2002 5 14 2002F00469 1 20020425 A 4960 211734220 CONTROL UNIT BOEING 757 75733N 1384931 NM APU FAILED G AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 553TZ 1974 1974 32587 FLIGHT NUMBER 454, DURING TAXI PREPARING TO DEPART RSW THE APU HAD AN AUTO SHUTDOWN (FAULT LIGHT ILLUMINATED AND EICAS M ESSAGE APU FAULT DISPLAYED). AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE APU CONTROL UNIT (ECU ) IN ACCORDANCE WITH AMM 49-61-05, FUNCTIONAL CHECKS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2002051400113 20020514 00113 NE 2002 5 14 2002F00470 2 20020505 A 7321 GOVERNOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAILED G AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 520AT 27976 31558 AFTER PUSHBACK FROM GATE AND UPON LEFT ENGINE START, RECEIVED EICAS ADVISORY MESSAGE S L ENG EEC AND L ENG LIMITER, AS W ELL AS L ENG LIMITER INOP LIGHT AND L ENG EEC INOP LIGHT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE FUEL FLOW GO VERNOR PER MM 73-21-01 AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002051400114 20020514 00114 NM 2002 5 14 2002UALA00787 1 20020426 A 5313 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 A/C FUSELAGE IS DENTED AT STATION 400 AND STRINGER 36L. STRINGER IS DEFLECTED .50 INCHES OVER 20 INCH LENGTH. ALSO, FW D CARGO PIT STRINGER 34L HAS 2 INCH CRACK AT STA 390. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW STRINGERS, THE DENT WI TH STRING DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002051400115 20020514 00115 NM 2002 5 14 2002UALA00788 1 20020429 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 THERE IS A 2.5 INCH CRACK IN FUSELAGE AT LOWER AFT RADIUS OF DOOR 1R OPENING. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE INSTALLED. VERIFIED CRACK FREE AFTER DAMAGE REMOVED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051400116 20020514 00116 NM 2002 5 14 2002UALA00789 1 20020428 A 3350 BATTERY PACK BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 936UA 26667 EMERGENCY EXIT LIGHTS ROWS 8 THROUGH 14 INOPERATIVE. ORANGE LIGHT AT EMERGENCY EXIT ROW 9 DIM. RECONNECTED LIGHT STRIP . OPS CHECK FOUND SHORTED POWER PACK. REPAIRED POWER PACK. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051400117 20020514 00117 NM 2002 5 14 2002UALA00791 1 20020501 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 RIGHT HAND AFT SIDE OF BODY STATION 188 FRAME IS CRACKED IN THE RADIUS OF THE WEB AT WL 207. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME REPAIR. VERIFIED NO CRACKS AFTER DAMAGE REMOVED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051400118 20020514 00118 NM 2002 5 14 2002UALA00792 1 20020430 A 3397 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EEL LIGHT INOP AT SEAT 35C. REPLACED THE EEL SEAT HARNESS. 2 L 7 4 4F 4 F RT A20WE E24NE 2002051400119 20020514 00119 NM 2002 5 14 2002UALA00793 1 20020501 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 LEFT HAND AFT SIDE OF BODY STATION 188 FRAME IS CRACKED IN THE RADIUS OF THE WEB AT WL 207. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE INSTALLED. VERIFIED NO CRACKS AFTER DAMAGE REMOVED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002053000067 20020530 00067 NM 2002 5 30 2002UALA00796 1 20020206 A 5330 145T252421 STRAP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 609UA 21870 DURING C-CHECK FOUND CRACK IN FAIL-SAFE STRAP. CRACK IN THE FAIL-SAFE STRAP AT STA 955.1 ON THE LEFT SIDE WAS CAUSED BY FATIGUE. OTHER CONTRIBUTING FACTORS TO THE CRACK ORIGINATION ARE BEING DETERMINED BY THE OEM WITH FURTHER ANALYSIS OF THE CRACKED PART. THE CORRECTIVE ACTION WAS REPLACEMENT OF THE FAIL-SAFE STRAP WITH A NEW FAIL-SAFE STRAP PER ORIGINAL MANUFACTURERS DRAWINGS. 2 L 7 2 4F 4 F RT A1NM E3NE 2002051400120 20020514 00120 NM 2002 5 14 2002UALA00797 1 20020501 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 935UA 26663 CABIN FRAME STATION 616R BELOW FLOOR FORWARD OF OVERWING EXIT IS CRACKED (FRAME INNER CHORD). MAJOR REPAIR ACCOMPLISHED . CUT OUT DAMAGED FRAME WEB. MANUFACTURED AND INSTALLED NEW WEB SECTION AND SPLICE DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051400121 20020514 00121 NM 2002 5 14 2002UALA00798 1 20020502 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 935UA 26663 TWO DENTS IN RIGHT SIDE FUSELAGE AT 4 O'CLOCK AT FIRST CIRCUMFERENTIAL AFT OF RADOME BULKHEAD STA 188, STRINGER 20 RIGHT . MAJOR REPAIR ACCOMPLISHED. EXTERNAL DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051400122 20020514 00122 NM 2002 5 14 2002UALA00799 1 20020502 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR CANNING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 AFT CARGO DOOR SKIN DENT COUPLED WITH OIL-CANNING: 14 INCHES DOWN AND 9 INCHES FORWARD FROM UPPER AFT CORNER OF DOOR. M AJOR REPAIR ACCOMPLISHED. FILLER AND STIFFENER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072200063 20020722 00063 2002 7 22 2002UALA00801 4 20020501 A 3460 4072800901 CDU BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 774UA 26936 CAPT CDU WENT INOP AFTER TAKEOFF. CREW WAS UNABLE TO RESTORE THE SYSTEM. DUAL CDU REQUIRED PRIOR TO ENTERING CLASS 2 R NP-10 AIRSPACE. AT JFK, THE CENTER CDU WAS SWAPPED WITH THE INOPED CAPTAIN'S ONE AND DEFFERED. DEFECTIVE CDU WAS REPLA CED AT LHR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002051400123 20020514 00123 NM 2002 5 14 2002UALA00803 1 20020205 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 CABIN FLOORBEAM 365 EXCESSIVE MATERIAL LOSS FROM CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. INSTALLED UNDER FLANGE STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400124 20020514 00124 NM 2002 5 14 2002UALA00804 1 20020502 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 CABIN CREASE BEAM WEB UPPER SURFACE CORRODED BODY STATION 982, LBL 71 WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED CREA SE BEAM WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051400125 20020514 00125 NM 2002 5 14 ASAA024042 1 20020411 A 3397 810022605 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 SEA - DURING PREFLIGHT CHECK, FOUND FLOOR TRACK LIGHTS DISCONNECTED AT ROW 22. RECONNECTED WIRES. TRACK LIGHTS THEN OP ERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2002051400126 20020514 00126 WP 2002 5 14 MWEA020325 1 20020512 A 5313 59203192 LONGERON DOUG DC9 DC932 3022066 WP STATION 269 TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 DRILL START ON BOTTOM OF LONGERON 30 STATION 269. -- FABRICATED AND INSTALLED LONGERON SPLICE. 2 L 7 2 4F A6WE 2002051400127 20020514 00127 WP 2002 5 14 MWEA020330 1 20020512 A 5320 9911535501 SKIN DOUG DC9 DC932 3022066 WP STATION 756 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 STATION 756 LEFT SIDE 9 HOLES ARE TOO CLOSE TO WINDOW BELT SPLICE. -- FABRICATED AND INSTALLED REPAIR BUSHINGS. 2 L 7 2 4F A6WE 2002051400128 20020514 00128 WP 2002 5 14 MWEA020331 1 20020512 A 5320 9911535501 SKIN DOUG DC9 DC932 3022066 WP STATION 794 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 STATION 794 THROUGH 813, 16 HOLES WERE MISDRILLED IN BOTTOM 2 ROWS OF REPAIR ABOVE LONGERON 15 LEFT. -- FABRICATED AND INSTALLED REPAIR BUSHINGS AND PLUGS. 2 L 7 2 4F A6WE 2002051400129 20020514 00129 NM 2002 5 14 AWXA200200423 1 20020408 A 5230 65C362152 SKIN BOEING 737 7373Q8 1384670 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 0 0 23507 MCN - MAJOR REPAIR - DURING C-15 CHECK A CRACK WAS FOUND AT THE FORWARD CARGO DOOR INNER SKIN LOWER EDGE FASTEN HOLE, BS 450. MAINTENANCE CUTOUT AND REMOVED THE DAMAGED PORTION OF SKIN AT THE LOWER FASTENER HOLE BS 450; FABRICATED A DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13, FIG. 1, SHT 1-3. 2 L 7 2 4F RT A16WE 2002051400130 20020514 00130 NM 2002 5 14 AWXA200200424 1 20020505 A 5330 65457788 SKIN BOEING 737 7373Q8 1384670 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 0 0 23507 MCN - MAJOR REPAIR - DURING C-15 CHECK A CRACK WAS FOUND IN THE FUSELAGE SKIN OF THE R2 DOOR LOWER HINGE CUTOUT BS 948.5 , CONFIRMED BY HFEC INSPECTION AND 10X VISUAL. MAINTENANCE CUTOUT CRACKED AREA OF SKIN AT R2 DOOR LOWER HINGE CUTOUT; PE RFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A -1 REPAIR DOUBLER, -2 REPAIR TRIPLER, -3 FILLER, AND INS TALLED REPAIR PARTS IAW B737-300 SRM 53-60-01, FIG. 207, SHT 1-8. 2 L 7 2 4F RT A16WE 2002051400131 20020514 00131 WP 2002 5 14 P2EA2002V0034 1 20020507 A 5313 LONGERON DOUG DC9 DC982 3022082 WP OVERSIZED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 130NJ 49222 DURING C1+C2 INSPECTION:-FUSELAGE, LONGERON 17L-H WITH OVERSIZE FASTENER HOLES FROM BS Y254 TO BS Y258.-LONGERON 17 L-H REPAIRED FROM BS Y229 TO Y292 DUE TO OVERSEZED HOLES IAW SRM 53-02, FIG18.NOTE: SEE COOPESA WORK ORDER No. P10430 2-106, VAM100 No. 232 & SDA No. 130SDA009. 2 L 7 2 4F A6WE 2002051400132 20020514 00132 WP 2002 5 14 P2EA2002V0035 1 20020514 A 5730 SKIN DOUG DC9 DC982 3022082 WP CRACKED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 130NJ 49222 DURING C1+C2 INSPECTION:-L-H WING UPPER SURFACE T/E SKIN SECTION MISSING/CRACKED IN SPOILER No.2 AREA.-REPAIRED L-H WING UPPER SURFACE T/E SKIN SECTION FROM XRS263.5 TO XRS270.5 IAW COOPESA E.O. No. COO-9-57-276-02, DATED MAY 08,2002. DOCUM ENTED ON FAA 8110-3 FORM.NOTE: SEE COOPESA WORK ORDER No. P10430 5-8, VAM100 No.208 & 130SDA010. 2 L 7 2 4F A6WE 2002051500002 20020515 00002 NM 2002 5 15 2002FA0000592 1 20020320 A 3240 511531 HOUSING BOEING 737 737 UTILSYS NM SHUTTLE VALVE DAMAGED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 SHUTTLE VALVE HOUSING, HAS A PIN HOLE IN THE MOUNT. FATIGUED. REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 2002051500028 20020515 00028 NE 2002 5 15 ABXA010872 2 20020403 A 7497 WIRE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE COCKPIT DAMAGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 923AX 47165 NO IGNITION ON EITHER ENGINE. FOUND WIRES 1J6H24 AND 2J4D24 BURNT THROUGH THREE FEET LEFT OF PEDESTAL IN THE CAPTAIN'S CONSOLE. REPLACED THE DAMAGED SECTION OF WIRES AND OPS CHECKED BOTH ENGINE IGNITION SYSTEMS IAW DC-9 MM. NO DEFECTS NO TED. 2 L 7 2 4F 4 F A6WE E2EA 2002080500058 20020805 00058 WP 2002 8 5 ARWA20020501 1 20020506 A 5313 LONGERON DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 1804 45896 DURING C-CHECK, FORWARD CARGO COMPARTMENT LONGERON L-21L AT FUSELAGE FS 280 WITH 2 INCH CRACK. FABRICATED SHIM & REPAIR ANGLE IAW AS ELEVEN, INC DRAWING AS 11410, SHEET 1 & 2. INSTALLED PARTS IAW AS ELEVEN, INC DRAWING AS 11410, SHEET 1 & 2. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR. 2 L 7 4 4F 4A25 2002080500075 20020805 00075 WP 2002 8 5 ARWA20020502 1 20020506 A 5320 SPLICE DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 1804 45896 DURING C-CHECK, FORWARD LOWER CARGO COMPARTMENT FUSELAGE FS 340, FS 360, FS 380, FS 400, FS 420, FS 440 & FS 460; LBL 62 .5 FLOORBEAM SPLICE WITH 2.750 INCH CRACK. REMOVED AND REPLACED FLOORBEAM SPLICE PLATE IAW AS ELEVEN INC DRAWING AS 110 77, SHEET 1 OF 9, DATED 05/21/02. ISSUED FAA FORM 8110-2 APPROVING THIS WORK. 2 L 7 4 4F 4A25 2002060300051 20020603 00051 NE 2002 6 3 ARWA20020503 2 20020508 A 7261 GARLOCK SEAL DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE LEAKING A ARWA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 810BN 45905 NR 4 ENGINE OIL QUANTITY 3/4 OF A GALLON. PERFORMED INFLIGHT SHUT DOWN ABNORMAL. OIL PRESS WINDMILLING 20 PSI. SERVIC ED ENGINE OIL IAW DC-8 MM 12-20-1 AND PERFORMED ENGINE RUN-UP; FOUND OIL LEAK AT MAIN FUEL PUMP DRAIN. REMOVED AND REPL ACED MAIN FUEL PUMP GARLOC SEAL IAW P&W MM 72-0 PG 434A. PERFORMED ENGINE RUN-UP IAW P&W MM 72-0, NO LEAKS NOTED. 2 L 7 4 4F 4 F 4A25 1E8 2002051500030 20020515 00030 2002 5 15 ASAA0280097 4 20020321 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 SEA - FORWARD SERVICE R-1 DOOR EMERGENCY SLIDE LANYARD DISCONNECTED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2002051500032 20020515 00032 WP 2002 5 15 ASAA0280098 1 20020321 A 5320 5936666091 SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON CARGO TRACK LEFT LOWER SURFACE COMMON TO TRACK SPLICE AT FS 1211-1225. REPLA CED SPLICE PER SRM 51-30-5, FIG 1. (M) 2 L 7 2 4F RT A6WE 2002051500033 20020515 00033 WP 2002 5 15 AT0200057 1 20020405 A 5522 SKIN DOUG DC9 DC932 3022066 WP ELEVATOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 834AT 47488 LT ELEVATOR UPPER SKIN IS CRACKED AT I/B END. STOP DRILLED ENDS OF CRACK, LT ELEVATOR UPPER SKIN AT I/B END AS PER DC9 SRM 55-03. ACCOMPLISHED HFEC ON CRACK PER NDT SPM 06-00-07; CRACK CONTAINED. INSTALLED REPAIR DOUBLER AS PER DC9 SRM 5 5-03, FIGURE 15. 2 L 7 2 4F A6WE 2002051500034 20020515 00034 NM 2002 5 15 AWXA200200412 1 20020410 A 5241 143N61004 WEB BOEING 757 7572G7 1384963 NM R2 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 GYR - MAJOR REPAIR - DURING C-11 CHECK A .5 INCH CRACK WAS FOUND ON THE WEB OF THE R2 DOOR AT THE UPPER HINGE CUTOUT. M AINTENANCE CUTOUT DAMAGED AREA, FABRICATED A REPAIR DOUBLER AND FILLERS, AND INSTALLED REPAIR PARTS IAW AWA ER 19-5211-0 21280-ES1. 2 L 7 2 4F RT A2NM 2002051500035 20020515 00035 NM 2002 5 15 AWXA200200413 1 20020508 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE O OTHER CR CRUISE 1 WP 28 182AW 22649 PHX - EEL - FLT 0299 - EN ROUTE FROM LAS TO PHX FLIGHT CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ABOVE R2 DOOR FLASHES ON AND OFF DURING FLIGHT AND TAXI TO GATE. MAINTENANCE REPLACED BATTERIES AT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOO D. 2 L 7 2 4F RT A16WE 2002051500036 20020515 00036 WP 2002 5 15 MWEA020304 1 20020429 A 5313 5911423103 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 LONGERON 19 LEFT CUT AT STATION 956 AND AFT SECTION MOVED TO FACILITATE OTHER MAINTENANCE. INSTALLED SPLICE PER SRM 51- 30-5. INSTALLED LONGERON 19 IAW SRM 51-50-5. 2 L 7 2 4F A6WE 2002051500037 20020515 00037 WP 2002 5 15 MWEA020307 1 20020429 A 5313 591142397 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CORROSION PRESENT ON LONGERON 23 LEFT AT STATION 946. REMOVED DAMAGED SECTION OF LONGERON AND INSTALLED REPAIR SECTION AND SPLICES. 2 L 7 2 4F A6WE 2002051500038 20020515 00038 WP 2002 5 15 MWEA020309 1 20020501 A 5330 5911429101 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 LOWER FUSELAGE SKIN HAS A SMALL CRACK JUST FORWARD OF VENTRAL STAIRS. REMOVED AND INSTALLED SERVICEABLE SKIN IAW DC9 SR M 51-30-3 AND 53-30-0. 2 L 7 2 4F A6WE 2002051500039 20020515 00039 WP 2002 5 15 MWEA020311 1 20020508 A 5320 5920303501 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 AFT PIT LONGERON 30 END FITTING AT STATION 756 HAS BARE METAL AND POSSIBLE LIGHT CORROSION PRESENT. REMOVED AND REPLACE D LONGERON AND INSTALLED CORRECT LENGTH HI-LOKS. 2 L 7 2 4F A6WE 2002051500040 20020515 00040 WP 2002 5 15 MWEA020312 1 20020508 A 5320 39132911 SPLICE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 AFT PIT CORROSION ON LONGERON 28 LEFT SPLICE AT STATION 828. REMOVED AND REPLACED SPLICE. 2 L 7 2 4F A6WE 2002051500041 20020515 00041 WP 2002 5 15 MWEA020313 1 20020508 A 5311 991224343 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 CORROSION ON TOP OF STATION 965 ABOVE LONGERON 30. REMOVED AND REPLACED FRAME SEGMENT. FABRICATED AND INSTALLED SPLICE S. 2 L 7 2 4F A6WE 2002051500042 20020515 00042 WP 2002 5 15 MWEA020314 1 20020508 A 5320 39146771 SPLICE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 AFT PIT CORROSION ON LONGERON 29 LEFT SPLICE IN TWO LOCATIONS STATION 836 AND 844. REMOVED AND REPLACED SPLICE. 2 L 7 2 4F A6WE 2002051500043 20020515 00043 WP 2002 5 15 MWEA020315 1 20020508 A 5320 5911448509 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 CORROSION ON FLOOR SUPPORT STATION 352 LONGERON 28 RIGHT TO LONGERON 29 LEFT. FABRICATED AND INSTALLED SPLICE. 2 L 7 2 4F A6WE 2002051500044 20020515 00044 WP 2002 5 15 MWEA020316 1 20020508 A 5753 5910042505 VANE DOUG DC9 DC932 3022066 WP T/E FLAP GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 GOUGE ON LEADING EDGE OF MIDDLE FIXED VANE. FABRICATED AND INSTALLED FIXED VANE REPAIR. 2 L 7 2 4F A6WE 2002051500045 20020515 00045 WP 2002 5 15 MWEA020317 1 20020508 A 5311 99115173 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 FRAME AT STATION 180 LONGERON 30 HAS AREA OF CORROSION. CUT OUT DAMAGED AREA CHANNEL AND FILLER. FABRICATED AND INSTAL LED SPLICES AND FILLER. 2 L 7 2 4F A6WE 2002051500046 20020515 00046 WP 2002 5 15 UPS02837917 1 20020303 A 5713 STRINGER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C1 LEFT WING STRINGER 66 IS CRACKED AT APPROX XRS 370 AT FRONT SPAR. REMOVED STRINGER 66 SECTION, AND E ND FITTING, FABRICATED AND INSTALLED STRINGER, END FITTING, AND SPLICES IAW DWG 5751406, AND SRM 57-2-2 FIG 3D. 2 L 7 4 4F RT 4A25 2002051500047 20020515 00047 WP 2002 5 15 UPS02837918 1 20020222 A 5320 559764689 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C1 L-1 DOOR LOWER FWD CORNER SUPPORT ANGLE IS CRACKED AT STA 25 AT LONG 21L LOWER SIDE. REMOVED, FABRIC ATED, AND REPLACED ANGLE IAW DWG 5597646, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2002051500048 20020515 00048 WP 2002 5 15 UPS02837919 1 20020218 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C1 FWD AND AFT LOWER CORNERS OF L-1 DOOR JAMB SKIN, INTERNAL DOUBLER, AND FRAME TO CUSP FITTING ARE CRAC KED AT STA 25 AND 70 BETWEEN LONG 20L TO 21L. CUT OUT CRACKED SKIN, INTERNAL DOUBLER SEGMENT, FABRICATED AND INSTALLED SKIN SEGMENT, INTERNAL DOUBLER SEGMENT, DOUBLER, TRIPLER, AND FILLERS AND REPLACED FRAME TO CUSP FITTING, AND ANGLES IAW DWG 5597646, 8110-3 APPROVED DH SK 707-035. 2 L 7 4 4F RT 4A25 2002051500049 20020515 00049 2002 5 15 UPS02837925 4 20020321 A 3441 2SEI101A28M SWITCH DOUG DC8 DC871F 302199D WP CABIN FAILED A IPXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 729UP 46029 INSPECTION TYPE:N/A NUMBER 2 INS FAILED ON THE WAY TO DFW, RED FLAG APPEARED BUT NO FAULT CODE. IN ATTITUDE REF MODE SM ELLED SMOKE TURNED INS OFF AND PULLED CIRCUIT BREAKER. REMOVED AND REPLACED INU BATTERY AND BLOWER VANE SWITCH REF L/P 722257 ITEM 1 AND 722 256 ITEM 3, INS OPS CKS GOOD IAW MM 34-44-00. 2 L 7 4 4F RT 4A25 2002051500050 20020515 00050 WP 2002 5 15 UPS02837932 1 20020308 A 5330 5649028U DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 STA 25 TO 60 INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN LONG 26R TO 31R. REMOVED AND REPLACE D DOUBLER IAW DWG 5649028, AND SRM 51-1-20D, 51- 1-21. 2 L 7 4 4F RT 4A25 2002051500051 20020515 00051 WP 2002 5 15 UPS02837934 1 20020326 A 3411 6228051004 STATIC LINE DOUG DC8 DC873F 302199F WP PITOT/STATIC SYS CONTAMINATED A IPXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 851UP 46051 INSPECTION TYPE:N/A EN ROUTE IMC CONDITIONS LOST ALL STATIC INSTRUMENTS, AIRSPEED INCLUDING STANDBY ALTIMETERS & ILLEG SELECTED ALT STATIC, NO HELP. DIVERTED TO CAE. DRAINED MOISTURE FROM STATIC SYSTEM AND CLEANED PITOT AND STATIC LINES. REMOVED AND REPLACED NR 1 AND NR 2 ADC IAW MM 34-11-01, TESTED PER 34-11-01, TESTED PER 34-11-00. 2 L 7 4 4F RT 4A25 2002051500052 20020515 00052 WP 2002 5 15 UPS02837935 1 20020311 A 5320 46143972N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C1 STA 70 FWD SIDE LONG 31R UPPER FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW D WG 4614397, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2002051500053 20020515 00053 WP 2002 5 15 UPS02837958 1 20020330 A 2120 ODOR DOUG DC8 DC871F 302199D WP COCKPIT DETECTED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 706UP 46056 INSPECTION TYPE:N/A ODOR IN COCKPIT FROM A/C UNIT. RAN BOTH PACKS WITH GROUND CART AND OFF ENGINE BLEEDS, COULD NOT DUP LICATE ODOR. OK FOR CONTINUED SERVICE. 2 L 7 4 4F RT 4A25 2002051500054 20020515 00054 WP 2002 5 15 UPS02837959 1 20020328 A 5711 SPAR DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:N/A LEFT WING AFT SPAR UPPER CHORD CRACKED. DEFERRED PERMANENT REPAIR PER MM 28-10-01 PG 207 D234849 AS SIGNED. 2 L 7 4 4F RT 4A25 2002051500055 20020515 00055 2002 5 15 UPS02837962 4 20020330 A 2561 LIFE VEST DOUG DC8 DC871F 302199D WP COCKPIT TORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:N/A CAPTS LIFE VEST TORN. REPLACED CAPT LIFE VEST. 2 L 7 4 4F RT 4A25 2002051500056 20020515 00056 WP 2002 5 15 UPS02837972 1 20020330 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:N/A EMERGENCY LIGHTS DIM WHEN PERFORMING TEST PER A-CK METHODS. PERFORMED TEST OF POWER SUPPLY VOLTAGE CHECKS OK FOR CONTINUED SERVICE. 2 L 7 4 4F RT 4A25 2002051500057 20020515 00057 WP 2002 5 15 UPS02837973 1 20020329 A 3350 LIGHT DOUG DC8 DC871F 302199D WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. SECURED GROUND IAW DC8 MM 20-00. REMOVED AND REPLACED LIGHT BULB IN EME RGENCY EXIT ASSY AT ENTRY DOOR IAW DC8 MM 33-50, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2002051500058 20020515 00058 WP 2002 5 15 UPS02837977 1 20020401 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED BATTERY PACK, CKS GOOD IAW MM CHP 33. 2 L 7 4 4F RT 4A25 2002051500059 20020515 00059 WP 2002 5 15 UPS02837992 1 20020303 A 5320 3754473U1 SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C1 STA 388 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473, AND SRM 53 -1-0, 51-1-20D. 2 L 7 4 4F RT 4A25 2002051500060 20020515 00060 WP 2002 5 15 UPS02837994 1 20020228 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C1 REPAIR AT AFT UPPER CORNER OF D-PIT DOOR IS CATEGORY D BECAUSE OF SCREWS AND BLIND FASTENERS PER EO D C8-5330-12800, AND HAS CRACKED SKIN STA 1440 LONG 23R APPROX. REMOVED EXISTING REPAIR, CUT OUT DAMAGED AREA. NDT VERIF IED NO CRACKS AT CUTOUT. FABRICATED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 21. 2 L 7 4 4F RT 4A25 2002051500061 20020515 00061 WP 2002 5 15 UPS02838010 1 20020409 A 3350 SWITCH DOUG DC8 DC873F 302199F WP COCKPIT FAULTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:IN EMERGENCY EXIT LIGHTS INTERMITTENTLY ILLUMINATED CAN BE RESET BY CYCLING ARMING SWITCH. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS SWITCH IAW M/M 20-50-00, OPERATIONAL CHECK IAW M/M 33-50-01. 2 L 7 4 4F RT 4A25 2002051500062 20020515 00062 WP 2002 5 15 UPS02838034 1 20020404 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 REMOVED STEEL DOUBLER FROM R1 DOOR UPPER FWD CORNER. REMOVED STEEL DOUBLER RAIN GUTTER UPPER DOOR ST OP GILLINER ATTACH ANGLE AND WEB FABBED DOUBLERS IAW DC8 SRM 53-2-0 FIG 14. REMOVED CRACK IAW DC 8 SRM 53-2-0 FIG 14. ALODINED & PRIMED IAW 51-1-8. INSTALLED DOUBLER AND FILLER IAW DC8 SRM 51-1-20D. REINSTALLED DOOR STOP GILLINER ATTACH ANGLE AND WEB IAW 51-1-21, 51-3-0. PLUGGED HOLES & REINSTALLED. 2 L 7 4 4F RT 4A25 2002051500063 20020515 00063 WP 2002 5 15 UPS02838039 1 20020325 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 AFT PIT STA 1270 INSULATE PAD IS CRACKED AT TORQUE BOX. REMOVED ANGLE IAW DC8 SRM 51-1-21 & 51-1-20D AND INSTALLED ANGLE IAW DC8 SRM 51-1-120D. 2 L 7 4 4F RT 4A25 2002051500064 20020515 00064 SO 2002 5 15 000157 1 20020513 A 7722 SENSE LINE EMB 145 EMB145 3260210 SO LT ENGINE MALFUNCTIONED A CHQA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 11 280 LT ENGINE HIGH ITT AT TAKEOFF. REMOVED AND REPLACED BLEED SENSE LINE. 2 L 7 2 4F RT T00011AT 2002051500065 20020515 00065 CE 2002 5 15 0018 1 20020510 A 3232 48C48608102 ACTUATOR LEAR 35 35A 5170602 CE RT MLG DOOR OUT OF ADJUST E CIEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 03 553V 9751 35A141 AFTER TAKEOFF, THE GEAR RETRACTED NORMAL BUT RT MAIN GEAR SHOWED AN UNSAFE INDICATION. THE INBOARD GEAR DOOR DID NOT CL OSE ENOUGH TO COMPRESS THE INBOARD GEAR DOOR SWITCH. INBOARD GEAR DOOR ACTUATOR HAD BEEN RESEALED DURING A 600 HR INSPE CTION PRIOR TO TAKEOFF. THE DOOR ACTUATOR REMOVED, RESEALED, REINSTALLED & OPERATIONAL CHECKED PER LEAR JET MM PRIOR TO TAKEOFF. AFTER TAKEOFF HAD UNSAFE GEAR INDICATION, RETURNED TO AIRPORT, EXTENDED THE GEAR AND GEAR EXTENDED NORMAL. A FTER RETURN ACFT WAS PLACED ON JACKS. DURING RETRACTION, MX WAS ABLE TO DUPLICATE THE INDICATION. INBOARD GEAR DOOR AC TUATOR WAS READJUSTED AND GEAR WAS AGAIN CHECKED FOR OPERATION & CHECKED NORMAL. 2 L 7 2 4F A10CE 2002051500071 20020515 00071 EA 2002 5 15 02132628 1 20020512 A 7920 LINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE RT ENGINE FAILED A VTZA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 27 628BR 7240 GEE872470 PASSING THROUGH 8000 FT IN THE CLIMB, THE CREW NOTED THE R ENG OIL PRESS RED WARNING ON THE EICAS. THE QRH WAS COMPLIED WITH, THE ENGINE WAS SHUT DOWN. THE AIRCRAFT RETURNED TO CAE, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUN D THE B-SUMP OIL LINE HAD FAILED. REMOVED AND REPLACED THE RT ENGINE ASSY. 2 L 7 2 4F 4 F RT A21EA E15NE 2002051500072 20020515 00072 WP 2002 5 15 CALA2000287 1 20020515 A 5310 5936597509 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 CORROSION ON FLOOR SUPPORT ON UNDESIDE AT STA 1211 BETWEEN STR 30 & 29R 1"X24". REPLACED FLOOR SUPPORT IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2002051500073 20020515 00073 NM 2002 5 15 CALA2000288 1 20020515 A 5330 6545767 SKIN BOEING 737 7373T0 1384582 NM A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14347 23585 FUSELAGE SKIN STA 380-400 HAS 4"X2" DENT WITH OIL CANNING BETWEEN STR 17 & 18. INSTALLED DOUBLER IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2002051500074 20020515 00074 WP 2002 5 15 CALA2000289 1 20020515 A 5310 FRAME DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 TAIL COMPARTMENT RH SIDE STA 1446 AT LONGERON 18R FRAME HAS DEEP 1"X1" CHAFE. INSTALLED ANGLE AND FILLER IAW SRM 51-30- 5, 51-30-2, 51-70-5, FIG 1. 2 L 7 2 4F A6WE 2002051500075 20020515 00075 NM 2002 5 15 SWAA020948 1 20020506 A 3350 07912 COVER BOEING 737 7372T4 1384492 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 EEPLS COVER MISSING BETWEEN ROWS 8 AND 9. INSTALLED COVER PER MM. 2 L 7 2 4F A16WE 2002051500076 20020515 00076 NM 2002 5 15 SWAA020949 1 20020505 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 938, BETWEEN STR'S 21L AND 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002051500077 20020515 00077 NM 2002 5 15 SWAA020951 1 20020506 A 5312 6517583 WEB BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 191 AT RBL 5.7. REPAIRED WEB PER SRM. 2 L 7 2 4F A16WE 2002051500078 20020515 00078 NM 2002 5 15 SWAA020952 1 20020504 A 5311 9078223 STRAP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE CUTOUT DOUBLER STRAP CRACKED AT BS 303, STR 13L. REPAIRED D OUBLER STRAP PER SWA RA. 2 L 7 2 4F RT A16WE 2002051500079 20020515 00079 NM 2002 5 15 SWAA020953 1 20020505 A 2731 BACB28AK04030 BUSHING BOEING 737 7377H4 1384404 NM BOTH ELEVATORS WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 718SW 27852 DURING SCHEDULED SERVICE CHECK, SI 11038-55, FOUND BOTH LT AND RT ELEVATOR TAB HINGE BUSHINGS WORN. REMOVED AND REPLACE D ALL 4 HINGE BUSHINGS ON BOTH TABS PER MM. 2 L 7 2 4F RT A16WE 2002051500080 20020515 00080 NM 2002 5 15 SWAA020954 1 20020503 A 2731 BACB28AKMO7 BUSHING BOEING 737 7375H4 138449D NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 508SW 24185 DURING SCHEDULED RON, SWA SI 11111-55, FOUND RT ELEVATOR TAB NR 1 HINGE BUSHING WORN. REMOVED AND REPLACED NR 1 HINGE B USHING PER MM. 2 L 7 2 4F RT A16WE 2002051500081 20020515 00081 NM 2002 5 15 SWAA020956 1 20020503 A 2731 6959227 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 624SW 27934 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB LOCKOUT MECHANISM HAS PLAY AT FWD END LINKAGE. REMOVED AND REPLACED FWD END BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002051500082 20020515 00082 NM 2002 5 15 SWAA020959 1 20020505 A 2731 BACB28AMOS BUSHING BOEING 737 7373H4 1384600 NM BOTH ELEVATORS WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, ELEVATOR TABS FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED BOTH L T AND RT TAB CONTROL ROD BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002051500083 20020515 00083 NM 2002 5 15 SWAA020960 1 20020503 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (5 EA) AT STR 2R, BS'S 1020, 1065, 1097, 1099 AND 1117.5. REPA IRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002051500084 20020515 00084 NM 2002 5 15 SWAA020961 1 20020505 A 2731 BACB28AMO7 BUSHING BOEING 737 7372H4 138448C NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, FOUND RT ELEVATOR TAB BUSHINGS WORN ON ALL 4 HINGES. REMOVED AND REPLA CED RT TAB BUSHINGS AT ALL HINGES PER MM. 2 L 7 2 4F A16WE 2002051500085 20020515 00085 NM 2002 5 15 SWAA020962 1 20020505 A 2731 6959227 BUSHING BOEING 737 7372H4 138448C NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, FOUND LT ELEVATOR TAB LOCKOUT MECHANISM HAS PLAY. REMOVED AND REPLACED LOCKOUT MECH BUSHING PER MM. 2 L 7 2 4F A16WE 2002051500086 20020515 00086 NM 2002 5 15 SWAA020963 1 20020502 A 2731 65C25798 HINGE BOEING 737 7377H4 1384404 NM BOTH ELEVATORS WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 726SW 27858 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND LT AND RT TAB HINGE BOLTS WILL NOT ROTATE AT HINGES NR 1 THROUGH NR 4. REMOVED AND REPLACED LT AND RT TAB HINGES NR 1 THROUGH NR 4 PER MM. 2 L 7 2 4F RT A16WE 2002051500087 20020515 00087 2002 5 15 SWAA020965 4 20020506 A 2565 6557463 FITTING BOEING 737 7373T5 1384608 NM FWD ENTRY DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2002051500088 20020515 00088 2002 5 15 SWAA020969 4 20020507 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 622SW 27932 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2002051500089 20020515 00089 NM 2002 5 15 SWAA020971 1 20020507 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 797MX 27890 EEPLS LENS LOOSE AT ROW NR 1. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002051500090 20020515 00090 NM 2002 5 15 SWAA020974 1 20020507 A 5315 BAC1509 FLOORBEAM BOEING 737 7373T5 1384608 NM AFT CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS727A PLUS 18, WL 208 AT LBL 47. REPAIRED FLOORBEAM PER BFG ER. 2 L 7 2 4F RT A16WE 2002051500091 20020515 00091 NM 2002 5 15 SWAA020975 1 20020507 A 5313 6546546 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 649SW 27719 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS727, STR 15L. REMOVED AND REPLACED TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002051500092 20020515 00092 NM 2002 5 15 SWAA020979 1 20020507 A 2731 BACB28AKM07 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING PER SRM. 2 L 7 2 4F RT A16WE 2002051500093 20020515 00093 NM 2002 5 15 SWAA020981 1 20020507 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002051500094 20020515 00094 NM 2002 5 15 SWAA020982 1 20020507 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULE SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, BETWEEN STR'S 23L AND 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002051500095 20020515 00095 NM 2002 5 15 SWAA020983 1 20020507 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002051500096 20020515 00096 NM 2002 5 15 SWAA020994 1 20020508 A 5330 6545776 SKIN BOEING 737 7372K6 1364440 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 129SW 22340 DURING PRE-FLIGHT INSP, FOUND 1.5 INCH FUSELAGE SKIN CRACK AT BS 887, BETWEEN STR 24R AND 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002051500097 20020515 00097 NM 2002 5 15 SWAA020995 1 20020508 A 5730 6545776 SKIN BOEING 737 7372K6 1364440 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 129SW 22340 DURING SCHEDULED SPECIAL VISIT, FOUND 1.25 INCH SKIN CRACK AT LT WING T/E, WBL 168. REPAIRED LT WING SKIN PER SWA T1.. 2 L 7 2 4F RT A16WE 2002051500098 20020515 00098 NM 2002 5 15 SWAA020996 1 20020509 A 2731 BACB28AMO7 BUSHING BOEING 737 7373H4 1384600 NM ELEV TABS WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED C4 CHECK, SWA SI 11111-55, LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT AND RT ELEVATOR TAB PUSHROD BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002051500099 20020515 00099 NM 2002 5 15 SWAA020998 1 20020509 A 2731 6963391 BOLT BOEING 737 7373TO 138447G NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C4 CHECK, FOUND LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB PUSH ROD BOLT PER MM. 2 L 7 2 4F RT A16WE 2002051500100 20020515 00100 NM 2002 5 15 SWAA020999 1 20020508 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPECIAL VISIT, FOUND 1.5 INCH SKIN CRACK AT BS 942 ABOVE STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002051500101 20020515 00101 NM 2002 5 15 SWAA021001 1 20020509 A 3350 65C36053 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED RON, FOUND FWD GALLEY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED FWD GALLEY EMERGENCY EXIT LIGH T ASSY PER MM. 2 L 7 2 4F RT A16WE 2002051500102 20020515 00102 NM 2002 5 15 SWAA021002 1 20020508 A 5755 6546452 SPOILER BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED SERVICE CHECK, FOUND NR 4 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED NR 4 GROUND SPOILER PER MM. 2 L 7 2 4F RT A16WE 2002051500103 20020515 00103 NM 2002 5 15 SWAA021003 1 20020508 A 5330 6545771 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED C2 CHECK, FOUND 1.5 INCH SKIN CRACK AT AFT SVC DOOR CUTOUT BS 957, NEAR STR 14L. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 2002051500104 20020515 00104 NM 2002 5 15 SWAA021004 1 20020508 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED SERVICE CHECK, FOUND LT OUTBD AFT FLAP DELAMINATED AT INBD AFT T/E. REMOVED AND REPLACED LT OUTBD AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2002051500105 20020515 00105 NM 2002 5 15 SWAA021005 1 20020509 A 2731 BACB28AK04 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED RON, FOUND LT ELEVATOR TAB INBD HINGE BUSHING WORN. REMOVED AND REPLACED LT ELEVATOR TAB INBD HINGE BU SHING PER MM. 2 L 7 2 4F RT A16WE 2002051500106 20020515 00106 2002 5 15 SWAA021007 4 20020509 A 2565 NAS60426P FASTENER BOEING 737 7373H4 1384600 NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BC2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE CONTAINER UPPER FWD FASTENER LOOSE. REMOVED AND REP LACED EMERGENCY EVAC SLIDE CONTAINER FASTENER PER MM. 2 L 7 2 4F RT A16WE 2002051500107 20020515 00107 2002 5 15 SWAA021009 4 20020510 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 753SW 29848 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002051500108 20020515 00108 2002 5 15 SWAA021010 4 20020512 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2002051500109 20020515 00109 NM 2002 5 15 SWAA021013 1 20020509 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 4, STR 15R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002051500110 20020515 00110 NM 2002 5 15 SWAA021014 1 20020510 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 5, ABOVE STR 15R. REPAIRED SKIN PER MM. 2 L 7 2 4F RT A16WE 2002051500111 20020515 00111 NM 2002 5 15 SWAA021015 1 20020504 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 895, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002051500112 20020515 00112 NM 2002 5 15 SWAA021016 1 20020512 A 5751 6546454 AILERON BOEING 737 7372H4 138448C NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 DURING WALK AROUND INSPECTION, FOUND RT AILERON DELAMINATED ON BOTTOM CENTER. REMOVED AND REPLACED AILERON PER MM.. 2 L 7 2 4F A16WE 2002051500113 20020515 00113 NM 2002 5 15 SWAA021017 1 20020510 A 2731 65C26384 TAB BOEING 737 7375H4 138449D NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002051500114 20020515 00114 NM 2002 5 15 SWAA021018 1 20020512 A 5330 6545776 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR FUSELAGE SKIN CRACKED AT BS 950, UPPER HINGE CUT OUT. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 2002051500115 20020515 00115 NM 2002 5 15 SWAA021019 1 20020511 A 2731 65C2638415A TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED RON, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM . 2 L 7 2 4F RT A16WE 2002051500116 20020515 00116 NM 2002 5 15 SWAA021020 1 20020510 A 2731 65C268425M TAB BOEING 737 7375H4 138449D NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED A1 CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB P ER MM. 2 L 7 2 4F RT A16WE 2002051500117 20020515 00117 NM 2002 5 15 SWAA021024 1 20020511 A 5520 65C2638427A TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, FOUND LT ELEVATOR TAB CRACKED AT NR 1 HINGE CUT OUT. REMOVED AND REPLA CED ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002051500118 20020515 00118 NM 2002 5 15 SWAA021026 1 20020510 A 5230 6547952 SKIN BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED C3 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED 14 INCHES FROM FWD EDGE AND 3 INCHES FROM LOWER EDGE. REPA IRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002051500119 20020515 00119 NM 2002 5 15 SWAA021027 1 20020505 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 450R, BS 385R AND BS 380L. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2002051500120 20020515 00120 NM 2002 5 15 SWAA021028 1 20020505 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, WL 216 R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002051500121 20020515 00121 NM 2002 5 15 SWAA021029 1 20020509 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPECIAL VISIT, FOUND OVERHEAD EMERGENCY EXIT BULL NOSE LIGHT LOOSE AT ROW 7 ABC. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002051500122 20020515 00122 NM 2002 5 15 SWAA021030 1 20020509 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 733E, STR 20L AND BS 729E, STR 18R. REPAIRED S KIN PER SRM. 2 L 7 2 4F RT A16WE 2002051500123 20020515 00123 NM 2002 5 15 SWAA021031 1 20020509 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 355, STR 14L AND BETWEEN BS'S 450 AND 470, RT S IDE OF FUSELAGE CROWN. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002051500124 20020515 00124 NM 2002 5 15 SWAA021032 1 20020507 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10L, BS'S 484, 520 AND 500D + 15. REPAIRED SK IN PER SRM AND SWA RA. 2 L 7 2 4F RT A16WE 2002051500125 20020515 00125 NM 2002 5 15 SWAA021033 1 20020507 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002051500126 20020515 00126 NM 2002 5 15 SWAA021034 1 20020507 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 6, ABOVE STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002051500127 20020515 00127 NM 2002 5 15 SWAA021035 1 20020512 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED BC2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002051500128 20020515 00128 NM 2002 5 15 SWAA021037 1 20020513 A 2130 322684007 OUTFLOW VALVE BOEING 737 7373H4 1384600 NM FWD CARGO ERRATIC A SWAA A D UNSCHED LANDING RETURN TO BLOCK O OTHER CL CLIMB 1 SW 29 643SW 27716 AIR TURN BACK, DUE TO LOUD NOISE/SQUEAL AND CABIN PRESSURIZATION CONTROL FLUCTUATION. REMOVED AND REPLACED FWD CARGO OU TFLOW VALVE PER MM. 2 L 7 2 4F RT A16WE 2002051500129 20020515 00129 2002 5 15 SWAA021040 4 20020512 A 2565 1061323 SLIDE BOEING 737 7375H4 138449D NM AFT SVC DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED A1 CHECK, AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002051500130 20020515 00130 NM 2002 5 15 SWAA021041 1 20020513 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002051500131 20020515 00131 NM 2002 5 15 SWAA021042 1 20020511 A 5312 BAC1517 WEB BOEING 737 7373T5 1384608 NM LT A/C BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED D CHECK, FOUND VERTICAL WEB CORRODED AT BS 545, WL 152 AND LBL 41. REPAIRED WEB PER BFG ER. 2 L 7 2 4F RT A16WE 2002051500132 20020515 00132 NM 2002 5 15 SWAA021043 1 20020513 A 5320 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FWD CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 375 AND 380, WL 209 AND RBL 63. REPAIRED CREASE BEAM PE R SRM. 2 L 7 2 4F RT A16WE 2002051500133 20020515 00133 NM 2002 5 15 VNAA0205008 1 20020514 A 5297 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE GALLEY DOOR FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 440JS 3058 AFTER DEPARTING THE CREW RECEIVED A DOOR SWITCH FAIL AND A PROXI SYSTEM CAS MESSAGE. THE CREW TRIED TO PRESSURIZED THE AIRCRAFT BUT THE AIRCRAFT FAILED TO PRESSURIZE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND RETURNED TO CHS. MA INTENANCE INSPECTED AND REPAIRED THE WIRES ON THE GALLEY DOOR SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00 -00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002051500142 20020515 00142 NM 2002 5 15 2002UALA00805 1 20020503 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 CABIN STATION 827 STRINGER 9R FRAME IS CRACKED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051500145 20020515 00145 CE 2002 5 15 AWO2002F00000 1 20020501 A 3320 S15011 LIGHT CESSNA 185 A185F 2072821 CE CABIN INOPERATIVE A AW0R K NONE L NO TEST IN INSP/MAINT 1 GL 15 105NR 18503956 DURING ANNUAL INSPECTION FOUND LEFT HAND FORWARD DOOR POST LIGHT SWITCH IN CLOSE PROXIMITY TO MAIN FUEL LINES WHICH RUN DOWN FORWARD DOOR POST. THIS AD CALLS FOR AN INSULATOR TO BE INSTALLED ON THE BACK OF THE SWITCH. 1 H 7 1 3O 3A24 2002051500146 20020515 00146 NM 2002 5 15 2002UALA00806 1 20020503 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 CRACK FOUND AT LEFT HAND WHEEL WELL BULKHEAD STATION 665 LBL 32. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051500147 20020515 00147 CE 2002 5 15 CHI2002F00003 1 20020314 A 3250 12606311 ROD END CESSNA 206 U206F 2073333 CE NLG STEERING SHEARED A CHIR K NONE O OTHER IN INSP/MAINT 1 NM 09 77CR 20603458 NOSE GEAR WAS PROBABLY TURNED BEYOND LIMITS REPEATEDLY OVERTIME PUT STRESS ON THREADED PORTION OF THE ROD END. 1 H 7 1 3O A4CE 2002051500148 20020515 00148 NM 2002 5 15 2002UALA00807 1 20020503 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 DAMAGE FOUND FORWARD CABIN STATION 277 RBL 53 UPPER FLOORBEAM HOLE. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051500149 20020515 00149 NM 2002 5 15 2002UALA00808 1 20020504 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 BULKHEAD 178 RIGHT HAND CHORD AT WL 207 NEEDS TO BE REPLACED. MAJOR REPAIR ACCOMPLISHED. REPLACED CHORD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051500150 20020515 00150 CE 2002 5 15 CTU2002F00007 1 20020425 A 8120 4078109001 TURBOCHARGER CESSNA 414 414 2075908 CE ENGINE CRACKED B CTUR K NONE O OTHER IN INSP/MAINT 1 GL 21 4231C 4140531 TURBOCHARGER IS A FACTORY OVERHAULED UNIT. TOTAL TIME OF PART IS UNKNOWN. THE SEAM JUST INSIDE THE EXHAUST INLET FAILE D DUE TO HEAT STRESS WHICH IN TURN CAUSED A PREVIOUS WELDED REPAIR TO CRACK AS WELL. CAUSE OF FAILURE, TO BE RELATED TO HEAT STRESS AND AGE. 1 L 7 2 3O RT A7CE 2002051500151 20020515 00151 NM 2002 5 15 2002UALA00809 1 20020504 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 BODY STATION 178 BULKHEAD RBL 5.7, WL 207 PREVIOUSLY ROUTED OUT FOR ED PROBLEM, AND BULKHEAD SKIN UNDER CHORD ANGLE IS D AMAGED. MAJOR REPAIR ACCOMPLISHED TO AIRCRAFT ANGLE AND SKIN. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051500152 20020515 00152 SO 2002 5 15 DD52002F00000 1 20020408 A 5542 SKIN PIPER PA32 PA32R300 7103213 SO LYC 0540 IO540K1G5D 41532 SO RUDDER CRACKED E DD5A K NONE O OTHER IN INSP/MAINT 1 CE 05 6249J 596 32R7680340 L1975048A CRACKS ON TRAILING EDGE SKIN OF RUDDER. CRACKS IN AREA OF STIFFENER BEADS. 1 L 7 1 3O 3 O A3SO 1E4 2002053000069 20020530 00069 NM 2002 5 30 2002UALA00810 1 20020507 A 5320 CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 AFT PIT FUSELAGE STRINGER TO FRAME ATTACH CLIP GOUGED AT BODY STATION 727B STRINGER 26 RIGHT. MAJOR REPAIR ACCOMPLISHED . REPLACED ATTACH CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051500153 20020515 00153 WP 2002 5 15 EOO2002F00003 1 20020228 A 6230 369027609501 SWASHPLATE HUGHES 369 369D 4470706 WP MAIN ROTOR WORN B EOOR K NONE O OTHER IN INSP/MAINT 1 AL 03 C6PHC 5578 180257D DURING REGREASE OF THE MAIN ROTOR SWASHPLATE, IT WAS DISCOVERED THAT THE ROLLER BEARING ASSEMBLY WAS LOOSE AND SPINNING IN THE ROTATING SPAR - REPLACED UNIT WITH A SERVICEABLE UNIT. 1 G 7 1 3U H3WE 2002051500154 20020515 00154 NM 2002 5 15 2002UALA00811 1 20020505 A 5320 WEB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 934UA 26662 AFT PIT DOORWAY STATION 792-847 WL 160 RBL 21, WEB BLENDED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051500155 20020515 00155 GL 2002 5 15 EOO2002F00004 2 20020225 A 7230 6850921 FITTING HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ENGINE UNAPPROVED PART A EOOR K NONE O OTHER IN INSP/MAINT 1 AL 03 CGPHC 180257D CAE833793 WHILE READING THE COMPRESSOR FOR SHIPMENT AND REMOVING THE P/C FITTINGS (6850921), TO THAT END, IT WAS DISCOVERED THE UNITS DID NOT PASS THE CEB-1374, AND INSPECTION OF THE BRAZE FILLET. BOTH UNITS WERE REPLACED WITH SERVICEABLE PARTS. 1 G 7 1 3U 3 U H3WE E4CE 2002051500156 20020515 00156 NM 2002 5 15 2002UALA00812 1 20020505 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 CABIN FRAME 951 AT STRINGER 5R & 6R HAS FASTENER HOLES OVERSIZED PAST LIMITS. HOLES INDICATED CRACK FREE AT .2802, LIMI T .233. MAJOR REPAIR ACCOMPLISHED. INSTALLED FREEZE PLUGS. ALSO INSTALLED REPAIR FILLER, DOUBLER AND TAPERED SHIMS ON FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2002053000074 20020530 00074 NM 2002 5 30 2002UALA00813 1 20020505 A 2130 106070467 CONTROL VALVE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 311UA 23672 RETURNED TO DEN DUE TO UNABLE TO PRESSURIZE CABIN. LANDED OVERWEIGHT. THE AUTO FLOW CONTROL VALVE (FOUR-INCH) FAILED T O CLOSE. REPLACED THE AUTO FLOW CONTROL VALVE, THEN PRESSURIZED AIRCRAFT USING BOTH APU AND ENGINE BLEED PRESSURE TO EN SURE CORRECT OPERATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002053000075 20020530 00075 NE 2002 5 30 2002UALA00814 2 20020505 A 7530 32144464 VALVE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE MALFUNCTIONED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 347UA 24251 ABORTED TAKEOFF TWICE DUE TO NR 1 ENGINE BLEED LIGHT. A FAILURE OF THE HIGH STAGE VALVE OPENING AFTER BLEED SHIFT POINT CAUSING BLEED TRIP. REPLACED THE HIGH STAGE VALVE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051500157 20020515 00157 NM 2002 5 15 2002UALA00815 1 20020409 A 3350 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 955UA 26703 EMERGENCY EXIT LIGHT FLOOR MOUNTED LIGHTING STRIP AFT OF SEAT ROW 13 INOPERATIVE. REPLACED POWER STRIP & EMERGENCY EXIT LIGHT AS NEEDED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051500158 20020515 00158 NM 2002 5 15 2002UALA00816 1 20020429 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 306UA 23667 THERE IS A 2.5 INCH CRACK IN FUSELAGE COMING OFF LOWER AFT RADIUS OF DOOR 1R OPENING. MAJOR REPAIR ACCOMPLISHED. THREE LAYER REPAIR USED DUE TO CRACK THROUGH STRAP, SKIN & BONDED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051500159 20020515 00159 WP 2002 5 15 P2EA2002V0033 1 20020502 A 5310 SKIN DOUG DC9 DC982 3022082 WP DENTED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 130NJ 49222 DURING C1+C2 INSPECTION:-PERFORM PERMANENT REPAIR @ BS Y237, LONGERON 16 L-H.-FUSELAGE SKIN SECTION REPAIRED FROM BS Y22 3 TO BS Y263, BETWEEN LONGERON 15 & 18 L-H DUE TO TEMPORARY REPAIR IAW COOPESA E.O. No. COO-9-53-275-02 DATED MAY 08,200 2 & DOCUMENTED ON FAA 8110-3 FORM.NOTE:SEE COOPESA WORK ORDER No. P1-0430 1-1, VAM100 No.006 & 130SDA002. 2 L 7 2 4F A6WE 2002051500160 20020515 00160 NM 2002 5 15 2002UALA00817 1 20020503 A 2697 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE OVERHEAT SYS CHAFED A UALA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 182UA 25279 CREW REPORTS RIGHT BLEED DUCT LEAK, FOLLOWED FLIGHT MANUAL ISLN PROCEDURE AND INDIC REMAINED INTERMITTENT. NR 4 DUCT PR ESS WAS 14 PSI WITH VALVE DESELECTED. AFTER CREW REPORTED A (POSSIBLE) RIGHT BLEED DUCT LEAK ON CLIMB WITH MESSAGE EV ERY MINUTE AT FL250 AIRCRAFT, AKLMM FOUND NO DUCT LEAK BUT RESISTANCE CHECKS FROM THERMAL SWITCH (S890) TO STA 631 IDENT IFIED A SHORT IN INDICATION WIRING. CHAFED INSULATION ON WIRES (W642) UNDER P-CLAMP, MIDWAY FROM THERMAL SWITCH (S890) AND CONNECTOR D4644J ON WING WAS REPAIRED. ALL WIRE STRANDS WERE FOUND WITHOUT DAMAGE. 2 L 7 4 4F 4 F RT A20WE E24NE 2002060600178 20020606 00178 NE 2002 6 6 2002UALA00818 2 20020504 A 7261 AC9806F30Y1 OIL FILTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE DIRTY A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 513UA 376 24810 727201 RIGHT ENGINE OIL FILTER LIGHT ILLUMINATED. OIL FILTER AND CHIP DETECTORS CHECKED CLEAN. BYPASS SWITCH CHECKED GOOD. O IL FILTER REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002060600182 20020606 00182 NM 2002 6 6 2002UALA00819 1 20020505 A 3233 273N10045 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG BYPASSING A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 511UA 24799 GEAR UP DISAGREE LIGHT ILLUMINATED. NLG RETRACT ACTUATOR BYPASSING AND NOT RETRACTING GEAR. REPLACED NLG RETRACT ACTUA TOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051500161 20020515 00161 NM 2002 5 15 2002UALA00821 1 20020503 A 5320 BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 CABIN FLOOR STATION 345-365 BELOW I-BEAM IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. I-BEAM REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051500162 20020515 00162 NM 2002 5 15 2002UALA00825 1 20020505 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 CABIN FLOORBEAM STATION 1420 TOP SURFACE HAS GOUGES AROUND FASTENER HOLES, LBL 18 TO RBL 5 AT WL 208. MAJOR REPAIR ACCO MPLISHED. INSTALLED REINFORCEMENT STRAPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051500163 20020515 00163 NM 2002 5 15 2002UALA00826 1 20020505 A 5320 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 CABIN INTERCOSTAL BETWEEN STATION 540 AND 560 AT C-L UPPER ANGLE MISDRILLED AND WEB WAS DAMAGED. MAJOR REPAIR ACCOMPLIS HED. INTERCOSTAL UPPER ANGLE AND WEB REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051500164 20020515 00164 NM 2002 5 15 2002UALA00830 1 20020506 A 5320 ANGLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 MID CABIN DOOR SILL Z-ANGLE INNER AT STATION 720 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH A NEW SILL BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051500165 20020515 00165 NM 2002 5 15 2002UALA00831 1 20020507 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 CABIN FLOORBEAM UPPER CAP STATION 1640, RBL 51 CORRODED. MAJOR REPAIR ACCOMPLISHED. STRAP REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000073 20020530 00073 NM 2002 5 30 2002UALA00832 1 20020507 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 EXTERNAL FUSELAGE SKIN DENTED FROM STATION 1016 TO 1040 STRINGER 26L TO 27L. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED A ND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002053000079 20020530 00079 2002 5 30 2002UALA00833 4 20020507 A 3160 6229436101 SYMBOL GENERATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E/E BAY FAILED A UALA C ABORTED TAKEOFF I FLT. ATTITUDE INST. TO TAKEOFF 1 WP 29 395UA 24670 ABORTED TAKEOFF AT 100 KNOTS AFTER CAPTAINS ELECTRONIC ATTITUDE DIRECTION INDICATOR WENT BLANK. MAINTENANCE CONDUCTED A N EFIS BITE TEST VIA THE DFCS, RESULTING THE REPLACEMENT OF THE NR 1 SYMBOL GENERATOR MR41824-281. COMPONENT SHOP FOUND THAT THE UNIT HAD A CONFIRMED FAILURE OF THE A8U36 EEPROM DEVICE. ADDITIONAL DEVICES REPLACED AS A PRECAUTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072200015 20020722 00015 NM 2002 7 22 2002UALA00834 1 20020507 A 3250 30420001 ACTUATOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NLG MALFUNCTIONED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 796UA 26931 ABORTED TAKEOFF AT ABOUT 80 KTS DUE TO GEAR CONFIGURATION RED WARNING LIGHT AND HORN COMING ON. A/C TAXIED OFF RUNWAY W ITHOUT INCIDENT. ONE OF THE MAIN GEAR STEERING POWER CONTROL ACTUATORS (PCA) MAY BE SLOW TO LOCK OR IS LOCKING INTERMIT TENTLY. THE PCA WAS REPLACED. REMOVED PCA SENT TO AN OUTSIDE VENDOR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002051500166 20020515 00166 2002 5 15 COMA0260309 4 20020513 A 3410 PITOT LINE CNDAIR CL600 CL6002B19 1900309 EA A COMA J DUMP FUEL S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 868CA 7427 FLIGHT 5397 T/O ABORTED BECAUSE OF COPILOT AIRSPEED INDICATOR AMBER FLAG.PURGED PITOT/STATIC SYSTEM; SYSTEM CHECK SATISF ACTORY. 2 L 7 2 4F RT A21EA 2002051500167 20020515 00167 NM 2002 5 15 2002UALA00835 1 20020507 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 CABIN FLOORBEAM 1681 RBL 12 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND ANGLE REPAIRS WITH FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051500168 20020515 00168 NM 2002 5 15 2002UALA00836 1 20020507 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 AFT CABIN PRESSURE DECK CORRODED AT STATION 1681 RBL 12. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051500169 20020515 00169 NM 2002 5 15 2002UALA00840 1 20020507 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 BODY STATION 1219 LBL 30 T-CAP CORRODED UNDER NUT PLATES. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002051500170 20020515 00170 NM 2002 5 15 2002UALA00841 1 20020507 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 BODY STATION 852 LBL 55 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002051500171 20020515 00171 EA 2002 5 15 COMA0260310 1 20020510 A 7920 6087T04P05 PUMP CNDAIR CL600 CL6002B19 1900309 EA R/H LEAKING A COMA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 01 976CA 16971 7151 FLIGHT 5354 R/H ENGINE LOW OIL PRESSURE WARING IFSD.THE SCAVANGE LUBE PUMP WAS LEAKING AT THE PRESSURE SWITCH - REPLACED LUBE PUMP. 2 L 7 2 4F RT A21EA 2002051500172 20020515 00172 NM 2002 5 15 PCAA0205057 1 20020514 A 2933 82970009171 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM #1 NACELLE LEAKING A PCAA K NONE K FLUID LOSS LD LANDING 1 EA 13 816EX 329 PHL FLIGHT#3726. CREW REPORTED #2 HYDRAULIC QUANTITY DROPPED TO .5 (QUART) ON LANDING. HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED. MAINTENANCE REMOVED A RIGID HYDRAULIC LINE IN #1 NACELLE, FOR GEAR DOOR UPLOCK ACTUATOR. TEMPORARY F LEX LINE INSTALLED. GROUND RAN #2 ENGINE, AND BLED SYSTEM. OPERATIONAL CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2002051500173 20020515 00173 NM 2002 5 15 AWXA200200420 1 20020512 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM CABIN MISSING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 LAS - EEL - FLIGHT CREW REPORTED EMERGENCY LIGHT MISSING AT SEAT ROW 17 LT. MAINTENANCE INSTALLED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 17 LT IAW SWPM 20-30-12, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002051500174 20020515 00174 SO 2002 5 15 C2XA02CL110 1 20020507 A 5610 163500112 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT CRACKED A C2XA K NONE O OTHER CR CRUISE 1 SW 27 14907 2081 145468 CLE FLIGHT 3094 THE CREW REPORTED THE RIGHT WINDSHIELD SHATTERED IN FLIGHT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDEN T. MAINTENANCE REPLACED THE RIGHT WINDSHIELD. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002051500175 20020515 00175 WP 2002 5 15 EOO2002F00005 1 20020225 A 6230 369D27600 MIXER BOX HUGHES 369 369D 4470706 WP MAIN ROTOR WORN B EOOR K NONE O OTHER IN INSP/MAINT 1 AL 03 C6PHC 1802570 DURING AN ANNUAL INSPECTION IT WAS FOUND THAT THE MAIN ROTOR SWASHPLATE WAS FREE TO MOVE VERTICALLY TOWARD THE FRONT ABO UT .7500 OF AN INCH. THE ROOT CAUSE WAS SLOP ON MOST OF THE BEARINGS OF THE MIXER BUT THE WORST WAS ABOUT THE PIVOT POI NT OF THE LATERIAL BELLCRANK. REPLACED UNIT WITH A SERVICEABLE PART. 1 G 7 1 3U H3WE 2002051500176 20020515 00176 EA 2002 5 15 FL80981 2 20020416 A 7414 IO382584 CONTACTOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA RT MAG LT ENG LOOSE A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 4112K 975 318353006 RL599161A PILOT REPORTED INOPERATIVE RIGHT MDG ON LEFT ENGINE. UPON INSPECTION OF MAGNETO, THE CONTACT ASSEMBLY WAS FOUND TO BE T HE CAUSE. THE TWO RIVETS THAT HOLD THE CAM FOLLOWER ONTO THE CONTACT ASSEMBLY WERE LOOSE. ITLOOKS LIKE THE SLOT HEADS HAVE WORN INTO THE CAM FOLLOWER MANUAL. 1 L 7 2 3O 3 O A20SO E14EA 2002051500179 20020515 00179 CE 2002 5 15 HYI2002F00012 1 20020409 A 3213 51411012 STRUT CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO RT MLG DAMAGED D HYIA K NONE O OTHER IN INSP/MAINT 1 NM 01 618CA 5000 402C0620 DURING TAXI, RIGHT MAIN LANDING GEAR STRUT ASSEMBLY BROKE AT ACTUATOR ATTACH COLLAR. UPON INSPECTION, FOUND STRUT HAD L OST NITROGEN CHARGE AND HAD BEEN TAXIED IN THE FULLY DEPRESSED POSITION, POSSIBLY DAMAGING THE STRUT INTERNALLY. THE LA NDING GEAR DID NOT RETRACT SUCCESSFULLY AND THEN THE AIRCRAFT LANDED WITH THE GEAR JAMMED IN THE FULLY EXTENDED POSITION CAUSING THE UPPER BARREL TO FRACTURE AND FINALLY FAILED COMPLETELY WHILE TAXING TO THE GATE. 1 L 7 2 3O 3 O A7CE E8CE 2002051500180 20020515 00180 EA 2002 5 15 MGDA20021 2 20020507 A 8550 ENGINE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCC3Y HCC3YR2 NE LEFT MALFUNCTIONED E MGDA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 NM 03 27309 317752135 L724261A DJ11152A LEFT ENGINE LOST MANIFOLD PRESSURE AND RPM IN LEVEL CRUISE AT 16,000 FEET. PILOT ATTEMPTED TO KEEP THE ENGINE RUNNING W ITHOUT SUCCESS. PILOT SHUT DOWN THE ENGINE AND FEATHERED IT. AN EXACT CAUSE OF THE FAILURE HAS NOT BEEN DETERMINED. 1 L 7 2 3O 3 O A20SO E14EA 5 C P25EA 2002051500181 20020515 00181 SW 2002 5 15 MV52002F00002 1 20020425 A 5511 430010251 RIB GULSTM 690TP 695A 7630519 SW HORIZONTAL STAB CRACKED B MV5R K NONE O OTHER IN INSP/MAINT 1 GL 11 695AB 6682 96055 RIGHT HORIZONTAL STABILIZER RIB CRACKED. RIB LOCATED AT LEADING EDGE. 1 H 7 2 4T 2A4 2002051500182 20020515 00182 SW 2002 5 15 MV52002F00004 1 20020425 A 5511 43001081 RIB GULSTM 690TP 695A 7630519 SW HORIZONTAL STAB CRACKED B MV5R K NONE O OTHER IN INSP/MAINT 1 GL 11 695AB 6682 96055 RIGHT HORIZONTAL STABILIZER RIB CRACKED RIB LOCATED AT LEADING EDGE. 1 H 7 2 4T 2A4 2002051500183 20020515 00183 SW 2002 5 15 O9I2002F00002 1 20020424 A 5531 410008197 RIB GULSTM 690TP 690B 7630516 SW GARRTT TPE331 TPE3310T WP VERT STAB CRACKED B O9IR K NONE O OTHER IN INSP/MAINT 1 NM 09 60DB 5635 11420 DURING A ROUTINE PERIODIC INSPECTION A CRACK WAS FOUND IN VERTICAL STABILIZER BOTTOM RIB (PN 410008197) . THE CRACK RA DIATED FROM THE SIDE FLANGE (LEFT) FORWARD RIVET AND EXTENDED TO THE EDGE OF THE RIB. THE TOTAL CRACK LENGTH IS .375 IN CH. THE LOWER RIB OF THE VERTICAL STABILIZER SEEMS TO BE A CRACK PRONE AREA . 1 H 7 2 3T 4 T 2A4 E4WE 2002051500185 20020515 00185 SO 2002 5 15 UM92002F00000 1 20020425 A 6700 S14402104 LEVER ORLHEL H19 CH19ESKRSKY 8141616 SO CYCLIC STICK CRACKED A UM9A K NONE O OTHER IN INSP/MAINT 1 NM 13 94475 130141 DURING A PREFLIGHT INSPECTION IT WAS NOTED THAT THE LEFT CYCLIC INPUT LEVER ATTACHED TO THE MAIN TRANSMISSION WAS CRACKE D. PART WAS REMOVED FROM SERVICE PROBABLE CAUSE OF FAILURE IS COMPONENT AGE. 1 G 7 1 3R HR1SO 2002051500186 20020515 00186 CE 2002 5 15 VJ32002F00027 1 20020426 A 3230 SM50D7 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MLG STUCK B VJ3R A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 07 1569A CE1328 820447R LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. AIRCRAFT WAS PLACED ON JACKS AND THE LANDING GEAR CYCLED IAW MM. INSPEC TION OF THE SYSTEM FOUND THAT THE DYNAMIC RELAY WOULD STICK IN THE DOWN POSITION. A NEW DYNAMIC RELAY WAS INSTALLED AN D THE SYSTEM OPERATIONAL CHECKED NORMAL. 1 L 7 1 3O 3 O 3A15 E5CE 2002051500187 20020515 00187 CE 2002 5 15 VJ32002F00028 1 20020426 A 3600 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO AIR PUMP INOPERATIVE B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 1565A CE1331 825752R LOW OUT PUT FROM PUMP TO AIRCRAFT, REMOVED PUMP AND INSTALLED NEW PUMP OPERATION WAS NORMAL. PUMP SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002051500188 20020515 00188 EU 2002 5 15 VJ32002F00029 1 20020426 A 2420 115TA6003 BRACKET GROB ASTIR G102ASTIR 1660104 EU LYC O540 AEIO540D4A5 41532 EA ALTERNATOR CRACKED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 863AF 76 85003 L2802548A ALTERNATOR SUPPORT BRACKET CRACKED. PART REMOVED AND A NEW SUPPORT BRACKET INSTALLED. PART SENT IN FOR WARRANTY. 1 K 0 0 3 O G33EU 1E4 2002051500189 20020515 00189 EA 2002 5 15 WVB2002F00001 2 20020502 A 8520 CONNECTING ROD PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE DAMAGED A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 59764 5682 317652037 RL159361A DURING INSPECTION A LARGE PIECE OF CAST ALUMINUM WAS FOUND IN THE SUCTION SCREEN. THE ODD BANK OF CYLINDERS WERE REMOVE D TO LOOK FOR DAMAGE. NR 6 CONNECTING ROD CAP WAS OBSERVED TO BE SCUFFED. SEVERAL ACCESSORIES WERE REMOVED AND NO DAMA GE WAS NOTED IN THE ACCESSORIES SECTION. ENGINE WAS REMOVED AND REPLACED TEAR DOWN REPORT PENDING. 1 L 7 2 3O 3 O A20SO E14EA 2002051500190 20020515 00190 SO 2002 5 15 WVB2002F00002 1 20020507 A 3010 2H598 VALVE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA DEICER STUCK E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 3582P 318052103 L494561A PILOT COMPLAINED OF WING DE-ICE BOOTS STAYING INFLATED. REMOVED VALVE AND FOUND IT STUCK IN INFLATION MODE DUE EXCESSIV E SPACE BETWEEN THE GASKETS. THIS ALLOWS AIR PRESSURE TO VENT WHICH IS THE ACTUATION MODE FOR INFLATION. IT APPEARS TH AT THE SQUEEZE ON THE RIVETS MAY BE TOO LIGHT. PART WAS REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 2002051500191 20020515 00191 WP 2002 5 15 DHL2002801011 1 20020514 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP A DHLA O OTHER J WARNING INDICATION IN INSP/MAINT 1 SO 01 801DH 46033 1) WHEN SELECTING NO.2 ENG "B" LOOP, FIRE WARNING ACTIVATED INSTANTANEOUSLY. (WITHOUT SELECTING SHORTED LO OP OR FIRE WARN TEST)2) REPLACED CONNECTOR ON "B" LOOP. SYS LOOP P1-7050. SYS CHKS GOOD PER DC-8 MM 26-10-1 2 L 7 4 4F RT 4A25 2002051500192 20020515 00192 WP 2002 5 15 DHL2002801012 1 20020515 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 801DH 46033 1) ON T/O MASTER FIRE LIGHT ILLUMINATED AND BELL SOUNDED.REJECTED T/O ,BELIEVED TO BE #2 ENG RAN ENGINE FIRE EMERGENCY CHECKLISTAND SHUTDOWN #2MAX SPEED AT REJECT 70 KIAS2) FOUND #2 B-LOOP GIVING FALSE FIRE INDICATION.DEFERRED #2 ENG B-LO OP PER MEL 26-2-3 DMI # 9324 PLAC INSTALLED 2 L 7 4 4F RT 4A25 2002051500193 20020515 00193 EA 2002 5 15 WVBA2002010 2 20020507 A 8530 72257 TUBE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA PUSHROD TUBE CRACKED E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 59764 317652037 L785161A PILOT RETURNED FROM FLIGHT AND NOTIFIED MAINTENANCE OF AN OIL LEAK ON THE LEFT ENGINE. IT WAS DISCOVERED THAT A LEAK WA S COMING FROM NR 2 CYLINDER EXHAUST PUSHROD TUBE. WHEN THE TUBE WAS REMOVED A CRACK WAS FOUND APPROXIMATELY 4 INCHES FR OM THE CYLINDER END. THE CRACK STARTED AT A DENT IN THE TUBE WHICH SEEMS TO BE FROM SHIPPING DAMAGE. AS THIS ENGINE WA S NOT SHIPPED IN STANDARD CRATE SUCH AS THE MFG USES. THE PART WAS REMOVED AND REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 2002051500194 20020515 00194 SO 2002 5 15 WVBA2002012 1 20020507 A 3010 2H598 VALVE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA DEICER VALVE FAULTY E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 42WP 318252038 RL604551A DURING SCHEDULED INSPECTION FOUND DE-ICE WING LIGHT INOPERATIVE TROUBLESHOOTING REVEALED FAULTY DE-ICE VALVE, NEW VALVE, INOPERATIVE AS DELIVERED APPEARS THAT TOO MUCH AIR PRESSURE WAS DUMPING REPLACED VALVE. 1 L 7 2 3O 3 O A20SO E14EA 2002051500195 20020515 00195 NM 2002 5 15 UPS02438247 1 20020513 A 5340 SEAT TRACK BOEING 747 747200 1384847 NM FLIGHT DECK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 528UP 1 INSPECTION TYPE:N/A F/O SEAT TRACK IS CRACKED REMOVED AND REPLACED PILOTS SEAT TRACK 2 L 7 4 4F RT A20WE 2002051500196 20020515 00196 SO 2002 5 15 C2XA02CL114 1 20020511 A 2121 4611028900 FAN EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 12519 2518 145366 EWR FLIGHT 3406 CREW REPORTED BURNING SMELL COMING FROM PACK #1.NO SMOKE FOUND WHEN PACK #1 WAS DESELECTED SMELL WENT AW AYMAINTENANCE REPLACED #1 PACK RECIRCULATION FAN. OPERATIONAL CHECKS WERE GOOD.AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002051600005 20020516 00005 CE 2002 5 16 BLI2002F00001 1 20020320 A 2421 ALTERNATOR CESSNA 421 421B 2076014 CE CONT O520 GTSIO520F 17032 SO LEFT FAILED E BLIA K NONE O OTHER IN INSP/MAINT 1 SW 99 65AE 421B0953 LEFT ALTERNATOR FAILED TO COME ON LINE WHEN DEPARTURE WAS ATTEMPTED. ALTERNATOR WAS SHIPPED BY US TO REPAIR STATION. T HEY INSTALLED IT AND THE AIRCRAFT WAS RETURNED TO SERVICE AND TO OUR FACILITY. 1 L 7 2 3O 3 O A7CE E7CE 2002051600006 20020516 00006 EA 2002 5 16 JQV2002F00001 1 20020417 A 6230 SAEW12 LOCKWASHER SCWZER 269 269D 8059501 EA SWASHPLATE WORN E JQVA K NONE O OTHER IN INSP/MAINT 1 EA 17 269MS 152 S1813 REMOVE MAIN ROTOR BLADES AND DISASSEMBLE MAIN ROTOR HUB TO GAIN ACCESS TO SWASHPLATE DISASSEMBLE, FOUND WORN LOCKWASHER, REPLACED SAME. CLEANED, INSPECTED, AND RELUBED. REASSEMBLE PREVIOUSLY REMOVED COMPONENTS. 1 G 7 1 3U 0 4H12 2002051600007 20020516 00007 NM 2002 5 16 2002F00460 1 20020328 A 5312 BULKHEAD BOEING 727 727225 1384077 NM CARGO BAY CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND THREE CRACKS AT FORWARD PIT AFT BULKHEAD CENTER PANEL. (M) 2 L 7 3 4F A3WE 2002051600008 20020516 00008 NM 2002 5 16 2002F00461 1 20020328 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM FUSELAGE GOUGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND SEAT TRACK GOUGED AT STATION 848 TO 870 RB 44. (M) 2 L 7 3 4F A3WE 2002051600009 20020516 00009 NM 2002 5 16 2002F00462 1 20020328 A 5320 PANEL BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND CORROSION IN AFT PIT AT RIGHT TRANSITION PANEL TOP SIDE FROM STATION 950A TO 1066. (M) 2 L 7 3 4F A3WE 2002051600010 20020516 00010 NM 2002 5 16 2002F00463 1 20020328 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME UPPER CHORD CRACKED AT STATION 600 RBL 3. (M) 2 L 7 3 4F A3WE 2002051600011 20020516 00011 NM 2002 5 16 2002F00474 1 20020323 A 5755 BRACKET BOEING 727 727225 1384077 NM SPOILER ATTACH DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND NR 3 SPOILER INBOARD ATTACH BRACKET WITH TWO ELONGATED HOLES AT STATION 507 AND 515. (M) 2 L 7 3 4F A3WE 2002051600012 20020516 00012 NM 2002 5 16 2002F00475 1 20020325 A 5320 FLOOR SUPPORT BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STATION 644 RBL 9. (M) 2 L 7 3 4F A3WE 2002051600013 20020516 00013 NM 2002 5 16 2002F00476 1 20020328 A 5320 ANGLE BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND L-ANGLE CRACKED BELOW FORWARD CARGO DOOR CUTOUT, FORWARD WEB AT STATION 560 BETWEEN STRINGER 23 AND 24 R. (M) 2 L 7 3 4F A3WE 2002051600014 20020516 00014 NM 2002 5 16 2002F00477 1 20020328 A 5320 WEB BOEING 727 727225 1384077 NM FUSELAGE TORN A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND AFT CARGO DOOR CLOSE OUT WEB TORN AT STATION 620 ABOVE STRINGER 26R. (M) 2 L 7 3 4F A3WE 2002051600015 20020516 00015 2002 5 16 2002F00479 4 20020406 A 3442 DISPLAY DHAV DHC8 DHC8202 2809007 NM WX RADAR CONTAMINATED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 434YV 434 FLT 6207 - RETURNED TO FIELD BECAUSE WEATHER RADAR DISPLAY WENT BLANK AND WOULD NOT RESET. MAINTENANCE FOUND WATER IN S EPARATOR. CLEANED AND REPLACED DESICANTOR. OP CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 2002051600016 20020516 00016 EA 2002 5 16 2002F00480 1 20020121 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA AFT CEILING INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27173 7173 WHILE PERFORMING SERVICE CHECK NOTICED AFT CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED IAW 33-15-16. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002051600017 20020516 00017 EU 2002 5 16 C2XA02IA105 1 20020513 A 3350 3351106 WIRE AEROSP ATR42 ATR42320 8680930 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14834 193 IAH- DURING 1A CHECKIT WAS NOTED THAT THE AFT SERVICE DOOR EMERGENCY LIGHTON BOTTOM OUT. IAH- MAINTENANCE REPAIRED WI RE NUMBER3351-106 ON EXIT SIGN, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002051600018 20020516 00018 SO 2002 5 16 2002F00481 1 20020316 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DIRTY A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145416 FLT 6645 - PIT-BHM - DURING PREFLIGHT, CAPTAIN NOTICED TWO FLOOR PROXIMITY LIGHT STRIPS INOPERATIVE. MAINTENANCE INSPEC TED, CLEANED AND RECONNECTED LIGHT STRIP CONNECTORS. (M) 2 L 7 2 4T RT T00011AT 2002051600019 20020516 00019 SO 2002 5 16 2002F00482 1 20020317 A 3350 7267580501 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145416 FLT 5740 - PIT-CRW - DISCOVERED THE SECOND AND THIRD EMERGENCY EXIT LIGHTS STRIPS INTERMITTENTLY INOPERATIVE. MAINTENAN CE SECURED STRIPS. OP CHECKS GOOD. (M) 2 L 7 2 4T RT T00011AT 2002051600020 20020516 00020 EA 2002 5 16 2002F00483 1 20020317 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27173 7173 DURING ROUTINE MAINTENANCE, FOUND THE NR 5 EMERGENCY EXTERIOR LIGHT INOPERATIVE AT FS 416.50. REMOVED AND REPLACED LIGH T BULB. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002051600021 20020516 00021 SO 2002 5 16 2002F00484 1 20020317 A 3350 7267580501 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145359 FLT 5780 - PIT-GSO - DURING PREFLIGHT, CAPTAIN NOTICED TWO FLOOR PROXIMITY LIGHT STRIPS INOPERATIVE. MAINTENANCE INSPEC TED AND FOUND SYSTEM TO BE OPERATING NORMALLY. (M) 2 L 7 2 4T RT T00011AT 2002051600022 20020516 00022 SO 2002 5 16 2002F00485 1 20020317 A 3397 WIRE EMB 145 EMB145LR 3260212 SO FLOOR LIGHT BROKEN A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 828MJ 145218 FLT 5755 - BHM-PIT - FLOOR PROXIMITY LIGHTING INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OP CHECKS GOOD. (M) 2 L 7 2 4T RT T00011AT 2002051600023 20020516 00023 SO 2002 5 16 2002F00486 1 20020318 A 3350 7267580501 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST CR CRUISE 1 SW 07 828MJ 145218 FLT - 5741 - DURING FLIGHT F/A NOTICED TWO FLOOR PROXIMITY LIGHT STRIPS INOPERATIVE. UPON LANDING MAINTENANCE WAS NOTIF IED. MAINTENANCE REPLACED THE FLOOR LIGHTING STRIPS. OP CHECKS GOOD. (M) 2 L 7 2 4T RT T00011AT 2002051600024 20020516 00024 SO 2002 5 16 2002F00487 1 20020403 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145359 FLT 5815 - CLT-HSV - PILOT REPORTED THAT ROWS 4-7 EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE CONNECTED THE CONNECTO R. OP CHECKS GOOD. (M) 2 L 7 2 4T RT T00011AT 2002051600025 20020516 00025 SO 2002 5 16 2002F00488 1 20020404 A 3350 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 851MJ 145572 EMERGENCY LIGHTS GO ON WHEN SWITCH PUT IN THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND THE B ATTERY. OP CHECKS GOOD. (M) 2 L 7 2 4T RT T00011AT 2002051600026 20020516 00026 2002 5 16 2002F00489 4 20020405 A 3418 CONNECTOR EMB 145 EMB145LR 3260212 SO STALL WARNING LOOSE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 825MJ 145179 FLT 5717 - IN GSP, ABORTED TAKEOFF ROLL DUE TO SPS 1 AND 2 INOPERATIVE AND STICK SHAKER FAIL MESSAGE. MAINTENANCE RESEA TED CONNECTOR PLUG TO STICK SHAKER AND REMOVED AND REINSTALLED SPSP COMPUTER. MESSAGE CLEARED. SYSTEM OP CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002051600027 20020516 00027 EA 2002 5 16 2002F00490 1 20020403 A 3200 UPLOCK CNDAIR CL600 CL6002B19 1900309 EA NLG DAMAGED A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 17175 7175 FLT 5732 - PIT-PHL - RETURNED TO PHL, DUE TO NOSE LANDING GEAR DISAGREE TAKEOFF. MAINTENANCE REPLACED THE UPLOCK MECH. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002051600028 20020516 00028 EA 2002 5 16 2002F00491 1 20020409 A 3350 BC10020004 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37208 7208 FLT 5819 - CVG-PHL - DUIRNG OVERNIGHT MAINTENANCE NOTED THAT ONE CABIN EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE FLOOD LIGHT. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002051600029 20020516 00029 EA 2002 5 16 2002F00492 1 20020414 A 3350 363782 LIGHT CNDAIR CL600 CL6002B19 1900309 EA MAIN CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17217 7217 FLT 6152 - TUS-PHX - DURING MAINTENANCE IT WAS DISCOVERED THAT ONE CABIN EMERGENCY PROXIMITY LIGHT STRIP WAS INOPERATIVE . REPLACED LIGHT STRIP. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002051600030 20020516 00030 EU 2002 5 16 2002F00493 1 20020505 A 2810 L95F50603 VALVE AIRBUS 320 A320233 3930329 EU LT WING TANK DAMAGED A SOKF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 483TA 1509 FLT GU970 - SJO-GUA - DURING CRUISE, AN IN FILGHT FUEL TRANSFER WAS EXPERIENCED FROM RIGHT TANK TO THE LEFT, AND CENTER TANK. AIRCRAFT DIVERTED ITS FLIGHT TO EL SALVADOR STATION FOR MAINTENANCE. AFTER LANDING, TECHNICIANS PERFORMED INSPEC TION TO THE LEFT WING OVERPRESSURE PROTECTOR VALVES AS PER AMM 28-12-41 AND FOUND THAT THE OVERPRESSURE VALVE BETWEEN IN NER AND OUTER CELL DAMAGED. ENTERED ON DEFERRED DEFECT SHEET, PER MEL 28-12-01 ITEM 1. THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2002051600031 20020516 00031 NM 2002 5 16 2002F00494 1 20020328 A 5310 SHEAR TIE BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND SHEAR TIE CORRODED AT COMPARTMENT FRAME STATION 720A LBL 10. (M) 2 L 7 3 4F A3WE 2002051600032 20020516 00032 NM 2002 5 16 2002F00495 1 20020328 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME CRACKED AT STATION 560 RBL 3. (M) 2 L 7 3 4F A3WE 2002051600033 20020516 00033 NM 2002 5 16 2002F00496 1 20020328 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND CORROSION ON FRAME AT FORWARD ACCESS COMPARTMENT AFT OF DOOR AT STATION 227. (M) 2 L 7 3 4F A3WE 2002051600034 20020516 00034 NM 2002 5 16 2002F00497 1 20020402 A 5320 FLOOR SUPPORT BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND AFT PIT FLOOR SUPPORT CRACKED AT STATION 950F LBL 4. (M) 2 L 7 3 4F A3WE 2002051600035 20020516 00035 2002 5 16 A6WA200240010 4 20020421 A 3417 8220372140 ADC CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A A6WA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 GL 31 402AW 7281 MACH TRIM FAIL CAS, F/O ALT AND VERTICAL SPEED INDICATION DISAPEARED. ELT AND VSI RED MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2002051600036 20020516 00036 EA 2002 5 16 A6WA200240012 1 20020428 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A A6WA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 405AW 7362 PILOTS SIDE WINDOW SHATTERED IN FLIGHT MAINTENANCE REMOVED AND REPLACED PILOT 'B' SCREEN. OPERATIONAL AND PRESSURIZATIO N CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2002051600037 20020516 00037 NM 2002 5 16 AALA20020262 1 20020225 A 2121 COOLING FAN BOEING 777 777223 1385213 NM E/E COMPT OVERHEATED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 784AN 29588 AFW - SMOKE IN COCKPIT DETECTOR ECAS ALERT, SMOKE DETECT RESET. RAN BOTH ENGINES AT FULL POWER AND BOTH PACKS AT FULL H OT. REPLACED RIGHT EQUIPMENT COOLING FAN FOR POSSIBLE OVERHEAT. NO MORE SMOKE OR SMELL NOTED. (M) 2 L 7 2 4F RT T00001SE 2002051600038 20020516 00038 WP 2002 5 16 AALA20020333 1 20020321 A 3350 P4010049 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 454AA 49559 MIA - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING EMERGENCY EXIT DOOR LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT DOOR LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600039 20020516 00039 WP 2002 5 16 AALA20020334 1 20020321 A 3350 P4010049 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 454AA 49559 MIA - DURING OVERNIGHT MAINTENANCE, LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600040 20020516 00040 WP 2002 5 16 AALA20020335 1 20020323 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77421 49333 DFW - DURNG OVERNIGHT MAINTENANCE, FORWARD OVERHEAD EMERGENCY EXIT LIGHT INTERMITTENT. TIGHTENED EMERGENCY EXIT LIGHT W IRES ON BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600041 20020516 00041 WP 2002 5 16 AALA20020348 1 20020318 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FOUND FRAME 1416 CRACKED FROM UNDER FILLER BLOCKS LONGERON 2R AND LONGERON 2L. REMOVED AND REPLACED CRACKED ANGLE FRAME 1416 L5L TO L5R. (M) 2 L 7 2 4F RT A6WE 2002051600042 20020516 00042 WP 2002 5 16 AALA20020349 1 20020312 A 5310 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FUOND FRAME 1429 SHEAR TIE CRACKED LEFT AFT SIDE JUST OUTBOARD OF TAIL TIE FITTING. INSTALLED NEW SHEAR TIE PER S RM 53-01. (M) 2 L 7 2 4F RT A6WE 2002051600043 20020516 00043 WP 2002 5 16 AALA20020350 1 20020313 A 5310 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FUOND TWO SHEAR TIES CRACKED ON AFT SIDE OF FRAME 1433 JUST INBOARD OF STRINGER 3R AND STRINGER 3L. REMOVED AND R EPLACED WITH NEW SHEAR TIE PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2002051600044 20020516 00044 WP 2002 5 16 AALA20020351 1 20020308 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FOUND CORROSION ON LEFT CUSP AT STATION 1155. CUT OUT CORROSION AND INSTALLED DOUBLER PER SRM 53-01 PAGE 18. (M) 2 L 7 2 4F RT A6WE 2002051600045 20020516 00045 WP 2002 5 16 AALA20020352 1 20020313 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FOUND HOLE IN CUSP UNDER NR 6 SEAT TRACK. CUT OUT AND INSTALLED DOUBLER .025 7075 T6 PER AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2002051600046 20020516 00046 WP 2002 5 16 AALA20020356 1 20020322 A 5310 BEAM DOUG DC9 DC983 3022083 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FOUND CORROSION ON AFT CARGO DOOR BEAM STATION 1155-1212. REMOVED AND REPLACED AFT CARGO DOOR BEAM FROM STATION 1 117 TO 1250 PER AARD 53-10-00-3. (M) 2 L 7 2 4F RT A6WE 2002051600047 20020516 00047 WP 2002 5 16 AALA20020357 1 20020321 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FOUND CANT FRAME AT STATION 1485 HAS CRACKS UNDER AFT STAIR ACTUATOR CASTING ATTACH POINT. CUT OFF DAMAGED SECTIO N OF FRAME AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-33 (CANT FRAME REPAIR). (M) 2 L 7 2 4F RT A6WE 2002051600048 20020516 00048 WP 2002 5 16 AALA20020358 1 20020308 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FOUND FLOORBEAM LOWER FLANGE AT 389 RBL 15 DAMAGED FROM CARGO DOOR. CUT OUT DAMAGE AND INSTALLED L-ANGLE DOUBLER PER AARD 53-20-00-21. (M) 2 L 7 2 4F RT A6WE 2002051600049 20020516 00049 WP 2002 5 16 AALA20020359 1 20020307 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FOUND CORROSION SEAT TRACK NR 1 FS 1208-1209. CUT OUT DAMAGED AREA AND INSTALLED PLUG PER AARD-53-70-00-10. (M) 2 L 7 2 4F RT A6WE 2002051600050 20020516 00050 WP 2002 5 16 AALA20020360 1 20020311 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FOUND CREASE IN FUSE SKIN STATION 278 AT LONGERON 26 LT. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04 FIG 12B SHEETS 7-22 AND 35. (M) 2 L 7 2 4F RT A6WE 2002051600051 20020516 00051 WP 2002 5 16 AALA20020361 1 20020312 A 5511 RIB DOUG DC9 DC983 3022083 WP HORIZONTAL STAB TORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FOUND OUTBOARD LEADING EDGE RIB TORN AT AFT UPPER CORNER ON LEFT HORIZONTAL STABILIZER. INSTALLED NEW LEADING EDG E RIB ON LEFT HORIZONTAL STABILIZER OUTBOARD END PER SRM 55-01. (M) 2 L 7 2 4F RT A6WE 2002051600052 20020516 00052 WP 2002 5 16 AALA20020362 1 20020325 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 448AA 49474 DFW - DURING OVERNIGHT MAINTENANCE, AFT SECTION OF SEAT MOUNTED EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED BATTERY F OR AFT SECTION OF SEAT MOUNTED EMERGENCY PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600053 20020516 00053 WP 2002 5 16 AALA20020363 1 20020325 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 448AA 49474 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SECTION OF SEAT MOUNTED EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED BATTE RY FOR FORWARD SECTION OF SEAT MOUNTED EMERGENCY PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600054 20020516 00054 WP 2002 5 16 AALA20020367 1 20020327 A 3350 LIGHT DOUG DC9 DC982 3022082 WP AFT STAIRS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 245AA 49257 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWAY EMERGENCY EXIT FLOODLIGHT BROKEN. REPLACED AFT STAIRWAY EMERGENCY EXIT FLOODLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 9M) 2 L 7 2 4F A6WE 2002051600055 20020516 00055 WP 2002 5 16 AALA20020368 1 20020331 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 573AA 53092 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN COCKPIT AND FORWARD GALLEY ARE DIM. REPLACED EMEREGNCY EXI T LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 2002051600056 20020516 00056 NM 2002 5 16 AALA20020431 1 20020322 A 5720 SUPPORT BOEING 767 767323 1385205 NM TE FLAPS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AA 26996 AFW - FOUND CORROSION IN MOUNT HOLE AFT OUTBOARD HOLE, ON RIGHT INBOARD FLAP SUPPORT BEAM. PERFORM A DETAILED VISUAL IN SPECTION OF THE RE-WORKED HOLE TO VERIFY COMPLETE CORROSION REMOVAL. APPLY ALODINE AND TWO COATS OF PRIMER TO RE-WORKED AREAS. (M) 2 L 7 2 4F RT A1NM 2002051600057 20020516 00057 NM 2002 5 16 AALA20020437 1 20020404 A 4997 WIRE BOEING 757 757223 1384957 NM APU BROKEN A AALA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 21 642AA 24600 DFW - FLT 745 - EN ROUTE DFW-SNA, DETECTED APU FLAME OUT WHILE LEFT GENERATOR ON MEL. RETURNED DFW AND LANDED WITHOUT F URTHER INCIDENT. REPLACED APU DOOR OPEN SENSOR WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002051600058 20020516 00058 NM 2002 5 16 AALA20020441 1 20020401 A 2913 326879210 PUMP BOEING 767 767323 1385205 NM HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 381AN 25450 DFW - FLT 2342 - EN ROUTE DFW-ORD, AFTER TAKEOFF GEAR HANDLE PUT IN RETRACT POSITION 'C' HYDRAULIC PRESSURE DROPPED TO 7 10 PSI AND BOTH ELECTRICAL PUMP INOPERATIVE LIGHTS ILLUMINATED. AIRCRAFT RETURNED DFW LANDING WITHOUT INCIDENT. AIRCRA FT REMOVED AND FROM SERVICE FOR FURTHER EVALUATION. DFW MAINTENANCE REPLACED THE AIR DRIVEN PUMP AND PRESSURE REGULATOR SHUTOFF VALVE PER MM. ALL OPERATIONAL CHECKS NORMAL. SYSTEM GROUND CHECK OPERATION NORMAL. (M) 2 L 7 2 4F RT A1NM 2002051600059 20020516 00059 NM 2002 5 16 AALA20020442 1 20020409 A 3350 CONNECTOR BOEING 777 777223 1385213 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 MIA - FLT 999 - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT PATH LIGHTING AT SEAT 40C INOPERATIVE. RECONNECTED L OOSE CONNECTOR AT SEAT 40C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002051600060 20020516 00060 NM 2002 5 16 AALA20020443 1 20020405 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 324AA 22325 AFW - FOUND FLOORBEAM AT BL33 LEFT AND RIGHT STATION 890 AND STATION 933 HAD CORROSION BLEND FROM TOP SURFACE BEYOND SRM LIMITS. SEE ATTACHED DRAWINGS. REQUEST ENG APPROVAL TO SHOT-PEEN, ALODINE, 2 COATS OF PRIMER AND SEAL W/BMS 5-95. RE MOVED CORROSION PER REF 1A1. ROTO-PEEN BLENDED AREA. REFINISHED BLENDED AREAS WITH ALODINE AND 2 COATS PRIMER. FILL B LENDS W/BMS5-95 SEALANT. (M) 2 L 7 2 4F RT A1NM 2002051600061 20020516 00061 NM 2002 5 16 AALA20020444 1 20020312 A 5500 SPAR BOEING 767 767223 1385123 NM STAB DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 325AA 22326 AFW - FOUND SEVERAL SMALL HOLES RANGING .15 INCH DIAMETER TO .40 INCH DIAMETER THROUGH SURFACE PLIES AT FRONT SPAR. NO CORE DAMAGE. (M) 2 L 7 2 4F RT A1NM 2002051600062 20020516 00062 EU 2002 5 16 AALA20020448 1 20020411 A 3260 201251276 SENSOR FOKKER F28 F28MK0100 4990807 EU MLG OUT OF ADJUST A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 1411G 11369 ORD - FLT 559 - AFTER TAKEOFF ORD, EN ROUTE TO IAH, UNABLE TO RAISE LANDING GEAR GROUND/FLIGHT CONTROL ALERT ON MFDU. A LSO, RECEIVED LIFTED FAULT MESSAGE ON MFDU. RETURNED AND LANDED ORD WITHOUT INCIDENT. ADJUSTED RIGHT AIR/GROUND INBOAR D 3 SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002051600063 20020516 00063 EU 2002 5 16 AALA20020453 1 20020412 A 5347 CARGO TRACK FOKKER F28 F28MK0100 4990807 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1417D 11396 TUL - FOUND CORROSION STATION 20320 UNDER LEFT TIE DOWN TRACK AT BELT FRAME. INSTALLED REPAIR ANGLE PER F100 SRM 53-00- 025R07 NR 7.6B FIG 626 ON ESO 51000 4/5/02. (M) 2 L 7 2 4F RT 2002051600064 20020516 00064 WP 2002 5 16 CALA2000290 1 20020515 A 5320 601151618 FRAME DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 AFT PIT, F/S 1041, LONGERON 30 FRAME ATTACH ANGLE CORRODED - 80". REPLACED FRAME ANGLE IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2002051600065 20020516 00065 WP 2002 5 16 CALA2000291 1 20020515 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 F/S 1193 LONGERON 28 RIGHT INTERCOSTAL CORRODED 20"X1". INSTALLED NEW INTERCOSTAL T & L ANGLES IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2002051600066 20020516 00066 WP 2002 5 16 CALA2000292 1 20020516 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 F/S 1212 LONGERON 28 RIGHT INTERCOATAL CORRODED 1"X1". INSTALLED NEW INTERCOSTAL IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2002051600067 20020516 00067 EU 2002 5 16 MALA020284 1 20020505 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU CARGO BAY MALFUNCTIONED A MALA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 89XJ 340A089 CARGO SMOKE LIGHT ILLUMINATED DURING TAXI. MAINTENANCE REMOVED AND REPLACED CARGO SMOKE DETECTOR PN CGAB1201-01, SN/ON 755, SN/OFF 92 AMM 26-13-15-4. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002051600068 20020516 00068 EA 2002 5 16 2002F00501 1 20020220 A 2750 601R045011 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A MASA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 07 27172 7172 FLT 6416 - COS - FLAP FAIL AT ZERO DEGREES WHEN FLAPS WERE SELECTED TO 8 DEGREES DURING INITIAL APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT AND MAINTENANCE PERFORMED PART A INSPECTION IAW AD 98-20-01. SYSTEM RESET NORMALLY. THE AIRCRA FT WAS RETURNED TO SERVICE. MAINTENANCE REPLACED LEFT BPSU AND LEFT NR 5 FLEX SHAFT. (M) 2 L 7 2 4F RT A21EA 2002051600069 20020516 00069 SO 2002 5 16 C2XA02CL115 1 20020514 A 2150 8152403 ACM EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 17513 3905 145292 IAH FLIGHT # 3958 CREW REPORTED SMOKE IN CABIN WITH #1 PACK RUNNING. MAINTENANCE REPLACED #1 PACK ACM OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT T00011AT 2002051600070 20020516 00070 WP 2002 5 16 AALA20020312 1 20020317 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 413AA 49324 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE HANDLE EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED TAIL CONE HANDLE EMERGE NCY EXIT LIGHT WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600071 20020516 00071 WP 2002 5 16 AALA20020313 1 20020317 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP TAILCONE DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70524 49916 ORD - DURING OVERNIGHT MAINTENANCE, BOTH TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED TAIL CONE EMERGENCY EXIT LIGHT CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600072 20020516 00072 WP 2002 5 16 AALA20020314 1 20020315 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 402A 49313 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPINNED FORWARD ENTRY EME RGENCY PORTABLE FLASHLIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600073 20020516 00073 WP 2002 5 16 AALA20020315 1 20020315 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90511 49805 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED FIRST CLASS CEILING EMERGENCY EXIT LIGHTS CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600074 20020516 00074 WP 2002 5 16 AALA20020316 1 20020315 A 3260 833703 DOWNLOCK SENSOR DOUG DC9 DC982 3022082 WP NLG OUT OF ADJUST A AALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 21 501AA 49738 TPA - FLT 408 - ON LANDING TOUCHDOWN AT TPA NOSE GEAR WARNING RED LIGHT AND AURAL WARNING SOUNDED. GO AROUND EXECUTED. ACCOMPLISHED EMERGENCY PROCEDURE, GEAR LOWERED NORMALLY WITHOUT FURTHER INCIDENT. LANDED TPA WITHOUT FURTHER INCIDENT. NOSE GEAR PIN INSTALLED AFTER LANDING. ADJUSTED NOSE GEAR DOWN LOCK SENSOR GAP TO PROPER DIMENSION. CHANGED PROXIMIT Y BOX AS A PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600075 20020516 00075 WP 2002 5 16 AALA20020325 1 20020320 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7540A 49994 AUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AFT OF VAULT DOOR INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGH T AFT OF VAULT DOOR WIRE TO QUARTER TURN CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600076 20020516 00076 NM 2002 5 16 AALA20020327 1 20020319 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 ORD - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 34B INOPERATIVE. SECURED CONNECTOR AT WALL FOR SEAT 34B EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002051600077 20020516 00077 EU 2002 5 16 AALA20020331 1 20020318 A 5310 DOOR FRAME FOKKER F28 F28MK0100 4990807 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1432A 11417 TUL - FOUND CORROSION AROUND FASTENER HOLES ON FORWARD SIDE OF FRAME 22236 AT CARGO DOOR OPENING. INSTALLED DOUBLER PER ESO 51000 DATED 3/5/02. (M) 2 L 7 2 4F RT 2002051600078 20020516 00078 EU 2002 5 16 AALA20020332 1 20020318 A 5310 DOOR FRAME FOKKER F28 F28MK0100 4990807 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1432A 11417 TUL - FOUND CORROSION AROUND FASTENER HOLE ON AFT SIDE OF FRAME 20778 AT CARGO DOOR OPENING. INSTALLED DOUBLER PER ESO5 1000 DATED 3-5-02. (M) 2 L 7 2 4F RT 2002051600079 20020516 00079 WP 2002 5 16 AALA20020336 1 20020322 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70401 49312 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD EMERGENCY EXIT LIGHT BAT TERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600080 20020516 00080 WP 2002 5 16 AALA20020337 1 20020324 A 3350 P4010049 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 436AA 49454 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS AND HALF OF COACH EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002051600081 20020516 00081 WP 2002 5 16 AALA20020339 1 20020322 A 3350 P4010049 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 570AA 49352 SEA - DURING OVERNIGHT MAINTENANCE, FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD OVERWING EMERGE NCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002051600082 20020516 00082 WP 2002 5 16 AALA20020340 1 20020323 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 477AA 49652 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ENTRANCE EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY ENTRANCE EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600083 20020516 00083 WP 2002 5 16 AALA20020341 1 20020324 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3515 49892 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY ENTRANCE EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600084 20020516 00084 WP 2002 5 16 AALA20020342 1 20020324 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3515 49892 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS CONNECTOR BACKSHELL BROKEN. REPLACED EMERGENCY EXIT LIGHT CON NECTOR BACKSHELL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600085 20020516 00085 WP 2002 5 16 AALA20020343 1 20020322 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70401 49312 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY SEAT EXIT LIGHT AT SEAT 31D INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002051600086 20020516 00086 EU 2002 5 16 AALA20020365 1 20020322 A 5312 BULKHEAD FOKKER F28 F28MK0100 4990807 EU FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1432A 11417 TUL - FOUND SCREW GOUGE ON FORWARD SIDE OF AFT PRESSURE BULKHEAD UNDER NR 4 RIGHT AFT LAVATORY BENCH MOUNT BRACKET. REP AIRED PER AARD 53-65-00 ESO 51000 DATED 28 OCT 01. (M) 2 L 7 2 4F RT 2002051600087 20020516 00087 EU 2002 5 16 AALA20020366 1 20020322 A 5312 BULKHEAD FOKKER F28 F28MK0100 4990807 EU FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1432A 11417 TUL - FOUND SCREW GOUGE ON FORWARD SIDE OF PERSSURE BULKHEAD (AFT) UNDER NR 3 RIGHT AFT LAVATORY BENCH ASSEMBLY MOUNT BR ACKET. REPAIRED PER ESO 51000, DATED 26 OCT 01 AARD 53-65-00. (M) 2 L 7 2 4F RT 2002051600088 20020516 00088 EU 2002 5 16 AALA20020373 1 20020331 A 5610 PPGD20543406 WINDOW FOKKER F28 F28MK0100 4990807 EU COCKPIT CRACKED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 1401G 11352 DFW - FLT 1069 - AFTER TAKEOFF DFW, FIRST OFFICERS WINDOW INNER PLANE CRACKED ASSOCIATED WITH ELECTRICAL SPARK AND SMOKE EMITTING FROM CRACK. DECLARED AN EMERGENCY AND RETURNED DFW. LANDED DFW WITHOUT INCIDENT. REPLACED FIRST OFFICERS R1 WINDOW ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002051600089 20020516 00089 EU 2002 5 16 AALA20020375 1 20020401 A 2910 HYDRAULIC LINE FOKKER F28 F28MK0100 4990807 EU HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 1434A 11419 DFW - FLT 576 - ON TAKEOFF DFW, ACRID SMOKE FILLED CABIN. RETURNED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. REPAIRE D HYDRAULIC LEAK INTO DISTRIBUTION DUCT. REPLACED RECIRCULATION FAN FILTERS AND PRESSURE REGULATOR ON NR 1 AND NR 2 SYS TEM, AND PNEUMATIC DISTRIBUTION CHECK VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002051600090 20020516 00090 NM 2002 5 16 AALA20020384 1 20020401 A 2421 CON5330 IDG BOEING 767 767323 1385205 NM LEFT ENGINE FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 358AA 24039 HNL - FLT 123 - LEFT GENERATOR OFF LIGHT ILLUMINATED, WITH ASSOCIATED LIGHTS. PER QRH ATTEMPTED RESET, BUT NOT SUCCESSF UL. STARTED APU AND CONTINUED FLIGHT. REPLACED LEFT ENGINE IDG AND LT GCU PER MM. ENGINE RUN AND OPS CHECK OK. LEAK CHECK OF IDG OK. (M) 2 L 7 2 4F RT A1NM 2002051600091 20020516 00091 NM 2002 5 16 AALA20020385 1 20020328 A 3411 PROBE BOEING 777 777223 1385213 NM PITOT/STATIC SY FAULTY A AALA C ABORTED TAKEOFF G MULTIPLE FAILURE TO TAKEOFF 1 SW 21 798AN 30797 MIA - FLT 943 - ON TAKEOFF ROLL, AT 100 KNOTS AIRSPEED ON BOTH CA AND FO PFDS SHOWED 30 KNOTS. THEN EICAS MSG NAV AIR D ATA SYSTEM INOPERATIVE. CA AIRSPEEDS CAME BACK BUT FO'S DID NOT. REMOVED OBSTRUCTION FROM L, C AND R PITOT PROBES REPL ACED LEFT AND RIGHT PROBES AND ADMS WORK ACCOMPLISHED ON E58 91140111, 914012029140117. LCR PITOT AND STATIC SYSTEMS LE AK CHECK GOOD PER MM. (M) 2 L 7 2 4F RT T00001SE 2002051600092 20020516 00092 NM 2002 5 16 AALA20020386 1 20020330 A 2424 UNI1143 GCU BOEING 777 777223 1385213 NM E/E BAY FAILED A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 786AN 30250 JFK - FLT 104 - ELECT GEN OFF ILLUMINATED AT FL18000 WHEN THE LANDING LIGHTS WERE TURNED OFF. REPLACED LEFT GENERATOR C ONTROL UNIT IAW MM 24-22-02-4 ACCOMPLISHED ALL REQUIRED TESTS PER MM CHECKED GCU OPS PROGRAM ALL NORMAL. (M) 2 L 7 2 4F RT T00001SE 2002051600093 20020516 00093 NM 2002 5 16 AALA20020387 1 20020326 A 2421 IDG BOEING 767 767223 1385123 NM LT ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 329AA 22329 MIA - FLT 207 - LEFT GENERATOR DRIVE LIGHT ILLUMINATED AFTER TAKEOFF WITH ASSOCIATED EICAS MESSAGE. PLACARDED LEFT GENE RATOR DRIVE INOPERATIVE IAW MEL 2A01 AUTH 3-516 DC-A. CHECKED BOTH IDG FULL LEVEL OIL AND APU FULL LEVEL OIL. ENTERED ON MIC SHEET. REPLACED IDG GEN LEAK CHECK GOOD. OPS CHECK GOOD. CLEARED MEL. (M) 2 L 7 2 4F RT A1NM 2002051600094 20020516 00094 NM 2002 5 16 AALA20020495 1 20020418 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 10B INOPERATIVE. SECURED POWER SUPPLY PLU G AT SEAT 10B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002051600095 20020516 00095 NM 2002 5 16 AALA20020496 1 20020418 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 20-24B INOPERATIVE. SECURED POWER SUPPLY PLUG AT SEAT 20-24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002051600096 20020516 00096 NM 2002 5 16 AALA20020497 1 20020411 A 3350 P4010049 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 368AA 25195 MIA - FLT 905 - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEATS 2H, 3H, 7H, AND 8H INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002051600097 20020516 00097 NM 2002 5 16 AALA20020498 1 20020413 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 LAX - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 40H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY DUE TO BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002051600098 20020516 00098 NM 2002 5 16 AALA20020499 1 20020415 A 3350 PIN BOEING 767 767323 1385205 NM CONNECTOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 394AN 29431 LAX - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 2H INOPERATIVE. REPINNED LOOSE PIN IN CON NECTOR AT SIDEWALL FOR SEAT 2H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002051600099 20020516 00099 NM 2002 5 16 AALA20020500 1 20020417 A 3350 P4010049 BATTERY BOEING 767 767223 1385123 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 303AA 22309 LAX - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 20H AND 20J THROUGH 29H AND 29J INOPERATIV E. REPLACED BATTERY FOR EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002051600100 20020516 00100 NM 2002 5 16 AALA20020501 1 20020416 A 3350 BPS73 POWER SUPPLY BOEING 767 767223 1385123 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 306AA 22312 LAX - DURING OVERNIGHT MAINTENANCE, FOUND EXTERIOR EMERGENCY LIGHT, RIGHT AFT FUSELAGE INOPERATIVE. REPLACED BATTERY AN D POWER SUPPLY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002051600101 20020516 00101 WP 2002 5 16 ASAA0280099 1 20020322 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING PREFLIGHT CHECK, FOUND DISCONNECTED EMERGENCY TRACK LIGHTS IN THE 1ST CLASS CABIN. RECONNECTED LIGHT MODUL E. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002051600102 20020516 00102 WP 2002 5 16 ASAA0280101 1 20020324 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K CHECK, FOUND WEB CORRODED AT FS 712-731. REPAIRED WEB PER SRM 51-30-2, 53-01 FIG 1, 51-70-4 FIG 2, 51- 10-3, AND MM 53-20-01. (M) 2 L 7 2 4F RT A6WE 2002051600103 20020516 00103 WP 2002 5 16 ASAA0280102 1 20020325 A 5311 39364451 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION IN AFT CARGO BAY ON UPPER SURFACE OF LOWER FLANGE OF FAIL/SAFE ANGLE AT FASTENER HOLES AT FS 1117. REPLACED FAIL/SAFE ANGLE PER SRM 53-01 AND 51-30-02. (M) 2 L 7 2 4F RT A6WE 2002051600104 20020516 00104 WP 2002 5 16 ASAA0280103 1 20020327 A 5310 59124921 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND MECHANICAL DAMAGE ON RIGHT FORWARD SERVICE DOOR CUTOUT FORWARD LOWER CORNER. REPAIRED CUT OUT (JAMB PAN) PER EA 5301-02071. (M) 2 L 7 2 4F RT A6WE 2002051600105 20020516 00105 WP 2002 5 16 ASAA0280104 1 20020326 A 5320 993061217 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON WEB AT FS 984-1003. REPLACED WEB PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002051600106 20020516 00106 WP 2002 5 16 ASAA0280105 1 20020326 A 5320 993061237N WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON WEB AT FS 1193-1231. REPLACED WEB PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002051600107 20020516 00107 WP 2002 5 16 ASAA0280106 1 20020326 A 5320 993061223 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON FLOORWEB AT FS 1140. REPLACED WEB PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002051600108 20020516 00108 WP 2002 5 16 ASAA0280107 1 20020326 A 5754 99375723 RIB DOUG DC9 DC983 3022083 WP L/E SLAT GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND LEFT WING NR 1 SLAT INBOARD RIB GOUGED IN INTERCONNECTING PIN BORE. REPLACED INBOARD RIB PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002051600109 20020516 00109 WP 2002 5 16 ASAA0280108 1 20020326 A 5320 9957828 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON FORWARD SERVICE DOOR CUTOUT, JAMB, FORWARD EDGE ANGLE AT FLOOR. REPLACED ANG LE PER SRM 51-10-4, 51-30-2, AND 51-30-1. (M) 2 L 7 2 4F RT A6WE 2002051600110 20020516 00110 WP 2002 5 16 ASAA0280109 1 20020327 A 5320 9957828 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON FORWARD SERVICE DOOR CUTOUT (JAMB) AFT EDGE ANGLE AT FLOOR. REPLACED ANGLE P ER SRM 51-10-4, 51-30-2, AND 51-30-1. (M) 2 L 7 2 4F RT A6WE 2002051600111 20020516 00111 WP 2002 5 16 ASAA0280110 1 20020328 A 5320 5910369 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND APU COMPARTMENT CEILING CHAFED AT FS 1368. CUT OUT CHAFED AREA AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F RT A6WE 2002051600112 20020516 00112 WP 2002 5 16 ASAA0280111 1 20020327 A 5320 993061218 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND PAX CABIN CUSP WEB CRACKED AT FS 987-999. REPLACED WEB PER SRM 51-30-2, 51-30-5, AND 51-1 0-4. (M) 2 L 7 2 4F RT A6WE 2002051600113 20020516 00113 WP 2002 5 16 ASAA0280112 1 20020327 A 5320 4914807501 SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND FRAME TO FLOORBEAM SPLICE AT FS 984 TO HAVE ELONGATED HOLES. REPLACED SPLICE PER MM 20-10 -15 AND SRM 53-14-3. (M) 2 L 7 2 4F RT A6WE 2002051600114 20020516 00114 WP 2002 5 16 ASAA0280114 1 20020331 A 5310 995301630 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND FRAME SHEAR TIE CRACKED IN AIRSTAIR COMPARTMENT AT FS 1437. REPLACED TIE PER SRM 51-10-02 , 51-10-4, 51-30-04, AND 53-05. (M) 2 L 7 2 4F RT A6WE 2002051600115 20020516 00115 WP 2002 5 16 ASAA0280115 1 20020331 A 5320 993053866N WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND WEB CORRODED AT FS 237-256. REPLACED WEB PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002051600116 20020516 00116 WP 2002 5 16 ASAA0280116 1 20020331 A 5320 993061269 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND FLOOR WEB CORRODED AT FS 1098 TO 1174. REPLACED WEB PER SRM 51-30-1, 51-30-2, 51-10-04, A ND 53-1. (M) 2 L 7 2 4F RT A6WE 2002051600117 20020516 00117 WP 2002 5 16 ASAA0280117 1 20020331 A 5320 5937669513E STRAP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION FROM STRAP AT AFT GALLEY SERVICE DOOR CUTOUT FORWARD FRAME TO FLOOR JUNCTION. R EPLACED STRAP PER SRM 51-30-3, 51-10-04, AND DOUG DWG 5937669. (M) 2 L 7 2 4F RT A6WE 2002051600118 20020516 00118 WP 2002 5 16 ASAA0280118 1 20020331 A 5320 5937669503 STRAP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION FROM STRAP AT AFT GALLEY SERVICE DOOR CUTOUT FORWARD FRAME TO FLOOR JUNCTION. R EPLACED STRAP PER SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002051600119 20020516 00119 NM 2002 5 16 HNAA0200036 1 20020515 A 3350 6013211X BATTERY DHAV DHC8 DHC8201 2809001 NM DISCHARGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 992HA 10772 561 432 CREW REPORTED SECTIONS OF THE FLOOR LEVEL EMERGENCY LIGHTS WERE INOP. REPLACED EMERGENCY LIGHTS BATTERY AT 3352-PS2. 2 H 7 2 4T RT A13NM 2002051600120 20020516 00120 EA 2002 5 16 COMA0260311 1 20020512 A 5210 CABLE CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 FLIGHT 5833 PASSENGER DOOR WARNING DURING CLIMB-OUT OF CVG, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD.FOUND D OOR ASSIST CABLE TANGLED IN DOOR MECHANISM. UNTANGLED AND DOOR OPS NORMAL. 2 L 7 2 4F RT A21EA 2002051600121 20020516 00121 EA 2002 5 16 COMA0260312 1 20020515 A 7930 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 973CA 7146 FLIGHT 6000 R/H ENGINE LOW OIL PRESSURE WARNING I.F.S.D AIRCRAFT LANDED AT CMH SAFELY.TIGHTENED LOOSE LINES AT OIL PRESS URE TRANSDUCER AND SWITCH. 2 L 7 2 4F RT A21EA 2002051600122 20020516 00122 EA 2002 5 16 COMA0260314 1 20020514 A 5610 NP1393219 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 936CA 6685 7043 FLIGHT 9464. DURING REPOSITIONING FLIGHT TO TYS FROM CVG (NON-REVENUE) THE CAPTAINS' WINDSHIELD CENTER PANE SHATTERED WH EN CLIMBING THROUGH 13,500 FEET. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY.REPLACED THE CAPTAINS WINDSHIELD. 2 L 7 2 4F RT A21EA 2002051600123 20020516 00123 EA 2002 5 16 COMA0260315 1 20020514 A 3350 59465 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 978CA 7158 FLIGHT 5602 ROW 3 EMERGENCY LIGHT IS INOPERABLE.RECONNECTED POWER STRIP - OPS CHECK NORMAL. 2 L 7 2 4F RT A21EA 2002051600124 20020516 00124 WP 2002 5 16 P2EA2002V0036 1 20020516 A 5523 5910414403 TAB DOUG DC9 DC982 3022082 WP DELAMINATED A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 130NJ 49222 DURING C1+C2 INSPECTION:-L-H ELEVATOR GEAR TAB, UPPER SKIN DELAMINATED AT Sta. XET116.-REPAIRED ELEVATOR GEAR TAB P/N 59 10414-403, S/N 583KDL DUE TO DELAMINATION IAW COOPESA E.O. No. COO-CMP-9-55-274-02, DATED MAY 09,2002 & DOCUMENTED ON FA A 8110-3 FORM.NOTE: SEE COOPESA WORK ORDER No. P1-0430, 3-29 & 3-2, VAM100 No. 236 & 083 & 130SDAOO7. 2 L 7 2 4F A6WE 2002092000045 20020920 00045 NM 2002 9 20 AWXA200200425 1 20020514 A 7920 5A1451 RESTRICTOR VALVE AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 2 ENGINE OBSTRUCTED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 803AW 931 V10783 T/O ROLL APPROX 90 KTS, CAPT NOTICED NR 2 ENG HIGH OIL PRESSURE IND 332 PSI. AIRCRAFT RETURNED. MX REPLACED NR 2 ENG P RESSURE PUMP, NR 4 BEARING SCAVENGE VALVE & OIL FILTERS. PROBLEM PERSISTS, BUT OIL PRESSURE REDUCED TO ACCEPTABLE LIMIT S FOR FERRY TO PHX. FILTERS EXAMINED & FOUND CONTAMINATED WITH CARBON. MX FLUSHED NR 2 ENG OIL SYS & DISCONNECTED. IN SPECTED FOR DEBRIS & RECONNECTED OIL SYS RESTRICTORS & STRAINERS. NO DEBRIS FOUND. REPLACED NR 2 ENG INTERFACE UNIT, N R 4 BEARING PRESSURE TRANSDUCER & PROBLEM PERSISTS. REMOVED & REPLACED NR 2 ENG. DURING TEAR DOWN OF ENG OIL DISTRIBUT ION SYS, A PIECE OF SAFETY WIRE FOUND UPSTREAM OF OIL DISTRIBUTOR RESTRICTOR. OIL JETS FOUND SATISFACTORY. 2 L 7 2 4F 4 F RT A28NM E40NE 2002051600125 20020516 00125 NM 2002 5 16 AWXA200200426 1 20020515 A 2931 69547678 HOSE BOEING 737 737277 1384570 NM WS 136 L/H BURST A AWXA O OTHER J K S WARNING INDICATION FLUID LOSS AFFECT SYSTEMS CR CRUISE 1 WP 28 184AW 0 0 22651 PHX - EMERGENCY LANDING - FLT 0332 - EN ROUTE FROM SLC TO PHX THE "A" HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED AN D THEN THE GAUGE FLUCTUATED BACK AND FORTH, FLIGHT CREW DECLARED AN EMERGENCY AND LANDED SAFELY AT SCHEDULED DESTINATION . MAINTENANCE PRESSURIZED "A" SYSTEM HYDRAULICS AND FOUND A PRESSURE HOSE LEAKING JUST OUTBOARD OF THE "A" SYSTEM PRESSU RE MODULE LEFT AFT WING ROOT WS 136. MAINTENANCE REPLACED THE "A" SYSTEM PRESSURE HOSE, AND THE #1 AND #2 ENGINE CASE DR AIN AND RETURN FILTERS, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2002051600126 20020516 00126 NM 2002 5 16 AWXA200200427 1 20020515 A 3350 BMS13311122 WIRE BOEING 737 737277 1384570 NM SEAT ROW 17 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 LAS - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHTS WERE FOUND INOPERATIVE AT SEAT ROWS 17 AND 19 L/H. MAINTENANC E REPAIRED A BROKEN WIRE AT SEAT ROW 17 L/H AND REPLACED BULB ON SEAT LIGHT 19, FUNCTIONAL TEST GOOD IAW T/C A1C33006. 2 L 7 2 4F RT A16WE 2002051600127 20020516 00127 NM 2002 5 16 AWXA200200428 1 20020508 A 5311 65677757 FRAME BOEING 737 7373Q8 1384670 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 0 0 23507 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1" CRACK WAS FOUND ON FRAME AT L/H SIDE OF FUSELAGE JUST BELOW FLOOR LEVEL BS 6 16, STR 18 L/H. MAINTENANCE REMOVED DAMAGED SECTION OF FRAME AT BS 616, STR 18 L/H; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED STIFFENING ANGLE AND FILLER, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2002060500171 20020605 00171 NM 2002 6 5 F3LA200200137 1 20020425 A 5311 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 3415 24569 DURING C-4 CHECK, INSPECTION REPORTED FRAME CRACKED AT BS 663.75, STR 1R AND 2R. REMOVED DAMAGE IN FRAME PER SRM 53-00- 07 FIG 209. FABRICATED FILLERS AND REPAIRED AND INSTALLED FRAME PER SRM 53-00-07 FIG 209. 2 L 7 2 4F RT A16WE 2002060500172 20020605 00172 NM 2002 6 5 F3LA200200138 1 20020504 A 5320 PAN BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 3415 24569 DURING C-4 CHECK, INSPECTION REPORTED AFT LAV PAN BETWEEN STA 1016 AND THE AFT PRESSURE BULKHEAD HAD THREE CORRODED FAST ENERS ON RT SIDE, 16 INCHES FROM CENTER LINE. REMOVED CORRODED AREA ON CABIN FLOOR PAN AND INSTALLED A FILLER AND REPAI R DOUBLER PER EA 57-737-165 AND SRM 51-40-2. 2 L 7 2 4F RT A16WE 2002060500174 20020605 00174 NM 2002 6 5 F3LA200200139 1 20020504 A 5320 CHANNEL BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 3415 24569 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON Z-CHANNEL AFT GALLEY SUPPORTS, STA 1028, BBL 10L AND BBL 10R. REPLAC ED CORRODED Z-CHANNEL PER EA 53-737-165, SRM 51-20-01, MM 51-21-99, SOPM 20-41-02 AND EA 53-737-171. 2 L 7 2 4F RT A16WE 2002060500175 20020605 00175 NM 2002 6 5 F3LA200200140 1 20020429 A 5313 STRINGER BOEING 737 73736E 138443A NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 3461 25263 DURING C-2 CHECK, INSPECTION REPORTED STRINGER 18L AT STA 947.5 DAMAGED. REPLACED STRINGER PER SRM 53-00-03, 51-40-02 A ND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002060500177 20020605 00177 NM 2002 6 5 F3LA200200141 1 20020430 A 5311 FRAME BOEING 737 73736E 138443A NM FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 3461 25263 DURING C-2 CHECK, INSPECTION REPORTED LT FUSELAGE BETWEEN STRINGERS 17L AND 18L, STA 947.5, DENTED. REPAIRED PER EA 53- 737-168. 2 L 7 2 4F RT A16WE 2002051700004 20020517 00004 WP 2002 5 17 211001001 1 20020421 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 191AJ 53191 AFT PIT HAS SEVERAL SPOTS OF CORROSION ON FLOOR SUPPORT WEBBING AT AFT INBOARD CORNER OF DOOR CUTOUT STA. 1211-1218 AND S29R AND S28R. CORRECTIVE ACTION: CUT OUT CORRODED SECTION OF WEB. INSTALLED REPAIR DOUBLER AND FILLER. (NR 23657) 2 L 7 2 4F RT A6WE 2002051700005 20020517 00005 WP 2002 5 17 211001002 1 20020422 A 5720 CLIP DOUG DC9 DC983 3022083 WP LT WING CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 191AJ 53191 LEFT WING, LEADING EDGE RIB UPPER AFT CLIP IS CRACKED AT XRS 354. CORRECTIVE ACTION: REMOVED CRACKED CLIP, FABRICATED, HEAT TREATED, TRIMMED, DEBURRED, ALODINED, PRIMED AND INSTALLED NEW CLIP AT XRS 354 RIB LEFT WING LEADING EDGE. (NR 23 767) 2 L 7 2 4F RT A6WE 2002051700006 20020517 00006 WP 2002 5 17 211001005 1 20020424 A 5230 5910141 STRUCTURE DOUG DC9 DC983 3022083 WP CARGO DOOR CHAFED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 191AJ 53191 MID PIT DOOR HAS DEEP CHAFED AREAS FORWARD AND AFT LOWER END. CORRECTIVE ACTION: FABRICATED AND INSTALLED, 2 EA REPAIR DOUBLERS, 1 EA INTERCOASTAL, 2 EA REWORKED BEARINGS. (NR 23948) 2 L 7 2 4F RT A6WE 2002051700007 20020517 00007 WP 2002 5 17 211001006 1 20020501 A 5343 991008895 BRACE DOUG DC9 DC983 3022083 WP NLG WW CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 191AJ 53191 NOSE LANDING GEAR W/W RIGHT SIDE FS 78, NOSE GEAR SUPPORT BEAM BRACE IS CRACKED AT UPPER ENC, LOWER HOLE FORWARD BRACE. CORRECTIVE ACTION: REMOVED AND REPLACED BRACE NOSE LANDING GEAR RIGHT STA. 78. (NR 23993) 2 L 7 2 4F RT A6WE 2002051700008 20020517 00008 WP 2002 5 17 211001007 1 20020501 A 5310 THRESHOLD DOUG DC9 DC983 3022083 WP CARGO DOORWAY CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 191AJ 53191 MID CARGO COMPARTMENT DOOR THRESHOLD IS CORRODED, CORROSION RUNNING UNDER DOOR STOPS. CORRECTIVE ACTION: REMOVED AND R EPLACED MID CARGO COMPARTMENT DOOR THRESHOLD. (NR 23722) 2 L 7 2 4F RT A6WE 2002051700009 20020517 00009 WP 2002 5 17 211011004 1 20020421 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE MISREPAIRED B DU4R K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 191AJ 53191 IMPROPER REPAIR ON FUSELAGE AFT OF LEFT 1 DOOR FS 237 JUST BELOW L17L. CORRECTIVE ACTION: CUT OUT DENTED SECTION OF SK IN. FABRICATED AND INSTALLED REPAIR DOUBLERS (7) AT FS 237 L17L. (NR 23666) 2 L 7 2 4F RT A6WE 2002051700010 20020517 00010 CE 2002 5 17 AJC2002F00001 1 20020418 A 3411 853JF PITOT HEAD RAYTHN DH125 HAWKER800XP 7150012 CE PITOT STATIC SYS FAILED E AJCA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 EA 25 801MB 1596 258440 IN CRUISE, IN AND OUT OF CLOUDS ENROUTE, THE FOLLOWING EVENTS OCCURRED: MACH TRIM FAILURE, AUTOPILOT DISENGAGES, YAW DAMPER DISENGAGES, NO AIRSPEED INDICATION ON NR 1, COMPARATOR MONITOR ILLUMINATED, NR AIRSPEED INDICATOR ROLLED BACK, NO AIRSPEED INDICATION ON STANDBY, STALL IDENT 3 ILLUMINATED. PILOTS CONFIRMED PITOT PROBE HEAT SWITCH ARE ON. PILOTS TURNED ON IGN/ENGINE ANTI-ICE AND TKS SYSTEMS. WITHIN MINUTES, THE SYSTEMS RETURNED TO NORMAL AND FLIGHT CONTINUED. 2 L 7 2 4F RT A3EU 2002051700011 20020517 00011 SO 2002 5 17 ASO2002F00000 1 20020309 A 5753 12026501002 RIB EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE TE FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 EA 11 232AS 120036 DURING A HANGER INSPECTION, THE RIGHT INBOARD FLAP SUPPORT RIB WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACE D THE RIGHT INBOARD FLAP TRACK SUPPORT RIB. 2 L 7 2 4T 4 T RT A31SO E20NE 2002051700012 20020517 00012 SO 2002 5 17 ASO2002F00001 1 20020422 A 3350 AGC1 FUSE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE EMERGENCY LIGHTS BLOWN A ASOA K NONE L NO TEST IN INSP/MAINT 1 EA 11 273AS 120222 DURING A HANGER INSPECTION, THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE FUSE FOR THE RIGHT AFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002051700013 20020517 00013 SO 2002 5 17 ASO2002F00003 1 20020421 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 232AS 33420 120036 DURING GROUND INSPECTION, THE FLOOR EMERGENCY LIGHTS FROM ROW 1 TO ROW 5 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002051700014 20020517 00014 NE 2002 5 17 ASO2002F00004 2 20020420 A 7200 P25 VALVE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT ENGINE SMOKE A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 11 533AS 460 DURING CRUISE FLIGHT, THE CAPTAIN REPORTED THAT THE MASTER CAUTION ILLUMINATED WITH A CONTINUOUS CHIME AND THAT A ELECTR IC SMOKE WARNING WAS RECEIVED ON THE CENTRALIZED ALERTING PANEL. THE CAPTAIN AND FLIGHT ATTENDANT BOTH REPORTED SEEING SMOKE IN BOTH THE COCKPIT AND CABIN. AT THIS TIME AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED, WHERE IT MADE A N UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. IT IS SUSPECTED THAT THIS EVENT WAS CAUSED BY AN INOPERATIVE P2.5 SWITCHING VALVE THAT WAS CONTAMINATING THE BLEED SYSTEM WITH ENGINE OIL. 2 H 7 2 4T 4 T RT A53EU E20NE 2002051700015 20020517 00015 EA 2002 5 17 CHI2002F00002 1 20020308 A 6220 A02R25518 LINK BOEING BOEING 107 1072 9420604 EA M/R HEAD CRACKED B CHIR K NONE O OTHER IN INSP/MAINT 1 NM 09 191CH 3766 CH44 CREW CHIEF NOTIFIED OF A POSSIBLE CRACK ON THE FORWARD ROTOR HEAD GREEN GLADE EXTENSION LINK AT THE HORIZONTAL PIN LAG B ORE 6 OCLOCK POSITION. UPON DISASSEMBLY OF THE ROTOR HEAD IT WAS CONFIRMED THAT THE EXTENSION LINK WAS CRACKED. THE CR ACK EXTENDED APPROX. .500 INCHES FROM THE HORIZONTAL PIN BORE INWARD, ACROSS THE FACE AND MFG HAS BEEN NOTIFIED OF THIS DEFECT. 2 G 7 2 4U 1H16 2002060500179 20020605 00179 NM 2002 6 5 F3LA200200142 1 20020515 A 5720 ATTACH ANGLE BOEING 737 737228 13844AG NM LT WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 234TR 3417 23004 DURING C-1 CHECK, INSPECTION REPORTED CRACKED ATTACH ANGLE ON LT WING LOWER TRAILING EDGE PANEL ON MLG BEAM. FABRICATED AND INSTALLED REPLACEMENT L-ANGLE PER SOPM 20-41-02 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002051700016 20020517 00016 WP 2002 5 17 ABXA010877 1 20020429 A 5320 491627001 FITTING DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 FITTING WAS CRACKED OVER L29L AT FS 675. REPLACED CRACKED FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002051700017 20020517 00017 WP 2002 5 17 ABXA010878 1 20020429 A 5755 49257211 FITTING DOUG DC9 DC941 302207N WP SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 INBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002051700018 20020517 00018 WP 2002 5 17 ABXA010879 1 20020430 A 5320 595603433 FITTING DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 TEE FITTING WAS CRACKED - FORWARD END OF INTERCOSTALS, AT STA 218, L28L AND L28R. REPLACED FITTING IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 2002051700019 20020517 00019 WP 2002 5 17 CALA0200293 1 20020426 A 5322 7075T6 WEB DOUG DC9 DC982 3022082 WP FS200 14L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 FORWARD ENTRY DOOR JAMB INNER WEB CRACKED AT STATION 200 LONGERON 14L. INSTALLED REPAIR PER EC/RA 5314-01011 AND EA 9-53 14-2-A0950. 2 L 7 2 4F A6WE 2002051700020 20020517 00020 WP 2002 5 17 CALA0200294 1 20020427 A 5320 7075T6 STIFFENER DOUG DC9 DC982 3022082 WP FS1322 LONG30 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 VERTICAL STIFFENER FOR ATTACH ANGLE FOR FRAME CORRODED AT FS 1322 LONGERON 30. REMOVED AND REINSTALLED FABRICATED ANGLE PER SRM 51-30-2, 51-30-5, AND 53-01 FIG1. 2 L 7 2 4F A6WE 2002051700021 20020517 00021 WP 2002 5 17 CALA0200295 1 20020516 A 5347 593056675 SEAT TRACK DOUG DC9 DC982 3022082 WP LFT INB ST TRACK CORRODED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 83870 48056 LEFT INBOARD SEAT TRACK CORRODED FROM STATION 1094 THROUGHT 1215. REMOVED AND REPLACED SEAT TRACK PER SRM 51-10-02. 2 L 7 2 4F A6WE 2002051700022 20020517 00022 WP 2002 5 17 CALA0200297 1 20020517 A 5315 S2777905 ANGLE DOUG DC9 DC982 3022082 WP ST1232 STR26L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 CRACK ON FLOOR SUPPORT AT STATION 1231 ABOVE STRINGER 26LT ABB. STOP DRILLED CRACK AND INSTALLED REPAIR PER EC/RA 5320-0 1263. 2 L 7 2 4F A6WE 2002060500182 20020605 00182 NM 2002 6 5 F3LA200200143 1 20020509 A 5532 PANEL BOEING 737 737228 13844AG NM VERTICAL STAB CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 234TR 3417 23004 DURING C-1 CHECK, INSPECTION REPORTED LT VERTICAL PANEL 9507L INNER BRACE WORN AND CRACKED. FABRICATED PANEL RETAINER A ND INSTALLED PER SRM 51-40-2, 51-30-50 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002051700023 20020517 00023 GL 2002 5 17 EO02002F00000 2 20020225 A 7230 6850921 FITTING BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL COMP SCROLL FAILED B EOOR K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 CHECK STOCK FOR PART NUMBER AND PERFORMED CEB-1374 ON THE FITTING AND IT FAILED THE INSPECTION IN MFG SB. PART IS SCRA PPED. 1 G 7 1 3U 3 U H2SW E4CE 2002051700024 20020517 00024 NE 2002 5 17 ERA2002F00000 1 20020327 A 2910 AN6289D8 NUT SKRSKY S61 S61N 8142104 NE HYDRAULIC SYS SPLIT A ERAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 AL 03 562EH 61257 ON INBOUND FLIGHT, THE PRIMARY HYDRAULIC SYSTEM FAILED. AIRCRAFT WAS LANDED AT THE FIRST AVAILABLE PLACE. INSPECTED AN D FOUND PRIMARY HYDRAULIC TANK EMPTY DUE TO LEAK AT SPLIT HYDRAULIC FITTING JAM NUT. REMOVED AND REPLACED WITH A SERVIC EABLE NUT AN ORING. REPLACED HYDRAULIC PUMP DUE TO POSSIBLE RUN DRY CONDITION. LEAK AND OPS CHECK OK. 2 G 7 2 4U 1H15 2002051700025 20020517 00025 CE 2002 5 17 EWC2002F00000 1 20020423 A 2822 1C712 PUMP CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE FUEL BOOST INOPERATIVE B EWCR K NONE O OTHER IN INSP/MAINT 1 SO 05 68CK 7630 5600063 IMPELLER VANES SEPARATED FROM MOUNT PLATE. DEBRIS IN FILTER AND JAMMED CHECK VALVE OPEN BETWEEN BOOST PUMP AND JET PUMP CAUSING A LOW FUEL BOOST LIGHT TO COME ON. REPLACED BOOST PUMP AND FILTER. CLEANED LINER THAT MAY HAVE DEBRIS INSIDE. 2 L 7 2 4F 4 F RT A22CE E25EA 2002051700026 20020517 00026 NM 2002 5 17 F3LA200200144 1 20020509 A 5330 DOUBLER BOEING 737 737228 13844AG NM CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 234TR 3417 23004 DURING C-1 CHECK, INSPECTION REPORTED DOUBLER CRACKED AT LOWER AFT CORNER OF EXT. POWER DOOR CUTOUT. REMOVED CRACK IN D OUBLER AND REPAIRED PER SRM 53-30-01. 2 L 7 2 4F RT A16WE 2002051700027 20020517 00027 CE 2002 5 17 FFS2002F00005 1 20020418 A 3244 265K081 TIRE BEECH 1900 1900C 1154161 CE RT MLG SEPARATED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 575P UC95 A WALK AROUND CHECK REVEALED A SECTION OF TREAD APPROXIMATELY 16 INCH X 5 INCH MISSING FROM RIGHT HAND INBOARD TIRE. AP PARENTLY THE TREAD HAD SEPARATED UPON LANDING AND IMPACTED THE RIGHT INBOARD FLAP SEGMENT DAMAGING THE FLAP NACELLE FAIR ING, LOWER AFT SKIN AND TRIALING EDGE RIB. TREAD SEPARATION APPEARS TO HAVE OCCURRED IN CORD LAYER, NOT IN RECAP BOND. 2 L 7 2 4T RT A24CE 2002051700028 20020517 00028 EU 2002 5 17 GJQ2002F00002 1 20020318 A 4930 2345119059 BOLT AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE7312B WP OIL PUMP CLAMP BROKEN A GJQR O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 NM 01 38WP 1188 292 BOLT BROKE ON CLAMP SECURING OIL PUMP FILTER ASSEMBLY ON APU. OIL LEAK CAUSED SMOKE IN CABIN. REPLACED CLAMP ASSEMBLY AS PER MM. 2 L 7 3 4F 4 F A46EU E6WE 2002051700029 20020517 00029 EU 2002 5 17 GXP2002F00000 1 20020416 A 3260 GE327 LIGHT AMD FALC20 FALCON 2720302 EU MLG INDICATOR INOPERATIVE A GXPA K NONE L NO TEST IN INSP/MAINT 1 GL 23 179GA 100 NOSE GEAR LIGHT DOES NOT ILLUMINATE (DOES NOT TEST EITHER). REPLACED ( 2 GE 327) GEAR DOWN LIGHT BULBS. GEAR LIGHT IL LUMINATED AND TEST IS PROPER. 2 L 7 2 4F A7EU 2002051700030 20020517 00030 NM 2002 5 17 GXPA0202 1 20020416 A 7810 EXHAUST PIPE PIPER PA60 PA60601P 7106012 NM LYC O540 TIO540* 41532 EA LT ENGINE LOOSE E GXPA K NONE O OTHER IN INSP/MAINT 1 GL 23 601GA 61P0282064 11949 AIRCRAFT LANDED DUE TO FIRE WARNING ON LEFT ENGINE. FOUND OUTBOARD EXHAUST TUBE CLAMP CAME LOOSE AND EXHAUST TUBE WAS H ANGING FROM TURBOCHARGER. REINSTALLED TUBE AND GASKET AND TIGHTENED CLAMP AND SAFETY. OPS CHECKED GOOD, NO FIRE WARNIN G LIGHT. 1 M 7 2 3O 3 O RT A17WE E14EA 2002051700031 20020517 00031 CE 2002 5 17 HMG2002F00000 1 20020412 A 5610 SEAL LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP COCKPIT WINDOW LEAKING E HMGA K NONE O OTHER IN INSP/MAINT 1 SW 15 155RB 117 THE AIRCRAFT WAS PARKED OUTSIDE IN A HEAVY ALLOWING WATER TO ENTER CONNECTORS AFT OF THE PILOTS CIRCUIT BREAKER PANEL. APPROX. FIFTEEN MINUTES AFTER TAKEOFF, THE LEFT AND RIGHT ESSENTIAL (A) CIRCUIT BREAKERS OPENED. THE RIGHT ESSENTIAL (A ) BREAKER WAS RESET, ALLOWING THE CREW TO DECLARE AN EMERGENCY. RIGHT ESS. (A) BREAKER OPENED AGAIN ON FINAL APPROACH, AND ASSOCIATED WIRING WERE INSPECTED BY MFG MAINTENANCE, NO DEFECTS NOTED. ALL SYSTEM CHECKS SATISFACTORY. PILOTS SIDE WINDOW SEAL REPLACED. 2 L 7 2 4F 4 F A10CE E6WE 2002051700032 20020517 00032 SO 2002 5 17 IMP2002F00000 1 20020422 A 7120 5008906 SUPPORT BRACKET PIPER PA31T PA31T 7103124 SO PWA PT6 PT6* 52043 EA ENGINE CRACKED E IPMA K NONE O OTHER IN INSP/MAINT 1 WP 11 155CA 31T7820024 FOUND CRACKS EMINATING FROM LAST RIVET ON INBOARD UPPER ENGINE SUPPORT BRACKET. IT APPEARS THAT THIS RIVET WAS SMASHED HARDER THAT NECESSARY DURING MANUFACTURE. 1 L 7 2 3T 3 T A8EA E2NE 2002051700033 20020517 00033 CE 2002 5 17 JGV2002F00003 1 20020425 A 2432 CONNECTOR SAFT CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP SENSOR DAMAGED A JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 713QS 093895 6507103 CONNECTOR PINS RECESSES EXCESSIVELY INTO HOUSING OF CONNECTOR. FOUND DURING SCHEDULES INSPECTION OF BATTERY. PROBABLE CAUSE IS IMPROPER ASSEMBLY OF CONNECTOR DURING MANUFACTURE (BUILD-UP) OF SENSOR ASSEMBLY. RECOMMEND MANUFACTURER (SAFT) TIGHTEN THEIR QUALITY ASSURANCE PROCEDURES. 2 L 7 2 4F 4 F A9NM E6WE 2002051700034 20020517 00034 EU 2002 5 17 JGV2002F00004 1 20020423 A 3350 406608005 BATTERY PACK AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP CABIN WRONG PART A JGVR K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 09 163WW 052 FOUND THIS NON-PMAD BATTERY PACK INSTALLED IN CUSTOMERS PS823A. THIS SHOULD BE TRACED TO INSTALLER, TO MAKE SURE THEY A RE USING PMAD PACKS. 2 L 7 3 4F 4 F A46EU E6WE 2002051700035 20020517 00035 SW 2002 5 17 JIK2002F00000 1 20020501 A 5410 2735003003 CAP SWRNGN SA227 SA227AT 8780610 SW GARRTT TPE331 TPE331* 01514 WP NACELLE WORN E JIKA K NONE O OTHER IN INSP/MAINT 1 WP 01 556UP AT556 ENGINE CONTROL CABLE RUBBED THRU ON THE 90 DEGREES ANGLE FLANGE BY THE TOP OF THE LEFT NACELLE INBOARD SIDE. THIS CAP I S PART OF MAIN STRUCTURE OF THE NACELLE. FOUND AFTER UPPER NACELLE SKIN WAS REMOVED FOR REPAIR OF THE NACELLE. 2 L 7 2 4T 3 T RT A5SW E2WE 2002053000081 20020530 00081 NM 2002 5 30 2002UALA00842 1 20020508 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 934UA 26662 EXTERNAL FUSELAGE SKIN AFT OF AFT CARGO DOOR CUTOUT AT STRINGER 23R IS CRACKED AND SEPARATING FROM INTERNAL DOUBLER. MA JOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002051700036 20020517 00036 NM 2002 5 17 2002UALA00845 1 20020509 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 CABIN FLOORBEAM TOP FLANGE CORRODED BODY STATION 1640, RBL 44 THROUGH RBL 62. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPL ICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082300101 20020823 00101 NE 2002 8 23 2002UALA00849 2 20020509 A 7250 A8A2162 VANE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE CORRODED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 504UA 17483 24625 717942 NR 2 ENGINE EXPERIENCED EXCESSIVE VIBRATIONS. SUBJECT ENGINE EXPERIENCED HIGH VIBRATION. PIECES OF METAL WERE FOUND IN TAILPIPE AND ENGINE WAS REPLACED. THE ENGINE WAS FOUND TO HAVE EXPERENCED AN LPT FAILURE. THE ROOT CAUSE TO BE SULFID ATION OF THE 5TH STG VANES WITHIN THE LPT MODULE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002051700037 20020517 00037 WP 2002 5 17 AT0200052 1 20020227 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE TORN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 EXTERNAL FUSELAGE SKIN TORN AT LONGERON 18R APPROX STA 164. CUT OUT DAMAGED AREA. INSTALLED DOUBLER REPAIR PER DC-9 SR M 53-04 FIG 12B CLASS II. 2 L 7 2 4F A6WE 2002051700038 20020517 00038 WP 2002 5 17 AT0200053 1 20020227 A 5730 SKIN DOUG DC9 DC932 3022066 WP RT WING CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 RIGHT WING LEADING EDGE SKIN LOWER AREA CRACKED WING STA 215 XRS, JUST INBOARD FUEL PANEL DOOR. CUT OUT CRACK AREA, ACC OMPLISHED NDT CRACK CONTAINMENT CONFIRM. INSTALLED REPAIR PER DC-9 SRM 57-06B F1. 2 L 7 2 4F A6WE 2002051700039 20020517 00039 WP 2002 5 17 AT0200054 1 20020307 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 AFT PRESSURE BULKHEAD CORROSION FORWARD SIDE ABOVE 27L TO 27R. INSTALLED AFT PRESSURE BULKHEAD WEB REPAIR FROM LONG 28L T TO LONG 27RT IAW DC-9 SRM 53-03 FIG 33. 2 L 7 2 4F A6WE 2002051700040 20020517 00040 WP 2002 5 17 AT0200056 1 20020404 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 834AT 47488 AFT CARGO COMPARTMENT, AFT PRESSURE BULKHEAD LOWER T-CHORD CORROSION BETWEEN STR 29 LEFT TO STR 29 RIGHT BS 996. REMOVE D STIFFENER AT LONG 28 RIGHT AND LEFT FOR ACCESS AND REMOVED LEFT ANGLE BS 996 LONG 29R TO 29L. CUT OUT VERTICAL WEB ST A 996 (INTERIOR) FOR ACCESS. REMOVED AND REPLACED SECTION OF AFT PRESSURE BULKHEAD CHORD BETWEEN LONG 29L TO 29R AT STA 996 / SRM 53-03 FIGURE 37. 2 L 7 2 4F A6WE 2002051700041 20020517 00041 WP 2002 5 17 AT0200058 1 20020403 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 834AT 47488 FORWARD CARGO DOOR CUTOUT BETWEEN LOWER DOOR STOP FITTINGS HAS CRACKS ON FLANGE OF VERTICAL FRAME AND HAS BULGING (EVIDE NCE OF CORROSION). REMOVED FASTENERS AND CORROSION, MATERIAL LOSS BEYOND LIMITS. REMOVED LOWER PAN AT FORWARD CARGO DO OR. REMOVED LOWER DOOR STOPS. INSTALLED NEW PAN SECTION PIN 5912494-501N AT C-1 DOOR LOWER AREA AND SPLICED BETWEEN ST OP 2 AND 3 LONG 24 AND 25 PER SRM 53-05 FIGURE 44 AND RES NUMBER 02-0261. 2 L 7 2 4F A6WE 2002051700042 20020517 00042 WP 2002 5 17 AT0200059 1 20020404 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 834AT 47488 EXTERIOR FUSELAGE SKIN IS BULGED JUST FORWARD OF STA 996 AT STR 25L AND 23L. REMOVED FASTENERS AND TIE FITTING 25L AT S TA 996. REMOVED CORROSION, OUT OF LIMITS. REMOVED TIE FITTING 25L. REMOVED CORROSION. REMOVED SHIM BELOW FITTING 25L . SHIM CORRODED OUT OF LIMIT. INSTALLED TIE FITTING AT 25L STA 996 AT AFT PRESSURE BULKHEAD. INSTALLED TIE FITTING AT 23L STA 996 AT AFT BOTTOM PRESSURE BULKHEAD IN ACCORDANCE WITH DC9 SRM 51-30-02. 2 L 7 2 4F A6WE 2002051700043 20020517 00043 EU 2002 5 17 AWXA200200414 1 20020422 A 5312 D535852622118 FIREWALL AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 605AW 543 YWG - MAJOR REPAIR - DURING C-04 CHECK A CRACK WAS FOUND ON APU FIREWALL, RT SIDE (22WG), AT FIRE/OVERHEAT DETECTOR MOUN T BRACKET. MAINTENANCE REMOVED EXISTING CRACK ON LOWER FIREWALL SECTION AND BLENDED SHARP EDGES PER SRM CHAPTER 51 PROC EDURES, PERFORMED DVI TO VERIFY NO CRACKS EXIST. WELDED DAMAGED AREA, AND INSTALLED FILLER TO FILL VOIDS, BLENDED WELD TO ORIGINAL CONTOUR. ACCOMPLISHED REPAIR PER AWA ER 26-5350-02123-TB2. 2 L 7 2 4F RT A28NM 2002051700044 20020517 00044 EU 2002 5 17 AWXA200200415 1 20020512 A 2133 VFT300A1 OUTFLOW VALVE AIRBUS 320 A320231 3930325 EU CABIN PRESSURE INOPERATIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 625AW 23165 064 PHX - AIR TURNBACK - FLT 0239 - AFTER TAKEOFF FROM PHX EN ROUTE TO DTW SKIN AIR VALVE FAULTED WITH AVIONICS VENT ALREADY ON MEL 21-26-02 AND EXTRACT FAN OVERRIDE. ECAM INDICATED MAXIMUM ALTITUDE 10,000 MEA, TURNED BACK TO PHX. MAINTENANCE REMOVED AND REPLACED SKIN AIR VALVE IAW AMM 21-26-53-401; SKIN AIR VALVE WAS INSTALLED ONLY ONE FLIGHT EARLIER. MAINTE NANCE ALSO REPLACED THE AVIONICS COOLING FAN IAW AMM 21-26-51-401, BITE CHECK ON BOTH COMPONENTS WAS GOOD. 2 L 7 2 4F RT A28NM 2002051700045 20020517 00045 NM 2002 5 17 AWXA200200422 1 20020512 A 2560 P4010021000 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 PHX - EMERGENCY EQUIPMENT - F/A REPORTED THAT THE AFT EMERGENCY FLASHLIGHT NEAR THE RIGHT AFT F/A JUMPSEAT IS INOPERATIV E. MAINTENANCE REPLACED BATTERIES IN THE EMERGENCY FLASHLIGHT AT THE AFT F/A JUMPSEAT. 2 L 7 2 4F RT A28NM 2002051700046 20020517 00046 SO 2002 5 17 C2XA02CL111 1 20020508 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 12922 145338 DFW FLT 3166 CREW REPORTED EMERGENCY FLOOR PROXIMITY STRIP LIGHTS 2ND STRIP FROM FORWARD TO AFT INOP. MAINTENANCE RELEA SED AIRCRAFT IAW MEL 33-50-00. 2 L 7 2 4T RT T00011AT 2002051700047 20020517 00047 SO 2002 5 17 C2XA02CL112 1 20020509 A 2120 SMOKE EMB 145 EMB145LR 3260212 SO CABIN DETECTED A C2XA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 12922 145338 DAY FLIGHT 3740 CREW REPORTED LAV SMOKE WARNING ON INBOUND TAXI WITH SMOKE IN CABIN. MAINTENANCE RELEASE AIRCRAFT IAW M EL 49-00-00. 2 L 7 2 4T RT T00011AT 2002051700048 20020517 00048 SO 2002 5 17 C2XA02CL113 1 20020512 A 5240 CABLE EMB 135 EMB135ER 3260203 SO SERVICE DOOR OUT OF ADJUST A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 25504 145186 CLE FLIGHT 3093 CREW REPORTED GALLEY SERVICE DOOR CANNOT BE OPENED FROM THE OUTSIDE. MAINTENANCE ADJUSTED SERVICE DOOR LOCK BOX CABLES. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002051700049 20020517 00049 2002 5 17 C2XA02IA104 4 20020511 A 2210 AUTOPILOT SYS AEROSP ATR42 ATR42320 8680930 EU COCKPIT MALFUNCTIONED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 14828 179 IAH- DURING TAKEOFF ROLL THE CREW NOTED THAT THE AFCS FAIL INDICATION ILLUMINATED. THE CREW ABORTED TAKEOFF, FLIGHT 37 58. THE CREW PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE CREW RECEIVED CLEARANCE FOR TAKEOFF. NO DISCREPAN CIES NOTED. 2 H 7 2 4T RT A53EU 2002051700050 20020517 00050 SO 2002 5 17 C2XA02TY074 1 20020426 A 3350 G3664 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 22971 145149 DURING A ROUTINE CHECK THE AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LI GHT STRIP AND OPS CHECK WAS GOOD IAW AMM-33-50-12. 2 L 7 2 4F RT T00011AT 2002051700051 20020517 00051 SO 2002 5 17 C2XA02TY075 1 20020426 A 5210 14533395001 SKIN EMB 145 EMB145 3260210 SO PAX DOOR DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 DURING A SCHEDULED 1C/2C INSPECTION TWO DENTS AND A SCRATCH WERE FOUND IN THE MAIN DOOR. THE DENT'S AND SCRATCHES WERE FOUND WITHIN LIMITS. THE AREA WAS RESTORED TO ORIGINAL FINISH. NDT INSPECTED ALL AREAS. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL 1C/2C INSPECTION WORK. 2 L 7 2 4F RT T00011AT 2002051700052 20020517 00052 SO 2002 5 17 C2XA02TY086 1 20020510 A 2432 501122804 BATTERY EMB 145 EMB145 3260210 SO E/E BAY DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS DURING A SCHEDULED 1C/2C INSPECTION THE BACK-UP BATTERY FAIL THE FUNCTIONAL CHECK. MAINTENANCE REMOVED AND REPLACE D THE BACK-UP BATTERY IAW EMB-145 AMM 24-35-01 AND THE FUNCTIONAL CHECK WAS GOOD IAW EMB 145 AMM 24-35-01-700-801 A. AL L WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002051700053 20020517 00053 SO 2002 5 17 C2XA02TY087 1 20020510 A 5320 14522459003 ANGLE EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS DURING A SCHEDULED 1C/2C INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT FRAME 20. MAINTENANCE REMOVED AND REP LACED RT RAMP ANGLE AT FRAME 20 IAW EMB 145 SRM 51-40-02. THE WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETIO N OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002051700054 20020517 00054 SO 2002 5 17 C2XA02TY089 1 20020510 A 5315 14522460009 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS DURING A SCHEDULED 1C/2C INSPECTION THE TOP CAP AT FRAME 17-18 WAS CORRODED. MAINTENANCE REMOVED THE CORROSION AND BLENDED THE AREA, REPLACED THREE RIVET'S, ALODINE, PRIMED AND PAINTED IAW EMB 145 SRM 51-40-02, 51-10-02, 51-21-04-05-0 6. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002051700055 20020517 00055 SO 2002 5 17 C2XA02TY091 1 20020511 A 5315 14521700007 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS, DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THA LEFT OMEGA BEAM AT FRAME 20. MAINTENANCE CUT OUT THE COR RODED AREA, FABRICATED ANGLES, SHIMS AND FILLER, THEN INSTALLED. IAW EMB-145-SRM-53-21-10 AND 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002051700056 20020517 00056 SO 2002 5 17 C2XA02TY092 1 20020511 A 3397 WIRE EMB 145 EMB145 3260210 SO CABIN BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS, DURING A SCHEDULED INSPECTION, THE EMERGENCY PROXIMITY FLOOR LIGHT STRIP HAS A WIRE BROKEN. MAINTENANCE REMOVED AN D REPLACED THE LIGHT STRIP, OPERATIONAL CHECKED GOOD IAW EMB-145-AMM-33-50-12. THE REPAIR WAS SATISFACTORY AND THE AIRC RAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002051700057 20020517 00057 2002 5 17 CALA2000267 4 20020507 A 3460 1762000101 FMC BOEING 737 737824 13844BZ NM COCKPIT MALFUNCTIONED A CALA B EMER. DESCENT S AFFECT SYSTEMS CR CRUISE 1 SW 09 54241 28953 AIRCRAFT LOST ALL NAVIGATION DATA; BOTH CAPT AND F/O DEU DISPLAYS ARE BLANK. REMOVED AND REPLACED NR 1 FLIGHT MANAGEMEN T COMPUTER. 2 L 7 2 4F RT A16WE 2002051700058 20020517 00058 WP 2002 5 17 CALA2000273 1 20020511 A 5320 3918891 PLATE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 FWD SERVICE DOOR FLOOR SKIN BETWEEN GIRT LATCH SUPPORTS IS CORRODED. INSTALLED NEW PARTS PER SRM 51-30-00. 2 L 7 2 4F A6WE 2002051700060 20020517 00060 WP 2002 5 17 CALA2000275 1 20020511 A 5320 2929169 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 CENTER FLOOR PANEL FWD EDGE SUPPORT AT STA 200, RBL 4 IS CORRODED. REPLACED SUPPORT IAW SRM 51-10-02. 2 L 7 2 4F A6WE 2002051700063 20020517 00063 2002 5 17 CALA2000278 4 20020511 A 3140 COMPUTER BOEING 767 767424ER 1385270 NM COCKPIT MALFUNCTIONED A CALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 09 59053 29448 AT 90 KNOTS LOST ALL OIL PRESSURE ON LEFT ENGINE. REJECTED TAKEOFF. REPLACED RT DATA CONCENTRATOR UNIT PER MM 31-63-06 , PG 401. LOADED SOFTWARE IAW MM 31-63-06, PG 201. 2 L 7 2 4F RT A1NM 2002051700068 20020517 00068 WP 2002 5 17 CALA2000284 1 20020513 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 MID CARGO DOOR LOWER AFT CORNER SKIN CHAFED. INSTALLED DOUBLER IAW SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2002051700069 20020517 00069 EU 2002 5 17 DHL2002363005 1 20020509 A 2612 04035518048400 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE DEFECTIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 ON MANIFOLD TEST PANEL WHEN B-LOOP SELECTED, FAULT LIGHT COMES ON RT ENG AND APU. T/S FOUND LOOP 92HF AT FAULT REF WDM 26-16-13 PG 2. LOCATED ON TOP OF NR 2 ENG LEADING EDGE SECTION. REMOVED AND REPLACED SENSING ELEMENT 92HF, RT WING OVE R NR 2 ENG AS PER MM 26-16-12. PERFORMED OPS CHECK. OPS CHECKED OK. 2 L 7 2 4F RT A35EU 2002051700071 20020517 00071 NM 2002 5 17 DHL2002726519 1 20020418 A 5230 DOUBLER BOEING 727 727228 1384083 NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, MCD AFT UPPER CORNER FRAME DOUBLER (INTERNAL) CRACKED, AS VIEWED THROUGH THE MCD UPPER AFT LIGHTENING HO LE. REMOVED AFT UPPER FRAME CORNER DOUBLER IAW B-727 SRM 51-30-2. FABRICATED AND INSTALLED PART IAW B-727 SRM. 2 L 7 3 4F RT A3WE 2002051700073 20020517 00073 NM 2002 5 17 SPAA0200053 1 20020422 A 3350 6038443M POWER SUPPLY BOEING 737 7372Y5 1384554 NM POWER LOSS A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 712S 23038 AIRCRAFT BATTERY LOW VOLTS, POSSIBLE BATTERY AMP/VOLTS DRAW FROM OTHER SOURCE. 2 L 7 2 4U RT A16WE 2002051700074 20020517 00074 NM 2002 5 17 02051701 1 20020517 A 7331 8TJ124GGL1 TRANSMITTER BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E4 54555 NE #2 ENGINE FLUCTUATES A N8TA K NONE O OTHER CL CLIMB 1 WP 19 545NA 29944 31659 Right Engine fuel flow fluctuation on climbout. An uneventful flight occured. Upon return to LAS, removed and replaced fuel flow transmitter. Ops check good as per M/M 73-31-01 2 L 7 2 4F 4 F RT A2NM E12EU 2002051700075 20020517 00075 WP 2002 5 17 JRA2002F00003 1 20020424 A 2432 AK01953E BATTERY CVAC 640 640340D 2422814 WP RROYCE DART DART54210 54522 EU MAIN OVERHEATED A JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 587CA 463 AFTER ARRIVAL, AIRCRAFT POWERED BY BATTERY FOR 30 MIN. - FANS, LIGHTS, CARGO DOOR, ECT. WHEN POWERED UP, NOTED 18 V, T URNED ON BATT INTERLOCK OVERRIDE FOR A FEW MINUTES WITH GPU ON- BATTERY TEMP 120 DEGREES, FOLLOWED COM PROCEDURE AND LOW ERED BATTERIES. BATTERY COOLED AND CONTINUED, 10 MINUTES. 2 L 7 2 4T 4 T RT A793 E5EU 2002051700076 20020517 00076 NE 2002 5 17 JYD2002F00002 2 20020426 A 7230 670802 DISK SKRSKY S64 CH54B 8142610 NE PWA JFTD12 JFTD12A4A 52047 NE BLADE PIN HOLE CRACKED B JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 223AC 5115 64086 CRACK FOUND IN BLADE PIN RETENTION HOLE OF 2ND STAGE COMPRESSOR DISK. COMPRESSOR (SN 677810) REMOVED FOR OVERHAUL. DUR ING INSPECTION PROCESS, NDT DETECTED A CRACK IN BLADE PIN RETENTION HOLE, CENTER LAND, USING EDDY CURRENT. CRACK VERIFI ED BY FMPI. HOLDING THE DISK WITH THE PN ON THE DISK AT THE 7 OCLOCK POSITION, THROUGH CRACK BEGINS AT THE 12 OCKLOCK P OSITION OF HOLE AND EXTENDS OUTWARD APPROXIMATELY .200 INCH TOWARDS OUTER EDGE OF LAND AT 45 DEGREE ANGLE. CRACK DOES N OT EXTEND TO OUTER EDGE OF LAND. PROBABLE CAUSE IS UNKNOWN. 2 G 7 2 4U 4 U H6EA E15EA 2002051700077 20020517 00077 NE 2002 5 17 JYD2002F00003 1 20020503 A 6310 641520603041 SPAR SKRSKY S64 CH54B 8142610 NE MAIN ROTOR BLADE CRACKED A JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 223AC 8203 64M65475926 64086 MAIN ROTOR BLADE CRACKED. DURING POST-FLIGHT INSPECTION, AND REQUIRED COMPLIANCE WITH SB, (BLADE INSPECTION METHOD) IND ICATION WAS FOUND ON BLADE (SN 64M-6547-5926) BLADE WAS REMOVED. CRACK WAS DETECTED ON TOP SIDE BETWEEN POCKET NR8 AND NR9. CRACK LENGTH APPROXIMATELY 1.750 INCH. CORROSION, PITTING. 2 G 7 2 4U H6EA 2002051700078 20020517 00078 NE 2002 5 17 JYD2002F00004 1 20020503 A 6321 643520564101 WHEEL SKRSKY S64 S64E 8142604 NE M/R BRAKE CRACKED A JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 FCRN 64021 TWO CRACKS FOUND IN FORWARD INDEX WHEEL, HIGH-SPEED SHAFT (SN 46) REMOVED FROM SERVICE FOR O/H HAVING A TSO/ 2992.8 WITH AN UNK TT. DURING INSPECTION PROCESS, MAG PARTICLE INSP DETECTED TWO CRACKS. CRACK 1 LOCATION: BEGINNING AT 11 OCLOC K POSITION IN 1.625 INCH DIA. HOLE EXTENDING AT 45 DEGREE ANGLE FOR APPROX. .400 INCH, CRACK (Y) AT ATTACHMENT WEB EXTEN DING APPROX. .275 INCH INTO WEB. CRACK 2 LOCATION: BEGINNING AT 11 OCLOCK POSITION IN 1.625 DIA. HOLE EXTENDING AT 45 DEGREE ANGLE FOR APPROX. .325 CRACK (Y) AT ATTACHMENT WEB EXTENDING APPROX. .250 INTO WEB. TWO OF THREE 1.625 INCH DIA . HOLES EXHIBITED CRACKS. UNDER MAGNIFICATION BOTH CRACKS EITHER INITIATED OR ENDED AT A CORROSION PIT. 2 G 7 2 4U H4EA 2002051700079 20020517 00079 NM 2002 5 17 O9I2002F00001 1 20020430 A 5510 25W45002050251 TIP CAP ISRAEL 1125 1125 NM GARRTT TPE731 TFE7313C WP RT HORIZ STAB DELAMINATED B O9IR K NONE O OTHER IN INSP/MAINT 1 NM 09 699MC 3058 076 THE TRAILING EDGE OF THE RIGHT HORIZONTAL STABILIZER TIP CAP (PN 24W45002050251) WAS FOUND TO BE DELAMINATING ON THE TRA ILING EDGE . THIS IS A COMPOSITE ASSEMBLY AND THE DELAMINATION WAS EASILY SEEN BY VISUAL INSPECTION. THE DEFECTIVE PAR T WAS REPLACED. THIS PART OF THE AIRCRAFT WAS INSPECTED DURING THE LAST 250 HOUR/A CHECK INSPECTION WITH NO DEFECTS NOT ED. THE 250 HOUR/ A CHECK INSPECTION WAS PERFORMED 72 HOURS PRIOR TO THE DELAMINATION BEING DISCOVERED. 2 L 7 2 4F 4 F RT A16NM E6WE 2002051700080 20020517 00080 CE 2002 5 17 O9I2002F00003 1 20020501 A 5210 241127657557 HINGE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE7312 01518 WP PAX DOOR CRACKED B O9IR K NONE O OTHER IN INSP/MAINT 1 NM 09 45AE 6344 422 LOWER ENTRY DOOR FORWARD CORNER AT HINGE WAS FOUND CRACKED. DOOR WAS REPAIRED WITH MANUFACTURER SUPPLIED PARTS. THE PR OBABLE CAUSE MAY HAVE BEEN WORN DOOR CABLES FOR AN EXTENDED TIME. MFG RECOMMENDS USING DOOR SUPPORT RODS DURING ROUTINE MAINTENANCE TO PREVENT EXCESSIVE WEAR OF DOOR HINGE. DOOR SUPPORT RODS ARE AVAILABLE FROM MFG. 2 L 7 2 4F 4 F A10CE E6WE 2002051700081 20020517 00081 EU 2002 5 17 R7MR35087 1 20020221 A 2432 RG390E BATTERY BOLKMS 117 BK117B2 5626013 EU MAIN INOPERATIVE B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 62LF 21 7163 LEAD ACID BATTERY-UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H13EU 2002051700082 20020517 00082 SO 2002 5 17 S052002F00000 1 20020417 A 5210 89630004 CABLE PIPER PA46 PA46500TP 7104622 SO PAX DOOR FRAYED B SO5R K NONE O OTHER IN INSP/MAINT 1 NE 03 5322D 78 4697074 FORWARD DOOR CABLE, (PN 89630004) FRAYED AT UPPER SWAGGED FITTING WHERE T HANDLE SCREWS ON CABLE REPLACED WITH NEW. INA DEQUATE DESIGN OF SUPPORT CABLES. CABLE KINKS AT END OF SWAGGING WHICH CAUSE FAILURE. 1 L 7 1 3O RT A25SO 2002051700083 20020517 00083 EA 2002 5 17 S8A2002F00000 2 20020409 A 7230 3017463 IMPELLER BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA COMPRESSOR BROKEN B S8AR E A ENGINE SHUTDOWN UNSCHED LANDING R A J PARTIAL RPM/PWR LOSS FLAME/FIRE WARNING INDICATION NR NOT REPORTED 1 SO 05 266EB 6810 BB266 PCE80560 AIRCRAFT DEPARTED FOR RETURN TRIP HOME. APPROXIMATELY 80 MILES FROM DEPARTURE POINT, THE ENGINE STARTED HAVING COMPRESS OR STALLS AND FLAMES COULD BE SEEN IN THE EXHAUST STACKS. ENGINE WAS SHUT DOWN AND PROPELLER FEATHERED. PRELIMINARY IN VESTIGATION BY FIELD SERVICE REP, SUGGESTED THE PROBABLE CAUSE TO BE ICE INGESTION. THE IMPELLER HAD 25 PERCENT OF ONE BLADE MISSING AND SOME OTHER BLADES WERE ROLLED OVER IN THE DIRECTION OF ROTATION. THE PILOT REPORTED THAT UPON DEPARTU RE AND PASSING THROUGH 10,000 FEET HE PUT FULL ICE PROTECTION. 1 L 7 2 4T 4 T A24CE E4EA 2002051700084 20020517 00084 CE 2002 5 17 S8A2002F00001 1 20020409 A 2612 302158 FIRE DETECTOR BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA LT ENGINE FALSE ACTIVATION B S8AR E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 05 266EB 7807 BB266 PCE80560 AIRCRAFT DEPARTED FOR RETURN TRIP HOME. APPROX 80 MILES FROM DEPARTURE POINT ENGINE STARTED HAVING COMPRESSOR STALLS AN D FLAMES COULD BE SEEN IN EXHAUST STACKS. ENGINE WAS SHUT DOWN AND PROPELLER FEATHERED. PRELIMINARY INVESTIGATION FIEL D SERVICE REPRESENTATIVE SUGGESTED PROBABLE CAUSE TO BE ICE INGESTION. THE IMPELLER HAD 25 PERCENT OF ONE BLADE MISSING AND SOME OTHER BLADES WERE ROLLED OVER IN THE DIRECTION OF ROTATION. PILOT REPORTED THAT UPON DEPARTURE AND PASSING TH ROUGH 10, 000 FEET HE PUT FULL ICE PROTECTION ON. AFTER SECURING ENGINE AND TURNING BACK TO DEPARTURE POINT LEFT ENGINE FIRE WARNING LIGHT CAME ON. THIS WAS A FALSE INDICATION ATTRIBUTITED TO HEAVY MOISTURE BEING PRESENT DURING FLIGHT. 1 L 7 2 4T 4 T A24CE E4EA 2002051700085 20020517 00085 CE 2002 5 17 T4O2002F00000 1 20020422 A 5312 10144009811 BULKHEAD BEECH 200 B200 1152922 CE PWA PT6 PT6* 52043 EA UPPER WEB SCRATCHED B T4OR K NONE O OTHER IN INSP/MAINT 1 NE 03 200QS 7157 BB1130 DURING THE 10,000 CYC AFT PRESSURE BULKHEAD INSPECTION IT WAS FOUND. AFT PRESSURE BULKHEAD SCRATCHED IN TWO HORIZONTAL LINES, 1.5 INCHES APART TO .006 INCH DEEP, FORWARD SIDE OF BULKHEAD. CAUSED BY CUTTING TOO DEEP (CARPET OR INSULATION) ALONG EDGES OF CENTER INTERIOR TRIM EXTRUSION. REPAIRED AFT PRESSURE BULKHEAD BY INSTALLING A PATCH. 1 L 7 2 4T 3 T A24CE E2NE 2002051700086 20020517 00086 CE 2002 5 17 T4O2002F00001 1 20020422 A 5330 5012015681 SKIN BEECH 90 E90 1152914 CE PWA PT6 PT6A60A 52043 NE FUSELAGE CRACKED B T4OR K NONE O OTHER IN INSP/MAINT 1 NE 03 355JS 6851 LW257 RIGHT CENTER SECTION SKIN CRACKED 2.0 INCHES BETWEEN RIVETS AT DOUBLE ROW RIVET SKIN JOINT BETWEEN RIVETS. LOCATION ON SKIN IS JUST AFT OF MAIN WING SPAR CAP AT BL 16.25. THIS AREA IS PART OF THE PRESSURE VESSEL, BEFORE TRANSITION TO THE UNPRESSUREIZED WING. LEFT CENTER SECTION SKIN CRACKED .75 INCH BETWEEN RIVETS AT DOUBLE ROW SKIN JOINT-BETWEEN RIVETS. LOCATIONS ON SKIN IS JUST AFT OF MAIN WING SPAR CAP AT BL 16.25. THIS AREA IS PART OF THE PRESSURE VESSEL, BEFORE TRAN SITION TO THE UNPRESSUREIZED WING. PROBABLE CAUSE UNKNOWN. MAY BE RESULT OF PRESSURE CYCLES, OR FATIGUE FROM LANDING C YCLES, OR VIBRATION. 1 L 7 2 3T 4 T 3A20 E4EA 2002051700087 20020517 00087 SO 2002 5 17 UG82002F00000 1 20020429 A 3220 1159L205795 BUNGEE CYLINDER GULSTM G1159 G1159A 3970109 SO NLG DOWNLOCK FAILED A UG8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 590DA 5009 445 ON LANDING ROLL-OUT, NOSE GEAR SAFE LIGHT WENT OUT AND RED UNSAFE LIGHT CAME ON. RETAINING NUT FOR THE DOWN LOCK BUNGIE BODY HAD LOOSENED ALLOWING DOWNLOCK BUNGIE TO FAIL. DISASSEMBLED BUNGIE AND INSPECTED. NO DEFECTS NOTED. REASSEMBLED PER MM AND REINSTALLED ON NOSE GEAR. COMPLIED WITH GEAR SWING TO VERIFY OPERATION. AIRCRAFT RETURNED TO SERVICE. BUN GIE WAS REPLACED UPON RETURN TO AIRPORT AS A SAFETY PRECAUTION. 2 L 7 2 4F A12EA 2002051700088 20020517 00088 EU 2002 5 17 UO22002F00007 1 20020311 A 1430 AN470AD4 RIVET ISRAEL GALAXY GALAXY 4500307 EU FUSELAGE MISINSTALLED B UO2R K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 19 290GA 26 049 THIS IS A DISCREPANCY FROM THE FACTORY. FOUND A RIVET IN THE HOLE BUT NOT BUCKED. THIS WAS LOCATED IN THE FRAME STRUCT URE AND WIRE SUPPORT ATTACHMENT POINT, APPROXIMATELY 10 INCHES LEFT OF THE TOP CENTER OF THE FUSELAGE. 2 L 7 2 4F RT A53NM 2002051700089 20020517 00089 EU 2002 5 17 UO22002F00009 1 20020309 A 3233 4AS2521010508 SWIVEL ISRAEL GALAXY GALAXY 4500307 EU ACTUATOR MISINSTALLED B UO2R K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 19 108GX 046 THE TOP SWIVEL POINT APPEARS TO BE INCORRECTLY SWAGED ALLOWING GREASE TO EXCAPE PAST THE SWAG AND THE CASTING. 2 L 7 2 4F RT A53NM 2002051700090 20020517 00090 WP 2002 5 17 ASAA0280100 1 20020322 A 4990 S9413143 O-RING DOUG DC9 DC983 3022083 WP APU LEAKING A ASAA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 01 964AS 53078 PDX - FOUND OIL ODOR IN CABIN DURING FLIGHT. REPLACED LEAKING O-RING FOR APU OIL CLUSTER. OP CHECKED OK. (M) 2 L 7 2 4F RT A6WE 2002051700091 20020517 00091 NM 2002 5 17 ASAA0280119 1 20020330 A 3350 0105606 LIGHT DOUG MD80 MD83 3023681 NM CABIN OUT OF POSITION A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 53473 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 6 THROUGH 9. RECONNECTED (REPOSITIONED) LIGHT MODULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT 2002051700092 20020517 00092 WP 2002 5 17 ASAA0280120 1 20020331 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS. RECONNECTED LOOSE CONNECTORS. LIG HTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002051700093 20020517 00093 WP 2002 5 17 ASAA0280121 1 20020401 A 5320 59366711 STRAP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON AFT CARGO DOOR CUTOUT AT STRAP AFT SIDE AT FS 1211. REPLACED STRAP PER SRM 5 1-30-5. (M) 2 L 7 2 4F RT A6WE 2002051700094 20020517 00094 WP 2002 5 17 ASAA0280122 1 20020401 A 5311 5936674U5 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND AFT AIRSTAIR LOWER STRAP ASSY FRAME CRACKED JUST ABOVE LEFT WHEEL. REPLACED FRAME PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002051700095 20020517 00095 WP 2002 5 17 ASAA0280123 1 20020401 A 5310 DO602775 RECEPTACLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND LEFT FORWARD OVERWING EXIT JAMB LOWER FORWARD LATCH PIN RECEPTACLE CRACKED AT BOTTOM OF CO NE. REPAIRED LATCH PIN RECEPTACLE PER SRM 53-05, FIG 32A. (M) 2 L 7 2 4F RT A6WE 2002051700096 20020517 00096 WP 2002 5 17 ASAA0280124 1 20020403 A 5753 59367814 HINGE FITTING DOUG DC9 DC983 3022083 WP T/E FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON RIGHT WIND INBOARD FLAP OUTBOARD HINGE FITTING BEARING BORE. REPAIRED HINGE FITTING BORE PER EA 5750-01645. (M) 2 L 7 2 4F RT A6WE 2002051700097 20020517 00097 WP 2002 5 17 ASAA0280125 1 20020403 A 5753 591921717 RETAINER DOUG DC9 DC983 3022083 WP T/E FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTING BEARING RETAINER FASTENER HOLES. REPAIRED BEARING RETAINER FASTENER HOLES PER EA 5750-01647. (M) 2 L 7 2 4F RT A6WE 2002051700098 20020517 00098 WP 2002 5 17 ASAA0280126 1 20020403 A 5753 591921810 RETAINER DOUG DC9 DC983 3022083 WP T/E FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING LOWER BEARING RETAINER FASTENE R HOLES. REPAIRED BEARING RETAINER FASTENER HOLES PER EA 5750-01647. (M) 2 L 7 2 4F RT A6WE 2002051700099 20020517 00099 WP 2002 5 17 ASAA0280127 1 20020403 A 5753 5919289 RETAINER DOUG DC9 DC983 3022083 WP T/E FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING BEARING RETAINER FASTENER HOLES . REPAIRED BEARING RETAINER FASTENER HOLES PER EA 5750-01647. (M) 2 L 7 2 4F RT A6WE 2002051700100 20020517 00100 WP 2002 5 17 ASAA0280128 1 20020403 A 5753 591921718 RETAINER DOUG DC9 DC983 3022083 WP T/E FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON RIGHT WING OUTBOARD FLAP CENTER HINGE FITTING BEARING RETAINER FASTENER HOLES . REPAIRED BEARING RETAINER FASTENER HOLES PER EA 5750-01647. (M) 2 L 7 2 4F RT A6WE 2002060500183 20020605 00183 NM 2002 6 5 F3LA200200145 1 20020510 A 5320 SUPPORT BOEING 737 737228 13844AG NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 234TR 3417 23004 DURING C-1 CHECK, INSPECTION REPORTED CORROSION ON WEB SUPPORT, STR 21L, STA 967. REPLACED WEB SUPPORT PER 51-30-2 SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002051700101 20020517 00101 NM 2002 5 17 AWXA200200430 1 20020516 A 3350 164617 BALLAST BOEING 737 7373S3 1384711 NM BS 201.16 INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 0 0 23713 PHX - EEL - FLIGHT CREW REPORTED STANDBY POWER EMERGENCY INSTRUMENT PANEL FLOOD LIGHTS ARE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE M1181 BALLAST, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002060500185 20020605 00185 NM 2002 6 5 F3LA200200146 1 20020514 A 5320 INTERCOSTAL BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 316FL 3574 25264 DURING C-2 CHECK, INSPECTION REPORTED INTERCOSTAL CORRODED AT FLANGE, STA 857, RBL 18, WL 155.5. REPLACED INTERCOSTAL P ER SRM 51-40-02, SOPM 20-41-02 AND DRAWING 65-47957. 2 L 7 2 4F RT A16WE 2002060500186 20020605 00186 NM 2002 6 5 F3LA200200147 1 20020514 A 5311 FRAME BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 316FL 3574 25264 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FWD CARGO COMPARTMENT BOTTOM FRAME FOR AFT BULKHEAD CENTER PANEL. RE PLACED SUPPORT ANGLE PER SRM 57-10-02. 2 L 7 2 4F RT A16WE 2002060500187 20020605 00187 NM 2002 6 5 F3LA200200148 1 20020515 A 5320 INTERCOSTAL BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 316FL 3574 25264 DURING C-2 CHECK, INSPECTION REPORTED LIGHT SURFACE CORROSION ON INTERCOSTAL BETWEEN STA 727B AND 727C. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-30-02, 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002060500194 20020605 00194 NM 2002 6 5 F3LA200200149 1 20020515 A 5321 PANEL BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 316FL 3574 25264 DURING C-2 CHECK, INSPECTION REPORTED SURFACE CORROSION ON RT TRANSITION PANEL, STA 767 TO 794.5. FABRICATED AND INSTAL LED REPLACEMENT PANEL PER SRM 53-60-15 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002051700102 20020517 00102 EU 2002 5 17 RAIA00205145 1 20020507 A 3320 5108WW BULB JETAIR JETSTM JETSTM4101 1500501 EU BROKEN A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 568HK 41086 5570-STL- ELECTRICAL ODORS IN AFT CABIN DURING TAXI. MAINTENANCE REPLACED CEILING FLUORESCENT LIGHT BULB. 2 L 7 2 4T RT A41NM 2002051700103 20020517 00103 2002 5 17 RAIA00205146 4 20020509 A 3400 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 555HK 12588 1194 41072 5529-STL- NUMBER 1 SYMBOL GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED #1 SYMBOL GENERATOR. 2 L 7 2 4T RT A41NM 2002051700104 20020517 00104 2002 5 17 RAIA00205148 4 20020510 A 3460 7003110912 SCREEN AEROSP ATR72 ATR72202 8680940 EU BACKED OUT A RAIA A UNSCHED LANDING O OTHER TO TAKEOFF 1 CE 03 723TE 27922 25166 283 5590-STL- FO FLIGHT INFORMATION SYS SCREEN WENT BLANK. MAINTENANCE REMOVED AND REPLACED THE FO ELECTRONIC FLIGHT INFORMA TION SYSTEM TUBE. 2 H 7 2 4T RT A53EU 2002051700105 20020517 00105 EU 2002 5 17 RAIA00205149 1 20020510 A 7740 331EDP12 PANEL JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 563HK 10309 266 41079 5367-STL- RIGHT TORQUE GAUGE WENT BLANK. MAINTENANCE REMOVED AND REPLACED ENGINE INSTRUMENT PANEL. 2 L 7 2 4T RT A41NM 2002051700106 20020517 00106 EU 2002 5 17 RAIA00205150 1 20020510 A 2612 32145602 BLEED VALVE AEROSP ATR42 ATR42300 8680920 EU BROKEN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 426TE 1363 1224 228 5464-STL- RIGHT ENGINE FIRE INDICATION. MAINTENANCE FOUND CRACKED FLANGE ON THE #2 HP BLEED VALVE AND REMOVED AND REPLAC ED THE VALVE. 2 H 7 2 4T RT A53EU 2002051700107 20020517 00107 EU 2002 5 17 RAIA00205151 1 20020510 A 3350 AMC44 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 423TE 119 5554-STL- PAX STAIR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB. 2 H 7 2 4T RT A53EU 2002051700108 20020517 00108 EU 2002 5 17 RAIA00205152 1 20020510 A 3350 AMC44 LIGHT AEROSP ATR72 ATR72202 8680940 EU CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 722TE 220 5598-STL- LEFT FORWARD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB AT FORWARD EXIT LIGHT. 2 H 7 2 4T RT A53EU 2002051900001 20020519 00001 SO 2002 5 19 C2XA02IA115 1 20020515 A 3350 W192867822 WIRE EMB 145 EMB145ER 3260211 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14933 145018 IAH- WHILE PERFORMING PREFLIGHT INSPECTION THE CREW NOTED THAT A SECTION OF EMERGENCY LIGHTING DID NOT ILLUMINATE. IAH - MAINTENANCEREPAIRED A BROKEN WIRE ON THE EMEMGENCY LIGHT STRIP, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTI NG SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002051900002 20020519 00002 WP 2002 5 19 P2EA2002V0037 1 20020516 A 5220 TAB DOUG DC9 DC982 3022082 WP FAULTY A P2EA O OTHER O OTHER IN INSP/MAINT 1 CE 05 130NJ 49222 DURING C1+C2 INSPECTION:-TAIL CONE DIDN'T PASS EMERGENCY REALEASE SYSTEM TEST DESCRIBED IN VANGUARD AIRLINES TASK CARD N UMBER 80VG-5301.-REPLACED TAIL CONE L-H & R-H UPPER LATCHES AND TAIL CONE RELEASE MECHANISM ADJUSTED & CHECKED IAW M/M 5 3-53-0. NOTE: SEE COOPESA WORK ORDER NUMBER P10430, 3-25, 3-26, VAM100 No.222, 225. 2 L 7 2 4F A6WE 2002052000001 20020520 00001 WP 2002 5 20 0201609981 1 20020514 A 2910 314195 FLEX LINE DOUG DC9 DC931 3022065 WP RT HYD SYSTEM LEAKING A NWAA K NONE K S FLUID LOSS AFFECT SYSTEMS CR CRUISE 1 GL 01 994Z 47097 INBOUND TO VPS, THE AIRCRAFT LOST THE HYDRAULIC FLUID FROM THE RIGHT SYSTEM. CREW FOLLOWED COM PROCEDURES AND WAS ABLE T O LAND WITHOUT FURTHER INCIDENT IN VPS. MAINTENANCE FOUND A PREVIOUSLY INSTALLED TEMP FLEX LINE LEAKING. REPLACED THE FL EX LINE WITH TWO NEW TEMP FLEX LINES. ALSO, REPLACED THE ENGINE DRIVEN AND ELECTIRCAL HYDRAULIC PUMPS AND THEIR FILTERS. NO CONTAMINATION WAS FOUND IN ANY RIGHT SYSTEM HYDRAULIC FILTERS. SYSTEM WAS SERVICED AND LEAK CHECK OK. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F A6WE 2002052000002 20020520 00002 WP 2002 5 20 0201619883 1 20020509 A 7100 JT8D17 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE RT ENGINE A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 01 571MC 53431 47660 688772 DURING TAKEOFF, THE CREW REPORTED SMOKE IN THE AFT CABIN AREA WITH ASSOCIATED LEFT LAV SMOKE DETECTOR WARNING. AIRCRAFT RETURNED TO FAR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE. AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4F 4 F RT A6WE E2EA 2002052000003 20020520 00003 EU 2002 5 20 R7MR34739 1 20020303 A 6210 L621M1010054 BLADE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE MAIN ROTOR DAMAGED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 135N 490 0086 MAIN ROTOR BLADE, DAMAGED TO PITCH HORN BUSHINGS (PN L621M1010232). DAMAGED TO PITCH HORN BUSHINGS PNL621M1010232. AEC TECHNICAL SERVICES ADVISED US THAT THE WEAR IS CAUSED BY IMPROPER TORQUE OF THE UPPER HEX BOLT HARDWARD. REPLACED WITH LOANER UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052000004 20020520 00004 EU 2002 5 20 R7MR34755 1 20020306 A 6340 117902111 INDICATOR BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE TRIPLE TACH IND INOPERATIVE B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 117SU 1854 7527 TRIPLE TACH INDICATOR, UNIT INOPERATIVE. 2 PERCENT NEEDLE SPLIT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H13EU E19EU 2002052000005 20020520 00005 NE 2002 5 20 R7MR34816 2 20020202 A 7240 430144801 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 163BK 6532 7063 LE45154EA NR 3 BEARING SEAL, LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002052000006 20020520 00006 NE 2002 5 20 R7MR34817 2 20020202 A 7250 430150602 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 163BK 6532 7063 NR 2 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002052000007 20020520 00007 2002 5 20 R7MR34977 4 20020308 A 3160 L316M30C1003 DISPLAY UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE COCKPIT INTERMITTENT B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 135N 495 0086 COCKPIT DISPLAY UNIT, INTERMITTENT MISSING DIGIT SEGMENTS AT MAIN FUEL QUANTITY INDICATION AND TORQUE DISPLAY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052000008 20020520 00008 EU 2002 5 20 R7MR34978 1 20020219 A 2432 45043003 BATTERY BOX UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE MASTER INOPERATIVE B R7MR K NONE L NO TEST NR NOT REPORTED 1 NM 07 135SJ 2026 0054 BATTERY MASTER BOX, CAUSED BATTERY DISCONNECT TO ILLUMINATE AFTER GPV REMOVAL AND WHILE ENGINE WAS RUNNING. WITH BATTER Y ON, NO POWER FROM TB2 OR TB3. UNIT FAILED TEST FAILURE (FAILED BEFORE COMPLETING TEST). A LATER ATTEMPT TO TEST PASS ED BUT UNIT WAS SLUGGISH. A THIRD TEST WAS DONE WHICH RESULTED IN THE SAME RESULTS AS THE FIRST. REPLACED WITH NEW UNI T CORRECTED PROBLEM. NOTE: THE REPLACEMENT UNIT HAD SOME COSMETIC SHIPPING DAMAGE. 1 G 7 2 3U 3 U O H88EU E42NE 2002052000009 20020520 00009 EU 2002 5 20 R7MR34979 1 20020304 A 7930 642790041 TRANSMITTER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE OIL PRESS INTERMITTENT B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 96LG 4637 2817 TRANSMITTER, ENGINE OIL PRESSURE- UNIT CAUSES PRESSURE GUAGE TO FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002052000010 20020520 00010 EU 2002 5 20 R7MR34980 1 20020306 A 7930 642790041 TRANSMITTER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE OIL PRESS STUCK B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 96LG 4637 2817 TRANSMITTER, ENGINE OIL PRESSURE, UNIT INOPERATIVE. CAUSES INDICATOR TO READ MAX. CONTINOUSLY (STUCK). REPLACED WITH N EW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002052000011 20020520 00011 EU 2002 5 20 02FDEA00292 1 20020424 A 2611 LIGHT AIRBUS 300 A300F4605R 3930327 EU CARGO SMOKE FALSE INDICATION A FDEA F B ACTIVATE FIRE EXT. EMER. DESCENT N FALSE WARNING DE DESCENT 1 SO 25 674FE 781 02-103 FWD CARGO SMOKE LIGHT ILLUMINATED, CREW COMPLIED WITH ECAM AND DISCHARGED FIRE AGENT INTO COMPARTMENT. (ON APU ST ART AT MEM HAD SAME LIGHT FOR A FLICKER)** S/D ** COMING 2 L 7 2 4F RT A35EU 2002052000012 20020520 00012 EU 2002 5 20 02FDEA00294 1 20020426 A 3230 LANDING GEAR AIRBUS 310 A310203 3930313 EU MAINS MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 415FE 349 02-105 AFTER TAKE OFF, ALL 3 LANDING GEAR WOULD NOT RETRACT, GEAR NOT UP AND LOCKED DISPLAYED ON ECAM. ALL 3 RED GEAR DISAGREE ARROW LIGHTS DISPLAYED. LG SYS NR 2 SEL CYCLED GEAR TWICE NO HELP. NR 1 GEN COOLER VALVE CIRCUIT BREAKER POPP ED. ** S/D ** COMING 2 L 7 2 4F RT A35EU 2002052000013 20020520 00013 NE 2002 5 20 2002F00424 2 20020415 A 7320 47385 EEC BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LEFT ENGINE INOPERATIVE G AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 518AT 20837 20837 27974 31448 (ORIG-CLOSED) FLIGHT 8027, EEC AND ENGINE LIMITER (LT) INOPERATIVE LIGHT ILLUMINATED. EICAS MSG LT AND RT EEC AND LT ENG INE LIMITER DISPLAYED. MAINTENANCE REMOVED AND REPLACED THE POWER CONDITION AND CONT UNIT. OPERATIONAL CHECK GOOD, ALL F AULTS CLEARED. 2 L 7 2 4F 4 F RT A2NM E12EU 2002052000014 20020520 00014 NE 2002 5 20 2002F00425 2 20020415 A 7320 MRFB16E02204 LIGHT BOEING 757 75733N 1384931 NM RROYCE RB211 RB211* 54555 NE RIGHT ENGINE INOPERATIVE G O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 551TZ 2151 2151 32585 31798 (ORIG-CLOSED) FLIGHT 425, RT EEC INOPERATIVE LIGHT ILLUMINATED, EICAS MSG R ENG EEC DISPLAYED. MAINTENANCE REPLACED TB00 01S, REFERENCE WDM 71-51-11, RAN ENGINES AT IDLE, NO RT EEC OR RT ENG LIMITER INOP LIGHT ON. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM A12EU 2002052000015 20020520 00015 NE 2002 5 20 2002F00426 2 20020415 A 7320 MRFB16E02204 BLOCK BOEING 757 75733N 1384931 NM RROYCE RB211 RB211* 54555 NE RT ENGINE CRACKED G AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 551TZ 2151 2151 32585 31798 (ORIG-CLOSED)FLIGHT 505, RT EEC AND ENGINE LIMITER INOPERATIVE LIGHT ILLUMINATED. EICAS MSG RT ENGINE EEC & RT ENGINE LI MITER DISPLAYED. THROTTLES WERE AT IDLE. MAINTENANCE REPLACED TB0001S, REFERENCE WDM 71-51-11, RAN ENGINES AT IDLE, NO R ENG LIMITER INOP LIGHTS ON. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM A12EU 2002052000016 20020520 00016 NM 2002 5 20 DHL2002705002 1 20020426 A 2611 LAMP BOEING 727 72722C 138400F NM SMOKE DETECTOR INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705DH 19191 UPPER LEFT CABIN SMOKE DETECTOR LAMP, INOPERATIVE. REMOVED AND REPLACED BOTH UPPER CABIN SMOKE DETECTOR BULBS IAW MM 2 6- 17-00, 401. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002052000017 20020520 00017 NM 2002 5 20 VNAA0203017 1 20020312 A 3000 WARNING LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ANTI-ICE SYSTEM ILLUMINATED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 463PS 3087 AS THE AIRCRAFT STARTED ON THE TAKE OFF ROLL, THE CREW RECEIVED AN ICE DETECT FAIL MESSAGE AND ABORTED TAKE OFF. THE AI RCRAFT EXITTED THE RUNWAY AND THE INDICATION CLEARED BY ITSELF. THE CREW THEN ATTEMPTED A SECOND TAKE OFF AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002052000018 20020520 00018 EU 2002 5 20 AALA20020330 1 20020318 A 5312 BULKHEAD FOKKER F28 F28MK0100 4990807 EU FUSELAGE DAMAGED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 1432A 11417 TUL - FOUND DAMAGE TO AFT PRESSURE BULKHEAD DUE TO IMPROPER FASTENER INSTALLATION. INSTALLED DOUBLER LEFT SIDE OF AFT P RESSURE BULKHEAD PER ESO 51000, CHAPTER 53-65-00. (M) 2 L 7 2 4F RT 2002052000019 20020520 00019 NM 2002 5 20 AALA20020388 1 20020327 A 2430 GCU BOEING 767 767323 1385205 NM E/E COMPT FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 385AM 27059 MIA - FLT 68 - STARTED CYCLING ON AND OFF PRIOR TO OCEANIC ENTRY POINT AND CONTINUED FOR REMAINDER OF FLIGHT DIVERT TO M IA. REMOVED AND REPLACED LGCB AND RGBC. CHECKED GROUNDS AND GROUND WIRE BACK TO BPCU, CHECKS NORMAL. RAN ENGINES, STI LL NO HELP. REMOVED AND REPLACED LT AND RT GENERATOR CONTROL UNITS PRECAUTIONARY. ACCOMPLISHED BITE OF BPCU, CHECK OK. REPLACED K10109 RELAY. RAN ENGINE, GND CHECK OK. REMOVED AND REPLACED LT GENERATOR CB AND RT GENERATOR CB. REPLACED LT AND RT GENERATOR CONTROL UNITS, REF E58 9139260 AND 9139258. (M) 2 L 7 2 4F RT A1NM 2002052000020 20020520 00020 WP 2002 5 20 ASAA0280113 1 20020328 A 5610 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 962AS 53076 SEA - DURING PREFLIGHT CHECK, IT WAS DETERMINED THAT LOOSE WINDOW FOAM MOLDING WAS STOPPING THE SLIDING CLEARVIEW WINDOW FROM OPENING. RE-GLUED FOAM MOLDING. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002052000021 20020520 00021 WP 2002 5 20 ASAA0280129 1 20020403 A 5522 DWG5910412 SKIN DOUG DC9 DC983 3022083 WP RT ELEVATOR PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND HOLE PUNCHED THROUGH RIGHT ELEVATOR LOWER INBOARD END. REPAIRED ELEVATOR LOWER SKIN PER E A 5520-01117. (M) 2 L 7 2 4F RT A6WE 2002052000022 20020520 00022 2002 5 20 ASAA0280134 4 20020410 A 2565 3961899501 LANYARD DOUG DC9 DC982 3022082 WP PAX DOOR SLIDE DETACHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING PREFLIGHT CHECK, L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M) 2 L 7 2 4F A6WE 2002052000023 20020520 00023 WP 2002 5 20 ASAA0280135 1 20020410 A 5313 59364321 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON LONGERON 28 AT FS 1097 TO 1113. REPAIRED LONGERON 28 PER EA 5310-02078. (M) 2 L 7 2 4F RT A6WE 2002052000024 20020520 00024 WP 2002 5 20 ASAA0280136 1 20020410 A 5230 5910141105 PAN DOUG DC9 DC983 3022083 WP CARGO DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND AFT CARGO DOOR JAMB GOUGED AT LOWER FORWARD AND AFT BARRIER DOOR LOCK GUIDE BLOCK LOCATION S. BLEND REPAIRED DOOR JAMB PER EA 5230-01168. (M) 2 L 7 2 4F RT A6WE 2002052000025 20020520 00025 WP 2002 5 20 ASAA0280137 1 20020410 A 5610 59644202 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 27893 53451 SEA - DURING PREFLIGHT CHECK, FOUND IT WAS DETERMINED THAT THE RIGHT SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. RE-STOWED WINDOW ALIGNMENT PIN INTOP TRACK. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002052000026 20020520 00026 WP 2002 5 20 ASAA0280138 1 20020411 A 5330 59360331 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON EXTERNAL SKIN AT FS 1122-1128. REPAIRED FUSELAGE SKIN PER EA 5330-01575. (M ) 2 L 7 2 4F RT A6WE 2002052000027 20020520 00027 2002 5 20 ASAA0280139 4 20020402 A 2565 3961899501 LANYARD DOUG MD80 MD83 3023681 NM PAX DOOR SLIDE DETACHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 PHX - DURING PREFLIGHT CHECK, L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT 2002052000028 20020520 00028 WP 2002 5 20 ASAA0280140 1 20020415 A 5532 591216610 SKIN DOUG DC9 DC983 3022083 WP VERTICAL STAB CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND VERTICAL STABILIZER SKIN CHAFED FROM AFT TO CENTER AREA, WHERE BANANA FAIRING 3804A IS MOU NTED. REPAIRED VERTICAL STABILIZER SKIN PER EA 5530-01089. (M) 2 L 7 2 4F RT A6WE 2002052000029 20020520 00029 WP 2002 5 20 ASAA0280141 1 20020420 A 5210 5914730533 MECHANISM DOUG DC9 DC983 3022083 WP PAX DOOR DAMAGED A ASAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 01 960AS 53074 PHX - L1 DOOR HOLD OPEN MECHANISM WILL NOT LATCH. STRAIGHTENED HOLD OPEN HOOK. DOOR NOW LATCHES OPEN NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002052000030 20020520 00030 WP 2002 5 20 ASAA0280142 1 20020424 A 5330 59124921 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND FORWARD LOWER CORNER OF R1 DOOR CUTOUT DAMAGE. REPAIRED PER EA 5310-02071. (M) 2 L 7 2 4F RT A6WE 2002052000031 20020520 00031 WP 2002 5 20 ASAA0280143 1 20020424 A 5320 5936442 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON AFT CARGO BAY CLOSEOUT WEB FASTENER HOLES. REPAIRED CLOSEOUT WEB PER EA 5310 -02075. (M) 2 L 7 2 4F RT A6WE 2002052000032 20020520 00032 WP 2002 5 20 ASAA0280144 1 20020424 A 5320 993061215 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON WEB AT FS 1022-1041. REPLACED WEB PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002052000033 20020520 00033 WP 2002 5 20 ASAA0280145 1 20020425 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP MID CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 33148 53079 PHX - DURING LINE CHECK EXTERIOR, OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED POWER SUPPLY. EMERGENCY L IGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002052000034 20020520 00034 WP 2002 5 20 ASAA0280146 1 20020425 A 5530 991196213 WEB DOUG DC9 DC983 3022083 WP VERTICAL STAB CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND VERTICAL STABILIZER BULLET FAIRING WEB CHAFED AROUND EDGES WHERE PANEL 6308C TO UPPER TIP BULLET FAIRING IS INSTALLED. REPLACED WEB PER SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2002052000035 20020520 00035 EA 2002 5 20 ASOA02188 1 20020325 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 889AS 7538 FLT 4768 - DURING GROUND INSPECTION IN ATL, THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE BURNED OUT EXTERIOR OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SER VICE. (M) 2 L 7 2 4F RT A21EA 2002052000036 20020520 00036 SO 2002 5 20 ASOA02189 1 20020326 A 3350 W220029324 CONNECTOR EMB 120 EMB120RT 3260202 SO CABIN LOOSE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 236AS 120049 DURING GROUND INSPECTION IN ATL, THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WAS INOPERATVE. MAINTENANCE RESECURED A LOOSE CONNECTION BEHIND THE LAVATORY ASSEMBLY. SYSTEM OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002052000037 20020520 00037 SO 2002 5 20 ASOA02190 1 20020326 A 3350 1317 BULB EMB 120 EMB120RT 3260202 SO FUSELAGE INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 244AS 120073 DURING A HANGAR INSPECTION IN TXK, THE RIGHT FRONT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE BURNED OUT EXTERIOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002052000038 20020520 00038 SO 2002 5 20 ASOA02191 1 20020320 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 285AS 120265 DURING C-CHECK FOUND INSPECTION IN BNA, THE LOWER AFT FLOOR FLANGE AT FRAME 13 WAS CORRODED. MAINTENANCE REPAIRED THE C ORRODED FLOOR FLANGE IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002052000039 20020520 00039 SO 2002 5 20 ASOA02192 1 20020320 A 5347 12015997001 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 285AS 120265 DURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD WALL SEAT TRACK FROM FRAME 14 TO FRAME 32 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED WALL SEAT TRACK IAW SRM 51-40-02 AND ALSO REF ASA EO120-25-0007C, WHICH FACILITATES SEAT TRACK SPLICING INSTRUCTIONS AND ESTABLISHES WEAR LIMITS. (M) 2 L 7 2 4T RT A31SO 2002052000040 20020520 00040 SO 2002 5 20 ASOA02193 1 20020320 A 5347 12015995001 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 285AS 120265 DURING C-CHECK, FOUND INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT FLOOR SEAT TRACK BETWEEN FRAMES 17 AND 32. MAI NTENANCE REMOVED AND REPLACED THE CORRODED FLOOR SEAT TRACK IAW SRM 51-40-02 AND ALSO REF ASA EO120-25-0007C, WHICH FACI LITATES SEAT TRACK SPLICING INSTRUCTIONS AND ESTABLISHES WEAR LIMITS. (M) 2 L 7 2 4T RT A31SO 2002052000041 20020520 00041 EA 2002 5 20 ASOA02194 1 20020327 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 832AS 7243 FLT 4390 - DURING GROUND INSPECTION IN ATL, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE BURNED OUT OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002052000042 20020520 00042 EA 2002 5 20 ASOA02195 1 20020328 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 884AS 7513 FLT 4589 - DURING GROUND INSPECTION IN ATL, THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002052000043 20020520 00043 EA 2002 5 20 ASOA02196 1 20020328 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A ASOA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 SO 11 857AS 7411 DURING CRUISE FLIGHT FROM ATL-ORH, AT FL330, THE CAPTAINS WINDSHIELD SHATTERED. AN EMERGENCY WAS DECLARED AND AN EMERGE NCY DESCENT WAS PERFORMED AT A SLOWER AIRSPEED OF APPROXIMATELY 250 KIAS TO 10,000 FEET. AIRCRAFT DIVERTED TO JFK AND M ADE AN UNEVENTFUL LANDING. (M) 2 L 7 2 4F RT A21EA 2002052000044 20020520 00044 EA 2002 5 20 ASOA02197 1 20020328 A 5720 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 858AS 7417 DURING HANGAR MAINTENANCE IN MCN, THE RIGHT WING FITTING WAS FOUND TO BE CRACKED. MAINTENANCE WILL REPLACE THE RIGHT WI NG TRAILING EDGE RIB. (M) 2 L 7 2 4F RT A21EA 2002052000045 20020520 00045 EA 2002 5 20 ASOA02198 1 20020330 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 870AS 7500 FLT 4787 - DURING GROUND INSPECTION IN XNA, THE LEFT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVIC E. (M) 2 L 7 2 4F RT A21EA 2002052000046 20020520 00046 SO 2002 5 20 ASOA02199 1 20020330 A 3350 F02A250V1A FUSE EMB 120 EMB120ER 3260203 SO CABIN BLOWN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 503AS 120275 DURING A HANGAR INSPECTION IN MCN, THE FLOOR EMERGENCY LIGHTS IN FRONT OF THE GALLEY WERE INOPERATIVE. MAINTENANCE REPL ACED A BLOWN FUSE IN THE FUSE HOLDER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002052000047 20020520 00047 EA 2002 5 20 ASOA02211 1 20020409 A 2430 GCU CNDAIR CL600 CL6002B19 1900309 EA RIGHT FAILED A ASOA B A EMER. DESCENT UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 11 825AS 7207 FLT 4592 - DURING FLIGHT FROM ATL TO ISP, WITH HAVING THE AUXILIARY POWER UNIT PREVIOUSLY DEFERRED, THE RIGHT INTERGRATE D DRIVE GENERATOR FAILED. AN EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED AND LANDED SAFELY IN RDU. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE GENERATOR CONTROL UNIT (P/N 720846D) AND THE RIGHT ENGINE INTERGRATED DRIVE GENERATOR (P/N 7 55469E). OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002052000048 20020520 00048 EA 2002 5 20 ASOA02212 1 20020412 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 885AS 7521 DURING GROUND INSPECTION IN ATL, THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT RIGHT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002052000049 20020520 00049 EA 2002 5 20 ASOA02213 1 20020413 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 872AS 7542 DURING GROUND INSPECTION IN ATL, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002052000050 20020520 00050 EA 2002 5 20 ASOA02214 1 20020413 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 864AS 7502 DURING GROUND INSPECTION IN ATL, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002052000051 20020520 00051 SO 2002 5 20 ASOA02215 1 20020413 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE CANNING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 503AS 120275 DURING HANGAR MAINTENANCE IN MCN, THERE WAS OIL CANNING OF THE FUSELAGE SKIN UNDER THE FORWARD SIDE OF THE CARGO DOOR FR AME. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE SKIN ON THE LEFT SIDE OF THE FUSELAGE IAW SRM CHAPTERS 51 AND 53. (M) 2 L 7 2 4T RT A31SO 2002052000052 20020520 00052 EU 2002 5 20 ASOA02216 1 20020415 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 535AS 464 DURING C-CHECK INSPECTION IN BNA, THE TOP AND BOTTOM SURFACES WERE CORRODED ON THE TOP FLANGE OF THE FLOORBEAM AT FRAMES 36, 38, 39 AND 40. MAINTENANCE REPAIRED THE CORRODED FLOORBEAM TOP FLANGES IAW ASA EO 72-53-0130. (M) 2 H 7 2 4T RT A53EU 2002052000053 20020520 00053 SO 2002 5 20 ASOA02217 1 20020415 A 3350 3071BPE BULB EMB 120 EMB120RT 3260202 SO CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 274AS 120229 DURING A HANGAR INSPECTION IN TXK, THE FORTH LIGHT BULB IN THE EMERGENCY FLOOR LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY FLOOR LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M ) 2 L 7 2 4T RT A31SO 2002052000054 20020520 00054 EU 2002 5 20 ASOA02218 1 20020415 A 3350 3012000 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 534AS 463 DURING HANGAR INSPECTION IN MCN, THE FLOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE EMERGENCY LIGHTING POWER SUPPLY IN THE 61WL POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052000055 20020520 00055 SO 2002 5 20 ASOA02219 1 20020415 A 3350 AGC1 LIGHT EMB 120 EMB120RT 3260202 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 230AS 120032 FLT 4056 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE FLOOR EMERGENCY LIGHTS BETWEEN ROWS 2 AN D 4 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT FUSE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002052000056 20020520 00056 EA 2002 5 20 ASOA02222 1 20020416 A 3350 487191 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DIRTY A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 853AS 7374 FLT 4515 - DURING GROUN INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THAT ONE STRAP OF EMERGENCY FLOOR LEVEL LIGHTIN G WAS INOPERATIVE. MAINTENANCE CLEANED THE CONNECTOR ON THE INOPERATIVE STRIP OF EMERGENCY LIGHTING. OPERATIONAL CHECK S GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002052000057 20020520 00057 SO 2002 5 20 ASOA02223 1 20020401 A 5313 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 261AS 120141 DUIRNG C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON STRINGER 18 LEFT BETWEEN FRAMES 16 AND 18. MAINTENANCE REMOVED THE CORRODED SECTION OF THE STRINGER AND REPLACED IT WITH A SPLICE IAW SRMS 51-25-00, 51-40-02 AND 51-40-05. (M) 2 L 7 2 4T RT A31SO 2002052000058 20020520 00058 SO 2002 5 20 ASOA02224 1 20020401 A 5320 12026674001 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 261AS 120141 DURING C-CHECK INSPECTION IN BNA, THE FLOORBOARD SUPPORT ANGLE WAS FOUND CORRODED AT FRAME 13. MAINTENANCE REPAIRED THE CORRODED SECTION OF THE FLOORBOARD SUPPORT ANGLE IN ACCORDANCE WITH SRMS 51-21-04, 51-21-05, 51-21-06, AND 51-40-02. ( M) 2 L 7 2 4T RT A31SO 2002052000059 20020520 00059 SO 2002 5 20 ASOA02225 1 20020401 A 5320 12027857001 SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 261AS 120141 DURING C-CHECK INSPECTION IN BNA, THE COCKPIT STEP AREA FLOOR FLANGE, FORWARD LEFT CORNER WAS FOUND CORRODED AND BENT WI TH SOME RIVETS THAT WERE PULLED THROUGH. MAINTENANCE RETURNED THE STEP SUPPORT TO ITS ORIGINAL CONTOUR AND REMOVED AND REPLACED THE PULLED THROUGH RIVETS IAW SRM 51-40-02. MAINTENANCE ALSO REPAIRED THE CORROSION IAW SRMS 51-25-00, 51-40-0 5, 51-21-00, AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002052000060 20020520 00060 SO 2002 5 20 ASOA02226 1 20020401 A 5320 12004449001 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 261AS 120141 DURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD CROSSBEAM WAS FOUND CORRODED AT FRAME 40. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRMS 51-25-00, 51-21-03 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002052000061 20020520 00061 SO 2002 5 20 ASOA02227 1 20020401 A 5320 SILL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 261AS 120141 DURING C-CHECK INSPECTION IN BNA, THE COCKPIT RIGHT HAND OUTBOARD FLOOR SILL PLATE WAS CORRODED BETWEEN FRAMES 7 AND 13. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRMS 51-25-00, 51-21-00, AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002052000062 20020520 00062 SO 2002 5 20 ASOA02228 1 20020401 A 5347 12026884005 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 261AS 120141 DURING C-CHECK INSPECTION IN BNA, THE AFT SECTION OF THE LEFT FLOOR SEAT TRACK WAS CORRODED BETWEEN FRAMES 32 AND 39. M AINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR SEAT TRACK IAW SRMS 51-25-00 AND 51-21-02 AND AMM 53-01-05. (M) 2 L 7 2 4T RT A31SO 2002052000063 20020520 00063 SO 2002 5 20 ASOA02229 1 20020401 A 5347 12015996005 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 261AS 120141 DURING C-CHECK INSPECTION IN BNA, THE AFT SECTION OF THE RIGHT WALL SEAT TRACK WAS CORRODED BETWEEN FRAMES 34 AND 38. M AINTENANCE REMOVED THE CORRODED SEAT TRACK, FABRICATED A NEW ONE AND INSALLED IAW SRMS 51-40-02, 51-25-00, 51-21-02, 51- 21-05 AND 51-10-00. (M) 2 L 7 2 4T RT A31SO 2002052000064 20020520 00064 SO 2002 5 20 ASOA02230 1 20020401 A 5347 12005803001 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 261AS 120141 DURING C-CHECK INSPECTION IN BNA, THE RIGHT SEAT TRACK SILL PLATE FLANGE WAS FOUND CORRODED BEYOND LIMITS AT FRAMES 17, 19 AND 22. WHILE REPAIRING THE SILL PLATE (P/N 120-05803-01) THE RIGHT OUTBOARD CROSSBEAM (P/N 12004149-002) AT FRAME 1 6 WAS ALSO FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE FLANGE IAW SRMS 51-40-02 AND 51-21- 02. MAINTENANCE ALSO REMOVED AND REPLACED THE CORRODED CROSSBEAM AT FRAME 16 IAW SRMS 51-25-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002052000065 20020520 00065 SO 2002 5 20 ASOA02231 1 20020401 A 5320 12004171003 SILL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 261AS 120141 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT HAND SILL PLATE IN SPOTS BETWEEN FRAMES 29 AND 34. MA INTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRM'S 51-40-02, 51-40-02, 51-40-05, AND 51-20-02. (M) 2 L 7 2 4T RT A31SO 2002052000066 20020520 00066 SO 2002 5 20 ASOA02232 1 20020401 A 5310 12046163005 BUTT STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 261AS 120141 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT BUTT STRAP BETWEEN FRAMES 20 AND 32. MAINTENANCE REMO VED AND REPLACED THE CORRODED BUTT STRAP IAW SRM'S 51-40-02, 51-40-00, AND 51-21-02. (M) 2 L 7 2 4T RT A31SO 2002052000067 20020520 00067 SO 2002 5 20 ASOA02233 1 20020401 A 5310 12006158003 BUTT STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 261AS 120141 DURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP IN THE CARGO AREA BETWEEN FRAMES 40 AND 44 WAS CORRODED. MAINTE NANCE REMOVED AND REPLACED THE CORRODED CENTER BUTT STRAP IAW SRM'S 51-40-02 AND 51-25-00. (M) 2 L 7 2 4T RT A31SO 2002052000068 20020520 00068 EU 2002 5 20 ASOA02234 1 20020416 A 2530 COFFEEMAKER AEROSP ATR72 ATR72 EU GALLEY SMOKE A ASOA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 530AA 453 FLT 4051 - DURING CRUISE FLIGHT FROM ATL TO VPS, THE FLIGHT ATTENDANT REPORTED A BURNING SMELL COMING FROM THE GALLEY AR EA. THE CAPTAIN ADVISED THE FILGHT ATTENDANT TO PULL ALL THE GALLEY CIRCUIT BREAKERS, TURN OFF ALL THE SWITCHES, AND TH OROUGHLY CHECK FOR SIGNS OF SMOKE OR HEAT. AFTER THESE ACTIONS WERE PERFORMED THE SMELL SUBSIDED AND NO EVIDENCE OF SMO KE OR HEAT WAS FOUND. AIRCRAFT LANDED UNEVENTFULLY IN VPS. MAINTENANCE INSPECTED AND FOUND THE GALLEY COFFEE POTS EMPT Y WITH SMOLDERING COFFEE STAINS IN THE BOTTOM. MAINTENANCE CLEANED AND PERFORMED AN OPERATIONAL CHECK OF THE POTS AND N O MORE SMELL WAS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2002052000069 20020520 00069 EU 2002 5 20 ASOA02235 1 20020418 A 3350 167006 BULB AEROSP ATR72 ATR72212 8680945 EU CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 531AS 454 DURING HANGAR INSPECTION IN MCN, THE AFT FLOOR EMERGENCY TRACK LIGHTING WAS FOUND BURNED OUT. MAINTENANCE REMOVED AND R EPLACED THE BURNED OUT EMERGENCY LIGHT BULBS. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052000070 20020520 00070 EA 2002 5 20 ASOA02236 1 20020418 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 867AS 7463 DURING A SCHEDULED INSPECTION IN XNA, THE FORWARD CABIN OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE BURNED OUT OVERHEAD EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002052000071 20020520 00071 EA 2002 5 20 ASOA02237 1 20020418 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 861AS 7445 FLT 4505 - DURING A SCHEDULED INSPECTION IN XNA, THE FORWARD CABIN OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE BURNED OUT OVERHEAD EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002052000072 20020520 00072 SO 2002 5 20 ASOA02238 1 20020418 A 3350 BATTERY PACK EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 274AS 22391 120229 DURING GROUND INSPECTION IN DFW, THE CREW REPORTED THE MID SECTION OF FLOOR EMERGENCY LIGHTS AS WELL AS THE OVERWING EXI T LIGHTS STAYED ON EVEN AFTER SELECTED TO THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMEGENCY LIGHT BA TTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002052000073 20020520 00073 EA 2002 5 20 ASOA02239 1 20020418 A 5610 NP1393219 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA O OTHER O OTHER LD LANDING 1 SO 11 873AS 1249 7549 AFTER LANDING IN ATL, THE CAPTAINS WINDSHIELD CRACKED FOR UNKNOWN REASONS. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN S WINDSHIELD ASSEMBLY. OPERATIONAL CHECK OF WINDOW HEAT GOOD. PRESSURIZATION WAS CHECKED AT 6 DELTA P FOR TEN MINUTES WITH NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002052000074 20020520 00074 EU 2002 5 20 ASOA02240 1 20020418 A 2120 ODOR AEROSP ATR72 ATR72212 8680945 EU COCKPIT DETECTED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 11 533AS 460 FLT 4314 - DURING DESCENT INTO ATL, THE CAPTAIN REPORTED AN ELECTRIC SMOKE WARNING AND THE SMELL OF ELECTRICAL SMOKE IN THE COCKPIT. THE FLIGHT ATTENDANT ALSO REPORTED A SMOKE SMELL IN THE CABIN. THE CREW PERFORMED THE APPROPRIATE CHECKLI STS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE HANDLING BL EED VALVE (P/N 32897041) AND BOTH OF THE OVER TEMPERATURE SENSORS (P/N 6411343). MAINTENANCE PERFORMED POWER RUNS ON TH E AIRCRAFT FOR THE HMU WITH THE BLEEDS AND PACKS ON HIGH, AND NO SMOKE OR SMELL WAS NOTED. OPERATIONAL CHECKS GOOD. AI RCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052000075 20020520 00075 NM 2002 5 20 CALA0200298 1 20020519 A 5320 65465648 SHEAR TIE BOEING 737 7373T0 1384582 NM STA 986.5 CORRODED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 14347 23585 AFT BILGE AREA CORROSION WHERE ANGLE BRACKETS MEET AFT FACE OF FRAME STATION 986.5 BETTWEEN 27L AND 27R BL0. REMOVED AND REPLACED SHEAR TIE ANGLE PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002052000076 20020520 00076 WP 2002 5 20 CALA0200299 1 20020519 A 5313 2777922 LONGERON DOUG DC9 DC982 3022082 WP STA 351 CORRODED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 72822 49482 LONGERON 28R AT STATION 351 CORRODED. CUT OT DAMGED SECTION. SPLICED IN NEW SECTION PER SRM 53-02. 2 L 7 2 4F A6WE 2002052000077 20020520 00077 WP 2002 5 20 CALA0200300 1 20020519 A 5315 9915527506 CHANNEL DOUG DC9 DC982 3022082 WP STA 927 RT CRACKED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 83870 48056 CABIN FLOOR BEAM CHANNEL CRACKED AT MAIN FRAM ATTACH POINT AT STATION 927 RIGHT. INSTALLED NEW FLOOR BEAM CHANNEL PER SR M 51-30-00. 2 L 7 2 4F A6WE 2002052000078 20020520 00078 WP 2002 5 20 CALA0200302 1 20020520 A 5347 602500376 SEAT TRACK DOUG DC9 DC982 3022082 WP FS1174-1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 LEFT OUTBOARD SEAT TRACK HAS EXFOLIATION CORROSION STATION 1174 TO 1309. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-5 AND 51-30-1. 2 L 7 2 4F A6WE 2002052000079 20020520 00079 WP 2002 5 20 CALA0200303 1 20020517 A 5347 301FH050SS SEAT TRACK DOUG DC9 DC982 3022082 WP F/O SEAT WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 FIRST OFFICER UPPER AND LOWER SEAT TRACK WORN. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-1, 51-30-2, AND 51-10-4. 2 L 7 2 4F A6WE 2002052000080 20020520 00080 WP 2002 5 20 CALA0200304 1 20020517 A 5313 7075T6050 INTERCOSTAL DOUG DC9 DC982 3022082 WP FS 1136-1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 AFT PIT F/S 1136 TO 1155 LONGERON 30 INTERCOSTAL CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-5. 2 L 7 2 4F A6WE 2002052000081 20020520 00081 WP 2002 5 20 0201489921 1 20020424 A 5310 PRESSURE PANEL DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 47647 During Mck in ATL, a crack was found in the flight compartment horizontal pressure panel at station 105, at LH x=25 (1.0 ") long. Repaired per EA 99-189672. 2 L 7 2 4F A6WE 2002052000082 20020520 00082 WP 2002 5 20 0201499921 1 20020425 A 5410 RIB DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 47647 During MCK in ATL, the aft portion of the lower cap, P/N 9958159-57, of the closing rib was found cracked. The crack was approximately .7" long on extends from a fastener hole 3.7" forward from the aft end of the cap. 2 L 7 2 4F A6WE 2002052000083 20020520 00083 WP 2002 5 20 0201509921 1 20020502 A 5720 ANGLE DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 47647 During MCK in ATL, angle 5910465-33 was found cracked. Repaired per S/B 57-103 and EA 99-189678. 2 L 7 2 4F A6WE 2002052000084 20020520 00084 WP 2002 5 20 0201519921 1 20020506 A 5310 FRAME DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 47647 During MCK in ATL, while inspecting the interior structure, the RH side of the 598 frame was found to have 3.0 inch long crack between longeron 18 an 19, on the outboard flange. The crack runs fron the first fastener hole below the pocket t o the third hole. Repaired per EA 99-189681. 2 L 7 2 4F A6WE 2002052000085 20020520 00085 WP 2002 5 20 0201529954 1 20020502 A 5310 DOOR FRAME DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 921RW 47164 While in MSP during line operations a crack was found on the Non-ventral APB door jamb. The crack is located at the end of the LH side #2 radial.Repaired per EA 99-189338. 2 L 7 2 4F A6WE 2002052000086 20020520 00086 WP 2002 5 20 0201539861 1 20020509 A 5330 SKIN DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 770NC 47758 During MCK in ATL, corrosion was found in a temporary repair in the lower forward VHF antenna between stations 465-484 a nd longeron 30. After removal of repair several cracks were found. Repaired per EA 98-189679. 2 L 7 2 4F RT A6WE 2002052000087 20020520 00087 WP 2002 5 20 0201549861 1 20020501 A 5310 INTERCOSTAL DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 770NC 47758 During MCK in ATL, At sta 180 a crack found on the 9923484 intercostal at X=20. Repaired per EA 98-189693. 2 L 7 2 4F RT A6WE 2002052000088 20020520 00088 WP 2002 5 20 0201559861 1 20020508 A 5310 INTERCOSTAL DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 770NC 47758 During MCK in ATL, a crack was found on intercostal 991157-3 at sta. 148.5 to 160. approx. z 44. Repaired per EA 98-1896 71. 2 L 7 2 4F RT A6WE 2002052000089 20020520 00089 NM 2002 5 20 02FDEA00326 1 20020511 A 3610 CLAMP BOEING 727 727200 138407E NM PNEUMATIC SYS LOOSE A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 208FE 22930 LOWER AFT BODY OVERHEAT LIGHT FLICKERED SEVERAL TIMES THEN REMAINED ON STEADY FOR APPROX 20 SEC IN FLT WHILE EXECUTING P ROC IN ORH LIGHT WENT OUT. PERFORMED RESISTANCE CHECKS OF OVERHEAT ELEMENTS. ALL RESISTANCE CHECKS ARE GOOD PER MM 26- 14-001-2. GAIN ACCESS TO KEEL BEAM AND AFT CARGO DUCTING AND ELEMENTS TO BE PHYSICALLY CHECKED ON ENGINE RUN. NR 1 ENG INE PURGE VALVE PNEUMATIC DUCT CLAMP LEAKING AIR ON OVERHEAT LOOP AFT OF STA 1243 IN AFT AIRSTAIR AREA. TIGHTEN CLAMP A ND LEAKED CHECK OK. 2 L 7 3 4F RT A3WE 2002052000090 20020520 00090 NE 2002 5 20 02FDEA00327 2 20020511 A 7200 CF650C2 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 DAMAGED A FDEA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 25 307FE 48291 AT 31,000 FT ALT, JUST BEFORE DESCENT NR 3 ENGINE RUMBLED TWICE AND N1 STARTED TO DECREASE. RETARDED THROTTLE TO IDLE A ND N1 WAS 38 PERCENT. ADVANCE THROTTLE NO MOVEMENT ON ENGINE WHEN PASSED THROUGH 10,000 FT. ENGINE RUMBLED AND CAME BA CK TO NORM. REINSTALLED BORESCOPE PLUGS AND REMOVED TURNING TOOL AND REINSTALLED COVER PLATE. REMOVED AND REPLACED FUE L FLOW TRANSMITTER REF DC-10-30MM 73-31-02-2. LEAK AND OPS CHECKS GOOD ON ENGINE RUN. REMOVED AND REPLACED NR 3 ENGI NE PER W/C71T0101-3. PERFORMED ENGINE VIB CHECK PER DC10-30 M/M 72-00-00-5. ENG CHECKED NORMAL PER M/M. 2 L 7 3 4F 4 F A22WE E23EA 2002052300142 20020523 00142 NM 2002 5 23 02FDEA00328 1 20020510 A 5330 6554588 SKIN BOEING 727 727200 138407E NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 209FE 22931 N 321 SKIN CHAFED AT SKIN LAP STR 19 RT, BS 720D+13. R&R SKIN PER SRM 53-30-3 FIG 14. 2 L 7 3 4F RT A3WE 2002060600151 20020606 00151 NM 2002 6 6 02FDEA00329 1 20020512 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 GOUGE IN EXTERNAL SKIN AT STR 17L, BS 400. REMOVED AND REPLACED SKIN PER SRM 53-30-3 & EA 7-5330-54245. 2 L 7 3 4F RT A3WE 2002052000091 20020520 00091 NM 2002 5 20 02FDEA00331 1 20020513 A 2710 ARH7054517 ACTUATOR DOUG MD11 MD11 3023602 NM AILERON FAILED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 604FE 48460 ON TAKEOFF AFTER SLATS RETRACTED LVL 2 AIL DEFLECT DISAGREE ALERT ILLUM'D. REMOVED AND REPLACED LT & RT INBOARD DEFLECT AILERON ACTUATORS PER MM 27-16-01-4. RIGGED, ADJUSTED AND TESTED OK. 2 L 7 3 4F RT A22WE 2002052000092 20020520 00092 NM 2002 5 20 02FDEA00332 1 20020514 A 3610 CLAMP BOEING 727 727100 1384036 NM PNEUMATIC SYS LEAKING A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 191FE 19084 DURING INITIAL CLIMB, ENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED, WING ANTI ICE VERIFIED CLOSED, NR 1 ENG BLEED AIR SWITC H CLOSED AND NR 1 ENG THRUST LEVER TO IDLE IAW RED TABS, STRUT OVERHEAT LIGHT EXTINGUISHED AFTER 3 MINS AND OVERHEAT SYS TEM TESTED SATISFACTORY. FOUND NR 1 ENG DUCT BETWEEN SHUTOFF VALVE AND BLEED AIR HEAT EXCHANGER LEAKING. REPLACED CLAM P AND PERFORMED DUCT LEAKAGE TEST PER M/M REF 36-00-000-5. LEAK CKS OK. RAN ENGINES, OPS CK'D NR 1 BLEED SYSTEM IAW JR H 7-4, CK'D GOOD PER JRH. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2002052000093 20020520 00093 NM 2002 5 20 02FDEA00333 1 20020516 A 2612 FIRE WARNING BOEING 727 727200 138407E NM COCKPIT MALFUNCTIONED A FDEA O OTHER N FALSE WARNING DE DESCENT 1 SO 25 467FE 21449 ON DESCENT, RECEIVED ENGINE FIRE WARNING BELL AND ENGINE FIRE WARNING LIGHT WITH NO ASSOCIATED FIRE PULL HANDLE LIGHTS. ALL ENGINE PERFORMANCE PARAMETERS WERE NORMAL. FOLLOWED CHECKLIST. FIRE WARNING SYSTEM TEST SATISFACTORY. CONTINU ED DESCENT TO LANDING AT DESTINATION. T/S AND COMPLIED WITH ENGINE FIRE DETECTION IAW B727-200 AMM 26-11-000-5. ALSO C OMPLIED WITH CARGO SMOKE DETECTION TEST IAW B727-200 AMM 26-16-001-5, NO DEFECTS NOTED. SYSTEM OPERATES NORMAL. 2 L 7 3 4F RT A3WE 2002052000094 20020520 00094 NM 2002 5 20 02FDEA00334 1 20020516 A 2612 FIRE WARNING BOEING 727 727200 138407E NM COCKPIT MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 467FE 21449 ON DESCENT, RECEIVED ENGINE FIRE WARNING BELL AND ENGINE FIRE WARNING LIGHT WITH NO ASSOCIATED FIRE PULL HANDLE LIGHTS. ALL ENGINE PERFORMANCE PARAMETERS WERE NORMAL. FOLLOWED CHECKLIST. FIRE WARNING SYSTEM TEST SATISFACTORY. CONTINUED DESCENT TO LANDING AT DESTINATION. COMPLIED WITH ENGINE FIRE DETECTION IAW B727-200 AMM 26-11-000-5. ALSO COMPLIED WIT H CARGO SMOKE DETECTION TEST IAW B727-200 AMM 26-16-001-5, NO DEFECTS NOTED. SYSTEM OPERATES NORMAL. 2 L 7 3 4F RT A3WE 2002060600165 20020606 00165 NM 2002 6 6 02FDEA0330 1 20020512 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CORROSION ON SKIN BS 720D+16, STR 26L. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 5 & EA 7-5330-64102. 2 L 7 3 4F RT A3WE 2002052000095 20020520 00095 NM 2002 5 20 2002F00502 1 20020430 A 2612 710126 FIRE LOOP BOEING 757 75733N 1384931 NM LT ENGINE FAULTY G AMTA K NONE N FALSE WARNING CR CRUISE 1 GL 11 554TZ 1839 1839 32588 FLIGHT NUMBER 925, DURING CRUISE THE LEFT ENGINE FIRE LP NR 1 STATUS MESSAGE DISPLAYED. MAINTENANCE REMOVED AND REPLACE D THE NR1 FIRE LOOP DET PER MM 26-11-01-4. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002052000096 20020520 00096 NE 2002 5 20 2002F00503 2 20020505 A 7321 FFG022AD FUEL CONTROL BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE MALFUNCTIONED G AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 520AT 2126 2126 27976 31558 AFTER PUSHBACK FROM GATE AND UPON LEFT ENGINE START, RECEIVED EICAS ADVISORY MESSAGES L ENG EEC AND L ENG LIMITER, AS WE LL AS L ENG LIMITER INOP LIGHT AND L ENG EEC INOP LIGHT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE FUEL FLOW GOV ERNOR PER MM 73-21-01 AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002052000097 20020520 00097 2002 5 20 2002F00504 4 20020422 A 3460 4077880908 CDU BOEING 757 75723N 1384973 NM COCKPIT INOPERATIVE G K NONE J WARNING INDICATION CR CRUISE 1 GL 11 527AT 5399 5399 30886 FLIGHT NUMBER 273, DURING CRUISE FIRST OFFICERS CDU WENT BLANK. SELECTING ALTERNATE FMC DID NOT CORRECT FAULT. MAINTEN ANCE REMOVED AND REPLACED THE FLIGHT MANAGEMENT COMPUTER CONTROL DISPLAY UNIT PER MM 34-61-02. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002052000098 20020520 00098 NM 2002 5 20 2002UALA00848 1 20020508 A 7932 WARNING SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT ACTIVATED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 104UA 26902 NR 1 ENGINE INFLIGHT SHUTDOWN. NR 1 ENG OIL QTY DROPPED TO 1 QUART. OIL PRESSURE AND TEMPERATURE NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002052000100 20020520 00100 SO 2002 5 20 C2XA02IA103 1 20020510 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO A/C BAY FROZEN A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 27 12922 145338 IAH- FLIGHT 3724, DURING LANDING THE CREW NOTED THAT SMOKE IN THE CABIN DURING LANDING AND TAXI. MAINTENANCE REMOVED A ND REPLACED THE NR 2 ACM, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002052000101 20020520 00101 SO 2002 5 20 C2XA02IA106 1 20020512 A 2611 SMOKE WARNING EMB 145 EMB145LR 3260212 SO COCKPIT FALSE ACTIVATION A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 14977 145175 EWR- DURING FLIGHT 3440, THE CREW NOTED THAT A ERRONEOUS LAV SMOKE WARNING ILLUMINATED. THE CREW VERIFIED THAT THERE W AS NO SMOKE OR FIRE. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LAV SMOKE DETECTION SYSTEM, NO DEFECTS NOTED. TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002052000102 20020520 00102 SO 2002 5 20 C2XA02IA107 1 20020513 A 2611 FAU751A4 PANEL EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 14977 145175 IAH- FLIGHT 3969, EN ROUTE THE CREW NOTED THAT THE LAV SMOKE WARNING ILLUMINATED. NO INDICATION OF SMOKE OR FIRE FOUND , PULLED CB'S AS SPECIFIED IN QHR. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR PANEL, PERFORMED A OPERATIONAL C HECK OF THE SYSTEM AND NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002052000103 20020520 00103 SO 2002 5 20 C2XA02IA109 1 20020514 A 2611 CONNECTOR EMB 145 EMB145LR 3260212 SO LAVATORY DIRTY A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 14977 145175 ICT- FLIGHT 3796, THE CREW NOTED THAT THE LAV SMOKE DETECTOR LIGHT CAME ON INFLIGHT. MAINTENANCE CLEANED CONNECTORS P8 201 AND P8100, PERFORMED A OPERATIONAL CHECK OF THE LAV SMOKE DETECTION SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002052000104 20020520 00104 SO 2002 5 20 C2XA02IA110 1 20020515 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY DIRTY A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 14977 145175 CLE- FLIGHT 3040, THE CREW NOTED THAT THE LAV SMOKE INDICATION ILLUMINATED THROUGH APPROXIMATELY 18,000 ON CLIMBOUT FRO M BNA. PERFORMED A VISUAL INSPECTION OF LAV AND A VISUAL INSPECTION OF THE LAV EXTINGUISHER. NOTHING ABNORMAL FOUND. WARNING CEASED AFTER TESTING FROM F/A GALLEY. PULLED CB E11 & E12 PER QRH. CLEANED DUST FROM SMOKE SCREEN, PERFORMED A OPERATIONAL CHECK OF THE LAV SMOKE DETECTION SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4T RT T00011AT 2002052000105 20020520 00105 SO 2002 5 20 C2XA02IA111 1 20020515 A 2611 FAU751A4 PANEL EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 14977 145175 BOS- THE CREW NOTED THAT THE LAV SMOKE DETECTOR WAS INOP. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR PANEL, P ERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002052000106 20020520 00106 WP 2002 5 20 CALA2000285 1 20020514 A 5320 39361901 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 FWD SERVICE DOOR AFT GIRT LATCH SUPPORT AT STA 190, S18R, IS CORRODED. INSTALLED NEW SUPPORT IAW SRM 51-30-00. 2 L 7 2 4F A6WE 2002052000107 20020520 00107 WP 2002 5 20 CALA2000286 1 20020514 A 5320 39361902 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 FWD SERVICE DOOR FWD GIRT LATCH SUPPORT AT STA 160 S18R, IS CORRODED. INSTALLED NEW SUPPORT IAW SRM 51-30-00. 2 L 7 2 4F A6WE 2002052000108 20020520 00108 NM 2002 5 20 DHL2002708006 1 20020514 A 3040 WINDSHIELD WIPER BOEING 727 72725 1384006 NM WINDSHIELD OUT OF ADJUST A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 708DH 18275 CAPTAIN'S SIDE WINDSHIELD WIPER DOES NOT FUNCTION IN THE LOW POSITION THE WIPER DOES NOT HAVE ADEQUATE RANGE OF MOTION T O KEEP THE UPPER PORTION OF THE WINDSHIELD CLEAR. RECLOCKED AND TESTED CAPT'S WINDSHIELD WIPER IAW MM 30-42-01. OPS CH ECK NORMAL. 2 L 7 3 4F A3WE 2002052000109 20020520 00109 NM 2002 5 20 DHL2002726521 1 20020415 A 5310 DOOR FRAME BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 DURING C-CHECK, RT AND AFT EMERGENCY EXIT FUSELAGE CUTOUT LWR FWD CORNER INTERIOR EXFOLIATED CORROSION. REMOVED CORROSI ON ON RT AFT EMERGENCY EXIT LWR FWD CORNER IAW B-727 SRM 51-30-1. FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1. FAB RICATED AND INSTALLED DOUBLER IAW B-727 SRM 53-30-3. OPS CHECK GOOD IAW B-727 MM 21-30-0. 2 L 7 3 4F RT A3WE 2002052000111 20020520 00111 NM 2002 5 20 DHL2002727006 1 20020506 A 3350 BATTERY PACK BOEING 727 727228 1384083 NM CABIN OUT OF POSITION A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 727DH 20204 COCKPIT EMERGENCY EXIT LIGHT INOP. RERACKED BATTERY PACKED OPS CK GOOD MM 33-00. 2 L 7 3 4F RT A3WE 2002052000112 20020520 00112 NM 2002 5 20 DHL2002742002 1 20020507 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN OUT OF POSITION A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 742DH 21290 EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR WILL NOT ILLUMINATE. RERACKED EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR IAW B-M/M 33-50-101. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002052000113 20020520 00113 WP 2002 5 20 DHL2002804005 1 20020513 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 STA 310 10 INCHES BELOW DOOR HANDLE HAS .45 CRACK THOUGH SKIN A-PIT DOOR. INSTALLED MAJOR REPAIR A-PIT DOOR 10 INCHES B ELOW DOOR HANDLE PER BOEING MESSAGE DHL-CVG-02-00026H & DRAWING REF A DHLL020510/2 REF B FAX REPAIR SKETCH. 2 L 7 4 4F RT 4A25 2002052000114 20020520 00114 WP 2002 5 20 DHL2002804006 1 20020513 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 STA 310, 10 INCHES ABOVE A-PIT DOOR HANDLE HAS A .25 INCH CRACK THROUGH SKIN STA 1190, C-PIT DOOR 10 INCHES BELOW DOOR H ANDLE HAS A CRACK. INSTALLED MAJOR REPAIR A-PIT DOOR 10 INCHES ABOVE HANDLE PER BOEING MESSAGE DHL-CVG-02-00026H & DRAW ING. REF A/DHLL020510/2 REF B/ FAX REPAIR SKETCH. A .20 INCH LONG THROUGH SKIN STA 1190 C-PIT DOOR 10 INCHES ABOVE HAN DLE THERE ARE 3 EA 1/8 INCH RIVETS WORKING THROUGH SKIN. INSTALLED MAJOR REPAIR C-PIT DOOR 10 INCHES BELOW HANDLE PER B OEING MESSAGE DHL-CVG-02-0026H & DRAWING. REF A/DHLL020510/2 REF B/ FAX REPAIR SKETCH. 2 L 7 4 4F RT 4A25 2002052000117 20020520 00117 WP 2002 5 20 DHL2002807564 1 20020404 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 RT WING L/E LOWER SKIN CRACKED 5/16 AT XW 485.000. PERFORMED MAJOR REPAIR. STOP DRILLED CRACKED SKIN. FABRICATED AND INSTALLED DOUBLER PER EO DHL 020315, EO 2855, EO SEMAN 2002236. 2 L 7 4 4F RT 4A25 2002052000118 20020520 00118 WP 2002 5 20 DHL2002807565 1 20020404 A 5210 FILLER DOUG DC8 DC873F 302199F WP PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AFT PAX DOOR LWR FWD CORNER- FILLER CRACKED (UNDER DOUBLER) AT STA 1620.0. PERFORMED MAJOR REPAIR. REMOVED EXISTING DO UBLER AND TRIPLER. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER PER DHL-LIM 02-000044. 2 L 7 4 4F RT 4A25 2002052000119 20020520 00119 NM 2002 5 20 DL76G020410 1 20020405 A 5247 ACCESS DOOR BOEING 767 767332 1382001 NM APU MISSING A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 27 1608 30573 AFTER LEVEL LOUD BANG HEARD BY FLIGHT CREW FOLLOWED BY AIRFRAME VIBES. FLIGHT RETURNED TO ATL WHERE MTC FOUND BOTH APU ACCESS DOORS MISSING. ITEM UNDER INVESTIGATION. 2 L 7 2 4F RT A1NM 2002052000120 20020520 00120 NM 2002 5 20 DL76G020475 1 20020418 A 2120 ODOR BOEING 767 7673P6 1385105 NM CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 1501P 24983 DUE TO MISTY HYDRAULIC SMELL IN CABIN, AIRCRAFT RETURNED TO ATL. INT'L MTC RAN ENGINES TO POWER WITH PACKS ON AND OFF A ND WAS UNABLE TO DUPLICATE. A/C WAS RETURNED TO SERVICE WITH NO FURTHER PROBLEMS. 2 L 7 2 4F RT A1NM 2002052000121 20020520 00121 NE 2002 5 20 DL76G020484 2 20020426 A 7320 8901314 SENSOR BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 2 ENGINE MALFUNCTIONED A DALA K NONE O OTHER AP APPROACH 1 SO 27 156DL 25354 695690 RIGHT ENGINE SLOW TO SPOOL DOWN FROM CRUISE POWER TO IDLE SETTING. TOOK ABOUT 20-30 SECS FOR ENGINE TO SPOOL DOWN. EME RGENCY EQUIPMENT CALLED OUT, BUT NO EMERGENCY DECLARED. NR 2 ENG CIT SENSOR REMOVED. REPLACED NR 2 ENGINE CIT SENS PER M/M. LEAK CKS OK, PERFORMED TEST 2 AND 3 PER PFHB TESTS. 2 L 7 2 4F 4 F RT A1NM E13NE 2002052000122 20020520 00122 NM 2002 5 20 DL76G020490 1 20020429 A 2750 285T004953 FSEU BOEING 767 7673P6 1385105 NM E/E BAY MALFUNCTIONED A DALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 1501P 24983 T/E FLAP DISAGREE LIGHT WHEN FLAPS 25 SELECTED, EICAS MSG ALSO. FLAPS DID NOT MOVE TO 25 DEGS POSITION. USED ALT FLAP PROC. INSPECTED FLAP, NO DISCREPANCIES NOTED. FSEU BITE SHOWED M603 FLAP LEVER RVDT. REPLACED FSEU PER AMM. OPS CHEC KED NORMAL. NO HISTORY. 2 L 7 2 4F RT A1NM 2002052000123 20020520 00123 NM 2002 5 20 DL777020437 1 20020413 A 3320 SOCKET BOEING 777 777232 1385232 NM CREW REST BURNED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 861DA 29952 FLUORESCENT LIGHT ABOVE FLT ATT CREW REST BUNK NR 6 INTERMITTENT OPERATION HOT PLASTIC ODOR AND SCORCHED SPOT AT AFT END OF BUNK. FOUND FLUORESCENT BULB SOCKET BURNT. FWD TO MCO AND PLAC PER MEL 33-21-01. LIGHT DEACTIVATED, CAPPED AND ST OWED CANNON PLUG FOR BALLAST. 2 L 7 2 4F RT T00001SE 2002052000124 20020520 00124 NM 2002 5 20 DLM11020479 1 20020424 A 3350 5519881 BATTERY DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 806DE 48477 ON PREFLIGHT, EMERGENCY LIGHT TEST FAIL. EMERGENCY LIGHT BATTERY 6 LO MSG ON. REPLACED EMERGENCY LIGHT BATTERY 6 PER M /M. EMERGENCY LIGHT TEST PASS. 2 L 7 3 4F RT A22WE 2002052000125 20020520 00125 EU 2002 5 20 02138309 1 20020518 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 309UE 41022 During preflight inspection, the crew reported that the forward section of the emergency floor track lighting was inoper ative. Maintenance personnel secured a connector for the forward section of floor track lights. An operational check w as satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002052000126 20020520 00126 NE 2002 5 20 2002F00505 2 20020512 A 7200 ENGINE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RIGHT SURGES G AMTA K NONE R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 11 553TZ 32587 31808 FLIGHT NUMBER 926, ON DESCENT IN V NAV, AUTO THROTTLES ON, THE RIGHT ENGINE SURGES BETWEEN 1.43 TO 1.33 EPR. ALL OTHER ENGINE PARAMETERS SURGE AS WELL. MAINTENANCE PERFORMED TEST 3 IP/HP AIRFLOW TEST IN ACCORDANCE WITH MM 71-00-00, PAGE 5 21. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A2NM E12EU 2002052100047 20020521 00047 EU 2002 5 21 02139324 1 20020519 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 324UE 41017 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTS WAS INOPERATIVE. MAINTENANCE PERSONNEL SECURED A LOOSE CONNECTOR FOR THE FORWARD SECTION OF LIGHTS. AN OPERATIONAL CHECK WAS SATISFACT ORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002052000127 20020520 00127 EU 2002 5 20 02139328 1 20020519 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 328UE 41083 During preflight inspection, the crew reported that the forward section of emergency floor track lights was inoperative. Maintenance personnel secured the connector for the forward section of lights. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002052000128 20020520 00128 WP 2002 5 20 ARWA20020504 1 20020510 A 2730 179894 ACTUATOR DOUG DC8 DC862 3021970 WP COCKPIT FAILED A ARWA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 19 8968U 46069 AFTER TAKEOFF PTC BECAME INOP. DURING CLIMB FLAP POSITION INDICATOR FAIL, HYD OIL TEMP LIGHT ON TEMP 69 DEGREES & CLIMB ING. AT 31.0 FL HEAVY SMOKE OUT OF PEDESTAL AFT OF THROTTLE QUADRANT. DURING DESCENT NR 2 & 4 MANIFOLD OVERTEMP LIGHT ON. FOUND PTC ACTUATOR VERY HOT & STRONG BURNT ODOR, ENTERED ON DMI 16610. NO MORE SMOKE IN THE COCKPIT ACTUATOR DISCO NNECTED IN RETRACT POSITION. REMOVED AND REPLACED FLAP POSITION INDICATOR, OPS CHECK NORMAL. PERFORMED ENGINE RUN-UP & FOUND NR 2 EDP AT FAULT. REMOVED & REPLACED PUMP, OPS CK OK. REMOVED & REPLACED NR 2 ENGINE TEMP SENSOR, 2 AND NR 4 F AN AIR COOLING VALVE. REMOVED & REPLACED PTC ACTUATOR AND PTC COMPUTER, OPS CK FOUND NORM. DMI 16610 CLEARED. 2 L 7 4 4F 4A25 2002052000129 20020520 00129 WP 2002 5 20 DHL2002806011 1 20020504 A 5610 STRUCTURE DOUG DC8 DC873F 302199F WP COCKPIT BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 CAPT'S SLIDING WINDOW VERY DIFFICULT TO OPEN AND CLOSE. BROKEN TRIM ALONG BOTTOM OF WINDOW. FOUND INTERIOR TRIM INTERF ERING WITH WINDOW. SECURED INTERIOR TRIM IAW DC8 MM 20-20-0. BOTTOM WINDOW TRIM NOT BROKEN, TWO SEPARATE PIECES. 2 L 7 4 4F RT 4A25 2002052000130 20020520 00130 WP 2002 5 20 DHL2002807566 1 20020404 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AFT CARGO COMPT C-DOOR OUTER SKIN LOWER SECTION SHOWS 2 INTERIM REPAIRS ALSO 2 BREAKS FROM STA 1160 TO 1220. PERFORMED MAJOR REPAIR PER EO DHL 020316, EO 2856, EO SEMAN 2002238. TRIMMED OUT DAMAGED SKIN SEGMENT. FABRICATED AND INSTALLED NEW SKIN SEGMENT & DOUBLER SPLICE PER EO DHL 020316, EO 2856, EO SEMAN 2002238. 2 L 7 4 4F RT 4A25 2002052000131 20020520 00131 NM 2002 5 20 DL764020477 1 20020423 A 2424 766300D GCU BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE NR 1 ENGINE FAULTY A DALA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 835MH 29708 706205 LT GEN FAILED AND APU FAILED TO POWER BUS. RESET ALL GCUS HAD HARD FAULT 24-30102 RT GCU FAULT. REMOVED AND REPLACED R T G PER FIM. RAN ALL ENG GENS ALL GEN TOOK LOADS. OPS CHECKS OK. CHECKED IDG DELTA PS. CHECK OK. C/W EO 14-85612-3 REV A ME-O1. 2 L 7 2 4F 4 F RT A1NM E13NE 2002052000132 20020520 00132 NM 2002 5 20 DLM88020494 1 20020430 A 3350 FUSE DOUG MD88 MD88 3023688 NM CABIN BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 950DL 49881 EMERGENCY ESCAPE PATH LIGHTS INOP FROM 31DE AFT INCLUDING TAIL COMPARTMENT. 2 L 7 2 4F RT A6WE 2002052000133 20020520 00133 NM 2002 5 20 DLM88020495 1 20020501 A 4990 1945189004 OIL CAP DOUG MD88 MD88 3023688 NM APU LEAKING A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 958DL 10996 49977 AT T/O HAZE FORMED IN CABIN AND AFT SMOKE DETECTORS WENT OFF. ADJUSTED PACKS MANUALLY AND HAZE AND ODOR DISSIPATED. FO UND APU OIL CAP LEAKING CAUSING INLET CONTAMINATION. REPLACED OIL CAP, CLEANED APU INLET AND PERFORMED DUCT BURNOUT PRO CEDURE PER M/M. 2 L 7 2 4F RT A6WE 2002052000134 20020520 00134 NM 2002 5 20 F3LA200200136 1 20020508 A 2710 CONTROL CABLE BOEING 737 7373L9 1384470 NM AILERON BROKEN A F3LA K NONE F FLT CONT AFFECTED AP APPROACH 1 NM 03 313FL 1680 26442 FLIGHT CREW REPORTED SIGNIFICANT RT ROLL TENDENCY ON FINAL APPROACH AND LANDING. CORRECTED ON TOUCHDOWN. FOUND AILERON BUS CABLE BROKEN. REMOVED RT AILERON CABLE ABSB-4 AND FABRICATED, INSTALLED, ADJUSTED AND TESTED REPLACEMENT CABLE PER MM 27-11-0, 27-09-14 AND 20-10-91 AND SYSTEM CHECKED OKAY. 2 L 7 2 4F RT A16WE 2002052000135 20020520 00135 WP 2002 5 20 FE5F200200002 1 20020318 A 1430 H205 NUT DOUG DC9 DC983 3022083 WP ELEVATOR LOOSE Z FE5F K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 WP 03 49952 DURING THE 30,000 FH CHECK, THE ELEVATOR ATTACH FITTINGS FOUND BOTH THE LT AND RT OUTBOARD SUBJECT FASTENERS LOOSE. BOT H LT AND RT NUT CAN BE TURNED EASILY. THE LAST SCHEDULED INSPECTION OF THIS AREA WAS AT 15,000 FH. OPERATOR HAS PERFOR M ONE TIME INSPECTION OF REST MD80S FLEET AND NO FAULT FOUND. PER BOEING, NO OTHER OPERATORS HAVE REPORT THIS PROBLEM. 2 L 7 2 4F RT A6WE 2002061900095 20020619 00095 CE 2002 6 19 GLBA2002056 1 20020502 A 2150 A/C PACK BEECH 1900 1900D 1154162 CE A/C BAY MALFUNCTIONED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 226GL UE226 LEFT ENVIRONMENTAL FAILURE ON T/O. ENVIRONMENTAL SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2002061900096 20020619 00096 CE 2002 6 19 GLBA2002057 1 20020506 A 2130 1143800595 SHUTOFF VALVE BEECH 1900 1900D 1154162 CE A/C BAY FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 184UX 988 UE184 DUAL ENVIRONMENTAL FAILURE ON CLIMBOUT. REPLACED PRSOV VALVE. 2 L 7 2 4T RT A24CE 2002052000138 20020520 00138 SO 2002 5 20 GLBA2002058 1 20020504 A 3350 SOCKET EMB 120 EMB120ER 3260203 SO CABIN DEFECTIVE A GLBA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 03 71GL 120071 RED EMERGENCY LIGHT INOP. REPLACED SOCKET. 2 L 7 2 4T RT A31SO 2002052000139 20020520 00139 SO 2002 5 20 LR7A02033 1 20020507 A 5320 37234920 CAP LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 554 4606 DURING SCHEDULED B3 INSPECTION, FOUND LT CHINE CAP CORRODED AT FS 516, LBL 60, WL 146. REPLACED CHINE CAP FS 245 TO FS 516 IAW SRM SMP 583 51-10. 2 H 7 4 4T A1SO 2002052000140 20020520 00140 NE 2002 5 20 MALA020263 2 20020430 A 7210 GEARBOX SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE FAILED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 422XJ 340B422 ON APPROACH OF FLIGHT 2753 RT ENGINE FLAMED OUT. EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. WEATHER CLEAR. THE ENGI NE DID NOT FLAME OUT BUT WAS OPERATING NORMALLY. A/C DID HAVE AN UNCOMMANDED AUTO COARSEN EVENT. THE DATA INDICATES IT WAS NOT CAUSED BY THE AUTO COARSEN, BUT WAS MECHANICAL. MAINTENANCE REPLACE PGB, RECOMMENDATION FOR PRECAUTION. REPLA CE OSG, REPLACE PCU, AND PROPELLERS FOR LIMITS PER DOWTY. 2 L 7 2 4T 4 T RT A52EU E8NE 2002052000141 20020520 00141 EU 2002 5 20 MALA020264 1 20020429 A 3246 AHA1489 WHEEL BAC 146 AVRO146RJ85A 1500097 EU RT MLG DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 532XJ E2366 AFTER FLIGHT 3851, RIGHT O/B MAIN WHEEL ASSEMBLY MISSING A 14 INCH CHUNK. FOUND IN LEX BY SECURITY FORCES. MAINTENANCE INSTALLED SERVICEABLE LTEFT O/B WHEEL ASSEMBLY. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2002052000142 20020520 00142 WP 2002 5 20 MWEA020310 1 20020502 A 2120 ODOR DOUG DC9 DC981 3022081 WP CABIN DETECTED A MWEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 31 804ME 48030 BURNING ODOR CAME FROM CABIN FLOOR IN SEAT 19AB AREA. INSPECTED SEAT 19AB IMMEDIATELY AFTER LANDING AND NO SMELL WAS NO TED. INSPECTED THE FOLLOWING: BALLAST FOR LOWER SIDEWALL LIGHTING EMERGENCY BATTERY PACK IN CEILING PHONES, PSU PANELS AND O2 GENERATOR. RAN ENGINES AND PRESSURIZED AIRCRAFT WITH WARM PACKS. INSPECTED WHEEL WELL AREA AND CARGO COMPARTME NTS. ALL THE ITEMS INSPECTED WERE OK. THE ONLY SMELL NOTED WAS IN THE AFT CARGO COMPARTMENT BEFORE THE BAGS WERE REMOV ED AND THERE WAS A STRONG AMMONIA SMELL. ALSO INSPECTED THE RECIRCULATION FAN FOR OPERATION. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F A6WE 2002052000143 20020520 00143 WP 2002 5 20 MWEA020318 1 20020508 A 5310 591014211 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 FORWARD PIT, LOWER DOOR JAM WEB HAS SEVERAL SMALL DENTS AT STATION 418 AND 430. FABRICATED AND INSTALLED SECTION OF WEB AND DOUBLER. 2 L 7 2 4F A6WE 2002052000144 20020520 00144 WP 2002 5 20 MWEA020323 1 20020507 A 5350 59100913 RADOME DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 FOUND RADOME DAMAGE ON POST FLIGHT WALKAROUND. REMOVED AND REPLACED RADOME. 2 L 7 2 4F A6WE 2002052000145 20020520 00145 2002 5 20 MWEA020327 4 20020515 A 3418 9650449002 COMPUTER DOUG DC9 DC982 3022082 WP COCKPIT FAULTY A MWEA K NONE N FALSE WARNING CR CRUISE 1 GL 31 809ME 48071 STALL FAILURE LIGHT ILLUMINATED, LIGHT CAME ON AND OFF AFTER SELECTING FLAPS. REMAINED OUT FOR DURATION OF FLIGHT. REM OVED AND REPLACED NR 2 STALL COMPUTER SYSTEM, TEST GOOD. 2 L 7 2 4F A6WE 2002052000146 20020520 00146 WP 2002 5 20 MWEA020332 1 20020502 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP TAILCONE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 302ME 47102 EMERGENCY LIGHT BULBS INOP ABOVE TAIL CONE. REMOVED AND REPLACED BATTERIES IN BATTERY PACK. OPS CHECK OK. 2 L 7 2 4F A6WE 2002052000147 20020520 00147 NE 2002 5 20 NACA20020016 2 20020502 A 8500 R2800 ENGINE DOUG DC6 C118A 3021710 WP PWA R2800 R2800* 52026 NE NR 3 MALFUNCTIONED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 1377K 1702 1702 44596 P33192 NR 3 ENGINE BACKFIRES, FULL RICH AT ALL POWER SETTINGS. REPLACED THE NR 3 ENGINE. 2 L 7 4 4R 4 R 6A3 5E8 2002052000148 20020520 00148 2002 5 20 NACA20020017 4 20020502 A 6122 CONNECTOR DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE HAMSTD 43E 43E60 NE PROP GOVERNOR DEFECTIVE A NACA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 AL 03 99330 43576 P33821 N225013 NR 2 PROPELLER UNCONTROLLABLE, WILL NOT TOGGLE. REPLACED CANNON PLUG AND BREEZE FROM THE NR 2 PROP GOV STEP HEAD MOTOR TO NOSE CASE J-BOX. 2 L 7 4 4R 4 R 6A3 5E8 6 C P871 2002052000149 20020520 00149 NE 2002 5 20 NACA20020018 2 20020507 A 8530 356994 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 2 ENGINE LEAKING A NACA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CL CLIMB 1 AL 03 2907F 1868 1868 533265 NK510771 FEATHERED THE NR 2 ENGINE DUE TO OIL LOSS. REPLACED AND RESEALED NR 1 EXHAUST PUSH ROD HOUSING. RESEALED AND RETORQUED NR 1 EXHAUST SIDE BAFFLE STUD. REPLACED ROCKER ARM THRUST WASHER. BORESCOPED NR 1 COMPRESSION CHAMBER OF HEAD FOR PRE CAUTIONARY PURPOSES, NO DEFECTS NOTED. 2 L 7 4 4R 4 R A781 5E8 2002052000150 20020520 00150 WP 2002 5 20 P2EA2002M033 1 20020509 A 2760 WARNING SYSTEM DOUG DC9 DC982 3022082 WP COCKPIT ACTIVATED A P2EA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 05 141NJ 49932 ON TAKEOFF ROLL, SPOILER DEPLOYED ANNUNCIATOR ILLUMINATED. ABORTED TAKEOFF AND RETURNED TO GATE WITH NO INCIDENT. PERF ORMED OPERATIONAL TEST, NO DEFECTS NOTED. 2 L 7 2 4F A6WE 2002052000151 20020520 00151 WP 2002 5 20 P2EA2002M034 1 20020509 A 2760 SENSOR DOUG DC9 DC982 3022082 WP SPOILER DIRTY A P2EA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 05 141NJ 49932 ON TAKEOFF ROLL, SPOILER DEPLOYED ANNUNCIATOR ILLUMINATED. ABORTED TAKEOFF AND RETURNED TO GATE. CLEANED D1-48 AND B1- 45 SENSORS AND PERFORMED BITE CHECK OF PSEU IAW MM 37-60-00. 2 L 7 2 4F A6WE 2002052000152 20020520 00152 WP 2002 5 20 P2EA2002M035 1 20020511 A 2740 SWITCH DOUG DC9 DC982 3022082 WP HORIZ STAB OUT OF ADJUST A P2EA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 05 141NJ 49932 ON TAKEOFF ROLL, THE TAKEOFF CONFIGURATION HORN SOUNDED. ABORTED TAKEOFF AND RETURNED TO GATE WITH NO INCIDENT. ADJUST ED HORIZONTAL STABILIZER TAKEOFF WARNING SWITCH IAW MM 27-40-00. 2 L 7 2 4F A6WE 2002052000153 20020520 00153 WP 2002 5 20 P2EA2002M34 1 20020509 A 2760 SENSOR DOUG DC9 DC982 3022082 WP SPOILER DIRTY A P2EA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 05 141NJ 49932 ON TAKEOFF ROLL, SPOILER DEPLOYED ANNUNCIATOR ILLUMINATED. ABORTED TAKEOFF AND RETURNED TO GATE. CLEANED D1-48 AND B1- 45 SENSORS AND PERFORMED BITE CHECK OF PSEU IAW MM 37-60-00. 2 L 7 2 4F A6WE 2002052000154 20020520 00154 NM 2002 5 20 PCAA0204052 1 20020501 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT, EVERY OTHER LIGHT FOR EMERGENCY FLOOR LIGHTING ON RIGHT SIDE WAS FOUND TO BE INOPERATI VE. LEFT REAR LIGHTING ALSO INOPERATIVE. LEFT REAR CONNECTOR FOR EMERGENCY PATH LIGHTING REPAIRED. FUSES 6 AND 7 IN R EAR BATTERY PACK REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002052000155 20020520 00155 NM 2002 5 20 PCAA0205055 1 20020509 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM EXTERIOR INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 831EX 160 DURING ROUTINE MAINTENANCE VISIT RIGHT FORWARD AND LEFT AFT EXTERIOR EMERGENCY EXIT LIGHTS FOUND TO BE INOPERATIVE. RIG HT FORWARD LIGHT BULB, LENS AND SOCKET WERE REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002052000156 20020520 00156 EU 2002 5 20 QXEA0200734 1 20020501 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 498US 11181 SEA- MID CABIN EMERGENCY EXIT SIGNS INOPERATIVE. REMOVED AND REPLACED CABIN EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002052000157 20020520 00157 NM 2002 5 20 QXEA0200737 1 20020506 A 3620 1173T076204 SWITCH BOMBDR DHC8 DHC8401 NM BLEED AIR MALFUNCTIONED A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 409QX 4051 SEA-EN ROUTE FROM SEA TO BOI, NR 2 BLEED AIR HOT LIGHT ILLUMINATED. FOLLOWED CHECKLIST, LIGHT EXTINGUISHED. RETURNED T O BOI. REMOVED AND REPLACED NR 2 BLEED OVERTEMP SWITCH. OPERATIONAL CHECK GOOD. NO CAUTION LIGHT NOTED. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002052000158 20020520 00158 EA 2002 5 20 QXEA0200738 1 20020506 A 5610 601R330339 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 607QX 1502 10024 BOI- EN ROUTE FROM BOI TO SAN, CAPTAIN'S WINDSHIELD SHATTERED. RETURNED TO BOI. REMOVED AND REPLACED CAPTAIN'S WINDSHI ELD. GROUND CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002052000159 20020520 00159 NM 2002 5 20 QXEA0200739 1 20020507 A 3230 HANDLE DHAV DHC8 DHC8202 2809007 NM LANDING GEAR OUT OF POSITION A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 358PH 506 PDX-EN ROUTE FROM PDX TO SEA, LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. RETURNED TO PDX. FOUND LANDING GEAR HYDRAU LIC BYPASS HANDLE NOT FULLY STOWED. STOWED HANDLE AND RETRACTED AND EXTENDED LANDING GEAR FIVE TIMES. NO DEFECTS NOTED . NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002052900004 20020529 00004 NM 2002 5 29 02052001 1 20020519 A 3510 DOOR BOEING 757 75728A 1384976 NM CABIN OUT OF ADJUST A N8TA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 19 543NA 28161 ON TAXI-OUT, FLIGHT ATTENDANT EMERGENCY OXYGEN MASKS DEPLOYED WITHOUT COMMAND. OXYGEN GENERATOR(S) WAS/WERE NOT ACTIVAT ED. INSPECTION REVEALED OXYGEN MASK DOOR SPRING WEAK. OXYGEN MASKS WERE REPACKED AS PER M/M 35-21-01. DOOR WAS TEMPOR ARILY SECURED WITH TAPE. L-4 FLIGHT ATTENDANT SEATING PLACED ON MEL. DOOR ADJUSTED AND DROP CHECKED AS PER M/M 35-21-0 0. 2 L 7 2 4F RT A2NM 2002060400298 20020604 00298 WP 2002 6 4 DHL2002807006 1 20020517 A 2697 GROUND WIRE DOUG DC8 DC873F 302199F WP FIRE LOOP DAMAGED A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 807DH 45990 NR 2 B-LOOP SHORT LIGHT ON. FOUND AND FIXED STRIKING SOCKET AND GROUND WIRE AT ENGINE NR 2 LOOP-B. OPS CHECK GOOD IAW MM 26-10-4. 2 L 7 4 4F RT 4A25 2002052000160 20020520 00160 EA 2002 5 20 COMA0260313 1 20020514 A 3610 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 916CA 7014 FLIGHT 5280 LEFT ENGINE 14TH STAGE BLEED AIR LEAK WARNING.COULD NOT DUPLICATE. RESET SYSTEM, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2002052000161 20020520 00161 2002 5 20 SWAA021062 4 20020516 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052000162 20020520 00162 2002 5 20 SWAA021063 4 20020514 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR STRAP FRAYED. REPAIRED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052000163 20020520 00163 NM 2002 5 20 SWAA021064 1 20020511 A 3350 07912 COVER BOEING 737 7373Y0 1384671 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS COVERS CRACKED AT FWD END. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002052000164 20020520 00164 2002 5 20 SWAA021065 4 20020515 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052000165 20020520 00165 NM 2002 5 20 SWAA021066 1 20020514 A 3350 311500 LENS BOEING 737 7373Y0 1384671 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 OVERHEAD BIN BULL NOSE EMERGENCY LIGHT LENS LOOSE AT ROW NR 23 DEF. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002052000166 20020520 00166 NM 2002 5 20 SWAA021068 1 20020516 A 5330 6547955533 BEAR STRAP BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/4D CHECK, FOUND LOWER CARGO DOOR BEAR STRAP CORRODED AT BS 794.30, STR 26R TO 27R. REPAIRED BEAR STR AP PER SWA RA. 2 L 7 2 4F RT A16WE 2002052000167 20020520 00167 NM 2002 5 20 SWAA021070 1 20020509 A 5311 6546546 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAMES CORRODED (2 EA) BETWEEN STR'S 27L AND 27R, BS'S 807 AND 827. REPAIRE D FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2002052000168 20020520 00168 NM 2002 5 20 SWAA021071 1 20020515 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.. 2 L 7 2 4F RT A16WE 2002052000169 20020520 00169 NM 2002 5 20 SWAA021072 1 20020514 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207 AND LBL 28. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002052000170 20020520 00170 NM 2002 5 20 SWAA021073 1 20020515 A 5751 6546455 AILERON BOEING 737 7372T4 1384492 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED SPECIAL VISIT, FOUND RT AILERON DELAMINATED ON LOWER SURFACE OTBD OF TAB. REMOVED AND REPLACED AILERON PER MM. 2 L 7 2 4F A16WE 2002052000171 20020520 00171 NM 2002 5 20 SWAA021074 1 20020515 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKS (5 EA) AT BS 500A AT STR 10R, BS 500D AT STR 15R, BS 737 AT STR 18 R, BS 757 AT STR 10R AND BS 937 AT STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002052000172 20020520 00172 NM 2002 5 20 SWAA021075 1 20020515 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) BETWEEN STR'S 8L AND 9L AT BS'S 907, BS 380 AND BS 400.. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2002052000173 20020520 00173 NM 2002 5 20 SWAA021076 1 20020515 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) BETWEEN STR'S 8R AND 9R, AT BS 400, BS 440 AND BS 867. R EPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2002052000174 20020520 00174 NM 2002 5 20 SWAA021056 1 20020513 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 25R, BETWEEN BS 932 AND 943. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 2002052000175 20020520 00175 NM 2002 5 20 SWAA021059 1 20020513 A 5315 BAC1509 FLOORBEAM BOEING 737 7375H4 138449D NM AFT CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 747, RBL 14. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002052000176 20020520 00176 NM 2002 5 20 SWAA021060 1 20020513 A 5315 BAC1509 FLOORBEAM BOEING 737 7375H4 138449D NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 754, RBL 3. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002052000177 20020520 00177 NM 2002 5 20 SWAA021046 1 20020514 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 092SW 22964 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 892, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002052000178 20020520 00178 NM 2002 5 20 SWAA021048 1 20020514 A 5313 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR'S 14R AND 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002052000179 20020520 00179 NM 2002 5 20 SWAA021049 1 20020513 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 717SA 27851 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED AT ROW'S 12 AND 21. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002052000180 20020520 00180 NM 2002 5 20 SWAA021053 1 20020513 A 5315 BAC1509 FLOORBEAM BOEING 737 7375H4 138449D NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS CORRODED AT BS 770, BETWEEN LBL 12 TO RBL 8. REPAIRED FLOORBEAMS PER SWA RA. 2 L 7 2 4F RT A16WE 2002052000181 20020520 00181 NM 2002 5 20 SWAA021054 1 20020512 A 2731 BACBS8AM07 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 3 AND NR 4 RT ELEVATOR TAB HINGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002052000182 20020520 00182 NM 2002 5 20 SWAA021055 1 20020513 A 2731 BACB28AM07 BUSHING BOEING 737 7373H4 1384600 NM ELEVATORS WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED A2 CHECK, SWA SI 11111-55, LT AND RT ELEVATOR TAB LOCK OUT MECHANISMS HAVE EXCESSIVE PLAY AT FWD ATTACH POINTS. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR LOCK OUT MECHANISM LINK BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002060500040 20020605 00040 WP 2002 6 5 DHL2002807007 1 20020518 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 2 ENGINE FAILED A DHLA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 807DH 45990 NR 2 ENG B-LOOP SHORT CIRCUIT LIGHT ILLUMINATED. CHECKED LOOPS WITH A MEGER. FOUND LT & RT B-CORE DETECTOR LOOPS WITH LOW ISOLATION. REPLACED BOTH SIDES OF CORE DET LOOP AND TESTED SYSTEM PER M/M 26-10-1, ALL CKS GOOD. 2 L 7 4 4F RT 4A25 2002052000183 20020520 00183 NM 2002 5 20 UPS02238287 1 20020506 A 7830 BRACKET BOEING 727 72722C 138400F NM #3 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C #3 ENG. TR PRIMARY ACTUATOR FAIRING MID ATTACH BRACKET CRACKED REPLACED BRACKET IAW SRM 51-30-02 & MM 20-80-01 2 L 7 3 4F A3WE 2002052000184 20020520 00184 NM 2002 5 20 UPS02238288 1 20020506 A 7830 BRACKET BOEING 727 72722C 138400F NM #1 ENG. CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C #1 ENG. TR PRIMARY ACTUATOR FAIRING MID. ATTACH BRACKET CRACKED REPLACED BRACKET IAW SRM 51-30-02 & MM 20-80-01 2 L 7 3 4F A3WE 2002052000185 20020520 00185 NM 2002 5 20 UPS02238289 1 20020507 A 2730 BRACKET BOEING 727 72722C 138400F NM L/H ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C L/H ELEV. POSITION SENSOR LINKAGE ATTACHED TO FRONT SPAR OF ELEVATOR CRACKED. BRACKET OF POSITION SENSOR LINKAGE ATTACHED TO FRONT SPAR OF L/H ELE VATOR REPLACED IAW MM 20-80-01 2 L 7 3 4F A3WE 2002052000186 20020520 00186 NM 2002 5 20 UPS02238304 1 20020504 A 5510 BEAM BOEING 727 72722C 138400F NM STA. 115 TO 145 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C CORROSION ON RH STAB TE UPPER BEAM AT STAB STA. 115 TO 145 CORROSION REMOVED IAW SRM 51-10-06 FOUN D TO BE OUTSIDE LIMITS HFEC C/O IAW B727 NDTM PT 6 51-00-00 - NDF BEAM REPAIRED IAW SMRO EO 2002-027-003 UPS ENGINEERING FILE NO. 727-53-20053 2 L 7 3 4F A3WE 2002052000187 20020520 00187 NM 2002 5 20 UPS02238306 1 20020509 A 2750 FLAP TRACK BOEING 727 72722C 138400F NM RH WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C RH WING #8 FLAP TRACK SAILBOAT FAIRING, O/B ROLLER GUIDE TRACK IS CR ACKED #8 FLAP TRACK FAIRING T RACK GUIDE REPLACED IAW SRM 51-30-02 2 L 7 3 4F A3WE 2002052000188 20020520 00188 NM 2002 5 20 UPS02238313 1 20020507 A 2710 HINGE FITTING BOEING 727 72722C 138400F NM R/H O/B AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C R/H O/B AILERON, 2ND HINGE FITTING FROM O/B HAS 2 SUSPECT CRACKS EMA NATING FROM BOTH UPPER FITTING FA STNER HOLES REPLACED R/H O/B AILERON FITTING IAW DRAWING 65-19259 2 L 7 3 4F A3WE 2002052000189 20020520 00189 NM 2002 5 20 UPS02238317 1 20020510 A 5310 INTERCOSTAL BOEING 727 72722C 138400F NM BS 294.5 - 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C CORROAION ON INTERCOSTAL FROM BS 294.5 - BS 312 AT LBBL 40 APPROX INTERCOSTAL REPAIRED IAW SRM 51- 40-3 2 L 7 3 4F A3WE 2002052000190 20020520 00190 NM 2002 5 20 UPS02238319 1 20020508 A 5700 SKIN BOEING 727 72722C 138400F NM RH WING LE SKIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C SUSPECT CRACK ON RH WING LE SKIN AT CUT OUT FOR NO 6 LE SLAT O/B SLA T HOOK REPAIR CARRIED OUT IAW 57-30-4 SRM 2 L 7 3 4F A3WE 2002052000191 20020520 00191 NM 2002 5 20 UPS02238321 1 20020502 A 5330 LAP JOINT BOEING 727 72722C 138400F NM BS 650 S19R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C SUSPECT CORROSION AT LAP JOINT STR. 19R BS 650 REPAIR CARRIED OUT IAW SMRO EO 2002-027-002 UPS ENG INEERING FILE NO. 727-53-20053 2 L 7 3 4F A3WE 2002052000192 20020520 00192 NM 2002 5 20 UPS02538322 1 20020519 A 2611 2156606A SMOKE DETECTOR BOEING 757 75724APF 1384969 NM MAIN DECK 2B INOPERATIVE A IPXA O OTHER P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 452UP 25473 INSPECTION TYPE:N/A SMOKE DETECTOR 2B IS FAILING TEST IN MAIN CARGO AREA. REMOVED AND INSTALLED SMOKE DETECTOR. MM REF 26-16-01 OPS/CK GOOD. 2 L 7 2 4F RT A2NM 2002052000193 20020520 00193 EU 2002 5 20 MALA020278 1 20020412 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 514XJ E2330 DURING C-CHECK IN CVG, NR 3 SEAT RAIL CORRODED BEYOND ALLOWABLE SRM LIMITS. MAINTENANCE REPAIRED DAMAGE BY REPLACING DA MAGED SECTION PER SRM 53-00-32, PAGE BLOCK 201 AND EO A53026. 2 H 7 4 4F RT A49EU 2002052000194 20020520 00194 WP 2002 5 20 ABXA010884 1 20020423 A 5700 991932629 CLIP DOUG DC9 DC932 3022066 WP LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 LEADING EDGE SPLICE ANGLE CRACKED JUST OUTBOARD OF #6 SLAT TRACK CUT-OUT. REPLACED SPLICE IAW DC-9 SRM 51-30-2 AND 51-30 -5. 2 L 7 2 4F A6WE 2002052000195 20020520 00195 SO 2002 5 20 C2XA02TY094 1 20020520 A 5330 1202265605 SKIN EMB 145 EMB145LR 3260212 SO NOSE PUNCTURED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 16951 145063 TYS, Aircraft ferried in for skin damage on the right side between frames 1A and 2, stringers 14R and 15R. Maintenance r emoved and replaced the damaged skin and stringer 15R. I/A/W-EMB-135/145-SRM-51-40-02 and 51-21-04, 05 & 06. The repair procedure was satisfactory. 2 L 7 2 4T RT T00011AT 2002052000196 20020520 00196 WP 2002 5 20 ZW0A0205201 1 20020518 A 3350 8039001 POWER SUPPLY DOUG DC9 DC983 3022083 WP WORN A ZW0A K NONE O OTHER UK UNKNOWN 1 CE 13 970TW 53620 DURING OVERNIGHT MAINTENANCE, OPERATION CHECK OF EGRESS LIGHTING FAILED. REPAIRED BY REPLACING EMERGENCY LIGHT POWER SUP PLY (TWA PN 93-0267), OPS-CK ASSURED NORMAL PERFORMANCE. LAST-CC / STL 7/6/01 2 L 7 2 4F RT A6WE 2002052000197 20020520 00197 2002 5 20 RAIA00205155 4 20020516 A 3420 HG2010AC02 COMPUTER EMB 145 EMB145 3260210 SO OVERHEATED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 803HK 6322 6322 145077 5285-PIT- OVERHEAT INDICATION #2 AHRS. MAINTENANCE REMOVED AND REPLACED #2 AHRS COMPUTER. 2 L 7 2 4F RT T00011AT 2002052000198 20020520 00198 EU 2002 5 20 RAIA00205156 1 20020519 A 2435 23095002 STARTER GEN JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 558HK 8582 214 41071 5587-STL- LEFT GENERATOR FAIL LIGHT ILLUMINATED DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE STARTER/GENERATOR. 2 L 7 2 4T RT A41NM 2002052000199 20020520 00199 EU 2002 5 20 AWXA200200432 1 20020517 A 3350 E0052R8B3APNE CONNECTOR AIRBUS 320 A320231 3930325 EU SEAT ROW 19 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 0 0 66 ATL - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE CANNON PLUG AT THE WALL PLUG IN, SEAT ROW 19 L/H, OPERATIONAL CHECK WAS GOOD IAW AMM 33-51-00-710-0 01. 2 L 7 2 4F RT A28NM 2002052000200 20020520 00200 NM 2002 5 20 S02479016 1 20020518 A 7900 PW40563 ENGINE PWA BOEING 747 747400 NM PWA 4056 PW4056 NE #4 ENG W SAJF E ENGINE SHUTDOWN O OTHER CR CRUISE 1 WP 03 727845 29031 B18208 #4 ENG OIL LOST IN FLIGHT CAUSE IFSD AND DIVERT TO ANC.C/A:1.GND CHK FOUND #4 BEARING OIL PRESSURE TUBE LOOSEN FR OM INSIDE OF THE TURBINE EXHAUST CASE 7 OCLOCK POSITION. 2.TPE SENT AOG TEAM AND SPARE ENGINE TO ANC FOR #4 ENG CHANGE. 3.ENGINE CHANGE HAD BEEN FINISHED ON 5/19 01:00 TPE TIME. 4.WAIT ENGINE SHIP BACK TO TPE. 2 L 7 4 4F 4 F RT A20WE E24NE 2002052100001 20020521 00001 SW 2002 5 21 R7M2002F00001 1 20020314 A 6510 407040302109 SHAFT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR OUT OF BALANCE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 200LN 53497 SHAFT ASSEMBLY, BEARING HANGAR- OUT OF BALANCE FROM FACTORY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002052100002 20020521 00002 SW 2002 5 21 R7M2002F00002 1 20020315 A 6510 407040302109 SHAFT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR OUT OF BALANCE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 200LN 48 53497 SHAFT ASSEMBLY BEARING HANGAR OUT OF BALANCE FROM FACTORY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002052100003 20020521 00003 2002 5 21 R7M2002F00003 4 20020329 A 3421 5040121910 INDICATOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 220CF 253 3411 HORIZON REFERENCE INDICATOR INOPERATIVE. DRIFTS 10 DEGREES. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002052100004 20020521 00004 2002 5 21 R7M2002F00004 4 20020403 A 3444 066030440001 INDICATOR SNIAS 350 AS350B2 8680813 EU RADAR ALTIMETER INOPERATIVE B R7MR O OTHER L NO TEST NR NOT REPORTED 1 NM 07 220CF 265 3411 KNI416 - RADAR ALTIMETER INDICATOR INOPERATIVE. NO DH WARNINGS. REPLACED WITH LOANER UNIT CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2002052100005 20020521 00005 2002 5 21 R7M2002F00005 4 20020306 A 2312 9910951 TRANSCEIVER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE VHF SYSTEM MALFUNCTIONED B R7MR O OTHER L NO TEST NR NOT REPORTED 1 NM 07 220CF 222 3411 UHF/VHF/LOW/HI BAND TRANSCEIVER UNIT INOPERATIVE. ON ANY FREQUENCY, THE TRANSMISSION FADES OUT AFTER 6.7 SECONDS. REPL ACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002052100006 20020521 00006 EU 2002 5 21 R7M2002F00006 1 20020118 A 2913 704A34310006 PUMP SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE HYDRAULIC SYS FAILED B R7MR O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 220CF 114 3411 HYDRAULIC PUMP UNIT INOPERATIVE. AIRCRAFT EXPERIENCED HYDRAULIC FAILURE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002052100007 20020521 00007 2002 5 21 R7M2002F00007 4 20020313 A 3120 B1894522282A CLOCK SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 220CF 225 3411 CLOCK INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002052100008 20020521 00008 EU 2002 5 21 R7M2002F00008 1 20020126 A 6730 BFS1551 REGULATOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR INOPERATIVE B R7MR O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 3593X 9763 9763 FILTER REGULATOR UNIT PRODUCING STIFF TAIL ROTOR PEDDLES. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002052100009 20020521 00009 EU 2002 5 21 R7M2002F00009 1 20020127 A 6730 161847 VALVE SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR INOPERATIVE B R7MR O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 3593X 9762 1081 ELECTRO VALVE ON RUN-UP FAILED, TAIL ROTOR PEDALS VERY STIFF. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002052100010 20020521 00010 NE 2002 5 21 R7M2002F00010 2 20020216 A 7321 70BMB01010 ECU SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE FUEL CONTROL FAILED B R7MR O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 396LG 40 3336 ELECTRONIC CONTROL UNIT HAS A FAULT CODE. 135 FLT AMG GOV/LEFT MODULE FADEC. FAIL 2 0200 HEX. REPLACED WITH USED UNI T CORRECTED PROBLEM. NO LOG CARD IN ENGINE LOG BOOK. (OUR UNIT=40 HOURS. REPLACEMENT UNIT=1240 HOURS. DIFFERENCE 1200 HOURS. PLEASE CREDIT THE DIFFERENCE.) 1 G 7 1 3U 3 U H9EU E19EU 2002052100011 20020521 00011 2002 5 21 R7M2002F00011 4 20020307 A 2312 9910951 TRANSCEIVER SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE VHF SYSTEM INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 396LG 66 3336 UHF/VHF/LOW/HI BAND TRANSCEIVER - UNIT INOPERATIVE. WILL NOT TRANSMIT ON 467.975 TONE 21 (136.5) WITH GENERATOR ON-LINE . REPLACED WITH LOANER UNIT PN 971083-1 CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002052100012 20020521 00012 NE 2002 5 21 R7M2002F00012 2 20020227 A 7532 9550158250 BLEED VALVE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE FAILED B R7MR O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 397LG 775 3268 BLEED VALVE INOPERATIVE. WILL NOT CLOSE. REPLACED WITH USED UNIT CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002052100013 20020521 00013 2002 5 21 R7M2002F00013 4 20020329 A 3457 0110028000 GPS BELL 407 407 1182206 SW ALLSN 250C 250C47B GL COCKPIT INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 407SJ 1160 53422 GPS 430 UNIT INOPERATIVE. UNIT WILL NOT VDR LOCK IN VOR FREQUENCIES, ILS OR VOR STATIONS. MESSAGE INDICATES CDI INOPE RATIVE WHEN SWITCHING TO VLOC MODE. ALSO, UNIT WILL NOT INDICATE GPS MODE ON THE SCREEN (LOWER LT CORNER). REPLACED WI TH LOANER UNIT CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002052100014 20020521 00014 SW 2002 5 21 R7M2002F00014 1 20020215 A 6240 407375003107 INDICATOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TORQUE INTERMITTENT B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 407SJ 1082 53422 TORQUE INDICATOR OPERATES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002052100017 20020521 00017 EU 2002 5 21 R7M2002F00017 1 20020323 A 2432 RG390E BATTERY BOLKMS 117 BK117A3 5626015 EU MAIN DISCHARGED B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 424MB 7620 7082 LEAD ACID BATTERY WILL NOT HOLD A CHARGE. STAYS AT 20 VOLTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2002052100019 20020521 00019 NE 2002 5 21 R7M2002F00019 2 20020130 A 7260 230093304 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ACCESSORY DRIVE WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 527RM 8324 7111 LE45132EA -ANNULAR BALL BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002052100020 20020521 00020 EU 2002 5 21 R7M2002F00020 1 20020130 A 8011 408109008 GEAR BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE STARTER WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 527RM 8324 7111 STARTER GEAR ASSEMBLY HAS EXCESSIVE SPLINE WEAR. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002052100021 20020521 00021 2002 5 21 R7M2002F00021 4 20020402 A 2211 7004206901 COMPUTER BOLKMS 117 BK117A4 5626017 EU CSAS INOPERATIVE B R7MR O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 586BH 6175 7129 CSAS-COMPUTER INOPERATIVE. CAUSES 1 TO 2 HRTZ PER SECOND ROLL WHILE ROLL MODE ENGAGED. REPLACED WITH NEW UNIT CORRECTE D PROBLEM. 1 G 7 2 3U H13EU 2002052100022 20020521 00022 2002 5 21 R7M2002F00022 4 20020328 A 2211 117884141 COMPUTER BOLKMS 117 BK117A4 5626017 EU CSAS MALFUNCTIONED B R7MR O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 586BH 6165 7129 YAW/CSAS COMPUTER INOPERATIVE. ONLY OPERATES IN STANDBY MODE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2002052100023 20020521 00023 EU 2002 5 21 R7M2002F00023 1 20020307 A 2432 RG390E BATTERY BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101600A 41560 NE MAIN DISCHARGED B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 625MB 6766 7108 LEAD ACID BATTERY HAS WEAK POWER OUTPUT. VOLTAGE DROPS TO 15-16 VOLTS DURING STARTS AND SHOWS A CONSTANT HIGH RATE OF C HARGE IN-FLIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002052100031 20020521 00031 EU 2002 5 21 R7M2002F00036 1 20020214 A 2432 RG3545 BATTERY SNIAS 350 AS350D1 8680804 EU ALLSN 250C 250C30 03013 GL MAIN DISCHARGED B R7MR O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 779LF 7550 1621 LEAD ACID BATTERY WOULD NOT HOLD CHARGE. UNIT SCRAPPED ON SITE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E1GL 2002052100032 20020521 00032 SW 2002 5 21 R7MR35009 1 20020128 A 2844 407375007105 INDICATOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUEL PRESSURE INOPERATIVE B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 107LN 290 53483 FUEL PRESSURE/AMMETER INDICATOR INOPERATIVE. FUEL PRESSURE PEGGED OUT ON HIGH SIDE OF SCALE. ALSO, INDICATOR FLUCTUATE S WHEN GENERATOR TURNED ON. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002052100033 20020521 00033 NE 2002 5 21 R7MR35041 2 20020411 A 7230 COMPRESSOR WHEEL SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE ENGINE DAMAGED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 103LN 1498 3128 22032 AXIAL COMPRESSOR (MO2), DAMAGE TO NR 1 TURBINE WHEEL DUE TO IGNITER CENTER ELECTRODE FAILURE (EJECTED THROUGH WHEEL). T HIS IGNITER (9550168770 INSTALLED 7/11/01) AND SL 2171/02/ARRIEL 1-66 INDICATES THAT THIS IGNITER WOULD PREVNET FUTURE FAILURES OF THIS TYPE FROM HAPPENING. THIS SL DOES NOT REFERENCE BACK TO ARRIEL 2B, BUT EQUIPMENT IS OF THE SAME TYPE. REPLACED WITH RENTAL UNIT CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2002052100034 20020521 00034 NE 2002 5 21 R7MR35042 2 20020411 A 7230 70BM032010 COMPRESSOR WHEEL SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE GAS GENERATOR DAMAGED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 103LN 1498 3128 22032 GAS GENERATOR (MO3) , DAMAGE TO NR 1 TURBINE WHEEL DUE TO IGNITER CENTER ELECTRODE FAILURE (EJECTED THROUGH WHEEL). TH IS IGNITER (9550168770 INSTALLED 07/11/2001) AND SL 2171/02/ARRIEL 1-66) INDICATES THAT THIS IGNITER WOULD PREVENT FUT URE FAILURES OF THIS TYPE FROM HAPPENING. REPLACED WITH RENTAL UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2002052100035 20020521 00035 EU 2002 5 21 R7MR35085 1 20020129 A 2432 RG390E BATTERY BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101600A 41560 NE MAIN FAULTY B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 61LF 6 7230 BATTERY WILL NOT HOLD CHARGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002110500114 20021105 00114 SO 2002 11 5 ASOA02250 1 20020430 A 3350 3071BPE LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 505AS 120279 DURING A GROUND INSPECTION IN DFW, ONE OF THE EMERGENCY FLOOR LIGHTS AT ROW 8 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT FLOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002052100036 20020521 00036 WP 2002 5 21 CALA0200306 1 20020520 A 5311 9923407502N FRAME DOUG DC9 DC982 3022082 WP STA 905 RT CRACKED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 83870 48056 OVERWING CABIN AREA RIGHT CENTER FUSELAGE FRAME AT STATION 905 CRACKED WHERE CABIN FLOOR BEAM ATTACHES TO FRAME. REMOVED AND REPLACED MAIN FRAME AT STATION 905 PER SRM 51-30-00. 2 L 7 2 4F A6WE 2002052100037 20020521 00037 WP 2002 5 21 CALA0200308 1 20020520 A 5511 7075T6050C RIB DOUBLER DOUG DC9 DC982 3022082 WP HORIZ STAB LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 HORIZONTAL STABILIZER RIGHT INBOARD LEADING EDGE OF ELEVATOR INTERNAL RIB DOUBLER CRACKED BELOW DUCT COUPLING. REMOVED A ND REPLACED RIB DOUBLER PER SRM 51-30-2. 2 L 7 2 4F A6WE 2002052100038 20020521 00038 WP 2002 5 21 CALA0200310 1 20020520 A 5313 7075T6063C FRAME DOUG DC9 DC982 3022082 WP FS1401 CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 TAIL COMPARTMENT STATION 1401 AT LONGERON 21 R FRAME HAS DEEP CHAFE. BLENDED DAMAGE AND INSTALLED REPAIR PER SRM 51-30-2 , 51-30-5, AND 53-03 FIG 4. 2 L 7 2 4F A6WE 2002052100039 20020521 00039 NM 2002 5 21 BJNA020401 1 20020405 A 3350 BATTERY BOEING 737 737214 138446R NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED ALL DEPLETED BATTERIES APPLICABLE PER BMM 33-51-51 AND 33-51-101. REPLACED L-1 LIGHT ASSEMBLY PER BMM 33-51-101. REPLACED AFT AISLE LIGHT BATTERY PER BMM 33-51-71. TESTS NORMAL. (M) 2 L 7 2 4F A16WE 2002052100040 20020521 00040 EU 2002 5 21 COEA0202729 1 20020328 A 3250 AC61906 LINE FOKKER F27 F27MK600 4990706 EU NLG STEERING LEAKING A COEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 13 729FE 10385 ON DEPARTURE FROM GEG, NOSE GEAR IN TRANSIT LIGHT REMAINED ON AFTER GEAR SELECTED UP. MAINTENANCE REMOVED AND REPLACED LEAKING STEERING MOTOR SWIVEL LINE AND FOLLOW UP CONTROL VALVE TO CORRECT PROBLEM. AIRCRAFT APPROVED FOR RETURN TO SERV ICE. (M) 2 H 7 2 4T A817 2002052100041 20020521 00041 NM 2002 5 21 EIA2002020 1 20020330 A 5320 WEB BOEING 747 747132 1384882 NM SUB FLOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MZJ - DURING C-CHECK, FOUND SUBFLOOR WEB AT STATION 140, STRINGER 31A LEFT SIDE, IN LOWER NOSE COMPARTMENT, WAS FOUND TO HAVE A CRACK APPROXIMATELY 6 INCHES LONG. REMOVED DAMAGED AREA AND REPAIRED PER ECRA 479-53-154-2. (M) 2 L 7 4 4F A20WE 2002052100042 20020521 00042 NM 2002 5 21 EIA2002021 1 20020330 A 5311 FRAME BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MZJ - FOUND FRAME AT STATION 1940, WL 125, BETWEEN STRINGERS 36L AND 37L WAS FOUND CRACKED. INSTALLED NEW FRAME PER SRM 51-30-2. (M) 2 L 7 4 4F A20WE 2002052100043 20020521 00043 SO 2002 5 21 000159 1 20020518 A 2612 FIRE LOOP EMB 145 EMB145 3260210 SO FIRE DETECTION FAULTY A CHQA O OTHER N FALSE WARNING UK UNKNOWN 1 GL 11 291 P3370234 E-2 FIRE DETECTION MSG. REMOVED AND REPLACED ENGINE FIRE LOOP. 2 L 7 2 4F RT T00011AT 2002052100044 20020521 00044 WP 2002 5 21 0201569972 1 20020512 A 2150 39271411 VALVE DOUG DC9 DC931 3022065 WP A/C BAY FAILED A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 9336 47338 DURING CLIMBOUT WITH THE ENGINE AND AIRFOIL ANTI-ICE SYSTEM ACTIVATED, THE FORWARD AND LEFT REAR LAV SMOKE DETECTOR ALAR MS SOUNDED. THE RIGHT AIR CONDITION SUPPLY TEMP HIGH LIGHT ILLUMINATED FOR ABOUT 10-15 MINUTES AND THEN EXTINGUISHED. THE LAV SMOKE DETECTORS QUIT SOUNDING AFTER ABOUT 5 MINUTES. SMOKE WAS INITIALLY REPORTED TO BE IN THE CABIN AREA BUT I T DISSIPATED QUICKLY AND WAS GONE PRIOR TO LANDING. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE RE PLACED BOTH WATER SEPARATOR BAGS, RIGHT PRESSURE REGULATOR VALVE, AND A/C PILOT PRESSURE REGULATOR. A SEAL AND DUCT WER E REPLACED ON THE RIGHT TEMP CONTROL VALVE DUE TO HOLE IN THEM. OPERATIONAL CHECK OK. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F A6WE 2002052100045 20020521 00045 NM 2002 5 21 0201626624 1 20020514 A 2120 ODOR BOEING 747 747251B 1384892 NM CABIN DETECTED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 01 624US 21706 DURING DESCENT, A STRONG ELECTRICAL BURNING SMELL EMITTED ABOVE THE NR 1 MAIN DECK GALLEY AND UPPER DECK GALLEY. AIRCRA FT LANDED WITHOUT INCIDENT. VISUALLY INSPECTED AND OPERATIONALLY CHECKED VARIOUS CABIN AND GALLEY SYSTEM WITH NO FAULTS FOUND. 2 L 7 4 4F A20WE 2002052100046 20020521 00046 NM 2002 5 21 EIA2002022 1 20020330 A 5330 SKIN BOEING 747 747132 1384882 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MZJ - FOUND BULGE IN SKIN BETWEEN STATION 2638 AND 2658 AT STRINGER 11 LT. REMOVED AND REPLACED DAMAGED SKIN PER ECRA 4 79-53-156-2. (M) 2 L 7 4 4F A20WE 2002052100048 20020521 00048 EU 2002 5 21 02139326 1 20020519 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 326UE 41064 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHT AT SEAT ROW 8 WAS INOPERATIVE. MAIN TENANCE PERSONNEL REMOVED AND REPLACED THE LAMP FOR THE LIGHT AT SEAT ROW 8. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002052100049 20020521 00049 EU 2002 5 21 02FDEA00 1 20020517 A 3230 SEQUENCE VALVE AIRBUS 310 A310 EU RT MLG MALFUNCTIONED A FDEA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 442FE 353 AFTER T/O FROM LGB THE GEAR WAS RAISED AND WAS CONFIRMED UP AND LOCKED UNTIL SLATS WERE RETRACTED AT WHICH TIME A THUMP AND SLIGHT SHUDDER WAS FELT AND L MAIN GEAR INDICATED UNSAFE. GEAR HANDLE WAS PLACED IN THE DOWN POSITION WITH ALL GEAR INDICATING DOWN AND LOCKED. UNABLE TO DUPLICATED, SUSPECTED BAD UPLOCK ACTUATOR. WHEN PERFORMING GEAR SWING PER M/M 3 2-31-00-516, PUT GEAR HANDLE IN NEUTRAL POSITION W/GEAR UP, AND HYD MULE PRESS WAS ABLE TO DUPLICATE PROBLEM ON ANOTHER A310 W/SAME PROBLEM. IT WAS T/S TO OPPOSITE SIDE MLG SEQ VALVE. 2 L 7 2 4F RT A35EU 2002052100050 20020521 00050 NM 2002 5 21 EIA2002028 1 20020330 A 5511 RIB BOEING 747 747132 1384882 NM HORIZONTAL STAB DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MZJ - FOUND C-CHECK SEVERLY DAMAGED HORIZONTAL STAB CLOSURE RIB AND TOTAL STRUCTURAL FAILURE OF WEB ALL AT HORIZONTAL ST ABILIZER APPROXIMATELY STATION 2598. REMOVED DAMAGED RIB AND WEB AND FABRICATED NEW AND INSTALLED PER SRM 51-32-02, 51- 20-01, 51-10-02. (M) 2 L 7 4 4F A20WE 2002052100051 20020521 00051 NE 2002 5 21 EIA2002035 2 20020412 A 7230 ACTUATOR BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE ENG STATOR FAILED A EIAA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 NM 09 482EV 20713 663084 CBBI - AFTER NR 4 THRUST LEVER WAS RETARDED TO IDLE ON DESCENT THE NR 4 ENGINE HAD AN UNRECOVERABLE COMPRESSOR STALL. E NGINE SHUTDOWN ACCOMPLISHED. RESTART UNSUCCESSFUL. INSPECTED ENGINE. REPLACED NR 4 ENGINE EVC UNIT (P/N 7479555) AND STATOR VANE CONTROL ACTUATOR (P/N 719999-6) AND PERFORMED EVC TRIM PROCEDURE IAW MM 75-31-08, 75-31-02 AND 71-00-00. (M ) 2 L 7 4 4F 4 F A20WE E20EA 2002052100052 20020521 00052 NM 2002 5 21 EIAA2002023 1 20020330 A 5311 FRAME BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MZJ - FOUND STATION 2140, RBL 19 LOWER WEB FRAME WAS FOUND CRACKED. REPAIRED PER SRM 53-10-23 AND 53-10-04. (M) 2 L 7 4 4F A20WE 2002052900047 20020529 00047 NM 2002 5 29 02FDEA00336 1 20020516 A 2121 215201 GASPER FAN BOEING 727 727200 138407E NM CABIN OVERHEATED A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 25 210FE 22932 IN RANGE TO LAS DETECTED A SLIGHT SMELL LIKE OVERHEATED EQUIPMENT. SMELL SEEMED TO DISSIPATE AFTER LANDING. RELEASED F OR SERVICE PER MEL/CDL. GASPER FAN INOP. REMOVED AND REPLACED GASPER FAN PER MM 21-23-011-4, OPS CHECK NORMAL. 2 L 7 3 4F RT A3WE 2002052100053 20020521 00053 WP 2002 5 21 02FDEA00337 1 20020516 A 3610 VALVE DOUG DC10 DC1030 3023501 WP PNEUMATIC SYS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 308FE 48297 ON CLIMB NR 2 PNEU TEMP HI LIGHT ILLUM'D. SHUTDOWN PNEU SUPPLY SEL. PERFORMED RED TAB PROC. REMOVED AND REPLACED THE NR 3 PACK FLOW VALVE AND THE NR 1 PNEU PRESS REGULATOR VALVE. ALL CHECK OK. 2 L 7 3 4F A22WE 2002053100118 20020531 00118 NM 2002 5 31 02FDEA00338 1 20020513 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 EXTERIOR SKIN DAMAGED JUST AFT OF FWD E BAY DOOR AT BS 226, RBL 5. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 1. 2 L 7 3 4F RT A3WE 2002052100054 20020521 00054 NM 2002 5 21 EIAA2002025 1 20020330 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MZJ - NUMEROUS HOLES IN UPPER FLOORBEAMS AT STATIONS 340, 360, AND 380 WERE FOUND TO HAVE CORROSION. REPAIRED PER ECRA 53-162-2. (M) 2 L 7 4 4F A20WE 2002052900050 20020529 00050 NM 2002 5 29 02FDEA00339 1 20020513 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 HOLES IN SHEAR TIE AND SKIN AT BS 580 BETWEEN STR 27 & 28L. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4, 51-30-2 & E A 7-5330-54321. 2 L 7 3 4F RT A3WE 2002052100055 20020521 00055 NM 2002 5 21 2002F00506 1 20020513 A 2121 731376 COOLING FAN BOEING 757 75723N 1384973 NM A/C BAY INOPERATIVE G AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 517AT 20641 20641 27973 FLIGHT NUMBER 710, INFLIGHT RECEIVED EICAS EQUIPMENT OVERHEAT. FLIGHT CREW COMPLETED QRH 2.7 PROCEDURE, SELECTED AUX EQ UIP COOLING FAN. OVERHEAT LIGHT EXTINGUISHED. MAINTENANCE REMOVED AND REPLACED THE NR 1 EQUIPMENT COOLING FAN PER MM 2 1-58-06, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002052100056 20020521 00056 EU 2002 5 21 MALA020268 1 20020506 A 2752 ACTUATOR SAAB SF340 SF340A 7850100 EU T/E FLAP OUT OF ADJUST A MALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 15 142XJ DURING FLIGHT FLAPS WERE DROOPING 2-3 DEGREES, THEN POPPING BACK UP, CAUSING PITCH OSCILLATIONS. AIR RETURN TO MSP. MA INTENANCE ADJUSTED FLAP ACTUATOR, LEFT AND RIGHT FLAP INTERCONNECT PUSHRODS AND FLAP POTS IAW AMM 27-51-00. PERFORMED F LAP FUNCTIONAL TEST, RIGGED FLAP CONTROL SYSTEM POTS, PERFORMED OPERATIONAL TEST OF FLAP CONTROL SYSTEM AND TEST OF THE FLAP CONTROL, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002052100057 20020521 00057 NM 2002 5 21 EIAA2002029 1 20020330 A 5740 FITTING BOEING 747 747132 1384882 NM LT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MZJ - FOUND IN C-CHECK, LT WING WBL 235, UPPER TRAILING EDGE PANEL SUPPORT T-FITING CRACKED AT THE NR 4 FLAP TRACK. INS TALLED NEW T-FITTING PER SRM 51-30-05. (M) 2 L 7 4 4F A20WE 2002052100058 20020521 00058 2002 5 21 MALA020269 4 20020507 A 3414 640608901 INDICATOR SAAB SF340 340B 7860101 EU COCKPIT DEFECTIVE A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 367PX 340B271 DURING FLIGHT 3036 WHILE CRUISING, FLIGHT AT 22,000 FT AND -20 DEGREES CELSIUS THE F/O AIRSPEED INDICATOR INCREASED SLOW LY TO 350 KIAS NO OVERSPEED WARNING WAS TRIGGERED, CAPT AND STBY AIRSPEED INDICATOR OPERATES NORMALLY. AIR RETURN TO MS P. MAINTENANCE DRAINED AND PURGED W/DRY NITROGEN NR 2 PITOT SYSTEM, REMOVED AND REPLACED NR 2 ASI. NR 2 PITOT STATIC S YSTEM AND NR 2 ASI TEST GOOD IAW SF340 MM CHAP 34. PITOT HEAT TEST GOOD. 2 L 7 2 4T RT A52EU 2002052100059 20020521 00059 EU 2002 5 21 MALA020270 1 20020507 A 3230 BOLT SAAB SF340 340B 7860101 EU LT & RT MLG DEFECTIVE A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 402XJ 340B402 DURING FLIGHT 3115 INBOUND TO DTW, LEFT LANDING GEAR WOULD NOT LOCK IN DOWN POSITION. RAN QRH GEAR DOWN UNSAFE CONDITIO N. PUMPED GEAR DOWN AND PULLED EMERGENCY GEAR HANDLE, STILL LEFT MAIN LIGHT REMAINED OUT. DECLARED EMERGENCY AND LANDE D SUCCESSFULLY IN DTW. MAINTENANCE REPLACED LT AND RT MAIN GEAR EXPLOSIVE BOLTS AND LT MAIN GEAR O/B ASSIST SPRING AND CABLE ASSY. 2 L 7 2 4T RT A52EU 2002052100060 20020521 00060 NM 2002 5 21 EIAA2002030 1 20020330 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MZJ - FOUND DURING C-CHECK, STATION 400 FLOORBEAM AT RIGHT SIDE, 70 INCHES FROM BUTT LINE 0 WAS FOUND CORRODED. REPAIRE D PER ECRA 479-53-262-2. (M) 2 L 7 4 4F A20WE 2002052100061 20020521 00061 NM 2002 5 21 GAIA02024OP 1 20020312 A 7500 CLAMP BOEING 727 727223 1384074 NM NR 1 ENGINE LOOSE A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6806 19481 FLT 733 - DFW-FWA - DURING CLIMB-OUT, THE NR 1 STRUT OVERHEAT LIGHT CAME ON. THE AIRCRAFT RETURNED TO DFW AND THE LANDI NG WAS UNEVENTFUL. FOUND THE CLAMP FOR THE EIGHT STAGE BLEED VALVE LOOSE. TIGHTENED THE SAME AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002052100062 20020521 00062 EU 2002 5 21 MALA020271 1 20020508 A 2612 51533172 FIRE LOOP SAAB SF340 SF340A 7850100 EU FIRE DETECTION FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 991XJ 340A091 DURING FLIGHT 2801, LEFT BLEED AIR LEAK LIGHT ILLUMINATED INFLIGHT FOLLOWED QRH AFTER BLEEDS CLOSED 10 MINUTES LIGHT EXT INGUISHED. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED FIRE WIRE IAW 36-23-10-2 AND PERI SEALS ON LT FLAP COVE , OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2002052100063 20020521 00063 EU 2002 5 21 MALA020272 1 20020501 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 DURING 4K-CHECK IN CWA, SEAT TRACK LBL 18.3 HAS CORROSION. MAINTENANCE REPLACED SEAT TRACK FROM STA 297-329 IAW EO 5306 0. 2 L 7 2 4T RT A52EU 2002052100064 20020521 00064 NM 2002 5 21 GAIA02025OP 1 20020314 A 3610 652663919 DUCT BOEING 727 727223 1384074 NM NR 1 ENGINE WARPED A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6806 19481 FLT 873 - FWA-LAX - DURING CLIMB-OUT, THE NR 1 STRUT OVERHEAT LIGHT CAME ON FIVE MINUTES AFTER TAKEOFF. THE AIRCRAFT RE TURNED TO FWA AND THE LANDING WAS UNEVENTFUL. FOUND THE 13 STAGE DUCT IN THE STUB WING AT THE HIGH PRESSURE WING ANTI-I CE VALVE FLANGE WARPED. REMOVED AND REPLACED THE 13 STAGE DUCT AND OPERATIONALLY CHECKED GOOD AT ENGINE IDLE AND TAKEOF F POWER SETTINGS. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002052100065 20020521 00065 NE 2002 5 21 MALA020276 2 20020511 A 7532 6068T56P01 BLEED VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 367PX 340B271 DURING FLIGHT 2789, LT AIR VALVE LIGHT ILLUMINATED IN ICING CONDITIONS. LT AIR VALVE LIGHT CAME ON AT 16,000 FT MSL FOL LOWED QRH AND RESET SWITCH. LIGHT STAYED ON OPERATED LEFT ENGINE BELOW 86 PERCENT NG UNTIL CLEAR OF ICING CONDITIONS AS PER QRH. AIR RETURN TO MSP. MAINTENANCE REPLACED THE LT AIR VALVE IAW GE MM 75-00-00. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2002052100066 20020521 00066 EU 2002 5 21 MALA020277 1 20020412 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 514XJ E2330 DURING C-CHECK IN CVG, NR 1 SEAT RAIL CORRODED BEYOND ALLOWABLE SRM LIMITS. MAINTENANCE REPAIRED DAMAGE BY REPLACING DA MAGED SECTION PER SRM 53-00-32 PAGE BLOCK 201 AND EO A53026. 2 H 7 4 4F RT A49EU 2002052100067 20020521 00067 EU 2002 5 21 MALA020279 1 20020412 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 514XJ E2330 DURING C-CHECK IN CVG, NR 4 SEAT RAIL CORRODED BEYOND ALLOWABLE SRM LIMITS. MAINTENANCE REPAIRED DAMAGE BY REPLACING DA MAGED SECTION PER SRM 53-00-02, PAGE BLOCK 201 AND EO A53026. 2 H 7 4 4F RT A49EU 2002052100068 20020521 00068 EU 2002 5 21 MALA020280 1 20020412 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 514XJ E2330 DURING C-CHECK IN CVG, CORROSION WAS FOUND ON THE FRAME 18 O/B FLOORBEAM OF SEAT RAIL NR 3. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH RIL HC537H9257, BAE FAX BARA/AVR/5907/02-MGK AND EO A53082. 2 H 7 4 4F RT A49EU 2002052100069 20020521 00069 EU 2002 5 21 MALA020282 1 20020412 A 5753 FLAP BAC 146 AVRO146RJ85A 1500097 EU RT WING CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 514XJ E2330 DURING C-CHECK IN CVG, THE RT FLAP SUFFERED CHAFE DAMAGE TO THE LEADING EDGE BETWEEN RIBS 29 AND 30. MAINTENANCE REPAIR ED DAMAGE IN ACCORDANCE WITH BARA/AVR/5684/01-DC AND EO A57040. 2 H 7 4 4F RT A49EU 2002052100070 20020521 00070 EU 2002 5 21 QXEA0200740 2 20020508 A 7200 FIRE FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY555* 54521 EU NR 2 ENGINE DETECTED A QXEA E ENGINE SHUTDOWN A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 09 499US 11182 BOI- BOI TOWER REPORTED FLAMES AND SMOKE COMING FROM NR 2 ENGINE AT TOUCHDOWN, NO ABNORMAL INDICATIONS ON ENGINE GAUGES. SHUTDOWN NR 2 ENGINE ON ROLL OUT. PERFORMED VISUAL INSPECTION OF TAILPIPE/EXHAUST AND INTAKE, NO DEFECTS NOTED. PERF ORMED GROUND RUN AT NUMEROUS POWER SETTINGS WITH THROTTLE IDLE, NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A20EU E2EU 2002052100071 20020521 00071 NM 2002 5 21 QXEA0200741 1 20020502 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 9 SEAT TRACK IS CORRODED ON INBOARD FLANGE. REPAIRED IAW RD-8 53-4936. 2 H 7 2 4T RT A13NM 2002052100072 20020521 00072 NM 2002 5 21 GAIA02026OP 1 20020313 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM PAX DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 854AA 20995 DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE FORWARD ENTRY EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKS NORMAL. THE AIRCRAFT WAS RT URNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002052100073 20020521 00073 NM 2002 5 21 QXEA0200742 1 20020502 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 6 SEAT TRACK IS CORRODED ON INBOARD FLANGE STATION X545 - X549. REPAIRED IAW RD-8 53-4936. 2 H 7 2 4T RT A13NM 2002052100074 20020521 00074 NM 2002 5 21 QXEA0200743 1 20020502 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 6 SEAT TRACK CORRODED ON OUTBOARD FLANGE STATION X593 - X597. REPAIRED IAW RD-8 53-4936. 2 H 7 2 4T RT A13NM 2002052100075 20020521 00075 NM 2002 5 21 QXEA0200744 1 20020501 A 5320 FLANGE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- CARGO COMPARTMENT DECK PANEL CUT OUT FLANGE HAS CORROSION. REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-20-36 AND SRM 5 1-20-41. 2 H 7 2 4T RT A13NM 2002052100076 20020521 00076 NM 2002 5 21 QXEA0200745 1 20020502 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- CARGO DOOR THRESHOLD IS CORRODED ON UPPER SURFACE STATION X550 - X580. REPAIRED IAW DHC-8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002052100077 20020521 00077 NM 2002 5 21 QXEA0200746 1 20020503 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- CARGO DOOR THRESHOLD HAS SIGNS OF CORROSION ON LOWER SURFACE OF UPPER STRUCTURE AROUND NUT PLATES. REPAIRED IAW DH C-8 SRM 51-30-26 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002052100078 20020521 00078 NM 2002 5 21 QXEA0200747 1 20020503 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- CARGO DOOR THRESHOLD DRAIN AREA, ANGLE IS CORRODED STATION X566 - X580. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51 -20-36. 2 H 7 2 4T RT A13NM 2002052100079 20020521 00079 NM 2002 5 21 QXEA0200748 1 20020502 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- CARGO DOOR THRESHOLD, LOWER SURFACE OF UPPER STRUCTURE HAS CORROSION STATION X558 AND X572. REPAIRED IAW DHC-8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002052100080 20020521 00080 NM 2002 5 21 QXEA0200749 1 20020502 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- OUTER AIRCRAFT SKIN HAS LIGHT SURFACE CORROSION AT LOWER TCAS ANTENNA CUTOUT. REPAIRED IAW DHC-8 SRM 53-00-16 PG 2 & 3. 2 H 7 2 4T RT A13NM 2002052100081 20020521 00081 NE 2002 5 21 GAIA02030BOP 2 20020404 A 7200 ENGINE BOEING 727 727251 138408H NM PWA JT8 JT8D7B 52053 NE NR 1 FAILED A GAIA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 07 252US 19971 666105 FLT 734 - FWA-DFW - ON CLIMB AT FL270, THE FLIGHT CREW HEARD THE NR 1 ENGINE MAKE A GRINDING NOISE. THE OIL TEMP INCREA SED TO 120 AND THERE WAS A SHARP JUMP IN EPR. OIL PRESSURE DECREASED AND THE NR 1 ENGINE WAS SHUTDOWN. THE CREW DECLAR ED AN EMERGENCY AND RETURNED TO FWA. THE AIRCRAFT MADE A UNEVENTFUL LANDING. UPON INSPECTION OF THE NR 1 ENGINE, IT WA S DISCOVERED THAT THE T-3 AND T-4 TURBINE WAS DAMAGED. THE AIRCRAFT WAS MAINTENANCE FERRIED TO DFW FOR AN ENGINE CHANGE . THE NR 1 ENGINE WAS REMOVED, REPLACED, AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2002052100082 20020521 00082 NM 2002 5 21 QXEA0200750 1 20020503 A 5320 FLANGE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- CARGO COMPARTMENT DECK PANEL CUTOUT FLANGE HAS CORROSION ON MATING SURFACE. REPAIRED IAW DHC-8 SRM 51-20-10, SRM 5 1-20-36 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002052100083 20020521 00083 NM 2002 5 21 QXEA0200751 1 20020503 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- FORWARD CARGO DOOR, LOWER STOP BRACKET IS CHAFED. REPAIRED IAW DHC-8 SRM 51-00-06. 2 H 7 2 4T RT A13NM 2002052100084 20020521 00084 NM 2002 5 21 QXEA0200752 1 20020502 A 3220 ARM DHAV DHC8 DHC8202 2809007 NM NLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NOSE LANDING GEAR TRAILING ARM FORWARD EDGE HAS SEVERAL AREAS OF CHIPPED PAINT AND CHAFE DAMAGE. REPAIRED IAW RD-8 32-289. 2 H 7 2 4T RT A13NM 2002052100085 20020521 00085 NM 2002 5 21 QXEA0200753 1 20020505 A 5751 MOUNT DHAV DHC8 DHC8202 2809007 NM AILERON GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- RT AILERON WRAP AROUND PANEL 643ER MOUNT AND FLANGE HAVE GOUGES. REPAIRED IAW DHC-8 SRM 51-20-11, SRM 57-60-11 PG 5. 2 H 7 2 4T RT A13NM 2002052100086 20020521 00086 NM 2002 5 21 QXEA0200754 1 20020503 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX-RIGHT HAND OUTBOARD FLAP TOP SURFACE CHAFED. REPAIRED IAW RD-8 57-1734, RD-8 57-1549 AND DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2002052100087 20020521 00087 NM 2002 5 21 QXEA0200755 1 20020502 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- TOP FORWARD BAGGAGE DOOR STOP INBOARD FLANGE IS CHAFED. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2002052100088 20020521 00088 NM 2002 5 21 GAIA02032OP 1 20020410 A 2750 CONNECTOR BOEING 727 727251 138408H NM TE FLAPS DIRTY A GAIA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 252US 19971 FLT 713 - HSV-FWA - ON APPROACH, THE AIRCRAFT HAD OUTBOARD SPLIT FLAP INDICATION. THE CREW USED THE EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED AT HSV UNEVENTFUL. CLEANED THE CONNECTOR PLUG AT THE OUTBOARD FLAP TRA NSMITTERS. CYCLED THE FLAPS SEVERAL TIMES AND FOUND TO OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 L 7 3 4F A3WE 2002052100089 20020521 00089 NM 2002 5 21 QXEA0200757 1 20020503 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 9 SEAT TRACK IS CORRODED ON INBOARD FLANGE STATION X598. REPAIRED IAW RD-8 53-4936 AND HORIZON AIR EA 2-53-390. 2 H 7 2 4T RT A13NM 2002052100090 20020521 00090 NM 2002 5 21 QXEA0200758 1 20020506 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 3 SEAT TRACK HAS AREAS OF LIGHT CORROSION AT STATION X515 - X517, X529 - X531 AND X541 - X543. REPAIRED IAW DHC -8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002052100091 20020521 00091 NM 2002 5 21 QXEA0200759 1 20020506 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM BULKHEAD MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- RIVET MISSING AT COCKPIT BULKHEAD, BRACKET, STATION Z100, Y10.25R. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002052100092 20020521 00092 NM 2002 5 21 GAIA02033OP 1 20020411 A 2751 9660022001 TRANSMITTER BOEING 727 727251 138408H NM LT/RT WING INOPERATIVE A GAIA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 252US 19971 FLT 2863 - BWI-FWA - ON APPROACH, THE AIRCRAFT HAD THE OUTBOARD FLAPS ASYMMETRY BETWEEN ZERO AND TWO DEGREES FLAPS. THE CREW USED THE EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED AT FWA UNEVENTFUL. REMOVED AND REPLA CED LEFT AND RIGHT OUTBOARD FLAP POSITION TRANSMITTERS. ALSO, REPLACED THE LEFT OUTBOARD TRANSMITTER CANNON PLUG. CYCL ED THE FLAPS EVERAL TIMES AND FOUND TO OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002052100093 20020521 00093 NM 2002 5 21 GAIA02037OP 1 20020418 A 7500 CLAMP BOEING 727 727251 138408H NM NR 3 ENGINE OUT OF POSITION A GAIA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 278US 21157 FLT 875 - FWA-LAX - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, AND OPERATED AT REDUCED THRUST TO EXTINGUISHED THE LIGHT. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT LAX WAS UNEVENTFUL. RE POSITIONED CLAMP ON NR 3 ENGINE BLEED VALVE. OPERATED NR 3 ENGINE AND NO OTHER OVERHEAT INDICATION WAS NOTED AND WAS FO UND TO BE OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002052100094 20020521 00094 NM 2002 5 21 GAIA02038OP 1 20020419 A 3610 CLAMP BOEING 727 727251 138408H NM NR 3 ENGINE OUT OF POSITION A GAIA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 278US 21157 FLT 874 - LAX-FWA - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, AND OPERATED AT REDUCED THRUST TO EXTINGUISHED THE LIGHT. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT FWA WAS UNEVENTFUL. AD JUSTED SHIMS AND REPOSITIONED CLAMP ON NR 3 ENGINE BLEED VALVE. OPERATED NR 3 ENGINE AND NO OTHER OVERHEAT INDICATION W AS NOTED AND WAS FOUND TO BE OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002052100095 20020521 00095 WP 2002 5 21 0201579150 1 20020513 A 2931 SRL7F INDICATOR DOUG DC9 DC914 3022034 WP HYD SYSTEM MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 GL 01 8908E 45749 RIGHT HYDRAULIC SYSTEM PRESSURE WENT TO ZERO. RIGHT HYDRAULIC QUANTITY WENT TO 10 QUARTS FROM 7-8 THAT WAS SHOWING AT T AKEOFF. COMPLIED WITH COM AND LANDED AT MSP WITHOUT INCIDENT. THE AIRCRAFT WAS TOWED TO THE GATE FROM THE TAXIWAY. MA INTENANCE TESTED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP AND FOUND NO PROBLEMS WERE FOUND. THE WIRING FOR THE PUMP WAS A LSO INSPECTED AND NO TROUBLE WAS FOUND. NO INDICATIONS OF ANY HYDRAULIC SYSTEM FILTERS BEING CLOGGED. RIGHT HYDRAULIC SYSTEM FLUID QUANTITY WAS AT NORMAL OPERATING LEVELS AND NO LEAKS WERE FOUND. THE RIGHT HYDRAULIC SYSTEM PRESSURE INDI CATOR WAS REPLACED AS A PRECAUTION. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F A6WE 2002052100096 20020521 00096 NE 2002 5 21 GAIA02039OP 2 20020419 A 7532 BLEED VALVE BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE LEAKING A GAIA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 278US 21157 FLT 734- FWA-DFW - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THEN RN 3 BLEED, AND OPERATED AT REDUCED THRUST TO EXTINGUISH THE LIGHT. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT FWA WAS UNEVENTFUL. REPL ACED CLAMPS ON NR 3 ENGINE BLEED VALVE. ALSO, FOUND THE 13 STAGE MOD VALVE SENSE LINE CRACKED. REMOVED AND REPLACED TH E SAME. OPERATED NR 3 ENGINE WITH NO OTHER OVERHEAT INDICATION AND WAS FOUND TO OPERATIONALLY CHECKED GOOD. THE AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2002052100097 20020521 00097 WP 2002 5 21 0201599969 1 20020514 A 3241 391011D VALVE DOUG DC9 DC931 3022065 WP ANTI-SKID SYS LEAKING A NWAA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 9333 47246 DURING START WHEN THE CREW ATTEMPTED TO PRESSURIZE THE RIGHT HYDRAULIC SYSTEM, THE HYDRAULIC PRESSURE INDICATION DID NOT RISE AND THE HYDRAULIC QUANTITY INDICATION DROPPED TO ZERO. FLIGHT ABORTED THE START AND RETURNED TO THE GATE. MAINTE NANCE FOUND THE RIGHT OUTBOARD ANTI-SKID VALVE FITTING LEAKING. THE ANTI-SKID VALVE WAS REPLACED AS WAS THE ENGINE DRIV EN HYDRAULIC PUMP AND FILTERS AND THE ELECTRICAL HYDRAULIC PUMP AND FILTERS. SYSTEM WAS SERVICED, LEAK CHECKED, AND OPE RATIONALLY CHECKED WITHOUT FURTHER PROBLEMS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002052100098 20020521 00098 NM 2002 5 21 GAIA02040OP 1 20020429 A 2750 JACKSCREW BOEING 727 727223 1384074 NM TE FLAPS DAMAGED A GAIA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 6809 19484 FLT 879 - FWA-SJC - DURING CLIMB-OUT WHEN FLAPS SELECTED TO RETRACT. THE OUTBOARD FLAPS WHERE SPLIT. THE CREW DECLARED AND EMERGENCY LANDING, DUMPED FUEL AND RETURNED TO FWA. THE LANDING WAS UNEVENTFUL. REMOVED AND REPLACED THE LEFT OUT BOARD FLAP OUTBOARD JACKSCREW BALL END GUIDE. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002052100099 20020521 00099 NE 2002 5 21 GTIA020286 2 20020409 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE LEFT MALFUNCTIONED A GTIA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 23 817NK 49141 FLL - FLT 197 - LEFT ENGINE POWER LAGS BEHIND RIGHT ENGINE DURING POWER CHANGES IN CRUISE FLIGHT THROTTLES ARE SPLIT 1-1 .25 TO MAINTAIN EVEN POWER SETTINGS. THROTTLES ARE SPLIT 1.5 AT CLIMB POWER. THIS GETS MORE PRONOUNCED AS ALTITUDE INC REASES. AUTO THROTTLES DISCONNECTED SEVERAL TIMES DUE TO LEFT ENGINE LAGGING BEHIND ON POWER CHANGES. PERFORMED ENGINE RUN-UP AND TRIN ON NR 1 AND NR 2 ENGINES IAW MM 71-00-00, OPS CHECK NORMAL. (M) 2 L 7 2 4F 4 F A6WE E2EA 2002052100100 20020521 00100 WP 2002 5 21 GTIA020287 1 20020411 A 2700 SWITCH DOUG DC9 DC981 3022081 WP LE SLATS FAILED A GTIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 810NK 48015 DTW - FLT 595 - DURING SLAT EXTENSION, THE AUTO SLAT FAIL LIGHT ILLUMINATED AND THE SLAT DISAGREE LIGHT REMAINED ON. BO TH STALL WARNING SYSTEM PROPERLY. AUTO SLAT FAIL LIGHT REMAINED ILLUMINATED WITH SLATS RETRACTED. REMOVED AND REPLACED FLAP HANDLE SWITCH AND OPS CHECK GOOD IAW MM 27-80-07. (M) 2 L 7 2 4F A6WE 2002052100101 20020521 00101 WP 2002 5 21 GTIA020288 1 20020411 A 2750 FLAP DOUG DC9 DC983 3022083 WP RT TE FLAPS LACK OF LUBE A GTIA O OTHER F FLT CONT AFFECTED LD LANDING 1 GL 23 602CA 49415 LGA - FLT 1864 - FLAPS DID NOT FULLY RETRACT AFTER LANDING. CLEANED AND INSPECTED RIGHT TRAILING EDGE FLAP LUBED FLAPS, OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 2002052100102 20020521 00102 WP 2002 5 21 GTIA020289 1 20020411 A 3260 PROXIMITY SWITCH DOUG DC9 DC983 3022083 WP MLG FAILED A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 16892 49391 LGA - FLT 1774 - AFTER GEAR RETRACTION LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. PERFORMED QRH PROCEDURES. RED LIGH T REMAINED ILLUMINATED NO VIBRATION, SUSPECT MICROSWITCH ADJUSTMENT. REPLACED LEFT MLG DOWN LOCK PROX SWITCH AND REROUT ED WIRING CONDUIT. PERFORMED GEAR SWING OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2002052100103 20020521 00103 WP 2002 5 21 MEX2002003 1 20020201 A 2131 CONTROLLER DOUG DC9 DC987 3022087 WP CABIN PRESSURE FAILED A ASMF O OTHER J WARNING INDICATION CR CRUISE 1 SW 23 751RA 3227 49779 MEX-IAH - FLT 418 - AT ARRIVING CAPTAIN INFORMED A REPETITIVE REPORT RELATED WITH PRESSURIZATION, DFW TECHNICIAN INFORME D TO FAA AUTHORITIES. IT WAS PERFORMED A BITE TO BOTH PRESSURE CONTROLS, GIVING AS A RESULT AN ACTUATOR FAIL, IT WAS CH ANGED DURING TRANSIT CHECK. AT MEX RON, ELECTRONIC PERSONNEL CONFIRMED AIRCRAFT WITHOUT REPORTS AFTER CHANGE. TESTS OK IAW MM 21-32-5. (M) 2 L 7 2 4F RT A6WE 2002052100104 20020521 00104 WP 2002 5 21 ABXA010886 1 20020520 A 3260 7000010101ABX SWITCH DOUG DC9 DC931 3022065 WP DEFECTIVE A ABXA O OTHER O OTHER AP APPROACH 1 GL 23 907AX 47203 DURING INITIAL GEAR EXTENSION, THE NOSE LANDING GEAR LIGHT FLICKERED ON AND OFF AND CONTINUED TO DO SO UNTIL THE GEAR WA S RAISED. FOUND NOSE LANDING GEAR DOWN LOCK SWITCH TO BE STICKING. REPLACED SWITCH IAW DC-9 MM 32-60-01. PERFORMED A GEA R SWING. ALL INDICATIONS NORMAL. 2 L 7 2 4F A6WE 2002052100105 20020521 00105 NE 2002 5 21 MEX2002008 2 20020107 A 7230 BLADE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE CRACKED A ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 204AM 49404 FLT 259 - CJS-MEX - DURING TRANSIT CHECK REVISION IN THE STATION IT WAS INFORMED THAT THE NR 21 BLADE OF THE ENGINE 1 HA S A CRACK OF 4 INCHES IN LENGTH AND .25 INCH OF DEPTH APPROXIMATELY. THE BLADE WAS REWORKED AND THE AIRCRAFT WAS DISPAT CHED TO FLIGHT. AT ARRIVED TO MEX THE DAMAGE WAS VERIFIED FINDING IT OUT OF LIMITS, AT THE RON 07/08 IN MEX THE ENGINE 1 WAS REPLACED IAW MM 71-00-01, TESTS OK. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002052100106 20020521 00106 NE 2002 5 21 MEX2002012 2 20020113 A 7230 QEC217 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE DAMAGED A ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 1003X 39186 2314 48067 FLT 419 - IAH-MEX - BLADE OF ENGINE 1 HAS A FOLD OF 1.25 INCH TO .25 INCH FROM THE TRAILING EDGE, THE DAMAGE WAS REPAIRE D IAW MM 72-33-22, THE ENGINE RUN WAS OK. DURING RON 13/14 IN MEX THE ENGINE 1 WAS REPLACED IAW MM 71-00-02, TESTS OK. (M) 2 L 7 2 4F 4 F A6WE E9NE 2002052100107 20020521 00107 NM 2002 5 21 QXEA0200760 1 20020507 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- LIGHT FRETTING CORROSION ON CENTER CABIN FLOOR SUPPORT WHERE RUBBER STRIP IS DISBONDED. REPAIRED IAW DHC-8 SRM 51- 20-11, PG 5, 7, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002052100108 20020521 00108 NM 2002 5 21 QXEA0200761 1 20020502 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 6 SEAT TRACK IS WORN AND CORRODED ON INNER SURFACE AT STATION X542 - X545. REPAIRED IAW RD-8 53-4936. 2 H 7 2 4T RT A13NM 2002052100109 20020521 00109 NM 2002 5 21 QXEA0200762 1 20020503 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- SUPPORT ANGLE FOR PANEL 144CZ (AFT EDGE) IS CORRODED AT STATION X600, Y27R. REPAIRED IAW DHC-8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002052100110 20020521 00110 NM 2002 5 21 QXEA0200763 1 20020503 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 9841 PDX- SUPPORT ANGLE FOR PANEL 144BZ (AFT EDGE) IS CORRODED AT STATION X600, Y3R-Y8R. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002052100111 20020521 00111 NM 2002 5 21 QXEA0200764 1 20020503 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- SUPPORT ANGLE FOR PANEL 144BZ (AFT EDGE) IS CORRODED AT STATION X600, Y4L - Y7L. REPAIRED IAW DHC-8 SRM 51-20-11 A ND SRM 51-40-36. 2 H 7 2 4T RT A13NM 2002052100112 20020521 00112 NM 2002 5 21 QXEA0200765 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 1 SEAT TRACK CORRODED ON INNER SURFACE AT STATION X271 - X273. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052100113 20020521 00113 NM 2002 5 21 QXEA0200766 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 1 SEAT TRACK CORRODED ON UPPER AND INNER SURFACES AT STATION X277 - X281. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052100114 20020521 00114 NM 2002 5 21 QXEA0200767 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 1 SEAT TRACK CORRODED ON UPPER AND INNER SURFACES AT STATIONS X295 - X298. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052100115 20020521 00115 NM 2002 5 21 QXEA0200768 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 1 SEAT TRACK HAS DEEP GOUGES. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052100116 20020521 00116 NM 2002 5 21 QXEA0200769 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 1 SEAT TRACK IS CORRODED ON INNER SURFACE AT STATION X362.5. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052100117 20020521 00117 WP 2002 5 21 UPS02837883 1 20020218 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C23 L1 DOOR CORNER UPPER FWD DOUBLER CONDUCTIVITY TEST SHOWS NOT TO BE ALUMINUM. REMOVED EXISTING DOUBL ER, ROUTED OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLERS IAW DC8 SRM 53-2-0 FIG 15. 2 L 7 4 4F RT 4A25 2002052100118 20020521 00118 WP 2002 5 21 UPS02837995 1 20020409 A 5280 DOOR DOUG DC8 DC873F 302199F WP NLG DAMAGED A IPXA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SO 01 803UP 46073 INSPECTION TYPE:N/A VIBRATION FROM NOSE GEAR AREA. CREW DECLARED EMERGENCY. A/C LANDED SAFELY. LT NLG AFT DOOR HAS 8 INCH CRACK ON AFT END OF DOOR. DOOR REMOVED NLG DOORS REQUIRE ADJ AND TEST MM 32-22-01. FOUND LT AND RT NLG AFT DOORS BROKEN. LT DOOR WAS CRACKED. RT GEAR DOOR AFT HINGE BROKE OFF AT DOOR CAUSING PROBLEM. REMOVED AND REPLACED RT NLG AF T DOOR. PERFORMED NLG DOOR ADJ/TEST PROCEDURES, OPS CKS OK IAW MM 32-22-01. 2 L 7 4 4F RT 4A25 2002052100119 20020521 00119 WP 2002 5 21 IXXA0200020O 1 20020519 A 2121 FAN DOUG DC8 DC862 3021970 WP FWD BELLY DEFECTIVE A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 21CX 70359 724 45955 ENROUTE FROM BWI TO WRI, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT WHEN THE RIGHT RECIRCULATION FAN WAS OPERATING. T HE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPEC TED THE AIRCRAFT WHICH REVEALED THE RIGHT RECIRCULATION FAN DEFECTIVE. MAINTENANCE REPLACED THE FAN AND PERFORMED A SUCC ESFUL OPERATIONAL TEST IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002052100120 20020521 00120 WP 2002 5 21 IXXA0200016S 1 20020110 A 5200 DOOR DOUG DC8 DC871F 302199D WP STATION 340 GOUGED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 823BX 83172 2873 46064 DURING ROUTINE C-CHECK INSPECTION, A GOUGE WAS DETECTED ON THE C-1 DOOR CUTOUT, AFT SECTION BY THE LIGHT SWITCH, STATION 340. BLENDED OUT DAMAGED AREA. FABRICATED AND INSTALLED NEW REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR M ANUAL AND ENGINEERING ORDER 52-DC8-1836. 2 L 7 4 4F RT 4A25 2002052100121 20020521 00121 WP 2002 5 21 IXXA0200017S 1 20020209 A 5711 SPAR DOUG DC8 DC871F 302199D WP RIGHT WING CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 823BX 83172 2873 46064 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING LOWER SPAR INBOARD OF THE #4 ENGINE PYLON FORW ARD SECTION. FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 57-DC8-1837. 2 L 7 4 4F RT 4A25 2002052100122 20020521 00122 WP 2002 5 21 IXXA0200019S 1 20020128 A 5700 FITTING DOUG DC8 DC871F 302199D WP FLAP GOUGED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 823BX 83172 2873 46064 DURING ROUTINE C-CHECK INSPECTION A GOUGE WAS DETECTED ON THE FLAP SUPPORT FITTING INBOARD INNER EDGE, STATION 405. BLEN DED OUT DAMAGED AREA IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 57-DC8-1839. 2 L 7 4 4F RT 4A25 2002052100123 20020521 00123 WP 2002 5 21 UPS02838041 1 20020228 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 FWD ACCESSORY COMPT AT FS 660 RBL 12 MAIN CABIN FLOOR INTERCOSTAL IS CRACKED. FABRICATED DOUBLER IAW DC8 SRM 53-2-0, INSTALLED IAW DC8 SRM 51-1-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 2002052100124 20020521 00124 WP 2002 5 21 UPS02838042 1 20020328 A 5720 CLIP DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 O/B SKATE ANGLE CLIP BETWEEN STRINGER 62 AND STRINGER 63 CRACKED NR 1 PYLON NR 1 ALT. REMOVED AND RE PLACED CLIP IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002052100125 20020521 00125 WP 2002 5 21 UPS02838043 1 20020324 A 5320 3755843 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1230 BETWEEN L34R - L35R Z-FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC SRM 53-2-0 FIG 2D. FABBED SPLICE ANGLES IAW DC8 SRM 53-2-0, INSTALLED FITTING AND REPAIR ANGLES IAW DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2002052100126 20020521 00126 WP 2002 5 21 UPS02838045 1 20020324 A 5320 37558401 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 AFT PIT IN TORQUE BOX STA 1220-1228 BETWEEN LONG 33R TO 32R IS CORRODED. REMOVED AND REPLACED CORROD ED ANGLE IAW DC8 SRM 53-2-0 FIG 2D. FABBED SPLICE ANGLE IAW DC8 SRM 563-2-0, INSTALLED Z-ANGLES & SPLICES IAW DC8 SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002052100127 20020521 00127 WP 2002 5 21 UPS02838049 1 20020415 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:PFLT EMERGENCY LIGHTS BATTERY PACK INOP. EMERGENCY LIGHTS BATTERY PACK REMOVED AND REPLACED AS PER MM 3 3-50-00. 2 L 7 4 4F RT 4A25 2002052100128 20020521 00128 WP 2002 5 21 UPS02838050 1 20020416 A 2910 HYDRAULIC LINE DOUG DC8 DC873F 302199F WP LT MLG LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 01 806UP 46006 INSPECTION TYPE:N/A ATB DUE TO HYDRAULIC FAILURE. WHILE MANUALLY PUMPING OPEN CARGO DOOR, NOTED HYD LEAK IN LT W/W. TR ACED LEAK TO FLEX LINE ON DOWNLOCK BUNGEE, LEAKING JUST DOWNSTREAM OF FITTING ON BUNGEE. FOUND FLEX LINE LEAKING GOING TO LT GEAR DOWNLOCK REMOVED AND REPLACED SAME. LEAK CHECK GOOD. SERVICED HYD TO FULL. INSPECTED HIGH PRESS FILTERS OK REMOVED AND REPLACED LT AND RT HYD PUMP CAE DRAIN FILTERS IAW M/M 29-00-00 PG 218. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2002052100129 20020521 00129 WP 2002 5 21 UPS02838052 1 20020325 A 5240 DOOR DOUG DC8 DC871F 302199D WP AIRSTART DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 PERMANENT REPAIR ON SECOND AIRSTART DOOR IAW EO DC8-5330-12800. REPAIRED AREA IAW UPS EO DC8-5330-07 93 AND DAC DRWG 08530020. 2 L 7 4 4F RT 4A25 2002052100130 20020521 00130 WP 2002 5 21 UPS02838053 1 20020327 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 REPAIR AT BS 25.5 TO 39.25, L21L TO L22L FALLS INTO THE D CAT PER UPS EO DC8-5330-12800 AND REQUIRED FURTHER EVAL BY ENGINEERING BY REPAIR GOUGED BEYOND LIMITS. REMOVE OLD DOUBLER, FABBED NEW REPAIR DOUBLERS AND FILLER P ER 53-2-1 FIG 7, INSTALLED PER DC8 SRM 51-1-21 AND DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002052100131 20020521 00131 WP 2002 5 21 UPS02838055 1 20020323 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 A/C COMPT AT FS 24 ABOVE LONG 35R FRAME IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LI MITS. FABBED REPAIR PART IAW DWG DC8-53A-0II. INSTALLED PART IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002052100132 20020521 00132 WP 2002 5 21 UPS02838056 1 20020325 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 STA 240 LONG 9R CRACKED. CUT OUT DAMAGED SECTION OF LONG & FABBED NEW SECTION IAW DAC DWG 5755 649-5 09 & DC8 SRM 53-2-2. INSTALLED SPLICES & NEW LONGERON SECTION IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002052100133 20020521 00133 WP 2002 5 21 UPS02838057 1 20020326 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 CABIN FLOORBOARD STA 1480-1580 POS NR 7 HAS SOFT SPOT. FABRICATED FLOOR PANEL IAW UPS EO DC8-5320-96 91C. 2 L 7 4 4F RT 4A25 2002052100134 20020521 00134 WP 2002 5 21 UPS02838058 1 20020326 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 FLOORBOARD STA 340-460 POS 7 SOFT SPOT. FABRICATED FLOOR PANEL IAW UPS EO DC8-5320-9691C. 2 L 7 4 4F RT 4A25 2002052100135 20020521 00135 WP 2002 5 21 UPS02838060 1 20020322 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 REMOVED STEEL DOUBLER FROM R1 DOOR UPPER FWD CORNER. FABBED DOUBLERS IAW DC8 SRM 53-2-0 FIG 14. REM OVED CRACK IAW DC8 SRM 53- 2-0 FIG 14. INSTALLED DOUBLERS & FILLER IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002052100136 20020521 00136 WP 2002 5 21 UPS02838061 1 20020323 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 RT APB CRACKED STA 1766 L11R. REPAIRED AREA IAW REO G08569. 2 L 7 4 4F RT 4A25 2002052100137 20020521 00137 WP 2002 5 21 UPS02838062 1 20020328 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 AFT PIT FS 1200 ZEE FITTING AT L34R - L33R IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D. LOCATE D & DRILLED NEW FITTING I AW DC8 SRM 51-1-24, INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002052100138 20020521 00138 WP 2002 5 21 UPS02838063 1 20020324 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 FRAME AT FS 720 AND BETWEEN L35L AND 36 IS CRACKED. REMOVED AND REPLACED DAMAGED FRAME SPLICES IAW D AC DWG 9753750. 2 L 7 4 4F RT 4A25 2002052100139 20020521 00139 WP 2002 5 21 UPS02838064 1 20020322 A 5210 SKIN DOUG DC8 DC871F 302199D WP L2 DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 REMOVED STEEL DOUBLER FROM L2 LOWER AFT CORNER. REMOVED DOUBLER, PERFORMED HFEC AND NO CRACKS NOTED. FABBED AND INSTALLED DOUBLER TRIPLER AND FILLER IAW REO G08571. SEALED AREA IAW DC8 SRM 51-1-11. 2 L 7 4 4F RT 4A25 2002052100140 20020521 00140 WP 2002 5 21 UPS02838078 1 20020417 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 L1 FWD ENTRY DOOR LWR AFT CORNER HAS CRACK INDICATION. ROUTED OUT CRACKS IN FUSELAGE SKIN & INNER DO UBLER IAW DC8 SRM 53-2-0 FIG 15. 2 L 7 4 4F RT 4A25 2002052100141 20020521 00141 WP 2002 5 21 UPS02838079 1 20020325 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 STA 320 LONG 7R CRACKED. REMOVED CRACKED LONGERON FAB NEW LONG & SPLICES IAW DC8 SRM 53-2-2 AND DAC DWG 5755649. INSTALLED NEW LONGERON AND SPLICES IAW DC8 SRM 51-1-20D & 53-2-2. 2 L 7 4 4F RT 4A25 2002052100142 20020521 00142 WP 2002 5 21 UPS02838080 1 20020324 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 KEEL BEAM FITTING RT AT STA 854 CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002052100143 20020521 00143 WP 2002 5 21 UPS02838081 1 20020321 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1 KEEL BEAM FITTING RT AT STA 854 CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002052100144 20020521 00144 2002 5 21 372PA0008 4 20020519 A 2230 AUTOTHRUST SYS BOEING 737 737306 NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 372PA 23546 Autothrottle disengaged in flight and could not be reset. Bite test OK 2 L 7 2 4F RT A16NE 2002052100145 20020521 00145 SO 2002 5 21 COMA0210020 1 20020519 A 7603 7898415008 EEC EMB 120 EMB120RT 3260202 SO ENGINE DEFECTIVE A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 269CA 1029 120263 FLIGHT 5023 DURING CLIMB OUT OF MCO THE #2 ENGINE POWER LEVER INPUT WAS IN EXCESS OF ONE INCH BEFORE IT TOOK EFFECT.REPL ACED THE #2 EEC. 2 L 7 2 4T RT A31SO 2002052100146 20020521 00146 EA 2002 5 21 COMA0260316 1 20020516 A 5311 6003603024 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS718.0 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 986CA 11526 7174 THE R/H SIDE FRAME AT FS 718 WAS CRACKED BETWEEN STR'S 10 AND 11.REMOVED THE CRACKED PORTION OF FRAME AND INSTALLED A NE W SECTION OF FRAME I/A/W REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2002052100147 20020521 00147 EA 2002 5 21 COMA0260317 1 20020520 A 5311 SKIN CNDAIR CL600 CL6002B19 1900309 EA FS235 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 986CA 11526 7174 NLG WHEEL WELL SKIN CUT OUT HAS A CRACK IN THE R/H CORNER APPROXIMATELY 3/8 IN. LONG.REMOVED THE CRACKED PORTION OF SKIN CUT OUT, PERFORMED LPI INSPECTION, FABED REPAIR PARTS AND INSTALLED I/A/W CANADAIR R.E.O 601R-53-11-048 REV A AND W.V.A .C.E.O. 601R-53-3253. 2 L 7 2 4F RT A21EA 2002052100148 20020521 00148 EA 2002 5 21 COMA0260318 1 20020518 A 3620 355924400 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA PYLON DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 916CA 7014 FLIGHT 5791 DURING CRUISE FLIGHT AT 28,000 FEET, RECEIVED A LEFT 14TH STAGE DUCT HIGH TEMPERATURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY AND DIVERTED TO IND FOR A SAFE LANDING.REPLACED THE LEFT PYLON TEMPERATURE SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2002052100149 20020521 00149 EA 2002 5 21 COMA0260319 1 20020518 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 978CA 7158 FLIGHT 5468 - DURING DECENT INTO AZO RECEIVED A FLAP FAIL CAUTION MESSAGE AT 43 DEGREE FLAP POSITION.COMPLIED WITH AD 98 -20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3 (A,B,C AND E). FLAP SYSTEM WAS RESET W ITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2002053000103 20020530 00103 NM 2002 5 30 2002UALA00861 1 20020512 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 STATION 325-365, RBL 70, WL 208 CREASE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. CREASE BEAM DAMAGE BLEND BETWEEN STAT ION 325-365. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000106 20020530 00106 NM 2002 5 30 2002UALA00863 1 20020511 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 EXTERNAL FUSELAGE SKIN LT SIDE STATION 623, BETWEEN STRINGER 15L AND 16L HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. BLE NDED CORROSION. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000110 20020530 00110 NM 2002 5 30 2002UALA00866 1 20020512 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 CABIN INTERCOSTAL CORRODED AT NUT PLATE HOLES, STATION 735, WL 208, LBL 66. MAJOR REPAIR ACCOMPLISHED. BLENDED CORROSI ON. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000114 20020530 00114 NM 2002 5 30 2002UALA00870 1 20020510 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 CABIN FLOOR INTERCOSTAL CORRODED ON UPPER SURFACE AT STATION 310 TO 324 RBL 40 STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW INTERCOSTAL U-CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000115 20020530 00115 NM 2002 5 30 2002UALA00871 1 20020510 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 LT CABIN FLOOR CREASE BEAM WEB CORRODED STATION 920 TO 940 LBL 58 STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED N EW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000116 20020530 00116 NM 2002 5 30 2002UALA00872 1 20020511 A 5347 SEAT TRACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 RIGHT I/B SEAT TRACK AT RBL 25 CORRODED STATION 680 TO STATION 700 ON I/B FLANGE. MAJOR REPAIR ACCOMPLISHED. SEAT TRAC K REPLACED FROM STA 620-700. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000119 20020530 00119 NM 2002 5 30 2002UALA00875 1 20020513 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 AFT PIT FRAME AT STATION 1600 IS DENTED BETWEEN STRINGER 25 AND 26R. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL DOU BLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000124 20020530 00124 NM 2002 5 30 2002UALA00880 1 20020514 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 FLIGHT DECK EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2002052100150 20020521 00150 NE 2002 5 21 COMA0260320 2 20020519 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE A COMA E ENGINE SHUTDOWN X ENGINE FLAMEOUT LD LANDING 1 SO 01 451CA 7562 FLIGHT 5740 DURING LANDING APPROACH INTO AZO THE AIRCRAFT ENCOUNTERED A LIGHTNING STRIKE RESULTING IN FLAMING OUT THE #1 ENGINE.PERFORMED A LIGHTNING STRIKE INSPECTION, REPAIRED MINOR AIRFRAME SKIN BURN MARKS AND PERFORMED SUCCESSFUL ENGINE RUNS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002052100151 20020521 00151 NE 2002 5 21 HNAA0200038 2 20020515 A 7321 7898425009 ECU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE Zone 400 FLUCTUATES A HNAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 EA 07 907HA 26137 314 011 120636 CREW REPORTED #2 ENGINE TORQUE BEGAN FLUCTUATING +/- 10-15%. WHEN #2 ECU WAS SELECTED OFF THE CONDITION STABILIZED BRIEF LY THEN #1 ENGINE TORQUE BEGAN FLUCTUATING +/- 5-10%. AIRCRAFT RETURNED TO DCA. MAINTENANCE FOUND THE #1 ENGINE ECU FLAG GED ON THE ENGINE CONDITION PANEL. REPLACED THE #1 ECU. 2 H 7 2 4T 4 T RT A13NM E20NE 2002052100152 20020521 00152 EA 2002 5 21 COMA0260321 1 20020518 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 430CA 7461 FLIGHT 6085 DURING CLIMB OUT OF LGA A HISSING SOUND EMANATED FROM THE LOWER RIGHT CORNER OF CABIN DOOR.REMOVED FOD BETWE EN CABIN DOOR SEAL AND DOOR SEAL NIB. 2 L 7 2 4F RT A21EA 2002052100153 20020521 00153 EA 2002 5 21 COMA0260322 1 20020518 A 2711 PULLEY CNDAIR CL600 CL6002B19 1900309 EA A COMA K NONE S AFFECT SYSTEMS CR CRUISE 1 SO 01 926CA 7027 FLIGHT 5707 DURING CRUISE FLIGHT THE AILERON CONTROLS FELT SLUGGISH, BUT CONTROLLABLE.INSPECTED AILERON TENSION REGULATO RS, PERFORMED A DETAILED INSPECTION OF EXPOSED AILERON AND AUTO PILOT MECHANISM CONTROL PATH. CLEANED THE LEFT AND RIGH T AILERON QUADRANTS AND PCU OUTPUT OF MOISTURE. 2 L 7 2 4F RT A21EA 2002052100154 20020521 00154 EA 2002 5 21 COMA0260323 1 20020518 A 2430 IDG CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 995CA 7229 FLIGHT 5268 DURING TAKE OFF ROLL RECEIVED AN IDG AND GENERATOR #1 MESSAGE, TAKE OFF WAS ABORTED AND RETURNED TO THE GATE .SERVICED THE #1 ENGINE IDG WITH OIL AND PERFORMED FUNCTIONAL CHECK, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002052100155 20020521 00155 EA 2002 5 21 COMA0260342 1 20020519 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 783CA 7315 FLIGHT 5812 DUIRNG PRE-FLIGHT CHECK FOUND THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE.PLACED EMERGENCY LIGHTING ON DEFERRED DISCREPANCY LIST PER MEL 66-51-02. 2 L 7 2 4F RT A21EA 2002052100156 20020521 00156 EA 2002 5 21 COMA0260324 1 20020519 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 783CA 7315 FLIGHT 5812 DUIRNG PRE-FLIGHT CHECK FOUND THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE.PLACED EMERGENCY LIGHTING ON DEFERRED DISCREPANCY LIST PER MEL 66-51-02. 2 L 7 2 4F RT A21EA 2002052100157 20020521 00157 NM 2002 5 21 ANCF200200010 1 20020516 A 2410 696233B CSD DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE RH ENGINE W ANCF D RETURN TO BLOCK M OVER TEMP CL CLIMB 1 SO 23 583AN 17398 17398 53183 DURING CLIMB RIGHT CSD OUTLET TEMP HIGH WAS PRESENTED, CHECK LIST WAS PERFORMED AND THE RIGHT CSD DOESN’T DISCONNECTED, ALSO THE A.P.U. DID NOT START AT THE AND ALTITUDE OF 20000. THE CREW DECIDED TO TURN BACK TO CTG THE RIGHT CSD OIL PRESS LOW ANN CAME ON TROUGH 10000 FT AND THE APU START AT THE 3TH ATTEMPT.CORRECTIVE ACTION:WAS TRANSFER TO DMI 202 MEL 24-1 -1 CAT B, IN ORDER TO CLOSE THAT DMI, THE CSD WAS REPLACED IAW AMM 24-10-01 PAGE 401 AND OIL COOLER WAS REPLACED IAW AMM 24-10-03 PAGE 201 RUN UP RH ENGINE TEST SATISFACTORY IAW AMM 71-00-00 2 L 7 2 4F 4 F RT E9NE 2002052100158 20020521 00158 EU 2002 5 21 MALA020289 1 20020518 A 3040 WINDSHIELD SAAB SF340 340B 7860101 EU A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 453XJ 340B453 DURING FLIGHT #2891, LH FWD WIND SHIELD HEAT INOP. CRACK BEGAN TO DEVELOP. AIR TURNBACK TO DTW. MAINTENANCE REPLACED LH FRONT WINDSHIELD IAW SF340 AMM CHAP 56, PLEASE REFER TO 409 # 152933. 2 L 7 2 4T RT A52EU 2002052100159 20020521 00159 NM 2002 5 21 NACA20020021 1 20020521 A 5710 65162343 SPAR CAP BOEING 727 72723 1384004 NM L/H WING CORRODED A NACA O OTHER O OTHER IN INSP/MAINT 1 AL 03 930FT 63198 19387 DISCREPANCY: During "C" inspection, I.G. corrosion was discovered on the L/H wing aft spar lower chord, from w.s. 224.5 TO w.s. 241.0.CORRECTIVE ACTION: Lower spar cap being replaced from LBL 70.5 to W.S. 259. 2 L 7 3 4F A3WE 2002052100160 20020521 00160 NM 2002 5 21 AWXA200200437 1 20020515 A 5315 6545402 ANGLE BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 0 0 22653 YVR - MAJOR REPAIR - DURING INSPECTION A CRACK WAS FOUND ON SUPPORT ANGLE BELOW FLOOR WEB, R/H WHEEL WELL, RBL 40. MAINT ENANCE REMOVED AND REPLACED CRACKED ANGLE AT R/H W/W , RBL 40 IAW B737-200 SRM 51-30-2, PG. 8. 2 L 7 2 4F RT A16WE 2002052100161 20020521 00161 SO 2002 5 21 LR7A02036 1 20020512 A 5330 SKIN LKHEED 382 382G 526414U SO FS 727 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 4590 DURING SCHEDULED A CHECK PER JOB CARD HA1200 FOUND RH FS 727 FUSELAGE SKIN ROCK DENTED AT RBL 64, WL 152. DURING REPAIR ACCOMPLISHMENT FOUND FS 727 FRAME DENTED AT SAME LOCATION.REPAIRED SKIN IAW SRM SMP 583 51-140-12 AND FRAME DENT IAW 51 -140-23. GMM133 ITEM M3. 2 H 7 4 4T A1SO 2002052100162 20020521 00162 CE 2002 5 21 GLBA2002061 1 20020514 A 5200 1294000971 SEAL BEECH 1900 1900D 1154162 CE CABIN DOOR TORN A GLBA D RETURN TO BLOCK O OTHER CL CLIMB 1 NM 03 184UX UE184 CABIN DOOR SEAL LEAKING, REPLACED SEAL OPS CHECKED SATISFACTORY 2 L 7 2 4T RT A24CE 2002052100163 20020521 00163 CE 2002 5 21 GLBA2002065 1 20020519 A 2820 A29001 HOSE BEECH 1900 1900D 1154162 CE LEFT ENGINE LEAKING A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 253GL UE253 LEFT FUEL LOW PRESSURE LIGHT ILLUMINATED, REPLACED HOSE ASSEMBLY 2 L 7 2 4T RT A24CE 2002052100164 20020521 00164 CE 2002 5 21 GLBA2002059 1 20020509 A 7930 503890451 SWITCH BEECH 1900 1900D 1154162 CE LEFT INOPERATIVE A GLBA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 03 151GL UE151 LEFT ENGINE OIL PRESSURE ANNUNICATOR ILLUMINATED REPLACED PRESSURE SWITCH 2 L 7 2 4T RT A24CE 2002052200001 20020522 00001 WP 2002 5 22 AALA20020338 1 20020323 A 3350 P4010049 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 555AN 53085 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L245-L246 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002052200002 20020522 00002 WP 2002 5 22 AALA20020344 1 20020319 A 5320 SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FOUND CORROSION ON F/B SUPPORT STATION 1212 L29R-L30. INSTALLED NEW FLOOR SUPPORT AT STATION 1212 L29R TO L30 SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2002052200003 20020522 00003 WP 2002 5 22 AALA20020345 1 20020312 A 5320 STIFFENER DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FOUND THE VERTICAL STIFFENER ON THE FORWARD SIDE OF AFT PRESS BULKHEAD ABOVE VAULT DOOR IS CRACKED. REMOVED CRACK ED STIFFENER AND INSTALLED NEW STIFFENER PER SRM 51-01-00. (M) 2 L 7 2 4F RT A6WE 2002052200004 20020522 00004 WP 2002 5 22 AALA20020346 1 20020312 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FOUND FRAME 1429 SHEAR TIE CRACKED 2 PLACES RIGHT AFT SIDE LONGERON 2 RT. INSTALLED NEW SHEAR TIE SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2002052200005 20020522 00005 WP 2002 5 22 AALA20020347 1 20020319 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 590AA 53253 TUL - FOUND FRAME AT STATION 1401 HAS DEEP GOUGE AT INSTRUMENT AIRLINE ATTACH POINT AT LONGERON 21 RT. INSTALLED REPAIR DOUBLER AT STATION 1401 PER SRM 53-03 PAGE 5. (M) 2 L 7 2 4F RT A6WE 2002052200006 20020522 00006 WP 2002 5 22 MWEA020333 1 20020521 A 5321 99365843 FLOORBOARD DOUG DC9 DC982 3022082 WP STATION 256 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FLOOR BOARD HEAVILY CORRODED, AS SEEN FROM FORWARD CARGO BAY STATION 256 JUST AFT OF CABIN FLOOR BEAM, RIGHT TUNNEL. -- FABRICATED AND INSTALLED FLOORBOARD. 2 L 7 2 4F A6WE 2002052200007 20020522 00007 WP 2002 5 22 MWEA020334 1 20020521 A 5321 9936583 FLOORBOARD DOUG DC9 DC982 3022082 WP STATION 700 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 CENTER AISLE FLOORBAORD AT APPROXIMATELY STATION 700 IS DAMAGED AT THE FORWARD LEFT. -- FABRICATED AND INSTALLED FLOOR BOARD. 2 L 7 2 4F A6WE 2002052200008 20020522 00008 WP 2002 5 22 MWEA020335 1 20020521 A 5321 99365853 FLOOR PANEL DOUG DC9 DC982 3022082 WP STATION 927 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FLOOR PANEL, FORWARD OUTBOARD CORNER DAMAGED, STATION 927, NEXT TO #1 SEAT TRACK. -- FABRICATED AND INSTALLED FLOORBOA RD. 2 L 7 2 4F A6WE 2002052200009 20020522 00009 WP 2002 5 22 MWEA020343 1 20020521 A 5321 99365499 FLOORBOARD DOUG DC9 DC982 3022082 WP STATION 161 DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FORWARD GALLEY DOOR FLOORBOARD DELAMINATED, STATION 161-200. -- FABRICATED AND INSTALLED FLOORBOARD. 2 L 7 2 4F A6WE 2002052200010 20020522 00010 WP 2002 5 22 MWEA020344 1 20020521 A 5321 99365533 FLOORBOARD DOUG DC9 DC982 3022082 WP STATION 200 DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 RIGHT FLOORBOARD PANEL DELAMINATED, STATION 200-256, OUTBOARD OF #3 SEAT TRACK. -- FABRICATED AND INSTALLED NEW FLOORB OARD. 2 L 7 2 4F A6WE 2002052200011 20020522 00011 WP 2002 5 22 MWEA020345 1 20020521 A 5321 99579211 FLOOR PANEL DOUG DC9 DC982 3022082 WP STATION 804 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 LEFT OUTBOARD FLOOR PANEL CRACKED ON INBOARD EDGE AT STATION 804. -- FABRICATED AND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F A6WE 2002052200012 20020522 00012 WP 2002 5 22 MWEA020347 1 20020521 A 5321 99365841 FLOORBOARD DOUG DC9 DC982 3022082 WP STATION 321 PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 RIGHT INBOARD FLOORBOARD AT STATION 320 HAS PUNCTURE AT FORWARD INBOARD SIDE. -- FABRICATED AND INSTALLED CORE PLUG AN D DOUBLER REPAIR. 2 L 7 2 4F A6WE 2002052200013 20020522 00013 WP 2002 5 22 MWEA020352 1 20020521 A 5321 99328162 FLOOR PANEL DOUG DC9 DC982 3022082 WP STATION 256 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 CABIN FLOOR PANEL HEAVILY CORRODED, STATION 256, OUTBOARD OF #4 SEAT TRACK. -- FABRICATED AND INSTALLED DOUBLER AND FI LLER. 2 L 7 2 4F A6WE 2002052200014 20020522 00014 WP 2002 5 22 MWEA020353 1 20020521 A 5321 99365831 FLOOR PANEL DOUG DC9 DC982 3022082 WP STATION 864 PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 CABIN FLOOR PANEL PUNCTURED, STATION 864, BETWEEN #3 AND #4 SEAT TRACKS. -- FABRICATED AND INSTALLED FLOOR BOARD. 2 L 7 2 4F A6WE 2002052200015 20020522 00015 WP 2002 5 22 MWEA020354 1 20020521 A 5321 99579211 FLOOR PANEL DOUG DC9 DC982 3022082 WP STATION 870 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FLOOR PANEL CRACKED, STATION 870, NEXT TO #1 SEAT TRACK. -- FABRICATED AND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F A6WE 2002052200016 20020522 00016 WP 2002 5 22 MWEA020355 1 20020521 A 5321 99365851 FLOOR PANEL DOUG DC9 DC982 3022082 WP STATION 708 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FLOOR PANEL CRACKED, STATION 708, NEXT TO #SEAT TRACK. -- FABRICATED AND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F A6WE 2002052200017 20020522 00017 WP 2002 5 22 MWEA020356 1 20020521 A 5321 99365851 FLOOR PANEL DOUG DC9 DC982 3022082 WP STATION 701 PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FLOOR PANEL PUNCTURED, STATION 701, NEXT TO #1 SEAT TRACK. -- FABRICATED AND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F A6WE 2002052200018 20020522 00018 WP 2002 5 22 MWEA020358 1 20020521 A 5320 99177013 INTERCOSTAL DOUG DC9 DC982 3022082 WP STATION 1497 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 AFT ACCESSORY INTERCOASTAL IS BENT LOCATED BETWEEN CANTED FRAMES 1497 AND 1510 LEFT SIDE. -- FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2002052200019 20020522 00019 WP 2002 5 22 MWEA020359 1 20020521 A 5321 9957918501 FLOOR PANEL DOUG DC9 DC982 3022082 WP STATION 916 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FLOOR PANEL CRACKED, STATION 916, NEXT TO #1 SEAT TRACK. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002052200020 20020522 00020 WP 2002 5 22 MWEA020361 1 20020521 A 5321 99365477 FLOORBOARD DOUG DC9 DC982 3022082 WP STATION 180 DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FORWARD GALLEY FLOOR BAORD DELAMINATED, STATION 180-200. -- FABRICATED AND INSTALLED FLOOR BOARD. 2 L 7 2 4F A6WE 2002052200021 20020522 00021 WP 2002 5 22 MWEA020363 1 20020521 A 5321 99365461 FLOOR PANEL DOUG DC9 DC982 3022082 WP STATION 160 DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FLOOR PANEL FROM STATION 160 TO STATION 200, LEFT BUTT LINE 6 TO RIGHT BUTT LINE 6, IS DELAMINATED ALONG ITS FORWARD EDG E. -- FABRICATED AND INSTALLED FLOOR PANEL. 2 L 7 2 4F A6WE 2002052200022 20020522 00022 WP 2002 5 22 MWEA020364 1 20020521 A 5321 993653923 FLOORBOARD DOUG DC9 DC982 3022082 WP STATION 160 DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FLOORBOARD FROM STATION 148 TO STATION 160 RIGHT BUTT LINE 30 TO RIGHT BUTT LINE 45 REMOVED DUE TO DELAMINATION. -- FA BRICATED AND INSTALLED FLOORBOARD. 2 L 7 2 4F A6WE 2002052200023 20020522 00023 WP 2002 5 22 MWEA020365 1 20020521 A 5312 991224617 WEB DOUG DC9 DC932 3022066 WP STATION 1038 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT ACCESSORY COMPARTMENT BULKHEAD WEB AT FRAME STATION 1038 IS CRACKED AT LIGHTNING HOLE AT LONGERON 12 LEFT. -- FABR ICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002052200024 20020522 00024 WP 2002 5 22 MWEA020367 1 20020521 A 5712 59148658 FITTING DOUG DC9 DC932 3022066 WP STATION 606 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CENTER WING FORWARD LOWER BULKHEAD FITTING CRACKED AT STATION 606 AND LONGERON 24 RIGHT. -- REMOVED AND INSTALLED FITT ING. 2 L 7 2 4F A6WE 2002052200025 20020522 00025 WP 2002 5 22 MWEA020369 1 20020521 A 5310 591140911 LONGERON DOUG DC9 DC932 3022066 WP STATION 484 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 LONGERON 17 RIGHT IS CRACKED UNDER FRAME 484. -- FABRICATED AND INSTALLED LONGERON SECTION AND REPAIR SPLICE. 2 L 7 2 4F A6WE 2002052200026 20020522 00026 WP 2002 5 22 MWEA020371 1 20020521 A 5313 591140511 LONGERON DOUG DC9 DC982 3022082 WP STATION 207 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 LONGERON 5 LEFT HAS A UNFILLED HOLE. LOOKS LIKE A MISS DRILL DURING INSTALL STATION 207. -- FABRICATED AND INSTALLED R EPAIR DOUBLER. 2 L 7 2 4F A6WE 2002052200027 20020522 00027 WP 2002 5 22 AALA20020353 1 20020220 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE TORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND TORN CUSP AT STATION 237 LEFT. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002052200028 20020522 00028 WP 2002 5 22 AALA20020354 1 20020219 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND .125 INCH CRACK IN CUSP STATION 220 LEFT SIDE. INSTALLED NEW CUSP SHEET STATION 218-237 SRM 51-01. (M) 2 L 7 2 4F A6WE 2002052200029 20020522 00029 WP 2002 5 22 AALA20020364 1 20020325 A 3260 39281375001 UPLOCK SENSOR DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 480AA 49655 ORD - FLT 9689 - NOSE LANDING GEAR WOULD NOT RETRACT LANDED ORD WITHOUT INCIDENT. SWUNG GEAR 7-8 TIMES, COULD NOT DUPLI CATE ON GROUND. NEXT DAY REPEAT CONDITION. REPLACED NOSE GEAR UP SENSOR AND LOCK SENSOR, PROXIMITY BOX, AND NOSE GEAR BUNGEE NOSE LANDING GEAR. CONDUCTED FERRY FLIGHT AND NOSE LANDING GEAR DID NOT RETRACT, INDICATOR PIN RELEASED NOSE LAN DING GEAR LIGHT ON. NOISE AND VIBRATION INDICATED GEAR WAS EXTENDED OR GEAR DOORS OPEN. MADE 2 ATTEMPTS TO RETRACT. L ANDED ORD WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR RETRACT ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002052200030 20020522 00030 WP 2002 5 22 AALA20020369 1 20020328 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 474 49649 DFW - DURING OVERNIGHT MAINTENANCE, FOUND LEFT SIDE FUSELAGE SKIN DAMAGED BETWEEN STATIC PORTS. REQUIRED MAJOR REPAIR O F AREA BETWEEN CABIN PRESSURE RELIEF VALVES. REPLACED DAMAGE SKIN, ACCOMPLISHED FLUSH REPAIR WITH DOUBLERS. SYSTEMS GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002052200031 20020522 00031 NM 2002 5 22 AALA20020370 1 20020401 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 315AA 22317 BOS - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS AT SEAT 11B FOUND INOPERATIVE. RECONNECTED CONNECTOR FOUND ON INBOARD SIDE OF SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002052200032 20020522 00032 NM 2002 5 22 AALA20020371 1 20020402 A 2560 P2070003001 FLASHLIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 336AA 22334 BOS - DURING OVERNIGHT MAINTENANCE, FOUND MID GALLEY RIGHT FORWARD SEAT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLAS HLIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002052200033 20020522 00033 NM 2002 5 22 AALA20020372 1 20020302 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH EXIT LIGHTS AT SEAT 2H FOUND INOPERATIVE. REPLACED SEAT MOUNT ED EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002052200034 20020522 00034 WP 2002 5 22 AALA20020391 1 20020320 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7535A 49989 TUL - FOUND RIGHT CUSP AT STATION 869 PUNCTURED. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2002052200035 20020522 00035 WP 2002 5 22 AALA20020392 1 20020328 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7535A 49989 TUL - FOUND CORROSION ON UPPER ANGLE AFT SIDE OF FLOORBEAM STATION 160 RBL 12. INSTALLED FLOORBEAM TEE CAP REPAIR ON TO P SIDE OF FLOORBEAM STATION 160 FROM RBL 1 TO RBL 18 PER 53-05 FIG 20B SHEET 2. (M) 2 L 7 2 4F A6WE 2002052200036 20020522 00036 WP 2002 5 22 AALA20020393 1 20020322 A 5510 WEB DOUG DC9 DC982 3022082 WP HORIZONTAL STAB PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7535A 49989 TUL - FOUND PUNCTURE IN WEB OF RIGHT HORIZONTAL BETWEEN AFT SPARS. INSTALLED DOUBLER REPAIR PER ESO 80559 3/21/02. (M) 2 L 7 2 4F A6WE 2002052200037 20020522 00037 WP 2002 5 22 AALA20020394 1 20020325 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7535A 49989 TUL - FOUND DEEP GOUGE ON FUSELAGE SKIN LONGERON 18L AT APPROX STATION 252 APPROX .5 INCH LONG. CUT OUT DAMAGE PER 53-0 4 FIG 38. INSTALLED DOUBLER SRM 53-04 FIG 38 AND AARD 53-30-08.9. (M) 2 L 7 2 4F A6WE 2002052200038 20020522 00038 WP 2002 5 22 AALA20020395 1 20020325 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND DENT AND CRACK ON LEFT CUSP AT STATION 263. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2002052200039 20020522 00039 WP 2002 5 22 AALA20020396 1 20020404 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7535A 49989 TUL - FOUND CORROSION ON AFT CARGO DOOR FRAME LOWER BEAM SEVERAL AREAS. INSTALLED DOUBLER PER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2002052200040 20020522 00040 WP 2002 5 22 AALA20020397 1 20020404 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7535A 49989 TUL - FOUND CORROSION ON FLOORBOARD SUPPORT STATION 148 RBL 8. INSTALLED NEW FLOORBOARD SUPPORT AT STATION 148 RBL 8 SR M 51-01. (M) 2 L 7 2 4F A6WE 2002052200041 20020522 00041 WP 2002 5 22 AALA20020398 1 20020404 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7535A 49989 TUL - FOUND FLOORBOARD SUPPORT CORRODED WITH DEEP CUT BETWEEN NR 2/3 SEAT TRACKS. INSTALLED NEW FLOORBOARD SUPPORT SRM 51-01. (M) 2 L 7 2 4F A6WE 2002052200042 20020522 00042 WP 2002 5 22 AALA20020399 1 20020326 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7535A 49989 TUL - FOUND STATION 1184-1205 SEAT TRACK NR 2 CORRODED, OUT OF LIMITS. REMOVED AND REPLACED RN 2 SEAT TRACK PER SRM 53- 05 FIG 4F. (M) 2 L 7 2 4F A6WE 2002052200043 20020522 00043 WP 2002 5 22 AALA20020400 1 20020325 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7535A 49989 TUL - FOUND CORROSION ON CUSP, EMITTING FROM UNDER NR 1 SEAT TRACK STATION 1175. CUT OUT AFFECTED AREA AND INSTALLED DO UBLER REPAIR PER SRM 53-01 PAGE 18. (M) 2 L 7 2 4F A6WE 2002052200044 20020522 00044 WP 2002 5 22 AALA20020401 1 20020319 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 TUL - FOUND FORWARD SERVICE DOOR FRAME DAMAGED AT LOWER FORWARD CORNER, HOLE GOUGED IN LOWER DOOR PAN. REPLACED ENTIRE DOOR PAN ON E58'S NR 4208140, 9142105, 9109005 SRM REF 53-05-00/53-10-3/51-20, 51-30 AND 51-60. (M) 2 L 7 2 4F A6WE 2002052200045 20020522 00045 WP 2002 5 22 AALA20020402 1 20020313 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 TUL - FOUND CORROSION REMOVAL OUT OF LIMITS. SEAT TRACK REPLACED STATION 795-1032, 53-40-01-02 MM. (M) 2 L 7 2 4F A6WE 2002052200046 20020522 00046 WP 2002 5 22 AALA20020403 1 20020312 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 TUL 0 FOUND CORROSION REMOVAL BEYOND LIMITS. REPLACED NR 1 SEAT TRACK PER MM 53-40-01-02 STATION 1174-1308. (M) 2 L 7 2 4F A6WE 2002052200047 20020522 00047 WP 2002 5 22 AALA20020404 1 20020314 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 TUL - FOUND CORROSION REMOVAL OUT OF LIMITS. SEAT TRACK REPLACED MM 53-40-01-2. (M) 2 L 7 2 4F A6WE 2002052200048 20020522 00048 WP 2002 5 22 AALA20020405 1 20020318 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 TUL - FOUND FUSELAGE SKIN DENTED STATION 408 L30R/L29R. COLD WORKED DENT OUT THEN DYE CHECKED AREA. NO CRACKS FOUND. INSTALLED PERMANENT REPAIR DOUBLER PER SRM 53-04 PAGE 218H. (M) 2 L 7 2 4F A6WE 2002052200049 20020522 00049 WP 2002 5 22 AALA20020406 1 20020315 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND CORROSION ON NR 2 SEAT TRACK. INSTALLED SEAT TRACK PLUG STATION 1200 SRM 53-05-00. (M) 2 L 7 2 4F A6WE 2002052200050 20020522 00050 WP 2002 5 22 AALA20020407 1 20020315 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND CORROSION IN TRACK NR 6. INSTALLED SEAT TRACK PLUGS TRACK 6 STATION 655 AND 672, REF 53-20-00-10. (M) 2 L 7 2 4F A6WE 2002052200051 20020522 00051 NM 2002 5 22 2002UALA00881 1 20020514 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 CEILING EMERG EXIT LIGHT INOP AT 12A,B AND 17 A,B. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2002052200052 20020522 00052 WP 2002 5 22 AALA20020408 1 20020315 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND CORROSION IN SEAT TRACK. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2002052200053 20020522 00053 WP 2002 5 22 AALA20020409 1 20020315 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND CORROSION IN TRACK 1. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2002052200054 20020522 00054 WP 2002 5 22 AALA20020411 1 20020318 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND CENTER STIFFENER ABOVE VAULT DOOR HAS CRACK AT UPPER HI-LOCK. INSTALLED DOUBLER ON CENTER STIFFENER ABOVE V AULT DOOR PER SRM 53-01 PAGE 10. (M) 2 L 7 2 4F A6WE 2002052200055 20020522 00055 WP 2002 5 22 AALA20020412 1 20020318 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND SURFACE CORROSION ON CUSP. INSTALLED DOUBLER PER SRM 53-01-00 FIG 4. (M) 2 L 7 2 4F A6WE 2002052200056 20020522 00056 WP 2002 5 22 AALA20020413 1 20020318 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FUSELAGE SKIN DENTED FROM INSIDE STATION 584 APPROX 2 INCHES ABOVE LONGERON 25L. INSTALLED DOUBLER PER SRM 53-04 FIG 38 PAGE 218H. (M) 2 L 7 2 4F A6WE 2002052200057 20020522 00057 WP 2002 5 22 AALA20020414 1 20020318 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND GOUGE IN FUSELAGE STATION 1418 LONGERON 5L. INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3 PAGE 9. (M) 2 L 7 2 4F A6WE 2002052200058 20020522 00058 WP 2002 5 22 AALA20020415 1 20020319 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND CORROSION IN NR 1 SEAT TRACK. INSTALLED SERVICEABLE SEAT TRACK PLUG AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2002052200059 20020522 00059 WP 2002 5 22 AALA20020416 1 20020319 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND CORROSION NR 6 SEAT TRACK. INSTALLED SEAT TRACK PLUG STATION 826 TREATED AND PRIMED REF 53-20-00-10. (M) 2 L 7 2 4F A6WE 2002052200060 20020522 00060 WP 2002 5 22 AALA20020417 1 20020321 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND CORROSION AT SEAT TRACK NR 1 STATION 1208 AND 1237. REPLACED SEAT TRACK, STATION 1176 TO STATION 1309 PER S RM 51-30. (M) 2 L 7 2 4F A6WE 2002052200061 20020522 00061 WP 2002 5 22 AALA20020418 1 20020321 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND CRACK AT UPPER AFT CORNER OF WINDOW RING PAN, STATION 1079 LEFT SIDE. STOP DRILLED CRACK AND INSTALLED DOUB LER PER AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2002052200062 20020522 00062 WP 2002 5 22 AALA20020419 1 20020321 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND CRACK ON AFT UPPER CORNER OF WINDOW RING PAN STATION 1060 LEFT SIDE. STOP DRILLED, INSTALLED DOUBLER PER AA RD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2002052200063 20020522 00063 WP 2002 5 22 AALA20020420 1 20020326 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND CRACK IN FORWARD LOWER CORNER OF WINDOW RING PAN LEFT SIDE STATION 984. INSTALLED DOUBLER PER AARD 53-10-00 -25. (M) 2 L 7 2 4F A6WE 2002052200064 20020522 00064 WP 2002 5 22 AALA20020421 1 20020318 A 5300 5936038501 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND DOOR BEAM HAS SEVERAL AREAS OF CORROSION. INSTALLED FULL LENGTH DOUBLER PER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2002052200065 20020522 00065 WP 2002 5 22 AALA20020422 1 20020315 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 TUL - FOUND SCRATCH AT STATION 427 BETWEEN LONGERON 20-21R, JUST AFT OF DOOR. UPGRADED EXISTING CLASS III INTERIOR REPA IR TO CLASS I PERMANENT REPAIR DOUBLER REF SRM 53-04 FIG 12B VIEW D. (M) 2 L 7 2 4F A6WE 2002052200066 20020522 00066 WP 2002 5 22 MEX2002014 1 20020115 A 2824 107226B VALVE DOUG DC9 DC982 3022082 WP CROSSFEED FAILED A ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 501AM 6001 49188 FLT 587 - MEX-CUN - DURING MAINTENANCE INSPECTION MECHANIC REPORTED A FUEL LEAK BY THE DRAIN OF THE RIGHT WING FORWARD S PAR. ACCESS OPENED, FOUND THE MENTIONED LEAK IN THE FUEL CROSSFEED VALVE. CROSS FEED VALVE WAS CHANGE IAW MM 28-20-12, TESTS OK. AT MEX RON 15/16, WAS RE-CHECKED THE REPLACEMENT, EVERYTHING WAS OK. (M) 2 L 7 2 4F A6WE 2002052200067 20020522 00067 NM 2002 5 22 QXEA0200770 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 1 SEAT TRACK IS CORRODED ON INNER SURFACES. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052200068 20020522 00068 NM 2002 5 22 QXEA0200771 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 1 SEAT TRACK CORRODED ON INNER SURFACES AT STATION X404 - X406. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052200069 20020522 00069 WP 2002 5 22 UPS02838082 1 20020416 A 5320 559764631 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C1, L1 DOOR JAMB INTERCOSTAL IS CRACKED ON BOTH ENDS. FABBED NEW INTERCOSTAL IAW DAC DWG 5597646. INST ALLED DOOR PANS AND INTERCOSTAL IAW DC8 SRM 51-1-20D, 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 2002052200070 20020522 00070 WP 2002 5 22 UPS02838092 1 20020426 A 3350 CONNECTOR DOUG DC8 DC871F 302199D WP CABIN BURNED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS REMAINED ON. FOUND BURNT CONTACTS ON CANNON PLUGS. AIRCRAFT 779 COVERED FLIG HT PARTS ON ORDER. 2 L 7 4 4F RT 4A25 2002052200071 20020522 00071 WP 2002 5 22 UPS02838099 1 20020426 A 3397 WIRE DOUG DC8 DC871F 302199D WP COCKPIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS REMAINED ON AFTER SWITCHING TO SHIPS POWER. REPAIRED BROKEN WIRE AT EMERGENCY BATTERY PACK CANNON PLUG, OPS CHECK GOOD PER MM 33-50-02. 2 L 7 4 4F RT 4A25 2002052200072 20020522 00072 WP 2002 5 22 UPS02838100 1 20020430 A 3350 CONNECTOR DOUG DC8 DC871F 302199D WP COCKPIT NOT SEATED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:N/A DURING PREFLIGHT FOUND EMERGENCY LIGHT DISARM ARM SWITCH LIGHT DID NOT WORK. FOUND CONNECTOR P1-134 4 AT DIMMING BOX B5-60 NOT FULLY SEATED. SEATED CONNECTOR P1-1344 LIGHT OPS CK NORMAL REF WDM 33-50-01. 2 L 7 4 4F RT 4A25 2002052200073 20020522 00073 NM 2002 5 22 UPS02M37960 1 20020329 A 5320 STRUCTURE DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP INSPECTION TYPE:N/A CORROSION FOUND UNDER SM RAIL IN FWD LWR PIT DOOR SILL AREA. ACCOMPLISHED INTERIM REPAIR AS PER EO MD11-5310-16522-A. PERMANENT REPAIR TO BE ACCOMPLISHED DURING MAJOR MAINTENANCE VISIT. 2 L 7 3 4F RT A22WE 2002052200074 20020522 00074 NM 2002 5 22 UPS02M37968 1 20020330 A 5310 DOOR FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP INSPECTION TYPE:PS5 AFTER REMOVAL OF BRACKET ASSY FWD LWD PIT CARGO DOOR, FWD BRACKET ASSY CORROSION WAS FOUND AROUND NU T PLATE WITH PAN HEAD FASTENER. REMOVED CORROSION ON OUTER FRAME IAW EO MD11-5310-16524-A. 2 L 7 3 4F RT A22WE 2002052200075 20020522 00075 WP 2002 5 22 ZW0A0203101 1 20020313 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 941AS 49925 DURING CHECK-C MAINT FOUND CORROSION IN FLOOR SUPPORT FLANGES FROM STATION 160 TO 200, RBL 43. INSTALLED NEW FABRICATED SUPPORT AT STA 160 TO 200, PER SPM 6-70-01. 2 L 7 2 4F A6WE 2002052200076 20020522 00076 WP 2002 5 22 ZW0A0203102 1 20020312 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT IN AFT CABIN FOUND CORROSION ON FLOOR SUPPORT AT STA 1320, LONGERON 23L TO 23R. INSTALLED NEW FLOO R SUPPORT PER SPM 6-70-01, 4B. 2 L 7 2 4F A6WE 2002052200077 20020522 00077 WP 2002 5 22 ZW0A0203103 1 20020308 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT FOUND PILOTS AFT INBD SEAT TRACK WAS CORRODED. REMOVED AND REPLACED TRACK PER SRM 51-01, PAGE 1, I TEM C. 2 L 7 2 4F A6WE 2002052200078 20020522 00078 WP 2002 5 22 ZW0A0203104 1 20020308 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT FOUND CORROSION ON CAPTAINS KICKPLATE BULKHEAD AND FLOOR PANEL SUPPORT. REMOVED CORROSION PER SPM 6-80-01. FABRICATED NEW SUPPORT AND INSTALLED PER SRM 51-30-5. 2 L 7 2 4F A6WE 2002052200079 20020522 00079 WP 2002 5 22 ZW0A0203105 1 20020306 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT IN THE AFT CABIN AND CARGO BIN, THE FORMER RING WAS CORRODED AT STA 1271, LONGERON 27L TO 29R. INS TALLED NEW Z FRAME FROM LBL 37 TO RBL 11, PER SRM 53-02, FIG 2. 2 L 7 2 4F A6WE 2002052200080 20020522 00080 WP 2002 5 22 ZW0A0203106 1 20020306 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 6 RH O/B SEAT TRACK, FROM STA 256 TO 313. REPLACED SECTION OF SEAT TRACK USING SEAT TRACK SPLICE AT STA 421. TRACK CHANGED FROM STA 214 TO 421, PER SRM 53-05, PAGE 104. 2 L 7 2 4F A6WE 2002052200081 20020522 00081 NM 2002 5 22 ZW0A0203202 1 20020318 A 1420 SPLICE BOEING 757 7572Q8 1384972 NM CABIN DAMAGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 701TW 28160 THE EGRESS LIGHT AT CABIN ROW 12 WAS INOPERATIVE. REPAIRED THE SPLICE AT ROW 12. 2 L 7 2 4F RT A2NM 2002052200082 20020522 00082 WP 2002 5 22 ZW0A0203301 1 20020314 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT THE INTERCOSTAL WAS CORRODED AT STA 1308 TO 1322, BETWEEN LONGERON 27 AND 28, LT SIDE. DRILLED NEW INTERCOSTAL AND END FITTINGS AND INSTALLED PER SRM 51-30-2 AND 5, AND SPM 6-70-01. 2 L 7 2 4F A6WE 2002052200083 20020522 00083 WP 2002 5 22 ZW0A0203302 1 20020314 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT THE LT FLOOR TRACK IN THE AFT CARGO COMPARTMENT WAS CORRODED FROM STA 1211 TO 1320. INSTALLED NEW TRACK IN CARGO COMPARTMENT, LT SIDE, AND INSTALLED SPLICE PLATE PER SRM 53-05, FIG 4G. 2 L 7 2 4F A6WE 2002052200084 20020522 00084 WP 2002 5 22 ZW0A0203303 1 20020314 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 914TW 49185 DURING CHECK-C MAINT THE FORMER RING AND REPAIR WERE CORRODED AT STA 1309, LONGERON 27R TO 27L. REMOVED AND INSTALLED N EW FRAME AND INSTALLED REPAIR SPLICES PER SRM 53-03, FIG 2A. 2 L 7 2 4F A6WE 2002052200085 20020522 00085 NM 2002 5 22 ZW0A0203401 1 20020220 A 1420 SPLICE BOEING 757 757231 1384950 NM CABIN DAMAGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 705TW 28479 EGRESS LIGHTING AT S LAVATORY INOP. REPAIRED SPLICE IN EGRESS LIGHT STRIP AT S LAVATORY. 2 L 7 2 4F RT A2NM 2002052200086 20020522 00086 WP 2002 5 22 ZW0A0203501 1 20020322 A 3350 58203 SIGN DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 950U 49230 AFT STAIR EGRESS EXIT SIGN INOP. REPLACED EGRESS EXIT SIGN. 2 L 7 2 4F A6WE 2002052200087 20020522 00087 WP 2002 5 22 ZW0A0203502 1 20020325 A 4930 36011932 CAP DOUG DC9 DC983 3022083 WP APU LEAKING A ZW0A K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 13 9621A 53592 FUEL SMELL IN AIRCRAFT CABIN. REMOVED AND REPLACED LEAKING RUBBER CAP ON ATOMIZER IN APU COMBUSTION CHAMBER. 2 L 7 2 4F RT A6WE 2002052200088 20020522 00088 NM 2002 5 22 ZW0A0203902 1 20020327 A 5753 SKIN BOEING 757 757231 1384950 NM T/E FLAP CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 715TW 28483 DURING CHECK-C MAINT THE LT WING OTBD T/E FOREFLAP HAD 6 INCH LONG CRACK IN THE LOWER SURFACE, NEXT TO THE OTBD END. IN STALLED NEW PANEL PER SRM 51-10-02. 2 L 7 2 4F RT A2NM 2002052200089 20020522 00089 NM 2002 5 22 ZW0A0204101 1 20020407 A 3350 CONNECTOR BOEING 767 76733AER 1385230 NM CABIN LOOSE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 637TW 25403 THE EGRESS LIGHTS WERE INOPERATIVE ON LT SIDE OF CABIN ROWS 2 THROUGH 6. SEATED LOOSE CONNECTOR AT THE POWER SUPPLY. 2 L 7 2 4F RT A1NM 2002052200090 20020522 00090 WP 2002 5 22 ZW0A0204102 1 20020405 A 3350 408822101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST NR NOT REPORTED 1 CE 13 914TW 49185 THE EMERGENCY EVACUATION LIGHTS IN THE CABIN WERE ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. REPLACED THE BATTERI ES IN THE POWER SUPPLY. 2 L 7 2 4F A6WE 2002052200091 20020522 00091 NM 2002 5 22 ZW0A0204201 1 20020406 A 2910 HYDRAULIC LINE BOEING 717 717200 1383700 NM RT ENGINE CHAFED A ZW0A O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 13 418TW 55085 THE RT HYDRAULIC SYSTEM DROPPED TO 1.5 GALLONS. REPLACED THE RT ENGINE HYDRAULIC PRESSURE LINE FROM PUMP TO BULKHEAD FI TTING DUE TO A WORN SPOT. 2 L 7 2 4F TR A6WE 2002052200092 20020522 00092 NM 2002 5 22 ZW0A0204301 1 20020417 A 3350 CONNECTOR DOUG MD80 MD83 3023681 NM CABIN LOOSE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 951TW 53470 THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. RECONNECTED LOOSE CONNECTION. 2 L 7 2 4F RT 2002052200093 20020522 00093 WP 2002 5 22 ZW0A0204401 1 20020411 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9407R 49400 DENT FOUND IN FUSELAGE SKIN, 24 INCHES AFT OF FWD PASSENGER DOOR JAMB BELOW WINDOW BELT DOUBLER MOD. INSTALLED FLUSH DO UBLER PER ARA 17961. 2 L 7 2 4F RT A6WE 2002052200094 20020522 00094 NM 2002 5 22 ZW0A0204402 1 20020412 A 5330 SKIN BOEING 767 7673Y0 NM FUSELAGE DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 639TW 26208 DENT FOUND DURING ERPC AT STATION 1422, STRINGER 34L TO STRINGER 36L. REPAIRED DENT PER ARA 17962. 2 L 7 2 4F RT A1NM 2002052200095 20020522 00095 NM 2002 5 22 ZW0A0204601 1 20020422 A 3350 80741 LIGHT BOEING 767 7673Y0 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 639TW 26208 THE EGRESS LIGHT WAS INOPERATIVE AT SEATS 17AB AND 33AB. REPLACED THE LAMP AT BOTH LOCATIONS. 2 L 7 2 4F RT A1NM 2002052200096 20020522 00096 NM 2002 5 22 ZW0A0204602 1 20020420 A 3350 CONNECTOR BOEING 767 76733AER 1385230 NM CABIN NOT SEATED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 637TW 25403 THE EGRESS LIGHT WAS INOPERATIVE AT THE AFT RT DOOR, AND THE RT OUTSIDE EMERGENCY EXIT LIGHT, WERE INOPERATIVE. SEATED THE CONNECTOR AT BOTH POWER SUPPLIES. 2 L 7 2 4F RT A1NM 2002052200097 20020522 00097 WP 2002 5 22 ZW0A0204604 1 20020423 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 914TW 49185 THE EGRESS LIGHTING ROWS 7 TO 15 WERE INOPERATIVE. RESET THE CONNECTORS. 2 L 7 2 4F A6WE 2002052200098 20020522 00098 NM 2002 5 22 ZW0A0204605 1 20020416 A 5330 SKIN BOEING 757 757231 1384950 NM FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 721TW 29954 DURING CHECK-C MAINT FOUND INTERIM FUSELAGE SKIN REPAIR INSTALLED AT STA 405, BETWEEN STRINGER 10 AND 11 LEFT. ACCOMPLI SHED EMLR 71586 AND INSTALLED PERMANENT REPAIR PER SRM 53-00-01, FIG 204. 2 L 7 2 4F RT A2NM 2002052200099 20020522 00099 NE 2002 5 22 MEX2002015 2 20020118 A 7297 WIRE HARNESS BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A ASMF E ENGINE SHUTDOWN A J FLAME/FIRE WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 803AM 26268 FLT 239 - GDL-MEX - CREW REPORTED THAT DURING THE ENGINE STARTING, THE ENGINE 1 WAS NOT STABILIZED, THE RPM'S REMAINED A T 42 PERCENT AND MAINTENANCE AREA REPORTED THE PRESENCE OF FLAME IN SUCH ENGINE. AT CHECKING IT WAS FOUND A DAMAGE IN T HE WIRE BUNDLE NEAR PYLON, IT WAS REPAIRED, TEST OK. AT RON MEX 18/19 THE WIRE BUNDLE WAS RE-CHECKED IAW WDM 81-11-11, EVERYTHING OK. (M) 2 L 7 2 4F 4 F RT A2NM E17NE 2002052200100 20020522 00100 WP 2002 5 22 ZW0A0204606 1 20020307 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 967TW 53617 DURING CHECK-C MAINT FOUND CORROSION AROUND E/E COMPARTMENT DOOR FRAME. REMOVED AND REPLACED DOOR PAN STRUCTURE. 2 L 7 2 4F RT A6WE 2002052200101 20020522 00101 WP 2002 5 22 ZW0A0204701 1 20020502 A 2910 B-NUT DOUG DC9 DC983 3022083 WP HYD SYSTEM LOOSE A ZW0A O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 13 972TW 53622 THE LEFT HYDRAULIC SYSTEM FAILED. TIGHTENED A LEAKING B-NUT AT THE LEFT ENGINE THRUST REVERSER CONTROL VALVE. 2 L 7 2 4F RT A6WE 2002052200103 20020522 00103 NM 2002 5 22 ZW0A0204801 1 20020503 A 3397 WIRE BOEING 767 7673Y0 NM CABIN DAMAGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 639TW 26208 THE EGRESS LIGHTS WERE INOPERATIVE BELOW THE JUMPSEAT AT THE LEFT SIDE NUMBER 1 CABIN DOOR AND THE RT SIDE NUMBER 1 CABI N DOOR. REPAIRED WIRES AT THE EGRESS LIGHTS AT THE L1 AND R1 DOORS. 2 L 7 2 4F RT A1NM 2002052200104 20020522 00104 WP 2002 5 22 ZW0A0205001 1 20020507 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE SEVERED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9621A 53592 DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT, LONGERON 30 WAS FOUND SEVERED AT STA 1219. REPLACED LONGERON PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2002052200105 20020522 00105 WP 2002 5 22 ZW0A0205101 1 20020514 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9621A 53592 DURING CHECK-C MAINT THE FWD SUPPORT STRUCTURE FOR LT MAIN GEAR WELL DOOR SEAL WAS CRACKED AT INBD KEEL BEAM END, STA 94 6. INSTALLED NEW ANGLE PER SRM 51-30-0. 2 L 7 2 4F RT A6WE 2002052200106 20020522 00106 WP 2002 5 22 ZW0A0205102 1 20020514 A 5320 CHANNEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9621A 53592 DURING CHECK-C MAINT THE FWD SUPPORT STRUCTURE FOR THE LT MAIN GEAR WELL DOOR SEAL WAS CRACKED APPROXIMATELY 36 INCHES F ROM KEEL BEAM. INSTALLED NEW CHANNEL PER PRINT 5930584 AND SRM 51-30-0. 2 L 7 2 4F RT A6WE 2002052200107 20020522 00107 NM 2002 5 22 ZW0A0205202 1 20020517 A 3397 WIRE HARNESS BOEING 767 7673Y0 NM CABIN DAMAGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 638TW 26205 DURING GROUND MAINTENANCE, EGRESS LIGHT AT SEAT 33B INOP. REPAIRED INTERFACE CORD, OPS-CK ASSURED NORMAL PERFORMANCE. 2 L 7 2 4F RT A1NM 2002052200108 20020522 00108 WP 2002 5 22 ZW0A0205203 1 20020516 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9305N 49395 DURING CHECK-C MAINT THE NUMBER 4 LT LONGERON WAS CRACKED AT STA 160. REPLACED DAMAGED SECTION OF LONGERON PER SRM 53-0 2, FIG 18. 2 L 7 2 4F RT A6WE 2002052200109 20020522 00109 EU 2002 5 22 MALA020295 1 20020510 A 5320 SEAT TRACK SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K-CHECK IN CWA, RH CENTER AISLE SEAT TRACK BLO CORROSION OUT OF LIMITS PER SAAB SRM. MAITNENANCE COMPLETED SEAT TRACK SPLICE FROM STA 297 TO 378 IAW EO #S53060. 2 L 7 2 4T RT A52EU 2002052200110 20020522 00110 NM 2002 5 22 0201635530 1 20020408 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 530US 23845 DURING "L" CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 25. REPAIRED PER EA 55-189610. 2 L 7 2 4F RT A2NM 2002052200111 20020522 00111 NM 2002 5 22 MEX2002024 1 20020128 A 2700 3321150013 VALVE BOEING 757 7572Q8 1384972 NM LT WING LEAKING A ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 802AM 5953 26270 FLT 913 - MTY-MEX - AIRCRAFT ARRIVED TO PLATFORM WITH HYDRAULIC FLUID LEAK IN THE LEFT WING. IT WAS CHECKED AND THE LEA K WAS FOUND AT SPOILER PCA NR 3 LEFT SIDE, EHSV BODY. CANCELLED THE PRESSURE AND RETURN PORTS AND DISCONNECTED THE ELEC TRIC CONNECTOR OF THIS VALVE. AIRCRAFT DISPATCHED IAW MEL 27-61-2. AT RON MEX 28/29 THE PCA NR 3 WAS REPLACED IAW MM 2 7-61-02, TESTS OK. (M) 2 L 7 2 4F RT A2NM 2002052200112 20020522 00112 NM 2002 5 22 MEX2002026 1 20020131 A 2131 CONTROLLER BOEING 757 7572Q8 1384972 NM CABIN PRESSURE FAILED A ASMF A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SW 23 801AM 25624 FLT 906 - MEX-MTY - AIRCRAFT RETURNED TO PLATFORM AFTER A PRESSUATIZATION FAIL MESSAGE. MAINT TESTED BOTHE PRESSURE CO NTROLLERS AND FOUND THAT THE ACTUATOR FAILED. REPLACE ACTUATOR IAW MM. REPLACED BOTH CONTROLLERS. 2 L 7 2 4F RT A2NM 2002052200113 20020522 00113 NM 2002 5 22 MEX2002027 1 20020202 A 7830 315A18006 ACTUATOR BOEING 757 7572Q8 1384972 NM THRUST REVERSER FAILED A ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 802AM 26270 FLT 402 - MEX-NYC - DURING TRANSIT CHECKED ENGINE NR 1 AND THE REVERSER WAS FOUND DEACTIVATED. THE WIRE BUNDLE OF THE R EVERSER CONTROL VALVE WAS CHAFED AGAINST THE WIRE BUNDLE OF THE FIRE DETECTOR. WIRE BUNDLES WERE ISOLATED, REVERSERS WO RKED OK AND NO SCREEN MESSAGES. AT PUSH BACK, BEFORE DISPATCHING CREW INFORMED OF THE FOLLOWING MESSAGE 'STATUS LT ENG SEC CONT' AND 'LT ENG REV CONT'. PERFORMED A FIM PROCEDUE 73-21-00 AND AIRCRAFT DISPATCHED IAW MEL 78-31-1. AT RON MEX 02/03, THE UPPER ACTUATOR WAS REPLACED IAW MM 78-31-13 AND THE WIRE BUNDLES WERE REPAIRED IAW WDM 71-51-12, TESTS OK. (M) 2 L 7 2 4F RT A2NM 2002052200114 20020522 00114 WP 2002 5 22 MEX2002028 1 20020203 A 2150 A/C PACK DOUG DC9 DC987 3022087 WP CABIN COOLING CONTAMINATED A ASMF D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 23 753RA 20751 722 49587 FLT 419 - MEX-VSA - 5 MINUTES BEFORE PUSH BACK, CAPTAIN REPORTED THE PRESENCE OF SMOKE INSIDE THE CABIN, BOTH SMOKE DETE CTORS IN THE REAR LAVATORIES WERE ACTIVATED. FOUND OIL LEAKED INTO THE COOLING TURBINE OF THE LEFT A/C PACK. AIRCRAFT W AS DISPATCHED IAW MEL 21-1. AT RON MEX 03/04 IT WAS REPLACED THE ASSY COOLING TURBINE AND WATER SEPARATOR IAW MM 21-01 AND 21-20-2, TESTS OK. (M) 2 L 7 2 4F RT A6WE 2002052200115 20020522 00115 2002 5 22 MEX2002029 4 20020204 A 3460 COMPUTER DOUG DC9 DC987 3022087 WP E/E COMPT FAILED A ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 803ML 1388 1388 49726 FLT 403 - MEX-NYC - AIRCRAFT RETURNED TO MEX AS CONSEQUENCE OF NAVIGATIONAL INSTRUMENTS FAIL. DURING CLIMBING THE NR 2 SYMBOL GENERATOR MALFUNCTIONED. BOTH EFIS WERE SWAPPED, OPERATION REESTABLISHED, BUT AFTER BOTH SYMBOL GENERATORS AND BO TH FMA OUT OF SERVICE, FLIGHT COMPUTERS WERE CHANGED WITHOUT SOLUTION. AT RON MEX 04/05 THE FAIL WAS FOUND IN THE AHRS 2, IT WAS REPLACED IAW MM 34-21.00, TESTS OK. (M) 2 L 7 2 4F RT A6WE 2002052200116 20020522 00116 NE 2002 5 22 MEX2002030 2 20020206 A 7230 BLADE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE DAMAGED A ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 831LF 371 53050 FLT 227 - CJS-MEX - DURING TRANSIT CHECK, DETECTED DAMAGES TO 28 BLADES OF THE NR 1 ENGINE. C1 DISK WAS REPLACED IAW MM 72-20-33 AND TESTS WERE PERFORMED IAW MM 71-00-00. (M) 2 L 7 2 4F 4 F RT E9NE 2002052200117 20020522 00117 2002 5 22 MEX2002033 4 20020208 A 3460 4608000307 COMPUTER DOUG DC9 DC987 3022087 WP AHRS FAILED A ASMF O OTHER O OTHER NR NOT REPORTED 1 SW 23 803ML 51 49726 FLT 907 - MTY-MEX - PILOT REPORTED AHRS NR 2 OUT OF SERVICE.. (M) 2 L 7 2 4F RT A6WE 2002052200118 20020522 00118 WP 2002 5 22 MEX2002035 1 20020211 A 4990 APU DOUG DC9 DC987 3022087 WP APU BAY LEAKING A ASMF K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 23 753RA 49587 FLT 419 - MEX-VSA - CREW REPORTED THE PRESENCE OF SMOKE IN THE PASSENGER CABIN AND SMOKE DETECTORS ACTIVATED IN THE LAVA TORIES. LEFT A/C PACKAGE AND COOLING TURBINE CHIP DETECTOR WAS CHECKED, OK, IT WAS FOUND OIL WASTES FROM THE PNEUMATIC A PU. (M) 2 L 7 2 4F RT A6WE 2002052200119 20020522 00119 EU 2002 5 22 NSVA0207 1 20020305 A 3220 13889 BEARING SAAB SF340 340B 7860101 EU LT NOSE WHEEL SEIZED A NSVA O OTHER O OTHER LD LANDING 1 EA 27 237MJ 340B237 NOSE TIRES FLAT JUST AFTER LANDING. MAINTENANCE FOUND LEFT INNER BEARING SEIZED TO AXLE. BEARING AND AXLE DESTROYED. MAINTENANCE REMOVED AND REPLACED NOSE WHEEL ASSEMBLY AND AXLE. UPON FURTHER INVESTIGATION IT WAS DETERMINED THAT THE CA USE OF THE BEARING FAILURE WAS DUE TO THE INTRODUCTION OF WATER/CONTAMINANTS INTO THE BEARING CREATING A BREAK DOWN OF T HE LUBRICATING PROPERTIES OF THE GREASE. (M) 2 L 7 2 4T RT A52EU 2002052200120 20020522 00120 CE 2002 5 22 NSVA0210 1 20020425 A 3246 MS9021268 WHEEL BEECH 1900 1900D 1154162 CE NR 4 MLG SEPARATED A NSVA O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 EA 27 221CJ UE221 AIR DISPATCH RECEIVED A REPORT THAT AIRCRAFT HAD LOST THE NR 4 MAIN WHEEL ASSEMBLY DURING TAKEOFF. CREW CONTINUED TO IA D WHERE THE TOWER CONFIRMED THAT A WHEEL WAS MISSING. CREW DECLARED AN IN FLIGHT EMERGENCY. AIRCRAFT LANDED SAFELY. M AINTENANCE INSPECTED THE AXLE ASSEMBLY AND DECLARED IT AIRWORTHY. MAINTENANCE REMOVED AND REPLACED THE NR 3 AND NR 4 WH EEL ASSEMBLY AND THE NR 4 BREAK ASSEMBLY. QA CONDUCTED AN INSPECTION OF THE REMAINING PORTION OF THE INNER BEARING COMP ONENTS AND VIEWED PHOTOS OF THE MAIN WHEEL ASSEMBLY AND DETERMINED THAT THE WHEEL ASSEMBLY DEPARTED THE MAIN GEAR TRUCK ASSEMBLY DUE TO AN APPARENT CATASTROPHIC FAILURE OF THE MAIN WHEEL BEARING ASSEMBLY. THE ROOT CAUSE OF THE BEARING FAIL 2 L 7 2 4T RT A24CE 2002052200121 20020522 00121 EU 2002 5 22 REXA02002 1 20020404 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY FALSE ACTIVATION A REXA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 361PX 340B249 CREW RECEIVED FALSE INDICATION OF SMOKE IN THE CARGO AREA. BOTTLES WHERE EXPENDED, CREW DECLARED EMERGENCY AND MADE AN UNSCHEDULED, UNEVENTFUL LANDING. NO EVIDENCE OF SMOKE FOUND AIRCRAFT INSPECTED AND FERRIED TO MEMPHIS. MAINTENANCE REM OVED AND REPLACED BOTH FORWARD AND AFT CARGO SMOKE DETECTORS, SYSTEM OPERATIONALLY CHECK WITH NO DEFECTS FOUND. (M) 2 L 7 2 4T RT A52EU 2002052200122 20020522 00122 NM 2002 5 22 SWAA020906 1 20020430 A 3350 6104781 BALLAST BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 731SA 27863 DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST AND RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002052200123 20020522 00123 2002 5 22 SWAA020907 4 20020430 A 2565 61621469 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED S LIDE PER MM. 2 L 7 2 4F RT A16WE 2002052200124 20020522 00124 EU 2002 5 22 REXA02003 1 20020405 A 2611 MS90311287 SWITCH SAAB SF340 340B 7860101 EU SMOKE TEST MALFUNCTIONED A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 361PX 340B249 FLT 5810 - MEM-LFT, ON CLIMB-OUT, CREW RECEIVED CARGO SMOKE WARNING. DETERMINED THAT THIS WAS A FALSE WARNING. PER MAI NTENANCE CONTROLS INSTRUCTION AIRCRAFT RETURNED TO MEMPHIS WITH UNEVENTFUL LANDING. REMOVED AND REPLACED TEST SWITCH. SYSTEM OPERATIONALLY CHECKED GOOD. (M) 2 L 7 2 4T RT A52EU 2002052200125 20020522 00125 EU 2002 5 22 REXA02004 1 20020406 A 2611 CONNECTOR SAAB SF340 340B 7860101 EU SMOKE DETECTOR DIRTY A REXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 361PX 340B249 FLT 5835 - MEM-PFN - ON CLIMB-OUT, CREW RECEIVED CARGO SMOKE WARNING. DETERMINED THAT THIS WAS A FALSE WARNING. PER MA INTENANCE CONTROLS INSTRUCTION AIRCRAFT RETURNED TO MEMPHIS WITH UNEVENTFUL LANDING. FOUND FOREIGN MATERIAL IN CONTROLL ER ELECTRICAL CONNECTOR (DIRT), CLEANED CONNECTOR SYSTEM CHECKED GOOD. (M) 2 L 7 2 4T RT A52EU 2002052200126 20020522 00126 NM 2002 5 22 SWAA020910 1 20020501 A 3350 65C27093 LENS BOEING 737 7373H4 1384600 NM SERVICE DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 646SW 28331 FED SVC DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002052200127 20020522 00127 EU 2002 5 22 REXA02005 1 20020407 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY FALSE ACTIVATION A REXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 361PX 340B249 FLT NR 5770 - MEM-BTR, CREW RECEIVED CARGO SMOKE WARNING. PER MAINTENANCE CONTROLS INSTRUCTION AIRCRAFT RETURNED TO MEM PHIS WITH UNEVENTFUL LANDING. REMOVED AND REPLACED DUE TO FALSE WARNINGS. (M) 2 L 7 2 4T RT A52EU 2002052200128 20020522 00128 2002 5 22 SWAA020911 4 20020428 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 610WN 27696 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052200129 20020522 00129 NM 2002 5 22 SWAA020913 1 20020501 A 2170 180849 COALESCER BAG BOEING 737 7377H4 1384404 NM A/C BAY CONTAMINATED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 732SW 27864 F/A REPORTED ELECTRICAL/RUBBERIZED SMELL COMING FROM AIR COND IN MAIN CABIN DURING FLIGHT. REMOVED AND REPLACED RT AIR CONDITIONING COALESCER BAG. 2 L 7 2 4F RT A16WE 2002052200130 20020522 00130 SO 2002 5 22 SIMA200207805 1 20020312 A 5310 SILL EMB 145 EMB145 3260210 SO PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - THIS IS LEVEL 2 FINDING ON A CRIC NR 35573. LEFT SILL IS CORRODED BETWEEN FRAMES 19 AND 23. MAINTENANCE REMOVED LEFT SILL AND INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002052200131 20020522 00131 NM 2002 5 22 SWAA020914 1 20020501 A 3350 6574550 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED RON, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE LIGHTS INOP. REMOVED AND REPLACED SLIDE LIGHT BATT ERY PER MM. 2 L 7 2 4F A16WE 2002052200132 20020522 00132 NM 2002 5 22 SWAA020919 1 20020501 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002052200133 20020522 00133 NM 2002 5 22 SWAA020921 1 20020502 A 3350 300432 SOCKET BOEING 737 7372H4 138448C NM EXTERIOR DEFECTIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT SOC KET PER MM. 2 L 7 2 4F A16WE 2002052200134 20020522 00134 2002 5 22 SWAA020922 4 20020501 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDR PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002052200135 20020522 00135 NM 2002 5 22 SWAA020924 1 20020501 A 5320 6517583 STIFFENER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB ASSY CRACKED (2 EA) AT BS 178, LBL 6.0, WL 188 AND 191. REPAIRED W EB ASSY PER SRM. 2 L 7 2 4F A16WE 2002052200136 20020522 00136 NM 2002 5 22 SWAA020925 1 20020501 A 5320 6551698 SPLICE BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 907, STR 4R AND 4L. REPAIRED STR SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2002052200137 20020522 00137 NM 2002 5 22 SWAA020930 1 20020503 A 3350 604222 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED A1 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002052200138 20020522 00138 2002 5 22 SWAA020931 4 20020503 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052200139 20020522 00139 2002 5 22 SWAA020932 4 20020505 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052200140 20020522 00140 NM 2002 5 22 SWAA020933 1 20020505 A 3350 1000679 LIGHT BOEING 737 7372K6 1364440 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002052200141 20020522 00141 2002 5 22 SWAA020934 4 20020505 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED RON, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER M M. 2 L 7 2 4F A16WE 2002052200142 20020522 00142 NM 2002 5 22 SWAA020936 1 20020504 A 3397 BR2013 WIRE BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED RON, FOUND EEPLS INOP IN FWD CABIN. CONNECTED LOOSE WIRE ON EEPLS PER MM. 2 L 7 2 4F A16WE 2002052200143 20020522 00143 NM 2002 5 22 SWAA020937 1 20020504 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED C2 CHECK, FOUND LT EXTERIOR AFT EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002052200144 20020522 00144 2002 5 22 SWAA020939 4 20020503 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002052200145 20020522 00145 NM 2002 5 22 SWAA020946 1 20020505 A 5320 6517583 STIFFENER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4D CHECK, FOUND T-CHORD CRACKED AT BS 178, WL 188 AT RBL 5. REPAIRED T-CHORD PER SRM. 2 L 7 2 4F A16WE 2002052200146 20020522 00146 2002 5 22 SWAA020950 4 20020505 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 641SW 27714 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052200147 20020522 00147 NM 2002 5 22 SWAA020955 1 20020505 A 2731 654516618 ROD END BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 635SW 27708 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, ELEVATOR TABS FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED ROD EN D ASSY'S ON BOTH TABS. 2 L 7 2 4F RT A16WE 2002052200148 20020522 00148 NM 2002 5 22 SWAA020957 1 20020506 A 2731 654516618 ROD END BOEING 737 7373H4 1384600 NM ELEVATOR TAB LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB INBOARD PUSH ROD, AFT ROD END HAS LOOSE DUST SEAL. REM OVED AND REPLACED LT ELEVATOR TAB PUSH ROD END PER MM. 2 L 7 2 4F RT A16WE 2002052200149 20020522 00149 NM 2002 5 22 SWAA020958 1 20020505 A 2710 KP4R16FS428 ROLLER BOEING 737 737301 1384611 NM AILERON WORN A SWAA K NONE F FLT CONT AFFECTED CL CLIMB 1 SW 07 660SW 23230 BINDING IN AILERONS DURING FLAP MOVEMENT. REMOVED AND REPLACED CENTERING MECH CAM ROLLER PER MM. 2 L 7 2 4F RT A16WE 2002052200150 20020522 00150 NM 2002 5 22 SWAA020964 1 20020506 A 2760 1061337 CABLE BOEING 737 7372H4 138448C NM SPEED BRAKE FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 071SW 22358 AIR TURNBACK, AIR GROUND SAFETY SENSOR FAILED ON TAKEOFF. REMOVED AND REPLACED GROUND SPEED BRAKE VALVE CABLE PER MM. 2 L 7 2 4F A16WE 2002052200151 20020522 00151 NE 2002 5 22 SWAA020966 2 20020505 A 7260 641000 GEARBOX BOEING 737 7372H4 138448C NM PWA JT8 JT8D9 52048 NE NR 1 ENGINE FAILED A SWAA E B ENGINE SHUTDOWN EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 29 089SW 14136 22904 707334 INFLIGHT SHUT DOWN, DECLARED EMERGENCY, DURING FLIGHT LOST NR 1 ENGINE OIL PRESSURE, SHUT ENGINE DOWN. REMOVED AND REPL ACED NR 1 ENGINE PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2002052200152 20020522 00152 NM 2002 5 22 SWAA020967 1 20020507 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 626SW 27702 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002052200153 20020522 00153 2002 5 22 SWAA020968 4 20020507 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002052200154 20020522 00154 NM 2002 5 22 SWAA020970 1 20020507 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F A16WE 2002052200155 20020522 00155 NM 2002 5 22 SWAA020972 1 20020507 A 3350 6104781 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002052200156 20020522 00156 WP 2002 5 22 MWEA020370 1 20020521 A 5230 59101575 PAN DOUG DC9 DC932 3022066 WP AFT CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT CARGO DOOR INNER PAN CRACKED AT AFT LOCKING CAM. -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002052200157 20020522 00157 WP 2002 5 22 IXXA0200026O 1 20020522 A 2910 FLEX LINE DOUG DC8 DC863 302198A WP WHEEL WELL RUPTURED A IXXA O OTHER K FLUID LOSS CL CLIMB 1 SW 11 786AL 84009 2471 46121 ENROUTE FROM PDX TO TOL, DURING CLIMB OUT THE FLIGHT CREW NOTICED THE MAIN HYDRAULIC QUANTITY SYSTEM DECLINING. THE FLIG HT CREW FOLLOWED COMPANY PROCEDURES AND RETURN TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED AND LOCATED A RUP TURED HYDRAULIC LINE AT THE THRUST REVERSER PUMP. MAINTENANCE REPLACED THE LINE AND PERFORMED A SUCCESSFUL OPERATIONAL C HECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002053100131 20020531 00131 NM 2002 5 31 DHL2002753004 1 20020518 A 2782 1U11032 ACTUATOR BOEING 727 727223 1384074 NM L/E SLAT FAILED A DHLA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 753DH 22468 NR 6 L/E SLAT FAILED TO RETRACT AFTER T/O. FOLLOWED ABNORMAL PROC, STILL DID NOT SHOW RETRACTED. R&R NR 6 L/E SLAT AC TUATOR IAW DHL B727A MM 27-81-32. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2002052200158 20020522 00158 NM 2002 5 22 UPS02538356 1 20020521 A 5610 012NB77114 SLIDING WINDOW BOEING 757 75724APF 1384969 NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 475UP 28845 INSPECTION TYPE:N/A PILOT REPORT F/O SLIDING WINDOW CRACKED R & R COPILOT'S RT SLIDING WINDOW PER 767 MM 56-11-02-4, S/N,ILLEG 1586 ALSO R & R RT WINDOW ILLEG 2 L 7 2 4F RT A2NM 2002052200159 20020522 00159 SO 2002 5 22 COMA0210021 1 20020521 A 3350 1011105 LIGHT EMB 120 EMB120RT 3260202 SO CABIN BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 120262 FLIGHT 5063 DURING INSPECTION FOUND EMERGENCY EXIT SIGN AT 5A LOCATION INOPERATIVE.REPLACED THE EMERGENCY LIGHT ASSEMBLY . 2 L 7 2 4T RT A31SO 2002052200160 20020522 00160 2002 5 22 COMA0260325 4 20020520 A 3440 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA A COMA K NONE J WARNING INDICATION TO TAKEOFF 1 SO 01 430CA 7461 FLIGHT 5925 - DUIRNG APPLICATION OF POWER FOR T/O RECEIVED A GROUND SPOILER FAULT MESSAGE, AIRCRAFT RTURNED TO THE GATE. REMOVED, CLEANED AND REINSTALLED THE #1 RADAR ALTIMETER ANTENNA CONNECTOR. 2 L 7 2 4F RT A21EA 2002052200161 20020522 00161 EA 2002 5 22 COMA0260326 1 20020520 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 978CA 7158 FLIGHT 5422 - DURING DECENT INTO YYZ RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREE FLAP POSITION.COMPLIED WITH AD 98 -20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3 (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2002052200162 20020522 00162 NM 2002 5 22 SWAA020997 1 20020508 A 5753 6546435 FLAP BOEING 737 7373TO 138447G NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C4 CHECK, FOUND RT T/E OUTBOARD AFT FLAP DELAMINATED AT INBOARD T/E CORNER. REMOVED AND REPLACED RT T/ E OUTBOARD AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2002052200163 20020522 00163 2002 5 22 AWXA200200438 4 20020521 A 2230 RAA21964 SWITCH BOEING 737 73733A 1384673 NM ZONE 205 STICKING A AWXA C ABORTED TAKEOFF J N WARNING INDICATION FALSE WARNING TO TAKEOFF 1 WP 28 166AW 0 0 23627 SMF - ABORTED TAKEOFF - FLT 0259 - DURING TAKEOFF ROLL AT SMF THE TAKEOFF WARNING HORN SOUNDED, TAKEOFF WAS ABORTED. RES ET THE FLAPS, TRIM, AND SPEEDBRAKES; REATTEMPTED TAKEOFF BUT HORN SOUNDED AGAIN. MAINTENANCE CLEANED THROTTLE SWITCHES A T OVERHEAD IN E/E BAY; COMPLIED WITH TAKEOFF WARNING SYSTEM TEST T/C A1B31009, TAKEOFF WARNING SYSTEM CHECKED GOOD. 2 L 7 2 4F RT A16WE 2002052200164 20020522 00164 EU 2002 5 22 AWXA200200439 1 20020521 A 2910 22610117 O-RING AEROQUIP AIRBUS 320 A320231 3930325 EU ZONE 140 DETERIORATED A AWXA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CR CRUISE 1 WP 28 622AW 0 0 054 LAS - DIVERSION - FLT 0470 - EN ROUTE FROM PHX TO BUR ECAM INDICATED YELLOW HYDRAULIC SYSTEM LOW QUANTITY, AIRCRAFT DIVE RTED TO LAS. MAINTENANCE FOUND HYDRAULIC LEAK AT QUICK DISCONNECT (3701GM) ON YELLOW HYDRAULIC SYSTEM MAIN POWER MODULE, REMOVED AND REPLACED DETERIORATED O-RING AT QUICK DISCONNECT, OPERATIONAL AND LEAK CHECK COMPLIED WITH IAW AMM 20-29-00 -911-002. 2 L 7 2 4F RT A28NM 2002052300004 20020523 00004 NM 2002 5 23 CALA0200313 1 20020522 A 5330 65C3393013 SKIN BOEING 737 7373T0 1384582 NM STA 373 CRACKED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 47332 23570 SKIN CRACK AT EXHAUST COOLING FAN OUTLET 6 OCLOCK POSITION. INSTALLED REPAIR DOUBLER PER EC/RA 5330-02894. 2 L 7 2 4F RT A16WE 2002052300011 20020523 00011 2002 5 23 SWAA020973 4 20020507 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002052300012 20020523 00012 NM 2002 5 23 SWAA020976 1 20020507 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 649SW 27719 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS440, STR 16R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002052300013 20020523 00013 NM 2002 5 23 SWAA020977 1 20020507 A 5320 654583340 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB CRACKED AT BS 180, WL 207 AT RBL 26. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002052300014 20020523 00014 NM 2002 5 23 SWAA020978 1 20020507 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REPAIRED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002052300015 20020523 00015 NM 2002 5 23 SWAA020980 1 20020507 A 2731 65C26384 TAB BOEING 737 7373H4 1384600 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002052300016 20020523 00016 NM 2002 5 23 SWAA020993 1 20020508 A 3260 65C28034 SENSOR BOEING 737 7373G7 1384595 NM NLG MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 671SW 23785 DURING FLT, BOTH NLG RED AND GREEN LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. REMOVED AND REPLACED S845 SWITCH PER MM. 2 L 7 2 4F RT A16WE 2002052300017 20020523 00017 2002 5 23 SWAA021000 4 20020509 A 2565 D31354 SLIDE BOEING 737 7373TO 138447G NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052300018 20020523 00018 NM 2002 5 23 SWAA021006 1 20020509 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 767SW 29807 EEPLS INOP AT ROW 4. RELAMPED EEPLS AT ROW 4 PER MM. 2 L 7 2 4F RT A16WE 2002052300019 20020523 00019 2002 5 23 SWAA021008 4 20020511 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002052300020 20020523 00020 2002 5 23 SWAA021011 4 20020512 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052300021 20020523 00021 NM 2002 5 23 SWAA021012 1 20020509 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING IN FWD CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2002052300022 20020523 00022 EU 2002 5 23 R7M2002F00037 1 20020208 A 5320 350A58165800 STRUT SNIAS 350 AS350B3 8680954 EU TMECA ARRIUS ARRIU2F NE EQUIP COWLING WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 105LN 1137 3249 EQUIPED COWLING STRUT - WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS, CORRECTED PROBLEMS. 1 G 7 1 3U 3 U H9EU E34NE 2002052300023 20020523 00023 NM 2002 5 23 SWAA021021 1 20020510 A 2731 65C308781 CONTROL ARM BOEING 737 7375H4 138449D NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED RON, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TRIM TAB C ONTROL CRANK PER MM. 2 L 7 2 4F RT A16WE 2002052300024 20020523 00024 2002 5 23 SWAA021022 4 20020510 A 3120 350000001 CLOCK BOEING 737 7377H4 1384404 NM COCKPIT OVERHEATED A SWAA A UNSCHED LANDING M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 411WN 29821 DECLARED EMERGENCY, DIVERSION, ELECTRICAL SMOKE IN COCKPIT. FOUND CAPT'S CLOCK TO BE SOURCE, REMOVED AND REPLACED CAPT' S CLOCK PER MM. 2 L 7 2 4F RT A16WE 2002052300025 20020523 00025 NM 2002 5 23 SWAA021023 1 20020511 A 2731 BACB28AMO7 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED TAB LOCK MECHANISM BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002052300026 20020523 00026 NM 2002 5 23 SWAA021025 1 20020508 A 2910 AS116080264 HYDRAULIC LINE BOEING 737 7373H4 1384600 NM B SYSTEM LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 29 326SW 23690 AIR TURNBACK, DURING CLIMB LOST B-SYSTEM HYDRAULIC FLUID. REMOVED AND REPLACED HYDRAULIC LINE, FROM B-SYSTEM PRESS MODU LE TO THE ACOUSTIC FILTER ASSY PER MM. 2 L 7 2 4F RT A16WE 2002052300027 20020523 00027 NM 2002 5 23 SWAA021036 1 20020513 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 713SW 27847 UPPER EMERGENCY EXIT LIGHT LENS FELL OFF IN MID CABIN. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002052300028 20020523 00028 NM 2002 5 23 SWAA021038 1 20020513 A 3350 65C27093 LENS BOEING 737 7373H4 1384600 NM ENTRY DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002052300029 20020523 00029 2002 5 23 SWAA021039 4 20020513 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER UPON ARRIVAL. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052300030 20020523 00030 2002 5 23 SWAA021044 4 20020515 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052300031 20020523 00031 2002 5 23 SWAA021045 4 20020512 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052300032 20020523 00032 NM 2002 5 23 SWAA021047 1 20020514 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 234 AND LBL 15. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002052300033 20020523 00033 NM 2002 5 23 SWAA021050 1 20020513 A 3350 65C34691 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 717SA 27851 DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT LIGHTS INOP AT ROW'S 13 ABC, 23 DEF AND 21 DEF. REPAIRED O VERHEAD EXIT LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2002052300034 20020523 00034 EU 2002 5 23 R7MR036449 1 20020409 A 3150 AWEUR03 SIGNAL COND UNIT UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE COCKPIT INTERMITTENT B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 101HN 0162 SIGNAL PROCESSING UNIT - INTERMITTENT FULL BENDING INDICATION ON START-UP AND WILL STAY AT MAX INDICATION FOR DURATION O F FLIGHT. SOMETIMES UNIT WILL NOT FLUSH SELF TEST PROCEDURE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052300035 20020523 00035 2002 5 23 R7MR34634 4 20020407 A 2210 41600297004 MODULE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE AUTOPILOT SYS INOPERATIVE B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 101HN 270 0162 APM2000 AUTO PILOT MODULE - UNIT INOPERATIVE. FAILURE WITH YELLOW BARS ON PFD SHOWN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052300036 20020523 00036 NM 2002 5 23 SWAA021051 1 20020513 A 3350 D71702001 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 717SA 27851 DURING SCHEDULED C2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002052300037 20020523 00037 NM 2002 5 23 SWAA021052 1 20020513 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 717SA 27851 DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP BETWEEN ROW'S 21 AND 23. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002052300038 20020523 00038 NM 2002 5 23 SWAA021057 1 20020515 A 3350 071702001 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 717SA 27851 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR RT SIDE SLIDE LIGHT INOP. REMOVED AND REPLACED DOOR SLIDE LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002052300039 20020523 00039 2002 5 23 SWAA021058 4 20020512 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052300040 20020523 00040 NM 2002 5 23 SWAA021061 1 20020515 A 3350 65C34691 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY LIGHT INOP AT ROW NR 3 DEF. REMOVED AND REPLACED LI GHT PER MM. 2 L 7 2 4F RT A16WE 2002052300041 20020523 00041 NM 2002 5 23 SWAA021067 1 20020516 A 5610 5717623122 WINDOW BOEING 737 7373Q8 1384670 NM COCKPIT DEFECTIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 F/O'S WINDOW WILL NOT OPEN FROM THE OUTSIDE USING THE EMERGENCY RELEASE HANDLE. REMOVED AND REPLACED F/O'S WINDOW PER M M. 2 L 7 2 4F RT A16WE 2002052300042 20020523 00042 NM 2002 5 23 SWAA021069 1 20020516 A 5511 6547990 RIB BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED D-CHECK, FOUND LT HORIZ STAB L/E RIB CRACKED AT STA 184.70. REMOVED AND REPLACED LT L/E RIB PER SRM. 2 L 7 2 4F RT A16WE 2002052300043 20020523 00043 EA 2002 5 23 SWIA200210809 1 20020420 A 5270 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR OUT OF ADJUST A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 587SW 7062 UPON CLIMBOUT OF SLC, RECEIVED 'PAX DOOR LATCH' CAUTION MESSAGE. FOUND PS2M3 SWITCH HITTING EXTERNAL HANDLE. ADJUSTED PER MM 52-70-04. DOOR CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002052300044 20020523 00044 EU 2002 5 23 R7MR34741 1 20020209 A 6720 41800876800 ACTUATOR UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE TAIL ROTOR INTERMITTENT B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 101HN 164 0162 SMART ELEC MECHA ACTUATOR - INOPERATIVE INDICATION SHOWS ON DISPLAY INTERMITTENLY. INOPERATIVE AUTOPILOT DURING PREFLIG HT CHECK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052300045 20020523 00045 2002 5 23 SWIA200210810 4 20020413 A 3425 COMPUTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 190SW 120050 DURING CLIMBOUT, FIRST OFFICER'S HEADING INDICATOR STARTED STICKING WITH A 30 DEGREE DIFFERENCE BETWEEN HI'S WITH NO ASS OCIATED FLAGS OR ALARMS. AFTER TURNING BACK TOWARD DEN, THE GYRO BEGAN WORKING PROPERLY. FIRST OFFICER RECEIVED COMPU TER FLAG DURING TAXI IN. RERACKED HEADING COMPUTER. OPS CHECK GOOD ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2002052300046 20020523 00046 SO 2002 5 23 SWIA200210811 1 20020416 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT 3260202 SO T/E FLAP FAILED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 1110J 5038 5038 120110 RIGHT OUTBOARD FLAP CAME DOWN 5 DEGREES SITTING ON RAMP WITH ENGINES OFF AND APU RUNNING. RAN QRH AND FLAP FAILED TO RE TRACT. REPLACED RIGHT OUTBOARD FLAP ACTUATOR. OPERATED FLAPS SEVERAL TIMES. OPS CHECK GOOD. NO LEAKS FOUND. 2 L 7 2 4T RT A31SO 2002052300047 20020523 00047 SO 2002 5 23 SWIA200210812 1 20020421 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 567SW 120342 EMERGENCY LIGHTS OUT ON ROW 9. REPAIRED BROKEN WIRE IN OVERHEAD BIN AT ROW 9. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002052300048 20020523 00048 EA 2002 5 23 SWIA200210813 1 20020421 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 587SW 7072 ON CLIMBOUT THERE WAS AN APPRECIABLE CHANGE IN THE SOUND OF THE SLIPSTREAM, FOLLOWED BY A PASSENGER DOOR OUTER HANDLE CA UTION MESSAGE. RETURNED TO SLC. FOUND PS2MB DOOR HANDLE PROXIMITY SWITCH HITTING THE HANDLE. ADJUSTED PER MM 52-70-04 . DOOR OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002052300049 20020523 00049 SO 2002 5 23 SWIA200210814 1 20020421 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 586SW 120354 FOUND BROKEN WIRE TO OVERHEAD EMERGENCY EXIT LIGHT ROW 9. LIGHT WILL NOT ILLUMINATE. REPAIRED WIRE WITH SPLICE. OPS C HECK GOOD. 2 L 7 2 4T RT A31SO 2002052300055 20020523 00055 EU 2002 5 23 R7MR34754 1 20020220 A 6220 350A31190703 STARFLEX SNIAS 350 AS350B3 8680954 EU TMECA ARRIUS ARRIU2F NE MAIN ROTOR DEBONDED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 105LN 1157 3249 STARFLEX - BUSHINGS DEBONDING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E34NE 2002052300056 20020523 00056 2002 5 23 SWAA021107 4 20020520 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002052300057 20020523 00057 NM 2002 5 23 SWAA021108 1 20020521 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM AFT SVC DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR ONERHEAD EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LEN S PER MM. 2 L 7 2 4F RT A16WE 2002052300058 20020523 00058 NM 2002 5 23 SWAA021112 1 20020521 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002052300059 20020523 00059 NM 2002 5 23 SWAA021113 1 20020520 A 5511 6547984 SKIN BOEING 737 7373H4 1384600 NM LT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED C4 CHECK, FOUND LT HORIZ STAB SKIN LOWER SURFACE CRACKED AT STA 108 NEAR AFT SPAR. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2002052300060 20020523 00060 NM 2002 5 23 SWAA021114 1 20020521 A 2731 6959227 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED BUSHINGS FOR LT OTBD LOCKOUT MECHANISM PER MM. 2 L 7 2 4F RT A16WE 2002052300061 20020523 00061 2002 5 23 SWAA021094 4 20020516 A 2565 65C19901 CABLE BOEING 737 7372T4 1384492 NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002052300062 20020523 00062 NM 2002 5 23 SWAA021098 1 20020516 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 778SW 27883 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED THROUGHTOUT CABIN. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002052300063 20020523 00063 NM 2002 5 23 SWAA021100 1 20020520 A 5313 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 767, STR 25L. REMOVED AND REPLACED TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002052300064 20020523 00064 NM 2002 5 23 SWAA021101 1 20020518 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 3, LBL 8 AND RBL 3. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002052300065 20020523 00065 NM 2002 5 23 SWAA021102 1 20020517 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 727SW 27859 DURING SCHEDULED SERVICE CHECK,SWA SI 11038-55, FOUND RT ELEVATOR TAB NR 2 AND NR 4 HINGES WORN. REMOVED AND REPLACED N R 2 AND NR 4 TAB HINGE BUSHINGS PER SRM. 2 L 7 2 4F RT A16WE 2002052300066 20020523 00066 NM 2002 5 23 SWAA021103 1 20020520 A 5330 6545767 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 071SW 22358 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, FWD OF AFT RAD ALT ANTENNA, BL 0. REPAIRED SKIN PER S WA RA. 2 L 7 2 4F A16WE 2002052300067 20020523 00067 NM 2002 5 23 SWAA021104 1 20020518 A 5330 6545774 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 827, BETWEEN STR'S 23L AND 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002052300068 20020523 00068 NM 2002 5 23 SWAA021105 1 20020519 A 5330 6546567 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 1006, BETWEEN STR'S 26L AND 27L. REPAIRED SKIN PER SWA RA . 2 L 7 2 4F A16WE 2002052300069 20020523 00069 NM 2002 5 23 SWAA021106 1 20020517 A 5311 6545871 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED C2 CHECK, FOUND FRAME CRACKED AT FWD SVC DOOR UPPER HINGE CUTOUT. REPAIRED FRAME PER SWA RA. 2 L 7 2 4F RT A16WE 2002052300070 20020523 00070 NM 2002 5 23 SWAA021079 1 20020519 A 3350 604222 BATTERY BOEING 737 7375H4 138449D NM CABIN INTERMITTENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/4D CHECK, FOUND FWD EMERGENCY LIGHTS INTERMITTENT. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2002052300071 20020523 00071 NM 2002 5 23 SWAA021081 1 20020519 A 5330 6547955 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED D CHECK, FOUND BEAR STRAP CORRODED AT BS 796, WL 156 AND RBL 33. REPAIRED BEAR STRAP PER SRM. 2 L 7 2 4F RT A16WE 2002052300072 20020523 00072 NM 2002 5 23 SWAA021082 1 20020519 A 5330 6545890 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED D CHECK, FOUND BEAR STRAP CRACKED AT BS 312, WL 235 AND 259 LT. REPAIRED BEAR STRAP PER BFG ER. 2 L 7 2 4F RT A16WE 2002052300073 20020523 00073 NM 2002 5 23 SWAA021083 1 20020516 A 2731 BACB28AK04 BUSHING BOEING 737 7375H4 138449D NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED A2 CHECK, SWA SI 11138-55, FOUND RT ELEVATOR TAB HINGE BUSHINGS WORN AT NR 1, NR 3, AND NR 4 HINGE ATTA CH POINTS. REMOVED AND REPLACED BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002052300074 20020523 00074 NM 2002 5 23 SWAA021084 1 20020516 A 2731 65C2638415 TAB BOEING 737 7375H4 138449D NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED A2 CHECK, SWA SI 11138-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TA B AND HINGE BUSHINGS FOR NR 1 AND NR 2 HINGE POINTS PER MM. 2 L 7 2 4F RT A16WE 2002052300075 20020523 00075 NM 2002 5 23 SWAA021085 1 20020518 A 2731 BACB28AK04 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH INBD AND OTBD HINGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002052300076 20020523 00076 NM 2002 5 23 SWAA021086 1 20020516 A 5753 6446435238 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OTBD AFT T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002052300077 20020523 00077 NM 2002 5 23 SWAA021087 1 20020518 A 5754 65C26601 SLAT BOEING 737 7373A4 1384585 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT CRACKED UNDER PREVIOUS REPAIR. REMOVED AND REPLACED NR 1 L/E SLAT PER MM . 2 L 7 2 4F RT A16WE 2002052300078 20020523 00078 NM 2002 5 23 SWAA021088 1 20020519 A 2731 BACB28AK04 BUSHING BOEING 737 7373H4 1384600 NM LT/RT ELEV WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55,BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLAC ED NR 1 HINGE BUSHINGS ON BOTH LT AND RT TABS PER MM. 2 L 7 2 4F RT A16WE 2002052300079 20020523 00079 NM 2002 5 23 SWAA021089 1 20020519 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUAELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002052300080 20020523 00080 NM 2002 5 23 SWAA021090 1 20020516 A 5315 6545410 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL BEAM CRACKED AT BS 667, WL 206.5 AND LBL 25. REPAIRED BEAM PER BFG ER. 2 L 7 2 4F RT A16WE 2002052300081 20020523 00081 NM 2002 5 23 SWAA021091 1 20020518 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002052300082 20020523 00082 NM 2002 5 23 SWAA021092 1 20020518 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 16R, BS'S 444 AND 466. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002052300083 20020523 00083 EU 2002 5 23 R7MR35027 1 20020403 A 2140 JBS8803 VALVE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE HEATER INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 101HN 259 0162 MIXING VALVE (HEATER/EJECTOR) - UNIT INOPERATIVE. WILL NOT ALLOW WARM AIR TO COME FROM ENGINE, EVEN THROUGH (BLEED AIR) IS ILLUMINATED ON COCKPIT DISPLAY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052300084 20020523 00084 EU 2002 5 23 R7MR35028 1 20020405 A 2140 JBS8803 VALVE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE HEATER INTERMITTENT B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 101HN 0162 MIXING VALVE (HEATER/EJECTOR) - UNIT OPERATES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052300085 20020523 00085 EU 2002 5 23 R7MR35043 1 20020412 A 6720 41800876800 ACTUATOR UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE TAIL ROTOR INOPERATIVE A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 101HN 284 0162 SMART ELEC MECHA ACTUATOR - UNIT INOPERATIVE. PRE-FLIGHT AUTOPILOT CHECK FAILED. DURING FLIGHT PILOT REPORTS AMBER Y O N PFD AND ACTUATOR LIGHT ON CAD. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052300086 20020523 00086 SO 2002 5 23 SIMA200207902 1 20020319 A 5320 DOUBLER EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20. REMOVED P REVIOUS REPAIR (CORROSION LIMITED TO PREVIOUS REPAIR). FABRICATED A DOUBLER ANGLE, FILLER, A PLATE, AND SHIMS. REPAIRE D IAW EMB 145 SRM 9SRM 145/1142 CHAPTER 53, REV 17) 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002052300087 20020523 00087 EU 2002 5 23 R7MR35044 1 20020416 A 6720 41800876800 ACTUATOR UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE TAIL ROTOR INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 101HN 292 0162 SMART ELEC MECHA ACTUATOR - UNIT INOPERATIVE. POPS CIRCUIT BREAKER. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052300088 20020523 00088 EU 2002 5 23 R7MR35052 1 20020315 A 6420 350A33214501 CONTROL ROD SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE PITCH CONTROL WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 385LR 256 3402 PITCH CONTROL ROD- WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002052300089 20020523 00089 EU 2002 5 23 R7MR35053 1 20020412 A 2140 JBS8803 VALVE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE HEATER INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 101HN 284 0162 MIXING VALVE (HEATER/EJECTOR) UNIT INOPERATIVE. VALVE FUNCTIONS PROPERLY, BUT (BLEED AIR) INDICATION CAD ALLWAYS ON RE GARDLESS OF HEATING STATUS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052300090 20020523 00090 2002 5 23 R7MR35057 4 20020407 A 3422 060001500 GYRO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 385LR 287 3402 KG0102A-DIRECTIONAL GYRO - UNIT INOPERATIVE. UNIT WILL NOT OPERATE IN SLAVE/FREE MODE. REPLACED WITH NEW UNIT, CORRECT ED PROBLEM. OEM WARRANTY APPLIES. 1 G 7 1 3U 3 U H9EU E19EU 2002052300091 20020523 00091 2002 5 23 R7MR35074 4 20020419 A 3160 B19030MC02 DISPLAY SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT MALFUNCTIONED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 106LN 1207 3251 VEMD (ASTAR AFTER 3018) DISPLAY PIXELS NOT READABLE IN LOWER SCREEN PORTION. REPLACED WITH NEW UNIT, CORRECTED PROBLE M. 1 G 7 1 3U 3 U H9EU E19EU 2002052300092 20020523 00092 EU 2002 5 23 RM7R35079 1 20020228 A 2432 RG355 BATTERY SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE MAIN DISCHARGED B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 385LR 231 3402 LEAD ACID BATTERY - WILL NOT HOLD CHARGE. BATTERY SCRAPPED LOCALLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002052300093 20020523 00093 SO 2002 5 23 SIMA200207906 1 20020319 A 5320 14521725013 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - THIS IS A LEVEL 2 FINDING. SERVICE DOOR FORWARD SILL CORRODED. REMOVED CORRODED SERVICE DOOR FORWARD SILL AND IN STALLED SERVICEABLE SILL IAW EMB 145 51-40-02 AND 51-20-03. (M) 2 L 7 2 4F RT T00011AT 2002052300094 20020523 00094 SO 2002 5 23 SIMA200207907 1 20020319 A 5320 14525480003 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 THIS IS A LEVEL 2 FINDING. CARGO DOOR LOWER SILL CORRODED. REMOVED DAMAGED CARGO DOOR SILL AND INSTALLED SERVICEABLE O NE IAW EMB145 SRM 51-40-02, 51-40-05, 51-20-03. (M) 2 L 7 2 4F RT T00011AT 2002052300095 20020523 00095 NM 2002 5 23 C1HA200293004 1 20020520 A 2611 SMOKE DETECTOR BOEING 727 727212 138407G NM INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 293AS 21348 Left aft lavatory smoke detector will not silence. No smoke noted in lavatory. Removed and replaced battery in lavatory smoke detector. Operationally checks good. 2 L 7 3 4F A3WE 2002052300096 20020523 00096 SO 2002 5 23 SIMA200208701 1 20020312 A 5320 14522459003 SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 THIS IS A LEVEL 2 FINDING. GALLEY RAMP SUPPORT CORRODED. INSTALLED SERVICEABLE GALLEY RAMP SUPPORT IAW EMB145 SRM 51-4 0-02. (M) 2 L 7 2 4F RT T00011AT 2002052300097 20020523 00097 SO 2002 5 23 VJ32002F00030 2 20020507 A 7414 6310 MAGNETO BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO ENGINE FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 01 5519A 1 CE1337 825759R MAGNETO FAILED IN FLIGHT AND A SAFE LANDING WAS MADE. GROUND CHECK OF THE MAGNETOS CONFIRMED THAT THE MAGNETO WAS DEAD. MAGNETO WAS REMOVED AND REPAIRED MAGNETO INSTALLED. GROUND OPERATION AND MAGNETO CHECKED NORMAL. PART SENT FOR WARRA NTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002052300098 20020523 00098 EA 2002 5 23 VJ32002F00031 2 20020507 A 7314 RG9570K1M PUMP GROB ASTIR G102ASTIR 1660104 EU LYC O540 AEIO540D4A5 41532 EA FUEL SYSTEM INOPERATIVE B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 01 863AF 76 85003 L2802548A AT 800 RPM THE FUEL PRESSURE DROPS BELOW MINIMUM AND THE LOW PRESSURE LIGHT CAME ON AT IDLE. SYSTEM WAS CHECKED AND FOU ND THAT THE PUMP OUT PUT WAS LOW. PUMP REMOVED AND A NEW PUMP INSTALLED. GROUND RUN AND FINAL ADJUSTMENTS TO THE PUMP WERE MADE. OPERATIONAL CHECK OF THE PUMP AT IDLE AND MAX RPM CHECKED NORMAL. PART WAS SENT FOR WARRANTY. 1 K 0 0 3 O G33EU 1E4 2002052300099 20020523 00099 SO 2002 5 23 VJ32002F00035 2 20020513 A 7414 6310 MAGNETO BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO ENGINE FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 5544A 95 CE1343 825767R MAGNETO FAILED ON GROUND RUN UP. MAGNETO WAS REMOVED AND A REPAIRED MAGNETO INSTALLED. WHEN THE COVER WAS REMOVED THE DISTRIBUTOR BLOCK WAS FOUNDED TO HAVE A GRAY POWDER DUST ON IT. TOTAL TIME ON MAGNETO FROM NEW IS 95.0 HOURS. PART SEN T IN FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002052300100 20020523 00100 SO 2002 5 23 VJ32002F00037 2 20020510 A 7314 64621216 PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO FUEL PRESSURE FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 38071 CE935 559970R UNABLE TO ADJUST LOW-END FUEL PRESSURE ON TRIM RUN OF A NEW OVERHAULED ENGINE FROM RAM. PUMP WAS REMOVED AND NEW PUMP I NSTALLED. COMPLETED TRIM RUNS OF ENGINE. OPERATIONAL CHECK OF ENGINE CHECKED NORMAL. PUMP SENT BACK TO RAM FOR WARRAN TY. 1 L 7 1 3O 3 O 3A15 E5CE 2002052300101 20020523 00101 CE 2002 5 23 WXH2002F00000 1 20020109 A 2821 07560361 STRAINER CESSNA 182 182S 2072701 CE LYC O540 IO540* 41532 EA FUEL SYSTEM DAMAGED B WXHR K NONE O OTHER IN INSP/MAINT 1 NM 01 1252E 1799 18280580 UPON REINSTALLATION OF FUEL STRAINER AFTER INSPECTION, STANDPIPE THREADS FATIGUED. FAILED WHEN STANDPIPE WAS TIGHTENED. INSPECTION REVEALED ONLY 1.5 TO 2 TURNS ENGAGEMENT THREADS, DO NOT GO UP TO THE TOP OF STANDPIPE AS IN 182 T MODELS W E THINK THIS IS A SAFETY ISSUE. (AD SHOULD BE ISSUED) 1 H 7 1 3O 3 O NT 3A13 1E4 2002052300102 20020523 00102 SO 2002 5 23 SIMA200208702 1 20020312 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - THIS IS A LEVEL 2 FINDING. GALLEY CENTER BEAM GUSSET CORRODED. INSTALLED SERVICEABLE CENTER BEAM GUSSET IAW EMB1 45 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002052300108 20020523 00108 SO 2002 5 23 SIMA200208703 1 20020312 A 5320 14522461011 DOUBLER EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - THIS IS LEVEL 2 FINDING, DOUBLER ON LEFT HAT BEAM BETWEEN FRAMES 65 AND 68 CORRODED. REMOVED DAMAGED DOUBLER, INS TALLED NEW DOUBLER IAW EMB 145 SRM 51-40-02, 51-40-06, 51-20-03. (M) 2 L 7 2 4F RT T00011AT 2002052300109 20020523 00109 SO 2002 5 23 SIMA200208704 1 20020312 A 5320 14522226003 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - THIS IS A LEVEL 2 FINDING. CENTER GUSSET IN LAVATORY CORRODED. INSTALLED NEW GUSSET IAW EMB145 SRM 51-40-02, 51- 40-06, 51-20-03. (M) 2 L 7 2 4F RT T00011AT 2002052300110 20020523 00110 SO 2002 5 23 SIMA200208705 1 20020312 A 5320 14529150001 CROSSBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - THIS IS LEVEL 2 FINDING. FOUND CORROSION ON GALLEY CROSSBEAM AND PROFILE. INSTALLED SERVICEABLE CROSS BEAM AND P ROFILE IAW EMB145 SRM 51-20-03, 51-40-02 AND 51-40-06. (M) 2 L 7 2 4F RT T00011AT 2002052300111 20020523 00111 SO 2002 5 23 SIMA200208706 1 20020312 A 5320 14522461011 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - THIS IS A LEVEL 2 FINDING. GALLEY AREA FORWARD DIAMOND GUSSET CORRODED. INSTALLED NEW FORWARD GUSSET IAW EMB 145 SRM 51-40-02, 51-20-03, 51-40-06. (M) 2 L 7 2 4F RT T00011AT 2002052300112 20020523 00112 SO 2002 5 23 SIMA200208801 1 20020319 A 5311 12010732001 FRAME EMB 145 EMB145 3260210 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - DURING INSPECTION OF AIRCRAFT, FOUND THE LOWER EDGE OF FRAME 81 CHAFED APPROXIMATELY 12 INCH. RAI FRAME 81 IAW EM B 145 (SRM 145-1142 CHAPTER 51, REV 17) 51-20-01, 51-40-02, 51-40-04, 51-40-07 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002052300113 20020523 00113 SO 2002 5 23 SIMA200208802 1 20020323 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - DURING INSPECTION OF AIRCRAFT, FOUND FORWARD DIGITAL IN GALLEY AREA CORRODED. REMOVED CORROSION BY CUT OUT. FABR ICATED A STRAP, DOUBLERS AND A SHIM IAW EMB145 SRM 145-1142 CHAPTER 53, REV 17, 53-21-10, AND STANDARD SRM PRACTICES. ( M) 2 L 7 2 4F RT T00011AT 2002052300114 20020523 00114 SO 2002 5 23 SIMA200208803 1 20020324 A 5313 STRINGER EMB 145 EMB145 3260210 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - DURING INSPECTION OF AIRCRAFT, FOUND STRINGER 19R CHAFED AT AFT BELLY PANEL. BLENDED OUT CHAFE. FABRICATED A DOU BLER AND SHIMS IAW EMB GST-0898/02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002052300115 20020523 00115 SO 2002 5 23 SIMA200208804 1 20020324 A 5313 STRINGER EMB 145 EMB145 3260210 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - DURING INSPECTION OF AIRCRAFT, FOUND STRINGER 19L CHAFED AT AFT BELLY PANEL. BLENDED OUT CHAFE. FABRICATED A DOU BLER AND SHIMS IAW EMB-GST-0898/02, AND STANDARD PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002052300116 20020523 00116 SO 2002 5 23 SIMA200208805 1 20020322 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 24 BEYOND SRM LIMITS AFTER BLENDING. R EMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, FILLER, AND TWO SHIMS. REPAIRED IAW EMB145 SRM (SRM 145-1142 CHAPTER 53, REV 17) 53-21-10 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002052300117 20020523 00117 SO 2002 5 23 SIMA200208807 1 20020325 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON SERVICE DOOR CENTER SILL. BLENDED CORROSION. FABRICATED A DOUBLER IA W EMB GST-0844/02 ITEM 5, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002052300118 20020523 00118 SO 2002 5 23 SIMA200208808 1 20020320 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY CENTER FLOOR SUPPORT BEYOND SRM LIMITS. REMOVED CORRODED GALLE Y CENTER FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW EMB145 SRM 145-1142 CHAPTER 51, REV 17, 51-40-02, GST-0844/02, ITEM 4, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002052300119 20020523 00119 SO 2002 5 23 SIMA200208809 1 20020327 A 5320 DOUBLER EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM PREVIOUS REPAIR AT FRAME 20. REMOVED PREVIOUS R EPAIR. FABRICATED A DOUBLER ANGLE, FILLER, A PLATE, AND SHIMS. REPAIRED IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 17 R EV 17 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002052300120 20020523 00120 SO 2002 5 23 SIMA200208908 1 20020312 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 35576. RIGHT CABIN SILL HAS CORROSION BETWEEN FRAMES 23-29. (M) 2 L 7 2 4F RT T00011AT 2002052300121 20020523 00121 EU 2002 5 23 SIMA200209601 1 20020406 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 545AT 545 CRW - CREW REPORTED THE FORWARD EMERGENCY EXITS LIGHTS AND NUMEROUS FLOOR PROXIMITY EMERGENCY LIGHTS WERE FOUND TO BE IN OPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE LEFT FORWARD POWER SUPPLY UNIT IAW ATR MM. OPERATI ONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052300122 20020523 00122 EA 2002 5 23 SIMA200209901 1 20020409 A 3350 13F50614903 SIGN CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 503AE 10021 DFW - FLT 3556 - CREW REPORTED THE FORWARD EXTERNAL EMERGENCY EXIT LIGHTS WILL NOT TEST. MAINTENANCE REMOVED AND REPLAC ED OVERHEAD EMERGENCY EXIT SIGN IAW CRJ MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002052300123 20020523 00123 SO 2002 5 23 SIMA200210017 1 20020401 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - THIS IS A LEVEL 2 FINDING, RIGHT FORWARD SILL IN GALLEY HAS CORROSION. REMOVED DAMAGED FORWARD SILL, INSTALLED NE W FORWARD SILL IAW EMB 145 SRM 51-40-02, 51-40-06, 51-20-03. (M) 2 L 7 2 4F RT T00011AT 2002052300124 20020523 00124 SO 2002 5 23 SIMA200210018 1 20020401 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - THIS IS A LEVEL 2 FINDING. RIGHT CENTER SILL IN GALLEY HAS CORROSION. REPAIRED IAW EMB GST-1140/02. (M) 2 L 7 2 4F RT T00011AT 2002052300125 20020523 00125 SO 2002 5 23 SIMA200210019 1 20020401 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 THIS IS A LEVEL 2 FINDING. RIGHT AFT SILL IN GALLEY HAS CORROSION. INSTALLED NEW AFT SILL IAW EMB 145 SRM 51-40-02, 51 -40-06, 51-20-03. (M) 2 L 7 2 4F RT T00011AT 2002052300126 20020523 00126 SO 2002 5 23 SIMA200210020 1 20020401 A 5320 14522461011 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 THIS IS A LEVEL 2 FINDING. AFT DIAMOND GUSSET IN GALLEY HAS CORROSION. INSTALLED SERVICEABLE AFT DIAMOND IAW EMB 145 S RM 51-40-02, 51-20-03, 51-40-06. (M) 2 L 7 2 4F RT T00011AT 2002052300127 20020523 00127 SO 2002 5 23 SIMA200210021 1 20020401 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - THIS IS A LEVEL 2 FINDING. GALLEY CENTER BEAM GUSSET CORRODED. INSTALLED SERVICEABLE GUSSET BEAM IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002052300128 20020523 00128 SO 2002 5 23 SIMA200210022 1 20020401 A 5320 14522459003 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - THIS IS A LEVEL 2 FINDING. GALLEY RAMP SUPPORT CORRODED. INSTALLED SERVICEABLE GALLEY RAMP IAW EMB145 SRM 51-40- 02. (M) 2 L 7 2 4T RT T00011AT 2002052300129 20020523 00129 SO 2002 5 23 SIMA200210023 1 20020401 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145 3260210 SO GALLEY CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - THIS IS A LEVEL 2 FINDING. GALLEY CENTER BEAM CORRODED. INSTALLED SERVICEABLE CENTER BEAM IAW EMB145 SRM 51-40-0 2. (M) 2 L 7 2 4F RT T00011AT 2002052300130 20020523 00130 SO 2002 5 23 SIMA200210024 1 20020401 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 THIS IS A LEVEL 2 FINDING. GALLEY LEFT SILL HAS CORROSION. INSTALLED LEFT SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002052300131 20020523 00131 EU 2002 5 23 SIMA200210025 1 20020227 A 5720 ANGLE AEROSP ATR42 ATR42300 8680920 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP8 INSPECTION, FOUND RIGHT WING REAR SPAR UPPER SPAR ANGLE TO BE CORRODED JUST OUTBOARD OF INBOARD AILER ON HINGE. REPAIRED IAW ATR FAX DO/TE/S560.0401/02-1004. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052300132 20020523 00132 EU 2002 5 23 SIMA200210026 1 20020405 A 5311 S5367131123051 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 FOUND RIGHT FRAME 37 CORRODED ON AFT SIDE JUST ABOVE SILL PLATE CORRODED. REMOVED AND REPLACED FRAME 37 RIGHT IAW SRM 51-25-02 AND 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052300133 20020523 00133 EU 2002 5 23 SIMA200210027 1 20020405 A 5320 S5367800920102 FLOOR SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 FOUND RIGHT FLOOR SUPPORT FROM FRAME 36 TO 38 CORRODED. REMOVED AND REPLACED RIGHT FLOOR SUPPORT IAW ATR42 SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052300134 20020523 00134 2002 5 23 R7MR34981 4 20020307 A 3416 3A433220F281CL ALTIMETER UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE COCKPIT INOPERATIVE B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 102HN 422 0159 ALTIMETER - UNIT INOPERATIVE. WILL NOT DESCEND LESS THAN 5000 FEET. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052300135 20020523 00135 EU 2002 5 23 SIMA200210028 1 20020405 A 5320 S5367800826901 FLOOR SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 FOUND RIGHT FLOOR SUPPORT FROM FRAME 38 TO 39 CORRODED. REMOVED AND REPLACED AND REPLACED RIGHT FLOO R SUPPORT IAW ATR 42 SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052300136 20020523 00136 EU 2002 5 23 R7MR34983 1 20020313 A 2435 23081057 STARTER GEN UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ENGINE INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 102HN 439 0159 STARTER GENERATOR - UNIT INOPERATIVE. ENGINE WOULD NOT START. REPLACED BRUSHES AND STILL NO START. NR1 WOULD NOT RISE HIGHER THAN 7.6 PERCENT. MADE LOUD SOUND. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052300137 20020523 00137 EU 2002 5 23 SIMA200210029 1 20020405 A 5320 S53671318280 SILL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AM 319 SAW - DURING CPCP FOUND SERVICE DOOR SILL PLATE CORRODED. REMOVED AND REPLACED WILL PLATE IAW SRM 51-25-01 AND 51-25-03 . AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052300138 20020523 00138 2002 5 23 R7MR35058 4 20020416 A 2300 9910951 TRANSCEIVER UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE UHF/VHF/LOW/ HI INTERMITTENT B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 102HN 511 0159 UHF/VHF/LOW/HI BAND TRANSCEIVER - UNIT INOPERATIVE. VHF DIGITAL READOUT BECAME INTERMITTENT FOR A FEW DAYS AND THEN WEN T COMPLETLY OUT. TRANSMIT/RECEIVE WORKED FINE, BUT AT WHIDH FREQUENCY IS UNKNOWN. REPLACED WITH NEW UNIT, CORRECTED PR OBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002052300139 20020523 00139 EU 2002 5 23 TI12002F00000 1 20020513 A 2700 11744120 CONTROL ROD BOLKMS 117 BK117B1 5626012 EU FLT CONTROL CRACKED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 311LS 2204 7144 DURING AIRFRAME INSPECTION FOUND THE COLLECTIVE FLIGHT CONTROL ROD END COLLAR CRACKED. 1 G 7 2 3U H13EU 2002052300143 20020523 00143 NM 2002 5 23 02FDEA00335 1 20020516 A 3260 INDICATOR BOEING 727 727200 138407E NM MLG DOOR FALSE ACTIVATION A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 288FE 21850 RED DOOR INDICATOR ON AFTER GEAR RETRACTION DEPARTING DAY. RECYCLED GEAR PER RED TAB PROCEDURE AND LIGHT WENT OUT. C YCLED GEAR DOORS SEVERAL TIMES PER MM 32-62-01. NO DEFECTS NOTED. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2002053100119 20020531 00119 NM 2002 5 31 02FDEA00340 1 20020513 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 SKIN DENTED AT BS 1130 3 INCHES BELOW STR 23 R. REMOVED AND REPLACED SKIN PER SRM 53-30-1 & 53-30-3 FIG 3. 2 L 7 3 4F RT A3WE 2002053100120 20020531 00120 NM 2002 5 31 02FDEA00341 1 20020513 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 SKIN DENTED AT BS 1130 2 INCHES ABOVE STR 25 R. 2 L 7 3 4F RT A3WE 2002060600156 20020606 00156 NM 2002 6 6 02FDEA00342 1 20020513 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 209FE 22931 DENT IN FRAME AT BS 1110 BETWEEN STR 25 - 26 L. REMOVED AND REPLACED FRAME PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2002052900051 20020529 00051 NM 2002 5 29 02FDEA00344 1 20020514 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 HOLES IN SHEAR TIE AND SKIN AT BS 600 BETWEEN STR 27 & 28 L. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4, 51-30-2 & EA 7-5330-54321. 2 L 7 3 4F RT A3WE 2002053100121 20020531 00121 NM 2002 5 31 02FDEA00345 1 20020513 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CORROSION ON FLOORBEAM UPPER SURFACE BS 348, LBL 25-50, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 2002061900192 20020619 00192 NM 2002 6 19 02FDEA00346 1 20020513 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CORROSION ON FLOORBEAM UPPER FLANGE BS 312, LBL 27, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 51-10-1. 2 L 7 3 4F RT A3WE 2002052300144 20020523 00144 WP 2002 5 23 02FDEA00347 1 20020517 A 2510 SEAT DOUG DC10 DC1010 3022110 WP COCKPIT SHORTED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 68059 46907 AT FL330 SMOKE IN COCKPIT, PERFORMED RED TAB PROCEDURES ORIGIN OF SMOKE APPEARED TO BE FROM SECOND OFFICER'S SEAT. PU LLED SECOND OFFICERS SEAT CIRCUIT BREAKERS AND DIVERTED TO KSLC. C/B'S REMAIN PULLED, AND ELECTRICAL CONNECTOR TO SE A CONTROLS IS DISCONNECTED FOR PRECAUTIONARY REASONS. REMOVED AND REPLACED F/E'S CREW SEAT IAW MM 25-11-03-4. OFF MF G 1057D25-10-06 SRL 1143 ON MFG 1057D25-10-06 SRL 1087RW 2 L 7 3 4F A22WE 2002060500203 20020605 00203 NM 2002 6 5 F3LA200200153 1 20020520 A 5347 CARGO TRACK BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 316FL 3574 25264 DURING C-2 CHECK, INSPECTION REPORTED CARGO TRACK AT STA 727A TO 727B, RBL 14, CORRODED AROUND NUT PLATE HOLES. REPLACE D CARGO TRACK PER SRM 51-40-2 AND 51-10-2. 2 L 7 2 4F RT A16WE 2002060500205 20020605 00205 NM 2002 6 5 F3LA200200154 1 20020520 A 5320 FLOOR SUPPORT BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 316FL 3574 25264 DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT CORROSION ON RT SIDE, AFT OF DOOR ON FLOOR-TO-SIDEWALL SUPPO RT. FABRICATED AND INSTALLED SIDEWALL SUPPORT PER SRM 51-20-01, SOPM 20-41-01 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002052300145 20020523 00145 NM 2002 5 23 AWXA200200441 1 20020522 A 3233 654482517 ACTUATOR BOEING 737 7373G7 1384595 NM ZONE 700 - LANDI A AWXA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 WP 28 156AW 37056 13013 23778 TUC - AIR TURN BACK - FLT 0662 - AFTER TAKEOFF FROM TUC EN ROUTE TO PHX THE RIGHT MAIN LANDING GEAR DID NOT RETRACT ON D EPARTURE, TURNED BACK AND LANDED SAFELY AT TUC. MAINTENANCE TROUBLESHOT RETRACTION PROBLEM PER BMM 32-32-00 PG. 101; CYC LED LANDING GEAR FOR 30 MINUTES, COULD NOT DUPLICATE PROBLEM. PERFORMED THERMAL CHECK OF BOTH L/H AND R/H LANDING GEAR A CTUATORS, BOTH WERE THE SAME. PERFORMED PRESSURE CHECK OF R/H MAIN LANDING GEAR DOWNLOCK ACTUATOR, PRESSURE WAS GOOD, WI TH PRESSURE GOOD TROUBLESHOOTING CHART RECOMMENDED REPLACEMENT OF R/H MLG DOWNLOCK ACTUATOR. REPLACED ACTUATOR IAW T/C R 4M32010, OPERATIONAL AND LEAK CHECK WAS GOOD. **SUPPLEMENTAL** SDR WILL BE SUBMITTED UPON RECEIPT OF VENDOR BENCH TEST R 2 L 7 2 4F RT A16WE 2002052300146 20020523 00146 NM 2002 5 23 AWXA200200442 1 20020522 A 3350 BMS13311122 WIRE BOEING 737 73733A 1384673 NM SEAT ROW 16 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 0 0 23625 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 L/H WAS FOUND INOPERATIVE. MAINTENANCE SPLI CED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 L/H PER CHAP. 20 WIRING PRACTICES, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002052300147 20020523 00147 EU 2002 5 23 AWXA200200443 1 20020522 A 3350 E0052R8B3APNE CONNECTOR AIRBUS 320 A320231 3930325 EU SEAT ROW 22 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 0 0 091 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 L/H WAS FOUND INOPERATIVE. MAINTENANCE FOUN D A WALL CONNECTOR DAMAGED WITH A WIRE PULLED OUT FROM BACKSHELL, REPLACED EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT WALL OF SEAT ROW 22 L/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002052400001 20020524 00001 2002 5 24 2002F00508 4 20020312 A 2565 D31517113 SLIDE AIRBUS 320 A320214 3930316 EU L2 DOOR DEPLOYED A RYNA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 GBXKD 0735 L2 SLIDE INADVERTENTLY DEPLOYED AT THE GATE IN PVR. (M) 2 L 7 2 4F RT A28NM 2002052400002 20020524 00002 NM 2002 5 24 2002F00509 1 20020306 A 5530 FRAME BOEING 727 727225 1384077 NM VERTICAL STAB CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 801EA 22432 AT C-CHECK FOUND VERTICAL STABILIZER FRAME CRACKED AT LEFT SIDE STATION 180.6 STRINGER 6. (M) 2 L 7 3 4F A3WE 2002052400003 20020524 00003 NM 2002 5 24 2002F00510 1 20020301 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 801EA 22432 AT C-CHECK, FOUND AFT CARGO PIT FLOORBEAM CORRODED AT STATION 1030 STRINGER 28R. (M) 2 L 7 3 4F A3WE 2002052400004 20020524 00004 NM 2002 5 24 2002F00511 1 20020301 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 801EA 22432 AT CHECK, FOUND AFT CARGO FLOORBEAM EXFOLIATED AT STATION 1030 STRINGER 30. (M) 2 L 7 3 4F A3WE 2002052400005 20020524 00005 NM 2002 5 24 2002F00512 1 20020224 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 801EA 22432 AT C-CHECK, FOUND CABIN SEAT TRACK FLANGE CORRODED AT STATION 620 RBL 48. (M) 2 L 7 3 4F A3WE 2002052400006 20020524 00006 NM 2002 5 24 2002F00513 1 20020118 A 5311 FRAME BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 AT C-CHECK, FOUND CRACKED FRAME (INSIDE COCKPIT) AT LEFT STATION 294.5 STRINGER 4L. (M) 2 L 7 3 4F A3WE 2002052400007 20020524 00007 NM 2002 5 24 2002F00514 1 20020117 A 5330 SKIN BOEING 727 727222 1384073 NM FUSELAGE GOUGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 AT -CHECK, FOUND LEFT LOWER FUSELAGE SKIN GOUGED AT STATION 1200 19 AND 20L. (M) 2 L 7 3 4F A3WE 2002052400008 20020524 00008 NM 2002 5 24 2002F00515 1 20020117 A 7931 36165 BRACKET BOEING 727 727222 1384073 NM NR 2 ENGINE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 AT C-CHECK, FOUND LOWER MOUNT BRACKET FOR THE OIL PRESSURE LIGHT SWITCH ON NR 2 ENGINE CRACKED. (M) 2 L 7 3 4F A3WE 2002052400009 20020524 00009 NM 2002 5 24 2002F00516 1 20020117 A 5753 SKIN BOEING 727 727222 1384073 NM T/E FLAP CHAFED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 AT C-CHECK, FOUND RIGHT INBOARD MID FLAP UPPER SKIN CHAFFED AT OUTBOARD SIDE WBL 243. (M) 2 L 7 3 4F A3WE 2002052400010 20020524 00010 WP 2002 5 24 GTIA020290 1 20020416 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 801NK 48048 BWI - FLT 2916 - THE EMERGENCY LIGHT PATH HAS SOME RED BULBS INOPERATIVE AT ROW 22. REPAIRED WIRING IAW MM 20-50-01. O PS OK. (M) 2 L 7 2 4F A6WE 2002052400011 20020524 00011 WP 2002 5 24 GTIA020291 1 20020416 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 801NK 48048 BWI - FLT 2916 - FOUND EMERGENCY LIGHT HAS AN INOPERATIVE BULB AT ROW 34. REPAIRED WIRING IAW MM 20-50-00. OPS OK. (M ) 2 L 7 2 4F A6WE 2002052400012 20020524 00012 2002 5 24 GTIA020292 4 20020417 A 2210 AUTOPILOT SYS DOUG DC9 DC9 3022002 WP COCKPIT MALFUNCTIONED A GTIA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 GL 23 130NK 47604 AEX - AUTOPILOT TURNS A/C RIGHT WITH TURN KNOB CENTERED AUTOPILOT OVER TRIMS AIRCRAFT DURING TURNS RESULTING IN LARGE OU T OF TRIM CORRECTIONS. (M) 2 L 7 2 4F A6WE 2002052400013 20020524 00013 WP 2002 5 24 GTIA020293 1 20020418 A 2612 CONNECTOR DOUG DC9 DC983 3022083 WP FIRE LOOP DIRTY A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 825NK 53012 DTW - FLT 9825 - FOUND RIGHT ENGINE FIRE DETECTOR LOOP 'A' LIGHT ILLUMINATED IN FLIGHT. ALL OTHER ENGINE INDICATIONS NO RMAL. CLEAN RIGHT ENGINE FIRE LOOP 'A' CONNECTOR, AND PERFORMED FIRE SYSTEM TEST, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2002052400014 20020524 00014 NM 2002 5 24 QXEA0200772 1 20020502 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 2 SEAT TRACK IS CORRODED ON INNER AND UPPER SURFACES AT STATION X437.5 - X440. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052400015 20020524 00015 NM 2002 5 24 QXEA0200773 1 20020502 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 2 SEAT TRACK IS CORRODED ON INNER AND UPPER SURFACES AT STATION X467 - X470. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052400016 20020524 00016 NM 2002 5 24 QXEA0200774 1 20020502 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX-NR 2 SEAT TRACK IS CORRODED ON INNER AND UPPER SURFACES AT STATION X484 - X486. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052400017 20020524 00017 NM 2002 5 24 QXEA0200775 1 20020430 A 3230 FITTING DHAV DHC8 DHC8202 2809007 NM LT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR FITTING, ADJACENT MATING SURFACE HAS SMALL AREA OF CORROSION BELOW UPP ER ATTACH HOLE FOR FITTING. REPAIRED IAW RD-8 54-1178. 2 H 7 2 4T RT A13NM 2002052400018 20020524 00018 NM 2002 5 24 QXEA0200776 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 10 SEAT TRACK CORRODED ON UPPER AND INNER SURFACES AT STATION X405 - X408. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052400019 20020524 00019 NM 2002 5 24 QXEA0200777 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 10 SEAT TRACK CORRODED ON UPPER AND INNER SURFACES AT STATION X422 - X424. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052400020 20020524 00020 NM 2002 5 24 QXEA0200778 1 20020502 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 11 SEAT TRACK CORRODED ON UPPER AND INNER SURFACES AT STATION X436 - X439. REPAIRED IAW RD-8 1342. 2 H 7 2 4T RT A13NM 2002052400021 20020524 00021 NM 2002 5 24 QXEA0200779 1 20020502 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 11 SEAT TRACK IS CORRODED ON UPPER AND INNER SURFACES AT STATION X452 - X454. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052400022 20020524 00022 NM 2002 5 24 QXEA0200780 1 20020502 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 11 SEAT TRACK IS CORRODED ON UPPER AND INNER SURFACES AT STATION X484 - X487. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052400023 20020524 00023 NM 2002 5 24 QXEA0200781 1 20020502 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 11 SEAT TRACK IS CORRODED ON UPPER AND INNER SURFACES AT STATION X498 - X501. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052400024 20020524 00024 NM 2002 5 24 QXEA0200782 1 20020508 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 8 SEAT TRACK HAS LIGHT SURFACE CORROSION ON OUTBOARD FLANGE AT STATION X442 - X478. REPAIRED IAW RD-8 53-1339, RD-8 53-4473 AND RD-8 53-4472. 2 H 7 2 4T RT A13NM 2002052400025 20020524 00025 NM 2002 5 24 QXEA0200783 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 8 SEAT TRACK IS CORRODED ON UPPER SURFACE AT STATION X484 - X486. REPAIRED IAW RD-8 53-4473, RD-8 53-4472 AND S RM 51-40-11. 2 H 7 2 4T RT A13NM 2002052400026 20020524 00026 NM 2002 5 24 QXEA0200784 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 8 SEAT TRACK IS CORRODED ON UPPER SURFACE AT STATION X514.5 - X516. REPAIRED IAW RD-8 53-4473, RD-8 53-4472 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002052400027 20020524 00027 NM 2002 5 24 QXEA0200785 1 20020506 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 4 SEAT TRACK HAS MULTIPLE AREAS OF CORROSION BEYOND LIMITS. REPAIRED IAW RD-8 53-1102, RD-8 53-2075, SRM 51-40- 11, SRM 51-40-00 AND RD-8 53-4473. 2 H 7 2 4T RT A13NM 2002052400028 20020524 00028 NM 2002 5 24 QXEA0200786 1 20020506 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 7 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002052400029 20020524 00029 NM 2002 5 24 QXEA0200787 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 10 SEAT TRACK CORRODED ON UPPER AND INNER SURFACES AT STATION X265 - X268. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052400030 20020524 00030 NM 2002 5 24 QXEA0200788 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 10 SEAT TRACK CORRODED ON UPPER AND INNER SURFACES AT STATION X278 - X280.5. REPAIRED IAW RD -8 53-1342. 2 H 7 2 4T RT A13NM 2002052400031 20020524 00031 NM 2002 5 24 QXEA0200789 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 10 SEAT TRACK CORRODED ON UPPER AND INNER SURFACES AT STATION X295 - X298. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052400032 20020524 00032 NM 2002 5 24 QXEA0200790 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 10 SEAT TRACK CORRODED ON UPPER AND INNER SURFACES AT STATION X310 - X313. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052400033 20020524 00033 NM 2002 5 24 QXEA0200791 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 10 SEAT TRACK CORRODED ON UPPER AND INNER SURFACES AT STATION X327 - X330. REPAIRED IAW RD-8 53-1342. 2 H 7 2 4T RT A13NM 2002052400034 20020524 00034 NM 2002 5 24 QXEA0200792 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 10 SEAT TRACK CORRODED ON UPPER AND INNER SURFACES STATION X341 - X343. REPAIRED IAW RD-8 53-1342, SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002052400035 20020524 00035 NM 2002 5 24 QXEA0200793 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 10 SEAT TRACK CORRODED ON UPPER AND INNER SURFACES AT STATION X360 - X363. REPAIRED IAW RD-8 53-1342, SRM 51-40 -00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002052400036 20020524 00036 WP 2002 5 24 GTIA020294 1 20020420 A 3231 LATCH DOUG DC9 DC932 3022066 WP LT MLG DOOR OUT OF ADJUST A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 12536 47113 DTW - FLT 9536 - FOUND LEFT LANDING GEAR UNSAFE LIGHT AND DOOR OPEN LIGHT REMAINED ON AFTER GEAR RETRACTION. GEAR RECYC LED IAW QRH SAME INDICATIONS. FOUND LEFT MAIN GEAR DOOR LATCH MECHANISM ASSEMBLY OUT OF ADJUSTMENT. ADJUSTED AND PERFO RMED TEST IAW DC-9. OPS CHECKS GOOD. (M) 2 L 7 2 4F A6WE 2002052400037 20020524 00037 WP 2002 5 24 GTIA020295 1 20020421 A 3230 59164605509 CONTROL VALVE DOUG DC9 DC932 3022066 WP LT MLG MALFUNCTIONED A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 12536 47113 DTW - FLT 9536 - LEFT GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR UP. RECYCLED GEAR. UPLATCH CHECK GEAR DOOR OPEN LIGHT IL LUMINATED. REPLACED LANDING GEAR CONTROL VALVE AND ADJUSTED LEFT GEAR DOOR LATCH MECH. PERFORMED GEAR SWING. ALL SATI SFACTORY AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002052400038 20020524 00038 WP 2002 5 24 GTIA020296 1 20020421 A 3260 UPLOCK SWITCH DOUG DC9 DC932 3022066 WP LT MLG FAULTY A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 12536 47113 FLT 8019 - DTW - PUT GEAR UP, LEFT GEAR UNSAFE LIGHT CAM ON, UP LATCH CHECK RED LIGHT STAYED ON AND GEAR DOOR LIGHT (AMB ER) CAME ON COMPLETED QRH PROCEDURE. REPLACED LT MLG UPLOCK SWITCH AND LT MLG DOOR SWITCH. VERIFIED LANDING GEAR RIGGI NG. NO DEFECTS. LUBED LT MLG. INSPECTION LT MLG BUMPER CLEARANCES. CHECKED UPLATCH HOOK AND ROLLER. ALL SATISFACTOR Y ON GEAR SWING. (M) 2 L 7 2 4F A6WE 2002052400039 20020524 00039 WP 2002 5 24 GTIA020297 1 20020419 A 2612 FIRE LOOP DOUG DC9 DC983 3022083 WP RT ENGINE MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 825NK 53012 DTW - FLT 902 - FIRE DET LOOP 'A' ON RT ENGINE ILLUMINATED IN FLIGHT. PERFORMED 'QRH' PROCEDURE-LGT EXTINGUISHED WHEN ' B' SELECTED. FLEW ON TO DTW. REMOVED AND REPLACED SENSING DETECTION LOOP FROM ENGINE NR 2. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2002052400040 20020524 00040 WP 2002 5 24 GTIA020298 1 20020417 A 2730 CONNECTOR DOUG DC9 DC982 3022082 WP ELEVATOR LOOSE A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 812NK 48021 MCO - FLT 1301 - ELEVATOR POWER ON LIGHT ILLUMINATED WOULD NOT GO OUT. TROUBLESHOT PSI SWITCH TO HAVE LOOSE CANNON PLUG , CLEANED PLUG. OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2002052400041 20020524 00041 WP 2002 5 24 GTIA020299 1 20020418 A 3260 SENSOR DOUG DC9 DC983 3022083 WP LT MLG DIRTY A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 16892 49391 LAX - FLT 906 - ON DEPARTURE FROM DTW, GOT LEFT GEAR UNSAFE LIGHT ALL OTHER LIGHTS OUT PASSING THROUGH 20,000 FEET GOT G EAR DOOR OPEN LIGHT. APPEARS MECH LATCH DID NOT HOLD. RAN QRH PROCEDURES. LIGHTS WENT OUT BASED UPON AIRCRAFT HANDLIN G LEFT GEAR DOOR WAS FLYING. WHEN WE GOT GEAR DOOR OPEN LIGHT LEFT PUMPS ON HIGH REMAINDER OF TRIP. CHECK LEFT GEAR PR OX SENSORS FOR ANY DAMAGE, NONE FOUND. CLEANED SENSORS AND PERFORMED PSEU TARGET TEST. OPS CHECK NORMAL. CHECKED MECH LOCK FOR DEFECTS NONE FOUND. OK FOR FLIGHT. (M) 2 L 7 2 4F RT A6WE 2002052400042 20020524 00042 WP 2002 5 24 GTIA020300 1 20020417 A 2760 3923153563 BAR DOUG DC9 DC983 3022083 WP LT SPOILER CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 602CA 49415 DTW - FOUND LEFT INBOARD SPOILER TORSION BAR AND CAM CORRODED. REMOVED AND REPLACED LEFT INBOARD SPOILER TORSION BAR AN D CAM IAW MD80 MM 27-61-06. (M) 2 L 7 2 4F RT A6WE 2002052400043 20020524 00043 WP 2002 5 24 GTIA020301 1 20020417 A 5753 PANEL DOUG DC9 DC983 3022083 WP T/E FLAP CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 602CA 49415 DTW - FOUND LEFT WING, FIXED VANE FILLER PANEL CRACKED. REPAIRED IAW MD80 57-01. (M) 2 L 7 2 4F RT A6WE 2002052400044 20020524 00044 WP 2002 5 24 GTIA020302 1 20020418 A 5751 ACCESS PANEL DOUG DC9 DC983 3022083 WP AILERON CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 602CA 49415 DTW - FOUND LEFT WING AILERON OUTBOARD ACCESS PANEL CRACKED. REPLACED LT WING AILERON OUTBOARD ACCESS PANEL. (M) 2 L 7 2 4F RT A6WE 2002052400045 20020524 00045 WP 2002 5 24 GTIA020304 1 20020322 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND MEMBRANE PANEL CRACKED/DAMAGED AT CORNERS STATION 826-927 RIGHT SIDE. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2002052400046 20020524 00046 WP 2002 5 24 GTIA020305 1 20020325 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND MEMBRANE PANEL AT STATION 973 TO STATION 1003 RIGHT SIDE HAS CRACKED AND PEELING OFF. STOPPED DRILLED THE C RACK. (M) 2 L 7 2 4F A6WE 2002052400047 20020524 00047 WP 2002 5 24 CALA0200314 1 20020524 A 5311 SR0953008681 FRAME DOUG DC9 DC982 3022082 WP STA1416 L2L CRACKED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 83870 48056 TAIL COMPARTMENT CANT CRACKED AT STATION 1416 AT L2. REPALCED CANT FRAME PER SRM 51-10-3. 2 L 7 2 4F A6WE 2002052400048 20020524 00048 WP 2002 5 24 CALA0200317 1 20020523 A 5311 7075T6063 FRAME DOUG DC9 DC982 3022082 WP FS1309-1322 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 AFT PIT STATION 1322 - 1309 AT L28 - L27 FRAME CORRODED. REMOVED FABRICATED AND REINSTALLED FRAME PER SRM 53-01 FIG1, 51 -30-2, 51-30-5, AND 51-10-03. 2 L 7 2 4F A6WE 2002052400049 20020524 00049 WP 2002 5 24 GTIA020306 1 20020320 A 5720 ATTACH ANGLE DOUG DC9 DC981 3022081 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - RIGHT WING CRACK AT ANGLE ATTACH NOSE CAP VORTILON. REMOVED VORTILON FAIRING ATTACH ANGLE. STOP DRILLED CRACK AN GLE. UPON REMOVAL OF VERTICAL ANGLE FITTING FOUND TO BE CRACKED. FABRICATED REPAIR DOUBLERS. LOCATED AND DRILLED HOLE S IN NEW ATTACH ANGLE. INSTALLED REPAIR. INSTALLED FITTING. (M) 2 L 7 2 4F A6WE 2002052400050 20020524 00050 WP 2002 5 24 GTIA020307 1 20020324 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR PANEL STATION 598-636 IS CRACKED/DAMAGE MID PIT. FORM NEW PANEL. (M) 2 L 7 2 4F A6WE 2002052400051 20020524 00051 WP 2002 5 24 GTIA020308 1 20020324 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FLIGHT COMPT FLOOR PANEL UNDER CAPTS SEAT HAS CRACKED/DAMAGE. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2002052400052 20020524 00052 WP 2002 5 24 GTIA020309 1 20020327 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FLIGHT AND FORWARD PASSENGER COMPARTMENT FLOOR PANEL RIGHT STATION 148.5 TO STATION 167.5 HAS CRACKED/DAMAGE MUSHY . FABRICATED NEW PANEL. (M) 2 L 7 2 4F A6WE 2002052400053 20020524 00053 WP 2002 5 24 GTIA020310 1 20020318 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND RIGHT EXTERIOR FUSELAGE SKIN CRACKED AT STATION Y 1381 LONGERON 14R. REMOVED DAMAGE AT STATION 1381 LONGERO N 14R. FABRICATED DOUBLER AND FILLER. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2002052400054 20020524 00054 WP 2002 5 24 GTIA020311 1 20020324 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FLIGHT AND FORWARD PASSENGER COMPARTMENT FLOOR PANEL RIGHT OUTBOARD STATION 148.5 TO STATION 167.5 HAS CRACKED MUS HY (SOFT). FORM NEW PANEL FOR STATION 148.5-167.5. (M) 2 L 7 2 4F A6WE 2002052400055 20020524 00055 WP 2002 5 24 GTIA020312 1 20020324 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - PASSENGER COMPARTMENT FLOOR PANEL LEFT INBOARD STATION 1271-1309 HAS CRACKED MUSHY SOFT. FABRICATED REPAIR FLOORB OARD. (M) 2 L 7 2 4F A6WE 2002052400056 20020524 00056 WP 2002 5 24 GTIA020313 1 20020324 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - PASSENGER COMPARTMENT FLOOR PANEL AT STATION 1271-1309 HAS CRACKED/DAMAGE. FABRICATED NEW PANEL. (M) 2 L 7 2 4F A6WE 2002052400057 20020524 00057 WP 2002 5 24 GTIA020314 1 20020324 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FLIGHT AND FORWARD PASSENGER COMPARTMENT FLOOR PANEL STATION 148.5-167.5 HAS CRACKED/DAMAGE. (M) 2 L 7 2 4F A6WE 2003040700054 20030407 00054 EU 2003 4 7 RU3A02003 1 20020419 A 2170 8323712 COALESCER BAG BRAERO DH125 BAE125800A 1500285 EU A/C SYSTEM CONTAMINATED A RU3A A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 94 258129 DURING CRUISE AT 10,000 FT, ACRID ODOR, CHECKED NO C/B'S POPPED. WITHIN 1 MIN OF 1ST ODOR, WHITE/GREY SMOKE APPEARED. COULD NOT ISOLATE. WENT ON OXYGEN, RAM DUMPED CABIN PRESS, DECLARED AN EMERG, & DESCENDED. RAN SMOKE/FUMES & ELEC FIR E C/L. LANDED & EMERG EGRESSED ON TAXIWAY. MAINT RAN NR 1 & NR 2 ENGS. SELECTED NR 1 MAIN AIR VALVE TO OPEN, REMOTE PRESENCE OF ODOR, NO SMOKE/VAPOR DETECTED. NR 1 & NR 2 MAIN AIR VALVES OPEN, NO ADD ODOR, AFTER 30 SEC, ODOR CLEARED. R & I AIR CON SYS WATER SEP ASSY. FOUND WATER SOCK SATURATED WITH WATER & SOOT. R & R WATER SOCK. PERFORMED GROUND RU N NR 2 WITH SYSTEMS POWERED, ENG RUN AT T/O POWER, REDUCED POWER TO IDLE FOR 60 MIN. NO SMOKE OR ODOR DETECTED. 2 L 7 2 4F RT A3EU 2002052400058 20020524 00058 EU 2002 5 24 SIMA200210030 1 20020405 A 5320 S53671217298 SILL DRAIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 FOUND SERVICE DOOR SILL DRAIN TRACK CORRODED. REMOVED AND REPLACED SILL PLATE DRAIN TRACK IAW SRM 51 -25-01 AND 51-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002052400059 20020524 00059 SO 2002 5 24 SIMA200210701 1 20020403 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - THIS IS A LEVEL 2 FINDING. RIGHT OMEGA BEAM HAS CORROSION BETWEEN FRAMES 23 AND 25. FABRICATED DOUBLER IAW EMB14 5 SRM 51-40-02, 51-40-06, 51-20-03 AND GST-1169/02. (M) 2 L 7 2 4F RT T00011AT 2002052400060 20020524 00060 SO 2002 5 24 SIMA200210702 1 20020401 A 5320 DOUBLER EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - THIS IS A LEVEL 2 FINDING. LEFT OMEGA BEAM REPAIR AT FRAME 20 HAS MINOR CORROSION. INSTALLED NEW OMEGA BEAM REPA IR AT FRAME 20 IAW EMB GST-1140-/02 AND SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002052400061 20020524 00061 SO 2002 5 24 SIMA200210703 1 20020320 A 5320 14529150001 CROSSBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 ABI - THIS IS A LEVEL 2 FINDING. GALLEY CROSSBEAM AND PROFILE CORRODED. REMOVED AND INSTALLED NEW GALLEY CROSSBEAM IAW EMB 145 51-40-02, 51-40-06, 51-20-03. (M) 2 L 7 2 4F RT T00011AT 2002052400062 20020524 00062 SO 2002 5 24 SIMA200210704 1 20020401 A 5320 14522459003 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - THIS IS A LEVEL 2 FINDING. PASSENGER ENTRY FLOORBOARD SUPPORT HAS CORROSION. INSTALLED NEW FLOORBOARD SUPPORT IA W EMB 145 SRM 51-40-02, 51-40-03, 51-40-06. (M) 2 L 7 2 4F RT T00011AT 2002052400063 20020524 00063 SO 2002 5 24 SIMA200210705 1 20020401 A 5320 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - THIS IS A LEVEL 2 FINDING. RIGHT CABIN FORWARD FLOOR SUPPORT HAS CORROSION. BLENDED CORROSION, RESTORED PROTECTI VE TREATMENT, ACCEPTED AS IS IAW EMB 145 GST-1140/02. (M) 2 L 7 2 4F RT T00011AT 2002052400064 20020524 00064 SO 2002 5 24 SIMA200210706 1 20020401 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 THIS IS A LEVEL 2 FINDING. LEFT OMEGA BEAM HAS CORROSION BETWEEN FRAMES 22 AND 23. BLENDED CORROSION, PERFORMED NDT, R ESTORED PROTECTIVE FINISH, ACCEPTED AS IS IAW EMB GST-1140/02. (M) 2 L 7 2 4F RT T00011AT 2002052400065 20020524 00065 2002 5 24 SWAA021115 4 20020521 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT CABIN DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED C2 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PE R MM. 2 L 7 2 4F RT A16WE 2002052400066 20020524 00066 NM 2002 5 24 SWAA021117 1 20020522 A 5240 6545871 FRAME BOEING 737 7373Q8 1384670 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED ABOVE AND INBD OF LOWER STOP. REMOVED AND REPLACED SVC DOOR PER MM. 2 L 7 2 4F RT A16WE 2002052400067 20020524 00067 NM 2002 5 24 SWAA021118 1 20020521 A 5312 6516300 WEB BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 201 AND RBL 5.0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002052400068 20020524 00068 NM 2002 5 24 SWAA021121 1 20020522 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT STR 10R, BETWEEN BS 496 AND BS 505 AND STR 15R, BS 505. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002052400069 20020524 00069 NM 2002 5 24 SWAA021122 1 20020522 A 5311 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002052400070 20020524 00070 NM 2002 5 24 SWAA021123 1 20020520 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED C3 CHECK, FOUND SKIN CRACKED AT FWD SVC DOOR CUT OUT LOWER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002052400071 20020524 00071 SO 2002 5 24 SIMA200210707 1 20020401 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - THIS IS A LEVEL 2 FINDING. LEFT OMEGA BEAM CORRODED AT FRAME 25. BLENDED CORROSION, PERFORMED NDT, RESTORED PROT ECTIVE FINISH, ACCEPTED AS IS IAW EMB 145 GST-1140/02. (M) 2 L 7 2 4F RT T00011AT 2002052400072 20020524 00072 SO 2002 5 24 ASO2002F00005 1 20020430 A 5300 12006173009 STRINGER EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C CHECK INSPECTION , STRINGER 18 LEFT WAS FOUND CORRODED BETWEEN FRAMES 16 AND STA 6653.1. THE STRINGER SPLICE AT FRAME 16 WAS ALSO FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER AND STRINGER SPLICE IAW SRM . 2 L 7 2 4T 4 T RT A31SO E20NE 2002060500202 20020605 00202 NM 2002 6 5 F3LA200200152 1 20020521 A 2612 655280915 FIRE DETECTOR BOEING 737 7372Y5 1384554 NM NR 1 ENGINE FALSE ACTIVATION A F3LA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 NM 03 118RW 641 23040 UPON ARRIVAL AT GATE, FLIGHT CREW REPORTED THE FIRE BELL SOUNDED AND THE NR 1 ENGINE FIRE HANDLE WAS ILLUMINATED. PULLE D NR 1 FIRE HANDLE AND DISCHARGED THE LEFT BOTTLE INTO THE NR 1 ENGINE. INSPECTED NR 1 ENGINE FOR EVIDENCE OF FIRE, NON E FOUND. INSPECTED FIRE DETECTION SYSTEM FOR DEFECTS PER MM 26-11-0. NO DEFECTS NOTED. INSPECTED FIRE LOOP. NO DEFEC TS NOTED. REPLACED FIRE DETECTION UNIT, FIRE CONTROL MODULE AND NR 1 ENGINE FIRE BOTTLE, RAN ENGINE FOR SEVERAL MINUTES AND NO DEFECTS WERE NOTED. 2 L 7 2 4U RT A16WE 2002052400073 20020524 00073 SO 2002 5 24 SIMA200210708 1 20020401 A 5320 CROSSBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - THIS IS A LEVEL 2 FINDING. GALLEY RIGHT CROSSBEAM HAS CORROSION AT NUTPLATE FORWARD OF CROSSBEAM AND PROFILE. RE PAIRED IAW EMB145 GST-1140/02, SRM 51-40-02, 51-40-06, 51-40-03. (M) 2 L 7 2 4F RT T00011AT 2002052400074 20020524 00074 SO 2002 5 24 SIMA200210709 1 20020409 A 3210 14571033009 CAP EMB 145 EMB145LR 3260212 SO RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 639AE 145182 ABI - THIS IS A LEVEL FINDING. RIGHT MAIN LANDING GEAR FORWARD MAIN BEARING CAP IS CORRODED. INSTALLED NEW CAP IAW EMB 145 AMM 32-10-01 AND 32-10-03. (M) 2 L 7 2 4T RT T00011AT 2002052400075 20020524 00075 SO 2002 5 24 SIMA200210710 1 20020410 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION IN TWO AREAS, FORWARD AND AFT, ON FORWARD DIGITAL. REMOVED CORROSION B Y BLENDING AREAS. FABRICATED TWO REPAIR DOUBLERS. REPAIR DONE IAW EMB GST-1140/02, DAMAGE NR 9, GST-1169/02, ITEM 4, A ND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002052400076 20020524 00076 SO 2002 5 24 SIMA200210711 1 20020409 A 5320 DOUBLER EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20. REMOVED PREVIOUS REPAIR (CORROSION LIMITED TO PREVIOUS REPAIR). FABRICATED A DOUBLER ANGLE, AND FILLER. REPAIRED IAW EMB145 SR M-145/1142, CHAPTERS 53, REV 17, 53-21-10, GST-1140/02 DAMAGE NR 11 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002052400077 20020524 00077 SO 2002 5 24 SIMA200210713 1 20020409 A 5320 BEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - DURING ABV INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY RIGHT BEAM AT FRAME 23. REMOVED CORROSION BY BLENDIN G. FABRICATED A U-SHAPE REPAIR. REPAIRED IAW EMB GST-1140/02, DAMAGE NR 7 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002052400078 20020524 00078 NM 2002 5 24 TSAA0233117 1 20020424 A 3350 9221009 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 2002052400079 20020524 00079 EA 2002 5 24 COMA0260327 1 20020522 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 436CA 7482 FLIGHT 5406 - DURING APPROACH INTO CVG RECEIVED A FLAP FAIL CAUTION MESSAGE AT 0 DEGREE FLAP POSITION, CREW DECLARED AN EMERGENCY, AIRCRAFT LANDED SAFELY.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENNACE ACTION, PARAG APH (B) 1,2,3 (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTIN MESSAGES. 2 L 7 2 4F RT A21EA 2002052400080 20020524 00080 EA 2002 5 24 COMA0260328 1 20020521 A 3260 61750 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA WHEEL WELL FAILED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 920CA 20117 7022 FLIGHT 5205 - WHILE TAXING TO THE GATE RECEIVED A GEAR DISAGREE WARNING MESSAGE, AIRCRAFT ARRIVED AT THE GATE SAFELY.REP LACED THE MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002052400081 20020524 00081 EA 2002 5 24 COMA0260329 1 20020522 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA A COMA K NONE S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 409CA 7441 FLIGHT 5100 - DURING PRE FLIGHT INSPECTION DISCOVERED CEILING EMERGENCY LIGHITNG INOPERATIVE AT ROW 13.TRANSFERRED INOPE RATIVE LIGHTING TO DEFERRED DISCREPANCY LIST PER MEL 33-51-01. 2 L 7 2 4F RT A21EA 2002052400082 20020524 00082 EA 2002 5 24 COMA0260330 1 20020521 A 3260 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NOSE SECTION FAILED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 920CA 784 7022 FLIGHT 5205 - WHILE TAXING TO THE GATE RECEIVED A GEAR DISAGREE WARNING MESSAGE, AIRCRAFT ARRIVED AT THE GATE SAFELY.REP LACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002071500057 20020715 00057 NM 2002 7 15 UPS02438358 1 20020519 A 7830 SKIN BOEING 747 747200 1384847 NM THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:N/A NR 4 ENG HONEYCOMB SKIN CRACKED 3 O'CLOCK POS INSIDE ON INSIDE OF T/R A/C FERRIED TO HKG FOR C CHECK REPAIR TO BE COMPLETED. NR 4 ENG T/R SLEEVE INNER SKIN CRACKED AND DELAM AREA REPAIRED REF SRM 54-34-03 FIG 26. 2 L 7 4 4F RT A20WE 2002052400084 20020524 00084 CE 2002 5 24 CA020419003 1 20020404 A 7620 77GB408R4A18 RELAY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE ENGINE CONTROLS CORRODED W K NONE L NO TEST IN INSP/MAINT 1 CA 14010 14010 (CAN) DURING PREFLIGHT CHECK PILOT PULLED THE FIRE HANDLE TO CHECK THE FUEL SHUTOFF VALVE OPERATION, WHEN HE PUSH IT BAC K THE VALVE STAYED CLOSED.AFTER INVESTIGATION WE FOUND ALL THE CONTACT ON RELAY (A236K1)CORRODED AND FEW PIN BROKEN. RE LAY AND WIRE WAS REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002052400085 20020524 00085 NM 2002 5 24 CA020507001 1 20020501 A 2420 TRANSFORMER BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE MALFUNCTIONED W O OTHER H F J ELECT. POWER LOSS-50 PC FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 CA (CAN) DURING FLIGHT NUMEROUS MOMENTARY POWER INTERUPTION CAUSING AUTO PILOT TO DISENGAGE AND NUMEROUS INSTRUMENT WARNING FLAGS. FOUND TO BE THE NR 1 ENGINE CURRENT TRANSFORMER AT FAULT. TRANSFORMER REPLACED. AIRCRAFT TIME 53656HRS 2 L 7 2 4F 4 F A16WE E2EA 2002052400087 20020524 00087 2002 5 24 CA020515001 4 20020509 A 2562 ELT SNIAS 350 AS350D 8680803 EU LYC LTS101 LTS101600A3 41560 NE CABIN FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA (CAN) AIRCRAFT ABOVE CRASHES PILOT REMOVES ELT GOES TO HIGH GROUND AND TURNS ELT ON. NO REPORTED ELT SWEEP ON FIG 121.5 WHEN ELT RECOVERED SWITCH WAS TURNED ON. 1 G 7 1 3U 3 U H9EU E5NE 2002052400089 20020524 00089 NM 2002 5 24 AWXA200200446 1 20020522 A 2560 694995613 CABLE BOEING 737 73733A 1384673 NM R2 DOOR FRAYED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 0 0 23634 PHX - EMERGENCY EVACUATION - DURING INSPECTION FOUND FRAYED R-2 DOOR ESCAPE SLIDE RELEASE CABLE. MAINTENANCE REMOVED AND REPLACED FRAYED RELEASE CABLE AT R2 DOOR, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002052400090 20020524 00090 NM 2002 5 24 AWXA200200447 1 20020505 A 5330 65458001205 SKIN BOEING 737 7373Q8 1384670 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 0 0 23507 MCN - MAJOR REPAIR - DURING C-15 CHECK HFEC INDICATED 3 EACH CRACKS EMANATING FROM COUNTER SINK FASTENER HOLES ON FUSELA GE EXTERNAL SKIN AT LOWER AFT CORNER OF R1 DOOR CUTOUT, BS 327.75, BS 327, AND BS 326.25, WL 212.3, WL 211, AND WL 210 RESPECTIVELY, 10X VISUAL CONFIRMED. MAINTENANCE TRIMMED OUT 3 EACH CRACKS FROM LOWER AFT CORNER OF R1 DOOR CUTOUT; PERFO RMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 3 EACH REPAIR PLATES AND 3 EACH FILLERS; INSTALLED REPAIR PAR TS AT BS 317 TO BS 339 R/H, WL 207.5 IAW AWA ER 03-5331-02141-KB3. 2 L 7 2 4F RT A16WE 2002052400091 20020524 00091 NM 2002 5 24 C7WA200200002 1 20020521 A 5610 5893543109 WINDSHIELD BOEING 727 727200 138407E NM BROKEN A C7WA A B G I UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED CABIN DEPRESSURIZATION O Z OTHER SIGNIFICANT FAILURE REPORT CR CRUISE 1 SO 17 902PG 20725 CRUISING AT 33,000 FEET FROM DAY TO BOS CAPTAINS L-1 WINDSHIELD OUTER AND INNER PANES SHATTERED. AIRSPEED WAS MACH .76. DONNEDE OXYGEN MASKES AND DESCENDNED TO 11,000 FEET AS INSTRUCTED BY ATC. FURTHER DESCENDED TO 10,000 FEET. REMOVED O XYGEN MASKS AND DIVERTED TO ALB FOR LANDING WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED L-1 WINDSHIELD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 2002052400092 20020524 00092 WP 2002 5 24 MWEA020382 1 20020524 A 5753 39129722 ATTACH FITTING DOUG DC9 DC932 3022066 WP RIGHT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 RIGHT FLAP #3 TRAILING EDGE PANEL UPPER INBOARD ATTACH FITTING CRACKED. -- REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 2002052400093 20020524 00093 EU 2002 5 24 RQIQ00205159 1 20020520 A 2435 23095002 STARTER GEN JETAIR JETSTM JETSTM4101 1500501 EU FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 558HK 124 41071 5520-STL- LEFT GENERATOR FAIL LIGHT ON DURING TAXI. MAINTENANCE REMOVED AND REPLACED STARTER/GENERATOR. 2 L 7 2 4T RT A41NM 2002052400094 20020524 00094 EU 2002 5 24 RAIA00205160 1 20020522 A 2436 51539019E GCU JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 558HK 12225 11 41071 5494-COU- DURING TAXI-OUT RIGHT GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED #2 GENERATOR CONTROL UNIT. 2 L 7 2 4T RT A41NM 2002052400095 20020524 00095 SO 2002 5 24 RAIA00205161 1 20020523 A 8012 3375499001 FILTER EMB 145 EMB145 3260210 SO A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 806HK 145112 5283-PIT- LEFT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED THE STARTER CONTROL VALVE FILTER. 2 L 7 2 4F RT T00011AT 2002052800001 20020528 00001 NM 2002 5 28 VNAA0205009 1 20020515 A 3350 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN INOPERATIVE A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 461PS 3075 THE CREW REPORTED THAT THE FORWARD OVERHEAD EMERGENCY LIGHT WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED TH E BULB IN THE LIGHT ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MNAUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002052800002 20020528 00002 NM 2002 5 28 VNAA0205014 1 20020520 A 3000 001A561A0000200 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 471PS 16400 3007 WHILE CLIMBING OUT OF PIT, THE CREW RECEIVED A LEFT HAND FORWARD WINDSHIELD HEAT FAIL. THE CREW CALLED MAINTENANCE CONT ROL AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND FORWARD WINDSHIELD IN ACCORDANCE WITH 56-00-0 0. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002052800003 20020528 00003 NM 2002 5 28 2002UALA00905 1 20020520 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 AFT PIT FRAME BENT AND GOUGED ABOVE STRINGER 26L STATION 1400. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002052800004 20020528 00004 NM 2002 5 28 2002UALA00912 1 20020520 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 SEAT EMERG LIGHT AT SEAT 3A AFT LAMP OUT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002052800005 20020528 00005 NM 2002 5 28 2002UALA00918 1 20020524 A 5330 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 AFT PIT FRAME 1440 DENT ABOVE STRINGER 26L. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002052800006 20020528 00006 EU 2002 5 28 02145309 1 20020525 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 309UE 41022 During preflight inspection, the crew reported that the forward emergency floor track lights were inoperative. Maintena nce personnel secured the electrical connector for the forward emergency floor track lights. An operational check was s atisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002052800007 20020528 00007 EA 2002 5 28 02147629 1 20020527 A 2740 3094334 SWITCH CNDAIR CL600 CL6002B19 1900309 EA A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 629BR 7251 During climb of the flight from IAD to BNA, the crew experienced uncommanded nose down pitch trim. The crew performed t he QRH procedures and returned to IAD and landed without further incident. Maintenance personnel removed the first offi cer's yoke pitch trim switch. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002052800008 20020528 00008 EA 2002 5 28 02147631 1 20020527 A 3230 601R7520615 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 631BR 7261 During climb of the flight from JFK to IAD, the crew reported that the landing gear would not retract. The aircraft ret urned to JFK and landed without incident. Maintenance control was contacted, MEL 32-30-01 was issued, and maintenance p rocedures were completed. At IAD, maintenance personnel removed and replaced the nose landing gear priority valve. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002052800009 20020528 00009 NE 2002 5 28 COMA0210022 2 20020523 A 7240 ENGINE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE A COMA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SO 01 463CA 120267 FLIGHT 5067 - DURING CRUISE FLIGHT, DESTINATION EYW THE RIGHT ENGINE WAS SHUT DOWN DUE TO LOSS OF OIL PRESSURE.REPLACED THE RIGHT ENGINE ASSEMBLY DUE TO HOT SECTION FAILURE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002052800010 20020528 00010 EA 2002 5 28 COMA0260331 1 20020523 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LEFT WING SEIZED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 978CA 12369 7158 FLIGHT 5924 - DURING APPROACH INTO CVG RECEIVED A FLAP CAUTION MESSAGE 30 DEGREE FLAP POSITION.REPLACED THE LEFT FLAP #1 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2002052800011 20020528 00011 WP 2002 5 28 AT0200064 1 20020525 A 7720 JT8D91 ENGINE DOUG DC9 DC932 3022066 WP A ZZDA E ENGINE SHUTDOWN O OTHER TO TAKEOFF 1 SO 15 845AT 47238 #1 ENGINE FAILED AT V2 ALL ENGINE PARAMETERS NORMAL EXCEPT EGT AT RED LINE 70% N1 1.4. NO OTHER ASSOCIATED LIGHTS, OIL PRESSURE, AND TEMPERATURE NORMAL. CORRECTIVE ACTION: REMOVED AND REPLACED #1 ENGINE. 2 L 7 2 4F A6WE 2002052800012 20020528 00012 EA 2002 5 28 COMA0260336 1 20020525 A 2610 899074 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP LOW A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 739CA 19138 7273 FLIGHT 5494 ENGINE BOTTLE #1 LOW CAUTION MESSAGE.REPLACED THE #1 FIRE BOTTLE. 2 L 7 2 4F RT A21EA 2002052800013 20020528 00013 EA 2002 5 28 COMA0260335 1 20020524 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 798CA 5978 7348 FLIGHT 5243 GEAR DISAGREE WARNING DURING APPROACH.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002052800014 20020528 00014 EA 2002 5 28 COMA0260334 1 20020524 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 978CA 18724 7158 FLIGHT 5256 SPOILERON STATUS MESSAGE DURING FLIGHT.REPALCED THE R/H SPOILERON INBD PCU. 2 L 7 2 4F RT A21EA 2002052800015 20020528 00015 EA 2002 5 28 COMA0260333 1 20020524 A 2610 24403615 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 931CA 7037 FLIGHT 5618 INTERMITTENT MLG BAY OVERHEAT WARNING.REPLACED MLG BAY FIRE LOOP. 2 L 7 2 4F RT A21EA 2002052800016 20020528 00016 WP 2002 5 28 CALA0200318 1 20020524 A 5311 FRAME DOUG DC9 DC982 3022082 WP STA 1322 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND FRAME CORRODED IN AFT PIT AT STA 1322, RBL 29-30. REMOVED TWO INTERCOSTALS AND TWO BULKHEAD ATTACH ANGL ES TO GAIN ACCESS TO FRAME. INSTALLED NEW FRAME IAW SRM 51-30-2 AND 51-30-5. REINSTALLED INTERCOSTALS AND BULKHEAD ATTAC H ANGLES. ALSO INSTALLED SHEAR TIE AND REPAIR SPLICE IAW SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2002052800017 20020528 00017 WP 2002 5 28 CALA0200319 1 20020524 A 5330 SKIN DOUG DC9 DC982 3022082 WP STA 1212 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND FUSELAGE BELLY SKIN DENTED AT STA 1212, L29L TO L29R. THE AREA WAS REPAIRED IAW ECRA 5331-01114 AND EA 9-5330-2-A0954. 2 L 7 2 4F A6WE 2002052800018 20020528 00018 WP 2002 5 28 CALA0200320 1 20020526 A 3350 WIRE DOUG DC9 DC982 3022082 WP EXIT LIGHT BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND THE L-2 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE IAW STANDARD WIRING PRACTICES 20-1 0-03 AND OPEARTION CHECKED GOOD IAW MM 33-53-00. 2 L 7 2 4F A6WE 2002052800019 20020528 00019 EA 2002 5 28 SWIA200210858 1 20020505 A 2150 CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA LEFT PACK HEAT E MALFUNCTIONED A SWIA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION DE DESCENT 1 NM 07 410SW 7066 LEFT PACK FAILED INFLIGHT. RIGHT PACK DEFERRED. PERFORMED EMERGENCY DESCENT PROCEDURE PER QRH. LEFT PACK HEAT EXCHANGE R CHECK VALVE HINGE AND SPRING WORN. REMOVED AND REPLACED CHECK VALVE (FAN BYPASS) PER MM 21-52-07. LEFT PACK OPS OK. P/N: 350023000. 2 L 7 2 4F RT A21EA 2002052800020 20020528 00020 EA 2002 5 28 SWIA200210864 1 20020521 A 5220 SEAL CNDAIR CL600 CL6002B19 1900309 EA EXIT DOOR DIRTY A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 416SW 7089 PRESSURIZATION SQUEAL BY RIGHT OVER-WING EXIT DOOR PRESENT AT DELTA P OF 4.5 PSI AND GREATER. CLEANED EXIT SEAL. OPS C HECK GOOD. 2 L 7 2 4F RT A21EA 2002052800021 20020528 00021 SO 2002 5 28 C2XA02SH007 1 20020521 A 5300 14521725015 PLATE EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV - DURING C-CHECK INSPECTION, THE SERVICE DOOR AFT SILL PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED SILL PLATE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002052800022 20020528 00022 SO 2002 5 28 C2XA02SH008 1 20020521 A 5300 14521725013 PLATE EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV - DURING C-CHECK INSPECTION, THE SERVICE DOOR FORWARD SILL PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED PLATE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002052800023 20020528 00023 NM 2002 5 28 AWXA200200459 1 20020523 A 5311 BAC1517706 FRAME BOEING 737 7373Q8 1384670 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 0 0 23507 MCN - MAJOR REPAIR - DURING C-15 INSPECTION A CRACK WAS FOUND IN RADIUS AT FASTENER HOLE ON FRAME BS 616, NEXT TO STR 8 L/H. MAINTENANCE TRIMMED OUT DAMAGED AREA OF FRAME AT BS 616, STR 8 L/H; PERFORMED HFEC INSPECTION TO VERFIY NO CRACKS E XIST; FABRICATED FILLER AND CHANNEL; INSTALLED REPAIR PARTS IAW B737-3OO SRM 53-00-07, PG. 204-206. 2 L 7 2 4F RT A16WE 2002052800024 20020528 00024 NM 2002 5 28 AWXA200200469 1 20020508 A 5330 652981829 BRACKET BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 0 0 23629 YVR - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON METAL BRACKET ATTACHED TO L/H FUSELAGE SKIN UNDER L1 DOOR BS 332. MAINTENANCE REMOVED DAMAGED GUSSET BRACKET AT BS 332, FABRICATED A NEW BRACKET AND INSTALLED REPAIR IAW B737-300 S RM 51-10-02, P.12, AND DWG 65-29818. 2 L 7 2 4F RT A16WE 2002052800025 20020528 00025 NM 2002 5 28 C1HA200297007 1 20020526 A 3350 1000677 LIGHT BOEING 727 727270 138408P NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 L-1 DOOR EMERGENCY EXIT LIGHT COMES ON WHEN A/C POWER IS SHUT OFF. (COCKPIT SWITCH OFF)REMOVED AND REPLACED LIGHT ASSY. OPS CHECK WAS GOOD REF: MM CH. 33-50. 2 L 7 3 4F RT A3WE 2002052800026 20020528 00026 NM 2002 5 28 C1HA200293005 1 20020526 A 2781 H1010261 SWITCH BOEING 727 727212 138407G NM A C1HA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 15 293AS 21348 AMBER LEADING EDGE FLAP LIGHT REMAINED ON DURING FLAP EXTENSION. FLAP LEADING EDGE #1 ON ANNUNCIATOR PANEL ON. PERFORMED COM PROCEDURE. LANDED NO INCIDENT. 2 L 7 3 4F A3WE 2002052800027 20020528 00027 NM 2002 5 28 C1HA200295009 1 20020526 A 3350 1000677 LIGHT BOEING 727 727290 138408W NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 L-1 DOOR EMERGENCY EXIT SIGN LIGHT ASSY IS INOPREMOVED AND REPLACED L-1 DOOR EMERGENCY EXIT LIGHT PER M/M 33-50-31 OPS C K GOOD 2 L 7 3 4F A3WE 2002052900002 20020529 00002 SO 2002 5 29 000160 1 20020519 A 2611 SMOKE DETECTOR EMB 145 EMB145 3260210 SO CARGO BAY FALSE INDICATION A CHQA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 373 301374 PILOT INITIATED FIRE EXTINGUISHER FOR THE BAGGAGE COMPARTMENT AFTER EICAS BAGGAGE SMOKE INDICATION IN FLIGHT. REMOVED A ND REPLACED THE BAGGAGE COMPARTMENT SMOKE DETECTOR ASSEMBLIES. 2 L 7 2 4F RT T00011AT 2002052900003 20020529 00003 NE 2002 5 29 00027 2 20020522 A 7200 ENGINE LEAR 24 24B 5170306 CE GE CJ610 CJ6106 30006 NE RIGHT FLAMED OUT E HAEA B EMER. DESCENT X ENGINE FLAMEOUT CL CLIMB 1 SW 05 233TW 24B221 251772A AIRCRAFT EN ROUTE FROM MMV TO DKB RT ENGINE FLAME-OUT CLIMBING THROUGH FL410 TO 430, DESCENT TO FL250 PERFORMED AIR STAR T ALL INDICATIONS NORMAL CONTINUED FLT. AT DESTINATION CREW INSPECTED ENGINE, NO DAMAGE NOTED. WILL UPDATE WHEN AIRCRA FT AT MAINTENANCE BASE. 2 L 7 2 4J 4 J A10CE 1E16 2002052900006 20020529 00006 EU 2002 5 29 02FDEA00348 1 20020517 A 7830 CONNECTOR AIRBUS 300 A300F4605R 3930327 EU PILOT VALVE CONTAMINATED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 655FE 742 ON TAKEOFF ECAM WARN NR 1 REVERSER PRESS FOLLOWED ECAM INSTRUCTIONS TO BRING NR 1 THROTTLE TO IDLE. FOUND CANNON PLUG G OING TO DIRECTIONAL PILOT VALVE WITH MOISTURE. CLEANED PLUG AND RAN NR 1 ENG. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2002052900007 20020529 00007 EU 2002 5 29 02FDEA00349 1 20020517 A 3411 B-NUT AIRBUS 300 A300F4605R 3930327 EU PITOT/STATIC SYS LOOSE A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 671FE 778 DURING TAKEOFF CAPT A/S INDICATOR READ 40 KIAS AT 110 KIAS. SECURED LOOSE B-NUT PER SMP & REMOVED AND REPLACED NR 1 ADC PER MM 34-11-34-4. 2 L 7 2 4F RT A35EU 2002052900008 20020529 00008 NM 2002 5 29 02FDEA00351 1 20020517 A 3260 POSITION SWITCH BOEING 727 727200 138407E NM RT MLG FAILED A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 288FE 21850 ON FINAL AT DSM, EXTENDED LANDING GEAR GOT 3 GREEN LIGHTS, RED DOORS LIGHT ON FORWARD PANEL AND AMBER RT MAIN GEAR DOOR LIGHT ON S/O PANEL. CYCLED GEAR, ALL INDICATIONS NORMAL. ACN RELEASED FOR SERVICE PER MEL/CDL. RT MAIN GEAR DOOR POSI TION SWITCH SHOWS NO CONTINUITY WITH DOOR OPEN OR CLOSED. REMOVED AND REPLACED RT MLG DOOR WARNING SWITCH PER 727-200 M M 32-62-011. OPS CHECK NORMAL. 2 L 7 3 4F RT A3WE 2002052900009 20020529 00009 WP 2002 5 29 02FDEA00352 1 20020517 A 5610 NBA6045501 WINDSHIELD DOUG DC10 DC1030 3023501 WP COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 308FE 48297 CAPTAINS FRONT WINDSHIELD (OUTER PANE) CRACKED. REMOVED AND REPLACED NR 1 CAPTAINS WINDSHIELD IAW M/M CHAPTER 56-11-00- 2. DUE TO BROKEN WIRE ON TERMINAL BLOCK R5-1071. PERFORM ANTI-ICE/DEFOG TEST IAW M/M CHAPTER 30-42-00 PAGE 201. INSTA LLED TERMINAL BLOCK PER S/W/P. ACCOMPLISHED ADJ AND TEST PER MM 30-42-00. 2 L 7 3 4F A22WE 2002060700005 20020607 00005 WP 2002 6 7 02FDEA00353 1 20020520 A 5753 FITTING DOUG DC10 DC1010F 3022111 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 RIGHT WING OUTBOARD FLAP - AT REAR SPAR JUST INBOARD OF TOP MOUNT BOLT FOR INBOARD HINGE SUPPORT FITTING IS CORRODED. R EMOVED AND REPLACED FITTING PER SRM 51-21-00 VOL 2. 2 L 7 3 4F A22WE 2002052900011 20020529 00011 WP 2002 5 29 02FDEA00354 1 20020521 A 2450 CONTROLLER DOUG DC10 DC1010 3022110 WP ELECTIRCAL SYS FAILED A FDEA K NONE H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 25 68052 47806 GEN BUS 1 FAILURE AT FL 280 (LAS) COMPLIED W/ RED TABS -ONLY RESTORED FOR 5-10 SEC AT BUS FAULT, ATTEMPTED CHECKLIST 2ND TIME AFTER APU STARTED/SAME, ATTEMPTED CHECKLIST 3RD TIME AFTER GEN 1 DISCONNECT/SAME, SHOT RAW DATA APP F/O SIDE. UNE VENTFUL LANDING WITH EMERGENCY POWER ON LAST 15 MIN. 2 L 7 3 4F A22WE 2002052900012 20020529 00012 WP 2002 5 29 02FDEA00355 1 20020519 A 2932 1611210 SEAL DOUG DC10 DC1030 3023501 WP HYD TRANSMITTER SPLIT A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 314FE 48312 HYD SYS 3 ELEV OFF LIGHT ILLUMINATED. PRESSURE WAS NORMAL, QTY ABOUT 4.5 GALS. RAN RED TABS. LANDED AT TJSJ. HYD LEA K CONFIRMED BY COMPANY MX AFTER LANDING. UPON EXAMINATION, FOUND LEAK TO BE COMING FROM NR 3 HYD PRESSURE XMITTER. REM OVED XMITTER AND FOUND SEAL WAS SPLIT. REPLACED SEAL, P/N NAS 1611-210 AS PER SMP. SERVICED NR 3 HYDRAULICS PER MM 12- 13-01. HYD SYS 3 ELEV OFF LIGHT EXTINGUISHED. 2 L 7 3 4F A22WE 2002053100122 20020531 00122 NM 2002 5 31 02FDEA00356 1 20020521 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 FRAME 600 DENTED AT OPEN HOLES 5R. REMOVED AND REPLACED FRAME PER SRM 53-10-4 FIG 1. 2 L 7 3 4F RT A3WE 2002053100123 20020531 00123 NM 2002 5 31 02FDEA00357 1 20020518 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CORROSION ON STR 27L, BS 657 LOWER LOBE (C53-111-01-2). REMOVED AND REPLACED STRINGER PER SRM 53-10-1, 51-20-2, 53-10-2 , 53-10-3. 2 L 7 3 4F RT A3WE 2002060600158 20020606 00158 NM 2002 6 6 02FDEA00359 1 20020519 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CORROSION ON LOWER SURFACE OF FLOORBEAM FWD FLANGE AT BS 360, LBL 3.1, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 5 3-10-8 FIG 3. 2 L 7 3 4F RT A3WE 2002060700006 20020607 00006 NM 2002 6 7 02FDEA00360 1 20020520 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 209FE 22931 CORROSION ON FRAME BS 720F FWD FACE BETWEEN STR 4 & 5 RT. 2 L 7 3 4F RT A3WE 2002060600159 20020606 00159 NM 2002 6 6 02FDEA00361 1 20020520 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 209FE 22931 DENT IN FRAME AT BS 700, STR 25 RT. REMOVED AND REPLACED FRAME PER SRM 53-10-1. 2 L 7 3 4F RT A3WE 2002052900014 20020529 00014 NM 2002 5 29 200200264 1 20020521 A 5315 65B1092918 FLOORBEAM BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 478EV 21033 DURING B-CHECK, A CRACKED FLOOR PANEL ATTACH HOLE COMMON TO THE BS 380 UPPER DECK FLOORBEAM UPPER CHORD WAS DISCOVERED P /N 65B10929-18 AT RBL 65.0. THE CRACKED UPPER CHORD IS BEING REPAIRED BY INSTALLING 2 STRAPS PER ECRA. 2 L 7 4 4F RT A20WE 2002052900015 20020529 00015 NM 2002 5 29 200200265 1 20020521 A 5315 65B10929506 FLOORBEAM BOEING 747 747SR46 1384816 NM FUSELAGE PUNCTURED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 478EV 21033 DURING B-CHECK A PUNCTURE WAS FOUND IN THE BS 380 FLOORBEAM WEB P/N 65B10929-506 AT APPROXIMATELY LBL 57. THE DAMAGE WA S TRIMMED OUT, HFEC INSPECTION PERFORMED AND DOUBLERS AND FILLERS FABRICATED AND INSTALLED PER ECRA 478-53-137-02. 2 L 7 4 4F RT A20WE 2002052900016 20020529 00016 EU 2002 5 29 20024 1 20020520 A 2432 VP400KH CELL SAFT CASA C212 C212 2410200 EU NR 1 BATTERY SHORTED E STZA H DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION CR CRUISE 1 AL 03 502FS 1000 176 86943 294 PILOT REPORTED THAT EN ROUTE BETWEEN KLG AND ANC THAT THE NR 1 BATTERY TEMP ANNUNCIATOR ILLUMINATED. PERFORMED BATTERY DISCONNECT PROCEDURE PER THE CASA AFM SECTION 2-8. REMAINDER OF TRIP REPORTED UNEVENTFUL. MAINTENANCE DISCHARGED BATTE RY AND FOUND ONE OF THE CELLS SHORTED INTERNALLY. BYPASSED CELL AND CONTINUED DISCHARGE OF BATTERY WITH NO OTHER FAULTS . 2 H 7 2 4T A43EU 2002052900017 20020529 00017 2002 5 29 2002F00507 4 20020518 A 3460 4052506955 COMPUTER BOEING 757 75733N 1384931 NM E/E BAY FAILED G AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 558TZ 347 347 32592 FLIGHT NUMBER 925, DURING CRUISE RECEIVED EICAS MSG L FMC FAIL. OTHER CDU DISPLAYS SINGLE FMC OPERATION MESSAGE. MAINTE NANCE REMOVED AND REPLACED THE LEFT FMC COMPUTER IN ACCORDANCE WITH MM 34-61-01-4. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002052900018 20020529 00018 NM 2002 5 29 USAABB02046 1 20020417 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 618AU 22210 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1 AND 4 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002052900019 20020529 00019 NM 2002 5 29 USAABB02047 1 20020417 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 618AU 22210 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002052900023 20020529 00023 SO 2002 5 29 000161 1 20020525 A 2121 COOLING FAN EMB 145 EMB145 3260210 SO E/E BAY OBSTRUCTED A CHQA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 11 376 CREW REPORTED PFD FAILURE AND POPPED C/B TO F30 ELECT BAY COOLING. CREW DECIDED TO RETURN TO FIELD. PFP OPS CHECK GOOD . CLEANED DEBRIS FROM COOLING FAN. 2 L 7 2 4F RT T00011AT 2002052900025 20020529 00025 SO 2002 5 29 000162 1 20020528 A 2150 A/C PACK EMB 145 EMB145 3260210 SO A/C BAY MALFUNCTIONED A CHQA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 11 262 P3370217 NR 2 PACK OVERLOAD ON EICAS FOLLOWED BY SMOKE IN CABIN. DEFERRED NR 2 PACK. 2 L 7 2 4F RT T00011AT 2002052900026 20020529 00026 SO 2002 5 29 000163 1 20020528 A 3244 TIRE EMB 145 EMB145 3260210 SO LT MLG WORN A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 11 284 LEFT O/B TIRE WORN AND FUEL SMELL IN CABIN. REMOVED AND REPLACED TIRE. GROUND RUN, NO FUEL SMELL NOTICED. 2 L 7 2 4F RT T00011AT 2002052900029 20020529 00029 NM 2002 5 29 HNAA0200039 1 20020526 A 2100 011355 FAN DHAV DHC8 DHC8201 2809001 NM OVERHEATED A HNAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 EA 07 986HA 14600 421 A BURNING SMELL WAS REPORTED COMING FROM THE GALLEY/COAT CLOSET AREA OF THE CABIN. AIRCRAFT DIVERTED TO AVL. REPLACED AV IONICS BAY COOLING FAN. 2 H 7 2 4T RT A13NM 2002052900032 20020529 00032 WP 2002 5 29 0201649911 1 20020520 A 4990 GTCP8598DCA APU DOUG DC9 DC931 3022065 WP APU BAY LEAKING A NWAA K NONE K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 GL 01 961N 47405 DURING GROUND COOLING IN CLT, THE FLIGHT ATTENDANT NOTED A TRACE OF SMOKE IN THE CABIN. PACK WAS ADJUSTED TO WARMER TEM P AND PROBLEM ENDED. ON TAKEOFF, THE SMOKE RETURNED AND CAUSED THE FORWARD LAV SMOKE DETECTOR TO ALARM FOR ABOUT 3 MINU TES THEN CEASED. THERE WERE NO OTHER PROBLEMS FOR THE REMAINDER OF THE FLIGHT. LANDING AT MSP WAS UNEVENTFUL. MAINTEN ANCE REPLACED THE APU FOR LEAKING OIL AND BOTH WATER SEPARATORS DUE TO OIL CONTAMINATION. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002052900034 20020529 00034 NM 2002 5 29 P5CA0200676 1 20020523 A 5330 NONE SKIN BOEING 747 747249F 1384849 NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 FOUND 1" CRACK IN LOWER SKIN FUSELAGE AT STA 2390, LBL70. FABRICATED REPAIR PLATE & DRILLED FASTENER HOLES. APPLIED AL ODINE TO CUT EDGES OF REPAIR PLATE & REPAIR SKIN AREA. PRIMED FAYING SURFACES. INSTALLED REPAIR PLATE W/ FASTENERS. U SED BMS 5-95 TO SEAL FAYING SURFACES & APPLIED TRIM CO'S IAW SRM 53-30-02/03. 2 L 7 4 4F A20WE 2002052900035 20020529 00035 EU 2002 5 29 QXEA0200843 1 20020528 A 2910 HYDRAULIC SYSTEM FOKKER F28 F28MK4000 4990810 EU ZONE 400 LOW A QXEA O OTHER K FLUID LOSS UK UNKNOWN 1 NM 09 493US 11161 SEA - DURING FLIGHT THE FLIGHT CONTROL HYDRAULIC QUANTITY DROPPED TO ZERO. LANDING AT SEA WAS UNEVENTFUL. MAINTENANCE IN SPECTED THE AIRCRAFT AND SERVICED THE FLIGHT CONTROL HYDRAULIC SYSTEM TO FULL. THE SYSTEM WAS PRESSURIZED FOR 45 MINUTES WITH NO LEAKS OR MIGRATION NOTED. THE # 1 HYDRAULIC SYSTEM ACCUMULATOR WAS ALSO SERVICED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002052900039 20020529 00039 WP 2002 5 29 0201659906 1 20020522 A 5260 591591523 SEAL DOUG DC9 DC931 3022065 WP FWD AIRSTAIRS OUT OF POSITION A NWAA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 GL 01 956N 47252 DURING CLIMBOUT, THE CABIN PRESSURE WARNING LIGHT ILLUMINATED. CABIN PRESSURE CLIMBED THROUGH 10,000 FEET TO 12,500 FEE T WHEN CREW ACCOMPLISHED AN EMERGENCY DESCENT TO 10,000 FEET AND DIVERTED TO MKE. NO MENTION OF COM OR OF MANUAL PRESSU RE CONTROL. LANDING WAS UNEVENTFUL. MAINTENANCE FOUND THE UPPER OF DOOR PRESSURE SEAL OUT OF THE RETAINER ON THE FORWA RD INTEGRAL STAIRS. THE SEAL WAS REINSTALLED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002052900040 20020529 00040 WP 2002 5 29 0201669941 1 20020516 A 2760 420913 CONTROL BOX DOUG DC9 DC932 3022066 WP SPOILER MALFUNCTIONED A NWAA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 GL 01 3324L 47103 DURING LANDING AT MSP, FLIGHT TOUCHED DOWN BUT SPOILERS FAILED TO EXTEND SO CREW INITIATED A GO-AROUND. ONCE AIRBORNE, COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT RETURNED AND LANDED USING MANUAL SPOILER CONTROL. APPARENTLY THE WIND CON DITIONS FOR LANDING WERE CAUSING EXCESSIVE FLOATING OF THE AIRCRAFT AND SPOILERS WERE NECESSARY. AFTER ENGINE SHUTDOWN AT GATE, THE SPOILER SYSTEM RECYCLED AND THE ANNUNCIATOR LIGHT EXTINGUISHED. MAINTENANCE REPLACED THE SPOILER CONTROL B OX AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002052900042 20020529 00042 2002 5 29 02142421 4 20020522 A 3460 COMPUTER DORNER DO32 DO328300 NM E/E BAY FAULTY A VTZA K NONE F FLT CONT AFFECTED DE DESCENT 1 EA 27 421FJ 3179 DURING APPROACH OF THE FLIGHT FROM CVG TO ALB, THE CREW REPORTED UNCOMMANDED ROLL AND YAW MOVEMENT OF THE AIRCRAFT. AN EMERGENCY WAS DECLARED WITH THE ALB TOWER AND THE AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL R EMOVED AND REPLACED THE NR 1 INTEGRATED AVIONICS COMPUTER (IAC), INSPECTED AND OPERATIONAL CHECKED ALL FLIGHT CONTROL SY STEMS AND SURFACES, AND CONDUCTED A MAINTENANCE ACCEPTANCE FLIGHT (MAF). ALL CHECKS AND THE MAF WERE SATISFACTORY AND T HE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002052900043 20020529 00043 NE 2002 5 29 02142640 2 20020522 A 7200 6089T11G01 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NR 2 MALFUNCTIONED A VTZA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 27 640BR 7109 7340 GEE782576 DURING CLIMB OF THE FLIGHT FROM ROA TO ORD, THE CREW NOTED HIGH VIBRATION AND NOISE FROM THE RT (NR 2) ENGINE FOLLOWED B Y LOSS OF OIL PRESSURE. THE ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED TO ROA AND LANDED WITHOUT INCIDENT. MAINTENAN CE PERSONNEL REMOVED AND REPLACED THE RT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002060400293 20020604 00293 NM 2002 6 4 DHL2002741007 1 20020525 A 2752 MOTOR BOEING 727 7272Q9 138448M NM T/E FLAP LEAKING A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 741DH 21931 A-SYS FLUID LOSS TO -0-, THEN PRESSURE DEC TO -0-. COMPLETED ALT PROCEDURE. FOUND O/B FLAP DRIVE RT W/W LEAKING. REPL ACED FLAP MOTOR, OPS/LEAK CHECKED SATISFACTORY. 2 L 7 3 4F RT A3WE 2002052900044 20020529 00044 EA 2002 5 29 02142673 1 20020522 A 5240 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 673BR 7599 DURING PREFLIGHT INSPECTION AT LEX, THE GROUND CREW REPORTED THAT THE SERVICE DOOR WOULD NOT OPEN FROM THE OUTSIDE. THE AIRCRAFT WAS FERRIED TO ORD FOR MAINTENANCE. MAINTENANCE PERSONNEL CLEANED AND LUBRICATED THE SERVICE DOOR HANDLE MECH ANISM. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002060600161 20020606 00161 NM 2002 6 6 02FDEA00362 1 20020524 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 WHILE WORKING FOUND FRAME CRACKED AT BS 720, LBL 2, WL 154. REMOVED AND REPLACED FRAME PER SRM 51-40-3 & EA 7-5310-6491 0. 2 L 7 3 4F RT A3WE 2002052900054 20020529 00054 NM 2002 5 29 2002F00518 1 20020520 A 2613 579601 OVERHEAT LOOP BOEING 757 75723N 1384973 NM LT ENGINE FAULTY G AMTA K NONE N FALSE WARNING CR CRUISE 1 GL 11 527AT 5557 5557 30886 FLIGHT NUMBER 109, DURING CRUISE LEFT ENG OVERHEAT LOOP 2 STATUS MESSAGE DISPLAYED. MAINTENANCE REMOVED AND REPLACED OV ERHEAT DETECTOR ELEMENT IN ACCORDANCE WITH MM 26-11-01. OPERATIONAL CHECKS GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2002061200031 20020612 00031 NM 2002 6 12 2002UALA00768 1 20020516 A 2130 87292325V04 COMPUTER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE E/E BAY FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 830UA 1243 RETURNED TO FIELD DUE TO AN AVIONICS VENT MESSAGE. *S/D* FAULT WAS ISOLATED TO MALFUNCTIONING AEVC (COMPUTER). REPLA CED SAME. 2 L 7 2 4F 4 F RT A28NM E40NE 2002052900098 20020529 00098 NE 2002 5 29 02FDEA00363 2 20020523 A 7530 SCREEN BOEING 727 727200 138407E NM PWA JT8 JT8D217C 52053 NE ENGINE DIRTY A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 215FE 22936 ON CLIMBOUT APPROX 1500 AGL AFTER SETTING QUIET EPR AND RETRACTING FLAPS TO 5 DEGREES, EXPERIENCED SEVERE COMPRESSOR STA LL WITH AUTOPACK TRIP, ENGINE PARAMETERS REMAINED WITHIN LIMITS RETURNED TO GTF. PERFORMED TROUBLESHOOTING PER PWA JT8D M/M 72-00-00 STEPS 1 THROUGH 4, CLEANED PRBC SCREENS. AS PRECAUTION PERFORMED TAKEOFF EPR AND ACCELERATION TEST PER FE DEX B727 JRH CHAP 6. ALL PARAMETERS CHECKED GOOD, A/C RELEASED FOR SERVICE. 2 L 7 3 4F 4 F RT A3WE E9NE 2002052900102 20020529 00102 NE 2002 5 29 02FDEA00364 2 20020525 A 7200 ENGINE BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE NR 3 FAILED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 265FE 21671 AFTER 30 MINUTES IN FLIGHT OIL TEMP CLIMBED TO YELLOW BAND DURING RED TAB PROCEDURES WITH ENGINE AT IDLE TEMP CLIMBED AB OVE RED BAND. SHUT DOWN NR 3 ENGINE IN ACCORDANCE WITH RED TABS. REMOVED AND REPLACED OIL TEMP BULB PER M/M 727-200 79 -34-021-4, LEAK AND OPS CHECK NORM. AT IDLE ENG NEEDS TO BE RUN AT HIGH POWER. REMOVED AND REPLACED MAIN OIL SCREEN FO R WINDMILL PER M/M 79-00-000-3-1, LEAK CHECK O/K SCREEN FOUND CLEAN. REMOVED NR 3 ENGINE IN REFERENCE TO 727-200 ENGINE CHANGE NR 3 W/C 70T0001-03. OPS AND LEAK CHECK GOOD, OK FOR SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2002052900104 20020529 00104 WP 2002 5 29 02FDEA00365 1 20020526 A 2120 ODOR DOUG DC10 DC1010 3022110 WP CARGO BAY DETECTED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 363FE 48263 TEN MINUTES AFTER T/O JUMPSEATERS AND F/O SMELLED FUMES IN CARGO COMPARTMENT. RETURNED TO MCO. INSPECTED CARGO COMPART MENT, OPENED EVERY CONTAINER ON MAIN DECK AND NO FUMES OR PROBLEMS FOUND. RAN ALL 3 PACKS ONE AT A TIME WITH APU AND EN GINE AIR AND NO PROBLEMS FOUND. A/C OK FOR SERVICE IAW M/M 26-15-00-0. 2 L 7 3 4F A22WE 2002052900115 20020529 00115 NM 2002 5 29 2002F00519 1 20020116 A 5210 SKIN BOEING 727 727222 1384073 NM L1 DOOR CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 AT C-CHECK, FOUND L1 DOOR EXTERIOR SKIN CRACKED AT THE FORWARD LOWER CORNER STATION 317 APPROXIMATELY SIX INCHES FROM FO RWARD EDGE OF DOOR. (M) 2 L 7 3 4F A3WE 2002052900117 20020529 00117 SW 2002 5 29 2002F00521 1 20020124 A 5270 WARNING SYSTEM SWRNGN SA227 SA227AC 8780603 SW COCKPIT FALSE ACTIVATION A BSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 05 160MC AC733B MSO - FLT 2583 - CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB 20 MILES NORTH OF THE STATION. CREW RETURNED TO THE STAT ION. NO APPARENT PROBLEM WAS FOUND. CARGO DOOR SWITCHES AND CLICK CLACKS WERE INSPECTED, THE SWITCHES WERE CLEANED. N O DEFECTS WERE REPORTED. A TEST FLIGHT WAS COMPLETED WITH NO DEFECTS FOUND. (M) 2 L 7 2 4T RT A8SW 2002052900119 20020529 00119 SW 2002 5 29 2002F00523 1 20020114 A 2910 2781032135 HYDRAULIC LINE SWRNGN SA227 SA227AC 8780603 SW HYD SYSTEM DAMAGED A BSAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 05 27465 AC755B FLT 1302 - DFW - 130 MILES FROM ORIGINATING STATION, AIRCRAFT LOST HYDRAULIC PRESSURE. CREW RETURNED TO STATION AT MAX GEAR EXTENSION SPEED. GEAR WAS PUMPED DOWN USING EMERGENCY CHECKLIST. HYDRAULIC LEAK CAUSED LOSS OF HYDRAULIC FLUID LE ADING TO LOSS OF HYDRAULIC PRESSURE. REPAIRED LINE BY SPLICING IN NEW SECTION PER MM. BOTH HYDRAULIC PUMPS CHANGED DUE TO EXCEEDING MM RESTRICTION ON LENGTH OF TIME THE PUMPS CAN RUN WITHOUT FLUID. (M) 2 L 7 2 4T RT A8SW 2002052900147 20020529 00147 NM 2002 5 29 SABA020062 1 20020529 A 3350 1306 BULB DHAV DHC8 DHC8103 1386005 NM CABIN BURNED OUT A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 801WP 086 Aircraft 801 on flight 8680 from CLT to CVG. On preflight before departing CLT two overhead emergency lights would not test. Maintenance removed and replaced the bulbs. System ops check good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002052900154 20020529 00154 SO 2002 5 29 SIMA200207801 1 20020227 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AE 145055 ABI - THIS IS A LEVEL 2 FINDING. RIGHT SILL IS CORRODED BETWEEN FRAMES 23-25. REMOVED CORROSION, NDT TREATED IAW EMB14 5 GST-0714/02. (M) 2 L 7 2 4T RT T00011AT 2002052900155 20020529 00155 SO 2002 5 29 SIMA200207804 1 20020308 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AE 145287 THIS IS LEVEL 2 ITEM. CORROSION ON SERVICE DOOR CENTER SILL. BLENDED AND RETREATED SERVICE DOOR CENTER SILL IAW EMB GS T-0798/02 AND EMB 135 CPM 51-14-02 AND 51-21-06. (M) 2 L 7 2 4F RT T00011AT 2002052900156 20020529 00156 SO 2002 5 29 SIMA200207806 1 20020225 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AE 145055 ABI - THIS IS A LEVEL 2 FINDING. LEFT SILL CORRODED BETWEEN FRAMES 19 AND 21. BLENDED CORROSION, FOUND TO BE ACCEPTED AS IS IAW EMB GST-0714/02. RETREATED AREA IAW EMB145 CPM 51-21-04, 51-21-05, 51-21-06. (M) 2 L 7 2 4T RT T00011AT 2002052900157 20020529 00157 SO 2002 5 29 SIMA200207807 1 20020225 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AE 145055 ABI - THIS IS LEVEL 2 FINDING. RIGHT SILL CORRODED BETWEEN FRAMES 15 AND 16. BLENDED CORROSION, FOUND TO BE ACCEPTED A S IS IAW EMB GST-0714/02. (M) 2 L 7 2 4T RT T00011AT 2002052900158 20020529 00158 SO 2002 5 29 SIMA200207808 1 20020225 A 5311 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AE 145055 ABI - THIS IS A LEVEL 2 FINDING. RIGHT PROFILE AT FRAME 18 IS CORRODED. BLENDED CORROSION, FOUND TO BE ACCEPTED AS IS IAW EMB GST-0714/02. (M) 2 L 7 2 4T RT T00011AT 2002052900159 20020529 00159 SO 2002 5 29 SIMA200207809 1 20020227 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AE 145055 ABI - THIS IS A LEVEL 2 FINDING. LEFT SILL IS CORRODED BETWEEN FRAMES 26-27. BLENDED CORROSION, NDT AND RETREATED AREA IAW EMB145 GST 0714/02. (M) 2 L 7 2 4T RT T00011AT 2002052900160 20020529 00160 SO 2002 5 29 SIMA200207810 1 20020227 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AE 145055 THIS IS A LEVEL 2 FINDING. LEFT FLOORBEAM CORRODED AT FRAME 26. REMOVED CORROSION, NDT AND RETREATED IAW EMB 145 GST-0 714/02. (M) 2 L 7 2 4T RT T00011AT 2002052900161 20020529 00161 SO 2002 5 29 SIMA200207903 1 20020319 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AE 145287 THIS IS A LEVEL 2 FINDING. CORROSION SERVICE DOOR CENTER SILL. BLENDED AND RESTORED SERVICE DOOR CENTER SILL IAW EMB G ST-0798/02 AND EMB135 CPM 51-14-02 AND 51-21-06. (M) 2 L 7 2 4F RT T00011AT 2002052900162 20020529 00162 SO 2002 5 29 SIMA200207904 1 20020319 A 3210 14571033007 CAP EMB 135 EMB135LR 3260305 SO LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 721HS 145283 ABI - THIS IS A LEVEL 2 FINDING. LEFT MAIN LANDING GEAR FORWARD BEARING CAP CORRODED. REMOVED AND REPLACED LEFT FORWAR D BEARING CAP IAW EMB 135 AMM 32-10-01. (M) 2 L 7 2 4F RT T00011AT 2002052900163 20020529 00163 SO 2002 5 29 SIMA200207905 1 20020319 A 3222 14571033007 CAP EMB 135 EMB135LR 3260305 SO NLG STRUT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 721HS 145283 ABI - THIS IS A LEVEL 2 FINDING. LEFT NOSE LANDING GEAR STRUT LOWER BEARING CAP CORRODED. REPLACED STRUT LOWER BEARING CAP IAW EMB 135 AMM 32-20-01. (M) 2 L 7 2 4F RT T00011AT 2002052900164 20020529 00164 SO 2002 5 29 SIMA200208301 1 20020225 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 720AE 145279 THIS IS A LEVEL 2 FINDING. CORROSION GALLEY FORWARD DIGITAL. RESTORED PROTECTIVE COATING, DAMAGE ACCEPTED AS IS IAW EM B GST-0634/02. (M) 2 L 7 2 4F RT T00011AT 2002052900166 20020529 00166 EU 2002 5 29 YENA200210 1 20020528 A 2597 3070581102 WIRE HARNESS AIRBUS 320 A320232 3930326 EU SEAT 7ABC & 8ABC FRAYED A YENA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 EA 15 520JB 1446 On Flt#20, TPA to JFK, Passenger noticed sparks coming from a wire on the floor at seat row #8A/C left. Turned live TV'S OFF, did not stop sparking, pulled LTV CB's and sparking stopped.T/S found seat to seat cable for seat 8ABC to 7ABC pin ched by passenger foot to seat frame causing short and sparks. Placed entire LTV on MEL 25-22-03, CB'S collared till cab le is replaced. OK to continue. Removed and replaced seat to seat cable 7ABC to 8ABC IAW MM 23-37-00, system CK OK. Pla card removed. 2 L 7 2 4F RT A28NM 2002052900167 20020529 00167 WP 2002 5 29 DHL2002805048 1 20020525 A 5610 SLIDING WINDOW DOUG DC8 DC873F 302199F WP A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 1) CAPT SLIDING WINDOW STICKS @ 50% OPEN WILL NOT OPEN FULLY2) ADJUSTED MICARTA RUB BLOCK FOR CLEARANCE PER MM 56-10- 3 OP CKS OKAY 2 L 7 4 4F RT 4A25 2002052900168 20020529 00168 WP 2002 5 29 ZW0A0205501 1 20020528 A 5610 NA WINDSHIELD DOUG DC9 DC982 3022082 WP A ZW0A A UNSCHED LANDING P NO WARNING INDICATION TO TAKEOFF 1 CE 13 905TW 49157 CAPTAIN'S WINDSHIELD CRACKED AND SHATTERED SHORTLY AFTER TAKEOFF.R/R CRACKED WINDSHIELD (P/N 217-0332), OPS CHECK WINDOW HEAT AND OPERATION NORMAL. --CLOSED-- LAST CHECK-C MCI 10/9/01 2 L 7 2 4F A6WE 2002052900169 20020529 00169 EU 2002 5 29 MALA020297 1 20020523 A 2430 GCU SAAB SF340 340B 7860101 EU A MALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 408XJ 340B408 DURING TAXI ON FLIGHT #3116, RH DC GEN WENT OFF LINE 2 TIMES DURING TAXI OUT TO RUNWAY, RESET BOTH TIMES AND FELL OFFLIN E AGAIN ON RETURN TO GATE. MAINTENANCE REMOVED AND REPLACED RH GCU.ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002052900170 20020529 00170 NM 2002 5 29 QXEA0200847 1 20020526 A 2120 3038400 ENGINE DHAV DHC8 DHC8202 2809007 NM PWC 150 PW150A EA ENGINE INOPERATIVE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 348PH 10730 484 PCEAG0050 PDX-AIRCRAFT APPEARS TO HAVE LIGHT HAZE IN COCKPIT AND CABIN, POSSIBLY FROM BLEED AIR. REMOVED AND REPLACED #2 ENGINE. O PERATIONAL CHECK AND GROUND RUN GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002052900171 20020529 00171 NM 2002 5 29 AWXA200200471 1 20020528 A 3350 BMS13311122 WIRE BOEING 757 7572S7 1384962 NM SEAT ROW 22 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 0 0 23568 PHX - EEL - DURING INSPECTION OF EMERGENCY ESCAPE PATH LIGHTING THE SEAT LIGHT AT SEAT ROW 22 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE LIGHT ASSEMBLY, SEAT ROW 22 L/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002052900172 20020529 00172 NM 2002 5 29 AWXA200200472 1 20020505 A 5330 65457788 SKIN BOEING 737 7373Q8 1384670 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 0 0 23507 MCN - MAJOR REPAIR - DURING C-15 CHECK A CRACK WAS FOUND AT FUSELAGE SKIN OF R2 DOOR LOWER HINGE CUTOUT BS 948.5. MAINTE NANCE CUTOUT CRACKED AREA OF SKIN AT R2 DOOR LOWER HINGE; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATE D A -1 DOUBLER, -2 TRIPLER, AND -3 FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01, FIG. 207, SHT 1-8. 2 L 7 2 4F RT A16WE 2002052900173 20020529 00173 NM 2002 5 29 AWXA200200473 1 20020508 A 5315 6545410156 WEB BOEING 737 7373Q8 1384670 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 0 0 23507 MCN - MAJOR REPAIR - DURING C-15 CHECK 5 EACH CRACKS WERE FOUND AT RIVET HOLES ON LOWER ROW OF FLOOR BEAM INTERCOASTAL W EB RBL 25, BS 706 TO BS 713. MAINTENANCE CUTOUT DAMAGED AREA OF WEB FROM BS 706 TO BS 713, RBL 25; PERFORMED HFEC INSPEC TION OF CUTOUT TO VERFIY NO CRACKS EXIST; REMOVED 3 EACH STIFFNERS FROM DAMAGED AREA; FABRICATED A FILLER AND DOUBLER; I NSTALLED REPAIR PARTS AND 3 EACH STIFFNERS IAW AWA ER 03-5715-21038-ES3. 2 L 7 2 4F RT A16WE 2002052900174 20020529 00174 NM 2002 5 29 AWXA200200475 1 20020513 A 5311 6545807 FRAME BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 0 0 23629 YVR - MAJOR REPAIR - DURING C-16 CHECK CRACKS WERE FOUND ON 3 EACH INTERCOASTAL TO SKIN ATTACH ANGLES AT BS 294.5, BELOW STR 12 R/H, AND BELOW & ABOVE STR 11. MAINTENANCE REMOVED, FABRICATED, AND INSTALLED 3 EACH INTERCOASTAL TO SKIN ATTACH ANGLES AT BS 294.5 IAW B737-300 SRM 51-10-2, PG. 12, AND SRM 51-40-2, PG. 3. 2 L 7 2 4F RT A16WE 2002053000003 20020530 00003 SO 2002 5 30 SIMA200208302 1 20020225 A 5320 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 720AE 145279 ABI - THIS IS A LEVEL 2 FINDING. CORROSION GALLEY CENTER BEAM GUSSET. RESTORED PROTECTIVE COATING, DAMAGE ACCEPTED AS IS IAW EMB GST-0636/02. (M) 2 L 7 2 4F RT T00011AT 2002053000004 20020530 00004 SO 2002 5 30 SIMA200208303 1 20020318 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 721HS 145283 ABI - THIS IS A LEVEL 2 FINDING. CORROSION ON SERVICE DOOR CENTER SILL. RESTORED PROTECTIVE COATING, DAMAGE ACCEPTED A S IS IAW EMB GST 0636/02. (M) 2 L 7 2 4F RT T00011AT 2002053000006 20020530 00006 SO 2002 5 30 SIMA200208304 1 20020225 A 5320 BEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 720AE 145279 ABI - THIS IS LEVEL 2 FINDING. CORROSION FOUND ON GALLEY RIGHT BEAM. RESTORED PROTECTIVE COATING, DAMAGE ACCEPTED AS I S IAW EMB GST-0636/02. (M) 2 L 7 2 4F RT T00011AT 2002053000007 20020530 00007 SO 2002 5 30 SIMA200208306 1 20020126 A 5320 14521725615 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AE 145276 DURING MBV INSPECTION, MAINTENANCE FOUND LEVEL 2 CORROSION ON THE SERVICE DOOR FORWARD SILL. MAINTENANCE REMOVED AND RE PLACED THE FORWARD SILL IAW EMB SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002053000008 20020530 00008 SO 2002 5 30 SIMA200208307 1 20020207 A 3210 14571033007 CAP EMB 135 EMB135LR 3260305 SO LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 145272 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE LEFT MAIN LANDING GEAR BEARING CAP TO BE CORRODED. BEARING CAP WAS R EMOVED AND REPLACED IAW EMB MM. (M) 2 L 7 2 4F RT T00011AT 2002053000009 20020530 00009 SO 2002 5 30 SIMA200208308 1 20020207 A 3210 14571033007 CAP EMB 135 EMB135LR 3260305 SO RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 145272 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE RIGHT MAIN LANDING GEAR BEARING CAP. MAINTENANCE REMOVE D AND REPLACED THE BEARING CAP IAW EMB MM. (M) 2 L 7 2 4F RT T00011AT 2002053000010 20020530 00010 SO 2002 5 30 SIMA200208707 1 20020318 A 5320 14522461003 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 721HS 145283 ABI - THIS IS A LEVEL 2 FINDING. FORWARD DIAMOND GUSSET IS CORRODED AT FRAME 20. REPLACED SERVICEABLE FORWARD DIAMOND GUSSET IAW EMB 135 SRM 51-40-06, 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002053000011 20020530 00011 SO 2002 5 30 SIMA200208708 1 20020318 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 721HS 145283 ABI - THIS IS A LEVEL 2 FINDING. SERVICE DOOR SILL CORRODED AROUND NUTPLATE AT FRAME 20. BLENDED AND TREATED CORROSION , ACCEPTED AS IS IAW GST-0925/02. (M) 2 L 7 2 4F RT T00011AT 2002053000012 20020530 00012 SO 2002 5 30 SIMA200208709 1 20020318 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 721HS 145283 ABI - THIS IS A LEVEL 2 FINDING. RIGHT FORWARD SILL IS CORRODED AROUND THE NUTPLATES AT FRAME 18 AND 20. BLENDED AND T REATED FOR CORROSION IAW GST-0925/02. (M) 2 L 7 2 4F RT T00011AT 2002053000013 20020530 00013 SO 2002 5 30 SIMA200208710 1 20020318 A 5320 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 721HS 145283 ABI - THIS IS A LEVEL 2 FINDING. CENTER BEAM GUSSET IS CORRODED AT FRAMES SO AND 22. BLENDED AND TREATED FOR CORROSION , ACCEPTED AS IS IAW GST-0725/02. (M) 2 L 7 2 4F RT T00011AT 2002053000014 20020530 00014 SO 2002 5 30 SIMA200208712 1 20020326 A 2612 FIRE WARNING EMB 135 EMB135LR 3260305 SO COCKPIT FALSE ACTIVATION A SIMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 732DH 145358 RDU - FLT 4549 - ON CLIMB-OUT, CREW HAD CARGO COMPARTMENT SMOKE WARNING AND DISCHARGED FIRE BOTTLES. DECLARED EMERGENCY AND RETURNED TO RDU. NO FIRE NOTICED. REPLACED CARGO FIRE BOTTLES. PERFORMED SYSTEMS OPS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2002053000015 20020530 00015 SO 2002 5 30 SIMA200209325 1 20020328 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - THIS IS A LEVEL 2 FINDING. CENTER BEAM GUSSET HAS CORROSION AT FRAME 20. INSTALLED NEW CENTER GUSSET IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002053000016 20020530 00016 NM 2002 5 30 PCAA0205061 1 20020529 A 3230 85411783001 FITTING DHAV DHC8 DHC8102 2809003 NM CRACKED CRACKED A PCAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 13 980HA 376 BGM-BUF FLIGHT#3779. CREW REPORTED RIGHT GEAR UNSAFE AND NOSE YELLOW DOOR LIGHT ILLUMINATED. BOTH GEAR CONFIRMED RETRACT ED AND RIGHT MAIN DOORS OPEN. CHATTERING HYDRAULIC NOISE FROM NOSE GEAR. MAINTENANCE FOUND OUTBOARD BUSHING (PN NAS75-12 -017) MISSING FROM RIGHT MAIN LANDING GEAR RETRACTION ACTUATOR FITTING, AND FITTING WAS CRACKED. REMOVED AND REPLACED RI GHT MAIN GEAR RETRACTION ACTUATOR FITTING IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 32-30-11 AND PIEDMONT TASK CARD 32-30-18I. CYCLED THE GEAR, OPERATIONAL CHECK GOOD 2 H 7 2 4T RT A13NM 2002053000018 20020530 00018 SO 2002 5 30 SIMA200209326 1 20020328 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - THIS IS A LEVEL 2 FINDING. CENTER BEAM GUSSET REMOVED CORROSION FOUND ON CENTER BEAM AT FRAME 20. CUT OUT DAMAGE D AREA AND REPAIRED IAW EMB135 SRM 53-21-10. (M) 2 L 7 2 4F RT T00011AT 2002053000020 20020530 00020 EU 2002 5 30 SIMA200209401 1 20020321 A 5347 S53375001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP8 INSPECTION, FOUND RIGHT FORWARD OUTBOARD, RIGHT FORWARD INBOARD, LEFT FORWARD INBOARD, RIGHT MID OUTB OARD, RIGHT MID INBOARD, LEFT MID OUTBOARD, RIGHT AFT INBOARD, LEFT AFT OUTBOARD SEAT TRACKS TO BE CORRODED BEYOND LIMIT S. REPLACED SEAT TRACKS IAW EO E1-53MR-271. (M) 2 H 7 2 4T RT A53EU 2002053000021 20020530 00021 EU 2002 5 30 SIMA200209402 1 20020321 A 5315 S5367240620801 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 INSPECTION, FOUND FLOORBEAMS 36, 38, AND 39 TO BE CORRODED BEYOND LIMITS. REPLACED FLOORBEAMS IAW AT R 42 SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053000022 20020530 00022 EU 2002 5 30 SIMA200209403 1 20020321 A 5330 S5387240420201 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP8 INSPECTION, FOUND AIRFRAME CUTOUT FOR AFT AVIONICS DOOR IS CORRODED BEYOND LIMITS. REPLACED CUTOUT R EINFORCING IAW ATR42 SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053000024 20020530 00024 EU 2002 5 30 SIMA200209404 1 20020321 A 5210 S52176431206 ATTACH ANGLE AEROSP ATR42 ATR42300 8680920 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP8 INSPECTION, FOUND PASSENGER DOOR LOWER ATTACH ANGLE FOR STEP SHELL IS CORRODED BEYOND LIMITS. REPLAC ED PASSENGER DOOR LOWER ATTACH ANGLE IAW ATR 42 SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053000025 20020530 00025 EU 2002 5 30 SIMA200209405 1 20020321 A 5242 S5387500001200 DOOR AEROSP ATR42 ATR42300 8680920 EU E/E BAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP8 INSPECTION, AFT AVIONICS COMPARTMENT DOOR HAS CORROSION AROUND CIRCUMFERENCE. REPLACED AFT AVIONICS COMPARTMENT DOOR IAW ATR 42 STANDARD PRACTICES MM 20-21-12. (M) 2 H 7 2 4T RT A53EU 2002053000026 20020530 00026 EU 2002 5 30 SIMA200209406 1 20020321 A 5315 S5367240921802 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 INSPECTION, FOUND FLOORBEAM 40 TO BE CORRODED. REPLACED FLOORBEAM 40 IAW ATR 42 SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053000027 20020530 00027 EU 2002 5 30 SIMA200209407 1 20020321 A 5347 S53570201200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP8 INSPECTION, FOUND LEFT MID INBOARD AND LEFT FORWARD OUTBOARD SEAT TRACK CORRODED. REPLACED SEAT TRAC KS IAW EO E1-53MR-271. (M) 2 H 7 2 4T RT A53EU 2002053000028 20020530 00028 EU 2002 5 30 SIMA200209408 1 20020321 A 5313 S5367125722151 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP8 INSPECTION, FOUND STRINGER 17R TO BE CORRODED. REPLACED STRINGER 17R IAW ATR 42 SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053000029 20020530 00029 EU 2002 5 30 SIMA200209409 1 20020227 A 5320 S53371293200 TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP8 INSPECTION, FOUND FORWARD CARGO DRAIN TRACK CORRODED. REPLACED FORWARD CARGO DRAIN TRACK IAW SRM 51- 25-02. (M) 2 H 7 2 4T RT A53EU 2002053000030 20020530 00030 EU 2002 5 30 SIMA200209410 1 20020227 A 5320 S53371293202 ATTACH FITTING AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP8 INSPECTION, FOUND FORWARD CARGO DRAIN TRACK ATTACH PLATE CORRODED. REPLACED FORWARD CARGO DRAIN TRAC K ATTACHED PLATE IAW SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053000031 20020530 00031 EU 2002 5 30 SIMA200209411 1 20020227 A 5312 BULKHEAD AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP8 INSPECTION, FOUND GROUNDING POINTS TO RADOME ON FORWARD PRESSURE BULKHEAD HAVE PITTING CORROSION. RE PAIRED LOWER RIGHT GROUNDING POINT ON FORWARD PRESSURE BULKHEAD ER-1 IAW ATR42 SRM 53-11-10. (M) 2 H 7 2 4T RT A53EU 2002053000032 20020530 00032 EU 2002 5 30 SIMA200209412 1 20020327 A 5320 S5367800820002 ANGLE AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 INSPECTION, FOUND LEFT Z-MEMBER CORRODED. REPLACED LEFT Z-MEMBER IAW ATR42 SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053000033 20020530 00033 EU 2002 5 30 SIMA200209413 1 20020327 A 5320 S5367800822251 FLOOR SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 INSPECTION, FOUND LEFT FLOOR SUPPORT BETWEEN 39-40 CORRODED. REPLACED FLOOR SUPPORT BETWEEN 39-40 IA W SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053000034 20020530 00034 EU 2002 5 30 SIMA200209414 1 20020327 A 5347 S53070308200 CARGO TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP4 INSPECTION, FOUND AFT CARGO SEAT TRACKS TO BE CORRODED. REPLACED SEAT TRACKS IAW EO E1-53MR-271. (M ) 2 H 7 2 4T RT A53EU 2002053000035 20020530 00035 EU 2002 5 30 SIMA200209415 1 20020327 A 5730 S5241053600200 ACCESS PANEL AEROSP ATR42 ATR42300 8680920 EU WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP4 INSPECTION, FOUND OVERWING ACCESS PANELS CORRODED. REPLACED OVERWING ACCESS PANELS IAW ATR42 JIC 57- 00-00OAC10000-012. (M) 2 H 7 2 4T RT A53EU 2002053000036 20020530 00036 EU 2002 5 30 SIMA200209416 1 20020327 A 5320 S53389538212 ATTACH FITTING AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 DURING CPCP4 INSPECTION, FOUND RIGHT FORWARD CARGO LOWER PANEL ATTACH FITTINGS CORRODED. REPLACED RIGHT FORWARD LOWER C ARGO ATTACH FITTINGS IAW ATR 42 SRM 51-25-01 AND 51-25-03. (M) 2 H 7 2 4T RT A53EU 2002053000037 20020530 00037 EU 2002 5 30 SIMA200209417 1 20020327 A 5320 S5367121720402 WEB AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 INSPECTION, FOUND LEFT WEB FROM FRAME 39-40 AT Z-MEMBER CORRODED. REPLACED LEFT WEB FROM FRAMES 39-4 0 AT Z-MEMBER 39-40 IAW SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053000039 20020530 00039 NM 2002 5 30 C1HA200286003 1 20020529 A 2923 105001 PUMP BOEING 727 7272S7 138407Z NM A C1HA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 686CA 22021 STANDBY HYD FLUID DECREASED TO ZERO & GREEN ON LOGHT ON ENG PANEL EXTINGUISHED INFLIGHT. POST FLIGHT REVEALED EVIDENCE OF LEAK ON AROUND STBY PUMP IN WING ROOT.REMOVED & REPLACED STANDBY PUMP ASSY IAW B727MM 29-21-11 LEAK & OPS CHK GOOD Q UANTITY NORMAL REMOVED & REPLACED STANDBY SYSTEM PRESSURE FILTER DUE TO PUMP DAMAGE IAW MM 29-21-32 & MM 29-21-21 LEAK A ND OPS CHK GOOD - OK FOR SERVICE 2 L 7 3 4F A3WE 2002053000041 20020530 00041 NM 2002 5 30 219PA0001 1 20020529 A 2420 GENERATOR BOEING 737 737222 1384473 NM A PIDA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 219PA 19956 Rt Generator failed at begining of take-off roll. Reset CSD could not duplicate. 2 L 7 2 4F A16WE 2002061300152 20020613 00152 WP 2002 6 13 02FDEA00366 1 20020528 A 5230 ADG70229 ATTACH FITTING DOUG DC10 DC1010 3022110 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 CENTER CARGO DOOR SNUBBER ATTACH ARM CRACKED. REMOVED SNUBBER PER MM 52-32-07-2. 2 L 7 3 4F A22WE 2002053000044 20020530 00044 WP 2002 5 30 200200266 1 20020528 A 5315 991159091 FLOORBEAM DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 835F 48005 WHILE ACCOMPLISHING POSITION SENSOR INSTALLATION ON THE CONTROL COLUMN, DAMAGE WAS FOUND ON THE BS 120 FLOORBEAM WEB. T WO HORIZONTAL CRACKS IN THE WEB. REPAIR WAS MADE BY TRIMMING THE WEB TO REMOVE THE CRACKS, PERFORMING A HFEC TO ENSURE DAMAGE REMOVAL AND FABRICATING AND INSTALLING REPAIR PARTS AS CALLED OUT IN EAC ECRA N835F-53-MD81-005. 2 L 7 2 4F A6WE 2002053000046 20020530 00046 NE 2002 5 30 2002F00517 2 20020512 A 7532 AC67926 BLEED VALVE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE MALFUNCTIONED G AMTA K NONE R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 11 553TZ 2141 2141 32587 31808 FLIGHT NUMBER 926, ON DESCENT IN V NAV, AUTO THROTTLES ON, THE RIGHT ENGINE SURGES BETWEEN 1.43 TO 1.33 EPR. ALL OTHER ENGINE PARAMETERS SURGE AS WELL. MAINTENANCE REMOVED AND REPLACED THE HP3 BLEED VALVE AND PERFORMED TEST 3 IP/HP AIRFLO W TEST IN ACCORDANCE WITH MM 71-00-00, PAGE 521. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002053000050 20020530 00050 NM 2002 5 30 2002UALA00730 1 20020417 A 5242 LATCH AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE E/E BAY DOOR OUT OF ADJUST A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 826UA 989 CREW REPORTS NOISE-VIBRATION-DRONING IN FORWARD CABIN COCKPIT AREA. NOISE REDUCED UPON REACHING CRUISE ALTITUDE. VIBRA TION COULD BE FELT IN COCKPIT FLOOR. GROUND ELECTRICAL CONNECTION DOOR VERY LOOSE. ADJUSTED LATCH DOOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2002053000056 20020530 00056 EA 2002 5 30 COMA0260332 1 20020528 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 976CA 13551 7151 R/H LOWER WING PLANK CRACKED AT 640 DB W.S. 95.950.BLENDED OUT DAMAGED AREA AND ROTO PEENED I/A/W REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002053000058 20020530 00058 EA 2002 5 30 COMA0260337 1 20020528 A 5311 60034017351 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS280 CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 986CA 11526 7174 FWD J ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL 9 IS CORRODED.REMOVED AND REPLACED FWD J-ANGLE AT FS 280.00 BETWEEN LBL9 AND RBL 9 I/A/W WVAC EO 601R-53-3229. 2 L 7 2 4F RT A21EA 2002053000084 20020530 00084 NM 2002 5 30 2002UALA00853 1 20020510 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 935UA 26663 RIGHT HAND FORWARD NOSE BODY STATION 188 FRAME CRACKED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002053000085 20020530 00085 NM 2002 5 30 2002UALA00854 1 20020510 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 935UA 26663 STATION 178 BULKHEAD RIGHT HAND CHORD CRACKED AT WL 207 AREA. MAJOR REPAIR ACCOMPLISHED. CHORD ANGLE SPLICE, VERTICAL WEB AND EXTERNAL DOUBLER REPAIRS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002053000087 20020530 00087 NM 2002 5 30 2002UALA00855 1 20020511 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 304UA 23665 SKIN CRACKED AFT OF EQUIPMENT COOLING EXHAUST, STATION 287. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002053000088 20020530 00088 NM 2002 5 30 2002UALA00856 1 20020512 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 937UA 26668 PRESSURE BULKHEAD WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002061200086 20020612 00086 NM 2002 6 12 2002UALA00857 1 20020511 A 2121 MR21265 FAN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 601UA 21862 ELECTRIC SMELL THROUGHOUT CABIN. FOUND LEFT RECIRC FAN MAKING LOUD GRINDING NOISE, CYCLED SWITCH FAN FAILED TO TURN ON. CABIN FILLED WITH SMOKE. REPLACED LEFT RECIRC FAN PER SMC 09-MM 21-25-01. FAN WAS REPLACED. NO FURTHER EVENTS OF S MOKE OCCURRED. RECIRCULATION FAN HAS NOT BEEN RECEIVED BY SHOP 154 FOR FINDINGS. 2 L 7 2 4F 4 F RT A1NM E3NE 2002072200029 20020722 00029 NM 2002 7 22 2002UALA00858 1 20020511 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 794UA 26953 SEAT 1B EEL LIGHT ON SEAT MISSING. REPLACED EEL LIGHT ASSY AT SEAT 1B. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002053000097 20020530 00097 NM 2002 5 30 2002UALA00859 1 20020510 A 2425 1701766 WARNING SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT FALSE INDICATION A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 773UA 26929 FLT GOT A SHEARED BACKUP GENERATOR SHAFT MSG AFTER DEPARTURE. SAMC ADVISED THAT FLIGHT MAY NOT CONTINUE ACROSS ATLANTIC . RETURNED TO IAD. NOT DUMPING FUEL. THERE WERE SEVERAL MAINTENANCE MESSAGES PRIOR TO THE RIGHT BACKUP GENERATOR SHEA RED SHAFT MAINTENANCE MESSAGE. THE AIRCRAFT RETURNED TO FIELD. THE RIGHT BACKUP GENERATOR WAS REPLACED. THE UNIT RECE IVED IN UAL SHOP AND FOUND THAT THE SHAFT WAS NOT SHEARED. REQUESTED BOEING TO FOLLOW UP ON THIS OCCURRENCE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002053000101 20020530 00101 NM 2002 5 30 2002UALA00860 1 20020512 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 CABIN CREASE BEAM WEB UPPER O/B CORRODED BETWEEN STATION 1160 AND 1180 RBL 70 STR 17R. MAJOR REPAIR ACCOMPLISHED. REPL ACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000104 20020530 00104 NM 2002 5 30 2002UALA00862 1 20020511 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 LEFT HAND SIDE OF FUSELAGE, 7 FT FWD OF DOOR 2L LOWER EDGE, HAS DENT THAT IS 4 INCHES LONG AND 3 INCHES WIDE WITH A DEPT H OF .095. DENT IS NEXT TO SKIN DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000107 20020530 00107 NM 2002 5 30 2002UALA00864 1 20020512 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 CABIN CREASE BEAM WEB IS CORRODED STATION 1020-1040 LBL 68-70, WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000108 20020530 00108 NM 2002 5 30 2002UALA00865 1 20020512 A 5320 CLIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 CABIN CREASE BEAM CLIP IS CORRODED, STATION 1037, LBL 70, WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000111 20020530 00111 NM 2002 5 30 2002UALA00867 1 20020512 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 CABIN CREASE BEAM INNER CHORD CORRODED STATION 730 LBL 69. MAJOR REPAIR ACCOMPLISHED. INNER CHORD REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000112 20020530 00112 NM 2002 5 30 2002UALA00868 1 20020510 A 5320 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 CABIN FLOOR BODY STATION 1695 TO 1713 RBL 50 SHEAR WEB IS CORRODED ON UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED. REPLAC ED SHEAR WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000113 20020530 00113 NM 2002 5 30 2002UALA00869 1 20020510 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 CABIN FLOORBEAM STATION 1680 CAP RBL 53 TO LBL 54 CORRODED. MAJOR REPAIR ACCOMPLISHED. CABIN FLOORBEAM CAP STRAP REPAI R INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000117 20020530 00117 NM 2002 5 30 2002UALA00873 1 20020511 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 CABIN FLOORBEAM UPPER T-CAP CORRODED AT STATION 324 FROM 35 RBL TO 60 RBL AT STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW T-CAP FROM LBL 7 TO RBL 70. 2 L 7 2 4F 4 F RT A2NM E17NE 2002053000118 20020530 00118 NM 2002 5 30 2002UALA00874 1 20020513 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 CABIN FRAME AT STATION 847 STRINGER 9R IS CRACKED AT RIVET. MAJOR REPAIR ACCOMPLISHED. FRAME DOUBLER MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002053000120 20020530 00120 NM 2002 5 30 2002UALA00876 1 20020515 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 937UA 26668 CABIN FLOORBEAM AT BODY STATION 294 HAS EXCESSIVE MATERIAL LOSS AT RBL 44 DUE TO CORROSION REMOVAL. MAJOR REPAIR ACCOMP LISHED. REPLACED CHORD AND SPLICES. 2 L 7 2 4F 4 F RT A16WE E2GL 2002053000121 20020530 00121 NM 2002 5 30 2002UALA00877 1 20020514 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 CABIN CREASE BEAM ANGLE IS CORRODED FROM STA 270 TO STA 360 RBL 64 TO RBL 53. MAJOR REPAIR ACCOMPLISHED. REPLACED CREA SE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002053000122 20020530 00122 NM 2002 5 30 2002UALA00878 1 20020514 A 3397 WIRE HARNESS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 652UA 25390 SECTION OF FLOOR EMERGENCY EXIT LIGHT BEGINNING AT RIGHT SIDE CLOSET AT MID GALLEY AND ENDING AT AFT EDGE OF MID LAV FOR WARD OF ROW 15 IS INOPERATIVE. REPAIRED CABLE EMERGENCY ESCAPE PATH LIGHTING. 2 L 7 2 4F 4 F RT A1NM E24NE 2002053000123 20020530 00123 NM 2002 5 30 2002UALA00879 1 20020514 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 DOOR THRESHOLD CEILING EMERGENCY EXIT LIGHTS INOP AT DOORS 4L & 4R, 3L, 2L AND 2R. RELAMPED EMERGENCY EXIT LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2002053000125 20020530 00125 NM 2002 5 30 2002UALA00882 1 20020516 A 5310 DOOR FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 937UA 26668 AFT CARGO PIT CUTOUT, LOWER SILL FRAME CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED SILL FRAME CHANNEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002053000136 20020530 00136 EU 2002 5 30 DHL2002363006 1 20020529 A 3242 2870921 CONTROL BOX AIRBUS 300 A300B4203 3930306 EU DEFECTIVE A DHLA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 363DH 85 DURING INITIAL TAKEOFF THE BRAKES HOT LIGHT ILLUMINATED TO 220(#8). TAKEOFF WAS REJECTED. ABNORMAL PROCEDURES COMPLETED. RETURNED TO START BLOCKS.REMOVED & REPLACED BRAKE CONTROL BOX. OPS CK GOOD IAW DHL MM 32-42-72.BRAKE FANS OPS CK GOOD I AW 32-48-00. 2 L 7 2 4F RT A35EU 2002053000138 20020530 00138 NE 2002 5 30 DLM88020497 2 20020501 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE #1 ENGINE UNSERVICEABLE A DALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 27 990DL 26400 53342 726047 ON CLIMB OUT VIBRATION FELT IN YOKE AND LOUD NOISE HEARD IN REAR OF A/C. WHEN LT THROTTLE RETARDED NOISE AND VIBRATION D ECREASED. CA BOROSCOPED NO.1 ENG S/N 726047 FOUND 3 1ST STAGE FAN BLADES BENT FWD. REPLACED NO.1 ENG C-1FAN PER TRANS 9T133 2 L 7 2 4F 4 F RT A6WE E9NE 2002053000139 20020530 00139 NM 2002 5 30 DLM88020498 1 20020502 A 3600 UNK CLAMP DOUG MD88 MD88 3023688 NM #2 ENGINE LOOSE A DALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 27 928DL 49715 TAIL COMPT HIGH WARNING DURING CLIMBOUT CA FOUND RT CROSSBLEED VALVE CLAMP LEAKING TIGHTENED CLAMP LK CKS GOOD. 2 L 7 2 4F RT A6WE 2002053000140 20020530 00140 NM 2002 5 30 DLM88020513 1 20020507 A 7600 750033503 DUCT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE #2 ENGINE BLOWN A DALA K NONE S AFFECT SYSTEMS LD LANDING 1 SO 27 922DL 49646 725436 RT ENG THROTTLE AND FUEL LEVER BINDING WORK IN PROGRESS. PLEASE UPDATE. CA FND A/I DUCT BLOWN. REPLD.ANTI-ICE VLV PRESSURE SWITCH.BAND DUCT. LEAK CKS GOOD. 2 L 7 2 4F 4 F RT A6WE E9NE 2002053000141 20020530 00141 NM 2002 5 30 DL72S020527 1 20020508 A 5330 SKIN BOEING 727 727232 1384082 NM FS 1040, S-4L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 FUSELAGE / SKIN / STRG. 4L / FS 1030-1110 / SKIN LAP JOINT: CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 1030 & 110 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONFIRMED A TOTAL OF 6 CRACKED FASTENER LOCATIONS. THE CRACKED AREAS OF THE SKIN WERE REPAIRED WITH EXTERNAL ALUMINUM DOUBLERS ON A TIME-LIMITED BASIS PER ER/A 383056-14AD. 2 L 7 3 4F A3WE 2002053000142 20020530 00142 NM 2002 5 30 DL72S020528 1 20020508 A 5330 SKIN BOEING 727 727232 1384082 NM S-4L, FS 400 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 FUSELAGE / SKIN / STRG. 4L / FS 360-480 / SKIN LAP SPLICE : CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 & 480 REVEALED CRACK INDICATIONS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC CONFIRMED A TOTAL OF 4 CRACK LOCATIONS. THE CRACK LOCATIONS WERE REPAIRED WITH EXTERNAL ALUMINUM DOUBLERS ON A TIME-LIMITED BASIS PER ER/A 383082-14AD, REV A. 2 L 7 3 4F A3WE 2002053000143 20020530 00143 NM 2002 5 30 DL76S020556 1 20020516 A 2400 CABLE BOEING 767 767332 1382001 NM _AFT FUS SHORTED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 137DL 0 25306 0 APU GENERATOR FEEDER CABLE SHORTED ABOVE WATER TANK @STA 16 00. ARCHING AND SOME HEAT DAMAGE TO AREA. CA RPLD FEEDER CABLE AND PERFORMED C/W EO 1-74974-3 REV B / FEEDER CABLE MODIFICATION. REPAIRED DAMAGED FEEDER CABLE STANDOFF BRACKET AT STA. 1582 PER SRM 51-70 2 L 7 2 4F RT A1NM 2002053000144 20020530 00144 NM 2002 5 30 DL72W020558 1 20020516 A 5700 UNK ANGLE BOEING 727 727247 138408F NM R/H WHEEL WELL CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 CRACK ON MLG W/W VERT ANGLE STA. 913 @ "H" BRACKET INSTALL TEMPORARY REPAIR PER M/M 53-11-000-8 2 L 7 3 4F A3WE 2002053000145 20020530 00145 NM 2002 5 30 DL738020559 1 20020516 A 3350 GE767 BULB BOEING 737 737832 13844CF NM LT FWD OVER WING BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3768 29630 LT. WING ( OVERWING FWD EMERGENCY LIGHT BULB INOP. CA RPLD BULB. 2 L 7 2 4F RT A16WE 2002053000146 20020530 00146 NM 2002 5 30 DLM11020561 1 20020516 A 3350 0201720005 SOCKET DOUG MD11 MD11 3023602 NM SEAT 34H SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 813DE 48600 2030 5/16/02 DURING PREFLIGHT INSPECTION EMERGENCY LIGHT TEST FAILED WITH A EMERGENCY LIGHT BATTERY LOW MESSAGE REPLACED BATTERY 4 AND CHARGER NO HELP FOUND IN SEAT LIGHT SOCKET AT 34H SHORTED. RPLD SAME. 2 L 7 3 4F RT A22WE 2002053000147 20020530 00147 NM 2002 5 30 DLM88020572 1 20020517 A 5330 5936434129 SKIN DOUG MD88 MD88 3023688 NM FS 237, S-30 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 941DL 49814 FUSELAGE / SKIN / FS 237 / STRG. 29L-30 / TCAS ANTENNA : CORROSION AND CRACK REPAIR THE FUSELAGE SKIN WAS FOUND WITH CORROSION AND SMALL CRACKS AT THE LOWER TCAS ANTENNA INSTALLATION AT FS 237 BETWEEN STRINGERS 29L & 30. THE ENTIRE ANTENNA AREA OF THE SKIN WAS CUTOUT TO REMOVE ALL DAMAGE. THE CUTOUT MEASURED 20" X 18". THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 383116-14. 2 L 7 2 4F RT A6WE 2002053000148 20020530 00148 NM 2002 5 30 DL73K020573 1 20020520 A 2900 BACT16BR060606P TEE FITTING BOEING 737 737232 1384475 NM NOSE WHEEL WELL CRACKED A DALA O OTHER K FLUID LOSS LD LANDING 1 SO 27 314DA 23086 IRREG/ LOSS OF A SYSTEM HYDRAULIC QUANTITY FOLLOWED BY A LOSS OF PRESSURE AFTER LOWERING THE LANDING GEAR CA/ FOUND TEE FITTING IN THE NOSE WHEEL WELL CRACKED ____REPLACED SAME SERVICED SYSTEM NO LEAKS FOUND 2 L 7 2 4F RT A16WE 2002053000149 20020530 00149 NM 2002 5 30 DL72S020580 1 20020522 A 5700 UNK WEB BOEING 727 727232 1384082 NM LT WING L/E CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 FOUND ON E1 LETTER CK I/B MOUNT WEB CRACKED #1 SLAT ACTUATOR. REPAIRED PER MM 57-20-21-8. 2 L 7 3 4F A3WE 2002053000150 20020530 00150 NM 2002 5 30 DL72S020581 1 20020522 A 5700 UNK ANGLE BOEING 727 727232 1384082 NM #2 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 FOUND ON E1 LETTER CK LOWER COVE SKIN ATTACH ANGLE IS CRACKED BELOW #2 SLAT TAI DUCT. REPAIRED PER MM 57-54-000-8 2 L 7 3 4F A3WE 2002053000151 20020530 00151 NM 2002 5 30 DL72S020582 1 20020522 A 5520 UNK SKIN BOEING 727 727232 1384082 NM L/H LOWER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 FOUND ON E1 LETTER CK 2 INCH CRACK L/H ELEVATOR LOWER SKIN FWD OF TAB WRITEN ON CARD 79 REPAIRED PER SRM 55-20-3D FIG 5 2 L 7 3 4F A3WE 2002053000152 20020530 00152 NM 2002 5 30 DL72S020584 1 20020522 A 5530 UNK SKIN BOEING 727 727232 1384082 NM R/H LWR VERT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 FOUND ON E1 LETTER CK 1/2 CRACK VISIBLE VERTICAL STAB AT LWR END SKIN AT AFT SPAR R/H SIDE REPAIRED PER M/M 55-30-000-8 FIG 801 2 L 7 3 4F A3WE 2002053000153 20020530 00153 NM 2002 5 30 DL72S020585 1 20020523 A 5330 SKIN BOEING 727 727232 1384082 NM FS 1067, S-28R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 FUSELAGE / SKIN / FS 1067 / STRG. 28R : CORROSION CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 1067 NEAR STRINGER 28R. THE CORROSION WAS REMOVED WITH A 5.75" X 2" CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383227-14. 2 L 7 3 4F A3WE 2002053000154 20020530 00154 NM 2002 5 30 DL76S020593 1 20020524 A 3350 CONNECTOR BOEING 767 767332 1382001 NM CABIN DISCONNECTED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 116DL 23275 SEAT ROW 40 AB EMERGENCY LIGHT INOP. FOUND DURING L/O CK. FOUND WIRE PULLED OUT OF CONNECTOR. REINSERTED PIN IN CONNEC TOR OPS CK NML. L2 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED OPS CK GOOD. 2 L 7 2 4F RT A1NM 2002053000155 20020530 00155 NM 2002 5 30 CALA0200323 1 20020528 A 5330 SKIN BOEING 737 737524 1384721 NM STA 215 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69603 27316 INSPECTION FOUND A 1/8" CRACK IN CAPTAIN'S WINDOW POST SKIN AT STA 215. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-10-01, FIGURE 210. 2 L 7 2 4F RT A16WE 2002053000156 20020530 00156 2002 5 30 DLM11020555 4 20020515 A 3410 06650011001 INDICATOR 066500011001 DOUG MD11 MD11 3023602 NM F/O SIDE OVERHEATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 807DE 2784 48478 AT CRUISE GOT A VERY STRONG ACRID ELEC SMELL NOTICED THAT F/O IVSI WENT BLANK AND WAS HOT TO TOUCH. PULLED CB AND DIVERT ED TO SNN CA FOUND F/OS IVSI TO HAVE BURNT SMELL. WIRING AND CONNECTOR INSPECTED NO TROUBLE FOUND. RPLD F/OS IVSI. 2 L 7 3 4F RT A22WE 2002053000157 20020530 00157 WP 2002 5 30 ABXA010891 1 20020513 A 5330 SKIN DOUG DC8 DC863 302198A WP F.S. 70 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 L-1 DOOR, LOWER FORWARD CORNER, HAD A CRACK INDICATION AT EDGE OF MIDDLE LAYER SKIN. FABRICATED DOUBLER AND TRIPLER, AND REPAIRED AREA IAW DC-8 SRM 51-1-21, 53-20, 53-2-0, 51-1-8, AND DOUGLAS NDT SPM 06-10-01-001. 2 L 7 4 4F 4A25 2002053000158 20020530 00158 WP 2002 5 30 ABXA010892 1 20020508 A 5740 STRAP DOUG DC8 DC863 302198A WP BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 LOWER FRONT SPAR CAP, OUTBOARD OF #3 PYLON, #4 MAIN STRAP WAS BROKEN. REPLACED STRAP AND COMPLIED WITH REA #D857-43875. 2 L 7 4 4F 4A25 2002053000159 20020530 00159 WP 2002 5 30 ABXA010894 1 20020513 A 5300 FITTING DOUG DC8 DC863 302198A WP LONG. 17 RIGHT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 EMPENNAGE INTERIOR LONGERON 17 RIGHT, WAS CRACKED AT F.S. 1769. REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 2002053000160 20020530 00160 WP 2002 5 30 ABXA010895 1 20020513 A 5730 SPAR DOUG DC8 DC863 302198A WP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 LEFT WING AT STATION 515 - 526, HOLES 4 AND 5 FROM THE INBOARD SIDE, SHOWED CRACK INDICATION. REPAIRED AREA IAW REA D857 -43866MR. 2 L 7 4 4F 4A25 2002053000161 20020530 00161 WP 2002 5 30 ABXA010896 1 20020516 A 5300 4772397L FITTING DOUG DC8 DC863 302198A WP EMPENNAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 EMPENNAGE INTERIOR LONGERON 17 LEFT, END FITTING WAS CRACKED AT F.S. 1769. REPLACED END FITTING IAW DC-8 SRM 51-1-21, 51 -3-2 AND 51-1-20D. 2 L 7 4 4F 4A25 2002060500239 20020605 00239 NE 2002 6 5 ARWA20020508 2 20020525 A 7200 JT3D7 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 MALFUNCTIONED A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 345JW 55646 4683 46042 671372 AFTER TAKEOFF, CLIMBING THROUGH 12 THOUSAND OIL QUANTITY CAME DOWN TO 2 GALLONS, FOLLOWED BY OIL PRESSURE LIGHT. PERFOR MED ABNORMAL CHECK LIST NR 4 ENGINE OFF (SHUTDOWN). CAME BACK TO SAN SALVADOR WITHOUT ANY MORE ABNORMALITIES. PREPARED NR 4 ENGINE FOR FERRY FLIGHT IAW ARROW AIR GENERAL MAINTENANCE MANUAL PAGE 6-3-4 AND PAGE 6-3-5. REMOVED AND REPLACED NR 4 ENGINE, OPERATIONS AND LEAK CHECK NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 2002053000162 20020530 00162 NM 2002 5 30 P5CA0200678 1 20020529 A 5411 NONE WEB BOEING 747 747249F 1384849 NM #3 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 CRACK 3.5" LONG FOUND #3 PYLON WEB BETWEEN RIVET HOLES BELOW STIFFNER (STA 211.42, MID SPAR WEB). DOUBLER REPAIR FABRIC ATED IAW SRM 54-14-03, PG 20. THE RIVETS WERE REMOVED PLUS FURTHER 3 EITHER SIDE OF CRACK. 2 OF FURTHER ROWS OF FASTEN ERS PITCHED FORWARD & REAR STIFFNER INCORPORATED DOUBLER ATTACHED USING HI-LOK BOLTS. DOUBLER MFG'D FROM 2024-T3 & TREAT ED IAW MM 51-10-02 & REPAIR SEALED IAW MM 51-31-00. 2 L 7 4 4F A20WE 2002053000163 20020530 00163 WP 2002 5 30 MWEA020384 1 20020525 A 2780 59225351 SLAT DOUG DC9 DC932 3022066 WP LEFT WING PUNCTURED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 602ME 48133 LEFT WING HIT DELTA BAG CART PUNCTURING LEFT OUTBOARD SLAT PANEL. -- REMOVED AND REPLACED SLAT. OPS CHECK GOOD. 2 L 7 2 4F A6WE 2002053100027 20020531 00027 NM 2002 5 31 2002UALA00883 1 20020516 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 STATION 827, STRINGER 9R, FUSELAGE FRAME CRACKED AT RIVET. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED FRAME DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002053100031 20020531 00031 NM 2002 5 31 2002UALA00884 1 20020515 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 562UA 26664 DENT AND GOUGES FOUND IN AND AROUND PREVIOUS REPAIR APPROX 80 INCHES FWD OF DOOR 2L AND 24 INCHES BELOW WINDOW LOWER CUT OUT. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002061200087 20020612 00087 NM 2002 6 12 2002UALA00885 1 20020515 A 2162 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT MALFUNCTIONED A UALA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 654UA 25392 AFTER TAKEOFF, CREW RECEIVED A FWD CARGO DOOR AND EQUIPMENT COOLING MESSAGE. FWD EQPT COOLING EICAS MSG DISPLAYED. PER FORMED OPERATION CHECK PER MM-21-58-00. NO FURTHER MSG DISPLAYED. NO FURTHER WRITE-UPS HAVE OCCURRED FOR EQUIPMENT COO LING SYSTEM. NO PARTS WERE REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002053100032 20020531 00032 NM 2002 5 31 2002UALA00886 1 20020516 A 5330 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 792UA 26934 DAMAGE TO FUSELAGE STATION 508 AND 533 AT STRINGER 39L. LONG TEAR IN SKIN, SEVERED STRINGER AND DEFORMATION OF SHEAR TI E. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002053100033 20020531 00033 NM 2002 5 31 TSAA0233118 1 20020418 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002053100034 20020531 00034 NM 2002 5 31 TSAA0233119 1 20020418 A 3350 9221009 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED AFT ENTRY IDENT EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002053100035 20020531 00035 NM 2002 5 31 TSAA0233120 1 20020418 A 3350 8621006 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED NR 6 EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002053100036 20020531 00036 NM 2002 5 31 TSAA0233121 1 20020418 A 3350 8621006 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED NR 2 EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002053100037 20020531 00037 NM 2002 5 31 TSAA0233122 1 20020418 A 3350 1000679 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED FORWARD SERVICE DOOR EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002053100038 20020531 00038 NM 2002 5 31 TSAA0233123 1 20020418 A 3350 1000679 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED FORWARD ENTRY DOOR EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002053100040 20020531 00040 NM 2002 5 31 TSAA0251107 1 20020412 A 5315 FLOORBEAM BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 FOUND A 2.5 INCH CRACK AT BS 710 FLOORBEAM BBL .07 ON THE WEB. CUT OUT DAMAGED AREA ON THE WEB. FABRICATED A REPAIR DO UBLER IAW FIGURE 6. INSTALLED DOUBLER, STIFFENERS AND FILLERS. REPAIR COMPLETED IAW ECO 2223 R1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002053100041 20020531 00041 NM 2002 5 31 USAABB02048 1 20020422 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 BOS - FOUND L2 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002053100042 20020531 00042 NM 2002 5 31 USAABB02049 1 20020422 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 BOS - FOUND LOW LEVEL EMERGENCY LIGHTS AT ROWS 13, 26, AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. M) 2 L 7 2 4F RT A2NM 2002053100043 20020531 00043 NM 2002 5 31 USAABB02050 1 20020420 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 MCO - FOUND LOW LEVEL EMERGENCY LIGHT AT ROW 1 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002053100044 20020531 00044 NM 2002 5 31 USAABB02051 1 20020423 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 631AU 27809 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002053100045 20020531 00045 NM 2002 5 31 USAABB02052 1 20020501 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 608AU 22204 BOS - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 6 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002053100046 20020531 00046 NM 2002 5 31 USAABB02053 1 20020501 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 608AU 22204 BOS - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4, 9, 13, 18, 23, 26, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED T HE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002053100047 20020531 00047 NM 2002 5 31 USAABB02055 1 20020502 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 627AU 27805 BDL - FOUND R2 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002053100048 20020531 00048 EU 2002 5 31 USAASA02037 1 20020419 A 3350 32145510 POWER SUPPLY AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 179UW 2765 1521 PIT - THE AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE LEFT S IDE EMERGENCY DOOR. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002053100049 20020531 00049 EU 2002 5 31 USAASA02038 1 20020423 A 3397 WIRE AIRBUS A319 A319112 3930323 EU CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 722US 1097 BDL - THE EMERGENCY LIGHT ON SEAT 8C WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED WIRING AT CONNECTOR ON BOTTOM OF SEAT. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002053100050 20020531 00050 EU 2002 5 31 USAASA02040 1 20020428 A 3350 321430 BATTERY AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 176UW 1499 CLT - FOUND THE LEFT AND RIGHT EMERGENCY BATTERIES WON'T TEST. MAINTENANCE REPLACED THE BATTERY POWER PACKS. OPERATION ALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002053100051 20020531 00051 NM 2002 5 31 USAASB02066 1 20020327 A 3350 20121A CHARGER BOEING 737 737401 1384701 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 425US 23992 PHL - MAINTENANCE REPORTED THE AFT RIGHT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE AFT RIGHT EMERGENCY LIGHT BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002053100052 20020531 00052 NM 2002 5 31 USAASB02067 1 20020329 A 2170 V1211 COALESCER BAG BOEING 737 737301 1384611 NM A/C BAY CONTAMINATED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 562AU 23550 CLT - FLT 897 - AFTER TAKEOFF FROM EWR, EN ROUTE TO CLT, A FOUL ODOR WAS REPORTED COMING FROM THE AIR CONDITION PACKS. ODOR DISSIPATED WITHIN 10-15 MINUTES. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT CLT. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT WATER SEPARATOR BAGS. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002053100053 20020531 00053 NM 2002 5 31 USAASB02068 1 20020330 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 573US 23560 PHL - DURING WEEKLY CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT BATTERIES LOW. MAINTENANCE FOUND THE AFT RIGHT BATTERY CHARGER INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER ALONG WITH SEVEN BATTERY PACKS THAT WERE LOW. OPERATIONAL CH ECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002053100054 20020531 00054 NM 2002 5 31 USAASB02070 1 20020411 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 514AU 23700 EWR - MAINTENANCE FOUND THE EMERGENCY LIGHT ON SEAT ROW 5ABC INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER SEAT 5C. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002053100056 20020531 00056 2002 5 31 MEX2002011 4 20020113 A 3417 4056512904 ADC DOUG MD88 MD88 3023688 NM E/E BAY MALFUNCTIONED A ASMF O OTHER J WARNING INDICATION IN INSP/MAINT 1 SW 23 158PL 333 49761 FLT 137 - AGU-MEX - AT PREFLIGHT REVISION, CADC POS 2 FAILED WITH A SIGN OF O/S, BOTH ADI AND TRI O/S, BITE WAS PERFORME D TO BOTH CADC'S RESULTS OK, SW CADC POS 01/02 OK, BOTH CADC WITH FAIL, IT WAS PERFORMED RESET UNIT SW CADC AND BOTH CAD C THE FAIL APPEARS AT PSO 1. DURING RON IN MEX BOTH CADC'S WERE IN THEIR ORIGINAL POSITION WORKING OK. PERFORMED A BIT E TO CADC'S, NO FAIL. THE RIGHT EFIS PANEL WAS REPLACED, TEST OK. (M) 2 L 7 2 4F RT A6WE 2002053100058 20020531 00058 NM 2002 5 31 MEX2002025 1 20020129 A 2910 00915202002 VALVE BOEING 757 7572Q8 1384972 NM HYD SYSTEM FAILED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 301AM 30045 FLT 913 - MTY-MEX - AIRCRAFT RETURNED TO PLATFORM, EICAS MESSAGE LEFT HYD RSVR PRESS WARNING. THREE QUARTERS OF HYDRAUL IC FLUID WAS ADDED, RVSR WAS DISCONNECTED AND CLEANED, AFTER ENGINE WAS STARTED FAIL APPEARED AGAIN, AIRCRAFT TOOKOFF IN THAT CONDITION. HYDRAULIC LEVEL WAS CHECKED AND PERFORMED A FIM PROCEDURE TO ERASE THE MESSAGE. LATER, THE LEFT VENT VALVE WAS REPLACED IAW 29-11-25, TESTS OK. (M) 2 L 7 2 4F RT A2NM 2002053100063 20020531 00063 NM 2002 5 31 MEX2002086 1 20020327 A 3213 59353477 STRUT DOUG MD88 MD88 3023688 NM RT MLG LEAKING A ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 168PL 34095 8716 53174 FLT 6142 - MEX-PVR - DURING OVERNIGHT SERVICE A LEAK WAS DETECTED IN RIGHT MAIN LANDING GEAR. MAIN GEAR STRUT WAS REPLA CED IAW MM 32-11-02. (M) 2 L 7 2 4F RT A6WE 2002053100067 20020531 00067 WP 2002 5 31 MEX2002112 1 20020415 A 5330 SKIN DOUG DC9 DC987 3022087 WP FUSELAGE DAMAGED A ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 204AM 49404 DURING TRANSIT CHECK, FOUND A BREAK IN THE FUSELAGE SKIN OF A PRESSURIZED ZONE, .25 INCHES BY 1 INCH WIDE, AT STATION 21 5 LONGERONS 17 AND 18 OF LEFT SIDE. FUSELAGE SKIN WAS REPLACED IAW ENGINEERING REPAIR NR 02-039. (M) 2 L 7 2 4F RT A6WE 2002053100069 20020531 00069 EU 2002 5 31 SIMA200209418 1 20020327 A 5320 S5367121729801 SILL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 INSPECTION, FOUND PASSENGER DOOR SILL PLATE DRAIN TRACK CORRODED. REPLACED PASSENGER DOOR SILL PLATE DRAIN TRACK IAW SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 2002053100070 20020531 00070 EU 2002 5 31 SIMA200209419 1 20020327 A 5210 S52176226210 CLIP AEROSP ATR42 ATR42300 8680920 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 INSPECTION, FOUND CLIPS ON PAX DOOR INTERCOSTAL TO CENTER RIB ABOVE VENT DOOR CORRODED. REPLACED CLI PS ON PASSENGER DOOR INTERCOSTAL IAW SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053100071 20020531 00071 EU 2002 5 31 SIMA200209420 1 20020327 A 5310 S52176205202 DOOR FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 INSPECTION, FOUND FRAME ON PAX DOOR ABOVE VENT DOOR CORRODED. REPLACED FRAME ON PASSENGER DOOR IAW S RM 51-25-02 AND 51-25-03. (M) 2 H 7 2 4T RT A53EU 2002053100072 20020531 00072 EU 2002 5 31 SIMA200209421 1 20020327 A 5320 S5367129037202 FITTING AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 INSPECTION, FOUND PAX DOOR SILL PLATE AFT TEE FITTINGS CORRODED. REPLACED AFT TEE FITTINGS ON PAX DO OR SILL PLATE IAW SRM 51-25-04. (M) 2 H 7 2 4T RT A53EU 2002053100073 20020531 00073 EU 2002 5 31 SIMA200209422 1 20020327 A 3830 S5368201500601 VENTURI AEROSP ATR42 ATR42300 8680920 EU LAVATORY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 INSPECTION, FOUND LAVATORY VENTURI TUBE CORRODED. REPLACED LAVATORY VENTURI TUBE IAW SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053100074 20020531 00074 EU 2002 5 31 SIMA200209423 1 20020327 A 5320 S5367129034801 FITTING AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP2 INSPECTION, FOUND PAX DOOR SILL PLATE FORWARD TEE FITTING CORRODED. REPLACED PAX DOOR FORWARD TEE FI TTING IAW SRM 51-25-03. (M) 2 H 7 2 4T RT A53EU 2002053100075 20020531 00075 EU 2002 5 31 SIMA200209424 1 20020327 A 2710 S2711009700320 LINK AEROSP ATR42 ATR42300 8680920 EU AILERON CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING INSPECTION, FOUND RIGHT AILERON DUAL LOAD PATH LINK CORRODED. REPLACED RIGHT AILERON DUAL LOAD PATH LINK I AW ATR-42 JIC 27-11-72 RAI 10000-002. (M) 2 H 7 2 4T RT A53EU 2002053100076 20020531 00076 EU 2002 5 31 SIMA200209425 1 20020327 A 5311 S5387110420201 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 MBV - FOUND DURING INSPECTION, FRAME 45 CORRODED BETWEEN STRINGER 18L AND 20 R. INSTALLED NEW SHEER TIE ON FRAME 45 BET WEEN STRINGER 18L AND 20R IAW ATR-42 SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053100077 20020531 00077 NM 2002 5 31 920WA0002 1 20020522 A 7120 65MK713511 BOLT BOEING 737 737236 1384476 NM A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 920WA 21791 Upon engine removal it was discovered that the bolt attaching the aft engine mount to the engine had signs of shear tens ion causing marks in the bolt and slight bending of the bolt. Investigation revealed that the bolt was improperly shimme d. The new bolt was installed per the M.M. procedure. 2 L 7 2 4F RT A16WE 2002053100079 20020531 00079 EU 2002 5 31 SIMA200209426 1 20020327 A 2710 S2711005200201 LINK AEROSP ATR42 ATR42300 8680920 EU AILERON CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING INSPECTION, FOUND RIGHT AILERON DUAL LOAD PATH LINK FITTINGS ON WING IS CORRODED. REPLACED WING FITTINGS F OR RIGHT AILERON DUAL LOAD PATH LINK IAW ATR-42 SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053100080 20020531 00080 EU 2002 5 31 SIMA200209427 1 20020401 A 2710 S2711009700320 LINK AEROSP ATR42 ATR42300 8680920 EU AILERON CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 MBV - DURING FOUND LEFT AILERON DUAL LOAD PATH LINK CORRODED. REPLACED LEFT AILERON DUAL LOAD PATH LINK IAW JIC 27-11-7 2-RAI-10000-002. (M) 2 H 7 2 4T RT A53EU 2002053100081 20020531 00081 EU 2002 5 31 SIMA200209428 1 20020402 A 5210 S5217640600001 SUPPORT AEROSP ATR42 ATR42300 8680920 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 DURING CPCP4 INSPECTION, FOUND ALL PAX DOOR TREAD SUPPORTS HAVE CORROSION. REPLACED ALL PAX DOOR TREAD SUPPORTS IAW SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2002053100084 20020531 00084 EU 2002 5 31 SIMA200209429 1 20020402 A 5753 S57510096200 FLAP AEROSP ATR42 ATR42300 8680920 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING INSPECTION, FOUND LEFT OUTBOARD FLAP FORWARD BEAM ATTACH POINT CORRODED. REPLACED LEFT OUTBOARD FLAP ASSY IAW JIC 57-53-00-RAI-10000-006. (M) 2 H 7 2 4T RT A53EU 2002053100085 20020531 00085 EU 2002 5 31 SIMA200209430 1 20020402 A 5753 S575100972000 FLAP AEROSP ATR42 ATR42300 8680920 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING INSPECTION, FOUND LEFT OUTBOARD FLAP AFT BEAM ATTACH FITTING CORRODED. REPLACED LEFT OUTBOARD FLAP ASSEMBL Y IAW JIC 57-53-00-RAI-10000-006. (M) 2 H 7 2 4T RT A53EU 2002053100088 20020531 00088 EU 2002 5 31 SIMA200209431 1 20020402 A 5753 S57510096201 FLAP AEROSP ATR42 ATR42300 8680920 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING INSPECTION, FOUND RIGHT OUTBOARD FLAP OUTBOARD FORWARD BEAM ATTACH FITTING CORRODED. REPLACED RIGHT OUTBOA RD FLAP ASSY IAW JIC-57-53-00-RAI-10000-006. (M) 2 H 7 2 4T RT A53EU 2002053100091 20020531 00091 EU 2002 5 31 SIMA200209432 1 20020402 A 5753 S57510092200 FLAP AEROSP ATR42 ATR42300 8680920 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING INSPECTION, FOUND LEFT OUTBOARD FLAP MIDDLE FORWARD BEAM ATTACH POINT CORRODED. REPLACED LEFT OUTBOARD FLA P ASSEMBLY IAW JIC 57-53-00-RAI-10000-006. (M) 2 H 7 2 4T RT A53EU 2002053100092 20020531 00092 SO 2002 5 31 SIMA200210004 1 20020328 A 5320 14522461003 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - THIS IS A LEVEL 2 FINDING. FORWARD DIAMOND GUSSET HAS CORROSION AROUND NUTPLATE AT FRAME 20. REMOVED AND REPLACE D SERVICEABLE FORWARD DIAMOND GUSSET IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002053100093 20020531 00093 SO 2002 5 31 SIMA200210005 1 20020328 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - THIS IS A LEVEL 2 FINDING. OMEGA BEAM HAS CORROSION AT FRAME 20. FABRICATED A DOUBLER FILLER AND SHIMS AND INSTA LLED IAW EMB135 SRM 53-21-10, 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002053100094 20020531 00094 NM 2002 5 31 USAASB02065 1 20020327 A 3260 189929 UPLOCK SENSOR BOEING 737 7373B7 1384580 NM LT MLG DEFECTIVE A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 383US 22956 PHL - FLT 1742 - AFTER TAKEOFF FROM BNA, EN ROUTE TO PHL, THE RIGHT MAIN LANDING GEAR RED LIGHT REMAINED ILLUMINATED WIT H GEAR IN THE UP POSITION. WHEN LANDING GEAR WAS PUT BACK DOWN, THE RED LIGHT EXTINGUISHED AND THE GREEN LIGHT ILLUMINA TED. FLIGHT LANDED AT PHL WITHOUT FURTHER INCIDENT. MAINTENANCE CONFIRMED FAULT AND FOUND THE RIGHT MAIN LANDING GEAR UPLOCK SENSOR S74 DEFECTIVE. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR UPLOCK SENSOR S74. RIGHT MLG INDICATION CHEC KS NORMAL. (M) 2 L 7 2 4F RT A16WE 2002053100095 20020531 00095 SO 2002 5 31 SIMA200210006 1 20020328 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - THIS IS A LEVEL 2 FINDING. CENTER BEAM GUSSET IS GOUGED FROM FRAME 20 TO 22. UPPER SURFACE IS CORRODED AROUND FA STENERS. REMOVED AND REPLACED GUSSET IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002053100096 20020531 00096 SO 2002 5 31 SIMA200210007 1 20020328 A 5320 14521725615 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - THIS IS A LEVEL 2 FINDING. RIGHT FORWARD DOOR SILL HAS CORROSION AROUND NUTPLATE AT FRAME 20. REMOVED CORROSION AROUND NUTPLATE IAW EMB 135 GST 1067/02. (M) 2 L 7 2 4F RT T00011AT 2002053100097 20020531 00097 SO 2002 5 31 SIMA200210008 1 20020328 A 5320 BRACKET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - THIS IS A LEVEL 2 FINDING. PASSENGER DOOR THRESHOLD ATTACHMENT BRACKETS ARE CORRODED AROUND NUTPLATE AT FRAME 16 AND 17. REPAIRED CORROSION ON PAX DOOR THRESHOLD IAW EMB 135 GST-1067/02. (M) 2 L 7 2 4F RT T00011AT 2002053100098 20020531 00098 SO 2002 5 31 SIMA200210009 1 20020328 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - THIS IS A LEVEL 2 FINDING. FORWARD DIGITAL HAS CORROSION AROUND FASTENERS AT FRAME 16. REPAIRED CORROSION IAW EM B GST-1067/02. (M) 2 L 7 2 4F RT T00011AT 2002053100099 20020531 00099 SO 2002 5 31 SIMA200210010 1 20020328 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - THIS IS A LEVEL 2 FINDING. CORROSION FOUND ON FORWARD CORNER OF AFT SERVICE DOOR SILL AT FRAME 22. REPAIRED CORR OSION IAW EMB 135 GST-1067/02. (M) 2 L 7 2 4F RT T00011AT 2002053100100 20020531 00100 SO 2002 5 31 SIMA200210011 1 20020328 A 5320 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - THIS A LEVEL 2 FINDING. AFT DIAMOND GUSSET IS CORRODED AT FRAME 22. REPAIRED CORRODED AREA IAW EMB135 GST-1067/0 2. (M) 2 L 7 2 4F RT T00011AT 2002053100101 20020531 00101 SO 2002 5 31 SIMA200210012 1 20020328 A 5320 14522459003 SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - THIS IS A LEVEL 2 FINDING. CENTER BEAM RAMP SUPPORT CORRODED AT FRAME 20. REMOVED AND REPLACED RAMP IAW EMB135 S RM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002053100105 20020531 00105 SO 2002 5 31 SIMA200210013 1 20020328 A 5320 14521725615 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - THIS IS A LEVEL 2 FINDING. SERVICE DOOR SILL IS CORRODED AROUND NUTPLATES, FRAME 20-22. REPAIRED CORRODED AREA I AW EMB135 GST 1067/02. (M) 2 L 7 2 4F RT T00011AT 2002053100107 20020531 00107 SO 2002 5 31 SIMA20021003 1 20020403 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OU T. FABRICATED A DOUBLER, FILLER, AND TWO SHIMS. WORK DONE IAW EMB145 SRM 145/1142, CHAPTER 53, REV 17, 53-21-10, AND S TANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002053100108 20020531 00108 2002 5 31 000146 4 20020529 A 2310 AUDIO PANEL SAAB SF340 SF340A 7850100 EU COCKPIT FAULTY A CHQA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 152 CREW REPORTED FEEDBACK IN AUDIO PANELS. REMOVED AND REPLACED RT & LT AUDIO PANEL AND OPS CHECK GOOD WITH CHAUTAUQUA HEA D SET A ND STATIC WICK. 2 L 7 2 4T RT A52EU 2002053100109 20020531 00109 NM 2002 5 31 TSAA0251108 1 20020412 A 5314 6545866 KEELBEAM BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA O OTHER O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 FOUND CRACK ON THE LOWER CHORD IN THE LEFT MAIN WHEEL WELL AT BS 652 KEEL BEAM FUSELAGE SKIN AREA. TRIMMED OUT CRACK AN D VERIFIED REMOVED USING HFEC METHOD. FABRICATED A REPAIR ANGLE AND FILLER. REPAIR COMPLETED IAW ECO 2726R3 PART II. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002053100110 20020531 00110 NM 2002 5 31 TSAA0251109 1 20020412 A 5314 A6545866 KEELBEAM BOEING 737 737230 1384401 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 FOUND CORROSION ON THE KEEL BEAM LOCATED IN THE MAIN WHEEL WELL AT BS 685 LEFT CHORD AT THE MOUNT SCREW HOLES. REPAIRED BY REMOVING CORROSION IAW DETAIL VII, VIII AND IX. REPAIR COMPLETED IAW SRM 53-10-1, FIGURE 7, BS 685. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002053100111 20020531 00111 NM 2002 5 31 TSAA0251110 1 20020412 A 5320 6548687 FITTING BOEING 737 737230 1384401 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 FOUND CORROSION ON THE FORWARD LOWER EXTRUSION ON THE FRAME IN THE LEFT WHEEL WELL AT BS 680. REMOVED THE FORWARD LOWER EXTRUSION. INSTALLED NEW EXTRUSION SECTION IAW SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002053100112 20020531 00112 NM 2002 5 31 TSAA0251111 1 20020412 A 5320 6548687 FITTING BOEING 737 737230 1384401 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 FOUND CORROSION ON THE FORWARD LOWER EXTRUSION, LOWER FRAME SECTION IN THE RIGHT WHEEL WELL BETWEEN BS 680 AND BS 690. CUT OUT DAMAGED SECTION OF WEB. FABRICATED AND INSTALLED NEW WEB SECTION IAW SRM 51-40-2. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4F RT A16WE 2002053100113 20020531 00113 NM 2002 5 31 TSAA0251130 1 20020510 A 5754 6573714 SLAT BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 24031 FOUND CORROSION ON THE RIGHT WING AFT OF THE NR 5 SLAT FITTING. BLENDED OUT CORROSION. FABRICATED AND INSTALLED PARTS. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4U 4 F RT A16WE E2EA 2002053100114 20020531 00114 NM 2002 5 31 TSAA0251133 1 20020510 A 5330 6573746 SKIN BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE FUSELAGE GOUGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 24031 FOUND GOUGE IN SKIN AT STRINGER 16L AT BS 843. BLENDED OUT DAMAGED AREA TO A SMOOTH SURFACE. VERIFIED NO CRACKS USING HFEC. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4U 4 F RT A16WE E2EA 2002053100115 20020531 00115 NM 2002 5 31 TSAA0253131 1 20020423 A 5315 654541041 FLOORBEAM BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 24031 FOUND CRACKS AT BL 0 FLOOR BEAM AT BS 663 AND BETWEEN BS 700-717 WEB. REMOVED AND DISCARDED A SECTION OF THE WEB AND DO UBLER CONTAINING THE CRACKS. FABRICATED ALL REPAIR PARTS. INSTALLED SPLICE ANGLES AND STRAPS WITH NUT PLATES. COMPLET ED INSTALLATION OF REINFORCING ANGLE, FILLER AND SPLICE PLATES. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4U 4 F RT A16WE E2EA 2002053100116 20020531 00116 EU 2002 5 31 000147 1 20020529 A 7720 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU COCKPIT MALFUNCTIONED A CHQA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 11 104 RT ENGINE O/T ON TAKEOFF, LT ALPHA VANE LIGHT. CHECKED ALL L/P AND H/P BLEED LINES, PRESSURE TESTED AND FOUND NO LEAKS. RAN ENGINE TO 108 PERCENT TORQUE. ALL PARAMETERS INCLUDING TEMP WITHIN LIMITS. 2 L 7 2 4T RT A52EU 2002061300153 20020613 00153 NM 2002 6 13 02FDEA00367 1 20020529 A 5320 WEB BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 SHEAR WEB BULGING AROUND FASTENERS BS 1147, LBL 53-61, WL 208. REMOVED AND REPLACED WEB & FLOORBEAM PER SRM 51-40-2 FIG 1 & 53-10-8 FIG 3. 2 L 7 3 4F RT A3WE 2002061000197 20020610 00197 NM 2002 6 10 02FDEA00368 1 20020529 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 209FE 22931 CORROSION BS 870, WL 208, LBL 65 TO RBL 65. REMOVED AND REPLACED FLOORBEAM PER EA 7- 5310-54227. 2 L 7 3 4F RT A3WE 2002061000198 20020610 00198 NM 2002 6 10 02FDEA00369 1 20020529 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 209FE 22931 CORROSION ON TOP OF FRETTED FLOORBEAM BS 740, WL 208, LBL 60 - RBL 65. REMOVED AND REPLACED FLOORBEAM PER SRM 51-20-4, 51-30-2. 2 L 7 3 4F RT A3WE 2002053100124 20020531 00124 NE 2002 5 31 CA020521004 2 20020411 A 7310 416209004 FITTING BELL 222 222U 1182140 SW LYC LTS101 LTS101750C1 41560 NE FUEL SYSTEM WORN W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) ENROUTE TO VICTORIA AIRPORT STRONG SMELL OF JET FUEL NOTICED. THEY WERE JUST IN ZONE WITH TOWER. PILOT DECLARED EM ERGENCY WITH AIRPORT. A/C LANDED WITH NO INCIDENT AND AIR TAXI BACK TO HANGAR. INVESTIGATION OF ODOUR FUEL CONTROL TO START FUEL LINE FITTING ON FUEL CONTROL UNIT. SEE LTS101-4.4 ILLUSTRATED PARTS MANUAL SEC. 73-10-00 FIGURE 1 OF FUEL DI STRIBUTION SHEET 1 OF 2. THE FLARE ON FUEL CNTL FITTING WORN. LINE CONNECTING TO FITTING ON FUEL CNTL CHAFED OVER PERIOD OF TIME&WOULD NOT SEAL. LINE FOUND TO BE TIGHT AT TIME OF LEAK RETORQUEING LINE HAD NO EFFECT ON STOPPING THE LEAK. LAT ER INSP OF FLARES 1 G 7 2 3U 3 U H9SW E5NE 2002053100125 20020531 00125 EA 2002 5 31 CA020527001 2 20020507 A 7200 ENGINE BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL RIGHT MAKING METAL W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) ENGINE CHIP PLUG INDICATION NOTED WITH NO CHANGE IN ENGINE PARAMETERS, ENGINE SHUT DOWN CARRIED OUT IN CRUISE FLIG HT. INSPECTION OF OIL CHIP PLUG AND ENGINE OIL FILTER REVEALED METAL TRACES, ENGINE WAS REMOVED FOR FURTHER INSPECTION. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 2002053100127 20020531 00127 WP 2002 5 31 AALA20020561 1 20020430 A 3350 LIGHT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 488AA 49681 DURING OVERNIGHT MAINTENANCE FORWARD DETACHABLE EMERGENCY LIGHT MOUNT PINS WONT ENGAGE MOUNTS. REPLACED FORWARD DETACHA BLE EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2002053100128 20020531 00128 WP 2002 5 31 AALA20020562 1 20020430 A 3350 LIGHT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 77421 49333 DURING OVERNIGHT MAINTENANCE, FORWARD LEFT HAD OVERWING EMERGENCY EXIT LIGHT DIM. SECURED GROUND ON FORWARD LEFT HAND O VERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2002053100130 20020531 00130 NM 2002 5 31 0201715524 1 20020526 A 2910 271N61191 HYDRAULIC LINE BOEING 757 757251 1384970 NM LEFT WHEEL WELL LEAKING A NWAA O OTHER K FLUID LOSS LD LANDING 1 GL 01 524US 23618 LEFT HYDRAULIC SYSTEM FAILURE AT 80 KNOTS DURING LANDING ROLLOUT. LOSS OF STEERING RESULTED IN AIRCRAFT BEING TOWED FROM RUNWAY TO GATE. MAINTENANCE DISCOVERED HYDRAULIC LINE TO LEFT DOWNLOCK ACTUATOR LEAKING. REPLACED THE HYDRAULIC LINE PER MM 32-32-581. LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 2002053100132 20020531 00132 WP 2002 5 31 ZW0A0205601 1 20020529 A 3350 2930077 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ZW0A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 13 959U 49704 MAL-FWD OVERHEAD GALLEY LIGHT PN 293-0077 GETS VERY HOT AND SMELLS OF ELECTRICAL BURNING ODOR. DEACTIVATED AND REMOVED BULB. PLACARDED PER MEDP 33-2. PULLED AND BANDED FWD MIS CABIN AND LAV LT CB. HEAT AND SMELL GONE. LAST CHECK-C STL 6/28/01 2 L 7 2 4F A6WE 2002053100133 20020531 00133 WP 2002 5 31 ZW0A0205602 1 20020529 A 2913 80877 PUMP DOUG DC9 DC982 3022082 WP A ZW0A A UNSCHED LANDING O OTHER CL CLIMB 1 CE 13 927TW 49358 LOST LEFT HYD SYSTEM PRESSURE ON CLIMBOUT OF STL. CREW SHUT OFF LH ENG PUMP AND RETURNED TO STL. RR LH ENG PUMP PN 80877 PER MM 29-10-05 PG 201-208. OPS CK PER MM OK. LAST CHECK-C MCI 10/12/01.--CLOSED-- 2 L 7 2 4F A6WE 2002053100134 20020531 00134 NM 2002 5 31 AWXA200200474 1 20020512 A 5230 65479528 WEB BOEING 737 7373Q8 1384670 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 0 0 23507 MCN - MAJOR REPAIR - DURING C-15 CHECK A CRACK WAS FOUND AT LOWER FASTNER HOLE OF AFT CARGO DOOR LOWER BEAM WEB, BS 807. MAINTENANCE REPAIRED AFT CARGO DOOR CRACKED WEB LOWER BEAM FASTENER HOLE AT BS 807 IAW E.O. 52-33-02. 2 L 7 2 4F RT A16WE 2002053100135 20020531 00135 NM 2002 5 31 AWXA200200477 1 20020509 A 5313 69781638 WEB BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 0 0 23629 YVR - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND IN THE R/H STRINGER 18A SHEAR BEAM (WEB) AT ATTACHMENT TO STA 7 27 BULKHEAD. MAINTENANCE REMOVED CRACKED WEB AT BS 727, STR 18A R/H; FABRICATED A NEW WEB AND INSTALLED REPAIR IAW B737- 300 SRM 51-10-02, PG. 12. 2 L 7 2 4F RT A16WE 2002053100136 20020531 00136 NM 2002 5 31 AWXA200200478 1 20020509 A 5313 6878163U7 WEB BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 0 0 23629 YVR - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND IN THE L/H STRINGER 18A SHEAR BEAM (WEB) AT ATTACHMENT TO STA 7 27 BULKHEAD. MAINTENANCE REMOVED CRACKED WEB AT BS 727, STR 18A L/H; FABRICATED A NEW WEB AND INSTALLED REPAIR IAW B737- 300 SRM 51-10-02, PG. 12. 2 L 7 2 4F RT A16WE 2002053100137 20020531 00137 NM 2002 5 31 AWXA200200480 1 20020530 A 5330 2024T3050 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 0 0 22645 PHX - MAJOR REPAIR - DURING INSPECTION A CRACK WAS FOUND ON FUSELAGE SKIN AT BS 747, STR 16 L/HCRACK FOUND ON FUSELAGE L /H SIDE APPROX. STA. 747 STR.16L 2 L 7 2 4F RT A16WE 2002053100138 20020531 00138 SO 2002 5 31 RAIA00205162 1 20020510 A 3242 0132AFU1 SENSOR EMB 145 EMB145LR 3260212 SO READS HIGH A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 812HK 636 145373 5318-PIT- LEFT BRAKE TEMPERATURE HIGH DURING TAXI. MAINTENANCE DEFERRED IAW MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AN D REPLACING THE BRAKE TEMP SENSOR. 2 L 7 2 4T RT T00011AT 2002053100139 20020531 00139 2002 5 31 RAIA00205163 4 20020513 A 3100 S800200000 FLIGHT RECORDER JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 552HK 14645 41057 5482-STL- FLIGHT DATA RECORDER WARNING CAME ON. MAINTENANCE DEFERRED IAW MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING THE FLIGHT DATA RECORDER. 2 L 7 2 4T RT A41NM 2002053100140 20020531 00140 SO 2002 5 31 RAIA00205164 1 20020524 A 3242 15622101 TRANSDUCER EMB 145 EMB145 3260210 SO LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 802HK 8558 145066 5258-PIT- #1 HYDRAULIC SYSTEM FAILED. MAINTENANCE REMOVED AND REPLACED LEAKING PRESSURE TRANSDUCER. 2 L 7 2 4F RT T00011AT 2002053100141 20020531 00141 2002 5 31 RAIA00205165 4 20020528 A 3420 HG3010AC02 COMPUTER EMB 145 EMB145 3260210 SO OVERHEATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 803HK 4524 79 145077 5261-ITH- RECEIVED #2 ATTITUDE HEADING REFERENCE SYSTEM WARNING . MAINTENANCE REMOVED AND REPLACED THE #2 AHRS COMPUTER. 2 L 7 2 4F RT T00011AT 2002053100142 20020531 00142 EU 2002 5 31 RAIA00205166 1 20020526 A 2430 51539019E GCU JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 558HK 7591 13 41071 5533-PIA- RIGHT GENERATOR WILL NOT COME ON LINE. MAINTENANCE REMOVED AND REPLACED THE GENERATOR CONTROL UNIT. 2 L 7 2 4T RT A41NM 2002053100143 20020531 00143 SO 2002 5 31 RAIA00205167 1 20020530 A 8012 3375499001 FILTER ELEMENT EMB 145 EMB145 3260210 SO CLOGGED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 807HK 145119 5281-PIT- #2 ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED THE #2 ENGINE START VALVE FILTER. 2 L 7 2 4F RT T00011AT 2002060200001 20020602 00001 SO 2002 6 2 C2XA02IA119 1 20020531 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16918 145397 IAH- DURING PERFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHT BY THE GALLEY OTS. INOP. IAH- MAINTENANCE RMOVED AND RE PLACED THE #3 INVERTER, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002060200002 20020602 00002 SO 2002 6 2 C2XA02IA120 1 20020531 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 IAH- DURING PERFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT LIGHT IN MAIN DOOR WAY INOP. (NEAR FLOOR). MAINTENANCE RE MOVED AND REPLACED THE FWD.EMERGENCY LIGHT INVERTER, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002060200003 20020602 00003 SO 2002 6 2 C2XA02IA121 1 20020531 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 IAH- DURING PREFLIGHT INSPECTION THE CREW NOTED THAT THE EMERGENCY EXIT SIGN IN ROW 12 RIGHT SIDE INOP. IAH- MAINTENA NCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT INVERTER, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTE M, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, 2 L 7 2 4F RT T00011AT 2002060300001 20020603 00001 NE 2002 6 3 2002F00524 2 20020527 A 7200 ENGINE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RIGHT SURGES G AMTA K NONE O OTHER CL CLIMB 1 GL 11 553TZ 32587 31808 FLIGHT NUMBER 209, ON CLIMB-OUT, RIGHT ENGINE EPR BEGAN SURGING +/- 0.1 ALL OTHER INSTRUMENTS FOLLOWED. WHEN AUTOTHROTT LES TURNED OFF, ENGINE STABILIZED. IN CRUISE, ANY MOVEMENT OF THROTTLES WOULD RESTART SURGING. ITEM WAS DEFERRED PER M EL 77-11-01. 2 L 7 2 4F 4 F RT A2NM E12EU 2002060300002 20020603 00002 WP 2002 6 3 2002F00525 1 20020515 A 5320 BEAM LKHEED 1011 1011385115 5265015 WP FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 198AT 193B1111 DURING SCHEDULED INSPECTION MID FUSELAGE SECTION, LOWER GALLEY BOX BEAM AT FS 901, LBL 15 TO RBL 15 (FRONT OF LIFTS) WAS FOUND WITH LEVEL 2 CORROSION. MAINTENANCE REMOVED GALLEY BOX BEAM PER SRM 51-40-01. FABRICATED NEW BOX BEAM AND INSTA LLED IN ACCORDANCE WITH SRM 51-40-01. 2 L 7 3 4F A23WE 2002060300003 20020603 00003 WP 2002 6 3 2002F00526 1 20020514 A 5320 WEB LKHEED 1011 1011385115 5265015 WP FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 198AT 193B1111 DURING SCHEDULED INSPECTION FS 419, RBL 22 SHEAR WEB FOUND WITH LEVEL 2 CORROSION. MAINTENANCE REMOVED CORROSION ON WEB IN ACCORDANCE WITH SRM 53-11-11. SPLICE PLATE OF RBL 22, LONGERON CORRODED BEYOND LIMITS. REMOVED AND REPLACED SPLICE PLATE AND TWO FRAME CLIPS IN ACCORDANCE WITH SRM 51-40-01, AND 51-10-05. 2 L 7 3 4F A23WE 2002060300004 20020603 00004 WP 2002 6 3 2002F00527 1 20020515 A 5320 WEB LKHEED 1011 1011385115 5265015 WP FUSELAGE CORRODED G K NONE O OTHER IN INSP/MAINT 1 GL 11 198AT 193B1111 DURING SCHEDULED INSPECTION AFT FUSELAGE SECTION, C3 CARGO PIT, HORIZONTAL WEB AT STATION 1628, RBL 27 TO RBL 40 FLOOR L EVEL HAS CORROSION AROUND SURFACE AND NUT PLATES. MAINTENANCE REMOVED AND REPLACED DAMAGED WEB IN ACCORDANCE WITH SRM 5 1-40-01. 2 L 7 3 4F A23WE 2002060300006 20020603 00006 SO 2002 6 3 SIMA200207802 1 20020225 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 23 603AE 145055 ABI - THIS IS A LEVEL 2 FINDING, LEFT SILL IS CORRODED BETWEEN FRAMES 19 AND 21. BLENDED CORROSION, FOUND TO BE ACCEPTE D AS IS IAW EMB GST-0714/02. (M) 2 L 7 2 4T RT T00011AT 2002060300007 20020603 00007 SO 2002 6 3 SIMA200207803 1 20020225 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 23 603AE 145055 ABI - THIS IS A LEVEL 2 FINDING, LEFT SILL IS CORRODED BETWEEN FRAMES 37-39. BLENDED AREA IAW EMB GST-0714/02 AND RETRE ATED FOR CORROSION IAW EMB 145 CPM 51-21-04 AND 51-21-05. (M) 2 L 7 2 4T RT T00011AT 2002060300008 20020603 00008 SO 2002 6 3 SIMA200208305 1 20020220 A 5330 SKIN EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AE 145068 ABI - THIS IS A LEVEL 2 FINDING, CORROSION FOUND ALONG FUSELAGE SKIN EDGE JUST BELOW BATTERY COMPARTMENT ACCESS DOOR. B LENDED, INSPECTED DAMAGE AND IT WAS ACCEPTED AS IS IAW EMB GST 0623/02. (M) 2 L 7 2 4F RT T00011AT 2002060300009 20020603 00009 SO 2002 6 3 SIMA200209301 1 20020324 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL IS CORRODED AT FRAME 39. REPAIRED RIGHT SILL AT FRAME 39 IAW EMB 145 GST-10 14/02. (M) 2 L 7 2 4F RT T00011AT 2002060300010 20020603 00010 SO 2002 6 3 SIMA200209302 1 20020322 A 5320 BEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, RIGHT HAT BEAM IN GALLEY CORRODED BETWEEN FRAMES 17 AND 19. REPAIRED RIGHT HAT BEAM IN GALLEY BETWEEN FRAME 17 AND 19 IAW GST-1014/02. (M) 2 L 7 2 4F RT T00011AT 2002060300011 20020603 00011 NE 2002 6 3 00029 2 20020529 A 7200 ENGINE LEAR 25 25 5170506 CE GE CJ610 CJ6106 30006 NE RIGHT FLAMED OUT E HAEA B EMER. DESCENT X ENGINE FLAMEOUT CL CLIMB 1 SW 05 525TW 011 240C102A ACFT ROUTE FROM FNT TO ADS CLIMBING THROUGH FL398 FOR FL430 RT ENGINE FLAME-OUT, REQUEST LOWER ALT FL260. ENGINE RESTAR TED AND CLIMB BACK TO FL390 PROCEEDED TO ADS. MAINTENANCE AT ADS PERFORMED FLAME-OUT INSPECTION PER THE GE M/M AND PERF ORMED ENGINES RUNS, NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4J 4 J A10CE 1E16 2002060300012 20020603 00012 WP 2002 6 3 0201679866 1 20020526 A 2750 ROLLER DOUG DC9 DC951 3022051 WP WING LACK OF LUBE A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 775NC 47785 DURING TAKEOFF, FLAPS REMAINED AT 5 DEGREES. VISUALLY CONFIRMED FLAPS WERE EXTENDED. FLIGHT RETURNED TO MSP AND LANDED UNEVENTFULLY. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM ON THE GROUND. FLAP RETRACTION CHECKED GOOD. LUBRICATE D THE DOOR ROLLERS ON BOTH SIDES. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002061900188 20020619 00188 2002 6 19 0201696637 4 20020523 A 2330 VIDEO UNIT BOEING 747 747251B 1384892 NM CABIN FAILED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 637US 23548 NR 2 VTR OVERHEATS AND SMELLS LIKE BURNING WIRE. FLIGHT CONTINUED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED NR 2 VT R. OPERATIONAL CHECK OK. 2 L 7 4 4F A20WE 2002060300013 20020603 00013 NM 2002 6 3 0201706306 1 20020522 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 666US 23821 DURING LINE CHECK, FOUND ZONE 'C' LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED LIGHT AND RECONNECTED WIRES. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002060600183 20020606 00183 NM 2002 6 6 2002UALA00887 1 20020514 A 2133 7110032 OUTFLOW VALVE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 930UA 26655 DURING CLIMBOUT CABIN WOULD NOT PRESSURIZE. MADE UNSCHEDULED LANDING. A FAILURE IN THE AFT OUTFLOW VALVE A/C MOTOR CAU SED LACK OF VALVE MOVEMENT. REPLACED THE (AFT) MAIN OUTFLOW VALVE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300014 20020603 00014 NM 2002 6 3 2002UALA00888 1 20020514 A 5730 65454877 DOOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE WING DEPARTED A UALA K NONE D INFLIGHT SEPARATION CR CRUISE 1 WP 29 302UA 23643 DURING FLIGHT WING OUTBOARD FUEL BOOST PUMP DOOR DEPARTED AIRCRAFT. REPLACED DOOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060600184 20020606 00184 NM 2002 6 6 2002UALA00889 1 20020515 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 DOOR THRESHOLD CEILING EEL LIGHTS INOP AT DOORS 4 L & R, 3 L, 2 L & R. RELAMPED LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2002072200017 20020722 00017 2002 7 22 2002UALA00890 4 20020516 A 3140 8221033100 COMPUTER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 666UA 29238 R EICAS CMPTR EICAS MSG DISPLAYED. REPLACED EICAS COMPUTER AND LOADED CORRECT OPS AND OPC SOFTWARE. OPS OK. THERE WAS NO FAULT FOUND IN THE REMOVED EICAS COMPUTER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002060300015 20020603 00015 NM 2002 6 3 2002UALA00891 1 20020516 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 EXTERNAL FUSELAGE STATION 420 STRINGER 21R SKIN IS DENTED AND CREASED AT STRINGER. MAJOR REPAIR ACCOMPLISHED. INSTALLE D SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300016 20020603 00016 NM 2002 6 3 2002UALA00892 1 20020516 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 RIGHT HAND OVERWING FUSELAGE FRAME AT BODY STATION 616 IS CRACKED AT INNER CHORD, BELOW BOTTOM FASTENER, JUST BELOW CABI N FLOOR. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE DOUBLER AND FILLER MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300017 20020603 00017 NM 2002 6 3 2002UALA00893 1 20020516 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 STATION 927 TO 1006 RIGHT HAND INBOARD CREASE BEAM ANGLE CORRODED. MAJOR REPAIR ACCOMPLISHED. CREASE BEAM AND ANGLE RE PLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002061300025 20020613 00025 NM 2002 6 13 2002UALA00894 1 20020516 A 2150 MR21258 VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE E/E BAY FAILED A UALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 WP 29 656UA 25394 EQUIPMENT FAILURE ASSOCIATED WITH EQUIPMENT COOLING PROBLEM. INTERMITTENT HSI/ADI/TCAS/WX RADAR OCCURRED RIGHT AFTER TA KEOFF. SYSTEMS SOMEWHAT RESTORED ONCE FAN SELECTED TO OVERRIDE. REF INBD LOG1 FOR LOSS OF VARIOUS CRT'S W SOME A-P PRO BLEMS. AS PER LCL DIRECTIVE, EQUIP CLG OVERBOARD EXH VLV TO BE REPLACED. REF MM21-58-05-401 ACPD TO STEP 12. UNABLE T O REMOVE VLV DUE TO EXCESSIVE SEALANT. SPOILERS ARE NOT DEACTIVATED. CONT OF AMIS ITEM 4576002: FINISHED INSTALLATION AS REQUIRED PER MM 21-58-05. 2 L 7 2 4F 4 F RT A1NM E24NE 2002060300018 20020603 00018 NM 2002 6 3 2002UALA00895 1 20020516 A 2421 1701766 GENERATOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT ENGINE FAILED A UALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 224UA 30225 LEFT IDG AND BACKUP GENERATOR IS OFF OR HAS FAILED. RETURNED TO SEA. TWO EVENTS HAPPENED DURING FLIGHT. THE LEFT BACK UP GENERATOR SHEARED SHAFT MAINTENANCE MESSAGE THEN FOLLOWED BY SEVERAL LEFT INTEGRATED DRIVE GENERATOR (IDG) MAINTENANC E MESSAGES. THE LEFT IDG WAS MANUALLY DISCONNECTED. BOTH THE LEFT IDG AND BACKUP GENERATOR WERE REPLACED. REQUESTED B OEING AND HAMILTON SUNDSTRAND TO FOLLOW UP ON THIS OCCURRENCE WITH FINDING REPORTS OF BOTH UNITS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002060300019 20020603 00019 NM 2002 6 3 2002UALA00896 1 20020517 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 HOLE IN FUSELAGE FWD OF MID LAV SERVICE PANEL. HOLE IS LOCATED 2 INCHES ABOVE STRINGER 226 AT APPROX STA 691. HOLE MEA SURES .75 INCH IN DIAMETER. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002061200136 20020612 00136 NM 2002 6 12 2002UALA00897 1 20020516 A 2761 ACTUATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE SPOILER BROKEN A UALA K NONE K F FLUID LOSS FLT CONT AFFECTED IN INSP/MAINT 1 WP 29 307UA 23668 LEFT HAND WING NR 4 GROUND SPOILER ACTUATOR BROKEN. THE NUMBER 4 GROUND SPOILER HAD THE ROD END BREAK OFF IN THE THREAD S. IT APPEARS TO BE A FATIGUE FAILURE. REPLACE THE NUMBER 4 GROUND SPOILER ACTUATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300020 20020603 00020 NM 2002 6 3 2002UALA00898 1 20020518 A 3260 WARNING LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT ILLUMINATED A UALA K NONE J WARNING INDICATION LD LANDING 1 WP 29 917UA 25384 WHEN LANDING GEAR WAS SELECTED DOWN, RED NOSE GEAR LIGHT ILLUMINATED AND NO OTHER LIGHTS ILLUMINATED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300021 20020603 00021 NM 2002 6 3 2002UALA00899 1 20020517 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 937UA 26668 GALLEY DOOR CUTOUT FORWARD FRAME CRACKED JUST ABOVE CABIN FLOOR. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBL ER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300022 20020603 00022 NM 2002 6 3 2002UALA00900 1 20020519 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 938UA 26671 STATION 178 FORWARD BULKHEAD SKIN HAS EXCESSIVE MATERIAL LOSS. STATION 178 WL 239 RBL 12. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300023 20020603 00023 NM 2002 6 3 2002UALA00901 1 20020519 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 STATION 400 FRAME WEB CRACKED AT STRINGER 9R PASSENGER SERVICE UNIT SUPPORT ATTACH RIVET HOLE. MAJOR REPAIR ACCOMPLISHE D. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300024 20020603 00024 NM 2002 6 3 2002UALA00902 1 20020519 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 CABIN BODY FRAME WEB IS CRACKED AT BODY STATION 500A STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. SPLICED BODY FRAME WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300025 20020603 00025 NM 2002 6 3 2002UALA00903 1 20020519 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 CABIN BODY FRAME WEB IS CRACKED AT BODY STATION 480 STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. SPLICED BODY FRAME WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300026 20020603 00026 NM 2002 6 3 2002UALA00904 1 20020519 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 STATION 987 RBL 19 CABIN FLOORBEAM UPPER SURFACE IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002061200138 20020612 00138 NM 2002 6 12 2002UALA00906 1 20020520 A 2612 G718505 CONTROL PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAULTY A UALA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 WP 29 318UA 23950 CREW REPORTED GETTING A CARGO PANEL FIRE LIGHT WITH NO BELLS. MAINTENANCE FOUND FIRE DETECTION PANEL WOULD NOT TEST. R EPLACED CARGO COMPARTMENT PANEL. PERFORMED OPERATIONAL CHECK OF THE SYSTEM AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300027 20020603 00027 EU 2002 6 3 02147311 1 20020527 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 311UE 41029 During preflight inspection, the crew reported that the emergency floor track lights were inoperative. Maintenance pers onnel secured a loose connector for the emergency floor track lights. An operational check was satisfactory and the air craft was returned to service. 2 L 7 2 4T RT A41NM 2002060300028 20020603 00028 NM 2002 6 3 2002UALA00907 1 20020520 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 CABIN FLOOR SUPPORT UPPER SURFACE IS CORRODED BODY STATION 285 - 292, RBL 20 - 22, WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300029 20020603 00029 EU 2002 6 3 02146329 1 20020526 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 329UE 41097 During preflight inspection, the crew reported that the emergency floor track lights were inoperative. Maintenance pers onnel secured a loose connector for the emergency floor track lights. An operational check was satisfactory and the air craft was returned to service. 2 L 7 2 4T RT A41NM 2002060300030 20020603 00030 NM 2002 6 3 2002UALA00908 1 20020521 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 RIGHT HAND CABIN CREASE BEAM WEB UPPER SURFACE CORRODED BETWEEN STATION 1000 & 1020 WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002060300031 20020603 00031 NM 2002 6 3 2002UALA00909 1 20020521 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 AFT PIT STATION 747 FRAME INNER FLANGE IS DAMAGED AT STRINGER 19L. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER MANUFACTU RED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300032 20020603 00032 NM 2002 6 3 2002UALA00910 1 20020521 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 AFT PIT FRAME STATION 807 AT LBL 24 HAS DENT ON SURFACE. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER WAS MANUFACTURED AN D INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300033 20020603 00033 NM 2002 6 3 2002UALA00911 1 20020521 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 190UA 26879 EMERGENCY LIGHTS INOP AT SEAT 12 AB. SPLICED BROKEN WIRES IN SEAT EEL POWER CABLE. 2 L 7 4 4F 4 F RT A20WE E24NE 2002110400098 20021104 00098 NE 2002 11 4 2002UALA00913 2 20020521 A 7311 471111203600U COOLER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 780UA 19159 26944 777031 RIGHT ENGINE OIL TEMP INDICATION CLIMBING THROUGH FL290 AFTER DEPARTURE. CREW REDUCED POWER ON RIGHT ENGINE TO FLIGHT I DLE. REPLACED FUEL/OIL COOLER AND BYPASS VALVE ASSEMBLY. RAN ENGINE AT 1.25 EPR FOR 15 MINUTES. RT ENGINE OIL TEMP NO RMAL. FUEL/OIL COOLER HEAT EXCHANGER REVEALED NO DISCREPANCIES. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002060700132 20020607 00132 NM 2002 6 7 2002UALA00914 1 20020522 A 5754 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L/E SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 NR 4 LEADING EDGE SLAT LOWER SURFACE 6-8 INCHES OUTBOARD OF SLAT ACTUATOR SKIN IS CRACKED AT TWO FASTENERS. MAJOR REPAI R ACCOMPLISHED REINFORCEMENT DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060700134 20020607 00134 NM 2002 6 7 2002UALA00915 1 20020522 A 5754 SLAT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 LEFT HAND WING NR 2 SLAT HAS CRACK IN AFT ROW OF RIVETS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060700135 20020607 00135 NM 2002 6 7 2002UALA00916 1 20020523 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 AFT PIT FRAME STATION 827 LBL 22 - 26 HAS DENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060300034 20020603 00034 NM 2002 6 3 2002UALA00917 1 20020522 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 FORWARD EXTERNAL RIGHT HAND SIDE STATION 350 STR 25R JUST FWD AND ABOVE NLG SKIN HAS DENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002060300035 20020603 00035 WP 2002 6 3 ABXA010873 1 20020509 A 3230 39208025501 RETRACT CYLINDER DOUG DC9 DC933F 302207A WP LT MLG DEFECTIVE A ABXA K NONE K FLUID LOSS CR CRUISE 1 GL 23 931AX 7480 47384 SHORTLY AFTER TAKEOFF, RIGHT HYDRAULIC QUANTITY DROPPED TO 2 GALLONS. THE RIGHT HYDRAULIC PUMPS AND QUANTITY INCREASED TO 10 GALLONS DURING DESCENT. THE PUMPS WERE TURNED BACK ON AND THE QUANTITY ON THE RIGHT SIDE WENT TO ZERO. THE GEAR WAS EXTENDED MANUALLY. FOUND THE LEFT MAIN LANDING GEAR RETRACT CYLINDER LEAKING. REPLACED THE LEFT MAIN LANDING GEAR RETRACT CYLINDER IAW DC-9 MM 32-32-02-2-0004. 2 L 7 2 4F A6WE 2002060300036 20020603 00036 WP 2002 6 3 ABXA010874 1 20020511 A 3310 RHEOSTAT DOUG DC9 DC931 3022065 WP COCKPIT DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 937AX 47074 CAPTAIN'S MAP LIGHT SPARKED WHEN MOVED LENS BALL. REPLACED RHEOSTAT ON CAPTAIN'S MAP LIGHT IAW DC-9 MM 33-10-00. 2 L 7 2 4F A6WE 2002060300037 20020603 00037 NM 2002 6 3 ABXA010875 1 20020511 A 3350 BPS73 POWER SUPPLY BOEING 767 767281 1385109 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 774AX 22789 DURING MAINTENANCE INSPECTION, FOUND BOTH EMERGENCY LIGHTS INOPERATIVE. REPLACED PRIMARY EMERGENCY LIGHT POWER SUPPLY A ND TESTED IAW B767 MM 33-51-07. PRIMARY SUPPLY OPS CHECKED GOOD. LIGHTS ILLUMINATED. 2 L 7 2 4F RT A1NM 2002060300038 20020603 00038 NM 2002 6 3 ABXA010876 1 20020513 A 3350 20131A BATTERY PACK BOEING 767 767281 1385109 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 774AX 22789 DURING MAINTENANCE TEST OF EMERGENCY LIGHTING SYSTEM, FOUND STANDBY BATTERY INOPERATIVE. INSTALLED NEW BATTERY PACK IAW B767 MM 33-51-07-02. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2002060300039 20020603 00039 WP 2002 6 3 ABXA010880 1 20020516 A 2740 39208223 STOP FITTING DOUG DC9 DC915 3022036 WP HORIZ STAB SHEARED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX DCA383 45717 HORIZONTAL STABILIZER JACKSCREW, UPPER MECHANICAL STOP SHEARED OFF. REMOVED AND REPLACED THE JACKSCREW ASSEMBLY IAW DC- 9 MM. 2 L 7 2 4F A6WE 2002060300040 20020603 00040 WP 2002 6 3 ABXA010881 1 20020422 A 5543 5910257501 TRIM TAB DOUG DC9 DC932 3022066 WP RUDDER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 UPPER LEFT CORNER OF RUDDER TAB WAS DELAMINATED. REPLACED RUDDER TRIM TAB IAW DC-9 MM. 2 L 7 2 4F A6WE 2002060300041 20020603 00041 WP 2002 6 3 ABXA010882 1 20020422 A 5521 9918450503 SPAR DOUG DC9 DC932 3022066 WP ELEVATOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 X-RAY OF RIGHT ELEVATOR FORWARD SPAR INDICATED A 2 INCH CRACK ON SPAR AT STA XET 90. REPAIRED CRACK AT STA XET 90 IAW D C-9 SRM 55-02. 2 L 7 2 4F A6WE 2002060300042 20020603 00042 WP 2002 6 3 ABXA010883 1 20020423 A 2760 59242731 BRACKET DOUG DC9 DC932 3022066 WP RT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 LATERAL CONTROL MIXER, OUTBOARD SECTION, BRACKET CRACKED AT NUT PLATE ON THE BACK SIDE. REPLACED RIGHT LATERAL CONTROL MIXER IAW DC-9 MM 27-61-04-4-0007. 2 L 7 2 4F A6WE 2002060300043 20020603 00043 WP 2002 6 3 ABXA010885 1 20020503 A 2510 56441612 PANEL DOUG DC9 DC932 3022066 WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 RIGHT EYEBROW PANEL FORWARD LOWER CORNER JAMB CRACKED. JAMB ON UPPER AFT CORNER OF CLEARVIEW. REPAIRED CRACKS IAW DACO , SERVICE REWORK DRAWING 5952965. 2 L 7 2 4F A6WE 2002060300044 20020603 00044 WP 2002 6 3 ABXA010887 1 20020520 A 3260 LIGHT DOUG DC9 DC932 3022066 WP COCKPIT LOOSE A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 900AX 47380 WHEN LANDING GEAR EXTENDED, NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE RED INTRANSIT LIGHT WAS EXTINGUISHED ALONG WITH THE UNSAFE LIGHT. THE PROBLEM CORRECTED BY ITSELF. THE NOSE LANDING GEAR UNSAFE BULB WAS LOOSE IN THE SOCKET. REPLACED B ULB AND PERFORMED A GEAR SWING IAW DC-9 MM 32-60-00. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002060300045 20020603 00045 WP 2002 6 3 ABXA010888 1 20020528 A 3350 5708458503 BATTERY PACK DOUG DC8 DC863F 302198F WP CABIN DISCHARGED A ABXA K NONE O OTHER CR CRUISE 1 GL 23 816AX 46093 EMERGENCY LIGHTS WERE COMING ON INTERMITTENTLY. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC-8 MM. 2 L 7 4 4F 4A25 2002060300046 20020603 00046 WP 2002 6 3 ABXA010889 1 20020529 A 3350 5708458503 BATTERY PACK DOUG DC8 DC863F 302198F WP CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 224 46093 DURING MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT LIGHTS DIM. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK IAW DC-8 MM 33-50-01. 2 L 7 4 4F 4A25 2002060300047 20020603 00047 WP 2002 6 3 ABXA010890 1 20020524 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 975AX 47512 DURING MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW DC-9 AMM 33-5 3-02. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002060300048 20020603 00048 WP 2002 6 3 ABXA010893 1 20020513 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 EMPENNAGE INTERIOR LONGERON 17 RIGHT, END FITTING WAS CRACKED AT FS 1769. REPLACED END FITTING IAW DC-8 SRM 51-3-2 AND 51-1-20D. 2 L 7 4 4F 4A25 2002060300052 20020603 00052 WP 2002 6 3 ARWA20020506 1 20020521 A 2910 AE2460001J6030 HYDRAULIC LINE DOUG DC8 DC861 3021952 WP NR 2 ENGINE LEAKING A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 29UA 46159 AT 2225Z IN CLIMBING, HYDRAULIC QUANTITY DROPPED TO STAND PIPE PRESSURE DROPPED TO ZERO RETURNED TO KMIA. PERFORMED LOS S HYDRAULIC PRESSURE EMERGENCY CHECKLIST ON HYDRAULIC FLUID; PERFORMED EMERGENCY CHECKLIST ON HYDRAULIC CHECK, NO FURTHE R LOSS OF FLUID. USED ABNORMAL LANDING CHECKLIST. FOUND HYDRAULIC HOSE ASSY LEAKING AT NR 2 ENGINE; REMOVED AND REPLA CED NR 2 ENGINE HYDRAULIC PRESSURE HOSE ASSY AND REPLACED DRAIN CASE FILTER IAW MM 70-30-2 AND MM29-10-14; NO LEAKS NOTE D ON RUN-UP IAW MM 71-0 AND MM 29-00. OPS FOUND NORMAL AND SERVICED HYDRAULIC SYSTEM IAW MM 12-30-1. 2 L 7 4 4F 4A25 2002080500086 20020805 00086 WP 2002 8 5 ARWA20020507 1 20020507 A 5411 SPAR DOUG DC8 DC862 3021970 WP NR 4 PYLON CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 1804 45896 DURING C-CHECK, NR 4 PYLON INTERIOR, STA YN 165, RM UPPER CHORD WITH 4 INCH CRACK. REPAIRED UPPER SPAR CAP OF NR 4 PYLO N IAW AS ELEVEN INC DRAWING AS 11403, SHEET 1 TO 6. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR. 2 L 7 4 4F 4A25 2002060300053 20020603 00053 WP 2002 6 3 ARWA20020509 1 20020529 A 7120 37707451 MOUNT DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 46359 1061 45969 671003 DURING A-CHECK AT MIA THE FOLLOWING WAS FOUND, NR 4 ENGINE AFT MOUNT BROKEN. REPLACED FORWARD LT, FORWARD RT AND AFT EN GINE MOUNT ASSEMBLY IAW MM 71-20-2. AFT MOUNT SENT OUT FOR ANALYSIS. 2 L 7 4 4F 4 F 4A25 1E8 2002060300054 20020603 00054 WP 2002 6 3 AT0200060 1 20020430 A 5320 S26524791200 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 847AT 47555 FWD CABIN LEFT HAND SUBFLOOR, LONGITUDINAL FLOOR SUPPORT FROM BS 160 TO BS 200, LBL 40 IS HEAVILY CORRODED. INSTALLED N EW FLOOR SUPPORT FROM STA 160 TO STA 200 LBL 40 AS PER DC-9 SRM 51-30-0. 2 L 7 2 4F A6WE 2002060300055 20020603 00055 WP 2002 6 3 AT0200061 1 20020430 A 5320 S26524791200 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 847AT 47555 FWD CABIN, RIGHT HAND SUBFLOOR, LONGITUDINAL FLOOR SUPPORT FROM BS 160 TO BS 200, RBL 40 IS HEAVILY CORRODED. INSTALLED NEW FLOOR SUPPORT AT FWD CABIN RIGHT HAND SUBFLOOR BS 160 TO BS 200, RBL 40 IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002060300056 20020603 00056 WP 2002 6 3 AT0200062 1 20020502 A 5320 STRAP DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 847AT 47555 R1 SERVICE DOOR LOWER AFT THRESHOLD INNER STRAP CORRODED. REPAIRED THRESHOLD INNER STRAP IAW SRM 53-01 AND RES 02-0357. 2 L 7 2 4F A6WE 2002060300057 20020603 00057 WP 2002 6 3 AT0200063 1 20020428 A 5315 S2912758 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 847AT 47555 AFT CARGO COMPARTMENT OVERHEAD FLOORBEAM HAS CORROSION INDICATION AND BLUE WATER STAINS AT APPROX BS 965 ABOVE PULLEYS. INSTALLED NEW ANGLE AT FLOORBEAM BS 965 FROM RBL 5 TO RBL 55. 2 L 7 2 4F A6WE 2002060300058 20020603 00058 NM 2002 6 3 AWXA200200429 1 20020516 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 189AW 22656 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. MAIN TENANCE REMOVED AND REPLACED THE BATTERY PACKS AT THE L1 AND R1 DOORS, AND THE BATTERY PACK AT THE FWD DROP CEILING, OPE RATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002060300059 20020603 00059 2002 6 3 AWXA200200431 4 20020517 A 3431 6223257001 RECEIVER BOEING 737 7373G7 1384595 NM VOR/ILS SYSTEM DEFECTIVE A AWXA K NONE J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 28 160AW 20182 23782 LAX - BURNING SMELL - FLT 0102 - ON DESCENT INTO LAX INBOUND FROM LAS FLIGHT MANAGEMENT COMPUTER (FMC) FAIL MESSAGE APPE ARED ON THE FMC. SHORTLY AFTER THAT A SLIGHT BURNING ELECTRICAL SMELL WAS NOTICED, NAV INSTRUMENTS IN MANUAL ALSO FAILE D. BURNING SMELL WAS INTERMITTENT GOING AWAY AND COMING BACK APPROXIMATELY EVERY 3 SECONDS. MAINTENANCE PERFORMED A BI TE TEST ON FMC SYSTEM AND FOUND THE VOR /ILS NR 2 NAV RECEIVER FAULTING. REPLACED THE NR 2 NAV RECEIVER, BITE CHECK WAS GOOD, NO FAULTS OR BURNING SMELL NOTED. 2 L 7 2 4F RT A16WE 2002060300060 20020603 00060 EU 2002 6 3 AWXA200200433 1 20020517 A 5270 ABS012110 PROXIMITY SENSOR AIRBUS 320 A320231 3930325 EU CARGO DOOR MALFUNCTIONED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 634AW 091 PHX - AIR TURNBACK - FLT 0807 - AFTER TAKEOFF FROM PHX EN ROUTE TO SFO PASSING APPROXIMATELY 500 AGL THE FWD CARGO DOOR UNLOCK WARNING CAME ON. AIRCRAFT TURNED BACK TO PHX AND ON DOWNWIND RETURN FOR LANDING THE WARNING LIGHT WENT OUT. MAI NTENANCE REPLACED THE THE FWD CARGO DOOR PROXIMITY SWITCH, SWITCH WAS ADJUSTED TO CORRECT TOLERANCE IAW AMM 52-71-12-401 , AND OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002061000066 20020610 00066 NM 2002 6 10 AWXA200200435 1 20020519 A 2930 350E5151331 COMPUTER AIRBUS A319 A319132 3930340 NM HYD SYSTEM MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 802AW 37964 3618 924 IN CRUISE FLIGHT AT FL390 ECAM SHOWED YELLOW HYD RESERVOIR OVERHEAT FOLLOWED BY ECAM ACTION OVERHEAT ON LOWER DISPLAY UN IT, INDICATION FLASHED ON AND OFF THEN WENT AWAY, DIVERTED TO MCI. MX RECALLED EVENT THAT INDICATED YELLOW ELECTRIC HY D PUMP CAUSED RESERVOIR OVERHEAT. REMOVED AND REPLACED YELLOW ELECTRIC HYD PUMP. CHECK VALVE, LEAK CHECK WAS GOOD. AF TER REVIEWING HISTORY OF RECENT RESERVOIR OVERHEAT PROBLEMS NR 1 SYS DATA ACQUISITION CONCENTRATOR (SDAC) WAS IDENTIFIED AS A SUSPECT PART AND REPLACED. OPERATIONAL CHECK OF YELLOW HYD SYS GOOD. VENDOR BENCH TEST OF SDAC CONFIRMED FAILURE . UNIT FAILED ANALOG TEST DUE TO DEFECTIVE SRU. UNIT RETURNED TO SERVICE BY REPLACING THE DEFECTIVE ANALOG SRU. 2 L 7 2 4F RT A28NM 2002060300061 20020603 00061 NM 2002 6 3 AWXA200200436 1 20020515 A 5315 6567140127 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 YVR - MAJOR REPAIR - DURING INSPECTION A .375 INCH CRACK WAS FOUND ON LONGITUDINAL FLOORBEAM BS 675, LBL 24.75 AT THE AI LERON QUADRANT CUTOUT. MAINTENANCE REMOVED ANGLE AND PREVIOUS REPAIR PARTS, TRIMMED TAB ON CHORD AT BS 675, LBL 24.75, FABRICATED A NEW CHANNEL AND 3 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW AWA ER 15-5715-02145-KB1. 2 L 7 2 4F RT A16WE 2002060300062 20020603 00062 NM 2002 6 3 AWXA200200440 1 20020508 A 5315 6545410200 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 CHECK A CRACK WAS FOUND AT FASTENER HOLE ON UPPER CHORD FLANGE AT BS 727B-1, RBL 44. M AINTENANCE REMOVED DAMAGED SECTION. FABRICATED A FILLER, REPAIR STRAPS, AND A SHIM. INSTALLED REPAIR PARTS IAW AWA ER 03-5310-02141-KB2A. 2 L 7 2 4F RT A16WE 2002060300063 20020603 00063 NM 2002 6 3 AWXA200200444 1 20020522 A 3350 100865 POWER SUPPLY BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 LAS - EEL - WHEN THE AIRCRAFT WAS PLACED ON GROUND SERVICE BUS THE EMERGENCY EXIT LIGHTING NO ARMED AMBER LIGHT ILLUMINA TED ON THE OVERHEAD PANEL. MAINTENANCE REMOVED AND REPLACED FWD EMERGENCY BATTERY POWER SUPPLY IAW BMM 33-51-51 PG 206, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002060300064 20020603 00064 NM 2002 6 3 AWXA200200445 1 20020523 A 3350 20121 CHARGER BOEING 757 7572S7 1384962 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 904AW 23566 PHX - EEL - DURING INSPECTION THE R-3 DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. RELAMPED 3 TIMES, NO HE LP. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY FOR THE R-3 DOOR, OPERATIONAL CHECK WAS GOOD IAW BMM 33-51-00, PG 501. 2 L 7 2 4F RT A2NM 2002060300065 20020603 00065 NM 2002 6 3 AWXA200200448 1 20020523 A 5311 6546541504 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 INSPECTION A CRACK WAS FOUND ON FRAME BS 663.75 AT CUTOUT FOR STR 2 RT. MAINTENANCE CU T OUT DAMAGED AREA. FABRICATED FRAME REPAIR ANGLE, AND A FILLER. INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07 FIG 209, SHT 1-4, PG 225-228. 2 L 7 2 4F RT A16WE 2002060300066 20020603 00066 NM 2002 6 3 AWXA200200449 1 20020523 A 5311 6546541504 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 INSPECTION, A CRACK WAS FOUND ON FRAME BS 663.75 AT CUTOUT FOR STR 3 RT. MAINTENANCE C UT OUT DAMAGED AREA OF FRAME. FABRICATED FRAME REPAIR ANGLE, AND A FILLER. INSTALLED REPAIR PARTS IAW B737-300 SRM 53- 00-07, FIG 209, SHT 1-4, PG 225-228. 2 L 7 2 4F RT A16WE 2002060300067 20020603 00067 NM 2002 6 3 AWXA200200450 1 20020523 A 5320 65235745 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 INSPECTION A CRACK WAS FOUND ON STRINGER CLIP BS 706, STR 10 RT. MAINTENANCE REMOVED S TRINGER CLIP; FABRICATED A NEW STRINGER CLIP AND INSTALLED PART IAW BOEING DWG 66-23574, B737-300 SRM 51-10-02, PG 15-16 , AND SRM 51-40-02, PG 10-11. 2 L 7 2 4F RT A16WE 2002060300068 20020603 00068 NM 2002 6 3 AWXA200200451 1 20020523 A 5320 693535214 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 INSPECTION A CRACK WAS FOUND ON STRINGER CLIP BS 616, STR 5 RT. MAINTENANCE REMOVED ST RINGER CLIP AT BS 616, STR 5 RT; FABRICATED A NEW STRINGER CLIP AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 3, 4, & 38, AND SRM 51-40-05, PG 4. 2 L 7 2 4F RT A16WE 2002060300069 20020603 00069 NM 2002 6 3 AWXA200200452 1 20020523 A 5320 69353521 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 INSPECTION A CRACK WAS FOUND ON STRINGER CLIP BS 706, STR 3 RT. MAINTENANCE REMOVED ST RINGER CLIP AT BS 706, STR 3 RT; FABRICATED A NEW STRINGER CLIP, TREATED, AND INSTALLED REPAIR PART IAW B737-300 SRM 51- 40-02, PG 3, 4, 10, 11, & 38. 2 L 7 2 4F RT A16WE 2002060300070 20020603 00070 NM 2002 6 3 AWXA200200453 1 20020523 A 5320 69353521 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 INSPECTION A CRACK WAS FOUND ON STRINGER CLIP BS 639, STR 9 LT. MAINTENANCE REMOVED ST RINGER CLIP AT BS 639, STR 9 LT; FABRICATED A NEW STRINGER CLIP, TREATED, AND INSTALLED REPAIR PART IAW B737-300 SRM 51- 40-02, PG 3, 4, 10, 11 & 38. 2 L 7 2 4F RT A16WE 2002060300071 20020603 00071 NM 2002 6 3 AWXA200200454 1 20020523 A 5320 693535214 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 INSPECTION A CRACK WAS FOUND ON STRINGER CLIP BS 639, STR 2 RT. MAINTENANCE REMOVED ST RINGER CLIP AT BS 639, STR 2 RT; FABRICATED A NEW STRINGER CLIP, TREATED, AND INSTALLED REPAIR PART IAW B737-300 SRM 51- 40-02, PG 10 & 11. 2 L 7 2 4F RT A16WE 2002060300072 20020603 00072 NM 2002 6 3 AWXA200200455 1 20020523 A 5320 65353521 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 INSPECTION, A CRACK WAS FOUND ON STRINGER CLIP BS 597, STR 9 RT. MAINTENANCE REMOVED S TRINGER CLIP AT BS 597, STR 9 RT; FABRICATED A NEW STRINGER CLIP, TREATED, AND INSTALLED REPAIR PART IAW B737-300 SRM 51 -40-02, PG 3, 4, 10, 11 & 38. 2 L 7 2 4F RT A16WE 2002060300073 20020603 00073 NM 2002 6 3 AWXA200200456 1 20020523 A 5320 693535214 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 INSPECTION, A CRACK WAS FOUND ON STRINGER CLIP BS 639, STR 2 LT. MAINTENANCE REMOVED S TRINGER CLIP AT BS 639, STR 2 LT; FABRICATED A NEW STRINGER CLIP, TREATED, AND INSTALLED REPAIR PART IAW B737-300 SRM 51 -40-02, PG 3, 10 & 38. 2 L 7 2 4F RT A16WE 2002060300074 20020603 00074 NM 2002 6 3 AWXA200200457 1 20020523 A 5320 69353521 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 INSPECTION, A CRACK WAS FOUND ON STRINGER CLIP BS 663, STR 11 LT. MAINTENANCE REMOVED STRINGER CLIP AT BS 663, STR 11 LT; FABRICATED A NEW STRINGER CLIP, TREATED, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 3, 10 & 38. 2 L 7 2 4F RT A16WE 2002060300075 20020603 00075 NM 2002 6 3 AWXA200200458 1 20020523 A 5311 65465373 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 INSPECTION A CRACK WAS FOUND AT UPPER FASTENER HOLE ON FRAME FOOT BS 578, BELOW STR 13 LT. MAINTENANCE CUT OUT CRACKED AREA OF FRAME FOOT SHEAR TIE AT BS 578, STR 13 LT; FABRICATED REPAIR ANGLE, RADIUS FILL ER, AND A DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, PG 213-215. 2 L 7 2 4F RT A16WE 2002060300076 20020603 00076 NM 2002 6 3 AWXA200200460 1 20020507 A 5320 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 YVR - MAJOR REPAIR - DURING C-16 INSPECTION A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727D, STR 10 RT. MAINTENANCE R EMOVED STRINGER TIE CLIP AT BS 727D, STR 10 RT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737- 300 SRM 51-10-02, PG 12, AND DWG 69-35352-14. 2 L 7 2 4F RT A16WE 2002060300077 20020603 00077 NM 2002 6 3 AWXA200200461 1 20020507 A 5320 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 YVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 867, STR 14 RT. MAINTENANCE R EMOVED STRINGER TIE CLIP AT BS 867, STR 14 RT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737-3 00 SRM 51-10-02, PG 12 AND DWG 69-35352-14. 2 L 7 2 4F RT A16WE 2002060300078 20020603 00078 NM 2002 6 3 AWXA200200462 1 20020508 A 5320 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 YVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 639, STR 4 RT. MAINTENANCE RE MOVED STRINGER TIE CLIP AT BS 639, STR 4 RT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG 12 AND DWG 69-35352-14. 2 L 7 2 4F RT A16WE 2002060300079 20020603 00079 NM 2002 6 3 AWXA200200463 1 20020508 A 5320 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 YVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 639, STR 2 RT. MAINTENANCE RE MOVED STRINGER TIE CLIP AT BS 639, STR 2 RT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG 12 AND DWG 69-35352-14. 2 L 7 2 4F RT A16WE 2002060300080 20020603 00080 NM 2002 6 3 AWXA200200464 1 20020508 A 5320 69414372 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 YVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 663, STR 10 LT. MAINTENANCE R EMOVED STRINGER TIE CLIP AT BS 663, STR 10 LT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737-3 00 SRM 51-10-02, PG 12 AND DWG 69-41437-2. 2 L 7 2 4F RT A16WE 2002060300081 20020603 00081 NM 2002 6 3 AWXA200200465 1 20020507 A 5320 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 YVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 767, STR 10 RT. MAINTENANCE R EMOVED STRINGER TIE CLIP AT BS 767, STR 10 RT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737-3 00 SRM 51-10-02, PG 12 AND DWG 69-35352-14. 2 L 7 2 4F RT A16WE 2002060300082 20020603 00082 NM 2002 6 3 AWXA200200466 1 20020508 A 5320 69414372 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 YVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 663, STR 10 RT. MAINTENANCE R EMOVED STRINGER TIE CLIP AT BS 663, STR 10 RT. FABRICATED A NEW STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW B737-3 00 SRM 51-10-02, PG 12 AND DWG 69-41437-2. 2 L 7 2 4F RT A16WE 2002060300083 20020603 00083 NM 2002 6 3 AWXA200200467 1 20020508 A 5320 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 YVR - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON 2 EACH STRINGER TIE CLIPS AT BS 380, STR 1 & 2 RT. MA INTENANCE REMOVED STRINGER TIE CLIPS AT BS 380, STR 1 & 2 RT. FABRICATED A NEW STRINGER TIE CLIPS, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-10-02, PG 12 AND DWG 69-35352-14. 2 L 7 2 4F RT A16WE 2002060300084 20020603 00084 NM 2002 6 3 AWXA200200468 1 20020510 A 5315 654581094 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 YVR - MAJOR REPAIR - DURING C-16 INSPECTION, CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOORBEAM AT BS 312, BL 0, RBL 8, AND RBL 11. MAINTENANCE CUT OUT DAMAGED AREA OF FLOORBEAM T-CHORD AT BS 312, BL 0, RBL 8, AND RBL 11; FABRICATED REP AIR ANGLES, AND STIFFENER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205. 2 L 7 2 4F RT A16WE 2002060300085 20020603 00085 NM 2002 6 3 AWXA200200470 1 20020508 A 5311 6546526 BELTFRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 YVR - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON METAL ANGLE ATTACHED TO FUSELAGE WEB BETWEEN STR 13 & 14 RT, BS 400. MAINTENANCE CUT OUT CRACKED PORTION OF FRAME AT BS 400, BETWEEN STR 13 & 14; FABRICATED REPAIR ANGLE, AND INST ALLED REPAIR IAW B737-300 SRM 53-00-07, FIG 207 PG 219. 2 L 7 2 4F RT A16WE 2002060300086 20020603 00086 NM 2002 6 3 C1HA200281005 1 20020519 A 7830 SWITCH BOEING 727 7272S7 138407Z NM THRUST REVERSER LACK OF LUBE A C1HA K NONE N FALSE WARNING CR CRUISE 1 GL 15 681CA 22020 NR 3 REVERSER OPERATING LIGHT ILLUMINATED AT FL 330 AND NORMAL THRUST SETTING. PERFORMED COM PROCEDURE, LIGHT REMAINED ILLUMINATED. PERFORMED VISUAL INSPECTION OF TR ACTUATOR SWITCH AND CONNECTIONS. INSPECTED ACTUATOR AND TR BUCKETS FOR LOOSENESS. OPERATED ENGINE AND VERIFIED PROPER LIGHT FUNCTION. CLEANED AND LUBRICATED MOVING PARTS OF LIGHT SWITCH. 2 L 7 3 4F A3WE 2002060300087 20020603 00087 NM 2002 6 3 C1HA200283002 1 20020427 A 5310 SHEAR TIE BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 SHEAR TIE ON FRAME 950D BETWEEN STR 29L-28L HAS CORROSION. 2 L 7 3 4F A3WE 2002060300088 20020603 00088 NM 2002 6 3 C1HA200283003 1 20020427 A 5311 FRAME BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 SUB FRAME AT STA 985 STR 30- STR 27R HAS CORROSION. 2 L 7 3 4F A3WE 2002060300089 20020603 00089 NM 2002 6 3 C1HA200283009 1 20020425 A 5347 SEAT TRACK BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 SEAT TRACK RBL 45 IS CORRODED AT STA 448-453. 2 L 7 3 4F A3WE 2002060300090 20020603 00090 WP 2002 6 3 IXXA0200028O 1 20020601 A 2121 FAN DOUG DC8 DC862 3021970 WP FWD BELLY DEFECTIVE A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 31CX 74718 1393 45911 ENROUTE FROM KWI TO AVB, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT WHEN BOTH RECIRCULATION FANS WERE OPERATING. THE FLIGHT CREW SECURED THE FANS AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPE CTED THE AIRCRAFT AND FOUND THE FANS TO BE DEFECTIVE. THE FANS WERE PLACED ON DEFERRAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002060300091 20020603 00091 EA 2002 6 3 COMA0260338 1 20020603 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 971CA 13711 7145 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 550CB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002060300092 20020603 00092 EA 2002 6 3 COMA0260339 1 20020603 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 971CA 13711 7145 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 640EB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002060300093 20020603 00093 EA 2002 6 3 COMA0260340 1 20020603 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 971CA 13711 7145 CRACK FOUND ON RT LOWER WING PLANK AT PANEL 650AB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002060300094 20020603 00094 EA 2002 6 3 COMA0260341 1 20020603 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 971CA 13711 7145 CRACK FOUND ON LT LOWER WING PLANK AT PANEL 540CB.REPAIRED I/A/W 601R-57-21-030. 2 L 7 2 4F RT A21EA 2002060300095 20020603 00095 EA 2002 6 3 COMA0260343 1 20020530 A 4910 APU CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 712CA 7244 FLIGHT 5275 SMOKE IN CABIN AND COCKPIT WHEN BLEEDS SOURCE SELECTED TO APU.PLACED APU ON DEFERRED MAINT LIST PER MEL. 2 L 7 2 4F RT A21EA 2002060300096 20020603 00096 NE 2002 6 3 COMA0260344 2 20020530 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE R/H FAILED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 SO 01 713CA 19247 5469 7245 807022 FLIGHT 5376 R/H ENGINE OIL PRESSURE WARNING - FAILED BY ENGINE FAILURE.REPLACED R/H ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002060300097 20020603 00097 EA 2002 6 3 COMA0260345 1 20020527 A 2740 83963 TRIM MOTOR CNDAIR CL600 CL6002B19 1900309 EA VERT STAB MALFUNCTIONED A COMA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 01 929CA 7084 7035 FLIGHT 5433 TRIM CAUTION MESSAGE - TRIM STUCK AT 2.8REPLACED THE HORZ STAB TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 2002060300098 20020603 00098 EA 2002 6 3 COMA0260346 1 20020530 A 2750 853D10012 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA R/H #3 INOPERATIVE A COMA O OTHER J O WARNING INDICATION OTHER DE DESCENT 1 SO 01 973CA 13636 7146 FLIGHT 5695 FLAPS FAIL MESSAGE WHEN SELECTED 20 DEGREES. POST FLIGHT INSP FOUND R/H OUTBD FLAP TWISTED.REPLACED FAILED R /H #3 FLAP ACTUATOR AND ALL RELATED DAMAGED COMPONENTS PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002060500232 20020605 00232 EU 2002 6 5 02FDEA00372 1 20020601 A 7830 THRUST REVERSER AIRBUS 310 A310 EU NR 1 ENGINE UNLOCKED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 414FE 400 PDIS- AFTER TAKEOFF FROM TULSA HAD IND OF NR 1 REVERSER UNLOCKED, UPON SLAT RETRACTION HAD YAW COMMENSURATE WITH UNLOCKE D REVERSER. R/R LT THRUST REVERSER CDU SWITCH. 2 L 7 2 4F RT A35EU 2002060400037 20020604 00037 NM 2002 6 4 C1HA200283004 1 20020428 A 5320 FITTING BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 NLG DOOR LINKAGE FITTING AT STA 227.8 LBL 10 WL 183 HAS CORROSION ON UPPER FLANGE. 2 L 7 3 4F A3WE 2002060400038 20020604 00038 NM 2002 6 4 C1HA200283005 1 20020430 A 5320 ANGLE BOEING 727 7272S7 138407Z NM FUSELAGE CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 VERTICAL ANGLE IN FWD RT CORNER OF RT WHEEL WELL IS CRACKED, NDT HAS VERIFIED. 2 L 7 3 4F A3WE 2002060400039 20020604 00039 NM 2002 6 4 C1HA200283006 1 20020501 A 5313 STRINGER BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 STR 27L IS CORRODED OUT OF LIMITS ON BOTTOM SIDE BETWEEN STA 950F AND 970. 2 L 7 3 4F A3WE 2002060400041 20020604 00041 NM 2002 6 4 C1HA200283007 1 20020501 A 5311 FRAME BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 T-CHORD FROM STA 950 STR 26 TO 29R IS CORRODED OUT OF LIMITS. 2 L 7 3 4F A3WE 2002060400042 20020604 00042 NM 2002 6 4 C1HA200283008 1 20020424 A 5315 FLOORBEAM BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 FLOORBEAM STA 1130 IS CORRODED ON TOP SIDE OF UPPER FLANGE AT 2 EA FASTENER LOCATIONS LBL 44 & LBL 25. 2 L 7 3 4F A3WE 2002060400043 20020604 00043 NM 2002 6 4 C1HA200283010 1 20020425 A 5347 SEAT TRACK BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 SEAT TRACK RBL 45 IS CORRODED AT STA 380-400. 2 L 7 3 4F A3WE 2002060400044 20020604 00044 NM 2002 6 4 C1HA200283011 1 20020425 A 5315 FLOORBEAM BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 FLOORBEAM IS CORRODED AT STA 380 RBL 55. 2 L 7 3 4F A3WE 2002060400045 20020604 00045 NM 2002 6 4 C1HA200283012 1 20020425 A 5347 SEAT TRACK BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 SEAT TRACK LBL 45 IS CORRODED STA 344-380. 2 L 7 3 4F A3WE 2002060400046 20020604 00046 NM 2002 6 4 C1HA200283013 1 20020425 A 5347 SEAT TRACK BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 SEAT TRACK RBL 24 IS CORRODED AT STA 1100. 2 L 7 3 4F A3WE 2002060400047 20020604 00047 NM 2002 6 4 C1HA200283014 1 20020425 A 5347 SEAT TRACK BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 SEAT TRACK RBL 45 IS CORRODED AT STA 1100. 2 L 7 3 4F A3WE 2002060400048 20020604 00048 NM 2002 6 4 C1HA200283015 1 20020425 A 5347 SEAT TRACK BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 SEAT TRACK LBL 45 IS CORRODED AT STA 1093. 2 L 7 3 4F A3WE 2002060400049 20020604 00049 NM 2002 6 4 C1HA200283016 1 20020427 A 5320 WEB BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 CENTER FLOOR WEB 1148-1183 RBL 16 HAS CORROSION. 2 L 7 3 4F A3WE 2002060400051 20020604 00051 NM 2002 6 4 C1HA200283017 1 20020501 A 5753 ATTACH FITTING BOEING 727 7272S7 138407Z NM T/E FLAP CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 LT WING NR 4 FLAP TRACK FWD ATTACH FITTING IS CORRODED AND GOUGED. 2 L 7 3 4F A3WE 2002060400052 20020604 00052 NM 2002 6 4 C1HA200283018 1 20020427 A 5313 STRINGER BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 STR 29L O/B AT STA 1005 CORRODED. 2 L 7 3 4F A3WE 2002060400053 20020604 00053 NM 2002 6 4 C1HA200284001 1 20020520 A 3241 39353 CONTROL VALVE BOEING 727 7272S7 138407Z NM ANTI SKID SYS MALFUNCTIONED A C1HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 684CA 22491 MAIN GEAR ANTI-SKID OUTBOARD ANNUNCIATOR CAME ON AFTER TAKEOFF - INTERMITTENT. RETURNED BACK TO MSP. REMOVED AND REPLA CED LT O/B ANTI-SKID CONTROL VALVE IAW MM. OPS CHECKS NORMAL. 2 L 7 3 4F A3WE 2002060400054 20020604 00054 NM 2002 6 4 C1HA200286001 1 20020518 A 3350 BATTERY BOEING 727 7272S7 138407Z NM CABIN LOOSE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 686CA 22021 EMERGENCY EXIT LIGHT ON LEFT OVERWING INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT BATTERY. OPS CHECKS GOOD IAW MM. 2 L 7 3 4F A3WE 2002060400055 20020604 00055 NM 2002 6 4 C1HA200286002 1 20020524 A 3350 CHARGER BOEING 727 7272S7 138407Z NM CABIN INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 686CA 22021 LEFT OVERWING EXIT SIGNS INOP. FOUND BATTERY CHARGER AND BATTERY CARTRIDGE FAULTY AT OVERWING CEILING PANEL STA 840. R EMOVED AND REPLACED BATTERY CARTRIDGE AND BATTERY CHARGER IAW 727 MM 33-50-22, OPS CK NORMAL. 2 L 7 3 4F A3WE 2002060400056 20020604 00056 SO 2002 6 4 C2XA02CL116 1 20020528 A 3230 355022002MOD2 CONTROL UNIT EMB 135 EMB135ER 3260203 SO COCKPIT MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 27506 3062 145206 CLE FLIGHT 3309 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM CLEVELAND. THE AIRCRAFT RETURNE D AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002060400057 20020604 00057 SO 2002 6 4 C2XA02CL117 1 20020515 A 2530 CBC16707 RECEPTACLE EMB 135 EMB135LR 3260305 SO GALLEY BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 17524 145399 CLE FLIGHT 3178 THE CREW REPORTED BURNING SMELL FROM THE HOT JUG IN THE GALLEY. MAINTENANCE INSPECTED AND REPLACED THE HOT JUG RECEPTACLE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002060400058 20020604 00058 SO 2002 6 4 C2XA02CL118 1 20020527 A 5610 163500110 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT CRACKED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 15985 5429 145248 CLE FLIGHT 3201 THE CREW REPORTED THE FIRST OFFICER'S WINDSHIELD HAD SHATTERED ON CLIMBOUT. THE AIRCRAFT RETURNED TO CL EVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE OUTER GLASS PLY HAD SHATTERED. THE WI NDSHIELD WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002060400062 20020604 00062 WP 2002 6 4 AALA20020318 1 20020316 A 2150 1941101 HEAT EXCHANGER DOUG DC9 DC983 3022083 WP A/C BAY MALFUNCTIONED A AALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 594AA 53284 DFW - FLT 1645 - IMMEDIATELY AFTER TAKEOFF DFW EN ROUTE PDX, BLUISH GRAY SMOKE APPEARED IN COCKPIT AND CABIN WITH A BURN ED RUBBER SMELL. GALLEY POWER ANF RECIRCULATION FAN TURNED OFF. APPROXIMATELY 5 MINUTES LATER SMOKE SEEMED TO THIN. N O LOSS OF ENGINE OIL OR HYDRAULIC FLUID NOTED. ALL ELECTRICAL INDICATIONS NORMAL. RETURNED AND LANDED DFW WITHOUT INCI DENT. INCIDENT UNDER INVESTIGATION. REPLACED RIGHT PRIMARY AND SECONDARY HEAT EXCHANGER, ALSO RIGHT ACM. ACCOMPLISHED PACK BURN AND ACCOMPLISHED OVERWEIGHT INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002060400069 20020604 00069 WP 2002 6 4 AALA20020433 1 20020404 A 3010 SEAL DOUG DC9 DC982 3022082 WP ANTI-ICE SYS MISSING A AALA I A CABIN DEPRESSURIZATION UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 248AA 49259 AMA- FLT 717 - EN ROUTE DFW-OAK, AT 31,000 FEET FLIGHT ATTENDANTS REPORTED FUMES AND SMOKE IN REAR OF AIRCRAFT. PASSENG ER IN SEAT 24B REPORTED TO FLIGHT ATTENDANT THAT FLOOR WAS HOT AND GETTING HOTTER. AIR CONDITION SMOKE/FUMES CHECKLIST ACCOMPLISHED. CABIN SMOKE FUMES CHECKLIST ACCOMPLISHED. FLIGHT ATTENDANTS STILL REPORTED STRONG FUMES. AIRCRAFT AS DE PRESSURIZED AT 4.000 FEET. DIVERTED AND LANDED AMA WITHOUT INCIDENT. AIRCRAFT INSPECTED AND FOUND TO BE IN CONDITION F OR SAFE FLIGHT FROM AMA TO DFW FOR REPAIR OF WING ANTI-ICE DUCT. REPLACED DEFECTIVE AND MISSING SEALS IN WING ANTI-ICE DUCTING FORWARD LEFT SIDEWALL AREA OF AFT CARGO. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002060400071 20020604 00071 NM 2002 6 4 ASAA0210081 1 20020412 A 5241 6545871 SKIN BOEING 737 737290C 138448V NM GALLEY DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PAE - DURING SCHEDULED C-CHECK, FOUND FORWARD GALLEY DOOR SKIN DENTED. REPAIRED DENT PER SRM. (M) 2 L 7 2 4F A16WE 2002060400073 20020604 00073 NM 2002 6 4 ASAA0210084 1 20020421 A 3350 883200312 RECEIVER BOEING 737 737298C 1384490 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING SCHEDULED MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT SEAT PALLET 9-11 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002060400074 20020604 00074 NM 2002 6 4 ASAA0210085 1 20020423 A 5210 6529994 GUIDE BOEING 737 737210C 1384459 NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OME - AFTER BOARDING, L1 DOOR DIFFICULT TO CLOSE. ADJUSTED L1 DOOR GUIDE ARM, THEN OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002060400075 20020604 00075 NM 2002 6 4 ASAA0210086 1 20020502 A 5210 6529994 GUIDE BOEING 737 737290C 138448V NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 ANC - FLIGHT CREW REPORTED L1 DOOR HARD TO OPERATE INTO CLOSED POSITION. ADJUSTED, CLEANED AND LUBED UPPER GUIDE ARM, T HEN OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 2002060400076 20020604 00076 NM 2002 6 4 ASAA0210087 1 20020503 A 5320 69353521 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BODY STATION 987, STRINGER 27 CORRODED. REMOVED AND REPLACED STR INGER CLIP PER SRM. (M) 2 L 7 2 4F A16WE 2002060400078 20020604 00078 NM 2002 6 4 ASAA0210088 1 20020504 A 5310 6546548 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 747, LEFT BUTTOCK LINE 8 CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. (M) 2 L 7 2 4F A16WE 2002060400080 20020604 00080 NM 2002 6 4 ASAA0210089 1 20020505 A 5311 65622062 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 420, STRINGER 22L-25L DENTED. REPAIRED DENT PER SRM. (M) 2 L 7 2 4F A16WE 2002060400082 20020604 00082 NM 2002 6 4 ASAA0210090 1 20020506 A 5330 6573742 SKIN PANEL BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 1046-1048, STRINGER 22R DENTED. REPAIRED DENT PER SRM. (M) 2 L 7 2 4F A16WE 2002060400084 20020604 00084 NM 2002 6 4 ASAA0210091 1 20020506 A 5311 65C34355 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 480, STRINGER 21L DENTED. REPAIRED DENT PER SRM. (M) 2 L 7 2 4F A16WE 2002060400086 20020604 00086 NM 2002 6 4 ASAA0210092 1 20020508 A 5310 6546555 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BODY STATION 867, RIGHT BUTTOCK LINE 7 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002060400088 20020604 00088 NM 2002 6 4 ASAA0210093 1 20020508 A 5311 6546557 FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 887, STRINGER 19L-26L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002060400094 20020604 00094 NM 2002 6 4 ASAA0240044 1 20020418 A 5230 65498893 SKIN BOEING 737 7374Q8 138447Q NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PAE - DURING CHECK FOUND, NUMEROUS DENTS IN FORWARD CARGO DOOR OUTER SKIN. REMOVED AND REPLACED SKIN IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060400095 20020604 00095 NM 2002 6 4 ASAA0240045 1 20020418 A 5230 65498893 SKIN BOEING 737 7374Q8 138447Q NM CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PAE - DURING CHECK FORWARD CARGO DOOR INNER SKIN FOUND CRACK AT CONTROL ROD ACCESS PANEL. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060400096 20020604 00096 NM 2002 6 4 ASAA0240046 1 20020423 A 5320 BAC1496377 ANGLE BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 792AS 28887 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT RT Z-ANGLE HAS HEAVY CORROSION FROM STATION 727 TO 767. REMOVED AND REPLACE D IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060400098 20020604 00098 NM 2002 6 4 ASAA0240047 1 20020429 A 5320 654795733 SUPPORT BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 792AS 28887 SEA - DURING C-CHECK, FOUND STATION 847 TO 867 AND RBL 19 THRESHOLD SUPPORT STRAP AND STRUCTURE CORRODED. REMOVED AND R EPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060400099 20020604 00099 NM 2002 6 4 ASAA0240048 1 20020427 A 5320 654795733 ANGLE BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 792AS 28887 SEA - DURING C-CHECK, FOUND Z-ANGLE CORRODED AT BS 767 TO 793 AND RBL 23. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060400101 20020604 00101 NM 2002 6 4 ASAA0240049 1 20020427 A 5320 654795733 ANGLE BOEING 737 737490 1384715 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 792AS 28887 SEA - DURING C-CHECK, FOUND AFT END OF Z-ANGLE CRACKED AT BS 792 AND RBL 23. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060400105 20020604 00105 NM 2002 6 4 ASAA0240050 1 20020427 A 5320 654795733 INTERCOSTAL BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 792AS 28887 SEA - DURING C-CHECK, FOUND INTERCOSTAL AT BS 847-867 AND RBL 25 AND WL 160 CORRODED. REMOVED AND REPLACED IAW SRM. (M ) 2 L 7 2 4F RT A16WE 2002060400107 20020604 00107 NM 2002 6 4 ASAA0240051 1 20020507 A 5320 65479573 THRESHOLD BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 769AS 25103 PAE - DURING C-CHECK, FOUND AFT CARGO BAY SUB THRESHOLD WEB CORRODED. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060400110 20020604 00110 2002 6 4 MEX2002037 4 20020212 A 3421 258733513 GYRO DOUG MD80 MD83 3023681 NM E/E BAY FAILED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 946AS 3507 49658 FLT 443 - HMO-MZT - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF ANTI-SKID LIGHTS AND FLAG ON ATT IN ADI RIGHT. SWIT CH S1-130 WAS CLEANED AND VERTICAL GYRO WAS REPLACED, FAIL WAS CORRECTED, TESTS OK. THE S1-130 SWITCH WAS REPLACED AND ANTI-SKID SYSTEM WAS CHECKED IAW MM 32-43-00 AND 34-23-01. (M) 2 L 7 2 4F RT 2002060400113 20020604 00113 WP 2002 6 4 MEX2002038 1 20020213 A 2910 TD6403S RELAY DOUG DC9 DC982 3022082 WP HYD SYSTEM FAILED A ASMF O OTHER O OTHER IN INSP/MAINT 1 SW 23 1003Y 48068 FLT 119 - TIJ-GDL - PILOT REPORTED THAT L HYD PRESS LOW LIGHT DOES NOT TURN ON. LOW PRESSURE SWITCH WAS CHECKED AN SEVE RAL CYCLES WERE PERFORMED WITH THE CONTROL SURFACES. RELAYS R2-497 AND R2-498 WERE SWAPPED, TESTS OK. DURING TRANSIT C HECK IN GDL BOTH RELAYS WERE REPLACED IAW MM 29-30-04. RELAYS WERE VERIFIED AGAIN IAW MM 29-30-00, TESTS OK. (M) 2 L 7 2 4F A6WE 2002060400118 20020604 00118 NM 2002 6 4 MEX2002044 1 20020216 A 2910 HYDRAULIC LINE DOUG MD80 MD83 3023681 NM RT MLG WW LEAKING A ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 945AS 49643 FLT 448 - BJX-LAX - DURING RAMP INSPECTION IT WAS DETECTED AN HYDRAULIC LEAK IN THE RIGHT MLG COMPARTMENT. A PRESSURE L INE OF THE BRAKE MANIFOLD AND MANIFOLD SEAL CAP WAS REPLACED IAW MM 32-42-03, IPC ITEM 102, TEST OK. 5 QUARTS OF HYDRAU LIC FLUID WERE NEEDED, THE HYDRAULIC LINE WAS REPLACED AND IT WAS VERIFIED BY LEAKS, ALL OK. (M) 2 L 7 2 4F RT 2002060400123 20020604 00123 WP 2002 6 4 MEX2002054 1 20020301 A 2742 95901 MOTOR DOUG DC9 DC987 3022087 WP HORIZ STAB FAILED A ASMF O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SW 23 204AM 4267 49404 FLT 420 - MEX-MID - CABIN CREW REPORTED PRIMARY LONGITUDINAL TRIM O/S, AIRCRAFT WAS REPAIRED IN THE HANGAR FACILITIES. PRIMARY TRIM WAS REPLACED AND TESTS WERE PERFORMED IAW M/M 27-40-01. (M) 2 L 7 2 4F RT A6WE 2002060400129 20020604 00129 WP 2002 6 4 MEX2002087 1 20020327 A 2910 BEARING DOUG DC9 DC983 3022083 WP HYD SYSTEM FAILED A ASMF O OTHER K FLUID LOSS LD LANDING 1 SW 23 838AM 6856 49397 FLT 574 - CUN-MEX - AIRCRAFT ARRIVED TO PLATFORM WITH HYDRAULIC FLUID LEAK IN THE RIGHT SYSTEM. IT WAS CHECKED AND THE LEAK WAS FOUND AT THE PTU SHUTOFF VALVE. BEARINGS WERE CHANGED IAW MM 29-10-08. DURING OVERNIGHT SERVICE WERE DETECTED THAT THE SEPARATOR AIR CONDITIONING WATER WERE WITH POLLUTION WITH SKYDROL SO THEY WERE CHANGED IAW MM 21-20-02. (M) 2 L 7 2 4F RT A6WE 2002060400133 20020604 00133 NE 2002 6 4 MEX2002088 2 20020327 A 7230 BLADE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE DAMAGED A ASMF A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 23 161PL 49764 725644 FLT 222 - MEX-CJS - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF THREE DETONATIONS IN ENGINE NR 2. DURING TAKEOFF TH E AIRCRAFT HAD THREE STALLS, SUCH FAIL REPEATS WITH 90 PERCENT OF N1. DURING CHECK WERE DETECTED TWO BLADES DAMAGED. A IRCRAFT WAS SENT TO HANGAR AND ENGINE NR 2 WAS CHANGED AND TESTS WERE PERFORMED IAW MM 71-00-01. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002060400137 20020604 00137 SO 2002 6 4 SIMA200208810 1 20020325 A 5330 SKIN EMB 145 EMB145 3260210 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - DURING INSPECTION OF AIRCRAFT, FOUND DENT ON LEFT FUSELAGE AFT OF FRAME 20 BELOW STRINGER 11L. REMOVED DENT BY CU T OUT. FABRICATED A DOUBLER AND FILLER IAW EMB 145 SRM 145/1142 CHAPTER 53 REV 17, 53-21-01, AND STANDARD SRM PRACTICES . (M) 2 L 7 2 4F RT T00011AT 2002060400139 20020604 00139 SO 2002 6 4 SIMA200208901 1 20020325 A 5347 SEAT TRACK EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING. LEFT GUSSET UNDER PILOTS CONTROL YOKE AND LEFT SEAT TRACK CORROSION FOUND. TREATED CO RROSION IAW EMB 145 CPM 51-21-04, 51-21-05, 51-21-06. (M) 2 L 7 2 4F RT T00011AT 2002060400142 20020604 00142 SO 2002 6 4 SIMA200208902 1 20020324 A 5320 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING. RIGHT GUSSET UNDER PILOTS CONTROL COLUMN AND RIGHT SEAT SEAT TRACK IS CORRODED. TREAT ED CORROSION ON RIGHT GUSSET AND RIGHT SEAT TRACK IAW EMB 145 CPM 51-21-04, 51-21-05, 51-21-06. (M) 2 L 7 2 4F RT T00011AT 2002060400144 20020604 00144 SO 2002 6 4 SIMA200208903 1 20020322 A 5320 14521725013 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING. SERVICE DOOR FORWARD SILL CORRODED. REMOVED AND REPLACED DOOR FORWARD SILL IAW EMB 14 5 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002060400146 20020604 00146 SO 2002 6 4 SIMA200208904 1 20020322 A 5320 14521725015 SILL EMB 145 EMB145 3260210 SO FUSLEAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 THIS IS LEVEL 2 FINDING. SERVICE DOOR AFT SILL CORRODED. REMOVED AND REPLACED DOOR SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002060400147 20020604 00147 SO 2002 6 4 SIMA200208905 1 20020322 A 5320 14529150001 CROSSBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS A LEVEL 2 FINDING. CABIN FLOOR CROSS BEAM CORRODED AT FRAME 23. REMOVED AND REPLACED CROSS BEAM IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002060400148 20020604 00148 SO 2002 6 4 SIMA200208906 1 20020322 A 5320 14529150003 CROSSBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING. CROSS BEAM PROFILE AT FRAME 23 CORRODED. REMOVED AND REPLACED CROSS BEAM PROFILE IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002060400150 20020604 00150 SO 2002 6 4 SIMA200208907 1 20020322 A 5320 CROSSBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING. CABIN FLOOR CROSS BEAM AT FRAME 23 END BRACKET AT RIGHT SILL CORRODED. REMOVED AND RE PLACED CROSS BEAM IAW EMB 145 SRM 51040-02. (M) 2 L 7 2 4F RT T00011AT 2002060400152 20020604 00152 SO 2002 6 4 SIMA200209303 1 20020323 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL CORRODED AT FRAME 20. REMOVED CORROSION AND FOUND TO BE ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400153 20020604 00153 SO 2002 6 4 SIMA200209304 1 20020324 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING. RIGHT SILL CORRODED BETWEEN FRAMES 23 AND 37. REMOVED CORROSION AND ACCEPTED AS IS IA W EMB GST-1014/02. RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400155 20020604 00155 SO 2002 6 4 SIMA200209305 1 20020322 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING. LEFT SILL IS CORRODED BETWEEN FRAMES 61 AND 62. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400156 20020604 00156 SO 2002 6 4 SIMA200209306 1 20020325 A 5320 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, LEFT GUSSET UNDER COPILOTS CONTROL COLUMN AND LEFT SEAT TRACK IS CORRODED. REMOVED COR ROSION, ACCEPTED AS IS IAW EMB GST-1031/02, RETREATED AREA IAW EMB145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400158 20020604 00158 SO 2002 6 4 SIMA200209307 1 20020323 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 58 AND 59. REMOVED CORRODED, ACCEPTED AS IS IA W EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400159 20020604 00159 SO 2002 6 4 SIMA200209308 1 20020323 A 5320 CROSSBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, RIGHT CROSSMEMBER CORRODED AT FRAME 59. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST- 1014/02. TREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400160 20020604 00160 SW 2002 6 4 HEEA079063 1 20020515 A 5343 400052007103 BEAM BELL 407 407 1182206 SW MLG CORRODED E K NONE O OTHER IN INSP/MAINT 1 SW 03 612PH 53199 MLG ATTACH BEAM HAS CORROSION OUT OF LIMITS. 1 G 7 1 3U O H2SW 2002060400164 20020604 00164 SO 2002 6 4 SIMA200209309 1 20020324 A 5320 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, CENTER BEAM GUSSET IS CORRODED BETWEEN FRAMES 30 AND 34. REMOVED CORROSION, ACCEPTED A S IS IAW EMB GST-1014/02. TREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400166 20020604 00166 SO 2002 6 4 SIMA200209310 1 20020324 A 5320 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, CENTER BEAM GUSSET IS CORRODED AT FRAME 26. REMOVED CORROSION IAW EMB GST-1014/02. TR EATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400167 20020604 00167 SO 2002 6 4 SIMA200209311 1 20020324 A 5320 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, LEFT BEAM GUSSET IS CORRODED BETWEEN FRAMES 25 AND 26. REMOVED CORROSION IAW EMB GST-1 014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400169 20020604 00169 SO 2002 6 4 SIMA200209312 1 20020324 A 5320 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, LEFT BEAM GUSSET CORRODED BETWEEN FRAMES 31 AND 33. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400170 20020604 00170 SO 2002 6 4 SIMA200209313 1 20020323 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, LEFT SILL CORRODED AT FRAME 49. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400171 20020604 00171 SO 2002 6 4 SIMA200209314 1 20020324 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, LEFT SILL CORRODED BETWEEN FRAMES 43 AND 44. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, TREATED AREA IAW EMB 145 CPT 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400172 20020604 00172 SO 2002 6 4 SIMA200209315 1 20020324 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, LEFT SILL CORRODED BETWEEN FRAMES 31-36. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST 1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400173 20020604 00173 SO 2002 6 4 SIMA200209316 1 20020324 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, LEFT SILL CORRODED BETWEEN FRAMES 29 AND 30. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400174 20020604 00174 SO 2002 6 4 SIMA200209317 1 20020324 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 THIS IS A LEVEL 2 FINDING, LEFT SILL CORRODED BETWEEN FRAMES 29 AND 30. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1 014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400175 20020604 00175 SO 2002 6 4 SIMA200209318 1 20020322 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDNG, LEFT SILL CORRODED BETWEEN FRAMES 20-22. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST- 1014/02. RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400176 20020604 00176 SO 2002 6 4 SIMA200209319 1 20020323 A 5320 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, CENTER GUSSET IN LAVATORY HAS CORROSION. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST -1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400177 20020604 00177 SO 2002 6 4 SIMA200209320 1 20020323 A 5320 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, RIGHT GUSSET IN LAVATORY HAS CORROSION. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST- 1014/02. RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400178 20020604 00178 SO 2002 6 4 SIMA200209321 1 20020324 A 5320 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, LEFT GUSSET IN LAVATORY HAS CORROSION. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1 014/02. RETREATED AREA IAW EMB 145 CPM 51-21-02, 51-21-05. (M0 2 L 7 2 4F RT T00011AT 2002060400183 20020604 00183 SO 2002 6 4 SIMA200209322 1 20020324 A 5320 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL FLOORBOARD SUPPORT CORRODED AT FRAME 51-54. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST 1014/02. RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400184 20020604 00184 SO 2002 6 4 SIMA200209323 1 20020323 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL CORRODED BETWEEN FRAMES 48 AND 49. REMOVED CORROSION, ACCEPTED AS IS IAW EM B GST 1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400187 20020604 00187 SO 2002 6 4 SIMA200209324 1 20020323 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL CORRODED BETWEEN FRAMES 43 AND 44. REMOVED CORROSION, ACCEPTED AS IS IAW EM B GST 1014/02. RETREATED AREA IAW EMB145 CPM 51-21-04 AND 51-21-05. (M) 2 L 7 2 4F RT T00011AT 2002060400189 20020604 00189 SO 2002 6 4 SIMA200209327 1 20020330 A 5313 STRINGER EMB 145 EMB145 3260210 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19L GOUGED. BLENDED GOUGE. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. REPAIRED IAW EMB GST-1002/02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002060400190 20020604 00190 SO 2002 6 4 SIMA200209328 1 20020330 A 5320 14525480003 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND LOWER CARGO DOOR SILL CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SI LL (BEAM). INSTALLED NEW BEAM IAW EMB 145 (SRM 145/1142, CHAPTER 51, REV 17) 51-40-02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002060400191 20020604 00191 SO 2002 6 4 SIMA200209329 1 20020330 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIGHT HAT BEAM BETWEEN FRAMES 17 AND 19. REMOVED CORROSION BY BLENDING OUT. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED DOUBLER. WORK DONE IAW EMB GST-1014/02, ITEM 14, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002060400193 20020604 00193 SO 2002 6 4 SIMA200209330 1 20020328 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIGHT HAT BEAM BETWEEN FRAMES 23 AND 24. REMOVED CORROS ION BY BLENDING OUT. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED DOUBLER. WORK DONE IAW EMB GST-1014/02, ITEM 7 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002060400194 20020604 00194 SO 2002 6 4 SIMA200209331 1 20020328 A 5315 14521721009 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND GALLEY AREA FORWARD DIGITAL (RIGHT SIDE) CORRODED. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED DOUBLER. WORK DONE I AW EMB GST-1014/02, ITEM 4A, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002060400195 20020604 00195 SO 2002 6 4 SIMA200209332 1 20020328 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - DURING IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE SERVICE DOOR CENTER SILL. BLENDED CORROSION. PERFORME D AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. REPAIRED IAW EMB GST-1014/02, ITEM 3, AREA NR 3, A ND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002060400197 20020604 00197 SO 2002 6 4 SIMA200209333 1 20020328 A 5315 14522461003 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND GALLEY AREA FORWARD DIGITAL, LEFT SIDE, CORRODED. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. REPAIRED IAW EMB GST -1014/02 ITE M 4B, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002060400198 20020604 00198 SO 2002 6 4 SIMA200209334 1 20020401 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY CENTER FLOOR SUPPORT BEYOND SRM LIMITS AFTER BLEN DING. REMOVED CORRODED GALLEY CENTER FLOOR SUPPORT. INSTALLED NEW GALLEY CENTER BEAM. WORK DONE IAW EMB 145, SRM 145/ 1142 CHAPTER 51, REV 17, 61-20-01, 51-20-03, 51-40-04, CPM 51-21-04, GST 1014/02, ITEM 10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002060400201 20020604 00201 SO 2002 6 4 SIMA200209335 1 20020401 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON CENTER BEAM UNDER GUSSET AT FRAME 20. REMOVED CORROSION BY CUT OUT. REPAIRED IAW EMB 145 SRM 145/1142 CHAPTER 53, REV 17 53-21-10, AND STANDARD. (M) 2 L 7 2 4F RT T00011AT 2002060400202 20020604 00202 SO 2002 6 4 SIMA200209501 1 20020403 A 2740 PITCH CONTROL EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 603AE 145055 ORD - FLT 4023 - AT APPROX 800-1000 FT F/O MAIN AND STANDBY PITCH TRIM BECAME INOPERATIVE CAPTAIN MAIN AND STANDBY PITCH . ALSO, INOPERATIVE CHECKLIST FOLLOWED AND CREW DECLARED EMERGENCY AND RETURNED TO ORD WITHOUT INCIDENT NO ASSOCIATED E ICAS MESSAGES AND MOC WAS NOTIFIED OF RETURN TO FIELD BY DISPATCH. (M) 2 L 7 2 4T RT T00011AT 2002060400203 20020604 00203 SO 2002 6 4 SIMA200210014 1 20020322 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING. GUSSET CORRODED AT FRAME 19 ON RIGHT HAT BEAM. BLENDED OFF CORROSION IAW EMB 145 CPM 51-41-02. REPAIRED IAW EMB GST 1014/02. (M) 2 L 7 2 4F RT T00011AT 2002060400204 20020604 00204 SO 2002 6 4 SIMA200210015 1 20020322 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 THIS IS A LEVEL 2 FINDING. LEFT HAT BEAM GUSSET IS CORRODED BETWEEN FRAMES 65 AND 68. INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002060400205 20020604 00205 SO 2002 6 4 SIMA200210016 1 20020322 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AE 145074 ABI - THIS IS A LEVEL 2 FINDING. RIGHT SILL IS CORRODED AT FRAME 39. REPAIRED RIGHT SILL AT FRAME 39 IAW EMB 145 GST-1 014/02. (M) 2 L 7 2 4F RT T00011AT 2002060400206 20020604 00206 SO 2002 6 4 SIMA200211604 1 20020426 A 2770 PLUNGER EMB 135 EMB135KL 3260302 SO GUSTLOCK DIRTY A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 800AE 145425 CMH - FLT 3882 - DURING FLIGHT CREW REPORTED THE GUST LOCK LIGHT ILLUMINATED. CREW FOLLOWED AOM PROCEDURES AND LANDED A T NEAREST AIRPORT. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND THE GUSTLOCK PLUNGER FOR MICROSWIT CHES WAS DIRTY. PLUNGER WAS CLEANED AND AN OPERATIONAL CHECK WAS DONE. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2002060400207 20020604 00207 SO 2002 6 4 SIMA200212140 1 20020413 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - THIS IS A LEVEL 2 FINDING, RIGHT OMEGA BEAM CORRODED AT FRAME 25. BLENDED CORROSION, PERFORMED NDT INSPECTION. R ESTORED SURFACE FINISH, IAW EMB GST-1140/02. (M) 2 L 7 2 4F RT T00011AT 2002060400208 20020604 00208 SO 2002 6 4 SIMA200212142 1 20020418 A 5315 14521712009 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - THIS IS A LEVEL 2 FINDING, FORWARD DIGITAL CORRODED. INSTALLED SERVICEABLE SECTION OF FORWARD DIGITAL IAW EMB 145 SRM 53-21-10. (M) 2 L 7 2 4T RT T00011AT 2002060400209 20020604 00209 SO 2002 6 4 SIMA200212143 1 20020418 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - THIS IS A LEVEL 2 FINDING, AFT SERVICE DOOR SILL CORRODED. REMOVED AND REPLACE AFT SERVICE DOOR SILL, IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002060400210 20020604 00210 SO 2002 6 4 SIMA200212144 1 20020418 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - THIS IS A LEVEL 2 FINDING, FORWARD SERVICE DOOR SILL CORRODED. INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002060400217 20020604 00217 SO 2002 6 4 SIMA200212145 1 20020418 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - THIS IS A LEVEL 2 FINDING, AFT RIGHT HAT BEAM GUSSET CORRODED. INSTALLED NEW HAT BEAM GUSSET IAW EMB145 SRM 51-40 -02. (M) 2 L 7 2 4T RT T00011AT 2002060400218 20020604 00218 SO 2002 6 4 SIMA200212146 1 20020418 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - THIS IS A LEVEL 2 FINDING, LEFT OMEGA BEAM REPAIR CORRODED AT FRAME 20. REPAIRED IAW EMB145 SRM 51-40-02, 51-20-0 3 AND 53-21-10. (M) 2 L 7 2 4T RT T00011AT 2002060400219 20020604 00219 SO 2002 6 4 SIMA200212147 1 20020418 A 5320 14522461003 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - THIS IS A LEVEL 2 FINDING, FORWARD RIGHT HAT BEAM DIAMOND GUSSET CORRODED. INSTALLED SERVICEABLE GUSSET IAW EMB 1 45 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002060400221 20020604 00221 SO 2002 6 4 SIMA200212148 1 20020418 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - THIS IS A LEVEL 2 FINDING, LOWER CARGO DOOR SILL CORRODED BETWEEN FRAME 65 AND 68. INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02, 51-40-06, 51-20-03. (M) 2 L 7 2 4T RT T00011AT 2002060400223 20020604 00223 SO 2002 6 4 SIMA200212154 1 20020424 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 145312 ABI - THIS IS A LEVEL 2 FINDING, CORROSION SERVICE DOOR CENTER SILL. REPAIRED CORRODED SERVICE DOOR SILL IAW EMB GST-13 48/02. (M) 2 L 7 2 4F RT T00011AT 2002060400224 20020604 00224 SO 2002 6 4 SIMA200212155 1 20020424 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 145312 ABI - THIS IS A LEVEL 2 FINDING, CORROSION ON SERVICE DOOR FORWARD SILL. REPAIRED CORRODED FORWARD SILL IAW EMB GST 134 8/02. (M) 2 L 7 2 4F RT T00011AT 2002060400225 20020604 00225 SO 2002 6 4 SIMA200212156 1 20020416 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 145301 ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OU T. FABRICATED A DOUBLER ANGLE AND FILLER. REPAIRED IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 17 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002060400228 20020604 00228 SO 2002 6 4 SIMA200212157 1 20020428 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 145312 ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY RIGHT BEAM AT FRAME 19. REMOVED CORROSION BY BLEN DING. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. REPAIRED IAW EMB GST-1348/02, AND S TANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002060400231 20020604 00231 SO 2002 6 4 SIMA200212158 1 20020424 A 5311 12010732001 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND FRAME 81 GOUGED LOWER HALF. REMOVED GOUGED FRAME. INSTALLED NEW FRA ME IAW EMB 145 SRM 145/1142 CHAPTER 51, REV 17, 51-20-01, 51-20-03, 51-40-02, 51-40-04 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002060400232 20020604 00232 SO 2002 6 4 SIMA200212159 1 20020425 A 5320 145255480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - DURING IMBV INSPECTION OF AIRCRAFT, FOUND CARGO DOOR LOWER SILL CORRODED BETWEEN FRAMES 65 AND 68. REMOVED CORROD ED SILL (BEAM). INSTALLED NEW BEAM IAW EMB145 SRM 145/1142, CHAPTER 51, REV 17, 51-40-02 AND STANDARD SRM PRACTICES. ( M) 2 L 7 2 4T RT T00011AT 2002060400236 20020604 00236 SO 2002 6 4 SIMA200212160 1 20020428 A 5315 14521721009 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON FORWARD DIGITAL. REMOVED CORROSION BY CUT OUT. PERFORM ED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. REPAIRED IAW EMB145 SRM 145/1142, CHAPTER 53, REV 17, 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002060400243 20020604 00243 2002 6 4 UIEA02014 4 20020429 A 2210 37572021 COMPUTER BOEING 747 747230B 1384889 NM AUTOPILOT SYS FAULTY A UIEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 15 508MC 21644 AIT TURNBACK, DURING CLIMB-OUT FROM JFK EN ROUTE TO MIA LOWER RUDDER DEFLECTION 5 DEGREES LEFT TO 3 DEGREES RIGHT CONTIN UOUSLY. RETURNED TO JFK. DEFLECTIONS CONTINUED DURING DESCENT AND APPROACH. MAINTENANCE USED PITOT STATIC TEST EQUIPM ENT TO FIND FAULT. IT WAS DETERMINED THAT THE YAW DAMPER COMPUTER WAS AT FAULT. REMOVED AND REPLACED THE LOWER RUDDER YAW DAMPER COMPUTER AND OPS CHECKED NORMAL PER MM 22-16-00. (M) 2 L 7 4 4F A20WE 2002060400247 20020604 00247 NM 2002 6 4 USAASB02071 1 20020415 A 1430 NAS6604D12 BOLT BOEING 737 7373B7 1384580 NM MLG MISSING A USAA O OTHER J G WARNING INDICATION MULTIPLE FAILURE CL CLIMB 1 EA 19 525AU 23860 CLT - FLT 701 - AFTER TAKEOFF FROM DCA, EN ROUTE TO CLT, CREW COULD NOT GET THE LANDING GEAR TO THE UP POSITION. CREW A CCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND WAS THEN ABLE TO RAISE THE GEAR. AS FLIGHT CONTINUED, FLIGHT LOST P RESSURIZATION AND TRANSPONDERS AT 10,000 FEET. AIRCRAFT APPEARED TO BE IN THE GROUND MODE. CREW WAS ABLE TO REGAIN PRE SSURIZATION AND THE FLIGHT CONTINUED ONTO CLT WHERE IT LANDED AND PROCEEDED TO THE GATE WITHOUT FURTHER PROBLEMS. CAPTA IN REPORTED THE OXYGEN MASKS NEVER DROPPED BECAUSE PRESSURIZATION PROBLEM OCCURRED BEFORE FLIGHT REACHED 10,000 FEET. N O EMERGENCY WAS DECLARED. ON ARRIVAL TO GATE, MAINTENANCE FOUND THE AIR/GROUND PUSH PULL CABLE BOLT ASSEMBLY MISSING. 2 L 7 2 4F RT A16WE 2002060400251 20020604 00251 NM 2002 6 4 USAASB02073 1 20020417 A 2612 FIRE WARNING BOEING 737 7374B7 1384702 NM COCKPIT ACTIVATED A USAA F ACTIVATE FIRE EXT. J WARNING INDICATION LD LANDING 1 EA 19 440US 24811 PHL - FLT 437 - APU WAS STARTED ON FINAL INTO PHL AT 1,200 FEET, AND UPON TOUCHDOWN, CREW RECEIVED AN APU FIRE WARNING B ELL AND INDICATION LIGHT. AS AIRCRAFT CLEARED THE RUNWAY, CREW PULLED AND ROTATED THE APU FIRE HANDLE, DISCHARGING THE BOTTLE. FIRE LIGHT EXTINGUISHED AS CREW SWITCHED THE APU OFF. CREW ASKED TOWER IF THEY OBSERVED ANY SMOKE. TOWER RESP ONDED NO SMOKE WAS NOTED. FLIGHT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. (M) 2 L 7 2 4F RT A16WE 2002060400253 20020604 00253 NM 2002 6 4 USAASB02074 1 20020418 A 3350 20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 407US 23877 TPA - FOUND CENTER AISLE AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED TWO BATTERY PACKS. (M) 2 L 7 2 4F RT A16WE 2002060400255 20020604 00255 NM 2002 6 4 USAASB02075 1 20020419 A 3350 1012721 SOCKET BOEING 737 7374B7 1384702 NM CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 443US 24842 IND - FOUND EMERGENCY LIGHTS ON SEATS 24 AND 25 LEFT INOPERATIVE. MAINTENANCE FOUND THE LIGHT SOCKET AT SEAT 25 SHORTED AND THE FUSE ON THE POWER SUPPLY BLOWN. TEMPORARILY DISCONNECTED SEAT 25 AND REPLACED THE POWER SUPPLY FUSE. MAINTENA NCE REPLACED THE LIGHT. (M) 2 L 7 2 4F RT A16WE 2002060400257 20020604 00257 NM 2002 6 4 USAASB02076 1 20020422 A 3350 FUSE BOEING 737 737401 1384701 NM BATTERY CHARGER BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 23882 PIT - FOUND BROKEN FUSE ON EMERGENCY LIGHT CHARGER. MAINTENANCE REPLACED THE CHARGER. (M) 2 L 7 2 4F RT A16WE 2002060400258 20020604 00258 NM 2002 6 4 USAASB02077 1 20020422 A 3350 20121 CHARGER BOEING 737 737401 1384701 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 413US 23882 PIT - FOUND CIRCUIT INOPERATIVE ON EMERGENCY LIGHT BATTERY CHARGER. MAINTENANCE REPLACED THE BATTERY CHARGER. (M) 2 L 7 2 4F RT A16WE 2002060400259 20020604 00259 NE 2002 6 4 USAASB02078 2 20020421 A 7200 ENGINE BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE RIGHT MAKING METAL A USAA A UNSCHED LANDING M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 511AU 23594 724694 CLT - FLT 379 - AFTER TAKEOFF, CREW NOTED AN OVERTEMP CONDITION ON THE RIGHT ENGINE. THE TOWER INFORMED THE CREW THAT B LACK SMOKE WAS POURING FROM THE ENGINE. THE CREW REDUCED POWER ON THE RIGHT ENGINE. THE FLIGHT RETURNED TO CLT AND LAN DED WITH NO FURTHER INCIDENT. MAINTENANCE REPORTED METAL IN THE TAILPIPE. THE ENGINE IS SCHEDULED FOR REPLACEMENT. (M ) 2 L 7 2 4F 4 F RT A16WE E2GL 2002060400260 20020604 00260 NM 2002 6 4 USAASB02082 1 20020426 A 3397 WIRE BOEING 737 737401 1384701 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 405US 23885 EWR - FOUND EMERGENCY LIGHT ON END BAY OF SEAT 2C INOPERATIVE. MAINTENANCE SPLICED A BROKEN WIRE UNDER THE SEAT. (M) 2 L 7 2 4F RT A16WE 2002060400261 20020604 00261 NM 2002 6 4 USAASB02086 1 20020430 A 3350 1012721 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 443US 24842 IND - FOUND THE SEAT EMERGENCY LIGHT AT ROW 3 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 2002060400262 20020604 00262 NM 2002 6 4 USAASB02087 1 20020501 A 3350 30043231 LIGHT BOEING 737 7374B7 1384702 NM L1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 435US 24557 BOS - FOUND FORWARD LEFT ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 2002060400264 20020604 00264 2002 6 4 WRLA200203 4 20020212 A 3417 HG280D80 ADC DOUG DC10 DC1030F 3023504 WP E/E BAY FAILED A WRLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 304WL 47928 CAPTAIN HAD NO AIRSPEED ON TAKEOFF ROLL, GROUND ABORT. BLEW OUT CAPTAIN PITOT LINE AND GOT A SMALL AMOUNT OF DEBRIS. C LEARED LINE ALSO CADC FAILED AND ALL FLAGS SHOWN ON AIR SPEED INDICATOR. REPLACED CADC WITH FED EX LOANER AND PERFORMED PITOT STATIC TEST OK. CLEANED LINES AND REMOVED AND REPLACED CAPTAIN CADC. (M) 2 L 7 3 4F RT A22WE 2002060400266 20020604 00266 SO 2002 6 4 C2XA02IA112 1 20020514 A 4920 4501968B APU EMB 145 EMB145ER 3260211 SO APU BAY LEAKING A C2XA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14933 145018 AMA- THE CREW NOTED THAT AN ELECTRICAL SMELL WAS PRESENT IN THE CABIN/COCKPIT WHILE THE APU IS RUNNING, WITH THE APU BL EED SELECTED OFF. MAINTENANCE REMOVED AND REPLACED THE APU, PERFORMED A OPERATIONAL CHECK AND A LEAK CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002060400267 20020604 00267 2002 6 4 C2XA02IA113 4 20020517 A 3140 701700082407 COMPUTER EMB 145 EMB145 3260210 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 12957 145080 IAH- FLIGHT 3668, ON CLIMB THE CREW NOTED THAT THE PITCH TRIM MAIN SYSTEM WAS INOPERATIVE AND NO TRIM INDICATION. THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 IC600 COMPUTER, PERFORMED OPERATIONAL CHECKS AND NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002060400268 20020604 00268 2002 6 4 C2XA02IA114 4 20020517 A 3140 701700082407 COMPUTER EMB 145 EMB145 3260210 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 12957 145080 IAH- FLIGHT 3668, ON CLIMB THE CREW NOTED THAT THE CABIN ALTITUDE AND RATE WERE MISSING, AND THE CREW WAS UNABLE TO CON TROL THE CABIN ALTITUDE. THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 IC600 COMPUTER, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002060400269 20020604 00269 SO 2002 6 4 C2XA02IA116 1 20020523 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13935 145022 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT LIGHT ON THE LEFT HAND PANEL AROUND THE EMERGENCY DOOR OVER WING IS INOP. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT DC/AC INVERTER, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002060400270 20020604 00270 SO 2002 6 4 C2XA02IA117 1 20020527 A 3397 7287503607 WIRE HARNESS EMB 145 EMB145LR 3260212 SO CABIN BURNED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13988 145265 IAH- FLIGHT 4117, DURING CLIMB THE CREW NOTED SMOKE IN THE CABIN AND GOT LAV SMOKE ON THE EICAS. THE CREW RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AT SEATS 14A AND 15A. GROUND RAN AIRCRAFT AND FOUND NO D EFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002060400271 20020604 00271 SO 2002 6 4 C2XA02IA118 1 20020525 A 3350 20131A POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16918 145397 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE FIRST EMERGENCY LIGHTING FLOOR STRIP WAS NOT ILLUMINATED. MAINTENANCE RE MOVED AND REPLACED THE BATTERY POWER SUPPLY NR 2 AND PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002060400273 20020604 00273 SO 2002 6 4 C2XA02TY093 1 20020519 A 5210 14533677401 BUSHING EMB 145 EMB145ER 3260211 SO PAX DOOR OUT OF POSITION A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14925 145004 TYS, DURING A SCHEDULED INSPECTION THE HAT BUSHING ON THE MAIN DOOR LATCH BOLT WAS FOUND MIGRATING. MAINTENANCE REMOVED LOWER HAT BUSHING, CLEANED AND REINSTALLED WITH SEALANT TO SEAL THE GAP BETWEEN THE BUSHING AND FITTING IAW EMB-GST-168 2/01. THE REPAIR PROCEDURE WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002060400274 20020604 00274 SO 2002 6 4 C2XA02TY095 1 20020521 A 3260 23092900001 UPLOCK EMB 145 EMB145ER 3260211 SO NLG FALSE INDICATION A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 12946 145052 TYS AIRCRAFT WAS FERRIED INTO TYS DUE TO A GEAR RETRACTION INDICATION PROBLEM. MAINTENANCE CHANGED THE NOSE UPLOCK BOX AND ALL OPS CHECKS WERE GOOD IAW EMB AMM 32-33-07 AND FUNCTIONAL CHECK 32-41-00-700-801A, AND OPS CHECK WAS GOOD IAW AM M 32-30-00-700-801-A. ALL WORK WAS ACCOMPLISH AND WAS RELEASED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002060400275 20020604 00275 WP 2002 6 4 CALA0200296 1 20020517 A 5347 5936663503 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 CORROSION AROUND NUT PLATE HOLES ON LEFT TIE DOWN RAIL AT STATION 1260 ABB. REMOVED AND REPLACED TIE DOWN RAIL PER SRM 51-10-2. 2 L 7 2 4F A6WE 2002060400276 20020604 00276 WP 2002 6 4 CALA0200301 1 20020517 A 5320 J060228U3 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 FORWARD BAG BIN LOWER DOOR JAMB PAN CRACKED ON LOWER LEG STATION 393. REPAIRED LOWER DOOR JAMB PAN PER SRM 53-05 FIG 44 . 2 L 7 2 4F A6WE 2002060400277 20020604 00277 NM 2002 6 4 CALA0200305 1 20020521 A 3350 BR964411 SOCKET BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17356 23942 EMERGENCY ESCAPE PATH AISLE LIGHT INOP AT SEAT 23 LEFT. REPLACED LIGHT SOCKET ASSEMBLY PER MM 33-51-81. 2 L 7 2 4F RT A16WE 2002060400279 20020604 00279 WP 2002 6 4 CALA0200307 1 20020520 A 5311 59667641 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 TAIL COMPARTMENT CANT 1474 RIGHT LOWER SIDE CRACKED AT ATTACH POINT. INSTALLED FRAME PER SRM 51-40-3 AND 51-10-3. 2 L 7 2 4F A6WE 2002060400280 20020604 00280 WP 2002 6 4 CALA0200309 1 20020520 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 AFT ACCESSORY COMPARTMENT FRAME AT STATION 1380 LEFT SIDE HAS CHAFED FRAME WEB. CUT OUT DAMAGED AREA OF WEB, FABRICATED AND INSTALLED REPAIR PER SRM 53-01 FIG 94. 2 L 7 2 4F A6WE 2002060400281 20020604 00281 WP 2002 6 4 CALA0200311 1 20020521 A 5522 SKIN DOUG DC9 DC982 3022082 WP ELEVATOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 LEFT ELEVATOR LOWER SKIN DENTED. REMOVED ELEVATOR, REPAIRED AND BALANCED PER SRM 55-03 FIG 14, 55-20-2. REINSTALLED PE R MM 27-30-02 AND 27-30-00. 2 L 7 2 4F A6WE 2002060400282 20020604 00282 WP 2002 6 4 CALA0200312 1 20020521 A 5752 5955455508 TRIM TAB DOUG DC9 DC982 3022082 WP AILERON GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 RIGHT AILERON CONTROL TAB UPPER SURFACE GOUGED. REMOVED, REPAIRED, AND BALANCED CONTROL TAB PER MM 27-10-02, SRM 51-70- 1, AND SRM 57-50-1. REINSTALLED PER MM 27-10-02. 2 L 7 2 4F A6WE 2002060400284 20020604 00284 WP 2002 6 4 CALA0200315 1 20020523 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 AFT PIT WEB CORRODED AT STATION 1322 - 1309 R28 - R27. REMOVED, FABRICATED AND REINSTALLED INTERCOSTAL PER SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2002060400285 20020604 00285 WP 2002 6 4 CALA0200316 1 20020523 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 L2 DOORWAY CUSP WEB CORRODED LBL 44 TO LBL 54 AT STATION FS 1168. REMOVED AND REPLACED WEB AND STIFFENER PER SRM 51-30- 2 AND 51-30-5. 2 L 7 2 4F A6WE 2002060400286 20020604 00286 WP 2002 6 4 CALA0200321 1 20020527 A 3350 60030431LB BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16895 49394 THE OVERHEAD EMERGENCY LIGHTS AT ROW 5-9 STAYED ON WHEN POWER WAS SECURED DURING TEST. THE EMERGENCY LIGHT B5-101 BATTE RY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00. 2 L 7 2 4F A6WE 2002060400287 20020604 00287 NE 2002 6 4 CALA0200322 2 20020529 A 7532 ETPU10002C PRESSURE SWITCH BOEING 757 757224 1384958 NM RROYCE RB211 RB211535E4 54555 NE NR 1 ENGINE FAULTY A CALA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 SW 09 14118 22246 27560 31379 THE NR 1 ENGINE FLAMED OUT ON APPROACH TO EWR AT 5,000 FEET. THE ENGINE WAS SUCCESSFULLY RESTARTED WITHIN ONE MINUTE. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. THE EEC AND BVCU WERE BITE TESTED IAW MM 73-21-00 AND 75-32-01 AND NO FAUL TS WERE FOUND. A TPU BITE TEST FOUND THE UNIT AT FAULT. THE TPU WAS REMOVED AND REPLACED IAW MM 75-32-15 AND OPERATION AL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2002060400289 20020604 00289 WP 2002 6 4 CNMA200200003 1 20020330 A 7110 NTL6012503 COWLING DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 ENGINE MISSING A CNMA K NONE O OTHER UK UNKNOWN 1 SW 07 630AX 46596 455128 NR 2 ENGINE FAN COWL FOUND MISSING UPON WALK-AROUND AFTER LANDING. REPLACED LEFT ENGINE SIDE COWL AND ASSOCIATED HARDWA RE, NO OTHER DAMAGE NOTED. 2 L 7 3 4F 4 F A22WE E23EA 2002060400290 20020604 00290 NM 2002 6 4 DHL2002715008 1 20020529 A 3150 WARNING SYSTEM BOEING 727 727155C 138404Z NM COCKPIT MALFUNCTIONED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 715DH 19618 WHILE BRINGING POWER UP FOR TAKEOFF WITH AIRCRAFT CONFIGURED, GOT CONFIGURATION HORN AND SYSTEM THEN TESTED BAD ON TAXIW AY. ABORTED TAKEOFF. CYCLED FLAPS, TAKEOFF WARNING SYSTEM, OPS CHECKS GOOD IAW MM 31-26-00. 2 L 7 3 4F A3WE 2002060400291 20020604 00291 NM 2002 6 4 DHL2002741006 1 20020517 A 2611 SMOKE DETECTOR BOEING 727 7272Q9 138448M NM NR 6 INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 741DH 21931 ON PREFLIGHT THE NR 6 PRESS TO TEST SMOKE DETECTION SYSTEM WOULD NOT TEST. RELAMPED NR 6 SMOKE DETECTOR BEACON. OPS CH ECK GOOD IAW 727 MM 26-17-000. 2 L 7 3 4F RT A3WE 2002060400294 20020604 00294 NM 2002 6 4 DHL2002741008 1 20020526 A 2611 SMOKE WARNING BOEING 727 7272Q9 138448M NM COCKPIT ACTIVATED A DHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 741DH 21931 MAIN CABIN SMOKE DETECTOR ILLUMINATED INFLIGHT. RAN ENGINE PER JRH 5.2. PRESSURIZED AND OPS CHECKED THE ACM. OPS PER JRH 6.3 & 6.5, COMPLETED A 40 MIN RUNUP. RESULTS NORMAL. 2 L 7 3 4F RT A3WE 2002060400295 20020604 00295 NE 2002 6 4 DHL2002748002 2 20020518 A 7314 378200 PUMP BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE FAILED A DHLA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SO 01 748DH 22440 700372 ENGINE FAILURE NR 3 ENGINE AFTER GEAR RETRACTION. REMOVED NR 3 ENG FUEL PUMP & FCU PER M/M 73-11-1 PRATT & WHITNEY. IN STALLED SERVICEABLE FUEL PUMP & FCU IAW M/M 73-11-1 & 73-21-1. OPS CHECK SERVICEABLE. 2 L 7 3 4F 4 F A3WE E2EA 2002060400296 20020604 00296 NM 2002 6 4 DHL2002750003 1 20020525 A 3350 BATTERY BOEING 727 7272M7 138407S NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750DH 21951 EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES IAW 33-50-101. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002060400297 20020604 00297 NM 2002 6 4 DHL2002752001 1 20020517 A 3240 METERING VALVE BOEING 727 727223 1384074 NM RT MLG FAILED A DHLA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 709AA 22466 DURING MAX POWER ASSURANCE RUN, PARKING BRAKE FAILS TO SECURE A/C EPR IS 1.4 AND ABOVE. MLG BRAKES SAME AT POWER SETTIN G 1.6 AND ABOVE. PERFORMED PARKING T/S+RIG CHECK IAW M/M 32-44-0. OPS CHECK GOOD. PERFORMED HYD BRAKE SYS T/S IAW 32- 41-00. FOUND RT MLG BRAKE METERING VALVE OUT OF ADJ. BLEEDING TO RETURN SIDE UNABLE TO ADJ. REMOVED AND REPLACED BRAK E METERING VALVE. 2 L 7 3 4F A3WE 2002060400299 20020604 00299 NM 2002 6 4 DL72E020548 1 20020514 A 3350 900542 BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 21481 AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. FOUND BATTERY DEFECTIVE IN LIGHT ASSY. REPLACED BATTERY ASSY. 2 L 7 3 4F A3WE 2002060400300 20020604 00300 NM 2002 6 4 DL72L020517 1 20020508 A 5610 5893543130 WINDOW BOEING 727 727232 1384082 NM COCKPIT ARCED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 512DA 21314 R1 WINDOW HEAT INOP, SMOKE IN COCKPIT IN FLT. REPLACING R1 WINDOW AND CONTROLLER. 2 L 7 3 4F A3WE 2002060400301 20020604 00301 NM 2002 6 4 2002UALA00925 1 20020528 A 5313 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 MID CABIN BODY STATION 1022 LEFT HAND CREASE BEAM WEB CORRODED ON UPPER SURFACE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR A CCOMPLISHED.CREASE BEAM REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002060400302 20020604 00302 NM 2002 6 4 2002UALA00927 1 20020529 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 LEFT HAND UPPER FORWARD FUS SKIN DENTED, STATION 606 TO STATION 612, BETWEEN STRINGER 16 AND STRINGER 17L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.DOUBLER AND FILLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002060400303 20020604 00303 NM 2002 6 4 2002UALA00930 1 20020528 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 937UA 26668 LOWER LH SKIN HAS A LARGE DENT APPROX. 8" AFT OF THE POTABLE WATER SERVICE PANEL MAJOR REPAIR ACCOMPLISHED. DOUBLER RE PAIR PERFORMED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060400304 20020604 00304 NM 2002 6 4 2002UALA00931 1 20020525 A 2780 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 #3 SLAT OUTER LOWER SKIN IS CRACKED ON AFT ROW RIVETS, 38TH RIVET FROM INBD SIDE. MAJOR REPAIR ACCOMPLISHED. DAMAGE CU T OUT, DOUBLER REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060400305 20020604 00305 NM 2002 6 4 2002UALA00933 1 20020525 A 2780 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 #1 SLAT, LOWER TRAILING EDGE SKIN, 1 EA RIVET CRACKED ON INBD SIDE ON SKIN. AT 2ND FROM OUTBOARD AUX TRACK. MAJOR REPA IR ACCOMPLISHED. REPAIR DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060400306 20020604 00306 NM 2002 6 4 2002UALA00936 1 20020524 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 STATION 178 BLKHD HAS NUMEROUS CRACKS LOCATED AT STA 178, WL 188, LBL 1.5, STA 178, WL188, RBL 1.5, STA 178, WL 202M LBL 7. STA 178, WL206.5, RBL 1, STA 178, RBL 5, WL 198. MAJOR REPAIR ACCOMPLISHED. BULKHEAD DOUBLER AND STRAP REPAIR MANUF ACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060400307 20020604 00307 NM 2002 6 4 2002UALA00943 1 20020530 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 FORWARD CARGO DOOR CUT-OFF AFT FRAME STATION 492.4 INBD FRAME FLANGE BLENDED BEYOND LIMITS MAJOR REPAIR ACCOMPLISHED. REINFORCEMENT REPAIR ANGLE INSTALLED ON FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060400311 20020604 00311 WP 2002 6 4 DHL2002802501 1 20020521 A 5712 FORMER DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 802DH 46076 ITEM: REF: N/R 1747 RH WING L/E FORMER CRACKED .250 UPPER PART XFS622.500CORR: REMOVED FASTNERS IAW SRM 51-1-20D PG.1 . STOP DRILLED CRACK IAW SRM 57-2-0 PG/ 9-10. FABRICATED REINFORCING ANGLE( 2024T3.050) IAW SRM 57-2-0 PG. 9-10 , CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B INSTALLED REINFORCING ANGLE IAW SRM 51-1-20D PG.9 SRM 51-1-21 PG. 1 2 L 7 4 4F RT 4A25 2002060400312 20020604 00312 WP 2002 6 4 DHL2002802502 1 20020523 A 5313 3779659501 FITTING DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 802DH 79074 46076 ITEM: REF.: N/R 0455 MAIN CARGO COMP.- BATHTUB FITTING WITH 3.00" CRACK IN IT.CORR>: REMOVED CRACKED FITTING IAW SRM 51 -1-20D , SRM 51-1-23 FIG. 48. CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, PG. 9 , SRM51-1-23 FIG. 48 2 L 7 4 4F RT 4A25 2002060700007 20020607 00007 NM 2002 6 7 02FDEA00371 1 20020601 A 2613 OVERHEAT LOOP BOEING 727 727200 138407E NM A/C BAY FAULTY A FDEA K NONE N FALSE WARNING CR CRUISE 1 SO 25 234FE 21328 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. TROUBLESHOT DOWN TO LEAK BETWEEN NR 3 BLEED & RT PACK VALVE. OPEN ED KEEL BEAM ACCESS IN RT W/W AND LEAK CHECKED WITH NR 3 ENGINE RUNNING NO LEAKS FOUND IN KEEL BEAM AREA, CARGO COMPARTM ENT, OR AFT STAIRS AREA. ORDERED KEEL BEAM OVERHEAT DETECTOR PRECAUTIONARY. ALL OTHER OVERHEAT DETECTORS ARE IN STOCK AT GSO. FOUND GROUND IN M365 SECT 48 R OVERHEAT LOOP, REF AMM 26-14-000-1. REMOVED AND REPLACED SAME, OPS NORMAL PER A MM 26-14-001-2. SECURED AFT CARGO PANELS CLOSED PER SMP. 2 L 7 3 4F RT A3WE 2002060400313 20020604 00313 WP 2002 6 4 DHL2002802503 1 20020523 A 5313 3779658502 FITTING DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 802DH 79074 46076 ITEM: REF.: N/R MAIN CARGO COMP- BATHTUB FITTING WITH 3.00" CRACK IN IT , STA. 857.0000 , L3RCORR: REMOVED DAMAGED FITTI NG IAW SRM 51-1-20D, PG21 , SRM 51-1-23 FIG. 48 CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING & PLY-WASHERS IAW SRM 51-1-20D PG.9, SRM51-1-23 FIG. 48 2 L 7 4 4F RT 4A25 2002060400314 20020604 00314 WP 2002 6 4 DHL2002802506 1 20020520 A 5712 FORMER DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 802DH 79074 46076 ITEM:N/R 1914 LH WING OUTBD. L/E- FORMER AT STA. XFS825.000 WITH .500 CRACK IN IT.CORR: PERFORMED STOP DRILL IAW SRM 57- 2-0 PG. 9-10, FABRICATED DOUBLER WITH 2024T3AL.050 IAW SRM 57-2-0 PG. 9-10, CLEANED , TREATED ,AND PRIMED IAW SRM 51-1-8 B , INSTALLED DOUBLER IAW SRM 57-2-0 PG. 9-10 2 L 7 4 4F RT 4A25 2002060400315 20020604 00315 WP 2002 6 4 DHL2002802504 1 20020523 A 5313 3779658502 FITTING DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 802DH 79074 46076 ITEM: REF.: N/R 0454 MAIN CARGO COMPT- BATHTUB FITTING WITH 3.00" CRACK IN IT, STA 857.000 L3RCORR: REMOVED DAMAGED FITT ING IAW SRM 51-1-20D PG. 21 SRM 51-1-23 FIG. 48 CLEANED , TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING AND PLY-WASHER IAW SRM 51-1-20D PG. 9, SRM51-1-23 FIG. 48 2 L 7 4 4F RT 4A25 2002060400316 20020604 00316 WP 2002 6 4 DHL2002802505 1 20020520 A 5712 FORMER DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 802DH 79074 46076 ITEM: REF.: N/R 1916 LH WING OUTBD L/E - FORMER @ STA. XFS791.000 WITH .500 CRACK IN IT.CORR: PERFORMED STOP DRILL IAW S RM 57-2-0 PG. 9-10 , FABRICATED DOUBLER WITH 2024T3AL.050 IAW SRM 57-2-0 PG. 9-10 CLEANED, TREATED AND PRIMED IAW SRM 51 -1-8B , INSTALLED DOUBLER IAW SRM 57-2-0 PG. 9-10 2 L 7 4 4F RT 4A25 2002060400317 20020604 00317 WP 2002 6 4 DHL2002802507 1 20020520 A 5712 FORMER DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 802DH 79074 46076 ITEM: N/R 1915 LH WING OUTBD. L/E - FORMER AT STA.XFS841.000 WITH .500 CRACK IN IT.CORR.: PERFORMED STOP DRILL IAW SRM 5 7-2-0 PG. 9-10 . FABRICATED DOUBLER WITH 2024T3AL.050 IAW SRM 57-2-0 PG. 9-10 , CLEANED , TREATED , AND PRIMED IAW SRM 5 1-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 PG. 9-10 2 L 7 4 4F RT 4A25 2002060400318 20020604 00318 WP 2002 6 4 DHL2002802508 1 20020521 A 5712 FORMER DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 802DH 79074 46076 ITEM: N/R 1913 LH WING OUTBD L/E- FORMER AT STA. XFS803.750 WITH .500 CRACK IN IT.CORR: PERFORMED STOP DRILL IAW SRM 57- 2-0 PG. 9-10, FABRICATED DOUBLER WITH 2024T3AL .050 IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED AND PRIMED , IAW SRM 51-1- 8B INSTALLED DOUBLER IAW SRM 57-2-0 PG. 9-10 2 L 7 4 4F RT 4A25 2002060400319 20020604 00319 SO 2002 6 4 COMA0210023 1 20020531 A 3350 LAMP EMB 120 EMB120RT 3260202 SO A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 267CA 120259 FLIGHT 5005 ONE EMERGENCY FLOOR LIGHT AT ROW 8 IS INOP.DEFERRED MAINT PER MEL. 2 L 7 2 4T RT A31SO 2002060400320 20020604 00320 EA 2002 6 4 COMA0260347 1 20020601 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 821CA 7420 FLIGHT 5197 FLAPS FAIL MESSAGE WHEN SELECTED TO 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER MEL AND AD 98- 20-01. 2 L 7 2 4F RT A21EA 2002060400321 20020604 00321 EA 2002 6 4 COMA0260348 1 20020601 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 978CA 7158 FLIGHT 5262 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.COULD NOT DUPLICATE FOUND NO DEFECTS WITH CABIN DOOR. 2 L 7 2 4F RT A21EA 2002060400322 20020604 00322 EA 2002 6 4 COMA0260349 1 20020531 A 2610 355523255 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 988CA 7204 FLIGHT 5413 ANTI-ICE DUCT WARNING DURING TAXI.REPLACED THE R/H MLG WHEEL WELL AREA BLEED AIR LEAK SENSING LOOP. 2 L 7 2 4F RT A21EA 2002060400323 20020604 00323 SO 2002 6 4 C2XA02BT019 1 20020526 A 3230 23092900401 UPLOCK EMB 145 EMB145ER 3260211 SO FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13929 145009 EWR---CO3540, CREW REPORTED "LANDING GEAR DISAGREEMENT ON MAIN GEAR. AIRCRAFT AIR RETURNED" (TO NEWARK WITHOUT INCIDENT) .....MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED RIGHTHAND MAIN LANDING GEAR UPLOCK IAW EMB145 AMM #32-33-10. OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002060400324 20020604 00324 NM 2002 6 4 AWXA200200490 1 20020514 A 5311 6518420 FRAME BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 0 0 23258 MCN - MAJOR REPAIR - DURING C-16 CHECK A .2" CRACK WAS FOUND IN THE UPPER CORNER OF THE OUTBD FRAME OF THE CAPTAINS WIND SHIELD, VERIFIED BY HFEC INSPECTION. MAINTENANCE CUTOUT DAMAGED AREA OF CAPTAINS WINDSHIELD FRAME AT UPPER CORNER; PERFO RMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01, PG. 231-234. 2 L 7 2 4F RT A16WE 2002060400325 20020604 00325 NM 2002 6 4 AWXA200200493 1 20020516 A 5311 65465412 FRAME BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 0 0 23258 MCN - MAJOR REPAIR - DURING C-16 CHECK A 5/8" CRACK WAS FOUND ON FUSELAGE FRAME AT THE INBOARD END OF CUTOUT FOR STR 2 L/H, BS 663. MAINTENANCE REMOVED STRINGER SPLICE AND CUTOUT CRACKED AREA OF FRAME AT BS 663, STR 2 L/H; PERFORMED HFEC I NSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED A -1 ANGLE, 2 EACH -2 FILLERS, A STRINGER SPLICE, AND INSTALLE D REPAIR PARTS IAW B737-300 SRM 53-00-07, PG. 225-231. 2 L 7 2 4F RT A16WE 2002060400326 20020604 00326 NM 2002 6 4 AWXA200200494 1 20020516 A 5311 65465412 FRAME BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 0 0 23258 MCN - MAJOR REPAIR - DURING C-16 CHECK A 3/8" CRACK WAS FOUND ON FUSELAGE FRAME AT THE OUTBOARD END OF CUTOUT FOR STR 2 L/H, BS 663. MAINTENANCE REMOVED STRINGER SPLICE AND CUTOUT CRACKED AREA OF FRAME AT BS 663, STR 2 L/H; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED A -1 ANGLE, 2 EACH -2 FILLERS, A STRINGER SPLICE, AND INSTALL ED REPAIR PARTS IAW B737-300 SRM 53-00-07, PG. 225-231. 2 L 7 2 4F RT A16WE 2002060400327 20020604 00327 NM 2002 6 4 AWXA200200496 1 20020516 A 5311 65465412 FRAME BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 0 0 23258 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1/2" CRACK WAS FOUND ON FUSELAGE FRAME AT THE OUTBOARD END OF CUTOUT FOR STR 2 R/H, BS 663. MAINTENANCE REMOVED STRINGER SPLICE AND CUTOUT CRACKED AREA OF FRAME AT BS 663, STR 2 R/H; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED A -1 ANGLE, 2 EACH -2 FILLERS, A STRINGER SPLICE, AND INSTALL ED REPAIR PARTS IAW B737-300 SRM 53-00-07, PG. 225-231. 2 L 7 2 4F RT A16WE 2002060400328 20020604 00328 2002 6 4 GLBA2002068 4 20020522 A 3400 6226521016 CONTROL HEAD BEECH 1900 1900D 1154162 CE #1 STRIPPED A GLBA D RETURN TO BLOCK O OTHER CR CRUISE 1 NM 03 100UX 160 UE100 #1 NAV SELECT BUTTON STRIPPED, REPLACED CONTROL HAED 2 L 7 2 4T RT A24CE 2002060400329 20020604 00329 2002 6 4 GLBA2002070 4 20020525 A 3400 066306200 ALTIMETER BEECH 1900 1900D 1154162 CE #1 INOPERATIVE A GLBA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 NM 03 118GL 1413 UE118 CAPTAINS ALTIMETER FAILED ON T/O, REPLACED ALTIMETER OPS CHECKED SYSTEM SATISFACTORY 2 L 7 2 4T RT A24CE 2002061700034 20020617 00034 CE 2002 6 17 GLBA2002072 1 20020529 A 5210 12951405913 CABLE BEECH 1900 1900D 1154162 CE PAX DOOR BROKEN A GLBA K NONE O OTHER TX TAXI/GRND HDL 1 NM 03 153GL UE153 PAX DOOR WOULD NOT OPEN. INSPECTED FOUND INNER DOOR CABLE BROKEN. REPLACED INNER DOOR CABLES. 2 L 7 2 4T RT A24CE 2002060500019 20020605 00019 NM 2002 6 5 AWXA200200484 1 20020602 A 2530 416000123 COFFEEMAKER BOEING 737 7373B7 1384580 NM GALLEY DEFECTIVE A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 328AW 2634 735 23377 CLIMB-OUT A BURNT RUBBER SMELL WAS NOTICED BY THE F/A IN THE AFT GALLEY. RETURNED TO PHX & LANDED UNEVENTFULLY. PRIOR TO TAKEOFF ACFT HAD RETURNED TO GATE FOR THE SAME PROBLEM. DURING THIS EVENT MX HAD IDENTIFIED NR 2 COFFEEMAKER AS BEIN G VERY HOT & HAVING A BURNT ODOR, BOTH COFFEEMAKERS WERE REPLACED. THE SECOND EVENT (AIR TURNBACK) MX TROUBLESHOT FOR S MOKE OR FUMES FROM THE AIR CONDITIONING SYSTEM USING AMM 21-00-01, NO SMOKE OR FUMES WERE NOTED. AFT GALLEY WIRING WAS INSPECTED BEHIND BOTH COFFEEMAKERS AND IN THE OVERHEAD PANEL, MX ALSO INSPECTED THE SMOKE DETECTORS IN THE AFT LAVATORIE S FINDING NO DEFECTS OR BURNING SMELL. 2 L 7 2 4F RT A16WE 2002060500020 20020605 00020 EU 2002 6 5 AWXA200200485 1 20020531 A 2560 DIN40863R62 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 640AW 448 SEA - EMERGENCY EQUIPMENT - DURING INSPECTION THE EMERGENCY FLASHLIGHT AT THE AFT FLIGHT ATTENDANT JUMP SEAT WAS FOUND T O HAVE A LOW BATTERY. MAINTENANCE REPLACED THE BATTERIES IN EMERGENCY FLASHLIGHT AT THE AFT FLIGHT ATTENDANTS JUMP SEAT . 2 L 7 2 4F RT A28NM 2002060500021 20020605 00021 NM 2002 6 5 AWXA200200486 1 20020531 A 2560 P4010021 BATTERY BOEING 737 7373Q8 1384670 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 327AW 23507 PHX - EMERGENCY EQUIPMENT - FLT 0274 - FLIGHT CREW REPORTED THAT THE OUTBOARD AFT FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT BATTERIES, OPERATIONA L CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002060500023 20020605 00023 NM 2002 6 5 AWXA200200487 1 20020531 A 3510 174660N5 OXYGEN MASK BOEING 737 7373U3 13844CC NM COCKPIT DEFECTIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 335AW 28740 PHX - EMERGENCY EQUIPMENT - EXHALE FUNCTION OF CAPTAINS EMERGENCY OXYGEN MASK IS BLOCKED. MAINTENANCE REMOVED AND REPLA CED THE CAPTAINS EMERGENCY OXYGEN MASK IAW T/C R1B35001, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002060500026 20020605 00026 NM 2002 6 5 0201725507 1 20020529 A 5322 FITTING BOEING 757 757251 1384970 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 507US 23196 During "H" check found corrosion on door sill fitting at BS 1720. Repaired per EA 55-191086. 2 L 7 2 4F RT A2NM 2002060500027 20020605 00027 SW 2002 6 5 HEEA079169 1 20020523 A 6300 407010206103 BEARING BELL 407 407 1182206 SW M/R DRIVE DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 494PH 53396 MAIN ROTOR DRIVE BEARING HAS A WEAK AND DETERIORATED BOOT. 1 G 7 1 3U O H2SW 2002060500028 20020605 00028 NE 2002 6 5 C1HA200288012 2 20020601 A 7261 FILTER BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE NR 3 ENGINE BYPASSING A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 688CA 22344 ON TAKEOFF ROLL DURING POWER UP LOW OIL PRESSURE OR FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 MAIN ENG INE OIL FILTER MM CHPT 79-15-00. OPS & LEAK CHECK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2002060500041 20020605 00041 NM 2002 6 5 DL72E020526 1 20020509 A 5320 69678811 GUSSET BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 INSPECTION OF THE RT TORQUE BOX STRUCTURE OF THE VENTRAL STAIRWAY PER BAC S/B 727-53-0129 REVEALED A CRACK IN THE FS 127 3 HORIZONTAL BEAM UPPER GUSSET. THE CRACKED PART WAS REMOVED AND REPLACED WITH A NEW PART PER ER/A 383130-14. 2 L 7 3 4F A3WE 2002060500042 20020605 00042 NM 2002 6 5 DL72L020518 1 20020508 A 5610 5893543130 WINDSHIELD BOEING 727 727232 1384082 NM COCKPIT FAULTY A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 512DA 21314 DURING CLIMB R1 WINDOW BEGAN TO SMOKE AND SPARK. R1 WINDOW HEAT WAS TURNED OFF SMOKE AND SPARKS STOPPED. REMOVED AND R EPLACED R1 WINDOW AND SENSOR. CHECKS NORMAL. 2 L 7 3 4F A3WE 2002060500044 20020605 00044 NM 2002 6 5 DL72S020510 1 20020506 A 3350 S106 BATTERY PACK BOEING 727 727232 1384082 NM COCKPIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 521DA 21472 COCKPIT L1 AND L2 EMERGENCY EXIT LIGHTS INOP DUE TO BATTERY FAIL. REPLACED SAME, CHECKS OK. 2 L 7 3 4F A3WE 2002060500047 20020605 00047 NM 2002 6 5 DL72S020521 1 20020508 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 523DA 21583 FOUND FORWARD BULLNOSE EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2002060500048 20020605 00048 NM 2002 6 5 DL72S020539 1 20020512 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 515DA 21431 ON L/O, FOUND EMERGENCY EXIT SIGN IN FIRST CLASS AISLE INOP. REMOVED AND REPLACED BATTERY PACK PER M/M, OPS CHECKS NORM AL. 2 L 7 3 4F A3WE 2002060500050 20020605 00050 NM 2002 6 5 DL72S020546 1 20020513 A 3350 900542 CHARGER BOEING 727 727225A 1384077 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8891Z 21860 AISLE CEILING EMERGENCY EXIT SIGN IN FIRST CLASS FLICKERS ON AND OFF WITH SWITCH IN ARMED OR OFF POSITION. REPLACED THE BATTERY PACK CHARGER. NOW LIGHT ASSY CHECKS NORMAL. 2 L 7 3 4F RT A3WE 2002060500051 20020605 00051 NM 2002 6 5 DL72S020549 1 20020514 A 5313 STRINGER BOEING 727 727225A 1384077 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 FOUND ON D1 LETTER CK, CORROSION AT STR 28 RT AT STA 620. REPAIRED PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 2002060500053 20020605 00053 NM 2002 6 5 DL72S020571 1 20020517 A 5330 6518420406 SKIN BOEING 727 727225A 1384077 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 THE UPPER HINGE CUTOUT OF THE L1 DOOR CUTOUT WAS FOUND WITH A .5 INCH CRACK IN THE SKIN AND A CRACK INDICATION AT A FAST ENER HOLE IN THE BEAR STRAP. THE CRACKS WERE REMOVED AND REPAIRED WITH DOUBLERS PER ER/A 383169-14, REV B. 2 L 7 3 4F RT A3WE 2002060500057 20020605 00057 NM 2002 6 5 DL72S020583 1 20020522 A 5522 SKIN BOEING 727 727232 1384082 NM ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 FOUND ON E1 LETTER CK, LT ELEVATOR BONDED BEADED SKIN CRACKED AT STA 100 TO STA 103 FWD OF TAB. REPAIRED PER SRM 55-20- 3D FIG 3. 2 L 7 3 4F A3WE 2002060500058 20020605 00058 NM 2002 6 5 DL738020530 1 20020510 A 3350 8100017502 SIGN BOEING 737 737832 13844CF NM CABIN BROKEN A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 3760C 30816 L2 DOOR EMERGENCY EXIT SIGN BASE BROKEN. REPLACED LT ASSY. 2 L 7 2 4F RT A16WE 2002060500063 20020605 00063 NM 2002 6 5 DL738020535 1 20020511 A 3020 32156183 ANTI-ICE VALVE BOEING 737 737832 13844CF NM CFMINT CFM56 CFM567B26US NE NR 2 ENGINE FAILED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 394DA 30562 877440 APPLICATION OF PWR FOR TAKEOFF RIGHT YELLOW COWL ANTI-ICE CAUTION AND YELLOW MASTER CAUTION. ABORTED TAKEOFF 70 KTS AND RETURNED TO RAMP. TS PER FIM 20-21-00. REMOVED AND REPLACED NR 2 TAI VALVE PER MM 30-21-11. PERFORMED TAKEOFF PWR CH ECK, ALL INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002060500065 20020605 00065 NE 2002 6 5 DL738020547 2 20020514 A 7200 CFM567 ENGINE BOEING 737 737832 13844CF NM CFMINT CFM56 CFM567B26US NE NR 2 FIRE A DALA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 383DN 7740 7740 874954 30346 874954 RAMP REPORTED TAIL PIPE FIRE NR 2 ENG. DRY CHEM WAS USED TO EXTINGUISH FIRE. REPLACED ENGINE NR 2. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002060500066 20020605 00066 NM 2002 6 5 DL738020557 1 20020515 A 3350 D71702001 POWER SUPPLY BOEING 737 737832 13844CF NM CABIN DEFECTIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 379DA 30349 POWER SUPPLY AT STATION 952 LBL 14 HAS BAD OUTPUT FOR THE EMERGENCY AISLES LIGHTS. REPLACED PWR SUPPLY. 2 L 7 2 4F RT A16WE 2002060500068 20020605 00068 NM 2002 6 5 DL73K020511 1 20020507 A 5753 6546434141 FLAP BOEING 737 737232 1384475 NM LT WING DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 LEFT INBOARD AFT FLAP TRAILING EDGE BONDED ASSY WAS FOUND WITH MULTIPLE DELAMINATED AREAS. REPAIR PER ER/A 417277-14. 2 L 7 2 4F RT A16WE 2002060500071 20020605 00071 NM 2002 6 5 DL73K020519 1 20020508 A 2761 654456115 CAP BOEING 737 737247 138448D NM SPOILER ACTUATOR SPLIT A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 376DL 23603 HYDRAULIC SYSTEM A FAILURE IMMEDIATELY FOLLOWING TAKEOFF. FOUND CAP ON NR 7 SPOILER HAD SPLIT. REPLACED CAP AND O-RING . INSPECTED AND REPLACED CASE DRAIN AND PRESSURE FILTERS. SERVICED HYDS TO FULL. LEAK AND OPS CHECKS OK. 2 L 7 2 4F A16WE 2002060500072 20020605 00072 2002 6 5 HEEA079209 4 20020524 A 2312 064102300 TRANSCEIVER BELL 412 412 1182202 SW VHF SYSTEM INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 VHF SYSTEM TRANSCEIVER RECEIVES AND TRANSMITS ONLY INTERMITTENTLY. 1 G 7 2 4U H4SW 2002060500073 20020605 00073 NM 2002 6 5 DL73K020529 1 20020510 A 5753 SKIN BOEING 737 737232 1384475 NM T/E FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 INBOARD AFT FLAP TRAILING EDGE BONDED ASSEMBLY WAS FOUND WITH SKIN TO CORE DELAMINATION. REPAIR PER ER/A 417316-14. 2 L 7 2 4F RT A16WE 2002060500074 20020605 00074 NM 2002 6 5 DL73K020534 1 20020511 A 7333 CONNECTOR BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE DAMAGED A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 315DL 23087 717146 A/C RETURNED TO GATE DUE TO NR 2 FUEL FLOW INDICATION BEING ERRATIC. DISCONTINUED T/O AT 70 KTS - GW 117.0. NR 2 ENGIN E FUEL FLOW WENT TO MAX THEN ZERO FUEL FLOW. FOUND AFT CANNON PLUG ON FUEL FLOW TRANSMITTER DAMAGED. REPLACED NR 2 ENG INE FUEL FLOW TRANSMITTER PER M/M. RAN ENG LEAKS CKS OK. REPLACED CANNON PLUG D828 GOING TO FUEL FLOW TRANSMITTER. F UEL FLOW IND OPS NORMAL. REMOVED MCO/PLAC. 2 L 7 2 4F 4 F RT A16WE E2EA 2002060500075 20020605 00075 NM 2002 6 5 DL73K020537 1 20020511 A 3350 20131A BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 320DL 23092 EMERGENCY LIGHTS AT FWD CLOSET AND ROWS 1-4 SEATS GO OUT QUICKLY WHEN TESTED. REPLACED BATTERY PACK, TESTS OK. 2 L 7 2 4F RT A16WE 2002060500076 20020605 00076 NM 2002 6 5 DL73K020569 1 20020519 A 3350 20131A BATTERY BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 305DL 23077 RT OVERWING EMERGENCY EXIT SIGN INOP. REPLACED BATTERY, OPS NORMAL. 2 L 7 2 4F RT A16WE 2002060500077 20020605 00077 NM 2002 6 5 SABA020064 1 20020602 A 3350 1306 BULB DHAV DHC8 DHC8103 1386005 NM BURNED OUT A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 882CC 162 Flight 5216, Acft 882: During Preflight in Charlotte, Pilot reported Cabin overhead emergency light would not test. Main tenance removed and replaced bulbs. System ops checked good. Aircraft returned to service. 2 H 7 2 4T RT A13NM 2002060500078 20020605 00078 NM 2002 6 5 DL757020501 1 20020504 A 2932 31914906 O-RING BOEING 757 757232 1384965 NM HYD SYSTEM DAMAGED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 6704Z 30396 PILOT REPORT - L HYD QTY MSG ILLUMINATED. REPLACED DAMAGED O-RING ON S27 PRESS SW LT PYLON LEAK CK OK. SERVICED HYD FL UID TO FULL. 2 L 7 2 4F RT A2NM 2002060500079 20020605 00079 NM 2002 6 5 DL757020508 1 20020506 A 3350 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 662DN 24991 EMERGENCY LIGHT AT 26D INOP. REPLACED BASE, CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002060500080 20020605 00080 NM 2002 6 5 DL757020509 1 20020506 A 2130 1305026 CONTROL PANEL BOEING 757 757232 1384965 NM COCKPIT FAULTY A DALA K NONE O OTHER AP APPROACH 1 SO 27 638DL 23761 CABIN DEPRESSURIZED AT 3000 FEET. BITE CHECK OF NR 1 AND NR 2 PRESSURIZATION CONTROLLERS REVEALS NO FAULTS. REPLACED C ABIN PRESSURIZATION SELECTOR PANEL AS PRECAUTIONARY CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002060500081 20020605 00081 SW 2002 6 5 HEEA079210 1 20020524 A 6710 BUSHING BELL 206 206L3 1182108 SW SUPPORT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116P RE548 51530 MAIN ROTOR CONTROL SUPPORT BUSHING WORN. 1 G 7 1 3U H2SW 2002060500082 20020605 00082 NM 2002 6 5 DL757020523 1 20020509 A 3234 257T11032 MODULE BOEING 757 757232 1384965 NM COCKPIT FAULTY A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 6715C 30486 LANDING GEAR WOULD NOT RETRACT. THE GEAR HANDLE WOULD ONLY GO UP TO THE OFF POSITION, IT WOULD NOT GO BEYOND THAT POINT . RETURNED HANDLE TO DOWN POSITION, 3 GREENS. REMOVED AND REPLACED LANDING GEAR HANDLE, JACKED AC RAN GEAR SEVERAL TIM ES WITH HYDRO MULE AND WITH ELECTRIC PUMP, TIMED GEAR EXTENSION AND RETRACTION PER MM CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002060500083 20020605 00083 NM 2002 6 5 DL757020533 1 20020510 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 674DL 25979 ON LAYOVER FOUND AFT EMERGENCY LIGHTS INOP. REPLACED BATTERY CHARGER AND BATTERY OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2002060500084 20020605 00084 NM 2002 6 5 DL757020563 1 20020517 A 2121 6067723 FAN BOEING 757 757232 1384965 NM CARGO BAY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 688DL 27587 JUST AFTER LANDING AND SWITCHING TO APU BLEED AIR TO RUN THE PACKS A STRONG ELECTRICAL SMELL WAS PRESENT ACCOMPANIED BY RT RECIRC FAN INOP LIGHT. RT RECIRC FAN SELECTED OFF AND ODOR DISSIPATED. CONTRACT MTC OPERATED RT RECIRC FAN AND CONF IRMED STRONG BURNING RUBBER SMELL IN COCKPIT AND FORWARD CARGO BIN. REMOVED AND REPLACED RT RECIRC FAN, OP CKS GOOD. 2 L 7 2 4F RT A2NM 2002060500085 20020605 00085 NM 2002 6 5 DL757020570 1 20020519 A 3350 767 LIGHT BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 665DN 25013 L-4 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED, CHECKS OK. 2 L 7 2 4F RT A2NM 2002060500086 20020605 00086 NM 2002 6 5 DL757020574 1 20020519 A 3350 LIGHT BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 616DL 22823 ON LAYOVER FOUND EXTERIOR EMERGENCY LIGHT ABOVE LEFT WING AFT OF EXIT HATCH INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A2NM 2002060500088 20020605 00088 NM 2002 6 5 DL764020531 1 20020510 A 3350 D71702001 POWER SUPPLY BOEING 767 767432ER 1385134 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831MH 29702 BATTERY PACK FUSES BLOWN, EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY. 2 L 7 2 4F RT A1NM 2002060500089 20020605 00089 NM 2002 6 5 DL764020540 1 20020512 A 3350 D71702001 POWER SUPPLY BOEING 767 767432ER 1385134 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 834MH 29707 EMERGENCY EXIT SIGNS AFT OF DOORS 4L AND 4R FOUND INOP DURING PREDEPARTURE CHECK. REPLACED EMERGENCY LIGHT POWER MODULE M1210. 2 L 7 2 4F RT A1NM 2002060500090 20020605 00090 NM 2002 6 5 DL764020542 1 20020512 A 3350 D71702001 POWER SUPPLY BOEING 767 767432ER 1385134 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 834MH 29707 EMERGENCY EXIT LIGHTS AFT OF 4L AND 4R INOP. REPLACED POWER MODULE M1210. 2 L 7 2 4F RT A1NM 2002060500091 20020605 00091 NM 2002 6 5 DL764020543 1 20020513 A 3320 1873 LIGHT BOEING 767 767432ER 1385134 NM CABIN INTERMITTENT A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 827MH 29698 CABIN NIGHT LIGHT BY SEAT 6F FLICKERING WITH BURNT SMELL. INSPECTED NIGHT LIGHT ASSY. REMOVED BULB NEEDS NEW BULB NASI FLL. FWD TO MCO AND PLAC PER MEL 33-21-01A. 2 L 7 2 4F RT A1NM 2002060500094 20020605 00094 NM 2002 6 5 DL764020566 1 20020518 A 7920 COUPLING BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 2 ENGINE LOOSE A DALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 833MH 4737 29706 706193 AT TOP OF CLIMB THE RIGHT ENGINE OIL QUANTITY BEGAN TO DECREASE TO ZERO. OIL PRESSURE EVENTUALLY TURNED AMBER AND THEN BOXED RED. ENGINE SHUT DOWN. RETIRED MECH ON BOARD REPORTED EXCESSIVE OIL WETTING NOTED ON REAR TURBINE FRAME AREA UND ER CORE COWL. MTC ACTION IN PROGRESS. INSPECTED ENG, FOUND OIL SUPPLY TUBE COUPLING NUT LOOSE. TIGHTENED NUT AND SAFE TY WIRED PER M/M LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E23EA 2002060500095 20020605 00095 NM 2002 6 5 DL767020502 1 20020504 A 2121 6066223 FAN BOEING 767 767232 1385132 NM CABIN FAILED A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 113DA 22225 EICAS MSG INFLT - RT RECIR FAN, ALONG WITH INOP LIGHT IN RT RECIR FAN SWITCH. REPLACED RT RECIRC FAN, OP CKS GOOD. 2 L 7 2 4F RT A1NM 2002060500096 20020605 00096 NM 2002 6 5 DL76G020500 1 20020503 A 2597 WIRE HARNESS BOEING 767 7673P6 1385105 NM CABIN ARCED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 154DL 25241 ARCING COMING FROM UNDER SEAT 1FG. REMOVED HARNESS, INSTALLED NEW HARNESS. CHECKS GOOD, REMOVED MCO AND PLACARD. 2 L 7 2 4F RT A1NM 2002060500097 20020605 00097 NM 2002 6 5 DL76G020515 1 20020506 A 2560 BPS73 BATTERY PACK BOEING 767 7673P6 1385105 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 153DL 24985 EMERGENCY ESCAPE SYS FAILS SQUIB TEST. REPLACED LEFT ESCAPE BATTERY PACK, OPS OK. 2 L 7 2 4F RT A1NM 2002060500099 20020605 00099 NM 2002 6 5 DL76G020578 1 20020522 A 2131 CONTROLLER BOEING 767 7673P6 1385105 NM CABIN PRESSURE MALFUNCTIONED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 152DL 24984 AUTO PRESS CONTROLLER 1 AND 2 FAILED. F/A REPORTED FUMES IN AFT CABIN. RESET CONTROLLERS, NO FAULTS. RAN PACKS, OK. RAN ENGINES AND PRESSURIZED, ALL OK. NO ODORS NOTED IN CABIN. 2 L 7 2 4F RT A1NM 2002060500100 20020605 00100 NM 2002 6 5 DL76G020587 1 20020523 A 3350 LIGHT BOEING 767 7673P6 1385105 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 152DL 24984 RT SIDE AFT FUSELAGE EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2002060500102 20020605 00102 WP 2002 6 5 DHL2002802561 1 20020523 A 5101 377968U502 FITTING DOUG DC8 DC873 302199C WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 MAIN CARGO COMPT BATH TUB FITTING WITH 3 IN CRACK IN IT STA 857.000 L-71.REMOVED CRACKED FITTING PER SRM 51-1 20D PG 21, AND SRM 51-1-23 FIG 4B. CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B. INSTALLED NEW FITTING PER SRM 51-1-20D PG 9 AN D SRM 51-1-23 FIG 48. 2 L 7 4 4F RT 4A25 2002060500104 20020605 00104 SW 2002 6 5 HEEA079217 1 20020524 A 3213 212321103 CROSSTUBE BELL 412 412 1182202 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 1444 36019 FWD CROSSTUBE CORRODED BEYOND LIMITS. TUBE HAS SEVERAL CORROSION PITS OF .012 INCH IN AN AREA WHERE NO CORROSION IS ALL OWED. THESE PITS WERE FOUND ON THE TOP SIDE NEAR THE SADDLE MOUNTS. 1 G 7 2 4U H4SW 2002060500105 20020605 00105 NM 2002 6 5 DL76K020538 1 20020511 A 1430 114T41457 BOLT BOEING 767 767332 1382001 NM L/E SLAT SHEARED A DALA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 172DZ 29691 L/E SLAT ASSM AFTER LANDING. MTC FOUND NR 9 SLAT TRACK TARGET BOLT SHEARED. REPLACED BOLT, BUSHING AND AUX TRACK ARM R OLLER WASHER ASSY IPC 27-81-02-01 SH5 CIRCLE L. 2 L 7 2 4F RT A1NM 2002060500106 20020605 00106 NM 2002 6 5 DL76L020504 1 20020505 A 3620 WARNING SYSTEM BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE COCKPIT MALFUNCTIONED A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 187DN 23220 27582 727655 LT ENG HP S-O-V CAUTION MSG ON T/O ROLL. CYCLED BLEED SWITCHES, MSG CLEARED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002060500107 20020605 00107 SW 2002 6 5 HEEA079218 1 20020524 A 7120 BEARING BELL 206 206L3 1182108 SW ENGINE MOUNT UNSTAKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30KH 10185 51527 ENGINE MOUNT BEARING UNSTAKED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060500108 20020605 00108 NM 2002 6 5 DL76L020506 1 20020506 A 5753 ATTACH FITTING BOEING 767 767332 1382001 NM T/E FLAP BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 LT OUTBOARD FLAP OUTBOARD ATTACH POINT FOUND BROKEN. INSTALLED ATTACH FITTING PER SRM 51-10-02-0. 2 L 7 2 4F RT A1NM 2002060500110 20020605 00110 NM 2002 6 5 DL76L020522 1 20020509 A 2560 BPS73 BATTERY BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 199DN 28456 RT SQUIB FAILS TO TEST 1. REMOVED AND REPLACED SQUIB BATTERY RIGHT SIDE. OPS NORMAL. 2 L 7 2 4F RT A1NM 2002060500112 20020605 00112 NM 2002 6 5 DL76L020567 1 20020519 A 3350 LIGHT BOEING 767 767332 1382001 NM CABIN DAMAGED A DALA K NONE L NO TEST CR CRUISE 1 SO 27 185DN 27961 PASSENGER SEAT 10 F EMERGENCY TRACK LIGHT INOP/DAMAGE. FOUND EMERGENCY LIGHT SOCKET PULLED OUT AND WIRE BROKEN. NEW SO CKET INSTALLED BUT NO BULBS INSTALLED AND NEED MOUNTING FWD TO MCO AND PLACARD PER MEL 33-51-03. 2 L 7 2 4F RT A1NM 2002060500114 20020605 00114 NM 2002 6 5 DL76L020586 1 20020522 A 3350 LIGHT BOEING 767 767332 1382001 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 196DN 28453 TWO EXTERIOR EMERGENCY LIGHTS AFT OF LEFT WING INOP. RELAMPED SAME, OPS NORMAL. 2 L 7 2 4F RT A1NM 2002060500115 20020605 00115 NM 2002 6 5 DL76L020591 1 20020524 A 3350 LIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 176DN 25061 SEAT 2AB, 22AB, 29AB, 40AB 1 E-PATH LIGHT BULB. FWD TO MCO PER MEL 33-51-03. 2 L 7 2 4F RT A1NM 2002060500117 20020605 00117 NM 2002 6 5 DL76P020536 1 20020510 A 1430 114T41457 BOLT BOEING 767 767332 1382001 NM L/E SLAT SHEARED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 144DA 27584 ON TAXI OUT, GOT L/E ASYMMETRY T/S AND FOUND PROX SENSOR TARGET AT S286 LEFT SLAT NR 5 EXTEND PLATE MISSING AND ATTACH S CREW SHEARED. INSTALLED NEW TARGET AND ATTACHING SCREW. SYSTEM OPS NORMAL. 2 L 7 2 4F RT A1NM 2002060500118 20020605 00118 NM 2002 6 5 DL76P020562 1 20020516 A 3350 0201991008 LIGHT BOEING 767 767332 1382001 NM CABIN LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1402A 25989 EMERGENCY PATH LIGHTS INOP AT SEAT 4E-38B-42B. 2 L 7 2 4F RT A1NM 2002060500119 20020605 00119 NE 2002 6 5 DL76S020512 2 20020507 A 7200 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 FAILED A DALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 117DL 45054 456 580321 23276 580321 ENGINE STALLED ON TAKEOFF WITH EGT EXCEEDING REDLINE. NR 2 ENG REPLACED. 2 L 7 2 4F 4 F RT A1NM E13NE 2002060500120 20020605 00120 NM 2002 6 5 DL76S020544 1 20020511 A 4920 APU BOEING 767 767332 1382001 NM APU BAY MALFUNCTIONED A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 130DL 7416 24080 P2446 AFTER APU WENT TO RUN, APU ANNUNCIATED FAULT AND SHUT DOWN (ACCOMPANIED BY ACRID SMELL MOMENTS LATER). RESET APU ECU, R AN APU UNDER LOAD NO FAULTS. 2 L 7 2 4F RT A1NM 2002060500121 20020605 00121 NM 2002 6 5 DL76S020565 1 20020517 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 124DE 23438 OVERHEAD AISLE LIGHTS FIRST CLASS LEFT SIDE INOP. REPLACED BATTERY PACK AND RACK. 2 L 7 2 4F RT A1NM 2002060500125 20020605 00125 NE 2002 6 5 NACA20020026 2 20020604 A 7200 71700 GEARBOX PWA BOEING 727 72723 1384004 NM PWA JT8 JT8D NE #3 N² SEIZED A NACA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 AL 03 992AJ 0 655399 19428 655399 DISCREPANCY: #3 engine failure in flight. N¹ - 16%, N² - 2%, oil pressure 2 PSI.CORRECTIVE ACTION: Replaced the #3 engin e. 2 L 7 3 4F 4 F A3WE E2EA 2002060500126 20020605 00126 SW 2002 6 5 HEEA079226 1 20020524 A 6730 206076062003 CYLINDER BELL 206 206L3 1182108 SW SERVO LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 49EA 51507 SERVO CYLINDER LEAKING AND RATCHETY. REPLACED WITH SERVICEABLE SERVO. 1 G 7 1 3U H2SW 2002060500127 20020605 00127 NM 2002 6 5 DL76S020568 1 20020517 A 5512 185T10011 SKIN PANEL BOEING 767 767332 1382001 NM HORIZ STAB DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 A 2 FOOT, 6 INCH DIA AREA WAS FOUND DISBONDED ON THE LEFT HORIZONTAL STABILIZER UPPER INBOARD FORWARD SKIN PANEL BETWEEN FS 53.659 AND FS 80.896. THE DISBONDED SECTION OF HONEYCOMB CORE WAS REPLACED PER SRM 51-70-10 BY DEPT 382 ON SHOP ORD ER H05277. THE PANEL WAS REINSTALLED ON THE A/C. 2 L 7 2 4F RT A1NM 2002060500129 20020605 00129 SW 2002 6 5 HEEA079228 1 20020524 A 7810 407063001101 EXHAUST STACK BELL 407 407 1182206 SW ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 457PH 53147 ENGINE EXHAUST STACK CRACKED. 1 G 7 1 3U O H2SW 2002060500130 20020605 00130 NM 2002 6 5 DL777020577 1 20020521 A 2530 COFFEEMAKER BOEING 777 777232 1385232 NM GALLEY SPARKS A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 865DA 29737 GALLEY 412 DURING FLIGHT, F/A OBSERVED SPARKS FROM COFFEEMAKER NR 2. DEPOWERED ALL 3 C/BS TO ALL 3 COFFEEMAKERS. REMOV ED ALL COFFEEMAKERS OUT OF AFT GALLEY LEFT SIDE. INSPECTED ALL WIRES BEHIND COFFEMAKERS, FOUND NO DAMAGE. REINSTALLED ORIGINAL COFFEEMAKERS, ALL CHECK OK. 2 L 7 2 4F RT T00001SE 2002060500131 20020605 00131 SW 2002 6 5 HEEA079229 1 20020524 A 7810 407063001101 EXHAUST STACK BELL 407 407 1182206 SW ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 493PH 53393 ENGINE EXHAUST STACK CRACKED. 1 G 7 1 3U O H2SW 2002060500132 20020605 00132 SW 2002 6 5 HEEA079230 1 20020524 A 3340 A470DR LIGHT BELL 407 407 1182206 SW STROBE INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 498PH 53399 STROBE INOPERATIVE. 1 G 7 1 3U O H2SW 2002060500133 20020605 00133 2002 6 5 HEEA079231 4 20020524 A 2562 110324 ANTENNA BELL 206 206L3 1182108 SW ELT BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116L 51529 EMERGENCY LOCATOR TRANSMITTER ANTENNA BROKEN. SCRAPPED. 1 G 7 1 3U H2SW 2002060500134 20020605 00134 2002 6 5 HEEA079232 4 20020524 A 2562 110324 ANTENNA BELL 407 407 1182206 SW ELT BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8595X 53267 EMERGENCY LOCATOR TRANSMITTER ANTENNA BROKEN. SCRAPPED. 1 G 7 1 3U O H2SW 2002060500135 20020605 00135 SW 2002 6 5 HEEA079233 1 20020524 A 2840 1103P262 PRESSURE SWITCH BELL 412 412 1182202 SW FUEL SYSTEM INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 FUEL INDICATOR PRESSURE SWITCH LIGHT FLICKERS INTERMITTENTLY. SCRAPPED. 1 G 7 2 4U H4SW 2002060500136 20020605 00136 NM 2002 6 5 DLM11020579 1 20020522 A 3397 0201991005 WIRE HARNESS DOUG MD11 MD11 3023602 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 804DE 48475 EMERGENCY LIGHTS ON SEATS IN FWD BUSINESS CLASS WILL NOT STAY ON. FLASH ON AND OFF EVERY FEW MINUTES. FOUND DAMAGED WI RE HARNESS UNDER SEAT 1H. REPLACED WIRE HARNESS. OPN CKS GOOD. 2 L 7 3 4F RT A22WE 2002060500137 20020605 00137 2002 6 5 HEEA079234 4 20020524 A 3425 1113025 INDICATOR BELL 412 412 1182202 SW HSI MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893L 33006 HSI INDICATOR VOR NEEDLES WILL NOT POINT TO STATIONS. 1 G 7 2 4U H4SW 2002060500139 20020605 00139 NM 2002 6 5 DLM88020503 1 20020505 A 2150 20495062 ACM DOUG MD88 MD88 3023688 NM A/C BAY DAMAGED A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 960DL 49979 ATB - SMOKE IN AFT CABIN ON CLIMB, AFT LAV SMOKE DETECTORS SOUNDED, WHITE SMOKE, ELECTRICAL SMELL, STARTED 5 ROWS FWD OF MID JUMPSEAT. DISSIPATED AT 3000 FT. WING/ENG A/I OFF CROSSFEEDS CLOSED, APU OFF. FOUND CHUNKS MISSING FROM ACM TURB INE BLADES AND OIL IN DUCTS AFT OF ACM. REPLACED ACM PER M/M. LEAK CHECKS AND OPS CHECKS OKAY. 2 L 7 2 4F RT A6WE 2002060500140 20020605 00140 2002 6 5 HEEA079236 4 20020524 A 3425 1113025 INDICATOR BELL 412 412 1182202 SW HSI FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 HSI INDICATOR POPS CIRCUIT BREAKER. 1 G 7 2 4U H4SW 2002060500141 20020605 00141 NM 2002 6 5 DLM88020550 1 20020514 A 3397 WIRE DOUG MD88 MD88 3023688 NM AIRSTAIRS BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 915DL 49546 FOUND BROKEN WIRE ON EMERGENCY LIGHT IN AIRSTAIR AREA. REPAIRED SAME. 2 L 7 2 4F RT A6WE 2002060500142 20020605 00142 2002 6 5 HEEA079237 4 20020524 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW ATTITUDE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22608 33075 ATTITUDE INDICATOR WILL NOT TURN ON BOTH AXIS. 1 G 7 2 4U H4SW 2002060500143 20020605 00143 NM 2002 6 5 DLM88020551 1 20020514 A 3350 276005 FUSE DOUG MD88 MD88 3023688 NM CABIN BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 996DL 53363 FOUND F/C AND ROWS 10 AND 11 EMERGENCY LIGHTS INOP. REPLACED FUSE IN FWD EMERGENCY LIGHT BATTERY CRADLE. CHECKS NORMAL . 2 L 7 2 4F RT A6WE 2002060500144 20020605 00144 2002 6 5 HEEA079238 4 20020524 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW ATTITUDE DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 142PH 33150 ATTITUDE INDICATOR FLAG STICKS AND WON'T COME OUT WHEN POWER IS OFF. 1 G 7 2 4U H4SW 2002060500145 20020605 00145 NM 2002 6 5 DLM88020552 1 20020515 A 5330 5920323249 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 THE AFT C1 DOOR JAMB SKIN AND DOUBLER WERE FOUND CRACKED AT FS 427, L23R. DAMAGE WAS CUT OUT AND REPAIRED PER ERA 41303 5-14. 2 L 7 2 4F RT A6WE 2002060500147 20020605 00147 NM 2002 6 5 DLM88020553 1 20020515 A 5321 9952517176 FLOOR PANEL DOUG MD88 MD88 3023688 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 99525-71, -76 FLOOR PANELS WERE FOUND DISBONDED AND CRACKED. REPAIR PER ER/A 417223-14. 2 L 7 2 4F RT A6WE 2002060500148 20020605 00148 NM 2002 6 5 DLM88020554 1 20020506 A 5321 9952521127 FLOOR PANEL DOUG MD88 MD88 3023688 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 956DL 49887 FLOOR PANELS WERE FOUND DELAMINATED AND CRACKED. REPAIR PER ER/A 411194-14. 2 L 7 2 4F RT A6WE 2002060500149 20020605 00149 2002 6 5 HEEA079240 4 20020524 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW ATTITUDE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 ATTITUDE INDICATOR PITCH AND ROLL COMMAND BARS REMAIN IN VIEW, CAUSES AFCS LIGHT TO COME ON INTERMITTENTLY. 1 G 7 2 4U H4SW 2002060500150 20020605 00150 2002 6 5 HEEA079241 4 20020524 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW ATTITUDE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1202T 33112 CAUSES ERRATIC FEEDBACK TO FLIGHT DIRECTOR IN ROLL MODE. 1 G 7 2 4U H4SW 2002060500152 20020605 00152 SW 2002 6 5 HEEA079243 1 20020524 A 2437 124039 AMMETER BELL 412 412 1182202 SW COCKPIT STUCK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 DUAL AMMETER NEEDLE STICKS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060500153 20020605 00153 NM 2002 6 5 DLM88020560 1 20020517 A 2421 GENERATOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RT ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 938DL 20505 49811 726865 DIVERSION, RT A/C SYSTEM BUS FAILURE. COULD NOT PWR FROM OTHER SOURCES. FOUND DISTURB FAULT ON GCU AND CROSSTIE LOCKOU T ON EOAP INSP GEN FEEDER CABLES FROM GEN TO TAIL SECTION, CKS OK. MEGGED GEN CABLES, CKS OK. REMOVED AND REPLACED NR 2 CTS, 3 EACH AND GEN AND GCU PER MM RAN ENG CKS OK. 2 L 7 2 4F 4 F RT A6WE E9NE 2002060500154 20020605 00154 SW 2002 6 5 HEEA079244 1 20020524 A 2437 1240393 AMMETER BELL 412 412 1182202 SW COCKPIT STUCK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 NR 2 AMMETER STICKS. 1 G 7 2 4U H4SW 2002060500155 20020605 00155 NM 2002 6 5 DLM88020564 1 20020517 A 2170 COALESCER BAG DOUG MD88 MD88 3023688 NM A/C BAY DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 920DE 53423 SMELLED SMOKE AT 28K CRZ FOLLOWED BY AFT LAV SMOKE DETECTORS AND VISIBLE SMOKE AROUND CEILING OF CABIN. WITHIN 3 MINUTE S SMOKE HAD DISSIPATED. INSP ACM AND ENG, NTF. PERFORMED DUCT BURNOUT AND REPLACED COALESCOR BAGS. RAN ENGINES, CKS G OOD. 2 L 7 2 4F RT A6WE 2002060500156 20020605 00156 NM 2002 6 5 DLM90020499 1 20020502 A 3397 WIRE DOUG MD90 MD9030 3023690 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 916DN 53396 EMERGENCY FLOOR TRACK LIGHTS FROM BEHIND SEAT 38 TO AFT OF SEAT 39 INTERMITTENT WHEN TRACK IS TOUCHED. FOUND BROKEN WIR E, ALSO SECTION OF TRACK IS NOT SECURE. REPAIRED BROKEN WIRE AND SECURED TRACK 2 L 7 2 4F RT A6WE 2002060500157 20020605 00157 SW 2002 6 5 HEEA079245 1 20020524 A 2931 124043 INDICATOR BELL 412 412 1182202 SW HYD PRESS TEMP READS HIGH E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893L 33006 HYDRAULIC PRESSURE TEMPERATURE INDICATOR READS APPROX. 15 DEGREES HIGH. 1 G 7 2 4U H4SW 2002060500158 20020605 00158 SW 2002 6 5 HEEA079246 1 20020524 A 2931 124043 INDICATOR BELL 212 212 1181420 SW HYD PRESS TEMP STUCK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5736D 31135 HYDRAULIC PRESSURE TEMPERATURE INDICATOR NEEDLE STICKING ON HIGH SIDE. REPLACED WITH SERVICEABLE PART. 1 G 7 1 4U H4SW 2002060500159 20020605 00159 NM 2002 6 5 DLM90020507 1 20020506 A 3350 081691 SOCKET DOUG MD90 MD9030 3023690 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 913DN 53393 ON PREFLIGHT FOUND EMERGENCY LIGHT TRACK SECTION INOP FROM ROW 12 THROUGH ROW 22. FOUND EMERGENCY LIGHT ASSY BAD AT ROW S 14 & 16. REPLACED SAME. NOW CKS NORMAL. 2 L 7 2 4F RT A6WE 2002060500160 20020605 00160 NM 2002 6 5 DLM90020524 1 20020509 A 1420 TERMINAL DOUG MD90 MD9030 3023690 NM CABIN LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 916DN 53396 CEILING EMERGENCY LIGHT L2-781 IN NR 12 CEILING PNL INOP. FOUND LOOSE WIRE ON GROUND TERMINAL. SPLICED NEW TERMINAL EN D ON TO GROUND. LIGHT OPS NORMAL. 2 L 7 2 4F RT A6WE 2002060500161 20020605 00161 SW 2002 6 5 HEEA079247 1 20020524 A 2844 124044 INDICATOR BELL 412 412 1182202 SW FUEL PRESSURE FLUCTUATES E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893N 33010 FUEL PRESSURE INDICATOR FLUCTUATES 15 TO 20 PSI WITH JUST INVERTERS ON WITH PRESSURE TO SYSTEM. 1 G 7 2 4U H4SW 2002060500162 20020605 00162 SW 2002 6 5 HEEA079248 1 20020524 A 7931 13800040 TRANSDUCER BELL 412 412 1182202 SW OIL PRESSURE IND ERRATIC E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893L 33006 OIL PRESSURE INDICATOR TRANSDUCER ERRATIC. SCRAPPED. 1 G 7 2 4U H4SW 2002060500163 20020605 00163 2002 6 5 HEEA079249 4 20020524 A 3457 13824120234 GPS BELL 407 407 1182206 SW COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 612PH 53199 BACKUP BATTERY FAIL CODE AND HAS TO WIGGLE ON BUTTON. 1 G 7 1 3U O H2SW 2002060500164 20020605 00164 2002 6 5 HEEA079250 4 20020524 A 3457 13824120234 GPS BELL 206 206L3 1182108 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 54641 51184 GPS REQUIRED CODE EVERY TIME TURNED ON. PERFORMED PRELIMINARY INSPECTION. DISABLED SAFEGUARD CODE. FOUND NAV SWITCH, R F CONNECTOR AND BUTTONS BAD. REPLACED. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 2002060500165 20020605 00165 2002 6 5 HEEA079251 4 20020524 A 3457 13824120234 GPS BELL 206 206L3 1182108 SW COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 42EA 51542 GPS CONTROL BUTTON STICKS. 1 G 7 1 3U H2SW 2002060500166 20020605 00166 NM 2002 6 5 DLM90020541 1 20020513 A 5310 995301630 SHEAR TIE DOUG MD90 MD9030 3023690 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 FRAME CLIP FOUND CRACKED DURING HMV-1 AND WAS BEING REPLACED. BHEC INSPECT REVEALED A CRACK INDICATION. 2 L 7 2 4F RT A6WE 2002060500168 20020605 00168 NE 2002 6 5 HEEA079253 2 20020516 A 7321 0164248850 FUEL CONTROL SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 854PH 3248 FCU HAS CORROSION ON SURFACE. 1 G 7 1 3U 3 U H9EU E19EU 2002060500169 20020605 00169 GL 2002 6 5 EGIA1 2 20020520 A 7230 23005250 COMPRESSOR BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL ENGINE SEIZED E EGIA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 5007F 45186 890561 WHEN PILOT ATTEMPTED TO START ENGINE, STARTER WOULD NOT ROTATE COMPRESSOR. AFTER TROUBLESHOOTING START SYSTEM, DISCOVER ED COMPRESSOR SEIZED. COMPRESSOR SECTION WAS REMOVED AND STILL COULD NOT BE ROTATED BY HAND. NO OIL CONTAMINATION IN O IL SYSTEM SUGGESTING BEARING FAILURE. AXIAL COMPRESSOR DOES NOT APPEAR TO HAVE SHIFTED. ENGINE SENT TO MANUFACTURER RE PAIR FACILITY FOR INVESTIGATION. 1 G 7 1 3U 3 U H2SW E1GL 2002060500170 20020605 00170 EU 2002 6 5 HEEA079254 1 20020516 A 6220 117775P STARFLEX SNIAS 350 AS350B 8680801 EU M/R HEAD WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 856PH 3352 MAIN ROTOR HEAD STARFLEX BALL ENDS HAS WORN TEFLON. 1 G 7 1 3U H9EU 2002060500173 20020605 00173 EU 2002 6 5 HEEA079258 1 20020516 A 5210 350A2513500701 LOCK SNIAS 350 AS350B2 8680813 EU PAX DOOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 40466 3004 LT PASSENGER DOOR CENTER LOCK ASSY SHEARED PIN. 1 G 7 1 3U H9EU 2002060500176 20020605 00176 EU 2002 6 5 HEEA079259 1 20020516 A 6210 350A31177000 PIN SNIAS 350 AS350B 8680801 EU M/R BLADE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 856PH 3352 MAIN ROTOR BLADE PIN CORRODED. 1 G 7 1 3U H9EU 2002060500178 20020605 00178 EU 2002 6 5 HEEA079260 1 20020516 A 6220 350A31190703 STARFLEX SNIAS 350 AS350B 8680801 EU MAIN ROTOR HEAD CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 854PH 3248 STARFLEX CRACKED IN LEADING EDGE OF YELLOW ARM. 1 G 7 1 3U H9EU 2002060500180 20020605 00180 EU 2002 6 5 HEEA079261 1 20020516 A 6220 350A31191600 STARFLEX SNIAS 350 AS350B 8680801 EU MAIN ROTOR HEAD UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 971AE 430 3230 MAIN ROTOR HEAD STARFLEX BUSHING ON STAR ARM UNBONDED. 1 G 7 1 3U H9EU 2002060500181 20020605 00181 EU 2002 6 5 HEEA079262 1 20020516 A 6720 350A33214501 ROD SNIAS 350 AS350B 8680801 EU PITCH CONTROL DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 975AE 2777 TAIL ROTOR PITCH CONTROL ROD ELASTOMERIC DETERIORATED. 1 G 7 1 3U H9EU 2002060500184 20020605 00184 EU 2002 6 5 HEEA079263 1 20020516 A 2913 SPRING SNIAS 350 AS350B 8680801 EU PUMP COUPLING DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 856PH 3248 3352 HYDRAULIC PUMP DRIVE COUPLING SPRING SPLIT. 1 G 7 1 3U H9EU 2002060500188 20020605 00188 EU 2002 6 5 HEEA079265 1 20020516 A 2913 SPRING SNIAS 350 AS350B 8680801 EU PUMP COUPLING SPLIT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 855PH 3352 3351 HYDRAULIC PUMP COUPLING SPRING SPLIT. 1 G 7 1 3U H9EU 2002060500190 20020605 00190 EU 2002 6 5 HEEA079267 1 20020516 A 6220 350A37124420 SCREW SNIAS 350 AS350B 8680801 EU MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 856PH 3352 SCREW CORRODED, COATINGS WORN THROUGH. 1 G 7 1 3U H9EU 2002060500191 20020605 00191 EU 2002 6 5 HEEA079270 1 20020516 A 5210 355A08413338 PANEL SNIAS 350 AS350B 8680801 EU PAX DOOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 973AE 3229 DOOR PANEL CRACKED. SCRAPPED. 1 G 7 1 3U H9EU 2002060500192 20020605 00192 2002 6 5 HEEA079271 4 20020516 A 3421 504001790116 INDICATOR SNIAS 350 AS350B2 8680813 EU HORIZON GYRO ERRATIC E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 40466 3004 HORIZONTAL GYRO INDICATOR ERRATIC. REPLACED WITH SERVICEABLE INDICATOR. 1 G 7 1 3U H9EU 2002060500195 20020605 00195 EU 2002 6 5 HEEA079273 1 20020516 A 8000 845UN01Q4AA5F SWITCH SNIAS 350 AS350B 8680801 EU COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 970AE 3235 FAILURE DETECTED ON ENGINE SHUTDOWN. FAULT CODE POINTED TO A FAULTY OFF/IDLE/RUN SWITCH. REPLACED WITH SERVICEABLE SWIT CH. 1 G 7 1 3U H9EU 2002060500196 20020605 00196 NM 2002 6 5 F3LA200200150 1 20020517 A 5320 FLOOR SUPPORT BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 316FL 3574 25264 DURING C-2 CHECK, INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORTS, STA 771 - 857, RBL 8, L BL 7, RBL 3, LBL 3. REPLACED CORRODED SECTION PER SRM 53-00-53, FIG 201, DETAIL 1. 2 L 7 2 4F RT A16WE 2002060500198 20020605 00198 EU 2002 6 5 HEEA079275 1 20020516 A 2810 ER271 FUEL CAP SNIAS 350 AS350B2 8680813 EU FUEL CELL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 40466 3004 FUEL CELL CAP LEAKS WHEN FUEL TANK IS FULL. SCRAPPED. 1 G 7 1 3U H9EU 2002060500200 20020605 00200 NM 2002 6 5 F3LA200200151 1 20020519 A 5347 CARGO TRACK BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 316FL 3574 25264 DURING C-2 CHECK, INSPECTION REPORTED CARGO TRACK AT STA 940 TO 947, LBL 17, CORRODED. REPLACED FLOOR TRACK PER SRM 51- 40-02. 2 L 7 2 4F RT A16WE 2002060500201 20020605 00201 EU 2002 6 5 HEEA079279 1 20020516 A 7110 TL100AXE12L50 LATCH SNIAS 350 AS350B2 8680813 EU COWLING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 40466 3004 COWLING LATCH WORN. SCRAPPED. 1 G 7 1 3U H9EU 2002060500204 20020605 00204 2002 6 5 HEEA079280 4 20020516 A 3421 504001790116 INDICATOR BOLKMS 105 BO105S 5626006 EU HORIZON GYRO INACCURATE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 86CH S557 HORIZON GYRO INDICATOR SHOWS 5 DEGREES LEFT BANK AND SOMETIMES 10 DEGREES NOSE DOWN IN LEVEL FLIGHT. REPLACED WITH SERVI CEABLE PART. 1 G 7 2 3U H3EU 2002061900097 20020619 00097 CE 2002 6 19 GLBA2002060 1 20020509 A 3610 TUBE BEECH 1900 1900D 1154162 CE WING DAMAGED A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 153GL UE153 LEFT BLEED-AIR FAILURE. REPAIRED DAMAGED ENA TUBING AT WING, OPS GOOD. 2 L 7 2 4T RT A24CE 2002060500206 20020605 00206 EU 2002 6 5 HEEA079281 1 20020516 A 3340 A7151 LIGHT BOLKMS 105 BO105S 5626006 EU LANDING LIGHT BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8197X S808 FIXED LANDING LIGHT BROKEN OFF ON COPILOT SIDE. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 2002060500207 20020605 00207 CE 2002 6 5 GLBA2002062 1 20020517 A 7110 LATCH BEECH 1900 1900D 1154162 CE RT COWLING UNSECURE A GLBA A UNSCHED LANDING O OTHER TO TAKEOFF 1 NM 03 118GL UE118 RIGHT ENGINE COWL LATCH OPENED ON T/O. RESECURED, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2002061900100 20020619 00100 CE 2002 6 19 GLBA2002063 1 20020517 A 2130 1143810035 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE A/C BAY FAILED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 226GL UE226 LEFT ENVIRONMENTAL FAILURE ON T/O. REPLACED PRESSURE SWITCH. 2 L 7 2 4T RT A24CE 2002060500208 20020605 00208 EU 2002 6 5 HEEA079284 1 20020521 A 6220 1053172902 BUSHING BOLKMS 105 BO105S 5626006 EU MAIN ROTOR HEAD CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 PITTED CORROSION ON MAIN ROTOR HEAD BUSHING FLANGES. 1 G 7 2 3U H3EU 2002060500209 20020605 00209 CE 2002 6 5 GLBA2002064 1 20020519 A 5220 DOOR BEECH 1900 1900D 1154162 CE EMERGENCY EXIT OUT OF RIG A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 100UX UE100 EMERGENCY EXIT HANDLE NEEDED CHECK. RIGGED DOOR, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2002061900101 20020619 00101 CE 2002 6 19 GLBA2002066 1 20020520 A 1430 SCREW BEECH 1900 1900D 1154162 CE CLOSET LOOSE A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 260GL UE260 PAX DOOR MAKING A POPPING SOUND WHEN PRESSURIZING. TIGHTENED CLOSET SCREWS, TEST FLIGHT SATISFACTORY. 2 L 7 2 4T RT A24CE 2002060500210 20020605 00210 NE 2002 6 5 HEEA079285 2 20020521 A 7220 350A58160703 INLET SCREEN SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 40466 3004 ENGINE INLET SCREEN HAS BROKEN STRANDS. 1 G 7 1 3U 3 U H9EU E19EU 2002060500211 20020605 00211 CE 2002 6 5 GLBA2002067 1 20020429 A 1430 RIVET BEECH 1900 1900D 1154162 CE RUDDER SYS SHEARED A GLBA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 03 100UX UE100 PILOT REPORTED THAT RUDDER PEDAL WAS VERY DIFFICULT TO ADJUST. INSPECTION FOUND THE TORQUE TUBE BEARING HOLDER OUTBOARD SIDE HAD ALL BUT ONE RIVET FASTENER SHEARED (3EA). REPLACED RIVETS AND RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2002060500212 20020605 00212 GL 2002 6 5 HEEA079286 2 20020523 A 7532 23053176 BLEED VALVE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8199J 9900 S826 FAILED BLEED VALVE ALLOWING ENGINE TO PRODUCE HIGH TOT. 1 G 7 2 3U 3 U H3EU E4CE 2002060500213 20020605 00213 2002 6 5 HEEA079287 4 20020524 A 3457 13824120234 GPS SNIAS 350 AS350B2 8680813 EU COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 40466 3004 CANNOT ENTER WAYPOINT, LARGE KNOB WON'T GO OVER 2ND POSITION. 1 G 7 1 3U H9EU 2002060500214 20020605 00214 SO 2002 6 5 LR7A02037 1 20020523 A 2170 18084942 COALESCER BAG LKHEED 382 382G 526414U SO A/C BAY DIRTY A LR7A K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 401LC 37 4606 FLIGHT CREW REPORTED FLIGHT DECK AIR CONDITIONING PACK HAS STRONG OIL SMELL WHEN HEAT IS CALLED FOR. REPLACED WATER SEP ARATOR CONDENSER SOCK IAW SMP 581 21-50 PG 222. 2 H 7 4 4T A1SO 2002060500215 20020605 00215 EU 2002 6 5 HEEA079288 1 20020524 A 6410 355A12004008 BLADE SNIAS 350 AS350B 8680801 EU TAIL ROTOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 974AE 1729 2653 TAIL ROTOR BLADES HAVE SEVERAL CRACKS IN THE PAINT ON TOP OF TRAILING EDGE TAB. 1 G 7 1 3U H9EU 2002061000108 20020610 00108 SO 2002 6 10 LR7A02038 1 20020528 A 2150 20343041 ACM LKHEED 382 382G 526414U SO A/C BAY FAILED A LR7A K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 401LC 334 4606 FLIGHT CREW REPORTED FLIGHT DECK AIR CONDITIONING PACK HAS A NASTY OILY SMELL. REPLACED FLIGHT STATION COOLING TURBINE IAW SMP 581 21-50-12, OPS CHECKS NORMAL PER PAGE 201 - 204. 2 H 7 4 4T A1SO 2002060500216 20020605 00216 EU 2002 6 5 HEEA079289 1 20020524 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU MAIN ROTOR ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4573B 7109 S673 THE OUTBOARD ABRASION STRIP ON MAIN ROTOR BLADE HAS EROSION HOLE. 1 G 7 2 3U H3EU 2002060500217 20020605 00217 EU 2002 6 5 HEEA079290 1 20020524 A 6210 10581013 BLADE BOLKMS 105 BO105S 5626006 EU MAIN ROTOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 12054 S828 THE NOSE AND NECK SHELL HAS A CRACK NEAR THE BUTT PLATE ON MAIN ROTOR BLADE. 1 G 7 2 3U H3EU 2002060500218 20020605 00218 EU 2002 6 5 MALA020283 1 20020503 A 5320 SUPPORT BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 514XJ E2330 DURING C-CHECK IN CVG, FOUND CORROSION ON FRAME 20 SUPPORT PLATE UPPER SURFACE BETWEEN SEAT TRACK NR 3 AND 4, ALSO FOUND CORROSION ON FRAME 20 SUPPORT PLATED INBOARD OF FRAME NR 3. MAINTENANCE REPLACED FRAME 20 UPPER SURFACE PLATE WITH FAB RICATED PART IAW SRM 51-42-00, 51-43-00. 2 H 7 4 4F RT A49EU 2002060500219 20020605 00219 EU 2002 6 5 HEEA079291 1 20020524 A 6210 117150071 BLADE BOLKMS 117 BK117B1 5626012 EU MAIN ROTOR ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 4462 7092 THE LEADING EDGE ABRASION STRIP HAS EROSION HOLES NEAR THE TIP OF MAIN ROTOR BLADE. 1 G 7 2 3U H13EU 2002060500220 20020605 00220 EU 2002 6 5 HEEA079292 1 20020524 A 6210 117150071 BLADE BOLKMS 117 BK117B1 5626012 EU MAIN ROTOR ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 4462 7092 THE LEADING EDGE ABRASION STRIP HAS EROSION HOLES NEAR THE TIP OF MAIN ROTOR BLADE. 1 G 7 2 3U H13EU 2002060500221 20020605 00221 2002 6 5 HEEA079293 4 20020524 A 3457 13824120234 GPS BOLKMS 105 BO105S 5626006 EU COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 81992 S827 GPS RECEIVER RANDOMLY SKIPS WAYPOINTS WHEN THE WPT BUTTON IS DEPRESSED. PERFORMED PRELIMINARY INSPECTION. REPLACED "WPT" , "NAV", "MSG" SWITCHES. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 2002060500222 20020605 00222 EU 2002 6 5 MALA020286 1 20020514 A 2120 PANEL SAAB SF340 340B 7860101 EU COCKPIT LOOSE A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 368XJ DURING CLIMBOUT ON FLIGHT 3093, WHILE BRINGING PROPS TO 1270, IT APPEARS THE PROPS WOULD NOT SYNC. ADJUSTED PROP RPM AN D WHOP SOUND REMAINED. REDUCED TORQUE 20 PERCENT ON TIGHT ENGINE AND THEN LEFT, WHICH DID NOT CORRECT. ALL PROP AND EN GINE INDICATIONS APPEARED NORMAL. CONTROLS ALSO NORMAL. AIR TURNBACK TO MSP. MAINTENANCE NOTED NOISE THRUMMING SOUND VERIFIED DURING INITIAL GROUND RUN. FOUND VENT PANEL LOOSE ON BULKHEAD BEHIND CAPT SEAT. TIGHTENED PANEL, NO VIBRATION S NOTED WITH LP OR HP AIR SELECTED. 2 L 7 2 4T RT A52EU 2002060500223 20020605 00223 EU 2002 6 5 MALA020287 1 20020516 A 3020 44730501 CONTROLLER SAAB SF340 340B 7860101 EU DE-ICE SYSTEM FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 442XJ 340B442 DURING FLIGHT 3116, LT INTAKE HEAT INOP. AIR TURNBACK TO DTW. MAINTENANCE OHMED OUT INTAKE, UPPER DUCT, EXHAUST NOZZLE , BIR CATCH ALL CHECKS GOOD. SUSPECT BAD DE-ICE CONTROL. MAINTENANCE REPLACED DE-ICE CONTROL, GROUND RUN A/C FOR 30 MI NUTES ALL WORK DONE IAW SAAB 340 MM, ALL CHECKS GO. 2 L 7 2 4T RT A52EU 2002060500224 20020605 00224 EU 2002 6 5 MALA020290 1 20020519 A 2150 MOTOR SAAB SF340 340B 7860101 EU A/C SYSTEM FAILED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 414XJ 340B414 A/C ON AIRCRAFT WAS SMOKING AND PRODUCED SMOKE IN CABIN. NO PAX ON BOARD WHEN INCIDENT OCCURRED. MAINTENANCE REMOVED A ND REPLACED COMPRESSOR MOTOR, OPS CHECKED GOOD. 2 L 7 2 4T RT A52EU 2002060500225 20020605 00225 EU 2002 6 5 MALA020291 1 20020508 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K-CHECK IN CWA, RT FUSELAGE HAS A DENT STA 341 THAT IS 1.625 INCH ABOVE SL1622. MAINTENANCE REPAIRED DENT IAW E O 53122. 2 L 7 2 4T RT A52EU 2002060500226 20020605 00226 EU 2002 6 5 MALA020292 1 20020512 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K-CHECK IN CWA, FOUND CORROSION OUT OF SAAB SRM LIMITS ON LT CENTER AISLE SEAT TRACK LBL 18.3, FWD PORTION. MAI NTENANCE COMPLETED REPAIR FROM STA 297 TO 372 IAW EO 53060. 2 L 7 2 4T RT A52EU 2002060500227 20020605 00227 EU 2002 6 5 MALA020293 1 20020508 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K-CHECK IN CWA, FRAME ANGLE AT STA 225 BL 0 HAS CORROSION. MAINTENANCE REPAIRED IAW EO 53108. 2 L 7 2 4T RT A52EU 2002060500228 20020605 00228 EU 2002 6 5 MALA020294 1 20020508 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K-CHECK IN CWA, FRAME ANGLE AT STA 258 (TOP) HAS CORROSION. MAINTENANCE COMPLETED REPAIR FROM LBL 10 TO RBL 10 IAW EO 53108. 2 L 7 2 4T RT A52EU 2002060500229 20020605 00229 NM 2002 6 5 02152415 1 20020601 A 5610 WARNING SYSTEM DORNER DO32 DO328300 NM COCKPIT ACTIVATED A VTZA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 27 415FJ 3170 DURING CLIMB FROM JFK AND AGAIN DURING DESCENT TO BOS BELOW 100,000 FEET AGL, THE CREW NOTED AN ELECTRICAL BURNING ODOR IN THE COCKPIT. NO VISIBLE SMOKE WAS OBSERVED. DURING THE CLIMB A BLUE CAS MAINTENANCE MESSAGE ILLUMINATED REFERRING T O THE RT FWD WINDSHIELD. AT BOS, MAINTENANCE PERSONNEL PERFORMED OPERATIONAL CHECKS OF THE WINDSHIELD HEAT SYSTEM. NO DEFECTS OR FAULTS WERE NOTED AND NO SMELL WAS DETECTED. THE CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO S ERVICE. 2 H 7 2 4T RT A55NM 2002060500230 20020605 00230 NM 2002 6 5 02153414 1 20020602 A 2120 ODOR DORNER DO32 DO328300 NM COCKPIT DETECTED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 414FJ 3169 DURING CRUISE OF THE FLIGHT FROM CVG TO CAE, THE CREW REPORTED THE SMELL OF SMOKE IN THE COCKPIT. THE FLIGHT WAS DIVERT ED TO TRI WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL RESPONDED FROM CAE TO TRI. SYSTEM INSPECTI ONS AND OPERATIONAL CHECKS WERE SATISFACTORILY PERFORMED WITH NO EVIDENCE OF OVERHEATING OR SMOKE. THE AIRCRAFT WAS RET URNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002060500231 20020605 00231 NM 2002 6 5 02FDEA00370 1 20020531 A 3610 DUCT BOEING 727 727200 138407E NM PNEUMATIC SYS LEAKING A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 234FE 21328 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AFTER 1+10 FLIGHT TIME. DID RED TAB PROCEDURE. ISOLATED LEAK ON NR 3 ENG BE TWEEN BLEED VALVE AND RIGHT PACK VALVE. FOUND STARTER DUCT LEAKING ON NR 3 ENG BLEED MANIFOLD. STARTER DUCT WAS MISALI GNED, REALIGNED STARTER DUCT TO BLEED ENG MANIFOLD & TIGHTENED CLAMPS. OPS CK NORMAL REF PER MM 36-10-000-1. 2 L 7 3 4F RT A3WE 2002060500233 20020605 00233 NM 2002 6 5 02FDEA00373 1 20020601 A 3620 20035012007 CONTROLLER DOUG MD11 MD11 3023602 NM PNEUMATIC SYS MALFUNCTIONED A FDEA K NONE N FALSE WARNING CR CRUISE 1 SO 25 578FE 48458 IN CRUISE FL 290 ALL ANTI ICE ON, RECEIVED LEVEL 1 ALERT AIR MANIF 2 FAIL. BROUGHT NR 2 THROTTLE TO IDLE AND COMPLIED W ITH RED TABS IN QRH. ALERT WENT AWAY. LEFT THROTTLE 2 AT IDLE FOR REMAIN OF FLIGHT. AC RELEASED FOR SERVICE PER MEL/C DL. REPLACED 15A AND 15B LOOPS. LOOPS HAVE SHORT CIRCUIT. REPLACED THE MFC DUE TO TERMINATION OF COMMUNICATION WITH C OMP OCCURRED SEVERAL TIMES. PERFORMED DECAY CHECK WITH MD11 JRH, IT TOOK 27 SEC NR 2 MANI PRESS FROM 25 PSI TO 15 PSI, TEST WAS PASSED. 2 L 7 3 4F RT A22WE 2002060500234 20020605 00234 NM 2002 6 5 02FDEA00374 1 20020601 A 5610 NBA6045502 WINDSHIELD DOUG MD11 MD11 3023602 NM COCKPIT CRACKED A FDEA O OTHER A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 25 608FE 48548 PRIOR TO PUSHBACK F/O WINDSHIELD CRACKED AND CAUGHT ON FIRE. FOUND F/O WINDSHIELD DAMAGED FROM OVERHEAT CONDITION IMMEDI ATELY AFTER CREW REPORTED FIRE IN THE COCKPIT. REMOVED AND REPLACED WINDSHIELD ANTI-ICE CONTROLLER AND WINDSHIELD. 2 L 7 3 4F RT A22WE 2002071900088 20020719 00088 NM 2002 7 19 02FDEA00375 1 20020529 A 7830 FITTING DOUG MD11 MD11 3023602 NM THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 NR 2 ENG LT T/R COWL UPPER TRANSLATING SLEEVE CHANNEL END FOUND CRACK. HFEC CARRIED OUT CRACK LENGTH APPROX .625 INCH L ONG. R&R COWL & INSTALLED FITTING AT UPPER TRACK BEAM. 2 L 7 3 4F RT A22WE 2002071900089 20020719 00089 NM 2002 7 19 02FDEA00376 1 20020530 A 1430 BOLT DOUG MD11 MD11 3023602 NM NR 3 PYLON SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 NR 3 PYLON FWD WING TO PYLON ATTACHMENT BULKHEAD FOUND 2 EA BOLT SHEARED BELOW LOWER BEARING. R&R WING PER EA 1-5450-62 179. 2 L 7 3 4F RT A22WE 2002060500235 20020605 00235 NM 2002 6 5 2002F00528 1 20020424 A 5754 FORMER BOEING 727 727225 1384077 NM L/E FLAP CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CRACK ON RIGHT WING NR 5 KRUEGER FLAP, OUTBOARD INNER FORMER. (M) 2 L 7 3 4F A3WE 2002060500236 20020605 00236 NM 2002 6 5 2002F00529 1 20020514 A 5751 AILERON BOEING 727 727225 1384077 NM LT WING CHAFED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND LEFT OUTBOARD AILERON CHAFED, ON INBOARD END, AT STATION 492. (M) 2 L 7 3 4F A3WE 2002060500237 20020605 00237 WP 2002 6 5 2002F00530 1 20020512 A 5320 STRUCTURE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY, AT FLOORBOARDS TO SLOPED SIDE WALL SUPPORT ANGLE, LEFT SIDE, AT STATION 18 41 TO 1967. (M) 2 L 7 3 4F A22WE 2002060500238 20020605 00238 WP 2002 6 5 2002F00531 1 20020519 A 5320 STRUCTURE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON 'J' LEG, BETWEEN LONGERONS 48L AND 48R, AT STATION 1761. (M) 2 L 7 3 4F A22WE 2002060500240 20020605 00240 WP 2002 6 5 ARWA20020510 1 20020529 A 2760 WARNING SYSTEM DOUG DC8 DC861 3021952 WP COCKPIT MALFUNCTIONED A ARWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 29UA 46159 AT BEGINNING OF TAKEOFF, ROLL SPOILER EXTENDED, LIGHT ILLUMINATED. ABORTED TAKEOFF. PERFORMED VISUAL INSPECTION OF SPO ILERS DEPLOY SWITCHES AND MECHANISM; CLEANED CONNECTOR TO MICRO-SWITCH PERFORMED OPERATIONAL CHECK IAW MM 27-61-0 AND 27 -63-0. OPERATIONAL CHECK ON THE GROUND NORMAL. 2 L 7 4 4F 4A25 2002060500241 20020605 00241 NM 2002 6 5 ASAA0210066 1 20020322 A 5310 6546511 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 807, STRINGER 26R-27R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002060500242 20020605 00242 NM 2002 6 5 ASAA0210067 1 20020323 A 5310 65465545003 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BODY STATION 847, RBL 10 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002060500243 20020605 00243 NM 2002 6 5 ASAA0210068 1 20020323 A 5311 6546557 FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 887, STRINGER 19L-22L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002060500244 20020605 00244 NM 2002 6 5 ASAA0210069 1 20020323 A 5310 654659524 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 727A, STRINGER 24L-25L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002060500245 20020605 00245 NM 2002 6 5 ASAA0210070 1 20020324 A 5311 654655059 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 827, LBL 27 DENTED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002060500246 20020605 00246 NM 2002 6 5 ASAA0210073 1 20020325 A 5311 654655216 FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 787, LBL 24, LBL 34 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002060500247 20020605 00247 NM 2002 6 5 ASAA0210074 1 20020330 A 5314 65621252 KEELBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM AT BS 675-727, RBL 5 CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2002060500248 20020605 00248 NM 2002 6 5 ASAA0210075 1 20020330 A 5230 655469213 SKIN PANEL BOEING 737 737290C 138448V NM CARGO DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL ON CARGO DOOR AT BS 446, RBL 65 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002060500249 20020605 00249 NM 2002 6 5 ASAA0210076 1 20020330 A 3350 86210144 RECEIVER BOEING 737 7372Q8C 138448S NM CABIN INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 18 WOULD NOT EXTINGUISH. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002060500250 20020605 00250 NM 2002 6 5 ASAA0210079 1 20020408 A 5230 6547952 SKIN BOEING 737 737290C 138448V NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PAE - DURING SCHEDULED C-CHECK, FOUND INNER SKIN ON AFT CARGO DOOR DENTED AT BS 800, STRINGER 25R. REPAIRED DENT PER SR M. (M) 2 L 7 2 4F A16WE 2002060500251 20020605 00251 NM 2002 6 5 ASAA0210080 1 20020408 A 5754 6546422299A SLAT BOEING 737 737290C 138448V NM WING DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 22577 ANC - DURING SCHEDULED A-CHECK, FOUND NR 2 LEADING EDGE SLAT DELAMINATING AT WING BODY LINE 329.75. REPAIRED PER EA. ( M) 2 L 7 2 4F A16WE 2002060500252 20020605 00252 NM 2002 6 5 ASAA0210094 1 20020508 A 5311 6546548 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 747, STRINGER 22L-23L DENTED. REPAIRED DENT PER SRM. (M) 2 L 7 2 4F A16WE 2002060500253 20020605 00253 NM 2002 6 5 ASAA0210095 1 20020508 A 5313 6546595 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 27L, AT BS 727 PLUS 17 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002060500254 20020605 00254 NM 2002 6 5 ASAA0210096 1 20020508 A 5311 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 747, STRINGER 24R-25R DENTED. REPAIRED DENT PER SRM. (M) 2 L 7 2 4F A16WE 2002060500255 20020605 00255 NM 2002 6 5 ASAA0210098 1 20020509 A 5311 65C34356 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 500A, STRINGER 20R-24R DENTED. REPAIRED DENT PER SRM. (M) 2 L 7 2 4F A16WE 2002060500256 20020605 00256 NM 2002 6 5 ASAA0210099 1 20020509 A 5311 6546549 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 767, STRINGER 24R-25R DENTED. REPAIRED DENT PER SRM. (M) 2 L 7 2 4F A16WE 2002060500257 20020605 00257 NM 2002 6 5 ASAA0210100 1 20020509 A 5311 6546550 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 787, STRINGER 24R-25R DENTED. REPAIRED DENT PER SRM. (M) 2 L 7 2 4F A16WE 2002060500258 20020605 00258 NM 2002 6 5 ASAA0210101 1 20020509 A 5311 65C34357 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 500B, STRINGER 20R-24R DENTED. REPAIRED DENT PER SRM. (M) 2 L 7 2 4F A16WE 2002060500259 20020605 00259 NM 2002 6 5 ASAA0210102 1 20020510 A 5310 65465511 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 807, LBL 8 CORRODED. REPAIRED SHEAR TIE PER SRM. (M) 2 L 7 2 4F A16WE 2002060500260 20020605 00260 NM 2002 6 5 ASAA0210103 1 20020510 A 5310 65465511 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 807, LBL 8 CORRODED. REPAIRED SHEAR TIE PER SRM. (M) 2 L 7 2 4F A16WE 2002060500261 20020605 00261 NM 2002 6 5 ASAA0240034 1 20020322 A 5230 6549889 SKIN BOEING 737 7374Q8 138447Q NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 762AS 25099 PAE - DURING C-CHECK, FOUND FORWARD CARGO DOOR HAS NUMEROUS DENTS, AND PREVIOUS REPAIRS TO EXTERNAL SKIN. REMOVED AND R EPLACED SKIN IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060500262 20020605 00262 NM 2002 6 5 ASAA0240035 1 20020322 A 5311 6546560 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 762AS 25099 PAE - DURING C-CHECK, FOUND MECHANICAL DAMAGE ON FRAME IN AFT CARGO BAY UNDER RIGHT FLOOR TO SIDE WALL SUPPORT AT BS 947 , RBL 18, WL 175. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060500263 20020605 00263 NM 2002 6 5 ASAA0240036 1 20020402 A 5320 65479573 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 765AS 25102 PAE - DURING C-CHECK, FOUND AFT CARGO BAY SUB-THRESHOLD WEB IS CORRODED AT BS 793-847 AND RBL 20-28. REPAIR VIA REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060500264 20020605 00264 NM 2002 6 5 ASAA0240037 1 20020402 A 5330 6545768 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 765AS 25102 PAE - DURING C-CHECK, FOUND GOUGE ON OUTER SKIN AT STATION 369, 2 INCHES BELOW STRINGER 17L. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060500265 20020605 00265 NM 2002 6 5 ASAA0240038 1 20020402 A 5330 6545768 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 765AS 25102 PAE - DURING C-CHECK, FOUND GOUGE ON OUTER SKIN AT STATION 385, 4 INCHES BELOW STRINGER 17L. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060500266 20020605 00266 NM 2002 6 5 ASAA0240039 1 20020406 A 5522 65C25746141 SKIN BOEING 737 7374Q8 138447Q NM ELEVATOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 765AS 25102 PAE - DURING C-CHECK, FOUND AREA OF EXPOSED FIBER ON UPPER SKIN OF LEFT ELEVATOR UNDER TAB DRIVE ROD FAIRING OUTBOARD OF AFT FASTENER. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2002060500267 20020605 00267 NM 2002 6 5 ASAA0240040 1 20020406 A 5320 654795734 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 765AS 25102 PAE - DURING C-CHECK, FOUND CORROSION ON OUTBOARD C-CHANNEL IN AFT CARGO BAY THRESHOLD AT BS 794 TO 847, RBL 24 AND WL 1 50. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002060500268 20020605 00268 NM 2002 6 5 ASAA024043 1 20020413 A 3350 810022605 LIGHT BOEING 737 737490 1384715 NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 788AS 28885 SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS BROKEN AND DISCONNECTED AT ROW 16. REPLACED SECTION AND RECONNECTED W IRES. TRACK LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2002060500269 20020605 00269 NM 2002 6 5 AWXA200200476 1 20020506 A 5230 6546921 DOOR FRAME BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 YVR - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON THE FORWARD CARGO DOOR LOWER AFT FRAME AT THE OUTER RADIUS. MAINTENANCE REPAIRED THE FORWARD CARGO DOOR LOWER AFT FRAME AT OUTER RADUIS IAW EO 52-31-04. 2 L 7 2 4F RT A16WE 2002060500270 20020605 00270 NM 2002 6 5 AWXA200200479 1 20020511 A 5230 6547952170 CROSSBEAM BOEING 737 7373Q8 1384670 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 CHECK A .25 INCH CRACK WAS FOUND ON THE AFT CARGO DOOR LOWER FORWARD CROSS BEAM, LOWER ANGLE, 3RD FASTENER HOLE INBOARD. MAINTENANCE TRIMMED OUT T-CHORD FORWARD END OF CROSS BEAM; FABRICATED NEW SECTION OF T-CHORD AND DOUBLER, AND INSTALLED REPAIR PARTS IAW EO 52-33-02, PG 18-20. 2 L 7 2 4F RT A16WE 2002060500271 20020605 00271 NM 2002 6 5 AWXA200200481 1 20020515 A 5230 6546921 CROSSBEAM BOEING 737 737301 1384611 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON THE FORWARD CARGO DOOR LOWER BEAM WEB COMING OUT OF L OWER FASTENER HOLE RUNNING VERTICAL. HFEC CONFIRMED CRACK. MAINTENANCE REMOVED THE LOWER BEAM WEB AT CRACK COMING OUT OF FASTENER HOLE; FABRICATED FILLERS FOR WEB AND FLANGE; INSTALLED REPAIR PARTS IAW EO 52-31-04 FIG 4 PG 65. 2 L 7 2 4F RT A16WE 2002060500272 20020605 00272 NM 2002 6 5 AWXA200200482 1 20020516 A 5320 65677758 FITTING BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 MCN - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON FRAME END FITTING BS 616 RT, WL 202. MAINTENANCE REMOVED DA MAGED AREA OF FRAME FITTING AT BS 616 RT; PERFORMED HFEC INSPECTION TO VERIFY NO CRACK EXISTS; FABRICATED STIFFENING ANG LE AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2002060500273 20020605 00273 NM 2002 6 5 AWXA200200483 1 20020516 A 5320 65677757 FITTING BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 MCN - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON FRAME END FITTING BS 616 LT, WL 202. MAINTENANCE REMOVED DA MAGED AREA OF FRAME FITTING AT BS 616 LT; PERFORMED HFEC INSPECTION TO VERIFY NO CRACK EXISTS; FABRICATED STIFFENING ANG LE AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2002060500274 20020605 00274 NE 2002 6 5 HEEA079301 1 20020528 A 3212 7655202010105 HARNESS SKRSKY S76 S76A 8143006 NE EMERGENCY FLOAT CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 EMERGENCY FLOAT HARNESS CORRODED. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H1NE 2002060500275 20020605 00275 NM 2002 6 5 SWAA021200 1 20020531 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002060500276 20020605 00276 NM 2002 6 5 SWAA021201 1 20020530 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM AFT SVC DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2002060500277 20020605 00277 2002 6 5 SWAA021202 4 20020531 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD CABIN DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED C3 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PE R MM. 2 L 7 2 4F RT A16WE 2002060500278 20020605 00278 NM 2002 6 5 SWAA021203 1 20020530 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 418WN 29823 DURING SCHEDULED RON, FOUND EEPLS WOULD NOT EXTINGUISH IN MID CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002060500279 20020605 00279 2002 6 5 SWAA021204 4 20020529 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 774SW 27882 FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002060500280 20020605 00280 NM 2002 6 5 SWAA021209 1 20020531 A 2731 6959227 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, FOUND RT ELEVATOR TAB LOCK OUT FWD LINK BUSHING WORN. REMOVED AND REPL ACED LOCK OUT BUSHING PER MM. 2 L 7 2 4F RT A16WE 2002060500281 20020605 00281 NM 2002 6 5 SWAA021212 1 20020531 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 445, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002060500282 20020605 00282 NM 2002 6 5 SWAA021213 1 20020601 A 3230 1061226 SENSOR BOEING 737 7373H4 1384600 NM LT MLG OUT OF ADJUST A SWAA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 29 640SW 27713 AIR TURN BACK, THE LEFT MLG WOULD NOT RETRACT. ADJUSTED LEFT MLG UPLOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2002060500283 20020605 00283 2002 6 5 SWAA021215 4 20020601 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002060500284 20020605 00284 2002 6 5 SWAA021216 4 20020603 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002060500285 20020605 00285 2002 6 5 SWAA021217 4 20020603 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002060500286 20020605 00286 NM 2002 6 5 SWAA021220 1 20020603 A 3350 65C34691 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHTS LOOSE AT ROW'S 11ABC AND 15ABC. SECURED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2002060500287 20020605 00287 NM 2002 6 5 SWAA021222 1 20020602 A 2731 65C26384 TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEV ATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002060500288 20020605 00288 NM 2002 6 5 SWAA021224 1 20020602 A 5320 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED SERVICE CHECK, FOUND SHEAR TIE'S CRACKED (2 EA) BETWEEN STR'S 21R AND 22R AT BS'S 294.5 AND BS 277. RE PAIRED SHEAR TIE'S PER SRM. 2 L 7 2 4F RT A16WE 2002060500289 20020605 00289 NM 2002 6 5 SWAA021225 1 20020601 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND RBL 10.5. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002060500290 20020605 00290 NM 2002 6 5 SWAA021227 1 20020603 A 2731 65C26384 TAB BOEING 737 7373H4 1384600 NM RT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SERVICE CHECK, FOUND RT ELEVATOR TAB DELAMINATED ON T/E. REPAIRED RT ELEVATOR TAB PER SRM. 2 L 7 2 4F RT A16WE 2002060500291 20020605 00291 NM 2002 6 5 SWAA021164 1 20020528 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA ER. 2 L 7 2 4F RT A16WE 2002060500292 20020605 00292 NM 2002 6 5 SWAA021165 1 20020526 A 2731 BACB28AMO7 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, FOUND LT ELEVATOR TAB NR 2 AND NR 3 HINGES WORN. REMOVED AND REPLACED LEFT ELEVATOR TAB NR 2 AND NR 3 HINGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002060500293 20020605 00293 NM 2002 6 5 SWAA021166 1 20020526 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002060500294 20020605 00294 NM 2002 6 5 SWAA021167 1 20020526 A 3242 4271902 CONTROL UNIT BOEING 737 7373H4 1384600 NM E&E COMP ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 LT BRAKE FLUCTUATES AND RELEASES DURING BRAKING. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT PER MM. 2 L 7 2 4F RT A16WE 2002060500295 20020605 00295 2002 6 5 SWAA021168 4 20020527 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER M M. 2 L 7 2 4F RT A16WE 2002060500296 20020605 00296 NM 2002 6 5 SWAA021171 1 20020523 A 5320 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BELOW STR 14R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002060500297 20020605 00297 NM 2002 6 5 SWAA021173 1 20020526 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGERS CRACKED (2 EA) STR 13L BETWEEN BS 380 AND BS 400, AND BS 616, STR 4L. R EPAIRED STRINGERS PER CASCADE ERO. 2 L 7 2 4F RT A16WE 2002060500298 20020605 00298 NM 2002 6 5 SWAA021174 1 20020528 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 748SW 29800 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 11. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002060500299 20020605 00299 2002 6 5 SWAA021175 4 20020525 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002060500300 20020605 00300 NM 2002 6 5 SWAA021178 1 20020528 A 5753 6546435 FLAP BOEING 737 7375H4 138449D NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C4 CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OTBD AFT T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002060500301 20020605 00301 NM 2002 6 5 SWAA021179 1 20020529 A 2731 65C26384 TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVAT OR TAB PER MM. 2 L 7 2 4F RT A16WE 2002060500302 20020605 00302 NM 2002 6 5 SWAA021180 1 20020529 A 5311 6545765 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BETWEEN STR'S 20R AND 21R. REPAIRED FRAME PER SRM . 2 L 7 2 4F RT A16WE 2002060500303 20020605 00303 NM 2002 6 5 SWAA021181 1 20020529 A 2731 BACB28AM07 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED A1 CHECK, SWA SI 11111-55, FOUND RT ELEVATOR TAB NR 3 HINGE BUSHING WORN. REMOVED AND REPLACED NR 3 HI NGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2002060500304 20020605 00304 NM 2002 6 5 SWAA021182 1 20020528 A 5510 6573783 SKIN BOEING 737 7373H4 1384600 NM LT STABILIZER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED C4 CHECK, FOUND LT STABILIZER LOWER SKIN CRACKED AT FWD EDGE OF AFT SPAR. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002060500305 20020605 00305 NM 2002 6 5 SWAA021183 1 20020529 A 2731 6959227 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED A1 CHECK, SWA SI 11111-55, FOUND LT ELEVATOR TAB FWD LOCKOUT MECHANISM WORN. REMOVED AND REPLACED LOCK OUT MECHANISM FWD BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002060500306 20020605 00306 2002 6 5 SWAA021184 4 20020530 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 742SW 29278 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002060500307 20020605 00307 NM 2002 6 5 SWAA021185 1 20020529 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 724SW 27856 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROW'S 11 AND 21. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002060500308 20020605 00308 2002 6 5 SWAA021188 4 20020529 A 2565 65C16820 RETAINER BOEING 737 7372H4 138448C NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 103SW 23109 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE CASE RETAINER LOOSE. REMOVED AND REPLACED CASE RETAI NER PER MM. 2 L 7 2 4F A16WE 2002060500309 20020605 00309 2002 6 5 SWAA021195 4 20020529 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 724SW 27856 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002060500310 20020605 00310 NM 2002 6 5 SWAA021196 1 20020529 A 5312 6517583 WEB BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, WL 181.5 AND RBL 5.7. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002060500311 20020605 00311 NM 2002 6 5 SWAA021197 1 20020530 A 5313 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 787, STR 21R AND BS 727E, STR 25R. REMOVED A ND REPLACED TIE CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002060500312 20020605 00312 NM 2002 6 5 SWAA021198 1 20020530 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 102SW 23108 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 903, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002060500313 20020605 00313 NM 2002 6 5 VNAA0205020 1 20020514 A 6100 E62127 PROPELLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 423JS 14372 3421 3032 APPROXIMATELY SIX MILES FROM THE BAL VOR, THE CREW EXPERIENCED A FLASH AND LOUD BOOM. THE CREW ASSUMED THAT THE AIRCRAF T HAD BEEN STRUCK BY LIGHTNING. THE CREW DECLARED AN EMERGENCY AND LANDED WITH NO FURTHER INCIDENTS. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND PROPELLER IN ACCORDANCE WITH DORNIER MAINTENANCE M ANUAL 61-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002060500314 20020605 00314 2002 6 5 VNAA0205016 4 20020524 A 2200 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 3056 DURING TAKE OFF, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL CAS MESSAGE AND ABORTED TAKE OFF. THE AIRCRAFT RETUR NED TO THE GATE AND MAINTENANCE CONTROL DEFERRED THE FLIGHT GUIDANCE COMPUTER AND THE FLIGHT THEN CONTINUED ON TO RDU. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002060500315 20020605 00315 NE 2002 6 5 HEEA079302 1 20020528 A 3210 1945E235 ROD END SKRSKY S76 S76A 8143006 NE MLG CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 BEARING IS CRACKED END TO END ON ONE SIDE. SCRAPPED. 1 G 7 2 3U H1NE 2002060500316 20020605 00316 NE 2002 6 5 HEEA079303 1 20020528 A 7331 12281301 METER SKRSKY S76 S76A 8143006 NE FUEL FLOW FLUCTUATES E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 FLUCTUATING FUEL FLOW INDICATION. 1 G 7 2 3U H1NE 2002060500317 20020605 00317 NE 2002 6 5 HEEA079304 1 20020528 A 2435 200SGL115Q STARTER GEN SKRSKY S76 S76A 8143006 NE ENGINE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 UNACCEPTABLE SPLINE WEAR. DEEP VISIBLE GOUGING ON MATTING SURFACE OF SHAFT SPLINES. 1 G 7 2 3U H1NE 2002060500318 20020605 00318 NE 2002 6 5 HEEA079305 1 20020530 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE TAIL ROTOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 12045 760167 TAIL ROTOR BLADE LEADING EDGE ABRASION STRIP ON PADDLE "B" HAS A HOLE WITH MULTIPLE CRACKS. 1 G 7 2 3U H1NE 2002060500319 20020605 00319 NE 2002 6 5 HEEA079306 1 20020530 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE TAIL ROTOR ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15460 13273 760223 TAIL ROTOR BLADE NICKEL ABRASION STRIP IS UNBONDED ON PADDLE "A". BOTH PRIMARY RUBBER IS ERODED THROUGH AND THE TIP IS ERODED. 1 G 7 2 3U H1NE 2002060500320 20020605 00320 NE 2002 6 5 HEEA079307 1 20020530 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE TAIL ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 13555 760231 TAIL ROTOR BLADE PADDLE "B" HAS A HOLE IN THE TIP CAP. 1 G 7 2 3U H1NE 2002060500321 20020605 00321 NE 2002 6 5 HEEA079308 1 20020530 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15460 12746 760223 TAIL ROTOR BLADE PRIMARY POLYSTRIP WORN THROUGH TO THE FIBERGLASS. 1 G 7 2 3U H1NE 2002060500322 20020605 00322 NE 2002 6 5 HEEA079309 1 20020530 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE TAIL ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 10694 760076 TAIL ROTOR BLADE BOX BEAM ON THE PITCH HORNS HAS CORROSION BEYOND LIMITS. 1 G 7 2 3U H1NE 2002060500323 20020605 00323 NE 2002 6 5 HEEA079310 1 20020530 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE TAIL ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 760PH 7589 760078 TAIL ROTOR BLADE PADDLE "A" HAS A HOLE IN THE TIP CAP AREA. 1 G 7 2 3U H1NE 2002060500324 20020605 00324 NE 2002 6 5 HEEA079311 1 20020530 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE TAIL ROTOR ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 9426 760047 TAIL ROTOR BLADE END CAP ON PADDLE "A" ERODED BEYOND LIMITS. 1 G 7 2 3U H1NE 2002060500325 20020605 00325 NE 2002 6 5 HEEA079312 1 20020530 A 6220 7610208500045 SPINDLE SKRSKY S76 S76A 8143006 NE MAIN ROTOR HEAD WORN E K NONE O OTHER IN INSP/MAINT 1 SW 03 760PH 1861 760078 MAIN ROTOR HEAD SPINDLES HAVE WORN BEARINGS. REPAIRED AND RETURNED TO SERVICE. 1 G 7 2 3U H1NE 2002060500326 20020605 00326 NE 2002 6 5 HEEA079313 1 20020530 A 6230 7610408020047 SCISSORS SKRSKY S76 S76A 8143006 NE SWASHPLATE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 MAIN ROTOR SWASHPLATE SCISSOR BUSHINGS WORN. REPAIRED AND RETURNED TO SERVICE. 1 G 7 2 3U H1NE 2002060500327 20020605 00327 NE 2002 6 5 HEEA079314 1 20020530 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADES MISMANUFACTURED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 911MJ 760231 TIP CAP ON MAIN ROTOR BLADES HAVE LARGE SCREW HOLES ON BOTTOM SIDE MISMATCHED ANYWHERE FROM 1/4 INCH HOLE TO 1/2 INCH HO LE. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H1NE 2002060500328 20020605 00328 NE 2002 6 5 HEEA079315 1 20020530 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 199CH 760261 MAIN ROTOR BLADE TIP CAP LOWER OUTER DOUBLER CRACKED. THE FIBERGLASS NEAR THE TRAILING EDGE IS CRACKED ON BOTH SURFACE. 1 G 7 2 3U H1NE 2002060500329 20020605 00329 NE 2002 6 5 HEEA079316 1 20020530 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 MAIN ROTOR BLADE TIP CAP LEADING EDGE ABRASION STRIP SEPARATED AND BOTH INTERNAL DOUBLER. 1 G 7 2 3U H1NE 2002060500330 20020605 00330 NE 2002 6 5 HEEA079317 1 20020530 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 MAIN ROTOR TIP CAP LEADING EDGE ABRASION STRIP CRACKED AND SEPARATED. 1 G 7 2 3U H1NE 2002060500331 20020605 00331 NE 2002 6 5 HEEA079318 1 20020530 A 6210 7615009043054 TIP CAP SKRSKY S76 S76C 8143008 NE M/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 505PH 760505 MAIN ROTOR TIP CAP ABRASION STRIP CRACKED BEYOND LIMITS. 1 G 7 2 3U NC H1NE 2002060500332 20020605 00332 NE 2002 6 5 HEEA079319 1 20020530 A 6210 7615009043054 TIP CAP SKRSKY S76 S76C 8143008 NE M/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 505PH 760505 MAIN ROTOR TIP CAP LEADING EDGE ABRASION STRIP CRACKED. 1 G 7 2 3U NC H1NE 2002060500333 20020605 00333 NE 2002 6 5 HEEA079320 1 20020530 A 6210 7615009100042A BLADE SKRSKY S76 S76A 8143006 NE MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122G 10526 760232 MAIN ROTOR BLADE SKIN DEBONDED NEAR STATION 53 ON THE UPPER SURFACE. THE TIP CAP HAS "C" CHANNEL UNBONDED AND THE CRESE NT SHAPE DOUBLER. 1 G 7 2 3U H1NE 2002060500334 20020605 00334 NE 2002 6 5 HEEA079322 1 20020530 A 6210 7615009100051A BLADE SKRSKY S76 S76A 8143006 NE MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 14043 760050 MAIN ROTOR BLADE FIBERGLASS BEHIND THE SPLICE AREA IS TORN AND SEPARATED BEYOND LIMITS. HELICOIL AT THE ROOT END IS STR IPPED. 1 G 7 2 3U H1NE 2002060500335 20020605 00335 NE 2002 6 5 HEEA079323 1 20020530 A 6210 7615009100051A BLADE SKRSKY S76 S76A 8143006 NE MAIN ROTOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 12077 760035 MAIN ROTOR BLADE SPAR IS CRACK AT ROOT END. SCRAPPED. 1 G 7 2 3U H1NE 2002060500336 20020605 00336 NE 2002 6 5 HEEA079324 1 20020530 A 7160 7630103901102 ACTUATOR SKRSKY S76 S76A 8143006 NE ENGINE INTAKE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5435V 760158 ENGINE INTAKE ACTUATOR HAS SLOP IN GEARS DUE TO WEAR CAUSING A DELAY IN ENGINE RESPONSE WHEN "BEEPED". 1 G 7 2 3U H1NE 2002060500337 20020605 00337 GL 2002 6 5 HEEA079325 2 20020530 A 7200 7630407016041 TUBE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5435V 760158 TUBE CRACKED. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U 3 U H1NE E1GL 2002060500338 20020605 00338 NE 2002 6 5 HEEA079327 1 20020530 A 6320 SCREW 763510950004 SKRSKY S76 S76A 8143006 NE LUBE PUMP ADJUST CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X A08100144 760050 MAIN ROTOR GEARBOX LUBE OIL PUMP ADJUSTMENT SCREW CORRODED. 1 G 7 2 3U H1NE 2002060500339 20020605 00339 NE 2002 6 5 HEEA079328 1 20020530 A 7720 7645001076107 INDICATOR SKRSKY S76 S76A 8143006 NE TURBINE TEMP INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 792CH 760193 NR 2 T5 INDICATOR INSTRUMENT LIGHT FLICKERS INTERMITTENTLY. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H1NE 2002060500340 20020605 00340 NM 2002 6 5 UPS02238518 1 20020527 A 2500 SEAT TRACK BOEING 727 72731C 1384011 NM BS 655-710 LBL62 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C CORROSION ON SEAT TRACK AT BS 660 AND BS 680 LBL 62.5 SEAT TRACK REPLACED BS 655 BS 710 LBL 62.5 I AW SRM 53-10-5 FIGURE 1 2 L 7 3 4F A3WE 2002060500341 20020605 00341 NM 2002 6 5 UPS02238544 1 20020521 A 5210 STOP FITTING BOEING 727 72731C 1384011 NM FWD ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C 2 SUSPECT CRACKS ON LWR AFT ADJUSTABLE STOP FITTING ON FWD ENTRY DOO R STOP FITTING REPLACED IAW S MRO EO 2002-031-002 UPS ENGINEERING FILE NO. 727-52-20009 2 L 7 3 4F A3WE 2002060500342 20020605 00342 NM 2002 6 5 UPS02238545 1 20020521 A 5210 STOP FITTING BOEING 727 72731C 1384011 NM LWR AFT ENTRY D CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C 2 SUSPECT CRACKS ON LWR AFT ADJUSTABLE STOP FITTING ON FWD ENTRY DOO R STOP FITTING REPLACED IAW S MRO EO 2002-031-002 UPS ENGINEERING FILE NO. 727-52-20009 2 L 7 3 4F A3WE 2002060500343 20020605 00343 NE 2002 6 5 HEEA079329 1 20020530 A 7712 7645001078106 INDICATOR SKRSKY S76 S76A 8143006 NE DUAL TORQUE READS LOW E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 760158 DUAL TORQUE INDICATOR NR 1 NEEDLE READS 8-10 PERCENT LOW. 1 G 7 2 3U H1NE 2002060500344 20020605 00344 NE 2002 6 5 HEEA079330 1 20020530 A 7712 7645001078106 INDICATOR SKRSKY S76 S76A 8143006 NE DUAL TORQUE STUCK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 760158 NO INDICATION ON NR 1 SIDE. NEEDLE STAYED ON ZERO. 1 G 7 2 3U H1NE 2002060500345 20020605 00345 NE 2002 6 5 HEEA079332 1 20020530 A 2121 7650007901103 BLOWER SKRSKY S76 S76A 8143006 NE AIR DISTRIBUTION INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5435V 760158 AIR DISTRIBUTION BLOWER WILL NOT MOTOR. 1 G 7 2 3U H1NE 2002060500346 20020605 00346 NE 2002 6 5 HEEA079333 1 20020530 A 2121 7650007901103 BLOWER SKRSKY S76 S76A 8143006 NE AIR DISTRIBUTION INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5435V 760158 INOPERATIVE - WILL NOT TURN WITH POWER APPLIED. 1 G 7 2 3U H1NE 2002060500347 20020605 00347 NE 2002 6 5 HEEA079334 1 20020530 A 2140 7650007904101 PRESSURE SWITCH SKRSKY S76 S76A 8143006 NE HEATER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 BLEED AIR HEATER INOPERATIVE WITH ADVISORY LIGHT ON. SCRAPPED SWITCH. 1 G 7 2 3U H1NE 2002060500348 20020605 00348 NE 2002 6 5 HEEA079335 1 20020530 A 2140 7650007904101 PRESSURE SWITCH SKRSKY S76 S76A 8143006 NE HEATER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 BLEED AIR HEATER INOPERATIVE. SCRAPPED SWITCH. 1 G 7 2 3U H1NE 2002060500349 20020605 00349 NE 2002 6 5 HEEA079338 1 20020530 A 3340 7655002005101 SEARCH LIGHT SKRSKY S76 S76A 8143006 NE EXTERIOR MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 199CH 760261 SEARCH LIGHT STAYS ON AT ALL TIMES WITH SWITCH IN OFF POSITION OR STOW POSITION. 1 G 7 2 3U H1NE 2002060500350 20020605 00350 NE 2002 6 5 HEEA079339 1 20020530 A 3340 7655002005102 SEARCH LIGHT SKRSKY S76 S76A 8143006 NE EXTERIOR MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 199CH 760261 LIGHT WILL NOT STOP ROTATING WHEN IN STOW POSITION. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H1NE 2002060500351 20020605 00351 NE 2002 6 5 HEEA079340 1 20020530 A 3340 7655002005102 SEARCH LIGHT SKRSKY S76 S76A 8143006 NE EXTERIOR MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 199CH 760261 WHEN SWITCH IS PUT IN STOW POSITION, LIGHT WILL NOT STOW, KEEPS TURNING 360 DEGREES. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H1NE 2002060500352 20020605 00352 NE 2002 6 5 HEEA079341 1 20020530 A 2420 7655009005104 GCU SKRSKY S76 S76A 8143006 NE GENERATOR MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 GCU INTERMEDIATELY SHUTS GENERATOR OFF. 1 G 7 2 3U H1NE 2002060500353 20020605 00353 NE 2002 6 5 HEEA079342 1 20020530 A 2421 7655009005105 GENERATOR SKRSKY S76 S76A 8143006 NE AC FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 AC GENERATOR INTERMITTENTLY DROPS OFF LINE. 1 G 7 2 3U H1NE 2002060500354 20020605 00354 NE 2002 6 5 HEEA079343 1 20020530 A 2421 7655009005110 GENERATOR SKRSKY S76 S76A 8143006 NE AC SYSTEM FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122G 760232 AC GENERATOR WILL NOT COME ON LINE. 1 G 7 2 3U H1NE 2002060500355 20020605 00355 NE 2002 6 5 HEEA079344 1 20020530 A 2434 7655009006106 CONTROL UNIT SKRSKY S76 S76A 8143006 NE DC SYSTEM INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 DC CONTROL UNIT CAUSED GENERATOR SYSTEM TO BE INOPERATIVE. 1 G 7 2 3U H1NE 2002060500356 20020605 00356 NE 2002 6 5 HEEA079345 1 20020530 A 2434 7655009006106 CONTROL UNIT SKRSKY S76 S76A 8143006 NE DC SYSTEM INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 DC CONTROL UNIT CAUSED GENERATOR SYSTEM TO BE INOPERATIVE. 1 G 7 2 3U H1NE 2002060500357 20020605 00357 NE 2002 6 5 HEEA079346 1 20020530 A 2434 7655009006106 CONTROL UNIT SKRSKY S76 S76A 8143006 NE DC SYSTEM INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 DC CONTROL UNIT CAUSED GENERATOR SYSTEM TO BE INOPERATIVE. 1 G 7 2 3U H1NE 2002060500358 20020605 00358 NE 2002 6 5 HEEA079347 1 20020530 A 6321 7655009803103 MOTOR SKRSKY S76 S76A 8143006 NE ROTOR BRAKE MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15460 760223 ROTOR BRAKE MOTOR DOES NOT SHUT OFF. 1 G 7 2 3U H1NE 2002060500359 20020605 00359 NE 2002 6 5 HEEA079348 1 20020530 A 3297 7655202010105 HARNESS SKRSKY S76 S76A 8143006 NE MLG FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 911MJ 760231 MLG WIRE HARNESS FAILED CONTINUITY CHECK. SCRAPPED. 1 G 7 2 3U H1NE 2002060500360 20020605 00360 NE 2002 6 5 HEEA079353 1 20020530 A 6321 INDICATOR SKRSKY S76 S76A 8143006 NE ROTOR BRAKE INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 913UK 441 760276 WARNING LIGHT WON'T ILLUMINATE WITH ROTOR BRAKE ON. 1 G 7 2 3U H1NE 2002060500361 20020605 00361 NM 2002 6 5 AWXA200200500 1 20020529 A 3350 BMS13311122 WIRE BOEING 737 737301 1384611 NM BS 314 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 0 0 23258 MCN - EEL - DURING C-16 CHECK THE EXTERIOR EMERGENCY LIGHT AT L2 DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE TROUBLESH OT AND FOUND THE EXTERIOR EMERGENCY LIGHT WIRING TERMINALS BROKEN. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT WIRE TE RMINAL AT L2 DOOR IAW BSWPM 20.30.00 PG. 1-3. OPS CHECK GOOD IAW BMM 33.25.03 PG. 203. 2 L 7 2 4F RT A16WE 2002060500362 20020605 00362 SO 2002 6 5 LR7A02039 1 20020604 A 5230 SKIN LKHEED 382 382G 526414U SO FS 880 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING SCHEDULED A-CHECK INSPECTION PER JOB CARD HA1200 FOUND FS 880 CARGO DOOR SKIN CRACKED 1.5 IN. AT LBL 14, WL 200.R EPAIRED IAW SRM SMP 583 51-140-12. LP 13873, 2M. 2 H 7 4 4T A1SO 2002060500363 20020605 00363 NM 2002 6 5 S02232019 1 20020521 A 3200 69B839013 BRACKET BOEING 747 747400 NM PWA 4056 PW4056 NE BROKEN W SAJF O OTHER O OTHER CL CLIMB 1 WP 03 28712 B18205 AFT A/C T/O CAPT REPORTED LH BLG FAILED TO RETRACT, STATUS MSG GEAR TILT DISP. INSP FND LH BLG HYD FUSE SUPPLY TU BE LEAKS(IPC 32-13-67-01-95)BY CHAFING DUE TO BROKEN BRACKET.C/A:1.PER MM 20-11-05 USING FLEX HOSE FOR TEMP REPAIR & LEA K CHK OK. PFM HYD TUBE BLEED IAW MM 32-13-15, PSEU GRD TESTED PASS. 2.EON OF ONE TIME INSP WAS ISSUED FOR 744 & 742 FLEE T, WHEREIN B18275, N497, & N498 WERE FND THE SAME BRACKET BROKEN. 3.FOR 742,AMP 32-5-005-G IS ADDED FOR CHK CLAMPS & BRA CKETS OF LH/RH BLG HYD INSTALLATION WITH 1C INTERVAL, FOR 744, AMP 32-13-00-B IS ADDED WITH THE SIMILAR TASK. 4.ME REQUE STED BOEING TO PROVIDE COMMENTS & CONCERNS REGARDING TO THIS ISSUE 2 L 7 4 4F 4 F RT A20WE E24NE 2002060600001 20020606 00001 NE 2002 6 6 HEEA079331 1 20020530 A 2121 7650007901103 BLOWER SKRSKY S76 S76A 8143006 NE AIR DISTRIBUTION FAILED E HEEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 03 199CH 760261 BLOWER ASSY EMITTED A STRONG BURNING ODOR, THEN QUIT. 1 G 7 2 3U H1NE 2002060600002 20020606 00002 NE 2002 6 6 HEEA079349 1 20020530 A 2800 7665000901101 VALVE SKRSKY S76 S76A 8143006 NE FUEL SYSTEM SHORTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 VALVE POPS CIRCUIT BREAKER. 1 G 7 2 3U H1NE 2002060600003 20020606 00003 NE 2002 6 6 HEEA079350 1 20020530 A 3150 7665001001103 WARN PANEL SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA K NONE N L FALSE WARNING NO TEST IN INSP/MAINT 1 SW 03 3122H 760233 CAUTION LIGHTS ILLUMINATED ALONG WITH GEAR UNLOCKED LIGHT AND FLOAT WARNING AND TEST LIGHTS ALSO. 1 G 7 2 3U H1NE 2002060600004 20020606 00004 NE 2002 6 6 HEEA079351 1 20020530 A 6200 7665001802102 ACTUATOR SKRSKY S76 S76A 8143006 NE MAIN ROTOR LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 5435V 760158 VTA ACTUATOR PISTONS LEAK. 1 G 7 2 3U H1NE 2002060600005 20020606 00005 NE 2002 6 6 HEEA079352 1 20020530 A 6200 7665001802102 ACTUATOR SKRSKY S76 S76A 8143006 NE MAIN ROTOR LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 3122H 760233 VTA ACTUATOR HAS A HYDRAULIC LEAK FROM CROSSOVER TUBE. 1 G 7 2 3U H1NE 2002060600007 20020606 00007 2002 6 6 HEEA079354 4 20020530 A 2210 7690001802106 ACTUATOR SKRSKY S76 S76A 8143006 NE AFCS INTERMITTENT E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 911MJ 760231 NR 2 PITCH CHANNEL KICKING INTERMITTENTLY IN FLIGHT. 1 G 7 2 3U H1NE 2002060600008 20020606 00008 2002 6 6 HEEA079355 4 20020530 A 2210 7690001802106 ACTUATOR SKRSKY S76 S76C 8143008 NE AFCS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 505PH 4808 760505 FAILED TEST ON BRAKE OUT BOX CHATTERS DURING OPERATION. 1 G 7 2 3U NC H1NE 2002060600009 20020606 00009 2002 6 6 HEEA079356 4 20020530 A 2210 7690001802106 ACTUATOR SKRSKY S76 S76A 8143006 NE AFCS DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 760PH 3452 760078 AFCS ACTUATOR CHATTERS. 1 G 7 2 3U H1NE 2002060600017 20020606 00017 2002 6 6 HEEA079357 4 20020530 A 2210 KNOB SKRSKY S76 S76A 8143006 NE YAW INDICATOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 760PH 8012883 760078 KNOB CRACKED, SLIPS. 1 G 7 2 3U H1NE 2002060600018 20020606 00018 2002 6 6 HEEA079358 4 20020530 A 2210 7690001802106 ACTUATOR SKRSKY S76 S76A 8143006 NE AFCS INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 911MJ 4140 760231 NR 1 YAW ACTUATOR NOT RESPONDING ON SYSTEM CHECK. 1 G 7 2 3U H1NE 2002060600019 20020606 00019 2002 6 6 HEEA079359 4 20020530 A 2210 7690001808102 RATE GYRO SKRSKY S76 S76A 8143006 NE AFCS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 760158 GYRO CAUSES THE T/R GYRO CIRCUIT BREAKER TO POP. SENT TO MASCO FOR INSPECTION AND REPAIR. 1 G 7 2 3U H1NE 2002060600021 20020606 00021 2002 6 6 HEEA079360 4 20020530 A 3442 78806059008 DISPLAY SKRSKY S76 S76A 8143006 NE WX RADAR WILL NOT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 UNABLE TO ACCESS GROUND TEST MODE ON WEATHER RADAR UNIT. 1 G 7 2 3U H1NE 2002060600022 20020606 00022 2002 6 6 HEEA079361 4 20020530 A 3442 78806059008 DISPLAY SKRSKY S76 S76A 8143006 NE WX RADAR INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 WEATHER RADAR UNIT DISPLAY REMAINS BLANK. 1 G 7 2 3U H1NE 2002060600023 20020606 00023 2002 6 6 HEEA079362 4 20020530 A 3442 80510800001 DISPLAY SKRSKY S76 S76A 8143006 NE WX RADAR SYS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 761PH 760224 WEATHER RADAR UNIT UNRELIABLE. 1 G 7 2 3U H1NE 2002060600025 20020606 00025 2002 6 6 HEEA079363 4 20020530 A 3457 8143902240B GPS SKRSKY S76 S76A 8143006 NE COCKPIT INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545K 760047 GPS UNIT INOPERATIVE. 1 G 7 2 3U H1NE 2002060600026 20020606 00026 2002 6 6 HEEA079364 4 20020530 A 3457 8143902240B GPS SKRSKY S76 S76A 8143006 NE COCKPIT INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546K 760082 GPS UNIT HAS NO DISPLAY. 1 G 7 2 3U H1NE 2002060600027 20020606 00027 2002 6 6 HEEA079365 4 20020530 A 3457 8143902240B GPS SKRSKY S76 S76A 8143006 NE COCKPIT WILL NOT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 GPS UNIT WILL NOT TEST AND CDI WILL NOT CENTER. 1 G 7 2 3U H1NE 2002060600028 20020606 00028 2002 6 6 HEEA079366 4 20020530 A 3457 8144002241D GPS SKRSKY S76 S76C 8143008 NE COCKPIT INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 505PH 760505 GPS UNIT INOPERATIVE. 1 G 7 2 3U NC H1NE 2002060600029 20020606 00029 NE 2002 6 6 HEEA079367 1 20020530 A 2430 A1077D RELAY SKRSKY S76 S76A 8143006 NE DC SYSTEM STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 RELAY CONTACTS SERVICING PINS 21, 22 AND 23 ARE STUCK IN THE ENERGIZED POSITION. 1 G 7 2 3U H1NE 2002060600030 20020606 00030 NE 2002 6 6 HEEA079368 1 20020530 A 2430 A1077D RELAY SKRSKY S76 S76A 8143006 NE DC SYSTEM STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 CONTACTOR STUCK IN THE ENERGIZED POSITION ALLOWING STARTER TO BE POWERED ANYTIME AIRCRAFT POWER AND MASTER START WAS PLA CED ON. 1 G 7 2 3U H1NE 2002060600031 20020606 00031 2002 6 6 HEEA079369 4 20020530 A 2350 A3016W INTERPHONE SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5426U 760167 COPILOT HAS HOT MIC ON CABIN ICS. FOUND CAPACITOR C30, RESISTOR R71 AND LIGHT PANEL BAD. REPLACED, REPAIRED, BENCH CHEC K GOOD. 1 G 7 2 3U H1NE 2002060600032 20020606 00032 2002 6 6 HEEA079370 4 20020530 A 2350 A3016W INTERPHONE SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3122H 760233 FM BLEEDS INTO ICS. FOUND VOLUME AND TRANSMIT KNOBS, SWITCH S1, AND LIGHT PANEL BAD. RESOLDERED BROKEN WIRE IN LIGHT PA NEL AND REPLACED VOLUME AND TRANSMIT KNOBS AND SWITCH S1. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002060600033 20020606 00033 NM 2002 6 6 A6WA200230008 1 20020521 A 2432 BATTERY DORNER DO32 DO328100 2996000 NM NR 2 OVERHEATED A A6WA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 31 328LS 3025 ON TAKE OFF BATTERY OVERHEAT LIGHT ON RED WARNING PANEL ILLUMINATED. C/W CHECKLIST, SELECTED NR 2 BATTERY OFF. AFTER 5 MINUTES LIGHT WENT OFF. MAINTENANCE REMOVED AND REPLACED NR 2 BATTERY. OPS CHECKED OK. 2 H 7 2 4T RT A45NM 2002060600034 20020606 00034 2002 6 6 HEEA079371 4 20020530 A 2350 A3016W INTERPHONE SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 VHF BLEEDS OVER. FOUND SWITCH S1 BAD. REPLACED. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002060600035 20020606 00035 2002 6 6 HEEA079372 4 20020530 A 2350 A3016W INTERPHONE SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3122G 760232 FM FROM OTHER STATIONS BLEED OVER. CLEANED S1 SELECTOR SWITCH AND ALL MONITOR SWITCHES. REPAIRED PROBLEM. FOUND ICS SI GNAL DISTORTED WHEN UNIT IS FIRST TURNED ON THEN CLEARED UP AFTER UNIT WARMS UP. REPLACED BAD AR2 MODULE. REPAIRED PRO BLEM. ALSO REPLACED BAD LIGHT PANEL. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002060600036 20020606 00036 EA 2002 6 6 A6WA200240013 1 20020424 A 7830 22850860105 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NR 2 ENGINE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 409AW 3700 7447 NR 1 ENGINE THRUST REVERSER UPPER CASCADE IS CRACKED. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER UPPE R CASCADE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002060600037 20020606 00037 EA 2002 6 6 A6WA200240014 1 20020424 A 7830 22850860106 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NR 2 ENGINE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 409AW 3700 7447 NR 2 ENGINE THRUST REVERSER UPPER CASCADE IS CRACKED. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE THRUST REVERSER UPPE R CASCADE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002060600038 20020606 00038 EA 2002 6 6 A6WA200240015 1 20020424 A 7830 22850252101 FAIRING CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 409AW 3700 7447 NR 1 ENGINE UPPER STANG FAIRING CRACKED MAINTENANCE REMOVED AND REPLACED UPPER STANG FAIRING. 2 L 7 2 4F RT A21EA 2002060600039 20020606 00039 EA 2002 6 6 A6WA200240016 1 20020424 A 7830 22850253102 FAIRING CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 409AW 3700 7447 NR 2 ENGINE UPPER STANG FAIRING CRACKED MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE UPPER STANG FAIRING. 2 L 7 2 4F RT A21EA 2002060600040 20020606 00040 GL 2002 6 6 HEEA079373 2 20020530 A 7250 23062753 NOZZLE BELL 206 TH57A 1180821 SW ALLSN 250C 250C18A 03011 GL ENGINE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 70 162035 ENGINE TURBINE NOZZLE HAS STRIPPED THREADS AT GP SUPPORT MATING SURFACE. 1 G 7 1 3U 3 U EXPA1G71 E4CE 2002060600041 20020606 00041 EA 2002 6 6 A6WA200240017 1 20020521 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF POSITION A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 404AW 7294 PAX DOOR OUTER HANDLE MESSAGE ON CLIMB OUT (12,000 FT) INNER STOW HANDLE WILL NOT STOW CORRECTLY. MESSAGE WENT AWAY WHE N PRESS ON GROUND. ON CALL MAINTENANCE INSPECTED DOOR AND SURROUNDING AREA, NO DEFECTS. PRESSURIZED AIRCRAFT. NO OBVI OUS DEFECTS, CYCLED DOOR OPEN AND CLOSED SEVERAL TIMES DOOR OPS NORMAL. 2 L 7 2 4F RT A21EA 2002060600042 20020606 00042 GL 2002 6 6 HEEA079374 2 20020530 A 7250 23062753 NOZZLE BELL 206 TH57A 1180821 SW ALLSN 250C 250C18A 03011 GL ENGINE FOD E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 70 162035 TURBINE NOZZLE HAS FOREIGN MATERIAL ON AFT SIDE OF DIAPHRAGM. 1 G 7 1 3U 3 U EXPA1G71 E4CE 2002060600043 20020606 00043 EA 2002 6 6 A6WA200240018 1 20020521 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FALSE INDICATION A A6WA O OTHER N FALSE WARNING CR CRUISE 1 GL 31 404AW 7294 PAX DOOR OUTER HANDLE CAUTION MESSAGE AT 17,000 FT AIRCRAFT ALTITUDE. 100 CABIN ALTITUDE DIFF PRESS 6.3 MESSAGE DISAPPE ARS WHEN DOOR WAS OPENED AT THE GATE. 2 L 7 2 4F RT A21EA 2002060600044 20020606 00044 GL 2002 6 6 HEEA079375 2 20020530 A 7250 6886407 TURBINE WHEEL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8199J 1440 S826 CAE835939 TURBINE REMOVED FOR HIGH CYCLED WHEELS. UPON INSPECTION OF PARTS NOTED SULFIDATION AND CRACKED NR 1 WHEEL BLADES. SCRAP PED WHEEL. 1 G 7 2 3U 3 U H3EU E4CE 2002060600045 20020606 00045 SW 2002 6 6 HEEA079376 1 20020528 A 3246 206053184121 SKID BELL 407 407 1182206 SW MLG WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8595X 53267 SKID TUBE WORN ON THE MOST AFT LOCATION. 1 G 7 1 3U O H2SW 2002060600046 20020606 00046 SW 2002 6 6 HEEA079377 1 20020528 A 6730 206076062107 SERVO BELL 407 407 1182206 SW CYCLIC STICK MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 407PH 53003 LT CYCLIC KICK WHEN HYD TURNED ON. 1 G 7 1 3U O H2SW 2002060600047 20020606 00047 NM 2002 6 6 ASA2002F00000 1 20020324 A 5310 654659529 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 742AS 23136 PAE- DURING SCHEDULED C-CHECK FOUND SHEAR TIE AT BODY STATION 727A, STRINGER 21L-22L CORRODED. REPAIRED PER SRM. 2 L 7 2 4F A16WE 2002060600048 20020606 00048 NM 2002 6 6 ASA2002F00001 1 20020324 A 5320 507945 BEAM BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 742AS 23136 PAE- DURING SCHEDULED C-CHECK FOUND LOWER GATE BEAM AT BODY STATION 312-344, WATERLINE 210, CRACKED. REPAIRED PER SRM. 2 L 7 2 4F A16WE 2002060600049 20020606 00049 SW 2002 6 6 HEEA079379 1 20020528 A 6220 BEARING BELL 407 407 1182206 SW M/R UNIVERSAL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 723PH RXFS5806 53283 MAIN ROTOR UNIVERAL HAS WORN BEARING. 1 G 7 1 3U O H2SW 2002060600050 20020606 00050 NM 2002 6 6 ASAA0290003 1 20020405 A 5210 141A6097 GUIDE BOEING 737 737* NM ENTRY DOOR DEFECTIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 305AS 30013 SEA - DURING LINE MAINTENANCE, FOUND THE L1 DOOR HARD TO CLOSE. REPLACED GUIDE ARM. DOOR THEN FUNCTIONED PROPERLY. (M ) 2 L 7 2 4F RT A16WE 2002060600051 20020606 00051 SW 2002 6 6 HEEA079380 1 20020528 A 6420 BEARING BELL 407 407 1182206 SW T/R HUB ASSY WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 724PH 53200 53327 TAIL ROTOR HUB HAS A WORN FEATHERING BEARING. 1 G 7 1 3U O H2SW 2002060600052 20020606 00052 SO 2002 6 6 ASO2002F00006 1 20020430 A 5313 STRINGER EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE CORRODED B ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C CHECK INSPECTION, CORROSION WAS FOUND OUT OF LIMITS ON STRINGER 19 LEFT BETWEEN FRAME 13A AND STA 6653.1 TO FRA ME 21 AS WELL AS BETWEEN FRAMES 23 AND 24. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002060600053 20020606 00053 SO 2002 6 6 ASO2002F00007 1 20020430 A 5313 STRINGER EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE CORRODED B ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C CHECK INSPECTION, STRINGER 21 LEFT WAS FOUND CORRODED BEYOND LIMITS BETWEEN FRAMES 17 AND 18. MAINTENANCE REMO VED AND REPLACED THE CORRODED STRINGER SECTION AND INSTALLED A SPLICE IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002060600054 20020606 00054 SW 2002 6 6 HEEA079382 1 20020528 A 6420 PHI407112 LINK BELL 407 407 1182206 SW PITCH CONTROL LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 724PH 53327 TAIL ROTOR HUB HAS PLAY IN A PITCH LINK. 1 G 7 1 3U O H2SW 2002060600055 20020606 00055 SO 2002 6 6 ASO2002F00008 1 20020430 A 5320 12006964001 CROSSBEAM EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE CORRODED B ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C CHECK INSPECTION, ALL CROSS BEAMS AT FRAME 20 WERE FOUND CORRODED. THE RIGHT CENTER AND THE RIGHT OUTBOARD WER E FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE TWO CORRODED CROSS BEAMS IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002060600056 20020606 00056 SO 2002 6 6 ASO2002F00009 1 20020430 A 5320 12004149002 CROSSBEAM EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE CORRODED B ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C CHECK INSPECTION, ALL CROSS BEAMS AT FRAME 23 WERE FOUND CORRODED, BUT ONLY THE RIGHT OUTBOARD CROSS BEAM WAS F OUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS BEAM IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002060600057 20020606 00057 2002 6 6 HEEA079383 4 20020528 A 3422 060001500 GYRO BELL 206 206L3 1182108 SW DIRECTIONAL IND INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30KH 51527 DIRECTIONAL GYRO INOPERATIVE. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600058 20020606 00058 SO 2002 6 6 ASO2002F00010 1 20020430 A 5320 CROSSBEAM EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE CORRODED B ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C CHECK INSPECTION, ALL CROSS BEAMS AT FRAME 28 WERE FOUND TO BE CORRODED AND ALL WERE OUT OF LIMITS. MAINTENANC E REMOVED AND REPLACED ALL FOUR CORRODED CROSS BEAMS AT FRAME 28 IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002060600059 20020606 00059 SO 2002 6 6 ASO2002F00011 1 20020430 A 5320 12004170002 CROSSBEAM EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE CORRODED B ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C CHECK INSPECTION, ALL CROSS BEAMS AT FRAMES 36 AND 38 WERE FOUND CORRODED BEYOND ALLOWABLE LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS BEAMS IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002060600060 20020606 00060 SO 2002 6 6 ASO2002F00012 1 20020430 A 5320 12004449001 CROSSBEAM EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE CORRODED B ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C CHECK INSPECTION, THE LEFT CENTER CROSS BEAM AT FRAME 40 WAS FOUND CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS BEAM IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002060600061 20020606 00061 SO 2002 6 6 ASO2002F00013 1 20020430 A 5320 12046156001 BUTT STRAP EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE CORRODED B ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C CHECK INSPECTION, THE RIGHT HAND BUTT STRAP WAS FOUND CORRODED BEYOND LIMITS BETWEEN FRAMES 13 AND 21. MAINTEN ANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002060600062 20020606 00062 SW 2002 6 6 HEEA079384 1 20020528 A 6700 BEARING BELL 206 206L3 1182108 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6748D 51106 FLIGHT CONTROL BELLCRANK HAS A BEARING WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600063 20020606 00063 SO 2002 6 6 ASO2002F00014 1 20020430 A 5320 12007053005 BUTT STRAP EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE CORRODED B ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C CHECK INSPECTION, THE CENTER BUTT STRAP BETWEEN FRAMES 21 AND 26 WAS FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002060600064 20020606 00064 WP 2002 6 6 EIA2002045 1 20020502 A 3350 60030431 BATTERY DOUG DC9 DC933F 302207A WP PWA JT8 JT8D9 52048 NE CABIN DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 933F 47191 EMERGENCY EXIT LIGHT, BATTERIES DO NOT HOLD A CHARGE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY PER MM. SYST EMS OPS, NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 2002060600065 20020606 00065 SW 2002 6 6 HEEA079385 1 20020528 A 6320 206040184001 PUMP BELL 206 206B3 1181506 SW MAIN ROTOR LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2275Y 3626 MAIN ROTOR OIL PUMP LEAKING. REPLACED WITH SERVICEABLE PUMP. 1 G 7 1 3U H2SW 2002060600066 20020606 00066 NM 2002 6 6 EIA2002060 1 20020505 A 3340 5222457037 SWITCH BOEING 747 747212B 1384886 NM PWA JT9 JT9D* NE COCKPIT FAULTY A EIAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 486EV 20888 SMOKE SEEN COMING FROM THE NR HF RADIO PANEL, SMOKE STOPPED IMMEDIATELY WHEN RADIO WAS SWITCHED OFF. FOUND RIGHT INBOAR D LANDING LIGHT SWITCH BAD, REPLACED SWITCH AND HF CONTROL PANEL PER MM. 2 L 7 4 4F 4 F A20WE E20EA 2002060600067 20020606 00067 NM 2002 6 6 EIA2002062 1 20020510 A 2121 605457 FAN BOEING 747 747132 1384882 NM PWA JT9 JT9D3 52050 NE CABIN MALFUNCTIONED A EIAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 481EV 19896 NR 2 RECIRCULATION FANS MAKE WHINING NOISE AND SMELLS OF HOT ELECTRIC FUMES. REMOVED AND REPLACED NR 2 RECIRCULATION FA N AS PER MM. 2 L 7 4 4F 4 F A20WE E20EA 2002060600068 20020606 00068 SW 2002 6 6 HEEA079386 1 20020528 A 7110 206061249001 FITTING BELL 206 206L3 1182108 SW ENGINE COWL DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30KH 51527 ENGINE COWL FITTING DETERIORATED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600069 20020606 00069 SW 2002 6 6 HEEA079387 1 20020528 A 2820 206064263101 LINE BELL 206 206L3 1182108 SW FUEL SYSTEM DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30KH 51527 FUEL LINE DETERIORATED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600070 20020606 00070 CE 2002 6 6 GUU2002F00000 1 20020512 A 1430 EWB225 BOLT BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 53545 13903 UE185 AT SCHEDULED ROUTINE INSPECTION VERTICAL SPAR SECURITY CHECK ATTACH BOLTS REQUIRED RETORQUE. RETORQUED FOUR LOWER VERTI CAL BOLTS IAW MM. 2 L 7 2 4T 3 T RT A24CE E2NE 2002060600071 20020606 00071 CE 2002 6 6 GUU2002F00001 1 20020412 A 1430 EWB225 BOLT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A11 52043 NE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 49543 231 UE181 AT SCHEDULED ROUTINE INSPECTION VERTICAL FIN LOWER ATTACH BOLTS REQUIRED RETORQUE. RETORQUED FOUR LOWER VERTICAL BOLTS IAW MM. 2 L 7 2 4T 3 T RT A24CE E4EA 2002060600072 20020606 00072 SW 2002 6 6 HEEA079388 1 20020528 A 7160 206064213103 SCREEN BELL 206 206L3 1182108 SW ENGINE INTAKE DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30KH 51527 ENGINE INTAKE SCREEN DETERIORATED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600073 20020606 00073 EA 2002 6 6 GUU2002F00002 2 20020507 A 7261 OIL SYSTEM BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT ENGINE CONTAMINATED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87557 UE246 AT SCHEDULED ROUTINE INSPECTION (LINE CHECK) THE RIGHT ENGINE WAS DETERMINED TO HAVE DISCOLORED OIL. CHANGE OIL AND OIL FILTER. PLACED ENGINE ON OIL WATCH. 2 L 7 2 4T 3 T RT A24CE E2NE 2002060600074 20020606 00074 SW 2002 6 6 HEEA079389 1 20020528 A 3210 206323202 SUPPORT BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116P 51530 MLG SUPPORT HAS CORROSION. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600075 20020606 00075 2002 6 6 GUU2002F00003 4 20020414 A 3418 1143800515 COMPUTER BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA STALL WARNING MALFUNCTIONED A GUUA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 17 38537 UE158 DURING TAKE OFF STALL WARNING WENT OFF. REMOVED AND REPLACED STALL WARNING COMPUTER, OPERATIONAL CHECK NORMAL. TEST FL IGHT SATISFACTORY. 2 L 7 2 4T 3 T RT A24CE E2NE 2002060600076 20020606 00076 EA 2002 6 6 GUU2002F00004 2 20020504 A 7261 OIL SYSTEM BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ENGINE CONTAMINATED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 49543 UE181 AT SCHEDULED ROUTINE INSPECTION (A CHECK) THE RIGHT ENGINE WAS DETERMINED TO HAVE DISCOLORED "BLACK OIL". CHANGED THE E NGINE OIL AND OIL FILTER. PLACED ENGINE ON OIL WATCH. 2 L 7 2 4T 3 T RT A24CE E2NE 2002060600077 20020606 00077 2002 6 6 HEEA079390 4 20020528 A 2200 2593996333 TARSYN BELL 212 212 1181420 SW AUTO FLIGHT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 27805 31106 TARSYN333 MALFUNCTIONS, PILOT`S ATTITUDE SYSTEM CIRCUIT BREAKER POPPING. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 4U H4SW 2002060600078 20020606 00078 NE 2002 6 6 GUU2002F00005 2 20020504 A 7250 3044700 POWER UNIT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE FAILED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81556 10966 UE239 AT SCHEDULED ROUTINE INSPECTION THE RIGHT ENGINE WAS DETERMINED TO HAVE DISCOLORED (BLACK OIL). REPLACE THE RIGHT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. 2 L 7 2 4T 4 T RT A24CE E26NE 2002060600079 20020606 00079 SW 2002 6 6 HEEA079391 1 20020528 A 6240 206075681105 INDICATOR BELL 206 206L3 1182108 SW DUAL TACH FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3116P 51530 DUAL TACH INDICATOR N2 NEEDLE AT ZERO WHEN ROTOR IS AT 100 PERCENT. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U H2SW 2002091600136 20020916 00136 NM 2002 9 16 HALA0200098 1 20020423 A 4910 INLET BOEING 717 717200 1383700 NM APU CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 476HA 55118 HNL - PER EO 49-02-01-12 APU INELT DOOR TOP END CRACKED APPROX 2.5 INCH. ALSO, CRACKED ON LEADING EDGE APPROX 7 INCHES. DOOR REMOVED, ACCOMPLISHED INTERIM REPAIR PER HAL M105 476003. DOOR REINSTALLED PER MM 49-17-01 AND 49-17-02. DOOR O PS CHECK NORMAL. (M) 2 L 7 2 4F TR A6WE 2002060600080 20020606 00080 SW 2002 6 6 HEEA079392 1 20020528 A 3340 7028501 LIGHT BELL 412 412 1182202 SW STROBE SHORTED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 2148K 36001 STROBE LIGHT POPPING CIRCUIT BREAKER. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060600081 20020606 00081 NM 2002 6 6 HALA0200099 1 20020430 A 5247 SHAFT BOEING 717 717200 1383700 NM APU DOOR CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 477HA 55122 MAINTENANCE ENTRY: APU DOOR SHAFT WELD, CRACKED. REMOVED DOOR AND ROUTE TO AOH. NO ACCEPTABLE REPAIR, OK TO CONTINUE PER CDL ENTERED ON MIC SHT (DOOR REMOVED). 2 L 7 2 4F TR A6WE 2002060600083 20020606 00083 NM 2002 6 6 HALA0200100 1 20020504 A 4910 INLET BOEING 717 717200 1383700 NM APU CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 RAMS: 2 EACH CRACK ON APU DOOR INLET BOX. AT TOP AFT INBOARD CORNER OF BOX (IN AREA OF AFT SUPPORT STRUT). IN WORK. 2 L 7 2 4F TR A6WE 2002060600084 20020606 00084 SW 2002 6 6 HEEA079394 1 20020528 A 3340 G62504 LIGHT BELL 412 412 1182202 SW SEARCH LIGHT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22608 33075 SEARCH LIGHT WILL NOT RETRACT. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060600085 20020606 00085 NM 2002 6 6 HALA0200102 1 20020507 A 4910 DUCT BOEING 717 717200 1383700 NM APU CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 480HA 55125 CRACK ON APU INLET DOOR DUCT. REPAIRED PER HAL M105 FILE. 2 L 7 2 4F TR A6WE 2002060600086 20020606 00086 2002 6 6 HEEA079395 4 20020528 A 3442 MI585202 ANTENNA BELL 412 412 1182202 SW WX RADAR SYS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 PAINTING GHOSTS AND STREAKING. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 4U H4SW 2002060600087 20020606 00087 SW 2002 6 6 HEEA079396 1 20020528 A 6520 PHI2062003 HOUSING BELL 206 206L4 1182110 SW T/R GEARBOX LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 7074W 52033 TAIL ROTOR SEAL HOUSING ON GEARBOX LEAKS. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U NC H2SW 2002060600088 20020606 00088 NM 2002 6 6 TSAA0232137 1 20020512 A 3234 MS250081 SWITCH BOEING 737 73725A 1384481 NM PWA JT8 JT8D17 52049 NE COCKPIT STUCK A TSAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 13 819AL 23791 ANTI-SKID INOPERATIVE LIGHT ILLUMINATED ON BOTH SYSTEMS DURING FLIGHT. DUE TO WEATHER CONDITIONS, RUNWAY LENGTH AND AIR CRAFT WEIGHT FOR THE AIRPORT, THE AIRCRAFT RETURNED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED A DEFECTIVE LANDING GEAR LEVER UP SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002060600089 20020606 00089 SW 2002 6 6 HEEA079398 1 20020528 A 3212 206050247135 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4999 53323 EMERGENCY FLOAT COVER END CAPS DO NOT STAY CLOSED. 1 G 7 1 3U O H2SW 2002060600090 20020606 00090 NM 2002 6 6 TSAA0233129 1 20020418 A 3350 1000679 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 35921 23154 REPLACED FORWARD ENTRY DOOR EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2002060600091 20020606 00091 NM 2002 6 6 TSAA0233135 1 20020513 A 3350 9221009 BATTERY PACK BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D NE CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED LEFT OVERWING IDENT EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002060600092 20020606 00092 2002 6 6 HEEA079402 4 20020528 A 3457 13824120234 GPS BELL 206 206L3 1182108 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6610Y 51419 GPS RECEIVER DUMPS WAYPOINTS. REQUIRES CODE WHEN TURNED ON. PERFORMED PRELIMINARY INSPECTION. COULD NOT DUPLICATE PROB LEM. FOUND BATTERY GOOD. FOUND WPT AND AUX BUTTONS INTERMITTENT. REPLACED. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 2002060600093 20020606 00093 2002 6 6 HEEA079403 4 20020528 A 3457 13824120234 GPS BELL 206 206L3 1182108 SW COCKPIT INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 129MR 51129 GPS RECEIVER NAV BUTTON SWITCH INOPERATIVE. 1 G 7 1 3U H2SW 2002060600094 20020606 00094 NM 2002 6 6 TSAA0233136 1 20020509 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 46056 23045 REPLACED NR 6, EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002060600095 20020606 00095 2002 6 6 HEEA079404 4 20020528 A 3457 13824120234 GPS BELL 206 206B3 1181506 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22751 3627 GPS RECEIVER GOES INTO SAFEGUARD MODE WHEN TURNED ON. DISABLED SAFEGUARD CODE. FOUND UNIT TO LOCK UP WHEN SCROLLING THR OUGH WAYPOINTS. RESET MEMORY AND REPROGRAMMED WAYPOINTS. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 2002060600096 20020606 00096 2002 6 6 HEEA079405 4 20020528 A 3457 13824120234 GPS BELL 206 206L1 1182107 SW COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 406EH 45183 GPS RECEIVER LOCKING DEVICE IS INOPERATIVE. FOUND LOCKING DEVICE LOOSE, TIGHTENED, REPAIRED, TESTED AND FOUND UNIT SHOWS TEST FAIL ON PC. 1 G 7 1 3U H2SW 2002060600097 20020606 00097 2002 6 6 HEEA079406 4 20020528 A 3457 1624811 GPS BELL 206 206L1 1182107 SW COCKPIT INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5007N 45184 GPS RECEIVER WILL NOT TRACK SATELLITE. 1 G 7 1 3U H2SW 2002060600098 20020606 00098 SW 2002 6 6 HEEA079407 1 20020528 A 2822 164A1681 PUMP BELL 412 412 1182202 SW FUEL BOOST DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 FUEL BOOST PUMP PRODUCING LOW PRESSURE AND LOUD NOISE. 1 G 7 2 4U H4SW 2002060600099 20020606 00099 SW 2002 6 6 HEEA079408 1 20020528 A 2822 164A1681 PUMP BELL 412 412 1182202 SW FUEL BOOST LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2149S 36002 FUEL BOOST PUMP LEAKING AT WIRE PORT. 1 G 7 2 4U H4SW 2002060600100 20020606 00100 NM 2002 6 6 TSAA0251132 1 20020510 A 5753 654791214 BRACKET BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE T/E FLAP CHAFED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 39494 24031 FOUND NR 8 FLAP JACKSCREW TRAILING EDGE MOUNT BRACKET CHAFFING AT FLAP TRACK FAIRING. BLENDED OUT DAMAGED AREA. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4U 4 F RT A16WE E2EA 2002060600101 20020606 00101 GL 2002 6 6 HEEA079409 2 20020528 A 7261 174000101 FILTER BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE OIL DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 31077 51520 ENGINE OIL FILTER BYPASS BUTTON WEAK. 1 G 7 1 3U 3 U H2SW E1GL 2002060600102 20020606 00102 GL 2002 6 6 HEEA079410 2 20020528 A 7261 1740839 FILTER BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE OIL DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 31801 51074 ENGINE OIL FILTER BYPASS INDICATOR WILL NOT EXTEND. 1 G 7 1 3U 3 U H2SW E1GL 2002060600103 20020606 00103 SW 2002 6 6 HEEA079411 1 20020528 A 6420 20071849H BOLT BELL 214 214ST 1182106 SW T/R HUB BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 TAIL ROTOR HUB BOLT BROKE IN HALF. 2 G 7 2 4U H10SW 2002060600104 20020606 00104 SW 2002 6 6 HEEA079412 1 20020528 A 2435 200SGL1009 BRUSHES BELL 230 230 1182149 SW STARTER GEN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RC 2427XL 23037 STARTER GEN BRUSHES EXCESSIVELY WORN. 1 G 7 2 3U NC H9SW 2002060600105 20020606 00105 SW 2002 6 6 HEEA079413 1 20020528 A 2435 200SGL132Q STARTER GEN BELL 206 206L3 1182108 SW ENGINE INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 30KH 51527 STARTER GENERATOR FAILED TO COME ON LINE. 1 G 7 1 3U H2SW 2002060600106 20020606 00106 NM 2002 6 6 TSAA0253125 1 20020425 A 5711 6545455 SPAR BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 39494 24031 FOUND CORROSION ON RIGHT WING FRONT SPAR, LOWER CHORD FORWARD HORIZONTAL FLANGE FORWARD LIP AT FSS 413. REMOVED CORROSI ON BY BLEND OUT. HFEC AREA TO ENSURE FREE OF CRACKS AND CORROSION. FABRICATED A REPAIR FILLER. INSTALLED REPAIR FILLE R. REPAIR COMPLETED. AIRCRAFT RETURNED TO SURFACE. 2 L 7 2 4U 4 F RT A16WE E2EA 2002060600107 20020606 00107 NM 2002 6 6 TSAA0253126 1 20020423 A 5312 65C33143 BULKHEAD BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 24031 FOUND CRACK ON THE BLK 178 AT WL 212, LBL 5.7 DURING INSPECTION PER ECO 3137. CUT OUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERIFIED CRACK REMOVAL USING HFEC. FABRICATED DOUBLER AND FILLERS. INSTALLED REPAIR PARTS. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4U 4 F RT A16WE E2EA 2002060600108 20020606 00108 NM 2002 6 6 TSAA0253127 1 20020423 A 5312 65C33143 BULKHEAD BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 24031 FOUND CRACK ON THE BLK 178 AT WL 212, RBL 5.7 DURING INSPECTION. CUTOUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERI FIED CRACK REMOVAL USING HFEC. FABRICATED DOUBLER AND FILLERS. INSTALLED REPAIR PART. 2 L 7 2 4U 4 F RT A16WE E2EA 2002060600109 20020606 00109 NM 2002 6 6 TSAA0253128 1 20020423 A 5313 6545788 STRINGER BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 24031 FOUND DENT ACROSS STRINGER 15L AT BS 900. CUTOUT STRINGER SEGMENT AT BS 900. REMOVED THE SEGMENT OF THE STRINGER AFT T O THE PRODUCTION SPLICE. FABRICATED NEW STRINGER SEGMENT. INSTALLED STRINGER PER SRM 53-10-3. COMPLETED REPAIR. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4U 4 F RT A16WE E2EA 2002060600110 20020606 00110 NM 2002 6 6 TSAA0253134 1 20020513 A 5312 6537997 PRESSURE PANEL BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 39494 24031 FOUND CORROSION ON NOSE LANDING GEAR BULKHEAD AT BS 227.8. CUT OUT CORROSION AND VERIFIED REMOVED BY VISUAL INSPECTION. FABRICATED CHORD AND REPAIR ANGLES. INSTALLED CHORD AND REPAIR ANGLES. COMPLETED REPAIR. 2 L 7 2 4U 4 F RT A16WE E2EA 2002060600111 20020606 00111 EU 2002 6 6 USA2002F00002 1 20020502 A 3350 32145510 POWER SUPPLY AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 175US 1064 1496 THE EXIT LIGHT AT 3R DOOR IS INOPERATIVE. MAINTENANCE REPLACED THE 3R DOOR EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED, OK. 2 L 7 2 4F RT A28NM 2002060600112 20020606 00112 EU 2002 6 6 USA2002F00003 1 20020430 A 3260 ABS012110 PROXIMITY SENSOR AIRBUS A319 A319112 3930323 EU NLG FAULTY A USAA K NONE N FALSE WARNING CL CLIMB 1 EA 19 714US 1046 ENROUTE, AFTER TAKEOFF, THE LANDING GEAR DID NOT RETRACT. WHEN THE LANDING GEAR WAS RECYCLED, THE GEAR RETRACTED NORMA LLY. THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NOSE LANDING GEAR PROXIMITY SENSOR 25GA. FUNCTIONALLY CHECKED OK. 2 L 7 2 4F RT A28NM 2002060600113 20020606 00113 NM 2002 6 6 QXEA0200855 1 20020604 A 2130 8209023 VALVE BOMBDR DHC8 DHC8401 NM ZONE 200 FAILED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 404QX 187 187 4046 SEA - AIRCRAFT RETURNED TO FIELD WHEN IT FAILED TO PRESSURIZE ON CLIMB. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLOW CONTROL VALVE. OPERATIONAL CHECK AND LEAK CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002060600114 20020606 00114 2002 6 6 USA2002F00004 4 20020425 A 2565 CABLE AIRBUS 320 A320214 3930316 EU ESCAPE SLIDE BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 105UW 109 0868 FOUND OFFWING EMERGENCY ESCAPE SLIDE INFLATION RESERVOIR RELEASE CABLE END BROKEN OFF. MAINTENANCE REPLACED THE LEFT SI DE OFFWING ESCAPE SLIDE INFLATION RESERVOIR. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2002060600115 20020606 00115 EU 2002 6 6 USA2002F00005 1 20020430 A 2120 ODOR AIRBUS A321 A321211 3930370 EU COCKPIT DETECTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 169UW 1455 ON TAKEOFF, A HOT PLASTIC ODOR WAS NOTED IN THE COCKPIT, AND A LIGHT HAZE WAS NOTED IN THE CABIN. THE SMOKE BEGAN TO DI SSIPATE AFTER POWER REDUCTION. THE FLIGHT CONTINUED AND LANDED, WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED RAM AI R INLETS AND RAN ENGINE ABOVE IDLE FOR 30 MINUTES WITH PACKS ON. NO SMOKE WAS NOTED IN THE CABIN OR COCKPIT. UNABLE TO DUPLICATE. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2002060600116 20020606 00116 NM 2002 6 6 USA2002F00006 1 20020510 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 532AU 24479 IAD MAINTENANCE FOUND THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR EMERGENCY EXIT LIGHTS DIM/WEAK. MAINTENANCE REMOV ED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002060600117 20020606 00117 NM 2002 6 6 USA2002F00007 1 20020508 A 5534 ANGLE BOEING 757 757225 1384959 NM VERTICAL STAB CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AU 22196 SKATE ANGLE, .5000 CHAFED ANGLE- LOWER LEFT SIDE OF VERT FIN FRONT SPAR. REPLACED SKATE ANGLE. 2 L 7 2 4F RT A2NM 2002060600118 20020606 00118 EU 2002 6 6 02FDEA00380 1 20020604 A 2120 OUTFLOW VALVE AIRBUS 310 A310 EU N/A DAMAGED A FDEA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS O OTHER CL CLIMB 1 SO 25 423FE 281 OVBD VALVE FAULT PLACED SWITCH TO OFF PER ECAM A/C WOULD NOT PRESSURIZE MEL 04JUN02 23:17 MEM R ACN RELEASED FOR SERVICE PER MEL/CDL: 21-23-06 EQUIPMENT COOLING OVERBOARD VALVE FAULT LIGHT - INOP. VALVE MANUALLY SET PARTIALLY OP EN. FACT 05JUN02 06:33 MEM R RE-INSTALLED RELAY 69HR, REMOVED AND REPLACED EXTRACT OUTFLOW VALVE, RESET C/B'S, OPS CK'D GOOD ON GROUND. REF A310-200M/M 21-23-13-4 OK FOR SERVICE 2 L 7 2 4F RT A35EU 2002060600119 20020606 00119 NM 2002 6 6 USA2002F00008 1 20020429 A 2781 WARNING SYSTEM BOEING 767 767201 1385125 NM COCKPIT ACTIVATED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 650US 23902 ON APPROACH, CREW RECEIVED THE EICAS MESSAGE (LE SLAT ASYM) AND THE ASSOCIATED LIGHT. CREW BROKE OFF APPROACH AND PERFO RMED A GO AROUND. FLIGHT THEN LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED THE APPROPRIATE FIM PROCEDURE. N O PROBLEMS WERE FOUND AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A1NM 2002060600120 20020606 00120 SW 2002 6 6 HEEA079414 1 20020528 A 6710 204001307103 BOOT BELL 412 412 1182202 SW COLLECTIVE STICK DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 COLLECTIVE STICK BOOT DAMAGED SCRAPPED. 1 G 7 2 4U H4SW 2002060600121 20020606 00121 SW 2002 6 6 HEEA079415 1 20020528 A 6720 204001334101 CYCLIC STICK BELL 412 412 1182202 SW COPILOT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 COPILOT CYCLIC STICK ALIGNMENT HOLE WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060600122 20020606 00122 SW 2002 6 6 HEEA079416 1 20020528 A 6321 204001376003 BRAKE BELL 412 412 1182202 SW ROTOR CONTROL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 ROTOR BRAKE INTERNALLY FAILED. SCRAPPED. 1 G 7 2 4U H4SW 2002060600123 20020606 00123 NE 2002 6 6 USA2002F00009 2 20020514 A 7311 457311261 OIL COOLER BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE LEAKING A USAA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 610AU 26936 27122 ON TAKEOFF, CREW NOTED THE LEFT ENGINE OIL TEMPERATURE WAS HIGH (165 DEGREES C). THE TEMPERATURE DIMINISHED WHEN THE PO WER WAS DECREASED. CREW ALSO NOTED A LIGHT SMOKE/OIL SMELL IN THE COCKPIT. THE FLIGHT RETURNED TO AIRPORT. UPON ARRIV AL, FUEL AND OIL WERE OBSERVED DRIPPING FROM THE LEFT ENGINE. MAINTENANCE REPLACED THE FUEL COOLED OIL COOLER. 2 L 7 2 4F 4 F RT A2NM E12EU 2002060600124 20020606 00124 NM 2002 6 6 USA2002F00010 1 20020515 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 627AU 27805 FOUND SEAT MOUNTED EMERGENCY LIGHTS AT ROWS, 13, 16, AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. 2 L 7 2 4F RT A2NM 2002060600125 20020606 00125 EU 2002 6 6 USA2002F00011 1 20020510 A 3350 CONNECTOR AIRBUS 330 A330323 3930335 EU CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 673UW 0337 THE EPSU TEST FAILED. MAINTENANCE FOUND A LOOSE CONNECTOR AND SECURED IT. THE TEST WAS RERUN. SYSTEM CHECKED NORMAL. 2 L 7 2 4F RT A46NM 2002060600126 20020606 00126 NM 2002 6 6 USA2002F00012 1 20020516 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 617AU 27148 (BATTERY) FOUND EXIT IDENTIFIER AT L1 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. 2 L 7 2 4F RT A2NM 2002060600127 20020606 00127 SW 2002 6 6 HEEA079417 1 20020528 A 6321 204001376003 BRAKE ASSY BELL 412 412 1182202 SW ROTOR LOCKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 ROTOR BRAKE LOCKED UP. 1 G 7 2 4U H4SW 2002060600128 20020606 00128 NM 2002 6 6 USA2002F00013 1 20020516 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 617AU 27148 FOUND EXIT IDENTIFIER AT L1 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. 2 L 7 2 4F RT A2NM 2002060600129 20020606 00129 EU 2002 6 6 USA2002F00014 1 20020516 A 3350 321430 POWER SUPPLY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE L J NO TEST WARNING INDICATION IN INSP/MAINT 1 EA 19 677UW 0380 RECEIVED FAULT MESSAGE (BAT/EPSU 3R (16WL)) MAINTENANCE REPLACED THE EPSU. 2 L 7 2 4F RT A46NM 2002060600130 20020606 00130 EU 2002 6 6 USA2002F00015 1 20020509 A 3350 1012881 LIGHT AIRBUS A319 A319112 3930323 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 713UW 1040 SEAT MOUNTED EMERGENCY LIGHT AT SEAT 11ABC WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. O PERATIONALLY CHECKED OK. 2 L 7 2 4F RT A28NM 2002060600131 20020606 00131 NM 2002 6 6 USA2002F00016 1 20020502 A 1430 BACN10HR3CD NUT BOEING 767 7672B7 1385107 NM RT CDU MISSING A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 652US 24765 (NUT) RIGHT THRUST LEVER STUCK IN IDLE. MAINTENANCE FOUND THE NUT AND WASHER MISSING FROM THE END OF THE RIGHT CDU FEED BACK CABLE AT THE FEEDBACK ROD, AND REPLACED THEM. 2 L 7 2 4F RT A1NM 2002060600132 20020606 00132 NM 2002 6 6 USAA020185 1 20020426 A 5330 SKIN BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 628AU 26189 27806 SKIN CORRODED STA 1310-1660 BETWEEN S27L-S27R AROUND FASTENERS. CLEARED, POLISHED AND BEAD BLASTED AREAS, TREATED AND P AINTED. 2 L 7 2 4F RT A2NM 2002060600133 20020606 00133 SW 2002 6 6 HEEA079418 1 20020528 A 6720 BEARING BELL 412 412 1182202 SW LEVER ASSY WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 TAIL ROTOR ANTI TORQUE SYSTEM LEVER LINKAGE BEARING WORN. SCRAPPED. 1 G 7 2 4U H4SW 2002060600134 20020606 00134 NM 2002 6 6 COOSDR020147 1 20020601 A 5720 ANGLE BOEING 727 727233 138408A NM LT WING CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 LEFT WING REAR SPAR LOWER CHORD ANGLE, CORRODED. 2 L 7 3 4F RT A3WE 2002060600135 20020606 00135 NM 2002 6 6 COOSDR020148 1 20020601 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 MAIN CARGO CABIN - BS 1090 FLOORBEAM UPPER CHORD CORRODED. 2 L 7 3 4F RT A3WE 2002060600136 20020606 00136 NM 2002 6 6 COOSDR020149 1 20020601 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 MAIN CARGO CABIN - BS 1070 FLOORBEAM UPPER CHORD, CORRODED. 2 L 7 3 4F RT A3WE 2002060600137 20020606 00137 NM 2002 6 6 COOSDR020150 1 20020601 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 MAIN CARGO CABIN - BS 620 FLOORBEAM UPPER CHORD, CORRODED. 2 L 7 3 4F RT A3WE 2002060600138 20020606 00138 SW 2002 6 6 HEEA079419 1 20020528 A 6320 204040376003 PRESSURE SWITCH BELL 206 206L3 1182108 SW TRANSMISSION FAILED E HEEA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 03 6748D 51106 TRANSMISSION OIL PRESSURE LIGHT WILL NOT COME ON AFTER SHUTDOWN. SCRAPPED AND REPLACE PRESSURE SWITCH. 1 G 7 1 3U H2SW 2002060600139 20020606 00139 WP 2002 6 6 COOSDR02095 1 20020601 A 5320 5711283514 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT CARGO COMPARTMENT, AT STA 1445 LONGERON 34R LEVEL, SUPPORT FITTING HEAVY CORROSION. 2 L 7 4 4F RT 4A25 2002060600140 20020606 00140 SW 2002 6 6 HEEA079420 1 20020528 A 6320 204040376003 PRESSURE SWITCH BELL 412 412 1182202 SW M/R GEARBOX DAMAGED E K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 WORKING RIVETS ON CONNECTOR END OF THE GEARBOX PRESSURE SWITCH. SCRAPPED. 1 G 7 2 4U H4SW 2002060600141 20020606 00141 WP 2002 6 6 COOSDR02103 1 20020601 A 5523 57025792 SKIN DOUG DC8 DC873F 302199F WP ELEVATOR TAB DAMAGED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 HORIZONTAL STABILIZER RIGHT ELEVATOR GEAR TAB SKIN, INTERNAL DOUBLERS AND HONEY COMB CORE DAMAGE. 2 L 7 4 4F RT 4A25 2002060600142 20020606 00142 SW 2002 6 6 HEEA079421 1 20020528 A 6320 SEAL BELL 412 412 1182202 SW QUILL ASSY LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2149S A2942 36002 MAIN ROTOR GEARBOX QUILL ASSY SEAL LEAKING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060600143 20020606 00143 WP 2002 6 6 COOSDR02104 1 20020601 A 5730 56488941 PANEL DOUG DC8 DC873F 302199F WP LT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 LEFT WING, OUTER WING TRAILING EDGE, UPPER FIXED PANEL DELAMINATED. 2 L 7 4 4F RT 4A25 2002060600144 20020606 00144 WP 2002 6 6 COOSDR02132 1 20020601 A 5730 SKIN DOUG DC9 DC982 3022082 WP LT WING CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 130NJ 49222 LEFT WING, UPPER SURFACE, TRAILING EDGE SKIN AT XRS 267.0 INCHES, CRACKED. 2 L 7 2 4F A6WE 2002060600145 20020606 00145 SW 2002 6 6 HEEA079422 1 20020528 A 6320 204040379003 QUILL ASSY BELL 412 412 1182202 SW M/R GEARBOX LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 107X 33113 MAIN ROTOR GEARBOX QUILL ASSY LEAKING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060600146 20020606 00146 SW 2002 6 6 HEEA079423 1 20020528 A 6320 204040379003 QUILL ASSY BELL 412 412 1182202 SW M/R GEARBOX LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2149S 36002 MAIN ROTOR GEARBOX QUILL ASSY LEAKING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060600147 20020606 00147 WP 2002 6 6 COOSDR02144 1 20020601 A 5310 5936038501 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 813US 48093 AFT CARGO COMPARTMENT DOOR, DOOR JAMB BEAM, CORRODED. 2 L 7 2 4F A6WE 2002060600148 20020606 00148 NM 2002 6 6 COOSDR02146 1 20020601 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 MAIN CARGO CABIN BS 680 FLOOR BEAM UPPER CHORD CORRODED. 2 L 7 3 4F RT A3WE 2002061000295 20020610 00295 WP 2002 6 10 P2EA2002MO36 1 20020524 A 3222 5920603507 PISTON DOUG DC9 DC982 3022082 WP NLG STRUT FLAKING A P2EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 140NJ 9361 9361 49931 NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, RETURNED TO MCI FOR UNSCHEDULED LANDING. DURING INSPECTION, ON JACKS, FOUND CADMIUM PLATING FLAKING OFF THE NLG PISTON. REMOVED AND REPLACED PISTON AND AXLE ASSEMBLY IAW 32-21-02. DURING TE ARDOWN FOUND BEARING, P/N 5961561-1 AND RETAINER, P/N 3962423-1 SCRATCHED AND PARTS OF THE PLATING EMBEDDED ON SURFACE. BEARING AND RETAINER REPLACED IAW MM 32-21-02. OPERATIONAL CHECK IAW 32-30-00, NO DEFECTS NOTED. 2 L 7 2 4F A6WE 2002060600149 20020606 00149 NM 2002 6 6 COOSDR02151 1 20020601 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69741 22250 LOWER FUSELAGE SKIN CORRODED, BETWEEN STA 481 AND STA 500-STR 28R. 2 L 7 3 4F A3WE 2002060600150 20020606 00150 2002 6 6 000166 4 20020604 A 3140 WARNING SYSTEM EMB 145 EMB145 3260210 SO COCKPIT ACTIVATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 262 E2 ATTCS NO MARGIN EICAS MESSAGE. 2 L 7 2 4F RT T00011AT 2002060600152 20020606 00152 SW 2002 6 6 HEEA079424 1 20020528 A 6510 BALANCE WEIGHT BELL 412 412 1182202 SW T/R DRIVESHAFT SEPARATED E HEEA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SW 03 1202T A1709 33112 FOUND ONE BALANCE WEIGHT ON ENGINE DECK CAME OFF THE TAIL ROTOR DRIVESHAFT IN FLIGHT. 1 G 7 2 4U H4SW 2002060600153 20020606 00153 SW 2002 6 6 HEEA079425 1 20020528 A 6510 204040620011 DRIVE SHAFT BELL 412 412 1182202 SW TAIL ROTOR DENTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 TAIL ROTOR DRIVESHAFT DENTED. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060600154 20020606 00154 SO 2002 6 6 C2XA02BT022 1 20020606 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14952 145067 DURING SERVICE/ROUTINE CHECK ON OVERNIGHT MAINTENANCE FOUND EMERGENCY LIGHT ON PASSENGER DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULB ON PASSENGER DOOR IAW EMB145 AMM #33-50-06. OPS. CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2002060600155 20020606 00155 NM 2002 6 6 C1HA200282012 1 20020605 A 3350 900542 POWER SUPPLY BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 682CA 22019 LEFT WING CENTER EMERGENCY LIGHT COVERWING INOP. R&R BATTERY POWER SUPPLY IAW MM 33-50-22. ALL OPS CKS NORMAL. 2 L 7 3 4F A3WE 2002060600157 20020606 00157 SW 2002 6 6 HEEA079426 1 20020528 A 6510 BALANCE WEIGHT BELL 412 412 1182202 SW T/R DRIVESHAFT MISSING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH A1314954 33150 MISSING BALANCE WEIGHTS. SCRAPPED. 1 G 7 2 4U H4SW 2002060600160 20020606 00160 SW 2002 6 6 HEEA079428 1 20020528 A 3040 2315M245 WINDSHIELD WIPER BELL 412 412 1182202 SW WINDSHIELD WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 WINDSHIELD WIPER HAS WORN BLADES. SCRAPPED. 1 G 7 2 4U H4SW 2002060600162 20020606 00162 SW 2002 6 6 HEEA079429 1 20020528 A 3040 STRUCTURE BELL 412 412 1182202 SW WINDSHIELD WIPER CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 WINDSHIELD WIPER HAS CORRODED HARDWARE AND MOUNTING BRACKET. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060600163 20020606 00163 EU 2002 6 6 02FDEA00377 1 20020604 A 3411 PITOT TUBE AIRBUS 300 A300F4605R 3930327 EU PITOT/STATIC SYS OBSTRUCTED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 667FE 771 PDIS- ON TAKEOFF AT 80 KNOTS CALL BY 1ST OFF, CAPT'S AIRSPEED IND STILL READ ZERO (NO TREND). REMOVED BUG FROM PITOT TU BE, OPS CHECK PITOT SYSTEM PER MM 34-10-00-5. 2 L 7 2 4F RT A35EU 2002060600164 20020606 00164 EU 2002 6 6 02FDEA00378 1 20020604 A 3411 PITOT LINE AIRBUS 310 A310 EU PITOT/STATIC SYS OBSTRUCTED A FDEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 25 443FE 283 MDIS- FIRST OFFICERS AIRSPEED IND INOP ON ELECTRONIC FLT INSTRUMENT SYSTEM. DISCONNECTED FIRST OFFICERS PITOT CONNECTIO N FOUND BLOCKAGE, CLEANED PITOT LINE AND RECONNECTED. BLEW PITOT NR 2 SYSTEM AIR LINES OUT AND RECONNECTED PITOT LINES. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2002060600166 20020606 00166 2002 6 6 2002F00532 4 20020531 A 3460 4052506955 FMC BOEING 757 75723N 1384973 NM E/E BAY FAILED G AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 523AT 10317 10317 30232 FLIGHT NUMBER 710, RIGHT FMC FAILED ON TAXI OUT. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE R IGHT FMC COMPUTER IN ACCORDANCE WITH MM 34-61-01-024, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002060600167 20020606 00167 WP 2002 6 6 2002F00533 1 20020508 A 5312 PRESSURE PANEL LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 197AT 193P1082 DURING SCHEDULED INSPECTION THE LEFT MAIN LANDING GEAR WHEEL WELL UPPER PRESSURE DECK SKIN FS 1260, LBL 115 HAD LEVEL 2 CORROSION. MAINTENANCE REPAIRED PRESSURE DECK IN ACCORDANCE WITH ER/A L10-53R-4794. 2 L 7 3 4F A23WE 2002060600168 20020606 00168 SW 2002 6 6 HEEA079430 1 20020528 A 5311 205030161101 FRAME BELL 412 412 1182202 SW FUSELAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 36003 MAIN FRAME CAP CRACKED IN RADIUS AT STATION 166, WL 11.587. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060600169 20020606 00169 SW 2002 6 6 HEEA079431 1 20020528 A 5310 205030280141 STRUCTURE BELL 412 412 1182202 SW SERVICE DECK SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 SERVICE DECK STRUCTURE HAS SEPARATED. 1 G 7 2 4U H4SW 2002060600170 20020606 00170 SW 2002 6 6 HEEA079432 1 20020528 A 5302 205032813067 ACCESS PANEL BELL 412 412 1182202 SW TAIL BOOM DEBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 TAILBOOM BAGGAGE ACCESS PANEL DEBONDED. 1 G 7 2 4U H4SW 2002060600171 20020606 00171 WP 2002 6 6 2002F00534 1 20020516 A 5311 FRAME LKHEED 1011 10113851 5265010 WP FUSELAGE CRACKED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 197AT 193P1082 DURING SCHEDULED INSPECTION THE LEFT MAIN LANDING GEAR WHEEL WELL, LEFT FRAME FS 1266, WL 168, LBL 125 HAD ONE CRACK 1.0 0 INCHES IN LENGTH. MAINTENANCE REPLACED FRAME SEGMENT IN ACCORDANCE WITH SRM 51-40-01. 2 L 7 3 4F A23WE 2002060600172 20020606 00172 WP 2002 6 6 2002F00535 1 20020519 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 198AT 193B1111 DURING SCHEDULED INSPECTION THE CABIN FLOORBEAM, T-CAP AT FS 901, LBL 30 TO RBL 30 HAD SEVERAL AREAS OF LEVEL 2 CORROSIO N. MAINTENANCE REPAIRED DAMAGED T-CAP SECTION IN ACCORDANCE WITH SRM 53-23-00 AND 51-40-01. 2 L 7 3 4F A23WE 2002071800126 20020718 00126 EU 2002 7 18 2002UALA00770 1 20020527 A 5230 PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO DOOR STIFF A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 429UA 539 AFT CARGO DOOR ECAM WARNING ILLUMINATED. FOUND DOOR HANDLE PLATE STIFF. REMOVED PLATE, CLEANED, LUBED AND REINSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002060600173 20020606 00173 SW 2002 6 6 HEEA079433 1 20020528 A 5302 205032834101S COVER BELL 412 412 1182202 SW TAILBOOM CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 TAILBOOM TO HORIZONTAL RADIUS COVER CRACKED. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060600174 20020606 00174 SW 2002 6 6 HEEA079434 1 20020528 A 2822 205060606003 PUMP BELL 412 412 1182202 SW FUEL BOOST FLUCTUATES E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 107X 33113 FUEL BOOST PUMP MAKING LOUD GROWLING NOISE AND PRESSURE FLUCTUATING. 1 G 7 2 4U H4SW 2002060600175 20020606 00175 SW 2002 6 6 HEEA079435 1 20020528 A 2822 205060606003 PUMP BELL 412 412 1182202 SW FUEL BOOST MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 107X 33113 FUEL BOOST PUMP POPPING CIRCUIT BREAKER. 1 G 7 2 4U H4SW 2002060600176 20020606 00176 SW 2002 6 6 HEEA079436 1 20020528 A 2822 205060606003 PUMP BELL 412 412 1182202 SW FUEL BOOST MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22608 33075 LT FUEL BOOST PUMP CAUSES NOISE IN ADF AUDIO. 1 G 7 2 4U H4SW 2002060600177 20020606 00177 SW 2002 6 6 HEEA079437 1 20020528 A 2822 205060606003 PUMP BELL 412 412 1182202 SW FUEL BOOST INOPERATIVE E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 2149S 36002 FUEL BOOST PUMP QUIT IN FLIGHT. 1 G 7 2 4U H4SW 2002060600179 20020606 00179 SW 2002 6 6 HEEA079438 1 20020528 A 2140 205072277009 VALVE BELL 412 412 1182202 SW HEATER MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1202T 33112 HEATER MIXING VALVE PRODUCING LOW OUTPUT. 1 G 7 2 4U H4SW 2002060600180 20020606 00180 SW 2002 6 6 HEEA079439 1 20020528 A 2140 205072277009 VALVE BELL 412 412 1182202 SW HEATER INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893N 33010 HEATER MIXING VALVE INOPERATIVE. 1 G 7 2 4U H4SW 2002060600181 20020606 00181 SW 2002 6 6 HEEA079440 1 20020528 A 2910 205076044007 PRESSURE SWITCH BELL 412 412 1182202 SW HYD SYSTEM INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 PRESSURE SWITCH INTERMITTENTLY CAUSES LIGHT TO COME ON WITH PRESSURE APPLIED. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060600185 20020606 00185 NM 2002 6 6 372PA0009 1 20020601 A 2600 G718904 CONTROL PANEL BOEING 737 737306 NM DIRTY A PIDA O OTHER J WARNING INDICATION DE DESCENT 1 SO 05 372PA 23546 Bottles in cargo bay 1&2 auto discharged w/no fire or smoke. R&R bottles and control panel. 2 L 7 2 4F RT A16NE 2002060600186 20020606 00186 WP 2002 6 6 2002F00536 1 20020512 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION AT AFT CARGO BAY FRAME, AT STATION 1964, FROM L52 TO L45R. (M) 2 L 7 3 4F A22WE 2002060600187 20020606 00187 SW 2002 6 6 HEEA079441 1 20020528 A 6720 206001055001 BEARING BELL 206 206B3 1181506 SW ANTI TORQUE SYS CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2753F 2729 TAIL ROTOR ANTI TORQUE LINKAGE BEARING CORRODED AND RUSTY. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600188 20020606 00188 WP 2002 6 6 2002F00537 1 20020512 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY, AT FLOORBOARD AND BULKHEAD PANEL SUPPORT ANGLES, AT STATION 1967. (M) 2 L 7 3 4F A22WE 2002060600189 20020606 00189 WP 2002 6 6 2002F00538 1 20020514 A 5320 STRUCTURE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT WASTE SYSTEM COMPARTMENT, ON BOTH SERVICE PANELS, AT STATION 1967 TO 1986, L48L AND L 48R. (M) 2 L 7 3 4F A22WE 2002060600190 20020606 00190 WP 2002 6 6 2002F00539 1 20020517 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON AFT GALLEY TIE DOWN SUPPORT PLATE, AT STATION 1897, LBL 6. (M) 2 L 7 3 4F A22WE 2002060600191 20020606 00191 SW 2002 6 6 HEEA079442 1 20020528 A 6720 206001052001 BEARING BELL 206 206L3 1182108 SW COLLECTIVE UNSTAKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3108E 51498 COLLECTIVE CONTROL LINKAGE BEARING UNSTAKED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600192 20020606 00192 SW 2002 6 6 HEEA079443 1 20020528 A 6720 BEARING BELL 206 206L3 1182108 SW T/R CONTROL TUBE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 205FC 51130 TAIL ROTOR CONTROL TUBE HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600193 20020606 00193 SW 2002 6 6 HEEA079444 1 20020528 A 6720 BEARING BELL 206 206L3 1182108 SW T/R CONTROL TUBE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6603X 51412 TAIL ROTOR CONTROL TUBE HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600194 20020606 00194 SW 2002 6 6 HEEA079445 1 20020528 A 6710 206001096001 TUBE BELL 206 206B3 1181506 SW CYCLIC CONTROL CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2753F 2729 CYCLIC CONTROL LINKAGE TUBE IS CORRODED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600195 20020606 00195 NM 2002 6 6 371PA0006 1 20020531 A 3350 362624 LIGHT BOEING 737 737306 NM A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 Aft floor emergency lighting inop. R&R light strip and fuse. 2 L 7 2 4F RT A16NE 2002060600196 20020606 00196 SW 2002 6 6 HEEA079446 1 20020528 A 6710 206001099001 TUBE BELL 206 206B3 1181506 SW CYCLIC CONTROL CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2753F 2729 CORROSION ON OUTSIDE OF TUBE CHAMFER EDGE. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600197 20020606 00197 SW 2002 6 6 HEEA079447 1 20020528 A 6710 206001144021 TUBE BELL 206 206L3 1182108 SW CYCLIC CONTROL CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81SP 51029 CYCLIC CONTROL TUBE IS CORRODED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600198 20020606 00198 SW 2002 6 6 HEEA079448 1 20020528 A 6710 206001194005 TUBE BELL 206 206B3 1181506 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2753F 2729 CONTROL TUBE HAS CORROSION ON INSIDE OF TUBE CHAMFER EDGE. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600199 20020606 00199 SW 2002 6 6 HEEA079449 1 20020528 A 6710 206001330001 SUPPORT BELL 206 206B3 1181506 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2753F 2729 CYCLIC CONTROL LINKAGE SUPPORT CORRODED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600200 20020606 00200 SW 2002 6 6 HEEA079450 1 20020528 A 6710 206001343001 ELBOW BELL 206 206L3 1182108 SW M/R LINKAGE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81SP 51029 CYCLIC CONTROL LINKAGE ELBOW CORRODED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600201 20020606 00201 WP 2002 6 6 2002F00541 1 20020517 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION AT LEFT OUTBOARD SEAT TRACK CLIP NUT HOLES, FROM STATION 1942 TO 1964. (M) 2 L 7 3 4F A22WE 2002060600202 20020606 00202 WP 2002 6 6 2002F00542 1 20020517 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-EHCK, FOUND CORROSION AT GALLEY FLOOR SUPPORTS CLIP NUT HOLES, AT STATION 1911, RBL 50 TO RBL 82, AND LBL 50 TO LBL 82. (M) 2 L 7 3 4F A22WE 2002060600203 20020606 00203 WP 2002 6 6 2002F00543 1 20020517 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON AFT GALLEY FLOOR SUPPORT AT LBL 52, FROM STATION 1909-1964. (M) 2 L 7 3 4F A22WE 2002060600204 20020606 00204 WP 2002 6 6 2002F00544 1 20020517 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON TWO AFT GALLEY SUPPORT TRACKS, AT LBL 17 AND RBL 17, FROM STATION 1921 TO 1964. (M) 2 L 7 3 4F A22WE 2002060600205 20020606 00205 WP 2002 6 6 2002F00545 1 20020517 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON TWO AFT GALLEY SUPPORT TRACKS, AND THE ATTACHING PLATE, AT STATION 1966, BETWEEN RBL 37 T O RBL 43. (M) 2 L 7 3 4F A22WE 2002060600206 20020606 00206 WP 2002 6 6 2002F00546 1 20020517 A 5320 WEB DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND AFT LAV FLOOR WEB EXFOLIATED AT STATION 1964, RBL 32. (M) 2 L 7 3 4F A22WE 2002060600207 20020606 00207 WP 2002 6 6 2002F00547 1 20020517 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION AT FASTENER HOLES OF FLOOR SUPPORT IN AFT GALLEY, AT STATION 1942, FROM RBL 24 TO RBL 44. ( M) 2 L 7 3 4F A22WE 2002060600208 20020606 00208 SW 2002 6 6 HEEA079451 1 20020528 A 6700 BEARING BELL 206 206L1 1182107 SW IDLER LINKAGE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5007Q 45187 IDLER LINKAGE HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600209 20020606 00209 WP 2002 6 6 2002F00548 1 20020517 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON AFT GALLEY SUPPORT TRACK, AT STATION 1964, RBL 77. (M) 2 L 7 3 4F A22WE 2002060600210 20020606 00210 WP 2002 6 6 2002F00549 1 20020517 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION AT AFT LAV/GALLEY AREA FLOOR SUPPORTS, AT STATION 1964, FROM LBL 19 TO LBL 50. (M) 2 L 7 3 4F A22WE 2002060600211 20020606 00211 SW 2002 6 6 HEEA079452 1 20020528 A 6700 BEARING BELL 206 206L3 1182108 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30KH 51527 ROTOR CONTROL BELLCRANK HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600212 20020606 00212 WP 2002 6 6 2002F00550 1 20020517 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON THREE AFT GALLEY FLOOR SUPPORTS AT LBL 12, BL 0 AND RBL 12, FROM STATION 1890-1921. (M) 2 L 7 3 4F A22WE 2002060600213 20020606 00213 SW 2002 6 6 HEEA079453 1 20020528 A 6700 BEARING BELL 206 206L3 1182108 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31077 51520 ROTOR CONTROL BELLCRANK HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600214 20020606 00214 WP 2002 6 6 ABXA010909 1 20020510 A 5730 591348839 PANEL DOUG DC9 DC933F 302207A WP LEFT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 LEFT WING LOWER INBOARD BONDED PANEL HAD A LARGE AREA OF DELAMINATION AROUND FASTENERS. REPLACED BONDED PANEL IAW DC-9 S RM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 2002060600215 20020606 00215 WP 2002 6 6 ABXA010910 1 20020519 A 5300 56418502 FITTING DOUG DC9 DC933F 302207A WP FUSELAGE RUSTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 STEEL BEAM ABOVE THE RIGHT CLEARVIEW WAS RUSTED ON THE AFT END, BOTH INSIDE AND OUTSIDE OF BEAM. REPLACED BEAM IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2002060600216 20020606 00216 WP 2002 6 6 2002F00551 1 20020517 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT GALLEY AREA FLOOR SUPPORTS, AT CLIP NUTS AT FLOORBEAM STATION 1921, FROM LBL 50 THROU GH RBL 50. (M) 2 L 7 3 4F A22WE 2002060600217 20020606 00217 SW 2002 6 6 HEEA079454 1 20020528 A 6700 BEARING BELL 206 206L3 1182108 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 42EA 51542 ROTOR CONTROL BELLCRANK HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600218 20020606 00218 WP 2002 6 6 2002F00552 1 20020517 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON AFT GALLEY FLOOR SUPPORT, AT RBL 50, FROM STATION 1910 TO 1966. (M) 2 L 7 3 4F A22WE 2002060600219 20020606 00219 2002 6 6 250TR0004 4 20020531 A 2211 2589918902 POTENTIOMETER BOEING 737 7372K5 138448X NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 250TR 22597 "A" Auto-pilot jerky in all modes. R&R stab trim potentiometer. 2 L 7 2 4F RT A16WE 2002060600220 20020606 00220 WP 2002 6 6 2002F00553 1 20020517 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION AT RIGHT OUTBOARD SEAT TRACK CLIP NUTS, AT STATION 1887 TO 1960. (M) 2 L 7 3 4F A22WE 2002060600221 20020606 00221 SW 2002 6 6 HEEA079455 1 20020528 A 6700 BEARING BELL 206 206L4 1182110 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7074W 52033 ROTOR CONTROL BELLCRANK HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U NC H2SW 2002060600222 20020606 00222 WP 2002 6 6 2002F00554 1 20020517 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON AFT GALLEY SUPPORT TRACK, FROM STATION 1964 TO 2007, LBL 43. (M) 2 L 7 3 4F A22WE 2002060600223 20020606 00223 SW 2002 6 6 HEEA079456 1 20020528 A 6710 206001713101 SUPPORT BELL 206 206L3 1182108 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81SP 51029 MAIN ROTOR CONTROL LINKAGE SUPPORT IS CORRODED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600224 20020606 00224 WP 2002 6 6 2002F00555 1 20020517 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON AFT GALLEY SUPPORT TRACK, AT STATION 1965, RBL 3. (M) 2 L 7 3 4F A22WE 2002060600225 20020606 00225 SW 2002 6 6 HEEA079457 1 20020528 A 6720 BEARING BELL 206 206L3 1182108 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3108E 51498 TAIL ROTOR CONTROL BELLCRANK CENTER BEARING IS WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600226 20020606 00226 WP 2002 6 6 2002F00556 1 20020517 A 5320 STIFFENER DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION AT AFT PRESSURE BULKHEAD HORIZONTAL STIFFENER, AT STATION 2007, 5 INCHES BELOW FLOORLINE, FR OM RBL 25 TO RBL 73. (M) 2 L 7 3 4F A22WE 2002060600227 20020606 00227 SW 2002 6 6 HEEA079458 1 20020528 A 6210 206010200133 BLADE BELL 206 206B3 1181506 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2275Y 878 3626 MAIN ROTOR BLADE NR 2 LOWER DOUBLER SEPARATED APPROX. 4 1/2 INCH LONG WHICH EXTENDS UNDERNEATH THE NR 3 FINGER. 1 G 7 1 3U H2SW 2002060600228 20020606 00228 WP 2002 6 6 2002F00557 1 20020517 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, X-RAY INSPECTION INDICATES A CRACK IN LEFT FLOORBEAM LOWER CAP, AT FLOOR STRUT INTERSECTION LOWER OUTBOARD F ASTENER, AT STATION 879 LEFT. (M) 2 L 7 3 4F A22WE 2002060600229 20020606 00229 SW 2002 6 6 HEEA079459 1 20020528 A 6210 206010200133 BLADE BELL 206 206B3 1181506 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2268V 1570 3605 MAIN ROTOR BLADE HAS A HOLE IN THE SKIN ON THE LOWER SIDE AT STATION 66 AND 2 7/8 INCHES FROM THE TRAILING EDGE. 1 G 7 1 3U H2SW 2002060600230 20020606 00230 WP 2002 6 6 2002F00558 1 20020518 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FORWARD SIDE OF WEB AT PASSENGER COMPARTMENT FLOORBEAM, AT STATION 555 LEFT, AT LBL 67. (M) 2 L 7 3 4F A22WE 2002060600231 20020606 00231 WP 2002 6 6 2002F00559 1 20020517 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND EXFOLIATED CORROSION AT PASSENGER COMPARTMENT FLOORBEAM, LOWER CAP, AT PRESSURE PANEL FORWARD SIDE, AT STATION 555 LEFT, LBL 67. (M) 2 L 7 3 4F A22WE 2002060600232 20020606 00232 SW 2002 6 6 HEEA079460 1 20020528 A 7931 206075677103 INDICATOR BELL 206 206L3 1182108 SW ENGINE OIL PRESS READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3108E 51498 ENGINE OIL PRESSURE INDICATOR READS LOW. 1 G 7 1 3U H2SW 2002060600233 20020606 00233 WP 2002 6 6 2002F00560 1 20020517 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON UPPER SURFACE OF MAIN CABIN SEAT TRACK, AT RBL 10. (M) 2 L 7 3 4F A22WE 2002060600234 20020606 00234 WP 2002 6 6 2002F00561 1 20020517 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION AT AFT GALLEY FLOOR SUPPORTS AND FLOORBEAM, IN NUMEROUS PLACES, AT STATION 1887 FROM LBL 87 TO RBL 87. (M) 2 L 7 3 4F A22WE 2002060600235 20020606 00235 WP 2002 6 6 2002F00562 1 20020515 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON AFT FACE OF SHEAR TIE, AT STATION 1721, BETWEEN STRINGERS 51R AND 52. (M) 2 L 7 3 4F A22WE 2002060600236 20020606 00236 WP 2002 6 6 2002F00563 1 20020515 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FORWARD AND AFT SIDES OF SHEAR TIE, AT STATION 1741, BETWEEN STRINGERS 51R AND 52. (M) 2 L 7 3 4F A22WE 2002060600237 20020606 00237 WP 2002 6 6 2002F00564 1 20020515 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FORWARD SIDE OF SHEAR TIE, AT STATION 1112, BETWEEN LONGERONS 51L AND 52. (M) 2 L 7 3 4F A22WE 2002060600238 20020606 00238 EU 2002 6 6 AALA20020593 1 20020503 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1406A 11359 (LIGHT) DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT TRACK LIGHT AFT OF ROW 11, INOPERATIVE. CYCLES FROM DIM TO OFF. RE PLACED 4 FOOT SECTION OF EMERGENCY EXIT FLOOR PATH LIGHTING IN FORWARD ZONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2002060600239 20020606 00239 EU 2002 6 6 AALA20020598 1 20020502 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1402K 11353 (LIGHT ASSEMBLY) DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS, INOPERATIVE. REPLACED EMERGENCY EXIT F LOOR PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2002060600240 20020606 00240 EU 2002 6 6 AALA20020638 1 20020512 A 3397 GROUND WIRE FOKKER F28 F28MK0100 4990807 EU CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1425A 11408 (WIRE) DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT SIGN AT R1 DOOR INOPERATIVE. REPAIRED GROUND WIRE ON EMERGENCY EXIT SIGN R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2002060600241 20020606 00241 EU 2002 6 6 AALA20020639 1 20020512 A 3350 MODULE FOKKER F28 F28MK0100 4990807 EU CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1425A 11408 (LIGHT MODULE) DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH PROXIMITY POWER PACK INDICATED INOPERATIVE. RESE ATED EMERGENCY EXIT FLOOR PATH MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2002060600242 20020606 00242 NM 2002 6 6 AALA20020704 1 20020510 A 2761 ACTUATOR BOEING 757 757223 1384957 NM SPOILER LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 640A 24598 ACTUATOR, EN ROUTE, SJC-BOS RIGHT SYSTEM HYDRAULIC QUANTITY MESSAGE ON EICAS. HYDRAULIC QUANTITY INDICATED .47. SECURE D RIGHT SYSTEM PER OPERATIONS MANUAL. AIR INTERRUPTED MSP AND LANDED WITHOUT INCIDENT. REPLACED NUMBER 7 SPOILER POWER CONTROL ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2002080500056 20020805 00056 2002 8 5 377PA0001 4 20020602 A 2565 1061323541 SLIDE BOEING 737 7373L9 1384470 NM L1 DOOR UNSERVICEABLE A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 377PA 23718 L1 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE. 2 L 7 2 4F RT A16WE 2002060600243 20020606 00243 NM 2002 6 6 AALA20020706 1 20020516 A 2910 HYDRAULIC LINE BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 635AA 24593 (HYDRAULIC LINE) ENROUTE, LEFT HAND HYDRAULIC SYSTEM LOSS OF ALL FLUID IN FLIGHT. RETURNED TO AIRPORT AND LANDED WITHOU T INCIDENT. REPLACED HYDRAULIC LINE TO DOWNLOCK ACTUATOR, ENGINE DRIVEN PUMP AND ENGINE DRIVEN PUMP FILTERS. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2002060600244 20020606 00244 NM 2002 6 6 AALA20020710 1 20020516 A 3350 S283T0143 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39356 24037 DURING OVERNIGHT MAINTENANCE EMERGENCY ESCAPE PATH LIGHTS AT 2H, 3H, 7H, AND 8H INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (K) 2 L 7 2 4F RT A1NM 2002060600245 20020606 00245 NM 2002 6 6 AALA20210708 1 20020512 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 387AM 27184 DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT 26H INOPERATIVE. SECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT S EAT 26H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2002060600246 20020606 00246 WP 2002 6 6 COOSDR020081 1 20020601 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 MAIN CARGO CABIN FITTING, CORRODED. 2 L 7 4 4F RT 4A25 2002060600247 20020606 00247 WP 2002 6 6 COOSDR020082 1 20020601 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT CARGO COMPARTMENT FITTING, CRACKED. 2 L 7 4 4F RT 4A25 2002060600248 20020606 00248 WP 2002 6 6 COOSDR020083 1 20020601 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT CARGO COMPARTMENT FITTING, CRACKED. 2 L 7 4 4F RT 4A25 2002060600249 20020606 00249 WP 2002 6 6 COOSDR020084 1 20020601 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 MAIN CARGO CABIN FITTING, CORRODED. 2 L 7 4 4F RT 4A25 2002060600250 20020606 00250 WP 2002 6 6 COOSDR020085 1 20020601 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT CARGO COMPARTMENT SUPPORT ANGLE CRACKED. 2 L 7 4 4F RT 4A25 2002060600251 20020606 00251 WP 2002 6 6 COOSDR020086 1 20020601 A 5720 STIFFENER DOUG DC8 DC873F 302199F WP LT WING CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 LEFT WING TRAILING EDGE FIXED PANEL STIFFENER, CRACKED. 2 L 7 4 4F RT 4A25 2002060600252 20020606 00252 WP 2002 6 6 COOSDR020087 1 20020601 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT LOWER CARGO COMPARTMENT, FITTING CRACKED. 2 L 7 4 4F RT 4A25 2002060600253 20020606 00253 WP 2002 6 6 COOSDR020088 1 20020601 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 AFT LOWER CARGO COMPARTMENT, FITTING CORRODED. 2 L 7 4 4F RT 4A25 2002060600254 20020606 00254 WP 2002 6 6 COOSDR020089 1 20020601 A 5753 FLAP DOUG DC8 DC873F 302199F WP RT WING DAMAGED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 RIGHT WING INBOARD FLAP BAKELITE, DAMAGED. 2 L 7 4 4F RT 4A25 2002060600255 20020606 00255 NM 2002 6 6 COOSDR020114 1 20020601 A 5230 DOOR FRAME BOEING 727 72723 1384004 NM CARGO DOOR CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 AFT CARGO COMP. DOOR UPPER SECTION HINGE AREA JAMB CRACKED. 2 L 7 3 4F A3WE 2002060600256 20020606 00256 NM 2002 6 6 COOSDR020115 1 20020601 A 5230 DOOR FRAME BOEING 727 72723 1384004 NM CARGO DOOR CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 AFT CARGO COMP. DOOR UPPER SECTION HINGE AREA JAMB CRACKED. 2 L 7 3 4F A3WE 2002060600257 20020606 00257 NM 2002 6 6 COOSDR020152 1 20020601 A 5720 STIFFENER BOEING 727 727233 138408A NM LT WING CRACKED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 LEFT WING - NR 17 UPPER STIFFENER CRACKED AT WS 330.50. 2 L 7 3 4F RT A3WE 2002060600258 20020606 00258 NM 2002 6 6 COOSDR02105 1 20020601 A 5730 SKIN BOEING 727 727233 138408A NM RT WING CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 RIGHT WING, LOWER SKIN PANEL, INBOARD BOOST PUMP-CUTOUT, CORRODED. 2 L 7 3 4F RT A3WE 2002060600259 20020606 00259 NM 2002 6 6 COOSDR02106 1 20020601 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 BS 950C FLOOR BEAM UPPER CHORD CORRODED FROM RBL 48 TO RBL 60 AND FROM LBL 46 TO LBL 60. 2 L 7 3 4F RT A3WE 2002060600260 20020606 00260 NM 2002 6 6 COOSDR02107 1 20020430 A 5311 6516312132 FAILSAFE BOEING 727 72723 1384004 NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 NOSE WHEEL WELL, STA 294.5 FAIL SAFE CHORD CRACKED. 2 L 7 3 4F A3WE 2002060600261 20020606 00261 NM 2002 6 6 COOSDR02108 1 20020601 A 5743 BEAM BOEING 727 727233 138408A NM LT WING CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 LEFT WING, REAR TRUNNION SUPPORT BEAM - WBL 124.2, LOWER SURFACE CORRODED. 2 L 7 3 4F RT A3WE 2002060600262 20020606 00262 NM 2002 6 6 COOSDR02109 1 20020601 A 5514 BEAM BOEING 727 727233 138408A NM HORIZ STAB CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 LEFT HORIZONTAL STAB, TRAILING EDGE BEAM UPPER CHORD AT STAB STA 198 INCHES WITH CORROSION. 2 L 7 3 4F RT A3WE 2002060600263 20020606 00263 SW 2002 6 6 HEEA079461 1 20020528 A 7931 206075678103 INDICATOR BELL 206 206L3 1182108 SW ENGINE OIL PRESS READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3108E 51498 TRANSMISSION OIL PRESSURE READING 25 LBS LOW. SENT TO MASCO FOR INSPECTION AND REPAIR. 1 G 7 1 3U H2SW 2002060600264 20020606 00264 SW 2002 6 6 HEEA079462 1 20020528 A 7720 206075680103 INDICATOR BELL 206 206B3 1181506 SW TOT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 103PH 3000 READS ZERO WITH T1000 AND BARFIELD. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600265 20020606 00265 SW 2002 6 6 HEEA079463 1 20020528 A 7720 206075680103 INDICATOR BELL 206 206B3 1181506 SW TOT INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2275Y 3626 INDICATOR WOULD DROP TO ZERO DURING CRUISE FLIGHT THEN RETURN TO NORMAL READINGS. 1 G 7 1 3U H2SW 2002060600266 20020606 00266 SW 2002 6 6 HEEA079464 1 20020528 A 7720 206075680107 INDICATOR BELL 206 206B3 1181506 SW TOT INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 OVERTEMP LAMP ILLUMINATED WHEN BATTERY CYCLED ON. RESET LAMP OFF BUT ILLUMINATED AGAIN. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600267 20020606 00267 SW 2002 6 6 HEEA079465 1 20020528 A 7720 206075680107 INDICATOR BELL 206 206L3 1182108 SW TOT MALFUNCTIONED E HEEA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 03 6603X 51412 OVERTEMP LAMP ILLUMINATED. COULD RESET BUT LAMP WOULD RE-ILLUMINATE WHEN BATTERY SWITCH CYCLED. REPLACED WITH SERVICEAB LE PART. 1 G 7 1 3U H2SW 2002060600268 20020606 00268 SW 2002 6 6 HEEA079466 1 20020528 A 6730 206076031023 SERVO BELL 206 206B3 1181506 SW ROTOR SERVO SYS LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2753F 2729 ROTOR SERVO LEAKING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600269 20020606 00269 SW 2002 6 6 HEEA079467 1 20020528 A 6730 206076031023 SERVO BELL 206 206B3 1181506 SW ROTOR SERVO SYS LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2753F 2729 ROTOR SERVO LEAKING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600270 20020606 00270 SW 2002 6 6 HEEA079468 1 20020528 A 6730 206076031023 SERVO BELL 206 206B3 1181506 SW ROTOR SERVO SYS LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2753F 2729 ROTOR SERVO SYS LEAKING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600271 20020606 00271 SW 2002 6 6 HEEA079469 1 20020528 A 6321 206076047003 CYLINDER BELL 206 206L3 1182108 SW ROTOR BRAKE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 3116P 51530 ROTOR BRAKE CYLINDER HAS AN INTERNAL LEAK. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600272 20020606 00272 SW 2002 6 6 HEEA079470 1 20020528 A 2910 206076073001 TUBE BELL 206 206L3 1182108 SW HYD SYSTEM CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30KH 51527 HYDRAULIC TUBE CHAFED ON BOTTOM SIDE. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060600273 20020606 00273 SW 2002 6 6 HEEA079471 1 20020528 A 7712 206076373001 SHAFT BELL 206 206L3 1182108 SW TACH GEN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4835 51131 TACH GEN SHAFT HAS EXCESSIVE END PLAY. 1 G 7 1 3U H2SW 2002060600274 20020606 00274 SW 2002 6 6 HEEA079472 1 20020528 A 7714 206076373001 SHAFT BELL 206 206L3 1182108 SW TACH GEN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116P 51530 SPLINES FOR TRANS OIL PUMP SIDE WORN. SENT TO VENDOR FOR REPAIR. 1 G 7 1 3U H2SW 2002060600275 20020606 00275 SW 2002 6 6 HEEA079473 1 20020528 A 5260 206301109 STEP BELL 206 206L3 1182108 SW AIRSTAIR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8591X 51495 AIRSTAIR STEP CORRODED BEYOND LIMITS. SCRAPPED. 1 G 7 1 3U H2SW 2002060600276 20020606 00276 SW 2002 6 6 HEEA079474 1 20020528 A 5260 206301109 STEP BELL 206 206L3 1182108 SW AIRSTAIR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81SP 51029 AIRSTAIR STEP CORRODED BEYOND LIMITS. SCRAPPED. 1 G 7 1 3U H2SW 2002060600277 20020606 00277 SW 2002 6 6 HEEA079475 1 20020528 A 5260 206301120 STEP BELL 206 206L3 1182108 SW AIRSTAIR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81SP 51029 AIRSTAIR STEP CORRODED BEYOND LIMITS. SCRAPPED. 1 G 7 1 3U H2SW 2002060600278 20020606 00278 SW 2002 6 6 HEEA079476 1 20020528 A 3213 206321020 CROSSTUBE BELL 206 206B3 1181506 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2753F 2729 CROSSTUBE CORRODED BEYOND LIMITS. SCRAPPED. 1 G 7 1 3U H2SW 2002060600279 20020606 00279 SW 2002 6 6 HEEA079477 1 20020528 A 3213 206323017 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 206FS 51506 CROSSTUBE CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. 1 G 7 1 3U H2SW 2002060600280 20020606 00280 SW 2002 6 6 HEEA079478 1 20020528 A 3213 206323017 CROSSTUBE BELL 206 206B3 1181506 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2753F 2729 CROSSTUBE CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. 1 G 7 1 3U H2SW 2002060600281 20020606 00281 SW 2002 6 6 HEEA079479 1 20020528 A 3213 206323017 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251X 51552 CROSSTUBE CORRODED BEYOND LIMITS. SCRAPPED. 1 G 7 1 3U H2SW 2002060600282 20020606 00282 SW 2002 6 6 HEEA079480 1 20020528 A 3213 206323017 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6610C 51425 CROSSTUBE CORRODED BEYOND LIMITS. DEEP PITS OF CORROSION UNDER CLAMPS. SCRAPPED. 1 G 7 1 3U H2SW 2002060600283 20020606 00283 SW 2002 6 6 HEEA079481 1 20020528 A 3213 206323018 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251X 51552 CROSSTUBE CORRODED BEYOND LIMITS. SCRAPPED. 1 G 7 1 3U H2SW 2002060600284 20020606 00284 SW 2002 6 6 HEEA079482 1 20020528 A 3210 206323202 SUPPORT BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30KH 51527 SUPPORT CORRODED BEYOND LIMITS. SCRAPPED. 1 G 7 1 3U H2SW 2002060600285 20020606 00285 SW 2002 6 6 HEEA079483 1 20020528 A 3246 206324005 SKID BELL 206 206L1 1182107 SW MLG CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2124Z 45646 SKID TUBE CRACKED. SCRAPPED. 1 G 7 1 3U H2SW 2002060600286 20020606 00286 SW 2002 6 6 HEEA079484 1 20020528 A 3246 206324007 SKID BELL 206 206L1 1182107 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2245Y 45751 SKID TUBE CORRODED BEYOND LIMITS. SCRAPPED. 1 G 7 1 3U H2SW 2002060600287 20020606 00287 SW 2002 6 6 HEEA079485 1 20020528 A 3246 206324007 SKID BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31077 51520 SKID TUBE CORRODED BEYOND LIMITS. SCRAPPED. 1 G 7 1 3U H2SW 2002060600288 20020606 00288 SW 2002 6 6 HEEA079486 1 20020528 A 3246 206324008 SKID BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 53119 51575 DEEP CORROSION IN AREA OF FWD CROSSTUBE SADDLE, .025 INCH BEFORE CLEAN UP. DATE OF MANUFACTURE ON TUBE IS 6-20-00. 1 G 7 1 3U H2SW 2002060600289 20020606 00289 SW 2002 6 6 HEEA079487 1 20020528 A 3246 206324008 SKID BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6160Y 51609 SKID TUBE HAS CORROSION BEYOND LIMITS. SCRAPPED. 1 G 7 1 3U H2SW 2002060600290 20020606 00290 SW 2002 6 6 HEEA079488 1 20020528 A 3246 206324459 SKID BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251X 51552 SKID TUBE HAS CORROSION BEYOND LIMITS. SCRAPPED. 1 G 7 1 3U H2SW 2002060600291 20020606 00291 SW 2002 6 6 HEEA079489 1 20020528 A 3246 206324460 SKID BELL 206 206L3 1182108 SW MLG MISMANUFACTURED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81SP 51029 RT SADDLE IS OUT OF ROUND AND DOES NOT ALLOW FWD CROSSTUBE TO BE INSERTED. 1 G 7 1 3U H2SW 2002060600292 20020606 00292 SW 2002 6 6 HEEA079490 1 20020528 A 3246 206324460 SKID BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8591X 51495 CORROSION ON FWD SADDLE AND UNDER FLOAT RETAINERS. SCRAPPED. 1 G 7 1 3U H2SW 2002060600293 20020606 00293 SW 2002 6 6 HEEA079491 1 20020528 A 3212 206369002 FLOAT BELL 206 206L3 1182108 SW MLG LEAKING E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 30KH 51527 EMERGENCY FLOAT BAG LEAKS. 1 G 7 1 3U H2SW 2002060600294 20020606 00294 WP 2002 6 6 CALA0200324 1 20020604 A 5313 LONGERON DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A 2" CRACK IN L2R AT STA 1418. THE CRACKED AREA WAS CUT OUT AND A SPLICE REPAIR WAS INSTALLED IAW SRM 5 3-02, FIGURE 18. 2 L 7 2 4F A6WE 2002060600295 20020606 00295 WP 2002 6 6 CALA0200325 1 20020605 A 5311 FRAME DOUG DC9 DC982 3022082 WP STA 1416 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A 1/2" CRACK AT FASTENER IN FRAME AT STA 1416, LONGERON 4R. A NEW FRAME SECTION WAS INSTALLED IAW SRM 5 1-30-02 AND 51-30-05. 2 L 7 2 4F A6WE 2002060600296 20020606 00296 WP 2002 6 6 CALA0200326 1 20020605 A 5311 FRAME DOUG DC9 DC982 3022082 WP STA 1446 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A 3/4" CRACK AT FASTENER IN FRAME AT STA 1446, L4R. A NEW FRAME SECTION WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2002060600297 20020606 00297 WP 2002 6 6 CALA0200327 1 20020606 A 5712 RIB DOUG DC9 DC982 3022082 WP R/H WING DEFORMED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND THE R/H WING LEADING EDGE RIB DEFORMED INBOARD OF #4 SLAT TRACK(4TH RIB I/B). THE RIB WAS REMOVED AND R EPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2002060600298 20020606 00298 EA 2002 6 6 SWIA200210886 1 20020528 A 3620 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA LEFT ENGINE MALFUNCTIONED A SWIA A E UNSCHED LANDING ENGINE SHUTDOWN M J N OVER TEMP WARNING INDICATION FALSE WARNING CL CLIMB 1 NM 07 498SW 7483 LEFT 14TH STAGE DUCT LEAK MESSAGE. COMPLIED WITH QRH SHUTDOWN OF LEFT ENGINE. RETURNED TO SLC. REMOVED AND REPLACED L EFT ENGINE 14TH STAGE FIRE LOOP A58WK, A99WK IAW CRJ MM 36-21-04. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002060600299 20020606 00299 EU 2002 6 6 MALA020322 1 20020515 A 5320 7253721427 FRAME SAAB SF340 340B 7860101 EU A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K-CHECK IN CWA, LBL 11.0 ANGLE BETWEEN STA 236 & 258 HAS CORROSION. MAINTENANCE REMOVED CORRODED FRAME AND ANGL E, INSTALLED NEW FRAME PN 7253721-427 AND ANGLE PN 7253721-447 IAW SRM CHAPTER 51. 2 L 7 2 4T RT A52EU 2002060600300 20020606 00300 NM 2002 6 6 C1HA200282013 1 20020605 A 3350 1000677 LIGHT BOEING 727 7272S7 138407Z NM COCKPIT INOPERATIVE A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 682CA 22019 EMERGENCY PORT LIGHT IN COCKPIT INOP. R&R LIGHT ASSY PER MM 33-50-101. OPS CK GOOD. 2 L 7 3 4F A3WE 2002060700001 20020607 00001 SW 2002 6 7 HEEA079492 1 20020528 A 3212 206369002 FLOAT BELL 206 206L3 1182108 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81671 51301 RT MID FLOAT BAG HAS A SLOW LEAK. 1 G 7 1 3U H2SW 2002060700002 20020607 00002 SW 2002 6 7 HEEA079493 1 20020528 A 2810 206362002101 FUEL CAP BELL 206 206L3 1182108 SW FUEL CELL DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4180F LEVER ON FUEL CAP WILL NOT STAY LOCK DOWN WHEN SECURED. SCRAPPED. 1 G 7 1 3U H2SW 2002060700003 20020607 00003 SW 2002 6 7 HEEA079495 1 20020528 A 5320 206417152 PANEL BELL 206 206L3 1182108 SW FUSELAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81671 51301 FUSELAGE TRIM PANEL CRACKED. SCRAPPED. 1 G 7 1 3U H2SW 2002060700004 20020607 00004 WP 2002 6 7 0201739993 1 20020603 A 3210 59105285526 LANDING GEAR DOUG DC9 DC931 3022065 WP RT MLG COLLAPSED A NWAA O OTHER Z SIGNIFICANT FAILURE REPORT LD LANDING 1 GL 01 8986E 47402 LANDING GEAR COLLAPSED DURING LANDING ROLL. SPECIFICS UNKNOWN AT THIS TIME DUE TO THE LOG PAGES BEING SECURED FOR INVES TIGATION. 2 L 7 2 4F A6WE 2002061300154 20020613 00154 NM 2002 6 13 02FDEA00379 1 20020531 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 MECHANICAL DAMAGE TO FRAME AT BS 720, STR 4L AND CEILING SUPPORT. REMOVED AND REPLACED FRAME PER SRM 53-10-4. 2 L 7 3 4F RT A3WE 2002061300155 20020613 00155 NM 2002 6 13 02FDEA00381 1 20020601 A 5315 65198703 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CORROSION ON FLOORBEAM BS 900, LBL 43. REMOVED AND REPLACED FLOORBEAM PER EA 7- 5310-64924. 2 L 7 3 4F RT A3WE 2002072200024 20020722 00024 NM 2002 7 22 2002UALA00941 1 20020529 A 2750 JAD9E006 RELAY BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE T/E FLAP FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 942UA 26679 TRAILING EDGE FLAPS FAILED TO EXTEND UPON APPROACH. REPLACED RELAY R123. TENSIONED FLAP SYSTEM CABLES, RIG CHECKS GOOD . 2 L 7 2 4F 4 F RT A16WE E2GL 2002060700008 20020607 00008 WP 2002 6 7 ABXA010897 1 20020523 A 2750 FLAP DOUG DC8 DC863F 302198F WP WING OUT OF RIG A ABXA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 23 811AX 46113 ON TAKEOFF WITH FLAPS SELECTED TO 18 DEG, THE INDICATOR INDICATED 15 DEG, THEN INCREASED TO 20 DEGREES. ON APPROACH, FL AP INDICATION WAS AS FOLLOWS, 12 SELECTED, 10 INDICATED - 23 SELECTED, 23 INDICATED - 35 SELECTED, 40 INDICATED. AIRCRA FT WAS FERRIED FROM MIA TO ILN. MAINTENANCE RIGGED THE RIGHT FLAP FOLLOW-UP SYSTEM AND RELATED SYSTEM IAW DC-8 MM 27-50 -00-5. LUBRICATED LEFT AND RIGHT WING FLAPS IAW DC-8 MM 12-82-01-3. 2 L 7 4 4F 4A25 2002060700009 20020607 00009 WP 2002 6 7 ABXA010898 1 20020517 A 5320 J0602283 PAN DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 BULGING STRUCTURE AND SEVERAL POPPED FASTENERS ALONG BOTTOM OF FORWARD LOWER CARGO COMPARTMENT DOOR CUTOUT. INSTALLED N EW PAN AND REPAIRED AREA IAW DC-9 SRM 53-05. 2 L 7 2 4F A6WE 2002060700010 20020607 00010 WP 2002 6 7 ABXA010899 1 20020520 A 5310 9911840165 SHEAR TIE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 SHEAR TIE CRACKED AT FS 1171, VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE. REPLACED SHEAR TIE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002060700011 20020607 00011 WP 2002 6 7 ABXA010900 1 20020523 A 1430 NUT DOUG DC8 DC863F 302198F WP T/E FLAP MISSING A ABXA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 23 816AX 46093 UPON FLAP EXTENSION FOR LANDING, SPLIT FLAPS WERE INDICATED. CONFIRMED BY ROLL TENDENCY. LEFT FLAP WAS APPROXIMATELY 6 DEGREES BEHIND RIGHT FLAP. RIGHT FLAP AT 35 DEGREES, LEFT FLAP AT 29 DEGREES. FOUND LEFT INBOARD FLAP ACTUATOR IDLER ARM TRACK MISSING NUT AND HANGING. REPLACED MISSING NUT. INSPECTED FLAPS. RAN FLAPS UP AND DOWN SEVERAL TIMES. NO SP LIT NOTED IAW DC-8 MM 27-51-03. 2 L 7 4 4F 4A25 2002060700012 20020607 00012 NM 2002 6 7 ABXA010901 1 20020603 A 3350 38931002 BATTERY BOEING 767 767281 1385109 NM CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 791AX 23141 DURING PREDEPARTURE CHECK, FOUND COCKPIT OVER THE DOOR REMOVABLE EMERGENCY LIGHT BARELY GLOWING WHEN TESTED. REPLACED I NTERNAL BATTERIES IN EMERGENCY EXIT LIGHT. OPS CHECKED GOOD IAW B767 MM 33-51-0. 2 L 7 2 4F RT A1NM 2002060700013 20020607 00013 WP 2002 6 7 ABXA010902 1 20020531 A 2170 COALESCER BAG DOUG DC9 DC941 302207N WP A/C BAY CONTAMINATED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 974AX 47623 CREW REPORTED OIL SMELL FROM AIR PACKS WITH ENGINE RUNNING. REPLACED AIR CONDITIONING WATER COALESCER BAGS. LEAK CHECK ED GOOD IAW DC-9 MM 21-20-02-2-0001. 2 L 7 2 4F A6WE 2002060700014 20020607 00014 WP 2002 6 7 ABXA010903 1 20020601 A 3310 RHEOSTAT DOUG DC9 DC931 3022065 WP COCKPIT FAILED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 937AX 47074 CAPTAIN'S OVERHEAD MAP LIGHT WAS SPARKING AND SMOKING. REPLACED THE CAPTAIN'S OVERHEAD MAP LIGHT RHEOSTAT. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2002060700015 20020607 00015 NM 2002 6 7 ABXA010904 1 20020605 A 5210 ROLLER BOEING 767 767200 1385120 NM ENTRY DOOR OUT OF POSITION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 790AX 23140 ON ARRIVAL AT ILN, THE MAIN ENTRY DOOR WOULD NOT OPEN. FOUND AFT ROLLER OUT OF TRACK AND AFT INBOARD BRACKET LOOSE. RE INSTALLED ROLLER AND ADJUSTED BI-FOLD COVER IAW B767 MM 52-11-34. 2 L 7 2 4F RT A1NM 2002060700016 20020607 00016 SW 2002 6 7 HEEA079496 1 20020528 A 5230 206513211 ACTUATOR BELL 206 206L3 1182108 SW CARGO DOOR WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6160Z 51610 CARGO DOOR ACTUATOR WEAK. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060700017 20020607 00017 SW 2002 6 7 HEEA079497 1 20020528 A 2510 206919201 HARNESS BELL 206 206L3 1182108 SW SEAT BELTS STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251X 51552 SHOULDER HARNESS AND LAP BELT STICKS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060700018 20020607 00018 SW 2002 6 7 HEEA079499 1 20020528 A 2822 209062003001 PRESSURE SWITCH BELL 412 412 1182202 SW FUEL BOOST INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893N 33010 FUEL BOOST PRESSURE SWITCH INOPERATIVE. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700019 20020607 00019 NM 2002 6 7 ABXA010905 1 20020605 A 5210 ROLLER BOEING 767 767200 1385120 NM ENTRY DOOR OUT OF POSITION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 790AX 23140 CREW REPORTED MAIN ENTRY DOOR WOULD NOT FULLY OPEN. FOUND AFT ROLLER ON OVERHEAD MOVABLE INTERIOR PANEL OUT OF CAM SLOT . REPOSITIONED ROLLER, OPERATED DOOR SEVERAL TIMES. OPS CHECKED GOOD IAW B767 MM. 2 L 7 2 4F RT A1NM 2002060700020 20020607 00020 NM 2002 6 7 ABXA010906 1 20020606 A 5210 ROLLER BOEING 767 767200 1385120 NM ENTRY DOOR OUT OF POSITION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 790AX 23140 CREW REPORTED MAIN ENTRY DOOR BINDING SLIGHTLY DURING OPENING AND CLOSING. REPOSITIONED AFT ROLLER INTO CAM SLOT TRACK. OPERATED DOOR SEVERAL TIMES. OPS CHECKED GOOD IAW B767 AMM 52-11-00. 2 L 7 2 4F RT A1NM 2002060700021 20020607 00021 WP 2002 6 7 ABXA010907 1 20020508 A 5230 59101577 SKIN DOUG DC9 DC933F 302207A WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 CRACK INDICATION IN PAN AND HI-LOK AT THE NR 1 BEAM AFT END AFT LOWER CARGO DOOR. REPLACED THE OUTER SKIN AND PAN IAW D C-9 SRM 51-30-2. 2 L 7 2 4F A6WE 2002060700022 20020607 00022 SW 2002 6 7 HEEA079502 1 20020528 A 7921 209062502101 OIL COOLER BELL 412 412 1182202 SW ENGINE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 33023 OIL COOLER HAS CORROSION. 1 G 7 2 4U H4SW 2002060700023 20020607 00023 SW 2002 6 7 HEEA079503 1 20020528 A 7921 209062502101 OIL COOLER BELL 412 412 1182202 SW ENGINE MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 OIL COOLER PRODUCING HIGH FREQUENCY. (SHAFT CORRODED AND PITTING) 1 G 7 2 4U H4SW 2002060700024 20020607 00024 WP 2002 6 7 ABXA010908 1 20020509 A 5312 5910130392 TEE CHORD DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 AFT PRESSURE BULKHEAD NR 2 TEE HAD 2 VERTICAL CRACKS APPROXIMATELY 1 INCH IN LENGTH AT LONGERON 14 RIGHT AND LONGERON 16 RIGHT. REPLACED THE NR 2 TEE IAW EA 53120033-006 AND REA D953-44179. 2 L 7 2 4F A6WE 2002060700025 20020607 00025 SW 2002 6 7 HEEA079504 1 20020528 A 6200 STATOR BELL 412 412 1182202 SW BLOWER LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 51003838 36002 BLOWER STATOR LOOSE AND WEARING INTO BLOWER HOUSING. 1 G 7 2 4U H4SW 2002060700026 20020607 00026 SW 2002 6 7 HEEA079505 1 20020528 A 6200 BLOWER BELL 412 412 1182202 SW OIL COOLER DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X OCB082598 33113 OIL COOLER BLOWER PRODUCING A HIGH PITCHED WHINE. REPAIRED BY PHI. 1 G 7 2 4U H4SW 2002060700027 20020607 00027 WP 2002 6 7 ABXA010911 1 20020518 A 3233 57740355507ABX1 ACTUATOR DOUG DC8 DC863F 302198F WP LT MLG BROKEN A ABXA K NONE J WARNING INDICATION CR CRUISE 1 GL 23 828AX 45999 RED GEAR UNSAFE LIGHT ILLUMINATED IN CRUISE FLIGHT. LANDING GEAR AND DOOR LATCHING SYSTEM ILLUMINATED IN LEFT MAIN GEAR POSITION. ALTERNATE METHOD USED TO EXTINGUISH THE GEAR UNSAFE INDICATION. FOUND THE LEFT MAIN LANDING GEAR ACTUATOR A TTACHING PIN BROKEN. REPLACED THE LEFT MAIN LANDING GEAR ACTUATING CYLINDER AND PIN IAW DC-8 MM 32-32-02-2. OPS CHECKE D AND LEAK CHECKED GOOD. 2 L 7 4 4F 4A25 2002060700028 20020607 00028 NE 2002 6 7 HEEA079506 2 20020528 A 7261 209062527003 HOSE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE OIL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2148K 36001 ENGINE HOSE LEAKS OIL. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U 4 U H4SW E22EA 2002060700029 20020607 00029 NE 2002 6 7 HEEA079507 2 20020528 A 7200 209062761001 SOLENOID BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 WORN PLUNGER, WEAK EXTENSION NR 2. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U 4 U H4SW E22EA 2002060700030 20020607 00030 SW 2002 6 7 HEEA079508 1 20020528 A 2620 FITTING BELL 412 412 1182202 SW EXTINGUISHER CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 07056B2 33012 FIRE EXTINGUISHER FITTING CORRODED. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700031 20020607 00031 SW 2002 6 7 HEEA079509 1 20020528 A 7933 209070262101 REGULATOR BELL 412 412 1182202 SW ENG OIL TEMP READS LOW E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 TEMP READS LOW. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700033 20020607 00033 NM 2002 6 7 920WA0003 1 20020606 A 2910 HYDRAULIC SYSTEM BOEING 737 737236 1384476 NM A PIDA O OTHER J WARNING INDICATION DE DESCENT 1 SO 05 920WA 21791 During descent into CUN master caution hydrualics - both A system low pressure lights on. "A" system pressure gauge almo st 0. QRH accomplished. Declared emergency. - Inspected system, ground ran and performed test flight. No defects noted. 2 L 7 2 4F RT A16WE 2002060700035 20020607 00035 SO 2002 6 7 C2XA02BT020 1 20020512 A 3397 WIRE EMB 145 EMB145ER 3260211 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14943 145040 CREW REPORTED AISLE FLOOR PATH LIGHTING INOPERATIVE. MAINTENANCE REPAIR A BROKEN WIRE ON REAR SECTION OF EMERGENCY AISL E PATH LIGHTING AND OPS CHECKED SYSTEM GOOD. 2 L 7 2 4F RT T00011AT 2002060700036 20020607 00036 SW 2002 6 7 HEEA079511 1 20020528 A 7922 209070262101 INDICATOR BELL 412 412 1182202 SW ENGINE OIL READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 ENGINE OIL TEMP READS HIGH. 1 G 7 2 4U H4SW 2002060700037 20020607 00037 SW 2002 6 7 HEEA079512 1 20020528 A 7922 209070262101 INDICATOR BELL 412 412 1182202 SW ENGINE OIL INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2149S 36002 TEMPERATURE NEEDLE GOES TO ZERO. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700038 20020607 00038 SW 2002 6 7 HEEA079513 1 20020528 A 2437 209070264003 INDICATOR BELL 412 412 1182202 SW DUAL AMMETER FLUCTUATES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 DUAL AMMETER NR 1 NEEDLE FLUCTUATES. 1 G 7 2 4U H4SW 2002060700039 20020607 00039 SW 2002 6 7 HEEA079514 1 20020528 A 2437 209070264003 INDICATOR BELL 412 412 1182202 SW DUAL AMMETER MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 DUAL AMMETER NR 1 NEEDLE VIBRATES WITH AIRCRAFT BOUNCE. 1 G 7 2 4U H4SW 2002060700040 20020607 00040 SW 2002 6 7 HEEA079515 1 20020528 A 7923 CONNECTOR BELL 412 412 1182202 SW SHUTOFF VALVE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 1309 33010 TROUBLESHOOTING FOUND "A" PIN BROKEN IN VALVE PLUG RECEPTICLE OF ENGINE OIL SHUTOFF VALVE. REPLACED WITH SERVICEABLE PAR T. 1 G 7 2 4U H4SW 2002060700041 20020607 00041 NE 2002 6 7 HEEA079516 2 20020528 A 7532 209072433105 BLEED VALVE BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE COMPRESSOR INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 COMPRESSOR BLEED VALVE INOPERATIVE - VALVE WON'T OPEN. 2 G 7 2 4U 4 U H10SW E8NE 2002060700042 20020607 00042 SW 2002 6 7 HEEA079517 1 20020528 A 2912 2111328 FILTER BELL 206 206L3 1182108 SW HYD SYSTEM CLOGGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251Y 51556 HYD FILTER CLOGGED. FILTER BYPASSED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060700043 20020607 00043 SW 2002 6 7 HEEA079518 1 20020528 A 3040 211722 MOTOR BELL 412 412 1182202 SW WINDSHILED WIPER WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2149S 36002 WINDSHIELD WIPER MOTOR WEAK, WILL NOT MOVE ON LOW SPEEDS SETTING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700044 20020607 00044 SO 2002 6 7 C2XA02BT021 1 20020603 A 3230 355022002 CONTROL UNIT EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A C2XA O OTHER J WARNING INDICATION UK UNKNOWN 1 SW 27 13908 145465 CREW REPORTED LANDING GEAR AIR TO GROUND FAILURE WARNING, ENGINE NR 1- NR 1 THRUST REVERSER DISAGREE. MAINTENANCE REMOV ED AND REPLACED LGEU IAW EMB145 MM 32-32-01, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002060700045 20020607 00045 SO 2002 6 7 C2XA02CL119 1 20020531 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13990 145277 CLE FLIGHT 3248 THE CREW REPORTED THE APU CAUSES A SMELL IN THE CABIN. MAINTENANCE INSPECTED AND PERFORMED A OPERATIONA L CHECK OF THE APU AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002060700046 20020607 00046 SO 2002 6 7 C2XA02CL120 1 20020603 A 3350 3025103 LIGHT EMB 145 EMB145 3260210 SO EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13965 145125 DURING ROUTINE MAINTENANCE THE EXTERNAL FORWARD EMERGENCY LIGHT ON THE LEFT WAS FOUND TO BE INOPERATIVE. MAINTENANCE IN SPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE . 2 L 7 2 4F RT T00011AT 2002060700047 20020607 00047 SO 2002 6 7 C2XA02CL121 1 20020603 A 3350 66903 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 13964 145123 CLE FLIGHT 4040 THE CREW REPORTED THE CABIN EMERGENCY FLOOR LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002060700048 20020607 00048 SO 2002 6 7 C2XA02CL122 1 20020604 A 3350 3025103 LIGHT EMB 145 EMB145 3260210 SO EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16963 145116 DURING ROUTINE MAINTENANCE THE LEFT UPPER EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMER GENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002060700049 20020607 00049 SO 2002 6 7 C2XA02CL123 1 20020604 A 2730 050102003 REGULATOR EMB 145 EMB145LR 3260212 SO ELEVATOR SYS STICKING A C2XA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 27 14902 1763 145496 CLE FLIGHT 3083 THE CREW REPORTED VIBRATION IN THE CONTROL COLUMN/YOKE IN ALL PHASES OF FLIGHT. MAINTENANCE INSPECTED A ND REPLACED THE RIGHT AND LEFT ELEVATOR CABLE TENSION REGULATORS. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS TEST FLOWN WITH NO DEFECTS. 2 L 7 2 4T RT T00011AT 2002060700050 20020607 00050 SO 2002 6 7 C2XA02IA122 1 20020605 A 7830 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT ACTIVATED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 14923 145318 IAH- DURING FLIGHT 3921, THE CREW NOTED THAT THE NUMBER 1 ENGINE THRUST REVERSER DISAGREE MESSAGE ILLUMINATED ON THE EIC AS. THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT. 2 L 7 2 4T RT T00011AT 2002060700051 20020607 00051 NM 2002 6 7 CALA0200328 1 20020605 A 3210 654511320 PIN BOEING 737 737524 1384721 NM LT MLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59630 27534 THE LT MLG ACTUATOR BEAM ARM FAILED ULTRASONIC INSPECTION. THE AFT LUG (ANTI-ROTATION PIN LUG) HAD A 3 INCH CRACK. THE LT MLG ASSEMBLY WAS REMOVED AND REPLACED IAW MM 32-11-00. 2 L 7 2 4F RT A16WE 2002060700052 20020607 00052 SO 2002 6 7 C2XA02CL124 1 20020604 A 3231 22250100003 VALVE EMB 135 EMB135LR 3260305 SO FORWARD FUSELAGE LEAKING A C2XA K NONE E VIBRATION/BUFFET CL CLIMB 1 SW 27 12528 1333 145504 CLE FLIGHT#2980 THE CREW REPORTED A SLIGHT VIBRATION AND SAID IT SOUNDED LIKE THE NOSE GEAR DOORS WERE NOT FULLY CLOSING .MAINTENANCE REPLACED THE NOSE GEAR SOLENOID VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002060700053 20020607 00053 2002 6 7 CHQ000164 4 20020602 A 3140 WARNING SYSTEM EMB 145 EMB145 3260210 SO COCKPIT ACTIVATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 262 ENG 2 ATTCS NO MARGIN ON EICAS. FERRY A/C TO IND. 2 L 7 2 4F RT T00011AT 2002060700054 20020607 00054 SW 2002 6 7 HEEA079519 1 20020528 A 6710 212001035101 FORCE GRADIENT BELL 412 412 1182202 SW FLIGHT CONTORLS BINDING E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22608 33075 CYCLIC FORCE GRADIENT IS BINDING AND HANGING UP. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700055 20020607 00055 SW 2002 6 7 HEEA079520 1 20020528 A 6710 212001035101 FORCE GRADIENT BELL 412 412 1182202 SW CYCLIC STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 FORCE GRADIENT STICKING INTERMITTENTLY. SENT TO BELL HELICOPTER TEXTRON FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 2002060700056 20020607 00056 SW 2002 6 7 HEEA079521 1 20020528 A 7810 212001201012 MOUNT BELL 412 412 1182202 SW EXHAUST BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 EXHAUST MOUNT BROKEN. 1 G 7 2 4U H4SW 2002060700057 20020607 00057 SW 2002 6 7 HEEA079522 1 20020528 A 6420 BEARING BELL 412 412 1182202 SW T/R HUB WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 TAIL ROTOR HUB HAS A WORN FEATHERING BEARINGS. REPLACED BEARINGS AND RETURNED TO SERVICE. 1 G 7 2 4U H4SW 2002060700058 20020607 00058 SW 2002 6 7 HEEA079523 1 20020528 A 6720 BEARING BELL 412 412 1182202 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 TAIL ROTOR BELLCRANK HAS A WORN BEARING. SCRAPPED. 1 G 7 2 4U H4SW 2002060700059 20020607 00059 SW 2002 6 7 HEEA079524 1 20020528 A 6720 BEARING BELL 412 412 1182202 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 TAIL ROTOR BELLCRANK HAS A WORN BEARING. SCRAPPED. 1 G 7 2 4U H4SW 2002061000235 20020610 00235 NM 2002 6 10 F3LA200200155 1 20020605 A 5210 FAIRING BOEING 737 7373L9 1384470 NM L1 DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3389 26440 DURING C-2 CHECK, INSPECTION REPORTED UPPER HINGE FAIRING AT L1 DOOR BENT AT FWD END AND CRACKED AT AFT END. FABRICATED AND INSTALLED REPLACEMENT UPPER L1 DOOR HINGE FAIRING PER SRM 51-30-01. 2 L 7 2 4F RT A16WE 2002060700060 20020607 00060 SW 2002 6 7 HEEA079525 1 20020528 A 6720 BEARING BELL 412 412 1182202 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 TAIL ROTOR BELLCRANK HAS A WORN BEARING. SCRAPPED. 1 G 7 2 4U H4SW 2002060700061 20020607 00061 SW 2002 6 7 HEEA079526 1 20020528 A 6720 BEARING BELL 412 412 1182202 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 TAIL ROTOR BELLCRANK HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700062 20020607 00062 SW 2002 6 7 HEEA079527 1 20020528 A 6720 BEARING BELL 412 412 1182202 SW BELLCRANK UNSTAKED E K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 TAIL ROTOR BELLCRANK BEARING UNSTAKED. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700063 20020607 00063 SW 2002 6 7 HEEA079528 1 20020528 A 6720 BEARING BELL 412 412 1182202 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 TAIL ROTOR BELLCRANK HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700064 20020607 00064 SW 2002 6 7 HEEA079529 1 20020528 A 6720 BEARING BELL 412 412 1182202 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 TAIL ROTOR BELLOCRANK HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700065 20020607 00065 SW 2002 6 7 HEEA079530 1 20020528 A 6720 BEARING BELL 412 412 1182202 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 TAIL ROTOR BELLCRANK HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700066 20020607 00066 SW 2002 6 7 HEEA079531 1 20020528 A 6420 BEARING BELL 412 412 1182202 SW TAIL ROTOR HUB WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L A541 33006 TAIL ROTOR HUB HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700067 20020607 00067 SO 2002 6 7 CHQ000165 1 20020603 A 2150 ACM EMB 145 EMB145 3260210 SO A/C BAY FAILED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 265 SMOKE IN COCKPIT. MX FOUND NR 1 ACM BAD CAUSING SMOKE IN COCKPIT. REMOVED AND REPLACED NR 1 ACM. 2 L 7 2 4F RT T00011AT 2002060700068 20020607 00068 NM 2002 6 7 DHL2002708007 1 20020605 A 2612 FIRE LOOP BOEING 727 72725 1384006 NM NR 1 ENGINE OUT OF POSITION A DHLA K NONE N FALSE WARNING CR CRUISE 1 SO 01 708DH 18275 ENG NR 1 FIRE DETECTION GROUND FAULT LIGHT FLASHES IN FLIGHT. REPOSITIONED ENG NR 1 FIRE LOOP AND REMOVED AND REPLACED NR 1 GROUND FAULT LENS COVER WITH NEW LENS COVER. NO FAULTS DETECTED, OPS CHECKS GOOD IAW MM 26-11-000. 2 L 7 3 4F A3WE 2002060700069 20020607 00069 SW 2002 6 7 HEEA079532 1 20020528 A 6420 BEARING BELL 412 412 1182202 SW TAIL ROTOR HUB WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T A550 33112 TAIL ROTOR HUB HAS WORN FEATHERING BEARINGS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700070 20020607 00070 SW 2002 6 7 HEEA079533 1 20020528 A 6420 BEARING BELL 412 412 1182202 SW T/R HUB WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 6092 A590 33150 TAIL ROTOR HUB HAS WORN FEATHERING BEARINGS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700071 20020607 00071 WP 2002 6 7 DHL2002802555 1 20020507 A 5230 SKIN DOUG DC8 DC873 302199C WP CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 B-PIT BELLY DOOR EXTERNAL SKIN RT UPPER CORNER CRACKED 2 INCHES AROUND STA 520.000. PERFORMED MAJOR REPAIR PER EO DHL02 0504, EO-3046, EO SEMAN 2002569. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER EO DHL 020504, EO 3046, EO S EMAN 2002569. 2 L 7 4 4F RT 4A25 2002060700072 20020607 00072 SW 2002 6 7 HEEA079534 1 20020528 A 6410 BLADE BELL 412 412 1182202 SW TAIL ROTOR DENTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 4219 36007 TAIL ROTOR DENT IN LEADING EDGE OF BLADE. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700073 20020607 00073 SW 2002 6 7 HEEA079536 1 20020528 A 6420 BEARING BELL 412 412 1182202 SW T/R HUB WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z A1043 36019 TAIL ROTOR HAS WORN FLAPPING BEARINGS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700074 20020607 00074 WP 2002 6 7 DHL2002802560 1 20020528 A 2780 37701442N TORQUE TUBE DOUG DC8 DC873 302199C WP L/E SLOT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 LFT WING OUTBOARD SLOT TORQUE TUBE CRACKED (CRANK). REMOVED TORQUE TUBE FROM LEFT WING OUTBOARD SLOT PER M/M 27-80-2 PG 201. REMOVED AND REPLACED CRANK ASSY OF TORQUE TUBE PER SRM 51-1-21 PG 1. INSTALLED TORQUE TUBE ON LEFT WING OUTBOARD SLOT PER M/M 27-80-2 PG 203. OPS CHECK PERFOMED ON N/R 0339. 2 L 7 4 4F RT 4A25 2002060700075 20020607 00075 SW 2002 6 7 HEEA079537 1 20020528 A 6420 BEARING BELL 412 412 1182202 SW BELLCRANK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 TAIL ROTOR HAS WORN BEARINGS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700076 20020607 00076 SW 2002 6 7 HEEA079538 1 20020528 A 6320 212030104101 LINK BELL 412 412 1182202 SW XMSN CASE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 TRANSMISSION CASE LIFT LINK HAS WORN BEARINGS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061900102 20020619 00102 CE 2002 6 19 GLBA2002071 1 20020528 A 2130 WARNING SYSTEM BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 261GL UE261 RIGHT ENVIRONMENTAL FAIL ON T/O ROLL. RESET OVERPRESS LED ON BLEED AIR. 2 L 7 2 4T RT A24CE 2002060700077 20020607 00077 SW 2002 6 7 HEEA079539 1 20020528 A 6320 212030104101 LINK BELL 412 412 1182202 SW XMSN CASE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 TRANSMISSION LIFT LINK HAS AN UNSTAKED BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700078 20020607 00078 SW 2002 6 7 HEEA079541 1 20020528 A 3212 212030309001 ARM BELL 412 412 1182202 SW EMERGENCY FLOAT CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 EMRERGENCY FLOAT ARM CORRODED. SCRAPPED. 1 G 7 2 4U H4SW 2002060700079 20020607 00079 NE 2002 6 7 IXXA0200027O 2 20020522 A 7230 STATOR VANE DOUG DC8 DC871 302199A WP GE CFM56 CFM562C 13802 NE ENGINE MALFUNCTIONED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 829BX 85070 771 45994 AFTER TAKEOFF FROM TOL, THE FLIGHT CREW EXPERIENCED A WINDSHEAR WARNING ALERT. THE FLIGHT CREW FOLLOWED COMPANY PROCEDU RES AND THE NUMBER THREE ENGINE EXCEEDED NORMAL OPERATING TEMPERATURES. THE FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LA NDING. MAINTENANCE INSPECTED THE ENGINE IN ACCORDANCE WITH THE CFM MAINTENANCE MANUAL. THE INSPECTION REVEALED A DISCR EPANCY AT THE VARIABLE STATOR VANE FEEDBACK SYSTEM. MAINTENANCE CORRECTED THE DISCREPANCY, PERFORMED A SUCCESSFUL OPERA TIONAL CHECK IN ACCORDANCE WITH THE COMPANY ENGINE RUN HANDBOOK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A25 E2GL 2002060700080 20020607 00080 SO 2002 6 7 LR7A02040 1 20020606 A 5330 SKIN LKHEED 382 382G 526414U SO FS 156 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 559 4590 DURING SCHEDULED B1 CHECK INSPECTION PER JOB CARD HB0502 FOUND LH FS 156 FUSELAGE SKIN CRACKED AROUND PREVIOUS REPAIR AT LBL 66, WL 180.REPAIRED IAW SRM SMP 583 51-140-10. NR 2001. 2 H 7 4 4T A1SO 2002060700081 20020607 00081 SO 2002 6 7 LR7A02041 1 20020606 A 5330 SKIN LKHEED 382 382G 526414U SO FS 807E CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 559 4590 DURING SCHEDULED B1 CHECK INSPECTION PROGRAMMED REPLACEMENT OF PREVIOUS NON-FLUSH FUSELAGE SKIN REPAIR AT FS 807E, RBL 6 7, WL 150.REPAIRED IAW SRM SMP 583 51-140-10. NR 2002. 2 H 7 4 4T A1SO 2002060700082 20020607 00082 EU 2002 6 7 MALA020288 1 20020517 A 7933 4053T73P01 BULB SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT PGB FAULTY A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 450XJ 340B450 DURING FLIGHT 2945, LT PGB OIL TEMP FLUCTUATES. AIR RETURN TO DTW. MAINTENANCE REPLACED TEMP BULBS. MAINTENANCE INSPE CTED ELECTRICAL CONNECTORS AT LT PROP OIL TEMP GAUGE AND AT TEMP BULB. NO DISCREPANCIES NOTED. MAINTENANCE REMOVED AND REPLACED LT PGB TEMP BULB. ALL WORK IAW SF3 MM CHAP 79. OPS LEAK CHECK GOOD IAW SAME. 2 L 7 2 4T 4 T RT A52EU E8NE 2002060700083 20020607 00083 SW 2002 6 7 HEEA079542 1 20020528 A 3212 212030310001 ARM BELL 412 412 1182202 SW EMERGENCY FLOAT CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 EMERGENCY FLOAT ARM CORRODED. SCRAPPED. 1 G 7 2 4U H4SW 2002060700084 20020607 00084 EU 2002 6 7 MALA020296 1 20020523 A 3620 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU COCKPIT FALSE ACTIVATION A MALA E D ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 89XJ 340A089 DURING FLIGHT 2797 LT BLEED AIR LEAK LIGHT ILLUMINATED DURING TAXI. CREW RAN QRH REMAINED ON UNTIL ENGINE SHUTDOWN. A/ C RETURNED TO GATE. MAINTENANCE TROUBLESHOT, INSPECTED BLEED LEAK DETECTION LOOP, INSPECTED FOR LEAKS OR CHAFES, RAN FO R 15 MINUTES, CHECKING FOR BLEED LEAKS, NONE FOUND. COULD NOT DUPLICATE PROBLEM AT ANY TIME, AS A PRECAUTION CHANGED BL EED FAULT CONTROL UNIT, RAN ANOTHER 15 MINUTES AND NO DEFECTS NOTED. 2 L 7 2 4T RT A52EU 2002060700085 20020607 00085 SW 2002 6 7 HEEA079543 1 20020528 A 3246 212030436007 CAP BELL 412 412 1182202 SW MLG SKID TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 MLG SKID TUBE CAP HAS IT`S RUBBER TORN. 1 G 7 2 4U H4SW 2002060700086 20020607 00086 SW 2002 6 7 HEEA079544 1 20020528 A 3246 212030436007 CAP BELL 412 412 1182202 SW MLG SKID WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 MLG SKID CAP WORN. 1 G 7 2 4U H4SW 2002060700087 20020607 00087 SW 2002 6 7 HEEA079545 1 20020528 A 3246 212030436007 CAP BELL 412 412 1182202 SW MLG SKID DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 RUBBER DETERIORATED. 1 G 7 2 4U H4SW 2002060700088 20020607 00088 2002 6 7 MALA020298 4 20020526 A 2215 6225027002 SERVO SAAB SF340 SF340A 7850100 EU RUDDER FAILED A MALA K NONE F FLT CONT AFFECTED CR CRUISE 1 GL 15 109XJ 340A109 DURING FLIGHT AT CRUISE, AUTO PILOT YAW DAMPER INOP. AP DISENGAGED AND CAN NOT BE REENGAGED. MAINTENANCE REMOVED AND R EPLACED RUDDER SERVO IAW AMM 22-10-21-4. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002060700089 20020607 00089 2002 6 7 MALA020299 4 20020526 A 3460 4068300904 COMPUTER BAC 146 AVRO146RJ85A 1500097 EU COCKPIT FAILED A MALA K NONE J WARNING INDICATION CR CRUISE 1 GL 15 508XJ E2318 EN ROUTE FROM TYS TO DTW, FGC1 LIGHT ILLUMINATED. MAINTENANCE REPLACED FGC IAW 22/10-11. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2002061000236 20020610 00236 NM 2002 6 10 F3LA200200156 1 20020605 A 5320 FLOOR SUPPORT BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3389 26440 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT STA 767, RBL 3. REMOVED CORROSION ON FLOOR SUPPORT, FABRICATED REPLACEMENT PARTS AND INSTALLED REPAIR PER SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002061000237 20020610 00237 NM 2002 6 10 F3LA200200157 1 20020605 A 5320 FLOOR SUPPORT BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3389 26440 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STA 767. FABRICATED AND INSTALLED REPAIR ON CARGO TRACK AT STA 767, RBL 13.8, PER SRM 53-00-53, FIG 202. 2 L 7 2 4F RT A16WE 2002061000238 20020610 00238 NM 2002 6 10 F3LA200200158 1 20020605 A 5311 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3389 26440 DURING C-2 CHECK, INSPECTION REPORTED FRAME AT STA 460, RBL 7 TO 14, DAMAGED. FABRICATED AND INSTALLED REPAIR AND FRAME CLIP PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2002060700090 20020607 00090 WP 2002 6 7 MWEA020390 1 20020604 A 5754 9955846501 FITTING DOUG DC9 DC932 3022066 WP LEFT WING WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 #5 SLAT INBOARD SADDLE FITTING BUSHINGS WORN. -- REMOVED AND REPLACED RIB. 2 L 7 2 4F A6WE 2002060700091 20020607 00091 WP 2002 6 7 MWEA020397 1 20020604 A 5313 591970731 LONGERON DOUG DC9 DC932 3022066 WP STATION 851 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 A SERIES OF SMALL DENTS BETWEEN STATION 851-889, LONGERONS 24 & 25 RIGHT. (REFERENCE CO #6277) -- FABRICATED AND INSTA LLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002060700092 20020607 00092 WP 2002 6 7 MWEA020398 1 20020604 A 5320 591359612 SHEAR TIE DOUG DC9 DC932 3022066 WP STATION 1059 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT ACCESSORY COMPARTMENT FRAME STATION 1059 SHEAR TIE IS CRACKED BELOW LONGERON 15 RIGHT. -- FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2002060700093 20020607 00093 WP 2002 6 7 MWEA020399 1 20020604 A 5320 59105373N WEB DOUG DC9 DC932 3022066 WP LH AFT EMER DR TORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 WEB BELOW LEFT AFT OVERWING EMERGENCY EXIT DOOR HAS A LARGE HOLE/TEAR IN IT. -- REMOVED AND REPLACED WEB. 2 L 7 2 4F A6WE 2002060700094 20020607 00094 EU 2002 6 7 MALA020300 1 20020528 A 7697 WIRE SAAB SF340 SF340A 7850100 EU ENGINE CONTROL LOOSE A MALA O OTHER O OTHER LD LANDING 1 GL 15 991XJ 340A091 FLIGHT IDLE OVERRIDE PULLED ON LANDING ROLL. F1 FAILED TO OPEN. MAINTENANCE FOUND SPLICE 306VS-DF HAD A WIRE PULLED AN D LOOSE. REPAIRED SPLICE PER SF340W/M CHAP 20. OPS CHECK F1 STOP SYSTEM. ALL CHECKS GOOD IAW SF-340 MM CHAP 76/10. 2 L 7 2 4T RT A52EU 2002060700095 20020607 00095 2002 6 7 MALA020302 4 20020523 A 3425 COMPUTER SAAB SF340 340B 7860101 EU E/E BAY FAILED A MALA K NONE J WARNING INDICATION CR CRUISE 1 GL 15 370PX 340B300 DURING CRUISE CREW RECEIVED AN AVIONICS CAUTION ROLL COMPARITOR FLAG. FOLLOWED QRH AND ISOLATED RIGHT EADI AS BAD COMPO NENT. IN LEVEL FLIGHT EADI SHOWED CLIMBING LEFT TURN. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS COMPUTER O/C/G/. 2 L 7 2 4T RT A52EU 2002060700096 20020607 00096 SW 2002 6 7 HEEA079546 1 20020528 A 3246 212030436007 CAP BELL 412 412 1182202 SW MLG SKID WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 SKID CAP ON MLG HAS RUBBER WORN. 1 G 7 2 4U H4SW 2002122000108 20021220 00108 EU 2002 12 20 MALA020303 1 20020518 A 3242 50125893 BRAKE SAAB SF340 340B 7860101 EU LT MLG DRAGGING A MALA K NONE O OTHER TO TAKEOFF 1 GL 15 365PX 340B265 DURING TAKEOFF ROLL, THE LEFT BRAKE SEEMED TO START DRAGGING OR APPLY ITSELF. REMOVED FOOT FROM THE PEDAL AND A/C CONTI NUED TO PULL LEFT. MORE PRONOUNCED AFTER 40 KNOTS. MAINTENANCE NOTICED LEFT OUTBOARD BRAKE TO BE HOTTER THAN OTHER BRA KES. MAINTENANCE INSTALLED 4 BRAKE TEST GAUGES ON BRAKES. ALL INPUT PRESSURES ARE NORMAL. REF AMM 324003 INSPECTED BR AKE CONTROL VALVE. NO OBVIOUS DEFECTS OR BINDING NOTED. PERFORMED HIGH SPEED TAXI, COULD NOT FEEL ANY DRAGGING TO LEFT . REPLACED BRAKE AS A PRECAUTION PER JC 3240-301. (M) 2 L 7 2 4T RT A52EU 2002060700097 20020607 00097 SW 2002 6 7 HEEA079547 1 20020528 A 6520 SEAL BELL 412 412 1182202 SW T/R GEARBOX LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S AHP00712 36002 TAIL ROTOR GEARBOX HAS A LEAKING INPUT SEAL. REPLACED SEAL AND RETURNED TO SERVICE. 1 G 7 2 4U H4SW 2002060700098 20020607 00098 EU 2002 6 7 MALA020304 1 20020521 A 1430 BOLT BAC 146 AVRO146RJ85A 1500097 EU RT WING LOOSE A MALA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 15 501XJ E2208 FUEL LEAK AT RIGHT WING ROOT. MAINTENANCE FOUND LOWER 3 BOLTS ON REAR SPAR ATTACHMENT. REMOVED, CLEANED, RESEALED AND RETORQUED LOWER 3 BOLTS PER BAE REPAIR INST HC536H9077, LEAK CHECK GOOD. 2 H 7 4 4F RT A49EU 2002060700099 20020607 00099 EU 2002 6 7 MALA020305 1 20020525 A 3230 85106RC84SN6 CONNECTOR SAAB SF340 SF340A 7850100 EU NLG & MLG FAULTY A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 68XJ 340A068 DURING CONTINUITY CHECK/FUNCTION CHECK, OF SEPARATION BOLTS AND EMERGENCY EXTENSION OF MLG AND NLG FOUND BAD CONNECTORS AT BOTH LT & RT SEPARATION BOLTS. MAINTENANCE REMOVED AND REPLACED BOTH LT & RT CONNECTORS. 2 L 7 2 4T RT A52EU 2002060700100 20020607 00100 SW 2002 6 7 HEEA079548 1 20020528 A 6520 212040004009 GEARBOX BELL 412 412 1182202 SW TAIL ROTOR LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 16624 33073 LEAK OUTPUT SHAFT SEAL. REPLACED SEAL AND RETURNED TO SERVICE. 1 G 7 2 4U H4SW 2002060700101 20020607 00101 SO 2002 6 7 COMA0210024 1 20020604 A 3240 BRAKE ASSY EMB 120 EMB120RT 3260202 SO A COMA O OTHER O OTHER LD LANDING 1 SO 01 462CA 120264 FLIGHT 5064 DURING LANDING ALL 4 MLG TIRES BLEW OUT. REPLACED 4 MLG BRAKE ASSY, 4 MLG WHEEL AND TIRES. REPLACED BOTH BR AKE CONTROL VALVES FOR PREVENTIVE MAINT. & ANTI SKID CONTROL BOX - CAUSE OF LOCK UP UNDETERMINED. 2 L 7 2 4T RT A31SO 2002060700102 20020607 00102 SO 2002 6 7 COMA0210025 1 20020606 A 3150 CIRCUIT BREAKER EMB 120 EMB120RT 3260202 SO A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 268CA 120262 FLIGHT 5061 "TRIM" AURAL WARNING DURING T/O.RESET AURAL WARNING CIRCUIT BREAKER - SYSTEM CHECK NORMAL. 2 L 7 2 4T RT A31SO 2002060700103 20020607 00103 SW 2002 6 7 HEEA079549 1 20020528 A 6520 212040004009 GEARBOX BELL 412 412 1182202 SW TAIL ROTOR LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 5759N 33002 GEARBOX LEAKING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700104 20020607 00104 EU 2002 6 7 MALA020306 1 20020528 A 2910 O-RING BAC 146 AVRO146RJ85A 1500097 EU HYD SYSTEM FAILED A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 536XJ E2372 DURING FLIGHT 3512, GREEN HYDRAULIC SYSTEM FAILURE INDICATION. EMERGENCY DECLARED. CREW MADE AN EMERGENCY LANDING. HY DRAULIC QTY ANNUNCIATOR ON GREEN SYSTEM INDICATED 1/4, QRH PERFORMED EMERGENCY LANDING. MAINTENANCE REMOVED AND REPLACE D O-RING, SERVICED HYDRAULICS, AND REPLACED EDP. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2002060700105 20020607 00105 SW 2002 6 7 HEEA079550 1 20020528 A 6520 SEAL BELL 412 412 1182202 SW T/R GEARBOX LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 5759N AFT51543 33002 TAIL ROTOR GEARBOX HAS A LEAKING INPUT SEAL. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700106 20020607 00106 EU 2002 6 7 MALA020307 1 20020529 A 3020 44730501 MODULE SAAB SF340 340B 7860101 EU DEICE SYS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 429XJ 340B429 DURING FLIGHT 3345, LT INTAKE LIGHT ILLUMINATED IN FLIGHT, CYCLES ON AND OFF EVERY 3 TO 4 MINUTES. AIR TURNBACK TO MSP. MAINTENANCE REMOVED AND REPLACED LT DEICE MODULE IAW ACT SPRAY MAT CMM 30-21-03. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002060700107 20020607 00107 WP 2002 6 7 MWEA020328 1 20020515 A 3260 801801 SWITCH DOUG DC9 DC932 3022066 WP RT MLG FAULTY A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 204ME 47680 UPON GEAR RETRACTION RIGHT GEAR UNSAFE LIGHT STAYED ON WITH GEAR HANDLE UP. FOUND RIGHT MAIN GEAR DOWN SWITCH AT FAULT. REMOVED AND REPLACED SWITCH PER MM 32-60-1. 2 L 7 2 4F A6WE 2002060700108 20020607 00108 EA 2002 6 7 COMA0260350 1 20020606 A 5415 601370102 PYLON CNDAIR CL600 CL6002B19 1900309 EA EMPENNAGE CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 420CA 3313 7451 DURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY, DISCOVERED FRETTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTI NG RIB.REPAIRED IN ACCORDANCE WITH REO 601R-54-50-036. 2 L 7 2 4F RT A21EA 2002060700109 20020607 00109 WP 2002 6 7 MWEA020329 1 20020515 A 3260 801801 PROXIMITY SENSOR DOUG DC9 DC932 3022066 WP RT MLG FAILED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 204ME 47680 UPON GEAR RETRACTION RIGHT GEAR UNSAFE LIGHT (RED) STAYED ON WITH GEAR HANDLE UP. REMOVED AND REPLACED RIGHT MAIN LANDI NG GEAR UP LIMIT PROX SENSOR IAW MM 32-60-1. ALSO CHECKED WIRING IN RIGHT WHEEL WELL FOR GENERAL CONDITION AND SECURITY . NO DISCREPANCIES NOTED. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002060700110 20020607 00110 SW 2002 6 7 HEEA079552 1 20020528 A 6310 COUPLING BELL 412 412 1182202 SW ENGINE/XMSN DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T A2002248 33112 ENGINE TO GEARBOX DRIVESHAFT COUPLING SLINGING GREASE. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700111 20020607 00111 WP 2002 6 7 MWEA020336 1 20020521 A 5320 9936534165 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 GALLEY SERVICE DOOR FLOOR SUPPORT HAS SEVERE CORROSION AROUND/UNDER SCREW HOLES (SUPPORT IS FIRST IN FRONT OF GALLEY DOO R), STATION 168-200. FABRICATED AND INSTALLED FLOOR SUPPORT. 2 L 7 2 4F A6WE 2002060700112 20020607 00112 SW 2002 6 7 HEEA079553 1 20020528 A 6310 COUPLING BELL 412 412 1182202 SW ENGINE/GEARBOX DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L A2002438 33006 ENGINE TO GEARBOX SHAFT AFT SEAL SLINGING GREASE. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002060700113 20020607 00113 WP 2002 6 7 MWEA020337 1 20020521 A 5320 9936534183 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 GALLEY SERVICE DOOR FLOOR SUPPORT HAS SEVERE CORROSION UNDER LIP (SUPPORT LOCATED FORWARD OF SEAT TRACK NR 4) AT STATION 168 - 200. REMOVED AND INSTALLED REPLACEMENT FLOOR SUPPORT. 2 L 7 2 4F A6WE 2002060700114 20020607 00114 WP 2002 6 7 MWEA020338 1 20020521 A 5320 99365343 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 GALLEY SERVICE DOOR FLOOR SUPPORT HAS SEVERE CORROSION UNDER LIP (SUPPORT LOCATED BETWEEN FORWARD END OF SEAT TRACKS NR 3 & NR 4) AT STATION 200. FABRICATED AND INSTALLED SUPPORT. 2 L 7 2 4F A6WE 2002060700115 20020607 00115 WP 2002 6 7 MWEA020339 1 20020521 A 5347 59305475 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 NR 4 SEAT TRACK FORWARD END HAS MODERATE CORROSION UNDER A SCREW HOLE AND PREVIOUS CORROSION POT HOLES IN THE TRACK CENT ER (BOTH LOCATED APPROXIMATELY 8 TO 10 INCHES AFT FROM THE TRACK FORWARD END) FROM STATION 200. REMOVED AND REPLACED SE AT TRACK SECTION AND INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2002060700116 20020607 00116 WP 2002 6 7 MWEA020340 1 20020521 A 5320 993653435 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FORWARD GALLEY FLOOR CENTER SUPPORT HAS SEVERE CORROSION UNDER SCREW TANGS AT STATION 180. FABRICATED AND INSTALLED FLO OR SUPPORT. 2 L 7 2 4F A6WE 2002060700117 20020607 00117 SW 2002 6 7 HEEA079557 1 20020528 A 2840 412375001105 INDICATOR BELL 412 412 1182202 SW FUEL SYSTEM MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 RIGHT SIDE, ANALOG AND DIGITAL INDICATOR GOES TO ZERO OR SOME OTHER FIGURE OCASSIONALLY. 1 G 7 2 4U H4SW 2002060700118 20020607 00118 WP 2002 6 7 MWEA020341 1 20020521 A 5320 993693429 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FORWARD GALLEY DEAD CENTER FLOOR SUPPORT (APPROXIMATELY 10 INCHES LONG) HAS ONE SCREW TANG WITH MODERATE CORROSION ON TO P AT STATION 200. FABRICATED AND INSTALLED FLOOR SUPPORT. 2 L 7 2 4F A6WE 2002060700119 20020607 00119 WP 2002 6 7 MWEA020346 1 20020521 A 5321 99328161 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 RIGHT OUTBOARD FLOORBOARD AT STATION 315 HAS PUNCTURE ON INBOARD FORWARD END. FABRICATED AND INSTALLED DOUBLER AND FILL ER. 2 L 7 2 4F A6WE 2002060700120 20020607 00120 WP 2002 6 7 MWEA020348 1 20020521 A 5321 9936585 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 LEFT MID FLOORBOARD AT STATION 430 HAS A PUNCTURE AT INBOARD SIDE AND DELAMINATION ON FORWARD END. FABRICATED AND INSTA LLED FLOORBOARD. 2 L 7 2 4F A6WE 2002060700121 20020607 00121 WP 2002 6 7 MWEA020349 1 20020521 A 5321 9957918524 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 RIGHT OUTBOARD AT STATION 315 HAS A PUNCTURE IN MIDDLE OF FLOORBOARD. REPAIRED MIDDLE OF FLOORBOARD IAW SRM 53-05 FIGUR E 3, TINNERMAN SPEED NUT WASHER ASSEMBLY INSTALLATION. 2 L 7 2 4F A6WE 2002060700122 20020607 00122 WP 2002 6 7 MWEA020350 1 20020521 A 5321 99365341 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FLIGHT DECK FLOOR PANEL HAS A SMALL CRACK LOCATED BETWEEN PILOT'S AFT SEAT TRACKS AND 3 INCHES FORWARD OF EPC PANEL. RE MOVED DAMAGED AREA. LOCATED AND DRILLED DOUBLER AND FAIRING PLATE. INSTALLED DOUBLER AND FAIRING PLATE. 2 L 7 2 4F A6WE 2002060700123 20020607 00123 2002 6 7 HEEA079559 4 20020530 A 3424 71251 GYRO BELL 412 412 1182202 SW COCKPIT INTERFERENCE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 142PH 33150 TURN AND BANK INDICATOR INTERMITTENTLY INOPERATIVE. 1 G 7 2 4U H4SW 2002060700124 20020607 00124 WP 2002 6 7 MWEA020351 1 20020521 A 5310 5910537510 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FORWARD LEFT EMERGENCY EXIT DOOR JAMB IS CHAFED AND NICKED AT UPPER DOOR LATCH AREA. BLENDED AREA AND BLENDOUTS ARE WIT HIN LIMITS PER BOEING TELEX MWX-ORD-02-00271H DATED 5/10/02. 2 L 7 2 4F A6WE 2002060700125 20020607 00125 EA 2002 6 7 COMA0260351 1 20020602 A 7720 6030T41P02 THERMOCOUPLE GE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT ENG FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 964CA GED807463 7129 807463 FLIGHT 5640 LT ENG ITT HOT WARNING - ITT FLUCTUATED FROM NORMAL TO OVER 900 DEGREES.REPLACED THE LOW PRESSURE TURBINE A SSY DUE TO DEFECTIVE THERMOCOUPLE ASSY. 2 L 7 2 4F 4 F RT A21EA E15NE 2002060700126 20020607 00126 WP 2002 6 7 MWEA020357 1 20020521 A 5310 991555920 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 AFT ACCESSORY FRAME 1401 SHEAR TIE HAS CORROSION LOCATED JUST BELOW LONGERON 24 RIGHT. FABRICATED AND INSTALLED SHEAR T IE. 2 L 7 2 4F A6WE 2002060700127 20020607 00127 SW 2002 6 7 HEEA079560 1 20020530 A 7714 75028515 INDICATOR BELL 206 206L3 1182108 SW DUAL TACH MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4835 51131 DUAL TACH SEGMENT FOR INTELLISTART WILL NOT LOCK DOWN. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060700128 20020607 00128 WP 2002 6 7 MWEA020362 1 20020521 A 5524 99185433 BRACKET DOUG DC9 DC982 3022082 WP LT ELEVATOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 LEFT ELEVATOR HORN BALANCE WEIGHT ATTACH BRACKET IS HEAVILY CORRODED WHERE IT ATTACHES TO THE BALANCE WEIGHT. REMOVED A ND REPLACED ATTACH BRACKET. 2 L 7 2 4F A6WE 2002060700129 20020607 00129 EA 2002 6 7 COMA0260352 1 20020605 A 2520 INSULATION CNDAIR CL600 CL6002B19 1900309 EA CABIN OUT OF POSITION A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 455CA 7592 FLIGHT 5315 BURNING ODOR FROM FLIGHT ATTENDANT STATION. FOUND INSULATION TOUCHING F/A DOME LIGHT; REPOSITIONED INSULATI ON. 2 L 7 2 4F RT A21EA 2002060700130 20020607 00130 WP 2002 6 7 MWEA020368 1 20020521 A 5230 59101419 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT CARGO DOOR INNER PAN HAS A DEEP CHAFE NEXT TO AFT LOCK CAM. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002060700131 20020607 00131 WP 2002 6 7 MWEA020372 1 20020521 A 5313 591142923 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 AFT ACCESSORY LONGERON 24 RIGHT AT STATION 1400 HAS AN AREA OF LIGHT CORROSION. REMOVED AND REPLACED LONGERON SECTIONS AND INSTALLED SPLICES. 2 L 7 2 4F A6WE 2002060700133 20020607 00133 EA 2002 6 7 COMA0260353 1 20020603 A 2710 600911775 BELLCRANK CNDAIR CL600 CL6002B19 1900309 EA L/H BINDING A COMA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 914CA 7012 FLIGHT 5296 A/P LWD CAUTION MESSAGE - AILERON CONTROLS ARE STIFF.REPLACED THE L/H AFT AILERON CONTROLS BELLCRANK ASSY. 2 L 7 2 4F RT A21EA 2002060700136 20020607 00136 EA 2002 6 7 COMA0260354 1 20020603 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 466CA 548 7627 FLIGHT 5740 FLAPS FAILED AT GATE.REPLACED THE L/H BPSU. 2 L 7 2 4F RT A21EA 2002060700137 20020607 00137 EU 2002 6 7 2002UALA00919 1 20020527 A 3260 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LANDING GEAR FAILED A UALA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 WP 29 437UA 655 ON FINAL GOT L-G LGCIU 1 FAULT. EXTENDED THE GEAR AND GOT REVERSER NR 1 AS INOP SYSTEM. REPLACED LGCIU-1. 2 L 7 2 4F 4 F RT A28NM E40NE 2002072200021 20020722 00021 NE 2002 7 22 2002UALA00920 2 20020527 A 7532 AC69924 BLEED VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE FAILED A UALA K NONE O OTHER TX TAXI/GRND HDL 1 WP 29 435UA 613 V10390 NR 2 ENGINE EXPERIENCED A HUNG START. HPC BLEED VALVE TEST REVEALED FAILED HPC 7C BLEED VALVE AND WEAK HPC 7A SOLENOID VALVE. VALVES REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002061300117 20020613 00117 NM 2002 6 13 2002UALA00921 1 20020525 A 2720 MR272761545 PCU BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RUDDER MALFUNCTIONED A UALA L ABORTED APPROACH E F VIBRATION/BUFFET FLT CONT AFFECTED AP APPROACH 1 WP 29 370UA 33 24539 LANDED UNDER AMBER ALERT FOR RUDDER VIBRATION. SUPPLEMENTAL DATA UPDATE NUMEROUS FLIGHT CONTROL AND HYDRAULIC SYSTEM CO MPONENTS WERE TESTED. A VERIFICATION TEST FLIGHT WAS PERFORMED TO CHECK FOR VIBRATION. DURING THE TEST FLIGHT; THERE W ERE NO VIBRATIONS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002061200140 20020612 00140 NM 2002 6 12 2002UALA00922 1 20020528 A 3230 271N61191 HOSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT MLG RUPTURED A UALA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 29 555UA 26647 LEFT HYDRAULIC SYSTEM QUANTITY DECREASED TO .14 WITH ASSOCIATED LOW SYSTEM PRESSURE WARNING AND LEFT ENGINE AND ACMP LOW PRESSURE WARNING. LEFT MAIN GEAR DOWNLOCK HOSE RUPTURED. REPLACED HOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072200022 20020722 00022 NE 2002 7 22 2002UALA00923 2 20020529 A 7230 BLADE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT ENGINE FAILED A UALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 WP 29 435UA 12803 613 V10390 RIGHT ENGINE FAILED. BORESCOPE INSPECTION REVEALED FAILED HIGH PRESSURE COMPRESSOR STAGE 4 BLADES, CAUSING MAJOR INTERN AL ENGINE DAMAGE AND AUTO-SHUTDOWN. ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002061200141 20020612 00141 NM 2002 6 12 2002UALA00924 1 20020528 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 AFT EXTERNAL FUSELAGE, AFT WATER DRAIN MAST, CORROSION AROUND BASE, BODY STATION 1417, STRINGER 35R. MAJOR REPAIR ACCOM PLISHED. REPAIRED SKIN WITH EXTERNAL DOUBLER. 2 L 7 2 4F 4 F RT A1NM E3NE 2002060700138 20020607 00138 NM 2002 6 7 2002UALA00926 1 20020528 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 AFT PIT STATION 1520 STRINGER 23R TO 25R, FRAME UPPER CHORD AFT EDGE HAS GOUGES FROM CONTACT WITH SIDEWALL PANEL SCREWS. MAJOR REPAIR ACCOMPLISHED. FRAME SPLICE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002060700139 20020607 00139 NM 2002 6 7 2002UALA00928 1 20020529 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 CREASE BEAM WEB CORRODED AT STATION 1020, RBL 80, WL208, FWD END OF WEB. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002060700140 20020607 00140 2002 6 7 HEEA079561 4 20020530 A 3197 75028515 INDICATOR BELL 206 206L3 1182108 SW CAUTION PANEL SHORTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21497 51518 CAUTION PANEL FUEL FILTER SEGMENT SHORTED OUT AND LIGHT STAYING ON. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002061200142 20020612 00142 NM 2002 6 12 2002UALA00929 1 20020527 A 5750 FITTING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 604UA 21865 RIGHT HAND WING FRONT SPAR OUTBOARD PITCHLOAD FITTING CRACKED AT THE FORWARD UPPER RADIUS ABOVE FITTING LUG, CRACK FOUND AND CONFIRMED. MAJOR REPAIR ACCOMPLISHED. REPLACED OUTBOARD PITCHLOAD FITTING. 2 L 7 2 4F 4 F RT A1NM E3NE 2002060700141 20020607 00141 NM 2002 6 7 2002UALA00932 1 20020525 A 5754 SLAT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 LT WING NR 1 SLAT HAS CRACKS IN AFT ROW OF RIVETS, NR 29 THROUGH NR 33 FROM INBOARD SIDE FROM BLACK STRIP. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED HFEC INSPECTION ON CUTOUT AFTER DAMAGE REMOVAL. DOUBLER REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060700142 20020607 00142 NM 2002 6 7 2002UALA00934 1 20020524 A 5320 ANGLE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 938UA 26671 FWD GALLEY DOOR CUTOUT L-ANGLE CRACKED BETWEEN BS 294.5 FRAME AND DOOR SURROUND AT CREASE BEAM. MAJOR REPAIR ACCOMPLISH ED. REPLACED L-ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060700143 20020607 00143 NM 2002 6 7 2002UALA00935 1 20020524 A 5320 ANGLE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 938UA 26671 FWD CABIN RT CREASE BEAM INBOARD Z-ANGLE UPPER SURFACE CORRODED BETWEEN BS 277 AND 344, WL 208. MAJOR REPAIR ACCOMPLISH ED. INSTALLED NEW Z-ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060700144 20020607 00144 NM 2002 6 7 2002UALA00937 1 20020524 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 STATION 188 STRINGER 18L FUSE FRAME CHORD IS CRACKED IN RADIUS. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER WAS INSTALLE D OVER CHORD AND OVER EXTERNAL FUSE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060700145 20020607 00145 NM 2002 6 7 2002UALA00938 1 20020529 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 938UA 26671 FORWARD NOSE COMPARTMENT STA 188 FRAME CHORD IS CRACKED AT WL 207, RT SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBL ER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060700146 20020607 00146 NM 2002 6 7 2002UALA00939 1 20020529 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 938UA 26671 FORWARD NOSE COMPARTMENT STA 188 FRAME CHORD IS CRACKED AT WL 208, LT SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBL ER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002060700147 20020607 00147 NM 2002 6 7 2002UALA00940 1 20020529 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 AFT CABIN PRESSURE DECK CORRODED AT STATION 1684 RBL 52 IN. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002060700148 20020607 00148 NM 2002 6 7 COOSDR02110 1 20020601 A 5514 BEAM BOEING 727 727233 138408A NM HORIZ STAB CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 LEFT HORIZONTAL STAB TRAILING EDGE BEAM LOWER CHORD AT STAB STA 105 INCHES WITH CORROSION. 2 L 7 3 4F RT A3WE 2002060700149 20020607 00149 WP 2002 6 7 COOSDR02111 1 20020430 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED W EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 605AL 46106 LOWER FUSELAGE, SKIN CORRODED - YSTA 1690.0 LONGERON 34 LEFT. 2 L 7 4 4F RT 4A25 2002060700150 20020607 00150 NM 2002 6 7 COOSDR02112 1 20020430 A 3610 69171802 DUCT BOEING 727 72723 1384004 NM PNEUMATIC SYS CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 AIR CONDITIONING BAY STA 850 PNEUMATIC DUCT CRACKED. 2 L 7 3 4F A3WE 2002060700151 20020607 00151 NM 2002 6 7 COOSDR02113 1 20020430 A 5311 FRAME BOEING 727 72723 1384004 NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 LOWER FUSELAGE STATION 950 BULKHEAD, LOWER CHORD CORRODED STRINGER 29 LEFT. 2 L 7 3 4F A3WE 2002060700152 20020607 00152 NM 2002 6 7 COOSDR02116 1 20020601 A 5751 658175634 AILERON BOEING 727 727233 138408A NM RT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 RIGHT WING, OUTBOARD AILERON TRAILING EDGE WITH DELAMINATION. 2 L 7 3 4F RT A3WE 2002060700153 20020607 00153 NM 2002 6 7 COOSDR02117 1 20020601 A 5753 652163491 FLAP BOEING 727 727233 138408A NM LT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 LEFT WING, INBOARD AFT FLAP WITH DELAMINATION. 2 L 7 3 4F RT A3WE 2002060700154 20020607 00154 NM 2002 6 7 COOSDR02118 1 20020601 A 5753 6521630188 FLAP BOEING 727 727233 138408A NM RT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 RIGHT WING, INBOARD FORE FLAP WITH DELAMINATION. 2 L 7 3 4F RT A3WE 2002060700155 20020607 00155 NM 2002 6 7 COOSDR02119 1 20020601 A 5753 652163492 FLAP BOEING 727 727233 138408A NM RT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 RIGHT WING INBOARD AFT FLAP WITH DELAMINATION. 2 L 7 3 4F RT A3WE 2002060700156 20020607 00156 EA 2002 6 7 COMA0260355 1 20020604 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 952CA 7092 FLIGHT 5494 NOSE GEAR DISAGREE WARNING. NLG UNSAFE INDICATION.INSPECTED NLG AND PERFORMED EXT AND RETRACTION CHECKS. NO FAULTS FOUND. 2 L 7 2 4F RT A21EA 2002060700157 20020607 00157 NM 2002 6 7 COOSDR02120 1 20020601 A 5730 6521656621 PANEL BOEING 727 727233 138408A NM LT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 LEFT WING, MAIN LANDING GEAR PANEL WITH DELAMINATION. 2 L 7 3 4F RT A3WE 2002060700158 20020607 00158 NM 2002 6 7 COOSDR02121 1 20020601 A 5730 6521657253 PANEL BOEING 727 727233 138408A NM LT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 LEFT WING, TRAILING EDGE UPPER PANEL WITH DELAMINATION. 2 L 7 3 4F RT A3WE 2002060700159 20020607 00159 EU 2002 6 7 MALA020324 1 20020513 A 5320 7253720319 BEAM SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K-CHECK IN CWA, RH ANGLE BEAM BETWEEN STA 272-288 HAS CORROSION. MAINTENANCE INSTALLED NEW BEAM PN 7253720-319 AND ANGLE PN 7253720-337 BETWEEN STA 272-288 ON RH SIDE IAW SAAB SRM 51. 2 L 7 2 4T RT A52EU 2002060700160 20020607 00160 EU 2002 6 7 MALA020326 1 20020512 A 5320 7253720210 CLIP SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K-CHECK IN CWA, SEAT TRACK LBL 18.3 FWD CLIP HAS CORROSION. MAINTENANCE INSTALLED NEW CLIP PN 7253720-210 ON LH FWD SECTION OF SEAT TRACK IAW SAAB SRM 51. 2 L 7 2 4T RT A52EU 2002060700161 20020607 00161 SW 2002 6 7 HEEA079562 1 20020530 A 3150 75028517 INDICATOR BELL 206 206L3 1182108 SW CAUTION PANEL MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4180F TRANSMISSION CHIP CAUTION LIGHT SEGMENT LOOSE AND STAYS ON DIM. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002060700162 20020607 00162 2002 6 7 HEEA079563 4 20020530 A 3442 78806059008 DISPLAY BELL 206 206L3 1182108 SW WX RADAR INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4282Z 51499 WEATHER RADAR WILL NOT DISPLAY. 1 G 7 1 3U H2SW 2002060700163 20020607 00163 2002 6 7 HEEA079564 4 20020530 A 3442 80510800001 CONTROL BOX BELL 206 206L3 1182108 SW WX RADAR WILL NOT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 21497 51518 WEATHER RADAR CONTROL BOX FAILS IN SELF TEST OR WHEN IN OPERATE MODE. 1 G 7 1 3U H2SW 2002060700164 20020607 00164 NM 2002 6 7 UPS02238117 1 20020504 A 3350 BATTERY BOEING 727 727172C 1384058 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:PFLT FWD ENTRY DOOR EMER EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES OPS CHK GOOD. 2 L 7 3 4F A3WE 2002060700165 20020607 00165 2002 6 7 HEEA079565 4 20020530 A 3442 80510800001 CONTROL BOX BELL 206 206L3 1182108 SW WX RADAR SYS INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 54641 51184 WEATHER RADAR CONTROL BOX INOPERATIVE. SKYWATCH ERROR NR 19. 1 G 7 1 3U H2SW 2002060700167 20020607 00167 2002 6 7 HEEA079567 4 20020530 A 3442 80510800001 CONTROL BOX BELL 206 206L3 1182108 SW WX RADAR MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6748D 51106 WEATHER RADAR CONTROL BOX DATA FAIL ERROR CODE. 1 G 7 1 3U H2SW 2002060700169 20020607 00169 NM 2002 6 7 UPS02238231 1 20020514 A 3350 BATTERY BOEING 727 72730C 1384009 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE:AS-E BATTERIES IN THE COCKPIT EMERGENCY EXIT LIGHT ASSY ARE WEAK. UPON REPLACEMENT OF BATTERIES, THE BA TTERY TRAY END TAB BROKE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSY IN THE COCKPIT AS PER M/M 33-50-67. OP'S CHECKS GOOD. OK FOR SERVICE. 2 L 7 3 4F A3WE 2002060700170 20020607 00170 EA 2002 6 7 COMA0260356 1 20020605 A 7930 5018T49P03 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE R/H AGB LEAKING A COMA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 01 958CA 7111 807088 FLIGHT 5570 R/H ENGINE LOW OIL PRESSURE WARNING.REPLACED THE ACCESSORY GEAR BOX DRIVE SEALS AT AXIS D,F,&BB. 2 L 7 2 4F 4 F RT A21EA E15NE 2002060700171 20020607 00171 2002 6 7 HEEA079569 4 20020530 A 3442 80510800001 CONTROL BOX BELL 206 206L3 1182108 SW WX RADAR INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 30KH 51527 WEATHER RADAR CONTROL BOX INOPERATIVE. 1 G 7 1 3U H2SW 2002060700172 20020607 00172 2002 6 7 HEEA079570 4 20020530 A 3442 80510800001 CONTROL BOX BELL 206 206L3 1182108 SW WX RADAR SYS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 31801 51074 WEATHER RADAR CONTROL BOX SKYWATCH FAIL WITH CODE OF 144. 1 G 7 1 3U H2SW 2002060700173 20020607 00173 2002 6 7 HEEA079571 4 20020530 A 3442 80510800001 CONTROL BOX BELL 206 206L3 1182108 SW WX RADAR INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4282Z 51499 WEATHER RADAR CONTROL BOX INOPERATIVE. WILL NOT DISPLAY. 1 G 7 1 3U H2SW 2002060700174 20020607 00174 2002 6 7 HEEA079572 4 20020530 A 3442 80510800001 CONTROL BOX BELL 407 407 1182206 SW WX RADAR INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 501PH 53401 WEATHER RADAR CONTROL BOX INOPERATIVE. 1 G 7 1 3U O H2SW 2002060700175 20020607 00175 2002 6 7 HEEA079574 4 20020530 A 3457 81439000232 GPS BELL 412 412 1182202 SW COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1202T 33112 GPS WOULD NOT ACCEPT NEW OR REMOVED DATA CARD INPUTS. FOUND UNIT TO HAVE ALOT OF DUST AND DIRT INSIDE FACEPLATE AREA. C LEANED UNIT. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002060700176 20020607 00176 2002 6 7 HEEA079575 4 20020530 A 3457 81439000232 GPS BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 GPS UNIT INTERMITTENTLY CUTS OFF AND DROPS USER WAYPOINTS. FOUND ROTARY ENCODER SWITCH BAD AND REPLACED. REPAIRED. BEN CH CHECK GOOD. 1 G 7 2 4U H4SW 2002060700177 20020607 00177 2002 6 7 HEEA079576 4 20020530 A 3457 81439000232 GPS BELL 206 206L3 1182108 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 141BH 51303 GPS RECEIVER DISPLAY DOES NOT READ CORRECTLY ON POWER UP AND CANNOT RESET UNIT. 1 G 7 1 3U H2SW 2002060700178 20020607 00178 2002 6 7 HEEA079577 4 20020530 A 3457 81439000232 GPS BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 FM BLEEDS THROUGH REGARDLESS OF TOGGLE SWITCH POSITION. WILL NOT POWER UP. 1 G 7 2 4U H4SW 2002060700179 20020607 00179 2002 6 7 HEEA079578 4 20020530 A 3457 8143902240B GPS BELL 206 206L1 1182107 SW COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2777D 45299 GPS RECEIVER SELECTOR KNOB NOT WORKING PROPERLY. FOUND MSG AND NRST BUTTONS INTERMITTENT AND HAD NO DETENT WHEN PRESSED. CLEANED ALL KEYPAD BUTTON SWITCHES AND REALIGNED BUTTONS AND SWITCHES. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 2002060700180 20020607 00180 NM 2002 6 7 GAIA02041ST 1 20020429 A 5230 MS20253P47200 HINGE BOEING 727 727243 138408D NM CARGO DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SO 07 1269Y 21269 DURING A CPCP INSPECTION, IT WAS DISCOVERED THAT THE MAIN CARGO DOOR AFT HINGE UPPER SECTION CRACKED AT THE LAST TWO LOB ES, BS 650. REMOVED AND REPLACED MAIN CARGO DOOR HINGE. 2 L 7 3 4F RT A3WE 2002060700181 20020607 00181 2002 6 7 HEEA079579 4 20020530 A 3457 8143902240B GPS BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 GPS LOST MEMORY. 1 G 7 2 4U H4SW 2002060700182 20020607 00182 2002 6 7 HEEA079580 4 20020530 A 3457 8143902240B GPS BELL 206 206L3 1182108 SW COCKPIT INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 206FS 51506 GPS RECEIVER INOPERATIVE. 1 G 7 1 3U H2SW 2002060700183 20020607 00183 NM 2002 6 7 0201796622 1 20020602 A 2530 SWITCH BOEING 747 747251B 1384892 NM NBR 3 GALLEY A NWAA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE UK UNKNOWN 1 GL 01 622US 21704 DURING FLIGHT, THE NBR 2 AFT COFFEEMAKER IN THE NBR 3 GALLEY OVERFLOWED AND SPARKS FLAMED OUT NEAR WARMER PAD AND THE CI RCUIT BREAKER POPPED. THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE SWITCH FOR PULL OUT HOT PLATE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002060700184 20020607 00184 2002 6 7 HEEA079581 4 20020530 A 3457 8143902240B GPS BELL 412 412 1182202 SW COCKPIT WILL NOT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3911L 33023 2 YEAR INSPECTION. FOUND UNIT FAILS GPS TEST. MESSAGE BUTTON INTERMITTENT. 1 G 7 2 4U H4SW 2002060700185 20020607 00185 NM 2002 6 7 UPS02238548 1 20020530 A 5310 BEAM BOEING 727 72731C 1384011 NM BS 1183 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C CRACK INDICATING AT BS 1183 BEAM LBL 26.83 WL AT 250 APPROX REPAIR CARRIED OUT IAW EO B727-5311-06 31 APPENDIX D 2 L 7 3 4F A3WE 2002060700186 20020607 00186 NM 2002 6 7 UPS02238550 1 20020531 A 5310 BEAM BOEING 727 72731C 1384011 NM BS 1183 RBL 26 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C CRACK INDICATION AT BS 1183 BEAM RBL 26.83 WL 250 APPROX. REPAIR CARRIED OUT IAW EO B727-5311-0631 APPENDIX D 2 L 7 3 4F A3WE 2002060700187 20020607 00187 NM 2002 6 7 GAIA02042ST 1 20020429 A 5330 SKIN BOEING 727 727243 138408D NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 1269Y 21269 DURING A CPCP INSPECTION, IT WAS DISCOVERED THAT SEVERAL DISHED FASTENER HEADS ALONG STRINGER 28L AND 28R FROM BS 480-48 5. ACCOMPLISHED FUSELAGE SKIN REPAIR AT BS 480-495, STR 28R, AND REPAIRED STR 28R IAW B727 SRM. 2 L 7 3 4F RT A3WE 2002060700188 20020607 00188 NM 2002 6 7 UPS02238551 1 20020527 A 2780 RIB BOEING 727 72731C 1384011 NM #3 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C RIB CRACKED ON LE SLAT #3, RIB LOCATED I/B OF O/B TRACK #3 SLAT REMOVED TO CARRY OUT REPAIR ON CRA CKED RIB IAW MM 27-81-11 CRACKED RIB REPAIRED IAW SRM 57-50-3 FIG 9 #3 SLAT INSTALLED AFTER REPAIR COMPLETED IAW MM 27-8 1-11 2 L 7 3 4F A3WE 2002060700189 20020607 00189 NM 2002 6 7 UPS02238552 1 20020521 A 5720 SLAT BOEING 727 72731C 1384011 NM #6 SLAT LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C DENTS ON SLAT POSITIONS 6 & 8 DENTS RE-WORKED IAW SRM 51-40-1 HFEC INSP. CARRIED OUT IAW NDT MANUA L, PART 6 51-00-00 FIG 4 - #8 S LAT NDF. #6 SLAT SKIN CRACKED & CRACK ENDS MARKED. #6 SLAT REPAIRED IAW SRM 57-30-03 SL AT REMOVED & INSTALLED IAW MM 27-81-11 2 L 7 3 4F A3WE 2002060700190 20020607 00190 NM 2002 6 7 UPS02238553 1 20020521 A 5210 DOOR FRAME BOEING 727 72731C 1384011 NM FWD ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C CRACK IN DOOR FRAME AT AFT UPPER CORNER OF FWD ENTRY DOOR DOOR FRAME REPLACED IAW SMRO EO 2002-031 -001 UPS ENGINEERING FILE NO. 727-52-20008 2 L 7 3 4F A3WE 2002060700191 20020607 00191 NM 2002 6 7 UPS02238554 1 20020522 A 5210 DOOR FRAME BOEING 727 72731C 1384011 NM FWD ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C ON REMOVAL OF AFT LWR STOP WHICH IS CRACKED, DOOR FRAME FOUND CRACKE D AT LWR END ON FWD ENTRY DOOR REPAIR CARRIED OUT IAW SMRO EO 2002-031-002 UPS ENGINEERING FILE NO 727-52-20009 2 L 7 3 4F A3WE 2002072300169 20020723 00169 NM 2002 7 23 UPS02238555 1 20020522 A 5330 SKIN BOEING 727 72731C 1384011 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C CORROSION BETWEEN SKIN & INTERNAL DOUBLER AT BS 1180 BETWEEN S10L & 9L. REPAIR CARRIED OUT IAW SRM 51 -10-6 & 53-30-3, DAMAGE CUT OUT IAW 51- 10-6. REPAIRED IAW 51-10-2 AND 53-30-3 FIG 1 STEP 4. 2 L 7 3 4F A3WE 2002060700192 20020607 00192 NM 2002 6 7 UPS02238556 1 20020523 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 211.8 R/H CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C CRACK IN SECTION 41 FUSELAGE SKIN AT BS 211.8 R/H AT WL 197.5 REPAIR CARRIED OUT IAW SRM 53-30-3 F IG 3 USING 0.063" DOULER IAW EO B727-5330-0795-G 2 L 7 3 4F A3WE 2002060700193 20020607 00193 2002 6 7 HEEA079582 4 20020530 A 3457 8143902240B GPS BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 33008 36004 GPS TAKES TOO LONG TO GO INTO TRK. 1 G 7 2 4U H4SW 2002060700194 20020607 00194 NM 2002 6 7 GAIA02043ST 1 20020429 A 5313 STRINGER BOEING 727 727243 138408D NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 1269Y 21269 DURING A CPCP INSPECTION, IT WAS DISCOVERED THAT BS 490, STR 27L IS CORRODED. ACCOMPLISHED STRINGER REPAIR AT BS 490, S TR 27L IAW B727, SRM. 2 L 7 3 4F RT A3WE 2002060700195 20020607 00195 2002 6 7 HEEA079583 4 20020530 A 3457 8143802240D GPS BELL 206 206L1 1182107 SW COCKPIT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 83MT 45492 FACEPLATE COMING APART. FOUND DISPLAY LENS COMING APART. REPLACED DISPLAY LENS. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 2002060700196 20020607 00196 EA 2002 6 7 COMA0260357 1 20020530 A 2750 853D10012 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA R/H #3 INOPERATIVE A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 973CA 13636 7146 FLIGHT 5695 FLAPS FAIL MESSGE WHEN SELECTED 20 DEGREES. POST FLIGHT INSP FOUND R/H OUTBD FLAP TWISTED.REPLACED FAILED R/ H #3 FLAP ACTUATOR AND ALL RELATED DAMAGED COMPONENTS PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002060700197 20020607 00197 2002 6 7 HEEA079584 4 20020530 A 3457 8143802240D GPS BELL 206 206L3 1182108 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3207Q 51540 GPS RECEIVER CARD NEEDS ALIGNMENT. 1 G 7 1 3U H2SW 2002060700198 20020607 00198 NM 2002 6 7 COOSDR02122 1 20020601 A 5730 6521655479 PANEL BOEING 727 727233 138408A NM RT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 RIGHT WING MAIN LANDING GEAR TRAILING EDGE UPPER PANEL WITH DELAMINATION. 2 L 7 3 4F RT A3WE 2002060700199 20020607 00199 NM 2002 6 7 COOSDR02124 1 20020601 A 5730 6519381163 PANEL BOEING 727 727233 138408A NM LT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 994AJ 20942 LEFT WING, TRAILING EDGE LOWER PANEL WITH DELAMINATION. 2 L 7 3 4F RT A3WE 2002060700200 20020607 00200 NM 2002 6 7 COOSDR02125 1 20020601 A 5330 SKIN BOEING 727 72723 1384004 NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 LOWER FUSELAGE SKIN CORRODED, BS 720.0 STRINGER 21 RIGHT. 2 L 7 3 4F A3WE 2002060700201 20020607 00201 NM 2002 6 7 COOSDR02126 1 20020601 A 5711 SPAR BOEING 727 72723 1384004 NM CENTER WING CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 WING CENTER SECTION, FRONT SPAR LOWER CHORD FROM RBL 24.5 TO RBL 70.5, CORRODED. 2 L 7 3 4F A3WE 2002060700202 20020607 00202 NM 2002 6 7 COOSDR02127 1 20020601 A 5523 657279920 TAB BOEING 727 72723 1384004 NM ELEVATOR DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 ELEVATOR TAB DELAMINATED. 2 L 7 3 4F A3WE 2002060700203 20020607 00203 NM 2002 6 7 COOSDR02128 1 20020601 A 5755 651734748 SPOILER BOEING 727 72723 1384004 NM LT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 LEFT WING SPOILER NR 2 DELAMINATED. 2 L 7 3 4F A3WE 2002060700204 20020607 00204 NM 2002 6 7 COOSDR02129 1 20020601 A 5753 6521630173 FLAP BOEING 727 72723 1384004 NM LT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 FLAP, LEFT WING INBOARD FORE FLAP DELAMINATED. 2 L 7 3 4F A3WE 2002060700205 20020607 00205 NM 2002 6 7 COOSDR02130 1 20020601 A 5753 65192692 SPACER BOEING 727 72723 1384004 NM T/E FLAP CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 RIGHT WING INBOARD FLAP, INBOARD TRACK, CENTER SPACER BLOCK CRACKED. 2 L 7 3 4F A3WE 2002060700206 20020607 00206 NM 2002 6 7 COOSDR02131 1 20020601 A 5310 DOOR FRAME BOEING 727 72723 1384004 NM FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 FORWARD CARGO COMPARTMENT STA 520 AND AFT CARGO COMPARTMENT STA 1057.60 DOORWAY FRAMES, CRACKED 2 L 7 3 4F A3WE 2002060700207 20020607 00207 NM 2002 6 7 COOSDR02137 1 20020601 A 5514 65245711 BEAM BOEING 727 72723 1384004 NM HORIZ STAB CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 RIGHT AND LEFT HORIZONTAL STABILIZER, TRAILING EDGE, UPPER BEAM CORRODED. 2 L 7 3 4F A3WE 2002060700208 20020607 00208 NM 2002 6 7 COOSDR02138 1 20020601 A 5514 65241892 BEAM BOEING 727 72723 1384004 NM HORIZ STAB CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 RIGHT AND LEFT HORIZONTAL STABILIZER, TRAILING EDGE, LOWER BEAM CORRODED. 2 L 7 3 4F A3WE 2002060700209 20020607 00209 NM 2002 6 7 COOSDR02139 1 20020601 A 5330 SKIN BOEING 727 72723 1384004 NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 FUSELAGE, BS 480 BETWEEN STR 12R AND STR 14R, SKIN WITH CORROSION. 2 L 7 3 4F A3WE 2002060700210 20020607 00210 NM 2002 6 7 COOSDR02140 1 20020601 A 5330 DOUBLER BOEING 727 72723 1384004 NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 FUSELAGE, FROM BS 1148 TO BS 1155, BETWEEN STR 19L AND STR 21L, SKIN INTERNAL DOUBLER WITH CORROSION. 2 L 7 3 4F A3WE 2002060700211 20020607 00211 NM 2002 6 7 COOSDR02142 1 20020601 A 5511 SPAR BOEING 727 72723 1384004 NM HORIZ STAB CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 LEFT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD, CORRODED. 2 L 7 3 4F A3WE 2002060700212 20020607 00212 NM 2002 6 7 COOSDR02143 1 20020601 A 5511 RIB BOEING 727 72723 1384004 NM HORIZ STAB CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 LEFT RT HORIZONTAL STABILIZER TRAILING EDGE HINGE SUPPORT RIBS CRACKED. 2 L 7 3 4F A3WE 2002060700213 20020607 00213 NM 2002 6 7 COOSDR02145 1 20020601 A 5330 SKIN BOEING 727 72723 1384004 NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 SECTION 43, FROM BS 600 TO BS 640 AT STR. 26R, FUSELAGE SKIN CORRODED. 2 L 7 3 4F A3WE 2002060700214 20020607 00214 NM 2002 6 7 GAIA02044ST 1 20020429 A 5320 6548636378 ANGLE BOEING 727 727243 138408D NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 1269Y 21269 (ANGLE) DURING A CPCP INSPECTION, IT WAS DISCOVERED THAT BS 870 BULKHEAD WEB TO KEEL BEAM ATTACH ANGLE IS CRACKED IN TH E RIGHT WHEEL WELL AT RBL 8. REMOVED AND REPLACED BS 870 BULKHEAD TO KEEL BEAM ANGLE IAW SRM. 2 L 7 3 4F RT A3WE 2002061000242 20020610 00242 NM 2002 6 10 F3LA200200160 1 20020605 A 5310 DOOR FRAME BOEING 737 7373L9 1384470 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3389 26440 DURING C-2 CHECK, INSPECTION REPORTED HOLE IN AFT CARGO DOOR FWD FRAME CAP WEB. FABRICATED AND INSTALLED WEB REPAIR PER SRM 51-70-13, 51-10-02 AND 51-70-13. 2 L 7 2 4F RT A16WE 2002061000247 20020610 00247 NM 2002 6 10 F3LA200200161 1 20020605 A 5320 6549576 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3269 26293 DURING C-3 CHECK, INSPECTION REPORTED VERTICAL WEB CORRODED INBOARD OF C-2 DOOR THRESHOLD FROM STA 794 TO 847 AT STR 25R . REPLACED VERTICAL WEB. 2 L 7 2 4F RT A16WE 2002060700215 20020607 00215 WP 2002 6 7 DHL2002802509 1 20020516 A 5230 SKIN DOUG DC8 DC873 302199C WP A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 802DH 46076 ITEM: N/R: 0895 FUSELAGE DOORS- (BELLY DOOR) "B"LOWER INNER SKIN CRACKED 1"CORR: REMOVED FASTNERS IAW SRM51-1-21 PG. 1 , PERFORMED STOP DRILL ON LOWER INNER SKIN CRACKIAW SRM 52-2-0 FIG. 2 , FABRICATED DOUBLER (2024T3 AL .O4O) IAW SRM 52-4-1 FIG. 3, CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B , INSTALLED DOUBLER ON LOWER SKIN IAW SRM 52-4-1 FIG 3 AND SRM 51 -1-21 PG. 1 2 L 7 4 4F RT 4A25 2002060700216 20020607 00216 WP 2002 6 7 DHL2002802510 1 20020523 A 5313 47505211 FITTING DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 802DH 79074 46076 ITEM: N/R 0457 MAIN CARGO COMPT.-SPLICE FITTING CRACKED 3" STA. 902.000 L1CORR.: REMOVED CRACKED SPLICE FITTING ON MAIN CARGO COMPT. IAW SRM 51-1-23 FIG. 48 , CLEANED , TREATED AND PRIMED AREA IAW SRM 51-1-8B , INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D PAGE 9 AND SRM 51-1-23FIG. 8 2 L 7 4 4F RT 4A25 2002061000250 20020610 00250 NM 2002 6 10 F3LA200200163 1 20020605 A 5320 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3269 26293 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON C2 ENTRY SILL WEB ALONG OUTBOARD EDGE UNDER SCUFF PLATE CORNERS AND O N UNDERSIDE OF WEB AROUND NUT PLATES. REPLACED C2 ENTRY SILL WEB PER SRM 51-40-05, 51-40-08 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002060700217 20020607 00217 WP 2002 6 7 DHL2002802512 1 20020516 A 5230 SKIN DOUG DC8 DC873 302199C WP A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 802DH 46076 ITEM:N/R 0895 "B" BELLY DOOR LWR. INNER SKIN CRACKED 1" STA.520.000 (MAJOR REPAIR)PERFORMED MAJOR REPAIR IAW SRM 52-2-0 FIG. 2 SHEETS 3 , REMOVED FASTNERS IAW SRM 51-1-21 PAGE1,PERFORMED STOP DRILL ON LWR. INNER SKIN CRACKED IAW SRM52-2-0 F IG2 SHEET 3 FABRICATED DOULBER(2024 T3 AL .040) IAW SRM52-4-1 FIG. 3 , CLEANED ,TREATED AND PRIMED IAW SRM 51-1-8B , INS TALLED DOUBLER ON LOWER SKIN IAW SRM 52-4-1 FIG 3 AND SRM 51-1-21 PG.1 2 L 7 4 4F RT 4A25 2002061000252 20020610 00252 NM 2002 6 10 F3LA200200164 1 20020605 A 5522 6573795 SKIN BOEING 737 7372P6 1C84609 NM ELEVATOR DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3135 21613 ON WALKAROUND, FLIGHT CREW REPORTED LT ELEVATOR DELAMINATED ON TRAILING EDGE. REPAIRED PER SRM 51-40-9, PARAGRAPH 4 AND EA 55-737-063. 2 L 7 2 4F RT A16WE 2002060700218 20020607 00218 EU 2002 6 7 RAIA00205168 1 20020526 A 7930 8582 PRESSURE SWITCH JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 559HK 5 41075 5482-STL- LEFT ENGINE OIL PRESSURE WARNING LIGHT CAME ON DURING TAXI. GAUGE SHOWS GOOD PRESSURE. MAINTENANCE DEFERRED OI L PRESSURE WARNING LIGHT IAW J41 MEL 79-4. SUBSEQUENTLY MAINTENANCE CLEARED THE DMI REMOVING AND REPLACING THE #1 OIL PR ESSURE SWITCH. 2 L 7 2 4T RT A41NM 2002060700219 20020607 00219 SO 2002 6 7 RAIA00206169 1 20020601 A 3242 D3899926FA986 CONNECTOR EMB 145 EMB145 3260210 SO A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 801HK 145053 5290-RIC- DURING TAKE OFF GOT TAKEOFF CONFIGURATION BRAKE WARNING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BRAKE PRESSURE SWITCH CONNECTOR. 2 L 7 2 4F RT T00011AT 2002060700220 20020607 00220 EU 2002 6 7 RAIAOO206170 1 20020602 A 7800 141780015 STOP JETAIR JETSTM JETSTM4101 1500501 EU A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 571HK 41090 5529-STL- DURING TAXI LEFT ENGINE OVERHEAT LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE #! ENGINE EXHAUST PIP E STOP PLATES. 2 L 7 2 4T RT A41NM 2002060700221 20020607 00221 SO 2002 6 7 RAIA00206171 1 20020602 A 3350 1317 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 804HK 145082 5251-PIT- FOURTH OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB AT FOURTH OVERHEAD EMERGENCY LIGHT. 2 L 7 2 4F RT T00011AT 2002060700222 20020607 00222 EU 2002 6 7 RAIA00206172 1 20020602 A 2422 PC125123B INVERTER JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 569HK 13845 9622 41088 5473-STL- LEFT INVERTER FAIL INDICATION. MAINTENANCE REMOVER AND REPLACED THE LEFT INVERTER. 2 L 7 2 4T RT A41NM 2002061000001 20020610 00001 2002 6 10 HEEA079585 4 20020530 A 3457 8143902240B GPS BELL 206 206L3 1182108 SW COCKPIT INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 31077 51520 GPS RECEIVER INOPERATIVE. 1 G 7 1 3U H2SW 2002061000002 20020610 00002 SW 2002 6 10 HEEA079586 1 20020530 A 6210 EROSION SHIELD BELL 412 412 1182202 SW M/R BLADE TORN E K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 5592 A181 36003 EROSION SHIELD ON MAIN ROTOR BLADE IS TORN ON THE LOWER SIDE AT THE OUTBOARD END. 1 G 7 2 4U H4SW 2002061000003 20020610 00003 SW 2002 6 10 HEEA079587 1 20020530 A 6210 SPAR BELL 412 412 1182202 SW M/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 13477 A471 33076 MAIN ROTOR BLADE TRAILING EDGE SPAR BELOW THE MID SPAN TRIM TAB IS CRACKED. 1 G 7 2 4U H4SW 2002061000005 20020610 00005 SW 2002 6 10 HEEA079589 1 20020530 A 6210 412015300109 BLADE BELL 412 412 1182202 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 12800 36002 OUTBOARD ABRASION STRIP ON MAIN ROTOR BLADE HAS SEVERAL EROSION HOLES. SENT TO ROTOR BLADES, INC. FOR INSPECTION AND REP AIR. 1 G 7 2 4U H4SW 2002061000006 20020610 00006 SW 2002 6 10 HEEA079591 1 20020530 A 5310 412030009107A STRUCTURE BELL 412 412 1182202 SW FUSELAGE SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 ENGINE DECK STRUCTURE SEPARATED BEYOND REPAIR. 1 G 7 2 4U H4SW 2002061000007 20020610 00007 SW 2002 6 10 HEEA079592 1 20020530 A 5343 412030437101 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000008 20020610 00008 SW 2002 6 10 HEEA079593 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 MLG ATTACH CAP WORN. 1 G 7 2 4U H4SW 2002061000009 20020610 00009 SW 2002 6 10 HEEA079594 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000010 20020610 00010 SW 2002 6 10 HEEA079595 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000011 20020610 00011 SW 2002 6 10 HEEA079596 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000012 20020610 00012 SW 2002 6 10 HEEA079597 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 MLG ATTACH CAP HAS WORN RUBBER. REPLACED WITH SERVICEABLE CAP. 1 G 7 2 4U H4SW 2002061000013 20020610 00013 SW 2002 6 10 HEEA079598 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000014 20020610 00014 SW 2002 6 10 HEEA079599 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000015 20020610 00015 SW 2002 6 10 HEEA079600 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 MLG ATTACH CAP HAS WORN RUBBER. REPLACED WITH SERVICEABLE CAP. 1 G 7 2 4U H4SW 2002061000016 20020610 00016 SW 2002 6 10 HEEA079601 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000017 20020610 00017 SW 2002 6 10 HEEA079602 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000018 20020610 00018 SW 2002 6 10 HEEA079603 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000019 20020610 00019 SW 2002 6 10 HEEA079604 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000020 20020610 00020 SW 2002 6 10 HEEA079605 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000021 20020610 00021 SW 2002 6 10 HEEA079606 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000022 20020610 00022 SW 2002 6 10 HEEA079607 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000023 20020610 00023 SW 2002 6 10 HEEA079608 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000024 20020610 00024 SW 2002 6 10 HEEA079609 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000025 20020610 00025 SW 2002 6 10 HEEA079610 1 20020530 A 5343 412030437103 CAP BELL 412 412 1182202 SW MLG ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 MLG ATTACH CAP HAS WORN RUBBER. 1 G 7 2 4U H4SW 2002061000026 20020610 00026 SW 2002 6 10 HEEA079611 1 20020530 A 6320 CASE BELL 412 412 1182202 SW M/R GEARBOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 14007 A13 33076 RUST FOUND IN TOP OPENING OF M/R GEARBOX CASE. 1 G 7 2 4U H4SW 2002061000027 20020610 00027 SW 2002 6 10 HEEA079612 1 20020530 A 6320 412040002113 GEARBOX BELL 412 412 1182202 SW MAIN ROTOR MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 18429 33006 MAIN ROTOR GEARBOX MAKING METAL. 1 G 7 2 4U H4SW 2002061000028 20020610 00028 SW 2002 6 10 HEEA079613 1 20020530 A 6321 209040177101 ADAPTER 412040123101 BELL 412 412 1182202 SW QUILL ASSY WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N A131 33010 QUILL ASSY FLANGE ADAPTER WORN. SEND TO VENDOR FOR REPAIR. 1 G 7 2 4U H4SW 2002061000029 20020610 00029 WP 2002 6 10 0201749955 1 20020604 A 2132 WARNING SYSTEM DOUG DC9 DC931 3022065 WP COCKPIT FALSE INDICATION A NWAA G B O2 MASK DEPLOYED EMER. DESCENT N FALSE WARNING DE DESCENT 1 GL 01 922RW 47182 UPON DESCENT FROM FL290 TO FL270, THE CABIN PRESSURE LIGHT AND THE MASTER WARNING LIGHT ILLUMINATED. CREW INITIATED AN EMERGENCY DESCENT AND DONNED OXYGEN MASKS. ALL CABIN OXYGEN MASKS DEPLOYED. THE AIRCRAFT LEVELED OFF AT 10,000 FEET AN D CONTINUED TO DFW. MAINTENANCE INSPECTED ALL DUCTS IN THE TAIL COMPONENT BUT NO LEAKS WERE FOUND. ALL DOOR SEALS WERE CHECKED AND THE AIRCRAFT WAS PRESSURIZED TO 2.9 PSI. NO LEAKS WERE FOUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002061000030 20020610 00030 WP 2002 6 10 0201759955 1 20020604 A 3510 OXYGEN MASK DOUG DC9 DC931 3022065 WP F/A JUMPSEAT MALFUNCTIONED A NWAA B EMER. DESCENT O OTHER DE DESCENT 1 GL 01 922RW 47182 THE EMERGENCY OXYGEN MASK FOR THE FLIGHT ATTENDANT'S AFT JUMPSEAT DID NOT DEPLOY WHEN ALL OTHER PASSENGER MASKS DID DURI NG AN EMERGENCY DESCENT DUE TO LOSS OF CABIN PRESSURIZATION. THE MASK FINALLY DEPLOYED AFTER THE AIRCRAFT LEVELED OFF A T 10,000 FEET. MAINTENANCE REPACKED ALL MASKS AND PERFORMED A FUNCTIONAL CHECK OF THE DEPLOYMENT SYSTEM. OPERATIONAL C HECK GOOD AND ALL MASKS DEPLOYED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002061000031 20020610 00031 NM 2002 6 10 0201762296 1 20020531 A 2912 CLAMP BOEING 727 727251 138408H NM HYD SYSTEM BROKEN A NWAA K NONE K J FLUID LOSS WARNING INDICATION LD LANDING 1 GL 01 296US 21788 AFTER TOUCHDOWN ON LANDING, LOST -A- SYSTEM HYDRAULICS. AIRCRAFT WAS ABLE TO CLEAR RUNWAY BEFORE HAVING TO BE TOWED TO THE GATE DUE TO DEPLETION OF HYDRAULIC FLUID. ORD MAINTENANCE REPLACED THE BROKEN CLAMP FOUND ON MAIN RETURN FILTER. A LSO REPLACED COMPLETE FILTER MODULE. LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 2002061000032 20020610 00032 NM 2002 6 10 0201776641 1 20020601 A 3320 LIGHT BOEING 747 747212B 1384886 NM CABIN DEFECTIVE A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 641NW 21941 EN ROUTE TO AMS, SEAT 35A READING LIGHT WAS SMOKING AND SMELLED HOT. COVER AND BULB WERE REMOVED AND THE FLIGHT CONTINU ED TO AMS AND LANDED WITHOUT INCIDENT. REPLACED THE SEB. OPERATIONAL CHECK OK. 2 L 7 4 4F A20WE 2002061900189 20020619 00189 2002 6 19 0201786622 4 20020602 A 2330 9406006542 ELECTRICAL BOX BOEING 747 747251B 1384892 NM CABIN FAILED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 622US 21704 DURING CRUISE, SMOKE WAS COMING OUT OF CENTER SEAT IN ROW 37B. SHUT DOWN THE ENTERTAINMENT SYSTEM AND CONTINUED TO HNL AND LANDED WITHOUT INCIDENT. REPLACED SEAT 35ABC SEB. SEAT 37ABC CHECKED NORMAL. 2 L 7 4 4F A20WE 2002061000033 20020610 00033 SW 2002 6 10 HEEA079614 1 20020530 A 6320 412040243101 TUBE BELL 412 412 1182202 SW M/R GEARBOX CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 MAIN ROTOR GEARBOX TUBE IS CHAFED. REPLACED WITH SERVICEABLE TUBE. 1 G 7 2 4U H4SW 2002061000034 20020610 00034 NM 2002 6 10 0201806635 1 20020531 A 3397 WIRE BOEING 747 747227B 1384888 NM CABIN DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 635US 21682 DURING LINE CHECK, FOUND ZONE -A- LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRE AND REPLACED THE POWER SU PPLY BOX. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002061000035 20020610 00035 NM 2002 6 10 0201813128 1 20020529 A 2133 2079001AA OUTFLOW VALVE AIRBUS A319 A319114 3930350 NM CABIN PRESSURE FAILED A NWAA G B A O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 328NB 2773 01520 PRIOR TO FLIGHT, THE CABIN PRESSURE SYSTEM 2 WAS INOPERATIVE AND DEFERRED PER MEL 21-31-01. AT FL340, RECEIVED ECAM MES SAGE CABIN PR SYS 1 FAULT. CABIN PRESSURE BEGAN CLIMBING AT 4000-5000 FPM. BEGAN IMMEDIATE RAPID DESCENT AND SWITCHED TO MANUAL PRESSURIZATION CONTROL. CABIN HAD CLIMBED TO AN ALTITUDE OF APPROX 17,000 FEET WHEN MANUAL PRESSURIZATION CON TROL BECAME EFFECTIVE. CABIN OXYGEN MASKS DEPLOYED. DESCENDED TO 10,000 FEET AND RETURNED TO MSP AND LANDED WITHOUT IN CIDENT. REPLACED THE OUTFLOW VALVE AND NR 1 AND NR 2 PRESSURE CONTROLLERS. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002061000036 20020610 00036 SW 2002 6 10 HEEA079615 1 20020530 A 6230 SEAL BELL 412 412 1182202 SW MAST LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 6559Z A900040 36019 MAIN ROTOR MAST SEA HAS AN OIL SEEP AT SEAL. REPLACED WITH SERVICEABLE SEAL. 1 G 7 2 4U H4SW 2002061000037 20020610 00037 NE 2002 6 10 02158306 2 20020607 A 7320 31057742 SHAFT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE A VTZA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 EA 27 306UE 41020 During cruise of the flight from SWF to IAD, the crew reported that the L/H engine had flamed out. The engine oil press ure had been normal and there were no abnormal engine indications prior to the flame-out. The aircraft was diverted to ABE where it was landed without incident. Maintenance personnel found the splined shaft between the fuel control and fu el pump had sheared. The fuel control and fuel pump were removed and replaced. Operational and leak checks were satisf actory and the aircraft was returned to service. 2 L 7 2 4T 4 T RT A41NM E18NE 2002061000038 20020610 00038 2002 6 10 0201821232 4 20020523 A 2565 TUBE DOUG DC10 DC1030 3023501 WP EVAC SLIDE WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 232NW 65955 16022 46961 DURING ROUTINE FUNCTIONAL CHECK, UPPER INFLATION TUBE FAILED TO INFLATE FULLY DUE TO KINKED AND WORN HOSE. THESE WERE N OT REPLACED ON PREVIOUS OVERHAUL PER S/B 25-293 DATED 10/97. 2 L 7 3 4F A22WE 2002061000039 20020610 00039 WP 2002 6 10 0201831149 1 20020530 A 2931 INDICATOR DOUG DC10 DC1040 3023508 WP COCKPIT STICKS A NWAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 01 149US 46758 ON TAKEOFF ROLL, THE NR 1 HYDRAULIC SYSTEM QUANTITY INDICATOR DROPPED TO 2 GALLONS. FLIGHT CREW FOLLOWED COM PROCEDURE AND RETURNED TO MSP. FLIGHT LANDED WITHOUT INCIDENT. ON TAXI IN, THE NR 1 QUANTITY WENT TO 6 GALLONS. MAINTENANCE SER VICED AND LEAK CHECKED THE NR 1 SYSTEM. NO LEAKS WERE FOUND. FOUND NR 1 HYDRAULIC QUANTITY INDICATOR STICKING. REPLAC ED NR 1 QUANTITY INDICATOR. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 2002061000040 20020610 00040 WP 2002 6 10 0201849867 1 20020530 A 2751 TRANSMITTER DOUG DC9 DC951 3022051 WP T/E FLAP FAULTY A NWAA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 GL 01 776NC 47786 FLAPS SET TO 15 DEGREES FOR TAKEOFF, THE RIGHT FLAP INDICATOR SHOWED 15 DEGREES BUT THE LEFT INDICATOR SHOWED 18 DEGREES . CREW EXPERIENCED A TENDENCY TO ROLL TO THE RIGHT FROM LIFTOFF TO FLAP RETRACTION. FLIGHT CONTINUED TO DESTINATION AN D LANDED UNEVENTFULLY AT DTW. NO MENTION OF UNCOMMANDED ROLL OR FLAP POSITIONS DURING LANDING. MAINTENANCE REPLACED TH E LEFT FLAP POSITION INDICATOR TRANSMITTER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002061000042 20020610 00042 SW 2002 6 10 HEEA079616 1 20020530 A 3212 412050013109 FLOAT BELL 412 412 1182202 SW MLG DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 EMERGENCY FLOAT REINFORCEMENT PATCHES COMING UNGLUED. 1 G 7 2 4U H4SW 2002061000043 20020610 00043 SW 2002 6 10 HEEA079617 1 20020530 A 3212 412050013113 FLOAT BELL 412 412 1182202 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 EMERGENCY FLOAT LEAKS. 1 G 7 2 4U H4SW 2002061000045 20020610 00045 SW 2002 6 10 HEEA079618 1 20020530 A 3212 412050013113 FLOAT BELL 412 412 1182202 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 EMERGENCY FLOAT LEAKS. 1 G 7 2 4U H4SW 2002061000046 20020610 00046 SW 2002 6 10 HEEA079619 1 20020530 A 3212 412050013113 FLOAT BELL 412 412 1182202 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 EMERGENCY FLOAT BAG LEAKS. 1 G 7 2 4U H4SW 2002061000047 20020610 00047 SW 2002 6 10 HEEA079620 1 20020530 A 3212 412050013113 FLOAT BELL 412 412 1182202 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 EMERGENCY FLOAT BAG LEAKS. 1 G 7 2 4U H4SW 2002061000048 20020610 00048 SW 2002 6 10 HEEA079621 1 20020530 A 3212 412050013113 FLOAT BELL 412 412 1182202 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 EMERGENCY FLOAT BAG LEAKS. 1 G 7 2 4U H4SW 2002061000049 20020610 00049 SW 2002 6 10 HEEA079622 1 20020530 A 3212 412050013113 FLOAT BELL 412 412 1182202 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 EMERGENCY FLOAT BAG LEAKS. 1 G 7 2 4U H4SW 2002061000050 20020610 00050 SW 2002 6 10 HEEA079623 1 20020530 A 3212 412050013115 FLOAT BELL 412 412 1182202 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 EMERGENCY FLOAT BAG LEAKS. 1 G 7 2 4U H4SW 2002061000051 20020610 00051 SW 2002 6 10 HEEA079624 1 20020530 A 3212 412050013117 FLOAT BELL 412 412 1182202 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 EMERGENCY FLOAT BAG LEAKS. 1 G 7 2 4U H4SW 2002061000052 20020610 00052 SW 2002 6 10 HEEA079625 1 20020530 A 3212 412050013117 FLOAT BELL 412 412 1182202 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 EMERGENCY FLOAT BAG LEAKS. 1 G 7 2 4U H4SW 2002061000053 20020610 00053 SW 2002 6 10 HEEA079626 1 20020530 A 3212 412050013119 FLOAT BELL 412 412 1182202 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 EMERGENCY FLOAT BAG LEAKS. 1 G 7 2 4U H4SW 2002061000055 20020610 00055 SW 2002 6 10 HEEA079627 1 20020530 A 3246 412050015109 SKID BELL 412 412 1182202 SW MLG CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 SKID TUBE CRACKED AT FORWARD ATTACHMENT CUFF. 1 G 7 2 4U H4SW 2002061000056 20020610 00056 SW 2002 6 10 HEEA079628 1 20020530 A 3246 412050015109 SKID BELL 412 412 1182202 SW MLG MISMANUFACTURED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 INSERTS ON SKID TUBE FOR STEP ACTUATOR AND WIRE HARNESS ARE INCORRECT POSITIONS. 1 G 7 2 4U H4SW 2002061000057 20020610 00057 SW 2002 6 10 HEEA079629 1 20020530 A 3246 412050016101 SHOE BELL 412 412 1182202 SW SKID TUBE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 SKID TUBE SHOE WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000058 20020610 00058 SW 2002 6 10 HEEA079630 1 20020530 A 3246 412050016101 SHOE BELL 412 412 1182202 SW SKID TUBE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 SKID TUBE SHOE WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000059 20020610 00059 SW 2002 6 10 HEEA079631 1 20020530 A 3246 412050016101 SHOE BELL 412 412 1182202 SW SKID TUBE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 SKID TUBE SHOE WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000060 20020610 00060 SW 2002 6 10 HEEA079632 1 20020530 A 3246 412050016101 SHOE BELL 412 412 1182202 SW SKID TUBE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 SKID TUBE SHOE WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000061 20020610 00061 NM 2002 6 10 AWXA200200434 1 20020518 A 2930 TM113 SWITCH AIRBUS A319 A319132 3930340 NM HYD SYSTEM MALFUNCTIONED A AWXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 28 802AW 924 ICT - DIVERSION - FLT 0472 - DURING CRUISE EN ROUTE FROM DCA TO PHX ECAM INDICATED AN INTERMITTENT YELLOW HYDRAULIC RESE RVOIR CLASS 1 OVERHEAT MESSAGE, AIRCRAFT DIVERTED TO ICT. MAINTENANCE TROUBLESHOT PER TSM 29-13-00-810-802 AND FOUND NO OVERHEAT OR FAULTS. AIRCRAFT CONTINUED ON TO PHX WHERE MAINTENANCE FOLLOWED UP WITH TROUBLESHOOTING BY PERFORMING A YE LLOW HYDRAULIC SYSTEM INTERNAL LEAK CHECK PER AMM 29-00-00-280-003; SYSTEM BYPASS (APPROX 2 GPM) WAS WITHIN LIMITS. AS PRECAUTION THE YELLOW HYDRAULIC SYSTEM TEMPERATURE SWITCH WAS REPLACED PER AMM 29-33-11-401. 2 L 7 2 4F RT A28NM 2002061000062 20020610 00062 SW 2002 6 10 HEEA079633 1 20020530 A 3246 412050016101 SHOE BELL 412 412 1182202 SW SKID TUBE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 WELD BEADS ON SKID TUBE SHOE WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000063 20020610 00063 SW 2002 6 10 HEEA079634 1 20020530 A 3246 412050016102 SHOE BELL 412 412 1182202 SW SKID TUBE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 SKID TUBE SHOE HAS DAMAGED PUNCHER HOLE. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000064 20020610 00064 SW 2002 6 10 HEEA079635 1 20020530 A 3246 412050016102 SHOE BELL 412 412 1182202 SW SKID TUBE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 SKID TUBE SHOW WELDS WORN DOWN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000065 20020610 00065 SW 2002 6 10 HEEA079636 1 20020530 A 3246 412050016102 SHOE BELL 412 412 1182202 SW SKID TUBE BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 SKID TUBE SHOE HAS TWO BROKEN EARS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000067 20020610 00067 SW 2002 6 10 HEEA079637 1 20020530 A 3212 412050017133 COVER BELL 412 412 1182202 SW MLG WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 LOOP AND HOOK WORN ON EMERGENCY FLOAT COVER. 1 G 7 2 4U H4SW 2002061000068 20020610 00068 SW 2002 6 10 HEEA079638 1 20020530 A 3212 412050017133 COVER BELL 412 412 1182202 SW MLG WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 LOOP AND HOOK WORN ON EMERGENCY FLOAT COVER 1 G 7 2 4U H4SW 2002061000069 20020610 00069 NM 2002 6 10 AWXA200200491 1 20020602 A 2760 V3L2228 SWITCH BOEING 737 73733A 1384673 NM COCKPIT WORN A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 174AW 23633 PHX - ABORTED TAKEOFF - FLT 0511 - EN ROUTE FROM PHX TO OMA THE TAKEOFF WARNING HORN SOUNDED WHEN THROTTLES WERE ADVANC ED, REJECTED TAKEOFF. PILOT NOTED SPEED BRAKE WAS POSSIBLY NOT IN FULL DOWN POSITION. MAINTENANCE REMOVED AND REPLACED SPEED BRAKE TAKEOFF WARNING SWITCH (S651) AT TOP LT FORWARD POSITION ON CONTROL STAND IN COCKPIT IAW 31-26-26, OPERATIO NAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002061000070 20020610 00070 SW 2002 6 10 HEEA079639 1 20020530 A 3212 412050017133 COVER BELL 412 412 1182202 SW MLG TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 33073 LOOP AND HOOK TORN ON END CAP OF EMERGENCY FLOAT COVER. 1 G 7 2 4U H4SW 2002061000071 20020610 00071 SW 2002 6 10 HEEA079640 1 20020530 A 3212 412050017133 COVER BELL 412 412 1182202 SW MLG WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 EMERGENCY FLOAT COVER WORN. 1 G 7 2 4U H4SW 2002061000072 20020610 00072 NM 2002 6 10 AWXA200200492 1 20020518 A 5314 65458681 KEELBEAM BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 MCN - MAJOR REPAIR - DURING C-16 CHECK A 4 INCH CRACK WAS FOUND ON THE KEEL BEAM AT LT AIR CONDITIONING ACCESS BAY BS 53 0. MAINTENANCE CUT OUT DAMAGED SECTION OF KEEL BEAM AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICA TED ANGLE, FILLERS, AND REPLACEMENT CLIP, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5315-02151-TB3. 2 L 7 2 4F RT A16WE 2002061000073 20020610 00073 SW 2002 6 10 HEEA079641 1 20020530 A 3212 412050017133 COVER BELL 412 412 1182202 SW MLG WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 RT FWD FLOAT COVER LOOP AND HOOK WOULD NOT HOLD AND FLAP GETTING RAGGED. 1 G 7 2 4U H4SW 2002061000074 20020610 00074 NM 2002 6 10 AWXA200200495 1 20020521 A 5320 6559644501 SPLICE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT, BS 363. MX REMOVED CORRODED S TRINGER SPLICE AND CLIP FROM STRINGER 27 LT AT BS 363; FABRICATED NEW STRINGER SPLICE, AND INSTALLED NEW SPLICE AND CLIP IAW IAW B737-300 SRM 51-40-02 PG 10 & 11. 2 L 7 2 4F RT A16WE 2002061000075 20020610 00075 SW 2002 6 10 HEEA079642 1 20020530 A 3212 412050017133 COVER BELL 412 412 1182202 SW MLG TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 EMERGENCY FLOAT BAG COVER TORN. 1 G 7 2 4U H4SW 2002061000076 20020610 00076 NM 2002 6 10 AWXA200200497 1 20020515 A 5230 654692124 TEE CHORD BOEING 737 737301 1384611 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 MCN - MAJOR REPAIR - DURING C-16 CHECK .25 INCH CRACKS WERE FOUND ON THE FORWARD CARGO DOOR LOWER BEAM T-CHORD AT 3 FAST ENER HOLES IN THE VERTICAL LEG, BS 441, 442, 443. MAINTENANCE REMOVED THE LOWER BEAM T-CHORD AT BS 441-443; FABRICATED NEW REPLACEMENT T-CHORD, AND INSTALLED REPAIR IAW EO 52-31-04, PG 81-83. 2 L 7 2 4F RT A16WE 2002061000077 20020610 00077 EU 2002 6 10 AWXA200200498 1 20020603 A 3350 1013081 LIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 637AW 099 CMH - EEL - DURING INSPECTION THE L1 DOOR LOWER EMERGENCY LIGHT WAS FOUND TO BE INTERMITTENT. MAINTENANCE REMOVED AND R EPLACED THE L1 DOOR LOWER EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002061000078 20020610 00078 SW 2002 6 10 HEEA079643 1 20020530 A 3212 412050017133 COVER BELL 412 412 1182202 SW MLG TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 EMERGENCY FLOAT BAG COVER HAS TORN LOOP AND HOOK. 1 G 7 2 4U H4SW 2002061000079 20020610 00079 SW 2002 6 10 HEEA079644 1 20020530 A 3212 412050017135 COVER BELL 412 412 1182202 SW MLG TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 EMERGENCY FLOAT BAG TORN. 1 G 7 2 4U H4SW 2002061000080 20020610 00080 EU 2002 6 10 AWXA200200499 1 20020603 A 2560 P20700012015 FLASHLIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 628AW 67 LAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE LT FORWARD EMERGENCY FLASHLIGHT WAS NOT BLINKING. MAINTENANCE REPL ACED THE LT FORWARD EMERGENCY FLASHLIGHT. 2 L 7 2 4F RT A28NM 2002061000081 20020610 00081 SW 2002 6 10 HEEA079645 1 20020530 A 3212 412050017135 COVER BELL 412 412 1182202 SW MLG DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 EMERGENCY FLOAT BAG COVER LOOP AND HOOK WILL NOT STAY ON. 1 G 7 2 4U H4SW 2002061000082 20020610 00082 NM 2002 6 10 AWXA200200501 1 20020603 A 2560 P4010021 BATTERY BOEING 737 737301 1384611 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 326AW 23258 MCN - EMERGENCY EQUIPMENT - DURING C-16 CHECK MAINTENANCE FOUND THE AFT EMERGENCY FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED THE AFT FLASHLIGHT BATTERY IAW BMM 33-51-02 PG 102. 2 L 7 2 4F RT A16WE 2002061000083 20020610 00083 SW 2002 6 10 HEEA079646 1 20020530 A 3212 412050017135 COVER BELL 412 412 1182202 SW MLG DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 RT AFT FLOAT COVER LOOP AND HOOK WON'T HOLD AND KEEPS COMING OPEN IN FLIGHT. 1 G 7 2 4U H4SW 2002061000084 20020610 00084 SW 2002 6 10 HEEA079647 1 20020530 A 2820 412061619101 LINE BELL 412 412 1182202 SW FUEL SYSTEM CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 FUEL SUPPLY LINE CHAFED IN THREE PLACES. SCRAPPED. 1 G 7 2 4U H4SW 2002061000085 20020610 00085 2002 6 10 DL777020594 4 20020524 A 3140 CIRCUIT CARD BOEING 777 777232 1385232 NM COCKPIT MALFUNCTIONED A DALA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 861DA 29952 AT CRUISE FL370 CARGO HEAT AFT EICAS LIGHT ILLUMINATED. CHECKED ELEC SYNOPTIC-SHOWED NO POWER LT MAIN BUS. FUEL SYNOPT IC SHOWED LT AFT AND RT FWD FUEL PUMP SHOWS INOP. DIVERTED TO JFK. DUMPED FUEL. LT NOZZLE SHOWS INOP ON SYNOPTIC W/EI CAS AUTO JETTISON. NUMEROUS STATUS LIGHTS TO INCLUDE ELMS P110 PANEL. T/S PER FIM MSG24-18801 AND PER MCC REQUEST. SW APPED P110 POWER SUPPLY CARD S/N-1819 WITH P310 POWER SUPPLY CARD S/N 1851. PERFORMED INITIAL SELF TEST ON MAT, NO FA ULT. NO ACTIVE MSG, RAN BOTH ENGINES WITH ELECTRICAL LOADED ON. NO FAULTS. 2 L 7 2 4F RT T00001SE 2002061000086 20020610 00086 SW 2002 6 10 HEEA079648 1 20020530 A 2810 412061668101 CAP BELL 412 412 1182202 SW FUEL CELL BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 FUEL CAP RIVETS BROKEN. SCRAPPED. 1 G 7 2 4U H4SW 2002061000087 20020610 00087 NE 2002 6 10 GLBA2002073 3 20020529 A 6110 HCE4A3J PROPELLER BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3I NE RT ENGINE MALFUNCTIONED A GLBA K NONE O OTHER DE DESCENT 1 NM 03 254GL 1526 UE254 HJ1586 RIGHT PROP WOULD NOT ADJUST OR FEATHER ON GROUND. REPLACED PROPELLER ASSEMBLY. 2 L 7 2 4T RT A24CE 5 C P10NE 2002061000088 20020610 00088 SW 2002 6 10 HEEA079649 1 20020530 A 2810 412061668101 CAP BELL 412 412 1182202 SW FUEL CELL BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 FUEL CAP SCREW BROKE OFF (HARD TO OPEN) SCRAPPED. 1 G 7 2 4U H4SW 2002061000089 20020610 00089 SW 2002 6 10 HEEA079650 1 20020530 A 2510 412070820101 CUSHION BELL 412 412 1182202 SW COCKPIT SEAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 COCKPIT SEAT CUSHION TORN. REPLACED WITH SERVICEBLE CUSHION ASSY. 1 G 7 2 4U H4SW 2002061900104 20020619 00104 CE 2002 6 19 GLBA2002074 1 20020602 A 2120 5238001 BYPASS VALVE BEECH 1900 1900D 1154162 CE A/C BAY LEAKING A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 195GL 2889 UE195 LEFT ENVIRONMENTAL FAIL. REPLACED BYPASS VALVE. 2 L 7 2 4T RT A24CE 2002061000090 20020610 00090 SW 2002 6 10 HEEA079651 1 20020530 A 6710 412074101101 TRANSDUCER BELL 412 412 1182202 SW M/R CONTROL INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 YAW API HAS NO MOVEMENT WHEN AIRCRAFT RUN UP. SCRAPPED. 1 G 7 2 4U H4SW 2002061000091 20020610 00091 SW 2002 6 10 HEEA079652 1 20020530 A 6710 412074101101 TRANSDUCER BELL 412 412 1182202 SW M/R CONTROL STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 INDICATOR INTERMITTENTLY STICKING CAUSING CHANNELS TO DISAGREE. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000092 20020610 00092 SW 2002 6 10 HEEA079653 1 20020530 A 6710 412074101101 TRANSDUCER BELL 412 412 1182202 SW M/R CONTROL MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 NR 1 PITCH KICKS IN FLIGHT AND ON GROUND. SCRAPPED. 1 G 7 2 4U H4SW 2002061000093 20020610 00093 CE 2002 6 10 GLBA2002075 1 20020602 A 6120 LEVER BEECH 1900 1900D 1154162 CE COCKPIT OUT OF ADJUST A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 153GL UE153 BOTH PROPS WOULD NOT REACH 1700 RPM. ADJUSTED PROP RPM LEVER, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002080500119 20020805 00119 CE 2002 8 5 GLBA2002076 1 20020602 A 5210 1295140591 CABLE BEECH 1900 1900D 1154162 CE PAX DOOR BROKEN A GLBA K NONE O OTHER TX TAXI/GRND HDL 1 NM 03 211GL UE211 CABIN DOOR WILL NOT OPEN. REPLACED INNER DOOR CABLES, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002061000094 20020610 00094 SW 2002 6 10 HEEA079654 1 20020530 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW TORQUE STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 TORQUE INDICATOR NEEDLE STICKS. 1 G 7 2 4U H4SW 2002061000095 20020610 00095 SW 2002 6 10 HEEA079655 1 20020530 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW TORQUE MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 TORQUE INDICATOR LIGHT INOPERATIVE. 1 G 7 2 4U H4SW 2002061000096 20020610 00096 CE 2002 6 10 GLBA2002077 1 20020602 A 7720 PROBE BEECH 1900 1900D 1154162 CE RT ENGINE OUT OF ADJUST A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 253GL UE253 RIGHT ENGINE TEMP LIMITED. ADJUSTED TRIM PROBE, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2002061000097 20020610 00097 SW 2002 6 10 HEEA079656 1 20020530 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW TORQUE MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 TORQUE INDICATOR POPS THE CIRCUIT BREAKER. 1 G 7 2 4U H4SW 2002061000098 20020610 00098 SW 2002 6 10 HEEA079657 1 20020530 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW TORQUE READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 UNRELIABLE AND NOISY. READS 3 PERCENT HIGHER THAN PILOT SIDE ABOVE 80 PERCENT TORQUE. 1 G 7 2 4U H4SW 2002061000099 20020610 00099 SW 2002 6 10 HEEA079658 1 20020530 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW TORQUE STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 TORQUE INDICATOR NEEDLE IS STICKING. 1 G 7 2 4U H4SW 2002061000101 20020610 00101 SW 2002 6 10 HEEA079660 1 20020530 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 TRIPLE TACH INDICATOR GLASS FOGGED UP. 1 G 7 2 4U H4SW 2002061000102 20020610 00102 SW 2002 6 10 HEEA079661 1 20020530 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 TRIPLE TACH INDICATOR NR 2 NEEDLE INDICATES 2 PERCENT LOW. 1 G 7 2 4U H4SW 2002061000103 20020610 00103 NE 2002 6 10 GLBA2002078 3 20020603 A 6140 INDICATOR BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3A NE COCKPIT MALFUNCTIONED A GLBA O OTHER O OTHER CR CRUISE 1 NM 03 118GL UE118 NR 1 PROP INDICATOR FLUX. SWAPPED INDICATORS, OPS CHECKED SYSTEM SATISFACTORY. RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 5 C P10NE 2002061000104 20020610 00104 SW 2002 6 10 HEEA079662 1 20020530 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 TRIPLE TACH READS ERRONEOUSLY AND RATTLES INSIDE. 1 G 7 2 4U H4SW 2002061000105 20020610 00105 SW 2002 6 10 HEEA079663 1 20020530 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 TRIPLE TACH NR 1 NEEDLE STICKS. 1 G 7 2 4U H4SW 2002061000106 20020610 00106 2002 6 10 GLBA2002080 4 20020604 A 3418 1143800511 TRANSDUCER BEECH 1900 1900D 1154162 CE STALL WARNING INTERMITTENT A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 247GL 12865 UE247 STALL WARNING INTERMITTENT. REPLACED TRANSDUCER. 2 L 7 2 4T RT A24CE 2002061000107 20020610 00107 SW 2002 6 10 HEEA079664 1 20020530 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 TRIPLE TACH ALL NEEDLES INDICATE 1.5 PERCENT LOW. 1 G 7 2 4U H4SW 2002061000109 20020610 00109 SW 2002 6 10 HEEA079665 1 20020530 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 3 PERCENT INACCURACY OF TRIPLE TACH INDICATOR - NR 1 ENGINE READS HIGHER. 1 G 7 2 4U H4SW 2002061000110 20020610 00110 SW 2002 6 10 HEEA079666 1 20020530 A 7714 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 READS 1 PERCENT HIGH COMPARED TO OTHER TRIPLE TACH INDICATOR IN COCKPIT. 1 G 7 2 4U H4SW 2002061000111 20020610 00111 SW 2002 6 10 HEEA079667 1 20020530 A 7714 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 TRIPLE TACH READS 2 PERCENT HIGH. SENT TO MASCO FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 2002061000112 20020610 00112 2002 6 10 MALA020301 4 20020529 A 6122 CONNECTOR SAAB SF340 SF340A 7850100 EU PROP GOVERNOR DIRTY A MALA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 15 119XJ 340A119 LT TORQUE MOTOR LOCKOUT INOP. WOULD NOT COME OUT OF START FEATHER PROP RPM NEVER OVER 800 AND WOULD NOT GO INTO BOTTOM GOVERNOR. MAINTENANCE CLEANED CANNON PLUG ON OVERSPEED GOVERNOR. PERFORMED SEVERAL STARTS ON LT MOTOR. OPS CHECK GOOD . 2 L 7 2 4T RT A52EU 2002061000113 20020610 00113 SW 2002 6 10 HEEA079668 1 20020530 A 7714 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 TRIPLE TACH LIGHT INOPERATIVE. 1 G 7 2 4U H4SW 2002061000114 20020610 00114 SW 2002 6 10 HEEA079669 1 20020530 A 7714 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 TRIPLE TACH READS 3 PERCENT LOW. 1 G 7 2 4U H4SW 2002061000115 20020610 00115 EU 2002 6 10 MALA020308 1 20020528 A 2612 SENSOR SAAB SF340 340B 7860101 EU LT & RT ENGINE MALFUNCTIONED A MALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 445XJ 340B445 DURING TAKEOFF OF FLIGHT 3087, LT & RT TAILPIPE HOT LIGHTS ILLUMINATED. LT TAILPIPE HOT LIGHT CAME ON AT TAKEOFF AT ABO UT 40 KTS, ABORTED TAKEOFF AND THE RIGHT TAILPIPE HOT LIGHT CAME ON TAXIING OFF THE RUNWAY. MAINTENANCE CLEANED AND DRI ED SENSORS ON BOTH ENGINES. RAN ENGINES, CHECKED OK. 2 L 7 2 4T RT A52EU 2002061000116 20020610 00116 SW 2002 6 10 HEEA079670 1 20020530 A 7714 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 TRIPLE TACH NR 2 NEEDLE HAS NO INDICATION. 1 G 7 2 4U H4SW 2002061000117 20020610 00117 SW 2002 6 10 HEEA079671 1 20020530 A 7714 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 TRIPLE TACH NR 1 NEEDLE READS 3 PERCENT HIGH AT ALL TIMES. 1 G 7 2 4U H4SW 2002061000118 20020610 00118 SW 2002 6 10 HEEA079672 1 20020530 A 2422 412075101103 INVERTER BELL 412 412 1182202 SW AC SYSTEM FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 AFCS DROPS OFF LINE COMPLETELY WHEN INVERTER IS TURNED OFF. 1 G 7 2 4U H4SW 2002061000119 20020610 00119 SW 2002 6 10 HEEA079673 1 20020530 A 2422 412075101103 INVERTER BELL 412 412 1182202 SW AC SYSTEM INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 AC INVERTER INOPERATIVE. 1 G 7 2 4U H4SW 2002061000120 20020610 00120 EU 2002 6 10 MALA020309 1 20020531 A 2910 GPP125012 SWITCH SAAB SF340 SF340A 7850100 EU HYD SYSTEM FAILED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 46XJ 340A046 DURING FLIGHT 2824, HYDRAULIC SYSTEM WARNING INBOUND TO MSP. CREW PERFORMED EMERGENCY GEAR EXTENSION AND USED HYDRAULIC PUMP IN OVERRIDE TO GET RT MLG DOWN AND LOCKED. FROM LOG PAGE 1078212, HYDRAULIC CAUTION LIGHT ON INFLIGHT, PUMP INOP IN AUTO. EMERGENCY GEAR HANDLE PULLED. ON POST FLIGHT NOTED RIGHT MAIN GEAR DOORS DID NOT RELEASE. MAINTENANCE REMOVE D AND REPLACED HYDRAULIC SWITCH 9ML IAW 29-10-45-4 AND REPLACED LT SEP BOLT, FOUND RT SEP BOLT FAULTY, REPLACED. OPS CH ECK GOOD. 2 L 7 2 4T RT A52EU 2002061000121 20020610 00121 EU 2002 6 10 MALA020310 1 20020531 A 2120 MOTOR SAAB SF340 340B 7860101 EU CABIN SEIZED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 425XJ 340B425 DURING FLIGHT 2788, WHILE SITTING AT THE GATE WITH PAX LOADED, THERE WAS SMOKE COMING FROM THE CABIN. PASSENGERS UNLOAD ED. MAINTENANCE TROUBLESHOT A/C SYSTEM, FOUND SUPPLEMENTAL AIR MOTOR SEIZED UP. CLEARED SMOKE SMELL FROM CABIN, DEFERR ED SUPPLEMENTAL AIR SYSTEM. 2 L 7 2 4T RT A52EU 2002061000122 20020610 00122 2002 6 10 HEEA079674 4 20020530 A 3100 412075506101 CONTROL PANEL BELL 412 412 1182202 SW COCKPIT INOPERATIVE E HEEA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 03 1202T 33112 FORCE TRIM CONTROL PANEL WOULD NOT LIGHT FORCE TRIM CAUTION SEGMENT. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000123 20020610 00123 2002 6 10 HEEA079675 4 20020530 A 3100 412075513103A CONTROL PANEL BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2149S 36002 INTERCONNECT VALVE DOESN'T TEST CORRECTLY IN BUS 2. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000124 20020610 00124 2002 6 10 MALA020311 4 20020531 A 3425 INDICATOR BAC 146 AVRO146RJ85A 1500097 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 516XJ E2334 DURING FLIGHT 3677, CREW REPORTED THE LT AND RT EFIS TUBES BLANK. AIR RETURN TO CLT. NO OTHER INFORMATION AT THIS TIME . 2 H 7 4 4F RT A49EU 2002061000125 20020610 00125 SW 2002 6 10 HEEA079676 1 20020530 A 6710 BEARING BELL 412 412 1182202 SW UNIVERSAL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 8T7 36002 MAIN ROTOR UNIVERSAL HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000126 20020610 00126 EU 2002 6 10 MALA020312 1 20020531 A 3620 303200 SEAL BAC 146 AVRO146RJ85A 1500097 EU PNEUMATIC SYS LEAKING A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 520XJ E2345 DURING FLIGHT 3487, A/C HAD LEFT ZONE HIGH TEMP IN (SYSTEM BLEED LEAK). A/C NEEDED ICING CAPABILITY TO LAND IN STL. DI SPATCH RETURNED A/C TO MSP. AIR TURNBACK. MAINTENANCE FOUND DOLLS-EYE INDICATOR TRIPPED FOR NR 1 PYLON. REPLACED SEAL S P/N 303200 FOR TEMP SENSOR AND DUCT SLEEVE. LEAK CHECK GOOD DURING GROUND RUN. 2 H 7 4 4F RT A49EU 2002061000127 20020610 00127 SW 2002 6 10 HEEA079677 1 20020530 A 6710 BEARING BELL 412 412 1182202 SW UNIVERSAL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K SW627 36001 MAIN ROTOR UNIVERSAL HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000128 20020610 00128 EU 2002 6 10 MALA020313 1 20020531 A 3231 DOOR BAC 146 AVRO146RJ85A 1500097 EU RT MLG OUT OF ADJUST A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 530XJ E2364 DURING FLIGHT 3430, A/C DEPARTED MSP AND RT MLG INDICATED UNSAFE GEAR. CREW DECLARED AN EMERGENCY AND RETURNED TO MSP W ITHOUT FURTHER INCIDENTS. AIR TURNBACK TO MSP. MAINTENANCE ADJUSTED RT MAIN GEAR DOOR IAW 32-10-21, DID MULTIPLE GEAR SWINGS, OPS CHECKS AND RIG CHECKS GOOD. 2 H 7 4 4F RT A49EU 2002061000129 20020610 00129 SW 2002 6 10 HEEA079678 1 20020530 A 6710 BEARING BELL 412 412 1182202 SW UNIVERAL ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K BT771 36001 MAIN ROTOR UNIVERAL HAS A ROUGH BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000130 20020610 00130 EU 2002 6 10 MALA020314 1 20020602 A 3297 WIRE SAAB SF340 SF340A 7850100 EU LT MLG BROKEN A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 31XJ 340A031 DURING CONTINUITY CHECK OF SEPARATION BOLTS CIRCUITY, FOUND CANNON PLUG AT THE LT SEPARATION BOLT BAD AND WIRE BROKE. M AINTENANCE REMOVED AND REPLACED CANNON PLUG AT THE LT SEPARATION BOLT IAW SAAB WM20-30-00, REPAIRED BROKEN WIRE IAW SAAB WM20-20-01. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002061000131 20020610 00131 SW 2002 6 10 HEEA079679 1 20020530 A 6710 BEARING BELL 412 412 1182202 SW UNIVERAL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T BR779 33112 MAIN ROTOR UNIVERAL HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000132 20020610 00132 SW 2002 6 10 HEEA079680 1 20020530 A 6710 BEARING BELL 412 412 1182202 SW UNIVERSAL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N SW1050 33010 MAIN ROTOR UNIVERSAL HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000133 20020610 00133 SW 2002 6 10 HEEA079681 1 20020530 A 6710 BEARING BELL 412 412 1182202 SW UNIVERSAL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z BT2354 36019 MAIN ROTOR UNIVERSAL HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000134 20020610 00134 EU 2002 6 10 MALA020315 1 20020602 A 2120 COMPRESSOR SAAB SF340 340B 7860101 EU CABIN SEIZED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 454XJ 340B454 WHILE SHUTDOWN ON FLIGHT 2949/3059, F/A NOTED SMOKE IN VICINITY OF ROW 3 UPON SHUTDOWN WHILE SUPPLEMENTAL A/C WAS OPERAT ING. MAINTENANCE TROUBLESHOOTING REVEALED SEIZED SUPPLEMENTAL A/C COMPRESSOR. NO OTHER INFORMATION AVAILABLE AT THIS T IME. 2 L 7 2 4T RT A52EU 2002061000135 20020610 00135 SW 2002 6 10 HEEA079682 1 20020530 A 6710 BEARING BELL 412 412 1182202 SW UNIVERSAL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N BT3750 33002 MAIN ROTOR UNIVERSAL HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000136 20020610 00136 EU 2002 6 10 MALA020316 1 20020521 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 442XJ 340B442 DURING 4K-CHECK IN CWA, MAINTENANCE FOUND FWD PART OF CENTER AISLE SEAT TRACK BL 0 CORRODED. MAINTENANCE COMPLETED REPA IR FROM STA 297 TO STA 379 IAW EO 53060. 2 L 7 2 4T RT A52EU 2002061000137 20020610 00137 EU 2002 6 10 MALA020317 1 20020522 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 442XJ 340B442 DURING 4K-CHECK IN CWA, LT CENTER AISLE SEAT TRACK LBL 18.3 HAS HEAVY CORROSION ON FWD SECTION. MAINTENANCE REPAIRED SE AT TRACK IAW EO S53060 FROM STA 297 TO 329. 2 L 7 2 4T RT A52EU 2002061000138 20020610 00138 SW 2002 6 10 HEEA079683 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 MAIN ROTOR ROD END BEARING WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000139 20020610 00139 EU 2002 6 10 MALA020318 1 20020522 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 442XJ 340B442 DURING 4K-CHECK IN CWA, MAINTENANCE FOUND UPPER FLANGE OF BOTTOM FRAME AT STA 258 HAS CORROSION. MAINTENANCE COMPLETED REPAIR IAW EO S53102. 2 L 7 2 4T RT A52EU 2002061000140 20020610 00140 EU 2002 6 10 MALA020319 1 20020605 A 3350 2LA00511520 HOUSING SAAB SF340 340B 7860101 EU CABIN CRACKED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 424XJ 340B424 DURING OPS CHECK OF EMERGENCY LIGHT SYSTEM, MAINTENANCE NOTED MOST FWD PSU EMERGENCY LIGHTS INOP. MAINTENANCE FOUND BUL B HOUSING CRACKED. REMOVED AND REPLACED MOST FWD EMERGENCY COVE LIGHT ASSY. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002061000141 20020610 00141 SW 2002 6 10 HEEA079684 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000142 20020610 00142 EU 2002 6 10 MALA020320 1 20020605 A 3350 MS274061 SWITCH SAAB SF340 340B 7860101 EU COCKPIT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING LC1 MAINTENANCE NOTED F/A EMERGENCY LIGHT SWITCH ARM LIGHT WILL NOT LIGHT. MAINTENANCE REMOVED AND REPLACED COCK PIT ARM SWITCH. 2 L 7 2 4T RT A52EU 2002061000143 20020610 00143 SW 2002 6 10 HEEA079685 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000144 20020610 00144 EU 2002 6 10 MALA020321 1 20020512 A 5320 7253721447 CHANNEL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K-CHECK IN CWA, T-CHANNEL AT LBL 11.0 BETWEEN 225 & 226 HAS CORROSION. MAINTENANCE REMOVED OLD CORRODED PIECES AND INSTALLED NEW ANGLE AND NEW BEAM. 2 L 7 2 4T RT A52EU 2002061000145 20020610 00145 SW 2002 6 10 HEEA079686 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000146 20020610 00146 SW 2002 6 10 HEEA079687 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000147 20020610 00147 EU 2002 6 10 MALA020323 1 20020514 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K-CHECK IN CWA, O/B OF RBL 18 AT STA 272 FRAME ANGLE HAS CORROSION. MAINTENANCE REMOVED CORROSION, FABRICATED A NGLE DOUBLER AND REQUIRED SHIMS FROM MATERIAL LOT 309801, AND INSTALLED ON STA 272 FRAME TOP AS REQUIRED IAW SRM CHAPTER S 51-70-40, AND 51-70-30. 2 L 7 2 4T RT A52EU 2002061000148 20020610 00148 SW 2002 6 10 HEEA079688 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000149 20020610 00149 WP 2002 6 10 MWEA020373 1 20020521 A 5321 99365841 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FLOORBOARD BETWEEN TRACKS 1 AND 2 JUST AFT OF LEFT FORWARD COAT CLOSET. FABRICATED AND INSTALLED REPAIR DOUBLER AND COR E PLUG. 2 L 7 2 4F A6WE 2002061000150 20020610 00150 SW 2002 6 10 HEEA079689 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000151 20020610 00151 SW 2002 6 10 HEEA079690 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000152 20020610 00152 WP 2002 6 10 MWEA020375 1 20020521 A 5320 59148657 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CENTER WING FORWARD LOWER BULKHEAD FITTING CRACKED AT STATION 606 AND LONGERON 24 LEFT. REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 2002061000153 20020610 00153 SW 2002 6 10 HEEA079691 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000154 20020610 00154 SW 2002 6 10 HEEA079692 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000155 20020610 00155 WP 2002 6 10 MWEA020376 1 20020524 A 5220 5910537510 PAN DOUG DC9 DC982 3022082 WP EMERGENCY EXIT GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 RIGHT AFT OVERWING EMERGENCY EXIT DOOR JAMB PAN HAS GOUGE MARK. LOCATED TOP CENTER. BLENDED AREA, INSTALLED PAN REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002061000156 20020610 00156 WP 2002 6 10 MWEA020379 1 20020524 A 5347 593056675 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 NR 2 SEAT TRACK, HEAVY CORROSION, STATION 1271. FABRICATED AND INSTALLED SEAT TRACK SECTION AND SPLICE. 2 L 7 2 4F A6WE 2002061000157 20020610 00157 SW 2002 6 10 HEEA079693 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000158 20020610 00158 SW 2002 6 10 HEEA079694 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000159 20020610 00159 WP 2002 6 10 MWEA020380 1 20020524 A 5312 59148653 PRESSURE PANEL DOUG DC9 DC932 3022066 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CENTER WING FORWARD LOWER BULKHEAD WEB HAS 1 VERY DEEP GOUGE ON FORWARD SURFACE AT STATION 606 & LONGERON 25 LEFT. FABR ICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002061000160 20020610 00160 SW 2002 6 10 HEEA079695 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000161 20020610 00161 SW 2002 6 10 HEEA079696 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000162 20020610 00162 WP 2002 6 10 MWEA020381 1 20020524 A 5542 5910256501 SKIN DOUG DC9 DC932 3022066 WP RUDDER DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 LEFT SIDE OF RUDDER 5 INCHES AFT OF FORWARD SPAR BETWEEN ZR 117 AND ZR 113 HAS CREASE 2.5 INCHES LONG. FABRICATED AND I NSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002061000163 20020610 00163 WP 2002 6 10 MWEA020383 1 20020524 A 5610 575468828 RETAINER DOUG DC9 DC932 3022066 WP COCKPIT WINDOW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 RIGHT WINDOW RETAINER HAS A CRACK INDICATION IN THE TITANIUM DOUBLER. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002061000164 20020610 00164 SW 2002 6 10 HEEA079697 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000165 20020610 00165 SW 2002 6 10 HEEA079698 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000166 20020610 00166 SW 2002 6 10 HEEA079699 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000167 20020610 00167 WP 2002 6 10 MWEA020385 1 20020601 A 3260 801801 PROXIMITY SENSOR DOUG DC9 DC932 3022066 WP RT MLG FAULTY A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 205ME 47601 THE AMBER GEAR DOOR OPEN LIGHT CAME ON AND STAYED ON EVEN WITH ALL HYDRAULIC PUMPS ON. ON START OF DESCENT THE LIGHT WE NT OUT. WHEN SELECTING GEAR DOWN FOR LANDING ALL LIGHTS WORKED NORMAL. REMOVED AND REPLACED RIGHT GEAR DOOR PROXIMITY SENSOR AND PERFORMED MTC CHECK REF MM 32-60-3. 2 L 7 2 4F A6WE 2002061000168 20020610 00168 SW 2002 6 10 HEEA079700 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000169 20020610 00169 SW 2002 6 10 HEEA079701 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000170 20020610 00170 NE 2002 6 10 NACA20020019 2 20020515 A 8530 356993 CYLINDER DOUG DC6 DC6B 3021712 WP PWA R2800 R2800* 52026 NE NR 3 ENGINE DAMAGED A NACA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 AL 03 7919C 1647 1647 43554 P36225 NR 3 ENGINE PRECAUTIONARY SHUTDOWN, DUE TO LOW COMPRESSION PATTERN ON ANALYZER, NR 12 CYLINDER. REMOVED AND REPLACED NR 12 CYLINDER ON THE NR 3 ENGINE. 2 L 7 4 4R 4 R 6A4 5E8 2002061000171 20020610 00171 NE 2002 6 10 NACA20020020 2 20020517 A 8530 356993 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 3 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 779TA 819 819 45529 36210 PRECAUTIONARY SHUT DOWN NR 3 ENGINE IN CRUISE DUE TO BACKFIRING AT ALL POWER SETTINGS. REMOVED AND REPLACED THE NR 16 C YLINDER ON THE NR 3 ENGINE. 2 L 7 4 4R 4 R A781 5E8 2002061000172 20020610 00172 SW 2002 6 10 HEEA079702 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000173 20020610 00173 SW 2002 6 10 HEEA079703 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000174 20020610 00174 WP 2002 6 10 NACA20020022 1 20020508 A 5330 SKIN DOUG DC6 DC6 3021702 WP FUSELAGE CORRODED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 779TA 45529 FORWARD FUSELAGE, COPILOTS SLIDING WINDOW FRAME DOUBLER SURFACE CORROSION AND LIFTING AFT LOWER CORNER, AND TOP AFT CORN ER. REMOVED COPILOTS FACTORY WINDOW DOUBLER, REMOVED THREE DAMAGED SECTIONS OF SKIN. FABRICATED TWO DOUBLERS AND SHIMS . INSTALLED SHIMS, DOUBLERS AND WINDOW DOUBLER. 2 L 7 4 4R A781 2002061000175 20020610 00175 SW 2002 6 10 HEEA079704 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000176 20020610 00176 SW 2002 6 10 HEEA079705 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000177 20020610 00177 WP 2002 6 10 NACA20020023 1 20020514 A 5713 STRINGER DOUG DC6 DC6 3021702 WP RT WING CRACKED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 2907F 533265 RT LOWER WING, STRINGER 23 CRACKED AT AT STA 325, JUST FORWARD OF ACCESS PANEL (UNDER DOVETAIL). FABBED AND INSTALLED R EPAIR DOUBLER PER DRAWING NAC2002-05. 2 L 7 4 4R A781 2002061000178 20020610 00178 SW 2002 6 10 HEEA079706 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000179 20020610 00179 WP 2002 6 10 NACA20020024 1 20020522 A 5730 FILLER DOUG DC6 DC6 3021702 WP LT WING CHIPPED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 2907F 533265 LT WING L/E FILLER REPAIR CHIPPING OUT, TOP STA 240. FABRICATED AND INSTALLED SCARF PATCH PER DOUGLAS OHM FIG 13-34. 2 L 7 4 4R A781 2002061000180 20020610 00180 SW 2002 6 10 HEEA079707 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000181 20020610 00181 NE 2002 6 10 NACA20020025 2 20020531 A 8530 33641 HOUSING DOUG DC6 C118A 3021710 WP PWA R2800 R2800* 52026 NE NR 4 ENGINE LEAKING A NACA E A ENGINE SHUTDOWN UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 1377K 603 603 44596 P34403 FEATHERED THE NR 4 ENGINE DUE TO BACKFIRING AND OIL LOSS. REPLACED THE NR 3 CYLINDER PUSHROD HOUSING. 2 L 7 4 4R 4 R 6A3 5E8 2002061000182 20020610 00182 SW 2002 6 10 HEEA079708 1 20020530 A 6710 412310400101 BEARING BELL 412 412 1182202 SW M/R ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 MAIN ROTOR ROD END HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000183 20020610 00183 SW 2002 6 10 HEEA079709 1 20020530 A 2810 412361641101 FUEL CELL BELL 412 412 1182202 SW FUSELAGE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2261D 33076 FUEL CELL LEAKING. 1 G 7 2 4U H4SW 2002061000184 20020610 00184 NE 2002 6 10 NACA20020027 2 20020605 A 8500 R2800 ENGINE DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE NR 3 MALFUNCTIONED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 99330 499 499 43576 P33821 NR 3 ENGINE FEATHERED DUE TO BACKFIRING, AND DOUBLE SHORTED SECONDARY, NR 16 CYLINDER. BORESCOPED CYLINDER, NO DAMAGE R EVEALED. COMPRESSION TESTED CYLINDER, 80/72. BARO POWER OPS CHECK GOOD, MAG DROP 4 + 4, NO SIGNIFICANT RPM SPLIT. 2 L 7 4 4R 4 R 6A3 5E8 2002061000185 20020610 00185 SW 2002 6 10 HEEA079710 1 20020530 A 2841 412375001105 INDICATOR BELL 412 412 1182202 SW FUEL QTY READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 RIGHT SIDE FUEL QUANTITY READS LOW. 1 G 7 2 4U H4SW 2002061000186 20020610 00186 WP 2002 6 10 P2EA2002M037 1 20020528 A 7603 THROTTLE CABLE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE BINDING A P2EA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 05 130NJ 49222 717399 RIGHT THROTTLE (NR 2 ENGINE) MECHANICAL BINDING. ONLY APPROX 1/2 THROTTLE MOVEMENT. REMOVED AND REPLACED THE RIGHT ENG INE THROTTLE CABLE PER MM 76-11-01, OPS CHECK GOOD. 2 L 7 2 4F 4 F A6WE E9NE 2002061000187 20020610 00187 SW 2002 6 10 HEEA079711 1 20020530 A 7332 41800014 TRANSMITTER BELL 412 412 1182202 SW FUEL PRESSURE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 142PH 33150 FUEL PRESSURE WILL NOT DROP TO ZERO WITH BOOST PUMP OFF. SCRAPPED FUEL PRESSURE TRANSMITTER. 1 G 7 2 4U H4SW 2002061000188 20020610 00188 WP 2002 6 10 P2EA2002M039 1 20020529 A 1430 BOLT DOUG DC9 DC982 3022082 WP PNEUMATIC SYS MISSING A P2EA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 05 130NJ 49222 RIGHT ENGINE CROSSFEED VALVE HANDLE ON QUADRANT STUCK IN OPEN POSITION. FOUND BOLT AND HARDWARE MISSING ON RIGHT CROSSF EED VALVE TORQUE TUBE ATTACHMENT. REPLACED HARDWARE, OP'S CHECKED GOOD PER MM 36-10-03. 2 L 7 2 4F A6WE 2002061000189 20020610 00189 SW 2002 6 10 HEEA079712 1 20020530 A 7931 41800084 TRANSMITTER BELL 412 412 1182202 SW ENGINE OIL READS LOW E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 142PH 33150 ENGINE OIL INDICATOR READING 5 PERCENT LOW. SCRAPPED ENGINE OIL TRANSMITTER. 1 G 7 2 4U H4SW 2002061000190 20020610 00190 2002 6 10 HEEA079713 4 20020530 A 2210 420936903 TARSYN BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2149S 36002 TARSYN PITCH AND ROLL AXIS UNRELIABLE. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061000191 20020610 00191 SW 2002 6 10 HEEA079714 1 20020530 A 7910 4369 CAP BELL 206 206L3 1182108 SW OIL TANK LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 4835 51131 ENGINE OIL CAP LEAKS THROUGH CENTER. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002061000192 20020610 00192 2002 6 10 HEEA079715 4 20020530 A 3453 4530103 RECEIVER BELL 206 206L3 1182108 SW LORAN SYS INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 205FC 51130 LORAN SYSTEM LOSES POWER INTERMITTENTLY. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002061000193 20020610 00193 SW 2002 6 10 HEEA079716 1 20020530 A 2430 A1077 RELAY BELL 206 206L3 1182108 SW BATTERY INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6748D 51106 RELAY INTERMITTENTLY WHEN STARTER SWITCH ACTUATED NOTHING WOULD HAPPEN. 1 G 7 1 3U H2SW 2002061000194 20020610 00194 SW 2002 6 10 HEEA079717 1 20020530 A 2430 A1077V RELAY BELL 206 206L4 1182110 SW BATTERY INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7074W 52033 RELAY CONTACTOR INTERMITTENTLY STICKS OPEN. 1 G 7 1 3U NC H2SW 2002061000195 20020610 00195 2002 6 10 HEEA079718 4 20020530 A 3416 A30 ENCODER BELL 206 206L3 1182108 SW ALTIMETER INACCURATE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 21497 51518 ENCODER CAUSES ALTITUDE TO INDICATE 200 FEET OFF. REPAIRED. 1 G 7 1 3U H2SW 2002061100040 20020611 00040 NM 2002 6 11 02157413 1 20020606 A 2460 CONTROL UNIT DORNER DO32 DO328300 NM COCKPIT FAILED A VTZA K NONE O OTHER DE DESCENT 1 EA 27 413FJ 3168 DURING DESCENT OF THE FLIGHT FROM DAY TO CVG, THE CREW REPORTED THAT THE NR 1, 2 AND 3 FLIGHT DISPLAYS FAILED INTERMITTE NTLY. THE AIRCRAFT WAS LANDED AT CVG WITHOUT INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE DC GENERATOR CON TROL UNIT (1VE PANEL). AN OPERATIONAL CHECK AND A MAINTENANCE ACCEPTANCE FLIGHT WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002061000196 20020610 00196 2002 6 10 HEEA079719 4 20020530 A 3416 A30 ENCODER BELL 206 206L3 1182108 SW ALTIMETER MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 21497 51518 ENCODER WON'T INDICATE WITHIN SPECIFIED RANGE. REPAIRED. 1 G 7 1 3U H2SW 2002061000199 20020610 00199 2002 6 10 HEEA079720 4 20020530 A 2340 A3016R MIXER BOX BELL 412 412 1182202 SW COCKPIT INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1202T 33112 NR 1 CAM AUDIO SWITCH IS INTERMITTENT. CLEANED COM 1 AUDIO SWITCH AND REPLACED LIGHT PANEL. REPAIRED. BENCH CHECK GOOD . 1 G 7 2 4U H4SW 2002061000200 20020610 00200 2002 6 10 HEEA079721 4 20020530 A 2340 A3016R MIXER BOX BELL 412 412 1182202 SW COCKPIT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 VOLUME CONTROL HAS A DEAD SPOT. FOUND R72 BAD. REPLACED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000201 20020610 00201 2002 6 10 HEEA079722 4 20020530 A 2340 A3016R MIXER BOX BELL 412 412 1182202 SW COCKPIT INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 FM BLEEDS OVER REGARDLESS OF POSITION OF TOGGLE SWITCH. FOUND S1 SELECTOR INTERMITTENT, CLEANED S1 SWITCH, REPAIRED. BE NCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000202 20020610 00202 2002 6 10 HEEA079723 4 20020530 A 2340 A3016W INTERPHONE BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 NUMBER 2 COMM SWITCH BROKEN. FOUND SWITCHES S1, S3, LIGHT PANEL, VOLUME AND TRANSMIT KNOBS BAD. REPLACED. REPAIRED. B ENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000203 20020610 00203 NM 2002 6 10 02FDEA00382 1 20020605 A 3260 106071719 MODULE BOEING 727 727100 1384036 NM COCKPIT SHORTED A FDEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 187FE 19079 ON TAKEOFF, AFTER RAISING THE GEAR HANDLE THE PRESS TO TEST & LIGHTS C/B (P6-3, LANDING GEAR) POPPED. 1ST & 2ND VERTI ROWS ON THE DOOR LIGHT PANEL LIGHT UP. ON RECOVERY, NONE OF THE GEAR LIGHTS WOULD LIGHT. M/GEAR EXT ACCOMP. F/O NOTIC ED A SPARK BEHIND 3 GRN LIGHTS WHEN HANDLE UP. DOOR PNL LIGHTS W/N PRESS TO TEST. T/S SYS PER WDM 33-18-01. USING F/O STATEMENT OF OBSERVING SPARK, PULLED M/G WARN MOD FROM PANEL, SET C/B, WITH PANEL REMOVED C/B DID NOT POP. DOOR LIGHT PNL DOES PRESS TO TEST. FOUND BULB CONTACT FOR N/G GRN LIGHT HAD COME IN CONTACT WITH BASE GROUND SHORTING OUT THE CIRC UIT. REMOVED AND REPLACED L/G WARNING MODULE PER 32-61-001-4. OPS CK'D PER 32-61-021-5 AND 32-62-011-5. 2 L 7 3 4F RT A3WE 2002061000204 20020610 00204 2002 6 10 HEEA079724 4 20020530 A 2340 A3016W INTERPHONE BELL 412 412 1182202 SW COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 800Y 33134 HOT MIC IN PA. REPLACED BAD C30 CAPACITOR. REPAIRED PROBLEM BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000205 20020610 00205 2002 6 10 HEEA079725 4 20020530 A 2340 A3016W INTERPHONE BELL 412 412 1182202 SW COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2298Z 33077 LIGHT PANEL IS INOPERATIVE. REPLACED LIGHT PANEL. ALSO REPLACED BAD S2, S3, S4, S5, S6, S7, S8, S9 AND S11. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000206 20020610 00206 2002 6 10 HEEA079726 4 20020530 A 2340 A3016W INTERPHONE BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22347 36005 COMM 1 AND COMM 2 AUDIO SELECT KNOB WON'T MUTE AUDIO. FOUND SWITCHES S1, S2, S3, S4, S9, S10, S11, LIGHT PANEL, VOLUME A ND TRANSMIT KNOBS BAD. REPLACED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000207 20020610 00207 2002 6 10 HEEA079727 4 20020530 A 2340 A3016W INTERPHONE BELL 214 214ST 1182106 SW COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8045T 28101 FACEPLATE WORN. FOUND SWITCHES S1, S4, S7, S8, S9, S10, S11, TRANSMIT KNOB, RESISTOR R36 AND LIGHT PANEL BAD. REPLACED. REPAIRED. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 2002061000208 20020610 00208 WP 2002 6 10 02FDEA00383 1 20020606 A 2932 VT0107F TRANSMITTER DOUG DC10 DC1030 3023501 WP HYD SYSTEM LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 314FE 5325 5325 48312 AFTER 2+15 OF FLT HYD SYS 3 ELEV OFF LIGHT ILLUMINATED. PERFORMED RED TABS, WITH FLUID DOWN TO 4.5 GALS. WHEN ENG 3 HY D PUMPS TURNED BACK ON, STARTED TO SLOWLY DECREASE TO 3.5 GALS. ENG HYD PUMPS TURNED OFF WITH QTY HOLDING AT 3.5 GALS. ON LANDING APPROX, NR 3 HYD WENT TO 0.5 GALS/NEARLY ZERO. REMOVED AND REPLACED NR 3 HYD PRESSURE TRANSMITTER, FOUND LE AKING FROM SEAL. OPS CHECK GOOD AS PER MM CHAPTER 29-31-03-2. SERVICED HYD SYSTEM TO NORMAL READING AS PER MM CHAPTER 12-13-01-3. RAN ENGINES AS PER JRH CHAPTER 5 A AND PERFORMED HYD PUMP OPERATIONAL TEST AS PER JRH CHAPTER 9-1. ALL IND ICATIONS NORMAL, A/C OK FOR SERVICE. 2 L 7 3 4F A22WE 2002061000209 20020610 00209 2002 6 10 HEEA079728 4 20020530 A 2340 A3016W INTERPHONE BELL 412 412 1182202 SW COCKPIT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 SELECTOR SWITCH IS STICKING. FOUND SWITCH S1, VOLUME AND TRANSMIT KNOBS AND LIGHT PANEL BAD. REPLACED. REPAIRED. BENC H CHECK GOOD. 1 G 7 2 4U H4SW 2002061000210 20020610 00210 2002 6 10 HEEA079729 4 20020530 A 2340 A3016W INTERPHONE BELL 412 412 1182202 SW COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893P 33012 VHF NR 1 POSITION FUNCTIONS INTERMITTENTY. FOUND SWITCH S1, VOLUME AND TRANSMIT KNOBS BAD. REPLACED. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000211 20020610 00211 NM 2002 6 10 AWXA200200503 1 20020607 A 3350 1012623 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 326AW 23258 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT ON SEAT ROW 9 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ON SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002061000212 20020610 00212 2002 6 10 HEEA079730 4 20020530 A 2340 A3016W INTERPHONE BELL 412 412 1182202 SW COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 FM NR 1 AUDIO BLEEDS OVER. FOUND R72 VOLUME POT BAD, S1 SELECTOR SWITCH BAD, AR2 HEADSET AMP BAD. REPLACED AND REPAIRED . BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000213 20020610 00213 SO 2002 6 10 C2XA02CL125 1 20020605 A 3350 66903 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 13964 145123 CLE FLIGHT 3175, THE CREW REPORTED THE FORWARD AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE E MERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002061000214 20020610 00214 2002 6 10 HEEA079731 4 20020530 A 2340 A3016W INTERPHONE BELL 412 412 1182202 SW COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2261D 33076 SCRATCHY VOLUME CONTROL. VOLUME CONTROL DOES NOT TURN FREELY AND VOLUME AND TRANSMIT KNOB BAD. REPLACED. REPAIRED. BE NCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000215 20020610 00215 2002 6 10 HEEA079732 4 20020530 A 2340 A3016W INTERPHONE BELL 412 412 1182202 SW COCKPIT INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 NOT TRANSMITTING. BROKEN WIRE ON SWITCH S1, IR, 9. RESOLDERED BROKEN WIRE. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000216 20020610 00216 2002 6 10 HEEA079733 4 20020530 A 2340 A3016W INTERPHONE BELL 412 412 1182202 SW COCKPIT INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893P 33012 WORKS INTERMITTENTLY. FOUND AR2 AMP BOARD, AND WIRES ON AR2 AMP BOARD HAVE BROKEN INSULATION. REPLACED AR2 AMP BOARD AN D WIRES. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000217 20020610 00217 SO 2002 6 10 C2XA02CL126 1 20020606 A 3260 WARNING SYSTEM EMB 145 EMB145ER 3260211 SO COCKPIT MALFUNCTIONED A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 15948 145056 CLE FLIGHT 3037, THE CREW REPORTED A RIGHT MAIN LANDING GEAR AND LEVER DISAGREE MESSAGE AFTER TAKEOFF. THE MESSAGE RESE T AFTER 1ST CYCLE. MAINTENANCE PERFORMED AIR/GROUND OPERATIONAL CHECKS ON LANDING GEAR SYSTEMS. OPERATIONAL CHECKS WER E GOOD. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002061000218 20020610 00218 2002 6 10 HEEA079734 4 20020530 A 2340 A3016W INTERPHONE BELL 412 412 1182202 SW COCKPIT INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2148K 36001 SELECTOR SWITCH IS INTERMITTENT. FOUND SWITCH S4 AUDIO ALWAYS ON, FOUND BROKEN WIRE ON SWITCH S1 SECTION 2R TERMINAL 4, RESOLDERED WIRE BACK TO TERMINAL 4. ALSO FOUND LIGHT PANEL AND SWITCH S1 BAD. REPLACED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000219 20020610 00219 2002 6 10 HEEA079735 4 20020530 A 2340 A3016W INTERPHONE BELL 412 412 1182202 SW COCKPIT BROKEN E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 VHF NR 1 SWITCH BROKEN. FOUND VOLUME CONTROL R72, SWITCHES S2, S4, S5, S9, MIC AMP AR1, LIGHT PANEL, VOLUME AND SELECTOR KNOBS AND RESISTOR R33 BAD. REPLACED. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000220 20020610 00220 SO 2002 6 10 C2XA02IA123 1 20020607 A 2913 PV303211 PUMP EMB 145 EMB145 3260210 SO NR 2 ENGINE FAILED A C2XA O OTHER M OVER TEMP CR CRUISE 1 SW 27 16961 145103 OMA- DURING FLIGHT 3969, THE CREW NOTED THAT THE NUMBER 2 HYDRAULIC OVERHEAT/ HAD ZERO HYDRAULIC PRESSURE ON NUMBER 2 S IDE. THE CREW DECLARED EMERGENCY AND LANDED AT OMA WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 ENG INE DRIVEN HYDRAULIC PUMP, PERFORMED A OPERATIONAL AND LEAK CHECK OF THE HYDRAULIC PUMP. NO DEFECTS NOTED AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002061000221 20020610 00221 2002 6 10 HEEA079736 4 20020530 A 2340 A3016W INTERPHONE BELL 212 212 1181420 SW COCKPIT INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 102PH 30899 FM2 SWITCH WILL NOT TURN OFF FM. CLEANED S1 SWITCH. REPLACED S1 SWITCH. ALSO REPLACED BAD R72 VOLUME CONTROL, BAD S4, S5, S6, S7, S8 AND S11 SWITCHES, BAD SELECTOR AND VOLUME KNOBS AND BAD FACEPLATE. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 4U H4SW 2002061000222 20020610 00222 2002 6 10 HEEA079737 4 20020530 A 2340 A3016W INTERPHONE BELL 412 412 1182202 SW COCKPIT WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2261D 33076 VERY WEAK ON RADIO CHANNELS. FOUND TRANSMIT TOO LOW, VOLUME AND TRANSMIT KNOBS BAD. REPLACED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002061000223 20020610 00223 SO 2002 6 10 C2XA02IA124 1 20020607 A 2912 7588717101 FILTER EMB 145 EMB145 3260210 SO NR 2 ENGINE DIRTY A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 16961 145103 OMA- DURING FLIGHT 3969, THE CREW NOTED THAT THE NUMBER 2 HYDRAULIC OVERHEAT/ HAD ZERO HYDRAULIC PRESSURE ON NUMBER 2 S IDE. THE CREW DECLARED EMERGENCY AND LANDED AT OMA WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE, MA IN AND RETURN HYDRAULIC FILTERS, PERFORMED A LEAK CHECK. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 L 7 2 4F RT T00011AT 2002061000224 20020610 00224 SW 2002 6 10 HEEA079738 1 20020530 A 6220 222310460103 BEARING BELL 222 222U 1182140 SW M/R PITCH LINK STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6992 696 47521 M/R PITCH CONTROL LINK BEARING BETWEEN CLEVIS STICKING. SCRAPPED. 1 G 7 2 3U H9SW 2002061900086 20020619 00086 EU 2002 6 19 C2XA02IA125 1 20020607 A 3260 E0052R10B6SNE CONNECTOR AEROSP ATR42 ATR42320 8680930 EU LT MLG CONTAMINATED A C2XA K NONE N FALSE WARNING CL CLIMB 1 SW 27 86842 286 IAH- AFTER TAKEOFF FLIGHT 3671, THE CREW NOTED THAT SYSTEM NR 2 LANDING GEAR UNLOCK LIGHT ILLUMINATED. MAINTENANCE INS PECTED THE AIRCRAFT AND FOUND THE LEFT MAIN LANDING GEAR UPLOCK BOX CANNON PLUG TO BE CONTAMINATED. MAINTENANCE CLEANED THE AFFECTED PLUG, PERFORMED A SUCCESSFUL OPERATIONAL CHECK OF THE LANDING GEAR, AND APPROVED THE AIRCRAFT FOR RETURN T O SERVICE. 2 H 7 2 4T RT A53EU 2002061000225 20020610 00225 2002 6 10 HEEA079739 4 20020530 A 3461 065001580102 COMPUTER BELL 230 230 1182149 SW AUTO PILOT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RC 23037 COMPUTER WILL NOT ENGAGE AUTO PILOT WHEN AP BUTTON IS DEPRESSED. 1 G 7 2 3U NC H9SW 2002061000226 20020610 00226 SO 2002 6 10 C2XA02TY096 1 20020607 A 2910 3681001003 MANIFOLD EMB 145 EMB145 3260210 SO HYD SYSTEM OVERHEATED A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 13965 6544 145125 TYS WHILE EN ROUTE FROM IAH TO TYS THE A/C WAS OUT APPROXIMATELY THIRTY MINUTES WHEN THE EICAS GAVE A NR 1 HYD, SYSTEM OVERHEAT MESSAGE FOLLOWED BY 0 PRESSURE INDICATION ON NR 1 SYSTEM. THE CREW FOLLOWED THE QRH PROCEDURE AND LANDED THE A /C AT TYS. MAINTENANCE REMOVED AND REPLACED THE NR 1 HYD MANIFOLD ASSY IAW AMM 27-10-07. REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYD PUMP IAW 29-10-03. A/C WAS SERVICED AND ALL OPS CHECKS GOOD AND WAS RELEASED BACK TO SERVICE. 2 L 7 2 4F RT T00011AT 2002061000227 20020610 00227 2002 6 10 HEEA079740 4 20020531 A 2312 064100900 TRANSCEIVER BELL 212 212 1181420 SW VHF SYSTEM INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5736J 31140 VHF TRANSCEIVER WILL NOT TRANSMIT OR RECEIVE. REPLACED WITH SERVICEABLE PART. 1 G 7 1 4U H4SW 2002061000228 20020610 00228 2002 6 10 HEEA079741 4 20020531 A 2312 064100900 TRANSCEIVER BELL 212 212 1181420 SW VHF SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 102PH 30899 NO TRANSMIT. FOUND TRANSMIT POWER AND MODULATION FLUCTUATING. REMOVED CORROSION FROM RECEIVER/MODULATOR BOARD AND BOTTO M OF SYNTHESIZER BOARD IN VCO SECTION. APPLIED HUMISEAL TO VCO SECTION ON BOTTOM OF SYNTHESIZER BOARD FOR CORROSION CON TROL. REALIGNED TRANSMITTER. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 4U H4SW 2002061000229 20020610 00229 WP 2002 6 10 DHL2002802511 1 20020517 A 5512 SKIN DOUG DC8 DC873 302199C WP HORIZ STAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 79074 46076 RT HORZ STAB L/E WITH 10 INCH DENT BETWEEN STA XFS 72.500 - 85.000. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 PG 17. CUT A FFECTED AREA IAW SRM 55-2-1 PG 17. FABRICATED FILLER AND DOUBLER IAW SRM 55-2-1 PG 17. INSTALLED FILLER AND DOUBLER IA W SRM 55-2-1- PG 17. 2 L 7 4 4F RT 4A25 2002061000230 20020610 00230 2002 6 10 HEEA079742 4 20020531 A 2312 064100900 TRANSCEIVER BELL 212 212 1181420 SW VHF SYSTEM WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 102PH 30899 VHF TRANSCEIVER WEAK AND GARBLED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 4U H4SW 2002061000231 20020610 00231 2002 6 10 HEEA079743 4 20020531 A 2312 064100900 TRANSCEIVER BELL 212 212 1181420 SW VHF SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 102PH 30899 VHF TRANSCEIVER VERY GARBLED TRANSMISSION. REMOVED CORROSION BUILD UP UNDERNEATH VCO SHIELD ON BOTTOM OF SYNTHESIZER BOA RD. BENCH CHECK GOOD. 1 G 7 1 4U H4SW 2002061000232 20020610 00232 WP 2002 6 10 DHL2002804007 1 20020607 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP NR 5 INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 804DH 46124 NR 5 SMOKE DETECTOR WILL NOT TEST. RELAMPED NR 5 SMOKE DETECTOR IAW MM REF 26-10-1, GROUND OP CHECK GOOD. 2 L 7 4 4F RT 4A25 2002061000233 20020610 00233 2002 6 10 HEEA079744 4 20020531 A 2312 064102302 TRANSCEIVER BELL 212 212 1181420 SW VHF SYSTEM INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5736D 31135 VHF TRANSCEIVER WILL NOT TRANSMIT. FOUND TRANSMITTER VERY INTERMITTENT WHEN VIBRATED. FOUND COLD SOLDER ON PIN 1 OF P30 1 CONNECTOR. RESOLDERED PINS ON P301 CONNECTOR. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 4U H4SW 2002061000234 20020610 00234 2002 6 10 HEEA079745 4 20020531 A 2312 064102900 COUPLING BELL 212 212 1181420 SW VHF ANTENNA STUCK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3208H 31304 VHF ANTENNA COUPLING INTERMITTENTLY STICKS DURING TUNING PROCESS AND FILTER FITTING LOOSE. 1 G 7 1 4U H4SW 2002061000239 20020610 00239 2002 6 10 HEEA079746 4 20020531 A 2312 071127401 TRANSCEIVER BELL 212 212 1181420 SW VHF SYSTEM INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3208H 31304 VHF TRANSCEIVER NON FUNCTIONAL. 1 G 7 1 4U H4SW 2002061000240 20020610 00240 NM 2002 6 10 F3LA200200159 1 20020605 A 5347 CARGO TRACK BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3389 26440 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TRACK IN CARGO COMPARTMENT AT RBL 13.8, BETWEEN STA 795 AND 827 . REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-00-63, 53-00-53, 51-41-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002061000241 20020610 00241 SW 2002 6 10 HEEA079747 1 20020531 A 7714 212075037113 INDICATOR BELL 212 212 1181420 SW N1 INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 27805 31106 ENGINE N1 INDICATOR INOPERATIVE. 1 G 7 1 4U H4SW 2002061000243 20020610 00243 SW 2002 6 10 HEEA079748 1 20020531 A 2910 212076310001 LINE BELL 212 212 1181420 SW HYD SYSTEM LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 5736D 31135 HOLE IN HYDRAULIC LINE. SCRAPPED. 1 G 7 1 4U H4SW 2002061000244 20020610 00244 SW 2002 6 10 HEEA079749 1 20020531 A 2910 FERRULE BELL 212 212 1181420 SW HYD LINE LOOSE E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 102PH 30899 HYD LINE LEAKING AT FITTING FERRULE LOOSE ON LINE. SCRAPPED. 1 G 7 1 4U H4SW 2002061000245 20020610 00245 2002 6 10 HEEA079750 4 20020531 A 2300 G4434A CONTROL HEAD BELL 212 212 1181420 SW RADIO COMMS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1079U 31122 CONTROL HEAD WILL NOT RECEIVE ON 120.5 MHZ. FOUND BAD CR3 DIODE. BENCH CHECK GOOD. 1 G 7 1 4U H4SW 2002061000246 20020610 00246 2002 6 10 HEEA079751 4 20020531 A 2300 SWITCH BELL 212 212 1181420 SW CONTROL HEAD FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 27805 31106 CONTROL HEAD ON/OFF SWITCH INTERMITTENT. ON/OFF SWITCH BAD. REPLACED BAD S2 ON/OFF SWITCH. REPAIRED. BENCH CHECK GOOD . 1 G 7 1 4U H4SW 2002061000248 20020610 00248 NM 2002 6 10 F3LA200200162 1 20020605 A 5347 CARGO TRACK BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3269 26293 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR TRACK BETWEEN STA 795 AND 827, RBL 13.8. INSTALLED REPLA CEMENT CARGO TRACK PER SRM 53-60-53 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002061000249 20020610 00249 2002 6 10 HEEA079752 4 20020531 A 3442 MI5852013 INDICATOR BELL 212 212 1181420 SW WX RADAR SYS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 102PH 30899 RADAR SCREEN FLASHES ON THEN OFF WITH DISTORTED IMAGING. COULD NOT DUPLICATE PROBLEM. INSTALLED MOD 9. REPLACED U1901, U1902, U1903, IC ON PAGE DISPLAY BOARD. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 4U H4SW 2002061000251 20020610 00251 2002 6 10 HEEA079754 4 20020531 A 2312 064102300 TRANSCEIVER BELL 214 214ST 1182106 SW VHF SYSTEM INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 822H 28139 DF 88 HOMING INOPERATIVE. NO DETECTED AUDIO OUTPUT. INSTALLED ELT HONING MOD 1. REPAIRED. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 2002061000253 20020610 00253 2002 6 10 HEEA079755 4 20020531 A 2312 064102300 TRANSCEIVER BELL 214 214ST 1182106 SW VHF SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8045T 28101 VHF TRANSCEIVER UNRELIABLE, TRANSMIT LIGHT COMES ON WITH SQUELCH. ADJUSTED MIC GAIN AND SIDETONE. FOUND Q102, Q109 AND Q110 TRANSISTORS BAD AND Q110 SOCKET BAD DUE TO CORROSION. ALSO FOUND Q102, Q104 AND Q106 TRANSISTORS BAD. REPLACED. REPAIRED. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 2002061000254 20020610 00254 2002 6 10 HEEA079756 4 20020531 A 2312 064102300 TRANSCEIVER BELL 214 214ST 1182106 SW VHF SYSTEM INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8045T 28101 RECEIVES AND TRANSMITS INTERMITTENT. FOUND WHEN UNIT STOPPED RECEIVING THAT VCO VOLTAGE WAS FAR OUT OF SPECS. FOUND C/N SQUELCH HARD TO ADJUST TO SPECS AND RECEIVER HAS MOTORBOATING AND HIGH PITCH NOISE. ADJUSTED VCO AND ALIGNED RECEIVER SEVERAL TIMES. RESOLDERED COMPONENTS IN VCO SECTION AND RECEIVER WAS NO LONGER INTERMITTENT BUT STILL HAD MOTORBOATING AND HIGH PITCH NOISE AND HARD TO ADJUST C/N SQUELCH. REPLACED Q304, Q305, AND Q309 CAPACITOR. REPLACED C368 AND C372 C APACITORS AND L310 COIL. REPLACED C370 CAPACITOR. REPAIRED. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 2002061000255 20020610 00255 EU 2002 6 10 MALA020325 1 20020514 A 5320 7253720319 SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K-CHECK IN CWA, RT SEAT TRACK WRAP AROUND HAS CORROSION. MAINTENANCE INSTALLED NEW FRAME SUPPORT ON RT SEAT TRA CK IAW SAAB SRM 51. 2 L 7 2 4T RT A52EU 2002061000256 20020610 00256 2002 6 10 HEEA079757 4 20020531 A 3454 071121701 INDICATOR BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 59805 28141 INDICATOR BEARING POINTER STAYS STOWED. 2 G 7 2 4U H10SW 2002061000257 20020610 00257 2002 6 10 HEEA079758 4 20020531 A 3454 071121701 INDICATOR BELL 214 214ST 1182106 SW COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 59806 28140 INDICATOR HAS BROKEN THREADS FOR FRONT CONNECTOR. 2 G 7 2 4U H10SW 2002061000258 20020610 00258 SW 2002 6 10 HEEA079759 1 20020531 A 5260 214001423105 ACTUATOR BELL 214 214ST 1182106 SW AIRSTAIR STEP FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8045T 28101 RT PASSENGER STEP WILL NOT STOW. 2 G 7 2 4U H10SW 2002061000259 20020610 00259 SW 2002 6 10 HEEA079760 1 20020531 A 5260 214001423105 ACTUATOR BELL 214 214ST 1182106 SW AIRSTAIR STEP FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8045T 28101 RT PASSENGER STEP WILL NOT STOW. 2 G 7 2 4U H10SW 2002061000260 20020610 00260 SW 2002 6 10 HEEA079761 1 20020531 A 6510 214040600109 HANGER ASSY BELL 214 214ST 1182106 SW T/R DRIVESHAFT DAMAGED E HEEA K NONE E L VIBRATION/BUFFET NO TEST IN INSP/MAINT 1 SW 03 8045T 28101 HIGH VIBRATION READING FROM RDA SYSTEM. REPLACED TAIL ROTOR DRIVESHAFT HANGER. 2 G 7 2 4U H10SW 2002061000261 20020610 00261 EU 2002 6 10 MALA020327 1 20020515 A 5712 RIB SAAB SF340 340B 7860101 EU LT WING CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K-CHECK IN CWA, LT LEADING EDGE 511BL HAS CRACKED RIBS. MAINTENANCE FABRICATED REPAIR ANGLES FROM LOT 415071 AN D COMPLETED REPAIRS, IAW SRM 57-10-30, TO RIBS AS REQUIRED. 2 L 7 2 4T RT A52EU 2002061000262 20020610 00262 EU 2002 6 10 MALA020328 1 20020605 A 3260 PRINTED CKT BOAR BAC 146 AVRO146RJ85A 1500097 EU LANDING GEAR FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 520XJ E2345 DURING FLIGHT 3468 AFTER LEVELING OFF AT 14,000 FEET RIGHT MAIN GEAR GREEN DOWN AND LOCKED, ILLUMINATED SEVERAL TIMES. RETARD TO IDLE, REDUCED SPEED TO 210 KTS AND PROBLEM DISAPPEARED. UPON SELECTION OF GEAR DOWN, GREEN LIGHT (RIGHT MAIN) ILLUMINATED FOLLOWED BY RED UNLOCKED LIGHT. MAINTENANCE DURING TROUBLESHOOTING SUSPECT PCB GJ22 TO BE AT FAULT. REMOV ED AND REPLACED PCB GJ22 S/N ON A187589, S/N OFF A184215. REMOVED AND REPLACED RELAY GF4 AS REQ, SWUNG GEAR SEVERAL TIM ES. ALL CKS GOOD AT THIS TIME. 2 H 7 4 4F RT A49EU 2002061000263 20020610 00263 WP 2002 6 10 MWEA020387 1 20020604 A 5313 591287023 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT ACCESSORY COMPARTMENT LONGERON 15 LEFT HAS LIGHT CORROSION UNDER TOP FLANGE AT STATION 1076. REMOVED AND REPLACED L ONGERON SECTION AND SPLICE. 2 L 7 2 4F A6WE 2002061000264 20020610 00264 WP 2002 6 10 MWEA020388 1 20020604 A 5210 591008131 DOUBLER DOUG DC9 DC932 3022066 WP PAX DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FORWARD PASSENGER DOOR HANDLE CHAFING ON DOUBLER AROUND HANDLE CUTOUT. REMOVED AND REPLACED DOUBLER. 2 L 7 2 4F A6WE 2002061000265 20020610 00265 WP 2002 6 10 MWEA020389 1 20020604 A 5320 99236685 WEB DOUG DC9 DC932 3022066 WP FUSELAGE PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 COCKPIT SUBFLOOR AT STATION 134 APPROXIMATELY 24 INCHES RIGHT OF THE AIRCRAFT CENTERLINE IS PUNCTURED. FABRICATED AND I NSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002061000266 20020610 00266 SW 2002 6 10 HEEA079762 1 20020531 A 6320 214040840101 SEAL BELL 214 214ST 1182106 SW OUTPUT DRIVE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 5748M 28102 MAIN ROTOR GEARBOX OUTPUT DRIVE SEAL LEAKING. REPLACED WITH SERVICEABLE PART. 2 G 7 2 4U H10SW 2002061000267 20020610 00267 WP 2002 6 10 MWEA020391 1 20020604 A 5320 49193251 STRINGER CLIP DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT ACCESSORY COMPARTMENT LONGERON 22 CLIP RIGHT HAS LIGHT CORROSION, LOCATED JUST FORWARD OF CANTED FRAME STATION 1121. REMOVED AND REPLACED END FITTING. 2 L 7 2 4F A6WE 2002061000268 20020610 00268 SW 2002 6 10 HEEA079763 1 20020531 A 6320 214040840101 SEAL BELL 214 214ST 1182106 SW OUTPUT DRIVE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 5748M 28102 MAIN ROTOR GEARBOX OUTPUT DRIVE SEAL LEAKING. SCRAPPED. 2 G 7 2 4U H10SW 2002061000269 20020610 00269 WP 2002 6 10 MWEA020392 1 20020604 A 5330 5910228315 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT ACCESSORY COMPARTMENT, SKIN BELOW LONGERON 18 LEFT STATION 1086 TO CANTED FRAME 1121 HAS CORROSION ON INNER SURFACE. FABRICATED AND INSTALLED SKIN. 2 L 7 2 4F A6WE 2002061000270 20020610 00270 SW 2002 6 10 HEEA079764 1 20020531 A 7603 214060327101 CONTROL CABLE BELL 214 214ST 1182106 SW ENG CONTROLS BENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 CABLE IMPOSSIBLE TO MOVE. FOUND THREADED PORTION OF CABLE TO BE BENT. REPLACED WITH SERVICEABLE CABLE. 2 G 7 2 4U H10SW 2002061000271 20020610 00271 WP 2002 6 10 MWEA020393 1 20020604 A 5313 591142851 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT ACCESSORY COMPARTMENT LONGERON 21 LEFT HAS LIGHT CORROSION UNDER BOTTOM FLANGE AT STATION 1080. REMOVED AND REPLACE D LONGERON SECTION. 2 L 7 2 4F A6WE 2002061000272 20020610 00272 2002 6 10 HEEA079765 4 20020531 A 3442 40008310105 TRANSCEIVER BELL 214 214ST 1182106 SW RADAR SYS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 59806 28140 RADAR WILL NOT PAINT TARGET OR TEST CORRECTLY. 2 G 7 2 4U H10SW 2002061000273 20020610 00273 WP 2002 6 10 MWEA020394 1 20020604 A 5313 591022854 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT ACCESSORY COMPARTMENT LONGERON 19 LEFT HAS AREAS OF LIGHT CORROSION UNDER FLANGES ON TOP AND BOTTOM SIDE FROM STATIO N 1080 TO CANTED FRAME 1121. MANUFACTURED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 2002061000274 20020610 00274 2002 6 10 HEEA079767 4 20020531 A 3442 7021450601 INDICATOR BELL 214 214ST 1182106 SW RADAR SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5748M 28102 SHOWS A 10 MILE VERTICAL DISPLAY AFTER 20 MINUTES. 2 G 7 2 4U H10SW 2002061000275 20020610 00275 WP 2002 6 10 MWEA020395 1 20020604 A 5310 59129952 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 RIGHT FORWARD EMERGENCY EXIT DOOR JAMB IS CHAFED AT THE TOP LATCH. LOCATED, DRILLED, AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002061000277 20020610 00277 WP 2002 6 10 MWEA020396 1 20020604 A 5310 59129952 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT RIGHT EMERGENCY EXIT DOOR JAMB IS CHAFED AT UPPER LATCH ASSY. LOCATED, DRILLED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002061000278 20020610 00278 WP 2002 6 10 MWEA020400 1 20020604 A 5330 591142865 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT ACCESSORY COMPARTMENT SKIN HAS HEAVY CORROSION ON SKIN AT STATION 1009 BETWEEN LONGERON 18 AND 19 RIGHT. FABRICATED AND INSTALLED DOUBLER, FAIRING PLATE, AND SHIMS. 2 L 7 2 4F A6WE 2002061000279 20020610 00279 WP 2002 6 10 MWEA020401 1 20020604 A 5311 59114481 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 MODERATE CORROSION ON AFT FACE OF FORWARD FRAME 332 AT LONGERON 30, 29, & 28 RIGHT. REMOVED AND REPLACED FRAME SECTION REPAIR. 2 L 7 2 4F A6WE 2002061000280 20020610 00280 NE 2002 6 10 HEEA079769 2 20020531 A 7200 ENGINE BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE ENGINE BAY MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 9496 28102 GEE343015 ENGINE PRODUCING LOW POWER. HIGH MGT ON POWER ASSURANCE CHECK. REPAIRED ENGINE. FOUND MISSING COATING ON STG. 1 NOZZLE TIP PATH WHICH WAS POSSIBLE CAUSE FOR LOW POWER. REPLACED G/G STATOR ASSY, G/G ROTOR ASSY, COMBUSTION LINER AND OUTER BALANCE PISTON SEAL WITH NEW PARTS. 2 G 7 2 4U 4 U H10SW E8NE 2002061000281 20020610 00281 WP 2002 6 10 MWEA020402 1 20020604 A 5311 3912219509 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 LIGHT CORROSION ON AFT FACE OF FORWARD FRAME 237 FROM LONGERON 29 LEFT TO 26 RIGHT. FABRICATED AND INSTALLED REPAIR DOU BLERS. 2 L 7 2 4F A6WE 2002061000282 20020610 00282 WP 2002 6 10 MWEA020403 1 20020604 A 5311 5911448503 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT CARGO COMPARTMENT FRAME STATION 870 HAS LIGHT CORROSION AROUND LONGERON 30 ATTACH BOLTS. CUT OUT DAMAGED AREA OF FR AME AND INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2002061000283 20020610 00283 2002 6 10 HEEA079770 4 20020531 A 3457 N0002000 GPS BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3897N 28106 GPS SATELLITE MODEM HAS NO TRANSMIT, LED REMAINS RED DURING TRANSMIT. 2 G 7 2 4U H10SW 2002061000284 20020610 00284 SW 2002 6 10 HEEA079771 1 20020531 A 2432 RG214 BATTERY BELL 214 214ST 1182106 SW MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5748M 887 28102 BATTERY WEAK. 2 G 7 2 4U H10SW 2002061000285 20020610 00285 SW 2002 6 10 HEEA079772 1 20020531 A 2432 RG214 BATTERY BELL 214 214ST 1182106 SW MAIN DISCHARGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3897N 498 28106 BATTERY VOLTAGE BELOW 15. 2 G 7 2 4U H10SW 2002061000286 20020610 00286 SW 2002 6 10 HEEA079773 1 20020531 A 2432 RG214 BATTERY BELL 214 214ST 1182106 SW MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3897N 484 28106 BATTERY WEAK. 2 G 7 2 4U H10SW 2002061000287 20020610 00287 SW 2002 6 10 HEEA079774 1 20020531 A 2432 RG214 BATTERY BELL 214 214ST 1182106 SW MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5748M 489 28102 BATTERY WEAK. 2 G 7 2 4U H10SW 2002061000288 20020610 00288 SW 2002 6 10 HEEA079775 1 20020531 A 2432 RG214 BATTERY BELL 214 214ST 1182106 SW MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5748M 171 28102 BATTERY WEAK. 2 G 7 2 4U H10SW 2002061000289 20020610 00289 SW 2002 6 10 HEEA079776 1 20020531 A 2432 RG214 BATTERY BELL 214 214ST 1182106 SW MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8045T 495 28101 BATTERY WEAK. 2 G 7 2 4U H10SW 2002061000290 20020610 00290 SW 2002 6 10 HEEA079777 1 20020531 A 2432 RG214 BATTERY BELL 214 214ST 1182106 SW MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8045T 164 28101 BATTERY WEAK. 2 G 7 2 4U H10SW 2002061000291 20020610 00291 2002 6 10 HEEA079778 4 20020531 A 3414 206075725103 INDICATOR BELL 206 206L3 1182108 SW AIRSPEED READS LOW E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 AIRSPEED INDICATOR READING 10 KNOTS SLOW AT 130 KNOTS. 1 G 7 1 3U H2SW 2002061000292 20020610 00292 SW 2002 6 10 HEEA079779 1 20020531 A 2840 473203003 SIGNAL COND UNIT BELL 412 412 1182202 SW FUEL SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2149S 36002 SIGNAL COND UNIT WILL NOT HOLD CALIBRATION. 1 G 7 2 4U H4SW 2002061000293 20020610 00293 2002 6 10 HEEA079780 4 20020528 A 2312 064105430 TRANSCEIVER SNIAS 350 AS350B2 8680813 EU VHF SYSTEM FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 40466 3004 UNREADABLE AND GARBLED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H9EU 2002061000294 20020610 00294 2002 6 10 HEEA079782 4 20020530 A 2312 9710831 TRANSCEIVER SNIAS 350 AS350B 8680801 EU VHF SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 972AE 3234 VHF TRANSCEIVER RECEIVES BROKEN OR CLIPPING ON AIR EVAC FREQUENCIES. FOUND VHF RECEIVER HAS NARROW MODULATION BANDWIDTH STOPS RECEIVING AT AROUND 4 KHZ ON ALL VHF FREQUENCIES. 1 G 7 1 3U H9EU 2002061000296 20020610 00296 2002 6 10 HEEA079783 4 20020530 A 2312 064101900 TRANSCEIVER BOLKMS 117 BK117A1 5626010 EU VHF SYSTEM DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 217UC 7152 VHF TRANSCEIVER LED LIGHTS INOPERATIVE. REPLACED BAD DS501 DISPLAY AND APPLIED DOW CORNING NR 4 COMPOUND TO DISPLAY CONT ACTS. REPLACED BAD DISPLAY LENS. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 2002061000297 20020610 00297 NM 2002 6 10 P2EA2002MO38 1 20020523 A 2751 INDICATOR BOEING 737 737230 1384401 NM COCKPIT FAILED A P2EA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 05 124NJ 22122 T/E FLAPS WOULD NOT EXTEND FROM FULL UP POSITION UPON DEPARTURE FROM GATE. REMOVED AND REPLACED THE FLAP POSITION INDIC ATOR PER MM 27-58-41, OPS CHECK GOOD AT ALL POSITION SETTINGS. 2 L 7 2 4F RT A16WE 2002061000298 20020610 00298 2002 6 10 HEEA079784 4 20020530 A 3452 066106200 TRANSPONDER BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8197X S808 TRANSPONDER WOULD NOT PASS CERTIFICATION. FOUND FREQUENCY TO BE INTERMITTENT. RESOLDERED LOOSE WIRES ON V101 AND ADJUST ED FREQUENCY AND POWER TO SPECS. INSTALLED GROOVE PIN ON LOCKING MECHANISM. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 2002061000299 20020610 00299 WP 2002 6 10 P2EA2002V0038 1 20020528 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 131NJ 49846 DURING 1C INSPECTION: FWD CARGO COMPT, DOOR WITH SKIN CRACKED AT FWD LOWER CORNER. FWD CARGO DOOR LOWER FWD CUTOUT SKIN REPAIRED FROM BS 372.250 TO BS 383.0 DUE TO CRACK IAW COOPESA EO NUMBER COO-9-52-298-02, DATED MAY 21, 2002, APPROVED A ND DOCUMENTED ON FAA 8110-3 FORM. 2 L 7 2 4F RT A6WE 2002061000300 20020610 00300 WP 2002 6 10 P2EA2002V0039 1 20020529 A 5753 5930495506J VANE DOUG DC9 DC983 3022083 WP T/E FLAP DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 131NJ 49846 DURING 1C CHECK INSPECTION: RT WING INBOARD FLAP OUTBOARD FIXED VANE DELAMINATED. REPAIRED RT WING INBOARD FLAP OUTBOAR D FIXED VANE DUE TO DELAMINATION, IAW COOPESA EO NUMBER COO-CMP-9-57-299-02 APPROVED ON FAA 8110-3 FORM. 2 L 7 2 4F RT A6WE 2002061000301 20020610 00301 NM 2002 6 10 P5CA0200674 1 20020513 A 8012 INDICATOR BOEING 747 7472U3B 1384846 NM PWA JT9 JT9D7Q 52054 NE COCKPIT FAULTY A P5CA E J ENGINE SHUTDOWN DUMP FUEL N FALSE WARNING CL CLIMB 1 WP 23 923FT 22769 702243 NR 3 ENG START VALVE OPEN LIGHT CAME ON AFTER TAKEOFF AT 8,000 FT. SHUT DOWN NR 3 ENG, LIGHT WENT OUT AFTER SHUT DOWN A T APPROX 3,000 FT. TROUBLESHOT SYSTEM AND FOUND LIGHT INDICATION SYSTEM AT FAULT. 2 L 7 4 4F 4 F RT A20WE E3NE 2002061000302 20020610 00302 NM 2002 6 10 PCAA0206062 1 20020605 A 3260 841005 PSEU DHAV DHC8 DHC8102 2809003 NM AVIONICS RACK UNSERVICEABLE A PCAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 13 807EX 27951 292 LGA- FLIGHT# 3971. CREW REPORTED THAT AFTER GEAR WAS EXTENDED WITH 3 GREEN INDICATED DOWN AND LOCKED UPON SHORT FINAL, N OSE GEAR RED UNSAFE LIGHT ILLUMNINATED WITH LANDING GEAR WARNING HORN. UPON GO-AROUND, NOSE GEAR INDICATED GREEN WITH NO INPUT. MAINTENANCE REPLACED PROXIMITY SWITCH ELECTRONICS UNIT (PSEU), AND NOSE GEAR RIGHT WEIGHT ON WHEELS SWITCH. SELF TEST AND GEAR SWING CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061000303 20020610 00303 NM 2002 6 10 P5CA0200677 1 20020523 A 2997 GROUND WIRE BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE HYD SYSTEM BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 702066 NR 2 ENGINE PYLON HYD S/O VALVE GROUND WIRES, PYLON STA 270, BROKEN. REPAIRED GROUND WIRES IAW SWP 20-11-15. 2 L 7 4 4F 4 F A20WE E3NE 2002061000304 20020610 00304 NM 2002 6 10 P5CA0200679 1 20020530 A 7120 65B903693 MOUNT BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENGINE WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 702066 NR 2 ENG AFT UPPER ENG MOUNT BENT ON ALIGNMENT HOLE, MOUNT ASSY WORN. REMOVED & REPLACED AFT ENG MOUNT IAW MM 71-21-03. 2 L 7 4 4F 4 F A20WE E3NE 2002061000305 20020610 00305 NM 2002 6 10 P5CA0200680 1 20020530 A 7120 MOUNT BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENGINE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 702066 LEVEL 1 CORROSION FOUND ON ENG UPPER REAR MOUNT BULKHEAD FITTING LOWER LUGS WHILE REMOVING NR 2 ENG REAR UPPER MOUNT FOR REPAIRS. ACCOMPLISHED SB 747-54A2200. COATED MOUNT W/ BMS 14-4, TYPE 2. COATING IAW 747-A2200 SERMATECH ENGINEERING BULLETIN 249. 2 L 7 4 4F 4 F A20WE E3NE 2002061300122 20020613 00122 NM 2002 6 13 SABA020067 1 20020608 A 3350 1306 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 FLIGHT 5025 FROM CLT TO THL, DURING PREFLIGHT THE EMERGENCY FLOOR LIGHTS WOULD NOT TEST. MAINTENANCE REMOVED AND REPLAC ED BULBS. SYSTEM OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061000306 20020610 00306 WP 2002 6 10 DHL2002805049 1 20020608 A 2697 CONNECTOR DOUG DC8 DC873F 302199F WP A DHLA O OTHER J L WARNING INDICATION NO TEST IN INSP/MAINT 1 SO 01 805DH 46125 1) #2 ENG "B" SYS LOOP (FIRE) WILL NOT TEST2) R&R FIRE LOOP CONNECTOR PER DC8 WDM 26-01-01 & STANDARD WIRE PRACTICES C HAPT 20. OPS CK SERVICABLE. 2 L 7 4 4F RT 4A25 2002061000307 20020610 00307 SO 2002 6 10 C2XA02CL130 1 20020608 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13990 145277 DURING ROUTINE MAINTENANCE THE FLOOR PROXIMITY STRIP LIGHTS FROM ROW 12 TO LAST ROW WILL NOT ILLUMINATE.MAINTENANCE REPL ACED THE #6 EMERGENCY LIGHT AC/DC INVERTER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002061000308 20020610 00308 WP 2002 6 10 2002F00570 1 20020515 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON STRINGER 48R, AND THE OUTBOARD SIDE OF THE SPLICE AT STRINGER 48R, AT STATION 1705. (M) 2 L 7 3 4F A22WE 2002061000309 20020610 00309 WP 2002 6 10 2002F00571 1 20020515 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON SHEAR TIE, AT STATION 1741, BETWEEN STRINGER 47R AND 48R. (M) 2 L 7 3 4F A22WE 2002061000310 20020610 00310 WP 2002 6 10 DHL2002801013 1 20020609 A 2611 BULB DOUG DC8 DC873F 302199F WP A DHLA O OTHER J L WARNING INDICATION NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 1) MAIN DECK CARGO COMPT. DETECTOR #6 WONT TEST2) ENTERED ON DMI # 9542 IAW DHL MEL 26-6 CAT C PLACARD INSTALLED MARTI N 211513) REFER DMI #9542 MAIN DECK CARGO COMPT DETECTOR #6 WONT TEST4) RELAMPED #6 SMOKE DETECTOR BEACON TEST BULBS O PS CHECK NORMAL IAW MM 26-10-5 THIS CLEARS DMI # 9542 2 L 7 4 4F RT 4A25 2002061000311 20020610 00311 WP 2002 6 10 2002F00572 1 20020515 A 5320 PANEL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON BILGE COVER PANEL STRUCTURE NUTPLATE ANGLE, AT STATION 1761, ABOVE STRINGER 49R. (M) 2 L 7 3 4F A22WE 2002061000312 20020610 00312 WP 2002 6 10 2002F00573 1 20020515 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON SHEAR TIE AFT FACE, AT STATION 1751, BETWEEN STRINGERS 47R-48R. (M) 2 L 7 3 4F A22WE 2002061000313 20020610 00313 WP 2002 6 10 2002F00574 1 20020514 A 5320 ATTACH ANGLE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY, AT FRAME STATION 1964, ON LONGERON ATTACH ANGLE, BETWEEN LONGERON 48R AND LONGERON 51L. (M) 2 L 7 3 4F A22WE 2002061000314 20020610 00314 WP 2002 6 10 2002F00575 1 20020514 A 5320 INTERCOSTAL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY ON LONGERON INTERCOSTAL FRAME, AT STATION 1953 AND 1964, LONGERON 48R AND L ONGERON 46R. (M) 2 L 7 3 4F A22WE 2002061000315 20020610 00315 WP 2002 6 10 2002F00576 1 20020515 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSLEGAE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON THE FORWARD FACE OF SHEAR TIE, AT STATION 1761, BETWEEN STRINGER 46R AND 47R. (M) 2 L 7 3 4F A22WE 2002061000316 20020610 00316 WP 2002 6 10 2002F00577 1 20020515 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON SHEAR TIE FORWARD FACE, AT STATION 1761, BETWEEN STRINGERS 50R AND 51R. (M) 2 L 7 3 4F A22WE 2002061000317 20020610 00317 WP 2002 6 10 2002F00578 1 20020513 A 5320 BRACKET DOUG DC10 DC1010 3022110 WP FS 1721/1741 CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON ANTENNA SUPPORT BRACKET ON STRINGER 52, ALONG LOWER EDGE, BETWEEN STATION 1721 AND 1741. (M) 2 L 7 3 4F A22WE 2002061000318 20020610 00318 WP 2002 6 10 2002F00579 1 20020514 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY, ON LONGERON 52, BETWEEN FRAME STATION 1953 AND 1964. (M) 2 L 7 3 4F A22WE 2002061000319 20020610 00319 WP 2002 6 10 2002F00580 1 20020514 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY ON SHEAR TIE, AT FRAME STATION 1964, LONGERON 50R AND LONGERON 50L. (M) 2 L 7 3 4F A22WE 2002061000320 20020610 00320 WP 2002 6 10 2002F00581 1 20020513 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT CHECK, FOUND CORROSION ON SHEAR TIES IN AFT CARGO BAY, BETWEEN LONGERON 51R AND 47R, AND LONGERON 47R AND 48R, AT STA TION 1841. (M) 2 L 7 3 4F A22WE 2002061000321 20020610 00321 NM 2002 6 10 2002F00582 1 20020426 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CORROSION ON AFT CARGO COMPARTMENT FLOORBEAM STATION 950E RBL 27, FORWARD SIDE. (M) 2 L 7 3 4F A3WE 2002061000322 20020610 00322 NM 2002 6 10 2002F00583 1 20020426 A 5320 WEB BOEING 727 727225 1384077 NM FUSELAGE PUNCTURED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CABIN FLOOR WEB PUNCTURED AT STATION 1172, RBL 27. (M) 2 L 7 3 4F A3WE 2002061000323 20020610 00323 NM 2002 6 10 2002F00584 1 20020425 A 5313 STRINGER BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CORROSION ON STRINGER NR 30 FROM STATION 1010 TO 1090. (M) 2 L 7 3 4F A3WE 2002061000324 20020610 00324 NM 2002 6 10 2002F00585 1 20020425 A 5330 DOUBLER BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CORROSION ON ANTENNA DOUBLER AT STATION 1040 BETWEEN STRINGERS 30 AND 29R. (M) 2 L 7 3 4F A3WE 2002061000325 20020610 00325 NM 2002 6 10 2002F00586 1 20020402 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND FORWARD CABIN FLOORBEAM CRACKED IN RADIUS 1.5 INCHES LONG AT STATION 326 RBL 24. (M) 2 L 7 3 4F A3WE 2002061000326 20020610 00326 NE 2002 6 10 2002F00587 2 20020403 A 7200 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 MALFUNCTIONED A RYNA E J ENGINE SHUTDOWN DUMP FUEL R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 07 801EA 22432 696535 DURING CLIMB-OUT FROM DAY, CREW NOTED NR 1 ENGINE EPR DROP AND EGT RISE, WITH POSSIBLE COMPRESSORS STALL AT IDLE. NR 1 ENGINE WAS SHUT DOWN AND 7,000 POUNDS OF FUEL DUMPED. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED IN DAY WITHOUT INCIDE NT. NR 1 ENGINE CHANGE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2002061000327 20020610 00327 NM 2002 6 10 2002F00588 1 20020403 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME, UPPER CHORD, CRACKED AT STATION 580 RBL 3. (M) 2 L 7 3 4F A3WE 2002061000328 20020610 00328 NM 2002 6 10 2002F00589 1 20020412 A 5753 FLAP BOEING 727 727225 1384077 NM RT WING DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 815EA 22552 AT C-CHECK, FOUND DENT OUT OF LIMITS ON RIGHT WING INBOARD AFT FLAP. (M) 2 L 7 3 4F A3WE 2002061000329 20020610 00329 NM 2002 6 10 2002F00590 1 20020423 A 5313 STRINGER BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND RIGHT WHEEL WELL STRINGER 18 TO FITTING ATTACHMENT ANGLE CRACKED AT STATION 940. (M) 2 L 7 3 4F A3WE 2002061000330 20020610 00330 NM 2002 6 10 2002F00591 1 20020423 A 5320 ANGLE BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND RIGHT WHEEL WELL AFT BULKHEAD LOWER FAIRING ATTACHMENT ANGLE CRACKED AND CORRODED AT STATION 950 BL 12 -24. (M) 2 L 7 3 4F A3WE 2002061000331 20020610 00331 NM 2002 6 10 2002F00592 1 20020423 A 5210 DOUBLER BOEING 727 727225 1384077 NM ENTRY DOOR TORN A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND L1 DOOR INNER SKIN DOUBLER TORN JUST BELOW THE CENTERING GUIDE STOP PIN. (M) 2 L 7 3 4F A3WE 2002061000332 20020610 00332 NM 2002 6 10 2002F00594 1 20020424 A 5320 SUPPORT BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CRACK ON FORWARD PIT FRAME SUPPORT AT STATION 480 LBL 6 TO RBL 6. (M) 2 L 7 3 4F A3WE 2002061000333 20020610 00333 NM 2002 6 10 2002F00595 1 20020424 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND LEFT SEAT TRACK CRACKED APPROXIMATELY .325 INCHES LONG AT STATION 1137 BL 46L. (M) 2 L 7 3 4F A3WE 2002061000334 20020610 00334 NM 2002 6 10 2002F00596 1 20020424 A 5753 FLAP BOEING 727 727225 1384077 NM WING CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND LEADING EDGE OF NR 3 FLAP CRACKED ON THE UNDERSIDE OUTBOARD RIB, JUST ABOVE THE DATA PLATE. (M) 2 L 7 3 4F A3WE 2002061000335 20020610 00335 WP 2002 6 10 2002F00597 1 20020513 A 5320 ATTACH ANGLE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY LONGERON TO FRAME ATTACH ANGLE, AT STATION 1853 TO 1871, LONGERON 51L TO 51 R. (M) 2 L 7 3 4F A22WE 2002061000336 20020610 00336 WP 2002 6 10 2002F00598 1 20020513 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FLOOR SUPPORT, AT STATION 440, LBL 65. (M) 2 L 7 3 4F A22WE 2002061000337 20020610 00337 WP 2002 6 10 2002F00599 1 20020513 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FLOOR SUPPORT ANCHOR BOLTS, AT STATION 432, LBL 25. (M) 2 L 7 3 4F A22WE 2002061000338 20020610 00338 WP 2002 6 10 2002F00600 1 20020513 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FLOOR SUPPORT, AT STATION 440 LBL 10. (M) 2 L 7 3 4F A22WE 2002061000339 20020610 00339 WP 2002 6 10 2002F00601 1 20020513 A 5320 ATTACH ANGLE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY ON FRAME TO LONGERON ATTACH ANGLE, AT STATION 1931.5, LONGERON 50R TO LONGE RON 51L. (M) 2 L 7 3 4F A22WE 2002061000340 20020610 00340 WP 2002 6 10 2002F00602 1 20020513 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY ON LONGERON 48R, AT STATION 1921. (M) 2 L 7 3 4F A22WE 2002061000341 20020610 00341 WP 2002 6 10 ZW0A0206001 1 20020608 A 5330 7732 BULB DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 967TW 53617 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 21D TO 27D. REPLACED POWER SUPPLY, PN 60-0304-51, AND ALL THE BULBS. CHEC K-C 5-26-01 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2002061000342 20020610 00342 WP 2002 6 10 2002F00603 1 20020513 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FLOOR SUPPORT, AT STATION 459, LBL 50. (M) 2 L 7 3 4F A22WE 2002061000343 20020610 00343 WP 2002 6 10 2002F00540 1 20020517 A 5320 TEE CHORD DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION AT AFT PRESSURE BULKHEAD FLOOR LINE T-CHORD, ON LOWER SURFACE, AT STATION 2007. (M) 2 L 7 3 4F A22WE 2002061000344 20020610 00344 WP 2002 6 10 2002F00565 1 20020515 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT CHECK, FOUND CORROSION ON 'J' LEG FRAME, AT STATION 1741, BETWEEN STRINGERS 48L AND 48R. (M) 2 L 7 3 4F A22WE 2002061000345 20020610 00345 WP 2002 6 10 2002F00566 1 20020514 A 5320 SPLICE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON SPLICE, AT STRINGER 48R, STATION 1710. (M) 2 L 7 3 4F A22WE 2002061000346 20020610 00346 WP 2002 6 10 2002F00567 1 20020515 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON 'J' LEG FRAME, AT STATION 1781, BETWEEN STRINGER 51L AND 49R. (M) 2 L 7 3 4F A22WE 2002061000347 20020610 00347 WP 2002 6 10 2002F00568 1 20020515 A 5320 PANEL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON BILGE COVER PANEL, AND SUPPORT ANGLE WITH NUT PLATES, BETWEEN LONGERON 43R TO 51L, ON UND ERSIDE AT STATION 1781. (M) 2 L 7 3 4F A22WE 2002061000348 20020610 00348 NM 2002 6 10 UPS02438509 1 20020601 A 5340 SEAT TRACK BOEING 747 747259B 1384804 NM FLIGHT DECK SHEARED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:N/A CAPT SEAT TRACK STOP SHEARED OFF REF D238709 AND M238705 AND REQ A238705 CAPTS SEAT ELECTRICAL C HORD ISNTALLED AND ELECTRIC OPERATION NORMAL AT THIS TIME, THIS CLEARS M238705 R & R'D LH SEAT TRACK ASSY. (CAPT'S) (AFT OTBD) OPS NORMAL AT THIS TIME. THIS CLEARS D238709 2 L 7 4 4F RT A20WE 2002061000349 20020610 00349 NM 2002 6 10 CALA0200330 1 20020607 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 270-294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69348 23586 INSPECTION FOUND SEAT TRACK CORRODED AT STA 270-294, RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002061000350 20020610 00350 NM 2002 6 10 CALA0200332 1 20020608 A 5320 STRAP BOEING 737 7373T0 1384582 NM STA 1006-APB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69348 23586 INSPECTION FOUND R/H SIDE Y STRAP CORRODED FROM STA 1006 TO AFT PRESSURE BULKHEAD, RBL 6. THE STRAP WAS REMOVED AND REPL ACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002061000351 20020610 00351 NM 2002 6 10 CALA0200334 1 20020609 A 5330 SKIN BOEING 737 737524 1384721 NM STA 907 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16647 28908 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 907 BETWEEN S22R AND S23R. REPAIRED IAW SRM 53-00-01, FIGURE 224. 2 L 7 2 4F RT A16WE 2002061300123 20020613 00123 NE 2002 6 13 SABA020068 2 20020604 A 7321 7898426009 ECU DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE NR 1 ENGINE MALFUNCTIONED A SABA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 33 881CC 294 120772 FLIGHT 5047 FROM CLT TO TLH, AFTER ONE HOUR IN FLIGHT THE NUMBER ONE TORQUE STARTED TO SURGE. PILOT CUT-OFF THE ECU AND SURGE WENT AWAY. AIRCRAFT LANDED IN TLH WITH NO OTHER PROBLEMS. NO EMERGENCY WAS DECLARED. ECU WAS DEFERRED TO MSL. AIRCRAFT RETURNED TO CLT. MAINTENANCE REMOVED AND REPLACED THE ECU SYSTEM, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002061300126 20020613 00126 NM 2002 6 13 SPAA0200054 1 20020605 A 5330 6545767 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 48157 22529 PREFLIGHT MAINTENANCE NOTED APPEARANCE OF CRACK IN FUSELAGE SKIN BETWEEN BS 727A AND BS 727B ABOVE THE FLOOR LINE. NDT INSPECTION (EDDY CURRENT) VERIFIED DISCREPANCY TO BE 1 INCH CRACK IN FUSELAGE SKIN ABOVE STRINGER S-16L, FORWARD OF BS 7 27B. AIRCRAFT FERRIED TO REPAIR STATION. ACCOMPLISHED BOEING SERVICE BULLETIN 737-53-1065, PERMANENT SKIN REPAIR PER F IGURE 54. 2 L 7 2 4F A16WE 2002061000352 20020610 00352 NM 2002 6 10 AWXA200200506 1 20020609 A 3350 BMS13311122 WIRE BOEING 737 737277 1384570 NM SEAT ROW 4 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 L/H WAS FOUND INOPERATIVE. MAINTENANCE FOUND THE WIRING UNDER SEAT COMING OUT OF THE SPLICE. RE-SPLICED BROKEN E-PATH WIRE UNDER SEAT ROW 4 L/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002061000353 20020610 00353 NM 2002 6 10 AWXA200200508 1 20020609 A 7500 556115306001 HOSE AIRBUS A319 A319132 3930340 NM #2 ENGINE LEAKING A AWXA K NONE J S WARNING INDICATION AFFECT SYSTEMS CR CRUISE 1 WP 28 817AW 0 0 1373 TUS - DIVERSION - FLT 0179 - WHILE EN ROUTE FROM LAS TO MEX THE #2 ENGINE STARTED A BLEED SURGE, THE X-BLEED VALVE OPENE D AND SURGE CONTINUED IN X-BLEED AUTO WITH BOTH ENGINES SURGING SIMULTANEOUSLY. AUTO THRUST WAS TURNED OFF AND SURGE ON BOTH ENGINES STOPPED FOR APPROXIMATELY 3 TO 4 MINUTES THEN STARTED TO SURGE AGAIN. EPR RANGED FROM 1.20 TO 1.40 DURING S URGES ON BOTH ENGINES, DIVERTED TO TUS AND LANDED WITHOUT EVENT. MAINTENANCE TROUBLESHOT AND FOUND A SENSE LINE LEAKING ON THE #2 ENGINE. REPLACED SENSE LINE AND RAN BOTH THE #1 AND #2 ENGINE AT POWER WITH BLEED PRESSURE STEADY AT 46 PSI AN D NO FLUCTUATION. 2 L 7 2 4F RT A28NM 2002061100001 20020611 00001 SO 2002 6 11 SIMA200213002 1 20020505 A 3350 20131A BATTERY PACK EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 714BZ 145260 BOS - FLT 4527 - AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 4 BATTERY PACK IAW WC NR 33-700-15. OPS CHECK GOOD. (M ) 2 L 7 2 4F RT T00011AT 2002061100002 20020611 00002 SO 2002 6 11 SIMA200213003 1 20020505 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - DURING INSPECTION, FOUND DAMAGED SKIN AT FRAME 12A AND STRINGER 13R. REMOVED DAMAGED SKIN BY CUT OUT. FABRICATED DOUBLER, AND FILLER. REPAIR DONE IAW EMB GST 1420/02-A AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002061100003 20020611 00003 SO 2002 6 11 SIMA200213005 1 20020502 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - DURING INSPECTION, FOUND STRINGER 19L CHAFED. BLENDED CHAFED, FABRICATED TWO DOUBLER ANGLES, AND FOUR SHIMS IAW G ST-1405/02 ITEM 2 AND STANDARD PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002061100004 20020611 00004 SO 2002 6 11 SIMA200213006 1 20020505 A 5311 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - DURING INSPECTION, FOUND DENT WITH GOUGE ON LEFT FUSELAGE AT FRAME 19A-20, BETWEEN STRINGERS 15-16L. REMOVED DAMA GE SKIN BY CUTOUT. INSTALLED DOUBLER IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 1, 53-21-01, EMB GST-1478/02 DATED MAY 4 , 2002 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002061100005 20020611 00005 SO 2002 6 11 SIMA200213007 1 20020502 A 5311 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - DURING INSPECTION, FOUND ELONGATED RIVET HOLE ON RIGHT FORWARD FUSELAGE II, FRAME 12A. INSTALLED OVERSIZED RIVET IAW EMB GST-1368/02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002061100006 20020611 00006 SO 2002 6 11 SIMA200213008 1 20020502 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 DURING INSPECTION, FOUND DENT ON AFT LOWER FUSELAGE AFT OF FRAME 67, BETWEEN STRINGERS 20R AND 21R. REMOVED DAMAGED SKI N BY CUT OUT. FABRICATED A REPAIR DOUBLER, FILLER IAW EMB 145 SRM 145/1142, CHAPTER 53-21-01, EMB GST-1451/02, 2002 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002061100007 20020611 00007 SO 2002 6 11 SIMA200213009 1 20020507 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - DURING INSPECTION, FOUND STRINGER 19R GOUGED. BLENDED GOUGE. FABRICATED A DOUBLER ANGLE, AND TWO SHIMS IAW EMB G ST-1448/02 ITEM 10 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002061100008 20020611 00008 SO 2002 6 11 SIMA200213010 1 20020508 A 5311 12010732001 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - DURING INSPECTION, FOUND FRAME 81 CHAFED ON LOWER EDGE. REPLACED CHAFED FRAME IAW EMB 145 SRM 145/1142 CHAPTER 51 , REV 17, 51-40-02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002061100009 20020611 00009 SO 2002 6 11 SIMA200213011 1 20020507 A 5315 14521721009 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AE 145328 ABI - DURING INSPECTION, FOUND FORWARD DIGITAL CORRODED AT RIVETS AND NUTPLATE BETWEEN FRAME 16 AND 18. REMOVED CORROSI ON BY CUT OUT. REPAIRED IAW EMB 145, SRM 145/1142, CHAPTER 53 REV 17 53-21-10, AND STANDARD SRM PRACTICES. (M) (M) 2 L 7 2 4F RT T00011AT 2002061100010 20020611 00010 EU 2002 6 11 SIMA200213012 1 20020510 A 2121 EVCTA465A FAN SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 245AE 340B245 (FAN) CREW REPORTED THE RIGHT HAND RECIRCULATING FAN LIGHT CAME ON IN FLIGHT ACCOMPANIED BY A SLIGHT SMELL OF SMOKE. C/ A MAINTENANCE REMOVED AND REPLACED THE RIGHT REC. FAN IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2002061100011 20020611 00011 EU 2002 6 11 SIMA200213301 1 20020513 A 2913 4018502 PUMP SAAB SF340 340B 7860101 EU HYD SYSTEM FAILED A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 307AE 340B307 DURING APPROACH WHEN LANDING GEAR WAS EXTENDED CREW RECEIVED HYDRAULIC MESSAGE ON THE CWP ACCOMPANIED BY THE MAIN ACCUMU LATOR FALLING TO ZERO. CREW FOLLOWED EMERGENCY PROCEDURES AND GEAR WAS BLOWN DOWN. AIRCRAFT LANDED WITH NO FURTHER INC IDENTS. C/A MAINTENANCE REMOVED AND REMOVED THE HYDRAULIC PUMP IAW MFG MM. OPERATIONAL AND LEAK CHECK WAS GOOD AND AIR CRAFT WAS RETURNED TO SERVICE. BOTH LEFT AND RIGHT MAIN LANDING GEAR SEPARATION BOLTS WERE REPLACED PRIOR TO RETURN TO SERVICE. 2 L 7 2 4T RT A52EU 2002061100012 20020611 00012 SO 2002 6 11 SIMA200213805 1 20020510 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 DURING AN IMBV MAINTENANCE FOUND CORROSION ON LEFT HAND OMEGA BEAM BETWEEN FRAMES 20 AND 23. REMOVED CORROSION BY BLEND ING. FABRICATED A REPAIR DOUBLER REPAIR DONE IAW SRM. 2 L 7 2 4T RT T00011AT 2002061100013 20020611 00013 SO 2002 6 11 SIMA200213806 1 20020509 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 DURING AN IMBV MAINTENANCE FOUND CARGO DOOR LOWER SILL CORRODED. REMOVED SILL(BEAM). INSTALLED NEW SILL IAW SRM. 2 L 7 2 4T RT T00011AT 2002061100014 20020611 00014 SO 2002 6 11 SIMA200213807 1 20020516 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 DURING AN IMBV MAINTENANCE FOUND STRINGER 19L CHAFED. BLENDED CHAFE. PERFORMED NDT INSPECTION, NO DEFECTS. FABRICATED DOUBLER AND SHIMS. REPAIR DONE IAW SRM. 2 L 7 2 4T RT T00011AT 2002061100015 20020611 00015 SO 2002 6 11 SIMA200213808 1 20020516 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 145LR 6938 DURING AN IMBV MAINTENANCE FOUND STRINGER 19R CHAFED. BLENDED CHAFE. PERFORMED NDT INSPECTION, NO DEFECTS. FABRICATED A DOUBLER AND SHIMS. REPAIR DONE IAW SRM. 2 L 7 2 4T RT T00011AT 2002061100016 20020611 00016 SO 2002 6 11 SIMA200213809 1 20020515 A 5315 14521721007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 DURING AN IMBV MAINTENANCE FOUND CORROSION ON FORWARD DIGITAL. REMOVED CORROSION BY CUT OUT. FABRICATED A REPLACEMENT STRAP, TWO DOUBLERS AND SHIMS. REPAIR DONE IAW SRM. 2 L 7 2 4T RT T00011AT 2002061100017 20020611 00017 SO 2002 6 11 SIMA200213810 1 20020515 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 DURING AN IMBV MAINTENANCE FOUND CORROSION ON GALLEY UNDER FLOOR CENTER BEAM. REMOVED CORRODED GALLEY CENTER BEAM. INS TALLED NEW CENTER BEAM IAW SRM. 2 L 7 2 4T RT T00011AT 2002061100018 20020611 00018 SO 2002 6 11 SIMA200213811 1 20020515 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 727AE 145326 DURING AN MBV MAINTENANCE FOUND CORROSION ON LEFT HAND OMEGA BEAM AT FRAME 20 REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, FILLERS AND SHIMS. REPAIR DONE, IAW MFG SRM. 2 L 7 2 4F RT T00011AT 2002061100019 20020611 00019 EU 2002 6 11 SIMA200213812 1 20020510 A 5512 SKIN SAAB SF340 340B 7860101 EU HORIZ STAB DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AE 340B348 LEFT HAND HORIZONTAL STABILIZER FORWARD SPAR HAS TWO OVERSIZED HOLES, UPPER SKIN PANEL. PERFORMED AN NDT INSPECTION, NO DEFECTS NOTED. INSTALLED FASTENERS WET, DONE IAW MFG SRM. 2 L 7 2 4T RT A52EU 2002061100020 20020611 00020 EU 2002 6 11 SIMA200213815 1 20020518 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY FAILED A SIMA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 278AE 340B278 CREW REPORTED THE AVIONICS SMOKE LIGHT ON CWP ILLUMINATED IN FLIGHT. STAYED ON ABOUT 10 MINUTES. CREW DECLARED EMERGEN CY, LANDED AIRCRAFT WITH NO FURTHER INCIDENTS. C/A MAINTENANCE REMOVED AND REPLACED THE AVIONICS RACK SMOKE DETECTOR I AW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2002061100021 20020611 00021 NE 2002 6 11 SIMA200213816 2 20020518 A 7200 CT79B ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 2 FAILED A SIMA O OTHER O OTHER CL CLIMB 1 SW 21 374AE 340B374 CREW REPORTED AT 500-600 FT JUST AFTER CTOT ROTATION, 60-70 PERCENT ON CTOT, AND 80-85 TORQUE, THE NUMBER 2 ENGINE FAILE D. C/A MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE IAW WORK CARD 4903. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2002061100022 20020611 00022 EU 2002 6 11 SIMA200214001 1 20020520 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 356SB 340B356 DURING PREFLIGHT CREW REPORTED EMERGENCY OVERHEAD LIGHTS IN 7A, 8BC AND 10BC TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY LIGHT POWER SUPPLY UNIT IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 2 4T RT A52EU 2002061100023 20020611 00023 EU 2002 6 11 SIMA200214119 1 20020521 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 356SB 340B356 CREW REPORTED THE OVERHEAD EMERGENCY LIGHT AT 7A, 8C, AND 10C TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT 22LN IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2002061100024 20020611 00024 EU 2002 6 11 SIMA3881161 1 20020426 A 7712 10225N1W00 INDICATOR SAAB SF340 340B 7860101 EU COCKPIT FAILED A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 388AE 340B388 LOST RIGHT TORQUE INDICATION ON TAKEOFF/ ABORTED TAKEOFF NOTIFICATION WAS VIA TELLISIS FROM FLT CREW- C/A RIA RT TORQUE INDICATOR WITH SERVICEABLE TORQUE INDICATOR. OPS CHECK GOOD IAW MFG AMM. 2 L 7 2 4T RT A52EU 2002061100025 20020611 00025 WP 2002 6 11 2002F00569 1 20020515 A 5347 CARGO TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON THE LOWER SURFACE OF INBOARD FLANGE OF THE CARGO ROLLER TRACK, AT STATION 1701 RBL 26. ( M) 2 L 7 3 4F A22WE 2002061100026 20020611 00026 EU 2002 6 11 A6WA200260004 1 20020522 A 5330 SKIN BAC 146 146300A 1500267 EU FUSELAGE DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 DENT IN A VERTICAL DIRECTION AT STRINGER 26L BETWEEN FRAME 12 AND 13. FABRICATED A REPAIR PATCH. PERFORMED A DETAILED VISUAL INSPECTION TO ENSURE SOUND CRACK FREE STRUCTURE REMAINS. 2 H 7 4 4F RT A49EU 2002061100027 20020611 00027 EU 2002 6 11 A6WA200260009 1 20020522 A 5320 ATTACH ANGLE BAC 146 146300A 1500267 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 FLOOR BEAM TO CROSSMEMBER ATTACH ANGLE CRACKED AT STA 183.15 FORWARD SIDE AND LBL 47 OUTBOARD SIDE. CROSSMEMBER ATTACH ANGLE REPLACED IAW SRM. 2 H 7 4 4F RT A49EU 2002061100028 20020611 00028 EU 2002 6 11 A6WA200260011 1 20020522 A 5730 PANEL BAC 146 146300A 1500267 EU RT WING DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 DENTS FOUND IN LEFT AND RIGHT WINGS TRAILING EDGE PANELS BETWEEN RIB 14A AND 15B. INSPECTION CARRIED OUT IAW MFG MM. 2 H 7 4 4F RT A49EU 2002061100029 20020611 00029 EU 2002 6 11 A6WA200260012 1 20020522 A 5755 BRACKET BAC 146 146300A 1500267 EU LT SPOILER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 LEFT INBOARD SPOILER OUTBOARD END BRACKET CRACKED AT FORWARD TOP EDGE. CARRIED OUT IAW MFG NWH/RJ/0723-02. 2 H 7 4 4F RT A49EU 2002061100030 20020611 00030 EU 2002 6 11 A6WA200260013 1 20020522 A 5752 TRIM TAB BAC 146 146300A 1500267 EU LT AILERON DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 DENTS FOUND IN LEFT AILERON TRIM TAB. INSPECTION CARRIED OUT IAW MM. 2 H 7 4 4F RT A49EU 2002061100031 20020611 00031 EU 2002 6 11 A6WA200260015 1 20020523 A 5753 BEAM BAC 146 146200A 1500266 EU T/E FLAP DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 WEAR DAMAGE TO RIGHT NR 4 FLAP TRACK UPPER BEAM. AREA OF DAMAGE BLENDED AND POLISHED TO A SMOOTH MIRROR FINISH. MAINTE NANCE ENSURED A BLEMISH FREE BLEND WITHOUT INCREASE TO THE REPORTED DEPTH. PERFORMED A DV INSPECTION TO ENSURE A SOUND CRACK FREE STRUCTURE REMAINS. 2 H 7 4 4F A49EU 2002061100032 20020611 00032 EU 2002 6 11 A6WA200260016 1 20020523 A 5754 PANEL BAC 146 146200A 1500266 EU L/E FLAP CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 CRACK IN UPPER LANDING ANGLE OF LEFT FLAP LEADING EDGE ACCESS PANEL BETWEEN STATION WRX 311.4 AND WRX 323.0. FABRICATED A REPAIR STRIP. REPAIRED IAW MFG. 2 H 7 4 4F A49EU 2002061100033 20020611 00033 EU 2002 6 11 A6WA200260017 1 20020523 A 5753 TAB BAC 146 146200A 1500266 EU T/E FLAP WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 6 WEAR SPOTS, OUT OF LIMITS ON RIGHT INBOARD FLAP TAB, ALL AREAS OF DAMAGE BLENDED AND SMOOTHED TO A MIRROR FINISH. EN SURED A BLEMISH FREE BLEND WITHOUT INCREASE TO THE REPORTED DEPTH. PERFORMED A DV INSPECTION TO ENSURE A SOUND CRACK FR EE STRUCTURE REMAINS. 2 H 7 4 4F A49EU 2002061100034 20020611 00034 EU 2002 6 11 A6WA200260018 1 20020528 A 5230 DOOR BAC 146 146200A 1500266 EU CARGO DOOR OUT OF RIG A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 FORWARD CARGO DOOR UNABLE TO RIG THE DOOR INTO LIMITS AS PER MFG MM, ALLOWING AIRCRAFT TO REMAIN IN SERVICE FOR 500 CYCL ES. 2 H 7 4 4F A49EU 2002061100035 20020611 00035 NM 2002 6 11 GAIA02045ST 1 20020429 A 5524 ANGLE BOEING 727 727243 138408D NM ELEVATOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 1269Y 21269 DURING A CPCP INSPECTION, IT WAS DISCOVERED THAT RIGHT ELEVATOR INTERIOR Z ANGLE IS CRACKED AT ELEVATOR STATION 25. ACC OMPLISHED ELEVATOR Z ANGLE REPLACEMENT AT RIGHT ELEVATOR STATION 25.0 IAW SRM. 2 L 7 3 4F RT A3WE 2002061100036 20020611 00036 NM 2002 6 11 GAIA02046ST 1 20020429 A 5524 ANGLE BOEING 727 727243 138408D NM ELEVATOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 1269Y 21269 DURING A CPCP INSPECTION, IT WAS DISCOVERED THAT LEFT ELEVATOR INTERIOR Z ANGLE IS CRACKED AT ELEVATOR STATION 20.0. AC COMPLISHED ELEVATOR Z ANGLE REPLACEMENT AT LEFT ELEVATOR STATION 20.0 IAW SRM. 2 L 7 3 4F RT A3WE 2002061100037 20020611 00037 NM 2002 6 11 GAIA02047ST 1 20020429 A 5730 SKIN BOEING 727 727243 138408D NM WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 1269Y 21269 DURING A CPCP INSPECTION, IT WAS DISCOVERED THAT THE PLENUM AREA ABOVE LEFT PRIMARY HEAT EXCHANGER IS CORRODED. ACCOMPL ISHED WING CENTER SECTION LOWER SKIN REPAIR ABOVE THE LEFT PRIMARY HEAT EXCHANGER IAW SRM. 2 L 7 3 4F RT A3WE 2002061100038 20020611 00038 NM 2002 6 11 GAIA02048OP 1 20020430 A 3350 1000077 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 854AA 20995 DURING PERIODIC SERVICE CHECK MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTING OVER THE LEFT NUMBER 1 DOOR INOPERATIVE. MA INTENANCE REMOVED AND REPLACED THE UNSERVICEABLE LIGHT ASSEMBLY. OPERATIONAL CHECK PERFORMED OKAY. AIRCRAFT WAS RETURN ED TOO SERVICE. 2 L 7 3 4F A3WE 2002061100041 20020611 00041 NM 2002 6 11 GAIA2002F0000 1 20020508 A 3610 540998 DUCT BOEING 727 727222 1384073 NM NR 3 ENGINE BLOWN A GAIA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 07 180AX 20041 AFTER TAKEOFF, THE NR 3 FIRE WARNING CAME ON. THE CREW DECLARED AN EMERGENCY, SHUT DOWN NR 3 ENGINE AND THE WARNING LIG HT EXTINGUISHED. THE FLIGHT RETURNED TO AIRPORT AND LANDED UNEVENTFULLY. MAINTENANCE FOUND THE 13TH STAGE DUCT FROM TH E PRBC AND FUEL HEAT DUCT BLOWN OUT. REMOVED AND REPLACED THE DUCT. OPS CHECKED GOOD. A/C RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2002061100043 20020611 00043 NM 2002 6 11 AWXA200200504 1 20020608 A 3350 20131A BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 327AW 23507 PHX - EEL - R-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BA TTERY PACK, OPERATIONAL CHECK WAS GOOD IAW T/C A1C33009. 2 L 7 2 4F RT A16WE 2002073000020 20020730 00020 EU 2002 7 30 AWXA200200505 1 20020608 A 2934 C60AA0062 SWITCH AIRBUS 320 A320232 3930326 EU COCKPIT ERRATIC A AWXA O OTHER J WARNING INDICATION DE DESCENT 1 WP 28 640AW 31225 448 PHX - EMERGENCY LANDING - FLT 0612 - ON DESCENT INTO PHX EN ROUTE FROM YVR ECAM INDICATED GREEN HYDRAULIC SYSTEM RESERVO IR LOW QUANTITY INDICATION. MAINTENANCE TROUBLESHOT AND FOUND FLUID LEVEL NORMAL, INDICATION PROBLEM ONLY. REPLACED GR EEN HYDRAULIC LOW LEVEL SWITCH, OPERATIONAL CHECK WAS GOOD IAW AMM 29-31-00-51. **SUPP** VENDOR TEARDOWN OF LOW LEVEL SWITCH S/N 986 CONFIRMED FAILURE OF UNIT, SWITCH WAS SCRAPPED NO OTHER INFORMATION AVAILABLE. 2 L 7 2 4F RT A28NM 2002061100044 20020611 00044 NM 2002 6 11 AWXA200200507 1 20020609 A 3350 1012623 LIGHT BOEING 737 737301 1384611 NM CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 SNA - EEL - FLT 0267 - FLIGHT CREW REPORTED THAT EMERGENCY ESCAPE PATH LIGHT ON SEAT ROW 10 LT CAME OFF. MAINTENANCE RE MOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 10 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002061100045 20020611 00045 NM 2002 6 11 AWXA200200509 1 20020609 A 7603 THROTTLE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 ENGINE MALFUNCTIONED A AWXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 28 332AW 23384 725441 TUS - ABORTED TAKEOFF - FLT 0673 - WHILE PREPARING FOR TAKEOFF AT TUS EN ROUTE FOR PHX WHEN THRUST WAS APPLIED A LAG WAS EXPERIENCED IN THE NR 2 ENGINE. TAXIED OFF RUNWAY AND PERFORMED TWO MORE THROTTLE ADVANCES TO POWER WITH NO LAG EXPERI ENCED. CONTACTED MOC AND DEPARTED TOWARD SCHEDULED DESTINATION. 2 L 7 2 4F 4 F RT A16WE E21EU 2002061100051 20020611 00051 EU 2002 6 11 A1U2002F00003 1 20020418 A 6310 4639302044 SPRAG CLUTCH BOLKMS 117 BK117B1 5626012 EU ENGINE DAMAGED A A1UA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 770SL 299 S7135 (CLUTCH) DURING CRUISE FLIGHT NR 1 ENGINE NR 2 WERE NORMAL. NR 1 TORQUE DROPPED TO 25 PERCENT. RESIDUAL TORQUE REMAINE D AS NR 1 WAS BROUGHT TO IDLE. NR 1 ENGINE SECURED TO IDLE, RUN ON LANDING PERFORMED TO CGI. DURING TROUBLESHOOTING OF AIRCRAFT, REMOVED NR 1 CLUTCH. FOUND SPRAGS DISCOLORED, (BLUE TINT). INSTALLED SERVICEABLE CLUTCH, PERFORMED GROUND R UN AND MAINTENANCE CHECK FLIGHT. AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U H13EU 2002061100052 20020611 00052 2002 6 11 AHE02052 4 20020326 A 2297 065001580502 WIRE DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE AUTOFLIGHT LOOSE B E8UY O OTHER O OTHER NR NOT REPORTED 1 EA 35 92001 1380 90000040 BA0003 AUTO-PILOT COMPUTER - INSPECTION FOR WIRE CHAFING ON REMOVAL OF THE AUTO-PILOT COMPUTER. SOME CABLES WERE FOUND LOOSE UNDER CONSOLE CB PANEL. THE AUTO-PILOT CABLE BUNDLE HAD CHAFED AGAINST THE AP COMPUTER SECURING SCREWS. ACTION TAKEN: LOOSE CABLES SECURED UNDER THE CB PANEL, HEAT SHRINK COVER HAS BEEN APPLIED AROUND THE CABLE BUNDLE TO PREVENT FURTHER DESCRIPTION/CONTACT WITH STATED SCREWS ON AP COMPUTER. 1 G 7 2 3U 3 U NC H19NM E42NE 2002061100053 20020611 00053 NE 2002 6 11 C1HA200296015 2 20020608 A 7230 COMPRESSOR BOEING 727 7272J4 1384006 NM PWA JT8 JT8D17 52049 NE ENGINE STALLED A C1HA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 15 696CA 22574 ON TAKEOFF IN LAS HAD COMPRESSOR STALL, PULLED OFF RUNWAY CALLED MX CONTROL. RAN UP ENGINE, ALL ENGINE PARAMETERS NORMA L. INSPECTED ALL ENGINES AND NO DEFECTS FOUND. RAN ENGINES AT TAKEOFF POWER. ALL PARAMETERS NORMAL. OK FOR SERVICE P ER M/M 71-00. 2 L 7 3 4F 4 F RT A3WE E2EA 2002061100054 20020611 00054 2002 6 11 AHE02056 4 20020422 A 2297 065001580502 WIRE DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE AUTOFLIGHT FAILED B E8UY K NONE O OTHER IN INSP/MAINT 1 EA 35 92001 1406 90000040 AIRCRAFT ARRIVED AT DENHAM FOR MAIN ROTOR TRACK AND BALANCE. THE AUTO PILOT DISCONNECT CIRCUIT BREAKER ON CENTER CONSOL E WAS FOUND TO KEEP POPPING WHEN POWER WAS APPLIED, WHICH DISABLES THE WHOLE AUTO PILOT SYSTEM. FAULT INVESTIGATION WAS CARRIED OUT AND REVEALED THAT A WIRE FROM PIN 9 OF PLUG J142 WHICH CONNECTS TO PIN 8 OF PLUG J143 WAS CHAFED ON A P CL IP LOCKING NUT AMONG CONTROL RODS UNDERNEATH PILOTS SEAT. THIS WIRE WAS REPAIRED AND BUNDLED WITH THE MAIN LOOM THROUGH THE P CLIP. FULL FUNCTION CHECKS WERE CARRIED OUT AND FOUND SATISFACTORY. 1 G 7 2 3U 3 U NC H19NM E42NE 2002061100055 20020611 00055 SO 2002 6 11 C2XA02CL127 1 20020605 A 3232 21180100401 ACTUATOR EMB 145 EMB145LR 3260212 SO NLG LEAKING A C2XA K NONE J WARNING INDICATION DE DESCENT 1 SW 27 29906 1733 145472 CLE FLIGHT 3998 THE CREW REPORTED A LANDING AIR/GND FAIL MESSAGE WHEN EXTENDING THE LANDING GEAR AND STAYS ON UNTIL GEAR IS DOWN AND LOCKED. MAINTENANCE REPLACED THE LEFT NOSE LANDING GEAR DOOR ACTUATOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002061100056 20020611 00056 GL 2002 6 11 ALG2002F00035 2 20020512 A 7210 6895007 BEARING ALLSN BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TM BEARING GALLED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 577AL 682 CAG47062 53247 CAE847251 ENGINE WAS REMOVED DUE TO CHIP LIGHT. GEARBOX WAS DISASSEMBLED TO FIND SOURCE OF METAL. UPON REMOVAL OF T/M JOURNAL AN D INNER RACE FOUND EXCESSIVE GALLING, CAUSING METAL CONTAMINATION. ASSURE BEARINGS AND INNER RACE CAN WITH STAND HIGH L OADING CAPACITY. 1 G 7 1 3U 3 U O H2SW E1GL 2002061100057 20020611 00057 SO 2002 6 11 C2XA02CL128 1 20020607 A 3350 CONNECTOR EMB 145 EMB145ER 3260211 SO CABIN LOOSE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 14945 145049 CLE FLIGHT 3015 THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT THE MAIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED THE CONNECTOR AT THE SIGN. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002061100058 20020611 00058 SW 2002 6 11 ALG2002F00036 1 20020501 A 5320 206064213191 FLOOR SUPPORT BELL 407 407 1182206 SW ALLSN 250C 250C20 03013 GL FUSELAGE CRACKED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 497AL 53172 DURING MAJOR INSPECTION, SEVERE CORROSION AT ALL MATING SURFACES AND ENDS OF ALL STIFFENING STRINGERS CRACKED. ALL MOUN TING FLANGES CRACKED AND CORRODED. USE PROSEAL AND PRIME THE PARTS AFTER ASSEMBLY, INSTALL DOUBLER AROUND WATER WASH FI TTING TO PREVENT CRACKING. 1 G 7 1 3U 3 U O H2SW E4CE 2002061100059 20020611 00059 GL 2002 6 11 ALG2002F00037 2 20020430 A 7210 23071895 GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX SPALLED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 497AL 485 53172 GEARBOX WAS RECEIVED FOR CORRODED STUDS. UPON INITIAL VISUAL INSPECTION FOUND SPALLING PINION GEAR TEETH. EXCESSIVE SP ALLING AND LIGHT GALLING ON GEAR TEETH DUE TO IMPROPER MESHING OF TM AND PINION GEARS. ASSURE PROPER MESHING OF GEAR TE ETH AT FACTORY. 1 G 7 1 3U 3 U O H2SW E1GL 2002061100060 20020611 00060 SW 2002 6 11 ALG2002F00038 1 20020430 A 6510 407340339101 BEARING BELL 407 407 1182206 SW T/R DRIVESHAFT FAILED B ALGR A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 SW 03 617AL 53265 IN FLIGHT AIRCRAFT DEVELOPED EXCESSIVE VIBRATION. BEARING FAILURE. (THE BEARING WAS LUBRICATED AT AIRCRAFT TT 2920.31. ) 1 G 7 1 3U O H2SW 2002061100061 20020611 00061 SO 2002 6 11 C2XA02CL129 1 20020607 A 3260 23092900001 UPLOCK EMB 145 EMB145ER 3260211 SO RT MLG FAULTY A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 15948 9330 145056 CLE FLIGHT 3214 THE CREW REPORTED A RIGHT MAIN LANDING GEAR/LEVER DISAGREE. THE RIGHT MAIN INDICATES DOWN WITH THE HAND LE UP. THE SYSTEM RESET AFTER CYCLING. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MAIN GEAR UPLOCK BOX ASSEMBLY. OP ERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002061100062 20020611 00062 SW 2002 6 11 AO52002F00000 1 20020510 A 3212 407050202101 FLOAT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MLG CORRODED A A05A K NONE O OTHER IN INSP/MAINT 1 SW 03 973AA 53167 FLOAT WAS INSPECTED, AND WAS DETERMINED TO BE EXTREMELY CORRODED AND IN AN IMMANENT FAILURE CONDITION. 1 G 7 1 3U 3 U O H2SW E1GL 2002061100063 20020611 00063 EU 2002 6 11 KBM2002F00000 1 20020417 A 6420 BEARING SNIAS 350 AS350B1 8680811 EU T/R HINGE WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 5898 2009 BEARINGS WORN BEYOND LIMITS. REPLACED WITH NEW BEARINGS. 1 G 7 1 3U H9EU 2002061100064 20020611 00064 2002 6 11 CALA0200329 4 20020607 A 2565 BOTTLE BOEING 737 737524 1384721 NM EVAC SLIDE DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16632 22263 27900 THE R1 DOOR SLIDE BOTTLE PRESSURE WAS FOUND AT ZERO DURING SLIDE INSPECTION. THE R1 DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-60-10. 2 L 7 2 4F RT A16WE 2002061100065 20020611 00065 NM 2002 6 11 CALA0200331 1 20020607 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69348 23586 INSPECTION FOUND FLOOR SUPPORT UNDER R2 DOOR Z-ANGLE AT STA 969 CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IA W SRM 51-10-02, 51-40-02, AND 51-30-01. 2 L 7 2 4F RT A16WE 2002061100066 20020611 00066 WP 2002 6 11 CALA0200333 1 20020608 A 5350 CABLE DOUG DC9 DC982 3022082 WP TAILCONE OUT OF RIG A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 83872 49120 THE TAIL CONE DID NOT DROP WHEN USING AFT CABIN DOOR TAIL CONE EMERGENCY RELEASE. THE TAIL CONE CABLES WERE ADJUSTED IA W MM 53-53-00. 2 L 7 2 4F A6WE 2002061100067 20020611 00067 NM 2002 6 11 DHL2002708008 1 20020608 A 2612 FIRE LOOP BOEING 727 72725 1384006 NM NR 1 ENGINE OUT OF POSITION A DHLA K NONE N FALSE WARNING UK UNKNOWN 1 SO 01 708DH 18275 NR 1 FIRE PROTECTION DETECTOR LIGHT ON. REPOSITIONED FIRE LOOP NR 1 ENG, OPS CHECKED GOOD IAW M/M 26-11-00. 2 L 7 3 4F A3WE 2002061100068 20020611 00068 WP 2002 6 11 DHL2002802513 1 20020529 A 5320 27090861 CLIP DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 MAIN CARGO COMPT CLIP CRACKED 1/2 IN L-17 LT. PERFORMED MAJOR REPAIR PER ATM EO 111576 DWG 2709086 AND EO 2002606. REM OVED CLIP PER SRM 51-1-30D. FABRICATED NEW CLIP PER SRM 51-1-2B. INSTALLED NEW CLIP PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002061100069 20020611 00069 2002 6 11 KBMA113813 4 20020414 A 3416 066011560101 TRANSPONDER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ALTIMETER INTERMITTENT E K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 3296 ALTIMETER TRANSPONDER, INTERMITTENT. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2002061100070 20020611 00070 EU 2002 6 11 KBMA113814 1 20020410 A 2110 590008 COMPRESSOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE AIR CONDITIONER FAULTY E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 2337 A/C COMPRESSOR REPORTED TO BE FAULTY. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002061100071 20020611 00071 EU 2002 6 11 KBMA113815 1 20020417 A 6420 350A33215300 BEARING SNIAS 350 AS350B1 8680811 EU T/R HING LAM WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 5898 2009 BEARINGS WORN BEYOND LIMITS. REPLACED WITH NEW BEARINGS. 1 G 7 1 3U H9EU 2002061100072 20020611 00072 EU 2002 6 11 KBMA113816 1 20020419 A 6420 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TEETER BRGS WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 667 3296 BEARINGS WORN BEYOND LIMITS. REMOVED AND REPLACED WITH NEW. 1 G 7 1 3U 3 U H9EU E19EU 2002061100073 20020611 00073 EU 2002 6 11 KBMA113823 1 20020429 A 8011 524031 STARTER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE FAILED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 11 3296 STARTER WILL NOT ENGAGE. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2002061100074 20020611 00074 WP 2002 6 11 DHL2002802514 1 20020530 A 5712 FORMER DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 LEFT WING CTR L/E FORMER WITH CRACK AT STA XFS 335.000. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED DOUBLER PER SRM 5702-0 PG 9-10. INSTALLED DOUBLER PER SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002061100075 20020611 00075 NE 2002 6 11 KBMA113824 2 20020502 A 7420 IGNITION LEAD SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 2273A 300 2273 IGNITION LEADS, WORN. REPLACED WITH SERVICEABLE LEADS. 1 G 7 1 3U 3 U NC H9EU E19EU 2002061100076 20020611 00076 WP 2002 6 11 DHL2002802515 1 20020528 A 5730 SKIN DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 LT EXHAUST GATE UPPER SKIN WITH .75 INCH CRACK AT STA XF.277.000. PERFORMED MAJOR REPAIR PER SRM 57-2-5 FIG 1. REMOVED DAMAGED UPPER SKIN PER SRM 57-2-5 FIG 1. FABRICATED NEW SKIN PER SRM 57-2-5 FIG 1. INSTALLED NEW SKIN PER SRM 57-2-5 FIG 1. 2 L 7 4 4F RT 4A25 2002061100077 20020611 00077 EU 2002 6 11 KBMA113825 1 20020507 A 6510 BUSHING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE COUPLING WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 5785 2957 FORWARD COUPLING DISC ASSEMBLY, BUSHING WAS WORN OUT. REMOVED AND REPLACED WITH A NEW DISC ASSEMBLY. 1 G 7 1 3U 3 U NC H9EU E19EU 2002061100078 20020611 00078 EU 2002 6 11 KBMA113826 1 20020507 A 3610 0301027300 LINE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE P2 AIR LINE WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 5785 2957 P2 LINE WAS WORN BEYOND LIMIT. REPLACED WITH NEW P2 LINE. 1 G 7 1 3U 3 U NC H9EU E19EU 2002061100079 20020611 00079 WP 2002 6 11 DHL2002802516 1 20020525 A 5320 SPLICE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 AFT ACCESSORY COMPARTMENT SPLICE ANGLE WITH 2 INCH CRACK AT STA 1640.000 L-25L TO L26L. REMOVED DAMAGED SPLICE ANGLE PE R SRM 51-1-20D PG 21. FABRICATED NEW SPLICE ANGLE PER SRM 53-2-0 FIG 1B. INSTALLED NEW SPLICE ANGLE PER SRM 53-2-0 FIG 2B AND SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002061100080 20020611 00080 GL 2002 6 11 LCF2002F00000 2 20020520 A 7230 BEARING BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL COMPRESSOR SEIZED E LCFA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 5007F 10769 45186 PILOT ATTEMPTED TO START ENGINE WITH NO ROTATION NOTED. AFTER TROUBLESHOOTING START SYSTEM COMPRESSOR WAS FOUND TO BE S IEZED. COMPRESSOR WAS REMOVED AND STILL NOT ABLE TO ROTATE. NO METAL CONTAMINATION FOUND TO SUGGEST BEARING FAILURE. AXIAL COMPRESSOR DOES NOT APPEAR TO HAVE SHIFTED. 1 G 7 1 3U 3 U H2SW E1GL 2002061100081 20020611 00081 EU 2002 6 11 RCO2002F00000 1 20020523 A 6730 355A2700720001 LEVER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE T/R SERVO CNTL SEIZED A RC0R K NONE O OTHER IN INSP/MAINT 1 SW 17 4035W 3267 2912 DURING A SCHEDULED PHASE INSPECTION, WE ARE TO BE LOOKING FOR A HOLE THAT IS WORN OUT OF ROUND ON THE YAW CONTROL COMPEN SATOR LEVER. WHEN THE CONTROL WAS REMOVED IT WAS FOUND THAT THE BEARING HAD FROZEN. THE BEARIING STILL HAD MOVEMENT IN THE SMALL RANGE IT USES TO ACTUATE 30 DEGREES. BUT THE REST WAS IMMOBILE. THERE IS NO PROCEDURE FOR REMOVING AND REPL ACING OF THIS BEARING, SO THE COMPLETE UNIT HAS TO BE REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2002061100082 20020611 00082 WP 2002 6 11 DHL2002802517 1 20020528 A 5230 SKIN DOUG DC8 DC873 302199C WP CARGO DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C BELLY DOOR INTERIM REPAIR AND LOWER EXTERNAL SKIN EDGE WORN BETWEEN STA 1204.000 AND STA 1258. PERFORMED MAJOR REPAIR TRIMMED OUT THE DAMAGED SKIN SEGMENT PER EO DHL 020503 EO-3048 EO SEMAN 2002570. FABRICATED A NEW SKIN SEGMENT AND A D OUBLER SPLICE PER EO DHL 020503 EO-3048 EO SEMAN 2002570. INSTALLED NEW SKIN, SPLICE AND DOUBLER PER EO DHL 020503 EO-3 048 EO SEMAN 2002570. 2 L 7 4 4F RT 4A25 2002061100083 20020611 00083 WP 2002 6 11 DHL2002802518 1 20020526 A 5522 SKIN DOUG DC8 DC873 302199C WP ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 LT ELEVATOR LWR EXTERNAL SKIN (STA XAR 0 TO XE 132.000) DEFLECTED AND WITH IMPROPER RIVETS. PERFORMED MAJOR REPAIR PER EO DHL 020501 EO 3013 EO SEMAN 2002564. REMOVED DAMAGED SKIN PER EO DHL 020501 EO 3013 EO SEMAN 2002564. FABRICATED NE W SKIN PER EO DHL 020501 EO 3013 EO SEMAN 2002564. 2 L 7 4 4F RT 4A25 2002061100084 20020611 00084 WP 2002 6 11 DHL2002802519 1 20020530 A 5712 FORMER DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 LEFT WING O/B LEADING EDGE FORMER WITH .5 INCH CRACK AT STA XFS 635.000. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED DOUBLER PER SRM 57-2-0 PG 9-10. INSTALLED DOUBLER PER SRM 57-2-0 PG 9 -10 AND SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002061100085 20020611 00085 WP 2002 6 11 DHL2002802520 1 20020530 A 5712 FORMER DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 RIGHT WING O/B LEADING EDGE FORMER WITH .25 INCH CRACK AT STA XFS 672.500. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STO P DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED DOUBLER PER SRM 57-2-0 PG 9-10. INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002061100086 20020611 00086 WP 2002 6 11 DHL2002802521 1 20020530 A 5311 FRAME DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 LEFT MLG W/W FORMER CRACKED 2 INCHES AT STA 930.000 LBL 63. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1B. FABRICATED DOUBL ER PER SRM 53-2-0 FIG 1B. INSTALLED DOUBLER PER SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2002061100087 20020611 00087 EA 2002 6 11 COMA0260358 1 20020606 A 3230 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 975CA 13711 7150 FLIGHT 5882 GEAR DISAGREE WARNING, NLG DID NOT EXTEND - USED MANUAL EXTENSION.REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002061100088 20020611 00088 WP 2002 6 11 DHL2002802522 1 20020518 A 5230 DOOR FRAME DOUG DC8 DC873 302199C WP CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 B BELLY DOOR FRAME WITH 1 INCH CRACK AT LT UPPER CORNER AT STA 560.000. PERFORMED MAJOR REPAIR PER SRM 52-20 FIG 2 SHEE T 4. STOP DRILLED CRACK PER SRM 52-2-0 FIG 2 SHEET 4. FABRICATED REINFORCING ANGLE PER SRM 52-2-0 FIG 2 SHEET 4. INST ALLED NEW ANGLE PER SRM 52-2-0 FIG 2 SHEET 4 AND SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002061100089 20020611 00089 WP 2002 6 11 DHL2002802523 1 20020528 A 5230 SKIN DOUG DC8 DC873 302199C WP CARGO DOOR WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 A BELLY DOOR EXTERNAL LWR SKIN WORN AND SHOWS DENTS. PERFORMED MAJOR REPAIR PER SRM 52-4-1 PG 3. REMOVED DETERIORATED EXTERNAL SKIN PER SRM 51-1-2 PG 1. FABRICATED NEW SKIN PER SRM 52-4-1 PG 3. CLEANED, TREATED AND PRIMED NEW SKIN PER S RM 51-1-8B. INSTALLED NEW SKIN PER SRM 52-4-1 PG 3 AND SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002061100090 20020611 00090 WP 2002 6 11 DHL2002802524 1 20020528 A 5320 37542201 SPLICE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 FWD CARGO COMPT SPLICE FITTING WITH 4 INCH CRACK AT STA 200.000-220.000 L-31-L. PERFORMED MAJOR REPAIR PER ATM PO111585 DWG 3754220, EA SEMAN 2002601. REMOVED DAMAGED SPLICE FITTING PER SRM 51-1-20D PG 21. FABRICATED NEW SPLICE PER ATM P O111585 DWG 3754220, EA SEMAN 2002601. INSTALLED NEW SPLICE FITTING PER ATM PO111585 DWG 3754220, EA SEMAN 2002601. 2 L 7 4 4F RT 4A25 2002061100091 20020611 00091 WP 2002 6 11 DHL2002802525 1 20020526 A 5522 SKIN DOUG DC8 DC873 302199C WP ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 LT ELEVATOR TOP SURFACE WITH TEMP REPAIR AT STA XE 185.2013. PERFORMED MAJOR REPAIR PER EO DHL 020505 EO 3045 EO SEMAN 2002566. TRIMMED OUT DAMAGED AREA PER EO DHL 020505 EO 3045 EO SEMAN 2002566. FABRICATED REPAIR DOUBLER PER AND A FILL ER PER EO DHL 020505 EO 3045 EO SEMAN 2002566. INSTALLED FILLER AND DOUBLER PER EO DHL 020505 EO 3045 EO SEMAN 2002566. 2 L 7 4 4F RT 4A25 2002061100092 20020611 00092 WP 2002 6 11 DHL2002802526 1 20020529 A 5320 SPLICE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 FWD CARGO COMPT SPLICE FITTING WITH 2 INCH CRACK AT STA 440.000-460.000 L-31L. PERFORMED MAJOR REPAIR PER ATM R0111585 DWG 3754220 AND EA SEMAN 2002600. REMOVED DAMAGED SPLICE FITTING PER SRM 51-1-20D PG 21. FABRICATED NEW SPLICE FITTING PER ATM R0111585 DWG 3754220 AND EA SEMAN 2002600. INSTALLED NEW SPLICE FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002061100093 20020611 00093 WP 2002 6 11 MWEA020404 1 20020429 A 5310 5912995504 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 RIGHT FORWARD OVERWING EXIT DOOR JAMB HAS GOUGES AT TOP DOOR LATCH AREA. LOCATED AND DRILLED REPAIR ANGLE AND MODIFIED EXISTING SEAL DEPRESSOR. INSTALLED REPAIR ANGLE AND SEAL REINSTALLED DEPRESSOR. 2 L 7 2 4F A6WE 2002061100094 20020611 00094 NM 2002 6 11 P5CA0200681 1 20020601 A 5420 WEB BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 702066 CRACK 8 INCHES LONG FOUND NR 2 ENG PYLON FORWARD LOWER SPAR FLOOR WEB AT STA 270, MID SPAR (PANEL 452CL). COMPLETED REP AIRS IAW BOEING REPAIR SCHEME DWGS PAO-LGB-02-00056F, 55F, 54H, 53F & 52H. 2 L 7 4 4F 4 F A20WE E3NE 2002061100095 20020611 00095 EA 2002 6 11 COMA0260359 1 20020606 A 2710 SHIELD CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 937CA 7044 FLIGHT 6000 A/P LWD CAUTION MESSAGE. AILERON CONTROL FORCE VERY STIFF.ADJUSTED THE WHEEL BIN SPLASH GUARDS - NO OTHER DE FECTS NOTED. 2 L 7 2 4F RT A21EA 2002061100096 20020611 00096 NM 2002 6 11 PCAA0205058 1 20020516 A 3320 BALLAST DHAV DHC8 DHC8102 2809003 NM CABIN BURNED A PCAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 EICHP 258 CRW FLIGHT 3625, CREW REPORTED HOT ELECTRICAL SMELL WITH OVERHEAD CABIN LIGHTS ON. MAINTENANCE REMOVED DIM LIGHT BULB O VER SEATS 2AC. FLIGHT 3912, CREW REPORTED BURNING SMELL IN COCKPIT AND CABIN. MAINTENANCE INSPECTED AIRCRAFT AND VERIF IED SMELL TO BE COMING FROM OVERHEAD LIGHTS, CIRCUIT BREAKER S-2 PULLED AND NOTED OVERHEAD LIGHTS WERE PREVIOUSLY UNDER MEL DURING NEXT MAINTENANCE RON ON 17 MAY 2002, OVERHEAD CABIN LIGHTS WERE INSPECTED AND IT WAS DISCOVERED THAT THE LAMP CARRIER ABOVE SEAT AT ROW 1AC WAS BURNT. LAMP CARRIER WAS REPLACED, AND LAMP INSTALLED. OPERATIONAL CHECK GOOD. AIRC RAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061100097 20020611 00097 NM 2002 6 11 PCAA0205059 1 20020526 A 3350 SOCKET DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 810EX 308 DURING ROUTINE MAINTENANCE VISIT FORWARD RED FLOOR (EMERGENCY) LIGHT FOUND TO BE INOPERATIVE. SOCKET AND BULB REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061100098 20020611 00098 EA 2002 6 11 COMA0260360 1 20020607 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA AVIONICS DISCHARGED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 783CA 10171 7315 FLIGHT 5676 SEVERAL EMERGENCY LIGHTS ARE INOP.REPLACED THE #3 EMERGENCY BATTERY 2 L 7 2 4F RT A21EA 2002061100099 20020611 00099 NM 2002 6 11 PCAA0205060 1 20020529 A 3234 5352011 CONTROL HANDLE DHAV DHC8 DHC8102 2809003 NM COCKPIT FAULTY A PCAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 13 844EX 13599 339 MDT FLIGHT 3741, CREW REPORTED AFTER GEAR RETRACTION, GEAR HANDLE ILLUMINATED AND LEFT NOSE AND RIGHT RED LIGHTS REMAINE D ILLUMINATED. MAINTENANCE REPLACED GEAR HANDLE ASSEMBLY. FUNCTIONAL CHECKED IN ACCORDANCE WITH MAINTENANCE MANUAL 32- 30-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061100100 20020611 00100 EA 2002 6 11 COMA0260361 1 20020608 A 2910 AE7090052 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA LT PYLON LEAKING A COMA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 01 975CA 7150 FLIGHT 6657 #1 HYDRAULIC SYSTEM INDICATING ZERO PRESSURE AND ZERO QUANTITY.REPLACED THE HYDRAULIC LINES AT THE LT ENGINE TO PYLON INTERFACE. 2 L 7 2 4F RT A21EA 2002061100103 20020611 00103 NM 2002 6 11 QXEA0200794 1 20020507 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 10 SEAT TRACK CORRODED UPPER AND INNER SURFACES AT STATION X373-X376. REPAIRED IAW RD-8 53-1342, SRM 51-40-00 A ND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002061100104 20020611 00104 WP 2002 6 11 2002F00605 1 20020513 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FLOOR SUPPORT, AT STATION 432 LBL 25. (M) 2 L 7 3 4F A22WE 2002061100105 20020611 00105 WP 2002 6 11 2002F00606 1 20020513 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STATION 457.66, LBL 38. (M) 2 L 7 3 4F A22WE 2002061100106 20020611 00106 WP 2002 6 11 2002F00607 1 20020513 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FRAME IN AFT CARGO BAY FORWARD SIDE OF WEB, STATION 1942 LONGERON 46L. (M) 2 L 7 3 4F A22WE 2002061100107 20020611 00107 WP 2002 6 11 2002F00608 1 20020513 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON AFT CARGO BAY SHEAR TIE, AT STATION 1942, LONGERON 47L AND LONGERON 48L. (M) 2 L 7 3 4F A22WE 2002061100108 20020611 00108 EA 2002 6 11 COMA0260362 1 20020608 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 981CA 7163 FLIGHT 5207 FLAPS FAIL MESSAGE DURING LANDINGRESET THE FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002061100109 20020611 00109 WP 2002 6 11 2002F00609 1 20020513 A 5320 ATTACH ANGLE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY ON LONGERON TO FRAME ATTACH ANGLE, AT STATION 1902, LONGERON 52. (M) 2 L 7 3 4F A22WE 2002061100110 20020611 00110 WP 2002 6 11 2002F00610 1 20020513 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON AFT CARGO BAY SHEAR TIE, AT FRAME STATION 1902, LONGERON 52 AND 51R. (M) 2 L 7 3 4F A22WE 2002061100111 20020611 00111 WP 2002 6 11 2002F00611 1 20020513 A 5320 STRUCTURE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY, ON STRUCTURE AND AROUND ANTENNA REINFORCEMENT AREA, AT STATION 1902 TO 192 1, LONGERON 50R AND 51L. (M) 2 L 7 3 4F A22WE 2002061100112 20020611 00112 WP 2002 6 11 2002F00612 1 20020513 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY FLOORBEAM, ON UPPER AND LOWER SURFACE OF BEAM CAP AND ATTACH ANGLE, AT STAT ION 1902. (M) 2 L 7 3 4F A22WE 2002061100113 20020611 00113 NM 2002 6 11 2002F00613 1 20020515 A 5754 SKIN BOEING 727 727225 1384077 NM L/E SLAT DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND DENT IN OUTER SKIN OF NR 4 SLAT, LEFT WING STATION 410. (M) 2 L 7 3 4F A3WE 2002061100114 20020611 00114 NM 2002 6 11 2002F00614 1 20020426 A 3220 SUPPORT BOEING 727 727225 1384077 NM NLG CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CORROSION ON SUPPORT AND RADIUS ROD IN NOSE LANDING GEAR WHEEL WELL, STATION 227 LBL 8. (M) 2 L 7 3 4F A3WE 2002061100115 20020611 00115 NM 2002 6 11 2002F00615 1 20020510 A 5542 SKIN BOEING 727 727225 1384077 NM RUDDER CHAFED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND VERTICAL STAB LOWER RUDDER LEADING EDGE SKIN CHAFED AT STATION 150. (M) 2 L 7 3 4F A3WE 2002061300174 20020613 00174 EA 2002 6 13 COMA0260363 1 20020608 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 466CA 127 7627 FLIGHT 5117 FLAPS FAILED WHEN SELECTED UP AFTER T/O. REPLACED THE LT BPSU. 2 L 7 2 4F RT A21EA 2002061100116 20020611 00116 NM 2002 6 11 2002F00593 1 20020424 A 5741 FITTING BOEING 727 727225 1384077 NM LT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND LEFT WING REAR SPAR TO BODY 'BOTTLE PIN' INNER MATING SURFACE CORRODED. (M) 2 L 7 3 4F A3WE 2002061100117 20020611 00117 NM 2002 6 11 A6WA200230010 1 20020528 A 3020 001A716E1000010 BOOT DORNER DO32 DO328100 2996000 NM NR 2 ENGINE TORN A A6WA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 GL 31 339PH 3015 AFTER TURNING ANTI-ICE/PROP DE-ICE ON RIGHT ENGINE TORQUE LOSS OF 60 PERCENT NORMAL POWER FOLLOWED BY A RETURN OF NORMAL POWER AND RIGHT DE-ICE FAIL. MAINTENANCE REMOVED AND REPLACED INTAKE BOOT ASSEMBLY. (M) 2 H 7 2 4T RT A45NM 2002061100118 20020611 00118 EU 2002 6 11 A6WA200260005 1 20020522 A 5230 CAGE BAC 146 146300A 1500267 EU CARGO DOOR CRACKED A A6WA K NONE O OTHER NR NOT REPORTED 1 GL 31 616AW E3145 REAR CARGO DOOR UPPER AFT INNER SEAL RETAINER CAGE IS CRACKED APPROX 2 INCHES IN LENGTH. REPLACED UPPER AFT INNER CAGE IAW SRM 51-42-00. REPAIRS CARRIED OUT PER BARA/AVR/5007/00. (M) 2 H 7 4 4F RT A49EU 2002061100119 20020611 00119 EU 2002 6 11 A6WA200260006 1 20020522 A 5260 STRUCTURE BAC 146 146300A 1500267 EU PAX DOOR CHAFED A A6WA K NONE O OTHER NR NOT REPORTED 1 GL 31 616AW E3145 FOUND LEFT AFT PAX DOOR AIRSTAIR HOOK CUTOUT HAS CHAFING FROM HOOK. REPAIRS CARRIED OUT IAW BAE PROCEDURE REF NR CH/RJ/ 0735/02. (M) 2 H 7 4 4F RT A49EU 2002061100120 20020611 00120 EU 2002 6 11 A6WA200260007 1 20020522 A 7110 DOOR BAC 146 146300A 1500267 EU NR 4 COWLING CRACKED A A6WA K NONE O OTHER NR NOT REPORTED 1 GL 31 616AW E3145 NR 4 ENGINE INBOARD AFT COWL DOOR HAS A CRACK NEXT TO DRAIN TUBE. REPAIRED CRACK IAW BAE PROCEDURE REF NR NWH/RJ/0726-0 2 AND RIL HC7IIH9012. (M) 2 H 7 4 4F RT A49EU 2002061100121 20020611 00121 EU 2002 6 11 A6WA200260008 1 20020522 A 5242 RETAINER BAC 146 146300A 1500267 EU E/E BAY DOOR DAMAGED A A6WA K NONE O OTHER NR NOT REPORTED 1 GL 31 616AW E3145 ELECTRICAL EQUIPMENT BAY DOOR RETAINING ANGLE ON FORWARD FRAME DAMAGED. ANGLE REPAIRED IAW BAE PROCEDURE REF NR CH/RJ/0 734-02. (M) 2 H 7 4 4F RT A49EU 2002061100122 20020611 00122 EU 2002 6 11 A6WA200260010 1 20020522 A 7110 FRAME BAC 146 146300A 1500267 EU NR 3 COWLING CHAFED A A6WA K NONE O OTHER NR NOT REPORTED 1 GL 31 616AW E3145 NR 3 ENGINE FORWARD INBOARD COWL DOOR HAS CHAFE MARKS ON FORWARD MOST FRAME. REPAIRED IAW BAE RIL HC711H9089. (M) 2 H 7 4 4F RT A49EU 2002061100123 20020611 00123 EU 2002 6 11 A6WA200260014 1 20020523 A 5512 SKIN BAC 146 146200A 1500266 EU HORIZ STAB DAMAGED A A6WA K NONE O OTHER NR NOT REPORTED 1 GL 31 181US E2042 TWO AREAS OF MECHANICAL DAMAGE ON THE LEFT LOWER SKIN ON THE HORIZONTAL STAB. FABRICATED A REPAIR PATCH. REPAIRED IAW BAE RIL BARA/AVR/1034/02-DC. (M) 2 H 7 4 4F A49EU 2002061100124 20020611 00124 NM 2002 6 11 GAIA02062ST 1 20020517 A 5230 MS20253P47200 HINGE BOEING 727 7272J0 138407E NM CARGO DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THE MAIN CARGO DOOR HINGE AFT UPPER SECTION IS CRACKED. ACCOMPLISHED MAI N CARGO DOOR HINGE UPPER AFT SECTION REPLACEMENT IAW B727-200 MM AEI STC SA179SO. (M) 2 L 7 3 4F RT A3WE 2002061100125 20020611 00125 NM 2002 6 11 GAIA02063ST 1 20020517 A 5320 INTERCOSTAL BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION, IT WAS DISCOVERED IN THE AFT CARGO COMPARTMENT BETWEEN BS 1030 AND 1050 AT STRINGER 25L, IN TERCOSTAL IS CRACKED. ACCOMPLISHED INTERCOSTAL REPLACEMENT IAW B727 SRM 53-10-2 FIG 5. (M) 2 L 7 3 4F RT A3WE 2002061100126 20020611 00126 NM 2002 6 11 GAIA02064ST 1 20020517 A 5320 INTERCOSTAL BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION, IT WAS DISCOVERED IN THE FORWARD CARGO COMPARTMENT, INTERCOSTAL IS CRACKED BETWEEN BS 950A- 950B AT STRINGER 25L. ACCOMPLISHED INTERCOSTAL REPAIR IAW B727 SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F RT A3WE 2002061100127 20020611 00127 NM 2002 6 11 GAIA02065ST 1 20020517 A 5313 STRINGER BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION, IT WAS DISCOVERED STRINGER 18A RIGHT IS CRACKED AT BS 940 RUNNING AFT FROM RADIUS BLOCKS AT THE BASE OF THE HORIZONTAL LEG. ACCOMPLISHED STRINGER 18A REPAIR IAW BOEING DRAWING 65C27166. (M) 2 L 7 3 4F RT A3WE 2002061100128 20020611 00128 NM 2002 6 11 GAIA02066ST 1 20020517 A 5330 SKIN BOEING 727 7272J0 138407E NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION, IT WAS DISCOVERED DISHED FASTENERS ON FUSELAGE SKIN AT BS 351, BELOW STRINGER 26R. ACCOMPL ISHED SKIN PANEL AND T-CHORD REPLACEMENT IAW B727 SRM 53-30-2, FIG 2 AND SRM 51-30-2. (M) 2 L 7 3 4F RT A3WE 2002061100129 20020611 00129 WP 2002 6 11 GTIA020370 1 20020324 A 5320 ACCESS PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND MID CARGO JAMB ACCESS PANEL STATION 693 RIGHT CRACKED AND HAS CORROSION AROUND FASTENER HOLES. ACCESS PANEL AREA FOUND OUT OF LIMITS. DRILLED UP AND LOCATED NEW PANEL. (M) 2 L 7 2 4F A6WE 2002061100130 20020611 00130 WP 2002 6 11 GTIA020371 1 20020324 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FLIGHT FORWARD COMPARTMENT PRESSURE AND FLOOR SUPPORT, CORRODED AT SUPPORT FLOOR STATION 120.050. REMOVED FLOOR S UPPORT FROM A/C. FORMED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002061100131 20020611 00131 WP 2002 6 11 GTIA020372 1 20020325 A 5230 CAMSHAFT DOUG DC9 DC981 3022081 WP CARGO DOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - AFT CARGO DOOR LOCK BAR AND MECH ARE RUSTY. REMOVED AFT CAM SHAFT ROD FROM AFT CARGO DOOR. INSTALLED NEW CAM SHA FT ROD ON AFT CARGO DOOR. (M) 2 L 7 2 4F A6WE 2002061100132 20020611 00132 WP 2002 6 11 GTIA020373 1 20020322 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR PANEL LEFT STATION 826-864 CORRODED, BLUE WATER STAINS, CRACKED. FABRICATED FLOORBOARD REPAIR. (M) 2 L 7 2 4F A6WE 2002061100133 20020611 00133 WP 2002 6 11 GTIA020374 1 20020322 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR PANEL LEFT INBOARD STATION 927-1003 HAS CORROSION UNDER PANEL AND CRACKED. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002061100134 20020611 00134 WP 2002 6 11 P2EA2002M036 1 20020524 A 3220 5920603507 PISTON BOEING DOUG DC9 DC982 3022082 WP FLAKING A P2EA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CE 05 140NJ 9361 9361 CPI1651 49931 Nose Landing Gear would not retract after take-off, returned to MCI for unscheduled landing. During inspection, on jacks , found cadium plating flaking off the NLG piston. Removed and replaced Piston and Axel assembly IAW 32-21-02. During te ardown found Bearing, P/N 5961561-1 and Retainer, P/N 3962423-1 scratched and parts of the plating imbeaded on surface. Bearing and Retainer replaced IAW MM 32-21-02. Operational check IAW 32-30-00, no defects noted. This is closing action for P2EA2002M036 2 L 7 2 4F A6WE 2002061100135 20020611 00135 WP 2002 6 11 GTIA020375 1 20020324 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD B/B STATION 408 TO FORWARD BULKHEAD HAS MANY AREAS OF CORROSION ON L30. AREA FOUND TO BE OUT OF LIM ITS AT L30 STATION 294. REMOVED LONGERON L30 STATION 264-320. INSTALLED LONGERON L30 STATION 264-320. (M) 2 L 7 2 4F A6WE 2002061100136 20020611 00136 WP 2002 6 11 GTIA020376 1 20020322 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND CORROSION ON LONGERON 30 IN MANY PLACES FROM STATION 408-446. SECTION OF LONGERON FOUND OUT OF LIMITS. (M) 2 L 7 2 4F A6WE 2002061100137 20020611 00137 WP 2002 6 11 GTIA020377 1 20020322 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FOUND CORROSION FORWARD B/BAY LONGERON R-28 STATION 446-427 AS MARKED. AREA FOUND TO BE OUT OF LIMITS. REMOVED Z-ANGLE . FABRICATED Z-ANGLE, LOCATED AND DRILLED Z-ANGLE. INSTALLED Z-ANGLE. (M) 2 L 7 2 4F A6WE 2002061100138 20020611 00138 WP 2002 6 11 GTIA020378 1 20020318 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND AFT PIT/CABIN FLOOR, STATION 1155-1174 PLUS X23 LEFT MIDDLE SEAT TRACK AND SPLICE ARE CORRODED. REMOVED SEA T TRACK AT STATION 1098-1211. FABRICATED AND DRILLED UP NEW TRACK AND SPLICES. INSTALLED NEW SEAT TRACK AND TWO SPLICE S. (M) 2 L 7 2 4F A6WE 2002061100139 20020611 00139 WP 2002 6 11 GTIA020379 1 20020318 A 5310 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND RIGHT FWD MLG DOOR JAMB CRACKED AT INBOARD SUPPORT PREVIOUS DOUBLER REPAIR -X 6.25. REMOVED DOUBLER REPAIR AND TEE ANGLE. AFTER FURTHER EVALUATION ADDITIONAL CRACK WAS FOUND, LOCATED AND DRILLED NEW PARTS. FABRICATED 2 CHANNE LS TO BE USED AS SPLICE FOR NEW DOOR JAMB. INSTALLED TWO CHANNELS. (M) 2 L 7 2 4F A6WE 2002061100140 20020611 00140 WP 2002 6 11 GTIA020380 1 20020316 A 5712 RIB DOUG DC9 DC981 3022081 WP RT WING CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND RIGHT LOWER CENTER WING CORRODED AT RIB NR 8, FROM MLG DOOR JAMB. REMOVED CORROSION. RIB SPLICE FOUND TO B E OUT OF LIMITS. REMOVED DAMAGED SECTION OF THE RIB SPLICE. FABRICATED NEW SECTION OF RIB SPLICE AND REPAIR. INSTALLE D RIB SPLICE AND DOUBLER, STRAP. (M) 2 L 7 2 4F A6WE 2002061100141 20020611 00141 WP 2002 6 11 GTIA020381 1 20020316 A 5712 FORMER DOUG DC9 DC981 3022081 WP RT WING CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND RIGHT WING CORRODED AT NOSE CAP SECTION ATTACH, FORMERS VORTILON. FORMED FORMER. DRILLED AND LOCATED. INS TALLED ATTACHED FORMED ANGLE. (M) 2 L 7 2 4F A6WE 2002061100142 20020611 00142 WP 2002 6 11 GTIA020382 1 20020318 A 5730 SKIN DOUG DC9 DC981 3022081 WP RT WING DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND RIGHT WING LOWER SURFACE DELAMINATED/DETERIORATED AT PANEL TRAPEZOIDAL. REMOVED DELAMINATED SKIN FROM RIGHT WING TRAP PANEL. REPAIRED DELAMINATION. (M) 2 L 7 2 4F A6WE 2002061100143 20020611 00143 WP 2002 6 11 GTIA020383 1 20020314 A 5755 SKIN DOUG DC9 DC981 3022081 WP SPOILER DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND LEFT MIDDLE FLIGHT SPOILER, UPPERSIDE HAS AN AREA OF DELAMINATION 3 INCH SPAN BY 9 INCH CHORD, CENTER AREA O F SPOILER. DUE TO EXTENSIVE DAMAGE OF UPPER SKIN AND CORE, BONDED NEW CORE AND UPPER SKIN FULL SPAN OF PART. (M) 2 L 7 2 4F A6WE 2002061100144 20020611 00144 WP 2002 6 11 GTIA020384 1 20020314 A 5755 SPAR DOUG DC9 DC981 3022081 WP SPOILER CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND LEFT OUTBOARD FLIGHT SPOILER, OUTBOARD FORWARD CORNER IS BOWED, DELAMINATED AND WORKING RIVETS, AN AREA 4 IN CH SPAN BY 1.50 INCH CHORD. REMOVED PAINT ON OUTBOARD CORNER AND FOUND CRACK IN SPAR. STOP DRILLED CRACK IN SPAR. INS TALLED DOUBLERS TO DAMAGED AREA. CUT OUT PIECE OF CORE TO FIT CORNER AT LEFT INBOARD LOWER CORNER. FABRICATED FILLER A ND DOUBLER TO FIT UNDER INBOARD CORNER. PERFORMED HOT BOND REPAIR WITH CORE, FILLER, AND DOUBLER. (M) 2 L 7 2 4F A6WE 2002061100145 20020611 00145 WP 2002 6 11 GTIA020385 1 20020324 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND AFT CARGO FLOOR SUPPORT STATION 1212 HAS CORROSION AND DOUBLE DRILLED HOLES. FOUND BE OUT OF LIMITS. DRILL ED UP AND LOCATED NEW SUPPORT. (M) 2 L 7 2 4F A6WE 2002061100146 20020611 00146 WP 2002 6 11 GTIA020386 1 20020313 A 5320 THRESHOLD DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND AFT CARGO AT THRESHOLD CUT OUT THERES CORROSION. REMOVED CORROSION ON THE BEAM, OUT OF LIMITS. REMOVED BEA M FROM STA Y-1117, Y-1250, -X=16 INCHES. AFTER FURTHER EVALUATION, FOUND AFT LOWER SEAL DEPRESSOR OUT OF LIMITS. FABRI CATED DRILLED AND LOCATED NEW SEAL DEPRESSOR. INSTALLED SEAL DEPRESSOR. (M) 2 L 7 2 4F A6WE 2002061100147 20020611 00147 WP 2002 6 11 GTIA020387 1 20020325 A 7120 CLIP DOUG DC9 DC981 3022081 WP RT ENGINE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - RIGHT ENGINE FORWARD LOWER VIBRATION ABSORBER CLIP CRACKED. REMOVED RIGHT ENGINE FORWARD LOWER VIBRATION ABSORBER CLIP. FABRICATED REPAIR CLIP. INSTALLED REPAIR CLIP. (M) 2 L 7 2 4F A6WE 2002061100148 20020611 00148 WP 2002 6 11 GTIA020388 1 20020422 A 3397 WIRE DOUG DC9 DC981 3022081 WP TAILCONE DISCONNECTED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND EMERGENCY EXIT LIGHTS IN TAIL CONE INOPERATIVE. T/S SYSTEM FOUND WIRES NOT CONNECTED. CONNECTED WIRES TO C ORRECT LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2002061100149 20020611 00149 2002 6 11 GTIA020389 4 20020428 A 2565 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR UNSERVICEABLE A GTIA K NONE O OTHER CR CRUISE 1 GL 23 817NK 49141 FLT 386 - R1 DOOR SLIDE PACK COMING UNPACKED. REMOVED AND REPLACED R1 EVACUATION SLIDE IAW MD 80. (M) 2 L 7 2 4F A6WE 2002061100150 20020611 00150 WP 2002 6 11 GTIA020390 1 20020426 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST CR CRUISE 1 GL 23 16892 49391 FLL - FLT 197 - FOUND FORWARD ENTRY DOOR WALK AROUND EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FORWARD ENTRY DO OR WALK AROUND EMERGENCY LIGHT ASSEMBLY. OPS CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 2002061100151 20020611 00151 WP 2002 6 11 GTIA020391 1 20020426 A 3350 60030431 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 16892 49391 FLL - FLT 197 - FOUND CEILING EMERGENCY LIGHTS INOPERATIVE FROM ROW 1 TO ROW 6. REPLACED EMERGENCY BATTERY FOR CEILING EMERGENCY LIGHTS SEAT ROW 1 TO ROW 6. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2002061100152 20020611 00152 WP 2002 6 11 GTIA020392 1 20020427 A 2720 LIMITER DOUG DC9 DC982 3022082 WP RUDDER OUT OF ADJUST A GTIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 23 800NK 49144 FLT 1225 - RSW - RUDDER TRAVEL UNRESTRICTED LIGHT ILLUMINATED IN CRUISE FLIGHT. FOLLOWED PROCEDURE AND SELECTED RUDDER TO MANUAL. ON DESCENT, LIGHT WENT OUT AT 310 KTS ON APPROACH WE SELECTED RUDDER TO POWER AND IT OPERATED NORMALLY. ADJ USTED RUDDER THROW LIMITER IAW MD80. NO FURTHER DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2002061100153 20020611 00153 WP 2002 6 11 GTIA020393 1 20020430 A 3350 60030431 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 803NK 48087 FLL - FLT 9803 - ON CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE FROM STATION 845 THROUGH 1155. REPLACED BATTERIES IN BATT ERY PACKS B5-73, B5-26 AND B5-58. REPLACED BATTERY PACK B5-26, STATION 1079 REF MM 33-53-00, OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2002061100154 20020611 00154 WP 2002 6 11 GTIA020394 1 20020327 A 5320 ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND 'L' ANGLE CORRODED AT FS 147, BY 12.5, LOWER AREA OF EPC PANEL. REMOVED ANGLE. FORMED 'L' ANGLE. INSTALLE D 'L' ANGLE. (M) 2 L 7 2 4F A6WE 2002061100155 20020611 00155 WP 2002 6 11 GTIA020395 1 20020324 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND PASSENGER COMPARTMENT AND FLOOR SUPPORT CRACKED AT MEMBRANE WEB STATION 1309 PLUS X50. FORMED REPAIR DOUBLE R. INSTALLED IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002061100156 20020611 00156 WP 2002 6 11 GTIA020396 1 20020323 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND PIT LONGERON 28R STATION 1117 TO STATION 1155 CORRODED. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED NE W LONGERON SECTION. FABRICATED NEW LONGERON SPLICE. INSTALL LONGERON. INSTALLED SPLICE. (M) 2 L 7 2 4F A6WE 2002061100157 20020611 00157 WP 2002 6 11 GTIA020397 1 20020324 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND STATION 1309 -X17 TO +X17 FLOORBOARD SUPPORT UPPER SURFACE IS CORRODED. REMOVED PART. FABRICATED NEW PART AND INSTALLED. (M) 2 L 7 2 4F A6WE 2002061100158 20020611 00158 WP 2002 6 11 GTIA020398 1 20020320 A 5210 INTERCOSTAL DOUG DC9 DC981 3022081 WP PAX DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD PASSENGER DOOR INTERNAL STRUCTURE, FRAME CRACKED BETWEEN LL BEAM 4 AND 5 STATION Y185.5. REMOVED IN TERCOSTAL AT STATION Y 185.5 DRILLED AND LOCATED NEW INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002061100159 20020611 00159 WP 2002 6 11 AALA20020673 1 20020429 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 NR 1 CORRODED AT 1176, 1208 AND 1236. REPLACED SEAT TRACK, STA 1174 - 1309. 2 L 7 2 4F 4 F A6WE E2EA 2002061100160 20020611 00160 WP 2002 6 11 AALA20020674 1 20020503 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 FOUND CRACK IN INTERCOASTAL, STA 1287 - 1309 AT FLOOR BEAM LEVEL. REMOVED OLD INTERCOASTAL AND INSTALLED NEW SERVICEABL E INTERCOSTAL. 2 L 7 2 4F 4 F A6WE E2EA 2002061100161 20020611 00161 WP 2002 6 11 AALA20020675 1 20020507 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 INSTALLED NEW TIE DOWN. G-2 CENTER AND OUTBOARD GALLEY TIE DOWNS CORRODED. INSTALLED NEW TIE DOWNS. 2 L 7 2 4F A6WE 2002061100162 20020611 00162 WP 2002 6 11 AALA20020676 1 20020508 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 FLOORBOARD BETWEEN FOS SEAT TRACKS CORRODED STA 148, RBL 20 INCHES, TO RBL 29 INCHES. NEW FLOORBOARD INSTALLED ES841861 22. 2 L 7 2 4F 4 F A6WE E2EA 2002061100163 20020611 00163 WP 2002 6 11 AALA20020677 1 20020501 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 (SEAT TRACK) CORROSION AROUND CLIP NUT HOLES UNDERSIDE INBOARD SEAT TRACK NR 3 STA 1271-1309. INSTALLED NEW SECTION OF SEAT TRACK FROM STA 1258 TO STA 1309 PER SRM 51-30 AND SRM. 2 L 7 2 4F 4 F A6WE E2EA 2002061100164 20020611 00164 WP 2002 6 11 AALA20020678 1 20020501 A 5320 WEB DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 LIGHT CORROSION ON GALLEY SUBFLOOR UNDER G-2 GALLEY INBOARD AFT GALLEY MOUNT. CUT OUT DAMAGE AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F A6WE E2EA 2002061100165 20020611 00165 WP 2002 6 11 AALA20020679 1 20020430 A 5320 WEB DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 CORROSION ON CUSP RIGHT ON STA 594. INSTALLED DOUBLER ON CUSP PREP PER SRM. 2 L 7 2 4F 4 F A6WE E2EA 2002061100166 20020611 00166 WP 2002 6 11 AALA20020680 1 20020502 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 CORROSION ON FLOORBOARD UNDER FLO SEAT AND SEAT TRACK. INSTALLED DOUBLER REPAIRS AT STA 120 STA 148. 2 L 7 2 4F 4 F A6WE E2EA 2002061100167 20020611 00167 WP 2002 6 11 AALA20020761 1 20020527 A 4920 5940405503 APU DOUG DC9 DC983 3022083 WP APU BAY LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 76201 17429 53291 (APU) EN ROUTE, AFTER TAKE OFF CABIN FILLED WITH A HAZE. FLIGHT ATTENDANT IN REAR REPORTED IT WAS DIFFICULT TO SEE FROM REAR TO FRONT OF CABIN. LANDED WITHOUT INCIDENT. REPLACED APU ASSEMBLY DUE TO LEAKING AT INTAKE. ACCOMPLISHED PACK B URN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2002061100168 20020611 00168 WP 2002 6 11 AALA20020762 1 20020528 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 488AA 49681 DURING OVERNIGHT MAINTENANCE AFT SEAT MOUNTED EMERGENCY EXIT LIGHTS FROM ROW 20-31 INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE IN AFT AIR STAIRS AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2002061100169 20020611 00169 WP 2002 6 11 AALA20020763 1 20020528 A 3350 CONNECTING ROD DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 245AA 49257 DURING OVERNIGHT MAINTENANCE FLOOR LEVEL FORWARD GALLEY OUTBOARD EMERGENCY EXIT LIGHTS INOPERATIVE. RECONNECTED EMERGEN CY EXIT LIGHT CONNECTOR FOR FLOOR LEVEL FORWARD GALLEY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2002061100170 20020611 00170 NM 2002 6 11 AALA20020764 1 20020525 A 2910 AS115060172 HYDRAULIC LINE BOEING 757 757223 1384957 NM HYD SYSTEM BROKEN A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 650AA 24608 (LINE) EN ROUTE, MIA-BOG LOSS OF LEFT SYSTEM HYDRAULIC FLUID INDICATION. DECLARED EMERGENCY AND LANDED AT MBJ WITHOUT I NCIDENT. CHECKED AND FOUND BROKEN HYDRAULIC LINE ON NOSE GEAR DOOR ACTUATOR. REPLACED HYDRAULIC LINE. REPLENISHED SYS TEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2002061100171 20020611 00171 EU 2002 6 11 AALA20020765 1 20020528 A 2530 8609010000 OVEN AIRBUS 300 A300B4605R 3930308 EU GALLEY MALFUNCTIONED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 41063 506 (OVEN) EN ROUTE, AFTER TAKEOFF ELECTRICAL SMELL REPORTED IN FIRST CLASS GALLEY AND IN COCKPIT. RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. FOUND SMOKE COMING FROM NUMBER ONE OVEN IN FIRST CLASS. REPLACED NUMBER ONE OVEN. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2002061100172 20020611 00172 WP 2002 6 11 GTIA020399 1 20020313 A 5320 THRESHOLD DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND MID CARGO DOOR CUT OUT AT BASE OF THRESHOLD HAS CORROSION. JAMB BEAM MATERIAL LOSS FOUND TO BE OUT OF LIMIT S. REMOVED DOOR JAMB BEAM. DRILLED UP AND LOCATED NEW DOOR JAMB BEAM. INSTALLED DOOR JAMB BEAM. (M) 2 L 7 2 4F A6WE 2002061100173 20020611 00173 WP 2002 6 11 GTIA020400 1 20020330 A 5350 ATTACH FITTING DOUG DC9 DC981 3022081 WP TAIL CONE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND TAIL CONE BENT UP AT HOUSING TAIL CONE ATTACH PLATE SHEAR, 12 PLACES. UPON INSPECTION, FOUND ATTACH PLATE C ORROSION. FORMED REPAIR DOUBLERS. INSTALLED REPAIR DOUBLERS. (M) 2 L 7 2 4F A6WE 2002061100174 20020611 00174 WP 2002 6 11 GTIA020504 1 20020514 A 3397 WIRE DOUG DC9 DC982 3022082 WP COCKPIT LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 603CA 49508 MCO - FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY POWER PACK IN FORWARD DROP CEILING AND SECURED LOO SE CHARGING INPUT WIRE AT P1-1213. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2002061100175 20020611 00175 WP 2002 6 11 GTIA020505 1 20020515 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 814NK 49619 DTW - FOUND TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT DISCONNECTED. CONNECTED WIRING FOR TAIL COMPARTMENT OVERHEAD EMER GENCY LIGHT. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2002061100176 20020611 00176 2002 6 11 GTIA020506 4 20020514 A 3418 CAM DOUG DC9 DC982 3022082 WP HORIZ STAB OUT OF ADJUST A GTIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 23 812NK 48021 DTW - FLT 563 - SLACK IN THE CG ADJUSTMENT WHEEL OF TAKEOFF CONDITIONING COMPUTER. TAKEOFF WARNING HORN DURING INITIAL POWER UP FOR TAKEOFF TAXIED OFF OF RUNWAY. FOUND STABILIZER TAKEOFF WARNING ROLLER CAM OUT OF ADJUSTMENT. ADJUSTED CAM POSITION IAW MD80 MM 27-40-00. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002061100177 20020611 00177 WP 2002 6 11 GTIA020507 1 20020515 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 803NK 48087 FLT 461 - DTW - FOUND EMERGENCY CEILING LIGHTS INOPERATIVE BETWEEN SEATS 6 THROUGH 9. REMOVED AND REPLACED BATTERIES AN D CLEANED CONTACTS OF BATTERY PACK CLIPS, OPS OK ON CHECK PER MM 35-53-00. (M) 2 L 7 2 4F A6WE 2002061100178 20020611 00178 WP 2002 6 11 GTIA020508 1 20020515 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 803NK 48087 DTW - FLT 461 - FOUND EMERGENCY CEILING LIGHTS INOPERATIVE AT AFT OVERWING EXIT DOOR. REMOVED AND REPLACED BATTERIES. OPS OK PER MM 33-53-00. (M) 2 L 7 2 4F A6WE 2002061100179 20020611 00179 WP 2002 6 11 GTIA020509 1 20020324 A 5311 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - RIGHT AFT LAVATORY STATION 1338 -X45 TO -55 FRAME WEB IS CORRODED ON FORWARD AND AFT SIDES, WEB TORN/CRACKED AT X3 0 TO -33 INBOARD AND OUTBOARD SIDE OF LIGHTENING HOLE. FLOOR SUPPORT BEAM HAS TEAR 1 INCH TO 2 INCHES LONG AT LIGHTENIN G HOLE FS 1338, 36 INCHES RT OF C/L UNDER RT LAVATORY. REMOVED DAMAGED WEB. FABRICATED WEB AND DOUBLER. INSTALLED WEB AND DOUBLER AT FS 1338 -X10 TO -X58. (M) 2 L 7 2 4F A6WE 2002061100180 20020611 00180 2002 6 11 GTIA020511 4 20020519 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 SJU - L1 DOOR EMERGENCY ESCAPE SLIDE PACK FELL OFF. REINSTALLED L1 EMERGENCY ESCAPE SLIDE PACK. (M) 2 L 7 2 4F A6WE 2002061100181 20020611 00181 EA 2002 6 11 HNAA0200040 1 20020603 A 2611 3023143 SMOKE DETECTOR DHAV DHC8 DHC8311 1386006 EA BAG BAY #1 POS INTERMITTENT A HNAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 07 803SA 9005 221 CREW REPORTED THE BAG BAY SMOKE DETECTOR LIGHT WOULD COME ON INTERMITTENTLY. AIRCRAFT RETURNED TO ROA. REPLACED BOTH BAG BAY SMOKE DETECTORS. 2 H 7 2 4T RT A13NM 2002061100182 20020611 00182 EA 2002 6 11 HNAA0200041 1 20020603 A 2611 3023143 SMOKE DETECTOR DHAV DHC8 DHC8311 1386006 EA BAG BAY #2 POS INTERMITTENT A HNAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 07 803SA 4197 134 221 CREW REPORTED THE BAG BAY SMOKE DETECTOR LIGHT WOULD COME ON INTERMITTENTLY. AIRCRAFT RETURNED TO ROA. REPLACED BOTH BAG BAY SMOKE DETECTORS. 2 H 7 2 4T RT A13NM 2002061100183 20020611 00183 NM 2002 6 11 2002UALA00948 1 20020602 A 5315 CAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 CABIN FLOOR BEAM STATION 324 UPPER CAP CORRODED RBL40 TORBL60. MAJOR REPAIR ACCOMPLISHED.SPLICED IN NEW CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072200046 20020722 00046 NM 2002 7 22 2002UALA00955 1 20020604 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 FORWARD PIT FRAME BETWEEN STRINGER 22L AND 23L FOUND DENTED. MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002061200001 20020612 00001 NE 2002 6 12 CA020425007 2 20020404 A 7230 3040689 BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE IMPELLER DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LT ENGINE LP IMPELLER BLADES DAMAGED BEYOND LIMITS DUE TO FOD. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061200002 20020612 00002 NM 2002 6 12 CA020502013 1 20020326 A 7830 THRUST REVERSER BOEING 767 767333 1385301 NM GE CF6 CF680C2B6F 30025 NE ENGINES CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) BOTH REVERSERS ONLY DEPLOYED AT MID TRAVEL ON LANDING.FOUND MOISTURE TRAP IN THE THRUST REVERSERS CDU (CONTROL AND DRIVE UNIT). REMOVED ALL MOISTURE, FUNCTIONAL TEST CARRIED OUT, AIRCRAFT FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E13NE 2002061200003 20020612 00003 NE 2002 6 12 CA020502017 2 20020410 A 7321 7436024 FUEL CONTROL BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CA (CAN) 1ST ATTEMPT AT TAKEOFF NR 1 ENGINE STALLED AT APPROXIMATELY 1,70 EPR.RETURNED TO RAMP FOR MAINTENANCE (MAINTENANCE CHECKED AIRCRAFT SERVICEABLE). 2ND ATTEMPT TAKOFF NR 1 ENGINE STALLED TWICE BETWEEN V1 AND GEAR UP. IN BOTH CASES WHILE NR 1 ENGINE ACCELERATED N1 WENT UP IN JUMPS RATHER THAN SMOOTHLY. BORESCOPE INSPECTION OF 6,7,13TH STAGE COMPRESSORS AN D 1ST STAGE HP TURBINE CARRIED OUT. NO FAULTS FOUND. FCU AND PRBC REPLACED. TAKEOFF POWER RUN ACCOMPLISHED WITH NO FAUL TS AND ENGINE CONDITION CHECK ACCOMPLISHED WITH PERIMETERS FOUND WITH DATA PLATE LIMITS. 2 L 7 2 4F 4 F A16WE E2EA 2002061200004 20020612 00004 NE 2002 6 12 CA020502020 2 20020415 A 7321 6078T55P015 MFC CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RT ENGINE FAILED W A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 CA (CAN) IN CRUISE AT FL340, A LOUD SOUND WAS HEARD FOLLOWED BY THE RT ENGINE SHUTTING DOWN. NO INFLIGHT IGNITION ATTEMPTED . AIRCRAFT PERFORMED A SINGLE ENGINE LANDING. SENSOR TEMPERATURE INLET COMPRESSOR P/N 4071T72P01 S/N WYG86492 REPLACED. ENGINE RUN PERFOMED AND WERE UNSUCCESSFULLY. RIGHT HAND MFC P/N 6078T55P15 S/N WYG93927 REPLACED. ENGINE RUN PERFORMED AND WERE SUCCESSFULLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061200005 20020612 00005 EA 2002 6 12 CA020502021 1 20020418 A 2740 MS27473T24B61SP CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB CONTROL BURNED W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 CA (CAN) DEPARTED NORMALLY. CLIMB TO CRUISE ALTITUDE WAS UNEVENTFUL (FL270). AUTOPILOT ENGAGED & CLEARED DIRECT APPROX 20 NM NORTH, STAB CH 1 INOP WHILE STATUS MESSAGE ILLUMINATED. QRH PROCS REQUIRED ATTEMPTED RESET - UNSUCCESSFUL - QRH REQD NO FUTHER ACTION (STAB CH 2 IS REDUNDANT SYS). WE HOWEVER DID PULL & MARK QRH P. SHOULD CH 2 FAIL - WHICH OCCURRED LATE R - NOTIFIED MAINT VIA ARINC & WROTE UP STAB CH 1 INOP IN LOGBOOK. APPROX 80MIN LATER STAB CH 2 INOP & MACH TRIM INOP MA STER CAUTION MESSAGES ILLUMINATED ON ED 1. COMPLIED WITH QRH PROCEEDURES 2 L 7 2 4F 4 F RT A21EA E15NE 2002061200006 20020612 00006 EA 2002 6 12 CA020502022 1 20020422 A 7830 22850741115 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT TR STOW FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING FLIGHT AT FL290, THE RT REVERSER UNLOCK MESSAGE APPEARED. AIRCRAFT DIVERTED TO ATLANTA AND LANDED WITHOUT F URTHER INCIDENT. RT THRUST REVERSER DEFERRED PER MEL. LATER R&R RT ENGINE TR STOW SWITCH IAW AMM 78-37-01-400-801. RT TH RUST REERSER OPS CHECKED IAW AMM AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061200007 20020612 00007 NE 2002 6 12 CA020503001 2 20020403 A 7270 3021436 DUCT CESSNA 500 500CESSNA 2076602 CE PWA JD15 JT15D1A NE LT ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING PHASE I & II INSPECTION, LT ENGINE FRONT & REAR INNER BYPASS DUCT FOUND CRACKED. PARTS REMOVED FROM ENGINE INSPECTED & FOUND PARTS HAD BEEN REPAIRED PREVIOUSLY, WELDED AT OVERHAUL & CRACK NEXT TO WELDED AREA.PROBABLE CAUSE, HI- TIME PARTS, PREVIOUSLY REPAIR, CRACKED, METAL FATIGUE. INNER BYPASS DUCT P/N 3021436 AND 3020330 1 L 7 2 4F 4 F A22CE E25EA 2002061200010 20020612 00010 NE 2002 6 12 CA020503007 2 20020430 A 7230 ENGINE AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211TRENT77 NE NR 1 STALLED W D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA 41064 (CAN) AIRCRAFT RETURNED TO GATE , NR 1 ENGINE HAD A COMPREESOR STALL. AIRCRAFT IS PRESENTLY IN YYZ FOR AN ENGINE REPLACE MENT. WAITING FOR MORE DETAILS FROM YYZ. 2 L 7 2 4F 4 F RT A46NM E39NE 2002061200011 20020612 00011 CE 2002 6 12 CA020506001 1 20020503 A 3260 2621101030 BULB LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP MLG INDICATOR BURNED OUT W O OTHER P NO WARNING INDICATION AP APPROACH 1 CA (CAN) ON APPROACH, PILOT SELECTED GEAR DOWN, ALL GEAR GREEN LIGHTS ILLUMINATED, EXCEPT THE LT MAIN GEAR LIGHT. THE BULB WAS CONFIRMED BURNED AFTER BULB TEST, BUT PILOT AS PRECAUTIONARY MEASURE, ACTIVATED THE GEAR BLOW DOWN. AIRCRAFT LANDED WITH NO ADDITIONAL PROBLEMS. 2 L 7 2 4F 4 F A10CE E6WE 2002061200012 20020612 00012 CE 2002 6 12 CA020506002 1 20020503 A 2110 35141000 BLOWER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE EVAPORATOR SEIZED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) SMOKE SMELL IN CABIN & FLIGHT DECK AFTER LANDING.THIRTY MINUTE DELAY TO SWAP AIRCRAFT. INSPECTION REVEALED THAT TH E FORWARD EVAPORATOR BLOWER HAD SEIZED, AND BLOWN THE CURRENT LIMITER, PROTECTING IT'S CIRCUIT. THE EVAPORATOR BLOWER ASSY WAS REPLACED AND TESTED SERVICABLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2002061200013 20020612 00013 CE 2002 6 12 CA020506003 1 20020505 A 3230 5081032019 SOCKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE TORQUE LINK CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A ROUTINE INSPECTION THE LT AXLE SOCKET ASSY WAS NOTED TO HAVE A SMALL CRACK IN THE AREA OF THE LOWER TORQU E KNEE LUGS. INVESTIGATION OF THE RT SOCKET ASSY REVEALED THE SAME CRACK IN THE SAME AREA.BOTH AXLE AND PISTON ASSY'S WE RE REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002061200014 20020612 00014 CE 2002 6 12 CA020506004 1 20020403 A 3230 5081032019 SOCKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE TORQUE KNEE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13155 (CAN) DURING A ROUTINE INSPECTION A CRACK WAS NOTED IN THE AREA OF THE MAIN LANDING GEAR LOWER TORQUE KNEE LUGS.THE PIST ON AND AXLE ASSY WAS REPLACED.THE CRACKED AXLE AND PISTON ASSY WERE SENT FOR O/H.THE SOCKET ASSY WAS REPLACED AT THE OVE RHAUL FACILITY (CRACKED BEYOND LIMITS). 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002061200015 20020612 00015 CE 2002 6 12 CA020506005 1 20020404 A 5711 3146R SPAR BBAVIA 11 11AC 0191102 CE CONT A65 A658 17003 SO RT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON CLOSE VISUAL INSPECTION A CRACK WAS FOUND IN THE CENTRE OF THE BUTT OF THE RIGHT FRONT SPAR. THE CRACK RUNS A T LEAST AS FAR AS THE BUSHING AT THE WING ATTACH BRACKET, BUT IS HIDDEN FROM THE FRONT AND BACK BY THE DOUBLER PLATE. WI NG TO BE REMOVED FOR REPAIR. 1 H 7 1 3O 3 O A761 E205 2002061200016 20020612 00016 EU 2002 6 12 CA020507002 1 20020503 A 5230 D5237130300200 FITTING AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE CARGO DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CARGO DOOR HANDLE FITTINGS FOUND CRACKED IN RADIUS BELOW THE BUSHING HOUSING. FOUND ON MORE THAN ONE DOOR.AC TIME 35,253HRS, FITTINGS REPLACED. IPC REF 52-32-21 FIG 3 ITEM 140 2 L 7 2 4F 4 F RT A28NM E29NE 2002061200018 20020612 00018 WP 2002 6 12 CA020507004 1 20020424 A 6220 369D1225 HUB HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL MAIN ROTOR MISOVERHAULED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) 80.8 HOURS AFTER INSTALLATION OF A MAIN ROTOR HUB, RECEIVED FROM FACTORY OVERHAUL, THE SEAL POPPED OUT OF KIT LOCA TION. IT WOULD APPEAR THAT NO BONDING AGENT OF ANY KIND WAS USED TO RETAIN THE SEAL. 1 G 7 1 3U 3 U H3WE E4CE 2002061200019 20020612 00019 EU 2002 6 12 CA020507005 1 20020423 A 2913 704A3369004 BELT SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE HYD SYSTEM BROKEN W E ENGINE SHUTDOWN J WARNING INDICATION IN INSP/MAINT 1 CA (CAN) DURING START UP (3RD OF DAY) PILOT REPORTED HYD WARNING LIGHT DID NOT GO OUT. CYCLIC & ANTI-TORQUE PEDALS HAD NO HYDRAULIC ASSIST. A/C SHUTDOWN NORMALLY. INSP REEALED HYDRAULIC BELT P/N 704A3369004 WAS BROKEN. BREAKAGE SEEMS TO BE NE AR END OF DIRECTION OF ROTATION ARROW, WHERE BELT IS BONDED TOGETHER.WE HAVE HAD PREVIOUS PROBLEMS WITH HYDRAULIC BELT. WE HAVE CHECKED THAT OUR ENGINEERS ARE INSTALLING BELT AS PER MAINTENANCE MANUAL. ON REPLACING BELT, IT NOTICED BROKEN B ELT LOT TIGHTER. 1 G 7 1 3U 3 U NC H9EU E19EU 2002061200020 20020612 00020 EU 2002 6 12 CA020507006 1 20020306 A 6720 704A34130180 CONTROL CABLE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TAIL ROTOR BINDING W A UNSCHED LANDING F FLT CONT AFFECTED HO HOVERING 1 CA (CAN) . THE PILOT WAS ON APPROACH TO AN ISOLATED LANDING SIGHT. DID NOT HAVE FULL TAILROTOR AUTHORITY. HE ABORTED THE L ANDING APPROACH SINCE IT WAS IN A CONFINED AREA & RETURNED BACK TO BASE. LANDED AT THE BASE WITH NO INCIDENT. THE HELICO PTER WAS BROUGHT INSIDE THE BASE HANGAR. THE T/R CONTROL SYSTEM WAS INSPECTED. THE ENGINEERS FOUND THE TAIL ROTOR TELE F LEX CABLE (IN TRAINING MANUAL THE CABLE IS CALLED FLEXIBLE SLIDING BALL TYPE CONTROL) RATCHETY BUT AS THE AIRCRAFT WAS G ETTING TO ROOM TEMPERATURE IT WAS SMOOTHER. THE CABLE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U H9EU E19EU 2002061200022 20020612 00022 SW 2002 6 12 CA020507009 1 20020430 A 6320 205030164073 MOUNT BELL 205A1 BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE M/R GEARBOX CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 30299 (CAN) DURING MAIN ROTOR TRANSMISSION REMOVAL FOUND CRACK EXTENDING FROM LOWER MOST BOLT HOLE OF 5TH MOUNT ATTACHMENT ANG LE, RT SIDE OF TRANSMISSION PYLON AREA.CRACK REPAIRED I.A.W. THE BELL MEDIUM STRUCTURAL REPAIR MANUAL (BHT-MED-SRM-1) SE CTION 4-6-3, "MAIN BEAM ATTACHMENT ANGLE CRACKING". 1 G 7 1 4U 4 U H1SW E17EA 2002061200023 20020612 00023 SW 2002 6 12 CA020507010 1 20020417 A 5320 205030163095 BEAM BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE ENGINE DECK CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) SMALL CRACK FOUND ON TOP "T" CAP OF LT VERTICAL MAIN BEAM ASSEMBLY. CRACK WAS OBSERVED WERE "T" CAP TRANSITIONS FR OM UNDER THE ENGINE DECK GOING FORWARD THROUGH THE AFT SIDE OF THE MAIN ROTOR PYLON AREA.NEW "T" CAP INSTALLED IAW BELL MEDIUM STRUCTURAL REPAIR MANUAL (BHT-MED-SRM-1), SECTION 4-6, PARA B.3, "REPAIR/REPLACEMENT GUIDELINES". 1 G 7 1 4U 4 U H1SW E17EA 2002061200024 20020612 00024 WP 2002 6 12 0201851227 1 20020520 A 5730 SKIN DOUG DC10 DC1030 3023501 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 227NW 46969 During "H" check found crack on LH fixed leading edge skin and stringer doubler at XOS 789.6450 Repaired per EA 12-16222 3. 2 L 7 3 4F A22WE 2002061200025 20020612 00025 WP 2002 6 12 0201861227 1 20020516 A 5340 FITTING DOUG DC10 DC1030 3023501 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 227NW 46969 During "H" check found corrosion at BS 1964 stringer 37L fitting. Repaired per EA 12-162221. 2 L 7 3 4F A22WE 2002061200026 20020612 00026 NM 2002 6 12 0201875507 1 20020514 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 507US 23196 DURING "H" CHECK FOUND CORROSION ON FLOORBEAM AT BS 377 LBL 56-59. REPAIRED PER EA 55-106085. 2 L 7 2 4F RT A2NM 2002061200027 20020612 00027 CE 2002 6 12 2002F00616 1 20020605 A 3230 65216411 BRACKET CESSNA 500 560CESSNA 2076750 CE NLG CRACKED B K NONE O OTHER UK UNKNOWN 1 WP 07 359EJ 948 5600559 FOUND LEFT MAIN GEAR UPLOCK ACTUATOR HOOK BRACKET CRACKED AT ONE OF THE RIVET HOLES ATTACHING IT TO THE FORWARD WHEEL WE LL WALL. 2 L 7 2 4F RT A22CE 2002061200028 20020612 00028 EU 2002 6 12 CA020507011 1 20020425 A 7170 0301047700 VENT LINE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ENGINE CLOGGED W K NONE O OTHER IN INSP/MAINT 1 CA 9241 (CAN) REMOVED VENT TUBE FOR MORE DETAILED INSPECTION AND FOUND THAT THE TUBE WAS PLUGGED SOLID WITH WHAT APPEARED TO BE CARBON. THIS CAUSED THE REAR BEARING NOT VENT PROPERLY.THE COMPANY WILL ADD REMOVAL & INSPECTION OF THIS TUBE TO THE SCH EDULED 500 HOUR ENGINE INSPECTION. 1 G 7 1 3U 3 U H9EU E19EU 2002061200029 20020612 00029 EA 2002 6 12 CA020507012 1 20020425 A 7120 CSP28229 BOLT DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA ENG MOUNT SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ENGINE REMOVAL FROM A TWIN OTTER ONE OF THE TOP FOUR ENGINE MOUNT BOLT SHEARED OFF. THE BOLT SHEARED OFF AT THE AREA WHERE THE SHANK DIAMETER IS REDUCED. THIS BOLT TURNED APPROX. 1/4 TURN AND THEN SHEARED THE HEAD OFF. THIS BOL T WAS POST MODIFICATION (DH)6/1811. 1 H 7 2 3T 4 T RT A9EA E4EA 2002061200030 20020612 00030 EA 2002 6 12 CA020507013 1 20020424 A 7120 CSP28229 BOLT DHAV DHC6 DHC6200 2802620 EA PWA PT6 PT6A20 52043 EA ENGINE MOUNT SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ENGINE REMOVAL OF A PT6A-20 FROM A DHC-6-200, TWO OF THE TWELVE (12) LEFT HAND ENGINE MOUNT BOLT SHEARED OF F. 1 BOLT TOP MOUNT, 1 BOLT R/H SIDE MOUNT. BOTH BOLTS FOUND BROKEN OFF AT AREA WHERE SHANK AREA IS REDUCED . BOTH BOLTS TURNED APPROX 1/4 OF A TURN BEFORE THEY SHEARED. BOTH BOLTS ARE POST MODIFICATION T/1811. BOTH BOLTS APPEARED TO BE PRO PERLY INSTALLED AND NOT BOTTOMED INTO ENGINE CASE. 1 H 7 2 3T 3 T RT A9EA E4EA 2002061200032 20020612 00032 EA 2002 6 12 CA020507014 2 20020428 A 7414 10361631 POINTS BENDIX ROBSIN R44 R44 7640120 WP LYC O540 O540* 41532 EA MAGNETO LOOSE W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) THE POINTS THAT OPEN & CLOSE FOR THE ENGINE TACH IS NOT STAKED PROPERLY CAUSING THE POINTS TO OPEN INTERMITTENTLY, IN TURN THE ENGINE TACH BOUNCES & THE GOVERNOR TO GET ERRATIC INPUT AND GIVE BAD OUTPUT. I HAVE RECEIVED 1 OF THESE BAD POINTS FROM AN OVERHAUL SHOP IN ALBERTA AND 1 FROM AN OVERHAUL SHOP IN B.C. BOTH WITHIN 1 WEEK OF EACH OTHER. 1 G 7 1 3O 3 O H11NM E295 2002061200033 20020612 00033 SW 2002 6 12 CA020507015 1 20020425 A 5302 206020121010 FITTING BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TAILBOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) - FITTING LOOKED CRACKED ON REMOVAL, PART CRACKED IN HALF.- FITTING WAS PRO-SEALED TO TAILBOOM & HAD VERY LITTLE G IVE. 1 G 7 1 3U 3 U H2SW E4CE 2002061200034 20020612 00034 SW 2002 6 12 CA020507017 1 20020405 A 2750 19023 CONTROL CABLE BBAVIA 8 8GCBC 1220803 SW LYC O360 O360C2E 41514 EA TE FLAPS FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LT AND RT UPPER FLAP CABLES FRAYED AT WING ROOT PULLEY. 1 H 7 1 3O 3 O A21CE E286 2002061200037 20020612 00037 SW 2002 6 12 CA020507021 1 20020426 A 3250 STUD GULSTM 500 500S 0141107 SW LYC O540 IO540E1A5 41532 EA NLG STEERING SHEARED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) WHEN THE PILOT SELECTED GEAR DOWN, DID NOT RECEIVE A GREEN NOSE GEAR LIGHT. PILOT DID FLY BYS AND IT WAS NOTED NOS E GEAR WAS NOT IN LOCKED POSITION. PILOT LANDED & NOSE GEAR COLLAPSED WITH MINIMUM DAMAGE. INSPECTION REVEALED THAT P/N 750080-1 SPACER, (THAT ATTACHES STEERING ACTUATOR TO STEERING COLLAR) BOLT WAS SHEARED. THE BOLT IS FASTENED TO THE SPAC ER WITH A ROLL PIN. THE BOLT SHEARED AT THE ROLL PIN. THIS ALLOWED THE STEERING ACTUATOR TO TURN AND JAM UNDER THE NOSE CONE, NOT ALLOWING GEAR TO EXTEND FULLY TO OVER CENTRE.THE SPACER P/N 750080-1 HAS A SERVICE BULLETIN 228 TO CHECK IF ST UD HAS A COTTER PIN HOLE IN IT BUT THERE IS NO MENTION OF CHECKING ROLL PIN ATTACHMENT. 1 H 7 2 3O 3 O 6A1 1E4 2002061200038 20020612 00038 NM 2002 6 12 QXEA0200816 1 20020502 A 5341 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - 2 INCH CRACK IN RADIUS OF FORWARD RT WING TO FUSELAGE CONNECTION ANGLE UNDER PULLEYS BRACKET YW23.85X AND X384.500 . REPAIRED IAW RD 8-53-5192. 2 H 7 2 4T RT A13NM 2002061200040 20020612 00040 NM 2002 6 12 QXEA0200817 1 20020510 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - CHAFING ON FORWARD SPAR OF LT WING AT STATION YW202.000. REPAIRED IAW HORIZON AIR EA 2-57-163. 2 H 7 2 4T RT A13NM 2002061200041 20020612 00041 EU 2002 6 12 CA020507023 1 20020401 A 6320 4619303081 BEARING 4638001001 BOLKMS 105 BO105CBS 5626008 EU ALLSN 250C 250C20B 03013 GL M/R GEARBOX SPALLED W K NONE O OTHER IN INSP/MAINT 1 CA 1120 (CAN) REMOVED FOR METAL CONTAMINATION. DISASSEMBLED OUTER RACE OF BEARING AND IT SHOWS SIGNS OF EXCESSIVE PEELING 14.5 M M BY 78 MM,AREA 1131 SQ MM. 1 G 7 2 3U 3 U NC H3EU E4CE 2002061200042 20020612 00042 NM 2002 6 12 QXEA0200818 1 20020510 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - FRAME IS CHAFED ON INBOARD FLANGE AT X652, Y28R, X111.5. REPAIRED IAW HORIZON AIR EA 2-53-394. 2 H 7 2 4T RT A13NM 2002061200043 20020612 00043 NM 2002 6 12 QXEA0200819 1 20020512 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - MAIN CABIN DOOR THRESHOLD HAS CORROSION ON LOWER SURFACE IN AREA OF NUT PLATES. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002061200044 20020612 00044 NM 2002 6 12 QXEA0200820 1 20020509 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - NR 1 SEAT TRACK CORRODED HAS DEEP PITTING ON INNER SURFACE. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002061200045 20020612 00045 EU 2002 6 12 CA020507024 1 20020327 A 6320 463802024 BEARING 4638001001 BOLKMS 105 BO105CBS 5626008 EU M/R GEARBOX PEELING W K NONE O OTHER IN INSP/MAINT 1 CA 1062 (CAN) THIS TRANSMISSION RECEIVED FROM THE USA. REMOVED DUE TO METAL CONTAMINATION. ROLLER BEARING OUTER RACE SHOWED SIG NS OF EXCESSIVE PEELING. DAMAGE AREA 11 MM LONG BY 50 MM WIDE. 1 G 7 2 3U NC H3EU 2002061200046 20020612 00046 NM 2002 6 12 QXEA0200821 1 20020509 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - NR 12 SEAT TRACK IS CORRODED ON UPPER AND INNER SURFACED. REPAIRED IAW DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002061200047 20020612 00047 NM 2002 6 12 QXEA0200822 1 20020512 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - MAIN CABIN DOOR THRESHOLD HAS CORROSION ON UPPER SURFACE. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002061200048 20020612 00048 NM 2002 6 12 QXEA0200823 1 20020510 A 5312 BULKHEAD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - LOWER PRESSURE BULKHEAD SKIN CHAFED. NOSE LANDING GEAR BAY Z115.50 Y3R Z87. REPAIRED IAW HORIZON AIR EA 2-53-395 . 2 H 7 2 4T RT A13NM 2002061200049 20020612 00049 CE 2002 6 12 CA020508002 1 20020507 A 2761 LMCH3351 ROD LEAR 24170151 LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP ACTUATOR CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 10894 10894 127 (CAN) DURING 12 YEARS MAJOR AIRFRAME INSPECTION, RT WING SPOILER ACTUATOR WAS REMOVED TO GAIN ACCESS TO INSPECT THE RT F LAP ACTUATOR ATACHMENT FITTING. WHEN HANDLING THE SPOILER ACTUATOR FOUND PITTING COROSION ON THE PISTON-ROD (CHROME SURF ACE). NEW PART ORDERED. NEW PART WILL BE INSTALLED. 2 L 7 2 4F 4 F A10CE E6WE 2002061200051 20020612 00051 NM 2002 6 12 QXEA0200824 1 20020511 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - NR 1 ENGINE AFT FIREWALL INBOARD UPPER ANGLE WEB HAS CRACK. REPAIRED IAW HORIZON AIR EA 2-54-141. 2 H 7 2 4T RT A13NM 2002061200053 20020612 00053 NM 2002 6 12 QXEA0200825 1 20020509 A 5712 RIB DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - RT WING RIB AT YW369.0, OUTBOARD SIDE HAS TWO SMALL AREAS OF CORROSION. REPAIRED IAW HORIZON AIR EA 2-57-164. 2 H 7 2 4T RT A13NM 2002061200054 20020612 00054 NM 2002 6 12 QXEA0200826 1 20020514 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - MAIN CABIN DOOR THRESHOLD HAS CORROSION BELOW UPPER THRESHOLD ON UPPER SURFACE OF LOWER STRUCTURE. REPAIRED IAW D HC-8 SRM 51-20-11, PARAGRAPH 3. 2 H 7 2 4T RT A13NM 2002061200056 20020612 00056 EA 2002 6 12 QXEA0200828 1 20020518 A 5270 840506 PROXIMITY SWITCH CNDAIR CL600 CL6002C10 1390015 EA CARGO DOOR FAULTY A QXEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 09 607QX 10024 TUS - AIRCRAFT RETURNED TO FIELD WHEN THE AFT CARGO DOOR CAUTION LIGHT ILLUMINATED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE CARGO DOOR PROXIMITY SWITCH. AN OPERATIONAL CHECK WAS PERFORMED AND CHECKED GOOD. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F RT A21EA 2002061200057 20020612 00057 EA 2002 6 12 QXEA0200829 1 20020520 A 2810 457370 FUEL CAP CNDAIR CL600 CL6002C10 1390015 EA RT WING OPEN A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 609QX 10031 BOI - AIRCRAFT RETURNED TO FIELD WHEN THE RIGHT WING FUEL CAP OPENED IN FLIGHT. MAINTENANCE INSPECTED AND REINSTALLED F UEL CAP. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002061200059 20020612 00059 EU 2002 6 12 QXEA0200831 1 20020520 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU COCKPIT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 BOI- COCKPIT ENTRANCE OVERHEAD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002061200060 20020612 00060 EU 2002 6 12 QXEA0200832 1 20020515 A 3350 900835A BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 498US 11181 PDX- PATH WAY LIGHT ON SEAT ROWS 10-14 ARE INOP. REMOVED AND REPLACED AFT BATTERY CARTRIDGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002061200061 20020612 00061 EU 2002 6 12 QXEA0200833 1 20020515 A 3350 CONNECTOR FOKKER F28 F28MK4000 4990810 EU CABIN DEFECTIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 PDX- PATH WAY LIGHTS ON SEATS AT ROW 5-9 WILL NOT TURN OFF. REMOVED AND REPLACED ELECTRICAL CONNECTOR AT AT SEAT 9. OP ERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002061200062 20020612 00062 NE 2002 6 12 QXEA0200834 2 20020521 A 7200 3038400 ENGINE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 2 MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 345PH 8935 88 476 PDX- AIRCRAFT FILLED WITH SMOKE AFTER BOTH ENGINES WERE STARTED. REMOVED AND REPLACED NR 2 ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002061200063 20020612 00063 NM 2002 6 12 QXEA0200835 1 20020520 A 3260 858601 PSEU DHAV DHC8 DHC8202 2809007 NM NLG FAULTY A QXEA K NONE N FALSE WARNING CL CLIMB 1 NM 09 367PH 9252 9252 511 PDX- NOSE GEAR FAILED TO RETRACT ON DEPARTURE. GEAR RECYCLED PER CHECKLIST. ALL GEAR CAME UP WITH ALL GEAR DOORS CLOSE D. NO INDICATIONS OF PROBLEMS WITH MAIN GEAR. REMOVED AND REPLACED PSEU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061200064 20020612 00064 EU 2002 6 12 QXEA0200836 1 20020522 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 BOI- EMERGENCY EXIT SIGN LIGHT ABOVE PASSENGER CABIN ENTRANCE INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002061200065 20020612 00065 EU 2002 6 12 QXEA0200837 1 20020522 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 BOI- EMERGENCY EXIT SIGN ABOVE CENTER AISLE ROW 8 HAS SEVERAL LIGHTS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPER ATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002061200066 20020612 00066 NM 2002 6 12 QXEA0200838 1 20020525 A 5270 SENSOR BOMBDR DHC8 DHC8401 NM CARGO DOOR OUT OF ADJUST A QXEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 09 414QX 4061 GEG - FLIGHT WAS DIVERTED WHILE EN ROUTE TO SEA FOR A FUSELAGE DOORS WARNING LIGHT. MAINTENANCE INSPECTED AND ADJUSTED THE AFT CARGO DOOR SENSOR IAW AMM 52-31-00 (NO PARTS WERE REPLACED). AN OPERATIONAL CHECK WAS PERFORMED AND SYSTEM TEST ED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061200067 20020612 00067 NM 2002 6 12 QXEA0200795 1 20020430 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX- NR 10 SEAT TRACK CORRODED ON UPPER AND INNER SURFACES AT STATION X391-X394. REPAIRED IAW RD-8 53-1342, SRM 51-40-0 0 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002061200068 20020612 00068 NM 2002 6 12 QXEA0200797 1 20020509 A 7603 FE280000 POWER LEVER BOMBDR DHC8 DHC8401 NM COCKPIT DEFECTIVE A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 402QX 519 4032 MSO- ON TAKEOFF FLIGHT CREW REPORTED, NR 1 POWER LEVER UNABLE TO ADVANCE PAST FLIGHT IDLE. ABORTED TAKEOFF. FERRY FLIG HT TO PDX. REMOVED AND REPLACED POWER LEVER QUADRANT. OPERATIONAL CHECK GOOD, AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061200069 20020612 00069 NE 2002 6 12 QXEA0200799 2 20020512 A 7320 311489201 VALVE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE ENGINE MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 348PH 484 SEA- PILOT COMPLAINED OF SMOKE IN CABIN DURING ENGINE RUN. REMOVED AND REPLACED P2.5-P3 SWITCHING VALVE. RAN ENGINES, NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002061200070 20020612 00070 EA 2002 6 12 QXEA0200800 1 20020511 A 2120 ODOR CNDAIR CL600 CL6002C10 1390015 EA COCKPIT DETECTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 612QX 10042 SMF- ON DESCENT INTO SMF, THERE WAS A HOT PLASTIC SMELL IN THE CABIN AND THOUGH AIR VENTS IN COCKPIT. SMELL DISSIPATED AFTER 5 MINUTES. INSPECTED AIR VENTILATION AND AVIONICS COOLING. NO PARTS REPLACED. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002061200071 20020612 00071 NM 2002 6 12 QXEA0200801 1 20020513 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY FALSE ACTIVATION A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 345PH 476 PDX- ON FLIGHT DOWN TO PDX THE LAVATORY SMOKE DETECTOR WENT OFF. CHECKED LAVATORY FOR FIRE AND SMOKE, NONE WAS DETECTED . SMOKE DETECTOR CHECKS GOOD. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061200072 20020612 00072 EU 2002 6 12 QXEA0200802 1 20020512 A 4960 434897 CONTROL BOX FOKKER F28 F28MK4000 4990810 EU APU MALFUNCTIONED A QXEA K NONE A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 499US * 2425 11182 BOI- TOWER REPORTED PUFF OF SMOKE AND SMALL AMOUNT OF FLAME FROM AREA OF NR 2 ENGINE FOLLOWING TOUCHDOWN. NO ABNORMAL I NDICATIONS ON ENGINE INSTRUMENTS OR APU. REMOVED AND REPLACED START AND OVERSPEED CONTROL BOX. OPERATIONAL CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002061200073 20020612 00073 NM 2002 6 12 QXEA0200803 1 20020515 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 355PH 500 SEA- SMOKE WARNING, MASTER WARNING LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. REMOVED A ND REPLACED NR 2 SMOKE DETECTOR IN CARGO BAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061200074 20020612 00074 EA 2002 6 12 QXEA0200804 1 20020516 A 2824 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA FUEL SYS MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 602QX 10010 PDX- DURING CLIMB, MASTER CAUTION MESSAGE, LEFT TRANSFER SHUTOFF VALVE APPEARED. COMPLIED WITH EMERGENCY CHECK LIST. I NTERROGATED MDC. FOUND LEFT TRANSFER VALVE FAULT, CMP/POS DISAGREE, INTERMITTENT H POSITION. PERFORMED FAULT ISOLATION . FAULT DID NOT REOCCUR. NO PARTS REPLACED. GROUND RAN ENGINES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4F RT A21EA 2002061200075 20020612 00075 NM 2002 6 12 QXEA0200805 1 20020518 A 7931 APT761000100DW TRANSMITTER DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE MALFUNCTIONED A QXEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 NM 09 345PH 4841 476 PDX- DURING CLIMBOUT FROM ARCATA, NR 2 OIL PRESSURE DROPPED TO ZERO PSI THEN RANGED FROM 20-60 PSI, NO MASTER WARNING. NR 2 FUEL TEMP 25 DEGREES, NR 2 OIL TEMP 75 DEGREES. AIRCRAFT WAS DIVERTED TO PDX. REMOVED AND REPLACED NR 2 OIL PRESS URE TRANSMITTER. GROUND RAN AIRCRAFT FOR 10 MINUTES AT HIGH POWER SETTINGS, NO LEAKS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061200076 20020612 00076 NM 2002 6 12 QXEA0200806 1 20020507 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - NUMEROUS SCRATCHES AND GOUGES IN THE LOWER SPAR CAP, RT WING FRONT SPAR LOWER CAP FROM NACELLE TO YW288. REPAIRED IAW RD 8-57-1675. 2 H 7 2 4T RT A13NM 2002061200077 20020612 00077 NM 2002 6 12 QXEA0200807 1 20020507 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - VARIOUS SCRATCHES AND GOUGES IN UPPER FRONT SPAR CAP, RT WING, LEADING EDGE AREA. FRONT SPAR UPPER CAP FROM NACEL LE TO YW288. REPAIRED IAW RD 8-57-1675. 2 H 7 2 4T RT A13NM 2002061200078 20020612 00078 NM 2002 6 12 QXEA0200808 1 20020508 A 3213 STRUT DHAV DHC8 DHC8202 2809007 NM LT MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - LEFT-HAND MAIN LANDING GEAR SHOCK STRUT CHAFED AT UPLOCK HOOK ROLLER LUGS. REPAIRED IAW HORIZON AIR EA 2-32-49. 2 H 7 2 4T RT A13NM 2002061200079 20020612 00079 NM 2002 6 12 QXEA0200809 1 20020507 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - VARIOUS SCRATCHES AND GOUGES IN THE LOWER SPAR CAP. RT WING FRONT SPAR LOWER CAP, FROM NACELLE TO STATION YW288. REPAIRED IAW RD 8-57-2054. 2 H 7 2 4T RT A13NM 2002061200080 20020612 00080 NM 2002 6 12 QXEA0200810 1 20020506 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - SCRATCHES AND GOUGES IN UPPER FRONT SPAR CAP. RT WING LEADING EDGE AREA FRONT SPAR UPPER CAP FROM NACELLE TO STAT ION YW288. REPAIRED IAW RD 8-57-2054. 2 H 7 2 4T RT A13NM 2002061200081 20020612 00081 NM 2002 6 12 QXEA0200811 1 20020508 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - FRONT SPAR CAP HAS BEEN CHAFED BY LEADING EDGE. RT WING INBOARD LEADING EDGE LOWER SPAR CAP AT STATION YW57. REP AIRED IAW RD 8-57-811. 2 H 7 2 4T RT A13NM 2002061200082 20020612 00082 NM 2002 6 12 QXEA0200812 1 20020508 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - MULTIPLE SCRATCHES IN THE LOWER SPAR CAP AND ON THE FORWARD EDGE OF WING SKINS. RT WING LOWER FRONT SPAR CAP BETW EEN FUSELAGE AND NACELLE ADJACENT TO AFT EDGE OF LEADING EDGE. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-57-1150. 2 H 7 2 4T RT A13NM 2002061200083 20020612 00083 NM 2002 6 12 QXEA0200813 1 20020510 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - MULTIPLE SCRATCHES IN UPPER SPAR CAP ON FORWARD EDGES OF WING SKINS. REPAIRED IAW HORIZON AIR EA 2-57-265. 2 H 7 2 4T RT A13NM 2002061200084 20020612 00084 NM 2002 6 12 QXEA0200814 1 20020508 A 5320 WEB DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - WEB CHAFED BY UPPER AFT CORNER OF EMERGENCY EXIT OPENING. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002061200085 20020612 00085 NM 2002 6 12 QXEA0200815 1 20020511 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - NR 1 ENGINE INBOARD MID SPAN FIREWALL CRACKED WHERE IT IS ANGLED. REPAIRED IAW RD 8-54-806. 2 H 7 2 4T RT A13NM 2002061200088 20020612 00088 NM 2002 6 12 QXEA0200839 1 20020523 A 5753 SKIN BOMBDR DHC8 DHC8401 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX- LEFT OUTBOARD FLAP UPPER SKIN HAS CHAFE DAMAGE BETWEEN WING STATIONS YW191.200-YW281.019. REPAIRED IAW RD 8-4-57-0 16 AND HORIZON AIR EA 6-57-17. 2 H 7 2 4T RT A13NM 2002061200089 20020612 00089 NM 2002 6 12 QXEA0200840 1 20020521 A 5330 SKIN PANEL BOMBDR DHC8 DHC8401 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX- TWO NICKS IN SKIN PANEL AT STRINGER 2B STATION X25 AFT AT TOILET SERVICE DOOR. REPAIRED IAW DHC-84 SRM 51-25-05, P G 207, SRM 51-14-00 PG 213, AND SRM 51-21-10. 2 H 7 2 4T RT A13NM 2002061200090 20020612 00090 NM 2002 6 12 QXEA0200841 1 20020521 A 5330 SKIN BOMBDR DHC8 DHC8401 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX- NUMEROUS NICKS AT LOWER FORWARD CORNER OF AFT CARGO DOOR FROM STRINGER 14-22 AND STATION X715-X730. REPAIRED IAW D HC-84 SRM 51-25-05 PG 207, SRM 51-14-00 AND SRM 53-40-31. 2 H 7 2 4T RT A13NM 2002061200091 20020612 00091 EU 2002 6 12 02161309 1 20020610 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 309UE 41022 During preflight inspection, the crew reported that the emergency floor track lights at seat row 3 were inoperative. Ma intenance personnel secured a loose connector for the emergency floor track lights. An operational check was satisfacto ry and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002061200093 20020612 00093 NM 2002 6 12 CA020508009 1 20020508 A 2150 7786832 HEAT EXCHANGER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE A/C SYSTEM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12379 (CAN) DURING ROUTINE INSPECTION A CRACK WAS FOUND ALONG THE INSIDE WELD OF THE PRIMARY INLET HEADER (AMS 4015)REF: HAM S TD CMM 21-51-50 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061200094 20020612 00094 EA 2002 6 12 CA020508010 1 20020216 A 5210 C6FS36265 DOOR DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA FUSELAGE FAILED W C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 CA 28648 (CAN) DURING TAKEOFF ROLL THE CABIN AIRSTAIR DOOR OPENED. AIRCRAFT RETURNED TO THE TERMINAL AND PAX DISEMBARKED. THE AIR STAIR DOOR INSPECTED AND THE TOP FORWARD LATCH PIN WAS FOUND IN THE RETRACTED POSITION. IT IS STILL NOT CLEAR WHAT CAUSE D THE REAR PIN TO RETRACT AND OPEN THE AIRSTAIR DOOR. INVESTIGATION FOUND BADLY CORRODED COTTER PIN ALLOWED THE CLEVIS P IN TO MIGRATE OUTWARD DISCONNECTING THE LATCH PIN FROM THE OPERATING ROD AT THE FORWARD TOP AIRSTAIR DOOR.DOOR PANELS RE MOVED ALL CLEVIS PINS AND COTTER PINS INSPECTED AND FOUND SATISFACTORY. A NEW CLEVIS PIN AND COTTER PIN FITTED AT THE DI SCONNECTED LATCH PIN AND OPERATING ROD. AIRCRAFT RELEASED TO SERVICE. 1 H 7 2 3T 4 T RT A9EA E4EA 2002061200097 20020612 00097 WP 2002 6 12 AALA20020653 1 20020507 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND MULTIPLE DENTS AND IMPROPER DOUBLER INSTALLATION. CUT OUT DAMAGE STATION 190-228 LONGERON 26L, BELOW 28L. INSTALLED DOUBLER PER SRM 53-04 FIG 12C SHEET 5. (M) 2 L 7 2 4F A6WE 2002061200098 20020612 00098 WP 2002 6 12 AALA20020654 1 20020426 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND SCRATCH IN FUSELAGE STATION 690 LONGERON 26L. REPAIRED DAMAGED AREA BY INSTALLING INTERNAL DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2002061200099 20020612 00099 WP 2002 6 12 AALA20020655 1 20020426 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND FUSELAGE SKIN BENT AND GOUGED AT STATION 475 BETWEEN LONGERON 23R AND 25R, AFT SIDE OF FORWARD CARGO DOOR CU TOUT. BLENDED OUT DAMAGED AREA. INSTALLED EXTERNAL DOUBLER REPAIR PER AARD 53-30-00-6, REPAIR 6. (M) 2 L 7 2 4F A6WE 2002061200100 20020612 00100 WP 2002 6 12 AALA20020656 1 20020423 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND DEEP BLENDOUT ON FUSELAGE SKIN STATION 1082 ABOVE LONGERON 11 LEFT, DYE CHECK FOUND CRACKED. ACCOMPLISHED R EPAIR PER SRM 53-04 FIG 38 SHEET 6. INSTALLED RIVET AND SEALED, POLISHED AFFECTED AREA ON SKIN. (M) 2 L 7 2 4F A6WE 2002061200102 20020612 00102 WP 2002 6 12 AALA20020683 1 20020508 A 5320 WEB DOUG DC9 DC981 3022081 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 CORROSION ON BOTTOM SURFACE OF RIGHT CUSP STA 196-199. REMOVED CORROSION FROM RIGHT CUSP, INSTALLED DOUBLER REPAIR PER SRM. 2 L 7 2 4F 4 F A6WE E2EA 2002061200103 20020612 00103 WP 2002 6 12 AALA20020684 1 20020509 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 CRACKS EMITTING FROM FASTENER HOLE AT STA 1380 JUST ABOVE LONG 14L. REPAIRED CRACKS AT FASTENER HOLE STA 1380 ABOVE L14 L BY INSTALLING DOUBLER PER SRM. 2 L 7 2 4F 4 F A6WE E2EA 2002061200104 20020612 00104 WP 2002 6 12 AALA20020685 1 20020424 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND CRACK IN UNDERSIDE OF LEFT CUPS STATION 237. CUT OUT DAMAGED SECTION OF CUSP. INSTALLED DOUBLER REPAIR PER AARD 52-00-00-02 AND SRM 53-01. (M) 2 L 7 2 4F A6WE 2002061200106 20020612 00106 WP 2002 6 12 AALA20020686 1 20020426 A 5311 FRAME DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 FRAME WEB CRACKED AT END OF L 15L. REMOVED CRACKED AREA OF FRAME WEB, INSTALLED STRAP REPAIR PER MM. 2 L 7 2 4F 4 F A6WE E2EA 2002061200107 20020612 00107 WP 2002 6 12 AALA20020687 1 20020503 A 5330 DOUBLER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 WINDOW FRAME CRACKS AT RIGHT 1041 LOWER FORWARD CORNER. INSTALLED DOUBLER PER MM. 2 L 7 2 4F 4 F A6WE E2EA 2002061200109 20020612 00109 WP 2002 6 12 AALA20020688 1 20020507 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 WINDOW FRAME, WINDOW RING PAN CRACKED AT FASTENER. INSTALLED DOUBLER PER MM. 2 L 7 2 4F 4 F A6WE E2EA 2002061200111 20020612 00111 WP 2002 6 12 AALA20020689 1 20020503 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 WINDOW FRAME - WINDOW SHEER TIE CRACKED AT 1079 UPPER AFT, MARKED RIGHT SIDE. CUT OUT DAMAGED AREA PER MM. INSTALLED DO UBLER. 2 L 7 2 4F 4 F A6WE E2EA 2002061200112 20020612 00112 WP 2002 6 12 AALA20020690 1 20020514 A 5320 WEB DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 LOWER DOOR CUT OUT WEB DAMAGED BELOW TIE DOWN TRACK STA 1151. REPLACED WEB PER SRM. 2 L 7 2 4F 4 F A6WE E2EA 2002061200113 20020612 00113 WP 2002 6 12 AALA20020691 1 20020502 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 CORROSION, NR 6 SEAT TRACK AROUND FASTENER HOLE AT STA 1003. INSTALLED STRAP ON SEAT TRACK FLANGE PER AARD. 2 L 7 2 4F 4 F A6WE E2EA 2002061200114 20020612 00114 WP 2002 6 12 AALA20020692 1 20020508 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 FLOORBOARD ATTACH FASTENERS AND INSERTS CORRODED, FLOORBOARD OUTBOARD FO RIGHT SEAT TRACK STA 148 (FORWARD OF FORWARD GA LLEY). COMPLETED INSTALLATION OF STRAP AND FILLER. 2 L 7 2 4F 4 F A6WE E2EA 2002061200115 20020612 00115 WP 2002 6 12 AALA20020693 1 20020402 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 NR 3 SEAT TRACK CORROSION OUTBOARD LEG AT NUT PLATE STA 1235. INSTALLED STRAP ON SEAT TRACK FLANGE FOR AARD. 2 L 7 2 4F 4 F A6WE E2EA 2002061200116 20020612 00116 WP 2002 6 12 AALA20020694 1 20020508 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 CRACKS EMITTING FROM FASTENER HOLE AT STA 1380 ABOVE L14R. DAMAGED AREA OF SKIN, INSTALLED DOUBLER PER SRM. 2 L 7 2 4F 4 F A6WE E2EA 2002061200117 20020612 00117 WP 2002 6 12 AALA20020695 1 20020508 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 FOUND DENT APPROX 3 FEET AFT OF FORWARD ENTRY DOOR APPROX 1 INCH IN DIAMETER AND .050 DEEP. DAMAGED SKIN REMOVED, REPAI R DOUBLER INSTALLED PER SRM 53-04 FIG 12C. (M) 2 L 7 2 4F A6WE 2002061200118 20020612 00118 WP 2002 6 12 AALA22020681 1 20020502 A 5320 WEB DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 CRACKED ABOUT STA 173 ABOUT 19 INCHES FROM FORWARD ENTRY DOOR OPENING. INSTALLED REPAIR DOUBLER PER SRM. 2 L 7 2 4F 4 F A6WE E2EA 2002061200119 20020612 00119 WP 2002 6 12 AALA22020682 1 20020502 A 5320 WEB DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 CORROSION ON CUSP AT STA 680 RIGHT SIDE. BLENDED OUT CORROSION AND INSTALLED DOUBLER PER SRM. 2 L 7 2 4F 4 F A6WE E2EA 2002061200122 20020612 00122 EA 2002 6 12 COMA0260364 1 20020608 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 466CA 127 7627 FLIGHT 5324 FLAPS FAILED AT GATE WHEN SELECTED TO 20 DEGREES.REPLACED THE L/H BPSU. 2 L 7 2 4F RT A21EA 2002061200124 20020612 00124 EA 2002 6 12 COMA0260365 1 20020608 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 708CA 7235 FLIGHT 5860 FWD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP.CLEANED AND RESEATED WIRE CONNECTION. 2 L 7 2 4F RT A21EA 2002061200125 20020612 00125 EA 2002 6 12 COMA0260366 1 20020609 A 3230 16215 BRACKET CNDAIR CL600 CL6002B19 1900309 EA NLG BENT A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 446CA 7546 FLIGHT 5127 NLG WILL NOT RETRACT.STRAIGHTENED NLG CENTERED SENSOR BRACKET. 2 L 7 2 4F RT A21EA 2002061200126 20020612 00126 EA 2002 6 12 COMA0260367 1 20020610 A 2700 AILERON CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 01 978CA 7158 FLIGHT 5224 AIRCRAFT HAS A TENDENCY TO ROLL RIGHT DURING FLIGHT MOST NOTICEABLE DURING APPROACH.INSPECTED A/C AND FOUND NOTHING THAT WOULD RELATE TO A ROLL TENDENCY. 2 L 7 2 4F RT A21EA 2002061200127 20020612 00127 EU 2002 6 12 MALA020332 1 20020607 A 2560 LIFE VEST BAC 146 AVRO146RJ85A 1500097 EU A MALA K NONE P NO WARNING INDICATION NR NOT REPORTED 1 GL 15 513XJ E2329 DURING FLIGHT #3651, LIFE VEST IS MISSING AT SEAT 1A. SEATS 3E AND 4B LIFE VESTS ARE ON FLOOR. MAINTENANCE REPLACED LIF E VESTS AT SEATS 1A, 3E, AND 4B. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2002061200128 20020612 00128 NM 2002 6 12 CA020509003 1 20020507 A 2910 340545 VALVE BOEING 767 767375 1385217 NM GE CF6 CF680C2B6F 30025 NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING A M01 CHECK THE LEFT AND RIGHT HYDRAULIC SYSTEM EMPENNAGE FLIGHT CONTROL SHUTOFF VALVES WERE FOUND LEAKING. AFTER INVEASTIGATION , ONE OF THE L/H BOLT WAS SHEARED WHILE OTHERS WERE ENGAGED ONLY WITH A COUPLE OF THREADS. SIMILAR FINDINGS WERE FOUND ON A PREVIOUS AIRCRAFT. 2 L 7 2 4F 4 F RT A1NM E13NE 2002061200129 20020612 00129 NM 2002 6 12 CA020509004 1 20020110 A 3230 PSEU DHAV DHC8 DHC8* NM PWC 150 PW150A EA RT GEAR DOOR FAILED W O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA (CAN) GEAR MALFUNCTION DURING CRUISE AT FT 180, SEVERAL MAIN GEAR DOOR WARNING IN TRANSITION & RT HAND RED LIGHT OBNSERV ED ONE TIME. AT SAME TIME A/C SHAKING. SPEED REDUCED TO 200 KTS GEAR SPEED. EVENT MARKER PUSHED, THEN NO FURTHER EVENTS ON REST OF FLT. PROX SENSOR RIGGING FOR LDG GEAR SYS CHECKED VIA PROX SENSOR ELECTRONIC UNIT (PSEU). RT GEAR DOOR CLOSED SENSOR ADJUSTED ACC AMM 32-61-01. RT GEAR UPLOCK SENSOR REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061200130 20020612 00130 NM 2002 6 12 CA020509005 1 20020131 A 5270 82420109035 SENSOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA DOOR LOCK FAILED W O OTHER N FALSE WARNING CR CRUISE 1 CA (CAN) CARGO DOOR WARNING LIGHT ON DURING FLIGHT - INTERMITTENT. SYSTEM CHECKED WITHOUT ANY FINDINGS AFTER READ-OUT OF P SEU. PROBLEM RE-OCCURRED ON 04 FEB 2002 AND A WIRE FAULT WAS FOUND ON THE AFT BAGGAGE DOOR LOCK SENSOR. THE SENSOR WAS R EPLACED TO RECTIFY THE FAULT. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061200131 20020612 00131 NM 2002 6 12 CA020509006 1 20020122 A 5270 SENSOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA DOOR WARNING FROZEN W O OTHER J WARNING INDICATION DE DESCENT 1 CA (CAN) DOOR WARNINGS: 6000 FEET IN DESCENT, DOOR WARNING FOR RT AFT SERVICE DOOR, AT SAME TIME HAD LIGHT TO MODERATE TU RBULENCE. WARNING DISAPPEARED JUST BEFORE LDG. UPON ARRIAL, DOOR SENSOR LUBRICATED & RIGGING OF DOOR CHECKED W/O REMARKS . SAME PROBLEM APPEARED ON PREVIOUS DAY WITH EXACT SAME SYMPTOMS & DURING SAME STAGE OF FLT. SIX DAYS LATER, PROBLEM REA PPEARED & AGAIN ON 7TH DAY AFTER REPORTED INCIDENT DURING LAST 2 INCIDENTS, ICE REPORTED ON DOOR SENSOR & ADJUSTMENT PER FORMED, DUE TO SENSOR INDICATING FAR. SENSOR CLEANED, LUBRICATED&ADJUSTED. AFTER THAT, DOOR DID NOT GET WARNING UNTIL 19 FEB 2002, WHERE ICE AGAIN REMOVED FROM SENSOR. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061200133 20020612 00133 NM 2002 6 12 CA020509007 1 20020123 A 5270 85230535101 SPRING DHAV DHC8 DHC8* NM PWC 150 PW150A EA CARGO DOOR FROZEN W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA (CAN) AT 5000 FT CLIMBING WE RECEIVED "FUSELAGE DOOR" WARNING. CHECK ON MFD SYS P. DOORS INDICATED THAT AFT CARGO DOOR U NSAFE. PERFORMED NORMAL & ABNORMAL CHECKLISTS & THEN RETURNED UNEVENTFULLY. DOOR WARNING REMAINED ON ALL WAY IN TO PAR KING STAND. CREW & PASSENGERS DEBRIEFED AS NORMAL. VISUAL INSP OF CARGO DOOR AFTER LDG DID NOT REVEAL ANY EXTERIOR MALFS . MAINT INESTIGATION REVEALED CARGO DOOR CLOSED SWITCH FOUND STUCK. SWITCH LUBRICATEDAND SYS TESTED W/O FURTHER REMARKS. A/C RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061200134 20020612 00134 NM 2002 6 12 CA020509008 1 20020127 A 2780 PRESSURE SWITCH DHAV DHC8 DHC8* NM PWC 150 PW150A EA FLAP PWR UNIT FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) WHEN SELECTING FLAP 5 INBOUND ON FINAL APPROX. 3700 FT "FLAP POWER" CAUTION LIGHT CAME ON. RE-SET THE SYSTEM ACCOR DING TO CREW BULLETIN 02/01 UNSUCCESSFULLY. CARRIED OUT 0 DEG. FLAP LANDING. DURING TOUBLESHOOTING THE FLAP POWER UNIT WAS FOUND DEFECT AND THE UNIT WAS REPLACED. FLAP POWER AND FLAP DRIVE WARNINGS WERE RECEIVED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061200135 20020612 00135 NM 2002 6 12 CA020509009 1 20020504 A 2910 829700175 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM BROKEN W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 31626 (CAN) CREW NOTICED LEAK DRIPPING ONTO LT MLG TIRE. MAINTENANCE TRACED LEAK TO NR 2 SYSTEM DOOR OPEN HYDRAULIC TUBE ASSY BROKEN. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061200137 20020612 00137 NM 2002 6 12 CA020509010 1 20020205 A 3297 471515 HARNESS DHAV DHC8 DHC8* NM PWC 150 PW150A EA NLG SHORTED W O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 CA (CAN) AFTER GEAR UP SELECTION WE GOT 3 GREEN, 3 RED, AND LIGHT IN GEAR HANDLE. ABNORMAL CHECKLIST: ALTERNATE LANDING GE AR EXTENSION PERFORMED. AIRCRAFT LANDED UNEENTFULLY. PAX BRIEFING IN AIRCRAFT. MAINTENANCE INVESTIGATION DETERMINED THE NOSE WHEEL CENTERING SENSOR WIRES WERE FOUND LEAKING TO GROUND. THE WIRE HARNESS ASSEMBLY P/N 47151-5 WAS REPLACED. LAND ING GEAR RETRACTION/EXTENSION CHECKED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061200139 20020612 00139 NM 2002 6 12 CA020509011 1 20020128 A 5270 PROXIMITY SENSOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA PROX.SENSR SPRNG FROZEN W O OTHER N FALSE WARNING DE DESCENT 1 CA (CAN) DOOR WARNING - L2 DOOR DURING APPROACH DOOR WARNING LIGHT ON FOR 30 SEC. ON DOOR L2. DOOR CHECKED BY MAIANTENANCE AND FOUND OK. AIRCRAFT WAS RELEASED ON OPERATIONAL ACCEPTANCE BASED ON TECHNICAL ADVISE FROM TECHNICAL CONTROL CENTRE. THE PROXIMITY SENSOR WAS CLEANED FOR WATER. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002110400099 20021104 00099 NE 2002 11 4 2002UALA00944 2 20020602 A 7261 AC9806F30Y1 OIL FILTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE OBSTRUCTED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 513UA 292 24810 727201 RIGHT ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. BOTH THE DELTA "P" SWITCH AND THE FILTER WERE FORWARDED TO PWA FOR IN VESTIGATION. THE SWITCH WAS FOUND TO BE TO BE WITHIN OPERATIONAL LIMITS. THE FILTER WAS SENT TO THE PWA LAB AND FOUND TO CONTAIN SUB MICRON CARBON PARTICLES, BUT IT WAS NOT 100% PLUGGED. AT THIS TIME IT IS BELIEVED THAT THE CARBON IN THE FILTER WAS THE ROOT CAUSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072200041 20020722 00041 NE 2002 7 22 2002UALA00945 2 20020601 A 7230 6A4198 BLADE AIRBUS A319 A319131 3930317 NM IAE V2527 V2527A5 NE NR 1 ENGINE FRACTURED A UALA A UNSCHED LANDING R Y PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CL CLIMB 1 WP 29 822UA 1629 948 V10372 RETURNED TO FIELD DUE TO NR 1 ENGINE COMPRESSOR STALL. CAUSE OF STALL WAS FOUND TO BE LIBERATED SECTION OF HIGH PRESSUR E COMPRESSOR (HPC) 5TH STAGE BLADE. LIBERATION CAUSED DOWNSTREAM DAMAGE, INCREASED TIP CLEARANCE, AND REDUCED SURGE MAR GIN OF HPC TO STALL POINT. 2 L 7 2 4F 4 F RT A28NM E40NE 2002061200143 20020612 00143 NM 2002 6 12 2002UALA00946 1 20020531 A 5553 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 VERTICAL STABILIZER STATION 1016 FIN TERMINAL FITTING CORRODED. MAJOR REPAIR ACCOMPLISHED. CORROSION REMOVED AND FITTI NG REWORKED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002061200144 20020612 00144 NM 2002 6 12 2002UALA00947 1 20020602 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 FORWARD CABIN FLOOR STATION 365 BL 0 THROUGH RBL 65 UPPER T-CAP IS GOUGED AND CORRODED. MAJOR REPAIR ACCOMPLISHED. SP LICED IN REPAIR CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002061200145 20020612 00145 NM 2002 6 12 2002UALA00949 1 20020531 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 AFT PIT STATION 1480 FRAME UPPER CHORD HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002061200146 20020612 00146 NM 2002 6 12 2002UALA00950 1 20020603 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 936UA 26667 EXTERNAL FUSELAGE SKIN DENTED AT APPROXIMATELY STATION 340 JUST ABOVE STRINGER 16L. MAJOR REPAIR ACCOMPLISHED. FABRICA TED AND INSTALLED DOUBLER AND FILLER. TYPICAL SPLICE REPAIR WAS USED AT BUTT JOINT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002061200147 20020612 00147 NM 2002 6 12 2002UALA00951 1 20020603 A 5210 5093692 SEAL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE L1 DOOR DAMAGED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 927UA 26649 VERY LOUD PRESSURE LEAK AT DOOR 1L. FOUND PRESSURE SEAL DAMAGED IN LOWER FORWARD CORNER OF DOOR. SEAL REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002061200148 20020612 00148 NM 2002 6 12 2002UALA00952 1 20020603 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 CABIN AFT FRAME STATION 1681 STRINGER 17R RBL 57 I/B CAP EXFOLIATED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPA IR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072200044 20020722 00044 2002 7 22 2002UALA00953 4 20020604 A 3460 4058650931 CDU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 650UA 25287 RIGHT MULTIFUNCTION CONTROL DISPLAY UNIT FAILED. RIGHT FMC HMCDU FAIL. REPLACED THE RIGHT HMCDU. 2 L 7 2 4F 4 F RT A1NM E24NE 2002061200149 20020612 00149 NM 2002 6 12 2002UALA00954 1 20020604 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 EXCESSIVE MATERIAL REMOVED FOR CORROSION CLEAN UP AT BODY STATION 1640 RBL 14. MAJOR REPAIR ACCOMPLISHED. STRAP DOUBLE R INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002061200150 20020612 00150 NM 2002 6 12 2002UALA00956 1 20020604 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 DENT ON FRAME-SKIN SPLICE AT STA 1620 FWD OF NR 3L ENTRY DOOR AT FLOOR LEVEL. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAI R ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002061200151 20020612 00151 WP 2002 6 12 2002F00604 1 20020326 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND CABIN RIGHT GALLEY AFT OF SERVICE DOOR G-2, OUTBOARD SIDE HAS CORROSION AT FLOOR AREA. REMOVED DAMAGED AREA . FABRICATED REPAIR PARTS, INSTALLED REPAIR. (M) 2 L 7 2 4F A6WE 2002061200152 20020612 00152 WP 2002 6 12 AALA20020657 1 20020509 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND SKIN GOUGE STATION 620 BELOW LONGERON 19 RIGHT. INSTALLED DOUBLER PER ESO 80559 DATED 4-30-02. (M) 2 L 7 2 4F A6WE 2002061200153 20020612 00153 WP 2002 6 12 AALA20020658 1 20020508 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND GOUGE IN SHEAR TIE LONGERON 23 LEFT STATION 522. CUT OUT DAMAGE AND INSTALLED SHEAR TIE REPAIR PER SRM 53-0 3 FIGURE 6 SHEET 1. (M) 2 L 7 2 4F A6WE 2002061200154 20020612 00154 WP 2002 6 12 AALA20020659 1 20020420 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND CORROSION ON TOP AND INSIDE OF NR 2 SEAT TRACK, STATION 1200. CUT OUT CORRODED AREA, INSTALLED REPAIR PLUG PER SRM 53-05, FIG 4A. (M) 2 L 7 2 4F A6WE 2002061200155 20020612 00155 WP 2002 6 12 AALA20020660 1 20020422 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND CRACK IN LONGERON 3L AT STATION 160. INSTALLED NEW LONGERON SECTION WITH SPLICE IAW SRM 53-02 FIG 18 SHEETS 1, 4, 5 AND 6 AND AARD 53-00-00-05. (M) 2 L 7 2 4F A6WE 2002061200156 20020612 00156 WP 2002 6 12 AALA20020661 1 20020420 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND CORROSION ON TOP OF NR 2 SEAT TRACK, STATION 1300. CUT OUT CORRODED AREA. INSTALLED REPAIR PLUG PER SRM 53 -05, FIG 4A. (M) 2 L 7 2 4F A6WE 2002061200157 20020612 00157 WP 2002 6 12 AALA20020663 1 20020423 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND CUSP MEMBRANE FASTENERS HOLE CRACKED OUT UNDER NR 5 SEAT TRACK, FS 243.5. REMOVED CRACK, REPAIRED CUSP MEMB RANE PER AARD 53-00-00-02, PAGE 1 ITEM 2. (M) 2 L 7 2 4F A6WE 2002061200158 20020612 00158 WP 2002 6 12 AALA20020664 1 20020424 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND NR 5 SEAT TRACK CORRODED AT STATION 200. REMOVED CORRODED TRACK. INSTALLED NEW TRACK NR 5 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002061200159 20020612 00159 WP 2002 6 12 AALA20020666 1 20020429 A 5320 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND CORROSION AT LEFT TIE DOWN TRACK SPLICE STATION 1225. REMOVED AND REPLACED SPLICE, SRM 51-01. (M) 2 L 7 2 4F A6WE 2002061200160 20020612 00160 WP 2002 6 12 AALA20020667 1 20020426 A 2720 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP RUDDER CONTROL CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - RUDDER CONTROL SUPPORT BRACKET CRACKED AT RACE AREA. INSTALLED NEW BRACKET ASSEMBLY SRM 51-01. (M) 2 L 7 2 4F A6WE 2002061200161 20020612 00161 WP 2002 6 12 AALA20020668 1 20020423 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND CRACK IN STIFFENER AT UPPER MOST RIVET ABOVE THE AFT ENTRY DOOR. REMOVED CRACKED STIFFENER. INSTALLED NEW STIFFENER PER SRM 51-00. (M) 2 L 7 2 4F A6WE 2002061200162 20020612 00162 WP 2002 6 12 AALA20020669 1 20020423 A 5345 FITTING DOUG DC9 DC982 3022082 WP FUSELGAE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND G2 LOWER INBOARD TIEDOWN FITTING AT STATION 218 IS CORRODED, FITTING BELOW DIAPHRAGM SUB FLOOR. INSTALLED N EW G-2 INBOARD LOWER TIE DOWN FITTING STATION 217-218, SRM 51-01 (2C), 51-10-04 AND 51-30-05. (M) 2 L 7 2 4F A6WE 2002061200163 20020612 00163 WP 2002 6 12 AALA20020696 1 20020502 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 TUL - FOUND 15 INCH LONG DEPRESSION .125 INCH DEEP ADJACENT TO FORWARD DRAIN MAST ON RIGHT SIDE OF FUSELAGE. INSTALLED INTERNAL DOUBLER STATION 218 BETWEEN RIGHT L27 TO 26 PER SRM 53-04 FIG 38 SHEET 30 VIEW P ADJACENT TO FORWARD DRAIN MAST . (M) 2 L 7 2 4F A6WE 2002061200164 20020612 00164 WP 2002 6 12 AALA20020697 1 20020429 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 TUL - FOUND SCRATCH WITH DENT STATION 154-155.5 LEFT FUSELAGE SKIN BELOW STRAKE. REPAIRED PER SRM 53-04 FIG 38 SHT 20. (M) 2 L 7 2 4F A6WE 2002061200165 20020612 00165 WP 2002 6 12 AALA20020698 1 20020430 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 TUL - FOUND NR 2 SEAT TRACK CORRODED. REPLACED NR 2 SEAT TRACK STATION 1185-1309 PER AARD 51-60-00-08. (M) 2 L 7 2 4F A6WE 2002061200166 20020612 00166 NM 2002 6 12 0201886716 1 20020523 A 5330 SKIN BOEING 747 747251F 1384898 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 616US 21120 During "L" check found crack in the fuselage skin and bonded doubler at aft cargo door cutout. Repaired per EA 67-189583 . 2 L 7 4 4F A20WE 2002061200167 20020612 00167 NM 2002 6 12 0201895507 1 20020603 A 5311 STRINGER BOEING 757 757251 1384970 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 507US 23196 During "H" check found cracks in BS 660 stringers 11R and 11L and 14R and 14L. Repaired per EA-191087. 2 L 7 2 4F RT A2NM 2002061200168 20020612 00168 WP 2002 6 12 IXXA0200030S 1 20020225 A 5700 WING DOUG DC8 DC862 3021970 WP LT WING L/E CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 799AL 70276 2993 45922 DURING ROUTINE C-CHECK INSPECTION CORROSION WAS DETECTED AROUND THREE SCREW HOLES ON THE LEFT WING OUTBOARD LEADING EDGE AT STATION XFS 885. REPAIR ACCOMPLISHED, REMOVAL OF THE CORROSION, FACRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL MAINTENANCE MANUAL. 2 L 7 4 4F 4A25 2002061200169 20020612 00169 WP 2002 6 12 IXXA0200031S 1 20020226 A 5700 WING DOUG DC8 DC862 3021970 WP LEFT WING CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 799AL 70276 2993 45922 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AROUND SCREW HEADS ON THE LEFT WING OUTBOARD LEADING EDGE XFS8 92 TO XFS930. REPAIR ACCOMPLISHED REMOVAL OF THE CORROSION, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL MAINTENANCE MANUAL. 2 L 7 4 4F 4A25 2002061200170 20020612 00170 WP 2002 6 12 IXXA0200032S 1 20020306 A 5240 THRESHOLD DOUG DC8 DC862 3021970 WP C-1 DOOR CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 799AL 70276 2993 45922 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE C-1 DOOR UNDER THE THRESHOLD PLATE. REPAIR ACCOMPLISHE D REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR FILLER AND DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTUR AL MAINTENANCE MANUAL. 2 L 7 4 4F 4A25 2002061200171 20020612 00171 WP 2002 6 12 IXXA0200033S 1 20020306 A 5751 AILERON DOUG DC8 DC862 3021970 WP OB WING CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 799AL 70276 2993 45922 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING OUTBOARD AILERON INBOARD SIDE LOWER PLATING. R EPAIR ACCOMPLISHED, DAMAGED AREA CUT OUT, FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002061200172 20020612 00172 WP 2002 6 12 IXXA0200034S 1 20020307 A 5313 LONGERON DOUG DC8 DC862 3021970 WP STA 500 DENTED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 799AL 70276 2993 45922 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE EXTERNAL PLATING AT FUSELAGE STATION 480 AT STRINGER 21L. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND EXTERNAL REPAIR DO UBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL MAINTENANCE MANUAL AND ENGINEERING DIRECTIVE EDP82-1. 2 L 7 4 4F 4A25 2002061200173 20020612 00173 WP 2002 6 12 IXXA0200035S 1 20020316 A 5240 DOOR FRAME DOUG DC8 DC862 3021970 WP AFT SERVICE CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 799AL 70276 2993 45922 DURING ROUTINE C-CHECK INSPECTION, CORROSION AND CRACKS WERE DETECTED ALONG THE LOWER EDGE OF THE FUSELAGE AFT SERVICE D OOR AND DOOR FRAME BETWEEN LONGERONS 16 AND 17 AT AXXPRXIMATE FS1500. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABR ICATION AND INSTALLATION OF REPAIR DOUBLERS IN ACCORDANCE WITH DOUGLAS STRUCTURAL MAINTENANCE MANUAL AND ENGINEERING DIR ECTIVE EDP82-2. 2 L 7 4 4F 4A25 2002061200174 20020612 00174 WP 2002 6 12 IXXA0200037S 1 20020325 A 5200 DOOR DOUG DC8 DC862 3021970 WP FWD ENTRANCE CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 799AL 70276 2993 45922 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED UNDER A TEMPORARY REPAIR OF THE FORWARD ENTRANCE DOOR CUTOUT FOR WARD UPPER CORNER. REPAIR ACCOMPLSISHED REMOVAL OF THE TEMPORART REPAIR AND DAMAGED AREA. FABRICATED AND INSTALLED REP AIR FILLER AND EXTERNAL DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002061200176 20020612 00176 NM 2002 6 12 CALA0200335 1 20020610 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 907-935 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69348 23586 INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 907-935. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-60-52. 2 L 7 2 4F RT A16WE 2002061200177 20020612 00177 NM 2002 6 12 CALA0200337 1 20020612 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 907-940 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69348 23586 INSPECTION FOUND L/H I/B SEAT TRACK CORRODED AT STA 907-940. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2002061200178 20020612 00178 NM 2002 6 12 CA020509014 1 20020202 A 2742 ACTUATOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA PITCH TRIM FAILED W O OTHER O OTHER CL CLIMB 1 CA (CAN) DURING CLIMB OUT PITCH TRIM CAUTION LIGHT ILLUMINATED, AUTO TRIM FAIL MESSAGE ON PFD & TRIM INDICATOR FULLY NOSE U P. FAULTS LOGGED IN CDS: 67,E7,63,E3,ED,EE. SPEED APPROX 185 KTS. FLT OPERATED MANUALLY. UNEVENTFUL APPROACH & LANDING. TROUBLESHOOTING REVEALED GIVEN FAULTS LOGGED IN CDS SUGGEST PITCH TRIM RUNAWAY & FULLY NOSE UP INDICATOR. ON ELEVATOR TR IM INDICATOR SHOWS THAT LEFT PITCH TRIM ACTUATOR FAILED. INSPECTION OF THIS, NO SUBSEQUENT FAULTS HAVE OCCURRED ON SYS & INCID. IS THEREFORE REGARDED AS ONE-TIME EVENT, PROBABLY CAUSED BY MOISTURE IN LVDT PLUG FOR LT PITCH TRIM UNIT OR PLUG ON FCECU FROM LT PITCH TRIM UNIT. A/C RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061200180 20020612 00180 NM 2002 6 12 CA020510001 1 20020211 A 7540 8201003003 CONTROL UNIT HAMSTD 8201003003 DHAV DHC8 DHC8* NM PWC 150 PW150A EA BLEED AIR FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 98119797 (CAN) NR 1 AND NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED AFTER TAKEOFF. AFTER LANDING, PERFORMED INSPECTION BY MAINTENAN CE. NR 1 AND 2 BLEED HOT CAUTION LIGHT ILLUMINATED AFTER TAKEOFF WITHOUT BLEEDS SELECTED. FAULT CODES (L/CH AND R/CH 700 8, 4109, 7004, 3102).ECSECU REPLACED, OPS CHECK CARRIED OUT. FULL POWER ENGINE RUNS PERFORMED. AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061300001 20020613 00001 SO 2002 6 13 C2XA02TY100 1 20020612 A 5101 14521725001 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FWD CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 TYS During a scheduled inspection the left hand sidewall floor support at station 5292.0 was found to be corroded in s everal areas. Maintenance removed and replaced the flooor support IAW EMB-145 SRM 51-40-02, the repair was satisfactory . The aircraft will be released upon completion of inspection. 2 L 7 2 4F RT T00011AT 2002061300002 20020613 00002 NM 2002 6 13 ANCF200200011 1 20020609 A 2170 3212000590 COALESCER BAG DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE AIR CONDITIONING DIRTY W ANCF A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 23 632CT 49632 AFTER TAKE OFF A STRONG SMOKE SMELL WAS PRESENTED IN THE COCKPIT, INMEDIATELY, THE CABIN SUPPERVISOR INFORMED THAT THERE WAS A STRONG SMOKE SMELL ALONG THE PASSENGER CABIN, SPECIALLY IN THE REAR SECTION. THERE WAS NOT FUMES NOR FIRE VISIBLE AT ANY MOMENT. WE RETURNED INMEDIATELY TO THE AIRPORT IN VISUAL CONDITIONS IN ORDER TO LAND AS SOON AS POSIBLE. COALESC ER BAGS OF AIR CONDITIONING WATER SEPARADTOR WERE CLEANED IAW AMM 21-20-02 PAGE 202. WAS PERFORMED ENGINE RUN-UP TEST BY ONE HOUR WITH SATISFACTORY TEST IAW AMM 71-00-00 PAG BLOCK 501. 2 L 7 2 4F 4 F RT E9NE 2002061300003 20020613 00003 NM 2002 6 13 CA020510002 1 20020404 A 7933 304814801 SENSOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA OIL TEMP FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) DURING TAXI,, LOSS OF NR 1 ENGINE OIL TEMPERATURE INDICATION. A/C RETURNED TO RAMP AND HANDED OVER TO MAINTENANCE. FAULT CODE READ OUT CARRIED OUT ON ARCDU. FAULT CODES 721 AND 737. OIL TEMPERATURE SENSOR REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061300004 20020613 00004 NM 2002 6 13 CA020510003 1 20020305 A 2730 CONTROL UNIT DHAV DHC8 DHC8* NM PWC 150 PW150A EA ELE PITCH TRIM FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) PITCH TRIM CAUTION LIGHT ILLUMINATED AND AUTO TRIM FAIL MESSAGE DISPLAYED ON ED WITH A LOSS OF TRIM FUNCTION DURIN G CRUISE. PILOT DIVERTED TO BASE. SERVICE LETTER SL-27-003 CARRIED OUT BY MAINTENANCE PERSONNEL AND THE AIRCRAFT WAS RET URNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061300005 20020613 00005 NM 2002 6 13 CA020510004 1 20020426 A 2721 682015 SWITCH DHAV DHC8 DHC8* NM PWC 150 PW150A EA RUDDER TRIM FAILED W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE FLIGHT AT FLIGHT LEEL 190 THE CREW EXPERIENCED A RUNAWAY RUDDER TRIM ACTUATOR WITH A FULL RIGHT DEFL ECTION. RUDDER TRIM INDICATOR WAS NEUTRALIZED BY THE CREW AND THE RUDDER TRIM ACTUATOR CB F7 WAS PULLED ACCORDING TO THE EMERGENCY CHECKLIST. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061300006 20020613 00006 2002 6 13 CA020510005 4 20020318 A 6122 GOVERNOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA PROPELLER DAMAGED W E ENGINE SHUTDOWN F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 CA (CAN) ON MAR 18, 2002, CREW EXPERIENCED FLUCTUATING NP&TQ, POWERPLANT MESSAGE & PEC NR 1 CAUTION LIGHT WERE PRESENTED. W HEN POWER REDUCED, FOR DESCENT, NR 1 NP OVERSPEED. ENGINE SHUTDOWN. UNEVENTFUL LDG ACCOMPLISHED. FAULT CODES 719,939,998 ,718,161&999 REPORTED. PCU & PEC WERE REPLACED. FAULT CODES REMAINED. MPU PROBE REPLACED & ENGINE BEING GROUND RUN TO COMPLY WITH PROCS REQD FOLLOWING PEC & PCU REPLACED. MAINT RAN ENGINE & ABOUT 2 MINS INTO RUN ANOTHER INCIDENT OCCURRED. ENGINE AT DETENT POWER, WHEN LARGE BANG HEARD, FOLLOWED BY FIRE WARNING. ENGINE SHUTDOWN, & 1ST FIRE BOTTLE DISCHARGED. SOME TIME LATER ESTIMATED TO BE 30 SECONDS, FIRE WARNING STILL APPARENT. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061300007 20020613 00007 NM 2002 6 13 CA020510006 1 20020405 A 3320 404820 SOCKET DHAV DHC8 DHC8* NM PWC 150 PW150A EA LIGHT MELTED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) BURNED PLASTIC SMELL FROM LAVATORY. LAMP HOLDER FOUND MELTED. UPPER CONTACT AREA. LAMP HOLDER REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061300008 20020613 00008 EA 2002 6 13 CA020510011 2 20020502 A 7310 120980210 LINE PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA FUEL SYSTEM BENT W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING COMPLIANCE WITH AD 93-02-05 (FUEL INJECTION)TUBE WAS FOUND BENT, AFTER REMOAL, TUBE WAS FOUND WORN TOO. IT WAS NOT CHAFING ON OTHER COMPONENT. 1 L 7 2 3O 3 O 1A10 1E4 2002061300009 20020613 00009 EA 2002 6 13 CA020510012 1 20020429 A 2760 C13045BA02 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE SPOILERS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) ON APPROACH WITH FLIGHT SPOILERS EXTENDED, THE OB SPOILERONS(C) AND OB FLT SPOILERS(C) MESSAGE BECAME APPARENT IN ASSOCIATION WITH THE SPLR STAB FAULT MESSAGE. SSCU NR 2 WAS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061300010 20020613 00010 EA 2002 6 13 CA020510013 1 20020426 A 2820 CC670622581 SENSE LINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE FUEL EJECTOR BROKEN W O OTHER O OTHER DE DESCENT 1 CA (CAN) WHILE ON DESCENT, THE RT MAIN EJECTOR CAUTION MESSAGE BECAME APPARENT TO THE CREW. AT THE POINT OF SHUTDOWN, THERE WAS 80 LBS OF FUEL IN THE CENTRE TANK. MAINTENANCE FOUND THE RT MAIN EJECTOR PRESSURE SWITCH SENSE LINE (CC670-62258-1 )TO BE BROKEN JUST AT THE FERRULE GOING INTO THE "B" NUT. AFTER OBTAINING THE APPROPRIATE AUTHORIZATION, THE AIRCRAFT WA S FERRIED FOR INSTALLATION OF A REPLACEMENT PAN. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061300011 20020613 00011 EA 2002 6 13 CA020510015 1 20020508 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT LT SIDE CRACKED W B EMER. DESCENT O OTHER DE DESCENT 1 CA (CAN) NAT 07/2002: ON APPROACH FROM THE PILOT REPORTED THE LEFT SIDE WINDOW CRACKED. MAINTENANCE REPLACED THE LEFT SIDE WINDOW (S/N INSTALLED 01306H2383). 2 L 7 2 4F 4 F RT A21EA E15NE 2002061300013 20020613 00013 CE 2002 6 13 CA020510017 1 20020425 A 5620 1294300561 WINDOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE CABIN FAILED W B A EMER. DESCENT UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 CA 13194 (CAN) ON CLIMB OUT THROUGH APPROXIMATELY 17,000 FT EXPERIENCED A LOUD BANG IN THE CABIN. REALIZING CABIN WAS DECOMPRESSE D, THE CREW REQUESTED IMMEDIATE DESCENT. THE CREW DECIDED NOT TO DEPLOY PASSENGER MASKS SINCE THEY WERE AT A LOW ALTITUD E AND WOULD CAUSE MORE CONFUSION FOR THE PASSENGERS. THE AIRCRAFT RETURNED TO AIRPORT WITHOUT FURTHER INCIDENT. UPON I NVESTIGATION IT WAS NOTED NR 3 RT CABIN WINDOW WAS SHATTERED. THE REMAINING WINDOW WAS REMOVED AND SENT FOR FURTHER ANAL YSIS. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002061300014 20020613 00014 EA 2002 6 13 CA020510018 2 20020502 A 7414 4372 MAGNETO PARTEN P68 P68C 6780105 EU LYC O360 IO360A1B6 41514 EA ENGINE WEAK W O OTHER O OTHER TX TAXI/GRND HDL 1 CA (CAN) ENGINE HARD TO START WHEN HOT. 1 H 7 2 3O 3 O A31EU 1E10 2002061300019 20020613 00019 EU 2002 6 13 CA020510023 1 20020508 A 7603 HC760H0003092 CONTROL CABLE BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE THRUST LEVER BROKEN W E ENGINE SHUTDOWN E VIBRATION/BUFFET AP APPROACH 1 CA 31321 (CAN) INBOUND CREW REPORTED NR 1 ENGINE THRUST LEVER SEEMED TO HAVED SNAPPED. NO CONTROL OVER THRUST. ENGINE SHUT DOWN. MAINTENANCE FOUND NR 1 THRUST LEVER CABLE BROKEN AT PULLEY ON NR 1 ENGINE PYLON. 2 H 7 4 4F 4 F A49EU E6NE 2002061300020 20020613 00020 SO 2002 6 13 CA020510024 2 20020510 A 8530 646286 EXHAUST VALVE CESSNA 206 U206E 2073350 CE CONT O520 IO520F 17032 SO HARTZL HCC3Y HCC3YF1 GL ENG CYLINDER BURNED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE INSPECTING THE CYLINDER ASSEMBLIES IN ORDER TO PUT THE ENGINE "ON CONDITION", WE DISCOVERED THE EXHAUST VALV E ON CYLINDER NR 4 AND 5 SEVERELY BURNED. THE STEM AND NECK OF EXHAUST VALVE NR 4 APPEARS TO BE APPROXIMATELY 40 PERCEN T DETERIORATED AND EXHAUST VALVE NO 5 TO BE ABOUT 20 PERCENT DETERIORATED. ALL OTHER VALVES ON THIS ENGINE APPEAR TO BE FINE.THE FACE/SEAT OF THESE VALVES APPEAR TO BE FINE AS WELL. CATASTROPHIC FAILURE WAS EMINENT. THE CAUSE OF SUCH DETER IORATION IS UNCERTAIN BUT WE SPECULATE THAT IT MAY BE ASSOCIATED WITH THE USE OF 100LL FUEL AND LOW AIRCRAFT UTILIZATION . 1 H 7 1 3O 3 O A4CE E5CE 5 C P25EA 2002061300021 20020613 00021 CE 2002 6 13 CA020513001 1 20020507 A 3252 016A39212 ROD END MTSBSI MU2 MU2B60 5780460 CE GARRTT TPE331 TPE33110 01514 WP HARTZL HCB4T HCB4TN5 GL NLG SEPARATED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA (CAN) ROD END SEPARATED FROM PISTON.UNIT RETURNED TO VENDOR AND WAS OVERHAULED. SERVICE BULLETIN NR 169B EMBODIED TO PR ECLUDE FURTHER EVENTS. 1 H 7 2 3T 4 T RT A10SW E4WE 6 C P40EA 2002061300022 20020613 00022 EU 2002 6 13 CA020514001 1 20020503 A 4930 A2827042100600 TUBE AIRBUS 310 A310 EU GE CF6 CF680C2* GL APU FUEL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PRESENCE OF FUEL WAS DETECTED IN APU FUEL FEED LINE SHROUD, BENEATH CABIN FLOOR BETWEEN FRAMES 46 & 79. AFTER REMO VING A SECTION OF SHROUD FROM DRAIN TO FRAME 46 & GOING AFT, FUEL SHROUD AFT OF FRAME 79 STOPPED SHOWING PRESENCE OF FUE L. APU FUEL FEED TUBE SECTION FROM FRAME 79 TO FRAME 84 WAS REMVD & PRESSURE LEAK CHECKED. A MICROSCOPIC LEAK SOURCE WAS CONFIRMED FROM FUEL FEED TUBE SUPPORT FLANGE WELD. WELD CRACK IS TOO SMALL TO BE SEEN VISUALLY. FUEL FEED TUBE WAS REPL ACED PER AMM 49-31-21P.401. DAMAGED FUEL FEED TUBE FLANGE IS LOCATED ON SUPPORT BRACKET UNDER FLOOR, IN SERVICE COMPT AF T OF BULK CARGO, 40 IN FWD OF PRESSURE BULKHEAD. 2 L 7 2 4F 4 F RT A35EU E23EA 2002061300026 20020613 00026 NE 2002 6 13 QXEA0200842 2 20020525 A 7532 311489201 VALVE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE BLEED AIR SYS FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 348PH 484 MFR- AFTER NR 2 ENGINE START WHEN BLEED WAS TURNED ON, THE COCKPIT AND CABIN BEGAN TO FILL UP WITH AN ACRID HAZE. REMOV ED AND REPLACED P2.5-P3 SWITCHING VALVE PISTON, RING AND INNER HOUSING. GROUND RAN AIRCRAFT, NO SMOKE OR SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002061300027 20020613 00027 EA 2002 6 13 QXEA0200848 2 20020523 A 7321 312240013 FUEL CONTROL BOMBDR DHC8 DHC8401 NM PWC 150 PW150A EA COCKPIT DEFECTIVE A QXEA K NONE J WARNING INDICATION CL CLIMB 1 NM 09 413QX 765 4060 SEA- POWERPLANT MESSAGE APPEARED AFTER TAKEOFF. COMPLETED EMERGENCY CHECKLIST. NO ENGINE ABNORMALITIES NOTED. FLIGHT CONTINUED WITHOUT INCIDENT. MAINTENANCE PERFORMED TROUBLESHOOTING AND FOUND FAULT CODES 711 & 715 ENGINE NR 1. REMOVED AND REPLACED FADEC. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061300028 20020613 00028 NM 2002 6 13 QXEA0200851 1 20020523 A 3250 4063000501 CONTROL UNIT BOMBDR DHC8 DHC8401 NM NLG STEERING FAILED A QXEA O OTHER J WARNING INDICATION LD LANDING 1 NM 09 401QX 468 4031 BOI - NOSE WHEEL STEERING CAUTION ILLUMINATED JUST AFTER TOUCHDOWN. AFTER STOP, RAN NOSE STEERING ABNORMAL PROCEDURE CH ECK LIST AND WAS UNABLE TO RESOLVE THIS ISSUE. ELECTED TO BE TOWED TO GATE. PASSENGERS DISEMBARKED NORMALLY. MAINTENA NCE REPLACED NOSE WHEEL STEERING ELECTRONIC CONTROL UNIT. OPERATIONAL AND TAXI CHECK GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2002061300029 20020613 00029 NM 2002 6 13 QXEA0200852 1 20020531 A 3260 LIGHT BOMBDR DHC8 DHC8401 NM COCKPIT NOT SEATED A QXEA O OTHER N FALSE WARNING DE DESCENT 1 NM 09 411QX 4055 FCA - RIGHT HAND MAIN WOULD NOT INDICATE DOWN ON FINAL. SEATED LAMP. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRC RAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061300030 20020613 00030 EU 2002 6 13 QXEA0200853 1 20020602 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 BOI- AFT MID CABIN CEILING EXIT SIGN HAS SEVERAL LAMPS INOPERATIVE. REPLACED EXIT SIGN. OPERATIONAL CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002061300031 20020613 00031 EU 2002 6 13 QXEA0200854 1 20020530 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 PDX- EXIT SIGN ABOVE COCKPIT ENTRANCE IS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002061300032 20020613 00032 NM 2002 6 13 QXEA0200856 1 20020605 A 2612 CONNECTOR DHAV DHC8 DHC8202 2809007 NM FIRE DETECTION LOOSE A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 361PH 516 YVR- NR 1 FAULT B FIRE DETECTION CAUTION LIGHT ILLUMINATED. RESET CANNON PLUGS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061300033 20020613 00033 EU 2002 6 13 QXEA0200857 1 20020411 A 7120 MOUNT FOKKER F28 F28MK4000 4990810 EU NR 2 ENGINE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX- CORROSION ON FORWARD ENGINE MOUNT BEAM NR 2 SIDE. REPAIRED IAW FOKKER 20-20-05 AND 54-40-03, PG 201. 2 L 7 2 4F RT A20EU 2002061300035 20020613 00035 NM 2002 6 13 AUS20020388 1 20020423 A 2897 WIRE BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU FUEL SYSTEM LOOSE W O OTHER N FALSE WARNING NR NOT REPORTED 1 AU S (AUS) FUEL CROSSFEED SELECTOR LIGHT ILLUMINATED WITH SELECTOR CLOSED. PROBLEM TRACED TO AN INTERMITTENT FAULT IN WIRING BEHIND THE PLUG. 2 L 7 2 4F 4 F RT A16WE E21EU 2002061300037 20020613 00037 NM 2002 6 13 AUS20020391 1 20020323 A 5514 6965750045 FITTING BOEING 727 727281 138408N NM PWA JT8 JT8D17 52049 NE HORIZONTAL STAB CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S 40425 (AUS) HORIZONTAL STABLISER BEARING ATTACHMENT FITTINGS CORRODED. CPCP - LEVEL 2 CORROSION. 2 L 7 3 4F 4 F A3WE E2EA 2002061300039 20020613 00039 NM 2002 6 13 AUS20020393 1 20020316 A 5512 SKIN BOEING 727 727281 138408N NM PWA JT8 JT8D17 52049 NE HORIZONTAL STAB CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S 40425 (AUS) RT STABILISER SKIN CORRODED AT ATTACHMENT POINT TO REAR UPPER AUXILIARY SPAR CHORD ZONE 92, ELE 118.0 TO ELE 120.0 . CPCP -LEVEL 2 CORROSION. 2 L 7 3 4F 4 F A3WE E2EA 2002061300040 20020613 00040 NM 2002 6 13 AUS20020394 1 20020316 A 5520 692062212 SHIM BOEING 727 727281 138408N NM PWA JT8 JT8D17 52049 NE ELEVATOR CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S 40425 (AUS) RT STABILISER ELEVATOR SHIM PLATE FITTINGS CORRODED AT COUNTERWEIGHT ATTACHMENT POINT. CPCP - LEVEL 2 CORROSION. 2 L 7 3 4F 4 F A3WE E2EA 2002061300041 20020613 00041 NM 2002 6 13 AUS20020395 1 20020327 A 5520 692062212 SHIM BOEING 727 727281 138408N NM PWA JT8 JT8D17 52049 NE ELEVATOR CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S 40425 (AUS) LT ELEVATOR COUNTER WEIGHT SHIM PLATE FITTING HEAVILY CORRODEDZONE 93 STA ELE 210 TO STA ELE 222. CPCP - LEVEL 2 C ORROSION. 2 L 7 3 4F 4 F A3WE E2EA 2002061300043 20020613 00043 NM 2002 6 13 AUS20020399 1 20020318 A 5310 507978113 DOOR FRAME BOEING 727 727281 138408N NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S 40425 (AUS) CORROSION FOUND IN EMERGENCY DOOR EXIT (AFT OVERWING) AREA AT LOWER RH CORNER OF WEB ON HATCH ASSEMBLY FRAME ZONE 49 STN 825.95 TO STN 848.95. CPCP - LEVEL 2 CORROSION. 2 L 7 3 4F 4 F A3WE E2EA 2002061300044 20020613 00044 NM 2002 6 13 AUS20020405 1 20020323 A 5534 6965750045 FITTING BOEING 727 727281 138408N NM PWA JT8 JT8D17 52049 NE VERTICAL STAB CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S 40425 (AUS) VERTICAL STABILISER BEARING ATTACHMENT FITTINGS CORRODED. CPCP -LEVEL 2 CORROSION. 2 L 7 3 4F 4 F A3WE E2EA 2002061300046 20020613 00046 GL 2002 6 13 AUS20020415 1 20020426 A 2432 VENT PAC CT4 CT4B GL CONT O360 IO360HB 17025 SO HARTZL HCC2Y BHCC2YF1 GL BATTERY CHARGER FOD W O OTHER W INADEQUATE Q C CR CRUISE 1 AU S (AUS) PLASTIC BATTERY VENT TUBE INCOMPLETELY REMOVED DURING MAINTENANCE. THE LOOSE TUBE MOVED AFT AND LODGED IN THE ELEV ATOR BELLCRANK LOCATED IN THE TAILCONE. 1 L 7 1 3O 3 O RT A9PC E1CE 5 C P920 2002061300047 20020613 00047 NE 2002 6 13 AUS20020419 1 20020420 A 2910 48CT3A136000 HOSE SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1S 60030 NE HYD SYSTEM LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 AU S (AUS) RT MAIN LANDING GEAR DOWN' HYDRAULIC HOSE LEAKING. LOSS OF HYDRAULIC FLUID. 1 G 7 2 3U 3 U H1NE E19EU 2002061300048 20020613 00048 NE 2002 6 13 AUS20020420 1 20020429 A 6730 7826002 SERVO SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL1S 60030 NE TAIL ROTOR UNSERVICEABLE W O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 AU S 340 (AUS) TAIL ROTOR CONTROL SYSTEM SERVO FAULTY. 1 G 7 2 3U 3 U NC H1NE E19EU 2002061300049 20020613 00049 SO 2002 6 13 AUS20020421 2 20020430 A 8530 SA52000 EXHAUST VALVE CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO MCAULY D3A34 D3A34C404 GL ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 4 CYLINDER EXHAUST VALVE LEAKING. INVESTIGATION FOUND EROSION AROUND THE HEAD OF THE EXHAUST VALVE AS WELL AS L EAKING AT THE VALVE SEAT SEALING FACE. 1 H 7 1 3O 3 O A4CE E5CE 5 C P47GL 2002061300050 20020613 00050 SO 2002 6 13 AUS20020423 2 20020415 A 8530 EXHAUST VALVE CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO MCAULY 3A32C D3A32C90 GL ENGINE LEAKING W K NONE O OTHER IN INSP/MAINT 1 AU S 441 (AUS) ENGINE EXHAUST VALVES (2OFF) LEAKING. ENGINE HAD ONLY 441 HOURS SINCE FACTORY REMANUFACTURE. 1 H 7 1 3O 3 O A4CE E5CE 5 C P21EA 2002061300052 20020613 00052 SW 2002 6 13 AUS20020430 1 20020506 A 5343 2060313011215 SUPPORT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MLG ATTACH DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) REAR CROSS TUBE SUPPORT AREA DAMAGED. SUSPECT THE AREA HAD BEEN DAMAGED BY A HARD LANDING AND THEN INADEQUATELY R EPAIRED. THE HELICOPTER HAD ONLY RECENTLY BEEN IMPORTED INTO AUSTRALIA. PERSONNEL/MAINTENANCE ERROR. 1 G 7 1 3U 3 U H2SW E4CE 2002061300053 20020613 00053 SO 2002 6 13 AUS20020431 1 20020506 A 5711 17689 ATTACH ANGLE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL WING SPAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FORWARD SPAR ATTACHMENT STRUCTURE LT AND RT SIDE CRACKED. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2002061300054 20020613 00054 SO 2002 6 13 AUS20020433 2 20020414 A 8530 633129 BRACKET CESSNA 340 340CESSNA 2076404 CE CONT O520 TSIO520K 17040 SO MCAULY 3AF32C 3AF32C505 GL LT ENGINE CRACKED W O OTHER E VIBRATION/BUFFET DE DESCENT 1 AU S 1632 (AUS) LT ENGINE INDUCTION SYSTEM BALANCE TUBE FORWARD ATTACHMENT BRACKET BROKEN ALLOWING THE BALANCE TUBE TO SEPARATE FR OM THE MANIFOLD. 1 L 7 2 3O 3 O 3A25 E8CE 5 C P22EA 2002061300055 20020613 00055 SW 2002 6 13 AUS20020438 1 20020418 A 2912 24562 FILTER BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL HYDRAULIC SYS BLOCKED W A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 AU S (AUS) HYDRAULIC FILTER BLOCKED. DIFFERENTIAL PRESSURE INDICATOR BUTTON INOPERATIVE. 1 G 7 1 3U 3 U H2SW E4CE 2002061300056 20020613 00056 SO 2002 6 13 AUS20020444 1 20020510 A 2842 550697 TRANSMITTER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL FUEL QUANTITY DETERIORATED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FUEL TANK QUANTITY SYSTEM FLOAT VALVE DISINTEGRATING CAUSING CONTAMINATION OF THE FUEL SYSTEM AND FUEL FILTER. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2002061300057 20020613 00057 CE 2002 6 13 AUS20020446 1 20020501 A 7430 C2925010105 SWITCH CESSNA 172 172P 2072436 CE LYC O320 O320D2J 41508 EA MCAULY 1C160 1C160DTM GL IGNITION SYS FAULTY W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) IGNITION SWITCH CONTACTS DIRTY AND OILY. ONE CONTACT ARCING. SUSPECT INCORRECT LUBRICANT USED ON SWITCH. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 2002061300059 20020613 00059 NM 2002 6 13 AUS20020457 1 20020513 A 3222 450022002 SHAFT PIPER PA60 PA60601P 7106012 NM LYC O540 TIO540S1AD 41532 EA HARTZL HCC3Y HCC3YR2 NE NLG STRUT CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NOSE LANDING GEAR STRUT TORQUE TUBE SHAFT CRACKED FROM BOLT HOLE. FOUND DURING MAGNAFLUX INSPECTION. 1 M 7 2 3O 3 O RT A17WE E14EA 5 C P25EA 2002061300060 20020613 00060 SO 2002 6 13 AUS20020460 1 20020516 A 7922 SL53E19600 VALVE PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA HARTZL HCE3Y HCE3YR2 GL ENGINE OIL TEMP FAILED W O OTHER E K M VIBRATION/BUFFET FLUID LOSS OVER TEMP CL CLIMB 1 AU S 1800 (AUS) RT ENGINE OIL TEMPERATURE VALVE (VERNATHERM) FAILED. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2002061300061 20020613 00061 SO 2002 6 13 AUS20020462 2 20020419 A 8530 643767 VALVE GUIDE CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO MCAULY 3A32C D3A32C90 GL ENGINE FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 5 CYLINDER EXHAUST VALVE STICKING IN VALVE GUIDE. 1 H 7 1 3O 3 O A4CE E5CE 5 C P21EA 2002061300062 20020613 00062 SO 2002 6 13 AUS20020466 1 20020503 A 3234 L3011 SOLENOID PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA HARTZL HCE3Y HCE3YR2 GL MLG SELECTOR FAULTY W O OTHER O OTHER LD LANDING 1 AU S (AUS) LANDING GEAR SELECTOR SOLENOID STRIKER PIN BENT. NOSE LANDING GEAR INADVERTANTLY RETRACTED DURING TAXI CAUSING MAJ OR ENGINE, PROPELLER AND AIRFRAME DAMAGE. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2002061300063 20020613 00063 NM 2002 6 13 AUS20020469 1 20020521 A 3233 65C329561 ACTUATOR BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU MLG FAULTY W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AU S (AUS) LANDING GEAR ACTUATOR FAULTY. LIMITED INFORMATION PROVIDED. 2 L 7 2 4F 4 F RT A16WE E21EU 2002061300064 20020613 00064 NM 2002 6 13 AUS20020471 1 20020523 A 3610 16473301 DUCT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PNEUMATIC SYS CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT ENGINE LP SUPPLY DUCT CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061300067 20020613 00067 NM 2002 6 13 AUS20020476 1 20020523 A 5412 85410325 FIREWALL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE RT NACELLE CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S 33333 (AUS) RT ENGINE FIREWALL STRUCTURE CRACKED IN THE INSIDE RADIUS OF THEVERTICAL FACE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061300068 20020613 00068 NM 2002 6 13 AUS20020477 1 20020523 A 5522 85520057109 SKIN DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S 33333 (AUS) LT ELEVATOR TRAILING EDGE SKIN CRACKED ALONG THE TRAILING EDGE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061300069 20020613 00069 NM 2002 6 13 AUS20020478 1 20020523 A 1430 87140011007 FASTENER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENGINE COWLING WORN W K NONE O OTHER IN INSP/MAINT 1 AU S 33333 (AUS) LOWER ENGINE COWL INNER SKIN HAD A ROW OF TEMPORARY FASTENERS WORKING EXCESSIVELY. MANY RIVETS HOLES ELONGATED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061300071 20020613 00071 CE 2002 6 13 AUS20020482 1 20020518 A 6120 CONTROL CABLE CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO MCAULY D3A34 D3A34C404 GL PROPELLER FAULTY W O OTHER O OTHER CL CLIMB 1 AU S (AUS) CSU CONTROL SYSTEM OUTER CABLE STRETCHED. 1 H 7 1 3O 3 O A4CE E5CE 5 C P47GL 2002061300072 20020613 00072 NM 2002 6 13 AUS20020486 1 20020523 A 7500 10A21910050 CLAMP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENGINE BLEED AIR BROKEN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ENGINE LP BLEED SUPPLY DUCT CLAMP TANG BROKEN OFF. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061300073 20020613 00073 NM 2002 6 13 AUS20020488 1 20020515 A 3411 LINE BOEING 747 74748E 2FOR NM GE CF6 CF680C2* GL PITOT/STATIC DISCONNECTED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) ELEVATOR FEEL COMPUTER PITOT/STATIC LINES (4OFF) DISCONNECTED AND BLANKED. AIRCRAFT HAD COMPLETED FOUR FLIGHTS SI NCE HEAVY MAINTENANCE. PERSONNEL/MAINTENANCE ERROR. 2 L 7 2 4F 4 F RT A20WE E23EA 2002061300074 20020613 00074 CE 2002 6 13 AUS20020495 1 20020507 A 2434 632436 NUT CESSNA 421 421C 2076016 CE CONT O520 GTSIO520L 17032 SO MCAULY 3FF32 3FF32C501 GL DC GENERATOR MISSING W O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 AU S (AUS) RT ALTERNATOR DRIVE SHAFT COUPLING RETAINING NUT MISSING. SPLIT PIN WAS STILL INTACT. SUSPECT NUT SPLIT AND FELL O FF. LOOSE COUPLING CONTACTED ENGINE DRIVE GEARS CAUSING METAL CONTAMINATION OF THE ENGINE. 1 L 7 2 3O 3 O A7CE E7CE 5 C P45GL 2002061300075 20020613 00075 NM 2002 6 13 AUS20020498 1 20020528 A 2720 7G772 PRESSURE SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE RUDDER CONTROL FAULTY W O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) NR 2 RUDDER HYDRAULIC SYSTEM PRESSURE SWITCH FAULTY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061300076 20020613 00076 NM 2002 6 13 AUS20020502 1 20020525 A 2612 FIRE DETECTOR BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU NR 1 ENGINE FAILED W A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 AU S (AUS) NR 1 ENGINE FIRE WARNING SYSTEM A' AND B' LOOPS FAILED. 2 L 7 2 4F 4 F RT A16WE E21EU 2002061300077 20020613 00077 EU 2002 6 13 QXEA0200858 1 20020515 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX- THERE IS A SCRATCH IN THE FUSELAGE SKIN ABOVE THE RIGHT HAND STUBWING. REPAIRED IAW F-28 SRM 53-01-01 PAGE 3. 2 L 7 2 4F RT A20EU 2002061300078 20020613 00078 EU 2002 6 13 QXEA0200859 1 20020502 A 5240 STRUCTURE FOKKER F28 F28MK4000 4990810 EU SERVICE DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX- SERVICE EMERGENCY DOOR TOP FORWARD CORNER IS CHAFED. REPAIRED IAW F-28 SRM 51-31-01 AND SRM 51-10-05. 2 L 7 2 4F RT A20EU 2002061300079 20020613 00079 EU 2002 6 13 AUS20020389 1 20020421 A 2697 WIRE BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502R5 41580 NE FIRE PROTECTION LOOSE W O OTHER N FALSE WARNING CL CLIMB 1 AU S 8778 (AUS) NR 3 ENGINE NR 2 EXTINGUISHER USED' LIGHT ILLUMINATED. INITIAL INVESTIGATION FOUND THAT THE EXTINGUISHER PN 57333- 012 HAD NOT BEEN DISCHARGED. FURTHER INVESTIGATION FOUND THAT THE WIRES FROM THE BOTTLE USED' PRESSURE SWITCH WERE LOOS E AT THE TERMINAL BOARD ADJACENT TO THE EXTINGUISHER. 2 H 7 4 4F 4 F RT A49EU E6NE 2002061300080 20020613 00080 NM 2002 6 13 AUS20020396 1 20020320 A 5320 2024T3080 SILL BOEING 727 727281 138408N NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S 40425 (AUS) LT REAR ENTRY AND SERVICE DOOR AFT LOWER DOOR SILL CORRODED AT INNER PART OF SCUFF PLATE ZONE 24 STA 1035 TO STN 1 065. CPCP -LEVEL 2 CORROSION. 2 L 7 3 4F 4 F A3WE E2EA 2002061300081 20020613 00081 NM 2002 6 13 AUS20020397 1 20020320 A 5320 SILL BOEING 727 727281 138408N NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT AFT SERVICE DOOR SILL CHORD CORRODED AT INNER EDGE ATTACHMENT POINT. LEVEL 2 CORROSION. 2 L 7 3 4F 4 F A3WE E2EA 2002061300082 20020613 00082 EU 2002 6 13 AUS20020400 1 20020430 A 2751 676801007 ECU BAC 146 146200A 1500266 EU LYC ALF502 ALF502R3A 41580 NE TE FLAPS FAILED W O OTHER N FALSE WARNING CL CLIMB 1 AU S (AUS) FLAPS EXTENDED NORMALLY WITH THE FAULT LIGHT ILLUMINATED. INVESTIGATION FOUND THE FLAP ELECTRONIC CONTROL UNIT FAU LTY. 2 H 7 4 4F 4 F A49EU E6NE 2002061300083 20020613 00083 NM 2002 6 13 AUS20020401 1 20020423 A 3242 LINER BOEING 737 737800* NM GE CFM56 CFM567B24 NE BRAKE FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) AFTER PUSHBACK HOT BRAKE METAL WAS FOUND ON THE TARMAC. INITIAL INVESTIGATION FOUND NR 2 BRAKE STATOR LINER HAD FA ILED. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002061300084 20020613 00084 EU 2002 6 13 AUS20020403 1 20020427 A 2613 C8FCR230F SWITCH REIMS 406 F406 7535723 EU PWA PT6 PT6A112 52043 NE MCAULY 3G34C7 3GFR34C701 GL OVERHEAT DETECT FAULTY W O OTHER N FALSE WARNING CR CRUISE 1 AU S (AUS) DURING CRUISE THE LT WING OVERHEAT LIGHT ILLUMINATED. INVESTIGATION FOUND NO EVIDENCE OF BLEED AIR LEAK OR OVERHEA T CONDITION. SUSPECT FAULTY OVERHEAT SWITCH. 1 L 7 2 3T 3 T RT A54EU E4EA 5 C P60GL 2002061300085 20020613 00085 EA 2002 6 13 QXEA0200860 1 20020605 A 5210 BUSHING CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR NOT SEATED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 601QX 10009 PDX- MAIN CABIN DOOR VERY HARD TO OPEN, HANDLE BINDS ABOUT MID WAY DURING OPENING. FOUND AFT ROLL LATCH BINDING. REMOV ED TORQUE TUBE ASSY, RESEATED BUSHING AND REINSTALLED TORQUE TUBE ASSY. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002061300086 20020613 00086 NM 2002 6 13 QXEA0200861 1 20020608 A 3020 4100S02802 ADAPTER BOMBDR DHC8 DHC8401 NM NR 2 ENGINE FAULTY A QXEA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 407QX 4049 BZN- ENGINE ADAPTER HEAT 2 CAUTION ILLUMINATED INFLIGHT. FOUND INTAKE LIP HEAT CIRCUIT BREAKER POPPED. RESET CIRCUIT B REAKER, OPERATED ENGINE, POPPED AGAIN. SMELLED ELECTRICAL SMELL SHORTLY THEREAFTER. REMOVED AND REPLACED NR 2 ENGINE I NLET ADAPTER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061300087 20020613 00087 EU 2002 6 13 QXEA0200862 1 20020607 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 497US 11173 PDX- LIGHT OUT ON EXIT SIGN OVER ROW 8. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002061300088 20020613 00088 NM 2002 6 13 QXEA0200863 1 20020602 A 3350 10126271 SIGN DHAV DHC8 DHC8202 2809007 NM CABIN DETACHED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 359PH 514 YKM-EMERGENCY LIGHT SIGN AT SEAT 4D AT KNEE HEIGHT IS NO LONGER ATTACHED TO SIDEWALL. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061300090 20020613 00090 NM 2002 6 13 SABA020056 1 20020501 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 881CC 294 AIRCRAFT 881 ON FLIGHT 5077 FROM CLT TO AGS. DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHT OVER THE MAIN ENTRY DOOR W AS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE CONNECTION AT THE LIGHT. SYSTEM OPS CHECK GOOD. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061300091 20020613 00091 NE 2002 6 13 AUS20020406 2 20020430 A 7200 RB211524D419 ENGINE BOEING 747 747238B 1384828 NM RROYCE RB211 RB211524D419 54555 NE NR 4 VIBRATES W O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 AU S 63068 (AUS) DURING CLIMB NR 4 ENGINE VIBRATION INDICATED 2.0. ON B' SELECTION THE INDICATION WENT OFF SCALE WITH AVM ALERT FLA SHING. PRIOR TO SHUTDOWN A SLIGHT AIRFRAME VIBRATION WAS FELT THROUGH THE AIRCRAFT. 2 L 7 4 4F 4 F A20WE E12EU 2002061300092 20020613 00092 NM 2002 6 13 SABA020060 1 20020516 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN NOT SEATED A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 AIRCRAFT 883 ON FLIGHT 5099 FROM CLT TO PGV. DURING PREFLIGHT INSPECTION 2 EMERGENCY FLOOR LIGHTING BULBS WOULD NOT TES T. MAINTENANCE RESEATED THE BULBS IN THE SOCKETS. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061300093 20020613 00093 CE 2002 6 13 AUS20020408 1 20020504 A 2897 57181061 HARNESS CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP HARTZL HCB3T HCB3TN5 GL FUEL WIRING CHAFED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT FUEL TANK HARNESS WIRE CHAFFED BUT WITHIN ACCEPTABLE LIMITS OF SB CQB02-1. HARNESS MODIFIED IAW SB AND REINSTAL LED. 1 L 7 2 3T 4 T RT A28CE E4WE 6 C P15EA 2002061300098 20020613 00098 CE 2002 6 13 CA020607001 1 20020417 A 5524 HINGE BRACKET CESSNA 750 CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ELEVATORS CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 7500041 (CAN) A CRACK OF 0.30 INCHES WAS FOUND IN THE INBOARD SIDE OF THE HINGE BRACKET LOCATED IN THE FORWARD FROM THE TRAILING EDGE UNDER STIFFENER. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2002061300099 20020613 00099 NE 2002 6 13 CA020607007 2 20020602 A 7200 ENGINE LYC T5313B BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE NACELLE FAILED W B A EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION FF FIRE FIGHTING 1 CA LE07605 (CAN) A/C WAS IN PROGRESS OF FIREFIGHTING WHEN ENGINE 'FIRE WARNING' ILLUMINATED. AFTER VERIFYING FIRE VIBRATION, PILOT DECIDED TO CARRY OUT AN EMERG LDG. ON DESCENT FROM AP PROX 150 FEET, ENGINE CHIP LIGHT CAME ON AS WELL AS ENGINE OIL LOW PRESSURE WARNING LIGHT. AT SAME TIME PILOT COULD SEE ENGINE OIL PRESSURE DROPPING FAST. NEARING GROUND FIRE EXTINGUISH ER WAS ACTIVATED & OIL WAS SWITCHED OFF. A/C LANDED UNDER POWER. ENGINE WAS SHUTDOWN, CLOSING THROTTLE & SWITCHING FUEL OFF. BATTERY WAS SWITCHED OFF & PILOT AND FORESTY OFFICER EXITED A/C. COMBINED EFFORTS FROM FORESTRY PEOPLE & FIRECREW F INALLY PUT OUT FLAMES. 1 G 7 1 4U 4 U H1SW E17EA 2002061300100 20020613 00100 NM 2002 6 13 USA2002F00027 1 20020528 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM 1,4,6,9,13,18,23 DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 17 616AU 27147 (BATTERY) FOUND ALL FLOOR LEVEL EMERGENCY LIGHTS, INOPERATIVE. MAINTENANCE REPLACED ALL OF BATTERIES. 2 L 7 2 4F RT A2NM 2002061300101 20020613 00101 NM 2002 6 13 USA2002F00030 1 20020526 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 17 615AU 27146 (BATTERY) FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. 2 L 7 2 4F RT A2NM 2002061300102 20020613 00102 NM 2002 6 13 USA2002F00031 1 20020527 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM ROW 33 INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 17 609AU 22205 (LIGHT ASSEMBLY) FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2 L 7 2 4F RT A2NM 2002061300103 20020613 00103 NM 2002 6 13 USA2002F00032 1 20020530 A 3350 96210066 BATTERY BOEING 757 757225 1384959 NM 1,4,6,13,18 DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 17 602AU 22196 (BATTERIES) FOUND LOW LEVEL EMERGENCY LIGHTS AT ROWS 1,4,6,13 AND 18, INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. 2 L 7 2 4F RT A2NM 2002061300104 20020613 00104 NM 2002 6 13 USA2002F00033 1 20020526 A 2130 BOOT BOEING 737 737401 1384701 NM DUCT SEAL BOOT OUT OF POSITION A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 17 423US 23990 (DUCT SEAL BOOT) ENROUTE, THE CABIN ALTITUDE WARNING HORN SOUNDED ALERTING THE CREW THAT CABIN ALTITUDE WAS AT 10,000 F EET. WITH OUTFLOW VALVE CLOSED, CREW WAS UNABLE TO CONTROL CABIN ALTITUDE. CREW DESCENDED FLIGHT AND DIVERTED, WHERE T HE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND NO OXYGEN MASKS WERE DEPLOYED. MAINTENANCE RE SECURED DUCT SEAL BOOT IN KEEL BEAM AREA. LEAK CHECK GOOD. ALSO, REPLACED FORWARD ENTRY DOOR LOWER HINGE FLAP SEAL. L EAK CHECK GOOD. PERFORMED LEAK DOWN RATE TEST PER MM. OPERATIONAL TEST SATISFACTORY. 2 L 7 2 4F RT A16WE 2002061300105 20020613 00105 NM 2002 6 13 DLM88020589 1 20020523 A 5330 SKIN DOUG MD88 MD88 3023688 NM FS 246, S-30 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 914DL 49545 FUSELAGE / SKIN / TCAS ANTENNA CUTOUT / FS 246 / S-30 : CORROSION REPAIR THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION NEAR THE TCAS ANTENNA CUTOUT AT FS 246 BETWEEN STRINGERS 30 & 29L. THE CORROSION WAS REMOVED BY MACHINING AWAY. THE AREAWAS REINFORCED WITH AN EXTERNAL ALUMINUM DOUBLER TO ENCOMPASS THE ANTENNA INSTALLATION AREA. THE REPAIR WAS ACCOMPLISHED PER ER/A 383223-14, REV A. 2 L 7 2 4F RT A6WE 2002061300106 20020613 00106 NM 2002 6 13 DL757020596 1 20020526 A 3350 767 BULB BOEING 757 757232 1384965 NM EXTERIOR BURNED OUT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 664DN 25012 EXTERIOR EMERGENCY LIGHTS INOP AT R1 DOOR AND L3 DOOR. CA RELAMPED. 2 L 7 2 4F RT A2NM 2002061300107 20020613 00107 NM 2002 6 13 DL73K020598 1 20020528 A 3310 UNK BALLAST BOEING 737 737247 138448D NM COCKPIT FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 382DL 23609 COCKPIT CENTER FLORESCENT LIGHTS INOP CA RPLD BALLAST, OP CKS GOOD. 2 L 7 2 4F A16WE 2002061300108 20020613 00108 NM 2002 6 13 DL757020599 1 20020528 A 5330 146N37506 SKIN BOEING 757 757232 1384965 NM FS 1720, S-20R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 646DL 24217 FUSELAGE / SKIN / FS 1720 / STRG. 19R-20R : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED NEAR THE SKIN BUTT LINE AT FS 1720 JUST ABOVE THE SKIN LAP JOINT AT STRG. 20R. THE DENT WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383012-14, REV A. 2 L 7 2 4F RT A2NM 2002061300109 20020613 00109 NM 2002 6 13 DL757020602 1 20020525 A 5330 143N35219 SKIN BOEING 757 757232 1384965 NM FS 722, S-26L GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 646DL 24217 FUSELAGE / SKIN / FS 722 / STRG. 26L-27L : GOUGE REPAIR THE FUSELAGE SKIN WAS FOUND GOUGED AT FS 722 BELOW THE STRINGER 26L SKIN LAP JOINT. THE GOUGE WAS REMOVED WITH A 2" CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 383096-14, REV A. 2 L 7 2 4F RT A2NM 2002061300110 20020613 00110 NM 2002 6 13 DL757020603 1 20020525 A 5330 146N35318 SKIN BOEING 757 757232 1384965 NM FS 1459, S-28R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 646DL 24217 FUSELAGE / SKIN / FS 1455-1478 / STRG. 28R-29R : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH A LONG GOUGE BETWEEN STRINGERS 28R & 29R FROM FS 1455-1478. THE GOUGE SPANNED THE BUTT JOINT AT FS 1459. THE GOUGE WAS CUT OUT OF BOTH SKIN PANELS AND REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER ER/A 383014-14, REV A. 2 L 7 2 4F RT A2NM 2002061300111 20020613 00111 NM 2002 6 13 DL76S020611 1 20020601 A 7100 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE #1 ENGINE UNSERVICEABLE A DALA D RETURN TO BLOCK M OVER TEMP TO TAKEOFF 1 SO 27 129DL 50347 2170 24079 580209 ON TAKE OFF ROLL ABOUT 130 KIAS, LEFT ENGINE TEMP WENT TO 975, PULLED THROTTLE BACK TO KEEP WITHIN LIMITS, CONTINUED T AKE OFF AT 150 AGL, LEFT ENGINE ROLLED BACK TO IDLE AND TEMPWENT TO 1100. POWER CAME BACK TO IDLE AND RETURNED TO FIELD. THE ENGINE WAS NOT SHUTDOWN UNTIL AFTER LANDING. RPLCD NBR 1 ENG PER TRANS 1T144 2 L 7 2 4F 4 F RT A1NM E13NE 2002061300112 20020613 00112 NM 2002 6 13 DL73K020617 1 20020531 A 5230 6547952524A DOOR FRAME BOEING 737 737247 138448D NM C2 CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 DOORS / C2 CARGO DOOR / FWD FRAME / LAP SPLICE : CRACK REPAIR THE FWD FRAME OF THE C2 CARGO DOOR WAS FOUND WITH 2" CRACK IN THE UPPER FRAME AND A FASTENER HOLE CRACK IN THE LOWER FRAME AT FRAME LAP JOINT BETWEEN DOOR STOPS #3 & #4. THE CRACKED FRAMES WERE REPAIRED WITH 2 TITANIUM REPAIR ANGLES OVERLAPING THE EXISTING FRAME LAP PER ER/A 383269-14, REV A. 2 L 7 2 4F A16WE 2002061300113 20020613 00113 NM 2002 6 13 DLM88020628 1 20020606 A 5311 5912141 ATTACH ANGLE DOUG MD88 MD88 3023688 NM AFT FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 917DL 49573 THE LH FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE WAS FOUND CRACKED AT APPROXIMATELY STA 1474 CANT. THE CRACK WAS 0.5 " LONG AND TYPICAL AS THAT SHOWN IN MD-88 SRM 53-05, FIG. 23. THE ANGLE IS MADE FROM 0.080" THICK SOLUTION HEAD TREATED A-286 CRES MATERIAL. THE CRACK WAS TRIMMED OUT AND THE ANGLE REINFORCED. 2 L 7 2 4F RT A6WE 2002061300114 20020613 00114 EA 2002 6 13 SWIA200210895 1 20020602 A 5244 SERVICE DOOR CNDAIR CL600 CL6002B19 1900309 EA OXYGEN OPEN A SWIA A UNSCHED LANDING J N WARNING INDICATION FALSE WARNING CL CLIMB 1 NM 07 597SW 7293 ON ROTATION WE RECEIVED A STALL FAIL CAUTION MESSAGE. RAN QRH. ON DESCENT, AS AIRSPEED SLOWED, WE RECEIVED A MACH TRIM FAIL MESSAGE. RETURNED TO SLC. FOUND O2 SERVICE DOOR OPEN. INSPECTED O2 SERVICE DOOR AND FOUND NO DAMAGE. OPS CHEC KED STALL SYSTEM. NO DEFECTS NOTED IAW 27-35-00. 2 L 7 2 4F RT A21EA 2002061300115 20020613 00115 CE 2002 6 13 AUS20020409 1 20020503 A 2897 57181061 HARNESS CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP HARTZL HCB3T HCB3TN5 GL FUEL WIRING CHAFED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT FUEL TANK HARNESS WIRE CHAFED BUT WITHIN ACCEPTABLE LIMITS OF SB CQB02-1. HARNESS MODIFIED IAW SB AND REINSTALL ED. 1 L 7 2 3T 4 T RT A28CE E4WE 6 C P15EA 2002061300116 20020613 00116 NM 2002 6 13 USA2002F00037 1 20020601 A 3350 21007 SWITCH BOEING 757 7572B7 1384964 NM L4 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 17 632AU 27810 (SWITCH) EMERGENCY LIGHT TEST SWITCH ABOVE L4 DOOR INOPERATIVE. MAINTENANCE REPLACED THE SWITCH. 2 L 7 2 4F RT A2NM 2002061300118 20020613 00118 NM 2002 6 13 SABA020061 1 20020518 A 3350 101307150 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 841PH 082 AIRCRAFT 881 ON FLIGHT 5190 FROM AGS TO CLT. DURING POST FLIGHT INSPECTION AFTER ARRIVAL IN CLT THE EMERGENCY LIGHT AT 1A WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. SYSTEM OPS CHECK GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2002061300119 20020613 00119 2002 6 13 SABA020063 4 20020527 A 2210 4012373817 DAMPER DHAV DHC8 DHC8103 1386005 NM AUTOPILOT SYS FAILED A SABA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 33 801WP 086 AIRCRAFT 801 ON FLIGHT 5099 FROM CLT TO PGV. DURING CRUISE THE RIGHT AND LEFT YAW DAMP FAILED. AIRCRAFT RETURNED TO TH E FIELD AT CLT WITH NO OTHER PROBLEMS. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE YAW DAMP ACTUAT OR. A TEST FLIGHT WAS PERFORMED AND WAS SATISFACTORY. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061300120 20020613 00120 NM 2002 6 13 SABA020065 1 20020603 A 3150 80053519 CONTROL PANEL DHAV DHC8 DHC8103 1386005 NM COCKPIT OVERHEATED A SABA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 33 801WP 086 FLIGHT 5028 FROM TLH TO CLT, DURING CLIMBOUT AT TLH WINDSHIELD HEAT WAS TURNED ON. PILOT NOTICED A STRONG ELECTRICAL SM ELL. WINDSHIELD HEAT WAS TURNED OFF AND SMELL WENT AWAY. AIRCRAFT CONTINUED TO CLT. DURING DESCENT TO CLT THE SMELL R ETURNED. AIRCRAFT LANDED IN CLT WITH NO OTHER PROBLEMS AND NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE CENTRAL AN NUNCIATOR PANEL OVERHEATING. REMOVED AND REPLACED PANEL. SYSTEM OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061300121 20020613 00121 NM 2002 6 13 SABA020066 1 20020603 A 3150 80053519 CONTROL PANEL DHAV DHC8 DHC8103 1386005 NM COCKPIT OVERHEATED A SABA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 33 801WP 086 FLIGHT 5028 FROM TLH TO CLT, DURING CLIMBOUT AT TLH WINDSHIELD HEAT WAS TURNED ON. PILOT NOTICED A STRONG ELECTRICAL SM ELL. WINDSHIELD HEAT WAS TURNED OFF AND SMELL WENT AWAY. AIRCRAFT CONTINUED TO CLT. DURING DESCENT TO CLT THE SMELL R ETURNED. AIRCRAFT LANDED IN CLT WITH NO OTHER PROBLEMS AND NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE CENTRAL AN NUNCIATOR PANEL OVERHEATING. REMOVED AND REPLACED PANEL. SYSTEM OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061300124 20020613 00124 EU 2002 6 13 SDRS2002002 1 20020429 A 6410 117317411 BLADE BOLKMS BK117 BK117C1 5626025 EU TAIL ROTOR CRACKED E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 117SU 2309 549 7527 ON PREFLIGHT INSPECTION FOUND TAIL ROTOR BLADE CRACKED NEAR THE ROOT END OF THE BLADE. CRACK APPEARS TO ORIGINATE FROM THE OUTBOARD CORNER OF THE P/N PLACARD AREA AND EXTENDS APPROX 30 DEGREES TO THE TRAILING EDGE OF THE BLADE. 1 G 7 2 3U NC H13EU 2002061300125 20020613 00125 EU 2002 6 13 SDRS2002003 1 20020429 A 6410 117317411 BLADE BOLKMS BK117 BK117C1 5626025 EU TAIL ROTOR CRACKED E R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 117SU 1976 549 7527 ON PREFLIGHT INSPECTION FOUND A CRACK IN THE TAIL ROTOR BLADE. CRACK APPEARS TO ORIGINATE FROM THE PN WINDOW AND EXTEND S APPROX 30 DEGREES FOR A LENGTH OF APPROXIMATELY ONE INCH TOWARDS THE TRAILING EDGE OF THE BLADE. 1 G 7 2 3U NC H13EU 2002061300128 20020613 00128 NM 2002 6 13 SWAA021077 1 20020517 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS MISSING AT ROW 13 AND CRACKED AT FWD END. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002061300129 20020613 00129 NM 2002 6 13 SWAA021078 1 20020517 A 3150 65029423 LIGHT BOEING 737 7373H4 1384600 NM COCKPIT ERRATIC A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 319SW 23340 AIR TURNBACK, DURING CLIMB ENG ANNUNCIATOR WARNING LIGHT ILLUMINATED, ALL ENGINE PARAMETERS CHECK NORMAL. REMOVED AND R EPLACED F/O'S SIX PACK LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2002061300130 20020613 00130 NM 2002 6 13 SWAA021080 1 20020517 A 3350 612825 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED RON, FOUND OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHTS INOP AT ROW 9 DEF, ROW'S 18 AND 21 ABC. REMOVE D AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002061300131 20020613 00131 NM 2002 6 13 SWAA021093 1 20020516 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT ROW 11 AND ROW 18. RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2002061300132 20020613 00132 NM 2002 6 13 SWAA021095 1 20020516 A 3350 604222 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C3 CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002061300133 20020613 00133 2002 6 13 SWAA021096 4 20020516 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002072200048 20020722 00048 NM 2002 7 22 2002UALA00959 1 20020605 A 3350 BATTERY BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 609UA 21870 EMERGENCY FLOOR LIGHTS STAYED ON SEATS 16-32 LT SIDE. REPLACED BATTERY PACKS AND OVERHEAD PANEL ON-OFF-ARMED SWITCH. 2 L 7 2 4F 4 F RT A1NM E3NE 2002072200049 20020722 00049 NM 2002 7 22 2002UALA00960 1 20020606 A 2910 271N61191 HYDRAULIC LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT MLG RUPTURED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 541UA 25253 LEFT HYDRAULIC QUANTITY DROPPED TO ZERO. RIGHT MAIN GEAR DOWNLOCK HOSE RUPTURED. REPLACED HYDRAULIC HOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002061300134 20020613 00134 NM 2002 6 13 2002UALA00961 1 20020607 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 939UA 26672 AFT CABIN FRAME AT STATION 951 AT STRINGER 5R HAS A CRACK INDICATION IN STRAP. MAJOR REPAIR ACCOMPLISHED. INSTALLED FI LLER AND STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072200050 20020722 00050 NM 2002 7 22 2002UALA00962 1 20020606 A 3350 CHARGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INTERMITTENT A UALA O OTHER O OTHER CR CRUISE 1 WP 29 654UA 25392 ESCAPE PATH LIGHTING IN BACK OF AIRCRAFT COME ON AND OFF DURING FLIGHT. EEL LIGHT COMES ON AND OFF FROM ROWS 29FG AFT T O ROW 35FG. REPLACED BATTERY CHARGER-POWER SUPPLY AND BATTERY AT SEAT 33FG SIDEWALL. 2 L 7 2 4F 4 F RT A1NM E24NE 2002061300136 20020613 00136 NM 2002 6 13 QXEA0200844 1 20020526 A 2730 ELEVATOR DHAV DHC8 DHC8202 2809007 NM TAIL OUT OF RIG A QXEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 09 356PH 502 SEA - AIRCRAFT RETURNED TO FIELD WHEN ON TAKEOFF IT WAS NOTED THAT THE AIRCRAFT DOES NOT ROTATE NORMALLY AND TAKES ALMOS T FULL DEFLECTION BEFORE THE NOSE COMES OFF THE GROUND. MAINTENANCE INSPECTED THE AIRCRAFT AND RERIGGED THE ELEVATOR CO NTROL CABLES; CHECKED CABLE TENSION ON PILOTS ELEVATOR CONTROL CABLES; RIGGED THE RIGHT ELEVATOR CONTROL SURFACE; CHECKE D RIG OF LEFT ELEVATOR CONTROL SURFACE; ADJUSTED RIGGING ON ELEVATOR TRIM CABLES; RIGGED LEFT ELEVATOR SPRING TAB STOPS AND BOTH TABS, AND REPLACED LOOSE RIVETS AT BASE OF YOKE. AN OPERATIONAL CHECK WAS PERFORMED AND CHECKED GOOD. CHECK F LIGHT WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061300137 20020613 00137 NM 2002 6 13 QXEA0200846 1 20020522 A 2120 DRAIN LINE DHAV DHC8 DHC8202 2809007 NM A/C BAY PLUGGED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 348PH 484 PDX-FLIGHT ATTENDANT REPORTED ODORLESS HAZE IN CABIN AFTER START. HAZE WENT AWAY IN ONE MINUTE. UNPLUGGED DUCT DRAIN L INE FROM AIR CYCLE MACHINE. REINSTALLED DRAIN LINE. GROUND RAN AIRCRAFT. OPERATIONAL CHECK GOOD. NO HAZE OR MIST SEE N IN CABIN. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061300138 20020613 00138 EU 2002 6 13 RAIA00205140 1 20020502 A 3230 LANDING GEAR AEROSP ATR42 ATR42300 8680920 EU NLG & MLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 423TE 119 5619-STL- LANDING GEAR WILL NOT RETRACT. MAINTENANCE PERFORMED LANDING GEAR RETRACTION CHECK AND COULD NOT DUPLICATE MA LFUNCTION, OPS CHECK OK. 2 H 7 2 4T RT A53EU 2002061300139 20020613 00139 EU 2002 6 13 RAIA00205141 1 20020501 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 574HK 41093 STL- FORWARD ESCAPE PATH LIGHTING INOP. RECONNECTED LIGHTING STRIP CONNECTOR. 2 L 7 2 4T RT A41NM 2002061300140 20020613 00140 EU 2002 6 13 RAIA00205147 1 20020509 A 3350 SOCKET JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 559HK 41075 STL- FWD LEFT EMERGENCY ESCAPE LIGHT INOP. RESECURED EMERGENCY LIGHT SOCKET. 2 L 7 2 4T RT A41NM 2002061300141 20020613 00141 EU 2002 6 13 RAIA00205153 1 20020513 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 574HK 41093 STL- ESCAPE PATH LIGHTS OUT AT ENTRY DOOR. RESECURED CONNECTOR AT ESCAPE PATH LIGHTS. 2 L 7 2 4T RT A41NM 2002061300142 20020613 00142 EU 2002 6 13 RAIA00205154 1 20020515 A 3397 WIRE JETAIR JETSTM JETSTM4101 1500501 EU CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 574HK 41093 STL- EMERGENCY ESCAPE PATH LIGHTS INOP 1A TO 4A. REPAIRED BROKEN WIRE AT PATH LIGHT TRACK. 2 L 7 2 4T RT A41NM 2002061300143 20020613 00143 NE 2002 6 13 RAIA00205157 2 20020516 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LEFT FLAMED OUT A RAIA D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 CE 03 561HK 41077 76055 STL- LEFT ENGINE FLAMED OUT DURING TAXI. MAINTENANCE INSPECTED LEFT ENGINE AND PERFORMED GROUND RUN. ALL OPS NORMAL, N O DEFECTS NOTED. 2 L 7 2 4T 4 T RT A41NM E18NE 2002061300144 20020613 00144 EU 2002 6 13 RAIA00205158 1 20020520 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 551HK 41040 STL- EMERGENCY PATH LIGHTS INOP ROW 2-3. RESECURED PATH LIGHT CONNECTOR AT ROW 3. 2 L 7 2 4T RT A41NM 2002061300145 20020613 00145 NM 2002 6 13 RYN2002F00005 1 20020529 A 2550 PANEL BOEING 727 727222 1384073 NM CARGO BAY CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 C-CHECK, FOUND CORROSION IN AFT CARGO COMPARTMENT, ON LEFT TRANSITION PANEL, AT STATION 950E +8 TO 950F, LBL 18. 2 L 7 3 4F A3WE 2002061300146 20020613 00146 NM 2002 6 13 RYN2002F00007 1 20020528 A 5320 FLOOR SUPPORT BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 C-CHECK, FOUND IN AFT CARGO COMPARTMENT, FLOOR SUPPORT CRACKED AND HOLES DRILLED IN RADIUS OF ANGLE, AT STATION 950F B/L 0. 2 L 7 3 4F A3WE 2002061300147 20020613 00147 NM 2002 6 13 RYN2002F00008 1 20020528 A 5313 STRINGER BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 C-CHECK, FOUND IN AFT CARGO COMPARTMENT STATION 970, STRINGER 26L HAS A CRACK THAT IS STOPPED DRILLED. CRACK IS CONTINU ING PAST THE STOP DRILL HOLE. 2 L 7 3 4F A3WE 2002061300148 20020613 00148 NM 2002 6 13 RYN2002F00013 1 20020527 A 5320 FLOOR SUPPORT BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 C-CHECK, FOUND CRACK IN FLOOR SUPPORT, AT FORWARD FUSELAGE INTERIOR LOWER LOBE, AT STATION 310. 2 L 7 3 4F A3WE 2002061300149 20020613 00149 NM 2002 6 13 RYN2002F00014 1 20020526 A 3231 FITTING BOEING 727 727222 1384073 NM NLG DOOR CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 C-CHECK, FOUND CORROSION AT NOSE WHEEL WELL FORWARD BULKHEAD, ON DOOR LINKAGE FITTING, AT STATION 227.8, LEFT SIDE. 2 L 7 3 4F A3WE 2002061300150 20020613 00150 NM 2002 6 13 RYN2002F00015 1 20020526 A 5320 BRACKET BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 C-CHECK, FOUND CORROSION AT NOSE WHEEL WELL, ON RIGHT SUPPORT BRACKET, AT STATION 294.5. 2 L 7 3 4F A3WE 2002061300151 20020613 00151 NM 2002 6 13 RYN2002F00016 1 20020526 A 5330 SKIN BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 C-CHECK, FOUND CORROSION AT NOSE LANDING GEAR DRAG BRACE SUPPORT FITTING, LEFT SIDE ON SKIN, AT STATION 344.0. 2 L 7 3 4F A3WE 2002061300156 20020613 00156 EU 2002 6 13 02FDEA00384 1 20020608 A 2131 CONTROLLER AIRBUS 310 A310 EU CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 412FE 360 AIRCRAFT WOULD NOT PRESSURIZE. NR 1 FWD AND AFT OUTFLOW VALVE INDICATED FULL OPEN. PERFORMED FUNCTIONAL CHECK OF NR 1 AND NR 2 PRESSURIZATION CONTROLLERS. NR 1 SYSTEM CONTROLLER CONTINUOUSLY SHOWS THE AIRCRAFT AT AN ELEVATION OF 400 FT W HEN IT SHOULD READ APPROX 620'. SWAPPED CONTROLLERS AND PROBLEM FOLLOWED. PUT NEW CONTROL FROM STOCK IN NR 1POSITION B UT IT WAS BAD FROM STOCK. PUT OLD ONE BACK IN POS NR 1. NEW CONTROLLER ON ORDER. REMOVED AND REPLACED RELAYS 159GB A ND 144GB PER STANDARD MX PRACTICES. 2 L 7 2 4F RT A35EU 2002061300157 20020613 00157 NM 2002 6 13 02FDEA00385 1 20020611 A 2613 65249203 OVERHEAT LOOP BOEING 727 727200 138407E NM FIRE PROTECTION FAULTY A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 234FE 4000 4000 21328 DURING CRUISE FLT AT FL330 WHEN POWER WAS REDUCED TO DESCEND, LOWER AFT BODY OVERHEAT LIGHT FLICKERED THEN CAME ON STEAD Y. COMPLIED WITH RED TAB PROCEDURES, LIGHT WENT OUT. SYSTEM TEST SATISFACTORY. MONITORED FOR REMAINDER OF FLIGHT. RE MOVED AND REPLACED FIRE DETECTION UNIT PER M/M 26-14-00-5, OPS CHECK NORMAL. A/C OK TO CONTINUE SERVICE. 2 L 7 3 4F RT A3WE 2002062000014 20020620 00014 NM 2002 6 20 02FDEA00386 1 20020610 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 CRACKED STR WITH 4 OPEN HOLES BS 640, STR 27 LT. REMOVED AND REPLACED STRINGER PER SRM 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 2002061900193 20020619 00193 NM 2002 6 19 02FDEA00387 1 20020607 A 5230 STRUCTURE BOEING 727 727200 138407E NM CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 207FE 22929 AFT LWR CARGO DOOR HAS DAMAGE AT FWD UPPER CORNER. REMOVED AND REPLACED DOOR PER SRM 52-00-3 FIG 4, 52-00-2. 2 L 7 3 4F RT A3WE 2002061300158 20020613 00158 NM 2002 6 13 02FDEA00388 1 20020605 A 5230 ACA7223515 HINGE DOUG MD11 MD11 3023602 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK CARGO DOOR HINGE (AFT HINGE) CRACKED APPROX 0.025 INCH. 2 L 7 3 4F RT A22WE 2002080600008 20020806 00008 NM 2002 8 6 02FDEA00389 1 20020605 A 5344 ACA7223513 HINGE DOUG MD11 MD11 3023602 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK CARGO DOOR FUSELAGE HALF HINGE, HINGE LOBES ELONGATED AND ID EXCEEDED FITS CLEARANCE LIMITS. REMOVED AND RE PLACED HINGE PER JAMB INSTL DRAWING ACA7211. 2 L 7 3 4F RT A22WE 2002080600009 20020806 00009 NM 2002 8 6 02FDEA00390 1 20020605 A 5230 ACA73321 HINGE DOUG MD11 MD11 3023602 NM CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK CARGO DOOR FWD SUPPORT ASSY, HINGE LOBES ELONGATED AND BORE ID EXCEEDED CLEARANCE LIMIT. REMOVED AND REPLAC ED CARGO DOOR FWD SUPPORT ASSY PER 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2002062000015 20020620 00015 NM 2002 6 20 02FDEA00391 1 20020609 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 CORROSION ON TOP OF FLOORBEAM BS 360, RBL 6. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 3. 2 L 7 3 4F RT A3WE 2002080600010 20020806 00010 NM 2002 8 6 02FDEA00392 1 20020609 A 5414 SKIN BOEING 727 727200 138407E NM PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 SKIN CHAFED AT BS 1352 AT NR 2 ENG RT RAIN GUTTER 15 INCHES BELOW NR 3 PYLON T/E AND RAIN GUTTER. REMOVED AND REPLACED PER EA 7-5410-64955 & SRM 54-30-3. 2 L 7 3 4F RT A3WE 2002080600011 20020806 00011 NM 2002 8 6 02FDEA00393 1 20020610 A 5320 651632640 STRAP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 LAST HOLE IN REINFORCEMENT STRAP CRACKED. REMOVED AND REPLACED STRAP PER SRM 51-30- 5, 51-10-2. 2 L 7 3 4F RT A3WE 2002061300159 20020613 00159 NM 2002 6 13 02FDEA00394 1 20020610 A 5320 658065580 ANGLE BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 HOLE IN L-ANGLE CRACKED AT BS 783. 2 L 7 3 4F RT A3WE 2002061300160 20020613 00160 NM 2002 6 13 2002F00617 1 20020608 A 3230 LANDING GEAR BOEING 737 73783N 13844HI NM RT MLG MALFUNCTIONED G AMTA O OTHER J WARNING INDICATION LD LANDING 1 GL 11 308TZ 28244 FLIGHT NUMBER 381, WHEN LOWERING THE LANDING GEAR ON APPROACH INTO DEN, THE RIGHT GEAR WAS SLOW TO ILLUMINATE A GREEN LI GHT. THE GEAR WAS VERIFIED DOWN AND LOCKED BUT CHANGED TO A RIGHT GEAR UNSAFE INDICATION, MANUAL GEAR EXTENSION WAS UNS UCCESSFUL. THE AIRCRAFT LANDED AT DENVER WITHOUT INCIDENT. 2 L 7 2 4F RT A16WE 2002061300161 20020613 00161 NM 2002 6 13 2002F00618 1 20020528 A 3097 WIRE BOEING 757 75723N 1384973 NM WINDOW HEAT SHORTED G AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 516AT 24264 24264 27972 FLIGHT NUMBER 535, LEFT SIDE WINDOW EICAS MESSAGE LIGHT ILLUMINATED AS WELL AS LEFT SIDE WINDOW HEAT INOP LIGHT. UNABLE TO RESET IAW QRH PROCEDURE. BOTH L2 & L3 WINDOW COLD AFTER APPROX 1 HOUR. MAINTENANCE REMOVED AND REPLACED WINDOW HEA T CONTROLLER PER MM 30-41-01. FOUND WIRES AT C/P D2290A SHORTED TOGETHER, RECHECKED WIRES PER STD PRACTICES. OPS CHECK S NORMAL. 2 L 7 2 4F RT A2NM 2002061300162 20020613 00162 WP 2002 6 13 DHL2002804008 1 20020612 A 2697 DC63F22K14PN CONNECTOR DOUG DC8 DC873F 302199F WP A DHLA O OTHER J N WARNING INDICATION FALSE WARNING NR NOT REPORTED 1 SO 01 804DH 46124 1) ENG #2 SHORT CIRCUIT FIRE WARNING LOOP "B" LIGHT ON. LOOP "A" OK LOOP "B" SHORT INTERMITTENT2) CHECKED WIRING AS PE R WDM 26-01-01, ALL FOUND OK. ITEM TRANSF TO DMI 9566 IAW MEL 26-3-23) REF DMI 9566 ENGÑ2 SHORT CIRCUIT FIRE WARNING L OOP B LIGHT ON. LOOP A OK,LOOP B SHORT INTERMITTENT. 4) R&R CONNECTOR DC63F22K14PN IAW SPM 20-11-02.Ñ2 ENG FIRE WARNI NG TEST OK.THIS CLEARS DMI 9566. 2 L 7 4 4F RT 4A25 2002061300163 20020613 00163 CE 2002 6 13 613021 1 20020613 A 3020 CONTACTOR BEECH MU300 400A 1155402 CE HORIZ STAB FAILED E DJFA K NONE J WARNING INDICATION CR CRUISE 1 EA 23 442CW 4107 RK42 HORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT. 2 H 7 2 4F RT A16SW 2002061300164 20020613 00164 EU 2002 6 13 AWXA200200513 1 20020608 A 2750 D5757030500200A STRUT AIRBUS 320 A320231 3930325 EU T/E FLAP WORN A AWXA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 WP 28 643AW 315 PHX - EMERGENCY LANDING - FLT 0704 - WHILE ON APPROACH INTO PHX EN ROUTE FROM ATL WHEN FLAPS WERE SELECTED FROM 1 TO 2 R ECEIVED AN ALIGNMENT FAULT FOR FLIGHT CONTROL FLAPS LOCKED. MAINTENANCE TROUBLESHOT PER AMM 27-51-00-810-818 AND FOUND THE RT INTERCONNECTING STRUT WORN. REMOVED AND REPLACED INTERCONNECTING STRUT IAW AMM TASK 27-51-44-000-001, OPERATIONA L CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002061300165 20020613 00165 EU 2002 6 13 AWXA200200514 1 20020611 A 3350 52145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 627AW 2605 66 PHX - EEL - PROGRAMMING AND TEST PANEL FAILED TEST OF EMERGENCY LIGHT SYSTEM. MAINTENANCE REPLACED EMERGENCY POWER SUPP LY UNIT 10WL (LT FWD), AND 11WL (LT MIDDLE) IAW AMM 33-51-00-710-001, EMERGENCY LIGHT TEST CHECKED GOOD. 2 L 7 2 4F RT A28NM 2002061300166 20020613 00166 EU 2002 6 13 AWXA200200515 1 20020611 A 7810 FIRE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE TAILPIPE DETECTED A AWXA K NONE A FLAME/FIRE NR NOT REPORTED 1 WP 28 633AW 082 V0351 PHX - TAILPIPE FIRE - FLT 0192 - RAMP PERSONNEL REPORTED A BRIEF TAILPIPE FIRE IN NR 2 ENGINE AFTER SHUT DOWN. MAINTENA NCE PERFORMED A VISUAL INSPECTION OF THE NR 2 ENGINE TAILPIPE PER MM 78-10-00-06, NO DAMAGE OR DEFECTS NOTED. 2 L 7 2 4F 4 F RT A28NM E311NE 2002061300167 20020613 00167 NM 2002 6 13 AWXA200200516 1 20020612 A 3350 20131A BATTERY PACK BOEING 757 757225 1384959 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 907AW 22691 PHX - EEL - DURING INSPECTION THE EMERGENCY EXIT LIGHT ABOVE THE L4 DOOR AND THE LT BULLNOSE PANEL LIGHTS WERE FOUND INO PERATIVE. MAINTENANCE REPLACED THE AFT LT EMERGENCY EXIT LIGHT BATTERY PACK IAW BMM 33-51-07. OPERATIONAL CHECK WAS GO OD. 2 L 7 2 4F RT A2NM 2002061300168 20020613 00168 SO 2002 6 13 C2XA02SH010 1 20020606 A 3350 66368 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14977 145175 SHV - DURING SERVICE CHECK INSPECTION, THE AFT AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND TO BE INOP. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002061300170 20020613 00170 SO 2002 6 13 C2XA02TY097 1 20020612 A 5320 14521725013 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 TYS, DURING A SCHEDULE INSPECTION, THE SERVICE DOOR SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE CORRODED AREAS, AL ODINED AND PAINTED IAW-EMB-SRM-53-21-10. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002061300171 20020613 00171 SO 2002 6 13 C2XA02TY098 1 20020612 A 5320 14524131005 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 TYS, DURING A SCHEDULE INSPECTION, THE PAX DOOR SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE CORRODED AREAS, ALODIN ED AND PAINTED IAW-EMB-SRM-53-21-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF I NSPECTION. 2 L 7 2 4F RT T00011AT 2002061300172 20020613 00172 SO 2002 6 13 C2XA02TY099 1 20020612 A 5320 14590039003 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 TYS, DURING A SCHEDULE INSPECTION, THE AFT SERVICE DOOR SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE CORRODED AREAS , ALODINED AND PAINTED IAW-EMB-SRM-53-21-10. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLET ION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002061300173 20020613 00173 WP 2002 6 13 CALA0200336 1 20020610 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION MID CARGO COMPARTMENT DOOR CUTOUT FORWARD AND AFT LOWER CORNER FITTINGS CORRODED AT STA 636 AND 693 RESPECTIV ELY. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2002061300175 20020613 00175 EU 2002 6 13 DHL2002363007 1 20020608 A 3230 LIGHT AIRBUS 300 A300B4203 3930306 EU COCKPIT INOPERATIVE A DHLA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 363DH 85 LANDING GEAR ON WD PANEL INDICATES NO LIGHT ON LEFT MAIN GEAR. REPLACED LT MLG INDICATION LAMP ON FWD PANEL AND OPS CHE CKS GOOD IAW M/M 33-14-00. 2 L 7 2 4F RT A35EU 2002061300176 20020613 00176 2002 6 13 SWAA021097 4 20020516 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 778SW 27883 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061300177 20020613 00177 NM 2002 6 13 SWAA021099 1 20020520 A 5311 6516302 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME ASSY CRACKED (2 EA) AT BS 196.5, WL 208 AND LBL 28. REPAIRED FRAME PER S RM. 2 L 7 2 4F RT A16WE 2002061300178 20020613 00178 NM 2002 6 13 SWAA021109 1 20020521 A 3350 604222 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 095SW 23054 DURING SCHEDULED PM CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002061300179 20020613 00179 NM 2002 6 13 SWAA021110 1 20020520 A 1100 PLACARD BOEING 737 7377H4 1384404 NM EVAC SLIDE MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INSPECTION PLACARD MISSING. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061300180 20020613 00180 NM 2002 6 13 SWAA021111 1 20020521 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 501SW 24178 EEPLS INOP BETWEEN ROW'S 10 AND 13. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002061300181 20020613 00181 2002 6 13 SWAA021116 4 20020522 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002061300182 20020613 00182 NM 2002 6 13 SWAA021119 1 20020522 A 2731 6545166 ROD END BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED TAB ATTAC H ROD END ASSY'S PER MM. 2 L 7 2 4F RT A16WE 2002061300183 20020613 00183 NM 2002 6 13 SWAA021120 1 20020522 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE AND TIE CLIP CRACKED AT BS 663.75, STR 10. REPAIRED STR SPLICE AND R EMOVED AND REPLACED TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002061300184 20020613 00184 2002 6 13 SWAA021124 4 20020521 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061300185 20020613 00185 NM 2002 6 13 SWAA021125 1 20020522 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 EEPLS WIRES LOOSE ON CABIN FLOOR. SECURED WIRES PER MM. 2 L 7 2 4F RT A16WE 2002061300186 20020613 00186 NM 2002 6 13 SWAA021169 1 20020528 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002061300187 20020613 00187 NM 2002 6 13 SWAA021170 1 20020528 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER MM. 2 L 7 2 4F RT A16WE 2002061300188 20020613 00188 NM 2002 6 13 SWAA021172 1 20020528 A 3350 20121 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT OVERWING EXIT. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002061300189 20020613 00189 NM 2002 6 13 SWAA021176 1 20020528 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED C4 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT BROKEN AT ROW 23. REMOVED AND REPLACED EXIT LIGHT ASSY P ER MM. 2 L 7 2 4F RT A16WE 2002061300190 20020613 00190 NM 2002 6 13 SWAA021177 1 20020528 A 3350 604222 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 089SW 22904 OVERHEAD DOOR EMERGENCY EXIT LIGHTS AND EEPLS INOP. CHARGED EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F A16WE 2002061300191 20020613 00191 2002 6 13 SWAA021186 4 20020530 A 2565 61621 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED S LIDE PER MM. 2 L 7 2 4F RT A16WE 2002061300192 20020613 00192 CE 2002 6 13 GLBA2002081 1 20020610 A 7930 1143890005 OIL COOLER BEECH 1900 1900D 1154162 CE RT WING LEAKING A GLBA E ENGINE SHUTDOWN K FLUID LOSS DE DESCENT 1 NM 03 94GL 19807 UE94 #2 ENG LOST OIL PRESSURE, REPLACED OIL COOLER 2 L 7 2 4T RT A24CE 2002061300193 20020613 00193 NM 2002 6 13 AWXA200200519 1 20020609 A 5313 654988661 STRINGER BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 0 0 23778 MCN - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON STRINGER 16 R/H, AT BS 500C+4. MAINTENANCE TRIMMED OUT CRACK ON STRINGER 16 R/H AT BS 500C+4; PERFORMED HFEC INSPECTION OF CUTOUT TO VERFIY NO CRACKS EXIST; FABRICATED REPAIR CHANN EL, RADIUS FILLER, AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2002061300194 20020613 00194 NM 2002 6 13 S02271003 1 20020223 A 7100 POWERPLANT PWA BOEING 747 747200 1384847 NM PWA JT9 JT9D7R4G2 52054 NE #3 ENG W SAJF C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 03 725331 24308 B18771 A/C RREJECT T/O DUE TO #3 ENG SURGE AND ALL MAIN WHEEL TIRES DEFLATE.C/A:1.ENG CHANGE FOR SHOP INVESTIGATION/RPLD ALL MAIN WHEEL TIRES. 2.PERFORM #3 ENG REPLACEMENT IAW 4L71-301A, ENG R/U TEST COND NML. 3.ALL MAIN WHEEL TIRES(16EA)AN D BRAKES(16EA)RPLD, AND ANTI-SKID SYS, AUTO BRAKE SYS, FUNCTION TEST COND NML AND HIGH ENEERGY STOP INSP PERFORMED. 4.TH E ROOT CAUSE COULD BE MATERIAL DETERIORATION RESULTS IN T1 BLADES FRACTURE. 2 L 7 4 4F 4 F RT A20WE E3NE 2002061300195 20020613 00195 GL 2002 6 13 RAIA00206173 2 20020605 A 7532 23061056 BLEED VALVE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 806HK 5547 145112 310166 5253-PIT- NUMBER ONE ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED #1 ENGINE COMPRESSOR BLEED VALVE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002061300196 20020613 00196 EU 2002 6 13 RAIA00206174 1 20020610 A 2910 PV304426 PUMP JETAIR JETSTM JETSTM4101 1500501 EU OVERHEATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 573HK 20258 9463 41092 5493-STL- RIGHT HYDRAULIC HIGH TEMP CAPTION ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE RIGHT HYDRAULIC PUMP. 2 L 7 2 4T RT A41NM 2002061400002 20020614 00002 SW 2002 6 14 AUS20020414 1 20020426 A 6310 BOLT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL DRIVESHAFT FAILED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 AU S 1127 (AUS) MAIN DRIVESHAFT, FLEXOR BOLT MISSING. INVESTIGATION FOUND THAT THE BOLT HAD FRACTURED INTO TWO PIECES. 1 G 7 1 3U 3 U O H2SW E1GL 2002061400007 20020614 00007 NM 2002 6 14 AUS20020425 1 20020426 A 5310 BEAM BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU CARGO DOORWAY CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FORWARD CARGO DOOR CROSS BEAM OUTER T' CHORD CRACKED AT FORWARD FASTENER HOLE. FOUND DURING INSPECTION IAW AD/B73 7/142. 2 L 7 2 4F 4 F RT A16WE E21EU 2002061400008 20020614 00008 NM 2002 6 14 AUS20020426 1 20020429 A 5415 311T21021 PIN BOEING 767 767338 1385151 NM RROYCE RB211 RB211524* NE NR 1 STRUT CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 1 STRUT, MIDSPAR FUSE PIN CRACKED LONGITUDINALLY INSIDE THE BORE OF THE PIN. CRACK LENGTH APPROXIMATELY 30.48MM (1.2IN). FOUND DURING INSPECTION IAW AD/B767/78. 2 L 7 2 4F 4 F RT A1NM E12EU 2002061400009 20020614 00009 2002 6 14 AUS20020428 4 20020504 A 2565 WASHER BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL ESCAPE SLIDE MISINSTALLED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT ENTRY DOOR AND RT SERVICE DOOR EMERGENCY ESCAPE SYSTEM DEPLOYMENT BAR SEPARATION LINK WASHER INCORRECTLY POSITI ONED IN RELATION TO THE CIRCLIP. FOUND DURING INSPECTION IAW AD/B767/163AND EI 767-025-0412. PERSONNEL/MAINTENANCE ERROR . 2 L 7 2 4F 4 F RT A1NM E23EA 2002061400010 20020614 00010 EU 2002 6 14 AUS20020429 1 20020426 A 5311 TB1021010102 FRAME SOCATA TB10 TB10TOBAGO 8680696 EU LYC O360 O360A1A 41514 EA HARTZL HCC2Y HCC2YK1 GL FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FUSELAGE FRAME NR 9 CRACKED AT BOTH TOP CORNERS. 1 L 7 1 3O 3 O RT A51EU E286 5 C P920 2002061400011 20020614 00011 WP 2002 6 14 2002F00619 1 20020508 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7534A 49988 TUL - FOUND TEMPORARY CLASS III REPAIR DOUBLER REMOVED FOR INSTALLATION OF CLASS I REPAIR. DENT AFT OF TEMP DOUBLER INC LUDED IN DAMAGE CUT OUT. DAMAGE REMOVED FILLER AND DOUBLER INSTALLED PER SRM 53-04 FIG 12B CLASS I REPAIR. (M) 2 L 7 2 4F A6WE 2002061400014 20020614 00014 NE 2002 6 14 AUS20020435 2 20020429 A 7230 13245 COMPRESSOR BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE ENGINE DAMAGED W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S 17087 (AUS) NR 3 ENGINE COULD NOT BE STARTED. BOROSCOPE INSPECTION SHOWED COMPRESSOR AND STATOR DAMAGE. 2 L 7 4 4F 4 F RT A20WE E30NE 2002061400015 20020614 00015 EU 2002 6 14 AUS20020436 1 20020509 A 5497 KP260 WIRE BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE NACELLE/PYLON CHAFED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) WIRE WW268 TO NR 4 TRAILING EDGE PYLON OVERHEAT SWITCH CHAFING ON BOLT HEAD LOCATED IN RT WING ROOT/FLAP AREA (ZON E 286-02-00). 2 H 7 4 4F 4 F RT A49EU E6NE 2002061400016 20020614 00016 EU 2002 6 14 AUS20020437 1 20020510 A 5411 FRAME SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE NACELLE CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT ENGINE NACELLE FRAME (FIGURE 8 FRAME) CRACKED. CRACK LENGTH IS AT LEAST 100MM (4IN) LONG. SUSPECT AREA HAD BEEN SUBJECTED TO HIGH TEMPERATURES AND DISTORTION AT SOME STAGE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002061400017 20020614 00017 NM 2002 6 14 AUS20020439 1 20020511 A 2730 RIVET BOEING 747 74748E 2FOR NM GE CF6 CF680C2* GL ELEVATOR FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT ELEVATOR IDLER CRANK RIVETS SHEARED. 2 L 7 2 4F 4 F RT A20WE E23EA 2002061400018 20020614 00018 WP 2002 6 14 AALA20020670 1 20020425 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND LEFT VERTICAL STABILIZER TO FUSELAGE SKATE ANGLE CRACKED APPROX STATION 1485. REPAIRED PER AARD 53-10-00-2 DATED 10-02-2000. (M) 2 L 7 2 4F A6WE 2002061400019 20020614 00019 NM 2002 6 14 AUS20020440 1 20020509 A 7110 LATCH BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE ENGINE COWLING MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 3 ENGINE CORE COWL PANEL FORWARD LATCH AND RETAINING COVER MISSING. 2 L 7 4 4F 4 F RT A20WE E30NE 2002061400020 20020614 00020 NM 2002 6 14 AUS20020441 1 20020513 A 3241 CONNECTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE BRAKE ANTISKID LOOSE W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT INBOARD ANTI-SKID TRANSDUCER CONNECTOR PLUG LOOSE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002072200047 20020722 00047 EU 2002 7 22 2002UALA00957 1 20020606 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 415UA 475 AFT LEFT INT LOADS FAULT EMERGENCY LIGHT SYSTEM. REPLACED AFT LEFT EMERGENCY BATTERY. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2002061400021 20020614 00021 NE 2002 6 14 AUS20020442 2 20020509 A 7200 6058T83G01 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R375 R3754123F21 NE LEFT LEAKING W A UNSCHED LANDING E K VIBRATION/BUFFET FLUID LOSS CL CLIMB 1 AU S 7 (AUS) LT ENGINE LEAKING OIL FROM AREA OF THE B' SUMP. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P17NE 2002061400022 20020614 00022 EA 2002 6 14 AUS20020445 1 20020510 A 7931 PCE42139 INDICATOR DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL ENGINE OIL PRESS FAULTY W O OTHER N FALSE WARNING NR NOT REPORTED 1 AU S (AUS) LT ENGINE OIL PRESSURE INDICATION SYSTEM FAULTY. 1 H 7 2 3T 4 T RT A9EA E4EA 6 C P15EA 2002061400024 20020614 00024 EU 2002 6 14 AUS20020448 1 20020225 A 7722 54285538010 GAUGE AMD FALC50 FALCON900 2700160 EU GARRTT TFE731 TFE7315R 01518 WP ENGINE EGT/TIT FAULTY W O OTHER N FALSE WARNING NR NOT REPORTED 1 AU S 6 (AUS) ENGINE ITT GAUGE DIGITAL READOUT DIFFERENT TO ANALOGUE READOUT. 2 L 7 3 4F 4 F RT A46EU E6WE 2002061400025 20020614 00025 2002 6 14 AUS20020449 4 20020311 A 3417 7000700647 ADC AMD FALC50 FALCON900 2700160 EU GARRTT TFE731 TFE7315R 01518 WP COCKPIT FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) AIR DATA COMPUTER (ADC) FAULTY. 2 L 7 3 4F 4 F RT A46EU E6WE 2002061400029 20020614 00029 CE 2002 6 14 AUS20020453 1 20020509 A 1430 4410042 FASTENER CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP HARTZL HCB3T HCB3TN5 GL FUSELAGE MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) CHERRY RIVETS IN FUSELAGE EMERGENCY EXIT DOOR CUTOUT FRAMEPREVENTING OPERATION OF EMERGENCY EXIT. 1 L 7 2 3T 4 T RT A28CE E4WE 6 C P15EA 2002061400031 20020614 00031 CE 2002 6 14 AUS20020456 1 20020516 A 2435 230800251 STARTER GEN CESSNA 500 550 2076604 CE PWA 530 PW530A NE LT ENGINE SEIZED W A UNSCHED LANDING H F ELECT. POWER LOSS-50 PC FLT CONT AFFECTED CR CRUISE 1 AU S 129 (AUS) LT ENGINE STARTER-GENERATOR SEIZED. SUSPECT CAUSED BY FAILURE OF THE FAN END BEARING. EVIDENCE OF POLING. 1 L 7 2 4F 4 F A22CE E00053EN 2002061400032 20020614 00032 NE 2002 6 14 AUS20020463 2 20020515 A 7210 24105 GEAR AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL2B NE ENGINE BROKEN W K NONE O OTHER IN INSP/MAINT 1 AU S 301 (AUS) BROKEN GEAR TOOTH FOUND LODGED BEHIND THE REDUCTION GEAR MAGNETIC PLUG RECEPTACLE. 1 G 7 2 3U 3 U H10EU E00054EN 2002061400033 20020614 00033 CE 2002 6 14 AUS20020464 1 20020513 A 2897 57181061 HARNESS CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP HARTZL HCB3T HCB3TN5 GL FUEL BOOST WORN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT FUEL BOOST PUMP WIRING HARNESS CHAFED. FOUND DURING INSPECTION IAW SB CQB02-1. 1 L 7 2 3T 4 T RT A28CE E4WE 6 C P15EA 2002061400034 20020614 00034 NM 2002 6 14 DL72E020609 1 20020530 A 5711 65192923 SPAR BOEING 727 727247 138408F NM CENTER WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 INSPECTION OF THE CENTER WING REAR SPAR WEB PER AD 2000-14- 07 AND BAC S/B 727-57A0182 REVEALED A .25 INCH CRACK IN THE WEB BELOW THE UPPER SPAR CAP. THE CRACK WAS ROUTED OUT OF THE WEB WITH A 2 INCH CUTOUT AND REPAIRED WITH AN ALUMINUM R EPAIR DOUBLER PER ER/A 383243-14AD, REV A. 2 L 7 3 4F A3WE 2002061400035 20020614 00035 EA 2002 6 14 AUS20020465 2 20020510 A 7200 PT6A41 ENGINE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA HARTZL HCD4N3 HCD4N3A GL LT AND RT MAKING METAL W O OTHER E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 AU S (AUS) LT AND RT ENGINE CHIP DETECTORS ILLUMINATED IN FLIGHT. CHIP DETECTORS ON BOTH ENGINES CONTAMINATED WITH METAL FLAK ES. FLAKES APPEAR TO BE A MIXTURE OF BRONZE, FERROUS AND NON FERROUS PARTICLES. 1 L 7 2 4T 4 T A24CE E4EA 5 C STC 2002061400036 20020614 00036 NM 2002 6 14 DL72S020588 1 20020523 A 5330 6518420406 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 A CRACK WAS FOUND IN THE BONDED SKIN ASSY AND UNDERLYING BEARSTRAP OF THE LOWER HINGE CUTOUT OF THE L1 DOOR CUTOUT. THE CRACK WAS ROUTED OUT OF THE SKIN AND THE BEARSTRAP. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 383225-14, REV A. 2 L 7 3 4F A3WE 2002061400037 20020614 00037 NM 2002 6 14 AUS20020467 1 20020520 A 2530 34814 CHILLER BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL GALLEY FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AU S 3436 (AUS) CHILLER SUSPECT FAULTY. LIMITED INFORMATION PROVIDED. 2 L 7 2 4F 4 F RT A1NM E23EA 2002061400038 20020614 00038 GL 2002 6 14 AUS20020468 2 20020519 A 7321 8061865 MEC BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL FUEL CONTROL FAULTY W O OTHER E VIBRATION/BUFFET LD LANDING 1 AU S (AUS) LT MAIN ENGINE CONTROL FAULTY. LIMITED INFORMATION PROVIDED. 2 L 7 2 4F 4 F RT A1NM E23EA 2002061400039 20020614 00039 NM 2002 6 14 DL72S020595 1 20020526 A 2120 RAM AIR DOOR BOEING 727 727232 1384082 NM A/C SYSTEM STUCK A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 522DA 21582 AT GATE WITH APU POWER,TURNED PACKS ON AND CABIN FILLED WITH SMOKE. FOUND RT PACK RAM AIR SCOOP CK VALVE STUCK OPEN. F REED DOOR, RAN PACKS, RAN ENGINES 1 AND 3. PACK OPERATING, NO FURTHER SMOKE OR FUMES IN CABIN. OK FOR SERVICE. 2 L 7 3 4F A3WE 2002061400040 20020614 00040 EU 2002 6 14 AUS20020470 1 20020522 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R375 R3754123F21 NE AVIONICS BAY FAULTY W O OTHER N FALSE WARNING CL CLIMB 1 AU S (AUS) AVIONICS SMOKE DETECTION SYSTEM OPERATED. NO SIGN OF SMOKE COULD BE FOUND. SYSTEM COULD NOT BE FAULTED AND IT IS S USPECTED THAT DUST IN THE AVIONICS BAY MAY HAVE ACTIVATED THE DETECTORS. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P17NE 2002061400042 20020614 00042 NE 2002 6 14 AUS20020479 2 20020527 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R375 R3754123F21 NE RIGHT FAILED W O OTHER E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AU S (AUS) RT ENGINE LOST OIL ON STARTUP. OIL CONTAMINATION OF TURBINE BLADES. LIMITED INFORMATION PROVIDED. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P17NE 2002061400043 20020614 00043 WP 2002 6 14 CALA0200338 1 20020612 A 5320 WEB DOUG DC9 DC982 3022082 WP STA 1463 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12811 49265 INSPECTION FOUND TAIL COMPARTMENT BELTFRAME WEB CRACKED AT STA 1463 L18R AND L18L. BOTH CRACKS WERE 2" LONG. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 2002061400044 20020614 00044 NM 2002 6 14 CALA0200339 1 20020613 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 787 & 797 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69348 23586 INSPECTION FOUND MAIN CABIN FLOOR R/H I/B SEAT TRACK HAD CORROSION AND WORN LOBES AT BS 787 AND 797, THE CORRODED AND WO RN SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK SECTION WAS SPLICED IN IAW SRM 53-00-52, FIGURE 204. 2 L 7 2 4F RT A16WE 2002061400045 20020614 00045 NM 2002 6 14 CALA0200340 1 20020612 A 2612 894481 DETECTOR BOEING 737 737524 1384721 NM APU SHORTED A CALA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 09 17644 28905 THE APU FIRE WARNING SOUNDED AFTER APU START ON FINAL APPROACH TO ATL. THE BELL WAS SILENCED AND THE APU FIRE CHECKLIST WAS RUN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE PROBLEM WAS IDENTIFIED AS A FA LSE FIRE WARNING AND THE CAUSE WAS DETERMINED TO BE A SHORTED APU LOWER FIRE DETECTION LOOP. THE APU FIRE BOTTLE AND LOW ER FIRE LOOP WERE REMOVED AND REPLACED IAW MM 26-15-14 AND 26-22-11. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2002061400046 20020614 00046 WP 2002 6 14 CALA0200341 1 20020614 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12811 49265 INSPECTION FOUND A 1" CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, LONGERON 1. REPAIRED BELTFRAME IAW SRM 53-03, FIG URE 4. 2 L 7 2 4F A6WE 2002061400047 20020614 00047 NE 2002 6 14 DL72S020607 2 20020529 A 7230 COMPRESSOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE DAMAGED A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 543DA 79046 22392 687367 NR 3 ENG WOULD NOT ACCELERATE ON ADDING T/O POWER. ABORTED T/O AT ABOUT 30 KTS. BORESCOPE INSPECTED 3 ENG 6 AND 7 STG COMP. FOUND 7 STG COMP BLD DAMAGE BEYOND M/M LIMITS. FULL LENGTH OF BLD. ALL BBLDS DAMAGED (361774). REPLACED 3 ENG PER CARD DECK 4T203. 2 L 7 3 4F 4 F A3WE E2EA 2002061400048 20020614 00048 NM 2002 6 14 DL72S020624 1 20020604 A 5532 652274131 PANEL BOEING 727 727225A 1384077 NM VERTICAL STAB MISSING A DALA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 27 8875Z 21293 TOP CAP ON VERTICAL STABILIZER MISSING. REPLACED PANEL. 2 L 7 3 4F RT A3WE 2002061400049 20020614 00049 EA 2002 6 14 AUS20020480 2 20020523 A 8500 L3828614 ENGINE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL LEFT SEIZED W C ABORTED TAKEOFF E Y VIBRATION/BUFFET ENGINE STOPPAGE TO TAKEOFF 1 AU S (AUS) LT ENGINE SEIZED. LOSS OF ENGINE OIL. METAL CONTAMINATION OF OIL FILTER. LIMITED INFORMATION PROVIDED. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2002061400051 20020614 00051 NM 2002 6 14 DL733020608 1 20020530 A 5270 PROXIMITY SENSOR BOEING 737 737347 1384647 NM CARGO DOOR FAULTY A DALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 27 309WA 23442 FWD CARGO DOOR LIGHT CAME ON DURING T/O AT 130 KTS. CONTINUED T/O AND RETURNED TO AIRPORT. CARGO DOOR IND LIGHT INTERM ITTENT. REPLACED FWD CARGO DOOR SENSOR PER M/M, DOOR IND OPS NORMAL. 2 L 7 2 4F RT A16WE 2002061400052 20020614 00052 NM 2002 6 14 DL733020630 1 20020607 A 5330 6545857506 SKIN BOEING 737 737347 1384647 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312WA 23598 TWO LARGE DENTS WERE FOUND IN FUSELAGE SKIN BETWEEN STA 907 AND 957 AND S-20R AND 25R. THERE WAS ALSO AN EXISTING REPAI R IN THE AREA. THE DAMAGED SKIN AREA WAS TRIMMED AWAY AND EXISTING REPAIR REMOVED. A NEW SECTION OF SKIN WAS SPLICED I N AT FS 957 FORWARD TO END OF PANEL. 2 L 7 2 4F RT A16WE 2002061400053 20020614 00053 NM 2002 6 14 DL733020631 1 20020606 A 5330 654577655 SKIN BOEING 737 737347 1384647 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312WA 23598 A NEW SECTION OF SKIN WAS SPLICED IN FROM FS 907 TO 957 AND S-20R TO 25R PER ER/A 383228-14. A SECTION OF THE LOWER SKI N WAS FOUND TO BE ROUTED OUT IN THE LAP SPLICE AREA AT APPROXIMATELY FS 935 AND S-25R. AFTER INSTALLATION OF THE NEW UP PER SKIN, THE LOWER SKIN WAS REPAIRED PER SRM 53-00-01, FIGURE 210 WITH MINOR DEVIATIONS. 2 L 7 2 4F RT A16WE 2002061400054 20020614 00054 NM 2002 6 14 DL738020597 1 20020527 A 3350 A417424 LIGHT BOEING 737 737832 13844CF NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3746H 30488 FUSELAGE EMERGENCY LIGHT INOP ON RT SIDE OF AIRCRAFT BETWEEN THE FWD AND AFT EMERGENCY EXIT DOORS. RELAMPED EMERGENCY L IGHT. 2 L 7 2 4F RT A16WE 2002061400055 20020614 00055 NM 2002 6 14 DL757020590 1 20020524 A 2530 ODOR BOEING 757 757232 1384965 NM GALLEY DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 656DL 24396 SMOKE SMELL IN MID GALLEY AFTER 1 HOUR OF FLIGHT. PULLED ALL C/BS AND TURNED OFF ENTERTAINMENT EQUIPMENT. SMELL WENT AW AY, DON'T KNOW WHICH SYSTEM WAS THE CAUSE. PUSHED ALL C/BS IN MID GALLEY TURNED ON VIDEO AND COFFEEMAKERS AND LIGHTS, W AITED 20 MINUTES AND NO SMOKE SMELL NOTED COULD NOT DUPLICATE, OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2002061400056 20020614 00056 NM 2002 6 14 DL757020604 1 20020525 A 5310 146N851210 DOOR FRAME BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 646DL 24217 THE OUTER CHORD OF THE C2 DOOR OPENING LOWER SILL WAS FOUND CORRODED AND REQUIRED REPLACEMENT. THE LOWER SECTION OF CHO RD AND WEB WERE REMOVED. A NEW SILL CHORD WAS INSTALLED AND THE FRAME CHORD AND WEB SPLICED WITH ALUMINUM REPAIR ANGLES AND DOUBLERS PER ER/A 383023-14, REV A. 2 L 7 2 4F RT A2NM 2002061400057 20020614 00057 NM 2002 6 14 DL757020614 1 20020602 A 2432 BA0601 BATTERY BOEING 757 757232 1384965 NM E/E BAY SHORTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 678DL 25983 FLT CREW REPORTED VISIBLE SMOKE IN AFT GALLEY WHILE AT GATE PRIOR TO BOARDING. CONTRACT MTC FOUND APU BATTERY SHORTED A ND THE SOURCE OF SMELL/SMOKE. REPLACE THE APU BATTERY. THE BATTERY CHARGER AND THE K117 START CONTACTOR. 2 L 7 2 4F RT A2NM 2002061400058 20020614 00058 NM 2002 6 14 SWAA021187 1 20020529 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED PM CHECK, FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2002061400059 20020614 00059 NM 2002 6 14 SWAA021189 1 20020529 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 103SW 23109 DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2002061400060 20020614 00060 NM 2002 6 14 SWAA021190 1 20020530 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 691WN 23781 FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002061400061 20020614 00061 NM 2002 6 14 SWAA021191 1 20020530 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 612SW 27930 AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2002061400062 20020614 00062 NM 2002 6 14 SWAA021192 1 20020530 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002061400063 20020614 00063 NM 2002 6 14 SWAA021193 1 20020530 A 3350 65C27093 LIGHT BOEING 737 7372K6 1364440 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 129SW 22340 AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002061400064 20020614 00064 2002 6 14 SWAA021194 4 20020530 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002061400065 20020614 00065 NM 2002 6 14 SWAA021199 1 20020531 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 104SW 23110 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASS Y PER MM. 2 L 7 2 4F A16WE 2002061400066 20020614 00066 2002 6 14 SWAA021205 4 20020601 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061400067 20020614 00067 2002 6 14 SWAA021206 4 20020602 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 102SW 23108 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002061400068 20020614 00068 NM 2002 6 14 SWAA021207 1 20020531 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT ASSY FELL OUT. REINSTALLED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2002061400069 20020614 00069 NM 2002 6 14 SWAA021208 1 20020602 A 2612 0881031007 SWITCH BOEING 737 7373H4 1384600 NM COCKPIT DEFECTIVE A SWAA K NONE N FALSE WARNING CR CRUISE 1 SW 29 637SW 27710 DURING FLIGHT, THE FIRE WARNING BELL CAME ON. REMOVED AND REPLACED BELL CUTOUT SWITCH PER MM. 2 L 7 2 4F RT A16WE 2002061400070 20020614 00070 NM 2002 6 14 SWAA021210 1 20020531 A 2731 65C26384 TAB BOEING 737 7373H4 1384600 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002061400071 20020614 00071 NM 2002 6 14 SWAA021211 1 20020531 A 2782 285A1200 ACTUATOR BOEING 737 7377H4 1384404 NM L/E SLAT FAILED A SWAA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 29 758SW 27873 AIR TURNBACK, AFTER TAKEOFF L/E TRANSIT LIGHT ILLUMINATED, L/E DEVICES WOULD NOT FULLY RETRACT. REMOVED AND REPLACED NR 5, NR 7 AND NR 8 L/E SLAT ACTUATORS PER MM, ( S/N'S D00518, 2176 AND 5025 ). 2 L 7 2 4F RT A16WE 2002061400072 20020614 00072 SO 2002 6 14 C2XA02CL131 1 20020613 A 3350 110049 POWER SUPPLY EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14940 145033 DURING ROUTINE MAINTENANCE THE EXTERNAL EMERGENCY LIGHT OVER THE LEFT AND RIGHT WING AND AISLE CEILING LIGHT AT ROW 14 W ERE FOUND INOPERATIVE.MAINTENANCE REPLACED THE #4 BATTERY POWER SUPPLY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS REL EASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002061400073 20020614 00073 2002 6 14 SWAA021214 4 20020602 A 2565 D31354 SLIDE BOEING 737 7373TO 138447G NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER INADVERTENTLY. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061400074 20020614 00074 2002 6 14 SWAA021218 4 20020602 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 102SW 23108 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002061400075 20020614 00075 NM 2002 6 14 SWAA021219 1 20020602 A 3350 7003665 BALLAST BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM. 2 L 7 2 4F RT A16WE 2002061400076 20020614 00076 NM 2002 6 14 SWAA021221 1 20020603 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002061400077 20020614 00077 NM 2002 6 14 SWAA021223 1 20020602 A 2731 65L30878 TAB BOEING 737 7373H4 1384600 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVAT OR TAB CRANK ASSY PER MM. 2 L 7 2 4F RT A16WE 2002061400078 20020614 00078 NM 2002 6 14 SWAA021226 1 20020603 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 12L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002061400079 20020614 00079 SO 2002 6 14 SWIA200210815 1 20020423 A 1430 FASTENER EMB 120 EMB120ER 3260203 SO FUEL DOOR LOOSE A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 214SW 120280 ABORTED TAKEOFF AT 60 KIAS DUE TO A MAP RED DOOR LIGHT ILLUMINATING. FOUND CAMLOCK ON FUEL SERVICE DOOR UNSECURED. SEC URED CAMLOCK ON FUEL DOOR. OPS CHECK GOOD. ALL PANELS SECURED. 2 L 7 2 4T RT A31SO 2002061400080 20020614 00080 EU 2002 6 14 0129 1 20020102 A 2910 HYDRAULIC LINE AMD FALC50 FALCON50MYST 2730106 EU HYD SYSTEM CRACKED E DJFA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 23 523CW 23 AIRCRAFT DEPARTED CGF, DURING THE CLIMB THE PILOTS NOTICED THE HYDRAULIC PRESSURE DECREASING IN FLIGHT. CONTACTED TOWER AND REQUESTED RETURN TO CGF. DURING RETURN TO CGF AIRCRAFT LOST HYDRAULIC PRESSURE. LANDING GEAR WAS EXTENDED AND AIR CRAFT LANDED WITH NO PROBLEMS. TECHNICIANS FOUND STEEL LINE ATTACHED TO HYD ACCUMULATOR CRACKED. REPLACED LINE, ACCUMU LATOR, NUMBER 1 AND 2 ENGINE HYD PUMPS DUE TO THE POSSIBILITY OF OIL STARVATION. 2 L 7 3 4F A46EU 2002061400081 20020614 00081 CE 2002 6 14 613022 1 20020613 A 3010 CONTACTOR BEECH MU300 400A 1155402 CE HORIZ STAB FAILED E DJFA K NONE J WARNING INDICATION CR CRUISE 1 EA 23 494CW 3430 RK4 HORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT. 2 H 7 2 4F RT A16SW 2002061400082 20020614 00082 CE 2002 6 14 613023 1 20020613 A 3010 CONTACTOR BEECH MU300 400A 1155402 CE HORIZ STAB FAILED E DJFA K NONE J WARNING INDICATION CR CRUISE 1 EA 23 406CW 4702 RK6 HORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT. 2 H 7 2 4F RT A16SW 2002061400083 20020614 00083 EU 2002 6 14 AWXA200200517 1 20020612 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 5983 098 PHX - EEL - DURING L-2 DOOR SLIDE CHANGE AND TEST THE EMERGENCY LIGHT SYSTEM FAULTED, FOUND MIDDLE LT CABIN EMERGENCY PO WER SUPPLY UNIT HAD INTERIOR LIGHTS FAULT. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 11WL IAW 33-51- 32-401, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002061400084 20020614 00084 NM 2002 6 14 AWXA200200518 1 20020612 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 823AW 1463 CMH - EMERGENCY EQUIPMENT - DURING INSPECTION THE FORWARD INBOARD EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE FORWARD INBOARD EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002061400085 20020614 00085 EU 2002 6 14 CX7A194J7 1 20020613 A 2613 1734362450 SENSING ELEMENT SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A CX7A E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 03 305CE 340B202 RIGHT TAILPIPE HOT ILLUMINATED IN FLIGHT. RAN CHECK LIST, SHUTDOWN RT ENGINE. 2 L 7 2 4T RT A52EU 2002061400086 20020614 00086 NM 2002 6 14 DL757020619 1 20020603 A 3350 3166981 LIGHT BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 683DA 27103 L-1 DOOR EXT DOOR SLIDE EMERGENCY LIGHT INOP. REPLACED REFLECTOR. 2 L 7 2 4F RT A2NM 2002061400087 20020614 00087 NM 2002 6 14 DL757020621 1 20020603 A 5753 113N380084 SKIN BOEING 757 757232 1384965 NM T/E FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 622DL 22912 OUTBOARD AFT FLAP TRAILING EDGE REPAIR TO LOWER SKIN AND SPAR. REPAIRED PER ER/A 417406-14. 2 L 7 2 4F RT A2NM 2002061400088 20020614 00088 NE 2002 6 14 DL757020632 2 20020607 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 MALFUNCTIONED A DALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 625DL 41514 22915 716524 AT 10,000 FEET RT ENG SURGED, EGT WENT TO 678, A/C PITCHED LEFT. C/W ENG SURGE CK LIST, PER F/A SPARKS STILL COMING FRO M RT ENG. C/W RT ENG SHUTDOWN. REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002061400089 20020614 00089 NE 2002 6 14 DL76L020635 2 20020607 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 MALFUNCTIONED A DALA K NONE R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SO 27 186DN 23193 727679 27962 727679 LEFT ENGINE SURGE DET MSG ENG PARAMETERS NOTED ON PERF PG AUTO EVENT. BORESCOPE PER FIM 71-05-00. NO ABNORMAL COND NOT ED. PERFORMED ACCEL/DECEL SNAP TEST PER FIM. TEST OK. PERFORMED PFHB TEST 4. TEST OKAY. ALL PARAMETERS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2002061400090 20020614 00090 NM 2002 6 14 DL76S020600 1 20020528 A 2120 ODOR BOEING 767 767332 1382001 NM CABIN DETECTED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 128DL 24078 RTB - CREW REPORTS ELECTRICAL ODOR IN MID GALLEY / CABIN AREA. ONLY DETECTABLE ODOR COMING FROM MID GALLEY LIFE RAFT ST OWAGE COMPT, SEEMS TO BE COMING FROM LIFE RAFT ITSELF. RAN ENGS PACKS AND LOADED ALL ELECTRICS TAXIED A/C IN SAME CONFI G AS CREW UNABLE TO DUPLICATE. REMOVED LIFE RAFT PER MEL 25-99-02B, FWD TO MCO AND PLAC. 2 L 7 2 4F RT A1NM 2002061400091 20020614 00091 2002 6 14 DL76S020606 4 20020529 A 2330 250008632 PROJECTOR BOEING 767 767332 1382001 NM CABIN FAULTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 126DL 24076 AT CRUISE F/A'S NOTICED SMELL IN MID CABIN AREA. TENTATIVE IDENTIFIED AS PROJECTOR 525. ALL PROJECTORS TURNED OFF FOR DURATION OF FLT. PROJECTOR VERIFIED AS HAVING ELECT SMELL. DEACTIVATED PROJECTOR, FWD TO MCO AND PLA-MEL 25-20-02L. 2 L 7 2 4F RT A1NM 2002061400092 20020614 00092 NE 2002 6 14 DLM11020575 2 20020521 A 7200 PW44603 ENGINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 STALLED A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 808DE 26317 48479 733741 NR 3 ENG STALLED ON T/O ROLL AT 30 KNOTS. REMOVED AND REPLACED NR 3 ENG PER ROUTINE CARD DECK. 2 L 7 3 4F 4 F RT A22WE E24NE 2002061400093 20020614 00093 NE 2002 6 14 DLM11020625 2 20020605 A 7200 PW44603 ENGINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 2 MALFUNCTIONED A DALA J A DUMP FUEL UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 811DE 40910 723928 48566 723928 DURING CLIMB OUT TO 20K HAS SMOKE IN COCKPIT AND CABIN. SMOKE IN COCKPIT CLEARED AFTER PROCEDURES C/W. DUMPED FUEL AND DECLARED EMERGENCY. NR 2 ENGINE REPLACED DUE TO HISTORY OF NOSE BLEED AND WATER SEPARATOR BAG CONTAMINATION. 2 L 7 3 4F 4 F RT A22WE E24NE 2002061400094 20020614 00094 NE 2002 6 14 DLM11020633 2 20020605 A 7261 PW44603 ENGINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 LEAKING A DALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 811DE 40910 48566 723928 SMOKE IN COCKPIT AND CABIN DURING CLIMBOUT ALL SMOKE DETECTORS IN ALL LAVS WERE BEEPING. T/S TO NR 2 ENG INTAKE OIL LEA K, NEEDS ENGINE CHANGE. NEEDS DUCT BURNOUT PERFORMED. 2 L 7 3 4F 4 F RT A22WE E24NE 2002061400095 20020614 00095 NM 2002 6 14 DLM88020605 1 20020528 A 2910 AS15308K0254 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM CHAFED A DALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 968DL 53161 DURING DESCENT THROUGH 15,000 FT RECEIVED LOW RT HYD PRESS AND QUANTITY MESSAGES, HAD NOT USED FLAPS OR SPOILERS AT THAT POINT. HYD PRESSURE WAS ALREADY 0 AND HYD QTY WAS 1 QUART. RT PUMP WAS UNFEATHERED FOR 2 MINUTES BEFORE COMING TO THA T POINT IN CKLIST. FOUND BRAIDED PRESSURE LINE AT 2 ENG EDP PRESS FILTER MODULE CHAFED. REMOVED LINE. REPLACED LINE. LEAK CHECK OK. REPLACED RT ENG EDP RT EDP PRESS FILTER AND CASE DRAIN FILTER PER AMM. OPS AND LEAK CHECK OK. 2 L 7 2 4F RT A6WE 2002061400096 20020614 00096 NM 2002 6 14 DLM88020610 1 20020531 A 3320 MB10R20M CONNECTOR DOUG MD88 MD88 3023688 NM CABIN DAMAGED A DALA K NONE M OVER TEMP IN INSP/MAINT 1 SO 27 964DL 49983 FOUND DURING COMPLETION OF EO 9-85695-3AD REV A ME01 HEAT DAMAGE TO AIRCRAFT SIDE CONNECTOR OF BALLAST B6-51 ABOVE SEAT 12 D-E. REPLACED RECEPTACLE MB10R6, OPS CHECK NORMAL. 2 L 7 2 4F RT A6WE 2002061400097 20020614 00097 NM 2002 6 14 DLM88020613 1 20020602 A 2910 AS15308K025 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM RUPTURED A DALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 953DL 49884 RT ENG PRESSURE LINE IN AFT COMPARTMENT RUPTURED CAUSING RT SYS FAILURE AND LT GEAR DOOR DAMAGE ON LANDING. FOUND NR 2 ENG HIGH PRESSURE FLEX LINE BURST JUST BEFORE HIGH PRESSURE FILTER MODULE AND ADEL CLAMP BROKEN ON HYDRAULIC LINE WHERE IT MEETS THE FLEX LINE. REPLACED FLEX LINE AND BROKE CLAMP REF M/M. NEED LEAK CHECK. LEAK CHECK FLEX LINE. REPLACED RIGHT SYS ELECTRIC HYD PUMP AND RIGHT SYS FILTERS PER M/M. NO METAL NOTED AND FLUID IS CLEAN. LEAK CHECKS OK. 2 L 7 2 4F RT A6WE 2002061400098 20020614 00098 WP 2002 6 14 211001003 1 20020421 A 1430 BOLT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE SERVICE DOOR BROKEN B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 191AJ 53191 AFT GALLEY SERVICE DOOR INTERNAL HANDLE RETAINING BOLT BROKEN. REMOVED SHEARED BOLT IAW SM, REAMED HOLE IN SHAFT ASSEMB LY. INSTALLED HELI-COIL, REMOVED HOLE IN HANDLE, FABRICATED BUSHING, INSTALLED BUSHING IN HANDLE, INSTALLED DOOR HANDLE . 2 L 7 2 4F 4 F RT A6WE E2EA 2002061400099 20020614 00099 WP 2002 6 14 211002002 1 20020509 A 5330 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE BULGED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 BULGE AT STA 237 AND 1.1 INCH FROM CENTER OF LONGERON 17L UP TOWARD 16L. REPAIRED AND REINSTALLED ACCESS PARTS. 2 L 7 2 4F 4 F RT A6WE E2EA 2002061400100 20020614 00100 WP 2002 6 14 DU42002F00002 1 20020513 A 2560 MS2000197200 HINGE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE R1 DOOR CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 RIGHT NR 1 DOOR LINER ESCAPE SLIDE HINGE HAS CORROSION. CORRECTIVE ACTION: REMOVED ESCAPE SLIDE DOOR AND HINGE REMOVED CORROSION. MATERIAL LOSS MORE THAN 50 PERCENT, OUT OF LIMITS IAW SRM. REPLACED HINGE, INSTALLED SLIDE DOOR AND CLEANE D ALL IAW MM, SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002061400101 20020614 00101 WP 2002 6 14 DU4R211002003 1 20020509 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE BULGED A DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 LONGERON 18L UPPER LAP SEAM BULGE. PERFORMED INSPECTION OF INDICATED AREA, NO CRACKS NOTED. FABRICATED REPAIR DOUBLER AND INSTALLED ALL IAW SRM. 2 L 7 2 4F RT A6WE 2002061400102 20020614 00102 WP 2002 6 14 DU4R211002007 1 20020519 A 5347 59366634505 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 AFT CARGO RIGHT TIE DOWN TRACK CORRODED FS 1211-1320. REMOVED AND REPLACED RIGHT TIE DOWN TRACK FS 1211-1320 IAW SRM. 2 L 7 2 4F RT A6WE 2002061400103 20020614 00103 WP 2002 6 14 DU4R211002008 1 20020509 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 (SKIN) FS 1281 BETWEEN LONGERONS 25L AND 24L, THERE IS A DENT 2.5 ABOVE 25L CENTERLINE. DENT FOUND TO BE COND INBOARD C OLD WORKED. DENT TO CONTOUR OF FUSE SKIN HFEC INSPECTED AREA NO DEFECTS NOTED FABRICATED AND INSTALLED REPAIR DOUBLER I AS SRM. 2 L 7 2 4F RT A6WE 2002061400104 20020614 00104 WP 2002 6 14 DU4R211002009 1 20020513 A 5753 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP DENTED A DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 RIGHT INBOARD AFT FLAP SECTION, LOWER SURFACE HAS NUMEROUS DENT FROM STA. XCW 60.0 TO 104.5. REMOVED RIGHT INBOARD AFT FLAP SECTION STA XCW 60-104.5, REMOVED LOWER SKIN, FABBED, AND INSTALLED. 2 L 7 2 4F RT A6WE 2002061400105 20020614 00105 WP 2002 6 14 DU4R211002010 1 20020513 A 5753 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP GOUGED A DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 RT O/B AFT FLAP LOWER SKIN IS GOUGED AT STA XRS 270. INSTALLED REPAIRED DOUBLER IAW SRM. 2 L 7 2 4F RT A6WE 2002061400106 20020614 00106 WP 2002 6 14 DU4R211002239 1 20020517 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 DENT FOUND RIGHT FUSE STA 503-522 LONG 20. GAINED ACCESS INSTALLED PERMANENT REPAIR RIGHT FUSE FS 503 S22 LONG 20 IAW S RM. RESTORED AREA ACCESSED. 2 L 7 2 4F RT A6WE 2002061400107 20020614 00107 WP 2002 6 14 DU4R211022006 1 20020519 A 5347 S2922357 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 REMOVED AND REPLACED AFT CARGO TIE DOWN TRACK STA 1320-1140 LEFT IAW SRM. 2 L 7 2 4F RT A6WE 2002061400108 20020614 00108 NM 2002 6 14 RYN2002F00017 1 20020526 A 5312 PRESSURE PANEL BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 C-CHECK, FOUND CRACK AT RIGHT MAIN LANDING GEAR WEB, LOWER HALF OUTBOARD SIDE, AT STATION 870, WATER LINE 148. 2 L 7 3 4F A3WE 2002061400109 20020614 00109 NM 2002 6 14 RYN2002F00018 1 20020526 A 5312 PRESSURE PANEL BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 C-CHECK, FOUND CRACK IN WEB, AT LEFT MAIN LANDING GEAR, LOWER HALF OF OUTBOARD SIDE, AT STATION 870, WATER LINE 148. 2 L 7 3 4F A3WE 2002061400110 20020614 00110 NM 2002 6 14 RYN2002F00019 1 20020525 A 5320 SPLICE BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 C-CHECK, FOUND CORROSION IN E AND E COMPARTMENT, ON STRINGER SPLICE, AT STATION 440, STRINGER 24R. 2 L 7 3 4F A3WE 2002061400111 20020614 00111 NM 2002 6 14 RYN2002F00020 1 20020525 A 5320 SPLICE BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 C-CHECK, FOUND CORROSION IN THE E AND E COMPARTMENT, STRINGER 25R SPLICE, AT STATION 440. 2 L 7 3 4F A3WE 2002061400112 20020614 00112 NM 2002 6 14 RYN2002F00021 1 20020525 A 5311 FRAME BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 C-CHECK, FOUND CORROSION AT THE FORWARD ACCESSORY COMPARTMENT, LEFT SIDE DOOR CUTOUT, ON SHEAR TIE AND FRAME, AT STATION 211 TO 219. 2 L 7 3 4F A3WE 2002061400113 20020614 00113 WP 2002 6 14 RYN2002F00022 1 20020522 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 C-CHECK, FOUND CORROSION ON MAIN CABIN FLOOR SUPPORT, AT STATION 824, RBL 63. 2 L 7 3 4F A22WE 2002061400114 20020614 00114 WP 2002 6 14 RYN2002F00023 1 20020517 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 C-CHECK, FOUND CORROSION ON UPPER SURFACE OF MAIN CABIN SEAT TRACK, AT RBL 10. 2 L 7 3 4F A22WE 2002061400115 20020614 00115 NM 2002 6 14 RYN2002F00024 1 20020428 A 5320 FLOOR SUPPORT BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 C-CHECK, FOUND CRACK IN THE NOSE WHEEL WELL OVERHEAD CONTROL CABIN FLOOR PANEL SUPPORT ANGLE, AT STATION 258 LBL4 WL 148 .5. 2 L 7 3 4F A3WE 2002061400116 20020614 00116 NM 2002 6 14 RYN2002F00025 1 20020428 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 C-CHECK, FOUND A ONE INCH CRACK AT STATION 336 BELOW STRINGER 22L. 2 L 7 3 4F A3WE 2002061400117 20020614 00117 NM 2002 6 14 PCAA0206063 1 20020612 A 5315 85310380 FLOORBEAM DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 815EX 321 DURING ROUTINE MAINTENANCE VISIT NOSE GEAR FLOORBEAM AT STATION X97 FOUND CRACKED. CRACK WAS REPAIRED AT FUSELAGE FLOOR BEAM 85310380 AND NESTED DOUBLER IN ACCORDANCE WITH DER CAS AAL76 REVISION A AND DEHAVILLAND REPAIR DRAWING RD8-53-1336 ISSUE 5. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061400118 20020614 00118 NM 2002 6 14 RYN2002F00026 1 20020428 A 5320 CLIP BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 C-CHECK. FOUND SUPPORT CLIPS CRACKED IN LEFT FUSELAGE INTERIOR STATION 460, STRINGER 19, 20 AND 21. 2 L 7 3 4F A3WE 2002061400119 20020614 00119 NM 2002 6 14 RYN2002F00027 1 20020427 A 5320 SUPPORT BRACKET BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 C-CHECK, FOUND FIRE LOOP DETECTION SUPPORT BRACKET CRACKED AT LEFT VENTRAL STAIR WELL STATION 1185. 2 L 7 3 4F A3WE 2002061400120 20020614 00120 2002 6 14 USA2002F00001 4 20020506 A 3425 7725005009 ADI BOEING 737 7373B7 1384580 NM COCKPIT FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 530AU 31920 24412 ON DESCENT, AT APPROXIMATELY 13,000 FEET, THE CAPTAIN SMELLED SMOKE IN THE COCKPIT ON HIS SIDE, WHEREAS HE FOUND HIS ADI HAD FILLED WITH SMOKE. THERE WAS NOT AN IMPEDIMENT OF VISION IN THE COCKPIT, SMOKE WAS CONTAINED TO THE SIDE OF THE AD I GLASS BEHIND THE GAUGE. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND THE CIRCUIT BREAKER POPPED ON ITS OWN. THE SMOKE AND SMELL BEGAN TO DIMINISH. FLIGHT LANDED AND TAXIED TO THE GATE UNDER ITS OWN POWER. AN EMERGENCY WAS DEC LARED BY THE CAPTAIN. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS ADI AND PERFORMED FUNCTIONAL CHECK PER MM. FUNCTIO NAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002061400121 20020614 00121 NM 2002 6 14 USA2002F00017 1 20020522 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 626AU 27303 (BATTERIES) FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1,4,6,9,13,23,26,29 AND 33 INOPERATIVE. MAINTENANCE REPLACED TH E BATTERIES. 2 L 7 2 4F RT A2NM 2002061400122 20020614 00122 NM 2002 6 14 USA2002F00018 1 20020515 A 5753 BACB10ET14 ROLLER BOEING 737 737401 1384701 NM T/E FLAP OUT OF ADJUST A USAA L A ABORTED APPROACH UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 EA 17 424US 23991 ON APPROACH, CREW COULD NOT GET FLAP TO RESPOND WHEN FLAP LEVER WAS MOVED FROM THE UP DETENT. CREW ACCOMPLISHED QRH PRO CEDURES AND USED THE ALTERNATE FLAPS TO EXTEND FLAPS. DUE TO GUSTY WINDS AND THE SHORT RUNWAY LENGTH, CAPTAIN ELECTED T O DIVERT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT OUTBOARD TRA ILING EDGE AFT FLAP ROLLERS BINDING AND RUBBING HARD INTO THE MID FLAP. ADJUSTED ROLLERS. ALSO REMOVED AND REPLACED FL AP POSITION INDICATOR (PN 2061141) AND RIGHT FLAP TRANSMITTER (PN 1817389) PER MM. RAN FLAPS UP AND DOWN SEVERAL TIMES. OPERATIONAL CHECK OF FLAPS GOOD. 2 L 7 2 4F RT A16WE 2002061400123 20020614 00123 NM 2002 6 14 USA2002F00019 1 20020526 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 17 444US 24862 DURING OPERATION TEST OF EMERGENCY LIGHTS, MAINTENANCE FOUND ONE SECTION OF EMERGENCY LIGHT IN THE FORWARD CABIN FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002061400124 20020614 00124 NM 2002 6 14 USA2002F00020 1 20020524 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 17 517AU 23703 MAINTENANCE FOUND THE LAST SIX ROWS OF SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002061400125 20020614 00125 NM 2002 6 14 USA2002F00021 1 20020528 A 3350 CONNECTOR BOEING 737 7374B7 1384702 NM CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 17 433US 24555 MAINTENANCE FOUND THE FLOOR LEVEL EMERGENCY LIGHTS FROM SEAT ROWS 6 THROUGH 9, INOPERATIVE. MAINTENANCE REPAIRED A BAD CONNECTOR ON SEAT ROW 6 ABC. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002061400126 20020614 00126 NM 2002 6 14 USA2002F00022 1 20020527 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 17 443US 24842 MAINTENANCE FOUND THE EMERGENCY LIGHTS ABOVE THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT BATTERY CHARGER ASSEMBLY. 2 L 7 2 4F RT A16WE 2002061400127 20020614 00127 NM 2002 6 14 USA2002F00023 1 20020527 A 3397 WIRE BOEING 737 737301 1384611 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 17 334US 23231 MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ON SEAT ROW 6, LEFT SIDE, INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002061400128 20020614 00128 NM 2002 6 14 USA2002F00024 1 20020526 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 17 602AU 22196 FOUND LOW LEVEL EMERGENCY LIGHTS AT ROWS 6 AND 26, INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. 2 L 7 2 4F RT A2NM 2002061400129 20020614 00129 NM 2002 6 14 USA2002F00025 1 20020529 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 17 630AU 27808 FOUND LOW LEVEL EMERGENCY LIGHT ARE ROWS 23 AND 29, INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. 2 L 7 2 4F RT A2NM 2002061400130 20020614 00130 NM 2002 6 14 USA2002F00026 1 20020529 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 17 630AU 27808 FOUND L1 DOOR EXIT IDENTIFIER, INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. 2 L 7 2 4F RT A2NM 2002061400131 20020614 00131 NM 2002 6 14 USA2002F00028 1 20020526 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 17 615AU 27146 FOUND EXIT IDENTIFIER AT DOOR R3, INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. 2 L 7 2 4F RT A2NM 2002061400132 20020614 00132 EA 2002 6 14 COMA0260368 1 20020612 A 2710 AILERON CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 713CA 7245 FLIGHT 5759 HEAVIER THAN NORMAL CONTROL FORCE REQUIRED FOR ROLL AND PITCH.INSPECTED FLIGHT CONTROLS AND CABLE TENSIONS. NO DEFECTS FOUND. FORCE CHECKS WITHIN LIMITS. 2 L 7 2 4F RT A21EA 2002061400133 20020614 00133 EA 2002 6 14 COMA0260369 1 20020611 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 713CA 7245 FLIGHT 5285 FLAPS FAILED MESSAGE DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01 2 L 7 2 4F RT A21EA 2002061400134 20020614 00134 NM 2002 6 14 USA2002F00029 1 20020526 A 3350 8731002511REV15 SIGN BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 17 615AU 27146 FOUND EXIT IDENTIFIER AT R4 DOOR INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER ASSEMBLY. 2 L 7 2 4F RT A2NM 2002061400135 20020614 00135 EU 2002 6 14 USA2002F00035 1 20020524 A 3260 848401 SENSOR AIRBUS 320 A320214 3930316 EU RT MLG FAULTY A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 17 101UW 0936 EN ROUTE, AFTER DEPARTING, RECEIVED BOTH RED AND GREEN LANDING GEAR INDICATIONS. THE CREW RECYCLED THE GEAR AND CONTINU ED, WHERE THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED SENSOR 34GA. OPERATIONALLY CHECKED OK. 2 L 7 2 4F RT A28NM 2002061400136 20020614 00136 NM 2002 6 14 USA2002F00036 1 20020601 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 17 632AU 27810 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 29, INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. 2 L 7 2 4F RT A2NM 2002061400137 20020614 00137 NM 2002 6 14 USA2002F00038 1 20020531 A 3350 871002511REV15 SIGN BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 17 622AU 27201 FOUND THE L4 DOOR EXIT IDENTIFIER, INOPERATIVE. MAINTENANCE REPLACED THE ASSEMBLY. 2 L 7 2 4F RT A2NM 2002061400138 20020614 00138 EU 2002 6 14 USA2002F00039 1 20020527 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 17 671UW 0323 FOUND EPSU FAULTS FOR DOORS R1 AND R4. MAINTENANCE REPLACED THE ASSOCIATED BATTERIES. 2 L 7 2 4F RT A46NM 2002061400139 20020614 00139 EU 2002 6 14 USA2002F00040 1 20020524 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 17 670UW 0315 FAULT MESSAGES DISPLAYED FOR EPSU 11WL, 12 WL, 14WL, 17WL AND 18WL BATTERIES. MAINTENANCE REPLACED THE APPLICABLE BATTE RIES. 2 L 7 2 4F RT A46NM 2002061400140 20020614 00140 EU 2002 6 14 MALA020341 1 20020610 A 5320 7253721459 SEAT TRACK SAAB SF340 SF340A 7850100 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING 4Y/2Y-CHECK IN CWA, RH GALLEY SEAT TRACK HAS CORROSION. MAINTENANCE INSTALLED A NEW RH GALLEY SEAT TRACK PN 7253 721-459. REF: 409 #140299 FOR DETAILS. 2 L 7 2 4T RT A52EU 2002061400141 20020614 00141 WP 2002 6 14 P2EA2002M031 1 20020503 A 8000 103538754 IGNITER BOX DOUG DC9 DC982 3022082 WP A P2EA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 05 141NJ 49932 #1 Engine would not start, returned to blocks with no incedent. Removed and replaced #1 engine exciter box IAW MM 74-10- 01. Operational check normal. This is closing action for SDR P2EA2002M031. Reference log page 122455. 2 L 7 2 4F A6WE 2002061400142 20020614 00142 WP 2002 6 14 AALA20020671 1 20020424 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND NR 3 SEAT TRACK INBOARD FLANGE HAS ELONGATED HOLES AT STATION 833 AND 828. NR 3 SEAT TRACK INBOARD FLANGE H AS ELONGATED HOLES AT 846, 851, 856, AND 860. REPAIRED PER AARD 53-20-00-13. (M) 2 L 7 2 4F A6WE 2002061400143 20020614 00143 WP 2002 6 14 AALA20020672 1 20020509 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 TUL - FOUND SHEAR TIE GOUGED STATION 579 BETWEEN LONGERON 25L AND 26L. INSTALLED NEW SHEAR TIE SRM 51-01. (M) 2 L 7 2 4F A6WE 2002061400144 20020614 00144 WP 2002 6 14 AALA20020699 1 20020501 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 TUL - FOUND STATION 1276-1280 NR 3 SEAT TRACK CORRODED. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 1258-1309 PER SRM 51-01 AND AARD 51-60-00-08. (M) 2 L 7 2 4F A6WE 2002061400145 20020614 00145 WP 2002 6 14 AALA20020700 1 20020501 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 TUL - FOUND STATION 1300-1302 NR 3 SEAT TRACK CORRODED. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 1258-1309 PER SRM 51-01 AND AARD 51-60-00-08. (M) 2 L 7 2 4F A6WE 2002061400146 20020614 00146 WP 2002 6 14 AALA20020701 1 20020501 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 TUL - FOUND CORROSION ON LOWER SIDE OF NR 3 SEAT TRACK AROUND CLIPNUT HOLES BETWEEN STATION 1271-1309. INSTALLED NEW SE CTION OF SEAT TRACK FROM STATION 1258-1309 PER SRM 51-01 AND AARD 51-60-00-08. (M) 2 L 7 2 4F A6WE 2002061400147 20020614 00147 WP 2002 6 14 AALA20020702 1 20020501 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 TUL - FOUND G-2 GALLEY TIE DOWN PITTING CORRODED AT STATION 218 APPROX RBL 11. REMOVED AND REPLACED GALLEY MOUNT PER SR M 51-01-00. (M) 2 L 7 2 4F A6WE 2002061400148 20020614 00148 WP 2002 6 14 AALA20020703 1 20020514 A 5230 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7536A 49990 TUL - FOUND DOOR BEAM HAS CORROSION STATION 1160-1207. REPLACED DOOR BEAM PER SRM 51-01-00. (M) 2 L 7 2 4F A6WE 2002061400149 20020614 00149 WP 2002 6 14 AALA20020724 1 20020520 A 3230 LANDING GEAR DOUG DC9 DC982 3022082 WP NLG MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 70401 49312 LAX - FLT 808 - ON TAKEOFF, NOSE GEAR WOULD NOT RETRACT. LOWERED GEAR, GOT NORMAL GEAR DOWN INDICATION. RETURNED LAX A ND LANDED WITHOUT INCIDENT. JACKED AND CONFIGURED AIRCRAFT FOR TAKEOFF. ACCOMPLISHED GEAR SWING NUMEROUS TIMES WITH NO FAULTS NOTED. ACCOMPLISHED NOSE STRUT SERVICING. PRECAUTIONARY REPLACED GROUND PROXIMITY CONTROLLER. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002061400150 20020614 00150 WP 2002 6 14 AALA20020732 1 20020506 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7534A 49988 TUL - FOUND CORROSION FS 1200-1271. REPLACED NR 3 SEAT TRACK FROM STATION 1200-1271. (M) 2 L 7 2 4F A6WE 2002061400151 20020614 00151 WP 2002 6 14 AALA20020733 1 20020506 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7534A 49988 TUL - FOUND CORROSION FS 1200-1271. REPLACED NR 3 SEAT TRACK FROM STATION 1200-1271. (M) 2 L 7 2 4F A6WE 2002061400152 20020614 00152 WP 2002 6 14 AALA20020734 1 20020506 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7534A 49988 TUL - FOUND FASTENER HOLE DAMAGED DURING REMOVAL OF RIVET STATION 1098 4 INCHES AT LONGERON 15 RIGHT. OVERSIZED FASTENE R HOLE TO MAKE SIZE OF .260 INCH DIAMETER. INSTALLED HI-LOCK WET WITH SEALANT. ALL WORK ACCOMPLISHED PER ESO 80559 DAT ED 5/6/02. (M) 2 L 7 2 4F A6WE 2002061400153 20020614 00153 WP 2002 6 14 AALA20020735 1 20020506 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7534A 49988 TUL - FOUND DOOR PAN HAS CORROSION IN SEVERAL AREAS BETWEEN STATION 370-427. SPLICED IN NEW LOWER DOOR JAMB PAN PER SRM 53-05 FIG 44. (M) 2 L 7 2 4F A6WE 2002061400154 20020614 00154 WP 2002 6 14 AALA20020736 1 20020506 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7534A 49988 TUL - NR 5 SEAT TRACK HAS CORROSION AT FLOORBOARD ATTACH HOLE, AT STATION 200, RIGHT FLANGE. REMOVED CORROSION PER SRM 51-10-03. INSTALLED DOUBLER PER AARD 53-20-00-13. (M) 2 L 7 2 4F A6WE 2002061400155 20020614 00155 WP 2002 6 14 AALA20020737 1 20020501 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7534A 49988 TUL - FOUND CORROSION ON BRACKET. REMOVED AND REPLACED BRACKET PER MM 53-01. (M) 2 L 7 2 4F A6WE 2002061400156 20020614 00156 NM 2002 6 14 GAIA02051ST 1 20020517 A 5313 STRINGER BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STRINGER 15 LEFT IS CRACKED AT BS 720B PLUS 5. ACCOMPLISHED STRINGE R REPAIR AT BS 720B PLUS 5 STRINGER 15 LEFT IAW B727 SRM 53-10-3 FIG 5. (M) 2 L 7 3 4F RT A3WE 2002061400157 20020614 00157 NM 2002 6 14 GAIA02052ST 1 20020517 A 5313 STRINGER BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STRINGER 15 LEFT IS CRACKED AT BS 720B PLUS 15. ACCOMPLISHED STRING ER REPAIR AT BS 720B PLUS 15 STRINGER 15 LEFT IAW B727 SRM 53-10-3 FIG 5. (M) 2 L 7 3 4F RT A3WE 2002061400158 20020614 00158 NM 2002 6 14 GAIA02053ST 1 20020517 A 5347 SEAT TRACK BOEING 727 7272J0 138407E NM FUSELAGE DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE MAIN CABIN SEAT TRACK RBL 24.75 IS DAMAGED SEVERAL DIFFERENT PLA CES FROM BS 480-530. ACCOMPLISHED SEAT TRACK REPAIR AT BS 480-530 RBL 24.75 IAW B727 SRM 53-10-5 FIG 1. (M) 2 L 7 3 4F RT A3WE 2002061400159 20020614 00159 NM 2002 6 14 GAIA02054ST 1 20020517 A 5320 STIFFENER BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE PRESSURE BULKHEAD BS 1183 VERTICAL BEAM LBL 36.9 CRACKED AT WL 2 45. ACCOMPLISHED BS 1183 VERTICAL BEAM REPAIR AT LBL 36.9 IAW S/B 727-53-0192. (M) 2 L 7 3 4F RT A3WE 2002061400160 20020614 00160 NM 2002 6 14 GAIA02055ST 1 20020517 A 5330 SKIN BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE SKIN IS CRACKED AT THE FORWARD ENTRY DOOR LOWER HINGE C UT OUT. ACCOMPLISHED FUSELAGE SKIN REPAIR AT THE FORWARD ENTRY DOOR LOWER HINGE CUT OUT IAW S/B 727-53-0198. (M) 2 L 7 3 4F RT A3WE 2002061400161 20020614 00161 NM 2002 6 14 GAIA02056ST 1 20020517 A 5320 WEB BOEING 727 7272J0 138407E NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STATION 1230 AFT FACE OF THE TAIL SKIN CAVITY BULKHEAD, CORROSION ON SUPPORT ANGLE AND WEB VISIBLE THROUGH AIRSTAIR CUT-OUT, AFT OF THE TAIL SKID. ACCOMPLISHED BS 1230 WEB AND T-ANGLE REP AIR IAW B727 SRM 51-40-2 AND SRM 51-40-4. (M) 2 L 7 3 4F RT A3WE 2002061400162 20020614 00162 NM 2002 6 14 GAIA02057ST 1 20020517 A 5320 WEB BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A CHECK INSPECTION, IT WAS DISCOVERED THAT VENTRAL STAIR AREA STATION 1225 LBL 12, VERTICAL WEB HAS A CRACK AT TH E LIGHTENING HOLE. ACCOMPLISHED BS 1225, LBL 12 WEB REPAIR IAW B727 SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F RT A3WE 2002061400163 20020614 00163 NM 2002 6 14 GAIA02058ST 1 20020517 A 5320 WEB BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 01 284KH 21108 DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT VENTRAL STAIR AREA STATION 1232 LBL 14, VERTICAL WEB IS BUCKLED WITH A 3 INCH CRACK OUTBOARD OF 5TH STEP FROM TOP. ACCOMPLISHED BS 1232, LBL 14 CRACKED WEB ANGLE REPLACEMENT IAW B727 SRM 53-10-2 FIG 6. (M) 2 L 7 3 4F RT A3WE 2002061400164 20020614 00164 NM 2002 6 14 GAIA02059ST 1 20020517 A 5320 WEB BOEING 727 7272J0 138407E NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE VENTRAL STAIR AREA STATION 1244 RBL 12 VERTICAL WEB HAS 1 CRACK AT THE LIGHTENING HOLE. ACCOMPLISHED TORQUE BOX WEB REPAIR IAW B727 SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F RT A3WE 2002061400165 20020614 00165 NM 2002 6 14 GAIA02060ST 1 20020517 A 5711 SPAR BOEING 727 7272J0 138407E NM LT WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED LEFT WING FRONT SPAR LOWER CHORD IS CORRODED UNDER AND INBO ARD OF EXISTING REPAIR INSIDE L/E COVE AREA AT LES 200-240. ACCOMPLISHED LEFT WING LEADING EDGE LOWER SKIN AND SPAR CHO RD REPAIR IAW AVITAS ENGINEERING DRAWING FASI-022D-1. (M) 2 L 7 3 4F RT A3WE 2002061400166 20020614 00166 NM 2002 6 14 GAIA02061ST 1 20020517 A 5711 SPAR BOEING 727 7272J0 138407E NM LT WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 284KH 21108 DURING A C-CHECK INSPECTION AT FLIGHT STAR, IT WAS DISCOVERED LEFT WING FRONT SPAR UPPER SURFACE AT WS 410 IS CORRODED. ACCOMPLISHED LEFT WING FRONT SPAR LOWER CHORD UPPER SURFACE REPAIR IAW B727 SRM 57-30-4 FIG 6. (M) 2 L 7 3 4F RT A3WE 2002061400167 20020614 00167 WP 2002 6 14 GTIA020512 1 20020519 A 3246 WHEEL DOUG DC9 DC982 3022082 WP NLG LACK OF LUBE A GTIA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 23 820NK 49126 FLT 604 - FLL - ON TAKEOFF ROLL AT 60 IAS NOSE WHEEL DEVELOPED SEVERE VIBRATION, REJECTED TAKEOFF AT 70 KIAS RETURNED TO GATE. LUBRICATED NOSE GEAR ASSEMBLY. (M) 2 L 7 2 4F A6WE 2002061400168 20020614 00168 2002 6 14 GTIA020513 4 20020516 A 3460 4034241971 COMPUTER DOUG DC9 DC983 3022083 WP COCKPIT FAILED A GTIA O OTHER J WARNING INDICATION DE DESCENT 1 GL 23 826NK 49391 FLT 709 - LAX - AUTO THROTTLES AND AUTO PILOT CAME OFF ON DESCENT THROUGH 21,000 MASTER CAUTION. FOUND NR 1 DFGC BAD. REMOVED AND REPLACED NR 1 DFGC, RTS CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 2002061400169 20020614 00169 2002 6 14 GTIA020514 4 20020516 A 3460 4034241971 COMPUTER DOUG DC9 DC983 3022083 WP COCKPIT FAILED A GTIA O OTHER O OTHER DE DESCENT 1 GL 23 826NK 49391 LGA - FLT 1381 - NR 1 AUTO PILOT CLICK OFF ON THE DESCENT, AT THE SAME TIME AUTO THROTTLES CLICK OFF. BOTH FMAS AND DFG PANELS WENT BLANK FOLLOWED QRH PROCEDURES SWITCH TO AUTO PILOT NR 2 AND SYSTEM WORKED FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED NR 1 DFGC. PERFORMED RTS REF. (M) 2 L 7 2 4F RT A6WE 2002061400170 20020614 00170 2002 6 14 372PA0010 4 20020613 A 2230 AUTOTHRUST SYS BOEING 737 737306 NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 372PA 23546 Autothrottles Inop. Reset C/B's op's ck's OK. 2 L 7 2 4F RT A16NE 2002061400171 20020614 00171 2002 6 14 GTIA020517 4 20020518 A 2350 64300100 HEADSET DOUG MD80 MD83 3023681 NM COCKPIT OVERHEATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 822NK 49392 DEN - FLT 970 - MIC ON CAPTAIN HEADSET OVERHEATED AND IS INOPERATIVE. SMELLS BURNED AT SWIVEL ATTACHMENT. REMOVED AND REPLACED MIC-HEAD SET. OPS CHECKS NORMAL. (M) 2 L 7 2 4F RT 2002061400172 20020614 00172 NE 2002 6 14 GTIA020518 2 20020506 A 7261 OIL SYSTEM DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ENGINE LEAKING A GTIA O OTHER K FLUID LOSS IN INSP/MAINT 1 GL 23 602CA 49415 P696385 SJU - LOSS OF 4 QUARTS OF OIL DURING PUSH BACK ON RIGHT ENGINE. REMOVED AND REPLACED NR 2 ENGINE AS PER SPIRIT AIRLINES W/C 00191. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002061400173 20020614 00173 WP 2002 6 14 GTIA020520 1 20020520 A 2797 WIRE DOUG DC9 DC983 3022083 WP TRIM SWITCH BROKEN A GTIA O OTHER O OTHER DE DESCENT 1 GL 23 802NK 53168 RSW - FLT 926 - CAPTAINS LONGITUDINAL TRIM SWITCH WILL NOT WORK IN THE NOSE DOWN POSITION. REPAIRED BROKEN WIRE C1209A2 0 IN FORWARD CARGO PIT RIGHT TUNNEL FOR CAPTAINS PRIMARY TRIM, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2002061400174 20020614 00174 WP 2002 6 14 MEX2002045 1 20020220 A 2437 WARNING SYSTEM DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A ASMF D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 23 491SH 49150 FLT 180 - MLM-HMO - DURING TAXI, CAPTAIN INFORMED THAT DC BUS OFF LIGHT IS ON. RESET THE CIRCUIT BREAKER, LIGHT WAS NOT OFF. AIRCRAFT RETURNED TO PLATFORM. BOTH BATTERIES WERE DISCONNECTED AND CONNECTED, RESET THE RELAYS R2-21 AND R2-326 , TEST OK, IAW MM 24-30-03. (M) 2 L 7 2 4F A6WE 2002061400175 20020614 00175 EU 2002 6 14 MALA020345 1 20020612 A 5320 SEAT TRACK SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 DURING 4Y/2Y-CHECK IN CWA, RHIB GALLEY SEAT TRACK TOP HAS CORROSION. MAINTENANCE BLENDED OUT SURFACE CORROSION IAW SRM 51-70-40. REF; 409 # 140141 FOR DETAILS. A/C RELEASE DATE 6/12/02 2 L 7 2 4T RT A52EU 2002061400176 20020614 00176 EU 2002 6 14 MALA020346 1 20020612 A 5320 FRAME SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 DURING 4Y/2Y-CHECK IN CWA, FRAME TOP STA 272 AT APPROXIMATELY RBL 22 HAS CORROSION. MAINTENANCE BLENDED OUT CORROSION A T SA 272 APPROX RBL 22 IAW SRM 51-70-40. REF: 409 # 140140. A/C RELEASE DATE 6/13/2002. 2 L 7 2 4T RT A52EU 2002061400177 20020614 00177 EU 2002 6 14 MALA020347 1 20020612 A 5320 FRAME SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 DURING 4Y/2Y-CHECK IN CWA, WEB ON TOP OF FRAMES 288 & 294 HAVE CORROSION. MAINTENANCE BLENDED OUT CORROSION IAW SRM 51- 70-40. REF: 409 # 140139 FOR DETAILS. A/C RELEASED DATE 6/13/02. 2 L 7 2 4T RT A52EU 2002061400178 20020614 00178 EU 2002 6 14 MALA020348 1 20020612 A 5320 SEAT TRACK SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 DURING 4Y/2Y-CHECK IN CWA, CARGO CENTER AISLE SEAT TRACK BLO HAS CORROSION ON SIDE AT APPROXIMATELY STA 637. MAINTENAN CE BLENDED OUT CORROSION IAW 51-70-40. REF: 409 #140132 FOR DETAILS. A/C RELEASE DATE IS 06/13/2002. 2 L 7 2 4T RT A52EU 2002061400179 20020614 00179 EU 2002 6 14 MALA020349 1 20020613 A 2460 POWER SUPPLY SAAB SF340 340B 7860101 EU A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 368XJ DURING LC1 FOUND MANY CABIN EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED POWER SUPPLY AND BATTER SUPPLY (22LN) OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002062100041 20020621 00041 NM 2002 6 21 UPS02238614 1 20020612 A 5754 65162212 SLAT BOEING 727 72727C 138400J NM WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:AS NR 5 SLAT CRACKED OUTBOARD OF FENCE JUST OUTBOARD OF UPSTOP. REMOVED AND REPLACED NR 5 SLAT PER MM 2 7-81-11, RIG AND OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002061400180 20020614 00180 NM 2002 6 14 UPS02438607 1 20020529 A 5310 141U11072 WEB BOEING 747 747200 1384847 NM RH NOSE W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C CRACK FOUND AT RH NOSE W/W VERT BEAM WEB AT BS 280 LWR STANDOFF HOLE BETWEEN FIRST AND SECOND STIFFENE RS APPROX 1/4 INCH LONG AS MARKED. NOSE W/W BS 280 R/H VERT BEAM WEB WAS REPLACED AS PER SRM 51-10-01 PG. 8 2 L 7 4 4F RT A20WE 2002061400181 20020614 00181 NM 2002 6 14 UPS02438608 1 20020529 A 5310 141U11076 WEB BOEING 747 747200 1384847 NM NOSE W/W BS300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C CRACK FOUND AT RH NOSE W/W VERT BEAM WEB AT BS 300 I/B CHORD ATTACHED AREA BETWEEN 1ST AND 2ND STIFFEN ERS APPROX 1/2 INCH LONG AS MARKED. NOSE W/W R/H BS 300 VERT WEB REPLACED AS PER SRM 51-10-01 P.8 2 L 7 4 4F RT A20WE 2002061400182 20020614 00182 NM 2002 6 14 UPS02438610 1 20020529 A 5310 141U11074 WEB BOEING 747 747200 1384847 NM RH NOSE WW BS320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C CRACK FOUND AT RH NOSE W/W VERT BEAM WEB AT BS 320 BETWEEN FIRST AND SECOND STIFFENERS AT LWR STANDOFF HOLE APPROX 1 INCH LONG AS MARKED. BEAM WEB REPLACED AT BS 320 RH AS PER SRM 51-10-01 PG.8 2 L 7 4 4F RT A20WE 2002061400183 20020614 00183 NM 2002 6 14 UPS02438611 1 20020529 A 5310 141U11073 WEB BOEING 747 747200 1384847 NM LH NOSE WW BS320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C LH BS 320 NOSE W/W VERT BEAM WEB CRACK FOUND AT #2 AND 3 STANDOFF HOLES, COUNT FROM THE TOP, AS MARKED . NOSE W/W LH BS 320 VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 PG.8 2 L 7 4 4F RT A20WE 2002061400184 20020614 00184 NM 2002 6 14 UPS02438612 1 20020530 A 5310 FRAME BOEING 747 747200 1384847 NM M/D S/W BS440 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C M/D SIDEWALL FRAME O/B FLANGE CRACKED AT BS 440 S16R. BS 440 FRAME AT S16R REPAIRED AS PER SRM 51- 40-03 FIG.1 2 L 7 4 4F RT A20WE 2002061400185 20020614 00185 NM 2002 6 14 UPS02438613 1 20020602 A 5310 SEAT TRACK BOEING 747 747200 1384847 NM U/D CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C U/D - SEAT TRACK FOUND CORRODED AT STA 530-540 RBL 46". SEAT TRACK REPLACED AT U/D BS 480-530 RBL 46" AS PER SRM 51-10-01 PG. 8 AND SEAT TRACK REPAIR AT U/D STA 530-550 RBL 46" AS PER SRM 53-10-05 FIG.1A. CORROSION BLE ND OUT SIZE 0.035" X 1/2" X 1". 2 L 7 4 4F RT A20WE 2002073000021 20020730 00021 NM 2002 7 30 AWXA200200520 1 20020612 A 2780 65446519 ACTUATOR BOEING 737 737277 1384570 NM WING BINDING A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 182AW 35710 13974 22649 BOI - AIR TURN BACK - FLT 0166 - ON DEPARTURE OUT OF BOI EN ROUTE TO PHX THE NR 4 SLAT REMAINED IN EXTENDED POSITION; F LAPS WERE CYCLED AND NR 4 SLAT STILL REMAINED EXTENDED; TURNED BACK TO BOI AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE INSPECTED THE NR 4 SLAT AND FOUND SEVERAL ROLLERS STICKING DUE TO LACK OF LUBRICATION. ROLLERS AND TRACK WERE LUBRICATE D, AND FLAP SYSTEM WAS CYCLED SEVERAL TIMES WITH NO DEFECTS NOTED. A FOLLOW-UP (FUP) WAS WRITTEN TO REPLACE THE NR 4 SLA T ACTUATOR AND LUBRICATE SLATS/FLAPS PER BMM 12-22. TEARDOWN OF NR 4 SLAT ACTUATOR S/N 1660T CONFIRMED FAILURE FINDIN G THE BEARING, SEALS, RINGS, O-RINGS, RETAINERS, AND SCRAPERS WERE WORN. UNIT WAS OVERHAULED. 2 L 7 2 4F RT A16WE 2002061400186 20020614 00186 EU 2002 6 14 C2XA02IA126 1 20020611 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU PASSENGER DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14822 163 During scheduled maintenance the passenger door emergency light was found to be inoperative. Maintenance removed and rep laced the passenger door step emergency light assembly and the system operationally checked good. 2 H 7 2 4T RT A53EU 2002072500004 20020725 00004 NM 2002 7 25 QXEA0200875 1 20020613 A 5270 DOOR BOMBDR DHC8 DHC8401 1390041 NM CARGO BAY OUT OF ADJUST A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 405QX 4047 SEA- AFT CARGO DOOR WARNING LIGHT ILLUMINATED WHILE DECENDING INTO SEA. CREW FOLLOWED CHECKLIST AND BEGAN DEPRESSURIZATI ON OF AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND DOOR STOP PINS OUT OF ADJUSTMENT. ADJU STED, CLEANED, AND LUBED AFT BAGGAGE DOOR. INSPECTED CLOSING OF DOOR. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061400187 20020614 00187 NM 2002 6 14 P5CA0200684 1 20020614 A 2824 MA11A1173 ACTUATOR BOEING 747 747122 1384872 NM #1 XFEED VALVE FAILED A P5CA J A DUMP FUEL UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 WP 23 854FT 19754 #1 CROSSFEED VALVE FAILED CLOSED DURING FLIGHT. RETURNED TO JFK PER MOD LGB. FUEL DUMP ACCOMPLISHED DUE TO AIR TURN-BACK . MX CTL NOTIFIED. REMOVED & REPLACED #1 CROSSFEED VALVE ACTUATOR IAW MM 28-22-02. OPS CHECKED NORMAL. 2 L 7 4 4F A20WE 2002061400188 20020614 00188 SO 2002 6 14 RAIA00206176 1 20020512 A 5320 14522460015 GUSSET EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 804HK 145082 BLK CK - TASK# 53Z241214001A00 - CORROSION ON FLOORBOARD STRINGER AT BL 18L THRU CBL AT FRAME 18. REMOVED AND REPLACED G USSET IAW SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002061400189 20020614 00189 SO 2002 6 14 RAIA00206177 1 20020512 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 804HK 145082 CORROSION ON FLOORBOARD GUSSET AT CBL AT FRAME 18 AT FLOORBOARD HOLE. REMOVED AND REPLACED GUSSET IAW SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002061400190 20020614 00190 SO 2002 6 14 RAIA00206179 1 20020512 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 804HK 145082 BLK CK - TASK# 53Z241214001A00 - SURFACE CORROSION ON WEB SILL PLATE AT BL 18R AT FRAME 19. REMOVED AND REPLACED SILL PL ATE IAW SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002061400191 20020614 00191 SO 2002 6 14 RAIA00206180 1 20020512 A 5320 14522461011 DOUBLER EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 804HK 145082 BLK CK - TASK# 53Z241214001A00 - CORROSION ON DOUBLER AT CBL FRAME 19. REMOVED AND REPLACED DOUBLER IAW SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002061400192 20020614 00192 SO 2002 6 14 RAIA00206181 1 20020512 A 5320 14522459003 SUPPORT EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 804HK 145082 BLK CK - TASK# 53Z241214001A00 - CORROSION ON FLOOR SUPPORT AT CBL AND JUST AFT OF FRAME 19. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002061500001 20020615 00001 SO 2002 6 15 C2XA02TY102 1 20020615 A 5313 14533823009 STRINGER EMB 145 EMB145 3260210 SO STA.17727.0 CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 TYS DURING A 1C/2C INSPECTION,STRINGER 19R AT STA.17727.0 WAS FOUND CHAFED. MAINTENANCE MEASURED AREA(L=.4670" XW=.1495 " X D=.016") FOUND TO BE WITHIN LIMITS,BLENDED DYE PENTRANT INSPECTION,ALODINE,PRIMED AND RESORED TOPCOAT IAW EMB.135/14 5 SRM 53-24-02 AND CPM 51-21-04-05-06.ALL WORK WAS ACCOMPLISH AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002061700001 20020617 00001 NM 2002 6 17 AUS20020472 1 20020522 A 7170 UL37981 DRAIN LINE BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE ENGINE DRAINS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) NR 3 ENGINE MAINIFOLD DRAIN LINE LEAKING. 2 L 7 4 4F 4 F RT A20WE E30NE 2002061700002 20020617 00002 NE 2002 6 17 AUS20020484 2 20020524 A 7200 ENGINE BAC 146 AVRO146RJ70A 1500095 EU LYC ALF502 ALF502R4 41580 NE NR 2 VIBRATES W C ABORTED TAKEOFF E F VIBRATION/BUFFET FLT CONT AFFECTED TO TAKEOFF 1 AU S (AUS) NR 2 ENGINE FAILED. SEVERE VIBRATION AND FLAMES FROM EXHAUST AREA. ONE FIRE BOTTLE DISCHARGED. INVESTIGATION FOUND THE OIL TANK WAS FULL WITH NO SIGNS OF LEAKES. THE NR 2 BEARING SCAVENGE DRAIN WAS FOUND BROKEN OFF WHERE THE FITTING I S SOLDERED TO THE MAIN PIPE ADJACENT TO THE DIFFUSER CASE. 2 H 7 4 4F 4 F RT A49EU E6NE 2002061700003 20020617 00003 NM 2002 6 17 AUS20020485 1 20020514 A 3520 OXYGEN MASK BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE PASSENGER OXYGEN MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) OXYGEN MASKS INCORRECTLY PACKED. 2 L 7 4 4F 4 F RT A20WE E30NE 2002061700004 20020617 00004 NM 2002 6 17 AUS20020489 1 20020524 A 3230 V2436002 FUSE BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL MLG HYD SYS FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT MAIN LANDING GEAR RETRACTION SYSTEM HYDRAULIC FUSE FAULTY. 2 L 7 2 4F 4 F RT A1NM E23EA 2002061700005 20020617 00005 NM 2002 6 17 AUS20020490 1 20020527 A 4990 380029816 OIL TANK BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL APU LOW W K NONE E K VIBRATION/BUFFET FLUID LOSS IN INSP/MAINT 1 AU S 3803 P2416 (AUS) APU OIL QUANTITY LOW. APU SHUTDOWN. 2 L 7 2 4F 4 F RT A1NM E23EA 2002061700006 20020617 00006 EU 2002 6 17 AUS20020491 1 20020207 A 2913 42011 PUMP FOKKER F27 F27MK50 EU PWA PWA120 PW125B NE HYDRAULIC FAILED W O OTHER O OTHER NR NOT REPORTED 1 AU S 3306 (AUS) HYDRAULIC PUMP FAILED. 2 H 7 2 4T 4 T RT A817 E20NE 2002061700007 20020617 00007 EU 2002 6 17 AUS20020492 1 20020527 A 2697 WIRE BAC 146 146100A 1500260 EU LYC ALF502 ALF502R3A 41580 NE FIRE BTL SQUIB UNAPPROVED PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) APU FIRE BOTTLE SQUIB WIRE BETWEEN PIN 2 AND EARTH POINT WIRE WAS THE INCORRECT TYPE FOR THE APPLICATION. THE WIRE FITTED WAS A SINGLE CORE SHIELDED WIRE WITH 150 DEGREE BLUE AMP TERMINALS. THE CORRECT WIRE IS 16 GAUGE SINGLE CORE 260 DEGREE WIRE. A SIMILAR LENGTH OF WIRE WAS FOUND INSTALLED IN THE EXTINGUISHER USED CIRCUIT FROM EARTH POINT L1 TO TERMI NAL STRIP 311-03-00 B1. THIS WIRE SHOULD HAVE BEEN A 22 GAUGE 260 DEGREE SINGLE CORE WIRE. UNAPPROVED PART. PERSONNEL/MA INTENANCE ERROR. 2 H 7 4 4F 4 F RT A49EU E6NE 2002061700008 20020617 00008 NM 2002 6 17 AUS20020493 1 20020527 A 4990 P1034 OIL TANK BOEING 767 767* NM RROYCE RB211 RB211524* NE APU LOW W O OTHER E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION DE DESCENT 1 AU S (AUS) APU OIL QUANTITY LOW. NO EVIDENCE OF ANY LEAKS. TWO LITRES ADDED TO TOP UP THE OIL. 2 L 7 2 4F 4 F RT A1NM E12EU 2002061700009 20020617 00009 NE 2002 6 17 AUS20020494 2 20020528 A 7200 ENGINE BAC 146 146200A 1500266 EU LYC ALF502 ALF502R3A 41580 NE NR 1 FAILED W A UNSCHED LANDING E Y J VIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 AU S (AUS) NR 1 ENGINE FAILED. 2 H 7 4 4F 4 F A49EU E6NE 2002061700010 20020617 00010 NM 2002 6 17 AUS20020496 1 20020528 A 3610 79275515 CONTROLLER BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL PNEUMATIC SYS FAULTY W O OTHER J WARNING INDICATION NR NOT REPORTED 1 AU S 200203158 (AUS) BLEED AIR PRV CONTROLLER SUSPECT FAULTY. 2 L 7 2 4F 4 F RT A1NM E23EA 2002061700011 20020617 00011 EU 2002 6 17 AUS20020497 1 20020529 A 5270 TB2273A SWITCH FOKKER F27 F27MK50 EU PWA PWA120 PW125B NE DOOR WARNING SYS OUT OF ADJUST W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 AU S 27871 (AUS) AFT GALLEY DOOR WARNING SYSTEM SWITCH OUT OF ADJUSTMENT. 2 H 7 2 4T 4 T RT A817 E20NE 2002061700012 20020617 00012 NM 2002 6 17 AUS20020499 1 20020529 A 3320 LIGHT BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE CABIN ARCED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 AU S (AUS) FLUORESCENT LIGHT HOLDER LOCATED ABOVE SEAT 12AB ARCING. 2 L 7 4 4F 4 F RT A20WE E30NE 2002061700013 20020617 00013 CE 2002 6 17 AUS20020500 1 20020524 A 7500 1989001 VALVE CESSNA 525 525 2076601 CE WILINT FJ44 FJ441A GL ENGINE BLEED AIR BROKEN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT ENGINE BLEED AIR SYSTEM CHECK VALVE BROKEN. INVESTIGATION FOUND CENTRE SUPPORT WELDS FAILED CAUSING AIRFLOW BLO CKAGE. 1 L 7 2 4F 4 F RT A1WI E3GL 2002061700014 20020617 00014 NM 2002 6 17 AUS20020501 1 20020529 A 3233 273T62013 ACTUATOR BOEING 767 767* NM RROYCE RB211 RB211524* NE MLG FAULTY W O OTHER J WARNING INDICATION CL CLIMB 1 AU S 00738 (AUS) LT MAIN LANDING GEAR SIDE BRACE ACTUATOR FAULTY. 2 L 7 2 4F 4 F RT A1NM E12EU 2002061700015 20020617 00015 GL 2002 6 17 CA020501012 2 20020410 A 7323 252466715H GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED W C ABORTED TAKEOFF R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET TO TAKEOFF 1 CA (CAN) ASSEMBLY PURCHASED ON EXCHANGE OVERHAUL BASE ON OUR PO 2170 FOR REPLACEMENT OF A PREIOUS UNIT S/N 85430071 THAT HA D ALSO FAILED FOR THE SAME REASON WITH 1039.1 HOURS. ASSEMBLY RECEIVED FROM ESSENTIAL TURBINE PS 4806, AND ARC FOM 24-00 78 CERTIFICATE REF L1164/B-3032. GOVERNOR ASSEMBLY TBO ARE SET AT 2000 HOURS. THIS IS THE FOURTH OCCURRENCE OF GOVERNOR FAILURE OF THIS NATURE ON VARIOUS MODEL AIRCRAFT IN OUR FLEET FOR THE SAME REASON UNABLE TO ADJUST FOR MAX TRAVEL. UNIT IS SOONER WITH LESS HOURS USED UP ON THE ASSEMBLY. 1 G 7 1 3U 3 U H2SW E4CE 2002061700016 20020617 00016 NM 2002 6 17 CA020510007 1 20020419 A 3260 401020101 PROXIMITY SENSOR BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA NLG BROKEN W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) DURING TAXI, YAW DAMPER DISENGAGED, IAS FAIL FLAG APPEARED, AD INVALID MSG. CAME ON, STICK PUSHER ACTIVATED, WEIGH T ON WHEEL CAUTION LIGHT ILLUMINATED AND NOSE WHEEL STEERING STOPPED OPERATING. TAXI BACK TO PARKING STAND. CHECK PERFOR MED BY TECHNICAL STAFF. BROKEN NOSE WHEEL SENSOR FOUND AND REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061700017 20020617 00017 NM 2002 6 17 CA020510008 1 20020420 A 2910 82974216001 HYDRAULIC LINE DHAV DHC8 DHC8* NM PWC 150 PW150A EA LT NACELLE LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE THE FLIGHT CREW NOTICED THE NR 1 HYDRAULIC QUANTITY DECREASING. AN UNEENTFUL LANDING WAS COMPLETED. THE MAINTENANCE CREW DISCOVERED THE NR 1 ENGINE DRIVEN PUMP CASE DRAIN LINE HAD CHAFED THROUGH ON A FAIRLEAD CAUSING THE PIPE TO LEAK. THE PIPE WAS REPAIRED AND THE AIRCRAFT RETURNED TO SERVICE.AN INVESTIGATION DETERMINED THE CAUSE OF THE C HAFING WAS DUE TO A SUPPORT CLAMP NOT INSTALLED ON THE PIPE KEEPING IT AWAY FROM THE FAIRLEAD. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061700018 20020617 00018 NM 2002 6 17 CA020510009 1 20020506 A 2530 13B121ORN WIRE DHAV DHC8 DHC8* NM PWC 150 PW150A EA BULKHEAD CHAFED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) FLIGHT ATTENDANT REPORTED BEING SHOCKED BY GALLEY AND SEEING SPARKS. INVESTIGATION FOUND WIRE 13B-12-1/ORN CHAFED ON FORWARD BULKHEAD FOR AFT G3 GALLEY. IT WAS ALSO FOUND THAT THE GALLEY WAS NOT BONDED TO THE FUSELAGE, ZERO RESISTANCE BETWEEN IT AND THE SEAT RAIL. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061700019 20020617 00019 WP 2002 6 17 CA020515002 1 20020503 A 7931 ENGINE GRUMAN TS2 TS2ACALFORST 3951102 WP WRIGHT R1820 982C9HE2 67020 EA HAMSTD 43D 43D51 NE RIGHT MALFUNCTIONED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) AIRCRAFT WAS ENROUTE TO A FIRE FROM KAMLOOPS, DURING CRUISE THE OIL PRESSURE WAS NOTED TO BE LOW ON THE RIGHT HAND ENGINE. THE ENGINE WAS SHUTDOWN AND THE PROPELLER WAS FEATHERED. THE AIRCRAFT RETURNED TO THE KAMLOOPS TANKER BASE. THE ENGINE WAS REPLACED WITH A SERVICEABLE UNIT AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4R 4 R A25WE E259 6 C P8879 2002061700020 20020617 00020 NE 2002 6 17 CA020515005 2 20020506 A 7414 DRIVE GEAR CNDAIR CL215 CL2151A10 1900320 EA PWA R2800 CA3 52026 NE MAGNETO DAMAGED W C ABORTED TAKEOFF R Y J PARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 CA (CAN) ENGINE LOST POWER DURING TAKEOFF AND WAS SHUTDOWN IMMEDIATELY. PRIMARY INVESTIGATION REEALS THAT THE MAGNETO DRIVE IS DAMAGED. OIL CONTAMINATION WAS FOUND. ENGINE WILL BE SENT FOR DETAILED INSPECTION AND INVESTIGATION. 2 H 7 2 4R 4 R RT A14EA E231 2002061700021 20020617 00021 NE 2002 6 17 CA020515006 2 20020510 A 7200 CF343B1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT FAILED W O OTHER Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 CA (CAN) A/C 7325 EXPERIENCED UNCOMMANDED IFSD. A/C DIVERTED & LANDED IN FRESNO, CA. 2ND EENT WITH A/C & ENGINE. REFER TO L INK FOR PREVIOUS SER. AFTER 1ST EVENT FUEL CONTROL & FILTERS WERE REPLACED. FUEL CONTROL WENT TO REPAIR CAME BACK AS NFF . ENGINE HAS BEEN OP NORMALLY SINCE. ECTM PARAMATERS DO NOT SHOW ANY DEGRADATION TO ENGINE. UNCOMMANDED IFSD ON APPROACH INTO COLUMBUS, OH. IS 3RD EVENT WITH ENGINE. REF SER. FDR IS BEING REMOVED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061700022 20020617 00022 EA 2002 6 17 CA020515007 1 20020510 A 7931 O-RING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYD PUMP PAD MISINSTALLED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) AIRCRAFT 7318 REPOSITION FROM WVAC TO PHOENIX LOST OIL PRESSURE. A/C LANDED AT WITCHITA, ON PRELIMINARY INVESTIGAT ION FOUND OIL LOW. SERVICED WITH 5.5 QUARTS. ON CALL MECHANIC AT THIS POINT CANNOT FIND SOURCE OF LEAK. ALSO WVAC IS SE NDING A TEAM ETA FOR WVAC TEAM IS 10:40 AM MAR 26. A/C IS AOG FURTHER INVESTIGATION IS FINDING THAT THE OIL IS COMING FR OM THE AGB. SEAL AND PACKINGS ARE BEING LOOKED AT. MORE INFORAMTION TO FOLLOW AS IT BECOMES KNOWN. AIRCRAFT IS BACK IN SERVICE. OIL LEAKS FOUND AT HYDRAULIC PUMP PAD (SEAL REPLACED) AND IDG SHAFT "O" RING MISINSTALLED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061700023 20020617 00023 NM 2002 6 17 DLM88020618 1 20020603 A 3350 6011779 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 993DL 53345 OVERWING EMERGENCY LIGHTS FLICKERING. REPLACED BATTERY RACK, CHECKS GOOD. 2 L 7 2 4F RT A6WE 2002061700024 20020617 00024 NM 2002 6 17 DLM88020620 1 20020603 A 3350 0L307BPEGPL LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 900DE 53372 ON LAYOVER INSPECTION, FOUND EMERGENCY EXIT LIGHT AT PASSENGER SEAT 26DEF INOP. REPLACED EMERGENCY EXIT WHITE AISLE LIG HT AT SEAT 26DEF. CHECKS OK. 2 L 7 2 4F RT A6WE 2002061700025 20020617 00025 EU 2002 6 17 CA020515008 1 20020510 A 3242 SWIVEL PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL RT BRAKE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING THE ANNUAL INSPECTION, IT WAS NOTICED THAT THE LOWER RT BRAKE SWIVEL FITTING WAS LEAKING BREAK FLUID. THE P ART WAS REPLACED WITH NEW. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002061700026 20020617 00026 NM 2002 6 17 PCAA0206066 1 20020615 A 3350 1013075 SOCKET DHAV DHC8 DHC8102 2809003 NM FORWARD INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 842EX 341 DURING ROUTINE MAINTENANCE VISIT FORWARD RED EMERGENCY AISLE TRACK LIGHT FOUND INOPERATIVE. SOCKET PN 10-1307-5 REPLACED AND RELAMPED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002061700027 20020617 00027 NM 2002 6 17 DLM88020622 1 20020605 A 5310 5936038501 DOOR FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV CORROSION FOUND ON HORIZONTAL FLANGE OF C3 DOOR LOWER JAMB BEAM. PRIOR SRM REPAIR FOUND IN AREA. CORROSION REMOVED. FOUR FASTENER HOLES NOTED WITH LESS THAN 2D ED. ALL DAMAGE REMOVED AND REPAIRED IAW ERA 413057-14. 2 L 7 2 4F RT A6WE 2002061700028 20020617 00028 NM 2002 6 17 CA020515009 1 20020512 A 7921 ACTUATOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA OIL COOLER DOOR FAILED W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CLIMB, OIL TEMPERATURE NR 1 EXCEEDED UPPER LIMIT (1080C) ACCORDING AOM FOR APPROXIMATELY 3 MINUTES. CREW RE DUCED POWER AND ENTERED HOLDING FOR TROUBLESHOOTING. OIL TEMPERATURE THEN RETURNED TO NORMAL. FLIGHT LANDED FOR TECHNICA L INVESTIGATION. OIL COOLER AIR OUTLET FLAP ACTUATOR REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061700029 20020617 00029 NM 2002 6 17 DLM88020623 1 20020605 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV INSPECTION REVEALED CORROSION BETWEEN OUTER SKIN AND BEAR STRAP FOR THE C2 DOOR (FS 731 BETWEEN L29R AND L30) . CORROSION REMOVED AND REPAIRED PER ERA 413053-14. 2 L 7 2 4F RT A6WE 2002061700030 20020617 00030 NM 2002 6 17 DLM88020626 1 20020605 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 913DL 49544 15C MOUNTED EMERGENCY LIGHT INOP. RELAMPED LIGHT. 2 L 7 2 4F RT A6WE 2002061700031 20020617 00031 NM 2002 6 17 DLM90020627 1 20020606 A 2530 OVEN DOUG MD90 MD9030 3023690 NM GALLEY DIRTY A DALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 907DA 53387 FWD JUMPSEAT HALON EXTINGUISHER USED IN FWD GALLEY OVEN DUE TO A SMOLERING PIECE OF PAPER. CLEANED OVEN AND REPLACED HA LON EXTINGUISHER. 2 L 7 2 4F RT A6WE 2002061700035 20020617 00035 NE 2002 6 17 CA020515012 2 20020510 A 7220 102418002 DUCT PIPER PA46 PA46500TP 7104622 SO PWA PT6 PT6A42 52043 NE AIR INLET CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION BOTH INERTIA SEPARATORS WERE FOUND CRACKED IN SEVERAL PLACES WITH CRACKS EXTENDING BEYOND 3 INCH ES IN EITHER DIRECTIONS. REPLACED. 1 L 7 1 3O 4 T RT A25SO E4EA 2002061700036 20020617 00036 SO 2002 6 17 CA020515013 1 20020510 A 2612 653677 FIRE LOOP PIPER PA46 PA46500TP 7104622 SO PWA PT6 PT6A42 52043 NE ENGINE CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION OF THE FIRELOOP DETECTION SYSTEM THE FIRELOOP WAS FOUND CHAFING ON THE BAFFLES IN SEVERAL AREAS INCLUDING HEAT EXCHANGER PLUMBING AT ENGINE. 1 L 7 1 3O 4 T RT A25SO E4EA 2002061700037 20020617 00037 CE 2002 6 17 CA020515014 1 20020407 A 2810 MS20470AD6 RIVET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE LT FUEL TANK SHEARED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 13049 (CAN) UPON INVESTIGATION OF A FUEL LEAK LT AUXILIARY FUEL TANK, "PRC" REMOVED AND FOUND 6 RIVET HEADS ATTACHED TO THE "P RC", AT LT KEEL RIB INSTALLATION BL.91.75. SHANK'S REMOVED AND NEW RIVETS INSTALLED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002061700038 20020617 00038 NM 2002 6 17 CA020515015 1 20020119 A 3260 SENSOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA MLG MISRIGGED W O OTHER N FALSE WARNING DE DESCENT 1 CA (CAN) DURING DESCENT SPEED APPROX. 240 KTS & ALT 8000 FT, RECEIVED LDG ADVISORY LIGHT FOR APPROX. 1 SECONDS ON MLG. BEHA VIOR OF A/C SIMILAR TO NORMAL LDG GEAR EXTENTION, I.E. FELT DRAG & "SOUND". AFTER SYS WENT BACK TO NORMAL. 1ST ACTION O F CREW SPEED REDUCTION. AFTER APPROX. 30-60 SEC SAME EVENT, WITH MAIN GEAR, OCCURED AGAIN. NORMAL GEAR EXT. PREFORMED & NORMAL INDICATION, FOLLOWED BY NORMAL LDG. MAINT INVEST. DETERMINED LT GEAR DOOR CLOSED SENSOR GAP TO BE FAR. LT GEAR D OOR CLOSED SENSOR ADJUSTED. A/C RT-SRV. THE CAUSE FOR UNCOMMANDED DOOR CYCLING AN INCORRECT RIGGING OF GEAR DOOR CLOSED SENSOR. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061700039 20020617 00039 NE 2002 6 17 GLBA2002082 2 20020612 A 7320 CONTROLLER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 1 ENGINE OUT OF ADJUST A GLBA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 NM 03 153GL UE153 NR 1 ITT INDICATES HOT ENG ON CLIMB. ADJUSTED TRIM STICK. 2 L 7 2 4T 4 T RT A24CE E26NE 2002061700040 20020617 00040 CE 2002 6 17 GLBA2002083 1 20020612 A 2432 1013810087 PRINTED CKT BOAR BEECH 1900 1900D 1154162 CE CABIN FAULTY A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 255GL 2199 UE255 LEFT GEN TIE ANN ILL FOLLOWED BY BATTERY CHARGE ANN ILL. REPLACED ABO PCB. 2 L 7 2 4T RT A24CE 2002061700041 20020617 00041 NE 2002 6 17 GLBA2002084 2 20020612 A 7320 CONTROLLER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE OUT OF ADJUST A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 249GL UE249 LEFT ENG TEMP LIMITED ON TAKEOFF. ADJUSTED TRIM STICK. 2 L 7 2 4T 4 T RT A24CE E26NE 2002061700042 20020617 00042 NM 2002 6 17 HNAA0200042 1 20020530 A 2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8102 2809003 NM NR 1 MALFUNCTIONED A HNAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 07 917HA 075 DURING SINGLE ENGINE TAXI, CREW REPORTED LOST NR 1 STANDBY HYDRAULIC SYSTEM PRESSURE AND THE USE OF THE NORMAL BRAKE SYS TEM. CREW USED THE PARKING BRAKE TO STOP THE A/C. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. 2 H 7 2 4T RT A13NM 2002061700043 20020617 00043 NM 2002 6 17 HNAA0200043 1 20020601 A 2910 82970010399 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM LEAKING A HNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 07 931HA 132 CREW REPORTED LOSS OF HYDRAULIC FLUID FROM NR 2 HYD SYSTEM AND SUBSEQUENT ILLUMINATION OF ISO VALVE CAUTION LIGHT. CREW DECLARED AN EMERGENCY AND RETURNED TO MIA. FOUND 2 HYDRAULIC LINES (P/N'S 82970010-399 & 82970010-401) AT NR 1 MLG FWD DOOR ACTUATOR WITH PIN HOLES. INSTALLED TEMPORARY FLEX LINES IAW SPECIAL PROCEDURE 20.1. 2 H 7 2 4T RT A13NM 2002061900108 20020619 00108 EA 2002 6 19 HNAA0200044 1 20020527 A 2910 NAS161210 O-RING DHAV DHC8 DHC8311 1386006 EA HYD SYSTEM DETERIORATED A HNAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 07 284BC 3725 336 CREW REPORTED LOSS OF NR 1 HYDRAULIC SYSTEM FLUID. PRESSURE DID NOT GO TO ZERO. SYSTEM QUANTITY WAS AT ZERO FOR LESS T HAN 10 MINUTES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND LEAKING O-RING ON NR 1 HYD SYSTEM PRESSU RE MANIFOLD. REPLACED O-RING. 2 H 7 2 4T RT A13NM 2002061900111 20020619 00111 NM 2002 6 19 HNAA020043 1 20020601 A 2910 82970010399 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM LEAKING A HNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 07 931HA 36312 132 CREW REPORTED LOSS OF HYDRAULIC FLUID FROM NR 2 HYD SYSTEM AND SUBSEQUENT ILLUMINATION OF ISO VALVE CAUTION LIGHT. CREW DECLARED AN EMERGENCY AND RETURNED TO MIA. FOUND 2 HYDRAULIC LINES AT NR 1 MLG FWD DOOR ACTUATOR WITH PIN HOLES. INST ALLED TEMPORARY FLEX LINES IAW SPECIAL PROCEDURE 20.1. 2 H 7 2 4T RT A13NM 2002061700044 20020617 00044 WP 2002 6 17 IXXA0200029S 1 20020224 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 799AL 70276 2993 45922 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AROUND THE HI-LOK HEAD ON THE LEFT WING UPPER LEADING EDGE APP ROXIMATELY 21 INCHES OUTBOARD OF THE NR 2 PYLON. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLA TION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002061700045 20020617 00045 WP 2002 6 17 IXXA0200036S 1 20020318 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 799AL 70276 2993 45922 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RIGHT HAND WING LEADING EDGE AT STATION XFS 566. REPAI R ACCOMPLISHED REMOVAL DAMAGED AREA, FABRICATION AND INSTALLATION OF FILLERS AND EXTENDED DOUBLER IN ACCORDANCE WITH DOU GLAS MAINTENANCE MANUAL. 2 L 7 4 4F 4A25 2002061700046 20020617 00046 EU 2002 6 17 MALA020329 1 20020520 A 5753 SKIN BAC 146 AVRO146RJ85A 1500097 EU T/E FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 518XJ E2337 DURING C-CHECK IN CVG, LT FLAP SUFFERED CHAFE DAMAGE TO THE BOTTOM SKIN, INBOARD OF RIB NR 1 APPROXIMATELY 9 INCHES AFT OF THE LEADING EDGE. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH RIL HC579H9131 AND EO A57041. 2 H 7 4 4F RT A49EU 2002061700047 20020617 00047 NM 2002 6 17 CA020516001 1 20020122 A 3260 SENSOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA MLG MISRIGGED W O OTHER N FALSE WARNING CL CLIMB 1 CA (CAN) ABOUT ONE MINUTE AFTER TAKEOFF SUDDENLY RECEIVED GEARDOOR WARNING FOR 2 SECONDS AND THEN OFF. ABOUT FIVE SECONDS L ATER RECEIVED THE SAME INDICATION ONCE MORE + AT LEAST RT MLG INDICATION FOR ONE SECOND. THE REST OF THE FLIGHT WENT NOR MAL. LT AND RT GEAR DOOR CLOSED SENSORS AND UPLOCK SENSORS ADJUSTED. THE CAUSE FOR THE UNCOMMANDED DOOR CYCLING AND THE RT RED LIGHT IS INCORRECT RIGGING OF THE GEAR DOOR CLOSED SENSOR AND THE UPLOCK SENSOR. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061700048 20020617 00048 EA 2002 6 17 CA020516002 1 20020515 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 16192 (CAN) RIGHT WINDSCREEN CRACKED WHILE ON THE GROUND. REPLACED FIRST OFFICERS WINDSHIELD IAW 56-11-01. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061700049 20020617 00049 NM 2002 6 17 CA020516003 1 20020125 A 3260 UPLOCK SENSOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA MLG MISRIGGED W O OTHER N FALSE WARNING CR CRUISE 1 CA (CAN) AFTER LEVEL OFF FL180 AND DURING ACCELERATON MAIN GEAR DOOR AND MAIN GEAR UNSAFE ADVISORY LIGHTS CAME ON. WE COULD ALSO HEAR AND FEEL THAT THE GEAR OR DOORS OR BOTH WAS IN MOVEMENT. IT LASTED THOUGH FOR A SECOND OR SO. THIS HAPPENED T WICE WITHIN A COUPLE OF MINUTES. THE FLT. CONTINUED IAS 200. RT GEAR DOOR CLOSED SENSOR ADJUSTED. THE CAUSE FOR THE UNC OMMANDED DOOR CYCLING AND THE RED LIGHT IS INCORRECT RIGGING OF THE GEAR DOOR CLOSED SENSOR AND THE UPLOCK SENSOR. AIRCR AFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061700050 20020617 00050 EU 2002 6 17 CA020516004 2 20020515 A 7322 861115 DIAPHRAGM ROTAX 887266 DIAMON DA20 DA20A1 2990000 GL ROTAX 912 ROTAX912 55555 EU CARBURETOR SWOLLEN W K NONE E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 CA 953069 (CAN) ENGINE VIBRATION AND HESITATION WAS NOTED WITH POWER CHANGES. THE DIAPHRAGM IN THE LT CARBURETOR WAS FOUND TO HAV E SWOLLEN AND TO BE OF INCREASED DIAMETER. 1 L 7 1 3O 3 I NT TA4CH EXPE3I 2002061700051 20020617 00051 EU 2002 6 17 CA020516005 2 20020515 A 7322 861115 DIAPHRAGM ROTAX 887261 DIAMON DA20 DA20A1 2990000 GL ROTAX 912 ROTAX912 55555 EU CARBURETOR SWOLLEN W K NONE E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 CA 953289 (CAN) ENGINE VIBRATION AND HESITATION WERE NOTED DURING POWER CHANGES.THE RT CARB. DIAPHRAGM WAS FOUND TO HAVE SWOLLEN T O A LARGER DIAMETER. 1 L 7 1 3O 3 I NT TA4CH EXPE3I 2002061700052 20020617 00052 EU 2002 6 17 CA020516006 2 20020515 A 7322 961215 NEEDLE ROTAX 887266 DIAMON DA20 DA20A1 2990000 GL ROTAX 912 ROTAX912 55555 EU CARBURETOR WORN W K NONE E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 CA 953069 (CAN) THE JET NEEDLE FROM THE LT CARB ASSY WAS FOUND TO BE WORN. THE GAP BETWEEN NEEDLE POSITION 2 AND 3 WAS WORN AWAY, JOINING THE TWO NEEDLE POSITIONS.THE CIRCLIP WAS FOUND TO BE SITTING SIDEWAYS DUE TO THE MISSING MATERIAL. 1 L 7 1 3O 3 I NT TA4CH EXPE3I 2002061700053 20020617 00053 EU 2002 6 17 MALA020330 1 20020524 A 5315 FLOORBEAM BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 518XJ E2337 DURING C-CHECK IN CVG, CORROSION WAS FOUND ON THE FRAME 18 FLOORBEAM OUTBOARD OF SEAT RAIL NR 3. MAINTENANCE REPAIRED D AMAGE IN ACCORDANCE WITH RIL HC537H9257, BAE FAX BARA/AVR/5931/02-DC AND EO A53085. 2 H 7 4 4F RT A49EU 2002061700054 20020617 00054 EU 2002 6 17 MALA020331 1 20020606 A 2697 WIRE BAC 146 AVRO146RJ85A 1500097 EU NR 3 ENGINE OUT OF POSITION A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 506XJ E2314 DURING FLIGHT 3434, NR 3 ENGINE NR 1 FIRE BOTTLE INDICATION INOP. AIR RETURN TO DTW. MAINTENANCE REROUTED WIRES FROM T ERMINAL BLOCK, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2002061700055 20020617 00055 EU 2002 6 17 MALA020333 1 20020607 A 7931 INDICATOR SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A MALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 408XJ 340B408 ON TAXI OUT OF FLIGHT 2736, RT ENGINE OIL PRESSURE GAUGE INOP. AC RETURNED TO GATE. NO OTHER INFORMATION AVAILABLE AT THIS TIME. 2 L 7 2 4T RT A52EU 2002061700056 20020617 00056 NM 2002 6 17 CA020516007 1 20020214 A 3260 UPLOCK SENSOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA MLG OUT OF ADJUST W O OTHER N FALSE WARNING CL CLIMB 1 CA (CAN) AT CRUISE ALT FL190 WITH MAX ALLOWED SPEED, ALL OF SUDDEN LT & RT MAIN GEAR DOORS STARTED TO, WITHOUT CONTROL, EX TEND & RETRACT, RESULTING IN VIBRATIONS IN A/C, THAT HAPPENED SEVERAL TIMES. REDUCED SPEED TO 210 KTS INDICATED & CONT INUED. ON APPROACH GEAR EXTENDED NORMALLY, BUT AFTER LDG NOSE GEAR DOORS STARTED TO OPEN & CLOSE SEVERAL TIMES. NOSE GE AR LOCK SENSOR HARNESS REPLACED. MLG DOOR CLOSED & UPLOCK SENSORS ADJUSTED. A/C RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002081400025 20020814 00025 EU 2002 8 14 MALA020334 1 20020608 A 2150 11341041 MOTOR SAAB SF340 340B 7860101 EU A/C SYSTEM SPARKS A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 421XJ 340B421 BEFORE STARTING FLIGHT 2732, SUPPLEMENTAL AC INOP. FIVE MINUTES AFTER AC POWERED UP, SMOKE APPEARED IN COCKPIT AND CABI N. MAINTENANCE TROUBLESHOT AC SYSTEMS FOR SOURCE OF SMOKE, FOUND SUPPLEMENTAL AIR SYSTEM MOTOR ARCING SPARKS, SUSPECT M OTOR BURNING UP. MAINTENANCE REMOVED AND REPLACED AUX A/C COMPRESSOR MOTOR PN 1134104-1, SN/ON 450, SN/OFF 439, IAW CMM . 2 L 7 2 4T RT A52EU 2002081400028 20020814 00028 EU 2002 8 14 MALA020335 1 20020608 A 2150 11341041 MOTOR SAAB SF340 340B 7860101 EU A/C SYSTEM MALFUNCTIONED A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 453XJ 340B453 DURING PREFLIGHT OF FLIGHT 3031, WHILE PARKED AT CMI ON THE GROUND AFTER A/C QUIT, WITH EXTERNAL POWER ON, SMOKE DISCOV ERED COMING FROM AVIONICS BAY. SMOKE IN THE CABIN ON PREFLIGHT, DEPLANED PASSENGERS. MAINTENANCE INSPECTED AVIONICS BA Y/ AVIONICS EQUIPMENT FOR CONDITION, SECURITY, CHECKS ARE GOOD. SUSPECT SMOKE WAS COMING FROM SUPPLEMENTAL A/C UNIT, DE FERRED. RAN AVIONICS FAN ON EX POWER, NO DISCREPANCIES NOTED. RAN AVIONICS FAN FROM GEN POWER WITH A/C PACKS ON, NO DI SCREPANCIES NOTED. MAINTENANCE REPLACED COMPRESSOR MOTOR, RECEIVER/DRYER COMPRESSOR BELT GAUD REF MM 409 144407 AND CON TINUATION PG 071315 &16 REPLACED BELT COVER ASSY. 2 L 7 2 4T RT A52EU 2002061700058 20020617 00058 CE 2002 6 17 CA020516009 1 20020516 A 5311 FRAME BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11484 (CAN) FUSELAGE RIGHT HAND FRAME AT STA 158.00, STRINGER 10 CRACKED. SHEET METAL REPAIR TO BE DONE PRIOR TO FURTHER FLIGH T. 1 L 7 2 4T 4 T A24CE E4EA 2002061700059 20020617 00059 CE 2002 6 17 CA020516010 1 20020516 A 5311 FRAME BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11484 (CAN) FUSELAGE RIGHT HAND FRAME STA 167.625, STRINGER 10 CRACKED. SHEET METAL REPAIR TO BE DONE PRIOR TO FLIGHT. 1 L 7 2 4T 4 T A24CE E4EA 2002061700060 20020617 00060 WP 2002 6 17 MWEA020407 1 20020609 A 2781 3952485501 PLUNGER DOUG DC9 DC982 3022082 WP L/E SLAT CRACKED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 808ME 48070 SLAT DISAGREE LIGHT ILLUMINATED AFTER SLAT RETRACTED. REMOVED AND REPLACED CRACK, SPRINGS, PLUNGER ASSEMBLY CAM FOLLOW PER MD80 MAINTENANCE MANUAL 27-80-1. 2 L 7 2 4F A6WE 2002061700062 20020617 00062 EA 2002 6 17 CA020517001 1 20020514 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER LD LANDING 1 CA (CAN) ON FLIGHT THE CREW REPORTED RT WINDSHIELD INNER PLY SHATTERED UPON LANDING.ENGINEERS REPLACED WINDSHIELD BY S/N 01 180H2136 THE WINDSHIELD INSTALLED WAS A POST SERVICE BULLETIN WINDSHIELD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061700063 20020617 00063 NM 2002 6 17 P5CA0200682 1 20020607 A 5420 WEB BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 702066 FOUR CRACKS FOUND ON NR 2 ENG PYLON, AFT ENGINE MOUNT BULKHEAD FRAME, VERTICAL WEB STATION 221.9. (1. CRACK ON FRONT OUT BOARD WEB, 3 INCHES LONG. 2. CRACK ON FRONT OUTBOARD WEB, 1 INCH LONG. 3. CRACK ON FRONT INBOARD WEB, 3.5 INCH LONG. 4. CRACK ON FRONT OUTBOARD WEB, 3 INCHES LONG). REPAIRED BY INSTALLING WEB FILLERS, WEB DOUBLERS AND ANGLE CORDS ON LEF T AND RIGHT FWD FRAME HALVES IAW PAOE020523, DRAWING 65B07582-SHT 8, SB747-54-A2202 & SB747-54-2065. 2 L 7 4 4F 4 F A20WE E3NE 2002061700064 20020617 00064 NE 2002 6 17 CA020517002 2 20020516 A 7261 B-NUT AIRBUS 320 A320212 3930322 EU CFMINT CFM56 CFM565A3 NE NR 2 ENG OIL LOOSE W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) DIVERTED DUE TO DECREASING OIL QUANTITY NR 2 ENGINE. THIS ENGINE WAS CHANGED AND WAS ON ITS FIRST REVENUE FLIGHT. ALL LEAK CHECKS WERE COMPLIED WITH AS PER AMM 71-00-00 POWER PLAT REMOVAL AND INSTALLATION. INVESTIGATION REVEALED LOO SE "B" NUT ON LINE TO PRESSURE TRANSMITTER WHICH WAS TIGHTENED AND ENGINE OIL SERVICED. ENGINE RUNS AND LEAK CHECKS WERE ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E29NE 2002061700065 20020617 00065 WP 2002 6 17 AALA20020525 1 20020423 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 477AA 49652 DFW - DURING OVERNIGHT MAINTENANCE, AFT CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT CABIN EMERGENCY EXIT LIGH TS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002061700066 20020617 00066 WP 2002 6 17 AALA20020527 1 20020423 A 3350 P4010049 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 591AA 53254 SAT - DURING OVERNIGHT MAINTENANCE, ALL SEAT PATH AND EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EX IT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002061700067 20020617 00067 WP 2002 6 17 AALA20020528 1 20020423 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 510AM 49804 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROWS 27-29 AFT SERVICE OVERHEAD INOPERATIVE. REPLACED EMER GENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002061700068 20020617 00068 WP 2002 6 17 AALA20020547 1 20020425 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 291AA 49303 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY EXIT LIGHT INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHT WIRE ON BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002061700069 20020617 00069 WP 2002 6 17 AALA20020550 1 20020426 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7535A 49989 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002061700070 20020617 00070 NM 2002 6 17 AALA20020556 1 20020425 A 2121 6067723 FAN BOEING 757 757223 1384957 NM CABIN MALFUNCTIONED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 659AA 24617 PTY - FLT 2110 - EN ROUTE LIM-MIA - ACRID ELECTRICAL SMELL IN COCKPIT AND CABIN. RECIRCULATING FAN ALREADY TRIPPED OFF. SMELLS STOPPED WHEN RIGHT PACK TURNED OFF. AIR INTERRUPTED AND LANDED PTY WITHOUT INCIDENT. ACCOMPLISHED RECIRCULATI ON SYSTEM OPERATIONAL TEST FOR BOTH LEFT AND RIGHT RECIRCULATION FANS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002061700071 20020617 00071 GL 2002 6 17 CA020517005 3 20020514 A 6114 99150S12C HUB PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL PROPELLER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) PROPELLER LEAKS GREASE FROM BLADE CLAMP AREA. CAN OBSCURE PILOT'S VIEW THOUGH WINDSHEILD. TEFLON TAPE PROVIDES GRE ASE SEAL. WORN OUT BEFORE TBO.REPAIR TIME 2/3 DAYS. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002061700072 20020617 00072 NM 2002 6 17 AALA20020569 1 20020412 A 5753 SUPPORT FITTING BOEING 777 777223 1385213 NM T/E FLAP DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 788AN 30011 AFW - FOUND LEFT TIE FLAP SUPPORT FITTING OUTBOARD BEARING LUG HOLE OUTBOARD CHAMFER WAS OVER CHAMFER. FABRICATE A REPA IR SPACER FROM 17-4PN STAINLESS STEEL APPLY BMS 10-11 PRIMER TO REPAIR SPACER AND INSTALL SPACER WET WITH BMS 5-95 SEALA NT. (M) 2 L 7 2 4F RT T00001SE 2002061700073 20020617 00073 NM 2002 6 17 AALA20020571 1 20020424 A 5311 FRAME BOEING 777 777223 1385213 NM FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 AFW - TWO GOUGES FOUND IN FRAME OUTER CHORD AT STATION 246 WATER LINE 207. BLENDED TWO GOUGES. NDT CHECKED. ALODINED, PRIMED, PAINTED. CONTINUED IN SERVICE PER MRB 777-032. (M) 2 L 7 2 4F RT T00001SE 2002061700074 20020617 00074 SO 2002 6 17 C2XA02TY105 1 20020617 A 5542 12021755001 SKIN EMB 145 EMB145 3260210 SO NICKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 TYS, During a scheduled inspection the rudder 2 leading edge on the left side was found nicked. Maintenance blended the affected area, performed dye-pen. inspection, alodined and primed. I/A/W-GST-1886/02 and CPM-51-21-04/05/06. The repair was satisfactory and the aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002061700075 20020617 00075 2002 6 17 AALA20020582 4 20020501 A 2565 SLIDE BOEING 757 757223 1384957 NM PAX DOOR MALFUNCTIONED A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 197AN 32391 MIA - FLT 68 - UPON ARRIVAL AT MIA, FORWARD ENTRY DOOR SLIDE PARTIALLY DEPLOYED AFTER DOOR OPENED. SLIDE WAS REMOVED FR OM COMPARTMENT AND GIRT BAR BEFORE INFLATION OCCURRED. DOOR WAS DISARMED. INSPECTED SLIDE ARMING MECHANISM. OPERATION CHECKS GOOD. REPLACED L1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002061700076 20020617 00076 NM 2002 6 17 AALA20020648 1 20020514 A 2520 INSULATION BOEING 757 757223 1384957 NM CABIN BURNED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AM 24491 TUL - INSULATIONS SHOWS EVIDENCE OF BEING BURNED AT 860 STRINGER 29R AND AT 880 STRINGER 29R. INSPECT THE AREA FOUND NO STRUCTURAL HEAT DAMAGE. MODIFIED AND SECURED INSULATION BLANKET TO PROVIDE CLEARANCE BETWEEN HEAT SOURCE AND BLANKET, OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4F RT A2NM 2002061700077 20020617 00077 WP 2002 6 17 AALA20020651 1 20020516 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 557AN 53087 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS BETWEEN ROWS 28-31 INOPERATIVE. RESEATED EMERGENCY E XIT LIGHTS BATTERY ON BATTERY PACK B5-107. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002061700078 20020617 00078 NM 2002 6 17 AALA20020705 1 20020510 A 2424 73428F GCU BOEING 777 777223 1385213 NM NR 2 ENGINE FAULTY A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 762AN 31479 ORD - FLT 153 - EN ROUTE ORD-NRT - GENERATOR CONTROL OFF LIGHT CONTINUALLY CYCLED THROUGHOUT ENTIRE FLIGHT. RETURNED OR D AND LANDED WITHOUT INCIDENT. REPLACED RIGHT GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002061700080 20020617 00080 WP 2002 6 17 AALA20020712 1 20020518 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 580AA 53157 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ON SEATS 20D-31D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002061700081 20020617 00081 WP 2002 6 17 AALA20020713 1 20020517 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN OUT OF ADJUST A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 477AA 49652 DFW - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHTS DIM. ADJUSTED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002061700082 20020617 00082 WP 2002 6 17 AALA20020714 1 20020517 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 477AA 49652 DFW - DURING OVERNIGHT MAINTENANCE, PASSENGER DOOR EMERGENCY EXIT LIGHTS DIM. TIGHTENED EMERGENCY EXIT LIGHT WIRE CONNE CTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002061700083 20020617 00083 WP 2002 6 17 AALA20020715 1 20020517 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAIL CONE LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 246AA 49258 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY EXIT LIGHTS DIM. SECURED EMERGENCY EXIT LIGHT WIRE CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002061700084 20020617 00084 NM 2002 6 17 AALA20020716 1 20020516 A 2934 CONNECTOR BOEING 757 757223 1384957 NM HYD SYSTEM DIRTY A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 646AA 24604 MIA - FLT 1574 - EN ROUTE ORD-SJU - CENTER HYDRAULIC QUANTITY WENT TO 0, THEN BACK TO 1.01, THEN 0, THEN BACK TO 1.01. LANDED IN MIA WITHOUT INCIDENT. VISUALLY INSPECTED CENTER HYDRAULIC QUANTITY. FLUID LEVEL READS FULL. CLEANED CANNON PLUG ON HYDRAULIC QUANTITY HYDRAULIC TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002061700085 20020617 00085 NM 2002 6 17 AALA20020725 1 20020520 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 312AA 22315 LAX - DURING OVERNIGHT MAINTENANCE, TWO FIRST CLASS FLOOR LEVEL EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED FIRST CLASS FLOOR LEVEL EMERGENCY EXIT LIGHTS WIRE UNDER GALLEY FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002061700088 20020617 00088 EA 2002 6 17 CA020517008 1 20020404 A 5530 600926291 CROSSBEAM CNDAIR CL600 CL6001A11 1900302 EA LYC ALF502 ALF502L2 41580 NE RUDDER CONTROL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INTERNAL STRUCTURAL INSPECTION OF THE TAIL AREA, A 5/8 INCH CRACK WAS FOUND ON THE RUDDER CONTROL CROSS BEA M SUPPORT (EMPENNAGE).THE PROBABLE CAUSE MAY BE THAT ON THE LOWER LT OUTBOARD RIVETS WITH BELLOW MINIMUM EDGE DISTANCE. IN ADDITION, THE RIVET HEAD ARE IN THE RADIUS OF THE INSTALLATION. 2 L 7 2 4F 4 F RT A21EA E6NE 2002061700089 20020617 00089 CE 2002 6 17 CA020517009 1 20020516 A 5312 BULKHEAD BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11484 (CAN) BULKHEAD CRACKED BELOW FLOOR AT STATION 227.125 CENTER SECTION. SHEET METAL REPAIRS TO BE CARRIED OUT PRIOR TO FUR THER FLIGHT. 1 L 7 2 4T 4 T A24CE E4EA 2002061700090 20020617 00090 CE 2002 6 17 CA020521001 1 20020515 A 7120 50910279 MOUNT BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA ENGINE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 12037 12037 (CAN) MOUNT FRAME TUBES FOUND TO HAVE WEAR SPOTS THRU TUBE MATERIAL.WEAR WAS DISCOVERED AFTER ENGINE WAS REMOVED AND ARE AS MORE ACCESSABLE. THE WEAR WAS CAUSED FROM SURROUNDING FIRE SHIELDS, CABLES ETC. 1 L 7 2 3T 4 T A14CE E4EA 2002061700091 20020617 00091 NM 2002 6 17 CA020521002 1 20020518 A 2612 1010961 FIRE LOOP DHAV DHC8 DHC8* NM PWC 150 PW150A EA LT ENGINE MALFUNCTIONED W K NONE N FALSE WARNING IN INSP/MAINT 1 CA (CAN) AFTER ENGINE SHUTDOWN LT ENGINE FIRE WARNING CAME ON. AFTER COMPLETE POWER-OFF, OK. ( NO VISUAL SIGNS OF FIRE.) SYSTEM CHECKED ON GROUND. WORKS NORMAL ALL AFFECTED CONNECTORS CHECKED, NO FINDING. INSPECTED CABLES AS FAR AS POSSIBLE. PROPELLER ELECTRINIC CONTROL (PEC) FIRE LOOP WAS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061700093 20020617 00093 SW 2002 6 17 CA020521006 1 20020323 A 5302 206031004075 SKIN BELL 20603100471B BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL TAILBOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA BCJN5079 (CAN) A 1.5 INCH CRACK WAS FOUND EMMINATING FROM A RIVET ON THE LT SIDE OF THE BOOM AT STA 136.9. THE CRACK FORMED DOWNW ARD TO THE EDGE OF THE UPPER SKIN AND UPWARD FOR APPROXIMATELY 1.25 INCHES. TAILBOOM WAS REPAIRED IN ACCORDANCE WITH BEL L SRM. NR 1 BEARING HANGER AND DR GEARBOX MOUNTS WERE FOUND TO BE MISALIGNED. 1 G 7 1 3U 3 U H2SW E4CE 2002061700094 20020617 00094 NE 2002 6 17 CA020521007 1 20020325 A 2435 230811130 HOUSING LEARSIEGLER 23081043 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL STARTER GEN SEPARATED W K NONE L NO TEST IN INSP/MAINT 1 CA 809 (CAN) 5.9 HOURS AFTER A SCHEDULED BRUSH CHANGE A LOUD "HUM" WAS DETECTED ON NR 2 GENERATOR. THE HUM STOPPED WHEN THE GEN ERATOR WAS SELECTED OFF. THE STARTER/GENERATOR WAS REMOVED AND THE BELL HOUSING LEGS WERE FOUND TO BE SEPARATED FROM THE MOUNTING RING. THE STARTER/GENERATOR WAS REPLACED WITH A SERVICEABLE UNIT. 1 G 7 2 3U 3 U H1NE E1GL 2002061700095 20020617 00095 NM 2002 6 17 AALA20020726 1 20020520 A 3350 SOCKET BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 319AA 22320 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AROUND SEAT 20B FLASH INTERMITTENTLY. REPLACED TWO EMERGENCY EXIT LIGHT SOCKETS AT SEAT 20 A/B. ALSO, CLEANED AND TIGHTENED CONNECTION. SYSTEM GROUND CHECKED NORMAL OPE RATION. (M) 2 L 7 2 4F RT A1NM 2002061700096 20020617 00096 NM 2002 6 17 AALA20020728 1 20020521 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 332AA 22331 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 20F INOPERATIVE. RESET EMERGENCY EXIT SEAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002061700097 20020617 00097 EU 2002 6 17 CA020521008 1 20020514 A 6700 BALL JOINT 126892P AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20F 03013 GL CONTROL ROD WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AFTER LAST FLIGHT INSPECTION THE LOWER ROD END WAS FOUND TO BE LOOSE. THE STAKED AREA AROUND THE BALL WAS WORN ENO UGH TO ALLOW IT TO COME OUT OF THE ROD END. NEW ROD END INSTALLED. 1 G 7 2 3U 3 U H11EU E4CE 2002061700098 20020617 00098 EA 2002 6 17 CA020521009 1 20020515 A 2910 DSC252A40272 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE BRAKE ASSY CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) PILOT FOUND DURING WALK AROUND BEFORE DEPARTURE FROM YAD A SMALL QUANTITY OF HYD. FLUID UNDER NR 3 BRAKE ASSY. MAI NT ADVISED AND REQUEST THE PILOT TO APPLIED THE PARKING BRAKE TO CONFIRM THE LEAK. PILOT CONFIRM THAT LEAK IS FROM HYD. FLEX LINE CONNECTED TO NR 3 BRAKE ASSY. MECH. SENT OVER TO REPLACE THE DEFFECTIVE HYD LINE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061700099 20020617 00099 CE 2002 6 17 CA020521010 1 20020521 A 5311 5042006653 FRAME BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11484 (CAN) DURING STRUCTURAL INSPECTION FOUND FLIGHT DECK UPPER FUSELAGE LEFT HAND FORMER CRACKING IN TWO LOCATIONS. FORMER T O BE REPLACED PRIOR TO FURTHER FLIGHT. 1 L 7 2 4T 4 T A24CE E4EA 2002061700100 20020617 00100 WP 2002 6 17 AALA20020729 1 20020509 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7544A 53026 TUL - FOUND CORROSION ON SUBFLOOR STRUCTURE AT FORWARD ENTRY DOOR FROM STATION 168 TO STATION 200. INSTALLED DOUBLER AF TER CUT OUT OF AFFECTED AREA PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002061700101 20020617 00101 WP 2002 6 17 AALA20020730 1 20020501 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7544A 53026 TUL - FOUND CORROSION ON CUSP LONGERON 18 LEFT AT STATION 747. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002061700102 20020617 00102 EU 2002 6 17 QXEA0200874 1 20020614 A 3240 95437051 WHEEL FOKKER F28 F28MK4000 4990810 EU ZONE 700 DEFECTIVE A QXEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 09 499US 971 126 11182 SEA-DURING ROTATION MODERATE TO SEVERE VIBRATION FELT FROM NOSE WHEEL AREA. VIBRATION WAS EVIDENT IN CABIN AND COCKPIT. AIRCRAFT RETURNED TO SEA, LANDED AIRCRAFT WITHOUT INCIDENT. FIRE AND RESCUE MET AIRCRAFT ON LANDING. REPLACED #1 AND #2 NOSE WHEEL ASSY. INSPECTED NOSE LANDING GEAR, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002061700103 20020617 00103 WP 2002 6 17 AALA20020738 1 20020503 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7534A 49988 TUL - FOUND CORROSION ON HORIZONTAL AND VERTICAL LEGS OF MID CARGO LOWER DOOR BEAM. FORWARD AND AFT STOP BOLT HOLES AR E OUT OF LIMITS AFTER CORROSION REMOVAL. INSTALLED TWO DOUBLERS AT DOOR BEAM STOP BOLT AREAS PER AARD 53-10-00-16. (M) 2 L 7 2 4F A6WE 2002061700104 20020617 00104 NM 2002 6 17 AALA20020739 1 20020510 A 2424 GEN3014 GCU BOEING 777 777223 1385213 NM RIGHT FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 762AN 31479 ORD - FLT 0153 - RIGHT GEN CONTROL OFF LIGHT CONTINUALLY CYCLED THROUGH OUT ENTIRE FLIGHT. NO EICAS MESSAGE WHEN ON LOA D SHEDDING INDICATIONS WERE DISPLAYED WHEN OFF LIGHT ON. FOUND RIGHT GCU FAILED WITH CODE 24-33402. REPLACED RIGHT GCU . ALL CHECKS GOOD. (M) 2 L 7 2 4F RT T00001SE 2002061700105 20020617 00105 NM 2002 6 17 UPS02438635 1 20020531 A 5310 WEB BOEING 747 747200 1384847 NM MD BS1220 RBL110 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C M/D - BS 1220 RBL 110 FLR BEAM WEB CRK. FLOOR BEAM WEB REPAIR CARRIED OUT AS PER SRM 51-40-02 FIG. 1 2 L 7 4 4F RT A20WE 2002061700106 20020617 00106 NM 2002 6 17 UPS02438636 1 20020531 A 5310 WEB BOEING 747 747200 1384847 NM M/D BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C M/D - BS 1220 LBL 98-116 FLR BEAM WEB FOUND CRACKED. FLOOR BEAM WEB REPAIR CARRIED OUT AS PER SRM 51-40-02 FIG.1 2 L 7 4 4F RT A20WE 2002061700107 20020617 00107 NM 2002 6 17 UPS02438637 1 20020529 A 5310 WEB BOEING 747 747200 1384847 NM RH NOSE W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C CRACK FOUND AT RH NOSE W/W FRAME WEB AT BS 320 VERT BEAM ATTACHED AREA, SEE ATTACHED SKETCH FOR DETAIL S. NOSE W/W FRAME AT RH BS 320 AREA REPAIRED AS PER SRM 53-10-04. 2 L 7 4 4F RT A20WE 2002061700108 20020617 00108 NM 2002 6 17 UPS02438640 1 20020602 A 5340 SEAT TRACK BOEING 747 747200 1384847 NM M/D BS1940-1980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C M/D - BS 1940-1980 RBL 78 SEAT TRACK CROWN AND LIP FOUND COR. SEAT TRACK SECTION REPAIRED AT BTN B S 1930 - BS 1990 RBL 75 AS PER SRM 53-10-05 FIG. 1A. CORROSION BLEND OUT SIZE 0.060" X 0.5" X 2" 2 L 7 4 4F RT A20WE 2002061700110 20020617 00110 2002 6 17 AALA20020741 4 20020515 A 3442 RADAR BOEING 777 777223 1385213 NM COCKPIT MALFUNCTIONED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 782AN 30003 ORD - FLT 66 - WEATHER RADAR INOPERATIVE UNTIL 30 MINUTES FROM LONDON WEATHER SYSTEM ON STATUS PAGE STILL THERE. SAME P ROBLEM LEAVING CHICAGO BUT AFTER IT WAS FIXED, IT WENT INOPERATIVE 20 MINUTES AFTER TO WEATHER FAIL ALSO ON NAV DISPLAY. ACCOMPLISHED SYSTEM TEST OF BOTH LEFT AND RIGHT WEATHER RADAR SYSTEMS. ALL OPS NORMAL. (M) 2 L 7 2 4F RT T00001SE 2002061700111 20020617 00111 EA 2002 6 17 CA020522001 1 20020517 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 18412 (CAN) CLIMBING THUR 13,500 FT THE CAPT'S WINDSHIELD INNER PLY CRACKED. RETURNED AND REPLACED CAPT'S WINDSHIELD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061700112 20020617 00112 WP 2002 6 17 AALA20020744 1 20020521 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 498AA 49736 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVER COCKPIT DOOR INOPERATIVE. SECURED COCKPIT DOOR EMERGENCY EXIT LIGHT BATTERY WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002061700113 20020617 00113 WP 2002 6 17 AALA20020745 1 20020523 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 234AA 49181 DFW - DURING OVERNIGHT MAINTENANCE, LEFT FORWARD ENTRY DOOR CEILING EMERGENCY EXIT LIGHT DIM. TIGHTENED LEFT FORWARD EN TRY DOOR CEILING EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002061700114 20020617 00114 EA 2002 6 17 CA020522002 1 20020508 A 2140 A07D48 MOTOR CNDAIR CL215 CL2151A10 1900320 EA HEATER FAILED W F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) A/C HAD HEATER OVERHEAT LIGHT INDICATION. OVERHEAT SWITCH RESET. HEATER GROUND RUN & OVERHEAT INDICATION AGAIN. O VERHEAT SWITCH REPLACED. HEATER GROUND RUN FOR 5 MINS, CHECKED OK. NEXT GROUND OP BY PILOT RESULTED IN SMOKE IN COCKPIT . HEATER FIRE BOTTLE DISCHARGED. INVESTIGATION REVEALED HEATER BRUSH & CAP HAD FAILED RESULTING IN COMBUSTION BLOWER MO TOR STOPPING OVERHEATING CAN. WIRING NEAR MOTOR MELTED RESULTING IN COCKPIT SMOKE. FAILED BRUSH/SPRING VERY WORN COMPARE D TO OTHER BRUSH. HEATER'S LOW TIME & SUBSEQUEST FAILURE OF COMBUSTION BLOWER MOTOR MAY MAKE NECCESSARY A BRUSH INSPECTI ON BETWEEN HEATER OVERHAULS. 2 H 7 2 4R RT A14EA 2002061700115 20020617 00115 EU 2002 6 17 AALA20020749 1 20020523 A 3230 10SD8001 SOLENOID FOKKER F28 F28MK0100 4990807 EU COCKPIT FAILED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 1401G 11352 LGA - FLT 1045 - EN ROUTE LGA-YYZ - LANDING GEAR HANDLE WOULD NOT RETRACT AFTER TAKEOFF. RETURNED LGA AND LANDED LGA WI THOUT INCIDENT. REPLACED ANTI-RETRACTION SOLENOID. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002061700116 20020617 00116 NM 2002 6 17 CA020522003 1 20020519 A 6120 697073002 PCU DHAV DHC8 DHC8* NM PWC 150 PW150A EA ROTOL R408 CR4086123F17 EU PROPELLER FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) T/O ABORTED DUE TO "POWERPLANT" MESSAGE ON ED. AFTER TAXING OFF THE RUNWAY AND RT POWER LEVER IN DISC, PROP OSG TE ST IN PROG AND ABORT APPEARS UNCOMMANDED. ENGINE RUN PERFORMED, OSG TEST PERFORMED SUCCESSFULLY BUT WHEN POWER LEVER GOE S FROM FLIGHT IDLE BACK TO DISC SAME PROBLEM HAPPENS AGAIN AND POWERPLANT MESSAGE COMES ON AGAIN. A NEW PCU INSTALLED ON NR 2 ENG. PERFORMED OPERATIONAL TEST. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 6 C P17BO 2002061700117 20020617 00117 NM 2002 6 17 CA020522004 1 20020516 A 2910 AE2463530E240 HYDRAULIC LINE DHAV DHC8 DHC8301 1386003 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE NR 3 BRAKE SPLIT W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) AFTER LANDING PILOT WAS COMPLETING POST FLIGHT/PRE FLIGHT WALK AROUND INSPECTION AND FOUND THE NR 3 BRAKE LINE LEA KING HYDRAULIC FLUID. MAINTENANCE DISPATCHED WITH FLEXIBLE BRAKE LINE, HYDRAULIC FLUID AND TOOLING REQUIRED. NR 3 BRAKE FLEXIBLE LINE REPLACED. SYSTEM SERVICED AND BLEED AS PER AMM AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061700118 20020617 00118 EU 2002 6 17 AALA20020750 1 20020524 A 2120 A2127346100000 CHECK VALVE AIRBUS 300 A300B4605R 3930308 EU A/C BAY MISSING A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 14077 612 MIA - FLT 1305 - EN ROUTE MIA-SJU -ON CLIMB-OUT NOT ABLE TO CONTROL PRESSURIZATION IN REGULAR 1, REGULAR 2, OR MANUAL MO DES. RETURNED MIA AND LANDED WITHOUT INCIDENT. DISCOVERED AIR CONDITIONING CHECK VALVE MISSING AND DOOR OPEN. REPLACE D AIR CONDITIONING CHECK VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002061700119 20020617 00119 NM 2002 6 17 AALA20020751 1 20020522 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 664AA 25298 DFW - FOUND EMERGENCY EXIT SIGN AT ROW 30 ABC INOPERATIVE. REPLACED BATTERY PACK M735. SYSTEM GROUND CHECKED NORMAL OP ERATION. (M) 2 L 7 2 4F RT A2NM 2002061700120 20020617 00120 NM 2002 6 17 CA020522005 1 20020201 A 6123 CONTROLLER DHAV DHC8 DHC8* NM PWC 150 PW150A EA ROTOL R408 CR4086123F17 EU PROP FEATHERING MALFUNCTIONED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) TAKE OFF ABORTED DUE TO NO AUTOFEATHER ARM INDICATION. MAINTENANCE INVESTIGATION / ACTION FAULT CODE 420 (AUTOFEAT HER ARMED LOGIC) FOR LT PROP CHANNEL. A WAS FOUND IN THE CENTRAL DIAGNOSTIC SYSTEM. THE FAULT CODE WAS CLEARED SUCCESSFU LLY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 6 C P17BO 2002061700121 20020617 00121 NM 2002 6 17 AALA20020752 1 20020522 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 664AA 25298 DFW - FOUND EMERGENCY EXIT AISLE LIGHTS BETWEEN ROW 20 AND 24 INOPERATIVE. REPLACED BATTERY PACK M735. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002061700123 20020617 00123 EU 2002 6 17 AALA20020753 1 20020526 A 3350 P4010049 POWER SUPPLY AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA - EMERGENCY LIGHT AT L1 DOOR AND FROM SEAT 1G TO 5G INOPERATIVE. REPLACED POWER SUPPLY. SYSTEM GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002061700124 20020617 00124 EA 2002 6 17 CA020523001 1 20020522 A 2752 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) FLAPS FAIL ON SHORT FINAL, WITH FLAPS SELECTED AT 450, POST FLIGHT INSPECTION SHOWS RT OUTBOARD FLAP PANEL TWISTED . REMOVED AND REPLACED NR 3 AND 4 ACTUATORS ON RT SIDE. RT FLAP FLEX DRIVE TORQUE CHECKS CARRIED OUT, OK, AND BPSU BRA KE HOLDING CHECK C/W. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061700125 20020617 00125 EA 2002 6 17 CA020523002 1 20020522 A 2761 6007510315 PCU CNDAIR CL601 CL6012A12 1900303 EA SPOILERS FAILED W O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 CA (CAN) FLIGHT SPOILER HANDLE WOULD NOT REMAIN IN STOWED DETENT. FOUND (RT OB) FLIGHT SPOILER PCU WAS RESTRICTED INTERNALL Y, POSSIBLE HYDRAULIC LOCK BY FLUID BYPASSING TO WRONG SIDE OF PISTON INTERNALLY. THIS WOULD NOT ALLOW THE RIGHT FLIGHT SPOILER TO STOW COMPLETELY. 2 L 7 2 4F RT A21AE 2002061700126 20020617 00126 SO 2002 6 17 COMA0210026 1 20020615 A 2430 GENERATOR EMB 120 EMB120RT 3260202 SO A COMA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 01 463CA 120267 FLIGHT 5067 #1 GENERATOR FAILED AFTER T/O.DEFERRED MAINT ON #1 GENERATOR PER MEL. 2 L 7 2 4T RT A31SO 2002061700127 20020617 00127 EA 2002 6 17 COMA0260370 1 20020616 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 958CA 7111 FLIGHT 5483 EMERGENCY LIGHTS ARE INOP.COULD NOT DUPLICATE. ALL EMERGENCY LIGHTS FUNCTION. 2 L 7 2 4F RT A21EA 2002061700128 20020617 00128 EA 2002 6 17 COMA0260371 1 20020616 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 957CA 9562 7109 FLIGHT 6075 EMERGENCY LIGHTS ARE INOP.REPLACED EMERGENCY LIGHTS BATTERY. 2 L 7 2 4F RT A21EA 2002061700129 20020617 00129 EA 2002 6 17 COMA0260372 1 20020616 A 2620 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 959CA 7116 FLIGHT 5668 CARGO FIRE BOTTLE CAUTON MESSAGE.DEFERRED MAINT ON CARGO FIRE EXT. SYSTEM PER MEL. 2 L 7 2 4F RT A21EA 2002061700130 20020617 00130 EA 2002 6 17 COMA0260374 1 20020615 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 965CA 7131 FLIGHT 5124 DURING BLEED AIR TRANSFER, COCKPIT FILLED WITH SMOKE AFTER LANDING WHILE TAXIING TO THE GATE.SECURED R/H COO LING PACK AND DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2002061700131 20020617 00131 EA 2002 6 17 COMA0260375 1 20020614 A 3250 BRAKE CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 959CA 7116 FLIGHT 5875 AS THRUST ADVANCED FOR T/O, AIRCRAFT VEERED RT.COULD NOT DUPLICATE INSPECTED NWS, RUDDER TRAVEL AND BRAKES. NO DEECTS NOTED. 2 L 7 2 4F RT A21EA 2002061700132 20020617 00132 WP 2002 6 17 AALA20020755 1 20020524 A 7830 221CH54RB SWITCH DOUG DC9 DC982 3022082 WP THRUSU REVERSER MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 449AA 49475 PHL - FLT 1479 - EN ROUTE PHL-DFW - AFTER TAKEOFF, LEFT ENGINE REVERSER UNLOCK LIGHT ILLUMINATED AND REMAINED ON. RETUR NED AND LANDED PHL WITHOUT INCIDENT. REPLACED BOTH UPPER AND LOWER LATCH SWITCHES. PERFORMED OPERATION CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002061700133 20020617 00133 WP 2002 6 17 AALA20020756 1 20020527 A 2170 21D101 COALESCER BAG DOUG DC9 DC983 3022083 WP A/C BAY DIRTY A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 76201 53291 AUS - FLT 1669 - EN ROUTE HOU-AUS - AFTER TAKEOFF WITH CLIMB POWER SELECTED THE PASSENGER CABIN FILLED WITH A LIGHT FOG/ SMOKE AND A VERY LIGHT SMELL OF OIL. DISSIPATED WITHIN A FEW MINUTES PACKS, PRESSURIZATION, ALL ELECTRICAL NORMAL. LAN DED AUS WITHOUT INCIDENT. REPLACED COALESCER BAGS IN AIR CONDITIONING SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002061700134 20020617 00134 NM 2002 6 17 AALA20020757 1 20020525 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 635AA 24593 DFW - THE RIGHT EXTERIOR DOOR EMERGENCY LIGHT, THE BULLNOSE EMERGENCY FLOOD LIGHT AT 5E AND FORWARD ENTRY AISLE EMERGENC Y EXIT SIGN LIGHT INOPERATIVE. ALL INOPERATIVE LIGHTS POWERED BY BATTERY PACK M730. REPLACED BATTERY PACK M730. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002061700135 20020617 00135 NM 2002 6 17 AALA20020758 1 20020526 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AA 27446 LAX - EMERGENCY LIGHTS SEAT ROWS 9DE THROUGH 23DEF TOO DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS SEAT ROWS 9DE TH ROUGH 23DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002061700136 20020617 00136 WP 2002 6 17 AALA20020760 1 20020524 A 1430 BOLT DOUG DC9 DC983 3022083 WP APU LOOSE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 439AA 49457 BOS - FLT 509 - EN ROUTE BOS-ORD, AFTER TAKEOFF THERE WAS SMOKE IN THE CABIN, THEN IN COCKPIT. DECLARED EMERGENCY. SMO KE STAYED. RETURNED BOS AND LANDED WITHOUT INCIDENT. TIGHTENED BOLT ON APU MASTER CHIP DETECTOR. PERFORMED COMPLETE P ACK BURN. REPLACED COALESCER BAGS AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002061700137 20020617 00137 WP 2002 6 17 MEX2002075 1 20020320 A 2781 SENSOR DOUG DC9 DC983 3022083 WP L/E SLAT FAILED A ASMF D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 23 838AM 49397 FLT 429 - MIA-MEX - AIRCRAFT RETURNED TO RAMP AS CONSEQUENCE OF SLAT DISAGREE LIGHT COMES ON STEADY DURING TAXI. SLATS OPERATION WAS CHECKED, THE RIGHT AND LEFT PROXIMITY SWITCH CIRCUIT BREAKER WAS RESET AND WAS PERFORMED A BITE TO THE STA LL WARNING COMPUTER GIVING A FAIL IN THE ALFA VANE SENSOR AND SLAT INDICATION. THE SYSTEM WAS RESET AND THE FAIL CAME R IGHT, TESTS OK IAW MM 27-40-00. (M) 2 L 7 2 4F RT A6WE 2002061700138 20020617 00138 EU 2002 6 17 SIMA200211601 1 20020426 A 3350 3013017 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 550LL 550 MIA - FLT 5021 - CREW REPORTED CABIN INTERIOR EMERGENCY LIGHTING TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E AFT POWER SUPPLY UNIT IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061700139 20020617 00139 EU 2002 6 17 SIMA200212127 1 20020417 A 5311 S53671311200 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2, FOUND FRAME 36 JUST ABOVE SERVICE DOOR SILL PLATE CORRODED. REPAIRED FRAME IAW SRM 53-61-40. AIRCR AFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061700140 20020617 00140 EU 2002 6 17 SIMA200212128 1 20020418 A 5315 S5367240220000 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2 FOUND FLOORBEAM 30 CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061700141 20020617 00141 EU 2002 6 17 SIMA200212131 1 20020418 A 5320 S5367800820001 SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2, FOUND LEFT Z-MEMBER BETWEEN 39-40 IN LAVATORY IS CORRODED. REMOVED AND REPLACED LEFT Z-MEMBER BETWE EN FRAME 39-40 IAW ATR SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061700142 20020617 00142 EU 2002 6 17 SIMA200212132 1 20020420 A 5320 S5367121729801 SILL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2, FOUND PASSENGER DOOR SILL DRAIN TRACK IS CORRODED. REMOVED AND REPLACED PASSENGER DOOR SILL DRAIN T RACK IAW ATR 42 SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061700143 20020617 00143 EU 2002 6 17 SIMA200212133 1 20020425 A 5320 S5367131182001 SILL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2, FOUND SERVICE DOOR SILL PLATE TO BE CORRODED. REMOVED AND REPLACED SILL PLATE IAW SRM 51-25-02 AND 51-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061700144 20020617 00144 EU 2002 6 17 SIMA200212134 1 20020425 A 5320 CLIP AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2, FOUND SHEAR CLIP ON AFT SIDE OF FRAME 37 CORRODED. REMOVED AND REPLACES SHEAR CLIP IAW SRM 51-25-01 . AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061700145 20020617 00145 SO 2002 6 17 SIMA200213801 1 20020514 A 5315 14521721009 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - DURING AN IMBV MAINTENANCE, FOUND CORROSION ON FORWARD DIGITAL. REMOVED CORROSION BY CUT OUT. FABRICATED A REPLA CEMENT STRAP, TWO DOUBLERS AND SHIMS. REPAIRED IAW EMB 145 (SRM 145/1142 CHAPTER 53, REV 18) 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002061700146 20020617 00146 SO 2002 6 17 SIMA200213804 1 20020511 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - DURING AN IMV MAINTENANCE, FOUND CORROSION ON LEFT OMEGA BEAM, PREVIOUS REPAIR, AT FRAME 20. REMOVED PREVIOUS REP AIR (CORROSION LIMITED TO PREVIOUS REPAIR). FABRICATED A DOUBLER ANGLE AND SHIMS AND FILLERS. REPAIR DONE IAW EMB145 ( SRM 145/1142, CHAPTER 53, REV 17) 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002061700147 20020617 00147 WP 2002 6 17 MWEA020405 1 20020617 A 5311 99118778 FRAME DOUG DC9 DC932 3022066 WP STATION 1132 A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CANTED FRAME STATION 1132 FRAME IS CRACKED AND CORRODED APPROXAMITLY 8 INCHES RIGHT OF UPPER FUSELAGE CENTERLINE. -- R EMOVED DAMAGE FRAME SECTION. FABRICATED FILLERS AND STACKED ANGLES. 2 L 7 2 4F A6WE 2002061700148 20020617 00148 WP 2002 6 17 MWEA020406 1 20020617 A 5312 991224645 SHEAR TIE DOUG DC9 DC932 3022066 WP STATION 1038 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT ACCESSORY COMPARTMENT BULKHEAD FRAME STATION 1038 SHEAR TIE IS CRACKED JUST ABOVE LONGERON 18 LEFT. -- REMOVED SH EAR TIE SEGMENT. FABRICATED AND INSTALLED SHEAR TIE SEGMENT AND CLIPS. 2 L 7 2 4F A6WE 2002061800001 20020618 00001 EA 2002 6 18 CA020523003 1 20020518 A 2710 CONTROL CABLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE AILERONS DIRTY W O OTHER F FLT CONT AFFECTED CL CLIMB 1 CA 20067 (CAN) CLIMBING THROUGH 23000 FT THE AILERONS BECAME STIFF AT -22C . AUTOPILOT MANUALLY DISCONNECTED . AILERON TRIM MOVED BUT YOKE DID NOT. CONTROL RETURNED AT 20000 FT AND +4C . AIRCRAFT LANDED WITHOUT INCIDENT. LT & RT TENSION REGULATORS I NSPECTED FOR MOISTURE, NO MOISTURE FOUND. LT & RT AFT AILERON QUADS AND AUTOPILOT INSPECTED FOR MOISTURE , NO MOISTURE F OUND BUT THE AREA WAS DIRTY. LT & RT AFT QUADS AND OUTPUT ENDS OF THE PCU'S WHERE CLEANED WITH ALCOHOL AND DRIED WITH NI TROGEN. NO PARTS WHERE REPLACED.AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061800002 20020618 00002 EA 2002 6 18 CA020523004 1 20020518 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) IN CRUISE AT FL390, RIGHT WINDSHIELD CRACKED. FLIGHT DIVERTED TO BERLIN.WINDSHIELD REPLACED AND AIRCRAFT RETURNED IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061800003 20020618 00003 SW 2002 6 18 CA020523005 1 20020506 A 2435 23063371 SEAL BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL STARTER GEN TORN W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) STARTER/GENERATOR OIL SEAL LIPS TEARING AFTER INSTALLATION AND SHORT TIME USE. 2 SEALS AEPLACED AFTER 1 HOUR FLIGH T DUE TO SEAL TORN. ENGINE CEB1388 COMPLETED ON LAST ONE. NO FURTHER FAULT. 1 G 7 1 3U 3 U H2SW E4CE 2002061800004 20020618 00004 NM 2002 6 18 CA020523006 1 20020514 A 7921 20008A HOUSING ROBSIN R22 R22BETA 7640110 NM LYC O320 O320B2C 41508 EA OIL COOLER CRACKED W E ENGINE SHUTDOWN K FLUID LOSS TX TAXI/GRND HDL 1 CA (CAN) SMALL CRACK ON OUTSIDE OF OIL COOLER HOUSING CLOSE TO THE CENTRE. NOTED SMALL DROPS OF OIL FORMING ON EXTERIOR OF ENGINE OIL COOLER. 1 G 7 1 3O 3 O H10WE E274 2002061800005 20020618 00005 CE 2002 6 18 CA020523007 1 20020522 A 5311 FRAME BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11484 (CAN) FUSELAGE LT FRAME AT STATION 167.625 STRINGER 9 CRACKED. TO BE REPAIRED PRIOR TO FURTHER FLIGHT. 1 L 7 2 4T 4 T A24CE E4EA 2002061800006 20020618 00006 CE 2002 6 18 CA020523008 1 20020522 A 5311 FRAME BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11484 (CAN) FUSELAGE LT FRAME AT STATION 158.00 STINGER 9 CRACKED. TO BE REPAIRED PRIOR TO FURTHER FLIGHT. 1 L 7 2 4T 4 T A24CE E4EA 2002061800007 20020618 00007 SO 2002 6 18 CA020523009 1 20020522 A 7500 4562150 CLAMP EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA BLEED AIR SYS LOOSE W O OTHER F FLT CONT AFFECTED DE DESCENT 1 CA (CAN) PILOT REPORTED THAT FLAPS WOULD NOT OPERATE WHEN SELECTED. MAINTENANCE CONFIRMED THE SNAG ON THE RAMP. INVESTIGATI ON REVEALED THAT THE AREA AROUND THE FLAP PROTECTION BOX, FLAP MOTOR AND ASSYMETRIC ASSEMBLY WAS VERY WARM. THESE ITEMS ARE LOCATED UNDER THE CABIN FLOOR. FURTHER INVESTIGATION REVEALED THAT THE ABOVE BLEED AIR CLAMP WAS LOOSE AND THE GASKE T IN THE BLEED AIR LINE HAD BLOWN AWAY CAUSING HOT BLEED AIR TO SPILL ONTO THE FLAP PROTECTION UNIT CAUSING THE OVERHEAT PROTECTION CIRCUIT TO SHUT DOWN FLAP OPERATION. GASKETS WERE REPLACED, CLAMPS TIGHTENED AND OPERATION RETURNED TO NORMA L. 1 L 7 2 4T 4 T A21SO E4EA 2002061800008 20020618 00008 EA 2002 6 18 CA020523010 2 20020510 A 7230 BLADE BOMBDR DHC8 DHC8402 NM PWC 150 PW150A EA COMPRESSOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AFTER LANDING PILOT NOTICE A LOT OF SCRATCH ON ALL PROP BLADES. PAX REPORTED IMPACT NOISE ON FUSELAGE DURING LAND ING & TAKEOFF AT PREVIOUS AIRPORT. PILOT REPORT RWY WERE COVERED BY MELTED SNOW & WATER. COMPLETED A/C INSPECTION CUTO UT. ALL PROP BLADE LIGHT DAMAGE REPLACED IAW DOWTY MCTE MANUAL. COMPLETED BORESCOPE INSP. C/OUT ON BOTH ENGINE. FOUND LIGHT DAMAGE ONLY ON RT 1ST STAGE COMPRESSOR, REPAIRED. A/C FUSELAGE, MANY DAMAGE FOUND ON RT SIDE FROM STATION 560 TO 820 & LT SIDE FROM 260 TO 500 WITHIN LIMITS IAW SRM AFTER SMALL REWORK. CLOSE TO 60 DAMAGES FOUND ON FUSELAGE ON THOSE LOCATION REQUIRED WITHIN 800 FLTS IAW SRM. ONLY ONE REQUIRED PERMANENT REPAIR BEFORE FLIGHT. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061800009 20020618 00009 WP 2002 6 18 CA020523011 1 20020508 A 6210 500P2100101 BLADE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL MAIN ROTOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING 100 HOUR INSPECTION A "TONAL" DIFFERENCE WAS NOTED ON THE MAIN ROTOR BLADE IN THE AREA CALLED OUT IN SEC.90 OF THIS SNEET ABOUT 1/4 INCH AFT OF THE LEADING EDGE ON THE UPPER SURFACE. DUE TO NUMEROUS PREVIOUS PROBLEMS WITH THIS MANUFACTURER (HTC) 1 G 7 1 3U 3 U H3WE E4CE 2002061800010 20020618 00010 SW 2002 6 18 CA020523012 1 20020514 A 2750 19023 CONTROL CABLE BBAVIA 8 8GCBC 1220803 SW LYC O360 O360C2A 41514 EA RT & LT FLAPS FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LT AND RT FLAP UPPER CABLES FRAYED AT WING ROOT PULLEYS. 1 H 7 1 3O 3 O A21CE E286 2002061800011 20020618 00011 SW 2002 6 18 CA020523013 1 20020516 A 2750 19023 CONTROL CABLE BBAVIA 8 8GCBC 1220803 SW LYC O360 O360C2E 41514 EA LT TE FLAP FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LT UPPER FLAP CABLE FAYED AT WING ROOT PULLEY ON SECOND NOTCH OF FLAP. 1 H 7 1 3O 3 O A21CE E286 2002061800013 20020618 00013 GL 2002 6 18 CA020523015 2 20020508 A 7230 23007217 MOUNT ALLSN BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL COMPRESSOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 70505 (CAN) AT THE 100 HOUR ENGINE INSPECTION A CRACK WAS FOUND AT THE 6 O'CLOCK POSITION, ON THE COMPRESSOR MOUNT ASSEMBLY, A DJACENT TO THE HOLE APPROXIMATELY 1 1/2 INCHES LONG. 1 G 7 1 3U 3 U H2SW E1GL 2002061800015 20020618 00015 CE 2002 6 18 CA020524001 1 20020522 A 2130 99120264 DUCT HAMLTN 738834 CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE ACM DISCONNECTED W B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CA 910513 (CAN) AIRCRAFT AT 28,000 FT HAD LOSS OF CABIN PRESSURE CONTROL. AIRCRAFT EXECUTED EMERGENCY DESCENT TO 10,000 FT PROCEED ING TO DESTINATION WITHOUT FURTHER INCIDENT. MAINTENANCE INVESTIGATION REVEALED ACM FLEX DUCT HAD UNCOUPLED FROM MATING TUBE, SUSPECTED CAUSE OF THE DECOUPLING WAS A LOOSE GEAR CLAMP. 1 L 7 2 4F 4 F A22CE E1NE 2002061800016 20020618 00016 NM 2002 6 18 CA020524002 1 20020518 A 3233 10500103 ACTUATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG RUPTURED W O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA 31213 12923 (CAN) AIRCRAFT ON FLT EN ROUTE ON APPROACH AFTER A GEAR DOWN SELECTION CAPTAIN AND FIRST OFFICER NOTED THAT THE NR 2 HYD SYS CAUTION LIGHTS ILLUMINATED AND QTY GAUGE FOR THE NR 2 HYD SYSTEM INDICATED ZERO, THE AIRCRAFT LANDED WITHOUT INCID ENT. AFTER INITIAL INSPECTION OF THE AIRCRAFT IT WAS FOUND THAT THE NR 1 MAIN LANDING GEAR RETRACTION ACTUATOR HAD RUPTU RED THE FULL LENGTH OF THE HOUSING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061800017 20020618 00017 NE 2002 6 18 CA020524004 2 20020505 A 7200 CF343B1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT OVERTEMP W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON LANDING LT ENGINE OVERTEMP TO 998 FLASHING (HOT), AT GATE SHUTDOWN. MDC SHOWS ENGINE WENT TO 1165 DEGREES FOR 22 SECONDS. THIS AIRCRAFT JUST HAD LT ENGINE REPLACED ON 5/5/02, THE ORIGINAL ENGINE WAS REMOVED DUE TO COKING PROBLEMS . THE AIRCRAFT AFTER THE ENGINE CHANGE FLEW. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061800018 20020618 00018 EA 2002 6 18 CA020524005 1 20020517 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 21168 (CAN) LT WINDOW CRACKED DURING FLIGHT. DIVERTED FLIGHT. LEFT SIDE WINDOW REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061800020 20020618 00020 EA 2002 6 18 CA020524007 1 20020514 A 3250 89681 ACTUATOR DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NLG STEERING FAILED W D RETURN TO BLOCK D INFLIGHT SEPARATION TX TAXI/GRND HDL 1 CA 25016 (CAN) SUSPECT STOP ON END OF STEERING ACTUATOR LINK FAILED ALLOWING LINK TO PULL OUT CAUSING DAMAGE TO OTHER PARTS OF TH E NOSE GEAR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061800021 20020618 00021 NE 2002 6 18 CA020527003 2 20020517 A 7200 ENGINE LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NR 3 VIBRATION W E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CA (CAN) ENGINE NR 3, AT 22 000 FT, THE VIB. CHANNEL A + B , 2.6 TO 2.8 UNITS. ENGINE SHUT DOWN WAS CARRIED OUT PER QRH. A T TAKE OFF , THE VIB. WAS AT 2.0 TO 2.2 UNITS. ON CLIMB THE VIB. WAS 1.9 UNITS (BOTH CHANNELS), DID NOT APPEAR TO BE LIN EAR WITH THROTTLE MOVEMENT. MAINTENANCE CARRIED OUT A BOROSCOPE ON THE HP & TURBINE COMPRESSORS, INSPECTED THE MAGNETIC CHIP DETECTORS AND FILTERS AND NO FAULTS FOUND. THE ENGINE WAS REPLACED FOR COMPANY CONVENIENCE WITH. 2 L 7 3 4F 4 F A23WE E12EU 2002061800022 20020618 00022 WP 2002 6 18 CA020527004 1 20020516 A 5414 1615155103 ACCESS PANEL LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE NR 1 NACELLE DEPARTED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON ARRIVAL AT DESTINATION, FOUND INBOARD OF NR 1 ENGINE, INSPECTION PANEL (BLOW OUT), MISSING ( BROKEN AT HINGE LE VEL, REFERENCE IPC 57-33-10,ITEM 272). MAINTENANCE INSPECTED THE LT LOWER WING LEADING EDGE ACCESS AND NO DAMAGE FOUND. A LEAK CHECK WAS CARRIED OUT ON THE BLEED AIR DUCT AND NO LEAK FOUND. MAINTENANCE REPLACED THE PANEL. 2 L 7 3 4F 4 F A23WE E12EU 2002061800023 20020618 00023 SO 2002 6 18 CA020527005 1 20020514 A 5512 4650037 SKIN PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA HORIZONTAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 17101 (CAN) UPON INSPECTION THE RT HORIZONTAL STAB WAS FOUND TO BE CRACKED AT THE BOTTOM, OUTBOARD, AFT BOLT ATTACHMENT HOLE. THE STAB WAS REPLACED AND SENT FOR REPAIR. 1 L 7 2 3T 4 T A8EA E4EA 2002061800024 20020618 00024 WP 2002 6 18 CA020527007 1 20020519 A 2913 346931 SHAFT VICKERS 3508807 LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE HYD PUMP SHEARED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA MX463684 (CAN) 'D1' HYD SYSTEM PRESSURE AT 0 PSI WITH SWITCH LATCHED IN LOW PRESSURE LIGHT ON . NO HYD QUANTITY LOSS, NO HIGH T EMP 'CD' PTU SELECTOR TO BRING SYSTEM PRESSURE BACK TO 3000 PSI. D1 PUMP OFF. D SYSTEM ENG DRIVEN PUMP REMOVED AND FOUN D SHAFT SHEARED. PUMP REPLACED AS PER M/M. 2 L 7 3 4F 4 F A23WE E12EU 2002061800025 20020618 00025 EU 2002 6 18 CA020527008 1 20020419 A 2520 RDAX4431 ELECTRICAL BOX AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE PAX SEAT OVERHEATED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) DURING LEVEL FLIGHT AN ELECTRICAL BURNING ODOUR (ACRID SMELL) CAME FROM SEAT ROW 1-3 LEFT.AIRCRAFT DIVERTED AS A P RECAUTION. COMPLETE INSPECTION OF ROW 1-5 LEFT CARRIED OUT WITH NO OBVIOUS FAULTS WITH WIRING. SEB (SEAT ELECTRONIC BOX ) FOR SEATS 2ABC FOUND HEAT DAMAGED. NEW SEB INSTALLED AND OPERATION CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E29NE 2002061800027 20020618 00027 EA 2002 6 18 CA020527010 1 20020514 A 3246 6A02362007 FITTING DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE MLG FLOAT BROKEN W L ABORTED APPROACH O OTHER DE DESCENT 1 CA (CAN) ROUGH WATER LANDING - RT FORWARD FLOAT DECK FITTING FLYWIRE ATTACHMENT BROKE AT LOWER PIN LOCATION CAUSING FLYWIRE TO BREAK FREE FROM ITS ATTACHMENT. THESE ARE OLD TYPE DECK FITTINGS. DATE OF MANUFACTURE OF FLOATS JULY 1986. 1 H 7 1 3R 3 R A806 5E1 2002061800028 20020618 00028 CE 2002 6 18 CA020527011 1 20020516 A 3213 5081032019 SOCKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG STRUT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION OF MLG LOWER SOCKETS THEY WHERE FOUND TO BE CRACKED AS PER COMMUNIQUE NR 27 DATED FEB 1993. BLE NDING IS ALLOWED UP TO .050 INCH BUT DUE TO LOW HOURS SINCE NEW THEY WHERE SENT TO AN OVERHAUL FACILITY FOR EVALUATION O F REPAIR OR REPLACE. 2 L 7 2 4T 4 T RT A24CE E26NE 2002061800029 20020618 00029 NE 2002 6 18 CA020528001 2 20020330 A 7261 O-RING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE SCAVENGE PUMP DAMAGED W E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA 13771 (CAN) DURING APPROACH, MESSAGE RT ENG OIL PRESS (W) ALONG WITH RED PRESSURE INDICATION ON EICAS. RT ENGINE WAS SHUT DOW N AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE NOTICE AN HYDRAULIC LEAK COMING FROM THE ENGINE OIL AND SCAVENGE PUMP FLAN GE. THE PUMP O'RING WAS REPLACED AND THE SYSTEM TESTED SATISFACTORY. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061800030 20020618 00030 EA 2002 6 18 CA020528002 2 20020514 A 7261 LINE PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA OIL PRESSURE CORRODED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 11161 (CAN) ON INSPECTION, OIL WAS FOUND ON BOTTOM OF AIRCRAFT FUSELAGE. ON REMOVED OF FLORR PANELS, AN OIL PRESSURE LINE FOR THE LT ENGINE WAS FOUND PERFORATED DUE TO CORROSION. THE LINE WAS REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 2002061800031 20020618 00031 EA 2002 6 18 CA020528004 2 20020508 A 7230 BLADE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA COMPRESSOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A ROUTINE INSPECTION MAINTENANCE DISCOVERED THE RT INBOARD INERTIA VANE LINKAGE HAD COME APART. THE RETAINI NG PIN AND ROD WERE NOT FOUND. UPON INSPECTION OF FIRST STAGE COMPRESSOR ONE BLADE HAD TWO NICKS. IT IS SUSPECTED THAT T HE RETAINING PIN WAS INGESTED INTO THE COMPRESSOR. THE COMPRESSOR BLADE WAS REPAIRED IN ACCORDANCE WITH PT6A-65 MAINTENA NCE MANUAL. THE INERTIA VANE LINKAGE WAS REPLACED. A RECENT SAFETY COMMUNIQUE NR 195 FOR MODEL 1900D ADDRESSES THIS SUBJ ECT. AIR LABRADORS TWO 1900D AND ONE 1900C AIRCRAFT HAVE BEEN INSPECTED. 2 L 7 2 4T 4 T RT A24CE E4EA 2002061800032 20020618 00032 NM 2002 6 18 CA020528005 1 20020516 A 7500 652244131 DUCT BOEING 737 737297 1384480 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE RUPTURED W A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) SHORTLY AFTER TAKEOFF CREW OBSERVED NR 1 ENGINE OVERHEAT - WHEN POWERLEVER RETARDED, IND. EXTINGUISHED. WHEN POWER LEVER FOR NR 1 ENGINE ADVANCED, OVERHEAT WARNING ILLUMINATED. CREW DECLARED EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDE NT. CFR ON STANDBY. MAINT INSPECTION REVEALED NR 1 ENGINE OUTBOARD BLOWOUT PANEL FOUND OPEN & SUPPORT CABLE SEVERED. FURTHER INSPECTION REVEALED UPPER 13TH STAGE CROSS OVER DUCT RUPTUED. A WIRE TO UPPER FIRE LOOP SEPARATED & ALL PLASTIC /RUBBER SUPPORT FITTINGS AFT OF DUCT WERE HEAT DAMAGED. THRUST REVERSER FOLLOWUP CABLE ALSO DAMAGED. MAINT REPLACED & RE SECURED FIRE LOOP POWER WIRES, REPLACED ALL NON-AIRWORTHY PLASTIC STANDOFFS/CLAMPS FROM 13TH STAGE DUCT. 2 L 7 2 4F 4 F A16WE E2EA 2002061800033 20020618 00033 EU 2002 6 18 CA020528007 1 20020527 A 2823 B97E51655 SHUTOFF VALVE AIRBUS 310 A310 EU GE CF6 CF680C2A5 NE FUEL SYSTEM CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 38447 (CAN) FUEL SHUTOFF VALVE, DURING 8C CHECK RT ENGINE LOWERED TO ALLOW FOR MOUNT BOLT REPLACEMENT & CORROSION REPAIR. ON REINSTALLED ENGINE INTERNAL & EXTERNAL LEAK CHECK OF LP FUEL FIRE SHUTOFF VALVE REQUIRED PER J/C 71-400-001-2. FUNCTION CHECK REVEALED THAT VALVE LEAKING INTERNALLY. WHEN VALVE REMOVED OUTLET FLANGE OF VALVE FOUND TO HAVE SEVERE EXFOLIATIO N CORROSION TO POINT OF CREATING PINHOLE THROUGH FLANGE. DUE TO FINDING IT DECIDED TO CARRY OUT DETAILED VISUAL INSP OF LT FUEL SHUTOFF VALVE. INSPECTION AGAIN SHOWED EVIDENCE OF CORROSION. UPON REMOVAL OF VALVE OUTLET FLANGE FOUND TO HAV E SEVERE EXFOLIATION CORROSION. 2 L 7 2 4F 4 F RT A35EU E13NE 2002061800034 20020618 00034 EU 2002 6 18 AWXA200200489 1 20020601 A 3610 FILTER AIRBUS 320 A320231 3930325 EU BLEED AIR SYS CLOGGED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 627AW 11520 66 ON CLIMBOUT, CREW RECEIVED ECAM MESSAGE FOR NR 1 ENG BLEED FAULT; BLEED TEMP REACHED 280 DEGREES & CROSSFEED VALVE OPENE D; ACFT TURNED BACK TO PHX. MX REPLACED THE FAN AIR THERMOSTAT AND OPERATIONALLY CHECKED OUT SYS BY RUNNING ENG FOR AN EXTENDED PERIOD OF TIME AT POWER, CHECK GOOD. SYS WAS PREVIOUSLY PLACED ON MEL 36-11-04 COND. NR 1 FAN AIR VALVE INOPE RATIVE FOR SIMILAR EVENT OCCURRED 04/28/2002. NR 1 ENG FAN AIR VALVE REPLACED. VENDOR BENCH TEST REPORT FOR FAN AIR VA LVE, NO FAULT FOUND. VENDOR TEAR DOWN OF TEMP CONTROL THERMOSTAT CONFIRMED FAILURE. PROBLEM IDENTIFIED AS FILTER CLOGG ED BY POLLUTION. FILTER CLEANED, A PRESSURE REDUCING CLAPPER GUIDE & PACKING SEAL WERE REPLACED. 2 L 7 2 4F RT A28NM 2002061800035 20020618 00035 NM 2002 6 18 CA020528008 1 20020523 A 3246 29685 BEARING DHAV DHC8 DHC8* NM PWC 150 PW150A EA MLG WHEEL COLLAPSED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) A/C RETURNED TO STAND AFTER 2 REJECTED TAKEOFFS DUE TO ANTI-SKID OUTBOARD WARNING ILLUMINATED. NOTED SMOKE COMING FROM NR 1 MAINWHEEL HUB. INSPECTION REVEALED LUGS ON INBOARD FACE OF MAINWHEEL SHINNING DUE TO CATCHING & CLIPPING SOME THING. A/C JACKED TO REVEAL INNER BEARING COLLAPSED & DISINTERTATED. EXTENSIVE DAMAGE TO WHEEL ASSY, AXLE, BRAKE UNIT & TRANSDUCER DRIVE (HUBCAP). HEAT DAMAGE TO TRANSDUCER & WIRING. DUE TO SIGNS OF OVERHEATING (BLUEING) & DAMAGE. LT AXLE ASSEMBLY REPLACED. NR 1 MAINWHEEL, BRAKE UNIT, ANTI-SKID TRANSDUCER & WIRING REPLACED. NR 1 MAIN WHEEL REPLACED DUE TO OVERHEATED BEARING. INSP OF NR 3 & 4 MAINWHEELS DUE TO HOT ON 1ST TRANSIT REVEALED OVERHEATED/DAMAGED BEARINGS NR 3 & 4 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061800036 20020618 00036 2002 6 18 CA020528009 4 20020516 A 3417 HG2030AD09 ADC AIRBUS A319 A319114 3930350 NM CFMINT CFM56 CFM565A1 NE COCKPIT MALFUNCTIONED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) MULTIPLE RED, AMBER WARNING AND CAUTION MESSAGES: GRNG PROX WARNING, AIR DATA INERTIAL REFERENCE, INERTIAL REFEREN CE INDICATORS AND NAV & PRIMARY FLIGHT DISPLAYS, WENT BLANK, NUMEROUS RED OVERSPEED WARNINGS, SLAT FLAP, AND FLIGHT CONT ROL MESSAGES. ALL OCCURED WITH AIRCRAFT ON GROUND WHILE WAITING FOR TAKE-OFF. AIRCRAFT RETURNED TO GATE.AIRDATA / INERTI AL REFERENCE UNIT REPLACED AS PER AMM 34-12-34-420-050 SYSTEM CHECKED SERVICEABLE 2 L 7 2 4F 4 F RT A28NM E29NE 2002061800037 20020618 00037 NM 2002 6 18 P5CA0200683 1 20020607 A 5420 WEB BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 3 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 702114 THREE CRACKS FOUND ON NR 3 ENG PYLON, AFT ENGINE MOUNT BULKHEAD FRAME, VERTICAL WEB STATION 221.9. (1. CRACK ON FRONT O F OUTBOARD WEB, 2 INCHES LONG. 2. CRACK ON FRONT OUTBOARD WEB, 1 INCH LONG. 3. CRACK ON FRONT OUTBOARD WEB, 3 INCHES LO NG). BULKHEAD LOWER ASSY REPAIRED BY INSTALLING WEB FILLERS, WEB DOUBLERS AND ANGLE CORDS ON LEFT AND RIGHT FRAME HALVE S IAW PAOE020524, DRAWING 65B07582, SHT 8, SB747-54-A2202 & SB747-54-2065. 2 L 7 4 4F 4 F A20WE E3NE 2002061800038 20020618 00038 NE 2002 6 18 HEEA079326 1 20020530 A 3000 SENSOR SKRSKY S76 S76A 8143006 NE HEATED BELLMOUNT INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 792CH 760193 TEMP SENSOR CIRCUIT IS INOPERATIVE. 1 G 7 2 3U H1NE 2002061800040 20020618 00040 NE 2002 6 18 HEEA079337 1 20020530 A 3150 7655001001103 PANEL SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122G 760232 NO ENGINE OUT INDICATION ON PILOTS 5 PACK. SCRAPPED. 1 G 7 2 3U H1NE 2002061800041 20020618 00041 EA 2002 6 18 QXEA0200864 1 20020611 A 3260 TARGET CNDAIR CL600 CL6002C10 1390015 EA NLG OUT OF ADJUST A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 609QX 10031 PDX- RETURNED TO FIELD, GEAR DISAGREE, MASTER WARNING-ACCOMPANIED BY PROX SYSTEM FAULT 1 STATUS MESSAGE. AIRCRAFT LANDE D WITHOUT INCIDENT. ADJUSTED NOSE LANDING CENTER TARGETS. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A21EA 2002061800042 20020618 00042 NM 2002 6 18 QXEA0200865 1 20020608 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX- AT FUSELAGE STATION 140.359 TO 144.86 THERE ARE 3 PITS IN SKIN BETWEEN STRINGERS 23RT AND 28RT. REPAIRED IAW HORIZ ON AIR EA 2-53-398. 2 H 7 2 4T RT A13NM 2002061800043 20020618 00043 NM 2002 6 18 QXEA0200866 1 20020608 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX- AT FUSELAGE FRAME 123.9 TO 131.354 THERE ARE 3 PITS IN SKIN BETWEEN STRINGERS 23RT AND 28RT. REPAIRED IAW HORIZON AIR EA 2-53-398. 2 H 7 2 4T RT A13NM 2002061800044 20020618 00044 NM 2002 6 18 QXEA0200867 1 20020608 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX- AT FUSELAGE FRAME 204.0 THERE IS A .004 INCH PIT IN SKIN BETWEEN STRINGER 23RT AND 28RT. REPAIRED IAW HORIZON AIR EA 2-53-398. 2 H 7 2 4T RT A13NM 2002061800045 20020618 00045 NM 2002 6 18 QXEA0200868 1 20020607 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX- AT FUSELAGE SKIN 120.86 BETWEEN STRINGER 23RT AND 28RT THERE IS A .0025 INCH PIT IN THE SKIN. REPAIRED IAW DHC-8 S RM 51-20-11. 2 H 7 2 4T RT A13NM 2002061800046 20020618 00046 WP 2002 6 18 ZW0A0206301 1 20020613 A 3350 MS2721263 TERMINAL DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 9627R 53597 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 26 AFT. REPLACED TERMINAL BOARD THAT MAY HAVE BEEN ACCIDENTLY KICKED BY A P ASSENGER. CHECK-C 11-16-01 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2002061800047 20020618 00047 NM 2002 6 18 QXEA0200869 1 20020607 A 5522 SKIN DHAV DHC8 DHC8202 2809007 NM ELEVATOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX- RIGHT HAND ELEVATOR OUTBOARD TRAILING EDGE HAS DAMAGE NEAR OUTBOARD STATIC WICK. REPAIRED IAW DHC-8 RD 8-55-938. 2 H 7 2 4T RT A13NM 2002061800048 20020618 00048 NM 2002 6 18 QXEA0200870 1 20020608 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX- AT FUSELAGE FRAME 210.0 THERE IS A .025 PIT IN SKIN BETWEEN STRINGERS 23RT AND 28RT. REPAIRED IAW HORIZON AIR EA 2 -53-398. 2 H 7 2 4T RT A13NM 2002061800049 20020618 00049 NM 2002 6 18 QXEA0200871 1 20020608 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX- AT FUSELAGE FRAME 149.0 TO 165.4 THERE ARE 4 PITS IN SKIN BETWEEN STRINGERS 23RT AND 28RT. REPAIRED IAW HORIZON AI R EA 2-53-398. 2 H 7 2 4T RT A13NM 2002061800050 20020618 00050 NM 2002 6 18 QXEA0200872 1 20020608 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX- AT FUSELAGE SKIN THERE IS A .004 INCH PIT IN SKIN BETWEEN STRINGER 23RT AND 28RT. REPAIRED IAW HORIZON AIR EA 2-53 -398. 2 H 7 2 4T RT A13NM 2002061800051 20020618 00051 EU 2002 6 18 02FDEA00409 1 20020618 A 5532 SKIN AIRBUS 310 A310 EU VERTICAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 WIDESPREAD CORROSION ON FUSELAGE SKIN ON THE OUTBOARD SIDES OF THE VERTICAL STAB LT & RT ATTACHMENT. R/R ALL TRACES OF CORROSION. 2 L 7 2 4F RT A35EU 2002061800052 20020618 00052 EU 2002 6 18 RAIA00206175 1 20020606 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 550HK 41039 STL- EMERGENCY PATH LIGHTS OUT ROWS 3 THROUGH 5. SECURED PATH LIGHT CONNECTOR. 2 L 7 2 4T RT A41NM 2002061800053 20020618 00053 EU 2002 6 18 02FDEA00408 1 20020618 A 5400 PYLON AIRBUS 310 A310 EU N/A CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 CRACK FOUND ON HOLE #7 AND #6 ON OVERWING REFUEL APARTURE. ** S/D ** COMING 2 L 7 2 4F RT A35EU 2002061800054 20020618 00054 SW 2002 6 18 HEEA079427 1 20020528 A 6320 204040760003 FILTER BELL 412 412 1182202 SW GEARBOX OIL BYPASSING E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2149S 36002 ENGINE OIL FILTER BYPASSED AFTER FILTER CHANGE. 1 G 7 2 4U H4SW 2002061800055 20020618 00055 SO 2002 6 18 SWIA200210817 1 20020424 A 3233 ACTUATOR EMB 120 EMB120ER 3260203 SO RT MLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 235SW 5414 5414 120310 RIGHT MAIN GEAR WILL NOT RETRACT. RED -A- AND -B- LIGHTS ILLUMINATED. RIGHT MAIN LANDING GEAR WILL NOT RETRACT, SHOWIN G A & B DISAGREEMENT LIGHTS. GEAR CAME UP AFTER SECOND CYCLING AND A SHORT DELAY. REPLACED RIGHT MAIN GEAR INBOARD FOR WARD DOOR SEQUENCE VALVE DUE TO STICKING. OPS CHECKED GOOD DURING GEAR SWING. INSTALLED SERVICEABLE RIGHT MAIN GEAR AC TUATOR. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002061800056 20020618 00056 SO 2002 6 18 SWIA200210819 1 20020427 A 5280 DOOR EMB 120 EMB120ER 3260203 SO NLG UNLATCHED A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 268UE 120207 VIBRATION IN NOSE AFTER TAKEOFF. FOUND LEFT NOSE GEAR DOOR UNLATCHED FROM HOOK. SECURED LEFT GEAR DOOR. NO DAMAGE TO DOOR OR HOOK. OK FOR RETURN TO SERVICE. 2 L 7 2 4T RT A31SO 2002061800057 20020618 00057 SW 2002 6 18 HEEA079540 1 20020528 A 6320 BEARING BELL 412 412 1182202 SW G/B CASE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L TI292 33006 MAIN ROTOR GEARBOX LIFT LINK ASSY HAS WORN BEARINGS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061800058 20020618 00058 SW 2002 6 18 HEEA079551 1 20020528 A 6520 212040004009FM GEARBOX BELL 412 412 1182202 SW TAIL ROTOR VIBRATION E HEEA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SW 03 142PH 21326 33150 TAIL ROTOR GEARBOX HUM DETECTED. ABNORMALITY ON OUTPUT GEAR. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061800059 20020618 00059 SW 2002 6 18 HEEA079555 1 20020528 A 6320 212040233001 LINE BELL 212 212 1181420 SW M/R GEARBOX CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736D 31135 MAIN ROTOR GEARBOX HAS A CRACKED LINE. REPAIRED LINE. 1 G 7 1 4U H4SW 2002061800060 20020618 00060 SW 2002 6 18 HEEA079556 1 20020528 A 6320 212040243001 LINE BELL 412 412 1182202 SW M/R GEARBOX CHAFED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 2148K 36001 MAIN ROTOR LINE CHAFED. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002061800061 20020618 00061 2002 6 18 SWIA200210820 4 20020427 A 3425 COMPUTER EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 297SW 120327 ON CLIMBOUT RECEIVED A FIRST OFFICER HEADING FLAG ACCOMPANIED BY ATT DISPLAY MAP LIGHT AND INTERMITTENT TCAS FAIL. RETU RNED TO FAT. PERFORMED REINITIALIZATION OF FIRST OFFICER'S AHRS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002061800062 20020618 00062 EA 2002 6 18 SWIA200210821 1 20020427 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 587SW 7062 AFT PORTION OF FLOOR LEVEL EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHTING BATTERY PACK AND EM ERGENCY BATTERY INVERTER NR 4. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002061800063 20020618 00063 SO 2002 6 18 SWIA200210823 1 20020429 A 7722 CONNECTOR EMB 120 EMB120ER 3260203 SO LT ENGINE LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 LEFT T6 GAUGE ERRATIC AND INTERMITTENT ON BOTH THE DIGITAL AND ANALOG DISPLAYS. RETURNED TO SLC. FOUND LEFT ENGINE T6 CONNECTION LOOSE. RETORQUED NUTS AND COMPLIED WITH ENGINE RUN. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002061800064 20020618 00064 SO 2002 6 18 SWIA200210824 1 20020426 A 3260 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 189SW 120048 LEFT MAIN GREEN -B-' LIGHT NEVER WENT OFF DURING GEAR RETRACTION. UPON GEAR EXTENSION RED LEFT MAIN -B- LIGHT NEVER WEN T ON. RETURNED TO DEN. REPOSITIONED LEFT MAIN GEAR -B- DOWNLOCK HARNESS PROXIMITY SWITCH. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002061800065 20020618 00065 SO 2002 6 18 SWIA200210825 1 20020430 A 3231 DOOR EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJUST A SWIA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 07 301YV 120301 ON GEAR RETRACTION, LEFT INDICATION REMAINED RED IN EXCESS OF 12 SECONDS WITH SLIGHT VIBRATION. RETURNED TO PDX. ADJUS TED GEAR DOOR IAW MM 32-32-09 & 32-32-10 AND ADJUSTED TARGET IAW MM 32-61-01. SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD . 2 L 7 2 4T RT A31SO 2002061800066 20020618 00066 SO 2002 6 18 SWIA200210826 1 20020502 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 190SW 120050 IN CRUISE FLIGHT, FLAP LIGHT ON MAP PANEL ILLUMINATED ALONG WITH ADVANCED SWS LIGHT. FLAP INBOARD LIGHTS WERE ILLUMINAT ED. COMPLIED WITH QRH PROCEDURES. FLAPS WOULD NOT RESET. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. REPLACED ACTUATOR CANNON PLUG. OPERATED FLAPS SEVERAL TIMES, OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002061800067 20020618 00067 2002 6 18 HEEA079566 4 20020530 A 3442 80510800001 INDICATOR BELL 206 206L3 1182108 SW WX RADAR MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6603X 51412 AFTER 15 MINUTES OFF LIGHT SKYWATCH GIVES ERROR CODES. COULD NOT DUPLICATE PROBLEM. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 2002061800068 20020618 00068 SO 2002 6 18 SWIA200210827 1 20020429 A 3233 1959500007 ACTUATOR EMB 120 EMB120ER 3260203 SO RT MLG FAILED A SWIA A UNSCHED LANDING E F J VIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 235SW 3080 3080 120310 RIGHT MAIN GEAR RED DISAGREE LIGHTS ON WITH GEAR SELECTED UP. DOORS STAYED OPEN. COULD HEAR AND FEEL THE DRAG. REMOVE D AND REPLACED RIGHT MAIN GEAR ACTUATOR IAW EMB 120 MM 32-32-10 AND ADJUSTED SEQUENCE VALVE IAW EMB 120 MM 32-32-01. 2 L 7 2 4T RT A31SO 2002061800069 20020618 00069 2002 6 18 HEEA079785 4 20020530 A 3452 066106200 TRANSCEIVER BOLKMS 117 BK117A1 5626010 EU ATC MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 217UC 7152 ATC TRANSCEIVER INOPERATIVE. CLEANED ON/OFF SWITCH CONTACTS. STRAIGHTENED BENT CONTACTS ON ON/OFF SWITCH. REPAIRED PRO BLEM. FOUND POWER OUT WEAK. REPLACED BAD V101 CAVITY. ADJUSTED PULSE WIDTH, POWER OUT AND FREQUENCY. REPAIRED. BENC H CHECK GOOD. 1 G 7 2 3U H13EU 2002061800070 20020618 00070 SO 2002 6 18 SWIA200210828 1 20020505 A 2731 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 562SW 120336 ABORTED TAKEOFF IN SFO DUE TO RED FLASHING WARNING LIGHT AND TRIM FAIL ON MAP. RETURNED TO GATE. INSPECTED AND TESTED ELECTRIC TRIM SYSTEM. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002061800072 20020618 00072 2002 6 18 HEEA079787 4 20020530 A 3454 071121525 CONTROL UNIT BOLKMS 105 BO105S 5626006 EU VOR SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6607K S841 DISPLAY OUT. FOUND DISPLAY WOULD INTERMITTENTLY CUT OUT FOR A SECOND. FOUND MICROPROCESSOR LEADS VERY DIRTY. CLEANED. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 2002061800073 20020618 00073 EU 2002 6 18 HEEA079788 1 20020530 A 2432 30248001 BATTERY BOLKMS 105 BO105S 5626006 EU MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5421E S806 BATTERY WEAK. REPAIRED. 1 G 7 2 3U H3EU 2002061800074 20020618 00074 NE 2002 6 18 SWIA200210829 2 20020508 A 7297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE FAULTY A SWIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 NM 07 906SW 7510 LEVEL AT 27,000 FEET, AFTER COWL ANTI-ICE WAS TURNED ON AND ASSOCIATED THRUST REDUCTION WAS MADE, THE RIGHT ENGINE N1 FL UCTUATED UNCOMMANDED 89.0 TO 95 PERCENT. ALSO ON DESCENT, WITH THRUST LEVER REDUCTION, RIGHT N1 FROM 81 TO 83 PERCENT. NOTICED SOME N2 FLUCTUATION OF UP TO + -1 PERCENT. RETURNED TO DENVER. REMOVED AND REPLACED BLUE, BROWN AND YELLOW EN GINE HARNESS. OPS CHECKS GOOD DURING ENGINE RUN ON GROUND IAW 73-21-13, 77-11-03 AND 73-21-05. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061800075 20020618 00075 SO 2002 6 18 SWIA200210830 1 20020428 A 2720 3211001003 PCU EMB 120 EMB120ER 3260203 SO RUDDER MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 187SW 5734 5734 120037 ON TAKEOFF, COULD NOT MOVE RUDDER PAST HALF TRAVEL TO THE RIGHT. TURNING BLUE SYSTEM OFF MADE NO DIFFERENCE. UPON LAND ING FULL TRAVEL WAS RESTORED. REPLACED RUDDER PCU. INFLIGHT FUNCTIONAL TEST OF RUDDER SYSTEM NORMAL. FLIGHT TEST OK. 2 L 7 2 4T RT A31SO 2002061800076 20020618 00076 EU 2002 6 18 HEEA079789 1 20020530 A 2432 30248001 BATTERY BOLKMS 105 BO105S 5626006 EU MAIN MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 81992 S827 WHEN UNIT WAS FUNCTION CHECKED UPON INSTALLATION BOTH "BATT 50" AND "BATT 60" LIGHTS WERE ILLUMINATED. REPAIRED. 1 G 7 2 3U H3EU 2002061800077 20020618 00077 2002 6 18 HEEA079790 4 20020530 A 2312 4000103000 TRANSCEIVER BOLKMS 117 BK117A1 5626010 EU COCKPIT INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911TL 7198 TRANSCEIVER WOULD NOT TRANSMIT. 1 G 7 2 3U H13EU 2002061800078 20020618 00078 2002 6 18 HEEA079791 4 20020530 A 3421 504001790116 GYRO BOLKMS 117 BK117A1 5626010 EU COCKPIT MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RS S670 HORIZON GYRO FLAG STICKS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H13EU 2002061800079 20020618 00079 2002 6 18 HEEA079792 4 20020530 A 2350 AA95758 AUDIO CONTROL BOLKMS 105 BO105S 5626006 EU COCKPIT MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 818SH S753 SIDETONE WEAK. FOUND ICS AND RX KNOBS BAD. REPLACED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 2002061800080 20020618 00080 2002 6 18 HEEA079793 4 20020530 A 2370 ACS1278 MIXER BOX BOLKMS 117 BK117A1 5626010 EU COCKPIT MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 AUDIO MIXER BOX HAS BLEED OVER. 1 G 7 2 3U H13EU 2002061800081 20020618 00081 EU 2002 6 18 HEEA079794 1 20020530 A 2432 RG390E BATTERY BOLKMS 105 BO105S 5626006 EU MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 911PF 123 S718 BATTERY WEAK. 1 G 7 2 3U H3EU 2002061800082 20020618 00082 EU 2002 6 18 HEEA079795 1 20020530 A 2432 RG390E BATTERY BOLKMS 105 BO105S 5626006 EU MAIN DISCHARGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 818SH S753 BATTERY DEAD. 1 G 7 2 3U H3EU 2002061800083 20020618 00083 EU 2002 6 18 HEEA079796 1 20020530 A 2432 RG390E BATTERY BOLKMS 117 BK117A1 5626010 EU MAIN OVERHEATED E HEEA K NONE M OVER TEMP IN INSP/MAINT 1 SW 03 911RS 34 S670 BATTERY HOT ON CHARGE. 1 G 7 2 3U H13EU 2002061800085 20020618 00085 2002 6 18 HEEA079798 4 20020530 A 2300 TH3602ZZZY CONTROL HEAD BOLKMS 117 BK117A1 5626010 EU FM COMMS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 911TL 7198 DISPLAYING WRONG PL CODE AND CHANGING SETTINGS INDEPENDENTLY OF MASTER CONTROL HEAD. 1 G 7 2 3U H13EU 2002061800086 20020618 00086 EA 2002 6 18 SWIA200210831 1 20020507 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 590SW 7077 AFTER TAKEOFF AT 1000 FT AGL, BOTH STAB TRIM CH 1 & CH 2 AND MACH TRIM DISCONNECTED. BOTH STAB TRIMS WOULD NOT RE-ENGAG E. RETURNED TO SLC. REMOVED AND REPLACED FIRST OFFICER'S STAB TRIM DISCONNECT SWITCH IAW 27-41-30. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002061800087 20020618 00087 EA 2002 6 18 SWIA200210832 1 20020506 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA A/C BAY MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 405SW 7029 AFTER TAKEOFF, SWITCHED BLEEDS PER SINGLE PACK OPERATIONS. RECEIVED A HIGH PACK PRESSURE CAUTION MESSAGE ON THE LEFT PA CK. RESET BUT PACK HIGH PRESSURE CAUTION CAME BACK. RETURNED TO OAK. OPERATED THE AIRCRAFT AT TAKEOFF POWER AFTER REP AIRING THE RIGHT PACK. BOTH PACKS OPERATE NORMALLY WITH NO HIGH PRESSURE WARNINGS. 2 L 7 2 4F RT A21EA 2002061800088 20020618 00088 SO 2002 6 18 SWIA200210833 1 20020505 A 3250 12027361001 RELAY EMB 120 EMB120ER 3260203 SO NLG STEERING FAILED A SWIA O OTHER O OTHER TO TAKEOFF 1 NM 07 582SW 4319 4319 120350 AIRCRAFT PULLS LEFT ON TAKEOFF ROLL AT 80 KNOTS. REMOVED AND REPLACED NOSE WHEEL STEERING RELAY WITH SERVICEABLE UNIT I AW MM 32-50-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002061800089 20020618 00089 NM 2002 6 18 CA020528011 1 20020522 A 2420 941D3352 CIRCUIT BREAKER BOEING 737 737275 1384485 NM PWA JT8 JT8D17 52049 NE ELECTRICAL FAILED W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 CA (CAN) ON DESCENT LOST THE NR 2 AND 3 TRANSFORMER RECTIFIERS, ONE FUEL PUMP ON THE NR 1 TANK AND BOTH FUEL PUMPS ON THE N R 2 TANK ALSO F/O'S INSTRUMENTS AND NR 2 RADIO. CREW NOTICED SLIGHT ELECTRICAL SMELL AND ON BASE LEG THE TRANSFER BUS L IGHT CAME ON. CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. NR 2 T/R, GCU, AND GENERATOR REPLACED WITH FI NAL FIX BEING THE REPLACEMENT OF NR 2 GENERATOR BREAKER AND OPERATION THEN CHECKING SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 2002061800090 20020618 00090 SO 2002 6 18 SWIA200210834 1 20020428 A 2731 SENSOR EMB 120 EMB120RT 3260202 SO ELEVATOR MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 1105G 120105 TAKEOFF TRIM AURAL WARNING SOUNDED ON TAKEOFF ROLL. ABORTED TAKEOFF. TRIM WAS SET IN THE GREEN BAND. REPLACED RIGHT E LEVATOR TRIM SENSOR. OPS CHECK OF TRIM AURAL WARNING SOUNDS OUTSIDE OF GREEN BAND GOOD. 2 L 7 2 4T RT A31SO 2002061800091 20020618 00091 SO 2002 6 18 SWIA200210835 1 20020506 A 3297 WIRE HARNESS EMB 120 EMB120RT 3260202 SO LT MLG FAULTY A SWIA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 07 196CA 120196 WITH GEAR HANDLE DOWN THE LANDING GEAR REMAINED UP AND LOCKED. LEFT THE GEAR HANDLE DOWN AND ON GO-AROUND THE LANDING G EAR CAME DOWN AND LOCKED. REPLACED WIRING HARNESS FOR LEFT MAIN LANDING GEAR PROXIMITY SENSOR. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002061800092 20020618 00092 2002 6 18 SWIA200210836 4 20020504 A 3418 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 432SW 7548 AFTER TAKEOFF, STALL FAIL CAUTION MESSAGE APPEARED. RETURNED TO SLC. RESET STALL PROTECTION COMPUTER (SPC) CIRCUIT BRE AKERS AND RESET SPC MEMORY. MESSAGE CLEARED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002061800093 20020618 00093 CE 2002 6 18 CA020528012 1 20020513 A 5280 358150163 HINGE BEECH 3581505516 BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO MLG DOOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A SCHEDULED INSPECTION THE AFT MLG DOOR, HINGE WAS FOUND BROKEN, INSPECTION OF THE HINGES REVEALED THAT A N UNDETECTED CRACK HAD BEEN THERE FOR SOME TIME PRIOR TO FAILURE. AN INSPECTION OF THE RETRACTION SYSTEM DID NOT REVEAL ANY CAUSE OF THE CRACKING AND SUBSEQUENT FAILURE. THE HINGE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O RT 3A16 3E1 2002061800094 20020618 00094 EA 2002 6 18 SWIA200210837 1 20020503 A 2910 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 411SW 7067 HYDRAULIC SYSTEM NR 2 LOST ALL FLUID INFLIGHT. REMOVED AND REPLACED RIGHT ENGINE HYDRAULIC PUMP (EDP). PERMA SWAGGED P RESSURE LINE NR 2 SYSTEM AT ACCUMULATOR. RAN ENGINE AND ELECTRICAL PUMP. SERVICED SYSTEM. NO LEAKS NOTED. PERFORMED OPS CHECKS OF FLIGHT CONTROLS ASSOCIATED WITH NR 2 SYSTEM. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002061800095 20020618 00095 NM 2002 6 18 DLM88020615 1 20020602 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 920DE 53423 AFT CABIN EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY, OPS NORMAL. 2 L 7 2 4F RT A6WE 2002061800096 20020618 00096 EU 2002 6 18 SIMA200212301 1 20020501 A 5711 S57210580200 SPAR AEROSP ATR42 ATR42300 8680920 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 DURING CPCP2 LEFT WING AFT SPAR UPPER ANGLE CORRODED BETWEEN INBOARD AND OUTBOARD AILERON HINGE POINTS. LEFT WING AFT S PAR REPAIR BY BLENDOUT IAW EO E1-57MR-107. (M) 2 H 7 2 4T RT A53EU 2002061800097 20020618 00097 EU 2002 6 18 SIMA200213001 1 20020503 A 2810 ODOR AEROSP ATR72 ATR72212 8680945 EU CABIN DETECTED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 434AT 434 MIA - FLT 9534 - A/C SMELLS LIKE FUEL BOTH ON GROUND AND IN THE AIR. INSPECTED INSIDE CABIN FOR FUEL LEAK, OUTSIDE FOR FUEL LEAKS. AIRED OUT CABIN AND CROSS FEED FUEL AND RAN ENGINES. NO SMELL OF FUEL FOUND INCABIN. (M) 2 H 7 2 4T RT A53EU 2002061800098 20020618 00098 SO 2002 6 18 SIMA200213004 1 20020502 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - DURING INSPECTION, FOUND STRINGER 19R CHAFED. BLENDED CHAFE, FABRICATED DOUBLER ANGLES AND FOUR SHIMS. REPAIRED IAW EMB GST-1405/02 ITEM 2, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002061800099 20020618 00099 SO 2002 6 18 SIMA200213201 1 20020512 A 3350 BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISLODGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 809AE 145521 CLE - FLT 4334 - DURING PREFLIGHT CRWE REPORTED, THE FORWARD EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE FOUND THE FORWARD BATTERY PACK TO BE DISLODGED. THE SAME BATTERY PACK WAS REINSTALLED IAW THE EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002061800100 20020618 00100 EU 2002 6 18 SIMA200213701 1 20020517 A 3350 04B02D BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 242AT 242 MIA - FLT 5101 - CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PAC K IN POWER SUPPLY UNIT 10WL IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800101 20020618 00101 SO 2002 6 18 SIMA200213802 1 20020513 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - DURING AN IMBV MAINTENANCE, FOUND CORROSION ON GALLEY CENTER BEAM. REMOVED CORRODED GALLEY CENTER BEAM. INSTALLE D NEW BEAM IAW EMB 145 (SRM 145/1142, CHAP 51 REV 18) 51-40-02, GST 1128/02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002061800102 20020618 00102 SO 2002 6 18 SIMA200213803 1 20020511 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - DURING AN IMBV MAINTENANCE, FOUND CORROSION ON GALLEY RIGHT FLOORBEAM, THREE AREAS, BETWEEN FRAMES 20 AND 23. REM OVED CORROSION BY BLENDING. NDT PERFORMED, NO DEFECTS. FABRICATED THREE REPAIR DOUBLERS, REPAIR DONE IAW EMB GST-1491/ 02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002061800103 20020618 00103 EU 2002 6 18 SIMA200214101 1 20020517 A 5347 S53570201202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP 4 INSPECTION, LEFT MID INBOARD SEAT TRACK CORRODED. REMOVED AND REPLACED LEFT MID INBOARD SEAT TRACK IAW EO NR E1-53MR-271. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800104 20020618 00104 EU 2002 6 18 SIMA200214102 1 20020517 A 5347 S53570201202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP 4 INSPECTION, LEFT MID OUTBOARD SEAT TRACK CORRODED. REMOVED AND REPLACED LEFT MID INBOARD SEAT TRACK IAW EO NR E1-53MR-271. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800105 20020618 00105 EU 2002 6 18 SIMA200214103 1 20020517 A 5350 S5397140229401 FAIRING AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP4 INSPECTION, MAIN LANDING GEAR FAIRING AT FRAME 27A HAS CORROSION. REPAIRED CORRODED AREA IAW ATR 42 SRM 53-91-43 PAGES 430 THROUGH 433. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800106 20020618 00106 EU 2002 6 18 SIMA200214104 1 20020517 A 5315 S53672406208 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP 2 INSPECTION, FLOORBEAM AT FRAME 36 HAS NUMEROUS SPOTS OF CORROSION. AROUND SCREW HOLES TOP AND BOTTO M. INSTALLED NEW FLOORBEAM 36 IAW ATR42 SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800107 20020618 00107 SW 2002 6 18 CA020529001 1 20020516 A 5711 SPAR SWRNGN SA226 SA226TC 8780404 SW LT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13857 (CAN) WHILE PERFORMING THE INSPECTION REQUIRED BY SID 57-10-02 ON WING STATION 9 OF THE LOWER FORWARD SPAR. CORROSION WA S FOUND IN THIS AREA ON THE FORWARD SIDE OF THE FORWARD SPAR, REMOVAL OF THE FORWARD PRESSURE PLATE REVEALED THE CORROSI ON EXTENDED FROM LT WING STATION 15 TO RT WING STATION 29 AND A APPROXIMANTLY .5 INCHES CRACK WAS FOUND ON THE VERTICAL LEG OF THE FORWARD ALUMINUM ANGLE AT WING ST. 0. THE SPAR STRUCTURE IN THIS AREA CONSISTS OF THE SPAR CAP FOLLOWED BY A FORWARD AND AFT ALUMINUM ANGLE, TWO TITANIUM STRAPS AND A 4130 ANGLE. THE CORROSION WAS LIMITED TO THE FORWARD ALUMINU M ANGLE. NO EVIDENCE OF CORROSION WAS FOUND ON THE AFT SIDE OF THE FORWARD SPAR. 2 L 7 2 4T RT A8SW 2002061800108 20020618 00108 EU 2002 6 18 SIMA200214105 1 20020517 A 5347 S53570201200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP 4 INSPECTION, RIGHT MID INBOARD SEAT TRACK CORRODED. INSTALLED NEW RIGHT MIDDLE INBOARD SEAT TRACK IA W EO NR E1 53MR-271. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800109 20020618 00109 EU 2002 6 18 SIMA200214106 1 20020517 A 5347 S5367800125002 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP4 INSPECTION, RIGHT AFT INBOARD SEAT TRACK IS CORRODED. REMOVED AND REPLACED NEW RIGHT INBOARD SEAT TR ACK IAW EO E1-53-MR-271. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800110 20020618 00110 EU 2002 6 18 SIMA200214107 1 20020517 A 5347 S53678001212 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP 4 INSPECTION, AFT CARGO SEAT TRACK CORRODED. INSTALLED NEW AFT CARGO SEAT TRACK IAW 51-75-04 AND AS P ER EO E1-53MR-271. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800111 20020618 00111 EA 2002 6 18 CA020529002 1 20020524 A 5321 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE CABIN FLOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 21263 (CAN) DURING THE FLEET LEADER STRUCTURAL INSPECTION, THE INSPECTION REVEALED FOUR CRACKS TO THE PRESSURE FLOOR AT FS 460 .00, RBL 9.00 TO CENTER LINE AND LBL 9.00 TO CENTER LINE. AIRCARFT IS REPAIR PER REO 601R-53-41-090 2 L 7 2 4F 4 F RT A21EA E15NE 2002061800113 20020618 00113 GL 2002 6 18 CA020530001 2 20020529 A 7323 1056058312 SPRING ALLSN BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL TURBINE GOV BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA CAE835698 (CAN) DURING OPERATION 1 ON RT ENGINE, THE SPRING (GOVERNOR LEVER RETURN SPRING) WAS FOUND BROKEN AND REPLACED WITH A NE W SPRING. 1 G 7 2 3U 3 U H3EU E4CE 2002061800114 20020618 00114 NE 2002 6 18 MEX2002082 2 20020324 A 7321 FILTER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE FUEL CONTROL DIRTY A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 491SH 49150 FLT 430 - PVR-LAX - CAPTAIN REPORTED HIGH TEMPERATURE AT ENGINE STARTING, THE ENGINE STARTING WAS PERFORMED THREE TIMES, AT THIS LAST TIME THE STARTING WAS INSIDE THE PARAMETERS. AIRCRAFT STARTED THE TAXI, HOWEVER IT RETURNED TO PLATFORM A S CONSEQUENCE OF AN ENGINE TEMPERATURE INCREASE UNTIL 500 DEGREES CELSIUS. THE FILTER OF THE FCU AND OF THE PYD WAS REM OVED, AND WAS VERIFIED THE CHIP DETECTOR. TESTS OK. (M) 2 L 7 2 4F 4 F A6WE E9NE 2002061800115 20020618 00115 SW 2002 6 18 CA020530002 1 20020526 A 7500 BLEED BAND BELL 205 205A1 1181414 SW LYC T53 T5317A 41549 NE ENGINE OUT OF ADJUST W A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION HO HOVERING 1 CA (CAN) WHILE WATER BUCKETING A COMPRESSOR STALL OCCURRED. THE PILOT HOVER TAXIED WITH REDUCED POWER TO THE SHORELINE. AT THE SHORELINE HE DROPPED HIS LOAD AND THE AIRCRAFT WAS RETURNED BACK TO STAGING AREA AND A NORMAL ENGINE SHUTDOWN WAS C ARRIED OUT. AFTER THE COMPRESSOR STALL THE FUEL FILTER WAS CHECKED. THE ENGINEER FOUND CONTAMINATION IN THE FUEL FILTE R. THE ENGINE BLEED BAND AND VARIABLE INLET GUIDE VANES WERE FOUND OUT OF ADJUSTMENT. THE FUEL CONTROL IS GETTING NEAR OVERHAUL SO MAYBE IT WAS GETTING TIRED OR POSSIBLE FUEL CONTAMINATION MIGHT HAVE CONTRIBUTED TO THE COMPRESSOR STALL. 1 G 7 1 4U 4 U H1SW E17EA 2002061800116 20020618 00116 WP 2002 6 18 MEX2002092 1 20020330 A 2150 A/C PACK DOUG DC9 DC932 3022066 WP A/C BAY MALFUNCTIONED A ASMF A UNSCHED LANDING O OTHER CL CLIMB 1 SW 23 1003P FLT 115 - HMO-MEX - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF PRESSURIZATION PROBLEMS. BOTH AIR CONDITIONING PACK AGES FAIL DURING FLIGHT, RECOVERING LEFT PACKAGE DURING DESCENT. CHECKED THE OPERATION OF THE PRESSURIZATION CONTROL VA LVE AND CONTROLLERS RECOVERING THE RIGHT PACKAGE. TESTS WERE PERFORMED IAW MM 21-32-3 AND 21-32-5. (M) 2 L 7 2 4F A6WE 2002061800117 20020618 00117 NM 2002 6 18 CA020530003 1 20020527 A 2910 374612 CHECK VALVE AIRBUS A319 A319114 3930350 NM CFMINT CFM56 CFM565A1 NE HYD SYSTEM LEAKING W O OTHER O OTHER NR NOT REPORTED 1 CA (CAN) ECAM MESSAGE "Y SYST LO PR" AND 10 MIN LATER "LO LVL" ECAM ACTIONS COMPLETED. YELLOW HYDRAULIC SYSTEM PTU MANIFOLD CHECK VALVE FOUND LEAKING AND SAME REPLACED AS PER AMM. 29-13-15. 2 L 7 2 4F 4 F RT A28NM E29NE 2002061800118 20020618 00118 WP 2002 6 18 MEX2002093 1 20020331 A 2910 HYDRAULIC LINE DOUG DC9 DC987 3022087 WP HYD SYSTEM BROKEN A ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 753RA 49587 FLT 402 - PVR-MEX - DURING TRANSIT CHECK DETECTED A LEAK IN THE RIGHT HYDRAULIC SYSTEM. A BROKEN LINE AT ACCESSORY COMP ARTMENT AFFECTING THE VENTRAL STAIRWAYS, THE RIGHT ENGINE REVERSE AND THE DIRECTION RUDDER. A FLEXIBLE TUBE WAS INSTALL ED. DURING OVERNIGHT SERVICE WAS INSTALLED A STEEL TUBE AND THE SYSTEM WAS CHECKED IAW MM 29-01-03. (M) 2 L 7 2 4F RT A6WE 2002061800119 20020618 00119 CE 2002 6 18 CA020530004 1 20020523 A 3230 11972 SPRING CESSNA 425 425 2076018 CE MLG SOLENOID FAILED W O OTHER J WARNING INDICATION LD LANDING 1 CA (CAN) RFR: GEAR WOULD NOT GO DOWN.FINDINGS: FAULTY (OPEN) SOLENOID ASSEMBLY AND BROKEN SPRING. 1 L 7 2 3T RT A7CE 2002061800120 20020618 00120 NM 2002 6 18 MEX2002101 1 20020407 A 3250 59142965505 CONTROL VALVE DOUG MD80 MD83 3023681 NM NLG STEERING FAILED A ASMF O OTHER O OTHER TX TAXI/GRND HDL 1 SW 23 945AS 49643 FLT 583 - MEX-CUN - WHEN THE AIRCRAFT GETS PLATFORM BY ITSELF THE RIGHT GYRO WAS EXCEEDED AND THE ACTUATORS WERE STUCK. AIRCRAFT WAS SENT TO THE HANGAR AND THE STEERING CONTROL VALVE WAS CHANGED IAW MM 32-52-01. (M) 2 L 7 2 4F RT 2002061800122 20020618 00122 NM 2002 6 18 MEX2002105 1 20020410 A 7722 HAD18269 PROBE BOEING 757 7572Q8 1384972 NM NR 2 ENGINE FAILED A ASMF O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 23 803AM 26268 FLT 404 - MEX-JFK - AIRCRAFT WAS SENT TO THE HANGAR FOR HIGH EGT ON NR 2 ENGINE (930 GRADES). PERFORMED A FIM PROCEDURE DETECTED THE PROBES T/C 2 T/C 6 OUT OF LIMITS. THEY WERE CHANGED AND AN EGT TEST WAS PERFORMED DURING ENGINE RUNNING I AW MM 77-21-01. (M) 2 L 7 2 4F RT A2NM 2002062000028 20020620 00028 NM 2002 6 20 F3LA200200165 1 20020610 A 5320 SPLICE BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3389 26440 DURING C-2 CHECK, INSPECTION REPORTED FLOOR SPLICE IN AFT CARGO COMPARTMENT AT BS 767 CORRODED. FABRICATED AND INSTALLE D REPLACEMENT FLOOR SPLICE PER SRM 53-60-53. 2 L 7 2 4F RT A16WE 2002061800125 20020618 00125 NE 2002 6 18 MEX2002111 2 20020413 A 7321 FUEL CONTROL DOUG DC9 DC987 3022087 WP PWA JT8 JT8D217C 52053 NE NR 2 ENGINE OUT OF RIG A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 216AM 49586 FLT 278 - MEX-CJS - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF THRUST PROBLEM OF ENGINE NR 2. WHEN CAPTAIN TRIED T O MAKE EQUAL THE THRUST OF ENGINE TWO IT WAS UNDER 10 PERCENT. PERSONNEL REVIEW THE EPR'S TRANSMITTER AND THE PT2 AND P T7 LINES, ALL CORRECT. THERE WAS PERFORMED A TRIMMING AND RINGING TEST TO BOTH ENGINES IAW MM MD-80 71-00-01 76-11-00. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002061800127 20020618 00127 SO 2002 6 18 CA020530011 1 20020518 A 5711 SPAR MAULE M4 M4220C 5460114 SO FRNKLN 6AV350 6A350C1 27043 EA WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) SPARS CRACKED AT HINGE ATTACH AS A RESULT OF FLAPS - FLAPPING IN WIND WHEN TIED DOWN. 1 H 7 1 3O 3 O 3A23 E9EA 2002061800128 20020618 00128 2002 6 18 MEX2002115 4 20020418 A 3497 7274551 WIRE DOUG MD88 MD88 3023688 NM COCKPIT SHORTED A ASMF O OTHER J WARNING INDICATION IN INSP/MAINT 1 SW 23 160PL 49763 FLT 904 - MEX-HMO - DURING TRANSIT CHECK, FOUND THE DFGC SELECTOR IS OUT OF SERVICE (CB C17 SHUTS OFF), WIRING WERE REVI EWED DETECTING A SHORT CIRCUIT ON LINE 1C610X0RD. IT WAS REPAIRED IAW WM 22-16-11 AND THE BREAKER B10-367 WAS CHANGED A ND A LINE WAS INSTALLED IN S30-4. TESTS OK IAW MM 22-01-05. (M) 2 L 7 2 4F RT A6WE 2002061800129 20020618 00129 WP 2002 6 18 MEX2002116 1 20020418 A 3610 DUCT DOUG DC9 DC982 3022082 WP PNEUMATIC SYS LEAKING A ASMF E ENGINE SHUTDOWN M OVER TEMP TX TAXI/GRND HDL 1 SW 23 491SH 49150 FLT 489 - SJD-ACA - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCES OF HIGH TEMPERATURE IN ENGINE NR 2 (470 GRADES), ENGIN E WAS STARTED WITH A PNEUMATIC POWER GETTING 380 GRADES. DURING OVERNIGHT SERVICE WERE REPAIRED TWO PNEUMATIC LINES WIT H LEAKS, TESTS WERE PERFORMED IAW MM 71-00-00. (M) 2 L 7 2 4F A6WE 2002061800130 20020618 00130 NM 2002 6 18 CA020530012 1 20020527 A 3242 32600691 STATOR BOEING 767 767375 1385217 NM GE CF6 CF680C2B6F 30025 NE BRAKE ASSY DESTROYED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) AFTER LANDING BRAKE TEMP LIGHT ON RIGHT FOREWARD INNER MAIN. TEMP WENT TO 9 WITH AUTOBRAKE SETTING AT 2 FOR LANDIN G. NR 3 MAIN WHEEL AND BRAKE REMOVED. BRAKE INNER STATOR DISINTEGRATED AND CAUSED JAMMING OF BRAKE. TIRE DEFLATED DUE FUSE PLUG OVERHEAT. NEW BRAKE AND TIRE ASSYS INSTALLED. 2 L 7 2 4F 4 F RT A1NM E13NE 2002061800131 20020618 00131 EA 2002 6 18 CA020530013 1 20020525 A 3244 13685 BEARING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE MLG WHEEL FAILED W C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 CA (CAN) SEVERE NOSE SHIMMY ON TAKE-OFF. (VIBRATION) (L1159330) LT AND RT NOSE WHEEL ASSY'S REPLACED AND WHILE REPLACING R T WHEEL DAMAGE FOUND ON AXLE DUE TO BEARING FAILURE. NOSE LANDING GEAR ASSY. REPLACED AS PER MM 32-21-01-000-400, PG. 40 1. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061800133 20020618 00133 SW 2002 6 18 CA020530015 1 20020516 A 2432 206075295053 WIRE BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL BATTERY BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING VISUAL INSPECTION OF THE AIRCRAFT, THE POSITIVE LEAD CONNECTING TO THE BATTERY SOLONOID WAS FOUND TO BE VER Y LOOSE. UPON CLOSER INSPECTION HALF OF THE STRANDED BATTERY WIRE WAS BROKEN. 1 G 7 1 3U 3 U H2SW E1GL 2002061800135 20020618 00135 EA 2002 6 18 CA020531001 1 20020527 A 2731 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PITCH TRIM FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 10398 (CAN) "DURING CLIMB OF THE FLIGHT, THE CREW EXPERIENCED UNCOMMANDED NOSE DOWN PITCH TRIM. THE CREW PERFORMED THE QRH PR OCEDURES AND RETURNED TO BASE AND LANDED WITHOUT FURTHER INCIDENT." "MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FIRS T OFFICERS YOKE PITCH TRIM SWITCH. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE." 2 L 7 2 4F 4 F RT A21EA E15NE 2002061800136 20020618 00136 2002 6 18 MEX2002121 4 20020423 A 3460 4034241972 COMPUTER DOUG MD80 MD83 3023681 NM E/E BAY FAILED A ASMF O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 23 861LF 49826 FLT 935 - MTY-MEX - BOTH FMA'S OUT OF SERVICE WITH THE DFGC SWITCH IN THE NR 2 POSITION. PERFORMED A RESET TO THE ELECT RIC BARS, DFGC 1 DID NOT PERFORM THE POWER UP UNTIL THE DFGC SWITCH WAS CHANGED. THE COPILOT ADI WAS CHANGED BUT DID NO T CORRECT THE PROBLEM . BOTH DFGC WERE REMOVED, THEIR RESPECTIVE CIRCUIT BREAKERS WERE RESET. ALL THE ELECTRICAL POWER WAS INTERRUPTED AND AFTER 10 MINUTES WAS STABILIZED, AND ALL SYSTEMS WORK OK. IT WAS PERFORM AN AUTOLAND TEST OK. AT RON, 23/24 BOTH DFGC WERE REPLACED, AND TEST OK IAW MM 22-01-01. (M) 2 L 7 2 4F RT 2002061800137 20020618 00137 NE 2002 6 18 CA020531002 2 20020522 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) MAINTENANCE WAS ADVISED BY THE FLIGHT CREW THAT OIL LOW PRESSURE NECESSITATED THE RT ENGINE TO BE SHUTDOWN AS PER THE QRH. VIBRATION DETECTED IMMEDIATELY BEFORE SHUT-DOWN. CONTRACT MAINTENANCE COMFIRMED A SIGNIFICANT AMOUNT OF METAL I N THE GEARBOX. AN ENGINE CHANGE IS INITIATED. MAINTENANCE STAFF, PARTS AND EQUIPMENT WILL BE TRANSPORTED.AIRCRAFT RETURN ED INTO SERVICE 2 L 7 2 4F 4 F RT A21EA E15NE 2002061800138 20020618 00138 2002 6 18 MEX2002122 4 20020425 A 3436 WARNING SYSTEM DOUG DC9 DC987 3022087 WP COCKPIT ACTIVATED A ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 204AM 49404 FLT 491 - LAX-MEX - AIRCRAFT SUSPENDS TAKEOFF AS A CONSEQUENCE OF A SPEED REDUCTION AND A WINDSHEAR ALARM. AIRCRAFT RET URN TO PLATFORM AND A BRAKES ASSEMBLY REVISION WAS PERFORMED. (M) 2 L 7 2 4F RT A6WE 2002062000029 20020620 00029 NM 2002 6 20 F3LA200200166 1 20020610 A 5320 STRAP BOEING 737 7373L9 1384470 NM FUSELAGE TORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3389 26440 DURING C-2 CHECK, INSPECTION REPORTED SMALL TEAR IN FLOORBEAM STABILIZER STRAP AT STA 328, LBL 8, AND FASTENER HEADS WOR N DOWN. REPLACED DAMAGED STABILIZER STRAP PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002061800139 20020618 00139 NM 2002 6 18 2002F00624 1 20020502 A 5720 66147331 BRACE BOEING 727 727225 1384077 NM RT WING CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND BRACE CRACKED BELOW NUMBER EIGHT SPOILER, IN RIGHT INBOARD FLAP WELL, RBL 124. (M) 2 L 7 3 4F A3WE 2002061800140 20020618 00140 NM 2002 6 18 2002F00625 1 20020503 A 5754 SKIN BOEING 727 727225 1384077 NM L/E SLAT DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND NR 3 SLAT OUTER SKIN DENTED AT WING STATION 570L. (M) 2 L 7 3 4F A3WE 2002061800141 20020618 00141 NM 2002 6 18 2002F00626 1 20020420 A 5310 DOOR FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND TWO CRACKS IN MAIN CABIN DOOR JAMB WEB, ONE 2 INCH LONG, AND ONE .75 INCH LONG, AT STATION 350 LBL 62. (M) 2 L 7 3 4F A3WE 2002062000030 20020620 00030 NM 2002 6 20 F3LA200200167 1 20020610 A 5320 STRAP BOEING 737 7373L9 1384470 NM FUSELAGE TORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3389 26440 DURING C-2 CHECK, INSPECTION REPORTED FLOORBEAM STABILIZER STRAP TORN AND MISSING A SECTION, STA 312 TO 328, BL -0-. RE PLACED DAMAGED STABILIZER STRAP PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002061800142 20020618 00142 NM 2002 6 18 2002F00627 1 20020508 A 5523 65C2638428A TRIM TAB BOEING 737 737400 138449A NM ELEVATOR DAMAGED A RYNA O OTHER E VIBRATION/BUFFET CL CLIMB 1 CE 07 EIBXI 25052 ON CLIMB-OUT FROM MBJ, FLIGHT CREW NOTED AIR FRAME VIBRATION. REDUCING THRUST ON BOTH ENGINES HAD NO EFFECT. FLIGHT CR EW SELECTED FLAPS FIVE DEGREE POSITION DURING LANDING AND VIBRATION STOPPED. PERFORMED OVERWEIGHT LANDING IN MIA WITHOU T INCIDENT. POST FLIGHT INSPECTION REVEALED A PORTION OF THE RIGHT ELEVATOR SERVO TAB MISSING. ELEVATOR AND TAB ASSEMB LY TO BE REPLACED. (M) 2 L 7 2 4F RT A16WE 2002072500017 20020725 00017 NM 2002 7 25 QXEA0200892 1 20020617 A 5270 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 1390041 NM SERVICE DOOR MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 404QX 4046 SEA - ON TAKE-OFF, CREW RECEIVED A MASTER WARNING FOR THE AFT SERVICE DOOR. MAINTENANCE INSPECTED AND FOUND FAULT FOR TH E AFT SERVICE DOOR GAP TOO FAR. MAINTENANCE CLEANED THE PROXIMITY SENSOR AND TARGET. AIRCRAFT WAS PRESSURIZED AND AN OPE RATIONAL CHECK WAS PERFORMED. NO FAULT WERE NOTED AND THE PSEU SHOWS THE GAP AS SATISFACTORY. AIRCRAFT RETURNED TO SERVI CE. 2 H 7 2 4T RT A13NM 2002061800143 20020618 00143 NM 2002 6 18 2002F00628 1 20020509 A 2782 1U1110 ACTUATOR BOEING 727 727222 1384073 NM L/E SLAT LEAKING A RYNA A UNSCHED LANDING K J F FLUID LOSS WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 CE 07 7643U 20037 ON DEPARTURE FROM DAY TO ICT, 'A' SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. ALL APPLICABLE CHECKLISTS WERE ACCOMPLISHED A ND EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. (M) 2 L 7 3 4F A3WE 2002061800144 20020618 00144 WP 2002 6 18 ABAX010913 1 20020614 A 5610 LOCK DOUG DC8 DC861 3021952 WP OUT OF ADJUST A ABXA K NONE O OTHER NR NOT REPORTED 1 GL 23 852AX 46016 CAPTAIN'S SLIDING WINDOW WOULD NOT OPEN. ADJUSTED TOP WINDOW LOCK IAW DC-8 MM 56-10-03. 2 L 7 4 4F 4A25 2002062000031 20020620 00031 NM 2002 6 20 F3LA200200168 1 20020610 A 7110 COWLING BOEING 737 7373Q8 1384670 NM NR 1 ENGINE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3389 26293 DURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE OUTBOARD THRUST REVERSER COWL PUNCTURED AT AREA OF PRSOV VALVE. PERFO RMED DOUBLER REPAIR PER EA 54T-737-037, REV A. 2 L 7 2 4F RT A16WE 2002061800145 20020618 00145 NM 2002 6 18 2002F00629 1 20020427 A 2910 HYDRAULIC SYSTEM DOUG DC10 DC1040F 3023507 NM NR 1 & NR 2 MALFUNCTIONED A CLCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 141WE 46661 FLT 558 - MSLP-KMIA - DURING CLIMB-OUT, LOST HYDRAULIC SYSTEMS ONE AND TWO. RETURNED TO MSLP AND A NORMAL LANDING WITHO UT INCIDENT WAS MADE. NR 1 TIRE MISSING A LARGE SECTION OF TREAD, NR 5 TIRE DAMAGED BY GROUND DEBRIS. BOTH NR 1 AND 5 WHEELS WERE INTACT. LEFT WING INBOARD FLAP WELL AREA HAS NUMEROUS HYDRAULIC LINES DAMAGED. FLAP/AILERON CABLES DAMAGED . DAMAGE TO THE INBOARD LEFT FLAP AND FLAP FAIRING. DAMAGE TO NUMEROUS WIRE BUNDLES, BRACKETS AND LINKS. PRELIMINARY INVESTIGATION DETERMINED THAT A SECTION OF THRUST REVERSER TURNING VANE WAS FOUND ON THE RUNWAY IMMEDIATELY AFTER THIS I NCIDENT OCCURRED. AIRCRAFT UNDER REPAIR AT MSLP. (M) 2 L 7 3 4F RT A22WE 2002061800146 20020618 00146 CE 2002 6 18 2002F00630 1 20020429 A 2710 1295240483 PULLEY BRACKET BEECH 1900 1900D 1154162 CE AILERON LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 69547 13254 UE189 AT SCHEDULED THIRD 200 HOUR INSPECTION, DISCOVERED THE AILERON LEFT DOWN CONTROL CABLE TO BE FRAYED. DETERMINED CABLE F RAYING CAUSED BY INCOMPLETE INSTALLATION OF PULLEY MOUNTING BRACKET. SECURED BRACKET , AND REPLACED PULLEY AND CABLE. (M) 2 L 7 2 4T RT A24CE 2002061800147 20020618 00147 CE 2002 6 18 2002F00631 1 20020428 A 2697 WIRE BEECH 1900 1900D 1154162 CE FIRE BOTTLE LOOSE A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 87550 UE205 FLT 9311 - SRQ-MIA - LEFT FIRE EXTINGUISHER DISCHARGE LIGHT CAME ON NUMEROUS OCCASIONS. SECURED LOOSE WIRE AT LEFT FIRE BOTTLE. OPERATIONAL TEST NORMAL. (M) 2 L 7 2 4T RT A24CE 2002061800148 20020618 00148 NM 2002 6 18 QXEA0200897 1 20020613 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH * 344 529 PDX- RED EMERGENCY EXIT LIGHT STRIP ON PANEL 133CZ IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT PS6. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNE TO SERVICE. 2 H 7 2 4T RT A13NM 2002061800149 20020618 00149 CE 2002 6 18 2002F00632 1 20020427 A 2620 WARNING SYSTEM BEECH 1900 1900D 1154162 CE COCKPIT FALSE ACTIVATION A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 87550 UE205 FLT 9281 - RSW-TPA - LEFT FIRE EXTINGUISHER DISCHARGE LIGHT CAME ON, FLICKERING NUMEROUS TIMES. INSPECTED SYSTEM. PERF ORMED ENGINE RUN. NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A24CE 2002061800150 20020618 00150 CE 2002 6 18 2002F00633 1 20020425 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE LT ENGINE FAULTY A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 19 81536 UE152 FLT 9428 - MCO-MIA - DURING FLIGHT, LEFT FIRE LOOP AMBER ANNUNCIATOR CAME ON. REMOVED AND REPLACED LEFT ENGINE FORWARD FIRE LOOP. OPERATIONAL TEST NORMAL. (M) 2 L 7 2 4T RT A24CE 2002061800151 20020618 00151 EU 2002 6 18 2002F00622 1 20020425 A 5320 S536780020402 SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2, FOUND FORWARD OUTBOARD HOLD DOWN SUPPORT PLATE FOR LAVATORY CORRODED. REMOVED AND REPLACED SUPPORT IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800152 20020618 00152 WP 2002 6 18 AALA20020759 1 20020526 A 2613 SENSOR DOUG DC9 DC983 3022083 WP A/C BAY MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 436AA 49454 ORD - FLT 1381 - EN ROUTE ORD-SAT, DURING CLIMB-OUT, THE TAIL COMPARTMENT TEMPERATURE HIGH WARNING LIGHT ILLUMINATED. C HECKLIST WAS RUN AND LIGHT EXTINGUISHED. IAW THE CHECKLIST, THE LEFT SUPPLY SWITCH WAS RETURNED TO THE AUTO POSITION AN D DURING CLIMB THE WARNING LIGHT ILLUMINATED AGAIN. IT EXTINGUISHED WHEN HIGH PRESSURE BLEED OFF WAS AGAIN SELECTED. R ETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED LEFT AND RIGHT TAIL COMPARTMENT OVERHEAT SENSORS. PERFORMED HIGH POW ER RUN UP. CHECKED DUCT COUPLINGS AND VALVES FOR LEAKS DURING RUNUP. NO LEAK NOTED, TAIL COMPARTMENT HIGH TEMPERATURE WARNING LIGHT DID NOT ILLUMINATE DURING HIGH POWER RUN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002061800153 20020618 00153 NM 2002 6 18 EIA2002024 1 20020330 A 5312 PRESSURE PANEL BOEING 747 747132 1384882 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MZJ - FOUND STATION 1241, LEFT WING GEAR WHEEL WELL, FORWARD SIDE SKIN WAS FOUND CORRODED. REPAIRED PER ECRA 479-57-157 -2. (M) 2 L 7 4 4F A20WE 2002061800154 20020618 00154 NM 2002 6 18 EIA2002026 1 20020330 A 5712 BULKHEAD BOEING 747 747132 1384882 NM RT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 FOUND RIGHT WING TRAILING EDGE CAVITY, LOWER BULKHEAD CHORD CRACKED AT APPROXIMATELY WBL 245, BELOW INTERSECTION OF NR 7 AND NR 8 SPOILERS. REMOVED DAMAGE AND REPAIRED PER ECRA 479-57-160-2. (M) 2 L 7 4 4F A20WE 2002061800155 20020618 00155 NM 2002 6 18 EIA2002027 1 20020330 A 5330 SKIN BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MZJ - FOUND 1.5 INCH CRACK AND SKIN BULGED AT STATION 2229, STRINGER 34L TO 36L, NEXT TO OUTFLOW VALVE. REMOVED DAMAGE AND REPAIRED PER ECRA 479-53-155-2. (M) 2 L 7 4 4F A20WE 2002061800156 20020618 00156 NM 2002 6 18 EIA2002031 1 20020330 A 5753 FAILSAFE BOEING 747 747132 1384882 NM T/E FLAP GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MZJ - NR 5 FLAP TRACK FORWARD ATTACH FITTING FAIL/SAFE BORE HAS DEEP GOUGE. REPAIRED PER ECRA 479-57-159-2. (M) 2 L 7 4 4F A20WE 2002061800157 20020618 00157 NM 2002 6 18 EIA2002034 1 20020331 A 5320 DOUBLER BOEING 747 747121 1384871 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND BS 1241 CANTED WEB DOUBLER WAS FOUND CORRODED AT RBL 55, JUST ABOVE VERTICAL STIFFENER. REMOVED CORROSION A ND REPAIRED PER ECRA 480-53-111-2. (M) 2 L 7 4 4F A20WE 2002061800158 20020618 00158 WP 2002 6 18 GTIA020451 1 20020413 A 5230 SUPPORT FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND MID LOWER CARGO DOOR HAS CRACK AT LOWER FORWARD BRACKET SUPPORT FITTING. REWORKED LOWER FORWARD BRACKET SUP PORT FITTING. DRILLED UP AND LOCATED NEW FITTING. INSTALLED FITTING. (M) 2 L 7 2 4F A6WE 2002061800159 20020618 00159 WP 2002 6 18 GTIA020452 1 20020429 A 5523 TRIM TAB DOUG DC9 DC982 3022082 WP ELEVATOR DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - LEFT ELEVATOR ANTI-FLOAT TAB HAS THREE DENTS AND AREAS OF DELAMINATION. REMOVED ANTI-FLOAT TAB. INSTALLED LEFT E LEVATOR ANTI-FLOAT TAB. (M) 2 L 7 2 4F A6WE 2002061800160 20020618 00160 WP 2002 6 18 GTIA020453 1 20020313 A 3411 PITOT TUBE DOUG DC9 DC981 3022081 WP PITOT/STATIC SYS LEAKING A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 806NK 48051 FTW - AUTO-PILOT IN IAS WOULD HUNT FOR THE AIRSPEED. LEAK CHECK ON CAPTAINS AND COPILOTS PITOT TUBE, BOTH PITOT TUBES F AILED LEAK CHECK. CAPTAINS AND FIRST OFFICERS LEAK CHECKS OF PITOT SYSTEMS ACCOMPLISHED. (M) 2 L 7 2 4F A6WE 2002061800161 20020618 00161 WP 2002 6 18 GTIA020454 1 20020417 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - MID CARGO FITTING STATION 827 RIGHT INBOARD CORRODED GOUGED AND BARE METAL. REMOVED CORROSION. FABRICATED FITTIN G. PART WAS INSTALLED. (M) 2 L 7 2 4F A6WE 2002061800162 20020618 00162 WP 2002 6 18 GTIA020455 1 20020403 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - MID CARGO FITTING STATION 827 LEFT INBOARD CORROSION GAUGES AND BARE METAL. REMOVED CORROSION. FABRICATED FITTIN G. PART INSTALLED. (M) 2 L 7 2 4F A6WE 2002061800163 20020618 00163 WP 2002 6 18 GTIA020456 1 20020405 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND MID CARGO STATION 788 TO 826 LONGERON FITTING 29R GOUGES, CHAFING CORROSION. FOUND LONG FITTING OUT OF LIMI TS. LOCATED AND DRILLING LONGERON 29R. PART INSTALLED. (M) 2 L 7 2 4F A6WE 2002061800164 20020618 00164 WP 2002 6 18 GTIA020457 1 20020403 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND MID CARGO STATION 788 TO 826 LONGERON 29L ELONGATED HOLES, GOUGES, AND CORROSION. FOUND LONGERON OUT OF LIM ITS. LOCATED AND DRILLING LONGERON 29L. PART WAS INSTALLED. (M) 2 L 7 2 4F A6WE 2002061800165 20020618 00165 WP 2002 6 18 GTIA020458 1 20020403 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND MID CARGO FITTING STATION 827 RIGHT INBOARD GAUGES BARE METAL. REMOVED CORROSION MATERIAL FOUND TO BE OUT O F LIMITS. FABRICATED A NEW FITTING. PART WAS INSTALLED ON 18-N-00375. (M) 2 L 7 2 4F A6WE 2002061800166 20020618 00166 WP 2002 6 18 GTIA020459 1 20020403 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND MID CARGO FITTING TWO STATION 827 OUTBOARD LEFT GAUGES, BARE METAL. REMOVED CORROSION MATERIAL FOUND TO BE OUT OF LIMITS. FABRICATED TWO NEW FITTINGS. PART WAS INSTALLED. (M) 2 L 7 2 4F A6WE 2002061800167 20020618 00167 WP 2002 6 18 GTIA020460 1 20020324 A 5320 BRACKET DOUG DC9 DC981 3022081 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND CORROSION BETWEEN L30 AND L29R AND ON STRAP AT FUEL TANK. MID CARGO STATION 779 TO 826 LONGERON FITTING L30 CHAFING, GAUGES, AND CORROSION. REMOVED CORROSION. FABRICATED NEW FILLER TWO DOUBLERS. INSTALLED FILLER AND DOUBLER. FABRICATED ANGLE AND STRAP. FABRICATED FINGER DOUBLER. INSTALLED REPAIR ANGLE,STRAP AND TRAP FILLER. AFTER FURTHER EVALUATION FOUND BRACKET BROKEN AT STATION 788 LONGERON 28L. DRILLED UP AND LOCATED NEW BRACKET. INSTALLED NEW BRACKET . (M) 2 L 7 2 4F A6WE 2002061800168 20020618 00168 EA 2002 6 18 REXA02006 1 20020425 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A REXA K NONE J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 SO 25 8409N 7409 FLAPS FAILED ON APPROACH WHEN SELECTED DOWN. QRH PROCEDURES FOLLOWED AND AN UNEVENTFUL 0-FLAP LANDING WAS PERFORMED. S YSTEM WAS RESET PER FAULT RESET PROCEDURES OF THE BOMBARDIER FIM AND IAW AD 98-20-01. SYSTEM OPERATIONALLY CHECKED GOOD . (M) 2 L 7 2 4F RT A21EA 2002061800169 20020618 00169 EA 2002 6 18 REXA02007 1 20020424 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A REXA K NONE J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 SO 25 8458A 3125 7458 FLAPS FAILED ON APPROACH WHEN SELECTED DOWN. QRH PROCEDURES FOLLOWED AND AN UNEVENTFUL 0 FLAP LANDING WAS PERFORMED. S YSTEM WAS RESET PER FAULT RESET PROCEDURES OF THE BOMBARDIER FIM AND IAW AD 98-20-01. SYSTEM OPERATIONALLY CHECKED GOOD . (M) 2 L 7 2 4F RT A21EA 2002061800170 20020618 00170 EA 2002 6 18 REXA02008 1 20020427 A 5242 057322 SEAL CNDAIR CL600 CL6002B19 1900309 EA E/E BAY DOOR TORN A REXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 25 8409N 7409 THROUGH 12,000 FEET A WHISTLE WAS HEARD COMING FROM THE SERVICE DOOR AREA. PILOTS LEVELED OFF AT 22,000 FEET AND A LOUD RUMBLING FROM THE SERVICE DOOR AREA WAS HEARD. PILOTS DROPPED TO 6000 FEET AND RUMBLE WENT AWAY. MAINTENANCE FOUND TH E SERVICE DOOR SEAL TO BE ROLLED OUT OF SILL, THE GALLEY DRAIN WAS LEAKING AND THE SEAL ON THE AVIONICS BAY DOOR WAS TOR N. THE SERVICE DOOR SEAL WAS PUT BACK INTO PLACE, THE DRAIN CHECK VALVE WAS CLEANED, AND THE AVIONICS BAY DOOR SEAL WAS REPLACED. AIRCRAFT WAS PRESSURIZED AN NO LEAKS WERE NOTED. (M) 2 L 7 2 4F RT A21EA 2002061800171 20020618 00171 NE 2002 6 18 S2YA02015 2 20020417 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT MAKING METAL A S2YA K NONE J WARNING INDICATION AP APPROACH 1 GL 13 881SK UE88 PCE114191 FLT 1270 - MKE-CMH - THE LEFT OIL PRESSURE ILLUMINATED IN FLIGHT. THE CREW MADE AN UNEVENTFUL LANDING. OUT STATION MAI NTENANCE SERVICED THE LEFT ENGINE WITH OIL AND THE CREW DID A GROUND RUN. AFTER SHUTDOWN OF THE GROUND RUN, THERE WAS F LAMES COMING OUT OF THE EXHAUST. THE CREW DISCHARGED THE FIRE BOTTLE. MKE MAINTENANCE TRAVELED TO CMH INSPECTED THE LE FT ENGINE AND FOUND METAL IN THE OIL. MAINTENANCE REPLACED THE LEFT ENGINE, ENGINE ACCESSORIES, FIRE BOTTLE AND THE PRO P. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 2002061800172 20020618 00172 CE 2002 6 18 S2YA02016 1 20020429 A 6123 15M1 SWITCH BEECH 1900 1900D 1154162 CE COCKPIT STICKS A S2YA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 13 891SK UE89 FLT 1454 - DAY-MKE - DURING TAKEOFF, THE RIGHT AUTO FEATHER DISABLE ANNUNCIATOR ILLUMINATED. THE CREW ABORTED THE TAKEO FF. THE A/C WAS FERRIED BACK TO MKE. MAINTENANCE REPLACED THE AUTO FEATHER SWITCHES IN THE POWER LEVER, OPS CHECK GOOD . (M) 2 L 7 2 4T RT A24CE 2002061800173 20020618 00173 EU 2002 6 18 SIMA200212126 1 20020417 A 5311 S536725406200 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2, FOUND FRAME 37 JUST ABOVE SERVICE DOOR SILL PLATE CORRODED. REMOVED AND REPLACED DOUBLER ON FRAME 3 7 IAW EO E1-5300-234. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800174 20020618 00174 EU 2002 6 18 SIMA200212129 1 20020419 A 5315 S53672407200000 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2, FOUND FLOORBEAM 38 CORRODED ON TOP AND BOTTOM SIDES AND AROUND NUTPLATE HOLES. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800175 20020618 00175 EU 2002 6 18 SIMA200212130 1 20020418 A 5313 S5367125722151 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2, FOUND STRINGER 17R CORRODED BETWEEN FS 35-37. INSTALLED NEW STRINGER 17R IAW ATR 42 SRM 51-25-01. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800176 20020618 00176 EU 2002 6 18 SIMA200212135 1 20020425 A 5320 S5367800822401 SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2, FOUND FORWARD OUTBOARD HOLD DOWN SUPPORT PLATE FOR LAVATORY CORRODED. REMOVED AND REPLACED SUPPORT IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800177 20020618 00177 EU 2002 6 18 SIMA200212136 1 20020425 A 5320 S536780092002 FLOOR SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2, FOUND FLOOR SUPPORT BETWEEN FS 36-38 BY PASSENGER DOOR SILL PLATE CORRODED. REMOVED AND REPLACED SU PPORT IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800178 20020618 00178 EU 2002 6 18 SIMA200212137 1 20020425 A 5320 S5367800822201 FLOOR SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2, FOUND LAVATORY FLOOR SUPPORT BETWEEN FLOORBEAM 39-40 CORRODED. REMOVED AND REPLACED SUPPORT IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800179 20020618 00179 EU 2002 6 18 SIMA200212138 1 20020426 A 5347 EPNE95300013023 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING CPCP2, FOUND LEFT AND RIGHT FLIGHT ATTENDANTS SEAT TRACKS TO BE CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E2-53MR-115RA. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800180 20020618 00180 EU 2002 6 18 SIMA200214108 1 20020517 A 5347 S53375001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP4 INSPECTION, FOUND LEFT FORWARD CARGO INBOARD SEAT TRACK WAS FOUND CORRODED. REMOVED AND REPLACED WIT H NEW LEFT FORWARD INBOARD SEAT TRACK IAW EO E1-53MR-271. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800181 20020618 00181 EU 2002 6 18 SIMA200214109 1 20020517 A 5347 S53376001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP4 INSPECTION, RIGHT FORWARD OUTBOARD SEAT TRACK FOUND CORRODED. REMOVED AND REPLACED RIGHT FORWARD OUT BOARD SEAT TRACK IAW EO E1-53MR-271. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800182 20020618 00182 EU 2002 6 18 SIMA200214110 1 20020517 A 5347 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP4 INSPECTION, RIGHT MIDDLE OUTBOARD SEAT TRACK CORRODED. REMOVED AND REPLACED RIGHT MIDDLE OUTBOARD SE AT TRACK IAW EO E1-53MR-271. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800183 20020618 00183 EU 2002 6 18 SIMA200214111 1 20020517 A 5315 S5367241020002 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP4 INSPECTION, FOUND LOWER FLOORBEAM AT FRAME 41 HAS NUMEROUS SPOTS OF CORROSION AROUND NUTPLATE HOLES. REMOVED AND REPLACED FLOORBEAM 41 IAW SRM 51-25-01. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800184 20020618 00184 EU 2002 6 18 SIMA200214112 1 20020517 A 5315 S5367240820202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP4 INSPECTION, FOUND FLOORBEAM AT FRAME 39 HAS NUMEROUS SPOTS OF CORROSION AROUND NUTPLATE HOLES. RAID FLOORBEAM IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002061800185 20020618 00185 WP 2002 6 18 ABXA010913 1 20020614 A 5610 LOCK DOUG DC8 DC861 3021952 WP OUT OF ADJUST A ABXA K NONE O OTHER NR NOT REPORTED 1 GL 23 852AX 46016 CAPTAIN'S SLIDING WINDOW WOULD NOT OPEN. ADJUSTED TOP WINDOW LOCK IAW DC-8 MM 56-10-03. 2 L 7 4 4F 4A25 2002061800186 20020618 00186 NM 2002 6 18 C8GA20020007 1 20020613 A 2610 69182537 DUCT BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE BLOWN A C8GA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 15 89427 21365 666201 Flt 202 from SVMI to KMIA. On take off from SVMI, the engine fire warning bell sounded with no fire light and all engine gauges checked normal. Performed engine fire loop test, #2 engine fire loop did not test. Performed emergency procedure s and shut down #2 engine and notified ATC. Air turnback to SVMI, aircraft landed without incident. Post flight inspecti on revealed that the 8th stage bleed air duct was damaged as well as the #2 engine fire loop. Replaced #2 engine pneumat ic duct as well as the #2 engine fire detector loop. Performed leak and engine fire detection system test IAW MM 36-00-1 and 26-11-01. Operational test good and aircraft returned to service. 2 L 7 3 4F 4 F A3WE E2EA 2002071600155 20020716 00155 NM 2002 7 16 F3LA200200171 1 20020612 A 3350 BATTERY PACK BOEING 737 7372L9 1384497 NM CABIN DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 270FL 22733 MAINTENANCE REPORTED SECTION OF EMERGENCY AISLE PATH LIGHTING IN FWD CABIN INOPERATIVE. FERRIED AIRCRAFT TO DEN FOR REP AIR. UPON ARRIVAL, REPLACED THE FWD BATTERY AND POWER SUPPLY ASSY. PERFORMED OPERATIONAL TEST AND CHECKED OKAY. 2 L 7 2 4F RT A16WE 2002061800187 20020618 00187 NM 2002 6 18 AWXA200200528 1 20020616 A 3350 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 0 0 24711 PHX - EEL - DURING INSPECTION OF ESCAPE PATH LIGHTING, MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT 21 INOPERAT IVE. MAINTENANCE REPAIRED WIRES NEAR EMERGENCY LIGHT PER CHAPTER 20 STANDARD PRACTICES. EMERGENCY LIGHT AT ROW 21 OPERA TIONALLY CHECKED GOOD. 2 L 7 2 4F RT A16WE 2002061800188 20020618 00188 NM 2002 6 18 S02832020 1 20020528 A 3200 BOEING BOEING 737 737800* NM CFMINT CFM56 CFM567B26US NE W SAJF O OTHER O OTHER LD LANDING 1 WP 03 28406 B18608 AFT LANDING GRD CHK FOUND TAIL STRIKE. TAILSKID WEAR SHOE WASS MISSING(FOUND IN KHH RUNWAY). THE GREEN PART OF WA RNING DECAL OF THE TAILSKID CARTRIDGE WAS NOT VISIBLE. APU ACCESS DOOR WAS FOUND A SMALL HOLE ON THE OUTER SKIN.C/A:738 AMM 05-51-32 INSPECTIONS WERE PERFORMED. TAILSKID CARTRIDGE IS RPLD PER AMM 32-71-00. APU DOOR SMALL HOLE IS REPAIRED PE R SRM 52-00-01. TAILSKID SKIRT DENT WAS REWORK PER SRM 53-80-70. AFT AMM 05-51-32 INSPECTIONS AND REPAIRES, A/C RETURN T O SERVICE SCHEDULED FLT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002061900001 20020619 00001 EA 2002 6 19 CA020531003 1 20020401 A 7603 2285058310 BRACE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENG CONTROL UNSECURE W E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA (CAN) A/C LEVELED OFF AT FL290. CREW ATTEMPTED TO THROTTLE BACK & NOTICED LT POWER LEVER JAMMED AT 95.1 PERCENT N1. QRH / INFLT SHUT-DOWN PERFORMED ON LT ENGINE & A/C DIVERTED. ALL ENGINE PARAMETERS INDICATED NORMAL AT ITS PRESENT POWER SE TTING PRIOR TO SHUT-DOWN. UPON ARRIVAL, FOUND STAY BRACE STRUT NOT SECURED & INCURRED LT POWERLEVER JAM. SPRING CLIP T HAT CONTAINS STAY BRACE STRUT & SECURING PIN WERE INSPECTED FOR CONDITION, SECURITY & OP. NO ANOMALIES WERE NOTED.STAY B RACE STRUT CORRECTLY POSED & SECURED, OPAL CHECKS PERFORMED & A/C RT-SRV. NO REOCCURRENCE REPORTED TO-DATE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061900002 20020619 00002 NM 2002 6 19 CA020531004 1 20020308 A 3020 VALVE DHAV DHC8 DHC8* NM PWC 150 PW150A EA DUAL DIST FAILED W O OTHER J WARNING INDICATION CL CLIMB 1 CA (CAN) DEICE PRESSURE CAUTION LIGHT ON DURING CLIMBOUT IN ICING CONDITIONS. ICE DETECTED WAS DISPLAYED ON ENGINE DISPLAY . AIRFRAME MODE SELECTOR: SLOW WAS SELECTED. ICING CONDITION EXITED AND AIRFRAME MODE SELECTOR SELECTED OFF. RESET OF FAULT CODES IN CDS PERFORMED.THE DE-ICE PRESSURE CAUTIONS REAPPEARED AGAIN 11 MAR. AN ENGINE RUN AND BOOT CHECK WAS PE RFORMED WITHOUT ANY REMARKS. RESET OF FAULT CODES IN CDS PERFORMED. FAULT CODE DDV 5A FAILED WAS NOTED. TEST PERFORMED IN ACC WITH AMM 30-11-00. DURING TEST NO GREEN LIGHT FOR THE OUTER RT TAIL BOOT WAS RECEIVED ON THE IRPS PANEL. DUAL DIS TRIBUTING VALVE REPLACED ACC TO AMM 30-11-16. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061900003 20020619 00003 NM 2002 6 19 SWAA021312 1 20020615 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED A2 CHECK, FOUND EEPLS COVERS CRACKED AT ROW'S 12 AND 9. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002061900004 20020619 00004 2002 6 19 SWAA021314 4 20020614 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061900005 20020619 00005 2002 6 19 SWAA021315 4 20020614 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061900006 20020619 00006 NM 2002 6 19 SWAA021316 1 20020614 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, ABOVE STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002061900007 20020619 00007 NM 2002 6 19 SWAA021317 1 20020616 A 5311 6546569 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS'S 827 AND 907, BETWEEN STR'S 8L AND 9L AND STR'S 8R AND 9R . REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2002061900008 20020619 00008 NM 2002 6 19 SWAA021318 1 20020615 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 935, ABOVE STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002061900009 20020619 00009 2002 6 19 SWAA021319 4 20020616 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR. LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061900010 20020619 00010 NM 2002 6 19 SWAA021322 1 20020615 A 5751 654645423A AILERON BOEING 737 7372H4 138448C NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING WALK AROUND INSPECTION, FOUND LT AILERON DELAMINATED ON BOTTOM SURFACE 1.5 INCHES OTBD OF AILERON TAB CUTOUT SUPP ORT BRACE. REMOVED AND REPLACED AILERON PER MM. 2 L 7 2 4F A16WE 2002061900011 20020619 00011 NM 2002 6 19 SWAA021323 1 20020614 A 5610 58935578 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT CRACKED A SWAA D RETURN TO BLOCK P NO WARNING INDICATION CL CLIMB 1 SW 29 758SW 27873 AIR TURN BACK, F/O SLIDING WINDOW CRACKED DURING CLIMB. REMOVED AND REPLACED F/O SLIDING WINDOW AND WINDOW HEAT CONTROL LER PER MM. 2 L 7 2 4F RT A16WE 2002061900012 20020619 00012 NM 2002 6 19 SWAA021324 1 20020611 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 080SW 22675 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 916 AND 918, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002061900013 20020619 00013 NM 2002 6 19 SWAA021325 1 20020615 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 095SW 23054 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 894, ABOVE STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002061900014 20020619 00014 NM 2002 6 19 SWAA021326 1 20020614 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 080SW 22675 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT WINDOW BELT CUTOUT ON LT WINDOW'S NR 1, 2, 3, 4, 5, 6, 7, 8 AND 9. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F A16WE 2002061900015 20020619 00015 NM 2002 6 19 SWAA021327 1 20020614 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 080SW 22675 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT WINDOW BELT CUTOUT ON RT WINDOW'S NR 4, 10 AND 11. REPAI RED SKIN PER SWA SI 11050-53. 2 L 7 2 4F A16WE 2002061900016 20020619 00016 NM 2002 6 19 SWAA021228 1 20020604 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 1/2D CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2002061900017 20020619 00017 NM 2002 6 19 SWAA021230 1 20020603 A 5330 6545776 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002061900018 20020619 00018 NM 2002 6 19 SWAA021231 1 20020604 A 2731 6959227 BUSHING BOEING 737 7373H4 1384600 NM BOTH ELEVATORS WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, BOTH LEFT AND RIGHT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH LEFT AND RIGHT ELEVATOR TAB LOCKOUT MECHANISM BUSHINGS AND LINKS PER MM. 2 L 7 2 4F RT A16WE 2002061900019 20020619 00019 NM 2002 6 19 SWAA021232 1 20020604 A 5210 6545871 FRAME BOEING 737 7375H4 138449D NM FWD ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR AFT FRAME CRACKED AT CUTOUT FOR 5TH STOP FROM BOTTOM. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002061900020 20020619 00020 NM 2002 6 19 SWAA021233 1 20020603 A 5210 6545871 FRAME BOEING 737 7375H4 138449D NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED AT CUTOUT FOR 3RD STOP FROM BOTTOM. REPAIRED FRAME PE R SRM. 2 L 7 2 4F RT A16WE 2002061900021 20020619 00021 NM 2002 6 19 SWAA021234 1 20020601 A 2612 4739551 CONTROL PANEL BOEING 737 7377H4 1384404 NM COCKPIT FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 29 708SW 27842 DECLARED EMERGENCY, DIVERSION, F/O SPILLED WATER ON CENTER CONSOLE. FWD CARGO FIRE LIGHT ILLUMINATED SOME TIME LATER. DIVERTED TO MCI, AFTER LANDING CONFIRMED THERE WAS NO FIRE. FIRE SUPPRESSION NOT UTILIZED. NO FIRE MASTER LIGHT OR BEL L AT ANY TIME. REMOVED AND REPLACED FIRE CONTROL PANEL PER MM. 2 L 7 2 4F RT A16WE 2002061900022 20020619 00022 NM 2002 6 19 SWAA021236 1 20020603 A 3230 80607 CIRCUIT CARD BOEING 737 7375H4 138449D NM E/E COMP ERRATIC A SWAA K NONE J WARNING INDICATION AP APPROACH 1 SW 29 514SW 25153 ON APPROACH EXTENDED LANDING GEAR. RIGHT MLG SHOWED RED WITH NO GREEN. RECYCLED LANDING GEAR, OPERATED NORMALLY. REMO VED AND REPLACED RT MLG DOWN LOCK CIRCUIT CARD M961 PER MM. 2 L 7 2 4F RT A16WE 2002061900023 20020619 00023 NM 2002 6 19 SWAA021237 1 20020604 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 080SW 22675 DURING WALK AROUND INSP FOUND FUSELAGE SKIN CRACKED AT BS 763, WL 186 AFT OF WING TO BODY FAIRING. REPAIRED SKIN PER SR M. 2 L 7 2 4F A16WE 2002061900024 20020619 00024 NM 2002 6 19 SWAA021238 1 20020605 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CENTER CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 LT OVERWING HATCH EMERGENCY EXIT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002061900025 20020619 00025 NM 2002 6 19 SWAA021240 1 20020605 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002061900026 20020619 00026 NM 2002 6 19 SWAA021242 1 20020604 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED C4 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW NR 14 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002061900027 20020619 00027 NM 2002 6 19 SWAA021243 1 20020605 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 987, WL 208 AND LBL 21.5 TO 25.5. REPAIRED FLOORBEAM PER BFG E R. 2 L 7 2 4F RT A16WE 2002061900028 20020619 00028 NM 2002 6 19 SWAA021244 1 20020605 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002061900029 20020619 00029 NM 2002 6 19 SWAA021245 1 20020605 A 5240 6545854 FRAME BOEING 737 7373H4 1384600 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED AT STOP CUTOUT, 4TH FROM TOP. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002061900030 20020619 00030 NM 2002 6 19 SWAA021247 1 20020605 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED BETWEEN STR'S 8L AND 9L, AT BS'S 400, 440 AND 480. REPAIRED FRA MES PER SRM. 2 L 7 2 4F RT A16WE 2002061900031 20020619 00031 NM 2002 6 19 SWAA021248 1 20020605 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED BETWEEN STR'S 8R AND 9R, AT BS'S 360, 400 AND 440. REPAIRED FRA MES PER SRM. 2 L 7 2 4F RT A16WE 2002061900032 20020619 00032 NM 2002 6 19 SWAA021249 1 20020604 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 322, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002061900033 20020619 00033 NM 2002 6 19 SWAA021250 1 20020604 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002061900034 20020619 00034 NM 2002 6 19 SWAA021251 1 20020604 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002061900035 20020619 00035 NM 2002 6 19 SWAA021252 1 20020604 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002061900036 20020619 00036 NM 2002 6 19 SWAA021253 1 20020604 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002061900037 20020619 00037 NM 2002 6 19 SWAA021294 1 20020611 A 5330 6545800 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF CUTOUT FOR FWD SVC DOOR. REPAIRED SKIN PER SWA ER. 2 L 7 2 4F RT A16WE 2002061900038 20020619 00038 NM 2002 6 19 SWAA021296 1 20020611 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 837, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002061900039 20020619 00039 NM 2002 6 19 SWAA021297 1 20020611 A 2731 65C26384 BEARING BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, LH ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEV ATOR NR 2, 3 AND 4 TAB HINGE BEARINGS PER MM. 2 L 7 2 4F RT A16WE 2002061900040 20020619 00040 NM 2002 6 19 SWAA021298 1 20020611 A 5330 6545769 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 081SW 22730 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, BL O. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F A16WE 2002061900041 20020619 00041 NM 2002 6 19 SWAA021299 1 20020609 A 2450 6556666 RECEPTACLE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER LD LANDING 1 SW 29 323SW 23344 DURING LANDING F/A REPORTED SPARKS COMING FROM ELECTRICAL OUTLET IN FWD GALLEY. INSPECTED, CLEANED AND ADJUSTED RECEPTA CLE PER MM. 2 L 7 2 4F RT A16WE 2002061900042 20020619 00042 NM 2002 6 19 SWAA021276 1 20020608 A 2731 65C26384 TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED A1 CHECK, SWA SI 11111-55, LEFT ELEVATOR NR 1, 2 AND 4 TAB HINGE BEARINGS WORN. REMOVED AND REPLACED L T ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002061900043 20020619 00043 NM 2002 6 19 SWAA021277 1 20020608 A 2731 BACB28AMO7 BUSHING BOEING 737 7373Q8 1384670 NM BOTH ELEVATORS WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED A1 CHECK, SWA SI 11111-55, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED B OTH LEFT AND RIGHT ELEVATOR TAB NR 1 HINGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002061900044 20020619 00044 NM 2002 6 19 SWAA021278 1 20020606 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002061900045 20020619 00045 NM 2002 6 19 SWAA021279 1 20020606 A 2731 65C26384 TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVAT OR TAB PER MM. 2 L 7 2 4F RT A16WE 2002061900046 20020619 00046 NM 2002 6 19 SWAA021282 1 20020605 A 5311 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 847, BETWEEN STR'S 27L AND 27R. REPAIRED SHEAR TIE PER SR M. 2 L 7 2 4F RT A16WE 2002061900047 20020619 00047 NM 2002 6 19 SWAA021283 1 20020605 A 5710 6545445 RIB BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN S-2 AND S-3. REPAIRED CHORD PER B FG ER. 2 L 7 2 4F RT A16WE 2002061900048 20020619 00048 NM 2002 6 19 SWAA021285 1 20020607 A 2731 6959227 BUSHING BOEING 737 7373H4 1384600 NM RH ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 632SW 27707 DURING SCHEDULED A1 CHECK, SWA SI 11111-55, FOUND RT ELEVATOR TAB LOCKOUT FWD MOUNT BUSHINGS WORN. REMOVED AND REPLACED TAB LOCKOUT MOUNT BUSHINGS. 2 L 7 2 4F RT A16WE 2002061900049 20020619 00049 NM 2002 6 19 SWAA021286 1 20020610 A 2731 65C26384 TAB BOEING 737 7373A4 1384585 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED A2 CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB P ER MM. 2 L 7 2 4F RT A16WE 2002061900050 20020619 00050 NM 2002 6 19 SWAA021288 1 20020610 A 2100 20405011 ACM BOEING 737 7372H4 138448C NM RT A/C BAY OVERTEMP A SWAA D RETURN TO BLOCK O OTHER CL CLIMB 1 SW 29 092SW 22964 AIR TURN BACK, DURING TAKEOFF CABIN BEGAN FILLING WITH SMOKE. REMOVED AND REPLACED RT AIR CYCLE MACHINE PER MM. 2 L 7 2 4F A16WE 2002061900051 20020619 00051 2002 6 19 SWAA021254 4 20020608 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061900052 20020619 00052 2002 6 19 SWAA021255 4 20020606 A 2565 65C19901 CABLE BOEING 737 7373Y0 1384671 NM AFT SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002061900053 20020619 00053 2002 6 19 SWAA021256 4 20020606 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002061900054 20020619 00054 2002 6 19 SWAA021258 4 20020607 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 796SW 27889 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061900055 20020619 00055 NM 2002 6 19 SWAA021259 1 20020607 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 796SW 27889 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002061900056 20020619 00056 2002 6 19 SWAA021261 4 20020609 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061900057 20020619 00057 NM 2002 6 19 SWAA021264 1 20020607 A 3350 65C34691 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 3 ABC. SECURED LIGHT PER MM . 2 L 7 2 4F RT A16WE 2002061900058 20020619 00058 NM 2002 6 19 SWAA021265 1 20020606 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 OVERHEAD BIN BULL NOSE EMERGENCY EXIT LENS MISSING AT ROW NR 22 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002061900059 20020619 00059 NM 2002 6 19 SWAA021268 1 20020607 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 11. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002061900060 20020619 00060 NM 2002 6 19 SWAA021272 1 20020605 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002061900061 20020619 00061 NM 2002 6 19 SWAA021273 1 20020607 A 2910 BACH8A04NN0264T LINE BOEING 737 7372H4 138448C NM MLG W/W LEAKING A SWAA B EMER. DESCENT J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 29 081SW 22730 DECLARED EMERGENCY, HYDRAULIC SYSTEM A FAILED DURING CLIMB-OUT. REMOVED AND REPLACED SYSTEM AILERON PCU LINE PER MM. 2 L 7 2 4F A16WE 2002061900062 20020619 00062 NM 2002 6 19 SWAA021274 1 20020609 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002061900063 20020619 00063 2002 6 19 SWAA021305 4 20020612 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061900064 20020619 00064 2002 6 19 SWAA021306 4 20020613 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061900065 20020619 00065 2002 6 19 SWAA021308 4 20020613 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002061900066 20020619 00066 NM 2002 6 19 SWAA021309 1 20020612 A 2731 BACB28AM07 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002061900067 20020619 00067 NM 2002 6 19 SWAA021310 1 20020613 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, WL 160 AND RBL 36. REPAIRED FRAME PER BFG ER. 2 L 7 2 4F RT A16WE 2002061900069 20020619 00069 2002 6 19 SWAA021300 4 20020611 A 2565 6551463 BRACKET BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 790SW 30604 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT HOOK FASTENER LOOSE. INSTALLED FASTEN ER PER MM. 2 L 7 2 4F RT A16WE 2002061900070 20020619 00070 NM 2002 6 19 SWAA021301 1 20020611 A 3350 101114 LENS BOEING 737 7373Y0 1384671 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002061900071 20020619 00071 NM 2002 6 19 SWAA021302 1 20020611 A 5753 6546429 TRACK BOEING 737 7372H4 138448C NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED C4 CHECK, FOUND LT WING OTBD FLAP, INBD TRACK, OTBD AFT TRACK ATTACH HOLE CRACKED. REMOVED AND REPLACE D NR 2 FLAP TRACK PER MM. 2 L 7 2 4F A16WE 2002061900072 20020619 00072 CE 2002 6 19 CA020531007 1 20020325 A 5311 5042002857 FRAME BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 18845 (CAN) LT AND RT FRAMES WERE FOUND CRACKED AT FLOOR LEVEL DURING FUSELAGE INSPECTION AS PER B100 MAINTENANCE MANUAL CHAPT ER 53-10-00. CRACKS EMANATED FROM THE RADIUS WHERE THE FLOOR STRINGER PASSES THROUGH THE FRAME. 1 L 7 2 3T 4 T A14CE E4EA 2002061900073 20020619 00073 WP 2002 6 19 0201909951 1 20020605 A 2780 DUCT DOUG DC9 DC932 3022066 WP L/E SLAT DAMAGED A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 9347 45827 UPON SLAT EXTENSION, THE SLAT DISAGREEMENT ANNUNCIATOR LIGHT ILLUMINATED AND THE AIRCRAFT ROLLED. COMPLIED WITH COM PRO CEDURES AND THE AIRCRAFT LANDED IN MSP WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT -T- DUCT OUTER TOP FORWARD POSITION DAMAGED FROM CONTACT WITH DOOR. ALSO, THE DOOR BUNGEE SPRING WAS BROKEN AND A LARGE WASHER WAS LOOSE. REPLAC ED THE DAMAGED PARTS. LEAK AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002061900074 20020619 00074 WP 2002 6 19 0201919951 1 20020525 A 5754 DOOR DOUG DC9 DC932 3022066 WP L/E SLAT DAMAGED A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 9347 45827 DURING APPROACH FOR LANDING WHEN SLATS EXTENDED, THE AIRCRAFT ROLLED TO THE LEFT. THE SLAT DISAGREEMENT LIGHT WAS ON AN D THE SLATS RETRACTED LIGHT WAS OUT. CREW CYCLED THE SLAT EXTENSION PROCEDURES AND THE SLATS AGREED AND NO TENDENCY TO ROLL. ALL INDICATIONS WERE GOOD AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT IN MSP. MAINTENANCE FOUND THE NR 8 TR ACK DOOR ON THE RIGHT WING DAMAGED AND THE SPRING STOP BROKEN. REPLACED THE DOOR, SPRING, AND SPRING STOP. LUBED PIVOT POINTS AND ADJUSTED SYSTEM. FUNCTIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002061900075 20020619 00075 CE 2002 6 19 CA020531008 1 20020527 A 2434 DRIVE GEAR ELECTROSYS 646655A1 CESSNA 414 414 2075908 CE CONT O520 TSIO520JB 17040 SO MCAULY 3AF32C 3AF32C505 GL ALTERNATOR DAMAGED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE FLIGHT, THE RT ALTERNATOR FAIL LIGHT CAME ON. AFTER LANDING THE ALTERNATOR WAS REMOVED.THE ALTERNATO R DRIVE GEAR FAILED CAUSING THE DRIVE GEAR TO SLIP AND NOT TURN THE ALTERNATOR. THE RUBBER SURROUNDING THE GEAR WAS HALF GONE. THE DRIVE GEAR WAS REPLACED. 1 L 7 2 3O 3 O RT A7CE E8CE 5 C P22EA 2002061900076 20020619 00076 NM 2002 6 19 02061801 1 20020614 A 5330 SKIN BOEING 757 75723A 1384967 NM FUSELAGE DENTED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 757NA 24567 TWO DENTS IN SKIN, BS 611 AND 615 AT STR 16L LBL 65. INSTALLED DOUBLER OVER DAMAGE; CUTOUT PER SRM 53-00-01 AND ER 02-0 687. 2 L 7 2 4F RT A2NM 2002061900077 20020619 00077 NM 2002 6 19 02061802 1 20020615 A 5313 STRINGER BOEING 757 75723A 1384967 NM FUSELAGE DENTED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 757NA 24567 STRINGER 16L DENTED AT BS 612 AND BS 617. REPAIRED AS PER SRM 53-00-03 FIGURE 201 AND ER 02-0687. 2 L 7 2 4F RT A2NM 2002061900078 20020619 00078 EU 2002 6 19 02167319 1 20020616 A 5210 MECHANISM JETAIR JETSTM JETSTM4101 1500501 EU PAX DOOR LACK OF LUBE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 319UE 41042 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE MAIN CABIN ENTRY DOOR WAS DIFFICULT TO CLOSE. MAINTENANCE PERSO NNEL LUBRICATED THE MAIN CABIN DOOR OPERATING MECHANISMS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RE TURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002061900079 20020619 00079 EA 2002 6 19 02167633 1 20020616 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN NOT SEATED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 633BR 7274 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT AN EMERGENCY FLOOR TRACK LIGHT STRIP WAS INOPERATIVE. MAINTENANCE P ERSONNEL RESEATED THE EMERGENCY FLOOR TRACK LIGHT STRIP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RET URNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002061900080 20020619 00080 WP 2002 6 19 2002F00621 1 20020607 A 5210 AEH6333002 GEARBOX LKHEED 1011 10113853 5265020 WP L2 DOOR FAILED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 161AT 63337 63337 1219 DURING SCHEDULED INSPECTION THE L2 DOOR FAILS TO GO OPEN IN EMERGENCY MODE. MAINTENANCE REMOVED AND REPLACED FORWARD L2 DOOR GEARBOX IN ACCORDANCE WITH MM 52-12-04. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A23WE 2002061900081 20020619 00081 EU 2002 6 19 2002F00623 1 20020609 A 3242 BRAKE ASSY ISRAEL 1124 1124A 4500103 EU GARRTT TFE731 TFE73131G 29003 NE MLG LOCKED E K NONE M OVER TEMP LD LANDING 1 CE 05 118MP 340 UPON LANDING THE NR 1 BRAKE LOCKED OVERHEATING THE BRAKE. THE HEAT DAMAGED THE BRAKE, WHEEL AND AXLE. THE WHOLE ASSEMB LY WAS REPLACED AND FUNCTION CHECK SATISFACTORY. 2 M 7 2 4F 4 F A2SW E6WE 2002061900082 20020619 00082 NE 2002 6 19 ARWA20020601 2 20020614 A 7530 B-NUT DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE LOOSE A ARWA C ABORTED TAKEOFF J WARNING INDICATION CL CLIMB 1 SO 19 441J 53458 1068 45988 671378 ABORTED TAKEOFF DUE TO NR 4 ENGINE WOULD NOT GO TO MAX POWER. FOUND COMPRESSOR BLEED ACTUATOR TO CONTROL CLOSED TUBE B- NUT LOOSE; TIGHTENED B-NUT IAW MM 75-30-2; PERFORMED FLAG CHECK ENGINE RUN UP OPS CHECKED NORMAL IAW MM 75-30-3 AND 71-0 0 MAX TAKEOFF POWER (187). 2 L 7 4 4F 4 F 4A25 1E8 2002061900083 20020619 00083 NM 2002 6 19 AWXA200200521 1 20020523 A 5315 BAC1518338 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 LCQ - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON FLOORBEAM UPPER CHORD SURFACE AT BS 377, LBL 15, WL 208. MAINTENANCE REMOVED 64 INCHES CORRODED SECTION OF UPPER CHORD; FABRICATED A NEW CHORD, 2 REPAIR ANGLES, AND 2 STRAPS; IN STALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, FIG 203, PG 209-213. 2 L 7 2 4F RT A2NM 2002061900084 20020619 00084 NM 2002 6 19 AWXA200200522 1 20020614 A 2910 AE90432N FITTING BOEING 737 7373S3 1384711 NM HYD SYSTEM STUCK A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 316AW 23713 PHX- AIR TURNBACK- FLT 0663- ON DEPARTURE OUT OF PHOENIX EN ROUTE TO SNA, THE REPORT BY THE PILOT STATED THAT A LOSS OF -B- SYSTEM HYDRAULICS HAD OCCURRED AND THAT THE AIRCRAFT WAS RETURNING TO PHOENIX. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FOUND THE GROUND SERVICING PRESS MODULE QUICK DISCONNECT STUCK OPEN. MAINTENANCE PROCEEDED TO REMOVE AND REP LACE THE QUICK DISCONNECT FITTING, SERVICED HYDRAULICS, BLED SYSTEM LEAK AND OPERATIONAL TESTS WERE SUCCESSFUL. 2 L 7 2 4F RT A16WE 2002092000088 20020920 00088 NM 2002 9 20 AWXA200200523 1 20020615 A 2913 5509808 PUMP BOEING 737 7373S3 1384711 NM NR 2 ENGINE LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 316AW 64324 4480 23713 PHX - AIR TURN BACK - FLT 0320 - ON DEPARTURE FROM PHX EN ROUTE FOR ACA THE HYDRAULIC PUMP B-ENGINE NR 2 LIGHT ILLUMINAT ED. B-SYSTEM HYDRAULIC QUANTITY DROPPED TO APPROXIMATELY 3/8 FULL, PRESSURE WAS GOOD. MAINTENANCE FOUND NR 2 ENGINE DR IVEN HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP, PERFORMED ENGINE RUNS, NO MALFUNCTIONS OR LEAKS NOTED PER TASK CARD R5M29002. HYDRAULIC PUMP WAS CONFIRMED FAILURE BY VENDOR. 2 L 7 2 4F RT A16WE 2002072200035 20020722 00035 2002 7 22 AWXA200200524 4 20020615 A 3442 87292325V04 COMPUTER AIRBUS 320 A320231 3930325 EU RADAR SYS FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 637AW 5117 1594 099 IND - DIVERSION - FLT 0468 - EN ROUTE FROM IND TO LAS DURING CRUISE AIRCRAFT EXPERIENCED WEATHER RADAR PROBLEMS RESULTIN G FROM AN MEL APPLIED TO THE AEVC SYSTEM THAT RESULTED IN THE ANOMALY WITH THE WEATHER RADAR SYSTEM OCCURRING. DUE TO W EATHER CONDITIONS, AIRCRAFT DIVERTED TO DFW WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AEVC COMPUTER PER MM 21-26-34-04. PERFORMED AVIONICS EQUIPMENT VENTILATION TEST PER MM 21-26-00-05. AEVC AND SYSTEM TEST OK. VENDOR BEN CH TEST OF AEVC COMPUTER CONFIRMED FAILURE OF UNIT CITING PROBLEM AS SKIN TEMPERATURE LEVELS DRIFT. REPLACED U15 TO CORR ECT DRIFT, AND RETESTED UNIT PER CMM 21-26-34. 2 L 7 2 4F RT A28NM 2002061900085 20020619 00085 SO 2002 6 19 C2XA02BT023 1 20020614 A 2750 FLAP EMB 145 EMB145LR 3260212 SO WING MALFUNCTIONED A C2XA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 27 48901 145501 BHM/EWR---CO3374, CREW REPORTED, FLAP FAIL INFLIGHT, NO RESET. DECLARED EMERGENCY AIRCRAFT LANDED UNEVENTFULLY. MAINTE NANCE PERFORMED FLAP RESET. VISUALLY INSPECTED FLAPS, NO DEFECTS NOTED. OPERATED AND INSPECTED FLAPS IAW EMB145 MM 27- 50-00. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2002061900087 20020619 00087 SO 2002 6 19 C2XA02SH009 1 20020612 A 5315 14522226003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12921 145354 SHV- DURING C-CHECK INSPECTION, MULTIPLE AREAS OF CORROSION WERE FOUND ON THE LAV COMPARTMENT FLOORBEAM GUSSETTS. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED GUSSETTS IN ACCORDANCE WITH EMB-145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002061900088 20020619 00088 SO 2002 6 19 C2XA02TY101 1 20020615 A 5210 14533333401 SKIN EMB 145 EMB145 3260210 SO PAX DOOR DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 TYS DURING A SCHEDULED 1C/2C INSPECTION,THE PAX DOOR HAD TWO DENTS IN THE MIDDLE OF THE DOOR. A GST WAS USED TO MAKE T HE REPAIR (GST 1906/02) WHICH STATED REMOVE PAINT, RECONTOUR THE DENTED AREA, PERFORM A DYE-PENETRANT INSPECTION, NO CRA CK WAS FOUND. AREA WAS ALODINED, PRIMED AND PAINTED IAW WITH THE GST AND EMB 135/145 CPM 51-21-04-05-06. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF ALL 1C/2C INSPECTION. 2 L 7 2 4F RT T00011AT 2002061900089 20020619 00089 SO 2002 6 19 C2XA02TY103 1 20020615 A 5210 14533333401 SKIN EMB 145 EMB145 3260210 SO PAX DOOR DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 TYS DURING A 1C/2C INSPECTION THE MAIN DOOR FWD OF THE HANDLE HAD A DENT IN IT, MAINTENANCE TO REMOVED THE PAINT, RECO NTOUR THE DENTED AREA, PERFORM A DYE PENENTRANT INSPECTION AND NO CRACK WAS FOUND. CONTOURED DENT, ALODINED, PRIMED AND PAINTED. ALL WORK WAS ACCOMPLISHED IAW GST 1609/02--EMB 135/145 CPM 51-21-04-05-06. AIRCRAFT WILL BE RELEASED UPON CO MPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002061900090 20020619 00090 SO 2002 6 19 C2XA02TY104 1 20020617 A 5320 14521725401 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 TYS, DURING A SCHEDULED INSPECTION THE SERVICE DOOR, FORWARD SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE AFFECTED AREA, PERFORMED DYE-PEN. INSPECTION, ALODINED AND PRIMED IAW-GST-1886/02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002061900091 20020619 00091 EU 2002 6 19 DHL2002366005 1 20020614 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 01 366DH 249 ENGINE NR 2 LOOP -A- LIGHT ILLUMINATED. COMPLIED WITH ABNORMAL PROCEDURE. OPEN ENGINE, CHECKED BOTH FIRE LOOPS; FOUND OK. REPOSITIONED -A- LOOP AS A PRECAUTION. TESTED FIRE LOOPS AS PER MM 26-12-00. 2 L 7 2 4F RT A35EU 2002061900092 20020619 00092 EU 2002 6 19 DHL2002366006 1 20020615 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE CHAFED A DHLA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 01 366DH 249 ENGINE NR 2 LOOP -A- ILLUMINATED WITH MWP. CONDUCTED ABNORMAL PROCEDURE. BELOW PYLON AND JUST ABOVE HIGH PRESSURE VALV E, FOUND FIRE LOOP WIRES CHAFING. SECURED CLAMP WITHOUT INSULATION. REPOSITIONED WIRES, REMOVED & REPLACED CLAMP. CHE CKED SYSTEM AS PER MM 26-12-00. GROUND OPS CHECKED OK. 2 L 7 2 4F RT A35EU 2002061900093 20020619 00093 WP 2002 6 19 DHL2002803007 1 20020615 A 2611 SMOKE DETECTOR DOUG DC8 DC873 302199C WP NR 7 INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 803DH 46123 NR 7 SMOKE DETECTOR NOT TESTING. RELAMPED NR 7 SMOKE DETECTOR AND OP CHECKED IAW DC-8 70 SERIES M/M 26-0, OP CHECKS GOO D. 2 L 7 4 4F RT 4A25 2002061900094 20020619 00094 NM 2002 6 19 DL76G020612 1 20020601 A 2710 285T0017201 CONTROL UNIT BOEING 767 767324 1385203 NM E/E BAY MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 394DL 27394 IN CRUISE LOST LEFT SYMBOL GENERATOR FOLLOWED 5 MINS LATER BY RUDDER RATIO AND AILERON LOCKOUT EICAS MSGS AND LOSS OF AL L 3 AUTOPILOTS. FOUND LEFT SAM W/ FAULT BALL. WILL NOT RESET. CYCLED 1L AND 2LAC AND DC FLT CTL ELEC C/B'S. ALL FAUL TS CLEARED. REPLACED 1L AND 2L CSEUS AS PRECAUTION. RERACKED LEFT SYMBOL GEN. ALL OPS OK. PERFORMED TEST 40 FOR A/P. CHECKS OK. 2 L 7 2 4F RT A1NM 2002061900098 20020619 00098 EA 2002 6 19 ASOA02283 1 20020520 A 3350 1317 LAMP BRUCE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 875AS 7559 DURING A SCHEDULED INSPECTION, THE RIGHT EXTERNAL EMERGENCY LIGHT AFT OF THE WING WAS FOUND INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE BURNT OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A21EA 2002061900099 20020619 00099 EU 2002 6 19 CA020531009 1 20020528 A 2110 139312 SUPERCHARGER BRAERO 748 HS7482B 1500248 EU RROYCE DART DART532* EU CABIN PRESSURE FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) DURING CRUISE FLIGHT, THE CREW NOTICED THAT THE CABIN PRESSURE WAS FLUXUATING ABNORMALLY. THE CREW SELECTED MANUAL OPERATION AND SELECTED THE NR 1 SOURCE AND CONTINUED THE FLIGHT TO DESTINATION. MAINTENANCE FOUND THAT THE NR 1 SUPERCH ARGER HAD FAILED. BOTH ROTORS WERE MISSING LARGE SECTIONS OF ROTOR MATERIAL AND THE DRIVE QUILL SHAFT WAS SHEARED. THE FAILED SUPERCHARGER HAD UNDERGONE AN OPERATOR INSTIGATED ROTOR INSPECTION AT 500 HRS TSO WITH NO DEFECTS NOTED. 2 L 7 2 3T 4 T A24EU E297 2002061900103 20020619 00103 NM 2002 6 19 CA020531010 1 20020130 A 3297 CONNECTOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA BRAKE SYS FAILED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) AFTER LANDING BEFORE A/C CAME TO FULL STOP, RT OUTBOARD TIRE BLEW. WAITED ON RWY FOR INSPECTION AND TO ALLOW TIR ES TO COOL DOWN. JUST BEFORE A/C CAME TO FULL STOP IT FELT AS IF BRAKES LOCKED. HAPPENED TWICE IN SHORT SEQUENCE. LAST TIME WITH LOUD BANG, WITH SMOKE OUTSIDE A/C. COULD SMELL BURNED RUBBER. LANDING & RETARDATION NORMAL. MAIN WHEELS NR 3 & 4 REPLACED IAW AMM 32-41-01. A/C RELEASED FOR SERVICE. BRAKE PROBLEMS REOCCURRED NEXT DAY WHEN INBOARD ANTI SKI D FAULT CAME ON DURING LANDING ROLL. A WIRE FAULT IN PLUG P41 FOUND. WIRES REPLACED & TEST PERFORMED IAW AMM 32-46-00 W ITHOUT REMARKS. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061900105 20020619 00105 CE 2002 6 19 GLBA2002085 1 20020614 A 3610 TUBE BEECH 1900 1900D 1154162 CE WING DAMAGED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 100UX UE100 RT BLEED AIR FAILED IN FLIGHT. FOUND CHAFED HOLE IN EVA TUBING RT WING. REPAIRED HOLE. 2 L 7 2 4T RT A24CE 2002061900106 20020619 00106 SW 2002 6 19 CA020531011 1 20020524 A 8097 MS24185D1 RELAY GULSTM 690TP 690 0141720 SW GARRTT TPE331 TPE3315251K NM STARTER BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) RT ENGINE STARTED WITH NO PROBLEMS. LT ENGINE START SWITCH ACTIVATED, BUT PROP ROTATION VERY SLOW. ACFT AMMETER OBSERVED TO BE AT MAX DEFLECTION. CABIN BEGAN TO FILL WITH SMOKE. ACFT SHUTDOWN & EVACUATED. LT STARTER RELAY F OUND T O HAVE OVERHEATED CAUSING FIRE IN JUNCTION BOX. FIRE CONTAINED WITHIN JUNCTION BOX & EXTINGUISHED WHEN ACFT SHUTDOWN. SOME JUNCTION BOX WIRING & 2 RELAYS ABOVE LT STARTER RELAY WERE ALSO DAMAGED BY FIRE: JUNCTION BOX REMOVED FROM A/C, T HOROUGHLY INSPECTED & DAMAGED WIRING REPLACED OR REPAIRED, DAMAGED RELAYS WERE REPLACED, ACFT STRUCTURE BEHIND JUNCTIO N BOX INSPECTED FOR DAMAGE, NONE FOUND. JUNCTION BOX REINSTALLED & ALL ASSOCIATED SYSS WERE TESTED. 1 H 7 2 3T 4 T 2A4 E2WE 2002061900107 20020619 00107 2002 6 19 GLBA2002086 4 20020616 A 3445 80510001004 COMPUTER EMB 120 EMB120ER 3260203 SO TCAS FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 299UX 15332 120299 TCAS FAILS AND BOTH TRANSPONDERS FAIL. REMOVED AND REPLACED TCAS PROCESSOR, OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002061900109 20020619 00109 NM 2002 6 19 CA020531012 1 20020127 A 2721 682015 SWITCH DHAV DHC8 DHC8* NM PWC 150 PW150A EA RUDDER TRIM FAILED W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA (CAN) WHEN SETTING TAKEOFF POWER, CONFIGURATION WARNING SOUNDED. NO OTHER NON-NORMAL INDICATIONS WERE INDICATED. TAKEOF F WAS ABORTED IMMEDIATELY, AT APPROX 30KTS. INVESTIGATION SHOWS THAT INTERMITTENT T/O CONFIGURATION WARNING HAD OCCUR RED SEVERAL TIMES. DESPITE SEVERAL TESTS. NO INDICATION OF FAULTS HAVE BEEN FOUND. IT WAS COMPLAINED ABOUT SLOPPY FUNC TION OF RUDDER TRIM SWITCH, TOO FAST AND STARTED IN OPPOSITE DIRECTION. CONSEQUENTLY SWITCH WAS REPLACED. A/C RETURNED TO SERVICE. NO FURTHER COMPLAINT OF T/O CONFIGURATION OR RUDDER TRIM HAS BEEN ENTERED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061900110 20020619 00110 NM 2002 6 19 CA020531013 1 20020319 A 3246 TIRE DHAV DHC8 DHC8* NM PWC 150 PW150A EA MLG FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA (CAN) DURING ROLLOUT AFTER LANDING A LOUD BANG WAS HEARD AT APPR. 80-90 KTS. INSPECTION SHOWED THAT THE RT OUTER MLG TIR E HAD EXPLODED. BRAKES WAS NOT APPLIED HEAVILY DURING ROLLOUT. AIRCRAFT WAS TAXIED TO PARKING WITH NO DIRECTIONAL CONT ROL DIFFICULTIES. INVESTIGATION/ACTIONBOTH RT MAIN LANDING GEAR WHEELS REPLACED ACC AMM 32-40-01. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002071200013 20020712 00013 SO 2002 7 12 ASOA02200S 1 20020330 A 5753 12026501002 RIB EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE T/E FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 242AS 35000 120069 DURING HANGER MAINTENANCE, THE RIGHT WING INBOARD FLAP INBOARD TRACK SUPPORT RIB WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE FLAP SUPPORT RIB IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002061900112 20020619 00112 EU 2002 6 19 MALA020336 1 20020607 A 5347 SEAT TRACK SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING 4Y/2Y-CHECK IN CWA, RT I/B GALLEY SEAT TRACK TOP AND PROFILE HAVE CORROSION. MAINTENANCE REMOVED CORROSION IAW S RM 51-70-40 ON PROFILE. 2 L 7 2 4T RT A52EU 2002061900113 20020619 00113 GL 2002 6 19 CA020531014 2 20020522 A 7210 6789595 FILTER ALLSN CVAC 580 580 2422806 WP ALLSN 501D 501D13 03004 GL RGB CONTAMINATED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE THE CREW NOTICED THAT THE NR 2 ENGINE RGB OIL PRESSURE WAS DROPPING, THE ENGINE WAS SHUT DOWN AT 12 0 PSI. MAINTENANCE CREW CHECKED THE INDICATION SYSTEM AND FOUND IT TO BE SERVICEABLE. THE RGB MAGNETIC PLUG WAS INSPECT ED AND NO CONTAMINATION WAS FOUND. THE RGB OIL FILTER WAS REMOVED AND FOUND TO BE CONTAMINATED WITH HYLOMAR. THE FILTER WAS CLEANED AND REINSTALLED. THE ENGINE WAS GROUND RUN FOR 20 MINUTES IN HIGH RPM, RGB OIL PRESSURE WAS INDICATING 175 P SI. ENGINE WAS LEAK CHECKED AND FOUND SERVICEABLE. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT E282 2002061900114 20020619 00114 EU 2002 6 19 MALA020337 1 20020607 A 5347 7253721459 SEAT TRACK SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING 4Y/2Y-CHECK IN CWA, RT GALLEY SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED AND REPLACED GALLEY TRACK. 2 L 7 2 4T RT A52EU 2002061900115 20020619 00115 CE 2002 6 19 CA020603002 1 20020530 A 3222 04425037 FORK CESSNA 044250413 CESSNA 150 152 2071835 CE LYC O235 O235L2C 41505 EA OLEO STRUT ASSY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE OLEO ASSEMBLY WAS REMOVED FROM THE AIRCRAFT TO BE INSPECTED AND REBUILT. UPON INSPECTION OF THE INDIVIDUAL COM PONENTS, IT WAS DETERMINED THAT THE FORK WAS CRACKED ON THE OUTER SIDE NEAR THE TOP COLLAR. VERIFICATION OF THE CRACK WA S MADE WITH A 10X MAGNIFIER AND THE PART WAS SUBSEQUENTLY QUARANTINED. A NEW REPLACEMENT PART IS ON ORDER FOR THE ASSEM BLY.THE CAUSE OF THE DEFECT IS LIKELY FROM FATIGUE AS A RESULT OF BEING USED IN A FLIGHT TRAINING ENVIRONMENT FOR MANY Y EARS. THIS IS THE THIRD FINDING OF THIS TYPE FROM THE SAME FLEET. 1 H 7 1 3O 3 O NT 3A19 E223 2002061900116 20020619 00116 EU 2002 6 19 MALA020338 1 20020607 A 5311 FRAME SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING 4Y/2Y-CHECK IN CWA, WEB TOP OF FRAMES 294 & 288 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002061900117 20020619 00117 NM 2002 6 19 CA020603003 1 20020524 A 3243 82920010177 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PARKING BRAKE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) PARK BRAKE CONTROL VALVE LINE FOUND LEAKING IN RT ARMPIT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061900118 20020619 00118 EU 2002 6 19 MALA020339 1 20020609 A 5311 FRAME SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING 4Y/2Y-CHECK IN CWA, FOUND FRAME TOP CORRODED AT STA 272. MAINTENANCE COMPLETED REPAIR IAW EO S53102. 2 L 7 2 4T RT A52EU 2002061900119 20020619 00119 EU 2002 6 19 MALA020340 1 20020609 A 5320 7253721471 ANGLE SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING 4Y/2Y-CHECK IN CWA, RT SIDE OF FRAME STA 272 TOP ANGLE AND FRAME TOP HAVE CORROSION. MAINTENANCE REMOVED CORROSI ON IAW 51-70-40, INSTALLED NEW ANGLE IAW SRM 51-20. 2 L 7 2 4T RT A52EU 2002061900120 20020619 00120 NE 2002 6 19 CA020603004 2 20020530 A 7261 519587 CASE CNDAIR CL215 CL2151A10 1900320 EA PWA R1340 CWASP 52016 NE LT ENGINE STRIPPED W E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA (CAN) FLIGHT CREW OBSERVED OIL LEAKING FROM LT ENGINE AND INITIATED A PRECAUTIONARY ENGINE SHUTDOWN. AIRCRAFT LANDED SA FELY WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NOSE CASE PLUG THREADS HAD STRIPPED IN CASE. NOSE CASE WAS REPLACED AN D AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4R 3 R RT A14EA ATC14 2002061900121 20020619 00121 EU 2002 6 19 MALA020342 1 20020612 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 DURING 4Y/2Y-CHECK IN CWA, U-CHANNEL FLOORBOARD INTERCONNECT PIECES IN FWD CABIN AREA HAVE MINOR CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-20-42 AND 51-70-40. APPLIED PRIMER AND TOP COAT IAW SRM 51-20-43. 2 L 7 2 4T RT A52EU 2002061900122 20020619 00122 EU 2002 6 19 MALA020343 1 20020612 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 DURING 4Y/2Y-CHECK IN CWA, LT BEAM ANGLE BETWEEN STA 236.5 TO 258 HAS CORROSION. MAINTENANCE BLENDED OUT SURFACE CORROS ION ON LT BEAM ANGLE IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002061900123 20020619 00123 NM 2002 6 19 CA020603005 1 20020524 A 7922 45E041 CONTROL VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE OIL TEMP FAILED W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKEOFF RT OIL TEMPRATURE CLIMBED ABOVE 100 C INTO THE YELLOW ARC. AIRCRAFT RETURNED FOR LANDING. NR 2 ENG OIL TEMP CONTROL VALVE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061900124 20020619 00124 EU 2002 6 19 MALA020344 1 20020612 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 DURING 4Y/2Y-CHECK IN CWA, TOP FRAME ANGLE AT STA 258 HAS CORROSION. MAINTENANCE BLENDED OUT CORROSION IAW SAAB SRM 57- 70-40. 2 L 7 2 4T RT A52EU 2002061900125 20020619 00125 NE 2002 6 19 CA020603006 2 20020528 A 7322 39145217CL1 CARBURETOR CNDAIR CL215 CL2151A10 1900320 EA PWA R2800 R2800CA3 52026 NE HAMSTD 43E 43E60 NE ENGINE LEAKING W K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) DURING MAINTENANCE THE CREW WAS IN THE ENGINE SECTION AND THERE WAS A STRONG ODOUR OF FUEL PRESENT. THE FUEL SYST EM WAS PRESSURIZED ON THE ENGINE AND FUEL WAS NOTED COMING FROM THE CARB. THE MIXTURE CONTROL SHAFT SEAL NUT WAS FOUND S EPERATED FROM THE CARBURETOR. THE THREADS FOR THE NUT HAD BROKEN AWAY FROM THE CARB BODY. A SERVICEABLE CARBURETOR WAS I NSTALLED, LEAK CHECKED AND THE ENGINE WAS GROUND RUN CHECKED SERVICEABLE. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4R 4 R RT A14EA 5E8 6 C P871 2002061900126 20020619 00126 EU 2002 6 19 MALA020350 1 20020607 A 3350 501122804 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 15 362PX 340B258 DURING TAXI ON FLIGHT 2952 EMERGENCY POWER LIGHTS ILLUMINATED. MAINTENANCE REPLACED POWER PACK. 2 L 7 2 4T RT A52EU 2002061900127 20020619 00127 EA 2002 6 19 CA020604001 1 20020530 A 2710 AILERON CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT & RT JAMMED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA 12189 (CAN) AT FLIGHT LEVEL 310 AILERON SYSTEM PARTIALLY JAMMED RT AILERON 2 UNITS UP. REQUESTED LOWER ALTITUDE FLIGHT LEVEL 280 AND AILERON IMPROVED. AIRCRAFT FLOWN MANUALLY, APPROACH NORMAL (SUSPECT CABLE RUN HUMIDITY/FROZEN) AILERON REAR LT & RT QUADRANT LUBRICATED AND FUNCTIONAL (MANUAL) CHECKED SERVICEABLE AS PER MM 27-11-00 2 L 7 2 4F 4 F RT A21EA E15NE 2002061900128 20020619 00128 NE 2002 6 19 MALA020351 2 20020611 A 7297 WIRE HARNESS SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE FAULTY A MALA O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 GL 15 436XJ 340B436 DURING FLIGHT 3320, HAD A UNCOMMANDED AUTO COARSEN EVENT. EVENT OCCURRED DURING APPROACH TO CRW, AT 1,000 FT AGL. RT E NGINE AUTO COARSEN, ENGINE CONTINUED TO RUN, LANDED NORMALLY. MAINTENANCE BORESCOPED RT ENGINE, NO DEFECTS NOTED. REMO VED AND REPLACED RT PROP AND RT ENGINE HARNESS IAW TASK CARD 6110-303 AND GE SEI-576 CHAP 72. ALL OPERATIONAL CHECKS GO OD. 2 L 7 2 4T 4 T RT A52EU E8NE 2002061900129 20020619 00129 WP 2002 6 19 MWEA020408 1 20020617 A 5313 591143271 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT ACCESSORY COMPARTMENT LONGERON 2 LEFT AND HAS A CRACK AT STATION 1076. REMOVED DAMAGED SECTION 2 LEFT, FABRICATED, INSTALLED LONGERON. INSTALLED REPAIR SPLICE. 2 L 7 2 4F A6WE 2002061900130 20020619 00130 NM 2002 6 19 CA020604002 1 20020602 A 3230 5114904 PTU DHAV DHC8 DHC8* NM PWC 150 PW150A EA MLG UNSERVICEABLE W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER GEAR UP SELECTION THERE WAS A FAILURE OF THE NR 2 HYDRAULIC SYSTEM (PRESSURE ZERO,QUANTITY NORMAL). GEAR STA YED IN TRANSITION AND THE PTU ALSO FAILED. AFTER GEAR RECYCLED NORMAL PRESSURE INDICATIONS AND OPS AGAIN, BUT THE PTU RE MAINED U/S. RELANDING PERFORMED AND AIRCRAFT HANDED OVER TO MAINTENANCE.THE POWER TRANFER UNIT (PTU) WAS REPLACED AND TH E AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061900131 20020619 00131 NM 2002 6 19 CA020604003 1 20020531 A 7922 BYPASS VALVE BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA OIL COOLER FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AIRCRAFT RETURNED TO GATE. REPORTED NR 2 OIL INDICATION EXCEEDED THE HIGH END. OAT AT AIRPORT WAS SEEN AS 34 DEGRE ES C. REPLACED THE OIL COOLER BYPASS VALVE. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061900132 20020619 00132 WP 2002 6 19 MWEA020409 1 20020617 A 5311 591148509 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FORWARD PIT MODERATE CORROSION AT LONGERON 30 ON LOWER FLANGE OF FRAME 446. FABRICATED, INSTALLED NEW FRAME SECTION AND SPLICES. 2 L 7 2 4F A6WE 2002061900133 20020619 00133 EA 2002 6 19 CA020604004 1 20020529 A 2910 LINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE HYD SYSTEM FAILED W O OTHER K FLUID LOSS CR CRUISE 1 CA (CAN) HYDRAULIC NR 1 LOW PRESSURE AND QUANTITY "0". HYDRAULIC PUMP RAN DRY FOR 3 MIN. HYDRAULIC RETURN LINE FOR PRESSURE MANIFOLD FOUND LEAKING. NR 1 ENGINE HYDRAULIC PUMP CHANGED AS PER 29-11-01-400-801, HYDRAULIC LINE REPLACED PER STANDA RD PRACTICES 20-22-01, ALSO CARRIED OUT MM 05-51-33-210-801 PAGE 601-603. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061900134 20020619 00134 WP 2002 6 19 MWEA020410 1 20020617 A 5342 591214160 ATTACH ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 A .5 INCH CRACK IN RIGHT SIDE VERTICAL TO FUSELAGE ATTACH ANGLE AT STATION 1130, APPROXIMATELY 1 FOOT FORWARD OF RUDDER TORQUE TUBE. FABRICATED AND INSTALLED SPLICE, STRAP AND FILTER. 2 L 7 2 4F A6WE 2002061900135 20020619 00135 EA 2002 6 19 CA020604005 1 20020604 A 3233 21532020 MOUNT CNDAIR CL215 CL2151A10 1900320 EA MLG ACTUATOR DISPLACED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) FITTING BOLTS (NAS 6204-18) X 2 SHEARED AND FITTING (215-34014-2) WAS TORN OUT UPON GEAR RETRACTION ALONG WITH SUP PORTING STRUCTURE. THE AIRCRAFT INDICATED LT GEAR UNLOCKED IN THE UP POSITION. PILOT CYCLED THE GEAR SEVERAL TIMES BEFO RE RETURNING TO BASE, GEAR LOCKED AND INDICATED DOWN. THIS AIRCRAFT IS PRE SERVICE BULLETIN 215-0399. AFTER REPAIR, LAN DING GEAR WAS CHECKED FOR IMPROPER RIGGING AND FOUND TO BE OK. 2 H 7 2 4R RT A14EA 2002061900136 20020619 00136 WP 2002 6 19 MWEA020411 1 20020617 A 5313 591143271 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT ACCESSORY COMPARTMENT LONGERON 2 RIGHT HAS A CRACK AT STATION 1076. FABRICATED AND INSTALLED LONGERON SPLICE REPAIR . 2 L 7 2 4F A6WE 2002061900137 20020619 00137 EA 2002 6 19 CA020604006 1 20020602 A 3213 17064103 STRUT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TRUNNION RADIUS FAILED W O OTHER O OTHER LD LANDING 1 CA (CAN) A/C SLID DOWN RWY 4,000 FEET AT 21:55. WITH 50 PASSENGERS PLUS CREW. NOBODY HURT. A/C ENROUTE WHEN LDG, LT MLG F AILED JUST BELOW RADIUS BELOW AFT TRUNION FITTING. LT WING TIP LOWER SURFACE CONTACTED RWY AS A/C SLID DOWN RWY. LT INBO ARD & OUTBOARD FLAPS SUSTAINED EXTENSIVE DAMAGE FROM CONTACT WITH RWY. WING LEADING EDGE DAMAGED BY CONTACT WITH TAXI WA Y MARKER LIGHT. TAXI WAY LIGHT ALSO PUNCTURED HOLE IN LOWER WING SKIN ON WING TIP ASSY. LT OUTBOARD BRAKE HAD ON DISK C OME APART & DEPART. A/C IS ON JACKS & SECURED. NTSB HAS TAKEN POSSESION OF FDR & CVR. THEY ARE BEING TAKEN TO WASHING TO N, DC FOR ANALYSIS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061900138 20020619 00138 WP 2002 6 19 MWEA020412 1 20020617 A 5310 995823911N SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT ACCESSORY COMPARTMENT FRAME STATION 1019. DOUBLER HAS A CRACK LOCATED BELOW LONGERON 14 LEFT. FABRICATED AND INSTA LLED FORMER. 2 L 7 2 4F A6WE 2002061900139 20020619 00139 EU 2002 6 19 CA020604007 1 20020528 A 2820 D97C00501 ISOLATION VALVE AIRBUS 310 A310300 3930305 EU GE CF6 CF680C2* GL FUEL CELL FAILED W A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CA (CAN) AFT TRIM TANK MESSAGE AFTER ISO VALVE STARTED TO FLASH (VALVE IN TRANSIT). MAINTENANCE REPLACED THE AFT TRIM TANK ISO VALVE I.A.W. THE AMM 28-22-54 AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A35EU E23EA 2002061900140 20020619 00140 WP 2002 6 19 MWEA020413 1 20020617 A 5310 99124541 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FORWARD CARGO COMPARTMENT FRAME STATION 446 SHEAR TIE HAS NUMEROUS ELONGATED FASTENER HOLES LOCATED BETWEEN LONGERON 28 LEFT AND 26 RIGHT. FABRICATED AND INSTALLED FORMERS. 2 L 7 2 4F A6WE 2002072200066 20020722 00066 NM 2002 7 22 2002UALA00970 1 20020607 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 BS 790, LBL 11, WL 200 TOP OF FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072200067 20020722 00067 NM 2002 7 22 2002UALA00971 1 20020607 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 BS 400-420, STRINGER 36R-30R SKIN DOUBLER HAS BLIND FASTENERS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOU BLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072200095 20020722 00095 NM 2002 7 22 2002UALA00985 1 20020610 A 5411 SPAR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NAC STA 221, NR 2 ENGINE PYLON, AFT UPPER SPAR WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REP AIR PARTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072200103 20020722 00103 NM 2002 7 22 2002UALA00987 1 20020610 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 BS 1300 LBL 40-44 T-CAP FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP REPAIRS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072200105 20020722 00105 NM 2002 7 22 2002UALA00988 1 20020610 A 5411 SPAR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NAC STA 221, NR 2 ENGINE PYLON, UPPER SPAR WEB, IS CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072300195 20020723 00195 NM 2002 7 23 2002UALA00996 1 20020612 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 CABIN FLOORBEAM UPPER SURFACE GOUGED NEXT TO GALLEY FITTING AT BODY STATION 807, RBL 29. MAJOR REPAIR ACCOMPLISHED. RE MOVED AND REPLACED FLOORBEAM SPLICE DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072300196 20020723 00196 NM 2002 7 23 2002UALA00997 1 20020612 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 CABIN FLOOR STRUCTURE AT STATION 1200-1220 HAD DEEP GOUGES AT NUT CLIP HOLES, TO INNER CREASE BEAM AT 65 LBL STRINGER 17 L. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPLACEMENT AND INSTALLED WITH EXTERNAL SPLICE AT STA 1230 ONE L ANGLE AND L ANGLE WITH FLANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072300197 20020723 00197 NM 2002 7 23 2002UALA00998 1 20020613 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 CABIN FLOOR SUPPORT CORD HAD CORROSION ON UPPER FLANGE AT STATION 345 TO 365 BL 0 WL 208.10 MAJOR REPAIR ACCOMPLISHED. REMOVED T ANGLE CORD FROM BETWEEN STA 324 AND 417 DRILLED UP NEW PART AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072500063 20020725 00063 NM 2002 7 25 2002UALA01000 1 20020612 A 2751 TRANSMITTER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE T/E FLAP OUT OF RIG A UALA K NONE N FALSE WARNING AP APPROACH 1 WP 29 668UA 30024 FLAP ASYMMETRY JUST BEFORE FINAL APPROACH. OUT OF RIG FLAP LEVER TRANSMITTER. SUBJECT TRANSMITTER WAS RIGGED PER APPLI CABLE MAINTENANCE MANUAL. FLAP SYSTEM WAS OPS CHECKED PER APPLICABLE MAINTENANCE MANUAL AND ALL OPS CHECKS WERE GOOD. A BITE CHECK WAS ACCOMPLISHED ON THE FLAP/SLAT ELECTRONICS UNIT (FSEU) PER APPLICABLE MAINTENANCE MANUAL AND NO FAULTS W ERE FOUND. 2 L 7 2 4F 4 F RT A1NM E24NE 2002061900141 20020619 00141 WP 2002 6 19 MWEA020414 1 20020617 A 5330 59124371 PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 CORROSION ON LEFT LOWER DIAMOND PANEL FORWARD OF MAIN LANDING GEAR. FABRICATED AND INSTALLED FILLER. 2 L 7 2 4F A6WE 2002061900142 20020619 00142 EU 2002 6 19 CA020604008 1 20020603 A 6120 SD3471106XA CONTROL CABLE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE HARTZL HCB5M HCB5MP3 GL PROP CONTROL FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING UNSCHEDULED REMOVAL OF RT FCU IT OBSERVED THAT PROP CONTROL CABLE FRAYED AT PULLEY LOCATED IN RT WING CENTE R SECTION. PROP CONTROL MOVED TO ASSIST IN REMOVAL OF CABLE & AS DONE CABLE SNAPPED AT DIFFERENT LOCATION. CABLE SEGMEN T SD3-47-1106XA FRAYED CABLE AT CENTER SECTION & CABLE SEGMENT SD3-60-6016XA CABLE THAT BROKE AT PULLEY CLUSTER AT FRAME 74. INSPECTION INTERVAL FOR THESE CABLES IS AT EACH "D" CHECK WHICH IS EVERY 4800 HRS. IS SB- (SD360-76-08) FOR POWER L EVER CONTROL CABLES THAT REQUIRES REPETATIVE INSPECTION EVERY 1200 HRS. HAVE OPTED TO ADD PROP CONTROL CABLES & CONDITIO N LEVER CABLES TO SAME TIME INTERVAL. 2 H 7 2 4T 4 T A41EU E4EA 6 C P44GL 2002061900143 20020619 00143 WP 2002 6 19 MWEA020415 1 20020617 A 5330 591142831 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FUSELAGE INTERNAL SKIN DOUBLER SHOWS SIGNS OF EXFOLIATION CORROSION AT STATION 996 - 1019. REMOVED INTERNAL DOUBLER AND SKIN. FABRICATED AND INSTALLED INTERNAL DOUBLER AND INSTALLED NEW SKIN. 2 L 7 2 4F A6WE 2002061900144 20020619 00144 NM 2002 6 19 ZW0A0206401 1 20020615 A 2121 6457053 FAN BOEING 757 7572Q8 1384972 NM A ZW0A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 13 709TW 28168 OILY SMOKE WAS REPORTED THROUGHOUT THE CABIN DURING TAKEOFF. THE LH AIR CONDITIONING PACK WAS SHUT OFF AND SMOKE DISSIP ATED. THE LH PACK WAS PLACARDED INOPERATIVE PER MEL AND THE AIRCRAFT WAS OPERATED TO ANOTHER STATION WHERE THE LH RECIRC ULATION FAN WAS REPLACED. CHECK-C 9-18-01 LAX. --CLOSED-- 2 L 7 2 4F RT A2NM 2002061900145 20020619 00145 WP 2002 6 19 MWEA020416 1 20020617 A 5313 592032339 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AT STATION 484 LONGERON 19 RIGHT HAS A DENT BEYOND LIMITS PER SRM 53-04. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002061900146 20020619 00146 NM 2002 6 19 P2EA2002M040 1 20020612 A 7810 ACOUSTIC PANEL BOEING 737 73725A 1384481 NM NR 2 ENGINE GOUGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 239TA 23789 ON WALKAROUND, FOUND THE NR 2 ENGINE TAIL PIPE EXTENSION WITH GOUGE IN ACOUSTIC PANEL 4 INCHES LONG, .0625 INCH WIDE AND .5 INCH DEEP. WELD GOUGE ACCORDING TO MM 78-38-43. 2 L 7 2 4F RT A16WE 2002061900148 20020619 00148 NM 2002 6 19 P2EA2002M041 1 20020613 A 7810 TAILPIPE BOEING 737 737230 1384401 NM NR 1 ENGINE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 DURING TRANSIT CHECK FOUND THE NR 1 ENGINE TAIL PIPE EXTENSION WITH CRACK. REMOVED AND REPLACED THE NR 1 ENGINE TAIL PI PE EXTENSION WITH SERVICEABLE TAIL PIPE EXTENSION IAW 78-32-211. 2 L 7 2 4F RT A16WE 2002061900149 20020619 00149 EA 2002 6 19 CA020605001 1 20020526 A 5610 601R3303311 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) LEFT SIDE COCKPIT SIDE WINDOW CRACKED AT FL350. REMOVED AND REPLACED LT SIDE WINDOW. OPS AND LEAK CHECK GOOD 2 L 7 2 4F 4 F RT A21EA E15NE 2002061900150 20020619 00150 NM 2002 6 19 P2EA2002M042 1 20020613 A 7810 TAILPIPE BOEING 737 737230 1384401 NM NR 2 ENGINE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 DURING TRANSIT CHECK FOUND THE NR 2 ENGINE TAIL PIPE EXTENSION WITH CRACK. REMOVED AND REPLACED THE NR 2 ENGINE TAIL PI PE EXTENSION WITH SERVICEABLE EXTENSION IAW 78-32-211. 2 L 7 2 4F RT A16WE 2002061900151 20020619 00151 SO 2002 6 19 SWIA200210838 1 20020510 A 2731 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO ELEVATOR TAB FAULTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 236SW 120312 DURING TAKEOFF, TRIM AURAL WARNING SOUNDED. TAKEOFF WAS ABORTED. TRIM SETTING WAS 34. EVEN WITH TRIM IN MIDDLE OF GRE EN BAND, AURAL WARNING SOUNDED. REMOVED AND REPLACED BOTH RIGHT AND LEFT ELEVATOR TRIM TAB PROX SENSORS. OPS CHECKS GO OD. 2 L 7 2 4T RT A31SO 2002061900152 20020619 00152 NE 2002 6 19 CA020605002 2 20020603 A 7200 MODULE01 ENGINE BOEING 757 757* NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FAILED W F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 CA 17301 (CAN) FLT 1543 (CLT-BOS) AT 19502, FLAMES WERE SEEN COMING FROM RT ENGINE DURING ROTATION FROM CLT.AT 300-500 FEET AGL PILOT REPORTED HEARING A BOOM &, A/C YAWED, FOLLOWED BY RT ENGINE FIRE WARNING & HIGH EGT (1010C). BY TIME A IRCRAFT REA CHED 1000 & AGL, ONE FIRE BOTTLE HAD BEEN DISCHARGED, & ENGINE SHUTDOWN. EMERGENCY DECLARED & A/C RETURNED TO FIELD UNE VENTFULLY. SET 19 MINS. POST-INSP REVEALED ONE MISSING ANNULUS FILLER (POST-MOD 9177 STAND ARD), SEVERAL FAN BLADES WER E DAMAGED, LARGE HOLE IN FAN CASE AT FAN TRACK CONTAINED BY KEVLAR WRAP. LOOSE FILLER BITS WERE RECOVERED FROM RWY & BY PASS DUCT & HELD FOR INVEST. PART NR & SER-NR OF FILLER WILL BE REPORTED WHEN AVAILABLE.ENGINE ON HIS WAY TO RRC. 2 L 7 2 4F 4 F RT A2NM E12EU 2002061900153 20020619 00153 SO 2002 6 19 CA020605003 1 20020505 A 5540 4A3441 BRACKET EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA RUDDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 18435 18435 (CAN) DURING A SCHEDULED INSPECTION THE UPPER RUDDER ATTACHMENT BRACKET WAS FOUND CRACKED. 1 L 7 2 4T 4 T A21SO E4EA 2002061900154 20020619 00154 EA 2002 6 19 SWIA200210839 1 20020511 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE T/E FLAP FAILED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 405SW 7029 FLAPS FAIL CAUTION MESSAGE ILLUMINATED. REPLACED RIGHT BPSU. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061900155 20020619 00155 EA 2002 6 19 SWIA200210840 1 20020511 A 2750 7455001 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 437SW 7564 UPON SELECTED FLAPS 20 FLAPS FAILED. LANDED AT FLAPS 6. REMOVED AND REPLACED FLAP SELECTOR HANDLE. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061900156 20020619 00156 NE 2002 6 19 CA020605004 2 20020511 A 7310 3035618 LINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE FUEL SYSTEM CRACKED W E ENGINE SHUTDOWN K FLUID LOSS TX TAXI/GRND HDL 1 CA 13530 13530 (CAN) HEAVY FUEL LEAK OBSERVED ON LT ENGINE DURING GROUND RUN. AFTER INVESTIGATION, FOUND THAT THE PRESSURE LINE BETWE EN FCU AND FUEL FLOW DIVIDER WAS FOUND CRACKED AT THE B-NUT ON FCU SIDE. THE CRACK WAS PARALLEL TO THE WELDING OF THE B- NUT SEATING. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002061900157 20020619 00157 NM 2002 6 19 CA020605005 1 20020424 A 2100 311325001 PIN DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AIR PRESS VALVE MISALIGNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA 41322 41322 (CAN) FLIGHT CREW REPORTED SMOKE DURING DESCENT. AFTER INVESTIGATION FOUND THAT THE GUIDE PIN OF THE P2.5/3 AIR VALVE W AS MISALLIGNED IN THE SLOT OF THE SEAT ASSY CAUSING THE MALFUNCTION OF THE VALVE ASSY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061900158 20020619 00158 EA 2002 6 19 SWIA200210841 1 20020501 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM FAULTY A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 NM 07 720SW 7297 STAB TRIM NR 1 & NR 2 WILL NOT REMAIN ENGAGED IN FLIGHT. MACH TRIM INOP. A/C RETURNED TO SLC FOR LANDING. REMOVED AND REPLACED NR 1 STAB TRIM DISCONNECT SWITCH. 2 L 7 2 4F RT A21EA 2002061900159 20020619 00159 CE 2002 6 19 CA020605006 1 20020510 A 5610 101384025 WINDSHIELD BEECH B300 B300B350C CE PWA PT6 PT6A60A 52043 NE COCKPIT FAILED W B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) PILOTS WINDSCREEN SHATTERED WHILE CRUISING AT F230. 2 L 7 2 4T 4 T RT A24CE E4EA 2002061900160 20020619 00160 EA 2002 6 19 CA020605008 1 20020604 A 7810 8500017 EXHAUST STACK CNDAIR CL215 CL2151A10 1900320 EA PWA R2800 CA3 52026 NE HAMSTD 43E 43E60 NE NR 1 ENGINE SPLIT W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) DURING CLIMB THERE WAS A ZONE 1 FIRE INDICATION ON THE NR 1 ENGINE THE THROTTLE WAS RETARDED TO 2 20 INCH INDICATI ON STOPPED BUT REAPPEARED THE ENGINE WAS SHUT DOWN AND THE PROP WAS FEATHERED. THE AIRCRAFT RETURNED TO BASE. UPON INVES TIGATION BY MAINTENANCE STAFF THE EXHAUST STACK AT POSITION NR 9 WAS FOUND SPLIT, THE HEAT HAD CAUSED THE FIRE WIRE WAS BURNED THROUGH CAUSING THE FIRE INDICATION. THE EXHAUST STACK WAS REPLACED AS WELL AS THE FIRE WIRE. THE AIRCRAFT WAS INSPECTED FOR OTHER DAMAGE. FOUND SERVICEABLE. THE AIRCRAFT WAS RETURNED TO SERVICE. TOTAL TIME ON EXHAUST STACK IS UNKN OWN. 2 H 7 2 4R 4 R RT A14EA E231 6 C P871 2002061900161 20020619 00161 SO 2002 6 19 SWIA200210842 1 20020514 A 2751 3471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO COCKPIT FALSE INDICATION A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 579SW 5589 5589 120347 FLAPS WOULD NOT FULLY RETRACT IN FLIGHT. DISAGREEMENT BETWEEN OUTBOARD PAIR. CHECKED ON GROUND AND GOT DISAGREEMENT BE TWEEN INBOARD PAIR. PERFORMED SEVERAL FLAP CYCLES AND GOT ANNUNCIATOR TO FAIL. REPLACED ANNUNCIATOR WITH SERVICEABLE U NIT. OPERATED FLAPS SEVERAL TIMES. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002061900162 20020619 00162 WP 2002 6 19 CA020605009 1 20020524 A 7930 ST104E TRANSMITTER ALLSN 501D13 CVAC 580 580 2422806 WP ALLSN 501D 501D13 03004 GL OIL PRESSURE FALSE INDICATION W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE THE CREW RECEIVED A LOW OIL PRESSURE INDICATION FOR THE NR 2 ENGINE RGB. THE RED LOW OIL PRESSURE LI GHT DID NOT ILLUMINATE. THE ENGINE WAS SHUT DOWN AND THE PROP FEATHERED. THE AIRCRAFT RETURNED TO BASE. UPON INVESTIGATI ON IT WAS FOUND THAT THE OIL PRESSURE TRANSMITTER WAS FAULTY. THE PRESSURE TRANSMITTER WAS REPLACED ENGINE WAS GROUND R UN LEAK AND FUNCTION CHECKED SERVICEABLE. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT E282 2002061900163 20020619 00163 EA 2002 6 19 CA020606001 1 20020606 A 5610 NP1393215 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W O OTHER O OTHER DE DESCENT 1 CA (CAN) LT (CAPTAINS) FRONT WINSHIELD CRACKED DURING DESCENT (L1261423)LT WINSHIELD REPLACED AS PER AMM 56-10-01-400 2 L 7 2 4F 4 F RT A21EA E15NE 2002061900164 20020619 00164 EA 2002 6 19 SWIA200210843 1 20020514 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT BROKEN A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 406SW 7030 FIRST OFFICERS WINDOW BROKE WHILE EN ROUTE SMF. DIVERTED TO RNO. REMOVED AND REPLACED COPILOT'S WINDOW. PRESSURIZED A C, CHECKED FOR LEAKS. WINDOW HEAT CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061900165 20020619 00165 NM 2002 6 19 CA020606002 1 20020605 A 5314 KEELBEAM BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 59909 (CAN) FUSELAGE SKIN BULGED AND SUSPECT CORROSION RT KEELBEAM STA 520 STR 28 RT ALSO RIVETS HEADS SHEARED AND LOOSE STA 4 80 TO STA 520 (M1121878) SKIN CUT AND CORROSION REMOVED AS PER SRM 53-30-3 FIG 1.KEELBEAM STA 520 STR 28 RT WITHIN LIMIT S AFTER CORROSION REMOVAL PER SRM 53-30-1 FIG1. SKIN DOUBLER REPAIR INSTALLED AS PER SRM 53-30-3 FIG 6 2 L 7 2 4F 4 F A16WE E2EA 2002061900166 20020619 00166 CE 2002 6 19 CA020606005 1 20020605 A 2752 1045641 MOTOR BEECH 23 A24R 1151252 CE LYC O360 IO360A1B 41514 EA MCAULY 2D34C 2D34C9 GL TE FLAPS WORN W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) NOISE IN FLAP MOTOR CAUSED FURTHER INSPECTION. UPON ACCESSING MOTOR UNDER REAR SEAT, SPARKS WERE NOTED COMING OUT OF DRIVE AND OF MOTOR DURING ACTUATION. ARMATURE MOTOR BUSHINGS WERE WORN TO THE EXTENT THAT THERE WAS CONTACT WITH THE END PLATE DURING OPERATION. MOTOR REMOVED FOR OVERHAUL. 1 L 7 1 3O 3 O A1CE 1E10 5 C P7EA 2002061900167 20020619 00167 NE 2002 6 19 CA020606007 2 20020526 A 7414 SB9RU3 MAGNETO AYRES S2 S2RNORMAL 7630202 SO PWA R1340 R1340AN1 52016 NE HAMSTD 12D 12D40 NE ENGINE FAILED W C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA (CAN) BEARING FAILED ON DRIVE SHAFT CAUSING ROTOR TO WOBBLE, THERE BY CAUSING THE ROTOR PEGS TO STRIKE THE DISTRIBUTOR P EGS. THIS RESISTANCE CAUSED THE TWO SCREWS WHICH ATTACH THE ROTOR TO THE TIMING GEAR TO SHEAR AND THE ROTOR BECAME DETAC HED CAUSING SEVERE MISFIRING AS IGNITION WAS CREATED IN CYLINDERS THAT WERE NOT IN FIRING POSITION. VERY RARE OCCURRENCE . 1 L 7 1 3R 3 R NC A3SW 5E2 5 C P257 2002061900168 20020619 00168 SO 2002 6 19 SWIA200210844 1 20020514 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PAX DOOR OUT OF ADJUST A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 293SW 120320 ON TAKEOFF ROLL FORWARD DOOR LIGHT ILLUMINATED. ABORTED TAKEOFF. ADJUSTED PAX DOOR MICROSWITCH AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002061900169 20020619 00169 SO 2002 6 19 SWIA200210845 1 20020425 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 580SW 120348 LT AFT-MOST SEAT TRACK SECTION CORRODED IN AREAS AS MARKED. REMOVED AND REPLACED PASSENGER SEAT TRACK LT AFT. NO OTHER DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2002061900172 20020619 00172 CE 2002 6 19 CA020606010 1 20020604 A 3242 1338932 STATOR CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE BRAKE ASSY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AFTER DISASSEMBLING THE BRAKE UNIT, IT WAS FOUND THAT THE STATORS WERE VISUALLY CRACKED.AFTER NDT INSPECTION IT W AS FOUND THAT THE TORQUE PLATE HAD SEVERAL CRACKS GENERATING FROM THE RIVET HOLES. 1 L 7 2 4F 4 F A22CE E1NE 2002061900174 20020619 00174 NM 2002 6 19 CA020606011 1 20020423 A 3297 SENSOR DHAV DHC8 DHC8* NM PWC 150 PW150A EA NLG CENTERING BROKEN W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) LANDING GEAR FAILURE: WHEN SELECTING GEAR UP WE GOT 3 RED PLUS 3 GREEN, GEARHANDLE AMBER LIGHTS AND THE GEAR STAY ED DOWN. STOPED CLIMB AT 3000 FT TO CONSULT QRH AND CREW BULLENTINS. AFTER APP. 5 MINUTES THE GEAR RETRACTED WITHOUT ANY INPUT FROM OUR SIDE. GEAR DOWN BEFORE LANDING WAS OK. INVESTIGATION/ACTION: DURING TROUBLESHOOTING THE NOSE WHEEL C ENTERING SENSOR WIRE WAS FOUND BROKEN. NOSE WHEEL CENTERING SENSOR HARNESS REPLACED. LANDING GEAR RETRACTION/EXTENSION C HECKED ACCORDING AMM 32-31-00-710-801. THE GEAR UP SELECTION FAILURE WAS CAUSED BY THE DAMAGED NOSE WHEEL CENTERING SENS OR WIRES. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061900176 20020619 00176 CE 2002 6 19 CA020606013 1 20020605 A 3242 1338931 STATOR 215286 CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE BRAKE ASSY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 0846 (CAN) TCN = 584 AFTER DISASSEMBLY OF THE BRAKE UNIT IT WAS FOUND THAT THE STATOR DISC'S WERE CRACKED. DURING NDT INSPEC TION OF THE TORQUE PLATE IT WAS FOUND THAT THERE WERE SEVERAL SMALL CRACKS EMANATING FROM THE RIVET HOLES. 1 L 7 2 4F 4 F A22CE E1NE 2002061900177 20020619 00177 CE 2002 6 19 CA020606014 1 20020605 A 3242 1338932 STATOR 215286 CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE BRAKE ASSY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1583 (CAN) TCN = 588 AFTER DISASSEMBLY IT WAS FOUND THAT ONE STATOR DISC WAS CRACKED AND THE SECOND WAS BROKENCOMPLETELY THR OUGH AND SEPARATED APPROX 3/8 INCH. DURING NDT INSPECTION OF THE TORQUE PLATE IT WAS FOUND TO HAVE SEVERAL SMALL CRACKS EMANATING FROM THE RIVET HOLES 1 L 7 2 4F 4 F A22CE E1NE 2002061900178 20020619 00178 NM 2002 6 19 CA020606015 1 20020326 A 3010 4100S00501 VALVE 4100S00501 BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA DUAL DISTRIBUTIO FAILED W O OTHER O OTHER DE DESCENT 1 CA (CAN) DE-ICING SYSTEM FAILURE;DURING DESCEND "DE-ICE PRESS" CAUTION LIGHT CAME ON. POWER ADDED WITHOUT RESULT. NO GREEN LIGHT FOR THE MOST OUTER LEFT WING BOOT. CHECKLIST IN QRH PERFORMED WITHOUT RESULT. SUSPECTED BOOT PUNCTURE. TESTED IN B OTH MANUAL AND AUTO WITH NO SUCCESS. UNEVENTFULL LANDING. INVESTIGATION/ACTION; DUAL DISTRIBUTING VALVE WAS FOUND STUCK. DDV REPLACED ACCORDING AMM 30-11-16 AND DE-ICE SYSTEM TESTED CONCLUSION; THE INABILITY TO INFLATE THE BOOT WAS CAUSED B Y THE INOPERATIVE DDV.MANUFACTURE: AERAZUR 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061900179 20020619 00179 WP 2002 6 19 GTIA020401 1 20020507 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 826NK 49391 RSW - FLT 1228 - FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY IAW MD-80 MM 3 3-50-00. OPS CHECK NORMAL AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 2002061900180 20020619 00180 WP 2002 6 19 GTIA020402 1 20020323 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - AFT PIT CORRODED AT INTERCOSTAL STATION 1193 BETWEEN 28R, 29R. REMOVED CORROSION. FORMED INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002061900181 20020619 00181 EA 2002 6 19 CA020606016 1 20020606 A 2497 215T5218354 BUSS TIE CNDAIR CL215 CL2156B11415 EA PWA PW120 PW123 NE ELECTRICAL BURNED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOLLOWING A VISUAL INSPECTION WHILE SEARCHING THE CAUSE OF THE BREAKDOWN (FAILURE), THE BUSS BAR WAS FOUND OVERHEA TED AND THE FEED THROUGH WAS BURNED ALONG ITS CIRCUMFERENCE. 2 H 7 2 4T 4 T RT A14EA E20NE 2002061900183 20020619 00183 WP 2002 6 19 GTIA020403 1 20020320 A 5210 SKIN DOUG DC9 DC981 3022081 WP PAX DOOR GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FORWARD PASSENGER DOOR EXTERNAL SURFACE (HOLD/OPEN) HOOK CUT OUT AREA HAS GOUGES. REMOVED DAMAGE FROM FORWARD PAS SENGER DOOR HOOK CUT OUT AREA OUT OF LIMITS. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2002061900184 20020619 00184 WP 2002 6 19 GTIA020404 1 20020320 A 5320 STRUCTURE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND CABIN RIGHT FORWARD GALLEY (G-1) INBOARD SIDE AT FLOOR HAS CORROSION. REMOVED CORROSION. FABRICATED REPAIR . INSTALLED PARTS. (M) 2 L 7 2 4F A6WE 2002061900185 20020619 00185 WP 2002 6 19 GTIA020405 1 20020316 A 5755 FLAP DOUG DC9 DC981 3022081 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND RIGHT WING OUTBOARD FLAP T/E CRACKED/DAMAGED, THREE EACH. REPAIRED RIGHT WING OUTBOARD FLAP TRAILING EDGE. (M) 2 L 7 2 4F A6WE 2002061900186 20020619 00186 2002 6 19 000168 4 20020613 A 3417 ADC EMB 145 EMB145 3260210 SO E/E BAY FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 268 NR 1 ADC FAIL. 2 L 7 2 4F RT T00011AT 2002061900187 20020619 00187 SO 2002 6 19 000169 1 20020614 A 3411 DRAIN LINE EMB 145 EMB145 3260210 SO PITOT/STATIC SYS DEFECTIVE A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 268 P3370227 IAS FLAG AND SPS ADVANCED MSG ON EICAS. FOUND, REMOVED, AND CAPPED BAD PITOT DRAIN. RESCHEDULE. LEAK CHECK GOOD. 2 L 7 2 4F RT T00011AT 2002061900190 20020619 00190 EU 2002 6 19 0201923242 1 20020604 A 3397 WIRE AIRBUS 320 A320212 3930322 EU CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 342NW 00381 FIRST CLASS EMERGENCY PATH LIGHTS INOPERATIVE. CONNECTED LOOSE WIRE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002061900194 20020619 00194 NM 2002 6 19 02FDEA00396 1 20020614 A 2613 OVERHEAT LOOP BOEING 727 727200 138407E NM A/C BAY OUT OF POSITION A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 234FE 21328 DURING CR FLT AT FL350 BOTH PACKS ON GOT A LWR AFT BODY OVERHEAT WARNING LIGHT. COMPL WITH RED TABS. WHEN R/PACK & ENG NR 3 BLEED AIR VLVS CLOSED, LIGHT WENT OUT WITH THROTTLE NR 3 REDUCTION. SYSTEM CK GOOD. LEFT RT PACK AND NR 3 BLEED SWITCHES CLOSED. REPEAT WRITEUP. REMOVED LT & RT AFT BODY DET LOOPS, LWR BODY DET LOOPS, AND K/ BEAM DET LOOP PER MM 2 6-14-001-2. FOUND R/AFT BODY LOOP TOUCHING AIR CLEANER PURGE VLV. ROUTED NEW LOOP AWAY FROM VALVE. TESTED NORM. 2 L 7 3 4F RT A3WE 2002061900195 20020619 00195 NE 2002 6 19 02FDEA00397 2 20020613 A 7200 ENGINE BOEING 727 727100 1384036 NM PWA JT8 JT8D7 52053 NE NR 3 LEAKING A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 25 194FE 19143 649109 LOST OF OIL QUANTITY AND PRESSURE IN NR 3 ENG. SHUTDOWN PER CHECK LIST AND LANDED. INSPECTED CHIP DETECTORS, AND FILTE R FOUND TO BE CLEAN. FOUND OIL PUDDLED IN TAILPIPE, NO EVIDENCE OF OIL IN COLD STREAM AREA. SERVICED ENG OIL AND MOTOR ED. OIL QTY DROPPED STEADILY TO 0 AND OIL RAN FROM TAILPIPE. OIL COMING FROM ENG CORE. PER CREW REPORT AND ENG M/M 72 -00 P 518D PROBABLE ENG CHANGE. ENGINE REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 2002061900196 20020619 00196 NM 2002 6 19 02FDEA00398 1 20020611 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 CORROSION ON FLOORBEAM LWR FLANGE BS 900, LBL 54-68, WL 208 (C53-224-01, 2). 2 L 7 3 4F RT A3WE 2002080600012 20020806 00012 NM 2002 8 6 02FDEA00399 1 20020613 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 CORROSION ON UPPER FLANGE OF FLOORBEAM BS 1050, LBL 19, WL 208. 2 L 7 3 4F RT A3WE 2002080600013 20020806 00013 NM 2002 8 6 02FDEA00400 1 20020613 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 FRAME DENTED BS 500, STR 24 - 25L. 2 L 7 3 4F RT A3WE 2002061900197 20020619 00197 NM 2002 6 19 02FDEA00401 1 20020613 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22550 FRAME DENTED BS 680, STR 24R. 2 L 7 3 4F RT A3WE 2002061900198 20020619 00198 NM 2002 6 19 CA020607003 1 20020605 A 3060 697070212 BUSS TIE BOMBDR DHC8 DHC8402 NM PWC 150 PW150A EA ROTOL R4304 R4304* EU PROPELLER BURNED W E ENGINE SHUTDOWN E VIBRATION/BUFFET AP APPROACH 1 CA (CAN) IN APPROCH PILOT NOTICE THAT LT PROP RPM CHANGED FROM 850 TO 1070 RPM STEADY (OVERSPEED GOVERNING )WITH A PEC CAUT ION LIGHT AND A POWERPLANT MESSAGE ON ENGINE DISPLAY. PILOT FEATHER LT PROP IAW PROCEDURE AND COMPLETED AN SAFE APPROCH AND LANDING. ENGINE FAULT CODE 160 RECORDED FROM NR 1 ENGINE ONE BUS BAR FOUND PROTECTION DAMAGED AND CHAFED ON THE PR OP MAGNETIC PICK-UP. SUSPECT THAT WHEN PILOT APPLIED PROP ANTI-ICE THE PEC RECORDED A FAULTY RPM READ-OUT, CAUSING THE PEC TO GO TO OVERSPEED GOVERNING CONDITION. BUSS BAR REPLACED BETWEEN BLADE NR 2 AND 3 ALL OTHER INSPECTED FOR PROPER CL EARANCE SOME REPOSITIONNATED PROPERLY .FAULT CLEARED ALL SYSTEM FONCTIONNALLY TESTED SERVICEABLE. 2 H 7 2 4T 4 T RT A13NM E00062EN 6 C P890 2002080600014 20020806 00014 NM 2002 8 6 02FDEA00402 1 20020613 A 2897 BXS700724 WIRE DOUG MD11 MD11 3023602 NM E/E BAY BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 TWO WIRES FOUND BURNT & BROKEN ABOVE AVIONICS RACK IN CAC. REMOVED AND REPLACED WIRES PER C901-836-16C. OPS CHECK BOOS T PUMP CARRIED OUT AS PER WC E1-2821-7-5000-03 PART 3 & 4. 2 L 7 3 4F RT A22WE 2002061900199 20020619 00199 EU 2002 6 19 02FDEA00403 1 20020612 A 5420 FITTING AIRBUS 310 A310 EU LT PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 LT WING PYLON FWD SPIGOT BALL JOINT FOUND WITH BROWN STAINS ALL ROUND THE CIRCUMFERENCE OF FITTING. CONFIRMED CORROSION ON 12 JUNE 2002. 2 L 7 2 4F RT A35EU 2002061900200 20020619 00200 EU 2002 6 19 02FDEA00405 1 20020612 A 1430 NUT AIRBUS 310 A310 EU RT PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 RT WING PYLON AFT FITTING BALL JOINT ASSY NUT FOUND WITH GREENISH STAIN. CONFIRMED CORROSION ON 12 JUNE 2002. INSTALL ED NEW FITTING ASSY PER AIRBUS S/B A310-54-2021. 2 L 7 2 4F RT A35EU 2002061900201 20020619 00201 EU 2002 6 19 02FDEA00406 1 20020612 A 5420 FITTING AIRBUS 310 A310 EU LT PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 LT WING PYLON AFT FITTING BALL JOINT ASSY FACE FOUND WITH BROWN STAIN. CONFIRMED CORROSION ON 12 JUNE 2002. INSTALLED N EW FITTING ASSY PER S/B A310-54-2021 EA. 6-5150-59026. 2 L 7 2 4F RT A35EU 2002061900202 20020619 00202 NM 2002 6 19 02FDEA00407 1 20020615 A 2410 OIL COOLER BOEING 727 727200 138407E NM CSD FAULTY A FDEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 25 219FE 21102 DURING CLIMBOUT NR 1 CSD AND NR 3 CSD OVERHEATED (NR 1 REPEAT), NR 1 WAS 130C & NR 3 125C WITH NR 2 105C (IN LIMITS). I AW QRH NR 1 GEN BREAKER WAS TRIPPED AND WAS STILL OVER 120C AFTER 3 MIN. DISCONNECTED NR 1 CSD. NR 3 GEN WAS TRIPPED A ND WAS OVER 120C AFTER 3 MIN. DISCONNECTED NR 3 CSD. NR 2 CSD NEVER WENT ABOVE 110C. INSPECTED NR 01 AND 03 CSD OIL L EVEL AND MAGNETIC FILTERS, FOUND OK. REMOVED AND REPLACED NR 01 & 03 -IN- TEMP SENSORS (IPC 24- 10-02-01ZZ). REMOVED AND REPLACED NR 01 CSD OIL COOLER PER MM 24-10-061-4. RECONNECTED BOTH NR 01 AND 03 CSD'S, RAN THE ENGINES TO TAKEOFF P OWER DURING 5 MINUTES PER 727 JRH, SYS WORKED PROPERLY IAW MM 24-10-001-0. 2 L 7 3 4F RT A3WE 2002061900203 20020619 00203 EU 2002 6 19 02FDEA0404 1 20020612 A 5420 FITTING AIRBUS 310 A310 EU RT PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 RT WING PYLON SPIGOT BALL JOINT FOUND WITH BROWN STAIN ALL AROUND THE CIRCUMFERENCE OF FITTING. 2 L 7 2 4F RT A35EU 2002061900204 20020619 00204 EU 2002 6 19 CA020607005 1 20020529 A 2130 88003BO201 VALVE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE CABIN PRESSURE INOPERATIVE W B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) REACHING FL290 ABNORMAL CABIN RATE. DOING THE CHECK LIST, UNABLE CONTROL CABIN ALTITUDE. INITIATING EMERGENCY DESC ENT AND TURNING BACK TO DEPARTING AIRPORT. 2 L 7 2 4F 4 F RT A35EU E23EA 2002061900205 20020619 00205 WP 2002 6 19 GTIA020406 1 20020422 A 2797 WIRE DOUG DC9 DC981 3022081 WP HORIZ STAB BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND ALTERNATE TRIM CONTROL LEVERS ON CONTROL PEDESTAL INOPERATIVE. TROUBLESHOT, FOUND 4 SPLICE IN THE TAIL (HOR IZ STAB) PULLED OUT, NEED TO RESPLICE. REPAIRED BROKEN WIRES RESPLICED. (M) 2 L 7 2 4F A6WE 2002061900206 20020619 00206 WP 2002 6 19 CA020607009 2 20020530 A 7261 30714211 GASKET BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE7313R 01518 WP ENGINE MISSING W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) CREW NOTICED RT ENGINE OIL PRESSURE FLUCTUATING SLIGHTLY.- AFTER A PERIOD OF TIME THE OIL PRESSURE STARTED TO DEC AY TO WHERE THE RED LOW OIL PRESSURE LIGHT ILLUMINATED (~25PSI).- A PRECAUTIONARY MANUAL SHUTDOWN WAS PERFORMED ON THE R T ENGINE (S/N P84403). - AN UNSCHEDULED LANDING WAS SAFELY COMPLETED AT WINNIPEG INTERNATIONAL AIRPORT.-UPON INSPECTION IT WAS OBSERVED THAT OIL HAD LEAKED OUT FROM THE BOTTOM (6 O'CLOCK) POSITION BETWEEN THE NR 6 BEARING OIL OUT TUBE FLANG E AND WHERE ATTACHMENT IS MADE TO NR 6 BEARING HOUSING.- CLEANED UP AREA AND COMPLETED SERVICE BULLETIN TFE731-79-3053 I NSTALLING OIL OUT TUBE P/N 3075541-2 AND SEAL P/N M83248-1-015. 2 L 7 2 4F 4 F A3EU E6WE 2002061900207 20020619 00207 WP 2002 6 19 GTIA020407 1 20020318 A 5280 DOOR DOUG DC9 DC981 3022081 WP RT MLG DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND RIGHT MLG FLYWING DOOR POP-UP/DELAMINATED. REMOVED DELAMINATED AREA ON RIGHT MLG FLY WING DOOR. FORMED FIL LER AND DOUBLER. BONDED FILLER AND DOUBLER TO RIGHT MLG FLY WING DOOR. (M) 2 L 7 2 4F A6WE 2002061900208 20020619 00208 CE 2002 6 19 CA020607011 1 20020524 A 3222 5842000213 TRUNNION CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO NLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE PERFORMING AN NDT INSPECTION ON THE NOSE GEAR TRUNNION LUGS. IT WAS DISCOVERED THAT ONE OF TWO LUGS HAD A CR ACK OF APPROXIMATELY 1 1/2 INCHES AROUND THE CIRCUMFERENCE. THIS WAS BEYOND ANY SERVICEABLE LIMIT, CAUSING THE UPPER TRU NNION ASSEMBLY TO BE REPLACED. 1 L 7 2 3O 3 O A7CE E8CE 2002061900209 20020619 00209 NM 2002 6 19 CA020607014 1 20020607 A 7921 OIL COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 17206 17206 (CAN) NR 1 ENGINE OIL COOLER LEAKING, OIL COOLER REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061900210 20020619 00210 NM 2002 6 19 CA020607015 1 20020607 A 7921 OIL COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) NR 2 ENGINE OIL COOLER LEAKING,OIL COLLER REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002061900211 20020619 00211 WP 2002 6 19 GTIA020408 1 20020425 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - AFT CARGO COMPARTMENT STATION 1155/1212 L28R WEB HAS CORROSION, FOUND DURING BEAM REMOVAL. REMOVED CORROSION. FA BRICATED NEW WEB. (M) 2 L 7 2 4F A6WE 2002061900212 20020619 00212 NM 2002 6 19 CA020607016 1 20020527 A 7722 ENGINE DHAV DHC8 DHC8* NM PWC 150 PW150A EA NR 1 MALFUNCTIONED W E ENGINE SHUTDOWN H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CA (CAN) NR 1 ENG. SHUTDOWN AFTER NEG. ITT. AFTER APPROX. 45 SEC - 1 MIN COMPLETE ELECT. FAILURE: LT STARTER GEN REPLACED, FC TRIED START, NO OP. ENGINE NR 2 ALREADY STARTED. ENGINE NR 1 STARTED, SLOW TO ACCELERATE, FADEC CUT FUEL OFF AT 15 PERCENT NH, BY TIME CREW DESELECTING START SELECT SWITCH, RT SIDE OF COCKPIT DARK, BUS FAULT LIGHT, BUS RESET. THE LT STARTER/GEN REPLACED, WOULD NOT TURN. MTCE PREV REPLACED S/G, NO GO. GCU TRIED, NO GO. K1 RELAY TRIED, NO GO. DURING ISOLATION OF DEFECT, IT FOUND THAT CONNECTOR 2431-TB13 LOOSE, AS 2 CABLES COULD BE MOVED BY HAND. FURTHER INVE STIGATE LED TO FINDING GROUND STUD 2431-GS1 BURNED, BELOW LT SEAT TRACK, X 331, Y9.250. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002061900213 20020619 00213 WP 2002 6 19 GTIA020461 1 20020328 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD B/B LONGERON 30 CORROSION FROM STATION 522 TO 560. MID CARGO CENTER SECTION STATION 560 LONGERON 30 CORROSION. REMOVED CORROSION. REMOVED LONGERON AT STATION 512 TO 585. FOUND MORE CORROSION AT FRAME THAT CONNECT LON GERON AT STATION 541. REMOVED CORROSION AT FRAME STATION 541. REMOVED DAMAGE AREA OF FRAME FS 541 FROM LONGERON 28L TO 28R. INSTALLED LONGERON SPLICE REPAIR. INSTALLED FRAME REPAIR. (M) 2 L 7 2 4F A6WE 2002061900214 20020619 00214 EU 2002 6 19 CA020607017 1 20020202 A 4940 372697241 STARTER FOKKER F28 F28MK1000 4990808 EU APU FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THIS APU HAS HAD TWO OCCURRENCES OF THE STARTER DRIVE SHAFT SHEARING. THE AIRCRAFT WAS INSPECTED DURING C CHECK IN REGARDS TO THESE SNAGS WITH NO FAULTS. THE APU STARTER DRIVE TRAIN HAS HAD NO FAULTS SINCE. 2 L 7 2 4F RT A20EU 2002061900215 20020619 00215 NE 2002 6 19 CA020610001 2 20020530 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RIGHT MALFUNCTIONED W A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CA (CAN) AT FL270 RECEIVED A RT ENGINE OIL PRESSURE MESSAGE. ENGINE ROLLED BACK. PER QRH - ENGINE UNABLE TO START. SECUR ED ENGINE AND ACCOMPLISHED A SINGLE ENGINE LANDING. ON POST FLIGHT INSPECTION OBSERVED RT ENGINE CHIP DETECTOR LIGHT ON . VERBALLY REPORTED BY MAINTENANCE THAT THE GEARBOX APPEARS TO BE LOCKED. ROAD CREW AND REPLACEMENT ENGINE DESPATCHED ENGINE CHANGE IN PROGRESS. THE ENGINE S/N 807022, WAS INSTALLED ON DEC 7/1999 AFTER COMING OUT OF STRUTHERS. IT HAS HAD NO RECENT UNUSUAL MAINTENANCE ACCOMPLISHED OTHER THAN THE 'B' SUMP SCAVANGE EO 79-017AD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061900216 20020619 00216 EA 2002 6 19 CA020610002 1 20020601 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ACM BAY UNSERVICEABLE W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) AFTER TAKEOFF, WHILE CLIMBING THROUGH 10,000 FT, CREW GOT LT PACK HIGH PRESS CAUTION MESSAGE. PRESSURIZATION WAS N OT BEING MAINTAINED.REPLACED THE RT ACM TO ENABLE THE RIGHT PACK TO BE SERVICEABLE. THE PACKS WERE OPERATED AND FOUND TO BE SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061900217 20020619 00217 CE 2002 6 19 CA020610003 1 20020531 A 2820 050011874 LINE CESSNA 172 172K 2072430 CE LYC O360 O360A1A 41514 EA FUEL SYSTEM WORN W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) - FUEL LINE FROM UNION TO FIREWALL (STRAINER) FOUND RUBBING ON CO-PILOT STEERING TORQUE TUBE AND STEERING ARM. FUE L LINE HAD A SMALL PIN HOLE AND A SMALL AMOUNT OF FUEL WAS LEAKING. - NEW LINE WAS MANUFACTURED AND ROUTED AWAY FROM STE ERING ARM. 1 H 7 1 3O 3 O NT 3A12 E286 2002061900219 20020619 00219 WP 2002 6 19 GTIA020462 1 20020324 A 5347 CARGO TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - AFT CARGO TRACK STATION 1003-1155 HAS CORROSION AND ELONGATED HOLES. REMOVED CORROSION FROM AFT CARGO TRACK AND Z -ANGLE. FABRICATED NEW CARGO TRACK. INSTALLED CARGO TRACK. (M) 2 L 7 2 4F A6WE 2002061900220 20020619 00220 NM 2002 6 19 CA020610005 1 20020609 A 2121 215201 GASPER FAN BOEING 737 737275 1384485 NM PWA JT8 JT8D17 52049 NE CABIN FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) WHILE BOARDING PAX. SMOKE STARTED ENTERING CABIN IN MID-CABIN RIGHT SIDE AREA.(L1251724)PAX. DEPLANED VIA FWD ENTR Y DOOR. FOUND GASPER FAN CONNECTOR & FUSILAGE INSULATION BLANKET BURNT. REPLACED AIR COND. MODULE & CIRCUIT BREAKER AS P ER STANDARD PRACTICES. REPLACED GASPER FAN AS PER MM. 21-24-21 PG 401 2 L 7 2 4F 4 F A16WE E2EA 2002061900221 20020619 00221 WP 2002 6 19 GTIA020463 1 20020322 A 5730 PANEL DOUG DC9 DC981 3022081 WP LT WING CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND LEFT WING PANEL NR 1163C HAS BARE METAL AND SURFACE CORROSION AROUND EDGES. REMOVED CORROSION. MAT LOSS IS OUT OF LIMITS. COUNTERSINK NEW PANEL. (M) 2 L 7 2 4F A6WE 2002061900222 20020619 00222 WP 2002 6 19 GTIA020464 1 20020324 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND BLUE WATER AND STAINS FOUND IN LONGERON 30 FROM FORWARD BULKHEAD TO BULKHEAD IN FORWARD BAG BAY. REMOVED CO RROSION. REMOVED LONGERON 30 STATION 323-494. DRILLED AND LOCATED LONGERON STATION 323-494. INSTALLED LONGERON 30. ( M) 2 L 7 2 4F A6WE 2002061900223 20020619 00223 EA 2002 6 19 CA020610006 1 20020607 A 2710 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE AILERON QUADRANT LACK OF LUBE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AUTOPILOT TRIM RWD/LWD AFTER T/O AUTO PILOT DISCONNECTED AND FOUND DIFFICULT TO MOVE AILERONS.(L1255080) BOTH LT A ND RT AILERON QUADRANTS LUBRICATED WITH BRAYCO NR 300 TO DISPLACE MOISTURE AND AILERON INSPECTION CHECK CARRIED OUT. OPS CHKS NORMAL SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002061900225 20020619 00225 CE 2002 6 19 CA020611001 1 20020610 A 2897 57181061 WIRE HARNESS 1C1217 CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP BOOST PUMP CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION AND COMPLYING WITH AD 2002-09-13 AND CESSNA SERVICE BULLITEN CQB02-1 REV. 1, FOUND THAT THE BLA CK WIRE IN THE HARNESS WAS CHAFED THROUGH AND ARCING TO GROUND ON THE FUEL PUMP SHROUD. THE OTHER WIRES IN THE HARNESS WERE ALSO CHAFED, BUT NO INDICATION OF ARCING FROM THEM WAS DETECTED. 1 L 7 2 3T 4 T RT A28CE E4WE 2002061900226 20020619 00226 WP 2002 6 19 GTIA020465 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT STATION Y160 TO STA Y 197, X55. REMOVED FLOOR SUPPORT. FABRIC ATED NEW SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002061900227 20020619 00227 WP 2002 6 19 GTIA020466 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS Y162 TO Y197, X44. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002061900228 20020619 00228 EU 2002 6 19 CA020612003 1 20020610 A 2612 CONNECTOR GRAVINER BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU FIRE LOOP CONTAMINATED W B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) DEPARING YYH FOR YCB NR 2 ENGINE FIRE WARNING OBSERVED. DRILL CARRIED OUT AIRCRAFT RETURNED TO POINT OF DEPARTURE LANDING WITH OUT INCIDENT. MAINTENANCE FOUND FIRE LOOP CONNECTOR OIL FOULED, NO EIDENCE OF FIRE, CONNECTOR CLEANED, SYST EM CHECKED SERVICEABLE. BOTH NR 2 BOTTLES REPLACED AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 3T 4 T A24EU A196 2002061900229 20020619 00229 NM 2002 6 19 S02252010 1 20020413 A 5270 LATCH BOEING 747 747209B NM PWA JT9 JT9D7R4G2 52054 NE CARGO DOOR OUT OF ADJUST W SAJF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 03 24308 B18771 AFT T/O POWER SET SPEED BETWEEN 80 TO 100 KNOTS FOUND SIDE CARGO DOOR LIGHT ILLUM. FOUND BOTH OUTSIDE AND INSIDE MASTER LATCH LOCK HANDLES WERE POPPED OUT AND PRESSURE RELIEF DOOR WERE OPENED. 2.IAW AMM 52-32-06 P501 ADJUSTED MASTER LATCH LOCK MECHANISM. 3.OPERATED SIDE CARGO DOOR SEVERAL TIMES AND CONFIRM DOOR WAS LATCHED AND NO DOOR WARNING LIGHT I LLUM. 4 NO FURTHER SIMILAR REPORT ON SUBSEQUENTLY FLIGHT. 2 L 7 4 4F 4 F RT A20WE E3NE 2002061900230 20020619 00230 NM 2002 6 19 S02877006 1 20020330 A 7700 6672M213 MODULE BOEING 737 737800* NM CFMINT CFM56 CFM567B26US NE ANTI VIBRATION FAILED W SAJF O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 03 28407 874429 B18609 ENG-1 VIB IND UP TO 5.0 UNITS AFT T/O, EVEN T/L RETARD TO IDLE. THE VIB IND REMAINS THE SAME. THE OTHER PARAMETER S WAS NML. THE IND BACK TO NML AFT 45 MINS, CREW ALSO MENTIONED ABOUT O/T,ENG-1/125 DEG C,ENG-2/95 DEG C. AFT MAINTENAN CE INSP CONFIRM THAT IS CAUSED BY VIB IND DISPLAY PROBLEM. 2.THE ENG-1 VIB IND ITEM C/F TO D/D PER MEL 77-5. ALTHOUGH TH E IND BACK TO NML. A/C DISPATCHED & OPERATED NML OF SUBSEQUENT FLT. 3.IAW QAR DATA, ENG-1 VIB IND WILL SUDDENLY JUMP FM 0.5 TO 5.0 UNIT WITHOUT ENG POWER CHANGED. IT OBVIOUSLY IS A FALSE IND PROBLEM. 4.TPE O/N REPLACED AVM CONDITIONER AND S ENT BACK TO VENDOR FOR INVESTIGATION AND AS A RESULT OF NO FAULT FOUND. 5.BASE ON QAR DATA AND NO REPEAT SQUAWK WAS SHOW 2 L 7 2 4F 4 F RT A16WE E00055EN 2002061900244 20020619 00244 SO 2002 6 19 COMA0210027 1 20020617 A 2750 KRP138112VT ROLLER EMB 120 EMB120RT 3260202 SO R/H FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 463CA 120267 FLIGHT 6043 FLAP DISAGREEMENT WARNING AFTER T/O.REPLACED WORN ROLLERS ON R/H OUTBD FLAP. 2 L 7 2 4T RT A31SO 2002061900245 20020619 00245 EA 2002 6 19 COMA0260376 1 20020618 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 718.00 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 924CA 20401 7026 F.S. 718.00 FRAME CRACKED BELOW STRINGER 11 ON R/H SIDE.REPAIRED CRACKED FRAME BY REMOVING DAMAGED AREA, PERFORMED EDDY CURRENT ON AREA AND INSTALLED NEW FRAME SECTION I/A/W CANADAIR REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2002061900246 20020619 00246 EA 2002 6 19 COMA0260377 1 20020618 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS718.00 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 924CA 20401 7026 FS 718.00 FRAME CRACKED BELOW STRINGER 11 ON L/H SIDE.REPAIRED CRACKED FRAME BY REMOVING DAMAGED AREA, PERFORMED EDDY CU RRENT ON AREA AND INSTALLED NEW FRAME SECTION I/A/W CANADAIR REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2002062000001 20020620 00001 EU 2002 6 20 C2XA02IA128 1 20020616 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 86842 286 IAH- DURING POST FLIGHT INSPECTION THE CREW NOTED THAT THE EMERGENCY LIGHTS ON THE FORWARD LEFT HAND FLOOR SECTION FAIL ED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK, PERFORMED A OPERATIONAL CHECK OF T HE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVECE. 2 H 7 2 4T RT A53EU 2002062000016 20020620 00016 NM 2002 6 20 02FDEA00410 1 20020611 A 5314 KEELBEAM BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 RT WHEEL WELL KEELBEAM FWD VERTICAL CHORD IS CRACKED BETWEEN TWO FASTENERS. 2 L 7 3 4F RT A3WE 2002062000017 20020620 00017 WP 2002 6 20 02FDEA00411 1 20020614 A 2425 WARNING LIGHT DOUG DC10 DC1010 3022110 WP COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 25 365FE 46601 CLIMBING THROUGH FL200 THE NR 1 GEN OFF LIGHT CAME ON (AFTER LOSING THE NR 3 GEN ON T/O) RAN RED TABS. DISCONNECTED NR 1 GEN. TRIED UNSUCCESSFULLY TO START APU AT FL240, FL230, FL150, FL10. RETURNED TO MEM. APU STARTED ON TAXI IN. GROU ND RAN ENGINES IAW DC-10 JRH CHAPT 5A. PERFORMED ENGINE GEN TEST IAW DC-10 JRH CHAPT 8. ALL TESTS PASSED. CHECKED SER VICE ON NR 1 CSD, CHECKS GOOD. STARTED APU 4 TIMES ON GROUND IAW DC-10 JRH CHAPT 3. ALL STARTS CHECKED GOOD. NO FAULT S FOUND AT THIS TIME. OK FOR CONTINUED SERVICE. 2 L 7 3 4F A22WE 2002062000018 20020620 00018 WP 2002 6 20 02FDEA00412 1 20020612 A 5321 FLOOR PANEL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 N 540, 542, 544, 547, 551 CORROSION ON MAIN CABIN FLOOR PANELS. REMOVED AND REPLACED PANELS. 2 L 7 3 4F A22WE 2002062000019 20020620 00019 2002 6 20 2002F00634 4 20020616 A 3460 4052506955 FMC BOEING 757 75733N 1384931 NM E/E BAY FAULTY G AMTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 558TZ 590 590 32592 FLIGHT NUMBER 761, DURING CLIMB NO BEARING AND DISTANCE INFORMATION ON RIGHT CDU FOR ACTIVE WAYPOINT ONLY. WOULD NOT CO UPLE WITH RIGHT AUTOPILOT. AIRCRAFT MADE AN UNSCHEDULED LANDING AT DEPARTURE AIRPORT. MAINTENANCE REMOVED AND REPLACED THE RIGHT FMC IN ACCORDANCE WITH MM 34-61-00-5, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 2002062000020 20020620 00020 CE 2002 6 20 6182002 1 20020618 A 3010 CONTACTOR BEECH MU300 400A 1155402 CE HORIZ STAB BURNED E DJFA K NONE J WARNING INDICATION CR CRUISE 1 EA 23 418CW 4583 RK18 HORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT. 2 H 7 2 4F RT A16SW 2002062000021 20020620 00021 CE 2002 6 20 61820022 1 20020618 A 3010 CONTACTOR BEECH MU300 400A 1155402 CE HORIZ STAB BURNED E DJFA K NONE J WARNING INDICATION CR CRUISE 1 EA 23 417CW 4602 RK17 HORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT. 2 H 7 2 4F RT A16SW 2002062000022 20020620 00022 NM 2002 6 20 ABXA010912 1 20020614 A 2710 BEARING BOEING 767 767231 1385131 NM AILERON CONTROL SEIZED A ABXA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 GL 23 707AX 22570 CAPTAIN'S AND FIRST OFFICER'S AILERON CONTROL WHEEL BINDING. COMPLIED WITH FIM 27A-11-00, FIG 106, BLOCK 1,2. FOUND BE ARING ON LEFT WHEEL WELL QUADRANT CENTERING FORCE SEIZED. REPLACED BEARING IAW BOEING STANDARD OVERHAUL PRACTICES MANUA L 20-50-03. AILERONS OPERATED NORMALLY. 2 L 7 2 4F RT A1NM 2002062000023 20020620 00023 EU 2002 6 20 AWXA200200525 1 20020617 A 2910 NAS1611009 O-RING AIRBUS 320 A320232 3930326 EU HYD SYSTEM WORN A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 669AW 1792 CMH - DIVERSION - FLT 0249 - EN ROUTE FROM PHX TO PHL, DURING CRUISE AIRCRAFT EXPERIENCED AN ECAM MESSAGE FOR YELLOW SYS TEM HYDRAULIC LOW PRESSURE. CHECKED QTY, INDICATED EMPTY. INFLIGHT DIVERTED TO CMH ECAM ACTIONS COMPLETED. REMOVED AN D REPLACED O-RING AT NR 2 ENGINE PRESSURE TRANSDUCER. SERVICED YELLOW SYSTEM, LEAK CHECK PERFORMED, NO LEAKS NOTED. 2 L 7 2 4F RT A28NM 2002062000024 20020620 00024 2002 6 20 AWXA200200526 4 20020617 A 2565 D31517113 SLIDE AIRBUS 320 A320232 3930326 EU AFT DOOR DEPLOYED A AWXA K NONE O OTHER TX TAXI/GRND HDL 1 WP 28 654AW 1050 MEX - EMERGENCY EQUIPMENT - UPON ARRIVAL TO THE AIRCRAFT, PILOT REPORTED LT AFT DOOR SLIDE INFLATED AND STILL ATTACHED T O THE AIRCRAFT. MAINTENANCE ULTIMATLEY REMOVED AND REPLACED SLIDE. 2 L 7 2 4F RT A28NM 2002062000025 20020620 00025 EU 2002 6 20 AWXA200200527 1 20020617 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 627AW 29268 29268 66 CMH- EEL - DURING CHECKS OF THE EMERGENCY LIGHTING SYSTEM, MAINTENANCE FOUND LT OVERWING SLIDE EMERGENCY LIGHTS INOPERAT IVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY PER MM 33-51-32-401. LIGHTS CHECKED OK. 2 L 7 2 4F RT A28NM 2002062000026 20020620 00026 SO 2002 6 20 C2XA02CL132 1 20020614 A 3350 7287103507 CONTROL UNIT EMB 145 EMB145 3260210 SO CABIN MALFUNCTIONED A C2XA K NONE O OTHER CR CRUISE 1 SW 27 27962 3796 145110 CLE FLIGHT NR 3275 THE CREW REPORTED THE EMERGENCY LIGHT ARMED INDICATION WAS NOT ON WHILE IN FLIGHT. MAINTENANCE INSPE CTED AND REPLACED THE CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002062000027 20020620 00027 2002 6 20 C2XA02CL133 4 20020616 A 2210 AUTOPILOT SYS EMB 135 EMB135LR 3260305 SO COCKPIT MALFUNCTIONED A C2XA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14514 145303 CLE FLIGHT 4015 THE CREW REPORTED A AUTO PILOT FAIL MESSAGE AFTER FLIGHT INTO MODERATE TURBULENCE ASSOCIATED WITH BURNIN G SMELL IN THE COCKPIT AND CABIN. MAINTENANCE INSPECTED AND PERFORMED AUTO PILOT CHECKS AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002062000032 20020620 00032 EA 2002 6 20 SWIA200210846 1 20020515 A 2421 PIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE IDG CONNECTOR BROKEN A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 440SW 7589 ABORTED THE TAKEOFF DUE TO AN AMBER CAUTION IDG 2 MESSAGE ON THE EICAS AND IDG 2 FAULT ON THE OVERHEAD PANEL. INSPECTED IDG 2 & FOUND ELECTRICAL CONNECTOR FOR TEMP BULB HAS A BROKEN PIN. INSTALLED NEW PIN ON CONNECTOR & RESECURED CANNON P LUGS. RAN RIGHT ENGINE FOR SEVERAL MINUTES. OPS CHECK GOOD FOR IDG 2. 2 L 7 2 4F 4 F RT A21EA E15NE 2002062000033 20020620 00033 SO 2002 6 20 SWIA200210847 1 20020516 A 2731 SPLICE EMB 120 EMB120ER 3260203 SO ELEVATOR CORRODED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 581SW 120349 ON TAKEOFF OUT OF FAT, TRIM TAKEOFF WARNING SOUNDED. ABORTED TAKEOFF. TRIM WAS SET TO 25 PERCENT MAX (CENTER OF GREEN BAND). AFTER RESETTING THE TRIM COMPUTER, ATTEMPTED A STATIC TAKEOFF AND STILL GOT THE TRIM WARNING. REPLACED CORRODED SPLICES BY ELEVATOR TRIM PROXIMITY SENSORS. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002062000034 20020620 00034 WP 2002 6 20 2002FA0000719 1 20020503 A 5313 STRINGER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 WP 07 961R 46133 (STRINGER) FOUND DURING (D) CHECK INSPECTION, STRINGER 31R HAS CORROSION AT STA 680. 2 L 7 4 4F RT 4A25 2002062000039 20020620 00039 WP 2002 6 20 2002FA0000724 1 20020608 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 961R 46133 (LONGERON 24/ FITTING) FOUND DURING (D) CHECK INSPECTION, STA 960 AND LONGERON 24L HOLES ELONGATED IN FITTING AND LONGER ON 24 TWO FORWARD. 2 L 7 4 4F RT 4A25 2002062000040 20020620 00040 WP 2002 6 20 2002FA0000725 1 20020508 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 961R 46133 (LONGERON) FOUND DURING (D) CHECK INSPECTION, STA960 AND LONGERON 24L AFTER FITTING REMOVAL, FOUND CORROSION ON LONGERO N 24 AT FASTENER HOLES. 2 L 7 4 4F RT 4A25 2002062000041 20020620 00041 WP 2002 6 20 2002FA0000726 1 20020506 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 961R 84102 46133 (FLOORBEAM) FOUND DURING (D) CHECK INSPECTION. CORROSION AT STA 920. 63 INCHES LEFT OF CENTER, FLOORBEAM. 2 L 7 4 4F RT 4A25 2002062000042 20020620 00042 EA 2002 6 20 SWIA200210848 1 20020514 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE T/E FLAP FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 405SW 7029 FLAP FAIL MESSAGE ON CLIMBOUT. RECEIVED THE FAIL MESSAGE FROM FLAPS 8 DEGREES TO 0 DEGREES. UPON LANDING AND CHECKING THE FLAPS, FLAPS WERE AT 0 DEGREES OR FULLY UP. REMOVED AND REPLACED FLAP BRAKE POSITION SENSOR IAW MM 27-51-10. OPS C HECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002062000044 20020620 00044 NM 2002 6 20 A6WA200230011 1 20020531 A 2760 PSEU DORNER DO32 DO328100 2996000 NM GROUND SPOILER FAILED A A6WA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 31 328MX 3071 GROUND SPOILERS DEPLOYED ON TAKEOFF WITH ASSOCIATED TAKEOFF CONFIG MESSAGE. MAINTENANCE TROUBLESHOT AND PERFORMED PSEU AND PL/CL SWITCH CHECKS, NO FAULTS FOUND. REMOVED AND REPLACED RELAYS 4CS, 6CS, AND 8CS. PERFORMED OPS CHECK AND INFLI GHT INHIBIT CHECKS. ALL CHECKS GOOD. 2 H 7 2 4T RT A45NM 2002062000045 20020620 00045 SO 2002 6 20 SWIA200210849 1 20020512 A 5753 BRACKET EMB 120 EMB120ER 3260203 SO T/E FLAP BROKEN A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 251YV 120251 ON FLAP RETRACTION AFTER TAKEOFF, DISAGREEMENT LIGHT ILLUMINATED. AFTER FOLLOWING QRH AND RESETTING, LIGHT REMAINED ILL UMINATED. RETURNED TO LAX. REPLACED A BROKEN ROLLER BRACKET OF THE LEFT OUTBOARD TRAILING EDGE FLAP INBOARD BRACKET. FLAPS OPERATE NORMALLY. 2 L 7 2 4T RT A31SO 2002062000046 20020620 00046 CE 2002 6 20 AK62002F00000 1 20020531 A 5711 BRACKET CESSNA 414 414A 2075907 CE SPAR ATTACH CORRODED B AK6R K NONE O OTHER IN INSP/MAINT 1 SW 19 414CL 5834 414A0011 UPON REMOVAL OF WING TO STUB WING ATTACHMENT PANELS FOR AN ANNUAL INSPECTION. A SEVERELY CORRODED UPPER REAR SPAR ATTAC H BRACKET WAS FOUND. THIS FITTING HAS SEVERE INTER GRANULAR CORROSION. THE AIRCRAFT IS BASED OUT OF TEXAS AND HAS SPEN T LOTS OF TIME ON THE RAMP. 1 L 7 2 3O A7CE 2002062000047 20020620 00047 SO 2002 6 20 ASO2002F00016 1 20020322 A 5712 12026501002 RIB EMB 120 EMB120RT 3260202 SO RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 230AS 120032 DURING HANGER MAINTENANCE, THE RT INBOARD FLAP INBOARD FIXED TRACK SUPPORT WAS CRACKED. MAINTENANCE INSTALLED A TEMPORA RY REPAIR TO THE FLAP TRACK SUPPORT RIB IAW THIS EO SETS THE FLIGHT LIMIT NOT TO EXCEED 400 FLIGHT HOURS BEFORE THE PER MANENT REPAIR IS DONE AND ALSO STTES THE RIB MUST BE REPLACED AT THE NEXT (A) CHECK. MAINTENANCE REMOVED AND REPLACED T HE CRACKED FLAP TRACK SUPPORT RIB. 2 L 7 2 4T RT A31SO 2002062000048 20020620 00048 SO 2002 6 20 ASOA02203S 1 20020322 A 5712 12026501002 RIB EMB 120 EMB120RT 3260202 SO RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 230AS 120032 DURING HANGER MAINTENANCE, THE RIGHT INBOARD FLAP INBOARD FIXED TRACK SUPPORT WAS CRACKED. MAINTENANCE INSTALLED A TEMP ORARY REPAIR TO THE FLAP TRACK SUPPORT RIB IAW EO. THIS EO SETS THE FLIGHT LIMIT NOT TO EXCEED 400 FLIGHT HOURS BEFORE THE PERMANENT REPAIR IS DONE AND ALSO STATES THE RIB MUST BE REPLACED AT THE NEXT (A) CHECK. MAINTENANCE REMOVED AND RE PLACED THE CRACKED FLAP TRACK SUPPORT RIB IN ORDER TO COMPLY WITH A PERMANENT REPAIR OF THIS AIRCRAFT. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T RT A31SO 2002062000049 20020620 00049 EA 2002 6 20 SWIA200210850 1 20020516 A 2421 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA NR 1 ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 NM 07 909SW 7558 ON TAKEOFF OUT OF 2500 FT, THE NR 1 GENERATOR WENT OFFLINE. FOLLOWED QRH, ATTEMPTED TO RESET IT AND THE ADG DEPLOYED. RETURNED TO LAX. REMOVED AND REPLACED NR 1 IDG, GCU AND SERVICED NR 2 IDG WITH OIL. GROUND RAN. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002062000050 20020620 00050 EA 2002 6 20 ASOA02282 1 20020519 A 2760 CC670900301 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA SPOILERS OUT OF ADJUST A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 703EV 10038 DURING CLIMB OUT, AT APPROXIMATELY 29,000 FEET, THE CAPTAIN RECEIVED AN INBOARD GROUND LIFT SPOILER DEPLOYMENT MESSAGE. THE CAPTAIN DECREASED THE CLIMB AND NOTICED A BUFFET AT THAT TIME. SHORTLY THEREAFTER, THE MESSAGE CLEARED. AIRCRAFT RETURNED FOR A SAFE LANDING. MAINTENANCE REMOVED AND REPLACED THE GROUND SPOILER SELECTOR VALVE ON THE LEFT SIDE, THE L EFT SPOILER AND STABILIZER CONTROL UNIT, AND THE LEFT INBOARD GROUND SPOILER ACTUATOR. MAINTENANCE ALSO ADJUSTED ALL OF THE GROUND SPOILER PROXIMITY SENSORS AND TARGET WHICH WERE MOST LIKELY THE CAUSE OF THIS DISCREPANCY. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F RT A21EA 2002062000051 20020620 00051 EA 2002 6 20 ASOA02284 1 20020520 A 2120 SMOKE CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A ASOA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 11 843AS 7310 APPROXIMATELY TWO MINUTES AFTER TAKEOFF, THE CAPTAIN RECEIVED A SMOKE TOILET MESSAGE. THE FLIGHT ATTENDANT CALLED APPR OXIMATELY THREE SECONDS LATER TO REPORT THE SMELL OF SMOKE BUT NO ACTUAL SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED FOR SAFE BUT OVERWEIGHT LANDING. MAINTENANCE PERFORMED THE OVERWEIGHT LANDING INSPECTION, AND NO DEFECTS WERE NOTED. MAINTENANCE INSPECTED THE AIRCRAFT RUNNING BOTH ENGINES AS WELL AS BOTH AIR CONDITIONER PACKS, BUT THE DISCREPANCY WAS NOT DUPLICATED. THERE WAS NO EVIDENCE OF FIRE, SMOKE, OR HEAT NOTED AT THAT TIME. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002062000052 20020620 00052 SO 2002 6 20 SWIA200210851 1 20020519 A 5753 ROLLER EMB 120 EMB120ER 3260203 SO T/E FLAP WORN A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 579SW 120347 RECEIVED FLAP DISAGREEMENT MESSAGE WHILE CLIMBING OUT OF SUN. USED QRH TO FIX. REMOVED AND REPLACED ALL FLAP ROLLERS O N BOTH INBOARD FLAPS IAW EMB 120 MM 27-50-12. RAN FLAPS UP & DOWN SEVERAL TIMES. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002062000053 20020620 00053 EU 2002 6 20 ASOA02288 1 20020523 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 531AS 454 DURING (C) CHECK INSPECTION, THE RIGHT HAND OUTBOARD SEAT TRACK HAD CORROSION OUT OF LIMITS TEN INCHES AFT OF FRAME 34 A T THE (T1) NUTPLATE HOLE AREA. MAINTENANCE REPAIRED THE CORRODED SEAT TRACK IAW EO. 2 H 7 2 4T RT A53EU 2002062000054 20020620 00054 2002 6 20 SWIA200210852 4 20020517 A 3418 607300001 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 427SW 3248 3248 7497 AFTER TAKEOFF, THE STALL FAIL CAUTION MESSAGE CAME ON. COMPLIED WITH QRH. RETURNED TO SLC. REMOVED AND REPLACED NR 1 MACH TRANSDUCER. OPS CHECKS GOOD IAW 27-35-25. 2 L 7 2 4F RT A21EA 2002062000055 20020620 00055 SO 2002 6 20 SWIA200210853 1 20020411 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 236SW 120312 RIGHT SIDE SEAT TRACK IN FORWARD CABIN AREA HAS CORROSION AROUND SEVERAL SCREWS. REMOVED AND REPLACED RIGHT SIDE FORWAR D FLOOR SEAT TRACK IAW 53-01-05. 2 L 7 2 4T RT A31SO 2002062000056 20020620 00056 SO 2002 6 20 SWIA200210854 1 20020411 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 236SW 120312 CENTER OMEGA BEAM AT BUTT STRAP SPLICE A BEAM LAV HAS VISIBLE CORROSION EXTENDING MORE THAN 10 PERCENT INTO MATERIAL. R EMOVED AND REPLACED THE CENTER OMEGA BEAM IAW SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002062000057 20020620 00057 SO 2002 6 20 SWIA200210855 1 20020411 A 5320 BUTT STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 236SW 120312 CENTER BUTT STRAPS A BEAM LAV HAVE DEEP PITTING AND INTERGRANULAR CORROSION. REMOVED AND REPLACED (2) CENTER BUTT STRAP S IAW SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002062000058 20020620 00058 SO 2002 6 20 SWIA200210856 1 20020411 A 5320 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 236SW 120312 BOTH CENTER CROSS BEAMS ADJACENT TO CENTER OMEGA BEAM AT LAV AREA HAVE DEEP PITTING AND INTERGRANULAR CORROSION. REMOVE D AND REPLACED BOTH CENTER CROSS BEAMS IAW SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002062000059 20020620 00059 SO 2002 6 20 SWIA200210857 1 20020411 A 5320 BUTT STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 236SW 120312 RIGHT SIDE BUTT STRAP A BEAM LAV HAS DEEP PITTING AND INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT SIDE BUTT STR AP IAW SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002062000060 20020620 00060 2002 6 20 SWIA200210859 4 20020506 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT SYS FAULTY A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 268UE 5273 120207 ON TAKEOFF ROLL, AUTOPILOT AND TRIM FAIL LIGHTS ILLUMINATED. AP SELECTED TO FO. ABORTED TAKEOFF. REMOVED AND REPLACED AP COMPUTER NR 2. GROUND TESTED OK PER MM 22-10-00. 2 L 7 2 4T RT A31SO 2002062000061 20020620 00061 2002 6 20 SWIA200210860 4 20020514 A 3425 6229336400 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 433SW 1222 1222 7550 COPILOT'S PFD FAILED WITH ASSOCIATED MAG FAIL FLAG AND FLIGHT DIRECTOR FAILED FLAG. NO EFIS COMP MON OR COMPARITOR MESS AGES. REMOVED AND REPLACED NR 2 AHC89E. OPS CHECK GOOD. RELEASED FOR CAT II OPERATIONS. 2 L 7 2 4F RT A21EA 2002062000062 20020620 00062 SO 2002 6 20 SWIA200210861 1 20020517 A 3320 BALLAST EMB 120 EMB120ER 3260203 SO LAVATORY MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 209SW 120269 SMOKE COMING FROM LAV OVERHEAD LIGHTS. CIRCUIT BREAKER 30A POPPED. REPLACED LAV LIGHT BALLAST. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002062000063 20020620 00063 SO 2002 6 20 SWIA200210862 1 20020517 A 3230 12043270501 CONTROL BOX EMB 120 EMB120ER 3260203 SO LANDING GEAR MALFUNCTIONED A SWIA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 NM 07 216SW 5856 120285 GEAR WILL NOT RETRACT AFTER TAKEOFF. ALL GREEN LIGHTS ILLUMINATED AND ALL RED ILLUMINATED EXCEPT RIGHT MAIN -A- SYSTEM LIGHT DID NOT ILLUMINATE. BULBS TEST GOOD. RETURNED TO DRO. REPLACED LANDING GEAR RELAY BOX. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002062000064 20020620 00064 NE 2002 6 20 SWIA200210863 2 20020520 A 7321 EEC EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE NR 1 ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 269UE 120194 ABORTED TAKEOFF IN FAT DUE TO LEFT EEC FAILURE. RAN NR 1 ENGINE IAW 71-00-00. RAN WITHIN PARAMETERS. OPS CHECKS GOOD AT THIS TIME. NO OTHER DEFECTS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2002062000065 20020620 00065 EU 2002 6 20 MALA020357 1 20020618 A 2610 FIRE DETECTOR SAAB SF340 340B 7860101 EU A MALA K NONE L NO TEST NR NOT REPORTED 1 GL 15 366PX 340B267 BEFORE FLIGHT #3255, CARGO SMOKE NOT TESTING IN BJI. FERRIED AC TO MSP. MAINTENANCE REPAIRED BROKEN WIRE COMMON TO FW D CARGO SMOKE DETECTOR CONNECTOR. COMPLETED OPERATIONAL TEST IAW SF340 AMM 26-13-00-5 OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002062000066 20020620 00066 2002 6 20 SWAA021229 4 20020603 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002062000067 20020620 00067 NE 2002 6 20 ASOA2281 2 20020518 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A 30015 NE LEFT FAILED A ASOA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 11 835AS 7258 ON APPROACH, DESCENDING THROUGH 9,000 FEET, THE LT ENGINE OIL LOW PRESSURE WARNING LIGHT ILLUMINATED. THE OIL PRESSURE MOMENTARILY FLUCTUATED BACK TO THE GREEN ARC, BUT THEN DROPPED DOWN TO ZERO PSI. THE CAPTAIN COMPLETED THE ENGINE OIL P RESSURE CHECKLIST, WHICH INCLUDES THE SECURING OF THE ENGINE, FOLLOWED BY THE SINGLE ENGINE CHECKLIST. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE GEARBOX BOROSCOPE CRANK PAD COVER OFF. AFTER DOWN LOA DING THE DIGITAL FLIGHT DATA RECORDER, MAINTENANCE LEARNED THE LEFT ENGINE RAN FOR 2.5 MINUTES WITH NO OIL PRESSURE. MA INTENANCE REMOVED AND REPLACED THE LT ENGINE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002062000068 20020620 00068 WP 2002 6 20 0201939612 1 20020516 A 5320 DOOR DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612NW 47436 During line mtc operations at ORD, the inner skin of the MLG fuselage mounted door RHS was found to sustained crack dama ge at two locations. Repaired per EA96-189718. 2 L 7 2 4F A6WE 2002062000069 20020620 00069 WP 2002 6 20 0201949605 1 20020520 A 5330 SKIN DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 During Hck in DHN, a crack was found in the skin common to the fasteners picking up the APB tee cap. Repaired per EA 96- 190036. 2 L 7 2 4F A6WE 2002062000070 20020620 00070 WP 2002 6 20 0201959861 1 20020516 A 5310 BULKHEAD DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 770NC 47758 During Mck in ATL, a .65" crack was found in the upper bend radius of the APB channel.Repaired per EA 98-189685. 2 L 7 2 4F RT A6WE 2002062000071 20020620 00071 WP 2002 6 20 0201969862 1 20020521 A 5310 LONGERON DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 771NC 47769 During MCK in ATL, Corrosion was found around fastener holes in four places in the base flange of longeron 30 between fr ame 377 and 389. Repaired per EA 98-189737. 2 L 7 2 4F RT A6WE 2002062000072 20020620 00072 NM 2002 6 20 BJN2002F00000 1 20020516 A 3350 37067001 BATTERY BOEING 737 737282 13844AT NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVE AND REPLACE BATTERIES ON BATTERY PACK PER MM. OPS TEST NORMAL. 2 L 7 2 4F RT A16WE 2002062000073 20020620 00073 NM 2002 6 20 SWAA021235 1 20020603 A 2782 6544551 ACTUATOR BOEING 737 7373H4 1384600 NM KRUEGER FLAP FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 612SW 27930 AIR TURNBACK, DURING FLAP RETRACTION, THE L/E AMBER LIGHT AND NR 4 KRUEGER FLAP GREEN LIGHT SHOWED FULL EXTEND. RECYCLE D FLAPS, NO HELP. VISUAL INSPECTION SHOWED NR 4 KRUEGER FLAP WAS STUCK FULL DOWN. REMOVED AND REPLACED NR 4 KRUEGER FL AP ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2002062000074 20020620 00074 2002 6 20 SWAA021239 4 20020605 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 FWD ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2002062000075 20020620 00075 NM 2002 6 20 SWAA021241 1 20020604 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHTS AT FWD AND AFT ENTRY DOORS WITH SEVERAL BULBS INOP. RELAMPED LIG HTS PER MM. 2 L 7 2 4F RT A16WE 2002062000076 20020620 00076 NM 2002 6 20 SWAA021246 1 20020605 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 986.5, STR 24L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002062000077 20020620 00077 2002 6 20 SWAA021257 4 20020607 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002062000078 20020620 00078 2002 6 20 SWAA021260 4 20020605 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002062000079 20020620 00079 2002 6 20 SWAA021262 4 20020607 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002062000080 20020620 00080 NM 2002 6 20 SWAA021263 1 20020607 A 2560 P2070001 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 796SW 27889 DURING SCHEDULED PM CHECK, FOUND FWD UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002062000081 20020620 00081 NM 2002 6 20 N159PL0001 1 20020607 A 5315 ANGLE BOEING 737 737242 1384477 NM CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Vertical chord cracked on aft side of BS 178 bulkhead B/B 5.7L 2 L 7 2 4F A16WE 2002062000082 20020620 00082 NM 2002 6 20 SWAA021266 1 20020609 A 3350 AD20131A LIGHT BOEING 737 7373H4 1384600 NM SERVICE DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 629SW 27704 AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002062000083 20020620 00083 NM 2002 6 20 SWAA021267 1 20020607 A 3350 6104789 BATTERY BOEING 737 7372H4 138448C NM CARGO BAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED RON, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002062000084 20020620 00084 NM 2002 6 20 159PL0002 1 20020607 A 5315 ANGLE BOEING 737 737242 1384477 NM CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Vertical chord cracked on aft side of BS 178 bulkhead B/B 5.7L 2 L 7 2 4F A16WE 2002062000085 20020620 00085 2002 6 20 SWAA021269 4 20020606 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002062000086 20020620 00086 NM 2002 6 20 SWAA021270 1 20020605 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 EEPLS DAMAGED IN FWD CABIN. REMOVED AND REPLACED DAMAGED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002062000087 20020620 00087 NM 2002 6 20 SWAA021271 1 20020606 A 3350 604222 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED PM CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EXIT LIG HT BATTERY PER MM. 2 L 7 2 4F A16WE 2002062000088 20020620 00088 NM 2002 6 20 BJN2002F00001 1 20020516 A 3350 37067001 BATTERY BOEING 737 737282 13844AT NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 AFT ENTRY DOOR EMERGENCY LIGHT WILL NOT ILLUMINATE WITH SWITH IN ON POSITION. REMOVE AND REPLACE BATTERIES ON BATTERY P ACK PER MM. OPS TEST NORMAL. 2 L 7 2 4F RT A16WE 2002062000089 20020620 00089 NM 2002 6 20 SWAA021275 1 20020606 A 5523 BACB28AM07 BUSHING BOEING 737 7377H4 1384404 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 403WN 29815 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED TAB HINGE BUSHINGS AT NR 2, 3 AND 4 HINGES PER MM. 2 L 7 2 4F RT A16WE 2002062000090 20020620 00090 NM 2002 6 20 BJN2002F00002 1 20020530 A 3350 88829 BATTERY PACK BOEING 737 737282 13844AT NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL. 2 L 7 2 4F RT A16WE 2002062000091 20020620 00091 NM 2002 6 20 BJN2002F00003 1 20020603 A 3350 LIGHT BOEING 737 737282 13844AT NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 FLOOR EMERGENCY LIGHTS MID-SECTION INOPERATIVE. RECONNECTED LAMP TESTED. 2 L 7 2 4F RT A16WE 2002062000092 20020620 00092 NM 2002 6 20 BJN2002F00004 1 20020602 A 3350 LIGHT BOEING 737 737282 13844AT NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 FLOOR EMERGENCY LIGHTS AFT SECTION INOPERATIVE. CLEANED CONTACTS ON LAMPS. 2 L 7 2 4F RT A16WE 2002062000093 20020620 00093 CE 2002 6 20 CGO2002F00000 1 20020410 A 5520 10161000013 TAB BEECH 200 B200 1152922 CE PWA PT6 PT6A11 52043 NE ELEVATOR MISMANUFACTURED B CGOR K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 03 728AM BB1729 TAB, LEFT ELEVATOR. RECEIVED TAB ASSEMBLY, LEFT ELEVATOR NEW FROM MANUFACTURER MISSING THE REQUIRED RIVETS. ASSEMBLY W AS BONDED AND PRIMERED BUT HAD NOT BEEN RIVETED. 1 L 7 2 4T 3 T A24CE E4EA 2002062000094 20020620 00094 CE 2002 6 20 CGO2002F00001 1 20020417 A 2434 STATOR BEECH 36 A36 1151604 CE CONT O550 IO550* SO ALTERNATOR DAMAGED B CGOR K NONE O OTHER IN INSP/MAINT 1 GL 03 3224G 1045 E2924 675942 ALTERNATOR WAS REMOVED FROM ENGINE FOR CYLINDER REMOVAL ACCESS. WHILE REMOVED A 500 HOUR INSPECTION WAS INITIATED. THE STATOR WINDINGS WERE DISCOVERED TO BE OVERHEATED AND BLACKENED. ALTERNATOR HAD ACCUMULATED ONLY 241.7 HOURS SINCE LAS T 500 HOUR INSPECTION. THIS FACILITY HAS BEEN DOING 500 INSPECTIONS AT 400 HOUR INTERNALS. ALTERNATOR WAS WORKING FINE BEFORE INSPECTION. 1 L 7 1 3O 3 O 3A15 E3SO 2002062000095 20020620 00095 NM 2002 6 20 COOSDR02153 1 20020601 A 5755 651734781A SKIN BOEING 727 727224 1384076 NM RT SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69741 22250 RIGHT WING SPOILER NR 14 (PN 65-17347-81A)(SN 2420) UPPER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002062000096 20020620 00096 NM 2002 6 20 SWAA021280 1 20020605 A 5523 6959227 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED C3 CHECK, SWA SI 11111-55, FOUND LT ELEVATOR TAB CONTROL MECHANISM FWD LINKS WORN. REMOVED AND REPLACE D LT ELEVATOR LINKS AND BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002062000097 20020620 00097 NM 2002 6 20 COOSDR02154 1 20020601 A 5523 657279943 TAB BOEING 727 727224 1384076 NM ELEVATOR DELAMINATED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69741 22250 LEFT ELEVATOR TAB (PN 6572799-43)(SN 74084) UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002062000098 20020620 00098 2002 6 20 SWAA021281 4 20020610 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM CABIN DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2 L 7 2 4F A16WE 2002062000099 20020620 00099 NM 2002 6 20 COOSDR02155 1 20020601 A 5755 6517348108A SKIN BOEING 727 727224 1384076 NM LT SPOILER DELAMINATED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69741 22250 SPOILER NR 6 (PN 65-17348-108A)(SN 1214) UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002062000100 20020620 00100 NM 2002 6 20 COOSDR02156 1 20020601 A 5755 651734781A SKIN BOEING 727 727224 1384076 NM SPOILER DELAMINATED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69741 22250 SPOILER NR 1 (PN 65-17347-81A)(SN 2445) UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002062000101 20020620 00101 NM 2002 6 20 COOSDR02157 1 20020601 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE DAMAGED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69741 22250 EXTERNAL FUSELAGE FWD C/C CUTOUT SKIN DAMAGED AT BS 560. 2 L 7 3 4F A3WE 2002062000102 20020620 00102 NM 2002 6 20 SWAA021287 1 20020609 A 2782 3818001003 ACTUATOR BOEING 737 7377H4 1384404 NM L/E SLAT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 752SW 29804 AIR TURNBACK, L/E FLAP TRANSIT LIGHT REMAINED ON WITH ALL L/E DEVICES EXTENDED. REMOVED AND REPLACED NR 1, 6, 7 AND 8 L /E SLAT ACTUATORS PER MM. 2 L 7 2 4F RT A16WE 2002062000103 20020620 00103 NM 2002 6 20 COOSDR02158 1 20020601 A 5511 SPAR BOEING 727 727224 1384076 NM HORIZONTAL STAB CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 69741 22250 RT HORIZONTAL STABILIZER REAR SPAR LOWER CHORD WITH CORROSION. 2 L 7 3 4F A3WE 2002062000104 20020620 00104 NM 2002 6 20 SWAA021289 1 20020609 A 2731 65C25745 PUSHROD BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA B A EMER. DESCENT UNSCHED LANDING F E FLT CONT AFFECTED VIBRATION/BUFFET CL CLIMB 1 SW 29 621SW 28037 AIR TURNBACK, DECLARED EMERGENCY, DURING CLIMB AIRCRAFT STARTED SEVERE VIBRATION. REMOVED AND REPLACED LT ELEVATOR ASSY AND TAB. REMOVED AND REPLACED LEFT AND RT ELEVATOR TAB PUSHROD ASSY'S PER MM. 2 L 7 2 4F RT A16WE 2002062000105 20020620 00105 2002 6 20 SWAA021290 4 20020607 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002062000106 20020620 00106 CE 2002 6 20 CWQ2002F00001 1 20020407 A 7170 MS29513010 O-RING CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP SUMP DRAIN VLVE LEAKING B CWQR K NONE K FLUID LOSS IN INSP/MAINT 1 GL 05 790QS 6507090 AFTER DRAINING FUEL SUMPS DURING PRE-FLIGHT INSPECTION . NOTICED 5 DRAIN VALVES LEAKING. REPLACED O-RINGS. O-RINGS FO UND TO BE CRACKED, O-RINGS THAT ARE RESISTANT TO FUEL SHOULD BE USED. 2 L 7 2 4F 4 F A9NM E6WE 2002062000107 20020620 00107 2002 6 20 SWAA021291 4 20020611 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002062000108 20020620 00108 NM 2002 6 20 SWAA021292 1 20020610 A 3350 BR5013 COVER BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED PM CHECK, FOUND EEPLS FWD END CAP MISSING AND COVERS DAMAGED AT ROW'S 1, 6, 8, 11, 14 AND 17. INSTALLE D END CAP AND REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002062000109 20020620 00109 NM 2002 6 20 SWAA021293 1 20020607 A 3350 65C27093 LENS BOEING 737 7373H4 1384600 NM SERVICE DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LOWER LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASS Y PER MM. 2 L 7 2 4F RT A16WE 2002062000110 20020620 00110 NM 2002 6 20 SWAA021295 1 20020611 A 2731 65C26384 MECHANISM BOEING 737 7373A4 1384585 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED A2 CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB LOCKOUT MECHANISM AND LT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002062000111 20020620 00111 2002 6 20 SWAA021303 4 20020613 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002062000112 20020620 00112 2002 6 20 SWAA021304 4 20020612 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002062000113 20020620 00113 2002 6 20 SWAA021307 4 20020613 A 2565 62562 SLIDE BOEING 737 7377H4 1384404 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR NOT ALIGNED WITH RETAINER BRACKETS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002062000114 20020620 00114 NM 2002 6 20 SWAA021311 1 20020614 A 3350 6104781 BALLAST BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM. 2 L 7 2 4F RT A16WE 2002062000115 20020620 00115 2002 6 20 SWAA021313 4 20020615 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F A16WE 2002062000116 20020620 00116 2002 6 20 SWAA021320 4 20020616 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 102SW 23108 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002062000117 20020620 00117 2002 6 20 SWAA021321 4 20020615 A 2565 1061621469 SLIDE BOEING 737 7375H4 138449D NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002062000118 20020620 00118 SO 2002 6 20 DYV2002F00000 2 20020607 A 7313 INJECTOR CESSNA 421 421C 2076016 CE CONT O520 GTSIO520M 17032 SO FUEL SYSTEM CRACKED E DYVA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 911EA 2610 1010 421C0870 DURING CRUISE FLIGHT RT ENGINE ROUGHNESS AND AN OBVIOUS FUEL LEAK WAS EXPERIENCED. THE PILOT SHUTDOWN AND SECURED THE R T ENGINE AND MADE A SAVE PRECAUTIONARY LANDING AT AN ON AIRPORT LOCATION. THE COMPANY MECHANIC LOCATED A FUEL LEAK AT T HE NR 5 CYLINDER FUEL INJECTION TUBE AT THE MANIFOLD FITTING LOCATION. A CRACK IN THE SOLDERED JOINT WHERE THE FLARE BA LL END FITS TO THE TUBING WAS FOUND. THE LINE WAS REPLACED WITH A SERVICEABLE PART AND THE FUEL SYSTEM WAS LEAK CHECKED AND INSPECTED FOR NORMAL FUNCTION. 1 L 7 2 3O 3 O A7CE E7CE 2002062000119 20020620 00119 WP 2002 6 20 EIA2002019 1 20020210 A 2432 43B034LB03 BATTERY DOUG DC9 DC933F 302207A WP PWA JT8 JT8D9 52048 NE MAIN INOPERATIVE A EIAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 NM 09 945F 47279 DURING CRUISE AT FL 330, AT APPROX 2015Z, THE NR 1 NAV FAILED. SHORTLY AFTER THAT, THE CAPTAINS ADI TUMBLED THEN THE TR ANSMITT FUNCTION OF THE RADIOS FAILED. REPLIES WERE MADE BY THE IDENT ON THE TRANSPONDER. ALL LIGHTS IN THE COCKPIT OT HER THAN THE MASTER WARNING AND COMPARATOR LIGHT FAILED TO ILLUMINATE. ALSO AS AIRCRAFT DECENDED, THE CIRCUIT BREAKERS FOR THE PRESSURIZATION AND OVERHEAD LIGHT POPPED. REMOVED AND REPLACED BOTH AIRCRAFT BATTERIES PER N2402, NR 1 NAV SYST EM OPS CHECK GOOD PER MM. 2 L 7 2 4F 4 F A6WE E2EA 2002062000120 20020620 00120 NM 2002 6 20 159PL0003 1 20020607 A 5315 BEAM BOEING 737 737242 1384477 NM CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 B.S.967 floor beam at RBL24 has corroded spot at fastener hole 2 L 7 2 4F A16WE 2002062000121 20020620 00121 EU 2002 6 20 FJT02056571 1 20020515 A 5343 A1029E BOLT BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE331* 01514 WP NLG BROKEN E FJTA K NONE O OTHER IN INSP/MAINT 1 SO 03 657BA 657 WHILE PERFORMING THE 200 LANDING INSPECTION REQUIRED BY AD AND MFG SB, IT WAS DISCOVERED THE TWO UPPER MOUNT BOLTS FOR T HE NOSE LANDING GEAR RETRACTION ACTUATOR ATTACHMENTS WERE BROKEN. COMPLIED WITH INSPECTION REQUIRED, MFG SB AS DIRECTED BY THE ACCOMPLISHMENT INSTRUCTIONS IN PART B. REPLACED NOSE LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BOLTS AS DIREC TED IN PART A OF THE SB, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A21EU E2WE 2002062000122 20020620 00122 NM 2002 6 20 GAI2002F00001 1 20020531 A 3241 656021132 ACCESSORY UNIT BOEING 727 727287 1384020 NM MLG INOPERATIVE A GAIA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 916PG 21690 (LANDING GEAR ACCESSORY) SCHEDULED FLIGHT, DURING GEAR RETRACTION, PARKING BRAKE LIGHT ILLUMINATED. CREW RECYCLED THE GEAR WITH NO CHANGE IN INDICATION. CREW DECLARED AN EMERGENCY LANDING. AT ABOUT 1000 FEET THE LIGHT EXTINGUISHED AND T HE AIRCRAFT LANDING WENT UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT. OPERATION CHECK PERFORMED OK, ON THE GROUND. AIRCRAFT WAS THE RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 2002062000123 20020620 00123 NM 2002 6 20 GAIA02067OP 1 20020603 A 3244 26045611 TIRE BOEING 727 727224 1384076 NM LT MLG RUPTURED A GAIA J DUMP FUEL O OTHER TO TAKEOFF 1 SW 07 69740 20668 DURING TAKE OFF ROLL, CREW FELT A BUMP. WHILE ON ROUTE COMPANY OPERATIONS NOTIFIED CREW THEY HAD BLOWN THE NR 3 TIRE. CREW ELECTED TO CONTINUE ON ROUTE. CREW DUMPED FUEL AND DECLARED AN EMERGENCY LANDING. LANDING WENT UNEVENTFUL. AFTER POST FLIGHT IT WAS NOTED THAT THE NR 1 TIRE WAS THE ONE BLOWN. MAINTENANCE REPLACED BOTH MWA ON THE LEFT GEAR. PERFOR MED INSPECTIONS TO THE FOLLOWING: GEAR, WHEEL WELL AREA, AXIAL, NR 1,2, AND 3 ENGINES, FLAPS. SPECIAL INSPECTION FOR H IGH DRAG LOAD WAS PERFORMED. REPLACED LEFT GEAR DOOR DUE TO DAMAGE. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2002062000124 20020620 00124 NM 2002 6 20 GAIA02068OP 1 20020531 A 3241 ACCESSORY UNIT BOEING 727 727287 1384020 NM MLG INOPERATIVE A GAIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 916PG 21690 (LANDING GEAR ACCESSORY) SCHEDULED FLIGHT, DURING GEAR RETRACTION, THE PARKING BREAK ILLUINATED. CREW RECYCLED THE GE AR WITH ON CHANGE IN INDICATION. CREW DECLARED AN EMERGENCY LANDING. AT ABOUT 1000 FEET THE LIGHT EXTINGUISHED AND THE AIRCRAFT LANDING WENT UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT. OPERATION CHECK P ERFORMED OK ON THE GROUND. AIRCRAFT WAS THE RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 2002062000125 20020620 00125 CE 2002 6 20 GNB2002F00001 1 20020530 A 2720 571509615CR CONTROL CABLE CESSNA 404 404 2075901 CE RUDDER DAMAGED A GNBA K NONE O OTHER IN INSP/MAINT 1 SW 01 165SA 4040622 DURING FUSELAGE INSPECTION FORWARD LEFT RUDDER CABLE BLENDED WERE THE CABLE WEST THRU A RIB WHICH HAD A FANALIC BLOCK ON RIB FOR ANTI-CHAFE PROTECTION. 1 L 7 2 3O RT A25CE 2002062000126 20020620 00126 NE 2002 6 20 GSH2002F00000 2 20020505 A 8530 CYLINDER HEAD DOUG DC3 DC3CS1C3G 3021458 WP PWA R1830 R183092 52020 NE CYLINDER SPLIT E GSHA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SW 01 472AF 55 13485 58466 ENGINE FIRE DURING ATTEMPT AT RESTART ON RAMP. CREW FOUND INDUCTION PIPE MISSING ON NR 11 CYLINDER. FURTHER EXAMINATIO N ON MAY 2 REVEALED HEAD SPLIT FROM CYLINDER. LEFT ENGINE. 2 L 7 2 4R 4 R A669 5E4 2002062000127 20020620 00127 NE 2002 6 20 GSH2002F00001 2 20020505 A 8520 31820 STUD DOUG DC3 DC3CS1C3G 3021458 WP PWA R1830 R183092 52020 NE CRANKCASE SHEARED E GSHA K NONE O OTHER IN INSP/MAINT 1 SW 01 472AF 1156 13485 BP490624 CYLINDER BASE STUDS ON NR 8 CYLINDER SHEARED OFF, ALLOWING CYLINDER TO PULL OFF OF CYLINDER BASE SPIGOT. WHEN THE CYLIN DER GOT FAR ENOUGH OFF THE SPIGOT, THE BOTTOM RING SNAGGED THE BOTTOM OF THE CYLINDER, BREAKING THE RING AND PISTON. TH IS LET THE OIL ESCAPE, AND THE ENGINE LOST OIL PRESSURE. THE CREW FEATHERED THE RIGHT PROP ON APPROACH. 2 L 7 2 4R 4 R A669 5E4 2002062000128 20020620 00128 CE 2002 6 20 GUU2002F00006 1 20020601 A 5530 EWB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81535 14113 UE147 (BOLT) AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLT R EQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLT IAW MFG MM. 2 L 7 2 4T RT A24CE 2002062000129 20020620 00129 CE 2002 6 20 GUU2002F00007 1 20020514 A 5530 EWB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 47542 UE198 (BOLT) AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM. 2 L 7 2 4T RT A24CE 2002062000130 20020620 00130 CE 2002 6 20 GUU2002F00008 1 20020515 A 5530 EWB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 48544 13222 UE183 (BOLT) AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS R EQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM. 2 L 7 2 4T RT A24CE 2002062000131 20020620 00131 CE 2002 6 20 GUU2002F00009 1 20020520 A 5530 EWB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81546 13859 UE187 (BOLT) AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM. 2 L 7 2 4T RT A24CE 2002062000132 20020620 00132 CE 2002 6 20 GUU2002F00010 1 20020528 A 5530 EWB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81536 13798 UE152 AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM. 2 L 7 2 4T RT A24CE 2002062000133 20020620 00133 CE 2002 6 20 GUU2002F00011 1 20020521 A 5530 EWB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81538 12561 UE199 AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM. 2 L 7 2 4T RT A24CE 2002062000134 20020620 00134 CE 2002 6 20 GUU2002F00012 1 20020522 A 5530 WEB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87555 11635 UE234 AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRE D RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM. 2 L 7 2 4T RT A24CE 2002062000135 20020620 00135 CE 2002 6 20 GUU2002F00013 1 20020522 A 5530 WEB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87555 UE234 AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM. 2 L 7 2 4T RT A24CE 2002062000136 20020620 00136 CE 2002 6 20 GUU2002F00014 1 20020526 A 5530 EWB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 69549 13399 UE194 AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM. 2 L 7 2 4T RT A24CE 2002062000137 20020620 00137 CE 2002 6 20 GUU2002F00015 1 20020525 A 5530 EWB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 17541 12944 UE203 AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW BEECH MM. 2 L 7 2 4T RT A24CE 2002062000138 20020620 00138 SW 2002 6 20 GXP2002F00001 1 20020611 A 3220 STRUT SWRNGN SA226 SA226TC 8780404 SW NLG DISCHARGED E GXPA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 616GA TC377 NOSE GEAR DID NOT RETRACT. NOSE GEAR STRUT SERVICED. RETRACTION OF LANDING GEAR PERFORMED. OPS CHECKED GOOD. 2 L 7 2 4T RT A8SW 2002062000139 20020620 00139 EU 2002 6 20 GXP2002F00002 1 20020611 A 2913 MS287788 PUMP AMD FALCON FALCON20 2730103 EU HYDRAULIC SYS FAILED A GXPA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 23 183GA 147 LOOSING HYDRAULIC FLUID FROM SYSTEM 2. REMOVED AND REPLACED MS287788 PACKING ON ALL CONNECTIONS AND FILLED HYDRAULIC SY STEM. RESERVOIR NR 1 OR NR 2. STARTED NR 2 ENG AND LET STABILIZE. OPS CHECKED GOOD 2 L 7 2 4F RT A7EU 2002062000140 20020620 00140 NE 2002 6 20 HALA0200110 2 20020521 A 7260 39700911 ROTOR BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE GEN ROTOR INOPERATIVE A HALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 475HA 55121 DURING CLIMBOUT RIGHT ENGINE SYSTEM FAULT ALERT ON . CREW UNABLE TO CONFIRM FAULT CODE NUMBER. ON ARRIVAL HNL OIL PRES SURE DROPPED TO 2PSI OIL TEMP RISING TO 102 DEGREES. OIL QUANTITY DROPPED TO 2PSI OIL TEMP RISING TO 102 DEGREES. OIL QUANTITY DROPPED TO 2 QUARTS. REMOVED AND REPLACED NR 2 ENGINE GEARBOX ACCESSORY PER MM. REPLACED DEDICATED GENERATOR ROTOR AND DEDICATED GENERATOR STATOR PER MM. LEAK AND OPS CHECK, OK. OK FOR SERVICE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002062000141 20020620 00141 NM 2002 6 20 HALA0200132 1 20020524 A 3260 SWITCH BOEING 767 767300 1385204 NM MLG DEFECTIVE A HALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 584HA 24258 GEAR AND DOORS LIGHT ON AFTER RETRATION. AIRCRAFT RETURNED TO HNL, WHERE AND UNEVENTFUL LANDING WAS. JACKED AIRCRAFT P ER HALM249-767, SWING GEAR PER MM. FOUND ROTARY SWITHC DEFECT. AIRCRAFT BACK TO MORMAL CONDITION. 2 L 7 2 4F RT A1NM 2002091600137 20020916 00137 NE 2002 9 16 HALA0200139 2 20020525 A 7260 39700910 GEARBOX BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE RT ENGINE FAILED A HALA K NONE J WARNING INDICATION CR CRUISE 1 WP 13 480HA 55125 FLT 180 - HNL - FOUND RIGHT ENGINE FAIL LIGHT CAME ON IN FLIGHT. REMOVED NR 2 ENGINE GEARBOX, ACCESSORY PER MM 72-61-00 . INSTALLED GEARBOX PER MM 72-61-00 PARA E2P. LEAK AND OPS CHECK GOOD, PER TEST 5 TASK 71-0014-710-802. (M) 2 L 7 2 4F 4 F TR A6WE E00061EN 2002062000142 20020620 00142 NM 2002 6 20 HALA0200156 1 20020602 A 3030 RELAY BOEING 767 76733A 1385209 NM PITOT HEAT FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM: F/O PITOT HEAT WOULD NOT RESET. REPLACED AIR/GROUNG RELAY K528. PITOT HEAT CHECKS GOOD. NO FAULT MESSAGES. 2 L 7 2 4F RT A1NM 2002062000143 20020620 00143 WP 2002 6 20 JRA2002F00004 1 20020510 A 3297 800212 RELAY CVAC 640 640340D 2422814 WP RROYCE DART DART* NE MLG INTERMITTENT A JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 866TA 283 CLEANED RELAY WITH BRAKE AND ELECTRIC MOTOR CLEANER, LET SET FOR 5 MINUTES AND APPLIED LIGHT AIR PRESSURE. WHEN SYSTEM WAS RE-ENERGIZED, RELAY IGNITED. USED CABIN 13 LB BOTTLE TO EXTINGUISH. CLEANED FIRE EXTINGUISHER RESIDUE. 2 L 7 2 4T 4 T RT A793 2002062000144 20020620 00144 EU 2002 6 20 KBMA113829 1 20020518 A 3110 371GC01Y02 ELECTRICAL BOX SNIAS 350 AS350BA 8680817 EU GEN LIGHT FAILED A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 2300 GENERATOR LIGHT ON AND WAS UNABLE TO RESET. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2002062000145 20020620 00145 NM 2002 6 20 159PL0004 1 20020607 A 5300 TIE CLIP BOEING 737 737242 1384477 NM CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Stringer tie clips cracked upper lobe of cabin various locations (41) total 2 L 7 2 4F A16WE 2002062000146 20020620 00146 NM 2002 6 20 159PL0005 1 20020607 A 5315 FLOORBEAM BOEING 737 737242 1384477 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 CORROSION ON TOP OF 987 FLOORBEAM. 2 L 7 2 4F A16WE 2002062000147 20020620 00147 NM 2002 6 20 159PL0006 1 20020607 A 5347 SEAT TRACK BOEING 737 737242 1384477 NM CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Rt. I/B seat track corroded BS328 to BS360 2 L 7 2 4F A16WE 2002062000148 20020620 00148 NM 2002 6 20 159PL0007 1 20020607 A 5347 SEAT TRACK BOEING 737 737242 1384477 NM CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Rt. O/B seat track corroded BS328 to BS360 2 L 7 2 4F A16WE 2002062000149 20020620 00149 NM 2002 6 20 159PL0008 1 20020607 A 5210 FRAME BOEING 737 737242 1384477 NM FWD ENTRY DOOR CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Fwd entry door top frame cracked fwd of upper aft stop fitting 2 L 7 2 4F A16WE 2002062000150 20020620 00150 NM 2002 6 20 159PL0009 1 20020607 A 5240 DOOR FRAME BOEING 737 737242 1384477 NM FWD SERVICE DOOR CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 FWD SERVICE DOOR CRACKED IN AFT FRAME AT LOWER AFT CAM ROLLER. 2 L 7 2 4F A16WE 2002062000151 20020620 00151 NM 2002 6 20 159PL0010 1 20020607 A 5315 FLOORBEAM BOEING 737 737242 1384477 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 CORROSION AT CLIP NUT HOLE IN FLOORBEAM AT LBL6 STA 344. 2 L 7 2 4F A16WE 2002062000152 20020620 00152 NM 2002 6 20 159PL0011 1 20020607 A 5300 GALLEY TRACK BOEING 737 737242 1384477 NM CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Corrosion on right O/B galley track at fwd end 2 L 7 2 4F A16WE 2002062000153 20020620 00153 NM 2002 6 20 159PL0012 1 20020607 A 5310 TIE BOEING 737 737242 1384477 NM BS460 AT STR16LT CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 BS460 left frame tie cracked at lower fastener just above Str16Lt. 2 L 7 2 4F A16WE 2002062000154 20020620 00154 NM 2002 6 20 159PL0013 1 20020607 A 5315 FLOORBEAM BOEING 737 737242 1384477 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 CORROSION ON STA328 FLOORBEAM AT RBL30 2 L 7 2 4F A16WE 2002080500052 20020805 00052 NM 2002 8 5 159PL0014 1 20020607 A 5320 TIE CLIP BOEING 737 737242 1384477 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 STRINGER TIE CLIP CRACKED AT STA 500A STR 26 LT. 2 L 7 2 4F A16WE 2002062000155 20020620 00155 NM 2002 6 20 ZW0A0206601 1 20020619 A 3350 767 LIGHT BOEING 757 757231 1384950 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 721TW 29954 THE EMERGENCY LIGHT AT THE NUMBER 2 CABIN DOOR ON THE RIGHT SIDE, WAS INOPERATIVE. REPLACED THE BULB. CHECK-C 11-12-00 LAX. 2 L 7 2 4F RT A2NM 2002062000156 20020620 00156 NM 2002 6 20 159PL0015 1 20020607 A 5311 FRAME BOEING 737 737242 1384477 NM STA440 AT STR26L CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Frame cracked at Sta440 at Str26Lt. 2 L 7 2 4F A16WE 2002062000157 20020620 00157 NM 2002 6 20 159PL0016 1 20020607 A 5311 FRAME BOEING 737 737242 1384477 NM STA400 AT STR26L CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Frame cracked at Sta400 at Str26Lt. 2 L 7 2 4F A16WE 2002062000158 20020620 00158 NM 2002 6 20 159PL0017 1 20020607 A 5300 BEAM BOEING 737 737242 1384477 NM BS460 AT STR27RT CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Cargo floor beam cracked at BS460 at Str27Rt. 2 L 7 2 4F A16WE 2002062000159 20020620 00159 NM 2002 6 20 159PL0018 1 20020607 A 5300 SKIN BOEING 737 737242 1384477 NM STA 303 CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Fuselage skin cracked at fwd entry door lower hinge cutout at Sta303 2 L 7 2 4F A16WE 2002062000160 20020620 00160 NM 2002 6 20 159PL0019 1 20020607 A 5312 BULKHEAD BOEING 737 737242 1384477 NM BS178 CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Fwd side of BS178 bulkhead cracked at WL235 Lt. & Rt. sides (4 cracks total) 2 L 7 2 4F A16WE 2002062000161 20020620 00161 NM 2002 6 20 159PL0020 1 20020607 A 5300 SKIN BOEING 737 737242 1384477 NM BS908 CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Corrosion in fuselage skin at BS908 Butt joint 2 L 7 2 4F A16WE 2002062000162 20020620 00162 NM 2002 6 20 159PL0021 1 20020607 A 5300 SKIN BOEING 737 737242 1384477 NM BS986.5 CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Corrosion on fuselage skin at Sta986.5 at Str22Lt & Str23Lt. Corrosion on frame shear tie clip 2 L 7 2 4F A16WE 2002062000163 20020620 00163 NM 2002 6 20 159PL0022 1 20020607 A 5311 FRAME BOEING 737 737242 1384477 NM BS460 AT STR26LT CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 159PL 21186 Sta460 frame cracked past stop drill and new crack in frame at Str26Lt. 2 L 7 2 4F A16WE 2002062000164 20020620 00164 NM 2002 6 20 CALA0200350 1 20020618 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 277-294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17345 23583 INSPECTION FOUND SEAT TRACK CORRODED BELOW #1 GALLEY BETWEEN STA 277-294.5. THE SEAT TRACK WAS REPLACED IAW SRM 51-10-02 . 2 L 7 2 4F RT A16WE 2002062000165 20020620 00165 NM 2002 6 20 CALA0200351 1 20020618 A 5754 SKIN BOEING 737 7373T0 1384582 NM #6 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69348 23586 INSPECTION FOUND #6 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01. 2 L 7 2 4F RT A16WE 2002062000166 20020620 00166 WP 2002 6 20 CALA0200353 1 20020619 A 5320 WEB DOUG DC9 DC982 3022082 WP STA 208 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A 1.5" CRACK IN TANG OF L-1 DOOR TORQUE BOX WEB AT STA 208, LONGERON 15L. A DOUBLER AND FILLER WERE INS TALLED IAW ECRA 5314-01010. 2 L 7 2 4F A6WE 2002062000167 20020620 00167 WP 2002 6 20 CALA0200354 1 20020619 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FS 1271-1287 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND LONGERON 29R CORRODED AT FS 1271-1287. A LONGERON SPLICE REPAIR AND FITTING WERE INSTALLED IAW SRM 51-3 0-2 AND 53-02, FIGURE 18. 2 L 7 2 4F A6WE 2002062000168 20020620 00168 WP 2002 6 20 CALA0200355 1 20020619 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1041-1250 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND L/H I/B SEAT TRACK CORRODED AT FS 1041-1250. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIG URE 4F. 2 L 7 2 4F A6WE 2002062000169 20020620 00169 WP 2002 6 20 CALA0200356 1 20020619 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND FLOORBEAM CORRODED UNDER NUTPLATES AT FS 1338, RBL 58 TO LBL 58. THE UPPER FLOORBEAM CAP WAS REMOVED AN D REPLACED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002062000170 20020620 00170 NM 2002 6 20 02062001 1 20020620 A 3397 W3532050320 WIRE BRUCE BOEING 757 75728A 1384976 NM FWD. CABIN BROKEN A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 549NA 24544 six emergency lights on floor between rows 5 and 6 INOP. Found and repaired broken wire as per WDM 33-51-21, ops ok. 2 L 7 2 4F RT A2NM 2002062100001 20020621 00001 NM 2002 6 21 377PA0002 1 20020618 A 3350 LIGHT BOEING 737 7373L9 1384470 NM A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 377PA 23718 Emergency floor path will not illuminate from row 6 to row 12. Repaired wiring floor emerg. path and acc. test IAW MM 3 3-53-00. Test OK 2 L 7 2 4F RT A16WE 2002062100002 20020621 00002 2002 6 21 371PA0007 4 20020616 A 2330 SMOKE BOEING 737 737306 13844BG NM A PIDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 05 371PA 23543 Smoke from center pedestal after take off. Numerous electrical items inop: #2 reverser unlocked on; #1 start valve lig ht; #2 oil filter bypass; audio panel mic selector light; #2 oil pressure light; aileron trim inop. Discrepancy caused by beverage spill onto pedestal. Found control cabin lighting section 2 CB out. Cleaned effected instruments with cont act cleaner. Reset CB. All systems ops check normal. 2 L 7 2 4F RT A16NE 2002062100003 20020621 00003 EU 2002 6 21 N9W2002F00001 1 20020505 A 3320 AL1235320 LIGHT ISRAEL 1124 1124A 4500103 EU NR 2 RT WINDOW MELTED A N9WA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 11 407W 8370 407 AIRCRAFT DEPARTED, CREW NOTICED SMOKE AND FUMES IN THE CABIN AND COCKPIT. CREW ACCOMPLISHED EMERGENCY ACTION CHECKLIST, MANUALLY DEPLOYED OXYGEN MASKS AND PERFORMED AN EMERGENCY DECENT. THE PILOT IN COMMAND ELECTED TO DIVERT FLIGHT TO TH E NEAREST AIRPORT FOR LANDING. A/C LANDED WITHOUT INCIDENT. REMOVED CABINET AND PANELS AND FOUND LIGHT TUBE (PN AL-123 5-320), AT THE NR 2 RIGHT HAND WINDOW SHORTED AND MELTED. IN ADDITION THE ASSOCIATED LIGHTING ASSY WIRES, RECEPTACLE AN D ADJACENT WALL PANEL WERE MELTED. PRELIMINARY INSP REVEALED THAT THE END CAP CONNECTOR OF THE LAMP ASSY HAD COME LOOSE . THIS CAUSED AN EXCESSIVE HEAT CONDITION. MAINTENANCE IS IN THE PROCESS OF CHECKING ALL ASSOC CONNECTORS AND POWER SU 2 M 7 2 4F A2SW 2002062100004 20020621 00004 NM 2002 6 21 377PA0003 1 20020621 A 5300 SKIN BOEING 737 7373L9 1384470 NM DAMAGED A PIDA K NONE O OTHER EX EXTERNAL LOAD 1 SO 05 377PA 23718 Fuselage skin damaged by belt loader sta 767 to sta 772 between str27Lt. and str27Rt. 2 L 7 2 4F RT A16WE 2002062100005 20020621 00005 NM 2002 6 21 377PA0004 1 20020621 A 5300 SKIN BOEING 737 7373L9 1384470 NM DAMAGED A PIDA K NONE O OTHER EX EXTERNAL LOAD 1 SO 05 377PA 23718 Fuselage skin damaged by belt loader sta 797 to sta 818 at str27Lt. 2 L 7 2 4F RT A16WE 2002062100006 20020621 00006 NM 2002 6 21 377PA0005 1 20020621 A 5300 SKIN BOEING 737 7373L9 1384470 NM DAMAGED A PIDA K NONE O OTHER EX EXTERNAL LOAD 1 SO 05 377PA 23718 Fuselage skin damaged by belt loader at sta 789 to sta 799 between str26Rt. and str27Rt. 2 L 7 2 4F RT A16WE 2002062100007 20020621 00007 NM 2002 6 21 DHL2002745005 1 20020718 A 2740 SWITCH BOEING 727 727224 1384076 NM HORIZ STAB DIRTY A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 745DH 20665 RTO AT PHX DUE TO TAKEOFF WARNING HORN. EVERYTHING SET PROPERLY. CLEANED AND RAN STAB TRIM LIMIT SWITCHES PERFORMED A SATISFACTORY TAKEOFF WARNING TEST MM 27-40-61. 2 L 7 3 4F A3WE 2002062100009 20020621 00009 NM 2002 6 21 QXEA0200849 1 20020530 A 6123 LIGHT BOMBDR DHC8 DHC8401 1390041 NM COCKPIT EXTINGUISHED A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 405QX 4047 PIH - ABORTED TAKEOFF, AUTO FEATHER ARM DISAPPEARED. SELECTED AUTO FEATHER TEST NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002062100010 20020621 00010 NM 2002 6 21 QXEA0200850 1 20020530 A 6123 LIGHT BOMBDR DHC8 DHC8401 1390041 NM COCKPIT EXTINGUISHED A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 405QX 4047 BOI - AUTO FEATHER ARM DISAPPEARED ON ENGINE DISPLAY ON TAKEOFF. COMPLIED WITH FUNCTIONAL CHECK VERIFICATION PER AMM 61 -20-00, PAGE 509-510. COMPLIED WITH TEST IAW AMM 61-20-00, PAGE 511-512. COMPLIED WITH FIM PROCEDURE 61-20-00, PAGES 2 72-274. COMPLIED WITH GROUND RUN ARMED SYSTEM FOUR TIMES. SYSTEM GROUND CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETU RNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002062100011 20020621 00011 NM 2002 6 21 SWAA021284 1 20020609 A 5523 BACB28AM07 BUSHING BOEING 737 7373A4 1384585 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR T AB BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002062100012 20020621 00012 EU 2002 6 21 UPS02138557 1 20020606 A 2150 A/C PACK AIRBUS A300 A300F4622R 3930360 EU A/C BAY MALFUNCTIONED A IPXA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 133UP 0817 INSPECTION TYPE:N/A DISCREPANCY IN CRUISE AT FL270 BOTH PACKS FAULTED OFF. ECAM PROCEDURES COMPLIED WITH AND EMERGENCY DESCENT INITIATED. PACKS WOULD NOT RESET. AT FL180 PACKS CAME BACK ON. PERFORMED BITE CHECK ON CABIN PRESSURE 10-2 BO X, PNEUMATIC PRESSURE CONTROLLER 102, NO FAULTS NO ECAM MESSAGES EITHER. OPS CK'D PACK 1 & 2, NO DEFECTS NOTED. PACKS OPEN, NORMAL. A/C OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2002062100014 20020621 00014 EU 2002 6 21 YENA200214 1 20020621 A 3350 2514355 LENS AIRBUS 320 A320232 3930326 EU MISSING A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 510JB 7387 1280 Emergency Light Lens cover borken at seat 16ABC. Replaced Lens cover Ops Test Emergency lightsystem. OK 2 L 7 2 4F RT A28NM 2002062100015 20020621 00015 WP 2002 6 21 COOSDR02159 1 20020601 A 5753 5930495506J SKIN DOUG DC9 DC983 3022083 WP RT WING TE FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 131NJ 49846 RIGHT WING, INBOARD FLAP, OUTBOARD VANE FLAP (PN 5930495)(SN 2706) DELAMINATED. 2 L 7 2 4F RT A6WE 2002062100016 20020621 00016 WP 2002 6 21 COOSDR02160 1 20020601 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 131NJ 49846 FORWARD LOWER CARGO COMPARTMENT DOOR, LOWER FORWARD CUT OUT OUTER SKIN CRACKED. 2 L 7 2 4F RT A6WE 2002062100018 20020621 00018 NM 2002 6 21 HALA0200111 1 20020519 A 4920 APU BOEING 767 76733A 1385209 NM APU BAY FAILED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM: APU FAILED TO START IN AIR. OAT-52, FL 360. APU EGT REACHED 594 DEGREES AND ONLY 8 RPM. TH EN ADD OIL LIGHT AND APU FAULT. VISUALLY CHECKED APU OIL QUANITY. OIL LEVEL WAS FULL, NO OIL ADDED. PERFORMED BITE CH ECK OF APU ECU PER 767 FIM 40-11-00. BITE CHECK OK. RAN APU, START NORMAL. NO LEAKS NOTED, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2002062100019 20020621 00019 EU 2002 6 21 KBMA113832 1 20020518 A 2197 DSQ201 SWITCH SNIAS 350 AS350BA 8680817 EU GENERATOR STUCK A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 1188P 11287 2347 GENERATOR SWITCH STICKS. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2002062100020 20020621 00020 NM 2002 6 21 UPS02238112 1 20020418 A 5330 DOUBLER BOEING 727 727180C 138406G NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C SUSPECT CORROSION BETWEEN FUSELAGE SKIN AND TOILET SERVICE PAN UPPER FLANGE, AFT SERVICE PAN. AREA P AINT STRIPPED, SERVICE PAN DE-RIVETED AND REMOVED, SKIN PANEL DE-RIVETED BETWEEN STR 17L-23L BS 1183 - 1150. INTERNAL D OUBLER AROUND PAN FOUND CORRODED AND REMOVED. NEW STIFFENER AND DOUBLER FABRICATED. PARTS REINSTALLED IAW SRM 51-30-02 AND DWG 65-18386 AND 65-18385. 2 L 7 3 4F A3WE 2002062100021 20020621 00021 NM 2002 6 21 UPS02238290 1 20020504 A 5514 BEAM BOEING 727 72722C 138400F NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C CORROSION ON RT STAB T/E BEAM (UPPER) AT STAB STA 205 AND STA 209. CORROSION REMOVED IAW SRM 51-10-06 & FOUND TO BE OUTSIDE LIMITS AFTER CORROSION REMOVAL HFEC CARRIED OUT IAW B727 NDT MANUAL PART 6, 51-00-00 - NDF. ARE A ON RT STAB T/E BEAM REPAIRED IAW SMRO EO 2002- 027-007 UPS ENGINEERING FILE 727-55-20006. 2 L 7 3 4F A3WE 2002062100022 20020621 00022 NM 2002 6 21 UPS02238291 1 20020504 A 5514 BEAM BOEING 727 72722C 138400F NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C CORROSION ON LT STAB T/E UPPER BEAM AT STAB STA 215. CORROSION REMOVED IAW SRM 51-10-06 FOUND TO BE O UTSIDE LIMITS HFEC C/O IAW B727 NDTM PT 6 51-00-00 - NDF. REPAIRED BEAM IAW EO 2002-027-006. 2 L 7 3 4F A3WE 2002062100023 20020621 00023 NM 2002 6 21 UPS02238292 1 20020504 A 5514 BEAM BOEING 727 72722C 138400F NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, CORROSION ON LT STAB T/E UPPER BEAM AT STAB STA 155. CORROSION REMOVED IAW SRM 51-10-06 FOUND TO BE OUTSIDE LIMITS HFEC C/O IAW B727 NDTM PT 6 51-00-00 - NDF. REPAIR CARRIED OUT IAW SMRO EO 2002-027-008 UPS ENGINEERING FILE 727-55-20006. 2 L 7 3 4F A3WE 2002062100024 20020621 00024 EU 2002 6 21 KBMA113835 1 20020516 A 6410 355A12004008 SPAR SNIAS 350 AS350BA 8680817 EU T/R BLADE CRACKED A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 2276 2300 TAIL ROTOR BLADE SPAR IS CRACKED. REPLACED WITH SERVICEABLE TAIL ROTOR BLADE. 1 G 7 1 3U NC H9EU 2002062100025 20020621 00025 NM 2002 6 21 UPS02238312 1 20020424 A 3211 TRUNNION BOEING 727 72722C 138400F NM RT MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C SUSPECT CRACK RT MLG FWD TRUNNION FITTING AT I/B SUPPORT LEG O/B FLANGE FITTING. RT MLG FWD TRUNNION FITTING REPLACED IAW SMRO EO 2002-027-001R1 UPS ENGINEERING FILE 727-51-20054. 2 L 7 3 4F A3WE 2002062100026 20020621 00026 NM 2002 6 21 UPS02238314 1 20020508 A 2782 BRACKET BOEING 727 72722C 138400F NM L/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, SUSPECT CRACKS ON NR 6 L/E FLAP ACTUATOR I/B & O/B ATTACH BRACKETS LWR FWD CORNERS. ATTACH BRACKETS FABRICATED IAW SRM 51-20-1 FIG 7, HEAT TREATMENT REF HT 02-27-03. BRACKETS INSTALLED IAW SRM 51-30-2 & DRAWING 65-16275 . 2 L 7 3 4F A3WE 2002062100027 20020621 00027 NM 2002 6 21 UPS02238315 1 20020502 A 5320 TIE BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C LWR BEAM TIE IN E&E BAY IS CRACKED BS 312 RBL 45. TYPICAL REPAIR CARRIED OUT IAW SRM 51-40-04. 2 L 7 3 4F A3WE 2002062100028 20020621 00028 SO 2002 6 21 CDM2002F00000 2 20020611 A 8550 9696001111 LINE BEECH 55 D55 1152730 CE CONT O520 IO520* 17032 SO OIL ACCUMULATOR BROKEN D CDMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 17 7952R TE706 PILOT DECLARED AN EMERGENCY. NOTICED OIL STREAMING FROM RIGHT ENGINE. MADE A SAFE LANDING. THE MECHANIC DISCOVERED TH E HARD-LINE FROM THE PROPELLER UNFEATHERING ACCUMULATOR HAD BROKEN AT THE FLARED END WHICH ATTACHED TO THE PROPELLER GOV ERNOR. THE SINGLE FLARE HAD SIGNS OF BEING LOCALLY FABRICATED AND OR DISTORTED AND NOT PROPERLY FORMED. PILOT REPO RTED EXCESSIVE OIL LEAK ON RIGHT ENGINE. REMOVED RIGHT UPPER COWL, SIDE COWLS, AND FORWARD LOWER NOSE COWL. PROPELLER UNFEATHERING HARDLINE (PN 96960011-11) BROKEN AT FLARE. REMOVED LINE AND CAPPED FITTING. TOPPED OIL ON RIGHT ENGINE, O NE QUART. REPLACED OIL FILTER. PLACARD INSTALLED. RIGHT HAND UNFEATHERING OPTION DISABLED END. 1 L 7 2 3O 3 O 3A16 E5CE 2002062100029 20020621 00029 NM 2002 6 21 UPS02238316 1 20020502 A 5320 TIE BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C LWR BEAM TIE CRACKED IN E & E BAY BS 328 RBL 25. TYPICAL REPAIR CARRIED OUT IAW SRM 51-40-4. 2 L 7 3 4F A3WE 2002062100030 20020621 00030 NM 2002 6 21 UPS02238318 1 20020506 A 5712 RIB BOEING 727 72722C 138400F NM WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, 3 SUPPORT RIBS CRACKED ON T/E PANEL BELOW NR 8 SPOILERS. RIBS REPLACED IAW SRM 51-30-2 & DRG 65-2165 6. 2 L 7 3 4F A3WE 2002062100031 20020621 00031 NM 2002 6 21 UPS02238494 1 20020529 A 3350 1000677 LIGHT BOEING 727 72725C 138400H NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:PFLT COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY AND CLEA NED CONNECTOR TO LIGHT ASSY MOUNTING PLATE, OPS CHECK GOOD PER MM 33-50-67. 2 L 7 3 4F A3WE 2002062100032 20020621 00032 NM 2002 6 21 UPS02238515 1 20020603 A 3350 BATTERY BOEING 727 7271A7C 13840X2 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP-L1 DOOR. REMOVED AND REPLACED BATTERY. 2 L 7 3 4F A3WE 2002062100033 20020621 00033 NE 2002 6 21 GW12002F00000 2 20020605 A 7300 3027791 LINE BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE AIR PRESSURE FRACTURED B GW1R A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 EA 03 992TJ 7519 BB992 PCE93313 PILOT EXPERIENCED LEFT ENGINE ROLL BACK TO IDLE, ENROUTE. INVESTIGATION REVEALED FRACTURED P3 AIR DELIVERY TUBE (PN 302 7791) AT THE TUBE/FERRULE JOINT (B) NUT ON THE FUEL CONTROL UNIT. THE P3 TUBE WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERIVCE. 1 L 7 2 4T 4 T A24CE E4EA 2002062100034 20020621 00034 NM 2002 6 21 UPS02238547 1 20020527 A 5330 SKIN BOEING 727 72731C 1384011 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, SURFACE CORROSION ON FUSELAGE SKIN INTERNAL AT BS 254.5 BETWEEN STR 5L & 6L. REPAIR CARRIED OUT IAW DRAWING 692161 & UPS EO B727-5310-1371 APPENDIX E. 2 L 7 3 4F A3WE 2002062100035 20020621 00035 CE 2002 6 21 HMN2002F00000 1 20020530 A 7603 311AS3146780 CONTROL CABLE MTSBSI MU2 MU2B35 5780411 CE POWER LEVER BROKEN B HMNR O OTHER O OTHER TX TAXI/GRND HDL 1 SW 15 450MA 10292 587 ON ENGINE SHUTDOWN, PILOT COULD NOT BRING LEFT PROP BACK ON LOCKS. INSPECTION FOUND LEFT ENGINE POWER LEVER CONTROL CAB LE BROKEN BELOW CENTER PEDISTAL IN COCKPIT AT LOWER PULLEY. (SW15200209701) 1 H 7 2 3T RT A10SW 2002062100036 20020621 00036 NM 2002 6 21 UPS02238549 1 20020528 A 5315 FLOORBEAM BOEING 727 72731C 1384011 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, CORROSION ON CHORD AT FLOOR LEVEL AT BS 1177 RT O/B. CHORD REPLACED IAW SRM 51-30-02 AND DRAWING 65- 19606. 2 L 7 3 4F A3WE 2002062100037 20020621 00037 NM 2002 6 21 UPS02238558 1 20020606 A 3350 BATTERY BOEING 727 7271A7C 13840X2 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES WITH NEW BATTERIES. 2 L 7 3 4F A3WE 2002062100038 20020621 00038 CE 2002 6 21 HMN2002F00001 1 20020530 A 7603 311AS3146780 CONTROL CABLE MTSBSI MU2 MU2B35 5780411 CE THROTTLE FRAYED B HMNR K NONE O OTHER IN INSP/MAINT 1 SW 15 640MA 8934 590 FRAYED CABLE FOUND DURING ROUTINE 100 HOUR INSPECTION. FRAYED PORTION IN AFT FUSELAGE ON A 90 DEGREE TURN PULLEY. FOUND AND REPLACED. (SW15200209702) 1 H 7 2 3T RT A10SW 2002062100039 20020621 00039 NM 2002 6 21 UPS02238567 1 20020607 A 3350 BATTERY BOEING 727 72725C 138400H NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT IN COCKPIT INOP. REMOVED AND REPLACED BATTERY, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2002062100040 20020621 00040 CE 2002 6 21 JEM2002F00001 1 20020524 A 2910 1015800241 LINE BEECH 200 B200 1152922 CE HYD SYSTEM CHAFED B JEMA K NONE K FLUID LOSS IN INSP/MAINT 1 CE 01 362EA BB1396 THIS LINE ASSEMBLY WAS CHAFING AGAINST AN ENGINE POWER CONTROL CABLE LOCATED BEHIND THE REMOVEABLE LEFT HAND INBOARD LEA DING EDGE PANEL. VIBRATION CAUSED THE OUTER SHEATH OF THE CONTROL CABLE TO CHAFE DEEP SERRATIONS INTO THIS LANDING GEAR HYDRAULIC LINE. IT IS RECOMMENDED THE LEADING EDGE BE COMPLETELY REMOVED AT INSPECTIONS TO FACILITATE A MORE THROUGH I NSPECTION OF THIS AREA. 1 L 7 2 4T A24CE 2002062100042 20020621 00042 NM 2002 6 21 UPS02238629 1 20020613 A 3350 BATTERY BOEING 727 72751C 1384015 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE:PFLT CABIN DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES BOTH EMERGENCY LIGHTS, OPS CH ECK NORMAL. 2 L 7 3 4F A3WE 2002062100043 20020621 00043 GL 2002 6 21 KBMA113836 2 20020514 A 7532 23053176 BLEED VALVE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE INOPERATIVE A KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 188TV 10115 2704 (BLEED VALVE) ENGINE POWER CHECK INDICATES ENGINE BELOW MINIMUM PERFORMANCE SUSPECTS FAULTY BLEED VALVE. REPLACED WITH SERVICEABLE BLEED VALVE. 1 G 7 1 3U 3 U H2SW E4CE 2002062100044 20020621 00044 NM 2002 6 21 UPS02238641 1 20020617 A 3350 BATTERY BOEING 727 72730C 1384009 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:PFLT FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM 33-50-01. 2 L 7 3 4F A3WE 2002062100045 20020621 00045 EU 2002 6 21 KBMA113837 1 20020515 A 7810 029280874 CLAMP SNIAS 350 AS350BA 8680817 EU EXHAUST BROKEN A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 2337 (STRAP) HEAT SHIELD STRAP IS BROKEN. REPLACED WITH SERVICEABLE PARTS. 1 G 7 1 3U NC H9EU 2002062100046 20020621 00046 NE 2002 6 21 UPS02438114 2 20020502 A 7200 ENGINE BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE NR 1 LEAKING A IPXA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 521UP 21944 INSPECTION TYPE:N/A FSA ITEM H22303 SMOKE IN COCKPIT. REMOVED AND REPLACED NR 1 ENGINE AS PER UPS TC5000 AND WAN 678705 . 2 L 7 4 4F 4 F RT A20WE E3NE 2002062100047 20020621 00047 EU 2002 6 21 KBMA113841 1 20020529 A 6730 AC67244 SERVO SNIAS 350 AS350BA 8680817 EU CYCLIC INOPERATIVE A KBMA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 19 1188P 1727 2347 CYCLIC PULLS TO THE LEFT. REPLACED WITH SERVICEABLE SERVO. 1 G 7 1 3U NC H9EU 2002062100048 20020621 00048 NM 2002 6 21 UPS02438115 1 20020502 A 3350 CONTROL PANEL BOEING 747 747123F NM CABIN FAULTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL PANEL IAW B747-33-51-09. 2 L 7 4 4F A20WE 2002062100049 20020621 00049 EU 2002 6 21 KBMA113842 1 20020520 A 2612 FIRE DETECTOR SNIAS 350 AS350BA 8680817 EU ENGINE CONTAMINATED A KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 2273A 2273 FIRE LIGHT STAYS ON/ FIRE DETECTOR SOAKED WITH OIL . DEGREASED FIRE DETECTOR. 1 G 7 1 3U NC H9EU 2002062100050 20020621 00050 NM 2002 6 21 UPS02438119 1 20020506 A 3350 LIGHT BOEING 747 747123 1384873 NM COCKPIT MISSING A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:N/A EMERGENCY LIGHT INOP RT SIDE OF MAIN DECK AFT OF LADDER. FOUND MISSING LIGHT ASSY. INSTALLED LIGHT B747 MM 33-51-00, OPS CHECK GOOD. 2 L 7 4 4F A20WE 2002062100051 20020621 00051 EU 2002 6 21 KBMA113843 1 20020520 A 5210 TAB SNIAS 350 AS350B2 8680813 EU DOOR MISSING A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 345SH 3345 METAL TAB ON POCKET DOOR MISSING. REMOVED POCKET DOOR FOR REPAIR/ REPLACED WITH SAME PART NUMBER. 1 G 7 1 3U H9EU 2002062100052 20020621 00052 CE 2002 6 21 KC82002F00001 1 20020530 A 2120 X11984 FILTER LEAR 25 25D 5170514 CE CABIN PRESSURE DIRTY E KC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 95CK 248 CABIN WOULD NOT PRESSURIZE. CLEANED PRESSURIZATION JET PUMP FILTER. PERFORMED GROUND PRESSURIZATION CHECK PER MFG MM. AIRCRAF TEST FLOWN AND FOUND SATISFACTORY. 2 L 7 2 4J A10CE 2002062100053 20020621 00053 NM 2002 6 21 UPS02438120 1 20020506 A 3397 GROUND WIRE BOEING 747 747123 1384873 NM CABIN LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY WEAK AT LIGHT ABOVE UPPER DECK EMERGENCY DOORWAY AREA. FOUND BAD GROUND AT EXIT SIGN ABOVE UPPER DECK EMERGENCY DOORWAY. RESECURED GROUND. OPS CHECK GOOD IAW B747 MM 33-51-00. 2 L 7 4 4F A20WE 2002062100054 20020621 00054 NM 2002 6 21 UPS02438147 1 20020422 A 5310 STOP FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - L3 DOOR FWD CUTOUT NR 6 STOP FITTING FOUND CRACKED. L3 DOOR FWD CUTOUT NR 6 STOP FITTING REPLAC ED AS PER SRM 51-10-01 PAGE 8. 2 L 7 4 4F A20WE 2002062100055 20020621 00055 NM 2002 6 21 KPV2002F00000 1 20020503 A 2750 DRIVE UNIT DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE FLAP DRIVE UNIT SLOW A KPVA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 13 808WP 026 NR 2 ADI PITCH/ROLL MISMATCH, AHRS DATA INVALID, YAW DAMPNER FAILED ON BOTH CHANNELS. FLAPS VERY SLOW MOVING AND STUCK AT 10 PERCENT. FLAPS WOULD NOT RETRACT ABOVE 5 DEGREE. DECLARED EMERGENCY AND RETURNED TO AIRPORT. LANDED WITHOUT INC IDENT. CORRECTIVE ACTION: 1) PERFORMED GMT TEST FOR BOTH NR 1 AND NR 2 AHS SYSTEM. TESTED GOOD - 2) PERFORMED GMT TES T FOR YAW DAMPNER SYS.(BOTH L & R CHANNELS). TESTED GOOD. 3) BLED NR 1 MAIN HYDRAULIC SYSTEM AND FPU. (B) FUNCTIONAL T EST OF WING FLAP SYSTEM GOOD. NO DEFECTS NOTED. NOTE: FLAPS SLOW TO MOVE, REMOVED AND REPLACED THE FLAP POWER DRIVE U NIT. ((TRACKING NUMBER KPVA 2002-9)) 2 H 7 2 4T 4 T RT A13NM E20NE 2002062100056 20020621 00056 NM 2002 6 21 UPS02438148 1 20020421 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C U/D - BS 620 S-6R STRINGER CRACK. BS 610 - BS 630 STR 6R SEGMENT REPAIRED AS PER SRM 53-10-03 FIG 4 A ND AREA FINISHED PAINT TOUCH UP PER MM 51-42-11. 2 L 7 4 4F A20WE 2002062100057 20020621 00057 NM 2002 6 21 UPS02438149 1 20020419 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D- FRAME FOUND CRACK AT STA 560 S24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2 L 7 4 4F A20WE 2002062100058 20020621 00058 CE 2002 6 21 L4Y2002F00001 1 20020509 A 3240 09108000 PIN CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO RT BRAKE ASSY BROKEN A L4YA K NONE O OTHER IN INSP/MAINT 1 SW 19 11NX 402C0480 UPON LANDING, RIGHT BRAKE ASSEMBLY, LOWER ANCHOR BOLT (TORQUE PIN) BROKE OFF, RENDERING BRAKE INOPERATIVE AND CAUSING D AMAGE TO TIME AND WHEEL. 1 L 7 2 3O 3 O A7CE E8CE 2002062100059 20020621 00059 NM 2002 6 21 UPS02438150 1 20020419 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - FRAME FOUND CRACK AT STA 580 S24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2 L 7 4 4F A20WE 2002062100060 20020621 00060 CE 2002 6 21 L4Y2002F00002 1 20020509 A 3243 0820577 SPRING CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO MASTER CYLINDER BROKEN A L4YA K NONE O OTHER IN INSP/MAINT 1 SW 19 67887 402C0436 BRAKE MASTER CYLINDER INTERNAL SPRING BROKEN. MASTER CYLINDER INOPERATIVE. 1 L 7 2 3O 3 O A7CE E8CE 2002062100061 20020621 00061 NM 2002 6 21 UPS02438151 1 20020417 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO - BS 920 - 940 STR 29R FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062100062 20020621 00062 SO 2002 6 21 MAS2002F00000 1 20020404 A 2910 DSC2524B40124 LINE PIPER PA32 PA32260 7103206 SO LYC O540 O540* 41532 EA HYD SYSTEM FAILED A MASA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 07 448MJ 32772 DURING FLIGHT EXPERIENCED A NR 2 HYDRAULIC SYSTEM FAILURE IN-FLIGHT. AFTER AN UNEVENTFUL LANDING, MECHANIC WAS CALLED. MECHANIC DISCOVERED THAT THE HYDRAULIC FLEX LINE RUPTURED TO THE SPU PRESSURE SWITCH. MECHANIC REMOVED AND REPLACED TH E FLEX LINE. OPS CHECK GOOD. (M02050) 1 L 7 1 3O 3 O A3SO E295 2002062100063 20020621 00063 WP 2002 6 21 GTIA020433 1 20020414 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND CABIN FLOOR SUPPORT FS 1287-1307 TOP FLANGE CRACKED AT -X0. REMOVED CABIN FLOOR SUPPORT. FABRICATED CABIN FLOOR SUPPORT FS 1287-1307. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062100064 20020621 00064 WP 2002 6 21 GTIA020434 1 20020411 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND RIGHT OUTBOARD SEAT TRACK -X44 FS 983 HAS CORROSION AND GOUGES. REMOVED CORROSION. CUT DAMAGED SECTION OF TRACK. DRILLED AND COUNTERSANK HOLES IN NEW SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2002062100065 20020621 00065 WP 2002 6 21 GTIA020435 1 20020411 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND RIGHT OUTBOARD SEAT TRACK -X44 FS 560 TO FS 582 HAS CORROSION, GOUGES, AND SCRATCHES. AREA FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2002062100066 20020621 00066 NE 2002 6 21 MYW2002F00000 2 20020513 A 7200 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE NR 2 MAKING METAL A MYWA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SO 19 803MA 22434 PRIOR TO DESCENT NR 2 ENGINE LOW OIL PRESS/FILTER BYPASS LIGHT ILLUMINATED. ENG NR2 PARAMETERS INDICATION ARE NORMAL OI L PRESS 47 PSI, OIL TEMP 81 DEGREE C, EPR NR 2-165, N1-80.9, EGT-400 DEG. C, N2-85.9, FF-3000PPH, CSD IN TEMP 50 DEG. C, RISE -8 DEG. C. GEN VOLTS-115, FREQ-400HZ. ACCOMPLISHED PROCEDURES LOW OIL PRESS/FILTER BYPASS LIGHT ILLUM CHECK LIST PAGE 2A.19.9. RESTARTED NR 2 ENGINE, THROTTLE TO IDLE AS PER CHECK LIST NO HELP. LIGHT REMAINED ILLUMINATED. LANDED, FOUND METAL IN MAIN OIL FILTER. FLUSHED SYST AND INSTALLED NEW FILTER. RAN ENGINE STILL HAD METAL SHAVINGS. REMOVED AND REPLACED NR 2 ENGINE. OPS CHECKED FOUND NO FAULTS. RETURNED A/C TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002062100067 20020621 00067 EU 2002 6 21 OIO2002F00000 1 20020506 A 2435 410965 BEARING AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE7312B WP STARTER GEN FAILED A OIOR K NONE L NO TEST IN INSP/MAINT 1 GL 03 148M 504 270 THE SUBJECT START-GEN WAS TEMPORARILY REMOVED FROM SERVICE FOR A PRECAUTIONARY BEARING INSPECTION. TSO WAS 504 HOURS. NEW BEARINGS FROM AN AUXILEC APPROVED DISTRIBUTOR WERE INSTALLED DURING OVERHAUL. INSPECTION OF THE SUBJECT BEARING FO UND IT COULD NOT BE ROTATED BY HAND. THE INNER RACE WAS OVERHEATED AS INDICATED BY A BLUE COLOR. THE OUTER RACE APPEAR ED TO BE A NORMAL COLOR. THE ARMATURE SHAFT SHOWED NO SIGNS OF THE RACE SPINNING. THE COLOR OF THE BEARING RETAINERS A LSO INDICATED OVERHEATING. A NEW BEARING WAS INSTALLED AND PART WAS OVERHAULED PRIOR TO IT BEING RETURNED TO SERVICE. BEARING WAS MFG WITH TOO LITTLE OR NO RADICAL CLEARENCE, AND THIS LEAD TO OVERHEATING AND IMMINENT FAILURE OF BEARING. 2 L 7 3 4F 4 F A46EU E6WE 2002062100068 20020621 00068 EU 2002 6 21 OIO2002F00001 1 20020506 A 2435 410965 BEARING AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP STARTER GEN ROUGH A OIOR K NONE O OTHER IN INSP/MAINT 1 GL 03 158M 140 273 THE SUBJECT STARTER-GEN WAS TEMPORARILY REMOVED FROM SERVICE FOR A PRECAUTIONARY BEARING INSPECTION. TSO OF STARTER-GE N WAS 140. NEW BEARINGS FROM AN AUXILEC APPROVED DISTRIBUTOR WERE INSTALLED DURING THE OVERHAUL. INSPECTION OF THE SUB JECT BEARING, FOUND IT ROUGH WHEN ROTATED BY HAND. A NEW BEARING WAS INSTALLED AND THE STARTER-GEN WAS RETURNED TO SERV ICE. 2 L 7 3 4F 4 F A46EU E6WE 2002062100069 20020621 00069 EU 2002 6 21 OIO2002F00002 1 20020416 A 2435 410965 BEARING AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE7312B WP STARTER GEN STIFF A OIOR K NONE O OTHER IN INSP/MAINT 1 GL 03 138M 252 274 STARTER-GEN WAS TEMPORARILY REMOVED FROM SERVICE FOR A PRECAUTIONARY BEARING INSPECTION. TSO OF STARTER-GEN WAS 252 HOU RS. NEW BEARINGS FROM MFG APPROVED DISTRIBUTOR WERE INSTALLED DURING OVERHAUL. INSPECTION OF SUBJECT BEARING FOUND IT STIFF TO ROTATE AND IT FELT VERY ROUGH WHEN ROTATED. SEALS WERE REMOVED AND GREASE (WHITE COLOR) APPEARED NORMAL. BEA RING WAS STILL STIFF AND ROUGH TO ROTATE. BEARING HAD NO RADIAL CLEARANCE, AND THE INNER RACE WAS OVERHEATING AS INDICA TED BY LOCALIZED DARK PURPLE TO LIGHT BLUE COLOR. THE ARMATURE SHAFT SHOWED NO SIGNS OF THE RACE SPINNING. THE COLOR O F THE BEARING RETAINERS ALSO INDICATED OVERHEATING. A NEW BEARING WAS INSTALLED AND THE PART WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A46EU E6WE 2002062100070 20020621 00070 NM 2002 6 21 OZR2002F00000 1 20020510 A 5730 SKIN BOEING 737 737* NM RT & LT WING CHAFED B OZRR K NONE O OTHER IN INSP/MAINT 1 SW 11 LVYYC 28210 DURING SCHEDULED INSPECTION, IT WAS DISCOVERED THAT THE WING LOWER SURFACE OF BOTH THE LEFT AND RIGHT WING SKIN WAS CHAF ED. THE CHAFING IS IN THE AREA OF ENGINE, AFT POSITION FAIRING LOCATED DIRECTLY AFT OF THE ENGINE. CHAFING HAS ALSO BE EN NOTED, ON THE LEFT AND RIGHT WING LOWER SURFACES AT EACH FLAP TRACK FAIRING. WITH EXCEPTION OF THE DAMAGE LOCATED AT THE FLAP TRACK FAIRING, ALL OF THE DAMAGE APPEARS TO BE CAUSED BY CONTACT BETWEEN THE WING LOWER SKIN AND THE BLADE SEA L, WHICH IS ATTACHED TO THE ENGINE AFT POSITION FAIRING. THE ANTICHAFE STRIPS BEING DISCUSSED IN MFG SB HAVE BECOME TYP E DESIGN INSTALLATION. 2 L 7 2 4F RT A16WE 2002062100071 20020621 00071 WP 2002 6 21 GTIA020436 1 20020410 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND LEFT FLOORBOARD BETWEEN INBOARD SEAT TRACK X22 AND OUTBOARD SEAT TRACK X44 AT STATION Y257 CORRODED. REMOVE D FLOORBOARD. FABRICATED A NEW PANEL. INSTALLED FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2002062100072 20020621 00072 WP 2002 6 21 GTIA020437 1 20020411 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND RIGHT INBOARD SEAT TRACK -X22 FS 673 TO FS 679 HAS CORROSION, GOUGES, AND SCRATCHES. AREA FOUND TO BE OUT O F LIMITS. REMOVED DAMAGED SECTION OF SEAT TRACK. DRILLED AND COUNTERSANK HOLES IN SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2002062100073 20020621 00073 WP 2002 6 21 GTIA020438 1 20020411 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FOUND RIGHT INBOARD SEAT TRACK -X22 FS 532 HAS CORROSION AND GOUGES. AFTER FURTHER EVALUATION CORROSION WAS FOUND AT FS 549 RIGHT INBOARD S/T -X22. REMOVED DAMAGED SECTION OF SEAT TRACK. FABRICATED SEAT TRACK FROM STATION 532-627 DRILLED AND LOCATED. INSTALL NEW SEAT TRACK AT STATION 532-627 -X22. (M) 2 L 7 2 4F A6WE 2002062100074 20020621 00074 WP 2002 6 21 GTIA020439 1 20020411 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND LEFT OUTBOARD SEAT TRACK X44 FS 1222 TO FS 1305 HAS CORROSION. REMOVED CORROSION. REMOVED SEAT TRACK FROM STATION 1222-1305. LOCATE AND DRILLED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2002062100075 20020621 00075 WP 2002 6 21 GTIA020440 1 20020411 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND RIGHT OUTBOARD TRACK -X44 FS 261 HAS GOUGES. REMOVED CORROSION. REMOVED SEAT TRACK AT -X44 FROM STATION 24 8-275. INSTALLED SEAT TRACK AT -X44 STATION 248-275. (M) 2 L 7 2 4F A6WE 2002062100076 20020621 00076 NM 2002 6 21 QXEA0200899 1 20020618 A 2150 S2L230 SEAL DHAV DHC8 DHC8202 2809007 NM ZONE 100 BLOWN A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 369PH 513 PDX-BLEED FLOW LOW, UNABLE TO COOL DUCT TEMP BELOW 20 DEGREES IN AUTO OR MANUAL ASSOCIATED SOUR SMELL FROM UNITS DURING OPERATIONS. REMOVED AND REPLACED BLOW OUT SEALS IN ECS BAY UPPER DUCTING. LEAK CHECK GOOD. GROUND RAN AND OPERATIONAL CH ECK OF ACM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002062100077 20020621 00077 EA 2002 6 21 COMA0260378 1 20020619 A 5311 6013000130 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FS 460.00 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 924CA 20401 7026 FS 640.00 FRAME HAS DOUBLER CRACKED ON R/H SIDE AT W.L. 120REMOVED CRACKED DOUBLER AT F.S. 640.00 FRAME ON R/H SIDE AND INSTALLED NEW DOUBLER I/A/W CRJ SRM 51-42-06 AND 51-42-21. 2 L 7 2 4F RT A21EA 2002062100078 20020621 00078 EA 2002 6 21 COMA0260379 1 20020619 A 5311 601R53615003 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FS 460.00 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 924CA 20401 7026 THE SKIN DOUBLER AT F.S. 640.00 W.L. 120 ON R/H SIDE IS CRACKED.REMOVED CRACKED SECTION OF INTERNAL SKIN DOUBLER, INSTAL LED FABRICATED INTERNAL REPAIR DOUBLERS, 2 EA EXTERNAL REPAIR DOUBLERS AND BEAM ANGLES I/A/W BOMBARDIER R.E.O. 601R-53-6 1-535 AND WVAC EO 601R-53-4019A. 2 L 7 2 4F RT A21EA 2002062100079 20020621 00079 EA 2002 6 21 COMA0260380 1 20020619 A 5311 6013600123 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 460.00 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 924CA 20401 7026 FS 640.00 FRAME ON R/H SIDE IS CRACKED.REMOVED CRACKED SECTION OF FRAME AT F.S. 640.00 ON R/H SIDE AND INSTALLED NEW SEC TION OF FRAME I/A/W BOMBARDIER REO 601R-53-61-487. SUBSTITUTED FASTENERS ON STRINGER CLIP I/A/W WVAC EO 601R-53-4024 2 L 7 2 4F RT A21EA 2002062100080 20020621 00080 NE 2002 6 21 COMA0260381 2 20020618 A 7261 6087T04P05 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT ENG LEAKING A COMA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 916CA 11902 7014 FLIGHT 5322 IFSD LEFT ENGINE DUE TO LOW OIL PRESSURE.REPLACED THE LUBE SCAVANGE OIL PUMP. 2 L 7 2 4F 4 F RT A21EA E15NE 2002062100081 20020621 00081 WP 2002 6 21 GTIA020442 1 20020405 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND STATION 864 L18L, OVERWING-WING TO BODY FAIRING ATTACH BRACKET IS BROKEN. REMOVED BROKEN ATTACH BRACKET. F ABRICATED ATTACH BRACKET. INSTALLED ATTACH BRACKET. (M) 2 L 7 2 4F A6WE 2002062100082 20020621 00082 WP 2002 6 21 GTIA020443 1 20020425 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND AFT CARGO TRACK RIGHT FORWARD 'Z' ANGLE GOUGED AND TRACK HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS . FABRICATED TRACK. INSTALLED CARGO TRACK. (M) 2 L 7 2 4F A6WE 2002062100083 20020621 00083 WP 2002 6 21 GTIA020444 1 20020425 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND AFT CARGO CORNER THRESHOLD SUPPORT STATION 1155 HAS CORROSION AROUND AND UNDER NUT PLATES. REMOVED CORROSIO N. FABRICATED THRESHOLD SUPPORT. INSTALLED NEW THRESHOLD SUPPORT. (M) 2 L 7 2 4F A6WE 2002062100084 20020621 00084 NE 2002 6 21 P9R2002F00001 2 20020404 A 7200 ENGINE BOEING 727 727231 1384079 NM PWA JT8 JT8D9A 52048 NE NR 1 CONTAMINATED A P9RA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 54344 21631 ON TAXI OUT IN CABIN AND COCKPIT FILLED WITH SMOKE. RETURNED TO GATE. REMOVED AND REPLACED NR 1 ENGINE SYSTEM A CHECK V ALVE. CLEANED RESIDUAL FLUID OUT OF LINE FROM NR 1 ENGINE CHECK VALVE FOR SYSTEM A HEAD PRESSURE. REMOVED AND REPLACED WATER SEPARATOR BAGS, RAN ENGINES AT POWER FOR SEVERAL MINUTES WITH PACKS ON AND OFF. OPS CHECK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2002062100085 20020621 00085 WP 2002 6 21 GTIA020445 1 20020418 A 5321 STIFFENER DOUG DC9 DC982 3022082 WP FLOORBOARD CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND CABIN FLOORBOARD STATION 1155-1250 X46 TO X56 STIFFENER CHANNEL CRACKING, REPAIR DEBONDING, PHENOLIC BACKSTR IPS BROKEN AND FASTENER HOLE ENLARGED. REPAIRED CABIN FLOOR PANEL STATION 1155-1250. (M) 2 L 7 2 4F A6WE 2002062100086 20020621 00086 NM 2002 6 21 P9R2002F00002 1 20020319 A 3350 08202120 LIGHT BOEING 727 727200 138407E NM CABIN LOOSE A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 906PG 20728 (TRACK, BASE, EPL) EMERGENCY EXIT ILLUMINATION STRIP ON RT SIDE OF AIRCRAFT AT ROW 6 CAME LOOSE. REATTACHED EMERGENCY ILLUMINATION STRIP ON RIGHT SIDE AT ROW 6. 2 L 7 3 4F RT A3WE 2002062100087 20020621 00087 WP 2002 6 21 GTIA020468 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT FS 160 TO 200, -X7. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062100088 20020621 00088 WP 2002 6 21 GTIA020469 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 160 X13. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTA LLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062100089 20020621 00089 2002 6 21 QQG2002F00000 4 20020523 A 3100 VALVE LKHEED 1329 1329 5263102 SO PWA JT12 JT12A6A 52042 NE ANTI-ICE SYS INOPERATIVE A QQGR K NONE O OTHER IN INSP/MAINT 1 SW 09 1BL 62 5097 ANTI-ICE VALVE FAILED AFTER 62.9 HOURS, AFTER OVERHAUL. VALVE STUCK IN THE CLOSED POSITION. SINCE THERE WAS NO REPLACE MENT VALVES AVAILABLE, AND ATTEMPT WAS MADE TO FREE THE VALVE UP TO MAKE A FLIGHT WHICH DID NOT WORK, FLIGHT WAS CANCELE D UNTIL A REPLACEMENT VALVE WAS SUPPLIED. IT IS THIS REPAIR STATIONS FINDING THAT THESE VALVES ARE NOT BEING PROPERLY T ESTED AFTER OVERHAUL. 2 L 7 4 4J 4 J 2A15 1E9 2002062100090 20020621 00090 WP 2002 6 21 GTIA020470 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 200 X9 TO X13. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPO RT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062100092 20020621 00092 WP 2002 6 21 GTIA020471 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 200 X5 TO X-5. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUP PORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062100094 20020621 00094 WP 2002 6 21 GTIA020409 1 20020417 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - E/E BAY LONGERON 29L IS CORRODED FROM STATION 200-218. REMOVED CORROSION. LONGERON WAS REMOVED. INSTALLED LONGE RON. (M) 2 L 7 2 4F A6WE 2002062100095 20020621 00095 WP 2002 6 21 GTIA020410 1 20020417 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - E/E BAY LONGERON 28L HAS CORROSION FROM STATION 190-210. REMOVED DAMAGED LONGERON. FABRICATED NEW PART. INSTALL ED LONGERON. (M) 2 L 7 2 4F A6WE 2002062100096 20020621 00096 WP 2002 6 21 GTIA020411 1 20020415 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND E/E COMPARTMENT LONGERON 25 LEFT STATION 160 HAS CORROSION. REMOVED CORROSION AT LONGERON. LOCATED AND DRI LLED LONGERON SECTION REPAIR AND SPLICE. INSTALLED LONGERON SECTION REPAIR AND SPLICE. (M) 2 L 7 2 4F A6WE 2002062100097 20020621 00097 WP 2002 6 21 GTIA020412 1 20020413 A 5320 SUPPORT FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND MID PIT CORRODED AT BRACKET SUPPORT FITTING CARGO. REMOVED CORROSION. REMOVED DAMAGED PART AND REPLACED WI TH NEW PART. (M) 2 L 7 2 4F A6WE 2002062100098 20020621 00098 WP 2002 6 21 GTIA020413 1 20020414 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND FORWARD PIT CORRODED AT RIGHT CARGO TRACK FROM STATION 370, STATION 351, STATION 313, STATION 294. REMOVED DAMAGED CARGO TRACK. FORMED CARGO TRACK. INSTALLED FORMED CARGO TRACK. (M) 2 L 7 2 4F A6WE 2002062100099 20020621 00099 WP 2002 6 21 GTIA020414 1 20020414 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND FORWARD PIT CORRODED AT LEFT CARGO TRACK STATION 351, STATION 370, STATION 389, STATION 408, STATION 427, ST ATION 446, STATION 484 AND STATION 503. REMOVED CORROSION AT LEFT CARGO TRACK STATION 351-503. REMOVED DAMAGED CARGO T RACK FROM STATION 351-503. FABRICATED NEW TRACK. FABRICATED SPLICE TRACK REPAIR. INSTALLED SPLICE CARGO TRACK. INSTA LLED CARGO TRACK. (M) 2 L 7 2 4F A6WE 2002062100100 20020621 00100 WP 2002 6 21 GTIA020415 1 20020414 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND FORWARD PIT CORRODED/ELONGATED HOLES AT FORWARD ZEE ANGLE STATION 370. REMOVED DAMAGED ZEE ANGLE. FABRICAT ED NEW ZEE ANGLE. INSTALLED ZEE ANGLE. (M) 2 L 7 2 4F A6WE 2002062100101 20020621 00101 WP 2002 6 21 GTIA020416 1 20020414 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND AFT PIT STATION 1007-1220, LEFT CARGO TRACK HAS AREAS OF CORROSION/BARE METAL ALONG ENTIRE LENGTH OF TRACK. FROM STATION 1089-1220 FOUND OUT OF LIMITS. REMOVED CARGO TRACK AND SPLICE FROM STATION 1089-1220. DRILLED UP AND COU NTERSANK NEW TRACK. INSTALLED CARGO TRACK AND SPLICES. (M) 2 L 7 2 4F A6WE 2002062100102 20020621 00102 WP 2002 6 21 GTIA020417 1 20020414 A 5320 STRAP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND AFT PIT STATION 1060 L29R-L29L, CORRODED FRAME TO LONGERON FASTENERS. REMOVED CORROSION. LOCATED AND DRILL ED NEW STRAPS. INSTALLED STRAPS. (M) 2 L 7 2 4F A6WE 2002062100103 20020621 00103 WP 2002 6 21 GTIA020418 1 20020414 A 5320 STRAP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND AFT PIT STATION 1193 L26L, FRAME SPLICE STRAP CORRODED. REMOVED CORROSION. REMOVED STRAP. FABRICATED REPL ACEMENT STRAP, INSTALLED. (M) 2 L 7 2 4F A6WE 2002062100104 20020621 00104 WP 2002 6 21 GTIA020419 1 20020414 A 2550 PANEL DOUG DC9 DC982 3022082 WP CARGO BAY CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - MID CARGO FORWARD DOOR JAMB CLOSE OUT PANEL CRACKED AND LIGHT CORROSION ON BACK. STOP DRILL CRACK OF PANEL. FORM ED DOUBLER FOR REPAIR AREA. INSTALLED DOUBLER. REMOVED LIGHT CORROSION. FOUND TO BE WITHIN LIMITS MATERIAL LOSS. (M) 2 L 7 2 4F A6WE 2002062100105 20020621 00105 WP 2002 6 21 GTIA020420 1 20020412 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND AFT CARGO FLOORBOARD STATION 1155-1212 HAS CORROSION AND BAD INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2002062100106 20020621 00106 WP 2002 6 21 GTIA020421 1 20020412 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - AT CARGO FLOORBOARD STATION 1212-1231 BROKEN 2 PLACES AND HAS CORROSION. FORMED NEW PANEL. (M) 2 L 7 2 4F A6WE 2002062100107 20020621 00107 WP 2002 6 21 GTIA020422 1 20020408 A 5730 PANEL DOUG DC9 DC982 3022082 WP RT WING DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND RIGHT WING L/E PANEL 1248C FASTENER HOLE BUSTED OUT FRONT AND BACK, TOOL MARKS, BARE METAL, CORROSION AND CH AFING. CUT OUT DAMAGED AREA. FABRICATED NEW SKIN SECTION. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER AND SKIN SECT ION. (M) 2 L 7 2 4F A6WE 2002062100108 20020621 00108 WP 2002 6 21 GTIA020423 1 20020405 A 2621 FIRE BOTTLE DOUG DC9 DC982 3022082 WP LAVATORY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - ALL LAVATORY FIRE EXTINGUISHER BOTTLES BADLY CORRODED. REMOVED ALL LAVATORY FIRE EXTINGUISHERS. INSTALLED ALL LA VATORY FIRE EXTINGUISHERS. (M) 2 L 7 2 4F A6WE 2002062100109 20020621 00109 WP 2002 6 21 GTIA020424 1 20020426 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND AFT CARGO FLOOR SUPPORT STATION 1136 HAS CORROSION. REMOVED CORROSION. LOCATED AND DRILLED NEW FLOOR SUPPO RT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062100110 20020621 00110 WP 2002 6 21 GTIA020425 1 20020412 A 2560 HOOK DOUG DC9 DC982 3022082 WP CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND OVERWING EMERGENCY EXITS ESCAPE LINES FOUR EACH, HOOKS CORRODED, SURFACE CORROSION. UPON CORROSION REMOVAL ESCAPE ROPES STARTED FRAYING AND STILL HOOK CORRODED UNDER ROPES, 4 EACH. REMOVED RIGHT FORWARD ESCAPE LINE. REMOVED L EFT FORWARD ESCAPE LINE. REMOVED RIGHT AFT E-LINE. REMOVED LEFT AFT E-LINE. INSTALLED RIGHT AFT ESCAPE LINE. INSTALL ED LEFT FORWARD ESCAPE LINE. INSTALLED LEFT AFT ESCAPE LINE, INSTALLED RIGHT FORWARD ESCAPE LINE. (M) 2 L 7 2 4F A6WE 2002062100111 20020621 00111 WP 2002 6 21 GTIA020426 1 20020409 A 5753 BRACKET DOUG DC9 DC982 3022082 WP T/E FLAP CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOND RIGHT T/E NR 3 FLAP INBOARD ATTACHED BRACKET CRACKED. REMOVED CRACKED BRACKET. FABRICATED BRACKET, INSTALLE D. (M) 2 L 7 2 4F A6WE 2002062100112 20020621 00112 CE 2002 6 21 DBC2002F00003 1 20020606 A 2731 660821718 INDICATOR LEAR 35 31 5170530 CE PITCH TRIM FAILED E DBCA O OTHER N FALSE WARNING LD LANDING 1 GL 13 350DS 39 002 UPON LANDING (TAKEOFF TRIM) ANNUNCIATOR ILLUMINATED. PILOT CHECKED PITCH TRIM INDICATOR AND FOUND IT INDICATED TRIM WAS WITHIN TAKEOFF LIMITS. OPERATION OF PITCH TRIM SWITCH WOULD ADJUST TRIM BUT INDICATOR DID NOT MOVE. TROUBLESHOT TO FA ILED TRIM INDICATOR. REMOVED TRIM INDICATOR (PN 6608217-18)(SN 88) REPLACED WITH SERVICEABLE UNIT. OPERATIONS CHECKED GOOD. 2 L 7 2 4F RT A10CE 2002062100113 20020621 00113 WP 2002 6 21 GTIA020427 1 20020409 A 5753 CHANNEL DOUG DC9 DC982 3022082 WP T/E FLAP BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND RIGHT FLAP TRAILING EDGE INBOARD FLANGE BROKEN. REMOVED BROKEN U-CHANNEL. FABRICATED NEW CHANNEL, INSTALLE D. (M) 2 L 7 2 4F A6WE 2002062100114 20020621 00114 WP 2002 6 21 GTIA020428 1 20020501 A 7830 DOOR DOUG DC9 DC982 3022082 WP THRUST REVERSER CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 823NK 48020 DTW - FOUND CRACK IN THE NR 2 UPPER T/R DOOR. STOP DRILLED CRACK AND INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2002062100115 20020621 00115 WP 2002 6 21 GTIA020429 1 20020506 A 3397 WIRE DOUG DC9 DC981 3022081 WP CABIN DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 805NK 48058 FLL - FOUND EMERGENCY LIGHTS ON THE FLOOR INOPERATIVE FROM ROW 1 TO ROW 8. REPAIR WIRING PER MM 20-50-01. OPS CHECK OK PER MM 33-50-00. (M) 2 L 7 2 4F A6WE 2002062100116 20020621 00116 2002 6 21 GTIA020430 4 20020509 A 3454 20412343421 RECEIVER DOUG DC9 DC982 3022082 WP COCKPIT FAILED A GTIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 23 800NK 49144 FLT 9826 - ACY - FOUND ON TWO ILS APPROACHES TO RWY 4L TO DTW (FREQ 111.95) AUTOPILOT DISCONNECTED AFTER 'S' TURNING AT 300 FEET AGL. AUTOPILOT WORKS OK DURING ALL OTHER PHASES OF FLIGHT. NR 1 HAD MULTIPLE FAIL CODES IN THE FLIGHT FAULT R EVIEW. REMOVED AND REPLACED NR 1 VHF NAV RECEIVER. OPS CHECKS GOOD. (M) 2 L 7 2 4F A6WE 2002062100117 20020621 00117 CE 2002 6 21 H792002F00001 1 20020514 A 7602 98620661 CONTROL CABLE CESSNA 210 T210N 2073456 CE MIXTURE FAILED E H79A A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 15 155RR 10000 21063286 THIS AIRCRAFT, ENROUTE, ON TAKEOFF THE PILOT NOTICED A ROUGHNESS IN THE ENGINE OPERATION. THE PILOT ELECTED TO LAND AT AIRPORT TO HAVE MAINTENANCE TROUBLESHOOT ROUGHNESS. MAINTENANCE DISCOVERED THAT THE MIXTURE CONTROL CABLE HAD FAILED AT THE CRIMP SWIVEL JOINT AT THE ENGINE FUEL CONTROLLER. THE CABLE HAD BROKE LEAVING ONLY THE ROD END AND SMALL PORTION O F MIXTURE CABLE ATTACHED TO THE ENGINE FUEL CONTROLLER CAUSING THE MIXTURE CONTROL TO BE IN THE LEANING POSITION. THIS CABLE IS A 1500 HOUR REPLACEMENT ITEM PER MFG. CABLE WAS REMOVED AND REPLACED, AIRCRAFT WAS RETURNED TO SERVICE. 1 H 7 1 3O 3A21 2002062100118 20020621 00118 CE 2002 6 21 HMN2002F00002 1 20020530 A 7603 311AS3146780 CONTROL CABLE MTSBSI MU2 MU2B35 5780411 CE THROTTLE FRAYED B HMNR K NONE O OTHER IN INSP/MAINT 1 SW 15 840MA 9970 612 FRAYED THROTTLE CABLE FOUND DURING ROUTINE 100 HOUR INSPECTION. FRAYED PORTION IN AFT FUSELAGE ON A 90 DEGREE TURN PULL EY. FOUND AND REPLACED. 1 H 7 2 3T RT A10SW 2002062100119 20020621 00119 CE 2002 6 21 HMN2002F00003 1 20020610 A 7603 311AS3146780 CONTROL CABLE MTSBSI MU2 MU2B35 5780411 CE POWER LEVER FRAYED B HMNR K NONE O OTHER IN INSP/MAINT 1 SW 15 940MA 8383 615 FRAYED LT ENGINE POWER LEVER CABLE FOUND DURING ROUTINE 100 HOUR INSPECTION. FRAYED PORTION UNDER CENTER PEDESTAL IN CO CKPIT. (SW15200210206) 1 H 7 2 3T RT A10SW 2002062100120 20020621 00120 CE 2002 6 21 R2J2002F00005 1 20020528 A 5520 115610010 HINGE BEECH 100 B100 1152919 CE LEFT ELEVATOR CRACKED B R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 78DA 6770 BE11 DURING PHASE INSPECTION RIBS AT LEFT ELEVATOR OUTBOARD HINGE FOUND CRACKED. NEW PARTS INSTALLED AND ELEVATOR REINSTALLE D AND ELEVATOR REINSTALLED. INSPECTORS SHOULD PAY PARTICULAR ATTENTION TO THIS AREA. MORE CRACKING WAS FOUND, AFTER EL EVATOR REMOVAL TO REPAIR VISIBLE CRACKING. 1 L 7 2 4T A14CE 2002062100121 20020621 00121 CE 2002 6 21 R2J2002F00006 1 20020528 A 3000 10091000279 TUBE BEECH 100 B100 1152919 CE GARRTT TPE331 TPE331* 01514 WP ENG ANTI ICE SYS DAMAGED B R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 78DA 6770 BE11 102026C WHILE COMPLYING WITH MFG SB, BOTH ENGINE HAD DAMAGE TO ENGINE ANTI-ICE TUBING AT THE FLARES, WHICH REQUIRED REPLACEMENT. ENGINE BLEED AIR FOR ENGINE ANTI-ICE WAS DUMPING INTO COWL INSTEAD OF GOING INTO DEICE MANIFOLDS. CAUSE WAS LOOSE (B) NUTS. NEED TO BE SAFTIED. 1 L 7 2 4T 3 T A14CE E2WE 2002080500055 20020805 00055 NM 2002 8 5 373PA0004 1 20020621 A 3350 86210066 BATTERY PACK BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 373PA 23749 ONE EMERGENCY EXIT LIGHT ASSEMBLY INOP. REMOVED AND REPLACED BATTERY PACK. PERFORMED OPS CHECK, LIGHT ASSEMBLY LIGHTS ILLUMINATED. A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002062100122 20020621 00122 NM 2002 6 21 UPS02438666 1 20020601 A 5310 SPLICE PLATE BOEING 747 747200 1384847 NM NLG W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C NLG W/W RH AFT LWR CORNER STA 400 INTERNAL SPLICE PLATE CRKD AT FILLET AREA BY 1" AS MARKED. NLG W /W RH BS 400 BETWEEN STR 38R TO 44R REPAIRED AS PER EO 747-5330-3520 APPENDIX B CIRCLE 5. 2 L 7 4 4F RT A20WE 2002062100123 20020621 00123 NM 2002 6 21 UPS02438667 1 20020530 A 5310 WEB BOEING 747 747200 1384847 NM RH BS 1241 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C R/H WING CENTER SECTION STA 1241 BULKHEAD FITTING REAR SPAR WEB AFT SURFACE FOUND CORROSION ADJACENT T O BOLTS #13, 14, 15, 24, 25 & 26. CORROSION IS REMOVED AS PER EO B747-5710-11129 PG 9, OPENED BOLT HOLES ARE REAMED TO 0.375", NDT C/OUT & CONFIRMED NO CRK ON BOLT HOLES AS PER NTM PART 6,51-00-00 FIG.16, ALODINE APPLIED TO ALL ALUMINUM SURFACE & ALL 6 EA BOLTS ARE REINSTALLED AS PER EO B747-5710-11129, LEAK CHK OF FUEL TANK C/OUT "SATIS" PER MM 28-11-00 2 L 7 4 4F RT A20WE 2002062100124 20020621 00124 NM 2002 6 21 UPS02438669 1 20020531 A 5310 SPLICE PLATE BOEING 747 747200 1384847 NM NLG W/W L/H AFT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C NLG W/W LH AFT LWR CORNER SPLICE PLATE CRACKED THROUGH 1EA FASTENER HOLE AT FILLET AREA BY 1.5" AS MAR KED. NLG W/W LH AFT LWR CORNER SPLICE PLATE REPAIRED AS PER EO B747-5330-3520 APPENDIX B CIRCLE NOTE 5 JUST AT BS 40 0 BTN STR 38L AND STR 44L. 2 L 7 4 4F RT A20WE 2002062100125 20020621 00125 NM 2002 6 21 UPS02438680 1 20020530 A 5310 WEB BOEING 747 747200 1384847 NM STA 1241 B/H LH CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C L/H WING CENTER SECTION STA 1241 BULKHEAD FITTING REAR SPAR WEB AFT SURFACE FOUND CORROSION ADJACENT T O BOLTS #14, 15, 25 AND 26. LH WING CENTER SECTION STA 1241 BULKHEAD FTG REAR SPAR WEB AFT SURFACE AT BOLT #14, 15, 25 & 26 BOLTS AREA CORROSION REPAIR C/OUT AS PER EO B747-5710-11129, REFER ATTACHED CWS FOR DETAIL WORK. 2 L 7 4 4F RT A20WE 2002062100126 20020621 00126 NM 2002 6 21 UPS02438681 1 20020602 A 5310 WEB BOEING 747 747200 1384847 NM STA 1241 B/H RH CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C R/H WING CENTER SECTION STA 1241 BULKHEAD CANTED PRESSURE DECK ANGLE REAR FACE CORRODED ADJACANT #5, 6 & 7 FASTENER HOLE AREA AS INDICATED. RH WING CENTER SECTION STA 1241 BULKHEAD CANTED PRESSURE DECK ANGLE REAR FACE CORROSION ADJACANT #5, 6 & 7 FASTENERS AREA CORROSION REPAIRED AS PER EO B747-5710-11129, REFER ATTACHED CWS FOR DETAILS WORK. 2 L 7 4 4F RT A20WE 2002062100127 20020621 00127 NM 2002 6 21 UPS02438683 1 20020529 A 5310 WEB BOEING 747 747200 1384847 NM LH NOSE W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C LH NOSE W/W BS 320 INNER CHORD FRAME WEB FOUND 3EA FASTENER HOLES CRKD, REF ATTACHED SKETCH FOR DETAIL S. LH NOSE W/W BS 320 INNER CHORD FRAME WEB REPAIRED AS PER HX RS R53-12-34829. 2 L 7 4 4F RT A20WE 2002062100128 20020621 00128 2002 6 21 801DM0004 4 20020514 A 2220 6228780103 AUTOPILOT SYS BOEING 757 757200 1384950 NM A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 801DM 26240 Aircraft will not maintain spped in "SPD" mode. Removed autopilot MCP for bench check. MCP was repaired and installed. Ops ck normal per MM 22-11-02. 2 L 7 2 4F RT A2NM 2002062100129 20020621 00129 NM 2002 6 21 SABA020069 1 20020620 A 3350 1306 BULB DHAV DHC8 DHC8102 2809003 NM CABIN A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 881CC 294 Flight 5097 from CLT to PGV: During preflight in Charlotte Pilot reported that the emergency lights at row # 4 would not test. Maintenance removed and replaced Bulbs. System ops checked good and aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002080500087 20020805 00087 NE 2002 8 5 ARWA20020603 2 20020619 A 7532 560339 BLEED VALVE DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE SEIZED A ARWA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 19 29UA 9536 1407 46159 643681 ENGINE NR 4 UNABLE TO SPOOL TO MAX POWER DURING TAKEOFF. REMOVED AND REPLACED ENGINE BLEED VALVE IAW MM 75-30-3; OPERAT IONS CHECKED NORMAL IAW MM 71-00. 2 L 7 4 4F 4 F 4A25 1E8 2002062100130 20020621 00130 NM 2002 6 21 DL76K020644 1 20020609 A 3350 NOTAPPLICABLE HARNESS BOEING 767 767332 1382001 NM SEAT 15F DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 176DZ 29697 EMERGENCY PATH LIGHT AT 15F INOP---FOUND HARNESS AT SEAT ROW 15FG DISCONNECTED. RECONNECTED AND SECURED HARNESS LIGHT O PERATES NORMAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS 2 L 7 2 4F RT A1NM 2002062100131 20020621 00131 NM 2002 6 21 DLM88020661 1 20020613 A 3350 UNK BATTERY DOUG MD88 MD88 3023688 NM MID CABIN UNSERVICEABLE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DL 49543 FWD OVERHEAD OVERWING EMERGENCY LIGHTS INOP...RPLD BATTERIES NOW OPS NML 2 L 7 2 4F RT A6WE 2002062100132 20020621 00132 NM 2002 6 21 DL76P020666 1 20020613 A 5330 141T3320199 SKIN BOEING 767 767332 1382001 NM FS 374, S-17L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 144DA 27584 FUSELAGE / SKIN / FS 374 / STRG. 17L / SKIN LAP JOINT : DENT REPAIR THE FUSELAGE SKIN AT FS 374 AT THE STRINGER 17L LAP JOINT WAS DENTED. THE DENT WAS REMOVED WITH A 4.5" X 3.9" CUTOUT IN THE UPPER AND LOWER SKIN OF THE LAP JOINT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 383329-14, REV B. 2 L 7 2 4F RT A1NM 2002062100133 20020621 00133 NM 2002 6 21 DLM88020670 1 20020614 A 3350 RPS1 RACK DOUG MD88 MD88 3023688 NM B5-12 UNSERVICEABLE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DL 49543 ALL AFT SECTION EMERGENCY LIGHTS INOP. REPLACED BATTERY AND RACK...NOW OPS NML 2 L 7 2 4F RT A6WE 2002062100134 20020621 00134 NM 2002 6 21 DL76S020676 1 20020616 A 2400 AC4500361 SWITCH 233N321152 BOEING 767 767332 1382001 NM COCKPIT LOOSE A DALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 SO 27 135DL 547 25145 STANDY BY POWER SWITCH LOOSE INTERNALLY CAUSING ALL THREE IRS'S TO FAIL . THIS HAPPENED IN FLIGHT ON PREV LEG. REF LOG SHEETS 792866 ITEM 2 AND 792871 ITEM 1 FOUND THAT WIGGLING STNBY PWR CAUSED TROUBLE REPLCD STBY POW PANEL IRUS OPS NML OFF SN ON SN DPN 1 D00812 D00547 311701501 2 L 7 2 4F RT A1NM 2002062100135 20020621 00135 NM 2002 6 21 DL757020681 1 20020617 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FS 570, S-16L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 645DL 24216 FUSELAGE / SKIN / FS 570-660 / STRG. 14L-19L : GROUND DAMAGE SPLICE REPAIR THE FUSELAGE SKIN WAS FOUND WITH 2 DENTS IN CLOSE PROXIMITY TO AN EXISTING SKIN REPAIR DOUBLER. TO REMOVE ALL DAMAGE AND ACCOMPLISH A REPAIR, THE SKIN WAS CUT AT FS 570 BETWEEN THE SKIN LAP JOINTS AT STRG. 14L & 19L AND THE AFT SECTION OF SKIN REMOVED. A NEW SKIN SECTION WAS SPLICE IN WITH AN INTERNAL AND EXTERNAL ALUMINUM SPLICE DOUBLER PER ER/A 383226-14, REV A. 2 L 7 2 4F RT A2NM 2002062100136 20020621 00136 NM 2002 6 21 DLM11020687 1 20020619 A 2500 2676SB020 CHILLER 2676SB020 DOUG MD11 MD11 3023602 NM AFT GALLEY FAILED A DALA C ABORTED TAKEOFF O OTHER CR CRUISE 1 SO 27 806DE 48477 AT CRUISE FLT ATTDS INFORMED US THERE WAS A STRONG ELECTRICAL SMELL IN THE AFT GALLEY CHILLER #8 RED FAIL LIGHT WAS FLASHING. SHUT DOWN CHILLER #8 AND #7. GALLEY POWER WAS ALSO TURNED OFF. DIVERTED TO JFK. SMELL SEEMED TO DISSAPATE. CORR ACTION: FOUND NBR 7 CHILLER FAN GRINDING. CHECKED AREA OF CHILLERS NO EVIDENCE OF ELECT WIRING CHAFFED OR BURNT. CHECKED AFT COOLING FAN FOUND OK #8 CHILLER OPS NORMAL. RPLD #7 CHILLER. PERFORMED OVER WEIGHT LANDING INSPECTION PER M.M. 2 L 7 3 4F RT A22WE 2002070300071 20020703 00071 NM 2002 7 3 AWXA200200533 1 20020609 A 5313 654988660 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 MCN - MAJOR REPAIR - DURING C-16 CHECK A CRACK WAS FOUND ON STRINGER 16 RT, AT BS 500C+4. MAINTENANCE TRIMMED OUT CRACK ON STRINGER 16 RT AT BS 500C+4; FABRICATED REPAIR CHANNEL, RADIUS FILLER, AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2002062100137 20020621 00137 NM 2002 6 21 AWXA200200536 1 20020603 A 5330 654576988 SKIN BOEING 737 737277 1384570 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 0 0 22653 YVR - MAJOR REPAIR - DURING C-15 CHECK TWO RIVET HEADS WERE FOUND POPPED FROM THE FUSELAGE AT STA. 495, STR. 495. MAINT ENANCE FABRICATED DOUBLER AND INSTALLED REPAIR PER SRM 51-10-02 PAGE 7. INTALLED PROTECTIVE FINISH PER MM 51-21-0 PAGE 1. 2 L 7 2 4F RT A16WE 2002062100138 20020621 00138 NM 2002 6 21 AWXA200200537 1 20020609 A 5311 6558280 FRAME BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 0 0 23778 MCN - MAJOR REPAIR - DURING C-16 CHECK, MAINTENANCE USING HVEC FOUND 2 CRACKS ON A ZEE FRAME AT BS 360 STR 14R AND 15R. MAINTENANCE REPAIRED THE AFFECTED AREA IAW B737-300 SRM 53-00-07 PAGES 219-221. THE CRACKS WERE IDENTIFIED AS A 5/8" CRA CK EXTENDING THRU TOP FASTNER HOLE, AND A CRACK 1 5/8" LONG THRU THE NEXT 3 FASTNER HOLES. 2 L 7 2 4F RT A16WE 2002062200001 20020622 00001 NM 2002 6 22 AWXA200200546 1 20020610 A 5312 6546568515 BULKHEAD BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 0 0 22653 YVR - MAJOR REPAIR - DURING C-15 INSPECTION A WEB CRACK WAS FOUND AT FOUR RIVETS AT STA 1016 S-6L NEAR THE FWD SIDE OF THE PRESSURE BULKHEAD. DAMAGED AREA WAS CUT OUT AND HVEC WAS PERFROMED AND INSPECTED PER NDT MANUAL PART 6 , 51-00-00 FI G. 23. NO CRACKS FOUND. INSTALLED REPAIR DOUBLER PER SRM 53-10-4 FIG 15 PAGE 47 AND AWA E.R. 15-5314-02168-TB2. SEALED A FFECTED AREA AND RE-INSTALLED FASTNERS AS REQUIRED. PAINTED AFFECTED AREA PER MM 51-21-0 PAGE 201. 2 L 7 2 4F RT A16WE 2002062300001 20020623 00001 SO 2002 6 23 RAIA00206182 1 20020527 A 5320 14524131007 FITTING EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 805HK 145096 BLK CK-TASK# 532100210805A00 FOUND "U" SHAPE LATERAL FITTING BENEATH PAX DOOR CORRODED. REMOVED AND REPLACED FITTING IAW EMB 145 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002062300002 20020623 00002 SO 2002 6 23 RAIA00206183 1 20020527 A 5320 14522460009 GUSSET EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 805HK 145096 BLK CK TASK 3 532300220804A00 FOUND CORROSION ON GUSSET AT FRAME 23-Y0 REMOVED AND REPLACED GUSSET AT FRAME 23 Y0 IAW EM B 145 SRM 51-40-02 2 L 7 2 4F RT T00011AT 2002062300003 20020623 00003 SO 2002 6 23 RAIA00206184 1 20020527 A 5320 14521725001 SILL EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 805HK 145096 BLK CK TASK 3 532300220804A00 FOUND CORROSION AT LEFT SILL BETWEEN FRAME 14&20 AT 16L. REMOVED AND REPLACED LEFT SILL BE TWEEN FRAMES 14&20 AT 16L IAW EMB-145 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002062300004 20020623 00004 SO 2002 6 23 RAIA00206185 1 20020527 A 5320 14522459003 SUPPORT EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 805HK 145096 BLK CK TASK 3 532300220804A00 FOUND CORROSION AT RAMP SUPPORT FRAME 20 Y0. REMOVED AND REPLACED RAMP SUPPORT FRAME 20 Y0 IAW EMB-145 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002062300005 20020623 00005 SO 2002 6 23 RAIA00206186 1 20020527 A 5320 14521699001 SUPPORT EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 805HK 145096 BLK CK TASK 3 532300220804A00 FOUND CORROSION AT LEFT DIGITAL BETWEEN FRAMES 20&23. REMOVED AND REPLACED LEFT DIGITAL BE TWEEN FRAMES 20&23 IAW EMB-145 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002062300006 20020623 00006 SO 2002 6 23 RAIA00206187 1 20020527 A 5320 14522460011 STRAP EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 805HK 145096 BLK CK TASK 3 532300220804A00 FOUND CORROSION ON STRAP AT FRAME 17 BETWEEN Y0 AND Y479. REMOVED AND REPLACED STRAP AT FR AME 17 BETWEEN Y0 AND Y479 IAW EMB-145 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002062300007 20020623 00007 SO 2002 6 23 RAIA00206188 1 20020527 A 5320 14521721005 STRAP EMB 145 EMB145 3260210 SO CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 805HK 145096 BLK CK TASK 3 532300220804A00 FOUND CORROSION ON STRAP AT FRAME 14 Y479. REMOVED AND REPLACED STRAP AT FRAME 14 Y479 IAW EMB-145 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002062300008 20020623 00008 2002 6 23 RAIA00206189 4 20020614 A 3420 HG2010AC02 COMPUTER EMB 145 EMB145 3260210 SO FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 803HK 120 145077 5271-PIT- #2 AHRS FAILED. MAINTENANCE REMOVED AND REPLACED THE #2 AHRS COMPUTER. 2 L 7 2 4F RT T00011AT 2002062300009 20020623 00009 EU 2002 6 23 RAIA00206190 1 20020616 A 7900 311854701 GARLOCK SEAL AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 722TE 220 124512 5556-STL- #1 ENGINE LOW OIL PRESSURE WARNING SOUNDED. MAINTENANCE FOUND #1 ENGINE STARTER GARLOCK SEAL LEAKING, REMOVED AND REPLACED THE GARLOCK SEAL, SERVICED OIL AND LK CK GOOD. 2 H 7 2 4T 4 T RT A53EU E2ONE 2002062300010 20020623 00010 EU 2002 6 23 RAIA00206191 1 20020618 A 3350 167001 LIGHT AEROSP ATR72 ATR72202 8680940 EU CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 721TE 217 5590-STL- ONE LIGHT INOP IN EMERGENCY PATH LIGHT STRIP. REMOVED AND REPLACED LIGHT BULB IN EMERGENCY PATH STRIP, OPS CK OK. 2 H 7 2 4T RT A53EU 2002062300011 20020623 00011 EU 2002 6 23 RAIA00206193 1 20020620 A 2432 407817 BATTERY JETAIR JETSTM JETSTM4101 1500501 EU OVERHEATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 569HK 10966 312 41088 5529-STL- BATTERY OVER TEMP LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED BATTERIES, OPS OK. 2 L 7 2 4T RT A41NM 2002062400001 20020624 00001 WP 2002 6 24 0202019963 1 20020612 A 4990 HONEYWELL GTCP8598DCA DOUG DC9 DC931 3022065 WP A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 913RW P159DCA 47171 DURING CLIMB, THE LEFT AFT SMOKE DETECTOR SOUNDED AND FLIGHT ATTENDANTS REPORTED ODOR IN THE CABIN. FLIGHT CREW RETURNED TO DEPARTURE AIRPORT. MAINTENANCE REPLACED COALESCER SOCKS AND PERFORMED A PACK BURNOUT. APU ON MEL. 2 L 7 2 4F A6WE 2002062400002 20020624 00002 WP 2002 6 24 211002004 1 20020517 A 5320 5936038501 THRESHOLD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 AFT CARGO THRESHOLD STRUCTURE HAS CORROSION AT 28R AND FROM 1155 TO 1212. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS MORE 2 PERCENT MATERIAL LOSS. FORMED, DRILLED AND INSTALLED. REPAIR DOUBLER IAW SRM. REMOVED AND REINSTALLED SCUFF PL ATE TO GAIN ACCESS IAW SRM. 2 L 7 2 4F RT A6WE 2002062400003 20020624 00003 GL 2002 6 24 ALG2002F00039 2 20020512 A 7210 6893672 PINION GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 577AL 682 53247 ENGINE WAS REMOVED DUE TO CHIP LIGHT. GEARBOX WAS DISASSEMBLED TO FIND SOURCE OF METAL. FOUND EXCESSIVE GALLING ON PIN ION GEAR, SPALLING AND GALLING ON T/M GEAR. BOTH GEARS HAVE VERY UNUSUAL WEAR PATTERN. ASSURE PROPER MESHING AND MACH INING OF GEAR TEETH AT FACTORY. 1 G 7 1 3U 3 U O H2SW E1GL 2002062400004 20020624 00004 GL 2002 6 24 ALG2002F00040 2 20020512 A 7210 23071895 PINION GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 577AL 53247 CAE847251 ENGINE WAS REMOVED DUE TO CHIP LIGHT. GEARBOX WAS DISASSEMBLED TO FIND SOURCE OF METAL. FOUND EXCESSIVE GALLING ON PIN ION GEAR, SPALLING AND GALLING ON T/M GEAR. BOTH GEARS HAVE VERY UNUSUAL WEAR PATTERN. ASSURE PROPER MESHING AND MACHI NING OF GEAR TEETH AT FACTORY. 1 G 7 1 3U 3 U O H2SW E1GL 2002062400005 20020624 00005 GL 2002 6 24 ALG2002F00041 2 20020425 A 7210 6893672 PINION GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX GALLED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 467AL 619 53190 GEARBOX WAS REMOVED DUE TO FWU BORE DAMAGE. UPON INSPECTION OF CHIP DETECTORS, FOUND METAL ON BOTH PLUGS. AFTER DISASS EMBLY FOUND EXCESSIVE GALLING ON TM AND PINION GEARS CAUSE FOR METAL. METAL CONTAMINATION WAS GENERATED FROM UNFINISHED MACHINING OF TM GEAR TEETH AT RADIUS. THIS CAUSED GALLING TO PINION GEARS. ASSURE PROPER MACHINING AND MESHING OF GEA R TEETH AND RADIUS AT FACTORY. 1 G 7 1 3U 3 U O H2SW E1GL 2002062400006 20020624 00006 GL 2002 6 24 ALG2002F00042 2 20020425 A 7210 23071895 GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX MISMANUFACTURED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 467AL 619 53190 GEARBOX WAS REMOVED DUE TO FWU BORE DAMAGE. UPON INSPECTION OF CHIP DETECTORS, FOUND METAL ON BOTH PLUGS. AFTER DISASS EMBLY FOUND EXCESSIVE GALLING ON TM AND PIINION GEARS CAUSE FOR METAL. METAL CONTAMINATION WAS GENERATED FROM UNFINISHE D MACHINING OF TM GEAR TEETH AT RADIUS. THIS CAUSED GALLING TO PINION GEAR. ASSURE PROPER MACHINING AND MESHING OF GEA R TEETH AND RADIUS AT FACTORY. 1 G 7 1 3U 3 U O H2SW E1GL 2002062400007 20020624 00007 SO 2002 6 24 D682002F00000 2 20020517 A 7414 6320 MAGNETO CESSNA 340 340A 2076405 CE CONT O520 TSIO520VB 17040 SO ENGINE SEIZED A D68L K NONE O OTHER IN INSP/MAINT 1 NE 05 340KG 340A1505 278307R OWNER-PILOT REPORTED BAD MAGNETO CHECK. RIGHT ENGINE LEFT MAGNETO INVESTIGATION FOUND LEFT MAGNETO WAS SEIZED AND COULD NOT BE TURNED BY HAND. PREVIOUSLY IT WAS THE RIGHT MAGNETO. REASON FOR MAG SEIZING IS EXCESSIVE HEAT, ALSO BEING PR ESSURIZED. NO LOGS AVAILABLE FOR TIME ON PART. 1 L 7 2 3O 3 O 3A25 E8CE 2002062400008 20020624 00008 SW 2002 6 24 EHA2002F00000 1 20020429 A 2897 WIRE BELL 212 212 1181420 SW FLOW SWITCH DEFECTIVE B EHAR K NONE O OTHER IN INSP/MAINT 1 AL 03 5017H 16658 30930 FLOW SWITCH HAD A BROKEN WIRE FROM STOCK. CAUSED AIRCRAFT TO HAVE LATE DEPARTURE 1 G 7 1 4U H4SW 2002062400009 20020624 00009 NM 2002 6 24 UPS02438152 1 20020421 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/ D- BS 2160 RBL 98 SEAT TRACK CRACK. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 8, P/N (BAC1520-154 5-7178T6511RK). 2 L 7 4 4F A20WE 2002062400010 20020624 00010 NM 2002 6 24 UPS02438153 1 20020419 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C, FWD CARGO - BS 880 RT FRAME I/B CHORD FOUND CRACKED AT STR - 38R. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52. 2 L 7 4 4F A20WE 2002062400011 20020624 00011 NM 2002 6 24 UPS02438154 1 20020419 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C, FWD CARGO COMPARTMENT LT STA 980 S38L STR END CRACKED AND ATTACHED SHIM DELAMINATED. STRINGER S-38L REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062400012 20020624 00012 NM 2002 6 24 UPS02438155 1 20020419 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C, FWD CARGO COMPARTMENT RT STA 980 S38R STR END CRACKED AND ATTACH SHIM DELAMINATED. FWD CARGO COMPART MENT BS 950 - BS 980 S38R STRINGER REPAIRED IAW SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062400013 20020624 00013 NM 2002 6 24 UPS02438156 1 20020418 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C, FWD CARGO - BS 880 STR 35R FOUND CHIPPED AS MARKED. FWD CARGO COMPT BS 870 BS 890 STR 35R STRINGER R EPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062400014 20020624 00014 WP 2002 6 24 EOO2002F00007 1 20020506 A 6230 369D2551021 DRIVE SHAFT HUGHES 369 369D 4470706 WP MAIN ROTOR OUT OF TOLERANCE B EOOR K NONE O OTHER IN INSP/MAINT 1 AL 03 CGVN6 1864 570132D DURING A ROUTINE INSPECTION OF THE MAIN ROTOR DRIVESHAFT IT WAS DISCOVERED THAT THE WEAR ON THE SPLINES WAS BEYOND LIMIT S. AFTER ONLY 37 PERCENT OF THE TIME WAS USED ON THE SHAFT. REPLACED UNIT. 1 G 7 1 3U H3WE 2002062400015 20020624 00015 WP 2002 6 24 EOO2002F00008 1 20020506 A 6220 SEAL HUGHES 369 369D 4470706 WP MAIN ROTOR HUB MISSING B EOOR K NONE O OTHER IN INSP/MAINT 1 AL 03 CGVH6 513 570132D DURING AN INSPECTION IT WAS DISCOVERED THAT THE LOWER MAIN ROTOR HUB GREASE SEAL WAS NOT INSTALLED BUT LAYING AT TOP THE MAIN ROTOR SWASHPLATE INSIDE OF THE UPPER DUST BOOT. REMOVED MAIN ROTOR HUB INSPECTED AND REGREASED NEW SEAL INSTALLED WITH NORMAL RESISTANCE MAIN ROTOR HUB REINSTALLED. 1 G 7 1 3U H3WE 2002062400016 20020624 00016 NM 2002 6 24 UPS02438157 1 20020419 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C, U/D - BTN BS 620 S-6L STRINGER CRACK. BS 610 - BS 630 S6L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. 2 L 7 4 4F A20WE 2002062400017 20020624 00017 WP 2002 6 24 EOO2002F00009 1 20020506 A 6210 500P2100101 BLADE HUGHES 369 369D 4470706 WP MAIN ROTOR DEBONDED B EOOR K NONE O OTHER IN INSP/MAINT 1 AL 03 CGVHG 122 570132D DURING INSPECTIONS A VOID AREA WAS FOUND .250 INCHES AFT OF THE LEADING EDGE OF THE BLADE BETWEEN STA. 56.75 AND 54.50 FROM .250 INCHES TO .375 INCHES WIDE ON THE UPPER SURFACE OF THE BLADE. REMOVED BLADE AND SENT IN FOR REPAIR. 1 G 7 1 3U H3WE 2002062400018 20020624 00018 NM 2002 6 24 UPS02438158 1 20020422 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 740 S-4L, S-3L AND S-2AL, S-3AR STRINGER END SPLICE AREA CRACKED. BS 790 S-4L, S-3L, S-2AL, S-3AR STRINGER REPAIRED IAW SRM 53-10-03 FIG 10. 2 L 7 4 4F A20WE 2002062400019 20020624 00019 CE 2002 6 24 HSY2002F00000 1 20020530 A 3220 26430096 BARREL CESSNA 208 208B 2073701 CE SHIMMY DAMPNER BURST E HSYR K NONE O OTHER IN INSP/MAINT 1 NM 07 952FE 8531 208B0060 FOUND NOSE GEAR SHIMMY DAMPNER BURST AT SNAP RING END OF SHIMMY DAMPNER CYLINDER. 1 H 7 1 3T A37CE 2002062400020 20020624 00020 NM 2002 6 24 UPS02438159 1 20020421 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C, BULK CARGO - BS 2140 RT FRAME CRACKED BTN STR 29R AND STR 30R. BS 2140 S-29R- 30R FRAME REPAIRED AS PER SRM 53-10-04 FIG 39. 2 L 7 4 4F A20WE 2002062400021 20020624 00021 NM 2002 6 24 UPS02438160 1 20020422 A 5320 TIE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 800 LT TENSION TIE FOUND CRACKED. BS 800 LT TENSION TIE REINFORCEMENT PATCH REPAIRED AS PER CUSTOMER EO B747-5310-5890 APPENDIX C FIG 2 AND AREA FINISHED PAINT PER MM 51-24-11. 2 L 7 4 4F A20WE 2002062400022 20020624 00022 NM 2002 6 24 UPS02438162 1 20020422 A 5320 TIE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 840 LT TENSION TIE FOUND CRACKED. BS 840 LT TENSION TIE REINFORCEMENT PATCH REPAIRED AS PER CUSTOMER EO B747-5310-5890 APPENDIX C FIG 2 AND AREA FINISHED PAINT TOUCH UP PER MM 51-42-11. 2 L 7 4 4F A20WE 2002062400023 20020624 00023 NM 2002 6 24 UPS02438163 1 20020422 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C, BULK CARGO BS 2120 RT FRAME WEB FOUND CORROSION BETWEEN STR 28R AND STR 29R. BS 2120 S28R S29R FRAME WEB REPAIRED AS PER SRM 53-10-04 FIG 39. BLEND OUT CORROSION DEPTH 0.030', WIDTH 1', LENGTH 1'. 2 L 7 4 4F A20WE 2002062400024 20020624 00024 NM 2002 6 24 UPS02438164 1 20020419 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C U/D - BS 540 LBL 20-40 FLOORBEAM FOUND CORROSION AS MARKED. FLOORBEAM REPAIR AT BS 540 LBL 30 TO LBL 55 AS PER SRM 53-10-07 FIG 21. 2 L 7 4 4F A20WE 2002062400025 20020624 00025 NM 2002 6 24 UPS02438165 1 20020419 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C U/D - BS 400 RBL 80 MOST O/B FLOOR SUPPORT CRACK. FLOOR SUPPORT REPAIRED AS PER SRM 53-10-04 FIG 76 A ND AREA FINISH PAINT TOUCH UP AS PER MM 51-24-11. 2 L 7 4 4F A20WE 2002062400026 20020624 00026 NM 2002 6 24 UPS02438166 1 20020418 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO - BS 840 LT FRAME I/B CHORD FOUND CORROSION AT STR 30L. FWD CARGO BS 840 LT FRAME I/B CHORD REPAIR AT STR 30L AS PER SRM 53-10-04 FIG 52. 2 L 7 4 4F A20WE 2002062400027 20020624 00027 NM 2002 6 24 UPS02438167 1 20020419 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSLEAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C U/D BS 330 LBL 0-40 FLOOR SUPPORT CORRODED. U/D BS 330 RBL 10 TO LBL 45 FLOOR SUPPORT REPAIR AS PER S RM 53-40-04 FIG 2. 2 L 7 4 4F A20WE 2002062400028 20020624 00028 NM 2002 6 24 UPS02438168 1 20020418 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 900 AND 940-960 RBL 33 SEAT TRACK CROWN FOUND CHAFING MARK AS MARKED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. (P/N: BAC1520-1566-7178T6511RK) 2 L 7 4 4F A20WE 2002062400029 20020624 00029 NM 2002 6 24 UPS02438169 1 20020416 A 5320 65B0689528 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C BULK CARGO - BS 1950-1960 S44R STRINGER SPLICE FOUND CORRODED AS MARKED. BS 1950-1960 S44R STRINGER S PLICE REPLACEMENT AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002062400030 20020624 00030 EU 2002 6 24 2002F00635 1 20020429 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 902AE 340B269 SPS - FLT 3580 - ON PREFLIGHT, CREW FOUND EMERGENCY EXIT SIGN OVER MAN CABIN DOOR AND FLIGHT ATTENDANT SEAT TO BE INOPER ATIVE. AIRCRAFT WAS FERRIED TO LAW. MAINTENANCE REMOVED AND REPLACED THE COCKPIT ARM SWITCH AND POWER SUPPLY UNITS 20L N AND 21LN IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002062400031 20020624 00031 EU 2002 6 24 2002F00636 1 20020429 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 902AE 340B269 SPS - FLT 3580 - ON PREFLIGHT, CREW FOUND EMERGENCY EXIT SIGN OVER MAIN CABIN DOOR AND FLIGHT ATTENDANT SEAT TO BE INOPE RATIVE. AIRCRAFT WAS FERRIED TO LAW. MAINTENANCE REMOVED AND REPLACED THE COCKPIT ARM SWITCH AND POWER SUPPLY UNITS 20 LN AND 21LN IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002062400032 20020624 00032 SW 2002 6 24 JBZ2002F00000 1 20020603 A 6220 407012019101 HEAD BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR DAMAGED B JBZR K NONE O OTHER IN INSP/MAINT 1 WP 27 108SD 3164 53075 DURING INSPECTION, DAMAGE WAS NOTED ON TAIR ROTOR CROSSHEAD PITCH CHANGE ARMS CAUSED BY CONTACT WITH THE P/C LINKS. 1 G 7 1 3U 3 U O H2SW E1GL 2002062400033 20020624 00033 CE 2002 6 24 R2J2002F00007 1 20020528 A 5320 505244327 BRACKET BEECH 100 B100 1152919 CE ELEVATOR CRACKED A R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 78DA 6770 BE11 WHILE COMPLETING INSPECTION OF CABIN ELEVATOR PULLEY BRACKET PER MFG SB. FOUND BRACKET CRACKED AND STOP DRILLED NOT APP ROVED REPAIR SB CALLS FOR NEW HEAVIER BRACKETS INSTALLED PER KIT. 1 L 7 2 4T A14CE 2002062400034 20020624 00034 CE 2002 6 24 R2J2002F00008 1 20020528 A 5753 50160003 RIB BEECH 100 B100 1152919 CE TE FLAP CRACKED A R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 78DA 6770 BE11 DURING PHASE INSPECTION FOUND CRACK IN SHIM UNDER RIGHT INBOARD FLAP IN AREA OF ACTUATOR ATTACH BRACKET. SKIN WAS CRACK ED BECAUSE THE FLAP RIB HAD BROKEN. THIS RIB IS WHAT THE FLAP ACTUATOR FOR INSPECTION. THE CRACKED SHIM WAS A RESULT OF RIB FAILURE. INSPECTORS SHOULD INSPECT AREA AT FLAP ACTUATORS ATTACH BRACKETS CLOSLY. RIB REQUIRED REPLACMENT. 1 L 7 2 4T A14CE 2002062400035 20020624 00035 NE 2002 6 24 RCO2002F00001 2 20020523 A 7421 FHE2464 IGNITER SCWZER G164 G164A 3952704 EA PWA JT15 JT15D4 52112 NE ENGINE BROKEN A RC0R K NONE O OTHER IN INSP/MAINT 1 SW 17 6637 150 766 PCE71690 DURING A SCHEDULED PHASE INSPECTION ON THIS AIRCRAFT, THE IGNITERS WERE REMOVED FOR TEST AND WEAR CHECK. ONE IGNITOR WA S MISSING THE CENTER ELECTRODE. THIS PART HAS 150 HOUR SENSE IT WAS REPLACED AT THE LAST INSPECTION. UPON CLOSER INSPE CTION THE CENTER ELECTRODE WAS NOT MISSING BUT HAD BROKEN OFF AND HAD SLID BACK INTO THE HOUSING. THE AIRCREW HAD NOT R EPORTED ANY PROBLEMS IN THE OPERATION OF THE ENGINE. 1 Q 7 1 3R 4 F 1A16 E1NE 2002062400036 20020624 00036 EA 2002 6 24 REX2002F00001 1 20020522 A 2750 HANDLE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS INOPERATIVE A REXA K NONE O OTHER IN INSP/MAINT 1 SO 25 8475B 7475 FLAP FAIL MESSAGE WHILE CONFIGURING FOR VISUAL APPROACH. QRH PROCEDURES FOLLOWED AND A UNEVENTFUL LANDING WAS PERFORMED . COMPLETED AD 98-20-01 FOUND FLAP HANDLE NOT IN DETENT, DI OPENED AND FLAPS WHERE MONITORED FOR SEVENTY TWO HOURS WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2002062400037 20020624 00037 EA 2002 6 24 REX2002F00002 1 20020522 A 3260 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG CENTERING OUT OF ADJUST A REXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 8560F 7560 (SWITCH) -ON DEPARTURE AFTER GEAR SELECTED UP, CREW RECEIVED A (NOSE DOOR OPEN) MESSAGE AND A GEAR DISAGREE WARNING. CH ECKLIST WAS FOLLOWED AND A UNEVENTFUL LANDING WAS MADE. FOUND NOSE LANDING GEAR STRUT CENTERING PROXIMITY SWITCH OUT OF ADJUSTMENT. 2 L 7 2 4F RT A21EA 2002062400038 20020624 00038 CE 2002 6 24 S8A2002F00002 1 20020601 A 7500 45A6351731 LINE MTSBSI MU300 MU300 5780602 CE PWA JT15 JT15D4 52112 NE BLEED AIR SYSTEM RUPTURED B S8AR O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 05 399MM A017SA PCE70648 CREW REPORTED REAR DUCT OVERHEAT WARNING WHILE ON THE GROUND AWAITING DEPARTURE. TROUBLESHOOTING REVEALED RIGHT ENGINE BLEED AIR DUCT PN 45A63517-31 (SUPERCEDED TO 128-550012-1) HAD RUPTURED IN THE LOWER BELLOWS. THIS PART IS THE SUBJECT OF AD 2001-0306 DATED 2/7/2001 WHICH CALLS FOR 400 HOUR REPETITIVE INSPECTIONS OF THE WIRE BRAID WHICH SURROUNDS THE BEL LOWS. PRIOR TO THIS FAILURE NO BROKEN STRANDS OR LEAKAGE HAD BEEN OBSERVED DURING COMPLIANCE WITH THE AD. 2 H 7 2 4F 4 F RT A14SW E1NE 2002062400039 20020624 00039 2002 6 24 GTIA0200448 4 20020413 A 2210 BRACKET DOUG DC9 DC982 3022082 WP YAW DAMPER CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - YAW DAMPER ACTUATOR ATTACHED BRACKET CORRODED. REMOVED RUDDER YAW DAMPER ACTUATOR MOUNT BRACKET. INSTALLED NEW Y AW DAMPER ACTUATOR MOUNT BRACKET. (M) 2 L 7 2 4F A6WE 2002062400040 20020624 00040 WP 2002 6 24 GTIA020431 1 20020507 A 2742 95906 MOTOR DOUG DC9 DC932 3022066 WP HORIZ STAB MALFUNCTIONED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 ACY - PRIMARY TRIM HESITATES NOSE UP DIRECTION OCCURS USING BOTH CAPTAINS OR F/O'S YOKE SWITCHES AND USING SUIT CASE HAN DLES. REMOVED AND REPLACED PRIMARY TRIM MOTOR. OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4F A6WE 2002062400041 20020624 00041 WP 2002 6 24 GTIA020432 1 20020405 A 5523 TRIM TAB DOUG DC9 DC982 3022082 WP ELEVATOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND LEFT ELEVATOR CONTROL TAB BOTTOM SIDE HAS TWO OUTBOARD WEEP HOLES CORRODED. REMOVED LEFT ELEVATOR CONTROL T AB. INSTALLED CONTROL TAB ON LEFT ELEVATOR. (M) 2 L 7 2 4F A6WE 2002062400042 20020624 00042 EA 2002 6 24 SH52002F00001 1 20020426 A 3320 T31W2B28LELE LIGHT CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE CABIN MELTED B SH5R K NONE M OVER TEMP IN INSP/MAINT 1 NE 03 318FX 2940 5415 THE CABIN ACCENT LIGHTING BULBS BECAME EXTREMELY HOT AND MELTED/BURNED ITS PLASTIC SHEATHING. THIS CONDITION HAS BEEN N OTICED BEFORE BUT NOT TO THIS EXTENT. IN THE PAST THE SHEATHING BECAME DISCOLORED FROM THE HEAT. 2 L 7 2 4F 4 F RT A21EA E15NE 2002062400043 20020624 00043 SW 2002 6 24 SL32002F00000 1 20020425 A 5312 206033308103 BULKHEAD BELL 206 206L1 1182107 SW FUSELAGE CRACKED A SL3R K NONE O OTHER IN INSP/MAINT 1 NE 01 76LG 45534 CRACK FOUND ON FUSELAGE TO TAILBOOM BULKHEAD AT UPPER RIGHT BOLT HOLE - STATION 230.76 INSTALLED NEW BULKHEAD. 1 G 7 1 3U H2SW 2002062400044 20020624 00044 WP 2002 6 24 TM92002F00000 1 20020514 A 2432 GE50C BATTERY LKHEED 188 188A 5262602 WP MAIN DISCHARGED I TM9B K NONE L NO TEST IN INSP/MAINT 1 GL 23 436HA 1043 (LEAD ACID BATTERY) IN CRUISE, ENROUTE LOST (A) BUS IN FLIGHT. LOST ALL RADIOS, BOTH COMMS AND BOTH NAVS. OVERWEIGHT L ANDING. RESET ALL MAIN FEEDER C/BS. OPS CHECKED GOOD ON GROUND RUN-UP. REMOVED AND REPLACED MAIN AIRCRAFT BATTERY CON NECTOR, OPS CHECKED GOOD COMPLIED WITH ONE - 119C, NO DEFECTS NOTED. 2 L 7 4 4T RT 4A22 2002062400045 20020624 00045 NM 2002 6 24 TSAA0251140 1 20020520 A 5311 6546535 FRAME BOEING 737 7372M6C 1384708 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 46847 21809 FOUND CRACK ON THE FRAME AT BS 480 ABOVE STRINGER 17R. CUT OUT AND REMOVED DAMAGED PORTION OF FORMED SECTION. VERIFIED CUTOUT WITH HFEC. DETERMINED FROM TABLES III, IV, AND V, THE NUMBER OF FASTENERS AND FASTENER ROWS REQUIRED. FABRICAT ED REPAIR PARTS FROM MATERIALS SPECIFIED IN TABLE 1. APPLIED ALODINE AND BMS10-11 TYPE 1 PRIMER TO ALL BARE ALUMINUM. INSTALLED REPAIR PARTS MAKING A FRAYING SURFACE SEAL AND FASTENERS WET WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW WITH SRM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002062400046 20020624 00046 WP 2002 6 24 GTIA020446 1 20020424 A 7830 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP THRUST REVERSER CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND ENGINE NR 1 T/R INTERLOCK MECH SUPPORT BRACKET CRACKED. REMOVED BRACKET NR 1 ENGINE T/R INTERLOCK MECH. IN STALLED BRACKET ON NR 1 ENGINE T/R INTERLOCK MECH. (M) 2 L 7 2 4F A6WE 2002062400047 20020624 00047 WP 2002 6 24 GTIA020447 1 20020413 A 5230 SUPPORT FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND MID LOWER CARGO DOOR HAS CRACK AT FORWARD UPPER BRACKET SUPPORT FITTING. REMOVED FORWARD UPPER BRACKET SUPP ORT FITTING. DRILLED UP AND LOCATED NEW FITTING. INSTALLED FITTING. (M) 2 L 7 2 4F A6WE 2002062400048 20020624 00048 WP 2002 6 24 GTIA020449 1 20020406 A 2797 WIRE DOUG DC9 DC982 3022082 WP ELEVATOR BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND LEFT ELEVATOR POSITION SENSOR FAILS DFDR TEST, OCTAL DISPLAY DOES NOT CHANGE. T/S FOUND 2 WIRES BROKEN. RE PAIRED BROKEN WIRES. (M) 2 L 7 2 4F A6WE 2002062400049 20020624 00049 WP 2002 6 24 GTIA020450 1 20020502 A 5320 CHANNEL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - E/E BAY COMPARTMENT AT STA Y 16 INCHES BY 33 INCHES -2=11 SUPPORT CHANNEL CRACKED. REMOVED CHANNEL. FABRICATED N EW DOUBLER. INSTALLED CHANNEL. (M) 2 L 7 2 4F A6WE 2002062400050 20020624 00050 WP 2002 6 24 GTIA020467 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT FS 180, X13 TO X38. REMOVED FLOOR SUPPORT. FABRICATED NEW FL OOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062400051 20020624 00051 WP 2002 6 24 GTIA020472 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 218, X13 TO X7. REMOVED CORROSION. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062400052 20020624 00052 WP 2002 6 24 GTIA020473 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 218, -X12. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED NEW FITTIN G. INSTALLED FITTING. (M) 2 L 7 2 4F A6WE 2002062400053 20020624 00053 WP 2002 6 24 GTIA020474 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 210 -12. REMOVED CORROSION. REMOVED FLOOR SUPPORT. FORMED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062400054 20020624 00054 WP 2002 6 24 GTIA020475 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 200, -X9.5 TO -X46. REMOVED CORROSION. REMOVED FLOOR SUPPO RT. FABRICATED, INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062400055 20020624 00055 WP 2002 6 24 GTIA020476 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT FS 161 TO 199, -X44. REMOVED FLOOR SUPPORT. FABRICATED NEW F LOOR SUPPORT AT STATION 161-199. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062400056 20020624 00056 NM 2002 6 24 TSAA0252137 1 20020513 A 5270 PROXIMITY SWITCH BOEING 737 7372S5C 1384499 NM PAX DOOR INOPERATIVE A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 DURING CLIMB, OUT THE CABIN RATE OF CLIMB WAS 1750 FPM WITH BOTH OUTFLOW VALVES CLOSED AND ALL DOOR LIGHTS. UNABLE TO P RESSURIZE THE CABIN, THE AIRCRAFT RETURNED TO HNL FOR MAINTENANCE WITH NO FURTHER INCIDENT. MAINTENANCE PERSONNEL FOUND THAT THE FORWARD ENTRY DOOR WAS NOT SECURED. THE DOOR PROXIMITY SWITCHES WERE CLEANED AND INSPECTED AND TOP AFT LATCH CAM FITTING WAS ADJUSTED IAW THE MM. OPERATIONAL CHECK OF THE DOOR AND PRESSURIZATION CHECK OF THE AIRCRAFT WERE GOOD A ND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002062400057 20020624 00057 WP 2002 6 24 GTIA020477 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT HAS CORROSION AT FS 188 AND 197, UNDER HAT CHANNEL -X54. REMOVED FLOOR SUP PORT. INSTALLED FLOOR SUPPORT. PART WAS FABRICATED. (M) 2 L 7 2 4F A6WE 2002062400058 20020624 00058 NM 2002 6 24 TSAA0253138 1 20020513 A 5330 6546595 SKIN BOEING 737 7372S5C 1384499 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 FUSELAGE SKIN CRACKED AT BS 275 STRINGER 15L. TRIMMED OUT THE CRACK MAINTAINING A .5 INCH MINIMUM RADIUS. HFEC INSPECT ED CUT OUT. FABRICATED REPAIR PLATE FROM 2024T3 CLAD. FINISHED ALL BARE ALUMINUM WITH ALODINE AND PRIMER. INSTALLED T HE REPAIR PLATE WITH THE FASTENERS. MAKING THE FRAYING SURFACES SEAL. REPAIR COMPLETED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002062400059 20020624 00059 WP 2002 6 24 GTIA020478 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 200, -46 TO -X57. REMOVED CORROSION FROM FLOOR SUPPORT. FA BRICATED NEW PART. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062400060 20020624 00060 NM 2002 6 24 TSAA0253139 1 20020513 A 5330 6547989 SKIN BOEING 737 7372S5C 1384499 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 FOUND A 4 INCH CRACK AT BS 780 STRINGER 15R. TRIMMED OUT CRACK, MAINTAINING A .5 INCH MINIMUM RADIUS AND 2D EDGE MARGIN FROM FASTENERS. HFEC INSPECTED THE CUTOUT. FABRICATED REPAIR .040 INCH AND .050 INCH FILLER AND .050 INCH DOUBLER FRO M 2024-T3 CLAD. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-11 TYPE 1 PRIMER. INSTALLED REPAIR PAR TS WITH FASTENERS IDENTIFIED ON FIGURE 1. SHIMMED ALL GAPS GREATER THAN .01 INCHES UP TO A MAX OF .04 INCHES PRIOR TO F ASTENERS INSTALLATION. INSTALLED REPAIR PARTS WITH BMS 5-95 SEALANT. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW E CO 3257R2. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002062400061 20020624 00061 WP 2002 6 24 GTIA020479 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT FS 237, X13 TO -X15.5. REMOVED CORROSION ON FLOOR SUPPORT. RE MOVED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062400062 20020624 00062 NM 2002 6 24 TSAA0253141 1 20020513 A 5730 6545408 SKIN BOEING 737 7372Y5 1384554 NM RT WING WORN A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 39494 24031 FOUND SKIN WORN THROUGH ON THE RIGHT LEADIN EDGE LOWER WING SKIN SURFACE AT FS 413. CUT OUT DAMAGED LEADING EDGE FILLER AND SKIN. FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED THE REPAIR PARTS WITH FASTENERS. APPLIED BMS 5-95 S EALANT TO THE MATING SURFACES. COMPLETED REPAIR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4U RT A16WE 2002062400063 20020624 00063 NM 2002 6 24 TSAA0253142 1 20020515 A 5730 6573746 SKIN BOEING 737 7372Y5 1384554 NM LT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 39494 24031 FOUND CORROSION ON THE LEFT HAND OUTBOARD WING MAIN BOX UPPER SKIN AT WBL 71.24, STR 5, 7 AND WBL92.5 STR 1, 5. BLENDED OUT CORROSION AT A 10:1 RATIO MINIMUM PER SRM. ULTRASOUND INSPECTED TO ENSURE NO REMAINING CORROSION. HFEC AFFECTED F ASTENER HOLE BORE FOR CRACK DETECTION. INSPECTED WING SURFACE USING 10X VISUAL. SHOT PEENED WING SURFACE PER OHM. REP LACED REMOVED FASTENERS WITH .0312 INCH OVERSIZE TENSION HEAD HI-LOKS. INSTALLED FASTENERS WITH BMS 5-95 SEALANT IN TRA NSITION FIT HOLES AND REFINISHED PER SRM IAW ECO. 2 L 7 2 4U RT A16WE 2002062400064 20020624 00064 WP 2002 6 24 GTIA020480 1 20020321 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA SEAT TRACK CORRODED AT FS 200 TO 225 -X44. REMOVED CORROSION. REMOVED SEAT TRACK SDT 20 0 TO 246 -X44. DRILLED AND LOCATED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2002062400065 20020624 00065 CE 2002 6 24 UG82002F00001 1 20020603 A 2722 41011120107 ACTUATOR CESSNA 750 750 2076810 CE RUDDER STICKING A UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 5113 7500013 UPPER RUDDER CHANNEL (B) FAILED DURING PREFLIGHT. FOUND UPPER RUDDER ACTUATOR INTERMITTENTLY STICKING. REMOVED AND REP LACED UPPER RUDDER ACTUATOR. OPERATIONAL CHECK IS GOOD. AIRCRAFT RELEASED FOR FLIGHT. 2 L 7 2 4J RT T00007WI 2002062400066 20020624 00066 GL 2002 6 24 UG82002F00002 2 20020516 A 7200 23057202 ENGINE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RIGHT OUT OF TOLERANCE A UG8A O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 5116 7500019 RIGHT ENGINE OIL PRESSURE OUT OF LIMITS, HI/RED 106 PSI AT 80-90 KTS. ENGINE INTERNAL BEARING SEAL AIR LEAKAGE WHICH MA Y OCCUR AS ENGINE APPROACHES ITS MIDLIFE INSPECTION. VISUALLY INSPECTED ENGINE OIL FILTER BYPASS BUTTON. PERFORMED TAK EOFF POWER RUN UP. FOUND OIL PRESSURE WITHIN LIMITS. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2002062400067 20020624 00067 CE 2002 6 24 UG82002F00003 1 20020522 A 2910 671774120 B-NUT CESSNA 750 750 2076810 CE HYDRAULIC LINE LOOSE E UG8A O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 23 5114 2795 7500017 TOTAL LOSS OF (A) HYDRAULIC SYSTEM FLUID. B-NUT ON LINE ASSEMBLY LOOSENED AND BACKED OFF DUE TO INCORPORATION OF SB. F URTHER INSTALLATIONS OF THIS BULLETIN HAVE BEEN TEMPORARILY TERMINATED BY MFG. SECURED B-NUT, SERVICED (A) HYDRAULIC S YSTEM. SERVICED EMERGENCY GEAR AND BRAKE BOTTLE WITH NITROGEN PER MFG MM. 2 L 7 2 4J RT T00007WI 2002062400068 20020624 00068 WP 2002 6 24 GTIA020481 1 20020313 A 7601 SYNCRONIZER DOUG DC9 DC981 3022081 WP NR 1 ENGINE FAILED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 806NK 48051 FTW - NR 1 ENGINE AT LOW LIMIT WOULD COMPLETELY UNSPOOL. PERFORMED TEST OF ENGINE SYNCHRONIZER SYSTEM. SYSTEM FAILED T EST, NO SYNCHRONIZATION OF ENGINE. PERFORMED ADJUSTMENT SYNCHRONIZER ENGINE ACTUATOR. SERVICED FUEL CONTROL UNIT ACCEL ERATION CHAMBER WITH SILICON. DRAINED FUEL CONTROL MOISTURE TRAP. OPS CHECK FAILED STEP 9. REMOVED ENGINE SYNCHRONIZE R ACTUATOR. INSTALLED SERVICEABLE ENGINE SYNCHRONIZER. (M) 2 L 7 2 4F A6WE 2002062400069 20020624 00069 NE 2002 6 24 UHL2002F00001 2 20020509 A 7200 GECT75A2 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT FAILED A UHLA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NE 03 158SD 340A158 AFTER TAKE OFF, SURGED BETWEEN 40 PERCENT TO 70 PERCENT, HAPPENED 3 TIMES. PILOT DECLARED EMERGENCY RETURNED TO AIRPORT . MECHANIC CHECKED BIRDCATCHER AND INLETS FOR DAMAGE. PERFORMED OPS CHECK ON GROUND AND COULD NOT DUPICATE. TOOK A GP A READING AND READINGS WERE WITHIN LIMITS. PERFORMED TEST FLIGHT. TEST FLIGHT WAS SATISFACTORY. COULD NOT DUPLICATE I NITIAL FAULT. ESTABLISHED NEW DDT. DUE TO HIGH ITT MARGIN, PLACED AIRCRAFT ON DERIVITIVE POWER. REMOVED ENGINE IN BED DUE TO HIGH ITT MARGIN. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002062400070 20020624 00070 NM 2002 6 24 UIE2002F00000 1 20020607 A 5750 65B1706870 FLAP TRACK BOEING 747 747341 13848AM NM WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 DURING CURRENT (D) CHECK AT SIAEC, THE NR 5 FLAP TRACK O/B LOWER FLANGE IN THE MID SECTION WAS FOUND WITH LEVEL 1 CORROS ION FOR APPROX 10 INCHES. CORROSION MACHINED OUT AND BLENDED MAINTAINING A 100 TO 1 BLEND RATIO TO ENSURE A SMOOTH FLAT SURFACE. AREA MAGNETIC PARTICLE INSPECTED TO ENSURE NO CRACKING DURING PROCESS. NO DEFECTS FOUND. AREA MEASURED AND RECORDED. 2 L 7 4 4F RT A20WE 2002062400071 20020624 00071 NM 2002 6 24 UIE2002F00001 1 20020607 A 5311 FRAME BOEING 747 747341 13848AM NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 51111 9549 23395 DURING CURRENT (D) CHECK, SIAEC, FOUND STA 440L FRAME CRACKED AT CUTOUT OF STR 10A. CRACK LENGTH .1875. STOP DRILLED C RACK, FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM. FRAME IS SUBJECT TO RECURRENT INSPECTIONS. 2 L 7 4 4F RT A20WE 2002062400072 20020624 00072 WP 2002 6 24 GTIA020482 1 20020320 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FORWARD ENTRY AREA FLOOR SUPPORTS AT R1 DOOR AREA STATION 160 AND 200 -X52 HAVE CORROSION. REMOVED CORROSION. RE MOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062400073 20020624 00073 EU 2002 6 24 UO22002F00010 1 20020425 A 3500 033720002XXX LINE ISRAEL GALAXY GALAXY 4500307 EU OXYGEN SYSTEM DAMAGED B UO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 108GX 046 FOUND NUMEROUS SMALL NICKS AND DENTS IN THE FLARES OF SOME OF THESE TUBES. AFTER PERFORMING CLEANING OF THESE VENDOR SU PPLIED OXYGEN CLEAN TUBES, INDICATIONS WERE THAT SOME OF THE TUBES WERE DIRTY FROM THE VENDOR. 2 L 7 2 4F RT A53NM 2002062400074 20020624 00074 EU 2002 6 24 UO22002F00011 1 20020213 A 3500 FITTING ISRAEL GALAXY GALAXY 4500307 EU OXYGEN SYSTEM OVERTORQUED B UO2R K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 108GX 046 WHILE INSPECTING (SN 046) FOUND THAT THE 2ND O2 BOTTLE INSTALLATION PLUMBING CAN NOT BE INSTALLED ACCORDING TO STC ST097 48SC. THIS STC CALLS OUT MAX TORQUES ON THE PLUMBING FITTINGS. THE FITTINGS LEAK AT MAX TORQUES EVEN WITH THE TAPE ALL OWED INSTALLED ON THE FITTING THREADS. THESE FITTINGS HAVE BEEN OVER TORQUED TO ACHIEVE NO LEAKS. I BELIEVE THAT ALTHO UGH THESE LINES ARE STAINLESS STEEL, THE OVERTORQUE SITUATION MAY CAUSE FAILURE. NO SOLUTION TO DATE. 2 L 7 2 4F RT A53NM 2002062400075 20020624 00075 WP 2002 6 24 GTIA020483 1 20020320 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND CABIN RIGHT FORWARD GALLEY AFT OF SERVICE DOOR (G2) FORWARD SIDE OF AFT BULKHEAD AT FLOOR HAS CORROSION. RE MOVED DAMAGED AREA. FABRICATED INNER SKIN. INSTALLED INNER SKIN. (M) 2 L 7 2 4F A6WE 2002062400076 20020624 00076 WP 2002 6 24 GTIA020484 1 20020320 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - CABIN RIGHT FORWARD GALLEY AFT OF SERVICE DOOR (G-2) LOWER SIDE AT FLOOR HAS CORROSION. REMOVED CORROSION. LOCAT ED AND DRILLED PARTS. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2002062400077 20020624 00077 EU 2002 6 24 UO22002F00012 1 20020501 A 1430 FASTENER ISRAEL GALAXY GALAXY 4500307 EU PWA 306 PW306B NE FUSELAGE TANK MISINSTALLED A UO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 290GA 26 049 TWO FASTENERS IN THE FUSELAGE TANK APPEAR TO BE MISINSTALLED WITH NO EDGE DISTANCE. THEY ALSO DUE NO SIT FLUSH. THESE FASTENERS ARE ACCESSED THRU THE UPPPER FUSELAGE PANELS 252 AR AND 250AT, AND ARE ONE ON EACH SIDE OF THE FAR UPPER CORNE RS OF THE TANK. 2 L 7 2 4F 4 F RT A53NM E35NE 2002062400078 20020624 00078 EA 2002 6 24 UQM2002F00001 2 20020524 A 8530 AEL65102101 CYLINDER PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA RT ENGINE FAILED E UQMA K NONE O OTHER IN INSP/MAINT 1 CE 01 900TS 1418 277405429 L1061748 CYLINDER WAS INSTALLED USING NEW RINGS AND GASKET SET FROM ECI ALSO. REMOVED CYLINDER DUE TO LOW COMPRESSION AND EXHAUS T STAINS AROUND THE EXHAUST AREA. FOUND THAT HEAD WAS CRACKED BETWEEN BOTH SPARK PLUG HOLES AND BY THE EXHAUST SEAT, WH ICH IN RETURN BURNED A HOLE NEXT THE EXHAUST FLANGE. 1 L 7 2 3O 3 O 1A10 1E4 2002062400079 20020624 00079 WP 2002 6 24 GTIA020485 1 20020320 A 5320 ATTACH ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND CRACK ON FLOORBOARD ATTACK ANGLE BETWEEN L26 AND L27 STATION 712. REMOVED ANGLE FOM WELDED. INSTALLED ANGL E. (M) 2 L 7 2 4F A6WE 2002062400080 20020624 00080 NM 2002 6 24 USA2002F00041 1 20020520 A 2450 CONTROL UNIT BOEING 767 767201 1385125 NM ELECTRICAL LOAD MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 17 650US 59344 23902 (ELCU) ENROUTE, CREW RECEIVED THE EICAS MESSAGE (C HYD PRIM 1) AND THE LOW PRESSURE LIGHT ILLUMINATED. FLIGHT RETURNED AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CENTER NR 1 ACMP AND THEN THE TIME DELAY RELAY. ON A SUB SEQUENT FLIGHT, THE PROBLEM REAPPEARED. THE ELECTRICAL LOAD CONTROL UNIT WAS REPLACED. 2 L 7 2 4F RT A1NM 2002062400081 20020624 00081 WP 2002 6 24 GTIA020486 1 20020320 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FRAME AT 731 BETWEEN LONGERON L29 AND R29 HAS CORROSION ON INTERCOSTAL 2 PLACES. REMOVED CORROSION ON FLOOR SUPPORT. REMOVED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002062400082 20020624 00082 NM 2002 6 24 USA2002F00042 1 20020604 A 5242 6522216113 DOOR BOEING 737 7373B7 1384580 NM E/E BAY UNLATCHED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 390US 23312 SHORTLY AFTER TAKEOFF, ENROUTE, CAPTAIN REPORTED A LOUD NOISE COMING FROM UNDER THE INSTRUMENT PANEL. HE ALSO REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. FLIGHT TAXIED TO GATE UNDER OWN POWER. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FORWARD E AND E COMPARTMENT DOOR OPEN. CLOSED AND SECURED DOOR. VERIFIED PROPER OPERATION OF BOTH E AND E COMPARTMENT DOOR WARNING LIGHTS. WARNING SYSTEM CHECKS GOOD. 2 L 7 2 4F RT A16WE 2002062400083 20020624 00083 NM 2002 6 24 USA2002F00043 1 20020602 A 5230 10608214 SEAL BOEING 737 7373B7 1384580 NM AFT CARGO DOOR TORN A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 19 534AU 24516 ENROUTE, THE AIRCRAFT LOST CABIN PRESSURIZATION AS MASTER CAUTION WARNING LIGHT ILLUMINATED. AUTO, STANDBY AND MANUAL P RESSURIZATION MODES WOULD NOT STOP CABIN FROM CLIMBING. CREW DONNED OXYGEN MASKS, ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND DECENDED. CREW DECLARED AN EMERGENCY AND THE CABIN WAS PREPPED FOR USE OF THE OXYGEN MASKS. OXYGEN MAS KS WERE DEPLOYED AND THE FLIGHT DIVERTED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFT CARGO DOOR SEAL AND THE MAIN ENTRANCE DOOR SEAL (PN BAC 1521-522). 2 L 7 2 4F RT A16WE 2002062400084 20020624 00084 NM 2002 6 24 USA2002F00044 1 20020601 A 3210 LANDING GEAR BOEING 737 737301 1384611 NM MAINS OUT OF RIG A USAA O OTHER J WARNING INDICATION LD LANDING 1 EA 19 337US 23235 IN PREPARATION FOR LANDING, CREW EXPERIENCED A LANDING GEAR INDICATION PROBLEM. GREW RECEIVED 3 GREEN AND 3 RED LANDING GEAR LIGHTS WHEN SELECTING GEAR DOWN. CREW ACCOMPLISHED GO AROUND AND RETRACTED GEAR. ALL INDICATIONS NORMAL. PLACED GEAR HANDLE BACK DOWN AND RECEIVED NORMAL INDICATION OF 3 GREEN AND NO RED LIGHTS. FLIGHT LANDED WITHOUT FURTHER INCID ENT. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE LANDING GEAR CONTROL SYSTEM OUT OF RIG. RERIGGED LANDING GEAR PE R MM. PERFORMED GEAR SWING. OPERATIONAL CHECK NORMAL. LIGHT INDICATION CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2002080500123 20020805 00123 2002 8 5 GLBA2002088 4 20020622 A 3442 6227580041 CONTROL PANEL BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT FAILED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 245GL UE245 WEATHER RADAR STOPPED WORKING. DIVERTED AIRCRAFT TO CYS. REMOVED AND REPLACED WEATHER RADAR CONTROL PANEL, OPS CHECKED GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2002062400085 20020624 00085 NE 2002 6 24 USA2002F00045 2 20020603 A 7230 US35848 ANNULAR FILLER BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE SEPARATED A USAA F A ACTIVATE FIRE EXT. UNSCHED LANDING F E J FLT CONT AFFECTED VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 603AU 20822 22198 AT ROTATION, FLAMES WERE SEEN COMING FROM THE RIGHT ENGINE. AT APPROXIMATELY 300 FEET, THE CREW HEARD A NOISE, FELT THE AIRCRAFT YAW, AND RECEIVED WARNING INDICATIONS. EGT ON THE RIGHT ENGINE READ 1000. CREW ACTIVATED ONE FIRE BOTTLE. F LIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. (SET 19 MINUTES) THE ENGINE WAS REPLACED. ENGINE WAS FODDED BY AN ANNULUS FILLER SEPARATING FROM THE NR 22 POSITION. 2 L 7 2 4F 4 F RT A2NM E12EU 2002062400086 20020624 00086 NM 2002 6 24 USA2002F00047 1 20020601 A 7722 CONNECTOR BOEING 737 737301 1384611 NM NR 2 ENGINE FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 575US 23740 AFTER TAKEOFF, THE NR 2 ENGINE EGT RED LIGHT ILLUMINATED AS EGT WENT TO 1,067 DEGREES. CREW REDUCED THROTTLE AND EGT RE TURNED TO NORMAL. ALL OTHER ENGINE INDICATIONS WERE WITHIN NORMAL LIMITS. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 2 ENGINE EGT HARNESS CONNECTION AT FORWARD JUNCT ION NR 9 UPPER/LOWER HARNESS LOOSE. REMOVED AND REPLACED JUNCTION (PN CA 152-01) AND CONNECTOR. PERFORMED ENGINE RUN. ENGINE NR 2 EGT CHECKS GOOD. 2 L 7 2 4F RT A16WE 2002062400087 20020624 00087 NM 2002 6 24 USA2002F00048 1 20020610 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM EXIT SIGNS DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 612AU 27124 FOUND EXIT IDENTIFIERS AT DOORS L1, R2, AND R4 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. 2 L 7 2 4F RT A2NM 2002062400088 20020624 00088 WP 2002 6 24 GTIA020487 1 20020318 A 5320 CLIP DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND AFT PIT CABIN FLOOR STATION 1271-1309 PLUS X17, STRAP AT BOTTOM OF FLOORBEAMS CORRODED. STRAP CLIP FOUND TO BE CORRODED OUT OF LIMITS. REMOVED CLIP. FABRICATED NEW CLIP. INSTALLED CLIP. (M) 2 L 7 2 4F A6WE 2002062400089 20020624 00089 NM 2002 6 24 USA2002F00049 1 20020607 A 3350 8731002511REV15 SIGN BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 631AU 27809 FOUND L1 EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2 L 7 2 4F RT A2NM 2002062400090 20020624 00090 NM 2002 6 24 USA2002F00050 1 20020606 A 3350 SIGN BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 613AU 27144 FOUND LEFT 1 DOOR EXIT IDENTIFIER, INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER ASSEMBLY. 2 L 7 2 4F RT A2NM 2002062400091 20020624 00091 NM 2002 6 24 USA2002F00051 1 20020604 A 3350 SIGN BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 FOUND RIGHT 4 DOOR EXIT IDENTIFIER, INOPERATIVE. MAINTENANCE REPLACED THE ASSEMBLY. 2 L 7 2 4F RT A2NM 2002062400092 20020624 00092 NM 2002 6 24 USA2002F00052 1 20020605 A 3260 188915 SENSOR BOEING 737 737401 1384701 NM MLG CUT A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 408US 23878 AFTER TAKEOFF, AT APPROXIMATELY 100 FEET, CAPTAIN ATTEMPTED TO RAISE THE LANDING GEAR BUT THE GEAR HANDLE FAILED TO RETR ACT. CAPTAIN ATTEMPTED TO RAISE THE LANDING GEAR BUT THE GEAR HANDLE FAILED TO RETRACT. CAPTAIN CONTINUED FLIGHT TO 5, 000 FEET AND STILL WAS UNABLE TO RETRACT THE GEAR. DECISION WAS MADE TO RETURN TO FIELD, WHERE THE FLIGHT LANDED WITHOU T FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED, REPLACED AND ADJUSTED THE S106 AIR SAFETY SENSOR. ACCOMPLISHED GEAR SWING. OPERATIONAL CHECK NORMAL. ACCOMPLISHED TEST HOP FOR LANDING GEAR. TEST HOP CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2002062400093 20020624 00093 NM 2002 6 24 USA2002F00053 1 20020602 A 3260 189929 SENSOR BOEING 737 737301 1384611 NM MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 300AU 23228 AFTER TAKEOFF, CREW WAS UNABLE TO MOVE THE LANDING GEAR SELECTOR HANDLE PAST THE OFF POSITION TO RETRACT THE GEAR. CRE W ALSO TRIED THE GEAR OVER RIDE WITH NO HELP. DUE TO THE TAKEOFF WARNING HORN SOUNDING AFTER THE FLAPS WERE FULLY RETRA CTED, CREW THINKS THE AIR/GROUND SENSING SYSTEM HAS FAILED. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDEN T. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE S106 AIR SAFETY SENSOR PER MM. SYSTEM OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002062400094 20020624 00094 NM 2002 6 24 USA2002F00054 1 20020603 A 3260 806002 CIRCUIT BOARD BOEING 737 737401 1384701 NM LOGIC CARD FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 408US 23878 AFTER TAKEOFF, CREW COULD NOT GET THE LANDING GEAR SELECTOR HANDLE TO MOVE PAST THE OFF POSITION TO RAISE THE GEAR. CRE W FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND NOTED THAT THE TAKEOFF WARNING HORN DID NOT SOUND WITH THE FLAPS UP. HOWEVER, THERE WAS A SIGNIFICANT VIBRATION AND RUMBLING NOISE WHICH LED THE CAPTAIN TO LEAVE THE GEAR EXTENDED AND RETU RN TO FIELD. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE M001 AIR SENSE LOGIC CARD AND R276 AIR SENSE RELAY. OPERATIONAL CHECK NORMAL PER MM. ALSO, CHECKED AND CLEAN S106 AIR SAFETY SENSOR (PN 1-899-29) AND INSPECTED TELEFLEX CABLE FOR BINDING ON RIGHT MAIN LANDING GEAR. ALL CHECKED NORMAL. L 2 L 7 2 4F RT A16WE 2002062400095 20020624 00095 NM 2002 6 24 USA2002F00055 1 20020609 A 3260 189929 UPLOCK SENSOR BOEING 737 737301 1384611 NM MLG FAULTY A USAA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 19 575US 23740 ENROUTE, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND REP ORTED THE GEAR OPERATED NORMALLY. LIGHT EXTINGUISHED WHEN GEAR HANDLE WAS PLACED TO DOWN POSITION. FLIGHT CONTINUED AN D LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT PROBLEM TO THE LEFT MAIN LANDING GEAR UPLOCK SENSOR. REMOVE D AND REPLACED UPLOCK SENSOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002062400096 20020624 00096 NM 2002 6 24 USA2002F00056 1 20020609 A 2131 7638101 CONTROLLER BOEING 737 737301 1384611 NM CABIN PRESSURE FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 591US 23936 AFTER DEPARTURE, CLIMBING THROUGH 11,000 FEET, CAPTAIN ADVISED THE CABIN PRESSURE BEGAN TO CLIMB AND COULD NOT BE CONTRO LLED. AIRCRAFT CONTINUED TO DEPRESSURIZE WITH CAPTAINS SLIDING WINDOW APPEARING NOT TO SEAL WITH AN AIRLEAK. CREW DECL ARED AN EMERGENCY AND RETURNED TO FIELD. UPON LANDING, AIRCRAFT DID NOT APPEAR TO FULLY DEPRESSURIZE. MAINTENANCE PRES SURIZED AIRCRAFT TO 3.5 PSI ON GROUND IN MANUAL MODE AND INSPECTED AIRCRAFT FOR LEAKS. NO LEAKS FOUND AND NO SQUEALING IN CABIN HEARD. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER PER MM. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002062400097 20020624 00097 CE 2002 6 24 UVV2002F00000 1 20020419 A 5730 765731220 PANEL RKWELL NA265 NA26580 7630108 CE GE CF700 CF700* 30010 NE RIGHT WING CORRODED B UVVR K NONE O OTHER IN INSP/MAINT 1 CE 03 910BH 38054 FOUND OVER FLAP PANEL UNDERSIDE CORRODED COMPLETELY THROUGH SKIN TO HONEYCOMB SUBSTRUCTURE. AREA NOT READILY INSPECTABL E DUE TO VELCRO APPLIED OVER AREA TO ACT AS CHAFE STRIPS FOR FLAP UPPER SURFACE. RECOMMEND CLOSE VISUAL INSPECTION OF A REA DURING 150 HOUR INSPECTION. 2 L 7 2 4F 4 F A2WE E7EA 2002062400098 20020624 00098 NM 2002 6 24 V3E2002F00000 1 20020425 A 3210 69636333 BOLT BOEING 727 727200 138407E NM RT MLG SHEARED A V3EY K NONE O OTHER IN INSP/MAINT 1 WP 33 876AA 10602 21388 BOLT ASSEMBLY - SIDE SPINDLE WAS FOUND WITH HEAD OF BOLT ASSEMBLY SHEARED OFF AND THE WAS BACKING OUT AFTER TOWING THE A IRCRAFT FROM STORAGE TO THE MAINTENANCE HANGAR. HEAD OF BOLT WAS FOUND ON FLOOR, THERE WAS NO MAINTENANCE BEING PERFORM ED ON THE LANDING GEAR. 2 L 7 3 4F RT A3WE 2002062400099 20020624 00099 SO 2002 6 24 VDN2002F00000 1 20020522 A 8120 6005104C HOUSING PIPER PA28 PA28R201T 7102813 SO CONT O360 TSIO360* 17025 SO TURBOCHARGER CRACKED E VDNA K NONE O OTHER IN INSP/MAINT 1 SW 09 3485M 28R7803172 DURING ANNUAL INSPECTION, THE TURBOCHARGER HOUSING PART NUMBER COULD NOT BE DETERMINED. THE TURBO HOUSING WAS REMOVED T O CHECK APPLICABILITY WITH AD. IT WAS DETERMINED THAT THIS TURBO HOUSING DOES NOT HAVE TO BE INSPECTED PER PARAGRAPH (J ) OF AD DUE TO PART NUMBER, HOWEVER, THE HOUSING WAS FOUND TO BE CRACKED. REPLACED CRACKED TURBO HOUSING WITH NEW ITEM (PN CF600510-0004D). SUGGEST INSPECTING THIS HOUSING DURING ANNUAL INSPECTIONS REGARDLESS OF PART NUMBER. 1 L 7 1 3O 3 O 2A13 E9CE 2002062400100 20020624 00100 EU 2002 6 24 VJ32002F00032 1 20020507 A 3600 1U128006 PUMP GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA DRY AIR SHEARED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 01 862AF 159 85002 L2802448 METAL SHAFT SHEARED IN PUMP. REMOVED AND INSTALLED NEW PUMP, SYSTEM OPERATIONAL CHECKED NORMAL. PUMP SENT IN FOR WARRA NTY. 1 L 7 1 3O 3 O RT A49CE 1E4 2002062400101 20020624 00101 EA 2002 6 24 VJ32002F00033 2 20020506 A 8530 115TA601004 BAFFLE GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA NR 3 CYLINDER CRACKED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 01 862AF 98 85002 ENGINE BAFFLE CRACKED ON NUMBER 3 CYLINDER. PART REMOVED AND NEW BAFFLE INSTALLED. PART SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O RT A49CE 1E4 2002062400102 20020624 00102 EA 2002 6 24 VJ32002F00034 2 20020506 A 8530 115TA601004 BAFFLE GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA NR 3 CYLINDER CRACKED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 01 862AF 141 85002 L2802448A ENGINE BAFFLE CRACKED ON NUMBER 3 CYLINDER. PART REMOVED AND NEW BAFFLE INSTALLED. PART SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O RT A49CE 1E4 2002062400103 20020624 00103 EU 2002 6 24 VJ32002F00036 1 20020510 A 2913 BA010500 PUMP GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA HYDRAULIC SYS FAILED B VJ3R O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 865AF 31 85005 L2826448A IN FLIGHT, THE LANDING GEAR HYDRAULIC PUMP CIRCUIT BREAKER POPPED WITH THE GEAR UP, THE GEAR WAS LOWERED AND A SAFE LAND ING WAS MADE. AIRCRAFT WAS PLACED ON JACKS AND THE GEAR SYSTEM WAS OPERATIONAL CHECKED. WITH THE GEAR UP AND LOCKED TH E HYDRAULIC PUMP WOULD NOT SHUT OFF, A TAP TO THE UP LOCK ASSEMBLY SHUT THE PUMP OFF. UP LOCK ASSEMBLY WAS REMOVED AND INSTALLED A NEW UP LOCK ASSEMBLY. OPERATIONAL CHECK OF THE GEAR SYSTEM CHECKED NORMAL. UP LOCK ASSEMBLY WAS SENT IN FO R WARRANTY. 1 L 7 1 3O 3 O RT A49CE 1E4 2002062400104 20020624 00104 EU 2002 6 24 VJ32002F00038 1 20020516 A 3600 1U128006 PUMP GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA DRY AIR PUMP FAILED B VJ3R O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 865AF 51 85005 L2826448A IN FLIGHT, THE INSTRUMENT VACUUM SYSTEM FAILED. THE AIRCRAFT RETURNED TO MAINTENANCE AND AN INSPECTION OF THE SYSTEM FO UNDED THAT THE ROTOR HAD FROZEN UP AND THE SHAFT HAD SHEARED. PUMP WAS REMOVED AND A NEW PUMP INSTALLED. OPERATIONAL C HECK OF THE SYSTEM CHECKED NORMAL. PART SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O RT A49CE 1E4 2002062400105 20020624 00105 EU 2002 6 24 VJ32002F00039 1 20020520 A 2710 120A4403 ROD GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA AILERONS CHAFED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 863AF 98 85003 2802548A AILERON ROD RUBBING AILERON BELL CRANK. REMOVED ROD AND INSTALLED NEW ROD. CONTROL ASSEMBLY WAS SHIMMED TO CORRECT THE PROBLEM. 1 L 7 1 3O 3 O RT A49CE 1E4 2002062400106 20020624 00106 EU 2002 6 24 VJ32002F00040 1 20020520 A 2730 120A4441 ROD GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA ELEVATOR TRIM CHAFED A VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 863AF 98 85003 L2802548A ELEVATOR CONTROL ROD RUBBING AILERON CROSS OVER TUBE. REMOVED TUBE AND INSTALLED NEW TUBE. NEW SHIM PLATES INSTALLED, TO CORRECT PROBLEM. 1 L 7 1 3O 3 O RT A49CE 1E4 2002062400107 20020624 00107 2002 6 24 VJ32002F00041 4 20020520 A 3120 115EG7780 CLOCK GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA COCKPIT BROKEN B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 863AF 98 85003 L2802548A LEFT HAND STOP PIN BROKEN OFF. REMOVED AND REPLACED NEW CLOCK. 1 L 7 1 3O 3 O RT A49CE 1E4 2002062400108 20020624 00108 EU 2002 6 24 VJ32002F00042 1 20020515 A 2913 X030001 PUMP GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA HYD SYSTEM BURNED OUT B VJ3R O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 861AF 182 85001 L2802548A LANDING GEAR FAILED, WHEN THE GEAR WAS SELECTED TO THE UP POSITION AFTER TAKE OFF. THE GEAR WAS LOWER AND A SAFE LANDIN G WAS MADE. INSPECTION OF THE GEAR SYSTEM FOUND THAT THE MOTOR ON THE HYDRAULIC PUMP BURNED OUT. PUMP ASSEMBLY WAS REM OVED AND A NEW PUMP ASSEMBLY INSTALLED. LANDING GEAR CYCLED IAW MM. SYSTEMS OPERATIONAL CHECKED NORMAL. 1 L 7 1 3O 3 O RT A49CE 1E4 2002062400109 20020624 00109 EA 2002 6 24 VJ32002F00043 2 20020516 A 8530 115TA601003 BAFFLE GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA NR 1 CYLINDER CRACKED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 865AF 51 85005 L2856448A ENGINE BAFFLE CRACKED ON NUMBER 1 CYLINDER. PART REMOVED AND NEW BAFFLE INSTALLED. 1 L 7 1 3O 3 O RT A49CE 1E4 2002062400110 20020624 00110 EA 2002 6 24 VJ32002F00044 2 20020521 A 8530 115TA601003 BAFFLE GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA NR 1 CYLINDER CRACKED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 864AF 194 85004 L2826348A ENGINE BAFFLE CRACKED ON NUMBER 1 CYLINDER. PART REMOVED AND NEW BAFFLE INSTALLED. 1 L 7 1 3O 3 O RT A49CE 1E4 2002062400111 20020624 00111 EU 2002 6 24 VJ32002F00045 1 20020521 A 3600 IU128006 PUMP GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA VACUUM SYS FAILED B VJ3R A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 07 864AF 194 85004 L2826348A IN FLIGHT THE INSTRUMENT VACUUM SYSTEM FAIL. THE AIRCRAFT RETURNED TO MAINTENANCE AND AN INSPECTION OF THE SYSTEM FOUND ED THAT THE ROTOR HAD FROZEN UP AND THE SHAFT HAD SHEARED. PUMP WAS REMOVED AND A NEW PUMP INSTALLED. OPERATIONAL CHE CK OF THE SYSTEM CHECKED NORMAL. 1 L 7 1 3O 3 O RT A49CE 1E4 2002062400112 20020624 00112 EA 2002 6 24 VJ32002F00046 2 20020605 A 7414 4371 MAGNETO PIPER PA28 PA28181 7102807 SO LYC O360 O360A4M 41514 EA ENGINE INOPERATIVE A VJ3R O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 WP 07 9299B 69 2843116 ROUGH ENGINE ON GROUND RUN, A MAGNETO CHECK WAS PERFORMED AND THE LEFT MAGNETO HAD EXCESSIVE MAGNETO DROP. MAGNETO WAS REMOVED AND A REPAIRED MAGNETO INSTALLED. MAGNETO OPERATION CHECK OF THE ENGINE WAS PERFORMED AND CHECKED NORMAL. 1 L 7 1 3O 3 O 2A13 E286 2002062400113 20020624 00113 EA 2002 6 24 VJ32002F00047 2 20020523 A 8530 115TA601003 BAFFLE GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA NR 1 CYLINDER CRACKED A VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 863AF 97 85003 2802548A ENGINE BAFFLE CRACKED ON NR 1 CYLINDER. PART REMOVED AND NEW BAFFLE INSTALLED. PART SENT FOR WARRANTY. 1 L 7 1 3O 3 O RT A49CE 1E4 2002062400114 20020624 00114 NE 2002 6 24 VQM2002F00000 2 20020514 A 7320 324475522211 FUEL CONTROL BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A42 52043 NE LT ENGINE MALFUNCTIONED E VQMA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 NM 03 725MC 277 BB169 PILOT REPORTED LEFT ENGINE TORQUE WAS SLOW TO RESPOND THEN ACCELLERATED RAPIDLY. REPLACED BOTH FUEL CONTROL UNIT AND EN GINE DRIVEN FUEL PUMP (SUSPECTED POSSIBLE BEARING WASH-OUT). PERFORMED GROUND RUNS SATISFACTORY. 1 L 7 2 4T 4 T A24CE E4EA 2002062400115 20020624 00115 WP 2002 6 24 GTIA020489 1 20020324 A 5230 SKIN DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FORWARD CARGO DOOR AFT SIDE (NEAR LOCK MECH) CHAFED, GOUGED, AND INNER AND OUTER SKIN CRACKED. CUT OUT DAMAGE. F ABRICATED FILLER. FABRICATED DOUBLER. INSTALLED FILLER AND DOUBLER. (M) 2 L 7 2 4F A6WE 2002062400116 20020624 00116 CE 2002 6 24 WC72002F00001 1 20020409 A 7400 A3705 FILTER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE NOISE SHORTED B WC7R K NONE O OTHER IN INSP/MAINT 1 GL 25 355EJ 4659 5600255 THE IGNITION LIGHT WAS NOT ILLUMINATED WITH THE IGNITION SELECTED ON CAUSING THE PILOT TO RETURN TO THE AIRPORT SHORTLY AFTER TAKEOFF. THE FUSE TO THE RIGHT IGNITION CIRCUIT WAS FOUND BLOWN. TROUBLESHOOTING DETERMINED THAT THERE WAS A SHO RT IN THE RIGHT IGNITION CIRCUIT SOMEWHERE BETWEEN THE EXCITER BOX AND THE JUNCTION BOX IN THE TAIL COMPARTMENT. IT WAS DETERMINED THAT THE NOISE FILTER WAS INTERNALLY SHORTED. 2 L 7 2 4F 4 F RT A22CE E25EA 2002062400117 20020624 00117 CE 2002 6 24 WIB2002F00003 1 20020426 A 2133 660020756 RELIEF VALVE LEAR 35 31A 5170531 CE GARRTT TFE731 TFE731* 01518 WP CABIN PRESSURE MALFUNCTIONED B WIBR K NONE O OTHER IN INSP/MAINT 1 SW 11 78PR 090 AIRCRAFT WOULD OPEN SAFETY VALVE AT 9.4, FOUND PRESSURE DIFFERENTIAL RELIEF VALVE OPENING TOO SOON. 2 L 7 2 4F 4 F RT A10CE E6WE 2002062400118 20020624 00118 WP 2002 6 24 WRLA200210 1 20020419 A 2752 AYG70305505 CONTROL VALVE DOUG DC10 DC1030 3023501 WP OUTBOARD FLAPS FAILED A WRLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 14075 46922 AFTER TAKEOFF OB FLAP FAILED TO RETRACT-CONFIRMED BY FLAP INDICATIONS TAPES AND PHYSICAL INSP. COMMENCING FUEL DUMP TO RETURN, FLAPS RETRACTED ON THERE OWN AND OPERATED NORMALLY FOR LANDING. DETERMINED LT OB FLAP AND RT OB FLAP ONE DID RE MAIN EXTENDED AFTER HANDLE WAS POSITIONED TO RETRACT POSITION. REMOVED ALL REAR SPAR LWR PANELS AND FLAP HINGE TO FLAP CONTROL VALUE ASSYS. RESCUED PILOT OVERRIDE CLAPPER CABLE. SUSPECT POSSIBLE OB FLAP CONTROL VALUE LT OR RT MALFUNCTION . REMOVED AND REPLACED LT AND RT OUTBOARD CONTROL VALUE ASSEMBLIES. ACCOMPLISHED FLAP OPS AND LEAK CHECKED. WITH NO DE FECTS NOTED. ALL PANELS REMOVED TO ACCOMPLISH CABLE ASSEMBLY. RUNS RESCUED. REPLACED BOTH OB FLAP CONTROL VALUES. 2 L 7 3 4F A22WE 2002062400119 20020624 00119 CE 2002 6 24 WVE2002F00007 1 20020403 A 2120 156CA3213A336 COUPLING LEAR 60 60LEAR 5170707 CE AFT TAILCONE MISSING B WVER O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 09 221FX 4398 111 PILOT REPORTED DUCT OVERHEAT CAUTION DURING SECOND FLIGHT AFTER 1200/2400 HOURS AND 3000 CYCLE INSPECTION AT 25,000 FEET . SUBSQUENTLY REPORTED GENERATOR AND INVERTER FAILED. DECLARED IFE AND RETURNED TO AIRFIELD. MECHANIC DID NOT INSTALL AN INNER COUPLING SLEEVE AS SHOWN IN AIRCRAFT IPC 36-11-41, PN 60190V5-001 AND POSSIBLY INSTALLED THE COUPLING INCORREC TLY. PROBABLE CAUSE: THE AIRCRAFT ARRIVE WITHOUT THE SLEEVE INSTALLED AND THE INSTALLATION PROCEDURE IN THE MM ALSO DO ES NOT SHOW THIS SLEEVE REQUIRED TO BE INSTALLED. 2 L 7 2 4F RT A10CE 2002062400120 20020624 00120 CE 2002 6 24 WVE2002F00008 1 20020404 A 3600 60190607 SLEEVE LEAR 60 60LEAR 5170707 CE AFT TAILCONE MISSING B WVER O OTHER O OTHER NR NOT REPORTED 1 EA 09 216FX 4398 103 AIRCRAFT ARRIVED FOR 600/1200 INSPECTION WITH FAIL SAFE SLEEVE MISSING FROM BLEED AIR MANIFOLD, PN 6019060-8 AS SHOWN IN IPC 36-10-09. PROBABLE CAUSE: MECHANIC FAILED TO INSTALL SLEEVE, POSSIBLY DUE TO ERROR IN THE PROCEDURE FOR BLEED AIR COUPLING INSTALLATION IN MM. 2 L 7 2 4F RT A10CE 2002062400121 20020624 00121 CE 2002 6 24 WVE2002F00009 1 20020403 A 7120 4571200011001 MOUNT LEAR 45 45LEAR 5170805 CE RT ENGINE CHAFED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 418FX 1022 120 DURING 600/1200 HOUR INSPECTION THE RIGHT FORWARD ENGINE MOUNT HAD TWO CHAFE MARKS MEASURING .017 INCHES DEEP. PROBABLE CAUSE: THE TWO UPPER ATTACH BOLTS FOR THE MOUNT FAIRING CHAFED THE MOUNT. RECOMMEND A FLUSH TYPE FASTENER BE APPROVED TO ATTACH FIRE SEAL TO FAIRING. 2 L 7 2 4F RT T00008WI 2002062400122 20020624 00122 CE 2002 6 24 WVE2002F00010 1 20020403 A 7120 4571200011001 MOUNT LEAR 45 45LEAR 5170805 CE ENGINE CHAFED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 418FX 1022 120 DURING 600/1200 HOUR INSPECTION LEFT FORWARD ENGINE MOUNT HAD TWO CHAFE MARKS MEASURING .017 INCH AND .006 INCH DEEP. P ROBABLE CAUSE: THE TWO UPPER ATTACH BOLTS FOR THE MOUNT FAIRING CHAFED THE MOUNT. RECOMMENDED A FLUSH TYPE FASTENER BE APPROVED TO ATTACH FIRE SEAL TO FAIRING. 2 L 7 2 4F RT T00008WI 2002062400123 20020624 00123 CE 2002 6 24 WVE2002F00011 1 20020419 A 7120 H148 MOUNT LEAR 45 45LEAR 5170805 CE ENGINE CHAFED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 417FX 114 DURING 600/1200 HOUR INSPECTION LEFT FORWARD ENGINE MOUNT HAD TWO CHAFE MARKS MEASURING .022 INCH AND .005 INCH DEEP. P ROBABLE CAUSE: THE TWO UPPER ATTACH BOLTS FOR THE MOUNT FAIRING CHAFED THE MOUNT. RECOMMEND A FLUSH TYPE FASTERNER BE APPROVED TO ATTCH FIRE SEAL TO FAIRING. 2 L 7 2 4F RT T00008WI 2002062400124 20020624 00124 CE 2002 6 24 WVE2002F00012 1 20020419 A 7120 H095 MOUNT LEAR 45 45LEAR 5170805 CE ENGINE CHAFED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 417FX 114 DURING 600/1200 HOUR INSPECTION RIGHT FORWARD ENGINE MOUNT HAD TWO CHAFE MARKS MEASURING .025 INCH AND .005 INCH DEEP. PROBABLE CAUSE: THE TWO UPPER ATTACH BOLTS FOR THE MOUNT FAIRING CHAFED THE MOUNT. RECOMMEND A FLUSH TYPE FASTENER BE APPROVED TO ATTACH FIRE SEAL TO FAIRING. 2 L 7 2 4F RT T00008WI 2002062400125 20020624 00125 CE 2002 6 24 WVE2002F00013 1 20020420 A 3246 13070891 WHEEL LEAR 45 45LEAR 5170805 CE MLG LOOSE B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 419FX 125 DURING 600/1200 HOUR INSPECTION; FOUND BOTH LEFT MAIN LANDING GEAR WHEEL ASSEMBLIES EXCESSIVELY LOOSE; WHEELS, BEARING S AND AXLES WERE INSPECTED NO FURTHER DISCREPANCY NOTED, REASSEMBLED IAW MM. PROBABLE CAUSE: IMPROPERLY TORQUED AT LAS T CHANGE AND/OR TORQUE PROCEDURES NEED REVISED. 2 L 7 2 4F RT T00008WI 2002062400127 20020624 00127 2002 6 24 GTIA020490 4 20020319 A 2565 SLIDE DOUG DC9 DC981 3022081 WP TAIL CONE UNSECURE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND AFT FUSELAGE COMPARTMENT TAIL SLIDE UNPACKED. REMOVED SLIDE. TAIL CONE INSTALLED. (M) 2 L 7 2 4F A6WE 2002062400128 20020624 00128 WP 2002 6 24 GTIA020491 1 20020324 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND PASSENGER COMPARTMENT FLOOR PANEL (MEMBRANE PHENOLIC) RIGHT OUTBOARD STATION 1271 TO STATION 1309 HAD DELAMI NATED. REPAIRED COMPARTMENT FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2002062400129 20020624 00129 WP 2002 6 24 GTIA020492 1 20020322 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR PANEL STATION 864 TO STATION 886 LEFT SIDE HAS DAMAGE/DELAMINATED. FABRICATED REPAIR FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002062400130 20020624 00130 WP 2002 6 24 GTIA020493 1 20020322 A 5320 CLIP DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD B/BAY STATION 372 CLIP FOR THRESHOLD HAS CORROSION. REMOVED CORROSION. REMOVED PARTS CLIPS AND T-A NGLE. FABRICATE CLIP. INSTALLED SUPPORT 2ND CLIP. (M) 2 L 7 2 4F A6WE 2002062400131 20020624 00131 WP 2002 6 24 GTIA020494 1 20020419 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND RIGHT COCKPIT FLOOR PANEL CRACKED AND BROKEN FORWARD CLOSEOUT. REPAIRED COCKPIT FLOOR PANEL USING 181 CLOTH . (M) 2 L 7 2 4F A6WE 2002062400132 20020624 00132 WP 2002 6 24 GTIA020496 1 20020410 A 5730 PANEL DOUG DC9 DC982 3022082 WP RT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND RIGHT WING LOWER EXTERNAL TRAPEZOIDAL PANEL HAS DELAMINATION. REPAIRED RIGHT WING LOWER EXTERNAL PANEL. (M ) 2 L 7 2 4F A6WE 2002062400133 20020624 00133 WP 2002 6 24 GTIA020497 1 20020410 A 5730 PANEL DOUG DC9 DC982 3022082 WP LT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND LEFT WING LOWER EXTERNAL TRAPEZOIDAL PANEL HAS DELAMINATED. REMOVED DELAMINATED PLIES. REPAIRED DELAMINATI ON. (M) 2 L 7 2 4F A6WE 2002062400134 20020624 00134 WP 2002 6 24 GTIA020498 1 20020506 A 3350 TERMINAL DOUG DC9 DC982 3022082 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND EMERGENCY LIGHTS INOPERATIVE AT FORWARD OVERWING EXIT LIGHTS (LT/RT) L2 EXIT (FWD LOWER CORNER) SEAT 34 STAN DBY LIGHT, BETWEEN SEATS 32 AND 33 STANDBY LIGHTS. RANG OUT STANDBY LIGHTING IN AFT CABIN SEAT 34 AND SEAT 32 AND 33. FOUND WIRES INSTALLED WRONG. SWAPPED WIRES. FOUND UNSECURED BATTERY TERMINAL. SECURED BATTERY TERMINAL. (M) 2 L 7 2 4F A6WE 2002062400135 20020624 00135 WP 2002 6 24 GTIA020499 1 20020410 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND LEFT INBOARD SEAT TRACK X22 FS 1222 TO FS 1305 HAS CORROSION. REMOVED SEAT TRACK. LOCATED AND DRILLED, INS TALLED. (M) 2 L 7 2 4F A6WE 2002062400136 20020624 00136 WP 2002 6 24 GTIA020500 1 20020409 A 2760 CONTROL VALVE DOUG DC9 DC982 3022082 WP SPOILER FAILED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND DURING OPS CHECK OF AUTO SPOILER SYSTEM. ONLY THE FLIGHT SPOILERS DEPLOY. TROUBLESHOT AND FOUND OPEN COILS ON BOTH RIGHT AND LEFT GROUND SPOILER CONTROL VALVES. REMOVED LEFT AND RIGHT GROUND SPOILERS CONTROL VALVES. INSTALLE D LEFT AND RIGHT GROUND SPOILERS CONTROL VALVES. (M) 2 L 7 2 4F A6WE 2002062400137 20020624 00137 NM 2002 6 24 GTIA020516 1 20020520 A 2420 947K9452 CONNECTOR DOUG MD80 MD83 3023681 NM NR 1 ENGINE LOOSE A GTIA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 23 822NK 49392 FLL - FLT 1440 - AT 30,000 ON CLIMB-OUT, LT ENGINE GENERATOR DROPPED OFFLINE, CROSSTIE LOCKOUT LIGHT ON LT GEN FEEDER FA ULT LIGHT ON LT GEN OFF LIGHT ON LOSS OF CONT LT AC BUS POWER OCCURRED. FOLLOWED QRH, DESCENDED TO 24,000, THE APU FINA LLY STARTED. QRH CREW PLACED LT APU BUS SWITCH ON AND CONT. RECOVERED LT AC BUS. CROSSTIE LOCKOUT AND LT GEN FEEDER F AULT REMAINED RETURNED TO FLL FOR A MX RTB. ACCOMPLISHED ENGINE RUN AND PERFORMED AC GENERATOR PREFERENTIAL AND LOAD CH ECK. OPENED NR 1 ENGINE COWLING AND INSPECTION GENERATOR FEEDER CABLES FROM AC GENERATOR FROM AC GENERATOR TO THE AFT P RESSURE BULKHEAD. NO DEFECTS NOTED, FOUND GENERATOR FEEDER CONNECTOR LOOSE AT ENGINE FIREWALL, SECURED CONNECTOR. (M) 2 L 7 2 4F RT 2002062400138 20020624 00138 WP 2002 6 24 MEX2002135 1 20020205 A 2910 HYDRAULIC LINE DOUG DC9 DC982 3022082 WP HYD SYSTEM LEAKING A ASMF D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SW 23 1003Y 48068 FLT 136 - MEX-AGS - FIFTEEN MINUTES BEFORE TAKEOFF, WHEN THE CAPTAIN TRIED TO PRESSURE THE HYDRAULIC SYSTEM A HYDRAULIC LEAK WAS DETECTED AT THE TAIL CONE AREA. AIRCRAFT WAS SENT TO THE HANGAR, THE LEAK WAS DETECTED IN THE SUPPLY LINE OF T HE HYDRAULIC AUXILIARY PUMP ASSY. IT WAS CHANGED IAW MM 20-12-03. THE ENGINE AND HYDRAULIC PUMP WAS CHECKED IAW MM 71- 00-00 AND 29-10-05, TESTS OK. ADDITIONALLY THE ACCESSORIES COMPARTMENT WAS CLEANED AND THE WATER SEPARATORS WERE CHANGE D IAW MM 12-22-00 AND 21-20-02 RESPECTIVELY. (M) 2 L 7 2 4F A6WE 2002062400139 20020624 00139 EU 2002 6 24 SIMA200210401 1 20020414 A 3350 6013211 BATTERY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 313AE 340B313 HPN - FLT 4719 - DURING PREFLIGHT, CREW REPORTED THE EMERGENCY FLOOR LIGHTS IN ROW 6, 7, 8B WILL NOT STAY ON. MAINTENAN CE REMOVED AND REPLACED EMERGENCY BATTERY 22LN IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 L 7 2 4T RT A52EU 2002062400140 20020624 00140 EU 2002 6 24 SIMA200210901 1 20020418 A 3320 8ES00558800 TRANSFORMER AEROSP ATR42 ATR42300 8680920 EU CABIN BURNED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 269AT 269 MIA - FLT 5029 - SMOKE AND SMELL OF ELECTRICAL BURNING REPORTED OVER SEAT 10A IN FLIGHT. MOC WAS NOTIFIED BY DISPATCH. PILOT ELECTED TO RETURN TO MIA. FOUND TRANSFORMER BURNED OUT AT SEAT 10 A/B ON THE PSU POWER SUPPLY. REMOVED AND REPL ACED POWER SUPPLY IAW AMM 33-25-00, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2002062400141 20020624 00141 EU 2002 6 24 SIMA200211101 1 20020421 A 2910 AE7065488 HYDRAULIC LINE SAAB SF340 340B 7860101 EU NLG FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 903AE 340B282 CREW REPORTED THE HYDRAULIC FAIL LIGHT ILLUMINATED ON THE CWP. CREW SELECTED TO OVERRIDE AND QUANTITY WENT TO ZERO. EM ERGENCY WAS DECLARED AND CREW RETURNED TO BWI. GEAR WAS EXTENDED BY EMERGENCY EXTENSION. MAINTENANCE REPLACED THE NOSE LANDING GEAR MAIN ACTUATOR HYDRAULIC LINE IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. MA IN LANDING GEAR SEPARATION BOLTS WERE ALSO REPLACED IAW SAAB MM. (M) 2 L 7 2 4T RT A52EU 2002062400142 20020624 00142 EU 2002 6 24 SIMA200211501 1 20020425 A 3350 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 314AM 314 MIA - FLT 5102 - CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY L IGHT POWER SUPPLY UNIT (P/N 301180, S/N 219) 3WL IAW ATR MM. BATTERIES WERE ALSO REPLACED AT POWER SUPPLY UNITS 30 WL ( P/N AD3127, S/N 25925), 15WL (P/N AD3127, S/N 18374), AND AT 3WL (P/N AD3127, S/N 26674). OPS CHECK WAS GOOD AND AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002062400143 20020624 00143 EU 2002 6 24 SIMA200211603 1 20020426 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU RT ENGINE FAULTY A SIMA B EMER. DESCENT N FALSE WARNING DE DESCENT 1 SW 21 400BR 340B400 DFW - FLT 3580 - CREW REPORTED THE RIGHT ENGINE TAIL PIPE HOT LIGHT ILLUMINATED. EMERGENCY WAS DECLARED AND AIRCRAFT WA S LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED ALL THREE DETECTORS IN THE RIGHT TAIL PIPE IAW SAAB MM. MAINTENANCE ALSO REPAIRED A BROKEN TERMINALS IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002062400144 20020624 00144 EU 2002 6 24 SIMA200211901 1 20020429 A 3350 MS2740601 SWITCH SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 902AE 340B269 SPS - FLT 3580 - ON PREFLIGHT CREW, FOUND EMERGENCY EXIT SIGN OVER MAIN CABIN DOOR AND FLIGHT ATTENDANT SEAT TO BE INOPE RATIVE. AIRCRAFT WAS FERRIED TO LAW. MAINTENANCE REMOVED AND REPLACED THE COCKPIT ARM SWITCH AND POWER SUPPLY UNITS 20 LN AND 21LN IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002062400145 20020624 00145 SO 2002 6 24 SIMA200212101 1 20020421 A 5315 14521721009 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON FORWARD DIGITAL. REMOVED CORROSION BY CUT OUT. PERFORM ED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A REPLACEMENT STRAP, TWO DOUBLERS AND A SHIM IAW EMB 145 (SRM145/1142, CHAPTER 53, REV 17) 53-10-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002062400146 20020624 00146 SO 2002 6 24 SIMA200212102 1 20020418 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING . FABRICATED A REPAIR DOUBLER. REPAIRED IAW EMB GST-1246/02, ITEM 4 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002062400147 20020624 00147 SO 2002 6 24 SIMA200212103 1 20020419 A 5320 DOUBLER EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - DURING AN IMBV INSPECTION OF AIRCRAF, FOUND CORROSION ON LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20. REMOVED P REVIOUS REPAIR, CORROSION LIMITED TO PREVIOUS REPAIR. FABRICATED A DOUBLER ANGLE, FILLER, A PLATE, AND TWO SHIMS. REPA IRED IAW EMB145 SRM145/1142, CHAPTER 53, REV 17, 53-21-10, FIG 201 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002062400148 20020624 00148 SO 2002 6 24 SIMA200212104 1 20020422 A 5320 14525480003 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CARGO DOOR CUT OUT LOWER SILL CORRODED. REMOVED CORRODED SILL (BEAM) . POSITIONED NEW BEAM AND INSTALLED. WORK DONE IAW EMB 145 (SRM 145/1142 CHAPTER 51, REV 17) 51-40-02, AND STANDARD SR M PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002062400149 20020624 00149 SO 2002 6 24 SIMA200212105 1 20020417 A 5320 BEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 145301 ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON CENTER BEAM AT FRAME 20. REMOVED CORRODED BY CUT OUT. F ABRICATED TWO DOUBLER ANGLES, A FILLER, AND A U-SHAPE DOUBLER CHANNEL. REPAIRED IAW EMB145 (SRM145/1142, CHAPTER 53, RE V 17) 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002062400150 20020624 00150 SO 2002 6 24 SIMA200212106 1 20020416 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSLEAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 145301 ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OU T. FABRICATED A DOUBLER ANGLE, FILLER, TWO SHIMS. WORK DONE IAW EMB 145 SRM 145/1141, CHAPTER 53, REV 17 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002062400151 20020624 00151 SO 2002 6 24 SIMA200212107 1 20020419 A 5330 SKIN EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 145301 DURING AN MBV INSPECTION OF AIRCRAFT, FOUND FOUR GROUPS OF GOUGES ON THE LEFT FORWARD FUSELAGE BETWEEN FRAMES 12 AND 13, ALONG STRINGER 16L. BLENDED GOUGES PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRI CATED A REPAIR DOUBLER. REPAIRED IAW EMB GST-1265/02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002062400152 20020624 00152 SO 2002 6 24 SIMA200212108 1 20020419 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 145301 ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING. FABRICATED A REPAIR DOUBLER. REPAIRED IAW EMB GST-1254/02, ITEM 4 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002062400153 20020624 00153 SO 2002 6 24 SIMA200212109 1 20020413 A 5315 14521721009 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING, GALLEY FORWARD DIGITAL CORRODED. REPAIRED GALLEY FORWARD DIGITAL IAW EMB145 SRM 53-21- 10. (M) 2 L 7 2 4F RT T00011AT 2002062400154 20020624 00154 SO 2002 6 24 SIMA200212110 1 20020415 A 5320 14525480003 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING, CARGO DOOR CUT OUT LOWER SILL CORRODED. INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51- 40-02. (M) 2 L 7 2 4F RT T00011AT 2002062400155 20020624 00155 SO 2002 6 24 SIMA200212111 1 20020412 A 5320 14521725001 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING. LEFT SILL BETWEEN 18 AND 21 CORRODED. INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02, 51 -40-06, 51-20-02. M) 2 L 7 2 4F RT T00011AT 2002062400156 20020624 00156 SO 2002 6 24 SIMA200212139 1 20020413 A 5311 12010732001 FRAME EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 THIS IS A LEVEL 2 FINDING, PROFILE CORRODED AT FRAME 23. INSTALLED NEW PROFILE IAW EMB 145 SRM 51-40-02, 51-20-01. (M) 2 L 7 2 4F RT T00011AT 2002062400157 20020624 00157 SO 2002 6 24 SIMA200212141 1 20020413 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 ABI - THIS IS A LEVEL 2 FINDING, FORWARD GIGITAL IN GALLEY HAS CORROSION. INSTALLED REPAIR DOUBLER IAW EMB GST-1140/02 AND 1169/02. (M) 2 L 7 2 4F RT T00011AT 2002062400158 20020624 00158 SO 2002 6 24 SIMA200212149 1 20020424 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 145312 THIS IS A LEVEL 2 FINDING, CORROSION GALLEY CENTRAL BEAM GUSSET. BLENDED CORROSION, PERFORMED NDT, RESTORED SURFACE PRO TECTION IAW EMB CPM 51-21-04, 51-21-05, 51-21-06. (M) 2 L 7 2 4F RT T00011AT 2002062400159 20020624 00159 SO 2002 6 24 SIMA200212150 1 20020424 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 145312 ABI - THIS IS A LEVEL 2 FINDING, CORROSION ON FORWARD DIGITAL. BLENDED CORROSION PERFORMED NDT, RESTORED SURFACE PROTEC TION IAW EMB CPM 51-21-04, 51-21-05, 51-21-06. (M) 2 L 7 2 4F RT T00011AT 2002062400160 20020624 00160 SO 2002 6 24 SIMA200212151 1 20020424 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 145312 ABI - THIS IS A LEVEL 2 FINDING, CORROSION FOUND ON AFT DIGITAL. BLENDED, PERFORMED NDT, RESTORED SURFACE PROTECTION. (M) 2 L 7 2 4F RT T00011AT 2002062400161 20020624 00161 SO 2002 6 24 SIMA200212152 1 20020423 A 5320 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 145312 ABI - THIS IS A LEVEL 2 FINDING, CORROSION ON DIAMOND GUSSET AT FRAME 20. BLENDED CORROSION, PERFORMED NDT, RESTORED SU RFACE PROTECTION IAW EMB GST-1348/01. (M) 2 L 7 2 4F RT T00011AT 2002062400162 20020624 00162 SO 2002 6 24 SIMA200212153 1 20020424 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 145312 ABI - THIS IS A LEVEL 2 FINDING, CORROSION ON CENTER BEAM AT FRAME 19. INSTALLED SERVICEABLE CENTER BEAM IAW EMB GST-13 48/02. (M) 2 L 7 2 4F RT T00011AT 2002062400163 20020624 00163 NM 2002 6 24 ABXA0916 1 20020624 A 5347 96FS66781421 SEAT TRACK BOEING 767 767200 1385120 NM AFT CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 CABIN SEAT TRACKS CORRODED STA 1165-1200, LBL 18. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-52. DR ILLED IAW DWG 96FS667807, INSTALLED TRACK IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2002062400164 20020624 00164 NM 2002 6 24 UPS02438175 1 20020418 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO BS 480-500 LT STR 35 EDGE FOUND CRACKED. BS 480- BS 500 LT STR 35 SEGMENT REPAIRED AS PER S RM 53-10-03 FIG 3 AND AN AREA PAINT TOUCH UP PER MM 51-24-11. 2 L 7 4 4F A20WE 2002062400165 20020624 00165 NM 2002 6 24 HNAA0200047 1 20020622 A 2497 1010815M PSU DHAV DHC8 DHC8102 2809003 NM CABIN 7AC CHAFED A HNAA K NONE O OTHER LD LANDING 1 EA 07 935HA 142 PLASTIC BURNING SMELL FROM OVERHEAD PANEL 1AC. FOUND WIRES PINCHED AND CHAFED AT PSU 7AC. REPLACED PSU. 2 H 7 2 4T RT A13NM 2002062400166 20020624 00166 NM 2002 6 24 AWXA200200552 1 20020608 A 5330 65558743 STOP FITTING BOEING 737 7373G7 1384595 NM WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 0 0 24010 MCN - MAJOR REPAIR - DURING C-14 CHECK A SHORT EDGE MARGIN WAS FOUND ON THE AFT GALLEY DOOR STOP FITTING BS 954, STR 11 R/H. MAINTENANCE REMOVED THE AFT GALLEY DOOR STOP FITTING AND TRIMMED DAMAGE AT THE END OF CLOSE OUT PLATES. FABRICATED 2 EACH FILLERS, 2 EACH -1 STRAPS, 2 EACH -2 FRAME SPLICE STRAPS, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5300-02165-JS4 . 2 L 7 2 4F RT A16WE 2002062400167 20020624 00167 NM 2002 6 24 AWXA200200553 1 20020616 A 5330 65558743 STOP FITTING BOEING 737 7373G7 1384595 NM WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 0 0 24010 MCN - MAJOR REPAIR - DURING C-14 CHECK A SHORT EDGE MARGIN WAS FOUND ON THE AFT ENTRY DOOR STOP FITTING BS 954, STR 11 L /H. MAINTENANCE REMOVED THE AFT ENTRY DOOR STOP FITTING AND TRIMMED DAMAGE AT THE END OF CLOSE OUT PLATES. FABRICATED 2 EACH FILLERS, 2 EACH -1 STRAPS, 2 EACH -2 FRAME SPLICE STRAPS, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5300-02165-JS4. 2 L 7 2 4F RT A16WE 2002062400168 20020624 00168 NM 2002 6 24 AWXA200200555 1 20020603 A 5313 654687782 WEB BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 0 0 22653 YVR - MAJOR REPAIR - DURING C-15 CHECK A 1/2" CRACK WAS FOUND ON R/H SRTINGER 18A SHEAR BEAM (WEB) AT BS 727 BULKHEAD A TTACHMENT. MAINTENANCE REMOVED CRACKED WEB, FABRICATED A NEW WEB, AND INSTALLED REPAIR IAW B737-200 SRM 51-10-1, PG. 8, DWG 65-46877 SHT 9, AND AWA ER 15-5314-02172-GF1. 2 L 7 2 4F RT A16WE 2002062400169 20020624 00169 NM 2002 6 24 AWXA200200559 1 20020611 A 5330 65558721 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 0 0 23778 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1/2" CRACK WAS FOUND ON THE TORQUE BOX WEB AT BS 947.5, STR 12 R/H. MAINTENANCE REMOVED THE TORQUE BOX WEB AT BS 947.5, STR 12 R/H; FABRICATED A NEW TORQUE BOX WEB; AND INSTALLED REPAIR IAW DWG 65-55 872, B737-300 SRM 51-40-02 PG. 3, 9, 38, & 42, AND SRM 51-20-01 PG. 10, 47. 2 L 7 2 4F RT A16WE 2002062400170 20020624 00170 NM 2002 6 24 AWXA200200560 1 20020615 A 5311 65465588 FRAME BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 0 0 23778 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1/4" CRACK WAS FOUND ON FRAME AT BS 907, STR 1 R/H, DUCT BRACKET MOUNT AREA. MA INTENANCE TRIMMED OUT DAMAGED AREA ON FRAME AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACK EXISTS. FABRICATED REPAIR ANGLE AND FILLER, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11, FIG. 1, PG. 1-6. 2 L 7 2 4F RT A16WE 2002062400171 20020624 00171 SO 2002 6 24 LR7A02042 1 20020624 A 3040 3505871 INSULATOR LKHEED 382 382G 526414U SO FS 117 LH BURNED A LR7A A J UNSCHED LANDING DUMP FUEL A FLAME/FIRE CL CLIMB 1 AL 03 403LC 671 4590 FLIGHT CREW REPORTED PILOT SIDE SWING WINDOW NESA (WIRE INSTALLATION) CAUGHT ON FIRE AFTER TAKEOFF. TURNED NESA SYSTEM OFF AND FIRE WENT OUT. DUMPED APPROX. 11,000 LBS. IN ACCORDANCE WITH QRH. RETURNED TO ETAR.REPLACED PILOT SIDE SWING W INDOW NESA HEAT CONNECTION POST AND INSULATION BUSHING IAW SMP581 30-40. OPS CHECK GOOD. LP 07601, PR1.NOTIFIED NTSB-A NC 24 JUN 02 APPROX. 1100 LCL. NTSB-ANC CONFIRMED NO REPORT REQUIRED. 2 H 7 4 4T A1SO 2002062500001 20020625 00001 2002 6 25 MDAS091010 4 20020624 A 3460 FMC BOEING 737 737800* NM W Q0MF L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 WP 03 28236 The aircraft Reg. number B-16802, s/n 28236, experienced both FMC lost near Sung Shan airport in Taiwan. During Approach RWY 28, both FMC were lost twice. First time the crew can restore the FMC, but second time were unable to restore. Due to that time got APP Clearance, the crew asked to fly to FUSIN and hold. On getting course, the crew could load the FMC. Aircraft landed normally. Maintenance action: IAW AMM 34-61-00, FMC C/B reset and ground test normal. 2 L 7 2 4F RT A16WE 2002062500002 20020625 00002 GL 2002 6 25 ALGA079294 2 20020528 A 7210 6893672 PINION GEAR 23063393 BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX GALLED H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 577AL 683 CAG47062 53247 FOUND EXCESSIVE GALLING ON PINION GEAR, SPALLING AND GALLING ON T/M GEAR. BOTH GEARS HAVE VERY UNUSUAL WEAR PATTERN. E NTRY MADE BY RNB 1 G 7 1 3U 3 U O H2SW E1GL 2002062500003 20020625 00003 GL 2002 6 25 ALGA079295 2 20020528 A 7210 23071895 GEAR 23063393 BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX GALLED H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 577AL 683 CAG47062 53247 FOUND EXCESSIVE GALLING ON PINION GEAR, SPALLING AND GALLING ON T/M GEAR. BOTH GEARS HAVE VERY UNUSUAL WEAR PATTERN. E NTRY MADE BY RNB. 1 G 7 1 3U 3 U O H2SW E1GL 2002062500005 20020625 00005 GL 2002 6 25 ALGA079297 2 20020529 A 7210 23071895 GEAR 23063393 BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX SPALLED H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 497AL 486 CAG47258 53172 GEARBOX WAS REMOVED FOR CORRODED STUDS, DURING INSPECTION FOUND SPALLING ON PINION GEAR TEETH. 1 G 7 1 3U 3 U O H2SW E1GL 2002062500006 20020625 00006 EU 2002 6 25 ALGA079298 1 20020529 A 8011 160SG140Q1 STARTER UROCOP EC120 EC120B 8680987 EU ENGINE DEFECTIVE H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 510AL 247 1251 AIRCRAFT WOULD NOT START WARRANTY REPAIR AND RETURN. 1 G 7 2 3U NC R0001RD 2002062500007 20020625 00007 GL 2002 6 25 ALGA079855 2 20020610 A 7210 6893673 GEARSHAFT 23063393 BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TORQUE METER GALLED H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 687AL 4782 CAG47311 53366 DUE TO T/M JOURNAL SUPPORT STUDS BACKING OUT OF COVER AN UNUSUAL WEAR PATTERN OF SPALLING AND GALLING OCCURRED ON GEAR T EETH. 1 G 7 1 3U 3 U O H2SW E1GL 2002062500008 20020625 00008 GL 2002 6 25 ALGA079856 2 20020610 A 7210 23065470 SHAFT 23063393 BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/M GEAR BEARING LOOSE H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 687AL 4782 CAG47311 53366 FOUND T/M GEAR, BEARING JOURNAL SHAFT AND SUPPORT LOOSE IN COVER ASSEMBLY. FOUND ALL 4 STUDS ON JOURNAL SUPPORT PULLED OUT AND 1 EACH WITH NO THREADS LEFT IN WORN BORE. THIS ALLOWED GEAR TO WEAR IN AN UNUSUAL MANNER, WHICH COULD HAVE RESU LTED IN A CATASTROPHIC GEAR FAILURE. 1 G 7 1 3U 3 U O H2SW E1GL 2002062500009 20020625 00009 GL 2002 6 25 ALGA079857 2 20020610 A 7250 BLADE BOLKMS 105 BO105CB* SW ALLSN 250C 250C20B 03013 GL TURBINE WHEEL MISSING H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 107AL 1028 S772 UPON INSPECTION OF ALL PARTS NR 2 WHEEL HAD ONE BLADE MISSING. 1 G 7 2 4U 3 U H3EU E4CE 2002062500010 20020625 00010 GL 2002 6 25 ALGA079858 2 20020610 A 7210 6898785 GEAR BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL GEARBOX SPALLED H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 355AL 51444 SPALLING AND GALLING ON GEAR TEETH DUE TO IMPROPER MESHING OF TEETH. 1 G 7 1 3U 3 U H2SW E1GL 2002062500011 20020625 00011 2002 6 25 ERAA079861 4 20020429 A 3457 8143902240D GPS SKRSKY S61 S61N 8142104 NE COCKPIT FAILED H ERAA K NONE L NO TEST IN INSP/MAINT 1 FS 01 561EH 1300 61471 GPS UNIT FAILED TEST. 2 G 7 2 4U 1H15 2002062500012 20020625 00012 2002 6 25 ERAA079862 4 20020429 A 3457 8143902240D GPS BELL 412 412 1182202 SW COCKPIT INTERMITTENT H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 415EH 106 33009 UNIT GIVES INTERMITTENT RECIPROCAL HEADINGS & READINGS. 1 G 7 2 4U H4SW 2002062500014 20020625 00014 2002 6 25 SWAA021329 4 20020616 A 2565 D31354 SLIDE BOEING 737 7373T0 1384582 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002062500015 20020625 00015 NM 2002 6 25 SWAA021330 1 20020617 A 3350 321500 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT LENS LOOSE AT ROW NR 3 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002062500016 20020625 00016 NM 2002 6 25 SWAA021331 1 20020616 A 3350 20131A BATTERY BOEING 737 737301 1384611 NM CABIN WEAK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 EMERGENCY EXIT LIGHTS ILLUMINATE WHEN SHIFTING PWR FROM A/C PWR TO GRD PWR. REMOVED AND REPLACED M1132 EMERGENCY LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002062500017 20020625 00017 NM 2002 6 25 SWAA021332 1 20020617 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS (2 EA) BETWEEN STR'S 22R AND 23R, AT BS 727D PLUS 18 AND BS 7 66.5. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002062500018 20020625 00018 NM 2002 6 25 SWAA021333 1 20020617 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002062500019 20020625 00019 NM 2002 6 25 SWAA021334 1 20020617 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 794, WL 148 AND RBL 8. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002062500020 20020625 00020 NM 2002 6 25 SWAA021335 1 20020615 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 969 AND BS 971, AT STR 21L. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2002062500021 20020625 00021 NM 2002 6 25 SWAA021337 1 20020616 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002062500022 20020625 00022 NM 2002 6 25 SWAA021338 1 20020617 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, BETWEEN STR 8L AND 9L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002062500023 20020625 00023 NM 2002 6 25 SWAA021340 1 20020617 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 8R AND 9R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002062500024 20020625 00024 2002 6 25 SWAA021342 4 20020617 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002062500025 20020625 00025 NM 2002 6 25 SWAA021344 1 20020617 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT LENS LOOSE AT ROW 23 DEF. REMOVED AND REPL ACED LENS PER MM. 2 L 7 2 4F RT A16WE 2002062500026 20020625 00026 2002 6 25 SWAA021345 4 20020618 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM AFT SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND COVER CRACKED. REMOVED AND REPLACED S LIDE PER MM. 2 L 7 2 4F A16WE 2002062500027 20020625 00027 NM 2002 6 25 SWAA021349 1 20020618 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED BETWEEN BS'S 747 AND 767, STR 10R. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2002062500028 20020625 00028 NM 2002 6 25 SWAA021350 1 20020618 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, WL 208 AND LBL 45. REPAIRED FLOORBEAM PER BF G ER. 2 L 7 2 4F RT A16WE 2002062500029 20020625 00029 NM 2002 6 25 SWAA021351 1 20020616 A 5230 6549889 FRAME BOEING 737 7373H4 1384600 NM FWD CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 440, WL 160. REMOVED AND REPLACED CARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 2002062500030 20020625 00030 NM 2002 6 25 SWAA021352 1 20020617 A 2751 6940659 ROLLER BOEING 737 7372H4 138448C NM LT WING WORN A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 29 073SW 22673 DURING EXTENSION OF FLAPS HEARD A LOUD POPPING GRINDING NOISE FROM LT WING T/E OTBD MID FLAP. REMOVED AND REPLACED LT W ING T/E MID FLAP DEFLECTION ROLLER PER MM. 2 L 7 2 4F A16WE 2002062500031 20020625 00031 NM 2002 6 25 SWAA021353 1 20020619 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED A1 CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT MISSING LENS AND BULB. INSTALLED LENS AND BULB PER MM. 2 L 7 2 4F RT A16WE 2002062500032 20020625 00032 2002 6 25 SWAA021354 4 20020618 A 2565 65C19901 CABLE BOEING 737 7373Y0 1384671 NM FWD SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002062500033 20020625 00033 NM 2002 6 25 SWAA021358 1 20020619 A 5755 654645262A SPOILER BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED D CHECK, FOUND NR 4 SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED NR 4 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2002062500034 20020625 00034 NM 2002 6 25 SWAA021359 1 20020618 A 5753 6546435334 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED RT OTBD AFT T/ E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002062500035 20020625 00035 NM 2002 6 25 SWAA021360 1 20020617 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002062500036 20020625 00036 NM 2002 6 25 SWAA021361 1 20020619 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 4, ABOVE STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002062500037 20020625 00037 NM 2002 6 25 SWAA021362 1 20020618 A 5311 6546569 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 081SW 22730 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L AND 27R. REMOVED AND REPLACED SHEA R TIE PER SRM. 2 L 7 2 4F A16WE 2002062500038 20020625 00038 NM 2002 6 25 SWAA021363 1 20020617 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 081SW 22730 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT WINDOW BELT CUTOUT ON LT WINDOW'S NR 1, 2, 3, 4, 5, 6, 7, 8, 9, 10 AND 11. REPAIRED SKIN PER SWA SI. 2 L 7 2 4F A16WE 2002062500039 20020625 00039 NM 2002 6 25 ABXA010916 1 20020624 A 5347 96FS66781421 SEAT TRACK BOEING 767 767200 1385120 NM AFT CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 CABIN SEAT TRACKS CORRODED STA 1165-1200, LBL 18. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-52. DR ILLED IAW DWG 96FS667807, INSTALLED TRACK IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2002062500040 20020625 00040 NM 2002 6 25 371PA0008 1 20020621 A 3350 TRACK BOEING 737 737306 13844BG NM BROKEN A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 371PA 23543 Aft 25feet of floor parth lighting top track broken in several parts. Aft lighting Inop.R&R 25feet section track. R&R aft electrical strip Ops check good in reference to MM33-51-41 2 L 7 2 4F RT A16NE 2002062500041 20020625 00041 NM 2002 6 25 SWAA021328 1 20020616 A 3350 65C27093 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED SERVICE CHECK, FOUND TWO BULBS INOP AT AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002062500042 20020625 00042 2002 6 25 ERAA079865 4 20020430 A 3444 40008330207 INDICATOR SKRSKY S61 S61N 8142104 NE RADAR CONTAMINATED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 563EH 1103 61808 UNIT WILL NOT POWER UP, CAN'T SEE ANYTHING. HAS MAJOR WATER DAMAGE. ACTION TAKEN: REPLACED BLOWN RESISTOR AND CLEANED CORROSION. 2 G 7 2 4U 1H15 2002062500044 20020625 00044 NM 2002 6 25 SWAA021336 1 20020617 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002062500045 20020625 00045 2002 6 25 ERAA079867 4 20020502 A 3444 40009650201 INDICATOR SKRSKY S61 S61N 8142104 NE RADAR SYS STRIPPED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 563EH 2151 61808 UNIT IS INOPERABLE. LOCK SCREWS ARE STRIPPED. HAS CORROSION, MAJOR WATER DAMAGE. ACTION TAKEN: CLEANED, REPLACED LOC KING SCREWS. ALSO REPLACED BROKEN KNOB. 2 G 7 2 4U 1H15 2002062500046 20020625 00046 GL 2002 6 25 ERAA079868 2 20020502 A 7323 252466715H GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE SLOW H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 153EH 3582 S572 ARM SHAFT STIFF, SLOW TO RESPONSE. DROOPING OUT OF SERVICE LIMITS. FOUND INTERNAL BEARINGS ROUGH/DRY, ECCENTRIC SHAFT UNDERSIZE; WORN, THROTTLE BUSHING WORN, OVERSIZE. 1 G 7 2 3U 3 U H3EU E4CE 2002062500047 20020625 00047 GL 2002 6 25 ERAA079869 2 20020502 A 7323 252466715H GOVERNOR BOLKMS 105 BO105A EU ALLSN 250C 250C20B 03013 GL ENGINE WORN H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 135EH 11833 S675 CAUSES NR TO BLEED OFF AFTER BEEPED TO 100 PERCENT. COVERED BY SEVERE PREMATURE WEAR. EVIDENCE OF TORSIONAL RESONANCE CONDITION BETWEEN PTG DRIVE & GEAR BOX DRIVE. WATER / RUST ON SEVERAL PARTS. SPEEDER SPRING & 2D CAM LEVER. ACTION TAK EN: SET PTG TORSIONAL DRIVE FILTER SHIMS TO HIGH LIMIT. AVOID GREASE CONTAMINATION OF DRIVE SPLINES, REPLACED WORN P ARTS, CLEANED, REASSEMBLED & RECALIBRATED GOVERNOR. 1 G 7 2 3U 3 U H3EU E4CE 2002062500048 20020625 00048 SW 2002 6 25 ERAA079870 1 20020502 A 6210 412015300109 BLADE BELL 412 412 1182202 SW MAIN ROTOR DAMAGED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 421EH 33067 MAIN ROTOR BLADES SN A-545, A-1290, A-1131 HAVE VOIDS AND CRACKED. ACTION TAKEN: REPAIRED AS PER 8130-3 BLOCK NR 13 FO R ALL REPAIRS PERFORMED. 1 G 7 2 4U H4SW 2002062500049 20020625 00049 EU 2002 6 25 ERAA079871 1 20020503 A 5302 STRUCTURE BOLKMS 105 BO105C 5626005 EU TAILBOOM CRACKED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 571 90 DEGREE GEARBOX FITTING EXFOLIATED / INNER GRAINULAR CORROSION, CRACKED HORIZONTAL STABILIZER DOUBLER LEFT SIDE, SEVER AL CORRODED RIVETS & NUT PLEATER. INSTALLED NEW 90 DEGREE GEARBOX FITTING, NEW HORIZONTAL STABILIZER DOUBLER AND REPLA CED ALL NECESSARY NUT PLATE AS NEEDED. CLEANED TREATED AND REPAIRED CORROSION AREAS AS INDICATED. 1 G 7 2 3U H3EU 2002062500050 20020625 00050 SW 2002 6 25 ERAA079872 1 20020507 A 6320 GEAR BELL 412 412 1182202 SW GEARBOX FAILED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 417EH 11867 ANG00080 33031 INSPECTION OF PLANETARY SYSTEM FOR BREAKDOWN. UPPER PLANETARY - BROKEN CAGE, SAME GEAR HAS SCORED ROLLER SET. REMOVED TOP CASE, REMOVED UPPER & LOWER PLANETARY AND ASSOCIATED GEARS. DISASSEMBLED, INSPECTED FOR BREAKDOWN, DETAILS ON BLUE FORMS ; FOUND NO BREAKDOWN OTHER THAN NORMAL WEAR, REASSEMBLED AND REINSTALLED PLANETARY'S AND GEAR IN TRANSMISSION. A LL WORK IAW BHT-412 CR&O63/ 1 G 7 2 4U H4SW 2002062500051 20020625 00051 EU 2002 6 25 ERAA079873 1 20020509 A 3110 6607190A WARNING LIGHT BOLKMS 105 BO105S 5626006 EU COCKPIT INOPERATIVE H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 128EH 129 572 PRESSURE SWITCH HAS NO T OIL LIGHT. INOPERABLE. 1 G 7 2 3U H3EU 2002062500052 20020625 00052 EU 2002 6 25 ERAA079874 1 20020509 A 3110 6607190A WARNING LIGHT BOLKMS 105 BO105S 5626006 EU COCKPIT INOPERATIVE H ERAA K NONE L NO TEST IN INSP/MAINT 1 FS 01 134EH 486 635 PRESSURE SWITCH IS INOPERABLE. T OIL LIGHT WILL NOT COME ON. 1 G 7 2 3U H3EU 2002062500053 20020625 00053 WP 2002 6 25 IVSA078654 1 20020507 A 6310 D2761 ACTUATOR ROBSIN R22 R22 7640102 WP CLUTCH DEFECTIVE H IVSA O OTHER O OTHER NR NOT REPORTED 1 FS 01 HP145 596 1031 CLUTCH ACTUATOR MOTOR FAILED. (4TH TIME) 1 G 7 1 3O H10WE 2002062500054 20020625 00054 SW 2002 6 25 YTRR079849 1 20020606 A 6220 412010182101 BEARING BELL 412 412 1182202 SW M/R WORN H YTRA K NONE O OTHER IN INSP/MAINT 1 FS 01 293CA 2890 33005 ROD END BEARING EXCESSIVELY WORN. 1 G 7 2 4U H4SW 2002062500055 20020625 00055 NM 2002 6 25 SWAA021339 1 20020615 A 5753 6571909117 SPAR BOEING 737 7372H4 138448C NM T/E FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED C2 CHECK, FOUND LT OUTBOARD MID FLAP AFT SPAR UPPER FLANGE CRACKED. REMOVED AND REPLACED LT OUTBOARD M ID FLAP PER MM. 2 L 7 2 4F A16WE 2002062500056 20020625 00056 NM 2002 6 25 SWAA021341 1 20020617 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002062500057 20020625 00057 NM 2002 6 25 SWAA021343 1 20020617 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED SERVICE CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AFT OF LT OVERWING EXIT. RELAMPED LIGHT PER MM . 2 L 7 2 4F RT A16WE 2002062500058 20020625 00058 SW 2002 6 25 YTRR079850 1 20020606 A 6220 412010182101 BEARING BELL 412 412 1182202 SW MAIN ROTOR WORN H K NONE O OTHER IN INSP/MAINT 1 FS 01 293CA 2032 33005 ROD END BEARING WORN EXCESSIVELY. 1 G 7 2 4U H4SW 2002062500059 20020625 00059 2002 6 25 SWAA021346 4 20020618 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002062500060 20020625 00060 2002 6 25 SWAA021347 4 20020618 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 DURING SCHEDULED RON, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002062500061 20020625 00061 NM 2002 6 25 SWAA021348 1 20020617 A 2530 41600019 COFFEEMAKER BOEING 737 7373Q8 1384670 NM GALLEY OVERHEATED A SWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 672SW 23406 STRONG ELECTRICAL ODOR NOTED AT FWD PART OF CABIN DISSIPATED WITH GALLEY PWR OFF. REMOVED AND REPLACED FWD GALLEY COFFE EMAKER PER MM. 2 L 7 2 4F RT A16WE 2002062500062 20020625 00062 NM 2002 6 25 SWAA021355 1 20020618 A 3350 57771 CAP BOEING 737 7373Y0 1384671 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING IN FWD CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2002062500063 20020625 00063 NM 2002 6 25 SWAA021356 1 20020618 A 2560 10107451 SIGN BOEING 737 7373H4 1384600 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 FWD ENTRY DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2002062500064 20020625 00064 NM 2002 6 25 SWAA021357 1 20020619 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STR CLIP PER MM. 2 L 7 2 4F RT A16WE 2002062500065 20020625 00065 SW 2002 6 25 YTRR079851 1 20020606 A 6220 412010182101 BEARING BELL 412 412 1182202 SW MAIN ROTOR WORN H YTRA K NONE O OTHER IN INSP/MAINT 1 FS 01 293CA 2891 33005 ROD END BEARING EXCESSIVELY WORN. 1 G 7 2 4U H4SW 2002062500066 20020625 00066 SW 2002 6 25 YTRR079852 1 20020606 A 6220 412010182101 BEARING BELL 412 412 1182202 SW MAIN ROTOR WORN H YTRA K NONE O OTHER IN INSP/MAINT 1 FS 01 293CA 2891 33005 ROD END BEARING EXCESSIVELY WORN. 1 G 7 2 4U H4SW 2002062500067 20020625 00067 NM 2002 6 25 UPS02238691 1 20020624 A 3350 LIGHT BOEING 727 727173C 1384059 NM COCKPIT NOT SEATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:N/A COCKPIT EMERGENCY LIGHT ILLUMINATED IN ARMED POSITION. RESEAT COCKPIT EMERGENCY EXIT LIGHT, OPS CHE CK GOOD. 2 L 7 3 4F A3WE 2002062500068 20020625 00068 NM 2002 6 25 UPS02438170 1 20020418 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO - BS 840 - 845 STR 30L STR WEB FOUND HEAVY CORROSION. FWD CARGO BS 840-845 STR 30L WEB REPA IRED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002062500069 20020625 00069 NM 2002 6 25 UPS02438171 1 20020419 A 5320 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO - BS 840 LT STR 30 SUPPORT WEB I/B CHORD SPLICE FOUND CORRODED. FWD CARGO BS 840 LT STR 30 SUPPORT WEB I/B CHORD SPLICE REPAIRED AS PER SRM 51-10-01 FIG 1. 2 L 7 4 4F A20WE 2002062500070 20020625 00070 NM 2002 6 25 UPS02438172 1 20020421 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - STA 2178 STR 1R STRINGER END CRACKED. BS 2178- BS 2150 S1R STRINGER SEGMENT REPAIR AS PER SRM 5 3-10-03 FIG 4 AND AREA FINISH PAINT TOUCH UP AS PER MM 51-24-11. 2 L 7 4 4F A20WE 2002062500071 20020625 00071 NM 2002 6 25 UPS02438173 1 20020424 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D BS 2178 LT NR 1 STRINGER END CRACKED. BS 2178 S1L, STRINGER SEGMENT REPAIR AS PER SRM 53-10-03 FI G 4 AND FINISHED PAINT TOUCH UP PER MM 51-24-11. 2 L 7 4 4F A20WE 2002062500072 20020625 00072 NM 2002 6 25 UPS02438174 1 20020421 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - STA 2182-2185 LT NR 1 STRINGER END FOUND CRACKED. BS 2172- BS 2188 S1L, STRINGER SECTIONAL REPA IRED AS PER SRM 53-10-03 FIG 4 AND FINISH PAINT APPLIED AS PER MM 51-24-11. 2 L 7 4 4F A20WE 2002062500073 20020625 00073 NM 2002 6 25 UPS02438176 1 20020421 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C AFT CARGO COMPT - BS 1640- 1643 STR 35R FOUND CORRODED. AFT CARGO COMPT BS 1640-1643 STR 35R REPAIRED AS PER SRM 51-10-01 FIG 1. 2 L 7 4 4F A20WE 2002062500074 20020625 00074 NM 2002 6 25 UPS02438177 1 20020422 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C U/D - BS 540-600 AND 610-640 LBL 66, SEAT TRACK CROWN AND FLANGE FOUND CORROSION. BS 540-600 AND 610- 640 LBL 66, SEAT TRACK CROWN AND FLANGE REPAIRED AS PER SRM 51-10-01. (P/N: BAC1520-1567-717876511RK). 2 L 7 4 4F A20WE 2002062500075 20020625 00075 NM 2002 6 25 UPS02438178 1 20020415 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C AFT COMPT - BS 1880 LBL 20 FLOORBEAM UPPER CHORD FOUND CORRODED CRACKED. AFT COMPT BS 1880 LBL 20 FLO ORBEAM UPPER CHORD REPAIRED AS PER SRM 51-10-01 FIG 2. 2 L 7 4 4F A20WE 2002062500076 20020625 00076 NM 2002 6 25 UPS02438179 1 20020415 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C AFT COMPT - BS 1880 LBL 26 FLOORBEAM UPPER CHORD FOUND CORRODED. AFT COMPT - BS 1880 LBL 26 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-10-01 FIG 01. 2 L 7 4 4F A20WE 2002062500077 20020625 00077 NM 2002 6 25 UPS02438180 1 20020421 A 2520 PANEL BOEING 747 747123 1384873 NM CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - L2 DOOR FWD CUTOUT LOWER REVEAL CRACKED. L2 DOOR FWD CUTOUT LOWER REVEAL PANEL REPAIRED IAW SRM 53-10-04 PG 84. 2 L 7 4 4F A20WE 2002062500078 20020625 00078 NM 2002 6 25 UPS02438182 1 20020419 A 2520 PANEL BOEING 747 747123 1384873 NM CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 2231 LT NR 5 DOOR FWD CUTOUT BETWEEN STR 22 & 23 CUTOUT CRACKED. BS 2231 L5 DOOR FWD CUTOUT REVEAL PANEL FROM STR 22L TO STR 25L REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002062500079 20020625 00079 NM 2002 6 25 UPS02438184 1 20020508 A 3350 SWITCH BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT SWITCH INOP. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH MODULE. OPS CHECK G OOD. 2 L 7 4 4F A20WE 2002062500080 20020625 00080 NM 2002 6 25 UPS02438185 1 20020422 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C BULK CARGO - BS 2060 - 2080 RT STR 28 FOUND CORRODED. BS 2060 - BS 2090 S28R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062500081 20020625 00081 NM 2002 6 25 UPS02438188 1 20020423 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D BS 150-160 LBL 50 MOST O/B FLOOR SUPPORT CORRODED. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2. 2 L 7 4 4F A20WE 2002062500082 20020625 00082 NM 2002 6 25 UPS02438189 1 20020423 A 5320 65B07941125 ANGLE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - NLG PRESSURE DECK UPPER SURFACE ANGLE FOUND CRACKED. ANGLE REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002062500083 20020625 00083 NM 2002 6 25 UPS02438190 1 20020423 A 5320 65B07941125 ANGLE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - NLG PRESSURE DECK UPPER SURFACE ANGLE FOUND CRACKED. ANGLE REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002062500084 20020625 00084 NM 2002 6 25 UPS02438191 1 20020422 A 5320 INTERCOSTAL BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 1220 LBL 119 BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002062500085 20020625 00085 NM 2002 6 25 UPS02438192 1 20020416 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C BULK CARGO - BS 2020-2021 LBL 8 FLOOR SUPPORT FOUND CORRODED CRACKED. FLOOR SUPPORT REPAIRED AS PER S RM 53-10-07 FIG 20. 2 L 7 4 4F A20WE 2002062500086 20020625 00086 NE 2002 6 25 219PA0002 2 20020624 A 7320 714810 VALVE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE A PIDA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 05 219PA 19956 657617 #2 engine would not produce calculated T/O thrust. T/O discontinued at approx. 60 kts.Verified. R&R'd #2 eng P&D valve IAW M/M73-12-1. Ops & Leak chks good. Also C/W work cardPAS-MF-25, JT8D eng. trim & data plate run. Ops chks good no d efects noted 2 L 7 2 4F 4 F A16WE E2EA 2002062500087 20020625 00087 NM 2002 6 25 UPS02438193 1 20020419 A 5411 SPAR BOEING 747 747123 1384873 NM NR 1 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C NR 1 PYLON - MID SPAR WEB CHAFING THROUGH AT NAC STA 238. MID SPAR WEB REPAIRED AS PER SRM 54-10-03 F IG 12. 2 L 7 4 4F A20WE 2002062500088 20020625 00088 NE 2002 6 25 YTRR079853 2 20020606 A 7323 25249995 GOVERNOR BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE MALFUNCTIONED H YTRA K NONE O OTHER IN INSP/MAINT 1 FS 01 293CA 33005 GOVERNOR WAS CAUSING A TORQUE SPLIT IN THE NR 2 ENGINE. 1 G 7 2 4U 4 U H4SW E22EA 2002062500089 20020625 00089 NM 2002 6 25 UPS02438195 1 20020421 A 5320 TIE CLIP BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - STA 1956-1960 LT NR 2 STRINGER END FOUND CRACK. TIE CLIP AT M/D BS 1960 S2L REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500090 20020625 00090 SW 2002 6 25 YTRR079854 1 20020606 A 7722 304547801 COMPENSATOR BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ITT TRIM ERRATIC H YTRA K NONE O OTHER IN INSP/MAINT 1 FS 01 293CA 33005 GAVE ERRATIC AND ERRONEOUS READINGS DURING GROUND RUN. TRIM COMPENSATOR WAS RECEIVED NEW FROM PRATT AND WHITNEY WITH THE ENGIEN AFTER OVERHAUL. 1 G 7 2 4U 4 U H4SW E22EA 2002062500091 20020625 00091 NM 2002 6 25 UPS02438196 1 20020421 A 5310 DOOR FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - R2 DOOR FWD CUTOUT REVEAL FOUND CRACKED. R2 DOOR FWD CUTOUT REVEAL REPAIRED IAW RS R53-22-34784 . 2 L 7 4 4F A20WE 2002062500092 20020625 00092 CE 2002 6 25 2002FA0000750 1 20020521 A 7603 311AS3146780 CONTROL CABLE MTSBSI MU2 MU2B35 5780411 CE ENGINE FRAYED E O OTHER O OTHER IN INSP/MAINT 1 SW 15 640MA 8934 590 DURING INSPECTION IN THE AFT FUSELAGE FOUND ONE OF THE ENGINE CONTROL CABLES FRAYED WHERE THE CABLE GOES OVER A PULLEY A ND TURNS 90 DEGREES. THIS IS THE 2ND OF THREE REPORTED BY THE SAME OPERATOR IN 90 DAYS. ALL HAVE BEEN THE LEFT ENGINE CO NTROL 1 H 7 2 3T RT A10SW 2002062500093 20020625 00093 NM 2002 6 25 UPS02438197 1 20020417 A 5310 65B11751601 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - L3 DOOR CUTOUT FWD LOWER CORNER REVEAL FOUND CRACKED. M/D L3 DOOR CUTOUT FWD LOWER CORNER REVEA L REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500094 20020625 00094 NM 2002 6 25 UPS02438198 1 20020421 A 5310 65B11751602 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - R3 DOOR FWD CUTOUT LOWER CORNER REVEAL FOUND CRACKED. LOWER CORNER REVEAL FITTING REPLACED AS P ER SRM 51-10-01 PG 8 & PAINT TOUCHED UP AS PER MM 21-24-11. 2 L 7 4 4F A20WE 2002062500098 20020625 00098 NM 2002 6 25 UPS02438199 1 20020422 A 5320 65B16951 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C RT BS 983 STR 38R LOWER DRAG SPLICE FITTING FOUND 1 EACH FASTENER HOLE CRACKED APPROX .125 INCH AS MAR KED. RT BS 983 STR 38R LOWER DRAG SPLICE FITTING REPLACED AS PER SRM 51-10-01 AND BOEING SB 747-53-2064. 2 L 7 4 4F A20WE 2002062500100 20020625 00100 NM 2002 6 25 UPS02438200 1 20020422 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 780 S-7R AND S-8R FRAME FOUND CRACK. FRAME REPAIRED IAW SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 2002062500103 20020625 00103 NM 2002 6 25 UPS02438201 1 20020419 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - FRAME FOUND CRACK AT STA 940 S24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2 L 7 4 4F A20WE 2002062500104 20020625 00104 NM 2002 6 25 UPS02438202 1 20020419 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - FRAME FOUND CRACK AT STA 600 S24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2 L 7 4 4F A20WE 2002062500105 20020625 00105 NM 2002 6 25 UPS02438203 1 20020419 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - FRAME FOUND CRACK AT STA 640 S25L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2 L 7 4 4F A20WE 2002062500107 20020625 00107 NM 2002 6 25 UPS02438204 1 20020419 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - FRAME FOUND CRACK AT STA 920 S24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2 L 7 4 4F A20WE 2002062500109 20020625 00109 NM 2002 6 25 UPS02438205 1 20020422 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C U/D - BS 780 S-7L AND S-8L FRAME FOUND CRACKED. FRAME REPAIRED IAW SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 2002062500111 20020625 00111 NM 2002 6 25 UPS02438206 1 20020422 A 5320 65B0484364 TIE CLIP BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C AFT CARGO - BS 1520 RTS FRAME ATT TIE CLIP FOUND CORROSION AT STR 29R. AFT CARGO - BS 1520 STR 29R TI E CLIP REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500112 20020625 00112 NM 2002 6 25 UPS02438207 1 20020422 A 5320 65B0465320 TIE CLIP BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C BULK CARGO - BS 2040 RT FRAME ATT TIE CLIP FOUND CORRODED AT STR 32R. TIE CLIP REPLACED AS PER SRM 51 -10-01. 2 L 7 4 4F A20WE 2002062500114 20020625 00114 NM 2002 6 25 UPS02438208 1 20020421 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - STA 2186 STRINGER 1R STRINGER END CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. 2 L 7 4 4F A20WE 2002062500115 20020625 00115 NE 2002 6 25 2002F00638 2 20020622 A 8530 399354 CYLINDER BEECH 18 E18S 1151006 CE PWA R985 R985AN14B 52008 NE ENGINE CRACKED E E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 05 8627A 3965 750 BA283 JP205004 AT CRUISE POWER LEFT ENGINE LOST POWER AND STARTED TO RUN ROUGH. ENGINE WAS SHUT DOWN AND DIVERTED TO LEX. NR 8 CYLINDER WAS FOUND CRACKED AT INTAKE PORT. 1 L 7 2 3R 3 R A765 5E1 2002062500116 20020625 00116 NM 2002 6 25 UPS02438209 1 20020422 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C U/D - BS 990 S-7L AND S-8L STRINGER END SPLICE SUSPECT CRACKED. HFEC INSPECTION CUTOUT AS PER NTM PAR T 6 51-00-00 FIG 4. BS 970 - 990 S-7L AND S-8L STRINGER REPAIRED IAW SRM 53-10-03 FIG 4 AT TWO LOCATIONS. 2 L 7 4 4F A20WE 2002062500117 20020625 00117 EU 2002 6 25 02175309 1 20020624 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 309UE 41022 During preflight inspection, the crew noted that the second section of the emergency floor track lighting was inoperativ e. Maintenance personnel secured a loose connector for the emergency floor track lighting system. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002062500120 20020625 00120 EA 2002 6 25 COMA0260382 1 20020621 A 2760 SPOILER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 991CA 7216 FLIGHT 5535 CONFIG SPOILERS CAUTION DURING T/O.FOUND SPOILER LEVER AJAR - RESET LEVER AND SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 2002062500126 20020625 00126 EA 2002 6 25 COMA0260383 1 20020622 A 2410 ALTERNATOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING E O VIBRATION/BUFFET OTHER CL CLIMB 1 SO 01 784CA 7319 FLIGHT 9478 - LOUD VIBRATION DURING GEAR RETRACTION.FOUND ADG DEPLOYED - STOWED ADG AND SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 2002062500131 20020625 00131 EA 2002 6 25 COMA0260384 1 20020621 A 3230 601R751461 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 784CA 6836 7319 FLIGHT 5004 - NLG DID NOT RETRACT.REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002062500132 20020625 00132 EA 2002 6 25 COMA0260385 1 20020623 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER DE DESCENT 1 SO 01 964CA 7129 FLIGHT 5858 GEAR DISAGREE WARNING DURING EXTENSION.COULD NOT DUPLICATE GEAR EXTENSION AND RETRACTION CHECKS WERE NORMAL. 2 L 7 2 4F RT A21EA 2002062500133 20020625 00133 NM 2002 6 25 UPS02438210 1 20020417 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO BS 720 LBL 25 LONGITUDINAL FLOOR SUPPORT AFT END FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500134 20020625 00134 EA 2002 6 25 COMA0260386 1 20020623 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 965CA 7131 FLIGHT 5160 FLAPS FAILED AT 45 DEGREES DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002062500135 20020625 00135 EU 2002 6 25 377PA0006 2 20020622 A 7200 CFM563B2 ENGINE BOEING 737 7373L9 1384470 NM CFMINT CFM56 CFM563B2 13802 EU A PIDA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 SO 05 377PA 23718 721788 At rotation had a loud engine vibration on Left engine. Inspected eng. intake, exhaust; opened cowlings & inspected; cl ose cowlings; BITE AVM per MM77-31-00. Eng. Insp. per MM71-00-47. Ran eng. Parameters & fan blade damage within limit s. 2 L 7 2 4F 4 F RT A16WE E21EU 2002062500141 20020625 00141 CE 2002 6 25 CA020619011 1 20020427 A 3233 824188896 SPACER BEECH 18 G18S 1151010 CE PWA R985 R985AN14B 52008 NE HAMSTD 22D 22D30 NE MLG MOTOR MISSING W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) SPACER OF THE LANDING GEAR MOTOR WAS MISSING. THIS MISSING PIECE CAUSED THE FAILURE OF THE MOTOR. 1 L 7 2 3R 3 R A765 5E1 5 C P736 2002062500144 20020625 00144 NM 2002 6 25 UPS02438212 1 20020419 A 2520 PANEL BOEING 747 747123 1384873 NM CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 2231 LT NR 5 DOOR FWD CUTOUT BETWEEN STR 16 & 15 CUTOUT CRACK. CUTOUT REVEAL PANEL REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002062500147 20020625 00147 NM 2002 6 25 UPS02438213 1 20020419 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO BS 520 - 540 STR S-29R STRINGER END FOUND CRACKED. BS 520 - 540 S-29R STRINGER SPLICE REPLA CED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002062500149 20020625 00149 NM 2002 6 25 UPS02438214 1 20020421 A 2520 PANEL BOEING 747 747123 1384873 NM CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - R5 DOOR FWD CUTOUT LOWER REVEAL FOUND CRACKED. REVEAL PANEL REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002062500150 20020625 00150 NM 2002 6 25 UPS02438215 1 20020422 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C U/D - BS 630-640, LBL 46 SEAT TRACK CROWN FOUND CORRODED AS MARKED. CORROSION REMOVED IAW SRM 51-10-0 1. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002062500151 20020625 00151 NE 2002 6 25 B3OR20020004 2 20020202 A 7230 3041214 COMBUSTION LINER CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE ENGINE FAILED B B3OR K NONE O OTHER IN INSP/MAINT 1 SW 03 26494 1390 1390 5500605 PCE71394 AIRCRAFT WAS INDUCTED INTO A PHASE 1,2, 5A & B INSPECTION. DURING THE INSPECTION THE ENGINE IGNITERS WERE TO BE REMOVED. WHILE REMOVING THE IGNITERS OF THE NR 2 ENGINE, THE OUTBOARD IGNITER BECAME STUCK ON THE FLOATING WASHER IN THE COMBUST ION LINER. THE IGNITER BROKE FREE FROM THE FLOATING WASHER AND THE WASHER SLID TO THE BOTTOM OF THE COMBUSTION LINER. TH E COMBUSTION LINER WAS REMOVED TO FACILITATE REWELDING OF THE FLOATING WASHER AND REINSTALLED. 1 L 7 2 4F 4 F A22CE E1NE 2002062500152 20020625 00152 EU 2002 6 25 B3OR20020006 1 20020522 A 6330 350A38021100 CROSSBEAM SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE MAIN ROTOR GROOVED B B3OR K NONE O OTHER IN INSP/MAINT 1 SW 03 5204Y 979 100 3101 9571 DURING A 1000 HOUR INSPECTION, THE CROSS BEAM WAS FOUND TO HAVE ONE DELAMINATED FWD. RUBBER ISOLATOR, AND DAMAGE TO THE AFT LATERAL LAMINATED RUBBER ISOLATER MOUNTING AREA. THE DAMAGE WAS CAUSED BY THE RUBBER ISOLATOR LOSING TORQUE, AND ROT ATING ON ITS MOUNTING AREA. THE DAMAGE WAS TO THE MOUNTING FACE AND THE INNER ISOLATOR MOUNTING AREA. THE DAMAGE WAS BEY OND REPAIR, THE CROSSBEAM HAD TO BE SCRAPPED. 1 G 7 1 3U 3 U H9EU E19EU 2002062500153 20020625 00153 NM 2002 6 25 UPS02438216 1 20020422 A 5310 DOOR FRAME BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - R3 DOOR FWD CUTOUT LOWER REVEAL FOUND DENT HOLE. R3 DOOR FWD CUTOUT LOWER REVEAL REPLACED AS PE R SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500154 20020625 00154 EU 2002 6 25 B3OR20020007 1 20020522 A 6310 350A35110500 GIMBAL RING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE MAIN ROTOR WORN B B3OR K NONE O OTHER IN INSP/MAINT 1 SW 03 5204X 985 100 3099 9570 DURING A 1000 HOUR INSPECTION, THE GIMBAL RING ON THE ENGINE TO MAIN GEARBOX MOUNT HAD EXCESSIVE PLAY IN THE BUSHINGS TH AT WAS OUT OF LIMITS. THE BUSHINGS ARE NOT REPLACEABLE, AND THE GIMBAL RING HAD TO BE SCRAPPED. 1 G 7 1 3U 3 U H9EU E19EU 2002062500155 20020625 00155 NM 2002 6 25 UPS02438217 1 20020422 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D BS 900 FRAME FOUND CRACKED AT S-11R. BS 900 SIDE FRAME AT STR 11R AREA REINFORCEMENT FRAME PATCH REPAIRED AS PER HX RS R53-22-34790. 2 L 7 4 4F A20WE 2002062500156 20020625 00156 NM 2002 6 25 DHL2002709003 1 20020625 A 3350 1000679 LIGHT BOEING 727 72782C 1384026 NM A DHLA K O NONE OTHER O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 1) FWD MAIN ENTRY DOOR EMERGENCY EXIT LIGHT VERY DIM.2) R/R EMERGENCY EXIT LIGHT ASSY IAW MM 33-50-00 OPS CK GOOD. 2 L 7 3 4F A3WE 2002062500157 20020625 00157 NM 2002 6 25 UPS02438218 1 20020418 A 5320 TIE CLIP BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO - BS 660 LT FRAME ATT TIE CLIP FOUND CRACKED AT STR 38L. BS 660 STR 38L TIE CLIP REPLACED A S PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500158 20020625 00158 NM 2002 6 25 UPS02438219 1 20020418 A 5320 TIE CLIP BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO BS 760 FRAME STR 30L ATT TIE CLIP FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEN D OUT NOT WITHIN SRM 53-10-01 PG 8. FRAME STR-30L ATT TIE CLIP REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500159 20020625 00159 NM 2002 6 25 UPS02438220 1 20020415 A 5320 SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C AFT COMPT - BS 1850 - 1856 RBL 8-16 FLOORBEAM UPPER SUPPORT PNL ATT PLATE FOUND CORRODED. CORROSION R EMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 51-10-01 PG 8. AFT CARGO BS 1840 - BS 1860 RBL 8 - 26 FLOORBEAM UPPE R SUPPORT PANEL & ATT PLATE REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500160 20020625 00160 NM 2002 6 25 UPS02438221 1 20020422 A 5310 SHEAR TIE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C BS 2180 BETWEEN S44R AND S46R AREA FRAME SHEAR TIE CRACK. BS 2180 SHEAR TIE BETWEEN STR 44R AND 46R R EPAIRED AS PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2002062500161 20020625 00161 NM 2002 6 25 UPS02438222 1 20020503 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO COMPT - AFTER STRINGER SPLICE REMOVED STRINGER END FOUND CRACK AT BS 740 STR 28R. STRINGER REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500162 20020625 00162 NM 2002 6 25 UPS02438223 1 20020419 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO - BS 740 - 760 STR-29R FOUND CRACKED. FWD CARGO COMPT BS 740 - 790 STR 29R STRINGER REPAIRE D IAW SRM 53-10 -03 FIG 1. BUTT JOINT SKIN REPAIRED FROM BS 740 - 752 BTN STR 28-30 PER SRM 53-30-03 FIG 47. 2 L 7 4 4F A20WE 2002062500163 20020625 00163 NM 2002 6 25 UPS02438224 1 20020421 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C BS 2180 S-50R STRINGER END CRACKED. BS 2180 - 2210 S-50R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062500164 20020625 00164 NM 2002 6 25 UPS02438225 1 20020418 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO - BS 520 RT FRAME WEB FOUND CRACKED BETWEEN STR 32R & STR 33R. FRAME WEB DOUBLER REPLACED A S PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002062500165 20020625 00165 NM 2002 6 25 UPS02438226 1 20020422 A 5240 WEB BOEING 747 747123 1384873 NM R3 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - R3 DOOR INNER WEB CRACKED. INNER WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002080500124 20020805 00124 2002 8 5 GLBA2002089 4 20020624 A 3442 6227337001 RADAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 253GL 8 UE253 LEFT HAND ENVIRO FAIL ILLUMINATED IN FLIGHT, WEATHER RADAR INOP IN FLIGHT. COULD NOT DUPLICATE LEFT HAND ENVIRO BLEED F AIL. REMOVED AND REPLACED RIGHT HAND WEATHER RADAR. 2 L 7 2 4T 4 T RT A24CE E26NE 2002062500166 20020625 00166 NM 2002 6 25 UPS02438227 1 20020416 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C AFT CARGO - BS 1840 - 1860 RBL 8 FLOOR SUPPORT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01, BL END OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS. AFT CARGO BS 1850 RBL 8 FLOOR SUPPORT FLANGE REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2002062500167 20020625 00167 NM 2002 6 25 UPS02438229 1 20020511 A 3350 FUSE BOEING 747 747259B 1384804 NM CABIN NOT SEATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT AT FWD PART OF UPPER DECK IS INOP. RESEATED FUSES IN POWER SUPPLY. OPS NORMAL PER MM 33-51-00. 2 L 7 4 4F RT A20WE 2002062500168 20020625 00168 NM 2002 6 25 UPS02438232 1 20020421 A 5320 65B1104638 STIFFENER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FX - STA 400 S41L STIFFENER FOUND CRACKED. STIFFENER REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500169 20020625 00169 NM 2002 6 25 UPS02438233 1 20020418 A 5320 ANGLE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO - BS 840 - 844 STR 30L STR WEB UPPER FWD SUPPORT ANGLE FOUND HEAVY CORROSION AT STR 30L. SU PPORT ANGLE REPLACED PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500170 20020625 00170 NM 2002 6 25 UPS02438234 1 20020503 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO COMPT - BS 710 STR 29R STRINGER CORROSION FOUND. BS 670 - 740 STR STRINGER REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500171 20020625 00171 NM 2002 6 25 UPS02438235 1 20020423 A 5320 STIFFENER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C AFT CARGO COMPT - BS 1800 S-34R AREA FRAME ATT STIFFENER CORRODED. AFT CARGO COMPT BS 1800 S-34R AREA FRAME ATT STIFFENER REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500172 20020625 00172 NM 2002 6 25 UPS02438236 1 20020416 A 5310 DOOR FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 800 FRAME S16L -17L LOCATION FOUND 2 EACH CRACKS AT REVEAL. BS 800 S16 TO S18L REVEAL REPAIR C/OUT IAW SRM 53-10-04 FIG 114 AND HX RS R53-22-34780. 2 L 7 4 4F A20WE 2002062500173 20020625 00173 NM 2002 6 25 UPS02438237 1 20020418 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO - BS 830 - 846 STR 29R FOUND HEAVY CORROSION. CORROSION REMOVED IAW SRM 51-10-01. BS 790 - 870 STR 29R REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062500174 20020625 00174 NM 2002 6 25 UPS02438238 1 20020421 A 5310 DOOR FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - R4 DOOR FWD CUTOUT LOWER REVEAL FOUND CRACKED. R4 DOOR REVEAL REPAIRED AS PER SRM 53-10-04 FIG 84. 2 L 7 4 4F A20WE 2002062500175 20020625 00175 NM 2002 6 25 UPS02438239 1 20020422 A 5210 DOOR FRAME BOEING 747 747123 1384873 NM L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - L1 DOOR FWD FRAME FOUND CRACKED AT LOWER HINGE AREA. FRAME REPAIRED AS PER SRM 52-10-02 FIG 12. 2 L 7 4 4F A20WE 2002062500176 20020625 00176 NM 2002 6 25 UPS02438240 1 20020418 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO - BS 460 - 480 STR 36R FOUND CRACKED AS MARKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 3 . 2 L 7 4 4F A20WE 2002062500177 20020625 00177 NM 2002 6 25 UPS02438241 1 20020422 A 5310 STOP FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - R3 DOOR CUTOUT STOP FITTING FOUND CRACKED (NR 5). R3 DOOR FWD CUTOUT NR 5 STOP FITTING REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002062500178 20020625 00178 NM 2002 6 25 UPS02438242 1 20020419 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - FRAME FOUND CRACK AT STA 540 S24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2 L 7 4 4F A20WE 2002062500179 20020625 00179 NM 2002 6 25 UPS02438243 1 20020419 A 5310 WINDOW FRAME BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - STA 400 - 420 S20R TO 22R WINDOW FORGING MATING SURFACE EDGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 56-20-01 LIMITS, STA 400 - 420 S20R-22R WINDOW FORGING REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500180 20020625 00180 NM 2002 6 25 UPS02438244 1 20020417 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 870 - 880 RBL 11 SEAT TRACK RT FLANGE FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS. M/D BS 870 - 1000 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. 2 L 7 4 4F A20WE 2002062500181 20020625 00181 NM 2002 6 25 UPS02438245 1 20020422 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C BS 2180 S-32R STRINGER END CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2. 2 L 7 4 4F A20WE 2002062500182 20020625 00182 NM 2002 6 25 UPS02438246 1 20020422 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C BULK CARGO - BS 2116 - 2120 RT STR 40 STR END FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BL END OUT NOT WITHIN SRM 53-10-01 LIMITS. BS 2110 - 2130 STR 40R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062500183 20020625 00183 NM 2002 6 25 UPS02438248 1 20020421 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C BS 2180 S-51L STRINGER END CRACK. BS 2180 - 2210 S-51L STRINGER REPAIR IAW SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062500184 20020625 00184 NM 2002 6 25 UPS02438249 1 20020421 A 5210 DOOR FRAME BOEING 747 747123 1384873 NM L1 DOOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - L1 DOOR FWD FRAME FOUND DENT AT UPPER HINGE AREA. FWD DOOR FRAME REPAIRED AS PER SRM 52-10-02 F IG 13. 2 L 7 4 4F A20WE 2002062500185 20020625 00185 NM 2002 6 25 UPS02438250 1 20020419 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO BS 740 - 760 STR 28R FOUND CRACKED. BS 740 - 770 STR 28R REPAIRED AS PER SRM 53-10-03 FIG 1 . 2 L 7 4 4F A20WE 2002062500186 20020625 00186 NM 2002 6 25 UPS02438251 1 20020421 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C BULK CARGO AFT COMPT BS 2180 S 44L STRINGER CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-41 FIG 1 LIMITS. BULK CARGO BS 2180 STR 44L REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062500187 20020625 00187 NM 2002 6 25 UPS02438252 1 20020421 A 5210 WEB BOEING 747 747123 1384873 NM R3 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D R3 DOOR INT WEB FOUND CRACKED AT FWD FRAME APPROX STOP FITTING NR 7 AREA. DOOR WEB REPAIRED AS PE R SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2002062500188 20020625 00188 NM 2002 6 25 UPS02438253 1 20020422 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C BS 2240 BETWEEN S49L AND S50L FRAME CRACK. FRAME REPAIRED AS PER SRM 53-10-04 FIG 71. 2 L 7 4 4F A20WE 2002062500189 20020625 00189 NM 2002 6 25 UPS02438254 1 20020429 A 5412 BULKHEAD BOEING 747 747123 1384873 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT AFT WEB APPROX 4 O'CLOCK (VIEW LOOKING FWD). NR 2 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER INSTRUCTION ON HAECO REPAIR SCHEME R-54-53-34787. 2 L 7 4 4F A20WE 2002062500190 20020625 00190 NM 2002 6 25 UPS02438255 1 20020418 A 5412 BULKHEAD BOEING 747 747123 1384873 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT FWD WEB APPROX 7 O'CLOCK (VIEW LOOKING FWD). NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACKED AREA REPAIRED AS PER HAECO RS R-54-53-34787. 2 L 7 4 4F A20WE 2002062500191 20020625 00191 NM 2002 6 25 UPS02438261 1 20020415 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C AFT COMPT - BS 1800 S-41L TO 42L FRAME UPPER CHORD FOUND CRACKED. AFT COMPT BS 1800 BETWEEN STR 38L T O 42L FRAME REPAIRED AS PER SRM 53-10-04 FIG 66. 2 L 7 4 4F A20WE 2002062500192 20020625 00192 NM 2002 6 25 UPS02438263 1 20020422 A 5210 STOP FITTING BOEING 747 747123 1384873 NM R1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C R1 DOOR FWD LOWER STOP FITTING FOUND CRACKED. R1 DOOR FWD LOWER STOP FITTING REPLACED AS PER SRM 51-1 0-01 PG 8. 2 L 7 4 4F A20WE 2002062500193 20020625 00193 NM 2002 6 25 UPS02438264 1 20020422 A 5210 DOOR FRAME BOEING 747 747123 1384873 NM R3 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - R3 DOOR FWD FRAME FOUND CRACKED AT NR 1 STOP FITTING AREA. FRAME REPAIRED AS PER SRM 52-10-02 F IG 8. 2 L 7 4 4F A20WE 2002062500194 20020625 00194 NM 2002 6 25 UPS02438265 1 20020421 A 5320 STIFFENER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C BULK CARGO AFT COMPT COMPT BS 2200 S-42R AREA FRAME ATT STIFFENER CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS. BS 2200 STR 42R FRAME ATT STIFFENER REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062500195 20020625 00195 NM 2002 6 25 UPS02438266 1 20020502 A 5320 ATTACH ANGLE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO COMPT - BS 700 S28R WEB I/B ATT ANGLE CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01 . BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS. FWD CARGO COMPT BS 690-730 S28R WEB I/B ATT ANGLE REPAIRED AS PER SRM 51-4 0-03 FIG 2. 2 L 7 4 4F A20WE 2002062500196 20020625 00196 NM 2002 6 25 UPS02438267 1 20020423 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C 2 EACH FASTENER HOLES FOUND CRACK ON LT BS 980 S38L SKIN PANEL. FX BS 980 LT STR SKIN REPAIRED AS PER SRM 53-30-03 FIG 60 AT BS 975 - 983 LT BETWEEN STR 37 - 39L. 2 L 7 4 4F A20WE 2002062500197 20020625 00197 SO 2002 6 25 C2XA02SH011 1 20020616 A 3397 W122827622 WIRE EMB 145 EMB145LR 3260212 SO SHORTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12921 145354 SHV-DURING C-CHECK INSPECTION, THE CEILING EMERGENCY LIGHT AT FRAME 24, AND LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOP. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND WIRE W122-8276-22 TO BE SHORTED. MAINTENANCE REPAIRED THE AFFECTED WIRE , OPERATIONALLY CHECKED THE EMERGENCY LIGHTING SYSTEM WITH NO DISCREPANCIES NOTED, AND THE AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002062500198 20020625 00198 NM 2002 6 25 UPS02438269 1 20020415 A 5312 BULKHEAD BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FX - LT SIDE STA 1000 BULKHEAD AFT FACE ATTACH WEB O/B CORNER FOUND CORROSION AT S38L JUST BELOW DRAG SPLICE FITTING. CORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS. BS 100 LT BULKHEAD WEB S -38L JUST BELOW DRAG SPLICE FITTING REPAIRED AS PER RS R-53-23-34786. 2 L 7 4 4F A20WE 2002062500199 20020625 00199 NM 2002 6 25 UPS02438270 1 20020419 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO - BS 880 RT FRAME I/B CHORD FOUND CRACKED BETWEEN STR 34R & STR 35R. FRAME I/B CHORD REPAIR ED AS PER RS R-53-22-34785. 2 L 7 4 4F A20WE 2002062500200 20020625 00200 NM 2002 6 25 UPS02438271 1 20020422 A 5210 DOOR FRAME BOEING 747 747123 1384873 NM R2 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - R2 DOOR FWD FRAME FOUND CRACKED AT LOWER HINGE CUTOUT AREA. R2 DOOR FWD FRAME LOWER HINGE CUTOU T AREA REPAIRED PER HAECO RS R-52-11-34782. 2 L 7 4 4F A20WE 2002062500201 20020625 00201 NM 2002 6 25 UPS02438274 1 20020422 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 960 S-5L FRAME FOUND CRACKED. SIDE FRAME REPAIRED AS PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 2002062500202 20020625 00202 NM 2002 6 25 UPS02438275 1 20020418 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C AFT LOWER CARGO DOOR CUTOUT UPPER EDGE FORWARD CORNER FOUND CRACK AT BODY SKIN APPROX .375 INCH IN LEN GTH FROM THE EDGE OF DOOR CUTOUT. DOOR CUTOUT FWD UPPER CORNER REPAIRED AS PER HAECO RS R-53-61-34789, SRM 53-30-03 FIG 62. 2 L 7 4 4F A20WE 2002062500203 20020625 00203 NM 2002 6 25 UPS02438280 1 20020516 A 3350 FUSE BOEING 747 747259B 1384804 NM CABIN NOT SEATED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:N/A EMERGENCY LIGHT INOP ON UPPER DECK. RESEATED FUSES IN PS, OPS NORMAL. 2 L 7 4 4F RT A20WE 2002062500204 20020625 00204 NM 2002 6 25 2002UALA01012 1 20020616 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 LEFT HAND FUSELAGE STRINGER 16L AT STATION 600 TO 620 DENT OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. STRINGER SPLICED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002062500205 20020625 00205 NM 2002 6 25 2002UALA01017 1 20020615 A 5320 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUSTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 STATION 310, S1 FASTENER HEAD HAS RUST ON EXTERNAL SURFACE. MAJOR REPAIR ACCOMPLISHED. INSTALLED SHEAR TIE AND DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002062500206 20020625 00206 NM 2002 6 25 2002UALA01018 1 20020615 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 STATION 334 RBL 26-45 WL 208, HAT CHANNEL CORRODED. MAJOR REPAIR ACCOMPLISHED. HAT CHANNEL REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002062500207 20020625 00207 NM 2002 6 25 2002UALA01049 1 20020619 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 CABIN FLOOR SUPPORT AT STATION 395-418, BL 0, WL 208 CORRODED. MAJOR REPAIR ACCOMPLISHED. CABIN FLOOR SUPPORT REPLACED . 2 L 7 2 4F 4 F RT A2NM E17NE 2002062500208 20020625 00208 NM 2002 6 25 2002UALA01057 1 20020620 A 5313 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 RIGHT HAND CREASE BEAM IN FLOOR BELOW SUPPORT ANGLE AT BODY STATION 837 RBL 63 UPPER SURFACE CORRODED AT NUT PLATE HOLE. MAJOR REPAIR ACCOMPLISHED. CREASE BEAM DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002062500209 20020625 00209 NM 2002 6 25 2002UALA01058 1 20020621 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 FUSELAGE SKIN HAS SEVERAL DENTS AT STATION 595-625 STRINGER 14L-18L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLERS, TRI PLERS, AND STRUCTURAL FILLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2002062500210 20020625 00210 WP 2002 6 25 DHL2002803008 1 20020623 A 2611 SMOKE DETECTOR DOUG DC8 DC873 302199C WP A DHLA O OTHER J L WARNING INDICATION NO TEST IN INSP/MAINT 1 SO 01 803DH 46123 1) #4 CARGO SMOKE DETECTOR WILL NOT TEST2) ITEM XFER TO DMI LOG PER MEL 26-6-1 DMI #9684 PLACARD INSTALLED3) REF. DMI # 9684. #4 CARGO SMOKE DECTECTION WILL NOT TEST.4) RELAMPED #4 MAIN CARGO SMOKE DETECTOR IAW DC-8 MM 26-10-5. THIS CLEA RSDMI. REMOVED PLACARD. 2 L 7 4 4F RT 4A25 2002062500211 20020625 00211 NM 2002 6 25 AWXA200200563 1 20020622 A 5311 65C3124019 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 0 0 23778 MCN - MAJOR REPAIR - DURING C-16 CHECK THE AFT CARGO DOOR FORWARD TONGUE BOX WEB WAS FOUND PUNCTURED AT BS 790, STR 23 R /H. MAINTENANCE CUTOUT DAMAGED SECTION OF WEB, FABRICATED A REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW B7 37-300 SRM 51-70-13, PG. 1-5. 2 L 7 2 4F RT A16WE 2002062500212 20020625 00212 NM 2002 6 25 02062501 1 20020622 A 5620 65457912 WINDOW BOEING 757 7572T7 1384914 NM ROW 1, D. A N8TA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 19 513NA 23895 During climb out at 25,000 ft., heard a loud bang from back. Flt attendants said window at Row 1D cracked, Aircraft retu rned to base, an uneventful landing was accomplished. 2 L 7 2 4F RT A2NM 2002062600001 20020626 00001 NM 2002 6 26 UPS02438268 1 20020423 A 5714 65B17069 FITTING BOEING 747 747123 1384873 NM CENTER WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C CRACK REVEAL ON THE FASTENER HOLE OF THE FITTING INSIDE WING CENTER TANK COMMON TO LT SIDE BATHTUB FIT TING RUNNING UPWARD APPROX .125" LONG. LT SIDE STA 983 S38L INSIDE DRY BAY BATHTUB DRAG FITTING REPLACED AS PER SRM 51- 30-02. 2 L 7 4 4F A20WE 2002062600002 20020626 00002 NM 2002 6 26 UPS02438299 1 20020422 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C U/D - BS 960 S-5R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 2002062600003 20020626 00003 NM 2002 6 26 UPS02438300 1 20020417 A 5320 141U11076 WEB BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C NWW TUNNEL - RT BS 300 VERTICAL BEAM WEB FOUND CRACKED AT LOWER STAND OFF HOLE BETWEEN FIRST AND SECON D CLIP (COUNT FROM TOP). NOSE W/W TUNNEL RT BS 300 VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 & BOEING DWG 624U0005 . 2 L 7 4 4F A20WE 2002062600004 20020626 00004 NM 2002 6 26 UPS02438301 1 20020418 A 5320 SUPPORT BRACKET BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FX - STA 1000, 1020, AND 1040 KEEL BEAM PNL SUPPORT BRACKET FOUND CORROSION AT LBL 9 & RBL 9 AREA. CO RROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS. KEEL BEAM PNL SUPPORT BRACKET REPLACE D JUST AT BS 1000 L/R, 1040 RT (TOTAL 3 EA) AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062600005 20020626 00005 NM 2002 6 26 UPS02438302 1 20020423 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C LT BS 340 UPPER DECK FLOORBEAM ONE EACH FASTENER HOLE CRACK REVEALED AT UPPER CHORD LAYER THROUGH THIC KNESS. U/D BS 340 FLOORBEAM UPPER CHORD PARTIALLY REPLACED FROM LBL 35 TO LT MOST O/B IAW HAECO RS R-53-15-34801 AND DW G 141U0044 SHEET 2 FOR REPAIR PARTS INSTALLATION. 2 L 7 4 4F A20WE 2002062600006 20020626 00006 WP 2002 6 26 GTIA020441 1 20020407 A 7120 BEAM DOUG DC9 DC982 3022082 WP LT PYLON BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND LEFT FORWARD UPPER VIBRATION ABSORBER LONG BEAM PRETUNED BROKEN. BROKEN BEAM REMOVED. INSTALLED ABSORBER B EAM PRETUNED. (M) 2 L 7 2 4F A6WE 2002062600007 20020626 00007 2002 6 26 GTIA020488 4 20020502 A 3460 COMPUTER DOUG DC9 DC981 3022081 WP COCKPIT FAILED A GTIA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND DFGS 1 AND 2 RTS FAIL TEST WITH FOLLOWING FAULTS, NOTED AIL MECH TORQUE 1 FAIL, AIL MECH TORQUE 2 FAIL, SPOI LER POSITION FAIL. NR 18 PER POSITION XMITTER. ADJUSTED FLAP POSITION TRANSMITTERS FOR AIL MECH. TORQUE 1 FAIL AND AI L MECH TORQUE 2 FAIL. (M) 2 L 7 2 4F A6WE 2002062600008 20020626 00008 WP 2002 6 26 GTIA020495 1 20020408 A 5247 RAM AIR DOOR DOUG DC9 DC982 3022082 WP APU CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND APU RAM AIR DOOR CRACKED RIGHT HINGE CORNER APPROX .5 INCH. DURING INSTALLATION OF REPAIR, FOUND SKIN CRACK ED LEFT CORNER OF SKIN AT HINGE, BOTH LEFT AND RIGHT STIFFENERS CRACKED AT THROUGH BOLT HOLE AND 2 FT BY 5 INCH PIECE OF METAL TORN OFF L/E OF RIGHT STIFFENER. REMOVED AIR INLET PANEL. INSTALLED NEW AIR INLET PANEL AND ORIGINAL ACTUATOR. (M) 2 L 7 2 4F A6WE 2002062600009 20020626 00009 NM 2002 6 26 MEX2002123 1 20020425 A 2612 285T003219 PANEL BOEING 757 7572Q8 1384972 NM COCKPIT FAILED A ASMF O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SW 23 806AM 26273 FLT 902 - MEX-MTY - AIRCRAFT GOT PLATFORM WITHOUT AUDIBLE FIRE ALARMS. PERFORMED A FIRE DETECTION TEST IAW FIM 26-11-00 AND WEU AUDIBLE SYSTEM TEST IAW FIM 31-51-00. M100 ELECTRONIC CARD WAS CHANGED AND TESTS WERE PERFORMED IAW MM 31-51-0 4. DURING OVERNIGHT SERVICE WAS CHANGED THE FIRE DETECTION PANEL TEST IAW MM 26-11-01. ADDITIONALLY WAS CHANGED THE EL ECTRONIC CARD M618 PER AN OCCASIONAL OF WARNING MASTER FAILING. (M) 2 L 7 2 4F RT A2NM 2002062600010 20020626 00010 2002 6 26 MEX2002136 4 20020305 A 3425 4608000307 COMPUTER DOUG DC9 DC987 3022087 WP COCKPIT FAILED A ASMF O OTHER J WARNING INDICATION CL CLIMB 1 SW 23 214AM 5075 49585 FLT 478 - MZT-HMO - THE CAPTAIN REPORT THAT DURING CLIMB MZT-HMO, THE AIRCRAFT HAD HEADING PROBLEMS. THE FO'S WAS OUT O F SERVICE AND THE FLIGHT DIRECTOR BARS WERE LOST WHEN EFIS BOTH WAS SELECTED ON 1, THE PROBLEM WAS INTERMITTENT DURING A LL THE FLIGHT. AT HMO, WERE VERIFIED THE MEMORIES OF DFGC NR 1 AND 2 AND THE AHRS NR 2 WAS CHANGED. IT WAS TESTED IAW MM 24-20-00. (M) 2 L 7 2 4F RT A6WE 2002062600011 20020626 00011 WP 2002 6 26 MEX2002138 1 20020506 A 7920 699151 FILTER DOUG DC9 DC987 3022087 WP OIL SYSTEM DIRTY A ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 753RA 33459 49587 FLT 501 - MEX-OAX - AIRCRAFT SUSPENDS TAKEOFF AS A CONSEQUENCE OF STRAINER CLOGGING OIL FILTER LIGHT COMES ON. STRAINER FILTER AND SWITCH OIL FILTER WAS REPLACED IAW MM 79-20-06 AND 79-34-01, TESTS OK. (M) 2 L 7 2 4F RT A6WE 2002062600012 20020626 00012 SO 2002 6 26 SIMA200212303 1 20020429 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 615AE 145087 ABI - DURING INSPECTION OF AIRCRAFT, FOUND CENTER HAT BEAM CORRODED THROUGH IN TWO SPOTS. REPLACED CENTER HAT BEAM IAW EMB 145 (SRM 145/1142, CHAPTER 51, REV 17), 51-40-02, GST-1128/02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002062600013 20020626 00013 EU 2002 6 26 SIMA200214113 1 20020517 A 5310 S5367121720402 CREASE BEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP-4 INSPECTION, FOUND LEFT CREASE BEAM WEB WAS FOUND CORRODED BETWEEN FRAMES 39 AND 40. REMOVED AND REP LACED LEFT CREASE BEAM WEB FS 39-40 IAW SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002062600014 20020626 00014 EU 2002 6 26 SIMA200214114 1 20020517 A 5320 S536780020002 SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP 4 INSPECTION, FOUND LEFT MEMBER CORRODED TOP AND BOTTOM SIDES. REMOVED AND REPLACED LEFT Z-MEMBER IAW SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002062600015 20020626 00015 EU 2002 6 26 SIMA200214115 1 20020518 A 5230 S5337129400001 TRACK AEROSP ATR42 ATR42300 8680920 EU CARGO DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP4 INSPECTION, FORWARD CARGO DOOR DRAIN TRACK CORRODED. REMOVED AND REPLACED DRAIN TRACK IAW SRM 52-25- 02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002062600016 20020626 00016 EU 2002 6 26 SIMA200214116 1 20020518 A 5230 S5337129320201 ATTACH FITTING AEROSP ATR42 ATR42300 8680920 EU CARGO DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP4 INSPECTION, FOUND FORWARD CARGO DOOR DRAIN TRACK ATTACH PLATE CORRODED. REMOVED AND REPLACED DRAIN T RACK PLATE IAW SRM 52-25-02 AND 03. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002062600017 20020626 00017 EU 2002 6 26 SIMA200214117 1 20020519 A 5310 S5337300021202 CREASE BEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP4 INSPECTION, FOUND RIGHT CREASE BEAM INBOARD CHORD CORRODED, TOP AND BOTTOM. REPAIRED RIGHT CHORD FRO M FRAME 13-18 IAW ATR 42 SRM NR 53-31-50. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002062600018 20020626 00018 EU 2002 6 26 SIMA200214118 1 20020521 A 3350 3023000 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 545AT 545 MIA - MAINTENANCE REPORTED SEVERAL FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A POWER SUPPLY UNIT IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002062600019 20020626 00019 SO 2002 6 26 SIMA200214201 1 20020517 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - DURING AN IMB MAINTENANCE, FOUND THE CARGO DOOR CUT OUT LOWER SILL CORRODED. REMOVED CORRODED SILL (BEAM). INSTA LLED NEW BEAM IAW EMB 145 (SRM 145/1142, CHAPTER 51, REV 17) 51-40-02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002062600020 20020626 00020 SO 2002 6 26 SIMA200214202 1 20020517 A 5310 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - DURING AN IMBV MAINTENANCE, FOUND FOUR CORRODED NUTPLATES AT PILOTS WINDSHIELD LOWER OUTBOARD CORNER. REMOVED COR RODED NUTPLATES. REAMED BEAM BOLTS HOLES TO .313 INCH TO REMOVE CORROSION. REPAIR DONE IAW EMB GST-1578/02-B, EMB 145 (SRM 145/1142, CHAPTER 51 REV 18) 51-40-02, 51-20-03, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002062600021 20020626 00021 SO 2002 6 26 SIMA200214203 1 20020518 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - DURING IN IMBV MAINTENANCE, FOUND DENT ON LOWER FUSELAGE BETWEEN FRAMES 64 AND 65, AND STRINGERS 21L AND 21R. REM OVED DAMAGED SKIN BY CUT OUT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB 145 (SRM 145/1142, CHAPTER 53, REV 18, GST-1618/02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002062600022 20020626 00022 SO 2002 6 26 SIMA200214204 1 20020519 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - DURING AN IMBV MAINTENANCE, FOUND CORROSION ON SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING. PERFORME D NDT INSPECTION, NO DEFECTS NOTED. FABRICATED THREE REPAIR DOUBLERS. REPAIR DONE IAW EMB GST-1552/02M ITEM NR 4, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002062600023 20020626 00023 SO 2002 6 26 SIMA200214205 1 20020517 A 5320 DOUBLER EMB 145 EMB145LR 3260212 SO AFUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - DURING AN IMBV MAINTENANCE, FOUND CORROSION ON LEFT OMEGA BEAM, PREVIOUS REPAIR, AT FRAME 20. REMOVED PREVIOUS RE PAIR, CORROSION LIMITED TO PREVIOUS REPAIR. FABRICATED A DOUBLER, PLATE AND SHIMS. REPAIR DONE IAW EMB145 SRM 145/1142 , CHAPTER 53 REV 18, 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002062600024 20020626 00024 NE 2002 6 26 SIMA200214401 2 20020521 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT MALFUNCTIONED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 339SB 340B339 GEE785392 CLE - FLT 4836 - DISC - AT CRUISE ALTITUDE OF FL 190', LEFT ENGINE OIL PRESSURE FLUCTUATED 15 TO 20 PSI. OIL PRESSURE D ROPPED APPROX 40 PSI FOR AN UNKNOWN DURATION. CREW SHUT DOWN ENGINE AND DECLARED EMERGENCY AND DIVERTED INTO PIT. REMO VED AND REPLACED LEFT ENGINE ASSY IAW W/C 4903. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2002062600025 20020626 00025 EU 2002 6 26 SIMA200214601 1 20020526 A 3260 328 LIGHT SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A SIMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 21 901AE 340B401 DFW - FLT 3594 - DURING APPROACH CREW REPORTED NO INDICATION FOR LEFT AND RIGHT MAIN LANDING GEAR DOWN AND LOCK LIGHT. APPROACH WAS ABORTED, LANDING GEAR WAS CYCLED TWICE AND THE RIGHT DOWN AND LOCK LIGHT REMAINED OUT. EMERGENCY WAS DECLA RED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LIGHT BULBS IN THE INDICATOR LIGHTS IAW SAAB MM. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002062600026 20020626 00026 SO 2002 6 26 SIMA200214801 1 20020501 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. LEFT CABIN SILL CORRODED FROM FRAME 23 TO 26. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST 1491/02. (M) 2 L 7 2 4T RT T00011AT 2002062600027 20020626 00027 SO 2002 6 26 SIMA200214802 1 20020502 A 5320 14525422007 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. RIGHT SILL IN CARGO IS CORRODED BETWEEN FRAME 68-71. REMOVED AND REPLACED RIGHT CARGO SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002062600028 20020626 00028 SO 2002 6 26 SIMA200214803 1 20020502 A 5320 14571033003 CROSSBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. RIGHT CROSSMEMBER IN CARGO IS CORRODED. REMOVED CORROSION AND PERFORMED NDT. FOUND T O BE ACCEPTED AS IS IAW EMB GST-1491/02. (M) 2 L 7 2 4T RT T00011AT 2002062600029 20020626 00029 SO 2002 6 26 SIMA200214804 1 20020502 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. LEFT FORWARD SILL IN CARGO IS CORRODED. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPT ED AS IS IAW EMB GST-1491/02. (M) 2 L 7 2 4T RT T00011AT 2002062600030 20020626 00030 SO 2002 6 26 SIMA200214805 1 20020502 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. LEFT BEAM GUSSET IN CARGO IS CORRODED AT FRAME 61. BLENDED AND PERFORMED NDT, FOUND T O BE ACCEPTED AS IS IAW EMB GST-1491/02. (M) 2 L 7 2 4T RT T00011AT 2002062600031 20020626 00031 SO 2002 6 26 SIMA200214806 1 20020503 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. GALLEY CENTER FLOOR SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT IAW EMB 145 SRM 51 -20-01, 51-20-03, 51-40-01, 51-40-02, 51-40-04, 51-40-07. (M) 2 L 7 2 4T RT T00011AT 2002062600032 20020626 00032 SO 2002 6 26 SIMA200214807 1 20020501 A 5311 12010732001 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. RIGHT PROFILE AT FRAME 23 IS CORRODED. REMOVED AND INSTALLED SERVICEABLE PROFILE IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002062600033 20020626 00033 SO 2002 6 26 SIMA200214808 1 20020501 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. FORWARD AND AFT DIAMOND GUSSET ARE CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002062600034 20020626 00034 SO 2002 6 26 SIMA200214809 1 20020501 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. LAVATORY LEFT SILL IS CORRODED. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491-02. (M) 2 L 7 2 4T RT T00011AT 2002062600035 20020626 00035 SO 2002 6 26 SIMA200214810 1 20020501 A 5320 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. CENTER GUSSET IN LAVATORY IS CORRODED. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTE D AS IS IAW EMB GST-1491/02. (M) 2 L 7 2 4T RT T00011AT 2002062600036 20020626 00036 SO 2002 6 26 SIMA200214811 1 20020501 A 5320 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. RIGHT GUSSET IN LAVATORY IS CORRODED. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491/02. (M) 2 L 7 2 4T RT T00011AT 2002062600037 20020626 00037 SO 2002 6 26 SIMA200214812 1 20020501 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. RIGHT CABIN SILL CORRODED BETWEEN FRAMES 53 AND 55. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491/02. (M) 2 L 7 2 4T RT T00011AT 2002062600038 20020626 00038 SO 2002 6 26 SIMA200214813 1 20020501 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. RIGHT CABIN SILL BETWEEN FRAMES 28 AND 34 IS CORRODED. BLENDED AND PERFORMED NDT, FOU ND TO BE ACCEPTED AS IS IAW EMB GST-1491/02. (M) 2 L 7 2 4T RT T00011AT 2002062600039 20020626 00039 SO 2002 6 26 SIMA200214814 1 20020501 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. RIGHT CABIN SILL CORRODED BETWEEN FRAMES 24 AND 28. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST 1491/02. (M) 2 L 7 2 4T RT T00011AT 2002062600040 20020626 00040 SO 2002 6 26 SIMA200214815 1 20020501 A 5347 SEAT TRACK EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. RIGHT SEAT TRACK PROFILE HAS CORROSION BETWEEN FRAMES 24 AND 29. BLENDED AND PERFORME D NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491/02. (M) 2 L 7 2 4T RT T00011AT 2002062600041 20020626 00041 SO 2002 6 26 SIMA200214816 1 20020502 A 5320 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 145086 ABI - THIS IS A LEVEL 2 FINDING. RIGHT BEAM GUSSET IN CARGO IS CORRODED. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPT ED AS IS IAW EMB GST-1491/02. (M) 2 L 7 2 4T RT T00011AT 2002062600042 20020626 00042 SO 2002 6 26 SIMA200214817 1 20020502 A 5320 14522461011 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AE 145328 ABI - THIS IS A LEVEL 2 FINDING. FORWARD DIAMOND GUSSET CORRODED AT FRAME 20. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002062600043 20020626 00043 SO 2002 6 26 SIMA200214818 1 20020502 A 5320 14522459003 SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AE 145328 ABI - THIS IS A LEVEL 2 FINDING. RAMP SUPPORT CORRODED AT FRAME 20. INSTALLED SERVICEABLE RAMP IAW EMB 145 SRM 51-40-0 2. (M) 2 L 7 2 4F RT T00011AT 2002062600044 20020626 00044 SO 2002 6 26 SIMA200214819 1 20020502 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AE 145328 ABI - THIS IS A LEVEL 2 FINDING. LEFT OMEGA BEAM CORRODED AT FRAME 20. BLENDED AND TREATED CORROSION IAW EMB GST-1472/ 02. (M) 2 L 7 2 4F RT T00011AT 2002062600045 20020626 00045 SO 2002 6 26 SIMA200214820 1 20020502 A 5320 14529603003 CROSSBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AE 145328 ABI - THIS IS A LEVEL 2 FINDING. FLOOR EXTENSION CROSSMEMBER CORRODED AT FRAME 22. REMOVED AND REPLACED CROSSMEMBER IA W EMB 135 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002062600046 20020626 00046 WP 2002 6 26 ABXA020002 1 20020624 A 7931 1G1741A SWITCH DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE # 1 ENGINE DEFECTIVE A ABXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 849AX 45891 669226 # 1 engine low oil pressure light on in flight. Oil pressure was 46 psi. Engine was shut down at 0905 Z. Windmilling oil pressure on secured engine was 12 psi for 19 minutes. Replaced low pressure switch IAW DC-8 MM 79-30. Ran # 1 engine, no leaks noted. Engine indication normal. Replaced # 1 engine main oil filter, leak checked good. 2 L 7 4 4F 4 F 4A25 1E8 2002062600047 20020626 00047 SO 2002 6 26 SIMA200214821 1 20020502 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 728AE 145328 ABI - THIS IS A LEVEL 2 FINDING. CENTER BEAM GUSSET CORRODED AT FRAME 20. REMOVED AND INSTALLED NEW CENTER BEAM IAW EM B 135 SRM 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2002062600048 20020626 00048 EU 2002 6 26 SIMAW00212302 1 20020501 A 5542 S55476000018 SKIN AEROSP ATR42 ATR42300 8680920 EU RUDDER CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - RUDDER HAS AN APPROX 4 INCH CRACK ON LEFT SIDE AND APPROX 1.5 INCH CRACK ON RIGHT SIDE WHERE BALANCE ARM FOR RUDDE R TAB PASSES THROUGH IT. RUDDER REPAIRED IAW EO E1-55MR-012. (M) 2 H 7 2 4T RT A53EU 2002062600049 20020626 00049 NM 2002 6 26 USAABB02056 1 20020505 A 3350 8731002511REV15 SIGN BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 600AU 22192 LAX - FOUND L2 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002062600050 20020626 00050 NM 2002 6 26 USAABB02057 1 20020505 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 600AU 22192 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002062600051 20020626 00051 NM 2002 6 26 USAABB02058 1 20020505 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002062600052 20020626 00052 NM 2002 6 26 USAABB02059 1 20020504 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 630AU 27808 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002062600053 20020626 00053 NM 2002 6 26 USAABB02060 1 20020507 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 622AU 27201 PHL - FOUND LOW LEVEL EMERGENCY LIGHTS AT ROWS, 1, 4, 6, 9, 13, 18, 23, 26 AND 33 DIM. MAINTENANCE REPLACED THE BATTERI ES. (M) 2 L 7 2 4F RT A2NM 2002062600054 20020626 00054 2002 6 26 USAASB02030 4 20020210 A 3418 861CAS3 VANE BOEING 737 737401 1384701 NM STALL WARNING DAMAGED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 408US 35243 23878 BUF - FLT 437 - ON ROTATION OUT OF BUF, EN ROUTE TO PHL, THE FIRST OFFICER REPORTED THE AIRCRAFT WENT INTO A CONTINUOUS STICK SHAKER MODE. CAPTAIN CHECKED FLAP SETTINGS AND FOUND NO INDICATIONS OF ANY OTHER ABNORMALITIES OTHER THAN THE STI CK SHAKER WARNING. CAPTAIN TOOK CONTROL OF THE AIRCRAFT, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT BUF WHERE THE F LIGHT LANDED WITHOUT FURTHER INCIDENT. ONCE AT THE GATE, THE LEFT STALL WARNING VANE WAS FOUND BENT AND HANGING FROM TH E AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE DAMAGE LEFT ANGLE OF ATTACH STALL WARNING VANE PER MM 27-32-11. OPERA TIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002062600055 20020626 00055 NM 2002 6 26 USAASB02083 1 20020427 A 3397 WIRE BOEING 737 7374B7 1384702 NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 443US 24842 BUF - FOUND EMERGENCY LIGHT AT ROW 25 LEFT INOPERATIVE. MAINTENANCE REPAIRED A WIRE AT THE SEAT ROW. (M) 2 L 7 2 4F RT A16WE 2002062600056 20020626 00056 NM 2002 6 26 USAASB02088 1 20020504 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 530AU 24412 SYR - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHT AT SEAT ROW 10C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002062600057 20020626 00057 NM 2002 6 26 USAASB02089 1 20020504 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 785AU 25024 EWR - MAINTENANCE FOUND THE BULLNOSE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 14 AND 18 RIGHT SIDE AND 16 AND 24 LEFT S IDE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK ABOVE CABIN CEILING PANEL AT SEAT ROW 20. OPERATIONAL CHECK GOO D. (M) 2 L 7 2 4F RT A16WE 2002062600058 20020626 00058 WP 2002 6 26 CALA0200365 1 20020625 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FS 428-440 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND FORWARD CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN FS 428 AND 440 AT S29R. A REPAIR WAS INSTALLED I AW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002062600059 20020626 00059 NM 2002 6 26 CALA0200366 1 20020625 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM STA 787-801 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17345 23583 INSPECTION FOUND CHANNEL CORRODED UNDER NUT PLATE BETWEEN STA 787 AND 801, RBL 9. THE CHANNEL WAS REPAIRED IAW SRM 53-00 -53, FIGURE 201. 2 L 7 2 4F RT A16WE 2002062600060 20020626 00060 NM 2002 6 26 UPS02438305 1 20020425 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 1220 LBL 96 LONGITUDINAL FLOOR SUPPORT TRACK SUPPORT WEB BOTTOM -T- CHORD HEAVY CORROSION. F LOOR LONGITUDINAL TRACK BOTTOM CHORD REPAIRED PER RS R53-45-34793. BEYOND SRM 53-10-01 ALLOWABLE. 2 L 7 4 4F A20WE 2002062600061 20020626 00061 NM 2002 6 26 UPS02438307 1 20020422 A 5714 SKIN BOEING 747 747123 1384873 NM CENTER WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - WING CENTER SECTION SURFACE FOUND CORRODED. WING CENTER SECTION CORRODED SKIN REPAIRED AT BS 12 20 LBL 97 AS PER RS R57-14-34799. 2 L 7 4 4F A20WE 2002062600062 20020626 00062 NM 2002 6 26 UPS02438308 1 20020422 A 5312 BULKHEAD BOEING 747 747123 1384873 NM FUSELAEG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 2141 RBL 76 CANT PRESSURE DECK FOUND CORRODED. BOND SKIN TRIMMED AS PER SRM 51-10-01. REPAI R PARTS FABRICATED AS PER RS R53-48-34796. 2 L 7 4 4F A20WE 2002062600063 20020626 00063 NM 2002 6 26 UPS02438309 1 20020422 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C U/D - BS 760 STR 6-8R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04. 2 L 7 4 4F A20WE 2002062600064 20020626 00064 NM 2002 6 26 UPS02438310 1 20020416 A 5312 BULKHEAD BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C RT SIDE TUNNEL BS 400 BULKHEAD O/B CORNER RADIUS FOUND CRACK AT S31R. RT SIDE TUNNEL BS 400 BULKHEAD O/B CORNER RADIUS REPAIRED AS PER SRM ADDENDUM 53-10 EO B747-5310-4659-B. 2 L 7 4 4F A20WE 2002062600065 20020626 00065 NM 2002 6 26 UPS02438311 1 20020416 A 5312 BULKHEAD BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C LT SIDE TUNNEL BS 400 BULKHEAD O/B CORNER RADIUS FOUND CRACK AT S31L. LT SIDE TUNNEL BS 400 BULKHEAD O/B CORNER RADIUS REPAIRED AS PER SRM ADDENDUM 53-10 EO B747-5310-4659-B. 2 L 7 4 4F A20WE 2002062600066 20020626 00066 NM 2002 6 26 UPS02438324 1 20020419 A 5320 SUPPORT BRACKET BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FX - STA 1063, LBL 9 KEEL BEAM PANEL SUPPORT BRACKET FOUND CORRODED. KEEL BEAM PNL SUPPORT BRACKET RE PLACE JUST AT BS 1063 LBL 9. 2 L 7 4 4F A20WE 2002062600067 20020626 00067 NM 2002 6 26 UPS02438325 1 20020419 A 5320 SUPPORT BRACKET BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FX - STA 1063 AND STA 1103, RBL 9 KEEL BEAM PNL SUPPORT BRACKET FOUND CORRODED. KEEL BEAM PNL SUPPORT BRACKET REPLACE JUST AT BS 1063, 1103 RBL 9 (TOTAL 2 EA). 2 L 7 4 4F A20WE 2002062600068 20020626 00068 NM 2002 6 26 UPS02438326 1 20020419 A 5320 ATTACH ANGLE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FX - STA 1083 LBL 3 - RBL 3 KEEL BEAM PNL SUPPORT FOUND CORRODED. TWO EACH ATT ANGLE REPLACED AT FX S TA 1083 LBL 3 - RBL 3 AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062600069 20020626 00069 NM 2002 6 26 UPS02438327 1 20020419 A 5320 SUPPORT BRACKET BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FX - LBL 9, STA 1177 AND 1223 KEEL BEAM PNL SUPPORT BRACKET FOUND CORRODED. KEEL BEAM PNL SUPPORT BRA CKET REPLACE JUST AT BS 1177, 1223 LBL 9. 2 L 7 4 4F A20WE 2002062600070 20020626 00070 NM 2002 6 26 UPS02438328 1 20020419 A 5320 SUPPORT BRACKET BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FX - STA 1177, 1201 AND 1223, RBL 9 KEEL BEAM PNL SUPPORT BRACKET FOUND CORRODED. KEEL BEAM PNL SUPPO RT BRACKET REPLACE JUST AT RBL 1177, 1223, RBL 9. 2 L 7 4 4F A20WE 2002062600071 20020626 00071 NM 2002 6 26 UPS02438329 1 20020419 A 5310 WINDOW FRAME BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - STA 580 - 620 S20R TO 22R WINDOW FORGINGS MATING SURFACE EDGE FOUND CORRODED. BS 580 - BS 600 R T SIDE WINDOW FORGING REPAIR. 2 L 7 4 4F A20WE 2002062600072 20020626 00072 NM 2002 6 26 UPS02438330 1 20020426 A 5310 WINDOW FRAME BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 1840 - 1860 RT BETWEEN S-20R AND S-22R WINDOW FORGINGS FOUND CORRODED AFTER NRC RECTIFICATION . REPAIR WINDOW FORGING AT M/D BS 1840 - 1860 RT BTN S20R - 22R. 2 L 7 4 4F A20WE 2002062600073 20020626 00073 NM 2002 6 26 UPS02438331 1 20020502 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO COMPT - BS 700 S28R AREA FRAME I/B CHORD CORRODED. BS 700 RIGHT FRAME CRACK REPAIR AT S28R AS PER RS R-53-22-34798 & EA 747-53-20067. 2 L 7 4 4F A20WE 2002062600074 20020626 00074 NM 2002 6 26 DHL2002745501 1 20020603 A 5710 651628912 FITTING BOEING 727 727224 1384076 NM CRACKED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 During C Check "Discrepancy"- R/H Wing rear spar O/B attach fitting crackecked ( Gear beam attach fitting).1) Removed R/ Wing R/spar O/B attach fitting for main gear beam I.A.W. B-727 S/B 57-167 R2.2) Drilled-up new replacement fitting P/N 6 5-16289-12 per B-727 S/B 57-167 R2.3) Treated and primed Aft. spar of R/Wing area of attach fitting mating surface per B -727 SRM 51-10-2.4) Installed and sealed new fitting and fasteners I.A.W. B-727 S/B 57-167 R2 and B-727 SRM 51-20-4.5) R emoved and replaced all three bushings in main gear beam O/B end, FWD. and AFT. gear beam O/B attach fitting I.A.W. B-72 7 S/B 57-167R2.6) Accomplished B-727 S/B 57-153 replacement of attach pin and fuel jettison valve. 2 L 7 3 4F A3WE 2002062600075 20020626 00075 NM 2002 6 26 UPS02438332 1 20020425 A 5320 SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 1241 - 1265 RBL 34 SLOPE CANTED BULKHEAD LONGITUDINAL FLOOR TRACK SUPPORT BOTTOM -T- CHORD FI NDING HEAVILY CORRODED. M/D BS 1241 - 1265 RBL 34 LONGITUDINAL FLOOR TRACK BOTTOM -T- CHORD REPLACED IAW SRM 51-10-01 P AGE 8. 2 L 7 4 4F A20WE 2002062600076 20020626 00076 NM 2002 6 26 UPS02438333 1 20020422 A 5330 144U00312 PANEL BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 1241 RT CLOSURE PNL FOUND CRACKED. CLOSURE PANEL REPLACED PER EO B747-5310-2758-E APPENDICES -E- AT RT SIDE ONLY. 2 L 7 4 4F A20WE 2002062600077 20020626 00077 NM 2002 6 26 UPS02438334 1 20020428 A 5754 65B101495 RIB BOEING 747 747123 1384873 NM L/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C DURING LHW NR 9 L/E FLAP GREASE LUBE AS NR 3 ROTARY ACTUATOR (COUNT FROM O/B) REMOVED, L/E RIB O/B FWD AREA FOUND CORROSION AT ILES 800. L/E RIB AT ILES 800 IS REPLACED AS PER SRM 51-10-01. CORROSION FOUND CRACKED THROUG H AT 2 LOCATIONS. 2 L 7 4 4F A20WE 2002062600078 20020626 00078 NM 2002 6 26 UPS02438337 1 20020423 A 5320 65B169521 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C 3 EA FASTENER HOLES FOUND CRACK ON THE BATH TUB FITTING OF LT SIDE BS 980 STR 38L. LT STA 980 S38L BA THTUB FITTING REPAIRED AS PER RS R53-23-34791. A PERMANENT REPAIR TO THE BATHTUB FITTING IS TO BE ACCOMPLISHED WITHIN 1 8 MONTHS. CONTINUE INSPECTION PLANS ON THE LT SIDE PER SB B747-53A2362 & SB 747-53A2444 AS PER UPS EO B747-5310-16873-A . 2 L 7 4 4F A20WE 2002062600079 20020626 00079 NM 2002 6 26 UPS02438346 1 20020418 A 5730 PANEL BOEING 747 747123 1384873 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C RHW - UPPER WING L/E AREA PNL BULGE UP AT WS 1410 - 1430. RHW UPPER SKIN AT OLES 1430 - 1450 L/E AREA IS REPAIRED AS PER RS R-57-25-34803. 2 L 7 4 4F A20WE 2002062600080 20020626 00080 SO 2002 6 26 C2XA02CL134 1 20020625 A 3260 23092137004 TARGET EMB 145 EMB145 3260210 SO MAIN GEAR OUT OF ADJUST A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15973 145159 CLE FLIGHT#3311 THE CREW REPORTED A LANDING GEAR AIR/GROUND SYSTEM FAILURE AFTER TAKEOFF.THE AIRCRAFT RETURNED TO CLEVEL AND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND ADJUSTED THE LEFT AND RIGHT MAIN LANDING GEAR WOW PROX IMITY SWITCH FRONT TARGETS.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS TEST FLOWN GOOD.RELEASED BACK TO SERVICE.LEFT F RONT TARGET P/N 2309-2137-003 2 L 7 2 4F RT T00011AT 2002062600081 20020626 00081 NM 2002 6 26 UPS02438347 1 20020422 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 1241 RBL 76 CANT PRESSURE DECK FOUND CORRODED. BLEND OUT CORROSION DEPTH 0.015, WIDTH 4", LE NGTH 6". THE BONDED DOUBLER REPAIRED AS PER HAECO RS R-53-48-34796. THIS REPAIR IS CONSIDERED TIME-LIMITED TO 24 MONTH S UNTIL AN IMPROVED DRAINAGE MOD SHOULD BE PERFORMED IAW BOEING SB 747-51A2054 REV 1 AS PER UPS EO B747-5310-16853-A. 2 L 7 4 4F A20WE 2002062600082 20020626 00082 NM 2002 6 26 UPS02438348 1 20020422 A 5312 BULKHEAD BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C M/D - BS 1241 RBL 35 CANTED PRESSURE BULKHEAD FOUND CRACKED. RT WLG W/W CANTED BULKHEAD WEB REPAIRED AT BS 1241 RBL 16 - RBL 47 AS PER RS R-53-48-34796. 2 L 7 4 4F A20WE 2002062600083 20020626 00083 NM 2002 6 26 UPS02438349 1 20020422 A 5312 BULKHEAD BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C RT WLG W/W CANTED BULKHEAD WEB CORRODED AROUND DRAIN HOSE ADAPTOR AT BS 1241 - 1243 RBL 36 - 39. REPA IRED AS PER HAECO RS R-53-48-34796. THE REPAIR IS CONSIDERED TIME-LIMITED TO 24 MONTHS UNTIL AN IMPROVED DRAINAGE MODI FICATION CAN BE INSTALLED IAW BOEING SB 747-51A2054 REV 1 AS PER UPS EO B747-5310-16853-A. 2 L 7 4 4F A20WE 2002062600084 20020626 00084 NM 2002 6 26 UPS02438351 1 20020422 A 5230 DOOR FRAME BOEING 747 747123 1384873 NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO DOOR BS 575 BETWEEN NR 1, NR 3 FRAME UPPER MASTER LATCH T/T INTERIOR AREA FOUND CORROSION (C OUNT FROM FWD) AS MARKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT NOT WITHIN SRM LIMIT 52-00-02 FIG 1. FWD CARGO DOOR INTERIOR LWR BEAM REPAIRED AT BS 575 BETWEEN NR 1 & NR 2 FRAME AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002062600085 20020626 00085 NM 2002 6 26 UPS02438352 1 20020422 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C RT WLG W/W PRESSURE DECK WEB CORROSION AT BS 1341 - 1343 RBL 54 - 56. CORROSION REMOVED IAW 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1. 2 L 7 4 4F A20WE 2002062600086 20020626 00086 NM 2002 6 26 UPS02438353 1 20020422 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C RT WLG W/W PRESSURE DECK PANEL CORROSION AT RBL 56 - 58 BS 1342 - 1344. CORROSION REMOVED IAW SRM 51- 10-01, BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1. PRESSURE DECK WEB REPAIRED AS PER SRM 53-10-07 FIG 2. 2 L 7 4 4F A20WE 2002062600087 20020626 00087 NM 2002 6 26 UPS02438355 1 20020521 A 3350 LIGHT BOEING 747 747123 1384873 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:N/A OVERHEAD EMERGENCY LIGHT STA 405 ONLY REMAINS ILLUMINATED FOR APPROX 5 SEC. REMOVED AND REPLACED LI GHT PACK ASSY, OPS NORMAL. 2 L 7 4 4F A20WE 2002062600088 20020626 00088 NM 2002 6 26 UPS02438357 1 20020519 A 5414 SKIN BOEING 747 747200 1384847 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:N/A NR 3 ENG SLOT SEAL AREA PYLON SKIN CRACK I/B SIDE REF D238005 AND REF LP702147. NR 3 ENG SLOT SEAL AREA PYLON SKIN REPAIRED AS PER HAECO RS R-54-51-34 826 & UPS EO 747-54-20019. 2 L 7 4 4F RT A20WE 2002062600089 20020626 00089 NE 2002 6 26 UPS02438377 2 20020522 A 7200 JT9D7Q ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE NR 2 MALFUNCTIONED A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING M E OVER TEMP VIBRATION/BUFFET CR CRUISE 1 SO 01 526UP 21937 702097 INSPECTION TYPE:N/A ATB NR 2 ENG OVERTEMP, VIBRATION (IFSD) CREW DECLARED EMERGENCY. REMOVED AND REPLACED NR 2 ENGINE I AW TC NO 5000 LEAK AND OPS CHECK NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 2002062600090 20020626 00090 NM 2002 6 26 UPS02438393 1 20020510 A 5320 654U6075594 ANGLE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C NOSE W/W INTERIOR TOP SURFACE LONGITUDINAL BEAM FOUND CRACKED AT BS 320 LBL 22. ANGLE REPLACED AND IN STALLED AS PER SRM 51-10-01 PG 08 & 51-30-02. 2 L 7 4 4F A20WE 2002062600091 20020626 00091 NM 2002 6 26 UPS02438394 1 20020510 A 5347 BAC15201566 SEAT TRACK BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D SEAT TRACK FOUND CORROSION CRACK. SEAT TRACK REPLACED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002062600092 20020626 00092 NM 2002 6 26 UPS02438395 1 20020506 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT-BS 920 S40R AREA SHEAR TIE CRACK. SHEAR TIE REPAIRED AS PER SRM 53-10-4 FIG 4. 2 L 7 4 4F A20WE 2002062600093 20020626 00093 NM 2002 6 26 UPS02438396 1 20020508 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO - BS 900 RT FRAME BETWEEN STR - 28R AND STR 29R FOUND CRACKED. FWD CARGO BS 900 RT FRAME BE TWEEN STR -28R & 29R REPAIRED AS PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2002062600094 20020626 00094 NM 2002 6 26 UPS02438397 1 20020510 A 5347 BAC15201566 SEAT TRACK BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D- SEAT TRACK FOUND CRACK BS 460 RBL R88. SEAT TRACK REPLACED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002062600095 20020626 00095 CE 2002 6 26 SQ7A032002 1 20020102 A 5315 FLOORBEAM BOEING 75 A75N1 1380134 CE FUSELAGE CORRODED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282 753789 YXD - DURING SCHEDULED MAINTENANCE CORROSION WAS FOUND T- EXTRUSION AT BS 720F LBL 10 RBL 10. REPLACED T SECTION PER SR M 51-20-1 & 51-30-1. 1 Q 7 1 3R A743 2002062600096 20020626 00096 NM 2002 6 26 UPS02438398 1 20020510 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D-BS 360 STR 14- 14AL FRAME WEB FOUND CRACK. FRAME WEB REPAIRED AS PER SRM 51-40-03 FIG 3. 2 L 7 4 4F A20WE 2002062600097 20020626 00097 NM 2002 6 26 UPS02438399 1 20020508 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO - BS 680 RT FRAME FOUND CRACKED BETWEEN STR 39R AND STR 40R. FRAME REPAIRED AS PER RS R-53- 22-34809. 2 L 7 4 4F A20WE 2002062600098 20020626 00098 NM 2002 6 26 UPS02438400 1 20020508 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO - BS 880 RT FRAME BETWEEN STR 30R AND STR 31R FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-1 0-04 FIG 4. 2 L 7 4 4F A20WE 2002062600099 20020626 00099 NM 2002 6 26 UPS02438401 1 20020512 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D SEAT TRACK FOUND CORROSION AT BS 2224 LBL 90. CORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT W ITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR SRM FIG 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002062600100 20020626 00100 NM 2002 6 26 UPS02438402 1 20020507 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C COCKPIT- FLOORBEAM FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-1 0-01 FIG 1 LIMITS, FOR REPAIR REF SRM FIG 53-10-07 FIG 23. 2 L 7 4 4F A20WE 2002062600101 20020626 00101 NM 2002 6 26 SQ7A042002 1 20020102 A 5320 NA ANGLE BOEING 727 727251 138408H NM CORRODED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - During scheduled maintenance corrosion was found on the T angle @ BS760, LBL 6 - RBL 6.Replaced T extrusion per SR M 53-20-1 & 53-30-1. 2 L 7 3 4F A3WE 2002062600102 20020626 00102 NM 2002 6 26 SQ7A052002 1 20020201 A 5320 ANGLE BOEING 727 727251 138408H NM CORRODED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - During scheduled maintenance the angle at BS740 - 759 was found corroded.Replaced angle per SRM 51-20-1 & 51-30-1. 2 L 7 3 4F A3WE 2002062600103 20020626 00103 NM 2002 6 26 UPS02438407 1 20020512 A 5320 65B140561 SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX-KEEL BEAM PANEL SUPPORT LOWER CHORD UPPER AND LOWER SURFACE FOUND SURFACE CORROSION AT STA 1287 RBL 16 TO LBL 16. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS FOR REPLACEMENT REFER TO S RM FIG 51-10-01. 2 L 7 4 4F A20WE 2002062600104 20020626 00104 NM 2002 6 26 UPS02438408 1 20020512 A 5320 65B140562 SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX- KEEL BEAM PANEL SUPPORT LOWER CHORD UPPER AND LOWER SURFACE FOUND SURFACE CORROSION AT STA 1307 LB L 16 TO RBL 16. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002062600105 20020626 00105 NM 2002 6 26 UPS02438409 1 20020512 A 5320 65B15085886 SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX- STA 1480 KEEL BEAM PANEL SUPPORT LOWER SURFACE FOUND SURFACE CORROSION AT LBL 17 TO RBL 17 (AS MAR K). CORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51- 10-01 PG 8. 2 L 7 4 4F A20WE 2002062600106 20020626 00106 NM 2002 6 26 UPS02438410 1 20020514 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT- RT BS 960 BETWEEN S38R - 39R FOUND FRAME SHEAR TIE 1 EA HOLE CRACK APPROX .25 INCH LO NG. FWD CARGO RT BS 960 BETWEEN S38R-39R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2002062600107 20020626 00107 NM 2002 6 26 UPS02438411 1 20020514 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT - LT BS 960 BETWEEN S38L FOUND FRAME SHEAR TIE 2 EA HOLES CRACK. FWD CARGO COMPT LT B S 960 BETWEEN S38L - 39L FRAME SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2002062600108 20020626 00108 NM 2002 6 26 UPS02438413 1 20020509 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C AFT CARGO - BS 1660-1680 LBL 20-40 FLOORBEAM SURFACE WEB FOUND CRACKED. AFT CARGO - BS 1660-1680 LBL 20-40 FLOORBEAM SURFACE WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002062600109 20020626 00109 NM 2002 6 26 UPS02438414 1 20020512 A 5320 69B118571 BRACKET BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX- BS 1205 RT SIDE KEEL BEAM PANEL ATT BRACKET FOUND SURFACE CORROSION AS MARK. CORROSION REMOVED IA W SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS FOR REPLACEMENT REFER TO SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002062600110 20020626 00110 NM 2002 6 26 UPS02438415 1 20020512 A 5320 69B118571 BRACKET BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX-RT KEEL BEAM BOX SUPPORT PANEL ATT BRACKET FOUND SURFACE CORROSION AT BS 1098 RBL 9. CORROSION REM OVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002062600111 20020626 00111 NM 2002 6 26 UPS02438416 1 20020514 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT- BS 980 LT STR 38 FOUND CRACK. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062600112 20020626 00112 NM 2002 6 26 UPS02438417 1 20020510 A 5320 69B105011 FITTING BOEING 747 747121 1384871 NM FUSELAGE DETERIORATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C AFT CARGO - BS 1480 STR 51R STRINGER FWD FITTING FOUND DETERIORATED. STRING END FITTING REPLACED AS P ER SRM 51-10-01. 2 L 7 4 4F A20WE 2002062600113 20020626 00113 NM 2002 6 26 UPS02438418 1 20020506 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT - BS 980 S46L FRAME CRACK. FWD CARGO COMPT BS 980 S46L FRAME CRACKED AREA REPAIRED AS PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2002062600114 20020626 00114 NM 2002 6 26 UPS02438419 1 20020510 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C AFT CARGO BS 1800 BETWEEN STR 48R & STR 49R SHEAR TIE FOUND CRACKED. AFT CARGO BS 1800 BETWEEN STR 48 R & STR 49R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A. 2 L 7 4 4F A20WE 2002062600115 20020626 00115 NM 2002 6 26 UPS02438420 1 20020510 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C AFT CARGO - BS 1800 BETWEEN STR 47R & STR 48R SHEAR TIE FOUND CRACKED. AFT CARGO BS 1800 BETWEEN STR 47R & STR 48R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A. 2 L 7 4 4F A20WE 2002062600116 20020626 00116 NM 2002 6 26 UPS02438421 1 20020510 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C AFT CARGO - BS 1680 BETWEEN STR 50R & STR 51R SHEAR TIE FOUND CRACKED AFT CARGO BS 1680 BETWEEN STR 50 R & STR 51R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2002062600117 20020626 00117 NM 2002 6 26 UPS02438422 1 20020510 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C AFT CARGO BS 1900 BETWEEN STR 43L TO STR 47L SHEAR TIE FOUND CRACKED. AFT CARGO BS 1900 BETWEEN STR 4 3L TO STR 47L SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A. 2 L 7 4 4F A20WE 2002062600118 20020626 00118 NM 2002 6 26 UPS02438423 1 20020520 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C AFT CARGO COMPT- BS 1900 BETWEEN STR 51L TO 51R SHEAR TIE FOUND CRACKED. AFT CARGO COMPT- BS 1900 BET WEEN STR 51L TO 51R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A. 2 L 7 4 4F A20WE 2002062600119 20020626 00119 NM 2002 6 26 UPS02438424 1 20020509 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C AFT CARGO - BS 1660 BETWEEN STR 47R & STR 48R SHEAR TIE FOUND CRACKED. AFT CARGO - BS 1660 BETWEEN ST R 47R & STR 48R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2002062600120 20020626 00120 NM 2002 6 26 UPS02438425 1 20020510 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C AFT CARGO - BS 1760 BETWEEN STR 48R & STR 49R SHEAR TIE FOUND CRACKED. AFT CARGO BS 1760 BETWEEN STR 48R & STR 49R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A. 2 L 7 4 4F A20WE 2002062600121 20020626 00121 NM 2002 6 26 UPS02438426 1 20020510 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C AFT CARGO - BS 1680 BETWEEN STR 49R & STR 50R SHEAR TIE FOUND CRACKED. AFT CARGO - BS 1680 BETWEEN ST R 49R & STR 50R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A. 2 L 7 4 4F A20WE 2002062600122 20020626 00122 NM 2002 6 26 UPS02438427 1 20020506 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT- BS 960 41R AREA SHEAR TIE CRACK. SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 40. 2 L 7 4 4F A20WE 2002062600123 20020626 00123 NM 2002 6 26 UPS02438428 1 20020513 A 5320 FLOOR SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D- FLOOR SUPPORT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLENDOUT NOT WITHIN SRM 53-10 -01 FIG 1 LIMITS, FOR REPAIR REFER SRM FIG 51-40-04 FIG 1. 2 L 7 4 4F A20WE 2002062600124 20020626 00124 NM 2002 6 26 UPS02438429 1 20020512 A 5320 BRACKET BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX- BS 1183 RT SIDE KEEL BEAM PANEL ATT BRACKET FOUND SURFACE CORROSION AS MARK. CORROSION REMOVED IA W SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002062600125 20020626 00125 NM 2002 6 26 UPS02438430 1 20020509 A 5311 65B0793460 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C NOSE WHEEL WELL FWD BULKHEAD VERTICAL FRAME CHORD FOUND CRACKED AT BS 260 RBL 11 NR 2 LATERAL BEAM (CO UNT FROM TOP). FRAME CHORD REPLACED AS PER SRM 51-10-01 PG 08 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2002062600126 20020626 00126 NM 2002 6 26 UPS02438431 1 20020514 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT- RT BS 980 STR 37 FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062600127 20020626 00127 NM 2002 6 26 UPS02438432 1 20020515 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C, BS 980 RT FWD UPPER DRAG SPLICE FITTING FOUND MOST AFT HOLE AT SKIN ATTACH FLANGE CRACKED RUNNING FWD APPROX .0625 INCH LONG. HOLE OVERSIZED TO 0.278 INCH PER SRM 51-30-05 WITHIN SRM 53-30-03 FIG 60 LIMITATIONS. 2 L 7 4 4F A20WE 2002062600128 20020626 00128 NM 2002 6 26 UPS02438433 1 20020506 A 5320 CLIP BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C NWW TUNNEL - RT BS 280 VERTICAL BEAM NR 2 STIFFENER CLIP (COUNT FROM TOP) FOUND CRACKED. NR 2 STIFFEN ER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 8 AND 51-30-02. 2 L 7 4 4F A20WE 2002062600129 20020626 00129 NM 2002 6 26 UPS02438434 1 20020506 A 5320 CLIP BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C NWW TUNNEL - LT BS 300 VERTICAL BEAM NR 4 STIFFENER CLIP FOUND CRACKED (COUNT FROM TOP). CLIP REPLACE D AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002062600130 20020626 00130 NM 2002 6 26 UPS02438435 1 20020506 A 5320 CLIP BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C NWW TUNNEL - LT BS 320 VERTICAL BEAM NR 2 STIFFENER CLIP FOUND CRACKED. CLIP REPLACED AS PER SRM 51-1 0-01. 2 L 7 4 4F A20WE 2002062600131 20020626 00131 NM 2002 6 26 UPS02438436 1 20020506 A 5320 141U109211 CLIP BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C NWW TUNNEL - LT BS 300 VERTICAL BEAM NR 3 CLIP (COUNT FROM TOP ) FOUND CRACKED. CLIP REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002062600132 20020626 00132 NM 2002 6 26 UPS02438437 1 20020508 A 5312 BULKHEAD BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C LT BS 1480 BULKHEAD WEB FASTENER HOLE NR 21 CRACK REVEALED APPROX 0.040 INCH IN LENGTH RUNNING O/B. R EPAIR CARRIED OUT IAW SB747-53A2390 FIG 11. 2 L 7 4 4F A20WE 2002062600133 20020626 00133 NM 2002 6 26 UPS02438438 1 20020508 A 5320 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C LT BS 1480 BULKHEAD NR 9 HOLE FOUND TWO CRACKS AT OUTER CHORD SPLICE FITTING. REPAIRED AS PER SB747-5 3A2390 FIG 11. 2 L 7 4 4F A20WE 2002062600134 20020626 00134 NM 2002 6 26 UPS02438439 1 20020509 A 5313 65B0794241 LONGERON BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C NOSE WHEEL WELL LT WALL LONGERON BEAM FOUND CRACKED AT BS 320-340 NR 3 BEAM (COUNT FROM TOP). REPLACE D AND INSTALLED AS PER SRM 51-10-01 PG 08 & 51-30-02. 2 L 7 4 4F A20WE 2002062600135 20020626 00135 NM 2002 6 26 SQ7A082002 1 20020130 A 5315 WEB BOEING 727 727251 138408H NM CORRODED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - During scheduled maintenance corrosion was found along BS1174 webs WL 208.1, RBL 23 to LBL 31 in aft cargo bay. 2 L 7 3 4F A3WE 2002062600136 20020626 00136 NM 2002 6 26 SQ7A102002 1 20020125 A 5311 FRAME BOEING 727 727251 138408H NM CRACKED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - During scheduled maintenance the R-1 door, fwd frame was found cracked @BS 378, WL 208.1,lower end of frame.Repair ed per SRM 51-10-3 2 L 7 3 4F A3WE 2002062600137 20020626 00137 NM 2002 6 26 SQ7A112002 1 20020125 A 5315 INTERCOSTAL BOEING 727 727251 138408H NM CRACKED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - During scheduled maintenance the bulkhead intercostal at BS 1183, WL 265, & LBL 60 was found cracked.Replaced the intercostal per SRM 51-30-2. 2 L 7 3 4F A3WE 2002062600138 20020626 00138 NM 2002 6 26 UPS02438294 1 20020422 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C U/D BS 960 S8L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 2002062600139 20020626 00139 NM 2002 6 26 UPS02438295 1 20020422 A 5320 STIFFENER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C LWLG - BS 1241 BULKHEAD LBL 87 CENTER TANK TRANSFER VALVE BONDING JUMPER ATTACHMENT VERT STIFFENER COR RODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 57-10-01 LIMITS. LWLG BS 1241 LBL 87 VERTICAL STI FFENER REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062600140 20020626 00140 NM 2002 6 26 UPS02438296 1 20020419 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C FWD CARGO - BS 680 RT FRAME FOUND CRACKED AT STR 34R. FRAME REPAIRED AS PER RS R-53-22-34783. 2 L 7 4 4F A20WE 2002062600141 20020626 00141 NM 2002 6 26 UPS02438297 1 20020422 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C U/D - BS 990 S-9L STRINGER END SPLICE AREA FOUND CRACKED. STRINGER REPAIRED SRM 53-10-03 FIG 4. 2 L 7 4 4F A20WE 2002062600142 20020626 00142 NM 2002 6 26 UPS02438298 1 20020422 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C U/D - BS 760 S-7L AND S-8L AREA FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 2002062600143 20020626 00143 NM 2002 6 26 0202035508 1 20020611 A 5313 STRINGER BOEING 757 757251 1384970 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 508US 23197 During "H" check found crack in stringer 14L at BS 660. Repaired per EA 55-191091. 2 L 7 2 4F RT A2NM 2002062600144 20020626 00144 NM 2002 6 26 SQ7A132002 1 20020129 A 5344 FRAME BOEING 727 727251 138408H NM CRACKED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - During scheduled maintenance a crack was found at the R-1 door cutout fwd frame upper hinge on an existing repair. Replaced the existing repair per SRM 51-40-3. 2 L 7 3 4F A3WE 2002062600145 20020626 00145 NM 2002 6 26 SQ7A142002 1 20020125 A 5315 GUSSET BOEING 727 727251 138408H NM CRACKED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - During scheduled maintenance the gusset at the R/H Frame at BS 825.95 just below floor level was found cracked. 2 L 7 3 4F A3WE 2002062600146 20020626 00146 NE 2002 6 26 ABXA020003 2 20020624 A 7314 6411194 PUMP DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE # 2 SHEARED A ABXA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 23 812AX 4312 46126 669330 #2 engine driven fuel pump was inop. Found spline shaft sheared on #2 engine driven fuel pump. Replaced pump IAW 73-10- 2. Ops and leak checked good IAW 71-00. 2 L 7 4 4F 4 F 4A25 1E8 2002062600147 20020626 00147 NM 2002 6 26 SQ7A152002 1 20020124 A 5311 ANGLE BOEING 727 727251 138408H NM CRACKED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - During scheduled maintenance the fuselage frame fail safe angle was found cracked at BS 804.5 Str. 14.Repaired per SRM 51-40-3 2 L 7 3 4F A3WE 2002062600148 20020626 00148 NM 2002 6 26 SQ7A182002 1 20020507 A 7500 BACC10DU250C CLAMP BOEING 727 727251 138408H NM LOOSE A SQ7A K NONE J WARNING INDICATION CR CRUISE 1 SO 01 282 21161 IND - #3 engine strut overheat warning light came on.Reduced power and light went out. Maintenance found loose starter s upply duct clamps. Replaced same.Ops checked normal 2 L 7 3 4F A3WE 2002062600149 20020626 00149 NM 2002 6 26 UPS02438338 1 20020422 A 5714 SPAR BOEING 747 747123 1384873 NM CENTER WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C RT BS 990 FRONT SPAR WEB ONE EACH FASTENER HOLE COMMON TO BATH TUB FITTING CRACK REVEALED AT FRONT SPA R WEB LAYER FOR DETAIL PLS REFER ATTACHED SKETCH. RT BS 990 FRONT SPAR WEB CRACKED HOLE OVERSIZED TO 0.660" AND FREEZE PLUG INSTALLED AND DRILLED AS PER BS R53-43-34792. 2 L 7 4 4F A20WE 2002062600150 20020626 00150 NM 2002 6 26 UPS02438340 1 20020422 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C RT BS 990 AT STR 38 RING CHORD ONE EACH FASTENER HOLE FOUND TWO CRACKS AS MARKED. FOR DETAIL PLS REFE R ATTACH SKETCH. LOWER CHORD SEGMENT REPAIRED PER SB 747-53-2362 FIG 9 AND CHORD LOCAL FABRICATED PER RS 53-43-34792 AR EA REPAIRED FOR RT ONLY A PERMANENT REPAIR IS REQUIRED WITHIN 18 MONTHS OR NEXT C-CHECK WHICHEVER COMES FIRST. 2 L 7 4 4F A20WE 2002062600151 20020626 00151 NM 2002 6 26 AWXA200200564 1 20020604 A 5311 65841002 WEB BOEING 737 737277 1384570 NM CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 0 0 22653 YVR - MAJOR REPAIR - DURING C-15 CHECK THE TOP OF THE SPOILER RATIO CHANGER WAS FOUND CHAFING INTO THE WHEEL WELL CEILIN G BS 700. MAINTENANCE BLENDED CHAFED AREA AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR T RIPLER AND FILLER AND INSTALLED REPAIR PARTS IAW AWA ER 15-5312-02173-GF2. 2 L 7 2 4F RT A16WE 2002062600152 20020626 00152 NM 2002 6 26 AWXA200200565 1 20020606 A 5330 654792987 SKIN BOEING 737 737277 1384570 NM ZONE 500 - LEFT WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 0 0 22653 YVR - MAJOR REPAIR - DURING C-15 CHECK THE L/H WING OUTBD MIDFLAP FLAPTRACK FAIRING CONTACT AREA WAS FOUND WORN ON LOWE R SKIN AT THE #2 FLAP TRACK POSITION. MAINTENANCE BLENDED DAMAGED, FABRICATED AN EXTERNAL DOUBLER, AND INSTALLED REPAIR IAW AWA 15-5754-02172-ES3. 2 L 7 2 4F RT A16WE 2002062700001 20020627 00001 NM 2002 6 27 UPS02438341 1 20020422 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C RT MLG W/W OVERRIDE JETTISON PUMP CUTOUT AND BONDING ATTACHMENT CORROSION FOUND AT STA 1241 RBL 90 - 9 6 WL 140 - 148. AS PER R-53-43-34797 IS THE LIMITED REPAIR FOR 18 MONTHS, WAN 681694 RAISED AS FOLLOW - UP TO CARRY OUT PERMANENT REPAIR AS PER EO B747-5710-16852-A WITHIN 18 MONTHS OR THE NEXT C-CHECK WHICHEVER IS EARLIER. 2 L 7 4 4F A20WE 2002062700002 20020627 00002 NM 2002 6 27 UPS02438342 1 20020422 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C LT MLG - BS 1241 BULKHEAD OVERRIDE JETTISON PUMP BONDING STRIP ATTACHMENT CORRODED. AS RS R-53-43-347 97 IS TIME LIMITED REPAIR FOR 18 MONTHS, WAN 681694 RAISED AS FOLLOW - UP TO CARRY OUT PERMANENT REPAIR AS PER EO B747-5 710-16852-A WITHIN 18 MONTHS OR THE NEXT C-CHECK WHICHEVER IS EARLIER. 2 L 7 4 4F A20WE 2002062700003 20020627 00003 NM 2002 6 27 UPS02438441 1 20020506 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT - BS 980 S41L FRAME CRACK. FWD CARGO COMPT BS 980 S-41L FRAME CRACKED AREA REPAIRED A S PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2002062700004 20020627 00004 NM 2002 6 27 219PA0003 1 20020625 A 7710 106073710 TRANSMITTER BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE A PIDA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 05 219PA 19956 Lower than normal acceleration at T/O EPR 1.95 Engs do not seem to produce thrust per EPR setting. Inspected PT2 system s on #1 and #2 engines and found both EPR transmitters bad. R&R #1 eng & #2 eng EPR transmitter per MM77-11-07, Ops che ck of eng paramaters test normal. OK for service. 2 L 7 2 4F 4 F A16WE E2EA 2002062700005 20020627 00005 NM 2002 6 27 UPS02438442 1 20020506 A 5312 141U11073 BULKHEAD BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C NWW TUNNEL - LT BS 320 VERTICAL BEAM WEB FOUND CRACKS AT NR 1, 2, 3 AND 6 STAND OFF HOLES (COUNT FROM TOP). VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002062700006 20020627 00006 NM 2002 6 27 UPS02438443 1 20020506 A 5312 141U11075 BULKHEAD BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C NWW TUNNEL - LT BS 300 VERTICAL BEAM WEB FOUND CRACK AT NR 1 STAND OFF HOLE (COUNT FROM TOP). WEB REP LACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062700007 20020627 00007 NM 2002 6 27 UPS02438444 1 20020506 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT- BS 900 S46R TO S47R SHEAR TIE CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND O UT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2002062700008 20020627 00008 NM 2002 6 27 UPS02438448 1 20020512 A 5320 65B140561 SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX-KEEL BEAM PANEL SUPPORT LOWER CHORD UPPER AND LOWER SURFACE FOUND SURFACE CORROSION AT STA 1329 LBL 16 TO RBL 16. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS FOR REPLACEMENT REFER TO S RM FIG 51-10-01. 2 L 7 4 4F A20WE 2002062700009 20020627 00009 NM 2002 6 27 UPS02438449 1 20020506 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT - BS 900 S41L AREA SHEAR TIE CRACK. SHEAR TIE REPAIRED PER SRM 53-10-04 FIG 40. 2 L 7 4 4F A20WE 2002062700010 20020627 00010 NM 2002 6 27 UPS02438450 1 20020511 A 5320 69B636541 ATTACH FITTING BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D-BS 262 LBL 51 FLOOR FITTING ATT PLATE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01, BLEND O UT NOT WITHIN SRM 51-10-01, LIMITS FOR REPLACEMENT. 2 L 7 4 4F A20WE 2002062700011 20020627 00011 NM 2002 6 27 UPS02438451 1 20020506 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT - BS 980 S39R FRAME CRACK. FRAME CRACK AREA REPAIRED AS PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2002062700012 20020627 00012 NM 2002 6 27 UPS02438452 1 20020506 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT- BS 900 S43L AREA SHEAR TIE CRACK. SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2002062700013 20020627 00013 NM 2002 6 27 UPS02438453 1 20020506 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT- BS 980 S39L FRAME CRACK. FRAME CRACK AREA REPAIRED AS PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2002062700014 20020627 00014 NM 2002 6 27 UPS02438454 1 20020506 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT- BS 960 S46R AREA SHEAR TIE CRACKED. SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2002062700015 20020627 00015 NM 2002 6 27 UPS02438455 1 20020508 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO - BS 860 RT FRAME FOUND CRACKED AT STR 38R. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52. 2 L 7 4 4F A20WE 2002062700016 20020627 00016 NM 2002 6 27 UPS02438456 1 20020514 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT RT BS 980 STR 38 FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062700017 20020627 00017 NM 2002 6 27 UPS02438457 1 20020509 A 5310 DOOR FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D- RT BS 2231 FRAME REVEAL FOUND CRACK AT REVEAL CUTOUT BETWEEN S24R AND S25R. M/D- RT BS 2231 S24R & S25R FRAME REVEAL REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002062700018 20020627 00018 NM 2002 6 27 UPS02438458 1 20020512 A 5320 69B128651 BRACKET BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX- KEEL BEAM PANEL SUPPORT ATT BRACKET FOUND SURFACE CORROSION AT STA 1287 RBL 9 AND LBL 9 BOTH SIDE (TWO EA). CORROSION REMOVED IAW SRM 51-10-01. BLEND-OUT NOT WITHIN SRM 53-10-01 FIG 1, LIMITS FOR REPLACEMENT REFER TO SRM FIG 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062700019 20020627 00019 NM 2002 6 27 UPS02438459 1 20020508 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C COCKPIT - FLOORBEAM FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53- 10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-07 FIG 23. 2 L 7 4 4F A20WE 2002062700020 20020627 00020 NM 2002 6 27 UPS02438460 1 20020512 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D- ZONE-E SEAT TRACK FOUND CORROSION AT BS 2240-2280 LBL 33. CORROSION REMOVED IAW SRM 51-10-01. B LEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002062700021 20020627 00021 NM 2002 6 27 UPS02438461 1 20020512 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D-ZONE-E SEAT TRACK FOUND CORROSION AT BS 2190-2220 RBL 33. CORROSION REMOVED IAW SRM 51-10-01. BL END OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002062700022 20020627 00022 NM 2002 6 27 UPS02438462 1 20020506 A 5312 141U11074 BULKHEAD BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C NWW TUNNEL - RT BS 320 VERTICAL BEAM WEB FOUND CRACK AT NR 1 STAND OFF HOLE (COUNT FROM TOP). WEB REP LACED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2002062700023 20020627 00023 NM 2002 6 27 UPS02438463 1 20020512 A 5320 69B118571 BRACKET BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX- BS 1227 RT SIDE KEEL BEAM PANEL ATT BRACKET FOUND SURFACE CORROSION. CORROSION REMOVED IAW SRM 51 -10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002062700024 20020627 00024 NM 2002 6 27 UPS02438464 1 20020511 A 5320 69B118571 BRACKET BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX- BS 1078 RT KEEL BEAM PANEL SUPPORT ATT BRACKET FOUND CORROSION AT RBL 9. CORROSION REMOVED IAW SR M 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002062700025 20020627 00025 NM 2002 6 27 UPS02438466 1 20020508 A 5320 TIE CLIP BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO- FRAME TIE CLIP FOUND CRACKED AT BS 840 STR 45L - 46L. FWD CARGO BS 840 STR 45L-46L FRAME T IE CLIP REPAIRED AS PER SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2002062700026 20020627 00026 NM 2002 6 27 UPS02438468 1 20020526 A 3350 LENS BOEING 747 747121 1384871 NM CABIN MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:N/A LENS ASSY MISSING FROM EMERGENCY LIGHT AT STA 340 RT MAIN CARGO DECK. REPLACED MISSING LENS ASSY. 2 L 7 4 4F A20WE 2002062700027 20020627 00027 NM 2002 6 27 UPS02438472 1 20020511 A 5347 BAC15201545 SEAT TRACK BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D- ZONE-E SEAT TRACK FOUND BULGE UP AT BS 2150 - 2163 LBL 98. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062700028 20020627 00028 NM 2002 6 27 UPS02438473 1 20020512 A 5320 7075000501N FLOOR SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D- ZONE-E FLOOR SUPPORT FOUND CORROSION AT BS 2200-2220 LBL 98. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002062700029 20020627 00029 NM 2002 6 27 UPS02438474 1 20020510 A 5320 LS4573 FLOOR SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C AFT CARGO - BS 1900 - 1910 RBL 43 LONGITUDINAL FLOOR SUPPORT FOUND CORRODED AT UPPER AND LWR CHORD. C ORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1, FOR REPLACEMENT REFER TO SRM FIG 51-10-01 P 8. 2 L 7 4 4F A20WE 2002062700030 20020627 00030 NM 2002 6 27 UPS02438475 1 20020510 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D SEAT TRACK FOUND CORRODED BS 406 TO 406, RBL R57. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002062700031 20020627 00031 NM 2002 6 27 UPS02438476 1 20020509 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D- BS 2188 S-3L STRINGER END FOUND CRACKED. CRACKED STRINGER REPAIRED PER RS R53-61-34819. 2 L 7 4 4F A20WE 2002062700032 20020627 00032 NM 2002 6 27 UPS02438477 1 20020510 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D- SEAT TRACK FOUND SLIGHTLY CORRODED BS 240 TO 260, RBL 50 TO RBL 53. CORROSION REMOVED IAW SRM 51 -10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002062700033 20020627 00033 NM 2002 6 27 UPS02438478 1 20020511 A 5320 BAC1505101016 FLOOR SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D- FLOOR SUPPORT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-1 0-01 FIG 1 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002062700034 20020627 00034 NM 2002 6 27 UPS02438479 1 20020511 A 5320 FLOOR SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D- FLOOR SUPPORT FOUND SLIGHTLY CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-07 FIG 8. 2 L 7 4 4F A20WE 2002062700035 20020627 00035 NM 2002 6 27 UPS02438480 1 20020512 A 5320 SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX-KEEL BEAM PANEL SUPPORT LOWER CHORD UPPER AND LOWER SURFACE FOUND SURFACE CORROSION AT STA 1276 TO STA 1350 LBL 16. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2002062700036 20020627 00036 NM 2002 6 27 UPS02438481 1 20020510 A 5320 HXB149953FT SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX- LT SIDE AIR CONDITIONING BAY BS 1241 SLOPE PANEL. LOWER SURFACE SUPPORT RETAINER FOUND CORROSION AT LBL 90 TO LBL 94. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, REPLACEMENT REFER T O SRM FIG 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062700037 20020627 00037 NM 2002 6 27 UPS02438485 1 20020510 A 5312 BULKHEAD BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX- LT BS 1480 BULKHEAD WEB CRACKED AT STR 34L AS MARKED. BULKHEAD WEB REPAIRED AS PER SRM 51-40-02. 2 L 7 4 4F A20WE 2002062700038 20020627 00038 NM 2002 6 27 UPS02438486 1 20020510 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX- LT BS 1480 BULKHEAD TO FX CHORD CRACKED AT STR 38L. CHORD REPAIRED AT BS 1480 STR 38L AS PER SRM 51-40-03. 2 L 7 4 4F A20WE 2002062700039 20020627 00039 NM 2002 6 27 UPS02438487 1 20020507 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C RT SIDE BS 800 FRAME FOUND ONE FASTENER HOLE CRACKED AT FRAME INNER CHORD ANGLE AND STRAP. FRAME CHOR D AND STRAP REPAIRED AS PER RS R-53-22-34808. 2 L 7 4 4F A20WE 2002062700040 20020627 00040 NM 2002 6 27 UPS02438488 1 20020507 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C, LT BS 800 FRAME INNER CHORD AND STRAP, ONE FASTENER HOLE CRACK FOUND ON S16 AREA, CRACK THROUGH THICK NESS RUNNING FWD AND AFT DETAIL. LT BS 800 FRAME CHORD AND STRAP S15L-17L REPAIRED REFER RS R53-22- 34808. 2 L 7 4 4F A20WE 2002062700041 20020627 00041 NM 2002 6 27 UPS02438490 1 20020515 A 5320 65B169515 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C, BS 980 LT FWD LOWER DRAG SPLICE FITTING FOUND SKIN ATT FLANGE 6TH FASTENER HOLE CRACKED RUNNING DOWN APPROX .0625 INCH LONG. BS 980 LT FWD LWR DRAG SPLICE FITTING REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062700042 20020627 00042 NM 2002 6 27 UPS02438491 1 20020504 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX- LT STA 780 - STA 800 STR 47 STRINGER FOUND WITH CORROSION CRACKED. STR 47L REPAIRED AS PER SRM 53 -10-03 FIG 1. 2 L 7 4 4F A20WE 2002062700043 20020627 00043 NM 2002 6 27 UPS02438492 1 20020511 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C M/D- SEAT TRACK FOUND SLIGHTLY CORRODED BS 510-BS 520, LBL 91. CORROSION REMOVED IAW SRM 51-10-01. B LEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2002062700044 20020627 00044 NM 2002 6 27 UPS02438493 1 20020515 A 5320 65B169513 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C, BS 980 LT FWD UPPER DRAG SPLICE FITTING. FOUND HORIZONTAL FLANGE MOST FWD HOLE CRACKED RUNNING I/B A PPROX .0625 INCH LONG STR L38 TO L38. BS 980 LT FWD UPPER DRAG SPLICE FITTING REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002062700045 20020627 00045 NM 2002 6 27 UPS02438504 1 20020508 A 5320 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C, LT BS 1480 STR L33 BULKHEAD NR 9 HOLE FOUND TWO CRACKS AT EXTENSION FITTING. REPAIR CARRIED OUT IAW REPAIR SCHEME HX-RS NR R53-63-34822 FOR FABRICATION OF REPAIR BUSHING AND WASHER REFER TO CWPC CONTROL SEQ TEHI 0 12 - 1 08 AND TEHI 0 12 - 109. 2 L 7 4 4F A20WE 2002062700046 20020627 00046 NM 2002 6 27 UPS02438510 1 20020510 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX- BS 440 STR 42L - 43L CORROSION. FOUND CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN S RM 53-30-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-30-03 FIG 1. 2 L 7 4 4F A20WE 2002062700047 20020627 00047 NM 2002 6 27 UPS02438512 1 20020509 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO - BS 720-740 STR - 33R FOUND CORRODED (2 LOCATION). CORROSION REMOVED IAW SRM 51-10-01. BL END OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2002062700048 20020627 00048 NM 2002 6 27 UPS02438519 1 20020510 A 5320 WEB BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C, NOSE W/W LT VERTICAL SIDEWALL WEB FOUND BULGE UP AT STA 380 WL 187. CORROSION REMOVED IAW SRM 51-10- 01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPAIR REFER TO RS R53-18-34814. 2 L 7 4 4F A20WE 2002062700049 20020627 00049 NM 2002 6 27 UPS02438520 1 20020510 A 5310 65B135667 STOP FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C, M/D - NR 1L DOOR FWD FRAME CUTOUT NR 1 STOP FITTING FOUND CRACKED (COUNT FROM LWR). M/D NR 1L DOOR F WD FRAME CUTOUT NR 1 STOP FITTING REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002062700050 20020627 00050 NM 2002 6 27 UPS02438521 1 20020506 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C AFT CARGO COMPARTMENT CUTOUT FWD UPPER CORNER FOUND CRACKS AT FUSELAGE SKIN AND SKIN DOUBLER BS 1820, STR R27. AFT CARGO COMPT DOOR CUTOUT FWD UPPER CORNER SKIN AND SKIN DOUBLER REPAIRED IAW RS R53-61-34807. 2 L 7 4 4F A20WE 2002062700051 20020627 00051 NM 2002 6 27 UPS02438522 1 20020507 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C, FWD CARGO - STRINGER END FOUND CRACKED AT BS 742 STR 40R. STRINGER END REPAIRED AS PER RS R53-21-348 11. 2 L 7 4 4F A20WE 2002062700052 20020627 00052 NE 2002 6 27 UPS02438564 2 20020605 A 7200 ENGINE BOEING 747 747123F NM PWA JT9 JT9D7A 52054 NE NR 3 FLAMED OUT A IPXA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SO 01 677UP 20391 INSPECTION TYPE:N/A ENGINE NR 3 FLAME-OUT AT FL350 APPROXIMATELY 15 MINUTES AFTER LEVEL OFF, CAUSE UNKNOWN. AOM PROCEDU RES ACCOMPLISHED AND ENGINE RESTARTED. AS PER MM T/S TREE 71-00-42 PG 219 AND 131 ACCOMPLISHED ALL CORRECTIVE ACTIONS F OR FLAME-OUT. NO DISCREPANCIES NOTED. RAN ENGINES AT PP, ALL ENGINE PARAMETERS CHECK NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 2002062700053 20020627 00053 NM 2002 6 27 UPS02438575 1 20020610 A 3350 LENS BOEING 747 747259B 1384804 NM CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:N/A LENS CRACKED ON DOME LIGHT AT UPPER DECK EMERGENCY EXIT. REMOVED AND REPLACED LIGHT ASSY. 2 L 7 4 4F RT A20WE 2002062700054 20020627 00054 NM 2002 6 27 UPS02438581 1 20020506 A 5311 BAC15142184 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FWD CARGO COMPT - BS 1000 BULKHEAD BETWEEN S41L AND 42L LOWER CHORD CRACK. C/OUT FWD CARGO COMPT - BS 1000 BULKHEAD LOWER CHORD BETWEEN S401 TO S451 SECTION SEGMENT REPLACED IAW SRM 51-10-01 PG 8 AND DWG 65B10098-1 AND SB -747-53-2444. 2 L 7 4 4F A20WE 2002062700055 20020627 00055 NM 2002 6 27 UPS02438582 1 20020509 A 5720 WEB BOEING 747 747121 1384871 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C FX- RT WING CTR SECTION FRONT SPAR LOWER CHORD ATT WEB EXTERIOR SURFACE FOUND HEAVY CORROSION AT BS 10 00 RBL 65-73. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 57-10-01 LIMITS, FOR REPAIR REFER TO RS R53 -43-34815. 2 L 7 4 4F A20WE 2002062700056 20020627 00056 NM 2002 6 27 UPS02438609 1 20020529 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C, LT NOSE W/W BS 300 INNER CHORD FRAME WEB FOUND 2 FASTENER HOLES CRACKED. LT NOSE W/W BS 300 FRAME CR ACKED, AREA REPAIRED AS PER SRM 53-10-04 FIG 94 DETAIL II. 2 L 7 4 4F RT A20WE 2002062700057 20020627 00057 NM 2002 6 27 UPS02438628 1 20020613 A 2612 FIRE WARNING BOEING 747 747121 1384871 NM COCKPIT FALSE INDICATION A IPXA K NONE N FALSE WARNING CL CLIMB 1 SO 01 683UP 20353 INSPECTION TYPE:N/A ON T/O ROLL AND INITIAL CLIMB THE GLARESHIELD, BOTH MASTER FIRE LIGHTS FLICKERED 3 TIMES WITH NO IND ICATION OF SOURCE. IN TESTING ALL FIRE DETECTION SYSTEMS WHEEL FIRE DID NOT TEST. AFTER RESET OF P-6 CB, ALL OPS NORMA L PER 26-11-00. 2 L 7 4 4F A20WE 2002062700058 20020627 00058 NM 2002 6 27 UPS02438638 1 20020530 A 5310 DOOR FRAME BOEING 747 747200 1384847 NM FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C M/D - RT NR 2 DOOR FWD LWR CORNER REVEAL CRACKED AT S-24R. CORNER REVEAL REPAIR CARRIED OUT AS PER SR M 53-10-04 FIG 84. 2 L 7 4 4F RT A20WE 2002062700059 20020627 00059 NM 2002 6 27 UPS02438643 1 20020618 A 3350 BATTERY BOEING 747 747200 1384847 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:PFLT EMERGENCY EXIT DOOR LIGHT OVER CREW SERVICE INOP. REMOVED AND REPLACED CREW SERVICE DOOR BATTERY P ER 33-51-05. OPS CHECKED GOOD. 2 L 7 4 4F RT A20WE 2002071500058 20020715 00058 NM 2002 7 15 UPS02438644 1 20020618 A 3240 BRAKE BOEING 747 747259B 1384804 NM LANDING GEAR MALFUNCTIONED A IPXA K NONE O OTHER LD LANDING 1 SO 01 527UP 21730 INSPECTION TYPE:N/A AUTOBRAKES DISENGAGED IMMEDIATELY AFTER TOUCHDOWN. PERFORMED AUTO BRAKES ADJUSTMENT TEST AS PER MM 34-43-00 NO DEFECTS NOTED. 2 L 7 4 4F RT A20WE 2002062700060 20020627 00060 NM 2002 6 27 UPS02438645 1 20020515 A 5320 65B169521 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C, BS 980 LT FWD BATHTUB FITTING FOUND CHORD MOUNTING FLANGE 3 HOLES CRACKED. ONE HOLE AT UPPER BATHTUB FOUND 2 CRACKS RUNNING I/B APPROX .0625 AND .125 ANOTHER HOLE AT LOWER BATHTUB FOUND CRACK RUNNING I/B APPROX .1875, TH E LOWEST HOLE OF THE FLANGE FOUND CRACK RUNNING DOWN APPROX .6250. CUTOUT BS 980 LT BATHTUB FITTING REPLACED IAW SRM 51 -10-01 PG 8. 2 L 7 4 4F A20WE 2002062700061 20020627 00061 NM 2002 6 27 UPS02438646 1 20020515 A 5320 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C BS 980 RT FWD BATHTUB FITTING (STR R38) FOUND CHORD MOUNTING FLANGE 2 HOLES CRACKED. ONE HOLE AT UPPE R BATHTUB FOUND CRACK RUNNING I/B APPROX .25 INCH LOWEST HOLE OF THE FLANGE FOUND 3 CRACKS APPROX .25 INCH LONG EACH. B S 980 RT FWD BATHTUB FITTING. REPAIRED AS PER RS R-53-23-34817. 2 L 7 4 4F A20WE 2002062700062 20020627 00062 NM 2002 6 27 UPS02438647 1 20020515 A 5312 BULKHEAD BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C, BS 980 RT BULKHEAD WEB STR R38 1 HOLE COMMON TO BATHTUB UPPER FITTING FOUND CORROSION FROM 5 O/C TO 9 O/C POSITION (LOOK FROM FWD). BS 980 RT BULKHEAD WEB STR R38 HOLE COMMON TO BATHTUB UPPER FITTING REPAIRED AS PER RS R 53-23-34817. 2 L 7 4 4F A20WE 2002062700063 20020627 00063 NM 2002 6 27 UPS02438649 1 20020531 A 5310 DOOR FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C M/D - RT NR 4 DOOR FWD LWR CORNER CUTOUT REVEAL CRACKED. R4 DOOR LOWER CORNER REVEAL REPAIRED AS PER SRM 53-10-04 FIG 84. 2 L 7 4 4F RT A20WE 2002062700064 20020627 00064 NM 2002 6 27 UPS02438661 1 20020607 A 5412 BULKHEAD BOEING 747 747SR46 1384816 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:SPC NR 1 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT AFT WEB DOUBLER APPROX .25 INCH IN LENGTH. NR 1 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER HX RS 54-53-34828. 2 L 7 4 4F RT A20WE 2002062700065 20020627 00065 NM 2002 6 27 UPS02438662 1 20020606 A 5412 BULKHEAD BOEING 747 747SR46 1384816 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:SPC CRACK REVEALED AT NR 4 PYLON REAR ENGINE MOUNT BULKHEAD FWD SIDE I/B DOUBLER, THE CRACK INITIATED FR OM ONE FASTENER HOLE PROPAGATED UPWARD TO THE EDGE CRACK LENGTH .1875 INCH. NR 4 PYLON REAR MOUNT BULKHEAD REPAIRED AS PER HX RS R-54-53-34828. 2 L 7 4 4F RT A20WE 2002062700066 20020627 00066 NM 2002 6 27 UPS02438663 1 20020607 A 5412 BULKHEAD BOEING 747 747SR46 1384816 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:SPC NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT AFT WEB DOUBLER APPROX .1875 INCH IN LENGTH. N R 2 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER R54-53-34828. 2 L 7 4 4F RT A20WE 2002062700067 20020627 00067 NM 2002 6 27 UPS02438668 1 20020507 A 5720 65B172235 SPLICE BOEING 747 747121 1384871 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C LT WING REAR SPAR TO WING CTR SECTION UPPER SPLICE FITTING FOUND CRACKED AT RADIUS AREA. LT UPPER SPL ICE FITTING REPLACED AS PER EO B747-5740-4366 APP H PG 46. 2 L 7 4 4F A20WE 2002062700068 20020627 00068 NM 2002 6 27 UPS02438670 1 20020528 A 5320 65B224321 CHANNEL BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C RT MLG W/W FWD LOWER SLOPE PANEL CORROSION FOUND AT STA 1251-1264 RBL 9-30. U-CHANNEL REPLACED AND RE INSTALLED AS PER SRM 51-10-01 AND SRM 51-30-02 AT RT MLG W/W FWD LOWER SLOPE PANEL. 2 L 7 4 4F RT A20WE 2002062700069 20020627 00069 NM 2002 6 27 UPS02438685 1 20020531 A 5320 PANEL BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C M/D - CTR SECTION RT CLOSURE PANEL FOUND CRACKED AT BS 1245 RBL 75 WL 185. CTR SECTION RT CLOSURE PAN EL REPLACED AS PER EO B747-5310-2758-E APPENDIX E & F. 2 L 7 4 4F RT A20WE 2002062700070 20020627 00070 NM 2002 6 27 UPS02438688 1 20020506 A 5414 ACCESS PANEL BOEING 747 747121 1384871 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C NR 1 PYLON ACCESS PANEL NR 452 BL CUTOUT ARE CRACKED AT 2 LOCATIONS AS MARKED. CUTOUT NR 1 PYLON ACCE SS PANEL NR 452 BL REAR CUTOUT TWO LOCATIONS REPAIRED IAW RS R54-51-34816. 2 L 7 4 4F A20WE 2002062700071 20020627 00071 EU 2002 6 27 DHL2002366009 1 20020626 A 2612 9515004 CONTROL UNIT AIRBUS 300 A300B4203 3930306 EU DEFECTIVE A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 366DH 249 DURING CLIMB AT 180 THE ENG 2 LOOP "A" LIGHT CAME ON WITH A SINGLE STROKE CHIME. THE ABNORMAL PROCEDURE WAS COMPLETED. T ESTED GOOD AND LOOP "B" WAS SELECTED. REMOVED AND REPLACED #2 ENG FIRE DETECTION CONTROL UNIT AS PER MM 26- 12-11. OPS C HECKED GOOD. 2 L 7 2 4F RT A35EU 2002062700072 20020627 00072 EU 2002 6 27 QXEA0200909 1 20020626 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU ZONE 100 INOPERATIVE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 497US 11173 SEA-REAR FACING PORTION OF EXIT SIGN IS INOPERATIVE AT EMERGENCY EXIT ROE. REMOVED AND REPLACED EXIT SIGN AT EMERGENCY E XIT ROW. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002062700073 20020627 00073 NM 2002 6 27 UPS02438693 1 20020620 A 2612 FIRE WARNING BOEING 747 747123 1384873 NM COCKPIT FALSE INDICATION A IPXA K NONE N FALSE WARNING CR CRUISE 1 SO 01 673UP 20325 INSPECTION TYPE:N/A AFTER APPROX 1 HOUR IN CRUISE FLIGHT. A RED WARNING LIGHT ON THE OVERHEAD ILLUMINATED FOR A SPLIT S ECOND. RESEATED ALL THE FIRE DET CARDS. TESTED SYSTEMS IAW MM 26-10-00, ALL TEST CHECKS GOOD. 2 L 7 4 4F A20WE 2002062700074 20020627 00074 NM 2002 6 27 UPS02438694 1 20020624 A 3350 LIGHT BOEING 747 747212B 1384886 NM EXTERIOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:N/A EXTERIOR ESCAPE SLIDE LIGHT INOP. 2 L 7 4 4F A20WE 2002062700075 20020627 00075 NM 2002 6 27 UPS02538121 1 20020508 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:N/A EVIDENCE AND AIR LEAKAGE AT 2L WINDOW. NOTICE AT BOTTOM CENTER WINDOW 2L WINDOW SEAL CLEANED AS PER MM 56-11-02. A/C PRESSURIZED WINDOW CHECKED SERVICE. 2 L 7 2 4F RT A2NM 2002062700076 20020627 00076 NM 2002 6 27 UPS02538276 1 20020517 A 5230 3943084 FITTING BOEING 757 75724APF 1384969 NM CARGO DOOR BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 460UP 25481 INSPECTION TYPE:N/A MX INSPECTION - LWR FWD DOOR HANDLE RETENTION SPRING AND ROD BROKEN. REPLACED MALE FITTING ON OVERC ENTER MECHANISM OF FRONT LOWER CARGO DOOR. WORK WAS DONE IAW B757 MM 52-34-22, OPS CHECK OK. 2 L 7 2 4F RT A2NM 2002062700077 20020627 00077 NM 2002 6 27 UPS02538277 1 20020517 A 5270 BRACKET BOEING 757 75724APF 1384969 NM L1 DOOR LOOSE A IPXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 406UP 23728 INSPECTION TYPE:N/A ATB-UNABLE TO PRESSURIZE. MX SECURED L1 DOOR SWITCH BRACKET. REPLACED PROX SWITCH MOUNTING BRACKET IAW 757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2002071500055 20020715 00055 NM 2002 7 15 UPS02438335 1 20020418 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C RT MLG W/W BS 1350 B/H LWR CHORD I/B UPPER SURFACE CORRODED AS MARKED. 3 EA 0.625 INCH HOLE INSPECTED , ALL WITHIN PRODUCTION TOLERANCES AND ARE CLEAN AND ROUND WITHOUT DAMAGE AS PER HX RAA 747-53-20057 REQUIREMENT. 2 L 7 4 4F A20WE 2002062700078 20020627 00078 NM 2002 6 27 UPS02438339 1 20020422 A 5320 65B169522 FITTING BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C HEAVY CORROSION REVEALED AT UPPER AND LOWER FASTENER HOLES OF BATH TUB FITTING AT BS 990 S38R. PLEASE REFER FIG. RT SIDE STA 980 S38R BATHTUB FITTING PERMANENT REPAIR CARRIED OUT AS PER RS R53-23-34791. CONTINUE INSPECT ION PLANS ON THE RT SIDE PER SB 747-53A2362 AND SB 747-53A2444 AS PER UPS EO B747-5310-16873-A. 2 L 7 4 4F A20WE 2002062700079 20020627 00079 NM 2002 6 27 UPS02438343 1 20020422 A 5320 ANGLE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C RT MLG W/W CANTED BULKHEAD LOWER CAP ANGLE UPPER EDGE CORRODED AT RBL 78 - 83 BS 1241 - 1242. THIS RE PAIR IS CONSIDERED TIME - LIMITED FOR 24 MONTHS UNTIL AN IMPROVED DRAIN AGE MODIFICATION CAN BE INSTALLED IAW BOEING SER VICE BULLETIN 747-51A2054 REV 1 AS PER UPS EO B747-5310-16853-A. 2 L 7 4 4F A20WE 2002062700080 20020627 00080 NM 2002 6 27 UPS02438344 1 20020501 A 5320 ANGLE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C RT WLG CANTED BULKHEAD LWR CAP FOUND CORROSION AT RBL 53 BS 1241 TO 1241. THIS REPAIR IS CONSIDERED T IME - LIMITED FOR 24 MONTHS UNTIL AN IMPROVED DRAINAGE MODIFICATION CAN BE INSTALLED IAW BOEING SERVICE BULLETIN 747-51A 2054 REV 1 AS PER UPS EO B747-5310-16853-A. 2 L 7 4 4F A20WE 2002062700081 20020627 00081 NM 2002 6 27 UPS02438440 1 20020509 A 5320 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C RT BS 1480 BULKHEAD HOLE NR 5 CRACK FOUND ON EXTENSION FITTING APPROX .0625 INCH RUNNING AFT. REPAIR CARRIED OUT IAW SB747-53A2390 FIG 11. 2 L 7 4 4F A20WE 2002071800132 20020718 00132 SO 2002 7 18 C2XA02BT027 1 20020616 A 2530 1095A30A COFFEEMAKER EMB 145 EMB145LR 3260212 SO GALLEY FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14542 145547 IAH- CREW REPORTED BURNING SMELL FROM HOT JUG. MAINTENANCE REMOVED AND REPLACED HOT JUG AND RT HOT JUG CONNECTOR IAW C& D CMM 25-31-45. 2 L 7 2 4T RT T00011AT 2002071800128 20020718 00128 SO 2002 7 18 C2XA02BT024 1 20020616 A 3350 7287580509 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14943 145040 EWR- DURING PREFLIGHT INSPECTION CREW REPORTED EMERGENCY LIGHTS FROM ROW 12 TO ROW 15 ARE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE EMERGENCY LIGHT STRIP IN ROW 12 TO ROW 15 FLOOR AREA IAW EMB145 MM 33-0-08. 2 L 7 2 4F RT T00011AT 2002071800130 20020718 00130 SO 2002 7 18 C2XA02BT025 1 20020616 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY ACTIVATED A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION UK UNKNOWN 1 SW 27 13978 145180 EWR- CREW REPORTED, LAV SMOKE INDICATOR WITH SMELL OF SMOKE, BUT LAV SMOKE INDICATOR EXTINGUISHED AFTER ONE MINUTE AND SMOKE SMELL DISSIPATED. MAINTENANCE RAN ENGINES WITH BOTH PACKS ON, TESTED LAV SMOKE NO SMELL IN CABIN OR COCKPIT, NO F AN SMOKE FAULT IAW EMB 145 MM 26-14-01. 2 L 7 2 4T RT T00011AT 2002062700082 20020627 00082 WP 2002 6 27 0202069881 1 20020624 A 2140 1173T0691 SWITCH DOUG DC9 DC951 3022051 WP PACK DUCTING A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 676MC 47652 WHILE CRUISING AT ALTITUDE, CREW AND PASSENGERS NOTICED A VERY STRONG RUBBER SMELL IN THE CABIN AND COCKPIT. ALSO, THERE WAS EXCESSIVE HEAT COMING FROM OVERHEAD AREA. DISSIPATED DURING DESCENT AT ABOUT 11,000 FEET. FLIGHT DIVERTED TO GRR. M AINTENANCE PERFORMED THERMO SWITCH SHUTDOWN CHECKS. CHECKS WERE GOOD. REPLACED THE WATER SEPARATOR BAGS AND DID PACK O IL PURGE RUN. FOUND PACK TEMP CONTROL VERY SENSITIVE AND REPLACED IT AFTER ONE DAY MEL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002062700083 20020627 00083 NM 2002 6 27 UPS02538278 1 20020517 A 2910 HYDRAULIC LINE BOEING 757 75724APF 1384969 NM LT MLG RUPTURED A IPXA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 SO 01 422UP 25324 INSPECTION TYPE:N/A ATB- LOSS OF LEFT SYSTEM HYD PRESSURE. FOUND LT MAIN GEAR DOWNLOCK PRESS LINE LEAKING. REMOVED AND REPLACED DOWNLOCK ACT RETRACT PRESS LINE. LEAKS CHECK GOOD PER MM 32-32-02. 2 L 7 2 4F RT A2NM 2002062700084 20020627 00084 NM 2002 6 27 UPS02538690 1 20020622 A 2611 FITTING BOEING 757 75724APF 1384969 NM SMOKE DETECTOR BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 460UP 25481 INSPECTION TYPE:N/A MAIN CARGO DECK, FWD RT SMOKE DETECTOR TUBE FITTING BROKEN. REMOVED AND REPLACED TUBE FITTING AS PE R MM 26-16-01-2. 2 L 7 2 4F RT A2NM 2002062700085 20020627 00085 WP 2002 6 27 UPS02838109 1 20020411 A 5347 605176 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 SEAT TRACK NR 6 CORRODED ON UNDERSIDE AT STA 783. REMOVED DAMAGED SECTION OF TRACK. FABRICATED NEW SECTION OF TRACK AND SPLICE IAW UPS EO NO DC8-5320-5167-6. INSTALLED TRACK AND SPLICES IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002062700086 20020627 00086 NE 2002 6 27 UPS02838113 2 20020502 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 1 FLAMED OUT A IPXA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SO 01 709UP 45914 INSPECTION TYPE:N/A NR 1 ENGINE FLAMED OUT DURING CLIMB THROUGH 210 ENGINE ANTI-ICE WAS ON LIGHT TURBULENCE COMPLETED F LAME-OUT CHECKLIST. SUCCESSFUL RESTART AT 6 T/S IAW MM 71-00-00 ALL PROCEDURES PERFORMED BY PHL MX, SECURED CDP PS 3 LI NE AT THE MED. REPLACED FUEL FILTER NO DEBRIS FOUND IN ORIGINAL FILTER PERFORMED PWR ASSURANCE CHECK IAW 71-00-00 P538- 547 ALL PARAMETERS GOOD PER FIG 516. 2 L 7 4 4F 4 F RT 4A25 E2GL 2002062700087 20020627 00087 WP 2002 6 27 UPS02838124 1 20020410 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 R2 UPPER AFT DOOR JAMB CORNER CRACKED S-2. REPAIRED R2 UPPER AFT JAMB IAW DC8 SRM 53-2-0 FIG 16 SHEE T 4 AND TR 53-130 & 53-131. 2 L 7 4 4F RT 4A25 2002062700088 20020627 00088 WP 2002 6 27 UPS02838125 1 20020410 A 5320 37540231N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 FLC PIT FLOOR FITTING HAS CORROSION AT FS 296 STR 33R. REMOVED CORROSION IAW DC8 SRM 51-1-8 FOUND OU T OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED FITTING REPAIR IAW DC8 SRM 53-2-0 PG 15/16. INSTALLED FITTING REPAIR & CLIP S AT STA 296 STR 33R IAW DC8 SRM 53-2-0 PG 15/16 & DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002062700089 20020627 00089 WP 2002 6 27 UPS02838126 1 20020410 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 FRAMED CRACKED AT FASTENER TO CUTOUT FS 720 RBL 24 LWR FUSE FILLET AREA. REMOVED AND REPLACED FRAME IAW DAC DWG 5750365. 2 L 7 4 4F RT 4A25 2002062700090 20020627 00090 WP 2002 6 27 UPS02838129 1 20020411 A 5313 37735121 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 R-2 DOOR LONG 11 RT IS CRACKED. REMOVED AND REPLACED LONGERON IAW DAC DWG 3773512 AND DC8 SRM 51-1-2 0 AND 51-1-21. 2 L 7 4 4F RT 4A25 2002062700091 20020627 00091 WP 2002 6 27 UPS02838130 1 20020410 A 5320 3755843501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 AFT LOWER CARGO STA 1150 Z-FITTING L34R AND L35R CRACKED. REMOVED CRACKED Z-FITTING, FABBED SPLICE A ND DOUBLER. INSTALLED FITTING SPLICE AND DOUBLER IAW DC8 SRM 53-2-0 & DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 2002062700092 20020627 00092 WP 2002 6 27 UPS02838131 1 20020428 A 5347 6015176 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 NR 1 SEAT TRACK AT STA 46 IS CORRODED. REPLACED SECTION OF SEAT TRACK WITH SPLICE IAW EO DC8-5320-51 67. 2 L 7 4 4F RT 4A25 2002062700093 20020627 00093 EA 2002 6 27 COMA0260387 1 20020624 A 2410 IDG CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 01 978CA 7158 FLIGHT 5494 IDG CAUTION MESSAGE AND GEN 1 OFF MESSAGE.DEFERRED MAINTENANCE ON L/H IDG PER MEL. 2 L 7 2 4F RT A21EA 2002072200072 20020722 00072 NM 2002 7 22 AWXA200200567 1 20020523 A 5320 141N8322 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 DURING C-08 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF OUTBOARD LONGITUDINAL FLOOR SUPPORT AT LBL 64, WL 208, FROM BS 377 TO 395. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS, REMOVED DAMAGED PORTION OF WEB, FABRIC ATED NEW WEB, AND INSTALLED REPAIR IAW B757-200 SRM 51-30-01, PG. 20, FIG. 7. 2 L 7 2 4F RT A2NM 2002072200073 20020722 00073 NM 2002 7 22 AWXA200200568 1 20020620 A 5330 6555821158 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 DURING C-18 CHECK A 1 1/4 INCH CRACK WAS FOUND ON L2 DOOR EXTERNAL SKIN AT THE UPPER AFT CORNER THROUGH COUNTERSINK FAST ENER HOLE, BS 985.75, CONFIRMED BY HFEC INSPECTION AND 10X VISUAL. MAINTENANCE CUTOUT CRACKED AREA OF SKIN, FABRICATED A REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 52-00-01, PG. 203-204. 2 L 7 2 4F RT A16WE 2002062800001 20020628 00001 NM 2002 6 28 UPS02438648 1 20020515 A 5711 SPAR BOEING 747 747121 1384871 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C, RT JETTISON PUMP ATT BONDING JUMPER ATT REAR SPAR BOLT HOLE SURFACE CORR AT WLG W/W STA 1241 RT AFT F ACE RBL 91.8. CUTOUT RT WLG W/W BS 1241 REAR SPAR WEB JETTISON PUMP, CUTOUT ATT BONDING JUMPER ATT. FASTENER HOLE REPA IRED IAW RS R57-12-34823. 2 L 7 4 4F A20WE 2002062800002 20020628 00002 NM 2002 6 28 UPS02638579 1 20020609 A 3230 SEQUENCE VALVE BOEING 767 76734AF 1385212 NM LT MLG FAILED A IPXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 317UP 27745 INSPECTION TYPE:N/A ATB AFTER T/O LEFT GEAR WOULD NOT GO UP, AFTER FEW TRIES, GEAR WENT UP BUT WOULD NOT COME DOWN. ALT ERNATE METHOD WAS USED TO LOWER THE GEAR. A/C REMAINS OUT OF SERVICE. PSER TEST CARRIED OUT, SYS OPS NORMAL PSEU BIT H ISTORY CHRO, REGISTERED SENSORS TESTED, NO INDICATION FAULTS FOUND. REMOVED SUSPECTED SEQUENCE VALVE (CONTAMINATED FLUI D OBSERVED) FLUSHED UNIT; REFITTED RIGHT SIDE. RETRACTION CHECKS GOOD USING A/C SYSTEMS AND THEN W/GROUND CONNECTIONS. ALL FUNCTIONS WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2002062800003 20020628 00003 WP 2002 6 28 UPS02838133 1 20020409 A 5312 97516493N BULKHEAD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 FS 680, STR 32 LT AFT SIDE OF BULKHEAD HAS 2 CRACKS. REMOVED OLD BULKHEAD AND INSTALLED NEW BULKHEAD IAW DC8 SRM 51-1-2 D WG'S 9750428, 3750826, 4750426, 5750365, 3750447. 2 L 7 4 4F RT 4A25 2002062800004 20020628 00004 WP 2002 6 28 UPS02838134 1 20020501 A 5311 97504287U FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 FABRICATE FRAME. FABRICATED FRAME IAW DAC DWG 9750428. 2 L 7 4 4F RT 4A25 2002062800005 20020628 00005 WP 2002 6 28 UPS02838135 1 20020420 A 5320 37504972N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 LWR FILLET AREA STA 660 L36R FITTING CRACKED. REMOVED FITTING AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800006 20020628 00006 WP 2002 6 28 UPS02838136 1 20020416 A 5720 STRUCTURE DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 CRACK INDICATION FOUND BY NDT ON HOLE NR 10 LT. REPAIRED IAW REO - G08603 REV A. 2 L 7 4 4F RT 4A25 2002062800007 20020628 00007 WP 2002 6 28 UPS02838137 1 20020414 A 5320 47507182 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 FITTING AT BS 702, L36 LT SIDE HAS CRACK. REMOVED AND REPLACED CRACKED FITTING IAW DC8 SRM 51-1-20D AND 51-3-2. 2 L 7 4 4F RT 4A25 2002062800008 20020628 00008 WP 2002 6 28 UPS02838138 1 20020414 A 5320 47507182 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 FITTING AT BS 702, L36 RT SIDE HAS CRACK. REMOVED AND REPLACED CRACK FITTING IAW DC8 SRM 51-1-20D, 5 1-3-1. 2 L 7 4 4F RT 4A25 2002062800009 20020628 00009 WP 2002 6 28 UPS02838139 1 20020414 A 5320 47504261 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 BS 683 LONGERON 36 LT SIDE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND DWG 6750428. 2 L 7 4 4F RT 4A25 2002062800010 20020628 00010 WP 2002 6 28 UPS02838140 1 20020414 A 5320 47504261 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 BS 683 LONGERON 36 RT SIDE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21D AND DWG 9750428. 2 L 7 4 4F RT 4A25 2002062800011 20020628 00011 WP 2002 6 28 UPS02838141 1 20020430 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 FASTENER HOLES AT INTERSECTION OF L34R AND FS FRAME AT STA 56 ARE CORRODED AND CRACKED. FABRICATED A ND INSTALLED REPAIR IAW DC8 SRM 53-2-2. 2 L 7 4 4F RT 4A25 2002062800012 20020628 00012 WP 2002 6 28 UPS02838143 1 20020409 A 5310 5750365770 SHEAR PIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 FS 717 STR 33 LT SHEAR TIE CRACKED. REMOVED AND REPLACED SHEAR TIE IAW DAC DWG 5750365. 2 L 7 4 4F RT 4A25 2002062800013 20020628 00013 WP 2002 6 28 UPS02838144 1 20020501 A 5311 5750365050 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 FS 702, STR 31 LT FRAME CRACKED AT END. REMOVED AND REPLACED FRAME IAW DAC DWG 5750365. 2 L 7 4 4F RT 4A25 2002062800014 20020628 00014 WP 2002 6 28 UPS02838145 1 20020411 A 5320 37592221N SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 LONGERON 34 RIGHT SPLICE FITTING CRACKED AT BS 1270 IN AFT PIT. REMOVED L34R IAW DC8 SRM 51-1-21, IN STALLED NEW LONGERON IAW DC8 51-1- 21. 2 L 7 4 4F RT 4A25 2002062800015 20020628 00015 WP 2002 6 28 UPS02838183 1 20020509 A 3350 6012235 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY BATTERY PACK, CHECKED WORKED OK. 2 L 7 4 4F RT 4A25 2002062800016 20020628 00016 WP 2002 6 28 UPS02838230 1 20020513 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:N/A GLARESHIELD AND EMERGENCY OVERHEAD LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT B ATTERY PACK PER MM 33-50-01. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2002062800017 20020628 00017 WP 2002 6 28 UPS02838256 1 20020416 A 5711 SPAR DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 CRACK INDICATIONS FOUND BY NDT ON HOLE NR 9 LT. REAMED AND COINED HOLE, FABBED AND INSTALLED BUSHING IAW REO G08603. 2 L 7 4 4F RT 4A25 2002062800018 20020628 00018 WP 2002 6 28 UPS02838257 1 20020411 A 5320 DC853B003501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 CORROSION ON LOWER SURFACE OF CABIN FLOOR PANEL BS 400 TO 480, LBL 24 IN FWD PIT. REMOVED AND REPLAC ED FITTINGS AND SPLICE IAW EO DC8-53202-5167, DC8 SRM 53-7-3, 51-3-0, 53-2-3, & 51-3-1F. 2 L 7 4 4F RT 4A25 2002062800019 20020628 00019 WP 2002 6 28 UPS02838258 1 20020409 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 FUS STA 857, BL 60 LEFT, ANGLE CRACKED, LOWER FILLET PANEL AREA. REMOVED AND REPLACED CRACKED ANGLE IAW REO-G-08094. 2 L 7 4 4F RT 4A25 2002062800020 20020628 00020 WP 2002 6 28 UPS02838259 1 20020414 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 BS 683 BETWEEN L31 & L30R HAS CRACKED FITTING. REMOVED DAMAGED FITTING IAW DC8 SRM 51-1-20D, LOCATED DRILLED AND DEBURRED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800021 20020628 00021 WP 2002 6 28 UPS02838260 1 20020507 A 5314 KEELBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 FWD LOWER CARGO L36 CORRODED BETWEEN FS 620 & FS 640. REPAIR FWD LWR CARGO L36 LT IAW REO G08587 REV A & UPS EO DC8-5300-1 6674-B. 2 L 7 4 4F RT 4A25 2002062800022 20020628 00022 WP 2002 6 28 UPS02838279 1 20020412 A 5532 SKIN DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:N/A CORROSION AND PILLOWING OF SKIN ON VERTICAL STAB AFT LT SIDE. REMOVED PANEL AND ROUTED TO VENDOR FO R FABRICATION. TRIMMED AND INSTALLED NEW PANEL. 2 L 7 4 4F RT 4A25 2002062800023 20020628 00023 WP 2002 6 28 UPS02838281 1 20020415 A 5711 SPAR DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 CRACK INDICATIONS FOUND BY NDT ON HOLE NR 9 LT. REAMED AND COINED HOLE, FABBED AND INSTALLED BUSHING IAW REO G08603. 2 L 7 4 4F RT 4A25 2002062800024 20020628 00024 WP 2002 6 28 UPS02838283 1 20020411 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 L-2 LWR FWD DOOR JAMB, CORNER CRACKED AT 3 FASTENER HOLES. TRIMMED DAMAGE, FABRICATED AND INSTALLED REPAIR PER DC8 SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2002062800025 20020628 00025 WP 2002 6 28 UPS02838285 1 20020416 A 5711 SPAR DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 CRACK INDICATIONS FOUND BY NDT ON HOLE NR 11 LT. REAMED AND COINED HOLE, FABBED AND INSTALLED BUSHIN G IAW REO G08603. 2 L 7 4 4F RT 4A25 2002062800026 20020628 00026 WP 2002 6 28 UPS02838286 1 20020411 A 5347 6015176 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:C2 SEAT TRACK NR 6 CORRODED ON UNDERSIDE AT STA 783. REMOVED DAMAGED SECTION OF TRACK. FABRICATED NEW SECTION OF TRACK AND SPLICE IAW UPS EO DC8-5320-5167-C. INSTALLED TRACK AND SPLICES IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002062800027 20020628 00027 WP 2002 6 28 UPS02838354 1 20020521 A 3350 6012235 BATTERY DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA H DEACTIVATE SYST/CIRCUITS G MULTIPLE FAILURE CL CLIMB 1 SO 01 880UP 46080 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ON AT ALL TIMES. DISARM CHECK NORMAL. REPLACED EMERGENCY LIGHTING BATTERY AN D RELAY UNIT IAW 33-50-01. 2 L 7 4 4F RT 4A25 2002062800028 20020628 00028 WP 2002 6 28 UPS02838359 1 20020423 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 L1 LWR AFT DOOR JAMB CORNER CRACKED EXT FUSELAGE SKIN AT FASTENER HOLE. FABBED FILLER AND DOUBLER I AW DC8 SRM 53-2-0 TR 53-128. INSTALLED FILLER AND DOUBLERS IAW DC8 SRM 53-2-0/TR 53-128. 2 L 7 4 4F RT 4A25 2002062800029 20020628 00029 WP 2002 6 28 UPS02838360 1 20020424 A 5320 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 AFT PIT FS 1490 L32L SPLICE FITTING IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D & 51-1-21, INS TALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800030 20020628 00030 WP 2002 6 28 UPS02838361 1 20020424 A 5320 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 AFT PIT FS 1490 L33L SPLICE FITTING IS CORRODED. REMOVED SPLICE FITTING RECD LOCATED DRILLED IAW DC 8 SRM 51-1-24, INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800031 20020628 00031 WP 2002 6 28 UPS02838362 1 20020503 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 LONGERON 19R IS CRACKED AT BS 490 IS CRACKED AT BS 490 IN UPPER CARGO COMPT. REMOVED DAMAGED SECTIO N IAW DC8 SRM 53-2-2 FIG 10. FABBED NEW STRAPS IAW DC8 SRM 53- 2-2 FIG 10, INSTALLED LONGERON AND STRAPS IAW 51-1-11, 5 1-1-21, 51-1-20D. INSTALLED LONGERON SPLICE IAW DC8 SRM 51-1-20D, REINSTALLED SKIN. 2 L 7 4 4F RT 4A25 2002062800032 20020628 00032 WP 2002 6 28 UPS02838363 1 20020422 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 CABIN (CARGO) SEAT TRACK AT RBL 25 BS 55 HAS BROKEN LOBES. BLENDED SEAT TRACK OUT OF LIMITS IAW DC8 SRM 53-2-3, FABBED SEAT TRACK IAW DC8 SRM 53-2-3 A&P IAW DC8 SRM 51-1-8. INSTALLED NEW TRACK AND FLOORBOARDS IAW DC8 S RM 51-3-0. 2 L 7 4 4F RT 4A25 2002062800034 20020628 00034 WP 2002 6 28 UPS02838368 1 20020422 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 IN MAIN CABIN BETWEEN STA 1140L & 1160L ABOVE HORIZONTAL SKIN SPLICE NEAR L16 FOUND SURFACE CORROSIO N ON LWR SIDE OF INTERCOSTAL. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-1-8 WITHIN LIMITS PER UPS DC 8 SRM 53-2-0, ALO DINED IAW UPS DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 2002062800035 20020628 00035 WP 2002 6 28 UPS02838369 1 20020423 A 5320 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 FWD CARGO PIT AT FS 440-460 LONG 31R SPLICE FITTING IS CRACKED. REMOVED INTERCOSTAL AND SPLICE, PRO CURED NEW SPLICE, LOCATED AND DRILLED HOLES, INSTALLED NEW SPLICE AND INSTALLED INTERCOSTAL IAW UPS DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002062800036 20020628 00036 WP 2002 6 28 UPS02838370 1 20020423 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1180 T-BOLT BACK UP FITTING IS CRACKED. REMOVED AND INSTALLED FITTING IAW DC8 S RM 51-3-2. 2 L 7 4 4F RT 4A25 2002062800037 20020628 00037 WP 2002 6 28 UPS02838371 1 20020423 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 AFT CARGO PIT FS 1190 T-BOLT BACK-UP FITTING IS CRACKED. REMOVED AND INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800038 20020628 00038 WP 2002 6 28 UPS02838372 1 20020423 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1200 T-BOLT BACK-UP FITTING IS CRACKED. REMOVED FITTING, LOCATED AND DRILLED EX ISTING HOLES IAW DC8 SRM 51-3-2, INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800039 20020628 00039 WP 2002 6 28 UPS02838373 1 20020423 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1210 T-BOLT BACK-UP FITTING IS CRACKED. REMOVED FITTING, LOCATED AND DRILLED EX ISTING HOLES IAW DC8 SRM 51-3-2, INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800040 20020628 00040 WP 2002 6 28 UPS02838374 1 20020502 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 B-PIT DOOR AREA FWD JAMB CRACKED. FABBED AND HEAT TREATED IAW DC8 SRM 51-1-8 DAC DWG 3712791, DRILL ED AND INSTALLED ANGLE IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 2002062800041 20020628 00041 WP 2002 6 28 UPS02838376 1 20020523 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA H DEACTIVATE SYST/CIRCUITS O OTHER CL CLIMB 1 SO 01 880UP 46080 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ON AT ALL TIMES. DISARM CHECK NORMAL. REMOVED AND REPLACED EMERGENCY BATTERY PACK. 2 L 7 4 4F RT 4A25 2002062800042 20020628 00042 WP 2002 6 28 UPS02838379 1 20020521 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ON AT ALL TIMES. DISARM CHECK NORMAL. REPLACED EMERGENCY LIGHTING BATTERY AN D RELAY UNIT IAW 33-50-01, CHECKS GOOD. 2 L 7 4 4F RT 4A25 2002062800043 20020628 00043 WP 2002 6 28 UPS02838380 1 20020507 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 AFT PIT FS 1152 INTERCOSTAL FITTING AT L33R IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D, RECD LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800044 20020628 00044 WP 2002 6 28 UPS02838381 1 20020502 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 AFT PIT FS 1220 BANANA FITTING AT L32R L34R IS CRACKED. REMOVED AND REPLACED NEW FITTING IAW DC8 SR M 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800045 20020628 00045 WP 2002 6 28 UPS02838382 1 20020424 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 EMPENNAGE INTERIOR L17 RT CRACKED AT FS 1769. REPAIRED AREA IAW DC8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2002062800046 20020628 00046 WP 2002 6 28 UPS02838383 1 20020425 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 EMPENNAGE INTERIOR L17 RT CRACKED AT FS 1769. REPAIRED IAW DC8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2002062800047 20020628 00047 WP 2002 6 28 UPS02838384 1 20020423 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 L2 UPPER AFT DOOR JAMB CORNER HAS CRACK INDICATION JUST ABOVE DOOR STOP, INNER LAYER. REPAIRED AREA IAW DC8 SRM 53-2-0 FIG 18 AND TR 53-134 AND 53-135. 2 L 7 4 4F RT 4A25 2002062800048 20020628 00048 WP 2002 6 28 UPS02838385 1 20020516 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 R2 UPPER AFT DOOR JAMB CORNER CRACKED 2ND OR 3RD LAYER AND INNER LAYER CRACKED. REPAIRED IAW EO DC8 5330-12075G. 2 L 7 4 4F RT 4A25 2002062800049 20020628 00049 WP 2002 6 28 UPS02838386 1 20020423 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1230 AT LONG 33R BANANA FITTING IS CRACKED. REMOVED AND REPLACED IAW DC8 SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 2002062800050 20020628 00050 WP 2002 6 28 UPS02838387 1 20020423 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1200 BETWEEN LONG 34R - 35R Z-FITTING IS CORRODED. FOUND FITTING TO BE CRACKED UPON FURTHER INSPECTION. REMOVED FITTING IAW DC8 SRM 51-1-20D, FABBED REPAIR SPLICES IAW DC8 SRM 53-2-0, AND INSTALLED FITTING AND SPLICES IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800051 20020628 00051 WP 2002 6 28 UPS02838388 1 20020423 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1200 BETWEEN L33R-L34R FITTING, Z-FITTING IS CORRODED AND HAS SHEARED FASTENERS. FOUND FITTING TO BE CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, LOCATED AND DRILLED NEW FITTING IAW DC8 SR M 51-1-24, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800052 20020628 00052 WP 2002 6 28 UPS02838389 1 20020423 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 AFT CARGO PIT AT FS 1180 BETWEEN LONG 33R - 34R Z-FITTING IS CRACKED. REMOVED CORROSION PER DC8 SRM 51-1-8, FOUND TO EXCEED LIMITS PER DC8 SRM 53-2-0. REMOVED PLD FITTING PER DC8 SRM 51-1-20D, LOCATED AND DRILLED NEW F ITTING AND REPAIR ANGLES PER DC8 SRM 53-2-0 FIG G, INSTALLED FITTING AND ANGLES PER DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800053 20020628 00053 WP 2002 6 28 UPS02838390 1 20020521 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 EMERGENCY LIGHT BATTERY DEAD. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK GOOD IAW UPS DC8 MM 3 3-50-01. 2 L 7 4 4F RT 4A25 2002062800054 20020628 00054 WP 2002 6 28 UPS02838391 1 20020510 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 SEAT TRACK E AT STA 1140 CORRODED AT POSITION-B. REMOVED AND REPLACED SECTION OF SEAT TRACK IAW DC8 SRM 53-2-3 AND UPS EO DC8-5320-5167C. 2 L 7 4 4F RT 4A25 2002062800055 20020628 00055 WP 2002 6 28 UPS02838392 1 20020423 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C13 AFT CARGO PIT FS 1170 T-BOLT BACK UP FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW DC8 SRM 53-2-0 & 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800056 20020628 00056 WP 2002 6 28 UPS02838404 1 20020512 A 5320 ATTACH FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 MAIN CABIN RT SIDE STA 759 L13R ATTACH FITTING CRACKED. REMOVED DAMAGED PART AND INSTALLED NEW PART IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800057 20020628 00057 WP 2002 6 28 UPS02838405 1 20020513 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 MAIN CABIN AT STA 345 STR 17R INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL. REMOVED DAMAGE INTERCOSTAL AND GUSSET, FABBED NEW INTERCOSTAL AND GUSSET, INSTALLED INTERCOSTAL AND GUSSET IAW TPS 1003 DC8 SRM. 2 L 7 4 4F RT 4A25 2002062800058 20020628 00058 WP 2002 6 28 UPS02838406 1 20020512 A 5320 37544731N SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 A-PIT L-31-L STA 380-400 SPLICE IS CRACKED 4 INCHES LONG. REMOVED CRACKED FITTING SPLICE IAW DC8 SRM 51-1-20D, LOCATED DRILLED AND DEBURRED NEW FITTING, INSTALLED AT LONG 31L, STA 390 IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800059 20020628 00059 WP 2002 6 28 UPS02838467 1 20020525 A 3243 ACCUMULATOR DOUG DC8 DC873F 302199F WP LT MLG LEAKING A IPXA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 01 804UP 46004 INSPECTION TYPE:N/A ATB NO BRAKES ON LT SIDE OF A/C FROM THE CAPTS, F/O, POS, WHILE TAXING HYD BRAKE PRESS IS LOW AND FW D ACCUMULATOR IS FLAT. UPON INVESTIGATION FOUND HYD FLUID COMING OUT OF FWD BRAKE ACCUMULATOR. REMOVED AND REPLACED FW D BRAKE ACCUMULATOR IAW 32-42-04 MM. SERVICED AS REQUIRED AND SYS OPS CHECK GOOD AND LEAK CHECK GOOD. 2 L 7 4 4F RT 4A25 2002062800060 20020628 00060 WP 2002 6 28 UPS02838470 1 20020526 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:N/A LIGHT BULBS VERY DIM WHEN EMERGENCY LIGHT SWITCH SELECTED TO ARM. SUSPECT LOW BATTERY. REMOVED AND REPLACED EMERGENCY BATTERY PACK MM 33-50-01, OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2002062800061 20020628 00061 WP 2002 6 28 UPS02838523 1 20020515 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 COCKPIT VERT WEB I/B SIDE AT FS 6 RBL 14. BLENDED CORROSION ON WEB IAW DC8 SRM 51-1-8, WITHIN LIMITS DC8 SRM 53-2-0. REMOVED L-ANGLE IAW DC8 SRM 51-1-21 OUT OF LIMITS IAW DC8 SRM 53-2-0, AND INSTALLED L-ANGLE IAW DC8 SR M 51-1-8 AND 51-1-21. 2 L 7 4 4F RT 4A25 2002062800062 20020628 00062 WP 2002 6 28 UPS02838524 1 20020513 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 STA 220 STR 20R FRAME CRACKED. REMOVED DAMAGE FRAME SECTION AND REPAIRED PER DC8 SRM 53-2-0 FIG 2 AN D 51-1-8. 2 L 7 4 4F RT 4A25 2002062800063 20020628 00063 WP 2002 6 28 UPS02838525 1 20020513 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 MAIN CABIN AT STA 240 BETWEEN STR 19R & STR 20R FRAME IS BENT AND IMPROPERLY REPAIRED. REMOVED OLD R EPAIR. FABRICATED AND INSTALLED FRAME REPAIR IAW DC8 SRM 53-2-0 FIG 2A. 2 L 7 4 4F RT 4A25 2002062800064 20020628 00064 WP 2002 6 28 UPS02838526 1 20020515 A 5320 ATTACH ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 MAIN CABIN AT STA 832 RBL 38 AFT SIDE OF INTERCOSTAL ATTACH ANGLE GOUGED. REMOVED AND REPLACED DAMAG ED ANGLE IAW DC8 SRM 51-1-20D & DAC DWG 5773 275. 2 L 7 4 4F RT 4A25 2002062800065 20020628 00065 WP 2002 6 28 UPS02838528 1 20020515 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 R-1 DOOR CUTOUT UPPER FWD CORNER SHOWS CRACK INDICATION ON THE FIRST FASTENER HOLE IN THE FIRST ROW O F RIVETS. REPAIRED DOOR CORNER IAW DC8 SRM 53-2-0 FIG 14. 2 L 7 4 4F RT 4A25 2002062800066 20020628 00066 WP 2002 6 28 UPS02838529 1 20020512 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 A-PIT TORQUE BOX WEB HAS BROKEN SHEAR TIE AT STA 280 L33R. FABRICATED WEB IAW DAC DWG 5753892. FABR ICATED SPLICE DOUBLER IAW DC8 SRM 53-2-0. INSTALLED WEB AND SPLICE IAW DC8 SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 2002062800067 20020628 00067 WP 2002 6 28 UPS02838531 1 20020515 A 5315 5779772485 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 AFT PIT - STA 1060 CABIN FLOORBEAM UPPER AFT FLANGE IS CRACKED HORIZONTALLY ACROSS AFT EDGE AT RBL 60 . CUTOUT CRACKED AREA IAW REO G08643. FABRICATED REPAIR ANGLE IAW REO G08643. INSTALLED REPAIR ANGLE AND FLOOR PANEL IAW DC8 SRM 51-1-20D, 51-1-11, & 51-3-0. 2 L 7 4 4F RT 4A25 2002062800068 20020628 00068 WP 2002 6 28 UPS02838532 1 20020512 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1, RT MLG W/W LONG 2R CRACKED BY UPLOCK MOUNT. FABRICATED REPAIR PARTS IAW DC8 SRM 53-2-2 TR 53-123. INSTALLED REPAIR IAW DC8 SRM 53-2-2 TR 53-123 AND DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800069 20020628 00069 WP 2002 6 28 UPS02838533 1 20020512 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1, A-PIT DOOR TORQUE BOX FRAME HAS EXFOLIATION CORROSION AT STA 280 L 32-33R INSIDE LIGHTNING HOLE. RE MOVED CORROSION FROM FRAME IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. FRAME REPAIRED IAW TIMCO REO G08626. 2 L 7 4 4F RT 4A25 2002062800070 20020628 00070 WP 2002 6 28 UPS02838534 1 20020512 A 5743 36560042 FITTING DOUG DC8 DC871F 302199D WP RT MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1, RT MLG W/W TRAPEZOID TO WING LOWER OUTBOARD FITTINGS CRACKED. REMOVED FITTINGS, DRILLED UP AND INST ALLED NEW FITTINGS IAW DAC DWGS 5656229, 3641117 AND 3656004. REINSTALLED STIFFENER AND ACCESS PNLS IAW DC8 M/M 51-1-20 D AND 51-3-0. 2 L 7 4 4F RT 4A25 2002062800071 20020628 00071 WP 2002 6 28 UPS02838535 1 20020529 A 5320 577384659 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1, CABIN FLOOR SUPPORT BRACKET HAS EXFOLIATED CORROSION AT STA 1754, BL 0. REMOVED CORRODED FITTING BR ACKET IAW DC8 SRM 51-3-0, BRACKET WAS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, INSTALLED FITTING SUPPORT BRACKET IA W DC8 SRM 51-3-1, 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800072 20020628 00072 NM 2002 6 28 ABXA020005 1 20020625 A 3610 7732846 SENSOR BOEING 767 767281 1385109 NM LEFT HAND DEFECTIVE A ABXA O OTHER O OTHER CR CRUISE 1 GL 23 788AX 28402 23021 Lt eng hi stage displayed. Lt hi stage light illuminated. Per non-normal check list the left pneumatic switch was cycled on/off with oily fumes coming into the cabin. Note: The remainder of the flight was operated with left engine bleed and left A/C pack off. Fumes cleared. Left pneumatic pressure read 14 psi with left side switch off. Replaced fan air temp sensor. Leak and ops checked good IAW B767 MM 36-11-17-4. 2 L 7 2 4F RT A1NM 2002062800073 20020628 00073 WP 2002 6 28 UPS02838536 1 20020515 A 5753 5751186504 FITTING DOUG DC8 DC871F 302199D WP T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 RT WING FLAP HINGE SUPPORT FITTING AT XF 339-7332 HAS A CRACK INDICATION WITH NDT OUTBOARD. FABBED B LOCK IAW DC8 DWG 5894377. INSTALLED FITTING IAW DC8 DWG 5751174 & 5894377. 2 L 7 4 4F RT 4A25 2002062800074 20020628 00074 WP 2002 6 28 UPS02838538 1 20020516 A 5320 575503226 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 FLOOR SUPPORT ANGLE CORRODED AT FS 1723 BL19R. REMOVED CORRODED SUPPORT ANGLE AT STA 1723 BL19R IAW DC8 SRM 51-3-0, SUPPORT ANGLE 5755032-26, DETERMINED TO BE CORRODED OUT OF LIMITS IAW DC8 SRM 53-2-0. INSTALLED NEW PA RT IAW DC8 SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 2002062800075 20020628 00075 WP 2002 6 28 UPS02838540 1 20020515 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 L-2 DOOR CUTOUT LOWER FWD CORNER SHOWS CRACK INDICATION ON FIRST FASTENER HOLE ABOVE DOOR PAN. FABRI CATED DOULBERS IAW DC8 SRM 53-2-0 FIG 18. INSTALLED DOUBLERS IAW DC8 SRM 51-1-8 & 51-3-0. 2 L 7 4 4F RT 4A25 2002062800076 20020628 00076 WP 2002 6 28 UPS02838541 1 20020520 A 5320 3704841501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1, STRINGER END FITTING CRACK STRINGER 51 2 MAIN. REMOVED AND REPLACED STRINGER END FITTING IAW DC8 SR M 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800077 20020628 00077 WP 2002 6 28 UPS02838542 1 20020517 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 INSIDE DOOR 60-VERT STAB CENTER SPAR CANTED BULKHEAD SHEAR TIE IS CRACKED BETWEEN L9L & L10L. FABRIC ATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-0 & 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800078 20020628 00078 WP 2002 6 28 UPS02838543 1 20020516 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 PROBLEM WITH FLOORBEAM CRACK UNDER FLANGE FS 1746 BL 2L. FABBED REPAIR PARTS IAW DC8 SRM 53-2-0. IN STALLED REPAIR PARTS IAW DC8 SRM 536-2-0 AND 51-2-20D. 2 L 7 4 4F RT 4A25 2002062800079 20020628 00079 WP 2002 6 28 UPS02838546 1 20020525 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 AFT PIT STA 1400 L33R & L34R WEB LIGHTENING HOLE CRACKED/SPLIT. CUT OUT DAMAGE PER DC8 SRM 53-2-0. INSTALLED PER DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002062800080 20020628 00080 WP 2002 6 28 UPS02838559 1 20020605 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY DISCHARGED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. CH ECKS OK. 2 L 7 4 4F RT 4A25 2002062800081 20020628 00081 NM 2002 6 28 DHL2002741011 1 20020627 A 2611 302842 SMOKE DETECTOR BOEING 727 7272Q9 138448M NM A DHLA A O UNSCHED LANDING OTHER J N WARNING INDICATION FALSE WARNING CR CRUISE 1 SO 01 741DH 21931 1) THE CARGO SMOKE LIGHT ILLUMINATED IN CRUISE AT FL 370. REMAINED ON UNTIL JUST PRIOR TO LANDING 2) DEFERRED PER MEL 26-14 COMPLIED WITH SP26-14 ASSIGNED DMI # 9726 PLACARD INSTALLED.3) REF TO DMI # 9726 (THE CARGO SMOKE LIGHT ILLUM. IN CRUISE AT FL 370 REMAINED ON UNTIL JUST PRIOR TO LANDING)4) REMOVED AND REPLACED #1 & #5 SMOKE DETECTOR UNITS AND TEST ED PER AEIB-727 M/M 26-00 OPS CHECKS GOOD DMI 9726 CLEARED PLACARD REMOVED. 2 L 7 3 4F RT A3WE 2002062800082 20020628 00082 WP 2002 6 28 UPS02838561 1 20020510 A 5320 3641004U1 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 LT WW FITTING AT STA 880 L4L HAS CORROSION. REMOVED FITTING, CUT NEW FITTING AND FABRICATED SPLICE P ARTS IAW DC8 SRM 53-2-0 FIG 8. INSTALLED FITTING IAW DC8 SRM 53-2-0 FIG 8 AND DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002062800083 20020628 00083 WP 2002 6 28 UPS02838563 1 20020527 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 MAIN CABIN INTERCOSTAL AT STA 67, RBL 44 IS CORRODED. TRIMMED OUT CORROSION AREA IAW DC8 SRM 53-2-0, FABRICATED REPAIR FILLER AND DOUBLER IAW DC8 SRM 53-2-0, INSTALLED REPAIR FILLER AND DOUBLER IAW DC8 SRM 53-2-0 AND DC8 SRM 51-1-20. 2 L 7 4 4F RT 4A25 2002062800084 20020628 00084 WP 2002 6 28 UPS02838565 1 20020515 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 AFT PIT FLOORBEAM CORRODED AT STA 1440 UPPER FWD FLANGE AT RBL 60. REMOVED CORROSION IAW DC8 SRM 51- 1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0. FOUND AFT FLANGE CORRODED REMOVED AFT FLANGE OF FLOORBEAM IAW TRSM 95T0345001 S TD 6310-001. FABBED REPAIR IAW REO G08652, INSTALLED REPAIR IAW DC8 SRM 51-1-20D & REO G08652. 2 L 7 4 4F RT 4A25 2002062800085 20020628 00085 WP 2002 6 28 UPS02838566 1 20020513 A 5320 26463482 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 LT MLG W/W STA 891 FITTING OVER LONG 24 CORRODED. REMOVED FITTING, DRILLED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D & 51-3-2. 2 L 7 4 4F RT 4A25 2002062800086 20020628 00086 WP 2002 6 28 UPS02838569 1 20020509 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 FUSELAGE SKIN BLENDOUT AT BS 550 RIGHT HAND SIDE ABOVE CARGO COMP DOOR EO DC8-5330-15732A, REPAIR AT C-CHECK. FABBED REPAIR DOUBLERS IAW DC8 SRM 53-2-0 FIG 20. INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 20. 2 L 7 4 4F RT 4A25 2002062800087 20020628 00087 WP 2002 6 28 UPS02838570 1 20020514 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 CTR FUSE SHEAR TIE CRACKED ON TOP OF FRAME STA 680 BL 0. REMOVED BRACKET DRILLED UP AND INSTALLED NE W BRACKET IAW DC8 SRM 51-1-8 AND DAC DWG 615535. 2 L 7 4 4F RT 4A25 2002062800088 20020628 00088 WP 2002 6 28 UPS02838576 1 20020607 A 5320 SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:B CK FWD PRESSURE BULKHEAD SUPPORT FRAME CRACK. FORMED DOUBLER IAW 53-2-0 FIG 1B. FABRICATED DOUBLERS PER SRM 53-2-0 FIG 1B. INSTALLED DOUBLER PER 53-2-0. 2 L 7 4 4F RT 4A25 2002062800089 20020628 00089 NM 2002 6 28 HNAA0200046 1 20020616 A 2431 5224871 MONITOR DHAV DHC8 DHC8102 2809003 NM INOPERATIVE A HNAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 07 906HA 17795 2102 9 MAIN AND AUX BATTERY HOT LIGHTS ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO TPA. REPLACED BATTERY TEMP MONITOR. 2 H 7 2 4T RT A13NM 2002062800090 20020628 00090 NM 2002 6 28 COOSDR020161 1 20020601 A 5330 SKIN BOEING 727 7272Q6 138407V NM FUSELAGE WORN A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 FUSELAGE SKIN - RIGHT SIDE BODY STATION 720D+11 INCHES, STRINGER 19R - SKIN WITH WEAR. 2 L 7 3 4F RT A3WE 2002062800091 20020628 00091 NM 2002 6 28 COOSDR020162 1 20020601 A 5712 RIB BOEING 727 7272Q6 138407V NM LT WING CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 RIB UPPER CHORD CORRODED, BETWEEN BS 836.95 AND BS 848.95 AT LEFT WING, BUTTOCK LINE 70.5. 2 L 7 3 4F RT A3WE 2002062800092 20020628 00092 NM 2002 6 28 COOSDR020163 1 20020601 A 5712 RIB BOEING 727 7272Q6 138407V NM LT WING CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 RIB UPPER CHORD CORRODED, BETWEEN BS 836.95 AND BS 848.95, AT LEFT WING, BUTTOCK LINE 70.5. 2 L 7 3 4F RT A3WE 2002062800093 20020628 00093 NM 2002 6 28 COOSDR020164 1 20020601 A 5330 SKIN BOEING 727 7272Q6 138407V NM FUSELAGE CRACKED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 SECTION 46-RIGHT FUSELAGE SKIN CRACKED AND CORRODED BETWEEN BS 1164.5 AND BS 1179 BETWEEN STR 26R AND STR 25R. 2 L 7 3 4F RT A3WE 2002062800094 20020628 00094 NM 2002 6 28 QXEA0200917 1 20020627 A 5270 HANDLE BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 DIRTY A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 411QX 4055 BOI - ABORTED TAKE-OFF DUE TO RIGHT REAR SERVICE DOOR CAUTION LIGHT ILLUMINATING. MAINTENANCE CLEANED AND LUBED SERVICE DOOR OUTSIDE HANDLE. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002062800095 20020628 00095 WP 2002 6 28 CALA0200369 1 20020628 A 5313 LONGERON DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 49635 INSPECTION FOUND A 1/4" CRACK IN LONGERON 2L AT BELTFRAME STA 1418. THE CRACKED SECTION OF LONGERON WAS CUT OUT AND A NE W SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 2002062800096 20020628 00096 WP 2002 6 28 CALA0200370 1 20020628 A 5320 WEB DOUG DC9 DC982 3022082 WP STA 1338 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND AFT R/H LAV SUBFLOOR AREA(WEB) BETWEEN INTERCOSTAL 23.875 AND 16.438 CRACKED AT THE O/B UPPER CORNER, S TA 1338. THE INTERCOSTAL WEB WAS REMOVED AND REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2002062800097 20020628 00097 WP 2002 6 28 CALA0200374 1 20020628 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 225 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND SEAT TRACK CORRODED AT STA 225, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51- 30-1. 2 L 7 2 4F A6WE 2002062800098 20020628 00098 WP 2002 6 28 ABXA020008 1 20020628 A 2822 4TL6 SWITCH DOUG DC9 DC931 3022065 WP COCKPIT A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 924AX 47403 WHEN CENTER FORWARD BOOST PUMP WAS TURNED ON, SPARKS CAME OUT OF THE PANEL AND TWO CIRCUIT BREAKERS TRIPPED.REPLACED THE FORWARD CENTER BOOST PUMP ON/OFF SWITCH. 2 L 7 2 4F A6WE 2002071600166 20020716 00166 NM 2002 7 16 F3LA200200174 1 20020625 A 5320 INTERCOSTAL BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT STA 500A TO 500B, RBL 25. FABRICATED AND INSTALLED RE PLACEMENT INTERCOSTAL PER BOEING DRAWING 69-41473, SRM 51-30-2 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002062800099 20020628 00099 EA 2002 6 28 COMA0260388 1 20020625 A 3230 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 991CA 9911 7216 FLIGHT 5294 GEAR DISAGREE WARNING DURING RETRACION.REPLACED THE MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002062800100 20020628 00100 EA 2002 6 28 COMA0260389 1 20020626 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 721CA 7259 FLIGHT 5726 CABIN DOOR WARNING AFTER T/O.OUTER HANDLE NOT STOWED PROPERLY - INSPECTED AND OPERATED DOOR - FOUND NO DEFEC T. 2 L 7 2 4F RT A21EA 2002062800101 20020628 00101 EA 2002 6 28 COMA0260390 1 20020626 A 5210 601R386493 ROD CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR BROKEN A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 969CA 7141 FLIGHT 5037 AIRCRAFT WOULD NOT PRESSURIZE AFTER T/O.REPLACED BROKEN ROD ASSY AT DOOR VENT VALVE. 2 L 7 2 4F RT A21EA 2002062800102 20020628 00102 EA 2002 6 28 SWIA200210967 1 20020602 A 5315 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FLOOR SUPPORT CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 418SW 7446 FUSELAGE STA 621 RIGHT FLOOR SUPPORT ANGLE CRACKED AT RBL 42. REPAIRED ANGLE IAW REO 601R-53-61-117, REV. A. 2 L 7 2 4F RT A21EA 2002062800103 20020628 00103 EA 2002 6 28 SWIA200210968 1 20020602 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 418SW 7446 FOUND FUSELAGE STA 625 STR 15R ANGLE CRACKED. REPLACED ANGLE IAW CRJ SRM 51-42-06. P/N: 601R-35012-52. 2 L 7 2 4F RT A21EA 2002062800104 20020628 00104 EA 2002 6 28 SWIA200210969 1 20020602 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 418SW 7446 FUSELAGE STA 625 STR 15L ANGLE FOUND CRACKED.REPLACED ANGLE IAW CRJ SRM 51-42-06. P/N: 601R-35012-51. 2 L 7 2 4F RT A21EA 2002062800105 20020628 00105 EA 2002 6 28 SWIA200210970 1 20020602 A 5315 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FLOOR BEAM ATTAC CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 418SW 7446 FUSELAGE STA 280 FLOOR BEAM ATTACH ANGLE CRACKED AT RBL 9 OUTBOARD. REPLACED CRACKED ANGLE IAW CRJ SRM 51-42-13 & 51-4 2-21. P/N: 601R31113-58. 2 L 7 2 4F RT A21EA 2002063000001 20020630 00001 SO 2002 6 30 RAIA00206194 1 20020617 A 3411 0851HU PROBE EMB 145 EMB145 3260210 SO INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 801HK 2130 460 145053 5278-PIT- PITOT HEAT FAIL INDICATION #2 PROBE. MAINTENANCE DEFERRED #2 PITOT HEAT IAW MEL 30-31-00. MAINTENANCE SUBSEQUE NTLY CLEARED DMI BY REMOVING AND REPLACING THE #2 PITOT HEAT PROBE. 2 L 7 2 4F RT T00011AT 2002063000002 20020630 00002 SO 2002 6 30 RAIA00206195 1 20020623 A 2913 MPEV30086 PUMP EMB 145 EMB145 3260210 SO OVERHEATED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 804HK 8136 145082 5266-PIT- #1 HYDRAULIC SYS OVERHEAT INDICATION. MAINTENANCE REMOVED AND REPLACED THE #1 ELECTRIC HYDRAULIC PUMP, OPS AND LK CK OK. 2 L 7 2 4F RT T00011AT 2002063000003 20020630 00003 2002 6 30 RAIA00206196 4 20020623 A 3420 HG2010AL02 COMPUTER EMB 145 EMB145 3260210 SO OVERHEATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 803HK 99 61 145077 5270-PIT- #2 AHRS OVERHEAT INDICATION. MAINTENANCE REMOVED AND REPLACED THE #2 ATTITUDE HEADING REFERENCE COMPUTER, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002063000004 20020630 00004 EU 2002 6 30 RAIA00206197 1 20020624 A 2421 200322 SEAL AEROSP ATR42 ATR42300 8680920 EU LEAKING A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 422TE 106 5553-SBN- OIL LEAKING FROM #2 ENGINE DRAIN. MAINTENANCE REMOVED AND REPLACED AC GENERATOR MOUNT PAD SEALS, OPS AND LK CK OK. 2 H 7 2 4T RT A53EU 2002063000005 20020630 00005 EU 2002 6 30 RAIA00206198 1 20020625 A 3350 167001 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 423TE 119 5516-STL- EMERGENCY LIGHT ON STEPS INOP. REMOVED AND REPLACED STEPS EMERGENCY LIGHT BULB, OPS CK OK. 2 H 7 2 4T RT A53EU 2002063000006 20020630 00006 2002 6 30 RAIA00206199 4 20020626 A 3400 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 559HK 15764 1477 41075 5468-STL #1 SYMBOL GENERATOR FAILED DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE #1 SYMBOL GENERATOR, OPS CK OK. 2 L 7 2 4T RT A41NM 2002063000007 20020630 00007 SO 2002 6 30 RAIA00206200 1 20020627 A 3242 38793500 SHUTOFF VALVE EMB 145 EMB145 3260210 SO BYPASSING A RAIA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 CE 03 804HK 7847 145082 5319-MEM- #1 HYDRAULIC SYSTEM OVERHEAT INDICATION. MAINTENANCE REMOVED AND REPLACED BRAKE SHUTOFF VALVE LK AND OPS CK OK . 2 L 7 2 4F RT T00011AT 2002070100001 20020701 00001 WP 2002 7 1 UPS02838577 1 20020523 A 5320 SUPPORT FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 AFT PIT C3 DOOR RAMP PANEL FOLDING DOOR SUPPORT FITTING IS CRACKED. REMOVED PANEL AND FOUND SKIN CRA CK FABRICATE NEW SKIN IAW DAC DWG 97540 58. ALODINED & PRIMED IAW DC8 SRM 51-1-8. REMOVED SUPPORT FITTING LOCATED NEW FITTING AND DRILLED EXISTING FASTENERS IAW DC8 SRM 51-1-24, INSTALLED SUPPORT FITTING AND SKIN IAW DC8 SRM 51-1-24. 2 L 7 4 4F RT 4A25 2002070100002 20020701 00002 WP 2002 7 1 UPS02838578 1 20020603 A 5320 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 AFT LWR ATTACH STRUCTURE FOR RADIO RACK CLOSEOUT PANEL HAS LIGHT CORROSION AND BARE METAL ON INTERNAL AND EXTERNAL SIDES. REMOVED ANGLE IAW DC8 SRM 53-2-9 AND IAW DAC DWG 564057 1. FABBED IAW DAC DWG 5640571, INSTALLED CHANNEL IAW DC8 SRM 51-2-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 2002070100003 20020701 00003 WP 2002 7 1 UPS02838584 1 20020515 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 C-PIT FRAME REINFORCEMENT ANGLE HAS SEVERAL CRACKS & AN IMPROPER REPAIR STA 1150, L32R. REMOVED ATTA CH ANGLE IAW DC8 SRM 51-1-21D, FABRICATED REPLACEMENT PARTS IAW DC8 SRM 51-1-20D, INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002070100004 20020701 00004 WP 2002 7 1 UPS02838586 1 20020515 A 5753 5751186504 SUPPORT FITTING DOUG DC8 DC871F 302199D WP T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 RT WING FLAP HINGE SUPPORT FITTING AT XF 339-7332 HAS A CRACK INDICATION WITH NDT OUTBOARD. FABBED B LOCKS IAW DC8 DWG 5894377. LOCATED, DRILLED AND DEBURRED 3751728-502 FITTING & BASE FITTING IAW DC8 DWG 5894377. INSTA LLED 5751 186-508, 3751728-502, 5894377-5 & -27 AND 3655134N2 IAW DC8 DWG 5751 174 & 5894377. 2 L 7 4 4F RT 4A25 2002070100005 20020701 00005 WP 2002 7 1 UPS02838587 1 20020611 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:IN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01, OPS CHECK NORMAL . 2 L 7 4 4F RT 4A25 2002070100006 20020701 00006 WP 2002 7 1 UPS02838588 1 20020515 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 MAIN CABIN TOP MLG PRESSURE WEB AREA FLOORBEAM IS CRACKED AND CORRODED ON FWD & AFT LEG AT STA 900 LB L 44. REMOVED MVD CORROSION FROM FLOORBEAM, OUT OF LIMITS. FABBED REPAIR PARTS IAW R EO G08638 MPI OF REPAIR PARTS IAW ASTM E1444. NO CRACKS NOTED. INSTALLED REPAIR PARTS IAW SRM 51-1-21, 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2002070100007 20020701 00007 WP 2002 7 1 UPS02838590 1 20020528 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB CORNER CRACKED AT FASTENER HOLE EXTERNAL FUSELAGE SKIN LENGTH APPROX .25 TO .3125 INCH LONG. FOUND BY EDDY CURRENT. REPAIRED DOOR JAMB IAW DC8 SRM 53-2-0 FIG 16. 2 L 7 4 4F RT 4A25 2002070100008 20020701 00008 WP 2002 7 1 UPS02838591 1 20020527 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 FLOORBEAM AT STA 759 CHAFED BETWEEN RBL 0-24. REPAIRED FLOORBEAM IAW DC8 SRM 532-0 TR 53-124. 2 L 7 4 4F RT 4A25 2002070100009 20020701 00009 WP 2002 7 1 UPS02838592 1 20020527 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 FLOORBEAM AT STA 742 CHAFED BETWEEN RBL 0-24. REPAIRED FLOORBEAM IAW DC8 SRM 53-2-0 TR 53-124. 2 L 7 4 4F RT 4A25 2002070100010 20020701 00010 WP 2002 7 1 UPS02838593 1 20020527 A 5230 PLATE DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 MCD AFT VERT SCUFF PLATE AND DOUBLER ARE CRACKED STA 272 AND L10L. FABBED DOUBLER IAW DC8 SRM 51-1-8 , INSTALLED DOUBLER IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002070100011 20020701 00011 WP 2002 7 1 UPS02838594 1 20020602 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 MAIN CABIN 680 S11L LONGERON FITTING CRACKED. REMOVED FITTING, ALODINED, PRIMED & INSTALLED NEW FITT ING IAW DC8 SRM 51-1-8, 51-1-20D & 51-1-24. 2 L 7 4 4F RT 4A25 2002070100012 20020701 00012 WP 2002 7 1 UPS02838596 1 20020607 A 5240 INTERCOSTAL DOUG DC8 DC873F 302199F WP R1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 R1 DOOR FWD TORQUE BOX INTERCOSTAL JUST ABOVE LOWER CLEAR HINGE IS CRACKED. REMOVED INTERCOSTAL, FAB INTERCOSTAL IAW DAC DWG 5615700, ALODINED & PRIMED IAW DC8 SRM 51-1-21 & 511-20D. 2 L 7 4 4F RT 4A25 2002070100013 20020701 00013 WP 2002 7 1 UPS02838598 1 20020524 A 2133 OUTFLOW VALVE DOUG DC8 DC873F 302199F WP CABIN PRESSURE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 AFT ACCY COMPT CABIN AIR OUTFLOW NOZZLE VALVE HAS CORROSION AROUND AREA. CORROSION ON NOZZLE VALVE O UT OF LIMITS. REMOVED AND REPLACED NOZZLE IAW DC8 MM 21-31-04, OPS CHECKED IAW DC8 MM 21-31-04. 2 L 7 4 4F RT 4A25 2002070100014 20020701 00014 WP 2002 7 1 UPS02838599 1 20020526 A 5320 3774605501 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 MAIN CABIN UNDER FLOOR AT STA 67 RBL 40 BULGING. BLENDED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE O UT OF LIMITS IAW DC8 SRM 53-2-0. FABBED AND INSTALLED T EXTRUSION IAW TIMCO REO G08633, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 2002070100015 20020701 00015 WP 2002 7 1 UPS02838600 1 20020603 A 5313 525972423 STRINGER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 STA 1700 STRINGER 34L HAS CORROSION. BLENDED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED NEW REPAIR AND STRAPS IAW DC8 SRM 53-4-1 & 53-2-2. INSTALLED NEW PARTS IAW DC8 SRM 53-2-2 FIG 8. 2 L 7 4 4F RT 4A25 2002070100016 20020701 00016 WP 2002 7 1 UPS02838603 1 20020512 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 A-PIT L35R HAS 1 INCH LONG CRACK AT STA 343. FABBED AND INSTALLED NEW SECTION OF LONGERON AND U-CHAN NEL IAW TIM CO REO G068621 AND DC8 SRM 53-2-2 FIG 10 AND 51-1-20. 2 L 7 4 4F RT 4A25 2002070100017 20020701 00017 WP 2002 7 1 UPS02838604 1 20020525 A 5240 DOOR FRAME DOUG DC8 DC873F 302199F WP R1 DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 RT FWD DOOR UPPER FWD ELONGATED HOLE ON FRAME. FABBED DOUBLER IAW DAC DRW 5615762 AND INSTALLED SAME IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002070100018 20020701 00018 WP 2002 7 1 UPS02838618 1 20020527 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 FLOORBEAM AT STA 717 CHAFED BETWEEN RBL 0-24. REPAIRED FLOORBEAM IAW DC8 SRM 53-2-0 TR 53-124. 2 L 7 4 4F RT 4A25 2002070100019 20020701 00019 WP 2002 7 1 UPS02838619 1 20020525 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 L2 DOOR LWR FWD CORNER CRACKED, FOUND BY X-RAY INSPECTION. REPAIRED AREA IAW DC8 SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2002070100020 20020701 00020 NE 2002 7 1 MEX2002160 2 20020518 A 7321 769606158 FUEL CONTROL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE MALFUNCTIONED A ASMF D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SW 23 168PL 53174 FLT 132 - MEX-BJX - AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF LOW ACCELERATION IN BOTH ENGINES. A THROTTLE BUMP P ROCEDURE WAS ACCOMPLISHED, BOTH COMBUSTION CHAMBERS WERE LUBRICATED AND BOTH ENGINE WATER TRAMPS WERE SERVICED IAW MM FS B 6-98-10. DURING OVERNIGHT SERVICE, THE PS3 FILTER WAS CLEANED AND THE PRBC AND FCU LINES WERE CHECKED ON BOTH ENGINES . ADDITIONALLY, THE FCU OF ENGINE NR 1 WAS CHANGED IAW MM 73-20-1. ENGINES WERE TESTED IAW MM 71-00-00. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002070100021 20020701 00021 WP 2002 7 1 MEX2002168 1 20020521 A 2150 39613011 CONTROL VALVE DOUG DC9 DC982 3022082 WP A/C BAY FAILED A ASMF O OTHER J WARNING INDICATION DE DESCENT 1 SW 23 505MD 49149 FLT 315 - MEX-ACA - CAPTAIN REPORT THAT DURING DESCENT WITH INDICATIONS OF 22 AND 19 IN BOTH AIR CONDITIONING PACKAGES A ND WITH ALL VALVES CLOSED THE FLOW LIGHT TURNS ON. AIRCRAFT WAS SENT TO THE HANGAR. AFTER CHECK, THE RIGHT FLOW CONTRO L VALVE, THE RIGHT AIR CONDITIONING CHECK VALVE, THE AUGMENTATION VALVE AND THE TURBINE COOLING WERE REPLACED IAW MM 21- 31-2, 21-20-9, 36-10-01 AND 21-51-01, RESPECTIVELY. DURING OVERNIGHT SERVICE THE PRIMARY AND SECONDARY RADIATORS WERE R EPLACED IAW MM 21-51-1. (M) 2 L 7 2 4F A6WE 2002070100026 20020701 00026 WP 2002 7 1 MWEA020437 1 20020628 A 5330 5911428501 SKIN DOUG DC9 DC981 3022081 WP STATION 1407 BULGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 AFT ACCESSORY SECTION: SKIN IS BULGING 2 PLACES AT LONGERON 19 LEFT STATION 1407 VIEWED FROM OUTSIDE THE AIRCRAFT. -- FABRICATED AND INSTALLED FIT AND DRILLED UP REPAIR. 2 L 7 2 4F A6WE 2002070100027 20020701 00027 NM 2002 7 1 ABXA020009 1 20020627 A 2720 658D1003 ACTUATOR BOEING 767 767200 1385120 NM ONLY DEFECTIVE A ABXA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 23 785AX 39127 23018 During flight at all altitudes, rudder appeared to be failed in the faired position. Rudder control tab appeared to work normally. Rudder position indicator on status page had negative movement with full rudder pedal deflection. Rudder trim was inop. Removed rudder panels 324BL and 324EL. Visually inspected aft compartment and tail section, cables, rudder me chanism and associated parts. No defects noted. Ops check of rudder trim system normal IAW B767 FIM 27-21-00, fig. 106/ Checked rudder linkages during ops check. No binding found. Replaced rudder trim actuator and aileron/rudder trim contro l panel IAW B767 AMM 27-21-11-2 and 27-28-05 as a precaution. Reinstalled panels 324BL and 324EL. Removed rig pins use 2 L 7 2 4F RT A1NM 2002070100028 20020701 00028 EU 2002 7 1 QXEA0200920 1 20020628 A 3260 602EN1616 SWITCH FOKKER F28 F28MK4000 4990810 EU ZONE 700 INOPERATIVE A QXEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 09 491US 11156 BOI - ON APPROACH AND AFTER GEAR EXTENSION, THE LEFT MAIN DOOR AMBER LIGHT REMAINED ILLUMINATED. THE APPROACH WAS ABORTE D AND THE ALTERNATE GEAR EXTENSION WAS USED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE PLACED THE MAIN GEAR DOWN SAFE SWITCH AND RESET THE MAIN GEAR DOOR ALTERNATE EXTENSION CABLE. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002070100029 20020701 00029 SO 2002 7 1 C2XA02CL141 1 20020630 A 3350 74441 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16961 145103 DURING ROUTINE MAINTENANCE THE MAIN DOOR EMERGENCY LIGHT WILL NOT ILLUMINATE.MAINTENANCE REPLACED THE MAIN DOOR EMERGENC Y LIGHT.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002070100030 20020701 00030 NM 2002 7 1 SWAA021364 1 20020620 A 1100 BAV29PP533025 PLACARD BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 LEFT AND RIGHT OVERWING EMERGENCY EXIT PLACARDS MISSING. INSTALLED PLACARDS PER MM. 2 L 7 2 4F RT A16WE 2002070100031 20020701 00031 2002 7 1 SWAA021365 4 20020620 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ALL CABIN DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED C2 CHECK, FOUND ALL 4 CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER M M. 2 L 7 2 4F RT A16WE 2002070100032 20020701 00032 2002 7 1 SWAA021366 4 20020620 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED C4 CHECK, FOUND BOTH CABIN SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002070100033 20020701 00033 NM 2002 7 1 SWAA021371 1 20020620 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 DURING SCHEDULED PM CHECK, FOUND EEPLS TRACK COVERS CRACKED AND MISSING AT ROW NR 3 AND AT BOTH ENDS. INSTALLED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002070100034 20020701 00034 NM 2002 7 1 SWAA021372 1 20020620 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 500 PLUS 16, STR 10R AND BS 500D PLUS 18, 12L. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2002070100035 20020701 00035 NM 2002 7 1 SWAA021373 1 20020619 A 5522 65C25745 ELEVATOR BOEING 737 7373H4 1384600 NM RT ELEVATOR DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 1/2D CHECK, FOUND RT ELEVATOR DEBONDED ON LOWER SKIN AT 2ND MOST INBD HINGE POINT. REPAIRED ELEVATOR P ER SRM. 2 L 7 2 4F RT A16WE 2002070100036 20020701 00036 NM 2002 7 1 SWAA021374 1 20020619 A 5754 65C266012390A SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT CRACKED ON LOWER SKIN. REMOVED AND REPLACED NR 6 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2002070100037 20020701 00037 NM 2002 7 1 SWAA021375 1 20020620 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 081SW 22730 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CORRODED FROM BS 992 TO BS 1014, STR 27L. REPAIRED STR PER SRM. 2 L 7 2 4F A16WE 2002070100038 20020701 00038 NM 2002 7 1 SWAA021376 1 20020619 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 500D PLUS 4, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002070100039 20020701 00039 2002 7 1 SWAA021377 4 20020623 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002070100040 20020701 00040 2002 7 1 SWAA021379 4 20020621 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002070100041 20020701 00041 NM 2002 7 1 SWAA021383 1 20020623 A 5330 6551698 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 663, STR'S 4R AND 9L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002070100042 20020701 00042 NM 2002 7 1 SWAA021384 1 20020622 A 5753 6546435237 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED PM CHECK, FOUND LT OTBD T/E FLAP DELAMINATED ON BOTTOM SURFACE. REMOVED AND REPLACED LT OTBD T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002070100043 20020701 00043 NM 2002 7 1 SWAA021385 1 20020622 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071900090 20020719 00090 NM 2002 7 19 SWAA021386 1 20020622 A 5753 6571909118 SPAR BOEING 737 7372H4 138448C NM T/E FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED C4 CHECK, FOUND RIGHT OTBD T/E MID FLAP CRACKED AT AFT SPAR. REMOVED AND REPLACED RIGHT OTBD T/E MID F LAP PER MM. FLAP REAR SPAR WAS REPAIRED PER SWA EA. 2 L 7 2 4F A16WE 2002070100044 20020701 00044 NM 2002 7 1 SWAA021387 1 20020620 A 5753 6546434369 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED C2 CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED ON BOTTOM SURFACE. REMOVED AND REPLACED LT INBD AFT T /E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002070100045 20020701 00045 NM 2002 7 1 SWAA021388 1 20020621 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 859, LBL 13 AND LBL 8. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002070100046 20020701 00046 NM 2002 7 1 SWAA021389 1 20020623 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002070100047 20020701 00047 NM 2002 7 1 SWAA021390 1 20020621 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKS (4 EA) 3 INCHES ABOVE STR 10R, AT BS'S 500, 500C PLUS 12, 500C PLUS 16 AND 500 PLUS 15. REPAIRED SKIN PER SWA RA AND ER. 2 L 7 2 4F RT A16WE 2002070100048 20020701 00048 NM 2002 7 1 SWAA021391 1 20020620 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 500 PLUS 16, STR 10L. REPAIRED SKIN PER SWA RA AND ER. 2 L 7 2 4F RT A16WE 2002070100049 20020701 00049 NM 2002 7 1 SWAA021392 1 20020621 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002070100050 20020701 00050 NM 2002 7 1 SWAA021396 1 20020624 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 DURING PREFLIGHT, FOUND EXPOSED EEPLS WIRING BETWEEN ROW'S NR 6 AND NR 7. REMOVED AND REPLACED DAMAGED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002070100051 20020701 00051 NM 2002 7 1 SWAA021398 1 20020623 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACK AT BS 760, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002070100052 20020701 00052 NM 2002 7 1 SWAA021399 1 20020624 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, WL 208 AND LBL 17. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002070100053 20020701 00053 2002 7 1 SWAA021400 4 20020624 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTED. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002070100054 20020701 00054 NM 2002 7 1 SWAA021401 1 20020623 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER BROKEN AT ROW NR 9. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002070100055 20020701 00055 NM 2002 7 1 SWAA021402 1 20020623 A 3040 286A2006001 HARNESS BOEING 737 7377H4 1384404 NM COCKPIT OVERTEMP A SWAA K NONE M OVER TEMP AP APPROACH 1 SW 29 708SW 27842 DURING DESCENT HAD SPARKS SHOOT OUT OF FO'S SIDE WINDOW CANNON PLUG, SMELL OF BURNING RUBBER. REMOVED AND REPLACED NR 2 WINDOW HEAT COILED HARNESS PER MM. 2 L 7 2 4F RT A16WE 2002070100056 20020701 00056 NM 2002 7 1 UPS02238710 1 20020628 A 3350 RELAY BOEING 727 72751C 1384015 NM CABIN FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:N/A EMERGENCY LIGHTS ABOVE COCKPIT DOOR ILLUMINATED IN FLIGHT WITH ARM SWITCH IN THE ARMED POSITION. RE MOVED R70 RELAY. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2002070100057 20020701 00057 NM 2002 7 1 SWAA021419 1 20020627 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB 2 HINGE WORN. REMOVED AND REPLACED NR 2 HINGE BU SHING PER MM. 2 L 7 2 4F RT A16WE 2002070100058 20020701 00058 NM 2002 7 1 SWAA021420 1 20020626 A 5241 6545871132 DOOR BOEING 737 7375H4 138449D NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT AFT LOWER DOOR STOP. REMOVED AND REPLACED FWD SVC DOOR PER MM. 2 L 7 2 4F RT A16WE 2002070100059 20020701 00059 NM 2002 7 1 SWAA021421 1 20020627 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 12R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002070100060 20020701 00060 NM 2002 7 1 SWAA021422 1 20020627 A 5330 6545774 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 727B AT STR 4L, BS 787 AT STR 4R AND BS 663 AT STR 9R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002070100061 20020701 00061 NM 2002 7 1 SWAA021423 1 20020627 A 5310 693543656 SHEAR TIE BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR'S 14L AND 15L. REMOVED AND REPLACED SHEAR T IE PER SRM. 2 L 7 2 4F A16WE 2002070100062 20020701 00062 NM 2002 7 1 SWAA021424 1 20020627 A 5311 6546546 FRAME BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 13R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2002070100063 20020701 00063 NM 2002 7 1 SWAA021425 1 20020627 A 5313 65C27314 TIE CLIP BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED TIE CLIP PER SRM. 2 L 7 2 4F A16WE 2002070100064 20020701 00064 NM 2002 7 1 SWAA021426 1 20020627 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 081SW 22730 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT WINDOW BELT CUTOUT ON LT WINDOW'S NR 21, 25, 26, 27 AND 2 9. REPAIRED SKIN PER SWA SI. 2 L 7 2 4F A16WE 2002070100065 20020701 00065 NM 2002 7 1 SWAA021427 1 20020627 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 081SW 22730 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT WINDOW BELT CUTOUT ON RT WINDOW'S NR 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 26, 27, 28, 29, 30 AND 32. REPAIRED SKIN PER SWA SI. 2 L 7 2 4F A16WE 2002070100066 20020701 00066 NM 2002 7 1 UPS02438696 1 20020514 A 5712 RIB BOEING 747 747121 1384871 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C RHW- NR 22 L/E FLAP O/B ROTARY ACTUATOR MOUNTING RIB SURFACE CORRODED. CORROSION BLEND OUT AT SURFACE AT MOUNT BOLT HOLES NR 1 & 2 - 0.025" AT BOLT HOLES BORE NR 1 TO 6 - FINAL DIA 0.312" NR 7 - 0.371", NR 8 - 0. 312" RT WING NR 22 L/E FLAP O/B ROTARY ACTUATOR MOUNTING RIB REPAIRED AS PER RS R-57-41-34824. 2 L 7 4 4F A20WE 2002070100067 20020701 00067 NM 2002 7 1 UPS02438697 1 20020516 A 5712 65B078426 RIB BOEING 747 747121 1384871 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C RHW - NR 24 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 2, 3, 5 - 8 BOLT HOLE FOUND SURFACE CORR OSION. CORROSION BLEND OUT FINAL SIZE NR 2 & 3 - 0.388", NR 7 & 8 - 0.498". RT WING - NR 24 L/E FLAP O/B ROTARY ACTUAT OR MOUNT RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2002070100068 20020701 00068 NM 2002 7 1 UPS02438698 1 20020516 A 5712 65B078406 RIB BOEING 747 747121 1384871 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C RHW- NR 24 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1 - 8 BOLT HOLE FOUND SURFACE CORRODED. CORROSION BLEND OUT AT BOLT HOLES NR 1 & 8 - 0.434", NR 2 & 3 - 0.530", NR 7 - 0.465", NR 4 - 0.404", NR 5 - 0.437" , NR 6 - 0.404". RT WING- NR 24 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2002070100069 20020701 00069 NM 2002 7 1 UPS02438699 1 20020516 A 5712 65B078366 RIB BOEING 747 747121 1384871 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C RT WING- NR 23 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1 - 8 BOLT HOLE FOUND SURFACE CORRODE D. CORROSION BLEND OUT AT MOUNT BOLT HOLES FINAL DIAMETERS 0.371" TO 0.434". RT WING - NR 23 L/E FLAP O/B ROTARY ACTUA TOR MOUNT RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2002070100070 20020701 00070 NM 2002 7 1 UPS02438700 1 20020516 A 5712 65B078346 RIB BOEING 747 747121 1384871 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C RT WING- NR 23 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1 - 8 BOLT HOLE FOUND SURFACE CORRODE D. CORROSION BLEND OUT AT MOUNT BOLT HOLES FINAL DIAMETERS 0.434" - 0.500". RT WING- NR 23 L/E FLAP I/B ROTARY ACTUATO R MOUNT RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2002070100071 20020701 00071 NM 2002 7 1 UPS02438701 1 20020516 A 5712 65B078286 RIB BOEING 747 747121 1384871 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C RT WING- NR 22 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 5 & 6 BOLT HOLE FOUND SURFACE CORRODE D. CORROSION BLEND OUT AT BOLT HOLES FINAL DIAMETERS 0.371" TO 0.434" WITH NR 4, 5, 6 OVERSIZED ECCENTRICALLY. RT WING - NR 22 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2002070100072 20020701 00072 NM 2002 7 1 VNAA0206015 1 20020624 A 2700 CIRCUIT BREAKER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 425JS 3037 DURING TAKE OFF, THE CREW RECEIVED A TAKEOFF MISCONFIGURE CAS MESSAGE AND ABORTED TAKE OFF. MAINTENANCE ADVISED THE CR EW TO RECYCLE THE IAC CIRCUIT BREAKER AND THE MESSAGE CLEARED. FLIGHT 4182 WAS THEN CLEARED FOR ANOTHER TAKE OFF ATTEMP T AND DEPARTED WITHOUT ANY FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070100073 20020701 00073 NM 2002 7 1 VNAA0206016 1 20020624 A 6100 PROPELLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH A VNAA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 07 427JS 3039 AT APPROXIMATELY 1000 FEET AGL, THE CREW EXPERIENCED A STRONG VIBRATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AN D FOUND A FLAT SPOT ON THE NOSE WHEEL TIRE. MAINTENANCE REPLACED THE NOSE WHEEL TIRES IN ACCORDANCE WITH DORNIER MAINTE NANCE MANUAL 32-00-00. MAINTENANCE ALSO FOUND THE LEFT HAND PROP TO BE OUT OF BALANCE. MAINTENANCE BALANCED THE LEFT H AND PROP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WA S RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070100074 20020701 00074 NE 2002 7 1 VNAA0206018 2 20020625 A 7300 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 442JS 3060 DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND ENGINE CONTROL UNIT AND GENERATOR FAIL INDICATION. THE CREW FOLLOWED TH E QUICK REFERENCE HANDBOOK AND THE MESSAGES CLEARED. FLIGHT 4019 WAS CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND DEPARTED PIT WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070100075 20020701 00075 NM 2002 7 1 VNAA0206019 1 20020626 A 5200 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 458PS 3068 THE CREW REPORTED THE EMERGENCY EXIT DOOR SWITCH WAS FAILING INTERMITTENTLY. OUTSTATION MAINTENANCE INSPECTED AND FOUN D THE EMERGENCY EXIT DOOR SENSOR TO BE TOUCHING ITS TARGET. OUTSTATION MAINTENANCE ADJUSTED THE SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-71-00. OPERATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070100076 20020701 00076 NM 2002 7 1 UPS02438702 1 20020506 A 5312 141U10872 PRESSURE PANEL BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C BS 400 PRESSURE PAN, ONE EA FASTENER HOLE CRACK INDICATION REVEALED. PRESSURE PAN BS 400 REPLACED AS PER SRM 51-10-01 AND DWG 624U0005 STEERING CABLE CONNECTED, RIGGING CHECK AND O/P CHECK AS PER MM 32-51-00 FOUND SATISFA CTORY. 2 L 7 4 4F A20WE 2002070100078 20020701 00078 2002 7 1 SWAA021367 4 20020620 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVCIE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002070100079 20020701 00079 2002 7 1 SWAA021368 4 20020620 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002070100080 20020701 00080 2002 7 1 SWAA021369 4 20020619 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002070100081 20020701 00081 2002 7 1 SWAA021370 4 20020620 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 102SW 23108 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002070100082 20020701 00082 NM 2002 7 1 SWAA021378 1 20020621 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 761RR 27875 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS FWD END CAP BROKEN AND LIGHT INOP. REMOVED AND REPLACED END CAP AND RELAMPE D LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002070100083 20020701 00083 2002 7 1 SWAA021380 4 20020620 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002070100084 20020701 00084 NM 2002 7 1 SWAA021381 1 20020623 A 5320 65C27314 TIE CLIP BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STR TIE CLIP PER SRM. 2 L 7 2 4F A16WE 2002070100085 20020701 00085 NM 2002 7 1 SWAA021382 1 20020623 A 5320 6551698 SPLICE BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F A16WE 2002070100086 20020701 00086 NM 2002 7 1 C1HA200295011 1 20020628 A 3350 900835A BATTERY BOEING 727 727290 138408W NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 295AS 22147 EMERGENCY LIGHTING INOP ON FORWARD L/H WING.REMOVED AND REPLACED BATTERY PACK AT STATION 800 IAW 33-50-22 MM. OPS CK GOO D. 2 L 7 3 4F A3WE 2002070100087 20020701 00087 NM 2002 7 1 C1HA200293006 1 20020630 A 2752 MS9391130ZE4C MOTOR BOEING 727 727212 138407G NM A C1HA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS CR CRUISE 1 GL 15 293AS 21348 ENROUTE SYSTEM A QAUNITY WENT ZERO FOLLOWED BY ENG 1 HYD A LOW PRESSURE AND ENG 2 HYD A LOW PRESSURE LIGHTS ILLUMINATED. HYD SYSTEM A FLUED LOSS CHECKLIST WAS PERFORMED. NO HYD SYSTEM A OVERHEAT LIGHT ILLUMINATION.REINSPECTED AND FOUND OU TB FLAP HYDRAULIC DRIVE MOTOR LEAKING. REMOVED & INSTALLED OUTB FLAP HYDRAULIC DRIVE MOTOR PER MM 27-51-62, LEAK & OPS CK OK. SEE L.P. A28572 ITEM 1 FOR PART INFO 2 L 7 3 4F A3WE 2002070100088 20020701 00088 EA 2002 7 1 SWIA200210982 1 20020622 A 3260 BRACKET CNDAIR CL600 CL6002B19 1900309 EA NOSE GEAR BENT A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 442SW 7609 AFTER DEPARTURE, RETRACTED GEAR AND RECEIVED A GEAR DISAGREE AURAL MESSAGE. ALSO NOTED NOSE GEAR WAS INDICATING GREEN, NOSE DOOR OPEN WITH GEAR HANDLE UP AND MAINS UP AND LOCKED. RETURNED TO DFW. FOUND NOSE GEAR EXTEND PROXIMITY SWITCH B RACKET BENT. REPOSITIONED BRACKET AND ADJUSTED PROXIMITY SWITCH TO .050". SWUNG GEAR IAW 32-30-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002070100089 20020701 00089 WP 2002 7 1 MWEA020438 1 20020628 A 5240 5912995504 DOOR FRAME DOUG DC9 DC981 3022081 WP RH FWD DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 RIGHT FORWARD EMERGENCY EXIT HAS DAMAGE IN THE UPPER CENTER PORTION OF THE DOOR FRAME OUTBOARD OF THE LATCH BAR. -- IN STALLED FASTENERS AND REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002070100090 20020701 00090 NM 2002 7 1 CALA0200375 1 20020629 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 727E CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77303 23354 INSPECTION FOUND A 2" CRACK IN R/H FUSELAGE SKIN AT STA 727E, S24R. REPAIRED IAW SRM 53-00-01, FIGURE 201. 2 L 7 2 4F RT A16WE 2002070100091 20020701 00091 NM 2002 7 1 QXEA0200922 1 20020627 A 3350 6138001 BATTERY BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 BURNED OUT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 779 0 4037 PDX- EMERGENCY LIGHTS AT PASSENGER DOOR ARE OUT, ALSO, EGRESS LIGHTS IN CEILING AND FUSELAGE FOR PASSENGER DOOR ARE OUT. REMOVED AND REPLACED BATTERY PACKS AT PS1 LOCATION. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002070100092 20020701 00092 SO 2002 7 1 C2XA02SH015 1 20020618 A 5300 14521721005 STRAP EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 SHV - DURING C-CK INSPECTION, THE CENTER STRAP AT BETWEEN FRAMES 14 AND 17 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVE D THE DAMAGED SECTION OF THE STRAP, FABRICATED AND INSTALLED A REPAIR DOUBLER IN ACCORDANCE WITH EMB-145 SRM 53-21-02, A ND THE AIRCRAFT WAS APPROVED FOR RTEURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002070100093 20020701 00093 NM 2002 7 1 FE5F20020003 1 20020630 A 2121 HONEYWELL BOEING 757 75727A NM W FE5F D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 03 381127 29607 When A/C pushed back for departure, cabin attendant reported odor in the cabin.And then right recirculation fan fail mes sage displayed. After replaced the recirculation fan, the burnt ordor was smelled. 2 L 7 2 4F RT A2NM 2002070200193 20020702 00193 NM 2002 7 2 SWAA021393 1 20020622 A 2781 256A39022 SENSOR BOEING 737 7373H4 1384600 NM KRUEGER FLAP FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 611SW 27697 AIR TURNBACK, ON DEPARTURE NR 3 KRUEGER FLAP WOULD NOT RETRACT. REMOVED AND REPLACED S173 FULL EXTEND SENSOR PER MM. 2 L 7 2 4F RT A16WE 2002070200194 20020702 00194 NM 2002 7 2 SWAA021395 1 20020624 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 EEPLS LOOSE AT ROW NR 2. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002070200195 20020702 00195 2002 7 2 SWAA021397 4 20020624 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 415WN 29836 AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002070200196 20020702 00196 NM 2002 7 2 SWAA021403 1 20020621 A 2560 92001503 HINGE BOEING 737 7372H4 138448C NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 AFT OVERHEAD EMERGENCY BIN DOOR WOULD NOT OPEN AT ROW NR 21DEF. REPAIRED DOOR HINGE PER MM. 2 L 7 2 4F A16WE 2002070200197 20020702 00197 NE 2002 7 2 SWAA021404 2 20020621 A 7200 CFM56 ENGINE BOEING 737 7377H4 1384404 NM GE CFM56 CFM56* 13802 NE NR 2 MALFUNCTIONED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 29 718SW 27852 874265 INFLIGHT SHUT DOWN, DIVERSION, DURING CRUISE NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED, LIGHT REMAINED ON EVEN AT IDLE. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002070200198 20020702 00198 NM 2002 7 2 SWAA021417 1 20020626 A 3350 20131A BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS INOP IN FWD CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002070200199 20020702 00199 2002 7 2 SWAA021418 4 20020627 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002070200200 20020702 00200 NE 2002 7 2 SWAA021428 2 20020625 A 7321 9368M57P21 MEC BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FAILED A SWAA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 SW 29 390SW 26593 INFLIGHT SHUT DOWN, DECLARED EMERGENCY, DIVERSION, DURING CRUISE NR 2 ENGINE FAILED. REMOVED AND REPLACED NR 2 ENGINE M EC AND FUEL PUMP PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002070200201 20020702 00201 2002 7 2 VNAA0203010 4 20020308 A 3418 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE STALL WARNING MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 433JS 3047 DURING TAKEOFF, THE CREW RECEIVED AN ANGLE OF ATTACK CAS MESSAGE AND ABORTED TAKEOFF. AS THE AIRCRAFT CLEARED THE RUNWA Y THE MESSAGE CLEARED BY ITSELF, THE CONDITIONS WERE EXTREMELY WINDY. FLIGHT 4049 WAS CLEARED FOR ANOTHER TAKEOFF ATTEM PT AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200202 20020702 00202 NM 2002 7 2 VNAA0203011 1 20020309 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 457PS 2014 77 3048 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 3, 4, AND 5 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REP LACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORM ED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200203 20020702 00203 NE 2002 7 2 VNAA0203014 2 20020309 A 7261 OIL SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ENGINE LOW A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 432JS 3045 APPROXIMATELY 10 TO 15 MILES NORTH OF TRI-CITYS THE CREW RECEIVED A LOW OIL PRESSURE CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CALLED MAINTENANCE CONTROL AND DECIDED TO DIVERT TO TRI-CITYS. THE CREW PUT THE ENGINE IN FLT IDLE AND PROCEEDED TO TRI CITYS. OUTSTATION MAINTENANCE INSPECTED AND FOUND THE ENGINE OIL LOW AND SERVICED THE EN GINE OIL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 12-00-00. THE ENGINE WAS RAN AND OIL LEAKS WERE CHECKED FOR AND NONE WERE FOUND. THE ENGINE WAS PUT ON AN OIL CONSUMPTION WATCH LIST. SINCE 09MAR02 THE ENGINE HAS NOT USED MORE OIL T HAN USUAL. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200204 20020702 00204 NM 2002 7 2 VNAA0203018 1 20020312 A 2530 ODOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE GALLEY DETECTED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 440JS 3058 THE CREW REPORTED A BURNING SMELL IN THE HOT JUG AREA. MAINTENANCE INSPECT AND FOUND NO DEFECTS. THE AIRCRAFT WAS RELE ASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200206 20020702 00206 NM 2002 7 2 VNAA0203019 1 20020313 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 436JS 15574 3052 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING STRIP WAS NOT WORKING. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANC E INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY AND THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MAN UAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200207 20020702 00207 NM 2002 7 2 VNAA0203020 1 20020313 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 431JS 13849 3028 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING STRIP WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMER GENCY POWER SUPPLY AND THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200208 20020702 00208 2002 7 2 VNAA0203021 4 20020313 A 3425 FLIGHT DIR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 436JS 3052 DURING THE TAKEOFF, THE CREW RECEIVED A VNAV SYSTEM FAIL INDICATION AND ABORTED TAKEOFF. BEFORE THE AIRCRAFT CLEARED TH E RUNWAY THE SYSTEM RESET ITSELF. THE CREW CALLED MAINTENANCE CONTROL AND WAS TOLD TO TRY ANOTHER TAKEOFF ATTEMPT IF AL L SYSTEMS WERE WORKING. FLIGHT 4092 THEN ATTEMPTED ANOTHER TAKEOFF. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200209 20020702 00209 2002 7 2 VNAA0203022 4 20020313 A 3425 FLIGHT DIR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 436JS 3052 DURING THE TAKEOFF, THE CREW RECEIVED A VNAV SYSTEM FAIL INDICATION AGAIN AND ABORTED TAKEOFF. FLIGHT 4092 RETURNED TO THE GATE. MAINTENANCE CONTROL THEN MEL'D THE SYSTEM. FLIGHT 4092 THEN ATTEMPTED ANOTHER TAKEOFF AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200210 20020702 00210 2002 7 2 VNAA0203024 4 20020316 A 3418 STALL WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 426JS 3038 THE FLIGHT WAS ON THE TAKEOFF ROLL WHEN THE FLIGHT CREW RECEIVED A STALL PUSHER FAIL WARNING MESSAGE ON THE EICAS DISPLA Y. THE FLIGHT CREW ABORTED THE TAKEOFF AND EXITED THE RUNWAY. ONCE CLEARING THE RUNWAY THE WARNING MESSAGE CLEARED ITS ELF WITH NO ACTION FROM THE FLIGHT CREW. THE FLIGHT CREW THEN ATTEMPTED ANOTHER TAKEOFF AND WAS SUCCESSFUL WITH NO FURT HER PROBLEMS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200211 20020702 00211 2002 7 2 VNAA0203025 4 20020316 A 3460 COMPUTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 442JS 3060 THE FLIGHT WAS ON THE TAKEOFF ROLL WHEN THE FLIGHT CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL WARNING MESSAGE ON THE EICAS DISPLAY. THE FLIGHT CREW ABORTED THE TAKEOFF AND EXITED THE RUNWAY. ONCE CLEARING THE RUNWAY THE WARNING MESSAGE CLEARED ITSELF WITH NO ACTION FROM THE FLIGHT CREW. THE FLIGHT CREW THEN ATTEMPTED ANOTHER TAKEOFF AND WAS SUCCESSFUL WITH NO FURTHER PROBLEMS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200212 20020702 00212 NM 2002 7 2 VNAA0203026 1 20020316 A 7330 1060K SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 442JS 15918 3060 THE FLIGHT CREW WAS CLIMBING OUT OF PIT WHEN THE RIGHT ENGINE FUEL FEED TEMPERATURE WENT TO 78 DEGREES C. THE FLIGHT CR EW FOLLOWED THE QRH PROCEDURES BUT THE TEMPERATURE CLIMBED BACK UP. THE FLIGHT CREW CONTACTED MAINTENANCE CONTROL WHICH ADVISED THEM TO RETURN TO PIT. THE FLIGHT CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FUEL TEMPERA TURE SENSOR IN ACCORDANCE WITH THE MAINTENANCE MANUAL AND OPERATIONAL CHECKS WERE COMPLETED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200213 20020702 00213 NM 2002 7 2 VNAA0203027 1 20020318 A 2450 330GA01Y CONTROL BOX DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ELECTRICAL SYS FAULTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 471PS 15944 3007 THE FLIGHT CREW ABORTED THE TAKEOFF AFTER RECEIVING A LEFT ALTERNATOR FAIL AND LEFT AC VOLT FAIL WARNING MESSAGE. AFTER EXITING THE RUNWAY AND CYCLING THE CONDITION LEVER THE MESSAGES CLEARED. THE FLIGHT CREW ATTEMPTED ANOTHER TAKEOFF AND THE MESSAGES RETURNED. THE TAKEOFF WAS ABORTED AND THE FLIGHT CREW RETURNED TO THE GATE. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND REPLACED THE AC JUNCTION BOX IN ACCORDANCE WITH THE MAINTENANCE MANUAL 24-50-00. OPERATIONAL CHECKS WERE C OMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200214 20020702 00214 NM 2002 7 2 VNAA0203029 1 20020319 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 463PS 3087 DURING CLIMBOUT FROM PIT THE FLIGHT CREW RECEIVED A FLAP OVERSPEED WARNING INDICATION. THE FLIGHT CREW CONSULTED WITH M AINTENANCE CONTROL AND THE FLIGHT CREW RETURNED TO PIT. THE LANDING WAS WITHOUT INCIDENT. MAINTENANCE PERFORMED THE FL AP OVERSPEED INSPECTION IN ACCORDANCE WITH INSPECTION 05-51-00 AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200215 20020702 00215 NM 2002 7 2 VNAA0203030 1 20020318 A 2497 WIRE HARNESS DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ELECTRICAL SYS SHORTED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 471PS 3007 THE FLIGHT CREW ABORTED THE TAKEOFF AFTER RECEIVING A LEFT ALTERNATOR AND LEFT AC VOLTAGE FAIL WARNING MESSAGE. THE FL IGHT CREW RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED AND FERRIED THE AIRCRAFT TO CAK AND THEN DAY FOR FURTHER MAIN TENANCE INVESTIGATION. THE WIRING HARNESS WAS FOUND TO HAVE AN INTERNAL SHORT AND MAINTENANCE REPAIRED THE WIRE HARNESS IN ACCORDANCE WITH DORNIER SPECIAL PROBLEM REPORT A19753. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200216 20020702 00216 NM 2002 7 2 VNAA0203031 1 20020320 A 3397 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DAMAGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 429JS 3043 DURING ENGINE START THE FLIGHT CREW NOTED THAT THE EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE INSPECTED AND COR RECTED WIRING ON THE 1VE JUNCTION BOX IN ACCORDANCE WITH THE DORNIER WIRING MANUAL. OPERATIONAL CHECK WAS COMPLETED AND THE AIRCRAFT RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200217 20020702 00217 NE 2002 7 2 VNAA0203032 2 20020320 A 7321 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE DIRTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 459PS 3070 DURING TAKEOFF THE FLIGHT CREW RECEIVED A LEFT ENGINE ELECTRONIC CONTROL UNIT FAIL WARNING MESSAGE. AFTER ABORTING THE TAKEOFF A LEFT GENERATOR FAIL AND RIGHT HX FAN FAIL MESSAGE ALSO ILLUMINATED. THE FLIGHT CREW NOTED A MIST IN THE CABI N WHICH DISSIPATED AS THE AIR CONDITIONING PACKS WERE SELECTED OFF. MAINTENANCE CLEANED THE LEFT ELECTRONIC CONTROL UNI T CONNECTOR AND DEFERRED PER MEL THE RIGHT HX FAN. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RELEASED FOR SERV ICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200218 20020702 00218 2002 7 2 VNAA0203034 4 20020321 A 3441 IRU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 459PS 3070 AS THE CREW ADVANCED THE POWER LEVERS, THE INERTIAL REFERENCE SYSTEM'S AUXILIARY SYSTEM FAILED AND THE CREW ABORTED TAKE OFF. THE FLIGHT THEN RETURNED TO THE GATE. MAINTENANCE ADVISED THE CREW TO TURN OFF ALL POWER AND ALLOW THE SYSTEM TO RESET. WHEN THE CREW POWERED UP THE SYSTEMS, FLIGHT 4124 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4124 THEN DEP ARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200219 20020702 00219 NM 2002 7 2 VNAA0203036 1 20020321 A 2450 2306C02Y04 PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 459PS 7 3070 AS THE AIRCRAFT WAS IN ROTATION, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL MESSAGE. THE CREW TOOK OFF AND CIRCLED THE FIELD AND LANDED. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE M ANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200220 20020702 00220 2002 7 2 VNAA0203037 4 20020322 A 3460 COMPUTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 3056 DURING TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL CAS MESSAGE AND ABORTED TAKEOFF. AFTER EXITING THE RU NWAY THE MESSAGE CLEARED AND FLIGHT 4099 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4099 THEN DEPARTED WITH NO FUR THER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200221 20020702 00221 NM 2002 7 2 VNAA0203038 1 20020324 A 2720 DAMPENER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RUDDER FAILED A VNAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 429JS 3043 AFTER DEPARTING, THE CREW REPORTED LOSING RUDDER CONTROL DURING CLIMBOUT. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOO K AND REPORTED TO DISPATCH FLIGHT 4084 WAS DIVERTING TO CAK DUE TO THIS PROBLEM. CAPTAIN REPORTED NO RUDDER CONTROL AND SLOWED TO 155 KNOTS TO RELEASE RUDDER LIMITER. THE RUDDER LIMITER SHOW UNLIMITED AND THE CREW HAD NO RESPONSE FROM THE RUDDER PEDALS. CREW CLIMBED TO 14,000 FEET, THE RUDDER PEDALS BEGAN WORKING ON DESCENT INTO CAK. THE AIRCRAFT LANDED SAFELY WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPLACED THE RUDDER DAMPENER IN ACCORDANCE WITH DORNIER MAIN TENANCE MANUAL 27-00-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200222 20020702 00222 NM 2002 7 2 VNAA0203039 1 20020325 A 2131 22260A030201 CONTROLLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN PRESSURE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 463PS 7982 3087 JUST NORTH OF RDU, THE CREW STARTED HAVING PROBLEMS WITH THE PRESSURIZATION. THE CREW CALLED DISPATCH AND TOGETHER ELEC TED TO DIVERT TO RDU. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED THE PRESSURE CONTROL UNI T IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEAS ED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200223 20020702 00223 NM 2002 7 2 VNAA0203041 1 20020325 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 440JS 3058 DURING THE TAKEOFF ROLL, THE CREW RECEIVED A PROXI SYSTEM CAS MESSAGE AND ABORTED TAKEOFF. THE CREW CALLED DISPATCH AND STATED THE MESSAGE HAD CLEARED, FLIGHT 4072 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4072 THEN DEPARTED WI TH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200224 20020702 00224 2002 7 2 VNAA0203045 4 20020329 A 3418 STALL WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 461PS 3075 AFTER TAKING THE RUNWAY THE FLIGHT RECEIVED A PUSHER FAIL WARNING MESSAGE ON THE EICAS DISPLAY. THE FLIGHT CREW EXITED THE RUNWAY AND RETURNED TO THE GATE. MAINTENANCE RESET THE STALL PUSHER SYSTEM IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-30-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200225 20020702 00225 NM 2002 7 2 VNAA0204001 1 20020405 A 3260 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 440JS 3058 WHILE HOLDING FOR TAKEOFF THE FLIGHT CREW RECEIVED A BLUE WEIGHT ON WHEELS EICAS MESSAGE. THE FLIGHT CREW EXITED THE RU NWAY AND CYCLED AIRCRAFT POWER WHICH RESULTED IN THE WARNING MESSAGE TO CLEAR. THE FLIGHT CREW THEN RETOOK THE RUNWAY A ND A SUCCESSFUL TAKEOFF WAS MADE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200226 20020702 00226 NM 2002 7 2 VNAA0204002 1 20020409 A 2430 1030200 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ELECTRICAL SYS FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 472PS 2374 3008 DURING FLIGHT 4053 PIT-YYZ THE LEFT DC GENERATOR FAILED. THE FLIGHT CREW PERFORMED THE PROCEDURES REQUIRED PER THE QUIC K REFERENCE HANDBOOK AND THE FAILED GENERATOR WOULD NOT RESET. DUE TO THE WEATHER CONDITIONS THE FLIGHT CREW RETURNED T O PIT. A NORMAL LANDING WAS PERFORMED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE HALL EFFECT SENSOR FOR THE LEFT DC GENERATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-30-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200227 20020702 00227 NM 2002 7 2 VNAA0204003 1 20020410 A 2131 CONTROLLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN PRESSURE MALFUNCTIONED A VNAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 07 459PS 3070 FORTY-FIVE MINUTES OUT OF DCA, THE CREW RECEIVED A CABIN ALTITUDE PRESSURE WARNING INDICATION. THE PRESSURIZATION WAS U NCONTROLLABLE. THE CREW DECLARED AN EMERGENCY, FOLLOWED THE QUICK REFERENCE HANDBOOK, AND DESCENDED TO 10,000 FEET. TH E CREW SWITCHED TO MANUAL MODE AND CONTINUED ON TO DCA WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND DEFERRED TH E AUTO MODE PRESSURIZATION. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200228 20020702 00228 NM 2002 7 2 VNAA0204004 1 20020411 A 3231 MECHANISM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG DOOR STUCK A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 442JS 3060 DURING TAKEOFF THE CREW HEARD AIR RUSHING. THE CREW DETERMINED THAT THE NOSE GEAR DOOR REMAINED OPEN AFTER THE GEAR WAS SELECTED UP. THE FLIGHT RETURNED TO PHL AND MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOOR LOCKING MECHANISM STUCK . MAINTENANCE FREED THE LOCKING MECHANISM THE LUBRICATED IT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OP ERATIONAL CHECKS WERE PERFORMED THEN THE AIRCRAFT WAS FERRIED TO DAY FOR AN OVER WEIGHT INSPECTION. MAINTENANCE PERFORM ED AN OVER WEIGHT INSPECTION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. NO DEFECTS WERE FOUND AND THE AIRC RAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200229 20020702 00229 2002 7 2 VNAA0204005 4 20020412 A 3460 FMC DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 3056 DURING TAKEOFF, THE HEADING MODE OF THE FLIGHT MANAGEMENT SYSTEM FAILED AND THE CREW ABORTED TAKEOFF. THE CREW CALLED M AINTENANCE CONTROL AND RESET THE SYSTEM. FLIGHT 4032 ATTEMPTED A SECOND TAKEOFF AND DEPARTED WITHOUT ANY OTHER INCIDENT S. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200230 20020702 00230 NM 2002 7 2 VNAA0204006 1 20020412 A 3060 LEAD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PROPELLER DAMAGED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 422JS 3018 AFTER TAKEOFF, THE RIGHT HAND PROPELLER HEAT FAILED AND FLIGHT 4147 RETURNED TO BTV. MAINTENANCE INSPECTED AND REPAIR T HE DE-ICE LEAD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRA FT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200231 20020702 00231 NM 2002 7 2 VNAA0204009 1 20020413 A 2432 31879001 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 462PS 58 3084 DURING CLIMB, THE CREW RECEIVED A NUMBER 1 BATTERY OVERHEAT CAS MESSAGE AND RETURNED TO THE FIELD. MAINTENANCE INSPECTE D AND REPLACED THE MAIN BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORM ED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200232 20020702 00232 NM 2002 7 2 VNAA0204011 1 20020416 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 457PS 12857 286 3048 THE CREW REPORTED THAT THE EMERGENCY LIGHTING IN ROWS 4 AND 5 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 5LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS W ERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200233 20020702 00233 NM 2002 7 2 VNAA0204012 1 20020416 A 2910 001A291A4104000 HYDRAULIC LINE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE HYD SYSTEM LEAKING A VNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 07 471PS 3007 IMMEDIATELY AFTER LEVEL OFF AT 10,000 FT, RECEIVED A HYD PRIORITY VALVE FAIL AND MAIN HYD QUANTITY LOW CAS MESSAGES. TH E CREW FOLLOWED THE QRH AND PLANNED A LANDING AT PHL. THEN RECEIVED A STANDBY HYD SYSTEM FAIL AND A MAIN HYD QUANTITY F AIL CAS MESSAGES. THE QRH INSTRUCTED THE CREW TO LAND AT THE NEAREST AIRPORT. THE CREW DECLARED AN EMERGENCY, HAND PUM PED THE GEAR DOWN, AND LANDED AT ABE WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND FOUND THE AC HYD MOTOR PRESSU RE LINE HAD DEVELOPED A HOLE. MAINTENANCE REPLACED THE PRESSURE LINE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-0 0-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200234 20020702 00234 NM 2002 7 2 VNAA0204013 1 20020417 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 472PS 15691 108 3008 THE CREW REPORTED THAT THE EMERGENCY PATH LIGHTING AT ROWS 1 TO 3 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLA CED THE EMERGENCY BATTERY AT THE 4LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECK S WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200235 20020702 00235 NM 2002 7 2 SWAA021429 1 20020628 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 740SW 29276 DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002070200236 20020702 00236 NM 2002 7 2 SWAA021432 1 20020628 A 3350 07912 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 EEPLS LENS MISSING IN FWD CABIN. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002070200237 20020702 00237 NM 2002 7 2 SWAA021434 1 20020629 A 5753 6546435236 FLAP BOEING 737 7372T4 1384492 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING WALK AROUND INSPECTION, FOUND RT OTBD AFT T/E FLAP DELAMINATED ON BOTH UPPER AND LOWER SURFACE. REMOVED AND REPL ACED RT OTBD AFT T/E FLAP PER MM. 2 L 7 2 4F A16WE 2002070200238 20020702 00238 NM 2002 7 2 SWAA021435 1 20020627 A 5510 65C25727 SKIN BOEING 737 7373H4 1384600 NM RT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED C4 CHECK, FOUND RT HORIZ STAB LOWER SKIN CRACKED AT THE AFT SPAR. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002070200239 20020702 00239 NM 2002 7 2 SWAA021436 1 20020628 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 FUSELAGE SKIN CRACKED BETWEEN BS 727 AND 727D, BELOW STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002070200240 20020702 00240 NM 2002 7 2 SWAA021410 1 20020625 A 3350 311500 LENS BOEING 737 7373K2 13844BA NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT LENS MISSING AT ROW NR 12DEF. INSTALLED LE NS PER MM. 2 L 7 2 4F RT A16WE 2002070200241 20020702 00241 NM 2002 7 2 SWAA021412 1 20020624 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002070200242 20020702 00242 NM 2002 7 2 SWAA021413 1 20020626 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT LT BS 352, WL 243. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2002070200243 20020702 00243 NM 2002 7 2 SWAA021414 1 20020625 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT RT STA 502, WL 236. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002070200244 20020702 00244 NM 2002 7 2 SWAA021407 1 20020625 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500D PLUS 16, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002072400118 20020724 00118 NM 2002 7 24 2002UALA01070 1 20020623 A 2410 106106611 CSD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 DAMAGED A UALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 WP 29 302UA 23643 AFTER TAKEOFF, ONE GENERATOR BECAME INOPERATIVE. RETURNED TO FIELD WHEN UNABLE TO START APU. METAL PARTICLES FOUND IN MAG PLUG BOSS. BOSS WAS BROKEN WITH TWO PIECES OF BRASS. ONE WEDGED IN CHECK VALVE OF BOSS. REPLACED CSD, OIL COOLER, AND CHANGED NR 1 GENERATOR. ACCOMPLISHED APU FADEC BITE TEST. FAULT HISTORY SHOWS NO FAULTS FOR PREVIOUS 7 STARTS. S TARTED APU SEVERAL TIMES, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002070200245 20020702 00245 NM 2002 7 2 2002UALA01073 1 20020623 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 EXTERNAL FUSELAGE HAS SEVERAL DENTS AT LEFT HAND SIDE STATION 600 TO 620 STRINGER 15L TO 17L. SUPPLEMENTAL DATA UPDATE M AJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER TRIPLER ON SKIN STATION 600 TO 640 STRINGER 15L TO 18L. 2 L 7 2 4F 4 F RT A2NM E17NE 2002070200246 20020702 00246 WP 2002 7 2 IXXA0200038S 1 20020421 A 5200 DOOR DOUG DC8 DC871F 302199D WP L/H PASSENGER CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 830BX 73236 2985 45973 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DISCOVERED ON THE LEFT HAND PASSENGER DOOR CUT OUT LOWER CORNER. REPAIR ACCOMPLISHED DAMAGED AREA CUT OUT, FABRICATION AND INSTALLATION OF FILLER AND REPAIR DOUBLER IN ACCORDANCE WITH THE DOUG LAS STRUCTURAL REPAIR MANUAL AND DRAWING SR08530021. 2 L 7 4 4F RT 4A25 2002070200247 20020702 00247 WP 2002 7 2 IXXA0200039S 1 20020423 A 5240 DOOR DOUG DC8 DC871F 302199D WP AFT SERVICE MISDRILLED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 830BX 73236 2985 45973 DURING ROUTINE C-CHECK INSPECTION, MISDRILLED HOLES WERE DETECTED IN THE RIGHT HAND AFT SERVICE DOOR JAMB LOWER EDGE EXT ERNAL SKIN FROM FUSELAGE STATION 1636 TO STATION 1648. REPAIR ACCOMPLISHED REMOVAL OF DEFECTIVE DOUBLER, FABRICATION AN D INSTALLATION OF NEW REPAIR DOUBLER AND TRIPLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND BOEINGS FAX #TI N-MIA-02-003F. 2 L 7 4 4F RT 4A25 2002070200248 20020702 00248 NM 2002 7 2 VNAA0204017 1 20020419 A 2425 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 459PS 3070 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKEOFF. AFTER LEAVING THE RUNWAY, THE CREW RESET THE GENERATOR AND ATTEMPTED ANOTHER TAKEOFF. FLIGHT 4018 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200249 20020702 00249 NM 2002 7 2 VNAA0204020 1 20020423 A 3250 2318000002 CONTROL BOX DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 430JS 9919 3044 DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE AIRCRAFT WAS THEN FER RIED TO PIT. MAINTENANCE INSPECTED AND SWAPPED THE NOSE WHEEL STEERING CONTROL BOX WITH N457PS IN ACCORDANCE WITH DORNI ER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200250 20020702 00250 2002 7 2 VNAA0204022 4 20020425 A 3418 STALL WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 433JS 3047 DURING TAKEOFF, THE CREW RECEIVED A STICK SHAKER FAIL AND ABORTED TAKEOFF. THE WINDS WERE GUSTING TO 18 KNOTS. AS THE AIRCRAFT EXITED THE RUNWAY, THE MESSAGE CLEARED BY ITSELF. THE CREW CALLED MAINTENANCE CONTROL WHO ADVISED THE CREW TO ATTEMPT ANOTHER TAKEOFF. FLIGHT 4028 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200251 20020702 00251 NM 2002 7 2 VNAA0204023 1 20020425 A 3060 B6444 LEAD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PROPELLER BROKEN A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 442JS 3060 WHILE PASSING THROUGH 19,000 FEET, THE CREW RECEIVED A RIGHT HAND PROP HEAT FAIL MESSAGE. THE CREW RESET THE SYSTEM BUT IT FAILED AGAIN. THE CREW WAS ADVISED THAT THE WEATHER WAS NOT ACCEPTABLE TO DEFER THE PROP HEAT AND THE CREW RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THREE BROKEN PROP LEADS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-00 -00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. FLIGHT 4032 WAS TRANSFERRED TO ANOTH ER AIRCRAFT TO FACILITATE MAINTENANCE AND FLIGHT 4032 CONTINUED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200252 20020702 00252 2002 7 2 VNAA0205001 4 20020502 A 3418 STALL WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 433JS 3047 DURING TAKEOFF, THE CREW RECEIVED A PUSHER, SHAKER CAS MESSAGE AND ABORTED TAKEOFF. WINDS WERE GUSTING TO 40 KNOTS. AS THE AIRCRAFT EXITED THE RUNWAY, THE MESSAGE CLEARED. FLIGHT 4083 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND THEN DEPA RTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200253 20020702 00253 NM 2002 7 2 VNAA0205003 1 20020503 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 438JS 15719 145 3056 THE AIRCRAFT RETURNED TO THE GATE AFTER DISCOVERING THAT THE EMERGENCY LIGHTING AT ROWS 2, 3, AND 4 WERE NOT ILLUMINATIN G. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN THE 4LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200254 20020702 00254 NM 2002 7 2 VNAA0205004 1 20020503 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 472PS 16607 3008 THE CREW REPORTED THAT THE FLOOR EMERGENCY LIGHTING STRIP AT ROWS 2 TO 4 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AN D REPLACED THE EMERGENCY BATTERY AT THE 5LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONA L CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200255 20020702 00255 NM 2002 7 2 VNAA0205005 1 20020505 A 5270 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE DOOR DIRTY A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 429JS 3043 EN ROUTE FROM DCA TO BTV, THE CREW RECEIVED AN OPEN CABIN DOOR LIGHT. FLIGHT 4149 THEN DIVERTED TO PHL. WHILE ON APPRO ACH THE LIGHT CLEARED ITSELF. MAINTENANCE INSPECTED AND CLEANED THE DEBRIS THAT WAS FOUND ON THE SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT THEN PROCEEDED ON TO BTV WI TH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200256 20020702 00256 NM 2002 7 2 VNAA0205006 1 20020513 A 2930 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE HYD SYSTEM CONTAMINATED A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 431JS 3028 DURING CLIMBOUT, THE CREW RECEIVED A MAIN HYD PUMP FAIL THEN A STANDBY SYSTEM FAIL CAS MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND SHUT DOWN BOTH THE MAIN AND STANDBY SYSTEMS. THE CREW CONTACTED DISPATCH AND A EMERGENCY LANDING WAS MADE AT PIT. THE LANDING WAS UNEVENTFUL. THE CREW BELIEVED THE PROBLEM WAS ONLY AN INDICATION PROBLEM. MX INSPECTED AND FOUND THE INSULATION AROUND THE 1 VPA CANNON PLUG TO BE SATURATED WITH WATER. MX THEN CLEANED AND DRIED THE CANNON PLUG IAW DORNIER MM 29-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE ACFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200257 20020702 00257 NM 2002 7 2 VNAA0205007 1 20020514 A 5270 869701 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PAX DOOR FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 429JS 3043 THE CREW RECEIVED A MAIN CABIN DOOR LIGHT AND A SQUEAL COMING FROM THE DOOR. THE CREW FOLLOWED THE QUICK REFERENCE HAND BOOK AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE OVER CENTER SWITCH ON THE MAIN CABIN DOOR IN ACCORDANC E WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE . 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200258 20020702 00258 NM 2002 7 2 VNAA0205011 1 20020518 A 3350 501122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 422JS 17797 1047 3018 THE CREW REPORTED THAT THE AFT EMERGENCY POWER SUPPLY WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE AFT EMERGE NCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRC RAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200259 20020702 00259 NM 2002 7 2 VNAA0205012 1 20020519 A 5210 ROD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PAX DOOR DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 472PS 3008 APPROXIMATELY 50 KILOMETERS SOUTH WEST OF CVG, THE CREW RECEIVED A MAIN CABIN DOOR LIGHT INDICATION. THE CREW CALLED MA INTENANCE CONTROL AND WERE INSTRUCTED TO DIVERT TO DAY. MAINTENANCE INSPECTED AND REPLACED THE DOOR ROD IN ACCORDANCE W ITH SI 328-52-077. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200260 20020702 00260 NM 2002 7 2 COOSDR020165 1 20020601 A 5310 SHEAR TIE BOEING 727 7272Q6 138407V NM FUSELAGE CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 AFT CARGO COMP. BS 950A SHEAR TIE CORRODED BETWEEN STR 28R AND STR 29R. 2 L 7 3 4F RT A3WE 2002070200261 20020702 00261 NM 2002 7 2 COOSDR020166 1 20020601 A 5755 6517348108A SPOILER BOEING 727 7272Q6 138407V NM LT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 LEFT WING SPOILER NR 6 UPPER AND LOWER SKIN, DELAMINATED AND HONEYCOMB CORE CORRODED. 2 L 7 3 4F RT A3WE 2002070200262 20020702 00262 NM 2002 7 2 COOSDR020167 1 20020601 A 5751 652176646 AILERON BOEING 727 7272Q6 138407V NM RT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 RIGHT WING OUTBOARD AILERON TRAILING EDGE UPPER AND LOWER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED. 2 L 7 3 4F RT A3WE 2002070200263 20020702 00263 NM 2002 7 2 COOSDR020168 1 20020601 A 5730 6521656630 PANEL BOEING 727 7272Q6 138407V NM RT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 RIGHT WING TRAILING EDGE LOWER FIX PANEL OUTER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED. 2 L 7 3 4F RT A3WE 2002070200264 20020702 00264 NM 2002 7 2 COOSDR020169 1 20020601 A 5751 652176645 AILERON BOEING 727 7272Q6 138407V NM LT WING DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 LEFT WING OUTBOARD AILERON TRAILING EDGE UPPER AND LOWER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED. 2 L 7 3 4F RT A3WE 2002070200265 20020702 00265 NM 2002 7 2 COOSDR020170 1 20020601 A 5755 651734757 SKIN BOEING 727 7272Q6 138407V NM SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 RIGHT WING SPOILER NR 14 UPPER AND LOWER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED. 2 L 7 3 4F RT A3WE 2002070200266 20020702 00266 NM 2002 7 2 COOSDR020171 1 20020601 A 5755 651734781A SKIN BOEING 727 7272Q6 138407V NM SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 LEFT WING SPOILER NR 3 UPPER SKIN DELAMINATED AND HONEYCOMB CORE SECTION CORRODED. 2 L 7 3 4F RT A3WE 2002070200267 20020702 00267 NM 2002 7 2 COOSDR020172 1 20020601 A 5752 652172641K SKIN BOEING 727 7272Q6 138407V NM AILERON TAB DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 LEFT WING OUTBOARD AILERON TAB UPPER, LOWER SKIN DELAMINATED AND HONEYCOMB CORE SECTION CORRODED. 2 L 7 3 4F RT A3WE 2002070200268 20020702 00268 NM 2002 7 2 COOSDR02133 1 20020601 A 5230 6518625100 DOOR FRAME BOEING 727 72723 1384004 NM CARGO DOOR CRACKED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1910 19385 AFT CARGO COMPARTMENT DOOR, FRAME-FORWARD TOP, CRACKED AT THE HINGE AREA. 2 L 7 3 4F A3WE 2002070200269 20020702 00269 NM 2002 7 2 COOSDR02136 1 20020601 A 5311 65198621 FRAME BOEING 727 72723 1384004 NM FUSELAGE CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SW 23 1910 19385 NOSE WHEEL WELL, TORQUE BOX, LEFT MID CHORD CORRODED. 2 L 7 3 4F A3WE 2002070200270 20020702 00270 NM 2002 7 2 VNAA0205013 1 20020519 A 2840 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUEL SYSTEM DIRTY A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 438JS 3056 DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND FUEL QUANTITY FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTE D AND CLEANED THE COAX CONNECTORS THEN PERFORMED A HIGH SPEED TAXI WITH THE CREW, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00, NO DEFECTS WERE NOTED AT THIS TIME. AFTER PERFORMING THESE OPERATIONAL CHECKS THE AIRCRAFT WAS RELEAS ED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200271 20020702 00271 NM 2002 7 2 VNAA0205015 1 20020520 A 2810 40006MODA PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT WING FAULTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 13256 951 3056 DURING TAKEOFF, THE CREW RECEIVED A FUEL QUANTITY FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLA CED THE REFUELING PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND T HE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200272 20020702 00272 NM 2002 7 2 VNAA0205017 1 20020527 A 3397 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN LOOSE A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 457PS 3048 THE CREW REPORTED THAT THE EMERGENCY LIGHTING STRIP AT ROWS 4, 5 AND 6 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND SECURED THE WIRING CONNECTION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200273 20020702 00273 2002 7 2 VNAA0205018 4 20020529 A 3425 FLIGHT DIR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 442JS 3060 DURING TAKEOFF, THE FLIGHT DIRECTOR FAILED AND THE CREW ABORTED TAKEOFF. THE CREW EXITED THE RUNWAY AND THE MESSAGE CLE ARED. FLIGHT 4124 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200274 20020702 00274 2002 7 2 VNAA0205019 4 20020529 A 3425 FLIGHT DIR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 442JS 3060 DURING TAKEOFF, THE FLIGHT DIRECTOR FAILED AND THE CREW ABORTED TAKEOFF. FLIGHT 4124 RETURNED TO THE GATE AND MAINTENAN CE DEFERRED THE FLIGHT DIRECTOR, 22-5 CODE C. FLIGHT 4124 THEN CONTINUED TO TRI WITH A SLIGHT DELAY. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200275 20020702 00275 NM 2002 7 2 VNAA0206001 1 20020604 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 472PS 14759 142 3008 THE CREW REPORTED THAT THE EMERGENCY LIGHTING IN FRONT OF SEAT 3D AND 3F WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIO NAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070200276 20020702 00276 NM 2002 7 2 ZW0A0205801 1 20020530 A 3397 WIRE BOEING 767 76733AER 1385230 NM CABIN BROKEN A ZW0A K NONE L NO TEST UK UNKNOWN 1 CE 13 637TW 25403 EGRESS LIGHT SYS WMD 33-51-17 INOP ROW 25H THROUGH 31H CAUSED BY BROKEN WIRE. REPAIRED SEAT TO SEAT CABLE. OPERATIONAL C HECK NORMAL. 2 L 7 2 4F RT A1NM 2002070200277 20020702 00277 2002 7 2 P5CA0200685 4 20020630 A 2210 NONE WIRE BOEING 747 747249F 1384849 NM "A" AUTOPILOT BROKEN A P5CA K NONE O OTHER UK UNKNOWN 1 WP 23 806FT 21827 "A" AUTOPILOT WILL NOT ACCEPT STEERING COMMANDS IN HDG OR INS MODES. ALSO INOP IN MANUAL. TRANSFERRED TO DEFERRED MX ITE M ID #036042 CTR #29299 IAW MEL 02-22-2-1 IN CONSULT W/ MTC & PLACARD INSTALLED. JFK MX FOUND BROKEN WIRE AT PINS 9 & 10 ON CONNECTOR DB193 "A" A/P CCA. REPINNED & SECURED WIRE AS PER MM 20-60-07. PERFORMED OPS CK PER MM 22-10-00. "A" A/P C HKD GOOD - DMI CLEARED. 2 L 7 4 4F A20WE 2002070300001 20020703 00001 WP 2002 7 3 ZW0A0205301 1 20020517 A 5240 DOOR FRAME DOUG DC9 DC983 3022083 WP R1 DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9305N 49395 DURING CHECK-C MAINT THE RT FWD GALLEY SERVICE DOOR HAD A CRACKED DOUBLER LOWER HINGE ARM. REPLACED WITH NEW FRAME PART PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2002070300002 20020703 00002 WP 2002 7 3 ZW0A0205302 1 20020517 A 5313 STRINGER DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9305N 49395 DURING CHECK-C MAINT STRINGER 3 LT WAS CRACKED AT STA 160, ABOVE ELECT PANEL. REPAIRED LONGERON 3 PER SRM 53-02, FIG 18 . 2 L 7 2 4F RT A6WE 2002070300003 20020703 00003 WP 2002 7 3 ZW0A0205303 1 20020522 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9305N 49395 DURING CHECK-C MAINT FOUND CORROSION IN LATERAL FLOOR BEAM AT STA 180, FROM RBL 8 TO RBL 43. FABRICATED AND INSTALLED F LOOR SUPPORT PER SRM 51-01, PAGE 1 ITEM C. 2 L 7 2 4F RT A6WE 2002070300004 20020703 00004 NM 2002 7 3 ZW0A0205502 1 20020528 A 3350 LIGHT BOEING 767 7673Y0 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 639TW 26208 DURING GROUND MAINTENANCE, EGRESS LIGHT AT LEFT FWD BULKHEAD INOP. REPLACED LENS AND LIGHT ASSEMBLY. OPS EGRESS LIGHT CH K OK. 2 L 7 2 4F RT A1NM 2002070300005 20020703 00005 2002 7 3 ZW0A0205603 4 20020529 A 2210 4034239901 ACCELEROMETER DOUG DC9 DC982 3022082 WP AUTOPILOT SYS MALFUNCTIONED A ZW0A O OTHER F FLT CONT AFFECTED CL CLIMB 1 CE 13 929TW 48014 AFTER TAKEOFF YAW DAMPER OFF LT-YAW KICKS LT-RT UNSKD LANDING AFTER UNCOMMANDED RUDDER INPUT. REMOVED AND REPLACED ACCE LEROMETER PER MM 22-19-01 PG 201. ACCOMPLISHED RTS PER MM 22-01-05 PG 201. 2 L 7 2 4F A6WE 2002070300006 20020703 00006 NM 2002 7 3 ZW0A02057 1 20020601 A 3350 CONNECTOR BOEING 767 7673Q8 1385142 NM CABIN LOOSE A ZW0A K NONE L NO TEST NR NOT REPORTED 1 CE 13 635TW 28207 FIRST FOUR EGRESS LIGHTS ON LEFT SIDE INOP. REPAIRED AND SECURED LOOSE CONNECTION AT LT ASSY. OPS CK EGRESS LTS OK. 2 L 7 2 4F RT A1NM 2002070300007 20020703 00007 WP 2002 7 3 ZW0A0205902 1 20020604 A 5320 TIE CLIP DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9305N 49395 DURING CHECK-C CRACKED TIE CLIP AT STA 1437 VERT BULKHEAD TO LONG 3R. REPLACED TIE CLIP PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2002070300008 20020703 00008 WP 2002 7 3 ZW0A0205903 1 20020603 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9622A 53593 DURING CHECK-C AFT CARGO, AFT CARGO COMPT FLOOR TRACK LT SIDE FROM STA 1211 TO STA 1322 HAS CORROSION IN NUT PLATE LUG H OLES. EVALUATED CORROSION WHICH REQUIRED PART REPLACEMENT, REMOVED OLD PART AND INSTALLED NEW PART PER SRM 51-10-4 AND S PM 6-70-01. 2 L 7 2 4F RT A6WE 2002070300009 20020703 00009 WP 2002 7 3 ZW0A0206002 1 20020607 A 3350 SIGN DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 967TW 53617 THE LOWER OVERWING EXIT SIGN WAS INOPERATIVE. REPLACED THE SIGN. 2 L 7 2 4F RT A6WE 2002070300010 20020703 00010 WP 2002 7 3 ZW0A0206003 1 20020605 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9305N 49395 DURING CHECK-C MAINT THE FLOOR BEAM CAP WAS GROUND BEYOND LIMITS AT STA 1322, LBL 34. REPAIRED FLOOR BEAM CAP PER SRM 5 3-05, FIG 20A. 2 L 7 2 4F RT A6WE 2002070300011 20020703 00011 WP 2002 7 3 ZW0A0206101 1 20020612 A 3350 60030451 BATTERY DOUG DC9 DC983 3022083 WP CABIN OUT OF POSITION A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 967TW 53617 THE EGRESS LIGHTS WERE INOPERATIVE AT ROW 14 THROUGH 19. REPOSITIONED THE BATTERY PACK BATTERIES. 2 L 7 2 4F RT A6WE 2002070300012 20020703 00012 WP 2002 7 3 ZW0A0206201 1 20020611 A 5320 FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9305N 49395 DURING CHECK-C MAINT THE FORMER FOOT WAS CRACKED AT STA 1361 BETWEEN LONGERON 23L AND 24L. FABRICATED AND INSTALLED NEW FORMER FOOT SECTION PER SPM 6-70-01, PAGE 2 AND 3, ITEM 4. FABRICATED AND INSTALLED PER SRM 51-30-02 AND 51-30-5. 2 L 7 2 4F RT A6WE 2002070300013 20020703 00013 NM 2002 7 3 ZW0A0206402 1 20020616 A 2150 20495055 ACM DOUG MD80 MD83 3023681 NM A/C BAY LEAKING A ZW0A K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 13 9413T 53188 A BURNING ODOR WAS IN CABIN AND COCKPIT ON DESCENT. NO SMOKE. FOUND RT ACM OIL PUDDLING IN ACM OUTLET. THE NEXT STATI ON REPLACED THE RT ACM. 2 L 7 2 4F RT 2002070300014 20020703 00014 WP 2002 7 3 ZW0A0206701 1 20020621 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 908TW 49169 LONGERON 24L WAS DAMAGED AT STA 325. REPAIRED LONGERON 24L PER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 2002070300015 20020703 00015 EA 2002 7 3 2002F00640 1 20020405 A 2612 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE LOOSE A MASA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 77278 7278 FLT 6097 - RETURNED TO GATE, DUE TO LEFT JET PIPE OVERHEAT FAIL ON LOOP A. MAINTENANCE WAS CALLED. MAINTENANCE SECURED CONNECTION. OP CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002070300016 20020703 00016 EA 2002 7 3 2002F00641 1 20020405 A 3150 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYS DIRTY A MASA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 17217 7217 FLT 6442 - RETURNED TO GATE, WITH THE RIGHT ANTI-ICE DUCT WARNING MESSAGE ON THE GROUND. MAINTENANCE CLEANED THE CANNON PLUG. OP CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002070300017 20020703 00017 EA 2002 7 3 2002F00642 1 20020404 A 5210 PUSHROD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DEFECTIVE A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 37178 7178 FLT 6418 - PHX-COS - RETURNED TO PHX DUE TO AIRCRAFT WOULD NOT PRESSURIZE IN FLIGHT. AFTER AN UNEVENTFUL LANDING MAINTE NANCE WAS CALLED. MAINTENANCE FOUND A BAD PUSH ROD ASSY IN MAIN CABIN DOOR. MAINTENANCE REPLACED THE PUSH ROD. OP CHE CKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002070300018 20020703 00018 WP 2002 7 3 GTIA020315 1 20020324 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLIGHT AND FORWARD PASSENGER COMPARTMENT FLOOR PANEL LEFT STATION 148.5 TO STATION 167.5 HAS CRACKED/MISSING INSERT. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2002070300019 20020703 00019 WP 2002 7 3 GTIA020316 1 20020322 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR PANEL AFT CABIN FRONT AFT ENTRY DOOR SEVERAL CRACKED, BLUE WATER STAINS, ELONGATED HOLES. FABRICATED NEW PANEL. (M) 2 L 7 2 4F A6WE 2002070300020 20020703 00020 WP 2002 7 3 GTIA020317 1 20020322 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR PANEL INBOARD LEFT STATION 886-927 CRACKED/DAMAGED. FABRICATED REPAIR FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002070300021 20020703 00021 WP 2002 7 3 GTIA020318 1 20020322 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR PANEL RIGHT INBOARD STATION 927-1002 DELAMINATED/DAMAGE. FABRICATED REPAIR FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002070300022 20020703 00022 WP 2002 7 3 GTIA020319 1 20020322 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR PANEL INBOARD RIGHT STATION 796-826 CRACKED/DAMAGE. FORM NEW PANEL. (M) 2 L 7 2 4F A6WE 2002070300023 20020703 00023 SO 2002 7 3 SIMA200212112 1 20020413 A 5320 14522461011 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS A LEVEL 2 FINDING, RIGHT BEAM FORWARD DIAMOND PLATE CORRODED. INSTALLED NEW BEAM IAW EMB145 SRM 51-40-02, 51 -20-03, 51-40-06. (M) 2 L 7 2 4F RT T00011AT 2002070300024 20020703 00024 SO 2002 7 3 SIMA200212113 1 20020413 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING, SERVICE DOOR FORWARD SILL CORRODED. INSTALLED SERVICEABLE FORWARD SILL IAW EMB 145 SRM 51-40-02, 51-40-06, 51-20-03. (M) 2 L 7 2 4F RT T00011AT 2002070300025 20020703 00025 SO 2002 7 3 SIMA200212114 1 20020413 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 THIS IS A LEVEL 2 FINDING, SERVICE DOOR AFT SILL CORRODED. INSTALLED NEW AFT SILL IAW EMB145 SRM 51-40-02, 51-40-04, 51 -40-06. (M) 2 L 7 2 4F RT T00011AT 2002070300026 20020703 00026 SO 2002 7 3 SIMA200212115 1 20020413 A 5320 14522461011 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING, AFT BEAM DIAMOND PLATE CORRODED. INSTALLED SERVICEABLE AFT DIAMOND IAW EMB145 SRM 51-4 0-02, 51-40-04, 51-40-06, 51-20-01, 51-20-03. (M) 2 L 7 2 4F RT T00011AT 2002070300027 20020703 00027 SO 2002 7 3 SIMA200212116 1 20020413 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING, PREVIOUS REPAIR AT LEFT OMEGA BEAM AT FRAME 20 IS CORRODED. REPAIR DONE IAW EMB145 SRM 53-21-10, FIG 201. (M) 2 L 7 2 4F RT T00011AT 2002070300028 20020703 00028 SO 2002 7 3 SIMA200212117 1 20020413 A 5320 14522459003 SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING, PASSENGER DOOR AFT THRESHOLD SUPPORT CORRODED. INSTALLED NEW PASSENGER DOOR SUPPORT IA W EMB145 SRM 51-40-02, 51-20-01. (M) 2 L 7 2 4F RT T00011AT 2002070300029 20020703 00029 SO 2002 7 3 SIMA200212118 1 20020413 A 5320 1452245003 SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING, PASSENGER DOOR FORWARD THRESHOLD SUPPORT CORRODED. INSTALLED NEW PASSENGER DOOR FORWAR D THRESHOLD SUPPORT IAW EMB145 SRM 51-40-02, 51-20-01. (M) 2 L 7 2 4F RT T00011AT 2002070300030 20020703 00030 SO 2002 7 3 SIMA200212119 1 20020413 A 5320 14529150001 CROSSBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 THIS IS A LEVEL 2 FINDING, CROSS BEAM AT FRAME 23 CORRODED. INSTALLED NEW CROSSBEAM IAW EMB145 SRM 51-40-02, 51-20-01. (M) 2 L 7 2 4F RT T00011AT 2002070300031 20020703 00031 SO 2002 7 3 SIMA200212120 1 20020413 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING, CENTER BEAM GUSSET CORRODED. INSTALLED NEW GUSSET IAW EMB145 SRM 51-40-02, 51-40-06, 5 1-20-03. (M) 2 L 7 2 4F RT T00011AT 2002070300032 20020703 00032 SO 2002 7 3 SIMA200212121 1 20020413 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL CABIN HAS CORROSION BETWEEN FRAMES 24-30. INSTALLED NEW SILL IAW EMB145 SRM 51-40-02, 51-20-01. (M) 2 L 7 2 4F RT T00011AT 2002070300033 20020703 00033 SO 2002 7 3 SIMA200212122 1 20020413 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING, CENTER BEAM RAMP SUPPORT CORRODED. INSTALLED NEW CENTER BEAM IAW EMB145 SRM 51-40-02, 51-20-03. (M) 2 L 7 2 4F RT T00011AT 2002070300034 20020703 00034 SO 2002 7 3 SIMA200212123 1 20020413 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING, LEFT BEAM GUSSET UNDER SEAT TRACK HAS CORROSION. REPAIRED IAW EMB GST-1284/02. (M) 2 L 7 2 4F RT T00011AT 2002070300035 20020703 00035 SO 2002 7 3 SIMA200212124 1 20020413 A 5320 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING, RIGHT CABIN SILL HAS CORROSION AT FRAME 38. REPAIRED IN IAW EMB 145 GST 1246/02. (M) 2 L 7 2 4F RT T00011AT 2002070300036 20020703 00036 SO 2002 7 3 SIMA200212125 1 20020413 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 145079 ABI - THIS IS A LEVEL 2 FINDING, SERVICE DOOR CENTER SILL CORRODED. REPAIRED IAW EMB145 GST-1246/02. (M) 2 L 7 2 4F RT T00011AT 2002070300037 20020703 00037 NM 2002 7 3 VNAA0206002 1 20020604 A 2150 A/C PACK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A/C BAY MALFUNCTIONED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 429JS 3043 WHILE BEGINNING THE CLIMBOUT, THE CREW RECEIVED A PACK OVER PRESSURE AND PACK FAIL MESSAGE FOR BOTH PACKS. THE CAPTAIN THEN DECIDED TO EXECUTE A RETURN TO THE FIELD. OUTSTATION MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS IN ACC ORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00 AND FOUND THAT BOTH PACKS WORKED NORMALLY. AFTER THESE POSITIVE OPERAT IONAL CHECKS, THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070300038 20020703 00038 2002 7 3 VNAA0206003 4 20020604 A 3460 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 442JS 3060 DURING THE TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE CONTROL UNIT LAT MODE FAIL CAS MESSAGE AND ABORTED TAKEOFF. AFT ER EXITING THE RUNWAY THE MESSAGE CLEARED ITSELF AND FLIGHT WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4097 THEN D EPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070300039 20020703 00039 NM 2002 7 3 VNAA0206004 1 20020606 A 2430 1030200 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ELECTRICAL SYS FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 460PS 17001 3061 DURING CLIMBOUT, THE CREW RECEIVED A LEFT HAND DC GENERATOR FAIL CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE HALL EFFECT SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PE RFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070300040 20020703 00040 NM 2002 7 3 VNAA0206005 1 20020612 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 439JS 15070 765 3057 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROW 10 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EM ERGENCY BATTERY AT THE 7LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PER FORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070300041 20020703 00041 NE 2002 7 3 VNAA0206006 2 20020616 A 7321 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 439JS 3057 WHILE HOLDING ON THE RUNWAY FOR TAKEOFF, THE CREW RECEIVED A RIGHT HAND ENGINE CONTROL UNIT FAIL MESSAGE AND ABORTED TAK EOFF. THE SYSTEM WAS RESET AND THE MESSAGE CLEARED ITSELF. FLIGHT 4101 TAXIED BACK TO THE GATE WHERE MAINTENANCE PERFO RMED OPERATIONAL CHECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. ALL OPERATIONAL CHECKS WERE GOOD AND NO DISCREPANCIES WERE FOUND. FLIGHT 4101 WAS THEN RELEASED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4101 THEN DEPARTED WITH N O FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070300042 20020703 00042 NM 2002 7 3 DHL2002727008 1 20020702 A 3350 1060091101 LIGHT BOEING 727 727228 1384083 NM A DHLA K O NONE OTHER O OTHER UK UNKNOWN 1 SO 01 727DH 20204 1) EMERGENCY EXIT LIGHT IN COCKPIT FELL AND BROKE.2) R&R EMERGENCY EXIT LIGHT ASSY. IAW BMM CH 33-50-01, OPS CK GOOD. 2 L 7 3 4F RT A3WE 2002070300043 20020703 00043 NM 2002 7 3 VNAA0206007 1 20020616 A 3250 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 3056 DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE AND ABORTED TAKEOFF. WHEN THE POWER WAS REDUCE D THE MESSAGE CLEARED. THE CREW CALLED MAINTENANCE CONTROL WHO HAD THE CREW RUN UP THE AIRCRAFT AT TAKEOFF POWER IN ACC ORDANCE WITH DORNIER MAINTENANCE MANUAL 71-01-00 AND NO FURTHER PROBLEMS OR DISCREPANCIES WERE NOTED. FLIGHT 8640 WAS THEN RELEASED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070300044 20020703 00044 2002 7 3 VNAA0206008 4 20020617 A 3140 DAU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 461PS 3075 DURING TAKEOFF, THE CREW RECEIVED A DATA ACQUISITION UNIT CHANNEL NUMBER 2 FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CR EW RESET THE SYSTEM AND WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4111 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002070300045 20020703 00045 NM 2002 7 3 SWAA021394 1 20020622 A 3830 158000911 TOILET BOEING 737 7377H4 1384404 NM LAVATORY CLOGGED A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 29 705SW 27839 DIVERSION, BOTH LAV'S (FWD AND AFT) WOULD NOT FLUSH. UNCLOGGED AFT LAV AND REMOVED AND REPLACED FWD LAV PER MM. 2 L 7 2 4F RT A16WE 2002070300046 20020703 00046 EU 2002 7 3 2002F00643 1 20020625 A 6410 117317411 BLADE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101600A 41560 NE TAIL ROTOR CRACKED B LN3A K NONE O OTHER IN INSP/MAINT 1 EA 03 117US 1162 7175 BLADE CRACKED, SKETCH 1 G 7 2 3U 3 U H13EU E5NE 2002070300047 20020703 00047 2002 7 3 SWIA200210866 4 20020522 A 3445 80510001004 COMPUTER EMB 120 EMB120ER 3260203 SO E/E BAY MALFUNCTIONED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 563SW 801 801 120338 TCAS TESTS OK, BUT REPORTS NO TARGETS IN THE AIR. REPLACED AND INITIALIZED TCAS PROCESSOR. OPS CHECK GOOD IAW MM 34-46 -00. 2 L 7 2 4T RT A31SO 2002070300048 20020703 00048 2002 7 3 SWIA200210867 4 20020523 A 3418 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 439SW 7578 STALL FAIL MESSAGE INFLIGHT. RETURNED TO SLC. RESET MEMORY ON CH1 & CH2 IN STALL COMPUTER IAW MM 27-35-01. PERFORMED TEST OF STALL SYSTEM. OPS CHECK GOOD, NO FAULTS NOTED. 2 L 7 2 4F RT A21EA 2002070300049 20020703 00049 SO 2002 7 3 SWIA200210868 1 20020426 A 5320 BRACKET EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 LEFT BRACKET FRAME 12 CRACKED AFT OF PILOT'S DIRECT VISION WINDOW. REPLACED LEFT BRACKET FRAME 12 AFT OF PILOT'S DV WIN DOW IAW MM 53-40-02. 2 L 7 2 4T RT A31SO 2002070300050 20020703 00050 SO 2002 7 3 SWIA200210869 1 20020426 A 5320 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 RIGHT HYDRAULIC RESERVOIR SUPPORT BRACKET CRACKED. REMOVED AND REPLACED RIGHT HYDRAULIC PACK LOWER SUPPORT BRACKET IAW SRM 51-40-02 AND 51-10-02-3A. 2 L 7 2 4T RT A31SO 2002070300051 20020703 00051 SO 2002 7 3 SWIA200210871 1 20020524 A 3010 BOOT EMB 120 EMB120ER 3260203 SO RT WING DAMAGED A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 224SW 120294 FOUND RIGHT INBOARD DEICE BOOT RIPPED. REMOVED & REPLACED DEICE BOOT IAW 30-10-00.. 2 L 7 2 4T RT A31SO 2002070300052 20020703 00052 SO 2002 7 3 SWIA200210872 1 20020525 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT 3260202 SO T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 269UE 5377 2351 120194 LEFT OUTBOARD FLAP DEPLOYED APPROXIMATELY 3 DEGREES (UNCOMMANDED) WHILE FLAP HANDLE IS IN ZERO POSITION. ANALOG INDICAT OR SHOWS ZERO DEGREES. FLAP ON MAP ILLUMINATED, ASYMMETRY ON FLAP PANEL INDICATOR ILLUMINATED. REPLACED LEFT OUTBOARD FLAP ACTUATOR PER EMB 120 27-50-00. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002070300053 20020703 00053 EA 2002 7 3 SWIA200210873 1 20020526 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 435SW 7555 LEFT SIDE COCKPIT SIDE WINDOW SHATTERED AT FL350. DIVERTED TO GJT. REMOVED AND REPLACED LEFT SIDE WINDOW. OPS AND LEA K CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002070300054 20020703 00054 EA 2002 7 3 SWIA200210874 1 20020504 A 5220 601R330501 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 499SW 7398 CREW ESCAPE HATCH OUTER HANDLE SEIZED. (DISCOVERED DURING C-CHECK INSPECTION). OUTER HANDLE ASSEMBLY FREED AND FOUND T O BE SEVERELY CORRODED. OUTER HANDLE ASSEMBLY REPLACED PER AMM 52-22-02. 2 L 7 2 4F RT A21EA 2002070300055 20020703 00055 SO 2002 7 3 SWIA200210875 1 20020528 A 2730 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO ELEVATOR MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 586SW 120354 ABORTED TAKEOFF FOR TRIM FAIL WARNING. REMOVED AND REPLACED PROXIMITY SWITCH FOR ELEVATOR OUT OF TRIM WARNING. OPS CHE CK GOOD. 2 L 7 2 4T RT A31SO 2002070300056 20020703 00056 NE 2002 7 3 SWIA200210876 3 20020522 A 6140 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 563SW 120338 AUTOFEATHER WARNING ON TAKEOFF - ABORTED TAKEOFF AND RETURNED TO GATE. PERFORMED STATIC ENGINE RUN AT TAKEOFF SETTINGS, COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 6 C P11NE 2002070300057 20020703 00057 SO 2002 7 3 SWIA200210877 1 20020525 A 7712 SEDLOC2R INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 233SW 5749 5749 120307 ON TAKEOFF ROLL, PAST 80 KIAS, THE NR 2 TORQUE GAUGE INDICATION WENT TO ZERO. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED RIGHT TORQUE INDICATOR. RAN THE ENGINE TO 100 PERCENT TORQUE FOR 1 MIN. NO FAULTS FOUND. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002070300058 20020703 00058 SO 2002 7 3 SWIA200210878 1 20020528 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO RT MLG FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 188SW 120039 RIGHT MAIN LANDING LIGHT REMAINS ILLUMINATED. RETURNED TO SLC. REPLACED RIGHT MAIN LANDING GEAR B CHANNEL DOWNLOCK PRO XIMITY SENSOR IAW 32-61-01. SWUNG LANDING GEAR 4 TIMES, OPERATIONS NORMAL. 2 L 7 2 4T RT A31SO 2002070300059 20020703 00059 EA 2002 7 3 SWIA200210879 1 20020528 A 7810 TAIL CONE CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591ML 7388 AIRCRAFT'S RIGHT ENGINE JET PIPE MISSING INSPECTION COVER AND TAIL CONE HAS A 1.5 INCH CUT. REPLACED RIGHT ENGINE TAIL CONE ASSEMBLY. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002070300060 20020703 00060 SO 2002 7 3 SWIA200210880 1 20020523 A 7714 INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT FLUCTUATES A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 270YV 120270 NR 1 NP GAUGE FLUCTUATES. RETURNED TO SBA. INSTALLED SERVICEABLE NP INDICATOR. RAN ENGINE IAW 71-00-00. GROUND OPS C HECKS GOOD. 2 L 7 2 4T RT A31SO 2002070300061 20020703 00061 SO 2002 7 3 SWIA200210881 1 20020528 A 3242 21661 BRAKE ASSY EMB 120 EMB120ER 3260203 SO LT MLG MALFUNCTIONED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 226SW 120296 WHEN BRAKES ARE APPLIED EVENLY, LEFT BRAKE GRABS AND PULLS HARD TO THE LEFT. REMOVED AND REPLACED NR 1 AND NR 2 BRAKE A SSEMBLIES WITH SERVICEABLE UNITS. OPS CHECK GOOD IAW MM 32-41-05. 2 L 7 2 4T RT A31SO 2002070300062 20020703 00062 NM 2002 7 3 AWXA200200529 1 20020616 A 2560 P4010021 BATTERY BOEING 737 737375 13844BN NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 336AW 23707 PHX - EMERGENCY EQUIPMENT - DURING INSPECTION THE FORWARD EMERGENCY FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLASHLIGHT BATTERY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2002070300063 20020703 00063 2002 7 3 AWXA200200530 4 20020616 A 2565 018300511 PROXIMITY SWITCH BOEING 757 7572S7 1384962 NM R1 DOOR WORN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 903AW 23323 LAX - EMERGENCY EQUIPMENT - DURING INSPECTION THE R-1 DOOR SLIDE GIRT BAR ENGAGEMENT LIGHT WAS FOUND INOPERATIVE.MAINTEN ANCE REMOVED AND REPLACED GIRT BAR PROXIMITY SWITCHES PER MM 25-66-11. OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F RT A2NM 2002070300064 20020703 00064 NM 2002 7 3 AWXA200200531 1 20020618 A 3350 20121 POWER SUPPLY BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 PHX - EEL - DURING ROUTINE INSPECTION, L-2 DOOR OVERHEAD EMERGENCY EXIT LIGHT VERY DIM. MAINTENANCE REMOVED AND REPLACE D POWER PACK ASSEMBLY IN AFT GALLEY FOR L-2 OVERHEAD EMERGENCY EXIT LIGHT. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2002070300065 20020703 00065 NM 2002 7 3 AWXA200200532 1 20020609 A 5315 654581292 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 MCN - MAJOR REPAIR - DURING C-16 CHECK, CORROSION WAS FOUND ON FLOORBEAM UPPER FLANGE BS 328 RBL 22 TO RBL 30. MAINTENA NCE REMOVED CORRODED FLOORBEAM UPPER T-CHORD BS 328 FROM RBL 5 TO 65. MADE REPAIR SECTION AND INSTALLED IAW B 737-300 S RM 53-10-51 PGS 220-223. 2 L 7 2 4F RT A16WE 2002070300066 20020703 00066 WP 2002 7 3 CALA0200379 1 20020701 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 200-220 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND SEAT TRACK CORRODED AT STA 200-220, RBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-4 AND 53-05, FIGURE 4. 2 L 7 2 4F A6WE 2002070300067 20020703 00067 WP 2002 7 3 CALA0200384 1 20020702 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FS 1200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND LONGERON SPLICES CORRODED AT FS 1200, L20L AND L21L. REMOVED AND REPLACED LONGERON SPLICES IAW SRM 53-0 1, FIGURE 1, 51-10-4, AND 51-30-5. 2 L 7 2 4F A6WE 2002070300068 20020703 00068 WP 2002 7 3 CALA0200387 1 20020702 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 200-236 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND SEAT TRACK CORRODED AT FS 200-236, LBL 44. A NEW SEAT TRACK AND SPLICE WERE INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2002070300069 20020703 00069 WP 2002 7 3 CALA0200389 1 20020702 A 5350 LATCH DOUG DC9 DC982 3022082 WP TAILCONE OUT OF RIG A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 49635 THE TAILCONE INTERIOR RELEASE HANDLE PULL WAS EXCESSIVE. THE TAILCONE LATCH LOCKPINS WERE ADJUSTED AND OPERATION CHECKED GOOD IAW MM 53-53-00. 2 L 7 2 4F A6WE 2002070300070 20020703 00070 WP 2002 7 3 CALA0200390 1 20020703 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 665 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND MID CARGO COMPARTMENT DOOR CUTOUT AREA SKIN CORRODED ON INNER SURFACE LOWER AFT CORNER AT FS 665. REPAI RED IAW EA 9-5312-2-A0957 AND ECRA 5330-03142. 2 L 7 2 4F A6WE 2002070300072 20020703 00072 NM 2002 7 3 P5CA0200688 1 20020629 A 5730 65B149624 PANEL BOEING 747 747249F 1384849 NM RH WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 CRACK 15" LONG FOUND RH WING UPPER SKIN LE FIXED PANEL AT WS 834 TO WS 862. PANEL SHOWS 15 X 30 IN. SQ AREA DELAMINATED. LEADING EDGE FIXED PANEL AT WS 834 TO WS 862 REMOVED & NEW PANEL INSTALLED IAW SRM 51-10-01, PG 8, SECT 6, PARA A-B-C. ALSO SRM 51-30-02. 2 L 7 4 4F A20WE 2002070300073 20020703 00073 NM 2002 7 3 AWXA200200534 1 20020612 A 5315 6546811511 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 YVR - MAJOR REPAIR - DURING C-15 CHK, CORROSION WAS FOUND ON FLOOR BEAM 987 IN THE CENTER OF THE CABIN AT BL 0 HAD CORRO SION ON TOP SURFACE. FLOORBEAM REPAIRED IAW SRM 53-10-9 PAGE 7 FIG 2. 2 L 7 2 4F RT A16WE 2002070300074 20020703 00074 NM 2002 7 3 AWXA200200535 1 20020603 A 5310 654797316 CREASE BEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 YVR - MAJOR REPAIR - DURING C-15 CHECK A CRACK WAS FOUND ON THE HORIZONTAL FLANGE OF THE RT INNER CHORD FO CREASE BEAM A T BS 639, RBL 64. MAINTENANCE REMOVED AND REPLACED THE RT CREASE BEAM INNER CHORD AT BS 639, RBL 64 PRE DRAWING 65-4797 3, AND B737-200 SRM 51-10-1, PG. 8. 2 L 7 2 4F RT A16WE 2002070300075 20020703 00075 NM 2002 7 3 AWXA200200538 1 20020609 A 5320 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 MCN - MAJOR REPAIR - DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER CLIP BS 597, STR 9L. MAINTENANCE REMOVED STRI NGER CLIP AT BS 597, STR 9L AND REPLACED STRINGER CLIP PER B737 SRM 51-40-02 PAGE 3 AND 10. 2 L 7 2 4F RT A16WE 2002070300076 20020703 00076 NM 2002 7 3 AWXA200200539 1 20020609 A 5320 69353502 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 MCN - MAJOR REPAIR- DURING C-16 INSPECTION, A CRACK WAS FOUND ON STRINGER CLIP BS 460 STR 16L. MAINTENANCE REMOVED AND R EPLACED STRINGER TIE CLIP PER B 737-300 SRM 51-40-05 PAGE 1 AND 4. 2 L 7 2 4F RT A16WE 2002081200037 20020812 00037 2002 8 12 P2EA2002M045 4 20020626 A 3460 7892475041 CONTROL UNIT DOUG DC9 DC983 3022083 WP COCKPIT MALFUNCTIONED A P2EA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 131NJ 49846 DURING FLIGHT TO LGA SMOKE EMANATED FROM CENTER CONSOLE. AIRCRAFT DECLARED EMERGENCY, DESCENDED AND MADE UNSCHEDULED LA NDING IN STL WITH NO INCIDENT. FOUND PMS MODULE OVERHEATED. DEFERRED PMS SYSTEM IAW MEL 34-37-01. PMS CIRCUIT BREAKER COLLARED. REMOVED AND REPLACED PMS CONTROL UNIT IAW MM 34-63-00, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 2002070300077 20020703 00077 NM 2002 7 3 AWXA200200540 1 20020610 A 5320 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 MCN - MAJOR REPAIR - DURING C-16 INSPECTION A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 380 STR 26L. MAINTENANCE FORME D A REPLACEMENT STRINGER CLIP, INSTALLED IAW BOEING DRAWING 69-35352 AND SRM 51-40-05, 51-20-01 PG 10 AND MM 51-20-00 PA GE 1 AND SRM 51-40-02 PAGES 10 AND 11. 2 L 7 2 4F RT A16WE 2002070300078 20020703 00078 WP 2002 7 3 ABXA020014 1 20020514 A 5344 49165641 FITTING DOUG DC9 DC933F 302207A WP LEFT FWD DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 LEFT FORWARD DOOR, FORWARD HINGE FITTING WAS CRACKED IN 3 PLACES.REPLACED DOOR FITTING P/N-4916564-1 IAW DC9 SRM 51-30-1 . 2 L 7 2 4F A6WE 2002071500164 20020715 00164 WP 2002 7 15 ABXA020011 1 20020514 A 5330 591141253 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 BULGE IN FUSELAGE SKIN AND FASTENER HEADS DISHED AT FS 446, L30 AND L29L. CLEANED CORROSION ON INNER SKIN PER DC9 SRM 5 1-10-3. REPLACED DOUBLERS DUE TO CORROSION PER DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2002070300079 20020703 00079 WP 2002 7 3 ABXA020012 1 20020514 A 5330 591141247 DOUBLER DOUG DC9 DC933F 302207A WP FS 439 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 BULGE IN FUSELAGE SKIN AND FASTNER HEADS DISHED AT FS 439 L30L AND 29L.REPLACED DOUBLER P/N-5911412-47 PER DC9 SRM 51-30 -2. 2 L 7 2 4F A6WE 2002070300080 20020703 00080 NM 2002 7 3 UPS02238718 1 20020612 A 5310 INTERCOSTAL BOEING 727 72722C 138400F NM BS219-211 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI SURFACE CORROSION ON INTERCOSTAL BETWEEN BS219+BS211 LBL 24 L/H. INTERCOSTAL FABRICATED IAW SRM 51-20-1 INTERCOSTAL INSTALLED IAW SRM 53-30-2 2 L 7 3 4F A3WE 2002070300081 20020703 00081 NM 2002 7 3 UPS02238719 1 20020615 A 5310 STRINGER BOEING 727 72722C 138400F NM BS448 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI SURFACE CORROSION STRINGER 21R BS 448 APPROX SURFACE CORROSION FOUND TO BE OUTSIDE LIMITS I.A.W SRM 53-10-1. STRINGER 21 R REPAIRED I.A.W SRM 53-10-3 FIG1. 2 L 7 3 4F A3WE 2002070300082 20020703 00082 NM 2002 7 3 UPS02238723 1 20020615 A 5310 STRINGER BOEING 727 72722C 138400F NM BS460-440 S19L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI INTERGRANULAR CORROSION S19L BS 460-440, CORROSION FOUND TO BE OUTSIDE LIMITS OF SRM 51-10-1. S TRINGER REPAIR ED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 2002070300083 20020703 00083 NM 2002 7 3 UPS02238726 1 20020607 A 5230 WEB BOEING 727 72722C 138400F NM FWD CRG.DR.STP. CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI FWD CARGO DOOR AFT LWR.STOP ON FUSELAGE HAS A CRACKED SUPPORT WEB. WEB REMOVED IAW SRM 51-30-02 . NEW WEB FABRICATED IAW SRM 53-10-2 FIG.3 AND SRM 51-20-1 FIG 7. WEB INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2002070300084 20020703 00084 NM 2002 7 3 UPS02238727 1 20020612 A 2730 HINGE BOEING 727 72722C 138400F NM LH ELEV #5 BL.PL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI FOUND ON #5 BALANCE PANEL(LH ELEV) 1.LIGHT SURFACE CORROSION ON AFT HINGE ASSY. 2.LIGHT SURFACE COR ROSION WHERE AFT HINGE MATES WITH BAL ANCE PANEL. UPON INVESTIGATION FOUND HALF OF AFT HINGE ASSY CORRODED BEYOND LI MI TS IAW SRM 51-80-7-AFT HINGE REPLACED. 2 L 7 3 4F A3WE 2002070300085 20020703 00085 NM 2002 7 3 UPS02238728 1 20020613 A 5320 ANGLE BOEING 727 72722C 138400F NM BS1180 RBL30 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI ANGLE CRACKED AT BS1180 RBL 30 APPROX IN LWR AFT CARGO BAY. CRACKED ANGLE REMOVED IAW SRM 51-30 -2 NEW ANGLE FAB. IAW SRM 51-20-1 FIG7 AND SRM 53-10-2 FIG 5 NEW ANGLE INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2002070300086 20020703 00086 NM 2002 7 3 UPS02238729 1 20020615 A 5320 BRACKET BOEING 727 72722C 138400F NM BS720 S17R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI BRACKET CRACKED AT RIVET HOLE(UPP FASTENER) AT I/B LEG OF FRAME BS72 0" STR 17R 4" ABOVE FLOOR LEVE L. BRACKET REPAIRED IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2002070300087 20020703 00087 NM 2002 7 3 2002F00644 1 20020412 A 2424 939D1502 REGULATOR BOEING 727 727251 138408H NM E/E BAY MALFUNCTIONED A FX7A J A DUMP FUEL UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 19 266US 19985 DURING CLIMB-OUT OF PHL, GEN 1 BTB, GB AND FIELD LIGHTS ILLUMINATED FOLLOWED ABNORMAL PROCEDURES DUMPED 22,000 LBS RETUR NED TO AIRPORT ONE GENERATOR ALREADY ON DMI SWAPPED RN 1 AND NR 2 VOLTAGE REGULATOR. OPS CHECK GOOD PER MM 24-20. AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002070400001 20020704 00001 SO 2002 7 4 C2XA02CL142 1 20020701 A 2610 3601133500230 FIRE DETECTOR EMB 145 EMB145 3260210 SO INTERMITTENT A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 13970 10468 145146 CLE FLIGHT#3012 THE CREW REPORTED A #2 ENGINE FIRE DETECTOR FAIL MESSAGE IN CRUISE.THE AIRCRAFT LANDED WITHOUT FURTHER I NCIDENT.MAINTENANCE REPLACED THE #2 ENGINE FIRE DETECTOR LOOP.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002080200032 20020802 00032 SO 2002 8 2 C2XA02SH013 1 20020619 A 5320 14526437001 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 SHV - DURING C-CHECK INSPECTION, THE RIGHT HAND OUTBOARD BUTT STRAP WAS FOUND TO BE CORRODED BEYOND LIMITS BETWEEN FRAME S 59 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB-145 SRM 51-20-0 3. 2 L 7 2 4F RT T00011AT 2002080200033 20020802 00033 SO 2002 8 2 C2XA02SH014 1 20020619 A 5320 14525422001 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 SHV - DURING C-CK INSPECTION, THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED BEYOND LIMITS BETWEEN FRAMES 59 & 61. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB-145 SRM 51-40-02 2 L 7 2 4F RT T00011AT 2002070500001 20020705 00001 EU 2002 7 5 02185328 1 20020704 A 2130 2099K021000 OUTFLOW VALVE JETAIR JETSTM JETSTM4101 1500501 EU A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 328UE 41083 During climb of the flight from IAD to DTW, the crew reported that the aircraft would not pressurize. The flight was re turned to IAD and landed without incident. Maintenance personnel removed and replaced the cabin pressurization pneumati c outflow valve. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002070500002 20020705 00002 WP 2002 7 5 MWEA020442 1 20020702 A 2420 EP410 RELAY DOUG DC9 DC981 3022081 WP COCKPIT LH INOPERATIVE A MWEA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 31 807ME 48033 A NOISE ( RELAY ) WAS HEARD TO THE LEFT OF THE CAPTAIN AND COMM #1 AND #2 FAILURE. -- REPAIRED AND REPLACED R 2-326 RE LAY. 2 L 7 2 4F A6WE 2002070500003 20020705 00003 WP 2002 7 5 ZW0A0206801 1 20020705 A 3240 ST107Q TRANSMITTER DOUG DC9 DC982 3022082 WP FALSE INDICATION A ZW0A O OTHER O OTHER CL CLIMB 1 CE 13 960TW 49231 DURING THE CLIMB STAGE OF FLIGHT, RH BRAKE PRESSURE GAUGE INDICATES 500 PSI WITH NO VISIBLE FLUID LOST. GAUGE STILL FAIL S TO CORRECTLY REGISTER WITH PUMPS PLACED TO THE "HI" POSITION. REMOVED AND REPLACED RH BRAKE SYSTEM TRANSMITTER (293-00 61), OPERATIONAL CHECK WAS NORMAL. LAST CC- STL 5/30/01 --CLOSED-- 2 L 7 2 4F A6WE 2002080500118 20020805 00118 CE 2002 8 5 GLAB2002100 1 20020703 A 5610 10138402518 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT CRACKED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 240GL UE240 FO'S WINDSHIELD CRACKED. REMOVED AND REPLACED WINDSHIELD. 2 L 7 2 4T RT A24CE 2002070500004 20020705 00004 CE 2002 7 5 GLAB2002101 1 20020703 A 5610 10138402517 WINDSHIELD BEECH 1900 1900D 1154162 CE CAPT'S CRACKED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 220GL 0 UE220 CAPT'S WINDSHIELD CRACKED, R&R WINDSHIELD 2 L 7 2 4T RT A24CE 2002070500005 20020705 00005 SO 2002 7 5 C2XA02BT029 1 20020705 A 3350 3015 LAMP EMB 145 EMB145LR 3260212 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 12922 145338 BTV---DURING SERVICE/ROUTINE INSPECTION MAINTENANCE FOUND LEFTHAND OVERWING EMERGENCY EXIT LIGHT INOPERATIVE.....REMOVED AND REPLACED LAMP IN LEFTHAND OVERWING EMERGENCY EXIT LIGHT ASSEMBLY IN PSU IAW EMB145 AMM #33-50-07. OPS.CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2002072200096 20020722 00096 NM 2002 7 22 AWXA200200581 1 20020703 A 2750 WIRE BOEING 737 7373G7 1384595 NM FLAP INDICATOR CHAFED A AWXA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 WP 28 154AW 8746 32 23776 ON DECENT, WHEN SELECTING FLAPS 1 NO IN-TRANSIT LIGHT ILLUMINATED AND LEADING EDGE AND TRAILING EDGE FLAPS DID NOT MOVE , WHILE FOLLOWING THE QUICK REFERENCE HANDBOOK THE FLAPS DID MOVE BUT BOTH LT AND RT STOPPED AT 1, DIVERTED. **SUPP** MAINTENANCE REPLACED THE LT FLAP POSITION INDICATOR. OP CHECK WAS GOOD. NOTE: PROBLEM RETURNED ON 07/05/2002 MAINTENA NCE TROUBLESHOT WIRING FOUND WIRE CHAFED BY TORQUE T/E FLAP TUBE 4 INCHES INBOARD OF AFT LT MLG TRUNION CAP IN THE LT FL AP WELL, REPAIRED WIRE. MAINTENANCE ALSO DISCOVERED A DAMAGED PIN ON FLAP POSITION TRANSMITTER CONNECTOR D4874, REPAIRE D PIN. 2 L 7 2 4F RT A16WE 2002071600169 20020716 00169 NM 2002 7 16 F3LA200200176 1 20020629 A 7110 GUSSET BOEING 737 7372P6 1C84609 NM NR 1 COWLING GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED MULTIPLE GOUGES IN NR 1 ENGINE OTBD COWLING LOWER CHORD AND GUSSET AT SECOND LATCH FITTING FROM FWD SIDE OF COWL. REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER PER SRM 51-40-3 AND 54-10-2. DOUBLE R CHANGED THICKNESS OF FORMED SECTION AND NECESSITATED FABRICATION OF TEE FITTING U-BOLT ATTACHMENT PER EA 71-737-022. INSTALLED PER SRM 51-40-3. 2 L 7 2 4F RT A16WE 2002071600170 20020716 00170 NM 2002 7 16 F3LA200200177 1 20020701 A 5320 FLOOR SUPPORT BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED SURFACE CORROSION ON FLOOR SUPPORT BETWEEN STA 987.5 AND 1006, BL 0. FABRICATED A ND INSTALLED REPLACEMENT FLOOR SUPPORT PER EA 53-737-173 AND SRM 51-30-02 AND SRM 53-10-2. 2 L 7 2 4F RT A16WE 2002071600171 20020716 00171 NM 2002 7 16 F3LA200200178 1 20020701 A 5320 FLOOR SUPPORT BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED SURFACE CORROSION ON FLOOR SUPPORT BETWEEN STA 967 AND 987.5, LBL 18. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER EA 53-737-173 AND SRM 51-30-02 AND SRM 53-10-02. 2 L 7 2 4F RT A16WE 2002071600172 20020716 00172 NM 2002 7 16 F3LA200200179 1 20020701 A 5320 65458752 SILL BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON R1 DOOR MOP SILL AND THRESHOLD SUPPORT. REMOVED CORROSION ON MOP SIL L AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REPLACED MOP SILL PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 2002071600173 20020716 00173 NM 2002 7 16 F3LA200200180 1 20020701 A 5320 SILL BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED R1 DOOR LOWER SILL WEB CRACKED AT FWD DRAIN HOLE. REMOVED DAMAGED WEB, FABRICATED REPAIR DOUBLER AND FILLER PER SRM 51-40-02, AND INSTALLED REPAIR PARTS PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002071600174 20020716 00174 NM 2002 7 16 F3LA200200181 1 20020702 A 5315 FLOORBEAM BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TOP OF FLOORBEAM AT STA. 947.5, RBL 38 TO RBL 43.75. REPAIRED FLOOR BEAM PER SRM 53-10-9. 2 L 7 2 4F RT A16WE 2002071600176 20020716 00176 NM 2002 7 16 F3LA200200182 1 20020702 A 5315 FLOORBEAM BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TOP OF FLOORBEAM AT STA 987.5, RBL 36 TO RBL 40. REPLACED FLOORBEAM PER SRM 53-10-9, FIG 3. 2 L 7 2 4F RT A16WE 2002071600181 20020716 00181 NM 2002 7 16 F3LA200200183 1 20020701 A 5320 FLOOR SUPPORT BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED FLOOR SUPPORT CORRODED BETWEEN STA 967 TO 987.5, RBL 20. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER EA 53-737-173 AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 2002070800001 20020708 00001 NM 2002 7 8 ANCF200200012 1 20020627 A 3260 PROXIMITY SENSOR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE MLG DOOR MALFUNCTIONED W ANCF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 23 190AN 53190 DURING TAKE OFF ROLL, GEAR DOOR OPEN ANNUNTIATION CAME ON. TAKE OFF WAS ABORTED. WAS ADJUSTED AND CLEANED DOOR PROXIMITY SENSOR IAW AMM 32-60-00. WAS PERFORMED BITE ON PSEU IAW AMM 32-60-04 PARAGRAPH 1C, PAGE 201. RESULTS SATISFACTORY. 2 L 7 2 4F 4 F RT E9NE 2002070800002 20020708 00002 WP 2002 7 8 ASM2002F00000 1 20020518 A 7711 LG80E1 COMPUTER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE NR 2 ENGINE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 505MD 6245 49149 AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF LOW ACCELERATION IN ENGINE NUMBER TWO AND THE THROAT EPR NR 2 WAS OUT OF SERVICE. THE EPR TX ASSY NUMBER TWO WAS REPLACED IAW MM. 2 L 7 2 4F 4 F A6WE E2EA 2002070800003 20020708 00003 NM 2002 7 8 0202045508 1 20020606 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 508US 23197 DURING "H" CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 45. REPAIRED PER EA 55-189888. 2 L 7 2 4F RT A2NM 2002070800004 20020708 00004 2002 7 8 ASM2002F00001 4 20020518 A 2565 100505107 SLIDE DOUG DC9 DC982 3022082 WP CABIN DEPLOYED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 1003X 3638 48067 WHILE IN TRANSIT, THE MECHANIC TRIED TO ADJUST THE BAR OF THE AFT GALLEY SLIDE AND IT WAS DEPLOYED. THE AIRCRAFT FERRIE D TO MEXICO BECAUSE NO SLIDE WAS AVAILABLE AT THE STATION. BARS AND FASTENERS WERE LUBRICATED AND ADJUSTED AND THE SLID E WAS REPLACED IAW MM. 2 L 7 2 4F A6WE 2002070800005 20020708 00005 NM 2002 7 8 ASM2002F00002 1 20020518 A 2823 ACTUATOR BOEING 757 7572Q8 1384972 NM FUEL SHUTOFF FAILED W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 803AM 26268 DURING INSPECTION, DETECTED A LEAK IN THE RIGHT FUEL TANK. THE LEAK WAS AT THE RIGHT SHUTOFF VALVE. RIGHT TANK WAS SE ALED. DURING OVERNIGHT SERVICE THE O-RINGS OF SHUTOFF VALVE ACTUATOR WAS REPLACED IAW MM. 2 L 7 2 4F RT A2NM 2002070800006 20020708 00006 WP 2002 7 8 ASM2002F00003 1 20020519 A 3230 BYPASS VALVE DOUG DC9 DC987 3022087 WP HYD SYSTEM MALFUNCTIONED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 1075T 49724 AIRCRAFT RETURNED FROM FLIGHT AS A CONSEQUENCE OF LANDING GEAR DOOR NOT RETRACTING. DURNING CHECK, THE LANDING GEAR BYP ASS VALVE WAS OPEN AND NOT SECURED. VALVE WAS REPOSITIONED. 2 L 7 2 4F RT A6WE 2002070800007 20020708 00007 2002 7 8 ASM2002F00004 4 20020519 A 2565 100502121 SLIDE DOUG DC9 DC982 3022082 WP CABIN FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 1003X 402 48067 ON ARRIVAL, FLIGHT ATTENDANT REPORTED THE AFT GALLEY SLIDE WAS LOCKED AND UNABLE TO UNLOCK. WHEN INSPECTED BY THE MECHA NIC THE SLIDE COVER SEPARATED FROM THE DOOR. THE COVER SLIDE WAS REINSTALLED ON THE DOOR, THE BAR WAS REPOSITIONED AND THE SAFETY PIN WAS REINSTALLED IAW MM. DURING OVERNIGHT SERVICE THE SLIDE WAS REPLACED IAW MM. 2 L 7 2 4F A6WE 2002070800008 20020708 00008 WP 2002 7 8 ASM2002F00005 1 20020520 A 2910 8365DG20 FUSE DOUG DC9 DC983 3022083 WP HYD SYSTEM LEAKING W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 838AM 7343 49397 AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF HYDRAULIC LEAK AND LOW PRESSURE INDICATION. DURING REVISION WAS DETECTE D A CRACK ON THE LEFT FUSE ASSEMBLY HYDRAULIC QUANTITY MEASURE. IT WAS CHANGED IAW MM, TEST OK. 2 L 7 2 4F RT A6WE 2002070800009 20020708 00009 2002 7 8 ASM2002F00006 4 20020520 A 3420 INDICATOR DOUG DC9 DC987 3022087 WP COCKPIT INACCURATE W ASMF O OTHER O OTHER NR NOT REPORTED 1 SW 23 205AM 49405 AIRCRAFT RETURN TO FLIGHT AS A CONSEQUENCE OF 60 DEGREE DIFFERENCE ON LEFT HEADING OR AUXILIARY AHRS, DIFFERENCE COULD N OT BE CORRECTED. AHRS ELECTRICAL CONNECTOR WAS CLEANED AND AHRS NR 1 WAS INTERCHANGED WITH AHRS NR 3, TESTS PERFORMED I AW MM. 2 L 7 2 4F RT A6WE 2002070800010 20020708 00010 WP 2002 7 8 ASM2002F00007 1 20020512 A 3230 ACTUATOR DOUG DC9 DC987 3022087 WP NLG FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 753RA 2361 49587 AIRCRAFT RETURN AS A CONSEQUENCE OF NOSE LANDING GEAR DOOR NOT RETRACTING AND A PRESSURIZATION FAILURE. AIRCRAFT WAS S ENT TO THE HANGAR. REPLACED THE NOSE GEAR ACTUATOR ASSEMBLY, NOSE GEAR BUNGEE CYLINDER, NOSE GEAR CONTROL VALVE, AND O- RINGS IAW MM. TESTS OK IAW MM. IN RELATION TO THE PRESSURIZATION REPORT, THE RIGHT FAN AND TWO CIRCUIT BREAKERS WERE C HANGED IAW MM. 2 L 7 2 4F RT A6WE 2002070800012 20020708 00012 SO 2002 7 8 CA020607012 1 20020603 A 5751 8656204 SKIN PIPER PA44 PA44180 7104402 SO LYC O360 O360A1H 41514 EA LT AILERON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 21443 (CAN) DURING AN EVENT NR 3 INSPECTION AN APPROXIMATE 1 INCH CRACK WAS FOUND ON THE LOWER SURFACE OF THE LT AILERON. THE CRACK WAS LOCATED NEAR THE INBOARD END OF THE AILERON AT THE TRAILING EDGE OF THE SIXTH STIFFENING BEAD. THE AILERON WAS REMOVED AND REPLACED WITH A SERVICEABLE AILERON. 1 L 7 2 3O 3 O A19S0 E286 2002070800018 20020708 00018 2002 7 8 CA020613005 4 20020423 A 3423 SEAL CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13D 03004 GL COMPASS LEAKING W O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) THE MAGNETIC STANDY COMPASS WAS FOUND BY THE AIR CREW TO BE LEAKING FLUID ACCOPAMIED BY A STRONG SOLVENT ODOUR. LA B RESULTS REPORTED THE FLUIDTO BE MINERAL SPIRITS CONTAINING AROMATIC HYDROCARBONS, CYCLIC HYDROCARBONS, ISOPARAFFINS AN D NORMAL PARAFFINS. THE CONCLUSION OF THE REPORT STATES IN PART: "THE AROMATIC HYDROCARBONS IN THE FLUID USED IN THE COM PASS PROBABLY CAUSED DAMAGE TO THE GASKET WITH THE RESULT BEING A LEAKY COMPASS". 2 L 7 2 4R 4 T 6A6 E282 2002070800019 20020708 00019 CE 2002 7 8 CA020614001 1 20020606 A 3213 5041000206 SEAL CESSNA 414 414 2075908 CE CONT O520 TSIO520NB 17040 SO MLG STRUT CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) RIGHT GEAR HAD LOST ITS NITROGEN CHARGE DURING FLIGHT. REPLACED SEALS IN OLEO AND WHILE SERVICING OLEO IT WAS NOTE D HYDRAULIC FLUID WAS APPEARING IN LOWER AREA OF BARREL. ON CLOSER INSPECTION FOUND BARREL CRACKED AT POINT WHERE BARREL L IS FITTED WITH MAIN GEAR DRAG BRACE ATTACHMENT LUG. UPPER TRUNNION REPLACED WITH REPAIRED PART. 1 L 7 2 3O 3 O RT A7CE E8CE 2002070800021 20020708 00021 SW 2002 7 8 CA020614004 1 20020610 A 3243 AM38022 COTTER PIN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP MASTER CYLINDER BENT W O OTHER J WARNING INDICATION LD LANDING 1 CA (CAN) ON FIRST FLIGHT AFTER REPLACEING THE BRAKE MASTER CYLNDERS WITH OVERHAULED UNITS IN ACCORDANCE WITH AD 2002-08-01. THE RT BRAKE LOCKED UP ON LANDING. THE PILOTS RT BRAKE CYLINDER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. A SUBSEQUENT TEARDOWN OF THE FAULTY BRAKE MATER CYLINDER REVEALED THAT THE AN380-2-2 COTTER PIN THAT SECURED THE A-50-H- 011 STOP WAS BENT PREVENTING THE BRAKE FROM RELEASING.IT IS SUSPECTED THAT THIS PIN WAS BENT DURING TOO AGGRESSIVE PRESS URE BLEEDING OF THE BRAKE SYSTEM. 2 L 7 2 4T 4 T RT A8SW E4WE 2002080700041 20020807 00041 2002 8 7 ARWA20020701 4 20020703 A 3421 258733511 GYRO DOUG DC8 DC861 3021952 WP NR 2 FAILED A ARWA C ABORTED TAKEOFF I FLT. ATTITUDE INST. TO TAKEOFF 1 SO 19 29UA 46159 AT START OF TAKEOFF ROLL F/O ARTIFICIAL HORIZON FAILED WITH FLAG, REJECTED TAKEOFF AT 40 KNOTS AND RETURNED TO RAMP. RE MOVED AND REPLACED NR 2 VERTICAL GYRO IAW MM 34-25-0. GROUND TEST OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002070800023 20020708 00023 SO 2002 7 8 ASOA02337 1 20020612 A 5300 12005744613 STRINGER EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 266AS 120188 DURING (C) CHECK INSPECTION, STRINGER 19 LEFT WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 15 AND 15A. MAINTEN ANCE REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER AND INSTALLED A SPLICE IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070800024 20020708 00024 SO 2002 7 8 ASOA02338 1 20020612 A 5300 12005744017 STRINGER EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 266AS 29712 120188 DURING (C) CHECK INSPECTION, STRINGERS 20 RIGHT AND 21 RIGHT WERE FOUND TO BE CORRODED OUT OF LIMITS AT FRAME 17. MAINT ENANCE REMOVED AND REPLACED THE CORRODED SECTIONS OF STRINGER AND INSTALLED SPLICES IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070800026 20020708 00026 GL 2002 7 8 CA020617006 2 20020613 A 7250 1473M51P01 MANIFOLD AIRBUS 310 A310 EU GE CF6 CF680C2* GL NR 1 ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOUND CRACK ON NR 1 ENGINE LPT AIR MANIFOLD SLEEVE BETWEEN 6-7 OCLOCK POSITION. A TEMPORARY REPAIR TO THE MANIFO LD SLEEVE WAS CARRIED OUT. A FLUID PENETRANT INSPECTION WAS CARRIED OUT; NO EVIDENCE OF CRACK FOUND. A DEFERRED MAINTE NANCE ITEM WAS RAISED, FOR RE-INSPECTION; WELDING TO BE INSPECTED FOR CRACK, EVERY 5 CYCLES UNTIL CRACK RECURS OR A/C NE XT CHECK, (SLEEVE IS TO BE REPLACED). 2 L 7 2 4F 4 F RT A35EU E23EA 2002070800027 20020708 00027 SO 2002 7 8 ASOA02339 1 20020612 A 5300 12006964001 CROSSBEAM EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 266AS 29712 120188 DURING (C) CHECK INSPECTION, THE LEFT INBOARD CROSS BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS AT FRAME 20. MAINTENANC E REMOVED AND REPLACED THE CORRODED CROSS BEAM IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070800028 20020708 00028 WP 2002 7 8 CALA0200392 1 20020704 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 200-300 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND R/H CENTER SEAT TRACK CORRODED FROM FS 200-300. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-04, FIGURE 4. 2 L 7 2 4F A6WE 2002070800029 20020708 00029 2002 7 8 CA020617007 4 20020614 A 2213 7003974722 COMPUTER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE COCKPIT FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 25139 (CAN) ENROUTE NR 2 FLIGHT DIRECTOR FLAGGED , F/D BARS COULD NOT BE REMOVED . AIRCRAFT RETURNED TO ORIGINATING STATION FO R NORMAL LANDING . NR 2 FLIGHT GUIDANCE COMPUTER REPLACED . AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002070800030 20020708 00030 EA 2002 7 8 COMA0260391 1 20020702 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 962CA 7123 FLIGHT 5668 FLAS FAIL MESSAGE AT 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002070800031 20020708 00031 SO 2002 7 8 ASOA02340 1 20020612 A 5300 12007089003 BUTT STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 266AS * 120188 120188 DURING (C) CHECK INSPECTION, THE CENTER BUTT STRAP WAS CORRODED BEYOND LIMITS BETWEEN FRAMES 13 AND 16. MAINTENANCE RE MOVED AND REPLACED THE CORRODED CENTER BUTT STRAP IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070800032 20020708 00032 EA 2002 7 8 COMA0260392 1 20020702 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 932CA 2547 7038 FLIGHT 5790 FLAPS FAIL MESSAGE DURING TAXI.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2002070800033 20020708 00033 SO 2002 7 8 ASOA02341 1 20020612 A 5300 12046158603 BUTT STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 266AS 29712 120188 DURING (C) CHECK INSPECTION, THE LEFT HAND BUTT STRAP WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN STA 6653.1 AND FRAM E 25. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070800034 20020708 00034 EA 2002 7 8 COMA0260393 1 20020628 A 7900 5018T49P01 SEAL CNDAIR CL600 CL6002B19 1900309 EA ACC GEAR BOX LEAKING A COMA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 01 949CA 1 1 7080 FLIGHT 5298 LEFT ENGINE OIL PRESSURE WARNING AFTER T/O, AIRCRAFT RETURNED TO MSP. (IFSD)REPLACED ACCESSORY GEAR BOX OIL SEALS AT AXIS D&F. 2 L 7 2 4F RT A21EA 2002070800035 20020708 00035 EU 2002 7 8 CA020617008 1 20020616 A 3240 SOLENOID VALVE BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE BRAKES SHORTED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) NO GREEN BRAKE PRESSURE INDICATION WHEN BRAKES APPLIED WITH GREEN SYSTEM SELECTED , AIRCRAFT STOPPED BUT SHOWS YEL LOW SYSTEM BRAKE PRESSURE INDICATION. GREEN ENABLE SOLENOID FOUND PIN A SHORTED TO GROUND & PIN A TO B OPEN CIRCUIT . GR EEN BRAKES ENABLE SOLENOID REPLACED. 2 H 7 4 4F 4 F A49EU E6NE 2002070800036 20020708 00036 EA 2002 7 8 COMA0260394 1 20020630 A 5210 1323901 SPRING CNDAIR CL600 CL6002B19 1900309 EA DOOR BROKEN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 963CA 7127 FLIGHT 5693 CABIN DOOR OUTER HANDLE MESSAGE.REPLACED SPRING ON OUTER DOOR HANDLE. 2 L 7 2 4F RT A21EA 2002070800037 20020708 00037 NM 2002 7 8 CA020617009 1 20020616 A 3297 WIRE HARNESS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NLG CHAFED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 99999 14247 (CAN) ON TAKEOFF NLG WOULD NOT RETRACT , AIRCRAFT RETURNED FOR NORMAL LANDING . INSPECTION FOUND WIRING FOR DRAG STRUT P ROXIMITY SENSOR CHAFFED . PROX SENSOR ASSEMBLY REPLACED . GEAR SWINGS CARRIED OUT . AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002070800038 20020708 00038 EA 2002 7 8 COMA0260395 1 20020628 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA AVIONICS DISCHARGED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 936CA 18152 7043 FLIGHT 5556 - EMERGENCY LIGHTS ARE INOP.REPLACED THE EMERGENCY BATTERIES. 2 L 7 2 4F RT A21EA 2002070800039 20020708 00039 EU 2002 7 8 CA020618003 1 20020613 A 2530 3510004409 COFFEEMAKER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GALLEY FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) 20 MINS.,INTO FLT, CSM ADVISED CAPTAIN THAT STRONG ELECT. SMELL & SMOKE IN AFT GALLEY AREA. FLT CREW ADVISED ATC O F SMOKE IN CABIN & REQ IMMEDIATE RETURN TO VANCOUVER. FLT CREW TURNED GALLEY POWER OFF, AND CSM ADVISED THAT SMOKE HAD C EASED & SMELL HAD DECREASED IN INTENSITY. ATC ADVISED THAT SITUATION UNDER CONTROL. OVERWT LDG COMPLETED. AFTER LDG CREW ENSURED THAT NO INCREASING SMOKE OR ODOUR IN CABIN AND THEN TAXIED TO GATE. MAINT DISCOVERED NR 3 AFT COFFEEMAKER HAD B URNED WIRING &T HAT LOW WATER SENSOR HAD EXITED FROM TOP OF BOILER. COFFEEMAKER REMOVED FROM A/C & RETURNED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002070800040 20020708 00040 CE 2002 7 8 CA020619001 1 20020613 A 3222 O4425037 FORK CESSNA 150 152 2071835 CE LYC O235 O235N2C 41505 EA MLG STRUT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AIRCRAFT WAS BROUGHT IN FOR ROUTINE INSPECTION. DECIDED TO DO A CLOSER INSPECTION ON THE OLEO COMPONENTS DUE TO T HE HIGH TIME ON THESE UNITS. A CLOSE VISUAL INSPECTION AIDED BY A MAGNIFIER REVEALED A CRACK ON THE TOP OUTER SURFACE OF THE FORK ASSEMBLY. THE UNIT WAS REMOVED FROM SERVICE. TOTAL TIME IS UNKNOWN BUT IS LIKELY HIGH BASED ON APPEARANCE AND KNOWN OPERATING ENVIRONMENT. 1 H 7 1 3O 3 O NT 3A19 E223 2002070800046 20020708 00046 EU 2002 7 8 CA020620001 1 20020619 A 4950 DUCT AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE APU LOOSE W B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) CLIMBING THROUGH 18000FT, CSM ADVISED OF SMELL OF SMOKE IN CABIN. EMERGENCY DECENT, A/C RETURNED TO HER(GREECE) PA SSENGERS COMMENTED THAT SIDE WALL PANELS AROUND ROW 25 - 30 WERE HOT. T/S REVEALED THAT CLAMP HOLDING APU BLEED DUCT HAD COME LOOSE, ALLOWING HOT AIR INTO THE CARGO HOLD/SIDEWALL AREA. NEW SEALS INSTALLED, CLAMP RE-ATTACHED, LEAK CKECKED OK . 2 L 7 2 4F 4 F RT A28NM E311NE 2002070800047 20020708 00047 2002 7 8 CA020621002 4 20020527 A 2312 WIRE CNDAIR CL601 CL6013A 8070802 EA GE CF34 CF343A 30015 NE MICROPHONE SHORTED W O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA (CAN) A BROKEN WIRE SHORTED TO GROUND ON CAPTAINS HAND MIKE JACK LOCATED ON LOWER CONTROL COLUMN PREVENTED NORMAL VHF TA NSMISSION. PILOTS OXYGEN MASK SELECTED TO EMERGENCY (EMERGENCY MIRE POSITION)AND COMMUNICATIONS WERE RESTORED. WIRE REPA IRED PER DRAWING WITH NO FUTHER PROBLEMS REPORTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070800049 20020708 00049 NM 2002 7 8 E220405 1 20020703 A 3230 MODULE BOEING 747 74745E 1384947 NM MLG HANDLE FAILED W QOCF O OTHER O OTHER AP APPROACH 1 WP 03 16405 40527142 STS MAG "GEAR MOMNITOR" REPLACED GEAR CONTROL HANDLE MODULE PERFORM ALL LANDING GEAR ALTE EXTENSIN SYS TEST NML. 2 L 7 4 4F RT A20WE 2002070800050 20020708 00050 EA 2002 7 8 COMA0260396 1 20020629 A 3350 59256 INVERTER CNDAIR CL600 CL6002B19 1900309 EA AVIONCIS MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 915CA 7013 FLIGHT 5883 - EMERGENCY LIGHTS AT ROW 1 ARE INTERMITTENT.REPLACED THE #1 INVERTER. 2 L 7 2 4F RT A21EA 2002070800051 20020708 00051 2002 7 8 COMA0260397 4 20020628 A 3440 6222855011 ALTIMETER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 01 924CA 20891 7026 FLIGHT 5747 PILOTS RADAR ALTIMETER INDICATES 700 FT AT 17,000 FT.REPLACED THE #1 RADAR ALTIMETER. 2 L 7 2 4F RT A21EA 2002070800052 20020708 00052 EA 2002 7 8 COMA0260398 1 20020627 A 3350 59465 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 958CA 7111 FLIGHT 5200 EMERGENCY FLOOR PATH LIGHTS INOP BETWEEN ROWS 2 AND 6.SECURED LOOSE WIRE CONNECTION AT ROW 6. 2 L 7 2 4F RT A21EA 2002070800053 20020708 00053 SO 2002 7 8 ASOA02342 1 20020612 A 5300 12005803001 SILL EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 266AS 29712 120188 DURING (C) CHECK INSPECTION, THE RIGHT HAND SILL PLATE WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 13 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070800054 20020708 00054 NM 2002 7 8 F3LA200200186 1 20020701 A 5315 FLOORBEAM BOEING 737 7372P6 1C84609 NM STA. 947.5 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TOP OF FLOOR BEAM AT STA. 947.5, RBL 38. REPAIRED FLOOR BEAM PER SRM 53-10-9. 2 L 7 2 4F RT A16WE 2002070800055 20020708 00055 SO 2002 7 8 ASOA02343 1 20020612 A 5300 12005802001 SILL EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 266AS 29712 120188 DURING (C) CHECK INSPECTION, THE LEFT FLOOR SILL PLATE WAS CORRODED OUT OF LIMITS BETWEEN FRAMES 15A AND 21. MAINTENANC E REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070800056 20020708 00056 EA 2002 7 8 ASOA02344 1 20020617 A 5300 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 824AS 7203 DURING HANGER MAINTENANCE, THE LEFT ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE CRACKED ENGIN E SUPPORT BEAM IAW REO. THIS REO GIVES REPAIR SPECIFICATIONS FOR THE ENGINE SUPPORT BEAM CRACK, AS WELL AS OUTLINES A T HRESHOLD OF CYCLES FOR THE PERMANENT REPAIR AND FOLLOW UP NDT INSPECTIONS. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070800057 20020708 00057 SW 2002 7 8 2002F00639 1 20020607 A 2497 205075265103 WIRE HARNESS 30E2061 BELL 205 205A1 1181414 SW STARTER GEN BURNED E GAKA A UNSCHED LANDING B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING NR NOT REPORTED 1 NM 11 205BD 5601 30097 SERVICE ABOUT 1415 HOURS. AFTER A NORMAL START PROCEDURE AND RUN-UP A DEPARTURE WAS MADE. ABOUT 10 MINUTES INTO FLIGHT , ACID SMELL WAS NOTICED. SCANNED THE INSTRUMENT PANEL ALL INSTRUMENTS WERE IN THE GREEN THERE WERE NO CAUTION LIGHTS. MASTER CAUTION LIGHT FLASHED, TURNED OFF THE MAIN GENERATOR. PLACED THE BUS SWITCH FROM NORMAL TO MANUAL AND TURNED TH E AIRCRAFT BACK TO THE AIRPORT. AFTER THE TURN TO THE AIRPORT, THE FIRE LIGHT BEGAN TO FLASH. AFTER LANDING FOUND THE MAIN WIRING HARNESS FROM THE GENERATOR THROUGH THE ENGINE DECK TO BE MELTED AND SMOLDERING. 1 G 7 1 4U H1SW 2002070800059 20020708 00059 GL 2002 7 8 2002FA0000789 2 20020405 A 7314 SEAL AEROSP AS355 AS355F2 8680812 EU ALLSN 250C 250C20F 03013 GL FUEL PUMP LEAKING D LN3A K NONE O OTHER IN INSP/MAINT 1 EA 03 941MS 5495 CAE840376 MECHANIC NOTICED DRIPPING OF FLUID WHILE AIRCRAFT TOOK OFF, RADIOED PILOT AND REQUESTED AIRCRAFT TO RETURN TO BASE. IN SPECTION FOUND FUEL COMING FROM (SEAL DRAIN). REMOVAL OF PUMP, INSPECTION FOUND SHAFT SEAL DETERIORATED. 1 G 7 2 3U 3 U H11EU E4CE 2002070800060 20020708 00060 EU 2002 7 8 2002FA0000806 1 20020625 A 6410 117317411 BLADE BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED B LN3A K NONE O OTHER IN INSP/MAINT 1 EA 03 117UP 050278 7508 TAIL ROTOR BLADE, CRACKED. 1 G 7 2 3U 3 U NC H13EU E19EU 2002070800061 20020708 00061 GL 2002 7 8 ALG2002F00043 2 20020512 A 7210 6893673 GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE GALLED E ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 687AL 4781 53366 847311 ENGINE WAS REMOVED DUE TO CHIP LIGHTS. UPON VISUAL INSPECTION FOUND CAUSE OF METAL DUE TO GALLING T/M AND PTO GEARS. D UE TO T/M JOURNAL SUPPORT STUDS BACKING OUT OF COVER AN UNUSUAL WEAR PATTERN OF SPALLING AND GALLING OCCURRED ON GEAR TE ETH. THIS COULD HAVE CAUSED A CATASTROPHIC GEAR FAILURE. ASSURE PROPER INSERTS IN THIS AREA, ALONG WITH PROPER MACHINI NG AND MESHING OF GEAR TEETH. 1 G 7 1 3U 3 U O H2SW E1GL 2002070800062 20020708 00062 GL 2002 7 8 ALG2002F00044 2 20020512 A 7210 23065470 COVER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 687AL 4781 2790 53366 847311 ENGINE HAD CHIP LIGHTS. UPON DISASSEMBLY OF GEARBOX FOUND T/M JOURNAL SUPPORT STUDS BACKED OUT OF COVER. FOUND T/M GEA R, BEARING JOURNAL SHAFT AND SUPPORT LOOSE IN COVER ASSEMBLY. FOUND ALL 4 STUDS ON JOURNAL SUPPORT PULLED OUT AND 1 EAC H WITH NO THREADS LEFT IN WORN BORE. THIS ALLOWED GEAR TO WEAR IN AN UNUSUAL MANNER, WHICH COULD HAVE RESULTED IN A CAT ASTROPHIC GEAR FAILURE. ASSURE GEARBOX AND ASSOCIATED ENGINE PARTS CAN WITHSTAND HIGH TORQUE. INSTALLED INSERTS AT ALL STUD AREAS INSIDE COVER ASSEMBLY. 1 G 7 1 3U 3 U O H2SW E1GL 2002070800064 20020708 00064 GL 2002 7 8 ALG2002F00046 2 20020322 A 7210 6898785 GEAR BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL GEARBOX SPALLED E ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 355AL 75 51444 CAE890701 UPON DISASSEMBLY OF GEARBOX. SPALLING AND GALLING ON GEAR TEETH DUE TO IMPROPER MESHING OF TEETH. ASSURE PROPER MESHIN G OF GEAR TEETH. 1 G 7 1 3U 3 U H2SW E1GL 2002070800065 20020708 00065 GL 2002 7 8 ALG2002F00047 2 20020502 A 7210 6893672 PINION GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX WORN E ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 403AL 752 53478 CAE847270 UPON DISASSEMBLY OF GEARBOX. UPON DISASSEMBLY OF GEARBOX FOUND EXCESSIVE GALLING AND SPALLING AND WEAR IN GEAR TEETH AN D UNEVEN WEAR AND HEAVY SPALLING OF T/M GEAR TEETH. ASSURE PROPER MESHING OF GEAR TEETH. 1 G 7 1 3U 3 U O H2SW E1GL 2002070800066 20020708 00066 GL 2002 7 8 ALG2002F00048 2 20020502 A 7210 23065470 COVER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX STRIPPED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 403AL 752 53478 CAE847270 (GEARBOX COVER) UPON DISASSEMBLY OF GEARBOX, FOUND 1 EACH STRIPPED STUD AND 2 EACH LOOSE STUDS AT 2.5 BEARING CAGE MATIN G SURFACE, ALSO FOUND 2 EACH STUDS AT TM SUPPORT JOURNAL LOOSE. NOTE: AT LOCATION OF STRIPPED STUD ON T.5 BEARING CAGE SURFACE, FOUND NO THREADS IN STUD BORE. NOTE: THISCONDITION COULD POSSIBLY CAUSE CATASTROPHIC GEAR FAILURE. URGENT: INSTALL HELICOILS IN STUD BORES AT FACTORY TO ALLOW FOR HIGH TORQUE OF ENGINE IN THIS AREA. 1 G 7 1 3U 3 U O H2SW E1GL 2002070800067 20020708 00067 EA 2002 7 8 ASOA02346 1 20020617 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 876AS 1363 7576 DURING GROUND INSPECTION, THE AFT EXTERIOR EMERGENCY LIGHT ON THE RIGHT HAND SIDE OF THE FUSELAGE WAS INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE BURNT OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OF FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070800068 20020708 00068 NE 2002 7 8 EGR2002F00003 2 20020620 A 7320 23072726 HYDROMECH UNIT BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE FUEL CONTROL LEAKING E EGRA K NONE O OTHER IN INSP/MAINT 1 EA 17 993PA 992 49050 DURING FLIGHT CREWS SMELLED FUEL FUMES AFTER LANDING AT HOSPITAL. PILOT SAW FUEL IN THE NR 2 ENGINE COMPARTMENT. CECHA NIC PINPOINTED FUEL LEAK TO THE AFT SIDE OF THE HMU, COMING FROM A PLATE WITH AN ADJUST/CONTROL. 1 G 7 2 3U 3 U RT H9SW E1GL 2002070800069 20020708 00069 NE 2002 7 8 EGR2002F00004 2 20020611 A 7320 23072726 HYDROMECH UNIT BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE NR 2 ENGINE INOPERATIVE E EGRA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 17 993PA 1171 49050 CAE844106 ON START UP, PILOT GOT A MECU 2 INDICATION ON THE IIDS. FAULTS WERE: STOPCMTFLT, WFHDFLT, CPU HARD FLT AND WDT HARD FL IGHT. REMOVED AND REPLACED HMU. CLEARED FAULTS. 1 G 7 2 3U 3 U RT H9SW E1GL 2002070800070 20020708 00070 EA 2002 7 8 ASOA02348 1 20020617 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN WEAK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 834AS 9365 7254 DURING TESTING OF EMERGENCY LIGHTS, THE EMERGENCY LIGHTS AT ROWS 10-12 WERE FOUND INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY LIGHTING BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070800071 20020708 00071 2002 7 8 801DM0005 4 20020705 A 3414 PITOT HEAD BOEING 757 757200 1384950 NM A PIDA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 05 801DM 26240 Rejected takeoff for airspeed discrepancy. Capt's 20 kts. less thatn F/O's @ 100 KIAS.Upon further examination found bl ockage in captain's pitot. Cleared blockage IAW MM 73-11-01.Performed high speed taxi up to 100(?) KIAS and no defects were noted. OK for continued service. 2 L 7 2 4F RT A2NM 2002070800072 20020708 00072 SW 2002 7 8 FSP2002F00000 1 20020605 A 7921 407340339101 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C* GL COOLER BLOWER FAILED E FSPA K NONE O OTHER IN INSP/MAINT 1 NE 05 407NN 242 53250 INSPECTED AIRCRAFT, FOUND DARK GRAY GREASE COMING FROM THE BEARINGS. IF THE EXPELLED GREASE HAS TURNED BLACK, THE BEARI NG MUST BE REMOVED FROM SERVICE. 1 G 7 1 3U 3 U O H2SW E4CE 2002070800073 20020708 00073 SW 2002 7 8 GAK2002F00000 1 20020607 A 2435 205075265103 WIRE HARNESS BELL 205 205A1 1181414 SW STARTER GEN MELTED E GAKA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 11 205BD 556 30097 DEPARTED AIRPORT ABOUT 1415 HOURS. AFTER A NORMAL START PROCEDURE AND RUN-UP A DEPARTURE WAS MADE TO AIRPORT. ABOUT 10 MINUTE INTO THE FLIGHT, ACRID SMELL WAS NOTICED. SCANNED THE INSTRUMENT PANEL ALL INSTRUMENTS WERE IN THE GREEN. THER E WERE NO CAUTION LIGHTS. ABOUT THE TIME I FINISHED MY SCAN THE MASTER CAUTION LIGHT FLASHED, TURNED OFF THE MAIN GENER ATOR. PLACED THE BUS SWITCH FROM NORMAL TO MANUAL AND TURNED THE AIRCRAFT BACK TO THE AIRPORT. AFTER THE TURN TO THE A IRPORT, THE FIRE LIGHT BEGAN TO FLASH. AFTER LANDING, FOUND THE MAIN WIRING HARNESS FROM THE GENERATOR THROUGH THE ENGI NE DECK TO BE MELTED AND SMOLDERING. 1 G 7 1 4U H1SW 2002070800074 20020708 00074 SW 2002 7 8 KBMA113839 1 20020510 A 6720 206001020029 TUBE BELL 206 206B 1181511 SW T/R CONTROL DAMAGED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 73DP 12317 2513 CONTROL TUBE IS SCARRED BEYOND LIMITS. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U H2SW 2002070800075 20020708 00075 EU 2002 7 8 KBMA113848 1 20020604 A 2822 94812209 PUMP SNIAS 350 AS350BA 8680817 EU FUEL BOOST INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 1188P 2347 BOOST PUMP INOPERATIVE. REPLACED WITH OVERHAULED UNIT. 1 G 7 1 3U NC H9EU 2002070800076 20020708 00076 EA 2002 7 8 ASOA02349 1 20020618 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 840AS 7290 7290 DURING A SCHEDULED INSPECTION, THE SECOND OVERHEAD EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE BURNT OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070800077 20020708 00077 EU 2002 7 8 KBMA113849 1 20020605 A 2435 30152603 SEAL SNIAS 350 AS350BA 8680817 EU STARTER GEN LEAKING E KBMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 270SH 21 1864 (STARTER/ GENERATOR SEAL) EXCESSIVE LEAKING. REPLACED WITH NEW SEAL. 1 G 7 1 3U NC H9EU 2002070800078 20020708 00078 NE 2002 7 8 KBMA113850 2 20020606 A 7532 3192100IND02 BLEED VALVE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE MALFUNCTIONED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 2300 (BLEED VALVE) BLEED VALVE IS NOT OPENING OR CLOSING. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002070800079 20020708 00079 NM 2002 7 8 PCAA0207073 1 20020706 A 3350 2078B BATTERY PACK DHAV DHC8 DHC8102 2809003 NM REAR INOPERATIVE A PCAA K NONE L NO TEST NR NOT REPORTED 1 EA 13 820EX 7389 1404 019 PHL- FLIGHT#126. CREW REPORTED EMERGENCY EXIT SIGN AT ROW 4 NOT ILLUMINATED. MAINTENANCE REPLACED REAR EMERGENCY LIGHT B ATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002070800080 20020708 00080 EU 2002 7 8 KBMA113851 1 20020606 A 2400 374GC014 ELECTRICAL BOX SNIAS 350 AS350BA 8680817 EU GENERATOR FAILED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 1188P 11379 2347 (MASTER ELECTRICAL BOX) GENERATOR WILL NOT COME ON LINE. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2002070800081 20020708 00081 EA 2002 7 8 ASOA02350 1 20020618 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EXT LIGHT ASSY BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 837AS 7271 DURING GROUND INSPECTION, THE FORWARD MOST EXTERNAL EMERGENCY LIGHT ON THE RIGHT HAND SIDE OF THE FUSELAGE WAS FOUND INO PERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070800082 20020708 00082 GL 2002 7 8 KBMA113855 2 20020510 A 7261 MS906007 BOLT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 73DP 12317 2513 TUBINE OIL PSI NOZZLE TO NR 5 BEARING ATTACHMENT BOLT BROKEN. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U H2SW E4CE 2002070800083 20020708 00083 SW 2002 7 8 KBMA113856 1 20020510 A 6320 206030539003 ISOLATION MOUNT BELL 206 206B 1181511 SW TRANSMISSION DEBONDED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 73DP 12317 2513 ISOLATION MOUNT DEBONDED. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U H2SW 2002070800084 20020708 00084 EU 2002 7 8 KBMA117604 1 20020605 A 5210 350A25152004 ROD SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE DOOR LATCH MISSING E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 4849 2337 (ROD) FORWARD PASSENGER DOOR LOWER LATCH ROD MISSING OR BROKEN. REINSTALLED ROD FOR LOWER LATCH. 1 G 7 1 3U 3 U NC H9EU E19EU 2002070800085 20020708 00085 EU 2002 7 8 KBMA117605 1 20020601 A 5330 COWLING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE MAIN GEARBOX DAMAGED E KBMA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 19 345SH 1530 3345 UPON TAKEOFF, HEARD STRANGE NOISE. UPON LANDING FOUND LEFT MGB COWLING RIPPED. REMOVED AND REPLACED LOWER SLEEVES WITH SERVICABLE UNITS. REMOVED AND REPLACED LEFT COWLING WITH SERVICABLE UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2002070800086 20020708 00086 NM 2002 7 8 UPS02238740 1 20020614 A 5510 RIB BOEING 727 72722C 138400F NM HOR-STAB L/H+R/H CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI INSPECT REMOVED STAB.RIBS. FOR CRACKS AND FORWARD FINDING TO ENGINEE RING(RETAIN CRACKED RIBS) DVI INSPECTION PERFORMED IAW CUSTOMER REQUEST :CRACKS NOTED @ L/H RI BS 17:20 AND 136:50 AND R/H RIBS 17:20 AND 66:50 AN D 99:79. 2 L 7 3 4F A3WE 2002070800087 20020708 00087 NM 2002 7 8 UPS02238745 1 20020615 A 5250 HINGE FITTING BOEING 727 72722C 138400F NM MID GALLEY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI SUSPECT CRACKS ON FWD.(FRAME)LWR. HINGE CUTOUT FITTING(MID GALLEY DO OR) REMOVED FITTING IAW SR M 51-30-2. INSTALLED NEW FITTING IAW DRG.65-16722. 2 L 7 3 4F A3WE 2002070800088 20020708 00088 NM 2002 7 8 UPS02238746 1 20020618 A 5310 FRAME BOEING 727 72722C 138400F NM BS338-STR.13R. CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI FRAME CRACKED AT BS338-STR.13R FRAME REPAIRED IAW SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 2002070800089 20020708 00089 EU 2002 7 8 ASOA02322 1 20020610 A 3350 7012210 LAMP AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE CABIN BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 631AS 21068 362 DURING GROUND INSPECTION, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKE N WIRE LEADING TO THE PASSENGER DOOR LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT E20NE 2002070800090 20020708 00090 NM 2002 7 8 F3LA200200187 1 20020703 A 5347 SEAT TRACK BOEING 737 7372P6 1C84609 NM BS 947-967 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TOP OF SEAT TRACK BETWEEN BS 947 AND BS 967, RBL 36.5. FABRICATED AN D INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2002070800091 20020708 00091 SO 2002 7 8 LR7A02043 1 20020705 A 5343 36058712 FITTING LKHEED 382 382G 526414U SO FS 165 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 185 4590 DURING SCHEDULED A CHECK INSPECTION PER JOB CARD HA1200 FOUND RH FS 165 NLG TRUNNION FITTING CRACKED APPROX. .75 IN. IN THE FITTING LIMITED TO THE FITTING OUTBD FLANGE ADJACENT TO THE OUTBD LOWER BOLT HOLE, RBL 18, WL 170.AIRCRAFT FERRIED T O EGSC FOR REPAIR. AT EGSC RH NLG TRUNNION FITTING REPLACED IAW SRM SMP 583-51-70 AND DWG 360587. WORK ORDER 02/06/01. 2 H 7 4 4T A1SO 2002070800136 20020708 00136 SW 2002 7 8 CA020611003 1 20020530 A 6320 02W116213 VALVE SEAT BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE FILTER BODY FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING THE SCHEDULED 25 HOUR INSPECTION THE AME NOTED THAT THE VALVE SEAT HAD UNSCREWED ITSELF FROM THE FILTER BOD Y AND DAMAGED THE FILTER, WAFER. THE VALVE SEAT WAS SECURED AND THE FILTER, WAFER WAS REPLACED. 1 G 7 1 4U 4 U H1SW E17EA 2002070800138 20020708 00138 NM 2002 7 8 CA020620006 1 20020617 A 7921 GASKET LORINORDAM 28E997 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE OIL COOLER LEAKING W E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 31960021 (CAN) NR 2 ENGINE OIL PRESSURE BETWEEN 45-65 PSI. MASTER WARNING OIL PRESSURE LIGHT NR 2 ALSO FLASHING. NR 2 ENGINE FEAT HERED. OIL PRESSURE STEADY AT 50 PSI. NR 2 ENGINE OIL COOLER FOUND LEAKING, REPLACED. TIMES AND CYCLES UNKOWN AT THIS T IME. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002070800139 20020708 00139 SW 2002 7 8 CA020621010 1 20020519 A 6320 204040424001 BEARING BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA HYDRAULIC QUILL FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) SUMP CHIP INDICATION DURING GROUND RUN PRIOR TO FLIGHT. METAL CONTAMINATION OF INTERNAL FILTER AND SUMP CHIP PLUG. TRANSMISSION REMOVED FROM SERVICE, TEARDOWN CARRIED OUT. HYDRAULIC QUILL DUPLEX BEARING IDENTIFIED AS SOURCE OF METAL GE NERATION. 1 G 7 1 4U 4 U H4SW E22EA 2002070800140 20020708 00140 NE 2002 7 8 CA020626009 2 20020619 A 8500 ENGINE DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE HARTZL HCB3Z HCB3Z302 GL NOSE FAILED W A UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) SHORTLY AFTER TAKEOFF, ENGINE BACKFIRED, HESITATED AND CLEARED ITSELF 4 TIMES IN SUCCESSION.PILOT PERFORMED EMERGE NCY LANDING AT BRAMPTON AIROPORT, WAS UNABLE TO LOWER GEAR IN TIME, AND LANDED ON FLOAT KEELS. DAMAGE TO FLOATS KEELS SU STAINED. CAUSE OF BACKFIRING UNDER INESTIGATION, FOLLOW-UP REPORT WILL BE ISSUED. 1 H 7 1 3R 3 R A806 5E1 5 C P907 2002070800141 20020708 00141 CE 2002 7 8 CA020626013 1 20020618 A 3220 59420011 BELLCRANK CESSNA 414 414 2075908 CE CONT O520 TSIO520N 17040 SO MCAULY 3AF32C 3AF32C93 GL NLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) SMALL CRACK ON BOTH RADII OF CENTRE BLOCK ON BELLCRANK. 1 L 7 2 3O 3 O RT A7CE E8CE 5 C P22EA 2002070800142 20020708 00142 NM 2002 7 8 CA020627003 1 20020626 A 2932 PRESSURE SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE SPOILERS FAILED W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA (CAN) PILOT REJECTED TAKEOFF DUE TO ROLL SPOILER OUTBOARD HYDRAULIC CAUTION LIGHT ILLUMINATED. NR 2 HYDRAULIC SYSTEM ROL L SPOILER PRESSURE SWITCH REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002070800144 20020708 00144 GL 2002 7 8 CA020702003 2 20020624 A 7323 23065121 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE FAILED W O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION HO HOVERING 1 CA (CAN) PILOT NOTICED THAT RESPONSE TO RPM CHANGES WAS GETTING SLOWER UNTIL GOVERNOR WOULD NOT KEEP UP TO THE RPM CHANGES. GOVERNOR WOULD DROOP UPON COLLECTIVE UP MOVEMENT BUT WOULD NOT RECOVER OR INCREASE RPM. THE SAME FOR COLLECTION DOWN MO VEMENT, THE RPM WOULD OVERSPEED AND WOULD NOT RECOVER AND BE CONTROLLED. SIMILAR OCCURRENCES HAVE HAPPENED AS REPORTED B EFORE AND INDICATED FAILURE IN A SHORT TIME TO COME. REMOVED AT A/F 11294.6JUNE 24/02INSTALLED AT A/F 11063.7JAN 03/02T IME SINCE REPAIR 230.9HOURS 1 G 7 1 3U 3 U H2SW E4CE 2002070800145 20020708 00145 WP 2002 7 8 ABXA020028 1 20020523 A 5315 4926223 FITTING DOUG DC9 DC933F 302207A WP FS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 FS 965 RIGHT BUTT LINE 48, FITTING WAS CRACKED AT FORWARD SIDE OF FLOOR BEAM. FABRICATED AND INSTALLED FITTING IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002070800146 20020708 00146 WP 2002 7 8 ABXA020029 1 20020529 A 5420 591326266 ANGLE DOUG DC9 DC933F 302207A WP RT. ENG. PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 RIGHT ENGINE PYLON LOWER ATTACH ANGLE BULGED AND CRACKED AT STATION 996. REPAIRED IAW SRM 54-04. 2 L 7 2 4F A6WE 2002070800147 20020708 00147 WP 2002 7 8 ABXA020015 1 20020514 A 5347 9957871553V SEAT TRACK DOUG DC9 DC933F 302207A WP COCKPIT CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 LEVEL I CORROSION AND EXFOLIATION ON SUBFLOOR AT SCREWS FOR PILOTS INBOARD AFT SEAT TRACK. DETERMINED CORROSION TO BE OU T OF LIMITS, REPLACED THE CAPTAIN'S SEAT TRACK IAW DC-9 SRM 51-10-4 AND 51-30-1. 2 L 7 2 4F A6WE 2002070800148 20020708 00148 WP 2002 7 8 ABXA020016 1 20020515 A 5311 49113832 FITTING DOUG DC9 DC933F 302207A WP FS 332 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 LEVEL I CORROSION ON FRAME FOOT AND ATTACH BOLTS AT FS 332, LONGERON 18 RIGHT. REPLACED THE FRAME FOOT FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1. 2 L 7 2 4F A6WE 2002070800149 20020708 00149 WP 2002 7 8 ABXA020017 1 20020515 A 5311 49113832 FITTING DOUG DC9 DC933F 302207A WP FS256 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 LEVEL I CORROSION ON FRAME FOOT AND ATTACH BOLTS AT FS 256, LONERON 18 RIGHT. REPLACED THE FRAME FOOT IAW DC-9 SRM 51-30 -5 AND 51-30-1. 2 L 7 2 4F A6WE 2002070800150 20020708 00150 WP 2002 7 8 ABXA020018 1 20020515 A 5315 99220422AX FITTING DOUG DC9 DC933F 302207A WP FS 237 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 CABIN FLOOR SUPPORT STRUT LOWER FITTING CRACKED AT FS 237, LONGERON 23 RIGHT. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2002070800151 20020708 00151 WP 2002 7 8 ABXA020019 1 20020515 A 5320 3920324501N FITTING DOUG DC9 DC933F 302207A WP FS 604 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 LEFT AND RIGHT ATTACH ANGLES FOR LONGERON 30, AFT OF FS 604 (PRESSURE DOME) WERE CRACKED. REPLACED ATTACH ANGLES IAW DC- 9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002070800152 20020708 00152 WP 2002 7 8 ABXA020021 1 20020515 A 5314 491627001 FITTING DOUG DC9 DC933F 302207A WP FS 676 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 FITTING CRACKED IN LEFT KEEL AREA, FS 676 AT LONGERON 29 LEFT. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002070800153 20020708 00153 WP 2002 7 8 ABXA020023 1 20020516 A 5315 99220501 FITTING DOUG DC9 DC933F 302207A WP FS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 FS 945 LEFT, CABIN FLOOR STRUT LINE FITTING WAS CRACKED. REPLACED THE STRUT LINE FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002070800154 20020708 00154 WP 2002 7 8 ABXA020024 1 20020516 A 5315 99220422AX FITTING DOUG DC9 DC933F 302207A WP FS 832 RIGHT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 FS 832 RIGHT, CABIN FLOOR SUPPORT STRUT LOWER FITTING WAS CRACKED. REPLACED THE SUPPORT FITTING IAW DC-9 SRM 51-10-4 AND 51-30-5. 2 L 7 2 4F A6WE 2002070800155 20020708 00155 WP 2002 7 8 ABXA020025 1 20020516 A 5315 99220421 FITTING DOUG DC9 DC933F 302207A WP FS 775 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 FS 775 LEFT, CABIN FLOOR SUPPORT STRUT LOWER FITTING WAS CRACKED. REPLACED THE LOWER FITTING IAW DC-9 SRM 51-30-1 AND 51 -30-5. 2 L 7 2 4F A6WE 2002070800156 20020708 00156 WP 2002 7 8 ABXA020026 1 20020516 A 5315 99220422 FITTING DOUG DC9 DC933F 302207A WP FS 775 RIGHT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 FS 775 RIGHT, CABIN FLOOR SUPPORT LOWER FITTING WAS CRACKED. REPLACED THE SUPPORT FITTING IAW DC-9 SRM 51-10-4 AND 51-30 -5. 2 L 7 2 4F A6WE 2002070800157 20020708 00157 SO 2002 7 8 ASOA02324 1 20020610 A 3600 M2275941229 WIRE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE SENSOR BROKEN A ASOA O A OTHER UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 502AS 23004 120274 DURING CLIMB OUT, AT APPROXIMATELY 19,000 FEET, CAPTAIN REPORTED THAT DUCT LEAK WARNING WAS RECEIVED WITH CORRESPONDING LEFT DUCT LEAK LIGHT ILLUMINATING. CAPTAIN RAN CHECKLIST. WITH APU BLEED CLOSED THE WARNING INDICATION WENT OUT BRIEF LY THEN RETURNED. WHEN LEFT BLEED WAS CLOSED INDICATION WENT OUT, BRIEFLY CAME BACK ON, THEN WENT AWAY AGAIN. DECISION WAS MADE TO RETURN TO AIRPORT. EMERGENCY WAS DECLARED. UPON CONTINUATION OF DUCT LEAK CHECKLIST, CAPTAIN FEATHERED THE LEFT ENGINE AND INDICATION LIGHT EXTINGUISHED, ENGINE WAS NOT SHUTDOWN. SINGLE ENGINE CHECKLIST WAS PERFORMED, AIRCRAF T LANDED SAFELY. REPAIRED WIRING TO SENSOR AT JUNCTION TO APU BLEED DUCT. OPERATION CHECKS OK. A/C OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070800158 20020708 00158 SO 2002 7 8 ASO2002F00017 1 20020611 A 3350 AGC1 FUSE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 273AS 28056 120222 DURING GROUND INSPECTION, BOTH AFT CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE EMERGENCY LIGHT FUSE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070800159 20020708 00159 WP 2002 7 8 ZW0A0206904 1 20020707 A 3350 408822101 CELL DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER NR NOT REPORTED 1 CE 13 969TW 53619 THE FIRST CLASS CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY. CHECK-C 6-2-01 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2002070800160 20020708 00160 SO 2002 7 8 ASOA02326 1 20020611 A 3350 1317 LAMP EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 230AS 37858 120032 DURING A HANGER INSPECTION, AN OVERWING EMERGENCY LIGHT ON THE RIGHT HAND SIDE OFTHE FUSELAGE WAS INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE BURNT OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070800161 20020708 00161 EA 2002 7 8 ASOA02327 1 20020611 A 2910 AE7120301 HOSE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ENG DRIVEN PUMP LEAKING A ASOA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 11 836AS 9420 7263 DURING FLIGHT, AIRCRAFT LOST ALL HYDRAULIC FLUID IN THE NR 1 SYSTEM. AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE ENGINE DRIVEN PUMP PRESSURE LINE AND ALSO REMOVED AND REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP ITSELF. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070800162 20020708 00162 NE 2002 7 8 C1HA200281006 2 20020708 A 7320 7436024 FUEL CONTROL BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE A C1HA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 15 681CA 5141 22020 655285 During climb through FL 29 the # 3 engine at fire wall thrust would only maintain 1.8 EPR N1 82 % EGT 480C N2 87% FF 350 0, at 35 engine # 3 EPR 1.25 N1 65% EGT 470, N2 70% FF 2000 applied engine anti-ice and fuel heat with no change.Removed and replaced # 3 ENG FCU per MM 72-21-01 performed full ENG TRIM/PWR CHK per MM 71-00-00 all parameters normal OPS and leak CHK good. 2 L 7 3 4F 4 F A3WE E2EA 2002070800163 20020708 00163 SO 2002 7 8 C2XA02SH021 1 20020708 A 3350 B6245305 LIGHT EMB 145 EMB145ER 3260211 SO INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 SHV- DURING C-CK INSPECTION, THE MAIN DOOR EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002070900001 20020709 00001 GL 2002 7 9 2002FA0000809 2 20020702 A 7230 EH230397911 SPLINE ADAPTER ALLSN 250C20F AEROSP AS355 AS355* EU ALLSN 250C 250C20F 03013 GL COMPRESSOR FRETTED B A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SW 21 2 CAC40289 5495 CAE841012 NEW COMPRESSOR SPLINE ADAPTER WAS PURCHASED FROM MANUFACTURER. SERVICE BULLETIN T-069 WAS PACKAGED WITH THE SPLINE ADAP TER, PROVIDING INSTRUCTIONS TO MODIFY THE IMPELLER THAT THE ADAPTER WAS GOING TO BE INSTALLED IN. BULLETIN WAS LATER REC ALLED BY MANUFACTURER, CAUSING ENGINE TO BE REMOVED TO REPLACE THE IMPELLER THAT WAS MODIFIED. REMOVAL OF SPLINE ADAPTE R AND IMPELLER REVEALED EXCESSIVE WEAR ON OD OF ADAPTER WITH ONLY 3 HOURS OF OPERATION ON IT. ADAPTER AND IMPELLER HAV E BEEN REMOVED AND SENT TO MANUFACTURER FOR INVESTIGATION. THIS EXCESSIVE WEAR HAS BEEN OBSERVED ON SEVERAL OF THE SAM E P/N ADAPTERS AFTER REMOVAL FROM ENGINES. 1 G 7 2 3U 3 U H11EU E4CE 2002070900002 20020709 00002 SO 2002 7 9 ASOA02330 1 20020615 A 3350 1317 LAMP EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 281AS 28860 120224 DURING GROUND INSPECTION, THE FORWARD MOST OVERWING EMERGENCY LIGHT ON THE RIGHT HAND SIDE OF THE FUSELAGE WAS INOPERATI VE. MAINTENANCE REMOVE AND REPLACED THE EXTERNAL EMERGENCY LIGHT BULB AND ALSO REMOVED AND REPLACED A FUSE. OPERATIONA L CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070900003 20020709 00003 SO 2002 7 9 ASOA02331 1 20020615 A 3350 3071BPE LAMP HONEYWELL EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 262AS 31806 120146 DURING A HANGER INSPECTION, THE EMERGENCY FLOOR LIGHTING WAS INOPERATIVE AT ROW 2. MAINTENANCE REMOVED AND REPLACED THE BURNT OUT EMERGENCY FLOOR LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070900004 20020709 00004 EA 2002 7 9 ASOA02333 1 20020615 A 5300 BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE SUPPORT BEAM CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 835AS 7258 DURING HANGER MAINTENANCE, CRACKS WERE FOUND ON THE ENGINE SUPPORT BEAM AT BL 36.20 ON BOTH SIDES. MAINTENANCE REPAIRED THE CRACKED ENGINE SUPPORT BEAM IAW REO. THIS REO GIVES REPAIR SPECIFICATIONS FOR THE ENGINE SUPPORT BEAM CRACK ON AIR CRAFT AS WELL AS OUTLINES A THRESHOLD OF CYCLES FOR THE PERMANENT REPAIR AND FOLLOW UP NDI INSPECTIONS. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070900005 20020709 00005 EA 2002 7 9 ASOA02334 1 20020616 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 828AS 7213 DURING GROUND INSPECTION, THE FORWARD MOST EXTERNAL EMERGENCY LIGHT ON THE LEFT SIDE OF THE FUSELAGE WAS INOPERATIVE. M AINTENANCE REMOVED AND REPLACED THE BURNT OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070900006 20020709 00006 EA 2002 7 9 ASOA02335 1 20020616 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 850AS 7355 DURING GROUND INSPECTION, WHEN SELECTED ON, THE EMERGENCY LIGHTS AT ROW 8 AND THE EXTERNAL OVERWING EXIT LIGHTS WOULD NO T STAY ON. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IN THE NR 3 POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070900007 20020709 00007 EA 2002 7 9 COMA0260399 1 20020706 A 5220 H341931 HANDLE CNDAIR CL601R CNDAIR CL600 CL6002B19 1900309 EA CREW ESCAPE HATC CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 821CA 3980 7421 7420 DURING A "C" CHECK INSPECTION, MECHANIC FOUND THAT THE OUTER HANDLE OF THE CREW ESCAPE HATCH WOULD NOT UNLOCK PROPERLY A LLOWING THE HANDLE TO EXTEND AND ROTATE.THE HANDLE WAS REMOVED FROM THE CREW ESCAPE HATCH AND WAS REPLACED WITH A SERVIC EABLE UNIT IN ACCORDANCE WITH CRJ STRUCTURE REPAIR MANUAL 51-42-06. 2 L 7 2 4F RT A21EA 2002070900008 20020709 00008 EA 2002 7 9 COMA0260400 1 20020707 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FS672-700 DAMAGED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 926CA 20383 7027 FUSE SKIN DAMAGED UNDER APU HEAT SHIELD @ F.S. 672 TO F.S. 700 BETWEEN STRINGERS 13R AND 15R.REMOVED DAMAGE, PERFORMED E DDY CURRENT INSP, INSTALLED FABRICATED DOUBLER AND SHIMS FABRICATED FROM 2024-T3.063 AND REINSTALLED HEAT SHIELD I/A/W W VAC E.O. 601R-53-3329B DATED 07/05/02. 2 L 7 2 4F RT A21EA 2002070900009 20020709 00009 EA 2002 7 9 ASOA02336 1 20020616 A 3350 6100945 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 823AS 7196 DURING GROUND INSPECTION, THE LEFT HAND SIDE OF THE CENTER EMERGENCY LIGHTED EXIT SIGN WAS INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070900010 20020709 00010 EA 2002 7 9 COMA0260401 1 20020701 A 5310 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS484.0 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 934CA 18550 7042 CRACKED ANGLES AND FLANGES FOUND @ F.S. 484.0 @ TOP CORNERS OF LBL-36, LBL-27, RBL-27, RBL-36.CRACKED ANGLES/FLANGES WER E REPLACED/REPAIRED WITH ANGLES FABRICATED FROM P/N S6144-4 I/A/W WVAC E.O. 601R-53-3308. 2 L 7 2 4F RT A21EA 2002070900011 20020709 00011 EA 2002 7 9 COMA0260402 1 20020630 A 5310 SKIN CNDAIR CL600 CL6002B19 1900309 EA FS 228.0 DAMAGED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 934CA 18550 7042 L/H FUSELAGE SKIN @ F.S. 228.0 HAS DAMAGED FASTENER HOLE FOR PNL 131 AL.REAMED HOLE TO .3465", FABRICATED FREEZE PLUG FR OM 7075-T6, INSTALLED FREEZE PLUG I/A/W WVAC E.O. 601R-53-3319. 2 L 7 2 4F RT A21EA 2002070900012 20020709 00012 EA 2002 7 9 COMA0260403 1 20020701 A 5551 BUSHING CNDAIR CL600 CL6002B19 1900309 EA VERTICAL STAB DAMAGED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 934CA 18550 7042 I/B HORIZONTAL TO VERTICAL ATTACH LUGS (ON HORIZONTAL) WERE FOUND TO BE OUT OF TOLERANCE (BUSING HOLES).BUSHING HOLES WE RE REAMED TO FIRST OVERSIZE, AND FIRST OVERSIZE BUSHINGS WERE INSTALLED. NEW BUSHINGS WERE THEN REAMED TO AN INTERNAL DI AMETER OF 1.50". ALL WORK WAS PERFORMED I/A/W BOMBARDIER REO 601R-55-11-022 REV A DATED 11 JUNE 97. REF MX LOG PG 429845 AND COMAIR W/O 37560 FOR DETAILS OF WORK PERFORMED. 2 L 7 2 4F RT A21EA 2002070900013 20020709 00013 EA 2002 7 9 ASOA02305 1 20020602 A 3350 100865 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 826AS 10894 7210 DURING HANGER INSPECTION, THE OVERHEAD LIGHTED EMERGENCY EXIT SIGN AT ROW 8 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070900014 20020709 00014 EA 2002 7 9 ASOA02307 1 20020603 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 863AS 7487 DURING SCHEDULED INSPECTION, THE AFT CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURN ED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002071600185 20020716 00185 NM 2002 7 16 F3LA200200188 1 20020704 A 5347 SEAT TRACK BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TWO SEAT TRACKS BETWEEN BS 947 AND BS 967, RBL 11.50. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 2002070900015 20020709 00015 EA 2002 7 9 COMA0260404 1 20020624 A 5551 600210617 BUSHING CNDAIR CL600 CL6002B19 1900309 EA R/H SIDE VERT ST DAMAGED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 934CA 7042 PIVOT BUSHING R/II VERT STAB REQUIRED REPLACEMENT P/N 600-21061-7REMOVED AND REPLACED BUSHING I/A/W WVAC E.O. 601R-55-33 11. 2 L 7 2 4F RT A21EA 2002070900016 20020709 00016 EA 2002 7 9 COMA0260405 1 20020701 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA WS 136.676 CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 934CA 18550 7042 L/H WING LOWER PLANK ACCESS HOLE 540FB HAS APPROX .008" DEEP CORROSION PIT ON FLAT HORIZONTAL SURFACE, FWD SIDE @ W.S. 1 36.676.BLENDED OUT DAMAGED AREA, PERFORMED NDI TO ENSURE COMPLETE DAMAGE REMOVAL, ROTO-PEENED REPAIR AREA AND APPLIED CO NVERSION COATING. WORK WAS PERFORMED I/A/W CANADAIR REO 601R-57-21-030 REV A DATED 06 NOV 98. REF MX LOG PG 429849 AND C OMAIR W/O 29956. 2 L 7 2 4F RT A21EA 2002072200057 20020722 00057 NM 2002 7 22 2002UALA00967 1 20020609 A 2612 896768 FIRE LOOP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE APU SHORTED A UALA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 WP 29 916UA 25383 AIRCRAFT HAD APU FIRE INDICATION ON FINAL APPROACH. INSPECTED APU OVERHEAT DETECTION SYSTEM AND FOUND APU TAILPIPE OVER HEAT DETECTOR LOOP SHORTED. ALL OTHER LOOPS CHECKED OK. REPLACED APU OVERHEAT DETECTOR LOOP. APU FIRE DETECTION SYSTE M WAS RESTORED TO NORMAL CONDITION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072300198 20020723 00198 NM 2002 7 23 2002UALA00999 1 20020612 A 7930 21SN04414 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 648UA 25285 NR 2 ENGINE BYPASS OIL LIGHT ILLUMINATED. FOUND OIL FILTER AND CHIP DETECTORS CLEAN. REPLACED OIL FILTER BYPASS SWITCH. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072400075 20020724 00075 EU 2002 7 24 2002UALA01035 1 20020618 A 2120 QB0639 FILTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E/E BAY COLLAPSED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 433UA 589 ABORTED TAKEOFF AT 90 KNOTS DUE TO VENT AVIONICS SYSTEM FAULT. THE AEVC SYSTEM FILTER WAS FOUND DIRTY AND COLLAPSED - RE PLACED FILTER. 2 L 7 2 4F 4 F RT A28NM E40NE 2002072400116 20020724 00116 NM 2002 7 24 2002UALA01069 1 20020621 A 5270 PROXIMITY SWITCH AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CARGO DOOR LOOSE A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 851UA 1664 RETURNED TO FIELD DUE TO A DOOR AFT CARGO ECAM WARNING. INSPECTED DOOR SENSOR AND TARGET, CHECKED SYSTEM THROUGH CFDS.C FDS FAULTED PROX SWITCH 32WV. FOUND PROX SWITCH LOOSE. CLEANED THE SWITCH AND SECURED. OPENED AND CLOSED DOOR SEVERA L TIMES, INDICATION NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2002070900017 20020709 00017 NM 2002 7 9 2002UALA01106 1 20020630 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 EXTERNAL FUSELAGE SKIN DENTED AT LOWER EDGE OF AFT CARGO PIT DOOR CUTOUT STATION 1427 SKIN LAYERS ALSO DISBONDED. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND TRIPLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002070900018 20020709 00018 NM 2002 7 9 2002UALA01112 1 20020701 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 STATION 338.5 DOOR 1L SURROUND STUB FRAME WL 278 HAS A GOUGE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. BLENDE D GOUGE, INSTALLED REPAIR ANGLE AND MODIFIED DOOR STOP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072900041 20020729 00041 NM 2002 7 29 2002UALA01117 1 20020702 A 5313 STRINGER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7455U 21909 FORWARD CARGO PIT AT BODY STATION 480, STRINGER 27L IS CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. STRINGER SPL ICE REPAIR. 2 L 7 3 4F 4 F A3WE E2EA 2002072900042 20020729 00042 NM 2002 7 29 2002UALA01118 1 20020702 A 5313 STRINGER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7455U 21909 FORWARD PIT STRINGER 27R CORRODED BEYOND LIMITS BODY STATION 630. MAJOR REPAIR ACCOMPLISHED. HAT SECTION REPAIR. 2 L 7 3 4F 4 F A3WE E2EA 2002072900048 20020729 00048 NM 2002 7 29 2002UALA01126 1 20020704 A 5310 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GROOVED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 DOOR 1L CUTOUT FORWARD FRAME 8-10 INCHES FROM TOP CORNER, I/B FLANGE HAD DEEP GROOVE WORN INTO IT. MAJOR REPAIR ACCOMPL ISHED. INSTALLED DOUBLER OVER FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2002070900019 20020709 00019 EA 2002 7 9 ASOA02069S 1 20020204 A 4950 361665014 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE COMPRESSOR WORN A ASOA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 11 857AS 7411 DURING THE INITIAL APPROACH, THE CAPTAIN RECEIVED A (SMOKE TOILET) INDICATION. THE FLIGHT ATTENDANT VERIFIED SMOKE IN T HE CABIN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. THE SMOKE HAD DISSIPATED AT TIME OF LANDING. THE TEAR DOWN REPORT OF THE APU FROM HONEYWELL STATES THAT THE COMPRESSOR SEAL WAS FOUND WORN CAUSING AN OILY ROTATING GROUP TO INFECT THE BLEED AIR WITH AN OIL SMELL. THIS COULD ALSO CAUSE SMOKE TO CIRCULATE THROUGHOUT THE CABIN. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070900020 20020709 00020 EA 2002 7 9 ASOA02309 1 20020603 A 5300 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 821AS 7194 DURING HANGER MAINTENANCE, A CRACK WAS DISCOVERED IN FRAME STATION 718 BETWEEN STRINGERS 10 AND 12 ON THE LEFT AND RIGH T SIDES. MAINTENANCE REPAIRED THE CRACKED FRAME IAW EO/REO. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070900021 20020709 00021 EA 2002 7 9 ASOA02310 1 20020604 A 5300 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE STA 718 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 839AS 7284 DURNG HANGER MAINTENANCE, A CRACK WAS DISCOVERED IN FRAME STATION 718 BETWEEN STRINGERS 10 AND 12 ON THE LEFT AND RIGHT SIDES. MAINTENANCE REPAIRED THE CRACKED FRAME IAW EO/REO/SRM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070900022 20020709 00022 EA 2002 7 9 COMA0260406 1 20020705 A 5311 601360012330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA F.S. 640 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 926CA 20384 7027 FUSELAGE FRAME AND AFT DOUBLER ARE CRACKED AT RIGHT HAND SIDE F.S. 640 BETWEEN W.L. 111 AND 119.REMOVED CRACKED SECTION OF FRAME AND AFT DOUBLER. INSTALLED NEW SECTION OF FRAME AND NEW AFT DOUBLER I/A/W CANADAIR REO 601R-53-61-487. 2 L 7 2 4F RT A21EA 2002070900023 20020709 00023 EA 2002 7 9 ASOA02311 1 20020604 A 5300 BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ENG SUPPT BEAM CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 839AS 9060 7284 DURING A HANGER INSPECTION, WHILE COMPLYING WITH EO, INSPECTION OF ENGINE SUPPORT BEAM CRACKS, A CRACK WAS DISCOVERED ON THE BEAM AT THE LEFT ACCESS PANEL FORWARD CORNER. MAINTENANCE REPAIRED THE CRACK IN THE ENGINE SUPPORT BEAM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070900024 20020709 00024 EA 2002 7 9 COMA0260407 1 20020707 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FS642-650 DENTED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 926CA 20384 7027 THE FUSELAGE SKIN IS DENTED AT FS 650 BETWEEN STRINGERS 20L AND 21L AND ANOTHER DENT AT APPROXIMATELY FS 642. TRIMMED O UT DAMAGED FUSELAGE SKIN. FABRICATED REPAIR DOUBLER FROM 2024-T3' AND INSTALLED I/A/W WVAC EO 601R-53-3330B. 2 L 7 2 4F RT A21EA 2002070900025 20020709 00025 EA 2002 7 9 ASOA02312 1 20020604 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FLOOD LT ASSY BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 8459 7300 DURING A SCHEDULED INSPECTION, THE AFT CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAIINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070900026 20020709 00026 SO 2002 7 9 ASOA02313 1 20020605 A 3350 AGC1 FUSE MS265721 EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 503AS 23490 120275 DURING A HANGER INSPECTION, THE FORWARD FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A FUS E. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070900027 20020709 00027 EA 2002 7 9 COMA0260408 1 20020707 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FS 605-621 DENTED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 926CA 20384 7027 THE FUSELAGE SKIN IS DENTED BETWEEN FS 605 AND FS621 BETWEEN STRINGERS 22L AND 23L. TRIMMED OUT DAMAGED FUSELAGE SKIN. FRABRICATED REPAIR DOUBLER FROM 2024-T3.063" AND INSTALLED I/A/W WVAC EO 601R-53-3328A. 2 L 7 2 4F RT A21EA 2002070900028 20020709 00028 EA 2002 7 9 COMA0260409 1 20020707 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FS 589-604 DENTED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 THE FUSELAGE SKIN HAS MULTIPLE DENTS BETWEEN FS 589 AND FS 604 BETWEEN STRINGERS 22 AND 23 LHS.REMOVED DAMAGED EXISTING REPAIR DOUBLER, FABRICATED NEW REPAIR DOUBLER FROM 2024-T3.63" AND INSTALLED I/A/W WVAC EO 601R-53-3331A. 2 L 7 2 4F RT A21EA 2002070900029 20020709 00029 EU 2002 7 9 ASOA02314 1 20020605 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 637AS 20299 535 383 DURING A HANGER INSPECTION, THE EMERGENCY LIGHT ON THE PASSENGER DOOR STEPS, SECOND STEP FROM THE BOTTOM, WAS INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE BURNT OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERV ICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2002070900030 20020709 00030 SO 2002 7 9 ASOA02294 1 20020525 A 3350 AGC1 FUSE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 237AS 37090 120051 DURING GROUND INSPECTION, THE LOWER EXTERNAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN FUS E GOING TO THE POWER SUPPLY FOR THE EXTERNAL EMERGENCY LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002080700045 20020807 00045 WP 2002 8 7 ARWA20020703 1 20020705 A 3242 26014122 BRAKE ASSY DOUG DC8 DC863 302198A WP LT MLG FIRE A ARWA F ACTIVATE FIRE EXT. A FLAME/FIRE IN INSP/MAINT 1 SO 19 345JW 46042 NR 1 MAIN BRAKE FIRE EXTINGUISHED WITH CO2 SMALL FIRE 15 SECOND DURATION A/C BRAKES WERE SLIGHTLY USED ON LANDING ROLL. REMOVED AND REPLACED NR 1 BRAKE ASSY IAW MM 32-42-1, ALSO REMOVED AND REPLACED NR 1 MAIN WHEEL ASSY IAW MM 32-40-1. AC COMPLISHED VISUAL INSPECTION OF LT GEAR AXLE NO DISCREPANCIES OR TRACE OF FIRE FOUND. REPLACED CO2 FIRE EXTINGUISHER BO TTLE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002070900031 20020709 00031 EA 2002 7 9 ASOA02295 1 20020525 A 5300 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 832AS 7243 DURING HANGER MAINTENANCE, A CRACK WAS FOUND TO FUSELAGE FRAME FS718.00 BETWEEN STRINGERS 10 AND 12. MAINTENANCE REPAIR ED THE CRACKED FRAME IAW EA/REO. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070900032 20020709 00032 SO 2002 7 9 ASOA02296 1 20020526 A 3350 AGC1 FUSE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 240AS 120060 DURING GROUND INSPECTION, BOTH AFT MOST EXTERNAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E AFT EMERGENCY LIGHT FUSE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070900033 20020709 00033 SO 2002 7 9 ASOA02297 1 20020526 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 263AS 24503 120157 DURING GROUND INSPECTION, ALL OF THE EXTERNAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE EMERGENCY LIGHTING BATTERY PACK IN THE NR 1 POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070900034 20020709 00034 EA 2002 7 9 ASOA02298 1 20020526 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 869AS 3308 7479 DURING A HANGER INSPECTION, THE CEILING EMERGENCY LIGHTING AT ROW 5 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED A BURNED OUT EMERGENCY LIGHT BULB AT ROW 5. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070900035 20020709 00035 EA 2002 7 9 ASOA02320 1 20020609 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 824AS 7203 DURING GROUND INSPECTION, AN EXTERNAL EMERGENCY LIGHT ON THE RIGHT HAND SIDE OF THE FUSELAGE WAS INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002071600186 20020716 00186 NM 2002 7 16 F3LA200200189 1 20020701 A 5320 FLOOR SUPPORT BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED SURFACE CORROSION ON FLOOR SUPPORT BETWEEN BS 947 AND BS 967, FROM RBL 11.50 TO RB L 36.50. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 51-30-02 AND EA 53-737-173. 2 L 7 2 4F RT A16WE 2002070900036 20020709 00036 SO 2002 7 9 ASOA02317 1 20020608 A 5280 12016085001 STRINGER EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LEFT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 501AS 120273 DURING HANGER MAINTENANCE, STRINGER NR 10 WAS FOUND CRACKED AT THE RIVET HOLE AROUND THE INBOARD FUEL PANEL, INBOARD OF THE LEFT NACELLE. MAINTENANCE REPAIRED THE CRACKED STRINGER IAW SRM. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070900037 20020709 00037 EU 2002 7 9 ASOA02319 1 20020609 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 20246 375 DURING HANGER INSPECTION, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BURNT OUT LIGHT BULB ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2002070900038 20020709 00038 EA 2002 7 9 ASOA02156S 1 20020221 A 5300 BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ENG SUPPT BEAM CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 821AS 7194 DURING (C) CHECK INSPECTION, WHILE COMPLYING WITH EO, VISUAL INSPECTION OF THE ENGINE SUPPORT BEAMS, BOTH SIDES WERE FOU ND TO HAVE A CRACK. MAINTENANCE COMPLIED WITH EO TO SERVICE AS THE PERMANENT REPAIR FOR THE ENGINE SUPPORT BEAM CRACK. 2 L 7 2 4F 4 F RT A21EA E15NE 2002070900039 20020709 00039 SO 2002 7 9 ASOA02301 1 20020527 A 5300 12006962001 CROSSBEAM EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE OB, IB CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 257AS 120126 DURING (C) CHECK INSPECTION, CORROSION WAS DISCOVERED ON THE LEFT HAND INBOARD AND OUTBOARD CROSS BEAMS AT FRAME 16. MA INTENANCE REMOVED AND REPLACED THE TWO CORRODED LEFT HAND CROSS BEAMS IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070900040 20020709 00040 SO 2002 7 9 ASOA02302 1 20020527 A 5300 CROSSBEAM EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 257AS 120126 DURING (C) CHECK INSPECTION, CORROSION WAS FOUND ON TOP OF THE LEFT HAND CROSSBEAM AT FRAME 28. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002080500116 20020805 00116 CE 2002 8 5 GBLA2002103 1 20020706 A 7714 TACH GENERATOR BEECH 1900 1900D 1154162 CE LT ENGINE FAULTY A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 255GL UE255 LEFT HAND PROP DROPPED TO ZERO. REMOVED AND REPLACED LEFT HAND TACH GENERATOR. 2 L 7 2 4T RT A24CE 2002070900041 20020709 00041 SO 2002 7 9 ASOA02304 1 20020527 A 5300 12046963001 BUTT STRAP EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 257AS 120126 DURING (C) CHECK INSPECTION, THE LEFT BUTT STRAP, BETWEEN FRAMES 14 AND 21, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAI NTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002070900042 20020709 00042 EU 2002 7 9 SIMA200216514 1 20020613 A 5300 SILL AEROSP ATR42 ATR42300 8680920 EU SILL PLATE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 DURING CPCP 2 INSPECTION FOUND SERVICE DOOR SILL PLATE CORRODED. 2 H 7 2 4T RT A53EU 2002070900043 20020709 00043 CE 2002 7 9 GLBA2002103 1 20020706 A 7714 TACH GENERATOR BEECH 1900 1900D 1154162 CE LT ENGINE FAILED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 255GL UE255 LEFT HAND PROP DROPPED TO ZERO / R&R LEFT HAND TACH GENERATOR 2 L 7 2 4T RT A24CE 2002070900044 20020709 00044 EU 2002 7 9 SIMA200216513 1 20020613 A 5300 PAN AEROSP ATR42 ATR42300 8680920 EU SERV DOOR PAN CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 DURING MBV INSPECTION FOUND LOWER CORNER OF SERVICE DOOR PAN CRACKED. 2 H 7 2 4T RT A53EU 2002070900045 20020709 00045 EU 2002 7 9 SIMA200216512 1 20020613 A 5300 SEAT SPRING AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 DURING CPCP2 INSPECTION FOUND AFT CARGO WALL AND LEFT MIDDLE INBOARD SEAT TRACKS TO BE CORRODED. 2 H 7 2 4T RT A53EU 2002070900046 20020709 00046 EU 2002 7 9 SIMA200216515 1 20020613 A 5300 FRAME AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 DURING CPCP 2 INSP FOUND FRAME 37R CORRODED AT FLOOR LEVEL. 2 H 7 2 4T RT A53EU 2002070900047 20020709 00047 NM 2002 7 9 SABA020070 1 20020707 A 3350 6104789 BATTERY DHAV DHC8 DHC8103 1386005 NM A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 801WP 086 Flight 5047 from CLT to TLH : During pre-flight in Clt, pilot reported the ceiling emergency light would not test at row seven. Maintenance removed and replaced the number three battery at row three. System ops checked good and Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002080500057 20020805 00057 NM 2002 8 5 751PA0001 1 20020704 A 2560 FLASHLIGHT BOEING 757 757200 1384950 NM CABIN INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 751PA 23928 R3 EMERGENCY FLASHLIGHT INOP. ITEM DEFERRED IAW MEL 25-63-4 CONT 0704003. 2 L 7 2 4F RT A2NM 2002071000001 20020710 00001 2002 7 10 251TR0001 4 20020707 A 2210 AUTOPILOT SYS BOEING 737 737228 13844AG NM A PIDA K NONE O OTHER UK UNKNOWN 1 SO 05 251TR 23792 Auto pilot V/S mode reverts to LVL change mode uncommanded. Deferred per MEL 22-15-8 CTL #0707002 CATC 2 L 7 2 4F RT A16WE 2002071000002 20020710 00002 GL 2002 7 10 HEEA079880 2 20020603 A 7250 23053299 TURBINE WHEEL BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 408PH 1552 53228 CAE847427 ENGINE REMOVED DUE TO VIBRATION AND MAKING LOUD NOISE. UPON INSPECTION OF TURBINE PARTS NOTED SULFIDATION ON NR 1 WHEEL LEADING EDGE BLADES. SCRAPPED PART. 1 G 7 1 3U 3 U O H2SW E1GL 2002071000003 20020710 00003 2002 7 10 920WA 4 20020708 A 2230 AUTOTHRUST SYS BOEING 737 737236 1384476 NM A PIDA K NONE O OTHER UK UNKNOWN 1 SO 05 920WA 21791 A/T disengages when throttles are advanced. Transferred to MEL log control #0709003 MEL 22-4. 2 L 7 2 4F RT A16WE 2002071000004 20020710 00004 2002 7 10 920WA0004 4 20020708 A 2230 AUTOTHRUST SYS BOEING 737 737236 1384476 NM A PIDA K NONE O OTHER UK UNKNOWN 1 SO 05 920WA 21791 A/T disengages when throttles are advanced. Transferred to MEL log control #0709003 MEL 22-4. 2 L 7 2 4F RT A16WE 2002071000005 20020710 00005 GL 2002 7 10 HEEA079881 2 20020603 A 7250 23053299 TURBINE WHEEL BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 740PH 729 53435 CAE847473 ENGINE REMOVED DUE TO NR 1 WHEEL DAMAGED. UPON INSPECTION OF TURBINE PARTS NOTED SULFIDATION ON NR 1 WHEEL LEADING EDGE BLADES. SCRAPPED PART. 1 G 7 1 3U 3 U O H2SW E1GL 2002071000006 20020710 00006 GL 2002 7 10 HEEA079882 2 20020607 A 7260 6899402 GEAR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL PTO WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 133AE 633 S800 CAE835247 ENGINE REMOVED DUE TO RECURRING CHIP LIGHTS. HEAVY STEP WEAR ON GEAR TEETH CAUSING PROBLEM IN EXCESS FOR NORMAL WEAR. R EQUEST CREDIT REIMBURSEMENT ON AFA#63953A. 1 G 7 2 3U 3 U H3EU E4CE 2002071000007 20020710 00007 GL 2002 7 10 HEEA079883 2 20020607 A 7260 23035299 GEAR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL GEARBOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 133AE 633 S800 CAE835247 ENGINE REMOVED DUE TO RECURRING CHIP LIGHTS. HEAVY STEP WEAR ON GEARTEETH CAUSING PROBLEM IN EXCESS FOR NORMAL WEAR. 1 G 7 2 3U 3 U H3EU E4CE 2002071000008 20020710 00008 2002 7 10 HEEA079884 4 20020607 A 2312 064100900 TRANSCEIVER SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 4253S 760035 GARBLED. COULD NOT DUPLICATE PROBLEM. ADJUSTED MODULATION, TX COMPRESSOR AND SIDETONE. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002071000009 20020710 00009 EU 2002 7 10 HEEA079885 1 20020611 A 2612 0301037070 HARNESS SNIAS 350 AS350B 8680801 EU PYROMETRIC BROKEN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 856PH 3352 WELDS AT PROBES BROKEN. 1 G 7 1 3U H9EU 2002071000010 20020710 00010 SO 2002 7 10 SIMA200216307 1 20020528 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 THIS IS A LEVEL 2 FINDING ON CRIC NR 36201. GALLEY FORWARD DIAMOND GUSSET HAS CORROSION INSTALLED SERVICEABLE DIAMOND G USSET IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002071000011 20020710 00011 NM 2002 7 10 2002F00726 1 20020603 A 5347 SEAT TRACK BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND SEAT TRACK CORRODED AT STATION 870, RBL 48. (M) 2 L 7 3 4F A3WE 2002071000012 20020710 00012 NM 2002 7 10 2002F00728 1 20020531 A 5712 65162629953 RIB BOEING 727 727222 1384073 NM RT WING CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND RIGHT WING TIP RIB CRACKED AT WBL 62.5. (M) 2 L 7 3 4F A3WE 2002071000013 20020710 00013 NM 2002 7 10 2002F00729 1 20020530 A 3211 TRUNNION BOEING 727 727222 1384073 NM LT MLG CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND LEFT MAIN LANDING GEAR TRUNNION ATTACH FITTING WITH CORROSION AND GOUGES IN SPOT FACE AREAS. (M) 2 L 7 3 4F A3WE 2002071000014 20020710 00014 NM 2002 7 10 2002F00730 1 20020529 A 5320 WEB BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CRACK IN AFT CARGO COMPARTMENT WEB, AT STATION 1030 TO 1050, STRINGER 26L. (M) 2 L 7 3 4F A3WE 2002071000015 20020710 00015 NM 2002 7 10 2002F00731 1 20020529 A 5320 FLOOR SUPPORT BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND BOTTOM SIDE OF FLOOR SUPPORT CRACKED AT CABIN STATION 846, BL 0.0. (M) 2 L 7 3 4F A3WE 2002071000016 20020710 00016 NM 2002 7 10 2002F00732 1 20020527 A 2550 PANEL BOEING 727 727222 1384073 NM CARGO BAY CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION IN FORWARD CARGO COMPARTMENT TRANSITION PANEL, AT STATION 480 TO 630A, RBL 20 TO 26. (M) 2 L 7 3 4F A3WE 2002071000017 20020710 00017 NM 2002 7 10 2002F00733 1 20020601 A 5753 STRUCTURE BOEING 727 727222 1384073 NM T/E FLAP CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND FLAP JOINT CORRODED AROUND RIVETS, AT STATION 480, STRINGER 26L. (M) 2 L 7 3 4F A3WE 2002071000018 20020710 00018 NM 2002 7 10 2002F00734 1 20020531 A 5714 FITTING BOEING 727 727222 1384073 NM CENTER WING BOX CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CENTER WING FUEL TANK FRONT SPAR UPPER FITTING CRACKED, AT STATION 740, LBL 45. (M) 2 L 7 3 4F A3WE 2002071000019 20020710 00019 NM 2002 7 10 2002F00735 1 20020531 A 5714 FITTING BOEING 727 727222 1384073 NM CENTER WING BOX CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND UPPER T-FITTING CRACKED, ON CENTER WING FUEL TANK FRONT SPAR, STATION 760, LBL 25. (M) 2 L 7 3 4F A3WE 2002071000020 20020710 00020 2002 7 10 HEEA079886 4 20020611 A 3442 MI5851345 DISPLAY SKRSKY S76 S76A 8143006 NE RADAR SYS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 911MJ 760231 RADAR INDICATOR DISPLAY IS DIM AT MAXIMUM INTENSITY. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H1NE 2002071000021 20020710 00021 NM 2002 7 10 2002F00736 1 20020531 A 1430 RIVET BOEING 727 727222 1384073 NM ELEVATOR MISSING A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND LEFT ELEVATOR TRAILING EDGE WITH LOOSE AND MISSING RIVETS, AT STATION 125. (M) 2 L 7 3 4F A3WE 2002071000022 20020710 00022 NM 2002 7 10 2002F00737 1 20020531 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION AT CABIN FLOORBEAM, AT STATION 1110.0, BL 0 TO LBL 60. (M) 2 L 7 3 4F A3WE 2002071000023 20020710 00023 GL 2002 7 10 HEEA079888 2 20020611 A 7250 6886407 TURBINE WHEEL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136H 1736 S833 CAE833901 ENGINE REMOVED DUE TO 1750 HOUR INSPECTION. UPON INSPECTION OF TURBINE PARTS NOTED SULFIDATION ON 1ST STAGE WHEEL BLADE S. SCRAPPED. 1 G 7 2 3U 3 U H3EU E4CE 2002071000024 20020710 00024 NM 2002 7 10 2002F00738 1 20020529 A 5320 ANGLE BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND AFT PIT ATTACH ANGLE WITH EXFOLIATION AT STATION 1183, STRINGER 18R. (M) 2 L 7 3 4F A3WE 2002071000025 20020710 00025 GL 2002 7 10 HEEA079889 2 20020611 A 7250 23053299 TURBINE WHEEL SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122G 592 760232 CAE890616S ENGINE WAS REMOVED DUE TO VIBRATION AND SULFIDATION OF TURBINE WHEELS. UPON INSPECTION OF TURBINE PARTS NOTED 25 PERCEN T OF THE 1ST STAGE WHEEL BLADE TIPS MISSING DUE TO SULFIDATION. SCRAPPED. 1 G 7 2 3U 3 U H1NE E1GL 2002071000026 20020710 00026 NM 2002 7 10 2002F00739 1 20020529 A 5311 FRAME BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, THE FORWARD CARGO COMPARTMENT LOWER LOBE FRAME HAS A THREE INCH CRACK AT STATION 500, RBL 50. (M) 2 L 7 3 4F A3WE 2002071000027 20020710 00027 NM 2002 7 10 2002F00740 1 20020529 A 5320 ANGLE BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND SUPPORT ANGLE FOR THE FLOORBEAM HAS A .5 INCH CRACK AT STATION 820, LBL 48. (M) 2 L 7 3 4F A3WE 2002071000028 20020710 00028 NM 2002 7 10 2002F00741 1 20020529 A 5320 FLOOR SUPPORT BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CARGO FLOOR SUPPORT CORRODED IN AFT CARGO COMPARTMENT, AT STATION 1035, RBL 2. (M) 2 L 7 3 4F A3WE 2002071000029 20020710 00029 NM 2002 7 10 2002F00742 1 20020528 A 5320 FLOOR SUPPORT BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND FLOOR SUPPORTS WITH CORROSION, AT STATION 520 TO 590, RBL 2-7. (M) 2 L 7 3 4F A3WE 2002071000030 20020710 00030 NM 2002 7 10 2002F00743 1 20020528 A 5512 SKIN BOEING 727 727222 1384073 NM HORIZ STAB DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER WITH DENT BEYOND LIMITS, AT STABILIZER STATION 20. (M) 2 L 7 3 4F A3WE 2002071000031 20020710 00031 NM 2002 7 10 2002F00744 1 20020528 A 5522 SKIN BOEING 727 727222 1384073 NM ELEVATOR DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND LEFT ELEVATOR LEADING EDGE SKIN CREASED, AT ELEVATOR STATION 188. (M) 2 L 7 3 4F A3WE 2002071000032 20020710 00032 SO 2002 7 10 SIMA200216305 1 20020528 A 5100 14529150001 CROSSBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FR 23, GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 THIS IS A LEVEL 2 FINDING ON CRIC NR 36200. GALLEY CROSSBEAM AND PROFILE HAS CORROSION AT FRAME 23. C/A- INSTALLED NEW CROSSBEAM AND PROFILE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002071000033 20020710 00033 NM 2002 7 10 2002F00745 1 20020528 A 5320 FLOOR SUPPORT BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND FLOOR SUPPORTS WITH CORROSION, AT STATION 520 TO 590, RBL 2-7. (M) 2 L 7 3 4F A3WE 2002071000034 20020710 00034 NM 2002 7 10 2002F00746 1 20020527 A 5720 WEB BOEING 727 727222 1384073 NM LT WING CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND LEFT FUEL TANK INTERIOR WEB CRACKED, BELOW RIB STATION 436.5. (M) 2 L 7 3 4F A3WE 2002071000035 20020710 00035 GL 2002 7 10 HEEA079890 2 20020611 A 7314 6899001E FUEL NOZZLE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C47B GL ENGINE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 199CH 1562 760261 FUEL NOZZLE FAILED BENCH CHECK. 1 G 7 2 3U 3 U H1NE E1GL 2002071000036 20020710 00036 WP 2002 7 10 2002F00645 1 20020514 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON SHEAR TIE AND J FRAME, BETWEEN STRINGERS 51R AND 51L, AT STATION 1701. 2 L 7 3 4F A22WE 2002071000037 20020710 00037 WP 2002 7 10 2002F00646 1 20020513 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY FLOORBEAM, AT STATION 1841 ON CENTER SEGMENT OF ANGLE, ALSO CORRODED ON LOW ER SURFACE. (M) 2 L 7 3 4F A22WE 2002071000038 20020710 00038 NM 2002 7 10 C7WA200200003 1 20020703 A 8012 20211342 START VALVE BOEING 727 727231 1384079 NM PWA JT8 JT8D219 52053 NE NR 3 ENGINE STUCK A C7WA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SO 17 24343 21630 726187 NR 3 ENGINE BLEED TRIP OCCURED ON CLIMB OUT WITH CLIMB POWER. STABILIZED IT WITH SWITCHING THE BLEED. LATER NR 3 ENGIN E FIRE IND ILLUMINATED. RETARDED NR 3 THROTTLE, LIGHT WENT OUT. FLIGHT CONTINUED WITHOUT INCIDENT. MAINTENANCE FOUND NR 3 START VALVE STUCK OPEN. REMOVED AND REPLACED NR 3 START VALVE AND OPERATIONAL CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E9NE 2002071000039 20020710 00039 WP 2002 7 10 2002F00647 1 20020513 A 5230 FITTING DOUG DC10 DC1010 3022110 WP CARGO DOOR CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY DOOR, AFT DOOR SILL DRAIN FITTING ATTACH AREA AT STATION 1841.1, AS VIEWED FROM INBOARD SIDE THROUGH LIGHTNING HOLE. (M) 2 L 7 3 4F A22WE 2002071000040 20020710 00040 WP 2002 7 10 2002F00648 1 20020513 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STATION 440 LBL 10. (M) 2 L 7 3 4F A22WE 2002071000041 20020710 00041 NM 2002 7 10 2002F00649 1 20020511 A 5310 AE234011 DOOR FRAME BOEING 727 727225 1384077 NM FUSELAGE GOUGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND MAIN CARGO COMPARTMENT DOOR CUTOUT, UPPER AFT SCUFF PLATE GOUGED AND HAS A HOLE, AT STATION 700. (M) 2 L 7 3 4F A3WE 2002071000042 20020710 00042 NM 2002 7 10 2002F00650 1 20020511 A 5523 65C2638427A TRIM TAB BOEING 737 737* NM ELEVATOR CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 EIBXI 25052 DURING ELEVATOR TAB HINGE INSPECTION, FOUND .3125 INCH CRACK ON LEFT ELEVATOR TRIM TAB ON TOP SIDE BY NUMBER TWO HINGE. REMOVED AND REPLACED ELEVATOR TRIM TAB. (M) 2 L 7 2 4F RT A16WE 2002071000043 20020710 00043 WP 2002 7 10 2002F00651 1 20020511 A 5320 INTERCOSTAL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON LOWER SURFACE OF INTERCOSTAL IN AFT CARGO BAY AT STATION 1787, FOURTEEN INCHES UP FROM LO NGERON 48R AND LONGERON 45R. (M) 2 L 7 3 4F A22WE 2002071000044 20020710 00044 WP 2002 7 10 2002F00652 1 20020511 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT, IN RIGHT SLIDING DOOR TRACK U-CHANNEL AND ATTACH CLIPS, TOP AND BOTTOM SIDES, AT STATION 873, ABOVE STRINGER 44R. (M) 2 L 7 3 4F A22WE 2002071000045 20020710 00045 WP 2002 7 10 2002F00653 1 20020511 A 5320 TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN FORWARD CARGO COMPARTMENT GALLEY SLIDING DOOR BASE GUIDE RAIL TRACK. LOCATED AT FLOOR LE VEL AND PARTIALLY UP LEFT SIDEWALL AT STATION 879, BETWEEN 23 AND 65 INCHES LEFT OF CENTER. (M) 2 L 7 3 4F A22WE 2002071000046 20020710 00046 WP 2002 7 10 2002F00654 1 20020511 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION AT THE INTERFACE OF THE FRAME/LONGERON, IN THE AFT CARGO BAY, STATION 1781 LONGERON 46R. (M ) 2 L 7 3 4F A22WE 2002071000047 20020710 00047 2002 7 10 RAIA00207201 4 20020701 A 3417 7000700967 ADC JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 561HK 13008 1240 41077 5484-STL- CAPT ALTIMETER OFF FLAG ON DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE #1 AIR DATA COMPUTER, OPS CK OK. 2 L 7 2 4T RT A41NM 2002071000048 20020710 00048 2002 7 10 RAIA00207202 4 20020702 A 3417 7000700967 ADI JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK G MULTIPLE FAILURE TX TAXI/GRND HDL 1 CE 03 561HK 13351 0 41077 5482-STL- PILOT REPORTED ALTIMETER AND AIR SPEED INDICATORS MALFUNCTIONING. MAINTENANCE REMOVED AND REPLACED #1 ADC, OPS CK OK. 2 L 7 2 4T RT A41NM 2002071000049 20020710 00049 EU 2002 7 10 RAIA00207203 1 20020702 A 5220 MS21523LL CLEVIS AEROSP ATR42 ATR42300 8680920 EU A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 424TE 124 5450-STL- TYPE 3 EMERGENCY EXIT FELL INTO THE CABIN. MAINTENANCE REMOVED AND REPLACED DOOR LATCH CLEVIS AND ADJUSTED DOO R LATCH MECHANISM, OPS CK OK. 2 H 7 2 4T RT A53EU 2002071000050 20020710 00050 EU 2002 7 10 RAIA00207204 1 20020702 A 3350 3011210 LIGHT AEROSP ATR72 ATR72202 8680940 EU A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 723TE 283 MX-STL- PAX DOOR EMERGENCY EXIT LIGHT INOP. REMOVE AND REPLACE LIGHT ASSEMBLY, OPS CK OK. 2 H 7 2 4T RT A53EU 2002071000051 20020710 00051 WP 2002 7 10 2002F00655 1 20020510 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND FORWARD SIDE OF SHEAR TIE CORRODED AT STATION 1119, BETWEEN LONGERONS 50L AND 49L, AT CENTER ACCESSORY COMPARTMENT. (M) 2 L 7 3 4F A22WE 2002071000052 20020710 00052 NM 2002 7 10 2002F00656 1 20020510 A 5310 DOOR FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CRACK IN AFT PIT, AT RIGHT SIDE CLOSE OUT WEB, FORWARD SIDE OF CARGO DOOR CUTOUT, STATION 950E. (M) 2 L 7 3 4F A3WE 2002071000053 20020710 00053 NM 2002 7 10 2002F00657 1 20020510 A 5754 65162252 FLAP BOEING 727 727225 1384077 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND RIGHT WING NUMBER FOUR LEADING EDGE FLAP CORRODED ON INBOARD UPPER CORNER. (M) 2 L 7 3 4F A3WE 2002071000054 20020710 00054 WP 2002 7 10 2002F00658 1 20020510 A 5320 CHANNEL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND J-CHANNEL CORRODED AT STATION 1119, BETWEEN LONGERONS 51R AND 51L AT CENTER ACCESSORY COMPARTMENT. (M ) 2 L 7 3 4F A22WE 2002071000055 20020710 00055 WP 2002 7 10 2002F00659 1 20020510 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FORWARD SIDE OF SHEAR TIE, BETWEEN LONGERONS 51L AND 52L AT STATION 1113, CENTER ACCESSOR Y COMPARTMENT. (M) 2 L 7 3 4F A22WE 2002071000056 20020710 00056 WP 2002 7 10 2002F00660 1 20020510 A 5320 TIE CLIP DOUG DC10 DC1010 3022110 WP FS 1821 CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FORWARD SIDE OF TIE CLIP IN AFT CARGO BAY, AT FRAME STATION 1821, BETWEEN LONGERON 48L AN D 47L, AND LONGERON 50L AND 51L. (M) 2 L 7 3 4F A22WE 2002071000057 20020710 00057 WP 2002 7 10 2002F00661 1 20020510 A 5320 ATTACH ANGLE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON FRAME TO LONGERON ATTACH ANGLE IN AFT CARGO BAY, STATION 1801 LONGERON 50L TO LONGERON 42 R. (M) 2 L 7 3 4F A22WE 2002071000058 20020710 00058 WP 2002 7 10 2002F00662 1 20020510 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON LONGERON 41R IN AFT CARGO BAY, FROM STATION 1787 TO 1801. (M) 2 L 7 3 4F A22WE 2002071000060 20020710 00060 2002 7 10 2002F00663 4 20020510 A 2230 MOUNT BRACKET DOUG DC10 DC1010 3022110 WP AUTOTHROTTLE SYS CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON OUTER SIDE OF AUTO THROTTLE CLUTCH ASSEMBLY MOUNT BRACKET, IN FORWARD E/E BAY. (M) 2 L 7 3 4F A22WE 2002071000061 20020710 00061 WP 2002 7 10 2002F00664 1 20020510 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION AT STATION 1787 TO 1801 STRINGER 43L, ALONG WITH LEVELING COMPOUND THAT NEEDS REPLACED DUE T O NOT ADHERING TO STRUCTURE. (M) 2 L 7 3 4F A22WE 2002071000063 20020710 00063 EU 2002 7 10 SIMA200215107 1 20020523 A 5300 ALCLAD2024T3 DOUBLER SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 DURING MBV INSPECTION NO SUBSTANTIATING DOCUMENTATION COULD BE FOUND FOR DOUBLER REPAIR ON LEFT AFT FUSELAGE AFT OF STAT IC PORT. REMOVED PREVIOUS INSTALLED REPAIR DOUBLER. PERFORMED NDT INSPECTION, NO DEFECTS NOTED. FAB REPAIR DOUBLER, I NSTALLED IAW SRM AND STANDARD SRM PRACTICES. 2 L 7 2 4T 4 U RT A52EU E8NE 2002071000064 20020710 00064 WP 2002 7 10 2002F00665 1 20020510 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY, ON RIGHT FLOOR TO SLOPED SIDEWALL SUPPORT ANGLE. (M) 2 L 7 3 4F A22WE 2002071000065 20020710 00065 WP 2002 7 10 2002F00666 1 20020510 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAEG CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON LONGERON 46R IN AFT CARGO BAY, AFT OF FRAME AT STATION 1801. (M) 2 L 7 3 4F A22WE 2002071000066 20020710 00066 WP 2002 7 10 2002F00667 1 20020509 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN BILGE ON SHEAR TIE AT STATION 1681, BETWEEN STRINGERS 47R AND 48R. (M) 2 L 7 3 4F A22WE 2002071000067 20020710 00067 WP 2002 7 10 2002F00668 1 20020509 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN BILGE ON THE SHEAR TIE AND THE FLASHER STROBE DOUBLER, BETWEEN STATION 1661 AND 1681, AND BETWEEN STRINGERS 51R AND 52R. (M) 2 L 7 3 4F A22WE 2002071000068 20020710 00068 WP 2002 7 10 2002F00669 1 20020509 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON SHEAR TIE IN LOWER BILGE AT STATION 1641, BETWEEN STRINGER 47R AND 48R. (M) 2 L 7 3 4F A22WE 2002071000069 20020710 00069 WP 2002 7 10 2002F00670 1 20020509 A 5320 SILL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY DOOR SILL, AND CARGO TIE DOWN TRACK DRAIN SYSTEM TUBING. FOUND FOUR SEGMEN TS PERFORATED DUE TO CORROSION. (M) 2 L 7 3 4F A22WE 2002071000070 20020710 00070 WP 2002 7 10 2002F00671 1 20020509 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION AT FORWARD CARGO DOOR FUSELAGE CUTOUT, AFT LOWER CORNER, INNER RADIUS WEB, AND INNER SKIN, A T STATION 999. (M) 2 L 7 3 4F A22WE 2002071000071 20020710 00071 WP 2002 7 10 2002F00672 1 20020509 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON SHEAR TIE AT STATION 1661, BETWEEN STRINGERS 51R AND 52R. (M) 2 L 7 3 4F A22WE 2002071000072 20020710 00072 NM 2002 7 10 2002F00673 1 20020508 A 5320 CLIP BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND AFT CLIP CRACKED AT RIGHT FORWARD LAVATORY FLOORBEAM UPPER CHORD, AT STATION 312 RBL 31. (M) 2 L 7 3 4F A3WE 2002071000073 20020710 00073 NM 2002 7 10 2002F00674 1 20020508 A 5320 CLIP BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND AFT CLIP CRACKED AT RIGHT FORWARD LAVATORY FLOORBEAM UPPER CHORD. AT STATION 312, RBL 31. (M) 2 L 7 3 4F A3WE 2002071000074 20020710 00074 WP 2002 7 10 2002F00675 1 20020508 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON SHEAR TIES AT STATION 1561, STRINGERS 47R, 48R, 49R, 51R, AND 52R. (M) 2 L 7 3 4F A22WE 2002071000075 20020710 00075 WP 2002 7 10 2002F00676 1 20020509 A 5320 STIFFENER DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON VERTICAL BULKHEAD BEAM FUSELAGE FRAME INTERFACE, IN AFT CARGO BAY, STATION 1787 LONGERON 48L. (M) 2 L 7 3 4F A22WE 2002071000076 20020710 00076 NM 2002 7 10 2002F00677 1 20020430 A 5754 SKIN BOEING 727 727225 1384077 NM L/E SLAT DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND NR 5 SLAT OUTER SKIN UPPER SURFACE DENTED AT STATION 380R. (M) 2 L 7 3 4F A3WE 2002071000077 20020710 00077 NM 2002 7 10 2002F00678 1 20020429 A 5312 BULKHEAD BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND THE NOSE WHEEL WELL AFT PRESSURE BULKHEAD WITH CORROSION BULGES, AT LEFT SIDE OF DRAG BRACE FITTING, S TATION 351 LBL 6 AND LBL 10. (M) 2 L 7 3 4F A3WE 2002071000078 20020710 00078 NM 2002 7 10 2002F00679 1 20020427 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND 1 AND .5 INCH CRACK AT RIGHT FORWARD FLOORBEAM UPPER CHORD, AT STATION 312 RBL 13. (M) 2 L 7 3 4F A3WE 2002071000079 20020710 00079 NM 2002 7 10 2002F00680 1 20020427 A 5320 CLIP BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND RIGHT FORWARD LAVATORY FLOORBEAM UPPER CHORD AFT SUPPORT CLIP CRACKED, AT STATION 312 RBL 20. (M) 2 L 7 3 4F A3WE 2002071000080 20020710 00080 NM 2002 7 10 2002F00681 1 20020426 A 3220 SUPPORT BOEING 727 727225 1384077 NM NLG CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CORROSION ON SUPPORT AND RADIUS ROD IN NOSE LANDING GEAR WHEEL WELL, STATION 227 LBL 8. (M) 2 L 7 3 4F A3WE 2002071000081 20020710 00081 NM 2002 7 10 2002F00682 1 20020425 A 5320 FLOOR SUPPORT BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CABIN FLOOR SUPPORT ANGLE CRACKED AT STATION 850 LBL 23. (M) 2 L 7 3 4F A3WE 2002071000082 20020710 00082 NM 2002 7 10 2002F00683 1 20020425 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CREASE IN SKIN AT STATION 380-400 STRINGER 5L-9L. (M) 2 L 7 3 4F A3WE 2002071000083 20020710 00083 NM 2002 7 10 2002F00684 1 20020423 A 5313 STRINGER BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND AFT PIT STRINGER 29R CORRODED AT STATION 950A-950C. (M) 2 L 7 3 4F A3WE 2002071000101 20020710 00101 EU 2002 7 10 SIMA200215108 1 20020529 A 5300 ALCLAD2024T3 FRAME SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE FR677 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 DURING AN MBV INSPECTION, FOUND FRAME 677 DENTED. REMOVED DAMAGE BY CUTOUT. PERFORMED NDT, NO DEFECTS. FAB REPAIR DOU BLER, REPAIR DONE IAW SDS AND STANDARD SRM PRACTICES. 2 L 7 2 4T 4 U RT A52EU E8NE 2002071000104 20020710 00104 GL 2002 7 10 HEEA079894 2 20020619 A 7260 23031219 BEARING 23035179 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30P 03013 GL NR 3 AND 4 FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K CAG90118 760082 CAE890152S ENGINE REMOVED DUE TO METAL IN OIL. PARTS REPLACED IN COMPLIANCE WITH CEBA-72-3217 R4. 1 G 7 2 3U 3 U H1NE E1GL 2002071000106 20020710 00106 GL 2002 7 10 HEEA079895 2 20020619 A 7260 230312681 BEARING CAGE 23035179 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30P 03013 GL NR 3 AND 4 FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K CAG90118 760082 CAE890152S ENGINE REMOVED DUE TO METAL IN OIL. PARTS REPLACED IN COMPLIANCE WITH CEBA-72-3217 R4. 1 G 7 2 3U 3 U H1NE E1GL 2002071000109 20020710 00109 GL 2002 7 10 HEEA079896 2 20020619 A 7260 230312683 BEARING CAGE 23035179 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 3 AND 4 FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 5888 CAG90510 760181 CAE890507S ENGINE REMOVED DUE TO TURBINE OVERHAUL. PARTS REPLACED IN COMPLIANCE WITH CEBA-72-3217 R4. 1 G 7 2 3U 3 U H1NE E1GL 2002071000111 20020710 00111 GL 2002 7 10 HEEA079897 2 20020619 A 7260 23031219 BEARING 23035179 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 3 AND 4 FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 5888 CAG90510 760181 CAE890507S ENGINE REMOVED DUE TO TURBINE OVERHAUL. PARTS REPLACED IN COMPLIANCE WITH CEBA-72-3217 R4. 1 G 7 2 3U 3 U H1NE E1GL 2002071000114 20020710 00114 GL 2002 7 10 HEEA079912 2 20020625 A 7250 6886407 TURBINE WHEEL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136H 1412 S833 CAE836298 ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED SULFIDATION ON 1ST STAGE WHEEL BLADES. SCRAPPED WHEEL. 1 G 7 2 3U 3 U H3EU E4CE 2002071000117 20020710 00117 2002 7 10 HEEA079916 4 20020625 A 3455 066104701 TRANSCEIVER SKRSKY S76 S76A 8143006 NE ADF SYSTEM FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 NO LOW BAND RECEPTION OR NEEDLE MOVEMENT. 1 G 7 2 3U H1NE 2002081400165 20020814 00165 EU 2002 8 14 SIMA200216508 1 20020606 A 5420 BEAM SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 RIGHT NACELLE INLET COMPARTMENT INBOARD BOX BEAM CHAFED ON EDGE. BLENDED BOX BEAM, PERFORMED NDT. NO DEFECTS NOTED. R ESTORED SURFACE PROTECTION. 2 L 7 2 4T RT A52EU 2002071000133 20020710 00133 EU 2002 7 10 2002F00725 1 20020619 A 5311 S536R005320000 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 SAW - DURING CPCP2 INSPECTION, FOUND FRAME 37R CORRODED AT FLOOR LEVEL. REPAIRED CORRODED AREA IAW ATR SRM 53-67-70. ( M) 2 H 7 2 4T RT A53EU 2002071000138 20020710 00138 EU 2002 7 10 SIMA200215102 1 20020524 A 5330 SKIN SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 DURING A MBV INSPECTION NO SUBSTANTIATING DOCUMENTATION COULD BE FOUND FOR DOUBLER REPAIR ON RIGHT FUSELAGE AFT OF ICE S HIELD. REMOVED PREVIOUS INSTALLED REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO DEFECTS. FAB. DOUBLER, REPAIR DONE IAW SRM AND STANDARD SRM PRACTICES. 2 L 7 2 4T 4 U RT A52EU E8NE 2002071000139 20020710 00139 SO 2002 7 10 SIMA200216201 1 20020611 A 5300 ALCLAD2024T3 BEAM EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FRAME 20 ELONGATED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 DURING AN IMBV INSPECTION FOUND CENTER BEAM UPRIGHT AT FRAME 20 HAD AN ELONGATGED HOLE. REMOVED DAMAGED UPRIGHT. FRABR ICATED A SERVICEABLE UPRIGHT IAW STANDARD SRM PRACTICES. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002071000140 20020710 00140 EU 2002 7 10 SIMA200215109 1 20020529 A 5311 FRAME SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AE 340B335 DURING A MBV INSPECTION FOUND FRAME 640 DENTED. PERFORMED NDT, NO DEFECTS. FABBED REPAIR DOUBLER, REPAIR DONE IAW SDS AND STANDARD SRM PRACTICES. 2 L 7 2 4T 4 U RT A52EU E8NE 2002071000141 20020710 00141 SO 2002 7 10 SIMA200216306 1 20020528 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 THIS IS A LEVEL 2 FINDING, GALLEY CENTER BEAM GUSSET HAS CORROSION. C/A-REMOVED AND REPLACED GUSSET IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002071000142 20020710 00142 EU 2002 7 10 SIMA200216501 1 20020606 A 5753 SKIN SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE T/E FLAP DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 RIGHT FLAP TOP SKIN HAS TWO DENTS OUTBOARD OF DOVETAIL, .5X .007, .4X .003. C/A-PERFORMED EDDY CURRENT AND THICKNESS TE ST, NO DEFECTS. DENTS ACCEPTED AS IS IAW SDS. 2 L 7 2 4T 4 U RT A52EU E8NE 2002071000143 20020710 00143 EU 2002 7 10 SIMA200216502 1 20020607 A 5311 FRAME SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 DENT RIGHT FUSELAGE FRAME 640 IN CARGO COMPARTMENT. REMOVED DAMAGE BY CUTOUT. FABRICATED AND INSTALLED. A REPAIR DOUB LER, IAW SRM PRACTICES. 2 L 7 2 4T 4 U RT A52EU E8NE 2002071000144 20020710 00144 EU 2002 7 10 SIMA200216505 1 20020606 A 5753 SKIN SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE T/E FLAP DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 LEFT FLAP BOTTOM SKIN HAS 2 DENTS APPROXIMATELY 8 INCH OUTBOARD IF INBOARD HINGE. PERFORMED EDDY CURRENT AND BOND CHECK , NO DEFECTS. DENTS FOUND TO BE WITHIN SRM LIMITS. 2 L 7 2 4T 4 U RT A52EU E8NE 2002071000145 20020710 00145 EU 2002 7 10 SIMA200216506 1 20020607 A 5330 SKIN SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 LEFT AFT FUSELAGE 1 PROTRUSION BELOW HORIZONTAL STABILIZER. PERFORMED EDDY CURRENT INSPECTION , NO DEFECTS. PROTRUSION FOUND TO BE WITHIN SRM AND LIMITS. 2 L 7 2 4T 4 U RT A52EU E8NE 2002081400164 20020814 00164 EU 2002 8 14 SIMA200216507 1 20020606 A 7110 FRAME SAAB SF340 340B 7860101 EU RT COWLING CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 RIGHT OUTBOARD MID-COWL HAS A CRACKED LOWER FRAME. FABRICATED A REPAIR DOUBLER AND INSTALLED IAW SRM. 2 L 7 2 4T RT A52EU 2002071000146 20020710 00146 EU 2002 7 10 SIMA200216509 1 20020606 A 5220 SKIN SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE EMERGENCY EXIT DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 RIGHT FORWARD EMERGENCY EXIT HAS ONE DENT 8.5 INCH FROM BOTTOM. PERFORMED EDDY CURRENT AND THICKNESS TEST, NO DEFECTS. DENT FOUND WITHIN SRM AND LIMITS. 2 L 7 2 4T 4 U RT A52EU E8NE 2002071000147 20020710 00147 EU 2002 7 10 SIMA200216510 1 20020607 A 5311 FRAME SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 DENT IN FUSELAGE FRAME 677 IN CARGO COMPARTMENT. REMOVED DAMAGE BY CUT OUT. FABRICATED AND INSTALLED. A REPAIR DOUBLE R, IAW SRM. 2 L 7 2 4T 4 U RT A52EU E8NE 2002071000148 20020710 00148 EU 2002 7 10 SIMA200216511 1 20020613 A 5532 SKIN AEROSP ATR42 ATR42300 8680920 EU VERTICAL STAB DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 DURING MBV 1 INSPECTION FOUND LEFT SIDE OF VERTICAL STABILIZER TO HAVE 2 DENTS. 2 H 7 2 4T RT A53EU 2002071000149 20020710 00149 SO 2002 7 10 SIMA200216310 1 20020612 A 5300 STRINGER EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL ALCLAD2024T3 CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 DURING AN IMBV INSPECTION FOUND STRINGER 19R CHAFED BETWEEN FRAMES 52 AND 53. BLENDED AREA, PERFORMED NDT INSPECTION NO DEFECTS. FABRICATED A DOUBLER ANGLE, AND TWO SHIMS. REPAIR DONE IAW STANDARD SRM PRACTICES. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002071000150 20020710 00150 NM 2002 7 10 UPS02238758 1 20020620 A 5310 INTERCOSTAL BOEING 727 72722C 138400F NM BS520 RBL15 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CRACKED BRACKET ON INTERCOSTAL BS520 RBL15, CABIN FLOOR. BRACKET REPAIRED IAW SRM 51-40-03 FIG 1 TYP FORMED SECTION REPAIR. 2 L 7 3 4F A3WE 2002071000151 20020710 00151 NM 2002 7 10 UPS02238760 1 20020613 A 5310 WEB BOEING 727 72722C 138400F NM BS1182 LBL54 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CRACK TO WEB AT BS 1182 LBL54 APPROX AT ACCESS HOLE FOR PIPE WORK WEB REPLACED IAW SRM 51-20-1 FIG7 AND SRM 51-30-2 2 L 7 3 4F A3WE 2002071000152 20020710 00152 NM 2002 7 10 UPS02238761 1 20020612 A 5310 BRACKET BOEING 727 72722C 138400F NM BS178 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CRACK ON SUPPORT ANGLE AT BS 178 BULKHEAD RBL24 SUPPORT BRAKET REPLACED IAW SRM 53-10-2 FIG1 AB D SRM 51-20-1 FIG 7 A ND SRM 51-30-2. 2 L 7 3 4F A3WE 2002071000153 20020710 00153 NM 2002 7 10 UPS02238764 1 20020613 A 5720 65C80678 CASTING BOEING 727 72722C 138400F NM WS304 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI #6 SPOILER CENTRE HINGE SUPPORT CASTING O/B FACE OF I/B HINGE LUG HA S EVIDENCE OF CORROSION. C ORROSION REMOVED IAW SRM 51-10-06 AND FOUND OUT OF LIMITS IAW SRM 5 1-10-01. HINGE CASTING REPLACED IAW DWG 65-16216 2 L 7 3 4F A3WE 2002071000154 20020710 00154 NM 2002 7 10 UPS02238766 1 20020613 A 5750 FLAP TRACK BOEING 727 72722C 138400F NM WS304 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI PITTING CORROSION IN BORE OF HOLES F+G ON NO3 FLAP TRACK TRACK REPLACED REF NRC 541795 FOR REPL ACMENT DETAILS. 2 L 7 3 4F A3WE 2002071000155 20020710 00155 SO 2002 7 10 SIMA200216311 1 20020612 A 5300 ALCLAD2024T3 STRINGER EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL STRING 19L CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 DURING AN IMBV INSPECTION FOUND STRINGER 19L CHAFED BETWEEN FRAMES 52 AND 53. BLENDED CHAFE. PERFORMED NDT INSPECTION NO DEFECTS. FABRICATED A DOUBLER ANGLER, AND TWO SHIMS. REPAIR DONE IAW STANDARD SRM PRACTICES. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002071000160 20020710 00160 2002 7 10 AALA20020060 4 20020117 A 2210 DAMPENER AIRBUS 300 A300B4605R 3930308 EU AUTOPILOT SYS BROKEN A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 50051 459 MIA - FLT 2139 - EN ROUTE MIA-CCS - UNCOMMANDED RUDDER MOVEMENT DURING CLIMB-OUT. ISOLATING A/P SYSTEM DID NOT HELP. N O AIRFRAME VIBRATION NOTICES. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 FLIGHT AUGMENTATION COM PUTERS. DID NOT RESOLVE PROBLEM. REPLACED YAW DAMPER SERVO ACTUATOR AND ACCOMPLISHED YAW DAMPER SERVO ACTUATOR OPERATI ONAL CHECK. DID NOT RESOLVE THE PROBLEM. REPLACED YAW DAMPENER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002071000161 20020710 00161 EU 2002 7 10 AALA20020377 1 20020402 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1458H 11478 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 8D INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002071000162 20020710 00162 SO 2002 7 10 SIMA200217102 1 20020619 A 2700 3622001009 ACTUATOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL TAIL INOPERATIVE A SIMA O OTHER F J Z FLT CONT AFFECTED WARNING INDICATION SIGNIFICANT FAILURE REPORT CR CRUISE 1 SW 21 631AE 145139 DISC-PITCH TRIM AUTO MSSG ON EICAS IN FLIGHT WITH AUTOPILOT ON THEN ALL PITCH TRIM SWITCHES FAILED. C/A MAINTENANCE REM OVED AND INSTALLED A NEW HORIZONTAL STABILIZER ACTUATOR. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002071000163 20020710 00163 EU 2002 7 10 AALA20020378 1 20020402 A 3350 6040681 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1453D 11465 MSP - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHTS UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002071000164 20020710 00164 NM 2002 7 10 AALA20020435 1 20020408 A 3350 P201003313025 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 648AA 24606 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002071000165 20020710 00165 NM 2002 7 10 AALA20020436 1 20020405 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 676AN 29426 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002071000166 20020710 00166 WP 2002 7 10 AALA20020445 1 20020410 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 275AA 49272 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AFT OF SEAT 7D DIM. REPLACED AFT EMERGENCY EXIT PATH L IGHTING ASSEMBLY AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000167 20020710 00167 WP 2002 7 10 AALA20020446 1 20020409 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT ABOVE FORWARD GALLEY SERVICE DOOR FLICKERS. REPLACED FORWARD GALLEY EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000168 20020710 00168 WP 2002 7 10 AALA20020447 1 20020411 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AA 49737 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT ABOVE DOORS ON BOTH SIDES INOPERATIVE. TIGHTENED EMER GENCY EXIT LIGHT CONNECTOR AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000169 20020710 00169 WP 2002 7 10 AALA20020449 1 20020412 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 490AA 49683 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT ROWS 13-16 DIM. CLEANED EMERGENCY EXIT LIGHT CONNE CTOR AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000170 20020710 00170 WP 2002 7 10 AALA20020450 1 20020414 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7536A 49990 DFW - DURING OVERNIGHT MAINTENANCE, LEFT OVERHEAD EMERGENCY EXIT LIGHT AT ROW 26 WILL NOT STAY ON. CLEANED EMERGENCY EX IT LIGHT CONNECTOR AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000171 20020710 00171 WP 2002 7 10 AALA20020451 1 20020414 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 595AA 53285 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 17D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBL Y. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002071000172 20020710 00172 WP 2002 7 10 AALA20020452 1 20020415 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 413AA 49324 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT FROM SEAT 19 TO FIRST CLASS INOPERATIVE. REPLACED EMERGEN CY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000173 20020710 00173 WP 2002 7 10 AALA20020504 1 20020418 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 295AA 49307 DFW - DURING OVERNIGHT MAINTENANCE, LOWER RIGHT SIDE WALL FORWARD EXIT SIGN AT ROW 20 INOPERATIVE. REPLACED EMERGENCY E XIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000174 20020710 00174 SO 2002 7 10 SIMA200215118 1 20020529 A 5300 FRAME EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FR20, STR 16L MISDRILLED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 145314 DURING AN MBV INSPECTION, FOUND DAMAGE TO STRINGER 16L FORWARD OF FRAME 20, AT JOINT DRILL MARKS AND OVERSIZE HOLE. REM OVED DRILL MARKS BY BLENDING. REAMED HOLES, INSTALLED NEW FASTENERS IAW STANDARD SRM PRACTICES. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002071000175 20020710 00175 WP 2002 7 10 AALA20020505 1 20020418 A 3350 LIGHT DOUG DC9 DC982 3022082 WP COCKPIT NOT SEATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 223AA 49173 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN COCKPIT DIM. SEATED EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000176 20020710 00176 WP 2002 7 10 AALA20020506 1 20020418 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7528A 49920 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ON SEAT 22D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS SOCKE T. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000177 20020710 00177 WP 2002 7 10 AALA20020507 1 20020421 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 295AA 49307 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS WILL NOT ILLUMINATE. REPLACED EMERGENCY EXIT LIGHT S BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000178 20020710 00178 EU 2002 7 10 AALA20020510 1 20020422 A 3350 POWER SUPPLY AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14056 463 MIA - FOUND MID AND AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLIES AT 4R AND 4L. SYSTEM GROUND CHECKE D NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002071000179 20020710 00179 WP 2002 7 10 AALA20020517 1 20020422 A 3350 TERMINAL DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 460AA 49565 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. TIGHTENED FIRST CLASS CEILIN G EMERGENCY EXIT LIGHT TERMINAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000180 20020710 00180 WP 2002 7 10 AALA20020518 1 20020422 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 559AA 53089 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM FIRST CLASS TO MID CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071000181 20020710 00181 NM 2002 7 10 AALA20020529 1 20020417 A 2421 GEN5103 IDG BOEING 767 767323 1385205 NM LT ENGINE MALFUNCTIONED A AALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 39365 24046 HNL - INITIATED ABORT AT 110 KTS AT HNL, DUE OT LEFT GEN DRIVE LIGHT ILLUMINATED. PEAK A/S DURING ABORT WAS APPROX 120 KTS OUTSIDE AIR TEMP WAS 29 DEGREES CELSIUS. BITE CHECKED BPCU, SERVICED LEFT ENGINE IDG, ENG RUN AND OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A1NM 2002071000182 20020710 00182 NM 2002 7 10 AALA20020531 1 20020419 A 2421 GEN5123 GENERATOR BOEING 767 767223 1385123 NM CENTER SYSTEM FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 322AA 22323 MIA - FLT 789 - REPLACED CENTER SYSTEM GENERATOR AND OPS CHECK OR BUT 5 MINUTES LATER IT FAILED SHOWING FAIL CODE 200. REMOVED AND REPLACED CENTER SG, OPS CHECKED NORMAL FOR SHTS, IAW MM ALL TESTS NORMAL. (M) 2 L 7 2 4F RT A1NM 2002071000183 20020710 00183 NM 2002 7 10 AALA20020533 1 20020415 A 2421 GEN3014 IDG BOEING 777 777223 1385213 NM LT ENGINE FAILED A AALA K NONE J WARNING INDICATION DE DESCENT 1 SW 21 750AN 30259 LHR - FLT 56 - ELECT GEN OFF L STATUS MESSAGE CAME ON PASSING THROUGH 140 ON DESCENT. REMAINED ON AFTER CHECKLIST ITEMS WERE COMPLETED. LEFT GENERATOR DISCONNECTED. REMOVED AND REPLACED LEFT ENG IDG PER MM. PERFORMED ALL APPLICABLE TEST S. OPS AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT T00001SE 2002071000184 20020710 00184 NM 2002 7 10 AALA20020534 1 20020406 A 2424 CON5330 GCU BOEING 767 767323 1385205 NM E/E BAY FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 386AA 27060 JFK - FLT 182 - AFTER 40 MINUTES OF FLIGHT LEFT GENERATOR OFF, WOULD NOT RESET. REMOVED AND REPLACED LEFT GCU AND LEFT IDG. PERFORMED OPERATIONAL CHECK OF LEFT GENERATOR SYSTEM. ALL OPS NORMAL. PERFORMED ENGINE RUN SYSTEM CHECKS NORMAL. NO LEAKS NOTED. OK FOR SERVICE. (M) 2 L 7 2 4F RT A1NM 2002071000185 20020710 00185 EU 2002 7 10 MALA020394 1 20020708 A 2560 LIFE VEST BAC 146 AVRO146RJ85A 1500097 EU A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 506XJ E2314 DURING FLIGHT #3534 LIFE VEST IN 4C FELL DOWN, MAINTENANCE RESECURED VELCRO. 2 H 7 4 4F RT A49EU 2002071000186 20020710 00186 EU 2002 7 10 MALA020395 1 20020709 A 2430 BATTERY SAAB SF340 SF340A 7850100 EU A MALA K NONE H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 GL 15 115XJ DURING EMERGENCY BATTERY CAPACITY CHECK, JC #243501 EMERGENCY BATTERY FAILED VOLTAGE/CAPACITY CHECK. MAINTENANCE REMOVE D AND REPLACED EMERGENCY BATTERY IAW JC #243502. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002071000187 20020710 00187 NM 2002 7 10 AALA20020539 1 20020422 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHT ON G3 GALLEY FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002071000188 20020710 00188 EU 2002 7 10 AALA20020545 1 20020425 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7062A 474 MIA - EXIT LIGHT ON ROW 25 RIGHT INOPERATIVE. SECURED LOOSE WIRE AT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERA TION. (M) 2 L 7 2 4F RT A35EU 2002071000189 20020710 00189 NM 2002 7 10 AALA20020555 1 20020428 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 624AA 24582 DFW - FOUND EXIT SIGN FORWARD OF MID LAVATORY CEILING FORWARD FACING SIGN INOPERATIVE. REPAIRED BROKEN WIRE. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002071000190 20020710 00190 EU 2002 7 10 AALA20020560 1 20020430 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1436A 11426 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT FROM FORWARD GALLEY TO SEAT 11D INOPERATIVE. TIGHTE NED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR FORWARD OF SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002071000191 20020710 00191 NM 2002 7 10 AALA20020564 1 20020420 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 308AA 22314 LAX - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 22 A AND B INOPERATIVE. REPLACED CONNE CTOR AT SIDEWALL FOR SEAT 22A AND B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002071000192 20020710 00192 NM 2002 7 10 AALA20020565 1 20020423 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 LFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT ROWS 22, 23, 24 INOPERATIVE. REPLACED SEAT CONNECTOR AT ROW 23 AND BATTERY PACK EQUIPMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002071000193 20020710 00193 NM 2002 7 10 AALA20020566 1 20020428 A 3350 POWER SUPPLY BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - DURING OVERNIGHT MAINTENANCE, FOUND R4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY FOR AT R4 . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002071000194 20020710 00194 SO 2002 7 10 SIMA200215105 1 20020525 A 5100 ALCLAD2024T3 STRINGER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL STR 19R CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 DURING AN IMBV INSPECTION, FOUND STRINGER 19R, CHAFED. BLENDED CHAFE. PERFORMED AN NDT INSPECTION NO DEFECTS. TWO DOU BLERS AND FOUR SHIMS. REPAIR DONE IAW STANDARD SRM PRACTICES. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002071000195 20020710 00195 SO 2002 7 10 LR7A02044 1 20020707 A 5312 STIFFENER LKHEED 382 382G 526414U SO FS 600 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3209 FOUND RMLG WHEEL WELL FS 600 WALL SKIN RISER CRACKED AT RBL 62, WL 1 63.REPAIRED IAW SRM SMP 583 53-40-10. NR 0023. 2 H 7 4 4T A1SO 2002071000196 20020710 00196 SO 2002 7 10 LR7A02048 1 20020707 A 5312 341973L FITTING LKHEED 382 382G 526414U SO FS 497 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP5369 FOUND LH FS 497 UPPER BOW BEAM FITTING CRACKED AT LBL 63, WL 258.REP AIRED IAW SRM SMP 583 51-70 AND DWG 341973. NR 0037. 2 H 7 4 4T A1SO 2002071000197 20020710 00197 SO 2002 7 10 LR7A02049 1 20020707 A 5312 341973R FITTING LKHEED 382 382G 526414U SO FS 497 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP5369 FOUND RH FS 497 UPPER BOW BEAM FITTING CRACKED AT RBL 63, WL 258.REP AIRED IAW SRM SMP 583 51-70 AND DWG 341973. NR 0038. 2 H 7 4 4T A1SO 2002071000198 20020710 00198 SO 2002 7 10 LR7A02050 1 20020707 A 5320 FRAME LKHEED 382 382G 526414U SO FS 140 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3207 FOUND FS 140 BATTERY BAY SUPPORT FRAME CRACKED ADJACENT TO LOWER CORN ER AT LBL 46, WL 158.REPAIRED IAW SRM SMP 583 51-140-19. NR 0041. 2 H 7 4 4T A1SO 2002071000199 20020710 00199 SO 2002 7 10 LR7A02051 1 20020707 A 5330 DOUBLER LKHEED 382 382G 526414U SO FS 573-597 CUT A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION CUT EXISITING FS 573 - 597 SKIN DOUBLER AT LBL 62, WL 144 TO PROVIDE ACCESS FOR CHINE ANG LE REPLACEMENT (NR 0033).REPAIRED IAW LAC MEA 382-53-02-032. NR 0070. 2 H 7 4 4T A1SO 2002071000200 20020710 00200 SO 2002 7 10 LR7A02052 1 20020707 A 5312 3769501 FITTING LKHEED 382 382G 526414U SO FS 497 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3208 FOUND LMLG FS 497 LOWER BOW BEAM FITTING CRACKED AT LBL 63, WL 150.RE PLACED FITTING IAW SRM SMP 583 51-70. NR 0073. 2 H 7 4 4T A1SO 2002071000201 20020710 00201 SO 2002 7 10 LR7A02053 1 20020707 A 5312 3769501 FITTING LKHEED 382 382G 526414U SO FS 537 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3208 FOUND LMLG FS 537 LOWER BOW BEAM FITTING CRACKED AT LBL 63, WL 150.RE PLACED FITTING IAW SRM SMP 583 51-70. NR 0074. 2 H 7 4 4T A1SO 2002071000202 20020710 00202 SO 2002 7 10 LR7A02054 1 20020707 A 5312 3769501 FITTING LKHEED 382 382G 526414U SO FS 557 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3208 FOUND LMLG FS 557 LOWER BOW BEAM FITTING CRACKED AT LBL 63, WL 150.RE PLACED FITTING IAW SRM SMP 583 51-70. NR 0075. 2 H 7 4 4T A1SO 2002071000203 20020710 00203 SO 2002 7 10 LR7A02055 1 20020707 A 5312 3769501 FITTING LKHEED 382 382G 526414U SO FS 557 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3209 FOUND RMLG FS 557 LOWER BOW BEAM FITTING CRACKED AT RBL 63, WL 150.RE PLACED FITTING IAW SRM SMP 583 51-70. NR 0076. 2 H 7 4 4T A1SO 2002071000204 20020710 00204 SO 2002 7 10 LR7A02056 1 20020707 A 5312 3769501 FITTING LKHEED 382 382G 526414U SO FS 497 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3209 FOUND RMLG FS 497 LOWER BOW BEAM FITTING CRACKED AT RBL 63, WL 150.RE PLACED FITTING IAW SRM SMP 583 51-70. NR 0077. 2 H 7 4 4T A1SO 2002071000205 20020710 00205 SO 2002 7 10 LR7A02057 1 20020707 A 5744 34862714R STIFFENER LKHEED 382 382G 526414U SO OWS 241 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC2704 FOUND RH OWS 241 FLAP TRACK STIFFENER CRACKED.REPLACED STIFFENER IAW SRM SMP 583 57-50-03. NR 0106. 2 H 7 4 4T A1SO 2002071000206 20020710 00206 SO 2002 7 10 LR7A02058 1 20020707 A 5751 SKIN LKHEED 382 382G 526414U SO AS 55 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC2704 FOUND LH AILERON UPPER SKIN CORRODED AT AS 55, FS 595.REPAIRED SKIN I AW SRM SMP 583 51-140-10. NR 0139. 2 H 7 4 4T A1SO 2002071000207 20020710 00207 SO 2002 7 10 LR7A02059 1 20020707 A 5311 ANGLE LKHEED 382 382G 526414U SO FS 946 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND FS 946 FRAME UPPER BEAM CAP ANGLE CRACKED AT RBL 14, WL 285.RE PAIRED IAW SRM SMP 583 51-140-23. NR 0250. 2 H 7 4 4T A1SO 2002071000208 20020710 00208 SO 2002 7 10 LR7A02060 1 20020707 A 5320 BEAM LKHEED 382 382G 526414U SO FS 528 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3208 FOUND LMLG BAY FS 528 SUPPORT BEAM CRACKED FROM UPPER ATTACHMENT BOLT HOLE AT LBL 64, WL 250.REPAIRED IAW LAC MEA 382-53-02-030. NR 0289. 2 H 7 4 4T A1SO 2002071000209 20020710 00209 SO 2002 7 10 LR7A02062 1 20020707 A 5315 355673201 FITTING LKHEED 382 382G 526414U SO FS 557 MISALIGNED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION LH FS 557 FLOOR END FITTING REPLACEMENT FOUND NEW FITTING PILOT HOLES NOT ALIGNED WITH S TRUCTURE.REWORKED FITTING IAW LAC MEA 382-53-02-035. NR 0375. 2 H 7 4 4T A1SO 2002071000210 20020710 00210 SO 2002 7 10 SIMA200215104 1 20020523 A 5100 STRINGER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL STR 19, FR 52 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 DURING AN IMBV INSPECTION, ONE RIVET HOLES WAS MISDRILLED ON STRINGER 19L, AT FRAME 52. REAMED HOLE, INSTALLED A HST10B J-8-6, AND HST79CK-8 FASTERNS. REPAIR DONE IAW STANDARD SRM PRACTICES. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002071000211 20020710 00211 EU 2002 7 10 02FDEA00478 1 20020710 A 5522 SKIN AIRBUS 310 A310 EU ELEVATOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 RT ELEVATOR TRAILING EDGE LOWER SKIN IS CORRODED 40 CM OUTBD OF INBOARD EDGE. CLEANED CORROSION WITHIN LIMITS IN SRM 55- 20-00. 2 L 7 2 4F RT A35EU 2002071000212 20020710 00212 EA 2002 7 10 COMA0260410 1 20020708 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 937CA 7044 FLIGHT 5998 CABIN DOOR LATCH MESSAGE AFTER T/O.ISPECTED DOOR, PRESSURIZED AIRCRAFT, COULD NOT DUPLICATE. NO DEFECTS FO UND. 2 L 7 2 4F RT A21EA 2002071000213 20020710 00213 EA 2002 7 10 COMA0260411 1 20020708 A 3260 172825 TARGET CNDAIR CL600 CL6002B19 1900309 EA R/H MLG LOOSE A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 963CA 7127 FLIGHT 5566 R/H MLG INDICATES INTRANSIT AFTER GEAR RETRACTION.TIGHTENED LOOSE PROX SENSOR TARGET ON UPLOCK. 2 L 7 2 4F RT A21EA 2002071000214 20020710 00214 EU 2002 7 10 SIMA200216503 1 20020607 A 5300 STABILIZER SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE LEFT HORZ STAB DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 LEFT HORIZONTAL STABILIZER TOP HAS FOUR DENTS. 2 L 7 2 4T 4 U RT A52EU E8NE 2002071000215 20020710 00215 EA 2002 7 10 COMA0260412 1 20020706 A 3230 750006000D SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 796CA 6812 7338 FLIGHT 5998 GEAR DISAGREE MESSAGE WHEN GEAR EXTENDED AT 240 KTS.REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002081400163 20020814 00163 EU 2002 8 14 SIMA200216504 1 20020606 A 5420 7254200357 INTERCOSTAL SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 18282 340B343 RIGHT NACELLE INLET COMPARTMENT INBOARD INTERCOSTAL CHAFED. REMOVED INTERCOSTAL AND INSTALLED SERVICEABLE IAW SRM. 2 L 7 2 4T RT A52EU 2002071000216 20020710 00216 EA 2002 7 10 COMA0260413 1 20020705 A 2450 HA4A039 RELAY CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 01 403CA 7428 FLIGHT 5803 AC ESS BUSS FAIL MESSAGE.REPLACED RELAY K3XD 2 L 7 2 4F RT A21EA 2002081200060 20020812 00060 SO 2002 8 12 RAIA00207205 1 20020703 A 3610 S2U2226 O-RING EMB 145 EMB145 3260210 SO BLEED AIR LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 809HK 145187 5251-RIC- CREW REPORTED NR 2 BLEED LEAK WARNING. MAINTENANCE REMOVED AND REPLACED NR 2 BLEED DUCT SEAL, LEAK AND OPS CH ECK OK. 2 L 7 2 4F RT T00011AT 2002071000217 20020710 00217 EU 2002 7 10 RAIA00207206 1 20020706 A 7710 31055863 SENSING ELEMENT JETAIR JETSTM JETSTM4101 1500501 EU FALSE INDICATION A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 554HK 12090 41067 9546-STL- CREW REPORTED #2 ENGINE TORQUE FLUX DURING CLIMB. MAINTENANCE REMOVED AND REPLACED THE SPEED MONOPOLE, OPS CK OK. 2 L 7 2 4T RT A41NM 2002071000218 20020710 00218 EA 2002 7 10 COMA0260414 1 20020705 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 960CA 7117 FLAPS FAILED MESSAGE AFTER LANDING.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002071000219 20020710 00219 EA 2002 7 10 COMA0260415 1 20020707 A 5300 601R35031239 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS 621 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 983CA 11583 7169 FS 621 FLOOR SUPPORT ANGLE CRACKED WL 73.50 RBL 41.COMPLIED WITH REO 601R-53-61-117 REV A AND WVAC EO 601R-53-3339. LOCA TED AND INSTALLED ANGLES 601R53-61-004-2, 601R53-61-004-6 AND 601R53-61-004-4. INSTALLED FABRICATED RADIUS BLOCK IAW REO 601R-53-3339. 2 L 7 2 4F RT A21EA 2002071000220 20020710 00220 EA 2002 7 10 COMA0260416 1 20020708 A 5210 FILLER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 938CA 11883 7046 FWD PAX DOOR SEAL STRIKER HAS PREVIOUS REPAIR AT TWO PLACES FS 310 AND FS 349 BOTH REPAIRS REQUIRE REWORK DUE TO FILLER MATERIAL CRACKED AND SEPERATED FROM REPAIR DOUBLER.REMOVED PREVIOUS REPAIRS AND INSTALLED NEW FWD PAX DOOR SEAL STRIKER REPAIR AT FS 310 AND FS 349 I/A/W REO 601R-52-11-008 REV B REPAIR A. 2 L 7 2 4F RT A21EA 2002071000221 20020710 00221 EU 2002 7 10 USAASA02054 1 20020609 A 2820 FRH280002 VALVE AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE RT WNG FUEL TANK MALFUNCTIONED A USAA K NONE K FLUID LOSS TO TAKEOFF 1 EA 19 717UW 9272 1069 ENROUTE, ON TAKEOFF, FUEL SEEN VENTING FROM RIGHT WING TIP. LEFT TANK FUEL INDICATED 200 LBS LESS THAN RIGHT WING. BY THE END OF THE FLIGHT, UPON LANDING, LEFT TANK FUEL WAS 480 LBS LESS THAN RIGHT WING. MAINTENANCE REPLACED RIGHT WING T ANK AIR RELEASE VALVE (FIM 87QM). OPERATIONALLY CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2002071000222 20020710 00222 EU 2002 7 10 USAASA02051 1 20020604 A 5610 NP1653115 WINDSHIELD AIRBUS A319 A319112 3930323 EU COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 758US 3678 1348 ENROUTE, DURING CRUISE FLIGHT, THE CAPTAINS WINDSHIELD CRACKED IN A SPIDER WEB PATTERN. FLIGHT RETURN TO FIELD IN PIT. MAINTENANCE REPLACED THE LEFT HAND WINDSHIELD. OPERATIONALLY AND BITE CHECKED THE NUMBER ONE WINDSHIELD HEAT COMPUTER. NO FAULTS FOUND. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2002071000223 20020710 00223 EA 2002 7 10 SWIA200211000 1 20020625 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 406SW 7030 FLIGHT CREW REPORTS INTERMITTENT WARNING FOR SERVICE DOOR CAUTION MESSAGE. RETURNED TO SLC. TIGHTENED HANDLE ON SERVIC E DOOR. OPS CHECK GOOD. NO WARNING MESSAGE. 2 L 7 2 4F RT A21EA 2002071000224 20020710 00224 NM 2002 7 10 AWXA200200586 1 20020708 A 3350 14803180 PLUG BOEING 737 7373G7 1384595 NM SEAT ROW 14 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 0 0 23782 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPL ACED THE EMERGENCY LIGHT HARNESS PLASTIC CONNECTOR AT SEAT ROW 14 L/H PER BMM CHAP 20. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002091100030 20020911 00030 NM 2002 9 11 AWXA200200589 1 20020709 A 3610 342B030000 FILTER AIRBUS A319 A319132 3930340 NM BLEED AIR CONTAMINATED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 660AW 7900 1234 PHX - AIR TURNBACK - FLT 0256 - WHILE CLIMBING OUT OF PHX EN ROUTE FOR PHL RECEIVED ECAM CAUTION AIR ENGINE NR 1 BLEED F AULT, BLEED TEMPERATURE EXCEEDED 300 DEGREES, TURNED BACK TO PHX DUE TO POSSIBLE ICING CONDITIONS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE TEMPERATURE CONTROL THERMOSTAT IAW AMM 36-11-43-401. PERFORMED ENGINE RUN, OPERATIONAL CHE CK WAS GOOD. VENDOR CONFIRMED FAILURE OF UNIT CITING THE FILTER WAS CONTAMINATED WITH POLLUTION. RESTORED UNIT BY CLEA NING THE PRESSURE REDUCING CLAPPER / GUIDE AND FILTER, AND REPLACING SCREW LOCKS AND PACKING. 2 L 7 2 4F RT A28NM 2002071000225 20020710 00225 EA 2002 7 10 SWIA200211006 1 20020702 A 5240 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NA GALLEY DOOR DIRTY A SWIA O OTHER E VIBRATION/BUFFET CL CLIMB 1 NM 07 590SW 7077 CLIMBING THROUGH 25,000 FEET, WITH A CABIN ALTITUDE OF 7.0, A VIBRATION STARTED THAT SEEMED TO BE COMING FROM THE FORWAR D GALLEY DOOR. THE FLIGHT ATTENDANT ALSO REPORTED LOUD NOISE AND VIBRATION COMING FROM GALLEY DOOR.REPLACED DOOR SEAL I AW MM 52-41-07. FOUND CENTER PLUNGER ASSEMBLY FORK BENT. REMOVED AND REPLACED SERVICE DOOR CENTER PLUNGER ASEEMBLY WI TH NEW PLUNGER ASSEMBLY IAW 52-41-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002071000226 20020710 00226 EA 2002 7 10 SWIA200211011 1 20020704 A 3150 FUSE CNDAIR CL600 CL6002B19 1900309 EA F3PA MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 588SW 7069 STANDBY PITOT HEAT CAUTION MESSAGE CYCLES ON AND OFF IN FLIGHT. RETURNED TO SLC. SERVICE TRU AND MAIN BATTERY SHOW 1 00 AMPS. REMOVED AND REPLACED FUSE F3PA. RAN LEFT AND RIGHT ENGINES ON GROUND, COULD NOT DUPLICATE CAUTION MESSAGE. O PS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002071100001 20020711 00001 SO 2002 7 11 C2XA02TY109 1 20020710 A 5753 14568000431 FLAP EMB 145 EMB145LR 3260212 SO CRAZED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16951 145063 TYS DURING A SCHEDULED ROUTINE CHECK THE LH INBD FLAP TRAILING EDGE,UPPER SURFACE AERODYNAMIC FILLER WAS FOUND CRAZING AND CRACKING. THE AREA WAS 18"L X8.25"W, WITH A AREA WITHIN THAT THAT WAS 1.25" X 1.5" THAT THE FILLER WAS MISSING. MAI NT. REQUESTED A GST FOR THE FLAP AND WAS ISSUED GST-2155/02 WHICH ALLOWED MAINTENANCE TO PUT SPEED TAPE OVER THE AREA AN D DO A GVI EVERY ROUTINE CHECK FOR 500FC IN THAT IT WILL BE REPAIRED OR REPLACED.ALL WAS C/W AND PUT ON DMI. 2 L 7 2 4T RT T00011AT 2002071100002 20020711 00002 SO 2002 7 11 C2XA02IA140 1 20020707 A 3350 20131A BATTERY EMB 145 EMB145ER 3260211 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 IAH- WHILE PERFORMING MAINTENANCE THE MECHANIC NOTED THAT THE GALLEY EMERGENCY LIGHTS FAILED TO ILLUMINATE. IAH- MAIN TENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY POSITION #2, PERFORMED A OPERATIONAL CHECK NO DEFECTS NOTED, AN D, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVECD, WHEN RELEASED FROM MOD LINE. 2 L 7 2 4F RT T00011AT 2002071100003 20020711 00003 NM 2002 7 11 DHL2002750004 1 20020708 A 3350 1060091102 BATTERY BOEING 727 7272M7 138407S NM A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 750DH 21951 1) EMERGENCY EXIT LIGHTS WILL NOT TEST. 2) REMOVED AND REPLACED COCKPIT & L1 DOOR EMERGENCY EXIT LIGHT BATTERY PACKS I AW B727 M/M CHP 33-50-101. OPS CKD NORMAL. 2 L 7 3 4F A3WE 2002071100004 20020711 00004 GL 2002 7 11 HEEA079918 2 20020625 A 7250 23053299 TURBINE WHEEL SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 595 760231 CAE890071S ENGINE REMOVED DUE TO CRACKED NR 1 NOZZLE. UPON INSPECTION OF TURBINE PARTS NOTED SLIGHT SULFIDATION ON ALL 1ST STAGE T URBINE WHEEL BLADES AND 1ST STAGE TIP DRAG WITH 2ND STAGE NOZZLE. SCRAPPED. 1 G 7 2 3U 3 U H1NE E1GL 2002071100005 20020711 00005 NE 2002 7 11 HEEA079919 1 20020625 A 6730 30006762102 MANIFOLD SKRSKY S76 S76A 8143006 NE SERVO SYSTEM DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 LEAKING DURING TESTING OF SERVO ASSY BETWEEN MANIFOLD AND SERVO VALVE CAP ASSY ON SYSTEM NR 2 PRESSURE PORT. FOUND A MI SSING PIN (LEE) PLUG ON THAT PORT. ALSO FOUND THAT THIS PORT REQUIRES AN OVERSIZE PLUG. 1 G 7 2 3U H1NE 2002071100006 20020711 00006 2002 7 11 HEEA079920 4 20020625 A 2230 7611113 AMPLIFIER SKRSKY S76 S76A 8143006 NE AUTOFLIGHT MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 NR 2 YAW NEEDLE DEFLECTED FULL LEFT AT ALL TIMES. 1 G 7 2 3U H1NE 2002071100007 20020711 00007 NE 2002 7 11 HEEA079921 1 20020625 A 7800 7630507001044 COVER SKRSKY S76 S76A 8143006 NE EXHAUST CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 EXHAUST COVER CRACKED. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H1NE 2002071100008 20020711 00008 2002 7 11 USAASA02052 4 20020605 A 2565 D31517113 SLIDE AIRBUS A319 A319112 3930323 EU PASSENGER CABIN READS LOW A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 741UW 6231 1269 THE L2 DOOR ESCAPE SLIDE INDICATES LOW PRESSURE. MAINTENANCE REPLACED THE L2 DOOR ESCAPE SLIDE. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2002071100009 20020711 00009 EU 2002 7 11 USAABA02015 1 20020615 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU 1L,2L,4R DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 675US 0370 MAINTENANCE FOUND EPSU FAULTS FOR 1L (1101L), 2L (13WL) AND 4R (18WL) BATTERIES. MAINTENANCE REMOVED AND REPLACED THE B ATTERIES. 2 L 7 2 4F RT A46NM 2002071100010 20020711 00010 NM 2002 7 11 USAABB02092 1 20020612 A 3350 SOCKET BOEING 767 767201 1385125 NM ROWS 20,24 FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 23898 FOUND EMERGENCY LOW LEVEL LIGHTING INOPERATIVE BETWEEN ROWS 20 AND 24. MAINTENANCE REPAIRED A LIGHT SOCKET. 2 L 7 2 4F RT A1NM 2002071100011 20020711 00011 WP 2002 7 11 AALA20020723 1 20020521 A 3397 WIRE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE TAIL CONE LOOSE A AALA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SW 21 581AA 53158 DURING OVERNIGHT MAINTENANCE TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. SECURED TAIL CONE EMERGENCY EXIT LIGHT BATTER Y WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2002071100013 20020711 00013 EU 2002 7 11 RAIA00207208 1 20020709 A 3350 167006 LIGHT AEROSP ATR72 ATR72202 8680940 EU CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 723TE 283 MX-STL- EMERGENCY LIGHT AT REAR OF CABIN HAS ONE BULB INOP. REMOVED AND REPLACED LIGHT BULB, OPS CK OK. 2 H 7 2 4T RT A53EU 2002071100014 20020711 00014 EU 2002 7 11 RAIA00207209 1 20020709 A 3350 3011210 LIGHT AEROSP ATR72 ATR72202 8680940 EU INOPERATIVE A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 723TE 283 MX-STL- PAX DOOR EMERGENCY LIGHT INOP.REMOVED AND REPLACED LIGHT ASSY, OPS CK OK. 2 H 7 2 4T RT A53EU 2002071100015 20020711 00015 GL 2002 7 11 RAIA00207210 2 20020709 A 7421 23062672 IGNITER EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 806HK 145112 310166 5275-PIT- #1 ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED #1 "B" IGNITER PLUG, OPS CK GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002071100017 20020711 00017 NM 2002 7 11 AALA20020535 1 20020409 A 2497 HAR5341 WIRE HARNESS BOEING 767 767323 1385205 NM LT ENGINE DAMAGED A AALA K NONE J WARNING INDICATION CL CLIMB 1 SW 21 383AN 26995 BOS - FLT 156 - LEFT GEN FAILED WOULD NOT RESET. REPLACE IDG AND TRIED GCU, NO HELP. SERVICED IDGS AND APU PER MPM24-0 1. IDG DISCONNECTED. BPCU FAULTS CT LOOP GND DP TRIP. MAIN BUS OVER LAP. GEN IFDR. REPAIRED T1/T2/AND T3 IDG LEADS WITH SPLICES AS EPR WIRING REPAIR DOCUMENT INSTALLED ALL LEADS TO IDG TO BE OPS CHECKED. ACCOMPLISHED OPS CHECK OF LEFT ENGINE GENERATOR. (M) 2 L 7 2 4F RT A1NM 2002071100018 20020711 00018 NM 2002 7 11 AALA20020567 1 20020425 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 797AN 30012 MIA - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 40C INOPERATIVE. REPAIRED BROKEN WIRE TO EMERGENCY ESCAPE PATH LIGHTING ON SEAT 40C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002071100019 20020711 00019 NM 2002 7 11 AALA20020615 1 20020503 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 384AA 26996 SFO - DURING OVERNIGHT MAINTENANCE, L1 EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED L1 EMERGENCY EXIT LIGHT CONTACTS AND R ELAMPED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002071100020 20020711 00020 NM 2002 7 11 AALA20020629 1 20020509 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 637AM 24595 DFW - FOUND EMERGENCY EXIT SIGN BETWEEN AFT LAVATORIES INOPERATIVE. REPAIRED BROKEN WIRE AT R4 DOOR FORWARD SIDEWALL FL OOR LEVEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002071100021 20020711 00021 EU 2002 7 11 AALA20020746 1 20020522 A 3350 POWER SUPPLY AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70079 619 POWER SUPPLY AT ROW 21 DOOR FAILED EMERGENCY LIGHT TEST. REPLACED POWER SUPPLY AT ROW 21 DOOR. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A35EU 2002071100022 20020711 00022 NM 2002 7 11 AALA20020718 1 20020517 A 7711 TRANSMITTER BOEING 757 757223 1384957 NM RT ENGINE MALFUNCTIONED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 628AA 24586 DFW - FLT 823 - EN ROUTE MIA-LAX, JUST PRIOR TO LEVELING FORM A CLIMB TO FL390, RIGHT ENGINE EPR WENT TO FULL INDICATION RESULTING IN A LOSS OF RIGHT ENGINE POWER. A DESCENT BACK TO FL350 WAS NECESSARY BECAUSE OF DECAYING AIRSPEED. AT FL3 50, SAME PROBLEMS REMAINED WITH ENGINE MATCHING ENGINE INDICATORS. RIGHT THROTTLE FOUR INCHES AHEAD OF LEFT THROTTLE DU E TO INABILITY TO GET NORMAL THRUST. LANDED IN DFW WITHOUT INCIDENT. ACCOMPLISHED MAINTENANCE CHECK MANUAL CARD 4228. NO LEAKS FOUND. ACCOMPLISHED BITE CHECK AND FOUND CODE 47. REPLACED EPR TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OP ERATION. (M) 2 L 7 2 4F RT A2NM 2002071100023 20020711 00023 NM 2002 7 11 AALA20020719 1 20020518 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 613AA 24489 SJU - FROM ROW 19 TO THE BACK OF AIRCRAFT, EMERGENCY LIGHTS WILL NOT LIGHT UP. SPLICED BAD CONNECTOR. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002071100024 20020711 00024 NM 2002 7 11 AALA20020720 1 20020517 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AA 27446 LAX - FOUND 17 SEATS 12D THROUGH 20D EMERGENCY SEAT MOUNTED LIGHTS DIM. REPLACED BATTERY PACK AT STATION 692. (M) 2 L 7 2 4F RT A2NM 2002071100025 20020711 00025 NM 2002 7 11 AALA20020721 1 20020517 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AA 27446 LAX - FOUND 17 SEATS 12D THROUGH 20D EMERGENCY SEAT MOUNTED LIGHTS DIM. REPLACED BATTERY PACK AT STATION 980. (M) 2 L 7 2 4F RT A2NM 2002071100026 20020711 00026 NM 2002 7 11 AALA20020722 1 20020518 A 3350 BATTERY BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 190AA 32384 LAX - FLT 297 - ON TAXI TO THE RUNWAY, EMERGENCY LIGHTS CAME BETWEEN ROWS 9 AND 15. RETURNED TO THE GATE. REPLACED M10 952 BATTERY MODULE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002071100027 20020711 00027 NM 2002 7 11 AALA20020727 1 20020522 A 3350 CHARGER BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 660AM 25294 JFK - FOUND EMERGENCY LIGHTS AT SEATS 17-23 ARE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY AND BATTERY CHARGER MODUL E M10800. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002071100028 20020711 00028 NM 2002 7 11 AALA20020747 1 20020522 A 3350 POWER SUPPLY BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 614AA 24490 JFK - FOUND LEFT ONE EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY M73D. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002071100029 20020711 00029 EU 2002 7 11 AALA20020794 1 20020602 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN OPEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 EMERGENCY LIGHT AT SEAT 21G INOPERATIVE. FOUND OPEN CIRCUIT ON SEAT HARNESS. REPAIRED PER MM. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A35EU 2002071100030 20020711 00030 WP 2002 7 11 AALA20020901 1 20020617 A 2560 P2070003001 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 587AA 53250 DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY PORTABLE FLASHL IGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071100031 20020711 00031 NM 2002 7 11 AALA20020904 1 20020617 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 698AN 26980 DFW - FOUND EMERGENCY LIGHTS FROM 25D GOING BACK ARE DIMMER THAN THE LIGHTS FORWARD OF THAT. REPLACED BATTERY PACK FOR THE EFFECTED LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002071100032 20020711 00032 WP 2002 7 11 AALA20020911 1 20020614 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 591AA 53254 DFW - DURING OVERNIGHT MAINTENANCE OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 26 INOPERATIVE. CLEANED OVERHEAD EMERGENCY EX IT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002071100033 20020711 00033 WP 2002 7 11 AALA20020912 1 20020617 A 2910 O-RING DOUG DC9 DC983 3022083 WP HYD SYSTEM LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 437AA 49455 PHX - FLT 471 - DURING CRUISE, NOTICED A PLUS/MINUS 200 LB FLUCTUATION IN RIGHT HYDRAULIC SYSTEM PRESSURE DURING DESCEN T. RIGHT HYDRAULIC SYSTEM PRESSURE LOW LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST FOR PRESSURE LOW LIGHT, WAS ABL E TO GET FLAPS 15 DEGREES BEFORE LOSING ALL RIGHT HYDRAULIC PRESSURE AND QUANTITY. PERFORMED EMERGENCY ALTERNATE GEAR E XTENSION. LANDED PHX WITHOUT INCIDENT. REPLACED O-RING ON RUDDER SHUTOFF VALVE PLUG. SYSTEM GROUND CHECKED NORMAL OPE RATION. (M) 2 L 7 2 4F RT A6WE 2002071100035 20020711 00035 EU 2002 7 11 AALA20020828 1 20020610 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7076A 610 DURING OVERNIGHT MAINTENANCE EMERGENCY ESCAPE PATH LIGHT AT SEAT 24G INOPERATIVE. SEATED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2002071100037 20020711 00037 WP 2002 7 11 GTIA020501 1 20020418 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - AFT PIT STATION 1155-1212 L28R, REPAIR STRAP ON DOOR JAMB BEAM HAS AREAS OF CORROSION ENTIRE LENGTH OF REPAIR. AF T PIT STATION 1155-1212 L28R EVIDENCE OF CORROSION BETWEEN SKIN/DOUBLER AND LOWER FLANGE OF DOOR JAMB BEAM. AFT CARGO F LOOR SUPPORT STATION 1155 HAS CORROSION AND DOUBLE DRILLED HOLES. REMOVED REPAIR STRAP. AFTER REMOVING STRAP AND REPAI R DOUBLER FOUND CORROSION ON DOOR BEAM TO BE OUT OF LIMITS. REMOVED DOOR JAMB CORNER ANGLE STATION 1155. CORNER ANGLE HAS CORROSION OUT OF LIMITS STATION 1155. REMOVED AFT CARGO DOOR FLOORBEAM FROM STATION 1117-1250 L28R. LOCATED AND DR ILLED NEW FLOORBEAM. INSTALLED NEW BEAM. (M) 2 L 7 2 4F A6WE 2002071100038 20020711 00038 NE 2002 7 11 HEEA079925 2 20020626 A 7200 ENGINE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE NACELLE FAILED E HEEA O OTHER L NO TEST NR NOT REPORTED 1 SW 03 3893N 6337 33010 WHEN PLACED IN MANUAL, GOVERNOR ENGINE COMPRESSOR STALLED AT APPROXIMATELY 70 & N1 SPEED. FLAME CAME OUT OF EXHAUST ST ACK. ENGINE REMOVED FOR OVERTEMP INSPECTION. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U 4 U H4SW E22EA 2002071100039 20020711 00039 2002 7 11 GTIA020637 4 20020609 A 3421 258733511 GYRO DOUG DC9 DC981 3022081 WP E/E BAY FAULTY A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 806NK 48051 FLT 779 - LGA - WITH DFGC NR 2 SELECTED AND AP ENGAGED, YOKE OSCILLATES BACK AND FORTH. REVIEWED FLIGHT LOGS ON STP FO NR 1 AND NR 2 AND DETERMINED SENSOR SIGNAL FAULTS ON NR 2 ATTITUDE SYSTEM RECORDED ON SEVERAL FLIGHT LEGS. REMOVED AND REPLACED THE NR 2 VG, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002071100040 20020711 00040 WP 2002 7 11 ZW0A0207102 1 20020708 A 3350 1315 LAMP DOUG DC9 DC983 3022083 WP BURNED OUT A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 966TW 53616 LOWER TAILCONE EMERGENCY LIGHTING INOP. RELAMPED LIGHT ASSEMBLY. LAST CHECK C PERFORMED IN STL 03/23/2001 --CLOSED-- 2 L 7 2 4F RT A6WE 2002071100041 20020711 00041 WP 2002 7 11 ZW0A0207103 1 20020708 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP DISCHARGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 966TW 53616 EMERGENCY OVERHEAD LIGHTS AT ROW 19 INOP. REPLACED BATTERIES IN BATTERY PACK. LAST CHECK C PERFORMED IN STL 03/23/2001 - -CLOSED-- 2 L 7 2 4F RT A6WE 2002071100042 20020711 00042 WP 2002 7 11 ZW0A0207104 1 20020708 A 3350 415698 LAMP DOUG DC9 DC983 3022083 WP UNSECURE A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 966TW 53616 EGRESS LIGHTING AT ROW 28 INOP. RESEATED LAMP IN SOCKET. LAST CHECK C PERFORMED IN STL 03/23/2001. --CLOSED-- 2 L 7 2 4F RT A6WE 2002071100043 20020711 00043 NE 2002 7 11 HEEA079926 2 20020626 A 7532 3043023 BLEED VALVE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 ENGINE PRODUCING LOW POWER, BLEED VALVE REPLACED 1 G 7 2 4U 4 U H4SW E22EA 2002071100044 20020711 00044 2002 7 11 GTIA020638 4 20020608 A 3421 2587335113 GYRO DOUG DC9 DC981 3022081 WP E/E BAY FAULTY A GTIA O OTHER O OTHER CL CLIMB 1 GL 23 806NK 48051 MCO - FLT 1864 - FOUND AUTOPILOT DFGC ON NR 1 HAS ERRATIC JERKING PITCH CONTROL ESPECIALLY NOTICEABLE IN CLIMB/DESCENT. REVIEWED THE FLT MEMORY LOGS ON THE NR 1 DFGC SYSTEM AND DETERMINED ATTITUDE SENSOR FAULTS ON SEVERAL FLIGHT LEGS. REM OVED AND REPLACED THE VERTICAL NR 1 VERTICAL GYRO, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002071100046 20020711 00046 2002 7 11 HEEA079928 4 20020603 A 2312 POTENTIOMETER BELL 407 407 1182206 SW TRANSCEIVER FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 740PH 53435 SOMETIMES TURNS OFF WHEN VOLUME IS ADJUSTED. FOUND WIGGLING VOLUME POTENTIOMETER CAUSES UNIT TO TURN OFF AND ON. REPLAC ED POTENTIOMETER S901. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 3U O H2SW 2002071100047 20020711 00047 2002 7 11 GTIA020639 4 20020608 A 2215 4034237905 SERVO DOUG DC9 DC981 3022081 WP AUTOPILOT SYS DAMAGED A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 806NK 48051 LGA - FLT 779 - FOUND AUTO PILOT PUMPS UP AND DOWN IN CLIMBS, TURNS AND CRUISE. DETERMINED M PINS AND P DAMAGED ON THE J2 RECEPTACLE ON THE ELEVATOR SERVO. REMOVED AND REPLACED THE ELEVATOR SERVO, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002071100048 20020711 00048 2002 7 11 HEEA079929 4 20020603 A 3452 066106200 TRANSCEIVER BELL 407 407 1182206 SW COCKPIT INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 724PH 53327 MODE "C" INTERMITTENT AND TWO DIGITS OFF. FOUND KNOB BROKEN. REPLACED FACEPLATE ASSY, REPAIRED. BENCH CHECK GOOD. 1 G 7 1 3U O H2SW 2002071100049 20020711 00049 2002 7 11 GTIA020640 4 20020609 A 2215 4034237915 SERVO DOUG DC9 DC982 3022082 WP AUTOPILOT SYS FAULTY A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 801NK 48048 TPA - FLT 632 - AUTO PILOT IS VERY SLOW TO TRIM DURING LEVEL OFFS AND WITH SPEED CHANGE. AUTO PILOT TRIM COMPARATOR LIG HT ILLUMINATES AND A/P WON'T ALWAYS CAPTURE ALTITUDE. BOTH DFGS 1 AND 2 DO THE SAME. REMOVED AND REPLACED DUPLEX ELEVA TOR SERVO DRIVE WITH SERVICEABLE UNIT. RAN RIGHTS CHECK ON NR 1 AND NR 2 SYSTEMS, BOTH SIDES GO. (M) 2 L 7 2 4F A6WE 2002071100050 20020711 00050 2002 7 11 HEEA079930 4 20020603 A 3452 RESISTOR BELL 407 407 1182206 SW TRANSCEIVER DETERIORATED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 407PH 74764 53003 DISPLAYS ERRONEOUS CODES. CLEAN SWITCH BOARD ASSY, REPAIRED, REPLACED R477 RESISTOR WHICH WAS DETERIORATED. ADJUSTED FR EQUENCY, POWER AND PULSE WIDTH. BENCH CHECK GOOD. 1 G 7 1 3U O H2SW 2002071100051 20020711 00051 2002 7 11 GTIA020642 4 20020610 A 2565 D29982125 SLIDE DOUG DC9 DC983 3022083 WP L1 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 FLL - FLT 258 - L1 DOOR SLIDE PACK FELL OFF. REMOVED AND REPLACED L1 DOOR SLIDE PACK IAW MD80 MM 25-62-00. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 2002071100052 20020711 00052 2002 7 11 HEEA079931 4 20020603 A 3452 066106200 TRANSCEIVER BELL 407 407 1182206 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 457PH 53147 TRANSCEIVER SQUAWK WAY OFF. 1 G 7 1 3U O H2SW 2002071100053 20020711 00053 2002 7 11 GTIA020643 4 20020610 A 3460 4034242923 CONTROL PANEL DOUG DC9 DC982 3022082 WP COCKPIT FAULTY A GTIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 23 801NK 48048 TPA - FLT 632 - DURING DESCENT, AUTO PILOT WILL NOT HOLD SELECTED MACH, IAS OR VERTICAL SPEED MODES. AUTO PILOT WILL TE ND TO SPEED PAST SELECTED MODE. WHILE AUTO PILOT IS SPEEDING PAST SELECTED MODE, THE AUTO PILOT TRIM ANNUNCIATOR LIGHT WILL ILLUMINATE, WHEN TURNING OFF THE AUTO PILOT TO CORRECT THE MALFUNCTION THE AIRCRAFT TENDS TO PITCH DOWN. REMOVED A ND REPLACED DFGC CONTROL PANEL. PERFORMED SYSTEM MAINTENANCE BIT SEQUENCE THREE, DIAGNOSTIC NUMBERS 146 THROUGH 177 PER MD80 MM 22-01-02, RAN RTS CHECK ON NR 1 AND NR 2 SYSTEMS IAW MD80 MM 22-01-05. (M) 2 L 7 2 4F A6WE 2002071100054 20020711 00054 WP 2002 7 11 GTIA020644 1 20020608 A 2781 CONNECTOR DOUG DC9 DC981 3022081 WP L/E SLAT DIRTY A GTIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 23 810NK 48015 ACY - FLT 1265 - AUTO SLAT FAIL LIGHT ILLUMINATED DURING FLAP EXTEND FOR T/O TESTED STALL WARN BOTH 1 AND 2 TEST WAS SAT ISFACTORY. RETURNED TO GATE FOR MAINTENANCE. TESTED AND CLEANED CONNECTORS ON GROUND PROXIMITY UNIT-CYCLED NUMEROUS TI MES, OPS CHECKS OK PER MM 32-60-04 AND 27-80-00. (M) 2 L 7 2 4F A6WE 2002071100055 20020711 00055 WP 2002 7 11 GTIA020645 1 20020609 A 5342 ATTACH ANGLE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 47605 FTW - FOUND RIGHT DORSAL FIN ATTACH ANGLE HAS CRACK (HORIZONTAL) AT FS Y1160, 2 INCHES AND .75 INCHES LONG. STOPPED DRI LLED CRACK. FABRICATED AND FORMED REPAIR ANGLES. INSTALLED REPAIR ANGLES TO RIGHT DORSAL FIN ATTACH FS Y1160. (M) 2 L 7 2 4F A6WE 2002071100056 20020711 00056 2002 7 11 GTIA020646 4 20020612 A 2210 RELAY DOUG DC9 DC982 3022082 WP AUTOPILOT SYS CORRODED A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 801NK 48048 FLT 632 - TPA - DURING CLIMBS/DESCENTS IN 'IAS' OR 'MACH' MODE, AP TRIM LIGHT ILLUMINATES. FOUND A/P TRIM RELAY CONTACT S CORRODED. REMOVED AND REPLACED RELAYS. OPS CHECKS GOOD IAW RTS 22-01-05. (M) 2 L 7 2 4F A6WE 2002071100057 20020711 00057 2002 7 11 GTIA020647 4 20020612 A 3431 6223255001 RECEIVER DOUG DC9 DC983 3022083 WP COCKPIT FAILED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 826NK 49391 OAK - FLT 249 - DFGC FMA AUTO PILOT FLIGHT DIRECTOR WOULD NOT CAPTURE GLIDE SLOPE TO GS FLAGS ON CAPTAINS SIDE. REMOVED AND REPLACED VOR/ILS RECEIVER NR 1. SYSTEM OPS CHECKS GOOD IAW MD80 MM CH 34-32-00. SWAPPED NR 1 AND NR 2 RECEIVERS. (M) 2 L 7 2 4F RT A6WE 2002071100058 20020711 00058 WP 2002 7 11 GTIA020648 1 20020614 A 2612 898400 FIRE LOOP DOUG DC9 DC982 3022082 WP FIRE DETECTION MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 804NK 49104 DEN - FLT 980 - FIRE DETECTOR LOOP LIGHT ILLUMINATED AFTER TAKEOFF AND WAS HANDLED IAW QRH. REMOVED AND REPLACED LOWER BURN B-LOOP. SYSTEM OP CHECKS GOOD. (M) 2 L 7 2 4F A6WE 2002071100059 20020711 00059 WP 2002 7 11 GTIA020650 1 20020403 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND MID CARGO FITTING STATION 827 OUTBOARD RIGHT CHAFING ELONGATED HOLES, GOUGES, BARE METAL. FABRICATED A NEW FITTING PER SPIRIT AIRLINES EA 5310-0212. (M) 2 L 7 2 4F A6WE 2002071100060 20020711 00060 WP 2002 7 11 GTIA020651 1 20020405 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND MID CARGO STATION 779 TO 826 LONGERON FITTING L30 CHAFING, GOUGES, AND CORROSION. REMOVED CORROSION, MAT FO UND TO BE OUT OF LIMITS. REPLACED LONGERON 30 END FITTING WITH NEW LONGERON END FITTING. (M) 2 L 7 2 4F A6WE 2002071100061 20020711 00061 WP 2002 7 11 GTIA020657 1 20020613 A 3231 LATCH DOUG DC9 DC982 3022082 WP RT MLG DOOR OUT OF RIG A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 823NK 48020 ORD - AFTER GEAR RETRACTION RIGHT MAIN GEAR RED LIGHT REMAINED ON. DID PROCEDURES ACCORDING TO QRH, GEAR DOOR LIGHT CAM E ON. LIGHT WENT OUT WITH RIGHT HYD PUMP ON HIGH RESTRICTED TO .70 M FOR REMAINDER OF FLIGHT. FOUND DOOR LATCH MECH OU T OF RIG. RIGGED RIGHT MAIN GEAR DOOR LATCH MECH AND MAIN GEAR UP SENSOR. SYSTEM OPS CHECK GOOD PER 32-31-04. AIRCRAF T OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 2002071100062 20020711 00062 SW 2002 7 11 HEEA079932 1 20020603 A 3246 206053184122 SKID BELL 407 407 1182206 SW MLG DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 53016 SKID TUBE HAS DAMAGE ON BOTTOM BEYOND LIMITS. SCRAPPED. 1 G 7 1 3U O H2SW 2002071100063 20020711 00063 WP 2002 7 11 GTIA020661 1 20020602 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 133NK 48111 DTW - FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY AT B5-25. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002071100064 20020711 00064 WP 2002 7 11 GTIA020662 1 20020602 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 133NK 48111 DTW - AFT FLIGHT EMERGENCY LIGHT STAY ON ALL THE TIME AND TAIL COMP EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT LEFT LAVATORY BATTERY POWER SUPPLY FOR AFT FLIGHT EMERGENCY LIGHT. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002071100065 20020711 00065 EA 2002 7 11 02191678 1 20020710 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 678BR 7653 During preflight inspection, the crew reported that the forward section of emergency floor track lighting was inoperativ e. Maintenance personnel removed and replaced the #2 emergency light inverter. An operational check was satisfactory a nd the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002071100066 20020711 00066 WP 2002 7 11 GTIA020663 1 20020602 A 3397 WIRE DOUG DC9 DC932 3022066 WP A/C BAY DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 133NK 48111 DTW - REF M-22 35589 AFT TAIL COMP WALKWAY EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRE FOR WALKWAY LIGHTS, OPS CHECK NO RMAL IAW DC9 MM 33-51-00. (M) 2 L 7 2 4F A6WE 2002071100067 20020711 00067 GL 2002 7 11 HEEA079933 2 20020603 A 7532 23005366 BLEED VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 724PH 53327 ENGINE PRODUCING HIGH MGT. REPLACED WITH SERVICEABLE BLEED VALVE. 1 G 7 1 3U 3 U O H2SW E1GL 2002071100068 20020711 00068 GL 2002 7 11 HEEA079934 2 20020603 A 7261 23066697 FILTER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE OIL BYPASSING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 498PH 53399 ENGINE OIL FILTER BYPASS POPPED. REPLACED WITH SERVICEABLE FILTER. 1 G 7 1 3U 3 U O H2SW E1GL 2002071100069 20020711 00069 GL 2002 7 11 HEEA079935 2 20020603 A 7261 23066697 FILTER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE OIL BYPASSING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8595X 53267 CEFA FILTER BUTTON BYPASSED. REPLACED WITH SERVICEABLE FILTER. 1 G 7 1 3U 3 U O H2SW E1GL 2002071100070 20020711 00070 WP 2002 7 11 GTIA020666 1 20020508 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT CARGO STATION 1079 L30 LIGHT CORROSION PREVIOUSLY BLENDED. AFT CARGO STATION 1022 L30 CORROSION ON LONG ERON. MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED LONGERON 30 FROM STATION 1007 TO STATION 1098. FABRICATED LONG ERON 30 PER EA 5310-0213. INSTALLED LONGERON 30 FROM STATION 1007 TO 1136. (M) 2 L 7 2 4F A6WE 2002071100071 20020711 00071 SW 2002 7 11 HEEA079936 1 20020603 A 7120 23069751 MOUNT BELL 407 407 1182206 SW ENGINE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 493PH 53393 ENGINE MOUNT HAS A BEARING WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U O H2SW 2002071100073 20020711 00073 GL 2002 7 11 HEEA079939 2 20020603 A 7310 CONNECTOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ECU CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 719PH 2325 53266 FADEC FAULT AND FADEC DEGRADE LIGHT ILLUMINATED. ECU HAS CORROSION ON CONNECTOR AND HAD QUIET MODE SWITCH FAULT INDICAT ED. REPLACED WITH SERVICEABLE ECU. 1 G 7 1 3U 3 U O H2SW E1GL 2002071100074 20020711 00074 GL 2002 7 11 HEEA079940 2 20020603 A 7320 23072725 HMU BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUEL CONTROL MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 723PH 3028 53283 WHEN HMU IS PLACED IN MANUAL MODE, NG DECAYS TO 54.9 PERCENT WITH HORN COMING ON. REPLACED WITH SERVICEABLE HMU. 1 G 7 1 3U 3 U O H2SW E1GL 2002071100075 20020711 00075 SW 2002 7 11 HEEA079941 1 20020603 A 2432 31908001 BATTERY BELL 407 407 1182206 SW MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 417PH 53038 BATTERY WEAK. REPLACED WITH SERVICEABLE BATTERY. 1 G 7 1 3U O H2SW 2002071100076 20020711 00076 SW 2002 7 11 HEEA079942 1 20020603 A 5343 400052007109 BEAM BELL 407 407 1182206 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 MOUNTING HARDWARE FROZEN IN BEAM ASSY. UPON REMOVAL FOUND INNER BUSHING FACE CORRODED BEYOND LIMITS. SCRAPPED. 1 G 7 1 3U O H2SW 2002071100077 20020711 00077 SW 2002 7 11 HEEA079943 1 20020603 A 6310 SEAL BELL 407 407 1182206 SW SUPPORT LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8595X A1136 53267 LEAKING FROM AFT SUPPORT. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U O H2SW 2002071100078 20020711 00078 SW 2002 7 11 HEEA079944 1 20020603 A 5210 PANEL BELL 407 407 1182206 SW CREW DOOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 720PH 53277 LT CREW DOOR TRIM PANEL CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1 G 7 1 3U O H2SW 2002071100079 20020711 00079 SW 2002 7 11 HEEA079945 1 20020603 A 5210 407070620138 PANEL BELL 407 407 1182206 SW CREW DOOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 720PH 53277 R/H CREW DOOR TRIM PANEL CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1 G 7 1 3U O H2SW 2002071100080 20020711 00080 SW 2002 7 11 HEEA079946 1 20020603 A 5210 407070620157 PANEL BELL 407 407 1182206 SW CREW DOOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 720PH 53277 LT AFT DOOR TRIM PANEL CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1 G 7 1 3U O H2SW 2002071100081 20020711 00081 SW 2002 7 11 HEEA079947 1 20020603 A 5260 407303003 STEP BELL 407 407 1182206 SW CREW DOOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 457PH 53147 FLIGHT STEP CORRODED AROUND BOLT HOLES. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U O H2SW 2002071100082 20020711 00082 SW 2002 7 11 HEEA079948 1 20020603 A 3212 407304225 GUARD BELL 407 407 1182206 SW FLOAT BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 EMERGENCY FLOAT GUARD HAS END BROKEN. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U O H2SW 2002071100083 20020711 00083 SW 2002 7 11 HEEA079950 1 20020603 A 5600 407540009 TRACK BELL 407 407 1182206 SW DOOR WINDOW CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 405PH 53207 COPILOT DOOR WINDOW HAS CORRODED SLIDING WINDOW TRACK. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U O H2SW 2002071100084 20020711 00084 SW 2002 7 11 HEEA079951 1 20020603 A 5610 407540010 TRACK BELL 407 407 1182206 SW COCKPIT WINDOW CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 405PH 53207 PILOT DOOR WINDOW HAS CORRODED SLIDING WINDOW TRACK. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U O H2SW 2002071100085 20020711 00085 SW 2002 7 11 HEEA079952 1 20020603 A 5630 407540119 WINDOW BELL 407 407 1182206 SW LT DOOR BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 720PH 53277 LT FWD DOOR SLIDING WINDOW BROKEN. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U O H2SW 2002071100086 20020711 00086 SW 2002 7 11 HEEA079953 1 20020603 A 3320 4596 LIGHT BELL 407 407 1182206 SW CABIN BURNED OUT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 490PH 53378 LIGHT BURNED OUT. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U O H2SW 2002071100087 20020711 00087 SW 2002 7 11 HEEA079954 1 20020603 A 3350 4596 LIGHT BELL 407 407 1182206 SW CABIN BURNED OUT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 490PH 53378 LIGHT BURNED OUT. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U O H2SW 2002071100088 20020711 00088 WP 2002 7 11 GTIA020668 1 20020510 A 2740 591096271 JACKSCREW DOUG DC9 DC982 3022082 WP HORIZ STAB EXCESS PLAY A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND HORIZONTAL STABILIZER DRIVE ACME SCREW/NUT FREE PLAY AT .003 INCH AND END PLAY AT .036 INCH OUT OF LIMITS. REMOVED HORIZONTAL STABILIZER JACK SCREW. INSTALLED JACKSCREW IAW MD80 MM 27-40-01. (M) 2 L 7 2 4F A6WE 2002071100089 20020711 00089 GL 2002 7 11 HEEA079955 2 20020603 A 7313 47101 FUEL NOZZLE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 510PH 53209 DELAYED LIGHT OFF. NOZZLE FLOW RATE TESTED AT THE MINIMUM FLOW RATE AT 125 PSIG. INSPECTED NOZZLE UNDER MAGNIFICATION, CHECK OK. RE-SHIMMED TO ADJUST FUEL RATE TO A HIGHER SETTING. UNIT TESTED SATISFACTORY. 1 G 7 1 3U 3 U O H2SW E1GL 2002071100090 20020711 00090 2002 7 11 HEEA079956 4 20020603 A 3422 5050031904 GYRO BELL 407 407 1182206 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8595X 53267 DG FLAGS OFF AND SPINS IN FLIGHT. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U O H2SW 2002071100091 20020711 00091 2002 7 11 HEEA079957 4 20020603 A 3120 M803B205VBATT CLOCK BELL 407 407 1182206 SW COCKPIT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 495PH 53397 GROUND CLIP FOR BATTERY BROKEN. 1 G 7 1 3U O H2SW 2002071100092 20020711 00092 WP 2002 7 11 GTIA020669 1 20020517 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FLOOR PANEL NR 15 RIGHT SIDE STATION 120 TO STATION 160 HAS CORROSION ATTACHING PANEL PAD. MATERIAL LOSS FO UND TO BE OUT OF LIMITS. REMOVED DAMAGED PADS. INSTALLED PAD IAW MD80 SRM 51-20-00. (M) 2 L 7 2 4F A6WE 2002071100094 20020711 00094 NM 2002 7 11 CALA0200393 1 20020709 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 500D CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND A 1/2" CRACK IN STRINGER 16R AFT OF STA 500D. THE CRACKED SECTION OF STRINGER WAS REMOVED AND A NEW STR INGER WAS INSTALLED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2002071100095 20020711 00095 SW 2002 7 11 HEEA079959 1 20020604 A 2840 473203003 SIGNAL COND UNIT BELL 412 412 1182202 SW FUEL SYSTEM READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 READS 200 LBS. LOW. WOULD NOT STAY ADJUSTED. 1 G 7 2 4U H4SW 2002071100096 20020711 00096 SO 2002 7 11 C2XA02CL144 1 20020710 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 13949 145057 CLE FLIGHT#3237 THE CREW REPORTED THE EMERGENCY EXIT ROW LIGHT AT 12C WAS INOPERATIVE.MAINTENANCE REPLACED THE #5 INVERT ER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002071100097 20020711 00097 EA 2002 7 11 SWIA200211021 1 20020705 A 5242 SERVICE DOOR CNDAIR CL600 CL6002B19 1900309 EA ELECTRICALF OPEN A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 907SW 7511 LOUD WHINE COMING FROM FRONT OF THE AIRCRAFT AFTER TAKEOFF. NOISE INCREASED WITH SPEED INCREASE. RETURNED TO LAX. FOU ND NOSE ELECTRICAL SERVICE PANEL DOOR OPEN. INSPECTED DOOR, FOUND NO DAMAGE. ALL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002071100098 20020711 00098 EA 2002 7 11 SWIA200211030 1 20020707 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERG LIGHTS DISCHARGED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 426SW 7468 AFT SECTION OF FLOOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 23-51-04. 2 L 7 2 4F RT A21EA 2002071100099 20020711 00099 NM 2002 7 11 SABA020071 1 20020708 A 3350 1306 LIGHT DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 801WP 086 DURING POST-FLIGHT INSPECTION THE EMERGENCY FLOOR LIGHT AT ROW SEVEN WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED BU LB AND SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002071100100 20020711 00100 SO 2002 7 11 C2XA02BT031 1 20020710 A 3320 HARNESS EMB 135 EMB135LR 3260305 SO FAULTY A C2XA O OTHER O OTHER UK UNKNOWN 1 SW 27 29515 145309 DSM/EWR---CO3463, CREW REPORTED "BURNING SMELL COMING FROM SIDEWALL PANEL IN ROW 4 SEAT A....MAINTENANCE IN DSM RELEASED AIRCRAFT IAW MEL #33-20-00 CATEGORY "C" PLACARD #023338 AIRCRAFT RETURNED TO SERVICE. CO 4362, EWR MAINTENANCE CLEARE D PLACARD BY REMOVING AND REPLACEING SIDEWALL LIGHTING HARNESS ASSEMBLY IAW EMB145 MM #33-21-00 OPS. CHECKED GOOD. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002071100101 20020711 00101 SW 2002 7 11 HEEA079960 1 20020607 A 5610 PHI206L3646 WINDOW BELL 206 206L3 1182108 SW COCKPIT DEPARTED E HEEA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SW 03 6603X 51412 LT SLIDING WINDOW DEPARTED THE AIRCRAFT. LEFT SEAT AND ALL OTHER PASSENGER SEATS WERE UNOCCUPIED. NO DAMAGE TO AIRCRAFT . 1 G 7 1 3U H2SW 2002071100102 20020711 00102 WP 2002 7 11 ABXA020035 1 20020605 A 5511 59225782 STRINGER DOUG DC9 DC941 302207N WP RT. O/B STAB. CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 962AX 47768 RIGHT STAB. INTERIOR, #3 UPPER STRINGER, WAS CRACKED AT XHS 158, 1" INBOARD TO OUTBOARD OF RIB. REPAIRED #3 STRINGER IAW DC-9 SRM 55-02. 2 L 7 2 4F A6WE 2002071100103 20020711 00103 WP 2002 7 11 ABXA020036 1 20020605 A 5511 59225782 STRINGER DOUG DC9 DC941 302207N WP RT. O/B STAB. CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 962AX 47768 RIGHT STAB. INTERIOR #2 UPPER STRINGER, WAS CRACKED AT XHS 204.1, APPROXIMATELY 1.5" INBOARD TO OUTBOARD OF RIB. REPAIRE D #2 STRINGER IAW DC-9 SRM 55-02. 2 L 7 2 4F A6WE 2002071100104 20020711 00104 WP 2002 7 11 ABXA020039 1 20020606 A 5700 99193317 FORMER DOUG DC9 DC932 3022066 WP LEFT WING L/E CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 901AX 47381 3RD LEADING EDGE NOSE RIB, OUTBOARD OF #11 SLAT TRACK, WAS CRACKED AT FASTENER, LOWER FORWARD END. REPLACED LEFT WING LE ADING EDGE RIB FORMER IAW DC-9 SRM 51-30-2, 51-30-5 AND 51-10-3. 2 L 7 2 4F A6WE 2002071100105 20020711 00105 WP 2002 7 11 ABXA020040 1 20020607 A 5700 99118777 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 901AX 47381 CANTED FRAME 1137 HAD 2 EACH CRACKS COMMON TO STIFFENERS AT 11 AND 1 O'CLOCK POSITIONS. REPLACED LEFT AND RIGHT FRAMES I AW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002071100106 20020711 00106 WP 2002 7 11 ABXA020041 1 20020618 A 5230 59101575 PAN DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 AFT LOWER CARGO DOOR INNER PAN, WAS CRACKED IN RADIUS BELOW AFT LATCH. REPAIRED AREA IAW DC-9 SRM 52-05. 2 L 7 2 4F A6WE 2002071100107 20020711 00107 WP 2002 7 11 GTIA020670 1 20020510 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND MID PIT CORROSION AT LONGERON 29L STATION 636-655, MID PIT CORROSION AT LONGERON. INSTALLED LONGERON SPLICE AT STATION 579-596. INSTALLED NEW LONGERON 30. FABRICATED AFT LONGERON 30 SPLICE. INSTALLED NEW AFT SPLICE AT LONGER ON 30 IAW MD80 SRM 51-3-5. (M) 2 L 7 2 4F A6WE 2002071100108 20020711 00108 NE 2002 7 11 HEEA079961 2 20020607 A 7323 25249995 GOVERNOR BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE MALFUNCTIONED E HEEA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 03 33008 36004 ON TAKEOFF, EXPERIENCED A TORQUE SPLIT. MAINTENANCE REPLACED THE #1 ENGINE GOVERNOR DUE TO LOW SIDE FAILURE. 1 G 7 2 4U 4 U H4SW E22EA 2002071100109 20020711 00109 WP 2002 7 11 GTIA020671 1 20020519 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT STATION 1130-1136 AND 1166-1170 L-30, CORROSION ON SKIN HIDDEN DAMAGE, FOUND AFTER LONGERON REMOVAL. FA BRICATED REPAIR DOUBLERS FOR SECTIONS 7, 8 AND 9 ALSO INCORPORATED DAMAGE ON 18-N-162 INTO REPAIR OF 7/8. FABRICATED RE PAIR DOUBLERS FOR SECTIONS 10 AND 4, OF ATTACHED DRAWINGS. REMOVED DAMAGED AREA OF SECTION NR 10. FABRICATED FILLER. INSTALLED DOUBLER FOR SECTION NR 4 AND 10 AND FILLER FOR SECTION NR 10. INSTALLED DOUBLERS FOR SECTIONS 7, 8, AND 9. ( M) 2 L 7 2 4F A6WE 2002071100110 20020711 00110 SW 2002 7 11 HEEA079962 1 20020607 A 5302 214021101111 SPAR BELL 214 214ST 1182106 SW TAIL BOOM CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 SPAR HAS CORROSION PITTING IN SEVERAL AREAS. 2 G 7 2 4U H10SW 2002071100111 20020711 00111 WP 2002 7 11 GTIA020672 1 20020519 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT PIT STATION 1130-1136 AND 1183-1189 CORROSION UNDER DOUBLER AT LONGERON 30, HIDDEN DAMAGE FOUND AFTER LO NGERON REMOVAL. AFT CARGO LONGERON 30 SPLICE STATION 1193-1240 HAS CORROSION. STRAP DOUBLER ARE OUT OF LIMITS. FABRIC ATED STRAP DOUBLER, FROM CONT LINE 1 FOUND LONGERON 30 SECTION TO BE OUT OF LIMITS. FABRICATED LONGERON 30 FROM 1193-12 40. INSTALLED STRAP DOUBLER. INSTALLED LONGERON 30 FROM STATION 1193-1240. FABRICATED A NEW LONGERON 30 PER SPIRIT AI RLINES EA 5310-0227. (M) 2 L 7 2 4F A6WE 2002071100112 20020711 00112 WP 2002 7 11 GTIA020673 1 20020514 A 5330 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT B/B DOUBLER AT STATION 1309, LONGERON 22L HAS CORROSION. REMOVED DOUBLER, PLATE AROUND NOZZLE VALVE, DU E TO CORROSION FOUND TO BE WITHOUT LIMITS. DRILLING AND LOCATE HOLES. INSTALLED NEW PART DOUBLER. (M) 2 L 7 2 4F A6WE 2002071100113 20020711 00113 WP 2002 7 11 GTIA020674 1 20020518 A 5230 FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FORWARD LOWER CARGO DOOR RUSTED/OXIDIZER AT UPPER FITTING NUTS AND BOLTS 4 EACH. AFTER REMOVAL OF RUSTED BO LTS FOUND AFT UPPER FITTING UNDERNEATH CRACKED. REMOVED CRACKED AFT UPPER FITTING. FABRICATED FITTING USING. INSTALLE D NEW FITTING. (M) 2 L 7 2 4F A6WE 2002071100114 20020711 00114 WP 2002 7 11 GTIA020675 1 20020512 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT CARGO CORNER SUPPORT STATION 1155 HAS CORROSION. FABRICATED NEW CORNER SUPPORT. INSTALLED CORNER SUPPO RT STATION 1155 IAW SRM MD80 51-30-5. (M) 2 L 7 2 4F A6WE 2002071100115 20020711 00115 WP 2002 7 11 GTIA020678 1 20020619 A 2740 575600015 SENSOR DOUG DC9 DC983 3022083 WP COCKPIT FAILED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 827NK 49793 DTW - FLT 237 - FOUND HORIZONTAL STABILIZER AUDIO SIGNAL IS NOT SOUNDED AND NO VOCAL WARNING IN AUTO PILOT MODE, AND MAN UAL IN FLIGHT AND GROUND OPS. REMOVED AND REPLACED HORIZONTAL MOTION SENSOR (U10-120) AND OPS NORMAL AS PER MM 27-40-11 . (M) 2 L 7 2 4F RT A6WE 2002071100116 20020711 00116 2002 7 11 GTIA020679 4 20020619 A 2215 4034237915 SERVO DOUG DC9 DC983 3022083 WP AUTOPILOT SYS FAULTY A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 827NK 49793 DTW - ERRATIC AUTO PILOT IN TURN'S WITH DFGS NR 2 AUTO PILOT DISCONNECTED IN TURNS. REMOVED AND REPLACED AILERON SERVO IAW MM 22-10-00, OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 2002071100117 20020711 00117 SW 2002 7 11 HEEA079963 1 20020607 A 7714 222375022111 INDICATOR BELL 222 222 1182122 SW ENGINE NG INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INDICATOR INOPERATIVE. 1 G 7 2 3U H9SW 2002071100118 20020711 00118 SW 2002 7 11 HEEA079964 1 20020607 A 7933 214040865101 MONITOR BELL 214 214ST 1182106 SW OIL COOLER MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 59805 28141 SWITCH WILL NOT EXTINGUISH OIL COOLER LIGHT ON A/C UNLESS THE UNIT IS TAPPED ON WHILE A/C IS OPERATING IN THE PROPER RAN GE. 2 G 7 2 4U H10SW 2002071100119 20020711 00119 SW 2002 7 11 HEEA079965 1 20020607 A 3213 206053203103 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 6160Z 51610 CORRODED BEYOND LIMITS. SCRAPPED TUBE. 1 G 7 1 3U H2SW 2002071100120 20020711 00120 SW 2002 7 11 HEEA079966 1 20020607 A 3213 206053203117 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 8591X 51495 CORRODED BEYOND LIMITS. SCRAPPED TUBE. 1 G 7 1 3U H2SW 2002071100121 20020711 00121 SW 2002 7 11 HEEA079967 1 20020607 A 3213 206053203103 CROSSTUBE BELL 206 206L1 1182107 SW MLG CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5742N 45477 CORRODED BEYOND LIMITS. SCRAPPED TUBE. 1 G 7 1 3U H2SW 2002071100122 20020711 00122 SW 2002 7 11 HEEA079968 1 20020607 A 3213 206053203103 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 CORROSION PITTING IN CURVE. SCRAPPED TUBE. 1 G 7 1 3U H2SW 2002071100123 20020711 00123 SW 2002 7 11 HEEA079969 1 20020607 A 3213 206053203103 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 CORROSION. SCRAPPED TUBE. 1 G 7 1 3U H2SW 2002071100124 20020711 00124 SW 2002 7 11 HEEA079970 1 20020607 A 3213 206053203103 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 CORROSION. SCRAPPED TUBE. 1 G 7 1 3U H2SW 2002071100125 20020711 00125 SW 2002 7 11 HEEA079971 1 20020607 A 3213 206053203101 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 CORROSION. SCRAPPED TUBE. 1 G 7 1 3U H2SW 2002071100126 20020711 00126 SW 2002 7 11 HEEA079972 1 20020607 A 3213 206053203101 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 CORROSION. SCRAPPED TUBE. 1 G 7 1 3U H2SW 2002071100127 20020711 00127 SW 2002 7 11 HEEA079973 1 20020607 A 3213 206053203101 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 CORROSION. SCRAPPED TUBE. 1 G 7 1 3U H2SW 2002071100128 20020711 00128 SW 2002 7 11 HEEA079974 1 20020607 A 3213 206053203101 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 4835 51131 CROSSTUBE HAS CORROSION. SCRAPPED TUBE. 1 G 7 1 3U H2SW 2002071100129 20020711 00129 SO 2002 7 11 SIMA200214701 1 20020528 A 5320 14521725001 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 ABI - THIS IS A LEVEL 2 FINDING, GALLEY LEFT SILL HAS CORROSION. INSTALLED SERVICEABLE SILL IAW EMB145 SRM 51-20-03, 51 -40-06 AND 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002071100130 20020711 00130 SO 2002 7 11 SIMA200214702 1 20020528 A 5320 14521725015 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 ABI - THIS IS A LEVEL 2 FINDING, GALLEY RIGHT AFT SILL HAS CORROSION. INSTALLED SERVICEABLE AFT SILL IAW EMB145 SRM 51- 40-02. (M) 2 L 7 2 4T RT T00011AT 2002071100131 20020711 00131 SO 2002 7 11 SIMA200214703 1 20020528 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 THIS IS A LEVEL 2 FINDING, LEFT OMEGA BEAM PREVIOUS REPAIR AT FRAME 20 HAS CORROSION. INSTALLED SERVICEABLE REPAIR DOUB LER, FILLER, PLATE AND SHIMS IAW EMB145 SRM 53-21-10. (M) 2 L 7 2 4T RT T00011AT 2002071100132 20020711 00132 SO 2002 7 11 SIMA200215119 1 20020519 A 7830 833990152 SWITCH EMB 145 EMB145 3260210 SO THRUST REVERSER FAILED A SIMA E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 SW 21 607AE 145064 AMA - FLT 3861 - FLIGHT CREW REPORTED ENGINE NR 2 THRUST REVERSER HAD FAILED INDICATION ON EICAS DURING APPROACH. REPLA CED LOWER OUTBOARD STOW SWITCHES AND BOTH UPPER STOW SWITCHES S/N'S 2374, 2370. (M) 2 L 7 2 4F RT T00011AT 2002071100133 20020711 00133 SO 2002 7 11 SIMA200215711 1 20020606 A 5320 14525369003 CLIP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 ABI - DURING AN IMBV INSPECTION, FOUND CARGO DOOR CUT OUT SHEAR CLIP CORRODED. REMOVED CORRODED SHEAR CLIP. INSTALLED NEW CLIP IAW EMB 145 SRM 145/1142, CHAPTER 51, REV 18, 51-20-03, 51-40-02, ETN EM-51-020 AND STANDARD SRM PRACTICES. (M ) 2 L 7 2 4T RT T00011AT 2002071100134 20020711 00134 SO 2002 7 11 SIMA200215712 1 20020606 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 DURING AN IMBV INSPECTION, FOUND CARGO DOOR LOWER SILL PLATE BETWEEN FRAMES 65 AND 68 CORRODED. REMOVED CORRODED SILL ( BEAM). INSTALLED NEW BEAM IAW EMB 145 (SRM 145/1142, CHAPTER 51, REV 18, 51-20-03, 51-40-02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002071100135 20020711 00135 2002 7 11 HEEA079983 4 20020610 A 2312 064105430 TRANSCEIVER BELL 407 407 1182206 SW COCKPIT WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 457PH 53147 VHF WEAK. FOUND S501 SWITCH AND DS501 BULB BAD. REPLACED AND REPAIRED. ADJUSTED SIDETONE. BENCH CHECK GOOD. 1 G 7 1 3U O H2SW 2002071100136 20020711 00136 2002 7 11 HEEA079984 4 20020610 A 2562 110324 ANTENNA BELL 407 407 1182206 SW ELT BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 495PH 53397 ELT ANTENNA BROKEN. SCRAPPED. 1 G 7 1 3U O H2SW 2002071100137 20020711 00137 SW 2002 7 11 HEEA079987 1 20020610 A 6400 206011721113 HOUSING BELL 407 407 1182206 SW T/R CONTROL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 510PH 53209 TAIL ROTOR CONTROL HOUSING LEAKING. 1 G 7 1 3U O H2SW 2002071100138 20020711 00138 SW 2002 7 11 HEEA079989 1 20020610 A 3212 206050247101 COVER BELL 407 407 1182206 SW FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 END COVER WORN AND TORN. 1 G 7 1 3U O H2SW 2002071100139 20020711 00139 SW 2002 7 11 HEEA079990 1 20020610 A 3212 206050247131 COVER BELL 407 407 1182206 SW FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 END COVER WORN AND TORN. 1 G 7 1 3U O H2SW 2002071100140 20020711 00140 SO 2002 7 11 SIMA200215801 1 20020607 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON GALLEY CENTER FLOORBEAM. REMOVED CORRODED GALLEY CENTER BEAM. INST ALLED NEW CENTER BEAM IAW EMB 145 SRM 145/1142, CHAPTER 51, REV 18, 51-40-02, ETN-EM53-020, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002071100141 20020711 00141 SW 2002 7 11 HEEA079991 1 20020610 A 3212 206050247137 COVER BELL 407 407 1182206 SW FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 495PH 53397 LT AFT COVER TORN. 1 G 7 1 3U O H2SW 2002071100142 20020711 00142 SO 2002 7 11 SIMA200215802 1 20020607 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, TWO SHIMS. INSTALLED IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 18, 53-21-10, AND STAN DARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002071100143 20020711 00143 SO 2002 7 11 SIMA200215803 1 20020607 A 5311 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 ABI - DURING AN IMBV INSPECTION, FOUND LOWER PORTION OF RIGHT FRAME 72 DENTED. RECONTOURED DENT. PERFORMED NDT, NO DEF ECTS. FABRICATED TWO L SHAPE DOUBLERS. INSTALLED IAW EMB GST-1776/02, ITEM NR 3 GST-1784/02, AND STANDARD SRM PRACTICE S. (M) 2 L 7 2 4T RT T00011AT 2002071100144 20020711 00144 SW 2002 7 11 HEEA079992 1 20020610 A 3212 206050247138 COVER BELL 407 407 1182206 SW FLOAT MISMARKED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 495PH 53397 TRIED TO INSTALL FLOAT COVER ON RT AFT POSITION. COVER HAS RT TAG PART NUMBER ON TAG, LOOKS LIKE SOMEONE CHANGED THE LA ST DIGIT (7) TO AN (8). THIS IS NOT FOR THE RIGHT SIDE. THE END CAPS ARE REVERSED. THE FWD CAP IS SUPPOSED TO HAVE TH E CUT OUT FOR THE LINES AND ON THIS COVER THE CUT OUT IS IN THE BACK. 1 G 7 1 3U O H2SW 2002071100145 20020711 00145 SO 2002 7 11 SIMA200215901 1 20020608 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 ABI - DURING AN IMBV INSPECTION MAINTENANCE, FOUND CORROSION ON GALLEY RIGHT FLOORBEAM. REMOVED CORRODED GALLEY RIGHT B EAM. INSTALLED NEW BEAM IAW EMB SRM 145/1142, CHAPTER 51, REV 18, 51-40-02, GST-1826/02, ITEM NR 1, AND STANDARD SRM PR ACTICES. (M) 2 L 7 2 4T RT T00011AT 2002071100146 20020711 00146 SW 2002 7 11 HEEA079993 1 20020610 A 3246 206053184121 SKID BELL 407 407 1182206 SW MLG WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 SKID TUBE WORN BEYOND LIMITS. 1 G 7 1 3U O H2SW 2002071100147 20020711 00147 SO 2002 7 11 SIMA200216301 1 20020528 A 5320 14522459003 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 ABI - THIS IS A LEVEL 2 FINDING, GALLEY RAMP SUPPORT HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE GALLEY RAMP IAW E MB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002071100148 20020711 00148 SW 2002 7 11 HEEA079994 1 20020610 A 3246 206053184122 SKID BELL 407 407 1182206 SW MLG WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 SKID TUBE WORN BEYOND LIMITS. 1 G 7 1 3U O H2SW 2002071100149 20020711 00149 SO 2002 7 11 SIMA200216302 1 20020528 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 ABI - THIS IS A LEVEL 2 FINDING, GALLEY RIGHT HAT BEAM HAS CORROSION. INSTALLED SERVICEABLE RIGHT HAT BEAM IAW EMB145 S RM 51-40-02 AND GST-1826/02. (M) 2 L 7 2 4T RT T00011AT 2002071100150 20020711 00150 SO 2002 7 11 SIMA200216303 1 20020528 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 ABI - THIS IS A LEVEL 2 FINDING, GALLEY RIGHT SILL (FORWARD) HAS CORROSION. REMOVED AND INSTALLED FORWARD SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002071100151 20020711 00151 SO 2002 7 11 SIMA200216304 1 20020531 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 ABI - THIS IS A LEVEL 2 FINDING, CORROSION ON LEFT OMEGA BEAM UNDER EDGE OF COMPOSITE FLOOR CROSSBEAM BETWEEN FRAMES 24- 25. FABRICATED AND INSTALLED A DOUBLER, IAW EMB145 SRM 53-21-10. (M) 2 L 7 2 4T RT T00011AT 2002071100152 20020711 00152 SW 2002 7 11 HEEA079995 1 20020610 A 2435 206062200113 STARTER GEN BELL 407 407 1182206 SW ENGINE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 493PH 3269 53393 BRUSHES WORN ON 300 HOUR INSPECTION. 1 G 7 1 3U O H2SW 2002071100153 20020711 00153 SO 2002 7 11 SIMA200216516 1 20020522 A 5320 14522459003 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - THIS IS A LEVEL 2 FINDING, PAX DOOR AFT THRESHOLD SUPPORT CORRODED. REMOVED AND INSTALLED SUPPORT IAW EMB145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002071100154 20020711 00154 SW 2002 7 11 HEEA079996 1 20020610 A 2435 206062200113 STARTER GEN BELL 407 407 1182206 SW ENGINE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 3124 53159 BRUSHES WORN ON 300 HOUR INSPECTION. 1 G 7 1 3U O H2SW 2002071100155 20020711 00155 SW 2002 7 11 HEEA079997 1 20020610 A 7800 206064203101 DUCT BELL 407 407 1182206 SW EXHAUST CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 724PH 53327 DUCT ASSY CRACKED AT SEAM. 1 G 7 1 3U O H2SW 2002071100156 20020711 00156 SO 2002 7 11 SIMA200216517 1 20020524 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - THIS IS A LEVEL 2 FINDING, GALLEY RIGHT FLOORBEAM AT FRAME 20 CORRODED. REPAIRED GALLEY FLOORBEAM IAW EMB145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002071100157 20020711 00157 SO 2002 7 11 SIMA200216518 1 20020522 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - THIS IS A LEVEL 2 FINDING, RIGHT HAT BEAM AT FRAME 23 CORRODED. FABRICATED AND INSTALLED DOUBLER IAW EMB 145 GST- 1707/02. (M) 2 L 7 2 4T RT T00011AT 2002071100158 20020711 00158 SO 2002 7 11 SIMA200216519 1 20020522 A 5320 14522459003 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - THIS IS A LEVEL 2 FINDING, CENTER BEAM RAMP SUPPORT CORRODED. REMOVED AND REPLACED RAMP SUPPORT IAW EMB145 SRM 51 -20-02. (M) 2 L 7 2 4T RT T00011AT 2002071100159 20020711 00159 SO 2002 7 11 SIMA200216520 1 20020522 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - THIS IS A LEVEL 2 FINDING, LEFT CABIN SILL CORRODED BETWEEN FRAMES 19 TO 21. REMOVED AND INSTALLED SERVICEABLE SI LL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002071100160 20020711 00160 SO 2002 7 11 SIMA200216521 1 20020522 A 5320 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - FOUND LEFT OMEGA BEAM PREVIOUS REPAIR CORRODED. FABRICATED AND INSTALLED A DOUBLER IAW EMB 145 SRM 53-21-10. (M) 2 L 7 2 4T RT T00011AT 2002071100161 20020711 00161 SW 2002 7 11 HEEA080007 1 20020610 A 6321 206076047101 CYLINDER BELL 407 407 1182206 SW ROTOR BRAKE WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406PH 53198 ROTOR BRAKE WEAK - MASTER CYLINDER LEAKS INTERNALLY. 1 G 7 1 3U O H2SW 2002071100162 20020711 00162 SW 2002 7 11 HEEA080009 1 20020610 A 3212 212073905001 GAUGE BELL 407 407 1182206 SW EMERGENCY FLOAT CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 RUST INSIDE GAUGE. 1 G 7 1 3U O H2SW 2002071100163 20020711 00163 GL 2002 7 11 HEEA080010 2 20020610 A 7532 23005366 BLEED VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 03 493PH 53393 TORQUE FLUCTUATION DURING CRUISE FLIGHT. REPLACED WITH SERVICEABLE BLEED VALVE. 1 G 7 1 3U 3 U O H2SW E1GL 2002071100165 20020711 00165 GL 2002 7 11 HEEA080011 2 20020610 A 7532 23005366 BLEED VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 03 496PH 53398 ENGINE HAS LOW POWER AND HIGH TOT. REPLACED WITH SERVICEABLE BLEED VALVE. 1 G 7 1 3U 3 U O H2SW E1GL 2002071100167 20020711 00167 GL 2002 7 11 HEEA080012 2 20020610 A 7532 23005366 BLEED VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 8595X 13287 53267 HIGH TOT. REPLACED WITH SERVICEABLE BLEED VALVE. 1 G 7 1 3U 3 U O H2SW E1GL 2002071100169 20020711 00169 EA 2002 7 11 COMA0260417 1 20020707 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 721CA 10786 7259 FLIGHT 5222 GEAR DISAGREE WARNING DURING GEAR EXTENSION.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002071100170 20020711 00170 GL 2002 7 11 HEEA080013 2 20020610 A 7532 23005366 BLEED VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 724PH 53327 HIGHER THAN NORMAL TOT. REPLACED WITH SERVICEABLE BLEED VALVE. 1 G 7 1 3U 3 U O H2SW E1GL 2002071100172 20020711 00172 GL 2002 7 11 HEEA080014 2 20020610 A 7320 23007827 VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE LEAKING E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 724PH 53327 LEAKS AND OPENS INTERMITTENTLY. REPLACED WITH SERVICEABLE VALVE. 1 G 7 1 3U 3 U O H2SW E1GL 2002071100173 20020711 00173 EA 2002 7 11 COMA0260418 1 20020706 A 2750 860D10018ABCD COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 940CA 1064 7048 FLIGHT 5322 FLAPS FAIL CAUTION MESSAGE DURING LANDING.REPLACED THE FECU 2 L 7 2 4F RT A21EA 2002071100174 20020711 00174 SW 2002 7 11 HEEA080023 1 20020610 A 3212 206050247135 COVER BELL 407 407 1182206 SW FLOAT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 53159 HOOK WORN. TO BE SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. 1 G 7 1 3U O H2SW 2002071600187 20020716 00187 NM 2002 7 16 F3LA200200190 1 20020630 A 3350 58678 INVERTER BOEING 737 73736E 138443A NM CABIN FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 317FL 29 25263 DURING SERVICE CHECK, INSPECTION REPORTED EMERGENCY AISLE PATH LIGHTING IN AFT CABIN INOPERATIVE. REPLACED INVERTER, PE RFORMED OPERATIONAL TEST AND CHECKED OKAY. 2 L 7 2 4F RT A16WE 2002071100186 20020711 00186 WP 2002 7 11 AALA20020774 1 20020529 A 2560 P2070003001 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7533A 49987 DURING OVERNIGHT MAINTENANCE EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2002071100187 20020711 00187 WP 2002 7 11 AALA20020775 1 20020529 A 2560 SIGN DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33502 49739 DURING OVERNIGHT MAINTENANCE AFT EMERGENCY EXIT SIGN LEFT OF GALLEY BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2002071100188 20020711 00188 WP 2002 7 11 AALA20020777 1 20020503 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 576AA 53153 (LIGHT ASSEMBLY) DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT 7D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASS EMBLY AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2002071100189 20020711 00189 WP 2002 7 11 AALA20020778 1 20020530 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 576AA 53153 DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT ABOVE RIGHT HAND SERVICE DOOR INOPERATIVE. CLEANED EMERGENCY EXIT LIG HT GROUND CONTACT ABOVE RIGHT HAND SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2002071100190 20020711 00190 EU 2002 7 11 AALA20020779 1 20020530 A 3233 415005 ACTUATOR FOKKER F28 F28MK0100 4990807 EU LT MLG FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 1416A 11395 EN ROUTE, AFTER TAKE OFF WITH LANDING GEAR UP RECEIVED A LEFT MAIN GEAR UNSAFE LIGHT. LOWERED GEAR DOWN AND RECEIVED UN SAFE ON BOTH MAIN GEARS AND GREEN ON NOSE GEAR. RAISED GEAR AND RECEIVED UNSAFE ON LEFT MAIN LANDING GEAR AGAIN. RETUR NED, LOWERED LANDING GEAR DOWN WITH ALTERNATE SYSTEM, LANDED WITHOUT INCIDENT. REPLACED LEFT HAND MAIN GEAR RETRACT ACT UATOR. SWUNG GEAR, SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2002071100191 20020711 00191 EU 2002 7 11 AALA20020780 1 20020528 A 5315 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1414D 11377 CORROSION ON TOP OF FLOORBEAM STA 3845 TO 4610 BL1127LH. REPLACE CORROSION WITH NEW ANGLE PROCURED FROM AA STOCK. 2 L 7 2 4F RT 2002071100192 20020711 00192 EU 2002 7 11 AALA20020781 1 20020529 A 5315 4025784 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1414D 11377 (FLOORBEAM) CORROSION ON TOP OF FLOORBEAM AT BL1127R FROM STA 4610 TO 4850. REPLACE TOP OF FLOOR SUPPORT WITH ANGLE PROC URED FROM AA STOCK. 2 L 7 2 4F RT 2002071100193 20020711 00193 2002 7 11 AALA20020792 4 20020603 A 3417 ADC AIRBUS 300 A300B4605R 3930308 EU E/E BAY MALFUNCTIONED A AALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 3075A 606 EN ROUTE, AIRCRAFT AIR INTERRUPTED DUE TO CAPTAINS AIRSPEED ERRONEOUS. RETURNED AND LANDED, WITHOUT INCIDENT. REPLACED NUMBER ONE AIR DATA COMPUTER. PERFORMED VISUAL INSPECTION OF CAPTAINS PITOT AND STATIC PORTS. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A35EU 2002071100194 20020711 00194 EU 2002 7 11 AALA20020803 1 20020604 A 5312 BULKHEAD FOKKER F28 F28MK0100 4990807 EU FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1431B 11416 (AFT PRESSURE BULKHEAD) WORN AREA ON AFT PRESSURE BULKHEAD LEFT AND BELOW PRESSURE RELIEF VALVE. BLENDED OUT WORN AREA T O A DEPTH OF .010. DYE CHECKED AREA. NO CRACKS FOUND. ALODINED AND PRIMED BLEND AREA THEN INSTALLED DOUBLER PER ESO. 2 L 7 2 4F RT 2002071100195 20020711 00195 WP 2002 7 11 AALA20020837 1 20020608 A 3350 BAT5014 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 583AA 53160 (BATTERY PACK) DURING OVERNIGHT MAINTENANCE ROW 17-22, EMERGENCY EXIT LIGHTS INOPERATIVE REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2002071100196 20020711 00196 WP 2002 7 11 AALA20020838 1 20020609 A 3350 BAT5014 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7518A 49895 DURING OVERNIGHT MAINTENANCE DISCOVERED ROW 28 EMERGENCY OVERHEAD LIGHT INOPERATIVE. REPLACED BATTERY PACK SYSTEM CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 2002071100197 20020711 00197 NM 2002 7 11 AALA20020493 1 20020418 A 2910 AS11504K0232 HYDRAULIC LINE BOEING 757 757223 1384957 NM HYD SYSTEM CRACKED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 668AA 25333 DFW - FLT 1089 - EN ROUTE DFW-PDX, LEFT HYDRAULIC QUANTITY LOSS. RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED LE FT MLG SIDE STRUT ACTUATOR DOWN HOSE WITH TEMPORARY HOSE. SERVICED LEFT HYDRAULIC SYSTEM RESERVOIR. LEAK AND OPERATION S CHECKED NORMAL. (M) 2 L 7 2 4F RT A2NM 2002071100198 20020711 00198 NM 2002 7 11 AALA20020516 1 20020422 A 2910 271N61192 HYDRAULIC LINE BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 633AA 24591 DFW - FLT 742 - EN ROUTE DFW-LGA, LEFT HYDRAULIC QUANTITY LOW CAUTION FOLLOWED BY LEFT HYDRAULIC PRESSURE FAILURE. RETU RNED AND LANDED DFW WITHOUT INCIDENT. FOUND LEFT MAIN GEAR DOWN LOCK FLEX LINE LEAKING. SYSTEM GROUND CHECKED NORMAL O PERATION. (M) 2 L 7 2 4F RT A2NM 2002071100199 20020711 00199 NM 2002 7 11 AALA20020558 1 20020426 A 2161 CONTROLLER BOEING 757 757223 1384957 NM E/E BAY FAILED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 656AA 24614 SJU - FLT 1013 - EN ROUTE BOS-AUA - UNABLE TO CONTROL COCKPIT OR CABIN TEMPERATURE IN MANUAL OR AUTOMATIC MOD. ALL 3 ZO NE TEMPERATURE CONTROL VALVE CIRCUIT BREAKERS POPPED. AIR INTERRUPTED AND LANDED SJU WITHOUT INCIDENT. REPLACED CABIN ZONE TEMPERATURE CONTROLLER PER MM. CLEANED THREE CABIN TEMPERATURE SENSORS. OPERATIONS CHECKED ALL THREE ZONE TEMPERA TURES AND FOUND WORKING. RESET ZONE TEMPERATURE CIRCUIT BREAKERS. (M) 2 L 7 2 4F RT A2NM 2002071100200 20020711 00200 NM 2002 7 11 AALA20020583 1 20020501 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 614AA 24490 DFW - NR 1 LEFT DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR NR 1 LEFT DOOR SLIDE. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002071100201 20020711 00201 NM 2002 7 11 AALA20020616 1 20020503 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 MIA - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY PATH LIGHTING AT 34H INOPERATIVE. REPAIRED BROKEN WIRE FOR E MERGENCY PATH LIGHTING AT SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002071100202 20020711 00202 NM 2002 7 11 AALA20020617 1 20020502 A 3350 S283T0143 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39365 24046 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS AT 2-11H INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH L IGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002071100203 20020711 00203 NM 2002 7 11 AALA20020618 1 20020503 A 2497 MPN332W5200104 WIRE HARNESS BOEING 777 777223 1385213 NM RT ENGINE DAMAGED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 21 785AN 30005 ONE HOUR INTO FLIGHT, RIGHT GENERATOR CONTROL LIGHT ILLUMINATED, ACCOMPLISHED CHECKLIST, ONE RESET ATTEMPTED, WOULD NOT RESET. REMOVED AND REPLACED NR 2 ENGINE IDG PER MM. LEAK CHECKS GOOD. FOUND DAMAGED WIRE HARNESS. REMOVED AND REPLAC ED THE RIGHT ENGINE IDG HARNESS ASSEMBLY 332W5200-104. RIGHT IDG OPS CHECKED GOOD. (M) 2 L 7 2 4F RT T00001SE 2002071100204 20020711 00204 NM 2002 7 11 AALA20020624 1 20020508 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 751AN 30798 DFW - DURING OVERNIGHT MAINTENANCE, LEFT SIDE WALL FORWARD GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FIRST CLAS S GALLEY EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002071100205 20020711 00205 EU 2002 7 11 AALA20020625 1 20020507 A 5312 DOUBLER FOKKER F28 F28MK0100 4990807 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1420D 11403 TUL - FOUND INTERIOR DOUBLER CRACKED AFT SIDE OF FORWARD PRESSURE BULKHEAD, D22213-079 FUSE FRAME REINFORCEMENT CHIP. F ABRICATED REPAIR DOUBLER AND INSTALLED PER ESO 51000. (M) 2 L 7 2 4F RT 2002071100206 20020711 00206 NM 2002 7 11 AWXA200200593 1 20020705 A 2421 BACC63CE2822S PLUG BOEING 737 7373Q8 1384670 NM WG DISC STA 219L SHORTED A AWXA A UNSCHED LANDING J S H WARNING INDICATION AFFECT SYSTEMS ELECT. POWER LOSS-50 PC CL CLIMB 1 WP 28 327AW 0 0 23507 PHX - AIR TURN BACK - FLT 7811 - ON TAKEOFF FROM PHX EN ROUTE TO SFO PRIOR TO 3000 FT, PRESSURE AUTO FAIL LIGHT ILLUMINA TED AND WHILE PASSING 7000 FT THE #1 GENERATOR BUS FAILED, VOLTS AND FREQUENCY CHECKED OK. GENERATOR WAS BROUGHT BACK ON LINE AT THIS TIME AND THE #1 TRANSFORMER RECTIFIER (TR) AND NORMAL EQUIPMENT COOLING CIRCUIT BREAKERS WERE FOUND POPPED. AIRCRAFT RETURNED TO PHX. MAINTENANCE REPLACED THE #1 ENGINE GENERATOR CIRCUIT BREAKER, AND DURING ENGINE RUN WITH #1 T R AND #1 GENERATOR EQUIPMENT COOLING NORMAL, THE "B" SYSTEM ELECTRIC PUMP C/B POPPED AND #1 GENERATOR CYCLED ON AND OFF. MAINTENANCE REPLACED THE #1 ENGINE 40KVA ELECTRIC GENERATOR IAW T/C R5M24002, THE GENERATOR BUS TIE BREAKER, AND THE GE 2 L 7 2 4F RT A16WE 2002071200001 20020712 00001 GL 2002 7 12 HEEA080015 2 20020610 A 7261 23066697 FILTER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE OIL BYPASSING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 501PH 53401 ENGINE OIL FILTER BYPASS INDICATOR OUT. REPLACED WITH SERVICEABLE FILTER. 1 G 7 1 3U 3 U O H2SW E1GL 2002071200002 20020712 00002 GL 2002 7 12 HEEA080016 2 20020610 A 7261 23066697 FILTER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE OIL BYPASSING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 493PH 53393 CEFA LUBE SIDE BYPASS INDICATOR EXTENDED. REPLACED WITH SERVICEABLE FILTER. 1 G 7 1 3U 3 U O H2SW E1GL 2002071200003 20020712 00003 GL 2002 7 12 HEEA080017 2 20020610 A 7261 23066697 FILTER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE OIL BYPASSING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 719PH 53266 BYPASS BUTTON POPPED. REPLACED WITH SERVICEABLE FILTER. 1 G 7 1 3U 3 U O H2SW E1GL 2002071200004 20020712 00004 SW 2002 7 12 HEEA080018 1 20020610 A 7722 23072790 ECU BELL 407 407 1182206 SW ENGINE MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 724PH 53327 HIGH PITCH SCREECHING SOUND AT END OF N1 SPILLDOWN. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U O H2SW 2002071200005 20020712 00005 SW 2002 7 12 HEEA080019 1 20020610 A 2432 31908001 BATTERY BELL 407 407 1182206 SW MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 722PH 53288 BATTERY WEAK. 1 G 7 1 3U O H2SW 2002071200006 20020712 00006 SW 2002 7 12 HEEA080020 1 20020610 A 6300 406010413119 TUBE BELL 407 407 1182206 SW PITCH LINK CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 PITCH LINK TUBE HAS CORROSION. 1 G 7 1 3U O H2SW 2002071200007 20020712 00007 SW 2002 7 12 HEEA080021 1 20020610 A 2842 206364601101 TRANSMITTER BELL 206 206L3 1182108 SW FUEL QTY READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 GAUGE FLUCTUATES AND READS 200 LBS. LOW. 1 G 7 1 3U H2SW 2002071200008 20020712 00008 SW 2002 7 12 HEEA080022 1 20020610 A 2841 473203003 SIGNAL COND UNIT BELL 412 412 1182202 SW FUEL QTY MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 LOW FUEL LIGHT ON WHEN FUEL FULL. 1 G 7 2 4U H4SW 2002071200009 20020712 00009 SW 2002 7 12 HEEA080024 1 20020610 A 6300 406010417101 BEARING BELL 407 407 1182206 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 720PH 53277 MAIN ROTOR BEARING WORN. 1 G 7 1 3U O H2SW 2002071200010 20020712 00010 SW 2002 7 12 HEEA080025 1 20020610 A 6710 406010425107 LEVER BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 720PH 53277 MAIN ROTOR LEVER ASSY HAS CORROSION. 1 G 7 1 3U O H2SW 2002071200011 20020712 00011 SW 2002 7 12 HEEA080026 1 20020610 A 6710 406010426101 LINK BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 720PH 2886 53277 MAIN ROTOR LINK ASSY WORN AND CORRODED. 1 G 7 1 3U O H2SW 2002071200012 20020712 00012 SW 2002 7 12 HEEA080027 1 20020610 A 6230 406010428109 BUSHING BELL 407 407 1182206 SW HUB SET CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 720PH 53277 HUB SET BUSHING WORN AND CORRODED. 1 G 7 1 3U O H2SW 2002071200014 20020712 00014 SW 2002 7 12 HEEA080028 1 20020610 A 6720 406012129101 LINK BELL 407 407 1182206 SW TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 494PH 53396 TAIL ROTOR LINK ASSY HAS WORN BEARINGS. 1 G 7 1 3U O H2SW 2002071200015 20020712 00015 SO 2002 7 12 ASOA02293 1 20020525 A 5280 BRACKET EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE LT MLG DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 286AS 24171 120268 DURING HANGER MAINTENANCE, THE LEFT MAIN LANDING GEAR FORWARD OUTBOARD DOOR AFT TENSIONER BRACKET HAD A CRACK. THE LEFT MAIN LANDING GEAR FORWARD INBOARD DOOR AFT HINGE ANGLE WAS ALSO DISCOVERED WITH A CRACK. MAINTENANCE REMOVED AND REPLA CED BOTH THE CRACKED TENSIONER BRACKET AND THE CRACKED HINGE ANGLE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002071200016 20020712 00016 SO 2002 7 12 ASOA02303 1 20020527 A 5320 12005805003 BUTT STRAP EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 257AS 120126 DURING C CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND CORRODED BEYOND LIMITS BETWEEN FRAMES 16 AND 21 AS WELL AS BE TWEEN STA 6653.1 AND FRAME 26. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTIONS OF BUTT STRAP IAW SRM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002071200017 20020712 00017 SW 2002 7 12 HEEA080043 1 20020610 A 6310 406040500131 FREEWHEEL UNIT BELL 407 407 1182206 SW MAIN ROTOR LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 741PH 53457 FREEWHEEL UNIT LEAKING. 1 G 7 1 3U O H2SW 2002071200018 20020712 00018 SW 2002 7 12 HEEA080044 1 20020610 A 6310 406040500131 FREEWHEEL UNIT BELL 407 407 1182206 SW MAIN ROTOR LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 407PH 53003 FREEWHEEL UNIT LEAKING. REPAIRED AND RETURNED TO SERVICE. 1 G 7 1 3U O H2SW 2002071200019 20020712 00019 SW 2002 7 12 HEEA080045 1 20020610 A 6710 406310405101 UNIVERSAL BELL 407 407 1182206 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 492PH 53390 UNIVERSAL HAS WORN BEARINGS. 1 G 7 1 3U O H2SW 2002071200020 20020712 00020 SW 2002 7 12 HEEA080046 1 20020610 A 6720 406312103101 LINK BELL 407 407 1182206 SW TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 408PH 53228 TAIL ROTOR LINK ASSY HAS WORN BEARINGS. 1 G 7 1 3U O H2SW 2002071200021 20020712 00021 SW 2002 7 12 HEEA080047 1 20020610 A 7921 406360500101 OIL COOLER BELL 407 407 1182206 SW ENGINE OIL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 742PH 53461 ENGINE OIL COOLER LEAKING. 1 G 7 1 3U O H2SW 2002071200022 20020712 00022 EA 2002 7 12 ASOA02306 1 20020602 A 3210 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LEFT FAILED A ASOA O OTHER O OTHER LD LANDING 1 SO 11 849AS 6845 7347 UPON LANDING ROLLOUT, THE CAPTAIN REPORTED THAT THE AIRCRAFT BEGAN DRIFTING TO THE LEFT AND SETTLED LEFT WING DOWN. THE CAPTAIN COUNTERACTED THE DRIFT WITH BRAKES AND STEERING INPUTS. EMERGENCY EQUIPMENT WAS REQUESTED AND THE AIRCRAFT WAS EVACUATED AFTER COMING TO A STOP. THE LEFT MAIN LANDING GEAR FAILED. THE INCIDENT IS UNDER INVESTIGATION. THIS MRR W ILL REMAIN OPEN PENDING INVESTIGATION. 2 L 7 2 4F 4 F RT A21EA E15NE 2002071200023 20020712 00023 SW 2002 7 12 HEEA080052 1 20020611 A 6420 407012101111 HUB BELL 407 407 1182206 SW TAIL ROTOR WILL NOT BALANCE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 498PH 53399 UNABLE TO BALANCE TAIL ROTOR HUB. REPAIRED AND RETURNED TO SERVICE. 1 G 7 1 3U O H2SW 2002071200024 20020712 00024 SW 2002 7 12 HEEA080055 1 20020611 A 5610 407030115123A WINDSHIELD BELL 407 407 1182206 SW COCKPIT CRAZED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 WINDSHIELD CRAZED. 1 G 7 1 3U O H2SW 2002071200025 20020712 00025 SW 2002 7 12 HEEA080056 1 20020611 A 5610 407030115125A WINDSHIELD BELL 407 407 1182206 SW COCKPIT CRAZED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 WINDSHIELD CRAZED. 1 G 7 1 3U O H2SW 2002071200026 20020712 00026 EA 2002 7 12 ASOA02315 1 20020605 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE WING MALFUNCTIONED A ASOA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SO 11 832AS 7243 ON DECENT, THE CAPTAIN RECEIVED A FLAP FAIL MESSAGE WHEN SELECTING FLAPS TO EIGHT DEGREES. EMERGENCY EQUIPMENT WAS REQU ESTED AS A PRECAUTION. A ZERO FLAP LANDING WAS PERFORMED. LANDING WAS UNEVENTFUL. MAINTENANCE CYCLED CIRCUIT BREAKERS 1F4 AND 2F4 AND DETERMINED PROPER OPERATION OF THE FLAP SYSTEM IAW AD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002071200027 20020712 00027 SO 2002 7 12 ASOA02316 1 20020608 A 5280 12012949001 HINGE BRACKET EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LT MLG DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 501AS 120273 DURING HANGER MAINTENANCE, THE LEFT MAIN LANDING GEAR OUTBOARD AFT GEAR DOOR AFT HINGE AFT L BRACKET WAS FOUND CRACKED. A CRACK WAS ALSO FOUND ON THE LEFT OUTBOARD FORWARD GEAR DOOR AFT HINGE FORWARD L BRACKET. MAINTENANCE REMOVED AND REP LACED THE CRACKED MAIN LANDING GEAR DOOR BRACKETS. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002071200028 20020712 00028 EA 2002 7 12 ASOA02318 1 20020608 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE COCKPIT DETECTED A ASOA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 900EV 7608 DURING TAKEOFF, BLEEDS OPEN AND APU DEFERRED, PILOT NOTED SMELL OF SOMETHING BURNING THAT WENT AWAY. ON ROTATION, SMELL CAME BACK VERY STRONG OUT OF VENTS ALONG WITH TRACE AMOUNTS OF SMOKE. PILOT SHUTOFF LEFT PACK WHICH STOPPED SMELL AND SMOKE COMING FROM VENTS. RT PRES GAUGE SHOWED 120 PSI AND LEFT SHOWED 138 PSI. AC RETURNED TO AIRPORT FOR A SAFE BUT O VERWEIGHT LANDING. MAINTENANCE PERFORMED AN OVERWEIGHT LANDING INSP WITH NO DEFECTS NOTED AT THAT TIME. MAINTENANCE RA N THE AC AT TAKEOFF POWER. 10TH STAGE BLEED PRESSURE WAS AT 118 PSI AND PACK PRESS READ 32 PSI. THERE WAS NO EVIDENCE OF SMELL OF SMELL OR SMOKE ONLY MINOR CONDENSATION FROM VENTS WAS OBSERVED. NO DEFECTS WERE NOTED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002071200029 20020712 00029 SO 2002 7 12 ASOA02321 1 20020610 A 3620 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE COCKPIT MALFUNCTIONED A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 502AS 120274 DURING CLIMBOUT, AT 12000 FEET, THE AURAL WARNING LIGHT ILLUMINATED FOLLOWED BY THE ILLUMINATION OF THE LEFT DUCT LEAK L IGHT. THE CAPTAIN FOLLOWED THE QRH PROCEDURES WHICH INCLUDED THE SECURING OF THE ENGINE. THE DUCT LEAK LIGHT EXTINGUIS HED. AN EMERGENCY WAS DECLARED. SINGLE ENGINE PROCEDURES WERE FOLLOWED BY THE CAPTAIN TO RETURN AND LAND SAFELY. MAIN TENANCE RAN THE LEFT ENGINE AND INSPECTED THE LEFT INBOARD DUCT AND OVERWING DUCT FOR LEAKS. OPERATIONAL CHECK WAS NORM AL AND NO LEAKS WERE FOUND IN THE DUCTS. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002071200030 20020712 00030 EA 2002 7 12 ASOA02323 1 20020610 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 825AS 7207 DURING A HANGER INSPECTION, THE SECOND, FROM FORWARD, EMERGENCY LIGHTING STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE EMERGENCY STRIP LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002071200031 20020712 00031 SO 2002 7 12 ASOA02325 1 20020611 A 3350 AGC1 FUSE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE CABIN BLOWN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 273AS 28056 120222 DURING GROUND INSPECTION, BOTH AFT CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE EMERGENCY LIGHT FUSE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002071200032 20020712 00032 EU 2002 7 12 ASOA02328 1 20020612 A 3350 3011206 LIGHT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 533AS 13727 460 DURING A HANGER INSPECTION, THE FORWARD MOST EXTERNAL EMERGENCY LIGHT ON THE LEFT HAND SIDE OF THE FUSELAGE WAS FOUND IN OPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE EXTERNAL EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD . AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2002071200033 20020712 00033 SO 2002 7 12 ASOA02329 1 20020615 A 3397 M2275941249 WIRE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE CABIN BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 240AS 120060 DURING GROUND INSPECTION, THE LIGHTED EMERGENCY EXIT SIGN ON THE AFT OF THE CLOSET WAS FOUND INOPERATIVE. THE LOWER LEF T EXTERNAL EMERGENCY LIGHT WAS ALSO INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE EMERGENCY EXIT SIGN. MAINTE NANCE ALSO REMOVED AND REPLACED THE INOPERATIVE EXTERNAL EMERGENCY LIGHT. OPERATIONAL CHECKS FOR BOTH LIGHTS GOOD. AIR CRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002071200034 20020712 00034 EA 2002 7 12 ASOA02332 1 20020615 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 835AS 7258 DURING HANGER MAINTENANCE, A CRACK WAS DISCOVERED IN FRAME STATION 718 BETWEEN STRINGERS 10 AND 12 ON THE LEFT AND RIGHT SIDES. MAINTENANCE REPAIRED THE CRACKED FRAME IAW SRM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002071200035 20020712 00035 EA 2002 7 12 ASOA02345 1 20020617 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 824AS 11496 7203 DURING HANGER MAINTENANCE, A CRACK WAS DISCOVERED ON FRAME 718 ON BOTH THE LEFT AND RIGHT SIDES. MAINTENANCE REPAIRED T HE CRACKED FRAME IAW EO. 2 L 7 2 4F 4 F RT A21EA E15NE 2002071200036 20020712 00036 SW 2002 7 12 HEEA080058 1 20020611 A 7810 407063001101 EXHAUST STACK BELL 407 407 1182206 SW ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 741PH 53457 EXHAUST STACK CRACKED. 1 G 7 1 3U O H2SW 2002071200037 20020712 00037 SO 2002 7 12 ASOA02347 1 20020617 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 240AS 26830 120060 DURING A GROUND INSPECTION, THE LOWER EXTERNAL EMERGENCY LIGHT ON BOTH SIDES OF THE FUSELAGE WERE INOPERATIVE. MAINTENA NCE CHARGED THE EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002071200038 20020712 00038 SW 2002 7 12 HEEA080059 1 20020611 A 5320 407064807119 SUPPORT BELL 407 407 1182206 SW FUSELAGE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406PH 53198 BOTTOM HOLE ON SUPPORT IS ELONGATED. 1 G 7 1 3U O H2SW 2002071200039 20020712 00039 EA 2002 7 12 ASOA02351 1 20020618 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE COCKPIT CRACKED A ASOA O OTHER O OTHER DE DESCENT 1 SO 11 867AS 3874 7463 DURING DESCENT, AT APPROXIMATELY 10,000 FEET AND 25D KIAS, THE FIRST OFFICERS WINDSHIELD (THIRD WINDOW FROM THE LEFT) SH ATTERED. THE CAPTAIN PERFORMED THE ABNORMAL PROCEDURES CHECKLIST FROM THE QRH. AN EMERGENCY WAS DECLARED, BUT LATER CA NCELED BY THE CAPTAIN. THE INNER WINDOW PANE REMAINED IN TACT AND NO GLASS ENTERED THE COCKPIT. AIRCRAFT LANDED SAFELY . MAINTENANCE REMOVED AND REPLACED THE SHATTERED WINDSHIELD. LEAK CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002071200041 20020712 00041 SW 2002 7 12 HEEA080061 1 20020611 A 3212 206373901103 SOLENOID VALVE 407073848101 BELL 407 407 1182206 SW FLOAT BOTTLE LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 408PH 236 53228 SOLENOID VALVE LEAKING. 1 G 7 1 3U O H2SW 2002071200042 20020712 00042 SW 2002 7 12 HEEA080062 1 20020611 A 3212 206373901103 SOLENOID VALVE 407073848101 BELL 407 407 1182206 SW FLOAT BOTTLE LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 612PH 337 53199 SOLENOID VALVE LEAKING. 1 G 7 1 3U O H2SW 2002071200043 20020712 00043 SW 2002 7 12 HEEA080063 1 20020611 A 2910 407073854101 TUBE BELL 407 407 1182206 SW HYD SYSTEM CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 HYDRAULIC TUBE PITTED. 1 G 7 1 3U O H2SW 2002071200044 20020712 00044 SW 2002 7 12 HEEA080064 1 20020611 A 2897 407076501109A WIRE HARNESS BELL 407 407 1182206 SW FUEL SYSTEM CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 53400 CHAFING 20 INCHES FROM TOP FUEL PROBE CONNECTORS. 1 G 7 1 3U O H2SW 2002071200045 20020712 00045 WP 2002 7 12 2002F00748 1 20020514 A 5320 SPLICE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON STRINGER SPLICE 51R, AT STATION 1710, LOWER INBOARD SERVICE. (M) 2 L 7 3 4F A22WE 2002071200046 20020712 00046 SW 2002 7 12 HEEA080065 1 20020611 A 3212 407350300101 FLOAT BELL 407 407 1182206 SW EMERGENCY FLOAT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 404PH 53188 FLOAT BAG FAILED 6 MONTH LEAK TEST. 1 G 7 1 3U O H2SW 2002071200047 20020712 00047 SW 2002 7 12 HEEA080066 1 20020611 A 3212 407350300101 FLOAT BELL 407 407 1182206 SW EMERGENCY FLOAT LEAKING E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 724PH 53327 RT FWD FLOAT BAG LEAKING THROUGH CHECK VALVE. 1 G 7 1 3U O H2SW 2002071200048 20020712 00048 SW 2002 7 12 HEEA080067 1 20020611 A 3212 407350302101 FLOAT BELL 407 407 1182206 SW EMERGENCY FLOAT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 404PH 53188 FLOAT BAG FAILED 6 MONTH LEAK TEST. TO BE SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. 1 G 7 1 3U O H2SW 2002071200049 20020712 00049 WP 2002 7 12 2002F00749 1 20020514 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON STRINGER 48R LOWER OUTBOARD LEG, AT STATION 1701. (M) 2 L 7 3 4F A22WE 2002071200050 20020712 00050 WP 2002 7 12 2002F00750 1 20020514 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON STRINGER 48L, AND STRINGER 48L SPLICE, AT STATION 1710. (M) 2 L 7 3 4F A22WE 2002071200051 20020712 00051 SW 2002 7 12 HEEA080070 1 20020611 A 2844 407362013101 PRESSURE SWITCH BELL 407 407 1182206 SW FUEL SYSTEM FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8595X 53267 LT TRANSFER LIGHT STAYS ON. CHANGED PRESSURE SWITCH. 1 G 7 1 3U O H2SW 2002071200052 20020712 00052 SW 2002 7 12 HEEA080071 1 20020611 A 2844 407362013101 PRESSURE SWITCH BELL 407 407 1182206 SW FUEL SYSTEM FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 612PH 53199 BOOST PUMP PRESSURE LIGHT WOULD NOT GO OUT. CHANGED PRESSURE SWITCH. 1 G 7 1 3U O H2SW 2002071200053 20020712 00053 SW 2002 7 12 HEEA080072 1 20020611 A 7930 407375004101 INDICATOR BELL 407 407 1182206 SW OIL TEMP/PRESS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 740PH 53435 ENGINE OIL TEMP/PRESS INDICATOR TEMP WENT TO ZERO. 1 G 7 1 3U O H2SW 2002071200054 20020712 00054 WP 2002 7 12 2002F00751 1 20020514 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON SHEAR TIE AT STATION 1701, BETWEEN STRINGER 47R AND 48R. (M) 2 L 7 3 4F A22WE 2002071200055 20020712 00055 WP 2002 7 12 2002F00752 1 20020514 A 5310 SHEAR TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON SHEAR TIE AT STATION 1701, BETWEEN STRINGER 48R AND 50R. (M) 2 L 7 3 4F A22WE 2002071200056 20020712 00056 SW 2002 7 12 HEEA080073 1 20020611 A 7933 407375005101 INDICATOR BELL 407 407 1182206 SW ENG OIL TEMP MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 719PH 53266 ENGINE OIL TEMP INDICATOR LED LIGHTING WILL NOT BRIGHTEN. 1 G 7 1 3U O H2SW 2002071200057 20020712 00057 WP 2002 7 12 2002F00753 1 20020514 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON INNER SKIN AROUND FLAPPER VALVE, BETWEEN STATIONS 1701 AND 1716, AND BETWEEN STRINGERS 51 L AND 52L. (M) 2 L 7 3 4F A22WE 2002071200058 20020712 00058 WP 2002 7 12 2002F00754 1 20020514 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK FOUND CORROSION ON J-LEG OF FRAME AT STATION 1720, BETWEEN STRINGERS 48L AND 51R. (M) 2 L 7 3 4F A22WE 2002071200059 20020712 00059 SW 2002 7 12 HEEA080074 1 20020611 A 7933 407375005101 INDICATOR BELL 407 407 1182206 SW ENG OIL TEMP INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 719PH 53266 ENGINE OIL TEMPERATURE INDICATOR INOPERATIVE. 1 G 7 1 3U O H2SW 2002071200061 20020712 00061 2002 7 12 2002F00755 4 20020314 A 6122 B210631 GOVERNOR STBROS SD3 SD360 8100606 EU LT ENGINE MALFUNCTIONED A DATA E ENGINE SHUTDOWN E VIBRATION/BUFFET AP APPROACH 1 GL 13 4498Y SH3625 THE LEG FROM MDT TO AVP ON FINAL APPROACH THE LEFT ENGINE BEGAN TO SURGE. THE PILOTS SHUT DOWN THE ENGINE TO STABILIZE THE AIRCRAFT AND TO CONTINUE WITH THE APPROACH. THE AIRCRAFT WAS LANDED JOHNSTONE, PA. THE AIRCRAFT LANDED WITHOUT INC IDENT. THE AVP MECHANIC WAS DISPATCHED TO THE AIRCRAFT. THE OVERSPEED GOVERNOR WAS REPLACED AND CHAFFED WIRES IN A BUN DLE WERE REPAIRED. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T A41EU 2002071200062 20020712 00062 WP 2002 7 12 2002F00747 1 20020514 A 5320 SPLICE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION STRINGER SPLICE, ON STRINGER 52, AT STATION 1711. (M) 2 L 7 3 4F A22WE 2002071200063 20020712 00063 EU 2002 7 12 REX2002F00009 1 20020517 A 7920 7271015515 TUBE SAAB SF340 SF340A 7850100 EU FLARE CRACKED A REXA E ENGINE SHUTDOWN K FLUID LOSS TO TAKEOFF 1 SO 25 111PX 340A024 JUST AFTER ATTAINING V1 SPEED DURING TAKEOFF, THE LEFT ENGINE LOW OIL PRESSURE WARNING ILLUMINATED. THE CLIMB OUT CONTI NUED TO SIX THOUSAND FEET AND THE FLIGHT CREW DETERMINED THAT WAS NOT AN INDICATION PROBLEM. THE FLIGHT CREW DECLARED A N EMERGENCY AND PERFORMED AN IN FLIGHT SHUT DOWN OF THE ENGINE IAW THE APPROVED CHECKLIST. THE AIRCRAFT CONTINUED WHERE AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND A BAD OIL PRESSURE SENSOR OIL LINE. THE LINE WAS REPLACED, THE ENGI NE TOPPED OFF WITH OIL AND A GROUND RUN UP WAS PERFORMED. NO OIL FURTHER LEAKAGE WAS NOTED. 2 L 7 2 4T RT A52EU 2002071200064 20020712 00064 SW 2002 7 12 HEEA080076 1 20020611 A 2841 407375009101 PROBE BELL 407 407 1182206 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 53400 FUEL GAUGE WOULD GO BLANK INTERMITTENTLY. CHANGED FUEL QTY PROBE. 1 G 7 1 3U O H2SW 2002071200065 20020712 00065 SW 2002 7 12 HEEA080077 1 20020611 A 5610 407706301105 TRACK BELL 407 407 1182206 SW COCKPIT WINDOW DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 SLIDING WINDOW TRACK IS DETERIORATED. 1 G 7 1 3U O H2SW 2002071200066 20020712 00066 2002 7 12 HEEA080078 4 20020611 A 3450 702500 INDICATOR BELL 407 407 1182206 SW DEPEND POSITION MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 724PH 53327 DEPENDENT POSITION DETERMINING SYSTEM DISPLAY REMAINS IN TEST MODE. 1 G 7 1 3U O H2SW 2002071200067 20020712 00067 SW 2002 7 12 HEEA080079 1 20020611 A 5210 900291 LATCH BELL 407 407 1182206 SW CREW DOOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 53159 DOOR LATCH ASSY WORN. 1 G 7 1 3U O H2SW 2002071200068 20020712 00068 SW 2002 7 12 HEEA080081 1 20020611 A 6320 BEARING BELL 407 407 1182206 SW COOLER BLOWER ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 495PH 53397 OIL COOLER BLOWER BEARING ROUGH. 1 G 7 1 3U O H2SW 2002071200069 20020712 00069 WP 2002 7 12 AALA20020195 1 20020228 A 2133 21171803 ACTUATOR DOUG DC9 DC982 3022082 WP OUTFLOW VALVE MALFUNCTIONED A AALA B I EMER. DESCENT CABIN DEPRESSURIZATION J WARNING INDICATION CR CRUISE 1 SW 21 90511 49805 FLT 1487 -ORD-LAX- DURING CRUISE FLIGHT AT 31,000 FT, WARNING LIGHTS ILLUM. ALTITUDE 10,500 FT AND CLIMBING. INITIATED E MERGENCY DESCENT, PACKS SHOWED NORMAL FLOW. NO STANDBY OR LOCKOUT LIGHT ILLUM. ARRESTED AT 11,000 FT AND STAYED BELOW 10 ,000 FT. LEVELED OFF AT 18,000 FT. AFTER APPROX 5 MIN ENTIRE SEQUENCE REOCCURRED. EMERGENCY DESCENT AT 18,000 FT TO 1 0,000 FT. STANDBY AND LOCKOUT ILLUM. CABIN ALTITUDE AT 10,000 FT BUT ERRATIC. DUMPED CABIN PRESSURE MANUALLY, LIGHTS EXTINGUISHED. CABIN THEN DESCENDED NORMALLY WITH AIRCRAFT DESCENT. LANDED LAS WITHOUT INCIDENT. INSPECTED TAILCONE AR EA NO DAMAGE NOTED REPLACED OUTFLOW VALVE ACTUATOR, PERFORMED BITE TEST ON NR 1 AND 2 CABIN PRESSURE CONTROLLERS. (M) 2 L 7 2 4F A6WE 2002071200070 20020712 00070 SW 2002 7 12 HEEA080082 1 20020611 A 6320 BEARING BELL 407 407 1182206 SW COOLER BLOWER ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 493PH 588 53393 OIL COOLER BLOWER BEARING ROUGH. 1 G 7 1 3U O H2SW 2002071200071 20020712 00071 SW 2002 7 12 HEEA080083 1 20020611 A 3212 206050247132 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 490PH 53378 FLOAT COVER ASSY WORN END CLOSURE. 1 G 7 1 3U O H2SW 2002071200072 20020712 00072 GL 2002 7 12 HEEA080085 2 20020611 A 7230 23064570 LINER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL COMPRESSOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 490PH 53378 COMPRESSOR LINER DAMAGED PRODUCING TORQUE FLUCTUATIONS. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U 3 U O H2SW E1GL 2002071200073 20020712 00073 SW 2002 7 12 HEEA080086 1 20020611 A 2432 31908001 BATTERY BELL 407 407 1182206 SW MAIN MALFUNCTIONED E HEEA K NONE L J NO TEST WARNING INDICATION IN INSP/MAINT 1 SW 03 490PH 53378 BATTERY HOT LIGHT ON INSTALLATION. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U O H2SW 2002071200074 20020712 00074 NE 2002 7 12 HEEA080088 2 20020611 A 7297 6038T53P01 WIRE HARNESS BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE ENGINE DAMAGED E HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 8045T 28101 ENGINE YELLOW ELECTRICAL HARNESS PRODUCING MGT FLUCTUATION ON GAUGE IN COCKPIT. TO BE SENT TO VENDOR. 2 G 7 2 4U 4 U H10SW E8NE 2002071200075 20020712 00075 SW 2002 7 12 HEEA080089 1 20020611 A 2432 RG214 BATTERY BELL 214 214ST 1182106 SW MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5748M 28102 BATTERY WEAK. TO BE SENT TO VENDOR. 2 G 7 2 4U H10SW 2002071200076 20020712 00076 SW 2002 7 12 HEEA080090 1 20020611 A 2432 RG214 BATTERY BELL 214 214ST 1182106 SW MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5748M 28102 BATTERY WEAK. TO BE SENT TO VENDOR. 2 G 7 2 4U H10SW 2002071200077 20020712 00077 NM 2002 7 12 AALA20020619 1 20020503 A 2842 UNI5457 COMPUTER BOEING 777 777223 1385213 NM FUEL SYSTEM FAULTY A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 786AN 30250 ORD - FLT 50 - APPROXIMATELY 45 MINUTES INTO THE FLIGHT THE FUEL GAUGE AND SYNOPTIC WENT BLANK FOR ABOUT 30 SECONDS. AP PROXIMATELY HALF AND HOUR LATER GOT A FUEL IMBALANCE EICAS MESSAGE AND RIGHT TANK DROPPED TO 34.5 WHILE THE LEFT TANK RE MAINED AT 54.5. THERE WAS NO EVIDENCE OF A LEAK AND AFTER APPROX 30 MINUTES THE RIGHT GAUGE GRADUALLY INCREASED BACK TO 54 AND FUNCTIONED NORMALLY. T/S FOUND EXISTING FAULT 28-20050 FQPU INTERNAL FAULT. REPLACED FQPU AND ACCOMPLISHED TES TS PER MM. ALL CHECKS NORMAL. (M) 2 L 7 2 4F RT T00001SE 2002071200078 20020712 00078 EU 2002 7 12 AALA20020626 1 20020507 A 5315 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1420D 11403 TUL - FOUND FLOOR FRAME BL 600L, CORROSION TOP SURFACE, STATION 3845-4610. INSTALLED NEW FLOOR FRAME AT BL 600L, STATIO N 3845-4610, PER 53-30-02=SR01. (M) 2 L 7 2 4F RT 2002071200079 20020712 00079 NM 2002 7 12 AALA20020627 1 20020508 A 5315 FLOORBEAM BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AM 24491 TUL - FOUND TOP OF FRAME 1640 FROM LEFT SIDE TO RIGHT HAS NUMEROUS AREAS OF HEAVY CORROSION UNDER NUT CLIPS. INSTALLED FABRICATED FLOORBEAM CAP AND ASSOCIATED PARTS PER SRM 51-10-010. (M) 2 L 7 2 4F RT A2NM 2002092300006 20020923 00006 NE 2002 9 23 AALA20020628 2 20020505 A 7230 TAY65015 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE NR 2 VIBRATION A AALA E A ENGINE SHUTDOWN UNSCHED LANDING E J B VIBRATION/BUFFET WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 1447L 11456 EN ROUTE, NR 2 ENGINE, SEVERE VIBRATION, VIBRATION HIGH NR 2 ON MFDU, CONFIRMED WITH ALTERNATE VIBRATION SWITCH. AT IDL E, VIBRATION STILL IN RED BAND OUT OF LIMITS. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. OIL AND HYDRAULIC ODORS ON TOUCHDOWN. REPLACED RT ENGINE PER ENGINE CHANGE CARD. ENGINE TRIM AND OPERATIONS CHECKED ACCOMPLISHED. GROUND CHEC KED NORMAL OPERATION. STRIP EXAMINATION OF THE ENGINE REVEALED THE STAGE OF LOW PRESSURE STAGE 1 NOZZLE GUIDE VANES (LP 1NGV) HEAVILY HOLED BY BURNING. A SINGLE LP1 TURBINE BLADE WAS FOUND FAILED IN THE NECK SECTION OF THE ROOT, JUST INBOA RD OF THE ROOT PLATFORM BUTTRESS. 2 L 7 2 4F 4 F RT E25NE 2002071200080 20020712 00080 SW 2002 7 12 HEEA080091 1 20020611 A 6300 BEARING BELL 214 214ST 1182106 SW M/R SUPPORT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 MAIN ROTOR SUPPORT HAS WORN BEARINGS. REPAIRED. 2 G 7 2 4U H10SW 2002071200081 20020712 00081 WP 2002 7 12 GTIA020320 1 20020322 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR PANEL LEFT STATION 769-826 CRACKED/DAMAGE. FORM NEW PANEL. (M) 2 L 7 2 4F A6WE 2002071200082 20020712 00082 2002 7 12 HEEA080093 4 20020611 A 2312 064101900 TRANSCEIVER BELL 222 222U 1182140 SW COCKPIT MALFUNCTIONED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 6992 47521 PILOT REPORTED INTERMITTENT TRANSMISSION AND RECEIVE. COULD NOT MAKE CONTACT WITH AIRPORT TOWER BUT COULD MAKE CONTACT WITH OTHER COMM (NR 2). VERY LOUD SIDETONE WHEN TRANSMITTING. ADJUSTED SIDETONE TO SPECS. FOUND UNIT WOULD INTERMITTEN TLY STOP RECEIVING. ADJUSTED VCO AND ALIGNED RECEIVER. NO HELP. FOUND WHEN UNIT STOPPED RECEIVING THE UNIT WOULD TRAN SMIT FAR OFF FREQUENCY. COULD NOT ADJUST FREQUENCY. ALSO FOUND WHEN UNIT WAS NOT RECEIVING AND TRANSMITTING THAT DISPL AY WOULD GO OUT SOMETIMES. REPLACED I111 MICROCOMPRESSOR IC CHIP. REPAIRED PROBLEM. ADJUSTED C/N SQUELCH, CARRIER SQU ELCH, FREQUENCY, MIC GAIN AND SIDETONE. FOUND BROKEN SCREW IN MODULATOR HEATSINK AND COULD NOT DRILL OUT. REPLACED MOD 1 G 7 2 3U H9SW 2002071200083 20020712 00083 WP 2002 7 12 GTIA020321 1 20020322 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR PANEL INBOARD STATION 826-869 CRACKED/DAMAGED. FABRICATED NEW PANEL. (M) 2 L 7 2 4F A6WE 2002071200084 20020712 00084 SW 2002 7 12 HEEA080094 1 20020611 A 6220 204031920003 DAMPER BELL 212 212 1181420 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 102PH 30899 RIGHT HAND FRICTION DAMPER LOWER ATTACHMENT EARS BROKEN. REPAIRED. 1 G 7 1 4U H4SW 2002071200085 20020712 00085 WP 2002 7 12 GTIA020322 1 20020322 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR PANEL INBOARD RIGHT STATION 886-927 HAS PUNCTURE/CRACKED. FABRICATED REPAIR FLOOR BOARD. (M) 2 L 7 2 4F A6WE 2002071200086 20020712 00086 WP 2002 7 12 GTIA020323 1 20020322 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR PANEL STATION 886-946 CENTER HAS CRACK AT FLANGE SUPPORT PANEL DELAMINATED. FABRICATED REPAIR DOUBLER . INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2002071200087 20020712 00087 SW 2002 7 12 HEEA080095 1 20020611 A 6320 204040368001 VALVE BELL 212 212 1181420 SW MAIN ROTOR MALFUNCTIONED E HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 5736D 31135 WHEN ENGINES ARE REDUCED TO IDLE TRANSMISSION OIL PRESSURE DROPS BELOW LOW RED AND TRANSMISSION OIL PRESSURE LIGHT ILLUM INATES. ADVANCING EITHER ENGINE TO 70 PERCENT N1 RESTORES PRESSURE TO NORMAL RANGE. WHEN OIL PRESSURE RELIEF VALVE WAS REMOVED IT WAS FOUND TO BE STUCK PARTIALLY OPEN. REPLACED DEFECTIVE OIL PRESSURE RELIEF VALVE. 1 G 7 1 4U H4SW 2002071200088 20020712 00088 WP 2002 7 12 GTIA020324 1 20020318 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - AFT PIT/CABIN FLOOR, STATION 1193 PLUS X45 TO SIDE OF BODY, CORROSION ON LOWER SURFACE OF SUB FLOOR. CUTOUT DAMAG ED AREA OF SUB FLOOR AT STATION 1193. LOCATED AND DRILLED FILLER AND DOUBLER. INSTALLED REPAIR PART AT STATION 1193. (M) 2 L 7 2 4F A6WE 2002071200089 20020712 00089 WP 2002 7 12 GTIA020325 1 20020319 A 3221 FITTING DOUG DC9 DC981 3022081 WP NLG CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND NLG WHEEL WELL LEFT TRUNNION WEB FORWARD UPPER IN FITTINGS CRACKED. REMOVED. INSTALLED NEW FITTINGS. (M) 2 L 7 2 4F A6WE 2002071200090 20020712 00090 WP 2002 7 12 GTIA020326 1 20020408 A 5320 BRACKET DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND BRACKET CRACKED AT FS 1338, ABOVE LONGERON 24R. REMOVED BRACKET, FORMED NEW BRACKET. INSTALLED NEW BRACKET . (M) 2 L 7 2 4F A6WE 2002071200091 20020712 00091 SW 2002 7 12 HEEA080096 1 20020611 A 6730 C4264112 SLEEVE 206076031023 BELL 206 206A 1181508 SW SERVO VALVE LEAKING E HEEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 RH0580 VENDOR REWORKED SLIDE AND SLEEVE ASSY CAUSES SERVO TO HAVE EXCESSIVE INTERNAL LEAKAGE DURING FINAL TEST. 1 G 7 1 3U H2SW 2002071200092 20020712 00092 WP 2002 7 12 GTIA020327 1 20020408 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - PASSENGER CABIN, AFT FUSELAGE AREA FLOORBOARD FROM STATION 1115-1236 CORNER CRACKED, INSERTS MISSING AND BROKEN. FORM NEW PANEL. (M) 2 L 7 2 4F A6WE 2002071200093 20020712 00093 WP 2002 7 12 GTIA020328 1 20020322 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND COCKPIT FLOORBOARD NR 4415C CRACKED AND BROKEN OUT ALONG EDGE AND LIGHT SURFACE CORROSION ON BACK. FABRICAT ED A REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2002071200094 20020712 00094 SW 2002 7 12 HEEA080098 1 20020614 A 6730 214001970111 ACTUATOR BELL 214 214ST 1182106 SW FBW ELEVATOR MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 TRIPS OFF LINE. WILL NOT STAY ERECT. 2 G 7 2 4U H10SW 2002071200095 20020712 00095 WP 2002 7 12 GTIA020329 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT FS 160 TO 200 X7. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SU PPORT. INSTALLED TRACK. (M) 2 L 7 2 4F A6WE 2002071200096 20020712 00096 2002 7 12 HEEA080099 4 20020614 A 2210 214074104101 SENSOR BELL 214 214ST 1182106 SW DUAL RATE MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 YAW CHANNEL OF SCAS KICKS OFF LINE. 2 G 7 2 4U H10SW 2002071200097 20020712 00097 SW 2002 7 12 HEEA080100 1 20020614 A 2840 473203003 SIGNAL COND UNIT BELL 412 412 1182202 SW FUEL INDICATION MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2149S 36002 LOW LIGHT COMES ON INTERMITTENTLY AND LOW FUEL INDICATION. 1 G 7 2 4U H4SW 2002071200098 20020712 00098 WP 2002 7 12 GTIA020667 1 20020509 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - AFT PIT STATION 1155 L28R-26R FORWARD DOOR FRAME IS CORRODED ON FORWARD AND AFT SIDES, HI-LOCKS ON FORWARD SIDE LO WER ANGLE MISSING NUTS AND WASHERS. MATERIAL LOSS FOUND TO BE OUT OF LIMITS. FOUND DOOR FRAMES STRAP AT STATION 1155 L 30-21R TO BE OUT OF LIMITS. FABRICATED DOUBLERS. INSTALLED FABRICATED DOUBLERS AND FILLERS. DUPLICATED THE 5936671-1 STRAP. MACHINE WORK ACCOMPLISHED PER DPS 4.710 AND SPIRIT AIRLINES EA 5310-0226. INSTALLED STRAP AT STATION 1165 L30 T O L21R. (M) 2 L 7 2 4F A6WE 2002071200099 20020712 00099 SW 2002 7 12 HEEA080101 1 20020614 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 ACTUATOR STEP WILL NOT GO UP. 1 G 7 2 4U H4SW 2002071200100 20020712 00100 EU 2002 7 12 REXA02001 1 20020302 A 2612 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU COCKPIT FALSE ACTIVATION A REXA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 401BH 340A057 DURING CLIMB-OUT FROM MEMPHIS, THE LEFT ENGINES TAIL PIPE HOT LIGHT ILLUMINATED. POWER WAS REDUCED BY 20-30 PERCENT AT 1000 FEET. CREW NOTICED TORQUE FLUCTUATION WHEN THE CTOT SYSTEM WAS SECURED. AT THAT POINT, THE CREW ELECTED TO DECLAR E AN EMERGENCY AND PERFORMED AN IN FLIGHT SHUTDOWN IAW EMERGENCY CHECKLIST. THE AIRCRAFT WAS VECTORED BACK INTO MEMPHIS . THE LANDING WAS UNEVENTFUL AND THERE WERE NO INJURIES. MAINTENANCE FOUND NO EVIDENCE OF THERE HAVING BEEN A FIRE OR OVERHEAT CONDITION. AIRCRAFT WAS RUN UP WITH NO INDICATION OF TORQUE SURGES OR OVERHEATING. (M) 2 L 7 2 4T RT A52EU 2002071200101 20020712 00101 SW 2002 7 12 HEEA080102 1 20020618 A 7810 212061202010 DUCT BELL 412 412 1182202 SW EXHAUST DAMAGED E HEEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 03 412SM 33197 DURING TAKEOFF THE NR 2 ENGINE FIRE LIGHT ILLUMINATED. REPLACED NR 2 ENGINE EXHAUST DUCT, AFTER CRACK WAS FOUND ALONG TH E FLANGE JOINT. 1 G 7 2 4U H4SW 2002071200103 20020712 00103 SW 2002 7 12 HEEA080103 1 20020618 A 3350 214175140103 POWER SUPPLY BELL 214 214ST 1182106 SW CABIN FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 WON'T CHARGE PROPERLY. LIGHTS DIM AND WON'T HOLD CHARGE OVERNIGHT. 2 G 7 2 4U H10SW 2002071200105 20020712 00105 SW 2002 7 12 HEEA080104 1 20020619 A 6710 214001970111 ACTUATOR BELL 214 214ST 1182106 SW MAIN ROTOR MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 KICKS OFF LINE DURING MOVEMENTS AFTER 30 MINUTES OF OPERATION. 2 G 7 2 4U H10SW 2002071200106 20020712 00106 SW 2002 7 12 HEEA080106 1 20020625 A 2435 BRUSHES BELL 230 230 1182149 SW STARTER GEN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RC 1489 2410 23037 STARTER GEN HAS WORN BRUSHES. 1 G 7 2 3U NC H9SW 2002071200107 20020712 00107 SW 2002 7 12 HEEA080107 1 20020625 A 6730 41004683 CYLINDER 212076005111 BELL 212 212 1181420 SW ROTOR SERVO CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 7134 CAUSING A LEAK DURING TEST BETWEEN LOWER CYLINDER AND CONNECTING CYLINDER. FOUND A SMALL PIT IN LOWER CYLINDER I.D. IN AREA WHERE THE ORING SEALS ON THE CONNECTING CYLINDER. SENT TO FORTNER ACCESSORY SERVICE CORP. FOR INSPECTION AND REPAIR . 1 G 7 1 4U H4SW 2002071200108 20020712 00108 SW 2002 7 12 HEEA080108 1 20020625 A 3212 D24650112 FLOAT BELL 212 212 1181420 SW EMERGENCY FLOAT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3131S 30953 HOLE IN FLOAT BAG. 1 G 7 1 4U H4SW 2002071200109 20020712 00109 SW 2002 7 12 HEEA080109 1 20020625 A 6510 212040365025 QUILL BELL 212 212 1181420 SW LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 5736J 31140 QUILL ASSY LEAKING. WORN SPACER P/N 212-040-156-001. REPLACED SPACER. 1 G 7 1 4U H4SW 2002071200110 20020712 00110 2002 7 12 HEEA080110 4 20020625 A 3455 071121701 AMPLIFIER BELL 214 214ST 1182106 SW ADF SYSTEM INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8045T 28101 ADF AMPLIFIER INOPERATIVE. 2 G 7 2 4U H10SW 2002071200111 20020712 00111 SW 2002 7 12 HEEA080113 1 20020625 A 2121 214073917101 BLOWER BELL 214 214ST 1182106 SW AIR DIST INOPERATIVE E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 59806 28140 BLOWER WILL NOT COME ON. IN SHOP FOR REPAIR. 2 G 7 2 4U H10SW 2002071200112 20020712 00112 EA 2002 7 12 HEEA080114 2 20020625 A 7532 DIAPHRAGM 312320301 BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA BLEED VALVE DAMAGED E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 5736J 28A359 31140 INCREASE OF 75 DEGREES ITT AND 4.5 PERCENT N1 IN CRUISE FLIGHT. FOUND HOLE IN DIAPHRAGM. REPLACED. 1 G 7 1 4U 4 U H4SW E22EA 2002071200113 20020712 00113 NE 2002 7 12 HEEA080115 2 20020625 A 7421 4053T22P01 IGNITER BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE ENGINE WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 59806 28140 IGNITER WORN. TO BE SENT TO VENDOR FOR CREDIT. 2 G 7 2 4U 4 U H10SW E8NE 2002071200114 20020712 00114 SO 2002 7 12 C2XA02CL147 1 20020708 A 3020 M835366402 RELAY EMB 145 EMB145LR 3260212 SO INOPERATIVE A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 13989 145271 IAH FLIGHT#3785 THE CREW REPORTED A ODER OF GAS FUMES DURING ICE TEST.MAINTENANCE INSPECTED AND REPLACED THE PACK SETDOW N RELAY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002071200115 20020712 00115 SO 2002 7 12 C2XA02CL148 1 20020708 A 2500 P2070011100 FLASHLIGHT EMB 145 EMB145ER 3260211 SO CABIN BROKEN A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 13936 145025 CLE FLIGHT# THE CREW REPORTED THE FLIGHT ATTENDENT'S FLASHLIGHT SWITCH CAME OFF.MAINTENANCE REPLACED THE FLASHLIGHT AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002071200116 20020712 00116 NM 2002 7 12 MAS2002F00003 1 20020607 A 3300 3017773 LIGHT DHAV DHC8 DHC8202 2809007 NM EXT LT FUSELAGE INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437YV 15580 437 FORWARD EMERGENCY EGRESS LIGHT ON LEFT AT PAX DOOR, INOPERATIVE MECHANIC REPLACED BULB. OPS CHECKS GOOD. 2 H 7 2 4T RT A13NM 2002071200117 20020712 00117 EA 2002 7 12 MAS2002F00004 1 20020616 A 2700 FLAP CNDAIR CL600 CL6002B19 1900309 EA RT OB FLAP INOPERATIVE A MASA D RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 SW 07 7260 7260 DECLARED AN EMERGENCY AND RETURNED TO FIELD DUE TO FLAP SYSTEM. FAILED DURING TAKEOFF. MECHANIC WAS DISPATCHED TO THE AIRCRAFT AND FOUND THE RIGHT OUTBOARD FLAP TWISTED AND BOUND UP. MECHANICS ARE IN THE PROCESS OF REPLACING ALL RELATED FLAP COMP. 3/20/02 MECHANIC REPLACED RIGHT OUTBOARD FLAP, NR 3,4 ACTUATOR. RIGHT NR 3,4,5 FLEX SHAFT. OUTBOARD BUTE D OOR. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002071200118 20020712 00118 NM 2002 7 12 RIVA020306 1 20020306 A 5542 SHIELD BOEING 727 727225 1384077 NM RUDDER CRACKED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 365PA 20628 PSM - FOUND RUDDER, LEFT LEADING EDGE CHAFE SHIELD CRACKED. STOP DRILLED CRACK ON RUDDER RUB STRIP PLATE AT STATION 206 .350 IAW BOEING SRM 51-40-20 FIG 13. FABRICATED DOUBLER IAW BOEING SRM 51-40-20 FIG 13. INSTALLED DOUBLER IAW BOEING S RM 51-30-2 AND 51-40-20 FIG 13. (M) 2 L 7 3 4F A3WE 2002071200119 20020712 00119 2002 7 12 S2YA02001 4 20020114 A 3425 6229681001 ADI BEECH 1900 1900D 1154162 CE COCKPIT FAILED A S2YA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 13 91SK UE91 FLT 1157 - MLI-MKE - THE CREW NOTED ELECTRICAL SMOKE IN THE COCKPIT AND EVACUATED THE A/C. OUTSTATION MAINTENANCE FOUND THE LEFT EADI HAD EMITTED THE SMOKE. MAINTENANCE DISCONNECTED THE EADI AND THE A/C WAS FERRIED TO MKE. MKE MAINTENANC E REPLACED THE IH EADI AND INSPECTED THE A/C BUT FOUND NO FURTHER DEFECTS. THE A/C WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 2002071200120 20020712 00120 NM 2002 7 12 S2YA02003 1 20020210 A 5330 001A524A0100019 SKIN PANEL DORNER DO32 DO328300 NM FUSELAGE DEPARTED A S2YA K NONE D INFLIGHT SEPARATION CR CRUISE 1 GL 13 358SK 3188 AFTER FLIGHT 2147, MKE-GRR, THE CREW NOTED THAT THE PANEL AFT OF THE RIGHT LANDING LIGHT HAD DEPARTED IN FLIGHT. THE A/ C WAS TEMPORARY REPAIRED UNDER SPR A000040527 AND FERRIED BACK TO MKE. THE REPAIR WAS PUT ON MCO UNTIL THE DOOR WAS REP LACED. (M) 2 H 7 2 4T RT A55NM 2002071200121 20020712 00121 CE 2002 7 12 S2YA02005 1 20020220 A 2425 503800485 RELAY BEECH 1900 1900D 1154162 CE COCKPIT FAILED A S2YA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 13 91SK UE91 DURING FLIGHT 1027 - MKE-ATW - THE CREW NOTED THAT THE LEFT AC BUS FAILED FOLLOWED BY A LOUD HISSING AND CRACKLING NOISE FOLLOWED BY SEEING AND SMELLING A SMALL AMOUNT OF SMOKE. MAINTENANCE INSPECTED THE A/C AND FOUND THE ANNUNCIATOR RELAY SHORTED. MAINTENANCE DISCONNECTED THE RELAY AND FERRIED THE A/C TO MKE. MAINTENANCE REPLACED THE LEFT AC BUS ANNUNCIA TOR CONTROL RELAY, INSPECTED THE WIRING AND FOUND NO FURTHER DEFECTS. (M) 2 L 7 2 4T RT A24CE 2002071200122 20020712 00122 EA 2002 7 12 MAS2002F00005 1 20020507 A 3200 601R751451 BYPASS VALVE CNDAIR CL600 CL6002B19 1900309 EA FWD NOSE COMP INOPERATIVE A MASA D RETURN TO BLOCK O OTHER CL CLIMB 1 SW 07 77260 7260 AFTER TAKEOFF, A GEAR DISAGREE WARNING MESSAGE. CAPT REPORTED A RHYTHMIC THUMPING FROM NOSE AREA. FLIGHT CREW EXTENDED THE GEAR AND RETRACTED WITH THE SAME RESULTS. GEAR WAS EXTENDED AND THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. FERRIED AIRCRAFT, MECHANIC IS TROUBLESHOOTING. MECHANIC REMOVED AND REPLACED THE MAIN LANDING GEAR RUNAROUND BYPASS VA LVE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002071200123 20020712 00123 NE 2002 7 12 S2YA02006 2 20020221 A 7220 INLET SCREEN DORNER DO32 DO328300 NM PWA 306 PW306B NE RT ENGINE DELAMINATED A S2YA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 13 356SK 3163 JUST AFTER TAKEOFF OF FLIGHT 2432, MKE-BDL, THE CREW NOTED LOUD POP AND SUCKING SOUND FROM THE RIGHT ENGINE. THE CREW D ID AN AIR-TURN-BACK AND A PRECAUTIONARY LANDING. MAINTENANCE INSPECTED THE A/C AND FOUND THE INLET SCREEN DELAMINATED A ND PART OF IT MISSING. MAINTENANCE REPLACED THE INLET AND INSPECTED THE ENGINE AND FOUND ONLY SLIGHT DAMAGE AND SCRATCH ES ON THE OUTER 3 INCHES OF THE FAN BLADES. THE DAMAGE WAS DEEMED AIRWORTHY LIMIT SO IT WAS BLENDED AND THE A/C WAS RET URNED TO SERVICE. (M) 2 H 7 2 4T 4 F RT A55NM E35NE 2002071200124 20020712 00124 NM 2002 7 12 USAA020155 1 20020430 A 5514 FITTING BOEING 737 737401 1384701 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 37852 23985 TPA - FOUND FITTING CORRODED .5 INCH AREA, FORWARD FACE, FORWARD UPPER JOINT CLEVIS, LT SIDE HORIZ STAB. CORROSION LEVE L 2. REMOVED CORROSION, TREATED, PRIMED, INSTALLED FILLER PER SRM 55-10-10 AND EA 94300. (M) 2 L 7 2 4F RT A16WE 2002071200125 20020712 00125 NM 2002 7 12 USAA020156 1 20020418 A 5240 SKIN BOEING 737 737301 1384611 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 23933 TPA - FOUND SKIN CRACKED THREE PLACES, .5 INCH, .004 INCH , .002 INCH, FORWARD SERVICE DOOR LOWER HINGE CUT OUT. INSTAL LED DOUBLER AND FILLER PER SRM 52-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2002071200126 20020712 00126 EU 2002 7 12 USAA020157 1 20020502 A 5330 SKIN AIRBUS 320 A320214 3930316 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 106US 5041 1044 TPA - FOUND SKIN CRACKED .150 INCH, FRAME 30 STRINGER 8L. INSTALLED DOUBLER AND FILLER PER SRM 53-21-11 AND 53-00-11. (M) 2 L 7 2 4F RT A28NM 2002071200127 20020712 00127 NM 2002 7 12 USAA020159 1 20020328 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 45390 23234 CLT - FOUND SKIN CRACKED TWO PLACES 2.25 INCH AND 1.25 INCH, STATION 730 STRINGER 23R AND 24R. INSTALLED DOUBLER PER SR M 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2002071200128 20020712 00128 NM 2002 7 12 USAA020160 1 20020501 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 44865 23862 PIT - FOUND SKIN CRACKED 15 INCHES BY 20 INCHES, STATION 178 BULKHEAD 7.50 RBL - 2.50 LBL, 217WL - 192WL. REPAIRED PER EO 5300V153, DOUBLER INSTALLED. (M) 2 L 7 2 4F RT A16WE 2002071200129 20020712 00129 NM 2002 7 12 USAA020161 1 20020501 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 44865 23862 PIT - FOUND SKIN CRACKED 23 INCHES BY 22.5 INCHES EXIT DOUBLER, FS 294.5 STRINGER 28L-28R. DOUBLER INSTALLED PART OF EO FOR TCAS ANTENNA INSTALL PER EO 5389X717. (M) 2 L 7 2 4F RT A16WE 2002071200130 20020712 00130 NM 2002 7 12 USAA020162 1 20020418 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 23862 PIT - FOUND FLOOR SUPPORT/BEAM CORRODED 8 INCHES LONG, LEFT AFT SIDE NOSE GEAR STATION 270 BL 0 WL 217 FLOORBEAM. CORRO SION LEVEL 2. INSTALLED DOUBLERS AND REPAIR ANGLES PER TYPICAL REP 53-20-08 AND EA 73795. (M) 2 L 7 2 4F RT A16WE 2002071200131 20020712 00131 NM 2002 7 12 USAA020163 1 20020428 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 44865 23862 PIT - FOUND STRINGER CORRODED 1 INCH BY 2 INCH, FS 325.9 AND S28R. REPLACED STRINGER PER SRM 53-00-03 FIG 201. (M) 2 L 7 2 4F RT A16WE 2002071200132 20020712 00132 NM 2002 7 12 USAA020164 1 20020428 A 5753 FLAP TRACK BOEING 737 7373B7 1384580 NM T/E FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 44865 23862 PIT - FOUND FLAP TRACK CORRODED 3 AREAS, 1 INCH BY .5 INCH, ALL FLAP TRACK ROLLER CONTACT AREAS, NR 2 FLAP TRACK. REPLA CED FLAP TRACK PER EO 5796X180. (M) 2 L 7 2 4F RT A16WE 2002071200133 20020712 00133 NM 2002 7 12 USAA020165 1 20020428 A 5753 FLAP TRACK BOEING 737 7373B7 1384580 NM T/E FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 44865 23862 PIT - FOUND FLAP TRACK WITH PITTING CORROSION 2 INCHES BY 3 INCHES, NR 3 FLAP TRACK, TOP AFT SECTION. TRACK REPLACED PE R EO 5796X180. (M) 2 L 7 2 4F RT A16WE 2002071200134 20020712 00134 NM 2002 7 12 USAA020166 1 20020428 A 5753 FLAP TRACK BOEING 737 7373B7 1384580 NM T/E FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 23862 PIT - FOUND FLAP TRACK CORRODED 2 INCHES BY 3 INCH PITTING CORROSION, NR 1 FLAP TRACK, TOP AFT SECTION. CORROSION LEVEL 1. TRACK REPLACED PER EO 5796X180. (M) 2 L 7 2 4F RT A16WE 2002071200135 20020712 00135 NM 2002 7 12 USAA020167 1 20020428 A 5753 FLAP TRACK BOEING 737 7373B7 1384580 NM T/E FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 44865 23862 PIT - FOUND FLAP TRACK CORRODED, NR 1 FLAP TRACK ROLLER CONTACT AREA. CORROSION LEVEL 1. REPLACED FLAP TRACK PER EO 57 96X180. (M) 2 L 7 2 4F RT A16WE 2002071200136 20020712 00136 NM 2002 7 12 USAA020168 1 20020326 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 24996 PIT - FOUND FLOOR SUPPORT CORRODED 2 INCHES BY 4 INCH AREA, FLOOR SUPPORT LBL 13 STATION 328-344.17. CORROSION LEVEL 2. CRM INSTALLED 113692 REF IPC 53-42-00-20, FASTENERS SRM 53-10-51 FIG 1. (M) 2 L 7 2 4F RT A16WE 2002071200137 20020712 00137 NM 2002 7 12 USAA020169 1 20020508 A 5320 STRINGER CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 780AU 31804 24997 CLT - FOUND FRAME STRINGER CLIP CRACKED .75 INCH, STATION 727E AND S24L, FRAME TO STRINGER CLIP. REPLACED CLIP PER SRM 53-00-03. (M) 2 L 7 2 4F RT A16WE 2002071200138 20020712 00138 NM 2002 7 12 USAA020170 1 20020415 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 46636 23316 PIT - FOUND FRAME CRACKED .062 INCH, FRAME 480 LEFT SIDE BETWEEN S8L AND S9L. REPAIRED PER TYPICAL REPAIR 53-10-14A. ( M) 2 L 7 2 4F RT A16WE 2002071200139 20020712 00139 EA 2002 7 12 MAS2002F00006 1 20020509 A 3200 161441 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA NOSE STRUT INOPERATIVE A MASA D RETURN TO BLOCK O OTHER CL CLIMB 1 SW 07 77331 7331 AIRSHUTTLE HAD GEAR DISAGREE MESSAGE. NOSE GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO AIRPORT. AFTER AN UNEVENTFUL LANDING MECHANIC WAS CALLED. MECHANIC IS TROUBLESHOOTING. MECHANIC REMOVED AND REPLACED THE NOSE STEERING TORQUE LINKS . SWUNG GEAR IAW CRJ AMM. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002071200140 20020712 00140 NM 2002 7 12 USAA020171 1 20020424 A 5542 SKIN BOEING 737 7373B7 1384580 NM RUDDER CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 23316 PIT - FOUND RIB AND SKIN WITH HEAVY CORROSION 4 INCHES LONG BY 1 INCH WIDE, RUDDER COUNTER BALANCE STRUCTURE, RUDDER STA TION 121.64. LEVEL 2 CORROSION. (M) 2 L 7 2 4F RT A16WE 2002071200141 20020712 00141 NM 2002 7 12 USAA020172 1 20020415 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 46636 23316 PIT - FOND FRAME CRACKED .064 INCHES LONG, FRAME 400 RIGHT SIDE BETWEEN S8R AND S9R. ACCOMPLISHED TYPICAL REPAIR 53-10- 14A. (M) 2 L 7 2 4F RT A16WE 2002071200142 20020712 00142 NM 2002 7 12 USAA020173 1 20020418 A 5534 65537447 ANGLE BOEING 737 7373B7 1384580 NM VERTICAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND DRAG ANGLE CRACKED .5 INCH, SECTION 48, RIGHT SIDE, AFT OF AFT LUGS FOR VERTICAL STABILIZER. FILLERS AND ST RAPS INSTALLED ON BOTH SIDES OF DRAG ANGLE PER TYPICAL REPAIR 53-80-03. (M) 2 L 7 2 4F RT A16WE 2002071200143 20020712 00143 NM 2002 7 12 USAA020174 1 20020429 A 5540 65C2584151 ARM BOEING 737 7373B7 1384580 NM RUDDER CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND RUDDER BALANCE ARM WITH CORROSION 3 INCH BY 12 INCH AREA, RUDDER BALANCE ARM STRUCTURE. CORROSION LEVEL 2. RUDDER REPLACED AND INSTALLED PER JOB CARD. (M) 2 L 7 2 4F RT A16WE 2002071200144 20020712 00144 NM 2002 7 12 USAA020175 1 20020506 A 5754 SKIN BOEING 737 7373B7 1384580 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND SKIN CRACKED IN 13 SMALL CONTINUOUS PLACES, RIGHT WING, NR 6 SLAT, LOWER SURFACE SLAT STATION 299.10-314. R EMOVED DAMAGED SKIN PER SRM 57-43-01. (M) 2 L 7 2 4F RT A16WE 2002071200145 20020712 00145 NM 2002 7 12 USAA020176 1 20020502 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND Z-FRAME CRACKED .25 INCH, STATION 807 BETWEEN S8R AND S9R. CUT OUT CRACKED, INSTALLED DOUBLER PER TYPICAL R EPAIR 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002071200146 20020712 00146 NM 2002 7 12 USAA020177 1 20020416 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 42644 23514 PIT - FOUND SKIN AND WEB PLATE CRACKED .625 INCH, BS 360-380, AT BL 10. SKIN DOUBLER ADDED PER TYPICAL REPAIR 53-30-07 AND EA 73800. (M) 2 L 7 2 4F RT A16WE 2002071200147 20020712 00147 NM 2002 7 12 USAA020178 1 20020418 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 46011 23934 PIT - FOUND SKIN CRACKED 1 INCH, FS 360-380 AND BL 0 - S28 LEFT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-30-07 A ND EA 73832. (M) 2 L 7 2 4F RT A16WE 2002071200148 20020712 00148 NM 2002 7 12 USAA020179 1 20020421 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 783AU 25022 PIT - FOUND T-CAP FLOORBEAM CORRODED 2 INCHES LONG, FLOORBEAM STATION 328 AT LBL 28. CORROSION LEVEL 1. INSTALLED REPA IR DOUBLER AND NEW T-CAP PER SRM 53-10-51, PAGE 220. (M) 2 L 7 2 4F RT A16WE 2002071200149 20020712 00149 NM 2002 7 12 USAA020180 1 20020508 A 5320 ATTACH ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 783AU 31714 25022 PIT - FOUND ATTACH ANGLE CRACKED .5 INCH, INTERCOSTAL ANGLE STATION 291.5 STRINGER 11R. REMOVED AND REPLACED PART NR 11 31199 PER SRM 51-00. (M) 2 L 7 2 4F RT A16WE 2002071200150 20020712 00150 NM 2002 7 12 USAA020181 1 20020430 A 5347 1132118 CARGO TRACK BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 783AU 31714 25022 PIT - FOUND FLOOR RAIL HAD CORROSION SCATTERED OVER 98.5 INCHES, CARGO FLOOR RAIL RBBL 13.80 STATION 853-780. CORROSION LEVEL 1. SPLICED IN NEW FLOOR RAIL PER SRM 53-00-53. (M) 2 L 7 2 4F RT A16WE 2002071200151 20020712 00151 NM 2002 7 12 USAA020182 1 20020425 A 5320 ATTACH ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 783AU 25022 PIT - FOUND ATTACH ANGLE CRACKED .5 INCH, INTERCOSTAL ATTACH ANGLE STATION 291.5 STRINGER 13R. INSTALLED NEW ANGLE PER SRM 51-40-03. (M) 2 L 7 2 4F RT A16WE 2002071200152 20020712 00152 NM 2002 7 12 USAA020183 1 20020422 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 783AU 31714 25022 PIT - FOUND FRAME AND CLIP CRACKED .5 INCH, RIVET HOLE AT FRAME STATION 907 BETWEEN S8 AND S9. INSTALLED CHANNEL AND FI LLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002071200153 20020712 00153 NM 2002 7 12 USAA020184 1 20020430 A 5541 RIB BOEING 737 737301 1384611 NM RUDDER CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 46636 23228 PIT - FOUND RUDDER CORRODED 3 INCHES BY 12 INCH AREA, COVER FACE OF RIB BEHIND BALANCE WEIGHTS ON BEAM. REPLACED RIB PE R SRM 51-10-02, 51-20-01, 51-20-00 AND 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002071200154 20020712 00154 NM 2002 7 12 USAABB02061 1 20020510 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 LAX - FOUND ALL SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED ALL TEN BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002071200155 20020712 00155 NM 2002 7 12 USAABB02062 1 20020510 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 606AU 22202 BOS - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002071200156 20020712 00156 NM 2002 7 12 USAABB02063 1 20020510 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 614AU 27145 BDL - FOUND L1 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002071200157 20020712 00157 NM 2002 7 12 USAABB02064 1 20020511 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 22199 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 9, 13, 18, 22, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERI ES. (M) 2 L 7 2 4F RT A2NM 2002071200158 20020712 00158 NM 2002 7 12 USAABB02065 1 20020511 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 621AU 27200 CLT - FOUND ALL FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002071200159 20020712 00159 NM 2002 7 12 USAABB02066 1 20020512 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AU 27807 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 6 AND 26. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002071200160 20020712 00160 EU 2002 7 12 USAASA02043 1 20020502 A 3260 ABS012110 PROXIMITY SENSOR AIRBUS A319 A319112 3930323 EU NLG FAULTY A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 714US 1046 BOS - FLT 2143 - EN ROUTE MHT-BOS, AFTER DEPARTURE FROM MHT, THE NOSE LANDING GEAR WOULD NOT RETRACT. WHEN THE LANDING GEAR HANDLE WAS CYCLED, THE LANDING GEAR RETRACTED NORMALLY. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAI NTENANCE REPLACED PROXIMITY SENSOR 25GA. SYSTEM FUNCTIONALLY CHECKED NORMALLY. (M) 2 L 7 2 4F RT A28NM 2002071200161 20020712 00161 EU 2002 7 12 USAASA02044 1 20020504 A 3260 PROXIMITY SENSOR AIRBUS A319 A319112 3930323 EU RT MLG OUT OF ADJUST A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 714US 1046 PIT - FLT 132 - EN ROUTE DEN-PIT - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF IN DEN. WHEN THE LANDING GEAR WAS C YCLED, THE LANDING GEAR RETRACTED NORMALLY. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT GEA R FORWARD MAIN LANDING GEAR PROXIMITY SENSOR NEEDED ADJUSTED. ADJUSTED SENSOR AND PERFORMED GEAR SWING AND BITE TEST. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002071200162 20020712 00162 EU 2002 7 12 USAASA02045 1 20020505 A 3231 CONTROL UNIT AIRBUS A319 A319112 3930323 EU LANDING GEAR MALFUNCTIONED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 714US 1046 CLT - FLT 9202 - EN ROUTE PIT-CLT - THE LANDING GEAR DOORS DID NOT CLOSE AFTER GEAR RETRACTION. THE LANDING GEAR WAS RE CYCLED AND THE LANDING GEAR DOORS CLOSED NORMALLY. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A BITE CHECK OF THE LANDING GEAR CONTROL AND INTERFACE UNIT. NO FAULTS WERE NOTED. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2002071200163 20020712 00163 NM 2002 7 12 SPAA0200055 1 20020709 A 2560 D31354525 SLIDE BOEING 737 7372T4 1384492 NM FAILED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 R-2 DOOR EMERGENCY ESCAPE SLIDE DID NOT DEPLOY FOR CREW TRAINING EXCERCISE. MAINTENANCE DETERMINED THAT SLIDE INFLATION CYLINDER SAFETY PIN WAS ENGAGED. SAFETY PIN WAS REMOVED AND STOWED. SLIDE WAS DEPLOYED. 2 L 7 2 4F A16WE 2002071200164 20020712 00164 NM 2002 7 12 USAASB02079 1 20020420 A 3260 189929 PROXIMITY SENSOR BOEING 737 7373B7 1384580 NM NLG FAULTY A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 521AU 23856 RIC - FLT 1039 - NOSE GEAR RED AND GREEN LIGHTS WERE ILLUMINATED WHEN THE GEAR HANDLE WAS IN THE UP POSITION. CREW CYCL ED THE GEAR. WITH HANDLE IN DOWN POSITION, ALL INDICATION WERE NORMAL. FLIGHT CONTINUED TO RIC AND LANDED WITHOUT FURT HER INCIDENT. MAINTENANCE REPLACED THE DOWN PROX SENSOR AND THE R374 RELAY. (M) 2 L 7 2 4F RT A16WE 2002071200165 20020712 00165 NM 2002 7 12 USAASB02080 1 20020420 A 3260 BR20AXH5V3 RELAY BOEING 737 7373B7 1384580 NM LANDING GEAR MALFUNCTIONED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 521AU 23856 RIC - FLT 1039 - NOSE GEAR RED AND GREEN LIGHTS WERE ILLUMINATED WHEN THE GEAR HANDLE WAS IN THE UP POSITION. CREW CYCL ED THE GEAR. WITH HANDLE IN DOWN POSITION, ALL INDICATION WERE NORMAL. FLIGHT CONTINUED TO RIC AND LANDED WITHOUT FURTH ER INCIDENT. MAINTENANCE REPLACED THE DOWN PROX SENSOR AND THE R374 RELAY. (M) 2 L 7 2 4F RT A16WE 2002071200166 20020712 00166 NM 2002 7 12 USAASB02081 1 20020424 A 2197 WIRE BOEING 737 737401 1384701 NM COCKPIT DAMAGED A USAA B A EMER. DESCENT UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 408US 23878 CLT - FLT 1050 - CLIMBING OUT OF CLT, PASSING FL270, AIRCRAFT LOST PRESSURIZATION. CREW PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED NUMEROUS LEAKS AT THE FORWARD AND AFT ENTRY DOORS AND AT THE E/E DOOR. FOUND DAMAGED WIRES BEHIND PRESSURE CONTROL SELECTOR PANEL AT DISCONN ECT D640. REPAIRED WIRES AT PINS 21, 22, 23, 24, 25 AND 40 PER BOEING WPM. FUNCTIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002071200167 20020712 00167 NM 2002 7 12 USAASB02084 1 20020427 A 3234 655421943 CONTROL HANDLE BOEING 737 737301 1384611 NM COCKPIT LACK OF LUBE A USAA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 EA 19 337US 23235 PHL - FLT 577 - ON GEAR EXTENSION FOR LANDING, CREW RECEIVED THREE GREEN LIGHTS AND THEN THREE RED LIGHTS. CREW EXECUTE D A MISSED APPROACH AND CYCLED THE GEAR. ALL INDICATIONS APPEARED NORMAL AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT . MAINTENANCE FOUND THE GEAR HANDLE STIFF, AND LUBED THE GEAR HANDLE AND MICROSWITCH. (M) 2 L 7 2 4F RT A16WE 2002071200168 20020712 00168 EA 2002 7 12 COMA0260419 1 20020711 A 5220 H341931 HANDLE CNDAIR CL601R CNDAIR CL600 CL6002B19 1900309 EA CREW ESCAPE HATC CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 408CA 3922 7441 7440 DURING A C CHECK INSPECTION, WHILE PERFORMING TASK 52-22-00-720-801 THE FUNCTIONAL TEST OF THE CREW ESCAPE HATCH THE MEC HANIC FOUND THAT THE OUTER HANDLE OF THE CREW ESCAPE HATCH WOULD NOT UNLOCK PROPERLY ALLOWING THE HANDLE TO EXTEND AND R OTATE.THE HANDLE WAS REMOVED FROM THE CREW ESCAPE HACH AND WAS REPLACED WITH A SERVICEABLE UNIT IN ACCORDANCE WITH CRJ S TRUCTURE REPAIR MANUAL 51-42-06. 2 L 7 2 4F RT A21EA 2002071200169 20020712 00169 EA 2002 7 12 COMA0260420 1 20020707 A 5415 601370101 PYLON CNDAIR CL600 CL6002B19 1900309 EA EMPENNAGE CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 979CA 12377 7159 DURING REMOVAL OF THE LEFT ENIGNE ASSEMBLY, DISCOVERS FRETTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTING RIB 6 TO 2 O'CLOCK POSITION ON FWD SIDE.REPAIRED IN ACCORDANCE WITH 601R-54-50-044. 2 L 7 2 4F RT A21EA 2002071200170 20020712 00170 EA 2002 7 12 COMA02604021 1 20020711 A 2820 601R404672 INSULATION CNDAIR CL600 CL6002B19 1900309 EA CARGO CONTAMINATED A COMA A UNSCHED LANDING O W OTHER INADEQUATE Q C CR CRUISE 1 SO 01 984CA 7171 FLIGHT 5861 STRONG ROW FUEL ODOR IN CABIN AND COCKPIT.REMOVED FUEL CONTAMINATED INSULATION UNDER CARGO FLOOR - CLEANED B ELLY OF A/C AND REPLACED INSULATION. 2 L 7 2 4F RT A21EA 2002071200171 20020712 00171 EA 2002 7 12 COMA0260422 1 20020710 A 7930 388700320153 CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA R/H ENG WORN A COMA A UNSCHED LANDING M S OVER TEMP AFFECT SYSTEMS CR CRUISE 1 SO 01 710CA 7241 FLIGHT 5703 R/H ENGINE OIL TEMP INDICATED 165 DEGREES C DURING CLIMBFOUND ENGINE OIL OVER SERVICED - DRAINED EXCESS OIL AND REPLACED LUBE PUMP OIL FILTER CHECK VALVE. 2 L 7 2 4F RT A21EA 2002071200172 20020712 00172 NM 2002 7 12 USAASB02085 1 20020427 A 2130 7207375 RELIEF VALVE BOEING 737 737301 1384611 NM CABIN PRESSURE FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 563AU 35440 23551 CLT - FLT 384 - ON CLIMB-OUT FROM TPA, CREW REPORTED AN AUTO FAIL LIGHT AND THE CABIN ALTITUDE CLIMBING AT 4000 FPM. ST ANDBY MODE HAD NO EFFECT. FLIGHT DESCENDED TO 10,000 FEET AND DIVERTED TO CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LOWER SAFETY RELIEF VALVE. (M) 2 L 7 2 4F RT A16WE 2002071200173 20020712 00173 NM 2002 7 12 USAASB02093 1 20020513 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 376US 22955 EWR - MAINTENANCE FOUND THE FORWARD TO MID CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BAT TERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002071200174 20020712 00174 EA 2002 7 12 COMA0260423 1 20020711 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR INOPERATIVE A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 430CA 7461 FLGIHT 5646 EMERGENCY LIGHTS ROW 8 AND AFT ARE INOP.REPLACED THE FLEXIBLE LAMP ASSY. 2 L 7 2 4F RT A21EA 2002071200175 20020712 00175 NM 2002 7 12 COOSDR020173 1 20020701 A 5753 651920612 FLAP TRACK BOEING 727 7272Q6 138407V NM T/E FLAP CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 RIGHT WING, FLAP TRACK NR 6, AFT PAD CORRODED. 2 L 7 3 4F RT A3WE 2002071200176 20020712 00176 NM 2002 7 12 COOSDR020174 1 20020701 A 5753 652165127 SUPPORT FITTING BOEING 727 7272Q6 138407V NM T/E FLAP CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 1279E 21971 LEFT AND RIGHT WING, INBOARD FLAP, INBOARD TRACK FORWARD SUPPORT FITTING WITH BORE CORRODED. 2 L 7 3 4F RT A3WE 2002071200177 20020712 00177 EA 2002 7 12 COMA0260424 1 20020711 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 467CA 604 7637 FLIGHT 5507 FLAPS FAILED CAUTION MESSAGE.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2002071200178 20020712 00178 NM 2002 7 12 COOSDR02175 1 20020701 A 5320 6516350303 STIFFENER BOEING 727 727227 1384078 NM FUSELAGE CRACKED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 BS 1183 AFT PRESSURE BULKHEAD, STIFFENERS CRACKED, LOCATED AT WL 227 LEFT AND RIGHT SIDE. 2 L 7 3 4F A3WE 2002071200179 20020712 00179 NM 2002 7 12 COOSDR02177 1 20020701 A 5311 FRAME BOEING 727 727227 1384078 NM FUSELAGE CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 AFT CARGO COMPONENT LOWER CHORD CORRODED AT BS 950 BULKHEAD, BETWEEN S-26L AND S28L. 2 L 7 3 4F A3WE 2002071200180 20020712 00180 NM 2002 7 12 COOSDR02178 1 20020701 A 5230 6559947501 RETAINER BOEING 727 727227 1384078 NM CARGO DOOR CRACKED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 AFT CARGO COMPARTMENT, NR 2 CARGO DOOR - FORWARD AND AFT LOWER CORNER (SEAL DEPRESSOR) CRACKED. 2 L 7 3 4F A3WE 2002071200181 20020712 00181 NM 2002 7 12 COOSDR02179 1 20020701 A 5320 651594024 BEAM BOEING 727 727227 1384078 NM FUSELAGE CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 BS 740 BULKHEAD, HORIZONTAL CHORD CORRODED, LOCATED AT WL 170 BETWEEN LBL 40 INCHES AND RBL 40 INCHES. 2 L 7 3 4F A3WE 2002071200182 20020712 00182 NM 2002 7 12 COOSDR02180 1 20020701 A 5743 651929615 FITTING BOEING 727 727227 1384078 NM LT WING CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 LEFT WING MAIN LANDING GEAR, REAR SPAR TRUNNION ATTACH FITTING CORRODED. 2 L 7 3 4F A3WE 2002071200184 20020712 00184 NM 2002 7 12 AWXA200200600 1 20020624 A 5315 65C3453719 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK A 2" CRACK WAS FOUND ON CABIN FLOOR BEAM VERTICAL WEB BS 706, RBL 25. MAINTENANCE CUTOUT CRACKED AREA OF WEB AT BS 706, RBL 25. PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND WEB; INSTALLED REPAIR PARTS IAW AWA ER 03-5702-02187-ES1. 2 L 7 2 4F RT A16WE 2002071200185 20020712 00185 NM 2002 7 12 AWXA200200607 1 20020628 A 5320 146N52465 FLOOR SUPPORT BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 LCQ - MAJOR REPAIR - DURING C-11 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 1660 TO BS 1680, LBL 56. MAINTENANCE R EMOVED DAMAGED FLOOR SUPPORT AT BS 1660 TO BS 1680, LBL 56. FABRICATED NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW B757-2 00 SRM 51-40-02, PG. 11-12. 2 L 7 2 4F RT A2NM 2002071200186 20020712 00186 EU 2002 7 12 QXEA0200950 1 20020710 A 3350 6008905 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU ZONE 100 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 9317 11161 PDX-LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE.REMOVED AND REPLACED BATTERY SUPPLY PACK IN OVERHEAD BIN AT ROW 9AB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002071200187 20020712 00187 SO 2002 7 12 C2XA02TY110 1 20020712 A 5100 14571529503 DOUBLER EMB 145 EMB145ER 3260211 SO FAIRING 191 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12934 145019 TYS During a scheduled inspection corrosion was found on fairing 191 leading edge doublers. Maintenance removed and r eplaced the leading edge doublers IAW EMB-145 SRM 51-10-02, 51-20-03,04, 05 and 06. The repair was satisfactory, the ai rcraft will be released upon completion of inspection. 2 L 7 2 4F RT T00011AT 2002071500001 20020715 00001 NM 2002 7 15 751PA0002 1 20020712 A 3350 FLASHLIGHT BOEING 757 757200 1384950 NM A PIDA K NONE O OTHER UK UNKNOWN 1 SO 05 751PA 23928 Ref. MEL 25-63-4 Cont. # 0704003 R3 Door Emer. Flashlight Inop. Replaced Battery: Ops chk. good. Ref. MM 25-63-00. Th is clears MEL #0704003. 2 L 7 2 4F RT A2NM 2002071500002 20020715 00002 2002 7 15 HEEA080116 4 20020626 A 3455 066104701 TRANSCEIVER BELL 412 412 1182202 SW ADF SYSTEM INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 TRANSCEIVER INOPERATIVE. NO AUDIO AND WILL NOT POINT. 1 G 7 2 4U H4SW 2002071500003 20020715 00003 2002 7 15 251TR0002 4 20020709 A 2230 VANE BOEING 737 737228 13844AG NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 251TR 23792 Reference DMIReference DMI #0702001, Auto throttle will not engage with Capt. F/D chosen and go to max EPR in cruise flt . T/S system. Found Alpha vane failed & #2 auto throttle servo intermittent. Removed #1 AOA sensor, installed servicea ble #1 AOA sensor I/A/W MM 27-32-11, Ops chk. good I/A/W MM 22-11-381. Removed #2 auto servo, installed serviceable aut o servo mech. I/A/W MM 22-31-01, ops. chk. good. This clears DMI # 0702001. Placard removed. 2 L 7 2 4F RT A16WE 2002071500004 20020715 00004 2002 7 15 251TR0003 4 20020712 A 2210 VANE BOEING 737 737228 13844AG NM A PIDA K NONE O OTHER UK UNKNOWN 1 SO 05 251TR 23792 Reference DMI #0707002. Auto pilot V/S mode reverts to LVL change uncommanded. Alpha vane replaced. See item #1 log p age 09871, test C/W I/A/W ch. 22-11-381, ops chk. good. This clears DMI 0707002. Placard removed. 2 L 7 2 4F RT A16WE 2002071500005 20020715 00005 SW 2002 7 15 HEEA080118 1 20020626 A 2140 10544D HEATER BELL 412 412 1182202 SW CABIN FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 HEATER FAILED ZONE 4 TOUCH TEST. 1 G 7 2 4U H4SW 2002071500006 20020715 00006 SW 2002 7 15 HEEA080119 1 20020626 A 2842 2000838000001 PROBE BELL 412 412 1182202 SW FUEL QTY INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 LOW LIGHT COMES ON INTERMITTENTLY AND LOW FUEL INDICATION ON LEFT SIDE. 1 G 7 2 4U H4SW 2002071500007 20020715 00007 SW 2002 7 15 HEEA080120 1 20020626 A 6720 204001855001 LEVER BELL 412 412 1182202 SW TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 33073 T/R CONTROL LEVER IN HELL HOLE WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002071500008 20020715 00008 SW 2002 7 15 HEEA080121 1 20020626 A 2822 205060606003 PUMP BELL 412 412 1182202 SW FUEL BOOST MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 NR 1 FUEL TRANSFER LIGHT COMING ON. TO BE SENT TO VENDOR FOR REPAIR. 1 G 7 2 4U H4SW 2002071500009 20020715 00009 NM 2002 7 15 UPS02238717 1 20020701 A 3350 38931002 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE:N/A EXIT LIGHT ABOVE COCKPIT ENTRANCE DOOR DOES NOT TEST. CABIN DOOR ENTRANCE LIGHT CHECKS OK BUT CHARG E STAT US IS IN-DOUBT. R/R EMERGENCY EXIT LIGHT BATTERIES IN COCKPIT ENTRANCE DOOR AND CABIN DOOR, REF UPS 727 M/M CHAP 33-50-67 OPS CHECKED EMERGENCY EXIT LIGHTS OK. 2 L 7 3 4F A3WE 2002071500010 20020715 00010 NM 2002 7 15 UPS02238720 1 20020610 A 5210 TORQUE BOX BOEING 727 72722C 138400F NM ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CRACK IN TORQUE BOX OF FWD ENTRY DOOR WHERE LATCH ROD GOES THROUGH T-BOX. REPAIRED IAW SMRO EO2002 -035-001 UPS ENG FILE NR 727-52-20010. 2 L 7 3 4F A3WE 2002071500011 20020715 00011 NM 2002 7 15 UPS02238721 1 20020614 A 5313 STRINGER BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CRACK ON STRINGER FLANGE S21R BS 580-BS600. UPON FURTHER INVESTIGATION STRINGER CRACKED DUE TO COR ROSION. CORRODED SECTION CUT AWAY AND STRINGER REPAIRED IAW SRM 53-10-3 FIG 1 2 L 7 3 4F A3WE 2002071500012 20020715 00012 NM 2002 7 15 UPS02238722 1 20020613 A 7110 MOUNT BOEING 727 72722C 138400F NM NR 3 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI NR 3 ENG, FWD MOUNT FITTING HAS PITTING CORROSION IN BOLT HOLES. REPAIR CARRIED OUT IAW EOB727-544 0-11592 APPENDIX B. 2 L 7 3 4F A3WE 2002071500013 20020715 00013 NM 2002 7 15 UPS02238725 1 20020618 A 5320 BRACKET BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI DUCT WEB BRACKET CRACKED BS 1090 LBL 45.5. DUCT WEB BRACKET REPLACED IAW SRM 51-20-1, 51-10-02 AND 51-30-02. 2 L 7 3 4F A3WE 2002071500014 20020715 00014 NM 2002 7 15 UPS02238737 1 20020702 A 3350 LIGHT BOEING 727 72730C 1384009 NM COCKPIT NOT SEATED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ABOVE CABIN DOOR INOP. SEATED EXIT LIGHT ASSY OPS CHECKS GOOD 2 L 7 3 4F A3WE 2002071500015 20020715 00015 NM 2002 7 15 UPS02238738 1 20020612 A 5753 65192028 CARRIAGE BOEING 727 72722C 138400F NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI FLAP CARRIAGE NR 8 HAS SUSPECT CORROSION INSIDE SPINDLE BORE HOLE. CORROSION FOUND TO BE OUTSIDE L IMITS IAW OHM 57-58-01. REPLACED FLAP CARRIAGE IAW MM 27-51-13. 2 L 7 3 4F A3WE 2002071500016 20020715 00016 SW 2002 7 15 HEEA080122 1 20020626 A 2822 209011711001 IDLER GEAR BELL 412 412 1182202 SW FUEL BOOST WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 IDLER ASSY BEARINGS WORN. SCRAPPED. 1 G 7 2 4U H4SW 2002071500017 20020715 00017 NM 2002 7 15 UPS02238739 1 20020708 A 5753 CARRIAGE BOEING 727 72722C 138400F NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI FLAP CARRIAGE NR 1 HAS SUSPECT CORROSION INSIDE SPINDLE BORE. REMOVAL OF HARDWARE CORROSION FOUND ON SPINDLE SMALL BEARING SEAT. CORROSION FOUND TO BE OUTSIDE LIMITS OF OHM 57-58-01. FLAP CARRIAGE REPLACED IAW MM27-5 1-13. 2 L 7 3 4F A3WE 2002071500018 20020715 00018 NM 2002 7 15 UPS02238741 1 20020612 A 5753 CARRIAGE BOEING 727 72722C 138400F NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI FLAP CARRIAGE NR 2 HAS SUSPECT CORROSION INSIDE SPINDLE BORE. CORROSION FOUND TO BE OUTSIDE LIMITS IAW OHM 57-58-01. REPLACED FLAP CARRIAGE IAW MM 27-51-13. 2 L 7 3 4F A3WE 2002071500019 20020715 00019 NM 2002 7 15 UPS02238742 1 20020614 A 5310 DOOR FRAME BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CRACK ON FRAME BS 540 AT CARGO DOOR FITTING. CRACKED LUG OF BS 540 FRAME AT MCD LATCH SUPPORT FITT ING CUT AWAY IAW SRM 51-40-3. REPAIR PARTS FABRICATED IAW SRM 51-40-3. PARTS INSTALLED IAW SRM 51-30-02 AND SRM 51-40- 3. 2 L 7 3 4F A3WE 2002071500020 20020715 00020 NM 2002 7 15 UPS02238743 1 20020620 A 5320 FITTING BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI FLOOR TIE LUG CRACKED AT BS 1180 RBL 38 AFT CARGO BAY. FABRICATED TWO NEW ANGLES IAW DRAWING NR 65 -19606 AND SRM 51-20-1 FIG 7. INSTALLED BOTH ANGLES IAW SRM 51-30-2 AND DRAWING NR 65-19606. 2 L 7 3 4F A3WE 2002071500021 20020715 00021 NM 2002 7 15 UPS02238744 1 20020614 A 5320 ANGLE BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI INTERGRANULAR CORROSION ON FRAME ANGLE BS 328 AT ATTACH POINT TO S22R. FRAME ANGLE REPLACED IAW SR M 51-40-3 FIG 1 FROM BELOW S21R TO BETWEEN S22R AND S23R. 2 L 7 3 4F A3WE 2002071500022 20020715 00022 NM 2002 7 15 UPS02238748 1 20020618 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CORROSION ON FLOORBEAM WEB AFT SURFACE AT BS 890 RBL25. CORROSION REMOVED AND FOUND TO BE WITHIN L IMITS IAW 51-10-6 2 L 7 3 4F A3WE 2002071500023 20020715 00023 SW 2002 7 15 HEEA080123 1 20020626 A 7920 209062010001 VALVE BELL 412 412 1182202 SW ENGINE OIL LEAKING E HEEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 6559Z 36019 SCREWS LOOSE AND LEAKING. REPLACED WITH SERVICEABLE VALVE. 1 G 7 2 4U H4SW 2002071500024 20020715 00024 SW 2002 7 15 HEEA080124 1 20020626 A 7931 209070262101 INDICATOR BELL 412 412 1182202 SW ENG OIL TEMP MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 READS 20 PSI WITHOUT AIRCRAFT RUNNING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002071500025 20020715 00025 SW 2002 7 15 HEEA080125 1 20020626 A 6420 212011701101FM1 HUB BELL 412 412 1182202 SW TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 3285 33023 FEATHERING BEARINGS WORN. ALSO PITCH HORN (2 EACH) P/N 212-011-708-001, S/N RE0283 AND RE0253 WORN AND CORRODED BUSHING BORE. REPAIRED AND REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 4U H4SW 2002071500026 20020715 00026 SW 2002 7 15 HEEA080126 1 20020626 A 6320 212030104101 LINK BELL 412 412 1182202 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 LIFT LINK ASSY WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002071500027 20020715 00027 SW 2002 7 15 HEEA080127 1 20020626 A 5320 212030331103 PANEL BELL 412 412 1182202 SW FUSELAGE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 PANEL CORRODED AND DEBONDED. 1 G 7 2 4U H4SW 2002071500028 20020715 00028 EA 2002 7 15 SWIA200210865 1 20020521 A 2612 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 499SW 7398 L JETPIPE OVHT FAIL MESSAGE ILLUMINATED AT FL350. FOLLOWED QRH PROCEDURE, SWITCHED TO LOOP A. MESSAGE DID NOT PERSIST. TEN MINUTES LATER L JET PIPE OVHT WARNING SOUNDED. FOLLOWED EMERGENCY MEMORY ITEMS FOR THIS. THE WARNING EXTINGUISHE D AT APPR. 70% N1 AND WE DIVERTED TO PNS FOR A NORMAL LANDING.INSPECTED TAIL PIPE FOR HOT SPOTS. COULD NOT DUPLICATE FA ILURE DURING TEST AND RUN UP. PERFORMED CHECK AND INSPECTED WIRES ON LEFT JET PIPE LOOPS. COULD NOT GROUND DUPLICATE PROBLEM. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002071500030 20020715 00030 SO 2002 7 15 SWIA200210870 1 20020512 A 2120 ODOR EMB 120 EMB120ER 3260203 SO CABIN DETECTED A SWIA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 196SW 120151 WITH THE APU POWERED ON THE GROUND, WE HEARD A LOUD CLICKING NOISE, ELECTRIC LIGHT 3 CHIMES DOOR LIGHT ON MAP. WE ALSO DETECTED A PACK BURNING SMELL. RAN APU ON GROUND WITH APU GENERATOR ONLINE FOR 20 MINUTES, COULD NOT DUPLICATE. OPS CH ECK GOOD. OPERATED BOTH PACKS IAW MM 21-50-00, OPERATED NORMALLY, NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4T RT A31SO 2002071500031 20020715 00031 NE 2002 7 15 SWIA200210882 2 20020526 A 7313 O-RING EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NR 1 ENGINE LEAKING A SWIA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 196SW 120151 NR 1 ENGINE SMOKING HEAVILY FROM THE TOP OF THE COWL AFTER SHUT DOWN. FUEL WAS DRIPPING FROM UNDERNEATH THE ENGINE. FO UND FUEL NOZZLE (9 O'CLOCK POSITION) TRANSFER TUBES NOT SEATED. REPLACED O-RINGS ON TRANSFER TUBES AND SEATED. PERFORM ED LEAK CHECK. LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002071500032 20020715 00032 EA 2002 7 15 SWIA200210883 1 20020527 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 913SW 1048 1048 7597 STAB CH 1 & 2 AND MACH TRIM FAILED SHORTLY AFTER TAKEOFF. RAN QRH, RESET AND IT FAILED AGAIN. WAS ABLE TO GET ALL TO W ORK WHILE FLYING TO BURN OFF GAS. RETURNED TO BOI. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW 27-42-05. REMOVED AND REPLACED HSTA IAW 27-42-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002071500033 20020715 00033 EA 2002 7 15 SWIA200210884 1 20020528 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FAILED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 499SW 7398 PASSENGER DOOR INNER HANDLE DISCONNECTED. REMOVED AND REPLACED DOOR LATCH MECHANISM PER MM 52-11-02. CHECKS OK. 2 L 7 2 4F RT A21EA 2002071500034 20020715 00034 NM 2002 7 15 UPS02238749 1 20020618 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CORROSION ON FLOORBEAM WEB AFT SURFACE AT BS890 RBL 34, CORROSION REMOVED IAW 51-10-6 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. 2 L 7 3 4F A3WE 2002071500035 20020715 00035 NM 2002 7 15 UPS02238754 1 20020708 A 3350 100679 LIGHT BOEING 727 727172C 1384058 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:N/A EMERGENCY LT ABOVE L1 DOOR INOP REPORTED BY PREFLT CREW. REMOVED AND REPLACED L1 DOOR PORTABLE EMER GENCY EXIT LT AND BATTERIES PER BMM 33-50-67. OPS CK GOOD. 2 L 7 3 4F A3WE 2002071500036 20020715 00036 NM 2002 7 15 UPS02238757 1 20020618 A 5320 WEB BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CRACK ON SHEAR WEB LOCATED AT BS1130 LBL24.5. REPAIR CARRIED OUT IAW SRM51-40- 2 FIG1. 2 L 7 3 4F A3WE 2002071500037 20020715 00037 NM 2002 7 15 UPS02238759 1 20020612 A 5753 651920219 CARRIAGE BOEING 727 72722C 138400F NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI FLAP CARRIAGE NR 7 HAS SUSPECT CORROSION INSIDE SPINDLE BORE. FLAP CARRIAGE REPLACED AS CORROSION OUTSIDE LIMITS. 2 L 7 3 4F A3WE 2002071500038 20020715 00038 NM 2002 7 15 UPS02238762 1 20020620 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI LIGHT SURFACE CORROSION AROUND ANCHOR NUT AT BS 480 LBL 8 FLOORBEAM. CORROSION REMOVED AND FOUND O UTSIDE ALLOWABLE LIMITS OF SRM53-10-1 FIG 5. 2 L 7 3 4F A3WE 2002071500039 20020715 00039 NM 2002 7 15 UPS02238763 1 20020617 A 5320 69144723 TIE BOEING 727 72722C 138400F NM BS950 STR9 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI STRINGER TIE CRACKED BS 950 STR 6L. STRINGER TIE REPLACED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2002071500040 20020715 00040 WP 2002 7 15 CALA0200395 1 20020712 A 5311 FRAME DOUG DC9 DC982 3022082 WP STA 1463 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77827 49487 INSPECTION FOUND A 1.25" CRACK IN FRAME AT STA 1463 BETWEEN LONGERON 16R AND 17R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 02. 2 L 7 2 4F A6WE 2002071500041 20020715 00041 NM 2002 7 15 CALA0200396 1 20020714 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND FLOORBEAM CORRODED AT STA 294, RBL 36 TO RBL 49. A REPAIR WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2002071500042 20020715 00042 NM 2002 7 15 CALA0200397 1 20020714 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 1006-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND STRINGER 26R CORRODED AT STA 1006-1016. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002071500043 20020715 00043 NM 2002 7 15 UPS02238765 1 20020614 A 5320 ANGLE BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CORROSION ON FAIRING SUPPORT ANGLE BS 760 AIR CONDITIONING BAY AT LBL 10 AND RBL 10. ANGLE SECTION REPLACED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2002071500044 20020715 00044 SW 2002 7 15 HEEA080130 1 20020626 A 7120 212061117001 TUBE BELL 412 412 1182202 SW ENGINE MOUNT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 ENGINE MOUNT TUBE HAS WORN BEARING. SCRAPPED. 1 G 7 2 4U H4SW 2002071500045 20020715 00045 NM 2002 7 15 UPS02238779 1 20020610 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI SUSPECT CRACK IN FUSELAGE SKIN FROM FASTENER HOLE AT FWD UPPER CORNER OF FWD ENTRY DOOR CUT OUT. H EFC INSP CARRIED OUT IAW NDT MANUAL PT 6 51-00-00 FIG 4, CRACK CONFIRMED AND MEASURED AS 5MM IN LENGTH. REPAIR CARRIED OUT IAW UPS EO B727-5330-1460C. 2 L 7 3 4F A3WE 2002071500046 20020715 00046 SW 2002 7 15 HEEA080131 1 20020626 A 6320 212075036101 INDICATOR BELL 412 412 1182202 SW G/B OIL TEMP READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 INDICATOR READS 3 PSI LOW. REPLACED WITH SERVICEABLE INDICATOR. 1 G 7 2 4U H4SW 2002071500047 20020715 00047 SW 2002 7 15 HEEA080132 1 20020626 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 STEP ACTUATOR WILL NOT RETRACT. 1 G 7 2 4U H4SW 2002071500048 20020715 00048 SW 2002 7 15 HEEA080133 1 20020626 A 6730 212076005105 CYLINDER BELL 412 412 1182202 SW MAIN ROTOR LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 4866 33073 MAIN ROTOR SERVO CYLINDER LEAKS. 1 G 7 2 4U H4SW 2002071500049 20020715 00049 SW 2002 7 15 HEEA080134 1 20020626 A 2910 212076015001 VALVE BELL 412 412 1182202 SW HYD SYSTEM LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1202T 33112 HYD VALVE LEAKS OUT OF WEEP HOLE. 1 G 7 2 4U H4SW 2002071500050 20020715 00050 NM 2002 7 15 UPS02238780 1 20020619 A 5320 FITTING BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI DURING EDDY CURRENT INSP 5 HOLES WERE FOUND TO CONTAIN CORROSION AT LT BS 870 FITTING. REPAIRED IA W SMRO EO 2002-035-004 2 L 7 3 4F A3WE 2002071500051 20020715 00051 2002 7 15 HEEA080135 4 20020626 A 2200 2593996333 TARSYN BELL 412 412 1182202 SW AUTO FLIGHT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22608 33075 TARSYN 333 CAUSES YAW CHANNEL TO KICK. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002071500052 20020715 00052 SW 2002 7 15 HEEA080136 1 20020626 A 6320 3023721 FITTING BELL 412 412 1182202 SW GEARBOX DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 SUSPECT THAT COMBINING GEARBOX IS TRANSFERRING TO THE NR 1 ENGINE. SCRAPPED FITTING DUE TO GOUGHES ON FITTING FLARES. 1 G 7 2 4U H4SW 2002071500053 20020715 00053 SW 2002 7 15 HEEA080137 1 20020626 A 2140 3032708 HEATER BELL 412 412 1182202 SW CABIN FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 HEATER FAILED ZONE 4 TOUCH TEST. 1 G 7 2 4U H4SW 2002071500054 20020715 00054 SW 2002 7 15 HEEA080138 1 20020626 A 6320 3034508WFC FILTER BELL 412 412 1182202 SW GEARBOX BYPASSING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 C-BOX BYPASS FILTER BUTTON POPPED. SCRAPPED FILTER. 1 G 7 2 4U H4SW 2002071500056 20020715 00056 SW 2002 7 15 HEEA080139 1 20020626 A 2841 39322419003 INDICATOR BELL 412 412 1182202 SW FUEL QTY ERRATIC E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2149S 36002 FUEL QTY INDICATOR HAS ERRATIC READINGS ON RIGHT SIDE AND DIGITAL TOTALIZER. 1 G 7 2 4U H4SW 2002071500059 20020715 00059 NM 2002 7 15 UPS02438703 1 20020516 A 5712 65B078466 RIB BOEING 747 747121 1384871 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C RT WING- NR 25 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1-NR 6 BOLT HOLE FOUND SURFACE CORROS ION. RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2002071500060 20020715 00060 SW 2002 7 15 HEEA080140 1 20020626 A 6230 412010406115 LINK BELL 412 412 1182202 SW SWASHPLATE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 LINK ASSY WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002071500061 20020715 00061 SW 2002 7 15 HEEA080141 1 20020626 A 6230 412010406115 LINK BELL 412 412 1182202 SW SWASHPLATE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 LINK ASSY WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002071500062 20020715 00062 SW 2002 7 15 HEEA080142 1 20020626 A 6210 412015300109 BLADE BELL 412 412 1182202 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2014K 12342 33020 OUTBOARD ABRASION STRIP HAS SEVERAL HOLES AND SEPARATION ON TRIM TABS. 1 G 7 2 4U H4SW 2002071500063 20020715 00063 SW 2002 7 15 HEEA080143 1 20020626 A 6210 412015300109 BLADE BELL 412 412 1182202 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2014K 11940 33020 OUTBOARD ABRASION STRIP HAS SEVERAL HOLES AND SEPARATION ON TRIM TABS. 1 G 7 2 4U H4SW 2002071500064 20020715 00064 SW 2002 7 15 HEEA080144 1 20020626 A 6210 412015300109 BLADE BELL 412 412 1182202 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 13660 33115 OUTBOARD ABRASION STRIP HAS SEVERAL HOLES THROUGH THE STRIP. 1 G 7 2 4U H4SW 2002071500065 20020715 00065 SW 2002 7 15 HEEA080145 1 20020626 A 6210 412015300109 BLADE BELL 412 412 1182202 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 9396 36019 OUTBOARD ABRASION STRIP HAS SEVERAL PIN HOLES. 1 G 7 2 4U H4SW 2002071500066 20020715 00066 SW 2002 7 15 HEEA080146 1 20020626 A 6210 412015300109 BLADE BELL 412 412 1182202 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 9396 36019 OUTBOARD ABRASION STRIP HAS SEVERAL PIN HOLES. 1 G 7 2 4U H4SW 2002071500067 20020715 00067 SW 2002 7 15 HEEA080147 1 20020626 A 3212 412050017133 COVER BELL 412 412 1182202 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 VELCRO IS TORN ON FLOAT COVER. 1 G 7 2 4U H4SW 2002071500068 20020715 00068 SW 2002 7 15 HEEA080148 1 20020626 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW TORQUE INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 NR 2 NEEDLE STICKS INTERMITTENTLY ON TORQUE INDICATOR. 1 G 7 2 4U H4SW 2002071500069 20020715 00069 NM 2002 7 15 UPS02438704 1 20020516 A 5712 65B101396 RIB BOEING 747 747121 1384871 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C RT WING- NR 20 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 5, NR 8 BOLT HOLE FOUND SURFACE CORRO SION. RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2002071500071 20020715 00071 NM 2002 7 15 UPS02438705 1 20020516 A 5712 65B078486 RIB BOEING 747 747121 1384871 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C RT WING- NR 25 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT BOLT HOLE FOUND SURFACE CORROSION. FROM NR 1 - NR 8 BOLT HOLE. RIB REPLACED IAW SRM 51- 10-01 PG 8 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2002071500072 20020715 00072 SW 2002 7 15 HEEA080150 1 20020626 A 2840 473203003 SIGNAL COND UNIT BELL 412 412 1182202 SW FUEL SYSTEM MALFUNCTIONED E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 2149S 36002 NR 1 FUEL TRANSFER LIGHT COMING ON IN FLIGHT. 1 G 7 2 4U H4SW 2002071500073 20020715 00073 NM 2002 7 15 UPS02438706 1 20020516 A 5712 65B101476 RIB BOEING 747 747121 1384871 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C RT WING- NR 18 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1-NR 8 BOLT HOLE FOUND SURFACE CORROS ION. RIB REPLACED IAW SRM 51- 10-01 PG 8 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2002071500074 20020715 00074 2002 7 15 HEEA080151 4 20020626 A 3421 504001790116 GYRO BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2149S 36002 TAKES A LOT OFF AMPS TO TEST. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002071500075 20020715 00075 NM 2002 7 15 UPS02438708 1 20020626 A 3350 LIGHT BOEING 747 747200 1384847 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 528UP 1 INSPECTION TYPE:N/A CREW SERVICE DOOR OVERHEAD EMERGENCY LIGHT INOP. R&R CREW SERVICE DOOR OVERHEAD EMERGENCY LIGHT ASS Y OPS CHECK PER MM 33-51-07. NO DEFECTS NOTED. 2 L 7 4 4F RT A20WE 2002071500076 20020715 00076 SW 2002 7 15 HEEA080152 1 20020626 A 2420 51509002R CONTROL UNIT BELL 412 412 1182202 SW GENERATOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 GENERATOR WENT OFF LINE AND WON'T RESET. 1 G 7 2 4U H4SW 2002071500078 20020715 00078 NM 2002 7 15 UPS02438716 1 20020628 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN DIRTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:PFLT EMERGENCY LIGHT OVER CREW SERVICE DOOR BULB INOP. CLEANED AND RESEATED CP AT UPPER LIGHT ASSY OPS CK OK. 2 L 7 4 4F A20WE 2002071500079 20020715 00079 SW 2002 7 15 HEEA080154 1 20020626 A 3212 D24922117 FLOAT BELL 412 412 1182202 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 EMERGENCY FLOAT BAG LEAKING. 1 G 7 2 4U H4SW 2002071500081 20020715 00081 SW 2002 7 15 HEEA080158 1 20020626 A 6720 PHI41294 BUSHING BELL 412 412 1182202 SW TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 BEARINGS AND BUSHINGS WORN. REPAIRED. 1 G 7 2 4U H4SW 2002071500082 20020715 00082 SW 2002 7 15 HEEA080162 1 20020626 A 6300 206033518005 STOP BELL 206 206L3 1182108 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251Y 51556 MAIN ROTOR STOP HAS WORN RUBBER. TO BE SENT TO VENDOR. 1 G 7 1 3U H2SW 2002071500083 20020715 00083 SW 2002 7 15 HEEA080163 1 20020626 A 6300 206033518007 STOP BELL 206 206L3 1182108 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251Y 51556 MAIN ROTOR STOP HAS WORN RUBBER. TO BE SENT TO VENDOR. 1 G 7 1 3U H2SW 2002071500084 20020715 00084 SW 2002 7 15 HEEA080164 1 20020626 A 3212 206050248117 FLOAT BELL 206 206L3 1182108 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251X 51552 EMERGENCY FLOAT BAG LEAKS. TO BE SENT TO VENDOR. 1 G 7 1 3U H2SW 2002071500085 20020715 00085 SW 2002 7 15 HEEA080165 1 20020626 A 3246 206323017 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141BH 51303 DEEP PITS OF CORROSION NEAR MOUNTING STRAPS FOR SADDLES AND ALSO UNDER SADDLE EDGE. TO BE SENT TO VENDOR. 1 G 7 1 3U H2SW 2002071500086 20020715 00086 SW 2002 7 15 HEEA080166 1 20020626 A 3246 206323017 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41791 51465 DEEP PITS OF CORROSION NEAR MOUNTING STRAPS FOR SADDLES AND ALSO UNDER SADDLE EDGE. TO BE SENT TO VENDOR. 1 G 7 1 3U H2SW 2002071500087 20020715 00087 SW 2002 7 15 HEEA080167 1 20020626 A 6320 406040056101 CASE 206040004107 BELL 206 206L3 1182108 SW GEARBOX CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8588X A10 51486 INDICATIONS FOUND ON WEBS DURING NDT INSPECTION OF CASE. TO BE SENT TO VENDOR. 1 G 7 1 3U H2SW 2002071500088 20020715 00088 SW 2002 7 15 HEEA080169 1 20020626 A 3212 1100891S FITTING BELL 407 407 1182206 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 723PH 53283 CORRODED AT FLARED END OF FITTING. 1 G 7 1 3U O H2SW 2002071500089 20020715 00089 SW 2002 7 15 HEEA080170 1 20020626 A 2822 1C2710 CARTRIDGE BELL 407 407 1182206 SW FUEL SYSTEM FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4999 53323 RT FUEL TRANSFER LIGHT ILLUMINATED IN FLIGHT. 1 G 7 1 3U O H2SW 2002071500090 20020715 00090 SW 2002 7 15 HEEA080171 1 20020626 A 6710 206001396001 SHAFT BELL 407 407 1182206 SW CYCLIC STICK BENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 496PH 53398 THREADS STRIPPED AND SHAFT BENT. 1 G 7 1 3U O H2SW 2002071500091 20020715 00091 SW 2002 7 15 HEEA080172 1 20020626 A 6520 206011728001 TRUNNION BELL 407 407 1182206 SW T/R GEARBOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 TAIL ROTOR GEARBOX TRUNNION WORN. 1 G 7 1 3U O H2SW 2002071500092 20020715 00092 SW 2002 7 15 HEEA080173 1 20020626 A 5311 206032308121S FRAME BELL 407 407 1182206 SW FUSELAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406PH 53198 FRAME CRACKED UPPER RT CORNER. 1 G 7 1 3U O H2SW 2002071500093 20020715 00093 SW 2002 7 15 HEEA080174 1 20020626 A 3212 206050247131 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 EMERGENCY FLOAT COVER TORN. 1 G 7 1 3U O H2SW 2002071500094 20020715 00094 SW 2002 7 15 HEEA080175 1 20020626 A 3212 206050247132 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 EMERGENCY FLOAT COVER TORN. 1 G 7 1 3U O H2SW 2002071500095 20020715 00095 SW 2002 7 15 HEEA080176 1 20020626 A 3212 206050247132 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 501PH 53401 EMERGENCY FLOAT COVER TORN AND VELCRO WORN. 1 G 7 1 3U O H2SW 2002071500096 20020715 00096 SW 2002 7 15 HEEA080177 1 20020626 A 3212 206050247135 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 EMERGENCY FLOAT COVER TORN. 1 G 7 1 3U O H2SW 2002071500097 20020715 00097 SW 2002 7 15 HEEA080178 1 20020626 A 3212 206050247135 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4999 53323 EMERGENCY FLOAT COVER FRONT CAP DETERIORATED. 1 G 7 1 3U O H2SW 2002071500098 20020715 00098 SW 2002 7 15 HEEA080179 1 20020626 A 3212 206050247135 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 501PH 53401 EMERGENCY FLOAT COVER TORN AND VELCRO WORN. 1 G 7 1 3U O H2SW 2002071500099 20020715 00099 SW 2002 7 15 HEEA080180 1 20020626 A 3212 206050247135 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 719PH 53266 EMERGENCY FLOAT COVER FRONT FLAP FRAYED AND TORN. 1 G 7 1 3U O H2SW 2002071500100 20020715 00100 SW 2002 7 15 HEEA080181 1 20020626 A 3212 206050247135 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 742PH 53461 EMERGENCY FLOAT COVER TORN AND WORN. 1 G 7 1 3U O H2SW 2002071500101 20020715 00101 SW 2002 7 15 HEEA080182 1 20020626 A 3212 206050247137 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 EMERGENCY FLOAT COVER TORN. 1 G 7 1 3U O H2SW 2002071500102 20020715 00102 SW 2002 7 15 HEEA080183 1 20020626 A 3212 206050247137 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 496PH 53398 EMERGENCY FLOAT COVER TORN. 1 G 7 1 3U O H2SW 2002071500103 20020715 00103 SW 2002 7 15 HEEA080184 1 20020626 A 3212 206050247138 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 53400 EMERGENCY FLOAT COVER TORN. 1 G 7 1 3U O H2SW 2002071500104 20020715 00104 SW 2002 7 15 HEEA080185 1 20020626 A 3212 206050247138 COVER BELL 407 407 1182206 SW EMERGENCY FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 501PH 53401 EMERGENCY FLOAT COVER TORN. 1 G 7 1 3U O H2SW 2002071500105 20020715 00105 SW 2002 7 15 HEEA080186 1 20020626 A 3246 206053184121 SKID BELL 407 407 1182206 SW MLG DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 LT SKID TUBE DAMAGED BEYOND LIMITS. 1 G 7 1 3U O H2SW 2002071500106 20020715 00106 SW 2002 7 15 HEEA080187 1 20020626 A 6510 206061432121 HOUSING BELL 407 407 1182206 SW BLOWER CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 723PH 53283 TAIL ROTOR BLOWER HOUSING CRACKED IN AFT UPPER LT CORNER. 1 G 7 1 3U O H2SW 2002071500107 20020715 00107 SW 2002 7 15 HEEA080188 1 20020626 A 2435 BRUSHES BELL 407 407 1182206 SW STARTER GEN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 495PH 940 Y0292 53397 STARTER GEN BRUSHES WORN AT 300 HOUR INSPECTION. 1 G 7 1 3U O H2SW 2002071500108 20020715 00108 SW 2002 7 15 HEEA080189 1 20020626 A 2435 BRUSHES BELL 407 407 1182206 SW STARTER GEN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 496PH 2207 99333 53398 STARTER GEN BRUSHES WORN. 1 G 7 1 3U O H2SW 2002071500109 20020715 00109 SW 2002 7 15 HEEA080190 1 20020626 A 2435 BRUSHES BELL 407 407 1182206 SW STARTER GEN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 501PH 3402 2591 53401 STARTER GEN BRUSHES WORN. 1 G 7 1 3U O H2SW 2002071500110 20020715 00110 SW 2002 7 15 HEEA080198 1 20020626 A 7160 206064912103 SEAL BELL 407 407 1182206 SW COWLING TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 COWLING SEAL TORN. 1 G 7 1 3U O H2SW 2002071500111 20020715 00111 SW 2002 7 15 HEEA080199 1 20020626 A 3212 206073847103 ADAPTER 407073848101 BELL 407 407 1182206 SW FLOAT BOTTLE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 263 53159 EMERGENCY FLOAT BOTTLE MANIFOLD ADAPTER CORRODED. 1 G 7 1 3U O H2SW 2002071500112 20020715 00112 SW 2002 7 15 HEEA080200 1 20020626 A 2913 206076030111 PUMP BELL 407 407 1182206 SW HYD SYSTEM WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 53400 HYD PUMP HAS WORN SPLINES. 1 G 7 1 3U O H2SW 2002071500113 20020715 00113 NM 2002 7 15 UPS02438750 1 20020707 A 3350 BATTERY BOEING 747 747121 1384871 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:N/A MAIN DECK EMERGENCY LIGHT INOP. CHARGED EMERGENCY LIGHTS, OPS CHECK NORMAL 2 L 7 4 4F A20WE 2002071500114 20020715 00114 SW 2002 7 15 HEEA080201 1 20020626 A 2810 206362002103 SEAL BELL 407 407 1182206 SW FUEL CAP CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 FUEL CAP SEAL CRACKED. 1 G 7 1 3U O H2SW 2002071500115 20020715 00115 SW 2002 7 15 HEEA080202 1 20020626 A 3212 206373902103 RELIEF VALVE BELL 407 407 1182206 SW FLOAT BOTTLE LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 494PH 53396 EMERGENCY FLOAT BOTTLE RELIEF VALVE LEAKING. 1 G 7 1 3U O H2SW 2002071500116 20020715 00116 NM 2002 7 15 UPS02438755 1 20020703 A 5412 BULKHEAD BOEING 747 747200 1384847 NM #3 NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE:SPC NR 3 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD CRACK REVEALED AT O/B FWD & AFT WEB AREA APPROX AT 5 O 'CLOCK POSTION. NR 3 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD CRACKED AREA REPAIRED PER HX RS R-54-53-34827 WITH REPAIR KIT INSTALLED PER REPAIR DWG 65B07 582 SHT 8. 2 L 7 4 4F RT A20WE 2002071500117 20020715 00117 SW 2002 7 15 HEEA080203 1 20020626 A 3212 212073905001 GAUGE BELL 407 407 1182206 SW FLOAT BOTTLE LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 494PH 53396 EMERGENCY FLOAT BOTTLE GAUGE IS LEAKING. 1 G 7 1 3U O H2SW 2002071500118 20020715 00118 SW 2002 7 15 HEEA080204 1 20020626 A 6340 214040806003 PRESSURE SWITCH BELL 407 407 1182206 SW GEARBOX PRESSURE FAILED E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 724PH 53327 TRANSMISSION PRESSURE LIGHT INTERMITTENT. 1 G 7 1 3U O H2SW 2002071500119 20020715 00119 NM 2002 7 15 UPS02538752 1 20020704 A 5610 WINDSHIELD BOEING 757 75724APF 1384969 NM COCKPIT ARCED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 437UP 25468 INSPECTION TYPE:N/A LT WINDSHIELD ARCING. R&R NR 1 WINDSHIELD REF L/P 836874 ITEM 2 & 3 REF 56-11-01-4 OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A2NM 2002071500120 20020715 00120 NM 2002 7 15 UPS02638751 1 20020706 A 5754 SKIN BOEING 767 76734AF 1385212 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 327UP 27753 INSPECTION TYPE:N/A NR 7 SLAT LEADING EDGE INBD CORNER CRACKED. REMOVED AND REPLACED NR 7 SLAT INBD BOTTOM SKIN PER SRM 51-10-02 & SRM 51-40-02, OPS CHK LEADING EDGE SLAT PER MM 27-81-00. 2 L 7 2 4F RT A1NM 2002071500121 20020715 00121 SW 2002 7 15 HEEA080205 1 20020626 A 7712 222375077119 TRANSMITTER BELL 407 407 1182206 SW TORQUE CONTAMINATED E HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 742PH 53461 ERRONEOUS HIGH READINGS, FOUND WATER IN WIRING CONNECTORS. 1 G 7 1 3U O H2SW 2002071500122 20020715 00122 GL 2002 7 15 HEEA080206 2 20020626 A 7532 23005366 BLEED VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4999 53323 ENGINE HAD A SUDDEN INCREASE IN TOT CAUSING A LOW POWER ENGINE. REPLACED WITH SERVICEABLE BLEED VALVE. 1 G 7 1 3U 3 U O H2SW E1GL 2002071500123 20020715 00123 GL 2002 7 15 HEEA080207 2 20020626 A 7532 23005366 BLEED VALVE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406PH 7246 53198 HIGH TOT. REPLACED WITH SERVICEABLE BLEED VALVE. 1 G 7 1 3U 3 U O H2SW E1GL 2002071500124 20020715 00124 SW 2002 7 15 HEEA080208 1 20020626 A 2912 23066697 FILTER BELL 407 407 1182206 SW HYD SYSTEM BYPASSING E HEEA O OTHER J WARNING INDICATION IN INSP/MAINT 1 SW 03 402PH 53159 FILTER POPPED BYPASS IND. 1 G 7 1 3U O H2SW 2002071500125 20020715 00125 WP 2002 7 15 0202139975 1 20020621 A 5310 FRAME DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9339 47382 During H-CK at ATL base MTC. a 1/2" crack was found at sta 1132 on the forward side of the 9911839-19 doubler. The crack extended from the upper pulley bracket hole for NAS 1105 on the LH side of the aircraft in the outboard direction. Repa ired per EA 99-190511. 2 L 7 2 4F A6WE 2002071500126 20020715 00126 WP 2002 7 15 0202149975 1 20020627 A 5710 CAP DOUG DC9 DC931 3022065 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9339 47382 During Mck in Atl, corrosion was found in the upper flange of the center wing upper skin cap. The cap is located at sta 681. The corrosion was blended out and at one location was determined to be out of limit. Repaired per EA 99-190519. 2 L 7 2 4F A6WE 2002071500127 20020715 00127 WP 2002 7 15 0202159975 1 20020627 A 5710 CAP DOUG DC9 DC931 3022065 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9339 47382 During an MCK in ATL, corrosion was found in the upper flange of the center wing upper skin cap. The cap is located at s ta 681. The corrosion was blended out and at three locations was determined to be ouit of limits. Repaired per EA 99-190 532. 2 L 7 2 4F A6WE 2002071500128 20020715 00128 WP 2002 7 15 0202169851 1 20020613 A 5310 INTERCOSTAL DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NC 47708 During an Mck in ATL, the centerline intercostal, between station 218 and 237 was found cracked.Repaired per EA 98-19047 6. 2 L 7 2 4F RT A6WE 2002071500129 20020715 00129 WP 2002 7 15 0202179851 1 20020617 A 5310 PRESSURE PANEL DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NC 47708 During MCK in ATL, cracks were found in the flight compartment horizontal pressure panel at statio 105. The cracks are l ocated at sta x=-25 (1.0") and x=-35 (.75"). Repaired per EA 98-190448. 2 L 7 2 4F RT A6WE 2002071500130 20020715 00130 WP 2002 7 15 0202189851 1 20020620 A 5330 DOOR FRAME DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NC 47708 During Mck in ATL, a crack was found in the forward passenger door doorjamb upper forward corner. Both the fuselage skin and the internal doorjamb doubler were cracked.Repaired per EA 98-190455. 2 L 7 2 4F RT A6WE 2002071500131 20020715 00131 WP 2002 7 15 0202199851 1 20020620 A 5310 INTERCOSTAL DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NC 47708 During an MCK in ATL, a crack was found in the intercostal that extends from station 148.5 to 160 at approx z=44. The cr ack extended from the upper edge of the inboard flange to the forward most lightning hole. Repaired per EA 98-190459. 2 L 7 2 4F RT A6WE 2002071500132 20020715 00132 WP 2002 7 15 0202209851 1 20020628 A 5310 DOOR FRAME DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NC 47708 During an MCK in ATL, a crack was found in the cargo doorjamb pan at station 1108 between doorstops 2 and 3. Repaired pe r EA 98-190540. 2 L 7 2 4F RT A6WE 2002071500133 20020715 00133 WP 2002 7 15 0202219851 1 20020701 A 5310 DOOR SEAL DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NC 47708 During Mck in ATL, the upper aft portion of the aft cargo door seal depressor was found broken at station 1108 between d oor stops 3 and 4. Repaired per EA 98-190490. 2 L 7 2 4F RT A6WE 2002071500134 20020715 00134 WP 2002 7 15 UPS02838620 1 20020525 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 MAIN CABIN FLOOR SUPPORT AT STA 1762 RBL 11 HAS DRILL STARTS WITH CORROSION. REMOVED FLOOR BOARD SUP PORT IAW DC8 SRM 51-1-20D. FABBED FLOOR BOARD SUPPORT IAW DC8 SRM 53-7-1 AND INSTALLED SUPPORT IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002071500135 20020715 00135 GL 2002 7 15 HEEA080209 2 20020626 A 7320 23072725 HMU BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUEL CONTROL FAILED E HEEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 03 3193E 1889 53276 WHEN ADVANCING THE THROTTLE UP FROM IDLE, COMPRESSOR STALLS. TURNING ON ENGINE ANTI-ICE WILL CAUSE PROBLEM TO GO AWAY. 1 G 7 1 3U 3 U O H2SW E1GL 2002071500136 20020715 00136 WP 2002 7 15 UPS02838621 1 20020526 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 MAIN CABIN FLOORBEAM CORRODED AROUND NUTPLATE STA 980 LBL 10. REPLACED SECTION OF FLOORBEAM CAP IAW DC8 SRM 53-2-0 TR 53-124 2 L 7 4 4F RT 4A25 2002071500137 20020715 00137 SW 2002 7 15 HEEA080210 1 20020626 A 5343 400052007109 BEAM BELL 407 407 1182206 SW MLG DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 DAMAGED AT BUSH AREA. TO BE SENT TO VENDOR. 1 G 7 1 3U O H2SW 2002071500138 20020715 00138 SW 2002 7 15 HEEA080211 1 20020626 A 1430 400052009101 BOLT BELL 407 407 1182206 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 MLG BOLT CORRODED BEYOND LIMITS. 1 G 7 1 3U O H2SW 2002071500139 20020715 00139 WP 2002 7 15 UPS02838622 1 20020527 A 5320 4751625A1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 LONGERON FITTING CRACKED STA 680-11R. R&R FITTING IAW DC8 MM 51-1-21 & 51-1-24. 2 L 7 4 4F RT 4A25 2002071500140 20020715 00140 SW 2002 7 15 HEEA080212 1 20020627 A 6510 406001704101 BELLCRANK BELL 407 407 1182206 SW TAIL ROTOR WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 490PH 2420 53378 TAIL ROTOR BELLCRANK HAS A WORN BEARING. 1 G 7 1 3U O H2SW 2002071500141 20020715 00141 WP 2002 7 15 UPS02838623 1 20020527 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 MAIN CABIN STA STA 1334 AND BL 0 SEAT TRACK IS CRACKED. R&R DAMAGED SECTION OF SEAT TRACK IAW UPS EO DC8-5320-5767 2 L 7 4 4F RT 4A25 2002071500142 20020715 00142 SW 2002 7 15 HEEA080215 1 20020627 A 6230 406010401117 SWASHPLATE BELL 407 407 1182206 SW MAIN ROTOR LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 491PH 2755 53386 MAIN ROTOR SWASHPLATE HAS GREASE LEAKING THROUGH UPPER SEAL. 1 G 7 1 3U O H2SW 2002071500143 20020715 00143 SO 2002 7 15 SIMA200217706 1 20020619 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 DURING AN IMBV INSPECTION FOUND CARGO DOOR LOWER SILL CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL. INSTALLED NEW BEAM IAW SRM. 2 L 7 2 4T RT T00011AT 2002071500144 20020715 00144 WP 2002 7 15 UPS02838624 1 20020523 A 5720 ANGLE DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 RT WING FLAPWELL ATTACH ANGLE AT XW0 REAR SPAR CRACKED. FABBED ANGLE IAW DAC DWG 5651221 & INSTALLE D ANGLE AND SKIN PANEL IAW DC8 SRM 51-1-21 51-3-0. 2 L 7 4 4F RT 4A25 2002071500145 20020715 00145 WP 2002 7 15 UPS02838626 1 20020524 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 AFT CARGO BAY FRAME IS CORRODED STA 1100 STR 36. REMOVED CORROSION, REMOVED DAMAGED SECTION OF FRAME , FABBED REPAIR ANGLE FILLERS & REPAIR STRAP LOCATED DRILLED REPAIR PARTS & INSTALLED REPAIR ANGLE FILLERS & REPAIR STR AP IAW UPS EO DC8-5310-117 28 APP B DC8 SRM 51-1-8 53-2-0 51-1-24 & DAC DWG 2537716 2 L 7 4 4F RT 4A25 2002071500146 20020715 00146 WP 2002 7 15 UPS02838627 1 20020524 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 AFT CARGO BAY CORRODED UNDER NUTPLATE ON FRAME STA 1020 STRINGER 34R. REMOVED CORROSION, OUT OF LIMI TS. FABBED DOUBLER & FILLERS. INSTALLED DOUBLERS & FILLER GUSSETS & CLIP IAW EO DC8-5310-11728 DWG DC8-53A-011 SRM 53-2 -0 51-1-8 51-1-24 51-1-20D 2 L 7 4 4F RT 4A25 2002071500147 20020715 00147 SO 2002 7 15 SIMA200216407 1 20020611 A 5300 GUSSET EMB 135 EMB135LR 3260305 SO CTR, FR 20-22 GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 CENTER GUSSET GOUGED FROM FRAMES 20 T0 22. C/A REMOVED GOUGED BY BLENDING, WITHIN SRM LIMITS. RESTORED SURFACE PROTECT ION. 2 L 7 2 4F RT T00011AT 2002071500148 20020715 00148 WP 2002 7 15 UPS02838630 1 20020512 A 5320 37549182N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 ABOVE RT CUSP AT STA 1170-1180 C PIT TORQUE BOX FITTING IS CRACKED. REMOVED AND REPLACED CRACKED FIT TING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002071500149 20020715 00149 WP 2002 7 15 UPS02838631 1 20020601 A 5210 5597646107 WEB DOUG DC8 DC871F 302199D WP L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 L1 DOOR FWD CENTER TORQUE BOX WEB CRACKED. REMOVED DAMAGED WEB. FABRICATED NEW WEB IAW DWG 5597646. INSTALLED WEB IAW DC8 SRM 51-3-0 2 L 7 4 4F RT 4A25 2002071500150 20020715 00150 WP 2002 7 15 UPS02838632 1 20020515 A 5320 5711283U515 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 C-PIT TORQUE BOX WEB AND FITTING HAVE ELONGATED HOLES. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1 -24 FABBED & INSTALLED DOUBLER IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 2002071500151 20020715 00151 WP 2002 7 15 UPS02838633 1 20020511 A 5320 3779970512 ATTACH FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C-1 MAIN CABIN LT SIDE STA 780 L14L FRAME TO LONGERON ATTACH FITTING IS CRACKED. REMOVED FITTING & INST ALLED NEW FITTING IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002071500152 20020715 00152 WP 2002 7 15 UPS02838642 1 20020614 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:PFLT COCKPIT EMERGENCY LIGHTS ILLUMINATED BUT UNABLE TO EXTINGUISH AFTER RESET AND ARMED. PERFORMED OPE RATIONAL CHECK PER MM 33-50-01 OPS CHECKS OK. 2 L 7 4 4F RT 4A25 2002071500153 20020715 00153 WP 2002 7 15 UPS02838650 1 20020529 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 AFT PIT FS 1160 C3 DOOR RAMP PANEL SUPPORT FITTING AT L27L - L34 IS CRACKED. REMOVED SUPPORT FITTING LOCATED & DRILLED HOLES IAW DC8 SRM 51-1-24 INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002071500154 20020715 00154 WP 2002 7 15 UPS02838652 1 20020607 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 STA 940 RT FRAME FITTING AT PRESSURE WEB IS CRACKED. REMOVED INTERCOSTAL AND FITTING L21 LOCATED & D RILLED NEW FITTING IAW DAC DWG 5751966 INSTALLED END FITTING AND INTERCOSTAL IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002071500155 20020715 00155 NM 2002 7 15 ABAX020004 1 20020625 A 5210 MECHANISM BOEING 767 767231 1385131 NM PAX DOOR OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 708AX 22571 THE FORCE TO MOVE THE MAIN ENTRY DOOR TO THE CLOSED POSITION WAS EXCESSIVE. COMPLIED WITH ENTRY DOOR COUNTERBALANCE ADJ USTMENT IAW 767 AMM 52-11-16. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2002071500156 20020715 00156 NM 2002 7 15 ABXA010914 1 20020618 A 2780 SLAT BOEING 767 767231 1385131 NM WING MALFUNCTIONED A ABXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 23 707AX 22570 FLT 407- THE CREW DECLARED AN EMERGENCY AND PERFORMED A GO-AROUND INBOUND TO ILN. EICAS MSG LE SLAT ASYM DISPLAYED. LE ADING EDGE LIGHT ILLUMINATED WITH FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. COMPLETED FIM PROCEDURES IAW B767 FIM 27A-81-00. LIGHTS AND MESSAGE EXTINGUISHED DURING PROCEDURES. TESTED GOOD. CYCLED FLAPS AND SLATS. NO FURTHER FAU LTS. 2 L 7 2 4F RT A1NM 2002071500157 20020715 00157 WP 2002 7 15 ABXA010915 1 20020620 A 2932 CONNECTOR DOUG DC8 DC863F 302198F WP HYD SYSTEM LOOSE A ABXA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 811AX 46113 AIR RETURN TO MIA DUE TO LOSS OF HYDRAULIC FLUID. AIRCRAFT DUMPED FUEL IN PREPARATION FOR RETURN TO MIA. FOUND CONNECT OR ON HYDRAULIC QUANTITY TRANSMITTER LOOSE. CLEANED AND RESECURED. SYSTEM OPS CHECKED GOOD. CHECKED FUEL DUMP SYSTEM AFTER USE, FOUND ALL NORMAL IAW DC-8 MM 28-30-0. 2 L 7 4 4F 4A25 2002071500158 20020715 00158 NM 2002 7 15 ABXA010917 1 20020624 A 5230 140T26073 CAP BOEING 767 767200 1385120 NM CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 FORWARD CARGO DOOR TOP T-CAP HAD OUT OF LIMITS CORROSION AT SEVERAL AREAS. FABRICATED T-CAP IAW BOEING DWG 140T2607. I NSTALLED T-CAP AND WEBS IAW B767 SRM 51-40-02. INSTALLED CARGO DOOR IAW B767 MM 52-34-01. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2002071500159 20020715 00159 WP 2002 7 15 ABXA010918 1 20020624 A 5610 5613217508 WINDOW DOUG DC8 DC861 3021952 WP COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 852AX 46016 CAPTAIN'S SLIDING WINDOW WOULD NOT CLOSE OR OPEN. WINDOW WAS JAMMED. FOUND CAPTAIN'S SLIDING WINDOW, TOP FORWARD CORNE R OUT OF ALIGNMENT. REALIGNED WINDOW. OPS CHECKED GOOD IAW DC-8 MM, CHAPTER 56. 2 L 7 4 4F 4A25 2002071500160 20020715 00160 WP 2002 7 15 ABXA020001 1 20020624 A 3350 LIGHT DOUG DC8 DC861 3021952 WP COCKPIT INOPERATIVE A ABXA K NONE L NO TEST NR NOT REPORTED 1 GL 23 853AX 46037 EMERGENCY EXIT LIGHT DISARM LIGHT, AMBER LIGHT WAS INOP. RELAMPED, OPS CHECKED NORMAL, REF DC-8 MM 33L. 2 L 7 4 4F 4A25 2002071500161 20020715 00161 WP 2002 7 15 ABXA020006 1 20020619 A 2170 21D10 COALESCER BAG DOUG DC9 DC941 302207N WP A/C BAY DIRTY A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 979AX 47492 AIR CONDITIONING SUPPLY AIR SMELLED HOT OR OILY AT HIGHER (CRUISE) POWER SETTINGS. REPLACED BOTH WATER SEPARATOR COALES CER BAGS IAW DC9 MM 21-20-02-2. 2 L 7 2 4F A6WE 2002071500162 20020715 00162 WP 2002 7 15 ABXA020007 1 20020628 A 2170 21D10 COALESCER BAG DOUG DC9 DC941 302207N WP A/C BAY DIRTY A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 23 979AX 47492 AIR CONDITIONING SMELLED DURING HIGH POWER SETTINGS. REPLACED BOTH COALESCER BAGS IAW DC9 MM 21-20-02-2. 2 L 7 2 4F A6WE 2002071500163 20020715 00163 WP 2002 7 15 ABXA020010 1 20020513 A 5320 WEB DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 E/E BAY STA 218, RBL 30- LBL 30, SUBFLOOR HAD MINOR CORROSION. REPAIRED AREA AT STATION 218 RBL 30, LBL 30 SUBFLOOR IAW DC9 SRM. 2 L 7 2 4F A6WE 2002071500165 20020715 00165 WP 2002 7 15 ABXA020013 1 20020514 A 5310 591015839 DOOR FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 CORROSION ON AFT LOWER CARGO DOOR JAMB AT WEB STATION 897-937. BLENDED CORROSION AND REPLACED A SECTION OF JAMB WEB IAW DC9 SRM. 2 L 7 2 4F A6WE 2002071500166 20020715 00166 WP 2002 7 15 ABXA020020 1 20020515 A 5320 3920324501 CAP DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 FS 604, LONGERON 29 LEFT END CAP WAS CRACKED. REPLACED END CAP AT FS 604 IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002071500171 20020715 00171 NM 2002 7 15 DHL2002705008 1 20020713 A 2611 100064901 SMOKE DETECTOR BOEING 727 72722C 138400F NM A DHLA K O NONE OTHER N L FALSE WARNING NO TEST IN INSP/MAINT 1 SO 01 705DH 19191 1) LOWER CARGO FIRE DETECTOR SHOWS A FALSE ALARM & A4291 CODE WHEN MX TEST. 2) R&R SMOKE DETECTOR ON AFT CARGO PIT, OP S CK GOOD IAW SMM 26-16-01. 2 L 7 3 4F A3WE 2002071500176 20020715 00176 SO 2002 7 15 C2XA02CL149 1 20020714 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11535 145518 DURING ROUTINE MAINTENANCE THE LEFT AND RIGHT UPPER EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE.MAINTENANCE REPLACED T HE #4 BATTERY POWER SUPPLY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002071500177 20020715 00177 EA 2002 7 15 A6WA200240020 1 20020616 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA OXYGEN DOOR OPEN A A6WA O OTHER N FALSE WARNING CR CRUISE 1 GL 31 413AW 7585 O2 DOOR OPENED IN FLIGHT. PRODUCED STALL WARNING CAS MESSAGE. MAINTENANCE FOUND O2 DOOR OPEN, DISRUPTED AIR FLOW OVER AOA VAIN CAUSING FAIL MESSAGE. INSPECTED DOOR NO DAMAGE NOTED. TESTED STALL WARNING SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002071500178 20020715 00178 EA 2002 7 15 A6WA200240021 1 20020613 A 5270 SWITCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 407AW 7424 PASSENGER DOOR OUTER HANDLE WARNING CAME ON DURING CLIMB THROUGH 17K FEET. CLEANED SWITCH, CYCLED DOOR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002071500179 20020715 00179 NM 2002 7 15 AALA20020773 1 20020523 A 2150 1942723 HEAT EXCHANGER BOEING 767 767223 1385123 NM A/C BAY MALFUNCTIONED A AALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 335AA 22333 (HEAT EXCHANGER) AFTER TAKEOFF, EN ROUTE, APPROXIMATELY 45 MINUTES FLIGHT RIGHT AIR CONDITIONING PACK STARTED TO CLIMB A T 500 FPM AND RIGHT PACK INOPERATIVE/R PAC TRIPPED. WOULD NOT HOLD ALTITUDE. DESCENDED TO 10000. RETURNED AND LANDED BOS OVERWEIGHT (280.5 GWT) WITHOUT INCIDENT. REPLACED RIGHT AND SECONDARY HEAT EXCHANGER, ALSO RIGHT HAND AIR CLYCLE MA CHNE. ACCOMPLISHED PACK BURN AND ACCOMPLISHED OVERWEIGHT INSPECTION. REMOVED MEL AND CLEARED MIC5426, DC2115B. SYSTEM GROUND CHECKED NORMAL OPERATION. AIR CYCLE MACHINE 2 L 7 2 4F RT A1NM 2002071500180 20020715 00180 GL 2002 7 15 ALG2002F00049 2 20020324 A 7250 23035128 TURBINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 ENGINE DAMAGED A ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 741SW 760070 TURBINE WAS REMOVED FROM AIRCRAFT DUE TO CRACKED EXHAUST COLLECTOR. REMOVED COMBUSTION SECTION AND FOUND HEAVY SULPHADA TION AND CRACKS ON NR 1 WHEEL BLADES. CHECK NR 1 WHEEL FOR PROPER COATING ON BLADES. 1 G 7 2 3U 3 U H1NE E1GL 2002071500181 20020715 00181 CE 2002 7 15 BSY2002F00009 1 20020509 A 7603 5038901229 THROTTLE CABLE BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO RT ENGINE FAILED E BSYA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 GL 07 4098S TH600 298744R RIGHT THROTTLE CABLE BROKE ON FINAL APPROACH. SHUT ENGINE DOWN, FEATHERED PROP, LANDED. NO PROBLEM. REMOVED AND REPLA CED RIGHT THROTTLE CABLE OPS. GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2002071500182 20020715 00182 CE 2002 7 15 BSY2002F00010 1 20020607 A 5210 354104565 LATCH BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO CABIN DOOR FAILED E BSYA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 297AT TH1349 299478R ON TAKEOFF, CABIN DOOR POPPED OPEN ON TOP SIDE, RETURNED TO AIRPORT. REPLACED UPPER TOP DOOR HOOK AND CHANNEL ASSEMBLY REPLACED WORN DOOR HANDLE. 1 L 7 2 3O 3 O 3A16 E5CE 2002071500183 20020715 00183 CE 2002 7 15 BSY2002F00011 1 20020607 A 5210 3550501P HANDLE BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO CABIN DOOR WORN E BSYA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 297AT TH1349 298866 ON TAKEOFF, OUT OF CABIN DOOR POPPED OPEN ON TOP SIDE, RETURNED TO AIRPORT REPLACED UPPER TOP DOOR HOOK AND CHANNEL ASSE MBLY. REPLACED WORN DOOR HANDLE. 1 L 7 2 3O 3 O 3A16 E5CE 2002071500184 20020715 00184 CE 2002 7 15 BSY2002F00012 1 20020607 A 5210 002430000109 CHANNEL BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO CABIN DOOR WORN E BSYA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 297AT TH1349 ON TAKEOFF, CABIN DOOR POPPED OPEN ON TOP SIDE, RETURNED TO AIRPORT. REPLACED UPPER TOP DOOR HOOK AND CHANNEL ASSEMBLY. REPLACED WORN DOOR HANDLE. 1 L 7 2 3O 3 O 3A16 E5CE 2002071500185 20020715 00185 CE 2002 7 15 BSY2002F00013 1 20020607 A 5230 SPRING CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE CARGO DOOR OUT OF ADJUST E BSYA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 242CS 208B0239 PCE19112 TOP CARGO DOOR CAME OPEN ON TAKEOFF, RETURNED TO AIRPORT. ADJUSTED SPRING TENSION ON UPPER DOOR HANDLE. OPS CHECK GOOD . 1 H 7 1 3T 3 T A37CE E4EA 2002071500186 20020715 00186 EA 2002 7 15 BTH2002F00002 2 20020701 A 7414 BL68256013 GEAR PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA MAGNETO DAMAGED E BTHA K NONE O OTHER IN INSP/MAINT 1 AL 01 4811T 327240086 DURING 500 HOUR INSPECTION MECHANIC FOUND MISSING TOOTH ON LEFT HAND DRIVE GEAR. THIS IS 2ND MAG INSTALLED ON AIRCRAFT DUE TO DRIVE GEAR FAILURE UNKNOWN. 1 L 7 1 3O 3 O A3SO 1E4 2002071500187 20020715 00187 SO 2002 7 15 BTV2002F00001 1 20020521 A 7603 1159P20059 THROTTLE CABLE GULSTM G1159 G1159 3953505 SO ENGINE CONTROL WORN B BTVR K NONE O OTHER IN INSP/MAINT 1 GL 23 5DL 7428 226 THREE EACH THROTTLE CABLES FRAYING WHERE THEY PASS OVER PULLEYS AT FS512. INSPECTED, FOUND NO EVIDENCE OF CHAFING ON ST RUCTURE AND CABLE TENSIONS WERE ADJUSTED PROPERLY. 2 L 7 2 4F RT A12EA 2002071500188 20020715 00188 CE 2002 7 15 CNQ2002F00001 1 20020604 A 2620 675860013 TUBE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL EXTINGUISH SYS CORRODED B CNQR K NONE O OTHER IN INSP/MAINT 1 CE 07 96RX 1761 7500044 WHEN THE AUXILIARY POWER UNIT FIRE EXTINGUISHER DEPLOYMENT TUBE WAS REMOVED FOR MAINTENANCE, TECHNICIANS FOUND APPROXIMA TELY THREE INCHES OF WATER IN THE VERTICALLY MOUNTED TUBE. MINOR CORROSION WAS REMOVED BEFORE REINSTALLING THE TUBE. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2002071500189 20020715 00189 CE 2002 7 15 CNQ2002F00002 1 20020614 A 2120 DUCT CESSNA 500 550 2076604 CE TAIL CONE CHAFED B CNQ6 O OTHER O OTHER NR NOT REPORTED 1 EA 25 316CS 308 5501010 FRESH AIR DUCT IN TAILCONE FOUND CHAFFING AGAINST SPEED BROKE CONTROL LINES. CHAFED THROUGH CREATING SEVERE LEAK. 1 L 7 2 4F A22CE 2002071500190 20020715 00190 NM 2002 7 15 UPS02238785 1 20020618 A 3210 1618497 BEARING BOEING 727 72722C 138400F NM MLG SUPPORT BEAM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI L/H MLG AFT TRUNNION BEARING CRACKED L/H MLG AFT TRUNNION REPLACED IAW 32-11-00 PARA 4AA(2) TO (4) PARA 5 (3) A TO E. 2 L 7 3 4F A3WE 2002071500191 20020715 00191 NM 2002 7 15 UPS02238787 1 20020612 A 5310 FRAME BOEING 727 72722C 138400F NM BS218 LBL24 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI INTERGRANULAR CORROSION ON FRAME WEB BS 218 LBL24 FASTENERS REMOVED, CORRODED SECTION OF FRAME WEB CUT OUT IAW 51-40-2 FIG1. PARTS FABRICATE, FRAME REPAIRED IAW SRM 51-40-2 FIGURE 1. 2 L 7 3 4F A3WE 2002071500192 20020715 00192 CE 2002 7 15 CWUA072D 1 20020601 A 2612 66084167 COMPUTER LEAR 35 35A 5170602 CE E/E BAY INTERMITTENT E CWUA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 05 950SP 35A450 AIRCRAFT EXPERIENCED RIGHT ENGINE FIRE WARNING SHORTLY AFTER TAKEOFF. CREW FOLLOWED CHECKLIST, DECLARED AN IFE, AND LAN DED WITHOUT INCIDENT. AFTER HOURS OF TROUBLESHOOTING, MAINTENANCE DETERMINED THEY COULD TURN ON AND OFF THE RIGHT ENGIN E FIRE LIGHT BY LIGHTLY TAPPING ON WARNING LIGHT COMPUTER. PART WAS REMOVED AND SHOWED NO SIGNS OF DAMAGE AND/OR MOISTU RE. REPLACEMENT PART WAS INSTALLED ON AIRCRAFT THE SAME DAY, AND PROBLEM WAS FIXED. 2 L 7 2 4F A10CE 2002071500193 20020715 00193 CE 2002 7 15 DEM2002F00000 1 20020122 A 5751 0322709 BRACKET CESSNA 195 195A 2073110 CE JACOBS R755 R7557 35003 EA AILERON CRACKED B DEMA K NONE O OTHER IN INSP/MAINT 1 CE 03 195DH 7588 THESE MAGNESIUM BRACKETS WERE SEVERELY CORRODED AND CRACKED UNDER THE PAINT AND COULD ONLY BE SEEN AFTER BEAD BLASTING. THESE BRACKETS ARE THE ATTACH FOR THE AILERONS AND ARE CRACKING COMPLETELY ACROSS THE RETAINING BOSS FOR THE BEARING. 1 H 7 1 3R 3 R A790 5E11 2002071500194 20020715 00194 CE 2002 7 15 DEM2002F00001 1 20020122 A 5751 03227091 BRACKET CESSNA 195 195A 2073110 CE JACOBS R755 R7557 35003 EA AILERON CRACKED D DEMA K NONE O OTHER IN INSP/MAINT 1 CE 03 195DH 7588 THESE MAGNESIUM BRACKETS WERE SEVERELY CORRODED AND CRACKED UNDER THE PAINT AND COULD ONLY BE SEEN AFTER BEAD BLASTING. THESE BRACKETS ARE THE ATTACH FOR THE AILERONS AND ARE CRACKING COMPLETELY ACROSS THE RETAINING BOSS FOR THE BEARING. 1 H 7 1 3R 3 R A790 5E11 2002071500195 20020715 00195 CE 2002 7 15 DEM2002F00002 1 20020220 A 5751 03227091 BRACKET CESSNA 195 195B 2073112 CE JACOBS R755 R7557 35003 EA AILERON CRACKED D DEMA K NONE O OTHER IN INSP/MAINT 1 CE 03 195JA 3800 7504 THESE BRACKETS ARE MADE OF MAGNESIUM AND ARE CORRODING SEVERELY AND CRACKING AT THE MOUNTING FEET AND THE MAIN BEARING B OSS. 1 H 7 1 3R 3 R A790 5E11 2002071500196 20020715 00196 CE 2002 7 15 DEM2002F00007 1 20020601 A 5521 033422013 SPAR CESSNA 195 195A 2073110 CE JACOBS R755 L4* 35003 EA ELEVATOR CRACKED D DEMA K NONE O OTHER IN INSP/MAINT 1 CE 03 1010D 7618 BOTH ELEVATOR SPARS CRACKED VERTICALLY INITIATING IN BEND RADIUS OF FLANGE TO MOUNT TIP RIB. 1 H 7 1 3R 3 R A790 TC121 2002071500197 20020715 00197 CE 2002 7 15 DEM2002F00008 1 20020601 A 5751 0322709 HINGE BRACKET CESSNA 190 190 2072902 CE AILERON CRACKED D DEMA K NONE O OTHER IN INSP/MAINT 1 CE 03 4339V 7245 FOUND BOTH INBOARD AILERON HINGE BRACKETS CRACKED COMPLETELY THROUGH THE BEARING BOSS. 1 H 7 1 3R NC A790 2002071500198 20020715 00198 CE 2002 7 15 DEM2002F00009 1 20020601 A 5751 03227091 HINGE BRACKET CESSNA 190 190 2072902 CE CONT R670 W670* 17016 SO AILERON CRACKED D DEMA K NONE O OTHER IN INSP/MAINT 1 CE 03 4339V 7245 FOUND BOTH INBOARD AILERON HINGE BRACKETS CRACKED COMPLETELY THROUGH THE BEARING BOSS. 1 H 7 1 3R 3 R NC A790 E162 2002071500199 20020715 00199 EA 2002 7 15 EEJ2002F00003 2 20020502 A 8520 LW12596 BOLT PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA ENGINE FAILED E EEJA O OTHER O OTHER NR NOT REPORTED 1 NM 07 78GH 716 317852121 247368A ENGINE SUFFERED WHAT APPEARS AS A CONNECTED ROD BOLT FAILURE OR ROD FAILURE. ROD ASSY BROKE-NR 1 CYLINDER PAD AREA DAMA GED. NOSE SECTION OF CASE BROKEN. 1 L 7 2 3O 3 O A20SO E14EA 2002071500200 20020715 00200 CE 2002 7 15 GNB2002F00002 1 20020619 A 7331 C6620200118RY INDICATOR CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO COCKPIT DEFECTIVE A GNBA K NONE O OTHER TX TAXI/GRND HDL 1 SW 01 402SA 19 402C0623 DURING TAXI, AFTER LANDING, PILOT NOTICED FUEL IN BOTTOM OF FIVE FLOW INDICATOR. 1 L 7 2 3O 3 O A7CE E8CE 2002071500201 20020715 00201 SW 2002 7 15 GXP2002F00003 1 20020611 A 3222 STRUT SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE331* 01514 WP NLG LOW E GXPA O OTHER O OTHER NR NOT REPORTED 1 GL 23 616GA TC377 NOSE GEAR DID NOT RETRACT. NOSE GEAR STRUT SERVICED. RETRACTION OF LANDING GEAR PERFORMED. OPS CHECKED GOOD. 2 L 7 2 4T 3 T RT A8SW E2WE 2002071500202 20020715 00202 EU 2002 7 15 GXP2002F00004 1 20020611 A 2910 MS287788 PACKING AMD FALCON FALCON20 2730103 EU GE CF700 CF700* 30010 NE HYD SYSTEM LEAKING E GXPA O OTHER K FLUID LOSS NR NOT REPORTED 1 GL 23 183GA 147 LOSING HYDRAULIC FLUID FROM SYSTEM 2. REMOVED AND REPLACED PACKING ON NR 2 ENGINE HYDRAULIC PUMP. SAFETIED ALL CONNECT IONS AND FILLED HYDRAULIC SYSTEM RESERVOIR NR 1 AND NR 2. STARTED NR 2 ENGINE AND LET STABILIZE. HYDRAULIC PRESSURE GO OD AND RESERVOIR NR 2 QUANTITY, GOOD. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A7EU E7EA 2002071500203 20020715 00203 CE 2002 7 15 JJB2002F00001 1 20020529 A 1430 AN17517A BOLT BEECH 1900 1900D 1154162 CE RUDDER BENT A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 837CA 3236 UE397 DURING INSPECTION OF RUDDER CONTROL SYSTEM, FOUND TORQUE TUBE MOUNT BOLTS LOOSE AND CONTROL HORN MOUNT BOLT BENT. PARTS RETURNED TO MFG FOR ANALYSIS, UNIT UNDER INVESTIGATION. 2 L 7 2 4T RT A24CE 2002071500204 20020715 00204 EU 2002 7 15 KBMA117606 1 20020608 A 2150 050008 RELAY SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE AIR CONDITIONING DEFECTIVE E KBMA O OTHER O OTHER CR CRUISE 1 WP 19 37SH 10715 2300 25 AMP AIR CONDITIONER CIRCUIT BREAKER POPS IN FLIGHT. REMOVED AND REPLACED 7 INCH BLOWER, STILL POPS. REPLACED 2 EACH RELAYS, OPS CHECK GOOD. 1 G 7 1 3U 3 U NC H9EU E19EU 2002080700216 20020807 00216 NE 2002 8 7 YENA200217 2 20020711 A 7200 7457000501 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 MALFUNCTIONED A YENA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 EA 15 520JB 4644 1446 V10934 FLT 88 ONT TO JFK, DIVERTED TO SLC DUE NR 1 ENGINE AUTO SHUTDOWN IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE PER AMM 71 -00-20 AND OPS CHECK OK PER AMM 71-00-00. 2 L 7 2 4F 4 F RT A28NM E40NE 2002071500205 20020715 00205 WP 2002 7 15 ZW0A0207201 1 20020711 A 4990 5910050ALLC0NF1 APU DOUG DC9 DC982 3022082 WP A ZW0A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 13 909TW 49170 THERE WAS A SMELL OF BURNING OIL AND HAZY SMOKE IN THE CABIN. FLIGHT RETURNED TO STL. FOUND OIL LEAKING INTO APU INLET . CLEANED UP OIL AND DEFERRED CORRECTIONS TO APU PER MEL. THE APU WAS LATER CHANGED. CHECK-C 4-27-01 MCI. --CLOSED-- 2 L 7 2 4F A6WE 2002071500206 20020715 00206 SO 2002 7 15 SIMA200216405 1 20020611 A 5300 EXTINGUISHER EMB 135 EMB135LR 3260305 SO CHAFED CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 AFT FLOOR EXTENTION IS CHAFED FROM FRAMES 22-23. C/A PERFORMED EDDY CURRENT INSPECTION. NO DEFECTS. BLENDED CHAFE IAW SRM LIMITS. 2 L 7 2 4F RT T00011AT 2002071500207 20020715 00207 SO 2002 7 15 SIMA200216409 1 20020610 A 5300 ALCLAD2024T3 BRACKET EMB 135 EMB135LR 3260305 SO APU GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 APU FIREWALL GOUGED BY APU BLEED AIR VALUE BRACKET. PERFORMED EDDY CURRENT, NO DEFECTS. REPAIR DONE ON GOUGE IAW SRM. 2 L 7 2 4F RT T00011AT 2002071500208 20020715 00208 SO 2002 7 15 SIMA200216408 1 20020611 A 5300 LONGERON EMB 135 EMB135LR 3260305 SO LWR IB LOGERON DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 LEFT UPPER COWLING LOWER INBOARD LONGERON DENTED. RECONTOURED LONGERON, PERFORMED EDDY CURRENT, NO DEFECTS. ACCEPTED A S IS IAW. TREATED FOR CORROSION. 2 L 7 2 4F RT T00011AT 2002071500209 20020715 00209 EU 2002 7 15 SIMA200217701 1 20020621 A 5300 S53174001200 BULKHEAD AEROSP ATR42 ATR42300 8680920 EU FRAME 1 CORRODED A SIMA O OTHER O OTHER IN INSP/MAINT 1 SW 21 971NA 017 DURING MBV1 INSPECTION FOUND BONDING POINTS ON FORWARD BULKHEAD TO BE CORRODED. REPAIRED IAW ATR SRM. AIRCRAFT WAS RET URNED TO SERVICE. 2 H 7 2 4T RT A53EU 2002071500210 20020715 00210 EU 2002 7 15 SIMA200216402 1 20020611 A 5700 PANEL AEROSP ATR42 ATR42300 8680920 EU WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 DURING MBV-1 INSPECTION, RIGHT AILERON OUTBOARD UPPER PANEL CORRODED AROUND SCREW HOLES. 2 H 7 2 4T RT A53EU 2002071500211 20020715 00211 EU 2002 7 15 SIMA200216401 1 20020611 A 5300 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 DURING MBV-1 INSPECTION, FRAME 25 LEFT AND RIGHT SIDES FOUND CRACKS IN LOWER OUTBOARD RADIUS OF HYDRAULIC LINE PASS THRO UGH CUTOUTS. 2 H 7 2 4T RT A53EU 2002071500212 20020715 00212 NM 2002 7 15 AWXA200200611 1 20020629 A 5313 BAC1498139 STRINGER BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON THE END OF STRINGER 23 R/H AT BS 363. MAINTENA NCE REMOVED DAMAGED SECTION OF STRINGER 23 R/H, AT BS 363 TO BS 390. FABRICATED NEW SECTION OF STRINGER AND INSTALLED RE PAIR PARTS IAW B737-300 SRM 53-00-03, FIG. 201, PG. 201-207. 2 L 7 2 4F RT A16WE 2002071500213 20020715 00213 NM 2002 7 15 AWXA200200612 1 20020629 A 5313 BAC1498139 STRINGER BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON THE END OF STRINGER 23 R/H AT BS 357. MAINTENA NCE REMOVED DAMAGED SECTION OF STRINGER 23 R/H, AT BS 326 TO BS 357. FABRICATED NEW SECTION OF STRINGER AND INSTALLED RE PAIR PARTS IAW B737-300 SRM 53-00-03, FIG. 201, PG. 201-207. 2 L 7 2 4F RT A16WE 2002071500214 20020715 00214 NM 2002 7 15 AWXA200200613 1 20020621 A 5330 65C267141 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4" CRACK WAS FOUND AT THE R/H WING LEADING EDGE KRUEGER FLAP DEFLECTION DOOR CUTOUT. MAINTENANCE CUTOUT THE DAMAGED AREA OF SKIN AT THE R/H WING LEADING EDGE KRUEGER FLAP DEFLECTION DOOR CUTOUT AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS I AW AWA ER 03-5741-02184-TB1. 2 L 7 2 4F RT A16WE 2002071600001 20020716 00001 SW 2002 7 16 HEEA080216 1 20020627 A 6230 SEAL BELL 407 407 1182206 SW SWASHPLATE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 742PH 1042 A1094 53461 SWASHPLATE UPPER GREASE SEAL WORN. 1 G 7 1 3U O H2SW 2002071600002 20020716 00002 SW 2002 7 16 HEEA080217 1 20020627 A 6220 STOP BELL 407 407 1182206 SW MAIN ROTOR HUB SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 510PH 4161 A22 53209 BLUE BLADE TIP UP STOP PAD SEPARATED. 1 G 7 1 3U O H2SW 2002071600003 20020716 00003 SW 2002 7 16 HEEA080218 1 20020627 A 6210 407015001117 BLADE BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 405PH 3786 53207 MAIN ROTOR BLADE HAS CORROSION AT THE TIP AREA. 1 G 7 1 3U O H2SW 2002071600004 20020716 00004 NM 2002 7 16 HNAA0200050 1 20020712 A 2711 7SC0284 POTENTIOMETER DHAV DHC8 DHC8102 2809003 NM R/H WING INOPERATIVE A HNAA K NONE O OTHER AP APPROACH 1 EA 07 912HA 43075 040 UNCOMMANDED LEFT WING DOWN TRIM IN FLIGHT, RECENTERED TRIM WITH AILERON TRIM SWITCH. REPLACED AILERON TRIM TAB POTENTIO METER. 2 H 7 2 4T RT A13NM 2002071600005 20020716 00005 SW 2002 7 16 HEEA080219 1 20020627 A 6210 407015001117 BLADE BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 405PH 3060 53207 MAIN ROTOR BLADE HAS CORROSION AT TIP AREA. 1 G 7 1 3U O H2SW 2002071600006 20020716 00006 SW 2002 7 16 HEEA080220 1 20020627 A 6210 407015001117 BLADE BELL 407 407 1182206 SW MAIN ROTOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 447PH 3725 53114 MAIN ROTOR BLADE HAS A CRACK ON TRAILING EDGE NEAR TRIM TAB. 1 G 7 1 3U O H2SW 2002071600007 20020716 00007 SW 2002 7 16 HEEA080221 1 20020627 A 6210 407015001117 BLADE BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 3335 53142 MAIN ROTOR BLADE TIP AREA CORRODED. 1 G 7 1 3U O H2SW 2002071600008 20020716 00008 SW 2002 7 16 HEEA080222 1 20020627 A 6220 406010413117 PITCH LINK BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 723PH 53283 PITCH LINK ASSY HAS CORROSION BEYOND LIMITS AT END OF BARREL. 1 G 7 1 3U O H2SW 2002071600009 20020716 00009 NM 2002 7 16 2002F00756 1 20020407 A 2910 HYDRAULIC LINE BOEING 747 747230B 1384889 NM HYD SYSTEM LOOSE A Q2SA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 743SA 22671 AIR TURN BACK, AFTER TAKEOFF, NR 1 HYDRAULIC SYSTEM QUANTITY DECREASING, LOW QUANTITY LIGHT ILLUMINATED. ACCOMPLISHED H YDRAULIC SYSTEM NR 1 FAILURE ABNORMAL PROCEDURE, LEAK STOPPED AT 1 GALLON INDICATED. FOUND PRESSURE LINE TO TRANSMITTER LEAKING. SECURED LINE AND SERVICED SYSTEM TO FULL. LEAK CHECKED GOOD IAW AMM 29-31-01. (M) 2 L 7 4 4F A20WE 2002071600010 20020716 00010 SW 2002 7 16 HEEA080223 1 20020627 A 6300 406010426101 LINK BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 723PH 53283 MAIN ROTOR LINK ASSY HAS CORROSION BEYOND LIMITS AROUND BOLT HOLE. 1 G 7 1 3U O H2SW 2002071600011 20020716 00011 SW 2002 7 16 HEEA080225 1 20020627 A 6230 406010427109 GIMBAL RING BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 723PH 53283 GIMBAL RING HAS CORROSION NEAR BOLT HOLE. 1 G 7 1 3U O H2SW 2002071600012 20020716 00012 SW 2002 7 16 HEEA080227 1 20020627 A 6321 406010429101 PIN BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 723PH 53283 CORROSION AROUND EDGE. 1 G 7 1 3U O H2SW 2002071600013 20020716 00013 NM 2002 7 16 2002F00757 1 20020404 A 2910 30001300017 HOUSING BOEING 747 747230B 1384889 NM HYD SYSTEM CRACKED A Q2SA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 743SA 22671 AIR TURN BACK, IMMEDIATELY AFTER GEAR RETRACTION, NR 1 HYDRAULIC SYSTEM QUANTITY WENT TO ZERO AND NR 1 HYDRAULICS SYSTEM PRESSURE ALSO WENT OT ZERO WITHING 30 SECONDS. FOUND LEFT CCA FILTER HOUSING CRACKED. REMOVED AND REPLACED LEFT CCA I AW AMM 27-11-08. (M) 2 L 7 4 4F A20WE 2002071600014 20020716 00014 WP 2002 7 16 GTIA020330 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 195-220, X15. REMOVED FLOOR SUPPORT FROM A/C. FABRICATED FLOOR S UPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002071600015 20020716 00015 WP 2002 7 16 GTIA020331 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT FS 160 X5 TO -X5. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUP PORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002071600016 20020716 00016 WP 2002 7 16 GTIA020332 1 20020321 A 5320 SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA, BEARING SUPPORT FOR FORWARD AIRSTAIR HANDLE MECH, FS 160-164 X10 TO X13. REMOVED BEARIN G AND SUPPORT. INSTALLED BEARING AND BRACKET ASSEMBLY. (M) 2 L 7 2 4F A6WE 2002071600017 20020716 00017 WP 2002 7 16 GTIA020333 1 20020321 A 5240 ANGLE DOUG DC9 DC981 3022081 WP SERVICE DOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD GALLEY SERVICE DOOR, ANGLE ATTACHED TO DOOR BELOW INTERIOR DOOR HANDLE HAS LIGHT CORROSION. FABRICA TED NEW ANGLE. INSTALLED NEW ANGLE. (M) 2 L 7 2 4F A6WE 2002071600018 20020716 00018 SW 2002 7 16 HEEA080228 1 20020627 A 6520 406040072105 SPLINE ADAPTER BELL 407 407 1182206 SW TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 53159 TAIL ROTOR SPLINE ADAPTER HAS WORN SPLINES. 1 G 7 1 3U O H2SW 2002071600019 20020716 00019 WP 2002 7 16 GTIA020334 1 20020320 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FORWARD ENTRY AREA, FLOORBOARD FROM STATION 200-260 X23 TO X44 HAS MISSING INSERTS, BROKEN INSERTS, PUNCTURES AND CORNERS CRACKED. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002071600020 20020716 00020 SW 2002 7 16 HEEA080229 1 20020627 A 6520 406040072105 SPLINE ADAPTER BELL 407 407 1182206 SW TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 53400 TAIL ROTOR SPLINE ADAPTER HAS WORN SPLINES. 1 G 7 1 3U O H2SW 2002071600021 20020716 00021 WP 2002 7 16 GTIA020335 1 20020320 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA, FLOORBOARD FROM STATION 160-200 X11 TO X46 HAS MISSING INSERTS, BROKEN INSERTS, EDGES DE LAMINATED. FORM NEW PANEL. (M) 2 L 7 2 4F A6WE 2002071600022 20020716 00022 WP 2002 7 16 GTIA020336 1 20020320 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FORWARD ENTRY AREA, FLOORBOARD FROM STATION 160-200 X6-X6 HAS INSERTS MISSING, BROKEN AND DELAMINATION. FORM NEW PANEL. (M) 2 L 7 2 4F A6WE 2002071600023 20020716 00023 WP 2002 7 16 GTIA020337 1 20020320 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA, FLOORBOARD FROM STATION 180-200 -X7 TO -X43 HAS INSERTS MISSING AND DELAMINATION. FORM NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2002071600024 20020716 00024 SW 2002 7 16 HEEA080233 1 20020627 A 6310 406040500123B FREEWHEEL UNIT BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 405PH 3016 53207 FREEWHEEL UNIT HAS CORROSION BEYOND LIMITS. 1 G 7 1 3U O H2SW 2002071600025 20020716 00025 WP 2002 7 16 GTIA020338 1 20020321 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT FS 180, -X9.5 TO -43. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPP ORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002071600026 20020716 00026 SW 2002 7 16 HEEA080234 1 20020627 A 6710 406310405101 UNIVERSAL BELL 407 407 1182206 SW M/R DRIVE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4999 53323 UNIVERSAL HAS A BEARING WORN. 1 G 7 1 3U O H2SW 2002071600027 20020716 00027 SW 2002 7 16 HEEA080235 1 20020627 A 6710 406310405101 UNIVERSAL BELL 407 407 1182206 SW M/R DRIVE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 741PH 53457 UNIVERSAL HAS A BEARING WORN. 1 G 7 1 3U O H2SW 2002071600028 20020716 00028 WP 2002 7 16 GTIA020339 1 20020320 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA, FLOORBOARD FROM STATION 200-260 -X22 TO -X43 HAS INSERTS MISSING, CORNER CRACKED AND EDG ES DAMAGED. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002071600029 20020716 00029 SW 2002 7 16 HEEA080236 1 20020627 A 6220 407001524105 BELLCRANK BELL 407 407 1182206 SW M/R HEAD DEBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 501PH 53401 BELLCRANK HAS BUSHINGS DISBONDED. 1 G 7 1 3U O H2SW 2002071600030 20020716 00030 WP 2002 7 16 GTIA020340 1 20020320 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA FLOORBOARD FROM STATION 160-200 X48-X55 HAS INSERTS MISSING, BROKEN AND EDGES DAMAGED. F ABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002071600031 20020716 00031 WP 2002 7 16 GTIA020341 1 20020318 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND AFT PIT/CABIN FLOOR STATION 1287-1309 XO, UPPER FLANGE IN INTERCOSTAL IS CRACKED AT FASTENER HOLES. FABRICA TED, LOCATED AND DRILLED INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002071600032 20020716 00032 WP 2002 7 16 GTIA020342 1 20020318 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - AFT PIT/CABIN FLOOR, STATION 1155-1174 PLUS X45 LEFT INBOARD SEAT TRACK AND SPLICE ARE CORRODED. REMOVED SEAT TRA CK STATION 1079-1155 AND SPLICE AT STATION 1155. FABRICATED REPAIR SEAT TRACK SPLICE. INSTALLED REPAIR SEAT TRACK AT S TATION 1079-1155. (M) 2 L 7 2 4F A6WE 2002071600033 20020716 00033 WP 2002 7 16 GTIA020343 1 20020316 A 5720 BRACKET DOUG DC9 DC981 3022081 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND RIGHT WING, UPPER DOG LEG, BRACKET ATTACH TO BODY CRACKED. REMOVED DAMAGED BRACKET RIGHT WING UPPER SURFACE . FABRICATED NEW BRACKET. INSTALLED NEW BRACKET. (M) 2 L 7 2 4F A6WE 2002071600034 20020716 00034 WP 2002 7 16 GTIA020344 1 20020316 A 5712 RIB DOUG DC9 DC981 3022081 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND RIGHT LOWER CENTER WING CRACKED AT THE NR 1 RIB, FROM DOOR JAMB. REMOVED NR 1 RIB CRACKED. FORMED INNER DO UBLER. LOCATED AND DRILLED. INSTALLED REPAIR PARTS. INSTALLED NR 1 RIB RIGHT LOWER CENTER WING. (M) 2 L 7 2 4F A6WE 2002071600035 20020716 00035 WP 2002 7 16 GTIA020345 1 20020321 A 5320 CHANNEL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA, CHANNEL CORRODED AT FS 160, X13. FABRICATED CHANNEL AND SPLICE. INSTALLED REPAIR. (M) 2 L 7 2 4F A6WE 2002071600036 20020716 00036 WP 2002 7 16 GTIA020346 1 20020321 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA SEAT TRACK CORRODED AT FS 200-255, -X22. REPLACEMENT OF SEAT TRACK FROM STATION 200-226. REMOVED CORRODED SEAT TRACK. LOCATED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK AND SPLICE. (M) 2 L 7 2 4F A6WE 2002071600037 20020716 00037 WP 2002 7 16 GTIA020347 1 20020324 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD FLIGHT COMPARTMENT FLOOR PANEL STATION 120.050 TO STATION 160 HAS MUSHY SOFT, RIGHT SIDE. FABRICATE D NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2002071600038 20020716 00038 WP 2002 7 16 GTIA020348 1 20020324 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - PASSENGER COMPARTMENT FLOOR PANEL (CENTER) STATION 1271 TO STATION 1309, HAS MUSHEY SOFT. FABRICATED NEW FLOORBOA RD CENTER STATION 1271-1309. (M) 2 L 7 2 4F A6WE 2002071600039 20020716 00039 WP 2002 7 16 GTIA020349 1 20020324 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND INTERNAL ACCESS PANEL CENTER COCKPIT (FLT COMPT) STATION 120 HAS MUSHY SOFT DAMAGE. FABRICATED NEW FLOORBOA RD. (M) 2 L 7 2 4F A6WE 2002071600040 20020716 00040 WP 2002 7 16 GTIA020350 1 20020322 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR PANEL STATION 946-1003 CENTER MUSHY SOFT AND HAS BLUE WATER STAINS. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2002071600041 20020716 00041 WP 2002 7 16 GTIA020351 1 20020318 A 7120 ISOLATOR DOUG DC9 DC981 3022081 WP RT ENGINE MISALIGNED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - RIGHT ENGINE FORWARD LOWER ISOLATOR ALIGNMENT MARK WAS MISALIGNED. REMOVED RIGHT ENGINE FORWARD LOWER ISOLATOR. INSTALLED NEW ISOLATOR. (M) 2 L 7 2 4F A6WE 2002071600042 20020716 00042 SW 2002 7 16 HEEA080237 1 20020627 A 6220 407010114101 CONE SEAT BELL 407 407 1182206 SW M/R HEAD CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 723PH 53283 CENTER CONE SEAT CHAFED AROUND EDGE. 1 G 7 1 3U O H2SW 2002071600043 20020716 00043 SW 2002 7 16 HEEA080238 1 20020627 A 6220 407010150101 FRAHM BELL 407 407 1182206 SW MAIN ROTOR HEAD BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 722PH 53288 BROKEN FRAHM ASSY SPRING. 1 G 7 1 3U O H2SW 2002071600044 20020716 00044 SW 2002 7 16 HEEA080239 1 20020627 A 6220 407010150101 FRAHM BELL 407 407 1182206 SW M/R HEAD BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 723PH 53283 BROKEN FRAHM ASSY SPRING. 1 G 7 1 3U O H2SW 2002071600045 20020716 00045 SW 2002 7 16 HEEA080240 1 20020627 A 6220 407010150109A FRAHM BELL 407 407 1182206 SW M/R HEAD BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 501PH 53401 BROKEN FRAHM ASSY SPRING. 1 G 7 1 3U O H2SW 2002071600046 20020716 00046 SW 2002 7 16 HEEA080241 1 20020627 A 6220 407010150109 FRAHM BELL 407 407 1182206 SW M/R HEAD BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 53400 BROKEN FRAHM ASSY SPRING. 1 G 7 1 3U O H2SW 2002071600047 20020716 00047 WP 2002 7 16 GTIA020352 1 20020423 A 2730 CONTROL SWITCH DOUG DC9 DC982 3022082 WP ELEVATOR MALFUNCTIONED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 812NK 48021 FLT 262 - ACY - ELEVATOR POWER ON LIGHT STAYED ON AFTER CONTROL CHECK. REMOVED AND REPLACED ELEVATOR POWER CONTROL PSI SWITCH. (M) 2 L 7 2 4F A6WE 2002071600048 20020716 00048 SW 2002 7 16 HEEA080242 1 20020627 A 6210 407015001109 BLADE BELL 407 407 1182206 SW MAIN ROTOR DELAMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 457PH 2563 53147 DELAMINATION ON BOTTOM OF BLADE NEAR TRIM TAB. 1 G 7 1 3U O H2SW 2002071600049 20020716 00049 WP 2002 7 16 GTIA020353 1 20020428 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 816NK 49140 FLL - FOUND OVERHEAD EMERGENCY LIGHTS IN AFT GALLEY INOPERATIVE. SECURED LOOSE CONNECTION AND REPLACED BATTERIES IN POW ER SUPPLY FOR AFT GALLEY OVERHEAD EMERGENCY LIGHTS. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2002071600050 20020716 00050 WP 2002 7 16 GTIA020354 1 20020415 A 5320 BRACKET DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND BRACKET CORRODED AT STATION Y826, ABOVE LONGERON 29L. FOUND AFTER REMOVAL OF LONGERON. MATERIAL LOSS OUT O F LIMITS. FORMED NEW BRACKET. (M) 2 L 7 2 4F A6WE 2002071600051 20020716 00051 WP 2002 7 16 GTIA020355 1 20020415 A 5320 BRACKET DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND BRACKET CORRODED AT STATION Y 826, ABOVE LONGERON 29R, FOUND AFTER REMOVAL OF LONGERON. BRACKET OUT OF LIMI TS. FORMED BRACKET. (M) 2 L 7 2 4F A6WE 2002071600052 20020716 00052 WP 2002 7 16 GTIA020356 1 20020412 A 5320 SUPPORT BRACKET DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND R1 DOOR THRESHOLD FLOOR SUPPORT AND TWO GIRT BAR LATCH SUPPORT BRACKETS CORRODED. GIRT BARS FOUND OUT OF LI MITS. LOCATE AND DRILLED GIRT BARS FITTING. (M) 2 L 7 2 4F A6WE 2002071600053 20020716 00053 WP 2002 7 16 GTIA020357 1 20020409 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR SUPPORT CRACKED AT FS 148, -X45, -X45 TO -X54. REMOVED FLOOR SUPPORT. FORMED NEW SUPPORT, INSTALLED. (M) 2 L 7 2 4F A6WE 2002071600054 20020716 00054 WP 2002 7 16 GTIA020358 1 20020330 A 5320 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND SEAT TRACK CLOSEOUT DOUBLER HAS CORROSION AND IS CRACKED STATION 200 PLUS X43. REMOVED SEAT TRACK DOUBLER. FORM NEW DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2002071600055 20020716 00055 SW 2002 7 16 HEEA080243 1 20020627 A 6210 407015001117 BLADE BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 723PH 2993 53283 POTTING SEPARATED AND CORROSION ON WEIGHT POCKET. 1 G 7 1 3U O H2SW 2002071600056 20020716 00056 SW 2002 7 16 HEEA080244 1 20020627 A 6210 407015001117 BLADE BELL 407 407 1182206 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 723PH 2993 53283 POTTING SEPARATED AND CORROSION ON WEIGHT POCKET. 1 G 7 1 3U O H2SW 2002071600057 20020716 00057 WP 2002 7 16 GTIA020359 1 20020330 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND COCKPIT FLOOR SUPPORT STATION 150 PLUS X5 TO -X5 CORROSION. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SU PPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002071600058 20020716 00058 SW 2002 7 16 HEEA080245 1 20020627 A 6210 407015001117 BLADE BELL 407 407 1182206 SW MAIN ROTOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 3439 53159 CRACK IN BLADE ROOT CAP IN TWO DIFFERENT PLACES; ONE BY LEADING EDGE MOUNT BOLT AND ONE IN TRAILING EDGE BY WEIGHT AND T AB NUMBERS. 1 G 7 1 3U O H2SW 2002071600059 20020716 00059 SW 2002 7 16 HEEA080252 1 20020627 A 3241 407050201101 CROSSTUBE BELL 407 407 1182206 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 CROSSTUBE CORRODED BEYOND LIMITS.. 1 G 7 1 3U O H2SW 2002071600060 20020716 00060 SW 2002 7 16 HEEA080253 1 20020627 A 3246 407050201103 CROSSTUBE BELL 407 407 1182206 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 53159 CROSSTUBE CORRODED BEYOND LIMITS. 1 G 7 1 3U O H2SW 2002071600061 20020716 00061 SW 2002 7 16 HEEA080255 1 20020627 A 7120 407060111101 MOUNT BELL 407 407 1182206 SW ENGINE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 405PH 53207 ENGINE BIPOD MOUNT WORN. 1 G 7 1 3U O H2SW 2002071600062 20020716 00062 WP 2002 7 16 GTIA020360 1 20020330 A 2700 CONTROL QUADRANT DOUG DC9 DC981 3022081 WP FLIGHT CONTROL CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND RUDDER AND ELEVATOR CABLE QUADRANT AFT OF PRESSURE BULKHEAD STATION 1338 -X30 CABLE KEEPER AND QUADRANT CORR ODED AND BLUEWATER STAINED. REPLACED CABLE KEEPER PINS ON RUDDER AND ELEVATOR CABLE QUADRANT. (M) 2 L 7 2 4F A6WE 2002071600063 20020716 00063 WP 2002 7 16 GTIA020361 1 20020329 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND CABIN AT STATION 1197, LEFT SIDE, SUB FLOOR/WEB UNDER GALLEY DRAIN FLANGE IS CRACKED. CUT OUT DAMAGED AREA. FABRICATED DOUBLER AND FILLER. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2002071600064 20020716 00064 SW 2002 7 16 HEEA080256 1 20020627 A 7120 407060111101 BIPOD MOUNT BELL 407 407 1182206 SW ENGINE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 492PH 53390 ENGINE BIPOD MOUNT WORN. 1 G 7 1 3U O H2SW 2002071600065 20020716 00065 WP 2002 7 16 GTIA020362 1 20020328 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND CABIN SEAT TRACK LEFT OUTBOARD TRACK FLANGE FROM STATION 1155 TO 1231 IS CORRODED. REMOVED DAMAGE ON SEAT T RACK. INSTALLED SEAT TRACK AND SPLICE FORWARD AND AFT. (M) 2 L 7 2 4F A6WE 2002071600066 20020716 00066 SW 2002 7 16 HEEA080257 1 20020627 A 7120 407060112101 BIPOD MOUNT BELL 407 407 1182206 SW ENGINE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 501PH 53401 ENGINE BIPOD MOUNT WORN. 1 G 7 1 3U O H2SW 2002071600067 20020716 00067 SW 2002 7 16 HEEA080258 1 20020627 A 7810 407063001101 EXHAUST STACK BELL 407 407 1182206 SW ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406PH 53198 EXHAUST STACK CRACKED ON AFT SEAM. 1 G 7 1 3U O H2SW 2002071600068 20020716 00068 SW 2002 7 16 HEEA080259 1 20020627 A 7810 407063001101 EXHAUST STACK BELL 407 407 1182206 SW ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 742PH 53461 EXHAUST STACK CRACKED AT TWO PLACES IN WELD OF FLANGE TO DUCT, LEFT FRONT AND REAR CORNERS. 1 G 7 1 3U O H2SW 2002071600069 20020716 00069 WP 2002 7 16 GTIA020363 1 20020329 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND CABIN FLOOR SUPPORT AT STATION 1155 PLUS X24 TO PLUS X48 IS CORRODED. REMOVED CABIN FLOOR SUPPORT. FORMED LOCATED AND DRILLED FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002071600070 20020716 00070 SW 2002 7 16 HEEA080260 1 20020627 A 5320 407070620111 TRIM PANEL BELL 407 407 1182206 SW CABIN CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 TRIM PANEL CRACKED. 1 G 7 1 3U O H2SW 2002071600071 20020716 00071 WP 2002 7 16 GTIA020364 1 20020328 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND SUB FLOOR STATION 200-218 APPROX PLUS X23 TO -X48 HAS CORROSION AND BLOWN OUT FASTENER HOLES. REMOVED DAMAG ED WEB. FABRICATED NEW SECTION OF SUB FLOOR. INSTALLED WEB. (M) 2 L 7 2 4F A6WE 2002071600072 20020716 00072 SW 2002 7 16 HEEA080261 1 20020627 A 5210 407070620137 PANEL BELL 407 407 1182206 SW CREW DOOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 495PH 53397 COPILOT DOOR TRIM PANEL CRACKED. 1 G 7 1 3U O H2SW 2002071600073 20020716 00073 SW 2002 7 16 HEEA080262 1 20020627 A 5210 407070620138 PANEL BELL 407 407 1182206 SW CREW DOOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 495PH 53397 PILOT DOOR TRIM PANEL CRACKED. 1 G 7 1 3U O H2SW 2002071600074 20020716 00074 SW 2002 7 16 HEEA080263 1 20020627 A 5210 407070620157 TRIM PANEL BELL 407 407 1182206 SW PAX DOOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 498PH 53399 LT AFT PASSENGER DOOR WINDOW TRIM CRACKED. 1 G 7 1 3U O H2SW 2002071600075 20020716 00075 SW 2002 7 16 HEEA080264 1 20020627 A 5210 407070620158 PANEL BELL 407 407 1182206 SW PAX DOOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 493PH 53393 DOOR PANEL CRACKED. 1 G 7 1 3U O H2SW 2002071600076 20020716 00076 SW 2002 7 16 HEEA080265 1 20020627 A 6321 407070631101 BRAKE BELL 407 407 1182206 SW MAIN ROTOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 53188 ROTOR BRAKE TRIM IS CRACKED. 1 G 7 1 3U O H2SW 2002071600077 20020716 00077 SW 2002 7 16 HEEA080266 1 20020627 A 3212 206373901103 SOLENOID VALVE BELL 407 407 1182206 SW FLOAT BOTTLE LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 197 53188 EMERGENCY FLOAT BOTTLE SOLENOID VALVE LEAKING. 1 G 7 1 3U O H2SW 2002071600078 20020716 00078 SW 2002 7 16 HEEA080267 1 20020627 A 3212 206373901103 SOLENOID VALVE BELL 407 407 1182206 SW FLOAT BOTTLE LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 723PH 236 53283 EMERGENCY FLOAT BOTTLE SOLENOID VALVE IS LEAKING. 1 G 7 1 3U O H2SW 2002071600079 20020716 00079 WP 2002 7 16 GTIA020365 1 20020327 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND COCKPIT AREA FLOOR PANEL WEB CORRODED SEVERAL PLACES BETWEEN STA Y 133 AND Y 160, X30 TO -X22, CORROSION AS FOUND AFTER CORRODED FLOOR SUPPORT REMOVAL. REMOVED COCKPIT WEB LBL 45 TO RBL 20 FS 160-140. FABRICATED NEW WEB. FORM ED NEW WEB SPLICE. COPILOTS INBOARD SEAT TRACK OUT OF LIMITS. FLOOR SUPPORT AT STATION 160 X 20 HAS CORROSION. FORMED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT AT STATION 160 X20. INSTALLED WEB AND WEB SPLICE. (M) 2 L 7 2 4F A6WE 2002071600080 20020716 00080 SW 2002 7 16 HEEA080268 1 20020627 A 3212 206373901103 SOLENOID VALVE BELL 407 407 1182206 SW FLOAT BOTTLE LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 344 EMERGENCY FLOAT BOTTLE SOLENOID VALVE LEAKING. 1 G 7 1 3U O H2SW 2002071600081 20020716 00081 SW 2002 7 16 HEEA080269 1 20020627 A 3212 407304125 GUARD BELL 407 407 1182206 SW EMERGENCY FLOAT CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 EMERGENCY FLOAT GUARD CRACKED. 1 G 7 1 3U O H2SW 2002071600082 20020716 00082 SW 2002 7 16 HEEA080270 1 20020627 A 3212 407304225 GUARD BELL 407 407 1182206 SW EMERGENCY FLOAT CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 EMERGENCY FLOAT GUARD CRACKED. 1 G 7 1 3U O H2SW 2002071600083 20020716 00083 WP 2002 7 16 GTIA020366 1 20020327 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FORWARD ENTRY AREA FLOOR PAN (WEB) CORRODED SEVERAL PLACES BETWEEN STATION Y 160 AND Y 200, X43 TO -X53, CORROSION WAS FOUND AFTER FLOOR SUPPORTS REMOVAL. REMOVED FLOOR PAN (WEB) FROM STATION 160-200, LBL 43 TO RBL 41. FABRICATED NE W SECTION FLOOR PAN (WEB). FLOOR SUPPORT STATION 195 LBL 16 TO 43 OUT OF LIMITS. FABRICATED NEW FLOOR SUPPORT AT STATI ON 195 TO LBL 16 TO 43. FORMED NEW WEB SPLICE. INSTALLED WEB SPLICES. INSTALLED FLOOR SUPPORT AT STATION 195 LBL 16 T O LBL 43. (M) 2 L 7 2 4F A6WE 2002071600084 20020716 00084 WP 2002 7 16 GTIA020367 1 20020327 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FLOOR SUPPORT CORRODED AT STATION Y 147 TO 159, X13 LOWER AREA OF EPC PANEL. REMOVED FLOOR SUPPORT. FORMED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002071600085 20020716 00085 SW 2002 7 16 HEEA080271 1 20020627 A 5260 407301110 STEP BELL 407 407 1182206 SW FUSELAGE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 STEP HAS SEVERAL SPOTS OF EXFOLIATION. 1 G 7 1 3U O H2SW 2002071600086 20020716 00086 WP 2002 7 16 GTIA020368 1 20020327 A 5730 ACCESS PANEL DOUG DC9 DC981 3022081 WP LT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND LEFT WING BOTTOM SIDE ACCESS PANEL INBOARD OF MLG, ANTI-SKID VALVE MOUNT PANEL IS DELAMINATED. REMOVED ACCE SS PANEL. REPAIRED LEFT WING BOTTOM SIDE PANEL OF MLG. INSTALLED ACCESS PANEL. (M) 2 L 7 2 4F A6WE 2002071600087 20020716 00087 NM 2002 7 16 WRLA200209 1 20020326 A 2497 WIRE DOUG MD11 MD11 3023602 NM ELECTRICAL SYS DAMAGED A WRLA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 273WA 48519 AFTER TAKEOFF AT 270 KNOTS STICK SHAKER FEATHERS BELOW HORIZON RIGHT SIDE NUMEROUS FURTHER STICK SHAKERS, LOW SPEED WARN ING, HIGH SPEED WARNING, ERRATIC UNRELIABLE AIRSPEED INDICATIONS. ALSO, AUTO SLAT FAIL ANNUNCIATED, RIGHT PITOT HEAT FA ILED, LEFT PITOT HEAT, NR 3 ENGINE OIL PRESSURE ALL ERRATIC AND TRANSIT FAULTS. DUMPED FUEL RETURNED FOR LANDING. REPA IRED BUS WIRE 28 VOLT AC, BUS 3 WIRE IS LOCATED BEHIND CIRCUIT BREAKER PANEL. HYDRAULIC QUANTITY INDICATOR, FUEL PRESSU RE ENGINE FCC2, DEU1, DEU2 AND DUE3 TEST ALL PASSED AND NO FAULT FOUND. REPAIRED BROKEN WIRE. (M) 2 L 7 3 4F RT A22WE 2002071600088 20020716 00088 SW 2002 7 16 HEEA080272 1 20020627 A 6420 407310203101 MOUNT BELL 407 407 1182206 SW TAIL ROTOR SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 405PH 53207 ELASTOMERIC ON MOUNT IS SEPARATED BEYOND LIMITS. 1 G 7 1 3U O H2SW 2002071600089 20020716 00089 SW 2002 7 16 HEEA080273 1 20020627 A 6420 407310203101 MOUNT BELL 407 407 1182206 SW TAIL ROTOR CONTAMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 501PH 53401 MOUNT OIL SOAKED. 1 G 7 1 3U O H2SW 2002071600090 20020716 00090 SW 2002 7 16 HEEA080275 1 20020627 A 6510 407340340103 DISC PACK BELL 407 407 1182206 SW TAIL ROTOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4999 53323 DISC PACK CRACKED. 1 G 7 1 3U O H2SW 2002071600091 20020716 00091 SW 2002 7 16 HEEA080276 1 20020627 A 6510 407340340103 DISC PACK BELL 407 407 1182206 SW TAIL ROTOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 742PH 53461 DISC PACK CRACKED. 1 G 7 1 3U O H2SW 2002071600092 20020716 00092 SW 2002 7 16 HEEA080277 1 20020627 A 3212 407350301101 FLOAT BELL 407 407 1182206 SW MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 499PH 53400 FLOAT BAG FOUND LEAKING ON 6 MONTH INSPECTION. 1 G 7 1 3U O H2SW 2002071600093 20020716 00093 SW 2002 7 16 HEEA080278 1 20020627 A 7714 407375002103 INDICATOR BELL 407 407 1182206 SW ENGINE NG MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 402PH 53159 NG INDICATOR LED DISPLAY GETTING DIMMER OVER TIME. 1 G 7 1 3U O H2SW 2002071600095 20020716 00095 2002 7 16 HEEA080279 4 20020627 A 3442 78806059008 DISPLAY BELL 407 407 1182206 SW WX RADAR INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 612PH 53199 WEATHER RADAR HAS NO DISPLAY. 1 G 7 1 3U O H2SW 2002071600096 20020716 00096 SO 2002 7 16 SIMA200215101 1 20020523 A 5330 SKIN EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 145314 DURING AN MBV INSPECTION, FOUND PREVIOUS REPAIR BETWEEN FRAMES 19 AND 20, AND STRINGER 15 AND 17L, RIVETS IMPROPERLY INS TALLED. REMOVED PREVIOUS REPAIR DOUBLER, INSTALLED IAW STANDARD SRM PRACTICES. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002071600097 20020716 00097 SO 2002 7 16 SIMA200215106 1 20020522 A 5310 WINDOW FRAME EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 DURING AN IMBV INSPECTION FOUND CORROSION IN SCREW HOLES/NUTPLATES OF WINDSHIELD CUTOUT LOWER EDGE. REAMED BEAM/BELT PI LOTS SIDE LEFT LOWER CORNER (4) HOLES UP TO .313 TO REMOVE CORROSION. INSTALLED BUSHING, REAMED HOLES IN BUSHING TO .19 0 INCHES INSTALLED NUTPLATES AND RESTORED FINISH. REPAIR DONE IAW STANDARD SRM PRACTICES. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002071600098 20020716 00098 SW 2002 7 16 HEEA080280 1 20020627 A 3212 8226003 FUSIBLE PLUG BELL 407 407 1182206 SW EMERGENCY FLOAT LEAKING E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 723PH 53283 EMERGENCY FLOAT FUSIBLE PLUG LEAKING. 1 G 7 1 3U O H2SW 2002071600099 20020716 00099 SO 2002 7 16 SIMA200215117 1 20020523 A 5330 SKIN EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 145314 DURING AN MBV INSPECTION FOUND PREVIOUS REPAIR BETWEEN FRAMES 19 AND 20, AND STRINGERS 15 AND 17L, RIVETS IMPROPERLY INS TALLED. REMOVED C PREV. REPAIR FAB A REPAIR DOUBLER, REPAIR DONE IAW STANDARD SRM PRACTICES. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002071600100 20020716 00100 SW 2002 7 16 HEEA080281 1 20020627 A 3000 96487 SOLENOID VALVE BELL 407 407 1182206 SW ANTI ICE SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 719PH 53266 SOLENOID VALVE STICKING OPEN AND INTERMITTENT OPERATION. 1 G 7 1 3U O H2SW 2002071600101 20020716 00101 SO 2002 7 16 SIMA200216404 1 20020611 A 7110 LONGERON EMB 135 EMB135LR 3260305 SO COWLING DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 RIGHT UPPER COWLING LOWER INBOARD LONGERON DENTED. C/A FABRICATED AND INSTALLED. A DOUBLER, REPAIR DONE IAW SRM. 2 L 7 2 4F RT T00011AT 2002071600102 20020716 00102 SW 2002 7 16 HEEA080284 1 20020627 A 7800 206064203101 DUCT BELL 206 206L3 1182108 SW BLEED AIR SYS CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6603X 51412 BLEED AIR DUCT IS CRACKED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002071600103 20020716 00103 SO 2002 7 16 SIMA200216406 1 20020611 A 5320 STRUCTURE EMB 135 EMB135LR 3260305 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 FORWARD FLOOR EXTENSION IS CHAFED AT FRAME 22. PERFORMED EDDY CURRENT INSPECTION NO DEFECTS. BLENDED OUT CHAFE, WITHIN MFG SRM LIMITS. 2 L 7 2 4F RT T00011AT 2002071600104 20020716 00104 SW 2002 7 16 HEEA080285 1 20020627 A 7603 206064713103 POWER LEVER BELL 206 206L3 1182108 SW COCKPIT WORN E K NONE O OTHER IN INSP/MAINT 1 SW 03 6603X 51412 POWER LEVER BOLT HOLE WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002071600105 20020716 00105 SW 2002 7 16 HEEA080286 1 20020627 A 6730 206076062003 CYLINDER BELL 206 206L3 1182108 SW MAIN ROTOR LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 49EA 51507 MAIN ROTOR CYLINDER LEAKING AND RATCHETY. REPLACED WITH SERVICEABLE CYLINDER. 1 G 7 1 3U H2SW 2002071600106 20020716 00106 GL 2002 7 16 SIMA200217301 2 20020617 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 FLAMED OUT A SIMA B EMER. DESCENT X ENGINE FLAMEOUT CR CRUISE 1 SW 21 629AE 145130 DISC - NR 2 ENGINE FLAME OUT DURING CRUISE. WOULD NOT RESTART. C/A REPLACED NR 2 ENGINE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002071600107 20020716 00107 SW 2002 7 16 HEEA080287 1 20020627 A 6320 214040805001 THERMOSWITCH BELL 206 206L3 1182108 SW GEARBOX OIL MALFUNCTIONED E HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 30KH 51527 TRANS OIL TEMP CAUTION LIGHT CAME ON WITH TEMP IN THE MIDDLE OF OPERATING RANGE. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002071600108 20020716 00108 SW 2002 7 16 HEEA080288 1 20020627 A 2432 CONNECTOR BELL 407 407 1182206 SW BATTERY BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9900455 CONNECTOR PLUG BROKEN. REPAIRED BATTERY. 1 G 7 1 3U O H2SW 2002071600109 20020716 00109 SO 2002 7 16 SIMA200217302 1 20020620 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO NR 2 FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 636AE 145160 DISC- FLIGHT CREW NOTED VISIBLE SMOKE IN CABIN DURING FLIGHT. C/A NR 2 PACK ACM IAW SRM. OPS CHECK GOOD 2 L 7 2 4T RT T00011AT 2002071600110 20020716 00110 SW 2002 7 16 HEEA080289 1 20020627 A 6210 412015300109 BLADE BELL 412 412 1182202 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 14379 36005 OUTBOARD ABRASION STRIP HAS SEVERAL HOLES. TO BE SENT TO VENDOR FOR REPAIR. 1 G 7 2 4U H4SW 2002071600111 20020716 00111 EU 2002 7 16 02FDEA00493 1 20020716 A 5700 WING AIRBUS 310 A310 EU N/A CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 INBD LT WING UNDER SURFACE TRAILING EDGE AT ZONE 575 FND CORRODED. TEMPORARY REPAIR PER E.A. 6-5710-64295. 2 L 7 2 4F RT A35EU 2002071600112 20020716 00112 SW 2002 7 16 HEEA080290 1 20020627 A 6210 412015300106 BLADE BELL 412 412 1182202 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 8330 33077 THE TWO LOWER FRETTING PADS ARE SEPARATED. TO BE SENT TO VENDOR FOR REPAIR. 1 G 7 2 4U H4SW 2002071600113 20020716 00113 EU 2002 7 16 02FDEA00492 1 20020716 A 5730 SKIN AIRBUS 310 A310 EU N/A CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 RT WING LOWER SKIN CORRODED ON LWR SURFACE ON NR 2 PANEL AT AFT EDGE AT RIB 9. STRUCTURAL REPAIR PER E.A. 6-5710-64296. 2 L 7 2 4F RT A35EU 2002071600114 20020716 00114 SO 2002 7 16 SIMA200217303 1 20020622 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN NOT SEATED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 717AE 145272 FLOOR EMERGENCY LIGHT ROW 5 INOPERATIVE. C/A SEATED FLOOR EMERGENCY STRIP IN ROW 5 OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2002071600115 20020716 00115 SW 2002 7 16 HEEA080291 1 20020627 A 7120 206064105101 LEG ASSY BELL 206 206L3 1182108 SW ENGINE MOUNT MISMARKED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 ENGINE MOUNT LEG ASSY IDENTIFIED AS LEFT HAND BUT IS ACTUALLY A RIGHT HAND. 1 G 7 1 3U H2SW 2002071600116 20020716 00116 SO 2002 7 16 SIMA200217703 1 20020622 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 DURING IMBV INSPECTION FOUND CORROSION ON GALLEY RIGHT HAND FLOORBEAM. REMOVED CORRODED GALLEY RT BEAM. INSTALLED NEW BEAM IAW STANDARD SRM PRACTICES. 2 L 7 2 4T RT T00011AT 2002071600117 20020716 00117 SO 2002 7 16 SIMA200217704 1 20020621 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 DURING AN IMBV INSPECTION FOUND CORROSION ON SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING. FABRICATED A REP AIR DOUBLER. REPAIR DONE IAW GST. 2 L 7 2 4T RT T00011AT 2002071600118 20020716 00118 SO 2002 7 16 SIMA200217705 1 20020621 A 5315 14521721009 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 DURING IMBV INSPECTION, FOUND CORROSION ON FORWARD DIGITAL REMOVED CORROSION BY CUT OUT. FABRICATED A REPLACEMENT STRAP , TWO DOUBLERS. REPAIR DONE IAW STANDARD SRM PRACTICES. 2 L 7 2 4T RT T00011AT 2002071600119 20020716 00119 2002 7 16 HEEA080292 4 20020702 A 2210 214074303115 AMPLIFIER BELL 214 214ST 1182106 SW AUTOFLIGHT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 AMPLIFIER ASSY ROLL CHANNEL KICKS OFF IN HOVER. COULD NOT ADJUST. 2 G 7 2 4U H10SW 2002071600120 20020716 00120 SO 2002 7 16 SIMA200217707 1 20020620 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 DURING IMBV INSPECTION FOUND CORROSION ON LEFT HAND BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBL ER ANGLE, PLATE, FILLER, AND SHIMS. REPAIR DONE IAW AND STANDARD SRM PRACTICES. 2 L 7 2 4T RT T00011AT 2002071600121 20020716 00121 EU 2002 7 16 SIMA200217708 1 20020619 A 2612 WIRE AEROSP ATR42 ATR42300 8680920 EU RT ENGINE BROKEN A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 269AT 269 DURING CLIMB, CREW REPORTED A RIGHT ENGINE FIRE WARNING. CREW FOLLOWED EMERGENCY PROCEDURES AND SHUT DOWN ENGINE AND RE TURNED TO DEPARTURE FIELD. C/A, MAINTENANCE FOUND AND REPAIRED TWO BROKEN WIRES (3137-7006-22 AND 3137-7013-22) IAW ATR WM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2002071600122 20020716 00122 SW 2002 7 16 HEEA080294 1 20020702 A 3340 214175140103 POWER SUPPLY BELL 214 214ST 1182106 SW EXTERIOR LIGHTS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 POWER SUPPLY WILL NOT CHARGE. 2 G 7 2 4U H10SW 2002071600123 20020716 00123 EU 2002 7 16 HEEA080295 1 20020607 A 2913 350A35013004 DRIVE GEAR SNIAS 350 AS350B 8680801 EU HYD PUMP WORN E HEEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 973AE 1589 3229 DURING CRUISE FLIGHT, PILOT REPORTED HYDRAULIC AUDIO AND WARNING LIGHT ILLUMINATED. CONTROLS STARTED FEELING HEAVY. PE RFORMED PRECAUTIONARY LANDING. INSPECTION REVEALED HYDRAULIC PUMP DRIVE SPLINES WORN. REPLACED PUMP DRIVE AND REPLACED HYDRAULIC PUMP. 1 G 7 1 3U H9EU 2002071600124 20020716 00124 EU 2002 7 16 HEEA080299 1 20020611 A 6510 593404 BEARING SNIAS 350 AS350B 8680801 EU TAIL ROTOR ROUGH E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 856PH 3352 TAIL ROTOR BEARING IS ROUGH. 1 G 7 1 3U H9EU 2002071600129 20020716 00129 EU 2002 7 16 HEEA080300 1 20020611 A 6720 BEARING BOLKMS 105 BO105S 5626006 EU CONTROL ROD ASSY WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 8197X S808 CONTROL ROD ASSY HAS WORN BEARINGS. REPAIRED. 1 G 7 2 3U H3EU 2002071600130 20020716 00130 EU 2002 7 16 HEEA080301 1 20020611 A 3246 10550103 SKID BOLKMS 105 BO105S 5626006 EU MLG CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5031U S678 LANDING GEAR SKID CORRODED AND DENTED. SCRAPPED. 1 G 7 2 3U H3EU 2002071600131 20020716 00131 GL 2002 7 16 HEEA080302 2 20020611 A 7323 23054628 TUBE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE CRACKED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5031U S678 FOUND A STRESS CRACK IN THE FLARE OF TUBE. SCRAPPED. 1 G 7 2 3U 3 U H3EU E4CE 2002071600132 20020716 00132 EU 2002 7 16 HEEA080303 1 20020611 A 6520 BUSHING BOLKMS 117 BK117A1 5626010 EU T/R GEARBOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911TL 6668 507 7198 TAIL ROTOR GEARBOX HAS A WORN BUSHING. REPAIRED. 1 G 7 2 3U H13EU 2002071600133 20020716 00133 NM 2002 7 16 F3LA200200169 1 20020610 A 7110 COWLING BOEING 737 7373Q8 1384670 NM NR 2 ENGINE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3269 26293 DURING C-3 CHECK, INSPECTION REPORTED HOLE IN NR 2 ENGINE INBD CORE COWL, TOP FWD INSIDE CORNER. REPAIRED NR 2 ENGINE T HRUST REVERSER BIFURCATION PANEL PER EA 54T-737-037, REV. A. 2 L 7 2 4F RT A16WE 2002071600134 20020716 00134 EU 2002 7 16 HEEA080304 1 20020611 A 2510 1058251806 ROLLER BOLKMS 105 BO105S 5626006 EU SEAT CHAFED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5031U S678 SEAT ROLLERS CHAFED INTO SEAT RAIL. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H3EU 2002071600135 20020716 00135 EU 2002 7 16 HEEA080305 1 20020625 A 5610 TRACK SNIAS 350 AS350B2 8680813 EU COCKPIT WINDOW BROKEN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 40466 3004 SLIDING WINDOW TRACK BROKEN. 1 G 7 1 3U H9EU 2002071600136 20020716 00136 EU 2002 7 16 HEEA080306 1 20020625 A 2121 0500847 BLOWER SNIAS 350 AS350B 8680801 EU CONDENSOR FAILED E HEEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 03 972AE 3234 CONDESER BLOWER HAS SMOKE SMELL AND INTERMITTENT OPERATION. 1 G 7 1 3U H9EU 2002071600137 20020716 00137 EU 2002 7 16 HEEA080307 1 20020625 A 6220 350A32308801 FLANGE SNIAS 350 AS350B 8680801 EU MAIN ROTOR WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 971AE 1285 3230 WEAR ON FLANGE ASSEMBLY. SCRAPPED LOCALLY. 1 G 7 1 3U H9EU 2002071600138 20020716 00138 EU 2002 7 16 HEEA080308 1 20020625 A 6321 350A32501000 LINER SNIAS 350 AS350B 8680801 EU ROTOR BRAKE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 971AE 326 M918 3230 MAIN ROTOR BRAKE HAS A WORN LINING. 1 G 7 1 3U H9EU 2002071600139 20020716 00139 EU 2002 7 16 HEEA080309 1 20020625 A 6510 350A33215300 BEARING SNIAS 350 AS350B 8680801 EU TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 972AE 3234 TAIL ROTOR LAMINATED HINGE BEARING WORN. 1 G 7 1 3U H9EU 2002071600140 20020716 00140 EU 2002 7 16 HEEA080310 1 20020625 A 6730 SC5083 SERVO SNIAS 350 AS350B 8680801 EU ROTOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 973AE 1621 3229 PILOT VALVE LOCK PIN STICKING WHEN YOU LOSE HYDRAULICS PRESSURE AND SERVO HARD OVERS TO THE RIGHT. 1 G 7 1 3U H9EU 2002071600141 20020716 00141 NM 2002 7 16 F3LA200200170 1 20020610 A 5412 FIREWALL BOEING 737 7373Q8 1384670 NM NR 2 ENGINE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 318FL 3269 26293 DURING C-3 CHECK, INSPECTION REPORTED HOLE IN FIREWALL UNDER SEALANT IN NR 2 ENGINE LT THRUST REVERSER COWL. REPAIRED D AMAGE PER EA 54T-737-037, REV A. 2 L 7 2 4F RT A16WE 2002071600142 20020716 00142 EU 2002 7 16 HEEA080311 1 20020625 A 6210 10515150 BLADE BOLKMS 105 BO105S 5626006 EU MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50293 6737 S677 THE OUTBOARD ABRASION STRIP HAS A HOLE PENETRATED THROUGH THE STRIP. 1 G 7 2 3U H3EU 2002071600143 20020716 00143 EU 2002 7 16 HEEA080312 1 20020625 A 6220 BEARING BOLKMS 105 BO105S 5626006 EU ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136H S833 MAIN ROTOR HEAD ROD END BEARINGS WORN. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H3EU 2002071600144 20020716 00144 EU 2002 7 16 HEEA080313 1 20020625 A 6220 BEARING BOLKMS 105 BO105S 5626006 EU ROD END ASSY WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136H S833 MAIN ROTOR HEAD ROD END BEARINGS WORN. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H3EU 2002071600145 20020716 00145 EU 2002 7 16 HEEA080314 1 20020625 A 6420 1053172901 HUB BOLKMS 105 BO105S 5626006 EU TAIL ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8199J S826 TAIL ROTOR HEAD AND BLADES ARE DAMAGED. 1 G 7 2 3U H3EU 2002071600146 20020716 00146 EU 2002 7 16 HEEA080315 1 20020625 A 6410 11731743 BLADE BOLKMS 117 BK117A1 5626010 EU TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911TL 7198 TAIL ROTOR BLADE HAS WORN PAINT. 1 G 7 2 3U H13EU 2002071600147 20020716 00147 EU 2002 7 16 HEEA080316 1 20020625 A 6410 11731743 BLADE BOLKMS 117 BK117A1 5626010 EU TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911TL 7198 TAIL ROTOR BLADE HAS WORN PAINT. 1 G 7 2 3U H13EU 2002071600148 20020716 00148 EU 2002 7 16 HEEA080317 1 20020625 A 6420 10531738101 SLEEVE BOLKMS 117 BK117A1 5626010 EU T/R HEAD WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8765J 7054 TAIL ROTOR HEAD SLEEVE HAS A WORN BEARING JOURNAL. 1 G 7 2 3U H13EU 2002071600149 20020716 00149 EU 2002 7 16 HEEA080318 1 20020625 A 6520 4619003003 SPLINE ADAPTER BOLKMS 105 BO105S 5626006 EU TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U 11698 S678 WORN PITCH SHAFT SPLINES AND CORROSION ON CASE. REPAIRED. 1 G 7 2 3U H3EU 2002071600150 20020716 00150 2002 7 16 HEEA080319 4 20020625 A 2370 8143802240D GPS BOLKMS 105 BO105S 5626006 EU COCKPIT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136H S833 ALL DATA UNREADABLE DUE TO DISTORTED FACEPLATE ON GPS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 2002071600151 20020716 00151 EU 2002 7 16 HEEA080320 1 20020626 A 6520 BEARING BOLKMS 117 BK117A1 5626010 EU T/R GEARBOX WORN E HEEA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SW 03 8765J 3963 673 7054 SEVERE VIBRATION DURING FLIGHT. WORN FEATHERING BEARINGS. REPLACED PARTS AND REPAIRED. 1 G 7 2 3U H13EU 2002071600152 20020716 00152 EU 2002 7 16 HEEA080321 1 20020626 A 2497 4639215002 HARNESS BOLKMS 105 BO105S 5626006 EU ELECTRICAL SHORTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136H S833 SHORT IN WIRE FOR STRAIN RELIEF. REPLACED HARNESS. 1 G 7 2 3U H3EU 2002071600153 20020716 00153 2002 7 16 HEEA080322 4 20020627 A 2330 AA21400 AMPLIFIER BOLKMS 105 BO105S 5626006 EU PA SIREN INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U S678 INOPERATIVE. TO BE SENT TO VENDOR FOR REPAIR. 1 G 7 2 3U H3EU 2002071600154 20020716 00154 NM 2002 7 16 ANCF200200013 1 20020706 A 2133 1305026 OUTFLOW VALVE BOEING 767 767383 1385214 NM PWA 4060 PW4060 52119 NE CABIN PRESSURE FAILED W ANCF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 984AN 24357 AT FL 350 CABIN ALT ALERT PRESENTED ON EICAS, CABIN ALTITUDE MODE SELECTED SWITCHED TO AUTO 1, CABIN CONTINUED DESPRESSU RIZING, THEN SWITCHED TO MANUAL, VALVE CLOSED MANUALLY, CABIN CONTINUED CLIMBING AND REACHED 11000 FT, THEN WE DESCENT T O 12000 FT AND CABIN PRESSURIZATION CONTROLLED MANUALLY UPON LANDING, THE CREW RETURNED TO MIA. PERFORMED TROUBLESHOOTI NG AS PER FIM 21-30-00 FIG 108, REMOVED AND REPLACED CABIN OUTFLOW VALVE AND CABIN PRESS SELECT PANEL, GROUND OPERATION WAS SATISFACTORY IAW AMM 21-31-03, ACCOMPLISHED PRESSURIZATION CHECK IAW AMM 21-30-00, WITH SATISFACTORY RESULTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002071600156 20020716 00156 NM 2002 7 16 F3LA200200172 1 20020624 A 5220 COVER AIRBUS A319 A319111 3930336 NM EMERGENCY EXIT OUT OF ADJUST A F3LA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 908FR 1759 ABORTED TAKEOFF. FLIGHT CREW REPORTED LT OVERWING EMERGENCY EXIT OPEN INDICATION AT 100 KTS. ADJUSTED LT OVERWING EXIT DOOR HANDLE COVER FLAP. TESTED PER MM 25-23-47-401, TASK 25-23-47-991-017, FIG 402, AND CHECKED OKAY. 2 L 7 2 4F RT A28NM 2002072400097 20020724 00097 NM 2002 7 24 2002UALA01050 1 20020619 A 3260 189983 SWITCH BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE LANDING GEAR FAILED A UALA O OTHER G MULTIPLE FAILURE CR CRUISE 1 WP 29 915UA 25382 AT 35000 FT, TCAS FAIL AND ATC NOT RECEIVING TRANSPONDER ON LT OR RT, STARTING DESCENT RECEIVED WARNING HORN WHEN SPEED BRAKES DEPLOYED, AT SAME TIME CABIN ALT CLIMBED ABOVE 10,000. EXECUTED RAPID DEPRESS CHECK LIST, HALF WAY THROUGH DESC ENT - AUTO FAIL. OUTFLOW VALVE WENT FULL OPEN, RECEIVED LOW IDLE LIGHT, ALSO VNAV DISCONNECTED. REPLACED AIR SENSE RE LAYS R432 AND R282, REPLACED CONNECTOR D5212J ON E3-2 DISCONNECT BRACKET DUE TO BENT AND BURNT PIN. ALSO REPLACED AIR AND GROUND SENSE SENSORS S105 AND S106. 2 L 7 2 4F 4 F RT A16WE E2GL 2002071600157 20020716 00157 NM 2002 7 16 2002UALA01136 1 20020705 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 FUSELAGE SKIN HAD DENT AT FRAME AT STA.288 APPROX. TO STRINGER 19R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002071600158 20020716 00158 NM 2002 7 16 2002UALA01137 1 20020705 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 FUSELAGE SKIN HAS MULTIPLE DENTS BETWEEN STATION 740 AND 780, AND STRINGER 14L AND 18L. MAJOR REPAIR ACCOMPLISHED. INS TALLED DOUBLER AND TRIPLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002071600159 20020716 00159 NM 2002 7 16 2002UALA01138 1 20020706 A 5315 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 FORWARD CABIN FLOOR INTERCOSTAL AT STATION 301 TO 310.5 RBL 40 HAS EXCESSIVE MATERIAL REMOVED DURING CLEANUP. MAJOR REP AIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002071600160 20020716 00160 NM 2002 7 16 2002UALA01141 1 20020706 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 CABIN AFT PRESSURE DECK SKIN BLENDED BEYOND LIMITS STATION 1693, RBL 51 AND STATION 1685, RBL 51.5. MAJOR REPAIR ACCOMP LISHED. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002071600161 20020716 00161 NM 2002 7 16 2002UALA01144 1 20020709 A 2421 745329C GENERATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DIODE,ROTOR, EXC DEFECTIVE A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 663UA 27160 ON CLIMB FROM SFO RIGHT HAND GENERATOR DROPPED OFFLINE AND WAS UNABLE TO BE RESET. SUPPLEMENTAL DATA UPDATE REPLACED RIG HT GENERATOR.DEFECTIVE PARTS - FOUND DIODE, ROTOR AND EXCITER FAILED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002071600162 20020716 00162 NM 2002 7 16 2002UALA01155 1 20020710 A 5330 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 779UA 26941 EXTERNAL SKIN DAMAGED AT STA. 220.5 AT STRINGER 36L. MAJOR REPAIR ACCOMPLISHED. EXTERNAL DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002071600163 20020716 00163 WP 2002 7 16 IXXA0200046O 1 20020712 A 3230 4597340550 CYLINDER DOUG DC8 DC871F 302199D WP WHEEL WELL DEFECTIVE A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 823BX 83846 674 46064 ENROUTE FROM BFI TO PDX, THE LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING THE LANDING UPLATCH CHECK. THE FIIGHT CREW CYC LED THE LANDING GEAR TO EXTINGUISH THE WARNING INDICATION. THE FLIGHT CONTINUED TO PDX FOR AN UNEVENTFUL LANDING. MAINTE NANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE LEFT MAIN GEAR UPLATCH CYLINDER DEFECTIVE. MAINTENANCE REPLACED THE UPLA TCH CYLINDER IN ACCORDANCE WITH THE MAINTENANCE MANUAL AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK. THE AIRCRAFT WAS RE TURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002071600164 20020716 00164 NM 2002 7 16 F3LA200200173 1 20020625 A 5347 CARGO TRACK BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO TRACK TIE DOWN SOCKET AT STA 947, LBL 17. REMOVED SECTION OF C ARGO TRACK IN AFT BAY AT LBL 17 FROM STA 917 TO STA 947. SPLICED IN NEW SECTION OF CARGO TRACK PER SRM 51-30-02, 53-40- 5 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002071600165 20020716 00165 NM 2002 7 16 AWXA200200616 1 20020714 A 3350 BMS13311122 WIRE BOEING 737 737277 1384570 NM SEAT ROW 7 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 PHX - EEL - DURING INSPECTION THE EMERGENCY EXIT PATHWAY LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 7 L/H. MAINTENANCE SPLI CED A BROKEN WIRE AT SEAT ROW 7 L/H IAW CHAP 20 SWPM, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002071600167 20020716 00167 NM 2002 7 16 UIE2002F00004 1 20020703 A 5310 WEB BOEING 747 74747UF 1384949 NM BS2658 ATLBL25 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 491MC 12440 29252 DURING ROUTINE INSPECTION AT CURRENT C CHECK, FOUND LOWER BULKHEAD WEB CRACKED 0.60 INCH LONG AT BS 2658, BETWEEN WL 260 AND 265 AND BETWEEN L/S LBL 25 AND LBL 30. CUT WAY CRACKED AREA. PERFORMED DYE CHECK INSPECTION OF CUT-OUT AREA PER S OPM 20-20-20. NO ADDITIONAL CRACKING FOUND. FABRICATED FILLER, REPAIR DOUBLER AND ANGLE. INSTALLED PER STANDARD SRM. REFINISHED PER SRM. 2 L 7 4 4F RT 1384945 2002071600168 20020716 00168 NM 2002 7 16 F3LA200200175 1 20020625 A 5230 SKIN BOEING 737 7372P6 1C84609 NM CARGO DOOR DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED DENT IN AFT CARGO DOOR AT TOP OF DOOR. CUT OUT DAMAGE PER SRM 52-00-3. REMOVED S TIFFENER PER SRM 51-30-02. FABRICATED DOUBLER PER SRM 52-00-03. INSTALLED REPAIR DOUBLER AND STIFFENER PER SRM 52-00-3 AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 2002071600175 20020716 00175 NM 2002 7 16 RYN2002F00028 1 20020530 A 5330 SKIN BOEING 727 727222 1384073 NM FUSELAGE SKIN CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT (C) CHECK, FOUND FUSELAGE SKIN CORRODED WITH RIVETS DISHED AND SKIN BULGED. BELOW FORWARD JACK POINT, AT STATION 340 . 2 L 7 3 4F A3WE 2002071600177 20020716 00177 NM 2002 7 16 RYN2002F00029 1 20020526 A 5100 FITTING BOEING 727 727222 1384073 NM NOSE WW STA227.8 CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT (C) CHECK, FOUND NOSE WHEEL WELL FORWARD BULKHEAD DOOR LINKAGE FITTING CORRODED, AT STATION 227.8, LEFT SIDE. 2 L 7 3 4F A3WE 2002071600178 20020716 00178 NM 2002 7 16 RYN2002F00030 1 20020531 A 2550 SEAT TRACK BOEING 727 727222 1384073 NM STA1090-1180 CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT (C) CHECK, FOUND CORROSION ON CABIN SEAT TRACK AT STATION 1090TO 1180, LBL 94. 2 L 7 3 4F A3WE 2002071600179 20020716 00179 NM 2002 7 16 RYN2002F00031 1 20020528 A 5100 WEB BOEING 727 727222 1384073 NM SHEAR WEB CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT (C) CHECK, FOUND CABIN SHEAR WEB SEVERAL AREAS OF CORROSION AT STATION 1148 TO 1183, RBL 24 TO 48. 2 L 7 3 4F A3WE 2002071600180 20020716 00180 NM 2002 7 16 RYN2002F00032 1 20020601 A 5720 RIB BOEING 727 727222 1384073 NM STA686.5 STR6 CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT (C) CHECK, FOUND CRACK IN RIGHT WING NUMBER THREE TANK, ON LOWER WEB, OUTBOARD STATION 686.5, STRINGER NUMBER SIX. 2 L 7 3 4F A3WE 2002071600182 20020716 00182 2002 7 16 ZW0A0207301 4 20020711 A 2565 D30654122 SLIDE BOEING 757 757231 1384950 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 711ZX 28481 THE RIGHT SIDE FWD CABIN DOOR EVACUATION SLIDE BOTTLE PRESSURE WAS LOW. REPLACED THE SLIDE. CHECK-C 11-29-01 MCI. --C LOSED-- 2 L 7 2 4F RT A2NM 2002071600183 20020716 00183 NM 2002 7 16 F3LA200200184 1 20020701 A 5320 SILL BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR OPENING LOWER WEB SILL. REPLACED CARGO WEB SILL PER S RM 51-30-2. 2 L 7 2 4F RT A16WE 2002071600184 20020716 00184 NM 2002 7 16 F3LA200200185 1 20020702 A 5347 SEAT TRACK BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR TRACK, STA 797 TO 809, RBL 14. REPLACED CARGO FLOOR TRAC K PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 2002071600188 20020716 00188 EU 2002 7 16 A6WA200260021 1 20020621 A 5311 FRAME BAC 146 146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 CRACKS AND CORROSION TO LOWER HALF OF FRAME 18 FROM 18L TO STR 18R. 2 H 7 4 4F A49EU 2002071600189 20020716 00189 CE 2002 7 16 GUU2002F00016 1 20020611 A 1430 EWB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 69549 13090 UE194 AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW WITH BEECH MAINTENANCE MANUAL. 2 L 7 2 4T RT A24CE 2002071600190 20020716 00190 CE 2002 7 16 KC82002F00002 1 20020619 A 2910 HYDRAULIC LINE LEAR 25 25D 5170514 CE HYD SYSTEM CRACKED E KC8A O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 23 95CK 248 AIRCRAFT LOST HYDRAULIC PRESSURE AFTER CREW SELECTED THE GEAR DOWN. THE GEAR HAD 3 GREEN DOWN AND LOCKED INDICATIONS AN D 2 RED UNSAFE INDICATIONS. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND HYDRAULIC LINE CRACKED UNDERNEA TH ATTACHING ADEL CLAMP. HYDRAULIC LINE WAS REPLACED, HYDRAULICS WERE SERVICED, LANDING GEAR WAS CYCLED, AND EMERGENCY AIR WAS SERVICED USING PROCEDURES IN THE MFG MM. 2 L 7 2 4J A10CE 2002071600191 20020716 00191 NM 2002 7 16 KPV2002F00001 1 20020629 A 3230 CONTROL CABLE DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE NLG BROKEN A KPVA O OTHER O OTHER NR NOT REPORTED 1 WP 13 808WP 026 NOSEWHEEL ALT EXTENSION HANDLE/CABLE BROKE. REMOVED AND REPLACED NOSEWHEEL ALT EXTENSION HANDLE CABLE, RIGGED NLG ALTER NATE RELEASE CONTROL IAW MM. OPS CHECK OF ALT EXTENSION SYSTEM GOOD IAW MM. 2 H 7 2 4T 4 T RT A13NM E20NE 2002071600192 20020716 00192 NE 2002 7 16 KPV2002F00002 2 20020629 A 7321 FUEL CONTROL DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE NR 2 ENGINE OUT OF RIG A KPVA O OTHER O OTHER UK UNKNOWN 1 WP 13 808WP 026 NR 2 ENGINE TORQUE BEGAN SURGING/FLUCTUATING +-15 PERCENT AT TAKE OFF. CONTINUED FOR A COUPLE OF MINUTES WITHOUT OTHER GAUGE INDICATIONS. TRIED MANUAL FUEL CONTROL (DROPPED AS IT SHOULD TO 68 PERCENT TORQUE), RESELECTED ECU. FO COULD FE EL SURGES. AFTER STEADYING OUT FOR A COUPLE OF MINUTES, SURGES BECAME +- 20 PERCENT AND WE BROUGHT POWER TO IDLE, PROP M IN. - STABLE AFTER THAT. INSPECTED AND CHECKED NR 2 ENGINE POWER AND CONDITION LEVERS. FOUND NR 2 ENGINE OUT OF RIG. RIGGED NR 2 ENGINE POWER AND CONDITION LEVERS IAW DHC 8 ENGINE RIGGING MANUAL. GROUND RUN CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2002071600193 20020716 00193 NM 2002 7 16 KPV2002F00003 1 20020516 A 3230 CONTROL CABLE DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE NLG FRAYED A KPVA O OTHER O OTHER NR NOT REPORTED 1 WP 13 805WP 353 NOSE WHEEL ALT EXTENSION CABLE FRAYED. REMOVED AND REPLACED NOSE WHEEL ALT EXTENSION HANDLE CABLE, RIGGED NLG ALT EXTEN SION RELEASE CONTROL IAW DHC 8 MM. OPS CHECK GOOD IAW DHC8 MM. 2 H 7 2 4T 4 T RT A13NM E20NE 2002071600194 20020716 00194 SO 2002 7 16 LAB2002F00001 1 20020602 A 2721 TUBE PIPER PA32 PA32300 7103212 SO RUDDER TRIM CRACKED E LABA K NONE O OTHER IN INSP/MAINT 1 AL 05 54KA 3218 327840197 RUDDER TRIM ADJ. TUBE, FOUND CRACKED ON PHASE INSPECTION OF AIRCRAFT. 1 L 7 1 3O A3SO 2002071600195 20020716 00195 SO 2002 7 16 LD22002F00000 1 20020605 A 2913 1159SCH5057 PUMP GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE HYD SYSTEM CONTAMINATED B LD2R K NONE O OTHER IN INSP/MAINT 1 GL 15 93M 1276 567 11241 FLUID SAMPLE TAKEN AT 100 HOUR INTERVAL SHOWS THAT THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP WILL CONTINUE TO TAKE F LUID SAMPLES AT 100 HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. 2 L 7 2 4F 4 F RT A12EA E00057EN 2002071600196 20020716 00196 EU 2002 7 16 MALA020404 1 20020713 A 2930 L387105A SWIVEL SAAB SF340 SF340A 7850100 EU A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 89XJ 340A089 DURING FLIGHT #3105 AFTER GEAR RETRACTION AFTER TO, CREW RECEIVED A HYDRAULIC MC ON CWP. HYDRAULIC FLUID QUANITY WENT TO ZERO. MAIN ACCUMULATOR WENT TO ZERO. PERFORMED QRH AND PERFORMED EMERGENCY GEAR EXTENSION. AIR RETURN TO DTW. MAINTE NANCE INSTALLED NEW HYDRAULIC SWIVEL PN L387105A. PERRFORMED OPS CHECKS IAW SF 340 AMM CHAPO 32. ALL CHECKS GOOD AT THI S TIME. 2 L 7 2 4T RT A52EU 2002071600197 20020716 00197 EU 2002 7 16 MALA020405 1 20020713 A 7930 8543 PRESSURE SWITCH SAAB SF340 SF340A 7850100 EU A MALA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 15 369XJ DURING TAKEOFF ON FLIGHT #3037, LEFT ENGINE OIL PRESSURE LIGHT ILLUMINATED ON TAKEOFF ROLL. A/C RETURNED TO GATE WITHOU T INCIDENT. MAINTENANCE REPLACED LH ENGINE PGB OIL PRESSURE SWITCH PN 8543 2 L 7 2 4T RT A52EU 2002111800081 20021118 00081 NM 2002 11 18 C7WA200200005 1 20020713 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE DENTED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE BS 310 BETWEEN STRINGER 23R AND 24R SKIN WITH DENT OUT OF LIMITS. RE PAIRED FUSELAGE SKIN SECTION FROM BS 312.5 TO BS 308 BETWEEN STRINGER 23R AND 24R IAW SRM 53-30-3 FIG 13. (M) 2 L 7 3 4F A3WE 2002111800080 20021118 00080 NM 2002 11 18 C7WA200200004 1 20020713 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE DENTED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE BS 40 BETWEEN STRINGER 19R AND 20R SKIN WITH DENT OUT OF LIMITS. INS TALLED REPAIR IAW SRM 53-30-3 FIG 13. (M) 2 L 7 3 4F A3WE 2002071600198 20020716 00198 NE 2002 7 16 MEX2002192 2 20020618 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 POWER LOSS W ASMF C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 23 162PL 49765 AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF LOW ACCELERATION IN ENGINE NUMBER 2. AIRCRAFT WAS SENT TO THE HANGER. ENGINE NUMBER TWO WAS REPLACED IAW MM. ACCELERATION TEST WAS PERFORMED IN BOTH ENGINES IAW MM. 2 L 7 2 4F 4 F RT A6WE E9NE 2002071600199 20020716 00199 CE 2002 7 16 MXI2002F00000 1 20020624 A 3233 23271087 ACTUATOR LEAR 35 35A 5170602 CE RT MLG LEAKING E MXIA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 21 431AS 431 RIGHT MAIN LANDING GEAR ACTUATOR LEAKING HYDRAULIC FLUID. PLUNGER O-RING PART NUMBER M83461/1-146 FAILED BY ROLLING IN THE ACTUATOR. INSTALLED ACTUATOR REPAIR KIT WHICH CONTAINED AN IMPROVED SEAL. 2 L 7 2 4F A10CE 2002071600201 20020716 00201 NM 2002 7 16 Q2S2002F00001 1 20020617 A 3610 3206254 VALVE BOEING 747 747230B 1384889 NM NR 3 ENGINE MALFUNCTIONED A Q2SA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 744SA 22363 AIR TURN BACK: AFTER LIFT OFF, HIGH STAGE LIGHT ILLUMINATED ABOUT 200 FEET. FIRE DETECTION LIGHT ILLUMINATED AT MASTER CAUTION PANEL, NO LIGHT IN HANDLE. A AND B NEEDLE INDICATORS WERE AT 7.5. TESTED SYSTEM, NR 3 LIGHT CAME ON AND STAYE D ON. SHUT DOWN ENGINE AND LIGHT WENT OUT AFTER START LEVER PLACED IN CUTOFF. REMOVED AND REPLACED NR 3 ENGINE PRESSUR E RELIEF VALVE IAW MM. 2 L 7 4 4F A20WE 2002071600202 20020716 00202 NE 2002 7 16 QFY2002F00001 2 20020612 A 7421 01049586 ELECTRODE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D1 52060 NE IGNITER LOOSE E QFYR K NONE O OTHER IN INSP/MAINT 1 NE 03 22AF 150 5600129 CENTER ELECTRODE IGNITER WAS FOUND TO BE LOOSE IN THREE OUT OF FOUR IGNITERS INSTALLED ON AIRCRAFT AT PHASE INSPECTION. 2 L 7 2 4F 4 F RT A22CE E1NE 2002071600203 20020716 00203 WP 2002 7 16 CALA0200398 1 20020715 A 5320 WEB DOUG DC9 DC982 3022082 WP FS 1250-1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND L/H CUSP WEB CORRODED FROM FS 1250-1309. A NEW WEB AND FITTING WERE INSTALLED IAW SRM 51-30-2, 51-30-1, AND 51-30-5. 2 L 7 2 4F A6WE 2002071600204 20020716 00204 WP 2002 7 16 CALA0200399 1 20020715 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FS 1117 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND LONGERON 21L CORRODED ON OUTBOARD SURFACE AT FS 1117. THE CORRODED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW ECRA 5310-04264. 2 L 7 2 4F A6WE 2002071600205 20020716 00205 WP 2002 7 16 CALA0200400 1 20020715 A 5320 WEB DOUG DC9 DC982 3022082 WP FS 1136 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND AFT CARGO COMPARTMENT DOOR CUTOUT LOWER TORQUE BOX WEB PUNCTURED AT FS 1136 WITH A 1" CRACK AT FS 1212. THE TORQUE BOX WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-1, AND 51-30-5. 2 L 7 2 4F A6WE 2002071600206 20020716 00206 WP 2002 7 16 CALA0200401 1 20020715 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 200-228 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 200-228. THE CORRODED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 53- 05, FIGURE 4F, SHEET 1. 2 L 7 2 4F A6WE 2002071600207 20020716 00207 WP 2002 7 16 CALA0200402 1 20020715 A 5320 WEB DOUG DC9 DC982 3022082 WP FS 1040-1060 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND CUSP WEB CORRODED AT FS 1040-1060, LBL 44-58. A NEW WEB AND FITTINGS WERE INSTALLED IAW SRM 51-30-2, 51 -30-1, AND 51-30-5. 2 L 7 2 4F A6WE 2002071600208 20020716 00208 EU 2002 7 16 REX2002F00006 1 20020613 A 2620 M30903870 SQUIB SAAB SF340 SF340A 7850100 EU CARGO BAY DAMAGED A REXA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 SO 25 407BH 2526 340A078 WHILE INVESTIGATING REASON FOR CARGO SMOKE WARNING IT WAS FOUND THAT THE CARGO FIRE EXTINGUISHER BOTTLE WAS NOT FIRED. CREW REPORTED THAT THE BOTTLE WAS FIRED IAW EMERGENCY PROCEDURES. THE CARGO BOTTLE SQUIB WAS FOUND TO HAVE BENT ELECTRI CAL PINS. SQUIB WAS REPLACED THE THE SYSTEM WAS OPERATIONALLY TESTED. 2 L 7 2 4T RT A52EU 2002071600209 20020716 00209 EA 2002 7 16 REX2002F00007 1 20020610 A 2510 501947403 HANDLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT BROKEN A REXA K NONE O OTHER IN INSP/MAINT 1 SO 25 8432A 3818 7432 INERTIA REEL LOCK HANDLE BROKEN. REMOVED AND REPLACED INERTIAL REEL LOCK HANDLE WITH NEW PART. 2 L 7 2 4F RT A21EA 2002071600210 20020716 00210 EA 2002 7 16 REX2002F00008 1 20020524 A 2611 SMOKE WARNING CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FALSE ACTIVATION A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 8580A 7580 AIRCRAFT HAD A LAVATORY SMOKE CAUTION MESSAGE IN FLIGHT. FLIGHT CREW DECLARED AN EMERGENCY AND AN OTHERWISE UNEVENTFUL LANDING WAS MADE. MAINTENANCE PERFORMED A SUCCESSFUL OPERATIONAL CHECK OF THE SMOKE DETECTION SYSTEM IAW APPROVED AMM P ROCEDURES. 2 L 7 2 4F RT A21EA 2002071600211 20020716 00211 NM 2002 7 16 QXEA0200954 1 20020708 A 3350 61047811 BATTERY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 14440 529 PDX-EMERGENCY LIGHTS CAN NOT BE CONTROLLED OFF BATTERY BUS ALONE. WORK OFF WITH EXTERNAL POWER. REPLACED 3351-K4 RELAY. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002071600212 20020716 00212 EU 2002 7 16 RF12002F00000 1 20020604 A 3200 441731 STRUT PARTEN P68 P68TCOBS 6780108 EU LANDING GEAR CRACKED A RF1R O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 01 737 4788 40004OTC INSPECTION PERFORMED AT 3940.0 TTAF. NO CRACKS FOUND AT THIS TIME. STRUT BEGINS LEAKING FLUID APPROX 700 HOURS LATER. CRACKS FOUND AT 4788.6 WHILE TROUBLE SHOOTING LEAKS. TT ON PART AFTER MAGNETIC PARTICLE INSPECTION-848.6. 1 H 7 2 3O RT A31EU 2002071600213 20020716 00213 EU 2002 7 16 USAABA02016 1 20020619 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 672UW 0333 FOUND EPSU TEST FAILED FOR DOORS 2L AND 4R. MAINTENANCE REPLACED THE BATTERIES AT DOORS 2L AND 4R. 2 L 7 2 4F RT A46NM 2002071600214 20020716 00214 NM 2002 7 16 USAABB02094 1 20020619 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 FOUND THE EXTERIOR EMERGENCY LIGHT FOR THE AFT RIGHT DOOR SLIDE GROUND ILLUMINATION INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A1NM 2002071600215 20020716 00215 NE 2002 7 16 GUU2002F00017 2 20020612 A 7200 3044900 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE MALFUNCTIONED A GUUA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 17 16540 12572 UE172 DURING CLIMB OUT AT 10,000 FEET, RIGHT ENGINE SURGED AND TORQUE DROPPED 1500 FT LBS. DIVERTED RIGHT ENGINE SECURED FOR LANDING. REMOVED AND REPLACED RIGHT GAS GENERATOR. 2 L 7 2 4T 4 T RT A24CE E26NE 2002071600216 20020716 00216 EU 2002 7 16 U30A200200016 1 20020714 A 3150 350E053020303 FWC AIRBUS 320 A320214 3930316 EU ZONE 128 FAULTY A U30A K NONE J WARNING INDICATION CR CRUISE 1 EA 17 260AV 194 1564 Flight 165 PUJ-PHL; Flap position indicator occasionally showing slats in movement with flaps up - Master Wrn Lt shows " Master" on Capt side & "Warn" on F/O side concurrently with slat indication - no change in VMAX indication on PFD and no aural warning. With this additional info,problem moved to #1 side. Swapped FWC's to put suspect FWC in # 2 position, I/ A/W AMM 31-53-43-401. S/N 0E0006298 now in #2 position, S/N 0E0006243 now in # 1 position. C/W Ops Ck of FWS, AFS Land T est & Ground Scanning of Central Warning System I/A/W AMM 22-97-00-501 & AMM 31-50-00-501. All Systems Ops Ck'd ok. Defe rred # 2 FWC per MEL 31-53-06. 2 L 7 2 4F RT A28NM 2002111800084 20021118 00084 NM 2002 11 18 C7WA200200008 1 20020713 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN BULGED FROM BS 344 TO BS 360 BETWEEN STRINGER 19R AND 24R. REPA IRED FUSELAGE SKIN FROM BS 337.5 TO BS 360 BETWEEN STRINGER 19R AND 24R IAW SRM 53-30-4 FIG 12 WITH DOUBLER TO REMOVED L EVEL 2 CORROSION. (M) 2 L 7 3 4F A3WE 2002071600217 20020716 00217 NM 2002 7 16 RYN2002F00033 1 20020529 A 5100 PANEL BOEING 727 727222 1384073 NM STA620-720DRBL20 CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT (C) CHECK, FOUND FORWARD PIT TRANSISTION PANEL WITH CORRODED AREAS, STATION 620 TO 720D, RBL 20 TO 26, ON UPPER AND L OWER SURFACES. 2 L 7 3 4F A3WE 2002071600218 20020716 00218 NM 2002 7 16 RYN2002F00034 1 20020529 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT (C) CHECK, FOUND CABIN FLOOR BEAM WITH .5000 INCH CRACK PROTRUDING FROM LIGHTENING HOLE, AT STATION 820, LBL 48. 2 L 7 3 4F A3WE 2002071600219 20020716 00219 NM 2002 7 16 RYN2002F00035 1 20020529 A 5311 FRAME BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT (C) CHECK, FOUND FORWARD CARGO COMPARTMENT LOWER LOBE FRAME HAS A THREE INCH CRACK, AT STATION 520, RBL50. 2 L 7 3 4F A3WE 2002111800091 20021118 00091 NM 2002 11 18 C7WA200200012 1 20020713 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION STRINGER 21L BETWEEN BS 720 AND 740. REPAIRED FUSELAGE STRINGER 21L F ROM BS 720E PLUS 3 TO BS 740 IAW SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2002071600220 20020716 00220 NE 2002 7 16 ASOA02089S 2 20020211 A 7260 5019T39P023 GEAR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE BROKEN A ASOA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 11 852AS 7369 872329 FLT 4563 - WHILE CLIMBING-OUT OF FWA, AT 21,000 FEET, THE LEFT ENGINE N2 VIBRATION SPIKED APPROXIMATELY 2.6 MILS. THE F LIGHT ATTENDANT AND PASSENGERS REPORTED A LOUD NOISE FROM THE LEFT ENGINE. THE LEFT ENGINE SHUT ITSELF DOWN. THE CAPTA IN DECLARED AN EMERGENCY AND RETURNED TO FWA FOR AN OVERWEIGHT LANDING. MAINTENANCE PERFORMED THE OVERWEIGHT LANDING IN SPECTION. NO DEFECTS WERE NOTED. THE LEFT ENGINE WAS REMOVED AND REPLACED. TEAR DOWN REPORTS FROM LUFTHANSA AERO REVE AL THE MAIN CAUSE OF THE FAILURE WAS EXTENSIVE DAMAGE OF THE ACCESSORY GEAR BOX CAUSED BY A PIECE OF THE AXIS-P GEAR BRE AKING OFF. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2002071600221 20020716 00221 WP 2002 7 16 MWEA020447 1 20020713 A 7932 OIL SYSTEM DOUG DC9 DC914 3022034 WP ENGINE A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 500ME 45711 ON DEPARTURE OUT OF MILWUAKEE RIGHT ENGINE OIL QTY INDICATION DECREASED TO ZERO. -- DEFERRED RIGHT ENGINE OIL QTY PER MEL 79-3 2 L 7 2 4F A6WE 2002071600222 20020716 00222 NM 2002 7 16 MWEA020446 1 20020713 A 7932 OIL SYSTEM DOUG MD88 MD88 3023688 NM ENGINE A MWEA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 GL 31 701ME 49760 LEFT OIL QTY WENT TO ZERO QTS. -- REMAINS UNCORRECTED AT THIS TIME. 2 L 7 2 4F RT A6WE 2002082000158 20020820 00158 EA 2002 8 20 COMA0260425 1 20020715 A 5514 600210615 BUSHING CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 15001 7117 THE RIGHT VERTICAL STABILIZER HINGE BUSHING WAS DAMAGED AND REQUIRES REPLACEMENT. REMOVED AND REPLACED BUSHING IAW WVAC EO 601R-55-3359 CRJ AMM 20-26-00-910-803. 2 L 7 2 4F RT A21EA 2002111800094 20021118 00094 NM 2002 11 18 C7WA200200014 1 20020713 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FUSELAGE STRINGER 25L BETWEEN BS 720F AND BS 740. REPAIRED FUSELA GE STRINGER 25L BETWEEN BS 720E PLUS 5.00 AND BS 740 IAW SRM 53-10-3 FIG 3. (M) 2 L 7 3 4F A3WE 2002111800096 20021118 00096 NM 2002 11 18 C7WA200200015 1 20020713 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION AT COOPESA-SJO, FOUND LEVEL 2 CORROSION ON STRINGER 21R BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 21R BETWEEN BS 720E PLUS 4.00 TO BS 740 IAW SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2002111800097 20021118 00097 NM 2002 11 18 C7WA200200016 1 20020713 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 22R BETWEEN BS 720 AND BS 740. REPAIRED FUSELAGE STRINGE R 22R BETWEEN BS 720E PLUS 1.50 TO BS 740 IAW SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2002111800098 20021118 00098 NM 2002 11 18 C7WA200200017 1 20020713 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 25R BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRING ER 25R FROM BS 720D PLUS 5.00 TO BS 740 IAW SRM 53-10-3 FIG 3. (M) 2 L 7 3 4F A3WE 2002111800099 20021118 00099 NM 2002 11 18 C7WA200200018 1 20020713 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FS STRINGER 26L BETWEEN BS 480 AND BS 720D. REPAIRED FUSELAGE STR INGER 26L FROM BS 480 TO BS 680 IAW SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2002111800104 20021118 00104 NM 2002 11 18 C7WA200200022 1 20020713 A 5210 SKIN BOEING 727 727232 1384082 NM L1 DOOR CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND FORWARD ENTRY DOOR OUTER SKIN UPPER HINGE AREA CRACKED. REPAIRED FORWARD ENTRY DOOR SK IN FROM BS 325 TO BS 316 UPPER HINGE CUTOUT IAW SRM 52-00-3 FIG 4. (M) 2 L 7 3 4F A3WE 2002111800105 20021118 00105 NM 2002 11 18 C7WA200200023 1 20020713 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND EXT FUSELAGE SKIN BULGED AT BS 950F PLUS 10.0 AT STRINGER 4R. REPAIRED FUSELAGE SKIN L EVEL 2 CORROSION FROM BS 950F PLUS 8.00 TO BS 950F PLUS 19.5 BETWEEN STRINGER 3R AND STRINGER 5R IAW SRM 53-30-3 FIG 14 DETAIL IV. (M) 2 L 7 3 4F A3WE 2002111800107 20021118 00107 NM 2002 11 18 C7WA200200025 1 20020713 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN CRACK AT BS 196.5 WL 217. REPAIRED FUSELAGE SKIN FROM BS 191.5 TO BS 203.0 BETWEEN WL 212.5 AND WL 222.5 LBL 38.0 IAW S/B 727-53-0183 SECTION III PART I PARA C. (M) 2 L 7 3 4F A3WE 2002071700001 20020717 00001 SW 2002 7 17 AUS20020504 1 20020530 A 2770 2770066004 TUBE SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UA 01514 WP MCAULY 4HFR34 4HFR34C652 NE GUST LOCK DAMPER CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RUDDER GUST LOCK PLUNGER GUIDE TUBE FRACTURED APPROXIMATELY HALFWAY ALONG THE LENGTH. THE LOWER HALF OF THE FRACTU RED TUBEHAD MOVED AND STARTED TO ENGAGE IN THE RUDDER GUST LOCK QUADRANTPREVENTING THE CORRECT OPERATION OF THE RUDDER. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002071700002 20020717 00002 SW 2002 7 17 AUS20020505 1 20020602 A 5711 SPAR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) WING SPAR INNER WEB CRACKED IN TWO PLACES. CRACK LENGTH 12.7MM (0.5IN) LOCATED AT THE UPPER CENTER OF THE PORT STR INGER 13 CUTOUT. CRACK LENGTH 12.7MM (0.5IN) LOCATED AT THE LOWER RH CORNER OF THE STARBOARD STRINGER 13 CUTOUT. FOUND D URING INSPECTION IAW AD/SWSA226/86. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002071700003 20020717 00003 SO 2002 7 17 AUS20020509 2 20020523 A 8550 20522 WASHER PIPER PA34 PA34220T 7103420 SO CONT O360 LTSIO360RB SO ENGINE UNLOCKED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) RT ENGINE SCAVENGE PUMP COVER BOLT TAB WASHERS WERE NOT LOCKED. THE BOLTS WERE TIGHT. AREA HAD NOT BEEN DISTURBED SINCE FACTORY ASSEMBLY. 1 L 7 2 3O 3 O A7SO E9CE 2002071700004 20020717 00004 WP 2002 7 17 AUS20020511 1 20020524 A 5540 IBDN33130 INTERCOSTAL GOVT N22 N22B 3880102 WP ALLSN 250B 250B17C GL HARTZL HCA3V HCA3VF7 GL RUDDER SEPARATED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RUDDER INTERCOSTAL LOCATED BETWEEN WL 166.55 AND WL 192.65 SEPARATED FROM SKINS. 1 H 7 2 3T 3 T A7PC E10CE 5 C P6EA 2002071700005 20020717 00005 NM 2002 7 17 AUS20020513 1 20020530 A 2432 279202 CHARGER BOEING 747 747338 NM RROYCE RB211 RB211* 54555 NE BATTERY FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) APU BATTERY CHARGER FAULTY. 2 L 7 2 4F 4 F RT A20WE A12EU 2002071700007 20020717 00007 SO 2002 7 17 ASOA02163 1 20020311 A 5320 12005803001 SILL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 500AS 120272 DURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SILL WAS CORRODED BETWEEN FRAMES 13 AND 21. MAINTENANCE REMOVED AND R EPLACED THE CORRODED FLOOR SILL IAW SRM'S 51-20-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002071700008 20020717 00008 SO 2002 7 17 ASOA02164 1 20020314 A 5315 12005807007 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 500AS 120272 DURING C-CHECK INSPECTION IN BNA, THE CABIN FLOOR CENTER OMEGA BEAM HAD CORROSION THAT WAS BLENDED OUT OF LIMITS AT FRAM E 16. MAINTENANCE REPAIRED THE FLOOR CENTER OMEGA BEAM IAW ASA EO 120-53-0175. THIS EO REFERENCES EAC FAX GST-0894/02, DATED 18 MARCH 2002 AND SRM CHAPTER 51. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002071700009 20020717 00009 EU 2002 7 17 ASOA02165 1 20020323 A 2530 120VK01N0GB30S SWITCH AEROSP ATR72 ATR72212 8680945 EU GALLEY FAILED A ASOA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 535AS 464 FLT 4338 - DURING CRUISE FLIGHT FROM TRI TO ATL, THE FLIGHT ATTENDANT REPORTED AN UNUSUAL BURNED ODOR COMING FROM THE GA LLEY AREA. THE CAPTAIN REQUESTED THAT THE FLIGHT ATTENDANT PULL THE RELATED CIRCUIT BREAKERS, TURN OFF ALL THE SWITCHES AND CHECK FOR HEAT OR SIGNS OF SMOKE. NONE WERE FOUND, AND THE SMELL DID NOT GET WORSE. AIRCRAFT LANDED SAFELY IN ATL . MAINTENANCE REMOVED AND REPLACED THE GALLEY HEATER NR 2 PUSH BUTTON SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FO R SERVICE. (M) 2 H 7 2 4T RT A53EU 2002071700010 20020717 00010 NM 2002 7 17 AUS20020515 1 20020527 A 2121 FAN BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL AIR DISTRIBUTION FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 AU S (AUS) FORWARD EQUIPMENT EXHAUST FAN BURNED OUT. 2 L 7 2 4F 4 F RT A1NM E23EA 2002071700011 20020717 00011 EA 2002 7 17 ASOA02166 1 20020323 A 2752 85D10011 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 11 832AS 9372 7243 FLT 4466 - ON APPROACH INTO YYZ, AT 7000 FEET, THE FIRST OFFICER, PILOT FLYING, SELECTED THE FLAPS TO 8 DEGREES AND RECE IVED A FLAP FAIL MESSAGE. AN EMERGENCY WAS DECLARED. PROCEDURES WERE FOLLOWED FOR A ZERO FLAP LANDING IAW THE QRH. AI RCRAFT MADE AN UNEVENTFUL LANDING IN YYZ. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD FLAP ACTUATOR. OPERATIONAL CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002071700012 20020717 00012 EU 2002 7 17 ASOA02167 1 20020323 A 3350 7012210 LIGHT AEROSP ATR72 ATR72 EU EXIT SIGN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 640AS 405 FLT 4104 - DURING GROUND INSPECTION IN ATL, A MISSING LIGHT BULB WAS DISCOVERED IN THE PASSENGER DOOR EXIT SIGN. MAINTE NANCE REPLACED THE MISSING EMERGENCY EXIT LIGHT BULB. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2002071700013 20020717 00013 NE 2002 7 17 AUS20020517 2 20020527 A 7200 ENGINE BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE LEFT MALFUNCTIONED W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S (AUS) LT ENGINE HARD TO START DURING INFLIGHT START ON TEST FLIGHT FOLLOWING HEAVY MAINTENANCE. 2 L 7 2 4F 4 F RT A1NM E3NE 2002071700014 20020717 00014 SO 2002 7 17 ASOA02168 1 20020323 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 269AS 120210 FLT 4994 - DURING GROUND INSPECTION IN DFW, THE FRONT EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AN D REPLACED THE FORWARD MOST EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002071700015 20020717 00015 EU 2002 7 17 ASOA02169 1 20020324 A 3350 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN CORRODED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 531AS 454 FLT 4259 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY LIGHT ON THE PASSENGER DOOR AS WELL AS THE EXTERIOR EMERGENCY LIGHT ON THE AFT FUSELAGE WERE INOPERATIVE. MAINTENANCE CLEANED OFF CORROSION THAT WAS FOUND ON THE EMERGENCY LIGHTS ON THE PASSENGER DOOR AND THE AFT SECTION OF FUSELAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002071700016 20020717 00016 SO 2002 7 17 ASOA02170 1 20020314 A 5310 12002545003 SHEAR TIE EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 500AS 120272 DURING C-CHECK INSPECTION IN BNA, A SHEAR TIE WAS FOUND CORRODED AT FRAME 21 BETWEEN STRINGERS 19 AND 20 RIGHT AND ALSO BETWEEN STRINGERS 20 AND 21 RIGHT. MAINTENANCE REMOVED AND REPLACED THE CORRODED SHEAR TIE IAW SRM'S 51-25-00, 51-40-02 , AND 51-40-05. (M) 2 L 7 2 4T RT A31SO 2002071700017 20020717 00017 SO 2002 7 17 ASOA02171 1 20020314 A 5320 12007089603 BUTT STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 500AS 120272 DURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 13 AND 16 AND ALSO BETWEEN FRA MES 18 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTIONS OF THE CENTER BUTT STRAP IAW SRM'S 51-21-02, 51-2 5-00 AND 51-40-02. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 2002071700018 20020717 00018 SO 2002 7 17 ASOA02172 1 20020314 A 5320 12046158003 BUTT STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 500AS 120272 DURING C-CHECK INSPECTION IN BNA, THE RIGHT BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 21 AND 26. THE LEFT B UTT STRAP WAS ALSO FOUND WITH CORROSION BETWEEN FRAMES 21 AND 26 WITH IT ONLY BEING OUT OF LIMITS FROM FRAME 21 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE CORRODED RIGHT AND LEFT BUTT STRAPS IAW SRM'S 51-25-00, 51-14-02, AND 51-40-0 2. (M) 2 L 7 2 4T RT A31SO 2002071700019 20020717 00019 SO 2002 7 17 ASOA02173 1 20020314 A 5320 12005802001 SILL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 500AS 120272 DURNG C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT FLOOR SILL BETWEEN FRAMES 15 AND 21. MAINTENANCE REMOV ED AND REPLACED THE CORRODED LEFT FLOOR SILL IAW SRM'S 51-25-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002071700020 20020717 00020 SO 2002 7 17 ASOA02174 1 20020314 A 5320 12004149001 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 500AS 120272 DURING C-CHECK INSPECTION IN BNA, FOUND CORROSION WAS FOUND ON THE RIGHT OUTBOARD CROSSBEAM AT FRAME 20. MAINTENANCE RE MOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRM'S 51-20-05, 51-40-04, AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002071700021 20020717 00021 SO 2002 7 17 ASOA02175 1 20020314 A 5320 12008896001 CROSSBEAM EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 500AS 120272 DURING C-CHECK INSPECTION IN BNA, BOTH THE LEFT INBOARD AND RIGHT INBOARD CROSS FRAMES WERE FOUND CORRODED AT FRAME 16. MAINTENANCE REMOVED AND REPLACED BOTH RIGHT AND LEFT CORRODED CROSS BEAMS IAW SRM 51-40-02. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 2002071700022 20020717 00022 SO 2002 7 17 ASOA02176 1 20020314 A 5347 12015995003 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 500AS 120272 DURING C-CHECK INSPECTION IN BNA, BOTH THE LEFT INBOARD AND OUTBOARD SEAT TRACKS WERE FOUND TO BE CORRODED BETWEEN FRAME S 16 AND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACKS IAW SRM'S 51-20-01 AND 51-40-02 AND ALSO REFEREN CING ASA EO120-25-0007C. (M) 2 L 7 2 4T RT A31SO 2002071700023 20020717 00023 SO 2002 7 17 ASOA02177 1 20020314 A 5313 12006173009 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 500AS 120272 DURING C-CHECK INSPECTION IN BNA, STRINGER 18 LEFT WAS CORRODED BETWEEN FRAMES 13A AND 20. MAINTENANCE REMOVED AND REPL ACED THE CORRODED STRINGER IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002071700024 20020717 00024 NM 2002 7 17 AUS20020518 1 20020530 A 3310 245904 RHEOSTAT BOEING 747 747438 NM CABIN FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 AU S 3881 (AUS) DIMMER FAILED. LIMITED INFORMATION PROVIDED. 2 L 7 4 4F RT A20WE 2002071700025 20020717 00025 SO 2002 7 17 ASOA02178 1 20020314 A 5313 12005744019 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 500AS 120272 DURING C-CHECK INSPECTION IN BNA, STRINGER 19 RIGHT WAS FOUND CORRODED BETWEEN FRAMES 13 AND 17. MAINTENANCE REMOVED AN D REPLACED THE CORRODED STRINGER IAW SRM 51-40-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002071700026 20020717 00026 SO 2002 7 17 ASOA02179 1 20020314 A 5313 12005744017 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 500AS 120272 DURING C-CHECK INSPECTION IN BNA, FOUND CORROSION ON STRINGER 20 RIGHT BETWEEN FRAME 13 AND STATION 6653.1. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 51-22-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002071700027 20020717 00027 SO 2002 7 17 ASOA02180 1 20020320 A 5320 12005805003 BUTT STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 285AS 120265 DURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 13 AND 23. MAINTENANCE REMOVE D AND REPLACED THE CORRODED BUTT STRAP IAW SRM'S 51-25-00, 51-21-02, 51-14-00, AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002071700028 20020717 00028 SO 2002 7 17 ASOA02181 1 20020320 A 5320 12005806003 BUTT STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 285AS 120265 DURING C-CHECK INSPECTION IN BNA, THE RIGHT BUTT STRAP WAS CORRODED BETWEEN FRAMES 18 AND 21. MAINTENANCE REMOVED AND R EPLACED THE CORRODED RIGHT BUTT STRAP IAW SRM'S 51-25-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002071700029 20020717 00029 CE 2002 7 17 AUS20020519 1 20020524 A 7931 56001071 LINE CESSNA 340 340A 2076405 CE CONT O520 TSIO520N 17040 SO MCAULY 3AF32C 3AF32C93 GL ENGINE OIL PRESS CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) LT ENGINE OIL PRESSURE INDICATOR LINE LOCATED IN THE STUB WING ADJACENT TO THE NACELLE WORN THROUGH IN SEVERAL PLA CES BY CONTACT WITH THE LH ENGINE BLEED AIR DUCT. 1 L 7 2 3O 3 O 3A25 E8CE 5 C P22EA 2002071700030 20020717 00030 SO 2002 7 17 ASOA02182 1 20020320 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 285AS 120265 DURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SEAT TRACK WAS FOUND CORRODED BEYOND LIMITS FROM FRAME 14 TO 32 AND FR OM FRAMES 34 TO 40. MAINTENANCE REMOVED AND REPLACED THE TWO CORRODED SECTIONS OF THE RIGHT SEAT TRACK IAW SRM'S 51-21- 00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002071700031 20020717 00031 SO 2002 7 17 ASOA02183 1 20020320 A 5347 12026863001 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 285AS 120265 DURING C-CHECK INSPECTION IN BNA, THE LEFT WALL SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 32 TO FRAME 40. MAINTENA NCE REMOVED AND REPLACED THE CORRODED LEFT WALL SET TRACK IAW SRM'S 51-25-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002071700032 20020717 00032 WP 2002 7 17 AUS20020521 2 20020213 A 7200 P97189 ENGINE AMD FALC50 FALCON900 2700160 EU GARRTT TFE731 TFE7315R 01518 WP NR 2 OVERTEMP W O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 AU S 1566 (AUS) NR 2 ENGINE ITT EXCEEDED LIMITS. 2 L 7 3 4F 4 F RT A46EU E6WE 2002071700033 20020717 00033 SO 2002 7 17 ASOA02184 1 20020320 A 5320 12005802001 SILL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 285AS 120265 DURING C-CHECK INSPECTION IN BNA, THE LEFT FLOOR SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 15A AND 23. MAINTENANC E REMOVED AND REPLACED THE CORRODED FLOOR SILL IAW SRM'S 21-25-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002071700034 20020717 00034 EU 2002 7 17 AUS20020522 1 20020201 A 3260 84738702 PROXIMITY SWITCH AMD FALC50 FALCON900 2700160 EU NLG FAULTY W O OTHER N FALSE WARNING NR NOT REPORTED 1 AU S (AUS) LT NOSE LANDING GEAR DOOR PROXIMITY SWITCH INTERMITTENT INOPERATION. 2 L 7 3 4F RT A46EU 2002071700035 20020717 00035 SO 2002 7 17 ASOA02185 1 20020320 A 5320 12005803001 SILL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 285AS 120265 DURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD FLOOR SILL WAS FOUND WITH CORROSION FROM FRAME 13 TO 23. MAINTENAN CE REMOVED AND REPLACED THE CORRODED FLOOR SILL IAW SRM'S 51-25-00, 51-40-05, 51-21-02, 51-21-04, AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002071700036 20020717 00036 WP 2002 7 17 AUS20020523 1 20020605 A 6220 BUSHING HUGHES 269 269B 4470502 WP LYC O360 HIO360A1A 41514 EA MAIN ROTOR HEAD MISINSTALLED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) MAIN ROTOR GRIP BLADE BOLT BUSHES INCORRECTLY FITTED ON ALL THREE GRIPS. THE BUSHES WERE FITTED UPSIDE DOWN LEAVIN G A GAP BETWEEN THE GRIPS AND THE BLADES. WHEN THE BLADE BOLTS WERE TIGHTENED,THE GRIPS WERE DISTORTED. 1 G 7 1 3O 3 O 4H12 1E10 2002071700037 20020717 00037 NE 2002 7 17 AUS20020527 2 20020604 A 7200 ENGINE BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE NR 1 OVERSPEED W O OTHER E VIBRATION/BUFFET CR CRUISE 1 AU S (AUS) NR 1 ENGINE OVERSPEED. DURING INVESTIGATION AN ANOMALLY WITH THE ORIGINAL BUILD OF THE WIRING LOOMS WAS ALSO FOUND . 2 H 7 4 4F 4 F RT A49EU E6NE 2002071700038 20020717 00038 SO 2002 7 17 ASOA02186 1 20020320 A 5320 1200889601 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 285AS 120265 DURING C-CHECK INSPECTION IN BNA, THE FRAME 16 RIGHT INBOARD CROSS FRAME WAS FOUND TO HAVE CORROSION OUT OF LIMITS. MAI NTENANCE REMOVED AND REPLACED THE CORRODED CROSS FRAME AT FRAME 16 IAW SRM'S 51-40-02 AND 51-40-07. (M) 2 L 7 2 4T RT A31SO 2002071700039 20020717 00039 EU 2002 7 17 AUS20020529 1 20020524 A 2621 57333012 FIRE BOTTLE BAC 146 AVRO146RJ70A 1500095 EU NR 2 ENGINE DISCHARGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 2 ENGINE NR 2 FIRE BOTTLE EMPTY. FIRE BOTTLE HAD NOT BEEN DISCHARGED. 2 H 7 4 4F RT A49EU 2002071700040 20020717 00040 CE 2002 7 17 AUS20020530 1 20020531 A 2897 57181061 WIRE HARNESS CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP HARTZL HCB3T HCB3TN5 GL FUEL BOOST CHAFED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FUEL BOOST PUMP WIRING HARNESSES CHAFED. FOUND DURING INSPECTION IAW AD/CESSNA400/111 (SB CQB02-1R1). 1 L 7 2 3T 4 T RT A28CE E4WE 6 C P15EA 2002071700041 20020717 00041 NM 2002 7 17 AUS20020531 1 20020604 A 3230 LANDING GEAR BOEING 767 767* NM RROYCE RB211 RB211524* NE LEFT FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 AU S (AUS) LT MAIN LANDING GEAR FAILED TO RETRACT. 2 L 7 2 4F 4 F RT A1NM E12EU 2002071700042 20020717 00042 EU 2002 7 17 AUS20020536 1 20020131 A 2432 23531 BATTERY FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU MAINS OVERTEMP W O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 AU S D1166C02676 (AUS) FORWARD BATTERY OVERTEMPERATURE. 2 L 7 2 4F 4 F RT A20EU E2EU 2002071700043 20020717 00043 SO 2002 7 17 AUS20020544 1 20020503 A 2432 45521181640 RELAY PIPER PA34 PA34220T 7103420 SO CONT O360 TSIO360RB 17025 CE BATTERY/CHARGER FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) BATTERY RELAY SEIZED IN THE ON' POSITION. INVESTIGATION FOUND THAT WATER HAD LEAKED PAST THE AFT CABIN DOOR SEAL AND DRIPPED ONTO THE RELAY. 1 L 7 2 3O 3 O A7SO E9CE 2002071700044 20020717 00044 CE 2002 7 17 AUS20020545 2 20020420 A 7313 INJECTOR CESSNA 337 337 2075702 CE CONT IO360 IO360* 17025 CE MCAULY 2AF34C D2AF34C59 GL REAR ENGINE CONTAMINATED W C ABORTED TAKEOFF E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 AU S (AUS) REAR ENGINE FUEL INJECTOR NOZZLES (4OFF) CONTAMINATED WITH AN UNKNOWN SUBSTANCE. NO CONTAMINATION WAS FOUND IN THE UPSTREAM FILTER. 1 H 7 2 3O 3 O A6CE E1CE 5 C P5EA 2002071700045 20020717 00045 EA 2002 7 17 ASOA02197S 1 20020328 A 5720 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 858AS 7417 DURING HANGAR MAINTENANCE IN MCN, THE RIGHT WING FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT AILERON INBOARD CLOSURE RIB IAW SRM 51-00. (M) 2 L 7 2 4F RT A21EA 2002071700046 20020717 00046 NM 2002 7 17 AUS20020549 1 20020606 A 4920 ENGINE BOEING 737 737* NM GE CFM56 CFM567B24 NE APU CONTAMINATED W C ABORTED TAKEOFF B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 AU S 556 (AUS) APU LOAD COMPRESSOR PLENUM AND APU BLEED CONTROL VALVE PLUMBING CONTAMINATED WITH OIL. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002071700047 20020717 00047 SO 2002 7 17 ASOA02200 1 20020330 A 5712 12026501002 RIB EMB 120 EMB120RT 3260202 SO RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 242AS 120069 DURING HANGAR MAINTENANCE IN TXK, THE RIGHT WING INBOARD FLAP INBOARD TRACK SUPPORT RIB WAS FOUND TO BE CRACKED. MAINTE NANCE INSTALLED A TEMPORARY REPAIR. (M) 2 L 7 2 4T RT A31SO 2002071700048 20020717 00048 EA 2002 7 17 ASOA02201 1 20020331 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA K NONE O OTHER TX TAXI/GRND HDL 1 SO 11 832AS 9665 7243 WHILE SITTING AT THE GATE IN ATL, THE CAPTAINS WINDSHIELD SHATTERED FOR UNKNOWN REASONS. MAINTENANCE REMOVED AND REPLAC ED THE CAPTAINS CRACKED WINDSHIELD. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002071700049 20020717 00049 NE 2002 7 17 AUS20020550 2 20020602 A 7200 CFM567B24 ENGINE BOEING 737 737800* NM GE CFM56 CFM567B24 NE NR 2 MALFUNCTIONED W C ABORTED TAKEOFF E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AU S 68 (AUS) NR 2 ENGINE POWER LOSS. LIMITED INFORMATION PROVIDED. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002071700050 20020717 00050 SO 2002 7 17 ASOA02202 1 20020309 A 5712 12026501002 RIB EMB 120 EMB120RT 3260202 SO RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 232AS 120036 DURING A HANGAR INSPECTION IN TXK, THE RIGHT INBOARD FLAP SUPPORT RIB WAS FOUND TO BE CRACKED. MAINTENANCE INSTALLED A TEMPORARY REPAIR IAW ASA EO120-57-0122. THIS EO REF SST-3404/00 AND SRM 57-20-07. (M) 2 L 7 2 4T RT A31SO 2002071700051 20020717 00051 NM 2002 7 17 AUS20020551 1 20020608 A 2913 DRIVE SHAFT BOEING 737 737* NM GE CFM56 CFM567B24 NE HYDRAULIC PUMP SHEARED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AU S 910 (AUS) SYSTEM A' ENGINE DRIVEN HYDRAULIC PUMP DRIVE SHAFT SHEARED. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002071700052 20020717 00052 2002 7 17 AUS20020553 4 20020606 A 2565 20131AQF1 BATTERY BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL ESCAPE SLIDE FAULTY W K NONE L NO TEST IN INSP/MAINT 1 AU S (AUS) LT AND RT SIDE ESCAPE SLIDE SQUIB BATTERY PACKS FAULTY. 2 L 7 2 4F 4 F RT A1NM E23EA 2002071700053 20020717 00053 EU 2002 7 17 AUS20020555 1 20020606 A 2450 S2653007 CIRCUIT BREAKER BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE AC POWER SHORTED W O OTHER H B ELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 AU S (AUS) CABIN LOUVRE FAN THREE PHASE CIRCUIT BREAKER INTERNAL SHORT CIRCUIT. CB OVERHEATED AND BURNED WIRES HA014A, HA015B AND HA016C. AC2 BUS BAR B MODULE SUFFERED HEAT DAMAGE. 2 H 7 4 4F 4 F A49EU E6NE 2002071700054 20020717 00054 EU 2002 7 17 AUS20020557 1 20020515 A 7603 CABLE BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502R5 41580 NE POWER LEVER FOULED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 4 ENGINE THROTTLE CABLE CAUGHT AROUND ELECTRICAL CONNECTOR LOCATED IN CABIN ROOF AREA AT SEAT ROW 2/3. 2 H 7 4 4F 4 F RT A49EU E6NE 2002071700055 20020717 00055 SO 2002 7 17 ASOA02203 1 20020322 A 5712 12026501002 RIB EMB 120 EMB120RT 3260202 SO RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 230AS 120032 DURING HANGAR MAINTENANCE IN TXK, THE RIGHT INBOARD FLAP INBOARD FIXED TRACK SUPPORT WAS CRACKED. MAINTENANCE INSTALLED A TEMPORARY REPAIR TO THE FLAP TRACK SUPPORT RIB IAW ASA EO120-57-0123. THIS EO REFERENCES SST-3404/00 AND SRM 57-20-0 7. (M) 2 L 7 2 4T RT A31SO 2002071700056 20020717 00056 2002 7 17 AUS20020559 4 20020611 A 2397 WIRE MOONEY M20 M20J 5870219 SW LYC O360 IO360A3B6 41514 EA MCAULY 2D34C B2D34C214 GL COMMUNICATIONS CHAFED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) BURNING SMELL IN AIRCRAFT. INVESTIGATION COULD FIND NO CAUSE OF THE SMELL BUT FOUND THE AUDIO PANEL CIRCUIT BREAKE R (3A) POPPED AND TWO WIRES LOCATED BEHIND THE INSTRUMENT PANEL RUBBING ON ARADIO RACK. A BROKEN EXHAUST STUB WAS ALSO F OUND. 1 L 7 1 3O 3 O 2A3 1E10 5 C P7EA 2002071700057 20020717 00057 EA 2002 7 17 AUS20020562 2 20020602 A 7322 SHAFT PIPER PA28 PA28161 7102803 SO LYC O320 O320D3G 41508 EA SNSNCH 74D 74DM EA CARBURETOR BINDING W O OTHER F FLT CONT AFFECTED LD LANDING 1 AU S 3 (AUS) CARBURETOR THROTTLE SHAFT BINDING. SUSPECT CAUSED BY ICING OFTHE CARBURETOR. COCKPIT CONTROL AND THROTTLE SHAFT BE NT. 1 L 7 1 3O 3 O 2A13 E274 5 N P88614 2002071700058 20020717 00058 EU 2002 7 17 AUS20020566 1 20020319 A 2432 23531 BATTERY FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU MAIN OVERTEMP W O OTHER H M J ELECT. POWER LOSS-50 PC OVER TEMP WARNING INDICATION DE DESCENT 1 AU S 190 (AUS) MAIN BATTERY OVERTEMPERATURE. 2 L 7 2 4F 4 F RT A20EU E2EU 2002071700059 20020717 00059 EU 2002 7 17 AUS20020567 1 20020407 A 2432 23531 BATTERY FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU AFT MAIN OVERTEMP W O OTHER H M J ELECT. POWER LOSS-50 PC OVER TEMP WARNING INDICATION NR NOT REPORTED 1 AU S 388 D1433 (AUS) AFT MAIN BATTERY OVERTEMPERATURE. 2 L 7 2 4F 4 F RT A20EU E2EU 2002071700060 20020717 00060 EU 2002 7 17 AUS20020568 1 20020407 A 2432 23531 BATTERY FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU MAIN OVERTEMP W O OTHER H M J ELECT. POWER LOSS-50 PC OVER TEMP WARNING INDICATION CR CRUISE 1 AU S 190 G1184 (AUS) BATTERY OVERTEMPERATURE. 2 L 7 2 4F 4 F RT A20EU E2EU 2002071700061 20020717 00061 EU 2002 7 17 AUS20020570 1 20020423 A 2432 23531 BATTERY FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU MAIN OVERTEMP W O OTHER H M J ELECT. POWER LOSS-50 PC OVER TEMP WARNING INDICATION NR NOT REPORTED 1 AU S 95 A01060 (AUS) MAIN BATTERY OVERTEMPERATURE. 2 L 7 2 4F 4 F RT A20EU E2EU 2002071700062 20020717 00062 EU 2002 7 17 AUS20020576 1 20020225 A 2150 A/C PACK FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU NR 2 FAILED W O OTHER O OTHER CL CLIMB 1 AU S (AUS) NR 2 AIR CONDITIONING PACK FAILED. INVESTIGATION COULD FIND NO FAULT. 2 L 7 2 4F 4 F RT A20EU E2EU 2002071700063 20020717 00063 EA 2002 7 17 ASOA02204 1 20020402 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 886AS 7531 DURING GROUND INSPECTION IN ATL, THE RIGHT EXTERNAL EMERGENCY LIGHT IN THE SECOND POSITION WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002071700064 20020717 00064 WP 2002 7 17 AUS20020577 2 20020604 A 7261 PUMP CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP ENGINE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 AU S (AUS) LT ENGINE TORQUE FLUCTUATIONS. METAL CONTAMINATION OF OIL FILTER AND CHIP DETECTOR. SUSPECT CAUSED BY FAILURE OF O IL SCAVENGE PUMP. 1 L 7 2 3T 4 T RT A28CE E4WE 2002071700065 20020717 00065 SO 2002 7 17 ASOA02205 1 20020403 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 267AS 28249 120198 DURING GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THAT WHEN HER EMERGENCY LIGHT SWITCH WAS IN THE CLOSED PO SITION THE EMERGENCY LIGHT CIRCUIT BREAKER WOULD POP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY I N THE NR 2 POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002071700066 20020717 00066 NM 2002 7 17 AUS20020581 1 20020608 A 4990 OIL SYSTEM BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU APU OVERTEMP W O OTHER K M J FLUID LOSS OVER TEMP WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) APU SHUTDOWN DUE TO HIGH OIL TEMPERATURE. 2 L 7 2 4F 4 F RT A16WE E21EU 2002071700067 20020717 00067 NM 2002 7 17 AUS20020582 1 20020610 A 2520 SEAT BOEING 737 737800* NM CABIN LOOSE W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) SEAT 7 LT ROW LOOSE IN TRACK. 2 L 7 2 4F RT A16WE 2002071700068 20020717 00068 EU 2002 7 17 AUS20020584 1 20020306 A 5753 SKIN AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE TE FLAP DEBONDED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT INBOARD TRAILING EDGE FLAP DISBONDED. 2 L 7 2 4F RT A35EU E24NE 2002071700069 20020717 00069 EU 2002 7 17 AUS20020585 2 20020306 A 7230 RB18355515 BLADE FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU COMPRESSOR DAMAGED W A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 AU S (AUS) NR 1 ENGINE HPC BLADE TRAILING EDGE DAMAGED. 2 L 7 2 4F 4 F RT A20EU E2EU 2002071700070 20020717 00070 EU 2002 7 17 AUS20020591 1 20020613 A 2420 BUSS BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502R5 41580 NE AC GENERATION FAILED W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 AU S (AUS) NR 2 AC BUS FAILED. THE FOLLOWING COMPONENTS WERE REPLACED:- 1. NR 4 GENERATOR CONTROL UNIT 2. GENERATOR LINE CONT ACTOR 4XB33. NR 4 ENGINE GENERATOR AND CSD 2 H 7 4 4F 4 F RT A49EU E6NE 2002071700071 20020717 00071 EU 2002 7 17 ASOA02206 1 20020404 A 3350 3012000 BATTERY PACK AEROSP ATR72 ATR72 EU CABIN DISCHARGED A ASOA K NONE O OTHER CR CRUISE 1 SO 11 641AS 387 DURING A HANGAR INSPECTION IN MCN, THE FLIGHT ATTENDANT REPORTED THAT THE EMERGENCY LIGHT ABOVE HER SEAT FLICKERS INTERM ITTENTLY DURING FLIGHT. THE PASSENGER DOOR EMERGENCY LIGHT WAS ALSO REPORTED INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE FLICKERING BULB FROM THE CEILING EMERGENCY LIGHT ASSEMBLY. MAINTENANCE ALSO REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IN THE 62 WL POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2002071700072 20020717 00072 EU 2002 7 17 AUS20020593 1 20020613 A 1430 FASTENER BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE RT WING FAILED W D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 AU S (AUS) RT WING TIP FAIRING CAMLOC FASTENER FAILED AND MIGRATED REARWARDSAND LODGED IN THE OUTBOARD AILERON HINGE CAUSING THE AILERON TO JAM. FOD. 2 H 7 4 4F 4 F A49EU E6NE 2002071700073 20020717 00073 NM 2002 7 17 AUS20020594 1 20020612 A 4920 ENGINE BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL APU FAILED W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S (AUS) APU FAILED TO START. REPLACING THE STARTER FAILED TO FIX THEPROBLEM. 2 L 7 2 4F 4 F RT A1NM E23EA 2002071700074 20020717 00074 2002 7 17 AUS20020595 4 20020612 A 3421 INDICATOR BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU ATTITUDE GYRO FAILED W A UNSCHED LANDING O OTHER CR CRUISE 1 AU S (AUS) LT ELECTRONIC ATTITUDE DEVIATION INDICATOR (EADI) SOCKET AND PLUG FOR PIN NR 7 BLACKENED AND CORRODED. 2 L 7 2 4F 4 F RT A16WE E21EU 2002071700075 20020717 00075 NM 2002 7 17 AUS20020597 1 20020615 A 2780 7321856002 VALVE BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL LE SLAT FAULTY W C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 AU S (AUS) OUTBOARD LEADING EDGE SLAT CONTROL VALVE FAULTY. 2 L 7 2 4F 4 F RT A1NM E23EA 2002071700076 20020717 00076 EA 2002 7 17 ASOA02207 1 20020407 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 840AS 7290 DURING HANGAR INSPECTION IN MCN, THE CEILING EMERGENCY LIGHT AT ROW 10 WAS INOPERATIVE. MAINTENANCE RESET A LOOSE BULB IN THE CEILING EMERGENCY LIGHT ASSEMBLY AT ROW 10. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002071700077 20020717 00077 NM 2002 7 17 AUS20020598 1 20020612 A 4920 ENGINE BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU APU FAILED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) APU AUTO SHUTDOWN. LIMITED INFORMATION PROVIDED. 2 L 7 2 4F 4 F RT A16WE E21EU 2002071700078 20020717 00078 EA 2002 7 17 ASOA02208 1 20020407 A 3350 487190 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 884AS 7513 DURING GROUND INSPECTION IN ATL, THE FIRST STRIP OF ORANGE EMERGENCY FLOOR LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REATTACHED A LOOSE CONNECTOR TO THE FLOOR LIGHTING. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002071700079 20020717 00079 NM 2002 7 17 AUS20020599 1 20020614 A 2421 AM739515B IDG BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL AC GENERATOR FAILED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) LT INTEGRATED DRIVE GENERATOR (IDG) FAILED. 2 L 7 2 4F 4 F RT A1NM E23EA 2002071700080 20020717 00080 NM 2002 7 17 AUS20020601 1 20020614 A 4930 BACR13CG2A RELAY BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL APU ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) APU FUEL VALVE RELAY FAILED. 2 L 7 2 4F 4 F RT A1NM E23EA 2002071700081 20020717 00081 NM 2002 7 17 AUS20020602 1 20020617 A 2597 WIRE BOEING 747 747438 NM CALL LIGHT DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) READING AND ATTENDANT CALL LIGHT WIRING DAMAGED IN AREA LOCATED BEHIND 34HJK OVERHEAD LOCKER. CIRCUIT BREAKER P414 -11F TRIPPED. 2 L 7 4 4F RT A20WE 2002071700082 20020717 00082 NM 2002 7 17 AUS20020603 1 20020618 A 4920 ENGINE BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL APU INOPERATIVE W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S (AUS) APU INOPERATIVE. LIMITED INFORMATION PROVIDED. 2 L 7 2 4F 4 F RT A1NM E23EA 2002071700083 20020717 00083 NE 2002 7 17 AUS20020605 2 20020622 A 7321 FMU603MK2 FMU BOEING 747 747438 NM RROYCE RB211 RB211524* NE FUEL CONTROL LEAKING W O OTHER E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) NR 1 ENGINE FUEL METERING UNIT (FMU) LEAKING. 2 L 7 4 4F 4 F RT A20WE E12EU 2002071700084 20020717 00084 NM 2002 7 17 AUS20020606 1 20020618 A 5230 PUSHROD BOEING 747 747238B 1384828 NM RROYCE RB211 RB211524D419 54555 NE CARGO DOOR FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FORWARD CARGO DOOR FAILED TO OPEN. A LOUD NOISE WAS HEARD AND SEVERAL PUSHRODS HAD SHEARED. 2 L 7 4 4F 4 F A20WE E12EU 2002071700085 20020717 00085 CE 2002 7 17 AUS20020609 1 20020415 A 3233 1053840001 ACTUATOR BEECH 76 76 1153005 CE NLG LEAKING W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AU S 6120 (AUS) NLG ACTUATOR LEAKING. SWIVEL SEAL O-RINGS WORN. 1 L 7 2 3O A29CE 2002071700086 20020717 00086 NM 2002 7 17 BJNA020402 1 20020405 A 3230 LANDING GEAR BOEING 737 737282 13844AT NM MLG MALFUNCTIONED A BJNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 11 789TM 23046 WHEN LANDING GEAR HANDLE IS RAISED IN FLIGHT, RED LEFT GEAR LIGHT REMAINS ILLUMINATED. WHEN GEAR HANDLE IS POSITIONED T O OFF GREEN LEFT GEAR LIGHT ILLUMINATES AND LEFT MAIN EXTENDS. WHEN HANDLE IS PLACED IN DOWN POSITION ALL GREEN GEAR LI GHTS ILLUMINATE AND ALL GEAR ARE DOWN AND LOCKED. ACCOMPLISHED LUBE OF ALL LANDING GEAR AND ASSOCIATED LINKAGES PER MM 12-21. ACCOMPLISHED SEVERAL GEAR RETRACTIONS AND FREE-FALL OPERATIONS OPS CHECK OK, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002071700087 20020717 00087 NM 2002 7 17 BJNA020403 1 20020406 A 3350 1000679 LIGHT BOEING 737 737282 13844AT NM COCKPIT INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 FOUND COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY PER BMM 33-51-101, GROUND CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2002071700088 20020717 00088 NM 2002 7 17 BJNA020404 1 20020406 A 3350 6104789 POWER SUPPLY BOEING 737 737282 13844AT NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 L1 AND R1 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY FORWARD CARGO COMPARTMENT PER BMM 33-51- 71, CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2002071700089 20020717 00089 NM 2002 7 17 BJNA020405 1 20020407 A 3230 65448106 ACTUATOR BOEING 737 737282 13844AT NM LT MLG FAILED A BJNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 11 789TM 23046 LEFT MAIN LANDING GEAR RED LIGHT REMAINS ON AFTER GEAR IS RAISED AND WHEN GEAR HANDLE IS IN OFF POSITION, LEFT MAIN GEAR FALLS TO THE DOWN POSITION. REMOVED AND REPLACED LEFT MAIN LANDING GEAR UPLOCK ACTUATOR, PER BMM 32-32-41. PERFORMED MAIN LANDING GEAR EXTENSION AND RETRACTION TEST PER BMM 32-32-0. PERFORMED MANUAL EXTENSION TEST PER BMM 32-34-0. (M) 2 L 7 2 4F RT A16WE 2002071700090 20020717 00090 NM 2002 7 17 USAABB02039 1 20020329 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 619AU 27198 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002071700091 20020717 00091 NM 2002 7 17 USAABB02040 1 20020329 A 3350 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 632AU 27810 CLT - WITH ATTENDANTS PANEL SWITCH ON, MULTIPLE FLOOR LEVEL EMERGENCY LIGHTS WERE EXTINGUISHED. MAINTENANCE REPLACED AL L OF THE FLOOR LEVEL LIGHT BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002071700092 20020717 00092 NM 2002 7 17 USAABB02041 1 20020303 A 3350 20131A BATTERY BOEING 767 7672B7 1385107 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 656US 26847 PHL - FOUND EMERGENCY FLOOR LIGHTING ON LEFT SIDE, ROWS 8-16 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A1NM 2002071700093 20020717 00093 NM 2002 7 17 USAABB02042 1 20020404 A 2120 ODOR BOEING 757 7572B7 1384964 NM CABIN DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 610AU 27122 BWI - FLT 1800 - PASSENGER AND FLIGHT ATTENDANT NOTED AN ELECTRICAL SMELL IN THE CABIN. CREW CHECKED FOR ABNORMAL READI NGS AND CIRCUIT BREAKER TRIPS. NO PROBLEM WERE FOUND. FLIGHT LANDED AT BWI WITH NO FURTHER INCIDENT. MAINTENANCE INSP ECTED THE AIRCRAFT CABIN AND COULD FIND NO DISCREPANCIES. (M) 2 L 7 2 4F RT A2NM 2002071700094 20020717 00094 NM 2002 7 17 USAABB02043 1 20020406 A 2530 2510000704 OVEN BOEING 757 757225 1384959 NM GALLEY DIRTY A USAA F ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 EA 19 601AU 10344 22193 CLT - FLT 94 - EN ROUTE, A FLIGHT ATTENDANT USED A HALON EXTINGUISHER TO PUT OUT A FIRE IN THE FORWARD RIGHT OVEN. MAIN TENANCE FOUND CHARRED FOOD REMAINS IN THE OVEN AND REPLACED THE OVEN. (M) 2 L 7 2 4F RT A2NM 2002071700095 20020717 00095 WP 2002 7 17 USAAD02017 1 20020329 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 823US 49142 IND - SEVERAL LOW LEVEL EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2002071700096 20020717 00096 NM 2002 7 17 AUS20020613 1 20020619 A 5523 6591700816 BEARING BOEING 737 73733A 1384673 NM CFMINT CFM56 CFM563B1US GL LT & RT ELEVATOR WORN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT AND RT ELEVATOR TAB BEARINGS WORN BEYOND LIMITS. FOUND DURING INSPECTION IAW SB B737-55A 1070. 2 L 7 2 4F 4 F RT A16WE E2GL 2002071700099 20020717 00099 NM 2002 7 17 AUS20020614 1 20020621 A 4950 69386261 DUCT BOEING 737 73733A 1384673 NM CFMINT CFM56 CFM563B1US GL APU BLEED AIR DAMAGED W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S (AUS) BLEED AIR DUCT CORRODED AND HAS A HOLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002071700100 20020717 00100 NM 2002 7 17 AUS20020615 1 20020613 A 3230 BACH8A0GNN0250T HOSE BOEING 737 73733A 1384673 NM CFMINT CFM56 CFM563B1US GL LT MLG FAILED W D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 AU S 24545 (AUS) LT MAIN LANDING GEAR RAM DOWN HOSE FAILED ADJACENT TO THE END FITTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2002071700102 20020717 00102 EU 2002 7 17 SIMA200218102 1 20020628 A 5500 S55171202202 SPAR AEROSP ATR42 ATR42300 8680920 EU STABILIZER CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 DURING MBV-1 INSPECTION, RIGHT HORIZONTAL STABILIZER AFT SPAR HAS AREA OF CORROSION. C/A: REPAIRED CORROSION IAW EO. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2002071900049 20020719 00049 NM 2002 7 19 F3LA200200191 1 20020705 A 5320 ANGLE BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR ANGLE INBD OF R1 GUTTER AT BS 336, RBL 54. FABRICATED AND INST ALLED REPLACEMENT SUPPORT ANGLES PER BOEING DRAWING 65C15677 AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 2002071700103 20020717 00103 NM 2002 7 17 AUS20020616 1 20020625 A 3242 S160T400510 BOLT BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL BRAKE LOOSE W K NONE O OTHER IN INSP/MAINT 1 AU S 6703 (AUS) NR 2 BRAKE ASSEMBLY TIE BOLTS LOOSE. 2 L 7 2 4F 4 F RT A1NM E23EA 2002071700104 20020717 00104 NM 2002 7 17 AUS20020617 1 20020625 A 2434 727810C GENERATOR BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL DC SYSTEM FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S 1560 1944 (AUS) APU GENERATOR FAULTY. LIMITED INFORMATION PROVIDED. 2 L 7 2 4F 4 F RT A1NM E23EA 2002071700105 20020717 00105 NM 2002 7 17 AUS20020620 1 20020430 A 2720 SPRING BOEING 737 737800* NM RUDDER CONTROL BROKEN W O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 AU S (AUS) RUDDER FEEL AND CENTERING MECHANISM INNER SPRING BROKEN. 2 L 7 2 4F RT A16WE 2002071700106 20020717 00106 CE 2002 7 17 CA020426002 1 20020425 A 1400 PIN BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA CONTROL CABLE CUT W K NONE O OTHER IN INSP/MAINT 1 CA 12598 (CAN) WHILE TRYING TO ADJUST THE CABLE TENSION DURING AN OPS IT WAS NOTED THAT THE TURN BARREL WAS VERY STIFF TO TURN AN D THE LOCK PIN SLOT WAS FULL OF CUTTINGS. AT DISASSEMBLY TO INVESTIGATE THE TURN BARREL IT WAS FOUND THAT THE TURN BARR EL HAD BEEN STRIPPED AND THE THREADED END OF THE CABLE, WHEN VIEWED AGAINST A LIGHT BACKGROUND, APPEARED TO HAVE A DOUBL E CUT THREAD. 1 L 7 2 3T 4 T A14CE E4EA 2002071700107 20020717 00107 NE 2002 7 17 A4J2002F00000 2 20020524 A 7260 B6002 CHIP DETECTOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LT ENGINE WORN A A4JA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 35 11FQ 49759 DEPARTED UNDER NORMAL CONDITIONS. LEVELING OFF AT 28,000 FEET, CRUISE ALTITUDE, LOSS OF LT ENGINE OIL QUANTITY AND LOW OIL PRESSURE WAS OBSERVED BY THE FLIGHT CREW. THE NR 1 ENG WAS SHUT DOWN. FLIGHT WAS DIVERTED AND LANDED WITH NO FURTH ER INCIDENTS. DURING POST FLIGHT INSP AND IN PROCESS OF TROUBLESHOOTING CAUSE OF THE NR 1 ENGINES LOSS OF OIL QUANTITY AND LOW OIL PRESSURE MAINTENANCE FOUND THE ACCESSORY GEAR BOX CHIP DETECTOR LYING IN THE BOTTOM OF THE NR 1 ENGINE LOWER COWLING. A CLOSE INSPECTION OF THE CHIP DETECTOR HOUSING REVEALED EXCESSIVE WEAR WITH PART OF THE HOUSING RETAINER BRO KEN AWAY. THE CHIP DETECTOR ASSEMBLY WAS REPLACED WITH A NEW ASSEMBLY IAW MM. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E9NE 2002071700109 20020717 00109 CE 2002 7 17 GUU2002F00018 1 20020607 A 1430 EWB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 17534 13911 UE141 AT REDUCED INTERVAL, FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRE D RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM. 2 L 7 2 4T RT A24CE 2002071700110 20020717 00110 CE 2002 7 17 GUU2002F00019 1 20020608 A 1430 EWB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 69548 12924 UE193 AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM. 2 L 7 2 4T RT A24CE 2002071700111 20020717 00111 CE 2002 7 17 GUU2002F00020 1 20020605 A 1430 EWB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81556 10956 UE239 AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLT REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLT IAW MFG MM. 2 L 7 2 4T RT A24CE 2002071700112 20020717 00112 CE 2002 7 17 GUU2002F00021 1 20020606 A 1430 EWB225 BOLT BEECH 1900 1900D 1154162 CE VERTICAL STAB LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87552 12150 UE216 AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM. 2 L 7 2 4T RT A24CE 2002071700113 20020717 00113 SO 2002 7 17 SIMA200218101 1 20020624 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 DURING AN IMBV INSPECTION FOUND CORROSION ON GALLEY CENTER FLOOR BEAM. REMOVED CORRODED GALLEY CENTER BEAM. INSTALLED NEW FLOOR BEAM IAW SRM AND STANDARD SRM PRACTICES. 2 L 7 2 4T RT T00011AT 2002071700114 20020717 00114 NE 2002 7 17 CA020517003 2 20020515 A 7313 3038495X FUEL NOZZLE PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL ENGINE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) EXCHANGE FUEL NOZZLE SET WAS ORDERED TO PERFORM ROUTINE MAINTENANCE. SET RECEIVED FROM P&W CANADA ACCESSORIES SERV ICES, LONGUEUIL. PACKING BOX APPEARED NORMAL. WHEN IDIVIDUAL NOZZLE PACKINGS WERE OPENED 10 OUT OF 14 HAD VISIBLE CORROS ION. SOME WERE RUSTY RED AND OTHERS HAD A WHITE POWDER TYPE CORROSION. COMPLETE SET WAS REJECTED BEFORE INSTALLATION. P& W WAS CONTACTED & EMAIL PICTURES WERE FORWARDED TO THEM. REPLACEMENT SET OF NOZZLES WAS ORDERED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002071700115 20020717 00115 NE 2002 7 17 GUU2002F00022 2 20020607 A 7250 3044700 POWER UNIT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE CONTAMINATED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 49543 12715 UE181 114375 AT SCHEDULED ROUTINE INSPECTION (A CHECK) THE RIGHT ENGINE WAS DETERMINED TO HAVE DISCOLORED (BLACK OIL). C/A CHANGED T HE ENGINE OIL AND OIL FILTER. PLACED ENGINE ON OIL WATCH. REPLACED THE RIGHT POWER SECTION MODULE AND ROUTED FAILED UN IT FOR FURTHER ANALYSIS AND REPAIR. 2 L 7 2 4T 4 T RT A24CE E26NE 2002071700116 20020717 00116 CE 2002 7 17 GUU2002F00023 1 20020616 A 2121 1143800287 BLOWER BEECH 1900 1900D 1154162 CE CABIN SHORTED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 17 53545 UE185 AFTER AIRCRAFT POWER IS TURNED ON SMOKE IN AIRCRAFT. INSPECTED AIRCRAFT. REMOVED AND REPLACED AFT VENT BLOWER. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2002071700117 20020717 00117 NE 2002 7 17 MEX2002190 2 20020618 A 7321 76960615 FUEL CONTROL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED W ASMF O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SW 23 162PL 49765 AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF LOW ACCELERATION IN ENGINE NUMBER 2. CAPTAIN REPORTED THE FOLLOWING IN FORMATION N2 44 PERCENT FF 12. AIRCRAFT WAS SENT TO THE HANGAR. THE FOLLOWING ITEMS WERE REPLACED: POWER SUPPLY (IAW MM), FCU, FUEL FLOW TX (IAW MM), CONTROL ASSEMBLY BLED VALVE AND PRBC VALVE. OPERATIONAL TESTS WERE PERFORMED IAW MM. 2 L 7 2 4F 4 F RT A6WE E9NE 2002071700118 20020717 00118 SO 2002 7 17 SIMA200217709 1 20020624 A 2700 3621001007 HYDRAULIC SYSTEM EMB 145 EMB145 3260210 SO TAIL INOPERATIVE A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SW 21 609AE 145069 IN CRUISE FLIGHT MAIN PITCH TRIM WAS ENGAGING BY ITSELF CREW DROP OFF AUTO PILOT AND IT WAS STILL DOING IT. CALLED MOC AND HAD THE CREW PULL THE NO 1 TRIM C/B STILL DID NOT HELP. CREW ELECTED TO DIVERT TO GET THE AIRCRAFT ON THE GROUND AS SOON AS POSSIBLE. C/A: MAINTENANCE REMOVED AND REPLACED THE HSCU IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002071700119 20020717 00119 2002 7 17 MEX2002198 4 20020626 A 3418 10000165101 TRANSDUCER DOUG MD88 MD88 3023688 NM STALL WARNING FAILED W ASMF O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 23 169PL 6043 53175 AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF AUTO SLAT FAIL LIGHT AND TRI COMPUTER OUT OF SERVICE. SLAT SYSTEM RECYC LE WAS PERFORMED IAW MM TESTS, OK. IN RELATION TO TRI COMPUTER WAS RESTED ON BOTH DFGC, TESTS OK IAW MM. DURING TRANSI T IN MEX WERE CHANGED THE R2-3, R2-6 TRANSMITTER ANGLE ATTACK AND F15 BREAKER OF IRU NR 1. TESTS TO THE NAVIGATION SYST EM WAS PERFORMED IAW MM AND STP TEST WAS PERFORMED IAW MM. DURING OVERNIGHT SERVICE WAS CHECKED AUTO SLAT AND STALL IAW MM ALL CORRECT. 2 L 7 2 4F RT A6WE 2002071700120 20020717 00120 NM 2002 7 17 MEX2002199 1 20020626 A 2910 147425 SHUTOFF VALVE DOUG MD88 MD88 3023688 NM HYD SYSTEM FAILED W ASMF O OTHER O OTHER NR NOT REPORTED 1 SW 23 168PL 6428 53174 CAPTAIN REPORT LOW PRESSURE ON RIGHT HYDRAULIC SYSTEM. WHEN AUXILIARY PUMP WAS IN USE BREAKER POPS OUT AND INDICATES 25 00 PSI. THE SPOILER SHUTOFF VALVE WAS CHANGED AND SYSTEM DEPRESSURIZATION WAS CHECKED IAW MM. 2 L 7 2 4F RT A6WE 2002071700121 20020717 00121 NM 2002 7 17 MEX2002205 1 20020603 A 2740 575600015 SENSOR DOUG MD80 MD83 3023681 NM HORIZ STAB FAILED W ASMF A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 23 946AS 49658 AIRCRAFT RETURN TO FLIGHT AS A CONSEQUENCE OF STABILIZERS MOVEMENT ALARM, STABILIZER MOVEMENT SENSOR WAS REPLACED, TESTS WERE PERFORMED IAW MM. 2 L 7 2 4F RT 2002071700122 20020717 00122 WP 2002 7 17 MEX2002206 1 20020603 A 2720 SB0927030187 CONTROL UNIT DOUG DC9 DC982 3022082 WP RUDDER MALFUNCTIONED W ASMF A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 SW 23 1003X 48067 AIRCRAFT RETURN TO FLIGHT AS A CONSEQUENCE OF RUDDER CONTROL PROBLEMS. DURING CHECK WAS DETECTED A 4 INCH OF MISALIGNME NT. AIRCRAFT WAS SENT TO THE HANGAR. RUDDER PACKAGE WAS CHANGED, PEDALS MECHANISM WAS LUBRICATED AND ACTUATOR ASSY RUD DER POWER CONTROL WAS CHANGED, TESTS WERE PERFORMED IAW MM. 2 L 7 2 4F A6WE 2002071900051 20020719 00051 NM 2002 7 19 F3LA200200193 1 20020705 A 5320 SILL BOEING 737 7372P6 1C84609 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED R1 DOOR LOWER SILL WEB CRACKED AT FWD DRAIN HOLE. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002071700123 20020717 00123 NE 2002 7 17 Q2S2002F00002 2 20020621 A 7520 9057M84G03 DUCT BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE RN 2 ENGINE BLOWN A Q2SA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 744SA 22363 AIR TURNBACK, ON TAKEOFF, AT 2500 FEET MSL, WITH TAKEOFF POWER AT 113.0 N1, NR 2 ENGINE FIRE LIGHT AND BELL CAME ON. NA CELLE INDICATOR BOTH A AND B READ 6.5 SHUTDOWN ENGINE IAW QRH. DUMPED 18,700 LBS OF FUEL. NO EVIDENCE OF FIRE FOUND ON INSPECTION OF ENGINE. FOUND BLOWN 14TH STAGE DUCT ON LEFT SIDE OF ENGINE. REMOVED AND REPLACED NR 2 ENGINE BLEED AIR DUCT IAW AMM. 2 L 7 4 4F 4 F A20WE E23EA 2002071900052 20020719 00052 NM 2002 7 19 F3LA200200194 1 20020705 A 5320 STRAP BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON STRAP AT BS 857, RBL 18. REPLACED STRAP PER SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F RT A16WE 2002071700124 20020717 00124 NM 2002 7 17 RYN2002F00036 1 20020610 A 5320 WEB BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT (C) CHECK, FOUND WEB WITH EXFOLIATED CORROSION, FROM STATION 1110 TO 1130, RBL 54.0. 2 L 7 3 4F A3WE 2002071700125 20020717 00125 NM 2002 7 17 SCNA02001 1 20020614 A 3350 LIGHT BOEING 737 7378Q8 13844BX NM EXTERIOR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 804SY 30689 DURING WALKAROUND FOUND EMERGENCY LIGHT FOR L2 EXTERIOR DOOR LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT ASSEMBLY AT DO OR L2. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2002071700126 20020717 00126 SO 2002 7 17 SIMA200216006 1 20020609 A 5300 FRAME EMB 145 EMB145LR 3260212 SO STR15R,FRM9 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 DENT ON FRAME 9 BELOW STRINGER 15R .005 X .7 X 1.0. SUP, DENT ACCEPTED AS IS IAW MFG GST. 2 L 7 2 4T RT T00011AT 2002071700127 20020717 00127 NM 2002 7 17 SCNA02002 1 20020623 A 3350 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21616 EMERGENCY FLOOR PATH LIGHT AT SEAT 13 INOPERATIVE RELAMPED, OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2002071700128 20020717 00128 NM 2002 7 17 TSA2002F00000 1 20020619 A 4997 WIRE HARNESS BOEING 737 7372X6C 1384552 NM APU WORN A TSAA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 817AL 23292 ENROUTE , THE APU SHUTDOWN DUE TO AN OVERSPEED. THE AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE RESTARTED THE APU AND CONDUCTED AN OPERATIONAL CHECK OF THE UNIT. THE OPERATIONAL CHECK WAS GOOD AND AN OVERWEIGHT LANDING INSPEC TION WAS COMPLETED. THE AIRCRAFT WAS RELEASED AND RESTRICTED TO SERVICE DUE TO HF INTERFERENCE WITH THE APU OPERATION. INSPECTED THE APU WIRING AND REPAIRED A BROKEN/WORN HARNESS AT THE APU TACH GENERATOR. GROUND OPERATIONAL CHECK WAS GO OD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A16WE 2002071700129 20020717 00129 SO 2002 7 17 SIMA200216005 1 20020609 A 5300 FRAME EMB 145 EMB145LR 3260212 SO FRM18,STR20L DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 DENT FORWARD OF FRAME 18 BELOW STRINGER 20L. .013 X 2.0 X 1.7 (SUP) DENT ACCEPTED AS IS IAW MFG GST. 2 L 7 2 4T RT T00011AT 2002071700130 20020717 00130 NE 2002 7 17 TSA2002F00001 2 20020611 A 7261 777889 BEARING BOEING 737 737209 13844AE NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE BROKEN A TSAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 13 827AL 37466 23913 CLIMBING THROUGH 15,000 FEET THE NUMBER 2 ENGINE OIL PRESSURE DROPPED TO 20 PSI AND OIL TEMPERATURE CLIMBED TO 130 DEGRE ES. THE NUMBER 2 ENGINE WAS SHUTDOWN IAW THE QRH. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING. REMOVED AND RE PLACED THE NR 2 ACCESSORY GEARBOX ASSEMBLY. FOUND THE OIL PUMP GEARSHAFT BEARING BROKEN. LEAK AND OPERATIONAL CHECKS G OOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002071700131 20020717 00131 SO 2002 7 17 SIMA200216004 1 20020609 A 5200 DOOR EMB 145 EMB145LR 3260212 SO PASSENGER DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 DENT IN PASSENGER DOOR ABOVE WINDOW, .006 X 1.0 X 1.1. (SUP) DENT ACCEPTED AS IS IAW MFG GST. 2 L 7 2 4T RT T00011AT 2002071700132 20020717 00132 NM 2002 7 17 TSAA0251145 1 20020520 A 5330 6546550 SKIN BOEING 737 7372M6C 1384708 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 REPAIRED FUSELAGE SKIN CRACK AT BS 727B, S-17. CUT OUT DAMAGED AREA AND PERFORMED HFEC INSPECTION AROUND CUT OUT, PERFO RMED INSURANCE CUT OF .040 INCH, FABRICATED AND INSTALLED REPAIR DOUBLER AND TEAR STRAP. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002071700133 20020717 00133 SO 2002 7 17 SIMA200216001 1 20020609 A 5300 FRAME EMB 145 EMB145LR 3260212 SO FRM19,STR13L DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 DENT AFT FRAME 19 BELOW STRINGER 13L. .006 X 2.5 X 1.1. (SUP) DENT ACCEPTED AS IS IAW MFG GST. 2 L 7 2 4T RT T00011AT 2002071700134 20020717 00134 NM 2002 7 17 SWAA021542 1 20020712 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 713SW 27847 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 9. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002071700135 20020717 00135 2002 7 17 SWAA021545 4 20020713 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED GIRT BAR CABLE PER MM. 2 L 7 2 4F RT A16WE 2002071700136 20020717 00136 2002 7 17 SWAA021548 4 20020712 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 713SW 27847 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002071700137 20020717 00137 NM 2002 7 17 SWAA021552 1 20020712 A 2560 P2070001 BATTERY BOEING 737 7373G7 1384595 NM CABIN WEAK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED A1 CHECK, FOUND BOTH AFT EMERGENCY FLASHLIGHTS HAVE WEAK BATTERIES. REMOVED AND REPLACED FLASHLIGHT BA TTERIES PER MM. 2 L 7 2 4F RT A16WE 2002071700138 20020717 00138 NM 2002 7 17 SWAA021553 1 20020712 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) 2 ABOVE LAP AT STR 10L, BS'S 500 AND 500B PLUS 5. REPAIRE D SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071700139 20020717 00139 NM 2002 7 17 SWAA021555 1 20020714 A 2720 65C254106 FEEL UNIT BOEING 737 7377H4 1384404 NM TAIL COMP BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED SERVICE CHECK, FOUND RUDDER FEEL AND CENTERING UNIT INNER SPRING BROKEN. REMOVED AND REPLACED RUDDER F EEL AND CENTERING UNIT PER MM. 2 L 7 2 4F RT A16WE 2002071700140 20020717 00140 NM 2002 7 17 SWAA021556 1 20020714 A 5320 6547951 STRAP BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED 1/4D CHECK, FOUND FAIL/SAFE STRAP CRACKED AT BS 794, BETWEEN STR 19R AND 27R. REPAIRED STRAP PER SRM. 2 L 7 2 4F RT A16WE 2002071700141 20020717 00141 NM 2002 7 17 SWAA021560 1 20020711 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 DURING SCHEDULED BC2 CHECK, SWA SI 11075-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHING ON NR 1 HINGE ATTACH POINT PER MM. 2 L 7 2 4F RT A16WE 2002071700142 20020717 00142 NM 2002 7 17 SWAA021561 1 20020711 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 DURING SCHEDULED BC2 CHECK, SWA SI 11038-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR T AB HARDWARE AND BUSHINGS AT HINGES NR 1, 3 AND 4 ATTACH POINTS PER MM. 2 L 7 2 4F RT A16WE 2002071700143 20020717 00143 NM 2002 7 17 SWAA021483 1 20020704 A 3350 101073 LENS BOEING 737 7372T4 1384492 NM FWD ENTRY DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F A16WE 2002071700144 20020717 00144 NM 2002 7 17 SWAA021484 1 20020705 A 5752 654645519 TAB BOEING 737 7373A4 1384585 NM LT AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED PM CHECK, FOUND LT AILERON TAB DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LT AILERON TAB PER M M. 2 L 7 2 4F RT A16WE 2002071700145 20020717 00145 NM 2002 7 17 SWAA021485 1 20020705 A 5754 6546423261 SLAT BOEING 737 7372H4 138448C NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 080SW 22675 DURING SCHEDULED RON, FOUND NR 3 LT L/E SLAT DELAMINATED ON UPPER INBD SURFACE. REMOVED AND REPLACED NR 3 LT L/E SLAT P ER MM. 2 L 7 2 4F A16WE 2002071700146 20020717 00146 NM 2002 7 17 SWAA021487 1 20020705 A 5513 183A8100 TAB BOEING 737 7377H4 1384404 NM BOTH ELEVATORS VIBRATION A SWAA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 29 742SW 29278 LOW FREQUENCY AIRFRAME VIBRATION OCCURRED FOR ABOUT 2 MINUTES IN-FLIGHT. ACCOMPLISHED POST LCO (LIMIT CYCLE OSCILLATION ) INSPECTION, REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TABS PER MM. 2 L 7 2 4F RT A16WE 2002071700147 20020717 00147 NM 2002 7 17 SWAA021490 1 20020705 A 7710 JT8D9 ENGINE BOEING 737 7372H4 138448C NM JT8 JT8D9 52048 NE RT WING POWER LOSS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 095SW 23054 687735 AIR TURN BACK, AT ROTATION, NR 2 ENGINE LOST POWER. EPR INDICATION DROPPED FROM 1.89 TO APPROX 1.75. REMOVED AND REPLA CED NR 2 ENGINE PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2002071700148 20020717 00148 NM 2002 7 17 SWAA021492 1 20020706 A 3350 101073 LENS BOEING 737 737317 138447P NM FWD ENTRY DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT L ENS PER MM. 2 L 7 2 4F RT A16WE 2002071700149 20020717 00149 NM 2002 7 17 SWAA021493 1 20020706 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071700150 20020717 00150 2002 7 17 SWAA021496 4 20020706 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM FWD SVC DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002071700151 20020717 00151 NM 2002 7 17 SWAA021456 1 20020703 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM FWD SVC DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED RON, FOUND FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2002071700152 20020717 00152 NM 2002 7 17 SWAA021458 1 20020703 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED AT ROW'S NR 4, 10, 14, 16, 17, 22 AND 23. REMOVED AND REPLACED CO VERS PER MM. 2 L 7 2 4F RT A16WE 2002071700153 20020717 00153 2002 7 17 SWAA021459 4 20020703 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F A16WE 2002071700154 20020717 00154 2002 7 17 SWAA021460 4 20020703 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F A16WE 2002071700155 20020717 00155 NM 2002 7 17 SWAA021462 1 20020704 A 3350 101114 COVER BOEING 737 7377H4 1384404 NM FWD SVC DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 749SW 29801 FWD SVC DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2002071700156 20020717 00156 NM 2002 7 17 SWAA021469 1 20020703 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 759, BELOW STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071700157 20020717 00157 NM 2002 7 17 SWAA021470 1 20020704 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071700158 20020717 00158 NM 2002 7 17 SWAA021471 1 20020702 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 820, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071700159 20020717 00159 NM 2002 7 17 SWAA021472 1 20020703 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071700160 20020717 00160 NM 2002 7 17 SWAA021473 1 20020702 A 5330 6545768 SKIN BOEING 737 7372K6 1364440 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 129SW 22340 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, BETWEEN STR'S 28L AND 28R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071700161 20020717 00161 NM 2002 7 17 SWAA021474 1 20020704 A 5311 6546546 FRAME BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, WL 190.1. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2002071700162 20020717 00162 NM 2002 7 17 SWAA021475 1 20020630 A 5330 589357 SKIN BOEING 737 7373H4 1384600 NM WINDOW POST CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED C3 CHECK, FOUND NR 1 COCKPIT WINDOW POST SKIN CRACKED AT UPPER LT CORNER. REPAIRED WINDOW POST SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2002071700163 20020717 00163 NM 2002 7 17 SWAA021476 1 20020704 A 5330 6545768 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND SKIN CRACKED AT FWD ENTRY DOOR LOWER AFT CORNER CUT OUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002071700164 20020717 00164 NM 2002 7 17 SWAA021477 1 20020704 A 5310 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L AND 14L. REMOVED AND REPLACED SHEAR TIE PE R SRM. 2 L 7 2 4F RT A16WE 2002071700165 20020717 00165 NM 2002 7 17 SWAA021479 1 20020704 A 5311 6558280 FRAME BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13R AND BETWEEN STR 15L AND 16L. REPAIRED FRAM E PER SRM. 2 L 7 2 4F A16WE 2002071700166 20020717 00166 NM 2002 7 17 SWAA021480 1 20020704 A 5311 65465441 FRAME BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STR 2R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2002071700167 20020717 00167 NM 2002 7 17 SWAA021444 1 20020702 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 738CB 27870 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002071700168 20020717 00168 NM 2002 7 17 SWAA021445 1 20020702 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 752SW 29804 DURING SCHEDULED A1 CHECK, FOUND EEPLS COVERS BROKEN AT ROW NR 1 AND 11. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002071700169 20020717 00169 NM 2002 7 17 SWAA021449 1 20020702 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT WINDOW BELT CUTOUT ON RT WINDOW NR 10. REPAIRED SKIN PER SWA S I. 2 L 7 2 4F RT A16WE 2002071700170 20020717 00170 NM 2002 7 17 SWAA021450 1 20020702 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, ABOVE STR 25R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002071700171 20020717 00171 NM 2002 7 17 SWAA021451 1 20020701 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4R, BS 727D AND 727E. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071700172 20020717 00172 NM 2002 7 17 SWAA021452 1 20020701 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071700173 20020717 00173 NM 2002 7 17 SWAA021454 1 20020701 A 5330 6545768 SKIN BOEING 737 7372K6 1364440 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 129SW 22340 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, BETWEEN STR 29L AND 29R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071700174 20020717 00174 NM 2002 7 17 SWAA021455 1 20020702 A 5313 BAC1498 STRINGER BOEING 737 7372K6 1364440 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 129SW 22340 DURING SCHEDULED A2 CHECK, FOUND STRINGER CORRODED AT BS 360, STR 26L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2002071700175 20020717 00175 NM 2002 7 17 SWAA021437 1 20020701 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, ABOVE STR 13R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071700176 20020717 00176 NM 2002 7 17 SWAA021438 1 20020701 A 5313 65C27314 TIE CLIP BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STR TIE CLIP PER SRM. 2 L 7 2 4F A16WE 2002071700177 20020717 00177 2002 7 17 SWAA021441 4 20020629 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM BOTH AFT DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED C3 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDE'S P ER MM. 2 L 7 2 4F RT A16WE 2002071700178 20020717 00178 SO 2002 7 17 SIMA200215902 1 20020608 A 5200 DOOR EMB 145 EMB145LR 3260212 SO CARGO DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 CARGO DOOR NEAR MIDDLE HAS 3 DENTS 1).006 X 1.3 X 1.0 2).009 X 1.3 X 1.8 3) .003 X .3 X .5. (SUP) THREE DENTS F OUND TO BE WITHIN MFG SRM LIMITS. 2 L 7 2 4T RT T00011AT 2002071700179 20020717 00179 NM 2002 7 17 TSAA0253144 1 20020601 A 5311 65C33722 FRAME BOEING 737 7372M6C 1384708 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 REPAIRED RIGHT OUTBOARD CHORD AT BS727, S18A DUE TO FASTENER HOLE CRACK. UTILIZED HIGH FREQUENCY EDDY CURRENT AND ULTRA SONIC METHODS. REMOVED AND INSTALLED CHORD ASSEMBLY, REASSEMBLED AND INSTALLED ALL COMPONENTS AND FASTENERS, APPLIED BM S 5-95, TYPE I SEALANT TO ALL FAYING SURFACES, CLEAN AND TREATED ALL BARE SURFACES IAW ECO. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4F RT A16WE 2002071700180 20020717 00180 NM 2002 7 17 TSAA0253146 1 20020425 A 5730 6545455 SKIN BOEING 737 7372Y5 1384554 NM RT WING WORN A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 24031 RIGHT WING LEADING EDGE LOWER SKIN AT FSS 413 WORN BEYOND LIMITS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER , SPLICE PLATE AND DOUBLER. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4U RT A16WE 2002071700181 20020717 00181 NM 2002 7 17 CA020528010 1 20020513 A 5310 STRUCTURE BOEING 767 7673Y0 NM PWA 4060 PW4060 52119 NE CARGO BAY DAMAGED W F ACTIVATE FIRE EXT. A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA (CAN) ON FINAL APPROACH AFT CARGO FIRE AND WARNING INDICATED. QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT, FIRE EXTIN GUISHING SYSTEM ACTIVATED AND EMERGENCY DECLARED. EMERGENCY CREWS FOUND SMOKE PRESENT WITH FIRE HAVING BEEN PREVIOUSLY E XTINGUISHED. AIRCRAFT PARKED JUST SHORT OF GATE AND PASSENGERS DISEMBARKED VIA AIRSTAIRS. AFT CARGO FUSELAGE FRAME STA 1395, RBL 0 TO 36 FOUND BADLY WARPED AND HEAT DAMAGED ALSO LOWER SIDE OF CARGO FLOOR PANEL AT SAME LOCATION FOUND SCORC HED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002071700182 20020717 00182 SO 2002 7 17 SWIA200210885 1 20020517 A 2730 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO ELEVATOR FAILED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 581SW 120349 ON TAKEOFF, WITH TRIM SET AT 37 PERCENT, RECEIVED A TRIM AURAL WARNING. PERFORMED A STATIC RUNUP WITH TRIM SET AT 30 PE RCENT AND ALSO GOT A TRIM AURAL WARNING. REPLACED BOTH ELEVATOR TRIM PROXIMITY SENSORS WITH SERVICEABLE UNITS IAW EMB 1 20 MM 27-32-05. OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002071700183 20020717 00183 NM 2002 7 17 QXEA0200957 1 20020713 A 2710 SERVO DHAV DHC8 DHC8202 2809007 NM ZONE 500 FOULED A QXEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 09 354PH 498 PDX - AIRCRAFT RETURNED TO FIELD WHEN A SLIGHT BINDING WAS NOTED IN THE AILERON. MAINTENANCE INSPECTED THE AIRCRAFT AND REPOSITIONED THE SAFETY WIRE PIGTAILS ON THE AILERON SERVO. OPERATIONAL CHECK WAS PERFORMED AND WAS GOOD. THE AIRCRAFT W AS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002071700184 20020717 00184 GL 2002 7 17 CA020607004 2 20020529 A 7323 1056058312 SPRING BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL RT ENGINE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A OPS NR 1 ON RT ENGINE, THE SPRING P/N 105-60583.12 WAS FOUND BROKEN.SPRING WAS REPLACED WITH A NEW SPRING P/N 105-60583.12. 1 G 7 2 3U 3 U H3EU E4CE 2002071900053 20020719 00053 NM 2002 7 19 F3LA200200195 1 20020705 A 5544 STRUCTURE BOEING 737 7372P6 1C84609 NM RUDDER CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON RUDDER BULLNOSE BY NR 3 HINGE. REPLACED CORRODED AREA OF RUDDER BULL NOSE PER SRM 51-40-02 AND BOEING DRAWING 65-53740. 2 L 7 2 4F RT A16WE 2002071700186 20020717 00186 NM 2002 7 17 C1HA200282014 1 20020629 A 3340 COVER BOEING 727 7272S7 138407Z NM LT MLG BROKEN A C1HA O OTHER O OTHER NR NOT REPORTED 1 GL 15 682CA 22019 LT MAIN GEAR LIGHT COVER BROKEN. RESECURED LIGHT COVER AS REQUIRED. 2 L 7 3 4F A3WE 2002071700187 20020717 00187 NM 2002 7 17 C1HA200288013 1 20020616 A 2797 WIRE HARNESS BOEING 727 7272S7 138407Z NM L/E SLAT DAMAGED A C1HA K NONE N FALSE WARNING UK UNKNOWN 1 GL 15 688CA 22344 FLAP DID NOT AGREE WITH INDICATOR FLAP NR 1 LEADING EDGE SLAT WAS UP BUT INDICATED DOWN. FOUND WIRE BUNDLE BETWEEN NR 3 SLAT ACTUATOR & OUTBOARD SLAT TRACK ARCED THROUGH MULTIPLE WIRES. REPAIRED WIRES IN AREA USING STD PRACTICES IN MM 20- 11-31. 2 L 7 3 4F A3WE 2002071700188 20020717 00188 NM 2002 7 17 C1HA200292006 1 20020616 A 2611 SMOKE DETECTOR BOEING 727 727212 138407G NM LAVATORY INOPERATIVE A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 292AS 21458 LEFT AFT LAV SMOKE DETECTION INOP. INSPECTED AND RESCHEDULED PLACARD INSTALLED AND LAV LOCKED OUT. 2 L 7 3 4F A3WE 2002071700189 20020717 00189 WP 2002 7 17 ABXA020022 1 20020516 A 5315 9922397501 FLOORBEAM DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 FS 937, RBL 22, HAD LEVEL I CORROSION ON THE CABIN FLOORBEAM HORIZONTAL FLANGE. REPAIRED THE FLOORBEAM IAW DC-9 SRM 53-0 5. 2 L 7 2 4F A6WE 2002071700190 20020717 00190 WP 2002 7 17 ABXA020027 1 20020520 A 5315 99115468 FLOORBEAM DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 CORROSION ON AFT FACE OF TRANSVERSE FLOOR BEAM AT WEB STATION 996, BL 0, LBL 36. 2 L 7 2 4F A6WE 2002071700191 20020717 00191 WP 2002 7 17 ABXA020030 1 20020625 A 5330 5779934521 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 CORROSION OUT OF LIMITS ON FUSELAGE SKIN, STATION 280, LONGERON 35 LEFT AND STATION 335, LONGERON 35 RIGHT. INSTALLED RE PAIR DOUBLER IAW REA D853-44492. 2 L 7 4 4F 4A25 2002071700192 20020717 00192 WP 2002 7 17 ABXA020031 1 20020625 A 5330 5779942515 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 SKIN CORROSION OUT OF LIMITS JUST AFT OF GYRO COMPARTMENT. INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-0. 2 L 7 4 4F 4A25 2002071700193 20020717 00193 CE 2002 7 17 GLBA2002106 1 20020712 A 5600 10138402518 WINDSHIELD BEECH 1900 1900D 1154162 CE COPILOT CRACKED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 247GL UE247 COPILOT WINDSHIELD CRACKED, REPLACED WINDSHIELD 2 L 7 2 4T RT A24CE 2002071700194 20020717 00194 WP 2002 7 17 ABXA020032 1 20020625 A 5320 3643758501 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT WHEEL WELL AREA, STATION 920, FITTING WAS CRACKED AT CENTER KEEL. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-21 AND 51-1-20. 2 L 7 4 4F 4A25 2002071700195 20020717 00195 WP 2002 7 17 ABXA020033 1 20020708 A 3350 60030451 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 953AX 47608 MAINTENANCE FOUND EMERGENCY EXIT LIGHTS DIM. REPLACED BOTH BATTERIES FOR EMERGENCY EXIT LIGHT AND CHECKED BATTERY PACK FOR CHARGING. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2002071700196 20020717 00196 WP 2002 7 17 ABXA020034 1 20020708 A 2510 831061405 CUSHION DOUG DC9 DC932 3022066 WP COCKPIT DEFECTIVE A ABXA K NONE O OTHER CR CRUISE 1 GL 23 980AX 47176 FIRST OFFICER'S SEAT CUSHION DID NOT FIT OR ATTACH TO SEAT FRAME PROPERLY. SOMETIMES RESTRICTED AFT MOVEMENT OF CONTROL COLUMN. REPLACED FIRST OFFICER'S SEAT CUSHION AS REQUIRED IAW DC-9 MM. 2 L 7 2 4F A6WE 2002071700197 20020717 00197 WP 2002 7 17 ABXA020037 1 20020606 A 5712 99193295 RIB DOUG DC9 DC932 3022066 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 901AX 47381 CRACK INDICATION ON AFT END OF LEADING EDGE NOSE RIB, INBOARD OF NR 10 SLAT TRACK. REPAIRED NOSE RIB IAW REA D957-44307 -MR. 2 L 7 2 4F A6WE 2002071700198 20020717 00198 NM 2002 7 17 02071501 1 20020715 A 2913 3508805 PUMP BOEING 757 757200 1384950 NM RROYCE RB211 RB211535E4 54555 NE FAILED A N8TA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 WP 19 512NA 26962 30823 Left Engine E.D.P. failed in Flight. Aircraft returned to base, an uneventful landing was accomplished. Removed and Rep laced #1 Engine Engine Driven Pump, Operational Check good, as per M/M. 2 L 7 2 4F 4 F RT A2NM E12EU 2002071700199 20020717 00199 WP 2002 7 17 ABXA020038 1 20020606 A 5712 99193303 RIB DOUG DC9 DC932 3022066 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 901AX 47381 4 EACH LEADING EDGE NOSE RIBS BETWEEN TRACKS 10 AND 11, HAD CRACK INDICATIONS AT AFT EDGES. REPAIRED NOSE RIBS AT STATI ONS XRS 466-473-479-491 IAW REA D957-44307-MR. 2 L 7 2 4F A6WE 2002071700200 20020717 00200 WP 2002 7 17 ABXA020042 1 20020618 A 5313 592480225 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 LONGERON 17, STATION 389, WAS CRACKED APPROXIMATELY 3/4 INCH. REPAIRED LONGERON 17 IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2002071700201 20020717 00201 WP 2002 7 17 ABXA020043 1 20020618 A 5313 592480225 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 LONGERON 17, STATION 408, WAS CRACKED APPROXIMATELY .5-.75 INCH. REPAIRED LONGERON 17 IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2002071700202 20020717 00202 WP 2002 7 17 ABXA020044 1 20020619 A 5315 992362913 FLOORBEAM DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 FLOORBEAM SUPPORT CRACKED AT LOWER END, FS 617 AND LONGERON 23L. REPAIRED FLOOR BEAM SUPPORT IAW DC-9 SRM 51-30-2 AND 5 1-30-5. 2 L 7 2 4F A6WE 2002071700203 20020717 00203 WP 2002 7 17 ABXA020045 1 20020619 A 5312 991224381 BULKHEAD DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 CRACK IN LEFT BULKHEAD WEB, FS 1041 AT LONGERON 17L, INBOARD END. REPAIRED BULKHEAD IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002071700204 20020717 00204 WP 2002 7 17 ABXA020046 1 20020709 A 3260 WARNING SYSTEM DOUG DC9 DC931 3022065 WP COCKPIT MALFUNCTIONED A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 945AX 47551 UPON SELECTING GEAR DOWN, NOSE GEAR UNSAFE LIGHT ILLUMINATED AND NOSE GEAR GREEN LIGHT DID NOT COME ON. GEAR WARNING HO RN SOUNDED. RECYCLED GEAR, ALL INDICATIONS NORMAL. OPS CHECKED GOOD IAW DC-9 MM 32-60. 2 L 7 2 4F A6WE 2002071700205 20020717 00205 WP 2002 7 17 ABXA020058 1 20020713 A 3260 WARNING SYSTEM DOUG DC8 DC863F 302198F WP COCKPIT MALFUNCTIONED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 816AX 46093 GEAR UNSAFE LIGHT REMAINED ILLUMINATED ON RETRACTION. LEFT GEAR DOWN INDICATED NOT LATCHED. RECYCLED ONCE, NO HELP. R UNNING ABNORMAL TO UPLATCH CHECK POSITION LIGHT EXTINGUISHED. 2 L 7 4 4F 4A25 2002071700206 20020717 00206 NM 2002 7 17 AWXA200200541 1 20020610 A 5320 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 MCN - MAJOR REPAIR - DURING C-16 INSPECTION A CRACK WAS FOUND AT BS 380 STR 26R. MAINTENANCE FORMED A REPLACEMENT STRING ER CLIP, AND INSTALLED IAW BOEING DRAWING NR 69-35352, SRM 51-40-05 AND SRM 51-20-01 PAGE 10, MM 51-20-00 PAGE 1, SRM 51 -40-02 PAGES 10 AND 11. 2 L 7 2 4F RT A16WE 2002071700208 20020717 00208 NM 2002 7 17 AWXA200200542 1 20020609 A 5320 693535215 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 MCN - MAJOR REPAIR - DURING C-16 INSPECTION A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 907 STR 11R. MAINTENANCE REMOV ED AND REPLACED STRINGER TIE CLIP AT BS 907 STR 11R IAW B737-300 SRM 51-40-02 PAGE 38 AND SRM B737-300 SRM 51-40-02 PAGE S 10,11,AND 13. 2 L 7 2 4F RT A16WE 2002111800082 20021118 00082 NM 2002 11 18 C7WA200200006 1 20020713 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CANNING A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN BS 469 TO 458 BETWEEN STRINGER 21R AND 23R OIL CANNED. REPAIRED WITH DOUBLER AND FILLER IAW SRM 53-30-4 FIG 4. (M) 2 L 7 3 4F A3WE 2002111800083 20021118 00083 NM 2002 11 18 C7WA200200007 1 20020713 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND EXT FUSELAGE BETWEEN BS 440 AND BS 450 AT STRINGER 23R SKIN BULGED. REPAIRED STRINGER 2 3R FROM BS 440 TO BS 473 DUE TO LEVEL 2 CORROSION IAW SRM 53-10-3 FIG 1. FUSELAGE SKIN FOUND SATISFACTORY. (M) 2 L 7 3 4F A3WE 2002111800085 20021118 00085 NM 2002 11 18 C7WA200200009 1 20020713 A 5312 BULKHEAD BOEING 727 727232 1384082 NM FUSELAGE CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND AFT AFT PRESSURE BULKHEAD BS 1183 WITH 1.5 INCH CRACK AT WL 188.31 LBL 13. REPAIRED BS 1183 WEB WITH DOUBLERS LBL 9.5 TO LBL 22 BETWEEN WL 181.5 AND WL 193.5 IAW COOPESA EO COO-2-53-345-02. (M) 2 L 7 3 4F A3WE 2002071700209 20020717 00209 NM 2002 7 17 CALA0200352 1 20020619 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69348 23586 INSPECTION FOUND KEEL BEAM LT LOWER O/B CHORD CORRODED AT STA 727. REPAIRED IAW ECRA 5311-01127. 2 L 7 2 4F RT A16WE 2002071700210 20020717 00210 NM 2002 7 17 CALA0200357 1 20020619 A 3397 WIRE BOEING 737 737524 1384721 NM CABIN OUT OF POSITION A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 27610 27323 THE WHITE EMERGENCY PATH LIGHT AT SEAT 18C WAS FOUND INOPERATIVE DUE TO A PULLED WIRE. THE LIGHT ASSEMBLY WAS REMOVED AN D REPLACED IAW MM 33-51-81. 2 L 7 2 4F RT A16WE 2002071700211 20020717 00211 NM 2002 7 17 CALA0200363 1 20020624 A 5210 PAN BOEING 737 7373T0 1384582 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17345 23583 INSPECTION FOUND A 0.375 INCH CRACK IN L1 DOOR PAN SKIN AT NR 5 FROM BOTTOM STOP PIN ACCESS HOLE. A REPAIR WAS INSTALLE D IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 2002071700212 20020717 00212 NM 2002 7 17 CALA0200364 1 20020624 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17345 23583 INSPECTION FOUND CARGO FLOOR SUPPORT CORRODED AT STA 847, LBL 2.5 AND RBL 2.5. THE CORRODED AREAS WERE CUT OUT AND REPA IRS WERE INSTALLED IAW ECRA 5320-01603. 2 L 7 2 4F RT A16WE 2002071700213 20020717 00213 NM 2002 7 17 CALA0200367 1 20020626 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17345 23583 INSPECTION FOUND CARGO FLOOR SUPPORTS CORRODED AT STA 772, RBL 2.5 AND LBL 2.5. REPAIRED FLOOR SUPPORTS IAW ECRA 5320-0 1603 AND SRM 53-60-53. 2 L 7 2 4F RT A16WE 2002071700214 20020717 00214 NM 2002 7 17 CALA0200368 1 20020626 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17345 23583 INSPECTION FOUND CARGO FLOOR SUPPORT CORRODED AT STA 772, LBL 7.5 AND LBL 12. REPAIRED FLOOR SUPPORT IAW ECRA 5320-01603 AND SRM 53-60-53. 2 L 7 2 4F RT A16WE 2002071700215 20020717 00215 WP 2002 7 17 CALA0200371 1 20020628 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A PUNCTURE IN THE FRAME WEB OF AFT ACCESSORY COMPARTMENT AT RT SIDE, BS 1463, S17R. THE DAMAGE WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-4 AND 51-70-4, FIGURE 2, SHEET 2. 2 L 7 2 4F A6WE 2002071700216 20020717 00216 WP 2002 7 17 CALA0200372 1 20020628 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND SUB FLOOR PUNCTURED AT FS 196, LBL 26. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4 AND 51-3 0-2. 2 L 7 2 4F A6WE 2002071700217 20020717 00217 WP 2002 7 17 CALA0200373 1 20020628 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A CRACK AT FASTENER HOLE OF FORWARD ENTRY SUB FLOOR AT FS 218, LBL 20. THE CRACK WAS LESS THAN 1/8 INC H LONG. A DOUBLER WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2002082000159 20020820 00159 EA 2002 8 20 COMA0260426 1 20020715 A 7110 COWLING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 15000 7117 RIGHT ENGINE FIXED CORE COWL IS CRACKED IN AFT CHANNEL APPROX 1/5 INCH. REPAIRED CRACK BY STOP DRILLING AND INSTALLING A DOUBLER IAW SHORTS CMM 71-13-01 REPAIR SRS 065 AND REO 601R-71-13-1989. 2 L 7 2 4F RT A21EA 2002071700218 20020717 00218 NM 2002 7 17 CALA0200376 1 20020630 A 5414 SKIN BOEING 737 7373T0 1384582 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17345 23583 INSPECTION FOUND 1/2 INCH CRACK IN NR 1 PYLON ACCESS PANEL CUTOUT FOR PANEL 5727L. THE CRACK WAS STOP DRILLED AND A DOU BLER WAS INSTALLED IAW ECRA 5430-01230. 2 L 7 2 4F RT A16WE 2002071700219 20020717 00219 WP 2002 7 17 CALA0200377 1 20020701 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND FLOOR WEB CORRODED NEAR FORWARD ENTRY AREA AT FS 186-194. THE DAMAGED AREA WAS CUT OUT AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 4 AND 51-30-2. 2 L 7 2 4F A6WE 2002071700220 20020717 00220 GL 2002 7 17 CA020612006 2 20020531 A 7230 23031922 SPUR ADAPTER BELL 206 206L 1181522 SW ALLSN 25OC 250C20R GL COMPRESSOR SPALLED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ENGINE CHIP LIGHT FOUND METAL PARTICLES ON BOTH CHIP PLUGS. 2 1/2 BEARING AND INNER RACE ON THE SPUR ADAPTER FOUND SPALLED. 1 G 7 1 3U 3 U H2SW E4CE 2002071700221 20020717 00221 WP 2002 7 17 CA020612007 2 20020316 A 7230 30703177 STATOR ISRAEL 1125 1125 NM GARRTT TFE731 TFE7313A 01518 WP COMPRESSOR SEPARATED W A UNSCHED LANDING D E J INFLIGHT SEPARATION VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKEOFF AT APPROXIMATELY 3,000 FT ASL EXPERIENCED A VIBRATION AND NOISE FROM THE RT ENGINE. THE POWER LEVER WAS RETARDED TO IDLE AND ALL VIBRATION AND NOISE DISAPPEARED, AND ENGINE INDICATIONS WHERE WITHIN LIMITS AT THIS TIME. R EQUESTED VECTORS BACK TO CYUL FOR AN ILS AND FOR EMERGENCY EQUIPMENT TO STANDBY. THE LANDING WAS NORMAL, AND THE RT ENGI NE WAS SHUTDOWN ON THE GROUND. 2 L 7 2 4F 4 F RT A16NM E6WE 2002071700223 20020717 00223 EA 2002 7 17 CA020617004 1 20020527 A 5320 COVER DHAV DHC6 DHC6200 2802620 EA PWA PT6 PT6A20 52043 EA COCKPIT FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CA (CAN) THE PLASTIC COVER UNDER THE PILOT SEAT THAT PROTECTS THE AILERON PULLEY AND CABLE WAS DAMAGED. THE AIRCRAFT HIT SO ME TURBULENCE AND A SMALL ROCK CAME OFF THE FLOOR AND DOWN INTO THE PULLEY BETWEEN THE CABLE AND PULLEY JAMMING THE CONT ROL. AIRCRAFT MADE A SAFE LANDING WITH AILERON CONTROLS JAMMED IN NEUTRAL POSITION. MAINTENANCE MADE UP AN ALUMINIUM COE R TO REPLACE THE PLASTIC ONE. AIRCRAFT RETURNED TO SERVICE. 1 H 7 2 3T 3 T RT A9EA E4EA 2002071700224 20020717 00224 WP 2002 7 17 CA020617010 1 20020615 A 7810 CON80535 EXHAUST STACK GRUMAN TS2 TS2ACALFORST 3951102 WP WRIGHT R1820 982C9HE2 67020 EA HAMSTD 43D 43D51 NE PORT ENGINE SEPARATED W A UNSCHED LANDING D J INFLIGHT SEPARATION WARNING INDICATION CL CLIMB 1 CA (CAN) SHORTLY AFTER TAKEOFF THE PORT ENGINE FIRE WARNING LIGHT ILLUMINATED. THE PILOT IMMEDIATELY TURNED AROUND AND LAND ED. AFTER LANDING ON THE ROLL OUT, THE WARNING LIGHT EXTINGUISHED. UPON INVESTIGATION BY THE MAINTENANCE CREW, IT WAS D ISCOVERED THAT AN EXHAUST PIPE HAD BROKEN OFF. THE FIREWALL WAS INSPECTED FOR DAMAGE AND NONE WAS FOUND. THE EXHAUST STA CK WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4R 4 R A25WE E259 6 C P8879 2002071700225 20020717 00225 EA 2002 7 17 COMA0260427 1 20020717 A 5346 WEB CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 959CA 7116 LOWER WEB ON L/H AND R/H ENGINE SUPPORT BEAM AT FS 625.30 FS 640.0 WL 111.09 ARE CRACKED.PERFORMED A MAJOR REPAIR TO CRA CKED ENGINE SUPPORT BEAM LOWER WEB L/H AND R/H FS 625.30 FS 640.0 WL 111.09 I/A/W CRJ REO 601R-53-61-366 REV 2 L 7 2 4F RT A21EA 2002071700226 20020717 00226 EA 2002 7 17 COMA0260428 1 20020715 A 2750 860D10018ABC COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 932CA 10992 7038 FLIGHT 5806 - FLAPS FAIL CAUTION MESSAGE.REPLACED THE FECU 2 L 7 2 4F RT A21EA 2002071700227 20020717 00227 NM 2002 7 17 CA020618001 1 20020612 A 7712 TORQUE SENSOR DHAV DHC8 DHC8301 1386003 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 1 ENGINE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA 26010 26010 (CAN) NR 1 ENGINE UNCOMMANDED AUTOFEATHER AFTER TAKE OFF AT 100 FT. ENGINE WAS THEN SHUT DOWN. INVESTIGATION SUSPECTS FA ILURE OF NR 1 ENGINE TORQUE SENSOR PROBE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002071700228 20020717 00228 NE 2002 7 17 CA020618006 2 20020618 A 7230 COMPRESSOR BEECH B300 B300B350C CE PWA PT6 PT6A60A 52043 NE RT ENGINE SEIZED W E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CA (CAN) IN CRUISE PILOT SAW AND HEARD RT ENGINE FLUCTUATION, POWER BACK THE ENGINE TO FLIGHT IDLE & STILL FLUCTUATING, TOR QUE GOING DOWN, ITT GOING UP, SHUT DOWN ENGINE AND LANDED AT DESTINATION WITHOUT ANY PROBLEM. SENT MECHANIC ON SITE, FOU ND THAT COMPRESSOR SECTION OF ENGINE IS SEIZED , OIL CAME OUT OF THE FRONT PART OF COMPRESSOR AND FROM BLEED AIR VALVE. RESULT IS UNSCHEDULED ENGINE CHANGE. 2 L 7 2 4T 4 T RT A24CE E4EA 2002071700229 20020717 00229 WP 2002 7 17 CALA0200378 1 20020701 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND SUBFLOOR WEB CRACKED AT FS 200 LBL 10 AND FS 200 RBL 10. THE CRACKS WERE 1 INCH LONG. THE CRACKS WERE STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED AT EACH LOCATION IAW SRM 53-01, FIGURE 2, 51-30-2, AND 53-01, FIGURE 4. 2 L 7 2 4F A6WE 2002071700230 20020717 00230 WP 2002 7 17 CALA0200380 1 20020701 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND SUBFLOOR CORRODED AT FS 218, RBL 30. THE CORRODED AREA WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 53-14-1, FIGURE 11. 2 L 7 2 4F A6WE 2002071700231 20020717 00231 WP 2002 7 17 CALA0200381 1 20020701 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND SUBFLOOR UNDER G1 GALLEY DRAIN PAN CORRODED. THE CORRODED AREA WAS REMOVED AND A DOUBLER REPAIR WAS IN STALLED IAW SRM 53-11-1, FIGURE 13 AND 53-01, FIGURE 1. 2 L 7 2 4F A6WE 2002071700233 20020717 00233 NM 2002 7 17 CALA0200383 1 20020701 A 3397 GROUND WIRE BOEING 757 757224 1384958 NM CABIN LOOSE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14107 27297 INSPECTION FOUND EMERGENCY AISLE LIGHTS AT ROWS 15-24 INOPERATIVE. A LOOSE GROUND WIRE WAS FOUND AT GROUND LUG. RESECU RED GROUND WIRE AND OPERATION OF THE EMERGENCY LIGHTS CHECKED GOOD. 2 L 7 2 4F RT A2NM 2002071700234 20020717 00234 WP 2002 7 17 CALA0200385 1 20020702 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT STA 196, LBL 15 TO LBL 44. THE FLOOR SUPPORT WAS REMOVED AND R EPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2002071700235 20020717 00235 WP 2002 7 17 CALA0200386 1 20020702 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND FORWARD ENTRY SUBFLOOR STIFFENER BENT AND CRACKED AT STA 200-218, RBL 30. REMOVED AND REPLACED STIFFEN ER IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2002071700236 20020717 00236 WP 2002 7 17 CALA0200388 1 20020702 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT STA 200, LBL 10 TO LBL 14. THE FLOOR SUPPORT WAS REMOVED AND R EPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2002071700237 20020717 00237 EA 2002 7 17 COMA0260429 1 20020713 A 2750 7805013 LEVER CNDAIR CL600 CL6002B19 1900309 EA INST. PANEL MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 938CA 3376 851 7046 FLIGHT 5694 FLAPS FAIL CAUTION MESSAGE.REPLACED THE FLAP CONTROL LEVER ASSY. 2 L 7 2 4F RT A21EA 2002071700238 20020717 00238 NM 2002 7 17 CALA0200391 1 20020703 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17345 23583 INSPECTION FOUND KEEL BEAM LOWER CHORD I/B FLANGE CORRODED AT S28R AND S28L BETWEEN STA 500D AND 520. REPAIRED IAW ECRA 5311-01128. 2 L 7 2 4F RT A16WE 2002071700239 20020717 00239 WP 2002 7 17 CALA0200394 1 20020710 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77827 49487 INSPECTION FOUND AFT BAGGAGE BIN RT TIE DOWN TRACK CORRODED AT STA 1211-1231. THE TIE DOWN TRACK WAS REMOVED AND REPLAC ED IAW SRM 53-05. 2 L 7 2 4F A6WE 2002071700240 20020717 00240 NM 2002 7 17 CALA0200403 1 20020716 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND LT AFT LAV DIAGONAL FLOOR SUPPORT CORRODED AT SCREW HOLES, BS 986-1006, LBL 14. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002071700241 20020717 00241 EA 2002 7 17 COMA0260430 1 20020713 A 2750 601R930507 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 965CA 4091 7131 FLAPS FAILED CAUTION AT 30 DEGREES.REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2002071700242 20020717 00242 NE 2002 7 17 VNAA0206011 2 20020619 A 7532 311995704 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 07 440JS 14772 4660 3058 DURING CLIMBOUT, THE CREW EXPERIENCED AN UNCOMMANDED REDUCTION IN TORQUE ON THE RIGHT HAND ENGINE FOLLOWED BY AN ENGINE CONTROL UNIT FAIL MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND RESET THE SYSTEM. AGAIN, THE ENGINE CO NTROL UNIT FAILED AND THE CREW DECIDED TO RETURN TO THE FIELD. MAINTENANCE INSPECTED AND REPLACED THE INTERCOMP BLEED V ALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT WAS RELE ASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002071700243 20020717 00243 NE 2002 7 17 MALA020407 2 20020716 A 7220 1F5071F ENGINE BAC 146 AVRO146RJ85A 1500097 EU LF507 LF5071F NE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 501XJ E2208 DURING FLIGHT #3505 CREW REPORTED AT 1,000 FT. THE #4 ENGINE HAD TWO LOUD BANGS AND THE EGT WENT HIGH. INFLIGHT SHUTDOWN . AIR RETURN TO MSP. MAINTENANCE REPLACED #4 ENGINE PN lF507-1F SN/OFF P07877 SN/ON P07854 REF TASK CARD 7100-502 FOR DETAILS. 2 H 7 4 4F 4 F RT A49EU E6NE 2002071700244 20020717 00244 NM 2002 7 17 QXEA0200958 1 20020716 A 7930 800600M01 ACTUATOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 FAILED A QXEA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 NM 09 403QX 2814 2814 4037 BOI - AIRCRAFT RETURNED TO FIELD WHEN THE CREW NOTICED THE NUMBER 2 ENGINE OIL TEMP RISE TO 126 DEGREES CENTIGRADE. MAIN TENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NUMBER 2 ENGINE OIL COOLER AIR OUTLET FLAP ACTUATOR AND THE ENGINE COCKP IT INTERFACE UNIT. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002071700245 20020717 00245 NM 2002 7 17 C1HA200285011 1 20020716 A 3350 900835A BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 685CA 22492 AFT LH EMERGENCY EXTERIOR OVERWING LIGHT INOPREMOVED AND REPLACED BATTERY PACK AS PER MM 33-50-22 OPS CHECK GOOD 2 L 7 3 4F A3WE 2002071700246 20020717 00246 NM 2002 7 17 AWXA200200621 1 20020620 A 5330 654577892 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 1/8" CRACK WAS FOUND ON FUSELAGE EXTERNAL SKIN AND BONDED DOUBLER AT THE R2 D OOR FUSELAGE LOWER HINGE CUTOUT EXTENDING FORWARD BENEATH THE WINDOW BELT DOUBLER BS 951, RBL 66. CRACK CONFIRMED BY HFE C INSPECTION AND 10X VISUAL. MAINTENANCE CUTOUT DAMAGED PART OF SKIN, BONDED DOUBLER, AND BEAR STRAP AT R2 DOOR FUSELAGE LOWER HINGE CUTOUT BS 951, RBL 66. PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER, DOUBLER, A ND TRIPLER, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01, PG. 225-234. 2 L 7 2 4F RT A16WE 2002071700247 20020717 00247 NM 2002 7 17 AWXA200200623 1 20020701 A 5330 65918793 SKIN PANEL BOEING 737 7373G7 1384595 NM BUCKLED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK WRINKLED SKIN WAS FOUND ON THE LOWER KEEL BEAM PANEL FROM BS 663 TO BS 727. MANTE NANCE REMOVED LOWER KEEL BEAM PANEL, FABRICATED NEW KEEL BEAM PANEL AND 3 EACH INNER DOUBLERS, AND INSTALLED REPAIR PART S IAW AWA ER 03-5311-02175-JS1. 2 L 7 2 4F RT A16WE 2002071700248 20020717 00248 NM 2002 7 17 AWXA200200624 1 20020629 A 5311 65458661079 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4" CRACK WAS FOUND ON THE STIFFNER WEB BETWEEN THE L/H AND R/H KEEL BEAMS BS 710, LBL 6 TO RBL 6. MAINTENANCE REMOVED STIFFNER WEB BETWEEN THE L/H AND R/H KEEL BEAMS BS 710, FABRICATED A NEW STIFFN ER WEB, AND INSTALLED REPAIR IAW DWG 65-45866, AND B737-300 SRM 51-40-05, PG. 4 & 5. 2 L 7 2 4F RT A16WE 2002071700249 20020717 00249 NM 2002 7 17 AWXA200200625 1 20020629 A 5311 65458661065 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1" CRACK WAS FOUND ON THE LOWER KEEL BEAM STIFFNER WEB BELOW AUXILLARY HYDRAULI C PUMP BS 710, LBL 6 TO RBL 6. MAINTENANCE REMOVED STIFFNER WEB BS 710, LBL 6 TO RBL 6, FABRICATED A NEW STIFFNER WEB, A ND INSTALLED REPAIR IAW DWG 65-45866, B737-300 SRM 51-40-05, PG. 4 & 5, AND SRM 51-20-01, PG. 10 & 47. 2 L 7 2 4F RT A16WE 2002071700250 20020717 00250 NM 2002 7 17 AWXA200200626 1 20020701 A 5313 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/2" CRACK WAS FOUND ON STRINGER CLIP IN THE L/H AFT CARGO COMPARTMENT BS 807, SRT 25 L/H. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 807 STR25 L/H, FABRICATED A NEW STRINGER CLIP AND INSTALLED REPAIR IAW DWG 69-35352, AND B737-300 SRM 51-40-02, PG. 2-3, 10-11, & 38. 2 L 7 2 4F RT A16WE 2002071700251 20020717 00251 NM 2002 7 17 AWXA200200627 1 20020702 A 5315 7178T6511 SEAT TRACK BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK CORROSION WAS FOUND ON THE SEAT TRACK BETWEEN BS 324 TO 344, RBL 45, WL 208. MAIN TENANCE CUTOUT DAMAGED SECTION OF SEAT TRACK, FABRICATED A NEW SECTION OF SEAT TRACK, A RADIUS FILLER, AND A FILLER. IN STALLED REPAIR PARTS IAW B737-300 SRM 53-00-52, PG. 202-209. 2 L 7 2 4F RT A16WE 2002071700252 20020717 00252 NM 2002 7 17 AWXA200200628 1 20020706 A 5315 6517688131 ANGLE BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK INTERGRANULAR CORROSION WAS FOUND ON THE BOTTON SIDE OF CREASE BEAM (ANGLE) AT NU T PLATE HOLE BS 326, LBL 60, WL 208. MAINTENANCE REMOVED DAMAGED SECTION OF ANGLE AT BS 326, LBL 60. FABRICATED A NEW AN GLE, AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG 3, 4, & 38. 2 L 7 2 4F RT A16WE 2002071800001 20020718 00001 NM 2002 7 18 UPS02238803 1 20020610 A 5330 LAP JOINT BOEING 727 72722C 138400F NM BS465-497 STR19R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI SUSPECT CORROSION AT LAP JOINT BS 490 TO 470 AT S19R/H LFEC INDICATES MATERIAL LOSS 15-20% BS 4 98-465 AT STR 19R.CORROSION REMOVED FROM LAP JOINT AT BS470-480, FOUND WITHIN LIMITS AND LAP CLO SED IAW SRM 51-40-5 AND 51-30-2. AREA BETWEEN BS 485-497 FOUND OUTSI DE LIMITS AND DAMAGE CUT AWAY, REPAIRED IAW UPS EO 5330-0509 APP 8.3 AND UPS EO 727-53-20059 2 L 7 3 4F A3WE 2002071800002 20020718 00002 NM 2002 7 18 UPS02238804 1 20020621 A 5310 STRINGER BOEING 727 72722C 138400F NM BS 460 STR8L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI STR NO8 L/H HAS EVIDENCE OF CRACKING ON ROOT OF INSIDE LOWER FLANGE AT BS 460 REPAIR CARRIED OU T IAW SRM 53-10-3 FIGURE 3. 2 L 7 3 4F A3WE 2002071800003 20020718 00003 NM 2002 7 18 UPS02238809 1 20020614 A 3210 652163716 SUPPORT FITTING BOEING 727 72722C 138400F NM R/HMLG WING DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI R/H MLG WING DOOR ACTUATOR SUPPORT FITTING CRACKED. FITTING REPLACED IAW EO B727-3210-2583 APP D,E,F,G. 2 L 7 3 4F A3WE 2002071800004 20020718 00004 NM 2002 7 18 UPS02238810 1 20020611 A 5310 BUTT JOINT BOEING 727 72722C 138400F NM 1080 S4L TO S6L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI LFEC INSPECTION INDICATES MATERIAL LOSS AT BS 1080 BETWEEN S4L AND 6 L AREA REPAIRED IAW UPS EN GINEERING ORDER B727-5330-1177 APPEDIX 7.BET WEEN STRINGER 5L AND 6L AT BS 1080. BUTT JOINT RESEALED AND FASTENED IAW S RM 51-30-02. 2 L 7 3 4F A3WE 2002071800005 20020718 00005 NM 2002 7 18 UPS02238814 1 20020610 A 5330 SKIN BOEING 727 72722C 138400F NM BS441-521 S1 TO7 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI SUSPECT MATERIAL LOSS ON CROWN SKIN AT BS 500 TO 519 BETWEEN STRINGE R 1 L TO STRINGER 3L SKIN DERIVETED BETWEEN BS441 AND 521 S2L TO 10L IAW SRM 51-10-2, COR ROSION FOUND OUT OF LIMITS, SKIN CUT BETWEEN BS441 BS521 BETWEEN S1L AND S2L AND REMOVED. NEW SKIN SPLICED IN RUNNING BETWEEN BS 441 TO BS 481(MCD CUTOUT) AT STRINGER 7L AND 4 41 TO 521 BETWEEN S1L AND S2 L. IAW UPS AUTHORISATION 727-53-20065 2 L 7 3 4F A3WE 2002071800006 20020718 00006 NM 2002 7 18 ANCF200200014 1 20020713 A 3230 MS288891 VALVE 5940338507 DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE NLG STRUT FAILED W ANCF B EMER. DESCENT N FALSE WARNING CL CLIMB 1 SO 23 190AN SCPI1017 53190 AFTER T/O THE NLG DID NOT GO UP. PROCEDURES CHECKLIST WERE ACCOMPLISHED. AIRCRAFT WAS TURNED BACK TO BOGOTA. AIR VALVE W AS REPLACED. WAS ACCOMPLISHED SERVICE ON SHOCKSTRUT AND PERFORMED RETRACTION TEST IAW AMM 32-30-00 PAG 1. RESULTS SATISF ACTORY. 2 L 7 2 4F 4 F RT E9NE 2002071800007 20020718 00007 EU 2002 7 18 AUS20020512 1 20020525 A 3213 B105M CLIP FOKKER FOKKER FOKKERFVIIB EU JACOBP R755 R755A2M1 35006 SW HAMSTD 2B 2B20 NE MLG FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT MAIN LANDING GEAR OLEO RETAINING CIRCLIP DISLODGED FROM THE CIRCLIP GROOVE ALLOWING THE STRUT TO SEPARATE. AIRC RAFT DAMAGED DURING EMERGENCY LANDING. 1 H 7 2 3R 3 R NC EXPA1H72 TC237 5 C P255 2002071800008 20020718 00008 SW 2002 7 18 CA020619007 1 20020606 A 6310 205040242001 BEARING BELL 205 205A1 1181414 SW LYC T53 T5313A 41549 NE FREEWHEEL UNIT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHEN TURNING FREEWHEEL ROUGHNESS WAS DETECTED, FURTHER INVESTIGATION REEALED A CLICKING NOISE. THE MAIN ROTOR TRAN S. INPUT ADAPTER FREEWHEEL UNIT WAS REMOVED. THE FREEWHEEL UNIT WAS DISASSEMBLED, A BEARING THAT SUPPORTS THE INNER/OUTE R COUPLING WAS DETERMINED TO BE THE CAUSE. 1 G 7 1 4U 4 U H1SW E17EA 2002071800009 20020718 00009 NE 2002 7 18 CA020619008 2 20020524 A 7414 BSM9F MAGNETO DHAV DHC3 DHC3 2800202 EA PWA R1340 R134059 52016 NE ENGINE FAILED W A UNSCHED LANDING D R INFLIGHT SEPARATION PARTIAL RPM/PWR LOSS CR CRUISE 1 CA (CAN) 1) ENGINE BACKFIRING AND HAVING LOSS OF POWER SYMPTOMS MORE PRONOUNCED WHEN ENGINE HOT. 2) DUE TO LOW TIME OF ENGI NE, POOR FUEL MIXTURE WAS MAIN SUSPECT. ENGINE WOULD RUN A LOT BETTER WHEN CARB HEAT APPLIED. 3) PROBLEM SOLVED WHEN BOT H MAGS UPLOAD. SUSPECT FAILURE OF BOTH CAPACITORS IN MAGS. MAGS ARE BEING SENT FOR FURTHER EVALUATION AT FACTORY APPROVE D O/H SHOP. 1 H 7 1 3R 3 R A815 5E2 2002071800010 20020718 00010 NM 2002 7 18 CA020619009 1 20020508 A 2721 682015 SWITCH DHAV DHC8 DHC8* NM PWC 150 PW150A EA RUDDER CONTROL FAILED W O OTHER F FLT CONT AFFECTED CL CLIMB 1 CA 612 (CAN) AFTER TAKE-OFF RUDDER TRIM COULD ONLY BE MOVED TO THE RIGHT REGARDLESS OF THE TRIM SWITCH POSITION. (ENDING UP AT FULL RIGHT DEFLECTION) .AIRCRAFT HAD TO BE FLOWN MANUALLY WITH FULL LT RUDDER. AFTER CB F7 PULLED AND RESET, TRIM FUNCTI ON WAS BACK AGAIN. ROTARY SWITCH REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002071800011 20020718 00011 NM 2002 7 18 CA020619010 1 20020612 A 2820 82830105139 LINE DHAV DHC8 DHC8* NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE FUEL SYSTEM CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING A FIRE EXTINGUISHER WEIGHT CHECK, A FUEL LEAK WAS NOTICED IN THE WING ROOT. APU FUEL TUBE ASSY LT WAS FOUND CHAFING AGAINST THE PNEUMATIC LINE. THE CLAMP HOLDING THE TUBE WAS TIGHTENED TOO MUCH. THIS RESULTED IN A DISTORTION OF THE TUBE CAUSING A CHAFING AGAINST THE PNEUMATIC LINE.THE TUBE ASSY LT WAS REPLACED.AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002071800012 20020718 00012 CE 2002 7 18 CA020619013 1 20020617 A 2612 302158 FIRE DETECTOR BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA RT ENGINE MALFUNCTIONED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 19000 19000 (CAN) AFTER TAKE-OFF, RT ENGINE FIRE ANNUNCIATOR ILLUMINATED, THEN EXTINGUISHED. CREW VIEWED ENGINE FOR ANY SIGNS OF FIR E AND VERIFIED ALL ENGINE PARAMETERS NORMAL. CREW DECIDED TO RETURN TO BASE. MAINTENANCE FOUND RT ENGINE ,FOWARD TOP FIR E DETECTOR FAULTY. REPLACED FIRE DETECTOR, AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4T 4 T A24CE E4EA 2002071800013 20020718 00013 EA 2002 7 18 CA020620002 1 20020605 A 5610 601R330339 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) CREW REPORTED THAT PILOT'S WINDSHIELD CRACKED IN FLIGHT.THE AIRCRAFT WAS ENROUTE AND TURNED BACK TO LAND. MAINT R EPLACED THE WINDSHIELD PER AMM. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002071800014 20020718 00014 CE 2002 7 18 CA020620003 1 20020509 A 2434 ALT9422 ALTERNATOR CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO LEFT FAILED W A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CA (CAN) LT ALTERNATOR FAILED LIGHT CAME ON IN FLIGHT. RETURN TO BASE. MECHANICS CHECKED CONNECTIONS ON ALTERNATOR AND FOUN D ALL WIRING CORRECT. THEY REMOVED THE ALTERNATOR AND FOUND THAT THE FRONT BEARING ON THE ALTERNATOR HAD FAILED. THIS IN TURN HAD CAUSED THE CLUTCH ASSEMBLY TO FAIL WHICH HAD DAMAGED THE DRIVE GEAR ON THE CRANKSHAFT. ENGINE WAS REMOVED AND SENT OUT FOR REPAIR. 1 L 7 2 3O 3 O 3A10 E5CE 2002071800015 20020718 00015 NE 2002 7 18 CA020620004 2 20020512 A 7200 CF343B1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT FAILED W A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 CA (CAN) FOLLOWING TAKE OFF AND PASSING THROUGH 8000 FT ASL, THE FLIGHT CREW RECEIVED A RT ENGINE OIL PRESSURE WARNING MESS AGE. THE CREW COMPLIED WITH THE QRH AND INITIATED AN ENGINE SHUTDOWN. THE AIRCRAFT WAS RETURNED AND AN EMERGENCY WAS DEC LARED FDR SHOWN ENGINE OPERATION 5 PSI FOR GREATER THAN ONE MINUTE. ENGINE CHANGE CARRIED OUT. 2 L 7 2 4F 4 F RT A21EA E15NE 2002071800016 20020718 00016 EA 2002 7 18 CA020621001 1 20020615 A 3242 06610800 LINER DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A34 52043 EA BRAKE ASSY CRACKED W F ACTIVATE FIRE EXT. K A B FLUID LOSS FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA (CAN) NEW BRAKE LININGS WERE INSTALLED ONTO BACKING PLATES & PRESSURE PLATES FOR BRAKE CYLINDER ASSY, USING PROPER RIVET S ASSPECIFIED BY CLEVELAND WHEELS & BRAKES. A/C TAXIED FOR CONDITIONING BRAKE LININGS AS PER MANUFACTURE FOR NONASBESTOS ORGANIC LININGS.A/C TAXIING BACK TO HANGAR WHEN IT DISCOVERED LOSS OF BRAKE PRESSURE APPLIED BY PILOT. A/C DID MANAGED TO COME TO STOP. ESCAPING HYDRAULIC FLUID & HOT BRAKE PARTS CREATED FIRE IN WHEEL WELL. PILOT QUICKLY EXTINGUISHED BLAZE WITH ONE OF A/C ONBOARD FIRE EXTINGUISHERS. LARGE POOL(S) OF HYDRAULIC FLUID FROM LT MAIN UNDERCARRIAGE BRAKE CYLINDERS 1ST DISCOVERED BY MAINT STAFF UPON APPROACHING A/C. 1 H 7 2 3T 4 T RT A9EA E4EA 2002071800017 20020718 00017 NE 2002 7 18 CA020621003 2 20020610 A 7414 A5838GR1 MAGNETO DOUG B26 B26C 3200524 WP PWA R2800 R280079 52026 NE RT ENGINE OUT OF ADJUST W E A ENGINE SHUTDOWN UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 CA (CAN) RT ENGINE SHUTDOWN IN FLIGHT, BACKFIRING IN CLIMB. INTERNAL TIMING FOUND TO BE OUT - TIMING ADJUSTED. GROUND RUN F OUND SERVICEABLE. 2 M 7 2 4R 4 R L34 5E8 2002071800019 20020718 00019 SO 2002 7 18 000170 1 20020623 A 3240 SENSOR EMB 145 EMB145 3260210 SO RT MLG MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 274 RIGHT I/B BRAKE TEMP IN RED. REMOVED AND REPLACED RIGHT IB BRAKE TEMP SENSOR. 2 L 7 2 4F RT T00011AT 2002071800020 20020718 00020 NM 2002 7 18 SWAA021411 1 20020625 A 2560 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LEFT AND RIGHT PHOTO-LUMINESCENT EMERGENCY EXIT STRIPS DELAMINATED AT ROW NR 9. REMOVED AND REPLACED STRIPS PER MM. 2 L 7 2 4F RT A16WE 2002071800021 20020718 00021 NM 2002 7 18 SWAA021466 1 20020704 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AND LENS MISSING AT ROW NR 1. RELAMPED LIGHT AND INSTALLED LENS PER MM . 2 L 7 2 4F RT A16WE 2002071800022 20020718 00022 NM 2002 7 18 CA020621005 1 20020514 A 2910 LINE DHAV DHC8 DHC8* NM PWC 150 PW150A EA HYDRAULIC SYSTEM CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) HYDRAULIC AND FUEL LINES WERE FOUND CHAFING IN FWD NACELLE, ZONE 3, ON FAIRLEAD COVER PLATES. DURING REASSY FROM STRUCTURAL MODS PROGRAM HYDRAULIC TUBE FAIRLEAD REMOVED AT ZONE 3 STRUCTURE ASSY TO ALLOW EASIER ALIGNMENT BETWEEN REMOV ED HYD TUBES IN RT WHEEL WELL AND THOSE FWD OF FIREWALL. FOUND METAL PORTION OF FAIRLEAD HAD CHAFED PRESSURE TUBE BEYOND ALLOWABLE LIMITS. REMOVED SAME FAIRLEAD FROM LT NACELLE AND DISCOVERED SAME CONDITION EXISTED, TUBE IN LT NACELLE BEING CHAFED BEYOND ALLOWABLE LIMITS AS WELL. INSPECTION OF INST HAS FOUND THAT ALL 3 OF HYDRAULIC TUBES RUNNING THROUGH FAIR LEAD ARE CHAFED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002071800023 20020718 00023 NM 2002 7 18 CA020621006 1 20020408 A 2435 BRUSHES ELECTROSYS ROBSIN R22 R22BETA 7640110 NM LYC O320 O320B2C 41508 EA ALTERNATOR WORN W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 3092978 (CAN) THE ALTERNATOR IS "ON CONDITION", AND THERE IS NO REQUIREMENT BY EITHER ROBINSON HELICOPTERS OR TRANSPORT CANADA R EGULATIONS TO INSPECT THE ALTERNATOR OR THE BRUSHES ON A REGULAR INTERVAL. AS A CONSEQUENCE, THIS ALTERNATOR HAD BRUSHES THAT RAN APPROX 50 - 100 HOURS BEYOND THE LIMITS FOR THE BRUSHES. ONE OF THE BRUSHES WAS FOUND TO HAVE SLIPPED COMPLETE LY OUT OF THE BRUSH RETAINER AND WAS BESIDE THE SLIP RING, WITH THE TAIL PIECE FROM THE BRUSH WIRE BROKEN OFF. 1 G 7 1 3O 3 O H10WE E274 2002071800024 20020718 00024 NM 2002 7 18 SWAA021467 1 20020704 A 3350 6574550 RECEPTACLE BOEING 737 7373Y0 1384671 NM SERVICE DOOR DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED INNER RECEPTACLE PER MM. 2 L 7 2 4F RT A16WE 2002071800025 20020718 00025 EA 2002 7 18 CA020621008 1 20020618 A 7332 5905587 FUEL FILTER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 1 ENGINE CONTAMINATED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) IN CLIMBOUT NR 1 ENGINE FUEL BYPASS CAUTION LIGHT ILLUMINATED. NR 1 ENGINE LP AND HP FUEL FILTERS REPLACED. HP FUE L FILTER FOUND WITH CONTAMINATION. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002071800026 20020718 00026 NM 2002 7 18 SWAA021468 1 20020704 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT LIGHTS INOP AT ROW'S 3 ABC AND 20 DEF. RELAMPED EXIT LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2002071800027 20020718 00027 NM 2002 7 18 SWAA021478 1 20020704 A 5320 6940367 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 360, STR 5L AND BS 887, STR 4L. REMOVED AND REPLACE D STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002071800028 20020718 00028 NM 2002 7 18 CA020621009 1 20020618 A 7312 FUEL HEATER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENGINE FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 11196 (CAN) NR 1 ENGINE FUEL INLET TEMP AT RED LINE IN FLIGHT. FAULT REPAIRED BY REPLACEMENT OF FUEL HEATER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002071800029 20020718 00029 NM 2002 7 18 CA020624001 1 20020623 A 2910 82910009113 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W E D ENGINE SHUTDOWN RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) ON START UP OF NR 2 ENGINE PILOTS REPORTED SMOKE FROM NOSE AREA. SMOKE CONFIRMED AS HYDRAULIC MIST DUE TO PIN HOLE IN GEAR DOWN RIGID HYDRAULIC LINE AT BEND TWO INCHES FROM END OF FITTING.IPC REF 29-20-00 FIG 5 ITEM 130 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002071800030 20020718 00030 NM 2002 7 18 SWAA021481 1 20020704 A 5320 6551698 SPLICE BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICES CRACKED (4 EA) AT BS 663.75, STR 2R, 2L, 3R AND 3L. REMOVED AND REP LACED STR SPLICES PER SRM. 2 L 7 2 4F A16WE 2002071800031 20020718 00031 2002 7 18 SWAA021482 4 20020705 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002071800032 20020718 00032 NM 2002 7 18 SWAA021486 1 20020707 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002071800033 20020718 00033 CE 2002 7 18 CA020624002 1 20020620 A 2435 3021565 SHAFT BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA STARTER GEN WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE STARTER GENERATOR GEARSHAFT DRIVE WAS FOUND WORN TO LIMITS WITH ONLY 1242 HOURS SINCE NEW. THE ENGINE WAS PURC HASED WITH 0 TIME SINCE NEW. 1 L 7 2 3T 4 T A14CE E4EA 2002071800035 20020718 00035 NM 2002 7 18 SWAA021488 1 20020705 A 2782 65445517 ACTUATOR BOEING 737 7373Q8 1384670 NM L/E FLAP FAILED A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 29 688SW 23254 AIR TURNBACK, AFTER TAKEOFF NR 2 KRUEGER FLAP WOULD NOT RETRACT. REMOVED AND REPLACED NR 2 KRUEGER FLAP ACTUATOR PER MM . 2 L 7 2 4F RT A16WE 2002071800036 20020718 00036 NM 2002 7 18 SWAA021489 1 20020705 A 3233 654482518 ACTUATOR BOEING 737 7373H4 1384600 NM LT MLG FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 636WN 27709 AIR TURNBACK, UNSAFE LT MLG (RED) LIGHT ILLUMINATED AFTER TAKEOFF, CYCLED LANDING GEAR AND GOT SAME INDICATION. REMOVED AND REPLACED LT MLG UPLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2002071800037 20020718 00037 2002 7 18 SWAA021491 4 20020707 A 2565 61621469 SLIDE BOEING 737 7373G7 1384595 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLID E PER MM. 2 L 7 2 4F RT A16WE 2002071800038 20020718 00038 2002 7 18 SWAA021494 4 20020707 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002071800039 20020718 00039 NM 2002 7 18 CA020624004 1 20020611 A 2497 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ELECTRICAL DAMAGED W C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 CA (CAN) ON TAKEOFF, MASTER CAUTION & LT AND RT STALL WARNING CAUTION ILLUMINATED AT SAME TIME AS LT AC BUS, RT AC BUS, LT RU, RT RU. THERE WAS NO VOLTS OR LOADS ON VARIABLE AC GAUGES, NO TRU CIRCUIT BREAKERS POPPED. CREW HAD NO AC POWER, BUT NO AC BUS CAUTION LIGHTS. CREW RESET AC GENERATORS, AND RESTORED ALL SYSTEMS. MAINT DEFRERRED NR 2 STALL SYSTEM. THE NEX T DAY JUNE 12TH, MAINT REPLACED BOTH AC GENS. NR 1 AC GEN WOULD NOT COME ON LINE. AIRCRAFT DOWNED FOR FUTHER TROUBLESHOO TING. ON JUNE 13TH ONE BARE WIRE WAS FOUND, AND REPAIRED IN THE LT CONTACTOR BOX. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002071800040 20020718 00040 2002 7 18 SWAA021495 4 20020707 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002071800041 20020718 00041 NM 2002 7 18 SWAA021497 1 20020707 A 2560 P2070001 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED RON, FOUND BOTTOM AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002071800042 20020718 00042 2002 7 18 SWAA021540 4 20020712 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002071800043 20020718 00043 NM 2002 7 18 SWAA021541 1 20020712 A 3350 7003665 BALLAST BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 783SW 29809 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT BALLAST PE R MM. 2 L 7 2 4F RT A16WE 2002071800044 20020718 00044 NM 2002 7 18 SWAA021543 1 20020713 A 3350 7003667 BALLAST BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT BALLAST PER MM. 2 L 7 2 4F RT A16WE 2002071800045 20020718 00045 NM 2002 7 18 SWAA021544 1 20020711 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE AT ROW NR 17. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002071800046 20020718 00046 NM 2002 7 18 SWAA021546 1 20020714 A 3350 1000679 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 702ML 22054 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2002071800047 20020718 00047 2002 7 18 SWAA021547 4 20020714 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002071800048 20020718 00048 NM 2002 7 18 SWAA021549 1 20020714 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 EEPLS LOOSE BETWEEN ROW'S NR 5 TO NR 8. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002071800049 20020718 00049 NM 2002 7 18 SWAA021550 1 20020714 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 EEPLS LOOSE AT ROW NR 9. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002071800050 20020718 00050 NM 2002 7 18 SWAA021551 1 20020711 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 092SW 22964 DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2002071800051 20020718 00051 NM 2002 7 18 SWAA021554 1 20020712 A 2121 215201 GASPER FAN BOEING 737 7373H4 1384600 NM A/C BAY MALFUNCTIONED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 600WN 27694 FLT ATTENDANTS REPORTED BURNING PLASTIC SMELL IN CABIN. REMOVED AND REPLACED GASPER FAN MOTOR PER MM. 2 L 7 2 4F RT A16WE 2002071800052 20020718 00052 NM 2002 7 18 SWAA021557 1 20020712 A 2910 280205 FUSE BOEING 737 7377H4 1384404 NM HYD SYSTEM MALFUNCTIONED A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 29 744SW 29490 AIR TURNBACK, AFTER TAKEOFF L/E FLAPS WOULD NOT RETRACT. RESET HYD FUSES PER MM. 2 L 7 2 4F RT A16WE 2002071800053 20020718 00053 NM 2002 7 18 SWAA021558 1 20020712 A 2910 280205 FUSE BOEING 737 7377H4 1384404 NM HYD SYSTEM MALFUNCTIONED A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 29 755SA 27871 AIR TURNBACK, AFTER TAKEOFF L/E FLAPS WOULD NOT RETRACT. RESET HYD FUSES PER MM. 2 L 7 2 4F RT A16WE 2002071800054 20020718 00054 NM 2002 7 18 SWAA021559 1 20020712 A 2751 2061141 INDICATOR BOEING 737 7373Y0 1384671 NM COCKPIT MALFUNCTIONED A SWAA B EMER. DESCENT N FALSE WARNING DE DESCENT 1 SW 29 664WN 23495 DECLARED EMERGENCY, DURING DESCENT T/E FLAPS WOULD NOT LOWER BELOW 15 DEGREES. REMOVED AND REPLACED T/E FLAP POSITION I ND PER MM. 2 L 7 2 4F RT A16WE 2002071800055 20020718 00055 WP 2002 7 18 CA020625001 1 20020622 A 7931 982C9HE2MR5 ENGINE 982C9HE2MR5 GRUMAN TS2 TS2ACALFORST 3951102 WP WRIGHT R1820 982C9HE2 67020 EA HAMSTD 43D 43D51 NE NACELLE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) THE AIRCRAFT DEPARTED CYXS ENROUTE TO A FIRE. DURING CLIMB THE LOW OIL PRESSURE LIGHT ILLUMINATED. THE OIL TEMP WA S RISING, THE THROTTLE WAS RETARDED AND WHEN THE OIL PRESSURE REACHED 40 PSI THE ENGINE WAS SHUT DOWN. THE AIRCRAFT RETU RNED TO CYXS. THE ENGINE WAS REMOVED AND A SERVICEABLE QCU WAS INSTALLED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4R 4 R A25WE E259 6 C P8879 2002071800056 20020718 00056 NE 2002 7 18 CA020626001 2 20020618 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE NACELLE LEAKING W C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CA (CAN) TAKEOFF ABORTED DUE TO OIL FLUCTUATION. MAINTENANCE FOUND OIL LEVEL LOW. AS OIL HAD BEEN TOPPED UP 3 AIR HOURS BEFORE - LEAK RUNS WERE CARRIED OUT. ENGINE RUN FOR 1/2 HOUR WITH NO OIL CONSUMPTION. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002071800057 20020718 00057 NM 2002 7 18 DHL2002721003 1 20020716 A 2610 1014A POWER UNIT BOEING 727 727228 1384083 NM A DHLA K O NONE OTHER L O NO TEST OTHER IN INSP/MAINT 1 SO 01 721DH 19545 1) WHILE PERFORMING APU FIRE WARNING TEST APU BLT C/B POPPED. 2) R/R APU OPERATING POWER UNIT IAW WDM 49-41-01 APU FIR E WARNING GRD OP CK GOOD. 2 L 7 3 4F RT A3WE 2002071800058 20020718 00058 NM 2002 7 18 VNAA0207002 1 20020701 A 2121 26006881102 FAN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 458PS 16097 3068 WHILE EN ROUTE FROM CAE TO DCA, THE CREW RECEIVED AN AHARS OVERHEAT MESSAGE. THE CAPTAIN CONTACTED MAINTENANCE CONTROL AND THE DECISION TO DIVERT TO PIT WAS MADE. WHEN AT PIT, MAINTENANCE INSPECTED AND REPLACED THE AHARS FAN IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002071800059 20020718 00059 SO 2002 7 18 000172 1 20020627 A 5270 WARNING SYSTEM EMB 145 EMB145 3260210 SO COCKPIT MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 294 LEFT EMERGENCY EXIT DOOR INDICATED OPEN ON EICAS. BY THE TIME A/C GOT BACK TO GATE, MSG WAS GONE. MAINTENANCE FOUND DO OR SECURE. OPENED, CLOSED, AND SECURED DOOR, OPS CHECK GOOD AND INDICATION OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2002071800060 20020718 00060 NE 2002 7 18 CA020626002 2 20020614 A 7414 A5838GR1 MAGNETO DOUG B26 B26C 3200524 WP PWA R2800 R280079 52026 NE RT ENGINE WORN W E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) RT ENGINE BACKFIRING AND RUNNING ROUGH. ENGINE SHUTDOWN. AIRCRAFT RETURNED TO BASE. LT MAGNETO DISTRIBUTOR ROTOR R EPLACED. RUN ON GROUND FOUND TO RUN SATISFACTORY. 2 M 7 2 4R 4 R L34 5E8 2002071800062 20020718 00062 SO 2002 7 18 000173 1 20020630 A 3040 ANTI-ICE SYSTEM EMB 145 EMB145 3260210 SO COCKPIT FAILED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 267 CREW REPORTS WINDSHIELD HEAT NR 2 FAIL ON T/O. ABORTED TAKEOFF. DEFERRED WINDSHIELD HEAT 2. 2 L 7 2 4F RT T00011AT 2002071800064 20020718 00064 EA 2002 7 18 CA020626005 1 20020609 A 2731 SKIN DHAV C3TE1106 DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A34 52043 EA RT ELEVATOR SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA 1042 (CAN) HINGE SEPARATING FROM SERVO TAB IN FLIGHT. ELEVATO BOTTOM SKIN SEPARATED 24 INCHES ALONG TRAILING EDGE. CENTRE SPA R BROKEN IN 3 PARTS.TAILING SPAR BROKEN IN 2 PIECES. 1 H 7 1 3R 4 T A815 E4EA 2002071800065 20020718 00065 EU 2002 7 18 000174 1 20020701 A 3240 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU COCKPIT ACTIVATED A CHQA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 11 108 CREW LOWERED GEAR ON FINAL INTO AOO AND GOT ANTI-SKID FAIL. OPS DEFERRABLE, DISPATCH ADVISED AIRCRAFT CAN'T TAKEOFF FRO M AOO WITH THE ANTI-SKID MEL. DISPATCH RETURNED AIRCRAFT TO PIT. 2 L 7 2 4T RT A52EU 2002071800066 20020718 00066 2002 7 18 SWAA021405 4 20020625 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 FWD SERVICE DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002071800067 20020718 00067 NM 2002 7 18 SWAA021406 1 20020624 A 2560 P2070001 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 351SW 24572 BOTH FWD EMERGENCY FLASHLIGHTS INOP. REMOVED AND REPLACED BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2002071800068 20020718 00068 NM 2002 7 18 SWAA021408 1 20020622 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002071800070 20020718 00070 NE 2002 7 18 SWAA021409 2 20020625 A 7261 RD3018 O-RING BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE LEAKING A SWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 29 094SW 23053 IN FLIGHT SHUTDOWN, DECLARED EMERGENCY, DURING DESCENT NR 2 ENGINE OIL QUANTITY INDICATED ZERO, PRESS WAS DROPPING. REM OVED AND REPLACED STUD ON OIL FILTER AND REMOVED AND REPLACED O-RINGS ON VENT ABOVE BANJO FITTINGS PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2002071800071 20020718 00071 NM 2002 7 18 SWAA021415 1 20020624 A 3210 6598371297 PIN BOEING 737 7373H4 1384600 NM LT MLG SHEARED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 629SW 27704 AIR TURN BACK, LEFT MAIN GEAR WOULD NOT RETRACT AFTER T/O, GEAR INDICATED DOWN AND LOCKED ON ALL 3 AFTER PUTTING HANDLE BACK DOWN, UNEVENTFUL LANDING AT ONT. FOUND LEFT MLG TRUNNION PIN SHEARED AT MAIN GEAR ACTUATOR. FOUND LT MLG FWD TRUN NION YOKE OTBD LOCK BOLT SHEARED. REMOVED AND REPLACED BOTH LT TRUNNION PIN AND TRUNNION LOCK BOLT PER MM. MX FERRY TO PHX FOR GEAR SWING. FOUND BROKEN HAT BUSHING CORRODED. REMOVED AND REPLACED LT MLG PER MM. 2 L 7 2 4F RT A16WE 2002071800072 20020718 00072 NM 2002 7 18 SWAA021416 1 20020626 A 2120 ODOR BOEING 737 7377H4 1384404 NM GALLEY DETECTED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 703SW 27837 DIVERSION, FUEL SMELL IN AFT GALLEY. INSPECTED AFT GALLEY, ALL COMPARTMENTS, RAN APU, BOTH PACKS AND ENGINES. NO ODOR DETECTED. 2 L 7 2 4F RT A16WE 2002071800073 20020718 00073 NM 2002 7 18 SWAA021430 1 20020628 A 3350 10126211 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED RON, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002071800074 20020718 00074 NM 2002 7 18 SWAA021431 1 20020628 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 EEPLS LOOSE AT ROW NR 8. REMOVED AND REPLACED EEPLS STRIP AT ROW NR 8 PER MM. 2 L 7 2 4F RT A16WE 2002071800075 20020718 00075 2002 7 18 SWAA021433 4 20020628 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 788SA 30603 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER IN JETWAY. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002071800076 20020718 00076 NM 2002 7 18 SWAA021439 1 20020701 A 2910 65C26839 HYDRAULIC LINE BOEING 737 7373H4 1384600 NM HYD SYSTEM LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 29 394SW 27380 AIR TURNBACK, B-SYSTEM HYDRAULIC FAILURE AFTER TAKEOFF. REMOVED AND REPLACED HYD PRESS LINE BETWEEN B-ELEC PUMP AND B-S YSTEM MODULE PER MM. 2 L 7 2 4F RT A16WE 2002071800077 20020718 00077 2002 7 18 SWAA021440 4 20020630 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER WHILE OPENING THE DOOR. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002071800078 20020718 00078 NM 2002 7 18 SWAA021442 1 20020629 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGH T ASSY PER MM. 2 L 7 2 4F RT A16WE 2002071800079 20020718 00079 NM 2002 7 18 SWAA021443 1 20020702 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN DETERIORATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS STRIP DETERIORATED IN FWD CABIN. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2002071800080 20020718 00080 2002 7 18 SWAA021446 4 20020702 A 2565 61621469 SLIDE BOEING 737 7375H4 138449D NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLID E PER MM. 2 L 7 2 4F RT A16WE 2002071800081 20020718 00081 NM 2002 7 18 SWAA021447 1 20020702 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 RT OVERWING EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY. 2 L 7 2 4F RT A16WE 2002071800082 20020718 00082 2002 7 18 SWAA021448 4 20020629 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 FWD SERVICE DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002071800083 20020718 00083 NM 2002 7 18 SWAA021453 1 20020702 A 5751 654645423A AILERON BOEING 737 7372T4 1384492 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING WALKAROUND INSPECTION, FOUND LT AILERON DELAMINATED. REMOVED AND REPLACED LT AILERON AND TAB PER MM. 2 L 7 2 4F A16WE 2002071800084 20020718 00084 2002 7 18 SWAA021457 4 20020701 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002071800085 20020718 00085 NM 2002 7 18 SWAA021461 1 20020703 A 3350 207330 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2002071800086 20020718 00086 NM 2002 7 18 SWAA021463 1 20020704 A 2560 A170033 STRAP BOEING 737 7377H4 1384404 NM FLASHLIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 EMERGENCY FLASHLIGHT STRAP LOOSE IN FWD GALLEY. SECURED STRAP PER MM. 2 L 7 2 4F RT A16WE 2002071800087 20020718 00087 NM 2002 7 18 SWAA021464 1 20020702 A 3350 65C27093 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 OVERHEAD EMERGENCY EXIT LIGHT COVER LOOSE AT OVERWING EXIT'S. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002071800088 20020718 00088 NM 2002 7 18 SWAA021465 1 20020704 A 3350 300432 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002071800089 20020718 00089 NM 2002 7 18 VNAA0206010 1 20020619 A 2133 CONTROLLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN PRESSURE MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 422JS 3018 DURING TAKEOFF, THE CREW RECEIVED A CPCS AUTO FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CPCS AUTO MODE WAS DEFERRED, 21 -9-1 CODE C, AND THE FLIGHT CONTINUED TO CAE ON TIME. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002071800090 20020718 00090 NE 2002 7 18 VNAA0206012 2 20020620 A 7321 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE DIRTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 460PS 3061 DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND ENGINE CONTROL UNIT FAIL AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND CLEANED THE ENGINE CONTROL UNIT CANNON PLUG IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002071800091 20020718 00091 NM 2002 7 18 VNAA0206017 1 20020625 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 439JS 13676 103 3057 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROW 9A WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 7L K EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL TESTS WERE PERFORMED AND THE AI RCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002071800093 20020718 00093 CE 2002 7 18 CA020626010 1 20020624 A 3230 CONNECTOR BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA MLG CONTAMINATED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 15725 (CAN) AFTER TAKOFF THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO BASE. MAINTENANCE DISCOVERED THAT THE RIGHT HAND WIRING CONECTOR IN THE WHEEL WELL WAS DIRTY AND PREVENTED THE PROPER INDICATION TO ALLOW THE LANDING GEAR TO BE RET RACTED. THE CONNECTOR WAS CLEANED AND CHECKED FOR SEALING. THREE GEAR SWING COMPLETED AND CHECKED SERVICABLE 1 L 7 2 3T 4 T A14CE E4EA 2002071800094 20020718 00094 CE 2002 7 18 CA020626011 1 20020626 A 5610 17360106 WINDSHIELD LEAR 45 45LEAR 5170805 CE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) DURING A CVR FLIGHT TEST RT WINDSHEILD GLASS CRACKED. PILOT IMMEDIATLY RETURN TO WHERE IT TOOK OFF. 2 L 7 2 4F RT T00008WI 2002071800096 20020718 00096 EA 2002 7 18 CA020626014 2 20020619 A 7421 URHB32E SPARK PLUG PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA NR 5 CYLINDER FAILED W D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 CA (CAN) MAG DROPPED 300 RPM ON RIGHT HAND ENGINE DURING RUN-UP. CYLINDER NR 5 BOTTOM SPARK PLUG WAS FOUND UNSERVICEABLE. SPARK PLUG REPLACED WITH NEW ONE. 1 L 7 2 3O 3 O A20SO E14EA 2002071800097 20020718 00097 EA 2002 7 18 CA020626015 2 20020613 A 7314 LW15473 PUMP PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA FUEL SYSTEM FAILED W D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 CA (CAN) DURING A RUN-UP THE PILOT NOTICED FLUCTUATIONS OF THE ENGINES PARAMETERS AS WELL AS ONTHE FUEL FLOW INDICATOR. THE MECHANICAL FUEL PUMP WAS FOUND TO BE THE CAUSE OF THESE FLUCTUATIONS. THE PUMP WAS REPLACED. 1 L 7 2 3O 3 O 1A10 1E4 2002071800098 20020718 00098 NE 2002 7 18 CA020626016 2 20020620 A 7200 ENGINE CNDAIR CL600 CL600* EA LYC ALF502 ALF502L 41580 NE LEFT FAILED W C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 CA (CAN) WHILE PERFORMING THE 5TH TOUCH AND GO DURING A TRAINING FLIGHT, THE AIRCRAFT PULLED TO THE LT AS ENGINE POWER WAS INCREASED TO TAKEOFF. THE CREW APPLIED RT RUDDER TO CENTER THE AIRCRAFT. THE CO-PILOT NOTED N1 ON THE LT ENGINE TO BE AP PROX. 1-3 PERCENT AND TEMPERATURE PEAKED WITH RED ANNUNCIATOR LIGHT. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT MADE AN UN EVENTFUL CONTROLLED STOP. 2 L 7 2 4F 4 F RT A21EA E6NE 2002071800099 20020718 00099 EU 2002 7 18 02FDEA00499 1 20020708 A 5300 STRINGER AIRBUS 310 A310 EU N/A CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 N 108 STRINGER 56R AT CONNECTOR AFT OF FRAME 72. R&R STRINGER PER SRM 53-10-14. 2 L 7 2 4F RT A35EU 2002071800100 20020718 00100 2002 7 18 GTIA020630 4 20020606 A 2215 4034237915 SERVO DOUG DC9 DC982 3022082 WP AUTOPILOT SYS DEFECTIVE A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 801NK 48048 WHEN LEVEL W/AUTO PILOT THE ALTITUDE WANDERS UP AND DOWN 200 FEET EITHER WAY. AUTO PILOT TRIM LIGHT COMES ON AND REMAIN S ON, DISCONNECTING AUTO PILOT CAUSES BIG PITCH (TRIM). AFTER RETRIM AND AUTO PILOT BACK ON SEEMS OK, BUT HAPPENED TWIC E. HAPPENS W/ AUTO PILOT IN NR 1 POSITION NO TIME TO CHECK NR 2 AUTO PILOT. REMOVED AND REPLACED DUPLEX ELEVATOR SERVO DRIVE. RAN RTS CHECK ON NR 1 AND NR 2 SYSTEMS, BOTH SYSTEMS GO IAW MFG MM. 2 L 7 2 4F A6WE 2002071800101 20020718 00101 WP 2002 7 18 GTIA020635 1 20020603 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN DISCONNECTED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 131NK 47605 PAX CABIN CEILING EMERGENCY LIGHT INOPERATIVE AT SEVERAL PLACES. T/S SYSTEM FOUND SEVERAL WIRES DISCONNECTED AT BATTERY PACK. RECONNECTED WIRES. 2 L 7 2 4F A6WE 2002071800103 20020718 00103 WP 2002 7 18 GTIA020636 1 20020604 A 5420 SASB00035 ANGLE DOUG DC9 DC941 302207N WP RT PYLON CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 47605 RIGHT PYLON AT FS Y1057 ANGLE CRACKED. REMOVED DAMAGE. FABBED FILLER AND DOUBLER. INSTALLED. 2 L 7 2 4F A6WE 2002071800104 20020718 00104 SW 2002 7 18 CA020626018 1 20020623 A 3212 VALVE BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE SHEARHEAD FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) FLOAT BAGS FOUND TO BE PARTIALLY INFLATED, BOTTLE PRESSURE DOWN 1100 PSI. BOTTLE HAD BEEN LOOSING CHARGE OVER TIME . INVESTIGATION/TROUBLESHOOTING INCLUDED REPLACEMENT OF RELIEF VALVE AND CHARGE VALVE. FINAL DISSASEMBLY DETERMINED SH EAR HEAD TO HAVE FAILED. 1 G 7 1 4U 4 U H4SW E22EA 2002071800105 20020718 00105 SO 2002 7 18 SIMA200216002 1 20020609 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 DENT INBOARD OF RIGHT WIPER MOTOR ARM. THREE DENTS ACCEPTED AS IS IAW MFG GST. 2 L 7 2 4T RT T00011AT 2002071800106 20020718 00106 SO 2002 7 18 SIMA200217316 1 20020619 A 5330 SKIN EMB 135 EMB135LR 3260305 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 732DH 3218 145358 THREE GOUGES BETWEEN FRAMES 15-16, BETWEEN STRINGERS 16L AND 17L. (SUP) BLENDED GOUGES, PERFORMED NDT WITH NO DEFECTS. GOUGES ACCEPTED AS IS IAW MFG GST. 2 L 7 2 4F RT T00011AT 2002071800107 20020718 00107 SO 2002 7 18 SIMA200217317 1 20020619 A 5330 SKIN EMB 135 EMB135LR 3260305 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 732DH 145358 GOUGE IN FUSELAGE SKIN BETWEEN FRAMES 71 AND 72 AND STRINGERS 16R AND 17R. BLENDED GOUGE, PERFORMED NDT WITH NO DEFECTS . GOUGE ACCEPTED AS IS IAW MFG GST. 2 L 7 2 4F RT T00011AT 2002071800108 20020718 00108 SO 2002 7 18 SIMA200217318 1 20020619 A 5210 SKIN EMB 135 EMB135LR 3260305 SO PAX DOOR GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 732DH 3218 145358 GOUGE ON FORWARD EDGE OF MAIN DOOR SKIN. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. GOUGED ACCEPTED AS IS IAW MFG GST. 2 L 7 2 4F RT T00011AT 2002071800109 20020718 00109 SO 2002 7 18 SIMA200217319 1 20020619 A 5320 STRUCTURE EMB 135 EMB135LR 3260305 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 732DH 145358 GOUGE BETWEEN JUNCTION 1 AND FRAME 14, ALONG STRINGER 15L. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IA W MFG GST. 2 L 7 2 4F RT T00011AT 2002071800110 20020718 00110 SO 2002 7 18 SIMA200217320 1 20020619 A 5320 STRUCTURE EMB 135 EMB135LR 3260305 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 732DH 3218 145358 GOUGE BETWEEN FRAMES 16-17 BETWEEN STRINGERS 16L AND 17L. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST. 2 L 7 2 4F RT T00011AT 2002071800111 20020718 00111 SO 2002 7 18 SIMA200217321 1 20020619 A 5730 SKIN EMB 135 EMB135LR 3260305 SO LT WING GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 732DH 145358 LEFT NR 1 LEADING EDGE GOUGED 11 INCH INBOARD OF LANDING LIGHT LENS COVER. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. A CCEPTED AS IS IAW MFG GST. 2 L 7 2 4F RT T00011AT 2002071800112 20020718 00112 SO 2002 7 18 SIMA200217322 1 20020621 A 4910 FRAME EMB 135 EMB135LR 3260305 SO APU COWLING BENT A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 732DH 3218 145358 APU COWLING INTERIOR FORWARD FRAME IS BENT ABOVE THE TOP LEFT MOUNT HOLE, RECONTOURED FORWARD FRAME, PERFORMED NDT, NO D EFECTS. DONE IAW SRM AND MFG GST. 2 L 7 2 4F RT T00011AT 2002071800113 20020718 00113 NM 2002 7 18 CA020627005 1 20020626 A 2910 82950010173 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM RUPTURED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) LT WING SPOILER RETURN LINE RUPTURED ABOUT 18 INCHES FROM O/B END. LINE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002071800114 20020718 00114 CE 2002 7 18 T4O2002F00002 1 20020612 A 3233 99812257652 ACTUATOR BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA LT MLG FAILED B T4OR K NONE O OTHER IN INSP/MAINT 1 NE 03 266RH 8025 BB778 FOUND DURING PHASE INSPECTION LANDING GEAR RETRACTION TEST; THE LEFT LANDING GEAR RETRACT ACTUATOR JACKSCREW NUT ASSEMB LY BROKE (THREADED SCREW DISCONNECTED FROM CHROME TUBE), AND THE LEFT LANDING GEAR FELL DOWN, BUT NOT LOCKED. PROBABLE CAUSE: BAD ACTUATOR NUT BRAZE. THIS PROBLEM IS ADDRESSED BY MFG SB. THE FAILED ACTUATOR NUT WAS ONE OF THE AFFECTED N UT PART NUMBERS IN SB. 1 L 7 2 4T 4 T A24CE E4EA 2002071800115 20020718 00115 NM 2002 7 18 CA020627006 1 20020626 A 2750 TORQUE TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE TE FLAP DRIVE CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LT WING OUTBOARD FLAP DRIVE TORQUE TUBE ASSY CHAFED ON CONDUIT. CHAFED 11.5 INCH FROM O/B END OF TUBE. CHAFE IS .7 5 INCH WIDE AND .03125 INCH DEEP. TORQUE TUBE ASSY REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002071800116 20020718 00116 SW 2002 7 18 CA020627007 1 20020620 A 2820 FUEL CELL BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE FUSELAGE CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRYSTALS WERE FOUND IN THE FUEL CELL WHILE IT WAS FIRE-FIGHTING HOUSE LAKE FIRE. THE CRYSTALS WERE FOUND DUE TO A BLOCKED EJECTOR PUMP. SOURCE OF THE CRYSTALS IN UNKNOWN. A SAMPLE OF THE CRYSTALS WAS PROVIDED FOR ANALYSIS. IT WAS DETERMINED THAT THE CRYSTALS WERE SOLUBLE IN WATER, HAVE A MELTING POINT AND CONTAIN MAJOR PROPORTIONS OF MAGNESIUM AND CALCIUM AND TRACE AMOUNTS OF SODIUM. BELIEVE THESE CRYSTALS WOULD NOT PASS THROUGH THE NO-GO FILTERS ON THE FUEL DELIVE RY SYSTEM THERE IS THE POSSIBILITY THAT THEY WERE INTRODUCED DIRECTLY INTO THE AIRCRAFT FUEL TANK. 1 G 7 1 4U 4 U H1SW E17EA 2002071800117 20020718 00117 GL 2002 7 18 CA020627008 2 20020614 A 7314 D107318D PUMP BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL FUEL BOOST FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) SUPPLY FUEL BOOST PUMP FAILED. 1 G 7 2 3U 3 U H3EU E4CE 2002071800118 20020718 00118 WP 2002 7 18 CA020627009 1 20020622 A 6123 1E777BL1 PUMP GRUMAN TS2 TS2ACALFORST 3951102 WP WRIGHT R1820 982C9HE2 67020 EA HAMSTD 43D 43D51 NE FEATHERING FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER ENGINE OIL TEMP ROSE & OIL PRESSURE FELL, PILOT SHUTDOWN ENGINE & ATTEPTED TO FEATHER PROP. TRIED SEVERAL TI MES WITH NO SUCCESS. A/C RETURNED. ENGINE & PUMP WERE RETURNED. FEATHERING PUMP & MOTOR WERE DISASSEMBLED & MOTOR SHOW ED SIGNS OF EXCESSIVE HEAT. WIRES TO BRUSHES WERE MELTED OFF & ARMATURE SHOWED SIGNS OF EXCESSIVE HEAT CAUSING FAILURE O F PUMP. BECAUSE OF HIGH OIL TEMP IT IS BELIEVED TO HAVE CAUSED FAILURE OF PROP TO FEATHER. WE ARE CURRENTLY INVESTIGATIN G SEVERAL AVES WHICH MAY HAVE ATTRIBUTED TO FAILURE OF PUMP. ONCE INVEST. IS COMPLETE WE WILL FWD DETAILS OF OUR FINDING S TO TC. 2 H 7 2 4R 4 R A25WE E259 6 C P8879 2002071800119 20020718 00119 EU 2002 7 18 CA020628003 1 20020603 A 2530 72012400 COFFEEMAKER AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE GALLEY BURNED W B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) AT FLT.LEVEL 35000FT IN CRUISE, CABIN CREW & PASSENGERS NOTICED SMOKE IN FWD GALLEY AREA.CABIN CREW PULLED GALLEY CB'S AND NOTIFIED FLIGHT CREW WHO IN TURN PULLED MAIN GALLEY SUPPLY BREAKERS. A/C DIVERTED INTO SDL (AMSTERDAM) ON FUR THER INSPECTION NR 2 COFFEE MAKER WAS FOUND TO HAVE BURNED ELECTRICAL WIRING. COFFEE MAKER REMOVED AND SENT FOR STRIP RE PORT. 2 L 7 2 4F 4 F RT A28NM E311NE 2002071800123 20020718 00123 NE 2002 7 18 CA020702005 2 20020629 A 7250 ENGINE BOEING 737 737296 1384486 NM PWA JT8 JT8D9A 52048 NE NR 2 LEAKING W O OTHER K FLUID LOSS LD LANDING 1 CA (CAN) NR 2 ENGINE HAD REPORT LOW OIL QUANTITY ON ARRIVAL. MAINTENANCE SERVICED ENGINE WITH 11 LITRES. OIL TRENDS DID NOT INDICATE HIGH CONSUMPTION. RAN ENGINE AND FOUND OIL SMOKE COMING FROM EXHAUST. RETURN OIL FILTER FOUND FOULED WITH CARB ON. SUSPECT CARBON SEAL FAILURE. ENGINE BEING REMOVED FROM NR 2 POSITIION. THIS IS PRELIMINARY REPORT FOR CANJET AIRLINE S. 2 L 7 2 4F 4 F RT A16WE E2EA 2002071800124 20020718 00124 WP 2002 7 18 CA020702009 1 20020623 A 3260 833703 PROXIMITY SENSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NLG FAILED W K NONE J WARNING INDICATION CR CRUISE 1 CA (CAN) NOSE LANDING GEAR UNSAFE (RED LIGHT) INDICATION IN FLIGHT WITH GEAR HANDLE UP. MECHANICAL INDICATOR SHOWED GEAR UP AND GEAR DOOR WAS CLOSED. ON EXTENSION, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON MECHANICAL INDICATOR SHOWED NOSE GEA R DOWN. UP/DOWN LOCK PROXIMITY SENSOR REPLACED I.A.W. M.M. 32-60-05. BITE CHECK PERFORMED ON PSEU CHECK SERVICEABLE. 2 L 7 2 4F 4 F RT A6WE E9NE 2002071800125 20020718 00125 SW 2002 7 18 CA020702010 1 20020624 A 5302 SKIN BELL 407030801 BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAILBOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 53017 (CAN) CRACK IN TAILBOOM SKIN FOUND ON LEFT HAND SIDE EXTENDING FROM FORWARD RIVET ON UPPER LEFT HAND ANGLE SUPPORT P/N 4 07-023-800-117 TO NEXT RIVET UP ON TAILBOOM SKIN. TAILBOOM REMOVED FROM SERVICE AND IS BEING SHIPPED TO BELL HELICOPTERS FOR EVALUATION. REPLACEMENT TAILBOOM WAS INSTALLED. 1 G 7 1 3U 3 U O H2SW E1GL 2002071800129 20020718 00129 SW 2002 7 18 ALG2002F00050 1 20020203 A 6320 23071895 GEAR BELL 206 206L3 1182108 SW GEARBOX CONTAMINATED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 343AL 1037 51372 UPON DISASSEMBLY AND INSPECTION OF PARTS DUE TO METAL CONTAMINATION. PINION GEAR HAS EXCESSIVE GALLING ON GEAR TEETH DU E TO IMPROPER MACHINING AND MESHING WITH T/M GEAR. BOTH PARTS WERE SCRAPPED AND SENT FOR WARRANTY CREDIT. ASSURE PROPE R MACHINING AND MESHING OF GEAR TEETH. 1 G 7 1 3U H2SW 2002071800131 20020718 00131 SO 2002 7 18 C2XA02BT026 1 20020618 A 3320 LIGHT EMB 145 EMB145LR 3260212 SO CABIN DEFECTIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 14972 145151 EWR- CREW REPORTED, LATERAL LIGHT AT SEAT 9A SMOKES. MAINTENANCE INSPECTED AND PLACED AIRCRAFT ON MEL. AIRCRAFT RELEAS ED IAW MEL 33-20-00 CATEGORY C. MAINTENANCE REMOVED AND REPLACED LATERAL PASSENGER CABIN LIGHT ASSY IAW EMB145 MM 33-21 -06. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2002071800133 20020718 00133 SO 2002 7 18 C2XA02BT028 1 20020703 A 3230 23092900001 UPLOCK EMB 145 EMB145LR 3260212 SO RT MLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14953 145071 EWR- CREW REPORTED AFTER TAKEOFF LG/GEAR DISAGREEMENT (INDICATION), RT MAIN GEAR. AIRCRAFT AIR RETURNED TO EWR. MAINTEN ANCE REMOVED AND REPLACED RT MAIN LANDING GEAR UPLOCK BOX IAW EMB145 MM 32-33-10 AND PROXIMITY SWITCH IAW EMB145 MM 32-6 1-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002071800134 20020718 00134 SO 2002 7 18 C2XA02BT030 1 20020705 A 2150 HOSE EMB 145 EMB145LR 3260212 SO HEAT EXCHANGER DISCONNECTED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 12922 145338 EWR- AIRCRAFT RETURNED TO GATE DUE TO SMOKE IN THE CABIN. MAINTENANCE FOUND TWO HOSES DISCONNECTED. REINSTALLED NUMBER TWO RECIRCULATING FAN OUTLET HOSE AND REINSTALLED HEAT EXCHANGER OUTLET HOSE AS REQUIRED. LEAK AND OPERATIONAL CHECK I AW EMB145 MM 21-51-00 GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002071800135 20020718 00135 SW 2002 7 18 ALG2002F00052 1 20020601 A 6210 206015001119 BLADE BELL 206 206L4 1182110 SW MAIN ROTOR DEBONDED B ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 177AL 673 52157 DISCOVERED DURING ROUTINE AIRFRAME INSPECTION. SPAR LEADING EDGE EXFOLIATED ALONG ENTIRE LENGTH OF BLADE, SKIN/SPAR DIS BOND AT LOWER SURFACE STA 58.5, CAUSED BY IMPROPER HEAT TREATING. REVIEW MANUFACTURING PROCESS AND IMPROVE QUALITY CONT ROL. 1 G 7 1 3U NC H2SW 2002071800136 20020718 00136 GL 2002 7 18 ALG2002F00053 2 20020618 A 7210 23071895 GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX MISMANUFACTURED B ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 7210 167 53230 CAE847257 ENGINE WAS REMOVED DUE TO MAKING METAL. UPON DISASSEMBLY AND INSPECTION OF PARTS, FOUND T/M GEAR TEETH RADIUS ROUGH AND UNFINISHED MACHINING CAUSING PINION GEAR TO GALL. IMPROPER AND UNFINISHED MACHINING OF T/M GEAR CAUSING PINION GEAR TE ETH TO GALL. ASSURE PROPER MACHINING AT FACTORY. 1 G 7 1 3U 3 U O H2SW E1GL 2002071800137 20020718 00137 GL 2002 7 18 ALG2002F00054 2 20020215 A 7210 23071895 GEAR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL GEARBOX MISMANUFACTURED B ALGA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 31211 965 760225 GEARBOX WAS DISASSEMBLED DUE TO ENGINE CHIP LIGHT. IMPROPER MACHINING AND MESHING OF GEAR TEETH, CAUSING PINION GEAR TO GALL. ALSO CAUSED EXCESSIVE METAL CONTAMINATION. ASSURE PROPER MACHINING AND MECHING OF GEAR TEETH AT FACTORY. 1 G 7 2 3U 3 U H1NE E1GL 2002071800138 20020718 00138 2002 7 18 C2XA02CL135 4 20020627 A 3452 7510700726 TRANSPONDER EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 18557 188 145596 CLE FLIGHT 3040 THE CREW REPORTED THE NR 1 AND NR 2 TRANSPONDERS WERE INOPERATIVE IN CRUISE ABOUT HALF AN HOUR OUT OF CL EVELAND. THEY ALSO REPORTED THE NR 2 COMM FAILED. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDE NT. MAINTENANCE INSPECTED AND REPLACED BOTH RCZ'S. OPERATIONAL CHECKS WERE PERFORMED WITH NO DEFECTS FOUND. THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002071800139 20020718 00139 SW 2002 7 18 ALG2002F00055 1 20020316 A 6720 407001732101 BELLCRANK BELL 407 407 1182206 SW TAIL ROTOR DAMAGED B ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 537AL 294 53230 DURING SERVICE CHECK, NAS BOLT BORE ELONGATED ON SINGLE EAR OF BELLCRANK. MODIFY WITH STEEL TOP-HAT BUSHING. 1 G 7 1 3U O H2SW 2002071800140 20020718 00140 SO 2002 7 18 C2XA02CL136 1 20020627 A 2612 3601133500 FIRE LOOP EMB 135 EMB135LR 3260305 SO NR 2 ENGINE CHAFED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 15527 145413 DTW FLIGHT 3318 THE CREW REPORTED A NR 2 FIRE DETECT FAIL MESSAGE ON TAKEOFF. THE TAKEOFF WAS ABORTED AND AIRCRAFT RETU RNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FIRE LOOP DETECTOR AND CLEANED THE NR 2 ENGINE FIR E BOTTLE CANNON PLUG. 2 L 7 2 4F RT T00011AT 2002071800141 20020718 00141 GL 2002 7 18 ALG2002F00056 2 20020410 A 7310 47104 NOZZLE BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL FUEL SYSTEM BENT B ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 3186P 45776 DURING TESTING OF NOZZLE. FOUND ORIFACE BENT CAUSING STREAKS IN SPRAY. 1 G 7 1 3U 3 U H2SW E1GL 2002071800142 20020718 00142 GL 2002 7 18 ALG2002F00057 2 20020318 A 7250 23053299 TURBINE WHEEL SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL ENGINE CORRODED B ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 707AL 863 760189 TURBINE WAS REMOVED FROM AIRCRAFT DUE TO LOW POWER. REMOVED COMBUSTION SECTION AND FOUND SULPHADATION ON NR 1 WHEEL BLA DES. 1 G 7 2 3U 3 U H1NE E1GL 2002071800143 20020718 00143 SO 2002 7 18 C2XA02CL137 1 20020628 A 3350 74441 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14945 145049 CLE FLIGHT 3297 THE CREW REPORTED THE EMERGENCY EXIT ROW LIGHT ABOVE FA SEAT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002071800144 20020718 00144 SO 2002 7 18 C2XA02CL138 1 20020629 A 3350 66368 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 14998 145302 CLE FLIGHT 3230 THE CREW REPORTED THE AISLE PATH EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002071800145 20020718 00145 GL 2002 7 18 C2XA02CL139 2 20020630 A 7230 COMPRESSOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE STALLED A C2XA C ABORTED TAKEOFF R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT TO TAKEOFF 1 SW 27 11547 1028 145563 CAE312072 ORF FLIGHT 3037 THE CREW REPORTED THE NR 1 ENGINE DID A COMPRESSOR STALL WHEN TAKEOFF POWER WAS APPLIED. THE ITT ALSO I NCREASES TO 920 DEGREES. MAINTENANCE REPLACED THE NR 1 ENGINE. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002071800146 20020718 00146 EU 2002 7 18 KBMA117609 1 20020608 A 6510 593404 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE NR 3 DRIVESHAFT WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 345SH 1531 3345 (BEARING) NR 3 DRIVE SHAFT BEARING, WORN. REPLACED WITH NEW BEARING. 1 G 7 1 3U 3 U H9EU E19EU 2002071800147 20020718 00147 SO 2002 7 18 C2XA02CL140 1 20020630 A 2612 WARNING SYSTEM EMB 145 EMB145 3260210 SO COCKPIT MALFUNCTIONED A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 13970 145146 BDL FLIGHT 3292 THE CREW REPORTED A NR 2 ENGINE FIRE DETECTOR FAIL MESSAGE DURING CRUISE. THE AIRCRAFT LANDED WITHOUT F URTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF FIRE DETECTOR SYSTEM. OPERATIONAL CHECKS WE RE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE 2 L 7 2 4F RT T00011AT 2002071800148 20020718 00148 SO 2002 7 18 C2XA02CL143 1 20020705 A 3350 744412 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 13935 145022 CLE FLIGHT 4007 THE CREW REPORTED THE EMERGENCY LIGHT ON THE WALL FACING SEAT 3A WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002071800149 20020718 00149 SO 2002 7 18 C2XA02CL145 1 20020705 A 2120 ODOR EMB 135 EMB135ER 3260203 SO CABIN DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14508 145220 CLE FLIGHT 3149 THE CREW REPORTED A BURNT RUBBER SMELL WITH THE PACK SYSTEM ON. MAINTENANCE INSPECTED AND PERFORMED OPE RATIONAL CHECKS OF THE PACK SYSTEM. NO DEFECTS WERE NOTED. 2 L 7 2 4F RT T00011AT 2002071800150 20020718 00150 EU 2002 7 18 KBMA117610 1 20020614 A 2150 902V1651 BRUSHES SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE EVAPORATOR MOTOR FAILED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 1408 3296 FORWARD AIR CONDITIONER EVAPORATOR MOTOR, INOPERATIVE. REPLACED BRUSHES. 1 G 7 1 3U 3 U H9EU E19EU 2002071800151 20020718 00151 EU 2002 7 18 KBMA117611 1 20020614 A 5420 TL100AXE12L50DIL LATCH SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE COWL WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 1408 3296 RIGHT REAR ENGINE COWL LATCH WAS WORN. REPLACED WITH NEW LATCH. 1 G 7 1 3U 3 U H9EU E19EU 2002071800152 20020718 00152 NE 2002 7 18 KBMA117612 2 20020615 A 7532 9550158260 BLEED VALVE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE STICKING E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 33 2300 BLEED VALVE WAS STICKING. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002071800153 20020718 00153 EU 2002 7 18 KBMA117614 1 20020609 A 7160 350A54108004 INTAKE SNIAS 350 AS350BA 8680817 EU FUSELAGE CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 1188P 2347 AIR INTAKE WAS CRACKED ON UPPER SIDE. REPLACED WITH REPAIRED SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2002071800154 20020718 00154 EU 2002 7 18 KBMA117616 1 20020623 A 2910 12TW13 SWITCH SNIAS 350 AS350BA 8680817 EU HYD CUTOFF INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 5973 2957 HORN LIGHT WOULD NOT EXTINGUISH. REPLACED WITH SERVICEABLE HYDRAULIC CUTOFF SWITCH. 1 G 7 1 3U NC H9EU 2002071800155 20020718 00155 EU 2002 7 18 KBMA117617 1 20020613 A 2150 590008 COMPRESSOR SNIAS 350 AS350BA 8680817 EU AIR CONDITIONING INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 4886 2337 AIR CONDITIONER BELT MELTED. REMOVED AND REPLACED COMPRESSOR WITH OVERHAULED UNIT. 1 G 7 1 3U NC H9EU 2002071800156 20020718 00156 2002 7 18 KBMA117618 4 20020609 A 2300 DISPLAY SNIAS 350 AS350BA 8680817 EU RADIO MALFUNCTIONED E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 230SH 4866 2337 DIGITAL DISPLAY FLICKERING. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2002071800157 20020718 00157 EU 2002 7 18 KBMA117620 1 20020617 A 4997 WIRE SNIAS 350 AS350BA 8680817 EU APU BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 1864 A/C WILL NOT ACCEPT APU POWER. REPAIRED BROKEN WIRE PG/NE INOPERATIVE IN AFT BAGGAGE COMPARTMENT. 1 G 7 1 3U NC H9EU 2002071800158 20020718 00158 EU 2002 7 18 KBMA117621 1 20020623 A 2432 100FU01050 FUSE SNIAS 350 AS350BA 8680817 EU BATTERY SWITCH FAILED E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 350SH 5973 2957 NO POWER WHEN BATTERY SWITCH IS DEPRESSED. REPLACED 50 AMP FUSE. 1 G 7 1 3U NC H9EU 2002071800159 20020718 00159 SO 2002 7 18 C2XA02CL146 1 20020710 A 3397 WIRE HARNESS EMB 135 EMB135LR 3260305 SO CABIN FAULTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 29515 145309 CLE FLIGHT 3462 THE CREW REPORTED A ELECTRICAL SMELL COMING FROM SIDE WALL PANEL AT ROW 4A. MAINTENANCE INSPECTED AND F OUND A MELTED PLASTIC CONNECTOR FOR THE CABIN LIGHT BULB. THE AIRCRAFT WAS RELEASED FOR SERVICE. REPLACED SIDEWALL LIG HTING HARNESS ASSEMBLY IAW EMB145 MM 33-21-00 OPS. 2 L 7 2 4F RT T00011AT 2002071800160 20020718 00160 EU 2002 7 18 KBMA117623 1 20020619 A 6310 AM542 COMBINING BOX SNIAS 350 AS350B1 8680811 EU TRANSMISSION INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 6044 2009 ICS INOPERATIVE. REPLACED WITH SERVICEABLE COMBINING BOX. 1 G 7 1 3U H9EU 2002071800161 20020718 00161 EU 2002 7 18 KBMA117625 1 20020610 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH LINK WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 1387 3296 NR 1 TAIL ROTOR, P/C LINK ROD WORN BEYOND LIMITS. REPLACED WITH OVERHAULED P/C LINK. 1 G 7 1 3U H9EU 2002071800162 20020718 00162 EU 2002 7 18 KBMA117626 1 20020610 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH LINK CHIPPED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 3296 NR 2 TAIL ROTOR P/C LINK. BUSHING CHIPPER AND CRACKED. REPLACED WITH OVERHAULED P/C LINK. 1 G 7 1 3U H9EU 2002071800163 20020718 00163 EU 2002 7 18 KBMA117627 1 20020610 A 6520 350A33200406 BUSHING SNIAS 350 AS350B2 8680813 EU T/R SPIDER WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 1174 3296 SPLIT BUSHING WORN ON TAIL ROTOR SPIDER. REPLACED WITH SERVICEABLE SPIDER ASSEMBLY. 1 G 7 1 3U H9EU 2002071800164 20020718 00164 EU 2002 7 18 KBMA117628 1 20020619 A 6510 7A3819 BUSHING SNIAS 350 AS350BA 8680817 EU TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 10756 2300 NR 3 TAIL ROTOR DRIVE SHAFT OUTER RUBBER BUSHING WORN. REPLACED WITH NEW. 1 G 7 1 3U NC H9EU 2002071800165 20020718 00165 EU 2002 7 18 KBMA117629 1 20020619 A 6720 350A27191120 BEARING SNIAS 350 AS350BA 8680817 EU T/R CONTROL WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 2300 TAIL ROTOR CONTROL, PUSH/PULL TUBE BEARING EXCESS LIMIT. REPLACED BUSHINGS WITH NEW. 1 G 7 1 3U NC H9EU 2002071800166 20020718 00166 EU 2002 7 18 KBMA117630 1 20020625 A 2560 504084401 INERTIA REEL SNIAS 350 AS350B2 8680813 EU SEAT BELT BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 3710 3141 REEL LOCKS UP/ LOCKING MECHANISM BROKEN. REPLACED WITH SERVICABLE SEATBELT. 1 G 7 1 3U H9EU 2002071800167 20020718 00167 EU 2002 7 18 KBMA117631 1 20020624 A 6720 350A27119120 BEARING SNIAS 350 AS350BA 8680817 EU T/R CONTROL WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 9112 1864 NR 1 AND NR 4 TAIL ROTOR CONTROL TUBE FLANGE GUIDE BEARINGS, WORN. REPLACED WITH NEW. 1 G 7 1 3U NC H9EU 2002071800168 20020718 00168 NE 2002 7 18 KBMA117632 2 20020612 A 7532 9550158260 BLEED VALVE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE STICKS E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 2957 BLEED VALVE STICKS OPEN. REPLACED WITH SERVICEABLE BLEED VALVE. 1 G 7 1 3U 3 U NC H9EU E19EU 2002071800169 20020718 00169 GL 2002 7 18 C2XA02CL150 2 20020714 A 7313 3035060 FUEL NOZZLE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 ENGINE MALFUNCTIONED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13989 145271 CAE311432 CLE FLIGHT 3299 THE CREW REPORTED A BURNING EXHAUST FUME SMELL DURING ICE TEST. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002071800170 20020718 00170 EU 2002 7 18 KBMA117633 1 20020617 A 3340 DSQ201 SWITCH SNIAS 350 AS350BA 8680817 EU TAXI LIGHT INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 9078 1864 TAXI LIGHT SWITCH INOPERATIVE. REPLACED WITH NEW SWITCH. 1 G 7 1 3U NC H9EU 2002071800171 20020718 00171 EU 2002 7 18 KBMA117634 1 20020617 A 2400 23312P SOCKET SNIAS 350 AS350BA 8680817 EU FUSE BROKEN D KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 9078 1864 FUSE HOLDER BROKEN. REPLACED WITH SERVICEABLE ITEM. 1 G 7 1 3U NC H9EU 2002071800172 20020718 00172 EU 2002 7 18 KBMA117636 1 20020628 A 7921 95092 BLOWER SNIAS 350 AS350BA 8680817 EU OIL COOLER INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 386 1864 OIL COOLER BLOWER WAS INOPERATIVE. REPLACED WITH OVERHAULED BLOWER FAN. 1 G 7 1 3U NC H9EU 2002071800173 20020718 00173 EU 2002 7 18 KBMA117638 1 20020630 A 7900 55S15 CLAMP SNIAS 350 AS350B2 8680813 EU OIL VENT LINE CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 1485 3296 ENGINE OIL VENT LINE CLAMP WAS CRACKED. REPLACED WITH NEW CLAMP. 1 G 7 1 3U H9EU 2002111800086 20021118 00086 NM 2002 11 18 C7WA200200010 1 20020713 A 5311 FRAME BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND FUSELAGE FRAME AT BS 1110 WITH LEVEL 2 CORROSION AND HOLE DAMAGED IN UPPER SECTION BETW EEN STRINGER 27L AND STRINGER 29L. REPAIRED FUSELAGE FRAME UPPER SECTION AT BS 1110 BETWEEN STRINGER 25L AND 27L IAW SRM 51-40-3. (M) 2 L 7 3 4F A3WE 2002071800174 20020718 00174 EU 2002 7 18 KBMA117639 1 20020626 A 6720 350A27119120 GUIDE SNIAS 350 AS350BA 8680817 EU TAIL ROTOR WORN A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 5992 2957 NR 5 INNER FLANGE GUIDE WAS WORN. REPLACED WITH NEW GUIDE. 1 G 7 1 3U NC H9EU 2002071800175 20020718 00175 EU 2002 7 18 KBMA117640 1 20020628 A 6230 350A37105720 TAPE SNIAS 350 AS350B2 8680813 EU M/R MAST WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 1473 3296 MAST TAPE WAS TORN AND WORN. REPLACED WITH NEW TAPE. 1 G 7 1 3U H9EU 2002071800176 20020718 00176 EU 2002 7 18 KBMA117642 1 20020626 A 6720 350A33214501 PITCH LINK SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 3713 3141 TAIL ROTOR PC LINK WAS REMOVED. REPLACED WITH SERVICEABLE PC LINK. 1 G 7 1 3U H9EU 2002071800177 20020718 00177 SW 2002 7 18 KBMA133853 1 20020510 A 5302 AN47A BOLT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL VERTICAL FIN SHEARED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 73DP 1231 2513 VERTICAL FIN SUPPORT BRACKETT BOLT SHEARED. REPLACED WITH NEW BOLT. 1 G 7 1 3U 3 U H2SW E4CE 2002071800178 20020718 00178 GL 2002 7 18 KBMA133854 2 20020510 A 7421 CH34168 IGNITER BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE SHEARED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 73DP 12317 2513 IGNITER WORN AND SHEARED. REPLACED WITH NEW IGNITER. 1 G 7 1 3U 3 U H2SW E4CE 2002071800179 20020718 00179 SW 2002 7 18 PG92002F00001 1 20020601 A 6730 206076062003 SERVO BELL 206 206L1 1182107 SW ALLSN 250B 250B* GL MAIN ROTOR LEAKING E PG9A K NONE O OTHER IN INSP/MAINT 1 WP 19 2072M 18887 2103 45720 MAIN ROTOR SERVO EXCESSIVE LEAKS. REPLACED SERVO, PROBLEM CURED. 1 G 7 1 3U 3 T H2SW E10CE 2002071800180 20020718 00180 EU 2002 7 18 TXE2002F00000 1 20020614 A 3212 205131 BRACKET UROCOP EC120 EC120B 8680987 EU FLOAT CORRODED E TXEA K NONE O OTHER IN INSP/MAINT 1 SW 09 116KG 940 1152 DURING A GROUND HANDLING OPERATION, IT WAS DISCOVERED THE FLOAT ASSEMBLIES OFFERED RESISTANCE TO MOVEMENT, SWINGING FROM A FIXED FLIGHT POSITION, TO A GROUND HANDLING POSITION. FURTHER INVESTIGATION REVEALED, THE RIGHT FORWARD ATTACH BRACK ET OF THE FLOAT ASSEMBLY WAS CORRODED/CRACKED. THE (ALUMINUM) FIXED BRACKETS, FOR/AFT ARE ATTACHED TO THE INSIDE OF THE BOX-BEAM SUPPORT OF EACH FLOAT ASSEMBLY, THROUGH A BOLT/WASHER ATTACHMENT. THE MAIN BODY OF EACH BRACKET, SECURED INSI DE THE BOX BEAM, ONLY REVEALS THE AIRFRAME ATTACH POINT OF EACH BRACKET, RENDERING THE MAJORITY OF THE BRACKET HIDDEN WE N INSTALLED. WITH THE DISCOVERY OF THE DISCREPANT BRACKET, THE FLOAT ASSEMBLIES WERE REMOVED FROM THE AIRCRAFT, TO REMO 1 G 7 2 3U NC R0001RD 2002071800181 20020718 00181 SW 2002 7 18 ALG2002F00051 1 20020613 A 6510 407040303109 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL NR 1 T/R DSHAFT FAILED E ALGA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SW 03 647AL AFS287 53357 BEARING FAILED IN FLIGHT. MAJOR BEARING FAILURE. 1 G 7 1 3U 3 U O H2SW E1GL 2002111800092 20021118 00092 NM 2002 11 18 C7WA200200013 1 20020713 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 22L BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRING ER 22L FROM BS 720E PLUS 4.00 TO BS 740 IAW SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2002111800100 20021118 00100 NM 2002 11 18 C7WA200200019 1 20020713 A 5312 BULKHEAD BOEING 727 727232 1384082 NM FUSELAGE CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND FUSELAGE BS 178 BULKHEAD WITH CRACK BETWEEN LBL 4.00 AND LBL 10.00 BETWEEN WL 232.T AND WL 238.5. REPAIRED CRACKED WEB IAW SRM 53-10-9 FIG 4. (M) 2 L 7 3 4F A3WE 2002111800101 20021118 00101 NM 2002 11 18 C7WA200200020 1 20020713 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE DENTED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND DENT AT BS 421 BETWEEN STRINGER 16R AND 17R. REPAIRED FUSELAGE SKIN FROM BS 416.25 TO BS 428 BETWEEN STRINGER 16R AND STRINGER 18R IAW SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 2002111800102 20021118 00102 NM 2002 11 18 C7WA200200021 1 20020713 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE DENTED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENT AT BS 360 BETWEEN STRINGER 16L AND 17L. REPAIRED FUSELAGE SKIN FROM BS 360 TO BS 371.50 BETWEEN STRINGER 16L AND STRINGER 21L IAW SRM 53-30-4 FIG 12. (M) 2 L 7 3 4F A3WE 2002111800106 20021118 00106 NM 2002 11 18 C7WA200200024 1 20020713 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 203.8 BETWEEN RIGHT WL 219 AND WL 220. REPAIRED FUS ELAGE SKIN FROM BS 191.0 TO BS 209.0 BETWEEN WL 214 AND 224.5 RBL 38.0 IAW S/B 727-53-0183 SECTION III PART I PARA C. ( M) 2 L 7 3 4F A3WE 2002111800108 20021118 00108 NM 2002 11 18 C7WA200200026 1 20020713 A 5280 SKIN BOEING 727 727232 1384082 NM NLG DOOR DELAMINATED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION AT , FOUND NLG LEFT AFT DOOR DELAMINATED. REPAIRED DELAMINATION IAW COOPESA EO COO-CMP-2-52-3 69-02 WITH DER APPROVAL. (M) 2 L 7 3 4F A3WE 2002111800126 20021118 00126 NM 2002 11 18 C7WA200200027 1 20020713 A 5751 652176633 SKIN PANEL BOEING 727 727232 1384082 NM AILERON DELAMINATED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND LT WING OUTBOARD AILERON TRAILING EDGE PANEL DELAMINATED. REPAIRED LEFT WING OUTBOARD AILERON IAW COOPESA EO COO0CMP-2-57-366-02 WITH DER APPROVAL. (M) 2 L 7 3 4F A3WE 2002071800182 20020718 00182 NM 2002 7 18 CW7A200200011 1 20020713 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION FOUND LEVEL 2 CORROSION ON STR 29R FROM BS 480 TO BS 540. REPLACED STR 29R SECTION BETWEEN BS 480 AND BS 545 IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2002071800183 20020718 00183 NM 2002 7 18 AWXA200200547 1 20020604 A 5315 6546540 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 YVR - MAJOR REPAIR - DURING C-15 INSPECTION A CRACK WAS FOUND ON A FLOORBEAM WEB AT BS 639 BETWEEN RIVETS AT STA RBL 64. MAINTENANCE REPAIRED CABIN FLOOR BEAM BS 639 WEB RBL 64 IAW AWA ER 15-5310-02168-JS1. 2 L 7 2 4F RT A16WE 2002071800184 20020718 00184 NM 2002 7 18 AWXA200200549 1 20020622 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 PHX - MAJOR REPAIR - DURING INSPECTION A CRACK WAS FOUND ON THE FORWARD UPPER CORNER OF THE INTERCOASTAL LOCATED BETWEEN FLOORBEAMS AT BS 328-344, LBL 45. MAINTENANCE REMOVED DAMAGED SECTION OF INTERCOASTAL, FABRICATED 3 EACH REPAIR ANGLES , 2 CHANNELS, AND 1 FILLER AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2002071800185 20020718 00185 NM 2002 7 18 AWXA200200551 1 20020623 A 3350 BR964411 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 322AW 25400 LAS - EEL - EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 6 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ES CAPE PATH LIGHT ASSEMBLY AT SEAT ROW 6 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002071800186 20020718 00186 NM 2002 7 18 AWXA200200556 1 20020620 A 5320 654581225 STIFFENER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - MAJOR REPAIR - DURING INSPECTION A 1/4 INCH CRACK WAS FOUND ON FLOORBEAM SUPPORT ANGLE (STIFFENER) AT BS 328, RBL 40. MAINTENANCE REMOVED CRACKED STIFFENER AT RBL 40, BS 328, FABRICATED A NEW STIFFENER, AND INSTALLED REPAIR IAW DWG 65 -45812, AND B737-300 SRM 51-40-02, PG 3 & 10. 2 L 7 2 4F RT A16WE 2002071800187 20020718 00187 GL 2002 7 18 ALG2002F00058 2 20020416 A 7310 47104 SHROUD BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL FUEL NOZZLE DEFECTIVE B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 3186P 45776 DURING TESTING OF NOZZLE, WHEN NOZZLE WAS TORN DOWN FOR REPAIR, FOUND UNSERVICEABLE. NEW SHROUD FROM STOCK WAS DEFECTIV E FROM FACTORY. TRIED TO REASSEMBLED SHROUD AND PARTS WOULD NOT PROPERLY FIT. 1 G 7 1 3U 3 U H2SW E1GL 2002071800190 20020718 00190 NM 2002 7 18 SCNA02004 1 20020715 A 2922 654479011 FILTER HOUSING BOEING 737 7378Q8 13844BX NM A SCNA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 801SY 2186 30332 Hydraulic "A" system RF after landing. Fault code 293 180 00. Found filter bowl assembly disengaged from filter. Remove d & replaced hydraulic system "A" return filter IAW Task 2-11-61-000-802, ops checks good. 2 L 7 2 4F RT A16WE 2002071800191 20020718 00191 EU 2002 7 18 MALA020410 1 20020717 A 2150 7769106 ACM SAAB SF340 340B 7860101 EU A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 447XJ 340B447 DURING FLIGHT #2701, INFLIGHT BURNING SMELL IN COCKPIT NOT IN CABIN. COCKPIT DID NOT COOL DOWN, AUTO OR MANUAL. ON FIN AL, BURNING SMELL INTENSIFIED. WAS TOLD BY FLIGHT ATTENDANT SHE COULD SMELL IT ALSO. NON-NORMAL SOUND COMING FROM BACK OF THE A/C. MAINTENANCE REMOVED AND REPLACED RIGHT ACM PN 776910-6 IAW TASK CARD 215181, SN/ON 960645.SN/OFF 900776. 2 L 7 2 4T RT A52EU 2002071800192 20020718 00192 NM 2002 7 18 AWXA200200631 1 20020620 A 5330 6545800598 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4" CRACK WAS FOUND ON EXTERNAL FUSELAGE SKIN AT THE R1 DOOR CUTOUT FORWARD LO WER CORNER; CRACK RUNS FROM THE EDGE OF A COUNTER SUNK FASTENER TO THE EDGE OF CUTOUT, BS 301. MAINTENANCE TRIMMED OUT D AMAGE ON FUSELAGE SKIN AT THE R1 DOOR CUTOUT BS 301, AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXISIT. FABRICATE D 3 EACH FILLERS, 3 EACH REPAIR PLATES, AND INSTALLED REPAIR PARTS IAW 03-5330-02197-SS2. 2 L 7 2 4F RT A16WE 2002071800193 20020718 00193 NM 2002 7 18 AWXA200200632 1 20020626 A 5311 66558722 FRAME BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK HFEC INSPECTION IDENTIFIED A 1 5/8" CRACK RUNNING FROM A FASTENER HOLE ON THE FOR WARD FRAME AT THE PAN COMMON TO THE #3 STOP OF THE L2 DOOR, BS 956. MAINTENANCE TRIMMED OUT CRACK IN FRAME AT BS 956. PE RFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED 3 EACH REPAIR FILLERS, A REPAIR ANGLE, A SEAL FITTING, A ND A STRAP, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5330-02197-SS3. 2 L 7 2 4F RT A16WE 2002071800194 20020718 00194 NM 2002 7 18 AWXA200200633 1 20020620 A 5330 6545800589 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK AFTER REMOVING AN EXISTING REPAIR DOUBLER FOR A DENT IN SKIN, 2 EACH CRACKS WERE FOUND EXTENDING PAST STOP DRILL HOLES AT BS 326, WL 206, AND BS 328, WL 204. MAINTENANCE TRIMMED OUT SKIN, DOUBLER, AND STRAP AT BS 326, WL 206, AND BS 328, WL 204. PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A INNER P LATE, A MIDDLE PLATE, AN OUTER PLATE, 2 EACH FILLERS, AND 2 EACH TAPERED FILLERS, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5330-02197-SS1. 2 L 7 2 4F RT A16WE 2002071900001 20020719 00001 NM 2002 7 19 SWAA021530 1 20020707 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUT OUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071900002 20020719 00002 NM 2002 7 19 SWAA021531 1 20020709 A 7722 D1208P CONNECTOR BOEING 737 7373H4 1384600 NM CFM56 CFM56* 13802 NE NR 1 ENGINE DAMAGED A SWAA D RETURN TO BLOCK J M WARNING INDICATION OVER TEMP CL CLIMB 1 SW 29 656SW 28401 721390 AIRTURN BACK, INFLIGHT SHUTDOWN, OVERTEMP ON NR 1 ENG EGT WENT TO 1200 DEGREES DURING CLIMB AT 33,000 FT. RETARDED THRO TTLE TO IDLE, EGT IND WENT BLANK BUT RED LIGHT REMAINED ILLUMINATED UNTIL ENG WAS SHUT DOWN. FOUND EGT CONNECTOR D1208P DAMAGED. REMOVED AND REPLACED EGT CONNECTOR D1208P PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002071900003 20020719 00003 2002 7 19 SWAA021517 4 20020709 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT SVC DOOR DISCONNECTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR LANYARD CABLE DISCONNECTED. CONNECTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002071900004 20020719 00004 NM 2002 7 19 SWAA021518 1 20020709 A 2120 215201 GASPER FAN BOEING 737 7372H4 138448C NM A/C COMP OVERTEMP A SWAA K NONE O OTHER CL CLIMB 1 SW 29 081SW 22730 DURING CLIMB ELECTRICAL FUMES IN COCKPIT AND CABIN. WITH GASPER AIR FAN OFF FUMES WENT AWAY. REMOVED AND REPLACED GASP ER FAN PER MM. 2 L 7 2 4F A16WE 2002071900005 20020719 00005 NM 2002 7 19 SWAA021519 1 20020708 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 18R, BS'S 727E AND 747. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 2002071900006 20020719 00006 NM 2002 7 19 SWAA021520 1 20020709 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D PLUS 5, ABOVE STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071900007 20020719 00007 NM 2002 7 19 SWAA021521 1 20020708 A 5753 6546435317 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED C2 CHECK, FOUND LT OTBD AFT T/E FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED LT OTBD AFT T/ E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002071900008 20020719 00008 NM 2002 7 19 SWAA021522 1 20020708 A 5330 589357 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED ON F/O NR 1 WINDOW POST AT OTBD UPPER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071900009 20020719 00009 NM 2002 7 19 SWAA021524 1 20020709 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 767 + 6, LBL 12.50. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002071900010 20020719 00010 NM 2002 7 19 SWAA021525 1 20020709 A 5753 6546434 FLAP BOEING 737 7377H4 1384404 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED PM CHECK, FOUND LT INBD T/E AFT FLAP CRACKED ON LOWER SURFACE. REPAIRED LT INBD T/E AFT FLAP PER SWA R A. 2 L 7 2 4F RT A16WE 2002071900011 20020719 00011 2002 7 19 SWAA021532 4 20020710 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD CABIN DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED C3 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT BAR ASSY'S OUT OF ADJUST. ADJUSTED BOTH FWD SLIDES PER MM. 2 L 7 2 4F RT A16WE 2002071900012 20020719 00012 NM 2002 7 19 SWAA021533 1 20020711 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 EEPLS COVER LOOSE AT ROW NR 2. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2002071900013 20020719 00013 NM 2002 7 19 SWAA021535 1 20020710 A 5330 6545768 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD RADIO ALTIMETER ANTENNA CUT OUT, BS 370 AND WL 148. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002071900014 20020719 00014 NM 2002 7 19 SWAA021536 1 20020711 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM LT/RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 744SW 29490 DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLA CED HARDWARE AND BUSHINGS ON ALL HINGE ATTACH POINTS PER MM. 2 L 7 2 4F RT A16WE 2002071900015 20020719 00015 NM 2002 7 19 SWAA021538 1 20020711 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR'S 7R AND 8R, AT BS 360 AND 480. REPAIRED FRA MES PER SRM. 2 L 7 2 4F RT A16WE 2002071900016 20020719 00016 NM 2002 7 19 SWAA021498 1 20020706 A 2910 NAS1611 O-RING BOEING 737 7372H4 138448C NM RT MLG W/W PINCHED A SWAA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 29 085SW 22826 DECLARED EMERGENCY, COMPLETE LOSS OF A SYSTEM HYDRAULIC FLUID. FOUND PINCHED O-RING AT PRESS MODULE. REMOVED AND REPLA CED O-RING PER MM. 2 L 7 2 4F A16WE 2002071900017 20020719 00017 NM 2002 7 19 SWAA021501 1 20020708 A 3350 604222 BATTERY BOEING 737 7373A4 1384585 NM CABIN ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT ILLUMINATED CONTINOUSLY. REMOVED AND REPLACED EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002071900018 20020719 00018 NM 2002 7 19 SWAA021503 1 20020708 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUT OUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071900019 20020719 00019 NM 2002 7 19 SWAA021504 1 20020707 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 767 PLUS 6, RBL 3. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002071900020 20020719 00020 NM 2002 7 19 SWAA021505 1 20020707 A 5311 6546569 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 927, STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002071900021 20020719 00021 NM 2002 7 19 SWAA021506 1 20020707 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 727 PLUS 5, LBL 12. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002071900022 20020719 00022 NM 2002 7 19 SWAA021508 1 20020708 A 5320 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 360, STR 17R AND WL 208. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2002071900023 20020719 00023 NM 2002 7 19 SWAA021510 1 20020708 A 5320 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R AND 15R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002071900024 20020719 00024 NM 2002 7 19 SWAA021511 1 20020708 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 323, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071900025 20020719 00025 NM 2002 7 19 SWAA021512 1 20020708 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D PLUS 5, ABOVE STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071900026 20020719 00026 NM 2002 7 19 SWAA021513 1 20020708 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, ABOVE STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002071900027 20020719 00027 NM 2002 7 19 SWAA021514 1 20020708 A 5311 6546569 FRAME BOEING 737 7373H4 1384600 NM AFT CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 955.5, WL 206 AND RBL 54. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002071900028 20020719 00028 NM 2002 7 19 SWAA021515 1 20020708 A 5510 6547985 RIB BOEING 737 7373H4 1384600 NM RT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED D CHECK, FOUND RT HORIZ STABILIZER RIB CRACKED AT STAB STA 120.3. REMOVED AND REPLACED RT HORIZ STAB L OWER RIB CHORD. 2 L 7 2 4F RT A16WE 2002071900029 20020719 00029 2002 7 19 SWAA021562 4 20020715 A 2565 D31591478 SLIDE BOEING 737 7375H4 138449D NM FWD ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED AT GATE. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002071900030 20020719 00030 NM 2002 7 19 SWAA021564 1 20020715 A 5510 65C25727 SKIN BOEING 737 7373H4 1384600 NM RT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED D CHECK, FOUND RT HORIZ STAB SKIN CRACKED ON LOWER SURFACE AT STAB STA 125. REPAIRED SKIN PER BFG ER. 2 L 7 2 4F RT A16WE 2002071900031 20020719 00031 2002 7 19 SWAA021565 4 20020715 A 2565 829934215 NUT PLATE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 102SW 23108 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CONTAINER ATTACH NUT PLATE MISSING. INSTALLED NUT PLATE AND REINSTALLED SLIDE PER MM. 2 L 7 2 4F A16WE 2002071900032 20020719 00032 NE 2002 7 19 SWAA021567 2 20020713 A 7240 CFM56 ENGINE BOEING 737 7377H4 1384404 NM CFM56 CFM56* 13802 NE RT WING OVERTEMP A SWAA D RETURN TO BLOCK J M WARNING INDICATION OVER TEMP CL CLIMB 1 SW 29 787SA 29812 876671 AIR TURN BACK, NR 2 ENG EGT IND OVERTEMP, (965 DEGREES FOR 1 SECOND). COMPLIED WITH ENG BOROSCOPE INSPECTION AND PWR AS SURANCE RUN. NO DAMAGE NOTED. OPS CK GOOD PER MM. MAINTENANCE FERRY TO PHX AND REMOVED AND REPLACED NR 2 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002071900033 20020719 00033 NM 2002 7 19 20027190202 1 20020619 A 3242 C20508000 BRAKE ASSY BOEING 767 767300 1385204 NM Zone 700 DRAGGING A FWTA K NONE Z SIGNIFICANT FAILURE REPORT NR NOT REPORTED 1 SO 19 316LA 30842 AIRCRAFT IS NEW FROM FACTORY AT TAC 822 AND TAC 737 CHANGED NUMBER 1 AND 5 BRAKE ASSY FOR STUCK AND HOT. TEAR DOWN OF THESE BRAKES REVEAL THAT ADJUSTER PINS WHERE CUT (SHEARED). THIS DID NOT ALLOW BRAKES TO PROPERLY RELEASE. BRAKE SERIAL NUMBERS 01705 AND 01706 2 L 7 2 4F RT A1NM 2002071900039 20020719 00039 GL 2002 7 19 ERAA080325 2 20020605 A 7200 ENGINE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NACELLE LEAKING H ERAA K NONE K FLUID LOSS IN INSP/MAINT 1 FS 01 292EH 6044 562 CAE836497 ENGINE ASSY LEAKING AT SPLIT LINE. PULLED STUDS ON GEARBOX AND RESET STUDS 1 G 7 2 3U 3 U H3EU E4CE 2002071900040 20020719 00040 WP 2002 7 19 211003001 1 20020612 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 191AJ 53191 AFT CARGO DOOR HANDLE CUT OUT CRACKED AND DEFORMED. INSTALLED REPAIR SCUFF PLATE IAW SRM. 2 L 7 2 4F RT A6WE 2002071900041 20020719 00041 WP 2002 7 19 211003002 1 20020612 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 191AJ 53191 MID CARGO DOOR HANDLE CUT OUT IS CRACKED AND DEFORMED. TRIMMED CRACKED AND DEFORMED AREA, FABRICATED AND INSTALLED REPA IR SCUFF PLATE IAW SRM. 2 L 7 2 4F RT A6WE 2002071900042 20020719 00042 WP 2002 7 19 211003003 1 20020612 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 191AJ 53191 FORWARD CARGO DOOR HANDLE CUT OUT IS CRACKED AND DEFORMED. INSTALLED REPAIR SCUFF PLATE IAW SRM. 2 L 7 2 4F RT A6WE 2002071900044 20020719 00044 WP 2002 7 19 211004002 1 20020616 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 MID CARGO DOOR HANDLE CUT OUT CRACKED AND DEFORMED. INSTALLED REPAIR SCUFF PLATE, MID CARGO DOOR HANDLE CUTOUT IAW SRM. 2 L 7 2 4F RT A6WE 2002071900045 20020719 00045 WP 2002 7 19 211004003 1 20020616 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 AFT CARGO DOOR HANDLE CUT OUT CRACKED AND DEFORMED. INSTALLED REPAIR SCUFF PLATE AFT CARGO DOOR CUT OUT IAW SRM. 2 L 7 2 4F RT A6WE 2002071900046 20020719 00046 WP 2002 7 19 211004004 1 20020617 A 5313 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 DENT AT STA 200 RIGHT SIDE LONGERON 23. FABRICATED AND INSTALLED REPAIR SKIN IAW SRM. 2 L 7 2 4F RT A6WE 2002071900050 20020719 00050 NM 2002 7 19 F3LA200200192 1 20020705 A 5320 65458752 SILL BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON R1 DOOR MOP SEAL AND THRESHOLD SUPPORT. REMOVED CORROSION PER SRM 53 -10-01 AND INSTALLED NEW MOP SEAL PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 2002071900055 20020719 00055 GL 2002 7 19 ERAA080337 2 20020611 A 7321 252464430 FUEL CONTROL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL ENGINE OUT OF ADJUST A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 124EH 6996 S559 FCU OUT OF CALIBRATION. METERING VALVE FUEL FLOW SETTING FOUND LOW 1 G 7 2 3U 3 U H3EU E4CE 2002071900056 20020719 00056 GL 2002 7 19 ERAA080338 2 20020611 A 7210 SHAFT BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE CORRODED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 124EH 13254 S559 CAE833283 ENGINE MAKING METAL. FOUND GEARSHAFT TEETH DAMAGED GEARBOX HOUSING CORRODED. ACTION TAKEN: INSTALLED NEW GEARSHAFT & O VERHAULED GEARBOX. 1 G 7 2 3U 3 U H3EU E4CE 2002071900057 20020719 00057 GL 2002 7 19 ERAA080339 2 20020611 A 7200 BEARING BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE MAKING METAL H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 124EH 15424 S559 CAE822403 ENGINE MAKING METAL. INITIAL INSPECTION FOUND COMPRESSOR ATTACHMENT HARDWARE LOOSE. 2 1/2 BEARING MAKING METAL. ACTION TAKEN: INSTALLED NEW 2 1/2 BEARING AND PTO GEAR. COMPLIED WITH CEB-A-1351 REPLACE OIL TUBE. 1 G 7 2 3U 3 U H3EU E4CE 2002071900058 20020719 00058 GL 2002 7 19 ERAA080340 2 20020612 A 7200 ENGINE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NACELLE MAKING METAL H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 298EH 7779 S845 CAE836452 ENGINE IS MAKING METAL. INITIAL INSPECTION FOUND COMPRESSOR ATTACHMENT HARDWARE LOOSE. 2 1/2 BEARING MAKING METAL, SPIN ADAPTER GEARSHAFT MAKING METAL. COMPRESSOR DUE 1750 INSPECTION. CHANGED CASE HALVES.ACTION TAKEN: INSTALLEDD NEW 2 1/ 2 BEARING INSTALLED NEW SPUR ADAPTER COMPLIANCE CEB-A-1386 - GEARBOX ASSY INSPECTION OF HELICAL TORQUEMETER GEARSHAFT. CHECKED AD2001-24-12. 1 G 7 2 3U 3 U H3EU E4CE 2002071900059 20020719 00059 NM 2002 7 19 DL72S020642 1 20020609 A 3260 WARNING SYSTEM BOEING 727 727225A 1384077 NM COCKPIT ACTIVATED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 8882Z 21579 CREW REPORTS NOSE GEAR UNSAFE INDICATION AND VIBRATION ON GEAR RETRACTION. JACKED NOSE AND SWUNG GEAR, ALL OPS NORMAL. 2 L 7 3 4F RT A3WE 2002071900060 20020719 00060 NM 2002 7 19 DL72S020691 1 20020620 A 5754 SPAR BOEING 727 727225A 1384077 NM L/E SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 FOUND ON B2 LETTER CK 1 IN CRACK NR 7 SLAT SPAR AT TAI DUCT CUTOUT UPPER INBD CORNER. REPAIRED PER MM 57-54-000-8 AND E RA. 2 L 7 3 4F RT A3WE 2002071900061 20020719 00061 EU 2002 7 19 ERAA080341 1 20020612 A 6420 10531714 HEAD BOLKMS 105 BO105S 5626006 EU TAIL ROTOR BINDING H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 125EH 5245 S562 TAILROTOR IS BINDING. PITCH CHANGE BUSHINGS WORN. TEFLON BUSHINGS WORN, CONTROL LEVER BOLTS AND BUSHINGS WORN, 2 SPAC ERS CORRODED, SEALS ROTTEN, END CAPS ROTTEN, THREADS STRIPPED ON ONE CONTROL LEVEL TO MOUNTING FORK BOLT, BLADE PAINT CR ACKING, 1 BLADE BOLT DAMAGED. ACTION TAKEN: DISASSEMBLED, CLEANED & VISUALLY INSPECTED. REPLACED CONTROL LEVER BOLTS & BUSHINGS, MOUNTING FORK TEFLON BUSHINGS, SPACERS SEALS & END CAPS. ASSEMBLED WITH 2 SERVICEABLE BLADES AND 1 NEW BLADE BOLT AND STATIC BALANCED. REPAIRED IAW BO105 REM 301, NM CHAPTER 34 & 107 TT 5244.8 TSI 305.4 1 G 7 2 3U H3EU 2002071900062 20020719 00062 NM 2002 7 19 DL72W020656 1 20020613 A 5753 652163234 SPAR BOEING 727 727247 138408F NM T/E FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 DURING ACCOMPLISHMENT OF TERMINATING ACTION ON NR 3 MIDFLAP REAR SPAR UPPER CHORD, CRACKED FASTENER HOLE WAS DISCOVERED. REPAIR PER ER/A 417400-14AD. 2 L 7 3 4F A3WE 2002071900063 20020719 00063 NM 2002 7 19 DL738020668 1 20020614 A 2560 P2070003001 FLASHLIGHT BOEING 737 737832 13844CF NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3768 29630 REMOVED AND REPLACED EMERGENCY FLASHLIGHT AT R2 FLIGHT ATT SEAT. 2 L 7 2 4F RT A16WE 2002071900064 20020719 00064 NE 2002 7 19 DL73K020636 2 20020607 A 7261 GARLOCK SEAL BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE LEAKING A DALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 27 382DL 49226 23609 709157 NR 1 ENG OIL QTY SHOWED A STEADY DECREASE AS FLIGHT PROGRESSED. ULTIMATELY QUANTITY WENT TO ZERO INDICATION. OIL TEMP AND PRESSURE REMAINED STEADY IN THE NORMAL RANGE AT ALL TIMES. FOUND NR 1 ENG GARLOCK SEAL AT STARTER LEAKING. REPLAC ED STARTER GARLOCK SEAL REF M/M 72-61-0. RAN ENG AT TAKEOFF POWER ALL NORMAL NO LEAKS. A/C OK FOR SVC. 2 L 7 2 4F 4 F A16WE E2EA 2002071900065 20020719 00065 NM 2002 7 19 DL73K020648 1 20020611 A 3397 WIRE BOEING 737 737247 138448D NM CABIN CHAFED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 242WA 23516 ON ARRIVAL FOUND RIGHT OVERWING EMERGENCY EXIT SIGN INOP. REPLACED EXIT SIGN OVERHEAD BATTERY AND BATTERY POWER SUPPLY, REPAIRED CANNON PLUG WIRING AT POWER SUPPLY DUE TO CHAFED WIRING. ALL CHECK NORMAL. 2 L 7 2 4F A16WE 2002071900066 20020719 00066 NM 2002 7 19 DL73K020649 1 20020611 A 3350 CONNECTOR BOEING 737 737232 1384475 NM CABIN DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 325DL 23097 ON LAYOVER FOUND EMERGENCY LIGHT AT ROW 19 INOP. FOUND CONNECTOR DISCONNECTED, RECONNECTED OPS NORMAL. 2 L 7 2 4F RT A16WE 2002071900067 20020719 00067 2002 7 19 DL73K020686 4 20020619 A 3442 20412170416 TRANSCEIVER BOEING 737 737232 1384475 NM COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 308DL 23080 EN ROUTE GOT R/T FAULT ON THE RADAR INDICATOR. REMOVED AND REPLACED RADAR TRANSCEIVER PER M/M. OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 2002071900068 20020719 00068 EU 2002 7 19 IO5R080345 1 20020710 A 6330 L633M2010101 MOUNT UROCOP EC135 EC135P1 8680990 EU TRANSMISSION FAILED H IO5R A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 FS 01 551BA 119 188 UNIT COLLASPED 1 MINUTE AFTER TAKE-OFF. ALL FLUID LEAKED OUT HIGH VIBRATION OVER 100 KNOTS. REMOVED AND REPLACED 1 G 7 2 3U O H88EU 2002071900069 20020719 00069 NE 2002 7 19 IO5R080346 2 20020710 A 7261 704A34621004 OIL FILTER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE CRACKED H IO5R O OTHER K FLUID LOSS CR CRUISE 1 FS 01 557CB 123 3431 AFTER MULTIPLE SEAL CHANGES, OBSERVES HAIRLINE CRACK IN MATING SURFACE REMOVED AND REPLACED 1 G 7 1 3U 3 U H9EU E19EU 2002071900071 20020719 00071 NM 2002 7 19 DL757020652 1 20020611 A 2120 ODOR BOEING 757 757232 1384965 NM CABIN DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 6704Z 30396 F/A, PASS, AND F/O OBSERVED ODOR OF BURNT POPCORN ON RT SIDE OF AIRCRAFT BETWEEN ROWS 31 AND 34. ODOR BEGAN AT 35,000FT AND RETURNED 2 TIMES DURING FLIGHT. ODOR DISSIPATED AFTER 10 MINUTES. NO ABNORMALITIES W/PES OR PACKS. DURING T/S AL L LAV HOT WATER HEATERS TURNED OFF. TURNED ON LAV WTR HTRS. INSPT ROW 31-34 DEF PSUS. CHECKS OK. REMOVED CEILING PAN ELS OVER 31-34 DEF NO PROBLEMS NOTED. CHECKED SEAT HARNESS AND SEBS CHECKED ALL READING AND ATTENDANT LIGHTS IN AREA. NO SMELL OR DEFECTS NOTED. 2 L 7 2 4F RT A2NM 2002071900072 20020719 00072 NM 2002 7 19 DL757020663 1 20020614 A 5230 146N66031 SKIN BOEING 757 757232 1384965 NM CARGO DOOR WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 607DL 22814 THE NR 2 CARGO DOOR OUTER SKIN WAS FOUND WORN BEYOND SRM LIMITS. REPAIR PER ER/A 417449-14. 2 L 7 2 4F RT A2NM 2002071900073 20020719 00073 SW 2002 7 19 JJWA080369 1 20020715 A 5320 206031106017S STIFFENER BELL 206 206A 1181508 SW FUSELAGE CRACKED H JJWA K NONE O OTHER IN INSP/MAINT 1 FS 01 281CB 10354 3303 FOUND STIFFNER CRACKED DURING INSPECTION - CRACK ORIGINATED IN LOWEST HI-LOCK FASTNER POSITION 2.875 1 G 7 1 3U H2SW 2002071900074 20020719 00074 NM 2002 7 19 DL757020665 1 20020614 A 3610 VALVE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 669DN 10897 25142 727290 AT FLT 350-370 LT ENG FLUCTUATED EPR 1.11-1.24, EGT 438-460 AND N1 79.1-82.2. DUCT PRESS FLUX 30-60 PSI. MCC REQUESTED TURN OFF LT BLEED AND FLUX STOPPED. DIVERTED TO MCO DUE TO EN ROUTE WX. PERF PFHB TEST 06 AND 13, NO ANOMALIES NOTED. REPLACED HIGH STAGE PILOT VALVE PER FIM 36-11-08. PERF HS PILOT TEST PER AMM 36-11-08 715 085. OPER CKS NORMAL. LEA K CKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002071900075 20020719 00075 NM 2002 7 19 DL757020678 1 20020617 A 3397 WIRE BOEING 757 757232 1384965 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 669DN 25142 EMERGENCY EXIT LIGHTS (IN SEAT) INOP FROM ROW 27DEF TO 37DEF, REPAIRED BROKEN PWR SUPPLY WIRE AT SEAT 27DEF. CHECKS OK. 2 L 7 2 4F RT A2NM 2002071900077 20020719 00077 NM 2002 7 19 DL757020680 1 20020615 A 2121 6067723 FAN BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 27 694DA 29726 ON FINAL APPROACH STRONG SMELL OF SMOKE, 30 SEC LATER RT RECIRC INOP LIGHT ILLUMINATED AND RT FAN MESSAGE. R&R RT RECIR C FAN. 2 L 7 2 4F RT A2NM 2002071900079 20020719 00079 NM 2002 7 19 DL757020690 1 20020620 A 2560 MV10 MEGAPHONE BOEING 757 757232 1384965 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 681DA 26957 CRACKED PLASTIC AROUND MOUTHPIECE. REMOVED AND REPLACED MEGAPHONE. 2 L 7 2 4F RT A2NM 2002071900082 20020719 00082 SO 2002 7 19 2002F00758 2 20020711 A 8530 646657A2 CYLINDER HEAD CESSNA 414 414A 2075907 CE CONT O520 TSIO520NB 17040 SO LT ENGINE CRACKED B BIGA E ENGINE SHUTDOWN D INFLIGHT SEPARATION CL CLIMB 1 NM 04 414PG 414A0811 514461 CYLINDER HEAD SEPERATED FROM BARREL DURING CLIMB OUT. ENGINE FEATHERED AND AIRCRAFT LANDED SAFTELY. CYLINDER HEAD CRACKE D ABOVE THREADED AREA TO BARREL. 1 L 7 2 3O 3 O A7CE E8CE 2002071900083 20020719 00083 NM 2002 7 19 DL764020659 1 20020613 A 1430 114T41457 BOLT BOEING 767 767424ER 1385270 NM L/E SLAT BROKEN A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 830MH 29701 AFTER PUSHBACK WHILE LOWERING FLAPS/SLATS GOT LEADING EDGE SLAT DISAGREE. FOUND BROKEN BOLT FOR PROX SWITCH TARGET AND TARGET MISSING. REINSTALLED SAME. 2 L 7 2 4F RT A1NM 2002071900084 20020719 00084 NM 2002 7 19 VNAA0207006 1 20020704 A 3200 SHIM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 471PS 3007 AFTER LANDING IN CAK, THE NOSE GEAR AND MAIN GEAR INDICATION WAS NORMAL AND GREEN. HOWEVER, THE GEAR HANDLE WAS FLASHIN G AND THE AURAL HORN WAS HEARD. MAINTENANCE INSPECTED AND FOUND THE DOWN LOCK PROXI SENSOR TO BE OUT OF GAP .030 ON TH E BACK SIDE. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE THEN INSPECTED AND REPLACED THE SHIMS IN ACCORDANCE WI TH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002071900085 20020719 00085 NM 2002 7 19 VNAA0207008 1 20020709 A 3300 501122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FWD FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 426JS 15688 1510 3038 THE CREW REPORTED THAT THE FORWARD EMERGENCY POWER SUPPLY WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGE NCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL TESTS WERE PERFORMED AND THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002071900086 20020719 00086 NM 2002 7 19 VNAA0207014 1 20020711 A 2497 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 460PS 3061 DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND FOUND A TERMINAL WIRE CREATING A LOOSE CONNECTION. MAINTENANCE REPAIRED THE WIRE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002071900087 20020719 00087 NM 2002 7 19 VNAA0207019 1 20020713 A 2400 GENERATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 423JS 3032 DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND DC GENERATOR FAILURE CAS MESSAGE. AFTER CLEARING THE RUNWAY, THE CREW R ESET THE RIGHT HAND GENERATOR AND THE MESSAGE EXTINGUISHED. FLIGHT 4015 WAS THEN CLEARED FOR ANOTHER TAKE OFF ATTEMPT. FLIGHT 4015 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002071900091 20020719 00091 NM 2002 7 19 SWAA021499 1 20020706 A 2742 6355800103 MOTOR BOEING 737 7377H4 1384404 NM HORIZ STAB FAILED A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 29 744SW 29490 AIR TURNBACK, INFLIGHT FAILURE OF BOTH NORM AND AUTOPILOT ELECTRIC PITCH TRIM. REMOVED AND REPLACED STAB TRIM MOTOR PER MM. 2 L 7 2 4F RT A16WE 2002071900092 20020719 00092 NM 2002 7 19 SWAA021500 1 20020708 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 EEPLS LOOSE IN MID CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F A16WE 2002071900093 20020719 00093 NM 2002 7 19 SWAA021502 1 20020708 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 EEPLS LOOSE AT ROW NR 13. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002071900094 20020719 00094 NM 2002 7 19 SWAA021507 1 20020708 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002071900096 20020719 00096 NM 2002 7 19 SWAA021509 1 20020708 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICES CRACKED (2 EA) AT STR 4R, BS 360 AND 908. REMOVED AND REPLACED STR SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2002071900097 20020719 00097 NM 2002 7 19 SWAA021516 1 20020708 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 EEPLS WIRES LOOSE IN MID CABIN. REPAIRED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2002071900098 20020719 00098 NM 2002 7 19 SWAA021523 1 20020709 A 3350 604222 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATT ERY PER MM. 2 L 7 2 4F RT A16WE 2002071900099 20020719 00099 NE 2002 7 19 SWAA021526 2 20020707 A 7250 9995M14G GUIDE VANE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE ERODED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 368SW 26579 723136 AIR TURNBACK, DURING CLIMB F/A REPORTED FUMES IN CABIN. FOUND NR 2 ENGINE HPT NOZZLE GUIDE VANES ERODED. REMOVED AND R EPLACED NR 2 ENGINE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002071900100 20020719 00100 NM 2002 7 19 SWAA021527 1 20020710 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002071900101 20020719 00101 EA 2002 7 19 COMA0260431 1 20020718 A 5311 6003603024 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA F.S.718.0,R/H&L/ CRACKED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 959CA 15027 7116 R/H F.S. 718.0 FRAME AND DOUBLER, AND L/H SIDE 718.0 DOUBLER ARE CRACKED.REPALCED R/H SIDE F.S. 718.0 FRAME P/N 600-3603 0-24 AND DOUBLER P/N 600-36030-32, AND L/H F.S. 718.0 FRAME DOUBLER P/N 600-36030-31. ALL WORK PERFORMED I/A/W CANADAIR REO 601R-53-61-193 REV A, REF COMAIR W/O 29977 AND MX LOG PAGES 520526,520535 AND 520536 AND C/O 7116902. 2 L 7 2 4F RT A21EA 2002071900102 20020719 00102 2002 7 19 SWAA021528 4 20020710 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002071900103 20020719 00103 2002 7 19 SWAA021529 4 20020709 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002071900105 20020719 00105 NM 2002 7 19 SWAA021534 1 20020710 A 2530 41600019 COFFEEMAKER BOEING 737 7373H4 1384600 NM GALLEY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 334SW 23938 AFT GALLEY COFFEEMAKER ARCHING AND BURNING ELECTRICAL SMELL WAS NOTED. REMOVED AND REPLACED COFFEEMAKER PER MM. 2 L 7 2 4F RT A16WE 2002071900106 20020719 00106 EA 2002 7 19 COMA0260432 1 20020717 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 436CA 3374 7482 FLIGHT 5648 GEAR DISAGREE MESSAGE.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002071900108 20020719 00108 NM 2002 7 19 SWAA021537 1 20020711 A 5523 65C25798 HINGE BOEING 737 7377H4 1384404 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLA CED HARDWARE AT ALL HINGE ATTACH POINTS PER MM. 2 L 7 2 4F RT A16WE 2002071900109 20020719 00109 EA 2002 7 19 COMA0260433 1 20020717 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR DETERIORATED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 957CA 7109 FLIGHT 5975 EMERGENCY FLOOR PATH LIGHTING IS DIM FROM ROW 8 AFT.REPLACED FLOOR LIGHT STRIPS. 2 L 7 2 4F RT A21EA 2002071900110 20020719 00110 NM 2002 7 19 SWAA021539 1 20020711 A 2612 894093 FIRE LOOP BOEING 737 7372T4 1384492 NM PWA JT8 JT8D9 52048 NE NR 2 ENGINE FAULTY A SWAA E F B ENGINE SHUTDOWN ACTIVATE FIRE EXT. EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 29 722WN 22698 707416 DECLARED EMERGENCY, IN FLIGHT SHUT DOWN, NR 2 ENGINE FIRE BELL WARNING LIGHT ILLUMINATED. SHUT DOWN NR 2 ENGINE AND DIS CHARGED BOTH FIRE BOTTLES. REMOVED AND REPLACED NR 2 ENGINE LOWER FIRE DETECTOR LOOP AND ENGINE FIRE DETECTOR ACCY UNIT PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2002071900111 20020719 00111 NM 2002 7 19 SWAA021563 1 20020715 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED RON, FOUND EEPLS LOOSE AT ROW NR 1. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002071900112 20020719 00112 2002 7 19 2002FA0000813 4 20020627 A 2565 61620468 SLIDE BOEING 737 737400 138449A NM RIGHT TWISTED G M56B K NONE L NO TEST IN INSP/MAINT 1 EA 05 37NY 23976 DURING AN EMERGENCY EVACUATION DEMONSTRATION REQUIRED BY FAR PART-125, THE RT FORWARD EMERGENCY ESCAPE SLIDE INFLATED IN A TWISTED CONDITION WHICH POSITIONED THE SLIDE IN A VERTICAL POSITION RENDERING IT UNUSABLE. A PHONE CALL TO THE MANU FACTURER REVEALED THAT THIS SAME SITUATION HAD BEEN REPORTED TO THEM ON SEVERAL OCCASIONS. THE MANUFACTURER STATED THAT THE PACKING AND FOLDING PROCEDURE HAD BEEN RECENTLY REVISED (5/11/02) TO ELIMINATE THIS PROBLEM FROM RECURRING. 2 L 7 2 4F RT A16WE 2002071900113 20020719 00113 WP 2002 7 19 AALA20020503 1 20020417 A 2120 CLAMP DOUG DC9 DC982 3022082 WP A/C BAY LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 70524 49916 BOS-ORD - TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED APPROXIMATELY 1 MINUTE AFTER TAKEOFF. LIGHT EXTINGUISHED WITHIN 2 MINUTES OF MOVING SWITCHES TO HP BLEED OFF. AIR INTERRUPTED AND LANDED BOS WITHOUT INCIDENT. TIGHTENED LEFT A IR CONDITIONING PRESSURE 2EG VALUE V BAND CLAMP. PERFORMED LEAK CHECK AT HIGH ENGINE POWER SETTING, NO LEAKS NOTED HIGH TEMPERATURE LIGHT DID NOT ILLUMINATE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071900114 20020719 00114 2002 7 19 AALA20020515 4 20020422 A 3460 FMC BOEING 757 757223 1384957 NM COCKPIT MALFUNCTIONED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 191AN 32385 LAX - FLT 297 - EN ROUTE LAX-HNL - BOTH FMC'S FAILED TO PERFORM NAVIGATION CALCULATIONS FOLLOWING TAKEOFF. RESET PER OP ERATIONS MANUAL. RETURNED AND LANDED LAX WITHOUT INCIDENT. VERIFIED SOFTWARE FOR FMC: OPC, OPS, FDO, AMI ALL GOOD PER MAINTENANCE MANUAL. RELOADED FMC NAVIGATION DATA SOFTWARE PROGRAM AA8-0204-001. GROUND CHECKS NORMAL. (M) 2 L 7 2 4F RT A2NM 2002071900115 20020719 00115 WP 2002 7 19 AALA20020519 1 20020421 A 2150 20495061 ACM DOUG DC9 DC982 3022082 WP A/C BAY LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 552AA 53034 JFK - FLT 1567 - AFTER TAKEOFF, EN ROUTE LGA-MIA - AT 6000 FEET, FLIGHT ATTENDANT NOTIFIED COCKPIT OF SMOKE IN THE CABIN . SMELLED LIKE ELECTRICAL IN NATURE. AIR INTERRUPTED AND LANDED FJK WITHOUT INCIDENT. REPLACED AIR CONDITIONING DUCT AFT OF WATER SEPARATOR DUE TO RIGHT ACM INTERNAL OIL LEAK. REPLACED RIGHT ACM AND ASSOCIATED DUCTS AND LINES. PRECAUTI ONARY REPLACED COALESCER BAG AFTER RUN UP ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071900116 20020719 00116 WP 2002 7 19 AALA20020520 1 20020412 A 5320 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7530 49922 TUL - FOUND AFT CARGO DOOR BEAM HAS CORROSION ON HORIZONTAL AND VERTICAL LEGS. INSTALLED DOUBLER PER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2002071900117 20020719 00117 WP 2002 7 19 AALA20020548 1 20020425 A 2910 B-NUT DOUG DC9 DC982 3022082 WP HYD SYSTEM LOOSE A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 452AA 49553 BOS - FLT 2018 - EN ROUTE ORD-BOS - LOSS HYDRAULIC FLUID FROM LEFT HYDRAULIC SYSTEM. DECLARED EMERGENCY AND LANDED BOS WITHOUT INCIDENT. TIGHTENED LOWER B-NUT ON LEFT REVERSER CONTROL VALVE, REPLACED LEFT ENGINE DRIVEN PUMP, AND REPLACED PRESSURE CASE DRAIN AND RETURN FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071900120 20020719 00120 NM 2002 7 19 CALA0200404 1 20020716 A 5311 FRAME BOEING 737 7373T0 1384582 NM STA 616 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND A 3/4" CRACK ON BOTTOM END OF R/H MAIN FRAME AT STA 616 BELOW FLOOR. REPAIRED IAW ECRA 5311-01129. 2 L 7 2 4F RT A16WE 2002071900121 20020719 00121 WP 2002 7 19 CALA0200405 1 20020717 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 1136-1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND L/H CENTER SEAT TRACK CORRODED AROUND FLOOR PANEL MOUNT HOLES BETWEEN STA 1136 AND 1174. A NEW SEAT TRA CK SECTION WAS INSTALLED IAW SRM 53-05. 2 L 7 2 4F A6WE 2002071900122 20020719 00122 WP 2002 7 19 CALA0200407 1 20020718 A 5311 FRAME DOUG DC9 DC982 3022082 WP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND FRAME CORRODED AT FRAME TO LONGERON ATTACH POINTS, STA 1174, LONGERON 20L-25L. THE CORRODED SECTION OF FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-04. 2 L 7 2 4F A6WE 2002071900123 20020719 00123 WP 2002 7 19 CALA0200408 1 20020718 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 1220-1231 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND AFT CARGO COMPARTMENT SKIN CORRODED AROUND LONGERON 26R AT FS 1220-1231. THE CORRODED AREA WAS REMOVED AND A SPLICE, TIE ROD, FINGER DOUBLER, AND NEW LONGERON SECTION WERE INSTALLED IAW SRM 51-10-4, 51-30-2, 51-30-5, AND EC RA 5310-04263. 2 L 7 2 4F A6WE 2002071900124 20020719 00124 WP 2002 7 19 CALA0200409 1 20020718 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP FS 1291 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND SHEAR TIE CORRODED AT FS 1291 JUST ABOVE LONGERON 24L. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 5 1-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002071900125 20020719 00125 WP 2002 7 19 CALA0200410 1 20020718 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP L2 GIRT BAR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND FORWARD AND AFT GIRT BAR SUPPORT FITTINGS CORRODED AT L-2 DOOR JAMB. REMOVED AND REPLACED TWO EACH GIRT BAR SUPPORTS IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2002071900126 20020719 00126 WP 2002 7 19 CALA0200411 1 20020718 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FS 1100-1200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND AFT CARGO COMPARTMENT DOOR CUTOUT TORQUE BOX VERTICAL SUPPORTS FOR SKIN CORRODED AT LOWER ATTACH ANGLES , FS 1100-1200. REMOVED SCUFF PLATE FOR ACCESS IAW SRM 51-30-1. REPLACED TWO EACH INTERCOSTALS IAW SRM 51-30-2 AND 51-30 -5. 2 L 7 2 4F A6WE 2002071900127 20020719 00127 WP 2002 7 19 CALA0200412 1 20020718 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FS 1155-1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1155-1174, LONGERON 21L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51 -10-4. 2 L 7 2 4F A6WE 2002071900128 20020719 00128 WP 2002 7 19 CALA0200413 1 20020718 A 5330 DOUBLER DOUG DC9 DC982 3022082 WP FS 1128 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND L-2 DOOR FAIL SAFE DOUBLER CORRODED AT FS 1128, LONGERON 19L. THE FAIL SAFE DOUBLER WAS REMOVED AND REP LACED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002071900129 20020719 00129 WP 2002 7 19 CALA0200414 1 20020718 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FS 1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND LONGERON 19L CORRODED AT FS 1174. THE CORRODED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW EA 9-53 12-2-A0961. 2 L 7 2 4F A6WE 2002071900130 20020719 00130 WP 2002 7 19 CALA0200415 1 20020718 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1180 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND O/B SEAT TRACK CORRODED AT #4 GALLEY ATTACH POINT, FS 1180, LBL 54. THE SEAT TRACK WAS REMOVED AND REPL ACED IAW SRM 51-10-4. 2 L 7 2 4F A6WE 2002071900131 20020719 00131 WP 2002 7 19 CALA0200417 1 20020718 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP G-3 GALLEY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT G-3 GALLEY ATTACH POINT. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 2002071900132 20020719 00132 WP 2002 7 19 CALA0200418 1 20020718 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FS 1200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND LONGERON 26L CORRODED ON O/B SURFACE AT FS 1200. THE LONGERON WAS REMOVED AND REPLACED IAW ECRA 5310-04 268. 2 L 7 2 4F A6WE 2002071900133 20020719 00133 EU 2002 7 19 B3OR20020008 1 20020523 A 6310 350A35110205 COUPLER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ENG/XMSN MOUNT WORN B B3OR K NONE O OTHER IN INSP/MAINT 1 SW 03 5204Y 979 100 3101 9571 DURING 1000 HOUR INSPECTION, THE ENGINE TO TRANSMISSION MOUNT TUBE WAS FOUND TO HAVE EXCESSIVE PLAY. THE GIMBAL RING MOU NT BUSHINGS ON THE TUBE WERE MEASURED, AND FOUND TO BE OUT OF LIMITS. UPON FURTHER INVESTIGATION, AND A PHONE CALL TO AM ERICAN EUROCOPTER, WE FOUND THE FORWARD LATERAL LAMINATED ISOLATOR WAS DELAMINATING. ALSO, THE AFT LATERAL LAMINATED ISO LATOR WAS FOUND TO HAVE BROKEN TORQUE, AND CAUSED FURTHER DAMAGE TO THE CROSSBEAM UNDER THE TRANSMISSION. THE ENGINE TO TRANSMISSION MOUNT TUBE HAD TO BE SCRAPPED, THE BUSHINGS ARE NOT REPLACEABLE. 1 G 7 1 3U 3 U H9EU E19EU 2002071900134 20020719 00134 EU 2002 7 19 B3OR20020009 1 20020523 A 6330 579065H ISOLATOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE XMSN MOUNT DELAMINATED B B3OR K NONE O OTHER IN INSP/MAINT 1 SW 03 5204Y 979 100 3101 9571 DURING A 1000 HOUR INSPECTION, THE FORWARD LATTERAL LAMINATED ISOLATOR MEMBER WAS FOUND TO BE DELAMINATED. THERE WAS NO OIL OR HYDRAULIC FLUID PRESENT IN THE AREA OR ON THE LAMINATED ISOLATOR MEMBER ITSELF. WE SUSPECT THAT THE AFT ISOLATO R MEMBER LOSS OF TORQUE HAD CAUSED THE FORWARD MEMBER TO BECOME STRESSED AND CAUSED IT TO START TO DELAMINATE. 1 G 7 1 3U 3 U H9EU E19EU 2002071900135 20020719 00135 WP 2002 7 19 AALA20020579 1 20020415 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 TUL - FOUND NR 3 SEAT TRACK CORRODED FROM STATION 1174-1287. SPLICE INSTALLED FROM STATION 1174-1287 PER SRM 53-05. (M ) 2 L 7 2 4F A6WE 2002071900136 20020719 00136 WP 2002 7 19 AALA20020580 1 20020411 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 TUL - FOUND NR 2 SEAT TRACK CORRODED BEYOND LIMITS ON SEAT AT STATIONS 1287-1288. MECHANIC INSTALLED SEAT TRACK REPAIR PLUG PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002071900137 20020719 00137 WP 2002 7 19 AALA20020581 1 20020416 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 TUL - FOUND CORRODED STATION 1155-1212. DOUBLER INSTALLED PER AARD 53-10-00. (M) 2 L 7 2 4F A6WE 2002071900138 20020719 00138 WP 2002 7 19 AALA20020587 1 20020423 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AA 49459 TUL - FOUND DOOR PAN CORRODED. REPAIRED DOOR PAN BY CUTTING OUT LOWER DOOR PAN AND INSTALLED A NEW LOWER DOOR PAN PER S RM 53-05 PART 2 FIG 44. (M) 2 L 7 2 4F A6WE 2002071900139 20020719 00139 NE 2002 7 19 AALA20020589 2 20020506 A 7260 O-RING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE ENGINE LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 448AA 49474 JFK - FLT 705 - EN ROUTE LGA-DFW - ON LIFTOFF SMOKE OBSERVED, SMELL IN CABIN AND STRONG SMELL IN COCKPIT. DISSIPATED AT 9,000-10,000 FEET (2-3 MINUTES). LANDED JFK WITHOUT INCIDENT. REPLACED O-RING ON MAGNETIC CHIP DETECTOR AND CHECK VAL VE. ACCOMPLISHED ENGINE RUN. NO LEAKS FOUND. CLEANED OIL FROM INLET DOOR ACTUATOR AREA AND INLET AREA BEFORE PACK BUR N. REPLACED BOTH COALESCER BAGS PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 2002071900140 20020719 00140 WP 2002 7 19 AALA20020596 1 20020501 A 2120 CDK29491 BOOT DOUG DC9 DC982 3022082 WP A/C BAY BLOWN A AALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 228AA 49178 DFW - FLT 1191 - EN ROUTE DFW-SMF - APPROXIMATELY 10 MINUTES AFTER TAKEOFF, CLIMBING THROUGH 17,000 FEET TAIL COMPARTMEN T TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED CHECKLIST AND AFTER ABOUT 3.5 MINUTES WITH PACKS IN HP BLEED OFF AND POWER REDUCED FOR LEVEL OFF AT 20,000 FEET THE LIGHT FLICKERED AND WENT OUT. RETURNED TO DFW AND LANDED WITHOUT INCIDE NT. REPLACED DUCT BOOT ON RIGHT TEMPERATURE CONTROL VALVE IN AFT ACCESSORY COMPARTMENT. POWER ENGINE RUN WITH PACKS ON , NO LEAKS NOTED NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002071900141 20020719 00141 WP 2002 7 19 AALA20020599 1 20020424 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND FUSELAGE SKIN CRACKED FROM FASTENER HOLE AT STATION 1380 ABOVE L14L. REMOVED DAMAGE AND INSTALLED DOUBLER P ER SRM 53-04. (M) 2 L 7 2 4F A6WE 2002082600114 20020826 00114 NM 2002 8 26 DHL2002705007 1 20020711 A 2611 SMOKE DETECTOR BOEING 727 72722C 138400F NM CARGO BAY FAULTY A DHLA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 705DH 19191 LWR CARGO SMOKE DETECTOR TEST ALARM FAULT ILLUMINATED WITH CODE F6929. REMOVED AND REPLACED FWD LWR CARGO SMOKE DET TES TED CHECK OK AS PER DHL B727-200 ADV MM SUPPLEMENT 26-16-01. 2 L 7 3 4F A3WE 2002071900143 20020719 00143 CE 2002 7 19 CNQ2002F00000 1 20020613 A 2910 651711073 LINE CESSNA 500 550 2076604 CE PWA 530 PW530A NE SPEED BRAKE CHAFED B CNQ6 K NONE K FLUID LOSS IN INSP/MAINT 1 EA 25 308CS 830 5500976 THE ORANGE FRESH AIR DUCT IN THE TAILCONE IS CHAFING AGAINST THE SPEED BRAKE LINES. THIS RESULTED IN A FAILURE IN THE S PEED BRAKE LINE. THE CREW AND PASSENGERS OF THE AIRCRAFT REPORTED A HYD FLUID MIST COMING OUT OF THE WEMACS IN THE CABI N. REPLACED DUCT AND SPEED BRAKE LINE WITH NEW. FOLLOWED BY THE APPLICATION OF ANTI-CHAFE MATERIAL TO THE SPEED BRAKE LINES. ALSO REPLACED VENTILATION JUNCTION BOX, REPLACED CABIN FRESH AIR DUCTS AND REMOVED ATOMIZED HYD FLUID IN THE AF FECTED AREAS. 1 L 7 2 4F 4 F A22CE E00053EN 2002071900144 20020719 00144 CE 2002 7 19 D4O2002F00000 1 20020614 A 2450 CIRCUIT BREAKER BEECH 100 B100 1152919 CE GARRTT TPE331 TFE33112UHR WP MAIN BUS TRIPPED E D4OA K NONE O OTHER IN INSP/MAINT 1 EA 21 19DA 7568 BE87 WHILE IN FLIGHT, POWER WAS LOST TO RT SIDE OF INSTUMENT PANEL. PILOT TRIED TO EXTEND LANDING GEAR. GEAR DID NOT EXTEND . EMERGENCY WAS DECLARED AND PILOT RETURNED TO ALTITUDE AND MANUALLY EXTENDED LANDING GEAR. PILOT COMUNICATED WITH ANO THER PILOT WHO TOLD HIM TO CHECK HIS MAIN BUS CIRCUIT BREAKERS. PILOT FOUND C/B POPPED AND RESENT THEM. POWER RETURNED TO INSTRUMENT PANEL. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS JACKED. OP CHECK OF GEAR AND ELECTRICALY SYSTEM WAS SATISFACTORY. 1 L 7 2 4T 4 T A14CE E4WE 2002071900145 20020719 00145 SO 2002 7 19 EWO2002F00001 2 20020617 A 8530 646277 LIFTER BEECH 36 A36 1151604 CE CONT O550 IO550B SO NR 3 CYLINDER SPALLED B EW0R K NONE O OTHER IN INSP/MAINT 1 GL 25 8085N 886 E2740 675762 UPON REMOVAL OF NR 3 CYLINDER DUE TO LOW COMPRESSION. THE EXHAUST LIFTER AND CAMSHAFT WERE FOUND SEVERELY SPALLED. THE INTAKE LIFTER HAD MINOR SPALLING. THE LUBRICATION SYSTEM WAS FOUND TO BE CONTAMINATED WITH METAL. BOTH LIFTER HAD COR ROSION ON THE SIDEWALKS, CAUSING THE UNITS TO STICK IN THE CRANKCASE. 1 L 7 1 3O 3 O 3A15 E3SO 2002071900146 20020719 00146 CE 2002 7 19 HYI2002F00013 1 20020624 A 2435 99103971 RELAY CESSNA 402 402C 207590R CE STARTER FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NM 01 88833 402C0265 BATTERY SHOWED HIGH RATE OF CHARGE. BOTH ALTERNATORS, AMPERE OUTPUT, TOTAL AVIONICS FAILURE, UTILIZED AVIONICS BYPASS, REGAINED PARTIAL AVIONICS. AIRCRAFT LANDED WITHOUT INCIDENT. MECHANIC REMOVED AND REPLACED RIGHT STARTER RELAY (UNIT H AD FAILED) AND RIGHT STARTER MOTOR AS A PRECAUTIONARY MEASURE. AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 3O A7CE 2002071900147 20020719 00147 NM 2002 7 19 DHL2002705010 1 20020719 A 3510 3581529V OXYGEN MASK BOEING 727 72722C 138400F NM A DHLA K O NONE OTHER O OTHER NR NOT REPORTED 1 SO 01 705DH 19191 1) F/O'S O2 MASK BREATHER VALVE STUCK OPEN, MASK WILL NOT PULL TO FACE UPON INHALE.2) R + R F/O'S O2 MASK IAW B727 M/M 35-11-00, OP AND LEAK CHECK GOOD. 2 L 7 3 4F A3WE 2002071900149 20020719 00149 NM 2002 7 19 MHJ2002F00003 1 20020701 A 5310 250002505 DOOR PIPER PA60 PA60601 7106010 NM PAX DOOR DEPARTED E MHJA A UNSCHED LANDING D INFLIGHT SEPARATION NR NOT REPORTED 1 SW 05 942TJ 4590 610583796213 UPPER CABIN DOOR DEPARTED IN FLIGHT. ABOUT 1 HOUR INTO FLIGHT PILOT REPORTED CREAKING SOUND. SHORTLY AFTERWARD, DOOR D EPARTED. PILOT LANDED WITHOUT INCIDENT. 1 M 7 2 3O RT A17WE 2002071900150 20020719 00150 WP 2002 7 19 AALA20020601 1 20020429 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND SKIN GOUGED AT STATION 863 L9R. BLENDED DAMAGE PER SRM 53-04, ALODINED PER SRM 51-10-3, INSTALLED REPAIR DO UBLER PER SRM 53-04-00. (M) 2 L 7 2 4F A6WE 2002071900152 20020719 00152 WP 2002 7 19 AALA20020602 1 20020423 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND FUSELAGE SKIN CRACKED AT FASTENER HOLE STATION 1380 ABOVE LONGERON 14R. INSTALLED DOUBLER PER SRM 53-04. ( M) 2 L 7 2 4F A6WE 2002071900153 20020719 00153 WP 2002 7 19 AALA20020603 1 20020421 A 5313 STRINGER DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND STRINGER 4 LEFT CRACKED LOWER FLANGE AT STATION 160. INSTALLED REPAIR SPLICE PER SRM 53-00. (M) 2 L 7 2 4F A6WE 2002071900155 20020719 00155 WP 2002 7 19 AALA20020604 1 20020422 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE TORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND STRUCTURE UNDER FLOORING AT STATION 218, RIGHT INBOARD TORN. REPLACED STRUCTURE CUSP AT STATION 218-237 PER SRM 51-01 PAGE 1. (M) 2 L 7 2 4F A6WE 2002071900156 20020719 00156 WP 2002 7 19 AALA20020605 1 20020430 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND CORROSION AROUND MOUNT HOLE FOR G-4 GALLEY IN NR 1 SEAT TRACK, STATION 1174. REMOVED CORRODED TRACK. INSTA LLED NEW TRACK, STATION 1174 TO 1309 PER SRM 51-00. (M) 2 L 7 2 4F A6WE 2002071900157 20020719 00157 CE 2002 7 19 T4O2002F00003 1 20020529 A 5521 50610000487 RIB BEECH 90 C90 1152913 CE ELEVATOR CRACKED A T4OR K NONE O OTHER IN INSP/MAINT 1 NE 03 91TJ 7863 LJ744 FOUND DURING PHASE INSPECTION: LT ELEVATOR HAD A CRACKED INBOARD RIB, RIB DOUBLER BRACKET, AND INBOARD MAIN SPAR FLA NGE AT INBOARD 90 DEGREE BEND, ALL WHERE THE ELEVATOR TORQUE TUBE ATTACHES. CRACKS VARY IN LENGTH FROM 1.3 INCHES ON SP AR FLANGE TO 3.5 INCHES AROUND RIB CIRCUMFRENTIALLY FOLLOWING THE SHAPE OF THE TORQUE TUBE ATTACH CASTING. 1 L 7 2 3T 3A20 2002071900158 20020719 00158 WP 2002 7 19 AALA20020606 1 20020430 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND INDICATION OF CRACK IN LONGERON 16L STATION 1437. INSTALLED LONGERON REPAIR PER SRM 53-02-00. REINSTALLED SERVICEABLE SHELF INTERCOSTAL PER ESO 80559. (M) 2 L 7 2 4F A6WE 2002071900159 20020719 00159 WP 2002 7 19 AALA20020607 1 20020425 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND CORROSION LOWER SIDE OF RIGHT CUSP STATION 1160. REMOVED CORROSION AND INSTALLED DOUBLER AS PER AARD 53-00- 00-02. (M) 2 L 7 2 4F A6WE 2002071900160 20020719 00160 CE 2002 7 19 T4O2002F00004 1 20020613 A 5521 RIB BEECH 90 E90 1152914 CE PWA PT6 PT6A60A 52043 NE ELEVATOR CRACKED B T4OR K NONE O OTHER IN INSP/MAINT 1 NE 03 965LG 11640 LW204 FOUND DURING PHASE INSPECTION: LEFT ELEVATOR HAD A CRACKED INBOARD RIB (PN 50-610000-355), RIB DOUBLER BRACKET, AND INB OARD MAIN SPAR FLANGE AT INBOARD 90 DEGREES BEND, ALL WHERE THE ELEVATOR TORQUE TUBE ATTACHES. CRACKS VARY IN LENGTH FR OM 1.3 INCHES ON SPAR FLANGE TO 3.4 INCHES AROUND RIB CIRCUMFRENTIALLY FOLLOWING THE SHAPE OF THE TORQUE TUBE ATTACH CAS TING. 1 L 7 2 3T 4 T 3A20 E4EA 2002071900161 20020719 00161 WP 2002 7 19 AALA20020608 1 20020425 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND CORROSION ON FLOOR PAN CUSP, BETWEEN SEAT TRACK 1 AND 2. REMOVED CORROSION AND INSTALLED NEW SECTION OF CUS P STATION 1250-1309 AS PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002071900162 20020719 00162 WP 2002 7 19 AALA20020609 1 20020425 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND DAMAGED FASTENER HOLE ON LEFT CUSP AT STATION 1250. DOUBLER INSTALLED AT LEFT CUSP STATION 1240-1250, AND S EALED PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002071900163 20020719 00163 WP 2002 7 19 AALA20020610 1 20020422 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND NR 5 SEAT TRACK HAS EXFOLIATED CORROSION BETWEEN STATION 200-207. REPLACED SEAT TRACK NR 5 FROM STATION 200 -245 AS PER SRM 53-05 SHEET 1. (M) 2 L 7 2 4F A6WE 2002071900164 20020719 00164 WP 2002 7 19 AALA20020611 1 20020418 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND HORIZONTAL ANGLE CRACKED IN RADIUS LOCATED BELOW F/O BRIEFCASE SHELF FORWARD SIDE OF FRAME STATION 120 RBL 4 9. REMOVED ANGLE AND REPLACED WITH NEW SRM 51-01. (M) 2 L 7 2 4F A6WE 2002071900165 20020719 00165 WP 2002 7 19 AALA20020612 1 20020416 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND WINDOW FRAME CRACKED LOWER FORWARD LEG STATION 984 AT LONGERON 15R. CUT OUT DAMAGE AND INSTALLED DOUBLER PE R SRM 53-10-00-25. (M) 2 L 7 2 4F A6WE 2002071900166 20020719 00166 WP 2002 7 19 AALA20020613 1 20020415 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND CRACK IN LOWER FORWARD WINDOW FRAME STATION 807R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-29 . (M) 2 L 7 2 4F A6WE 2002071900168 20020719 00168 WP 2002 7 19 AALA20020614 1 20020426 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 TUL - FOUND CORROSION ON NR 2 SEAT TRACK INBOARD FLANGE AT CLIP NUTS STATION 1190-1205. BLENDED CORROSION PER SRM 53-01 . INSTALLED DOUBLER STRAP PER AARD 53-22-00-13. (M) 2 L 7 2 4F A6WE 2002071900173 20020719 00173 SO 2002 7 19 N6P2002F00000 1 20020709 A 1430 40646000 RIVET PIPER PA31 PA31350 7103110 SO BRACKET FAILED E N6PA K NONE O OTHER IN INSP/MAINT 1 EA 13 27682 7956 317852105 DURING A ROUTINE 100 HOUR INSPECTION IT WAS DISCOVERED UPON OPENING THE TAIL CONE, THAT TWO RIVETS WERE MISSING IN THE L EFT AND RIGHT BRACKET. THIS BRACKET SUPPORTS THE AFT FUSELAGE, FORWARD OF THE ELEVATOR CONTROL ARM HINGE POINT. EVIDENC E SHOWS THAT THESE RIVETS WERE PREVIOUSLY INSTALLED AND PART OF A RIVET WAS FOUND INSIDE THE LOWER FUSELAGE NEAR THIS PO INT. AN INSPECTION FOR HIDDEN DAMAGE REVEALED NOTHING ELSE RELATED TO THIS PROBLEM. 1 L 7 2 3O A20SO 2002071900174 20020719 00174 EA 2002 7 19 VNW2002F00001 2 20020528 A 7321 25244405 FCU BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA RT ENGINE FAILED E VNWA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 15 431R B71 RIGHT ENGINE WAS SHUTDOWN IN FLIGHT. DUE TO INTERNAL FAILURE IN THE FUEL CONTROL UNIT (FCU). FAILURE RESULTING IN A PO SSIBLE ENGINE RUN AWAY CONDITION. FLIGHT WAS DEVERTED TO AN ALTERNATE AIRPORT AND AN UNEVENTFUL LANDING WAS MADE. 1 L 7 2 3T 4 T A14CE E4EA 2002071900175 20020719 00175 CE 2002 7 19 I5W2002F00000 1 20020620 A 3210 28233330511 FITTING RKWELL NA265 NA26565 7630107 CE ACT DOOR FITTING BROKEN A I5WA K NONE O OTHER TO TAKEOFF 1 SO 05 88BF 4257 722962 46560 LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. THE MAIN GEAR INNER DOOR ACTUATOR SUPPORT FITTING PN 2823330511 BROKE AT THE ACTUATOR ATTACH POINT. MANUALLY RETRACTED THE RIGHT GEAR DOOR AND INSPECTED THE AIRCRAFT AND DEEMED THE AIRCRAFT S AFE FOR THE FERRY FLIGHT. A SPECIAL FLIGHT PERMIT WAS ISSUED AND THE AIRCRAFT RETURNED TO AIRPORT. REPLACED THE RIGHT MAIN GEAR INNER DOOR WITH A SERVICEABLE DOOR, RIGGED IAW MM AND OPERATIONAL AND WARNING TESTED LANDING GEAR. 2 L 7 2 4J A2WE 2002071900176 20020719 00176 NM 2002 7 19 UPS02238827 1 20020620 A 5310 SEAT TRACK BOEING 727 72722C 138400F NM BS 360 BLO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CORROSION ON SEAT TRACK FLANGE AT BS 360 BLO. CORROSION BLENDED AND FOUND TO BE OUTSIDE LIMITS, TRACK CUT AT BS 41 0 AND NEW SECTION SPLICED IN IAW SRV-SNN-02-00124H AND 00134H UPS AU THORISATION 727-53-20064 2 L 7 3 4F A3WE 2002071900177 20020719 00177 NM 2002 7 19 UPS02238830 1 20020620 A 5310 NPN DOUBLER BOEING 727 72722C 138400F NM DELTA BEAM BS747 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI BULGING ON EXTERNAL DOUBLER ATTACHED TO DELTA BEAM BS 747 Y/H DOUBLER REMOVED IAW SRM 51-30-2, CORROSION FOUND ON UDERSIDE OF DOUB LER, DELTA BEAM FAYING SURFACE INSPECTED AND LIGHT SURFACE CORROSION FOUND, REMOVED AND FOUND WITHIN LIMITS, REPROTECTED IAW SRM 51-10-2 . CORROSION ON DOUBLER OUTSIDE OF LIMITS, NEW DOUBLER FABRICATED I AW SRM 51-20-01 AND INSTALLED IAW SRM 51-30-2 2 L 7 3 4F A3WE 2002071900178 20020719 00178 NM 2002 7 19 UPS02238839 1 20020615 A 5330 FLOOR SUPPORT BOEING 727 72722C 138400F NM BS343 RBL 15 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CORROSION FOUND ON FLOOR SUPPORT STRUCTURE AT BS 343 RBL 15. TOILET PARTITION REMOVED FOR ACCES S IAW MM25-40-00, CORROSION REMOVE D IAW SRM 51-10-6 , FOUND OUTSIDE LIMITS IAW SRM 53-10-1, PARTS FABV RICATED IAW DWG 65-26173. INSTALLED PARTS IAW DWG 65-26173 AND SRM 5 1-30-2. PARTITION REINSTALLED IAW MM25-40-00 AND OHM 20-50-01. 2 L 7 3 4F A3WE 2002071900179 20020719 00179 NM 2002 7 19 UPS02238851 1 20020620 A 5310 INTERCOSTAL BOEING 727 72722C 138400F NM BS950 LBL 6. CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI BS 950 LBL 6 ANGLE CRACKED AT FLOOR BEAM INTERCOSTEL. NEW ANGLE FABRICATED IAW SRM 51-20-1 FIG. 7 ANGLE INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2002071900180 20020719 00180 NM 2002 7 19 ABXA020047 1 20020617 A 5700 114T412251 SLAT BOEING 767 767200 1385120 NM RIGHT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 RIGHT WING #11 SLAT INBOARD LEADING EDGE ANGLE WAS CORRODED. REMOVED CORROSION OUT OF LIMITS IAW B767 SRM 57-43-02. REPA IRED AREA IAW B657-43913MR. 2 L 7 2 4F RT A1NM 2002071900181 20020719 00181 NM 2002 7 19 ABXA020049 1 20020523 A 5700 112T7006U13 FITTING BOEING 767 767200 1385120 NM LEFT WING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783AX 23016 LEFT WING OUTBOARD PITCH LOAD FITTING HAD EXISTING SHORT E.D. REPAIRED AREA IAW REA B657-43882MR. 2 L 7 2 4F RT A1NM 2002071900182 20020719 00182 NM 2002 7 19 ABXA020051 1 20020512 A 5300 146T32212 SKIN BOEING 767 767200 1385120 NM AFT FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783AX 23016 AFT CARGO, FORWARD BULKHEAD, F.S. 1065, LONGERON 37 LEFT, AT DRAIN VALVE WAS CORRODED. REPAIRED AREA IAW REA B653-43879. 2 L 7 2 4F RT A1NM 2002071900183 20020719 00183 NM 2002 7 19 FX72002F00000 1 20020607 A 2700 651948218 JACKSCREW BOEING 727 727224 1384076 NM STABILIZER INOPERATIVE A FX7A O OTHER O OTHER IN INSP/MAINT 1 SO 19 296SC 22449 WHILE DOING (C) CHECK, ROUTINE CARD 65-C-1 FOUND METAL SHAVINGS IN AUX BRAKE CAVITY. REMOVED AND REPLACED STABILIZER J ACKSCREW PER MM. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2002071900184 20020719 00184 EA 2002 7 19 COMA0260434 1 20020718 A 2750 853D10018 ACTUATOR EATON CNDAIR CL600 CL6002B19 1900309 EA R/H OUTBD FLAP BINDING A COMA K NONE S AFFECT SYSTEMS UK UNKNOWN 1 SO 01 868CA 4132 1200AB 7427 FLIGHT 5306 FLAPS FAIL MESSAGE AT 30 DEGREES.REPLACED R/H #3 AND #4 FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 2002071900185 20020719 00185 EA 2002 7 19 COMA0260435 1 20020718 A 2750 853D10012 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RIGHT WING BINDING A COMA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 868CA 4132 7427 FLIGHT 5306 RECEIVED A FLAP FAIL CAUTION MESSAGE AT 30 DEGREES. REPLACED THE RIGHT WING #4 FLAP ACTUATOR 2 L 7 2 4F RT A21EA 2002071900186 20020719 00186 EA 2002 7 19 COMA0260436 1 20020717 A 2910 AE2460010H0264 HOSE CNDAIR CL600 CL6002B19 1900309 EA L/H PYLON LEAKING A COMA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 806CA 7359 FLIGHT 5966 HYDRAULIC SYSTEM #1 LOW PRESSURE WARNING.REPLACED LEAKING HOSE ASSY IN L/H ENGINE PYLON. 2 L 7 2 4F RT A21EA 2002071900187 20020719 00187 EA 2002 7 19 COMA0260437 1 20020718 A 2750 853D10018 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RIGHT WING BINDING A COMA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 868CA 4132 7427 FLIGHT 5306 RECEIVED A FLAP FAIL CAUTION MESSAGE AT 30 DEGREES.REPLACED THE RIGHT WING #3 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2002071900188 20020719 00188 NM 2002 7 19 UIE2002F00006 1 20020504 A 7920 9175M72P03 GASKET BOEING 747 747230B 1384889 NM FUEL OIL HEAT EX UNSECURE A UIEA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL J K WARNING INDICATION FLUID LOSS CL CLIMB 1 EA 15 509MC 21221 NR 2 ENGINE SHUTDOWN DURING CLIMB OUT, DUE TO OIL CONTENT LOSS AND LOW OIL PRESSURE. DUMPED 28,000 KGS OF FUEL TO MAX L ANDING WEIGHT. ENGINE WINDMILLED AT 24 PERCENT N1 UNITIL LANDING. C/A: SERVICED ENGINE OIL SYSTEM. FOUND GASKET AT F UEL OIL HEAT EXCHANGER NOT SECURED. LOWER TWO BOLTS NOT TIGHT. REMOVED GASKET AND FOUND UNSERVICEABLE DUE SEAL DAMAGED . INSTALLED NEW GASKET IAW MM. REMOVED AND REPLACED ENGINE OIL FILTER IAW MM. FILTER INSPECTION FOUND OK. REMOVED AN D INSPECTED CHIP DETECTORS IAW MM. NO DEFECTS NOTED. ENGINE RUN SATISFACTORY. OIL TANK SERVICED. LEAK CHECK GOOD. 2 L 7 4 4F A20WE 2002071900189 20020719 00189 NM 2002 7 19 AWXA200200634 1 20020622 A 5313 6546877168 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 1/2" CRACK WAS FOUND IN STRINGER WEB 18A R/H, BS 725. MAINTENANCE REMOVED ANG LE, AND SLOTTED STRINGER WEB EXTENDING THE CRACK TO SECOND FASTENER HOLE. FABRICATED GUSSET AND RADIUS FILLER, AND INSTA LLED REPAIR PARTS & ANGLE IAW AWA ER 03-5300-02192-ES1. 2 L 7 2 4F RT A16WE 2002071900190 20020719 00190 NM 2002 7 19 AWXA200200635 1 20020621 A 5313 6546877167 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 1/4" CRACK WAS FOUND ON THE AFT END OF STRINGER WEB 18 L/H AT INBOARD FASTENE R HOLE BS 725. MAINTENANCE REMOVED ANGLE, AND SLOTTED STRINGER WEB EXTENDING THE CRACK TO SECOND FASTENER HOLE. FABRICAT ED GUSSET AND RADIUS FILLER, AND INSTALLED REPAIR PARTS & ANGLE IAW AWA ER 03-5300-02193-ES2. 2 L 7 2 4F RT A16WE 2002071900191 20020719 00191 NM 2002 7 19 AWXA200200638 1 20020718 A 3350 BMS13311122 WIRE BOEING 737 737375 13844BN NM SEAT ROW 15 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 0 0 23707 PHX - EEL - DURING INSPECTION WIRES WERE FOUND BROKEN ON THE EMERGENCY ESCAPE PATH LIGHT SEAT ROW 15 L/H. MAINTENANCE RE PAIRED BROKEN WIRES ON THE EMERGENCY ESCAPE PATH LIGHT SEAT ROW 15 L/H PER CHAP 20 SWPM, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002072200002 20020722 00002 WP 2002 7 22 211004001 1 20020616 A 5230 SKIN DOUG DC9 DC983 3022083 WP FWD CARGO DOOR CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 192AJ 53192 FORWARD CARGO DOOR HANDLE CUTOUT CRACKED AND DEFORMED. C/A: INSTALLED REPAIR SCUFF PLATE FOR FORWARD CARGO DOOR HANDLE CUTOUT IAW SRM. (NR 27205) 2 L 7 2 4F RT A6WE 2002072200003 20020722 00003 CE 2002 7 22 CJP2002F00000 1 20020701 A 3230 48C48641 SELECTOR VALVE LEAR 35 35A 5170602 CE MLG FAILED E CJPA K NONE O OTHER IN INSP/MAINT 1 NM 03 261PG 329 LANDING GEAR WOULD NOT EXTEND WHEN GEAR HANDLE WAS SELECTED TO DOWN POSITION. FLIGHT CREW COMPLETED AN EMERGENCY LANDIN G GEAR EXENSION AND LANDED WITHOUT INCIDENT. MAINTENANCE JACKED AIRCRAFT AND DUPLICATED PROBLEM. LANDING GEAR TROUBLES HOOTING DETERMINED LANDING GEAR SELECTOR VALVE FAILED. PART WAS REPLACED AND A FUNCTIONAL CHECK OF THE GEAR SYSTEM WAS NORMAL. 2 L 7 2 4F A10CE 2002072200004 20020722 00004 CE 2002 7 22 CJP2002F00001 1 20020701 A 2612 4299100 CONNECTOR LEAR 25 25D 5170514 CE NR 2 FIRELOOP CONTAMINATED E CJPA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 NM 03 600GM 290 NR 2 ENGINE FIRE WARNING LIGHT CAME N IN FLIGHT. AIRCRAFT LANDED AFTER NR 2 ENGINE WAS SHUTDOWN IN FLIGHT AS A PRECAUTI ON. MAINTENANCE PERSONNEL DISCONNECTED, CLEANED AND RECONNECTED, CLEANED AND RECONNECTED FIRE LOOP CONNECTOR ASSY AND FIRE DETECT TEST WAS NORMAL, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4J A10CE 2002072200005 20020722 00005 CE 2002 7 22 CJP2002F00002 1 20020701 A 2612 4299100 CONNECTOR LEAR 25 25D 5170514 CE NR 2 FIRELOOP CONTAMINATED E CJPA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 NM 03 600GM 290 NR 2 ENGINE FIRE WARNING LIGHT CAME ON IN FLIGHT. AIRCRAFT LANDED AFTER NR 2 ENGINE WAS SHUTDOWN IN FLIGHT AS A PRECAUT ION. MAINTENANCE PERSONNEL DISCONNECTED, CLEANED AND RECONNECTED FIRE LOOP PLUG ASSEMBLY AND FIRE DETECT TEST WAS NORMA L, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4J A10CE 2002072200006 20020722 00006 CE 2002 7 22 CWQ2002F00002 1 20020517 A 7170 MS29513010 O-RING CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP FUEL SUMP DRAIN DETERIORATED B CWQR K NONE O OTHER IN INSP/MAINT 1 GL 05 797QS 6507097 AFTER DRAINING FUEL SUMP DURING PRE-FLIGHT INSPECTION, FOUND FUEL SUMP DRAIN LEAKING FUEL. FOUND FUEL SUMP DRAIN ORING DRY ROTTED. REMOVED AND REPLACED O-RING. THIS IS A COMMON PROBLEM, NEW O-RING MATERIAL NEEDED. 2 L 7 2 4F 4 F A9NM E6WE 2002072200007 20020722 00007 NE 2002 7 22 EVAB2002001 2 20020710 A 7310 247779 INTAKE PIPE CURTIS C46 C46FFLYTIGER SO PWA R2800 R280075 52026 NE NR 10 CYLINDER CRACKED I EVAB E A ENGINE SHUTDOWN UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION NR NOT REPORTED 1 AL 01 1837M 22388 EXPERIENCED AN ENGINE FIRE ACCOMPANIED BY BOTH AUDIO AND VISUAL WARNING. FIRE WAS OBSERVED FROM THE COWLING. WHEN THE THROTTLE WAS PULLED BACK THE FIRE WENT OUT AND ALL WARNINGS STOPPED. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED . SUBSEQUENT INVESTIGATION FOUND THAT THE INTAKE WYE PIPE TO NR 10 CYLINDER HAD SPLIT ALLOWING RAW FUEL/ AIR MIXTURE TO BE BLOWN DIRECTLY ON TO A HOT EXHAUST PIPE. REPLACEMENT OF THE PIPE AND SEALS FIXED THE PROBLEM. 2 L 7 2 4R 4 R A772 5E8 2002072200009 20020722 00009 NE 2002 7 22 GAI2002F00003 2 20020703 A 7311 548003 OIL COOLER BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE LEAKING A GAIA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 07 180AX 20041 IN CRUISE, THE CREW NOTICE A SUDDEN PARTIAL LOSS OF POWER ON THE NR 2 ENGINE FOLLOWED BY A CONTINUED DECREASE IN PERFORM ANCE WITH A CONSTANT FUEL FLOW. THE CREW MADE A PRECAUTIONARY ENGINE SHUTDOWN AND DECLARED AND EMERGENCY THE AIRCRAFT D IVERTED. AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND A FUEL LEAK ON THE FUEL OIL COOLER. REMOVED AND REPLACED T HE FUEL OIL COOLER. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002072200010 20020722 00010 NE 2002 7 22 GUU2002F00024 2 20020708 A 7200 3044700 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT DAMAGED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87557 11124 899 UE246 114440 DURING OIL FILTER INSPECTION METAL FLAKES DISCOVERED. FURTHER INSPECTION OF THE RT ENGINE DETERMINED EXCESSIVE DISCOLOR ED (BLACK OIL). REPLACED THE RIGHT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. 2 L 7 2 4T 4 T RT A24CE E26NE 2002072200011 20020722 00011 SW 2002 7 22 HKG2002F00000 1 20020610 A 2742 DL5040M6 ACTUATOR FRCHLD SA227 SA227CC 3377522 SW PITCH TRIM FAILED E HKGA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 SW 17 718C 28427 AC572 SECOND IN COMMAND IN RT SCAT REPORTED TO CAPTAIN THAT THE PITCH TRIM WOULD NOT TRIM NOSE DOWN. PILOT IN CHARGE ATTEMPTE D TRYING AUX TRIM SWITCH WITH SAME RESULTS. PITCH TRIM WAS TRANSFERRED TO THE NR 1 POSITION, PILOT IN CHARGE REPORTED T HAT THERE WAS STILL NO NOSE DOWN TRIM. PILOT IN CHARGE REPORTED THAT HE TRANSFERRED TRIM FROM NR 1 TO NR 2 AND BACK TO NR 1 POSITIONS, SEVERAL TIMES. TRIM ACTION RETURNED TO NORMAL. PILOT IN CHARGE ELECTED TO DIVERT TO NEAREST AIRPORT, L ANDED WITHOUT INCIDENT. FURTHER TROUBLESHOOTING INDICATED THAT THERE WAS AN INTERNAL FAILURE OF THE PITCH TRIM ACTUATOR . THE SUPECT COMPONENT WAS REMOVED, AND AN OVERHAULED REPLACEMENT WAS INSTALLED. 2 L 7 2 4T RT A18SW 2002072200012 20020722 00012 WP 2002 7 22 0202319919 1 20020717 A 2150 20495055 ACM DOUG DC9 DC932 3022066 WP RIGHT A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 01 941N 47450 FLIGHT ATTENDANT REPORTED SLIGHT HAZE, FUMES, AND THE AFT LAV SMOKE DETECTOR SOUNDED DURING TAKEOFF. SYMPTOMS LASTED A C OUPLE OF MINUTES THEN CLEARED AND THE ALARM STOPPED. FLIGHT RETURNED TO AN UNEVENTFUL LANDING AT MSP. MAINTENANCE REPLAC ED THE RIGHT ACM AND WATER SEPARATORS AND CLEARED DUCTS OF RESIDUE. RAN PACKS FOR TWO HOURS. NO HAZE OR SMELL DEVELOPED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002072200013 20020722 00013 CE 2002 7 22 JZ22002F00000 1 20020624 A 2910 620701098 LINE CESSNA 650 650 2076802 CE HYD SYSTEM CHAFED B JZ2R K NONE K FLUID LOSS IN INSP/MAINT 1 GL 03 900JD 5013 6500213 DURING A ROUTINE POST FLIGHT INSPECTION, A SIGNIFICANT AMOUNT OF HYDRAULIC FLUID WAS NOTICED ON THE RT WING LOWER SURFAC E FORWARD AND INBOARD OF THE MLG WW AREA. FURTHER INVESTIGATION REVEALED A RT WING SPOILER HYDRAULIC LINE ASSY. HAD C HAFED ON THE RT WING AILERON CONTROL ALCLAD CABLES TO THE POINT OF LEAKING FLUID. A NEW LINE ASSEMBLY WAS INSTALLED AND LINE ROUTING WAS ADJUSTED TO PROVIDE CLEARANCE FROM AILERON CONTROL CABLES. NO EVIDENCE OF LIKE CHAFING WAS DETECTED I N THE LT WING AREA. 2 L 7 2 4F A9NM 2002072200014 20020722 00014 EA 2002 7 22 MAS2002F00007 1 20020608 A 2750 114SD100501 BPSU CNDAIR CL600 CL6002B19 1900309 EA FLAP SYSTEM FAILED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 77181 7181 FLAPS FAIL CAUTION MESSAGE ON CLIMB OUT. AFTER AN UN-EVENTFUL LANDING. MECHANIC COMPLIED WITH. PART A AND B REPLACED THE BPSU AND THE NR 5 FLEX DRIVE. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002072200016 20020722 00016 NM 2002 7 22 MEX2002200 1 20020627 A 2923 PUMP DOUG MD88 MD88 3023688 NM HYD SYSTEM FAILED A ASMF O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 23 168PL 235 53174 CAPTAIN REPORT HIGH TEMPERATURE IN RT HYD SYSTEM. DURING CHECK WAS DETECTED SOME COMPONENTS IN RT HYDRAULIC COMPARTMENT WITH HIGH TEMPERATURE. FILTERS, HYD AUXILIARY PUMP AND HYD RESERVOIR ASSY WERE REPLACED IAW MM, TESTS OK. 2 L 7 2 4F RT A6WE 2002072200018 20020722 00018 2002 7 22 REX2002F00004 4 20020612 A 8300 PLUG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A 30015 NE ACCESSORY G/B LEAKING A REXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 25 8477R 7477 WHEN POWER WAS REDUCED ON FINAL APPROACH, THE RT ENGINE OIL PRESSURE WARNING ILLUMINATED. THE FLIGHT CREW DECLARED AN E MERGENCY AND SHUTDOWN RT ENGINE USING THE APPROVED CHECKLIST. AN OTHERWISE UNEVENTFUL LANDING WAS MADE. MAINTENANCE FO UND THE ACCESSORY GEARBOX DRIVE PLUG LEAKING. NEW PLUG AND O-RING WAS INSTALLED. THE ENGINE WAS SERVICED WITH OIL AND GROUND LEAK CHECKED WITH NO FURTHER LEAKAGE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002072200019 20020722 00019 WP 2002 7 22 0202359140 1 20020624 A 2150 DUCT DOUG DC9 DC914 3022034 WP WATER SEPARATOR DISCONNECTED A NWAA B EMER. DESCENT J O WARNING INDICATION OTHER CL CLIMB 1 GL 01 930RC 45729 AT 14,000 FEET, THE CABIN PRESSURE ANNUNCIATOR ILLUMINATED. CABIN ALTITUDE WAS 10,000 FEET. VERY SOON AFTER THE WARNING LIGHT CAME ON AND CABIN WENT TO 15,000 FEET AND MASKS DEPLOYED. COMPLIED WITH COM PROCEDURES AND PRESSURE CONTROLLER WAS FULL FORWARD. FLIGHT RETURNED TO MSP AND LANDED SAFELY. MAINTENANCE FOUND A BLOWN DUCT AT THE LEFT WATER SEPARATOR AND A LOOSE CLAMP AT THE RIGHT WATER SEPARATOR. INSTALLED THE DUCT AND SECURED THE CLAMP. REPACKED AL THE OXYGEN GENERATORS AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002072200020 20020722 00020 CE 2002 7 22 RU3A02004 1 20020627 A 2121 MS24166D1 RELAY BEECH 300 300BEECH 1152930 CE BLOWER BURNED E RU3A B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 15 74 FF9 WHITE SMOKE FILLED CABIN FROM BACK. OBSERVER SAID IT WAS NOT COMING FROM EQUIPMENT RACKS. SMELLED LIKE BURNING WOOD OR PAPER . FIRE DEPARTMENT FOUND NO UNUSUAL HOT SPOTS. RUNWAY 18R WAS CLOSED FOR APPROX 20 MIN WHILE FIRE DEPARTMENT INV ESTIGATED. AIRCRAFT WAS THEN TAXIED WITHOUT INCIDENT. FOUND K3 CONDENSER BLOWER RELAY (PN MS24166D1) BURNED. REPLACE D BLOWER RELAY AND TRANSORB DIODE. 2 L 7 2 4T A24CE 2002072200023 20020722 00023 NM 2002 7 22 UIE2002F00002 1 20020616 A 2612 CONNECTOR BOEING 747 747230B 1384889 NM FIRE LOOP DIRTY A UIEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 508MC 21644 AIR TURN BACK-AT TOP OF CLIMB ALL MAIN DECK FIRE WARNING LIGHTS ("A" AND "B" LOOPS) ILLUMINATED AT THE SAME TIME. AFTER 4 MINUTES ALL LIGHTS EXTINGUISHED SIMULTANEOUSLY. LOAD MASTER WENT DOWN TO THE MAIN DECK AND VERIFIED THAT NO FIRE WAS PRESENT. CREW DECIDED TO RETURN TO RMS. SYSTEM WAS TROUBLESHOT PER WDM. CLEANED CONNECTORS ON TEST PANEL, CHECKED CO NNECTOR ON NR 1 A & B SMOKE DETECTOR. CHECKED CONNECTORS FOR CLEANLINESS AND FOUND OK. SYSTEM TEST NORMAL. AIRCRAFT O K FOR SERVICE. 2 L 7 4 4F A20WE 2002072200025 20020722 00025 NE 2002 7 22 UIE2002F00003 2 20020622 A 7530 CLAMP BOEING 747 7472D3B 1384805 NM GE CF6 CF650C2 30018 NE NR 3 ENGINE LOOSE A UIEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 506MC 21252 AFTER TAKEOFF NR 3 ENGINE FIRE WARNING LIGHT CAME ON AND NACELLE HEAT FOR NR 3 ENGINE READ 8 ON BOTH SIDES. AFRTER LEVE LING OFF AND REDUCING POWER, THE LIGHT WENT OUT. ENGINE SHUT DOWN PERFHB AIRCRAFT RETURNED TO AIRPORT. C/A: FOUND 14T H STAGE DUCT CLAMPS LOOSE AT 3 POSITION. RESECURED DUCT. INSPECTED ALL ENGINE DUCTS AND PERFORMED LEAK CHECK PER PG. 2 L 7 4 4F 4 F RT A20WE E23EA 2002072200026 20020722 00026 WP 2002 7 22 W6N2002F00000 2 20020523 A 7230 BOLT BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110 01514 WP COMPRESSOR LOOSE B W6NR A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 25 120HR 752 P63198 WHILE IN FLIGHT/ FLIGHT CREW NOTICED SMOKE IN THE CABIN. LANDED AIRCRAFT SAFELY. MECHANICS FOUND OIL IN THE ENVIRONMEN TAL BLEED AIR ON THE RT ENGINE. INSPECTED ENGINE AND FOUND LOOSE THRU BOLTS ON THE COMPRESSOR BEARING STUDS. REMOVED E NGINE SENT. DISASSEMBLED GEARBOX OF ENGINE. FOUND CRACKED ACCESSORY DRIVE HOUSING AT COMPRESSOR BEARING CARRIER THRU B OLTS. ALL THRU BOLTS LOOSE ALSO. ENGINE IS NOW UNDER EVALUATION. 2 L 7 2 4T 4 T RT A21EU E4WE 2002102300050 20021023 00050 NM 2002 10 23 WRLA200212 1 20020528 A 3020 CONNECTOR DOUG MD11 MD11 3023602 NM ANIT ICE SYSTEM DISCONNECTED A WRLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 11 278WA 48746 NR 2 ANTI-ICE DISAGREE. (AIRCRAFT ABORTED TAKE OFF) CLEANED CONNECTOR PLUG NR 2 ANTI-ICE OPERATED SEVERAL TIMES OPS C HECKED NORMAL. CLEANED AND RESET CONNECTOR PLUG. POOR CONNECTION AT CONNECTOR PLUG. 2 L 7 3 4F RT A22WE 2002072200027 20020722 00027 EA 2002 7 22 WVE2002F00014 1 20020618 A 2760 600913621 CLAMP CNDAIR CL600 CL6002B16 1900305 EA POSITION XMITTER CRACKED B WVER K NONE L NO TEST IN INSP/MAINT 1 EA 09 309FX 5306 DURING A, 2A, 4A, AND 12A CHECKS THE CLAMP SECURING THE LEFT FLIGHT SPOILER POSITION TRANSMITTER WAS FOUND CRACKED. STR ESS FROM OVER TORQUE OF THE TRANSMITTER CLAMP BOLT/NUT. 2 L 7 2 4F RT A21EA 2002072200028 20020722 00028 EA 2002 7 22 WVE2002F00015 1 20020620 A 5242 6003512865 STRUCTURE CNDAIR CL600 CL6002B16 1900305 EA E/E BAY DOOR DAMAGED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 309FX 5306 DURING ACCOMPLISHMENT OF EO, AFT EQUIPMENT BAY DOOR MODIFICATION REPAIR FOUND THE AFT SERVICE DOOR DAMAGED AT THE DOOR O PEN SUPPORT STRUT ATTACHMENT LT AND RT SIDE. 2 L 7 2 4F RT A21EA 2002072200030 20020722 00030 WP 2002 7 22 AALA20020620 1 20020506 A 3244 ETY2132547 TIRE DOUG DC9 DC983 3022083 WP RT MLG FAILED A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 21 589AA 53252 BNA - FLT 1307 - EN ROUTE BNA-LAX - TIRE BLEW ON TAKEOFF. RETURNED BNA AND LANDED WITHOUT INCIDENT. REPLACED NR 3 AND 4 MLG TIRE AND WHEEL ASSEMBLY. RIGHT MLG SPRAY DEFLECTOR, RIGHT MLG DOWNLOCK SENSOR. SYSTEM GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 2 4F RT A6WE 2002072200031 20020722 00031 WP 2002 7 22 AALA20020621 1 20020506 A 3222 5920602513 STRUT DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 463AA 49593 LAX - FLT 808 - EN ROUTE LAX-SJC - NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. RETURNED AND LANDED LAX WITHOUT INCIDENT. REPLACED INNER CYLINDER AND OUTER CYLINDER. REPACKED GEAR, PRESSURE CHECK OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002072200032 20020722 00032 WP 2002 7 22 AALA20020645 1 20020512 A 3610 5953625521 DUCT DOUG DC9 DC983 3022083 WP A/C BAY BLOWN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 598AA 53288 EWR - FLT 1927 - ON CLIMB-OUT, EN ROUTE EWR-ORD, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER AIRFOIL ANTI- ICE SWITCHES PLACED ON. LIGHT WENT OUT AFTER COMPLETED PROCEDURE. PRESSURIZATION FLOW LIGHT ALSO CAME ON SEVERAL TIMES . RETURNED AND LANDED EWR WITHOUT INCIDENT. REPLACED RAM AIR EXHAUST DUCT. (M) 2 L 7 2 4F RT A6WE 2002072200033 20020722 00033 2002 7 22 USA2002F00057 4 20020621 A 2565 D30664105 SLIDE AIRBUS 320 A320214 3930316 EU PASSENGER CABIN INTERMITTENT A USAA K NONE J W WARNING INDICATION INADEQUATE Q C TX TAXI/GRND HDL 1 EA 19 106US 1044 THE FORWARD CABIN, RIGHT SIDE, EMERGENCY ESCAPE SLIDE WAS DIFFICULT TO ARM AND INTERMITTENTLY INDICATED DISARMED. MAINT ENANCE REPLACED THE EMERGENCY ESCAPE SLIDE. OPERATIONAL CHECKED OK. 2 L 7 2 4F RT A28NM 2002072200034 20020722 00034 SO 2002 7 22 ASOA02187 1 20020325 A 3350 1317 LIGHT EMB 120 EMB120RT 3260202 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 232AS 120036 DURING A HANGAR INSPECTION IN MCN, THE FORWARD OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED ADN REPLAC ED THE BURNED OUT OVERHEAD EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002072200036 20020722 00036 NM 2002 7 22 AWXA200200543 1 20020614 A 5414 311N504614 SKIN BOEING 757 7572S7 1384962 NM NR 1 PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 LCQ - MAJOR REPAIR - DURING C-8 INSPECTION A CRACK WAS FOUND ON THE NR 1 ENGINE PYLON FRAME AT THE LOWER FORWARD CORNER OF ACCESS APNEL 433AL CUTOUT. MAINTENANCE STOP DRILLED CRACK IAW B757 SRM 51-10-02 PAGE 17. FABRICATED REPAIR DOUBLER .1 25 STELL 15 SPH, HEAT TREATED IAW BAC 5619 PAGE 5 AND PASSVATED DOUBLER IAW E.R. 19-5451-02163-SS3. MAINTENANCE THEN INS TALLED DOUBLER AND ACCESS PANEL IAW AWA ER 19-5451-02163-SS3. 2 L 7 2 4F RT A2NM 2002072200037 20020722 00037 NM 2002 7 22 AWXA200200544 1 20020522 A 5532 174N3000 SKIN BOEING 757 7572S7 1384962 NM VERTICAL STAB CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 23567 DURING C-8 INSPECTION TWO CHAFED AREAS OF SKIN WERE FOUND ON THE VERTICAL STAB LEADING EDGE AT FIN STATION 80 AND 90. MAINTENANCE BLENDED AND REMOVED CHAFED AREAS OF SKIN AT FSS STA.80 PER ASTM E797-95 PAGES 369-374 AND B757 SRM 55-30-01 FIG 101 PAGE 104. MAINTENANCE BLENDED AND REMOVED CHAFFED AREA OF SKIN AT FSS STA 90 IAW ASTM 797-95 PAGES 369-374 AND B 757 SRM 55-30-01 FIG 101 PAGE 104. MAINTENANCE TREATED AND PRIMED AREAS IAW B757 SRM 51-20-01 PAGE 9 AND B757 AMM 51-21- 10 PAGE 701. MAINTENANCE INSTALLED REPAIR DOUBLERS IAW B757 SRM 55-30-01 PAGES 201-202. 2 L 7 2 4F RT A2NM 2002072200038 20020722 00038 NM 2002 7 22 AWXA200200545 1 20020609 A 5315 6533940179 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 DURING C-16 INSPECTION CORROSION WAS FOUND ON FLOORBEAM UPPER FLANGE AREA AT BS 294.5 LBL 11 TO LBL 14. MAINTENANCE REMO VED FLOORBEAM UPPER T-CHORD, FROM LBL 21.5 TO RBL 60, 2 L 7 2 4F RT A16WE 2002072200039 20020722 00039 NM 2002 7 22 AWXA200200548 1 20020621 A 7830 WARNING LIGHT BOEING 737 73733A 1384673 NM NR 1 ENG T/R ILLUMINATED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 174AW 23633 ABORTED TAKEOFF - FLT 0130 - TAKING OFF FROM SNA TO LAS. NR 1 ENGINE THRUST REVERSER LIGHT ILLUMINATED ON TAKEOFF AT 10 0KTS. NR 1 THRUST REVERSER DEACTIVATED AND PLACED ON "MEL 78-7 CONDITION NR 1. SUPPLIMENTAL OPEN 2 L 7 2 4F RT A16WE 2002072200040 20020722 00040 NM 2002 7 22 AWXA200200550 1 20020622 A 2121 6454051 FAN BOEING 737 7373G7 1384595 NM ZONE 210 BURNED OUT A AWXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 308AW 50108 8227 24710 DURING TAXI OUT A WHINING NOISE WAS HEARD AND A BURNING SMELL FILLED CABIN. RETURNED TO GATE AND FOUND THE CABIN AIR REC IRCULATION FAN CIRCUIT BREAKER HAD OPENED. CIRCUIT BREAKER WAS COLLARED AND SYSTEM WAS PLACED ON MEL 21-31-C1, RECIRCULA TION FAN INOPERATIVE. MAINTENANCE AT PHX REMOVED AND REPLACED THE CABIN AIR RECIRCULATION FAN IAW BMM 21-21-22, OPERATI ONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002072200042 20020722 00042 NM 2002 7 22 AWXA200200557 1 20020620 A 5320 654581211 STIFFENER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 DURING INSPECTION A 3/8 INCH CRACK WAS FOUND ON LT SIDE FORWARD FACE OF FLOORBEAM STIFFNER JUST ABOVE BATTERY BOX, BS 32 8, LBL 27. MAINTENANCE REMOVED CRACKED STIFFNER AT BS 328, LBL 27. FABRICATED A NEW STIFFNER AND INSTALLED REPAIR IAW DW G 65-45812, AND B737-300 SRM 51-40-02, PG. 3, 10, 11, & 38. 2 L 7 2 4F RT A16WE 2002072200043 20020722 00043 NM 2002 7 22 AWXA200200558 1 20020609 A 5315 654581094 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 DURING C-16 CHECK CORROSION WAS FOUND OF FLOORBEAM UPPER FLANGE AT BS 312, RBL 8.5 TO RBL 12. MAINTENANCE BLENDED CORROS ION AND FOUND MATERIAL LOSS TO EXCEED ALLOWABLE LIMITS, REMOVED DAMAGED FLOORBEAM UPPER TEE FROM EXISTING REPAIR SPLICE RBL 8.5 TO RBL 61.5, FABRICATED A NEW FLOORBEAM UPPER TEE, AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG. 44-45, AN D SRM 53-10-51, PG. 220-223. 2 L 7 2 4F RT A16WE 2002072200045 20020722 00045 NE 2002 7 22 AWXA200200561 2 20020623 A 7261 LINE AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 1 ENGINE LOOSE A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 804AW 1049 FLT 841 - ENROUTE FROM PHX TO RDU THE NR 1 ENGINE INDICATED LOW OIL QUANTITY, ENGINE WAS LOSING OIL AT A RATE OF 1 QUAR T OF OIL IN 5 MINUTES, DIVERTED AND LANDED AT BNA, UPON ARRIVAL AT GATE ENGINE HAD 7.5 QUARTS OF OIL REMAINING. MAINTE NANCE INSPECTED THE NR 1 ENGINE AND FOUND THE OIL FEED LINE AT THE BOTTOM OF THE ENGINE JUST AFT OF THE FORWARD EDGE OF C-DUCTS LOOSE AND LEAKING OIL. RETORQUED AND SAFETIED THE LINE, RAN ENGINE WITH NO LEAKS NOTED. PERFORMED MAINTENANCE IA W AMM 70-23-11, AND 71-00-00-710-012. 2 L 7 2 4F 4 F RT A28NM E40NE 2002072200051 20020722 00051 NM 2002 7 22 2002UALA00963 1 20020608 A 5512 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 940UA 26675 LEFT HAND HORIZONTAL STABILIZER REMOVABLE LEADING EDGE INBOARD END SKIN IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALL ED FLUSH REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072200052 20020722 00052 NM 2002 7 22 2002UALA00964 1 20020608 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 940UA 26675 AFT CABIN FLOORBEAM GOUGED AT STATION 986 RBL 44 INCH. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072200053 20020722 00053 NM 2002 7 22 2002UALA00965 1 20020609 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 939UA 26672 FORWARD CABIN STATION 295 RBL 54 WL 208 FUSELAGE FRAME IS CRACKED ON INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. MANUFA CTURED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072200054 20020722 00054 NM 2002 7 22 2002UALA00966 1 20020610 A 5310 CREASE BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 939UA 26672 CABIN CREASE BEAM INNER CHORD IS CRACKED AND CORRODED BS 280-360. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072200055 20020722 00055 EU 2002 7 22 AWXA200200562 1 20020624 A 2121 VD390003 FAN AIRBUS 320 A320232 3930326 EU CABIN BURNED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 649AW 16849 803 FLT 175 - DURING FLT, PAX AND F/A REPORTED A STRONG ELECT BURNING ODOR AT OVER WING AREA, F/O VERIFIED BURNING ODOR AND A/C DIVERTED. ENGS WERE RUN TO T/O POWER AND PACKS WERE OPERATED BOTH SEPARATE AND TOGETHER IN BOTH THE HOT AND COLD M ODE. HYD PUMPS WERE OP CKD AND INSPECT. CIDS PANEL WAS CKD FOR STATUS FAULTS AND THE CFDS WAS CKD FOR POST FLT REPORTS. ALL SYSTEMS OPED NORM AND NO DEFECTS NOTED. PREPARING FOR DEPARTURE, A BURNING ODOR WAS NOTICED AT MID CABIN, ONBO ARD MAINT TECH FOUND ODOR FROM AFT CABIN FAN (14HG), BOTH FWD AND AFT RECIRC FANS WERE PLACED ON MEL 21-21-01 COND. 2. A/C DEPARTED AND ARRIVED WITHOUT FURTHER INCIDENT. MAINT R/R THE RT RECIRC FAN (14HG) AND FILTERS, OP CK WAS GOOD. 2 L 7 2 4F RT A28NM 2002072200056 20020722 00056 NE 2002 7 22 CX7A194J12 2 20020720 A 7320 6068T72P23 HMU SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE A CX7A A UNSCHED LANDING O OTHER CL CLIMB 1 GL 03 304CE 11000 199 340B198 785545 During climbout of MDW noticed that L/H engine torque was fluctuating 3%. Fluctuations then went to 5% swings. Ran che cklist and put in T/M lockout. With T/M lockout engine still fluxed +/- 3% with prop sync on and off.R/R L/H engine HMU IAW SAAB AMM 2 L 7 2 4T 4 T RT A52EU E8NE 2002072200058 20020722 00058 NM 2002 7 22 SWAA021566 1 20020714 A 2731 TRIM TAB BOEING 737 7377H4 1384404 NM ELEVATOR VIBRATION A SWAA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SW 29 700GS 27835 DURING CLIMB AIRCRAFT STARTED A HIGH RATE OF VIBRATION WHICH WAS FELT UNDER PILOT'S SEAT AND FEET, ALSO FELT THROUGH OUT CABIN BY F/A. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TABS. REMOVED AND REPLACED NR 1 ENG IDG. REMOVED AND REPL ACED NR 2 ENG MOUNT HARDWARE. COMPLIED WITH AIRFRAME VIBRATION CONDITION INSP, OPS CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 2002072200059 20020722 00059 NM 2002 7 22 VNAA0207003 1 20020702 A 2450 230GC02Y02 CONTROL PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 460PS 637 3061 AFTER THE PASSENGERS HAD BEEN BOARDED, HALFWAY THROUGH THE PREFLIGHT BRIEFING SMOKE BEGAN FORMING IN THE CABIN. THE FIR ST OFFICER EVACUATED THE PASSENGERS AND THEN THE FLIGHT ATTENDANT. THE APU GENERATOR HAD FAILED, THUS CAUSING THE HX FA N TO NOT OPERATE WHICH CAUSED THE LEFT HAND PACK TO OVERHEAT. THE FIRE DEPARTMENT WAS DISPATCHED TO THE AIRCRAFT. THE FIRST OFFICER, FLIGHT ATTENDANT, AND FIRE FIGHTERS LOOKED FOR EVIDENCE OF A FIRE. THE AIRCRAFT WAS FERRIED TO DAY WHER E MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL AND THE BUS POWER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072200060 20020722 00060 NM 2002 7 22 VNAA0207004 1 20020705 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 426JS 3038 DURING TAKEOFF, THE CREW RECEIVED A CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. AFTER EXITING THE RUNWAY, THE SYSTEM RESET ITSELF AND THE MESSAGE EXTINGUISHED. FLIGHT 4159 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072200061 20020722 00061 NE 2002 7 22 VNAA0207005 2 20020707 A 7200 ENGINE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT SURGES A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 462PS 3084 DURING TAKEOFF, THE RIGHT HAND ENGINE SURGED AND THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL CAS MESSAGE. THE CREW AB ORTED TAKEOFF. THE CREW THEN FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE MESSAGE CLEARED. FLIGHT 4090 WAS THEN CLEAR ED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072200062 20020722 00062 NM 2002 7 22 UIE2002F00007 1 20020514 A 5730 65B1496431 PANEL BOEING 747 7472D7B 1384803 NM GAP PANEL SEPARATED A UIEA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 EA 15 527MC 22471 TURN BACK DUE TO ENGINE NR 1 AND ENGINE NR 4 GAP PANELS SEPARATED FROM AIRCRAFT ON TAKE OFF ROLL. INSTALLED NR 1 ENGINE GAP PANEL ISW SRM. REPAIRED NR 4 GAP PANEL PER SRM. REINSTALLED GAP PANEL ON NR 4 ENGINE IAW MM. CHAPTER 5 INSPECTIO N NOT REQUIRED. ACCOMPLISHED A GENERAL THROUGH VISUAL INSPECTION OF THE FUSELAGE, TAIL, WINGS, GEARS AND ENGINES. NO D ISCREPANCIES FOUND. 2 L 7 4 4F RT A20WE 2002072200064 20020722 00064 NM 2002 7 22 2002UALA00968 1 20020607 A 5315 141W85191 FLOORBEAM BOEING 777 777222 1385219 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 207UA 12816 30213 246 MIDCHORD CRACKED AT RBL 38. MAJOR REPAIR ACCOMPLISHED. CRACKED MID CHORD REPAIRED PER 777 SRM 53-10-51. 2 L 7 2 4F RT T0001SE 2002072200065 20020722 00065 NM 2002 7 22 2002UALA00969 1 20020607 A 5315 141W85191 FLOORBEAM BOEING 777 777222 1385219 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 207UA 12816 30213 STA 246 MIDCHORD (FLOORBEAM) CRACKED AT LBL 38.5. MAJOR REPAIR ACCOMPLISHED. CRACKED MID CHORD REPAIRED PER 777 SRM 53 -10-51. 2 L 7 2 4F RT T0001SE 2002072200068 20020722 00068 NM 2002 7 22 2002UALA00972 1 20020607 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 BS 287 FLOORBEAM CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072200069 20020722 00069 NM 2002 7 22 2002UALA00973 1 20020610 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 AFT CABIN RIGHT HAND SIDE FRAME AT STA 887 IS CRACKED WHERE AIR GRILL ATTACHES. MAJOR REPAIR ACCOMPLISHED. INSTALLED D OUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072200070 20020722 00070 EU 2002 7 22 AWXA200200566 1 20020625 A 7500 6730B01 VALVE AIRBUS 320 A320232 3930326 EU NR 1 & 2 ENG FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 648AW 17626 770 FLT 0751 - DURING CLIMB AT 6000 FT A NR 2 ENGINE BLEED OCCURRED (315 DEG C NOTED) , THE CROSS-BLEED VALVE OPENED AND BOT H PACKS WERE RUNNING OFF THE NR 1 ENGINE, ATTEMPTED TO START APU BUT THE APU AUTO SHUTDOWN, NR 1 ENGINE THEN EXPERIENCED A BLEED FAULT, AIRCRAFT TURNED BACK TO PHX. MAINTENANCE TROUBLESHOT AND REPLACED THE NR 1 & NR 2 ENGINE FAN AIR VALV ES IAW AMM 36-11-54-401, PG. 1-6, OPERATIONAL CHECKS WERE GOOD IAW AMM 71-00-00-710-043. AS A PRECAUTION BOTH THE NR 1 & 2 ENGINE TEMPERATURE CONTROL THERMOSTATS WERE REPLACED. MAINT ALSO R&R THE APU PNEUMATIC SENSOR ASSEMBLY TO CORRECT TH E APU AUTO SHUTDOWN PROBLEM, LEAK AND OPERATIONAL CHECK WERE GOOD. 2 L 7 2 4F RT A28NM 2002072200071 20020722 00071 2002 7 22 2002UALA00974 4 20020610 A 3442 6225122103 POWER SUPPLY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RADAR CONTAMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 534UA 25129 WEATHER RADAR FAIL ANNUNCIATED. SUPPLEMENTAL DATA UPDATE THE UNIT HAD A FAILED POWER SUPPLY ASSEMBLY. NOTE WORTHY IS TH AT THE UNIT HAD BEEN ON THE AIRCRAFT SINCE 01AUG96 AND WAS TOTALLY CLOGGED WITH DUST WHICH ULTIMATELY LED TO THE POWER S UPPLY FAILURE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072200074 20020722 00074 NM 2002 7 22 AWXA200200569 1 20020626 A 3350 321430 BATTERY PACK AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 812AW 1178 DURING INSPECTION THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERG ENCY POWER SUPPLY UNIT (12WL) AND BATTERY PACK AT RT OVERWING DOOR IAW AMM 33-51-38-000-001, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002072200075 20020722 00075 NM 2002 7 22 AWXA200200570 1 20020628 A 2560 P4010021000 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 830AW 1565 DURING INSPECTION THE AFT LT EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN THE AFT LT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002072200076 20020722 00076 EU 2002 7 22 2002UALA00975 1 20020609 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 438UA 678 EMERGENCY EXIT LIGHT BETWEEN OVERWING DOORS INOPERATIVE ON TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2002072200077 20020722 00077 NM 2002 7 22 AWXA200200571 1 20020630 A 3260 189915 UPLOCK SENSOR BOEING 737 7373G7 1384595 NM LT MLG DEFECTIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 160AW 23782 FLT 0484 - AFTER T/O, LT MLG INDICATED UNSAFE AFTER RETRACTION. RECYCLED THE GEAR AND STILL HAD AN UNSAFE INDICATION. G EAR WAS CLEARLY RETRACTED WITH NO BUFFET, NOISE OR YAW. TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOV ED AND REPLACED THE LT MLG UPLOCK SENSOR IAW BMM 32-61-21-4. OPERATIONAL CHECK WAS GOOD IAW BMM 32-61-00-5. 2 L 7 2 4F RT A16WE 2002072200078 20020722 00078 NM 2002 7 22 AWXA200200572 1 20020628 A 3350 20121 CHARGER BOEING 757 7572S7 1384962 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 904AW 23566 DURING INSPECTION ALL FIRST CLASS SEAT EMERGENCY ESCAPE PATH LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE BATTERY CHARGER , OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002072200079 20020722 00079 NM 2002 7 22 2002UALA00976 1 20020610 A 5320 CHANNEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 CABIN FLOOR STRUCTURE AT STA 334, WL 208, BL 0 TO RBL 25, U-CHANNEL INTERCOSTAL HAD EXCESSIVE CORROSION ON UPPER SURFACE . MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW U-CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072200080 20020722 00080 NM 2002 7 22 2002UALA00977 1 20020611 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 MID-CABIN FLOORBEAM STA 880, LBL 49 TO 65, IS GOUGED AROUND CLIP NUT HOLES, FORWARD TOP SIDE AND AFT LOWER SURFACE RADIU S. MAJOR REPAIR ACCOMPLISHED. INSTALLED FREEZE PLUG AND STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072200081 20020722 00081 NM 2002 7 22 PCAA0207077 1 20020719 A 7931 PW120A ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT LEAKING A PCAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 13 838EX 28043 4464 220 120900 HVN-PHL FLIGHT#3702. CREW REPORTED AFTER CLIMBOUT AT 16,000 FEET, #1 ENGINE OIL PRESSURE BETWEEN 40-45 PSI. NUMBER ONE E NGINE SHUT DOWN, DIVERTED TO LGA, EMERGENCY DECLARED. MAINTENANCE FOUND ENGINE FORWARD BREATHER CARBON SEAL NICKED,CAUSE D BY DISTORTED MATING SURFACE OF MAIN ACCESSORY GEAR SHAFT ASSEMBLY. CARBON SEAL REPLACED. ENGINE ASSEMBLY REPLACED IN A CCORDANCE WITH JOBCARD 008-71-01-349, PRATT AND WHITNEY MAINTENANCE MANUAL 71-00, AND DEHAVILLAND DASH 8 MAINTENANCE MA NUAL 71-00. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002072200082 20020722 00082 NM 2002 7 22 2002UALA00978 1 20020610 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 BS 786, LBL 12, FLOORBEAM CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW FLOORBEAM SECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072200083 20020722 00083 NM 2002 7 22 2002UALA00979 1 20020610 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 BS 830-870, RBL 11, WL 200, UPPER CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM REPAIR . 2 L 7 2 4F 4 F RT A1NM E24NE 2002072200084 20020722 00084 NM 2002 7 22 2002UALA00980 1 20020610 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 BS 852, LBL 34, FLOORBEAM CORRODED, MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SECTION AND SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072200085 20020722 00085 EU 2002 7 22 AWXA200200573 1 20020628 A 2560 P20700012015 FLASHLIGHT AIRBUS 320 A320231 3930325 EU CABIN FAILED A AWXA O OTHER L NO TEST TX TAXI/GRND HDL 1 WP 28 634AW 091 FLIGHT CREW REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT WAS NOT INDICATING PROPER CHARGE. MAINTENANCE REMOVED AND RE PLACED THE FWD CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK OF NEW FLASHLIGHT GOOD. 2 L 7 2 4F RT A28NM 2002072200086 20020722 00086 NM 2002 7 22 AWXA200200574 1 20020630 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM SEAT ROW 4 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT WAS FOUND INOPERATIVE AND BROKEN OFF SEAT. MAINTENAN CE REPLACED BOTTLE CAP SEAT LIGHT ASSEMBLY AT SEAT ROW 4 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002072200087 20020722 00087 NM 2002 7 22 2002UALA00981 1 20020610 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 BS 1809.5, RT EXTERIOR FUSELAGE, HAS EXCESSIVE CHAFFING AT LOWER BANANA FAIRING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072200088 20020722 00088 NM 2002 7 22 2002UALA00982 1 20020610 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 BS 1809.5, LT FUSELAGE AT HORIZONTAL STABILIZER, LOWER SURFACE SKIN CHAFFED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002092000046 20020920 00046 NM 2002 9 20 AWXA200200575 1 20020630 A 2751 2061141 INDICATOR BOEING 737 7373G7 1384595 NM COCKPIT FALSE INDICATION A AWXA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 WP 28 154AW 7976 23776 LAX - DIVERSION - FLT 0663 - EN ROUTE FROM PHX TO SNA WHEN FLAPS WERE LOWERED TRAILING EDGE FLAPS SPLIT AND WOULD NOT EX TEND PAST 2 UNITS OF FLAPS DOWN, DIVERTED TO LAX WITH LONGER RUNWAY. MAINTENANCE REMOVED AND REPLACED THE LT TRAILING ED GE FLAP POSITION INDICATOR IAW BMM 27-58-41, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002072200089 20020722 00089 NM 2002 7 22 2002UALA00983 1 20020612 A 5310 CREASE BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 940UA 26675 CABIN CREASE BEAM WEB IS CORRODED BODY STATION 747-767, LBL 70, WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072200090 20020722 00090 NM 2002 7 22 AWXA200200577 1 20020630 A 3350 900542 POWER SUPPLY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 DURING INSPECTION THE EMERGENCY EXIT LIGHTS AT BOTH LWR L2 & R2 DOORS WERE FOUND INOPERATIVE, RELAMP NO HELP. MAINTENANC E REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY, OPERATIONAL CHECK WAS GOOD IAW BMM 33-51-11. 2 L 7 2 4F RT A16WE 2002072200091 20020722 00091 NM 2002 7 22 AWXA200200578 1 20020630 A 3350 900542 POWER SUPPLY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 DURING INSPECTION THE LOWER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE ON LEFT EMERGENCY EXIT DOOR. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY, OPERATIONAL CHECK WAS GOOD IAW BMM 33-51-11. 2 L 7 2 4F RT A16WE 2002072200092 20020722 00092 2002 7 22 2002UALA00984 4 20020611 A 3442 6225122103 TRANSCEIVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RADAR FAULTY A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 531UA 25042 WEATHER RADAR INOPERATIVE. THE POWER OUT IS MEASURING 125W MAXIMUM, DURING TEST. THE MINIMUM ACCEPTABLE POWER OUTPUT F OR A SERVICEABLE UNIT IS 175W. MOST UNITS ARE IN THE 250W RANGE. REPLACED THE A5 ASSEMBLY . THE LRU'S LOW POWER OUT C ONDITION CORRELATES TO THE WRITE-UP OF NO RETURN BEYOND 40NM RANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072200093 20020722 00093 EU 2002 7 22 AWXA200200579 1 20020703 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 651AW 14713 866 DURING INSPECTION THE FORWARD SECTION EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMER GENCY POWER SUPPLY UNIT ABOVE (10WL) OVER THE L1 DOOR, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002072200094 20020722 00094 NM 2002 7 22 AWXA200200580 1 20020703 A 3350 BR364411 LIGHT BOEING 737 7373B7 1384580 NM SEAT ROW 9 MISSING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 FAA RAMP CHECK IDENTIFIED THE WHITE EMERGENCY LIGHT MISSING FROM SEAT ROW 9 LT. MAINTENANCE INSTALLED WHITE EMERGENCY LI GHT ON SEAT ROW 9 LT PER E.O. 33-50-37, AND DWG BR 2013-P-7373HP. 2 L 7 2 4F RT A16WE 2002072200097 20020722 00097 EU 2002 7 22 AWXA200200587 2 20020625 A 7200 ENGINE BOEING 737 7373Q8 1384670 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 MALFUNCTIONED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 327AW 23507 721714 FLT 0662 - AFTER BEING CLEARED FOR TAKEOFF AND RELEASING THE BRAKES BOTH ENGINES SPOOLED UP EVENLY. SELECTED THE TOGA B UTTON AND THE NR 1 ENGINE ACCELERATED NORMALLY, NR 2 ENGINE DID NOT RESPOND TO THRUST LEVER MOVEMENT. WAITED 2 TO 3 SECO NDS FOR NR 2 ENGINE TO RESPOND, NO RESPONSE WAS DETECTED SO BOTH THRUST LEVERS WERE RETARDED TO IDLE AND TAKEOFF WAS RE JECTED. TAXIED OFF RUNWAY AND CHECKED ENGINE PARAMETERS, ALL ENGINE WERE PARAMETERS NORMAL. RE-CLEARED FOR TAKEOFF AND B OTH ENGINES SPOOLED EVENLY WITH NR 2 SOMEWHAT SLOWER. AIRCRAFT DEPARTED FOR SCHEDULED DESTINATION. 2 L 7 2 4F 4 F RT A16WE E21EU 2002072200098 20020722 00098 NM 2002 7 22 2002UALA00986 1 20020611 A 5210 VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 DOOR 2R DOOR ASSIST BOTTLE PRESSURE OVER LIMIT AT 2100 PSI. FOUND SCHRADER SERVICE VALVE BAD. REPLACED VALVE AND SEAL. SERVICED AND CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2002072200099 20020722 00099 NM 2002 7 22 AWXA200200588 1 20020709 A 2560 P2070001214 FLASHLIGHT BOEING 737 737300 1384610 NM LAVATORY INOPERATIVE A AWXA O OTHER L NO TEST TX TAXI/GRND HDL 1 WP 28 331AW 23747 FLIGHT CREW REPORTED THE FOWARD BULKHEAD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FOWA RD BULKHEAD EMERGENCY FLASHLIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002072200100 20020722 00100 NM 2002 7 22 AWXA200200590 1 20020710 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 311AW 24712 DURING INSPECTION THE FORWARD GALLEY EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FO RWARD GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002072200101 20020722 00101 EU 2002 7 22 AWXA200200591 1 20020710 A 2120 87292325V04 COMPUTER AIRBUS 320 A320232 3930326 EU COCKPIT FAILED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 669AW 352 1792 FLT 0645 - ON TAKE-OFF ROLL RECEIVED ECAM "AVIONICS VENT, AVIONICS SMOKE" MESSAGES. REJECTED TAKEOFF AND RETURNED TO GA TE. MAINTENANCE TROUBLESHOT AVIONICS EQUIPMENT VENTILATION COMPUTER (AEVC) FAULT AND REPLACED THE AEVC COMPUTER PER TASK 21-26-34-000-001, OPERATIONAL CHECK WAS GOOD IAW 21-26-710-001. 2 L 7 2 4F RT A28NM 2002072200102 20020722 00102 NM 2002 7 22 AWXA200200592 1 20020710 A 2560 P4010021 BATTERY BOEING 737 737277 1384570 NM LAVATORY DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 180AW 22647 FORWARD EMERGENCY FLASHLIGHT INOPERATIVE, PLACED IN CHARGER BACKWARDS. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMER GENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002073000023 20020730 00023 EU 2002 7 30 AWXA200200594 1 20020710 A 2421 740120C GCU AIRBUS 320 A320232 3930326 EU NR 2 ENGINE FAILED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 665AW 2098 1644 ATL - ABORTED TAKEOFF - FLT 0615 - ON TAKEOFF OUT OF ATL EN ROUTE FOR PHX AT APPROXIMATELY 70 KTS THE NR 2 GENERATOR FAU LTED OFF LINE, REJECTED TAKEOFF AND RETURNED TO GATE. CONTRACT MAINTENANCE MADE LOG BOOK ENTRY FOR MEL 24-20-01, COND. 2 - NR 2 INTEGRATED DRIVE GENERATOR (IDG) INOPERATIVE AND AIRCRAFT DEPARTED FOR PHX. AT PHX MAINTENANCE TROUBLESHOT WIRIN G TO IDG CHECKING PINS 12, 13, & 14 FINDING NO DEFECTS. REMOVED AND REPLACED NR 2 GENERATOR CONTROL UNIT PER AMM 24-22-0 00-001. PERFORMED ENGINE RUN OPERATIONAL CHECK ON NR 2 ENGINE, NO DEFECTS NOTED. **SUPP** VENDOR BENCH TEST OF GENERATOR CONTROL UNIT S/N 6697 CONFIRMED FAILURE, UNIT FAILED INCOMING TEST TS5221 ISOLATING FAILURE TO THE A2PWBA R43 EXCITER F 2 L 7 2 4F RT A28NM 2002072200104 20020722 00104 EU 2002 7 22 AWXA200200595 1 20020710 A 3150 350E017271616 COMPUTER AIRBUS 320 A320232 3930326 EU FLIGHT WARNING DEFECTIVE A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 650AW 37601 8939 856 FLT 0185 - ON TAKEOFF ROLL THE NR 2 FLIGHT WARNING COMPUTER (FWC) FAULTED, REJECTED TAKEOFF AT LESS THAN 80 KTS. MAINT ENANCE PLACED SYSTEM ON MEL 31-53-01, FOR FWC NR 2 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 FWC IAW AMM 31-52-00-0001. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002072200106 20020722 00106 NM 2002 7 22 2002UALA00989 1 20020607 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 BS 287 FLOORBEAM CRACKED, LEFT HAND SIDE. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072200107 20020722 00107 NE 2002 7 22 AWXA200200596 2 20020709 A 7200 ENGINE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 FIRE A AWXA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 WP 28 646AW 271 VO219 FLT 0279 - AFTER LANDING AT IAH INBOUND FROM PHX, AFTER ENGINE SHUTDOWN AT GATE, GROUND CREW OBSERVED FIRE IN THE TAILPI PE OF THE NR 1 ENGINE. FLIGHT CREW MOTORED ENGINE APPROXIMATELY 1 MINUTE BEFORE FLAME EXTINGUISHED, ESTIMATE TAILPIPE FI RE LASTED TOTAL OF 2-3 MINUTES. THERE WERE NO FIRE WARNING OR OVERHEAT INDICATIONS ON FLIGHT DECK. MAINTENANCE INSPECTED THE NR 1 ENGINE, NO OIL WAS FOUND POOLING IN THE TAILPIPE, AND NO LEAKAGE AT THE NR 7 TURBINE BLADES. PERFORMED ENGINE RUN, OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2002072200108 20020722 00108 NM 2002 7 22 2002UALA00990 1 20020610 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 CABIN FLOORBEAM UPPER SURFACE CORRODED AT BS 800-825, RBL 54. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072200109 20020722 00109 EU 2002 7 22 AWXA200200597 1 20020711 A 3350 E0261CF22 WIRE AIRBUS 320 A320231 3930325 EU SEAT ROW 2 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 55 FLT 0683 - EMERGENCY AISLE LIGHTS INOPERATIVE SEAT ROWS 1 & 2. MAINTENANCE REPAIRED BROKEN WIRE UNDER SEAT ROW 2, OPERAT IONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 2002072200110 20020722 00110 NM 2002 7 22 AWXA200200598 1 20020711 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM SEAT ROW 12 INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 325AW 23260 EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 LT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 12 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002072200111 20020722 00111 NM 2002 7 22 2002UALA00991 1 20020613 A 5320 STRAP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 940UA 26675 STRINGER 21R, STATION 951 TOP STRAP HAS BAD HOLE WITH CRACK ABOVE STRINGER FRAME ATTACH POINT. MAJOR REPAIR ACCOMPLISHE D REPLACED STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072200112 20020722 00112 NM 2002 7 22 AWXA200200599 1 20020623 A 5347 6545410200 SEAT TRACK BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 DURING C-18 CHECK A 1 5/8 INCH CRACK WAS FOUND COMING FROM FASTENER HOLE ON MAIN CABIN SEAT TRACK OUTBOARD FLANGE BS 727 B, WL 208.1, RBL 46. MAINTENANCE CUTOUT CRACK AT SEAT TRACK BS 727B, RBL 46. PERFORMED HFEC INSPECTION TO VERIFY NO CRAC KS EXIST. FABRICATED 2 EACH STRAPS, A FILLER, AND A SHIM; INSTALLED REPAIR PARTS IAW AWA ER 03-5702-02191-SS2. 2 L 7 2 4F RT A16WE 2002072200113 20020722 00113 NM 2002 7 22 AWXA200200601 1 20020624 A 5320 69374114 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 DURING C-18 CHECK A CRACK WAS FOUND ON THE UPPER FORWARD FASTENER HOLE OF STRINGER TIE CLIP AT BS 277, STR 19 RT. MAINTE NANCE REMOVED AND REPLACED THE STRINGER TIE CLIP AT BS 277, STR 19 RT IAW B737-300 SRM 51-40-02, PG.10. 2 L 7 2 4F RT A16WE 2002072200114 20020722 00114 NM 2002 7 22 AWXA200200602 1 20020625 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 DURING C-18 CHECK A 3/4 INCH CRACK WAS FOUND ON THE UPPER T-CHORD AT BS 727B, RBL 25. MAINTENANCE TRIMED OUT CRACKED ARE A OF UPPER T-CHORD AT BS 727B, RBL 25. PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED 2 EACH STRAPS, A FILLER, AND A SHIM; INSTALLED REPAIR PARTS IAW AWA ER 03-5702-02191-SS1. 2 L 7 2 4F RT A16WE 2002072200115 20020722 00115 NM 2002 7 22 AWXA200200603 1 20020625 A 5315 FLOORBEAM BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 DURING C-11 CHECK EXFOILIATION CORROSION WAS FOUND ON THE LOWER SIDE OF FLOORBEAM UPPER CHORD BETWEEN THE BEAM AND NUTPL ATE BRACKET, BS 1680, RBL 15 - 20. REMOVED DAMAGED SECTION OF FLOORBEAM UPPER CHORD, FABRICATED 2 EACH REPAIR ANGLES AND 2 EACH STRAPS, AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, FIG. 201, PG. 206-208. 2 L 7 2 4F RT A2NM 2002072200116 20020722 00116 NM 2002 7 22 AWXA200200604 1 20020701 A 5320 146N5318 PAN BOEING 757 7572G7 1384963 NM CABIN FLOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 DURING C-11 CHECK CORROSION WAS FOUND ON CABIN FLOOR PAN AT BS 1681-1720, RBL 12. MAINTENANCE BLENDED OUT CORROSION, TRE ATED AREA, FABRICATED A REPAIR DOUBLER, AND INSTALLED REPAIR IAW B757-200 SRM 53-60-51, PG. 204. 2 L 7 2 4F RT A2NM 2002072200117 20020722 00117 NM 2002 7 22 AWXA200200605 1 20020630 A 5315 FLOORBEAM BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 DURING C-11 CHECK CORROSION WAS FOUND ON FLOORBEAM NUTPLATE HOLE AT BS 1340 RT, JUST INBOARD OF THE R-3 DOOR. MAINTENANC E REMOVED INBOARD CHORD RT FROM BS 1300 TO BS 1400, FABRICATED NEW REPAIR CHORD, AND INSTALLED REPAIR IAW B757-200 SRM 5 3-60-13. 2 L 7 2 4F RT A2NM 2002072200118 20020722 00118 NM 2002 7 22 AWXA200200606 1 20020626 A 5320 146N5318 PAN BOEING 757 7572G7 1384963 NM CABIN FLOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 DURING C-11 CHECK CORROSION WAS FOUND ON CABIN FLOOR PAN AT BS 1718, RBL 14 TO RBL 40. MAINTENANCE REMOVED CORROSION, MA TERIAL LOSS OUT OF LIMITS AT BS 1718, RBL 23. TREATED AND PRIMED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B757- 200 SRM 53-60-51, PG. 204-208. 2 L 7 2 4F RT A2NM 2002072200119 20020722 00119 NM 2002 7 22 2002UALA00992 1 20020612 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 AFT CABIN RIGHT HAND SIDE FRAME AT STATION 807 IS CRACKED WHERE AIR GRILL ATTACHES. MAJOR REPAIR ACCOMPLISHED. INSTALL ED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072200120 20020722 00120 NM 2002 7 22 AWXA200200608 1 20020625 A 5347 CARGO TRACK BOEING 757 7572G7 1384963 NM CARGO BAY CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 DURING C-11 CHECK CORROSION WAS FOUND ON THE FORWARD CARGO COMPARTMENT RT LOADING JACK SCREW TRACK BS 691 TO BS 696, RBL 4. MAINTENANCE REMOVED DAMAGED SECTION OF FLOOR TRACK, FABRICATED A NEW SECTION OF TRACK AND 2 EACH REPAIR DOUBLERS; IN STALLED REPAIR PARTS IAW B757-200 SRM 51-70-12, PG. 1. 2 L 7 2 4F RT A2NM 2002072200121 20020722 00121 NM 2002 7 22 AWXA200200609 1 20020626 A 5320 BAC1509100506 ATTACH ANGLE BOEING 757 7572G7 1384963 NM GALLEY SUPPORT CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 DURING C-11 CHECK CORROSION WAS FOUND ON CABIN FLOOR ATTACH ANGLES (GALLEY SUPPORT) AT BS 1718, LB 0, RBL 10. MAINTENANC E REMOVED DAMAGED HAT SECTION, FABRICATED NEW HAT SECTION, AND INSTALLED REPAIR PARTS IAW DWG 146N5300, AND B757-200 SRM 51-40-02, PG. 1-6. 2 L 7 2 4F RT A2NM 2002072200122 20020722 00122 NM 2002 7 22 2002UALA00993 1 20020612 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 AFT CABIN LEFT HAND SIDE FRAME AT STATION 867 IS CRACKED WHERE AIR GRILL ATTACHES. MAJOR REPAIR ACCOMPLISHED. INSTALLE D DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072200123 20020722 00123 NM 2002 7 22 AWXA200200610 1 20020713 A 2760 V3L2228 SWITCH BOEING 737 73733A 1384673 NM SPEEDBRAKES DIRTY A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 164AW 23625 FLT 0631 - WHILE PREPARING TO TAKEOFF FROM LAS EN ROUTE TO OAK TAKEOFF CONFIGURATION WARNING SOUNDED AFTER APPLYING FULL THRUST, TAKEOFF ABORTED. MAINTENANCE CLEANED THE SPEED BRAKE WARNING SWITCH, TAKEOFF WARNING TEST WAS GOOD IAW BMM 31-2 6-00 AND T/C A1B31009. 2 L 7 2 4F RT A16WE 2002072200124 20020722 00124 NM 2002 7 22 2002UALA00994 1 20020612 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 STATION 178 BULKHEAD WEB IS CRACKED AT BL 0 JUST ABOVE LOCALIZER ANTENNA MOUNT (VIEWED FROM AFT SIDE). MAJOR REPAIR ACC OMPLISHED 2 L 7 2 4F 4 F RT A16WE E2GL 2002092000141 20020920 00141 2002 9 20 AWXA200200614 4 20020714 A 3442 3511218060 REGULATOR AIRBUS 320 A320232 3930326 EU TRANSCEIVER SHORTED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 605AW 4953 543 LAS - AIR TURN BACK - FLT 0726 - ON CLIMB OUT OF LAS EN ROUTE TO ORD THE WEATHER RADAR DISPLAYED WX R/T IN RED AND QUIT PAINTING WEATHER. TURNED BACK TO LAS. MAINTENANCE R&R THE WEATHER RADAR TRANSCEIVER IAW AMM 34-41-33-401, AND THE WEAT HER RADAR CONTROL UNIT IAW 34-41-12-401. OPERATIONAL CHECK WAS GOOD, TESTED WEATHER PATTERNS ON RAMP, ALL INDICATIONS N ORMAL. VENDOR BENCH TEST OF WX RADAR RT S/N 4953 CONFIRMED FAILURE OF UNIT FINDING THE 5VDC REGULATOR SHORTED. REPLACE D INTEGRATED CIRCUIT A2A2U6 TO CORRECT 5VDC. 2 L 7 2 4F RT A28NM 2002072200125 20020722 00125 NM 2002 7 22 C1HA200285012 1 20020721 A 7931 UNK OIL FILTER BOEING 727 7272S7 138407Z NM A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 685CA 22492 #1 low oil pressure light illuminated on takeoff roll below 60 ktts. Aborted takeoff. Replaced #1 engine main oil filter per MM. Leak checks good. 2 L 7 3 4F A3WE 2002072200126 20020722 00126 NM 2002 7 22 C1HA200294009 1 20020721 A 3350 6104789 BATTERY PACK BOEING 727 727290 138408W NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 294AS 22146 LH and RHG aft emergency slide lights are inoperative. Removed and replaced battery pack. Operational checks good. 2 L 7 3 4F A3WE 2002081600124 20020816 00124 2002 8 16 AWXA200200615 4 20020714 A 2350 ACP2788AB04 AUDIO PANEL AIRBUS A319 A319132 3930340 NM COCKPIT MALFUNCTIONED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 801AW 13885 889 CRUISE, A LOUD BANG & FLASH OF LIGHT BEHIND F/O SEAT ON ELECTRICAL PANEL, DEBRIS & SMOKE FOLLOWED. NO INDICATIONS OF PR OBLEM ON ECAM, STARTED SMOKE REMOVAL PROCEDURES. DISCONNECTED PWR FROM GALLEY, DID NOT DISCONNECT GENERATOR. SMOKE STO PPED 15 MIN. MX IDENTIFIED NR 3 AUDIO CONTROL PANEL AS HAVING BURNT ELECT SMELL; REPLACED NR 3 ACP. LIGHTING CONTROLLE R 16LF REPLACED DUE TO HISTORY OF C/B POPPING. OPERATED NR 1 & 2 PACKS, ALL FLT DECK & EXTERIOR LIGHTING, ALL 3 HYD SYS , NO FAULTS FOUND. VENDOR BENCH TEST AND TEARDOWN NR 3 ACP COULD NOT CONFIRM REASON FOR REMOVAL. UNIT HAD BURNT SMELL, NO BURN INSIDE, & UNIT OPS NORM. PIA IC MN3 UPPER BOARD REPLACED, AS Z1 & Z2 OPTOCOUPLERS. 2 L 7 2 4F RT A28NM 2002072200127 20020722 00127 NM 2002 7 22 AWXA200200617 1 20020714 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 DURING INSPECTION THE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE AT THE COCKPIT ENTRANCE. MAINTENANCE REMOVED AND REPLAC ED BATTERIES FOR FORWARD EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002072200128 20020722 00128 NM 2002 7 22 AWXA200200618 1 20020714 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 DURING INSPECTION THE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE ABOVE L2 DOOR. MAINTENANCE REMOVED AND REPLACED THE BAT TERIES AT THE EMERGENCY EXIT LIGHT ABOVE THE L2 DOOR, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002072200129 20020722 00129 NM 2002 7 22 AWXA200200619 1 20020715 A 2560 EF1 FLASHLIGHT BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 183AW 22650 FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AFT LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LT EMERGENCY FLASHLIGHT. 2 L 7 2 4F RT A16WE 2002072200130 20020722 00130 NM 2002 7 22 AWXA200200620 1 20020716 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM SEAT ROW 6 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 DURING INSPECTION THE EMERGENCY ESCAPE PATH SEAT LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 6 LT. MAINTENANCE REMOVED AND R EPLACED SEAT LIGHT ASSEMBLY PER BMM 33-51-21, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002072200131 20020722 00131 NM 2002 7 22 AWXA200200622 1 20020707 A 5314 65458789 COVER BOEING 737 7373G7 1384595 NM KEELBEAM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 DURING C-18 CHECK A 3 INCH CRACK WAS FOUND IN THE UPPER AFT END RADIUS OF THE KEELBEAM MOUNTING COVER JUST BELOW THE AFT LT MOUNT OF THE AUXILLARY HYDRAULIC PUMP, BS 710. MAINTENANCE REMOVED DAMAGED AREA OF MOUNTING COVER BS 710, FABRICATED 4 EACH REPAIR ANGLES AND A FILLER, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11, PG. 1-6. 2 L 7 2 4F RT A16WE 2002091000113 20020910 00113 2002 9 10 AWXA200200629 4 20020717 A 2213 4038891916 COMPUTER BOEING 737 737277 1384570 NM AUTOPILOT SYS FAULTY A AWXA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED TO TAKEOFF 1 WP 28 179AW 44799 21 22646 ON TAKEOFF WHEN ENGAGING THE A-AUTOPILOT AIRCRAFT WENT TO CWS PITCH MODE AND NOSE PITCHED UP 5 TO 10 ABOVE NORMAL TAKEOF F ATTITUDE. SWITCHED TO B-CHANNEL AND SYS OPERATED NORMALLY. MX PLACED SYS ON MEL 22-01-11, COND 1 A-AUTOPILOT INOPERA TIVE. TROUBLESHOT SYS & FOUND WHEN ON GROUND AND A-AUTOPILOT IS ENGAGED YOKE MOVES BACK FORCEFULLY. FOUND NR 1 FLT CON TROL COMPUTER FAILING BITE TEST. REMOVED AND REPLACED NR 1 FCC PER BMM 22-11-33, FUNCTIONAL TEST WAS GOOD. VENDOR BENC H TEST CONFIRMED FAILURE OF NR 1 FLT CONTROL COMPUTER FOR EXCEEDING VOLTAGE TOLERANCES DURING TESTS 3106 & 2111. REPLAC ED K1 RELAY & U8 MICROCIRCUIT. UNIT FUNCTIONAL TESTED GOOD. 2 L 7 2 4F RT A16WE 2002072200132 20020722 00132 NM 2002 7 22 AWXA200200630 1 20020717 A 2611 PU90499R4 SMOKE DETECTOR BOEING 757 7572S7 1384962 NM LAVATORY FAILED A AWXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 902AW 23322 FLT 0051 - RETURNED TO GATE DUE TO STRONG ELECTRICAL ODOR COMING FROM THE FORWARD LAVATORY. MAINTENANCE IDENTIFIED BURNI NG ODOR WAS COMING FROM FORWARD LAVATORY SMOKE DETECTOR. REMOVED AND REPLACED SMOKE DETECTOR, OPERATIONAL CHECK GOOD PER BMM 26-14-00. 2 L 7 2 4F RT A2NM 2002072200133 20020722 00133 NM 2002 7 22 AWXA200200637 1 20020626 A 5310 6546561509 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 DURING C-18 CHECK HFEC INSPECTION IDENTIFIED A 1 1/8 INCH CRACK RUNNING FROM LOWER FASTENER HOLE ON FRAME AT THE PAN COM MON TO THE NR 3 STOP OF THE R2 DOOR BS 956, STR 10 RT. MAINTENANCE TRIMMED OUT CRACK IN FRAME AT BS 956. PERFORMED A HFE C INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER, STRAP, AND A FRAME SPLICE STRAP, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5300-02198-SS3. 2 L 7 2 4F RT A16WE 2002072200134 20020722 00134 SO 2002 7 22 C2XA02CL153 1 20020719 A 3260 852701 SWITCH EMB 145 EMB145ER 3260211 SO GEAR OUT OF ADJUST A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 14925 145004 CLE FLIGHT#3597 THE CREW REPORTED THE GEAR WOULD NOT RETRACT AND THEY RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE.MA INTENANCE INSPECTED AND ADJUSTED THE RIGHT MAIN LANDING GEAR REAR WOW PROXIMITY SWITCH.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002072200135 20020722 00135 WP 2002 7 22 AALA20020478 1 20020410 A 5510 HINGE DOUG DC9 DC983 3022083 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND CORROSION IN LEFT STAB HINGE BORE OUTBOARD SIDE BETWEEN LUG AND BUSHING. REMOVED CORROSION PER ESO 80559 DA TED 4-11-02 AND INSTALLED OVERSIZE BUSHING. (M) 2 L 7 2 4F RT A6WE 2002072200136 20020722 00136 WP 2002 7 22 AALA20020479 1 20020401 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND CABIN FLOORBOARD SUPPORT CORRODED AT STATION 200 RBL 62. REMOVED CORRODED SUPPORT ANGLE, INSTALLED NEW SUPP ORT 51-01. (M) 2 L 7 2 4F RT A6WE 2002072200137 20020722 00137 WP 2002 7 22 AALA20020480 1 20020404 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND STATION 1300 LEFT CUSP CRACKED. INSTALLED DOUBLER PER SRM 53-01-00. (M) 2 L 7 2 4F RT A6WE 2002072200138 20020722 00138 WP 2002 7 22 AALA20020481 1 20020408 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND LEFT AFT CABIN FLOOR CUSP CRACKED BETWEEN LIGHTENING HOLES, INBOARD OF PREVENTIVE DOUBLER, STATION 1300. RO UTED-OUT DAMAGED SECTION OF CUSP. INSTALLED INTERIM REPAIR FILLER AND DOUBLER PER ESO 80559. (M) 2 L 7 2 4F RT A6WE 2002072200139 20020722 00139 WP 2002 7 22 AALA20020482 1 20020328 A 5310 WINDOW FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND WINDOW FRAME CRACKED STATION 1021 LONGERON 12L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-25 P AGE 2 FIG 1. (M) 2 L 7 2 4F RT A6WE 2002072200140 20020722 00140 WP 2002 7 22 AALA20020483 1 20020328 A 5310 WINDOW FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND WINDOW FRAME CRACKED STATION 947 LONGERON 12L. STOP DRILLED, CRACK AND INSTALLED DOUBLER PER 53-10-00-25 PA GE 2 FIG 1. (M) 2 L 7 2 4F RT A6WE 2002072200141 20020722 00141 WP 2002 7 22 AALA20020484 1 20020405 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND CORROSION IN J-ANGLE OF FRAME STATION 1271, AFT SIDE AT LONGERON 20. REMOVED CORROSION. TREATED AND PRIMED AREA. INSTALLED J-ANGLE REPAIR DOUBLER PER AARD 53-10-00-14, REPAIR 1. (M) 2 L 7 2 4F RT A6WE 2002072200142 20020722 00142 WP 2002 7 22 AALA20020485 1 20020405 A 5310 WINDOW FRAME DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND OVERSIZED HOLE LOCATED ON TOP LEFT CORNER OF CAPTAINS AFT WINDOW FRAME. OVERSIZED DAMAGED HOLE AND INSTALLE D DOUBLER PER ENGINEERING ESO. (M) 2 L 7 2 4F RT A6WE 2002072200143 20020722 00143 WP 2002 7 22 AALA20020486 1 20020327 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND LEFT WINDOW FRAME ANGLE CRACKED. STOP DRILLED END OF CRACK, CONFIRMATION WITH DYE CHECK. INSTALLED ANGLE D OUBLER PER AARD 53-10-00-25. (M) 2 L 7 2 4F RT A6WE 2002072200144 20020722 00144 WP 2002 7 22 AALA20020487 1 20020401 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND CORROSION ON SEAT TRACK NR 2 STATION 1305-1307. INSTALLED SEAT TRACK PLUG PER SRM 53-05-00 FIG 4A. (M) 2 L 7 2 4F RT A6WE 2002072200145 20020722 00145 WP 2002 7 22 AALA20020488 1 20020403 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND CORROSION STATION 1203 NR 1 TRACK. INSTALLED NEW TRACK STATION 1174 TO 1307 51-01. 2 L 7 2 4F RT A6WE 2002072200146 20020722 00146 WP 2002 7 22 AALA20020489 1 20020408 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND FUSELAGE SKIN WORN AT LONGERON 7R PLUS 4 INCHES. INSTALLED DOUBLER AT STATION 599 L7R PLUS 4 INCHES PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F RT A6WE 2002072200147 20020722 00147 WP 2002 7 22 AALA20020521 1 20020403 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7530 49922 TUL - FOUND CORROSION AT LOWER CARGO DOOR FRAME LOWER BEAM. PUT DOUBLERS IN TWO PLACES FS 655, FS 674 MM AARD 53-10-00- 3. (M) 2 L 7 2 4F A6WE 2002072200148 20020722 00148 WP 2002 7 22 AALA20020522 1 20020408 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7530 1753 TUL - FOUND CORROSION NR 3 SEAT TRACK FS 1589. INSTALLED SPLICE REPAIR IAW SRM 53-05. (M) 2 L 7 2 4F A6WE 2002072200149 20020722 00149 WP 2002 7 22 AALA20020523 1 20020409 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7530 49922 TUL - FOUND SEVERAL AREAS OF CORROSION ALONG DOOR PAN WAS BLENDED OUT BUT EXCEEDS SRM LIMITS. SPLICED IN NEW DOOR PAN A SSEMBLY IAW SRM 53-05 PAGE 103-116 FIG 44. (M) 2 L 7 2 4F A6WE 2002072200150 20020722 00150 WP 2002 7 22 AALA20020524 1 20020410 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7530 49922 TUL - FOUND FUSELAGE DENT IN FUSELAGE SKIN, FS 243. CUT OUT DAMAGE, INSTALLED DOUBLER WITH FILLER PER SRM 53-04 FIG 38 VIEW H. (M) 2 L 7 2 4F A6WE 2002072200151 20020722 00151 WP 2002 7 22 AALA20020646 1 20020513 A 2130 39271012 VALVE DOUG DC9 DC982 3022082 WP A/C BAY MALFUNCTIONED A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 492AA 49730 IND - FLT 1946 - EN ROUTE MCO-ORD - WHILE IN CRUISE AT 31,000 FEET FLIGHT ATTENDANTS REPORTED CABIN FILLING WITH SMOKE A ND A STRONG ACRID SMELL. SELECTED AIR SUPPLY TO HP BLEED OFF AND SMOKE DISSIPATED. FOLLOWED EMERGENCY PROCEDURE LANDED IND WITHOUT INCIDENT. REPLACED LEFT AND RIGHT AIRCRAFT PRESSURE REGULATING VALVES AND ACCOMPLISHED PACK BURNOUT. NO O DORS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002072200152 20020722 00152 WP 2002 7 22 GTIA020532 1 20020515 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FLOORBOARD AT STATION 160-200 PLUS X6 TO -X6. FABRICATED NEW PASSENGER CABIN FLOOR PANEL STATION 160-200. (M) 2 L 7 2 4F A6WE 2002072200153 20020722 00153 WP 2002 7 22 GTIA020533 1 20020529 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FLOORBOARD STATION 200-236 LEFT HAS CORROSION ON INSERTS. FABRICATED NEW FLOOR PANEL STATION 200-236. (M) 2 L 7 2 4F A6WE 2002072200154 20020722 00154 WP 2002 7 22 GTIA020534 1 20020517 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FLOORBOARD STATION 200-250 FORWARD LAV CHANNELS DEBONDED. REPAIRED FLOORBOARD OF FORWARD LAVATORY AT STATIO N 200-250. (M) 2 L 7 2 4F A6WE 2002072200155 20020722 00155 SO 2002 7 22 C2XA02BT034 1 20020720 A 3350 78812 LIGHT EMB 145 EMB145LR 3260212 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 15555 145594 BTV---CO3048, DURING 2A INSPECTION, MAINTENANCE FOUND EMERGENCY FLOOR LIGHT STRIP AT EMERGENCY EXIT ROW INOPERATIVE..... REMOVED AND REPLACED EMERGENCY ROW FLOOR PROXIMITY LIGHT IAW EMB145 AMM 33-50-12. OPS.CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2002072200156 20020722 00156 WP 2002 7 22 GTIA020535 1 20020516 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FLOORBOARD STATION 180-200 INSERTS MISSING AND HAS CORROSION. FABRICATED FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002072200157 20020722 00157 WP 2002 7 22 GTIA020536 1 20020516 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FS 150-160 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FLOORBOARD STATION 150-160 HAS CORROSION ON INSERTS. FABRICATED NEW PANEL. (M) 2 L 7 2 4F A6WE 2002072200158 20020722 00158 WP 2002 7 22 GTIA020537 1 20020516 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND COCKPIT FLOORBOARD STATION 150-160 LEFT HAS CORROSION ON INSERT, EDGES BROKEN OUT AND TORN. FABRICATED NEW PANEL. (M) 2 L 7 2 4F A6WE 2002072200159 20020722 00159 SO 2002 7 22 C2XA02BT035 1 20020721 A 3350 1317 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14972 145151 MAINTENANCE FOUND EMERGENCY LIGHT ON MAIN CABIN DOOR INOPERATIVE DURING SERVICE ROUTINE CHECK. REMOVED AND REPLACED EME RGENCY LIGHT BULB IN MAIN CABIN DOOR IAW EMB145 AMM 33-50-00. OPS. CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2002072200160 20020722 00160 WP 2002 7 22 GTIA020538 1 20020517 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FLOORBOARD STATION 1174 TO 1117 IS MUSHEY/SOFT. FABRICATED FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2002072200161 20020722 00161 WP 2002 7 22 GTIA020539 1 20020517 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FLOORBOARD STATION 1003 TO 1079 HAS DELAMINATED DAMAGE AT CORNER. FABRICATED NEW PAX CABIN FLOORBOARD STATI ON 1003-1079. (M) 2 L 7 2 4F A6WE 2002072200162 20020722 00162 WP 2002 7 22 GTIA020540 1 20020517 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FLOORBOARD STATION 1174 TO STATION 1250 HAS MUSHY SOFT. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002072200163 20020722 00163 EU 2002 7 22 QXEA0200960 1 20020720 A 3350 5515900004 CIRCUIT CARD FOKKER F28 F28MK4000 4990810 EU ZONE 200 INOPERATIVE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 491US 11156 SEA-EMERGENCY EXIT SIGN HAS BULBS INOPERATIVE, CENTER OVERHEAD. REPLACED EMERGENCY EXIT SIGN CIRCUIT CARD. OPERATIONAL C HECK GOOD. AIRCRAFT RETURNED TO SERVICES. 2 L 7 2 4F RT A20EU 2002072200164 20020722 00164 EU 2002 7 22 QXEA0200951 1 20020710 A 2420 914F5824 CONTROL UNIT FOKKER F28 F28MK4000 4990810 EU ZONE 200 BURNED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 497US 9746 11173 BOI-SMOKE IN COCKPIT-ELECTRICAL SMELL. FOUND STRONG BURNT SMELL FROM GENERATOR POWER CONTROL UNIT. NO OTHER DEFECTS NOTE D. GROUND RAN ENGINES AND PERFORMED AC GENERATOR SYSTEM WITH NO DEFECTS NOTED. REPLACED EXTERNAL POWER CONTROL UNIT AND EXTERNAL POWER CONTACTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002072200165 20020722 00165 SO 2002 7 22 C2XA02BT033 1 20020720 A 3350 3025103 LIGHT EMB 145 EMB145ER 3260211 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14933 145018 EWR---CO4085, CREW REPORTED, "BOTH EMERGENCY LIGHTS OVER WING INOPERATIVE....MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT UNITS FOR BOTH EMERGENCY LIGHTS OVER THE WINGS IAW EMB145 AMM #33-50-04. OPS.CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2002072200167 20020722 00167 GL 2002 7 22 HEEA080400 2 20020708 A 7230 STUD 23033193 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL COMPRESSOR BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8592X 291 CAC91106 51508 CAE895560 REMOVED DUE TO COMPRESSOR SCROLL STUD BROKEN. UPON INSPECTION OF COMPRESSOR PARTS NOTED WORN TANGS AND SLOTS, CHIPS A ND PITS ON CARBON FACE. 1 G 7 1 3U 3 U H2SW E1GL 2002072200168 20020722 00168 GL 2002 7 22 HEEA080401 2 20020708 A 7260 23063371 SEAL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL GEARBOX TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81992 S827 CAE836413 ENGINE REMOVED DUE TO MAKING METAL ON TEST CELL. FOUND NEW SEAL LIP TORN AND LEAKING. 1 G 7 2 3U 3 U H3EU E4CE 2002072200169 20020722 00169 GL 2002 7 22 HEEA080403 2 20020708 A 7260 23063371 SEAL 23035179 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL GEARBOX SPLIT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911UK CAG90528 760275 CAE890525S GEARBOX SEAL SPLIT (LEAKED ON TEST CELL RUN). 1 G 7 2 3U 3 U H1NE E1GL 2002072200170 20020722 00170 GL 2002 7 22 HEEA080404 2 20020708 A 7250 23068265 TIE BOLT BELL 206 TH57A 1180821 SW ALLSN 250C 250C18A 03011 GL ENGINE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 080 465 162044 ENGINE REMOVED DUE TO EXCEEDING TOT ON START. UPON INSPECTION OF TURBINE PARTS NOTED EXCESSIVE PITTING ON TIE BOLT MUTE . 1 G 7 1 3U 3 U EXPA1G71 E4CE 2002072200171 20020722 00171 2002 7 22 HEEA080405 4 20020709 A 3421 102005901 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT ERRATIC E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22342 760096 ATTITUDE INDICATOR ERRATIC. TO BE SENT TO VENDOR FOR REPAIR. 1 G 7 2 3U H1NE 2002072200172 20020722 00172 NE 2002 7 22 HEEA080406 1 20020709 A 6230 7610408020047 SCISSORS SKRSKY S76 S76A 8143006 NE MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 MAIN ROTOR ROTATING SCISSORS WORN. REPAIRED. 1 G 7 2 3U H1NE 2002072200173 20020722 00173 NE 2002 7 22 HEEA080407 1 20020709 A 7714 7645001076101 TACH GENERATOR SKRSKY S76 S76A 8143006 NE ENGINE MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 911UK 760275 WITH STARTER ENGAGED N1 READS BETWEEN 1 AND 6 PERCENT INTERMITTENTLY. REPAIRED. 1 G 7 2 3U H1NE 2002072200174 20020722 00174 NE 2002 7 22 HEEA080408 1 20020709 A 2420 7655009005104 GCU SKRSKY S76 S76A 8143006 NE ELECTRICAL WILL NOT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22342 760096 GCU WILL NOT TEST. 1 G 7 2 3U H1NE 2002072200175 20020722 00175 2002 7 22 HEEA080409 4 20020709 A 2215 7690001802106 ACTUATOR SKRSKY S76 S76A 8143006 NE AFCS INOPERATIVE E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 22342 760096 AFCS ACTUATOR INOPERATIVE. TO BE SENT TO VENDOR FOR REPAIR. 1 G 7 2 3U H1NE 2002072200176 20020722 00176 2002 7 22 HEEA080410 4 20020709 A 2200 7690001810112 DAMPER SKRSKY S76 S76C 8143008 NE PEDAL LEAKING E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 505PH 760505 PEDAL DAMPER LEAKING. TO BE SENT TO VENDOR FOR REPAIR. 1 G 7 2 3U NC H1NE 2002072200177 20020722 00177 2002 7 22 HEEA080411 4 20020709 A 2215 L109CBM ACTUATOR SKRSKY S76 S76C 8143008 NE COLLECTIVE FAILED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 505PH 760505 OUT OF DETENT ON AUTOPILOT. SHEARED CLEVIS. COLLECTIVE ACTUATOR FAILED IN FLIGHT. TO BE SENT TO VENDOR FOR REPAIR. 1 G 7 2 3U NC H1NE 2002072200178 20020722 00178 2002 7 22 HEEA080412 4 20020709 A 2312 064100900 TRANSCEIVER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1546K 760082 WON'T RECEIVE ON FREQUENCY 119.27. FOUND UNIT WOULD NOT RECEIVED ON ANY FREQUENCY. REMOVED CORROSION FROM MODULATOR BOA RD. REPLACED R433 POTENTIOMETER DUE TO BAD. REPLACED I303 IC CHIP DUE TO BAD VOLTAGES. REPLACED R321 RESISTOR DUE TO BAD. UNIT STARTED RECEIVING. FOUND MODULATION DISTORTED. REALIGNED TRANSMITTER. SWAPPED C513 AND C514 CAPACITORS. R EPLACED C525 AND C527 CAPACITORS. REPAIRED. REMOVED CORROSION FROM BOTTOM OF SYNTHESIZER BOARD IN VCO SECTION. UNIT B ENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002072200179 20020722 00179 2002 7 22 HEEA080413 4 20020709 A 2312 064100900 TRANSCEIVER SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5435V 760158 LOW POWER OUTPUT AND OVERMODULATES WHEN TRANSMITTING. VERIFIED COMPLAINT. REPAIRED. FOUND RECEIVER WEAK AND C/N SQUELC H SETTING WOULD DRIFT AS UNIT HEATED UP. REALIGNED RECEIVER. REPLACED Q304 TRANSISTOR. NO HELP. REPLACED Q301 TRANSI STOR. REALIGNED RECEIVER. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002072200180 20020722 00180 NM 2002 7 22 CALA0200419 1 20020719 A 5320 STIFFENER BOEING 737 7373T0 1384582 NM STA 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND APB FORWARD FACE LOWEST POINT CENTER STIFFENER CORRODED AT R/H AND L/H SIDE STA 1016, BL 0. STIFFENER R EPAIRS WERE INSTALLED IAW SRM 51-70-11. INSPECTED CAPSULATED FASTENERS AND APPLIED LEVELING COMPOUND. 2 L 7 2 4F RT A16WE 2002072200181 20020722 00181 WP 2002 7 22 CALA0200421 1 20020719 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 200-228 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 200-228. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 53-05, FIGURE 4 F, SHEET 1. 2 L 7 2 4F A6WE 2002072200182 20020722 00182 WP 2002 7 22 CALA0200422 1 20020720 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FS 1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND LONGERON 20L CORRODED AT FS 1174. REPAIRED IAW ECRA 5310-04264. 2 L 7 2 4F A6WE 2002072200183 20020722 00183 WP 2002 7 22 CALA0200423 1 20020720 A 5320 FITTING DOUG DC9 DC982 3022082 WP FS 1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND FLOORBEAM TO FRAME END FITTING CORRODED AT FS 1174. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30- 5. 2 L 7 2 4F A6WE 2002072200184 20020722 00184 WP 2002 7 22 CALA0200424 1 20020720 A 5320 WEB DOUG DC9 DC982 3022082 WP FS 1155-1212 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND CUSP WEB CORRODED AT FS 1155-1212, LBL 48-58. REPAIRED IAW ECRA 5310-04269. 2 L 7 2 4F A6WE 2002072200185 20020722 00185 WP 2002 7 22 ABXA020060 1 20020520 A 5300 4614067 FITTING DOUG DC8 DC863 302198A WP F.S. 70 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 FORWARD CARGO AT STA. 70, STRING 25 LEFT, LONGERON END FITTING WAS CORRODED. REPLACED FITTING IAW DC-8 SRM 51-1-21, 51-1 -20D AND 51-3-0. 2 L 7 4 4F 4A25 2002072200186 20020722 00186 WP 2002 7 22 ABXA020061 1 20020520 A 5340 SHEAR TIE DOUG DC8 DC863 302198A WP STA. 1520 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 AFT CARGO AT STATION 1520, BETWEEN LONGERON 35 LEFT AND LONGERON 36, SHEAR TIE WAS CORRODED. REPAIRED AREA, FABRICATED A ND INSTALLED NEW CLIP IAW DC-8 SRM 51-1-21, 53-2-0, 51-9-0, 53-4-1, 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 2002072200187 20020722 00187 WP 2002 7 22 ABXA020062 1 20020520 A 5340 SHEAR TIE DOUG DC8 DC863 302198A WP STA. 1520 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 AFT CARGO AT STATION 1520, BETWEEN LONGERON 35 RIGHT AND LONGERON 36, SHEAR TIE WAS CORRODED. REPAIRED AREA, FABRICATED AND INSTALLED NEW CLIP IAW DC-8 SRM 51-1-21, 53-2-0, 51-9-0, 53-4-1, 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 2002072200188 20020722 00188 WP 2002 7 22 ABXA020063 1 20020520 A 5310 37384511 STRAP DOUG DC8 DC863 302198A WP F.S. 485 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 FORWARD CARGO STATION 485, LONGERON 34 RIGHT, DOUBLER ON BACKSIDE OF LONGERON WAS CORRODED. REPLACED STRAP IAW DC-8 SRM 51-1-24 AND 51-1-20D. 2 L 7 4 4F 4A25 2002072200189 20020722 00189 WP 2002 7 22 ABXA020064 1 20020517 A 5730 SKIN DOUG DC8 DC863 302198A WP XFS 515 - 526 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 RIGHT WING, INBOARD OF THE #4 PYLON, STATION XFS 515.00 - 526.76, HAD CRACK INDICATION AT HOLES 2 AND 4 GOING OUTBOARD. REPAIRED AREA AND INSTALLED NEW FILLER AND DOUBLER IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-21, 51-3-0, 51-1-20D AND REA D857-4 3890-MR. 2 L 7 4 4F 4A25 2002072200190 20020722 00190 WP 2002 7 22 ABXA020066 1 20020519 A 5330 ATTACH ANGLE DOUG DC8 DC863 302198A WP F.S. 986 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 AFT LOWER CARGO STATION 986, FLOOR ATTACH ANGLE, BETWEEN LONGERON 33 RIGHT AND LONGERON 34 RIGHT, WAS CORRODED. REPAIRED AREA AND INSTALLED NEW FLOOR ATTACH ANGLE IAW DC-8 SRM 51-1-21, 51-1-20D AND REA D853-43896-MR. 2 L 7 4 4F 4A25 2002072200191 20020722 00191 WP 2002 7 22 ABXA020067 1 20020520 A 5310 LONGERON DOUG DC8 DC863 302198A WP F.S. 520 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 FORWARD CARGO STATION 520, LONGERON 35 RIGHT, INBOARD FLANGE WAS CRACKED. REPAIRED AREA IAW REA D853-43899-MR. 2 L 7 4 4F 4A25 2002072200192 20020722 00192 NM 2002 7 22 AWXA200200641 1 20020710 A 5311 6555874503 STOP FITTING BOEING 737 7373G7 1384595 NM WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 0 0 24012 YVR - MAJOR REPAIR - DURING C-14 CHECK THE AFT ENTRY DOOR FORWARD FRAME, 3RD STOP FITTING FROM THE TOP WAS FOUND TO HAVE INSUFFICIANT EDGE MARGIN AT THE DOOR ASSIST HANDLE ATTACH BS 954. MAINTENANCE REMOVED DOOR STOP FITTING BS 954, FABRICA TED A FRAME FILLER, A STRAP, AND 2 EACH SPLICE STRAPS, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5311-02200-ES3 2 L 7 2 4F RT A16WE 2002072200193 20020722 00193 WP 2002 7 22 GTIA020547 1 20020514 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND PAX CABIN SEAT TRACK AT FS 705, -X44 HAS CORROSION. REMOVED CORROSION AREA OUT OF LIMITS. FABRICATED REPAI R TRACK. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2002072200194 20020722 00194 WP 2002 7 22 GTIA020549 1 20020515 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FLOOR BROKEN AND DELAMINATED, PLUS X8 UP TO PLUS X45 BETWEEN STATION 160 AND STATION 200. FORMED NEW PANEL. (M) 2 L 7 2 4F A6WE 2002072300001 20020723 00001 2002 7 23 HEEA080414 4 20020709 A 2312 064102300 TRANSCEIVER SKRSKY S76 S76A 8143006 NE VHF SYSTEM MALFUNCTIONED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 911UK 760275 WILL NOT RECEIVE ON FREQUENCY 126.30 MHZ. PERFORMED PRELIMINARY INSPECTION AND FOUND UNIT WOULD NOT RECEIVE ON ANY FREQU ENCY INTERMITTENTLY. FOUND COLD SOLDER ON EMITTERS OF Q320 AND Q321 TRANSISTORS. RESOLDERED TRANSISTOR LEADS. REPAIRE D. ADJUSTED C/N SQUELCH AND REALIGNED TRANSMITTER. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002072300002 20020723 00002 2002 7 23 HEEA080415 4 20020709 A 2312 064102300 TRANSCEIVER SKRSKY S76 S76A 8143006 NE VHF SYSTEM INOPERATIVE E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1545K 760047 WEAK RECEIVE AND TRANSMIT. FOUND RECEIVER GOOD BUT FOUND TRANSMIT POWER AND MODULATION DROPPING OFF AND INTERMITTENT. F OUND RF CONNECTOR NOT SOLDERED PROPERLY. RESOLDERED RF CONNECTOR. MODULATION STILL DROPS OFF. SWAPPED Q109 AND Q110 T RANSISTORS. NO HELP. SENT TO GREATLAKES AVIONICS FOR INSPECTION AND REPAIR. 1 G 7 2 3U H1NE 2002072300003 20020723 00003 2002 7 23 HEEA080416 4 20020709 A 3452 066104100 TRANSPONDER SKRSKY S76 S76A 8143006 NE ATC SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 760158 ATC TRANSPONDER TRANSMITS OFF FREQUENCY AND OUT OF LIMITS. 1 G 7 2 3U H1NE 2002072300004 20020723 00004 2002 7 23 HEEA080417 4 20020709 A 3452 066104100 TRANSPONDER SKRSKY S76 S76A 8143006 NE ATC SYSTEM INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 760158 ATC REPORTS INTERMITTENT OPERATION AND UNRELIABLE ALTITUDE READOUT. REPLACED CATHODE ASSY AND PERFORMED VIDEO BOARD ALIG NMENT. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002072300005 20020723 00005 2002 7 23 HEEA080418 4 20020709 A 3452 066104100 TRANSPONDER SKRSKY S76 S76A 8143006 NE ATC SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 760158 INTERROGATES ON THE EDGE IN MODE "A" AND OUT OF RANGE IN "C" MODE. FOUND FREQUENCY AND POWER AND VIDEO ALIGNMENT OUT OF SPECS. ALIGNED AND ADJUSTED ANODE AND CATHODE ASSY AND V101 CAVITY OSCILLATOR TO SPECS. ALIGNED VIDEO BOARD AND BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002072300006 20020723 00006 2002 7 23 HEEA080419 4 20020709 A 3434 066104400 RECEIVER SKRSKY S76 S76A 8143006 NE MARKER BEACON WILL NOT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 760158 MARKER BEACON SYSTEM WILL NOT TEST. REPAIRED. 1 G 7 2 3U H1NE 2002072300007 20020723 00007 2002 7 23 HEEA080420 4 20020709 A 3455 066104701 TRANSCEIVER SKRSKY S76 S76A 8143006 NE ADF SYSTEM INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 ADF TRANSCEIVER HAS NO LOW BAND RECEPTION OR NEEDLE MOVEMENT. REPAIRED. 1 G 7 2 3U H1NE 2002072300008 20020723 00008 2002 7 23 HEEA080421 4 20020709 A 3444 066304400 INDICATOR SKRSKY S76 S76A 8143006 NE RADAR ALTIMETER WILL NOT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 31219 760230 RADAR ALTIMETER STICKING AND DOESN'T TEST. 1 G 7 2 3U H1NE 2002072300009 20020723 00009 2002 7 23 HEEA080422 4 20020709 A 3454 066400700 RECEIVER SKRSKY S76 S76A 8143006 NE VORLOC SYSTEM INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 760158 VOR WILL NOT POINT TO STATION AND CDI INOPERATIVE. REPLACED I501, C503, C502, R601, Q601. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002072300010 20020723 00010 2002 7 23 HEEA080423 4 20020709 A 3416 212070238003 INDICATOR SKRSKY S76 S76A 8143006 NE ALTIMETER INACCURATE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 ALTIMETER INDICATES 200 FEET OFF IN FLIGHT. 1 G 7 2 3U H1NE 2002072300011 20020723 00011 NE 2002 7 23 HEEA080424 1 20020709 A 2821 23003143 FUEL FILTER SKRSKY S76 S76A 8143006 NE FUEL SYSTEM UNSERVICEABLE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 760158 FUEL FILTER CAUSING ENGINE T5, TQ, N1, N2, FUEL FLOW OSCILLATING AT HIGH POWER SETTINGS. REPLACED WITH SERVICEABLE FILTE R. 1 G 7 2 3U H1NE 2002072300012 20020723 00012 GL 2002 7 23 HEEA080425 2 20020709 A 7510 23007827 VALVE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ANTI ICE SYSTEM INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 760167 ANTI ICE VALVE INOPERATIVE, CAUSING BOTH GREEN AND YELLOW CAUTION LIGHTS TO ILLUMINATE ON MASTER CAUTION PANEL. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U 3 U H1NE E1GL 2002072300013 20020723 00013 NE 2002 7 23 HEEA080426 1 20020709 A 7714 23007981 PICKUP SKRSKY S76 S76A 8143006 NE TRIPLE TACH INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 TRIPLE TACH PICKUP SENSOR IS INTERMITTENTLY INOPERATIVE. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H1NE 2002072300014 20020723 00014 GL 2002 7 23 HEEA080427 2 20020709 A 7250 23053299 TURBINE WHEEL SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 1150 760076 CAE890823S ENGINE REMOVED DUE TO CRACKED EXHAUST COLLECTOR. UPON INSPECTION OF TURBINE PARTS NOTED SULFIDATION ON ALL 1ST STAGE WH EEL BLADES. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U 3 U H1NE E1GL 2002072300015 20020723 00015 GL 2002 7 23 HEEA080428 2 20020709 A 7250 23053299 TURBINE WHEEL SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122H 620 760233 CAE890460S ENGINE REMOVED DUE TO NOISY TURBINE AND CRACKED EXHAUST COLLECTOR. UPON INSPECTION OF TURBINE PARTS NOTED SULFIDATION O N ALL 1ST STAGE WHEEL BLADES. BLADES TRAILING EDGES WERE BROKEN OFF DUE TO SULFIDATION. SCRAPPED AND REPLACED WITH SERV ICEABLE PART. 1 G 7 2 3U 3 U H1NE E1GL 2002072300016 20020723 00016 NE 2002 7 23 HEEA080429 1 20020709 A 2435 BRUSHES SKRSKY S76 S76A 8143006 NE STARTER GEN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 13717 296 760231 STARTER GEN HAS WORN BRUSHES. REPAIRED AND RETURNED TO SERVICE. 1 G 7 2 3U H1NE 2002072300017 20020723 00017 NE 2002 7 23 HEEA080430 1 20020709 A 2435 23081002 STARTER GEN SKRSKY S76 S76A 8143006 NE NR 2 ENGINE MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 16033 760193 NR 2 STARTER GEN WOULD NOT COME ON LINE ON ENGINE DRY CYCLE. NR 2 STARTER WOULD NOT MOTOR AFTER ENGINE WAS SHUTDOWN. RE PAIRED AND RETURNED TO SERVICE. 1 G 7 2 3U H1NE 2002072300018 20020723 00018 NE 2002 7 23 HEEA080431 1 20020710 A 6730 30006762102 MANIFOLD 765500980511 SKRSKY S76 S76A 8143006 NE MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 0537 LEAKING LEE PLUGS IN DRILLED PASSAGE GOING TO RETURN PORTS ON BOTH SYSTEM 1 & 2. 1 G 7 2 3U H1NE 2002072300019 20020723 00019 NE 2002 7 23 HEEA080432 1 20020710 A 6730 30006762102 MANIFOLD 766500980511 SKRSKY S76 S76A 8143006 NE MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 0608 DURING FINAL TEST, A PIN (LEE) PLUG BLEW OUT OF BACK SIDE OF MANIFOLD ON SYSTEM NR 1 (RT LINKAGE 41004076) NEAR MOUNT B EARING. 1 G 7 2 3U H1NE 2002072300020 20020723 00020 GL 2002 7 23 HEEA080433 2 20020711 A 7230 23031922 SHAFT BELL 206 TH57A 1180821 SW ALLSN 250C 250C18 03011 GL COMPRESSOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 078 826 162042 CAE270134 SHAFT HAS SPALLING AND STEP WEAR ON GEAR TEETH BEYOND NORMAL WEAR. 1 G 7 1 3U 3 U EXPA1G71 E4CE 2002072300021 20020723 00021 SW 2002 7 23 HEEA080436 1 20020708 A 6710 214001347005 ACTUATOR BELL 214 214ST 1182106 SW ROTARY STICKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 ROTARY ACTUATOR STICKING. 2 G 7 2 4U H10SW 2002072300022 20020723 00022 2002 7 23 HEEA080437 4 20020708 A 3400 PHI0506001803 ANTENNA BELL 407 407 1182206 SW NAVIGATION SYS FRACTURED E HEEA O OTHER D F INFLIGHT SEPARATION FLT CONT AFFECTED NR NOT REPORTED 1 SW 03 741PH 53457 ANTENNA BROKE OFF APPROXIMATELY 3/4 INCHES FROM BASE. THE LOOSE END CONTACTED AND DAMAGED TAIL ROTOR BLADE AND ONE MAIN ROTOR BLADE WHILE ROTORS WERE IN MOTION. REPLACED TAIL ROTOR AND MAIN ROTOR BLADE. 1 G 7 1 3U O H2SW 2002072300023 20020723 00023 SW 2002 7 23 HEEA080438 1 20020708 A 6310 MS2456W10SL3S CONNECTOR BELL 412 412 1182202 SW OIL PRESS XMITER DIRTY E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 22347 36005 COMBINING BOX OIL PRESSURE FLUCTUATING. FOUND CONNECTOR PLUG AT OIL PRESSURE TRANSMITTER DIRTY AND THE COMBINING BOX VEN PLUG. CLEANED PLUG AND VENT. 1 G 7 2 4U H4SW 2002072300024 20020723 00024 2002 7 23 HEEA080439 4 20020709 A 3461 065001580102 COMPUTER BELL 230 230 1182149 SW AUTO PILOT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RC 23037 FOUND PROBLEM TO BE IN THE "FORCE TRIM CB ON" LOGIC. PREFLIGHT TEST IS NORMAL HOWEVER AUTOPILOT WILL NOT ENGAGE. ENTER ED DIAGNOSTIC MODE AND INTO THE DISCRETE I/O SCREEN. FOUND BIT NR 13 OF PORT 1 IN THE DISCRETE INPUTS TO BE "1" WITH TH E FORCE TRIM CB IN. CYLCED THE CB REPEATEDLY AND THE INPUT RESPONSE WAS INTERMITTENT. CHECKED FOR PROPER VOLTAGE AND GE NERAL CONDITION OF PIN 56 IN RACK CONNECTOR 9A1P2 AND CHECKED OK. 1 G 7 2 3U NC H9SW 2002072300025 20020723 00025 NE 2002 7 23 HEEA080441 2 20020709 A 7532 5044T08P11 BLEED VALVE BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE NR 1 ENGINE MALFUNCTIONED E HEEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 03 3897N 28106 NR 1 ENGINE HAS LOW POWER DUE TO MALFUNCTIONING BLEED VALVE. TO BE SENT TO VENDOR FOR REPAIR. 2 G 7 2 4U 4 U H10SW E8NE 2002072300026 20020723 00026 SW 2002 7 23 HEEA080442 1 20020709 A 7603 MS0276474 BEARING BELL 212 212 1181420 SW BELLCRANK WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 102PH 30899 WORN BEARING P/N MS027647-4. REPLACED BEARING AND RETURNED TO SERVICE. 1 G 7 1 4U H4SW 2002072300027 20020723 00027 NM 2002 7 23 VNAA0207007 1 20020709 A 2910 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE HYD SYSTEM DIRTY A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 461PS 3075 EN ROUTE FROM PIT TO CVG, THE CREW RECEIVED A MAIN HYDRAULIC PUMP INOP CAS MESSAGE. THE NOSE WHEEL STEERING AND ANTI SK ID WERE TURNED OFF FOR LANDING FOLLOWING THE QUICK REFERENCE HANDBOOK PROCEDURE. FLIGHT 4087 LANDED WITH NO INCIDENTS A ND TAXIED OFF THE RUNWAY. THE CREW HAD THE AIRCRAFT TOWED FROM THE TAXI WAY TO THE GATE. MAINTENANCE WAS DISPATCHED FR OM PIT TO CVG. MAINTENANCE INSPECTED AND CLEANED THE ELECTRICAL CONNECTION ON THE HYDRAULIC PUMP, CLEANED THE HYDRAULIC CANNON PLUG, AND RESET THE PUMP POWER NR 2 CIRCUIT BREAKER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-00-00. MAI NTENANCE PERFORMED SEVERAL OPERATIONAL TESTS AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072300028 20020723 00028 NM 2002 7 23 VNAA0207009 1 20020710 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 472PS 14080 262 3008 THE CREW REPORTED THAT THE FIRST EMERGENCY FLOOR LIGHTING TRACK WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACE D THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED A ND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072300029 20020723 00029 NM 2002 7 23 VNAA0207010 1 20020711 A 5270 BRACKET DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EMERGENCY EXIT OUT OF ADJUST A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 423JS 3032 EN ROUTE, THE CREW RECEIVED A DOORS RED WARNING PANEL LIGHT. ALL DOORS WERE SECURE AND THE AIRCRAFT DID NOT LOSE PRESSU RIZATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO PIT. MAINTENANCE INSPECTED AND ADJUSTED THE 9 A EMERGENCY DOOR PROXIMITY SENSOR BRACKET IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WE RE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072300030 20020723 00030 NM 2002 7 23 VNAA0207011 1 20020711 A 2450 3280021AMENDC PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 462PS 8830 3084 DURING CLIMBOUT, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL MESSAGE AND RETURN TO DAY. MAINTENANCE INSPECTED AND REP LACED THE AC/DC PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS AND A FUNCTIONAL CHECK FLIGHT WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072300031 20020723 00031 NM 2002 7 23 VNAA0207012 1 20020711 A 2810 96020111 PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT WING MALFUNCTIONED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 471PS 13256 3007 FLIGHT 9405 RETURNED TO THE FIELD AFTER THE AIRCRAFT BEHIND THEM REPORTED SOMETHING FELL OFF THE AIRCRAFT. THE CREW ALS O RECEIVED A FEEDER TANK LOW CAS MESSAGE. MAINTENANCE INSPECTED AND FOUND THAT A SMALL BIRD HAD STRUCK THE VERTICAL STA BILIZER. MAINTENANCE THEN INSPECTED AND REPLACED THE RIGHT HAND REFUELING BOX IN ACCORDANCE WITH 28-00-00. OPERATIONAL CHECKS AND A FUNCTIONAL CHECK FLIGHT WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072300032 20020723 00032 NM 2002 7 23 VNAA0207013 1 20020711 A 2430 1030200 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ELECTRICAL SYS FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 462PS 974 13 3084 DURING CLIMBOUT, THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL MESSAGE AND RETURNED TO DAY. MAINTENANCE INSPECTED AND R EPLACED THE RIGHT HAND WING HALL EFFECT SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHEC KS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072300033 20020723 00033 EA 2002 7 23 HEEA080443 2 20020709 A 7320 324473514 FUEL CONTROL BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA ENGINE MALFUNCTIONED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 102PH 36 30899 ENGINE HAD TORQUE AND N1 OSCILLATIONS. REPLACED WITH SERVICEABLE FUEL CONTROL. 1 G 7 1 4U 4 U H4SW E22EA 2002072300034 20020723 00034 NM 2002 7 23 VNAA0207017 1 20020712 A 2752 1048A000002 ACTUATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE T/E FLAP FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 439JS 5963 3057 EN ROUTE FROM DAY TO DCA, THE CREW RECEIVED A FLAP CONTROL FAIL, LEFT HAND PUSHER, SHAKER, AND AILERON TRIM CAS MESSAGES . FLIGHT 4058 THEN DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE FLAP ACTUATOR IN ACCORDANCE WITH DORNIER MA INTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072300035 20020723 00035 NM 2002 7 23 VNAA0207018 1 20020713 A 3231 DOOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG MALFUNCTIONED A VNAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 457PS 3048 AFTER TAKEOFF, THE CREW EXPERIENCED A VIBRATION IN THE NOSE SECTION OF THE AIRCRAFT. A GEAR DOOR WAS OBSERVED BY GROUND PERSONNEL AS REMAINING OPEN WHEN THE GEAR WAS RETRACTED. FLIGHT 4044 RETURNED TO CAK. MAINTENANCE INSPECTED AND PERFO RMED SEVERAL GEAR SWINGS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. NO DISCREPANCIES WERE FOUND. THE AIRC RAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072300036 20020723 00036 NM 2002 7 23 VNAA0207020 1 20020714 A 3350 PSEU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN MALFUNCTIONED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 458PS 3068 THE CREW REPORTED THAT THE LEFT HAND EMERGENCY DOOR SWITCH WAS INDICATING OPEN INTERMITTENTLY. MAINTENANCE INSPECTED AN D RERACKED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE A IRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072300037 20020723 00037 NM 2002 7 23 VNAA0207021 1 20020715 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 458PS 14568 98 3068 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 4 TO 7 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REP LACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORM ED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072300038 20020723 00038 EA 2002 7 23 HEEA080444 2 20020709 A 7320 324473514 FUEL CONTROL BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA NR 2 ENGINE MALFUNCTIONED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 102PH 30899 NR 2 ENGINE HAS N1 AND TORQUE OSCILLATIONS. REPLACED WITH SERVICEABLE FUEL CONTROL. 1 G 7 1 4U 4 U H4SW E22EA 2002072300039 20020723 00039 2002 7 23 VNAA0207022 4 20020717 A 3425 7015327905 FLIGHT DIR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 463PS 11273 3087 WHEN ADVANCING THE POWER LEVERS, THE CREW RECEIVED A TAKEOFF CONFIGURATION MESSAGE ON THE RED WARNING PANEL AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE FLIGHT DIRECTOR/AUTO PILOT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUA L 22-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072300040 20020723 00040 SW 2002 7 23 HEEA080445 1 20020710 A 6730 30006762102 MANIFOLD BELL 206 206L3 1182108 SW MAIN ROTOR LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 RT LINKAGE HOUSING HAS LEAKING LEE PLUG AND SUSPECT RESTRICTED PASSAGES, CAUSES VERY SLOW MOVEMENT (EXTEND) ON VELOCITY TEST OF SERVO ASSY. PROBLEMS ON SYSTEM NR 1 - RT LINKAGE ONLY. 1 G 7 1 3U H2SW 2002072300041 20020723 00041 NM 2002 7 23 VNAA0207023 1 20020717 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 457PS 13711 35 3048 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 4 AND 5 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND RE PLACED THE EMERGENCY BATTERY AND POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECK S WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072300042 20020723 00042 NM 2002 7 23 VNAA0207024 1 20020717 A 7330 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 430JS 3044 THE CREW JUST RECEIVED CLEARANCE FOR TAKEOFF AND EXPERIENCED A LEFT HIGH FUEL FEED TEMPERATURE HIGH CAS MESSAGE AND ABOR TED TAKEOFF. FLIGHT 4173 CLEARED THE RUNWAY AND THE MESSAGE CLEARED BY ITSELF. FLIGHT 4173 WAS THEN CLEARED FOR ANOTHE R TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002072300043 20020723 00043 WP 2002 7 23 GTIA020541 1 20020517 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FLOORBOARD STATION 1750 TO STATION 1270 LEFT SIDE HAS SOFT/DAMAGE ALL CORNERS. FABRICATED FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002072300044 20020723 00044 WP 2002 7 23 GTIA020542 1 20020517 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FLOOR PANEL STATION 1308 TO STATION 1278 HAS MUSHY SOFT/CRACKED AROUND THE EDGE. FORMED NEW PANEL. (M) 2 L 7 2 4F A6WE 2002072300045 20020723 00045 WP 2002 7 23 GTIA020543 1 20020510 A 5230 DOOR FRAME DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND MID CARGO, ENTIRE LOWER DOOR JAMB HAS AREAS OF CORROSION STATION 636 TO STATION 693. REMOVED DOUBLE REPAIR. FORMED NEW DOUBLER REPAIR. INSTALLED DOUBLE REPAIR. (M) 2 L 7 2 4F A6WE 2002072300046 20020723 00046 WP 2002 7 23 GTIA020544 1 20020514 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND PAX CABIN, SEAT TRACK AT FS 1119 X22, FS 1131 X22, FS 1088 X22 HAS CORROSION. CUT AND REMOVED SEAT TRACK SE CTION FROM STATION 1032 TO STATION 1146. LOCATED AND DRILLED NEW SEAT TRACK. LOCATED AND DRILLED SEAT TRACK SPLICE AT X22 STATION 1146. INSTALLED SEAT TRACK AND SPLICE. (M) 2 L 7 2 4F A6WE 2002072300047 20020723 00047 WP 2002 7 23 GTIA020545 1 20020514 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND PASSENGER CABIN, SEAT TRACK AT FS 1241 X22 HAS CORROSION AND GOUGES. SEAT TRACK AT FS 1173 X22 HAS CORROSIO N. REMOVED SEAT TRACK FROM STATION 1146 TO STATION 1250. LOCATED AND DRILLED NEW SEAT TRACK AND SPLICE. INSTALLED SEA T TRACK. (M) 2 L 7 2 4F A6WE 2002072300048 20020723 00048 WP 2002 7 23 GTIA020546 1 20020514 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND PASSENGER CABIN, SEAT TRACK FROM STA Y 1237 TO STATION 1308 HAS CORROSION, GOUGES AND SCRATCHES. REMOVED SE AT TRACK FROM -X22 STATION 1224-1308. DRILLED AND LOCATED NEW SEAT TRACK AD SPLICE. INSTALLED SEAT TRACK AND SPLICE. (M) 2 L 7 2 4F A6WE 2002072300049 20020723 00049 WP 2002 7 23 GTIA020548 1 20020515 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FLOOR SUPPORT SURFACE CORRODED PLUS X5 BETWEEN STATION 160 AND 200. REMOVED FLOOR SUPPORT. DRILLED AND LOC ATED HOLES IN FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002072300050 20020723 00050 WP 2002 7 23 GTIA020550 1 20020516 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FORWARD CABIN ENTRY, FLOOR SUPPORT AT FS 160-200R, BL 44R CORRODED. REMOVED FLOOR SUPPORT. FORMED NEW FLOO R SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002072300051 20020723 00051 WP 2002 7 23 GTIA020551 1 20020516 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FORWARD CABIN ENTRY, FLOOR SUPPORT AT FS 180R, BL9-43R CORRODED. REMOVED FLOOR SUPPORT. DRILLED AND LOCATED HOLE . INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002072300052 20020723 00052 WP 2002 7 23 GTIA020552 1 20020325 A 5730 993757541 PANEL DOUG DC9 DC981 3022081 WP LT WING CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND LEFT WING PANEL NR 1165C HAS BARE METAL AND CHAFE MARKS AROUND EDGES. CORROSION FOUND TO BE OF LIMITS. REC EIVED SERVICEABLE PART. (M) 2 L 7 2 4F A6WE 2002072300053 20020723 00053 WP 2002 7 23 GTIA020553 1 20020516 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FORWARD CABIN ENTRY FLOOR SUPPORT AT FS 200 RBL 58R CORRODED. REMOVED THE FLOOR SUPPORT PART. LOCATED AND DRILLED NEW SUPPORT. INSTALLED NEW SUPPORT PART. LOCATED AND DRILLED NEW SUPPORT. INSTALLED NEW SUPPORT. (M) 2 L 7 2 4F A6WE 2002072300054 20020723 00054 WP 2002 7 23 GTIA020554 1 20020516 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FORWARD CABIN ENTRY, FLOOR SUPPORT AT FS 200R, BL9-43R CORRODED. REMOVED FLOOR SUPPORT. FORMED NEW SUPPORT . INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002072300055 20020723 00055 WP 2002 7 23 GTIA020555 1 20020516 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FORWARD CABIN ENTRY, SUBFLOOR WEB AT FS 200R, BL 6-20R CORRODED. REMOVED FLOOR SUPPORT (APPROX 1 INCH). MATERIAL ON FLOOR SUPPORT (APPROX 1 INCH) IS TO BE OUT OF LIMITS. FABRICATED FLOOR SUPPORT. CUT OUT DAMAGED AREA ON SUB FLOOR WEB. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED FLOOR SUPPORT. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2002072300056 20020723 00056 WP 2002 7 23 GTIA020556 1 20020516 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FORWARD CABIN ENTRY, FLOOR SUPPORT AT FS 200, BL 5R-5L CORRODED. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT . INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002072300057 20020723 00057 EU 2002 7 23 HEEA080446 1 20020709 A 6720 350A33214501 ROD SNIAS 350 AS350B 8680801 EU PITCH CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 970AE 3235 TAIL ROTOR PITCH CONTROL ROD HAS WORN SPHERICAL BEARINGS. 1 G 7 1 3U H9EU 2002072300058 20020723 00058 EU 2002 7 23 HEEA080447 1 20020709 A 6500 350A33215300 BEARING SNIAS 350 AS350B 8680801 EU TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 970AE 3235 TAIL ROTOR LAMINATED HINGE BEARING WORN. 1 G 7 1 3U H9EU 2002072300059 20020723 00059 EU 2002 7 23 HEEA080448 1 20020709 A 6420 355A09103601 BEARING SNIAS 350 AS350B 8680801 EU TAIL ROTOR WORN E K NONE O OTHER IN INSP/MAINT 1 SW 03 970AE 3235 TAIL ROTOR ELASTOMERIC BEARINGS HAVE SEVERAL CRACKS. 1 G 7 1 3U H9EU 2002072300060 20020723 00060 EU 2002 7 23 HEEA080449 1 20020709 A 6420 355A09103601 BEARING SNIAS 350 AS350B 8680801 EU TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 973AE 3229 TAIL ROTOR ELASTOMERIC BEARINGS HAVE SEVERAL CRACKS. 1 G 7 1 3U H9EU 2002072300061 20020723 00061 EU 2002 7 23 HEEA080450 1 20020709 A 6510 10531541 SHAFT BOLKMS 105 BO105S 5626006 EU TAIL ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U S678 PITTED ON AFT END AND FLANGE RIVETS HAVE CORROSION. REPLACED SHAFT P/N 105-31546, S/N 709 DUE TO CORROSION AND DISC P/ N 1121-31531 DUE TO COATING DAMAGED. 1 G 7 2 3U H3EU 2002072300062 20020723 00062 NE 2002 7 23 GTIA020557 2 20020529 A 7220 INLET SCREEN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 603CA 49508 DTW - FOUND NR 2 ENGINE INLET WIRE MESH DELAMINATED AT 9 O'CLOCK POSITION. REPAIRED DELAMINATED IAW MD80 SRM 54-04. (M ) 2 L 7 2 4F 4 F A6WE E9NE 2002072300063 20020723 00063 WP 2002 7 23 GTIA020558 1 20020518 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND COCKPIT, SUB FLOOR WEB CORRODED, FS 144-160, BL 12L-15R, SEVERAL PLACES. CUT OUT DAMAGED AREA. LOCATED AND DRILLED DOUBLER AND FILLER. INSTALLED REPAIR PARTS. REMOVED CORROSION ON 1 FLOOR SUPPORT STATION 160 BL 5L-5R. FORME D NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002072300064 20020723 00064 WP 2002 7 23 GTIA020559 1 20020529 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 812NK 48021 FOUND EMERGENCY LIGHTS INOPERATIVE IN FORWARD PAX CABIN. FOUND BATTERIES IN BATTERY PACK DEAD, INSTALLED NEW BATTERIES FOUND PACK WOULD COME ON WHEN POWER REMOVED FROM A/C. REMOVED AND REPLACED B5-24 BATTERY PERFORMED OPS CHECK. (M) 2 L 7 2 4F A6WE 2002072300065 20020723 00065 WP 2002 7 23 GTIA020560 1 20020516 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FORWARD CABIN ENTRY, FLOOR SUPPORT AT FS 200-256L, BL 14L EXFOLIATED, CORRODED. REMOVED FLOOR SUPPORT FS 200-256L . LOCATE AND DRILLED HOLES. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002072300066 20020723 00066 GL 2002 7 23 HEEA080451 2 20020709 A 7510 1092T1002W SERVO BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ANTI ICE FAILED E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 7136H S833 NR 1 ANTI ICE INOPERATIVE AND LIGHT FLASHES. 1 G 7 2 3U 3 U H3EU E4CE 2002072300067 20020723 00067 WP 2002 7 23 GTIA020561 1 20020509 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - AFT PIT STATION 1212 L29R-L28R, INTERCOSTAL CORRODED ON UPPER AND LOWER FLANGES. FABRICATED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002072300068 20020723 00068 EU 2002 7 23 HEEA080452 1 20020709 A 6510 112131521 SHAFT BOLKMS 105 BO105S 5626006 EU TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81992 6282 S827 BEARINGS SPIN ON SHAFT. REPLACED SHAFT P/N 1121-31526, S/N 705 DUE TO BORES WORN; BEARINGS P/N BB1B649616B (4 EACH) DU E TO CORROSION; SLEEVE P/N 1121-31521.05 (4 EACH) DUE TO WORN; SPRING PIN P/N 1121-31521.12 (3 EACH) DUE TO CORROSION; N UTS P/N LN9348-05 (3 EACH) DUE TO WORN. 1 G 7 2 3U H3EU 2002072300069 20020723 00069 WP 2002 7 23 GTIA020562 1 20020511 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND MID PIT CORROSION AT SHEAR TIE STATION 656. REMOVED SECTION DAMAGED. FORMED SHEAR TIE SECTION. INSTALLED SHEAR TIE SECTION REPAIR. (M) 2 L 7 2 4F A6WE 2002072300070 20020723 00070 NM 2002 7 23 A6WA200230013 1 20020705 A 2120 5729C000002 ECU DORNER DO32 DO328100 2996000 NM LEFT INOPERATIVE A A6WA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 350AD 13995 3050 PILOTS REPORTED SMOKE IN CABIN DURING TAXI, SMOKE STOPPED AFTER DE-SELECTING LEFT PACK. MAINTENANCE INSPECTED AND FOUND LEFT AIR CONDITIONING PACK INOPERATIVE. 2 H 7 2 4T RT A45NM 2002072300071 20020723 00071 EA 2002 7 23 SWIA200211054 1 20020714 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NA FLAP POSITION IN SHORTED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 445SW 7651 UPON ROTATION IN OKC, THROUGH 10 DEGREE PITCH UP, STICK SHAKER ACTIVATED. WINDSHEAR FAIL STATUS MESSAGE AND CONTINUOUS IGNITION, AIRSPEED WAS ROUGHLY 165 KTS. THEN ON FINAL IN SLC, GEAR WAS COMING DOWN, WINDSHEAR FAIL MESSGE APPEARED AGAI N, CONTINUOUS IGNITION LIGHT CAME ON MOMENTARILY. NO STICK SHAKER ACTIVATION. REPLACED #2 ADSHC. GROUND FUNCTIONAL CH ECK GOOD. UPDATE 7/17/02: FOUND WIRE CG51C22 SHORTING AT FLAP POSITION TRANSMITTER CANNON PLUG. REMOVED DAMAGED WIRE LENGTH AND REPLACED SOCKETS ON ALL WIRES TO CONNECTOR. FLAP OPERATION CHECKS GOOD. FAULT CODES CLEARED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002072300072 20020723 00072 WP 2002 7 23 GTIA020563 1 20020512 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT CARGO STATION 1155 INTERCOSTAL ASSEMBLY HAS CORROSION. FOUND 1 TEE TO BE OUT OF LIMITS. FABRICATED T-A NGLE. (M) 2 L 7 2 4F A6WE 2002072300073 20020723 00073 WP 2002 7 23 GTIA020564 1 20020512 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT CARGO INTERCOSTAL ASSEMBLY STATION 1203 HAS CORROSION AND TOOL MARKS. T-ANGLE OUT OF LIMITS. FABRICATE D T-ANGLE. (M) 2 L 7 2 4F A6WE 2002072300074 20020723 00074 WP 2002 7 23 GTIA020565 1 20020517 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - AFT CARGO INTERCOSTAL ASSEMBLY STATION 1165 HAS CORROSION AND POSSIBLY CRACKED. FOUND T-ANGLE TO BE OUT OF LIMITS . FORMED NEW T-ANGLE. INSTALLED INTERCOSTAL AND T-ANGLE TO STATION 1165. (M) 2 L 7 2 4F A6WE 2002072300075 20020723 00075 WP 2002 7 23 GTIA020566 1 20020512 A 5320 CLIP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT CARGO CLIP STATION 1250 HAS CORROSION. REMOVED CORROSION. FABRICATED NEW CLIP. (M) 2 L 7 2 4F A6WE 2002072300077 20020723 00077 NM 2002 7 23 USAASB02063 1 20020325 A 3230 6301001033 CONTROL CABLE BOEING 737 7373B7 1384580 NM MANUAL EXTENSION EXCESS PLAY A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 514AU 23700 FLT 493 - FINAL APPROACH TO RDU, APPROX 4,000 FT AGL, CREW DID NOT RECEIVE THE RT MLG GREEN LIGHT ON GEAR EXTENSION. CR EW ABORTED APPROACH AND REPLACED BULB FOR RT MLG INDICATION WITH NO HELP. CREW ACCOMPLISHED MANUAL GEAR EXTENSION PROCE DURES WITH STILL NO CHANGE IN RT MLG LIGHT STATUS. CREW DECLARED AN EMERGENCY AND PREPPED FOR AN EMERGENCY LANDING. FL T LANDED INCIDENT. MX FOUND THE WRONG TYPE OF BULB INSTALLED FOR THE RT MLG INDICATION. REPLACED BULB WITH CORRECT TYP E. OPERATIONAL CHECK GOOD. AIRCRAFT WAS FERRIED FOR REPAIR OF RT MLG MANUAL EXTENSION PULL HANDLE NOT STOWING. APPROX 5 INCHES OF SLACK WAS IN CABLE. MX RESET RT MLG MANUAL EXTENSION PULL HANDLE, CHECKED CABLE RUN AND ADJUSTMENT.(M) 2 L 7 2 4F RT A16WE 2002072300079 20020723 00079 WP 2002 7 23 GTIA020567 1 20020512 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT CARGO INTERCOSTAL ASSEMBLY HAS ELONGATED HOLES AND LIGHT CORROSION STATION 1193. FOUND T-ANGLE TO BE OU T OF LIMITS. FABRICATED ANGLE. (M) 2 L 7 2 4F A6WE 2002072300083 20020723 00083 NM 2002 7 23 COOSDR020183 1 20020701 A 5753 652165114 FITTING BOEING 727 727232 1384082 NM T/E FLAP CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 511PE 20634 RIGHT WING INBOARD FLAP INBOARD TRACK, FORWARD ATTACH FITTING CORRODED. 2 L 7 3 4F A3WE 2002072300084 20020723 00084 NM 2002 7 23 COOSDR020184 1 20020701 A 5753 652165113 FITTING BOEING 727 727232 1384082 NM T/E FLAP CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 511PE 20634 LEFT WING INBOARD FLAP INBOARD TRACK, FORWARD ATTACH FITTING CORRODED. 2 L 7 3 4F A3WE 2002072300086 20020723 00086 NM 2002 7 23 COOSDR02176 1 20020701 A 5720 65281213 FITTING BOEING 727 727227 1384078 NM LT & RT WING WORN B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 LEFT AND RIGHT WING - FITTINGS WITH WEAR. LOCATED AT WBL 297.3 OUTBOARD ACTUATOR SCREW FAIRING. 2 L 7 3 4F A3WE 2002072300087 20020723 00087 NM 2002 7 23 COOSDR02181 1 20020701 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 FUSELAGE SKIN CORRODED LOCATED FROM BS 920 TO BS 923, STR 18A LEFT LEVEL. 2 L 7 3 4F A3WE 2002072300088 20020723 00088 NM 2002 7 23 COOSDR02182 1 20020701 A 5313 655623652 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 511PE 20634 FORWARD CARGO COMPARTMENT FROM BS 480 TO BS 540, STRINGER 26R CORRODED. 2 L 7 3 4F A3WE 2002072300089 20020723 00089 NM 2002 7 23 COOSDR02185 1 20020701 A 5730 SKIN BOEING 727 727227 1384078 NM RT WING CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 RIGHT WING, LOWER SKIN - LOWER SURFACES CORRODED AT WS 637, BETWEEN STIFFENER NR 8 AND STIFFENER NR 9. 2 L 7 3 4F A3WE 2002072300090 20020723 00090 SO 2002 7 23 COMA0210028 1 20020721 A 3150 WIRE EMB 120 EMB120RT 3260202 SO A COMA C ABORTED TAKEOFF F N FLT CONT AFFECTED FALSE WARNING TO TAKEOFF 1 SO 01 269CA 120263 FLIGHT 5080 TAKE OFF TRIM CONFIG WARNING DURING T/O.REPAIRED BROKEN WIRE AT ELEVATOR TAB PROX SENSOR. 2 L 7 2 4T RT A31SO 2002072300091 20020723 00091 WP 2002 7 23 GTIA020568 1 20020514 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49190 FTW - FOUND AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN FS 1322 AND FS 1335 ABOVE LONGERON 22 LEFT. REMOVED INTE RCOSTAL ABOVE LONGERON 22L. REMOVED INTERCOSTAL BELOW LONGERON 21L STATION 1338. FABRICATED REPAIR INTERCOSTALS. INST ALLED INTERCOSTALS. (M) 2 L 7 2 4F A6WE 2002072300092 20020723 00092 WP 2002 7 23 GTIA020569 1 20020515 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FLOOR SUPPORT CORRODED STATION 200 PLUS X6 ALONG UP TO PLUS X10. REMOVED SUPPORT ANGLE. FORMED NEW FLOOR S UPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002072300093 20020723 00093 WP 2002 7 23 GTIA020570 1 20020516 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND CABIN ENTRY FORWARD FLOOR SUPPORT TRACK AT FS 148.55-200R, BL 5.5-9.5R EXFOLIATED. REMOVED FLOOR SUPPORT. FABRICATED NEW SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002072300094 20020723 00094 SO 2002 7 23 COMA0210029 1 20020718 A 3350 1317 LAMP EMB 120 EMB120RT 3260202 SO CABIN BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 264CA 120256 FLIGHT 5047 EMERGENCY LIGHT INOP.REPLACED LIGHT BULB. 2 L 7 2 4T RT A31SO 2002072300095 20020723 00095 WP 2002 7 23 GTIA020571 1 20020522 A 7120 ISOLATOR DOUG DC9 DC982 3022082 WP RT ENGINE OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND RIGHT ENGINE FORWARD LOWER VIBRATION ISOLATOR MIGRATION. REMOVED ISOLATOR FORWARD, LOWER, NR 2 ENGINE. INS TALLED SERVICEABLE ISOLATOR, NR 2 ENGINE LOWER, FORWARD. (M) 2 L 7 2 4F A6WE 2002072300096 20020723 00096 WP 2002 7 23 GTIA020572 1 20020511 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND MID PIT, CORRODED AT RIGHT END BOTTOM ANGLE BULKHEAD STATION 788. REPAIR PARTS FABRICATED. INSTALLED REPAI R PARTS. (M) 2 L 7 2 4F A6WE 2002072300097 20020723 00097 EA 2002 7 23 COMA0260438 1 20020719 A 3350 59465 CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR FAULTY A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 805CA 7354 FLIGHT 5200 EMERGENCY FLOOR LIGHTING IS INOP ROWS 2 THRU 5.REPLACED LIGHT STRIP CONNECTOR CABLE. 2 L 7 2 4F RT A21EA 2002072300099 20020723 00099 WP 2002 7 23 GTIA020573 1 20020513 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT CARGO FRAME ASSEMBLY STATION 1098 HAS CORROSION AND DOUBLE DRILLED HOLES. FRAME IS FOUND TO BE WITHIN L IMITS. REMOVED ONE HOLE FROM FRAME TO SECOND OVERSIZE. REMOVED CORROSION FROM FORMER ANGLE STATION 1098. LOCATED AND DRILLED NEW PART. (M) 2 L 7 2 4F A6WE 2002072300101 20020723 00101 WP 2002 7 23 GTIA020574 1 20020512 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT CARGO INTERCOSTAL STATION 1220 HAS CORROSION AND TOOL MARKS. FABRICATED 1 TEE ANGLE. (M) 2 L 7 2 4F A6WE 2002072300102 20020723 00102 EA 2002 7 23 COMA0260439 1 20020720 A 5240 ACCESS DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER W INADEQUATE Q C CL CLIMB 1 SO 01 917CA 7017 FLIGHT 6067 LOUD HUMMING SOUND FROM NOSE AREA OF AIRCRAFT.FOUND GPU ACCESS PANEL OPEN - INSPECTED FOR DAMAGE - CLOSED PA NEL. 2 L 7 2 4F RT A21EA 2002072300103 20020723 00103 CE 2002 7 23 AMTA200200950 1 20020717 A 2560 2463 PANEL CESSNA 310 310D 2074212 CE CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 186A 39175 WITH EVAC SIGNAL COMMAND ACTIVATED, THE PANEL AT L1 DOOR DOES NOT SILENCE WHEN BUTTON IS PRESSED. 1 L 7 2 3O 3A10 2002072300104 20020723 00104 NE 2002 7 23 KBMA117643 2 20020703 A 7314 P94B12209 PUMP SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE FUEL SYSTEM INOPERATIVE E KBMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 53SH 1424 2009 FUEL PRESSURE CAUTION LIGHT INDICATION IS ON. FUEL PUMP IS INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2002072300105 20020723 00105 EA 2002 7 23 COMA0260440 1 20020721 A 2740 83963 TRIM MOTOR CNDAIR CL600 CL6002B19 1900309 EA HORZ STAB MALFUNCTIONED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 01 986CA 17125 7174 FLIGHT 5297 STAB AND MACH TRIM FAIL MESSAGE.REPLACED THE HSTA 2 L 7 2 4F RT A21EA 2002072300106 20020723 00106 2002 7 23 GTIA020578 4 20020603 A 2230 2587781901 SERVO DOUG DC9 DC981 3022081 WP AUTOTHROTTLE SYS DEFECTIVE A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 805NK 48058 ORD - FLT 1453 - AT CRUISE AUTO THROTTLE DISENGAGED, SWITCHED COMP 1 TO 2. AUTO THROTTLE WOULD NOT REENGAGE. PERFORMED TROUBLE SHOOTING FOUND AUTO THROTTLE SERVO BAD. REMOVED AND REPLACED AUTO THROTTLE SERVO DRIVE. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002072300107 20020723 00107 EU 2002 7 23 KBMA117644 1 20020702 A 5414 TL100AXE9L LATCH SNIAS 350 AS350B1 8680811 EU RT ENG COWL WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 6083 2009 RIGHT REAR ENGINE COWLING LATCH IS WORN. REPLACE WITH SERVICEABLE LATCH. 1 G 7 1 3U H9EU 2002072300108 20020723 00108 EU 2002 7 23 KBMA117645 1 20020703 A 7712 305731366 INDICATOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TORQUE INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 2273A 2273 TORQUE GUAGE INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002072300109 20020723 00109 2002 7 23 KBMA117652 4 20020706 A 3421 RCA26BK12 INDICATOR BELL 206 206B 1181511 SW ATTITUDE INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 73DP 943 2513 ATTITUDE INDICATOR INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U H2SW 2002072300110 20020723 00110 2002 7 23 KBMA117653 4 20020709 A 3421 RCA26BX12 INDICATOR BELL 206 206B 1181511 SW ATTITUDE PRECESSES E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 73DP 6 2513 ATTITUDE INDICATOR PRECESSES 10 DEGREES IN 10 MINUTES OR LESS. 1 G 7 1 3U H2SW 2002072300111 20020723 00111 EA 2002 7 23 COMA0260441 1 20020720 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 436CA 5749 7482 FLIGHT 5099 GEAR DISAGREE WARNING - NLG DID NOT EXTEND.REPALCED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002072300112 20020723 00112 EU 2002 7 23 KBMA117646 1 20020703 A 5230 350A2513501901 LOCK SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE DOOR INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 2273A 2273 RIGHT SLIDING DOOR DOES NOT LATCH. REMOVED AND REPLACED WITH NEW CYLINDER LOCK. 1 G 7 1 3U 3 U NC H9EU E19EU 2002072300113 20020723 00113 EA 2002 7 23 COMA0260443 1 20020720 A 3230 555405 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 916CA 19063 7014 FLIGHT 9460 GEAR DISAGREE - NLG DID NOT EXTEND UNTIL EMERGENCY RELEASE WAS PULLED.REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002072300114 20020723 00114 NM 2002 7 23 QXEA0200967 1 20020721 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 14572 321 504 PDX-EMERGENCY LEFT HAND AFT EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT HAND FORWARD CEILING EMERGENCY BATTERY I N CABIN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072300115 20020723 00115 NM 2002 7 23 ZW0A0206901 1 20020619 A 5414 SKIN BOEING 757 7572Q8 1384972 NM NR 1 PYLON CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 701TW 28160 DURING CHECK-C MAINT ON NUMBER 1 PYLON FOUND A 1 7/8 INCH CRACK EXTENDING FROM UPPER FORWARD CORNER OF FORWARD LIGHTNING HOLE IN LT SIDE SKIN OF PYLON. CONFIRMED BY EDDY CURRENT. INSTALLED FORWARD DOUBLER ON OTBD SIDE PER SERVICE BULLETIN 757-54-0037 AND EMLR 73125. --CLOSED-- 2 L 7 2 4F RT A2NM 2002072300116 20020723 00116 NM 2002 7 23 ZW0A0206902 1 20020620 A 5410 STRUCTURE BOEING 757 7572Q8 1384972 NM NR 2 PYLON CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 701TW 28160 DURING CHECK-C MAINT ON RT PYLON, THE FWD OTBD SIDE LIGHTNING HOLE ON THE NUMBER 2 PYLON WAS CRACKED ABOUT 1/2 INCH LONG . CONFIRMED BY NDT. REPAIRED PER SERVICE BULLETIN 757-54-0037 AND EMLR 73125. --CLOSED-- 2 L 7 2 4F RT A2NM 2002072300117 20020723 00117 NM 2002 7 23 2002UALA01169 1 20020712 A 5330 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 AFT PIT LH SIDE STATION 1400 ABOVE STRINGER 26L TOP OF FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW DOUBLER, STRAP AND CAP INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072300118 20020723 00118 NM 2002 7 23 2002UALA01170 1 20020712 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 STRINGER 14L AT STATION 620 HAS A DENT. MAJOR REPAIR ACCOMPLISHED. SPLICED IN HAT CHANNEL REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072300119 20020723 00119 NM 2002 7 23 2002UALA01172 1 20020713 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 AFT PIT AT STATION 1440 ABOVE STRINGER 26 LEFT, TOP OF FRAME FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED. FRAME DOUBLER IN STALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072300120 20020723 00120 NM 2002 7 23 2002UALA01179 1 20020715 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 LEFT HAND FUSELAGE STATION 600-640 STRINGER 13L-18L HAS MULTIPLE DENTS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISH ED. INSTALLED FLUSH REPAIR, DOUBLERS AND TRIPLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072300121 20020723 00121 NM 2002 7 23 2002UALA01182 1 20020717 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 FUSELAGE DENTED AT STATION 1690-1706, BELOW STRINGER 17R-RADIUS. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND TRIPLER INSTALL ED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072300122 20020723 00122 WP 2002 7 23 GTIA020579 1 20020601 A 3397 WIRE DOUG DC9 DC981 3022081 WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 805NK 48058 TPA - FLT 632 - FOUND FORWARD EMERGENCY PATH LIGHTING NOT ILLUMINATING. REPAIRED BROKEN WIRE AT IAE. SYSTEM OPS CHECK SATISFACTORY WITH SAME. (M) 2 L 7 2 4F A6WE 2002072300123 20020723 00123 2002 7 23 GTIA020580 4 20020603 A 2215 2587788902 SERVO DOUG DC9 DC932 3022066 WP AUTOPILOT SYS FAULTY A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 12536 47113 TPA - FLT 276 - AUTO PILOT AILERON SERVO IS ERRATIC IN ALL REQUIRES OF FLIGHT 276. REMOVED AND REPLACED SERVO AUTO DRIV E. OPS CHECK OK. BITE CHECK FOR SERVO PORTION OF CHECK ON ROLL COMP. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2002072300124 20020723 00124 2002 7 23 GTIA020581 4 20020530 A 2215 4034237915 SERVO DOUG DC9 DC982 3022082 WP AUTOPILOT SYS MALFUNCTIONED A GTIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 GL 23 801NK 48048 ACY - FLT 259 - FOUND AUTO PILOT FAILED ON DESCENT A/P TRIM LIGHT WAS ON. A/P FAILED TO CAPTURE ALT ON DESCENT USING NR 1 A/P. REMOVED AND REPLACED ELEVATOR SERVO DRIVE ASSY RTS CHECK RAN, OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2002072300125 20020723 00125 WP 2002 7 23 GTIA020582 1 20020529 A 5730 SKIN DOUG DC9 DC981 3022081 WP WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 DTW - FOUND SKIN CRACKED ON LEADING EDGE WING AT STATION 3281.75. REPAIRED LEADING EDGE, IAW MD80 M/M. (M) 2 L 7 2 4F A6WE 2002072300126 20020723 00126 WP 2002 7 23 GTIA020583 1 20020529 A 5754 SLAT DOUG DC9 DC981 3022081 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 DTW - FOUND RIGHT WING LEADING EDGE THE NR ZERO SLAT TRACK THE SLAT IS CRACKED ON THE INBOARD SIDE. REPAIRED IAW MD80. (M) 2 L 7 2 4F A6WE 2002072300127 20020723 00127 WP 2002 7 23 GTIA020584 1 20020603 A 2612 CONNECTOR DOUG DC9 DC982 3022082 WP FIRE DETECTION FAULTY A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 603CA 49508 DTW - FLT 503 - PREFLIGHT, LEFT ENGINE FIRE DETECTION SYSTEM DOES NOT TEST CORRECTLY. WHEN TESTED, LIGHT IN FIRE HANDLE FLICKERS, WARNING WILL NOT SILENCE AND LOOP 'B' LIGHT FLICKERS. REPLACED CONNECTOR AT FIRE LOOP 'B' SIDE ON LEFT ENGIN E, OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2002072300128 20020723 00128 WP 2002 7 23 GTIA020585 1 20020529 A 7711 CONNECTOR DOUG DC9 DC982 3022082 WP RT EPR DIRTY A GTIA O OTHER O OTHER TO TAKEOFF 1 GL 23 820NK 49126 DTW - FLT 313 - WHILE APPLYING TAKEOFF POWER RIGHT EPR GAUGE STUCK AT 148 AUTO THROTTLE DISENGAGED DURING TAKEOFF. FOUN D RIGHT ENGINE EPR CANNON PLUG DIRTY CLEANED CANNON PLUG REINSTALLED, OPS CHECK NORMALLY. AUTO THROTTLES OPS NORMAL. ( M) 2 L 7 2 4F A6WE 2002072300129 20020723 00129 EU 2002 7 23 02FDEA00498 1 20020717 A 2130 82010B040901 CONTROLLER AIRBUS 310 A310 EU ZONE 300 A FDEA A UNSCHED LANDING J O WARNING INDICATION OTHER CL CLIMB 1 SO 25 448FE 260 CLIMBING OUT OF SEA, ECAM ALERT - "EXCESS CAB ALT". DONNED O2 MASKS AND TRIED TO TROUBLESHOOT PROBLEM. SWAPPED REGULAT ORS FOR PRESS. TRIED MANUALLY PRESS AIRPLANE. NO SUCCESS. RETURNED TO SEA FOR LANDING. UPON BLOCK-IN, COULD NOT TES T EITHER SYS 1 OR 2. FOUND #1 SYS BITE UNIT ROTARY SWITCH OUT OF "NORM FLT" POSITION. RESET TO NORMAL POSITION AND #1 UNIT TESTS OK PER A310 MM 21-31-00-5-01. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2002072300130 20020723 00130 WP 2002 7 23 MWEA020453 1 20020705 A 5343 59258521 FITTING DOUG DC9 DC982 3022082 WP LH GEAR WELL CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 LEFT GEARWELL "PORKCHOP" FITTING HAS A CRACK APPROXIMATELY 6 INCHES DOWN & FORWARD OF MAIN LANDING GEAR SIDE BRACE ATTAC H BOLT. -- REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 2002072300131 20020723 00131 NM 2002 7 23 ZW0A0206903 1 20020620 A 5414 SKIN BOEING 757 7572Q8 1384972 NM RT PYLON CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 701TW 28160 DURING CHECK-C MAINT ON THE RT PYLON THE FWD INBD SIDE LIGHTNING HOLE ON NUMBER 2 PYLON WAS CRACKED 1/2 INCH LONG. CONF IRMED BY NDT. REPAIRED PER SERVICE BULLETIN 757-54-0037, AND EMLR 73125. --CLOSED-- 2 L 7 2 4F RT A2NM 2002072300132 20020723 00132 NM 2002 7 23 ZW0A0207001 1 20020707 A 3350 BULB BOEING 767 767300 1385204 NM CABIN BURNED OUT A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 691LF 25137 AFT-RIGHT CABIN FLOOR EGRESS LIGHTING INOPERATIVE. REPLACED LAMPS AND LENS COVER. LAST CHECK C PERFORMED 09/23/2000 A T LAX. --CLOSED-- 2 L 7 2 4F RT A1NM 2002072300133 20020723 00133 WP 2002 7 23 ZW0A0207003 1 20020708 A 2170 COALESCER BAG DOUG DC9 DC983 3022083 WP AC PACK CONTAMINATED A ZW0A O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 13 9620D 53591 SMOKE WAS PRESENT IN CABIN AFTER STARTING APU. CHECKED WATER SEPARATORS AND PERFORMED MD9-49-06 MAINTENANCE SHEET. LAST CHECK C PERFORMED 10/25/2001 AT MCI. --CLOSED-- 2 L 7 2 4F RT A6WE 2002072300134 20020723 00134 WP 2002 7 23 ZW0A0207202 1 20020712 A 2150 20495054 ACM DOUG DC9 DC982 3022082 WP AIR CONDITIONING OVERHEATED A ZW0A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 13 909TW 49170 THE RT AIR CONDITIONING PACK OVERHEATED AND CAUSED SMOKE IN THE MAIN CABIN. SHUT DOWN THE RIGHT PACK. DEFERRED CORRECT IONS TO RT PACK PER MEL. THE AIR CYCLE MACHINE OIL QUANTITY WAS VERY LOW AND THE ACM WAS COVERED WITH OIL. THE ACM WAS REPLACED. CHECK-C 4-27-01 MCI. --CLOSED-- 2 L 7 2 4F A6WE 2002072300135 20020723 00135 WP 2002 7 23 ZW0A0207203 1 20020708 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 966TW 53616 THE EMERGENCY OVERHEAD LIGHTS WERE INOPERATIVE AT ROW 19 AND 22. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 3 -23-01 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2002072300136 20020723 00136 WP 2002 7 23 ZW0A0207204 1 20020708 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 966TW 53616 THE RT AND LT SIDE EMERGENCY OVERWING EXIT LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK- C 3-23-01 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2002072300137 20020723 00137 WP 2002 7 23 ZW0A0207205 1 20020708 A 3350 BULB DOUG DC9 DC983 3022083 WP TAIL CONE BURNED OUT A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 966TW 53616 THE OVERHEAD CENTER EMERGENCY LIGHT IN THE TAIL CONE AREA, AND THE EGRESS LIGHT AT ROWS 7 AND 31, WERE INOPERATIVE. REPL ACED THE BULB PN 1315 IN TAIL CONE AREA, AND REPLACED THE BULB PN 7732 AT BOTH ROWS 7 AND 31. CHECK-C 3-23-01 STL. --C LOSED-- 2 L 7 2 4F RT A6WE 2002072300138 20020723 00138 WP 2002 7 23 ZW0A0207401 1 20020718 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 960TW 49231 THE EMERGENCY LIGHTS IN THE COCKPIT AND ENTRY DOOR OVERHEAD, AND THE EGRESS LIGHTS IN THE FIRST CLASS SECTION, WERE INOP ERATIVE. REPLACED THE POWER SUPPLY FOR THE EMERGENCY LIGHT MALFUNCTION, AND THE AIRCRAFT MAINTENANCE FERRIED TO STL FOR CORRECTION OF THE EGRESS LIGHTS. THE EGRESS LIGHT FEEDER STRIP IN FIRST CLASS WAS CLEANED AND RESECURED. CHECK-C 5-30 -01 STL. --CLOSED-- 2 L 7 2 4F A6WE 2002072300139 20020723 00139 NM 2002 7 23 ZW0A0207501 1 20020720 A 3397 WIRE BOEING 767 767300 1385204 NM CABIN DAMAGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 640TW 25411 THE FORWARD BULKHEAD LEFT SIDE EGRESS LIGHT WAS INOPERATIVE. INSTALLED SPLICE IN FEEDER CABLE. CHECK-C 11-9-01 LAX. - -CLOSED-- 2 L 7 2 4F RT A1NM 2002072300140 20020723 00140 NM 2002 7 23 ZW0A0207502 1 20020721 A 3397 WIRE BOEING 757 757231 1384950 NM SEAT 1B DAMAGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 725TW 30338 THE EGRESS LIGHT IN FRONT OF SEAT 1B WAS INOPERATIVE. REPAIRED FEEDER CABLE. CHECK-C 2-14-02 MCI. --CLOSED-- 2 L 7 2 4F RT A2NM 2002072300141 20020723 00141 2002 7 23 ZW0A205901 4 20020602 A 3418 COMPUTER DOUG DC9 DC982 3022082 WP STALL WARNING FAILED A ZW0A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 13 958U 49703 ON TAKEOFF OUT OF STL LT AND RT GEAR UNSAFE LITES AND SLAT DISAGREE LIGHTS ON INTERMITTENTLY WITH A SLAT OVRSP WARNING O N CLIMB OUT THRU 11000 FT. RETURN TO STL. PROX BOX 90348 -TWA-8-336-04 FAILURE. R&R PROX BOX SELF TEST STALL WARNING COM PUTERS CHECKED WOW AND MLG SENSORS CYCLED SLATS NUMEROUS TIMES AND RAN ENGINES. ALL OPS NORMAL. LAST CHECK-C STL 11/27/0 1. --CLOSED-- 2 L 7 2 4F A6WE 2002072300142 20020723 00142 NM 2002 7 23 ZWOA0207002 1 20020708 A 3350 BULB BOEING 757 7572Q8 1384972 NM CABIN BURNED OUT A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 715TW 28483 EGRESS LIGHTING AT SEAT 19C INOP. RELAMPED LIGHT. LAST CHECK C PERFORMED 10/14/2000 AT LAX. --CLOSED-- 2 L 7 2 4F RT A2NM 2002072300143 20020723 00143 WP 2002 7 23 ZWOA0207101 1 20020709 A 3350 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9627R 53597 RIGHT OVERWING FLOOR EGRESS LIGHTS INOP. REPLACED WIRE SECTION AND REPLACED MISSING COVERS. LENS MFG PN 0105607 3015MI-9 32831/ COVER MFG PN 0105601003 PA57-932841/ WIRE SECTION MFG PN 0105606 0055MI-93289 LAST CHECK C PERFORMED IN STL 11/1 6/2001. --CLOSED-- 2 L 7 2 4F RT A6WE 2002072300144 20020723 00144 EU 2002 7 23 XNOA01039 1 20020312 A 2910 VALVE AIRBUS 300 A300B4203 3930306 EU NLG LEAKING A XN0A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 370PC 134 DURING CRUISE, HYDRAULIC GREEN SYSTEMS 'LEVEL LO' LITE ILLUMINATED WITH HYD QTY INDICATING NEAR ZERO. HYDRAULIC SYSTEMS LOSS AND LANDING GEAR GRAVITY EXTENSION CHECKLIST ACCOMPLISHED. UPON INSPECTION FOUND NLG VENT VALVE LEAKING. R2 NLG VENT VALVE IAW A300 MM CH32-32-14. PERFORMED RESTORATION OF LANDING GEAR ACTUATING SYSTEM IAW A300 MM CH32-30-00 A1 PG 2 01. PERFORMED NOSE LANDING GEAR FREE FALL EXTENSION TEST IAW A300 MM CH32-30-00 & NLG NORMAL EXTENTION & RETRACTION TEST IAW A300 MM CH32-30-00. OPS CHECK GOOD AT THIS TIME, NO LEAKS NOTED. 2 L 7 2 4F RT A35EU 2002072300145 20020723 00145 NE 2002 7 23 XNOA01040 2 20020326 A 7200 ENGINE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 1 OUT OF TRIM A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 472AS 125 NR 1 ENGINE IS SLOW TO SPOOL & WILL NOT OBTAIN MAX POWER. TRIMMED NR 1 ENGINE MEC IAW A300 MM 71-00-00. OPS & LEAK CHEC K GOOD. 2 L 7 2 4F 4 F RT A35EU E23EA 2002072300146 20020723 00146 2002 7 23 XNOA01041 4 20020328 A 3421 GYRO AIRBUS 300 A300B4203 3930306 EU COCKPIT INOPERATIVE A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 474AS 219 PLATFORM LIGHT MWP "G" FLAG ON ADI WHEN HAS 3 SELECTED. REMOVED AND REPLACED NR 3 VERTICAL GYRO. NR 3 VERTICAL GYRO ST ILL INOP. TRANSFERRED TO DMI #2225 IAW ENA MEL 34-22-03. PLACARDS INSTALLED. 2 L 7 2 4F RT A35EU 2002072300147 20020723 00147 NE 2002 7 23 XNOA01042 2 20020329 A 7200 ENGINE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 1 OUT OF RIG A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 472AS 125 NR 1 ENGINE IS SLOW TO SPOOL. LAGS BEHIND NR 2 ENGINE BY 35 PERCENT N1. PERFORMED STATIC RIG CHECK VSV. NO FAULT FOUN D. BOROSCOPED 1,5,6,13,14 COMPRESSOR, HPT-1 LPT-2. NO FAULTS FOUND ALL IAW A300 MM 71-00-00. 2 L 7 2 4F 4 F RT A35EU E23EA 2002072300148 20020723 00148 2002 7 23 XNOA01043 4 20020330 A 3417 ADC AIRBUS 300 A300B4203 3930306 EU COCKPIT FAILED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 372PC 196 NR 1 AIR DATA SYSTEM FAILED ON TAXI OUT. R & R NR 1 ADC IAW AB MM 34-11-20. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2002072300149 20020723 00149 EU 2002 7 23 XNOA01044 1 20020416 A 3340 LIGHT AIRBUS 300 A300B4203 3930306 EU ANTI COLLISION INOPERATIVE A XN0A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 372PC 196 RETURNED TO BLOCK FOR MAINTENANCE. NOTICED LOWER ANTI-COLLISION LIGHT INOP. REPAIRED WIRE AT ANTI-COLLISION LIGHT. OPS CHECK GOOD IAW A300 MM 33-48-00. 2 L 7 2 4F RT A35EU 2002072300150 20020723 00150 2002 7 23 XNOA01045 4 20020416 A 2210 DAMPER AIRBUS 300 A300B4203 3930306 EU NR 2 YAW INOPERATIVE A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 224KW 073 NR 2 YAW DAMPER WILL NOT ENGAGE AFTER START UP. TRANSFERRED TO DMI 2268 IAW ENA MEL 22-21-01. CAT "C" PLACARDS INSTALL ED. 2 L 7 2 4F RT A35EU 2002072300151 20020723 00151 NE 2002 7 23 XNOA01046 2 20020416 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D9 52048 NE NR 2 MALFUNCTIONED A XN0A O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 23 793A 20774 ON TAKE OFF ALL EGTS APPEARED RED, ENG NR 2 N1 APPROACHED RED LINE. POWER BACK TO 1.66 TO GET INTO GREEN. AT ALT 260 A IRFRAME (315K) VIBRATION. INSPECTED ENGINES IAW B727 MM 71-00. ALL PARAMETERS IN LIMITS IAW B727 MM 71-00. FOUND LOOS E COOLING PACK INLET DUCT CAUSING VIBRATION WITH ACM OPERATION. SECURED DUCT IAW B727 MM 36-00-1 ACM OPS CHECK GOOD IAW B727 MM 21-51-0. 2 L 7 3 4F 4 F A3WE E2EA 2002072300152 20020723 00152 EU 2002 7 23 XNOA01047 1 20020510 A 2781 ACTUATOR AIRBUS 300 A300B4203 3930306 EU LE SLATS LOCKED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 224KW 073 ON TAXI AFTER SLATS & FLAPS SELECTION, NO INDICATION ON THE SFPI OF SLATS. FOUND RT INBOARD SLAT ACTUATOR IN LOCKED OU T POSITION. UNLOCKED ACTUATOR L/E SLAT SYSTEM. OPS CHECKS GOOD IAW AMM 27-81-00. 2 L 7 2 4F RT A35EU 2002072300153 20020723 00153 EU 2002 7 23 XNOA01048 1 20020604 A 2710 INDICATOR AIRBUS 300 A300B4203 3930306 EU LT AILERON INCORRECT A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 224KW 073 COULD NOT GET FULL DEFLECTION LT AILERON. REMOVED & REPLACED SURFACE POSITION INDICATORS AS REQ IAW A300 MM REF 27-25 -00. CONTROL SURFACES NORMAL. OPS CHECK GOOD ON GROUND. 2 L 7 2 4F RT A35EU 2002081500122 20020815 00122 NM 2002 8 15 F3LA200200197 1 20020719 A 2742 AR6460M2 ACTUATOR BOEING 737 73736E 138443A NM HORIZ STAB MALFUNCTIONED A F3LA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 03 317FL 730 25263 FLIGHT CREW REPORTED MOMENTARY PITCH TRIM RUNAWAY ON CLIMBOUT AT FL260. NOSE DOWN FOR APPROXIMATELY 2 SECONDS. BACK PR ESSURE WAS APPLIED TO COUNTER TRIM AND NOSE UP ELECTRIC TRIM WAS SELECTED AND TRIM STOPPED. AUTO PILOT WAS OFF. REPLAC ED STABILIZER TRIM ACTUATOR AND R64 RELAY, PERFORMED OPERATIONAL TEST AND CHECKED OKAY. 2 L 7 2 4F RT A16WE 2002072300154 20020723 00154 EU 2002 7 23 XNOA01049 1 20020604 A 3411 PITOT TUBE AIRBUS 300 A300B4203 3930306 EU PITOT STATIC CONTAMINATED A XN0A D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 373PC 218 NO AIRSPEED INDICATION ON EITHER SIDE DURING TAKEOFF ROLL. CLEANED CAPT., FO, & STBY PITOT TUBES IAW A300 MM 34-11-40. OPS CHECK GOOD ON GROUND. 2 L 7 2 4F RT A35EU 2002072300155 20020723 00155 EU 2002 7 23 XNOA01050 1 20020611 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A XN0A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 13974 126 ON START UP SMOKE/ CABIN SMOKE DETECTOR ALARM. RESET MAIN DECK SMOKE DETECTION UNIT. SYS. OPS CHECK GOOD. IAW 26-11-0 0 MM. 2 L 7 2 4F RT A35EU 2002072300156 20020723 00156 2002 7 23 XNOA01051 4 20020618 A 3414 INDICATOR AIRBUS 300 A300B4203 3930306 EU AIRSPEED FAILED A XN0A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 23 372PC 196 ABORTED T/O DUE TO AIRSPEED INDICATOR FAILURE. REMOVED & REPLACED NR 1 ADC, NR 1 A/S OP CKS NORMAL IAW 34-11-40 A300 M/M. PERFPRMED PITOT STATIC CHECK IAW A300 M/M 34-11-10. 1 & 2 A/S IND OP CK NORMAL USING PILOT/STATIC BOX P/N 101-00164 S/N 599. NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 2002072300157 20020723 00157 NM 2002 7 23 XNOA01052 1 20020620 A 2910 LINE BOEING 727 727227 1384078 NM HYD SYSTEM FAILED A XN0A C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 23 793A 20774 ON DEPARTURE OUT OF KMSY LOST A SYSTEM HYDRAULIC PRESSURE AND QUANTITY. REPLACED HYD. FLEX LINE TO TAIL SKID IAW STAND ARD PRACTICE CHAPT. 20. LEAK CHECK GOOD. 2 L 7 3 4F A3WE 2002072300158 20020723 00158 NE 2002 7 23 XNOA01053 2 20020621 A 7532 RELAY AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE GROUND SAFETY LOOSE A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 370PC 134 DURING NR 2 ENGINE START ALL ENGINE PARAMETERS EXCEEDED NORMAL AND IDLE VALVES. FOUND GROUND SAFETY RELAY 91GB LOOSE. REINSTALLED GROUND SAFETY RELAY AND SECURED IAW SP. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A35EU E23EA 2002072300159 20020723 00159 EU 2002 7 23 XNOA01054 1 20020628 A 2930 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU HYD SYSTEM ILLUMINATED A XN0A D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 GL 23 372PC 196 GREEN SYSTEM HYD TEMP HI LIGHT ON. BLED & SERVICED HYD SYS IAW A300 MM CH 12-12-00. SYS OPS CHECK GOOD & NO TEMP LITE WITH ENG. RUN. 2 L 7 2 4F RT A35EU 2002072300160 20020723 00160 EU 2002 7 23 XNOA01055 1 20020628 A 3620 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU NR PNEU REG ILLUMINATED A XN0A D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 GL 23 474AS 219 NR 1 REGULATOR FAULT LIGHT ON. TRANSFERED TO DMI LIST PER ENA A300 MEL 36-11-10. DMI #2443. 2 L 7 2 4F RT A35EU 2002072300161 20020723 00161 EU 2002 7 23 XNOA01057 1 20020709 A 2730 INDICATOR AIRBUS 300 A300B4203 3930306 EU ELEVATOR INOPERATIVE A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 307FV 235 AFTER PUSH BACK, FCPI ELEVATOR INDICATION INOP. TRANSFERED TO DMI #2460 IAW MEL 27-15-01. SP C/W (CAT"B"). 2 L 7 2 4F RT A35EU 2002072300162 20020723 00162 2002 7 23 XNOA01058 4 20020709 A 3414 PITOT TUBE AIRBUS 300 A300B4203 3930306 EU PITOT STATIC SYS OBSTRUCTED A XN0A O OTHER J WARNING INDICATION UK UNKNOWN 1 GL 23 307FV 235 CAPTAIN'S AIRSPEED INDICATOR AND F/O'S INDICATOR ARE SPLIT. SPLIT WENT FROM 50 KTS. DIFFERENCE AND THEN WOULD GO TO 20 K TS SPLIT. REMOVED OBSTRUCTION FROM F/O ASI PITOT PROBE. PERFORMED OPS CHECK IAW MM 34-11-10 & IAW FAR 91.414 PART 43 APP E. 2 L 7 2 4F RT A35EU 2002072300163 20020723 00163 2002 7 23 XNOA01059 4 20020709 A 3442 PACKING AIRBUS 300 A300B4203 3930306 EU WAVEGUIDE ANT DAMAGED A XN0A O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 371PC 157 RADAR ANTENNA TEST FAIL. FOUND BAD PACKING ON ANTENNA WAVEGUIDE CONNECTION. R&R PACKING. OPS CHECK GOOD IAW A300MM 34- 41-11. 2 L 7 2 4F RT A35EU 2002072300164 20020723 00164 EU 2002 7 23 XNOA01060 1 20020711 A 7930 CONNECTOR AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE OIL PRESS XMITER DAMAGED A XN0A O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 13974 126 NR 1 ENGINE OIL PRESSURE GAUGE READS ZERO WITH ENGINE RUNNING-ALL OTHER PARAMETERS NORMAL. CLEANED & RESET CONNECTOR A T OIL PRESS TRANSMITTER. OPS CHECK NORMAL IAW MM 79-00-00. 2 L 7 2 4F 4 F RT A35EU E23EA 2002072300165 20020723 00165 WP 2002 7 23 GTIA020586 1 20020512 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND EMERGENCY LIGHTS INOPERATIVE AT COCKPIT CAPTAINS SIDE, FORWARD ENTRANCE (TWO EACH), LEFT AND RIGHT, STATION 7213 BETWEEN GALLEY AND LAVATORY, FORWARD. REMOVED BATTERY PACKS AT FS 211 CTR BS-23. INSTALLED SERVICEABLE BATTERY PA CKS IN B5-23. (M) 2 L 7 2 4F A6WE 2002072300166 20020723 00166 WP 2002 7 23 GTIA020587 1 20020407 A 7110 STIFFENER DOUG DC9 DC982 3022082 WP NR 1 COWLING CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND NR 1 ENGINE UPPER COWL AFT STIFFENER CHAFED. REMOVED DAMAGE. REPAIRED DAMAGED AREA, SPIRIT AIRLINES EA 541 0-0202. (M) 2 L 7 2 4F A6WE 2002072300167 20020723 00167 WP 2002 7 23 GTIA020588 1 20020422 A 5753 SKIN DOUG DC9 DC982 3022082 WP FLAP VANE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND RIGHT WING NR 5 FLAP VANE DENTED 2 PLACES ON UPPER SURFACE. REPAIRED BOTH DENTS ON UPPER SURFACE OF VANE PE R SPIRIT AIRLINES EA 5750-0205. (M) 2 L 7 2 4F A6WE 2002072300168 20020723 00168 WP 2002 7 23 GTIA020589 1 20020422 A 5753 SKIN DOUG DC9 DC982 3022082 WP FLAP VANE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND RIGHT WING, NR 2 FLAP VANE HAS SEVERAL DENTS ON UPPER AND LOWER SURFACE. REPAIRED DAMAGE PER SPIRIT AIRLINE S EA 5750-0205. (M) 2 L 7 2 4F A6WE 2002072300170 20020723 00170 NM 2002 7 23 UPS02238786 1 20020621 A 5230 HINGE BOEING 727 72722C 138400F NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI SEVERAL MAIN HINGES CORRODED ON MAIN CARGO DOOR. HINGES REPLACED IAW OHM 20-50-01. 2 L 7 3 4F A3WE 2002072300171 20020723 00171 NM 2002 7 23 UPS02238788 1 20020620 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CORROSION ON TOP OF FLOORBEAM BS 540 LBL12. REPAIRED IAW SRM 53-10-8 FIGURE 5 2 L 7 3 4F A3WE 2002072300172 20020723 00172 NE 2002 7 23 KBMA117647 2 20020701 A 7532 9550164960 BLEED VALVE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE STICKING E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 345SH 922 3345 BLEED VALVE WAS STICKING. REPLACED WITH SERVICEABLE VALVE. 1 G 7 1 3U 3 U H9EU E19EU 2002072300173 20020723 00173 NM 2002 7 23 UPS02238789 1 20020620 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CORROSION ON TOP OF FLOOR BEAM BS 560 LBL 40. REPAIR CARRIED OUT IAW SRM 53-10-08 FIGURE 5 2 L 7 3 4F A3WE 2002072300174 20020723 00174 SW 2002 7 23 KBMA117648 1 20020701 A 6320 2060315903 SUPPORT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TRANSMISSION WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 73DP 12456 2513 TRANSMISSION MOUNT MAKES CLICKING SOUND. RIGHT SIDE, BEARING WAS WORN BEYOND LIMITS. REPLACED WITH NEW SUPPORT AND BEA RING. 1 G 7 1 3U 3 U H2SW E4CE 2002072300175 20020723 00175 NM 2002 7 23 UPS02238790 1 20020620 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CORROSION ON UNDER SIDE OF FLOORBEAM TOP CAP BS 560 LBL12. REPAIRED IAW SRM 53-10-8 FIGURE 5 . 2 L 7 3 4F A3WE 2002072300176 20020723 00176 EU 2002 7 23 KBMA117650 1 20020701 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 345SH 706 3345 BEARINGS ARE WORN. REMOVED AND REPLACED WITH NEW BEARINGS. 1 G 7 1 3U 3 U H9EU E19EU 2002072300177 20020723 00177 NM 2002 7 23 UPS02238791 1 20020618 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CORROSION ON FLOORBEAM LOWER CHORD BS 1030 LBL 52. REPAIRED IAW BOEING INSTRUCTIONS SRV-SNN-02-001 12H AND 00132H B727-53-20058 2 L 7 3 4F A3WE 2002072300178 20020723 00178 NE 2002 7 23 KBMA117651 2 20020701 A 7250 BLADE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE 1ST STAGE WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 345SH 1518 3345 1ST STAGE TURBINE BLADES, ALL WORN UNEVENLY AT THE TRAILING SIDE OF THE BLADE TIPS. INSTALLED RENTAL ENGINE. 1 G 7 1 3U 3 U H9EU E19EU 2002072300179 20020723 00179 EU 2002 7 23 KBMA117654 1 20020706 A 2150 0500521 MOTOR SNIAS 350 AS350BA 8680817 EU FWD EVAPORATOR INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 2273A 2273 FORWARD EVAPORATOR, INOPERATIVE. REPLACED WITH NEW MOTOR. 1 G 7 1 3U NC H9EU 2002072300180 20020723 00180 CE 2002 7 23 MHJ2002F00004 1 20020709 A 2820 65050911 TRANSFER PUMP CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO TIP TANK INOPERATIVE E MHJA K NONE O OTHER IN INSP/MAINT 1 SW 05 3959C 402B0834 THESE PUMPS ARE A CONTINUAL PROBLEM WITH MFG. IN THIS CASE BOTH PUMPS WERE INOPERATIVE. SOMETHING NEEDS TO BE DONE DIF FERENT. 1 L 7 2 3O 3 O A7CE E8CE 2002072300181 20020723 00181 NM 2002 7 23 UPS02238798 1 20020618 A 5711 65185373 SPAR BOEING 727 72722C 138400F NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI DURING INSPECTIONS OF THE WING CENTER SECTION AFT SPAR AREA AIR CON, TWO FASTENERS FOUND POPPED ON THE WING CENTER SECTION REAR SPAR LOWER CHORD VERTICAL FLANGE AT BS 870 LBL38. NDT CONFIRMS CORROSION PRESENCE. REAR S PAR CHORD AND ASSOCIATED STRUCTURE REMOVED. LWR CHORD REPLACED IAW DWG 65-16202 AND DWG 65C21566. 2 L 7 3 4F A3WE 2002072300183 20020723 00183 NM 2002 7 23 UPS02238799 1 20020614 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI SUSPECT CORROSION BETWEEN SKIN AND DOUBLER AT BS 1080 TO BS 1110 STR 11RT TO STR 13 RT. AREA OPENE D UP IAW SRM 51-10-1, FOUND CORROSION BS1080-1100 AND AROUND SKIN CUTOUT TOP AFT CORNER WINDOW AT BS 1090 BETWEEN STRING ERS 11 AND 13 RT. FOUND OUTSIDE LIMITS REPAIRED IAW SRV-SNN-02-00109H AND 00129H AND UPS AUTHORIZATION 727-53-20061 2 L 7 3 4F A3WE 2002072300184 20020723 00184 NM 2002 7 23 UPS02238800 1 20020614 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CORROSION ON FLOORBEAM AT BS 480 AT RBL 27.39. CORRODED FLANGES CUTOUT AT STA 480 RBL 27-31 AS COR ROSION NOT ALLOWED AND AT RBL 35-39 IAW SRM 53-10-8. FLOORBEAM REPAIR IAW SRM 53-10-8 FIGURE 5. 2 L 7 3 4F A3WE 2002072300185 20020723 00185 NM 2002 7 23 UPS02238801 1 20020612 A 3220 CAP BOEING 727 72722C 138400F NM NLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI NOSE LANDING GEAR LT TRUNNION CAPS CORRODED. TRUNNION CAPS REWORKED IAW SRM 53-40-01. FLUORESCENT PENETRANT INSPECTION COMPLIED WITH NDF. NEW BEARINGS FABRICATED IAW SOPM AND OHM. 2 L 7 3 4F A3WE 2002072300186 20020723 00186 NM 2002 7 23 UPS02238802 1 20020610 A 5320 65163394 CASTING BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI NLG FWD WHEEL WELL BS 227, BULKHEAD FITTING FOR NLG DOOR OPERATION CORRODED AT OUTBOARD UPPER SURFA CE, ATTACHES TO RADIUS ROD. CASTING REMOVED IAW SRM 51-30-02, NEW CASTING INSTALLED IAW DWG 65-1 6306 AND SRM 51-30-02. 2 L 7 3 4F A3WE 2002072300187 20020723 00187 NM 2002 7 23 UPS02238805 1 20020613 A 5210 DOOR FRAME BOEING 727 72722C 138400F NM ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI 1 INCH CRACK FOUND ON FWD DOOR AFT FRAME AT LOWER LATCH ROLLER TORQUE SHAFT CUTOUT. CRACKING STOP DRILLED PREVIOUSLY. DOOR FRAME REPAIRED IAW BOEING INSTRUCTION SRV-SNN-02-00135H 00100H. 2 L 7 3 4F A3WE 2002072300188 20020723 00188 NM 2002 7 23 UPS02238807 1 20020607 A 5210 6516479 GATE BOEING 727 72722C 138400F NM ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI FWD ENTRY DOOR GATE STOP LUG CRACKED ON UPPER GATE. GATE REMOVED IAW MM 52-11-01, GATE REPLACED IA W MM52-11-01 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2002072300189 20020723 00189 NM 2002 7 23 UPS02238808 1 20020614 A 3232 652163715 SUPPORT FITTING BOEING 727 72722C 138400F NM LT MLG DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI LT WING LANDING GEAR DOOR ACTUATOR SUPPORT FITTING HAS EVIDENCE OF CORROSION. CORROSION FOUND TO B E OUT OF LIMITS, OLD FITTING WAS REMOVED AND NEW FITTING INSTALLED IAW UPS EO B727-3210-2583 APP D,E,F,G. 2 L 7 3 4F A3WE 2002072300190 20020723 00190 NM 2002 7 23 UPS02238811 1 20020615 A 5230 BRACKET BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI AFT CARGO DOOR HAS SUSPECT CRACKS AT FWD END AFT HINGE ATTACH POINTS FRAME ANGLES. CRACKED BRACKET S REMOVED IAW SRM 51-30-2, TWO NEW BRACKETS FABRICATED IAW SRM 51-20-1 F7. TWO NEW BRACKETS INSTALLED IAW DWG NR 65-186 25 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2002072300191 20020723 00191 NM 2002 7 23 UPS02238813 1 20020620 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI LIGHT SURFACE CORROSION FOUND ON TOP CAP OF FLOORBEAM AT BS 344 BETWEEN LBL 4 TO RBL 30. CORROSION BLENDED BETWEEN LBL 4 AND RBL 30, FOUND TO BE OUTSIDE LIMITS. REPLACED TOP CAP OF FLOORBEAM AT BS 344 IAW DWG 65-16316 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2002072300192 20020723 00192 EA 2002 7 23 COMA0260444 1 20020719 A 5414 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 959CA 7116 WEB AND CHANNEL IN THE R/H MLG BAY @ F.S. 50.45 WERE INADVERTANTLY DAMAGED DURING GEAR RETRACTION.TRIMMED OUT DAMAGED WE B SKIN AND REPROFILED THE CHANNEL LIP. EDDY CURRENT INSPECTION WAS PERFORMED TO ENSURE CHANNEL INTEGRITY, FILLER AND REP AIR DOUBLER WERE FABRICATED FROM 2024-T3" 0.063" P/O #22808/1. REPAIR ANGLE WAS FABRICATED FROM S6144-13 PREFORMED ANGLE AND 2 EA REAPAIR STRAPS WERE FABRICATED FROM 2024-T3 0.032" P/O #18715/1. REPAIR PARTS WERE INSTALLED "WET" USING PR 14 22 B SEALANT AND PROTECTIVE FINISH WAS RESTORED. WORK WAS PERFORMED I/A/W WVAC E.O. 601R-53-3378 APPROVED BY 8110-3 DATE D 07/19/2002. REF COMAIR W/O 29978, MX LOG PAGE 520538 AND WVAC C/O 7116902. 2 L 7 2 4F RT A21EA 2002072300193 20020723 00193 NM 2002 7 23 UPS02238825 1 20020612 A 5314 KEELBEAM BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CRACK FOUND ON KEELBEAM WEB FWD OF APU CUTOUT IN RIGHT HAND WHEEL WELL. KEEL BEAM REPAIRED IAW SRM ADDENDUM EO B727-5330-1995. 2 L 7 3 4F A3WE 2002072300194 20020723 00194 NM 2002 7 23 UPS02238832 1 20020615 A 5320 SILL BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI LT SLIDING WINDOW SILL CHORD CORRODED BETWEEN BS236 AND 244L. REMOVED SLIDING WINDOW IAW 56-12-11, REMOVED CHORD IAW DWG 5-71775 A ND SRM 51-30-02, NEW CHORD FABRICATED IAW SRM 51-20-1 FIG 7, CHORD INSTALLED IAW DWG 5- 71775 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2002072300199 20020723 00199 NM 2002 7 23 2002UALA01001 1 20020613 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 939UA 26672 STATION 188 FRAME CORD IS CRACKED AT STRINGER 17L WL207. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072300200 20020723 00200 NM 2002 7 23 2002UALA01002 1 20020613 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 CRACK IN INBOARD RADIUS OF FORWARD GALLEY DOOR CUTOUT, FORWARD FRAME JUST ABOVE STRINGER 17R. MAJOR REPAIR ACCOMPLISHED INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072300201 20020723 00201 NM 2002 7 23 2002UALA01003 1 20020613 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 LEFT HAND BODY STATION 188 FRAME CHORD CRACKED VERTICALLY CENTER WL APPROXIMATELY 207 TO 208 BELOW STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072300202 20020723 00202 NM 2002 7 23 2002UALA01004 1 20020614 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 MID CABIN STRINGER CLIP IS CRACKED AT STATION 706 STRINGER 11L. MAJOR REPAIR ACCOMPLISHED, REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072300203 20020723 00203 NM 2002 7 23 2002UALA01005 1 20020614 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 FUSELAGE INTERCOSTAL TO EXTERIOR FUSELAGE SKIN ATTACH ANGLE CRACKED BELOW FASTENER AT BODY STATION 291 STRINGER 10R INSI DE CABIN. MAJOR REPAIR ACCOMPLISHED, REPLACED ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072300204 20020723 00204 NM 2002 7 23 2002UALA01006 1 20020615 A 5320 SILL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 LEFT HAND AFT ENTRY DOOR LOWER SILL ANGLE HAS CORROSION AT NUTPLATES. MAJOR REPAIR ACCOMPLISHED, CREASE BEAM WEB REPLAC EMENT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072300205 20020723 00205 NM 2002 7 23 2002UALA01007 1 20020616 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 FORWARD CABIN FRAME CRACKED STATION 400 STRINGER 9L AT RIVET HOLE. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072300206 20020723 00206 NM 2002 7 23 2002UALA01008 1 20020616 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 FORWARD ENTRY DOOR CUTOUT WEB CRACKED AT BODY STATION 294 STRINGER 12L. MAJOR REPAIR ACCOMPLISHED, INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072300207 20020723 00207 NM 2002 7 23 2002UALA01009 1 20020616 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 STATION 927 TO 1000 CABIN FLOOR RIGHT HAND INNER CREASE BEAM CHORD IS CORRODED. MAJOR REPAIR ACCOMPLISHED, CREASE BEAM REPLACEMENT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072300208 20020723 00208 2002 7 23 OZIA200243004 4 20020507 A 3140 7013348936 DAU DORNER DO32 DO328300 NM FAILED A OZIA K NONE J WARNING INDICATION DE DESCENT 1 CE 05 430Z 2346 3127 Multiple CAS miscompares--FWC, Misc CPCS10XX, Misc Fuel, Misc Engine. 2 H 7 2 4T RT A55NM 2002072300209 20020723 00209 NM 2002 7 23 OZIA200243006 1 20020615 A 3242 ACM31356 SPEED SWITCH DORNER DO32 DO328300 NM SEIZED A OZIA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 CE 05 430Z 5052 3127 On landing roll out norm anti-skid and alt anti-skid degrade CAS message, OB LH MLG tire flat spotted. 2 H 7 2 4T RT A55NM 2002072300210 20020723 00210 NM 2002 7 23 2002UALA01011 1 20020615 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 CABIN FLOORBEAM STATION 365, STRINGER 17R UPPER SURFACE OF UPPER I BEAM FLANGE HAD EXCESS MATERIAL REMOVED DURING CORROS ION CLEANUP BETWEEN RBL 4 OUT TO RBL 60. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIRED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072300211 20020723 00211 NM 2002 7 23 2002UALA01013 1 20020616 A 5320 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 AFT CABIN DECK PLATE REPAIR DOUBLER CORRODED AT STATION 1680 TO 1685, RBL 50 TO 55. MAJOR REPAIR ACCOMPLISHED. REMOVE D OUBLER AND NEW DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072300212 20020723 00212 NM 2002 7 23 2002UALA01014 1 20020615 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 CABIN FLOORBEAM STATION 1640, RBL15-53R, WL208 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072300213 20020723 00213 NM 2002 7 23 2002UALA01015 1 20020615 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 CABIN FLOOR CREASE BEAM AT STATION 410, LBL 72, WL 208 CORRODED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072300214 20020723 00214 NM 2002 7 23 2002UALA01016 1 20020615 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 AFT FUSE STATION 1830 AT STRINGER 20R WAS PUNCTURED. STRINGER 20R WAS ALSO CRACKED. MAJOR REPAIR ACCOMPLISHED. FUSELA GE SKIN DOUBLER INSTALLED. STRINGER SPLICED WAS INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072300215 20020723 00215 NM 2002 7 23 SABA020072 1 20020718 A 3231 864202 WIRE DHAV DHC8 DHC8103 1386005 NM A SABA O OTHER O OTHER CL CLIMB 1 SO 33 801WP 086 Aircraft 801 on flight 5028 from TLH to CLT, During take-off and climb out the gear had to be cycled several times to ge tthe left gear door to close. With the gear door closed, aircraft continued and landed in Charlotte with no other proble ms. No emergency was declared. Maintenance found a broken wire on the foward door sensor. Wire was reparied, retraction check completed. Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002072300216 20020723 00216 WP 2002 7 23 MWEA020455 1 20020723 A 5312 49125151 CLIP DOUG DC9 DC914 3022034 WP LH 17L GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 SHOVEL CLIP JUST AFT OF APB LEFT 17 LONGERON IS GOUGED. -- REPAIRED GOUGE AND INSTALLED SHOVEL CLIP. 2 L 7 2 4F A6WE 2002072300217 20020723 00217 WP 2002 7 23 MWEA020456 1 20020723 A 5230 99576643 INTERCOSTAL DOUG DC9 DC914 3022034 WP FWD CARGO DR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 INTERCOSTAL IS CRACKED AROUND FASTENER HOLES FORWARD CARGO DOOR BELOW #1 BEAM FORWARD END OF DOOR (DOT JH 23). -- REMO VED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2002072300218 20020723 00218 NM 2002 7 23 801DM0006 1 20020710 A 2560 BATTERY BOEING 757 757200 1384950 NM A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 801DM 26240 Cockpit bulkhead mounted left and right side emergency flashlights inop. Removed and replaced emergency flashlight batt eries IAW MM 25-10-00. Ops. ck. was good. 2 L 7 2 4F RT A2NM 2002072300219 20020723 00219 NM 2002 7 23 AWXA200200647 1 20020701 A 5415 65C2670128 ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1" CRACK WAS FOUND ON THE #2 PYLON ATTACH ANGLE AT THE FRONT SPAR LOWER CHORD A REA, NACELLE STA 254. MAINTENANCE TRIMMED OUT CRACKED SECTION OF ANGLE, FABRICATED A NEW REPAIR SECTION ANGLE, AND INSTA LLED REPAIR IAW AWA ER 03-5711-02191-SS3. 2 L 7 2 4F RT A16WE 2002072300220 20020723 00220 NM 2002 7 23 AWXA200200648 1 20020701 A 5330 65C3579415 SKIN BOEING 737 7373G7 1384595 NM SCRATCHED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A 3" SCRATCH WAS FOUND ON EXTERNAL SKIN AT BS 727, BETWEEN STR 21 & 22 L/H. MAINT ENANCE BLENDED OUT SCRATCH, MATERIAL LOSS OUT OF LIMITS PER B737-300 SRM 53-00-01, PG. 101-104. CUTOUT DAMAGED AREA OF S KIN; FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-00-01, PG. 104-106, AND SRM 51-40-02, PG. 3. 2 L 7 2 4F RT A16WE 2002072300221 20020723 00221 NM 2002 7 23 AWXA200200649 1 20020701 A 5311 654580734 ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/2" CRACK WAS FOUND ON THE FRAME SUPPORT ANGLE OF THE R1 DOOR, BS 291.5, ABOVE STR 8 R/H. MAINTENANCE REMOVED CRACKED FRAME SUPPORT ANGLE AT BS 291.5, ABOVE STR 8 R/H. FABRICATED A NEW ANGLE AND INS TALLED REPAIR IAW B737-300 SRM 51-40-02, PG. 3-4, & 38. 2 L 7 2 4F RT A16WE 2002072300222 20020723 00222 NM 2002 7 23 AWXA200200650 1 20020701 A 5311 654580731 ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/2" CRACK WAS FOUND ON THE FRAME SUPPORT ANGLE OF THE R1 DOOR, BS 291.5, ABOVE STR 10 R/H. MAINTENANCE REMOVED CRACKED FRAME SUPPORT ANGLE AT BS 291.5, ABOVE STR 10 R/H. FABRICATED A NEW ANGLE AND I NSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG. 3-4, & 38. 2 L 7 2 4F RT A16WE 2002072300223 20020723 00223 NM 2002 7 23 AWXA200200651 1 20020701 A 5311 654580769 ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/2" CRACK WAS FOUND ON THE FRAME SUPPORT ANGLE OF THE R1 DOOR, BS 291.5, ABOVE STR 13 R/H. MAINTENANCE REMOVED CRACKED FRAME SUPPORT ANGLE AT BS 291.5, ABOVE STR 13 R/H. FABRICATED A NEW ANGLE AND I NSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG. 3-4, & 38. 2 L 7 2 4F RT A16WE 2002072300224 20020723 00224 NM 2002 7 23 AWXA200200652 1 20020701 A 5311 654580730 ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/2" CRACK WAS FOUND ON THE FRAME SUPPORT ANGLE OF THE R1 DOOR, BS 291.5, ABOVE STR 12 R/H. MAINTENANCE REMOVED CRACKED FRAME SUPPORT ANGLE AT BS 291.5, ABOVE STR 12 R/H. FABRICATED A NEW ANGLE AND I NSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG. 3-4, & 38. 2 L 7 2 4F RT A16WE 2002072300225 20020723 00225 NM 2002 7 23 AWXA200200655 1 20020620 A 5330 654577710 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 0 0 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 3/8" CRACK WAS FOUND ON EXTERNAL SKIN, INTERNAL DOUBLER, AND STRAP AT L2 DOOR FORWARD LOWER CUTOUT BS 950, STR 17 L/H. HFEC & 10X VISUAL CONFIRMED. MAINTENANCE STOP DRILLED CRACK ON SKIN, INTERNAL DOUBLER, AND STRAP AT L2 DOOR FORWARD LOWER CUTOUT BS 950, STR 17 L/H, PERFORMED A HFEC INSPECTION TO VERIFY CRACK IS CO NTAINED. FABRICATED 3 EACH REPAIR DOUBLERS AND TAPERED SHIMS, INSTALLED RIVET IN STOP DRILL HOLE, AND INSTALLED REPAIR P ARTS IAW AWA ER 03-5300-02196-TB3. 2 L 7 2 4F RT A16WE 2002072300226 20020723 00226 NM 2002 7 23 AWXA200200656 1 20020629 A 5311 69719478 FRAME BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A CRACK WAS FOUND ON THE FIRST OFFICERS WINDSHIELD FRAME AT THE UPPER OUTBOARD CO RNER. MAINTENANCE CUTOUT CRACK IN FRAME THAT REVEALED A 3/8" CRACK IN GUSSET, CUT DAMAGED AREA OF GUSSET AND PERFORMED A HFEC INSPECTION ON BOTH CUTOUTS. FABRICATED A DOUBLER AND FILLER AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01, PG. 231-234. 2 L 7 2 4F RT A16WE 2002072300227 20020723 00227 NM 2002 7 23 ABA020073 1 20020717 A 3260 SENSOR DHAV DHC8 DHC8103 1386005 NM A SABA O OTHER J WARNING INDICATION CR CRUISE 1 SO 33 882CC 168 Aircraft 882on flight 5028 from TLH to CLT : Aircraft was inbound to Charlotte and at cruse altitude. The weight on whee ls switch light illuminated. No emergency was declared. Aircraft landedc at Charlotte with no other problems. Maintenanc e troubleshot the system to the right inboard sensor. Cleaned the sensor switch and repositioned wire bundle. System ops checked good and aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002082000142 20020820 00142 NM 2002 8 20 SABA020073 1 20020717 A 3260 SWITCH DHAV DHC8 DHC8103 1386005 NM RT MLG DIRTY A SABA O OTHER N FALSE WARNING CR CRUISE 1 SO 33 882CC 168 AIRCRAFT 882 ON FLIGHT 5028 FROM TLH TO CLT: AIRCRAFT WAS INBOUND TO CHARLOTTE AND AT CRUISE ALTITUDE. THE WEIGHT ON W HEELS SWITCH LIGHT ILLUMINATED. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED AT CHARLOTTE WITH NO OTHER PROBLEMS. MAINT ENANCE TROUBLESHOT THE SYSTEM, TO THE RIGHT INBOARD SENSOR, CLEANED SENSOR SWITCH AND REPOSITIONED WIRE BUNDLE. SYSTEM OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072300228 20020723 00228 SO 2002 7 23 C2XA02SH025 1 20020710 A 5300 14521721009 BUTT STRAP EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 SHV - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND 18. MAINTENANCE RE MOVED THA DAMAGED SECTIONS OF BUTTSTRAP, AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB-145 SRM 53-21-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002072300229 20020723 00229 SO 2002 7 23 C2XA02SH026 1 20020710 A 5300 14526437001 BUTT STRAP EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 SHV - DURING C-CHECK INSPECTION, THE LEFT, CENTER, AND RIGHT HAND BUTT STRAPS WERE FOUND TO BE CORRODED. MAINTENANCE REM OVED AND REPLACED THE AFFECTED SECTIONS OF BUTT STRAPS IN ACCORDANCE WITH EMB-145 SRM 51-40-02, AND THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002072300230 20020723 00230 SO 2002 7 23 C2XA02SH027 1 20020710 A 5300 14521725013 CREASE BEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 SHV - DURING C-CHECK INSPECTION, THE RIGHT HAND O/B CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 17 AND 19. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF CREASE BEAM IN ACCORDANCE WITH EMB-145 SRM 51-40-02, AND THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002072400001 20020724 00001 SO 2002 7 24 C2XA02SH028 1 20020710 A 5300 14521725015 CREASE BEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 SHV-DURING C-CHECK INSPECTION.THE RIGHT HAND O/B CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 21 AND 22.MAINTENAN CE REMOVED AND REPLACED THE AFFECTED SECTION OF CREASE BEAM IN ACCORDANCE WITH EMB-145 SRM 51-40-02,AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002072400007 20020724 00007 EU 2002 7 24 DNW2002F00000 1 20020709 A 2913 S40 COUPLING SNIAS 350 AS350D 8680803 EU ALLSN 250C 250C30 03013 GL HYD PUMP WORN E DNWA K NONE O OTHER IN INSP/MAINT 1 WP 13 90Q 6565 2324 CAE897506 SPLINES ON DRIVE COUPLING WORN, SPLINED ON PUMP SHOW SIGNS OF MINOR WEAR DIFFICULT TO SEE INSIDE DRIVE COUPLING AT DEGRE ASE. 1 G 7 1 3U 3 U H9EU E1GL 2002072400008 20020724 00008 CE 2002 7 24 HMG2002F00001 1 20020708 A 5312 00244002377 BULKHEAD BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO FUSELAGE CRACKED E HMGA K NONE O OTHER IN INSP/MAINT 1 SW 15 82LB 6163 TH910 282169R DURING ANNUAL INSPECTION, CRACKS WERE FOUND IN BULKHEAD FS 257.6. 1 L 7 2 3O 3 O 3A16 E5CE 2002072400009 20020724 00009 2002 7 24 MALA020352 4 20020615 A 2340 SPEAKER SAAB SF340 340B 7860101 EU CABIN SHORTED A MALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 416XJ 340B416 ON FLIGHT 3349, F/A NOTED SMOKE FROM ANC SPEAKER, ROW 3 / 4A. FOLLOWED BY AN ELECTRICAL ODOR, F/A SHUT OFF ANC AND ODO R WENT AWAY. MAINTENANCE PERFORMED OPS CHECK OF ANC SYSTEM IAW SF-340 MM 23, NO DEFECTS NOTED. 2 L 7 2 4T RT A52EU 2002072400010 20020724 00010 NE 2002 7 24 MALA020353 2 20020615 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT MALFUNCTIONED A MALA L ABORTED APPROACH R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 GL 15 457XJ 340B457 DURING APPROACH OF FLIGHT 3326, RH ENGINE POWER SURGE. UNCOMMANDED TORQUE POWER SURGES OF 15 PERCENT ON RT ENGINE DURING CRUISE FLIGHT AT 60 PERCENT TORQUE. THIS WAS AN ACTUAL POWER SURGE WITH AN ASSOCIATED YAW. AC LANDED WITHOUT INCIDENT . MAINTENANCE REMOVED AND REPLACED CTOT PANEL. ALSO SHOTGUNNED AT THE TIME WERE: HUM, PCU, PROP OVERSPEED GOV., FWD NP SENSOR, LEFT SIDE OF ENGINE WIRE HARNESS, ALT. AND STATOR. 2 L 7 2 4T 4 T RT A52EU E8NE 2002072400011 20020724 00011 NE 2002 7 24 MALA020354 2 20020616 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 413XJ 340B413 DURING CLIMBOUT ON FLIGHT 2935, RT TORQUE AND RT ITT GAUGE FLICKERING, ABOUT 4-5 PERCENT. ALL OTHER ENGINE AND PROP INDI CATIONS WERE NORMAL. AIR RETURN TO MEM. MAINTENANCE CHECKED FOR SHORTS BETWEEN PINS 16,17 & 18 OF DECU, CLEANED CONNECT OR PLUG. NO DEFECTS NOTED. DID ENGINE RUN AND IT OPERATED WITHIN LIMITS AND NO FLUCTUATION NOTED. REF 409 049821. 2 L 7 2 4T 4 T RT A52EU E8NE 2002072400012 20020724 00012 2002 7 24 MALA020356 4 20020618 A 3425 6226190113 COMPUTER SAAB SF340 SF340A 7850100 EU AHRS FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 115XJ DURING FLIGHT 2767, ALTITUDE AND HEADING RED FLAGGED ON F/O'S SIDE. USED X-SIDE DATA AS PER QRH. AIR RETURN TO SUX. M AINTENANCE INSPECTED AC AND FOUND SAFE FOR ONE TIME FERRY FLIGHT FROM SUX TO MSP FOR INTERMITTANT F/O'S AHARS. MSP MAIN TENANCE REMOVED AND REPLACED NR 2 AHRS COMPUTER PN 622-6190-113 SN/ON 2950 SN/OFF 2940, NR 2 AHRS OPS CHECKS GOOD IAW S F340MM CHAP 34. 2 L 7 2 4T RT A52EU 2002072400013 20020724 00013 EU 2002 7 24 MALA020358 1 20020619 A 2121 FAN BAC 146 AVRO146RJ85A 1500097 EU CABIN FAILED A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 507XJ E2316 BEFORE FLIGHT 3576, CABIN FAN QUIT WORKING. F/A SAID AN ELECTRICAL ODOR WAS PRESENT, RETURN TO GATE TO MAKE SURE NO FUR THER PROBLEMS. MAINTENANCE FOUND ELECTRIAL ODOR WAS RELATED TO CABIN FAN THAT FAILED. NO FURTHER INFORMATION IS AVAILA BLE.REPLACED CABIN FAN. 2 H 7 4 4F RT A49EU 2002072400014 20020724 00014 EU 2002 7 24 MALA020359 1 20020620 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 099 099 EMERGENCY LIGHTING SYSTEM INOP - R&R BATTERY SUPPLY AND BATTERY PACKS. 2 L 7 2 4T RT A52EU 2002072400015 20020724 00015 EU 2002 7 24 MALA020360 1 20020620 A 2120 ODOR SAAB SF340 340B 7860101 EU CABIN DETECTED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 424XJ 340B424 ENROUTE TO OMA RT AC SYSTEM BLOWING AN OILY ODOR INTO CABIN - COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4T RT A52EU 2002072400016 20020724 00016 EU 2002 7 24 MALA020361 1 20020620 A 3230 CONTROL VALVE SAAB SF340 SF340A 7850100 EU MLG MALFUNCTIONED A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 099XJ 099 WHEN SELECTING GEAR DOWN DID NOT GET 3 GREEN LIGHTS, RESET LANDING GEAR CONTROL CB AND GOT 3 GREEN. R&R LANDING GEAR CO NTROL VALVE IAW AMM32, PERFORMED GEAR SWING AND LEAK CHECKS. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002072400017 20020724 00017 EU 2002 7 24 MALA020362 1 20020624 A 3230 CONNECTOR SAAB SF340 340B 7860101 EU MLG DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 340B406 FOUND RT SEPARATION BOLT CONNCETOR PLUG BAD. REMOVED AND REPLACED CONNECTOR PLUG. 2 L 7 2 4T RT A52EU 2002072400018 20020724 00018 EU 2002 7 24 MALA020363 1 20020625 A 3230 WIRE SAAB SF340 340B 7860101 EU CONNECTOR PLUG BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 442XJ 340B442 FOUND BROKEN WIRE AND CONNCETOR PLUG BAD ON SEPARATION BOLT. REPAIRED WIRE AND REPLACED CONNECTOR PLUG. 2 L 7 2 4T RT A52EU 2002072400019 20020724 00019 2002 7 24 MALA020364 4 20020625 A 3442 CONNECTOR SAAB SF340 340B 7860101 EU WX RADAR SYS DIRTY A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 427XJ 340B427 WEATHER RADAR FAILED DURING CRUISE. PAINTED STRAIGHT LINES ON RT SWEEP, NOTHING ON LT SWEEP. CLEANED CONNECTOR PLUG AT RX/TX AND AT WAVEGUIDE. PERFORMED TEST PER AMM 32-42-00. TEST PASSES. 2 L 7 2 4T RT A52EU 2002072400020 20020724 00020 EU 2002 7 24 MALA020365 1 20020625 A 2913 PUMP SAAB SF340 SF340A 7850100 EU HYD SYSTEM LEAKING A MALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 048XJ 048XJ LOST HYDRAULIC PRESSURE ON TAXI OUT. HYDRAULIC CAUTION LIGHT CAME ON ON CWP. TRIED OVERRIDE, PUMP DID NOT COME ON THE MA IN, ACCUMULATORS DRAINED DOWN TO RED LINE. REPLACED HYDRAULIC PUMP. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002072400021 20020724 00021 EU 2002 7 24 MALA020366 1 20020626 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT FALSE INDICATION A MALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 407XJ 340B407 CONFIGURATION WARNING LIGHT ILLUMINATED ON TAKEOFF AROUND 90 KTS.COMPLETED CONFIGURATION WARNING TEST, TEST OK PER 31-50 -00. 2 L 7 2 4T RT A52EU 2002072400022 20020724 00022 EU 2002 7 24 MALA020367 1 20020626 A 2121 FAN SAAB SF340 340B 7860101 EU AVIONICS BAY FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 443XJ 340B443 AVIONICS VENT LIGHT ON CWP. REPLACED AVIONICS VENT FAN. 2 L 7 2 4T RT A52EU 2002072400023 20020724 00023 EU 2002 7 24 MALA020368 1 20020627 A 2910 ISOLATION VALVE BAC 146 AVRO146RJ85A 1500097 EU HYD SYSTEM FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 506XJ E2314 ON CLIMBOUT FROM DTW YELLOW HYDRAULIC HI TEMP LIGHT ILLUMINATED. YELLOW PSI & QTY WERE NORMAL. LIGHT EXTINGUISHED AFTER RAN QRH.R&R HYDRAULIC ISOLATION VALVE 1MC3. RAN A/C FOR 45 MINS. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2002072400024 20020724 00024 NE 2002 7 24 MALA020369 2 20020627 A 7320 HMU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE FAILED A MALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 991XJ 340A091 LT ENGINE OVERTEMP. HIGH ENERGY ABORT. MAX WAS 936. NO OVERTEMP LIGHT ILLUMINATED. REPLACED LT HMU AND T4.5 TRIMMER ADJ USTED, GPA CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002072400025 20020724 00025 EU 2002 7 24 MALA020370 1 20020628 A 3150 WARNING SYSTEM SAAB SF340 340B 7860101 EU RT ENGINE ACTIVATED A MALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 412XJ 340B412 ABORTED TAKEOFF DUE TO RT TORQUE INDICATION. RESET CIRCUIT BREAKER. 2 L 7 2 4T RT A52EU 2002072400026 20020724 00026 EU 2002 7 24 MALA020371 1 20020629 A 7603 LOCK SAAB SF340 SF340A 7850100 EU THROTTLE MALFUNCTIONED A MALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 109XJ 340A109 CONFIG LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF, NOT HIGH ENERGY ABORT. CLEANED FRICTION LOCKS, ALL CHECK S GOOD. 2 L 7 2 4T RT A52EU 2002072400027 20020724 00027 EU 2002 7 24 MALA020372 1 20020629 A 2497 CONNECTOR SAAB SF340 SF340A 7850100 EU F/A PANEL ARCED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 110XJ 340A110 FLIGHT ATTENDANT REPORTED SPARKS BEHIND FA PANEL. MX FOUND CONNECTOR PLUG ARCING TO SWITCHES. WRAPPED CONNECTOR PLUG WI TH COMPRESSION TAPE. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002072400028 20020724 00028 EU 2002 7 24 MALA020373 1 20020629 A 3150 WARNING LIGHT SAAB SF340 SF340A 7850100 EU COCKPIT ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 142XJ 142XJ RT DUCT TEMP LIGHT ILLUMINATED IN FLIGHT. AIR TURNBACK TO DTW.R&R PRSOV. 2 L 7 2 4T RT A52EU 2002072400029 20020724 00029 EU 2002 7 24 MALA020374 1 20020630 A 5410 CAMLOCK SAAB SF340 SF340A 7850100 EU RT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 119XJ 340A119 RT OUTBOARD NACELLE AT FIG 8 CAMLOCK HAS HOLE AND CRACKS.REPAIRED IAW EO 54058. 2 L 7 2 4T RT A52EU 2002072400030 20020724 00030 EU 2002 7 24 MALA020375 1 20020630 A 5320 STRUCTURE SAAB SF340 SF340A 7850100 EU GALLEY AREA CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 119XJ 340A119 CORROSION FOUND IN FWD RT GALLEY AREA UNDER PANEL 122AZ. REMOVED IAW SRM 53-70-40. 2 L 7 2 4T RT A52EU 2002072400031 20020724 00031 EU 2002 7 24 MALA020376 1 20020630 A 5347 GALLEY TRACK SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 119XJ 340A119 RT I/B GALLEY SEAT TRACK HAS LIGHT CORROSION. REMOVED CORROSION IAW SRM 53-70-40. 2 L 7 2 4T RT A52EU 2002072400032 20020724 00032 EU 2002 7 24 MALA020377 1 20020630 A 5347 SEAT TRACK SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 119XJ 340A119 AISLE SEAT TRACK ANGLE FROM STA 339 TO STA 622 HAS LIGHT CORROSION.REMOOVED CORROSION IAW SRM 53-70-60. 2 L 7 2 4T RT A52EU 2002072400033 20020724 00033 EU 2002 7 24 MALA020378 1 20020630 A 5321 FLOOR PANEL SAAB SF340 SF340A 7850100 EU COCKPIT CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 119XJ 340A119 FLIGHT DECK FLOOR HAS LIGHT CORROSION. REMOVED AND TREATED IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002072400034 20020724 00034 EU 2002 7 24 MALA020379 1 20020630 A 5321 FLOOR PANEL SAAB SF340 SF340A 7850100 EU COCKPIT CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 119XJ 340A119 PITTING CORROSION LOCATED ON THE FLOOR, LT SIDE OF CAPTAINS CONTROL COLUMN STA 177 TO STA 185. REMOVED AND REPAIRED DEC K FLOOR IAW 177-185 EO S53124. 2 L 7 2 4T RT A52EU 2002072400035 20020724 00035 EU 2002 7 24 MALA020380 1 20020630 A 1430 FASTENER SAAB SF340 SF340A 7850100 EU COCKPIT FLOOR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 119XJ 340A119 SEVERAL AREAS AROUND FLT DECK FLOOR SNAP FASTENERS HAVE PITTING CORROSION. REMOVED AND TREATED IAW SRM 51-70-40. PERFOR MED REPAIRS IAW SRM 53-60-50. 2 L 7 2 4T RT A52EU 2002072400036 20020724 00036 EU 2002 7 24 MALA020381 1 20020630 A 2720 SHAFT SAAB SF340 SF340A 7850100 EU RUDDER CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 119XJ 340A119 CORROSION FOUND AT RUDDER CONCENTRIC SHAFT ASSY. REMOVED AND REPLACED SHAFT. 2 L 7 2 4T RT A52EU 2002072400037 20020724 00037 EU 2002 7 24 MALA020382 1 20020630 A 5330 SKIN SAAB SF340 SF340A 7850100 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 119XJ 340A119 RT AFT FUSELAGE SKIN CHAFED FROM ELEVATOR CANOE PANEL. REPAIRED SKIN IAW SAAB STATEMENT 340 SDS004056. 2 L 7 2 4T RT A52EU 2002072400038 20020724 00038 EU 2002 7 24 MALA020383 1 20020630 A 5410 FRAME SAAB SF340 SF340A 7850100 EU RT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 119XJ 340A119 RT NACELLE FWD LOWER FRAME AT NS 197.00 CRACKED. R&R FRAME IAW EO S54058. 2 L 7 2 4T RT A52EU 2002072400039 20020724 00039 EU 2002 7 24 MALA020384 1 20020701 A 3233 ACTUATOR SAAB SF340 340B 7860101 EU MLG DAMAGED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 367PX 340B271 ON APPROACH TO YNG RT MLG LIGHT DID COME ON AFTER SELECTING GEAR DOWN/TRANSIT LIGHT STILL ON. FOLLOWED QRH WHEN RECYCLE D THE GEAR UP, THEN DOWN, THE RIGHT GEAR MADE A LARGE CLUNK NOISE. GEAR DOWN W/T 2/3 SECONDS THEN LT AND NLG SHOWED DOWN . ON POST FLIGHT NOTED GEAR DOOR DAMAGE. MAINTENANCE INSPECTED RT GEAR, FOUND RETRACT ACTUATOR BROKE AND MINOR SHEETME TAL DAMAGE TO GEAR DOOR. FERRIED A/C TO DTW FOR REPAIRED. 2 L 7 2 4T RT A52EU 2002072400040 20020724 00040 EU 2002 7 24 MALA020385 1 20020629 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 DENT IN FUSELAGE AFT OF ICE SHIELD ABOVE STRINGER SL1622 RH SIDE.REPAIRED IAW EO S53126. 2 L 7 2 4T RT A52EU 2002072400041 20020724 00041 EU 2002 7 24 MALA020386 1 20020630 A 3610 CONTROL VALVE SAAB SF340 340B 7860101 EU PNEUMATIC SYS MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 425XJ 340B425 SYSTEM INDICATES LT ENGINE BLEED LEAK, QRH CPMPLETED, INDICATION CLEARED WITH HP & LP BLEED VALVES CLOSED. R & R TEMP CO NTROL VALVE AFTER INSTALLING NEW O-RINGS AT DUCTING FLANGES. 2 L 7 2 4T RT A52EU 2002072400042 20020724 00042 EU 2002 7 24 MALA020387 1 20020701 A 2840 INDICATOR SAAB SF340 340B 7860101 EU FUEL FLOW INOPERATIVE A MALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 441XJ 340B441 ABORTED TAKEOFF AT 80 KTS DUE TO RT FUEL FLOW GAUGE READING ZERO. RESET BREAKER, FUEL FLOW INDICATED NORMAL. CND 2 L 7 2 4T RT A52EU 2002072400043 20020724 00043 NE 2002 7 24 MALA020388 2 20020702 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT OVERTEMP A MALA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 GL 15 098XJ 098XJ LT ENGINE ITT WENT TO 930. INSPECTED ENGINE INLET AND FOUND DEBRIS THAT CAUSED BLOCKAGE. FOUND NO DAMAGE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002072400044 20020724 00044 EU 2002 7 24 MALA020389 1 20020703 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 340B420 STA 258 UPPER FLANGE OF BOTTOM FRAME IN CENTER SECTION HAS CORROSION. COMPLETED REPAIR IAW EO S53108. 2 L 7 2 4T RT A52EU 2002072400045 20020724 00045 EU 2002 7 24 MALA020390 1 20020703 A 5320 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 340B420 FRAME 272 HAS LIGHT CORROSION ON TOP ANGLE. R&R'D ANGLE IAW SRM 51. 2 L 7 2 4T RT A52EU 2002072400046 20020724 00046 EU 2002 7 24 MALA020391 1 20020703 A 5320 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 340B420 FRAME BETWEEN STA 272 AND 288 RT OF 0 BL HAS CORROSION ON TOP ANGLE.R&R'D ANGLE IAW SRM 51. 2 L 7 2 4T RT A52EU 2002072400047 20020724 00047 EU 2002 7 24 MALA020392 1 20020703 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 340B420 LT O/B CARGO SEAT TRACK AND ANGLE FROM STA 630.112 TO 686.888 HAS CORROSION. REMOVED CORROSION IAW 51-70-40. 2 L 7 2 4T RT A52EU 2002072400048 20020724 00048 EU 2002 7 24 MALA020396 1 20020613 A 5315 FLOORBEAM BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 513XJ E2329 DURING C-CHECK IN CVG, CORROSION WAS FOUND ON THE FRAME 18 FLOORBEAM BETWEEN SEAT RAILS 3 & 4. MAINTENANCE REPAIRED DAM AGE IAW RIL HC531H9486, BAE APPROVED FAX/BARA/AVR/5950/02-DC AND EO 53086. 2 H 7 4 4F RT A49EU 2002072400049 20020724 00049 NM 2002 7 24 C1HA200295012 1 20020722 A 3350 900835A BATTERY PACK BOEING 727 727290 138408W NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 LH forward overwing emergency exit light inoperative. Removed and replaced LH forward overwing emergency light battery p ack per MM. Operational checks good. 2 L 7 3 4F A3WE 2002072400050 20020724 00050 NM 2002 7 24 2002UALA01020 1 20020616 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 CABIN STATION 825-850, RBL 34, TRANSVERSE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED BEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072400051 20020724 00051 NM 2002 7 24 2002UALA01021 1 20020616 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 AFT PIT T-CAP CORRODED AT BODY STATION 1175, BL 0 TO RBL 40. MAJOR REPAIR ACCOMPLISHED. REPAIRED AND INSTALLED FLOORBE AM T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072400052 20020724 00052 NM 2002 7 24 2002UALA01022 1 20020616 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 AFT PIT T-CAP CORRODED BODY STATION 1285, LBL 40. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072400053 20020724 00053 NM 2002 7 24 2002UALA01023 1 20020616 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 AFT PIT T-CAP CORRODED BODY STATION 1207 AND RBL 40. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072400054 20020724 00054 NM 2002 7 24 2002UALA01024 1 20020617 A 2612 SMOKE WARNING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT FALSE ACTIVATION A UALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 770UA 26925 CARGO FIRE INDICATION, DISCHARGED BOTH BOTTLES. CREW ACTIVATED FIRE EXTINGUISHING SYSTEM AFTER AFT CARGO FIRE INDICATIO N. BOTH DUMP BOTTLES & 3 METERED BOTTLES WERE DISCHARGED. AIRCRAFT DIVERTED SNN. INSPECTION OF CARGO COMPARTMENT REVE ALED NO EVIDENCE OF FIRE. AFT CARGO SMOKE DETECTOR UNIT WAS INSPECTED AND NO DEBRIS OR MOISTURE FOUND IN INLETS OR OUTL ETS. SMOKE DETECTOR WAS REPLACED AND UNIT SENT TO OEM FOR FURTHER TESTING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002072400055 20020724 00055 EU 2002 7 24 MALA020397 1 20020621 A 5315 FLOORBEAM BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 513XJ E2329 DURING C-CHECK IN CVG, CORROSION FOUND ON THE FLOORBEAM AT FRAME 15, 10 INCHES INBOARD FROM THE LT SIDE. MAINTENANCE RE PAIRED DAMAGE INBOARD FROM THE LT SIDE. DAMAGE REPAIRED IAW BAE APPROVED FAX/BARA/AVR/5966/02-DC AND EO A53087. 2 H 7 4 4F RT A49EU 2002072400056 20020724 00056 NM 2002 7 24 2002UALA01025 1 20020615 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 941UA 26676 FUSELAGE HAS .4375 INCH HOLE ABOUT 3 FEET AFT OF FORWARD ENTRY DOOR AND 8 INCHES ABOVE FLOOR LINE. MAJOR REPAIR ACCOMPL ISHED. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400057 20020724 00057 NM 2002 7 24 2002UALA01026 1 20020617 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 FRAME CHORD WEB CRACKED AT STATION 616 LEFT STRINGER 17 LEFT LBL 45. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTA LLED FILLERS, SHIMS AND ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400058 20020724 00058 2002 7 24 MALA020398 4 20020709 A 3442 6227337001 RADAR SAAB SF340 340B 7860101 EU WEATHER UNIT INOPERATIVE A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 427XJ 340B427 DURING FLIGHT 3034, THE RADAR IS INOPERATIVE. PAINTS NORMAL ON A RIGHT TO LEFT SWEEP, ON THE SWEEP LEFT TO RIGHT PAINTS LINES. AIR TURNBACK TO MSP. MAINTENANCE REPLACED WX RADAD R/T PN 622-7337-001, SN/OFF 4748, SN/ON 4663. WX RADAR OPS CHECKS GOOD IAW SF340 MM CHAP 34. 2 L 7 2 4T RT A52EU 2002072400059 20020724 00059 NM 2002 7 24 2002UALA01027 1 20020617 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 AFT PIT SHEAR TIE CRACKED AT STATION 708 BETWEEN STRINGER 27L AND 27R. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INS TALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400060 20020724 00060 EU 2002 7 24 MALA020399 1 20020709 A 1100 PLACARD BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR MISSING A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 514XJ E2330 DURING POST FLIGHT OF FLIGHT 3529, A PIECE OF THE PAX DOOR OUTSIDE EMERGENCY OPENING INSTRUCTIONS IS MISSING. 2 H 7 4 4F RT A49EU 2002072400061 20020724 00061 NM 2002 7 24 2002UALA01028 1 20020617 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 STRINGER 10 LEFT CRACKED AT STATION 297. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECTION OF STRINGER AND STRINGER T IE CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400062 20020724 00062 NM 2002 7 24 2002UALA01029 1 20020618 A 5313 STRINGER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 941UA 26676 FOUND DAMAGE TO STRINGER, 3 FEET AFT OF DOOR 1L 8 INCHES ABOVE FLOOR LINE. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRING ER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400063 20020724 00063 EU 2002 7 24 MALA020400 1 20020710 A 7931 IPTE1191000200 TRANSMITTER SAAB SF340 SF340A 7850100 EU OIL PRESS MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 110XJ 340A110 DURING CRUISE ON FLIGHT 3001, LT ENGINE MASTER WARNING LIGHT FLICKERED TWICE AT CRUISE. CREW NOTED LT PROP OIL PRESSURE DROPPED FROM NORMAL RANGE TO ZERO CAUSING MASTER WARNING LIGHT TO "FLICK" ON/OFF. ENGINE /PROP RAN FINE. LANDED WITHO UT INCIDENT. MAINTENANCE REMOVED AND REPLACED LT PROP OIL PRESS TRANSMITTER IAW MM PN IPTE119-1000-200D1, SN/ON 4181-4- 428/382 SN/OFF 4487-1-38/12. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2002080900027 20020809 00027 NM 2002 8 9 2002UALA01030 1 20020617 A 7797 HAD21986 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE DEFECTIVE A UALA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 774UA 20000 26936 777008 INOPERATIVE EGT INDICATION ON NR 2 ENGINE. REPLACED EGT HARNESS WO635 CHECKED CONTINUITY AND PERFORMED HIGH POWER RUNUP . OPS CHECKED OK. ALUMEL/CHROMEL TERMINALS ON LEG NR 4 SEPARATED FROM WIRES. INSULATION BREAKDOWN. RESISTANCE CHECKE D AT 5 TO 50 MEGA OHMS (SHOULD BE 1000 TO 2000). 2 L 7 2 4F 4 F RT T0001SE E46NE 2002072400064 20020724 00064 NM 2002 7 24 2002UALA01031 1 20020617 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 LEFT HAND FUSELAGE HAS SEVERAL DENTS BETWEEN STATION 600 AND 620 ON AND BELOW STRINGER 16L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072400065 20020724 00065 EU 2002 7 24 MALA020401 1 20020710 A 7931 CONNECTOR SAAB SF340 SF340A 7850100 EU PROP OIL PRESS FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 110XJ 340A110 DURING FLIGHT 3084 LT PROP OIL PSI DROPPED TO ZERO AFTER START. A/C RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED PGB OIL PRESSURE TRANSMITTER CONNECTOR PLUG 15HE. ALL CHECKS GOOD IAW SF-340, MM CHAP. 79. 2 L 7 2 4T RT A52EU 2002072400066 20020724 00066 EU 2002 7 24 MALA020402 1 20020710 A 2760 917481 SELECTOR VALVE BAC 146 AVRO146RJ85A 1500097 EU SPOILERS FAILED A MALA O OTHER J WARNING INDICATION LD LANDING 1 GL 15 507XJ E2316 DURING LANDING ROLL OUT OF FLIGHT 3410, SPOILER SYSTEM "GREEN FAIL" LIGHT ILLUMINATED . SPOILERS OPERATED FINE. FLIGHT TERMINATED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GREEN SYSTEM LIFT SPOILER SELECTOR VALVE IAW 27-61-1 7-201 AVRO AMM PN AIR 91748-1, SN/ON APB000008, SN/OFF APB990387. OPS CHECK AND LEAK CHECK GOOD. 2 H 7 4 4F RT A49EU 2002072400067 20020724 00067 NM 2002 7 24 2002UALA01032 1 20020617 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 CABIN FLOOR SUPPORT IS WORN AT STATION 365 RBL 46. MAJOR REPAIR ACCOMPLISHED. CABIN FLOOR SUPPORT AT STATION 365 RBL 4 6 WAS REPAIRED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072400068 20020724 00068 NM 2002 7 24 2002UALA01033 1 20020617 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 CABIN FLOOR SUPPORT IS CORRODED AT STATION 365 RBL 26. MAJOR REPAIR ACCOMPLISHED. CABIN FLOOR SUPPORT AT STATION 365 R BL 26 WAS REPAIRED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072400069 20020724 00069 EU 2002 7 24 MALA020403 1 20020711 A 3150 6071T02P18 CONTROL UNIT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R389 R3894123F25 NE COCKPIT FAILED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 452XJ 340B452 DURING FLIGHT 3395, LT PROP RPM INDICATION WENT TO ZERO. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED DECU, ALS O REPLACED YELLOW HARNESS. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P30NE 2002072400070 20020724 00070 NE 2002 7 24 MALA020406 2 20020717 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 68XJ 340A068 DURING FLIGHT 3313 RT ENGINE SHUTDOWN DUE TO LOW OIL PRESSURE. AIR RETURN TO DTW. NO OTHER INFORMATION IS AVAILABLE AT THIS TIME. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002072400071 20020724 00071 NM 2002 7 24 2002UALA01034 1 20020618 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 FUSELAGE STRINGER AT STATION 625 HAS A DENT AT STRINGER 18L. MAJOR REPAIR ACCOMPLISHED. STRINGER SPLICED IN NEW SECTIO N USING HAT CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072400072 20020724 00072 EU 2002 7 24 MALA020408 1 20020715 A 2120 DUCT SAAB SF340 340B 7860101 EU AIR CONDITIONING BURNED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 412XJ 340B412 DURING FLIGHT 3058 DURING TAXI, CREW REPORTED SMOKE IN CABIN. UPON INSPECTION FOUND DUCT COMING FROM SUPPLEMENTAL A/C M OTOR BURNED. NO OTHER INFORMATION AT THIS TIME. 2 L 7 2 4T RT A52EU 2002072400073 20020724 00073 EU 2002 7 24 MALA020409 1 20020605 A 7500 9303688100 DUCT SAAB SF340 340B 7860101 EU BLEED AIR LEAKING A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 418XJ 340B418 DURING FLIGHT 2819, RT BLEED AIR LEAK CAUTION LIGHT ILLUMINATED DURING FLIGHT. AIR RETURN TO MEM. MAINTENANCE REPLACED RT FLEX DUCT PN 9303688-100 AT ACM INLET PIPE LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2002072400074 20020724 00074 EU 2002 7 24 MALA020411 1 20020718 A 7720 INDICATOR SAAB SF340 340B 7860101 EU RT ENG ITT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 408XJ 340B408 ON CLIMB AND IN CRUISE OF FLIGHT 2936, RT ENGINE ITT INDICATION. FUNCTIONED INTERMITTANTLY INDICATING BETWEEN 400 AND 700. IRRATICALLY ALL OTHER ENGINE INDICATIONS WERE NORMAL. AIR RETURN TO DTW. MAINTENANCE CND. INSTALLED SERICEABLE RT ITT INDICATOR SN/OFF 9704655A SN/ON 342A. ALL CHECKS GOOD DONE IAW AMM CHAP 77 . 2 L 7 2 4T RT A52EU 2002072400076 20020724 00076 NM 2002 7 24 2002UALA01036 1 20020619 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 939UA 26672 EXTERNAL FUSELAGE SKIN HAS EXCESSIVE MATERIAL REMOVED AT STATION 800 SKIN LAP JUST BELOW AFT CARGO DOOR CUTOUT SILL PLAT E. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400077 20020724 00077 NM 2002 7 24 2002UALA01037 1 20020619 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 939UA 26672 EXTERNAL FUSELAGE SKIN WAS DAMAGED AT STATION 827 STRINGER 25R CARGO DOOR LOWER LAP SKIN. MAJOR REPAIR ACCOMPLISHED. F ABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400078 20020724 00078 NM 2002 7 24 2002UALA01038 1 20020619 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 AFT FUSELAGE AT STATION 1006 BETWEEN STRINGER 12L & 14L SKIN HAS 3 DENTS IN CLOSE PROXIMITY. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400079 20020724 00079 NM 2002 7 24 2002UALA01039 1 20020619 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 STRINGER 14 LEFT CRACKED AT STATION 360. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER END FITTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400080 20020724 00080 NM 2002 7 24 2002UALA01040 1 20020619 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 BODY STATION 400 FUSELAGE FRAME CRACKED AT STRINGER 9 LEFT. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED ANGL E DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400081 20020724 00081 NM 2002 7 24 2002UALA01041 1 20020619 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 FUSELAGE FRAME CRACKED STATION 868 STRINGER 9 RIGHT. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED ANGLE DOUBL ER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400082 20020724 00082 NM 2002 7 24 2002UALA01042 1 20020619 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 FUSELAGE FRAME AT BODY STATION 827 STRINGER 9R CRACKED AT RIVET. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED N EW ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400083 20020724 00083 NM 2002 7 24 2002UALA01043 1 20020619 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 FUSELAGE FRAME BODY STATION 847 STRINGER 9R CRACKED THROUGH RIVET. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW ANGLE AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400084 20020724 00084 NM 2002 7 24 2002UALA01044 1 20020619 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 BODY STATION 867 STRINGER 9L FRAME CRACKED AT RIVET TAIL. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR A NGLE AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400085 20020724 00085 NM 2002 7 24 2002UALA01045 1 20020619 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 BODY STATION 847 STRINGER 9L FRAME CRACKED AT RIVET TAIL. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW ANGL E AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400086 20020724 00086 NM 2002 7 24 2002UALA01046 1 20020619 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 BODY STATION 827 STRINGER 9L FRAME CRACKED AT RIVET TAIL. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW ANGL E AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400087 20020724 00087 NM 2002 7 24 2002UALA01047 1 20020619 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 BODY STATION 887 STRINGER 9L FRAME CRACKED AT RIVET TAIL. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW ANGL E AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400088 20020724 00088 EU 2002 7 24 02204330 1 20020723 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 330UE 41098 During preflight inspection, the crew reported that the forward section of emergency floor track lights were inoperative . Maintenance personnel secured a loose connector for the forward emergency floor track lights. An operational check w as satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002072400089 20020724 00089 EU 2002 7 24 DHL2002365008 1 20020721 A 2610 344001056 CONTROLLER AIRBUS 300 A300B4203 3930306 EU DEFECTIVE A DHLA K NONE N FALSE WARNING CR CRUISE 1 SO 01 365DH 149 1) DURING CRUISE FLIGHT SSC (SINGLE STROKE CHIME) AND MWP "LOOPS" LIGHT ILLUMINATED. FIRE DETECTOR LOOP PANEL CHECKED A ND LOOPS A & B TESTED NORMAL. MWP LOOPS & SSC CONTINUED INTERMITTENT. 2) TROUBLESHOT AND FOUND MASTER WARNING CONTROLLER DEFECTIVE. REMOVED AND REPLACED MASTER WARNING CONTROLLER PER MM REF 33-15-11. OK TO CONTINUE. 2 L 7 2 4F RT A35EU 2002072400090 20020724 00090 EA 2002 7 24 COMA0260445 1 20020721 A 2750 601R930303 POTENTIOMETER CNDAIR CL600 CL6002B19 1900309 EA L/H FLAP MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 962CA 15075 7123 FLIGHT 6085 LEFT FLAP INDICATION FLUCTUATED BETWEEN 4 AND 0 DEGREES DURING FLIGHT.FECU AND DFDR VERIFIED THERE WAS NO FL AP MOVEMENT. REPLACED L/H FLAP POSITION POT. 2 L 7 2 4F RT A21EA 2002072400091 20020724 00091 EA 2002 7 24 COMA0260446 1 20020722 A 3350 WIRE CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 805CA 7354 FLIGHT 5314 EMERGENCY FLOOR LIGHTING AT ROW 12 IS INOPERATIVE.RECONNECTED LOOSE CONNECTOR WIRE. 2 L 7 2 4F RT A21EA 2002072400092 20020724 00092 EA 2002 7 24 COMA0260447 1 20020722 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 868CA 7427 FLIGHT 5020 FLAPS FAIL CAUTION MESSAGE AT 26 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002072400093 20020724 00093 NM 2002 7 24 2002UALA01048 1 20020619 A 2910 01215209002 ISOLATION VALVE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE HYD SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 664UA 29236 ISOLATION VALVE LEAKED AND LOST LEFT HYDRAULIC SYSTEM. LEFT HYD SYSTEM ISOLATION VALVE LEAKING AT LOWER PORT UNION. RE F MM 29-22-05 PG 402 FIG 401. REPLACED DEFORMED O-RING, LEAK CHECKED WITH ALL HYD SYSTEMS RUNNING. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072400094 20020724 00094 NE 2002 7 24 MALA020412 3 20020712 A 6110 PROPELLER SAAB SF340 SF340A 7850100 EU ROTOL R389 R3894123F26 NE LEFT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 119XJ 340A119 DURING FLIGHT 3237, DURING INITIAL CLIMBOUT OF ATY, AFTER REDUCING CTST AND SELECTING CTOT SW OFF LT ENGINE TORQUE INCRE ASED RAPIDLY TO APPROXIMATELY 120 PERCENT TORQUE AND ITT INCREASED TO 903 C. AFTER REDUCING POWER LEVER POSITION BELOW 64 DEGREES SWITCH ENGINE REDUCED TO 40 PERCENT WHILE TROUBLE SHOOTING PROBLEM. AIR RETURN TO ATY. MAINTENANCE REPLACED LT PROP. 2 L 7 2 4T RT A52EU 6 C P30NE 2002072400095 20020724 00095 NM 2002 7 24 2002UALA01019 1 20020615 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 AFT PIT FLOORBEAM T-CAP CORRODED BODY STATION 1241, RBL 44. MAJOR REPAIR ACCOMPLISHED. REPAIRED AND INSTALLED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072400096 20020724 00096 EU 2002 7 24 MALA020413 1 20020703 A 5321 FLOOR PANEL SAAB SF340 SF340A 7850100 EU COCKPIT CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 112XJ DURING 4K-CHECK IN CWA, RT FLIGHT DECK FLOOR HAS CORROSION. MAINTENANCE REPAIRED CORROSION AROUND FLOOR "SNAP" FASTENER S IAW SAAB SRM 53-60-50 AND SAAB STATEMENT 340SDS004125. REFER TO 409 109815 2 L 7 2 4T RT A52EU 2002072400098 20020724 00098 NM 2002 7 24 2002UALA01051 1 20020620 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 DENT AT STATION 386 JUST BELOW STRINGER 16. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DENT REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400099 20020724 00099 EU 2002 7 24 MALA020414 1 20020706 A 5330 SKIN SAAB SF340 SF340A 7850100 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 112XJ DURING 4K-CHECK IN CWA, RT UPPER TAIL SKIN AT APPROXIMATELY STA 812. 5 1/4 INCH BELOW RUDDER FAIRING 5/8 INCH DIA .036 I NCH DEEP. MAINTENANCE COMPLETED REPAIR IAW SRM 53-90-10. PARA 2 AND MAL EO #S53127. RELEASE DATE 7/17/02 2 L 7 2 4T RT A52EU 2002072400100 20020724 00100 NM 2002 7 24 2002UALA01052 1 20020620 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 STATION 986 CABIN FLOORBEAM TOP CAP IS CORRODED FROM CENTER LINE TO RBL 42 IN SEVERAL AREAS. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW T-CAP AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400101 20020724 00101 EU 2002 7 24 MALA020415 1 20020705 A 5321 FLOOR PANEL SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 112XJ DURING 4K-CHECK IN CWA, LT FLIGHT DECK FLOOR HAS CORROSION ON THE FLOOR AND RIVET HEADS. MAINTENANCE PERFORMED REPAIRS AND REMOVED CORROSION IAW SRM 51-70-40 AND 53-60-50-2. REMOVED CORRODED RIVETS IAW 51-40-21. REFER TO 409# 109814. RELE ASE DATE 7/17/02. 2 L 7 2 4T RT A52EU 2002072400102 20020724 00102 NM 2002 7 24 2002UALA01053 1 20020620 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 CABIN FUSELAGE FRAME AT BODY STATION 887 STRINGER 9R CRACKED AT RIVET. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTA LLED ANGLE AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400103 20020724 00103 NM 2002 7 24 2002UALA01054 1 20020620 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 RIGHT HAND EXTERNAL FUSELAGE SKIN HAS DENT AT STATION 259 AND WL 173. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTAL LED NEW DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400104 20020724 00104 2002 7 24 2002UALA01055 4 20020620 A 3414 2083111 INDICATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAULTY A UALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 29 371UA 24540 FLIGHT ABORTED TAKEOFF AT HIGH SPEED DUE TO ERRATIC AIRSPEED INDICATION. ABORT TAKEOFF DUE TO AIRSPEED INDICATOR RED FL AG AND LOSS OF POINTER. REPLACED THE CAPTAINS MACH AIRSPEED INDICATOR AND THE NR 1 AIR DATA COMPUTER. THE MACH AIRSPEE D INDICATOR REMOVED WAS FOUND TO HAVE A FAULTY POWER SUPPLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400105 20020724 00105 NM 2002 7 24 2002UALA01056 1 20020620 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 CABIN FLOORBEAM STA 365 RBL 18 MATERIAL REMOVED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. CABIN FLOORBEAM UPPER CAP RE PLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072400106 20020724 00106 NM 2002 7 24 2002UALA01059 1 20020620 A 7330 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 646UA 25283 LEFT ENGINE CONTROL MESSAGE DISPLAYED ON EICAS IN FLIGHT AND ENGINE, REVERTED TO IDLE SPEED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072400107 20020724 00107 NM 2002 7 24 2002UALA01060 1 20020622 A 5310 DOOR FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 940UA 26675 FORWARD RIGHT HAND FUSELAGE PIT DOOR CUTOUT FORWARD LOWER END WAS BLENDED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. IN STALLED DOUBLER AND TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400108 20020724 00108 NM 2002 7 24 2002UALA01061 1 20020621 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 CABIN FLOORBEAM BODY STATION 295 RBL 31 TO RBL 44 UPPER SURFACE HAS EXCESS MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. F LOORBEAM UPPER CAP SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400109 20020724 00109 NM 2002 7 24 2002UALA01062 1 20020622 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 940UA 26675 BODY STATION 188 FRAME CHORD CRACKED AT WL 207 ON RIGHT HAND SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR AND EXTENDED EXTERNAL FUSELAGE SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400110 20020724 00110 NM 2002 7 24 2002UALA01063 1 20020622 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 FUSELAGE FRAME AT BODY STATION 616 CRACKED BELOW STRINGER 17L LOWER END INBOARD FLANGE FORWARD FACE. MAJOR REPAIR ACCOM PLISHED. INSTALLED ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400111 20020724 00111 NM 2002 7 24 2002UALA01064 1 20020622 A 5754 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L/E SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 NR 1 SLAT LOWER SKIN CRACKED AT FASTENER BETWEEN ACTUATOR AND ANTI-ICE TUBE, ALSO CRACKED BELOW INBOARD AUXILIARY TRACK. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400112 20020724 00112 EU 2002 7 24 MALA020416 1 20020705 A 5320 FLOOR SUPPORT SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 112XJ DURING 4K-CHECK IN CWA, LT OUTBOARD FLOORBOARD ANGLE AFT OF WING BOX CORRODED. MAINTENANCE REMOVED CORROSION IAW SRM 51- 70-40. REFER TO 409 109862. RELEASE DATE 7/17/2002 2 L 7 2 4T RT A52EU 2002072400113 20020724 00113 NM 2002 7 24 2002UALA01066 1 20020623 A 5320 STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 AFT PIT LOWER DOOR SILL INBOARD STRAP BODY STATION 773 TO 857 IS CORRODED AT SCREW HOLES. MAJOR REPAIR ACCOMPLISHED. R EPLACED INBOARD STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400114 20020724 00114 EU 2002 7 24 MALA020417 1 20020706 A 5347 SEAT TRACK SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 112XJ DURING 4K-CHECK IN CWA, AISLE SEAT TRACK HAS LIGHT CORROSION TO STA 535.0. MAINTENANCE REMOVED CORROSION IAW SRM 51-70- 40. REFER TO 409 109839, RELEASED DATE 7/17/02. 2 L 7 2 4T RT A52EU 2002080900029 20020809 00029 NE 2002 8 9 2002UALA01067 2 20020622 A 7230 6A5994 RUB STRIP AIRBUS A319 A319131 3930317 NM IAE V2527 V2527A5 NE NR 1 ENGINE DEBONDED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 801UA 6453 686 V10002 DIVERTED UNDER AMBER ALERT DUE TO VIBRATION IN NR 1 ENGINE. ENGINE REPLACED. HPC RUB STRIP DISBONDED CAUSING COMPRESSO R VIBRATION. ENGINE UPGRADED WITH RUB STRIP MODIFICATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2002072400115 20020724 00115 NM 2002 7 24 2002UALA01068 1 20020622 A 2750 FLAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE WING MALFUNCTIONED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 345UA 24249 AFTER DEPARTURE ON FLAP RETRACTION FROM FLAPS 1 TO FLAPS UP, THE FLAPS SPLIT ACCORDING TO THE FLAP POSITION INDICATOR. RETURNED TO THE FIELD AND MADE A FLAPS UP LANDING. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072400117 20020724 00117 EU 2002 7 24 MALA020418 1 20020706 A 1430 RIVET SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 112XJ DURING 4K-CHECK IN CWA, RT OUTBOARD FUSELAGE WING BOX RIVET HEADS HAVE LIGHT CORROSION STA 401-STA 475.5. MAINTENANCE R EMOVED CORROSION IAW SRM 51-70-40. REFER TO 409 109840. RELEASE DATE 7/17/02 2 L 7 2 4T RT A52EU 2002072400119 20020724 00119 EU 2002 7 24 MALA020419 1 20020706 A 5320 FLOOR SUPPORT SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 112XJ DURING 4K-CHECK IN CWA, RT OUTBOARD FLOORBOARD ANGLE RLB 36 AFT OF WING BOX HAS CORROSION. MAINTENANCE REMOVED CORROSIO N IAW SRM 51-70-40. REFER TO 409 # 109881, RELEASE DATE 7/17/02. 2 L 7 2 4T RT A52EU 2002072400120 20020724 00120 EU 2002 7 24 MALA020420 1 20020715 A 5330 SKIN SAAB SF340 SF340A 7850100 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 112XJ DURING 4K-CHECK IN CWA, AN EXISTING REPAIR TO THE FUSELAGE SKIN BETWEEN STA 298 AND 351 WAS INVESTIGATED AND THE AREA WA S FOUND TO HAVE ADDITINAL DENTS, OIL CANNING AND IRREGULAR HOLES. MAINTENANCE REPAIRED THE FUSELAGE SKIN AND UNDERLYING STRUCTURE IAW SAAB STATEMENT 340SDS004125 AND EO #S53129. REFER TO 409#140680, 140681. RELEASE DATE 7/17/02 2 L 7 2 4T RT A52EU 2002072400121 20020724 00121 EU 2002 7 24 MALA020421 1 20020716 A 5414 SKIN SAAB SF340 SF340A 7850100 EU LT NACELLE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 112XJ DURING 4K-CHECK IN CWA, LT INBOARD COWL AFT UPPER CORNER FOUND DENT AND A PIECE OF SKIN MISSING. MAINTENANCE REPAIRED D AMAGE IAW SAAB STATEMENT 340SDS004112 AND EO S54059. REFER TO 409 109730. RELEASE DATE 7/17/02 2 L 7 2 4T RT A52EU 2002072400122 20020724 00122 EU 2002 7 24 MALA020422 1 20020717 A 5753 SKIN SAAB SF340 SF340A 7850100 EU TE FLAP DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 112XJ DURING 4K-CHECK IN CWA, RT FLAP UPPER SKIN PANEL HAS DENT AT FLAP STA 142. MAINTENANCE COMPLETED REPAIR IAW EO 57050. REFER TO 409 109888, RELEASE DATE 7/17/02. 2 L 7 2 4T RT A52EU 2002072400123 20020724 00123 EU 2002 7 24 MALA020423 1 20020718 A 2150 3502B000004 VALVE BAC 146 AVRO146RJ85A 1500097 EU NR 2 A/C PACK FAILED A MALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 517XJ E2335 DURING FLIGHT 3483, PACK NR 2 HI TEMP LIGHT ILLUMINATED PACK NR 2 DUCT TEMP AT 100 DEGREES. GATE RETURN. MAINTENANCE R EMOVED AND REPLACED 31 PAC COUPLING ALSO REMOVED AND REPLACED NR 2 PAC VALVE PN 3502B000-004 SN/OFF 1086 SN/ON 1069. IAW AVRO AMM 21-10-11-401. SEE MM 409 086167 FOR DETAILS ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2002072400124 20020724 00124 EU 2002 7 24 MALA020424 1 20020718 A 3260 CONNECTOR BAC 146 AVRO146RJ85A 1500097 EU MLG DAMAGED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 513XJ E2329 DURING FLIGHT 3574, RT MAIN GEAR INTRANSIT LIGHT REMAINS ON WHEN GEAR SLECTED UP. A/C DIVERTED FROM DTW TO CVG. WEATHE R WAS ALSO INVOLVED. MAINTENANCE FOUND RT MLG UPLOCK SENSOR CONNECTOR PLUG LOOSE. REMOVED AND CLEANED CONNECTOR PLUG A ND REINSTALLED. REMOVED AND CLEANED DOOR UPLOCK SENSOR CONNECTOR PLUG AND REINSTALLED. PERFORMED GEAR SWING IAW AMM 32 -30-00. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2002080100027 20020801 00027 NE 2002 8 1 MALA020425 2 20020718 A 7320 219333010 HMA BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 4 ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 520XJ E2345 DURING FLIGHT 3524 IN TUL, SMELL OF FUEL INSIDE A/C AND FUEL LEAK INFLIGHT. MAINTENANCE FOUND ECOLOGY TANK TO BE FULL A ND OVERBOARD DRAIN LINE TO BE OUT OF POSITION. REPOSITION DRAIN LINE AND RAN NR 4 ENGINE TO DRAIN ECOLOGY TANK. ECOLOG Y TAKE SYSTEM OPERATED NORMALLY. MAINTENANCE REPLACED THE HMA. 2 H 7 4 4F 4 F RT A49EU E6NE 2002072400125 20020724 00125 EU 2002 7 24 MALA020426 1 20020719 A 2430 GCU SAAB SF340 340B 7860101 EU NR 2 GEN FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 433XJ 340B433 INFLIGHT ON 3238, THE RT GEN LIGHT CAME ON FOLLOWED QRH GEN RESET APPROXIMATLEY 5 MINUTES RT GEN LIGHT COMES ON, FOLLOW ED QRH GEN WOULD NOT RESET. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED RT DC GEN AND RT GCU.ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2002072400126 20020724 00126 2002 7 24 MALA020427 4 20020719 A 3440 CONNECTOR SAAB SF340 340B 7860101 EU RADIO ALTIMETER FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 439XJ 340B439 DURING FLIGHT 3054 CREW REPORTED FALSE AND WILD INDICATIONS AND FLUXUATIONS IN THE RADIO ALTIMETER. AIR RETURN TO DTW. MAINTENANCE FOUND AFT ALT. BAD ATENNA CONNECTOR BAD. REPLACED CONNECTOR. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002072400127 20020724 00127 EU 2002 7 24 MALA020428 1 20020720 A 7930 SEAL SAAB SF340 SF340A 7850100 EU LT ENGINE LEAKING A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 46XJ 340A046 DURING FLIGHT 2764, CREW REPORTED LT ENGINE OIL PSI LIGHT ILLUMINATED AND THE GAUGE WAS FLUXUATING. CAME BACK JUST BELO W GREEN ARC. OVERFLEW STC. MAINTENANCE COMPLETED MAL JC 791107. B-SUMP SCREEN CHECKS. VERIFIED C-SUMP SEAL LEAKING, A FTER COMPLETION OJ JOB CCARDS, NO OIL COMPLETION OF JOB CARDS, NO OIL COMPUMTION NOTED. 2 L 7 2 4T RT A52EU 2002072400128 20020724 00128 EU 2002 7 24 MALA020429 1 20020720 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 368PX 340B274 RT FUSELAGE TWO SKIN DENTS STA 340, WL 78.0 .035 DEPTH. STA 340, WL 94.5 , .032 DEPTH. MAINTENANCE REPAIRED BOTH DENT S IAW EO #S53009. 2 L 7 2 4T RT A52EU 2002072400129 20020724 00129 WP 2002 7 24 GTIA020590 1 20020422 A 5753 SKIN DOUG DC9 DC982 3022082 WP FLAP VANE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 FTW - FOUND LEFT WING INBOARD FLAP VANE NR 1 TWO EACH LARGE DENTS ON UPPER SURFACE OF VANE. REPAIRED DAMAGE, PER SPIRIT AIRLINES EA 5750-0205. (M) 2 L 7 2 4F A6WE 2002072400130 20020724 00130 WP 2002 7 24 GTIA020591 1 20020508 A 5751 ACCESS PANEL DOUG DC9 DC982 3022082 WP AILERON CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - LEFT WING, OUTBOARD AILERON DAMPENER ACCESS, SECTION OF METAL CRACKED AND BROKEN OUT. REMOVED METAL CRACKED. FOR MED NEW METAL FORMER IAW MD80 SRM 51-10-2. INSTALLED NEW FORMER IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002072400131 20020724 00131 WP 2002 7 24 GTIA020592 1 20020509 A 5320 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT PIT STATION 1220 L26R, LONGERON SPLICE IS CORRODED ON LOWER SURFACE. REMOVED SPLICE, REMOVED CORROSION. FORMED NEW END. INSTALLED END FITTING IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002072400132 20020724 00132 WP 2002 7 24 GTIA020593 1 20020511 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FORWARD LOWER CARGO PIT CORRODED/ELONGATED HOLES AT AFT CENTER BULKHEAD ANGLE. REMOVED ANGLE. FABRICATED N EW PART. ANGLE ATTACH CLIP FOUND TO BE OUT OF LIMITS. FABRICATED NEW CLIP. INSTALLED ANGLE AND CLIP PER MD80 SRM 51-3 0-2. (M) 2 L 7 2 4F A6WE 2002072400133 20020724 00133 WP 2002 7 24 GTIA020594 1 20020511 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FORWARD LOWER CARGO PIT, CORRODED AT RT CARGO TRACK STATION 427. REMOVED RIGHT CARGO TRACK STATION 427 TO 636. F ABRICATED A NEW TRACK. INSTALLED NEW TRACK FRONT STATION 427-636. (M) 2 L 7 2 4F A6WE 2002072400134 20020724 00134 WP 2002 7 24 GTIA020595 1 20020512 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT CARGO DOOR SUPPORT FITTING HAS CORROSION. FITTING IS OUT OF LIMITS. REMOVED AND REPLACED FITTING. (M) 2 L 7 2 4F A6WE 2002072400135 20020724 00135 WP 2002 7 24 GTIA020596 1 20020513 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 AFT CARGO FRAME ASSEMBLY STATION 1117 HAS CORROSION, DOUBLER DRILLED HOLES, HOLES WITH NO PITCH AND TOOL MARKS. REMOVED AND INSTALLED FRAME ASSEMBLY. (M) 2 L 7 2 4F A6WE 2002072400136 20020724 00136 WP 2002 7 24 GTIA020597 1 20020513 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND MID PIT, CORROSION AT LONGERON 28L STATION 807. REMOVED LONGERON 28L AT STATION 815 TO 798. FABRICATED LON GERON 28L. INSTALLED NEW LONGERON AND SPLICE. (M) 2 L 7 2 4F A6WE 2002072400137 20020724 00137 WP 2002 7 24 GTIA020598 1 20020520 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND E/E COMPARTMENT AFT PRESSURE BULKHEAD HAS CORROSION BETWEEN L27 AND L29 STATION 218. CUT DAMAGE WEB SECTION . FABRICATED DRILLED UP AND LOCATED NEW SECTION OF WEB AND REPAIR STRAP. INSTALLED NEW WEB SECTION. (M) 2 L 7 2 4F A6WE 2002072400138 20020724 00138 WP 2002 7 24 GTIA020599 1 20020521 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND UPON INSPECTION OF CLEANING FOUND CORROSION AT STATION 160 LONGERON 22L AND STATION 133-148 LONGERON 28L-27L . CUT AND REMOVED DAMAGED LONGERON L22 FROM STATION 140-226. DRILLED AND LOCATED NEW LONGERON AND SPLICE. INSTALLED L ONGERON, SPLICE, AND INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002072400139 20020724 00139 WP 2002 7 24 GTIA020600 1 20020525 A 5320 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FORWARD CARGO LONGERON SPLICE 28L STATION 226 HAS CORROSION. REMOVED SPLICE LONGERON 28L STATION 226. FABR ICATED REPAIR SPLICE. INSTALLED REPAIR SPLICE. (M) 2 L 7 2 4F A6WE 2002072400140 20020724 00140 WP 2002 7 24 GTIA020601 1 20020522 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND FORWARD CARGO COMPARTMENT SHEAR TIE HAS HIGH STRESS EVIDENCE STATION 237 LEFT BETWEEN L20 AND L19 NEXT TO LA V DRAIN. REMOVED DAMAGED SHEAR TIE. FABRICATED NEW SHEAR TIE. INSTALLED SHEAR TIE. (M) 2 L 7 2 4F A6WE 2002072400141 20020724 00141 WP 2002 7 24 GTIA020602 1 20020601 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND AFT FUSELAGE BESIDE RIGHT AIRSTAIR ACTUATOR, FLOOR PANEL CRACKED. REMOVED CRACKED FLOOR PANEL RIGHT SIDE AI RSTAIR. FABRICATED REPAIR. INSTALLED FABRICATED PARTS ON THE REMOVED PANEL. (M) 2 L 7 2 4F A6WE 2002072400142 20020724 00142 WP 2002 7 24 GTIA020603 1 20020509 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT PIT STATION 1148-1220 L30-L26R, THRESHOLD CLOSURE WEB IS CORRODED IN NUMEROUS PLACES ON UPPER AND LOWER SURFACE. REMOVED WEB FROM A/C. FABRICATED NEW WEB. INSTALLED CLOSURE WEB. (M) 2 L 7 2 4F A6WE 2002072400143 20020724 00143 WP 2002 7 24 GTIA020604 1 20020509 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT PIT STATION 1309 L23L, CORROSION ON SIDEWALL SUPPORT POST LOWER END. FOUND FRAME CORRODED OUT OF LIMITS . REMOVED FRAME STATION 1309 FROM L27L TO L18L. (M) 2 L 7 2 4F A6WE 2002072400144 20020724 00144 WP 2002 7 24 GTIA020605 1 20020509 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW 0- FOUND AFT PIT STATION 1147 L29R-L29L STUB FRAME HAS CORROSION ON FORWARD AND AFT SIDE. FLOOR ATTACH ANGLE FOUND TO BE CORRODED OUT OF LIMITS AND HAVE DOUBLER HOLES. SHEAR TIE BETWEEN 30 AND 29R FOUND TO BE OUT OF LIMITS. NEW SHEAR TIE FABRICATED. VERIFY NEW FLOOR ATTACH BRACKET. LOCATED AND DRILLED UP NEW HOLES ON NEW BRACKET. INSTALLED SHEAR TI E AND STUB FRAME AT STATION 1147 L29R-L29L. INSTALLED NEW ATTACH BRACKET AT STATION 1147. (M) 2 L 7 2 4F A6WE 2002072400145 20020724 00145 WP 2002 7 24 GTIA020606 1 20020509 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT PIT STATION 1174 L29R-L30, CORROSION ON FRAME TO SKIN SHEAR TIE AND ADJACENT SKIN. REMOVED DAMAGE SHEAR TIE. FABRICATED NEW PARTS. VERIFY NEW PART FOR FRAME. DRILLED AND LOCATED HOLES AT FRAME. INSTALLED SHEAR TIE REPAI R. VERIFY NEW PART FOR FLOOR SUPPORT. DRILLED AND LOCATED HOLES AT FLOOR SUPPORT. INSTALLED NEW FRAME STATION 1174. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002072400146 20020724 00146 WP 2002 7 24 GTIA020607 1 20020509 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT PIT STATION 1322 L22L, CORROSION ON FRAME WEB AND LOWER FLANGE UPPER SURFACE. REMOVED DAMAGED SECTION O F FRAME. FABRICATED NEW SECTION OF FRAME. INSTALLED SECTION OF FRAME. INSTALLED FRAME WEB. (M) 2 L 7 2 4F A6WE 2002072400147 20020724 00147 WP 2002 7 24 GTIA020608 1 20020508 A 7110 NOSE COWL DOUG DC9 DC982 3022082 WP RT ENGINE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND RIGHT ENGINE, NOSE COWL L/W PITTING CORROSION ON AND AFT OF REPAIR PATCH AT 5 O'CLOCK POSITION. NOSE COWL R EMOVED AND REPLACED WITH SERVICEABLE UNIT. (M) 2 L 7 2 4F A6WE 2002072400148 20020724 00148 WP 2002 7 24 GTIA020609 1 20020529 A 7130 FIRESEAL DOUG DC9 DC982 3022082 WP NR 2 ENGINE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND NR 2 ENGINE FIRE SEAL BROKEN AT SEVERAL SPOTS. REMOVED NR 2 ENGINE FIRE SEAL INSTALLED FIRE SEAL AT NR 2 EN GINE. (M) 2 L 7 2 4F A6WE 2002072400149 20020724 00149 WP 2002 7 24 GTIA020610 1 20020524 A 5310 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND E/E COMPARTMENT CORROSION EXISTS ON LONGERONS, FRAMES, AND WEBS STATION 200 FROM LONGERON 18L TO 21L. MATER IAL ON LONGERON 18L END CAP FITTING OUT OF LIMITS. FORMED NEW END CAP FITTING. INSTALLED END CAP FITTING. (M) 2 L 7 2 4F A6WE 2002072400150 20020724 00150 WP 2002 7 24 GTIA020611 1 20020510 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND MID PIT HAS CRACKED AT LT AFT SUPPORT FRAME STATION 712. REMOVED LEFT AFT SUPPORT FRAME. REPAIRED MID PIT LEFT AFT SUPPORT. INSTALLED MID PIT LEFT AFT SUPPORT FRAME 712. (M) 2 L 7 2 4F A6WE 2002072400151 20020724 00151 WP 2002 7 24 GTIA020612 1 20020523 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND E/E BAY INTERCOSTAL CORRODED FROM STATION Y200 TO Y207 ABOVE LONGERON 21L. REMOVED CORROSION. FORMED INTER COSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002072400152 20020724 00152 WP 2002 7 24 GTIA020613 1 20020517 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT CARGO FLOOR SUPPORT BROKEN IN HALF STATION Y130. LOCATED AND DRILLED. INSTALLED PER MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002072400153 20020724 00153 WP 2002 7 24 GTIA020614 1 20020509 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT PIT STATION 1212 L29R-L30, FLOOR SUPPORT CRACKED/BENT AT FASTENER HOLE IN UPPER SURFACE. REMOVED FLOOR SUPPORT. DRILLED AND LOCATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002072400154 20020724 00154 WP 2002 7 24 GTIA020615 1 20020526 A 5320 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND MID CARGO COMPARTMENT STATION Y730 FORMER FRAME CORRODED ABOVE LONGERON 30. REMOVED FRAME TO LONGERON ATTAC H ANGLE. LOCATED AND DRILLED NEW ANGLE INSTALLED NEW ANGLE. (M) 2 L 7 2 4F A6WE 2002072400155 20020724 00155 2002 7 24 GTIA020616 4 20020601 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 MCO - FLT 927 - FOUND L1 SLIDE PACK CAME OFF DOOR WHEN IT WAS OPENED. REINSTALLED L1 SLIDE PACK. (M) 2 L 7 2 4F A6WE 2002080200024 20020802 00024 EU 2002 8 2 C2XA02IA146 1 20020719 A 3150 35OA23008314 COMPUTER AEROSP ATR42 ATR42320 8680930 EU COCKPIT FALSE INDICATION A C2XA K NONE N FALSE WARNING AP APPROACH 1 SW 27 34820 159 IAH - FLT 3584 - CREW REPORTED THAT A FORWARD SMOKE WARNING INDICATION ILLUMINATED DURING FLIGHT. THE CREW DECLARED AN EMERGENCY AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND FOUND THE WARNING TO BE A FALSE INDICATION. MAINTENANCE THEN REMOVED AND REPLACED THE CENTRAL CREW ALERTING COMPUTER. THE SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN SERVICE. 2 H 7 2 4T RT A53EU 2002072400156 20020724 00156 NM 2002 7 24 UPS02438867 1 20020629 A 5310 65B083156 SPLICE BOEING 747 747123F NM BS 1301 S12L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C M/D - BS 1301 S12L FRAME ATTACH SPLICE FOUND CRACKED. M/D - BS 1301 S12L FRAME ATT SPLICE REPLACED AS PER SRM 51-10-01 P.8 . 2 L 7 4 4F A20WE 2002072400157 20020724 00157 NM 2002 7 24 UPS02438868 1 20020702 A 5310 65B072972 SPLICE BOEING 747 747123F NM BS 990 S10L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C U/D - BS 990 S-10L STRINGER SPLICE FOUND CRACKED. BS 990 S10L SPLICE REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002072400158 20020724 00158 NM 2002 7 24 UPS02438872 1 20020628 A 5410 WEB BOEING 747 747123F NM #2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C NO.2 PYLON - LOWER SPAR BOTTOM AREA FOUND CRACK AT NAC STA 228 AS MARKED. LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 2 AND SRM 54-10-03 FIG 22. 2 L 7 4 4F A20WE 2002072400159 20020724 00159 SO 2002 7 24 C2XA02BT036 1 20020723 A 4900 4501968C APU EMB 145 EMB145 3260210 SO TAILCONE FAILED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16963 6083 145116 EWR/BTV---CO3526, ON TAXI, CREW REPORTED APU FAIL AND SMOKE ENTERED COCKPIT.....AIRCRAFT RETURNED TO GATE UNEVENTFULLY. MAINTENANCE INSPECTED AIRCRAFT/APU AND FOUND APU SHAFT TURBINE NOT TO SPIN. RAN BOTH ENGINES #1 AND #2. NO SMOKE IN COC KPIT. ALL SYSTEMS CHECKED GOOD. AIRCRAFT RELEASED IAW MEL 49-00-00 CONTROL NUMBER 023128 APU INOPERATIVE. AIRCRAFT RETUR NED TO SERVICE.....BTV CO3387, MAINTENANCE REMOVED AND REPLACED APU IAW EMB145 AMM #49-10-01. OPS. AND LEAK CHECKED GOOD . MEL CLEARED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002072400160 20020724 00160 NM 2002 7 24 AWXA200200658 1 20020701 A 5311 654580733 ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/2" CRACK WAS FOUND ON THE FRAME SUPPORT ANGLE OF THE R1 DOOR, BS 291.5, ABOVE STR 8 & 9 R/H. MAINTENANCE REMOVED CRACKED FRAME SUPPORT ANGLE AT BS 291.5, ABOVE STR 8 & 9 R/H. FABRICATED A NEW ANGL E AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG. 3-4, & 38. 2 L 7 2 4F RT A16WE 2002072400161 20020724 00161 NM 2002 7 24 AWXA200200659 1 20020705 A 5313 65582802 SHEAR TIE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/2" CRACK WAS FOUND ON SHEAR TIE BS 360, BETWEEN STR 14 & 15 R/H. MAINTENANCE CUTOUT DAMAGE ON SHEAR TIE BS 360, BETWEEN STR 14 & 15 R/H, FABRICATED A REPAIR SHEAR TIE, AND INSTALLED REPAIR IAW SRM 53-00-07, PG. 219-221, AND DWG 65-58280-2. 2 L 7 2 4F RT A16WE 2002072400162 20020724 00162 NM 2002 7 24 AWXA200200661 1 20020702 A 5313 654988629 STRINGER BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/2" CRACK WAS FOUND ON STRINGER END UPPER LOBE BS 500C+5, STR 16 L/H, HFEC CON FIRMED. MAINTENANCE CUTOUT DAMAGED SECTION OF STRINGER 16 L/H, BS 500C+5. FABRICATED A FILLER AND REPAIR CHANNEL, AND IN STALLED REPAIR PARTS IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2002072400163 20020724 00163 NM 2002 7 24 AWXA200200662 1 20020702 A 7830 315A1303 BEAM BOEING 737 7373G7 1384595 NM WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK ELONGATED HOLES WERE FOUND ON THE # 1 ENGINE INBOARD THRUST REVERSER UPPER SUPPOR T BEAM. MAINTENANCE DRILLED DAMAGED HOLES ON # 1 ENGINE INBOARD THRUST REVERSER UPPER SUPPORT BEAM TO A LARGER DIAMETER, FABRICATED 2 EACH DOUBLERS AND FREEZE PLUG BUSHINGS, AND INSTALLED REPAIR PARTS IAW AWA ER 03-7831-02200-ES4. 2 L 7 2 4F RT A16WE 2002072400164 20020724 00164 NM 2002 7 24 AWXA200200663 1 20020627 A 5330 148N3611 SKIN BOEING 757 7572G7 1384963 NM CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 0 0 24522 LCQ - MAJOR REPAIR - DURING C-11 CHECK THE FUSELAGE SKIN WAS FOUND CHAFED BELOW THE AFT END OF THE L/H HORIZONTAL STABIL IZER BS 1865. MAINTENANCE REMOVED DAMAGED SKIN PANEL PER B737-300 SRM 51-40-02, PG. 16. FABRICATED A NEW SKIN PANEL, A F ILLER, AND A DOUBLER, AND INSTALLED REPAIR PARTS IAW AWA ER 19-5381-02200-ES1. 2 L 7 2 4F RT A2NM 2002072400165 20020724 00165 WP 2002 7 24 GTIA020620 1 20020512 A 5230 ANGLE DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT CARGO STATION 1155 CARGO DOOR ANGLE HAS CORROSION. ANGLE FOUND TO BE CRACK IN RADIUS. LOCATED AND DRIL LED NEW SUPPORT. INSTALLED NEW SUPPORT. (M) 2 L 7 2 4F A6WE 2002072400166 20020724 00166 NM 2002 7 24 QXEA0201045 1 20020722 A 3350 6138001 BATTERY PACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 1592 1592 4053 PDX- AFT THREE AISLE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BOTH BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072400167 20020724 00167 SO 2002 7 24 C2XA02SH029 1 20020713 A 5300 14525422001 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 SHV - DURING C-CHECK INSPECTION THE LEFT HAND SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 60 AND 65. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED SILL IN ACCORDANCE WITH EMB-145 SRM51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. 2 L 7 2 4F RT T00011AT 2002072500001 20020725 00001 SO 2002 7 25 C2XA02SH030 1 20020710 A 5300 14522460013 BUTT STRAP EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 SHV-DURING C-CHECK INSPECTION,THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 18 AND 22.MAINTENANCE REMOVE D AND REPLACED THE DAMAGED SECTIONS OF BUTT STRAP IN ACCORDANCE WITH EMB-145 SRM 51-40-02,AND THE AIRCRAFT WAS WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002072500002 20020725 00002 2002 7 25 C2XA02IA148 4 20020724 A 2350 7511001939 AUDIO CONTROL EMB 145 EMB145LR 3260212 SO COCKPIT BURNED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13550 145575 LBB- FLIGHT 3814, DURING CLIMB THE CREW NOTED THAT INFLIGHT SMOKE ODOR, AND, APPEARANCE AFTER LOST CAPT. AUDIO PANEL. S MOKE CLEARED AFTER THIRTY SECONDS,THE ODOR REMAINED. THE CREW DECLAIRED EMERGENCY, AND, LANDED AT LBB WITHOUT INCIDENT. LBB- MAINTENANCE REMOVED AND REPLACED THE CAPTS. AUDIO CONTROL PANEL, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED , AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002072500003 20020725 00003 EA 2002 7 25 QXEA0200873 1 20020611 A 3240 6007300 SENSOR CNDAIR CL600 CL6002C10 1390015 EA BRAKE ASSY OVERHEATED A QXEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 NM 09 605QX 10022 FLIGHT BETWEEN EUG - LAX WAS DIVERTED TO SMF. LEVEL AT FL370. BRAKE OVERHEAT WARNING MESSAGE ILLUMINATED. TEMPERATURE FL UXUATED BETWEEN 0-20, AFTER GEAR EXTENTION, TEMP WENT DOWN TO 0 WITH OCCASIONAL FLUXUATION. BACK TO 20 WITH ACCOMPANING WARNING. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT HAND BRAKE TEMP SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002072500005 20020725 00005 NM 2002 7 25 QXEA0200876 1 20020608 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX-AT STATION 387, STRINGER 33 FOWARD OF COVER PLATE THERE IS A PITTED SKIN MARK. REPAIRED IAW HORIZON AIR EA. 2-53-398 . AND DHC-8 SRM 57-20-11. 2 H 7 2 4T RT A13NM 2002072500006 20020725 00006 NM 2002 7 25 QXEA0200877 1 20020607 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX-AT STATION 428, STRINGER 33 THERE IS A PITTED SKIN MARK. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002072500007 20020725 00007 NM 2002 7 25 QXEA0200878 1 20020607 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX-AT STATION 439, STRINGER 33 THERE IS A PITTED SKIN MARK. REPAIRED IAW RD8-53-2181 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002072500008 20020725 00008 NM 2002 7 25 QXEA0200879 1 20020608 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE BURNED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX-BETWEEN STATION 165 AND STATION 173 THERE ARE 3 BURN MARKS. REPAIRED IAW HORIZON AIR EA. 2-53-398 AND DHC-8 SRM 51- 20-11. 2 H 7 2 4T RT A13NM 2002072500009 20020725 00009 NM 2002 7 25 QXEA0200880 1 20020607 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE BURNED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX-AT STATION 418, STRINGER 33 HAS A BURN MARK. REPAIRED IAW RD8-53-2181 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002072500010 20020725 00010 NM 2002 7 25 QXEA0200881 1 20020607 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM FUSELAGE SKIN BURNED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX-BETWEEN STATION 527 AND STATION 607 THERE ARE 6 BURNED RIVET HEADS. REPAIRED IAW DHC-8 SRM 51-40-11 2 H 7 2 4T RT A13NM 2002072500011 20020725 00011 NM 2002 7 25 QXEA0200882 1 20020608 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX-AT STATION 327, STRINGER 33 THERE IS A PITTED MARK. REPAIRED IAW HORIZON AIR EA. 2-53-398 AND DHC-8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002072500012 20020725 00012 NM 2002 7 25 QXEA0200883 1 20020607 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX-AT STATION 291, STRINGER 33 THERE IS A PITTED SKIN MARK. REPAIRED IAW RD8-53-2181 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002072500013 20020725 00013 NM 2002 7 25 QXEA0200884 1 20020607 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX-AT STATION 312, STRINGER 33 AND STRINGER 32L THERE IS 2 PITTED RIVET HEADS. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002072500014 20020725 00014 NM 2002 7 25 QXEA0200885 1 20020607 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX-AT STATION 333 AND STRINGER 32L THERE IS 2 PITTED SKIN MARKS. REPAIRED IAW RD8-53-2181 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002072500015 20020725 00015 NM 2002 7 25 QXEA0200886 1 20020608 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 PDX-AT STATION 371 AND STRINGER 32R THERE IS 2 PITTED SKIN MARKS. REPAIRED IAW HORIZON AIR EA. 2-53-398 AND DHC-8 SRM 51 -20-11. 2 H 7 2 4T RT A13NM 2002072500016 20020725 00016 NM 2002 7 25 QXEA0200887 1 20020613 A 3230 54C546349 SEQUENCE VALVE DHAV DHC8 DHC8202 2809007 NM LT MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 379PH 6693 6693 530 PSC- AFTER TAKEOFF WHEN GEAR WAS SELECTED UP NR 2 HYD PRESSURE AND QUANTITY DROPPED TO ZERO. NR 2 ENGINE HYDRAULIC PUMP ILLUMINATED. MLG REMAINED RED, WHILE NOSE GEAR RETRACTED. LT MLG DOOR DID NOT OPEN, THE NOSE AND RT GEAR DOOR REMAINED AMBER. NR 2 HYD PUMP OPERATED WITHOUT FLUID FOR 23 TO 25 MINUTES. AIRCRAFT RETURN TO FIELD WITHOUT INCIDENT. REMOVED AN D REPLACED NR 1 MLG SEQUENCE VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500018 20020725 00018 NM 2002 7 25 QXEA0200893 1 20020615 A 2120 ODOR DHAV DHC8 DHC8202 2809007 NM CABIN DETECTED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 09 366PH 510 SEA-CREW SMELLED ABNORMAL SMELL ON FINAL APPROACH. GROUND RAN AIRCRAFT AT VARIOUS POWER SETTINGS AND AT LP AND HP POSITI ON AIR. ISOLATED BLEED BETWEEN 1 AND 2. NO SMELL NOTED. INSPECTED ACM AREA, NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAF T RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500019 20020725 00019 NM 2002 7 25 QXEA0200894 1 20020614 A 5242 SKIN DHAV DHC8 DHC8202 2809007 NM DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX-SKIN PEELED BACK AT CENTER HINGE AREA OF FORWARD LEFT HAND NOSE DOOR ON FUSELAGE. REPAIRED IAW HORIZON AIR EA. 2-53- 399. 2 H 7 2 4T RT A13NM 2002072500020 20020725 00020 NM 2002 7 25 QXEA0200895 1 20020614 A 3350 6138001 POWER SUPPLY BOMBDR DHC8 DHC8401 1390041 NM EXTERIOR LIGHTS INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 409QX 1964 19 4051 SEA- FORWARD RT EXTERIOR EMERGENCY LIGHT EXTINGUISHED WITH SWITCH ON. REMOVED AND REPLACED NR 1 AND 2 FORWARD EMERGENCY LIGHT POWER SUPPLYS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500021 20020725 00021 EU 2002 7 25 QXEA0200896 1 20020616 A 3350 5515800106 BULB FOKKER F28 F28MK4000 4990810 EU CABIN BURNED OUT A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 497US 11173 PDX- MID CABIN CEILING EMERGENCY EXIT SIGN HAS BULBS BURNED OUT. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002072500022 20020725 00022 NM 2002 7 25 QXEA0200898 1 20020613 A 3397 WIRE DHAV DHC8 DHC8202 2809007 NM CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 375PH 529 PDX- EMERGENCY LIGHT STRIP CONNECTOR HAS BROKEN WIRE AT FLOOR PANEL 133DZ. CRIMPED NEW PIN ON WIRE CONNECTOR. OPERATIONA L CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500023 20020725 00023 EU 2002 7 25 QXEA0200900 1 20020620 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 11159 BOI-EMERGENCY EXIT SIGN LIGHT INOPERATIVE ABOVE COCKPIT ENTRYWAY. REMOVED AND REPLACED EXIT SIGN AT COCKPIT ENTRYWAY. OP ERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002072500024 20020725 00024 NM 2002 7 25 QXEA0200901 1 20020621 A 5410 RIVET BOMBDR DHC8 DHC8401 1390041 NM NR 2 NACELLE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 PDX - ON WALKAROUND FOUND 3 LOOSE RIVETS ON NR 2 ENGINE NACELLE HORSE COLLAR. REINSTALLED HORSE COLLAR. NO PARTS REPLACE D. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500025 20020725 00025 NM 2002 7 25 QXEA0200902 1 20020622 A 5310 PRESSURE PANEL BOMBDR DHC8 DHC8401 1390041 NM NLG WW DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 413QX 4060 PDX - HOLE IN NLG WW LT AFT UPPER CORNER ABOVE WIRE HARNESS. REPAIRED IAW HORIZON AIR EA 6-53-80. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2002072500026 20020725 00026 NM 2002 7 25 QXEA0200903 1 20020623 A 3251 4063000501 CONTROL UNIT BOMBDR DHC8 DHC8401 1390041 NM NLG STEERING INOPERATIVE A QXEA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 NM 09 413QX 964 4060 SEA - ABORTED TAKE-OFF NOSE STEERING FAIL WHEN LINING UP FOR TAKE-OFF AND TWICE WHEN TURNING INTO PARKING SPOT. REPLACE D NOSE WHEEL STEERING ELECTRONIC CONTROL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500027 20020725 00027 2002 7 25 QXEA0200904 4 20020621 A 3420 42000332501 COMPUTER BOMBDR DHC8 DHC8401 1390041 NM AHRS INOPERATIVE A QXEA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 NM 09 407QX 1973 4049 PDX-DURING CLIMBOUT, LOST NR 2 AHRS, ELEVATOR FEEL CAUTION LIGHT CAME ON. NR 2 RPM WENT FROM 900 TO 1020 RPM. YAW DAMPER WOULD NOT RE-ENGAGE. TOOK BOTH CONDITION LEVERS FROM 900 TO 1020 THEN BACK TO 850 RPM. SYMMETRICAL TORQUE RESTORED. RE TURNED TO FIELD, LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED AHRS. FDR & DATE SHOWS POWER LEVER WAS M OVED 5 DEGREES ABOVE RATING DETENT WHICH WILL CAUSE AN INCREASE OF RPM TO 1020, THIS IS NORMAL FOR MOVEMENT OF POWER LEV ER IN THIS RANGE. ELEVATOR FEEL CAUTION WAS RELATED TO FAILURE OF AHRS. REPLACEMENT OF AHRS CLEARED ELEVATOR FEEL CAUTIO N LIGHT PROBLEM. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500028 20020725 00028 NM 2002 7 25 QXEA0200905 1 20020624 A 2910 DSC252B40124 LINE DHAV DHC8 DHC8202 2809007 NM HYD SYSTEM LEAKING A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 354PH 498 PDX-AIRCRAFT RETURNED TO FIELD, NR 2 HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED ON TAKEOFF. NR 2 HYDRAULIC QUANTITY WAS AT .5 QUARTS. MAITENANCE INSPECTED AIRCRAFT AND FOUND NOSE LANDING GEAR ACTUATOR UPLINE LEAKING. REMOVED AND REPLACED NOSE LANDING GEAR ACTUATOR UPLINE. NO LEAKS NOTED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500029 20020725 00029 NM 2002 7 25 QXEA0200906 1 20020626 A 2730 PITCH CONTROL BOMBDR DHC8 DHC8401 1390041 NM ELEVATOR MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 405QX 4047 SEA - AIRCRAFT RETURNED TO FIELD WHEN PITCH TRIM CAUTION ILLUMINATED, AND AUTO TRIM FAIL MESSAGE APPEARED. NO TRIM WAS A VAILABLE TO EITHER SIDE AND AUTO PILOT WOULD NOT ENGAGE. TRIM INDICATOR DISPLAYED FULL NOSE UP. MAINTENANCE INSPECTED TH E AIRCRAFT AND COMPLIED WITH THE SERVICE INFORMATION LETTER DHC8-400-SL-27-003 PROCEDURE. NO DEFECTS WERE NOTED, NO PART S REPLACED, AND OPERATIONAL CHECK WAS OK. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500030 20020725 00030 2002 7 25 QXEA0200907 4 20020626 A 3420 42000332501 COMPUTER BOMBDR DHC8 DHC8401 1390041 NM AHRS INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 407QX 142 4049 BOI-AFTER TAKEOFF FROM BOI ELEVATOR FEEL TRIM CAUTION LIGHT ILLUMINATED. ALL FLIGHT INSTRUMENTS ON CAPTAINS SIDE BECAME NON-FUNCTIONAL. AIRCRAFT RETURNED TO BOI WITH OUT FURTHER INCIDENT. REPLACED NR 1 AHRS. OPERATIONAL CHECKS NORMAL. AIRCR AFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500031 20020725 00031 EU 2002 7 25 QXEA0200908 1 20020626 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 SEA-FLIGHT ATTENDANT REPORTS FORWARD EXIT SIGN ONLY WORKS INTERMMITANTLY, MOST OF THE TIME IT IS OFF. REPLACED FORWARD E XIT SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002072500032 20020725 00032 EA 2002 7 25 QXEA0200910 1 20020623 A 5210 BUSHING CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR DISLODGED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 601QX 10009 PDX- MAIN CABIN DOOR WILL NOT UNLOCK. PRESSED BUSHINGS ON FORWARD AND AFT FITTINGS TO CORRECT FLUSHNESS AND REPAIRED IA W CRJ-700 MM 52-11-02-400-807-A01. 2 L 7 2 4F RT A21EA 2002072500033 20020725 00033 NM 2002 7 25 QXEA0200912 1 20020621 A 5710 WING DHAV DHC8 DHC8202 2809007 NM LEFT LEAKING A QXEA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 374PH 528 PDX- LEAKING FUEL RESIDUE NOTED AT 3 RIVETS ON TOP SIDE OF THE LT WING, CLOSE TO THE WING AND NACELLE AT STATION YW189.0 00 & THE FRONT SPAR X384.500. REPAIRED IAW DHC-8 SRM 51-40-11 AND APPLIED PR1422B 1/2 SEALANT. 2 H 7 2 4T RT A13NM 2002072500034 20020725 00034 2002 7 25 QXEA0200916 4 20020623 A 3160 C19190AB04 DISPLAY BOMBDR DHC8 DHC8401 1390041 NM COCKPIT INOPERATIVE A QXEA O OTHER O OTHER CR CRUISE 1 NM 09 411QX 1344 4055 BOI-DURING ENROUTE ENGINE DISPLAY PAGE WENT DARK AND SHIFTED DISPLAY TO NR 1 MFD. PERFORMED EMERGENCY CHECKLIST, DISPLAY RETURNED TO MFD. REPLACED ENGINE DISPLAY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500035 20020725 00035 EA 2002 7 25 QXEA0200918 1 20020629 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FALSE ACTIVATION A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 613QX 10045 SEA - AIRCRAFT ABORTED TAKE OFF WHEN AILERON WARNING MESSAGE APPEARED. MAINTENANCE INTERROGATED THE MAINTENANCE DIAGNOST ICS COMPUTER. NO FAULTS WERE NOTED. MAINTENANCE COMPLIED WITH THE FAULT ISOLATION MANUAL CRJ 27-11-00-810-002-A01. AN AI LERON FUNCTIONAL TEST WAS COMPLETED AND THE OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002072500036 20020725 00036 NM 2002 7 25 QXEA0200919 1 20020629 A 3260 864202 PROXIMITY SENSOR DHAV DHC8 DHC8202 2809007 NM NLG FAILED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 367PH 511 PDX - IMMEDIATELY AFTER GEAR RETRACTION, THE NOSE GEAR TRIED TO EXTEND 2-3 TIMES. THE RED AND GREEN LIGHTS FLASHED REPEA TEDLY FOR 10 - 15 SECONDS. GEAR STAYED UP NORMALLY. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE DRAG STRUT PROXI MITY SENSOR. THE SENSOR WAS ADJUSTED AND A FUNCTIONAL CHECK OF THE LANDING GEAR WAS PERFORMED. FUNCTIONAL CHECKS WERE GO OD AND THE RII WAS COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500037 20020725 00037 NM 2002 7 25 QXEA0200921 1 20020628 A 2120 SMOKE DHAV DHC8 DHC8202 2809007 NM COCKPIT DETECTED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 359PH 514 PDX- SMOKE IN COCKPIT AFTER NR 1 ENGINE START. GROUND RAN ENGINES AND COMPLETED SEVERAL STARTING SEQUENCES. COULD NOT DU PLICATE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500038 20020725 00038 EU 2002 7 25 QXEA0200923 1 20020628 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 BOI- CABIN EXIT SIGN HAS SEVERAL LAMPS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002072500039 20020725 00039 NM 2002 7 25 QXEA0200924 1 20020628 A 2613 SWITCH BOMBDR DHC8 DHC8401 1390041 NM NACELLE MALFUNCTIONED A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 408QX 4050 SEA- NR 1 BLEED HOT ILLUMINATED DURING APPROACH. COMPLIED WITH EMERGENCY CHECKLIST, WHILE LIGHT REMAINED ILLUMINATED EVE N AFTER ENGINES SHUTDOWN. DUCT TEMPERATURES APPEARED TO BE NORMAL. INTERROGATED CDS AND FOUND FAULT CODE 7002-L, 7006-L AND 1801-L. REMOVED AND REPLACED NACELLE DUCT LEAK OVERTEMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2002072500040 20020725 00040 NM 2002 7 25 QXEA0200925 1 20020629 A 6120 697073002 PCU BOMBDR DHC8 DHC8401 1390041 NM ROTOL R408 CR4086123F17 EU NR 2 ENGINE MALFUNCTIONED A QXEA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 09 403QX 345 4037 PDX - NR 2 ENGINE FEATHERED (UNSCHEDULED) IN FLIGHT WHEN FLAPS SELECTED 35 DEGREES AT 1000 FT AGL ON FINAL APPROACH. CON TINUED LANDING UNEVENTFULLY. REPLACED NR 2 PEC NO HELP. FINAL FIX REPLACED PCU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P17BO 2002072500041 20020725 00041 EA 2002 7 25 QXEA0200926 1 20020702 A 5270 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA FWD CARGO DOOR FALSE INDICATION A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 605QX 10022 SJC - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKE-OFF THE CREW RECEIVED A CAUTION LIGHT FOR THE FORWARD CARGO DOOR. MAIN TENANCE INSPECTED THE AIRCRAFT AND THE FORWARD CARGO DOOR PROXIMITY SENSORS. NO DISCREPANCIES WERE NOTED AND THE MDC VER IFIED CORRECT SENSOR STATUS. THE DOOR HANDLE RESET BUTTON WAS RESET AND A OPERATIONAL CHECK WAS COMPLIED WITH. OPERATION AL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002072500042 20020725 00042 NM 2002 7 25 QXEA0200927 1 20020704 A 2910 4213402 POWER UNIT BOMBDR DHC8 DHC8401 1390041 NM HYD SYSTEM FAILED A QXEA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 NM 09 405QX 2206 2206 4047 SEA - AIRCRAFT HAD AN UNCOMMANDED YAW ON TAKE-OFF ROLL. TAKEOFF AND LANDING WERE UNEVENTFUL. MAINTENANCE INSPECTED THE A IRCRAFT AND REPLACED THE HYDRAULIC POWER UNIT. OPERATIONAL AND FUNCTIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2002091700033 20020917 00033 NM 2002 9 17 QXEA0200928 1 20020705 A 5270 TARGET BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR OBSTRUCTED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 408QX 4050 PDX - AIRCRAFT RETURNED TO FIELD WHEN THE CREW RECEIVED A FUSELAGE DOORS WARNING ON ROTATION. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE FORWARD CARGO DOOR PROXIMITY SWITCH SAFETY WIRE OBSTRUCTING TARGET. THE PROXIMITY SWITCH WAS RE -SAFETY WIRED AND OPERATIONAL CHECKS WERE GOOD. NO PARTS WERE REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500043 20020725 00043 EU 2002 7 25 QXEA0200929 1 20020702 A 3350 1820 LIGHT FOKKER F28 F28MK4000 4990810 EU COCKPIT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 497US 11173 PDX-ONE COCKPIT EMERGENCY LIGHT UNDER GLARESHIELD ON F/O'S SIDE FAILS TO ILLUMINATE WHEN SELECTED ON. REPLACED 3RD FROM RIGHT EMERGENCY LIGHT ASSEMBLY UNDER GLARESHIELD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002072500044 20020725 00044 EA 2002 7 25 QXEA0200933 1 20020618 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 609QX 10031 PDX - LEFT SIDE OF FUSELAGE HAS DENT IN THE SKIN. DENT IS APPROXIMATELY 0.060 INCHES DEEP AND 4 INCHES LONG. DENT IS CE NTERED AT STATION 387.5 ABD US 10 INCHES BELOW CABIN WINDOW LOWER EDGE. AIRCRAFT WAS REPAIRED IAW EA R-53-021. 2 L 7 2 4F RT A21EA 2002072500045 20020725 00045 NM 2002 7 25 QXEA0200935 1 20020705 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - MULTIPLE DENTS FOUND ON LEFT SIDE OF FUSELAGE AFT OF THE ICE SHIELD. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND TO BE OK FOR CONTINUED SERVICE. THE DENTS WERE PLACED ON THE YELLOW DOT PROGRAM IAW EA 6-53-88 AND TO BE REPAIRED WITHIN 500 FLIGHT HOURS. 2 H 7 2 4T RT A13NM 2002072500046 20020725 00046 EA 2002 7 25 QXEA0200938 1 20020706 A 2150 ACM CNDAIR CL600 CL6002C10 1390015 EA ACM BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 605QX 10022 PDX-LOUVER MISSING FROM LEFT HAND AIR CYCLE MACHINE EXHAUST AND ONE LOUVER IS CRACKED. REPAIRED IAW CRJ-700 SRM 51-42-06 AND HORIZON AIR EA R-21-13A. 2 L 7 2 4F RT A21EA 2002072500047 20020725 00047 NM 2002 7 25 QXEA0200949 1 20020710 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 364PH 8900 524 SEA-AFT CABIN CEILING & AFT RIGHT HAND EXIT FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 4 POWER PACK & BATTERY. O PERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500048 20020725 00048 NM 2002 7 25 QXEA0200952 1 20020715 A 3350 10126271 LENS DHAV DHC8 DHC8202 2809007 NM CABIN MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PSC- EXIT LENS MISSING FROM RIGHT HAND UNDERWING EMERGENCY EXIT DOOR THRESHOLD LIGHT. REMOVED AND REPLACED LIGHT ASSEMBL Y. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500049 20020725 00049 NM 2002 7 25 QXEA0200953 1 20020714 A 3350 XD4N RELAY BOMBDR DHC8 DHC8401 1390041 NM CABIN MALFUNCTIONED A QXEA O OTHER O OTHER CR CRUISE 1 NM 09 409QX 4051 SEA- CABIN EMERGENCY LIGHTS CAME ON DURING TURBULENCE IN ARM. SWITCH DOES CONTROL ON AND OFF. REMOVED AND REPLACED 3351- K1 RELAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500050 20020725 00050 NM 2002 7 25 QXEA0200955 1 20020708 A 3350 61047811 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 375PH 6377 529 PDX-FORWARD EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2002072500051 20020725 00051 NM 2002 7 25 QXEA0200956 1 20020711 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM COCKPIT ILLUMINATED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 411QX 4055 BZN - AIRCRAFT RETURNED TO FIELD WHEN THE PITCH TRIM AND AUTO TRIM CAUTION LIGHT ILLUMINATED AT APPROXIMATELY 8500 FEET. AUTO PILOT WAS OFF. MAINTENANCE INSPECTED THE AIRCRAFT AND COMPLIED WITH SERVICE LETTER 8-400-SL-27-003 ATA 2730. OPERA TIONAL CHECK WAS GOOD AND NO CAUTION LIGHTS OR MESSAGES WERE NOTED BEFORE OR AFTER THE OPERATIONAL CHECK. THE AIRCRAFT W AS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500052 20020725 00052 EA 2002 7 25 QXEA0200959 1 20020715 A 2711 AL00102 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA AILERON TRIM FAILED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 613QX 306 306 10045 PDX - AIRCRAFT ABORTED TAKEOFF WHEN THE CREW RECEIVED A MASTER WARNING FOR TAKEOFF CONFIGURATION ON ROLL. MAINTENANCE RE PLACED THE AILERON TRIM ACTUATOR AND CHECKED WIRING IAW COMPLIANCE ORDER 052426. OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002072500053 20020725 00053 EA 2002 7 25 QXEA0200962 1 20020719 A 3150 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ILLUMINATED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 613QX 10045 LAX - AIRCRAFT ABORTED TAKEOFF WHEN THE MASTER WARNING FOR TAKEOFF CONFIGURATION, AILERON, WAS RECEIVED. MAINTENANCE INS PECTED THE AIRCRAFT AND COMPLIED WITH FIM TASK 27-11-00-810-802-A01. GROUND RAN ENGINES ABOVE 70 PERCENT AND NO TAKEOFF CONFIGURATION WARNING WAS NOTED. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002072500054 20020725 00054 EA 2002 7 25 QXEA0200963 1 20020720 A 3150 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ILLUMINATED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 613QX 10045 LAX - CREW ABORTED TAKEOFF WHEN THE MASTER WARNING FOR THE TAKEOFF CONFIGURATION, AILERON, WAS RECEIVED. MAINTENANCE INS PECTED THE AIRCRAFT AND COMPLIED WITH THE FAULT ISOLATION MANUAL, TASK 27-11-00-810-801-A01. TAKEOFF WARNING SYSTEM TEST ED GOOD. OPERATIONAL CHECK IS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002072500055 20020725 00055 NM 2002 7 25 QXEA0200964 1 20020715 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX- PITTING CORROSION ON RIGHT HAND INBOARD SEAT TRACK NUMBER 7 AT STATION 182-222. REPAIRED IAW DHC-8 SRM 51-40-00, 51 -40-11, RD 8-53-1339 AND RD 8-53-1102. 2 H 7 2 4T RT A13NM 2002072500056 20020725 00056 NM 2002 7 25 QXEA0200965 1 20020716 A 5540 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 PDX- AFT RUDDER IS CRACKED ON RT SIDE ABOUT 4 INCHES DOWN FROM TOP. REPAIRED IAW HORIZON AIR EA 6-55-13. 2 H 7 2 4T RT A13NM 2002072500057 20020725 00057 EA 2002 7 25 QXEA0201043 1 20020721 A 2840 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA CROSSFLOW PUMP ILLUMINATED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 602QX 10010 TUS- ABORTED TAKEOFF DUE TO A CROSSFLOW PUMP CAUTION MESSAGE WAS DISPLAYED, ALONG WITH BOTH LEFT AND RIGHT CROSSFLOW SEL ECT SWITCH LIGHTS DISPLAYING FAIL. THE CROSSFLOW PUMP ON THE FUEL SYNOPTIC IS AMBER. POWER DOWN AIRCRAFT AND RE-POWERED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED 2 L 7 2 4F RT A21EA 2002072500058 20020725 00058 WP 2002 7 25 GTIA020617 1 20020511 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND MID PIT CORRODED AT DOUBLER RAD ALT RCVR-2 AT 8 NUT PLATES RUSTED, STATION 712-731. REMOVED DOUBLER AND NUT PLATES. LOCATED AND DRILLED NEW PART. INSTALLED DOUBLER AND NUT PLATES. (M) 2 L 7 2 4F A6WE 2002072500059 20020725 00059 WP 2002 7 25 GTIA020618 1 20020520 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND E/E COMPARTMENT AFT PRESSURE BULKHEAD FRAME HAS CORROSION STATION 218 BETWEEN 27L FROM 26R, BEHIND. LOCATED AND DRILLED NEW SECTION FRAME. AFTER FURTHER EVALUATION, FOUND BRACKET ON STATION 218 UNDER INTERCOSTAL OUT OF LIMITS. DRILLED AND LOCATED NEW BRACKET. FORMED FRAME REPAIR. INSTALLED FRAME SPLICES. INSTALLED NEW BRACKET AT STATION 218 UNDER INTERCOSTAL. INSTALLED NEW SECTION OF FRAME AND SHEAR TIE (TWO EACH) SECTIONS OF WEB BULKHEAD ON LEFT AND RIGHT AT FS 218 PER SRM MD80 51-30-2. (M) 2 L 7 2 4F A6WE 2002072500060 20020725 00060 WP 2002 7 25 GTIA020619 1 20020517 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT CARGO FRAME STATION 1309 HAS CORROSION. REMOVED CORROSION. LOCATED AND DRILLED THE NEW FRAME. INSTALL ED FRAME. (M) 2 L 7 2 4F A6WE 2002072500061 20020725 00061 WP 2002 7 25 GTIA020621 1 20020512 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - AFT CARGO STATION 1231 INTERCOSTAL ASSEMBLY HAS CORROSION. REMOVED CORROSION FROM INTERCOSTAL ATTACHING T-ANGLES. FABRICATED 2 T-ANGLES. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002072500062 20020725 00062 WP 2002 7 25 GTIA020622 1 20020510 A 5314 KEELBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND MID PIT CORRODED AT LONGERON 30 STATION 788. LOCATED AND DRILLED KEEL BEAM FITTING. INSTALLED KEEL BEAM FI TTING. CORROSION FOUND ON 2 LEGS OF FORMER. LOCATED AND DRILLED REPAIR FORMERS. INSTALLED REPAIR PARTS ON FORMER. RE MOVED SUPPORT ANGLES AT STATION 788 FRAME ASSEMBLY L27L AND L27R. MATERIAL FOUND TO BE OUT OF LIMITS. FORMED REPAIR AN GLES. INSTALLED REPAIR ANGLES AT STATION 788 L27L AND L27R. (M) 2 L 7 2 4F A6WE 2002072500064 20020725 00064 NM 2002 7 25 UPS02238838 1 20020617 A 5511 SPAR BOEING 727 72722C 138400F NM HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI HORIZONTAL STAB RT SIDE FRONT SPAR LOWER CHORD IS CRACKED AT STAB STA 60.28. FRONT SPAR WEB SECTIO N CUT FROM ST 82.16 AND 44.6 IAW SRM 51-10-0, DAMAGED SECTION OF CHORD REMOVED IAW SRM 51-10-01, REPAIR PARTS FABRICATED IAW BOEING TELEX SRV-SNN-02-00101H 00102H 00116H AND UPS AUTHORIZATION 727-55-20008. 2 L 7 3 4F A3WE 2002072500065 20020725 00065 NM 2002 7 25 UPS02238841 1 20020612 A 5740 69139004 PIN BOEING 727 72722C 138400F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CORROSION ON RT WING FRONT SPAR BOTTLE PIN HEAD AFT FLANGE. BOTTLE PIN REPLACED IAW MM57-41-01. 2 L 7 3 4F A3WE 2002072500066 20020725 00066 NM 2002 7 25 UPS02238842 1 20020614 A 5755 65173522 CASTING BOEING 727 72722C 138400F NM SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI NR 12 SPOILER SUPPORT CASTING O/B ATTACH ANGLE LWR HOLE HAS CRACK INDICATION. SUPPORT CASTING REPL ACED IAW SRM 51-30-02 2 L 7 3 4F A3WE 2002072500067 20020725 00067 NM 2002 7 25 UPS02238844 1 20020627 A 5230 DOOR FRAME BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI SUSPECT CRACKS ON 2 FRAMES AND FRAME ATTACH ANGLES ON OUTER FACE OF AFT CARGO DOOR. FRAMES AND ANG LES REPLACED IAW DWG 65-18625, LOWER FRAME REPAIRED IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2002072500068 20020725 00068 NM 2002 7 25 UPS02238845 1 20020611 A 5320 CLEVIS BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI CORROSION AT RT BS 870 FRAME SPLICE ON WW WALL WBL 60 APPROX. CORROSION LOCATED ON HORIZONTAL CLEV IS FLANGES, CRACKS ALSO LOCATED. CORROSION AND CRACKS BEYOND LIMITS. 870 RT CLEVIS REPAIRED IAW SB 727-53-0077 R2 AND B OEING INSTRUCTIONS SRV-SNN-02-00105H, 00133H AND UPS AUTHORIZATION 727-53-20063. 2 L 7 3 4F A3WE 2002072500069 20020725 00069 NM 2002 7 25 UPS02238846 1 20020610 A 5311 FRAME BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI NOSE LANDING GEAR BAY, EVIDENCE OF CORROSION IN TORQUE BOX AREA. ARE A JUST AFT OF LT FWD NLG DOOR AT BS 288 LT. CORROSION REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-1. OLD CHORD REMOVED IAW SRM 51-30-2 AND NEW CHORD DRILLED OFF IAW DWG 6 5-18415. NEW CHORD INSTALLED IAW DWG 65-18415 AND SRM 51-30-2. CRACK WAS THEN FOUND AT SKIN BS 350 LBL 18, NEW REPAIR INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 2002072500070 20020725 00070 NM 2002 7 25 UPS02238847 1 20020718 A 2612 CONTROL PANEL BOEING 727 72722C 138400F NM COCKPIT FAULTY A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 930UP 19096 INSPECTION TYPE:N/A WHEEL WELL FIRE LIGHT INDICATION ON TAKEOFF. RAN CHECKLIST FOR WW, FIRE LIGHT EXTINGUISHED. RETURN ED FOR LANDING. AFTER LANDING WHEEL WELL FIRE INDICATIONS RESUMED. NO FIRE OBSERVED. LANDED 1300 LBS OVER LANDING WEI GHT. REMOVED AND REPLACED FIRE DETECTION PANEL OPS CHECKS GOOD IAW 26-11-02. 2 L 7 3 4F A3WE 2002072500071 20020725 00071 NM 2002 7 25 UPS02238849 1 20020701 A 5343 65852081 FITTING BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI DURING RECTIFICATION UPPER LT AFT TENSION TIE FITTING FOUND CRACKED IN TAIL SKID UNIT CAVITY. UPPE R LT TENSION TIE REMOVED IAW SRM 51-30-02 UPPER LT TENSION TIE INSTALLED IAW 51-30-02. 2 L 7 3 4F A3WE 2002072500072 20020725 00072 NM 2002 7 25 C8GA20020009 1 20020723 A 2130 65627372 DUCT BOEING 727 727227 1384078 NM AC PIT BLOWN A C8GA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 15 308AS 43628 22002 Flt CCI723 from KBOS to KROS. After take off, in climb, @ FL250 and 280 knots, aircraft started to vibrate. reduced sp eed to 250 knots then heard 2 bangs from behind the Flight Engineer station. After second bang, aircraft would not main tain pressurization. Switched to STBY and closed the cargo heat outflow valve. At FL 4.0, outflow indicator went full open and aircraft depressurized completely. Aircraft returned to KBOS and landed without further incident. Found slat actuator panel on right wing loose. Resucured panel. Also found manifold duct blown. Repaired duct. Aircraft returne d to service. 2 L 7 3 4F A3WE 2002072500073 20020725 00073 NM 2002 7 25 SABA020074 1 20020720 A 3350 1306 LIGHT DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 801WP 086 FLIGHT 5015 FROM CLT TO AGS AIRCRAFT 801: DURING PRE-FLIGHT IN CHARLOTTE THE EMERGENCY FLOOR LIGHT AT ROW 7A WOULD NOT T EST. MAINTENANCE REMOVED AND REPLACED BULBS AND SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072500074 20020725 00074 NM 2002 7 25 UIEA200200024 1 20020528 A 5300 UNKNOWN SKIN PANEL BOEING 747 74747UF 1384949 NM PUNCTURED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 496MC 13983 29257 Fuselage Skin damaged from BS 460 to 480 from between Stringer 38R and 39R by cargo container during loading operation. Stringers 38R and 39R at this location deformed by container. Damaged skin area trimmed out. Damaged area of stringer 38 R trimmed out. Stringer 39R was straightened. Area NDT inspected after straightening. No cracks found. Repair doubler s, fillers and stringer repair sections fabricated and installed per standard practices. Briles fasteners used in fusela ge skin repair IAW SRM 53-00-03 Figure 204 2 L 7 4 4F RT 1384945 2002072500075 20020725 00075 WP 2002 7 25 AALA20020461 1 20020327 A 5345 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND GALLEY TIE DOWN FITTING CORRODED FORWARD OF NR 6 SEAT TRACK STATION 214. INSTALLED SERVICEABLE TIE DOWN FIT TING SRM 51-01. (M) 2 L 7 2 4F A6WE 2002072500076 20020725 00076 WP 2002 7 25 AALA20020462 1 20020327 A 5320 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND FLOORBEAM ATTACH ANGLE CRACKED IN RADIUS AT LOWER END, BELOW NR 2 SEAT TRACK, AT STATION 927. REMOVED AND R EPLACED ATTACH ANGLE, SRM 51-01. (M) 2 L 7 2 4F A6WE 2002072500077 20020725 00077 WP 2002 7 25 AALA20020463 1 20020325 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND GOUGE ON RIVET HEAD AND CUSP STATION 387 LEFT SIDE. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002072500078 20020725 00078 WP 2002 7 25 AALA20020464 1 20020328 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND CUSP CRACKED AT STATION 218 RIGHT AT NR 6 SEAT TRACK OUTBOARD ATTACH FASTENER. INSTALLED DOUBLER PER SRM 53 -01. (M) 2 L 7 2 4F A6WE 2002072500079 20020725 00079 WP 2002 7 25 AALA20020465 1 20020327 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND CRACK IN LONGERON 17L AT STATION 237. INSTALLED LONGERON SPLICE PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 2002072500080 20020725 00080 WP 2002 7 25 AALA20020466 1 20020306 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND LONGERON 4L CRACKED AT STATION 160. INSTALLED LONGERON SPLICE REPAIR AS PER SRM 53-02. (M) 2 L 7 2 4F A6WE 2002072500081 20020725 00081 WP 2002 7 25 AALA20020467 1 20020405 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND SCREW DAMAGE IN WEB AT STATION 1155 ABOVE L28R. INSTALLED FORWARD CORNER WEB SPLICE PER AARD 53-10-00-24. (M) 2 L 7 2 4F A6WE 2002072500082 20020725 00082 WP 2002 7 25 AALA20020468 1 20020325 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND SEAT TRACK NR 3 CORRODED AT STATION 1299-1300. REMOVED CORROSION INSTALLED PLUG REPAIR PER AARD 53-20-00-10 FIGURE 1 SHEET 1. (M) 2 L 7 2 4F A6WE 2002072500083 20020725 00083 WP 2002 7 25 AALA20020469 1 20020401 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND HEAVY CORROSION ON OUTBOARD LEG OF NR 5 SEAT TRACK AT CLIP NUT HOLE, STATION 204. INSTALLED REPAIR PER AARD 53-20-00-13 AND ESO 80559 DATED 03/28/02. (M) 2 L 7 2 4F A6WE 2002072500084 20020725 00084 WP 2002 7 25 AALA20020470 1 20020326 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 696-706. REMOVED CORROSION, CUT OUT DAMAGE FOR PLUG TREATED ALL METAL AND PRIMED. INSTALLED PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2002072500085 20020725 00085 WP 2002 7 25 AALA20020471 1 20020326 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 633-642. INSTALLED PLUG REPAIR PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2002072500086 20020725 00086 WP 2002 7 25 AALA20020472 1 20020327 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND SKIN CRACKED STATION 1380 LONGERON 14L. STOP DRILLED CRACK INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2 SHE ET 3. (M) 2 L 7 2 4F A6WE 2002072500087 20020725 00087 WP 2002 7 25 AALA20020474 1 20020415 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND GOUGE AT STATION 526 BETWEEN L29R AND L30. REPAIRED GOUGE AT STATION 526, L29R, L30 PER SRM 53-04, FIG 28. (M) 2 L 7 2 4F A6WE 2002072500088 20020725 00088 WP 2002 7 25 AALA20020475 1 20020402 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND 1.5 INCH DENT IN FUSELAGE SKIN AT STATION 1383 BETWEEN LONGERONS 8L AND 9L. CUT OUT DAMAGE, INSTALLED DOUBL ER AND FAIRING PIECE PER SRM 53-01 FIG 4, SHEET 3. (M) 2 L 7 2 4F A6WE 2002072500089 20020725 00089 WP 2002 7 25 AALA20020476 1 20020405 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND DEEP GOUGE IN FUSELAGE STATION 404, LONGERON 29L. REPAIRED WITH FINGER DOUBLER PER SRM 53-04 FIG 38 CONDITI ON 3. (M) 2 L 7 2 4F A6WE 2002072500090 20020725 00090 WP 2002 7 25 AALA20020477 1 20020328 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 FOUND SKIN CRACKED STATION 1380, LONGERON 14R. STOP DRILLED CRACK AND INSTALLED DOUBLER PER 53-01. (M) 2 L 7 2 4F A6WE 2002072500091 20020725 00091 WP 2002 7 25 AALA20020490 1 20020409 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND SKIN CRACKED AROUND FASTENER LONGERON 13L AT STATION 1380. REMOVED DAMAGE. DYE CHECK SKIN, INSTALLED DOUBL ER PER SRM 53-01 FIGURE 2. (M) 2 L 7 2 4F RT A6WE 2002072500092 20020725 00092 WP 2002 7 25 AALA20020491 1 20020410 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND SKIN AND FASTENER HEAD WORN STATION 1338 L5R. INSTALLED DOUBLER AND NEW FASTENERS PER SRM 53-04 FIG 12B SHE ET 7. (M) 2 L 7 2 4F RT A6WE 2002072500093 20020725 00093 WP 2002 7 25 AALA20020492 1 20020405 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 TUL - FOUND FUSELAGE SKIN GOUGE AT STATION 237 LONGERON 18L, DENT IN SKIN STATION 241 LONGERON 18 AND 19L, DENT IN SKIN STATION 247 LONGERON 18 AND 19L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B SHEET 34/AARD 53-30-00-11. (M) 2 L 7 2 4F RT A6WE 2002072500094 20020725 00094 WP 2002 7 25 AALA20020540 1 20020415 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP FS 1250 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND HOLE IN BELTFRAME STATION 1250 ABOVE LONGERON 28R. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER FILLER PLATE PER SRM 53-03. (M) 2 L 7 2 4F A6WE 2002072500095 20020725 00095 WP 2002 7 25 AALA20020541 1 20020424 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AA 49343 TUL - FOUND CORROSION IN CENTER OF LONGERON 30 AT STATION 1287. CUT OUT CORRODED SECTION AND INSTALLED NEW SECTION AND SPLICED PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 2002072500096 20020725 00096 NM 2002 7 25 AALA20020552 1 20020425 A 5610 WINDOW BOEING 757 757223 1384957 NM COCKPIT CRACKED A AALA H B DEACTIVATE SYST/CIRCUITS EMER. DESCENT B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 660AM 25294 ORD - FLT 1876 - EN ROUTE LAX-ORD, CRUISING AT 37,000 FEET, FRONT RIGHT COCKPIT WINDOW BEGAN TO ARC AND BURNED LINE THRO UGH LAMINATE. WINDOW HEAT WAS TURNED OFF SHORTLY AFTER A LOAD POP AND LAMINATE OR OUTER PAIN SHATTERED. PERFORMED EMER GENCY DESCENT AND SLOWED TO 250 KNOTS AND CONTINUED TO ORD. LANDED ORD WITHOUT INCIDENT. REPLACED R-1 WINDOW PER MM 56 -11-01-4. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002072500097 20020725 00097 NM 2002 7 25 AALA20020575 1 20020501 A 2530 COFFEEMAKER BOEING 757 757223 1384957 NM GALLEY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 650AA 24608 SJU - FLT 623 - EN ROUTE SJU-FLL - FLIGHT ATTENDANT REPORTED SMOKE ODOR AROUND 2R AREA. AIR INTERRUPTED AND LANDED SJU WITHOUT INCIDENT. INSPECTED AREA AND FOUND BURNED TEA BAG RAPPER AND TIED RAP UNDER COFFEE MAKER IN THE MID GALLEY. RE MOVED BOTH COFFEE MAKERS AND CLEANED AREA. REPLACED BOTH COFFEE MAKERS AS PRECAUTIONARY ACTION. INSPECTED FORWARD CARG O AND E/E COMPARTMENT. NO EVIDENCE OF SMOKE. (M) 2 L 7 2 4F RT A2NM 2002072500098 20020725 00098 WP 2002 7 25 AALA20020623 1 20020508 A 2560 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 422AA 49334 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002072500099 20020725 00099 NM 2002 7 25 AALA20020630 1 20020509 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT AT 25H INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGH T CONNECTOR AT SEAT 25H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002072500100 20020725 00100 NM 2002 7 25 AALA20020631 1 20020512 A 3350 S283T0143 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 392AN 29429 MIA - DURING OVERNIGHT MAINTENANCE EMERGENCY ESCAPE PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY ESCAPE P ATH LIGHTS BATTERY PACK FOR FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002072500101 20020725 00101 NM 2002 7 25 AALA20020632 1 20020512 A 3350 S283T0143 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 377AN 25446 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS ROW 2H AND 8H INOPERATIVE. REPLACED EMERGENCY ESCAPE P ATH LIGHTS BATTERY PACK FOR ROWS 2H AND 8H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002072500102 20020725 00102 NM 2002 7 25 AALA20020633 1 20020509 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS COACH SECTION INOPERATIVE. REPLACED EMERGENCY ESCAPE P ATH LIGHTS BATTERY PACK FOR COACH SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002072500103 20020725 00103 EU 2002 7 25 AALA20020641 1 20020511 A 2913 O-RING FOKKER F28 F28MK0100 4990807 EU HYD PUMP DAMAGED A AALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 21 1442E 11437 TUL - FLT 560 - EN ROUTE TUL-ORD, GEAR DOORS WOULD NOT RETRACT DUE TO LOSS OF HYDRAULIC PRESSURE. RETURNED TUL AND LAND ED WITHOUT INCIDENT. REPLACED O-RING ON NR 1 ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002072500104 20020725 00104 WP 2002 7 25 GTIA020623 1 20020511 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND MID PIT CORROSION AT RIGHT CARGO TRACK STATION 636 TO 617. REMOVED Z-ANGLE. FABRICATED NEW Z-ANGLE. INSAT LLED NEW Z-ANGLE. INSTALLED NEW Z-ANGLE. (M) 2 L 7 2 4F A6WE 2002072500105 20020725 00105 WP 2002 7 25 GTIA020624 1 20020508 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT PIT STATION 1203 L29L LOWER SURFACE OF LONGERON FLANGE CORRODED AROUND SPLICE FASTENERS. ADDITIONAL COR ROSION IN LONGERON STATION 1293-1155 AROUND FASTENERS. THE CORROSION ON LOWER SURFACE ON LONGERON FLANGE ARE OUT OF LIM ITS. FABRICATED LONGERON 29L SECTION FROM STATION 1146 TO STATION 1203 PER SPIRIT EA 5310-0217. FABRICATED LONGERON 29 L SPLICE. INSTALLED LONGERON 29L 1146-1203. (M) 2 L 7 2 4F A6WE 2002072500106 20020725 00106 WP 2002 7 25 GTIA020625 1 20020509 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT PIT STATION 1193-1212 L28L, LOWER SURFACE OF LONGERON FLANGE IS CORRODED AT SPLICE FASTENERS. REMOVED C ORROSION. AREA FOUND TO BE OUT OF LIMITS. REMOVED LONGERON FROM SPLICE. FABRICATED LONGERON SECTION STATION 1193-1212 PER SPIRIT AIRLINES EA 5310-0222. FABRICATED LONGERON L28 SPLICE. LOCATED AND DRILLED NEW LONGERON SPLICE STATION 119 3 TO 1212. INSTALLED SPLICE ON LONGERON 28 LEFT BETWEEN STATION 1193 TO 1212. INSTALLED LONGERON SECTION. (M) 2 L 7 2 4F A6WE 2002072500107 20020725 00107 EU 2002 7 25 QXEA0201058 1 20020723 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 BOI-BOTH MID CABIN EXIT SIGNS EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BOTH EMERGENCY EXIT SIGNS IN MID CABIN. OPERATIONAL CHECK GOOD. AORCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002072500108 20020725 00108 WP 2002 7 25 GTIA020626 1 20020509 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT PIT STATION 1131-1250 L30, AREAS OF CORROSION WITH PITTING IN LONGERON AROUND LONGERON TO SKIN FASTENERS , AND ON LWR SURFACE OF FLANGE AT SPLICE FASTENERS STATION 2002. REMOVED CORROSION. MATERIAL OUT OF LIMITS. REMOVED L ONGERON 30 FROM STATION 1117 TO STATION 1193. LOCATED AND DRILLED LONGERON SECTION. INSTALLED LONGERON 30 SECTION FROM STATION 1112-1193. (M) 2 L 7 2 4F A6WE 2002072500109 20020725 00109 WP 2002 7 25 GTIA020627 1 20020509 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND AFT PIT STATION 1174 AND 1193 L29R-L28R, STRAPS ON THRESHOLD CLOSURE WEB ARE CORRODED. REMOVED STRAPS FROM STATION 1174 AND 1193. FABRICATED STRAPS. INSTALLED STRAPS. (M) 2 L 7 2 4F A6WE 2002072500110 20020725 00110 WP 2002 7 25 GTIA020628 1 20020509 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - AFT PIT STATION 1231-1212 L29R, THRESHOLD/FLOORBOARD SUPPORT HAS AREAS OF CORROSION ON UPPER AND LOWER SURFACE. A FTER BLEND OUT AREA FOUND TO BE OUT OF LIMITS. FABRICATED FLOORBOARD SUPPORT 'T'. (M) 2 L 7 2 4F A6WE 2002072500111 20020725 00111 2002 7 25 GTIA020629 4 20020531 A 3460 4034241972 COMPUTER DOUG DC9 DC981 3022081 WP NR 1 INOPERATIVE A GTIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 23 810NK 15351 48015 ACY - FLT 259 - AUTO PILOT DOES NOT HOLD SELECTED VERTICAL SPD IN VERTICAL SPPED MODE OR SELECTED IAS MODE WHEN DESCENDI NG. FOUND INOPERATIVE DFGC COMPUTER NR 1 REMOVED AND REPLACED DFGC NR 1 AND RAN RETURN TO SERVICE TEST NO FAULT NOTED C HECKED GOOD. (M) 2 L 7 2 4F A6WE 2002072500112 20020725 00112 WP 2002 7 25 GTIA020631 1 20020606 A 3220 LANDING GEAR DOUG DC9 DC982 3022082 WP NLG VIBRATION A GTIA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 23 820NK 49126 FLL - FLT 380 - ON INITIAL TAKEOFF ROLL, A HARD SHIMMY SEEMING TO COME FROM THE NOSE WHEEL OCCURRED. ABORTED TAKEOFF AT 70 KNOTS. INSPECTED ALL TIRES AND BRAKES NO DEFECTS MWA'S. INSPECTED AND LUBRICATED NOSE LANDING GEAR. NO DEFECTS NO TED. (M) 2 L 7 2 4F A6WE 2002072500113 20020725 00113 WP 2002 7 25 GTIA020633 1 20020602 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 131NK 47605 FTW - FOUND CABIN EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRE IAW MD80 WDM 33-51-01. (M) 2 L 7 2 4F A6WE 2002072500114 20020725 00114 WP 2002 7 25 GTIA020634 1 20020608 A 1420 TERMINAL DOUG DC9 DC941 302207N WP A/C BAY DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 131NK 47605 FTW - FOUND TAIL COMP ESCAPE SLIDE EMERGENCY LIGHT INOPERATIVE, LEFT ONLY. TERMINAL LUG OF WIRE L9SV18 INSTALLED ON TB 53-156 FOUND DAMAGE. TERMINAL LUG REPLACED. (M) 2 L 7 2 4F A6WE 2002072500115 20020725 00115 NM 2002 7 25 2002UALA01071 1 20020623 A 2697 6130446514 WIRE HARNESS BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU PINCHED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 320UA 23952 DIVERTED UNDER AMBER ALERT DUE TO THE ILLUMINATION OF APU FIRE WARNING LIGHT. NORMAL LANDING. INSPECTED APU COMPARTMEN T AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. INSPECTED APU FIRE WARNING DETECTION SYSTEM AND FOUND PINCHED WI RES IN WIRE BUNDLE THAT GO TO PLUG D4816P. REPLACED APU FIRE BOTTLE AND SQUIB. REPLACED DAMAGED WIRE BUNDLE AND APU FI RE DETECTION SYSTEM CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500116 20020725 00116 NE 2002 7 25 2002UALA01072 2 20020623 A 7230 COMPRESSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 ENGINE STALLED A UALA J A DUMP FUEL UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 116UA 26908 COMPRESSOR STALL OF NR 1 ENGINE. ENGINE RECOVERED AND RESUMED NORMAL OPERATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2002072500117 20020725 00117 NM 2002 7 25 2002UALA01074 1 20020624 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 940UA 26675 STATION 178 BULKHEAD CHORD ANGLE CRACKED IN RADIUS, WL 207, AREA ON RIGHT HAND SIDE. MAJOR REPAIR ACCOMPLISHED. FRAME SPLICE FABRICATED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500118 20020725 00118 SO 2002 7 25 SWIA200210887 1 20020530 A 2120 ODOR EMB 120 EMB120ER 3260203 SO COCKPIT DETECTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 565SW 120340 DURING CRUISE A STRONG ELECTRICAL ODOR IN THE COCKPIT LASTED 1 MINUTE. NO ABNORMAL INDICATIONS ON GAUGES OR ELECTRICAL PANEL. LOWERED AND INSPECTED OVERHEAD AND CIRCUIT BREAKER PANELS. REMOVED PILOT AND COPILOT SIDE CONSOLE PANELS, INSPE CTED FOR SIGN OF OVERHEATED AND BURNED WIRES AND ELECTRICAL COMPONENTS. NO DISCREPANCIES NOTED. 2 L 7 2 4T RT A31SO 2002072500119 20020725 00119 NE 2002 7 25 2002UALA01075 2 20020624 A 7200 ENGINE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 804UA 759 RETURNED TO ORD UNDER AMBER ALERT DUE TO NR 2 ENGINE VIBRATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2002072500120 20020725 00120 NM 2002 7 25 2002UALA01077 1 20020624 A 2751 WARNING SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 335UA 24230 DURING DESCENT EXPERIENCED ASYMMETRICAL FLAP INDICATION PROBLEM. LANDED UNDER AMBER ALERT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500121 20020725 00121 NM 2002 7 25 2002UALA01078 1 20020624 A 2613 WARNING SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 355UA 24361 RETURNED TO FIELD DUE TO WING BODY OVERHEAT INDICATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500122 20020725 00122 2002 7 25 2002UALA01079 4 20020625 A 3442 RADAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 460UA 1248 RETURN TO FIELD DUE TO LOSS OF WEATHER RADAR. 2 L 7 2 4F 4 F RT A28NM E40NE 2002072500123 20020725 00123 NM 2002 7 25 2002UALA01080 1 20020626 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 CABIN RIGHT HAND CREASE BEAM HAS CORROSION AROUND 2 NUTPLATES STATION 1020 TO STATION 1029 RBL 64. MAJOR REPAIR ACCOMPL ISHED. REPLACED AND SPLICED IN NEW SECTION OF INNER CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072500124 20020725 00124 NM 2002 7 25 2002UALA01081 1 20020626 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 CABIN FLOOR CREASE BEAM WEB CORRODED AT STATION 1004 RBL 68 UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072500125 20020725 00125 NM 2002 7 25 2002UALA01082 1 20020627 A 5330 DOUBLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7455U 21909 SLIGHT EDGE DAMAGE TO REPAIR DOUBLER FOUND UNDER AFT PIT BELOW LOADING THRESHOLD. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND QUADRUPLER. 2 L 7 3 4F 4 F A3WE E2EA 2002072500126 20020725 00126 NM 2002 7 25 2002UALA01083 1 20020627 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7455U 21909 AFT PIT FRAME AT BODY STATION 950F BETWEEN STRINGER 27L AND 28L, FRAME AND SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHE D. REPAIRED SHEAR TIE. 2 L 7 3 4F 4 F A3WE E2EA 2002072500127 20020725 00127 NM 2002 7 25 2002UALA01084 1 20020627 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 395UA 24670 BODY STATION 191 WL 207 STRINGER 17R STRINGER CRACKED BETWEEN RIVET HOLES. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED NEW PARTS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500128 20020725 00128 NM 2002 7 25 2002UALA01085 1 20020627 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 FORWARD PIT STATION 500 LBL 1 BILGE AREA FRAME CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500129 20020725 00129 NM 2002 7 25 2002UALA01086 1 20020627 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 MLG CEILING HAS CRACK FORWARD AND OUTBOARD OF AILERON TOWER SHAFT. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOU BLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500130 20020725 00130 NM 2002 7 25 2002UALA01087 1 20020627 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 RIGHT HAND FUSELAGE FRAME AT STATION 294.5 CRACKED JUST ABOVE FLOOR. THIS IS THE FORWARD GALLEY DOOR CUTOUT FORWARD FRA ME. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500131 20020725 00131 NM 2002 7 25 2002UALA01088 1 20020627 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 FUSELAGE FRAME WEB CRACKED AT STATION 847 STRINGER 9L AT SIDEWALL VENT ATTACH BRACKET FASTENER. MAJOR REPAIR ACCOMPLISH ED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500132 20020725 00132 NM 2002 7 25 2002UALA01089 1 20020627 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 FUSELAGE FRAME WEB CRACKED STATION 847 STRINGER 9R AT SIDEWALL VENT ATTACH BRACKET FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500133 20020725 00133 NM 2002 7 25 2002UALA01090 1 20020627 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 FUSELAGE FRAME WEB CRACKED STATION 827 STRINGER 9R AT SIDEWALL VENT ATTACH BRACKET FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500134 20020725 00134 NM 2002 7 25 2002UALA01091 1 20020628 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 FUSELAGE FRAME WEB CRACKED STATION 867 STRINGER 9R AT SIDEWALL VENT ATTACH BRACKET FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500135 20020725 00135 NM 2002 7 25 2002UALA01092 1 20020627 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 CABIN FLOOR BODY STATION 365 T-CAP IS CORRODED FROM BL 0 TO RBL 62. MAJOR REPAIR ACCOMPLISHED. REPLACED T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072500136 20020725 00136 NM 2002 7 25 2002UALA01093 1 20020628 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 FUSELAGE FRAME WEB CRACKED AT STATION 827 S9L AT SIDEWALL VENT ATTACH BRACKET FASTENER IN CABIN. MAJOR REPAIR ACCOMPLIS HED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500137 20020725 00137 NM 2002 7 25 2002UALA01094 1 20020629 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 AFT GALLEY DOOR THRESHOLD ANGLE HAS CORROSION FROM STATION 960-986. MAJOR REPAIR ACCOMPLISHED. REPLACE RIGHT HAND ZEE ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072500138 20020725 00138 WP 2002 7 25 P2EA2002M049 1 20020716 A 7100 JT8D219 ENGINE DOUG DC9 DC982 3022082 WP A P2EA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 CE 05 141NJ 49932 During flight from LGA to MCI the right engine flamed out at 35,000 ft. Attempt to re-start was unseccessful. Performed unscheduled landing at PIT without incedent. Removed and replaced right engine IAW Job Card 80VG-1A-1. This closes SDR . ..M049. 2 L 7 2 4F A6WE 2002072500139 20020725 00139 EA 2002 7 25 COMA0260448 1 20020722 A 5324 ANGLE CNDAIR CL600 CL6002B19 1900309 EA F.S. 484 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 713CA 9298 7245 THE ANGLES AT BL 27 LH AND RH AND INTERCOSTAL AT RBL 36 AT FS 484 WERE FOUND CRACKED.REMVOED DISCREPANT PARTS, FABRICATE D AND INSTALLED AND REPLACEMENT PARTS I/A/W WVAC EO 601R-53-3380 DATED 07/22/02. 2 L 7 2 4F RT A21EA 2002072500140 20020725 00140 EA 2002 7 25 COMA0260449 1 20020723 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA F.S 310.00 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 713CA 9298 7245 PAX DOOR NIB IS DAMAGED AT F.S. 310.00CUT OUT DAMAGE AND INSTALLED STRAP P/N 601R-52-11-008-1 I/A/W CRJ EO 601R-52-11-00 8 REV B REPAIR A. 2 L 7 2 4F RT A21EA 2002072500141 20020725 00141 EA 2002 7 25 COMA0260450 1 20020724 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 713CA 7245 I/H WING LOWER SKIN FUEL PANEL LANDINGS @ W.S. 106.40, 127.25, 264.00 AND 294.50 HAVE CORROSION FROM 0.010" - 0.012" DEE P.REMOVED CORROSION BY BLENDING. PERFORMED EDDY CURRENT INSP TO ENSURE COMPLETE DAMAGE REMOVAL. FLAP PEENED RE-WORKED AR EAS, AND REAPPLIED PROTECTIVE FINISH. ALL WORK WAS PERFORMED I/A/W BOMBARDIER INC. REO 601R-57-21-030 REV A DATED 06 NOV 98. 2 L 7 2 4F RT A21EA 2002072500142 20020725 00142 EA 2002 7 25 COMA0260451 1 20020723 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 962CA 13257 7123 FLIGHT 5085 FLAPS FAILED AT 45 DEGREES.REPLACED THE L/H BPSU. 2 L 7 2 4F RT A21EA 2002072500143 20020725 00143 EU 2002 7 25 MALA020430 1 20020721 A 3260 GJ9 PROXIMITY SWITCH BAC 146 AVRO146RJ85A 1500097 EU A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 520XJ E2345 DURING FLIGHT #3571, NOSE GEAR DOWN INDICATION REMAINED ILLUMINATED AFTER GEAR SELECTED UP. RIGHT MAIN GEAR INTRANSIT R EMAINED ILLUMINATED AFTER GEAR SELECTED UP. MAINTENANCE REPLACED PROXIMITY SWITCH AT GJ9 SEE 409 #149298 FOR DETAILS. 2 H 7 4 4F RT A49EU 2002072500144 20020725 00144 EU 2002 7 25 MALA020432 1 20020724 A 2611 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU E&E BAY MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 48XJ DURING FLIGHT 2920, AVIONICS SMOKE LIGHT ILLUMINATED. NO SMOKE VIEWED BY CREW. CREW DECIDED TO RETURN TO MSP. MAINTEN ANCE DEFERRED SMOKE DETECTION SYSTEM. 2 L 7 2 4T RT A52EU 2002072500145 20020725 00145 NM 2002 7 25 PCAA0207080 1 20020723 A 2910 A44700009 ACTUATOR DHAV DHC8 DHC8102 2809003 NM CRACKED A PCAA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 EA 13 810EX 26874 26874 308 #1 HYDRALIC ISOLATION VALVE LIGHT ILLUMINATED PRYER TO FLIGHT, HYD RIGHT LEFT WING. INSPECTED AND FOUND RIGHT INBOARD RO LL SPOILER ACTUATOR BODY CRACKED AND LEAKING. REMOVED AND REPLACED ACTUATOR I.A.W. -8 MAINT MANUALL 27-14-05. OPPS AND L EAK CHECKS OK. 2 H 7 2 4T RT A13NM 2002072600001 20020726 00001 WP 2002 7 26 CNMA200200005 1 20020713 A 2612 CIRCUIT BREAKER DOUG DC10 DC1010 3022110 WP A CNMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 07 450AX 46942 On taxi out #2 Engine fire warning C/B popped (1 reset), Pilot overhead B20. 2 L 7 3 4F A22WE 2002072600002 20020726 00002 WP 2002 7 26 CNMA200200006 1 20020713 A 2612 LIGHT DOUG DC10 DC1010 3022110 WP A CNMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 07 450AX 46942 On taxi out fire-X handle & Fuel lever lights C/B Engine #2 opened. 2 L 7 3 4F A22WE 2002072600003 20020726 00003 NM 2002 7 26 SWAA021574 1 20020716 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED C2 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED IN CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2002072600004 20020726 00004 NM 2002 7 26 SWAA021576 1 20020716 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EXIT LENS PER MM. 2 L 7 2 4F RT A16WE 2002072600005 20020726 00005 NM 2002 7 26 SWAA021577 1 20020715 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK AT BS 500B PLUS 14, ABOVE STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2002072600006 20020726 00006 NM 2002 7 26 SWAA021579 1 20020717 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 520, WL 255, RT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002072600007 20020726 00007 NM 2002 7 26 SWAA021580 1 20020717 A 5330 6545776 SKIN BOEING 737 7372K6 1364440 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 129SW 22340 DURING WALK AROUND INSPECTION, FOUND RT FUSELAGE SKIN CRACKED BETWEEN BS 907 AND BS 927, WL 170. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002072600008 20020726 00008 2002 7 26 SWAA021569 4 20020714 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 420WN 29825 AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002072600009 20020726 00009 NM 2002 7 26 SWAA021571 1 20020715 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) 1.5 LONG AT STR 10R, BS 382, BS 500 PLUS 5 AND BS 500 PLUS 13. REPAIRED SKIN PER SWA RA AND SRM. 2 L 7 2 4F RT A16WE 2002072600010 20020726 00010 NM 2002 7 26 SWAA021573 1 20020716 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) ABOVE STR 10L AT BS 455 AND BS 500 PLUS 4. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2002072600011 20020726 00011 2002 7 26 SWAA021594 4 20020718 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002072600012 20020726 00012 2002 7 26 SWAA021598 4 20020718 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002072600013 20020726 00013 2002 7 26 SWAA021601 4 20020717 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 071SW 22358 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F A16WE 2002072600014 20020726 00014 NM 2002 7 26 SWAA021607 1 20020720 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 EEPLS WIRES EXPOSED AT ROW NR 7. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002072600015 20020726 00015 NM 2002 7 26 SWAA021609 1 20020720 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002072600016 20020726 00016 NM 2002 7 26 SWAA021610 1 20020720 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002072600017 20020726 00017 NM 2002 7 26 SWAA021611 1 20020720 A 5510 65C25727 SKIN BOEING 737 7373H4 1384600 NM RT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPECIAL VISIT, FOUND LOWER SKIN CRACKED ON RT HORIZ STAB AFT SPAR AT NR 1 BALANCE BAY. REPAIRED SKIN P ER SWA EA. 2 L 7 2 4F RT A16WE 2002072600018 20020726 00018 NM 2002 7 26 SWAA021612 1 20020720 A 5241 65505734 GATE BOEING 737 7375H4 138449D NM FWD SVC DOOR OUT OF ADJUST A SWAA D RETURN TO BLOCK O OTHER CL CLIMB 1 SW 29 504SW 24181 AIR TURNBACK, DURING CLIMB ABRUPTLY EXTREMELY LOUD NOISE COMING FROM FWD SVC DOOR. ADJUSTED LOWER GATE ON DOOR PER MM. 2 L 7 2 4F RT A16WE 2002072600019 20020726 00019 NM 2002 7 26 SWAA021613 1 20020721 A 5311 6546536 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) AT BS 493, WL 161 RT AND BS 616, WL 202 RT. REPAIRED FRA MES PER SRM. 2 L 7 2 4F RT A16WE 2002072600020 20020726 00020 NM 2002 7 26 SWAA021615 1 20020721 A 5311 6546529 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND SHEAR TIES CORRODED (2 EA) AT BS 460, BETWEEN STR 26L AND 27L AND BS 787, BETWEEN STR'S 26L AND 27L. REPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2002072600021 20020726 00021 NM 2002 7 26 SWAA021616 1 20020721 A 5310 6547978 CREASE BEAM BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CRACKED AT BS 520, WL 280 AND LBL 65. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2002072600022 20020726 00022 NM 2002 7 26 SWAA021618 1 20020721 A 5315 6546804 FLOORBEAM BOEING 737 7373T5 1384608 NM FWD CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 294, WL 208 AND LBL 38. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2002072600023 20020726 00023 NM 2002 7 26 SWAA021624 1 20020722 A 5320 6547978 CREASE BEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 287, WL 208 AND RBL 53. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2002072600024 20020726 00024 NM 2002 7 26 SWAA021625 1 20020722 A 5320 6547978 CREASE BEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 913,WL 208 AND LBL 58. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2002072600025 20020726 00025 NM 2002 7 26 SWAA021626 1 20020722 A 5320 6546529 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, WL 149 RH SIDE. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002072600026 20020726 00026 NM 2002 7 26 SWAA021628 1 20020722 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FWD CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 328, BL 0.0. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2002072600027 20020726 00027 NM 2002 7 26 SWAA021631 1 20020720 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) ABOVE STR 10L, BS 520 PLUS 5 AND BS 500C PLUS 13. RE PAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002072600028 20020726 00028 NM 2002 7 26 SWAA021632 1 20020720 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 510, ABOVE STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002072600029 20020726 00029 NM 2002 7 26 SWAA021634 1 20020720 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727E PLUS 6, ABOVE STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002072600030 20020726 00030 NM 2002 7 26 SWAA021635 1 20020721 A 5330 589358 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT UPPER CORNER OF R-1 COCKPIT WINDOW. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2002072600031 20020726 00031 2002 7 26 C2XA02CL154 4 20020724 A 2330 28EB12E120 CONVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 22909 145459 CLE FLIGHT# 3246 THE CREW REPORTED AFTER LANDING THE F/A SMELLED SMOKE FROM THE CD PLAYER AND THE CIRCUIT BREAKER WAS PO PPED.MAINTENANCE INSPECTED AND REPLACED THE DC POWER CONVERTER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FO R SERVICE. 2 L 7 2 4T RT T00011AT 2002072600032 20020726 00032 WP 2002 7 26 CALA0200427 1 20020724 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND L/H CENTER SEAT TRACK CORRODED AT STA 1070. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 2002072600033 20020726 00033 WP 2002 7 26 CALA0200429 1 20020724 A 5320 ANGLE DOUG DC9 DC982 3022082 WP L2 DR JAMB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND L-2 DOOR JAMB ANGLE AT FORWARD LOWER CORNER CORRODED AT LOWER END, STA 1136. THE CORRODED SECTION OF AN GLE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW ECRA 5311-01130. 2 L 7 2 4F A6WE 2002072600034 20020726 00034 WP 2002 7 26 CALA0200430 1 20020725 A 5210 SKIN DOUG DC9 DC982 3022082 WP L-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND A 1/4" CRACK AT RIVET IN L-1 DOOR SKIN AND THE CORNER WAS BENT. THE CRACK WAS LOCATED AT THE UPPER AFT CORNER OF DOOR. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 32 AND 51-10-3B. 2 L 7 2 4F A6WE 2002081500124 20020815 00124 NM 2002 8 15 F3LA200200199 1 20020722 A 5320 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED A CRACK IN TIE CLIP TO STRINGER AT STATION 540, STRINGER 5R. MAINTENANCE REMOVED AND REPLACED STRINGER CLIP, IN ACCORDANCE WITH SRM 51-40-02 AND 51-20-01 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002081500125 20020815 00125 NM 2002 8 15 F3LA200200200 1 20020722 A 5313 STRINGER BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED A CRACK IN TIE CLIP TO STRINGER AT STA 616, STR 4R. MAINTENANCE REMOVED AND REPLA CED CRACKED STRINGER WITH NEW PART IN ACCORDANCE WITH SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002072600035 20020726 00035 WP 2002 7 26 ZW0A0207701 1 20020722 A 2612 474007 PANEL DOUG DC9 DC983 3022083 WP A ZW0A A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 CE 13 9405T 53141 THE MID CARGO COMPARTMENT SHOWED FIRE INDICATION. ONE FIRE BOTTLE WAS DISCHARGED AND THE FLIGHT MADE AN UNSCHEDULED LAN DING AT DFW. THERE WAS NO INDICATION OF FIRE. CORRECTIONS TO THE INDICATION PROBLEM WAS DEFERRED PER MEL. THE COCKPIT CONTROL PANEL WAS LATER REPLACED. CHECK-C 10-01-01 MCI. --CLOSED-- 2 L 7 2 4F RT A6WE 2002072600036 20020726 00036 NM 2002 7 26 UPS02438893 1 20020704 A 5310 WEB BOEING 747 747123F NM LH BLG W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C LH BLG W/W - CEILING COR CRACK AT FS 1355, LBL 76. PRESSURE WEB REPAIRED AT BS 1335-1375 LBL 55 - LBL 80 AS PER SRM 53-10-07 FIG 2. 2 L 7 4 4F A20WE 2002072600037 20020726 00037 NM 2002 7 26 SABA020075 1 20020724 A 3350 1306 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 AIRCRAFT 882 ON FLIGHT 5014 FROM CLT TO AGS, DURING PRE-FLIGHT THE CREW REPORTED THAT THE OVERHEAD EMERGENCY LIGHT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED BULBS AND SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072600038 20020726 00038 NM 2002 7 26 SABA020076 1 20020725 A 3350 1305 LIGHT DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 882CC 168 FLIGHT 5054 AIRCRAFT 883 FROM CLT TO PGV, AIRCREW REPORTED THAT THE RED FLOOR LIGHTS IN FRONT OF THE CABIN WOULD NOT TES T. MAINTENANCE REMOVED AND REPLACED BULBS AND SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002072600039 20020726 00039 EU 2002 7 26 AWXA200200664 1 20020725 A 2780 NAS16128 O-RING AIRBUS 320 A320231 3930325 EU ZONE 140 LEAKING A AWXA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 WP 28 628AW 0 0 67 PHX - AIR TURN BACK - FLT 0175 - EN ROUTE FROM PHX TO MEX IN CRUISE ECAM INDICATION FOR GREEN HYDRAULIC SYSTEM LOW LEVEL FOLLOWED BY ECAM HYDRAULIC LEVEL IN AMBER. ON RETURN TO PHX TURNED ON GREEN PUMP / PTU AUTO PER ECAM INSTRUCTIONS AND R ECOVERED NORMAL PRESSURE. LOWERED LANDING GEAR AND RECOVERED 1/2 OF HYDRAULIC QUANTITY, NO FURTHER HYDRAULIC LOSS. LANDE D SAFELY AT PHX, AIRCRAFT TOWED TO GATE. MAINTENANCE FOUND HYDRAULIC LEAK AT SLAT POWER CONTROL UNIT ON R/H SIDE LOWER F LEX LINE UNION. REPLACED O-RINGS ON FLEX LINE UNIONS. OPERATIONAL AND LEAK CHECK WAS GOOD PER 27-84-00-710-001. PART NAM E; O-RING, MFG; NATIONAL AEROSPACE STANDARDS (NAS), P/N; NAS1612-6, COND; LEAKING, LOC; ZONE 140. 2 L 7 2 4F RT A28NM 2002072600040 20020726 00040 EU 2002 7 26 AWXA200200665 1 20020725 A 3350 E0052R8B3APNE CONNECTOR AIRBUS 320 A320231 3930325 EU SEAT ROW 26 L/H. BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 637AW 0 0 099 PHX - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPLACE D CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 L/H PER SWPM, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 2002072600041 20020726 00041 NM 2002 7 26 AWXA200200666 1 20020723 A 3350 20121 CHARGER BOEING 757 7572G7 1384963 NM STA 1663 DEFECTIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 0 0 24522 LCQ - EEL - DURING C-11 CHECK EMERGENCY EXIT LIGHTS AND SLIDE LIGHTS AT THE L4/R4 DOOR INOP ALSO AFT SECTION OF EMERGENC Y ESCAPE PATH SEAT MOUNTED LIGHTS WILL NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE AFT SEAT LIGHT BATTERIES AND B ATTERY CHARGER ASSEMBLY, OPERATIONAL CHECK WAS GOOD IAW B757 MM 33-51-07, PG. 203-207. 2 L 7 2 4F RT A2NM 2002072600042 20020726 00042 NM 2002 7 26 AWXA200200668 1 20020705 A 5311 6545807U79 FRAME BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/2" CRACK WAS FOUND ON THE R1 DOOR FRAME AND SUPPORT ANGLE AT THE LOWER FORWAR D DOOR CUTOUT, BS 294.5. MAINTENANCE REMOVED R1 DOOR LOWER FORWARD STUB FRAME, SUPPORT ANGLE, AND DOOR STOP FITTING. FAB RICATED A NEW SUPPORT ANGLE AND FRAME, REINSTALLED DOOR STOP FITTING, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40- 02, AND DWG 69-37402. 2 L 7 2 4F RT A16WE 2002072700001 20020727 00001 CE 2002 7 27 GUUA07270202 1 20020722 A 2730 50524537 GEAR BEECH 1900 1900D 1154162 CE DIRTY A GUUA K NONE O OTHER DE DESCENT 1 SO 17 16540 UE172 CAPTAINS ELECTRIC TRIM SWITCH STICKS.CLEANED AND LUBED TRIM WHEEL 2 L 7 2 4T RT A24CE 2002072700002 20020727 00002 CE 2002 7 27 GUUA07270203 1 20020721 A 2720 S77170 KNOB BEECH 1900 1900D 1154162 CE LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87555 11964 UE234 RUDDER TRIM KNOB LOOSETIGHTENED TRIM KNOB SET SCREW 2 L 7 2 4T RT A24CE 2002072700003 20020727 00003 CE 2002 7 27 GUUA07270204 1 20020723 A 2720 S77170 KNOB BEECH 1900 1900D 1154162 CE LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87550 12668 3 UE205 RUDDER TRIM KNOB LOOSETIGHTENED SET SCREW IN KNOB 2 L 7 2 4T RT A24CE 2002072700004 20020727 00004 CE 2002 7 27 GUUA07270206 1 20020720 A 6120 11236401733 CONNECTOR BEECH 1900 1900D 1154162 CE Zone 200 LOOSE A GUUA K NONE O OTHER CR CRUISE 1 SO 17 87550 12648 17 UE205 LEFT AUTOFEATHER ANNUNCIATOR INTERMITTENT IN FLIGHTRSECURED ELECTRICAL CONNECTOR AT RELAY 2 L 7 2 4T RT A24CE 2002072700005 20020727 00005 CE 2002 7 27 GUUA07270207 1 20020722 A 2710 MS276456A BEARING BEECH 1900 1900D 1154162 CE WORN A GUUA K NONE E VIBRATION/BUFFET CR CRUISE 1 SO 17 53545 17297 2 UE185 INTERMITTENT VIBRATION FELT IN CONTROL WHEEL IN FLIGHTDETERMINED RIGHT YOKE BEARING TO BE WORN, BUT WITHIN LIMITS. REP LACED RIGHT AILERON YOKE BEARING 2 L 7 2 4T RT A24CE 2002072700006 20020727 00006 CE 2002 7 27 GUUA07270208 1 20020716 A 2730 3094301 TRIM SWITCH BEECH 1900 1900D 1154162 CE DIRTY A GUUA K NONE O OTHER DE DESCENT 1 SO 17 87552 12369 UE216 ELECTRIC TRIM LOCKS TRIM IN POSITION. OPERATES NORMAL WHEN ELECTRIC TRIM IS DISENGAGEDCLEANED ELECTRIC TRIM SWITCH IN C APTAINS YOKE 2 L 7 2 4T RT A24CE 2002072700007 20020727 00007 2002 7 27 GUUA07270209 4 20020717 A 2210 STD97912 SWITCH BEECH 1900 1900D 1154162 CE DIRTY A GUUA K NONE O OTHER CR CRUISE 1 SO 17 87552 12379 UE216 YAW DAMPER DISENGAGES BOTH LEFT AND RIGHT, IN FLIGHTCLEANED CAPTAINS YOKE DISCONNECT SWITCH 2 L 7 2 4T RT A24CE 2002072700008 20020727 00008 CE 2002 7 27 GUUA07270212 1 20020716 A 2810 MS20426AD RIVET BEECH 1900 1900D 1154162 CE LEAKING A GUUA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 17 87550 12631 UE205 FUEL LEAKING FROM RIVET TOP OF LEFT WINGINSTALLED CLICK PATCH 2 L 7 2 4T RT A24CE 2002072900001 20020729 00001 SO 2002 7 29 SWIA200210888 1 20020601 A 2752 3082001007 ACTUATOR EMB 120 EMB120ER 3260203 SO LT TE FLAP MALFUNCTIONED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 196SW 5404 1881 120151 TRAILING EDGE FLAPS COME DOWN WITHOUT HYDRAULIC POWER. REMOVED AND REPLACED LT NACELLE FLAP ACTUATOR IAW MM 27-50-08. OPS CHECK AND LEAK CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002072900002 20020729 00002 SO 2002 7 29 SWIA200210889 1 20020530 A 2160 SQUAT SWITCH EMB 120 EMB120ER 3260203 SO AIR CONDITIONING MALFUNCTIONED A SWIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 196SW 120151 LEFT AND RIGHT PACKS FAILED ON THE GROUND WITH APU BLEED PACKS ON LOW. FOLLOWED QRH PROCEDURE. TURNED PACKS OFF, THEN ON. BOTH PACKS FAILED WITHIN 15 SECONDS AND SMOKE ENTERED THE CABIN. UPDATE 6/3: BOTH PACKS FAILED ON THE GROUND. RE MOVED AND REPLACED LEFT AND RIGHT PACK OVERTEMP SWITCHES. OPS CHECK GOOD. 6/3: REMOVED AND REPLACED GROUND PROXIMITY SENSOR AND HARNESS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002072900004 20020729 00004 SW 2002 7 29 2002F00765 1 20020702 A 5302 407023800129 SUPPORT FITTING BELL 407 407 1182206 SW TAILBOOM CRACKED B ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 409AL 769 53494 TAILBOOM SUPPORT FITTING CRACKED FROM EDGE THROUGH FIRST SCREW HOLE THEN UP RIVETED FLANGE BETWEEN 3RD AND 4TH FASTENER HOLES. CRACK APPEARS TO START FROM TOOLING MARKS DUE TO STRESS. INCREASE STRENGTH OF MATERIAL, POLISH EDGES TO REMOVE TOOLING MARKS, AND GET A CLOSER MATCH TO CONTOUR OF STABILIZER. SUPPORT ANGLE SENT TO MFG FOR EVALUATION AND WARRANTY C REDIT. 1 G 7 1 3U O H2SW 2002072900021 20020729 00021 SW 2002 7 29 ALG2002F00060 1 20020601 A 6210 206015001119 BLADE BELL 206 206L4 1182110 SW MAIN ROTOR DEBONDED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 177AL 673 52157 DISCOVERED DURING ROUTINE AIRFRAME INSPECTION. SPAR LEADING EDGE EXFOLIATED ALONG ENTIRE LENGTH OF BLADE, SKIN/SPAR DIS BOND AT LOWER SURFACE STA 58.5. CAUSED BY IMPROPER HEAT TREATING. C/A: REVIEW MANUFACTURING PROCESS AND IMPROVE QC. 1 G 7 1 3U NC H2SW 2002072900022 20020729 00022 SW 2002 7 29 ALG2002F00061 1 20020702 A 6230 406010419109 CAP BELL 407 407 1182206 SW SWASHPLATE CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 537AL 2495 53230 DURING DISASSEMBLY FOR 2500 HOUR OVERHAUL. EXCESSIVE CORROSION ON LOWER FLANGE MATING SURFACE OF SWASHPLATE. 1 G 7 1 3U O H2SW 2002072900023 20020729 00023 EA 2002 7 29 JEM2002F00002 2 20020621 A 7261 GASKET CHAMPION PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA OIL FILTER FAILED E JEMA K NONE O OTHER IN INSP/MAINT 1 CE 01 4118B 753 318452021 L175968A PILOT REPORTED LOSS OF OIL PRESSURE ON NR 2 ENGINE DURING CLIMB OUT AND SHUT ENGINE DOWN. AIRCRAFT RETURNED TO AIRPORT WITH OUT INCIDENT. UPON INSPECTION OF RIGHT ENGINE IT WAS NOTED THAT THE OIL FILTER MOUNTING PLATE GASKET WAS FOUND PRO TRUDING OUT FROM ITS INTENDED SEALING SURFACE ALLOWING LOSS OF OIL QUANTITY AND PRESSURE. FAILED PARTS WERE REMOVED AND REPLACED AND OIL QUANTITY SERVICED. AIRCRAFT WAS GROUND RUN, AND TEST FLOWN PRIOR TO RETURNING TO SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 2002072900024 20020729 00024 NM 2002 7 29 2002UALA01095 1 20020629 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 CABIN FUSELAGE FRAME WEB CRACKED AT STATION 887 S9L AT SIDEWALL VENT ATTACH BRACKET FASTENER. MAJOR REPAIR ACCOMPLISHED . INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900025 20020729 00025 NM 2002 7 29 2002UALA01096 1 20020629 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 CABIN FUSELAGE FRAME WEB CRACKED AT STATION 867 S9L AT SIDEWALL VENT ATTACH BRACKET FASTENER. MAJOR REPAIR ACCOMPLISHED . INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900026 20020729 00026 NM 2002 7 29 2002UALA01098 1 20020630 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 LEFT HAND EXTERNAL FUSELAGE SKIN DENTED AT STATION 999 JUST BELOW S14L. MAJOR REPAIR ACCOMPLISHED. NEW DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900027 20020729 00027 NM 2002 7 29 2002UALA01099 1 20020628 A 5313 STRINGER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7455U 21909 FORWARD PIT STRINGER 28R CORRODED ON LOWER SIDE AT BODY STATION 494. MAJOR REPAIR ACCOMPLISHED. SPLICE REPAIR. 2 L 7 3 4F 4 F A3WE E2EA 2002072900028 20020729 00028 NM 2002 7 29 2002UALA01100 1 20020628 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7455U 21909 FORWARD PIT INTERNAL SKIN STATION 500 AT STRINGER 28R IS BLENDED BEYOND LIMITS DUE TO CORROSION REMOVAL. MAJOR REPAIR A CCOMPLISHED. INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 3 4F 4 F A3WE E2EA 2002072900029 20020729 00029 NM 2002 7 29 2002UALA01101 1 20020628 A 5310 SHEAR TIE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7455U 21909 FORWARD CARGO PIT AT BODY STATION 480-500, STRINGER 28R, INTERCOSTAL LOWER FLANGE IS CORRODED AND SHEAR TIE CORRODED. M AJOR REPAIR ACCOMPLISHED. REPAIRED INTERCOSTAL LOWER FLANGE & SHEAR TIE. 2 L 7 3 4F 4 F A3WE E2EA 2002072900030 20020729 00030 NM 2002 7 29 2002UALA01102 1 20020628 A 2400 ELECTRICAL SYS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 WP 29 814UA 862 RETURNED TO ORD UNDER AMBER ALERT DUE TO ELECTRICAL PROBLEMS. 2 L 7 2 4F 4 F RT A28NM E40NE 2002072900031 20020729 00031 NM 2002 7 29 2002UALA01103 1 20020630 A 3020 21SN4152 PRESSURE SWITCH BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED A UALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 29 353UA 24321 LANDED DEN UNDER AMBER ALERT DUE TO A NR 1 ENGINE COWL ANTI-ICE WARNING LIGHT, WHICH CAUSED THE CREW TO SHUT DOWN THE EN GINE. PRESSURE SWITCH 21SN41-52 FAILED. MAINTENANCE REPLACED PRESSURE SWITCH, OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900032 20020729 00032 NM 2002 7 29 2002UALA01104 1 20020630 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 CABIN FLOORBEAM BODY STATION 310 FLOORBEAM HAS EXCESSIVE MATERIAL LOSS DUE TO CORROSION AT RBL 42 UPPER SURFACE T-CAP. MAJOR REPAIR ACCOMPLISHED. CUT OUT FILLER AND REINFORCE ANGLES. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072900033 20020729 00033 NM 2002 7 29 2002UALA01105 1 20020630 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 CABIN FLOOR BODY STATION 324 FLOORBEAM CAP AT RBL 41 TO RBL 43 HAS SURFACE CORROSION DAMAGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT, FILLER AND ANGLE INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072900034 20020729 00034 NM 2002 7 29 2002UALA01107 1 20020630 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 CABIN FLOORBEAM HAD EXCESS CORROSION AT STATION 740 RBL 62 STRINGER 17L, ALSO GUTTER UNDER STRUCTURE L-CHANNEL WAS CORRO DED STATION 740, 62 RBL. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SECTION OF INNER CREASE BEAM FROM 664 TO 756. A NEW UNDER GUTTER L-CHANNEL WAS FABRICATED, ALSO U-CHANNEL FOR BETWEEN STATION 720-740. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072900035 20020729 00035 NM 2002 7 29 2002UALA01108 1 20020630 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 FORWARD CABIN FLOOR T-CAP BODY STATION 324 RBL 59-61 HAS SURFACE CORROSION. MAJOR REPAIR ACCOMPLISHED. CUT OUT FILLER AND ANGLE, INSTALLED FOR T-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072900036 20020729 00036 NM 2002 7 29 2002UALA01109 1 20020701 A 5320 CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 STATION 663 STRINGER 10R FRAME CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900037 20020729 00037 NM 2002 7 29 2002UALA01110 1 20020701 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 CABIN BODY FRAME STRINGER CLIP IS CRACKED BODY STATION 706 AFT SIDE STRINGER 11L. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900038 20020729 00038 NM 2002 7 29 2002UALA01111 1 20020701 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 FUSELAGE FRAME WEB CRACKED STATION 887 STRINGER 9R AT SIDEWALL VENT ATTACH BRACKET FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900039 20020729 00039 NM 2002 7 29 2002UALA01113 1 20020627 A 2913 3508806 PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 657UA 27112 LOSS OF HYDRAULIC FLUID FROM RIGHT SYSTEM. REPLACED RIGHT ENGINE HYD PUMP DUE TO LEAK BETWEEN MATING SEAM. ACP ENG RUN , NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002080900030 20020809 00030 NE 2002 8 9 2002UALA01114 2 20020701 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 FLAMED OUT A UALA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 WP 29 666UA 29238 727990 FLAME-OUT OF NUMBER 2 ENGINE. INADEQUATE FUEL SUPPLY PROVIDED TO NR 2 ENGINE. CONDUCTED EXTENSIVE ENGINE AND FUEL SYST EM DIAGNOSTIC TESTING. DISCOVERED NO INDICATION OF MECHANICAL OR ELECTRONIC SYSTEM FAULTS. CAREFULLY TRACKED AIRPLANE OPERATION AFTER INCIDENT WITH NO FURTHER ANOMALIES INDICATED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002080900052 20020809 00052 NM 2002 8 9 2002UALA01115 1 20020702 A 4990 38801602 SCAVENGE PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU FAILED A UALA K NONE A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 645UA 25280 61846 APU TAILPIPE FIRE. FOUND TURBINE SCAVENGE PUMP FAILED WITH NO ROTATION DURING OPERATION. IN ADDITION, THE TIE SHAFT DR IVE INSERT WAS FOUND LOOSE. THE POWER SECTION WAS ROUTED FOR DISASSEMBLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2002072900040 20020729 00040 NM 2002 7 29 2002UALA01116 1 20020703 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 CABIN LEFT HAND CREASE BEAM WEB UPPER SURFACE CORRODED FROM STATION 867 TO STATION 882 AT LBL 68. MAJOR REPAIR ACCOMPLI SHED. REPLACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900043 20020729 00043 NM 2002 7 29 2002UALA01120 1 20020702 A 2120 ODOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DETECTED A UALA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 178UA 24385 ONE TO TWO HOURS AFTER TAKEOFF FLIGHT ATTENDANT REPORTED SMOKE-ELECTRICAL ODOR IN CABIN. FLIGHT ATTENDANT INDICATED SMO KE-ODOR EMANATED FROM CART LIFT AREA. 2 L 7 4 4F 4 F RT A20WE E24NE 2002072900044 20020729 00044 NE 2002 7 29 2002UALA01121 2 20020702 A 7230 COMPRESSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 ENGINE STALLED A UALA J A DUMP FUEL UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 109UA 26906 AIRCRAFT SUSTAINED COMPRESSOR STALL ON TAKEOFF NR 2 ENGINE. NO SHUTDOWN. 2 L 7 4 4F 4 F RT A20WE E24NE 2002072900045 20020729 00045 NM 2002 7 29 2002UALA01122 1 20020705 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 EEL LIGHT DAMAGED AT SEAT 1E. INSTALLED SERVICEABLE EEL LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002082300103 20020823 00103 NE 2002 8 23 2002UALA01123 2 20020703 A 7321 EEC BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 584UA 26706 727195 LT ENGINE COMPRESSOR STALL AT CLIMB THRUST CLIMBING THROUGH 10,000 FT. ENGINE RECOVERED AND CONTINUED NORMAL OPERATION. THE 14TH STAGE BLEED CONVERTER VALVE WAS REPLACED AS PRECAUTIONARY ALONG WITH EEC AS A RESULT OF EICAS MESSAGE 275-27. COMPONENT SHOP CURRENTLY INVESTIGATING 14TH STAGE BLEED CONVERTER VALVE AND EEC TO VERIFY FAILURE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072900046 20020729 00046 NM 2002 7 29 2002UALA01124 1 20020703 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 CABIN STRINGER 1 STATION 869-873 HAS TOOL MARKS AND EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISH. INSTALLED STRING ER REPAIR DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900047 20020729 00047 NM 2002 7 29 2002UALA01125 1 20020704 A 2751 WARNING SYSTEM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 942UA 26679 LANDED UNDER AMBER ALERT DUE TO SPLIT FLAPS. NO FLIGHT CONTROL PROBLEMS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900049 20020729 00049 NM 2002 7 29 2002UALA01127 1 20020706 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 CABIN FLOORBEAM INTERCOSTAL UPPER FLANGE IS CRACKED AT BODY STATION 384 BL 0 WL 208. MAJOR REPAIR ACCOMPLISHED. NEW WE B MANUFACTURED AND REPLACED ALONG WITH NEW ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900050 20020729 00050 NM 2002 7 29 2002UALA01128 1 20020706 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 FORWARD CABIN STATION 294 FLOORBEAM UPPER CAP HAS EXCESS MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. SPLICE CAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900051 20020729 00051 NM 2002 7 29 2002UALA01129 1 20020707 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 941UA 26676 AFT PIT FRAME STATION 787 RBL 30 HAS DENT ON UPPER CHORD. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900052 20020729 00052 NM 2002 7 29 2002UALA01130 1 20020707 A 5310 CREASE BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 941UA 26676 CABIN RIGHT FORWARD CREASE BEAM CORRODED AND CRACKED IN RADIUS AT STA 294.5, RBL 54, WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM INBOARD ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900053 20020729 00053 NM 2002 7 29 2002UALA01131 1 20020707 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 STATION 188 FRAME CRACKED LEFT HAND SIDE WL 207 AND HORIZONTAL WEB. MAJOR REPAIR ACCOMPLISHED. INSTALLED WEB REPAIR AN GLE AND SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900054 20020729 00054 NM 2002 7 29 2002UALA01132 1 20020707 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 STATION 188 RIGHT HAND SIDE FRAME CRACKED WL 207 AND HORIZONTAL WEB. MAJOR REPAIR ACCOMPLISHED. INSTALLED WEB REPAIR A NGLE AND SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900055 20020729 00055 NE 2002 7 29 2002UALA01133 2 20020705 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 POWER LOSS A UALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 414UA 472 ABORTED TAKEOFF AT 90-100 KNOTS DUE TO NR 1 ENGINE NOT PRODUCING ENOUGH THRUST. 2 L 7 2 4F 4 F RT A28NM E40NE 2002072900056 20020729 00056 NM 2002 7 29 2002UALA01134 1 20020703 A 2540 LAVATORY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE AFT LEAKING A UALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 WP 29 803UA 748 IMMEDIATELY AFTER TAKEOFF CREW NOTICED WATER LEAKING FROM THE AFT LAV. FLIGHT RETURNED TO SFO FOR REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2002072900057 20020729 00057 2002 7 29 2002UALA01135 4 20020707 A 2312 VHF COMM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 189UA 26878 LOST NR 1 VHF COMMUNICATIONS RADIOS. SUPPLEMENTAL DATA UPDATE LT RADIO CONTROL PANEL AND LT VHF TRANSCEIVER WERE REPLACE D. AUDIO MANAGEMENT UNIT WAS PREVIOUSLY REPLACED FOR FAILURE OF THE RIGHT CHANNEL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002072900058 20020729 00058 NM 2002 7 29 2002UALA01139 1 20020706 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE ELONGATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 FORWARD CABIN FLOOR BODY STATION 395 LBL 2 T-CAP FASTENER HOLE IS ELONGATED. MAJOR REPAIR ACCOMPLISHED. INSTALLED 10 I NCH STRAP AND NESTED ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080800080 20020808 00080 NM 2002 8 8 2002UALA01140 1 20020705 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ENGINE MALFUNCTIONED A UALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 WP 29 767UA 2582 1501 26918 LOSS OF RIGHT ENGINE GENERATOR ON CLIMBOUT. ENGINE NOT SHUTDOWN. MAINTENANCE MESSAGE 24-31712 WAS PRESENT. MAINTENANC E ACCOMPLISHED CH5588 WITH NO DISCREPANCIES FOUND. REPLACED RIGHT GCU. THE RIGHT IDG AND GCU WERE PREVIOUSLY REPLACED. SUSPECTED THE IDG MIGHT BE AT FAULT. THE GCU'S WERE TESTED AT UAL SHOP WITH NO FAULT FOUND. FINDING REPORT WILL BE O BTAINED FROM HAMILTON SUNDSTRAND WHEN AVAILABLE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002072900059 20020729 00059 2002 7 29 KBMA117635 4 20020626 A 3422 5050010902 GYRO SNIAS 350 AS350BA 8680817 EU COCKPIT INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 1188P 792 2347 DIRECTIONAL GYRO COMPLETELY INOPERATIVE. NON RESPONSIVE WITH POWER APPLIED. REPLACED WITH OVERHAULED UNIT. 1 G 7 1 3U NC H9EU 2002072900060 20020729 00060 CE 2002 7 29 KZ52002F00000 1 20020619 A 2700 115524046 TORQUE SHAFT BEECH 99 C99 1154006 CE TAIL SECTION CORRODED B KZ5R K NONE O OTHER IN INSP/MAINT 1 GL 15 7207E 10096 U223 DURING A SCHEDULED INSPECTION OF THE TAIL AREA THE TECHNICIAN DISCOVERED CORROSION HAD PENETRATED THROUGH THE TORQUE SHA FT. TUBE IS MADE OF STEEL AND IS SUBJECT TO RUST. 1 L 7 2 3T A14CE 2002072900061 20020729 00061 EU 2002 7 29 PHALG0201 1 20020627 A 3230 BEARING BAG JETSTM JETSTM4112 EU MLG DEFECTIVE D PAIR K NONE O OTHER IN INSP/MAINT 1 SO 05 DEFECTIVE/ MISSING CHROME PLATING ON INSIDE DIAMETER OF CAPSULES. CONDITION CAN LEAD TO PREMATURE FAILURE OF BEARING RI NG AND EXCESSIVE/ UNEVEN WEAR TO BEARING CARRIER AND METERING PIN. CONDITION FOUND ON (6) SIX CAPSULES / GEARS AT FIRST OVERHAUL. CONDITION COULD CAUSE INABLILITY TO EXTEND GEAR FOR LANDING. 1 L 7 2 4T RT A196 2002072900062 20020729 00062 CE 2002 7 29 TOX2002F00000 1 20020509 A 5510 12326232 SUPPORT CESSNA 207 207A 2073604 CE CONT O520 IO520* 17032 SO HORIZONTAL STAB CRACKED C T0XM K NONE O OTHER IN INSP/MAINT 1 SW 09 6415H 4294 20700514 DURING A ROUTINE INSPECTION, NOT RELATED TO MFG, THE LOWER LEFT FOLDED TAB WAS FOUND BROKEN OUTBOARD OF THE BOLT HOLE. UPON REMOVAL, A CRACK WAS DISCOVERED ACROSS ABOUT 80 PERCENT OF THE FORWARD FLANGE. THE EFFECTIVE SUPPORT OF THE LEFT S TABILIZER WAS REDUCED FROM 3 BOLTS TO ONE. ALTHOUGH NOT LIFE THREATENING AT THIS STAGE, THE STABILIZER COULD BE MOVED V ERTICALLY AND HORIZONTALLY. 1 H 7 1 3O 3 O A16CE E5CE 2002072900063 20020729 00063 CE 2002 7 29 VJ32002F00049 1 20020703 A 3600 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO AIR PUMP FAILED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 5585Y 371 CE1389 820461R DURING GROUND RUN UP, OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT 800 RPM. RAN AIRCRAFT UP TO 1600 RPM BEFORE PRESSURE READ 4.5. CHECKED PRESSURE SYSTEM FOR LEAKS AND CHECKED REGULATOR ALL CHECKED WELL. 1 L 7 1 3O 3 O 3A15 E5CE 2002072900064 20020729 00064 SO 2002 7 29 VJ32002F00050 2 20020628 A 7324 6314272A20 FLOW DIVIDER BEECH 33 F33A 1151425 CE CONT O520 IO520B 17032 SO ENGINE FAILED B VJ3R O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 WP 07 5582X 29 CE1353 825800R AT NORMAL POWER SETTINGS THE ENGINE RAN ROUGH AT 6000 TO 7000 FEET. REMOVED FUEL FLOW MANIFOLD VALVE AND INSTALLED NEW FUEL FLOW MANIFOLD VALVE. GROUND OPERATION OF THE ENGINE CHECKED NORMAL. PART SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O 3A15 E5CE 2002072900065 20020729 00065 SO 2002 7 29 XPCA800S 1 20020619 A 7120 5008906 SUPPORT BRACKET PIPER PA31T PA31T 7103124 SO ENGINE CRACKED D IPMV K NONE O OTHER IN INSP/MAINT 1 WP 11 111KV 31T7920035 FOUND CRACKS EMINATING FROM LAST RIVET ON OUTBOARD UPPER ENGINE SUPPORT BRACKET. IT APPEARS THAT THIS RIVET WAS SMASHED HARDER THAN NECESSARY DURING MANUFACTURE. 1 L 7 2 3T A8EA 2002072900066 20020729 00066 NM 2002 7 29 2002UALA01143 1 20020708 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7455U 21909 FORWARD LOWER FUSELAGE SKIN, BODY STATION 312-328, DRAIN HOLE AFT OF NOSE LANDING GEAR WHEEL WELL IS PUNCTURED AND BROKE N OUT. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 3 4F 4 F A3WE E2EA 2002072900067 20020729 00067 NM 2002 7 29 2002UALA01145 1 20020708 A 2910 HYDRAULIC SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT FAILED A UALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 525UA 24978 LOSS OF LEFT SYSTEM HYDRAULICS. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080900055 20020809 00055 NM 2002 8 9 2002UALA01146 1 20020708 A 2613 65528087 CONTROL UNIT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE OVERHEAT SYS MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 916UA 25383 APPROXIMATELY 15 MINUTES AFTER DEPARTURE WING BODY OVERHEAT LIGHT ILLUMINATED. RETURNED TO FIELD. CREW REPORTED LEFT W ING BODY OVERHEAT LIGHT ON AFTER DEPARTURE. TURNED LEFT PACK OFF, LEFT BLEED OFF AND CLOSED APU ISOLATION VALVE. LEFT WING BODY OVERHEAT LIGHT WENT OUT IN APPROXIMATELY 1 MINUTE. MAINTENANCE CHECKED ALL LOOPS AND FOUND THEM TO BE WITHIN LIMITS. REPLACED COMPARTMENT OVERHEAT CONTROL UNIT AND TESTED THE SYSTEM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900068 20020729 00068 NM 2002 7 29 2002UALA01147 1 20020709 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 FORWARD CABIN FRAME IS CRACKED STATION 440 STRINGER 9L AT PASSENGER SERVICE UNIT ATTACHMENT. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900069 20020729 00069 NM 2002 7 29 2002UALA01148 1 20020709 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 FORWARD CABIN FRAME IS CRACKED STATION 400 STRINGER 9L PASSENGER SERVICE UNIT ATTACHMENT. MAJOR REPAIR ACCOMPLISHED, DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900070 20020729 00070 NM 2002 7 29 2002UALA01149 1 20020710 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 FUSELAGE FRAME CRACKED AT FASTENER HOLE TO INBOARD FREE FLANGE TO CREASE BEAM IN CHORD STATION 727A LEFT SIDE. MAJOR RE PAIR ACCOMPLISHED. INSTALLED J-REPAIR DOUBLER AND STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900071 20020729 00071 NE 2002 7 29 C1HA200292007 2 20020624 A 7200 ENGINE BOEING 727 727212 138407G NM PWA JT8 JT8D17 52049 NE NR 2 LEAKING A C1HA E A ENGINE SHUTDOWN UNSCHED LANDING K M J FLUID LOSS OVER TEMP WARNING INDICATION CL CLIMB 1 GL 15 292AS 21458 688133 DURING CLIMB THROUGH FL280 NR 2 ENGINE OIL TEMP INDICATED BEYOND REDLINE RADIAL. NR 2 ENGINE SHUTDOWN 2 GALLONS OF OIL LOST, OIL PRESSURE 5PSI DURING DESCENT. OIL TEMP BACK IN GREEN AND AFTER SHUTDOWN NR 2 ENGINE WINDMILLED FOR 21 MINUTES. REMOVED AND REPLACED ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 2002072900072 20020729 00072 NE 2002 7 29 2002UALA01150 2 20020708 A 7230 COMPRESSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 ENGINE STALLED A UALA B E A EMER. DESCENT ENGINE SHUTDOWN UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 174UA 24381 COMPRESSOR STALL ON NR 4 ENGINE. SUPPLEMENTAL DATA UPDATE THIS IS A GROUP 3 (TAKEOFF ) SURGE DUE TO EXCESSIVE HPC REAR STAGE BLADE TIP CLEARANCE. ENGINE WAS REPLACED AT TERMINATION OF THE FERRY FLIGHT FOR COMPRESSOR REFURBISHMENT. PW4000 ENGINE TAKE-OFF SURGES ARE BEING MANAGED PER AD 2001-25-11 2 L 7 4 4F 4 F RT A20WE E24NE 2002072900073 20020729 00073 NM 2002 7 29 C1HA200292008 1 20020607 A 5313 STRINGER BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 STR 27 LT CORRODED FROM STA 950F - 1010 IN NUMEROUS AREAS 2 L 7 3 4F A3WE 2002080900058 20020809 00058 2002 8 9 2002UALA01151 4 20020709 A 3442 6225125001 DRIVE UNIT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE WEATHER RADAR FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 955UA 26703 CREW REPORTED WX RADAR FAILED ON CLIMBOUT. BECAUSE OF ADVERSE WEATHER AHEAD, RETURNED TO FIELD. REPLACED THE WEATHER R ADAR COMPUTER AND WEATHER RADAR ANTENNA DRIVE UNIT. THE SHOP FOUND THE WEATHER RADAR ANTENNA DRIVE UNIT TO HAVE A VERIF IED FAILURE WITH THE FLAT SPRINGS WITHIN THE UNIT. THERE WERE NO PROBLEMS FOUND WITH THE WEATHER RADAR COMPUTER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900074 20020729 00074 NM 2002 7 29 C1HA200292009 1 20020608 A 5313 STRINGER BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 STR 27 LT IS EXFOLIATED AT STA 1120 2 L 7 3 4F A3WE 2002072900075 20020729 00075 NM 2002 7 29 2002UALA01152 1 20020710 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 941UA 26676 CABIN BODY STUB FRAME INBOARD FLANGE, RADIUS CRACKED AT BODY STATION 296, RBL 55, WL 209. MAJOR REPAIR ACCOMPLISHED. M ANUFACTURED AND INSTALLED REPAIR DOUBLER AND CLIPS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900076 20020729 00076 NM 2002 7 29 C1HA200292010 1 20020620 A 5311 FRAME BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 CORROSION AT FS 720C BETWEEN STR 28 LT AND 28 RT UNDER LEVELING COMPOUND IN FWD PIT 2 L 7 3 4F A3WE 2002072900077 20020729 00077 NM 2002 7 29 C1HA200292011 1 20020517 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 STA 420 FLOORBEAM IS CORRODED BETWEEN TRACK 24 RT AND FLOOR WEB 2 L 7 3 4F A3WE 2002072900078 20020729 00078 NM 2002 7 29 C1HA200292012 1 20020518 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 FLOORBEAM STA 1110 LBL 24- RBL 28 TOP FLANGE AND REPAIR HAVE CORROSION. LBL 22 HAS FLOORBOARD ATTACH HOLE WITH NO PITCH . 2 L 7 3 4F A3WE 2002072900079 20020729 00079 NM 2002 7 29 2002UALA01153 1 20020710 A 2130 7110024 CONTROL PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 379UA 2438 24654 RETURNED TO THE FIELD DUE TO CABIN PRESSURIZATION PROBLEMS. THE CABIN PRESSURE SELECTOR PANEL FAILED. REPLACED THE CAB IN PRESSURE SELECTOR PANEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900080 20020729 00080 NM 2002 7 29 C1HA200292013 1 20020518 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 FLOORBEAM AT STA 1070 TOP IS CORRODED LBL 24-45 2 L 7 3 4F A3WE 2002072900081 20020729 00081 NM 2002 7 29 C1HA200292014 1 20020520 A 5313 STRINGER BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 STR 29 LT IS EXFOLIATED AT STA 1050. 2 L 7 3 4F A3WE 2002072900082 20020729 00082 NM 2002 7 29 2002UALA01154 1 20020710 A 2432 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE E/E BAY DISCHARGED A UALA J A DUMP FUEL UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 180UA 25224 CONSTANT BATTERY DISCHARGE OCCURRED AFTER TAKE-OFF. SUPPLEMENTAL DATA UPDATE THE MAIN BATTERY AND MAIN BATTERY CHARGER W ERE REPLACED. NO FURTHER PROBLEMS WERE REPORTED. SHOP REPORTED NO FAULTS FOUND FOR REMOVED BATTERY AND BATTERY CHARG ER. 2 L 7 4 4F 4 F RT A20WE E24NE 2002072900083 20020729 00083 NM 2002 7 29 C1HA200292015 1 20020523 A 3230 ATTACH FITTING BOEING 727 727212 138407G NM LT MLG CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 LT MLG FWD TRUNION BEARING ATTACH FITTING HAS CORROSION AND PITTING ON INBD SIDE OF INBD FLANGE 2 L 7 3 4F A3WE 2002072900084 20020729 00084 NM 2002 7 29 2002UALA01156 1 20020711 A 5512 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 941UA 26676 LEFT HAND HORIZONTAL STABILIZER LEADING EDGE, 14 INCHES FROM FUSELAGE, SKIN IS DENTED. MAJOR REPAIR ACCOMPLISHED. DOUB LER MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900085 20020729 00085 NM 2002 7 29 C1HA200292016 1 20020520 A 5754 SKIN BOEING 727 727212 138407G NM RT WING LE FLAP DELAMINATED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 RT WING FORE FLAP INBRD LOWER SKIN HAS AREA OF DELAMINATION JUST AFT OF CENTER ATTACH ARM. (AREA 12 INCHES X 6 INCHES) 2 L 7 3 4F A3WE 2002072900086 20020729 00086 NM 2002 7 29 2002UALA01157 1 20020711 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 FORWARD CABIN, STATION 360 FLOORBEAM FORWARD SIDE HAS EXCESSIVE MATERIAL LOSS FROM GOUGE BLENDING LBL 18. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED L-REPAIR ANGLE & FASTENERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900087 20020729 00087 NM 2002 7 29 C1HA200292017 1 20020519 A 5754 SKIN BOEING 727 727212 138407G NM LT WING TE FLAP DEBONDED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 LT INBRD TRAILING EDGE AFT FLAP LOWER SURFACE AT INBRD END HAS REPAIR DISBONDING 2 L 7 3 4F A3WE 2002072900088 20020729 00088 NM 2002 7 29 2002UALA01158 1 20020712 A 5512 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 RIGHT HAND HORIZONTAL STABILIZER, LOWER SKIN AT REAR SPAR IS CRACKED AT STABILIZER STA 120.3-129.5. MAJOR REPAIR ACCOMP LISHED. FLUSH REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900089 20020729 00089 NM 2002 7 29 2002UALA01159 1 20020711 A 2751 WARNING SYSTEM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 902UA 25002 FLIGHT HAD SPLIT FLAPS ON FINAL APPROACH, AN AMBER ALERT WAS DECLARED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900090 20020729 00090 NM 2002 7 29 2002UALA01160 1 20020713 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 941UA 26676 STATION 188 LEFT HAND FRAME OUTBOARD CHORD CRACKED IN RADIUS AT WL 208. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER R EPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900091 20020729 00091 NM 2002 7 29 2002UALA01161 1 20020713 A 5320 WEB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 941UA 26676 RIGHT HAND FORWARD FUSELAGE BETWEEN 188 AND 196.5 AT WL 207 HORIZONTAL WEB CRACKED AT INBOARD CORNER. MAJOR REPAIR ACCO MPLISHED. REPLACED WEB AND INSTALLED SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900092 20020729 00092 NM 2002 7 29 C1HA200292018 1 20020517 A 5320 ATTACH ANGLE BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 ATTACH ANGLE FOR TIE DOWN IS CORRODED UNDER NUT PLATE ON FWD CARGO DOOR CUT OUT FWD FRAME ABOVE STR 23-24 RT. 2 L 7 3 4F A3WE 2002072900093 20020729 00093 NM 2002 7 29 C1HA200292019 1 20020606 A 5340 STRINGER BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 STR 27 RT AT APPROX STA 1060 IS CORRODED 2 L 7 3 4F A3WE 2002072900094 20020729 00094 NM 2002 7 29 2002UALA01163 1 20020713 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 CABIN STATION 827 FRAME AT STRINGER 9R IS CRACKED AT INBOARD FASTENER FOR AIR GRILL ATTACHMENT. MAJOR REPAIR ACCOMPLISH ED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900095 20020729 00095 NM 2002 7 29 2002UALA01164 1 20020713 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 FORWARD CABIN FRAME IS CRACKED STATION 480 STRINGER 9L AT PASSENGER SERVICE UNIT ATTACHMENT. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900096 20020729 00096 NM 2002 7 29 2002UALA01165 1 20020714 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 FORWARD CABIN FRAME IS CRACKED STATION 400 STRINGER 9R PASSENGER SERVICE UNIT ATTACHMENT. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900060 20020809 00060 NM 2002 8 9 2002UALA01166 1 20020712 A 7920 B-NUT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ENGINE LOOSE A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 316UA 23948 720436 SHUT DOWN ENGINE DUE TO LOSS OF OIL AND MADE UNSCHEDULED LANDING UNDER AMBER ALERT. OIL LOSS WAS THE RESULT OF A LOOSE AFT SUMP OIL SUPPLY TUBE B-NUT. TIGHTENED B-NUT. OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082300104 20020823 00104 NM 2002 8 23 2002UALA01167 1 20020713 A 2730 654476122 PCU BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ELEVATOR LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 29 361UA 40000 24454 LANDED UNDER AMBER ALERT DUE TO A SYSTEM LOW HYDRAULIC PRESSURE LIGHT ON. MAINTENANCE REPLACED LEFT ELEVATOR PCU (A-SYS T HYD). SYSTEM LEAK CHECKED OK. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900097 20020729 00097 NM 2002 7 29 C1HA200292020 1 20020608 A 5330 SKIN BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 SKIN IS EXFOLIATED AT STA 1130 O/B OF STR 27L. 2 L 7 3 4F A3WE 2002072900098 20020729 00098 NM 2002 7 29 C1HA200292021 1 20020531 A 5310 SHEAR TIE BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 SHEAR TIE HAS LIGHT SURFACE CORROSION AT STA 965 JUST OUT BOARD OF RBL 28 2 L 7 3 4F A3WE 2002072900099 20020729 00099 NM 2002 7 29 C1HA200292022 1 20020520 A 5313 STRINGER BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 STR 29L IS EXFOLIATED AT STA 1050 2 L 7 3 4F A3WE 2002072900100 20020729 00100 NM 2002 7 29 C1HA200292024 1 20020523 A 5313 FRAME BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 FRAME 950A IS CORRODED ON FWD SIDE BETWEEN STR 28R AND 30 2 L 7 3 4F A3WE 2002072900101 20020729 00101 NM 2002 7 29 C1HA200292025 1 20020526 A 5310 SHEAR TIE BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 SHEAR TIE AT STA 950B IS CORRODED ON FWD SIDE BETWEEN INTERCOSTAL AND STR 29 LT. 2 L 7 3 4F A3WE 2002072900102 20020729 00102 NM 2002 7 29 C1HA200292026 1 20020522 A 5321 FLOOR PANEL BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 CENTER FLOOR WEB STA 1148 - 1176 HAS CORROSION TOP AND BOTTOM 2 L 7 3 4F A3WE 2002072900103 20020729 00103 NM 2002 7 29 C1HA200292027 1 20020531 A 5313 STRINGER BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 STR 30 IS EXFOLIATED ON RT SIDE BETWEEN STA 950 AND 950A. 2 L 7 3 4F A3WE 2002072900104 20020729 00104 NM 2002 7 29 C1HA200292028 1 20020521 A 5310 SHEAR TIE BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 SHEAR TIE AT STA 970 BL 30-LBL 29 IS CORRODED 2 L 7 3 4F A3WE 2002072900105 20020729 00105 NM 2002 7 29 C1HA200292029 1 20020524 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 FLOORBEAM STA 1030 LBL 45 - RBL 8 HAS CORROSION AND LBL 12 HAS A HOLE WITH NO EDGE DISTANCE. 2 L 7 3 4F A3WE 2002072900106 20020729 00106 NM 2002 7 29 C1HA200295010 1 20020617 A 2910 LINE BOEING 727 727290 138408W NM HYD SYSTEM CRACKED A C1HA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 295AS 22147 HYDRAULIC B SYSTEM FAILURE IN FLIGHT.LANDED FLAPS 15 AT 160,000 FT.INSPECTED A/C FOUND RT SPOILER RETURN LINE CRACKED IN STALLED INTERM REPAIR FLEX LINE PER MP&P.CH 1-15-5. INST. PERMANANT B SYS RETURN LINE FOR RT SPOILER IAW B72MM 29-10-00 OPS NORMAL REMOVED TLD MXC ADVISED. REMOVED AND REPLACED NR 1 "B" ELECT PUMP. OPS LEAK CHECKED GOOD MM 29-12-11. REMO VED AND REPLACED NR 2 "B" ELECT PUMP - OPS LEAK CHECKED GOOD MM29-12-11. REMOVED AND REPLACED "B" SYSTEM CASE DRAIN F ILTERS. OPS LEAK CHECKED GOOD MM 29-12-21 2 L 7 3 4F A3WE 2002072900107 20020729 00107 NM 2002 7 29 CIHA200292023 1 20020521 A 5330 LAP JOINT BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 CORROSION AT LAP SEAM STR 14 RT STA'S 1138-1223 & 1246-1342 2 L 7 3 4F A3WE 2002072900108 20020729 00108 NM 2002 7 29 2002UALA01168 1 20020714 A 2932 106055437 TRANSMITTER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HYD SYSTEM FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 361UA 24454 AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO INDICATED LOSS OF HYDRAULIC FLUID QUANTITY. REPLACED A SYSTEM QUANTITY TRAN SMITTER. RAN ENGINES AND MOVED FLIGHT CONTROLS. SYSTEM QUANTITY AND PRESSURE REMAINED STEADY. 2 L 7 2 4F 4 F RT A16WE E2GL 2002072900109 20020729 00109 NM 2002 7 29 2002UALA01171 1 20020713 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 STATION 220 STRINGER 17L WL 208 FUSELAGE SKIN DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080900068 20020809 00068 NM 2002 8 9 2002UALA01173 1 20020712 A 3260 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT MLG MALFUNCTIONED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 545UA 25323 GEAR DISAGREE LIGHT EICAS MESSAGE. PSEU BITE CHECK SHOWS SENSORS 59 AND 239 (SYSTEM 1 & 2 RIGHT GEAR UPLOCK). SENSORS PASSED TARGET TEST FOR TARGET FAR AND WHEN SLUGGED. NO OTHER DISCREPANCIES. 2 L 7 2 4F 4 F RT A2NM E17NE 2002072900110 20020729 00110 NM 2002 7 29 COOSDR020186 1 20020701 A 5755 651734874C STRUCTURE BOEING 727 727227 1384078 NM SPOILERS CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 RT WING, SPOILER NR 8 (PN 65-17348-74C) (SN 6114W) UPPER, LOWER SKIN AND HONEYCOMB CORE CORRODED. 2 L 7 3 4F A3WE 2002072900111 20020729 00111 NM 2002 7 29 COOSDR020187 1 20020701 A 5751 STRUCTURE BOEING 727 727227 1384078 NM RT WING AILERON CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 RIGHT WING OUTBOARD AILERON TRAILING EDGE (PN 652176634) (SN 226) UPPER, LOWER SKIN AND HONEYCOMB CORE, CORRODED. 2 L 7 3 4F A3WE 2002072900112 20020729 00112 NM 2002 7 29 COOSDR020189 1 20020701 A 5753 STRUCTURE BOEING 727 727227 1384078 NM RT WING TE FLAP CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 RIGHT WING INBOARD AFT FLAP (PN 65-21634-80) (SN BN375) UPPER, LOWER SKIN AND HONEYCOMB CORE CORRODED. 2 L 7 3 4F A3WE 2002072900113 20020729 00113 NM 2002 7 29 COOSDR020190 1 20020701 A 5245 655851312 ACCESS PANEL BOEING 727 727227 1384078 NM FUSELAGE DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 AIR CONDITION BAY ACCESS PANEL (PN 65-58513-12) INNER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002072900114 20020729 00114 NM 2002 7 29 COOSDR020191 1 20020701 A 5754 6521630 STRUCTURE BOEING 727 727227 1384078 NM LT WING LE FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 LEFT WING INBOARD FORE FLAP (PN 652130-188) (SN BN720) UPPER, LOWER SKIN AND HONEYCOMB CORE DELAMINATED SECTION. 2 L 7 3 4F A3WE 2002072900115 20020729 00115 NM 2002 7 29 COOSDR020192 1 20020701 A 5754 6521631274 STRUCTURE BOEING 727 727227 1384078 NM RT WING LE FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 RIGHT WING OUTBOARD FORE FLAP (PN 65-21631-274) (SN BN386) UPPER SKIN AND HONEYCOMB CORE DELAMINATED SECTION. 2 L 7 3 4F A3WE 2002072900116 20020729 00116 NM 2002 7 29 COOSDR020198 1 20020701 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM MAIN CARGO CABIN CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 MAIN CARGO CABIN BS 1130 LOWER CHORD CORRODED. 2 L 7 3 4F A3WE 2002072900117 20020729 00117 NM 2002 7 29 COOSDR020202 1 20020701 A 5753 STRUCTURE BOEING 727 7272J7 138400E NM RT WING TE FLAP CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 RIGHT WING, INBOARD AFT FLAP (PN 65-21634-92) (SN BN480) UPPER, LOWER SKIN AND HONEYCOMB CORE CORRODED. 2 L 7 3 4F A3WE 2002072900118 20020729 00118 NM 2002 7 29 COOSDR020203 1 20020701 A 5710 65216522 PANEL BOEING 727 7272J7 138400E NM RT WING T/E DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 RIGHT WING, TRAINLING EDGE - LOWER FIX PANEL (PN 65216522) DELAMINATED. 2 L 7 3 4F A3WE 2002072900119 20020729 00119 NM 2002 7 29 COOSDR02193 1 20020701 A 5320 ANGLE BOEING 727 7272J7 138400E NM CARGO DOOR FRAME CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 MAIN CARGO DOOR (PER STC NO SA1797SO) UPPER JAMB, FORWARD AND AFT CORNER ANGLE CRACKED. 2 L 7 3 4F A3WE 2002072900120 20020729 00120 NM 2002 7 29 COOSDR02194 1 20020701 A 5755 STRUCTURE BOEING 727 7272J7 138400E NM RT WING SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 RIGHT WING, SPOILER NR 10, PN 65-17348-75, SN 4268H WITH DELAMINATION. 2 L 7 3 4F A3WE 2002072900121 20020729 00121 NM 2002 7 29 COOSDR02195 1 20020701 A 5755 STRUCTURE BOEING 727 7272J7 138400E NM RT WING SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 RIGHT WING, SPOILER NR 8 (PN 651734866A) WITH DELAMINATION. 2 L 7 3 4F A3WE 2002072900122 20020729 00122 NM 2002 7 29 COOSDR02196 1 20020701 A 5755 STRUCTURE BOEING 727 7272J7 138400E NM RT WING SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 RIGHT WING, SPOILER NR 14, (PN 651734757), SN 9126S WITH DELAMINATION. 2 L 7 3 4F A3WE 2002072900123 20020729 00123 NM 2002 7 29 COOSDR02197 1 20020701 A 5730 6521657242 PANEL BOEING 727 7272J7 138400E NM RT WING T/E DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 RIGHT WING, TRAILING EDGE-UPPER PANEL (PN 6521657242) DELAMINATED. 2 L 7 3 4F A3WE 2002072900124 20020729 00124 NM 2002 7 29 COOSDR02200 1 20020701 A 5730 6521652616 PANEL BOEING 727 7272J7 138400E NM RT WING T/E DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 RIGHT WING, TRAILING EDGE - LOWER PANEL (PN 6521652616) DELAMINATED. 2 L 7 3 4F A3WE 2002072900125 20020729 00125 NM 2002 7 29 COOSDR02201 1 20020701 A 5310 DOOR FRAME BOEING 727 727227 1384078 NM LT MLG CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 LEFT MAIN LANDING GEAR, WING DOOR AFT FRAME CRACKED. 2 L 7 3 4F A3WE 2002072900126 20020729 00126 NM 2002 7 29 COOSDR0220188 1 20020701 A 5753 652163585 SKIN BOEING 727 727227 1384078 NM LT WING TE FLAP DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 794AJ 21243 LEFT WING OUTBOARD AFT FLAP (PN 65-21635-85) (SN BN486) UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2002072900127 20020729 00127 NM 2002 7 29 COOSDR02204 1 20020701 A 5755 SKIN BOEING 727 7272J7 138400E NM LT WING SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 LEFT WING, SPOILER NR 4, (PN 65-17347-42), (SN TC-248) WITH DELAMINATION AT UPPER SKIN. 2 L 7 3 4F A3WE 2002072900128 20020729 00128 NM 2002 7 29 COOSDR02205 1 20020701 A 5755 651734875 SKIN BOEING 727 7272J7 138400E NM LT WING SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 LEFT WING, SPOILER NR 5, (PN 65-17348-75), (SN 1781P) WITH DELAMINATION AT UPPER SKIN AND LOWER SKIN. 2 L 7 3 4F A3WE 2002072900129 20020729 00129 WP 2002 7 29 MWEA020459 1 20020725 A 5241 991157911 BRACKET DOUG DC9 DC932 3022066 WP GALLEY DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CRACKED ANGLE BRACKET FORWARD END UNDER #1 BEAM OF GALLEY DOOR (DOT JH 36). -- FABRICATED AND INSTALLED BRACKET. 2 L 7 2 4F A6WE 2002072900130 20020729 00130 WP 2002 7 29 AALA20020559 1 20020429 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 589AA 53252 ORD - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT AIRSTAIR PANEL LIGHT PULLED OUT. REPLACED FORWARD EMERGENCY EXIT AIRSTAIR PANEL LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002072900131 20020729 00131 WP 2002 7 29 AALA20020563 1 20020501 A 3350 SWITCH DOUG DC9 DC983 3022083 WP CABIN LOOSE A AALA K NONE O OTHER CR CRUISE 1 SW 21 437AA 49455 BDL - FLT 1110 - EN ROUTE DFW-BDL, AISLE EMERGENCY EXIT PATH LIGHTING ILLUMINATED TWICE DURING CRUISE FOR APPROXIMATELY ONE MINUTES. LANDED BDL WITHOUT INCIDENT. RESECURED FLIGHT ATTENDANTS ON/OFF SWITCH FOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002072900132 20020729 00132 WP 2002 7 29 AALA20020588 1 20020505 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAILCONE CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 ORD - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT CEILING LIGHT RIGHT SIDE DOES NOT ILLUMINATE PROPERLY. REPAIRED EMERGENCY EXIT TAIL CONE SLIDE EMERGENCY EXIT LIGHT HOUSING WIRES AND REPLACED AFT AIRSTAIR EMERGENCY EXIT CEIL ING LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002072900133 20020729 00133 WP 2002 7 29 AALA20020590 1 20020505 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 432AA 49350 DFW - DURING OVERNIGHT MAINTENANCE TWO EMERGENCY EXIT LIGHTS ABOVE FLIGHT ATTENDANTS SEAT INOPERATIVE. SEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002072900134 20020729 00134 WP 2002 7 29 AALA20020591 1 20020504 A 3397 SPLICE DOUG DC9 DC983 3022083 WP AFT AIRSTAIRS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 436AA 49454 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT LEFT SIDE SIDEWALL INOPERATIVE. REPAIRED AFT AIRS TAIR EMERGENCY EXIT SIDEWALL LIGHT WIRE SPLICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002072900135 20020729 00135 WP 2002 7 29 AALA20020592 1 20020504 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN OUT OF ADJUST A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 577AA 53154 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROWS 22 THROUGH 26 INOPERATIVE. ADJUSTED EMERGENCY EXIT LIGHT BATTERY CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002072900136 20020729 00136 NM 2002 7 29 UPS02438897 1 20020629 A 5310 STRINGER BOEING 747 747123F NM BS 990 S-10L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C M/D - BS 990 S-10L STRINGER END FOUND CRACKED. BS 990 S10L STR REPAIRED AS PER RS R53-21-34835. ( UPS REPAIR / ATERATION AUTHORIZATION #747-53-20088 ). 2 L 7 4 4F A20WE 2002072900137 20020729 00137 EU 2002 7 29 MALA020437 1 20020726 A 3150 005WS00 WEU SAAB SF340 340B 7860101 EU A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 404XJ 340B404 DURING FLIGHT #2736 THE WHITE BITE LIGHT, LH FIRE WARNING AND CONFIG WARNING LIGHT ON. AIR RETURN TO MEM. MAINTENANCE REPLACED WARNING ELECTRICAL UNIT. WEU OPS CHECK GOOD. PN 005WS00 SN/ON 1394 SN/OFF 1586. AC OK FOR SERVICE IAW 31-50- 05-4. 2 L 7 2 4T RT A52EU 2002072900138 20020729 00138 WP 2002 7 29 MWEA020462 1 20020717 A 5311 991551735 FRAME DOUG DC9 DC932 3022066 WP STATION 1000 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LOWER FRAME ASSY STATION 1000 IS CRACKED, INLINE WITH LONGERON 28 RIGHT. -- INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2002072900139 20020729 00139 WP 2002 7 29 MWEA020463 1 20020717 A 5330 591142959 SKIN DOUG DC9 DC932 3022066 WP STATION 999 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FUSELAGE SKIN DENTED AT STATION 999 AFT OF LONGERON 27 RIGHT. -- CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002072900140 20020729 00140 NM 2002 7 29 AWXA200200669 1 20020702 A 5754 65C26602217 SKIN BOEING 737 7373G7 1384595 NM DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 DURING C-14 CHECK DELAMINATION WAS FOUND ON THE OUTBOARD TRAILING EDGE OF THE NR 2 SLAT. MAINTENANCE REMOVED DAMAGED ARE A, FABRICATED A DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, FIG 13. 2 L 7 2 4F RT A16WE 2002072900141 20020729 00141 NM 2002 7 29 AWXA200200671 1 20020726 A 3350 31882 TERMINAL BOEING 737 737277 1384570 NM SEAT ROW 6 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 0 0 22651 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 6 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE TERMINAL CONNECTOR AT SEAT ROW 6 L/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002072900142 20020729 00142 EU 2002 7 29 AWXA200200672 1 20020726 A 3350 E0052R8B3APNE CONNECTOR AIRBUS 320 A320232 3930326 EU SEAT ROW 22 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 647AW 0 0 762 PHX - EEL - DURING INSPECTION VARIOUS EMERGENCY LIGHTS OUT IN CABIN 4 (EA) SEAT 1 (EA) CEILING WERE FOUND INOPERATIVE. M AINTENANCE REPAIRED A CONNECTOR AT SEAT ROW 22 L/H, OPERATIONAL CHECK OF LIGHTING SYSTEM WAS GOOD. 2 L 7 2 4F RT A28NM 2002073000001 20020730 00001 NM 2002 7 30 COOSDR020206 1 20020701 A 5753 652163479 SKIN BOEING 727 7272J7 138400E NM LT WING TE FLAP CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 LEFT WING, INBOARD AFT FLAP (PN 65-21634-79)(SN BN147) UPPER, LOWER SKIN AND HONEYCOMB CORE CORRODED. 2 L 7 3 4F A3WE 2002073000002 20020730 00002 NM 2002 7 30 COOSDR020207 1 20020701 A 5752 652172633 STRUCTURE BOEING 727 7272J7 138400E NM AILERON TAB DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 LEFT WING, OUTBOARD AILERON TAB (PN 65-21726-33) TMC 189 WITH DELAMINATION. 2 L 7 3 4F A3WE 2002073000003 20020730 00003 NM 2002 7 30 COOSDR020208 1 20020701 A 5755 651734874 SKIN BOEING 727 7272J7 138400E NM RT WING SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 RIGHT WING SPOILER NR 9 (PN 65-17348-74) (SN 9087K) LOWER SKIN WITH DELAMINATION. 2 L 7 3 4F A3WE 2002073000004 20020730 00004 NM 2002 7 30 COOSDR020209 1 20020701 A 5755 651734874 SKIN BOEING 727 7272J7 138400E NM LT WING SPOILER DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 LEFT WING SPOILER NR 7 (PN 65-17348-74) (SN 7888K) LOWER SKIN WITH DELAMINATION. 2 L 7 3 4F A3WE 2002073000005 20020730 00005 NM 2002 7 30 COOSDR020210 1 20020701 A 5753 652163585 SKIN BOEING 727 7272J7 138400E NM LT WING TE FLAP CORRODED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 LEFT WING, OUTBOARD AFT FLAP (PN 65-21635-85) (SN BN120) UPPER SKIN AND HONEYCOMB CORE SECTION CORRODED. 2 L 7 3 4F A3WE 2002073000006 20020730 00006 NM 2002 7 30 COOSDR020214 1 20020701 A 5751 652176666 STRUCTURE BOEING 727 7272J7 138400E NM RT WING AILERON DELAMINATED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 128NA 20879 RIGHT WING, OUTBOARD AILERON TRAILING EDGE (PN 65-21766-66)(SN BN-26) WITH DELAMINATION. 2 L 7 3 4F A3WE 2002073000013 20020730 00013 CE 2002 7 30 GVR2002F00000 1 20020719 A 2520 551900940 SEAT BACK CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE CABIN CRACKED A GVRR K NONE O OTHER IN INSP/MAINT 1 CE 05 84GC 5500493 UPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. CHAIR WAS REPAIRED IAW STC STRUCTURAL SEAT REPAIR. 1 L 7 2 4F 4 F A22CE E1NE 2002073000014 20020730 00014 CE 2002 7 30 VJ32002F00051 1 20020705 A 2721 972394 TRIM SWITCH BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO RUDDER FAILED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 01 8112T 257 CE1539 825753R DURING GROUND RUN, TESTED RUDDER TRIM SWITCH. RUDDER TRIM MOVED TO THE LEFT BUT WOULD NOT MOVE TO THE RIGHT. PROBABLE CAUSE IS INTERNAL FAILURE OF THE SWITCH CIRCUITS. 1 L 7 1 3O 3 O 3A15 E5CE 2002073000015 20020730 00015 CE 2002 7 30 VJ32002F00052 1 20020711 A 3230 SM50D7 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520* 17032 SO MLG FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 8112T 584 CE1539 825753R LANDING GEAR FAILED TO COME UP IN FLIGHT. JACKED AIRCRAFT AND OPS CHECKED LANDING GEAR SYSTEM AND RELAY FAILED. TAPPED ON UP SIDE OF RELAY AND POINTS RELEASE ALLOWING GEAR TO ROTATE UP. THIS RELAY HAD A MINIMUM OF 1032 GEAR CYCLES ON IT. RECOMMENDATION FOR PREVENTATIVE RECURRENCE IS MAKING THIS PART A LIFE LIMIT PART OF 500 HOURS OF 1000 GEAR CYCLES WHIC H EVER COMES FIRST. 1 L 7 1 3O 3 O 3A15 E5CE 2002073000016 20020730 00016 CE 2002 7 30 VJ32002F00053 1 20020708 A 3230 SM50D7 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MLG FAILED B VJ3R O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 1565A 549 CE1331 825752R DURING FLIGHT LANDING GEAR FAIL TO RETRACT. UP SIDE OF DYNAMIC RELAY POINTS FAIL TO RELEASE. PROBABLE CAUSE IS HEAT AN D NUMBER OF GEAR RECYCLED. RECOMMENDATIONS FOR PREVENTIVE RECURRENCE DEVELOP BETTER RELAY. 1 L 7 1 3O 3 O 3A15 E5CE 2002073000017 20020730 00017 CE 2002 7 30 VJ32002F00054 1 20020711 A 3230 SM50D7 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO LANDING GEAR FAILED B VJ3R O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 5540P 543 CE1335 820456R LANDING GEAR FAILED TO COME UP IN FLIGHT. JACKED AIRCRAFT AND OPS CHECKED LANDING GEAR SYSTEM AND RELAY FAILED. TAPPED ON UP SIDE OF RELAY AND POINTS RELEASE ALLOWING GEAR TO ROTATE UP. THIS RELAY HAD A MINIMUM OF 1031 GEAR CYCLES ON IT RECOMMENDATION FOR PREVENTATIVE RECURRENCE IS MAKE THIS PART A LIFE LIMIT PART OF 500 HOURS OF 1000 GEAR CYCLES WHICH E VER COMES FIRST. 1 L 7 1 3O 3 O 3A15 E5CE 2002073000018 20020730 00018 SO 2002 7 30 VJ32002F00055 1 20020711 A 3610 RA215CC PUMP PIPER PA28 PA28181 7102807 SO LYC O360 O360A4M 41514 EA DRY AIR FAILED B VJ3R O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 9299B 2843116 RL1775936A DURING FLIGHT OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE. CHECKED SYSTEM FOR LEAKS AND CHEC KED REGULATOR FOR PROPER OPERATION, ALL CHECKED WELL. SUSPECT PROBABLE CAUSE IS HEAT. NO RECOMMENDATION FOR CORRECTIVE ACTION AT THIS TIME. 1 L 7 1 3O 3 O 2A13 E286 2002073000019 20020730 00019 EA 2002 7 30 WVBA2002016 2 20020725 A 8550 LW13388 GASKET PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA LT ENGINE MISINSTALLED A WVBA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 AL 01 4082T 226 318152089 FLIGHT DEPARTED, PILOT NOTICED FLAMES FLICKERING THROUGH THE INSPECTION DOOR ON THE LEFT ENGINE AFTER REDUCING POWER, HE NOTED NO OIL PRESSURE AND SECURED THE ENGINE. THE AIRCRAFT RETURNED TO AIRPORT WITHOUT FURTHER INCIDENT. IT WAS DISCO VERED THAT CONVERTER KIT LW-13904D HAD BEEN INSTALLED SEVERAL HUNDRED HOURS PRIOR WITHOUT THE TECHNICIANS KNOWLEDGE OF T HE REQUIREMENTS OF MSB 543A SUPP NR1 ENGINE IS RETIRED FROM SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 2002073000022 20020730 00022 NM 2002 7 30 AWXA200200584 1 20020705 A 2110 VFT300B00 VALVE AIRBUS A319 A319132 3930340 NM ZONE 126 FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 808AW 10564 1088 DEN - AIR TURN BACK - FLT 0543 - AFTER TAKEOFF FROM DEN EN ROUTE TO LAS RECEIVED ECAM MESSAGE FOR "VENT SKIN VALVE FAULT " ACCOMPLISHED ECAM ACTIONS AND RETURNED TO DEN. MAINTENANCE PLACED VENT SKIN AIR VALVE ON MEL 21-26-04 COND. 1, EXTRACT VALVE INOPERATIVE. ON 07/06/2002 IN PHX MAINTENANCE REMOVED AND REPLACED THE VENT SKIN AIR VALVE (22HG) IAW AMM 21-26-5 3-401, OPERATIONAL CHECK WAS GOOD AND THE MEL PLACARD WAS REMOVED. **SUPP** VENDOR BENCH TEST OF SKIN AIR VALVE S/N 2125 COULD NOT CONFIRM FAILURE (NO FAULT FOUND), UNIT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002073000024 20020730 00024 NM 2002 7 30 AWXA200200636 1 20020718 A 7500 6774E010000 VALVE AIRBUS A319 A319132 3930340 NM NR 2 ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 807AW 1064 RDU - AIR TURN BACK - FLT 0528 - AFTER TAKEOFF FROM RDU EN ROUTE FOR PHX ECAM DISPLAYED AIR ENGINE NR 2 BLEED FAULT. FOL LOWED ECAM ACTION AND FAULT CLEARED, FAULT REAPPEARED AND CLEARED SEVERAL TIMES BEFORE PRESSURE REGULATING VALVE CLOSED FOR GOOD. ECAM THEN DISPLAYED AIR ENGINE NR 1 BLEED FAULT, BLEED PAGE REVEALED HIGH PRECOOLER TEMPERATURE OF 305 DEGREES . AIRCRAFT TURNED BACK TO RDU AND LANDED WITHOUT FUTHER EVENT. **SUPP** MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE THERMOSTATIC TEMPERATURE CONTROL IAW AMM 36-11-43-04, AND THE NR 2 ENGINE BLEED PRESSURE REGULATING VALVE IAW AMM 36-11 -52-04, OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2002073000025 20020730 00025 NM 2002 7 30 AWXA200200639 1 20020626 A 5315 BAC1518338 FLOORBEAM BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 LCQ - MAJOR REPAIR - DURING C-11 CHECK CORROSION WAS FOUND ON CABIN FLOORBEAM AT BS 1640, LBL 25 TO LBL 35. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM BS 1640, FABRICATED 2 EACH REPAIR ANGLES, 2 EACH STRAPS, AND A CHORD, AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, PG. 209-213. 2 L 7 2 4F RT A2NM 2002073000026 20020730 00026 NM 2002 7 30 AWXA200200640 1 20020702 A 5712 654646047 RIB BOEING 737 7373G7 1384595 NM RT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 YVR - MAJOR REPAIR - DURING C-14 CHECK A CRACK WAS FOUND ON THE RT WING T/E, AT THE INBOARD SIDE OF THE AILERON HINGE S UPPORT RIB, WS 340. MAINTENANCE REMOVED THE CRACKED SUPPORT RIB AT WS 340, FABRICATED A NEW RIB, AND INSTALLED REPAIR IA W DWG 65-46460-47, AND B737-300 SRM 51-10-2, PG. 12. 2 L 7 2 4F RT A16WE 2002073000027 20020730 00027 NM 2002 7 30 AWXA200200642 1 20020710 A 5310 6555874503 FITTING BOEING 737 7373G7 1384595 NM DOOR FRAME WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 YVR - MAJOR REPAIR - DURING C-14 CHECK THE AFT GALLEY DOOR FORWARD FRAME, 2ND STOP FITTING FROM THE TOP WAS FOUND TO HAV E INSUFFICIANT EDGE MARGIN AT THE DOOR ASSIST HANDLE ATTACH BS 951. MAINTENANCE REMOVED DOOR STOP FITTING BS 951, FABRIC ATED A FRAME FILLER, A STRAP, AND 2 EACH SPLICE STRAPS, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5311-02200-ES3 2 L 7 2 4F RT A16WE 2002073000028 20020730 00028 NM 2002 7 30 AWXA200200643 1 20020704 A 5313 6978163U8 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 YVR - MAJOR REPAIR - DURING C-14 CHECK A 3/4 INCH CRACK WAS FOUND ON THE R/H STRINGER 18A SHEAR BEAM WEB AT BS 727 ATTAC HMENT. MAINTENANCE REMOVED CRACKED RT STRINGER 18A SHEAR BEAM WEB AT BS 727, FABRICATED A NEW SHEAR BEAM WEB, AND INSTA LLED REPAIR IAW DWG 65-46877, AND B737-300 SRM 51-40-02, PG. 12. 2 L 7 2 4F RT A16WE 2002073000029 20020730 00029 NM 2002 7 30 AWXA200200644 1 20020722 A 3350 10003113 LIGHT BOEING 737 73733A 1384673 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 166AW 23627 LAS - EEL - DURING INSPECTION THE LEFT AFT GALLEY EMERGENCY AISLE PATHWAY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE LEFT AFT GALLEY EMERGENCY AISLE PATHWAY LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002073000030 20020730 00030 NM 2002 7 30 AWXA200200645 1 20020722 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 820AW 5653 1397 PHX - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHTING AT SEAT ROWS 14, 17, AND 20 LT WERE FOUND INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 13WL PER AMM 33-51-04, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002073000031 20020730 00031 WP 2002 7 30 AALA20020594 1 20020503 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 472AA 49647 TUL - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK B5-27 INOPERATIVE. REPLACE D B5-27 EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002073000032 20020730 00032 WP 2002 7 30 AALA20020595 1 20020502 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 574AA 53151 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING AND LOWER TAIL CONE LIGHTS DIM. REPLACED EMERGENCY EXIT LIGH T BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002073000033 20020730 00033 WP 2002 7 30 AALA20020597 1 20020502 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 558AA 53088 TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK B5-23 INOPERATIVE. REPLACED B5-2 3 EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002073000034 20020730 00034 WP 2002 7 30 AALA20020622 1 20020507 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAILCONE DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70401 49312 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. RECONNECTED TAIL CONE OVERHEAD EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002073000035 20020730 00035 WP 2002 7 30 AALA20020635 1 20020511 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 466AA 49596 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002073000036 20020730 00036 WP 2002 7 30 AALA20020637 1 20020511 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7535A 49989 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FORWARD OF ENTRY HARNESS OF FIRST CLASS DIM. REPLACED EMERGEN CY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002073000037 20020730 00037 WP 2002 7 30 AALA20020640 1 20020512 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 573AA 53092 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT INOPERATIVE. REPLACED FIRST CLASS EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002073000038 20020730 00038 2002 7 30 AWXA200200646 4 20020722 A 2565 D31865109 COVER AIRBUS A319 A319132 3930340 NM ESCAPE SLIDE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 803AW 38356 931 PHX - EMERGENCY ESCAPE EQUIPMENT - DURING POST FLIGHT INSPECTION THE EDGE OF THE LT OVERWING DUAL LANE SLIDE COVER WAS F OUND DELAMINATING. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING ESCAPE SLIDE PACK ASSEMBLY IAW T/C R1A25301. 2 L 7 2 4F RT A28NM 2002073000039 20020730 00039 NM 2002 7 30 AWXA200200653 1 20020623 A 5347 6545410200 SEAT TRACK BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK A 3/4 INCH CRACK WAS FOUND ON MAIN DECK SEAT TRACK FLANGE, FORWARD INBOARD SIDE, BS 727B, RBL 45.5. MAINTENANCE REMOVED AND DISCARDED EXISTING STRAP; TRIMMED OUT CRACKED AREA; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND 2 EACH STRAPS, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5702-02191-S S1. 2 L 7 2 4F RT A16WE 2002073000040 20020730 00040 WP 2002 7 30 AALA20020649 1 20020514 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 203AA 49145 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS AT ROWS 13-21 GO DIM TO OFF. SEATED EMERGENCY EXIT CE ILING LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002073000041 20020730 00041 WP 2002 7 30 AALA20020650 1 20020514 A 2560 P2070003001 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 411AA 49322 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002073000042 20020730 00042 NM 2002 7 30 AWXA200200654 1 20020628 A 5320 655966412 SPLICE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 MCN - MAJOR REPAIR - DURING C-18 CHECK A 2 3/4 INCH CRACK WAS FOUND ON STRINGER SPLICE AT BS 360, STR 23 RT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE AT BS 360, STR 23 RT, FABRICATED A NEW STRINGER SPLICE, AND INSTALLED REPAIR IAW B737-3 00 SRM 51-40-02, PG. 3-4. 2 L 7 2 4F RT A16WE 2002073000043 20020730 00043 EU 2002 7 30 AWXA200200657 1 20020723 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DEFECTIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 659AW 9422 1166 PHX - EEL - FORWARD FLIGHT ATTENDANT PANEL INDICATES INTERIOR EMERGENCY LIGHT FAULT CODE. MAINTENANCE REMOVED AND REPLAC ED EMERGENCY POWER SUPPLY UNIT (10WL) IAW AMM 33-51-38-000-001, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002073000044 20020730 00044 NM 2002 7 30 AWXA200200660 1 20020701 A 5313 69374112 TIE BOEING 737 7373G7 1384595 NM STRINGER CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/2 INCH CRACK WAS FOUND ON STRINGER TIE CLIP BS 277, STR 15 RT. MAINTENANCE RE MOVED STRINGER TIE CLIP AT BS 277, STR 15 RT, FABRICATED A NEW STRINGER TIE, AND INSTALLED REPAIR IAW SRM 5I-40-02, PG. 3-4, 10-11, & 38, AND DWG 69-37411. 2 L 7 2 4F RT A16WE 2002073000045 20020730 00045 NE 2002 7 30 AWXA200200667 2 20020724 A 7230 BLADE BOEING 737 737277 1384570 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A AWXA O OTHER J WARNING INDICATION CR CRUISE 1 WP 28 178AW 22645 P708323B PHX - EMERGENCY LANDING - EN ROUTE FROM AUS TO PHX FLIGHT CREW NOTICED A NR 1 ENGINE VIBRATION WITH A SPIKE IN EGT, ALL ENGINE GAUGES LOOKED NORMAL, LANDED AT PHX. DAMAGE NOTED TO TURBINE SECTION, MAINTENANCE REMOVED AND REPLACED THE NR 1 E NGINE PER T/C'S R5M71003 AND F5M71002. VENDOR TEARDOWN OF ENGINE S/N P708323B DETERMINED CAUSE OF FAILURE WAS DUE TO FRA CTURED T3 BLADES AIRFOIL. OTHER SIGNIFICANT FINDING INCLUDE: C1, T2 BLADES SCRAPPED FOR NICKS AND CRACKS, T3 & T4 BLADES SCRAPPED DUE TO FRACTURE, T2 DISK, LPT SHAFT, T3 & T4 INNER AIR SEALS SCRAPPED FOR RUBBING, AND T3 & T4 OUTER AIR SEALS SCRAPPED FOR NICKS. ENGINE REBUILT, ALL DEFECTIVE PARTS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 2002073000046 20020730 00046 NM 2002 7 30 AWXA200200673 1 20020727 A 2560 P2070001101 FLASHLIGHT BOEING 757 757225 1384959 NM CABIN DISCHARGED A AWXA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 28 914AW 22208 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THAT THE EMERGENCY FLASHLIGHT AT 5TH JUMPSEAT NEEDS TO BE REPLACED. MAI NTENANCE REMOVED AND REPLACED THE 5TH JUMPSEAT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002073000047 20020730 00047 NM 2002 7 30 AWXA200200674 1 20020728 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 801AW 889 LAS - EEL - DURING INSPECTION THE FORWARD EMERGENCY ESCAPE PATH LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002073000048 20020730 00048 SO 2002 7 30 SIMA200213601 1 20020516 A 2760 SPOILER EMB 135 EMB135KL 3260302 SO WING MALFUNCTIONED A SIMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 815AE 145545 OAK - FLT 3403 - DURING APPROACH CREW NOTED SPOILER FAIL IND ON EICAS. SPOILERS WOULD NOT RETRACT AND CREW HAD TO LAND A/C WITH SPOILERS DEPLOYED. CREW DECLARED EMERGENCY UPON LANDING, AFTER LANDING IND WENT AWAY AND SPOILERS RETRACTED. AIRCRAFT LANDED SAFELY AND NO FURTHER INCIDENTS WERE REPORTED. PERFORMED OPS CHECK OF SPOILER SYSTEM, CHECK OK. (M) 2 L 7 2 4F RT T00011AT 2002073000049 20020730 00049 EU 2002 7 30 SIMA200215110 1 20020519 A 5347 S53375001204 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP4 INSPECTION, FOUND FORWARD SEAT TRACK CORRODED. RAI'D LEFT FORWARD SEAT TRACK IAW EO E1-53MR-271. AI RCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002073000050 20020730 00050 EU 2002 7 30 SIMA200215111 1 20020529 A 5320 S5367121729801 TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW DURING CPCP4 INSPECTION, SERVICE DOOR DRAIN TRACK CORRODED. INSTALLED NEW SERVICEABLE DRAIN TRACK IAW ATR 42 SRM 5 1-25-01. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002073000051 20020730 00051 EU 2002 7 30 SIMA200215112 1 20020529 A 5320 S5367131828001 SILL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP 4 INSPECTION, SERVICE DOOR SILL PLATE CORRODED. INSTALLED NEW SERVICE DOOR SILL PLATE IAW ATR 42 SRM 51-25-01. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002073000052 20020730 00052 NM 2002 7 30 ABXA020050 1 20020527 A 5730 114T0222 SKIN BOEING 767 767200 1385120 NM LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783AX 23016 LEFT WING, FRONT SPAR, LOWER CHORD, JUST OUTBOARD OF THE NR 1 PYLON, WAS CORRODED AT APPROXIMATELY 0FSS 400. REPAIRED AR EA IAW REA B657-43893. 2 L 7 2 4F RT A1NM 2002073000053 20020730 00053 NM 2002 7 30 ABXA020052 1 20020616 A 2730 BEARING BOEING 767 767200 1385120 NM LT ELEVATOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 786AX 23019 LEFT ELEVATOR, OUTBOARD PCA HAD A WORN AFT ATTACH BEARING. REPLACED ELEVATOR PCA IAW B767 MM. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2002073000054 20020730 00054 EU 2002 7 30 SIMA200215113 1 20020529 A 5753 S5751004900300 GUIDE AEROSP ATR42 ATR42300 8680920 EU T/E FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING MBV-1, FOUND RIGHT WING INBOARD FLAP INBOARD DEFLECTOR INBOARD CAM GUIDE CORRODED. REPLACED RIGHT WING INB OARD FLAP INBOARD DEFLECTOR INBOARD CAM GUIDE IAW SRM 57-52-20 FIG 401. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002073000055 20020730 00055 EU 2002 7 30 SIMA200215114 1 20020529 A 5320 S5367800920002 FLOOR SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP2, FOUND LEFT FLOOR SUPPORT FROM FRAME 36-38 CORRODED. INSTALLED NEW LEFT FLOOR SUPPORT FROM 36-38 IAW ATR 42 SRM 51-25-01. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002073000056 20020730 00056 EU 2002 7 30 SIMA200215115 1 20020529 A 5311 S53671311206 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 DURING CPCP2 FOUND RIGHT FRAME 37 CORRODED ON FORWARD SIDE BELOW SILL PLATE. RAI'D RIGHT FRAME 37 IAW SRM 51-25-02 AND 51-25-04. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002073000057 20020730 00057 EU 2002 7 30 SIMA200215116 1 20020529 A 5210 S5217620520201 DOOR FRAME AEROSP ATR42 ATR42300 8680920 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP2 FOUND PASSENGER DOOR INTERNAL FRAME JUST ABOVE VENT DOOR CORRODED. REMOVED AND REPLACED FRAME IAW SR M 51-25-02 AND 51-25-03. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002073000058 20020730 00058 EU 2002 7 30 SIMA200215601 1 20020526 A 5753 S5751008002000 ATTACH FITTING AEROSP ATR42 ATR42300 8680920 EU T/E FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING MBV-1 INSPECTION, FOUND LEFT OUTBOARD FLAP, OUTBOARD ATTACHMENT FITTING AND FORWARD SPAR CORRODED. REMOVED AND REPLACED FLAP ASSEMBLY IAW ATR JIC 57-53-00-RAI-10000. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002073000060 20020730 00060 SO 2002 7 30 SIMA200215702 1 20020531 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - DURING INSPECTION FOUND CORROSION ON PREVIOUS REPAIR, FORWARD DIGITAL. REMOVED PREVIOUS REPAIR. FABRICATED AND I NSTALLED NEW DOUBLER IAW EMB SST-249/00, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002073000061 20020730 00061 SO 2002 7 30 SIMA200215703 1 20020531 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - DURING INSPECTION FOUND CORROSION ON GALLEY CENTER FLOORBEAM. REPLACED GALLEY CENTER BEAM IAW EMB 145 SRM 145/114 2, CHAPTER 51, REV 18, ETN EM-53-028, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002073000062 20020730 00062 SO 2002 7 30 SIMA200215704 1 20020602 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - DURING INSPECTION, FOUND CORROSION ON GALLEY RIGHT FLOORBEAM AT FRAME 20. REMOVED CORROSION BY BLENDING. FABRICA TED AND INSTALLED DOUBLER IAW EMB GST-1707/02, ITEM NR 2, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002073000063 20020730 00063 SO 2002 7 30 SIMA200215706 1 20020530 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - DURING INSPECTION FOUND CORROSION ON GALLEY RIGHT FLOORBEAM FRAME 23. REMOVED CORROSION BY BLENDING. FABRICATED AND INSTALLED DOUBLER IAW EMBGST1707/02, ITEM NR 2, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002073000064 20020730 00064 NM 2002 7 30 ABXA020053 1 20020616 A 2710 251T15973 TUBE BOEING 767 767200 1385120 NM RT LCCA WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 786AX 23019 RIGHT LCCA TUBE ASSEMBLY HAD WORN/RUSTED PIVOT BEARINGS. REPLACED LCCA TUBE ASSEMBLY IAW B767 MM. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2002073000065 20020730 00065 SO 2002 7 30 SIMA200215707 1 20020602 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - DURING INSPECTION FOUND STRINGER 19R CHAFED AT FRAME 53. BLENDED CHAFE, FABRICATED AND INSTALLED DOUBLER, WITH TW O SHIMS IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 18 53-25-02, ETN EM 51-020, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002073000066 20020730 00066 NM 2002 7 30 ABXA020054 1 20020616 A 2710 BEARING BOEING 767 767200 1385120 NM RT AILERON WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 786AX 23019 RT OUTBOARD AILERON, OUTBOARD PCA REACTION LINK BEARINGS WORN. REPLACED AILERON PCA IAW B767 MM. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2002073000067 20020730 00067 SO 2002 7 30 SIMA200215708 1 20020605 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 ABI - DURING INSPECTION FOUND STRINGER 19L CHAFED AT FRAME 53. BLENDED CHAFE. FABRICATED AND INSTALLED DOUBLER ANGLE, WITH TWO SHIMS IAW EMB 145 (145/1142, CHAPTER 53, REV 18) 532-24-02, ETN EM-51-020, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002073000068 20020730 00068 NM 2002 7 30 ABXA020055 1 20020616 A 2710 BEARING BOEING 767 767200 1385120 NM RT AILERON WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 786AX 23019 RT OUTBOARD AILERON, INBOARD PCA REACTION LINK BEARINGS WORN. REPLACED AILERON PCA IAW B767 MM. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2002073000069 20020730 00069 SO 2002 7 30 SIMA200215709 1 20020603 A 5320 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 ABI - DURING INSPECTION FOUND CORROSION ON PREVIOUS REPAIR FORWARD DIGITAL. REMOVED PREVIOUS REPAIR. FABRICATED AND IN STALLED DOUBLER, IAW EMB SST-2906/00, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002073000070 20020730 00070 NM 2002 7 30 ABXA020056 1 20020616 A 2710 251T130515 TUBE BOEING 767 767200 1385120 NM LEFT LCCA WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 786AX 23019 LEFT LCCA CONTROL TUBE ASSEMBLY HAD WORN PIVOT BEARINGS. REPLACED LEFT LCCA TRUBE ASSEMBLY IAW B767 MM. OPS CHECKED GOOD . 2 L 7 2 4F RT A1NM 2002073000071 20020730 00071 SO 2002 7 30 SIMA200215710 1 20020602 A 5320 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 DURING INSPECTION, FOUND CORROSION ON LEFT OMEGA BEAM PREVIOUS REPAIR AT FRAME 20. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED DOUBLER ANGLE, FILLER, PLATE, WITH TWO SHIMS IAW EMB 145, SRM 145/1142, CHAPTER 53, REV 18, 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002073000072 20020730 00072 WP 2002 7 30 ABXA020057 1 20020710 A 2611 FIRE DETECTOR DOUG DC8 DC863F 302198F WP CARGO BAY FALSE INDICATION A ABXA B EMER. DESCENT N FALSE WARNING AP APPROACH 1 GL 23 815AX 46097 ON ONE MILE FINAL, THE LOWER CARGO FIRE LIGHT ILLUMINATED. MX DISPLAY SHOWED "FWD A FIRE". EMERGENCY DECLARED INTO KILN BY CREW. LANDED AND CLEARED RUNWAY, TOWER AND CRASH CREW OBSERVED NO EVIDENCE OF FIRE. APPROXIMATELY 5 MINUTES AFTER, CA RGO FIRE INDICATED LIGHT EXTINGUISHED. TAXIED TO GATE AND DID BATTERY SHUT DOWN. INSPECTED CARGO HOLD 1 AND 2, NO FIRE. PERFORMED FIRE DETECTION SYSTEM TEST. SYSTEM CHECKED GOOD. PERFORMED ADJUSTMENT/TEST IAW DC-8 SMM 26-15-00. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2002073000073 20020730 00073 NM 2002 7 30 2002UALA01175 1 20020715 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 CABIN STATION 887 FRAME WEB IS CRACKED AT STRINGER 9L INBOARD RIVET FOR AIR GRILL ATTACHMENT. MAJOR REPAIR ACCOMPLISHED . REMOVED DAMAGED AREA, DRILLED MATERIAL, TRIMMED TO SIZE AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002073000074 20020730 00074 NM 2002 7 30 2002UALA01176 1 20020715 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 FORWARD CABIN FRAME IS CRACKED STATION 380 STRINGER 9L PASSENGER SERVICE UNIT ATTACHMENT. MAJOR REPAIR ACCOMPLISHED. I NSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002073000075 20020730 00075 NM 2002 7 30 2002UALA01178 1 20020715 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 RIGHT HAND LOWER FUSELAGE SKIN IS DENTED AT STATION 326 3 INCHES BELOW STRINGER 22R. MAJOR REPAIR ACCOMPLISHED. INSTAL LED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002073000076 20020730 00076 NM 2002 7 30 2002UALA01180 1 20020625 A 5754 FILLER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE L/E SLAT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 216UA 30549 FILLER WAS MISSING FROM THE SPANWISE BULB SEAL ON SLAT NR 14 AND 15 INCHES OF THE OUTBOARD END OF THE FILLER WAS MISSING FROM THE NR 1 SEAL. MAJOR REPAIR ACCOMPLISHED. FILLER INSTALLED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002073000077 20020730 00077 NE 2002 7 30 ABXA020059 2 20020719 A 7320 7436024 FUEL CONTROL DOUG DC9 DC941 302207N WP PWA JT8 JT8D15 52051 NE NR 1 ENGINE MALFUNCTIONED A ABXA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 23 964AX 23 47781 686282 NR 1 ENGINE WOULD NOT DECELERATE FROM FULL POWER TO IDLE, WOULD NOT RESPOND AFTER THE THROTTLE WAS RETARDED. IN-FLIGHT S HUTDOWN AND DID AN AIR TURN BACK. REPLACED THE FUEL CONTROL AND MAIN FUEL PUMP IAW DC-9 MM 73-20-01-2. 2 L 7 2 4F 4 F A6WE E2EA 2002073000078 20020730 00078 NE 2002 7 30 2002UALA01181 2 20020715 A 7250 BLADE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ENGINE FAILED A UALA E ENGINE SHUTDOWN G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 WP 29 116UA 26908 EXPERIENCED PROBLEMS W/EEC, BLEED, OIL QTY AND PRESSURE. SUPPLEMENTAL DATA UPDATE ENGINE SURGED DUE TO FAILURE OF HPT T -2 BLADE. T2 BLADE FAILURE WAS DUE TO CORROSION UNDER THE BLADE PLATFORM. RESULTANT VIBRATION FRACTURED NR 4 BEARING OIL TUBE AND EGT HARNESS CAUSING LOSS OF OIL PRESSURE AND ERRONEOUS EGT INDICATION. ENGINE WAS REMOVED FOR REFURBISHMENT A ND INSTALLATION OF IMPROVED T-2 BLADES PER SB PW4ENG 72-716. 2 L 7 4 4F 4 F RT A20WE E24NE 2002073000079 20020730 00079 WP 2002 7 30 ABXA020065 1 20020520 A 5340 37558241 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 FORWARD CARGO, FS 300, BETWEEN LONGERON 33 RIGHT - LONERON 34 RIGHT, "Z" FITTING WAS CORRODED. REPLACED "Z" FITTING AND REPAIRED AREA IAW DC-8 SRM 51-3-2, 51-1-20D AND DAC DRAWING #3755824. 2 L 7 4 4F 4A25 2002073000080 20020730 00080 WP 2002 7 30 ABXA020068 1 20020723 A 2120 ODOR DOUG DC9 DC932 3022066 WP COCKPIT DETECTED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 985AX 47522 DURING FLIGHT, SMELLED A SULFUR ODOR TWICE. EACH LASTED FOR ABOUT 30 SECONDS, THEN WENT AWAY. VERY MUCH LIKE A MATCH BEI NG LIT AND THEN SNUFFED OUT. CHECKED ALL CIRCUIT BREAKERS, NONE TRIPPED. CHECKED ELECTRICAL COMPONENTS. OPS CHECKED NORM AL. RAN BOTH A/C PACKS, CHECKED NORMAL. COULD NOT REPRODUCE THE SMELL OR ODOR. 2 L 7 2 4F A6WE 2002073000081 20020730 00081 NM 2002 7 30 2002UALA01183 1 20020625 A 5754 FILLER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE L/E SLAT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 222UA 30553 SLATS NR 1 & 14 FILLERS WERE MISSING FROM SPANWISE BULB SEALS. MAJOR REPAIR ACCOMPLISHED. FILLERS INSTALLED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002073000082 20020730 00082 NM 2002 7 30 2002UALA01184 1 20020717 A 5320 SILL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 FORWARD GALLEY DOOR CUTOUT LOWER SILL INBOARD CHORD HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW CHORD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900071 20020809 00071 EU 2002 8 9 2002UALA01185 1 20020717 A 2421 766219 IDG AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE OVERTEMP A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 416UA 479 ABORTED TAKEOFF AT 80 KNOTS DUE TO LEFT ENGINE IDG FAULT LIGHT. NR 1 ENGINE IDG FAULT LIGHT CAME ON DURING TAKEOFF. NR 1 IDG REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002073000083 20020730 00083 NM 2002 7 30 2002UALA01186 1 20020717 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 CABIN FLOORBEAM STATION 1660 BL 0 UPPER FLANGE HAS 18.6 PERCENT MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLO ORBEAM UPPER CAP. BLEND OUT ANGLE AND STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082300105 20020823 00105 NM 2002 8 23 2002UALA01187 1 20020717 A 2612 896768 FIRE LOOP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE APU SHORTED A UALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 916UA 25383 AIRCRAFT HAD AN APU FIRE INDICATION DURING INITIAL CLIMBOUT, FOLLOWED PROCEDURES, AND RETURNED TO THE FIELD. MAINTENANC E INSPECTED THE APU AREA, CHECKED ALL PNEUMATIC DUCTS AND SEALS FOR LEAKS AND NO DEFECTS (LEAKS) WERE FOUND. INSPECTED APU OVERHEAT DETECTION SYSTEM, AND FOUND INTERMITTENT SHORT TO GROUND AT CONNECTOR D4934P, PINS A & C. REPLACED APU TAI LPIPE OVERHEAT DETECTOR LOOP M717 AND HARNESS M9324. APU FIRE DETECTION SYSTEM CHECKED GOOD AND AIRCRAFT WAS RETURNED T O SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900073 20020809 00073 NM 2002 8 9 2002UALA01189 1 20020718 A 2933 7586630 INDICATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYD PUMP FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 565UA 26669 RIGHT HYDRAULIC SYSTEM SHOWED EMPTY. DIFFERENTIAL PRESSURE INDICATOR (DPI) ON RT ENGINE DRIVEN PUMP HYDRAULIC PRESSURE MODULE FAILED. REPLACED DPI, EDP AND FILTER MODULE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080900074 20020809 00074 EU 2002 8 9 2002UALA01190 1 20020718 A 2913 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 440UA 702 RETURNED TO FIELD DUE TO OVERHEAT ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE OF GREEN HYDRAULIC PUMP. CHANGED G REEN SYSTEM LOW PRESSURE, HIGH PRESSURE AND CASE DRAIN FILTERS. 2 L 7 2 4F 4 F RT A28NM E40NE 2002080900076 20020809 00076 EU 2002 8 9 2002UALA01191 1 20020718 A 3240 A253151 VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE PARKING BRAKE LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 464UA 1290 LOSS OF YELLOW HYDRAULIC SYSTEM. REPLACED YELLOW SYSTEM PARK BRAKE VALVE 2579GM. 2 L 7 2 4F 4 F RT A28NM E40NE 2002082600024 20020826 00024 NE 2002 8 26 2002UALA01192 2 20020718 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 POWER LOSS A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 535UA 29924 9989 25130 726594 POWER LOSS IN NR 2 ENGINE. THE TEST ON THE FUEL CONTROL UNIT P/N 779100-5, S/N F22470 EXHIBITED SEVERAL PARAMETERS THAT WERE OUT-OF-LIMITS. HOWEVER NONE WERE DEEMED TO HAVE BEEN THE CAUSE OF THE ENGINE SURGE EXPERIENCED ON-WING. FURTHERM ORE, THE TESTS FOUND OUT OF SPEC ARE TYPICAL OF UNITS THAT HAVE ACCRUED NEARLY 10,000 FLIGHT HOURS. FUEL PUMP IS ALSO B EING DISASSEMBLED AND NO NOTICEABLE FAILURES HAVE BEEN IDENTIFIED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002073000084 20020730 00084 NM 2002 7 30 SWAA021568 1 20020716 A 2560 6557463 ATTACH FITTING BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTINGS OUT OF POSITION. REPOSITIONED FITTINGS PER MM. 2 L 7 2 4F RT A16WE 2002073000085 20020730 00085 2002 7 30 SWAA021570 4 20020715 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT CABIN DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 080SW 22675 DURING SCHEDULED C3 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2 L 7 2 4F A16WE 2002073000086 20020730 00086 NM 2002 7 30 SWAA021572 1 20020716 A 2720 65C370539 PCU BOEING 737 7373H4 1384600 NM RUDDER FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 LEFT RUDDER RATCHETING DURING FULL THROW OF RUDDER. RIGHT RUDDER OK. HAPPENS ON BOTH SIDES CAPT AND FO. REMOVED AND R EPLACED RUDDER PCU PER MM. 2 L 7 2 4F RT A16WE 2002073000087 20020730 00087 NM 2002 7 30 SWAA021575 1 20020717 A 3350 900542 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 092SW 22964 DURING SCHEDULED SERVICE CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2002073000088 20020730 00088 NM 2002 7 30 SWAA021578 1 20020716 A 2121 4101054 COOLING FAN BOEING 737 7373H4 1384600 NM E/E BAY OVERHEATED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 640SW 27713 DIVERSION, DETECTED ODOR IN AFT CABIN AND FLT DECK. REMOVED AND REPLACED EQUIPMENT COOLING FAN PER MM. 2 L 7 2 4F RT A16WE 2002073000089 20020730 00089 NM 2002 7 30 SWAA021593 1 20020719 A 3350 90083 BATTERY BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT IN AFT CEILING INOP. REMOVED AND REPLACED EMERGENCY LIGH T BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002073000090 20020730 00090 EU 2002 7 30 U30A200200005 1 20020624 A 2760 B372BAM0509 CONTROL UNIT AIRBUS 320 A320214 3930316 EU NR 1 SPOILER FALSE INDICATION A U30A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 17 261AV 1660 1660 1615 NR 1 SPOILER & ELEVATOR COMPUTER (NR 1 SEC) FAULTED ON ECAM DURING TAXI OUT. RETURNED TO GATE. RE-SET SEC NR 1, PERFOR MED SEC SYSTEM CHECK PER AMM 27-94-00-501 AND AMM 27-94-00-710-053. NO DEFECTS NOTED, OPS CK'D OK. 2 L 7 2 4F RT A28NM 2002073000091 20020730 00091 EU 2002 7 30 U30A200200006 1 20020627 A 3350 1013101 SIGN AIRBUS 320 A320214 3930316 EU CABIN INOPERATIVE A U30A K NONE L NO TEST IN INSP/MAINT 1 EA 17 261AV 1683 1683 1615 AFT CENTER OVERHEAD EMERGENCY EXIT SIGN DID NOT ILLUMINATE ON TEST. LIGHT ASSEMBLY FOUND TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN ASSY. OPERATIONALLY CHECKED OK. 2 L 7 2 4F RT A28NM 2002073000092 20020730 00092 2002 7 30 U30A200200007 4 20020705 A 3460 B546CAM0103 COMPUTER AIRBUS 320 A320214 3930316 EU NR 1 FLIGHT CON MALFUNCTIONED A U30A K NONE L NO TEST IN INSP/MAINT 1 EA 17 260AV 1643 1643 1564 NR 1 AUTOPILOT FAULTED DURING PRE-FLIGHT IN PUJ (FLT 0125 PUJ-BWI). DEFERRED NR 1 AUTOPILOT PER MEL 22-10-01-1 ON 07/05/ 2002. UPON RETURN TO MAINTENANCE BASE(07/06/2002) IN PHL, REMOVED & REPLACED NR 1 FLIGHT MANAGEMENT GUIDANCE COMPUTER ( NR 1 FMGC) IN ACCORDANCE WITH AMM 22-83-34-000-001. UPLOADED FMGC PER AMM 22-70-00-610-005. AFS CK'D PER AMM 22-96-00-71 0-001, OPS CHECKED NORMAL. 2 L 7 2 4F RT A28NM 2002073000093 20020730 00093 EU 2002 7 30 U30A200200008 1 20020708 A 3150 WARNING SYSTEM AIRBUS 320 A320214 3930316 EU COCKPIT FALSE INDICATION A U30A O OTHER N FALSE WARNING LD LANDING 1 EA 17 260AV 1564 AFTER LANDING AT PUJ, FLT 258, ECAM MESSAGE FLT/CNTL FLAPS LOCKED WING TIP BRAKE (WTB) ON, FLAP SYSTEM NR 2 FAULT. (ALSO HAD FLIGHT WARNING COMPUTER FAULT, FWC. SEE U30A200200009). COMPLIED WITH BITE TEST 27-54-00-710-002, NO FAULT FOUND, S YSTEM RESET. FLAPS OPS CHECKED NORMAL. 2 L 7 2 4F RT A28NM 2002073000094 20020730 00094 EU 2002 7 30 U30A200200009 1 20020708 A 3150 WARNING SYSTEM AIRBUS 320 A320214 3930316 EU COCKPIT MALFUNCTIONED A U30A O OTHER N FALSE WARNING LD LANDING 1 EA 17 260AV 1564 AFTER LANDING AT PUJ, FLT 258, ECAM NESSAGE FOR FWC NR 2 FAULTED ( IN CONJUNCTION WITH FLT/CNTL FLAPS LOCKED - WTB ON, F LAP SYSTEM NR 2 FAULTED, SEE U30A200200008). POWERED DOWN AIRCRAFT, BITE TEST PERFORMED - MESSAGE CLEARED. 2 L 7 2 4F RT A28NM 2002073000095 20020730 00095 NM 2002 7 30 SWAA021595 1 20020720 A 3350 100885 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED PM CHECK, FOUND EEPLS LIGHTS INOP (2 EA) JUST AFT OF OVERWING EXITS. REMOVED AND REPLACED EEPLS BATTER Y PER MM. 2 L 7 2 4F RT A16WE 2002073000096 20020730 00096 NM 2002 7 30 SWAA021596 1 20020721 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002073000097 20020730 00097 2002 7 30 SWAA021597 4 20020719 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 102SW 23108 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002073000098 20020730 00098 WP 2002 7 30 2002F00761 1 20020529 A 5320 FLOOR SUPPORT LKHEED 1011 1011385115 5265015 WP FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 198AT 193B1111 DURING SCHEDULED INSPECTION CABIN FLOOR SUPPORT, LEVEL 2 CORROSION ON T-CAP UPPER SURFACE AT FS 900 TO FS 902, WL 200, R BL 30 TO RBL 120. MAINTENANCE REPAIRED T-CAP IN ACCORDANCE WITH LOCKHEED L1011 SRM 53-21-00. 2 L 7 3 4F A23WE 2002073000099 20020730 00099 WP 2002 7 30 2002F00762 1 20020605 A 5711 SPAR LKHEED 1011 10113851 5265010 WP RT WING CRACKED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 186AT 193C1074 THE RIGHT WING REAR SPAR WEB WAS CRACKED AT INBOARD AILERON, INBOARD ACTUATOR FITTING W.S 606.20. MAINTENANCE REPAIRED T HE SPAR WEB IN ACCORDANCE WITH SRM 57-11-00, FIG 813. 2 L 7 3 4F A23WE 2002073000100 20020730 00100 NM 2002 7 30 2002F00763 1 20020527 A 7710 LK83104 TUBE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RIGHT ENGINE MISSING G AMTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 11 553TZ 32587 31808 FLIGHT NUMBER 209. ON CLIMB-OUT, RIGHT ENGINE EPR BEGAN SURGING +/- 0.1. ALL OTHER INSTRUMENTS FOLLOWED. WHEN AUTOTHROTT LES TURNED OFF, ENGINE STABILIZED. IN CRUISE, ANY MOVEMENT OF THROTTLES WOULD RESTART SURGING. MAINTENANCE FOUND PF RAKE PITOT PROBE AT NINE O'CLOCK POSITION ON RIGHT ENGINE MISSING. PERFORMED PITOT TUBE TO STRUT BOND REPAIR IN ACCORDANCE W ITH ERA 757-72T-4666. 2 L 7 2 4F 4 F RT A2NM E12EU 2002073000101 20020730 00101 NM 2002 7 30 2002F00766 1 20020701 A 3397 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHTS BROKEN G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 520AT 27976 DURING SCHEDULED MAINTENANCE EGRESS FLOOR LIGHTS INOP FROM ROW 31 THROUGH 35. MAINTENANCE RECONECTED BROKEN WIRE AS REQU IRED, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002073000102 20020730 00102 NM 2002 7 30 2002F00767 1 20020628 A 3397 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHTS BROKEN G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 520AT 27976 DURING SCHEDULED MAINTENANCE THE FIRST WHITE FLOOR PATH LIGHT WAS INOP. MAINTENANCE RECONNECTED THE WIRES, OPERATIONAL C HECK GOOD. 2 L 7 2 4F RT A2NM 2002073000103 20020730 00103 NM 2002 7 30 2002F00768 1 20020706 A 3397 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHTS BROKEN G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 525AT 30548 DURING SCHEDULED MAINTENANCE EGRESS LIGHT AT ROW 10 E,D INOP. MAINTENANCE REPAIRED EGRESS LIGHTY WIRING AT 10 E,D IN ACC ORDANCE WITH 33-51-11. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002073000104 20020730 00104 NM 2002 7 30 2002F00769 1 20020716 A 3350 1010428 LIGHT BOEING 757 75723N 1384973 NM CABIN BROKEN G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 522AT 13736 29330 DURING SCHEDULED MAINTENANCE THE OVERHEAD EMERGENCY LIGHT AT ROW 16 DEF WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLAC ED ROW 16 DEF AISLE LIGHT PER M/M 33-51-05. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002073000105 20020730 00105 NM 2002 7 30 2002F00770 1 20020711 A 4900 7321387012 ACTUATOR BOEING 757 75723N 1384973 NM APU INLET DOOR MALFUNCTIONED G AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 528AT 30887 FLIGHT NUMBER 275. DURING CRUISE APU DOOR EICAS MESSAGE DISPLAYED IN FLIGHT. MAINTENANCE PERFORMED FIM 49-11-00, REMOVED AND REPLACED APU INLET DOOR ACTUATOR IN ACCORDANCE WITH M/M 49-15-06-4, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 2002073000106 20020730 00106 NM 2002 7 30 2002F00771 1 20020710 A 3397 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHTS LOOSE G AMTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 11 526AT 30735 FLIGHT NUMBER 209. DURING GROUND HANDLING EMERGENCY ESCAPE PATH TRACK LIGHTING INOP FROM FRONT OF AIRCRAFT TO ROW 4. MAI NTENANCE SECURED LOOSE TRACK TERMINAL CONNECTION PER M/M 33-51-11, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002073000107 20020730 00107 NM 2002 7 30 2002F00772 1 20020723 A 3397 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHTS DISCONNECTED G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 525AT 30548 DURING SCHEDULED MAINTENANCE EMERGENCY EGRESS LIGHT ROW DEF 1 THROUGH 10 INOP. MAINTENANCE RECONNECTED LOOSE WIRE, OPERA TIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002073000108 20020730 00108 NM 2002 7 30 2002F00773 1 20020723 A 3350 8100022608 LIGHT BOEING 757 75723N 1384973 NM CABIN INOPERATIVE G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 517AT 27973 DURING SCHEDULED MAINTENANCE MULTIPLE EGRESS FLOOR LIGHTS INOP FROM ROW 5 TO FORWARD GALLEY. MAINTENANCE REMOVED AND REP LACED LIGHT ASSY AT ROW 5 PER M/M 33-51-11, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002073000109 20020730 00109 NM 2002 7 30 2002F00774 1 20020723 A 3350 CONNECTOR BOEING 757 75723N 1384973 NM EMERGENCY LIGHTS DAMAGED G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 517AT 27973 DURING SCHEDULED MAINTENANCE 3 EGRESS FLOOR TRACK LIGHTS INOP IN FRONT OF R1 LAVATORY. MAINTENANCE RECONNECTED PINS AT L IGHT ASSY PER M/M 33-51-11, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002073000110 20020730 00110 NM 2002 7 30 SWAA021599 1 20020719 A 3350 6104781 BATTERY BOEING 737 7373H4 1384600 NM CARGO BAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED SERVICE CHECK, FOUND RT OTBD OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002073000111 20020730 00111 NM 2002 7 30 SWAA021600 1 20020719 A 3350 65C36053 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP JUST AFT OF AFT ENTRY DOOR. REMOVED AND REPLACED EMERGE NCY EXIT LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2002073000112 20020730 00112 NM 2002 7 30 SWAA021602 1 20020720 A 2560 6557463 FITTING BOEING 737 737301 1384611 NM ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTINGS, LOOSE FASTENERS AT FWD ENTRY DOOR. SECU RED FASTENERS PER MM 2 L 7 2 4F RT A16WE 2002073000113 20020730 00113 NM 2002 7 30 SWAA021603 1 20020720 A 3350 BR2013 LIGHT BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 EEPLS LOOSE AT AFT GALLEY. REMOVED AND REPLACED EEPLS AT AFT GALLEY PER MM. 2 L 7 2 4F RT A16WE 2002073000114 20020730 00114 NM 2002 7 30 SWAA021604 1 20020719 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 501SW 24178 SEVERAL EEPLS INOP IN CABIN. RECONNECTED WIRE PER MM. 2 L 7 2 4F RT A16WE 2002073000115 20020730 00115 SO 2002 7 30 SWIA200210890 1 20020527 A 2750 FLAP EMB 120 EMB120ER 3260203 SO WING MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 209SW 120269 ON DEPARTURE RECEIVED A FLAP DISAGREEMENT ON THE OUTBOARD PAIR. WHILE ON THE RAMP WITHOUT ANY HYD POWER HAD A NACELLE D ISAGREEMENT. LEFT NACELLE FLAP WAS HANGING DOWN A FEW DEGREES ALONG WITH ONE LIGHT BAR ILLUMINATED ON THE FLAP ANNUNCIA TOR PANEL. REMOVED AND REPLACED ALL ROLLERS, BOTH FLAPS, AND FIXED INBOARD TRACK ON RIGHT OUTBOARD FLAP. CYCLED FLAPS WITH HYDRAULIC POWER. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073000116 20020730 00116 NE 2002 7 30 2002F00775 2 20020710 A 7200 GASKET BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535* NE RT ENGINE CRACKED G AMTA K NONE J WARNING INDICATION CL CLIMB 1 GL 11 517AT 27973 FLIGHT NUMBER 214. 15 MINUTES AFTER CLIMB-OUT PASSING 18,000 FEET, RT ENGINE OVERHEAT EICAS MESSAGE AND RT STRUT OVERHEA T DET 1 STATUS MESSAGE ILLUMINATED. LIGHT EXTINGUISHED AFTER RT BLEED SWITCH WAS TURNED OFF AND THRUST LEVER RETARDED (A FTER 3 MINUTES). MAINTENANCE PERFORMED FIM 26-11-00, FOUND E GASKET CRACKED ON UPPER HP SHUTOFF VALVE. REPLACED E GASKET AND PERFORMED HIGH POWER RUN IN ACCORDANCE WITH M/M 71-00-00, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2002073000117 20020730 00117 NM 2002 7 30 AMTA200200949 1 20020718 A 3350 110049 CHARGER LKHEED 1011 1011 N/A-SDR NM EMERGENCY LIGHTS INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 186 193C174 EGRESS LIGHTS INOP IN "A" ZONE FRONT HALF 2 L 7 3 4F RT A23WE 2002073000118 20020730 00118 NM 2002 7 30 AMTA200200951 1 20020718 A 2560 2471 CONTROL PANEL LKHEED 1011 1011 N/A-SDR NM COCKPIT INOPERATIVE A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 196 193B1076 EVAC SIGNAL IN FLIGHT DECK WILL NOT SOUND. 2 L 7 3 4F RT A23WE 2002073000119 20020730 00119 EA 2002 7 30 SWIA200210892 1 20020531 A 2612 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CHAFED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 410SW 7066 RECEIVED RIGHT 14TH STAGE DUCT LEAK WARNING CLIMBING THROUGH 7000 FT. AS PER QRH, RETARDED RIGHT ENGINE THRUST TO IDLE. AFTER 40 SECONDS STILL HAD THE WARNING. CLOSED THE RIGHT 14TH STAGE BLEED AND WARNING CLEARED. RETURNED TO OMA. FOU ND 14TH STAGE LOOP TO BE CHAFED IN RIGHT ENGINE PYLON. REMOVED AND REPLACED CHAFED SECTION. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002073000120 20020730 00120 NM 2002 7 30 PCAA0207081 1 20020729 A 2910 82970009189 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM LEFT GEARWELL LEAKING A PCAA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 EA 13 826EX 389 SYR-FLIGHT#3992. CREW REPORTED #2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED IN FLIGHT, LANDING GEAR ALTERNATE EXTENSION PERFORMED. MAINTENANCE INSPECTED AND FOUND HYDRAULIC LINE FROM DOGBONE ON LEFT FORWARD GEAR LEAKING. INTERIM F LEX LINE INSTALLED. HYDRAULIC SYSTEM SERVICED AND ISOLATION LIGHT RESET. AIRCRAFT RAN WITH NO LEAKS NOTED. AIRCRAFT RETU RNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002073000122 20020730 00122 2002 7 30 SWIA200210893 4 20020530 A 3160 6229810012 DISPLAY CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 438SW 7574 CAPTAIN'S MFD WENT BLANK ON DEPARTURE. RETURNED TO SLC. REMOVED AND REPLACED NR 1 MFD IAW CRJ MM 31-61-01. OPS CHECK GOOD. A/C RELEASED FOR CAT II OPERATION. 2 L 7 2 4F RT A21EA 2002073000123 20020730 00123 EU 2002 7 30 VJ32002F00056 1 20020619 A 3610 1U128006 PUMP GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA DRY AIR FAILED B VJ3R A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 07 865AF 75 85005 L2826448A IN FLIGHT THE INSTRUMENT VACUUM SYSTEM FAIL. THE AIRCRAFT RETURNED TO MAINTENANCE AND AN INSPECTION OF THE SYSTEM FOUND ED THAT THE ROTOR SHAFT HAD SHEARED. PUMP WAS REMOVED AND A NEW PUMP INSTALLED. OPERATIONAL CHECK OF THE SYSTEM CHECKE D NORMAL. PART SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O RT A49CE 1E4 2002073000124 20020730 00124 2002 7 30 VJ32002F00057 4 20020719 A 3451 SWITCH ALIDSG GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA DME FAILED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 862AF 294 85002 L2802448A DURING INSPECTION OF A DME FAILURE. FOUND WIRE TO SWITCH BROKEN FROM PIN 1. BELIEVE THIS IS BECAUSE OF THE ANGLE THAT THE WIRE IS ROUTED BEHIND THE INSTRUMENT PANEL. SUGGEST MAKING THIS WIRE AN INCH LONGER OR RE-ROUTE TO RELIEF STRESS ON WIRES. 1 L 7 1 3O 3 O RT A49CE 1E4 2002073000125 20020730 00125 EA 2002 7 30 SWIA200210894 1 20020530 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 906SW 2933 2933 7510 FLAPS FAIL CAUTION MESSAGE APPEARED WHILE CLIMBING THROUGH 10,000 FEET. FLAPS IN ZERO POSITION. DIVERTED TO FAT WHILE EN ROUTE TO OAK. REPLACED LEFT BPSU IAW CRJ MM 27-51-10 AND COMPLETED AD FORM 98-20-01-02. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002073000126 20020730 00126 EA 2002 7 30 SWIA200210896 1 20020602 A 2613 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MALFUNCTIONED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 592SW 7279 RECEIVED BLEED AIR DUCT AURAL WARNING AND RED LEFT 14TH DUCT LEAK WARNING MESSAGE IN FLIGHT. COMPLETED MEMORY ITEMS AND QRH PROCEDURES. SHUTDOWN LEFT ENGINE. REPLACED LEFT 14TH PYLON LOOP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002073000127 20020730 00127 NE 2002 7 30 SWIA200210897 2 20020603 A 7321 EEC EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 561SW 120335 ON CLIMBOUT, THE RIGHT ENGINE STARTED TO SURGE WITH THE EEC ON AND OFF. RETURNED TO SAN. INSPECTED RIGHT ENGINE EEC & HMU FOR CONDITION. RAN LEFT AND RIGHT ENGINES THROUGH VARIOUS CONFIGURATIONS, WITH THE RIGHT ENGINE EEC ON THE ENGINE S URGES. INSPECTED EEC CANNON PLUG, CLEANED AND DID AN OHM CHECK. NO DEFECTS NOTED. OPERATIONAL CHECK GOOD IAW EMB 73-2 2-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2002073000128 20020730 00128 NM 2002 7 30 2002UALA01119 1 20020702 A 2841 2120621U1 INDICATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 392UA 24667 AIRCRAFT RETURNED TO FIELD DUE TO SUSPECTED CENTER TANK FUEL LEAK. SUPPLEMENTAL DATA UPDATE MAINTENANCE CHECKED CENTER TANK FUEL QUANTITY CALIBRATION PER MAINTENANCE MANUAL AND FOUND CALIBRATION WITHIN THE MAINTENANCE MANUAL LIMITS. REPLA CED CENTER TANK INDICATOR DUE TO DIM INDICATOR READOUT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002073000138 20020730 00138 EA 2002 7 30 CA020726002 1 20020615 A 2910 LINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE HYD SYSTEM PUNCTURED W O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CA (CAN) IN FLIGHT, LOST NUMBER ONE HYDRAULIC PRESSUE AND QUANTITY. FOUND NUMBER ONE PUMP PRESSURE LINE PUNCTURED. LINE R EPLACED AND PUMP MPN 887055,OPERATION CHECKED NORMAL 2 L 7 2 4F 4 F RT A21EA E15NE 2002073000139 20020730 00139 EA 2002 7 30 SWIA200211069 1 20020717 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA FLAP CANNON PLUG SHORTED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 445SW 7651 AT ROTATION, WINDSHEAR FAIL STATUS MESSAGE AND STICK SHAKER ACTUATION UP TO 180 KNTS. RETURNED FOR LANDING AT SLC. FOUND WIRE CG51C22 SHORTING AT FLAP POSITION TRANSMITTER CANNON PLUG P1CF. REMOVED DAMAGED WIRE LENGTH AND REPLACED SOC KETS ON ALL WIRES TO CONNECTORS. FLAP OPERATIONS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002073000140 20020730 00140 EA 2002 7 30 SWIA200211071 1 20020720 A 2720 JACKSCREW CNDAIR CL600 CL6002B19 1900309 EA RUDDER PEDAL ADJ BROKEN A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 403SW 7028 CAPTAIN'S RUDDER PEDALS WILL NOT ADJUST BACK. REMOVED AND REPLACED BROKEN JACKSCREW ON CAPTAIN'S SIDE PEDAL ADJUST MECH ANISM IAW CRJ MM 27-21-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002073000141 20020730 00141 WP 2002 7 30 MWEA020466 1 20020730 A 5230 591014119 DOUBLER DOUG DC9 DC914 3022034 WP FWD CARGO DR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO DOOR #2 OUTBOARD UPPER ATTACH HOLE IS CRACKED. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002073000142 20020730 00142 WP 2002 7 30 MWEA020467 1 20020730 A 5230 995766419 ANGLE DOUG DC9 DC914 3022034 WP FWD CARGO DR OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO DOOR ANGLE HAS OVERSIZED HOLES. -- REMOVED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2002073000143 20020730 00143 WP 2002 7 30 MWEA020469 1 20020730 A 5313 59114081 FINGER DOUBLER DOUG DC9 DC914 3022034 WP STATION 525 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 SKIN CRACKED INDICATION NOTED STATION 525 JUST RIGHT OF LONGERON ONE (MARKED). -- FABRICATED AND INSTALLED SKIN PLUG A ND FINGER DOUBLER. 2 L 7 2 4F A6WE 2002073000144 20020730 00144 WP 2002 7 30 MWEA020470 1 20020730 A 5311 59100821 DOUBLER DOUG DC9 DC914 3022034 WP AFT SIDE DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 PER PCI 9274 FOUND SMALL SKIN CRACK INTO DOOR STOP ADJUST HOLE ON AFT SIDE OF DOOR 3RD HOLE FROM THE TOP (MARKED). -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002073000145 20020730 00145 WP 2002 7 30 CALA0200432 1 20020729 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FS 1117-1136 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1117-1136, L21L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2002073000146 20020730 00146 WP 2002 7 30 MWEA020464 1 20020730 A 5230 995766433 ANGLE DOUG DC9 DC914 3022034 WP CARGO DOOR OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO DOOR ANGLE HAS OVERSIZED HOLES. -- REMOVED AND REPLACED ANGLE. 2 L 7 2 4F A6WE 2002073000147 20020730 00147 WP 2002 7 30 MWEA020465 1 20020730 A 5230 3926046505 FITTING DOUG DC9 DC914 3022034 WP CARGO DOOR OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FORWARD CARGO DOOR FITTINGS HAS OVERSIZED HOLES. -- REMOVED AND INSTALLED FITTINGS. 2 L 7 2 4F A6WE 2002073000148 20020730 00148 WP 2002 7 30 MWEA020468 1 20020730 A 5313 59114061 FASTENER DOUG DC9 DC914 3022034 WP STATION 180 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 SKIN CRACK INDICATION NOTED STATION 180 JUST RIGHT OF LONGERON ONE. -- REMOVED AND INSTALLED FASTENERS INTO FORMERS. 2 L 7 2 4F A6WE 2002073000149 20020730 00149 NM 2002 7 30 02209409A 1 20020728 A 3350 3214302 BATTERY PACK DORNER DO32 DO328300 NM A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 409FJ 3161 During preflight inspection, the crew reported that the emergency floor track lights at seat rows 2 and 3 were dim. Mai ntenance personnel removed and replaced the emergency exit lighting battery pack. An operational check was satisfactory and the aircraft was returned to service. 2 H 7 2 4T RT A55NM 2002073000150 20020730 00150 EA 2002 7 30 02209662 1 20020728 A 3350 364191 LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 662BR 7526 During preflight inspection, the crew reported that the emergency floor track lights at seat rows 2 and 3 were dim. Mai ntenance personnel initially deferred this item per CRJ MEL 33-51-10-5. Later the flexible lamp was removed and replace d, an operational check was satisfactory, the MEL deferral was cleared and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002073000151 20020730 00151 SO 2002 7 30 SWIA200210898 1 20020530 A 2422 PC2511C INVERTER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NR 1 FAILED A SWIA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 NM 07 199SW 6199 120237 INVERTER NR 1 WENT INOP EN ROUTE AND WOULD NOT RESET. RETURNED TO DEN. REMOVED AND REPLACED NR 1 INVERTER. OPS CHECK GOOD. INSTALLED SERVICEABLE INVERTER IAW MM 24-20-01. OPS CHECK GOOD. FURTHER INVESTIGATION IN PROGRESS. 2 L 7 2 4T 4 T RT A31SO E20NE 2002073000152 20020730 00152 SO 2002 7 30 SWIA200210899 1 20020519 A 2710 BEARING EMB 120 EMB120ER 3260203 SO LT AILERON RATCHETING A SWIA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 NM 07 581SW 120349 LEFT AILERON RATCHETS WHEN MOVED FULL UP AND DOWN. REPLACED LEFT AILERON WING QUADRANT BEARING, VERTICAL SWIVEL JOINT A ND ACTUATING ARM WITH SERVICEABLE UNITS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073000153 20020730 00153 SO 2002 7 30 SWIA200210900 1 20020508 A 5753 ROLLER EMB 120 EMB120ER 3260203 SO T/E FLAP CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 237SW 120314 LEFT OUTBOARD FLAP OUTBOARD ROLLER HAS CORROSION PITTING. REMOVED AND REPLACED OUTBOARD FLAP ROLLER IAW MM 27-50-12. 2 L 7 2 4T RT A31SO 2002073000154 20020730 00154 SO 2002 7 30 SWIA200210901 1 20020508 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 237SW 120314 LEFT SIDE AFT SECTION OF SEAT RAIL NEEDS TO BE REPLACED DUE TO CORROSION. REMOVED AND REPLACED SEAT RAIL IAW MM 53-01-0 5. 2 L 7 2 4T RT A31SO 2002073000155 20020730 00155 EA 2002 7 30 SWIA200210902 1 20020603 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN BROKEN A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 499SW 7398 FORWARD RED FLOOR EMERGENCY LIGHTS INOP. REPLACED WIRE AS NEEDED FOR FORWARD EMERGENCY LIGHTS. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002073000156 20020730 00156 2002 7 30 SWIA200210903 4 20020528 A 3418 C818061 COMPUTER EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 297SW 5747 5747 120327 STICK SHAKER CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED NR 1 STALL WARNING COMPUTER SYSTEM. OPS CHECK GOO D. 2 L 7 2 4T RT A31SO 2002073000157 20020730 00157 SO 2002 7 30 SWIA200210904 1 20020605 A 2752 CONNECTOR EMB 120 EMB120ER 3260203 SO FLAP ACTUATOR DIRTY A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 232SW 120306 RECEIVED FLAP CONTROL FAULT ON TAXI WHEN FLAPS 15 IS SELECTED. COMPLIED WITH QRH PROCEDURES AND PROBLEMS STILL EXISTED. CLEANED CANNON PLUG ON OUTBOARD FLAP ACTUATOR. POWERED DOWN SYSTEM. REMOVED FCU. CHECKED CONNECTIONS, REINSTALLED F CU. OPERATED FLAP SYSTEMS THROUGH ALL MODES OF OPERATIONS. NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2002073000158 20020730 00158 SO 2002 7 30 SWIA200210905 1 20020607 A 2750 FLAP EMB 120 EMB120ER 3260203 SO WING MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 214SW 120280 FLAP DISAGREEMENT IN FLIGHT. RETURNED TO SLC. PERFORMED OPS CHECKS IAW 27-50-00. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4T RT A31SO 2002073000159 20020730 00159 SO 2002 7 30 SWIA200210906 1 20020601 A 7722 INDICATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE COCKPIT ERRATIC A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 214SW 120280 LEFT ENGINE T6 GAUGE ERRATIC. RETURNED TO DEN. REPLACED LEFT T6 GAUGE. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002073000160 20020730 00160 EU 2002 7 30 02210308 1 20020729 A 3350 DM21 CONNECTOR BAG JETSTM JETSTM4112 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 308UE 41023 During preflight inspection, the crew reported that the rear section of emergency floor track lighting was inoperative. Maintenance personnel secured a loose connector for the emergency floor track lights. An operational check was satisfa ctory and the aircraft was returned to service. 1 L 7 2 4T RT A196 2002073000161 20020730 00161 2002 7 30 SWAA021668 4 20020726 A 2565 6556685 BRACKET BOEING 737 7372H4 138448C NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE SUPPORT BRACKET PER MM. 2 L 7 2 4F A16WE 2002073000162 20020730 00162 NM 2002 7 30 SWAA021671 1 20020725 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 772SW 27880 DURING SCHEDULED 1/2D CHECK, FOUND EEPLS COVER MISSING AT OVERWING EXIT. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002073000163 20020730 00163 NM 2002 7 30 SWAA021680 1 20020726 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 794SW 30605 DURING SCHEDULED C1 CHECK, FOUND EEPLS LENS MISSING AT ROW NR 1. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002073000164 20020730 00164 2002 7 30 SWAA021682 4 20020728 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM AFT ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002073000165 20020730 00165 2002 7 30 SWAA021686 4 20020727 A 2565 6556685 BRACKET BOEING 737 7373H4 1384600 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED BC1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2002073000166 20020730 00166 NM 2002 7 30 SWAA021687 1 20020728 A 5311 6546569 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 967, BL O. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002073000167 20020730 00167 NM 2002 7 30 SWAA021688 1 20020727 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002073000168 20020730 00168 NM 2002 7 30 SWAA021689 1 20020727 A 5520 65C26384 TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 602SW 27953 DURING SCHEDULED SERVICE CHECK, FOUND LT ELEVATOR TAB DELAMINATED ON UPPER SKIN AT NR 1 HINGE CUT OUT. REMOVED AND REPL ACED LT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002073000169 20020730 00169 NM 2002 7 30 SWAA021690 1 20020727 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 095SW 23054 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 727B, ABOVE STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002073000170 20020730 00170 NM 2002 7 30 SWAA021691 1 20020728 A 5520 183A8100 TAB BOEING 737 7377H4 1384404 NM BOTH ELEVATORS VIBRATION A SWAA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 29 743SW 29279 DURING CRUISE NOTICED A VERY HIGH FREQUENCY VIBRATION, COULD BE FELT IN ALL CONTROLS AS WELL AS ALL SURFACES IN COCKPIT. REMOVED AND REPLACED BOTH ELEVATOR TRIM TABS PER MM. 2 L 7 2 4F RT A16WE 2002073000171 20020730 00171 NM 2002 7 30 SWAA021692 1 20020726 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 DURING SCHEDULED C3 CHECK, FOUND RT ELEVATOR TAB NR 4 HINGE WORN. REMOVED AND REPLACED NR 4 HINGE HARDWARE AND BUSHING PER MM. 2 L 7 2 4F RT A16WE 2002073000172 20020730 00172 2002 7 30 SWAA021659 4 20020725 A 2565 1061323478 SLIDE BOEING 737 7373A4 1384585 NM FWD ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 FWD ENTRY DOOR EMERGENCY EVAC SLIDE DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002073000173 20020730 00173 2002 7 30 SWAA021663 4 20020724 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002073000174 20020730 00174 NM 2002 7 30 SWAA021665 1 20020725 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002073000175 20020730 00175 NM 2002 7 30 SWAA021666 1 20020725 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, BETWEEN STR 20L AND 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002073000176 20020730 00176 NM 2002 7 30 SWAA021667 1 20020724 A 2710 BACB10A691 BEARING BOEING 737 7372T4 1384492 NM RT MLG W/W WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED C4 CHECK, FOUND EXCESSIVE MOVEMENT AT RT OTBD AILERON QUADRANT PIVOT. REMOVED AND REPLACED AILERON QUA DRANT BEARINGS PER MM. 2 L 7 2 4F A16WE 2002073000177 20020730 00177 NM 2002 7 30 SWAA021651 1 20020724 A 5312 6547978 WEB BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 340, WL 208 AND LBL 55. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2002073000178 20020730 00178 NM 2002 7 30 SWAA021652 1 20020724 A 5315 BAC1509 FLOORBEAM BOEING 737 7373K2 13844BA NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 774, LBL 3. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002073000179 20020730 00179 NM 2002 7 30 SWAA021653 1 20020724 A 5313 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE'S CRACKED (2 EA) AT BS 908, STR 4R AND STR 4L. REPAIRED SPLICE'S PE R SRM. 2 L 7 2 4F RT A16WE 2002073000180 20020730 00180 NM 2002 7 30 SWAA021654 1 20020724 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002073000181 20020730 00181 NM 2002 7 30 SWAA021655 1 20020724 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 732SW 27864 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB HINGE ATTACH POINTS NR 2, NR 3 AND NR 4 WORN. RE MOVED AND REPLACED HARDWARE AND BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002073000182 20020730 00182 NM 2002 7 30 SWAA021656 1 20020724 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 732SW 27864 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB HINGE ATTACH POINTS NR 2 AND NR 4 WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002073000183 20020730 00183 NM 2002 7 30 SWAA021657 1 20020724 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 761RR 27875 DURING SCHEDULED C4 CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB HINGE ATTACH POINTS NR 2, NR 3 AND NR 4 WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002073000184 20020730 00184 NM 2002 7 30 SWAA021658 1 20020724 A 2731 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 761RR 27875 DURING SCHEDULED C4 CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB HINGE POINT NR 2 WORN. REMOVED AND REPLACED HARDWARE AND BUSHING PER MM. 2 L 7 2 4F RT A16WE 2002073000185 20020730 00185 NM 2002 7 30 ZW0A0207901 1 20020729 A 3260 361424 INDICATOR BOEING 757 7572Q8 1384972 NM A ZW0A O OTHER O OTHER IN INSP/MAINT 1 CE 13 707TW 27625 LT MLG POSITION INDICATOR LOOSE IN SOCKET AND WILL NOT STAY LATCHED IN. R & R LT MLG POS IND 26-1424. OPS CK POS IND OK. LAST CHECK C PERFORMED LAX 8/3/01. --CLOSED-- 2 L 7 2 4F RT A2NM 2002073000186 20020730 00186 EA 2002 7 30 COMA0260452 1 20020726 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 936CA 7043 FUSE SKIN @ F.S. 409.96 @ STRINGERS 24R & 25R HAS A 2"X3"X.100" DENT.CUT OUT DAMAGED SECTION OF SKIN PERFOMRED EDDY CURR ENT INSP TO ENSURE STRUCTURAL INTEGRITY. FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER FROM 2024 T3-.063" P/O 22808 I/A/W CRJ SRM 53-00-31 REPAIR #1 FIG 204 SHEET 3. REAPPLIED PROTECTIVE FINISH AND PERFORMED PRESSURE/LEAK CHECK. 2 L 7 2 4F RT A21EA 2002073000187 20020730 00187 EA 2002 7 30 COMA0260453 1 20020728 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 936CA 7043 L/H WING, LOWER SKIN FUEL PANEL LANDING @ WS95.950 HAS CORROSION .008" DEEP.REMOVED CORROSION BY BLENDING. PERFORMED EDD Y CURRENT INSP TO ENSURE COMPLETE DAMAGE REMOVAL. FLAP PEENED REWORKED AREAS, AND REAPPLIED PROTECTIVE FINISH. ALL WORK WAS PERFORMED I/A/W BOMBARDIER INC REO 601R-57-21-030 REV A. 2 L 7 2 4F RT A21EA 2002073000188 20020730 00188 EA 2002 7 30 COMA0260454 1 20020727 A 5300 6013501217 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS 621 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 936CA 18932 7043 THERE WAS A CRACKED INTERCOSTAL ANGLE AT STR 12L BETWEEN FS621 AND FS625.3.REMOVED THE CRACKED ANGLE. FABRICATED PER SAM PLE (FROM S6144-4 PERFORMED ANGLE) A REPAIR ANGLE AND INSTALLED THE REPAIR ANGLE I/A/W WVAC EO 601R-53-3390. 2 L 7 2 4F RT A21EA 2002073000189 20020730 00189 EA 2002 7 30 COMA0260455 1 20020723 A 2750 853D10018 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA R/H #3 BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 868CA 38 38 7427 FLIGHT 5037 FLAPS FAIL CAUTION MESSAGE.REPLACED THE R/H #3 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2002073000190 20020730 00190 EA 2002 7 30 COMA0260456 1 20020724 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 821CA 7420 FLIGHT 5160 FLAPS FAILED AT 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002073000191 20020730 00191 EA 2002 7 30 COMA0260457 1 20020725 A 3230 172825 TARGET CNDAIR CL600 CL6002B19 1900309 EA R/H MLG LOOSE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 981CA 7163 FLIGHT 5771 GEAR DISAGREE MESSAGE - R/H MLG INDICATED UNSAFE.FOUND R/H MLG UPLOCK SENSOR TARGET LOOSE - TIGHTENED TARGET . 2 L 7 2 4F RT A21EA 2002073000192 20020730 00192 EA 2002 7 30 COMA0260458 1 20020727 A 3350 364911 LAMP CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 979CA 7159 FLIGHT 5089 1ST SECTION OF EMERGENCY FLOOR LIGHTING IS INOP.REPLACED 1ST SECTION OF FLEXIBLE LAMP. 2 L 7 2 4F RT A21EA 2002073000193 20020730 00193 2002 7 30 GLBA2002109 4 20020726 A 2300 BW9001B SWITCH BEECH 1900 1900D 1154162 CE STUCK A GLBA D RETURN TO BLOCK S AFFECT SYSTEMS CL CLIMB 1 NM 03 211GL UE211 #1 COMM FAILED, REPLACED PTT SWITCH OPS CHECKED SATISFACTORY 2 L 7 2 4T RT A24CE 2002073000194 20020730 00194 SO 2002 7 30 C2XA02BT037 1 20020727 A 3350 375911 SIGN EMB 145 EMB145LR 3260212 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 13903 145479 BTV---CO3387, DURING SERVICE CHECK MAINTENANCE FOUND OVERWING EMERGENCY EXIT LOCATING LIGHT INOPERATIVE.....REMOVED AND REPLACED EMERGENCY EXIT LOCATING SIGN ASSEMBLY IAW EMB145 AMM #33-50-15. OPS.CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2002073000195 20020730 00195 SO 2002 7 30 C2XA02BT038 1 20020727 A 3230 745501 LEVER EMB 145 EMB145 3260210 SO COCKPIT DEFECTIVE A C2XA A UNSCHED LANDING S AFFECT SYSTEMS TO TAKEOFF 1 SW 27 27962 145110 EWR---CO3869, CREW REPORTED, "AFTER T/O. LDG SELECTED UP. NOSE GEAR FAILED TO RETRACT. CYCLED GEAR AND MAIN GEAR FAILED TO RETRACT. CYCLED GEAR A SECOND TIME AND ALL GEAR FAILED TO RETRACT. AIRCRAFT AIR RETURNED TO EWR AND LANDED UNEVENTFUL LY.....MAINTENANCE TROUBLESHOT SYSTEM AND REMOVED AND REPLACED LANDING GEAR LEVER CONTROL IAW EMB145 AMM REFERENCE #32-3 2-02. OPS.CHECKED GOOD IAW EMB145 AMM #32-32-00 ALSO, REFERENCE M-602 #513174. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002073000196 20020730 00196 EA 2002 7 30 SWIA200211076 1 20020719 A 2910 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA #2 SYSTEM A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J M FLUID LOSS WARNING INDICATION OVER TEMP CR CRUISE 1 NM 07 430SW 7523 DURING CRUISE, HYDRAULIC PUMP #2 PRESSURE DROPPED TO 1800 PSI AND TEMPERATURE ROSE TO 95 DEGREES C. ACCOMPLISHED BOTH Q RH'S, THEN HYDRAULIC QUANTITY DROPPED TO ZERO. ACCOMPLISHED QRH PROCEDURE. PUMP RAN FOR 49 MINS AT ZERO PRESSURE. RE TURNED TO SLC. REMOVED AND REPLACED #2 SYSTEM HYDRAULIC LINE PN 601-75238-43 AS REQUIRED. REMOVED AND REPLACED #2 EN GINE HYDRAULIC PUMP IAW 29-13-00. OPS AND LEAK CHECKS GOOD. PN ON 887055 SN OFF MX547123. 2 L 7 2 4F RT A21EA 2002080500129 20020805 00129 NE 2002 8 5 GLBA2002094 2 20020627 A 7310 3038454 FILTER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE RESTRICTED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 96ZK 120096 LEFT FUEL FILTER ANNUNCIATOR ILLUMINATED AT 25 - 30 PERCENT TQ. REPLACED HIGH AND LOW PRESSURE FUEL FILTERS OPS CHECKED SATISFACTORY 2 L 7 2 4T 4 T RT A31SO E20NE 2002080700050 20020807 00050 SO 2002 8 7 GLBA2002104 1 20020709 A 3230 12038594501 CONTROL BOX EMB 120 EMB120ER 3260203 SO LANDING GEAR INTERMITTENT A GLBA O OTHER O OTHER AP APPROACH 1 NM 03 96ZK 800 120096 LANDING GEAR WOULD NOT EXTEND ON FIRST TRY. REPLACED CONTROL BOX OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A31SO 2002073000197 20020730 00197 NM 2002 7 30 AWXA200200681 1 20020708 A 5313 654988630 STRINGER BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 0 0 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK HFEC CONFIRMED 1/2" CRACK FROM THE FORWARD EDGE OF STRINGER 16 R/H TO AN UNDETERM INED POINT BENEATH A FASTENER AND WASHER, BS 500C+14. MAINTENANCE CUTOUT CRACKED AREA OF STRINGER 16 R/H, BS 500C+14, FA BRICATED A SPLICE REPAIR, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2002080700052 20020807 00052 SO 2002 8 7 GLBA2002107 1 20020713 A 2750 3075001017 CONTROL UNIT EMB 120 EMB120ER 3260203 SO T/E FLAP INOPERATIVE A GLBA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 03 96ZK 8332 120096 FLAP DISAGREEMENT. REPLACED FLAP CONTROL UNIT OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A31SO 2002073100001 20020731 00001 SO 2002 7 31 SWIA200210918 1 20020608 A 7722 SELOC19EG INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT ERRATIC A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 568SW 1130 6 120343 LEFT ENGINE HAD ERRATIC T6 ANALOG NEEDLE READINGS AND HIGH DIGITAL INDICATION (1200 DEGREES C) WITH ASSOCIATED T6 WARNIN G. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE T6 GAUGE. RAN LEFT ENGINE. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002073100002 20020731 00002 SO 2002 7 31 SWIA200210919 1 20020609 A 3060 LEAD EMB 120 EMB120ER 3260203 SO RT PROPELLER DEFECTIVE A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 583SW 120351 RIGHT PROPELLER DEICE FAILED IN FLIGHT ON TIMERS 1 AND 2. RETURNED TO SLC. REMOVED AND REPLACED FULL SET OF DEICE LEAD S ON RIGHT PROP IAW MM 30-60-00. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002073100003 20020731 00003 EA 2002 7 31 SWIA200210920 1 20020608 A 2760 54C54677E01 MANIFOLD CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION UK UNKNOWN 1 NM 07 406SW 6894 6894 7030 OUTBOARD GROUND SPOILER MESSAGE ON EICAS. REMOVED AND REPLACED GROUND SPOILER MANIFOLD ASSEMBLY IAW MM 27-63-05. OPS C HECKS GOOD. 2 L 7 2 4F RT A21EA 2002073100004 20020731 00004 SO 2002 7 31 SWIA200210921 1 20020611 A 5230 BRACKET EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CARGO DOOR CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 251YV 120251 FORWARD CARGO DOOR TRACK SUPPORT BRACKET ON FRAME 40 CRACKED. INSTALLED A NEW BRACKET IAW EMBRAER DER APPROVAL GST 1880 /02. 2 L 7 2 4T 4 T RT A31SO E20NE 2002073100005 20020731 00005 SO 2002 7 31 SWIA200210922 1 20020509 A 5260 ACTUATOR EMB 120 EMB120ER 3260203 SO PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 PASSENGER DOOR STEP ACTUATOR ARM FOUND CORRODED. REMOVED AND REPLACED PASSENGER DOOR STEP ACTUATOR ARM WITH NEW. OPS C HECK GOOD. 2 L 7 2 4T RT A31SO 2002073100006 20020731 00006 SO 2002 7 31 SWIA200210923 1 20020509 A 5260 TORQUE TUBE EMB 120 EMB120ER 3260203 SO PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 NR 2 AND NR 3 PASSENGER DOOR STEP RODS FOUND CORRODED DURING INSPECTION. REMOVED AND REPLACED NR 2 AND NR 3 PASSENGER D OOR STEP TORQUE TUBES IAW EMB MM 52-10-03. 2 L 7 2 4T RT A31SO 2002073100007 20020731 00007 SO 2002 7 31 SWIA200210924 1 20020509 A 2497 WIRE EMB 120 EMB120ER 3260203 SO ELECTRICAL SYS BURNED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 WIRE AT CANNON PLUG J0958 PIN F ON RIGHT SIDE DC RELAY BOX IS BURNED AND NEEDS TO BE REPLACED. REMOVED AND REPLACED WIR E W208-0064 AT CANNON PLUG J0958 PIN F WITH A NEW WIRE 1 GAUGE LARGER AND PERFORMED OPERATIONAL CHECK AS PER MM 30-40-00 . OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073100008 20020731 00008 SO 2002 7 31 SWIA200210925 1 20020509 A 5210 12026533003 LINK EMB 120 EMB120ER 3260203 SO PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 PASSENGER DOOR PUSH-PULL LINKS CORRODED (FORWARD AND AFT). REMOVED AND REPLACED PASSENGER DOOR FORWARD AND AFT PUSH-PUL L LINKS IAW EMB MM 52-11-03. 2 L 7 2 4T RT A31SO 2002073100009 20020731 00009 EA 2002 7 31 SWIA200210926 1 20020608 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 588SW 7069 EMERGENCY EXIT PLACARD NEAR FORWARD PASSENGER DOOR IS INOP. REMOVED AND REPLACED THE LIGHTED PLACARD. 2 L 7 2 4F RT A21EA 2002073100010 20020731 00010 SO 2002 7 31 SWIA200210928 1 20020607 A 2750 3472001001 COMPUTER EMB 120 EMB120ER 3260203 SO T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 579SW 5785 5785 120347 ON CLIMBOUT, RECEIVED FLAP AND DISAGREEMENT CAUTION LIGHTS, OUTBOARD PAIR. QRH PROCEDURE CORRECTED FAULT. REMOVED AND REPLACED THE FLAP CONTROL COMPUTER. OPERATED THE FLAPS. NO FURTHER PROBLEM NOTED AT THIS TIME. 2 L 7 2 4T RT A31SO 2002073100011 20020731 00011 EA 2002 7 31 SWIA200210929 1 20020613 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 589SW 7072 LEFT EMERGENCY EXIT WARNING COMES ON INTERMITTENTLY INFLIGHT. CABIN PRESSURE REMAINS NORMAL. CLEANED DOOR SEAL, PROXIM ITY SENSOR, AND STRIKER PLATE OF DIRT AND MOISTURE. REINSTALLED DOOR. OPS CHECK OF EICAS DOOR PAGE INDICATIONS CHECK G OOD. DOOR FIT CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002073100012 20020731 00012 SO 2002 7 31 SWIA200210930 1 20020610 A 3320 BALLAST EMB 120 EMB120ER 3260203 SO LAVATORY SHORTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 567SW 120347 ELECTRICAL FUMES/BURNING SMELL IN AIRCRAFT. FOUND LIGHT BALLAST SHORTED. COULD NOT DUPLICATE BURNING SMELL. INSPECTED GALLEY BALLAST FOR EVIDENCE OF BURNING. NO BURN DETECTED. REMOVED AND REPLACED LAV LIGHT BALLAST FOR POSSIBLE CAUSE O F BEING BAD IAW MM 33-22-00. OPS CHECK GOOD. NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2002073100013 20020731 00013 EA 2002 7 31 SWIA200210931 1 20020609 A 2742 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 412SW 7101 STAB TRIM CH2 WILL NOT ENGAGE. REPLACED HORIZONTAL STAB ACTUATOR IAW 27-42-01 AND REPLACED HORIZONTAL STAB MOTOR CONTRO L UNIT IAW 27-42-05. OPS CHECK GOOD IAW MM. OK FOR CAT II OPERATIONS. 2 L 7 2 4F RT A21EA 2002073100014 20020731 00014 EA 2002 7 31 SWIA200210932 1 20020613 A 3320 LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR INOPERATIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 407SW 7034 PASSENGER DOOR BOARDING LIGHT IS INOP. REMOVED AND REPLACED TOP PASSENGER DOOR STEP LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002073100015 20020731 00015 SO 2002 7 31 SWIA200210933 1 20020523 A 5411 FRAME EMB 120 EMB120ER 3260203 SO NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 198SW 120227 FRAME CRACKED THROUGH ON FORWARD SIDE OF HYDRAULIC BAY BULKHEAD TOWARD OUTBOARD END AT FIREWALL. FABRICATED AND INSTALL ED FRONT AND BACK SIDE DOUBLERS IAW SRM 54-20-04, 51-70-06, AND 51-40-02. 2 L 7 2 4T RT A31SO 2002073100016 20020731 00016 SO 2002 7 31 SWIA200210934 1 20020523 A 5280 DOOR FRAME EMB 120 EMB120ER 3260203 SO RT MLG DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 198SW 120227 ONE INCH LONG CRACK IN TOP GEAR DOOR FRAME ABOVE TENSIONER ARM BRACKET, RIGHT GEAR OUTBOARD. REMOVED DAMAGE. FABRICAT ED AND INSTALLED REPAIR DOUBLER AND FILLER IAW EMB SRM 51-70-05 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002073100017 20020731 00017 SO 2002 7 31 SWIA200210935 1 20020523 A 5420 INTERCOSTAL EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 198SW 120227 CRACK IN INTERCOSTAL RIGHT GEAR WELL, OUTBOARD SIDE, AT MID STRINGER AFT END. FABRICATED AND INSTALLED A DOUBLER IAW SR M 51-40-02 AND 51-00-00. 2 L 7 2 4T RT A31SO 2002073100018 20020731 00018 SO 2002 7 31 SWIA200210936 1 20020523 A 5420 BRACKET EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 198SW 120227 LEFT HYDRAULIC PACK MOUNTING BRACKET INBOARD SIDE IS CRACKED ON THE INSIDE OF THE BRACKET. REMOVED AND REPLACED THE LEF T HYDRAULIC PACK MOUNTING BRACKET IAW EMB SRM 51-00-00 & 51-40-02. 2 L 7 2 4T RT A31SO 2002073100019 20020731 00019 NM 2002 7 31 SABA020077 1 20020729 A 3350 1305 LIGHT DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 883CC 168 AIRCRAFT 883 ON FLIGHT 5014 FROM CLT TO AGS, AIRCREW REPORTED A EMERGENCY LIGHT WOULD NOT TEST AT ROW THREE. MAINTENANCE REMOVED AND REPLACED BULB AND SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002073100020 20020731 00020 EA 2002 7 31 SWIA200210938 1 20020602 A 4920 38004883 CASE CNDAIR CL600 CL6002B19 1900309 EA APU CRACKED A SWIA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 NM 07 426SW 4144 4144 7468 APU AUTO SHUTDOWN ON GROUND. OIL OBSERVED UNDER THE TAIL. REPLACED APU WITH SERVICEABLE UNIT DUE TO CRACKED CASE. NEW APU ASSEMBLY OPS AND LEAK CHECKS NORMAL. INSTALLED IAW CRJ MM 49-10-00. 2 L 7 2 4F RT A21EA 2002073100021 20020731 00021 NE 2002 7 31 SWIA200210939 2 20020618 A 7310 FUEL LINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE CRACKED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CL CLIMB 1 NM 07 217SW 120286 AFTER TAKEOFF FUEL DISCOVERED LEAKING FROM RIGHT ENGINE. ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO THE FIELD. FOUND CRA CKED FUEL LINE AT HMU. REPLACED LINE. LEAK CHECK GOOD. REMOVED AND REPLACED HMU FUEL RETURN HOSE IAW EMB POWERPLANT B UILDUP 71-00-00. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002073100022 20020731 00022 SO 2002 7 31 SWIA200210940 1 20020602 A 2731 SENSOR EMB 120 EMB120ER 3260203 SO ELEVATOR MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 207SW 120266 TAKEOFF TRIM AURAL WARNING FAILURE. ABORTED TAKEOFF. REPLACED BOTH LEFT AND RIGHT ELEVATOR TRIM SENSORS. RAN BOTH ENG INES TO TAKEOFF POWER SETTINGS AND ALL TRIM SETTINGS IN GREEN BAND. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073100023 20020731 00023 SO 2002 7 31 SWIA200210942 1 20020608 A 5753 SKIN EMB 120 EMB120ER 3260203 SO T/E FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 217SW 120286 LEFT NACELLE FLAP CRACKED ON LOWER SIDE. REINFORCEMENT ADDED OVER AFFECTED AREA IAW EMB120 51-10-02. 2 L 7 2 4T RT A31SO 2002073100024 20020731 00024 2002 7 31 SWIA200210954 4 20020618 A 3425 COMPUTER EMB 120 EMB120ER 3260203 SO E/E BAY MALFUNCTIONED A SWIA C ABORTED TAKEOFF I FLT. ATTITUDE INST. TO TAKEOFF 1 NM 07 299SW 120329 ABORTED TAKEOFF FOR ATTITUDE DISPLAY MESSAGE. REPLACED NR 1 AHRS COMPUTER WITH SERVICEABLE UNIT AND REINITIALIZED AS RE QUIRED. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002073100025 20020731 00025 2002 7 31 SWIA200210955 4 20020618 A 2210 6229815204 CIRCUIT CARD CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS DEFECTIVE A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 587SW 7062 YAW DAMPER NR 2 INOP, WILL NOT ENGAGE IN FLIGHT. REMOVED AND REPLACED NR 2A FCC 4000 CARD. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002073100026 20020731 00026 EA 2002 7 31 SWIA200210956 1 20020617 A 2761 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 587SW 7062 UPON ENGINE NR 1 START DURING TAXI, RECEIVED A SPOILERON FAULT MESSAGE. RETURNED TO THE GATE. INSTALLED SERVICEABLE PC U ACTUATOR FOR LEFT OUTBOARD SPOILERON IAW 27-60-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002073100027 20020731 00027 2002 7 31 SWIA200210957 4 20020608 A 3418 CONNECTOR EMB 120 EMB120ER 3260203 SO STICK SHAKER LOOSE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 214SW 120280 FIRST OFFICER'S STICK SHAKER NOT WORKING ON FIRST FLIGHT OF THE DAY CHECK. FOUND CONNECTOR LOOSE ON SHAKER UNIT. TIGHT ENED CONNECTOR. OPS CHECK PER 27-60-00 GOOD. 2 L 7 2 4T RT A31SO 2002073100028 20020731 00028 SO 2002 7 31 SWIA200210958 1 20020616 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 217SW 120286 COCKPIT ENTRY RED FLOOR LEVEL EMERGENCY LIGHTING INOP. REMOVED AND REPLACED COCKPIT FLOOR LEVEL LIGHTS. OPS CHECK GOOD . 2 L 7 2 4T RT A31SO 2002073100029 20020731 00029 EA 2002 7 31 SWIA200210959 1 20020620 A 1430 SCREW CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 591SW 7079 PASSENGER STOW HANDLE MESSAGE ON EICAS. UNABLE TO CLOSE AND LATCH PASSENGER DOOR. FOUND BROKEN SCREW IN LATCHING MECHA NISM. REPLACED SCREW IAW A/C MM 51-11-02. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002073100030 20020731 00030 SO 2002 7 31 SWIA200210960 1 20020615 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 593SW 4769 120191 FLOOR LEVEL EMERGENCY LIGHTS AND EXIT LIGHT IN ROW 9 WILL NOT ILLUMINATE. REMOVED AND REPLACED AFT ELBP WITH A SERVICEA BLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073100031 20020731 00031 2002 7 31 SWIA200210961 4 20020615 A 2210 CONTROL PANEL EMB 120 EMB120RT 3260202 SO AUTOPILOT SYS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 593SW 120191 WITH AUTOPILOT SELECTED TO EITHER SIDE AND AUTOPILOT ENGAGED, RECEIVED AN AURAL TRIM FAIL WITH ASSOCIATED MAP LIGHT ON A P PANEL, RED AP & E LIGHTS ILLUMINATED. REPLACED APP-65 WITH SERVICEABLE UNIT. OPS CHECK GOOD. RERACKED APC65. BOTH SIDES TESTED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073100032 20020731 00032 EA 2002 7 31 SWIA200210962 1 20020620 A 2761 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION UK UNKNOWN 1 NM 07 597SW 7293 RECEIVED LEFT SPOILERON CAUTION MESSAGE. INSTALLED SERVICEABLE PCU ON LEFT OUTBOARD SPOILERON IAW 27-60-00. 2 L 7 2 4F RT A21EA 2002073100033 20020731 00033 2002 7 31 SWIA200210963 4 20020613 A 3425 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA NR 2 MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 407SW 7034 YAW DAMPER NR 2 FAILED DUE TO NR 2 AHRS FAILURE. INSTALLED SERVICEABLE AHRS COMPUTER AT NR 2 POSITION. AHRS OPS CHECK GOOD. YAW DAMPER NR 2 OPS CHECK GOOD. RETURNED TO CAT II SERVICE. 2 L 7 2 4F RT A21EA 2002073100034 20020731 00034 SO 2002 7 31 SWIA200210964 1 20020625 A 3610 DUCT EMB 120 EMB120RT 3260202 SO LT WING LEAKING A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 269UE 120194 AT ABOUT 50 KTS ON TAKEOFF ROLL, TRIPLE CHIME DUCT LEAK RED LIGHT ON MAP AND DUCT LEAKAGE ON LEFT SIDE OVERHEAD. ABORTE D TAKEOFF. LIGHTS REMAINED ON FOR ONLY 10-15 SECONDS, THEN WENT OUT. INSTALLED SERVICEABLE LEFT WING BLEED LINE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073100035 20020731 00035 EA 2002 7 31 SWIA200210965 1 20020611 A 2752 853D10017 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 908SW 2320 2320 7540 ON FINAL APPROACH INTO LAX, SELECTED FLAPS 20 DEGREES AND FLAPS STOPPED AT 18 DEGREES. REMOVED AND REPLACED LEFT OUTBOA RD NR 3 AND NR 4 FLAP ACTUATORS IAW CRJ MM 27-53-05. CYCLED FLAPS NUMEROUS TIMES. OPS CHECK GOOD ON GROUND. COMPLIED WITH AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2002073100036 20020731 00036 EA 2002 7 31 SWIA200210966 1 20020620 A 2742 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 403SW 3192 3192 7028 STABILIZER TRIM CHANNEL 1 POPPED THE CIRCUIT BREAKER. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW 27-41-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002073100037 20020731 00037 SO 2002 7 31 SWIA200210971 1 20020612 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 229SW 120305 PRIOR TO BRAKE RELEASE ON TAKEOFF, THE AUTOFEATHER GREEN ARMED LIGHT WAS ILLUMINATED. IMMEDIATELY AFTER BRAKE RELEASE, THE AURAL WARNING FOR AUTOFEATHER SOUNDED AND TAKEOFF WAS ABORTED. REMOVED AND REPLACED AURAL WARNING UNIT WITH SERVICE ABLE UNIT. PERFORMED ENGINE RUN-UP AT TAKEOFF POWER SETTINGS WITH AUTO FEATHER SYSTEM ARMED. ALL CHECKS GOOD, NO AUTOF EATHER AURAL WARNING. AUTO FEATHER FUNCTIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073100038 20020731 00038 EA 2002 7 31 SWIA200210972 1 20020612 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 588SW 7069 PITOT BASE HEAT MESSAGE ON DURING CLIMBOUT. QRH PROCEDURES WOULD NOT CLEAR MESSAGE. RETURNED TO SLC. POWERED DOWN AND POWERED UP. PITOT BASE HEAT MESSAGE CLEARED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002073100039 20020731 00039 2002 7 31 SWIA200210973 4 20020620 A 3160 DISPLAY CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 442SW 7609 ON DEPARTURE FROM DFW, FIRST OFFICER'S MFD WENT BLANK. RETURNED TO DFW. RERACKED RIGHT MFD. PULLED AND RESET CB P-2 K -2. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2002073100040 20020731 00040 EA 2002 7 31 SWIA200210974 1 20020622 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION UK UNKNOWN 1 NM 07 498SW 7483 SPOILERON FAULT WITH ASSOCIATED INBOARD GROUND SPOILERS FAULT. REMOVED AND REPLACED NR 2 SECU IAW 27-61-04. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002073100041 20020731 00041 EA 2002 7 31 SWIA200210975 1 20020624 A 2741 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 432SW 2121 2121 7548 STAB TRIM CHANNEL NR 2 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU IAW MM 27-41-00. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002073100042 20020731 00042 EA 2002 7 31 SWIA200210976 1 20020623 A 5210 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 PASSENGER DOOR FRAME DAMAGED FORWARD AND AFT WHERE DOOR PINS HAVE BENT AND CRACKED THE DOOR SEAL SEAT. REMOVED DAMAGED REPAIR AT STA 310.00 AND 349.00 AND FABRICATED AND INSTALLED NEW PER REO 601R-52-11-008. 2 L 7 2 4F RT A21EA 2002080200003 20020802 00003 2002 8 2 C2XA02BT032 4 20020720 A 2330 INVERTER EMB 145 EMB145LR 3260212 SO CD PLAYER FAULTY A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 22909 145459 BDL---CO4083, CREW REPORTED AFTER LANDING, FLIGHT ATTENDANT OPENED UP CD PLAYER DOOR AND SMELLED SMOKE. THE CD PLAYER W ILL NOT COME ON AND THE CIRCUIT BREAKER POPPED. AIRCRAFT RETURNED TO SERVICE. REMOVED AND REPLACED THE POWER INVERTER FOR THE CD PLAYER. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002073100043 20020731 00043 SO 2002 7 31 SWIA200210977 1 20020604 A 3232 ACTUATOR EMB 120 EMB120ER 3260203 SO RT MLG FAILED A SWIA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 07 199SW 120237 ON GEAR RETRACTION, THE RIGHT MAIN GEAR RED LIGHTS REMAINED ILLUMINATED WITH ASSOCIATED GEAR DOOR FLUTTER SOUND. RETURN ED TO PSP. GEAR EXTENDED NORMALLY. REPLACED RIGHT MLG MAIN ACTUATOR WITH SERVICEABLE UNIT PER MM 32-32-10. GEAR SWING OPS CHECKS GOOD. NO LEAKS NOTED. 2 L 7 2 4T RT A31SO 2002073100044 20020731 00044 SO 2002 7 31 SWIA200210978 1 20020624 A 3350 FUSE EMB 120 EMB120ER 3260203 SO CABIN CORRODED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 250YV 120250 THE REAR TWO THIRDS OF THE EMERGENCY FLOOR LIGHTING ILLUMINATED. EMERGENCY LIGHT IN ROW 9 ILLUMINATED. ALL EMERGENCY L IGHT SWITCHES IN NORMAL POSITION. AT TIMES, THE LIGHTS WILL EXTINGUISH THEN COME BACK ON. INSPECTED E-LIGHTS SYSTEM. FOUND FUSE X0017 TO BE CORRODED. REPLACED FUSE WITH A SERVICEABLE UNIT. ALSO REPLACED AFT ELBP WITH A SERVICEABLE UNIT . OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002073100045 20020731 00045 SO 2002 7 31 SWIA200210979 1 20020624 A 5610 WINDOW EMB 120 EMB120ER 3260203 SO LEFT LACK OF LUBE A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 563SW 120338 LEFT DIRECT VISION WINDOW IS HARD TO IMPOSSIBLE TO OPEN. LUBED WINDOW AND MADE IT EASIER TO OPEN. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073100046 20020731 00046 EA 2002 7 31 A6WA200240022 1 20020625 A 2530 3501003903 COFFEEMAKER CNDAIR CL600 CL6002B19 1900309 EA GALLEY DEFECTIVE A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 409AW 7447 EXPLOSION NEAR RIGHT COFFEE MAKER AND FILLED AREA WITH WHITE POWDER. MAINTENANCE INSPECTED COFFEE MAKER AND FOUND WATER RESERVOIR HEATING ELEMENT SHORTED AND DETACHED. MAINTENANCE REMOVED AND REPLACED COFFEE MAKER. (M) 2 L 7 2 4F RT A21EA 2002073100047 20020731 00047 NM 2002 7 31 ASAA0210150 1 20020610 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT SEAT PALLETS 9 AND 10 INOPERATIVE. REPLACED RE MOTE ASSEMBLY BATTERIES, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002073100048 20020731 00048 NM 2002 7 31 ASAA0210151 1 20020613 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT SEAT PALLET 8-9 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002073100049 20020731 00049 NM 2002 7 31 ASAA0210152 1 20020622 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT LEFT OVERWING EXIT INOPERATIVE. REPLACED REMOT E ASSEMBLY BATTERY, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002073100050 20020731 00050 NM 2002 7 31 ASAA0210153 1 20020623 A 3350 873100232 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY EXIT IDENTIFIER AT LEFT OVERWING EXIT INOPERATIVE. REPLACED LIGHT AS SEMBLY, THEN LIGHT TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002073100051 20020731 00051 NM 2002 7 31 ASAA0240068 1 20020606 A 1420 8100022608 TERMINAL BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 JNU - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROW 16 INOPERATIVE. RECONNECTED WIRE TERMINAL ENDS, OPS CHEC KED GOOD. (M) 2 L 7 2 4F RT A16WE 2002073100052 20020731 00052 NM 2002 7 31 ASAA0240073 1 20020624 A 3397 8100022601 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 776AS 25109 FAI - DURING LINE CHECK, FOUND FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE AT ROW 25, 26 AND AFT LAVATORY AREA. RECONNECTE D FLOOR TRACK WIRING, OPERATIONAL CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2002073100053 20020731 00053 NM 2002 7 31 ASAA0270007 1 20020616 A 5730 113A92102 SKIN BOEING 737 737790 13844CN NM WING FAIRING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 614AS 30343 SEA - DURING C-CHECK, THE RIGHT WING FAIRING OUTBOARD BONDING JUMPER ATTACHMENT SCREW HOLE WAS ENLARGED. REPAIRED SKIN PER EA 5750-01696. (M) 2 L 7 2 4F RT A16WE 2002073100054 20020731 00054 NM 2002 7 31 ASAA0270008 1 20020617 A 5720 113A92251 RIB BOEING 737 737790 13844CN NM WING FAIRING DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 614AS 30343 SEA - DURING C-CHECK, THE RIGHT WING FAIRING AFT RIB DAMAGE. REMOVED RIB. REPAIRED RIB PER EA 5750-01697. REPLACED RI B. (M) 2 L 7 2 4F RT A16WE 2002073100055 20020731 00055 2002 7 31 ASAA0280193 4 20020528 A 2565 3961899501 LANYARD DOUG DC9 DC982 3022082 WP EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING PREFLIGHT CHECK, R2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. ATTACHED LANYARD. (M) 2 L 7 2 4F A6WE 2002073100056 20020731 00056 2002 7 31 ASAA0280194 4 20020530 A 2565 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING PREFLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. ATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2002073100057 20020731 00057 WP 2002 7 31 ASAA0280195 1 20020529 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 15855 53063 LAX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT. OP TESTED OK. (M) 2 L 7 2 4F RT A6WE 2002073100058 20020731 00058 2002 7 31 ASAA0280196 4 20020602 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 SEA - DURING PREFLIGHT CHECK, L2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. ATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2002073100059 20020731 00059 NM 2002 7 31 ASAA0280208 1 20020615 A 3350 0105606 CONNECTOR DOUG MD80 MD83 3023681 NM CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 981AS 53472 LAS - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING IN AFT CABIN WAS FOUND TO BE INOPERATIVE. RECONNECTED LOOSE CONN ECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT 2002073100060 20020731 00060 WP 2002 7 31 ASAA0280209 1 20020615 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING IN FORWARD CABIN WAS FOUND TO BE INOPERATIVE. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002073100061 20020731 00061 WP 2002 7 31 ASAA0280210 1 20020616 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 YVR - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING IN 1ST CLASS CABIN WAS FOUND TO BE INOPERATIVE. RECONNECTED LOOS E CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002073100062 20020731 00062 WP 2002 7 31 ASAA0280211 1 20020617 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 OAK - DURING LINE CHECK, EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED POWER SUPPLY. EMERGENCY L IGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002073100063 20020731 00063 CE 2002 7 31 NSVA02011 1 20020502 A 5260 1145140309106 CONTROL CABLE BEECH 1900 1900C 1154161 CE AIRSTAIR DOOR OUT OF RIG A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 119CJ UC19 BOS - CREW REPORTED THAT THE AIRSTAIR DOOR WOULD NOT LOCK. SECURED AIRSTAIR DOOR TO LOCKED POSITION FOR FERRY FLIGHT. SFP ISSUED TO FERRY AIRCRAFT FROM BOS TO HYA. HYA MAINTENANCE RIGGED THE AIRSTAIR DOOR CABLE IAW BMM 52-10-00, OPERATIO NAL CHECK WAS SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 2002073100064 20020731 00064 CE 2002 7 31 NSVA0212 1 20020501 A 5260 1145140309106 CONTROL CABLE BEECH 1900 1900C 1154161 CE AIRSTAIR DOOR BROKEN A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 119CJ UC19 LEB - CREW REPORTED THAT THE AIRSTAIR DOOR HANDLE WOULD NOT SECURE CLOSED. FOUND BROKEN CABLE INSIDE AIRSTAIR DOOR LATC H MECHANISM. MAINTENANCE ACCOMPLISHED TEMP FIX TO SECURE DOOR. SFP ISSUED TO FERRY AIRCRAFT FROM LEB TO HYA. HYA MAIN TENANCE REPLACED AIRSTAIR DOOR CABLE, OPERATIONAL CHECK WAS SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 2002073100065 20020731 00065 SO 2002 7 31 SIMA200215701 1 20020531 A 5320 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - DURING INSPECTION, FOUND CORROSION ON PREVIOUS REPAIR AFT DIGITAL. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTA LLED NEW DOUBLER IAW EMB 145 SST-249/00 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002073100066 20020731 00066 SO 2002 7 31 SIMA200215705 1 20020602 A 5320 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - DURING INSPECTION FOUND CORROSION ON LEFT OMEGA BEAM, PREVIOUS REPAIR AT FRAME 20. REMOVED PREVIOUS REPAIR FABRIC ATED AND INSTALLED NEW DOUBLER ANGLE, FILLER, PLATE AND TWO SHIMS IAW EMB 145, SRM 145/1142, CHAPTER 53, REV 18 53-21-10 , AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002073100067 20020731 00067 NM 2002 7 31 USAA020202 1 20020606 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 23876 PIT - FOUND LEADING EDGE SKIN DAMAGED .25 INCH BY .5 INCH, L00, LE, STATION 169. WET LAY UP REPAIR PER EA 74124. (M) 2 L 7 2 4F RT A16WE 2002073100068 20020731 00068 NM 2002 7 31 USAA020203 1 20020510 A 5320 ATTACH ANGLE BOEING 767 7672B7 1385107 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651US 50498 24764 PIT - FOUND ATTACH ANGLE CRACKED 4 INCHES, STATION 1373 BETWEEN STRINGER 30R AND 29R. DEFECTIVE PART REPLACED WITH IDEN T PART PER SRM 51-10-02. (M) 2 L 7 2 4F RT A1NM 2002073100069 20020731 00069 NM 2002 7 31 USAA020204 1 20020510 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 22952 PIT - FOUND KEEL BEAM CORRODED 3 INCHES BY 1 INCH CORRODED, 13.5.546 STRINGER 28L. CORROSION LEVEL 2, TASK NR C53-212-0 1. REMOVED DAMAGED AREA, INSTALLED NEW SECTION AND INSTALLED DOUBLER PER EA 73807. (M) 2 L 7 2 4F RT A16WE 2002073100070 20020731 00070 NM 2002 7 31 USAA020205 1 20020515 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 22952 PIT - FOUND INTERCOSTAL CRACKED 1.5 INCH, JUST ABOVE AFT ENTRANCE DOOR BS 967. INSTALLED NEW ATTACH ANGLE. (M) 2 L 7 2 4F RT A16WE 2002073100071 20020731 00071 NM 2002 7 31 USAABB02090 1 20020610 A 3350 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 612AU 27124 SFO - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4, 23, 26, 29, AND 32 INOPERATIVE. MAINTENANCE REPLACED THE BATTERI ES. (M) 2 L 7 2 4F RT A2NM 2002073100072 20020731 00072 NM 2002 7 31 USAABB02093 1 20020618 A 3350 86210066 BATTERY PACK BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 PVD - EMERGENCY LIGHT AT SEAT ROW 29D INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2002073100073 20020731 00073 NM 2002 7 31 USAABB02095 1 20020619 A 3350 20131A BATTERY PACK BOEING 767 7672B7 1385107 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 PHL - FOUND THE EXTERIOR EMERGENCY LIGHT FOR THE AFT RIGHT DOOR SLIDE GROUND ILLUMINATION INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A1NM 2002073100074 20020731 00074 NM 2002 7 31 USAABB02096 1 20020619 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 BOS - FOUND A LOW LEVEL ESCAPE PATH EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY. OPERATI ONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2002073100075 20020731 00075 NM 2002 7 31 USAABB02097 1 20020619 A 3350 9221009 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 BOS - FOUND THE EMERGENCY EXIT IDENTIFIER LIGHTS AT DOORS R2, R3 AND R4 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BATTERIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2002073100076 20020731 00076 NM 2002 7 31 USAABB02098 1 20020625 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 621AU 27200 SFO - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 9, 18, 26 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002073100077 20020731 00077 NM 2002 7 31 USAABB02099 1 20020625 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 621AU 27200 SFO - FOUND EXIT IDENTIFIERS AT L4 AND R4 DOORS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002073100078 20020731 00078 NM 2002 7 31 USAABB02100 1 20020625 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 621AU 27200 SFO - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 29 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002073100079 20020731 00079 NM 2002 7 31 USAABB02101 1 20020626 A 3350 873100151REV12 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 614AU 27145 LAX - FOUND L1 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002073100080 20020731 00080 NM 2002 7 31 USAABB02103 1 20020630 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INTERMITTENT A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 615AU 27146 BOS - FLOOR LEVEL EMERGENCY LIGHT AT ROW 6 ILLUMINATES INTERMITTENTLY. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002073100081 20020731 00081 NM 2002 7 31 USAABB02104 1 20020701 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 624AU 27245 SFO - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002073100082 20020731 00082 EU 2002 7 31 USAASA02050 1 20020531 A 3350 32145510 POWER SUPPLY AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 164UW 1425 TPA - AIRCRAFT FAILED THE EMERGENCY EXIT LIGHTS TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNITS. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002073100083 20020731 00083 EU 2002 7 31 USAASA02053 1 20020606 A 3350 CONNECTOR AIRBUS A319 A319112 3930323 EU CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 706US 0946 RDU - THE EMERGENCY LIGHTS FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE RECONNECTED THE RIGHT AFT SLIDE LIGHT HARNESS CONNECTOR. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2002073100084 20020731 00084 EU 2002 7 31 USAASA02055 1 20020612 A 3350 321430 POWER SUPPLY AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 756US 1340 BOS - THE RIGHT EMERGENCY POWER SUPPLY UNIT WAS FOUND TO REQUIRE REPLACEMENT. MAINTENANCE REPLACED THE RIGHT EMERGENCY POWER SUPPLY UNIT BATTERY. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002073100085 20020731 00085 EU 2002 7 31 USAASA02059 1 20020628 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 764US 1369 DCA - THE EMERGENCY LIGHTS TEST INDICATED AN EMERGENCY POWER SUPPLY UNIT 'INT LOAD FWDL' FAULT. MAINTENANCE REPLACED TH E FORWARD EMERGENCY POWER SUPPLY UNIT. SYSTEM TESTS OK. (M) 2 L 7 2 4F RT A28NM 2002073100086 20020731 00086 EU 2002 7 31 USAASA02060 1 20020702 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 108UW 1061 DCA - AN EMERGENCY POWER SUPPLY FAULT WAS INDICATED ON THE FLIGHT ATTENDANTS PANEL. MAINTENANCE REPLACED AN EMERGENCY P OWER SUPPLY UNIT WITH BATTERIES. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002073100087 20020731 00087 NM 2002 7 31 USAASB021009 1 20020606 A 3350 20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 421US 23988 LGA - MAINTENANCE FOUND THE EMERGENCY LIGHTS FROM SEAT ROWS 6 THROUGH 9 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002073100088 20020731 00088 NM 2002 7 31 USAASB02105 1 20020603 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 532AU 24479 IAD - MAINTENANCE FOUND THE FLOOR LEVEL EMERGENCY LIGHT, AT SEAT ROW 21, INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIR E. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002073100089 20020731 00089 NM 2002 7 31 USAASB02110 1 20020607 A 3350 30043229 SOCKET BOEING 737 737401 1384701 NM EXTERIOR DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 421US 23988 TPA - MAINTENANCE FOUND THE AFT RIGHT FUSELAGE EMERGENCY EXIT ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE SOCKET/LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002073100090 20020731 00090 NM 2002 7 31 USAASB02113 1 20020609 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 24934 BOS - MAINTENANCE FOUND THE AFT OVERHEAD EMERGENCY LIGHTS DIM/WEAK. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK A T CHARGER D3580. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002073100091 20020731 00091 NM 2002 7 31 USAASB02115 1 20020616 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 394US 23316 CLT - FOUND MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 20C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER SEAT ROW 20C. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002073100092 20020731 00092 NM 2002 7 31 USAASB02116 1 20020616 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 517AU 23703 SYR - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHT ON SEAT ROW 17ABC INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIR E UNDER SEAT ROW 17ABC. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002082800038 20020828 00038 NM 2002 8 28 DHL2002752003 1 20020731 A 3230 656021132 ACCESSORY UNIT BOEING 727 727223 1384074 NM LANDING GEAR FAULTY A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 752DH 22466 ON TAKEOFF AFTER GEAR RETRACTION, LEFT MAIN GEAR UNSAFE (RED) LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE UP, ALL OTHER GEAR AND DOOR LIGHTS NORMAL. AIR TURNBACK TO MSP. REPLACED LANDING GEAR ACCESSORY IAW MM 32-09-121. GROUND FUNCTION C HECKS NORMAL, OK FOR SERVICE. 2 L 7 3 4F A3WE 2002073100093 20020731 00093 NM 2002 7 31 USAASB02119 1 20020622 A 3397 SPLICE BOEING 737 737301 1384611 NM CABIN DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 575US 23740 TPA - MAINTENANCE FOUND THE SEAT END EMERGENCY EXIT LIGHT AT THE EMERGENCY EXIT ROW INOPERATIVE. MAINTENANCE REPLACED A BAD SPLICE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002073100094 20020731 00094 NM 2002 7 31 USAASB02121 1 20020621 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 780AU 24997 PIT - MAINTENANCE FOUND THE AFT RIGHT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BATTERY PACK. OPERATIONALLY CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2002073100095 20020731 00095 NM 2002 7 31 USAASB02122 1 20020624 A 2797 WIRE BOEING 737 737401 1384701 NM L/E SLAT CHAFED A USAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 19 423US 23990 PIT - FLT 1591 - ON CLIMB-OUT FROM PHL, EN ROUTE TO ORD, CAPTAIN REPORTED THE NR 3 LEADING EDGE SLAT WAS INDICATING INTR ANSIT AND WOULD NOT RETRACT. LEFT AILERON TRIM OF 1.5 TO 2 UNITS WAS REQUIRED TO LEVEL WINGS AT 230 KNOTS. DECISION WA S MADE TO DIVERT TO PIT WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CHECKED AND F OUND WIRES IN NR 3 SLAT CONDUIT CHAFFED. REPLACED WIRES FROM ACTUATOR ROD END SWITCH TO LEADING EDGE OF WING. ALL INDI CATIONS CHECK NORMAL. CHECKED SLAT OPERATION. NO DISCREPANCIES OR BINDING FOUND. (M) 2 L 7 2 4F RT A16WE 2002073100096 20020731 00096 NM 2002 7 31 USAASB02125 1 20020626 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN PINCHED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 385US 22958 RDU - MAINTENANCE FOUND THE SIDEWALL EMERGENCY EXIT LIGHTS AT THE FORWARD FLIGHT ATTENDANT POSITION AND FORWARD GALLEY P OSITION INOPERATIVE. ALSO, FOUND THE AISLE EMERGENCY LIGHTS IN SEAT ROWS 1 THROUGH 4 INOPERATIVE. MAINTENANCE REPAIRED A PINCHED WIRE AT THE FORWARD LEFT EMERGENCY EXIT SIGN. OPERATIONAL TEST GOOD. (M) 2 L 7 2 4F RT A16WE 2002073100097 20020731 00097 NM 2002 7 31 USAASB02126 1 20020628 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 776US 24934 CLE - MAINTENANCE FOUND SEVERAL AFT CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 6 BATTE RY CHARGER ASSEMBLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002073100098 20020731 00098 NM 2002 7 31 USAASB02127 1 20020629 A 3350 20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN NOT SEATED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 413US 23882 IND - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 20 THROUGH 23 AND AT THE AFT LEFT SERVICE DOOR INOPERATIVE. M AINTENANCE RERACKED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002073100099 20020731 00099 NM 2002 7 31 USAASB02128 1 20020629 A 3350 20121 CHARGER BOEING 737 737401 1384701 NM CABIN INOPERATIVE A USAA K NONE O OTHER CR CRUISE 1 EA 19 425US 23992 CLT - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHTS FLASH OFF AND ON DURING FLIGHT. LIGHTS STOP FLASHING WHEN CYCLED ON , OFF AND BACK TO ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTERY CHARGER ASSEMBLY AND BATTERY PA CK. SYSTEM OPERATIONALLY CHECKS GOOD PER MM 33-51-02. (M) 2 L 7 2 4F RT A16WE 2002073100100 20020731 00100 NM 2002 7 31 USASB02118 1 20020618 A 3397 WIRE BOEING 737 737401 1384701 NM CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 412US 23881 CLE - MAINTENANCE FOUND THE AISLE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 6, 7, 8, 9 AND 11 INOPERATIVE. MAINTENANCE RE PAIRED SHORTED SEAT WIRING AT SEAT ROW 6ABAC. ALSO, REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK G OOD. (M) 2 L 7 2 4F RT A16WE 2002073100101 20020731 00101 NE 2002 7 31 SWIA200210907 2 20020604 A 7321 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE EEC CONTAMINATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 578SW 120346 EEC FAILED ON TAKEOFF ROLL, EEC AURAL WARNING. UNABLE TO DETERMINE WHICH EEC FAILED. ABORTED TAKEOFF. FOUND OIL CONTA MINATION IN CONNECTOR P0305. CLEANED AND RESECURED CONNECTOR. SWAPPED EEC AND TORQUE SIGNAL CONDITIONER WITH RIGHT ENG INE. RAN ENGINES. BOTH EEC'S TEST NORMALLY. 2 L 7 2 4T 4 T RT A31SO E20NE 2002073100102 20020731 00102 SO 2002 7 31 SWIA200210908 1 20020604 A 3231 PIN EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT MLG DOOR OUT OF POSITION A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 585SW 120353 RIGHT LANDING GEAR DOOR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO GJT. DISCOVERED LATCH PIN WAS BROKEN, LEFT SIDE O F RIGHT MAIN GEAR DOOR. FOUND AFT LATCH SAFETY PIN CAME OUT. RESAFETIED AND LATCHED DOOR. OPS CHECK GOOD. REINSPECTE D BY SLC CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002073100103 20020731 00103 2002 7 31 SWIA200210910 4 20020605 A 3425 6226190204 COMPUTER EMB 120 EMB120ER 3260203 SO NR 2 MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 227SW 6344 6344 120304 CAPTAIN'S RMI FLAG, FIRST OFFICER'S ADI GYRO AND COMPUTER FLAGS AND HSI HDG FLAG APPEARED ON TAKEOFF ROLL. ABORTED TAKE OFF. REPLACED NR 2 AHRS COMPUTER AND REINITIALIZED NR 2 AHRS SYSTEM. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073100104 20020731 00104 EA 2002 7 31 SWIA200210911 1 20020606 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 409SW 8966 8966 7056 DURING TAXI TO GATE, RECEIVED A SPOILERONS MESSAGE ON THE STATUS PAGE. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU WITH SERVICEABLE UNIT IAW MM 27-62-01. LEAK CHECK AND OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002073100105 20020731 00105 SO 2002 7 31 SWIA200210912 1 20020607 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 227SW 120304 FLOOR EMERGENCY LIGHT BURNED OUT AT ROW 9. RELAMPED FLOOR EMERGENCY LIGHT AT ROW 9. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073100106 20020731 00106 SO 2002 7 31 SWIA200210913 1 20020605 A 6123 RELAY EMB 120 EMB120ER 3260203 SO AUTO FEATHER FAILED A SWIA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NM 07 214SW 120280 UPON ADDING POWER ON TAKEOFF, LEFT TORQUE GAUGE WOULD NOT GO ABOVE 75PERCENT, THEN AURAL AUTO FEATHER WARNING SOUNDED AN D THE RIGHT ENGINE FEATHERED. UPON PULLING BACK POWER TO GROUND IDLE BOTH SIDES (ABORT), LEFT TORQUE GAUGE REMAINED AT 75 PERCENT AND RIGHT PROPELLER REMAINED FEATHERED. AFTER TURNING OFF AUTO FEATHER SWITCH, BOTH TORQUE INDICATORS NORMAL AND RIGHT PROP ON FEATHER. FDR DOWNLOAD INFORMATION INDICATED THE LEFT ENGINE AUTO FEATHER WAS STUCK IN THE TEST MODE, KEEPING LEFT TORQUE INDICATING 75 PERCENT AND RIGHT ENGINE PROPELLER IN FEATHER. REMOVED AND REPLACED AUTO FEATHER TES T RELAY M8353616-022M. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002073100107 20020731 00107 SO 2002 7 31 SWIA200210914 1 20020608 A 2750 3472001001 FCU EMB 120 EMB120ER 3260203 SO T/E FLAP MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 199SW 5421 280 120237 CONTROL FAULT ON TAXI OUT, COULD NOT RESET. REMOVED AND REPLACED FLAP CONTROL UNIT AND RIGHT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNITS IAW MM 27-00-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073100108 20020731 00108 EA 2002 7 31 SWIA200210915 1 20020604 A 2613 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE COCKPIT FALSE ACTIVATION A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 499SW 7398 LEFT JET PIPE OVERHEAT FAIL MESSAGE ON CLIMBOUT FROM LAS AT 27,000 FT. MESSAGE CLEARED, THEN RETURNED. LEFT JET PIPE O VERHEAT SYSTEM OPS CHECK GOOD AT THIS TIME. NO FAULTS FOUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2002073100109 20020731 00109 2002 7 31 SWIA200210916 4 20020608 A 3425 6226190204 COMPUTER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE E/E BAY MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 190SW 6653 5081 120050 AUTOPILOT/YAW FAILURE IN FLIGHT. INSTALLED SERVICEABLE AHC85 COMPUTER. OPS CHECKS GOOD. CAPTAIN'S COMPUTER AND GYRO F LAGS ARE INTERMITTENT IN FLIGHT. INSTALLED SERVICEABLE AHC85 COMPUTER. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002073100110 20020731 00110 SO 2002 7 31 SWIA200210917 1 20020607 A 3150 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE HORIZ STAB MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 585SW 120353 TAKEOFF AURAL WARNING TRIM SOUNDED ON START OF TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. RESET AURAL WARNING SYSTEM. OPS CHECKS GOOD. AURAL TRIM WARNING WILL NOT STOP. REPLACED PROXIMITY SENSORS. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002073100113 20020731 00113 NM 2002 7 31 UPS02438915 1 20020704 A 5310 SEAT TRACK BOEING 747 747123F NM M/D FLR PNL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C M/D - AFTER FLOOR PANEL REMOVED, BS 1940 RBL 11" SEAT TRACK FOUND HEAVY CORRODED. CORROSION BLEND OUT 0.044" X 1" X 1" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. 2 L 7 4 4F A20WE 2002073100114 20020731 00114 NM 2002 7 31 UPS02438917 1 20020630 A 5310 WEB BOEING 747 747123F NM BS 2231 S26L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C M/D - BS 2231 S26L BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. M/D BS 2231 S26L BELOW FLOOR INTERCO STAL WEB REPLACED AS PER SRM 51-10-01 P.8. 2 L 7 4 4F A20WE 2002073100115 20020731 00115 SO 2002 7 31 SWIA200210941 1 20020608 A 2510 STRUCTURE EMB 120 EMB120ER 3260203 SO CONSOLE OUT OF POSITION A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 290SW 120317 ELEVATOR TRIM STICKS WHEN MOVING WHEEL FORWARD OR BACK. CONSOLE TRIM RUBBING ON RIGHT TRIM WHEEL. REPOSITIONED CONSOLE TRIM. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002073100116 20020731 00116 NE 2002 7 31 SWIA200210980 3 20020625 A 6140 CONNECTOR EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE NP INDICATOR LOOSE A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 251YV 120251 RIGHT NP GAUGE DROPPED TO ZERO WHEN POWER WAS SET ON TAKEOFF. ABORTED TAKEOFF. FOUND CANNON PLUG FOR RIGHT NP GAUGE LO OSE. TIGHTENED CANNON PLUG AND RAN ENGINE UP TO POWER TWO TIMES. ALL CHECKED GOOD. 2 L 7 2 4T RT A31SO 6 C P11NE 2002073100117 20020731 00117 2002 7 31 SWIA200210981 4 20020624 A 2340 509612 HEADSET EMB 120 EMB120ER 3260203 SO CABIN SHORTED A SWIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 186SW 4538 4538 120034 ELECTRICAL BURNING SMELL IN CABIN ASSOCIATED WITH TWO FLASHING CABIN PASSENGER LIGHTS ON CAPTAIN'S SIDE. REMOVED AND RE PLACED FLIGHT ATTENDANT'S HANDSET IAW MM 23-41-01. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002073100118 20020731 00118 SO 2002 7 31 SWIA200210993 1 20020628 A 2120 HINGE PIN EMB 120 EMB120ER 3260203 SO RAM AIR DOOR DISLODGED A SWIA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 07 294SW 120321 ON CLIMBOUT, A SLIGHT PACK BURNING SMELL WAS OBSERVED. ABOUT 10 MINUTES INTO THE FLIGHT, THE LAV SMOKE DETECTOR SOUNDED . RETURNED TO LAX. FOUND RIGHT RAM AIR DOOR HINGE PIN DISLODGED. RESECURED RAM AIR DOOR HINGE PIN IAW MM. OPERATED P ACKS. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002073100119 20020731 00119 SO 2002 7 31 SWIA200210994 1 20020628 A 7930 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 297SW 120327 TRIPLE CHIME OIL AURAL WARNING WITH MAP LIGHT AT 85 KIAS ON TAKEOFF. ABORTED TAKEOFF. CHECKED OIL SERVICING, CHECKED O IL PRESSURE SWITCH, ASSOCIATED WIRING AND PRESSURE LINES. RAN ENGINES AND PILOT PERFORMED HIGH SPEED TAXI AT 85 KTS. A LL SYSTEMS WORKING AND INDICATING PROPERLY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073100120 20020731 00120 EA 2002 7 31 COMA0260459 1 20020729 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 957CA 7109 FLIGHT 5273 FLAPS FAILED AT 45 DEGREES AFTER LANDING.RESET THE FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002073100121 20020731 00121 SO 2002 7 31 SWIA200210995 1 20020627 A 6123 COVER EMB 120 EMB120ER 3260203 SO AUTOFEATHER SYS OUT OF POSITION A SWIA C ABORTED TAKEOFF R F PARTIAL RPM/PWR LOSS FLT CONT AFFECTED TO TAKEOFF 1 NM 07 186SW 120034 ABORTED TAKEOFF WHEN LEFT ENGINE FEATHERED ON TAKEOFF ROLL. INSPECTED AND FOUND SWITCH COVER FOR LEFT ENGINE ELECT FEAT HER INTERFERING WITH THE SWITCH. REPOSITIONED SWITCH COVER AND ENSURED CLEARANCE ON SWITCH. PERFORMED EXTENSIVE GROUND RUNS WITH NO FURTHER INCIDENTS OF AUTO FEATHER. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073100122 20020731 00122 SO 2002 7 31 SWIA200210996 1 20020629 A 5712 FRAME EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 RIGHT INBOARD LEADING EDGE INBOARD FRAME CRACKED AT UPPER AND LOWER TERMINATION. REPAIRED RIGHT INBOARD LEADING EDGE IN BOARD PER SRM 51-30-01, 51-10-02. 2 L 7 2 4T RT A31SO 2002073100123 20020731 00123 2002 7 31 SWIA200210997 4 20020629 A 2211 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT SYS FAILED A SWIA C ABORTED TAKEOFF J F WARNING INDICATION FLT CONT AFFECTED TO TAKEOFF 1 NM 07 289YV 3910 2967 120289 TRIM FAIL AND AUTOPILOT FAIL MAP LIGHTS ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED FIRST OFFICER'S AUTOPIL OT COMPUTER. FLIGHT DIRECTOR SYSTEM TESTS NORMAL PER MM 22-11-00. 2 L 7 2 4T RT A31SO 2002073100124 20020731 00124 EA 2002 7 31 SWIA200210998 1 20020625 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB FAILED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 432SW 2121 2121 7548 NR 2 STAB TRIM CHANNEL WILL NOT ENGAGE. REMOVED AND REPLACED HSTA. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW 27-42-0 5. PERFORMED OPS CHECK. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002073100125 20020731 00125 WP 2002 7 31 DHL2002806501 1 20020625 A 5730 561104142 PANEL DOUG DC8 DC873F 302199F WP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C CHECK FOUND R/H WING T/E LWR PANEL DELAMINATED.REMOVED AND REPLACED R/H WING LWR PANEL FROM STA XF219.000-339.0 00, PER SRM 51-3-0 PAGE 4. 2 L 7 4 4F RT 4A25 2002073100126 20020731 00126 WP 2002 7 31 DHL2002806502 1 20020626 A 5730 56110154105 PANEL DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C CHECK FOUND R/H WING LWR PANEL EXTERNAL SKIN DELAMINATED (STA XF 339.000-409.000)REMOVED AND REPLACED EXTERNAL SKIN PANSL PER SRM 52-3-0 PG 1. 2 L 7 4 4F RT 4A25 2002073100127 20020731 00127 WP 2002 7 31 DHL2002806503 1 20020626 A 5730 5611015409J PANEL DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C CHECK FOUND L/H WING T/E LWR PANEL EXTERNAL SKIN DELAMINATED BETWEEN XF 339.000 TO XF 409.000.REMOVED AND REPLA CED DELAMINATED PANEL PER SRM 51-1-21 PG 7. 2 L 7 4 4F RT 4A25 2002073100128 20020731 00128 WP 2002 7 31 DHL2002806505 1 20020624 A 5330 57103571 FILLET DOUG DC8 DC873F 302199F WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C CHK FOUND LWR FUESLAGE SIN FILLET # 741 EXTERNAL SKIN DELAMINATED (STA.1080.000-1100.000)REMOVED FILLET# 741 PE R SRM 51-3-0 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-18B.INSTALLED NEW FILLET PER SRM 51-3-0 PG7 AND SRM 51-3-1 PG7. 2 L 7 4 4F RT 4A25 2002073100129 20020731 00129 EA 2002 7 31 SWIA200211001 1 20020702 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN CONTAMINATED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 493SW 7450 FOUR SECTIONS IN A ROW OF EMERGENCY FLOOR LIGHTING ARE INOP. FOUND MOISTURE IN THE EMERGENCY FLOOR LIGHT TRACK. CLEANE D MOISTURE OUT OF LIGHT STRIPS. REINSTALLED STRIPS AND COVER. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002073100130 20020731 00130 EA 2002 7 31 SWIA200211002 1 20020701 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 430SW 2690 2690 7523 AT THE GATE, STAB TRIM CH 2 WILL NOT ENGAGE. REMOVED AND REPLACED HST ACTUATOR AND MCU IAW 27-41-00. ALL OPS CHECKS GO OD. 2 L 7 2 4F RT A21EA 2002073100131 20020731 00131 2002 7 31 SWIA200211004 4 20020630 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO AUTOPILOT SYS BINDING A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 190SW 2260 2260 120050 RUDDER PEDALS FEEL LIKE RUDDERS ARE BINDING UP. INSTALLED SERVICEABLE SVO65 AUTOPILOT SERVO. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002073100132 20020731 00132 2002 7 31 SWIA200211005 4 20020702 A 3425 INDICATOR EMB 120 EMB120RT 3260202 SO PWA 118 PW118A NE COCKPIT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 1105G 120105 FIRST OFFICER'S EHSI SCREEN BURNED OUT. REPLACED FIRST OFFICER'S EHSI SCREEN. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002073100133 20020731 00133 SO 2002 7 31 SWIA200211008 1 20020701 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 295UX 120295 EXIT SIGN ON ROW 9 OVERHEAD BIN INOP. REPAIRED BROKEN WIRE FOR EMERGENCY EXIT SIGN AT ROW 9 OVERHEAD. OPS CHECK GOOD. NO OTHER DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2002073100134 20020731 00134 SO 2002 7 31 SWIA200211009 1 20020701 A 3231 LATCH EMB 120 EMB120ER 3260203 SO LT MLG DOOR BROKEN A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 295UX 120295 LEFT MAIN GEAR RED LIGHT REMAINED ON AFTER GEAR RETRACTION AND RECYCLE. RETURNED TO SAN. LEFT GEAR FORWARD INBOARD DOO R LATCH BROKEN. REPLACED LATCH AND CYCLED DOORS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002073100135 20020731 00135 EA 2002 7 31 COMA0260460 1 20020729 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 986CA 6009 7174 FLIGHT 5234 GEAR DISAGREE MESSAGE ON APPROACH.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002073100136 20020731 00136 SO 2002 7 31 SWIA200211010 1 20020704 A 2422 RELAY EMB 120 EMB120ER 3260203 SO INVERTER FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 298SW 120328 NR 1 INVERTER FAILED DURING CLIMBOUT. FOLLOWED QRH PROCEDURE BUT INVERTER WOULD NOT RESET. RETURNED TO SLC. REMOVED A ND REPLACED RELAY K0001 IAW WM 24-20-00. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002073100137 20020731 00137 SO 2002 7 31 SWIA200211012 1 20020703 A 2752 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 186SW 3217 3092 120034 FLAP CONTROL FAULT INDICATION WITHOUT SELECTING ANY FLAP SETTINGS. LEFT OUTBOARD FLAP ACTUATOR FAILED THE OHM TEST. RE MOVED AND REPLACED ACTUATOR ON LEFT OUTBOARD FLAP IAW 27-50-00. 2 L 7 2 4T RT A31SO 2002073100138 20020731 00138 EA 2002 7 31 COMA0260461 1 20020729 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 819CA 7415 FLIGHT 5872 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.COULD NOT DUPLICATE. INSPECTED DOOR, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2002073100139 20020731 00139 SO 2002 7 31 SWIA200211013 1 20020630 A 5610 WINDOW EMB 120 EMB120ER 3260203 SO COCKPIT LACK OF LUBE A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 189SW 120048 CAPTAIN'S DIRECT VISION WINDOW REQUIRES EXCESSIVE FORCE TO SECURE TO THE CLOSED POSITION. CLEANED AND LUBRICATED TRACKS . OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002073100140 20020731 00140 SO 2002 7 31 SWIA200211014 1 20020701 A 5270 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 189SW 120048 CARGO DOOR WARNING CAME ON DURING TAKEOFF. RETURNED TO SLC. UNABLE TO DUPLICATE. OPS CHECK OF CARGO DOOR IS GOOD. 2 L 7 2 4T RT A31SO 2002073100141 20020731 00141 SO 2002 7 31 SWIA200211015 1 20020615 A 5411 RIB EMB 120 EMB120ER 3260203 SO NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW 120151 BOTH ENGINE OUTBOARD TAIL PIPE HOLDERS NEED TO BE CHECKED FOR POSSIBLE BROKEN RIB. THE HOLDERS HAVE MOVEMENT. REPLACED RIBS IAW 120 SRM 51-20-02. 2 L 7 2 4T RT A31SO 2002073100142 20020731 00142 SO 2002 7 31 SWIA200211016 1 20020615 A 5534 WEB EMB 120 EMB120ER 3260203 SO VERTICAL STAB CHAFED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW 120151 VERTICAL STAB RUDDER TRIM CABLES ARE CHAFING ON WEBBING WHERE CABLES CHANGE DIRECTION TO GO TO THE RUDDER TRIM ACTUATOR. THE WEBBING IS DAMAGED. REPAIRED IAW GST-1980/02 AND SB 120-27-0082. 2 L 7 2 4T RT A31SO 2002073100143 20020731 00143 SO 2002 7 31 SWIA200211017 1 20020615 A 5531 FRAME EMB 120 EMB120ER 3260203 SO VERTICAL STAB CHAFED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW 120151 BRACKET AND FRAME CHAFED WHERE RUDDER TRIM CABLES PASS FROM AFT RIGGING BAY INTO VERTICAL STAB. REPAIRED IAW GST-1980/0 2 AND SB 120-27-0082. 2 L 7 2 4T RT A31SO 2002073100144 20020731 00144 SO 2002 7 31 SWIA200211018 1 20020615 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW 120151 LEFT INBOARD NACELLE, WHEEL WELL AREA, FRAME CRACKED (JUST FORWARD OF POWER/CONDITION CABLE PULLEY BRACKET ASSEMBLY). NEW FRAME INSTALLED IAW SRM120 51-10-02. ALSO NEW FASTENERS INSTALLED IAW SRM120 51-40-02. 2 L 7 2 4T RT A31SO 2002073100145 20020731 00145 SO 2002 7 31 SWIA200211019 1 20020615 A 5712 RIB EMB 120 EMB120ER 3260203 SO RT & LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW 120151 RIGHT AND LEFT INBOARD LEADING EDGE RIBS EACH HAVE A CRACK. DOUBLER ADDED TO MENTIONED AREA IAW SRM 120 51-10-02. 2 L 7 2 4T RT A31SO 2002073100146 20020731 00146 SO 2002 7 31 SWIA200211020 1 20020615 A 5320 12006219001 SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW 120151 TWO SKIN SUPPORTS CRACKED AT FORWARD CARGO DOOR TRACK ATTACH POINTS. REPLACED BOTH SKIN SUPPORTS AND SECURED SAME IAW S RM 51-10-02. 2 L 7 2 4T RT A31SO 2002073100147 20020731 00147 EA 2002 7 31 SWIA200211022 1 20020703 A 3232 16520101 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A SWIA A UNSCHED LANDING F E J FLT CONT AFFECTED VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 07 597SW 2197 2197 7293 ON TAKEOFF FROM SLC, GEAR DISAGREEMENT FOLLOWED BY NOSE DOOR OPEN. RAN QRH. INDICATIONS CLEARED WHEN MLG LOWERED. RET URNED TO SLC. REMOVED AND REPLACED ACTUATOR IAW CRJ MM 32-23-01. NOSE LANDING GEAR SLOW TO STOW (GEAR DISAGREE) WITH O NE PUMP RUNNING. REMOVED AND REPLACED NLG PRIORITY VALVE PER MM 32-33-15. CYCLED GEAR. OPS CHECK GOOD. PERFORMED EME RGENCY EXTENSION. OPS CHECKS GOOD. NO LEAKS NOTED. 2 L 7 2 4F RT A21EA 2002073100148 20020731 00148 EA 2002 7 31 SWIA200211023 1 20020706 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILER MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 439SW 7578 OUTBOARD GROUND SPOILER FAULT STATUS MESSAGE AND, AFTER ENGINE START, SPOILERONS AND FAULT SPOILER CAUTION MESSAGE. RES ET SECU'S IAW FIM 27-61-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2002073100149 20020731 00149 EA 2002 7 31 SWIA200211024 1 20020703 A 5210 SPRING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FAILED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 406SW 7030 PASSENGER DOOR LATCH CANNOT BE STOWED FROM INSIDE THE AIRPLANE. REPLACED SPRING IN THE PUSH BUTTON ON OUTER PAX DOOR HA NDLE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002073100150 20020731 00150 NM 2002 7 31 AWXA200200679 1 20020729 A 2560 P2070001214 FLASHLIGHT BOEING 737 737301 1384611 NM BS 294.5 INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 0 0 23261 LAS - EMERGENCY EQUIPMENT - DURING INSPECTION THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE (I NBOARD POSITION). MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AND HOLDER ASSEMBLE (INBOARD POSITION), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002073100151 20020731 00151 NM 2002 7 31 AWXA200200680 1 20020729 A 2560 P2070001214 FLASHLIGHT BOEING 737 737301 1384611 NM BS 294.5 INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 0 0 23261 LAS - EMERGENCY EQUIPMENT - DURING INSPECTION THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE (O UTBOARD POSITION). MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AND HOLDER ASSEMBL E (OUTBOARD POSITION), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002073100152 20020731 00152 2002 7 31 ANCF200200015 4 20020729 A 2311 7926140001 COUPLING BOEING 767 767 UTILUSE NM PWA 4060 PW4060 52119 NE DAMAGED W ANCF A UNSCHED LANDING O OTHER CR CRUISE 1 SO 23 421AV 12963 12963 25421 TRANSMISSION ON BOTH HF INOPERATIVE AT ALL STATIONS.CORRECTIVE ACTION:PERFORMED FIM 23-11-00 OPERATION FOUND NORMAL ON L H HF, ON RH SYSTEM WAS REPLACED HF COUPLER AND HF TRANCEIVER AS PER AMM 23-11-03 ANS 23-11-01, ACCOMPLISHED OPERATIONAL TEST ON BOTH SYSTEM WIT SATISFACTORY RESULTS 2 L 7 2 4F 4 F RT A1NM E24NE 2002080100001 20020801 00001 EU 2002 8 1 C2XA02SH038 1 20020731 A 3350 3011180 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 93840 271 SHV-DURING MAINTENANCE CHACK,MAINTENANCE FOUND ROW 6,7, AND 9 AISLE PATH LIGHTING INOP, AND RIGHT HAND LOWER FORWARD EME RGENCY EXIT LIGHT INOP.MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK 10WL IN ACCORDANCE WITH ATR MM 33-51-21,A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080100002 20020801 00002 EU 2002 8 1 C2XA02SH039 1 20020731 A 3350 3011180 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 93840 271 SHV-DURING MAINTENANCE CHECK,MAINTENANCE FOUND AFT CENTER EMERGENCY EXIT LIGHT INOP AND SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP.MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK 15WL IN ACCORDANCE WITH ATR MM 33-51-21,AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080100003 20020801 00003 NM 2002 8 1 DL76S020671 1 20020615 A 2120 SMOKE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE CABIN DETECTED A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 119DL 33061 4436 23278 580398 AFTER T/O SMOKE IN MID CABIN WITH SMOKE DETECTOR GOING OFF IN MID CABIN. RETURNED TO LAND. LT PACK TRIPPED AND LT ENG BLEED LIGHT ILLUMINATED. ON GROUND SMOKE DISSIPATED. COMPRESSOR WASH NUMBER 1 ENGINE. AFTER WASH - RUN ENG 5 MINS AT IDLE, RUN PACKS/CYCLE A/I SYS. RUN ENG AT PWR ABOVE 60 N1 FOR 5 MIN-R PACKS/CYCLE A/I SYS. TO PREVENT ATB OR RTO DUE TO SMOKE/OD IN CABIN. PERFORMED ENG WASH PER 72-00-00-7-G-00. 2 L 7 2 4F 4 F RT A1NM E13NE 2002080100004 20020801 00004 NM 2002 8 1 DLM11020640 1 20020608 A 3350 SOCKET DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 804DE 48475 EMERGENCY LIGHTS IN FIRST CLASS DO NOT COME ON DURING TEST. REMOVED AND REPLACED 1 BATTERY IN COCKPIT PER M/M. NO HELP . FOUND TROUBLE TO BE IN SEAT 1J AND H REMOVED AND REPLACED LIGHT SOCKET AT 1J/H. FIRST CLASS EMERGENCY LIGHTING CKS G OOD. 2 L 7 3 4F RT A22WE 2002080100005 20020801 00005 NM 2002 8 1 DLM11020643 1 20020609 A 2120 ODOR DOUG MD11 MD11 3023602 NM CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 804DE 48475 APPROX 11 HRT INTO FLIGHT F/A IN AFT GALLEY AREA SMELLED. BURNING PLASTIC SMELL AT 4L AREA. SMELL DISSIPATED QUICKLY. OVENS WERE OFF AND LAVS WERE EMPTY AND PANELS NOT WARM. CEILING ABOVE F/A 4L JUMPSEAT IS SOOTED AROUND AIRVENT. CHECK ED AFT C/B PANEL IN CEILING. NO C/B WERE POPPED. INSP AFT GALLEY CEILING PANELS AND O/H EQUIP ABOVE CEILING. INSP 4L LAV UNDERSINK AND TRASH CONTAINER AREA. HEAT IND AND FIRE BOTTLES NORM. REMOVED 4L PA STANCHION AND INSP OK. ALL GALL EY EQUIP OPS NORMAL. ALL LIGHTS OP OK. SOOT AT AIRVENT IS DUST. CLEAN SAME. NO SMELL NOTED. 2 L 7 3 4F RT A22WE 2002080100006 20020801 00006 NM 2002 8 1 DLM11020679 1 20020617 A 2611 72130001013 SMOKE DETECTOR DOUG MD11 MD11 3023602 NM LAVATORY MALFUNCTIONED A DALA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 27 811DE 48566 LAVATORY SMOKE LEVEL-1 INDICATION ILLUMINATED IN COCKPIT. DURING PREFLIGHT. REPLACED SMOKE DETECTOR, OP CHECKS GOOD. 2 L 7 3 4F RT A22WE 2002080100007 20020801 00007 NM 2002 8 1 DLM88020637 1 20020608 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 900DE 53372 AFT CABIN EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY, CHECKS GOOD. 2 L 7 2 4F RT A6WE 2002080100008 20020801 00008 NM 2002 8 1 DLM88020638 1 20020608 A 3350 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 950DL 49881 AFT CABIN EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY, CHECKS GOOD. 2 L 7 2 4F RT A6WE 2002080100009 20020801 00009 NM 2002 8 1 DLM88020639 1 20020608 A 2450 ELECTRICAL SYS DOUG MD88 MD88 3023688 NM COCKPIT MALFUNCTIONED A DALA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SO 27 960DL 49979 JUST BEFORE TAXI OUT LOST BOTH BUSSES, ENGINE BUSSES DID NOT PICK UP FROM APU. COMPLETE ELECTRICAL FAILURE. RESET LT A ND RT GEN SWITCHES TO ON. RAN ENGS BOTH GENS OPS CHECK OK. 2 L 7 2 4F RT A6WE 2002080100010 20020801 00010 NM 2002 8 1 DLM88020641 1 20020609 A 3320 D77311001 BALLAST DOUG MD88 MD88 3023688 NM CABIN OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 938DL 49811 WHITE SMOKE CAME FROM OVERHEAD BIN, FROM A RECESSED PANEL IN OVERHEAD BIN. POWER WAS REMOVED FROM AIRCRAFT. PERFORMED OPS 5088. FOUND OVERHEAD CEILING LIGHT BALLAST OVERHEATED. REPLACED BALLAST. ELECTRICAL PIGTAIL BAD. REPLACED SAME. 2 L 7 2 4F RT A6WE 2002080100011 20020801 00011 NM 2002 8 1 DLM88020647 1 20020610 A 2910 HYDRAULIC SYSTEM DOUG MD88 MD88 3023688 NM RT MLG WW LEAKING A DALA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 947DL 49878 CREW REPORTED ON FINAL APPROACH WITH PACKS IN FULL COLD GOT SMOKE IN THE CABIN. FOUND HYDRAULIC LEAK IN RIGHT WHEEL WEL L. FLUID HAD TRANSITIONED TO APU INLET CONTAMINATING A/C SYSTEM. COMPLIED WITH OPERATIONS 5088 AND 5089 DUCT BURN OUT PROCEDURE. CLEANED INLET. 2 L 7 2 4F RT A6WE 2002080100012 20020801 00012 NM 2002 8 1 DLM88020650 1 20020611 A 3397 WIRE HARNESS DOUG MD88 MD88 3023688 NM CABIN DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 918DL 49583 RED EMERGENCY EXIT LIGHTS INOP AT ROW 24 DE (EXIT ROW). FOUND WIRE HARNESS UNPLUGGED UNDER SEAT. LIGHTS OP NORMAL AFTE R PLUG RECONNECTED. 2 L 7 2 4F RT A6WE 2002080100013 20020801 00013 NM 2002 8 1 DLM88020653 1 20020612 A 5330 593600731 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DL 49532 DURING HMV-3, THE C3 DOOR CUT OUT AFT EDGE SKIN AND DOUBLER WERE FOUND DENTED AT THE NR 3 DOOR STOP. DAMAGE REPAIRED PE R ERA 413069-14. 2 L 7 2 4F RT A6WE 2002080100014 20020801 00014 NM 2002 8 1 DLM88020654 1 20020612 A 3260 H141016 SWITCH DOUG MD88 MD88 3023688 NM NLG MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 917DL 49573 ON DEPT AFTER NORMAL RETRACTION RED NOSE GEAR LIGHT CAME ON. FOLLOWED CK LIST PROCEDURE TO RECYCLE, CAME DOWN NORMAL. ATTEMPTED TO RETRACT. NOSE GEAR REMAINED DOWN AND LOCKED. HANDLE PLACED BACK DOWN. ALL GEAR DOWN AND LOCKED. RETURNE D TO CVG. REPLACED S1-412 INTERLOCK SW AND D1-32 PROX SW. JACKED NOSE AND CYCLED GEAR. GEAR IND NORMAL. LOWERED A/C AND REMOVED JACK PAD. 2 L 7 2 4F RT A6WE 2002080100015 20020801 00015 EA 2002 8 1 02212657 1 20020731 A 3350 GE317 LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 657BR 7491 During preflight inspection, the crew reported that the R/H forward exterior emergency exit light was inoperative. Main tenance of this discrepancy was initially deferred IAW the CRJ MEL 33-51-02. Later, maintenance personnel removed and r eplaced the R/H forward emergency exit light lamp. An operational check was satisfactory and the aircraft was returned to normal service. 2 L 7 2 4F RT A21EA 2002080100016 20020801 00016 NM 2002 8 1 DLM88020655 1 20020612 A 7711 7958537501 SENSE LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE CRACKED A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 925DL 49712 718217 UNABLE TO MAKE T/O POWER AT 70 KNOTS N1 REACHED 106 PERCENT FOR FOUR SECONDS. REJECTED TAKEOFF. A/C FERRY TO ATL FOR E NG CHANGE. MTC FOUND PT7 LINE CRACKED. REPLACED NR 2 ENG PER TRANS 9T102. 2 L 7 2 4F 4 F RT A6WE E9NE 2002080100017 20020801 00017 NM 2002 8 1 DLM88020658 1 20020613 A 2450 91976 SELECTOR SWITCH DOUG MD88 MD88 3023688 NM COCKPIT FAULTY A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 937DL 49810 ON TAXI OUT AFTER STARTING NR 2 ENGINE THE OVERHEAD PANEL STARTED TO SMOKE. FOUND A/C VOLT/FREQ SELECTOR SW ON OVHD PAN EL BAD. REPLACED SAME, CKS GOOD. 2 L 7 2 4F RT A6WE 2002080100018 20020801 00018 NM 2002 8 1 DLM88020660 1 20020613 A 2450 91976 SELECTOR SWITCH DOUG MD88 MD88 3023688 NM COCKPIT SHORTED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 937DL 49810 ON TAXI AC VOLT/FREQ SELECTOR SWITCH ON OVHD PANEL STARTED TO SMOKE. WHEN RIGHT SELECTED VOLTS/FREQS READ ZERO WITH ENG INE RUNNING. SELECTED LEFT SMOKE STOPPED. RTB. FOUND VOLTMETER/AMMETER SELECT SWITCH BURNED AND SHORTED. REPLACED SA ME. ALL OK. ACFT OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2002080100019 20020801 00019 NM 2002 8 1 DLM88020667 1 20020614 A 5350 TAIL CONE DOUG MD88 MD88 3023688 NM FUSELAGE DEPARTED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 976DL 53257 AT PUSHBACK GOT TAIL CONE UNSAFE MESSAGE WITH ASSOCIATED TAILCONE SEPARATED FROM A/C AND LYING ON GROUND BEHIND THE ACA. INSTALLED NEW TAILCONE PER M/M AND REMOVED AND INSTALLED NEW SLIDE PACK. 2 L 7 2 4F RT A6WE 2002080100020 20020801 00020 NM 2002 8 1 DLM88020683 1 20020618 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 950DL 49881 EMERGENCY LIGHTS INOP AFT OF ROW 31. REPLACED POWER SUPPLY NOW CHECK NORMAL. 2 L 7 2 4F RT A6WE 2002080100021 20020801 00021 NM 2002 8 1 DLM88020685 1 20020619 A 5330 9912455505 DOUBLER DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DL 49532 DURING HMV-3 THE TIME-LIMITED REPAIR INSTALLED PER ERA 368951-14 (ORIG ISSUE) WAS REMOVED AND A LARGER PERMANENT REPAIR WAS INSTALLED. REPAIR IS FOR CORROSION FOUND AT THE FWD CARGO DOOR SURROUND DOUBLER. EXISTING REPAIR REMOVED AND A NEW REPAIR INSTALLED PER ERA 368951-14, REV A. 2 L 7 2 4F RT A6WE 2002080100022 20020801 00022 NM 2002 8 1 DLM90020672 1 20020615 A 5610 SEAL DOUG MD90 MD9030 3023690 NM COCKPIT WINDOW LOOSE A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 912DN 53392 LOUD VIBRATION PASSING THRU 10,000 FT ON CAPTAINS WINDOW SIDE. FOUND AERODYNAMIC SEAL LOOSE ON CAPTAINS WINDOW ON THE U PPERSIDE. REMOVED LOOSE SEAL. APPLIED NEW SEALER PER M/M. 2 L 7 2 4F RT A6WE 2002080100023 20020801 00023 EU 2002 8 1 0202413234 1 20020724 A 5347 SEAT TRACK AIRBUS 320 A320212 3930322 EU CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 334NW 339 During "L" check found corrosion on seat track at BS 765 between frames 18 and 20. Repaired per EA 32-191967. 2 L 7 2 4F RT A28NM 2002080100024 20020801 00024 NM 2002 8 1 0202426743 1 20020722 A 5315 FLOORBEAM BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 643NW 22245 DURING "M" CHECK FOUND CORROSION ON FLOORBEAM AT BS 520 LBL 13 TO RBL 21. REPAIRED PER EA 67-191810. 2 L 7 4 4F RT A20WE 2002080100025 20020801 00025 NM 2002 8 1 0202436743 1 20020716 A 5315 FLOORBEAM BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 643NW 22245 DURING "M" CHECK FOUND CORROSION ON MAIN DECK FLOORBEAM AT BS 620 BL 11 L&R. REPAIRED PER EA 67-191798. 2 L 7 4 4F RT A20WE 2002080100026 20020801 00026 NM 2002 8 1 0202446743 1 20020702 A 5311 SHEAR TIE BOEING 747 747249F 1384849 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 643NW 22245 During "M" check found cracks in shear tie at BS 520 between S8L and S10L. Repaired per EA 67-191111. 2 L 7 4 4F A20WE 2002080100028 20020801 00028 NE 2002 8 1 MALA020431 2 20020723 A 7200 CT75A2 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 119XJ 340A119 DURING FLIGHT 2919, LT ENGINE AND ITT SPIKED TO 980 DEGREES. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED LT EN GINE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002080100029 20020801 00029 EU 2002 8 1 MALA020433 1 20020724 A 5320 STRUCTURE SAAB SF340 340B 7860101 EU FUSELAGE PUNCTURED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 362XJ FOUND RT FUSELAGE PUNCTURED AT STA 363 BELOW PAX WINDOW REINFORCEMENT DOUBLER. COMPLETED REPAIR IAW EO S53009. 2 L 7 2 4T RT A52EU 2002080100030 20020801 00030 EU 2002 8 1 MALA020434 1 20020724 A 3231 DOOR BAC 146 AVRO146RJ85A 1500097 EU LT MLG MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 532XJ E2366 DURING FLIGHT 3684, LANDING GEAR WOULD NOT UPLOCK. AIR RETURN TO MEM. MAINTENANCE REPINNED LT MAIN GEAR DOOR IN CORREC T POSITION. 2 H 7 4 4F RT A49EU 2002080100031 20020801 00031 2002 8 1 MALA020435 4 20020721 A 3442 6227337001 TRANSCEIVER SAAB SF340 340B 7860101 EU WEATHER RADAR MALFUNCTIONED A MALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 15 429XJ 340B429 DURING FLIGHT 3384, CREW REPORTED THE LT INTAKE HEAT IS INOP. THE WEATHER RADAR IS INOP AND THE ENGINE POWER ROLLED BAC K INFLIGHT. MAINTENANCE REPLACED WEATHER RADAR TXCVR, THE LT ENGINE ANTI-ICE MASTER CAUTION, LT INTAKE LIGHT ON. CND O N GROUND, RAN A/C FOR 25 MINUTES NO FAULT NOTICED. OPS CHECK GOOD. POWER ROLLBACK ON LEFT SIDE EVERYTHING WENT BACK TO NORMAL AFTERWARDS, ICING CONDITIONS WERE EXISTING AT THE TIME. MAINTENANCE INSPECTED LT INTAKE, NO FOD FOUND. A/C WAS IN ICING. NO FURTHER ACTION REQUIRED AT THIS TIME. ALL IAW GE MM 72-00-00. 2 L 7 2 4T RT A52EU 2002080100032 20020801 00032 EU 2002 8 1 MALA020436 1 20020722 A 7722 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 114XJ 340A114 DURING FLIGHT 2956 RIGHT ENGINE ITT SPIKE IN TEMP 50-55 PERCENT SPIKE OCCURRED EVERY 3-4 MINUTES. AIR RETURN TO MSP. M AINTENANCE REMOVED CANNON PLUG FROM TRIMMER, AND OHMS CHECKED GOOD. REMOVED CANNON PLUGS FROM ECU, INSPECTED, NO DEFECT S NOTED. CLEANED CANNON PLUGS AND REINSTALLED ON ECU AND TRIMMER. RAN A/C FOR 45 MINUTES AT POWER, NO DISC NOTED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002080100033 20020801 00033 NE 2002 8 1 MALA020438 2 20020726 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT POWER LOSS A MALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 15 411XJ 340B411 DURING FLIGHT 3392, EXPERIENCED ROLLBACK AT 21,000 FT. -11 DEGREES CELSIUS, 59 PERCENT TORQUE. IN ICING CONDITIONS NO S HIFT IN ITT OR TORQUE WAS NOTICED. IGNITION LIGHT DID NOT ILLUMINATE. CREW COULD NOT DETERMINE WHICH ENGINE HAS THE RO LLBACK BUT BELIEVE IT WAS THE RIGHT ENGINE. MAINTENANCE OK'D A/C TO RETURN TO SERVICE. POSTFLIGHT NO DEBRIS OR OBSTRUC TION FOUND IN ENGINE INLETS. UNDER THE DIRECTION OF MXC AND GMM RE FAULT 150 72-00-00 TABLE 101 TROUBLE 5 PAR B. NO FU RTHER ACTION. 2 L 7 2 4T 4 T RT A52EU E8NE 2002080100034 20020801 00034 2002 8 1 SWAA021605 4 20020721 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002080100035 20020801 00035 NM 2002 8 1 SWAA021606 1 20020721 A 3350 BR2013 LIGHT BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 EEPLS LOOSE AT ROWS NR 9 AND NR 10. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002080100036 20020801 00036 2002 8 1 SWAA021608 4 20020720 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN DOOR WAS OPENED. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002080100037 20020801 00037 NM 2002 8 1 SWAA021617 1 20020721 A 5311 6552880 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 294, WL 209 AND RBL 55. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002080100038 20020801 00038 NM 2002 8 1 SWAA021619 1 20020721 A 5320 BAC1490 ANGLE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND Z-CHORD CORRODED AT BS 270, WL 208 AND RBL 2. REPAIRED Z-CHORD PER SRM. 2 L 7 2 4F RT A16WE 2002080100039 20020801 00039 2002 8 1 SWAA021620 4 20020722 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 081SW 22730 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002080100040 20020801 00040 2002 8 1 SWAA021621 4 20020721 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002080100041 20020801 00041 2002 8 1 SWAA021622 4 20020721 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002080100042 20020801 00042 NM 2002 8 1 SWAA021623 1 20020721 A 5312 6545409 PRESSURE PANEL BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED A1 CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, RBL 40. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002080100043 20020801 00043 NM 2002 8 1 SWAA021627 1 20020722 A 5320 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002080100044 20020801 00044 NM 2002 8 1 SWAA021629 1 20020722 A 3234 6554219 CONTROL HANDLE BOEING 737 7373H4 1384600 NM COCKPIT FAULTY A SWAA K NONE J WARNING INDICATION AP APPROACH 1 SW 29 336SW 23940 DURING APPROACH WITH GEAR HANDLE DOWN, GOT THREE GREEN LIGHTS AND THREE RED LIGHTS, RECYCLED GEAR TWICE BEFORE RED LIGHT S WENT OUT. CLEANED AREA AROUND S-78 SWITCH AND LUBED RETURN SPRING PER MM. 2 L 7 2 4F RT A16WE 2002080100045 20020801 00045 NM 2002 8 1 SWAA021630 1 20020722 A 2710 6555731 DRUM BOEING 737 7372T4 1384492 NM E/E BAY OUT OF ADJUST A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 722WN 22698 AILERON CONTROL RESPONDING ERRATIC WHEN TURNING LEFT AT SLOW SPEEDS. FOUND,UPPER BUS DRUM LUG, OUT OF ADJUSTMENT. ADJU STED PER MM. 2 L 7 2 4F A16WE 2002080100046 20020801 00046 NM 2002 8 1 SWAA021633 1 20020721 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SPECIAL VISIT, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, RBL 41. REPAIRED PRESS WEB PER SRM. 2 L 7 2 4F RT A16WE 2002080100047 20020801 00047 2002 8 1 SWAA021647 4 20020724 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 102SW 23108 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F A16WE 2002080100048 20020801 00048 NM 2002 8 1 SWAA021648 1 20020724 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 1/2D CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT BASE BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY P ER MM. 2 L 7 2 4F RT A16WE 2002080100049 20020801 00049 2002 8 1 SWAA021649 4 20020724 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED RON, FOUND BOTH SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF LIMITS. REMOVED AND REPLACED BOT H SVC DOOR SLIDES PER MM. 2 L 7 2 4F RT A16WE 2002080100050 20020801 00050 2002 8 1 SWAA021650 4 20020724 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002080100051 20020801 00051 NM 2002 8 1 SWAA021660 1 20020725 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 EEPLS LOOSE AT ROW NR 12. REMOVED AND REPLACED EEPLS AT ROW NR 12 PER MM. 2 L 7 2 4F RT A16WE 2002080100052 20020801 00052 2002 8 1 SWAA021661 4 20020724 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002080100053 20020801 00053 NM 2002 8 1 SWAA021662 1 20020724 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED EXIT LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2002080100054 20020801 00054 NM 2002 8 1 SWAA021664 1 20020724 A 3350 20131A BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED PM CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002080100055 20020801 00055 NM 2002 8 1 SWAA021669 1 20020726 A 2560 BATTERY BOEING 737 7372H4 138448C NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 090SW 22905 AFT EMERGENCY FLASH LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002080100056 20020801 00056 2002 8 1 SWAA021670 4 20020726 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002080100057 20020801 00057 NM 2002 8 1 SWAA021672 1 20020726 A 3350 900835A LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS INOP AT MID AND FWD CABIN. REMOVED AND REPLACED LI GHT ASSY PER MM. 2 L 7 2 4F A16WE 2002080100058 20020801 00058 NM 2002 8 1 SWAA021673 1 20020725 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C3 CHECK, FOUND EEPLS WORN BETWEEN ROW'S NR 7 AND NR 9. REMOVED AND REPLACED EEPLS BETWEEN ROW'S NR 7 AND NR 9. 2 L 7 2 4F RT A16WE 2002080100059 20020801 00059 NM 2002 8 1 SWAA021674 1 20020726 A 3350 6574550 CONNECTOR BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 1/2D CHECK, FOUND LT EMERGENCY EXIT LIGHTS INOP. SECURED CANNON PLUG TO BATTERY. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2002080100060 20020801 00060 NM 2002 8 1 SWAA021675 1 20020726 A 3350 20121 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 1/2D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002080100061 20020801 00061 2002 8 1 SWAA021676 4 20020726 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002080100062 20020801 00062 2002 8 1 SWAA021677 4 20020727 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002080100063 20020801 00063 NM 2002 8 1 SWAA021678 1 20020727 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 EEPLS LOOSE AT ROW'S NR 12 AND NR 13. REPAIRED WIRES AND INSTALLED MISSING COVERS PER MM. 2 L 7 2 4F RT A16WE 2002080100064 20020801 00064 NM 2002 8 1 C1HA200288014 1 20020730 A 3350 900835A BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 688CA 22344 R/H aft exterior emergency overwing light INOP.Removed and replaced R/H AFT battery pack. 2 L 7 3 4F A3WE 2002080100065 20020801 00065 NM 2002 8 1 SWAA021679 1 20020727 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASS Y PER MM. 2 L 7 2 4F A16WE 2002080100066 20020801 00066 NM 2002 8 1 SWAA021681 1 20020728 A 3350 071701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002080100067 20020801 00067 NM 2002 8 1 SWAA021683 1 20020727 A 3350 65C27093 CONNECTOR BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. SECURED LOOSE CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2002080100068 20020801 00068 NM 2002 8 1 SWAA021684 1 20020728 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 103SW 23109 DURING SCHEDULED PM CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT OVERWING EXIT. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002080100069 20020801 00069 2002 8 1 SWAA021685 4 20020728 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 778SW 27883 AFT SVC DOOR EMERGENCY EXIT EVAC SLIDE INADVERTENTLY WAS PULLED FROM CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002080100070 20020801 00070 NE 2002 8 1 00030 2 20020619 A 7200 ENGINE LEAR 24 24F 5170317 CE GE CJ610 CJ6106 30006 NE RIGHT FLAMED OUT E HAEA B EMER. DESCENT X ENGINE FLAMEOUT CL CLIMB 1 SW 05 444TW 348 251305 AIRCRAFT EN ROUTE FROM ELP TO MCI CLIMBING THROUGH FL420 TO FL450 RT ENGINE FLAMED OUT. DESCENT TO FL250, PERFORMED RES TART AND CLIMBED BACK TO FL410, COMPLETED TRIP NO FURTHER INCIDENT. PILOT INSPECTED FOR FOD OR OTHER DAMAGE AT MCI, NON E FOUND. C/W FLAME-OUT INSPECTION AND PERFORMANCE RUN AT ADS. NO DISCREPANCIES AT THIS TIME. 2 L 7 2 4J 4 J A10CE 1E16 2002080100071 20020801 00071 EU 2002 8 1 00031 1 20020620 A 3232 ACTUATOR AMD FALC20 FALCON 2720302 EU NLG DOOR OUT OF ADJUST E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 158TW 158 ACFT DEPARTED ADS, GEAR DOOR RED LIGHTS WOULD NOT GO OUT, RETURN TO ADS. WILL UPDATE AFTER MAINTENANCE. ADJUSTED NOSE GEAR DOOR ACTUATOR ROD END OP'S CK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F A7EU 2002080100072 20020801 00072 2002 8 1 MWEA020418 4 20020604 A 3442 MI585307403 TRANSCEIVER DOUG DC9 DC932 3022066 WP COCKPIT MALFUNCTIONED A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 207ME 47794 JUST AFTER DEPARTURE FROM MILWAUKEE RADAR INDICATOR BLANKED OUT. RECYCLED UNIT OFF AND ON DISPLAY CAME YELLOW ONLY AND FLICKERED DISPLAY WAS SAME ALL THE WAY TO GATE. RETURNED TO MILWAUKEE. REPAIRED AND REPLACED WEATHER RADAR TRANSCEIVER SYSTEM OPS CHECK OK, REFERENCE MM 34-40. 2 L 7 2 4F A6WE 2002080100073 20020801 00073 WP 2002 8 1 MWEA020419 1 20020606 A 3234 VALVE DOUG DC9 DC981 3022081 WP LANDING GEAR MALFUNCTIONED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 805ME 48031 DEPARTURE OUT OF DCA RED GEAR UNSAFE LIGHT ON WITH GEAR UP. RAN QRH PRECAUTIONARY LANDING AT IAD GROUND SHIFT CONTROL R ELAYS PULLED X2323 PER QRH DUE TO AIRCRAFT NOT GOING INTO FLIGHT MODE. NORMAL LANDING MADE ON 19L. RESET CB'S ON GROUN D NORMAL TAXI BACK TO GATE. FOUND BAD VALVE. REMOVED AND REPLACED VALVE SERVICE IAW MM 32-21-02. NO LEAKS NOTED AT TH IS TIME. NO DAMAGE TO NOSE GEAR. 2 L 7 2 4F A6WE 2002080100074 20020801 00074 NM 2002 8 1 DL76K020688 1 20020619 A 2530 ODOR BOEING 767 767332 1382001 NM GALLEY DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 176DZ 29697 DURING DESCENT F/A REPORTED STRONG ELECTRICAL SMELL IN AFT GALLEY. FOLLOWED PROCEDURES AND TURNED OFF UTILITY BUS SWITC HES AND SMELL DISSIPATED. UNABLE TO DUPLICATE, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2002080100075 20020801 00075 NE 2002 8 1 DL76L020645 2 20020607 A 7230 COMPRESSOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE STALLED A DALA K NONE R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 27 186DN 23193 27962 727679 COMPRESSOR STALL AT TOP OF DESCENT WHILE PULLING BACK POWER. REPLACING ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002080100076 20020801 00076 NM 2002 8 1 DL76L020674 1 20020615 A 5610 141T480150 WINDOW BOEING 767 767332 1382001 NM COCKPIT CRACKED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 185DN 27961 R1 WINDOW SHATTERED IN FLIGHT. NOTICED ARCHING AROUND WINDOW THEN PULLED CIRCUIT BREAKER FOR CONTROLLER AND THEN THE WI NDOW SHATTERED. WINDSHIELD REPLACED AS PER M/M 56-11-01-4. 2 L 7 2 4F RT A1NM 2002080100077 20020801 00077 NE 2002 8 1 DL76L020677 2 20020617 A 7200 PW40603 BOSS BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 187DN 23036 27582 727621 ENGINE REMOVED DUE TO IGNITOR BOSS THREAD DAMAGE. HANGER MACHINE SHOP FORCIBLY REMOVED BOSS FOUND MAJOR THREAD DAMAGE O N BOTH THE BOSS AND THE ENG CASE. REMOVED AND REPLACED NR 2 ENG ON R/C DECK. 2 L 7 2 4F 4 F RT A1NM E24NE 2002080100078 20020801 00078 SO 2002 8 1 SWIA200211025 1 20020704 A 5270 STRIKER EMB 120 EMB120RT 3260202 SO CARGO DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 196CA 120196 AFTER TAKEOFF, CARGO DOOR LIGHT ILLUMINATED, MASTER WARNING DOORS AND DOOR CAPTION ON MAP ILLUMINATED. WARNING DOES NOT OCCUR ON GROUND. RETURNED TO RDD. ADJUSTED CARGO DOOR AFT STRIKER PLATE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002080100079 20020801 00079 NE 2002 8 1 SWIA200211026 2 20020707 A 7321 3037603 SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 578SW 120346 RIGHT ENGINE RED EEC GLARESHIELD ILLUMINATED WITH AURAL WARNING ENGINE CONTROL DURING TAKEOFF ROLL. ABORTED TAKEOFF. R EMOVED AND REPLACED T1.8 SENSOR. OPS CHECK GOOD IAW 73-23-01. 2 L 7 2 4T 4 T RT A31SO E20NE 2002080100080 20020801 00080 EA 2002 8 1 SWIA200211027 1 20020706 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 442SW 7609 ON APPROACH RECEIVED A FLAPS FAIL MESSAGE. LANDED WITH FLAPS AT ZERO. COMPLIED WITH AD 98-20-01/03. NO DISCREPANCIES NOTED ON FLAP INSPECTION. RESET FLAP COMPUTER WITH NO FURTHER INSTANCES OF FLAP FAILURE. FLAP SYSTEM IS OPERATING NORM ALLY. 2 L 7 2 4F RT A21EA 2002080100081 20020801 00081 SO 2002 8 1 SWIA200211028 1 20020709 A 3241 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT ACTIVATED A SWIA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 07 234SW 120308 LEFT ANTISKID INOP ON APPROACH TO LANDING. ON SECOND APPROACH THE LEFT ANTISKID FAILED AGAIN FOLLOWED BY THE RIGHT ABOU T 10 SECONDS LATER. RETURNED TO FAT. INSPECTED ANTISKID SYSTEM, UNABLE TO DUPLICATE DISCREPANCY AT THIS TIME. REMOVED AND REPLACED LEFT AND RIGHT ANTISKID RELAYS FOR TROUBLESHOOTING. OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002080100082 20020801 00082 EA 2002 8 1 SWIA200211029 1 20020706 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 413SW 7102 INBOARD GROUND SPOILER FAULT AND SPOILERS FAULT MESSAGES ON TAXI OUT. RETURNED TO THE GATE. RESET SECU NR 2. ALL MESS AGES CLEARED AND ALL SURFACES OPERATE NORMALLY. 2 L 7 2 4F RT A21EA 2002080100083 20020801 00083 EA 2002 8 1 SWIA200211031 1 20020708 A 3234 555405 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER E F J VIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 720SW 7297 NOSE GEAR DID NOT GO DOWN & LOCKED AFTER EXTENDING GEAR. ALSO RECEIVED GEAR DISAGREE WARNING MESSAGE. RECYCLED ONCE AN D IT EXTENDED NORMALLY. REMOVED AND REPLACED NOSE LANDING GEAR SELECTOR VALVE IAW CRJ MM 32-33-10. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2002080100084 20020801 00084 2002 8 1 SWIA200211032 4 20020707 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 587SW 7062 CAPTAIN'S STICK PUSHER DOES NOT WORK. REMOVED AND REPLACED THE STALL PANEL COMPUTER. NR 1 SPC OPERATES NORMALLY. 2 L 7 2 4F RT A21EA 2002080100085 20020801 00085 SO 2002 8 1 SWIA200211033 1 20020704 A 7931 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 186SW 120034 AFTER TAKEOFF AT 100 AGL, RECEIVED AN AURAL OIL WITH TRIPLE CHIME. NO ASSOCIATED MAP WARNINGS AND NO ENGINE PARAMETERS TO SUPPORT THE WARNING. ALARM WAS CONTINUOUS AND COULD NOT BE CANCELLED. RETURNED TO SLC. REMOVED AND REPLACED OIL PR ESSURE TRANSDUCER CANNON PLUG AND AURAL WARNING UNIT. 2 L 7 2 4T 4 T RT A31SO E20NE 2002080100086 20020801 00086 EA 2002 8 1 SWIA200211034 1 20020708 A 2741 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE HORIZ STAB MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 592SW 1861 1861 7279 STAB CH 1 INOP STATUS MESSAGE TRIM NR 1 WON'T ENGAGE. REMOVED AND REPLACED STAB TRIM MOTOR CONTROL UNIT AND ACTUATOR, O PS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080100087 20020801 00087 EA 2002 8 1 SWIA200211035 1 20020710 A 2421 755469B IDG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 403SW 6247 6247 7028 RECEIVED A GEN 1 OFF CAUTION DURING T/O ROLL. ABORTED T/O. REMOVED AND REPLACED IDG ON LT ENGINE. OPS CHECK GOOD AT T HIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080100088 20020801 00088 EA 2002 8 1 SWIA200211036 1 20020709 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE SERVICE DOOR LOOSE A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 403SW 7028 INTERMITTENT SERVICE DOOR CAUTIONS FOR FIRST 15 MINUTES OF FLIGHT. CABIN PRESSURE AND DOOR LATCH INDICATORS NORMAL. TI GHTENED INNER HANDLE ON SERVICE DOOR. SERVICE DOOR IND, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080100089 20020801 00089 EU 2002 8 1 00032 1 20020628 A 3260 SQUAT SWITCH AMD FALC20 FALCONE 2720305 EU LANDING GEAR MALFUNCTIONED E HAEA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 285TW 285 AIRCRAFT CLIMBING OUT OF LIT EN ROUTE TO DET AIRCRAFT STARTED TO DEPRESSURIZE, LEVELED OFF STILL WOULD NOT HOLD CABIN. DIVERTED TO MEM. REMOVED AND REPLACED RT SQUAT SWITCH AND ALTITUDE CONTROLLER, GROUND CK GOOD. RETURNED AIRCRAFT TO SE RVICE. 2 L 7 2 4F A7EU 2002080100090 20020801 00090 EU 2002 8 1 00033 1 20020627 A 5230 DOOR AMD FALC20 FALCON 2720302 EU CARGO BAY OPEN E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 232TW 32 AIRCRAFT DEPARTED KDUJ EN ROUTE TO KMBS SHORTLY AFTER FLAP RETRACTION CARGO DOOR CAME OPEN. RETURNED TO DEPARTURE AIRPO RT. INSPECTED CARGO DOOR FOR OPERATION AND LOCKING, NO DEFECTS FOUND. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F A7EU 2002080100091 20020801 00091 NE 2002 8 1 00034 2 20020711 A 7200 ENGINE LEAR 25 25 5170506 CE GE CJ610 CJ6106 30006 NE RIGHT FLAMED OUT E HAEA B EMER. DESCENT X ENGINE FLAMEOUT CL CLIMB 1 SW 05 525TW 011 240102 AIRCRAFT EN ROUTE FROM ADDISON TX TO WINDSOR CANADA RT ENGINE FLAME-OUT CLIMBING FROM 390 TO 410. RESTART NORMAL, CLIMB BACK TO 410 AND CONTINUED TRIP. PILOT INSPECTED ENGINE FOR FOD DAMAGE AT DESTINATION, NO DAMAGE FOUND. AIRCRAFT MOVED TO MAINTENANCE BASE AT YIP. FLAME-OUT INSPECTIONS COMPLETED PER THE GE M/M, NO DEFECTS NOTED AT THIS TIME. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4J 4 J A10CE 1E16 2002080100092 20020801 00092 WP 2002 8 1 MWEA020420 1 20020608 A 2131 CONTROLLER DOUG DC9 DC932 3022066 WP CABIN PRESSURE MALFUNCTIONED A MWEA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 301ME 47190 PRESSURIZATION INOP DURING CLIMB, SWITCHED TO MANUALLY CONTROLLED PRESSURIZATION AT CRUISE ABOUT 10 MINUTES. CABIN WENT TO FULL CLIMB BUT COULD NOT BE CONTROLLED MANUALLY. INITIATED EMERGENCY DESCENT, HAD NORMAL PACK PRESSURE. DEFERRED P ER MEL 21-25 T FUNCTION COMPLIED WITH PLACARD INSTALLED BREAKERS PULLED AND COLLARED. OUTFLOW VALVE SECURED OPEN. 2 L 7 2 4F A6WE 2002080100093 20020801 00093 NM 2002 8 1 MWEA020424 1 20020619 A 5230 59562735 BRACKET DOUG MD88 MD88 3023688 NM CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 AFT CORNER ANGLE BRACKET IS CRACKED ON AFT CARGO DOOR HORIZONTAL SUPPORT FOR AFT HOLD OPEN HOOK. DRILLED UP CLIP. REMO VED AND REPLACED ANGLE BRACKET. 2 L 7 2 4F RT A6WE 2002080100094 20020801 00094 WP 2002 8 1 MWEA020425 1 20020620 A 2822 B19001 CIRCUIT BREAKER DOUG DC9 DC932 3022066 WP COCKPIT TRIPPED A MWEA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 204ME 47680 ON CLIMBOUT ALL LEFT MAIN FUEL TANK PUMP CIRCUIT BREAKERS POPPED. VISUALLY INSPECTED THE EXTERNAL POWER, GENERATOR AND CROSS TIE RELAYS. CHECKED CIRCUIT BREAKERS INSIDE EPC AND FOUND THE AIRPHONE CIRCUIT BREAKER HAD SIGNS OF ARCHING. AIR PHONES DEFERRED, PLACARDS INSTALLED, CIRCUIT BREAKERS PULLED AND COLLARD DMI 6-63. 2 L 7 2 4F A6WE 2002080100095 20020801 00095 WP 2002 8 1 MWEA020426 1 20020623 A 3260 833605 PROXIMITY SWITCH DOUG DC9 DC982 3022082 WP LANDING GEAR MALFUNCTIONED A MWEA K NONE N FALSE WARNING DE DESCENT 1 GL 31 809ME 48071 NOSE GEAR UNSAFE LIGHT ILLUMINATED. GEAR HANDLE UP, SPEED 250 KNOTS. THE NOSE GEAR UNSAFE LIGHT REMAINED ON UNTIL GEAR EXTENDED. NOTE: GEAR EXTENDED NORMALLY ALL THREE GREEN. NOTED PSEU FAILED SELF TEST, FAULTS PRESENT ON ALL LANDING GE AR CHANNELS. REMOVED AND REPLACED PROX BOX IAW MM 32-60-04. SWUNG GEAR SEVERAL TIMES, NO UNSAFE LIGHTS. OPS CHECKED G OOD. 2 L 7 2 4F A6WE 2002080100096 20020801 00096 WP 2002 8 1 MWEA020427 1 20020626 A 2741 CIRCUIT BREAKER DOUG DC9 DC932 3022066 WP COCKPIT FAILED A MWEA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 GL 31 602ME 48133 CREW NOTED PRIMARY TRIM WAS INOP. ALTERNATE TRIM WORKED NORMALLY. ALL SWITCHES AND CIRCUIT BREAKERS WERE IN NORMAL POS ITIONS. PERFORMED TROUBLESHOOTING PROCEDURES IAW MM 27-40-0. VERIFIED BAD PRIMARY LONGITUDINAL TRIM CONTROL CIRCUIT BR EAKER. REMOVED AND REPLACED CIRCUIT BREAKER IAW SWP 20-10-3. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002080100097 20020801 00097 WP 2002 8 1 MWEA020429 1 20020628 A 5310 3913662501 STOP FITTING DOUG DC9 DC932 3022066 WP FUSELAGE STRIPPED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 PAX JAMB DOOR STOP FITTING (THIRD FROM BOTTOM AFT JAMB) HAS STRIPPED OUT THREADS. REMOVED AND INSTALLED FITTING. 2 L 7 2 4F A6WE 2002080100098 20020801 00098 WP 2002 8 1 MWEA020430 1 20020628 A 5320 59560343 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FORWARD CARGO BAY HAS A CRACKED FITTING ON FRAME 503 AT LONGERON 28 RIGHT. REMOVED AND INSTALLED FITTING. 2 L 7 2 4F A6WE 2002080100099 20020801 00099 WP 2002 8 1 MWEA020431 1 20020628 A 5320 3913291501N SPLICE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 LONGERON SPLICE CRACKED AT FS415 AND 29 LEFT. FABRICATED AND INSTALLED SPLICE AND SHIMS. 2 L 7 2 4F A6WE 2002080100100 20020801 00100 WP 2002 8 1 MWEA020432 1 20020628 A 5320 5913537503 GUSSET DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 AFT PIT STRAP ON DOOR THRESHOLD CORRODED BETWEEN STATION 904 AND STATION 885 LONGERON 29 LEFT. REMOVED AND INSTALLED GU SSET. 2 L 7 2 4F A6WE 2002080100101 20020801 00101 WP 2002 8 1 MWEA020433 1 20020628 A 5330 5911412187 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FUSELAGE DENT AT STATION 353 1.5 INCH BELOW LONGERON 29 LEFT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002080100102 20020801 00102 WP 2002 8 1 MWEA020441 1 20020629 A 7933 CONNECTOR DOUG DC9 DC915 3022036 WP LT ENGINE FAULTY A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 900ME 45841 LEFT ENGINE OIL TEMPERATURE IS PEGGED. PRESSURE AND QUANTITY IS NORMAL PER QRH. ENGINE NOT SHUT DOWN WITHIN 15 MINUTE LIMIT WHEN AIRCRAFT LANDED AT MILWAUKEE. FUEL TEMPERATURE ALSO DID NOT INCREASE. REPAIRED AND REPLACED LEFT ENGINE OIL TEMPERATURE CONNECTOR AND TEMPERATURE BULB. 2 L 7 2 4F A6WE 2002080100103 20020801 00103 WP 2002 8 1 MWEA020443 1 20020706 A 2131 CONTROLLER DOUG DC9 DC932 3022066 WP CABIN PRESSURE OUT OF ADJUST A MWEA G O2 MASK DEPLOYED G MULTIPLE FAILURE CR CRUISE 1 GL 31 212ME 47102 AT 31,000 FEET THE AIRCRAFT LOST PRESSURE AND COULD NOT CONTROL IN AUTO OR MANUAL. MASKS AUTOMATICALLY DEPLOYED. PERFO RMED ADJUSTMENT / TEST CABIN PRESSURE CONTROL REFERENCE 21-32-0-201. NO DISCREPANCY NOTED. 2 L 7 2 4F A6WE 2002080100104 20020801 00104 WP 2002 8 1 MWEA020444 1 20020625 A 5311 5911448509 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FORWARD CARGO BAY FRAME AT STATION 446 LONGERON 30 IS EXFOLIATED. INSTALLED FRAME SECTION AND SPLICE. 2 L 7 2 4F A6WE 2002080100105 20020801 00105 WP 2002 8 1 MWEA020445 1 20020712 A 5720 991935027 STIFFENER DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 RIGHT WING LIGHT CORROSION ON UPPER SURFACE OF HORIZONTAL STIFFENER ON INBOARD SIDE OF XRS 91 RIB ABOVE STRINGERS 17 TO 19. REMOVED AND INSTALLED STIFFENER AND FLAPPER VALVE. 2 L 7 2 4F A6WE 2002080100106 20020801 00106 EA 2002 8 1 COMA0260462 1 20020731 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 409CA 7441 FLIGHT 6092 GEAR DISAGREE MESSAGE, MLG DID NOT EXTEND.COULD NOT DUPLICATE. LANDING GEAR EXTENSION AND RETRACTION CHECKS WERE 170R MAL. 2 L 7 2 4F RT A21EA 2002080100107 20020801 00107 2002 8 1 MWEA020448 4 20020716 A 3421 258733513 GYRO DOUG DC9 DC932 3022066 WP COCKPIT FAILED A MWEA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 GL 31 216ME 47740 CAPTAIN'S ATTITUDE INDICATOR FAILED. REMOVED AND REPLACED NR 1 VERTICAL GYRO. OPS CHECK OK REF MM 34-27-0. 2 L 7 2 4F A6WE 2002080100108 20020801 00108 WP 2002 8 1 MWEA020449 1 20020717 A 5713 59112802 STRINGER DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 RIGHT WING STRINGER 21 HAS LIGHT CORROSION ON UPPER AND LOWER AFT LEG BETWEEN XRS 91&111. BLENDED CORROSION OUT OF STRI NGER. 2 L 7 2 4F A6WE 2002080100109 20020801 00109 EA 2002 8 1 COMA0260463 1 20020730 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 712CA 7244 FLIGHT 5575 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.COULD NOT DUPLCITE. OPERATION OF CABIN DORO NORMAL. 2 L 7 2 4F RT A21EA 2002080100110 20020801 00110 WP 2002 8 1 MWEA020451 1 20020718 A 5320 5910163123 SPLICE PLATE DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT PRESSURE BULKHEAD PLUG DOOR JAMB HAS A CRACK AT APPROXIMATELY THE 6 O'CLOCK POSITION IN THE SPLICE PLATE CONNECTION. REMOVED AND INSTALLED SPLICE PLATE. 2 L 7 2 4F A6WE 2002080100111 20020801 00111 EA 2002 8 1 COMA0260464 1 20020731 A 2750 853D10018 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA R/H #3 BINDING A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 810CA 2616 7370 FLIGHT 5332 FLAPS FAIL CAUTION MESSAGE.REPLACED THE R/H #3 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2002080100112 20020801 00112 WP 2002 8 1 MWEA020452 1 20020718 A 3350 60030451 SWITCH DOUG DC9 DC932 3022066 WP COCKPIT FAULTY A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 216ME 47740 CABIN EMERGENCY LIGHTS, NO SMOKING LIGHTS AND FASTEN SEATBELT LIGHTS FLASHING ON AND OFF RAPIDLY. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT SWITCH AND B5-23 BATTERY PACK FOR PRECAUTION. 2 L 7 2 4F A6WE 2002080100113 20020801 00113 WP 2002 8 1 MWEA020454 1 20020723 A 5320 5910163108 CLIP DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 APB RADIAL NR 16 LEFT END CLIP HAS A CRACK AROUND END FASTENER HOLE. FABRICATED AND INSTALLED CLIP. 2 L 7 2 4F A6WE 2002080100114 20020801 00114 WP 2002 8 1 MWEA020458 1 20020716 A 5312 5910130387 TEE FITTING DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 AFT PRESSURE BULKHEAD TEE WAS DENTED BETWEEN LONGERONS 29 RIGHT AND 28 RIGHT. REMOVED TEE SECTION FROM LONGERON AND INS TALLED NEW TEE SECTION AND REPAIR SPLICES. 2 L 7 2 4F A6WE 2002080100115 20020801 00115 NM 2002 8 1 MWEA020460 1 20020717 A 5321 993655211 FLOOR PANEL DOUG MD88 MD88 3023688 NM FUSELAGE DETERIORATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 CABIN FLOOR IN FRONT OF FWD LAV SEEMS SOFT. FABRICATED AND INSTALLED FLOOR PANEL. 2 L 7 2 4F RT A6WE 2002080100116 20020801 00116 WP 2002 8 1 CALA0200433 1 20020730 A 5330 SKIN DOUG DC9 DC982 3022082 WP STA 712-731 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14831 49491 INSPECTION FOUND LOWER FUSELAGE SKIN CORRODED BETWEEN STA 712 AND 731, LONGERONS 29R-30. A REPAIR DOUBLER AND TRIPLER WE RE INSTALLED IAW ECRA 5331-01116. 2 L 7 2 4F A6WE 2002080100117 20020801 00117 WP 2002 8 1 CALA0200434 1 20020731 A 5532 SKIN DOUG DC9 DC982 3022082 WP LH VERT STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14831 49491 INSPECTION FOUND THAT THE LEADING EDGE OF BOTTOM L/H BANANA FAIRING HAD GOUGED SKIN OF VERTICAL STABILIZER. THE LEADING EDGE PLATING WAS REMOVED AND REPLACED IAW SRM 53-30-0. 2 L 7 2 4F A6WE 2002080100118 20020801 00118 WP 2002 8 1 CALA0200435 1 20020731 A 5210 SKIN DOUG DC9 DC982 3022082 WP MCD CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14831 49491 INSPECTION FOUND A 0.44" CRACK IN SKIN AT BOTTOM EDGE OF MAIN CABIN DOOR. THE CRACK WAS LOCATED APPROXIMATELY 16 INCHES AFT OF FORWARD EDGE. A REPAIR WAS INSTALLED IAW ECRA 5210-01478. 2 L 7 2 4F A6WE 2002080100119 20020801 00119 NM 2002 8 1 QXEA021099 1 20020731 A 7330 MS280343 SENSOR DHAV DHC8 DHC8202 2809007 NM ZONE 400 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 375PH 529 PDX - AIRCRAFT RETURNED TO FIELD WHEN ON CLIMBOUT THE NUMBER 2 ENGINE FUEL TEMP GAUGE FLUCTUATED BETWEEN 60 AND 80 DEGRE ES. TEMPERATURE GAUGE INDICATED NORMAL ON GROUND. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NUMBER 2 FUEL TEMP ERATURE BULB. OPERATIONAL CHECKS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080100120 20020801 00120 EU 2002 8 1 AWXA200200687 1 20020725 A 3350 D9292214800000 CABLE AIRBUS 320 A320231 3930325 EU SEAT ROWS 9&11R CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 643AW 0 0 315 YWG - EEL - DURING C-08 CHECK EMERGENCY ESCAPE PATH LIGHT CABLES WERE FOUND CUT AND CHAFED AT SEAT ROWS 26 L/H, 9 R/H, A ND 11 R/H. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CABLES AT SEAT ROWS 26 L/H, 9 R/H, AND 11 R/H PE R ESPM 20-33-10, OPERATIONAL TEST WAS GOOD IAW AMM 33-51-00-710-001. 2 L 7 2 4F RT A28NM 2002080100121 20020801 00121 WP 2002 8 1 P2EA2002V0040 1 20020729 A 5330 STIFFENER DOUG DC9 DC982 3022082 WP CRACKED A P2EA O OTHER O OTHER UK UNKNOWN 1 CE 05 140NJ 49931 AFTER HARD LANDING INSPECTION:-AFT FUSELAGE Sta.Y=1380, APU INTERNAL COVER LOWER SECTION ( +X4 & -X4 ) STIFFENERS CRACKE D.-REPAIRED STIFFENERS 2ea ON +X4 & -X4 BETWEEN -Z10 & -Z23 DUE TO CRACKS IAW SRM 53-02 FIG 18.NOTE: SEE COOPESA´S WORK ORDER No. P10701,1-19, VAM 100 No. 035 & 140SDA007. 2 L 7 2 4F A6WE 2002080100122 20020801 00122 WP 2002 8 1 P2EA2002V0041 1 20020731 A 5340 ANGLE DOUG DC9 DC982 3022082 WP CRACKED A P2EA O OTHER O OTHER LD LANDING 1 CE 05 140NJ 49931 AFTER HARD LANDING INSPECTION:-AFT FUSELAGE, Sta Y1345, LOWER SECTION AT -Z37, BETWEEN -X14 TO +X13, ANGLE BENDED & CRAC KED.-REPAIRED APU ENCLOSURE ANGLE IN Sta Y1345 BETWEEN +X9 & +X17 AND BETWEEN -X8 & -X16, -Z33 & -Z37 DUE TO CRACK, IAW COOPESA E.O. No.COO-9-53-408-02, DATED JULY 22,2002. DOCUMENTED IN FAA 8110-3 FORM.Note: SEE COOPESA´S WORK ORDER No.PI0 701,1-30, VAM100No.036 & 140SDA008. 2 L 7 2 4F A6WE 2002080100123 20020801 00123 WP 2002 8 1 P2EA2002V0044 1 20020730 A 5310 SKIN DOUG DC9 DC982 3022082 WP WORN A P2EA O OTHER O OTHER LD LANDING 1 CE 05 140NJ 49931 AFTER HARD LANDING INSPECTION:-AFT FUSELAGE, LOWER SECTION Sta Y1380, BETWEEN +X12 AND +X14, SKIN PANEL WITH WEAR.-FUSEL AGE SKIN PANEL REPAIRED FROM Sta Y1380 TO Y1384, BETWEEN +X12 AND +X16.750, AT -Z37 DUE TO WEAR IAW COOPESA E.O.# COO-9- 53-392-02, DATED JULY 15,2002, DOCUMENTED ON FAA 8110-3 FORM.Note: SEE COOPESA´S WORK ORDER No.P10701,1-47, VAM100 No.05 3 AND 140SDA011. 2 L 7 2 4F A6WE 2002080100124 20020801 00124 WP 2002 8 1 P2EA2002V0045 1 20020731 A 5310 SKIN DOUG DC9 DC982 3022082 WP WORN A P2EA O OTHER O OTHER LD LANDING 1 CE 05 140NJ 49931 AFTER HARD LANDING INSPECTION:-AFT FUSELAGE, FROM Sta Y1338 TO Y1344, BETWEEN LONG 28 R-H TO 28 L-H, SKIN PANEL WITH WEA R.-FUSELAGE SKIN PANEL REPAIRED FROM STA Y1338 TO STA Y1344.250, BETWEEN LONG 27L-H TO 27R-H DUE TO WEAR IAW COOPESA E.O . No. COO-9-53-392-02, DATED JULY 15,2002 AND DOCUMENTED ON FAA 8110-3 FORM.Note: SEE COOPESA´S WORK ORDER No.P10701,1-4 9, VAM100 No.055 & 140SDA012. 2 L 7 2 4F A6WE 2002080100125 20020801 00125 WP 2002 8 1 P2EA2002V0046 1 20020801 A 5310 SKIN DOUG DC9 DC982 3022082 WP WORN A P2EA O OTHER O OTHER LD LANDING 1 CE 05 140NJ 49931 AFTER HARD LANDING INSPECTION:-AFT FUSELAGE, FROM Sta Y1331 TO Y1338, BETWEEN LONGERONS 29R-H & 29L-H, SKIN WITH WEAR.-F USELAGE SKIN PANEL REPAIRED FROM Sta Y1315.5 TO Y1338 BETWEEN LONGERONS 27L-H TO 27R-H DUE TO WEAR IAW SRM 53-04 FIG 12C .Note: SEE COOPESA´S WORK ORDER No.P10701,1-54, VAM100 No.060 & 140SDA013. 2 L 7 2 4F A6WE 2002080100126 20020801 00126 WP 2002 8 1 P2EA2002V0047 1 20020801 A 5310 SKIN DOUG DC9 DC982 3022082 WP BENT A P2EA O OTHER O OTHER LD LANDING 1 CE 05 140NJ 49931 AFTER HARD LANDING INSPECTION:-AFT FUSELAGE, Sta Y1405 L-H SIDE, VENTRAL STAIR JAMB, SKIN PANEL BENT.-FUSELAGE SKIN PANE L REPAIRED FROM Sta Y1401 TO Y1408.5 BETWEEN +X16 & +X24.5, -Z37 DUE TO BENT IAW COOPESA E.O.No.COO-9-53-409-02 DATED JU LY 22,2002 AND DOCUMENTED ON FAA 8110-3 FORM.Note: SEE COOPESA´S WORK ORDER No. P10701,1-56, VAM100 No.062 & 140SDA014. 2 L 7 2 4F A6WE 2002080100127 20020801 00127 WP 2002 8 1 P2EA2002V0048 1 20020801 A 5311 FRAME DOUG DC9 DC982 3022082 WP BENT A P2EA O OTHER O OTHER LD LANDING 1 CE 05 140NJ 49931 AFTER HARD LANDING INSPECTION:-AFT FUSELAGE Sta Y1380 BETWEEN LONGERONS 23 & 24 R-H SIDE WEB FRAME BENT.-WEB FRAME REPAI RED IN Sta 1380, BETWEEN LONGERONS 23 & 24 R-H SIDE IAW SRM 51-70-4 FIG 1.Note: SEE COOPESA´S WORK ORDER No. P10701,1-70 , VAM 100 No. 079 & 140SDA015. 2 L 7 2 4F A6WE 2002080100128 20020801 00128 SO 2002 8 1 C2XA02TY116 1 20020801 A 5315 14522460005 GUSSET EMB 135 EMB135LR 3260305 SO FWD GALLEY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24517 145332 TYS DURING A SCHEDULED 1-C INSPECTION THE AFT GUSSET IN THE GALLEY WAS FOUND CORRODED. MAINTENANCE R/R THE AFT GUSSET I AW 135/145 SRM 51-40-02.R/R SCREWS IAW EMB 135/14553-01-06. ALL WORK WAS ACCOMPLISH AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002080200001 20020802 00001 EU 2002 8 2 00035 1 20020618 A 3411 PITOT TUBE AMD FALC20 FALCON 2720302 EU COCKPIT OBSTRUCTED E HAEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 05 977TW 13 AIRCRAFT STARTED TAKEOFF ROLL AT ADS, COPILOTS AIRSPEED INDICATOR DID NOT COME ALIVE. TAKEOFF ROLL ABORTED. BLOCKAGE F OUND IN COPILOTS PITOT TUBE. REPAIRED AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F A7EU 2002080200002 20020802 00002 EU 2002 8 2 00036 1 20020729 A 3260 SQUAT SWITCH AMD FALC20 FALCON 2720302 EU LANDING GEAR OUT OF ADJUST E HAEA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 240TW 40 AIRCRAFT DEPARTED KYIP, DURING CLIMB AIRCRAFT NOT PRESSURIZING, RETURN TO KYIP. MAINTENANCE FOUND SQUAT SWITCH OUT OF A DJUSTMENT. ADJUSTED PER MM, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F A7EU 2002080200004 20020802 00004 SO 2002 8 2 C2XA02CL151 1 20020716 A 3234 7455501 CONTROL HANDLE EMB 145 EMB145LR 3260212 SO COCKPIT INTERMITTENT A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13979 6745 145181 CLE FLIGHT 3051 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM CLEVELAND. THE AIRCRAFT RETURNE D TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL ASSEMBL Y. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002080200005 20020802 00005 SO 2002 8 2 C2XA02CL152 1 20020715 A 4920 4504113 APU EMB 145 EMB145LR 3260212 SO APU BAY BURNED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 16918 2551 145397 MEM FLIGHT 4067 THE CREW REPORTED A APU FIRE INDICATION ON SHORT FINAL FOR 10 SECONDS. MAINTENANCE REPLACED THE APU. O PERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002080200006 20020802 00006 GL 2002 8 2 C2XA02CL155 2 20020726 A 7313 3035060 FUEL NOZZLE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 ENGINE COKED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 16999 145307 CLE FLIGHT 3244 THE CREW REPORTED A PUNGENT SMELL IN THE CABIN DURING ICE PROTECTION SYSTEM OPERATION. MAINTENANCE INSP ECTED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002080200007 20020802 00007 SO 2002 8 2 C2XA02CL156 1 20020728 A 3234 7455501 CONTROL HANDLE EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 16954 145072 CLE FLIGHT 3280 THE CREW REPORTED THE LANDING GEAR LEVER WOULD NOT MOVE INTO THE UP POSITION AFTER TAKEOFF. THE DOWNLOC K RELEASE OVERRIDE WAS USED AND THE GEAR WAS RETRACTED. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER. OPERATION AL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002080200008 20020802 00008 SO 2002 8 2 C2XA02IA129 1 20020614 A 2120 ODOR EMB 135 EMB135LR 3260305 SO COCKPIT DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 27 16525 145403 CLE- FLIGHT 4138, AFTER LANDING THE CREW NOTED THAT THERE WAS A FUEL SMELL IN THE COCKPIT. MAINTENANCE PERFORMED AN AI R BLEED SYSTEM OPERATIONAL CHECK, NO DEFECTS NOTED, COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080200009 20020802 00009 EU 2002 8 2 C2XA02IA130 1 20020623 A 5220 MS212513S TURNBUCKLE AEROSP ATR42 ATR42320 8680930 EU EMERGENCY EXIT BENT A C2XA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 27 14825 170 IAH - DURING TAKEOFF ROLL THE LEFT FORWARD EMERGENCY EXIT DOOR CAME DISLODGED. THE CREW ABORTED THE TAKEOFF AND RETURNE D TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE DOOR AND FOUND THE SHOOT BOLT ACTUATING TURNBUCKLE TO BE BENT . THE TURNBUCKLE WAS REMOVED AND REPLACED, AND THE DOOR WAS FUNCTIONALLY CHECKED. THE AIRCRAFT WAS THEN RETURNED TO SE RVICE. 2 H 7 2 4T RT A53EU 2002080200010 20020802 00010 SO 2002 8 2 C2XA02IA131 1 20020623 A 3260 852701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO NLG MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 15986 145254 IAH- FLIGHT 3809, L/G / AIR GROUND FAILED AT ROTATION. MAINTENANCE REMOVED AND REPLACED THE WOW PROX SWITCH, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002080200011 20020802 00011 EU 2002 8 2 C2XA02IA132 1 20020624 A 3350 44 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14828 179 IAH- WHILE PERFORMING A 4A CHECK THE MECHANIC NOTED THAT THE PAX DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. MAINTENANC E REMOVED AND REPLACED THE LIGHT BULB, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE WHEN RELEASED FROM 4A CHECK. 2 H 7 2 4T RT A53EU 2002080200012 20020802 00012 EU 2002 8 2 C2XA02IA133 1 20020630 A 7603 CONTROL CABLE AEROSP ATR42 ATR42320 8680930 EU NR 2 THROTTLE LACK OF LUBE A C2XA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 27 14819 156 IAH- FLIGHT 3581, THE CREW NOTED THAT THE NUMBER TWO (2) POWER LEVER WAS BINDING ON TAKEOFF ROLL. THE CREW ABORTED TAK EOFF. MAINTENANCE INSPECTED THE POWER LEVER QUADRANT AND FOUND NO OBSTRUCTION AT THE CONSOLE. INSPECTED THE ENGINE POW ER LEVER QUADRANT AND FOUND NO OBSTRUCTIONS. LUBED CABLE ASSY INSIDE AND OUT, NO BINDING AT THIS TIME. THE AIRCRAFT WA S APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080200013 20020802 00013 SO 2002 8 2 C2XA02IA134 1 20020628 A 3350 82308 CONNECTOR EMB 145 EMB145 3260210 SO CABIN LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13964 145123 IAH- THE CREW NOTED THAT THE FORWARD EXIT EMERGENCY LIGHT INTERMITTENT. MAINTENANCE SECURED A LOOSE CONNECTOR ON THE E MERGENCY EXIT LIGHT ASSY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080200014 20020802 00014 SO 2002 8 2 C2XA02IA135 1 20020630 A 3230 23092900001 UPLOCK EMB 145 EMB145 3260210 SO NLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16963 145116 IAH- FLIGHT 3815, THE CREW NOTED THAT THE NOSE LANDING GEAR DID NOT RETRACT. THE CREW RETURNED TO IAH WITHOUT INCIDENT . MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK BOX. PERFORMED A OPERATIONAL CHECK, AND A LEAK CHECK, NO DEFECTS NOT ED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080200015 20020802 00015 SO 2002 8 2 C2XA02IA136 1 20020702 A 3230 23092900001 UPLOCK EMB 145 EMB145LR 3260212 SO RT MLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14953 145071 EWR- FLIGHT 4161, THE CREW NOTED THAT THE LANDING GEAR DISAGREEMENT LIGHT ILLUMINATED FOR THE RIGHT MAIN GEAR. THE CRE W RETURNED TO EWR WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN GEAR UPLOCK BOX, PERFORMED A OPERAT IONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002080200016 20020802 00016 EU 2002 8 2 C2XA02IA137 1 20020703 A 3230 1005383Y00 CONTROL VALVE AEROSP ATR42 ATR42320 8680930 EU LT MLG MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 99838 259 IAH- FLIGHT 3806, WHILE PREPARING TO LAND AT IAH THE CREW NOTED THAT THE LANDING GEAR FAILED TO EXTEND WHEN THE GEAR WA S SELECTED TO THE DOWN POSITION, THE HANDLE WAS RECYCLED FIVE (5) TIMES, THE CIRCUIT BREAKER WAS RESET, NO EFFECT. THE CREW USED EMERGENCY EXTENSION OF THE LANDING GEAR AND LANDED AT IAH WITHOUT INCIDENT. EMERGENCY WAS DECLARED. MAINTENA NCE REMOVED AND REPLACED THE LANDING GEAR CONTROL VALVE, PERFORMED A OPERATIONAL CHECK AND A LEAK CHECK, NO DEFECTS NOTE D. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080200017 20020802 00017 EU 2002 8 2 C2XA02IA138 1 20020703 A 3260 D228780001 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU NLG MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 99838 259 IAH- FLIGHT 3806, WHILE PREPARING TO LAND AT IAH, THE CREW NOTED THAT THE LANDING GEAR FAILED TO EXTEND WHEN THE GEAR W AS SELECTED TO THE DOWN POSITION, THE HANDLE WAS RECYCLED FIVE (5) TIMES, THE CIRCUIT BREAKER WAS RESET, NO EFFECT. THE CREW USED EMERGENCY EXTENSION OF THE LANDING GEAR AND LANDED AT IAH WITHOUT INCIDENT. EMERGENCY WAS DECLARED. MAINTEN ANCE REMOVED AND REPLACED THE NOSE LANDING GEAR PROX SWITCH, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, N O DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080200018 20020802 00018 EU 2002 8 2 C2XA02IA139 1 20020707 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 21837 202 IAH- WHILE PERFORMING MAINTENANCE THE MECHANIC NOTED THAT THE PAX DOOR GROUND EMERGENCY LIGHT FAILED TO ILLUMINATE. MAI NTENANCE REMOVED AND REPLACED THE PAX DOOR GROUND EMERGENCY LIGHT ASSEMBLY. PERFORMED A OPERATIONAL CHECK OF THE EMERGE NCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080200019 20020802 00019 SO 2002 8 2 C2XA02IA141 1 20020710 A 3350 BC10020002 LIGHT EMB 145 EMB145ER 3260211 SO EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15926 145005 IAH- DURING MAINTENANCE THE MECHANIC NOTED THAT THE RIGHT HAND FORWARD WING EMERGENCY LIGHT FAILED TO ILLUMINATE. MAIN TENANCE REMOVED AND REPLACED THE RIGHT HAND FORWARD WING EMERGENCY LIGHT ASSEMBLY. PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080200020 20020802 00020 EU 2002 8 2 C2XA02IA142 1 20020711 A 3230 70204 CONNECTOR AEROSP ATR42 ATR42320 8680930 EU NLG CONTAMINATED A C2XA K NONE O OTHER CL CLIMB 1 SW 27 14819 156 IAH- FLIGHT 3821, WHEN GEAR IS RETRACTED LOUD THUMPING IS HEARD FROM ALL THREE (3) WHEELS. GEAR DOES NOT RETRACT FULLY , EVEN AFTER THIRTY (30) SECONDS AND FLAPS DO NOT COME UP AS WELL. WHEN HANDLE IS CYCLED GEAR FALLS WITH LOUD THUMP. W HEN RETRACTED FOR THE SECOND TIME SAME THUMPING, BUT EVENTUALLY DOES RETRACT. MAINTENANCE CLEANED MOISTURE AND DEBRIS F ROM NOSE WHEEL WELL INTERCONNECT CANNON PLUG. PERFORMED GEAR SWING, OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080200021 20020802 00021 EU 2002 8 2 C2XA02IA143 1 20020712 A 3297 D227010001 WIRE HARNESS AEROSP ATR42 ATR42320 8680930 EU NLG CHAFED A C2XA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 27 14819 156 IAH- DURING PREFLIGHT THE CREW NOTED THAT THE NOSE GEAR UNLOCK INDICATION ON THE OVERHEAD PANEL ILLUMINATED. MAINTENANC E REMOVED AND REPLACED THE NOSE LANDING GEAR WIRE HARNESS, VERIFIED NORMAL OPERATION AND NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080200022 20020802 00022 SO 2002 8 2 C2XA02IA144 1 20020718 A 3230 355022002MOD2 CONTROL UNIT EMB 145 EMB145ER 3260211 SO COCKPIT MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14937 145026 IAH- FLIGHT 3935, DURING CLIMB THE CREW NOTED THAT THE GEAR WOULD NOT RETRACT AS SELECTED, GEAR HANDLE DISAGREE. THE C REW RETURNED THE GEAR HANDLE TO THE DOWN POSITION AND RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACE D THE LANDING GEAR ELECTRONIC UNIT IAW EMB 145 MM 32-32-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080200023 20020802 00023 SO 2002 8 2 C2XA02IA145 1 20020718 A 5610 163500111 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT CRACKED A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 14543 145553 MCI- DURING FLIGHT 3843, THE CAPT OUTER PANE WINDSHIELD SHATTERED. THE CREW DECLARED AN EMERGENCY, DIVERTED TO MCI AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPT WINDSHIELD IAW EMB 145 AMM 56-10-01 AND THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002080200025 20020802 00025 EU 2002 8 2 C2XA02IA149 1 20020724 A 3350 10155651 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN OUT OF POSITION A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14821 160 IAH- WHILE PERFORMING A 3A CHECK IT WAS NOTED THAT THE EMERGENCY LIGHT FLOOR STRIP HAS A LIGHT OUT AT SEAT 3AB. MAINTE NANCE REPOSITIONED THE CABIN FLOOR EMERGENCY LIGHT STRIP, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM , NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080200026 20020802 00026 SO 2002 8 2 C2XA02IA150 1 20020727 A 3620 0132ADT SENSOR EMB 145 EMB145LR 3260212 SO CARGO BAY FAULTY A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 15983 145239 IAH- FLIGHT 4127, THE CREW NOTED THAT NR 2 BLEED OVERTEMP LIGHT ILLUMINATED INFLIGHT. THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 BLEED TEMP SENSOR, IN THE CARGO COMPARTMENT IAW EMB 14 5 MM 36-11-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002080200027 20020802 00027 SO 2002 8 2 C2XA02IA151 1 20020727 A 3620 0132ADT SENSOR EMB 145 EMB145LR 3260212 SO NR 2 PYLON FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 15983 145239 IAH- FLIGHT 4127, THE CREW NOTED THAT NR 2 BLEED OVERTEMP LIGHT ILLUMINATED INFLIGHT. THE CREW RETURNED THE AIRCRAFT T O IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 BLEED TEMP SENSOR IN THE NR 2 PYLON IAW EMB 145 MM 36 -11-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002080200028 20020802 00028 SO 2002 8 2 C2XA02IA152 1 20020727 A 3350 7287580501 CONNECTOR EMB 145 EMB145ER 3260211 SO CABIN LOOSE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 14937 145026 IAH - CREW REPORTED THAT ONE OF THE FLOOR PROXIMITY EMERGENCY LIGHT STRIPS DID NOT ILLUMINATE. MAINTENANCE INSPECTED TH E AIRCRAFT AND FOUND THE NR 3 FLOOR STRIP CONNECTOR TO BE LOOSE. THE CONNECTOR WAS RESECURED, THE FLOOR STRIP OPERATION ALLY CHECKED GOOD, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080200029 20020802 00029 SO 2002 8 2 C2XA02IA153 1 20020727 A 3350 LIGHT EMB 145 EMB145ER 3260211 SO CABIN MALFUNCTIONED A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 14937 145026 MEM - CREW REPORTED THAT THE EMERGENCY LIGHTING STAYED ON WITH SWITCH SELECTED TO THE OFF POSITION. AN ELECTRICAL RESET OF THE SYSTEM WAS ACCOMPLISHED AND THE EMERGENCY LIGHTING SYSTEM OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2002080200030 20020802 00030 SO 2002 8 2 C2XA02IA154 1 20020728 A 3350 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14938 145029 DURING PREFLIGHT THE CREW NOTED THAT THE CABIN DOOR AND ROW TWELVE (12) WINDOW EXIT EMERGENCY LIGHTING FAILED TO ILLUMIN ATE. 2 L 7 2 4F RT T00011AT 2002080200031 20020802 00031 SO 2002 8 2 C2XA02SH012 1 20020618 A 5315 14522461001 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 SHV- DURING C-CK INSPECTION, THE RIGHT HAND INBOARD FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF FLOORBEAM IAW EMB-145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4F RT T00011AT 2002080200034 20020802 00034 SO 2002 8 2 C2XA02SH016 1 20020621 A 5315 14530633003 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 SHV - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE R EMOVED THE DAMAGED SECTION OF OMEGA BEAM AND INSTALLED A REPAIR DOUBLER IN ACCORDANCE WITH EMB-145 SRM 53-22-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080200035 20020802 00035 SO 2002 8 2 C2XA02SH017 1 20020621 A 5315 14523186001 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 SHV - DURING C-CK INSPECTION, THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 & 25. MAINTENANCE REM OVED THE DAMAGED SECTION OF THE OMEGA BEAM AND INSTALLED A REPAIR DOUBLER IN ACCORDANCE WITH EMB-145 SRM 53-21-10, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080200036 20020802 00036 SO 2002 8 2 C2XA02SH018 1 20020618 A 5315 14521713003 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 SHV - DURING C-CHECK INSPECTION, THE LEFT HAND INBOARD OMEGA BEAM LOWER FLANGE WAS FOUND TO BE CORRODED BETWEEN FRAMES 2 2 & 23. MAINTENANCE REMOVED THE DAMAGED SECTION OF FLANGE AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-01219, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080200037 20020802 00037 SO 2002 8 2 C2XA02SH019 1 20020622 A 5315 14500095003 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 SHV - DURING C-CHECK INSPECTION, THE RT OUTBOARD OMEGA BEAM AT FRAME 55 WAS FOUND TO BE CORRODED AROUND A SCREW HOLE. M AINTENANCE REMOVED THE CORRODED SECTION AND INSTALLED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERIN G CHANGE AND REPAIR AUTHORIZATION EC5320-01065, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080200038 20020802 00038 SO 2002 8 2 C2XA02SH020 1 20020622 A 5315 14500094001 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 27 15932 145015 SHV - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM AT FRAME 59 WAS FOUND TO BE CORRODED AROUND A NUT PLATE. MAINTEN ANCE REMOVED THE CORROSION AND INSTALLED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5320-01065 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080200039 20020802 00039 SO 2002 8 2 C2XA02SH022 1 20020708 A 3350 1317 LIGHT EMB 145 EMB145ER 3260211 SO EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15932 145015 SHV - DURING C-CHECK INSPECTION, THE SERVICE DOOR EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFFECTED LIGHT BULB AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080200040 20020802 00040 SO 2002 8 2 C2XA02SH023 1 20020713 A 5315 14521713005 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 SHV - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 16 AND 25. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED SECTION OF OMEGA BEAM IN ACCORDANCE WITH EMB-145 SRM 51-20-03, AND 51-40-02. 2 L 7 2 4F RT T00011AT 2002080200041 20020802 00041 SO 2002 8 2 C2XA02SH024 1 20020710 A 5320 14520600003 CROSSBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 SHV - DURING C-CHECK INSPECTION, THE CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED CROSS BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080200042 20020802 00042 CE 2002 8 2 2002F00779 1 20020516 A 2913 11438800013 POWERPACK BEECH 1900 1900D 1154162 CE LANDING GEAR MALFUNCTIONED A AMWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 233YV UE233 AIRCRAFTS LEFT MAIN LANDING GEAR WOULD NOT RETRACT ON CLIMB-OUT. THE MAIN GEARS WAS THEN HAND PUMPED DOWN UNTIL THREE G REENS WERE INDICATED. RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE FOR AIR MIDWEST REMOVED AND REPLACED THE HYDRAULIC POWER PACK FOR CORRECTIVE ACTIVE. (M) 2 L 7 2 4T RT A24CE 2002080200043 20020802 00043 NM 2002 8 2 A6WA200230012 1 20020626 A 2120 SMOKE DORNER DO32 DO328100 2996000 NM COCKPIT DETECTED A A6WA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 340PH 3064 DURING ENGINE START, CREW REPORTS SMOKE IN COCKPIT. MAINTENANCE GROUND RAN ENGINES, PERFORMED CHECKS OF ECS. ALL OPERA TE NORMAL. (M) 2 H 7 2 4T RT A45NM 2002080200044 20020802 00044 NM 2002 8 2 AALA20020769 1 20020523 A 3350 S283T0143 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 NM 01 374AA 25201 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS ROW 26H AND AFT INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002080200045 20020802 00045 NM 2002 8 2 AALA20020770 1 20020516 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHT ABOVE R3 DOOR INOPERATIVE. REPLACED BATTERY PACK AT R3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002080200046 20020802 00046 NM 2002 8 2 AALA20020771 1 20020519 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 330AA 22330 BOS - DURING OVERNIGHT MAINTENANCE, FOUND FORWARD RIGHT EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPAIRED BROKEN WIR E FOR FORWARD RIGHT EMERGENCY ESCAPE PATH LIGHTING PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002080200047 20020802 00047 NM 2002 8 2 ASAA0270005 1 20020520 A 3350 D71702001 POWER SUPPLY BOEING 737 737790 13844CN NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 615AS 30344 SEA - DURING MAINTENANCE CHECK, FOUND FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY. EMERG ENCY LIGHTS THEN FUNCTIONED PROPERLY. (M) 2 L 7 2 4F RT A16WE 2002080200048 20020802 00048 WP 2002 8 2 ASAA0280158 1 20020502 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 PDX - DURING PREFLIGHT CHECK, FOUND INOPERATIVE EMERGENCY TRACK LIGHTING IN 1ST CLASS CABIN. RESECURED LOOSE ELECTRICAL CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002080200049 20020802 00049 NE 2002 8 2 ASAA0280176 2 20020511 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217 52053 NE RIGHT FAILED A ASAA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 NM 01 972AS 53448 P725732D SEA - DURING CLIMB, EXPERIENCED RIGHT ENGINE INTERNAL FAILURE, SUSPECT BIRD STRIKE. FIRST INDICATION JOLT OCCURRED AT 2 00 FT, WITH OBVIOUS FAILURE OCCURRING AT 29,000 FT. PERFORMED AIR TURNBACK, RETURNING TO SEA. REPLACED ENGINE. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002080200050 20020802 00050 WP 2002 8 2 ASAA0280177 1 20020516 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN MALFUNCTIONED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 SEA - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT WOULD NOT EXTINGUISH. REPLACED PORTABLE LIGHT ASSEMBLY. OP TES TED OK. (M) 2 L 7 2 4F RT A6WE 2002080200051 20020802 00051 NM 2002 8 2 ASAA0280178 1 20020516 A 3350 0105606 MODULE DOUG MD80 MD83 3023681 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 981AS 53472 PDX - DURING LINE CHECK, DISCOVERED EMERGENCY TRACK LIGHTS AT ROW 10-15 WERE INOPERATIVE. RECONNECTED LAMP HOLDER MODUL E. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT 2002080200052 20020802 00052 WP 2002 8 2 ASAA0280179 1 20020516 A 3397 0105606 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 FAI - DURING PREFLIGHT CHECK, DISCOVERED EMERGENCY TRACK LIGHTS AT ROW 2-9 WERE INOPERATIVE. REPLACED AND RESPLICED CON NECTOR WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002080200053 20020802 00053 WP 2002 8 2 ASAA0280180 1 20020517 A 5753 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OAK - DURING C-CHECK, DETERMINED RIGHT OUTBOARD FLAP SKIN TEMP REPAIR REQUIRED REPLACEMENT WITH PERMANENT REPAIR. REPLA CED TEMP REPAIR DOUBLER WITH PERMANENT REPAIR DOUBLER PER EA 5750-01526 REV B. (M) 2 L 7 2 4F RT A6WE 2002080200054 20020802 00054 WP 2002 8 2 ASAA0280181 1 20020518 A 5610 59644202 MECHANISM DOUG DC9 DC983 3022083 WP COCKPIT WINDOW LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 28276 53451 PDX - DURING PREFLIGHT CHECK, THE FIRST OFFICER'S SLIDING CLEARVIEW WINDOW DIFFICULT TO OPEN. LUBRICATED WINDOW MECHANI SM. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002080200055 20020802 00055 WP 2002 8 2 ASAA0280182 1 20020518 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 PDX - DURING LINE CHECK, FOUND INOPERATIVE EMERGENCY TRACK LIGHTING IN 1ST CLASS CABIN. RESECURED LOOSE ELECTRICAL CONN ECTION. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002080200056 20020802 00056 WP 2002 8 2 ASAA0280183 1 20020520 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING PREFLIGHT CHECK, FORWARD 1ST CLASS EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. SECURED FIRST CLA SS TRACK LIGHTING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002080200057 20020802 00057 WP 2002 8 2 ASAA0280184 1 20020521 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING LINE CHECK, 1ST CLASS EMERGENCY TRACK LIGHTING ROWS 1-4 WERE FOUND TO BE INOPERATIVE. SECURED FIRST CLASS TRACK LIGHTING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002080200058 20020802 00058 WP 2002 8 2 ASAA0280185 1 20020521 A 4990 3812761 SWITCH DOUG DC9 DC983 3022083 WP APU LEAKING A ASAA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 01 976AS 27079 188 53452 LAX - SMOKE AND FUMES WERE NOTED IN CABIN SHORTLY AFTER TAKEOFF. FIRE ALARMS ANNUNCIATED. REPLACED LEAKING LOP SWITCH ON APU. SUBSEQUENT OPERATION CAUSED NO FUMES OR SMOKE. (M) 2 L 7 2 4F RT A6WE 2002080200059 20020802 00059 NM 2002 8 2 ASAA0280186 1 20020520 A 5320 SR095200089 SPACER DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 PAE - DURING C-CHECK, FOUND CORROSION ON AFT CARGO BAY THRESHOLD SPACER AT FS 1160-1207. REPAIRED PER EO 5300-0101. (M ) 2 L 7 2 4F RT 2002080200060 20020802 00060 2002 8 2 ASAA0280187 4 20020522 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DETACHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 SAN - DURING PREFLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. ATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2002080200061 20020802 00061 NM 2002 8 2 ASAA0280188 1 20020523 A 5210 5910081 SKIN DOUG MD80 MD83 3023681 NM PAX DOOR BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 PAE - DURING C-CHECK, FOUND FORWARD PAX ENTRANCE DOOR SKIN BENT ALONG FORWARD BOTTOM EDGE. REPAIRED PER SRM 52-05, FIG 37. (M) 2 L 7 2 4F RT 2002080200062 20020802 00062 WP 2002 8 2 ASAA0280189 1 20020524 A 5310 5936038501 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OAK - DURING C-CHECK, AFT CARGO BAY DOOR JAMB BEAM WAS FOUND TO BE CORRODED ON HORIZONTAL AND VERTICAL LEGS FROM FS 1155 -1212. REPLACED DOOR JAMB BEAM PER SRM'S 51-10-3, 51-30-2, AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002080200063 20020802 00063 NM 2002 8 2 ASAA0280190 1 20020524 A 5310 5936038501 DOOR FRAME DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 PAE - DURING C-CHECK, FOUND MID CARGO BAY LOWER DOOR BEAM TO BE CORRODED ON VERTICAL FACE AND LOWER HORIZONTAL LUG. REP AIRED PER EA 5310-02090. (M) 2 L 7 2 4F RT 2002080200064 20020802 00064 WP 2002 8 2 ASAA0280191 1 20020528 A 5313 5936037501 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OAK - DURING C-CHECK, FOUND PITTING CORROSION ON LONGERON 29R, AFT CARGO BAY DOOR BEAM. REPLACED BEAM PER SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002080200065 20020802 00065 WP 2002 8 2 ASAA0280192 1 20020524 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING LINE CHECK, DISCOVERED EMERGENCY TRACK LIGHT AT ROW 25 WAS INOPERATIVE. RECONNECTED LAMP ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002080200066 20020802 00066 2002 8 2 ASAA0280202 4 20020610 A 2565 3961899501 LANYARD DOUG DC9 DC982 3022082 WP EVAC SLIDE DETACHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING PREFLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. ATTACHED LANYARD. (M) 2 L 7 2 4F A6WE 2002080200067 20020802 00067 WP 2002 8 2 ASAA0280203 1 20020610 A 5610 5913217520 MECHANISM DOUG DC9 DC982 3022082 WP COCKPIT WINDOW LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 934AS 49235 LAX - DURING PREFLIGHT CHECK, THE FIRST OFFICERS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. LUBRICATED WINDOW MECHAN ISM. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002080200068 20020802 00068 WP 2002 8 2 ASAA0280204 1 20020613 A 5310 59360381 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OAK - DURING C-CHECK, FOUND CORROSION ON MID CARGO BAY DOOR BEAM HORIZONTAL AND VERTICAL FACE. INSTALLED REPAIR DOUBLER PER TASK CARD 28553000. (M) 2 L 7 2 4F RT A6WE 2002080200069 20020802 00069 WP 2002 8 2 ASAA0280213 1 20020620 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN LOW A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 964AS 22582 6106 53078 SEA - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT TO BE VERY DIM. REPLACED PORTABLE LIGHT ASSEMBLY. OPS TESTED O K. (M) 2 L 7 2 4F RT A6WE 2002080200070 20020802 00070 WP 2002 8 2 ASAA0280214 1 20020620 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 964AS 15274 2244 53078 SEA - DURING LINE CHECK, EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND TO REMAIN ON WITH SWITCH TURNED OFF. REPLACED PO WER SUPPLY. EMERGENCY LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002080200071 20020802 00071 NM 2002 8 2 EIAA2002084 1 20020622 A 3350 51356B37 LIGHT BOEING 747 747132 1384882 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479EV 19898 JFK - R5 EMERGENCY DOOR FLOOD LIGHT INOPERATIVE. FOUND BAD LIGHT ASSEMBLY, REPLACED LIGHT ASSEMBLY IAW MM 33-52-00. (M ) 2 L 7 4 4F A20WE 2002080200072 20020802 00072 NM 2002 8 2 HALA0200253 1 20020625 A 4910 INLET BOEING 717 717200 1383700 NM APU CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 482HA 55127 HNL - FOUND APU INLET DOOR TOP END AT SHAFT CRACKED APPROX 1.25 INCH. REMOVED DOOR FOR REPAIR. OK TO CONTINUE PER CLD 49-17-1. (M) 2 L 7 2 4F TR A6WE 2002080200073 20020802 00073 NM 2002 8 2 TSAA0229150 1 20020626 A 2910 HYDRAULIC LINE BOEING 737 737282C 13844AU NM HYD SYSTEM RUPTURED A TSAA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 826AL 23051 FLT 833 - OGG-HNL - EN ROUTE TO HNL, THE HYDRAULIC 'A' SYSTEM FAILED LOSING ALL HYDRAULIC FLUID. THE AIRCRAFT LANDED IN HNL WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED A RUPTURED NR 2 ENGINE HYDRAULIC PRESSURE FLEX-LINE. THE NR 2 ENGI NE DRIVEN HYDRAULIC PUMP WAS ALSO REPLACED AS A PRECAUTIONARY DUE TO PUMP CAVITATION. LEAK AND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002080200074 20020802 00074 WP 2002 8 2 ASAA0280205 1 20020613 A 5320 NAS1739E63 PAN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OAK - DURING C-CHECK, FOUND CORROSION ON FORWARD CARGO BAY DOOR JAMB PAN VERTICAL LEG. REMOVED CORROSION BEYOND SRM 53- 01 FIG 1 LIMITS, AND SPLICED IN NDW SECTION PER SRM 53-05 FIG 44. (M) 2 L 7 2 4F RT A6WE 2002080200075 20020802 00075 SO 2002 8 2 SWIA200211037 1 20020708 A 2432 501122804 BATTERY EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE E/E BAY DISCHARGED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 299SW 3976 3976 120329 T/O BRAKES AURAL WARNING ON T/O ROLL WITH BRAKES RELEASED. ABORTED T/O. REMOVED AND REPLACED EMERGENCY BATTERY, OPS CH ECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002080200076 20020802 00076 EA 2002 8 2 SWIA200211038 1 20020710 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN DISCONNECTED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 493SW 7450 ON PREFLIGHT, AFT 6 ROWS OF FLOOR EMERGENCY LIGHTS INOP. RECONNECTED WIRES TO AFT PORTION OF FLOOR EMERGENCY LIGHTS. O PS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080200077 20020802 00077 EA 2002 8 2 SWIA200211039 1 20020711 A 3260 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NLG BENT A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 592SW 7279 NOSE GEAR WON'T RETRACT. RETURNED TO DFW. INSPECTED NOSE GEAR FOUND GEAR PROX SENSOR BENT. STRAIGHTENED BRACKET, SWUN G GEAR AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080200078 20020802 00078 EA 2002 8 2 SWIA200211040 1 20020714 A 2730 10231007 DAMPENER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ELEVATOR DEFECTIVE A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 NM 07 591SW 1694 1694 7079 DURING STABLE FLIGHT, AIRPLANE EXPERIENCED FLUTTER. WHEN PUTTING LOADS ON ELEVATOR, FLUTTER WENT AWAY. RETURNED IN STE ADY, STABLE FLIGHT. GREATER FLUTTER AT HIGHER SPEEDS, HAPPENED AT ALL ALTITUDES. RETURNED TO SLC. REMOVED AND REPLACE D LT ELEVATOR FLUTTER DAMPERS WITH SERVICEABLE UNITS IAW MM 27-34-05. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080200079 20020802 00079 2002 8 2 SWIA200211041 4 20020711 A 6122 GOVERNOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 NM 07 393SW 120330 LEFT ENGINE DID NOT ACCELERATE ABOVE 90 PERCENT NP ON TAKEOFF. ABORTED T/O. RAN UP ENGINES W/EEC ON & OFF WITH SIMILAR RESULTS. REMOVED AND REPLACED LT OVERSPEED GOVERNOR IAW HS 61-22-00. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002080200080 20020802 00080 SO 2002 8 2 SWIA200211043 1 20020617 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 223SW 120291 C-CHECK, LEFT SIDE UPPER SEAT RAIL CORROSION FOUND IN 28 LOCATIONS. INSTALLED LEFT SIDE UPPER SEAT RAIL IAW 53-01-05. 2 L 7 2 4T RT A31SO 2002080200081 20020802 00081 SO 2002 8 2 SWIA200211044 1 20020617 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 223SW 120291 RIGHT NACELLE FRAME 1 CRACKED AT O/B TOP TORQUE MOUNT BOLT WEB. REMOVED AND REPLACED FRAME 1 IAW SB 120-54-0036 REV 02, 09 JUN 99. 2 L 7 2 4T RT A31SO 2002080200082 20020802 00082 SO 2002 8 2 SWIA200211045 1 20020617 A 5411 FRAME EMB 120 EMB120ER 3260203 SO NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 223SW 120291 RIGHT AND LEFT NACELLE, ABOVE WING, I/B & O/B SIDE, BENEATH EXHAUST PIPE MOUNT, CRACKS IN FRAMES. STOP-DRILLED CRACKS A ND INSTALLED REPAIR DOUBLERS ON THE FRAMES IAW EMB SRM 51-70-05. 2 L 7 2 4T RT A31SO 2002080200083 20020802 00083 SO 2002 8 2 SWIA200211046 1 20020607 A 5312 FIREWALL EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 284YV 120284 LEFT SIDE APU FIREWALL HAS SMALL CRACK AT LARGE CANNON PLUG TOP, RIGHT MOUNT SCREW. STOP-DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-10-00. 2 L 7 2 4T RT A31SO 2002080200084 20020802 00084 SO 2002 8 2 SWIA200211047 1 20020607 A 5230 STOP FITTING EMB 120 EMB120ER 3260203 SO CARGO DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 284YV 120284 CARGO UPPER FWD LATERAL STOP MOUNT PAD POSSIBLE CRACK (POSITION NR 1). FABRICATED AND INSTALLED DOUBLER AT POSITION NR 1, UPPER FWD LATERAL STOP MOUNT OF CARGO DOOR PER SRM 52-30-02 AND RII 52-301. 2 L 7 2 4T RT A31SO 2002080200085 20020802 00085 SO 2002 8 2 SWIA200211048 1 20020607 A 5230 SUPPORT EMB 120 EMB120ER 3260203 SO CARGO DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 284YV 120284 CARGO DOOR AFT TRACK TOP MOUNT SUPPORT CRACKED. REPLACED TOP SUPPORT WITH SERVICEABLE UNIT FOR CARGO DOOR AFT TRACK. 2 L 7 2 4T RT A31SO 2002080200086 20020802 00086 EA 2002 8 2 SWIA200211049 1 20020710 A 4940 21188002 ECU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE APU FAULTY A SWIA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 NM 07 411SW 7067 DURING START OF APU, APU HANGS AT 9 PERCENT. STARTED ON FOURTH ATTEMPT WHICH RESULTED IN FIRE IN THE TAILPIPE, CAUSING DELAMINATION TO THE LOWER SIDE OF RIGHT ENGINE PYLON. REMOVED AND REPLACED APU IAW MM 49-10-00 DUE TO HIGH EGT & METAL ON CHIP DETECTOR. APU PN/ ON 3800488-3, S/N OFF P-676. ALSO REMOVED AND REPLACED APU ECU S/N OFF 44-F001. (THE CAUSE OF THE HUNG STARTS). OPS CHECK GOOD. PYLON REPAIRED IAW REO 601R-54-62-037. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080200087 20020802 00087 EA 2002 8 2 SWIA200211050 1 20020716 A 3244 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT MLG BLOWN A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 916SW 7634 AC RETURNED TO PHX DUE TO HIGH ENGINE VIBRATION ON LEFT ENGINE. VIBRATION CAUSED BY FOD INGESTION DURING GROUND OPERATI ON OR TAKEOFF. A LEFT MAIN TIRE BLEW ON ROTATION. ON LANDING THE OTHER LEFT MAIN TIRE FAILED. REPLACED BOTH LEFT MAIN WHEEL ASSYS IAW 32-41-01. INSPECTED LEFT ENGINE FOR DAMAGE. BORESCOPE INSPECTED 1ST STAGES OF COMPRESSOR, FOUND NO EV IDENCE OF INTERNAL DAMAGE OR PIECES OF TIRE. REPLACED 28 FAN BLADES, DID NOT REPLACE ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080200088 20020802 00088 NE 2002 8 2 SWIA200211051 2 20020713 A 7320 3035659 HMU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 393SW 120330 AFTER START OF TAKEOFF ROLL, AURAL WARNING ENGINE CONTROL SOUNDED. REMOVED AND REPLACED LT HMU IAW EMB 120 MM 73-21-00 . OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002080200089 20020802 00089 SO 2002 8 2 SWIA200211052 1 20020714 A 5243 ACCESS DOOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HYD SYSTEM MISSING A SWIA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 NM 07 215SW 120281 POST FLIGHT INSPECTION - LEFT HYDRAULIC PANEL MISSING. TRIMMED NEW DOOR TO FIT AND INSTALLED NEW LATCHES, CAMLOCKS AND NEW HINGE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002080200090 20020802 00090 NM 2002 8 2 0202472275 1 20020730 A 3211 NUT BOEING 727 727251 138408H NM RT GEAR CRACKED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 275US 21154 WHILE PERFORMED SCHEDULED MAINTENANCE IN DTW, THE RIGHT MAIN LANDING GEAR FORWARD TRUNNION FITTING ATTACH BOLT OUTBOARD NUT WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED THE NUT PER IAW MM 32-11-51. 2 L 7 3 4F A3WE 2002080200091 20020802 00091 WP 2002 8 2 0202489933 1 20020725 A 4990 HONEYWELL GTCP8598DCA DOUG DC9 DC931 3022065 WP A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 1334U P182DCA 47280 DURING CLIMB, FLIGHT ATTENDANT NOTICED SMOKE IN CABIN AND FORWARD LAV ALARM SOUNDED. FLIGHT CREW RETURNED AIRCRAFT TO DE PARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND AN APU OIL LEAK. OIL LEAK WAS CORRECTED, CLEANE D APU AREA, AND COMPLIED WITH PACK BURNOUT PROCEDURE. REPLACED COALESCER BAGS. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 2002080200092 20020802 00092 EA 2002 8 2 SWIA200211053 1 20020714 A 2750 860D10018 ECU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 442SW 1321 1321 7609 FLAPS FAIL MSG DURING CLIMB. CONTINUED TO SLC. ZERO DEGREE FLAP LANDING AT 43,000 LBS. RERIGGED FLAPS AND INSTALLED N EW FECU C/W AD 98-20-01/02. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002080200093 20020802 00093 SO 2002 8 2 SWIA200211055 1 20020707 A 3297 WIRE HARNESS EMB 120 EMB120ER 3260203 SO RT MLG FAULTY A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 223SW 120291 THE CABIN PRESSURE DROPPED BELOW LEVEL WITH AUTO MODE, IDLE NR 1 & 2 UNLK LIGHTS CAME ON AND DOWNLOCK RELEASE WAS REQUIR ED TO PUT THE GEARS UP. REMOVED AND REPLACED RT MLG HARNESS ASSY WITH SERVICEABLE PART. PERFORMED OPS CHECK FOR DISCRE PANCIES. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4T RT A31SO 2002080200094 20020802 00094 EA 2002 8 2 SWIA200211056 1 20020714 A 2721 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 909SW 7558 RUDDER TRIM ROTARY SWITCH INOP. UNABLE TO ACTIVATE TRIM NOSE RIGHT WHEN ROTATING SWITCH TO FULLY RIGHT. REPLACED RUDDE R TRIM CONTROL PANEL WITH SERVICEABLE PANEL. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002080200095 20020802 00095 EA 2002 8 2 SWIA200211057 1 20020714 A 2731 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT DEFECTIVE A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 405SW 7029 YAW DAMPER CH 1 INTERMITTENT, WILL NOT STAY ENGAGED. RETURNED TO THE GATE. REMOVED AND REPLACED CAPTAIN'S STAB TRIM DI SCONNECT SWITCH. YAW DAMPER SYSTEM, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080200096 20020802 00096 EA 2002 8 2 SWIA200211058 1 20020717 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA NR 2 MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 NM 07 413SW 6838 2226 7102 YELLOW GROUND SPOILER DEPLOY MESSAGE AND AIRCRAFT ROLLING LEFT AND RIGHT IMMEDIATELY AFTER TOUCHDOWN. MESSAGE AND ROLLI NG CEASED AFTER 4 SECONDS THEN GREEN GROUND SPOILER DEPLOY GREEN MESSAGE APPEARED. REMOVED AND REPLACED NR 2 SECU. OPS CHECK GOOD ON ALL SPOILERS. 2 L 7 2 4F RT A21EA 2002080200097 20020802 00097 SO 2002 8 2 SWIA200211059 1 20020630 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 290SW 120317 LEFT CABIN FLOOR SEAT TRACK CORRODED FORWARD AND AFT. REMOVED AND REPLACED LEFT CABIN FLOOR SEAT TRACKS IAW EMB120 MM 5 3-01-05. 2 L 7 2 4T RT A31SO 2002080200098 20020802 00098 SO 2002 8 2 SWIA200211060 1 20020630 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 290SW 120317 RIGHT NACELLE FRAME 1 CRACKED. REPLACED FRAME 1 ON RIGHT NACELLE IAW SB 120-54-0036. 2 L 7 2 4T RT A31SO 2002080200099 20020802 00099 SO 2002 8 2 SWIA200211061 1 20020630 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 290SW 120317 BUTT STRAP IN CARGO COMPARTMENT CORRODED BEYOND LIMITS PER SRM 53-20-10. REPLACED AFFECTED BUTT STRAP IAW EMB120 SRM 51 -10-02 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002080200100 20020802 00100 SO 2002 8 2 SWIA200211062 1 20020630 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 290SW 120317 LEFT SIDE OF CABIN FORWARD AND AFT, FLOOR BUTT STRAP CORRODED. REPLACED AFFECTED BUTT STRAPS IAW SRM 51-10-02. 2 L 7 2 4T RT A31SO 2002080200101 20020802 00101 SO 2002 8 2 SWIA200211063 1 20020715 A 2120 SMOKE EMB 120 EMB120ER 3260203 SO CABIN DETECTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 235SW 120310 CABIN FILLING WITH SMOKE WITH APU RUNNING AND BLEEDS AND PACKS ON AUTO. RAN BOTH PACKS WITH APU IN ALL MODES. CHECKS N ORMAL AT THIS TIME. 2 L 7 2 4T RT A31SO 2002080200102 20020802 00102 NM 2002 8 2 P5CA0200692 1 20020727 A 5210 NONE DOOR BOEING 747 747283B 1384867 NM CABIN CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 CRACK 7/8" LONG FOUND AT #5 RH CABIN DOOR, STATION 2231, BELOW STRINGER 25R. CRACK STOP DRILLED IAW SRM 51-10-01 & REPA IR CARRIED OUT IAW SRM 53-10-04, FIG 4. 2 L 7 4 4F A20WE 2002080200103 20020802 00103 EA 2002 8 2 SWIA200211064 1 20020717 A 2741 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 918SW 286 286 7645 STAB CH1 WILL NOT ENGAGE. REMOVED AND REPLACED TRIM UNIT, HORIZONTAL STAB IAW CRJ MM 27-41-05. PERFORMED OPS AND FUNCT IONAL CHECK. OPS CHECKED GOOD. AIRCRAFT RETURNED TO CAT II STATUS. 2 L 7 2 4F RT A21EA 2002080200104 20020802 00104 EA 2002 8 2 SWIA200211065 1 20020720 A 3010 SWITCH CNDAIR CL600 CL6002B19 1900309 EA RT WING MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 588SW 7069 SELECTING WING ANTI-ICE ON RECEIVED AN ANTI-ICE DUCT MESSAGE. RETURNED TO SLC. REMOVED AND REPLACED RIGHT WING THERMAL SWITCHES FOR OUTBOARD RIGHT WING SEGMENT P/N 60159320-1. INSPECTED PICCOLO TUBE FOR OUTBOARD AND MIDDLE WINGS, NO CRA CKS NOTED. RAN WING ANIT-ICE, NO LEAKS NOTED AT REMOVED SECTIONS. WING ANITI-ICE CHECKS GOOD ON GROUND RUN UP. 2 L 7 2 4F RT A21EA 2002080200105 20020802 00105 EA 2002 8 2 SWIA200211066 1 20020723 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 920SW 51 51 7660 FLAP FAIL MESSAGE APPEARED DURING TAXI IN. REMOVED AND REPLACED RIGHT FLAP BPSU IAW CRJ MM 27-51-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002080200106 20020802 00106 EA 2002 8 2 SWIA200211068 1 20020724 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB FAILED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 590SW 1563 1563 7077 STAB CH 2 INOP STATUS MESSAGE IN FLIGHT, WOULD NOT RE-ENGAGE. REMOVED AND REPLACED THE HSTA AND MOTOR CONTROL UNIT WITH SERVICEABLE HSTA AND MOTOR CONTROL UNIT. OPS AND FUNCTION CHECK GOOD IAW CRJ MM 27-40-00, 27-42-00 & 27-42-05. 2 L 7 2 4F RT A21EA 2002080200107 20020802 00107 NM 2002 8 2 UPS02438922 1 20020709 A 5310 BRACKET BOEING 747 747123F NM M/D B2231 S26R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C M/D - BS 2231, S26R FRAME ATT BRACKET CRACKED. ( AT FLOOR LEVEL AREA ). M/D BS 2231 S26R FLOOR LEV EL AREA FRAME ATT BRACKET REPLACED AS PER SRM 51-10-01. P.8. 2 L 7 4 4F A20WE 2002080200108 20020802 00108 NM 2002 8 2 UPS02438930 1 20020629 A 5330 SKIN BOEING 747 747123F NM RH SIDE STA 392 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - EXTERIOR SKIN FOUND CRACKED AROUND RIVET FASTENER AT RH SIDE STA 392 STR 44R. NOSE WHEEL WELL RH AFTER CORNER SKIN REPAIRED AS PER EO B747-5330-3520E AND DWG 141U1099 AND HX RS R53-11-34838 WITH UPS ENGINEERING FI LE NUMBER 747-53-20090. 2 L 7 4 4F A20WE 2002082200098 20020822 00098 NM 2002 8 22 02FDEA00541 1 20020731 A 5330 SKIN BOEING 727 72722 1384002 NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 EXTERNAL SKIN CHAFED AT STR 19R BS 720D+13. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 14. 2 L 7 3 4F A3WE 2002080200109 20020802 00109 EA 2002 8 2 02213635 1 20020801 A 3350 364911 LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 635BR 7295 During preflight inspection, the crew reported that a section of the emergency floor track lighting was inoperative. Ma intenance personnel secured a connector for one of the emergency floor track flex lamps. An operational check was satis factory and the aircraft was was returned to service. 2 L 7 2 4F RT A21EA 2002091200101 20020912 00101 WP 2002 9 12 IXXA0200049O 1 20020802 A 7910 OIL CAP DOUG DC8 DC871F 302199D WP NR 1 ENGINE LOOSE A IXXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 11 821BX 82657 2667 45811 EN ROUTE FROM PDX TO BFI, THE FLIGHT CREW NOTICED THE NUMBER ONE ENGINE OIL QUANTITY DECLINING. THE FLIGHT CREW FOLLOWE D COMPANY PROCEDURES AND SECURED THE ENGINE AND CONTINUED TO BFI FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE E NGINE LOCATING THE STARTER OIL SERVICING CAP OFF. MAINTENANCE SERVICED THE ENGINE STARTER AND SECURED THE SERVICING CAP . MAINTENANCE PERFORMED LEAK CHECK AND OPERATIONAL CHECK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002080500001 20020805 00001 EU 2002 8 5 000177 1 20020708 A 7722 THERMOCOUPLE SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A CHQA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 11 140 RT ENGINE ITT FLUCTUATION. REMOVED AND REPLACED THERMOCOUPLE RAKE. 2 L 7 2 4T RT A52EU 2002080500002 20020805 00002 SO 2002 8 5 000180 1 20020715 A 5220 DOOR EMB 145 EMB145 3260210 SO EMERGENCY EXIT OPEN A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 294 LT WING EMERGENCY EXIT HATCH OPEN LIGHT ILLUMINATED ON EICAS ON CLIMBOUT. MAINTENANCE SECURED LT WING EMERGENCY EXIT HA TCH. 2 L 7 2 4F RT T00011AT 2002080500003 20020805 00003 SO 2002 8 5 000181 1 20020718 A 2150 A/C PACK EMB 145 EMB145 3260210 SO A/C BAY MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 373 NR 2 PACK DOES NOT WORK. NR 1 PACK ON MEL. PERFORMED OPERATIONAL CHECK ON PACK 2 SYSTEM OPS CHECKS GOOD NO GROUND. NO EICAS OR CMC MESSAGES. PRESSURIZATION FUNCTIONS NORMALLY AUTO AND MANUAL. 2 L 7 2 4F RT T00011AT 2002080500004 20020805 00004 SO 2002 8 5 000183 1 20020725 A 2760 SWITCH EMB 145 EMB145 3260210 SO SPOILER DIRTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 266 E1 REV DISAGREE AND SPOILER FAIL EICAS MSG. CLEANED ALL DOWNLOCK SWITCHES AND RESET A/C OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2002080500005 20020805 00005 SO 2002 8 5 000184 1 20020726 A 2611 SMOKE WARNING EMB 145 EMB145 3260210 SO COCKPIT FALSE ACTIVATION A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 270 LAV SMOKE INDICATION CAME ON. INDICATION WENT AWAY. PERFORMED LAV SMOKE SYSTEM TEST AND GROUND RAN WITH ENGINE AND APU BLEEDS. COULD NOT DUPLICATE. 2 L 7 2 4F RT T00011AT 2002080500006 20020805 00006 SO 2002 8 5 000185 1 20020731 A 2611 SMOKE DETECTOR EMB 145 EMB145 3260210 SO CARGO BAY MALFUNCTIONED A CHQA K NONE N FALSE WARNING UK UNKNOWN 1 GL 11 140 CARGO SMOKE WARNING. REMOVED AND REPLACED CARGO SMOKE DETECTOR AND OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2002080500007 20020805 00007 SO 2002 8 5 000717 1 20020623 A 7710 B-NUT EMB 145 EMB145 3260210 SO NR 2 ENGINE LOOSE A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 268 PILOT REPORTED E2 ATTCS NO MARGIN ON EICAS. REMOVED INSPECTED THE START BLEED CONTROL SENSE LINE FOUND LOOSE B-NUT. 2 L 7 2 4F RT T00011AT 2002080500008 20020805 00008 NM 2002 8 5 0201976635 1 20020615 A 3350 BATTERY PACK BOEING 747 747227B 1384888 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 635US 21682 DURING LINE CHECK, FOUND ZONE-A FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPERA TIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002080500009 20020805 00009 NM 2002 8 5 0201986628 1 20020619 A 3350 BATTERY BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 635US 22389 DURING LINE CHECK, FOUND D-ZONE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES. OPERATIONAL CH ECK GOOD. 2 L 7 4 4F A20WE 2002080500010 20020805 00010 NM 2002 8 5 0201995635 1 20020620 A 3350 BATTERY PACK BOEING 747 747227B 1384888 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 635US 21682 DURING LINE CHECK, FOUND FIRST CLASS FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002080500011 20020805 00011 NE 2002 8 5 0202002709 2 20020618 A 7314 378200 PUMP BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE LT ENGINE FAILED A NWAA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 GL 01 818EA 5974 22555 700626 DURING CLIMBOUT, THE LEFT ENGINE EXPERIENCED A FLAME-OUT. AIRCRAFT RETURNED TO TPA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE FUEL PUMP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002080500012 20020805 00012 WP 2002 8 5 0202021162 1 20020611 A 3210 LANDING GEAR DOUG DC10 DC1040 3023508 WP LT MLG MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 162US 46771 ON TAKEOFF UPON GEAR RETRACTION, THE LEFT MAIN GEAR RED LIGHT REMAINED ON. PROCEEDED WITH COCKPIT OPERATING MANUAL PROC EDURE. VISUALLY CHECKED GEAR WHICH APPEARED DOWN. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REP LACED THE LEFT MAIN LANDING GEAR. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 2002080500013 20020805 00013 WP 2002 8 5 0202059919 1 20020630 A 2611 SMOKE DOUG DC9 DC932 3022066 WP CABIN DETECTED A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 941N 47450 THE FORWARD LAV SMOKE DETECTOR ACTIVATED IMMEDIATELY AFTER TAKEOFF AND THE LEAD FLIGHT ATTENDANT OBSERVED SMOKE IN THE C ABIN. FLIGHT RETURNED TO MSP AND LANDED SAFELY. MAINTENANCE REMOVED, INSPECTED AND REINSTALLED THE LAV SMOKE DETECTOR. THERE WAS NO EVIDENCE OF SMOKE OR OTHER DAMAGE NOTED IN THE LAV OR ANY ADJACENT AREAS. TESTS ALL CHECKED NORMAL. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002080500014 20020805 00014 WP 2002 8 5 0202079976 1 20020622 A 2910 O-RING DOUG DC9 DC931 3022065 WP HYD SYSTEM DAMAGED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 9340 47389 LEFT HYDRAULIC PRESSURE AND QUANTITY WENT TO ZERO. COMPLIED WITH COM PROCEDURES AND THE LEFT QUANTITY RETURNED TO 5 QUA RTS BUT PRESSURE REMAINED AT ZERO. FLIGHT RETURNED TO A SAFE UNEVENTFUL LANDING BACK TO DTW. MAINTENANCE FOUND THE RES ERVOIR EMPTY AND FOUND A LEAK DUE TO A BAD O-RING ON THE CHECK VALVE AT THE LEFT THRUST REVERSER CONTROL VALVE. THE O-R ING AND THE ENGINE DRIVEN HYDRAULIC PUMP WERE REPLACED. ALSO, NEW FILTERS AND CHECK VALVE WERE INSTALLED. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F A6WE 2002080500015 20020805 00015 NE 2002 8 5 0202089885 2 20020621 A 7510 577957 DUCT DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT ENGINE CRACKED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 401EA 47682 688716 DURING CLIMB, THE LEFT ENGINE EXPERIENCED A FIRE WARNING INDICATION. CREW RETARDED THE LEFT ENGINE THRUST TO IDLE. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE LEFT ENGINE FUEL HEAT DUCT. ENGINE OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2002080500016 20020805 00016 EU 2002 8 5 0202093215 1 20020623 A 2150 1263A000003 ACM AIRBUS 320 A320211 3930320 EU A/C BAY SEIZED A NWAA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 01 315US 11413 6395 00171 FLIGHT ATTENDANT REPORTED SMOKE IN AFT CABIN. CAPTAIN NOTICED LIGHT SMOKE IN THE COCKPIT. SMOKE CLEARED WITHIN A FEW M INUTES. AFTER LANDING, RECEIVED PACK 1 OVERHEAT WARNING. FOUND NR 1 AIR CYCLE MACHINE SEIZED. REPLACED THE NR 1 AIR C YCLE MACHINE. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002080500017 20020805 00017 NM 2002 8 5 0202106303 1 20020620 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 635US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM DOOR 2R TO 3R. RECONNECTED WIRE. OPERATIONAL CHE CK GOOD. 2 L 7 4 4F RT A20WE 2002080500018 20020805 00018 WP 2002 8 5 0202119952 1 20020628 A 2120 SMOKE DOUG DC9 DC931 3022065 WP CABIN DETECTED A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 916RW 47144 SMOKE WAS REPORTED IN THE CABIN SHORTLY AFTER TAKEOFF. SMOKE CLEARED PRIOR TO LANDING A FEW MINUTES LATER. AFT LAV SMO KE DETECTOR SOUNDED. FLIGHT LANDED BACK AT RAP SAFELY. MAINTENANCE RAN PACKS AND APU, CHECKED FOR WIRING FAULTS OR HOT BALLAST. NO TROUBLE FOUND IN ANY COMPONENTS. TWO DAYS LATER APU DISCOVERED LEAKING OIL AND LEAKS CORRECTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002080500019 20020805 00019 NM 2002 8 5 0202126301 1 20020629 A 2121 732591B GASPER FAN BOEING 747 747451 1384940 NM CABIN FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 661US 50424 3821 23719 DURING CRUISE, FLIGHT CREW NOTICED AN ELECTRICAL SMOKE SMELL IN THE CABIN. AIRCRAFT DIVERTED TO SEA AND LANDED WITHOUT INCIDENT. REPLACED THE GASPER FAN. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002080500020 20020805 00020 WP 2002 8 5 0202229954 1 20020708 A 2131 CONTROLLER DOUG DC9 DC931 3022065 WP CABIN PRESSURE MALFUNCTIONED A NWAA G B O2 MASK DEPLOYED EMER. DESCENT O OTHER CR CRUISE 1 GL 01 621RW 47164 WHILE LEVEL AT FL290, THE CABIN PRESSURE ALTITUDE WOULD FLUCTUATE BETWEEN A 2000 FPM CLIMB TO ZERO. AS THE ACTUAL CABIN ALTITUDE REACHED 10,000 FEET, THE CREW MANUALLY DEPLOYED THE PASSENGER MASKS AND AN EMERGENCY DESCENT WAS INITIATED. C ABIN ALTITUDE REACHED 24,000 FEET. COMPLIED WITH COM PROCEDURES AND FLIGHT CONTINUED TO DESTINATION AT A LOWER ALTITUDE AND LANDED AT IND WITHOUT INCIDENT. MAINTENANCE PLACED THE PRESSURE CONTROLLER ON MEL, PLACARD 875312 AND VERIFIED THA T MANUAL PRESSURIZATION IS OPERATIONAL. 2 L 7 2 4F A6WE 2002080500021 20020805 00021 WP 2002 8 5 0202231242 1 20020609 A 2170 COALESCER BAG DOUG DC10 DC1030 3023501 WP A/C BAY CONTAMINATED A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 242NW 47845 DURING CLIMB, THE COCKPIT AND CABIN FILLED WITH SMOKE AND LAV SMOKE DETECTORS SOUNDED. FOLLOWED COM PROCEDURE AND RETUR NED TO SEA WITHOUT INCIDENT. PERFORMED PACK BURNOUT. REPLACED ALL THREE PACK SOCKS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A22WE 2002080500022 20020805 00022 NE 2002 8 5 0202242275 2 20020702 A 7320 654233 VALVE BOEING 727 727251 138408H NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE DAMAGED A NWAA C ABORTED TAKEOFF X ENGINE FLAMEOUT TO TAKEOFF 1 GL 01 275US 45652 2579 21154 653954 DURING TAKEOFF ROLL AT 100 KNOTS, THE NR 2 ENGINE FLAMED OUT. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 2 ENGINE PRESSURE AND DUMP VALVE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002080500023 20020805 00023 NM 2002 8 5 0202256309 1 20020703 A 2530 OVEN BOEING 747 747451 1384940 NM GALLEY OVERHEATED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 669US 24224 DURING FLIGHT, THE LEFT OVEN IN THE NR 1 GALLEY OVERHEATED AND SMOKED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WIT HOUT INCIDENT. REPLACED THE OVEN. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002080500024 20020805 00024 NM 2002 8 5 0202266624 1 20020705 A 2530 OVEN BOEING 747 747251B 1384892 NM GALLEY MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 624US 21706 DURING CLIMB, A BURNING ODOR EMITTED IN ZONE-A, ZONE-B AND UPPER DECK. SHUT OFF UPPER DECK OVENS AND PULLED CIRCUIT BRE AKERS AND THE ODOR DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED BOTH OVENS IN T HE UPPER DECK GALLEY. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002080500025 20020805 00025 NM 2002 8 5 0202276303 1 20020705 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND THE RIGHT SIDE FLOOR PATH EMERGENCY LIGHTS ROWS 21-31 ILLUMINATING INTERMITTENTLY. RECONNECTED WIRE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002080500026 20020805 00026 NM 2002 8 5 0202286316 1 20020702 A 2530 COFFEEMAKER BOEING 747 747451 1384940 NM GALLEY DIRTY A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 676NW 33002 DURING FLIGHT, A FLIGHT ATTENDANT REPORTED AN ELECTRICAL FUME ODOR IN THE AREA BENEATH THE STAIRS. AIRCRAFT CONTINUED T O DESTINATION AND LANDED WITHOUT INCIDENT. CLEANED COFFEEMAKER, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002080500027 20020805 00027 WP 2002 8 5 0202299907 1 20020717 A 2520 43501 PSU DOUG DC9 DC931 3022065 WP CABIN DEFECTIVE A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 957N 47253 FLIGHT ATTENDANT REPORTED ELECTRICAL SMOKE SMELL AIRBORNE AND FELT IT WAS ASSOCIATED WITH SEAT 21AB CALL LIGHT. AIRCRAF T RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED SEAT 21AB PSU. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 2002080500028 20020805 00028 NE 2002 8 5 0202302702 2 20020714 A 7314 378201 PUMP BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE DAMAGED A NWAA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 GL 01 877Z 32765 3022 21450 695293 DURING APPROACH FOR LANDING, THE NR 2 ENGINE FLAMED OUT. AIRCRAFT COMPLETED LANDING WITHOUT FURTHER INCIDENT. MAINTENA NCE REPLACED THE NR 2 ENGINE FUEL PUMP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002080500029 20020805 00029 2002 8 5 0202329943 4 20020713 A 2565 SLIDE DOUG DC9 DC931 3022065 WP TAILCONE MALFUNCTIONED A NWAA K NONE L NO TEST NR NOT REPORTED 1 GL 01 1308T 47315 TAIL CONE WAS ACCIDENTALLY DROPPED AND THE EVACUATION SLIDE DID NOT DEPLOY. MAINTENANCE REINSTALLED THE SLIDE AND CHECK ED THE INSTALLATION. ALSO, THE DAMAGE TO THE TAIL CONE WAS TEMPORARILY REPAIRED TO ALLOW THE AIRCRAFT TO BE FERRIED TO MEM. 2 L 7 2 4F A6WE 2002080500030 20020805 00030 WP 2002 8 5 0202339995 1 20020711 A 3340 SWITCH DOUG DC9 DC931 3022065 WP COCKPIT DEFECTIVE A NWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 8978E 47327 WHEN THE NOSE TAXI LIGHTS WERE TURNED ON AFTER POWERBACK, SPARKS AND SMOKE CAME OUT FROM UNDER THE NOSE LIGHT SWITCH PAN EL. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE NOSE TAXI LIGHT SWITCH. OPERATIONAL CHECK OK. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002080500031 20020805 00031 WP 2002 8 5 0202349150 1 20020708 A 2913 314195 PUMP DOUG DC9 DC914 3022034 WP HYD SYSTEM MALFUNCTIONED A NWAA K NONE F FLT CONT AFFECTED CR CRUISE 1 GL 01 8908E 45749 WHILE IN CRUISE FLIGHT WITH THE ENGINE DRIVEN HYDRAULIC PUMPS IN LOW, THE RIGHT HYDRAULIC SYSTEM WENT TO ZERO PRESSURE F OR 3-5 SECONDS THEN RETURNED TO NORMAL 1500 PSI. THIS OCCURRED TWICE AND THE RIGHT HYDRAULIC PRESSURE LOW AND RUDDER CO NTROL MANUAL LIGHTS ILLUMINATED. THE AIRCRAFT YAWED AS THE HYDRAULIC SYSTEM WENT BETWEEN RUDDER MANUAL POWERED MODES. FLIGHT CONTINUED AND LANDED SAFELY AT MEM. MAINTENANCE REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002080500032 20020805 00032 WP 2002 8 5 0202369982 1 20020721 A 3244 95608924 TIRE DOUG DC9 DC932 3022066 WP LT MLG SEPARATED A NWAA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 01 982US 45790 LEFT MAIN INBOARD TIRE FAILED DURING ROTATION ROLL ON TAKEOFF. OBJECTS DEPARTING THE FAILED TIRE DAMAGED THE LEFT FLAP TRAILING EDGE, THE LEFT ENGINE COWL, AND A PORTION OF THE SEPARATED TIRE TREAD WAS INGESTED INTO THE LEFT ENGINE. FLIGH T RETURNED TO A SAFE LANDING AT BIL. MAINTENANCE REPLACED THE NR 1 AND NR 2 TIRES, THE NR 1 ENGINE, AND THE LEFT MAIN G EAR RETRACT ACTUATOR CYLINDER LINE. THE AIRCRAFT STRUCTURAL COMPONENTS ARE STILL BEING EVALUATED. 2 L 7 2 4F A6WE 2002080500033 20020805 00033 WP 2002 8 5 0202379921 1 20020716 A 2120 DUCT DOUG DC9 DC932 3022066 WP A/C BAY DAMAGED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 943N 47647 AT FL280 WITH ENGINE AND WING ANTI-ICE ON, THE CABIN ALTITUDE STARTED TO CLIMB AT ABOUT 700 FPM. ACCOMPLISHED COM PER R ED BORDER CHECKLIST AND WENT TO FULL CLOSED MANUALLY. AIRCRAFT PERFORMED AN EMERGENCY DESCENT AND CABIN PRESSURE CONTRO L WAS REGAINED AT 13,000 FEET. LANDING AT GTF WAS UNEVENTFUL. MAINTENANCE FOUND THE RIGHT DUCT TORN AND BLOWN FROM CLA MP. REPLACED THE DUCT AND CLAMP. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002080500034 20020805 00034 WP 2002 8 5 0202389937 1 20020719 A 2131 10256861 CONTROLLER DOUG DC9 DC931 3022065 WP CABIN PRESSURE MALFUNCTIONED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 908H 47517 WHILE IN CRUISE AT FL250, THE CABIN ALTITUDE WENT TO 12,000 FEET. CREW ACCOMPLISHED AN EMERGENCY DESCENT TO 9,000 FEET AND LEVELED OFF. MASKS DID NOT DEPLOY AND FLIGHT CONTINUED TO DESTINATION. LANDING AT BUF WAS UNEVENTFUL. CREW STATED THAT THE MANUAL SPRING WAS BROKEN. MAINTENANCE REPLACED THE AUTO PRESSURE CONTROLLER, THE CONTROLLER AMPLIFIER, AND TH E DIFFERENTIAL SENSOR. AIRCRAFT ENTERED INTO L-CHECK AT DHN. 2 L 7 2 4F A6WE 2002080500035 20020805 00035 NE 2002 8 5 0202399856 2 20020721 A 7314 384300 PUMP DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE RT ENGINE FAILED A NWAA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 GL 01 765NC 25042 6181 47718 696729 DURING AIRCRAFT ROTATION FOR FLIGHT, THE RIGHT ENGINE EXPERIENCED A FLAME-OUT. AIRCRAFT RETURNED TO DTW. MAINTENANCE R EPLACED THE RIGHT ENGINE FUEL PUMP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2002080500036 20020805 00036 NE 2002 8 5 0202406717 2 20020724 A 7200 ENGINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7J 52054 NE NR 4 MALFUNCTIONED A NWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING X J A ENGINE FLAMEOUT WARNING INDICATION FLAME/FIRE CL CLIMB 1 GL 01 617US 21121 662502 WHILE CLIMBING THROUGH FL280, THE NR 4 ENGINE FLAMED OUT FOLLOWED BY THE FIRE WARNING ACTIVATING FOR THE NR 4 ENGINE. C OM PROCEDURES WERE FOLLOWED TO SECURE THE ENGINE AND BOTH FIRE BOTTLES WERE DISCHARGED. AN EMERGENCY WAS DECLARED AND T HE AIRCRAFT RETURNED TO SIN. THE AIRCRAFT WAS MET ON THE RUNWAY BY CFR AND FIRE SUPPRESSION EQUIPMENT WAS USED ON THE N R 4 ENGINE. THE AIRCRAFT WAS TOWED OFF THE RUNWAY. MAINTENANCE REPLACED THE NR 4 ENGINE. 2 L 7 4 4F 4 F A20WE E20EA 2002080500037 20020805 00037 2002 8 5 0202459997 4 20020726 A 2565 SLIDE DOUG DC9 DC931 3022065 WP TAILCONE MALFUNCTIONED A NWAA K NONE L NO TEST NR NOT REPORTED 1 GL 01 8933E 47142 TAIL CONE WAS DROPPED AT THE GATE AND THE SLIDE DID NOT DEPLOY AS DESIGNED. THE TAIL CONE DID NOT RECEIVE ANY DAMAGE AN D WAS RE-ATTACHED BACK INTO POSITION AND THE AIRCRAFT WAS FERRIED TO ATL FOR SLIDE MAINTENANCE AND RIGGING. PERFORMED C OMPLETE ADJUSTMENT AND TEST OF TAIL CONE. ALL PARAMETERS WERE NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002080500038 20020805 00038 WP 2002 8 5 0202469609 1 20020728 A 2913 314195 PUMP DOUG DC9 DC932 3022066 WP HYD SYSTEM MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION AP APPROACH 1 GL 01 609NW 47234 DURING DESCENT FOR LANDING INTO MSP, THE RIGHT HYDRAULIC SYSTEM PRESSURE WENT TO ZERO PSI AND THE QUANTITY WENT TO MAX H IGH SCALE. THE RUDDER CONTROL MANUAL ANNUNCIATOR LIGHT ILLUMINATED. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LAND ED WITHOUT INCIDENT AT MSP. MAINTENANCE REPLACED THE RIGHT HYDRAULIC RESERVOIR, THE RIGHT HYDRAULIC ENGINE DRIVEN PUMP, AND FILTER AND RESERVICED THE SYSTEM. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002080500039 20020805 00039 NM 2002 8 5 0202496310 1 20020730 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE AFT OF ROW 51. RECONNECTED WIRE. OPERATIONAL CHECK GO OD. 2 L 7 4 4F RT A20WE 2002080500040 20020805 00040 NM 2002 8 5 0202506717 1 20020728 A 2612 FIRE WARNING BOEING 747 747251F 1384898 NM COCKPIT FALSE ACTIVATION A NWAA K NONE N FALSE WARNING DE DESCENT 1 GL 01 617US 21121 DURING DESCENT, THE MASTER FIRE WARNING BELL SOUNDED AND THE LIGHTS ILLUMINATED FOR THREE SECONDS. AIRCRAFT CONTINUED D ESCENT AND LANDED WITHOUT INCIDENT. RESEATED ALL FIRE WARNING CIRCUIT CARDS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002080500041 20020805 00041 NM 2002 8 5 0202516642 1 20020728 A 2120 ODOR BOEING 747 747212B 1384886 NM CABIN DETECTED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 642NW 21942 DURING FLIGHT, AN ELECTRICAL FUME EMITTED IN THE UPPER DECK. PULLED UPPER DECK GALLEY CIRCUIT BREAKERS AND AIRCRAFT CON TINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. VISUALLY INSPECTED AND OPERATIONALLY CHECKED UPPER DECK WITH NO FAUL TS FOUND. 2 L 7 4 4F A20WE 2002080500042 20020805 00042 NM 2002 8 5 0202526717 1 20020731 A 2612 CIRCUIT CARD BOEING 747 747251F 1384898 NM FIRE WARNING FAULTY A NWAA K NONE N FALSE WARNING DE DESCENT 1 GL 01 617US 21121 DURING DESCENT, THE MASTER FIRE WARNING BELL SOUNDED AND THE LIGHTS ILLUMINATED INTERMITTENTLY. AIRCRAFT CONTINUED DESC ENT AND LANDED WITHOUT INCIDENT. REPLACED APU FIRE DETECTOR CARD. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002080500043 20020805 00043 NM 2002 8 5 0202536717 1 20020730 A 2612 MODULE BOEING 747 747251F 1384898 NM FIRE WARNING MALFUNCTIONED A NWAA K NONE N FALSE WARNING DE DESCENT 1 GL 01 617US 21121 DURING DESCENT, THE MASTER FIRE WARNING BELL SOUNDED AND LIGHTS ILLUMINATED INTERMITTENTLY. AIRCRAFT CONTINUED DESCENT AND LANDED WITHOUT INCIDENT. RESEATED ALL FIRE WARNING CIRCUIT CARDS, EXERCISED WARNING RESET SWITCHES AND REPLACED ENG INE FIRE WARNING MODULE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002080500044 20020805 00044 EA 2002 8 5 02174628 1 20020623 A 5240 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 628BR 7240 DURING TURN AROUND SERVICING, THE CREW NOTED THAT THE GALLEY SERVICE DOOR COULD NOT BE OPENED FROM THE OUTSIDE. MAINTEN ANCE PERSONNEL LUBRICATED THE GALLEY SERVICE DOOR HANDLE OPERATING MECHANISM. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002080500045 20020805 00045 EA 2002 8 5 02179623 1 20020628 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN ENTRY MALFUNCTIONED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 623BR 7192 AFTER ARRIVAL, THE CREW REPORTED THAT THE MAIN CABIN ENTRY DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE PERSONNEL I NSPECTED THE MAIN CABIN DOOR, SEAL AND SEAL RETAINER AND OPERATED THE MAIN CABIN DOOR. NO DEFECTS WERE NOTED AND THE AI RCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002080500046 20020805 00046 EA 2002 8 5 02179703 1 20020628 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 703BR 7467 DURING PREFLIGHT INSPECTION, THE CREW NOTED THAT THE CEILING EMERGENCY EXIT LIGHTED SIGN WAS INOPERATIVE. MAINTENANCE P ERSONNEL REMOVED AND REPLACED THE LIGHT BULB. AN OPERATIONAL CHECK OF THE EMERGENCY EXIT LIGHTING SYSTEM WAS SATISFACTO RY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002080500047 20020805 00047 EA 2002 8 5 02181647 1 20020630 A 2120 SMOKE CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 674BR 7601 DURING THE CLIMB, THE CREW REPORTED THE SMELL OF SMOKE IN THE CABIN. THE BLEED AIR SOURCE WAS TRANSFERRED FROM THE APU TO THE ENGINES. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL INSPECTED THE APU AND FOUND N O DEFECTS OR FAULTS ON THE ECU. THE APU, ENGINES, AND BOTH AIR CONDITIONING PACKS WERE OPERATED AND BLEEDS TRANSFERRED FROM ENGINE TO APU AND BACK SEVERAL TIMES. NO DEFECTS WERE NOTED IN ANY SYSTEM. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002080500048 20020805 00048 EU 2002 8 5 02182309 1 20020701 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 309UE 41022 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIV E. MAINTENANCE PERSONNEL SECURED THE ELECTRICAL CONNECTOR FOR THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002080500049 20020805 00049 NM 2002 8 5 02192413 1 20020711 A 3350 CONNECTOR DORNER DO32 DO328300 NM CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 413FJ 3168 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE PERS ONNEL SECURED A CONNECTOR FOR THE EMERGENCY FLOOR TRACK LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002080500050 20020805 00050 EU 2002 8 5 02202324 1 20020721 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 324UE 41017 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE REAR EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE PERSON NEL SECURED A LOOSE ELECTRICAL CONNECTOR FOR THE AFT EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND T HE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002080500051 20020805 00051 NM 2002 8 5 02209409 1 20020728 A 2460 CONTROL UNIT DORNER DO32 DO328300 NM COCKPIT MALFUNCTIONED A VTZA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 27 409FJ 3161 DURING THE CLIMB, THE CREW REPORTED THAT ELECTRICAL POWER HAD BEEN LOST. ALL 5DAU SCREENS WENT BLANK AND RADIO COMMUNIC ATION WAS INTERMITTENT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE DC POWER CONTROL UNIT (1VE PANEL) P/N 230GC02404, THE NR 1 AND NR 2 INT EGRATED AVIONICS COMPUTER P/N 7017300-11123, AND THE BUSS POWER CONTROL UNIT P/N 106-000-4. OPERATIONAL CHECKS WERE SAT ISFACTORY. AN OVERWEIGHT LANDING INSPECTION WAS ACCOMPLISHED WITH NO FAULTS OR DAMAGE FINDINGS. THE AIRCRAFT WAS RETUR NED TO SERVICE. 2 H 7 2 4T RT A55NM 2002080500053 20020805 00053 NE 2002 8 5 02214303 2 20020802 A 7200 310349016 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE A VTZA A O UNSCHED LANDING OTHER X ENGINE FLAMEOUT AP APPROACH 1 EA 27 303UE 11271 3218 41015 76116 During approach the r/h engine bagan to surge and lose power with no annunciators illuminated. A go-around was initiate d and an emergency was declared. During the go-around, the engine shut down uncommanded. Maintenance personnel removed and replaced the r/h engine assy. Operational and leak checks were satisfactory and the aircraft was returned to servi ce. 2 L 7 2 4T 4 T RT A41NM E18NE 2002080500054 20020805 00054 EU 2002 8 5 02215314 1 20020803 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 314UE 41027 During preflight inspection, the crew reported that the forward emergency floor track lights were inoperative. Maintena nce personnel secured the connector for the forward emergency floor track lights. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002080500059 20020805 00059 2002 8 5 SWAA021721 4 20020801 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002080500060 20020805 00060 NM 2002 8 5 SWAA021722 1 20020801 A 5312 6517582 WEB BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 180, WL 234 AND LBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002080500061 20020805 00061 NM 2002 8 5 SWAA021723 1 20020801 A 5320 6547978 WEB BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 287, WL 208, RT SIDE. REMOVED AND REPLACED WEB SECTION P ER SRM. 2 L 7 2 4F RT A16WE 2002080500062 20020805 00062 NM 2002 8 5 SWAA021724 1 20020801 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 790, BETWEEN STR'S 18L AND 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002080500063 20020805 00063 NM 2002 8 5 SWAA021725 1 20020801 A 5311 6546546 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR'S 8R AND 9R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002080500064 20020805 00064 NM 2002 8 5 SWAA021726 1 20020801 A 5311 6546546 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR'S 8L AND 9L, BS 887 AND BS 827. REPAIRED FRA MES PER SRM. 2 L 7 2 4F RT A16WE 2002080500065 20020805 00065 NM 2002 8 5 SWAA021727 1 20020801 A 3260 1061226 SENSOR BOEING 737 7373H4 1384600 NM LT MLG ERRATIC A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 29 334SW 23938 LEFT MLG DOWN (RED) LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED, RECYCLED GEAR AND LIGHT WENT OUT, BUT ILLUMINAT ED TWICE DURING FLIGHT. REMOVED AND REPLACED LT MLG UPLOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2002080500066 20020805 00066 NM 2002 8 5 SWAA021693 1 20020726 A 5241 6545871 FRAME BOEING 737 7373H4 1384600 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR FRAME CRACKED IN RADIUS BELOW UPPER HINGE CUT OUT. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2002080500067 20020805 00067 NM 2002 8 5 SWAA021694 1 20020726 A 5210 6545871 FRAME BOEING 737 7373K2 13844BA NM AFT ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR AFT FRAME CRACKED AT 2ND DOOR STOP PIN ASSY. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002080500068 20020805 00068 NM 2002 8 5 SWAA021698 1 20020726 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS ON NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM. 2 L 7 2 4F RT A16WE 2002080500069 20020805 00069 NM 2002 8 5 SWAA021699 1 20020726 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM LT ELEVATOR. WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS ON NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM. 2 L 7 2 4F RT A16WE 2002080500070 20020805 00070 2002 8 5 SWAA021708 4 20020730 A 2565 6557463 BRACKET BOEING 737 7372T4 1384492 NM AFT SVC DOOR. LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 702ML 22054 DURING SCHEDULED CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET LOOSE. REMOVED AND REPLACED FWD GI RT BAR BRACKET FASTENERS PER MM. 2 L 7 2 4F A16WE 2002080500071 20020805 00071 NM 2002 8 5 SWAA021712 1 20020731 A 5311 6546543 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 202 AND RBL 65. REPAIRED FRAME PER SWA T1. 2 L 7 2 4F RT A16WE 2002080500072 20020805 00072 NM 2002 8 5 SWAA021713 1 20020731 A 5310 6547978 CREASE BEAM BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CRACKED AT BS 520, WL 208 LT SIDE. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2002080500073 20020805 00073 NM 2002 8 5 SWAA021715 1 20020731 A 5311 6546576 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED C4 CHECK, FOUND TAILCONE ATTACH FRAME CRACKED AT BS 1156, STR 20R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F A16WE 2002080500074 20020805 00074 NM 2002 8 5 SWAA021716 1 20020731 A 5520 65C26384 TAB BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED C3 CHECK, SWA SI 11075-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND B USHINGS ON RT TAB MAST ROD ENDS AND REMOVED AND REPLACED HARDWARE AND BUSHINGS IN NR 1 TAB HINGE ATTACH FITTING PER MM. 2 L 7 2 4F RT A16WE 2002080500076 20020805 00076 NM 2002 8 5 SWAA021700 1 20020729 A 3350 101114 LENS BOEING 737 7373Q8 1384670 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT LENSES LOOSE AT BOTH LEFT AND RIGHT OVERWING EXITS. SECURED LENSE S PER MM. 2 L 7 2 4F RT A16WE 2002080500077 20020805 00077 2002 8 5 SWAA021701 4 20020730 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FALLING OUT OF CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002080500078 20020805 00078 NM 2002 8 5 SWAA021703 1 20020730 A 5330 6545768 SKIN BOEING 737 7372K6 1364440 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 129SW 22340 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) BELOW STR 21L, AT BS'S 343, 342, 341 AND 340. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002080500079 20020805 00079 NM 2002 8 5 SWAA021706 1 20020730 A 5311 6546546 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 787, WL 151 AND LBL 9. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002080500080 20020805 00080 NM 2002 8 5 SWAA021707 1 20020730 A 5311 6546529 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 493, WL 161 AND RBL 35. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002080500081 20020805 00081 NM 2002 8 5 VNAA0207026 1 20020718 A 5200 PSEU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 440JS 3058 ENROUTE, THE CREW REPORTED AN INTERMITTENT PROXI SYSTEM FAIL CAS MESSAGE ALONG WITH A DOOR SWITCH FAIL CAS MESSAGE. MAI NTENANCE INSPECTED AND RERACKED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WER E PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002080500082 20020805 00082 NM 2002 8 5 VNAA0207032 1 20020722 A 2100 CLAMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 441JS 3059 THE CREW REPORTED A HOT SMELL IN THE CABIN APPROXIMATELY UNDER THE PACK AREA. MAINTENANCE INSPECTED AND FOUND A LOOSE C LAMP AROUND THE HOT AIR DUCT. MAINTENANCE RESECURED THE CLAMP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002080500083 20020805 00083 NM 2002 8 5 02215425 1 20020803 A 7700 30B370102 SENSOR DORNER DO32 DO328300 NM A VTZA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CL CLIMB 1 EA 27 425BR 3189 At 17000 feet in the climb, the crew reported a r/h engine vibration indication of 3.6 ips. The crew secured the r/h en gine, returned to CVG, and landed without further incident. Maintenance personnel removed and replaced the r/h engine v ibration sensor. An operational check was satisfactory and the aircraft was returned to service. 2 H 7 2 4T RT A55NM 2002080500084 20020805 00084 NM 2002 8 5 VNAA0207041 1 20020729 A 2400 31879001 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE #2 FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 458PS 600 284 3068 ENROUTE, THE CREW RECEIVED A BATTERY OVERHEAT INDICATION AND DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE NU MBER 2 MAIN BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE A IRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002080500085 20020805 00085 2002 8 5 VNAA0207043 4 20020729 A 3100 501122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 442JS 16775 970 3060 THE CREW REPORTED THAT THE EMERGENCY BACK UP BATTERY WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY P OWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002080500088 20020805 00088 EU 2002 8 5 02216305 1 20020804 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 305UE 41019 During preflight inspection, the crew noted that the emergency floor track light were inoperative between seat rows 3 an d 4. Maintenance personnel cleaned and secured the connector for the emergency floor track lights. An operational chec k was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002080500089 20020805 00089 EU 2002 8 5 02200330 1 20020719 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 330UE 41098 During preflight inspection, the crew reported that the forward emergency floor track lights were inoperative. Maintena nce personnel secured a loose connector for the forward emergency floor track lights. An operational check was satisfac tory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002080500090 20020805 00090 2002 8 5 AT0200066 4 20020626 A 2565 SLIDE DOUG DC9 DC932 3022066 WP L1 DOOR OUT OF POSITION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 SLIDE PACK FELL OFF DOOR L1. REINSTALLED SLIDE PACK IAW MM 25-62. 2 L 7 2 4F A6WE 2002080500091 20020805 00091 2002 8 5 AT0200067 4 20020624 A 2565 SLIDE DOUG DC9 DC932 3022066 WP R1 DOOR OUT OF POSITION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 R1 DOOR SLIDE PACK FELL OUT OF POSITION. REINSTALLED R1 SLIDE. 2 L 7 2 4F A6WE 2002080500092 20020805 00092 WP 2002 8 5 AT0200068 1 20020603 A 2150 ACM DOUG DC9 DC932 3022066 WP A/C BAY LOW A ZZDA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 15 837AT 45774 AFT LAVATORY SMOKE DETECTORS ACTIVATED ON TAKEOFF. FOUND RIGHT AIR CYCLE MACHINE GIVING OFF AN OIL SMELL. REMOVED AND REPLACED COALESCER BAG AND SERVICED AIR CYCLE MACHINE TO PROPER LEVEL. 2 L 7 2 4F A6WE 2002080500093 20020805 00093 WP 2002 8 5 AT0200069 1 20020708 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 817AT 47323 NR 1 LEFT HAND AFT ACCESSORY EMERGENCY LIGHT WILL NOT ILLUMINATE. REPAIRED BROKEN WIRE L795W18 AT VENTRAL STAIR EMERGEN CY LIGHTS PER WDM-31-51, OPS CHECK NORMAL. 2 L 7 2 4F A6WE 2002080500094 20020805 00094 SO 2002 8 5 C2XA02SH031 1 20020712 A 5320 14522459003 SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 SHV-DURING C-CHECK INSPECTION,THE SUPPORT RAMP AND REINFORCING ANGLE WERE FOUND TO BE CORRODED BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED AND REPLACED THE SUPPORT RAMP AND THE REINFORCING ANGLE IN ACCORDANCE WITH EMB-145 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2002080500095 20020805 00095 SO 2002 8 5 C2XA02SH034 1 20020710 A 5315 14521700005 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 SHV-DURING C-CHECK INSPECTION, THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 22 AND 23. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH ENGINEERING CHANGE/REPAIR AUTHORIZATION EC 5320- 01068. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080500096 20020805 00096 EU 2002 8 5 C2XA02SH035 1 20020730 A 3350 0L3042BPE LIGHT AEROSP ATR42 ATR42320 8680930 EU FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14825 170 SHV-DURING MAINTENANCE CHECK, MAINTENANCE FOUND ROW NR 1 LEFT AND RIGHT LOWER EMERGENCY EXIT SIGNS AND PASSENGER DOOR CU TOUT LOWER EMERGENCY EXIT SIGNS AND SERVICE DOOR CUTOUT LOWER EMERGENCY EXIT SIGNS ALL HAD BURNED OUT LIGHT BULBS. MAIN TENANCE REMOVED AND REPLACED ALL OF THE BURNED OUT EMERGENCY EXIT SIGNS LIGHT BULBS IN ACCORDANCE WITH ATR 42 CMM 33-91- 27 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080500097 20020805 00097 EU 2002 8 5 C2XA02SH036 1 20020730 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15827 175 SHV-DURING MAINTENANCE CHECK, MAINTENANCE FOUND PASSENGER STAIRCASE EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLA CED THE LIGHT ASSEMBLY ON PASSENGER DOOR STAIRCASE IN ACCORDANCE WITH ATR-42 CMM 33-51-25 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080500098 20020805 00098 EU 2002 8 5 C2XA02SH037 1 20020730 A 3350 0L3042BPE LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15827 175 SHV-DURING MAINTENANCE CHECK, MAINTENANCE FOUND LOWER EMERGENCY EXIT LIGHTS ON ROW NR 1 LEFT HAND AND RIGHT HAND SIDES W ERE BURNED OUT. MAINTENANCE REMOVED AND REPLACED BURNED OUT BULBS ON EMERGENCY EXIT LIGHTS IN ACCORDANCE WITH ATR-42 CM M 33-51-27 AND AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080500099 20020805 00099 EU 2002 8 5 C2XA02SH040 1 20020731 A 3350 LP1670 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16824 166 SHV-DURING MAINTENANCE CHECK, MAINTENANCE FOUND EMERGENCY AISLE PATH LIGHT AT ROW 2AB INOP. MAINTENANCE REMOVED AND REP LACED EMERGENCY EXIT AISLE PATH LIGHT BULB IN ACCORDANCE WITH ATR-42 CMM 33-51-00 AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080500100 20020805 00100 SO 2002 8 5 C2XA02TY106 1 20020621 A 5751 14569009408 BRACKET EMB 145 EMB145 3260210 SO AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND AILERON TO PCA BRACKET MOUNT HOLE WAS FOUND TO BE ELONGATED DUE TO WEA R. MAINTENANCE REMOVED AND REPLACED THE THE BRACKET IAW CONTINENTAL EXPRESS EC 5750-01177 AND EMB 145 SRM 57-60-02. TH E AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002080500101 20020805 00101 SO 2002 8 5 C2XA02TY107 1 20020702 A 5330 14520551001 SKIN EMB 135 EMB135LR 3260305 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28518 145334 TYS, DURING A SCHEDULED INSPECTION A DENT WAS FOUND IN THE SKIN BETWEEN FRAMES 25 AND 26, STRINGERS 12R AND 13R. MAINTE NANCE REFORMED THE DENT, PERFORMED DYE PENETRANT INSPECTION, ALODINED AND PRIMED IAW-EMB-GST-2071/02. THE REPAIR WAS SA TISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002080500102 20020805 00102 SO 2002 8 5 C2XA02TY111 1 20020722 A 5315 14522226003 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12934 145019 TYS DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM JUST FORWARD OF STATION 20793.0 WAS FOUND TO BE CORRODED IN SEVE RAL AREAS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB-145 SRM 51-40-02, 53-24-10, 51-20-03, 53-24-02 AND 51 -40-01. THE REPAIR WAS FOUND TO BE SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002080500103 20020805 00103 SO 2002 8 5 C2XA02TY112 1 20020722 A 5320 14522178005 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12934 145019 TYS DURING A SCHEDULED INSPECTION THE FORWARD SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE DOOR SILL IAW EMB-145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002080500104 20020805 00104 2002 8 5 C2XA02TY113 4 20020729 A 3425 COMPUTER EMB 145 EMB145ER 3260211 SO COCKPIT MALFUNCTIONED A C2XA O OTHER O OTHER CL CLIMB 1 SW 27 12934 145019 TYS AIR RETURN, PILOT REPORTED AHRS DISPLAYED ERRONEOUS HEADING. MAINTENANCE OPERATIONAL CHECKED AHRS SYSTEM IAW-EMB-1 45-MM-34-21-00-700-801A, ALL SYSTEMS OPERATIONAL CHECKED GOOD. AIRCRAFT RELEASED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080500105 20020805 00105 SO 2002 8 5 C2XA02TY114 1 20020801 A 5754 14565200401 SKIN EMB 135 EMB135LR 3260305 SO L/E SLAT DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24517 145332 TYS, DURING A SCHEDULED INSPECTION THE LEFT, NR 2 LEADING EDGE WAS FOUND DENTED AROUND A SCREW HOLE ON THE LOWER CENTER SIDE. MAINTENANCE REPAIRED THE DENT IAW-EMB-GST2378/02, THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED U PON COMPLETION OF THE INSPECTION. 2 L 7 2 4F RT T00011AT 2002080500106 20020805 00106 SO 2002 8 5 C2XA02TY115 1 20020801 A 5315 14521721005 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24517 145332 TYS, DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL WAS FOUND CORRODED FROM FRAME 13 TO 16. MAINTENANCE CUT OUT DAMA GED AREA, FABRICATED DOUBLER, SHIM AND INSTALLED, ALODINED, PRIMED AND PAINTED IAW-EMB-135/145-SRM-53-21-10 AND 51-40-02 . THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002080500107 20020805 00107 SO 2002 8 5 C2XA0SH032 1 20020713 A 5315 14533832401 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 SHV-DURING C-CHECK INSPECTION THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61. MAINTENANCE R EMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH ENGINEERING CHANGE/REPAIR AUTHORIZATION EC 5320-0 1067 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080500108 20020805 00108 SO 2002 8 5 C2XA0SH033 1 20020713 A 5315 14530657401 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 SHV-DURING C-CHECK INSPECTION THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61. MAINTENANCE REMO VED THE CORROSION AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH ENGINEERING CHANGE/REPAIR AUTHORIZATION EC 5320-0106 7 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002080500109 20020805 00109 GL 2002 8 5 CHQ000178 2 20020710 A 7200 ENGINE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL RIGHT MALFUNCTIONED A CHQA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 11 291 RIGHT ENGINE NEEDS REMOVED AND REPLACED DUE TO OIL SMELL AND VAPOR IN COCKPIT. REMOVED AND REPLACED FUEL NOZZLES NO FIX . REMOVED AND REPLACED RT ENGINE ASSY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002080500110 20020805 00110 SO 2002 8 5 CHQ000179 1 20020713 A 7722 INDICATOR EMB 145 EMB145 3260210 SO COCKPIT FLUCTUATES A CHQA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 140 RT ITT FLUX. FERRY TO IND. 2 L 7 2 4F RT T00011AT 2002080500111 20020805 00111 SO 2002 8 5 CHQ000182 1 20020723 A 2910 PRESSURE SWITCH EMB 145 EMB145 3260210 SO HYD SYSTEM FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 377 HYD 1 LO QTY AND ENG 1 HYD PUMP FAIL, THEN HYD FLUID WAS GONE AND ELECTRICAL PUMP MAKING TERRIBLE NOISE, THEN HYD 1 SYST EM FAILED. REMOVED AND REPLACED BRAKE PRESSURE SWITCH. BLED HYD SYSTEM, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2002080500112 20020805 00112 SO 2002 8 5 CX2A02RI005 1 20020715 A 2730 ELEVATOR EMB 145 EMB145LR 3260212 SO TAIL FLUTTER A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 27 15910 145455 IAD-FLT 3764- CREW REPORTED ELEVATOR SEVERE AND CONTINUOUS SHUTTER ABOVE 280 KNOTS. THE CREW DIVERTED TO BWI WITHOUT FU RTHER INCIDENT. MAINTENANCE PERFORMED ELEVATOR CABLE TENSION CHECKS FOUND TO BE WITHIN MANUFACTURER LIMITS. CHECKED SE RVO-TAB DEFLECTION FOUND TO BE WITHIN MANUFACTURER LIMITS. INSPECTED ENTIRE TAIL SECTION AS WELL AS ALL EXTERIOR PANELS NO DEFECTS NOTED. THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002080500115 20020805 00115 CE 2002 8 5 GBLA2002102 1 20020706 A 3260 SQUAT SWITCH BEECH 1900 1900D 1154162 CE LT MLG OUT OF ADJUST A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 NM 03 253GL UE253 AIRCRAFT WILL NOT PRESSURIZE AFTER TAKEOFF. MAINTENANCE ADJUSTED LEFT HAND SQUAT SWITCH, TEST FLIGHT FOR PRESSURIZATION SYSTEM SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2002080500117 20020805 00117 CE 2002 8 5 GLAB2002098 1 20020618 A 6120 STOP BEECH 1900 1900D 1154162 CE NR 1&2 ENGINE OUT OF ADJUST A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 260GL UE260 BOTH PROPS RPM REACHED 1650 RPM MAX. ADJ MAX PROP RPM STOPS ON NR 1 & NR 2 ENGINES. 2 L 7 2 4T RT A24CE 2002080500120 20020805 00120 EU 2002 8 5 MALA020443 1 20020804 A 2920 PTU BAC 146 AVRO146RJ85A 1500097 EU LF507 LF5071F NE A MALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 524XJ E2349 DURING TAXI OF FLIGHT #3444, GREEN SYSTEM HYDRAULIC HI TEMP CAUTION LIGHT ILLUMINATED AFTER 45 MINUTES OF TAXI. GATE RE TURN TO BLOCK. MAINTENANCE FOUND PTU GRINDING REMOVED AND REPLACED ptu. ALL CHECKS GOOD AT THIS TIME. 2 H 7 4 4F 4 F RT A49EU E6NE 2002080500121 20020805 00121 EU 2002 8 5 MALA020446 1 20020805 A 2560 PBE BAC 146 AVRO146RJ85A 1500097 EU A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 535XJ E2371 ON FLIGHT #3678, FWD CABIN PBE IS SOFT. MAINTENANCE REPLACED THE PBE. 2 H 7 4 4F RT A49EU 2002080500122 20020805 00122 NE 2002 8 5 GLBA2002087 2 20020622 A 7320 1182090091 SENSE LINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE FAILED A GLBA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 NM 03 220GL UE220 LEFT HAND ENGINE OVER TEMPED ON TAKEOFF. FERRY FLIGHT TO CYS, REMOVED AND REPLACED RIGHT HAND ENGINE P-3 HOSE ASSY. 2 L 7 2 4T 4 T RT A24CE E26NE 2002080500125 20020805 00125 CE 2002 8 5 GLBA2002090 1 20020624 A 2120 ODOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN DETECTED A GLBA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 118UX UE118 ELECTRICAL SMELL IN CABIN AFTER NR 2 ENGINE STARTED. INSPECTED AIRCRAFT SYSTEMS, NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 2002080500126 20020805 00126 SO 2002 8 5 GLBA2002091 1 20020625 A 3150 PIN EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE WARNING SYSTEM DAMAGED A GLBA O OTHER N FALSE WARNING CR CRUISE 1 NM 03 96ZK 120096 AURAL TAKEOFF WARNING ABOVE 65 PERCENT TORQUE IN CRUISE. REPAIRED PIN A ON P1001 AND CLEANED CANNON PLUG. 2 L 7 2 4T 4 T RT A31SO E20NE 2002080500127 20020805 00127 CE 2002 8 5 GLBA2002092 1 20020625 A 5220 DOOR BEECH 1900 1900D 1154162 CE EMERGENCY EXIT LEAKING A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 204GL UE204 THE 6C EMERGENCY EXIT LEAKS. REMOVED AND REPLACED EMERGENCY DOOR. 2 L 7 2 4T RT A24CE 2002080500128 20020805 00128 CE 2002 8 5 GLBA2002093 1 20020627 A 3610 TUBE BEECH 1900 1900D 1154162 CE BLEED AIR DAMAGED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 195GL UE195 LEFT BLEED AIR FAIL ANNUNCIATION ILLUMINATED. REPAIRED EVA TUBING, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2002080500130 20020805 00130 CE 2002 8 5 GLBA2002095 1 20020628 A 6120 CONTROL CABLE BEECH 1900 1900D 1154162 CE NR 2 PROPELLER LACK OF LUBE A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 247GL UE247 NR 2 PROP CANNOT REGULATE PROP RPM AT A HIGHER RPM. T/S CLEANED AND LUBRICATED PROP CABLES AND ROD ENDS AT RIGHT ENGINE . 2 L 7 2 4T RT A24CE 2002080500131 20020805 00131 CE 2002 8 5 GLBA2002096 1 20020630 A 2150 SOLENOID BEECH 1900 1900D 1154162 CE AIR CONDITIONING DIRTY A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 261GL UE261 RIGHT ENVIRO FAIL. CLEANED PRESSURE SOLENOID, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002080500132 20020805 00132 CE 2002 8 5 GLBA2002097 1 20020701 A 2711 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT OUT OF ADJUST A GLBA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 03 219GL UE219 AILERON REQUIRES FULL TRIM RIGHT FOR LEVEL FLIGHT. CHECKED AILERON RIGGING AND TAB RIGGING, ADJUSTED TAB INDICATOR. 2 L 7 2 4T RT A24CE 2002080500133 20020805 00133 CE 2002 8 5 GLBA2002099 1 20020703 A 3610 TUBE BEECH 1900 1900D 1154162 CE BLEED AIR DAMAGED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 261GL UE261 RIGHT BLEED AIR FAIL ON TAKEOFF. REPAIRED EVA TUBING, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002080500134 20020805 00134 CE 2002 8 5 GLBA2002102 1 20020706 A 3260 SQUAT SWITCH BEECH 1900 1900D 1154162 CE LT MLG OUT OF ADJUST A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 NM 03 253GL UE253 AIRCRAFT WILL NOT PRESSURIZE AFTER TAKEOFF. MAINTENANCE ADJUSTED LEFT HAND SQUAT SWITCH, TEST FLIGHT FOR PRESSURIZATION SYSTEM SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2002082000136 20020820 00136 NE 2002 8 20 F3LA200200202 2 20020803 A 7250 TURBINE BOEING 737 737228 13844AG NM PWA JT8 JT8D17A 52049 NE NR 2 ENGINE FAILED A F3LA E ENGINE SHUTDOWN E VIBRATION/BUFFET AP APPROACH 1 NM 03 234TR 23004 709463 ON APPROACH, THE FLIGHT CREW NOTED A VIBRATION AT 30 PERCENT POWER IN THE RIGHT (NUMBER 2) ENGINE. THE FLIGHT CREW REDU CED POWER AND MADE A NORMAL LANDING. THE ENGINE WAS SHUT DOWN AND TAKEN TO THE GATE. DURING THE WALK AROUND INSPECTION , MAINTENANCE NOTED METAL FUSED TO THE ROSEBUD AND SIDES OF THE EXHAUST. 2 L 7 2 4F 4 F RT A16WE E2EA 2002080500135 20020805 00135 WP 2002 8 5 PNSA020702 2 20020718 A 7230 8934825 COMPRESSOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP CRACKED A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 41NE 23766 3255 AC741B P44724 Engine removed for low power. During disassembly found 2nd stage compressor missing one piece from trailing edge of vane appeared to be fatigue crack. 2 L 7 2 4T 4 T RT A8SW E4WE 2002080500136 20020805 00136 NM 2002 8 5 F3LA200200205 1 20020723 A 5313 TIE CLIP BOEING 737 737317 138447P NM CRACKED A F3LA O OTHER O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION NOTED CRASKS IN TIE CLIP TO STRINGER AT TOP RIVET AT STA 663 STR 10 LH. MAINTENANCE REPAIR ED THE CONDITION BY INSTALLING A NEW CLIP AT STA 663 STR 10 L IN ACCORDANCE WITH SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002080500137 20020805 00137 NE 2002 8 5 PNSA020707 3 20020731 A 6114 660710395 HUB ROTOL SAAB SF340 340B 7860101 EU ROTOL R390 R3904123F27 NE CRACKED A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 675PA 22038 1386 DRG1199089 340B206 DRG1199089 Prop was removed to reseal blades and during repair rear hub half was found cracked. 2 L 7 2 4T RT A52EU 6 C P31NE 2002080500138 20020805 00138 NM 2002 8 5 F3LA200200206 1 20020723 A 5313 TIE CLIP BOEING 737 737317 138447P NM CRACKED A F3LA O OTHER O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION FOUNG A BROKEN TIE CLIP TO STRINGER AT STA 639 STR 4L. mAINTENANCE INSTALLED NEW STRINGER TIE CLIP AT STA 639 STR 4L IN ACCORDANCE WITH SRM 51-10-02 AND 51-40-03. 2 L 7 2 4F RT A16WE 2002080500139 20020805 00139 NM 2002 8 5 F3LA200200209 1 20020723 A 5310 TIE CLIP BOEING 737 737317 138447P NM CRACKED A F3LA O OTHER O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION NOTED STRINGER TIE CLIP AT STA 727E, STR 7 L WAS CRACKED. MAINTENANCE REMOVED THE CLIP, FA BRICATED AND INSTALLED A NEW CLIP IN ACCORDANCE WITH THR ERQUIREMENTS OF BOEING DRAWING 69-35352 AND SRM 51-30-02 AND SR M 51-40-02. 2 L 7 2 4F RT A16WE 2002080500140 20020805 00140 NM 2002 8 5 C1HA200286004 1 20020726 A 3350 BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 686CA 22021 R1 DOOR EMERGENCY EXIT LIGHT ( ABOVE DOOR ) INOPR&R PORBITABLE EMERGENCY EXIT LIGHT ASSEMBLY & BATTERYS IAW 73-27 MM 33 -50-101 ( R1 DOOR ) 2 L 7 3 4F A3WE 2002080500141 20020805 00141 NM 2002 8 5 F3LA200200211 1 20020723 A 5310 TIE CLIP BOEING 737 737317 138447P NM CORRODED A F3LA O OTHER O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION NOTED CORROSION IN STRINGER CLIP AT STA 787, STR 26 R. MAINTENANCE FABRICATED STRINGER CLI P IN ACCORDANCE WITH BOEING DRAWING 69.35352. THE PART WAS THEN TREATED, PRIMED, PAINTED AND INSTALLED IN ACCORDANCE WI TH THE REQUIREMENTS OF SOPM 20.41.02 AND SRM 51.40.02. 2 L 7 2 4F RT A16WE 2002080500142 20020805 00142 NM 2002 8 5 F3LA200200212 1 20020723 A 5310 FLOOR PANEL BOEING 737 737317 138447P NM A F3LA O OTHER O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION NOTED LIGHT CORROSION IN THE AFT CARGO PIT AT FRAME STA 727 C, UNDER LEFT FLOOR TRANSITION PANEL. MAINTENANCE REMOVED THE SURFACE CORROSION IN ACCORDANCE WITH SRM 51-10-02, TREATED, PRIMED AND PAINTED THIS AREA IN ACCORDANCE WITH THE REQUIREMENTS OF MM 51-21-4A AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002080500143 20020805 00143 NM 2002 8 5 QXEA0201101 1 20020803 A 3350 6138001 BATTERY BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 2177 227 4051 PDX- NUMBER 4,5,6 AND 7 CENTER AISLE OVERHEAD EMERGENCY LIGHTS,AFT CENTER OVERHEAD EMERGENCY EXIT SIGN AND EXIT SIGN ON FORWARD SIDE OF AFT RIGHT HAND GALLEY BULKHEAD INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS. 2 H 7 2 4T RT A13NM 2002081500134 20020815 00134 NM 2002 8 15 F3LA200200215 1 20020723 A 5311 FRAME BOEING 737 737317 138447P NM FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION NOTED A DENT IN THE RADIUS OF THE FRAME AT BS 727 B, BETWEEN STRINGERS 22 L AND 23 L. MAIN TENANCE FABRICATED A REPAIR DOUBLER IAW SRM 51-70-11 AND INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002080600001 20020806 00001 NM 2002 8 6 UPS02438940 1 20020630 A 5310 FRAME BOEING 747 747123F NM BS 2231 S24L-25L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C LH BS 2231 FRAME TWO EACH FASTENER HOLES CRACK FOUND AT REVEAL AND STRAP. REVEAL AND STRAP REPAIR ED AS PER RS R-53-61-34845. (UPS EO B747-5310-17209-A, APPENDIX A) 2 L 7 4 4F A20WE 2002080600002 20020806 00002 NM 2002 8 6 UPS02438941 1 20020630 A 5310 FRAME BOEING 747 747123F NM BS 2231 S24R-26R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C R/H BS 2231 FRAME FOUND TWO CRACK AT REVEAL AND STRAP BETWEEN STR TO STR 26 AND CRACKS END MARKED. REVEAL & STRAP REPAIRED AT BS 2231 RH FRAME BETWEEN STR 24-26 AREA AS PER RS R-53-61-34845.(UPS EO B747-5310-17029-A, APPENDIX A) 2 L 7 4 4F A20WE 2002080600003 20020806 00003 NM 2002 8 6 UPS02438942 1 20020705 A 5310 STRAP BOEING 747 747123F NM BS 2231 S24R-25R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C R/H BS 2231 STR 24-26 AT REPAIR AREA FASTENER HOLES FOUND 1 EA FASTENER HOLE CRACK AT STRAP LAYER APPR OX 3/16" INCH IN LENGTH AND CRACK END AS MARKED. FOR DETAIL PLS REFER ATTACHED SKETCH. REVEAL & STRAP REPAIRED AT BS 2231 RH FRAME BETWEEN STR 24-26 AREA AS PER RS R-52-61-34845.(UPS EO B747-5310-17209-A, APPENDIX A) REFER HAECO NRC#621 5 FOR DETAIL. 2 L 7 4 4F A20WE 2002080600004 20020806 00004 NM 2002 8 6 UPS02438943 1 20020628 A 5310 FRAME BOEING 747 747123F NM BS 2231 S26R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C M/D - R5 DOOR FWD CUTOUT REVEAL CRACKED. BS 2231 STR 26R FRAME REVEAL REPAIRED A PER RS R-53-61-34 845, (UPS EO B747-5310-17209-A, APPENDIX A) REFER HAECO NRC# 6215 FOR DETAIL. 2 L 7 4 4F A20WE 2002080600005 20020806 00005 NM 2002 8 6 UPS02438947 1 20020704 A 5310 LONGERON BOEING 747 747123F NM BS 1460 LBL 110 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C LH BLG W/W - FS 1460 OVERWING LONGERON AFTER SPLICE FTG REMOVAL & CORROSION CLEAN UP, FOUND 3" LONG CR ACK AT LONGERON. BS 1460 LH OVERWING LONGERON REPAIRED AS PER HX RS R-53-43-34843. (UPS EO# B747-5310-17206-A) REFER HAECO NRC# 6792 FOR DETAIL. 2 L 7 4 4F A20WE 2002080600006 20020806 00006 NM 2002 8 6 UPS02438954 1 20020709 A 5310 LONGERON BOEING 747 747123F NM BS 1460 - 1470 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX LH OVERWING LONGERON AFT SPLICE END AT STA 1460 - 1470, FWD HOLE FOUND CRACKED 1/4" LONG & 1/4" DEP TH FROM TOP SURFACE WITH NDT AND MID & AFT HOLES BORE CORROSION IS REVEALED. BS 1350 - 1480 RH OVERWING LONGERON REP AIRED IAW RS R-53-43-34843. (UPS EO# B747-5310-17206-A) 2 L 7 4 4F A20WE 2002080600007 20020806 00007 NM 2002 8 6 UPS02438956 1 20020627 A 5330 SKIN BOEING 747 747123F NM BS 1800-1920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C AFT LOWER CARGO DOOR CUTOUT UPPER CORNER ( FWD SIDE AND AFT SIDE ) FOUND FASTENER HOLES ( TOTAL : 3 EA ) CRACKED AT SKIN. AFTER LOWER CARGO DOOR CUTOUT UPPER CORNER ( FWD SIDE & AFT SIDE ) REPAIRED AS PER RS R-53-61-34 833.(UPS RA ENGINEERING FILE NUMBER# 747-53-20086) 2 L 7 4 4F A20WE 2002080600015 20020806 00015 NM 2002 8 6 02FDEA00413 1 20020620 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 CHAFING ON FRAME FROM HYDRAULIC LINE AT BS 560, STR 4R. 2 L 7 3 4F RT A3WE 2002080600016 20020806 00016 NM 2002 8 6 02FDEA00414 1 20020620 A 5531 SPAR BOEING 727 727200 138407E NM VERTICAL STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 VERT FIN MID SPAR IS CHAFED AT STA 228, LEFT HAND SIDE. REMOVED AND REPLACED VERT FIN PER EA 7-5510-64976. 2 L 7 3 4F RT A3WE 2002080600017 20020806 00017 NM 2002 8 6 02FDEA00415 1 20020620 A 5531 SPAR BOEING 727 727200 138407E NM VERTICAL STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 VERT FIN MID SPAR IS CHAFED AT STA 228 RIGHT HAND SIDE. REMOVED AND REPLACED VERT FIN MID SPAR PER EA 7-5510-64975. 2 L 7 3 4F RT A3WE 2002080600018 20020806 00018 NM 2002 8 6 02FDEA00416 1 20020616 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 186FE 18872 SKIN DENTED AT BS 720, STR 16R. 2 L 7 3 4F RT A3WE 2002080600019 20020806 00019 NM 2002 8 6 02FDEA00418 1 20020615 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 186FE 18872 CORROSION STR 19L TO 23L, BS 350-360 SKIN BULGING AROUND FASTENERS. REMOVED AND REPLACED SKIN PER EA 7-5330-64974 & SRM 53-30-3. 2 L 7 3 4F RT A3WE 2002080600020 20020806 00020 NM 2002 8 6 02FDEA00419 1 20020618 A 1430 TLV200528 FASTENER DOUG MD11 MD11 3023602 NM CENTER WING BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 DURING B-CHECK FOUND 1 TAPER LOCK FASTENER BROKEN ON REAR SPAR LOWER CAP OF CENTER WING REF EA 1-5314-64689. R/R FASTEN ER PER E.A. 2 L 7 3 4F RT A22WE 2002081500065 20020815 00065 NM 2002 8 15 371PA0009 1 20020803 A 2612 9718904 CONTROL BOX BOEING 737 737306 13844BG NM FIRE WARNING MALFUNCTIONED A PIDA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 05 371PA 23543 FORWARD CARGO FIRE WARNING IN FLIGHT. FIRED NR 1 & 2 EXTINGUISHER BOTTLES. FOUND CARGO FIRE SUPPRESSION SYSTEM CONTROL PANEL FAULTY. COMPONENTS REPLACED NR 1 & 2 BOTTLES, METERING VALVE, DIVERTER VALVE, AND CONTROL PANEL. 2 L 7 2 4F RT A16NE 2002080600021 20020806 00021 NM 2002 8 6 ANCF200200016 1 20020801 A 3245 3203100010 PIN DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE DAMAGED W ANCF L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 23 632CT 49632 DURING APPROACH LEFT INBOARD ANTISKID ANNUNCIATION CAME ON, ABNORMAL CHECK LIST WAS PERFORMED AND IT WAS UNSUCCESFULL.DU E TO SHORT RUNWAY IN PEREIRA CREW RETURNED TO BOGOTA. ANTI-SKID CCONTROL TEST AND ANTI-SKID CONTROL BOX BITE WERE PERFOR MED IAW AMM 32-43-00 TEST ON GROUND IS SATISFACTORY. REPAIRED WIRE LINE "A" IN ELECTRICAL CONNECTOR TRANSDUCER No2 IAW A MM 32-43-00. 2 L 7 2 4F 4 F RT E9NE 2002080600022 20020806 00022 2002 8 6 070201 4 20020628 A 2210 TRIM SWITCH ISRAEL 1124 1124A 4500103 EU AUTOPILOT SYS MALFUNCTIONED E ESUA B EMER. DESCENT F FLT CONT AFFECTED CR CRUISE 1 CE 03 118MP 340 PILOT REPORTED UNCOMMAND VIOLENT ROLL TO LEFT. CREW LOST 15000 FT OF ALTITUDE BEFORE GAINING CONTROL. CONTINUED TO VAN NUYS & LANDED WITHOUT INCIDENT. GULFSTREAM TECHNICAL OPERATIONS CAME TO OBSERVE TEST IAW IAI REF LETTER DATED 6-26-2002 . PERFORMED A OPS CHECK OF THE RUDDER, RUDDER TRIM, THRUST REVERSER, AIRBRAKES, AND GROUND BRAKES BOTH WITH THE LANDING GEAR UP AND DOWN. ADDITIONALLY WITH THE AIRCRAFT IN THE GROUND MODE AND AIR MODE. PERFORMED A MEG-O-METER INSPECTION O F THE RUDDER TRIM SYSTEM WIRING, NO DEFECTS NOTED. REPLACED THE RUDDER TRIM SWITCH AND THE THRUST REVERSER FAULT TEST S WITCH. REPLACED SWITCHES WERE TAKEN TO GULFSTREAM TECHNICAL FOR TESTING. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 M 7 2 4F A2SW 2002080600023 20020806 00023 CE 2002 8 6 20025 1 20020701 A 3260 1CH16 SWITCH LEAR 35 35LEAR 5170600 CE LT MLG OUT OF ADJUST E STZA O OTHER N FALSE WARNING CR CRUISE 1 AL 03 90WR 15831 995 35022 PILOT REPORTED, LEFT MAIN GEAR UNSAFE LIGHT CAME ON THEN GEAR PARTIALLY HUNG OUT. MAINTENANCE ADJUSTED LEFT INBOARD GEA R DOOR UPLATCH SWITCH. RIGGING PROCEDURES PERFORMED PER LEAR 35 MM 32-31-02. OPERATIONAL CHECK FLIGHT PERFORMED WITH S ATISFACTORY RESULTS. 2 L 7 2 4F A10CE 2002080600024 20020806 00024 CE 2002 8 6 65000581 1 20020716 A 3260 WARNING LIGHT CESSNA 650 650 2076802 CE COCKPIT ILLUMINATED E ERYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 70DJ 6500058 ON CLIMBOUT FROM PDK, RETRACTED GEAR AND LEFT MAIN GEAR LIGHT STAYED ILLUMINATED. PERFORMED GEAR EXTENTION SUCCESSFULLY , LANDED PDK UNEVENTFULLY. 2 L 7 2 4F A9NM 2002080600025 20020806 00025 CE 2002 8 6 65000582 1 20020531 A 5730 SKIN CESSNA 650 650 2076802 CE RT WING DAMAGED E ERYA K NONE O OTHER TX TAXI/GRND HDL 1 CE 07 70DJ 6500058 FOUND SMALL HOLE IN RIGHT OUTBOARD HEATED LEADING EDGE. 2 L 7 2 4F A9NM 2002080600026 20020806 00026 CE 2002 8 6 6500582 1 20020717 A 3260 UPLOCK SWITCH CESSNA 650 650 2076802 CE LT MLG DISCONNECTED E ERYA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 70DJ 6500058 UPON TAKEOFF AND SUBSEQUENT CLIMB, RETRACTED GEAR AND LEFT MAIN GEAR GREEN LIGHT REMAINED ILLUMINATED AFTER COMPLETE CYC LE. MAINTENANCE REPAIRED OPEN CIRCUIT ON UPLOCK SWITCH. 2 L 7 2 4F A9NM 2002080600027 20020806 00027 2002 8 6 2002F00764 4 20020619 A 2210 DAMPENER ISRAEL 1124 1124A 4500103 EU AUTOPILOT SYS FAULTY E ESUA B EMER. DESCENT F FLT CONT AFFECTED CR CRUISE 1 CE 03 118MP 340 AT CRUISE ALTITUDE THE AIRCRAFT EXPERIENCED FULL LEFT RUDDER DEFLECTION. EMERGENCY PROCEDURES WHERE INITIATED. DURING RECOVERY PROCEDURES ALTITUDE LOSS OF 15,000 FEET. YAW DAMPENER WAS DISABLED AND AIRCRAFT CONTROLS RETURNED TO NORMAL. AIRCRAFT RETURNED TO DESTINATION WITHOUT FURTHER INCIDENT. 2 M 7 2 4F A2SW 2002080600028 20020806 00028 NM 2002 8 6 2002F00782 1 20020426 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CORROSION ON FRAME STATION 116 FROM STRINGER 30R TO 27R. (M) 2 L 7 3 4F A3WE 2002080600029 20020806 00029 NM 2002 8 6 2002F00783 1 20020426 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND DENT WITH SHARP CREASES AT STATION 520R, BETWEEN STRINGER 15R AND 16R. (M) 2 L 7 3 4F A3WE 2002080600030 20020806 00030 NM 2002 8 6 2002F00784 1 20020426 A 5320 INTERCOSTAL BOEING 727 727225 1384077 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CRACK ON THE INTERCOSTAL AND SPLICE, IN THE MAIN CARGO COMPARTMENT, AT STATION 346 TO 358 STRINGER 16L . (M) 2 L 7 3 4F A3WE 2002080600031 20020806 00031 NM 2002 8 6 2002F00785 1 20020426 A 5320 CHANNEL BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND HOLES AT THE EDGE OF THE 'U' AND 'Z' CHANNELS, IN THE AFT CARGO PIT STATION 1017 RBL 1.78 AND 5.38. ( M) 2 L 7 3 4F A3WE 2002080600032 20020806 00032 NM 2002 8 6 2002F00786 1 20020426 A 5320 CHANNEL BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CUT MARKS IN THE AFT CARGO U-CHANNEL AT STATION 1040 LBL 1.78. (M) 2 L 7 3 4F A3WE 2002080600033 20020806 00033 NM 2002 8 6 2002F00787 1 20020426 A 5320 THRESHOLD BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CORROSION ON THE L2 DOOR THRESHOLD Z-ANGLE AND AROUND NUTPLATES AT STATION 1030 TO STATION 1070 STRING ER 17L. (M) 2 L 7 3 4F A3WE 2002080600034 20020806 00034 NM 2002 8 6 2002F00788 1 20020426 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CORROSION ON FRAME 1166 LOWER ATTACH POINT, BETWEEN STRINGER 30L AND 29L, FORWARD AND AFT SIDES. (M) 2 L 7 3 4F A3WE 2002080600035 20020806 00035 NM 2002 8 6 2002F00789 1 20020426 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CORROSION ON FRAME 1166 FROM STRINGER 29R TO 28R. (M) 2 L 7 3 4F A3WE 2002080600036 20020806 00036 NM 2002 8 6 2002F00790 1 20020425 A 5755 651734874 SKIN BOEING 727 727225 1384077 NM SPOILER DELAMINATED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND DELAMINATION ON NR 8 GROUND SPOILER LOWER SURFACE. (M) 2 L 7 3 4F A3WE 2002080600037 20020806 00037 NM 2002 8 6 2002F00791 1 20020424 A 5753 652163017 SKIN BOEING 727 727225 1384077 NM T/E FLAP DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND DENT AT RIGHT FORE FLAP LOWER SURFACE WBL 95. (M) 2 L 7 3 4F A3WE 2002080600038 20020806 00038 NM 2002 8 6 2002F00792 1 20020424 A 5740 BACB30NE9H104 PIN BOEING 727 727225 1384077 NM LT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND LEFT WING FORWARD BOTTLE PIN CORRODED. (M) 2 L 7 3 4F A3WE 2002080600039 20020806 00039 NM 2002 8 6 2002F00793 1 20020528 A 5260 WEB BOEING 727 727222 1384073 NM VENTRAL STAIRS CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CRACK AT VENTRAL STAIRWAY, RIGHT TORQUE BOX VERTICAL WEB, AT LOWER LIGHTENING HOLE, .25 INCH LONG, AT STATION 1263. (M) 2 L 7 3 4F A3WE 2002080600040 20020806 00040 NM 2002 8 6 2002F00794 1 20020528 A 5260 WEB BOEING 727 727222 1384073 NM VENTRAL STAIRS CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CRACK AT VENTRAL STAIRWAY, RIGHT TORQUE BOX VERTICAL WEB, .75 INCHES LONG AT LIGHTENING HOLE, AT STATI ON 1235. (M) 2 L 7 3 4F A3WE 2002080600041 20020806 00041 NM 2002 8 6 2002F00795 1 20020528 A 5260 WEB BOEING 727 727222 1384073 NM VENTRAL STAIRS CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CRACK AT VENTRAL STAIRWAY, IN LEFT TORQUE BOX VERTICAL WEB, .5 INCH LONGERON AT STATION 1235. (M) 2 L 7 3 4F A3WE 2002080600042 20020806 00042 NM 2002 8 6 2002F00796 1 20020528 A 5260 WEB BOEING 727 727222 1384073 NM VENTRAL STAIRS CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CRACK AT VENTRAL STAIRWAY, LEFT TORQUE BOX VERTICAL WEB, AT STATION 1223. M) 2 L 7 3 4F A3WE 2002080600043 20020806 00043 NM 2002 8 6 2002F00797 1 20020702 A 3260 1899 SENSOR BOEING 727 727224 1384076 NM LT MLG FAULTY A FX7A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 296SC 22449 OUT OF SVMC AFTER TAKEOFF WITH LANDING GEAR LEVER IN UP POSITION AND FLAPS FROM 5 DEGREES TO 2 DEGREES THE TAKEOFF WARNI NG HORN STARTED TO SOUND, ACCOMPLISHED AIR GROUND SENSOR PROCEDURES AND AIRCRAFT RETURNED TO SVMC. THE LEFT GROUND AIR SENSOR WAS REPLACED PER MM 32-09-221. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002080600044 20020806 00044 NM 2002 8 6 2002F00798 1 20020618 A 3350 1000679 SIGN BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 802MA 22433 FOUND EXIT SIGN OVER R-1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY OVER R-1 DOOR AND OPS CHECKED. SATIS FACTORY AS PER MM 33-50-71. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002080600045 20020806 00045 NM 2002 8 6 2002F00799 1 20020617 A 3350 1000679 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 DURING DEPARTURE CHECK, FOUND COCKPIT DOOR EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW MM 33-50-71. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002080600046 20020806 00046 NM 2002 8 6 AALA20020766 1 20020525 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT AT 29 H/J INOPERATIVE. REPINNED EMERGENCY ESCAPE PATH L IGHT CONNECTOR AT SEAT 29 H/J. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002080600047 20020806 00047 NM 2002 8 6 AALA20020767 1 20020526 A 3350 POWER SUPPLY BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 EZE - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING FOR RIGHT SEATS 32 THROUGH 41 INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT POWER SUPPLY M739. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002080600048 20020806 00048 NM 2002 8 6 AALA20020768 1 20020523 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 36H INOPERATIVE. REPAIRED SEAT CONNECT OR AT SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002080600049 20020806 00049 EU 2002 8 6 AALA20020776 1 20020530 A 3350 321441 POWER SUPPLY AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 25071 514 JFK - FOUND 2R DOOR OVERHEAD EXIT SIGN AND OVERHEAD CEILING EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY FOR 2R DOOR EX IT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002080600050 20020806 00050 2002 8 6 AALA20020790 4 20020530 A 3417 ADC AIRBUS 300 A300B4605R 3930308 EU E/E BAY FAULTY A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 14061 471 MIA - FLT 1901 - EN ROUTE MAI-SDQ - LEFT CAPTAINS AIRSPEED ABOUT 50 KNOTS SLOW AT 250 KNOTS. 20 KNOTS SLOW AT 150 KNOTS . RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED NR 1 AIR DATA COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002080600051 20020806 00051 NM 2002 8 6 AALA20020791 1 20020528 A 5315 FLOORBEAM BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AA 24524 TUL - FOUND FS 1640 FLOORBEAM T-CAP CORRODED FROM BL 10L TO BL 61R. REPLACED 1640 T-CAP FROM BL 10L TO BL 61R PER SRM 5 3-00-51-2. (M) 2 L 7 2 4F RT A2NM 2002080600052 20020806 00052 EU 2002 8 6 AALA20020798 1 20020603 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1413A 11376 SAT - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT FLOOR PATH LIGHTING WOULD NOT ILLUMINATE. RECONNECTED FORWAR D EMERGENCY EXIT FLOOR PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002080600053 20020806 00053 WP 2002 8 6 ASAA0280147 1 20020426 A 2560 39361901 FITTING DOUG DC9 DC983 3022083 WP CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PAE - DURING 30K-CHECK, FOUND CORROSION ON FORWARD SERVICE DOOR GIRT BAR ATTACH FITTINGS ON FLOORBOARD. REPLACED FITTIN GS PER SRM 51-30-1. (M) 2 L 7 2 4F RT A6WE 2002080600054 20020806 00054 WP 2002 8 6 ASAA0280149 1 20020428 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SAN - DURING PREFLIGHT CHECK, DETERMINED THAT THE 1ST CLASS CABIN EMERGENCY TRACK LIGHTING WAS INOPERATIVE. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002080600055 20020806 00055 NM 2002 8 6 2002F00801 1 20020303 A 2120 SMOKE BOEING 727 727282 138408T NM PWA JT8 JT8D17 52049 NE CABIN DETECTED A RYNA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 07 281SC 21949 688213 AFTER LANDING AT GRR, THE CABIN FILLED WITH SMOKE AFTER ALL THREE ENGINES WERE IN REVERSE THRUST. NO EMERGENCY WAS DECL ARED. SMOKE CLEARED AFTER ENGINES WERE SHUT DOWN. (M) 2 L 7 3 4F 4 F RT A3WE E2EA 2002080600056 20020806 00056 EU 2002 8 6 2002F00800 1 20020520 A 2810 L95F50603 RELIEF VALVE AIRBUS 320 A320233 3930329 EU LT WING TANK DAMAGED A RJEF A UNSCHED LANDING O OTHER CL CLIMB 1 SO 23 484TA 1523 JFK - FLT 580 - DURING CLIMB, AN IN FLIGHT FUEL TRANSFER WAS EXPERIENCED FROM RIGHT TANK TO THE CENTER TANK. AIRCRAFT R ETURNED TO JFK STATION FOR MAINTENANCE. AT JFK STATION, TECHNICIANS PERFORMED INSPECTION AND FOUND THE OVERPRESSURE PRO TECTOR 96 QM DAMAGED IN THE CENTER TANK TO THE LEFT WING. IT WAS CHANGED AND TESTED AS PER AMM 28-12-41. RESULTS WERE NORMAL FOR OVERPRESSURE PROTECTOR 96 QM, ALSO AN INSPECTION FOR OVERWEIGHT LANDING WAS PERFORMED AS PRE AMM 05-51-11 AND NO DISCREPANCIES WERE FOUND. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2002080600057 20020806 00057 WP 2002 8 6 ASAA0280159 1 20020504 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 53079 PDX - DURING LINE CHECK, FOUND EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSO CIATED BATTERY PACK, POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002080600058 20020806 00058 NM 2002 8 6 PCAA0208085 1 20020802 A 2910 A44700009 ACTUATOR DHAV DHC8 DHC8102 2809003 NM INBOARD RIGHT CRACKED A PCAA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 EA 13 835EX 26694 26694 289 PHL-FLIGHT#3686. CREW REPORTED LOSS OF #1 HYDRAULIC SYSTEM FLUID JUST AFTER TAKEOFF.EMERGENCY DECLARD, AND AIRCRAFT RETU RNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND FOUND INBOARD RIGHT ROLL SPOILER ACTUATOR CRACKED AND LEAKING. INBOARD RIGHT ROLL SPOILER ACTUATOR REPLACED IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 27-14-05. LEAK CHECK GOOD . AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080600059 20020806 00059 NM 2002 8 6 C1HA200288015 1 20020730 A 3040 65528038 CONTROLLER BOEING 727 7272S7 138407Z NM A C1HA A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 15 688CA 22344 L1 Window heat inop.Removed and replaced L1 window heat control unit IAW MM 30-41-13. Ops check good. 2 L 7 3 4F A3WE 2002080900087 20020809 00087 NM 2002 8 9 2002UALA01206 1 20020725 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 EXTERNAL FUSELAGE DENT AFT OF DOOR 2L BODY STATION 740 STRINGER 16L. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALL ED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080600060 20020806 00060 NM 2002 8 6 2002UALA01221 1 20020729 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 2 CRACKS AT FWD SIDE OF LH FUSELAGE BETWEEN WINDOWS 10 AND 11. FIRST CRACK IS ABOVE ORANGE PAINT STRIPE ABOUT 10 INCHES AND IS ABOUT ONE TO ONE-AND-A-HALF INCHES LONG. THE AFT CRACK IS AT THE TOP PORTION OF THE ORANGE PAINT STRIPE JUST AFT OF PATCH LOWER AFT CORNER ABOUT ONE INCH LONG. MAJOR REPAIR ACCOMPLISHED. SKIN DOUBLERS INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080600061 20020806 00061 NM 2002 8 6 2002UALA01250 1 20020730 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 FUSELAGE STRINGER 16L DENTED STATION 610-615. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPL ICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080600062 20020806 00062 NM 2002 8 6 2002UALA01255 1 20020731 A 5311 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 FORWARD CABIN #2 LH SERVICE DOOR CUTOUT INTERCOSTAL CRACKED, BODY STATION 680 JUST BELOW STRINGER 11L CRACKED TWO PLACES . SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080600063 20020806 00063 NM 2002 8 6 2002UALA01256 1 20020731 A 5311 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 FORWARD CABIN #2 RIGHT HAND SERVICE DOOR CUTOUT INTERCOSTAL CRACKED, BODY STATION 680 FORWARD OF #4 DOOR STOP PIN FITTIN G. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080600064 20020806 00064 NM 2002 8 6 2002UALA01257 1 20020731 A 5311 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 CAB INTERCOSTAL #12 LEFT HAND SIDE HAS CRACK AT O-B RADIUS BODY STATION 680. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOM PLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080600065 20020806 00065 NM 2002 8 6 2002UALA01265 1 20020731 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 EXTERIOR FUSELAGE BODY STATION 600-620 HAS SEVERAL DENTS ON SKIN FORWARD OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND TRIPLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080600066 20020806 00066 NM 2002 8 6 2002UALA01266 1 20020731 A 5311 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 FORWARD CABIN #2 SERVICE DOOR CUTOUT, INTERCOSTAL CRACKED AT BODY STATION 680 JUST BELOW STRINGER 11R. MAJOR REPAIR ACC OMPLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080600067 20020806 00067 NM 2002 8 6 2002UALA01272 1 20020801 A 5313 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FRACTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 RIGHT HAND WING LOWER CHORD SHEAR TIE AT WS313.5 BETWEEN STRINGER 10 AND STRINGER 11 WAS FRACTURED DURING FASTENER INSTA LLATION. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080600068 20020806 00068 NM 2002 8 6 2002UALA01273 1 20020802 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 FUSELAGE SKIN DENTED 6.75 IN IN FORWARD OF BODY STATION 1720 AND .5 IN BELOW STRINGER 20L. MAJOR REPAIR ACCOMPLISHED. E XTERNAL FUSELAGE SKIN REPAIRED. DOUBLER AND FILLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080600069 20020806 00069 EA 2002 8 6 CA020508001 2 20020506 A 7322 SHAFT BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA FUEL CONTROL SEIZED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA (CAN) AIRCREW EXPERIENCED LT ENGINE TORQUE FLUCTUATION FOLLOWED BY ITT RISE. POWER LEVER INPUT WAS INEFFECTIVE AT THIS T IME. ENGINE WAS SHUT DOWN AT FLIGHT LEVEL 180. INTERCONNECTING SHAFT BETWEEN FCU AND EDP (FCU DRIVE COUPLING)WAS FOUND S HEARED. FCU INPUT SHAFT BEARING WAS FOUND SEIZED. (FCU LAST OVERHAUL WAS MARCH 1995.) 1 L 7 2 3T 4 T RT 3A20 E4EA 2002080600070 20020806 00070 2002 8 6 CA020528006 4 20020521 A 2330 TH41JSK21W PROJECTOR BOEING 767 767300 1385204 NM GE CF6 CF680C2B6F 30025 NE CABIN INOPERATIVE W H DEACTIVATE SYST/CIRCUITS B M SMOKE/FUMES/ODORS/SPARKS OVER TEMP TX TAXI/GRND HDL 1 CA (CAN) NO PROJECTOR IN CABIN B WORKED FOR SAFTY DEMO. (L1075533) ELECTRICAL CONNECTOR REMOVED FROM PROJECTOR PRIOR TO TAK EOFF AND FLIGHT CONTINUED WITH SYSTEM DEACTIVATED. FINAL FIX WAS NEW PROJECTOR INSTALLED AND SYSTEM CHECKED SERVICEABLE . 2 L 7 2 4F 4 F RT A1NM E13NE 2002080600072 20020806 00072 SW 2002 8 6 CA020605007 1 20020604 A 6220 HOUSING BELL 406040400119 BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/R GEARBOX MISMANUFACTURED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA A1076 (CAN) DURING AN OVERHAUL IT WAS FOUND THAT AN OIL PASSAGE WAS MISSING IN THE GEARBOX HOUSING BEARING BORE OF THE INPUT S HAFT DUPLEX BEARING. AFTER INVESTIGATION, IT WAS DETERMINED THAT ALL A/C FROM A/C S/N 53392 ARE AFFECTED AS ARE ALL SPAR ES SHIPPED SINCE AUGUST 1999. 1 G 7 1 3U 3 U O H2SW E1GL 2002080600074 20020806 00074 2002 8 6 RAIA00207211 4 20020711 A 3420 7003110901 DISPLAY JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 550HK 13308 41039 5502-STL- CAPTAINS ELECTRONIC FLIGHT INFORMATION SYSTEM DISPLAY WENT BLANK. MAINTENANCE REMOVED AND REPLACED THE EFIS DI SPLAY, OPS CK OK. 2 L 7 2 4T RT A41NM 2002080600075 20020806 00075 EU 2002 8 6 RAIA00207212 1 20020711 A 7700 3103898 PRESSURE SWITCH JETAIR JETSTM JETSTM4101 1500501 EU A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 571HK 41090 5605-STL- RIGHT GREEN BETA LIGHT DOES NOT ILLUMINATE WHEN ENGINE IS OPERATING. MAINTENANCE REMOVED AND REPLACED THE RIGH T ENGINE BETA SWITCH, OPS AND LK CK OK. 2 L 7 2 4T RT A41NM 2002080600076 20020806 00076 EU 2002 8 6 YENA200220 1 20020802 A 2425 IDC AIRBUS 320 A320232 3930326 EU A YENA K NONE G MULTIPLE FAILURE CR CRUISE 1 EA 15 521JB 1554 1452 Flt 95, JFK to OAK, At cruise, Multiple spurious failures during flight: Capt PFO flickering, main PNL & PFD/main PNL l ights flickering GPWS. (unassociated w/above) FAL, RA#1 fail, nosewheel steering fail, ILS #1 fail, WX radar spoking & i ndicating receiver & transmitter failure. Removed & replaced 3XC contactor per 24-25-55-401, Ops chk per task 24-25-00-5 01 and checks OK. 2 L 7 2 4F RT A28NM 2002080600077 20020806 00077 WP 2002 8 6 ASAA0280152 1 20020501 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 PDX - DURING PREFLIGHT CHECK, FOUND INOPERATIVE EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN. REPLACED MODULE CONNECTOR AN D SECTION OF WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002080600078 20020806 00078 WP 2002 8 6 ASAA0280153 1 20020501 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 ANC - DURING LINE CHECK, FOUND INOPERATIVE EMERGENCY TRACK LIGHT IN CABIN. REPAIRED DAMAGED WIRE AND RECONNECTED. LIGH TS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002080600079 20020806 00079 WP 2002 8 6 ASAA0280154 1 20020502 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 SEA - DURING LINE CHECK, FOUND TAILCONE AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002080600080 20020806 00080 WP 2002 8 6 ASAA0280155 1 20020502 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND AFT CARGO BAY FRAME CORRODED AT FS 1193. REPLACED FRAME PER SRM 51-30-02 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002080600081 20020806 00081 WP 2002 8 6 ASAA0280156 1 20020502 A 5330 FINGER DOUBLER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND CORROSION ON PREVIOUS INTERNAL SKIN REPAIR FINGER DOUBLER AT FS 1287. REPLACED DOUBLER PER SRM'S 51-30-05, 53-01, 53-04, AND 53-10-3. (M) 2 L 7 2 4F RT A6WE 2002080600082 20020806 00082 WP 2002 8 6 ASAA0280157 1 20020502 A 5311 99360741 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND CORROSION ON AFT CARGO BAY FRAME AT FS 1148. REPLACED FRAME PER SRM'S 51-10-2, 51-10-3, 51- 10-4 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002080600083 20020806 00083 WP 2002 8 6 ASAA0280160 1 20020504 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING PREFLIGHT CHECK, DETERMINED THAT THE FIRST CLASS CABIN EMERGENCY TRACK LIGHTING WAS INOPERATIVE. RECONNECT ED WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002080600084 20020806 00084 WP 2002 8 6 ASAA0280161 1 20020505 A 3350 2550325 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT BATTERY. OPS TESTED OK. (M) 2 L 7 2 4F RT A6WE 2002080600085 20020806 00085 WP 2002 8 6 ASAA0280162 1 20020508 A 5311 953005729 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND CORROSION ON AFT CARGO BAY FRAME AT FS 1287. REPAIRED FRAME PER SRM 53-03. (M) 2 L 7 2 4F RT A6WE 2002080600086 20020806 00086 WP 2002 8 6 ASAA0280163 1 20020508 A 5320 3913208503 SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND CORROSION ON LONGERON 30 ON SPLICE AT FS 1292. REPLACED SPLICE PER SRM'S 51-30-2 AND 51-30- 5. (M) 2 L 7 2 4F RT A6WE 2002080600087 20020806 00087 EU 2002 8 6 YENA200221 1 20020803 A 2420 7405869505 HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE #1 ENG FIREWALL OVERHEATED A YENA K NONE G MULTIPLE FAILURE CR CRUISE 1 EA 15 521JB 5229 5229 1452 V10943 Flt#94, OAK to JFK, Multiple faults occurred in flight including RA1, Nose wheel steering, #1 PFD, ND, #1 TLS, GPS, Blue electrical Hyd, #1 RMP, MCDU.Found phase "C" of eng and firewall disconnect plugs overheated. plug 400VC1 firewall plug pin "C" replaced per SPM 20-48-23. Replaced eng gen electrical harness 400VC-A, Ops check of generators and system norm al per 24-21-00-710-042 normal. Closed cowling per AMM 71-13-00. 2 L 7 2 4F 4 F RT A28NM E40NE 2002080600088 20020806 00088 SO 2002 8 6 ASOA02352 1 20020619 A 5280 12049994001 BRACKET EMB 120 EMB120RT 3260202 SO LT MLG CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 264AS 120165 DURING HANGAR MAINTENANCE IN MCN, THE LEFT MLG INBOARD FORWARD GEAR DOOR CENTER ATTACHMENT AFT 'L BRACKET WAS FOUND TO B E CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED 'L' BRACKET. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002080600089 20020806 00089 NM 2002 8 6 252TR0001PA 1 20020805 A 5730 PANEL BOEING 737 737228 13844AG NM A PIDA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 05 252TR 23001 return to departure point due to high a/c vibration. insp complete exterior of a/c all panels & flight controls to inc lude doors,found several loose & missing screws on panel # 6537. replaced & retorqued screws on panel # 6537,no other de fects noted. 2 L 7 2 4F RT A16WE 2002080600090 20020806 00090 EA 2002 8 6 COMA0260465 1 20020801 A 7920 388700320153 CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA R/H ENG MALFUNCTIONED A COMA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 01 965CA 7131 FLIGHT 9471 R/H ENGINE HIGH OIL TEMP.REPLACED THE ENGINE LUBE PUMP BYPASS CHECK VALVE. 2 L 7 2 4F RT A21EA 2002080600091 20020806 00091 EU 2002 8 6 RAIA00207213 1 20020711 A 7500 31040994 GASKET JETAIR JETSTM JETSTM4101 1500501 EU LEAKING A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 550HK 41039 5623-STL- RIGHT ENGINE WILL NOT MAINTAIN TARGET TARQUE. MAINTENANCE REMOVED AND REPLACED BLEED AIR GASKET, OPS CK OK. 2 L 7 2 4T RT A41NM 2002080600092 20020806 00092 EU 2002 8 6 RAIA00207214 1 20020714 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU DEFECTIVE A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 423TE 119 5585-STL- WITH BATTERY AND EMERGENCY LIGHT SWITCH OFF, LAST THREE EMERGENCY LIGHTS REMAINED ON. MAINTENANCE REMOVED AND REPLACED #5 EMERGENCY LIGHT BATTERY PACK, OPS OK. 2 H 7 2 4T RT A53EU 2002080600093 20020806 00093 NE 2002 8 6 RAIA00207215 2 20020715 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 562HK 41078 75109 LEFT ENGINE OIL CONTAMINATION LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED #1 ENGINE. 2 L 7 2 4T 4 T RT A41NM E18NE 2002080600094 20020806 00094 EU 2002 8 6 RAIA00207217 1 20020717 A 3320 BC0072001 SOCKET JETAIR JETSTM JETSTM4101 1500501 EU DEFECTIVE A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 03 559HK 41075 5493-STL- WITH CABIN LIGHTS ON SMELLED SMOKE. MAINTENANCE REMOVED AND REPLACED LIGHT BULB SOCKET AT BOW 8-9 2 L 7 2 4T RT A41NM 2002080600095 20020806 00095 SO 2002 8 6 RAIA00207218 1 20020717 A 2913 MPEV30086 PUMP EMB 145 EMB145LR 3260212 SO FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 811HK 5870 2020 145256 5299-RIC- #1 ELECTRIC HYDRAULIC PUMP FAILED. MAINTENANCE REMOVED AND REPLACED THE #1 ELECTRIC HYDRAULIC PUMP, OPS AND LK CK OK. 2 L 7 2 4T RT T00011AT 2002080600096 20020806 00096 NE 2002 8 6 RAIA00207220 2 20020719 A 7200 31043412 GEARSHAFT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE SHEARED A RAIA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 CE 03 566HK 41084 75091 5625-STL- LEFT ENGINE FLAMED OUT DURING CLIMB, UN ABLE TO RESTART. MAINTENANCE FOUND INTERNAL GEAR SHAFT FAILED IN NOSE CASE. REMOVED AND REPLACED GEAR SHAFT OPS AND LK CK OK. 2 L 7 2 4T 4 T RT A41NM E18NE 2002080600097 20020806 00097 SO 2002 8 6 RAIA00207221 1 20020719 A 3230 355022022MOD2 CONTROL UNIT EMB 145 EMB145ER 3260211 SO MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 808HK 4636 145157 5263-GRR- LANDING GEAR LEVER DISAGREE WARNING, RIGHT MLG INDICATED DOWN WITH LEVER IN UP POSSESSION. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002080600098 20020806 00098 SO 2002 8 6 RAIA00207222 1 20020720 A 3243 38793500 SHUTOFF VALVE EMB 145 EMB145 3260210 SO BYPASSING A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 805HK 87423 145096 5279-MEM- HYDRAULIC SYSTEM #1 OVERHEATED. MAINTENANCE REMOVED AND REPLACED THE #1 BRAKE SHUT OFF VALVE, LK AND OPS CK OK . 2 L 7 2 4F RT T00011AT 2002080600099 20020806 00099 EU 2002 8 6 RAIA00207226 1 20020729 A 7700 31056294 PRESSURE SWITCH JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 550HK 5548 1831 41039 5514-STL- RIGHT ENGINE BETA LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE #2 BETA SWITCH. 2 L 7 2 4T RT A41NM 2002080600100 20020806 00100 EU 2002 8 6 RAIA00207228 1 20020719 A 2910 141910013 HYDRAULIC LINE JETAIR JETSTM JETSTM4101 1500501 EU CHAFED A RAIA O OTHER J WARNING INDICATION DE DESCENT 1 CE 03 556HK 41073 5606-XNA- LOW HYDRAULIC PRESSURE WARNING, LEFT SIDE. MAINTENANCE REMOVED AND REPLACED CHAFED HYDRAULIC PRESSURE LINE, LK AND OPS CK OK. 2 L 7 2 4T RT A41NM 2002080600101 20020806 00101 EU 2002 8 6 RAIA00207229 1 20020729 A 3350 AML44 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 423TE 119 5536-STL- PAX DOOR EMERPENCY LIGHT INOP. REMOVE AND REPLACE LIGHT BULB, OPS CK OK. 2 H 7 2 4T RT A53EU 2002080600102 20020806 00102 SO 2002 8 6 RAIA00208231 1 20020804 A 3040 16251 CONTROLLER EMB 145 EMB145LR 3260212 SO INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 810HK 4136 145231 5251-PIT- WINDSHIELD #1 FAIL WARNING. MAINTENANCE REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER, OPS CK OK. 2 L 7 2 4T RT T00011AT 2002080700001 20020807 00001 SW 2002 8 7 CA020606020 1 20020604 A 5530 302511 BRACE AIRTRC AT802 AT802 0390305 SW PWA PT6 PT6A67A 52043 NE HARTZL HCB5M HCB5MA3 GL HORIZONTAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION IT WAS NOTED THAT THE RH AUX VERTICAL STAB WAS VERY LOOSE. UPON FURTHER INVESTIGATION IT WAS NOT ED THAT BOTH THE FORWARD AND AFT AUX VERTICAL STAB BRACE PLATES WERE CRACKED COMPLETELY THROUGH. THE AUX VERTIACL STAB W AS REMOVED FROM THE AIRCRAFT. THE AICRAFT WAS INSPECTED FOR OTHER STRUCTURAL DAMAGE NONE FOUND AND FERRIED TO YXX WHERE REPAIRS COULD BE ACCOMPLISHED. THE BRACES ARE BEING REPLACED WITH NEW PARTS. UPON COMPLETION OF THE REPAIRS THE AIRCRAFT WILL BE RETURNED TO SERVICE. THE OTHER AT -802'S IN THE FLEET HAVE BEEN INSPECTED WITH NO OTHER DAMAGE NOTED. 1 L 7 1 3T 4 T NC A19SW E26NE 6 C P44GL 2002080700004 20020807 00004 SW 2002 8 7 CA020610008 1 20020610 A 6520 406040406109 CASE BELL 427042400105 BELL 427 427 1182207 SW PWC PW207 PW207D NE T/R GEARBOX DAMAGED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA NA (CAN) DURING AN OVERHAUL ON MODEL 407 GEARBOX ASSEMBLY, WHICH AS THE SAME DETAIL CASE ASSEMBLY PART NUMBER AS THE MODEL 427,IT WAS FOUND THAT AN OIL PASSAGE WAS MISSING IN THE GEARBOX HOUSING BEARING BORE OF THE INPUT SHAFT DUPLEX BEARING. AFTER INVESTIGATION, IT WAS DETERMINED THAT A/C S/N 56002, 56015, 56020, 56022 TO 56024, 56026 TO 56028 WERE DELIVERED W ITH . 1 G 7 1 3U 3 U R00001RC E42NE 2002080700010 20020807 00010 CE 2002 8 7 CA020612001 1 20020610 A 2720 505243262728 ARM BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE RUDDER PEDAL CRACKED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA (CAN) PILOT DISCOVERED BRAKING DIFFICULTY UPON LANDING AND TAXIING. UPON INSPECTION IT WAS DISCOVERED THAT BOTH HINGE P OINTS FOR THE BRAKE ACTUATOR ON THE LT PEDAL ARM HAD CRACKED THROUGH, RESULTING IN A LOSS OF LEVERAGE ON THE BRAKE ACTUA TOR. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT THE RIGHT HAND RUDDER PEDAL ASSY. WAS CRACKED ABOUT 80 PERCENT THRO UGH THE THICKNESS OF MATERIAL AT THE SAME POINT. 2 L 7 2 4T 4 T A24CE E4EA 2002080700011 20020807 00011 GL 2002 8 7 CA020612004 2 20020505 A 7323 8575472 LOCK GEAR WOODWARD 6873466 CVAC 580 580 2422806 WP ALLSN 501D 501D13 03004 GL SSC WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 55102 (CAN) SPEED SENSITIVE CONTROL , RECD FOR FOLLOWING COMPLAINT, "RT ENGINE QUIT ACCELERATING AT 3200 RPM WITH NO FUEL FLOW OR TIT. NO FUEL FOGGING VISIBLE FROM COCKPIT WITH TEMP DATUM (TD) IN NULL MODE." SSC FUNCTIONALLY TESTED UNSERVICEABLE WITH LOW NR 1 SWITCH ACCELERATION LIMITS. NR 1 SWITCH COVER REMOVED & LOW SPEED SPRING ADJUSTED TO INCREASE RPM. AT POIN T MILITARY LOCKING GEAR, P/N 8575472, FOUND INSTALLED IN UNIT. P/N IS NOT IN 1R C4 PARTS MANUAL&IS ONLY FOUND ON MILITAR Y S/S CONTROLS. MILITARY PART REMVD&CORRECT COMMERCIAL P/N 7007186 LOCK GEAR INSTALLED INTO UNIT.THE MILITARY GEAR DID N OT ADVERSELY AFFECT TE FUNCTION OF SSC 2 GEARS ARE PHYSICALLY SIMILAR&PERFORM SAME FUN 2 L 7 2 4T 4 T RT E282 2002080700016 20020807 00016 WP 2002 8 7 CA020624006 1 20020613 A 3310 13053WN SOCKET CVAC 440 440 2422902 WP ALLSN 501D 501D13D 03004 GL CABIN BURNED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) DURING CLIMBOUT, THE FLIGHT ATTENDANT HAD INFORMED THE CAPTAIN THAT SMOKE WAS EMITTING FROM AN OVERHEAD ISLE LIG HT (NUMBERS 3 AND 4) IN ROWS 4 AND 5. THE OVERHEAD LIGHT SWITCH HAD ALREADY BEEN PLACED IN THE OFF POSITON AT THIS POINT . WHEN THE FLIGHT ATTENDANT WENT TO DISABLE THE CIRCUIT BREAKER, IT WAS FOUND OPENED. 2 L 7 2 4R 4 T 6A6 E282 2002080700018 20020807 00018 EA 2002 8 7 CA020627010 1 20020622 A 5411 LONGERON DHAV DHC6 DHC6100 2802610 EA PWA PT6 PT6A20 52043 EA NACELLE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACK FOUND IN LONGERON IN NACELLE AS PER CF-81-07R4 (DHC SB6/509) 1 H 7 2 3T 3 T RT A9EA E4EA 2002080700019 20020807 00019 EA 2002 8 7 CA020627011 1 20020527 A 5520 SLEEVE DHAV DHC6 DHC6100 2802610 EA PWA PT6 PT6A20 52043 EA ELEVATOR LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION SLEEVE FOUND LOOSE. 1 H 7 2 3T 3 T RT A9EA E4EA 2002080700020 20020807 00020 NE 2002 8 7 CA020628001 2 20020627 A 7310 3011155 TUBE PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL FUEL MANIFOLD CONTAMINATED W K NONE C F.O.D. IN INSP/MAINT 1 CA (CAN) WHILE PERFOMING A SCHEDULED REMOVAL / INSTALLATION OF THE FUEL NOZZLES, A SMALL PIECE OF METAL DEBRIS WAS FOUND WI THIN THE INTERNAL PASSAGE OF ONE OF THE FUEL MANIFOLD TRANSFER TUBES. THE DEBRIS WAS LODGED WITHIN THE TUBE AND HAD TO B E EXTRACTED BY PUSHING IT THROUGH WITH A PUNCH. THE NOZZLES DID NOT SHOW ANY ABNORMAL CONDITION. A NEW TRANSFER TUBE WAS INSTALLED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002080700022 20020807 00022 EA 2002 8 7 CA020701001 1 20020621 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LT WINDSHIELD CRACKED DURING TURNAROUND REPLACED WINDSHIELD IAW AMM 56-11-01 - OPS TEST TEMP CONTROLLED STATUS. AN D LEAK CHECK STATUS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080700026 20020807 00026 NM 2002 8 7 CA020702011 1 20020626 A 3244 314802OPTA TIRE DHAV DHC8 DHC8301 1386003 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE MLG WHEEL FAILED W O OTHER O OTHER LD LANDING 1 CA (CAN) ON LANDING PRIOR TO BRAKE APPLICATION [PAX REPORT NR 4] RT TIRE FAILED, FOLLOWED BY FAILURE OF THE OTHER RT TIRE, AIRCRAFT BROUGHT TO CONTROLLED STOP USING DISC. AIRCRAFT TAXIED CLEAR OF RUNWAY. INSPECTION FOUND BOTH RT MLG WHEEL RIMS DAMAGED DURING THE ROLL OUT. BOTH RT BRAKES CONTAMINATED WITH TIRE MATERIAL . BOTH RT MAIN WHEEL & BRAKE ASSEMBLIE S REPLACED , AIRCRAFT RETURNED TO SERVICE . NR 4 TIRE HAD BEEN RECAPPED ONCE [337CY AT FAILURE], NR 3 TIRE WAS NEW [244C Y AT FAILURE]. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002080700027 20020807 00027 EA 2002 8 7 CA020704001 1 20020624 A 2741 3094334 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STABILIZER FAILED W B A EMER. DESCENT UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CA (CAN) CLIMBING THROUGH FL120 STAB CHANNELS 1 AND 2 DISCONNECTED (STAB TRIM SET AT 8.4 UNITS). CREW WAS UNABLE TO RECONN ECT EITHER CHANNEL. CREW DECLARED AN EMERGENCY AND LANDED. AFTER NTSB RELEASE OF A/C MX REPLACED BOTH TRIM SWITCHES AN D RETURNED A/C TO SERVICE. CVR AND FDR WERE REMOVED AWAITING DOWNLOAD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080700028 20020807 00028 EA 2002 8 7 CA020704002 1 20020621 A 5610 601R330339 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FAILED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) CREW REPORTED CAPTAIN'S WINDSHIELD SHATTERED IN CRUISE FLIGHT. FLIGHT DIVERTED. MAINTENANCE REMOVED AND REPLACED T HE CAPTAIN'S WINDSHIELD. OPS CHECK AND PRESSURIZATION CHECK CARRIED OUT.THE WINDSHIELD INSTALLED WAS PRE SERVICE BULLETI N 2 L 7 2 4F 4 F RT A21EA E15NE 2002080700029 20020807 00029 NM 2002 8 7 CA020704003 1 20020629 A 2910 82950010143 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) HYDRAULIC LEAK IN LT NACELLE TRACED TO LT WING LIFT DUMP PRESSURE LINE. IPC 29-00-00 FIG 25 ITEM 330. LINE REPLACE D. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002080700030 20020807 00030 NM 2002 8 7 CA020704004 1 20020630 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 26301 26301 (CAN) ON PILOT'S WALK AROUND OIL NOTICED LEAKING FROM WHAT APPEARED TO BE NR 2 OIL COOLER AREA. NR 2 OIL COOLER CONFIRME D TO BE LEAKING, AND REPLACED BY MAINTENANCE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002080700032 20020807 00032 EA 2002 8 7 CA020705001 1 20020705 A 7920 6016310053 LINE CNDAIR CL604 CL604 1900301 EA GE CF34 CF343B1 NE ENGINE OIL CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) RT ENGINE OIL REPLENISH LINE WHERE IT EXITS THE AFT EQUIPMENT BAY AND ENTERS THE RT ENGINE PYLON WAS FOUND CHAFED AGAINST A STEEL BRAIDED HYD LINE. OIL LINE REPLACED 2 L 7 2 4F 4 F RT A21EA E15NE 2002080700033 20020807 00033 CE 2002 8 7 CA020705002 1 20020622 A 3211 5081032019 SOCKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CYCLES SINCE O/H 2972 DURING ROUTINE MAINTENANCE LT AND RT MLG SOCKETS WHERE FOUND TO BE CRACKED IN SAME AREA REFE RENCED IN BEECH COMMUNIQUE NR 27 DATED FEB 1993.UNITS SENT TO REPAIR FACILITY FOR EVALUATION WHERE THEY REQUIRED REPLACE MENT. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002080700034 20020807 00034 EU 2002 8 7 CA020705003 1 20020702 A 5754 A5724853200100 PANEL AIRBUS 310 A310300 3930305 EU GE CF6 CF680C2A5 NE NR 2 SLAT DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING WEEKLY CHECK, NR 2 RT SLAT ACTUATOR PANEL ASSY. FOUND DAMAGED. PART OF THE COMPOSITE PANEL WAS MISSING. AIR CRAFT WAS AOG. THE PANEL WAS FLOWN IN. MAINTENANCE REPLACED THE PANEL I.A.W. AMM 57-40-00. 2 L 7 2 4F 4 F RT A35EU E13NE 2002080700035 20020807 00035 WP 2002 8 7 ARWA20020602 1 20020618 A 2720 370963501 FEEL UNIT DOUG DC8 DC861 3021952 WP RUDDER MALFUNCTIONED A ARWA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 30UA 45888 RUDDER OPERATION ERRATIC FOLLOWED ABNORMAL PROCEDURES BUT DID NOT HELP. LANDED AT MIA WITHOUT ANY FURTHER INCIDENTS. R EMOVED AND REPLACED RUDDER LOAD FEEL AND TRIM MECHANISM ADJUSTMENT AND TESTED ON GROUND FOUND NORMAL IAW MM 27-23-1 AND 27-20-0. PRECAUTIONARY, REMOVED AND REPLACED RUDDER LINEAR TRANSDUCER IAW MM 27-21-6. NO LEAK NOTED. PERFORMED YAW CH ANNEL SELF-TEST IAW MM 22-11-0 NORMAL. 2 L 7 4 4F 4A25 2002080700036 20020807 00036 WP 2002 8 7 CA020705005 1 20020623 A 7732 A24000004 SIGNAL COND UNIT LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE NR 2 ENGINE MALFUNCTIONED W E A ENGINE SHUTDOWN UNSCHED LANDING E N VIBRATION/BUFFET FALSE WARNING CL CLIMB 1 CA (CAN) IN CLIMB, EPR 1.515, ENG NR 2 , VIBRATION CONFIRMED ON BOTH CHANNELS, 4.2 INDICATED, CAUSED IN-FLT SHUTDOWN. -ALL MCD INSP & NO CONTAMINATION FOUND PER AMM 72-01-00- VISUAL INSP OF AIR INTAKE , LP COMPRESSOR & EXHAUST COLLECTOR C/OUT & NO FOD OR DEBRIS FOUND. PRESSURE & SCAVENGE FILTERS INSP & REPL PER AMM 72-01-00 (NO CONTAMINATION FOUND).- BOROSCOPE INSP C/OUT PER AMM 72-00-00 ON APPLICABLE STAGES THAT FAULT ISOLATION PROC CALLED FOR IN AMM 71-91-00; INTERMEDIATE PRES SURE COMPRESSOR STAGE 7 L/E , HPC STG 6 L/E, HPT L/E & T/E ; IPT L/E & T/E; NO DAMAGE FOUND ON STAGES MENTIONNED ABOVE. -LP FAN BLADES REMOVED , CLEANED & LUBRICATED & REINST IAW AMM 72-31-02, 72-31-05. 2 L 7 3 4F 4 F A23WE E12EU 2002080700037 20020807 00037 NM 2002 8 7 CA020708001 1 20020705 A 5730 FITTING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE WING MISINSTALLED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE CARRYING OUT ALERT SB A8-28-33, IT WAS DISCOVERED THAT ONE OF THE WIGGINS FITTING UNDER ACCESS PANEL 624CT(R T WING OUTBOARD PANEL) WAS INSTALLED BACKWARDS. THERE WAS NO DAMAGE TO THE STIFFNERS ON THE UNDERSIDE OF THE PANEL, WIGG INS FITTING WAS REPOSITIONED FOR CORRECT ORIENTATION AND AIRCRAFT RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002080700038 20020807 00038 WP 2002 8 7 ARWA20020604 1 20020621 A 3251 37536485001 CYLINDER DOUG DC8 DC862 3021970 WP NLG FAULTY A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 810BN 45905 AFTER T/O, HYD TEMP CLIMBED TO 83 DEG C, PERFORMED ABNORMAL CHECKLIST, NO CHANGE. RETURNED TO RAMP. REMOVED & REPLACED NR 3 ENG HYD DRIVEN PUMP, PERFORMED OPERATIONS CHECK, CHECKED NORMAL IAW MM 29-30-0. DURING TAXI FOR T/O, HYDRAULIC O IL TEMP CLIMBED TO 83 DEG C. HYD OIL TEMP LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST, NO CHANGE. RETURNED TO RAM P. PERFORMED HYD SYS OPS CHECK, REMOVED & REPLACED LT & RT NOSE GEAR STEERING CYLINDERS, NO LEAKS NOTED. ALSO REMOVED & REPLACED NR 3 ENGINE HYDRAULIC PUMP. OPS CHECKED, NO LEAKS NOTED. REPLACED LT MAIN GEAR DOOR ACTUATOR. OPS CHECKED NORMAL, NO LEAKS NOTED. PERFORMED OPERATIONAL CHECK OF ALL HYD SYS, CHK NORMAL, NO OVERTEMP. 2 L 7 4 4F 4A25 2002080700040 20020807 00040 EU 2002 8 7 CA020708004 1 20020705 A 5753 D5757185015200 SEAL AIRBUS 320 A320212 3930322 EU CFMINT CFM56 CFM565A3 NE LT OUTBRD FLAP SEPARATED W D RETURN TO BLOCK D INFLIGHT SEPARATION TX TAXI/GRND HDL 1 CA (CAN) FLAP, SEALING-FRONT, FOUND ON RUNWAY YYZ. FLEET INSPECTION CAMPAIGN REVEALED PART BELONGING TO OUR AIRCRAFT. FLIGH T CREW WERE UNAWARE OF EVENT. THE SEAL IS MOUNTED BY MEANS OF THREE SCREWS WHICH WERE ALSO MISSING. ANOTHER AIRCRAFT RE VEALED ONE SCREW MISSING. 2 L 7 2 4F 4 F RT A28NM E29NE 2002080700042 20020807 00042 NM 2002 8 7 CA020708005 1 20020603 A 2433 28VS200Y4DH GROUND WIRE DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE TRU BURNED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOLLOWING WIRES WERE FOUND BURNED / DAMAGED FROM CONNECTOR 2431-P19. WIRE 2431-10138BA16NA-1 TO GROUND STUD 243 1-GS13; 243110135C14A-1 TO 2431-P5A; 2431-10137C-1 TO 2431-P5-C; 2431-10115A22-2 TO 9811-P3-C. FROM SHUNT 2431-R6: WIRE 2431-20141A22-2 TO 9811-P3-M; 2431-20142B22-2 TO 9811-P3-L. INSULATION ON ENTIRE LENGTH OF WIRE TOTALLY MELTED OFF INDIC ATING VERY HIGH HEAT & CURRENT LOAD. WIRES REPLACED. THOROUGH INSPECTION OF ADJACENT WIRES CARRIED OUT. NO OTHER DAMAG E FOUND. TECHNICAL INFO BULLETIN STATES PROBLEM IS CAUSED BY TRU OPERATION WITH ONLY 2 PHASES OF AC POWER. LOSS OF PH ASES OCCURS AS RESULT OF CURRENT LIMITER IN AFFECTED AC PHASES OPENING. TRU THEN BECOMES UNBALANCED, WHICH CAUSES EXCES 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002080700043 20020807 00043 NM 2002 8 7 SABA020078 1 20020803 A 3350 1305 LIGHT DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 AIRCRAFT 883 ON FLIGHT 5057 FROM TLH TO CLT: DURING CREW CHANGE OVER AT CLT AND NEW CREW PREFLIGHT INSPECTION THE EMERGE NCY FLOOR LIGHT AT ROW ONE WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED BULBS AND OPS CHECKED GOOD. AIRCRAFT WAS RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080700044 20020807 00044 2002 8 7 ARWA20020702 4 20020703 A 3425 INDICATOR DOUG DC8 DC861 3021952 WP COCKPIT MALFUNCTIONED A ARWA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 SO 19 29UA 46159 ON CLIMBOUT OF MIAMI AT 17,000 FEET F/O ARTIFICIAL HORIZON FAILED WITH ATTITUDE FLAG. RETURNED WITHOUT INCIDENT. ACCOMP LISHED OVERWEIGHT LANDING AT 273,000 LBS. WIRING CHECK ACCOMPLISHED IAW MM 34-2-2. REMOVED AND REPLACED 2 AMP C/B B10- 58 AND NR 2 ADI AS PER MM 20-50-1 & 34-25-0, ALSO REMOVED AND REPLACED NR 2 INSTRUMENT AMPLIFIER. NR 2 HORIZON & COMPAS S SYSTEM GROUND TEST NORMAL IAW MM 34-25-0 & 34-21-0. TEST FLIGHT FOUND NR 2 HORIZON SYSTEM OPERATING NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002080700046 20020807 00046 WP 2002 8 7 ARWA20020704 1 20020707 A 2120 DUCT DOUG DC8 DC862 3021970 WP NLG WW LOOSE A ARWA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 810BN 45905 AFTER TAKEOFF, HEAVY VIBRATION / NOISE FELT COMING FROM THE COCKPIT FLOOR AREA, CAPTAIN'S SIDE. INSPECTED NOSE WHEEL WE LL AREA AND FOUND LT AIR DUCT BOOT LOOSE FOR FLOW CONTROL SYSTEM; REINSTALLED BOOT AND SECURED CLAMPS AND CHECK RT SIDE TOO FOR CONDITION FOUND NORMAL IAW STC ST466CH; CHECKED BRAKES TEMPERATURE AND FOUND BELOW 160°C IAW TEMP STICK GAUGE. 2 L 7 4 4F 4A25 2002080700047 20020807 00047 WP 2002 8 7 ARWA20020705 1 20020716 A 2910 O-RING DOUG DC8 DC862F 3021972 WP HYD SYSTEM DEFECTIVE A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 810BN 45905 APPROXIMATELY ONE AND HALF (1.5) HOURS AFTER TAKE OFF, HYDRAULIC QUANTITY DROPPED TO THE STAND PIPE. FOUND DEFECTIVE O- RING ON ENGINE DRIVEN PUMP PRESSURE LINE FITTING RT ENGINE DRIVEN PUMP. REMOVED AND REPLACED O-RING IAW MM 29-10-12; OP S CHECKED NORMAL ON ENGINE RUN-UP AND NO LEAKS FOUND. ALSO SERVICED HYDRAULIC RESERVOIR BLEED SYSTEM SEVERAL TIMES DURI NG ENGINE RUN-UP IAW MM 12-30-1 & 71-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002080700048 20020807 00048 NM 2002 8 7 AT0200065 1 20020624 A 3222 STRUT BOEING 717 717200 1383700 NM NLG LOW A ZZDA K NONE J WARNING INDICATION CL CLIMB 1 SO 15 975AT 55035 NOSE GEAR FAILED TO RETRACT CYCLED GEAR AND STILL FAILED TO RETRACT. LOCKED OKAY IN DOWN POSITION. INSPECTED AIRCRAFT NO DEFECT WITH NOSE GEAR OR RETRACTION SYSTEM. PUT AIRCRAFT ON JACK, CYCLED GEAR THROUGH 5 TIMES. NO DEFECTS NOTED DUR ING RETRACTION CHECK PER M/M 32-30. FOUND NOSE STRUT SERVICE TO BELOW, SERVICED NOSE STRUT PER MM 32-21. JACKED AIRCRA FT AGAIN AND RETRACTED GEAR. NO DEFECT NOTED. GEAR OPS CHECKS GOOD ON GROUND. 2 L 7 2 4F TR A6WE 2002080700049 20020807 00049 NE 2002 8 7 AT0200070 2 20020709 A 7321 114E6112G1 EEC BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE RT ENGINE FAILED A ZZDA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 15 951AT 55013 IN CRUISE AT FL330 .771 M RIGHT ENGINE WENT TO IDLE - ENG R SYS FAIL ILLUMINATED, SELECT FADEC ALT DISPLAY, SELECTED NO CHANGE SHUT ENGINE DOWN. ALL OTHER INDICATIONS NORMAL. EPR INDICATION DISPLAYED A -X-. DIVERTED TO SAV. REMOVED AND REPLACED NR 2 ENGINE ELECTRONIC CONTROL FOR EEC BOX FAULT. PERFORMED RETURN TO SERVICE. OK FOR SERVICE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002080700051 20020807 00051 2002 8 7 GLBA2002105 4 20020710 A 3418 1143800515 COMPUTER BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GLBA O OTHER N FALSE WARNING CR CRUISE 1 NM 03 179GL 15641 UE179 STALL WARNING SOUNDED AT 220 KNOTS INDICATED AIR SPEED AOG IN DEN. REPLACED STALL WARNING COMPUTER, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002080700053 20020807 00053 CE 2002 8 7 GLBA2002108 1 20020726 A 2730 ELEVATOR BEECH 1900 1900D 1154162 CE TAIL VIBRATION A GLBA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 03 260GL UE260 ELEVATOR VIBRATION. 2 L 7 2 4T RT A24CE 2002080700054 20020807 00054 CE 2002 8 7 GLBA2002110 1 20020727 A 3246 114800121 WHEEL BEECH 1900 1900D 1154162 CE NLG DEFECTIVE A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 240GL 245 UE240 NOSE GEAR NOISE ON RETRACTION. REPLACED NOSE WHEEL, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2002122000005 20021220 00005 CE 2002 12 20 GLBA2002111 1 20020729 A 5270 SWITCH BEECH 1900 1900D 1154162 CE PAX DOOR MALFUNCTIONED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 169GL UE169 CABIN DOOR ANNUNCIATOR ILLUMINATED ON TAKE OFF, CHANGED SWITCH OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2002080700055 20020807 00055 CE 2002 8 7 GLBA2002112 1 20020729 A 5420 TUBE BEECH 1900 1900D 1154162 CE LT NACELLE DISCONNECTED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 204GL UE204 SMOKE COMING FROM LEFT NACELLE. INSPECTED FOUND VENT TUBE DISCONNECTED. RESECURED, OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2002122000006 20021220 00006 CE 2002 12 20 GLBA2002113 1 20020729 A 2750 SWITCH BEECH 1900 1900D 1154162 CE TE FLAPS MALFUNCTIONED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 261GL UE261 FLAP STUCK AT 35 PERCENT, CHANGED FLAP SWITCH OPS CHECK GOOD 2 L 7 2 4T RT A24CE 2002122000007 20021220 00007 CE 2002 12 20 GLBA2002114 1 20020731 A 2134 1143840391 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE CABIN PRESSURE FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 226GL UE226 LEFT ENVIROMENTAL FAIL ON CLIMB-OUT, REMOVED AND REPLACE PRESSURE SWITCH OPS CHECK GOOD 2 L 7 2 4T RT A24CE 2002080700056 20020807 00056 NE 2002 8 7 GLBA200287 2 20020622 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT OVERTEMP A GLBA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 NM 03 220GL UE220 LEFT HAND ENGINE OVER TEMPED ON TAKEOFF. 2 L 7 2 4T 4 T RT A24CE E26NE 2002080700057 20020807 00057 NM 2002 8 7 HNAA0200048 1 20020620 A 3397 1013079 WIRE DHAV DHC8 DHC8201 2809001 NM CABIN BROKEN A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 969HA 468 NUMBER 3 AND NUMBER 4 RED FLOOR EMERGENCY LIGHTS INOP. NEW CREW FOUND BROKEN WIRES. REPAIRED BROKEN WIRE AT LIGHT ASSE MBLY. 2 H 7 2 4T RT A13NM 2002080700058 20020807 00058 WP 2002 8 7 IXXA0200040S 1 20020508 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 73236 2985 45973 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LOWER SECTION AFT OF THE NOSE WHEEL WELL STATION 16 AND L ONGERON 35R. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF EXTERNAL DOUBLER IN ACCORDANC E WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING DIRECTIVE EDQ27-1. 2 L 7 4 4F RT 4A25 2002080700059 20020807 00059 WP 2002 8 7 IXXA0200042O 1 20020701 A 2130 LINKAGE DOUG DC8 DC862F 3021972 WP OUTFLOW VALVE BINDING A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 799AL 70713 435 45922 EN ROUTE FROM QPG THE FLIGHT CREW NOTICED THE CABIN PRESSURIZATION COULD NOT BE MAINTAINED. THE FLIGHT CREW FOLLOWED CO MPANY PROCEDURES WITH NO EVAL AND RETURNED TO QPG FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH R EVEALED THE OUTFLOW VALVE LINKAGE BINDING THE SUGAR SCOOP. MAINTENANCE FREE, CLEANED, LUBRICATED AND ADJUSTED THE LINKA GE. MAINTENANCE PERFORMED A SUCCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS R ETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002080700128 20020807 00128 2002 8 7 IXXA0200043O 4 20020706 A 3422 1428302001 GYRO DOUG DC8 DC873F 302199F WP COCKPIT DEFECTIVE A IXXA O OTHER I FLT. ATTITUDE INST. CR CRUISE 1 SW 11 606AL 88286 38 46044 EN ROUTE FROM TOL, THE FLIGHT CREW NOTICED THE PITCH AND ROLL FLAGS DISPLAYED ON THE CAPTAINS AND FIRST OFFICERS ELECTRO NIC ATTITUDE DIRECTION INDICATOR. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND RETURNED TO TOL FOR AN UNEVENTFUL LAN DING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND BOTH FOG GYROS TO BE DEFECTIVE. MAINTENANCE REMOVED AND REPLACED TH E FOG GYROS IN ACCORDANCE WITH THE MAINTENANCE MANUAL AND PERFORMED SUCCESSFUL OPERATIONAL CHECKS. THE AIRCRAFT WAS RET URNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002080700129 20020807 00129 NE 2002 8 7 IXXA0200047O 2 20020801 A 7310 MS2719824 SEAL DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 2 ENGINE DEFECTIVE A IXXA O OTHER K X FLUID LOSS ENGINE FLAMEOUT CL CLIMB 1 SW 11 823BX 83922 750 46064 EN ROUTE FROM LRD TO TOL, THE NUMBER TWO ENGINE FLAMED OUT DURING CLIMBOUT FROM LRD. THE FLIGHT CREW FOLLOWED COMPANY P ROCEDURES AND CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE WHICH REVEALED THE FUEL FLOW TRANSMITTER LEAKING EXCESSIVE FUEL. MAINTENANCE REPLACED THE SUPPLY LINE GASCO SEAL. MAINTENANCE PERFORMED A SUCCESSF UL LEAK AND OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2002080700130 20020807 00130 WP 2002 8 7 ASAA0280164 1 20020508 A 5347 5936663521 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND CORROSION ON CARGO BAY LEFT TIEDOWN TRACK AT FS 1007 TO 1220. REPLACED CARGO TRACK PER SRM' S 51-10-3, 51-10-3B, 51-10-4, AND 53-05. (M) 2 L 7 2 4F RT A6WE 2002080700131 20020807 00131 WP 2002 8 7 ASAA0280165 1 20020508 A 5320 FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND MID CARGO BAY FITTING CRACKED AT FS 788. REPLACED FITTING PER SRM'S 51-30-5 AND 51-10-4. ( M) 2 L 7 2 4F RT A6WE 2002080700132 20020807 00132 WP 2002 8 7 ASAA0280166 1 20020508 A 5310 5936628113 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT LONGERON 30 IN MID CARGO BAY AT FS 787. REPLACED SHEAR TIE PER SR M'S 53-01 AND 51-30-02. (M) 2 L 7 2 4F RT A6WE 2002080700133 20020807 00133 WP 2002 8 7 ASAA0280167 1 20020508 A 5313 59363601 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND CORROSION AROUND LONGERON 30 FASTENERS AT FS 1029. REPAIRED PER EA 5330-01578. (M) 2 L 7 2 4F RT A6WE 2002080700134 20020807 00134 WP 2002 8 7 ASAA0280168 1 20020508 A 5320 59360713 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL IN MID CARGO BAY AT FS 698. FABRICATED AND INSTALLED NEW INTERCOST AL PER SRM 53-01 AND 51-10-04. (M) 2 L 7 2 4F RT A6WE 2002080700135 20020807 00135 WP 2002 8 7 ASAA0280169 1 20020508 A 2597 D29984103 HARNESS DOUG DC9 DC983 3022083 WP PAX DOOR FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 OAK - DURING C-CHECK, FOUND TAIL DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLIDE. SYSTEM CH ECKED OK. (M) 2 L 7 2 4F RT A6WE 2002080700136 20020807 00136 2002 8 7 ASAA0280170 4 20020508 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP L2 DOOR DETACHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 SEA - DURING PREFLIGHT CHECK, L2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. ATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2002080700137 20020807 00137 WP 2002 8 7 ASAA0280173 1 20020509 A 5313 59360281 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND CORROSION ON LONGERON 30 IN AFT CARGO BAY AT FS 1018. REPAIRED LONGERON PER EA 5310-02084. (M) 2 L 7 2 4F RT A6WE 2002080700138 20020807 00138 WP 2002 8 7 ASAA0280174 1 20020509 A 5313 5936628113 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND CORROSION ON LONGERON 30 FASTENER HOLE AT FS 781. REPAIRED LONGERON PER EA 5310-02086. (M) 2 L 7 2 4F RT A6WE 2002080700139 20020807 00139 WP 2002 8 7 ASAA0280175 1 20020509 A 5330 5936004503 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND CORROSION ON SKIN IN MID CARGO BAY AT FS 769. REPAIRED SKIN PER EA 5330-01578. (M) 2 L 7 2 4F RT A6WE 2002080700140 20020807 00140 EA 2002 8 7 ASOA022371 1 20020627 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 832AS 7243 DURING INSPECTION, MAINTENANCE FOUND THE AFT CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002080700141 20020807 00141 SO 2002 8 7 ASOA02353 1 20020619 A 5280 12030073005 BRACKET EMB 120 EMB120ER 3260203 SO RT MLG DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 639AS 120283 DURING HANGAR MAINTENANCE IN TXK, THE RIGHT MLG FORWARD INBOARD DOOR AFT TENSION BRACKET AND FLANGE WERE FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG DOOR TENSION BRACKET AND BRACKET FLANGE. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002080700142 20020807 00142 EA 2002 8 7 ASOA02354 1 20020619 A 2170 7536893 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA A/C BAY DIRTY A ASOA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 SO 11 840AS 7290 DURING DESCENT INTO MLU, THE CAPTAIN NOTICED A SMELL THAT HE ASSOCIATED WITH A HOT PACK. THE RIGHT PACK TEMPERATURE HAD BEEN UNSTABLE EARLIER IN THE FLIGHT. THE CAPTAIN MANUALLY COOLED THE PACK. THE FLIGHT ATTENDANT REPORTED A HAZE FORMI NG IN THE CABIN AND THE LAVATORY SMOKE DETECTOR WAS SOUNDING. AT THIS TIME THE CAPTAIN RECEIVED THE SMOKE TOILET MESSAG E IN THE COCKPIT. THE LAVATORY WAS VISUALLY CHECKED FOR FIRE AND THERE WAS NONE. THE CAPTAIN SHUT DOWN THE RIGHT PACK AND THE SMOKE AND SMELL DISSIPATED SHORTLY AFTER. AIRCRAFT LANDED SAFELY IN MLU. MAINTENANCE REMOVED AND REPLACED THE COALESCER BAG ON THE RIGHT PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002080700143 20020807 00143 EA 2002 8 7 ASOA02355 1 20020619 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 902EV 7820 FLT 4071 - DURING GROUND INSPECTION IN DFW, THE RIGHT WING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002080700144 20020807 00144 SW 2002 8 7 ASOA02356 1 20020621 A 3350 D36604001 BATTERY MOONEY M20 M20K 5870220 SW CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 231AS 250106 DURING GROUND INSPECTION IN ATL, WHEN TESTED, THE INTERIOR EMERGENCY EXIT LIGHTS GO OUT IN LESS THAN A MINUTE. MAINTENA NCE CHARGED THE EMERGENCY LIGHTING BATTERIES. OPERATIONAL TESTING OF THE EMERGENCY LIGHT GOOD AT THIS TIME. (M) 1 L 7 1 3O 2A3 2002080700145 20020807 00145 EA 2002 8 7 ASOA02357 1 20020621 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 SO 11 856AS 7395 DURING CRUISE FLIGHT FROM RDU TO DFW, AT APPROXIMATELY FL350, THE CAPTAINS WINDSHIELD SHATTERED ACCOMPANIED BY A LOUD BA NG. AN EMERGENCY WAS DECLARED AT THIS TIME. PRESSURIZATION REMAINED NORMAL, BUT CAPTAIN HAD AIRCRAFT DESCEND TO 10,000 FEET AND 250 KNOTS AS A PRECAUTION. AIRCRAFT DIVERTED TO THE NEAREST AVAILABLE AIRPORT, TXK, AND LANDED SAFELY. MAINT ENANCE REMOVED AND REPLACED THE CAPTAINS SHATTERED WINDSHIELD. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT OK FOR SERVIC E. (M) 2 L 7 2 4F RT A21EA 2002080700146 20020807 00146 SO 2002 8 7 ASOA02358 1 20020621 A 1100 25139915 PLACARD EMB 120 EMB120ER 3260203 SO CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 505AS 120279 FLT 4204 - DURING A GROUND INSPECTION IN ATL, THE LIGHTED EXIT SIGN ON THE RIGHT SIDE EMERGENCY EXIT AT ROW 5 WAS MISSIN G THE EXIT PLACARD. MAINTENANCE REPLACED THE MISSING EXIT PLACARD ON THE SIGN AT ROW 5. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002080700147 20020807 00147 EU 2002 8 7 ASOA02360 1 20020623 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72 EU CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 640AS 405 DURING A HANGAR INSPECTION IN MCN, SEVERAL EMERGENCY LIGHTS THROUGH OUT THE CABIN WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY IN THE 61WL POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2002080700148 20020807 00148 SO 2002 8 7 ASOA02361 1 20020623 A 2612 360173450 FIRE LOOP EMB 120 EMB120ER 3260203 SO RT MLG WW FAULTY A ASOA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 11 268AS 120202 FLT 4015 - ON FINAL APPROACH INTO ATL, THE CAPTAIN RECEIVED A RIGHT ENGINE/WHEEL WELL FIRE INDICATION. THE CAPTAIN ACTI VATED BOTH RIGHT ENGINE FIRE BOTTLES AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN ATL AND THE AIRCRAFT WAS EVAC UATED. NO EVIDENCE OF FIRE OR SMOKE WAS EVER NOTED. DUE TO THE ENGINE FIRE BOTTLES BEING DEPLOYED MAINTENANCE REMOVED AND REPLACED BOTH FIRE BOTTLES AND BOTH SQUIBS. MAINTENANCE REPLACED THE FIRE LOOP ON THE RIGHT ENGINE WITH NO HELP. M AINTENANCE REMOVED AND REPLACED THE FIRE LOOP IN THE WHEEL WELL AND THAT EXTINGUISHED THE INDICATION. AIRCRAFT OK FOR S ERVICE. (M) 2 L 7 2 4T RT A31SO 2002080700149 20020807 00149 SO 2002 8 7 ASOA02361S 1 20020623 A 2612 360173450 FIRE LOOP EMB 120 EMB120ER 3260203 SO RT MLG WW FAULTY A ASOA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 SO 11 268AS 120202 ON LANDING ROLL OUT IN ATL, THE CAPTAIN RECEIVED A RIGHT ENGINE FIRE/WHEEL WELL INDICATION. THE CAPTAIN ACTIVATED BOTH RIGHT ENGINE FIRE BOTTLES, BUT THIS DID NOT EXTINGUISH THE INDICATION LIGHT. EMERGENCY EQUIPMENT WAS REQUESTED AND THE AIRCRAFT WAS EVACUATED ON THE RUNWAY AFTER THE AIRCRAFT POWERED DOWN. NO EVIDENCE OF FIRE OR SMOKE WAS EVER NOTED. DUE TO THE ENGINE FIRE BOTTLES BEING DEPLOYED MAINTENANCE REMOVED AND REPLACED BOTH FIRE BOTTLES AND BOTH SQUIBS. MAINTENA NCE REPLACED THE FIRE LOOP ON THE RIGHT ENGINE WITH NO HELP. MAINTENANCE REMOVED AND REPLACED THE FIRE LOOP IN THE WHEE L WELL AND THAT EXTINGUISHED THE INDICATION. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002080700150 20020807 00150 EA 2002 8 7 ASOA02362 1 20020624 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 834AS 7254 DURING GROUND INSPECTION IN ATL, THE LAST FEW SECTIONS OF FLOOR EMERGENCY LIGHTING WERE DISCOVERED INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK IN THE NR 4 POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002080700151 20020807 00151 EA 2002 8 7 ASOA02363 1 20020624 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 846AS 7328 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHTING WAS INOPERATIVE THROUGH OUT THE CABIN. MAINTENANCE REMO VED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK IN THE NR 4 POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SE RVICE. (M) 2 L 7 2 4F RT A21EA 2002080700152 20020807 00152 EA 2002 8 7 ASOA02364 1 20020624 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 DURING HANGAR MAINTENANCE, THE LEFT AND RIGHT SIDES OF THE FRAME AT FRAME STATION 718 WERE CRACKED BETWEEN STRINGERS 10 AND 12. MAINTENANCE REPAIRED THE CRACKED FRAME IAW ASA EO 600-53-0067. THIS EO INCLUDES REPAIR SPECIFICATIONS FOR FS 7 18 CRACKS ON CRJ200 AIRCRAFT USING REO 601R-53-61-193, REO 601R-53-61-492, SRM 51-00 REV 14, AND SRM 53-00 REV 14 AS REF ERENCES. (M) 2 L 7 2 4F RT A21EA 2002080700153 20020807 00153 EA 2002 8 7 ASOA02365 1 20020624 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 WHILE COMPLYING WITH ASA EO 600-53-0069, INSPECTION OF FRAME STATION 640 AT BASE LINE 45, THE FRAME WAS FOUND TO BE CRAC KED BETWEEN STRINGERS 13 AND 14. MAINTENANCE WILL REPAIR THE CRACK IN THE FRAME IAW CNDAIR SRM 53-61-15. (M) 2 L 7 2 4F RT A21EA 2002080700154 20020807 00154 EA 2002 8 7 ASOA02366 1 20020624 A 5346 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 DURING HANGAR MAINTENANCE IN MCN, THE ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED ON BOTH THE RIGHT AND LEFT SIDES. MAI NTENANCE REPAIRED THE CRACKED ENGINE SUPPORT BEAM IAW REO 601R-53-61-366. (M) 2 L 7 2 4F RT A21EA 2002080700155 20020807 00155 EA 2002 8 7 ASOA02367 1 20020624 A 5346 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 DURING HANGAR MAINTENANCE IN MCN, THE CENTER ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REINS TALLED THE ANGLES FROM THE TOP AND BOTTOM OF THE BEAM TO COMPLY WITH HFEC INSPECTION WHICH WAS COMPLETED. NO CRACKS WER E FOUND. MAINTENANCE WILL REPAIR THE CRACKED CENTER ENGINE SUPPORT BEAM IAW REO 601R-53-61-345. (M) 2 L 7 2 4F RT A21EA 2002080700156 20020807 00156 EA 2002 8 7 ASOA02368 1 20020610 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 825AS 7207 DURING HANGAR MAINTENANCE IN MCN, FRAME 71B WAS FOUND CRACKED ON BOTH THE LEFT AND RIGHT SIDES BETWEEN STRINGERS 10-12. MAINTENANCE REPAIRED THE CRACKED FRAME IAW ASA EO 600-53-0067. THIS EO INCLUDES REPAIR SPECIFICATIONS FOR FS 718 CRACK S ON CRJ200 AIRCRAFT USING REO 601R-53-61-193, REO 601R-53-61-492, SRM 51-00 REV 14, AND SRM 53-00 REV 14 AS REF. (M) 2 L 7 2 4F RT A21EA 2002080700157 20020807 00157 EA 2002 8 7 ASOA02369 1 20020626 A 3350 RPS1B CHARGER CNDAIR CL600 CL6002B19 1900309 EA CABIN FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 834AS 7254 DURING GROUND INSPECTION IN ATL, THE LAST FEW SECTIONS OF FLOOR EMERGENCY LIGHTING WERE DISCOVERED INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK CHARGER. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002080700158 20020807 00158 SO 2002 8 7 ASOA02370 1 20020627 A 3397 M2275941229 WIRE EMB 120 EMB120RT 3260202 SO CABIN BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 282AS 120226 DURING GROUND INSPECTION IN DFW, THE LIGHTED EXIT SIGN ON THE FIRST ROW BULKHEAD WAS NOT ILLUMINATED. MAINTENANCE REPAI RED A BROKEN WIRE TO THE AFT CLOSET EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2002080700159 20020807 00159 NM 2002 8 7 SABA020079 1 20020804 A 3350 1305 LIGHT DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 882CC 168 AIRCRAFT 882 FLIGHT 5020 FROM CLT TO TLH : DURING PREFLIGHT THE AIRCREW REPORTED THAT THE EMERGENCY FLOOR LIGHT AT ROW W OULD NOT TEST. MAINTENANCE REMOVED AND REPLACED BULBS. SYSTEM OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080700160 20020807 00160 SO 2002 8 7 ASOA02372 1 20020630 A 3320 12032110001 LENS EMB 120 EMB120RT 3260202 SO CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 238AS 120053 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY EXIT AT ROW 8 WAS INHIBITED FROM OPENING COMPLETELY. MAINTENANCE FOUND THE DOOR TO BE JAMMED BY A BROKEN LENS COVER. MAINTENANCE REMVOED AND REPLACED THE BROKEN LENS COVER. OPERATIONAL CHEC K OF THE DOOR NORMAL. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002080700161 20020807 00161 WP 2002 8 7 GTIA020522 1 20020522 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 801NK 48048 FLL - FLT 1268 - FOUND EMERGENCY LIGHTING TRACK FROM ROW 22 TO 25 INOPERATIVE. FOUND LIGHT AT SEAT 22 WIRES PULL OUT OF SPLICE, SPLICED WIRES BACK TOGETHER FOR LIGHT. (M) 2 L 7 2 4F A6WE 2002080700162 20020807 00162 WP 2002 8 7 GTIA020523 1 20020527 A 7711 SENSE LINE DOUG DC9 DC982 3022082 WP ENGINE CRACKED A GTIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 23 803NK 48087 FLL - FLT 380 - ON TAKEOFF ROLL, THE THROTTLES MATCHED N1 BUT THE EPRS WERE OFF, NR 1 1.70, NR 2 1.99, UPON PUSHING NR 1 THROTTLE UP TO MATCH EPRS THE NR 1 N1 WENT TO 101, ABORTED AT SPEED 105 MAX. PERFORM OPERATIONAL CHECK ON NR 1 ENGINE EPR INDICATION. PERFORMED TROUBLESHOOTING PER MM 77-11-01. FOUND VERY LOOSE B-NUT AT PT7 LINE JUNCTION. TIGHTENED B-N UT, CHECKED ALL LINES FOR SECURITY AND CHECKED ALL FITTINGS, PT2 AND PT7 LINES LEAK CHECK OK. ITEM DUE OPS CHECK ON R/U SEE ITEM 31267-1. FOUND 2 PT7 LINES CRACKED AND LEAKDING REMOVED AND REPLACED LINES ALSO TRIMMED NR 1 AND NR 2 ENGINE PER MM 71-00-00 OPS AND LEAK CHECK OK. (M) 2 L 7 2 4F A6WE 2002080700163 20020807 00163 WP 2002 8 7 GTIA020524 1 20020524 A 4930 O-RING DOUG DC9 DC982 3022082 WP APU LEAKING A GTIA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 812NK 48021 MCO - FLT 927 - SMELL OF FUEL IN COCKPIT WHILE TAXIING AT MCO. REMOVED AND REPLACED FUEL SOLENOID O-RINGS SEALS. OPS A ND LEAK CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2002080700164 20020807 00164 WP 2002 8 7 GTIA020525 1 20020324 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FLIGHT AND FORWARD PASSENGER COMPARTMENT FLOOR PANEL RIGHT OUTBOARD STATION 148.5 TO STATION 167.5 HAS CRACKED MUS HY RACK 8. FORM NEW PANEL FOR STATION 148.5 TO 167.5. (M) 2 L 7 2 4F A6WE 2002080700165 20020807 00165 WP 2002 8 7 GTIA020526 1 20020408 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - PASSENGER CABIN, AFT FUSELAGE AREA FLOORBOARD X 45L FROM STATION Y 1115 TO STA Y 1256 CORNER CRACKED, INSERTS MISS ING AND BROKEN. FORM NEW PANEL. (M) 2 L 7 2 4F A6WE 2002080700166 20020807 00166 WP 2002 8 7 GTIA020527 1 20020321 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND FORWARD ENTRY AREA, SEAT TRACK CORRODED AT FS 232-X22. REMOVED SECTION AREA FROM STA Y 200 TO Y 266. LOCAT ED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK AND SPLICE. (M) 2 L 7 2 4F A6WE 2002080700167 20020807 00167 WP 2002 8 7 GTIA020528 1 20020527 A 7920 LINE DOUG DC9 DC983 3022083 WP LT ENGINE LEAKING A GTIA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 827NK 49793 DIVERT TO CVG AND ENGINE IN FLIGHT SHUT DOWN, LEFT OIL STRAINER CLOG LIGHT CAME ON, LOST OIL QUANTITY AND THEN OIL PRESS URE. OIL QTY WAS ZERO AND OIL PRESSURE WAS 29 PSI AT SHUTDOWN. PERFORMED QRH PROCEDURES. NO OIL PRESSURE AND QUANTITY FOR AT LEAST 10 MINUTES LESS THAN 20 MINUTES. REPLACED OIL LINE FROM GEAR BOX TO OIL PRESSURE TRANSMITTER IPC 79-30-00 . PERFORMED ENGINE WINDMILL INSPECTION. PERFORMED ENGINE GROUND UP CYCLE. OIL LINE AND FILTER LEAK CHECK OK. (M) 2 L 7 2 4F RT A6WE 2002080700168 20020807 00168 2002 8 7 GTIA020529 4 20020527 A 3497 WIRE DOUG DC9 DC983 3022083 WP A/C BAY CHAFED A GTIA O OTHER O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 DTW - FOUND DFGC SWITCH A CIRCUIT BREAKER POPPED AND NOT RESET. FOUND WIRE 1C610X20RD CHAFED IN AFT TAIL COMPARTMENT AR EA. REPAIRED WIRE. NO OTHER DISCREPANCIES NOTED. (M) 2 L 7 2 4F RT A6WE 2002080700169 20020807 00169 2002 8 7 GTIA020530 4 20020527 A 2210 4034233901 SENSOR DOUG DC9 DC983 3022083 WP RT SPOILER FAILED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 824NK 53015 LGA - FLT 874 - CIRCUIT BREAKER C17 WILL NOT RESET AUTO PILOT INOPERATIVE, WINDSHEAR INOPERATIVE, MACH TRIM INOPERATIVE, MACH TRIM INOPERATIVE DFGS NR 1 AND NR 2. PERFORMED RTS CHECK ON NR 1 AND NR 2 FAILED RT SPOILER POSITION SENSOR REPLA CED RT SPOILER POSITION SENSOR. PERFORMED RTS CHECK ON NR 1 AND NR 2 BOTH CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 2002080700170 20020807 00170 WP 2002 8 7 GTIA020531 1 20020524 A 5730 SKIN DOUG DC9 DC983 3022083 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FOUND CRACK ON LOWER RIGHT WING AT APPROX STATION XFS 281.750 ABOUT 1 INCH LONG, ON LEADING EDGE NEAR FUEL PANEL. REPAI RED CRACK IAW MD80 SRM 57-06A. (M) 2 L 7 2 4F RT A6WE 2002080700171 20020807 00171 WP 2002 8 7 GTIA020658 1 20020510 A 3260 PROXIMITY SENSOR DOUG DC9 DC981 3022081 WP RT MLG DOOR OUT OF ADJUST A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND RIGHT GEAR MLG DOOR INDICATES RED. RIGHT MLG LIGHT STAYED ON WITH TRANSFER PUMP. ADJUSTED PROX SENSOR IAW MD80 33-60-05. (M) 2 L 7 2 4F A6WE 2002080700172 20020807 00172 WP 2002 8 7 GTIA020659 1 20020511 A 3231 LATCH DOUG DC9 DC981 3022081 WP RT MLG DOOR OUT OF ADJUST A GTIA K NONE J WARNING INDICATION CL CLIMB 1 GL 23 806NK 48051 FTW - FOUND RIGHT MLG UNSAFE LIGHT ILLUMINATED ON RETRACT, EXTINGUISHED ON CLIMB-OUT. AFTER TROUBLESHOOTING FOUND MAIN GEAR DOOR LATCH MECH. NO PROPERLY ADJUSTED. INSTALLED SHIM AND ADJUSTED MAIN GEAR DOOR LATCH MECH. (M) 2 L 7 2 4F A6WE 2002080700173 20020807 00173 WP 2002 8 7 GTIA020660 1 20020508 A 3234 CONTROL HANDLE DOUG DC9 DC981 3022081 WP COCKPIT OUT OF ADJUST A GTIA K NONE O OTHER CL CLIMB 1 GL 23 806NK 48051 FTW - TEST FLIGHT FAILED, UNABLE TO RAISE GEAR HANDLE. PERFORMED TROUBLESHOOTING AND FOUND LANDING GEAR CONTROL LEVER A ND ANTI-RETRACTION LATCH OUT OF RIG. ADJUSTED LANDING GEAR CONTROL LEVER AND ANTI-LATCH. (M) 2 L 7 2 4F A6WE 2002080700174 20020807 00174 2002 8 7 GTIA020664 4 20020613 A 2565 SLIDE DOUG DC9 DC983 3022083 WP GALLEY DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 LAX - AFT GALLEY DOOR OPENED BY CLEANERS, SLIDE PACK FELL OFF. RESTOWED AFT GALLEY DOOR SLIDE PACK. OPS CHECK IAW MM 2 5-00-00. (M) 2 L 7 2 4F RT A6WE 2002080700175 20020807 00175 WP 2002 8 7 GTIA020686 1 20020622 A 2697 HARNESS DOUG DC9 DC981 3022081 WP FIRE DETECTION OUT OF POSITION A GTIA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 810NK 48015 FLL - FLT 1765 - FOUND FIRE DETECTOR LOOP ANNUNCIATOR LIGHT CAME ON DURING DESCENT. LOOP 'B' WAS ILLUMINATED. LOOP 'A' OK NOT ILLUMINATED NO OTHER FIRE INDICATORS. FOUND HARNESS AT UPPER BURN THROUGH BARRIER ROUTED TO CLOSE TO APRON BRAC KET. REPOSITIONED HARNESS AND CLEANED CONNECTIONS. OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 2002080700176 20020807 00176 WP 2002 8 7 GTIA020690 1 20020610 A 5311 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND MID PIT HAS CORROSION AT THE FRAME STATION 731. MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED FRAME ANG LE IN AREA. DRILLED AND LOCATED NEW FRAME ANGLE. INSTALLED NEW FRAME ANGLE. (M) 2 L 7 2 4F A6WE 2002080700177 20020807 00177 WP 2002 8 7 GTIA020691 1 20020603 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND WEB CORRODED AT FS 83, X=48 Z=11. AFTER CORROSION THE WEB IS FOUND OUT OF LIMITS. FABRICATED REPAIR DOUBLE R. INSTALLED REPAIR DOUBLER IAW IAW MD80 SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F A6WE 2002080700178 20020807 00178 WP 2002 8 7 GTIA020692 1 20020602 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - E/E COMPARTMENT STATION 189 -X6 WEB HAS CORROSION VIEWED, E/E CEILING. SUB FLOOR WEB FOUND OUT OF LIMITS. FABRIC ATED DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2002080700179 20020807 00179 WP 2002 8 7 GTIA020693 1 20020610 A 5320 SPLICE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND MID CARGO LONGERON 30 STATION 589 SPLICE HAS CORROSION. LOSS FOUND TO BE OUT OF LIMITS. DUPLICATED LONGERO N SPLICE, L30, AT FUSELAGE STATION 589. INSTALLED NEW SPLICE AT STATION 589 L30 IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002080700180 20020807 00180 WP 2002 8 7 GTIA020694 1 20020530 A 5730 PANEL DOUG DC9 DC981 3022081 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND RIGHT WING L/E PANEL NR 1246C HAS TOOL MARKS ARE BARE METAL ON BACK. UPON BLENDING CRACK FOUND AT FASTENER HOLE. FORMING DOUBLER. INSTALLED DOUBLER IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002080700181 20020807 00181 WP 2002 8 7 GTIA020695 1 20020601 A 5320 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND AFT FUSELAGE RIGHT BEHIND THE RUDDER TRIM AND LOAD-FEEL CABLE DRUM THERE IS A DOUBLER CRACKED. REMOVED EXIS TING REPAIR DOUBLER. FABRICATED NEW REPAIR DOUBLER. INSTALLED REPAIR DOUBLER PER DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002080700182 20020807 00182 WP 2002 8 7 GTIA020696 1 20020529 A 5730 PANEL DOUG DC9 DC981 3022081 WP RT WING CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND RIGHT WING L/E PANEL NR 1244C CHAFFED AND BARE METAL ON BACK, TOOL MARKS ON SKIN. IN THE PROCESS OF BLENDING CHAFING CORROSION WAS FOUND. FORMER STRAP REPAIR. INSTALLED STRAP REPAIR IAW SRM MD80 51-30-2. (M) 2 L 7 2 4F A6WE 2002080700183 20020807 00183 EU 2002 8 7 02218301 1 20020806 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 301UE 41012 During preflight inspection, the crew reported that the forward emergency floor track lights were inoperative. Maintena nce personnel secured the connector for the forward emergency floor track lights. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002080700184 20020807 00184 SO 2002 8 7 C2XA02IA156 1 20020803 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13994 6289 2347 145291 During preflight inspection the #4 emergency light pack was found to be discharged. Maintenance removed and replaced the affected battery pack and the aircraft was returned to service. 2 L 7 2 4T RT T00011AT 2002080700186 20020807 00186 EA 2002 8 7 CA020708010 2 20020703 A 7530 302968 FILTER DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A34 52043 EA P3 DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) P3 FILTER WAS IN THREE PIECES WHEN REMOVED FROM P3 HOUSING . IT WOULD APPEAR THAT THE BONDING AGENT THAT WAS USED FAILED OR NOT THE RIGHT QUANITY USED. 1 H 7 1 3R 4 T A815 E4EA 2002080700187 20020807 00187 EA 2002 8 7 CA020709001 1 20020618 A 8012 624907B CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE STARTER FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 15855 (CAN) RT ENGINE STAGNED AT APPROX. 30 PERCENT DUE TO THE LT ENGINE 10 STAGE CHECK VALVE FLAPPER BROKEN. THE LT VALVE WAS REPLACED, INSPECTION WAS PERFORMED ON THE DUCTS, STARTER VALVES AND ENGINE RUN 2 L 7 2 4F 4 F RT A21EA E15NE 2002080700189 20020807 00189 EA 2002 8 7 CA020710001 1 20020709 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A 30015 NE MLG DOOR MALFUNCTIONED W O OTHER N FALSE WARNING AP APPROACH 1 CA 14635 (CAN) ON APPROACH, AFTER LANDING GEAR SELECTED DOWN, MESSAGE GEAR DISAGREE (WARNING) POSTED ON EICAS ALONG WITH NOSE LAN DING GEAR BOX AMBER INDICATION. (MAIN GEAR WERE DOWN AND LOCKED.) FLIGHT CREW FOLLOWED THE QRH AND SELECTED THE MANUAL G EAR RELEASE. NOSE GEAR EXTENDED AND THE AIRCRAFT LANDED SAFELY. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080700190 20020807 00190 SW 2002 8 7 CA020710002 1 20020623 A 7600 ENGINE GULSTM 690TP 690 0141720 SW GARRTT TPE331 TPE3315251K NM LEFT FAILED W E C ENGINE SHUTDOWN ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CA (CAN) AIRCRAFT WAS ON BUTTON OF RUNWAY AND WAS CLEARED FOR TAKEOFF. THE CONDITION LEVERS WERE ADVANCED TO HIGH RPM. BOTH ENGINES ACCELERATED BUT AS THE RPM REACHED APPROX. 96 PERCENT AN UNUSUAL LOAD NOISE WAS HEARD AND BOTH ENGINES SHUT DOW N. OIL WAS DRIPPING FROM THE LT ENGINE. 1 H 7 2 3T 4 T 2A4 E2WE 2002080700191 20020807 00191 NE 2002 8 7 CA020710003 2 20020709 A 7230 BLADE DORNER DO32 DO328300 NM PWA 306 PW306B NE COMPRESSOR FRACTURED W A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CA (CAN) RIGHT ENGINE OF A/C B3967, EXPERIENCED IFSD IN WESTERN CHINA (CHONGQING) ABOUT 10 MINUTES AFTER TAKING OFF. A LA RGE "BANG" WAS HEARD AT THE ALTITUDE OF 6000 METERS ( REPORTED BY THE PILOT). A/C RETURNED TO GATE SAFETY WITH SINGLE EN GINE. BOROSCOPE INSPECTION DISCLOSED HPT BLADES TO BE FRACTURED. 2 H 7 2 4T 4 F RT A55NM E35NE 2002081900085 20020819 00085 NM 2002 8 19 QXEA0201104 1 20020802 A 2910 HYDRAULIC LINE DHAV DHC8 DHC8202 2809007 NM HYD SYSTEM LEAKING A QXEA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 NM 09 346PH 477 PDX- DURING TAXI, UPON TRANSFER OF HYDRAULIC FLUID FROM NR 2 SYSTEM TO NR 1 SYSTEM, LOST ALL FLUID FROM NR 1 NACELLE. R EMOVED AND REPLACED BRAKE LINE AND RESERVICE BOTH HYDRAULIC SYSTEMS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SER VICE. 2 H 7 2 4T RT A13NM 2002080700192 20020807 00192 CE 2002 8 7 GLBA2002115 1 20020802 A 5600 10138402518 WINDSHIELD BEECH 1900 1900D 1154162 CE CRACKED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 247GL 128 UE247 #2 WINDSHIELD CRACKED AT 24,000, REPLACED WINDSHIELD 2 L 7 2 4T RT A24CE 2002080700193 20020807 00193 NM 2002 8 7 02218402 1 20020806 A 7500 31B419703 SOLENOID DORNER DO32 DO328300 NM A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 402FJ 3147 During the climb, the crew reported that the R/H engine had exceeded ITT limits. The flight returned to CVG and landed without incident. Maintenance personnel performed an engine data download and engine runs with no defects or ITT exceed ence noted. The bleed shut-off valve solenoids were replaced as a precaution. 2 H 7 2 4T RT A55NM 2002080700194 20020807 00194 NM 2002 8 7 02FDEA00421 1 20020621 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 CORROSION AT INNER SKIN SURFACE AT BS 470, WL 138, BL 0, COMMON TO ANTENNA MOUNT AREA. 2 L 7 3 4F RT A3WE 2002080700195 20020807 00195 EU 2002 8 7 YENA20015 1 20020702 A 2751 WARNING SYSTEM AIRBUS 320 A320232 3930326 EU COCKPIT MALFUNCTIONED A YENA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 15 531JB 1650 ON FINAL FLAPS SELECTED TO 2 ECAM F/CTL FLAPS LOCKED MESSAGE. GO-AROUND WAS INITIATED. EMERGENCY DECLARED. PERFORMED VISUAL INSPECTION OF FLAP INTERCONNECTING STRUTS. NO DEFECTS NOTED. ALSO INSPECTED ASSOCIATED WIRING, NO DEFECTS NOTED . PERFORMED RESET OF WING TIP BRAKES THROUGH USE OF THE MCDU, AND SFCC 1&2. OPERATION CHECK GOOD. INSPECTED FLAP TORQ UE LIMITERS, NO DEFECTS. PERFORMED OPS CHECK OF FLAPS PER A320 27-54-00-701-001. PERFORMED OPS CHECK OF WINGTIP BRAKE. BRAKE RESET PER A320 AMM 27-50-00-364-006. ALL SYSTEM CHECKS GOOD. 2 L 7 2 4F RT A28NM 2002080700196 20020807 00196 EU 2002 8 7 YENA200208 1 20020323 A 2810 L95F50603 RELIEF VALVE AIRBUS 320 A320232 3930326 EU LT WING TANK FAULTY A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 523JB 2741 2741 1506 FLIGHT 91, JFK TO OAK, AIR TURNBACK TO JFK DUE CENTER TANK MODE SEL FAULT. THE ONLY TANK THAT BURNED FUEL WERE THE LEFT WING TANK. NO FUEL BURNED FROM CENTER OR RIGHT WING TANK. FOUND LT TANK TRANSFERRING FUEL TO CENTER TANK. REMOVED AN D REPLACED LT CENTER TANK FUEL PUMP CANNISTER PER MM 28-21-52-401, OPS AND TANK CHECK GOOD. WHILE REFUELING RECEIVED EC AM FUEL AUTO FEED FAULT. FOUND FUEL OVERPRESSURE PROTECTOR 96QM FAULTY, OPENED TANK PLATES ACCESS, REPLACED FUEL OVERPR ESSURE PROTECTOR PER AMM TASK 28-12-41-401 LEFT WING TANK, INSTALLED TANK PLATES 147AZ, 148AZ AND 550CB PER AMM 57-17-11 , LEAK & OPS CHECK OK. 2 L 7 2 4F RT A28NM 2002080700197 20020807 00197 NE 2002 8 7 CA020710004 2 20020709 A 8510 519587 CASE CNDAIR CL215 CL2151A10 1900320 EA PWA R1340 CWASP 52016 NE ENGINE DAMAGED W E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) FLIGHT CREW OBSERVED OIL LEAKING FROM RT ENGINE AND INITIATED A PRECAUTIONARY ENGINE SHUTDOWN. AIRCRAFT LANDED SAF ELY WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NOSE CASE PLUG INSERT THREADS HAD STRIPPED IN CASE. THREADS HAD BEEN REP AIRED IN ACCORDANCE WITH SB 1755 REVISION B AT OVERHAUL. NOSE CASE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4R 3 R RT A14EA ATC14 2002080700200 20020807 00200 NM 2002 8 7 CA020711003 1 20020704 A 3250 CONTROL UNIT BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA STEERING FAILED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA (CAN) PILOT REPORTED UNCOMMANDED YAW ON TAKE-OFF AT V1. NO WARNINGS, CAUTIONS OR MESSAGES. A HIGH SPEED TAXI TEST WAS CA RRIED OUT, AND COULD NOT DUPLICATE THE SNAG. MAINTENANCE TROUBLE SHOOTING DETERMINED THE FOLLOWING:CDS MESSAGES PHC AND PSW. NO FAULTS IN THE AUTOFLIGHT FLIGHT GUIDANCE CONTROL PANEL (FGCP). STEERING CONTROL UNIT REPLACED AS PART OF TROUBLE SHOOTING. OPERATION TESTS CARRIED OUT AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002080700201 20020807 00201 EU 2002 8 7 YENA200209 1 20020403 A 3260 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU LANDING GEAR OUT OF ADJUST A YENA O OTHER N FALSE WARNING CL CLIMB 1 EA 15 505JB 7284 5 1173 DEPARTING PBI, FLIGHT 74, PBI TO JFK, GEAR WOULD NOT RETRACT WITH GEAR LEVER IN UP POSITION. BOTH GREEN DOWNLOCK AND RE D UPLOCK LIGHTS WERE OBSERVED ON LANDING GEAR PANEL. NO ECAM WAS OBSERVED. AFTER RECYCLE OF GEAR HANDLE, NORMAL GEAR R ETRACTION AND SYSTEM STATUS NORMAL WAS OBSERVED. PERFORMED DETAIL VISUAL INSPECTION OF NOSE LANDING GEAR AS PER AMM 32- 21-00. FOUND PROX SENSOR OUT OF ADJUSTMENT. REPLACED TARGET BUSHED LEVER, CLEVIS AND LINK ASSY AND ATTACHING HARDWARE AS PER AMM 32-21-27. PERFORMED TSM TASK 32-21-00-810-815, NO FAULT FOUND, REPLACED PROX SENSOR 25GA AS PER AMM 32-31-73 , OPS CHECK OK. 2 L 7 2 4F RT A28NM 2002080700202 20020807 00202 EU 2002 8 7 YENA200211 1 20020528 A 3240 C20105000 TACHOMETER AIRBUS 320 A320232 3930326 EU NR 1 BRAKE DAMAGED A YENA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 503JB 1123 AT JFK FLT 77, EXPERIENCED BRAKE ECAM ON T/O ROLL AT LOW SPEED. ABORTED T/O AND RETURNED TO GATE. T/S FOUND NR 1 TACH SPLINE DAMAGED & HUB CAP, ALSO NR 3 HUB CAP SPLINE FAN TACH. REMOVED AND REPLACED NR 1 TACH, NR 1 HUB CAP AND NR 3 HUB CAP PER AMM 32-42-68, 32-38-51, PERFORMED OPS CHECK PER AMM 32-42-00, SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2002080700203 20020807 00203 EU 2002 8 7 YENA200212 1 20020601 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN FAILED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 503JB 1123 AT JFK, ON WEEKLY EMERGENCY LIGHT SYSTEM TEST HAD EPSU LEFT FAILURE. REMOVED AND REPLACED LEFT EPSU AND GROUND OPS CHEC KED OK PER MM 33-51-00. 2 L 7 2 4F RT A28NM 2002080700206 20020807 00206 EU 2002 8 7 YENA200213 1 20020601 A 2121 EVT3454H FAN AIRBUS 320 A320232 3930326 EU E/E BAY SEIZED A YENA O OTHER E B J VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 EA 15 516JB 6467 6467 1302 FLT 20 JFK TO ROC, ON DESCENT NOTICED VIBRATION AND SMELL OF SMOKE. RECEIVED ECAM VENT-EXTRACT FAULT. PERFORMED ECAM A CTION- EXTRACT OVRD. PERFORMED A VISUAL INSPECTION, FOUND EXTRACT FAN SEIZED, NO FURTHER DEFECT NOTED AT THIS TIME, OK TO CONTINUE. REMOVED AND REPLACED EXTRACT FAN IAW 21-26-51-401, OPS CHECK OK. PLACARD REMOVED IAW 23-73-00. 2 L 7 2 4F RT A28NM 2002080700207 20020807 00207 EA 2002 8 7 COMA0260466 1 20020805 A 7720 ENGINE CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SO 01 957CA 7109 FLIGHT 5596 TAKE OFF ABORTED DUE TO RIGHT HAND ITT 900 DEG.COULD NOT DUPLICATE NO DEFECTS FOUND, COMPLIED WITH RTO INSPE CTION. 2 L 7 2 4F RT A21EA 2002080700209 20020807 00209 EU 2002 8 7 CA020712004 1 20020712 A 2131 90221570210 CONTROLLER AIRBUS 320 A320212 3930322 EU CFMINT CFM56 CFM565A3 NE CABIN PRESSURE MALFUNCTIONED W B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) IN CRUISE AT FL 390, NOTICED A CHANGE IN CABIN PRESSURE, AND ECAM CRUISE PAGE INDICATEDCABIN V/S RATE OF +700FPM. THERE WERE NO ECAM WARNINGS OR ADVISERIES.INITIAL ACTIONS AS RECOMMENDED BY AIRBUS OEB 139/1 (FCOM 3.07) CARRIED OUT, I. E. 2 L 7 2 4F 4 F RT A28NM E29NE 2002080700210 20020807 00210 EA 2002 8 7 COMA0260467 1 20020802 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 987CA 4246 7199 FLIGHT 5730 EMERGENCY LIGHTS ARE INOPERABLE, SWITCH LEFT IN ON POSITION.REPLACED THE EMERGENCY LIGHTS BATTERY. 2 L 7 2 4F RT A21EA 2002080700212 20020807 00212 NM 2002 8 7 QXEA0201109 1 20020804 A 5210 BUSHING DHAV DHC8 DHC8202 2809007 NM ZONE 800 STICKING A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 353PH 496 SEA-FRONT DOOR STUCK, WOULD NOT OPEN. LOOSE SCREW ON HANDRAIL POSSIBLY BINDING UP. INSPECTED AND FOUND FORWARD HANDRAIL SUPPORT HINGE BOLT LOOSE AND MISSING THREADED BUSHING. REPLACED BUSHING AND BOLT. OPERATIONAL CHECK GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080700213 20020807 00213 EA 2002 8 7 COMA0260468 1 20020802 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 796CA 7338 FLIGHT 5898 EMERGENCY FLOOR LIGHTING IS INOPERABLE BETWEEN ROWS 2 AND 5.REPAIRED LOOSE WIRE CONNECTOR. 2 L 7 2 4F RT A21EA 2002080700215 20020807 00215 2002 8 7 YENA200216 4 20020704 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU CABIN SHORTED A YENA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 531JB 1650 FLIGHT 92 SLC TO JFK, IN FLIGHT LIVE TV ROWS 16-26 ABC BLACK SCREENS. VERBAL NOTIFICATION OF A SUSPECTED BURNT ODOR FRO M THE AREA OF ROW 27 MOMENTARILY PRIOR TO FAILURE. CB DID NOT TRIP. REMOVED AND REPLACED 27C SEB AND 27C SEAT CABLE, O PS CHECK OK PER LIVE TV MM 23-38-00. 2 L 7 2 4F RT A28NM 2002080700217 20020807 00217 EA 2002 8 7 CA020714001 1 20020712 A 5741 2153103658 ATTACH ANGLE CNDAIR CL215 CL2151A10 1900320 EA WING TO FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACK FOUND AT UPPER ATTACH FASTENER HOLE DURING NDT REQUIRED BY AD 1997-07R2 WHOSE REQUIREMENTS ARE EVERY 415 FLI GHT HOURS OR 1500 WATER DROPS, WHICHEVER COMES FIRST. THIS AIRCRAFT HAD 837 WATER DROPS SINCE THE LAST COMPLIANCE OF THI S AD. 2 H 7 2 4R RT A14EA 2002080700218 20020807 00218 EA 2002 8 7 CA020715002 1 20020712 A 5711 SPAR CAP CNDAIR CL215 CL2151A10 1900320 EA WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACK FOUND AT REAR LOWER SPAR CAP AT WS51 AND FS434 DURING NDT REQUIRED BY AD 92-26 WHOSE REQUIREMENTS ARE EVERY 600 FLIGHT HOURS OR 2000 WATER DROPS, WHICHEVER COMES FIRST.THE NDT INDICATION IS OF A 1/4 INCH CRACK AND IS NOT VISIBLE . THIS AIRCRAFT HAD 820 WATER DROPS SINCE THE LAST COMPLIANCE OF THIS AD. 2 H 7 2 4R RT A14EA 2002080700219 20020807 00219 NE 2002 8 7 NACA20020028 2 20020531 A 8530 356994 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 1 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 779TA 1072 1072 45529 P32778 NR 1 ENGINE SHUT DOWN AT 0210Z DUE TO THE RUNNING ROUGH. REPLACED THE NR 1 CYLINDER ON THE NR 1 ENGINE. 2 L 7 4 4R 4 R A781 5E8 2002080700221 20020807 00221 NE 2002 8 7 NACA20020029 2 20020621 A 8530 356994 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 3 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 779TA 755 755 45529 NK510318 NR 4 ENGINE PRECAUTIONARY SHUT DOWN, ENGINE WOULDN'T TAKE A LEAN, BACKFIRED AND RUNNING ROUGH. REMOVED AND REPLACED THE NR 3 CYLINDER ON THE NR 4 ENGINE. 2 L 7 4 4R 4 R A781 5E8 2002080700222 20020807 00222 WP 2002 8 7 NACA20020030 1 20020611 A 5330 SKIN DOUG DC6 DC6A 3021706 WP FUSELAGE CRACKED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 99330 43576 FUSELAGE SKIN CRACKED UNDER COPILOTS SLIDER WINDOW, IN 2 PLACES OUT OF RIVET HEAD. FABBED AND INSTALLED DOUBLER PATCH U SING .032 7075-T6 PER DC-6 O/H MANUAL FIGURES 11-7, 11-37, 11-52, AND 12-22. 2 L 7 4 4R 6A3 2002080700223 20020807 00223 WP 2002 8 7 NACA20020031 1 20020611 A 5330 SKIN DOUG DC6 DC6A 3021706 WP FUSELAGE CRACKED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 99330 43576 LOWER SKIN CRACKED AT STRINGER 25 RT. REPAIRED PER BOEING ROD SKETCH 02-06-20-001. 2 L 7 4 4R 6A3 2002080700224 20020807 00224 NE 2002 8 7 NACA20020032 2 20020715 A 7421 URHB32E SPARK PLUG DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 4 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 43872 396 396 533294 36434 PRECAUTIONARY SHUT DOWN THE NR 4 ENGINE IN CRUISE DUE TO SHORTED SECONDARY ON THE NR 11 CYLINDER. FOUND CRACKED NOSE CE RAMICS ON BOTH PLUGS. REMOVED AND REPLACED PLUGS. 2 L 7 4 4R 4 R A781 5E8 2002080700225 20020807 00225 NE 2002 8 7 NACA20020033 2 20020731 A 7510 652673831 DUCT BOEING 727 72723 1384004 NM PWA JT8 JT8* 52044 NE NR 2 ENGINE BROKEN A NACA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 03 992AJ 19428 654023 NR 2 ENGINE FIRE WARING LIGHT AND BELL ON CLIMBOUT, OUT OF ANCHORAGE. WARNING LIGHT WENT OUT WHEN POWER WAS REDUCED TO IDLE. REPLACED 13TH STAGE ANTI-ICE LINE. 2 L 7 3 4F 4 F A3WE E2EA 2002080700226 20020807 00226 NM 2002 8 7 PCAA0206064 1 20020613 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 MAINTENANCE DISCOVERED RIGHT FLOOR STRIP (EMERGENCY) LIGHTS FROM MID EXIT TO FORWARD EXIT INOPERATIVE. WIRING CONNECTOR S WERE REINSTALLED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080700227 20020807 00227 NM 2002 8 7 PCAA0206065 1 20020615 A 3610 SEAL DHAV DHC8 DHC8102 2809003 NM BLEED AIR LEAKING A PCAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 13 820EX 019 PHL-SYR FLIGHT 3814. WHILE IN CRUISE FLIGHT CREW REPORTED REAR BAY OVERHEAT CAUTION LIGHT FOR APU ILLUMINATED. CREW DE CLARED AN EMERGENCY AND DIVERTED TO MDT. MAINTENANCE FOUND A BLEED LEAK IN REAR BAY. O-RING AND PERRY SEALS REPLACED O N BLEED LINES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080700228 20020807 00228 NM 2002 8 7 PCAA0206068 1 20020620 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 819EX 016 MDT-FLIGHT 3800. CREW REPORTED THAT EMERGENCY LIGHTS CAME ON IN FLIGHT WITH NO POWER INTERRUPTION AND WILL NOT EXTINGUI SH. MAINTENANCE OPERATED EMERGENCY LIGHTS AS PER 33-50-03. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080700229 20020807 00229 NM 2002 8 7 PCAA0206069 1 20020623 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 811AW 201 DURING ROUTINE MAINTENANCE VISIT EMERGENCY AISLE LIGHT FOUND INOPERATIVE AND STRIP BROKEN. AFTER TROUBLESHOOTING FOUND BROKEN WIRE UNDER FLOOR. WIRE WAS REPAIRED AND LIGHT ASSEMBLY REPLACED. OPERATIONAL CHECK GOOD. BROKEN LENS SECTION R EPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080700230 20020807 00230 SO 2002 8 7 C2XA02TY120 1 20020807 A 7100 23072549 ENGINE RROYCE EMB 135 EMB135LR 3260305 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24517 CAE311571 145332 TYS, During a schedule inspection corrosion was found on the right engine fancase, lower side. Maintenance removed the c orrosion, applied chrome pickle solution to magnesium parts, applied corrosion resistant paint I/A/W-EC7000-01001, Ec722 0-01009, AE3007A-70-00-00-300-807 and 815. The repair was satisfactory and the aircraft will be released upon complectio n of the check. 2 L 7 2 4F RT T00011AT 2002080700233 20020807 00233 NM 2002 8 7 PCAA0207070 1 20020703 A 3350 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 843EX 335 DURING ROUTINE MAINTENANCE VISIT FORWARD UPPER, RIGHT UPPER EMERGENCY EXIT LAMP FOUND INOPERATIVE, FORWARD EXTERIOR LAMP INOPERATIVE, AND FORWARD OVERHEAD LAMP INOPERATIVE. ALL RELATED TO RIGHT POSITION EMERGENCY BATTERY POWER SUPPLIES. E MERGENCY LIGHT BATTERY REPLACED AT POSITION 200. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080700236 20020807 00236 SO 2002 8 7 C2XA02TY121 1 20020807 A 7100 23072549 ENGINE RROYCE EMB 135 EMB135LR 3260305 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24517 CAE311568 145332 TYS, During a schedule inspection corrosion was found on the left engine fancase, lower side. Maintenance removed the co rrosion, applied chrome pickle solution to magnesium parts, applied corrosion resistant paint I/A/W-EC7000-01001, EC7220 -01009, AE3007A-70-00-00-300-807 and 815. The repair was satisfactory and the aircraft will be released upon complection of the check. 2 L 7 2 4F RT T00011AT 2002080700237 20020807 00237 EA 2002 8 7 CA020715008 1 20020711 A 5220 H341931 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ESCAPE HATCH CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A C CHECK INSPECTION , WHILE PERFORMING TASK 52-22-00-720-801 THE FUNCTIONAL TEST OF THE CREW ESCAPE HATCH THE MECHANIC FOUND THAT THE OUTER HANDLE OF THE CREW ESCAPE HATCH WOULD NOT UNLOCK PROPERLY ALLOWING THE HANDLE TO EXTE ND AND ROTATE. THE HANDLE WAS REMOVED FROM THE CREW ESCAPE HATCH AND WAS REPLACED WITH A SERVICEABLE UNIT IN ACCORDANCE WITH CRJ SRTUCTURE REPAIR MANUAL 51-42-06.ADDITIONNAL INFO: HARTWELL IS THE MANUFACTURER 2 L 7 2 4F 4 F RT A21EA E15NE 2002080700238 20020807 00238 EU 2002 8 7 CA020715009 1 20020712 A 6320 4638001001 TRANSMISSION BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL MAIN ROTOR MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ONE CHIP LIGHT OCCURRENCE. CHIP PLUG AND FILTER INSPECTED AND AN EXCESSIVE AMOUNT OF MAGNETIC PARTICLES WERE FOUND . THE FILTER HAD BEEN INSPECTED 10 HRS PREVIOUSLY. THIS FAILURE IS USUALLY INDICATIVE OF A FAILED INPUT QUILL. 1 G 7 2 3U 3 U H3EU E4CE 2002080700239 20020807 00239 NM 2002 8 7 UPS02239011 1 20020723 A 5310 CHANNEL BOEING 727 72722C 138400F NM BS 1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C CRACK ON CHANNEL SECTION IN LWR AFT CARGO HOLD AT BS 1060 BBL 8L REPAIRED IAW SRM 53-10-5 FIG 4 2 L 7 3 4F A3WE 2002080700240 20020807 00240 NM 2002 8 7 UPS02239012 1 20020722 A 5310 WINDOW POST BOEING 727 72722C 138400F NM CENTER LH & RH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C CRACKS ON CENTER WINDOW POST ON LWR LHS & RHS COCKPIT CENTER WINDOW POST REPAIRED IAW UPS EO B727- 5330-5128 2 L 7 3 4F A3WE 2002080700242 20020807 00242 NM 2002 8 7 UPS02438989 1 20020708 A 5310 BULKHEAD BOEING 747 747123F NM BS 1480 L/R A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C CARRY OUT BS 1480 BULKHEAD AND SPLICE COMPONENT MODIFICATION AS PER SB 747-53A2390 R1 PLAN B. BS 1 480 L/R B/H & SPLICE COMPONENT MOD C/OUT AS PER SB 747-53A2390 R.1 PLAN B AS PER FIG 2,3,4,6,7,8,14,17,19,20,23 & 28, AP PENDIX 'A', 'C' & 'D', REFER HX RS R-53-43-34841 & UPS EO B747-5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. 2 L 7 4 4F A20WE 2002080700243 20020807 00243 NM 2002 8 7 UPS02438990 1 20020705 A 5310 BULKHEAD BOEING 747 747123F NM BS 1480 LH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C CRACK FOUND AT UPPER BULKHEAD FORGING RADIUS AREA, CRACK RUNNING UPWARD 1.5" IN LENGHT APPROX. L/H BS 1480 B/H CHORD FWD RADIUS CRACKED AREA TRIMMED OFF & REPAIRED PER HX RS R-54-43-34841 ITEM '14' & '15'. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-0 6. 2 L 7 4 4F A20WE 2002080700244 20020807 00244 NM 2002 8 7 UPS02438992 1 20020701 A 5310 SKIN BOEING 747 747123F NM BS1480 R/H CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C R/H BS 1480 FUSELAGE SKIN AT EXTENSION FITTING AREA CRACK AT HOLE #1 , 9 O'CLOCK POSITION AT I/B SURFA CE APPROX 0.100" IN LENGTH (LOOKING I/B). R/H BS 1480 FX SKIN CRACK AT HOLE #1, HOLE FINAL SIZE 0.6875" & PLAN B RE PAIR BUSHING INSTALL PER SB 747-53A2390 R.1 FIG 14. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06. 2 L 7 4 4F A20WE 2002080700245 20020807 00245 NM 2002 8 7 UPS02438995 1 20020701 A 5310 SKIN BOEING 747 747123F NM BS 1480 RH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C R/H OF BS 1480 FUSELAGE SKIN AT EXTENSION FITTING SRES FOUND CRACK AT HOLE #11 RUNNING AT 5 O'CLOCK PO SITION ( VIEW LOOKING I/B )WITH 1/16" IN LENGTH APPROX AT I/B SURFACE. RH BS 1480 FX SKIN AT HOLE #11 CRACK FREE FIN AL SIZE 0.6875" & PLAN B REPAIR BUSHING INSTALL PER SB 53A2390 R.1 FIG 14. REFER HX RS R-53-43-34841 & UPS EO 5310-17208 -A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06. 2 L 7 4 4F A20WE 2002080700246 20020807 00246 NM 2002 8 7 UPS02438996 1 20020701 A 5310 FITTING BOEING 747 747123F NM BS 1480 RH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C R/H OF BS 1480 B/H LONGERON EXTENSION FTG FOUND CRACK AT HOLE #9 AT 3 O'CLOCK POSITION ( VIEW LOOKING I/B ), THE CRACK 1/16" IN LENGTH APPROX AT I/B SURFACE. RH BS 1480 BULKHEAD LONGERON EXTENSION FITTING AT HOLE #9 CR ACK FREE FINAL SIZE 0.8125" & PLAN B REPAIR BUSHING INSTALL PER SB 53A2390 R1 PLAN B & HX RS R-53-43-34841. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11- 06. 2 L 7 4 4F A20WE 2002080700247 20020807 00247 NM 2002 8 7 UPS02438997 1 20020702 A 5310 FITTING BOEING 747 747123F NM BS 1480 LH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C L/H BS 1480 B/H AREA, HOLE #9 CRACKS FOUND AT EXTENSION FITTING RUNNING UPPER & FWD, CRACK THROUGH THI CKNESS. LH BS 1480 B/H LONGERON EXTENSION FTG HOLE #9 CRACK FREE FINAL SIZE 0.8745" & PLAN B REPAIR BUSHING INSTAL L PER SB 53A2390 R1 PLAN B. REFER HX RS R-53-43-34841 & UPS EO 5310-17028-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06. 2 L 7 4 4F A20WE 2002080700248 20020807 00248 NM 2002 8 7 UPS02439001 1 20020701 A 5310 SPLICE PLATE BOEING 747 747123F NM BS 1480 RH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C R/H OF BS 1480 B/H WEB SPLICE PLATE FOUND CRACK AT HOLE #15 LOCATED AFT SIDE SURFACE APPROX 1/16" IN L ENGTH. RH BS 1480 BULKHEAD WEB SPLICE PLATE AT HOLE #15 FINAL SIZE 0.500" & PLAN B REPAIR BUSHING INSTALL PER SB 53 A2390 R.1 FIG 14. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLA N PER SB 53A2390 & AD 2001-11-06. 2 L 7 4 4F A20WE 2002080700249 20020807 00249 NM 2002 8 7 UPS02439004 1 20020709 A 5310 SKIN BOEING 747 747123F NM BS 1480 LH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C CRACK FOUND AT BS 1480 LHS B/H ATTACHED SKIN AT 1 EA FASTENER HOLE OF S34L STRINGER ENG FTG LOWER HOLE . THE CRACK LOCATED AT 8 O'CLOCK POSITION AND WITH LENGTH 0.050" APPROX. LH BS 1480 B/H FX SKIN AT STR 34 AREA AT HO LE #9 CRACK FREE FINAL SIZE 0.500" AND REPAIR BUSHING INSTALL PER HX RS R-53-43-34841 ITEM '1' & '3' FIG '1'. REFER HX R S R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & 2001-11-06 . 2 L 7 4 4F A20WE 2002080700250 20020807 00250 NM 2002 8 7 UPS02439005 1 20020712 A 5310 SKIN BOEING 747 747123F NM BS 1480 RH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C R/H OF BS 1480 BULKHEAD S34R STRINGER END FITTING COMMON TO SKIN AREA, 1 EA FASTENER HOLE FOUND CRACK AT INNER SKIN AT FWD AND AFT DIRECTION CRACK LENGTH UNDETERMINED DUE COVERED BY OVERLAPPING SKIN. RH BS 1480 B/H AT STR 34R AREA SKIN 1 EA CRACK HOLE CRACK FREE FINAL SIZE 0.625" & REPAIR BUSHING INSTALL PER HX RS R-53-43-34841 ITEM 3 F IG 4. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2 390 & AD 2001-11-06. 2 L 7 4 4F A20WE 2002080700251 20020807 00251 EA 2002 8 7 CA020715011 1 20020706 A 5220 H341931 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ESCAPE HATCH CORRODED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) DURING A C CHECK INSPECTION WHILE PERFORMING THE CREW ESCAPE HATCH FUNCTIONAL CHECK, MAINTENANCE WERE UNABLE TO OP EN THE HATCH USING THE EXTERNAL HANDLE. THE HANDLE WOULD NOT UNLATCH WHEN THE EXTERNAL TRIGGER WAS PUSHED.FURTHER VERIFI CATION ON THE BENCH REVEALED CORROSION ON THE INNER SHAFT OF THE EXTERNAL ASSEMBLY. THE HANDLE WAS REMOVED AND A NEW HAN DLE WAS INSTALLED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080700252 20020807 00252 SW 2002 8 7 CA020716001 1 20020710 A 2436 VOLT REGULATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL GENERATOR UNSERVICEABLE W E H ENGINE SHUTDOWN DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 CA (CAN) AFTER NORMAL START, THE GENERATOR "ON" SWITCH WAS ACTIVATED, BUT THE GENERATOR DID NOT COME ON LINE.IN TROUBLESHOO TING THE PROBLEM, IT WAS TRACED TO A FAULTY VOLTAGE REGULATOR, WHICH WAS SUBSEQUENTLY REPLACED WITH AN AIRWORTHY PART. 1 G 7 1 3U 3 U H2SW E4CE 2002080700254 20020807 00254 EU 2002 8 7 CA020718001 1 20020711 A 6320 4638001009 TRANSMISSION BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL MAIN ROTOR MAKING METAL W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) WHILE IN NORMAL CRUISE CONFIGURATION "MAIN TRANSMISSION" LIGHT ILLUMINATED. PILOT ACTIVATED PULSE CHIP DETECTOR SY STEM AND LIGHT EXTINQUISHED. THE LIGHT RE-ILLUMINATED APPROX. 1.5 HOURS LATER. THE PILOT ONCE AGAIN ACTIVATED THE PULSE CHIP. DETECTOR SYSTEM, THE LIGHT EXTINGUISHED & REMAINED OUT FOR REMAINDER OF FLIGHT WHICH WAS APPROXIMATELY 45 MINUTES. MAINTENANCE PERSONNEL EXAMINED THE MAIN EXSN CHIP DETECTOR & EXTERNAL OIL FILTER. BOTH CONTAINED CONSIDERABLE AMOUNTS OF MAGNETIC METAL MATERIAL. AIRCRAFT SECURED & MAIN TRANSMISSION TO BE REPLACED. 1 G 7 2 3U 3 U H3EU E4CE 2002080700255 20020807 00255 EA 2002 8 7 CA020718002 1 20020712 A 5220 H341931 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ESCAPE HATCH CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A C CHECK INSPECTION WHILE PERFORMING THE CREW ESCAPE HATCH FUNCTIONAL CHECK, THE HANDLE WAS HARD TO UNLATC H.THE ASSEMBLY WAS REMOVED AND LIGHT CORROSION WAS FOUND ON THE SHAFT.THE LIGHT CORROSION ON THE SHAFT WAS REMOVED, THE HANDLE WAS REINSTALLED AND LUBRICATED.MULTIPLE OPERATIONS WERE SUCCESSFULLY CARRIED OUT. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080700256 20020807 00256 EU 2002 8 7 CA020718003 2 20020604 A 7200 ENGINE FOKKER F27 F27MK400 4990626 EU RROYCE DART DART5327 54509 EU RIGHT FAILED W O OTHER X ENGINE FLAMEOUT CR CRUISE 1 CA (CAN) A/C FLYING FROM YYC TO YVR. PROP & INLET ANTI-ICE WERE SELECTED ON & APPEARED TO BE WORKING. WHILE OVER YLW AT 16, 000, IN LIGHT TO MODERATE ICING, RT ENGINE FLAMED OUT. AFTER CARRYING OUT SHUTDOWN CHECKLIST, CREW PERFORMED SUCCESS RE- LIGHT, ENGINE POWER & RPM CAME UP NORMAL EXCEPT FOR SLIGHT SURGE WHICH APPEARED TO FOLLOW FUEL PRESSURE FLUX. ENGINE FUE L HEATER TURNED ON (IT OFF PRIOR TO FLAMEOUT). AT POINT SURGE&FUEL PRESSURE FLUXQUICKLY DISAPPEARED. A/C MADE UNEVENTFUL LANGING AT YVR. MAINT CHECKED ALL FUEL TANKS, COLLECTORS,&FUEL FILTERS&FOUND NO CONTAMINATION. FCU CHANGED OUT AS SCHED ITEM TO TAKE ADVANTAGE OF DOWNTIME BUT NOT TO CORRECT PROBLEM. 2 H 7 2 4T 4 T A817 E297 2002080700257 20020807 00257 WP 2002 8 7 CA020718004 2 20020622 A 7250 SEAL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL LT ENGINE LEAKING W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 21212 (CAN) WHILE ENROUTE FROM SEA TO YVR IN CRUISE, LT OIL PRESSURE DROPPED AS INDICATED ON GAUGE AND LOW OIL PRESSURE WARNIN G LIGHT ILLUMINATED. CREW DID A PLANNED SHUTDOWN AND MADE AN UNEVENTFUL LANDING AT YVR. ATC WAS NOTIFIED BUT EMERGENCY N OT DECLARED. MAINTENANCE INVESTIGATION REVEALED ENGINE NEARLY OUT OF OIL. FURTHER INVESTIGATION SHOWED OIL DRIPPING FROM ENGINE REAR BEARING, NO OTHER EXTERNAL LEAKS FOUND. SUSPECT OIL LOSS CAUSED BY FAILED BEARING SEAL. ENGINE REMOVED FOR SHIPMENT TO OVERHAUL SHOP. FURTHER INFORMATION TO BE REPORTED WHEN KNOWN. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002080700258 20020807 00258 NM 2002 8 7 PCAA0207071 1 20020705 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 984HA 377 DURING ROUTINE MAINTENANCE VISIT EMERGENCY LIGHT AT AIRSTAIR DOOR EXIT FOUND INOPERATIVE. WIRING REPAIRED AT ATTACH POI NT TO TERMINAL IN WARDROBE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080700259 20020807 00259 NM 2002 8 7 PCAA0207072 1 20020706 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN CRUSHED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 845EX 344 DURING ROUTINE MAINTENANCE VISIT 10TH RED EMERGENCY LIGHT ON FLOOR FOUND INOPERATIVE. INSPECTION REVEALED CRUSHED LEAD WIRE TO LAMP. WIRE REPAIRED USING SPLICE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080700260 20020807 00260 NM 2002 8 7 PCAA0207074 1 20020714 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 835EX 289 PHL- FLIGHT 3643. CREW REPORTED FORWARD SEGMENT OF FLOOR EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE RESECURED FORWARD SEGMENT OF EMERGENCY LIGHT PLUGS. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080700261 20020807 00261 EU 2002 8 7 CA020718006 1 20020711 A 2741 MO46Z1402 TRANSMITTER AIRBUS 310 A310300 3930305 EU GE CF6 CF680C2A5 NE PITCH POSITION FAILED W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA (CAN) ON TAKE OFF ROLL A "TAKE-OFF CONFIGURATION WARNING" WAS TRIGGERED. AIRCRAFT SPEED WAS BELOW 80 KTS, CREW PROCEEDED WITH AN ABORTED TAKE OFF.TROUBLESHOOTING REVEALLED A DISCREPANCY BETWEEN THE THS POSITION INDICATION ON ECAM AND THE PI TCH TRIM WHEEL INDEX. MAINTENANCE REPLACED THE THS POSITION TRANSMITTER AND THE SYSTEM WAS TESTED WITH NO FURTHER DISCRE PANCIES. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A35EU E13NE 2002080700262 20020807 00262 NM 2002 8 7 PCAA0207075 1 20020717 A 7603 SPRING DHAV DHC8 DHC8102 2809003 NM POWER LEVER WEAK A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 843EX 335 PHL-FLIGHT 3810. CREW REPORTED POWER LEVERS CAN BE SELECTED TO BETA WITHOUT LIFTING TRIGGERS. MAINTENANCE CLEANED AND LUBED POWER LEVER MECHANISM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. AS A FOLLOW UP, MAINTENANCE INSPEC TED POWER LEVER REVERSE GATE, ASSOCIATED BEARINGS FOR BINDING, REPLACED SPRING P/N MS24586C39 (SUSPECTED WEAK SPRING TEN SION), AND VERIFIED PROPER OPERATION / RIGGING OF BETA WARNING HORN SWITCH. NO OTHER DEFECTS WERE FOUND. 2 H 7 2 4T RT A13NM 2002080700263 20020807 00263 SW 2002 8 7 CA020718007 1 20020626 A 2612 PROBE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL LT ENGINE OUT OF POSITION W E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) AIRCRAFT UNDERWENT A CHANGE OF THE LT ENGINE. GROUND RUNS WERE MADE, ALL APPEARED NORMAL. AIRCRAFT WENT FLYING ON A TRIP FROM YVR TO SER. SHORTLY AFTER TAKEOFF, THE LT ENGINE FIRE WARNING LIGHT ILLUMINATED. THE CREW PERFORMED A SHUTDO WN AND DISCHARGED THE FIRE BOTTLE. THE AIRCRAFT RETURNED TO YVR AND LANDING WAS UNEVENTFUL. MAINTENANCE INVESTIGATION RE VEALED ONE OF THE FIRE PROBES WAS POSITIONED TOO CLOSE TO A LINE THUS PROVIDING A GROUND WHEN SUBJECTED TO THE VIBRATION S OF FLIGHT. PROBLEM CORRECTED BY REPOSITIONING PROBE AND PROTECTION BOOT. FIRE BOTTLE SERVICED. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002080700266 20020807 00266 EA 2002 8 7 CA020718011 2 20020627 A 7200 PT6T3 ENGINE BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA NR 1 FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING D Y J INFLIGHT SEPARATION ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CA (CAN) AFTER TAKEOFF ON A SCHEDULED TRIP FROM THE FIRE CAMP, THE PILOT LEELLED THE AIRCRAFT AND REDUCED POWER TO NORMAL C RUISE POWER. AT THIS MOMENT HE HEARD A LOUD BANG AND FELT A PRONOUNCED YAW. THE NR 1 ENGINE OUT LIGHT ILLUMINATED AND AL L NR 1 ENGINE INSTRUMENTS INDICATED ZERO. THE PILOT CLOSED NR 1 ENGINE THROTTLE AND IMMEDIATELY RETURNED TO THE FIRE CAM P. AFTER A NORMAL LANDING THE OTHER ENGINE WAS SHUTDOWN. AN ONE ENGINE FERRY FLIGHT (WITH FERRY FLIGHT PERMIT) TO SLAVE LAKE, AB WAS CARRIED OUT. THE ENGINE HAS BEEN REMOVED FOR FAILURE INVESTIGATION. 1 G 7 1 4U 4 U H4SW E22EA 2002080700267 20020807 00267 WP 2002 8 7 CA020719001 1 20020704 A 6210 500P200101 BLADE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) MAIN ROTOR BLADE CRACKED IN LOWER SKIN DISCOVERED AT STA 36.5. 1 G 7 1 3U 3 U H3WE E4CE 2002080700268 20020807 00268 2002 8 7 CA020719002 4 20020705 A 3416 DIAL AEROSONIC 10220011833 CESSNA 441 441 2076020 CE ALTIMETER MISMARKED W O OTHER W INADEQUATE Q C CR CRUISE 1 CA 165403 (CAN) THE ALTIMETER DIAL MARKED IN HG AND THE BARO SCALE SUB DIAL IS IN MB. 1 L 7 2 3T RT A28CE 2002080700269 20020807 00269 GL 2002 8 7 CA020719003 2 20020313 A 7250 BEARING HUGHES 369 369HS 4470728 WP ALLSN 250C 250C20 03013 GL NR 2 FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) CHIP LIGHT CAME ON AT START UP. ENGINE CHIP PLUGS WERE CLEANED ONLY TO COME ON AGAIN ON THE NEXT START UP. THE ENG INE WAS IMMEDIATELY PULLED AND SENT TO AN OVERHAUL SHOP. THEY DISCOVERED THAT THE PROBLEM WAS THE NR 2 BEARING RACE WAS BEING WARN AWAY. 1 G 7 1 3U 3 U H3WE E4CE 2002080700274 20020807 00274 NE 2002 8 7 CA020719008 2 20020702 A 7250 3037313 TURBINE WHEEL BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE ENGINE FAILED W A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKEOFF PILOTS HEARD A SOUND FROM RT SIDE OF AIRCRAFT. PILOTS NOTICED NO UNUSUAL ENGINE INDICATIONS BUT NOTI CED A HOLE IN THE EXHAUST STACK. THEY RETURNED TO THE AIRPORT AND AFTER LANDING SHUTDOWN THE ENGINE. ENGINEERING FOUND T HE SECOND STAGE PT TURBINE HAD LOST SOME BLADES. ENGINE WAS REMOVED AND RENTAL ENGINE INSTALLED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002080700277 20020807 00277 NM 2002 8 7 AWXA200200694 1 20020729 A 5315 BAC14902734 ANGLE BOEING 757 7572S7 1384962 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 0 0 23566 LCQ - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON REPAIR ANGLE AT LOWER FLOOR BEAM BS 377, LBL 02. MAINTENAN CE REMOVED REPAIR ANGLE AT LOWER FLOOR BEAM BS 377, LBL 02, FABRICATED A NEW REPAIR ANGLE, AND INSTALLED REPAIR IAW B757 -200 SRM 53-00-51, PG. 209-210. 2 L 7 2 4F RT A2NM 2002080700278 20020807 00278 2002 8 7 ZW0A0208501 4 20020806 A 2565 29982121 SLIDE DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9617R 53564 THE LEFT SIDE FORWARD CABIN DOOR ESCAPE SLIDE HAD LOW BOTTLE PRESSURE. REPLACED THE SLIDE ASSEMBLY. CHECK-C 10-11-01 MC I. --CLOSED-- 2 L 7 2 4F RT A6WE 2002080800001 20020808 00001 EU 2002 8 8 C2XA02IA159 1 20020807 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15827 175 IAH- DURING MAINTENANCE THE MECHANIC NOTED THAT NUMEROUS EMERGENCY LIGHTS DID NOT ILLUMINATE, POSITION 10WL. MAINTENAN CE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK AT LOCATION 10WL, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AN D, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080800002 20020808 00002 EU 2002 8 8 C2XA02IA160 1 20020807 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CBIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15827 175 IAH- DURING MAINTENANCE THE MECHANIC NOTED THAT NUMEROUS EMERGENCY LIGHTS FAILED TO ILLUMINATE AT POSITION 18WL. IAH- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY AT POSITION 18WL, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTE D, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002080800003 20020808 00003 NM 2002 8 8 02FDEA00423 1 20020621 A 7330 WARNING SYSTEM BOEING 727 727200 138407E NM COCKPIT MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 246FE 22068 FUEL HEAT ICING LIGHT ILLUMINATED ON ENG NR 3 APPROX 10-11000 MSL FOR ABOUT 1-2 MIN, THEN WENT OUT AND STAYED OUT. FUEL TEMP WAS +35DC. SUMPED ALL TANKS AND FOUND NO CONTAMINATION. FOUND FUEL FILTER PRESSURE SWITCH BACKSHELL EXTREMELY LO OSE AND WILL NEED TIGHTENING. REMOVED AND REPLACED CANNON PLUG BACKSHELL IAW 727-200 SMP'S NEEDS OPS CHECK, CANNON PLUG OPS CHECK GOOD. REMOVED AND REPLACED FUEL FILTER PRESS SWITCH FOR PRECAUTION IAW 727-200 M/M 73-14-021-4, LEAK CHECK G OOD. 2 L 7 3 4F RT A3WE 2002080800004 20020808 00004 NM 2002 8 8 02FDEA00424 1 20020622 A 3610 CLAMP BOEING 727 727200 138407E NM BLEED AIR LOOSE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 25 281FE 22348 LOWER AFT BODY OVERHEAT LIGHT CAME ON FOLLOWED RED TAB PROCEDURES. LIGHT EXTINGUISHED 1 MINUTE AFTER NR 3 BLEED AND RIG HT PACK VALVES WERE CLOSED. RAN NR 3 ENG PER JRH CHAPTER 5A, COULD NOT DUPLICATE. FAULT ON LEAK CHECK FOUND CLAMP LOOS E DOWN STREAM OF NR 3 ENG BLEED SHUT-OFF TIGHTENED SAME. C/W OVERHEAT ADJUSTMENT AND TEST OPS CHECKS NORMAL AS PER 727-2 00AMM26-14-000-5. 2 L 7 3 4F RT A3WE 2002080800005 20020808 00005 WP 2002 8 8 MWEA020422 1 20020603 A 3260 PROXIMITY SENSOR DOUG DC9 DC982 3022082 WP LANDING GEAR MALFUNCTIONED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 810ME 48072 AFTER TAKEOFF HAD 3 RED LIGHTS ON LANDING GEAR. ACCOMPLISHED QRH PROCEDURE. LANDING GEAR COULD BE HEARD CYCLING. HOWE VER ON RETRACTION GEAR LIGHT STILL RED. ON RETURN BACK TO MILWAUKEE ON DESCENT OUT OF 17,000 + 230 KTS TEMPERATURE +3 O N RAT GEAR LIGHTS WENT OUT. TROUBLESHOT LANDING GEAR INDICATING AND WARNING SYSTEM PER WDM 32-61-00 AND MM 32-60. FOUN D NO DISCREPANCIES. CLEANED AND TREATED SWITCH S1-89 AND LUBED SWITCH ACTUATOR. PERFORMED GEAR SWING. OPS CHECK OF IN DICATING/WARNING SYSTEM GOOD. REMOVED AND REPLACED PROX UNIT PER MM 32-60-04. OPS CHECK GOOD PER MM 32-60-04. 2 L 7 2 4F A6WE 2002080800006 20020808 00006 NM 2002 8 8 MWEA020461 1 20020721 A 7931 41800044 TRANSMITTER DOUG MD88 MD88 3023688 NM RT ENGINE FAULTY A MWEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 601ME 49762 THE RIGHT OIL PRESSURE WENT TO 56 & STARTED FLASHING LEFT WAS 52. DURING TAXI TO GATE BOTH OIL PRESS WERE AT 49. VERIF IED PROPER OIL PRESSURE RESTRICTOR FITTINGS (PRESSURE AND VENT) CLEANED VENT LINE AND REMOVED AND REPLACED RIGHT PRESSUR E TRANSMITTER REF DAC/MD80 MM 79-30. NO OIL PRESS ADJUSTMENT REQUIRED. 2 L 7 2 4F RT A6WE 2002080800007 20020808 00007 WP 2002 8 8 MWEA020471 1 20020730 A 3244 95502676 TIRE DOUG DC9 DC981 3022081 WP NLG VIBRATION A MWEA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 31 805ME 48031 AT AIRSPEED OF 30-40 KNOTS A STRONG SHIMMY AND VIBRATION OCCURRED IN THE NOSEWHEEL. REMOVED AND REPLACED LEFT AND RIGHT NOSE LANDING TIRE ASSEMBLY, LUBED NOSE LANDING GEAR AREA. TAXIED A/C AT HIGH SPEED WITH FLIGHT CREW. NO DISCREPANCIES NOTED AT THIS TIME. ALL WORK DONE IAW MD80 MM. 2 L 7 2 4F A6WE 2002080800008 20020808 00008 NM 2002 8 8 P2EA2002M046 1 20020627 A 5210 SKIN BOEING 737 737230 1384401 NM L1 DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 SKIN CRACK ON L1 DOOR AT LOWER AFT CORNER. REPAIRED SKIN IAW SRM 52-00-3. 2 L 7 2 4F RT A16WE 2002080800009 20020808 00009 NM 2002 8 8 P2EA2002M047 1 20020701 A 3350 LENS BOEING 737 737230 1384401 NM CABIN MISSING A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 122NJ 22120 ROW 4 EMERGENCY TRACK LIGHTING MISSING LENS. REMOVED AND REPLACED LENS IAW MM 33-53-0. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2002080800010 20020808 00010 WP 2002 8 8 P2EA2002M048 1 20020709 A 2897 WIRE HARNESS DOUG DC9 DC982 3022082 WP RT WING DEFECTIVE A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 137NJ 49229 DURING TROUBLESHOOTING THE RIGHT WING AFT FUEL BOOST PUMP WIRING HARNESS WAS FOUND DEFECTIVE. REMOVED AND REPLACED RIGH T WIND AFT BOOST PUMP WIRE HARNESS IAW MM 28-20-07. 2 L 7 2 4F A6WE 2002080800011 20020808 00011 WP 2002 8 8 P2EA2002M050 1 20020720 A 2120 VALVE DOUG DC9 DC987 3022087 WP A/C BAY MALFUNCTIONED A P2EA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 132NJ 49780 APPROX 25 MINUTES AFTER TAKEOFF WITH BOTH TEMP SWITCHES IN AUTO, BOTH AIR CONDITIONING PACKS SHUT DOWN. DESCENT INITIAT ED, CABIN ALT REACHED 15,000 FT BEFORE PACKS CAME BACK. PERFORMED AUGMENTATION VALVE ADJUSTMENT AND TEST IAW 36-10-04 O PS CHECK GOOD. INSPECTED ALL ELECTRICAL AND PNEUMATIC CONNECTIONS AT AUGMENTING VALVE, ALL GOOD. PERFORMED OPERATIONAL TEST OF A/C SYSTEM IAW 21-00-00, OPS CHECK GOOD. PERFORMED EVL FLIGHT, NO DEFECTS NOTED. 2 L 7 2 4F RT A6WE 2002080800012 20020808 00012 NM 2002 8 8 02FDEA00425 1 20020622 A 3231 SPRING DOUG MD11 MD11 3023602 NM LT MLG DOOR BROKEN A FDEA K NONE J WARNING INDICATION CL CLIMB 1 SO 25 578FE 48458 RED LIGHT IN BOTH PRIMARY AND SECONDARY LEFT MAIN GEAR AFTER TAKEOFF WHEN GEAR HANDLE IN THE UP POSITION. GEAR RECYCLED 3 TIMES, NO CHANGE. CONFORMED WITH QUICK REFERENCE HANDBOOK. CHECKED LT LANDING GEAR THEN FOUND LEFT LANDING GEAR DOO R LATCH SPRING BROKEN. REF TO IPC 32-34-05-01 ITEM 50. FOUND SPRING ON LEFT DOOR LATCH MECHANISM BROKEN AND WAS CAUGHT ON THE LOCK MECHANISM. INSPECTED LOCK AND RELATED MECHANISM, NO DEFECTS FOUND. REPLACED SPRING ON LEFT MLG DOOR LATCH PER MM 32-34-03-4 AND ALTERNATE RELEASE CHECK FOR LT MLG DOOR C/O PER REF MM 32-32-00-5. LEFT MLG PROX SENSOR TEST C/O PER MM 32-61-15-5 AND TESTED OK. OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2002080800013 20020808 00013 NM 2002 8 8 02FDEA00428 1 20020611 A 5314 KEELBEAM BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 RIGHT WHEEL WELL KEELBEAM FWD VERTICAL CHORD IS CRACKED BETWEEN TWO FASTENERS. R & R KEELBEAM PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002080800014 20020808 00014 NM 2002 8 8 02FDEA00429 1 20020621 A 5315 BAC1518332 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 CORROSION ON FLOORBEAM AT BS 890, LBL 50-52, WL 201 AFT SIDE OF LWR FLANGE UPPER SIDE. 2 L 7 3 4F RT A3WE 2002080800015 20020808 00015 NM 2002 8 8 02FDEA00431 1 20020626 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FOUND CORROSION ON SKIN UNDER WEB/INTERCOSTAL AT BS 950F - 970, LBL 14, WL 148. REPAIRED SKIN BS 950F - 970, LBL 14, WL 148 IAW SRM 53-30-3 FIG 3. 2 L 7 3 4F RT A3WE 2002080800016 20020808 00016 NM 2002 8 8 02FDEA00432 1 20020624 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CORROSION ON FRAME AND SHEAR TIE BS 990 BETWEEN STR 28-29 LT. REPAIRED SHEAR TIE & FRAME IAW FEDEX EA 7-5310-64980 & SR M 53-10-4 FIG 15. 2 L 7 3 4F RT A3WE 2002080800017 20020808 00017 NM 2002 8 8 02FDEA00433 1 20020626 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FOUND CORROSION AT STR 28L, BS 950F+8, WL 148. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 3. 2 L 7 3 4F RT A3WE 2002080800018 20020808 00018 NM 2002 8 8 02FDEA00434 1 20020625 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FOUND FRAME CORRODED AT BS 720C, RBL 25, WL 148 C53-111-01. REMOVED AND REPLACED FRAME PER SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2002080800019 20020808 00019 NM 2002 8 8 02FDEA00435 1 20020624 A 5320 ANGLE BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT AIRSTAIR RT LWR TORQUE BOX INTERNAL BS 1263 BULKHEAD UPPER FWD SIDE L-ANGLE IS CRACKED, JUST BELOW AIR STAIR ACTUATO R. REMOVED AND REPLACED AFT AIRSTAIR PER SRM 51-30-2 & 51-10-2. 2 L 7 3 4F RT A3WE 2002080800020 20020808 00020 WP 2002 8 8 02FDEA00436 1 20020619 A 5753 HINGE FITTING DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 370FE 46608 LEFT INBOARD FLAP OUTBOARD HINGE FITTING BOTTOM INBOARD ATTACH BOLT TO REAR SPAR BOX FITTING HAS RUST EMANATING FROM BET WEEN THE FITTING AND SPAR TANG. 2 L 7 3 4F A22WE 2002080800021 20020808 00021 NM 2002 8 8 02FDEA00437 1 20020626 A 5753 SUPPORT FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 RT WING INBOARD FLAP - OUTBOARD FWD HINGE SUPPORT FITTING LWR INBOARD BOLT AT ATTACH POINT IS EMITTING RUST BETWEEN MATT ING SURFACES. 2 L 7 3 4F RT A22WE 2002080800022 20020808 00022 NM 2002 8 8 02FDEA00438 1 20020626 A 5753 SUPPORT FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 RT WING INBOARD FLAP - OUTBOARD FWD HINGE SUPPORT FITTING LWR OUTBOARD BOLT AT ATTACH POINT IS EMITTING RUST AT MATTING SURFACE. 2 L 7 3 4F RT A22WE 2002080800023 20020808 00023 WP 2002 8 8 02FDEA00443 1 20020628 A 5753 BUSHING DOUG DC10 DC1010 3022110 WP T/E FLAP SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 RIGHT INBOARD FLAP OUTBOARD HINGE BUSHING ATTACHMENT FOUND SHEARED DURING REMOVAL OF FLAP PANEL ASSY. EVIDENCE LACK OF LUBRICATION. REF EA 8-5750-60767 SEQ 760. C/W EA 8-5750-60767 SEQ 760. 2 L 7 3 4F A22WE 2002080800024 20020808 00024 NM 2002 8 8 02FDEA00444 1 20020629 A 5753 SUPPORT FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING O/B FLAP I/B HINGE SUPPORT LWR ATTACH POINTS HAVE RUST EMITTING FROM MATING SURFACES. REMOVED AND REPLACED PE R MM 57-44-08. FAB 2 BUSHINGS PER CMM 57-44-08. 2 L 7 3 4F RT A22WE 2002080800025 20020808 00025 NM 2002 8 8 02FDEA00445 1 20020629 A 5753 SUPPORT FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING O/B FLAP HINGE SUPPORT FITTING LWR ATTACH POINTS HAVE RUST EMITTING FROM MATING SURFACES. REMOVED AND REPLACE D BOLT PER CMM 57-44-09. FAB BUSHING PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 2002080800026 20020808 00026 NM 2002 8 8 02FDEA00447 1 20020612 A 5751 652177613 FITTING BOEING 727 727200 138407E NM AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 186FE 18872 LEFT WING O/B AILERON FITTING CORRODED ON TOPSIDE OF FITTING. REMOVED AND REPLACED FITTING PER MM 27-10-131-4. 2 L 7 3 4F RT A3WE 2002080800027 20020808 00027 NE 2002 8 8 02FDEA00449 2 20020701 A 7230 COMPRESSOR AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE NR 2 ENGINE STALLED A FDEA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 25 405FE 237 IMMEDIATELY AFTER LEVEL OFF AT FL350, NR 2 ENG EXPERIENCED SEVERE COMPRESSOR STALLS. PWR WAS REDUCED, WHEN PWR WAS INCR EASED STALL RETURNED. F/F & EGT FLUX WAS EVIDENT AND N1 & 2 MOVED ACCORD. QRH PROC WAS ACCOMPL DURING DESCENT AND RETU RNED TO ABQ. WHEN HP VLV WAS SEL OFF PER QRH THERE WERE NO MORE STALLS, ACFT WAS NOW BELOW FL300. INSPECTED VSV ACTUAT ION SYSTEM, NO DAMAGE NOTED. INSPECTED MAGNETIC GEARBOX PLUG PER MM. NOTABLE MATTER FOUND. INSPECTED SCAV OIL FILTER PER MM, NO DEBRIS FOUND. 2 L 7 2 4F 4 F RT A35EU E13NE 2002080800028 20020808 00028 NM 2002 8 8 02FDEA00450 1 20020701 A 1430 ATTACH BOLT DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 LEFT WING INBOARD FLAP O/B HINGE LOWER ATTACHMENT BOLT INBOARD SIDE FOUND CORRODED. REMOVED AND REPLACED BOLT PER MM 57 -51-01. 2 L 7 3 4F RT A22WE 2002080800029 20020808 00029 NM 2002 8 8 02FDEA00451 1 20020701 A 1430 ATTACH BOLT DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 RIGHT WING INBOARD FLAP OUTBOARD HINGE LWR ATTACHMENT BOLT O/B SIDE FOUND CORROSION. REMOVED AND REPLACED BOLT PER MM 5 7-51-01, REF EA 1-5710-64290. 2 L 7 3 4F RT A22WE 2002080800030 20020808 00030 NM 2002 8 8 02FDEA00452 1 20020701 A 1430 ATTACH BOLT DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 LEFT WING I/B FLAP O/B HINGE LOWER ATTACHMENT BOLT O/B SIDE FOUND CORRODED. REMOVED AND REPLACED HINGE BOLT PER AMM 57- 51-01. 2 L 7 3 4F RT A22WE 2002080800031 20020808 00031 NM 2002 8 8 02FDEA00453 1 20020701 A 1430 BOLT DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 583FE 48421 RIGHT WING I/B TRAILING EDGE FLAP LOWER O/B HINGE BOLT CORRODED. REMOVED AND REPLACED BOLT PER EA 1-5710-64289. 2 L 7 3 4F RT A22WE 2002080800032 20020808 00032 NM 2002 8 8 02FDEA00454 1 20020701 A 1430 BOLT DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 583FE 48421 RIGHT WING I/B TRAILING EDGE FLAP LWR I/B HINGE BOLT CORRODED. REMOVED AND REPLACED BOLT PER MM 57-51-01-4. 2 L 7 3 4F RT A22WE 2002080800033 20020808 00033 NM 2002 8 8 02FDEA00455 1 20020701 A 1430 BOLT DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 583FE 48421 LEFT WING I/B TRAILING EDGE FLAP LWR O/B HINGE BOLT CORRODED. REMOVED AND REPLACED BOLT PER EA 1-5710-64289. 2 L 7 3 4F RT A22WE 2002080800034 20020808 00034 NM 2002 8 8 02FDEA00457 1 20020702 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 RIGHT WING O/B FLAP I/B HINGE LOWER REAR SPAR BEAM LUG FACES FOUND CORRODED. 2 L 7 3 4F RT A22WE 2002080800035 20020808 00035 NM 2002 8 8 02FDEA00458 1 20020702 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 LEFT WING O/B FLAP O/B HINGE REAR SPAR BEAM LOWER O/B HOLE FOUND CORRODED. REMOVED AND REPLACED HINGE PER CMM 57-44-09 FIG 401. 2 L 7 3 4F RT A22WE 2002080800036 20020808 00036 NM 2002 8 8 02FDEA00459 1 20020702 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 LEFT WING O/B FLAP O/B HINGE REAR SPAR BEAM LOWER I/B HOLE FOUND CORRODED. REMOVED AND REPLACED HINGE PER CMM 57-44-09 FIG 401, 20-11-01. 2 L 7 3 4F RT A22WE 2002080800037 20020808 00037 NM 2002 8 8 02FDEA00460 1 20020703 A 5610 WINDSHIELD DOUG MD11 MD11 3023602 NM COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 591FE 48527 FL 340, 300 MILES OUT OF CYWG, HEARD LOUD BANG. L1 OUTER WINDSCREEN SHATTERED. SAW POSSIBLE ARCING AFTER IT SHATTERED, COULD NOT TELL IF INNER WINDSHIELD WAS DAMAGED. REMOVED AND REPLACED L1 WINDSHIELD PER MD-11 M/M 56-11-01-4. OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION OFF MFG NBA6045-501. 2 L 7 3 4F RT A22WE 2002080800038 20020808 00038 NM 2002 8 8 02FDEA00461 1 20020705 A 1430 BOLT DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 RIGHT WING INBOARD T/E FLAPS OUTBOARD HINGE LWR OUTBOARD BOLT FOUND CORRODED. 2 L 7 3 4F RT A22WE 2002080800039 20020808 00039 EU 2002 8 8 02FDEA00462 1 20020705 A 3260 837101A PROXIMITY SENSOR AIRBUS 310 A310 EU LANDING GEAR MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 402FE 557 557 201 COULD NOT RETRACT GEAR ON POSITION 1 SELECTED POSITION 2 THE GEAR CAME UP (REPEAT WRITEUP) SUBSEQUENT INDICATIONS WERE PITCH TRIM INOP, ATS 2 OFF CAPT TAT INOP, (HEAT FAILURE) & CABIN PRESS REG 1 FAIL & NR 1 TRANSPONDER, NO ALTITUDE READO UT. REMOVED AND REPLACED PROX DETECTOR UNIT PER M/M 32-31-71-4. GEAR SWING CHECKS OK IN BOTH SYSTEM 1 AND 2. EXTENSIO N AND RETRACTION PERFORMED PER M/M 32-30-00-6. A/C OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A35EU 2002080800040 20020808 00040 NE 2002 8 8 02FDEA00465 2 20020709 A 7261 SEAL AIRBUS 310 A310 EU PWA JT9 JT9D7R4E1 52054 NE NR 1 ENGINE LEAKING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 NR 1 ENG STARTER DRIVE SHAFT OIL LEAKAGE. REMOVED AND REPLACED SEAL PER AMM 72-65-07-4-A. 2 L 7 2 4F 4 F RT A35EU E3NE 2002080800041 20020808 00041 EU 2002 8 8 02FDEA00466 1 20020709 A 5520 BEARING AIRBUS 310 A310 EU ELEVATOR WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 ELEVATOR HINGE ARM BEARING WORN BEYOND LIMITS AT ELEVATOR HINGE NR 7 RT. HINGE ARM REMOVED FOR BEARING REPLACEMENT. RE MOVED AND REPLACED BEARINGS & HINGE ARM PER AMM 55-10-43-4. 2 L 7 2 4F RT A35EU 2002080800042 20020808 00042 EU 2002 8 8 02FDEA00467 1 20020709 A 5553 PIN AIRBUS 310 A310 EU VERTICAL STAB ROTATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 VERTICAL STABILIZER LEFT MID ATTACH FITTING PIN INDICATOR LINE SHOWS PIN ROTATED. REMOVED AND REPLACED PIN PER AMM 55-3 6-39-6. 2 L 7 2 4F RT A35EU 2002080800043 20020808 00043 EU 2002 8 8 02FDEA00468 1 20020709 A 5520 BEARING AIRBUS 310 A310 EU ELEVATOR WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 ELEVATOR HINGE ARM BEARING WORN BEYOND LIMITS AT ELEVATOR HINGE NR 1 LT. HINGE ARM REMOVED FOR BEARING REPLACEMENT. RE MOVED AND REPLACED BEARINGS & HINGE ARM PER AMM 55-16-43-4. 2 L 7 2 4F RT A35EU 2002080800044 20020808 00044 EU 2002 8 8 02FDEA00469 1 20020709 A 5520 BEARING AIRBUS 310 A310 EU ELEVATOR WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 ELEVATOR HINGE ARM BEARING WORN BEYOND LIMITS AT ELEVATOR HINGE NR 5 RT. HINGE ARM REMOVED FOR BEARING REPLACEMENT. RE MOVED AND REPLACED BEARING AND HINGE ARM PER AMM 55-16-45. 2 L 7 2 4F RT A35EU 2002080800045 20020808 00045 EU 2002 8 8 02FDEA00470 1 20020709 A 5520 HINGE AIRBUS 310 A310 EU ELEVATOR WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 ELEVATOR HINGE ARM BEARING WORN BEYOND LIMITS AT ELEVATOR HINGE NR 6 RT. HINGE ARM REMOVED FOR BEARING REPLACEMENT. RE MOVED AND REPLACED HINGE ARM PER AMM 55-22-13. 2 L 7 2 4F RT A35EU 2002080800046 20020808 00046 EU 2002 8 8 02FDEA00471 1 20020709 A 5520 HINGE AIRBUS 310 A310 EU ELEVATOR WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 ELEVATOR HINGE ARM BEARING WORN BEYOND LIMITS AT ELEVATOR HINGE NR 1 RT. HINGE ARM REMOVED FOR BEARING REPLACEMENT. RE MOVED AND REPLACED BEARINGS PER AMM 55-16-43-4. 2 L 7 2 4F RT A35EU 2002080800047 20020808 00047 NM 2002 8 8 02FDEA00472 1 20020708 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CORROSION ON FRAME WEB BS 990, STR 24 RT. REPAIRED FRAME BS 990 STR 22-29 RT PER SRM 51-40-2. 2 L 7 3 4F RT A3WE 2002080800048 20020808 00048 WP 2002 8 8 02FDEA00473 1 20020707 A 3260 WARNING LIGHT DOUG DC10 DC1010 3022110 WP COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 371FE 46609 ON GEAR RETRACT GEAR HANDLE UP PILOT'S PANEL LT RED UNSAFE LIGHT REMAINED ON W S/O RT RED UNSAFE LIGHT ON. R/R PROX BOX MFG P/N 8-061-25 SN 237 2 L 7 3 4F A22WE 2002080800049 20020808 00049 NE 2002 8 8 02FDEA00474 2 20020709 A 7261 RELIEF VALVE BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE OUT OF ADJUST A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 490FE 21493 NR 2 OIL PRESSURE READ 60 PSI DURING INITIAL CLIMBOUT. AFTER REACHING 5K NR 2 THROTTLE PULLED TO IDLE IAW RED TAB PROCE DURE. OIL PRESSURE DROPPED TO 58 PSI INITIALLY THEN SLOWLY DROPPED INTO GREEN BAND APPROX 52 PSI AT IDLE AND REMAINED T HERE DURING APPROACH INTO MEM. ADJUSTED OIL PRESS RELIEF VALVE AND BROUGHT OIL PRESSURE IN LIMITS. RAN ENGINE AT HIGH POWER SETTING OIL PRESSURE WENT TO APPROX 48-49 PSI, 42 PSI AT IDLE. ALSO FOUND OIL TANK OVER SERVICED. SERVICED TO PR OPER LEVEL PER SMP REF PW ENGINE MANUAL 72-61-6. 2 L 7 3 4F 4 F RT A3WE E2EA 2002080800050 20020808 00050 NM 2002 8 8 02FDEA00475 1 20020710 A 2910 HYDRAULIC LINE BOEING 727 727200 138407E NM HYD SYSTEM LOOSE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 491FE 21529 RIGHT GEAR FAILED TO RETRACT AFTER T/O. GEAR DOOR INTRANSIT LIGHT FLICKERED GREEN, RIGHT GEAR LIGHT REMAINED ILLUM'D WI TH THE GEAR HANDLE IN THE OFF POSITION. SECURED LOOSE HYDRAULIC LINE ON SEQ VALVE AND RECENTERED RIGHT GEAR UPLOCK MECH MG, OPS CHECK OK PER MM 32-32-000-5. 2 L 7 3 4F RT A3WE 2002080800051 20020808 00051 NM 2002 8 8 02FDEA00476 1 20020706 A 1430 BOLT DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 RIGHT WING INBOARD T/E FLAP OUTBOARD HINGE LWR INBOARD BOLT FOUND CORRODED AND RUBBING SCARS ON SHANK. 2 L 7 3 4F RT A22WE 2002080800052 20020808 00052 NM 2002 8 8 02FDEA00477 1 20020706 A 1430 BOLT DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 LEFT WING INBOARD T/E FLAP OUTBOARD HINGE LWR INBOARD BOLT FOUND CORRODED AND RUBBING SCARS ON SHANK. 2 L 7 3 4F RT A22WE 2002080800053 20020808 00053 NM 2002 8 8 02FDEA00479 1 20020706 A 5720 SHIM DOUG MD11 MD11 3023602 NM RT WING OUT OF POSITION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 RIGHT WING FWD OF INBOARD FLAP OUTBOARD HINGE LWR OUTBOARD MOUNTING FOUND SUPPORT FITTING MOUNTING SHIM MIGRATED. LOCAT ED AT REAR SPAR BETWEEN POS XORS 298.5 TO 316.9. 2 L 7 3 4F RT A22WE 2002080800054 20020808 00054 NM 2002 8 8 02FDEA00480 1 20020709 A 5530 STRINGER BOEING 727 727200 138407E NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CRACKED STRINGER AT VERTICAL FIN STA 20, STR LT RIB NR 2. REPAIRED STR 4 LT AT VERTICAL FIN STA 20, RIB NR 2 IAW SRM 55 -30-4 FIG 1. REPAIRED STR 4 LT AT VERTICAL FIN STA 20, RIB NR 2 IAW SRM 55-30-4 FIG 1. 2 L 7 3 4F RT A3WE 2002080800055 20020808 00055 NM 2002 8 8 02FDEA00481 1 20020709 A 5530 STRINGER BOEING 727 727200 138407E NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CRACKED STRINGER AT VERT FIN STRINGER 8 AT RIB NR 2 RT. REMOVED AND REPLACED STRINGER PER SRM 55-30-4 FIG 1. 2 L 7 3 4F RT A3WE 2002080800056 20020808 00056 EU 2002 8 8 02FDEA00482 1 20020708 A 5720 STRUCTURE AIRBUS 310 A310 EU RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 NR 2 RT PYLON AFT FAIRING UPPER SIDE HYDRAULIC LINES HOLE ELONGATED ON THE FAIRING SIDE. REMOVED AND REPLACED HYD LINE HOLES PER EA 6-5710-64292. 2 L 7 2 4F RT A35EU 2002080800057 20020808 00057 EU 2002 8 8 02FDEA00483 1 20020708 A 5420 STRUCTURE AIRBUS 310 A310 EU LT PYLON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 LT PYLON AFT BRACKET WHERE HYD LINES PASSES THROUGH FROM WING TO PYLON FOUND HOLES ELONGATED. REMOVED AND REPLACED HOLE S PER IAW EA 26-5210-64291. 2 L 7 2 4F RT A35EU 2002080800058 20020808 00058 NM 2002 8 8 02FDEA00486 1 20020711 A 2930 SWITCH BOEING 727 727200 138407E NM HYD SYSTEM FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 463FE 22551 HYD A-SYSTEM OVERHEAT LIGHT ILLUMINATED ON TAXI OUT. RAN THE CHECKLIST AND LIGHT EXTINGUISHED. TALKED WITH MX T/O. DU RING CLIMBOUT HYD A-SYSTEM OVERHEAT LIGHT RE-ILLUMINATED. RAN THE CHECKLIST AND RETURNED TO MEM. REMOVED AND REPLACED NR 1 & NR 2 ENG HYD CASE DRAIN FILTER, OLD FILTERS WERE CLEAN. REMOVED AND REPLACED OVERHEAT SWITCH, RAN ENGINES LIGHT DID NOT COME ON. ALL WORK WAS DONE USING A STANDARD MAINTENANCE PRACTICE. 2 L 7 3 4F RT A3WE 2002080800059 20020808 00059 NM 2002 8 8 02FDEA00487 1 20020712 A 2424 GCU BOEING 727 727200 138407E NM NR 3 MALFUNCTIONED A FDEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 25 483FE 21465 NR 3 GENERATOR BREAKER TRIPPED. RESET IAW CHECK LIST. RETRIPPED AFTER APPROXIMATELY 1 MINUTE. NR 2 FIELD AND NR 2 GE NERATOR TRIPPED. ACCOMPLISHED CHECK LIST PROCEDURES. UNDER VOLTAGE INDICATED ON NR 2. REMOVED AND REPLACED NR 3 GENE RATOR CONTROL UNIT IAW SMP. RAN ENGINE NR 3 PER 727 JRH. OP'S CHECK GOOD IAW MM 24-22-000-2. REMOVED AND REPLACED NR 2 GENERATOR CONTROL UNIT IAW SMP. RAN ENGINE IAW 727. OP'S CHECK GOOD IAW 24-22-000-2. 2 L 7 3 4F RT A3WE 2002080800060 20020808 00060 NM 2002 8 8 02FDEA00488 1 20020712 A 2120 ODOR BOEING 727 727100 1384036 NM COCKPIT DETECTED A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 116FE 19298 WHEN POWER LEVER WAS PULLED TO IDLE,THERE WAS AN ACRID SMELL IN THE COCKPIT. ODOR SMELLS LIKE AN OVERHEATED ELECTRIC MO TOR. SMELL OCCURRED WITH GASPER FAN ON OR OFF. RAN ALL ENGINES WITH PACKS ON AND GASPER ON & OFF, NO ODORS DETECTED AN D NO BURNING NOTED. ALSO INSPECTED ALL E&E, NO SMELLS FOUND. AIRCRAFT OK TO CONTINUE. 2 L 7 3 4F RT A3WE 2002080800061 20020808 00061 WP 2002 8 8 02FDEA00489LA 1 20020714 A 2740 SK14869120 CHAIN DOUG DC10 DC1010 3022110 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 FOUND HAIRLINE CRACK ON CHAIN LINK SLEEVE OF HORIZONTAL STAB LOWER LT CHAIN. REMOVED AND REPLACED LT LOWER CHAIN MASTER LINK, SECURED, NEEDS REPOSITION & TENSION. REMOVED AND REPLACED UPPER AND LOWER LT CHAINS FOR LT ACME SCREW PER MM 27- 44-02-2-1. 2 L 7 3 4F A22WE 2002080800062 20020808 00062 NM 2002 8 8 02FDEA00490 1 20020712 A 2497 WIRE BOEING 727 727200 138407E NM NR 3 ENGINE CHAFED A FDEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 25 483FE 21465 REPEAT WRITE UP. NR 3 GENERATOR BREAKER TRIPPED, ACCOMPLISHED CHECKLIST PROCEDURES. RESET GENERATOR AND IT RE-TRIPPE D AFTER 1 MINUTE. REMOVED AND REPLACED NR 3 ENG DRIVEN GENERATOR IAW 727 MM 24-20-001-4. FOUND FIELD EXCITATION WIRE ( F) CHAFED THROUGH WIRE INSULATION ON GENERATOR BRACKET. REPAIRED WIRE AND REPOSITIONED TO PREVENT FUTURE CHAFING IAW ST ANDARD WIRING PRACTICES. REMOVED AND REPLACED NR 3 ENG GENERATOR CONTROL UNIT IAW 727 MM 24-22-000-2. OP'S CHECK FOUND WHEN A LOAD WAS PUT ON GENERATOR THE BUS TIE BREAKER WOULD TRIP. REMOVED AND REPLACED NR 3 BUS TIE BREAKER IAW 727 MM 24-20-041-4. RAN ENG AND OP'S CK'D PER 727 JRH. OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2002080800063 20020808 00063 NM 2002 8 8 02FDEA00491 1 20020712 A 5753 ARC2762502 BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 RIGHT WING INBOARD FLAP, INBOARD FLAP TRACK BRACKET ASSY TRACK & DRIVE SUPPORT FOUND CRACKED. REMOVED AND REPLACED FLAP ASSY PER MM 27-50-20. 2 L 7 3 4F RT A22WE 2002080800064 20020808 00064 WP 2002 8 8 02FDEA00494 1 20020716 A 1430 STUD DOUG DC10 DC1030 3023501 WP T/E FLAP SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 STUD SHEARED AT RIGHT O/B FLAP O/B FWD HINGE HALF AT AFT SPAR ATTACHMENT LWR O/B ATTACH POINT. REMOVED AND REPLACED ALL 4 STUDS AT AFT SPAR IAW 57-41-01-2. 2 L 7 3 4F A22WE 2002080800065 20020808 00065 NM 2002 8 8 02FDEA00495 1 20020716 A 2710 WARNING LIGHT DOUG MD11 MD11 3023602 NM COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 586FE 48487 LEVEL 2 -AIL DEFECT DISAG- ALERT ILLUMINATED DURING FLAP/SLAT RETRACTION ON T/O. RECYCLED FLAPS IAW QRH. ALERT EXTINGU ISHED MOMENTARY THEN REAPPEARED AFTER FLAP/SLAT RETRACTION. 2 L 7 3 4F RT A22WE 2002080800066 20020808 00066 NM 2002 8 8 02FDEA00496 1 20020717 A 3610 24098400 SLEEVE BOEING 727 727200 138407E NM A/C BAY DETERIORATED A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 281FE 22348 LOWER AFT BODY OVERHEAT LIGHT CAME ON 30 MIN INTO FLIGHT. COMPLIED WITH QRH & SECURED RIGHT PACK NR 3 ENG BLEED. LIGHT STAYED ON IAW QRH, MOVED NR 3 THROTTLE TO IDLE, AND OVERHEAT LIGHT IMMEDIATELY WENT OUT. QRH INDICATES LEAK IS BETWEEN NR 3 BLEED VALVE AND R/PACK VALVE. INSP DUCTING AND CHECKED CLAMPS. RAN ENG PER JRH & OPS CKD. NO FAULT OCCURRED. F OUND SLEEVES ON DUCTING TO S/O VALVE DETERIORATED. REMOVED AND REPLACED SLEEVES ON RT PACK SHUTOFF VALVE PER M/M 21-55- 031-4. RAN NR 3 ENGINE PER JRH TO POWER, NO LEAKS OR FAULTS NOTED. 2 L 7 3 4F RT A3WE 2002080800067 20020808 00067 NM 2002 8 8 PCAA0208086 1 20020807 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM #1 CARGO BAY FALSE ACTIVATION A PCAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 13 810EX 8126 308 MDT-PHL FLIGHT#3734. CREW REPORTED BAG BAY SMOKE DETECTOR ILLUMINTAED INTERMITTANTLY IN FLIGHT. EMERGENCY WAS DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND #1 SMOKE DETECTOR AT FAULT. #1 SMOKE DETECTOR REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL CHAPTER 26-12-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080800068 20020808 00068 GL 2002 8 8 AUS20020622 3 20020624 A 6111 BLADE CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MCAULY 3AF32C 3AF32C505 GL PROPELLER CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) PROPELLER BLADES CORRODED IN AREA OF BLADE SHANK RADIUS. 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 2002080800071 20020808 00071 NM 2002 8 8 AUS20020626 1 20020627 A 2913 6506606 PUMP BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL HYDRAULIC SYS CONTAMINATED W O OTHER J WARNING INDICATION DE DESCENT 1 AU S 32409 (AUS) LT ENGINE DRIVEN HYDRAULIC PUMP CONTAMINATED WITH METAL. 2 L 7 2 4F 4 F RT A1NM E23EA 2002080800072 20020808 00072 SW 2002 8 8 AUS20020630 1 20020621 A 6220 412010187101 BEARING BELL 412 412 1182202 SW PWA PT6T PT6T3 52045 EA MAIN ROTOR HEAD DELAMINATED W O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 AU S (AUS) MAIN ROTOR BLADE INBOARD ELASTOMERIC BEARING DELAMINATED. 1 G 7 2 4U 4 U H4SW E22EA 2002080800074 20020808 00074 NM 2002 8 8 02FDEA00497 1 20020716 A 3510 OXYGEN BOTTLE BOEING 727 727200 138407E NM OXYGEN SYS FAULTY A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 465FE 21289 THIRTY MINUTES INTO FLIGHT AT FL 350 OXYGEN QTY INDICATES ZERO. ALL OXYGEN REGULATORS WERE IN EMERGENCY-OFF POSITION. PERFORMED LEAK CHECK OF OXYGEN LINES IN E&E BAY, NO LEAKS. CHECKED ALL MASKS AT REGULATORS IN COCKPIT, CHECK OK. REPLA CED BOTH OXYGEN BOTTLES, O2 PRESSURE 1900 PSI. PERFORMED LEAK CHECK. NO LOSS OF PRESSURE. OK TO CONTINUE. 2 L 7 3 4F RT A3WE 2002080800075 20020808 00075 NM 2002 8 8 02FDEA00500 1 20020718 A 3610 CLAMP BOEING 727 727200 138407E NM BLEED AIR BROKEN A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 25 282FE 22349 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING CRUISE AT FL 310, 20 MINUTES AFTER TAKEOFF. ACCOMPLISHED CHECK LIST PR OCEDURES AND LIGHT EXTINGUISHED IAW CHECK LIST LEAK WAS BETWEEN BLEED VALVE AND PACK VALVE. REPLACED BROKEN SUPPORT CLA MP SET BLEED DUCT ON RT SIDE OF AFT STAIR, CARRIED OUT GROUND LEAK CHECK AND CHECKED CONDITIONS OF SENSE LINE NORMAL TES T PER MM 26-14-000-5, FOUND NORMAL. 2 L 7 3 4F RT A3WE 2002080800076 20020808 00076 SW 2002 8 8 AUS20020634 1 20020528 A 7334 42D218 PRESSURE SWITCH BELL 412 412 1182202 SW PWA PT6T PT6T3 52045 EA FUEL SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) FUEL PRESSURE SWITCH LEAKING FROM SOLDER JOINT. SUSPECT CAUSED BY INTERNAL FAILURE OF METAL DIAPHRAGM. 1 G 7 2 4U 4 U H4SW E22EA 2002080800077 20020808 00077 NM 2002 8 8 HNAA0200049 1 20020622 A 7920 LINE DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE LEAKING A HNAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 07 925HA 111 NR 2 ENGINE OIL PRESSURE FLUX AND WARNING LIGHT ILLUMINATED, SHUT DOWN ENGINE QT 45 PSI, FOUND HOT SECTION SOAKED. CLEA NED AND SERVICED ENGINE. NR 2 ENGINE LT NACELLE OIL COOLING LINE REMOVED AND REPLACED O-RINGS. RUN-UP AND LEAK CHECK G OOD. 2 H 7 2 4T RT A13NM 2002080800078 20020808 00078 CE 2002 8 8 071602 1 20020616 A 3010 12838405455 RELAY BEECH MU300 400A 1155402 CE DE-ICE SYS FAILED E DJFA K NONE J WARNING INDICATION CR CRUISE 1 EA 23 435CW RK35 TAIL DE-ICE INOP. 2 H 7 2 4F RT A16SW 2002080800079 20020808 00079 NM 2002 8 8 DHL2002753005 1 20020806 A 3200 H1010153 DOWNLOCK SWITCH BOEING 727 727223 1384074 NM A DHLA L O ABORTED APPROACH OTHER J WARNING INDICATION AP APPROACH 1 SO 01 753DH 22468 1) ON FINAL GREEN GEAR LITES EXTINGUISHED, RED GEAR LITE ILLUMINATED . ACCOMPLISHED ABNORMAL PROCEDURES . VIEWING POR T INDICATED N.G. DOWN & LOCKED. ON 2ND APPROACH , RED N.G. LITE EXTINGUISHED & GREEN N.G. LITE ILLUMINATED. ON GROUND WH EN TOW BAR WAS ATTACHED, RED NOSE GEAR LITE ILLUMINATED , GREEN LITE EXTINGUISHED . GEAR HORN SOUNDED. GEAR PINS REMOVE D FROM POUCH & INSTALLED. 2) R&R NOSE GEAR DOWNLOCK SENSOR WITH SERVICEABLE SENSOR. OPS CHECK GOOD IAW MM 32-61-71, GEA R PINS REMOVED AND STOWED IAW BMM CH 32-00-11. 2 L 7 3 4F A3WE 2002080800081 20020808 00081 NM 2002 8 8 02FDEA00501 1 20020719 A 3610 CLAMP BOEING 727 727200 138407E NM BLEED AIR LOOSE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 25 281FE 22348 LOWER AFT BODY OVERHEAT LIGHT CAME ON 30 MIN INTO FLIGHT. WHILE RUNNING THE QRH AND WITH BOTH PACKS NR 1 AND NR 3 BLEED S ON, THROTTLE WAS MOVED TO IDLE. OVERHEAT LIGHT THEN EXTINGUISHED. REPEAT WRITEUP. RETURNED TO NORMAL CONFIGURATION WITH NO REPEAT OCCURRENCE. INSPECTED OVERHEAT DETECTOR AND AIR LINES ON RT SIDE OF AIRSTAIRS FOUND LOOP TO BE INTACT AN D FOUND CLAMPS LOOSE ON PURGE VALVE FOR THE PRECOOLER AND CLAMPS LOOSE ON THE PRECOOLER. TIGHTENED CLAMPS AND LEAKED CH ECKED. FOUND NO LEAKS. RAN ENG NR 1 & NR 3 PER JRH TO TAKEOFF POWER AND LIGHT DID NOT COME ON WITH AIRSTAIRS DOWN OR I N THE UP POSITION. OKAY FOR SERVICE. 2 L 7 3 4F RT A3WE 2002080800082 20020808 00082 NM 2002 8 8 02FDEA00504 1 20020720 A 2613 OVERHEAT LOOP BOEING 727 727200 138407E NM FUSELAGE KEEL OUT OF POSITION A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING DE DESCENT 1 SO 25 281FE 22348 ON 2ND FLIGHT APPROACHING DESCENT INTO KMEM, LOWER AFT BODY OVERHEAT LIGHT CAME ON. FOLLOWED QRH AND ISOLATED RIGHT PAC K AND RIGHT BLEED (NR 3) ALONE W/ THE CARGO HEAT OUTFLOW. FINDING SAME AS REPEAT WRITE-UP. SYSTEM TEST GOOD, ALL C/BS CHECK GOOD. BEGAN TROUBLESHOOTING AS PER 727-200 AMM 26-14-000-1. INSPECTED ALL DUCTS WHILE PRESSURIZED, FOUND NO LEAK S. FOUND DETECT LOOP ALMOST TOUCHING A DUCT IN KEELBEAM AREA. PER M/M, NO LOOP IS TO BE LOCATED CLOSER THAN 2 INCHES T O DUCT. REALIGNED LOOP ACCORDINGLY. CLOSED ACCESS PANELS. USED TEMPERATURE SENSING LASER GUN TO SCAN AFT CARGO BELLY. NO UNUSAL TEMPS DISCOVERED. SUSPECT KEELBEAM LOOP AT FAULT. 2 L 7 3 4F RT A3WE 2002080800083 20020808 00083 NM 2002 8 8 02FDEA00505 1 20020720 A 2130 WARNING HORN BOEING 727 727200 138407E NM COCKPIT ACTIVATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 496FE 21670 ON INITIAL CLIMBOUT FROM COS THE ALTITUDE WARNING HORN CAME ON PASSING APPROX 12,500 FT MSL. A CHECK OF THE CABIN PRESS URE GAUGE SHOWED CABIN ALTITUDE IN EXCESS OF 10,000 FT MSL WITH THE CABIN STILL CLIMBING. DESCENDED BACK TO 10,000 FT MSL AND RAN THE PROC FROM THE QRH BOOK WITH NO CHANGE. THE OUTFLOW VALVE WAS FULL CLOSED THE ENTIRE TIME, HAD CONTROL O F THE VALVE IN ALL POSITIONS OF THE AUTOMATIC CONTROLLER. RETURNED TO COS. 2 L 7 3 4F RT A3WE 2002082200073 20020822 00073 WP 2002 8 22 02FDEA00506 1 20020718 A 5753 HINGE DOUG DC10 DC1030 3023501 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 PLI STACK LOOSE AND RUST EMITTING FROM RIGHT O/B FLAP I/B FWD HINGE AT AFT SPAR ATTACHMENT, O/B LWR STUD. REMOVED AND R EPLACED HINGE & FLAP ASSY PER MM 27-50-00. 2 L 7 3 4F A22WE 2002080800084 20020808 00084 NM 2002 8 8 02FDEA00507 1 20020722 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 CORROSION SKIN BULGE AT BS 1075, STRINGER R28. REMOVED AND REPLACED STRINGER PER SRM 53-10-1, 53-10-3. 2 L 7 3 4F RT A3WE 2002080800085 20020808 00085 NM 2002 8 8 02FDEA00508 1 20020720 A 5310 SHEAR TIE BOEING 727 727100 1384036 NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 151FE 19147 SHEAR TIE GOUGED AT BS 540, JUST BELOW STR 14R. REPAIRED SHEAR TIE BS 540 BELOW STR 14R IAW SRM 53-10-4, 53-10-2. 2 L 7 3 4F RT A3WE 2002080800086 20020808 00086 NE 2002 8 8 02FDEA00523 2 20020726 A 7200 ENGINE BOEING 727 727100 1384036 NM PWA JT8 JT8D7 52053 NE NR 3 MALFUNCTIONED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 25 124FE 19360 657211 NR 3 ENGINE OIL TEMPERATURE WENT INTO YELLOW BAND APPROX 10 MINUTES AFTER T/O. STARTED 15 MINUTE TIMING & COMPLIED WITH RED TABS. WHEN THRUST LEVER WAS RETARDED TOWARDS IDLE, OIL TEMP WENT INTO RED BAND. RED TABS DIRECTED AND ENGINE SHUT DOWN. AFTER SHUTDOWN, ENGINE OIL TEMP WENT TO APPROX 170 DEGREES. AFTER APPROX 10 MINUTES THE TEMPERATURE DECREASED IN TO THE YELLOW BAND. AFTER ENGINE SHUTDOWN, PEAK TEMP EXCEEDED RED BAND TO APPROX 170 DEGREES. REMOVED AND REPLACED NR 3 ENG PER W/C'S 70T0501-03. 2 L 7 3 4F 4 F RT A3WE E2EA 2002082200077 20020822 00077 NM 2002 8 22 02FDEA00524 1 20020729 A 3210 BLOCK DOUG MD11 MD11F 3023600 NM LANDING GEAR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 616FE 48747 CENTER LANDING GEAR LT PILLOW BLOCK FOUND CORRODED. REMOVED AND REPLACED PILLOW BLOCK PER CMM 32-15-01. 2 L 7 3 4F RT A22WE 2002082200080 20020822 00080 NM 2002 8 22 02FDEA00525 1 20020729 A 3210 BLOCK DOUG MD11 MD11F 3023600 NM LANDING GEAR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 616FE 48747 CENTER LANDING GEAR RIGHT PILLOW BLOCK FOUND CORRODED. REMOVED AND REPLACED CTR LANDING GEAR PER CMM 32-1501. 2 L 7 3 4F RT A22WE 2002080800087 20020808 00087 NM 2002 8 8 02FDEA00526 1 20020728 A 2710 PUSHROD DOUG MD11 MD11 3023602 NM AILERON DEFECTIVE A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 592FE 48550 LEVEL 2 -AILERON DEFLECT DISAGREE- DURING FLAP RETRACTION AT 3300 FT. PERFORMED QRH PROCEDURES. THE LEFT AILERON REMAI NED DEFLECTED AFTER FLAP RETRACTION. A/C ROLLS RIGHT. RELEASED FOR SERVICE PER MEL/CDL. INSTALLED FIXED PUSH-ROD IN L EFT OUTBOARD DEFLECT AILERON. 2 L 7 3 4F RT A22WE 2002080800088 20020808 00088 2002 8 8 02FDEA00527 4 20020727 A 2230 MODULE DOUG MD11 MD11 3023602 NM AUTOTHROTTLE SYS MALFUNCTIONED A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 582FE 48420 DURING CRUISE AT FL330, SMOKE BEGAN POURING FROM THROTTLE QUADRANT. DISCONNECTED AUTOTHROTTLES, AUTOPILOT & SMOKE QUICK LY DISSIPATED. EMERGENCY DECLARED AND REQUESTED PRIORITY HANDLING TO STANSTED UK. PER CREW DEBRIEF SMOKE DISAPPEARED S IMULTANEOUSLY WITH MANUAL DISCONNECTION OF AUTOTHROTTLES. PERFORMED FCC-1 THRUST CONTROL MODULE RTS TEST PER MM 22-00- 00-5. TEST FAILED FOR A/T SERVO WITH NO THROTTLE MOVEMENT DURING TEST. PERFORMED FCC-2 THRUST CONTROL MODULE RTS TEST PER MM 22-00-00-5 & ALL TESTS PASSED. SUSPECT NR 1 A/T SERVO FAILURE WITHIN THE TCM WAS CAUSE OF SMOKE. REQUIRES REPL ACEMENT OF THE THRUST CONTROL MODULE. 2 L 7 3 4F RT A22WE 2002082200083 20020822 00083 NM 2002 8 22 02FDEA00528 1 20020725 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 CORROSION ON FLOORBEAM AT NUT CLIP LOCATION BS 950F LBL 10.5 WL 208. REMOVED AND REPLACED FLOORBEAM AT BS 950F, LBL 1 0.5, WL 208 PER SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 2002080800089 20020808 00089 WP 2002 8 8 02FDEA00529 1 20020729 A 5753 ARAC2217407 FITTING DOUG DC10 DC1030 3023501 WP T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 FOUND DURING B-CHECK R/OUTBD FLAP CARRIAGE SUPPORT FITTING CRACKED APPROX 80 PERCENT OF FITTING. THIS IS SECOND CRACK F OUND IN THIS AREA. 2 L 7 3 4F A22WE 2002080800090 20020808 00090 EU 2002 8 8 02FDEA00530 1 20020729 A 5410 FITTING AIRBUS 310 A310222 3930315 EU RT PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 RIGHT PYLON THRUST AND SIDE LOAD FITTING FOUND BROWN STAIN ON TOP AND BOTTOM AREA. 2 L 7 2 4F RT A35EU 2002091200072 20020912 00072 EU 2002 9 12 02FDEA00531 1 20020729 A 5420 FITTING AIRBUS 310 A310 EU LT PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 LT WING PYLON THRUST & SIDE LOAD FITTING OUTBD TOP CORNER OF FITTING FOUND CHAFING. 2 L 7 2 4F RT A35EU 2002082200086 20020822 00086 NM 2002 8 22 02FDEA00532 1 20020730 A 5532 PANEL BOEING 727 727200 138407E NM VERTICAL STAB MISSING A FDEA O OTHER D INFLIGHT SEPARATION UK UNKNOWN 1 SO 25 242FE 21178 ON POST FLIGHT INSPECTION FOUND SLIDE PANEL ON RIGHT SIDE OF VERTICAL STAB MISSING. FOUND HINGE ASSY TORN & BROKEN. RE MOVED REMAINDER OF HINGE ASSY. ALSO NOTED FORWARD SLIDER TRACK HAS SECTION TORN OUT AND AFT TRACK WAS BENT. NOTED AFT HONEY COMB PANEL A DEEP SCRATCH EXPOSING SOME OF ITS HONEY COMB. REMOVED TRACKS AND PLATE ASSY. REPLACED ASSY, PERFORM ED OPERATIONAL CHECK IAW MM 27-40-000-5 AND 55-10-061-4. 2 L 7 3 4F RT A3WE 2002080800091 20020808 00091 EU 2002 8 8 02FDEA00534 1 20020730 A 2750 GEARBOX AIRBUS 310 A310222 3930315 EU T/E FLAP LACK OF LUBE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 LEFT WING FLAP SYS RT ANGLE GEARBOX FOUND NO OIL IN GEARBOX. R & R LT WING FLAP SYS RT ANGLE GEARBOX PER MM 27-54-13. RE F N00509 FOR FLAP SYS ADJ. 2 L 7 2 4F RT A35EU 2002082200088 20020822 00088 EU 2002 8 22 02FDEA00535 1 20020731 A 5530 A5557210100000 PIN AIRBUS 310 A310222 3930315 EU VERTICAL STAB ROTATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 VERTICAL STABILIZER TO FUSELAGE ATTACHMENT TAPERED PIN & SLEEVE ASSEMBLIES RED INDICATOR MARKS SHOW PIN ROTATION AT ALL SIX LOCATIONS. REMOVED AND REPLACED PINS PER AMM 55-30-11 & EA 6-5530-64304. 2 L 7 2 4F RT A35EU 2002082200090 20020822 00090 EU 2002 8 22 02FDEA00537 1 20020801 A 2730 CONTROL CABLE AIRBUS 310 A310222 3930315 EU ELEVATOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 CAPT SIDE & COPILOT SIDE ELEVATOR CONTROL CABLES CORRODED AT PULLEYS IN STAB COMPARTMENT. REMOVED AND REPLACED CABLES PER AMM 27-30-00-4. 2 L 7 2 4F RT A35EU 2002082200092 20020822 00092 EU 2002 8 22 02FDEA00538 1 20020801 A 2742 ACTUATOR AIRBUS 310 A310222 3930315 EU HORIZ STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 THS ACTUATOR LWR CLAW STOP RUBBER BUFFER BETWEEN INNER & OUTER RACE SHOWS AXIAL MIGRATION OF 5 MM. THS ACTUATOR SCREW THREAD HAS SCRATCH MARK ON UPPER FACE 27.5 CM ABOVE LWR CLAW STOP. REMOVED AND REPLACED ACTUATOR PER AMM 27-44-11-4. 2 L 7 2 4F RT A35EU 2002082200093 20020822 00093 NM 2002 8 22 02FDEA00539 1 20020731 A 5311 FRAME BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 CORROSION ON FRAME AT BS 680 STR 25R. REMOVED AND REPLACED FRAME PER EA 7-5310-65004 & SRM 53-10-9 FIG 11. 2 L 7 3 4F A3WE 2002082200095 20020822 00095 NM 2002 8 22 02FDEA00540 1 20020726 A 5320 STRINGER CLIP BOEING 727 72722 1384002 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 INTERIOR CABIN HAS CRACKED STR CLIP AT BS 680 STR 4L. REMOVED AND REPLACED CLIP PER SRM 51-30-2. 2 L 7 3 4F A3WE 2002082200099 20020822 00099 NM 2002 8 22 02FDEA00542 1 20020726 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 CORROSION ON FLOORBEAM AROUND 2 FASTENER HOLES BS 480 RBL 10 WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 2002080800092 20020808 00092 NM 2002 8 8 02FDEA00543 1 20020803 A 3234 SOLENOID BOEING 727 727200 138407E NM COCKPIT FAULTY A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 478FE 21395 AFTER LIFTOFF LANDING GEAR HANDLE WOULD NOT RAISE ABOVE THE OFF POSITION. CREW WENT THROUGH APPROPRIATE RED TABS. COUL D NOT FIX PROBLEM. RETURNED TO DEPARTURE AIRPORT. REPLACED L/G CONTL LEVER LOCK SOLENOID PER 727 MM 32-31-016-4. CYCL ED GEAR SEVERAL TIMES, OP'S CHECKS OK. 2 L 7 3 4F RT A3WE 2002080800093 20020808 00093 NM 2002 8 8 02FDEA00545 1 20020805 A 2410 700842A CSD BOEING 727 727200 138407E NM NR 3 ENGINE FAILED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 223FE 20935 REPEAT WRITE-UP, DURING CLIMBOUT NR 2 CSD OVERHEATED TO 125C WITH NR 1 & 3 CSD'S IN LIMITS AT 110C & 118C IAW QRH. DIS CONNECTED NR 2 GEN FOR 3 MIN COOLING. AFTER 2 MIN NR 3 CSD OVERHEATED TO 121C WITH NR 1 CSD 115C IAW QRH. DISCONNECTED NR 3 GEN AND RETURNED TO LAND. REMOVED AND REPLACED NR 3 CSD PER M/M 24-10-011-4 AND NR 3 CSD OIL COOLER PER M-M 24-10 -062-4, RAN ENGINES PER JRH CK'D OK. 2 L 7 3 4F RT A3WE 2002082300064 20020823 00064 NM 2002 8 23 02FDEA00546 1 20020806 A 3260 PROXIMITY SWITCH BOEING 727 727200 138407E NM LT MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 275FE 22040 ON TAKEOFF RED LEFT GEAR LIGHT ON FWD INSTRUMENT PANEL REMAINS ILLUMINATED WITH GEAR HANDLE UP. CYCLED GEAR AS PER QRH AND REMAINED ILLUMINATED WITH GEAR HANDLE UP. REMOVED AND REPLACED LT MAIN GEAR UPLOCK PROX SWITCH PER 727 M/M 32-61-08 1-4. OPS CHECKED SENSOR PER M/M 32-61-081-4, OPS CKS GOOD. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2002080800094 20020808 00094 NM 2002 8 8 02FDEA00547 1 20020806 A 2410 CSD BOEING 727 727200 138407E NM NR 3 ENGINE OVERHEATED A FDEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 25 223FE 20935 NR 3 CSD OVERHEATED DURING CLIMBOUT, 121C WITH NR 1 CSD AT 115C AND NR 2 CSD DISCONNECTED. ELECTED TO RTB AND NOT REDUC E TO ONE GEN OPERATIONS. 2 L 7 3 4F RT A3WE 2002080800095 20020808 00095 NM 2002 8 8 02FDES00456 1 20020701 A 1430 BOLT DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 583FE 48421 LEFT WING INBOARD T/E FLAP LWR I/B HINGE BOLT CORRODED. 2 L 7 3 4F RT A22WE 2002080800096 20020808 00096 CE 2002 8 8 072202 1 20020712 A 2130 99141244 VALVE CESSNA 650 650 2076802 CE CABIN PRESSURE STICKS E DJFA K NONE O OTHER CL CLIMB 1 EA 23 385CW 6500145 EMERGENCY PRESSURIZATION VALVE WILL NOT OPEN UNTIL 95 PERCENT N1. FOUND VALVE TO BE STICKING. 2 L 7 2 4F A9NM 2002080800097 20020808 00097 EU 2002 8 8 02219306 1 20020207 A 3350 8545K15T33T SWITCH JETAIR JETSTM JETSTM4101 1500501 EU A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 306UE 41020 During taxi for take-off, the crew reported that the emergency exit lights had illuminated with both engines running and the cockpit control switch in the "armed" position. Maintenance personnel removed and replaced the emergency exit ligh ts cockpit control switch. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002080800098 20020808 00098 CE 2002 8 8 072212002 1 20020722 A 2150 99141142 VALVE CESSNA 650 650 2076802 CE LEFT MALFUNCTIONED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 385CW 6500145 TROUBLESHOT FOUND INSUFFICIENT PRESSURE AT OUTLET OF THE LEFT HAND FLOW CONTROL VALVE. 2 L 7 2 4F A9NM 2002080800099 20020808 00099 NE 2002 8 8 072222002 2 20020722 A 7532 99141252 BLEED VALVE CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7313B 01518 NE LT ENGINE MALFUNCTIONED E DJFA K NONE O OTHER UK UNKNOWN 1 EA 23 385CW 6500145 LEFT BLEED VALVE DOES NOT CLOSE WHEN SELECTED OFF. 2 L 7 2 4F 4 F A9NM E6WE 2002080800100 20020808 00100 CE 2002 8 8 072232002 1 20020722 A 2131 2298853 CONTROLLER CESSNA 650 650 2076802 CE CABIN PRESSURE FAILED E DJFA O OTHER O OTHER CR CRUISE 1 EA 23 385CW 6500145 CABIN PCA FAILS TO HOLD CABIN PRESSURE IN NORMAL OR HIGH POSITION IN FLIGHT. 2 L 7 2 4F A9NM 2002080800101 20020808 00101 CE 2002 8 8 072242002 1 20020722 A 3610 621456120 TEE FITTING CESSNA 650 650 2076802 CE BLEED AIR CRACKED E DJFA O OTHER O OTHER CR CRUISE 1 EA 23 385CW 7069 6500145 UNABLE TO MAINTAIN CABIN PRESSURIZATION IN SIGNAL SOURCE. REPLACED SEVERAL VALVES PARTIALLY CORRECTED PROBLEM FURTHER I NSPECTION REVEALED BLEED AIR T-FITTINGS ON RIGHT HAND PRECOOLER INBOARD AND OUTBOARD SIDES CRACKED. REPLACED BOTH T-FIT TINGS, PERFORMED OPERATIONAL CHECK FLIGHT AND FOUND SATISFACTORY. 2 L 7 2 4F A9NM 2002080800102 20020808 00102 WP 2002 8 8 200200249 1 20020507 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED B EIAA K NONE O OTHER UK UNKNOWN 1 WP 07 941F 47193 REPAIRED WINDOW BELT LOCATION STA 218-237 LT, PER PART 2 OF ECRA, FAA FORM 8110-3, DC9 SRM 53-04 FIG 34 AND FAA FORM 811 0-3. 2 L 7 2 4F A6WE 2002080800103 20020808 00103 WP 2002 8 8 200200267 1 20020716 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 941F 47193 REPAIRED WINDOW BELT LOCATION STA 351-370 LT PER PART 2 OF ECRA, FAA FORM 8110-3, DC9 SRM 53-04 FIG 34 AND FAA FORM 8110 -3. 2 L 7 2 4F A6WE 2002080800104 20020808 00104 WP 2002 8 8 200200268 1 20020716 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 941F 47193 REPAIRED WINDOW BELT LOCATION STA 522-541 LT PER PART 2 OF ECRA, FAA FORM 8110-3, DC9 SRM 53-04 FIG 34 AND FAA FORM 8110 -3. 2 L 7 2 4F A6WE 2002080800105 20020808 00105 WP 2002 8 8 200200269 1 20020716 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 941F 47193 REPAIRED WINDOW BELT LOCATION STA 756-775 LT PER PART 2 OF ECRA, FAA FORM 8110-3, DC9 SRM 53-04 FIG 34 AND FAA FORM 8110 -3. 2 L 7 2 4F A6WE 2002080800106 20020808 00106 WP 2002 8 8 200200270 1 20020716 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 941F 47193 REPAIRED WINDOW BELT LOCATIONS STA 851-870 LT PER PART 2 OF ECRA, FAA FORM 8110-3, DC9 SRM 53-04 FIG 34 AND FAA FORM 811 0-3. 2 L 7 2 4F A6WE 2002080800107 20020808 00107 WP 2002 8 8 200200271 1 20020716 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 941F 47193 REPAIRED WINDOW BELT LOCATION STA 370-389 RT PER PART 2 OF ECRA, FAA FORM 8110-3, DC9 SRM 53-04 FIG 34 AND FAA FORM 8110 -03. 2 L 7 2 4F A6WE 2002080800108 20020808 00108 WP 2002 8 8 200200272 1 20020716 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 941F 47193 REPAIRED WINDOW BELT LOCATION STA 270-256 RT PER PART 2 OF ECRA, FAA FORM 8110-3, DC9 SRM 53-04 FIG 34 AND FAA FORM 8110 -3. 2 L 7 2 4F A6WE 2002080800109 20020808 00109 WP 2002 8 8 200200273 1 20020805 A 5610 5912350U68 WINDOW FRAME DOUG DC9 DC981 3022081 WP COCKPIT CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 832F 48002 CORROSION FOUND ON FIRST OFFICERS LOWER WINDOW FRAME, ALSO CORROSION FOUND ON UPPER SURFACE OF CENTER COCKPIT WINDOW. R EMOVED AND REPLACED ZEE ANGLE ON SIDE WINDOW LOWER SILL PER DC9/MD80 SRM 51-60-0 AND 51-10-3, 51-10-4, 51-30-5, 51-20-0 . REMOVED AND REINSTALLED CENTER COCKPIT WINDOW AND REMOVED AND REPLACED FIRST OFFICERS WINDSHIELD PER MD-80 MM 56-10-0 1, 56-10-02. 2 L 7 2 4F A6WE 2002080800110 20020808 00110 EU 2002 8 8 2002F00759 1 20020711 A 5511 A331130A03B RIB DORNER DO228 DO228202 2992030 EU HORIZ STAB CRACKED B BIGA K NONE O OTHER IN INSP/MAINT 1 NM 04 263MC 9197 8141 CRACKS FOUND ON RIB NR 12 ON RIGHT SIDE AND RIB NR 13 ON LEFT SIDE. LT RIB CRACKED THROUGH 4 RIVETS HOLES ON TOP SKIN, LENGTH OF CRACK WAS 5 INCHES. RT RIB CRACKED THROUGH 1 RIVET HOLE, LENGTH OF CRACK WAS 2 INCHES. CRACKS WERE FOUND DUR ING COMPLIANCE WITH AD 2001-21-01 AND DORNIER SB228-234. 2 H 7 2 4T RT A16EU 2002080800111 20020808 00111 EU 2002 8 8 2002F00760 1 20020626 A 2910 AE2460201G0192 HYDRAULIC LINE ISRAEL 1124 1124 4500102 EU HYD SYSTEM BURST E A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 05 290CA 216 NR 2 ENGINE HYDRAULIC PUMP LINE BURST. 2 M 7 2 4F A2SW 2002080800112 20020808 00112 WP 2002 8 8 GTIA020697 1 20020603 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND CABIN FLOORBOARD STATION 200-256 LEFT FOUR BROKEN INSERTS AND CORE BROKEN. FABRICATED A NEW FLOORBOARD STAT ION 200-256, LEFT. (M) 2 L 7 2 4F A6WE 2002080800113 20020808 00113 WP 2002 8 8 GTIA020698 1 20020610 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND MID CARGO INTERCOSTAL STATION 541-560 LONGERON 29R CRACKED, TOOL MARKED AND CORROSION. FORMED NEW INTERCOST AL. INSTALLED INTERCOSTAL AT STATION 541-560 L29R IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 2002080800114 20020808 00114 WP 2002 8 8 GTIA020699 1 20020529 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND FLOOR PAN SUBFLOOR/WEB CORRODED AT STATION Y200, -X20 TO -X43, VIEWED FROM E/E BAY. REMOVED CORRODED WEB SE CTION. FABRICATED NEW WEB SECTION. INSTALLED NEW SUB FLOOR. (M) 2 L 7 2 4F A6WE 2002080800115 20020808 00115 WP 2002 8 8 GTIA020700 1 20020602 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND PAX CABIN HAS CORROSION AT SUPPORT FLOOR STATION 200 PLUS 55 INCHES. FLOOR SUPPORT IS OUT OF LIMITS. FABRI CATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002080800116 20020808 00116 WP 2002 8 8 GTIA020701 1 20020602 A 5320 ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND MID PIT HAS CORROSION BARE METAL AT RIGHT AFT Z-ANGLE. REMOVED Z-ANGLE AT MID PIT STATION 693 MATERIAL LOSS FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED Z-ANGLE. (M) 2 L 7 2 4F A6WE 2002080800117 20020808 00117 WP 2002 8 8 GTIA020702 1 20020602 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND MID PIT HAS CORROSION AT LONGERON 30 SPLICE AND RUSTED NUTS AND HI-LOCKS (20 EACH) STATION 598, 579, 560 AND STATION 617. LONGERON 39 IS OUT OF LIMITS STATION 549-588. FABRICATED LONGERON 30. INSTALLED LONGERON 30 FROM STATIO N 496 TO 589. (M) 2 L 7 2 4F A6WE 2002080800118 20020808 00118 WP 2002 8 8 GTIA020703 1 20020602 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND MID PIT CORROSION AT AFT FITTING SUPPORT CARGO STATION 693. REMOVED FITTING. FOUND THAT FITTING WAS CRACKE D. INSTALLED NEW FITTING. (M) 2 L 7 2 4F A6WE 2002080800119 20020808 00119 WP 2002 8 8 GTIA020704 1 20020616 A 5210 BRACKET DOUG DC9 DC981 3022081 WP L1 DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND L1 DOOR UPPER BRACKET CRACKED. REMOVED CRACKED BRACKETS. FABRICATED NR 2 BRACKET. INSTALLED TWO BRACKETS. (M) 2 L 7 2 4F A6WE 2002080800120 20020808 00120 WP 2002 8 8 GTIA020705 1 20020610 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND PAX CABIN CORRODED AT THE WEB STATION 180 PLUS X57 INCHES. CUT OUT DAMAGED WEB SECTION AND FABRICATED NEW W EB SECTION AND DOUBLER. INSTALLED WEB SECTION. (M) 2 L 7 2 4F A6WE 2002080800121 20020808 00121 WP 2002 8 8 GTIA020706 1 20020605 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND SUB FLOOR FROM STATION 218 TO 237 -X48 TO -X56 IS CRACKED. REMOVED CRACKED SUB FLOOR. FABRICATED NEW SUB F LOOR. INSTALLED SUB FLOOR. (M) 2 L 7 2 4F A6WE 2002080800122 20020808 00122 WP 2002 8 8 GTIA020707 1 20020605 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND SUB FLOOR FROM STATION 200 TO 218, -X23 TO -X56 IS CORRODED AND CRACKED. REMOVED CORRODED WEB SECTION. FAB RICATED NEW SUB FLOOR WEB. INSTALLED NEW SUB FLOOR. (M) 2 L 7 2 4F A6WE 2002080800123 20020808 00123 WP 2002 8 8 GTIA020708 1 20020602 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND PASSENGER CABIN HAS CORROSION AT RIGHT OUTBOARD SEAT TRACK STATION 237, STATION 200. FOUND SEAT TRACK OUT O F LIMITS. DRILLED NEW SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2002080800124 20020808 00124 WP 2002 8 8 GTIA020709 1 20020602 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND PASSENGER CABIN CORROSION AT RIGHT INBOARD SEAT TRACK -X23 STATION 237 STATION 200. MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK. LOCATED AND DRILLED NEW SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK AND SPLICE. (M) 2 L 7 2 4F A6WE 2002080800125 20020808 00125 WP 2002 8 8 GTIA020710 1 20020602 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - PASSENGER CABIN HAS CORROSION AT SUPPORT FLOOR STATION 218 PLUS X2 INCHES. FLOOR SUPPORT FOUND OUT OF LIMITS. RE MOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002080800126 20020808 00126 WP 2002 8 8 GTIA020711 1 20020602 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA O OTHER O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND PASSENGER CABIN CORRODED AT LEFT INBOARD SEAT TRACK STATION 207, 218, 229 PLUS X23 INCHES. SEAT TRACK CORRO DED OUT OF LIMITS. LOCATED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2002080800127 20020808 00127 WP 2002 8 8 GTIA020712 1 20020607 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND AFT PIT HAS CORROSION AT LONGERON 23L STATION 1338. REMOVED CORROSION FROM AREA. FOUND FITTING TO BE OUT O F LIMITS. DRILLED UP AND LOCATED NEW FITTING. INSTALLED NEW FITTING. (M) 2 L 7 2 4F A6WE 2002080800128 20020808 00128 WP 2002 8 8 GTIA020713 1 20020616 A 5320 STIFFENER DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND MID PIT FORWARD BULKHEAD, STATION 541 L29R, VERTICAL BULKHEAD POST IS CRACKED IN 2 PLACES AT LOWER FORWARD I N RADIUS. REMOVED BULKHEAD POST AT STATION 541 L29R. STOPPED DRILLED CRACKS. FABRICATED DOUBLERS TWO EACH. INSTALLED REPAIR DOUBLERS. INSTALLED BULKHEAD POST. (M) 2 L 7 2 4F A6WE 2002080800129 20020808 00129 WP 2002 8 8 GTIA020714 1 20020604 A 5320 BRACKET DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND AFT PIT CORRODED AT GANG CHANNEL LEFT ATTACH BRACKET END OF CARGO TRACK SIDE, AND TWO RUSTED NUTS. MATERIAL LOSS IS FOUND TO BE OUT OF LIMITS. INSTALLED ATTACHING FITTING. (M) 2 L 7 2 4F A6WE 2002080800130 20020808 00130 WP 2002 8 8 GTIA020715 1 20020614 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND END FITTING AT LONGERON 22L STATION 1338 WITH EXFOLIATION. FITTING BEYOND LIMITS. REMOVED FITTING. LOCATE D AND DRILLED NEW FITTING. INSTALLED NEW FITTING. (M) 2 L 7 2 4F A6WE 2002080800131 20020808 00131 2002 8 8 MEX2002187 4 20020612 A 2565 80330035 SLIDE BOEING 757 7572Q8 1384972 NM PAX DOOR OUT OF ADJUST A ASMF O OTHER J WARNING INDICATION IN INSP/MAINT 1 SW 23 805AM 26272 FLT 170 - MEX-TIJ - CAPTAIN REPORTED THAT THE DOOR NR 1 SLIDE WAS NOT ARMED. DURING CHECK WAS DETECTED THAT THE ARMED L IGHT WAS INOPERATIVE AND THE ACTIVATION MECHANISM WAS IN AN ABNORMAL POSITION. TECHNICAL PERSONNEL TRIED TO REMOVED THE DOOR COVER AND THE EMERGENCY BOTTLE WAS ACTIVATED. ARM/DISARM MECHANISM WAS MISADJUSTED AND THE ARMED INDICATOR PIN CO ULD NOTE BE OBSERVED. SLIDE AND BOTTLE WERE REPLACED AND DOOR AND ARM/DISARM SLIDE MECHANISM WERE ADJUSTED IAW MM 25-66 -00. (M) 2 L 7 2 4F RT A2NM 2002080800132 20020808 00132 2002 8 8 MEX2002189 4 20020614 A 3442 6225136003 ANTENNA DOUG DC9 DC983 3022083 WP RADAR FAILED A ASMF O OTHER J WARNING INDICATION CL CLIMB 1 SW 23 836AM 49397 FLT 248 - MEX-GDL - AIRCRAFT RETURNED TO FLIGHT AS A CONSEQUENCE OF RADAR FAIL. DURING CHECK WAS DETECTED A RADAR FAIL SIGNAL AND ANTENNA CONNECTOR WIRING DAMAGED. TX RX RADAR ANTENNA WAS REPLACED AND WIRING ON ANTENNA CONNECTOR, PINS H A ND G WERE REPAIRED IAW MM 34-41-01 AND 34-41-01 AND WDM 34-43-02 RESPECTIVELY. (M) 2 L 7 2 4F RT A6WE 2002080800133 20020808 00133 NM 2002 8 8 MEX2002215 1 20020709 A 3412 RELAY DOUG MD88 MD88 3023688 NM TAT SYSTEM DAMAGED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 168PL 53174 FLT 413 - MIA-MEX - AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF TAT/SAT FLAGS. AUTO-TEST WAS PERFORMED ALL OK, BU T WHEN PUSHING BACK STARTED, CAPTAIN REPORTED TAKEOFF TEST COULD NOT BE ACCOMPLISHED. DURING CHECK WAS DETECTED THE REL AY R2-5 DAMAGED. IT WAS CHANGED IAW MM 34-15-00. (M) 2 L 7 2 4F RT A6WE 2002080800134 20020808 00134 WP 2002 8 8 MWEA020421 1 20020610 A 2150 SEAL DOUG DC9 DC981 3022081 WP A/C BAY LEAKING A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 814ME 48010 CLIMBING THROUGH 8,000 FEET THE TAIL COMPARTMENT TEMPERATURE LIGHT CAME ON. THE LIGHT WENT OUT WITH THE QRH PROCEDURE, WITH THE LEFT PACK BEING TURNED OFF THE RIGHT PACK WOULDN'T HOLD CABIN ALT AND FLOW LIGHT WAS ON. INSPECTED DUCTING FOR LEAKAGE USING APU AND ENGINES AT IDLE, NO LEAKAGE FOUND. REMOVED LEFT AND RIGHT SENSORS FOR BENCH CHECK. FOUND LEFT H EAT EXCHANGER SEAL TO BE LEAKING. REPOSITIONED SEAL. FOUND LEFT ACM OUTLET FOUND LEFT ACM TURBINE OUTLET TO BE LEAKING . RESHIMMED LEFT ACM, RAN ENGINE AT HIGH POWER FOR EXTENDED PERIOD OF TIME WITH BOTH PACKS IN AUTO. NO TAIL COMPARTMEN T TEMPERATURE HIGH LIGHT CAME ON. REPLACED RIGHT AIR CONDITIONING FLOW CONTROL VALVE IAW AMM 21-31-3. 2 L 7 2 4F A6WE 2002080800135 20020808 00135 SO 2002 8 8 SIMA200216312 1 20020613 A 5320 14529150003 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 ABI - THIS IS A LEVEL 2 FINDING. PROFILE AT FRAME 23 CORRODED. REMOVED CORRODED PROFILE ANGLE AND INSTALLED SERVICEABL E PROFILE IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002080800136 20020808 00136 SO 2002 8 8 SIMA200216313 1 20020613 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 ABI - THIS IS A LEVEL 2 FINDING. LEFT GALLEY FLOOR SILL BETWEEN FRAMES 19 AND 23 CORRODED. DAMAGE WAS BLENDED OUT AND NDT WAS PERFORMED WITH NO DEFECTS FOUND ACCEPTED AS IS IAW EMB GST-1895/02. (M) 2 L 7 2 4T RT T00011AT 2002080800137 20020808 00137 SO 2002 8 8 SIMA200216314 1 20020613 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 ABI - THIS IS A LEVEL 2 FINDING, FORWARD DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE FORWARD DIAMOND GUS SET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002080800138 20020808 00138 SO 2002 8 8 SIMA200216315 1 20020613 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 ABI - THIS IS A LEVEL 2 FINDING, AFT DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002080800139 20020808 00139 SO 2002 8 8 SIMA200216316 1 20020613 A 5347 14530659011 SEAT TRACK EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 ABI - THIS IS A LEVEL 2 FINDING, LEFT FORWARD LOWER SEAT TRACK CORRODED. REMOVED AND INSTALLED SERVICEABLE LEFT FORWARD INBOARD SEAT TRACK IAW EMB 145 AMM 53-01-06. (M) 2 L 7 2 4T RT T00011AT 2002080800140 20020808 00140 SO 2002 8 8 SIMA200216901 1 20020618 A 5610 163500111 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT CRACKED A SIMA K NONE O OTHER CR CRUISE 1 SW 21 627AE 145121 ORD - FLT 4174 - DURNIG CRUISE, THE CREW REPORTED THAT THE CAPTAINS WINDSHIELD CRACKED. THE FLIGHT CREW ELECTED TO CONT INUE TO ORD. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW EMB 145 AMM 56-10-01. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002080800141 20020808 00141 SO 2002 8 8 SIMA200217305 1 20020617 A 5315 14521721007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - THIS IS A LEVEL 2 FINDING. AFT DIGITAL HAS CORROSION. PERFORMED NDT INSPECTION AND FOUND NO DEFECTS. DIGITAL FO UND TO BE WITHIN EMB 145 SRM 53-21-10 LIMITS. (M) 2 L 7 2 4T RT T00011AT 2002080800142 20020808 00142 SO 2002 8 8 SIMA200217306 1 20020617 A 5320 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - THIS IS A LEVEL 2 FINDING, RIGHT HAT BEAM IN GALLEY HAS CORROSION. REPAIRED HAT BEAM IAW ETN 53-036. (M) 2 L 7 2 4T RT T00011AT 2002080800143 20020808 00143 WP 2002 8 8 CALA0200436 1 20020807 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 228 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND R/H CENTER AND R/H I/B SEAT TRACKS CORRODED AT STA 228. THE CORRODED SEAT TRACK SECTIONS WERE REMOVED A ND NEW SECTIONS WERE SPLICED IN IAW SRM 53-05, FIGURE 4F AND 51-30-0. 2 L 7 2 4F A6WE 2002080800144 20020808 00144 NM 2002 8 8 QXEA0201112 1 20020802 A 2930 DSC252840230 FLEX LINE DHAV DHC8 DHC8202 2809007 NM ZONE 700 LEAKING A QXEA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 NM 09 360PH 515 PDX- HOLDING SHORT OF RUMWAY, STARTED LOOSING NO.2 HYDRAULIC QUANTITY. NO.2 ENGINE HYDRUALIC PRESSURE LIGHT CAME ON. SHU T DOWN ENGINES AND WAS TOWED BACK TO THE GATE. REMOVED AND REPLACED FLEX LINE BETWEEN NO.3 MAIN LANDING GEAR BRAKE FITTI NG AND MAIN LANDING GEAR HARD LINE SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002080800145 20020808 00145 NM 2002 8 8 AWXA200200699 1 20020802 A 5347 146N5281U6 SEAT TRACK BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 LCQ - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON INBOARD SEAT TRACK FLOOR SUPPORT AT BS 1300 TO 1320, LBL 2 4. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 1300 TO 1320, LBL 24; FABRICATED A NEW FLOOR SUPPORT, AND INSTALLED REPAIR IAW B757-200 SRM 51-40-02, PG. 4-5, & 11. 2 L 7 2 4F RT A2NM 2002080800146 20020808 00146 NM 2002 8 8 AWXA200200700 1 20020729 A 5350 149N7664 RIB BOEING 757 7572S7 1384962 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 0 0 23566 LCQ - MAJOR REPAIR - DURING C-08 CHECK A CRACK WAS FOUND AT L/H AFT WING TO BODY FAIRING SUPPORT RIB BS 1300. MAINTENANC E REMOVED CRACKED AREA OF SUPPORT RIB, FABRICATED 2 EACH REPAIR ANGLES, AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-6 0-71, PG. 201-204. 2 L 7 2 4F RT A2NM 2002080800147 20020808 00147 NM 2002 8 8 AWXA200200701 1 20020729 A 5315 BAC1520792 SEAT TRACK BOEING 757 7572S7 1384962 NM CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 0 0 23566 LCQ - MAJOR REPAIR - DURING C-08 CHECK SEVERAL CHAFE MARKS WERE FOUND ON SEAT TRACK AT BS 377-400, LBL 45. MAINTENANCE R EMOVED DAMAGED SECTION OF SEAT TRACK AT BS 377-400, LBL 45. FABRICATED A NEW SECTION OF SEAT TRACK AND INSTALLED REPAIR IAW B757-200 SRM 53-00-52, PG. 101, FIG. 101. 2 L 7 2 4F RT A2NM 2002080800148 20020808 00148 EU 2002 8 8 AWXA200200702 1 20020807 A 3350 E0242A28A0 RELAY AIRBUS 320 A320231 3930325 EU ZONE 120 INOPERATIVE A AWXA D RETURN TO BLOCK S O AFFECT SYSTEMS OTHER TX TAXI/GRND HDL 1 WP 28 633AW 0 0 082 PHX - EEL - FLT 0056 - ON TAXI OUT THE FLIGHT ATTENDANT REPORTED THE OVERHEAD WING AND DOOR EMERGENCY EXIT LIGHTS WERE N OT ILLUMINATED, AIRCRAFT RETURNED TO GATE. MAINTENANCE TROUBLESHOT AND REPLACED POWER SUPPLY CONTROL RELAY (8WL), OPERAT IONAL CHECK OF OVERHEAD WING AND DOOR EMERGENCY EXIT LIGHTS WAS GOOD. 2 L 7 2 4F RT A28NM 2002080800149 20020808 00149 NM 2002 8 8 AWXA200200703 1 20020729 A 5320 6546812169 FLOOR SUPPORT BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOOR SUPPORT BETWEEN BS 967 & BS 986.5, LBL 18. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 967 TO BS 986.5, LBL 18; FABRICATED A NEW FL OOR SUPPORT AND INSTALLED REPAIR IAW B737-300 SRM 51-40-05, PG. 4, AND SRM 51-40-02, PG. 3-4, & 10-11. 2 L 7 2 4F RT A16WE 2002080800150 20020808 00150 NM 2002 8 8 AWXA200200704 1 20020725 A 5320 65479573 WEB BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 0 0 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF THE AFT CARGO T HRESHOLD AT BS 794 TO BS 847, RBL 21 TO RBL 28. MAINTENANCE REMOVED AFT CARGO COMPARTMENT THRESHOLD WEB AT BS 794 TO BS 847, RBL 21 TO RBL 28. FABRICATED A NEW THRESHOLD WEB AND INSTALLED REPAIR IAW B737-300 SRM 51-10-02, PG. 15-16. 2 L 7 2 4F RT A16WE 2002080800151 20020808 00151 NM 2002 8 8 02080802 1 20020801 A 5315 BAC1518338 FLOORBEAM BOEING 757256 BOEING 757 757256 1384925 NM FUSELAGE CORRODED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 508NA 21797 26244 26244 CORROSION ON FLOORBEAM AT BS 1640, RBL 52, WL 208. FLOORBEAM UPPER TEE FOUND TO BE OUT OF LIMITS AT RBL 52 PER SRM 53-00 -51. FLOORBEAM REPAIRED PER SRM 53-00-51 FIG. 205, 53-00-51 PG 216, AND SRM 51-20-01. (STANDARD STRAP, ANGLE, ANF FILLER REPAIR.). AIRCRAFT RETURNED TO SERVICE AT COMPLETION OF C-CHECK 2 L 7 2 4F RT A2NM 2002080800152 20020808 00152 NM 2002 8 8 02080101 1 20020801 A 3350 LAMP BOEING 757 757236 1384971 NM MAIN CABIN BURNED OUT A N8TA K NONE G MULTIPLE FAILURE IN INSP/MAINT 1 WP 19 544NA 29942 Emergency Escape Path Lighting INOP at multiple rows. Upon further investigation, lamps found to be burned out. Relamped and Operationally checked, as per M/M 33-51-10; Ops ck good. Aircraft returned to service. 2 L 7 2 4F RT A2NM 2002080900001 20020809 00001 NM 2002 8 9 0202546743 1 20020723 A 5311 FRAME BOEING 747 747249F 1384849 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 643NW 22245 During "M" Check found crack in frame at BS 460 between stringers 11R and 12R. Repaired per EA 67-191812. 2 L 7 4 4F A20WE 2002080900003 20020809 00003 NE 2002 8 9 AUS20020636 2 20020504 A 7230 PCEPR0087 COMPRESSOR PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL ENGINE FOD W O OTHER E VIBRATION/BUFFET CL CLIMB 1 AU S (AUS) ENGINE COMPRESSOR FIRST, SECOND, THIRD AND FOURTH STAGE ROTORS AND STATORS DAMAGED BY FOD. INLET SCREEN HOLED/DENT ED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002080900004 20020809 00004 EU 2002 8 9 AUS20020637 1 20020529 A 7410 9550176020 IGNITER BOX AEROSP SA365 SA365C 8680667 EU TMECA ARRIEL ARRIEL1A 60030 NE ENGINE CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ENGINE HIGH ENERGY IGNITION SYSTEM GENERATOR CONTAMINATED WITH WATER DUE TO INCORRECT SEALING OF THE UNIT DURING M ANUFACTURE. 1 G 7 2 3U 3 U H10EU E19EU 2002080900005 20020809 00005 NE 2002 8 9 AUS20020640 2 20020510 A 7210 310703301 BEARING EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14RF 14RF9 NE ENG RGB CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ENGINE REDUCTION GEARBOX BEARINGS NR 15 AND NR 19 PITTED. METAL CONTAMINATION OF FILTER. SUSPECT FAILURE DUE TO ST ATIC DISCHARGE. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2002080900006 20020809 00006 NM 2002 8 9 AUS20020641 1 20020605 A 5753 65B20225 FLAP TRACK BOEING 747 747238B 1384828 NM TE FLAPS BROKEN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT INBOARD TRAILING EDGE FOREFLAP TRACK BROKEN. 2 L 7 4 4F A20WE 2002080900007 20020809 00007 NE 2002 8 9 AUS20020645 2 20020626 A 7250 30537401 TURBINE WHEEL PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL ENGINE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ENGINE COMPRESSOR TURBINE HAD LARGE PIECES MISSING. FOUND DURING BOROSCOPE INSPECTION. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002080900008 20020809 00008 NM 2002 8 9 AUS20020646 1 20020703 A 2750 315 SWITCH BOEING 747 747338 NM TE FLAPS FAILED W K NONE L NO TEST IN INSP/MAINT 1 AU S (AUS) FLAP SWITCH S315 HAD HIGH RESISTANCE. FOUND DURING FUNCTIONAL TEST IAW TST 018632. 2 L 7 2 4F RT A20WE 2002080900009 20020809 00009 CE 2002 8 9 AUS20020647 1 20020521 A 5312 LAP JOINT BEECH 200 B200C 1152924 CE PWA PT6 PT6A42 52043 NE BULKHEAD SCRATCHED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) BULKHEAD LAP JOINT SCRATCHED. 1 L 7 2 4T 4 T A24CE E4EA 2002080900010 20020809 00010 WP 2002 8 9 AUS20020649 1 20020617 A 6320 269A505120 BEARING HUGHES 269 269C 4470504 WP LYC O360 HIO360D1A 41514 EA M/R GEARBOX FAILED W O OTHER O OTHER NR NOT REPORTED 1 AU S (AUS) MAIN ROTOR TRANSMISSION OUTPUT SHAFT BEARING DISINTEGRATED. TAILROTOR DRIVESHAFT TWISTED UP AT TRANSMISSION END. 1 G 7 1 3O 3 O 4H12 1E10 2002080900011 20020809 00011 NM 2002 8 9 AUS20020651 1 20020705 A 6310 A1902 BELT ROBSIN R22 R22BETA 7640110 NM LYC O320 O320B2C 41508 EA ENGINE/XMSN DISTORTED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) MAIN ROTOR DRIVE BELTS STRETCHED BEYOND LIMITS. 1 G 7 1 3O 3 O H10WE E274 2002080900012 20020809 00012 NM 2002 8 9 AUS20020652 1 20020611 A 3244 324001 TIRE BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C 13802 EU MLG DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S 387 (AUS) RT OUTBOARD MAIN WHEEL TIRE TREAD SEPARATED. 2 L 7 2 4F 4 F RT A16WE E21EU 2002080900013 20020809 00013 SO 2002 8 9 AUS20020653 2 20020703 A 8530 639272E CYLINDER BEECH 35 S35 1151532 CE CONT O520 IO520B 17032 SO MCAULY 2A36C 2A36C23 GL ENGINE LEAKING W K NONE O OTHER IN INSP/MAINT 1 AU S 123 (AUS) ENGINE CYLINDER LEAKING FROM HEAD/BARREL JOINT. 1 L 7 1 3O 3 O 3A15 E5CE 5 C P880 2002080900014 20020809 00014 NM 2002 8 9 AUS20020654 1 20020626 A 6310 A1902 BELT ROBSIN R22 R22BETA 7640110 NM LYC O320 O320B2C 41508 EA ENGINE/XMSN SEPARATED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ENGINE TO TRANSMISSION DRIVE BELT SEPARATED. 1 G 7 1 3O 3 O H10WE E274 2002080900015 20020809 00015 NM 2002 8 9 AUS20020655 1 20020614 A 6310 A1902 BELT ROBSIN R22 R22BETA 7640110 NM LYC O320 O320B2C 41508 EA ENGINE/XMSN FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ENGINE TO TRANSMISSION DRIVE BELTS FAULTY. ONE BELT FAILED ANDONE BELT STRETCHED BEYOND LIMITS. 1 G 7 1 3O 3 O H10WE E274 2002080900016 20020809 00016 CE 2002 8 9 AUS20020657 1 20020517 A 2434 D0FF10300B ALTERNATOR CESSNA 182 182Q 2072732 CE CONT O470 O470* 17026 SO MCAULY 2A34C 2A34C203 GL DC SYSTEM FAULTY W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 AU S 463 (AUS) ALTERNATOR SUSPECT FAULTY. INVESTIGATION FOUND THAT ALTERNATORWINDINGS HAD SHORT CIRCUITED. 1 H 7 1 3O 3 O NT 3A13 E273 5 C P3EA 2002080900017 20020809 00017 2002 8 9 AUS20020659 4 20020607 A 2210 7003652631 DISPLAY AMD FALC50 FALCON900 2700160 EU GARRTT TFE731 TFE7315BR WP AUTOPILOT SYSTEM FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S 89121396 (AUS) ADVISORY DISPLAY FROZE. AIRCRAFT IS RAAF FALCON 900 A26-077. 2 L 7 3 4F 4 F RT A46EU E6WE 2002080900018 20020809 00018 2002 8 9 AUS20020660 4 20020604 A 3418 861CAU2 TRANSMITTER AMD FALC50 FALCON900 2700160 EU GARRTT TFE731 TFE7315BR WP STALL WARNING FAULTY W O OTHER J WARNING INDICATION DE DESCENT 1 AU S 0185 (AUS) RT ANGLE OF ATTACK TRANSMITTER FAULTY. INVESTIGATION FOUND THAT THE INTERNAL POTENTIOMETER WAS OPEN CIRCUITED. AIR CRAFT IS A RAAF FALCON 900 A26-076. 2 L 7 3 4F 4 F RT A46EU E6WE 2002080900019 20020809 00019 NE 2002 8 9 2002F00777 2 20020717 A 7200 ENGINE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE WING SURGES G AMTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 513AT 32449 31795 DURING THROTTLE MOVEMENT ENGINE PARAMETERS SURGED WITH EEC ENGAGED. WITH EEC NOT ENGAGED, ENGINE STILL SURGED, BUT NOT A S MUCH. ENGINE FLUCTUATED WITH EEC ON OR OFF. PERFORMED TEST 13 TAKEOFF POWER, ALL PARAMETERS ON BOTH ENGINES ARE NORM AL WITHIN LIMITS IAW M/M 71-00-00, OK TO RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002080900020 20020809 00020 2002 8 9 AUS20020661 4 20020515 A 3418 861CAU2 TRANSMITTER AMD FALC50 FALCON900 2700160 EU GARRTT TFE731 TFE7315BR WP STALL WARNING FAULTY W O OTHER J WARNING INDICATION CL CLIMB 1 AU S 3040 (AUS) RT ANGLE OF ATTACK TRANSMITTER FAULTY. INVESTIGATION FOUND THAT THE INTERNAL POTENTIOMETER WAS SHORT CIRCUITED. A IRCRAFT IS A RAAF FALCON 900 A26-073. 2 L 7 3 4F 4 F RT A46EU E6WE 2002080900021 20020809 00021 2002 8 9 AUS20020662 4 20020529 A 3452 6226523001 CONTROLLER AMD FALC50 FALCON900 2700160 EU GARRTT TFE731 TFE7315BR WP ATC TRANSPONDER FAULTY W K NONE L NO TEST IN INSP/MAINT 1 AU S (AUS) ATC CONTROLLER FAULTY. INVESTIGATION FOUND THE CONTROLLER HAD ANUNSERVICEABLE PHOTOELECTRIC CELL. AIRCRAFT IS AN R AAF FALCON 900A26-070. 2 L 7 3 4F 4 F RT A46EU E6WE 2002080900022 20020809 00022 SW 2002 8 9 AUS20020663 1 20020628 A 7714 GEU7A TACH GENERATOR BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE FAULTY W O OTHER E VIBRATION/BUFFET LD LANDING 1 AU S (AUS) TACHOMETER GENERATOR FAILED. 1 G 7 2 4U 4 U H4SW E22EA 2002080900023 20020809 00023 NM 2002 8 9 2002F00778 1 20020608 A 3233 273A22011 ACTUATOR BOEING 737 73783N 13844HI NM RT MLG FAULTY G AMTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 308TZ 2065 28244 WHEN LOWERING THE LANDING GEAR, THE RIGHT GEAR WAS SLOW TO ILLUMINATE A GREEN LIGHT. THE GEAR WAS VERIFIED DOWN AND LOC KED BUT CHANGED TO A RIGHT GEAR UNSAFE INDICATION. MANUAL GEAR EXTENSION WAS UNSUCCESSFUL, LANDED WITH RIGHT GEAR OVERC ENTER, GEAR DID NOT COLLAPSE. REMOVED AND REPLACED INOPERATIVE DOWNLOCK ACTUATOR IAW MM TASK 32-32-51-400-801. 2 L 7 2 4F RT A16WE 2002080900025 20020809 00025 NM 2002 8 9 AUS20020665 1 20020709 A 3230 856920 PROXIMITY SWITCH BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE MLG FAULTY W O OTHER O OTHER CL CLIMB 1 AU S (AUS) PROXIMITY SENSE ELECTRICAL UNIT (PSEU) FAULTY. LANDING GEAR LEVER LOCK SOLENOID FAILED TO OPERATE. 2 L 7 4 4F 4 F RT A20WE E30NE 2002080900026 20020809 00026 NM 2002 8 9 AUS20020666 1 20020709 A 4920 380029816 ENGINE BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE APU LEAKING W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 AU S (AUS) APU LEAKING OIL. OIL FUMES IN CABIN. 2 L 7 2 4F 4 F RT A1NM E3NE 2002080900031 20020809 00031 2002 8 9 AUS20020668 4 20020620 A 3414 640608901 INDICATOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R354 R3544123F13 NE COCKPIT LEAKING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) AIR SPEED INDICATOR (ASI) FAULTY. ASI FOUND TO HAVE A CASE LEAK.FOUND DURING INSTALLATION CHECK. THE ASI HAD BEEN RECENTLYREPAIRED. PERSONNEL/MAINTENANCE ERROR. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P61GL 2002080900032 20020809 00032 NM 2002 8 9 AUS20020671 1 20020701 A 2700 82710202001 CONTROL QUADRANT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FLIGHT CONTROLS FAULTY W O OTHER F FLT CONT AFFECTED LD LANDING 1 AU S (AUS) UNCOMMANDED ROLL DISCONNECT. INVESTIGATION COULD FIND NO DEFINITE CAUSE FOR THE DEFECT BUT FOUND THE CABLES MARGIN ALLY SLACK AND ASLIGHT SMEARING OF GREASE ON THE CLUTCH FACES. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002080900033 20020809 00033 NM 2002 8 9 AUS20020672 1 20020620 A 3500 83510011107 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE OXYGEN SYSTEM MISREPAIRED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) OXYGEN LINES WRAPPED WITH INCORRECT SPIRAL WRAP AS PER SB A8-35 AND AD/DHC-8/14. PERSONNEL/MAINTENANCE ERROR. UNAP PROVED PART. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002080900034 20020809 00034 NM 2002 8 9 AUS20020673 1 20020627 A 3500 83510011107 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE OXYGEN SYSTEM MISREPAIRED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) OXYGEN LINES WRAPPED WITH INCORRECT SPIRAL WRAP AS PER SB A8-35 AND AD/DHC-8/14. PERSONNEL/MAINTENANCE ERROR. UNAP PROVED PART. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002080900035 20020809 00035 NM 2002 8 9 AUS20020675 1 20020613 A 7312 WA9056 ELEMENT STWARNER 10839E DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE FUEL HEATER FAULTY W O OTHER E M J VIBRATION/BUFFET OVER TEMP WARNING INDICATION CR CRUISE 1 AU S WA9056 (AUS) FUEL HEATER ELEMENT SUSPECT FAULTY. ENGINE FUEL SYSTEM FITTINGS LOOSE. LIMITED INFORMATION PROVIDED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002080900036 20020809 00036 EA 2002 8 9 AUS20020676 2 20020616 A 7314 B7849 DRIVE SHAFT ROMEC RG17980D BNORM BN2 BN2B20 1520302 EU LYC O540 IO540K1B5 41532 EA HARTZL HCC2Y HCC2YK2 GL ENG FUEL PUMP WRONG PART W K NONE K W FLUID LOSS INADEQUATE Q C IN INSP/MAINT 1 AU S 262 B7849 (AUS) ENGINE FUEL PUMP DRIVE SHAFT INCORRECT ITEM. INVESTIGATION FOUNDTHAT THE DRIVE SHAFT WAS APPROXIMATELY 6.35MM (0.2 5IN) SHORTERTHAN NORMAL. THE INCORRECT DRIVE SHAFT HAD BEEN FITTED AT THE LAST OVERHAUL/REPAIR OF THE PUMP. PERSONNEL/M AINTENANCE ERROR. UNAPPROVED PART. 1 H 7 2 3O 3 O A17EU 1E4 5 C P920 2002080900037 20020809 00037 EU 2002 8 9 AUS20020677 1 20020628 A 2120 ODOR BAC 146 146200A 1500266 EU LYC ALF502 ALF502R3A 41580 NE COCKPIT DETECTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) NR 1 ENGINE FUMES ENTERING CABIN. LIMITED INFORMATION PROVIDED. 2 H 7 4 4F 4 F A49EU E6NE 2002080900038 20020809 00038 EU 2002 8 9 AUS20020678 1 20020629 A 2150 11341041 MOTOR REIMS 406 F406 7535723 EU PWA PT6 PT6A112 52043 NE MCAULY 3G34C7 3GFR34C701 GL COOLING COMPRESS FAILED W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 AU S 1817 (AUS) REAR AIRCONDITIONING COMPRESSOR ELECTRIC MOTOR FAULTY. THECIRCUIT BREAKER WAS POPPED AND WHEN RESET, THE MOTOR WAS SPARKING EXCESSIVELY AND EMITTING SMOKE AT THE COMMUTATOR. 1 L 7 2 3T 3 T RT A54EU E4EA 5 C P60GL 2002080900039 20020809 00039 NM 2002 8 9 AUS20020680 1 20020708 A 6310 A1902 BELT ROBSIN R22 R22BETA 7640110 NM LYC O320 O320B2C 41508 EA ENGINE/XMSN DISTORTED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ENGINE TO TRANSMISSION "V" BELTS STRETCHED BEYOND LIMITS. 1 G 7 1 3O 3 O H10WE E274 2002080900040 20020809 00040 EU 2002 8 9 AUS20020685 1 20020710 A 5210 COVER BAC 146 146200A 1500266 EU LYC ALF502 ALF502R3A 41580 NE PAX DOOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) REAR (2L) DOOR LOWER HINGE COVER IMPACTED AND BUCKLED CAUSING COVER TO JAM ON THE DOOR WHEN CLOSED. PERSONNEL/MAIN TENANCE ERROR. 2 H 7 4 4F 4 F A49EU E6NE 2002080900041 20020809 00041 EA 2002 8 9 AUS20020686 2 20020714 A 8500 L1806848 ENGINE GULSTM 500 500S 0141107 SW LYC O540 IO540E1B5 41532 EA HARTZL HCC3Y HCC3YR2 NE LEFT MALFUNCTIONED W O OTHER E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AU S (AUS) LT ENGINE VIBRATING AND LOSING POWER. LIMITED INFORMATION PROVIDED. 1 H 7 2 3O 3 O 6A1 1E4 5 C P25EA 2002080900042 20020809 00042 CE 2002 8 9 AUS20020697 1 20020605 A 5500 STRUCTURE CESSNA 182 182P 2075816 CE CONT O470 O470* 17026 SO EMPENNAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) BOTH HORIZONTAL STABILISER AND FIN CONTAINED EXTENSIVE SURFACECORROSION. 1 H 7 1 3O 3 O NT TA13 E273 2002080900044 20020809 00044 NM 2002 8 9 HNAA0200051 1 20020807 A 2920 HCA1N022 CONTACTOR DHAV DHC8 DHC8201 2809001 NM INTERMITTENT A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 985HA 7990 479 WHEN #1 ENGINE WAS SHUTDOWN FOR SINGLE ENGINE TAXI THE #1 HYDRAULIC MAIN AND STANDBY SYSTEMS PRESSURE WENT TO ZERO. CREW HAD TO USE PARKING BRAKE TO STOP A/C. REPLACED CONTACTOR 2421-K2. 2 H 7 2 4T RT A13NM 2002080900045 20020809 00045 EA 2002 8 9 AUS20020700 2 20020712 A 7322 61E22534 CARBURETOR HUGHES 269 269C 4470504 WP LYC O360 HO360C1A 41514 EA ENGINE FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NEWLY FITTED ENGINE CARBURETTOR WAS UNABLE TO LEAN THE MIXTURE USING THE MIXTURE SCREW. 1 G 7 1 3O 3 O 4H12 E286 2002080900046 20020809 00046 EA 2002 8 9 HNAA0200045 1 20020616 A 2435 23088002B STARTER GEN DHAV DHC8 DHC8311 1386006 EA INOPERATIVE A HNAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 07 806SA 28300 2 279 #2 D.C. GENERATOR DROPPED OFF LINE. DUE TO #1 D.C. GENERATOR BEING PREVIOUSLY MEL'D CREW DECLARED AN EMERGENCY AND RETUR NED TO PIT. REPLACED #2 STARTER/GENERATOR. 2 H 7 2 4T RT A13NM 2002080900047 20020809 00047 SW 2002 8 9 AUS20020701 1 20020628 A 5280 DOOR SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UHR WP MLG STICKING W O OTHER O OTHER DE DESCENT 1 AU S (AUS) LH NOSE LANDING GEAR DOOR CATCHING ON FUSELAGE SKIN AT THE EDGE OF THE NOSE LANDING GEAR BAY PREVENTING NLG FROM E XTENDING. PERSONNEL/MAINTENANCE ERROR. 2 L 7 2 4T 4 T RT A5SW E4WE 2002080900048 20020809 00048 EA 2002 8 9 AUS20020707 1 20020715 A 5753 SKIN DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE TE FLAP CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT INBOARD FLAP CRACKED. CRACK IS LOCATED IN THE TOP PLANK ALONG THE TRAILING EDGE PARALLEL TO THE TRAILING EDGE CHANNEL. CRACKLENGTH IS LONGER THAN 381MM (15IN). INVESTIGATION FOUND A DENTAND DELAMINATION IN THE BOTTOM PLANK IN THE SAME AREA ASTHE CRACK. SUSPECT THAT THIS IS THE CAUSE OF THE CRACKING IN THE TOP PLANK. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002080900049 20020809 00049 NM 2002 8 9 AUS20020709 1 20020711 A 5270 MS24266R16 CONNECTOR BOEING 767 76733A 1385209 NM PWA 4056 PW4056 NE CARGO DOOR DAMAGED W O OTHER O OTHER LD LANDING 1 AU S (AUS) FORWARD CARGO DOOR CONNECTOR PLUG DAMAGED BEYOND REPAIR. SHORT CIRCUIT IN PLUG CAUSED FAULT IN PSEU AND PROXIMITY SWITCH.SUSPECT PLUG DAMAGED BY CONTAINER DURING UNLOADING. 2 L 7 2 4F 4 F RT A1NM E24NE 2002080900050 20020809 00050 EU 2002 8 9 AUS20020712 1 20020722 A 3240 NAS16126 O-RING BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE MLG SPLIT W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 AU S (AUS) PARK BRAKE HYDRAULIC SYSTEM MANIFOLD O-RING SEAL DEFECTIVE. HIGH PRESSURE HYDRAULIC MIST ENTERED CABIN. 2 H 7 4 4F 4 F RT A49EU E6NE 2002080900051 20020809 00051 EU 2002 8 9 AUS20020714 1 20020706 A 3242 AHA21745 BRAKE BAG BAE146 BAE146300A 1500267 EU LT MLG OVERHEATED W O OTHER M J OVER TEMP WARNING INDICATION LD LANDING 1 AU S (AUS) BOTH LT MAIN LANDING GEAR BRAKES OVERHEATED TO 800 DEGREES C. 2 H 7 4 4F RT A49EU 2002080900053 20020809 00053 CE 2002 8 9 AUS20020715 1 20020620 A 5341 817861020 BOLT BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60 52043 NE WING TO BODY CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT AND RT WING UPPER REAR AND LOWER REAR ATTACHMENT BOLTS EXHIBIT SIGNS OF CRACKING IN RADIUS. FOUND DURING INSPEC TION IAW AD/BEECH 300/8 AND RAYTHEON S.I.R.M. 2 L 7 2 4T 4 T A24CE E4EA 2002080900054 20020809 00054 2002 8 9 AUS20020719 4 20020622 A 6122 NODCFS290D7T3 GOVERNOR CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MCAULY 3AF32C 3AF32C87 GL PROPELLER MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT ENGINE GOVERNOR METAL CONTAMINATION. 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 2002080900056 20020809 00056 NM 2002 8 9 AUS20020720 1 20020712 A 2434 761574B GENERATOR BOEING 737 737* NM GE CFM56 CFM567B24 NE DC SYSTEM DISCONNECTED W O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 AU S 1434 (AUS) NR 1 ENGINE DRIVEN GENERATOR DISCONNECTED. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002080900057 20020809 00057 NM 2002 8 9 AUS20020722 1 20020712 A 3260 858601 PSEU ELDEC 858601 DHAV DHC8 DHC8315 2809010 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE MLG FAULTY W O OTHER N FALSE WARNING TO TAKEOFF 1 AU S 185 (AUS) PROXIMITY SENSE ELECTRONIC UNIT (PSEU) FAULTY. FAULT FOUND IN ELECTRONIC CIRCUIT BOARD. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002080900059 20020809 00059 2002 8 9 AUS20020723 4 20020716 A 3421 4019700902 INDICATOR BAC 146 146100A 1500260 EU LYC ALF502 ALF502R3A 41580 NE COCKPIT FAILED W O OTHER O OTHER CR CRUISE 1 AU S 16090 (AUS) NR 2 ATTITUDE DIRECTOR INDICATOR TOPPLED IN FLIGHT. 2 H 7 4 4F 4 F RT A49EU E6NE 2002080900061 20020809 00061 EU 2002 8 9 AUS20020724 1 20020713 A 2761 BOLT BAC 146 146100A 1500260 EU LYC ALF502 ALF502R3A 41580 NE SPOILER ACTUATOR LOOSE W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT AIRBRAKE ACTUATOR ATTACHMENT BOLT MIGRATED UPWARDS AND DAMAGED THE RT REAR FUSELAGE AT FRAME 50. INVESTIGATION FOUND THE NUT AND SPLIT PIN MISSING WITH THE WASHER FOUND IN THE AIRBRAKE BAY.SUSPECT SPLIT PIN NOT INSTALLED. PERSONNEL /MAINTENANCE ERROR. 2 H 7 4 4F 4 F RT A49EU E6NE 2002080900062 20020809 00062 NM 2002 8 9 AUS20020729 1 20020716 A 2780 CONNECTOR BOEING 737 737800* NM GE CFM56 CFM567B24 NE LE SLAT LOOSE W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LEADING EDGE STANDBY DRIVE SHUTOFF VALVE CONNECTOR LOOSE. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002080900063 20020809 00063 NM 2002 8 9 AUS20020731 1 20020717 A 4920 737M49503011 ENGINE BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU APU FAILED W E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) APU SHUTDOWN OCCURRED WITH LOW OIL PRESS' AND HIGH OIL TEMP' LIGHTS ILLUMINATED. 2 L 7 2 4F 4 F RT A16WE E21EU 2002080900064 20020809 00064 NM 2002 8 9 AUS20020732 1 20020712 A 2913 66087 PUMP BOEING 737 737800* NM GE CFM56 CFM567B24 NE HYDRAULIC SYS CONTAMINATED W O OTHER J WARNING INDICATION CR CRUISE 1 AU S (AUS) ENGINE DRIVEN HYDRAULIC PUMP CONTAMINATED WITH METAL. CASE DRAIN FILTER IMPLODED. METAL CONTAMINATION OF HYDRAULIC SYSTEM A'. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002080900065 20020809 00065 NM 2002 8 9 AUS20020734 1 20020721 A 2722 285T0014104 ACTUATOR BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL RUDDER FAULTY W D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 AU S (AUS) RUDDER RATIO ACTUATOR FAULTY. 2 L 7 2 4F 4 F RT A1NM E23EA 2002080900066 20020809 00066 2002 8 9 AUS20020739 4 20020722 A 3457 066040311122 RECEIVER PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL GPS MALFUNCTIONED W K NONE L NO TEST IN INSP/MAINT 1 AU S 836 (AUS) GPS LOST USER DATABASE DURING FLIGHT. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002080900067 20020809 00067 NM 2002 8 9 AUS20020740 1 20020720 A 5754 114T310023 SKIN BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL LE SLATS DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 3, NR 6 AND NR 9 LEADING EDGE SLATS DELAMINATED IN AREA OF AFT WEDGES. FOUND DURING INSPECTION IAW AD/B767/73. 2 L 7 2 4F 4 F RT A1NM E23EA 2002080900069 20020809 00069 NM 2002 8 9 AUS20020741 1 20020723 A 3510 83510011107 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CREW OXYGEN SYS CHAFED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LOW PRESSURE OXYGEN DISTRIBUTION PIPES FOR PILOT AND CO-PILOT OXYGEN SUPPLY EXTENSIVELY CHAFED FROM CONTACT WITH T HE LH AND RHFLIGHT COMPARTMENT SHELVES. CHAFING DAMAGE IN SOME AREAS WAS0.508MM TO 0.584MM (0.020IN TO 0.023IN) DEEP. DA MAGE LIMITIS 0.254MM (0.010IN). PIPES HAD PROTECTIVE TEFLON SPIRAL WRAP INSTALLED WHICH WAS IN GOOD CONDITION SUGGESTIN G THAT THE CHAFING HAD OCCURRED PRIOR TO FITMENT OF THE SPIRAL WRAP. FOUND DURING INSPECTION IAW TSI-DHC8-35-003. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002080900072 20020809 00072 NE 2002 8 9 AUS20020743 2 20020722 A 7220 754139785050 CONTROLLER BOEING 747 747238B 1384828 NM RROYCE RB211 RB211524D419 54555 NE ENGINE FAULTY W O OTHER E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 AU S 4512 (AUS) NO1 ENGINE VIGV CONTROLLER FAULTY. CONTROLLER COULD NOT BE ADJUSTED TO BRING ENGINE PARAMETERS WITHIN LIMITS. 2 L 7 4 4F 4 F A20WE E12EU 2002080900075 20020809 00075 NM 2002 8 9 AUS20020744 1 20020725 A 2150 HEAT EXCHANGER BOEING 767 767330 NM RROYCE RB211 RB211524* NE CABIN COOLING FAULTY W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 AU S (AUS) LT AIRCONDITIONING PACK HEAT EXCHANGER FAULTY. 2 L 7 2 4F 4 F RT A1NM E12EU 2002080900077 20020809 00077 NM 2002 8 9 2002UALA01193 1 20020721 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 BULKHEAD 178 CRACKED RBL 5, WL 200 AND AT RBL 8-9 WL 200. MAJOR REPAIR ACCOMPLISHED. SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900078 20020809 00078 SW 2002 8 9 AUS20020748 1 20020710 A 3213 369H600151 STRUT HUGHES 500N 500N 3027374 SW ALLSN 25OC 250C20R GL MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT MAIN LANDING GEAR STRUT CRACKED FROM RIVET HOLE. CRACK LENGTH 9.525MM (0.375IN). 1 G 7 1 3U 3 U NC H3WE E4CE 2002080900079 20020809 00079 GL 2002 8 9 AUS20020750 2 20020715 A 7200 ENGINE DOUG 600N 600N 3027377 NM ALLSN 250C 250C47M 03013 GL ENGINE BAY FAILED W O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 AU S (AUS) ENGINE PROBLEM. LIMITED INFORMATION PROVIDED. 1 G 7 1 3U 3 U NC H3WE E1GL 2002080900081 20020809 00081 NM 2002 8 9 2002UALA01194 1 20020721 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 STATION 178 BULKHEAD AFT SIDE LBL 5.7 CHORD AT WL 184.5 INTERSECTION CRACKED AT RADIUS GOING TO FASTENER HOLE. MAJOR RE PAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900082 20020809 00082 NM 2002 8 9 AUS20020753 1 20020726 A 4920 ENGINE BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL APU FAILED W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S (AUS) APU COULD NOT BE STARTED. 2 L 7 2 4F 4 F RT A1NM E23EA 2002080900083 20020809 00083 NM 2002 8 9 2002UALA01195 1 20020721 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 FORWARD GALLEY DOOR CUTOUT FRAME IS CRACKED AT FORWARD TOP STOP PAD FITTING LOWER OUTBOARD CORNER. MAJOR REPAIR ACCOMPL ISHED. INSTALLED NEW FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400100 20021104 00100 NM 2002 11 4 2002UALA01196 1 20020719 A 5270 C210214 SWITCH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L5 DOOR MALFUNCTIONED A UALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 29 104UA 26902 DOOR 5L WARNING LIGHT ILLUMINATED. REPLACED 5L DOOR WARNING SWITCH. OPERATION CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002082300107 20020823 00107 NM 2002 8 23 2002UALA01197 1 20020721 A 2720 RUDDER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE TAIL MALFUNCTIONED A UALA K NONE F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 375UA 24640 AIRCRAFT LANDED UNDER AMBER ALERT AFTER REPORTING UNCOMMANDED RUDDER MOVEMENT ON TAKEOFF. A UPDATE FROM THE FDR DATA, I T DOES NOT APPEAR THAT ANY FLIGHT CONTROL SYSTEM INITIATED THE EVENT. THE DATA DOES SUGGEST THAT THE INITIAL UPSET COUL D HAVE BEEN INDUCED BY AN ATMOSPHERIC DISTURBANCE. THE RUDDER PCU AND THE YAW DAMPER COUPLER WERE REPLACED. THERE WERE NO FAULTS FOUND WITH THE RUDDER PCU. THE YAW DAMPER COUPLER IS STILL BEING CHECKED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900084 20020809 00084 NM 2002 8 9 2002UALA01198 1 20020719 A 3397 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 771UA 26932 BOTH EEL LIGHTS INOP DUE TO BROKEN WIRING HARNESS. REPAIRED WIRING HARNESS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002080900085 20020809 00085 NM 2002 8 9 2002UALA01199 1 20020719 A 2751 INDICATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE TE FLAPS FAILED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 375UA 24640 AIRCRAFT MADE A REDUCED FLAP LANDING UNDER AMBER ALERT DUE TO A SPLIT FLAP INDICATION. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED THE FLAP POSITION INDICATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900086 20020809 00086 NM 2002 8 9 2002UALA01200 1 20020719 A 3260 SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NLG & MLG MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 323UA 23955 AIRCRAFT RETURNED TO FIELD WHEN THE LANDING GEAR WOULD NOT RETRACT. SUPPLEMENTAL DATA UPDATE THE MAIN LANDING GEAR SAFE TY SENSOR FAILED. REPLACED THE S105 LANDING GEAR SAFETY SWITCH. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900088 20020809 00088 EU 2002 8 9 2002UALA01207 1 20020726 A 3110 CONTROLLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 447UA 836 RETURNED TO FIELD. SMOKE ELECTRICAL SMELL IN CONTROL CABIN. CIRCUIT BREAKERS PHC2, AOA2, PITOT2, TAT2, AND PHC3 ALL PO PPED. REPLACED NR 2 PHC AND TESTED ALL PROBE HEATERS FOR PROPER OPERATION. SYSTEM OPERATED NORMAL WITH NO ADDITIONAL F AILURES NOTED ON SUBSEQUENT FLIGHTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2002080900089 20020809 00089 NM 2002 8 9 2002UALA01209 1 20020727 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 STATION 480 FRAME CRACKED OUT OF UPPER RIVET HOLE FOR STOW BIN ATTACH CLIP JUST ABOVE STRINGER 9L. MAJOR REPAIR ACCOMPL ISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900090 20020809 00090 NM 2002 8 9 2002UALA01210 1 20020728 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 945UA 26684 UPON ARRIVAL PRIOR TO MOVING JET BRIDGE A GOUGE WAS FOUND APPROX 26 IN AFT OF FORWARD LEFT DOOR NEAR ABOVE FLOOR LEVEL S TRINGER. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED STRINGER & SKIN REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900091 20020809 00091 NM 2002 8 9 2002UALA01211 1 20020728 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 STATION 440 FRAME CRACKED OUT OF UPPER RIVET HOLE FOR STOW BIN ATTACH CLIP JUST ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPL ISHED. REPAIR DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900092 20020809 00092 NM 2002 8 9 2002UALA01212 1 20020728 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 STATION 400 FRAME CRACKED OUT OF UPPER RIVET HOLE FOR STOW BIN ATTACH CLIP JUST ABOVE STRINGER 9L. MAJOR REPAIR ACCOMPL ISHED. REPAIR DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900093 20020809 00093 NM 2002 8 9 2002UALA01213 1 20020728 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 CABIN STATION 887 FRAME WEB CRACKED AT STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900094 20020809 00094 NM 2002 8 9 C8GA20020010 1 20020808 A 2611 100064901 SMOKE DETECTOR BOEING 727 727223 1384074 NM CARGO BAY DEFECTIVE A C8GA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 15 715AA 22470 FLT 2220 FROM PHX TO TOL. DURING CRUISE LEVEL, THE FORWARD CARGO COMPARTMENT FIRE LIGHT CAME ON. APPROPRIATE CHECK LIST WERE ACCOMPLISHED AND THE LIGHT EXTINGUISHED, THEN THE SMOKE LOWER FORWARD DETECTOR SYSTEM INOPERATIVE MAINTENANCE LIGHT CAME ON. NOTIFIED ATC, DECLARED EMERGENCY AND DIVERTED TO KICT AND LANDED WITHOUT INCIDENT. INSPECTED FORWARD CARGO PIT AND FIRE WARNING SYSTEM AND FOUND TWO SMOKE DETECTORS INOPERATIVE. MEL THE FORWARD LOWER CARGO DETECTION SYSTEM PER 26- 19-1. AIRCRAFT RETURNED TO SERVICE. MEL 26-19-1 WAS CLEARED 8/8/2002 BY REPLACING TWO SMOKE CARGO DETECTORS. SYSTEMS OPE RATIONAL CHECKED GOOD PER SECURAPLANE ST3000 MANUAL. 2 L 7 3 4F A3WE 2002080900095 20020809 00095 NM 2002 8 9 2002UALA01214 1 20020728 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 CABIN STATION 847 FRAME WEB AT STRINGER 9R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900096 20020809 00096 NM 2002 8 9 2002UALA01215 1 20020728 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 CABIN STATION 827 STRINGER 4R FRAME WEB WAS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900097 20020809 00097 NM 2002 8 9 2002UALA01216 1 20020729 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 CABIN BODY FRAME WEB IS CRACKED BODY STATION 440 STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. SPLICED BODY FRAME WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082300109 20020823 00109 NM 2002 8 23 2002UALA01217 1 20020726 A 2612 87858101 CONNECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FIRE WARNING SHORTED A UALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 309UA 23670 DURING CLIMBOUT, APU FIRE LIGHT ILLUMINATED WITH THE APU OFF. ON SECOND OCCURRENCE, APU FIRE HANDLE PULLED, BOTTLE DISC HARGED, AND RETURNED TO FIELD. INSPECTED APU OVERHEAT DETECTION SYSTEM AND FOUND A SHORT TO GROUND AT CONNECTOR D4934P ON BOTH PINS A & C. REPLACED CONNECTORS D1876 AND D1878. APU FIRE DETECTION SYSTEM CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900098 20020809 00098 NM 2002 8 9 2002UALA01218 1 20020728 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 STA 1640 FLOORBEAM UPPER CAP HAS EXCESS MATERIAL LOSS AT RBL 18 DUE TO CORROSION. MAJOR REPAIR ACCOMPLISHED USING STRAP REINFORCEMENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080900099 20020809 00099 NM 2002 8 9 2002UALA01219 1 20020728 A 5347 SEAT TRACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 CABIN SEAT TRACK MOUNT FLANGE UPPER SURFACE HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPLACED SEAT TRAC K BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080900100 20020809 00100 NM 2002 8 9 2002UALA01220 1 20020729 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 CABIN FLOORBEAM CAP UPPER SURFACE, STA 660 LBL 24, HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. STRAP AND ANGLE INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080900101 20020809 00101 SO 2002 8 9 AUS20020758 1 20020705 A 3230 9529900 STUD PIPER PA32 PA32R300 7103213 SO LYC O540 IO540K1G5 41532 EA HARTZL HCC2Y HCC2YK1 GL MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) MAIN LANDING GEAR SIDE BRACE STUDS CRACKED. FOUND DURING MAGNETIC PARTICLE INSPECTION IAW AD/PA32/79. 1 L 7 1 3O 3 O A3SO 1E4 5 C P920 2002082300111 20020823 00111 NM 2002 8 23 2002UALA01222 1 20020728 A 5610 141T480013 WINDSHIELD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT CRACKED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 651UA 17930 25389 ELECTRICAL ARC OCCURRED AT THE BOTTOM OF THE LEFT FORWARD WINDOW DURING CRUISE. CREW TURNED OFF WINDOW HEAT. SUBSEQUEN TLY WINDOW SHATTERED REMAINING IN ONE PIECE. REPLACED NUMBER 1 LEFT WINDSHIELD ASSEMBLY AS OUTLINED IN MM 56-11-01. AD DITIONALLY DUE TO WINDOW FAILURE AND SUBSEQUENT REPLACEMENT, REPLACED LEFT FORWARD WINDOW HEAT CONTROLLER M191 AS OUTLIN ED IN MM 30-41-01. 2 L 7 2 4F 4 F RT A1NM E24NE 2002080900103 20020809 00103 NM 2002 8 9 AUS20020760 1 20020729 A 6310 A1902 BELT ROBSIN R22 R22BETA 7640110 NM LYC O320 O320B2C 41508 EA ENGINE/XMSN DISTORTED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ENGINE TO TRANSMISSION V' BELTS STRETCHED WITH UNEVEN WEAR PATTERNS. BELTS WERE WRAPPED AROUND ACTUATOR ASSEMBLY. 1 G 7 1 3O 3 O H10WE E274 2002080900104 20020809 00104 NM 2002 8 9 AUS20020761 1 20020727 A 6310 A1902 BELT ROBSIN R22 R22BETA 7640110 NM LYC O320 O320B2C 41508 EA ENGINE/XMSN DAMAGED W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 AU S (AUS) ENGINE TO TRANSMISSION V' BELT CAME OFF PULLEYS. SUSPECT BELTS FAULTY. 1 G 7 1 3O 3 O H10WE E274 2002080900105 20020809 00105 NM 2002 8 9 AUS20020762 1 20020726 A 6310 A1902 BELT ROBSIN R22 R22BETA 7640110 NM LYC O320 O320B2C 41508 EA ENGINE/XMSN DISTORTED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ENGINE TO TRANSMISSION V' BELTS STRETCHED BEYOND LIMITS. 1 G 7 1 3O 3 O H10WE E274 2002080900106 20020809 00106 CE 2002 8 9 AUS20020764 1 20020724 A 2820 CONNECTOR CESSNA 182 182P 2075816 CE CONT O470 O470* 17026 SO FUEL LINE DETERIORATED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FLEXIBLE FUEL LINE CONNECTORS PERISHED. 1 H 7 1 3O 3 O NT TA13 E273 2002082300112 20020823 00112 NM 2002 8 23 2002UALA01223 1 20020727 A 7920 LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE LEAKING A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 520UA 24890 726532 LOW OIL INDICATION ON NR 2 ENGINE. ON DOWNWIND LEG, OIL PRESSURE AND QUANTITY DROPPED TO ZERO. WINDMILLED FOR ABOUT 7 MINS PER CREW. FOUND MAIN OIL PRESSURE TRANSMITTER LINE LEAKING. SECURED LINE, CHANGED OIL FILTER AND CHECKED CHIP DET ECTORS. CHIP DETECTORS CHECKED OKAY AND CLEANED. SERVICE ENG OIL TO FULL ADDED 18 QTS, ALL LEAK CHECKS GOOD. ENGINE W AS NOT REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080900107 20020809 00107 EA 2002 8 9 AUS20020771 1 20020701 A 8000 STARTER DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL ENGINE OVERHEATED W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AU S (AUS) LH ENGINE STARTER MOTOR ACTIVATED WITHOUT THE BATTERY MASTERSWITCH BEING SELECTED ON'. OVERHEAT AND SHORT CIRCUITI NG DAMAGE CAUSED TO WIRING AND COMPONENTS IN THE START SYSTEM. NO DEFINITE CAUSE FOR THE DEFECT COULD BE FOUND. 1 H 7 2 3T 4 T RT A9EA E4EA 6 C P15EA 2002080900108 20020809 00108 NM 2002 8 9 AALA20020998 1 20020711 A 3340 POWER SUPPLY BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 (POWER SUPPLY) DURING OVERNIGHT MAINTENANCE EXTERIOR R1 AND OVERWING EMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHTING POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2002080900109 20020809 00109 NM 2002 8 9 AALA20020992 1 20020710 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 396AN 29603 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 3B INOPERATIVE. RECONNECTED EMERGENCY ESCAPE PATH LIGHTING CONNECTOR AT SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATIONS. 2 L 7 2 4F RT A1NM 2002080900110 20020809 00110 NM 2002 8 9 2002UALA01227 1 20020729 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 STATION 400 FRAME CRACKED OUT OF UPPER RIVET HOLE FOR STOW BIN ATTACH CLIP JUST ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPL ISHED. MANUFACTURED AND INSTALLED FRAME DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900111 20020809 00111 NM 2002 8 9 DHL2002727009 1 20020807 A 2610 1014A POWER UNIT BOEING 727 727228 1384083 NM A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 727DH 20204 1) APU WOULD NOT PERFORM A FIRE TEST. 2) TROUBLESHOT SYSTEM AND FOUND APU OPERATING POWER UNIT FAULTY. REMOVED & REPLA CED POWER UNIT AND OPS CHECKED, WITH NO DEFECTS, PER B727 MM 26-23-00. 2 L 7 3 4F RT A3WE 2002080900112 20020809 00112 2002 8 9 249TR0006 4 20020802 A 3420 INDICATOR BOEING 737 7372K5 138448X NM A PIDA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 05 249TR 22598 Both ADI's had "speed" flags which made auto throttles inop. Installed serviceable ADI IAW 34-22-0, accomplished PDC Bi te of auto throttles per MM 22-31-01, ops check good 2 L 7 2 4F RT A16WE 2002080900113 20020809 00113 2002 8 9 249TR0007 4 20020807 A 2230 COMPUTER BOEING 737 7372K5 138448X NM A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 A/T fails bite test and goes completely inop at times. R&R A/T computer Ops normal per Bite test MM 22-31-01 2 L 7 2 4F RT A16WE 2002080900114 20020809 00114 NM 2002 8 9 2002UALA01228 1 20020729 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 CABIN STATION 947.5 BETWEEN LBL 5 & LBL 20 UPPER SURFACE OF FLOORBEAM HAS EXCESSIVE MATERIAL REMOVED. MAJOR REPAIR ACCO MPLISHED. INSTALLED ANGLE DOUBLER REPAIRS & FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900115 20020809 00115 NM 2002 8 9 SWAA021749 1 20020804 A 3350 65C34691 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT LOOSE AT ROW NR 16 DEF. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002080900116 20020809 00116 2002 8 9 SWAA021753 4 20020805 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F A16WE 2002080900117 20020809 00117 NM 2002 8 9 SWAA021754 1 20020804 A 5311 6516301 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002080900118 20020809 00118 NM 2002 8 9 SWAA021756 1 20020805 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 375, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2002080900119 20020809 00119 NM 2002 8 9 SWAA021757 1 20020801 A 5313 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND SHEAR TIES CRACKED (2 EA) AT BS 1040, BETWEEN STR'S 2R AND 3R AND BETWEEN STR'S 2L AND 3 L. REMOVED AND REPLACED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2002080900120 20020809 00120 NM 2002 8 9 SWAA021760 1 20020805 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 795, STR 26R. REPAIRED STR PER BFG ER. 2 L 7 2 4F RT A16WE 2002080900121 20020809 00121 NM 2002 8 9 SWAA021761 1 20020805 A 5311 6546546 FRAME BOEING 737 7373T5 1384608 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 867, WL 165 AND RBL 18. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002080900122 20020809 00122 NM 2002 8 9 SWAA021762 1 20020802 A 5610 5893543130 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT CRACKED A SWAA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 SW 29 744SW 29490 DIVERSION, F/O FWD WINDSHIELD ARCHED, DELAMINATED, AND THEN CRACKED. REMOVED AND REPLACED R1 WINDOW AND WINDOW HEAT CON TROLLER PER MM. 2 L 7 2 4F RT A16WE 2002080900123 20020809 00123 2002 8 9 SWAA021729 4 20020802 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD CABIN DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C2 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2 L 7 2 4F RT A16WE 2002080900124 20020809 00124 2002 8 9 SWAA021734 4 20020804 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 FWD ENTRY DOOR EMERGENCY EVAC SLIDE DEPLOYED BY FLIGHT ATTENDANT. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002080900125 20020809 00125 NM 2002 8 9 SWAA021737 1 20020803 A 5310 BAC1503 STIFFENER BOEING 737 7372K6 1364440 NM LH MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 129SW 22340 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663, LBL 56. REMOVED AND REPLACED STIFFENER PER SRM . 2 L 7 2 4F RT A16WE 2002080900126 20020809 00126 2002 8 9 SWAA021740 4 20020801 A 2565 6949956 CABLE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002080900127 20020809 00127 NM 2002 8 9 SWAA021741 1 20020803 A 5330 6545776 SKIN BOEING 737 7372K6 1364440 NM FUSELAGE BUCKLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 129SW 22340 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN BUCKLED AT BS 1006, STR 27R. REPAIRED SKIN PER SWA RA. 2 L 7 2 4F RT A16WE 2002080900128 20020809 00128 NM 2002 8 9 SWAA021742 1 20020802 A 3220 6558250 CIRCUIT BOARD BOEING 737 7373T5 1384608 NM E/E COMP FAULTY A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 29 692SW 23062 NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER RAISING GEAR HANDLE. REMOVED AND REPLACED PRINTED CIRCUIT BOARDS M983 AND M1215 PER MM. 2 L 7 2 4F RT A16WE 2002080900129 20020809 00129 NM 2002 8 9 SWAA021743 1 20020803 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207 AND LBL 39. REMOVED AND REPLACED FRAME PER SRM . 2 L 7 2 4F RT A16WE 2002080900130 20020809 00130 NM 2002 8 9 SWAA021744 1 20020804 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 1/2D CHECK, FRAME CORRODED, BS 767 BETWEEN STR'S 26R AND 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002080900131 20020809 00131 NM 2002 8 9 SWAA021745 1 20020804 A 5311 6546546 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 767, BETWEEN STR'S 8R AND 9R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002080900132 20020809 00132 NM 2002 8 9 SWAA021747 1 20020804 A 5320 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR'S 13L AND 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002080900133 20020809 00133 NM 2002 8 9 2002UALA01245 1 20020729 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 FORWARD CABIN FLOOR CREASE BEAM I/B CHORD HAS SURFACE CORROSION STATION 310 TO STATION 365 RBL 63. MAJOR REPAIR ACCOMPL ISHED. REPLACED CREASE BEAM I/B CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002080900134 20020809 00134 NM 2002 8 9 2002UALA01246 1 20020728 A 3244 TIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 FAILED A UALA O OTHER O OTHER TO TAKEOFF 1 WP 29 119UA 28812 NR 4 REAR TIRE BLEW ON TAKEOFF, FOUND UPON ARRIVAL. NR 3 REAR TIRE INVOLVED. SUPPLEMENTAL DATA UPDATE TIRE POSITION 4 R THROWN TREAD ON TAKEOFF. CAUSE UNDETERMINED (NO SIGN OF FOD OR LOW PRESSURE CONDITION) TIRE AND MATE (3R) REPLACED. TIRE WAS 1ST RECAP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002080900135 20020809 00135 NM 2002 8 9 2002UALA01247 1 20020730 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 STATION 294.5 FRAME JUST INBOARD OF STRINGER 4R IS BLENDED BEYOND LIMIT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900136 20020809 00136 NM 2002 8 9 2002UALA01248 1 20020724 A 5754 FILLER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE L/E SLAT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 223UA 30224 AT C-CHECK MAINTENANCE, UAL DISCOVERED 20 INCHES OF OUTBOARD END OF FILLER WAS MISSING FROM THE NR 1 SLAT SEAL. THIS FI LLER WAS INSTALLED PER THE MANUFACTURER. SUPPLEMENTAL DATA UPDATE UAL SUSPECTS THAT TENSION WAS INDUCED DURING THE INS TALLATION OF THE BULB SEAL FILLER, CAUSING IT TO EVENTUALLY TEAR AND BREAK. EVENTUALLY IT WORKED ITS WAY OUT OF THE BUL B SEAL DURING SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002080900137 20020809 00137 NE 2002 8 9 02FDEA00512 2 20020709 A 7261 SEAL AIRBUS 310 A310 EU PWA JT9 JT9D7R4E1 52054 NE NR 1 ENGINE LEAKING A FDEA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 25 446FE 224 NR 1 ENGINE, STARTER DRIVE SHAFT OIL LEAKAGE. REMOVED AND REPLACED SEAL PER AMM. 2 L 7 2 4F 4 F RT A35EU E3NE 2002080900138 20020809 00138 NE 2002 8 9 02FDEA00514 2 20020723 A 7200 JT8D17A ENGINE BOEING 727 727200 138407E NM PWA JT8 JT8D217C 52053 NE NR 2 MALFUNCTIONED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 205FE 22927 NR 2 ENGINE LOST OIL QUANTITY AND PRESSURE SHORTLY AFTER TAKEOFF, WITH CORRESPONDING LOW OIL PRESSURE/FILTER BYPASS LIGH T ON IN FRONT PANEL. SHUTDOWN ENGINE IAW CHECKLIST AND RETURNED FOR UNEVENTFUL LANDING. REPLACED NR 2 ENGINE. OPS AND LEAK CHECK OK. 2 L 7 3 4F 4 F RT A3WE E9NE 2002080900139 20020809 00139 2002 8 9 02FDEA00515 4 20020723 A 3417 HG480B13 ADC BOEING 727 727200 138407E NM COCKPIT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 492FE 21530 CAPTAINS AIRSPEED AND ALTIMETER AND VERTICAL SPEED INDICATOR FAILED ON ROTATION WITH WINDSHEAR WARNINGS. REPLACED CADC IAW MM. OPS CHECK GOOD. CAT STATUS DOWNGRADED TO CHK II, CHK II. OVERALL CAT STATUS IS NOT II. 2 L 7 3 4F RT A3WE 2002080900140 20020809 00140 NM 2002 8 9 02FDEA00516 1 20020724 A 1430 BOLT DOUG MD11 MD11 3023602 NM RT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 616FE 48747 RIGHT TRUNNION MOUNTING BOLTS FOUND EMITTING RUST. REMOVED AND REPLACED BOLTS PER MM. 2 L 7 3 4F RT A22WE 2002080900141 20020809 00141 NM 2002 8 9 02FDEA00517 1 20020718 A 2810 SHROUD DOUG MD11 MD11 3023602 NM CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 CENTER CARGO COMPARTMENT, FUEL DRAIN SHROUD ASSEMBLY CRACKED AT BS 1801. PERFORMED STOP DRILL ON CRACK PER SRM. 2 L 7 3 4F RT A22WE 2002080900142 20020809 00142 NM 2002 8 9 AALA20020993 1 20020711 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE LIGHTING AT SEAT 7B, INOPERATIVE. RECONNECTED LOOSE SEAT ROW CONNEC TOR AT SEAT 7B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2002080900143 20020809 00143 NM 2002 8 9 02FDEA00518 1 20020723 A 3070 HEATER DOUG MD11 MD11 3023602 NM ICE PROTECTION SPARKS A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 SPARK FOUND EMITTING FROM THE FORWARD WASTE DRAIN HEATER AT FORWARD AVIONICS COMPARTMENT SIDE, WHEN POWER SWITCHED ON. 2 L 7 3 4F RT A22WE 2002080900144 20020809 00144 NM 2002 8 9 02FDEA00519 1 20020722 A 1430 BOLT DOUG MD11 MD11 3023602 NM LANDING GEAR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 616FE 48747 TRUNNION MOUNTING LT BOLTS FOUND EMITTING WITH RUST. R&R BOLTS PER MM 32-15-01. 2 L 7 3 4F RT A22WE 2002080900145 20020809 00145 NM 2002 8 9 02FDEA00521 1 20020725 A 5310 SHEAR TIE BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 151FE 19147 CORROSION ON SHEAR TIE AT BS 968, RBL 3-5, WL 150. REPAIRED SHEAR TIE IAW SRM. 2 L 7 3 4F RT A3WE 2002080900146 20020809 00146 WP 2002 8 9 02FDEA00522 1 20020725 A 1430 BOLT DOUG DC10 DC1030 3023501 WP RT MLG SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 RIGHT MAIN GEAR W/W SHEARED AT VERTICAL FITTING TO TRAPEZOIDAL PANEL AT OM SIDE OF W/W BS 1381. INSTALLED NEW BOLT PER AOL 10-20088. 2 L 7 3 4F A22WE 2002080900147 20020809 00147 NM 2002 8 9 AALA20020989 1 20020710 A 3350 HOUSING BOEING 767 767323 1385205 NM LIGHT HSG INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 20H INOPERATIVE. REPLACED AFT LIGHT HOUSING A T SEAT 20H. SYSTEM GROUND CHECKED NORMAL OPERATIONS. 2 L 7 2 4F RT A1NM 2002080900148 20020809 00148 NM 2002 8 9 02FDEA00548 1 20020807 A 3260 WARNING SYSTEM BOEING 727 727200 138407E NM COCKPIT MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 494FE 21532 LEFT GEAR DOOR LIGHT REMAINED ILLUMINATED ON TAKEOFF. LIGHT STAYED ON AFTER CYCLING GEAR IAW RED TABS. OPERATED LEFT L ANDING GEAR DOOR SEVERAL TIMES. DOOR INDICATION OPS GOOD AT THIS TIME. 2 L 7 3 4F RT A3WE 2002080900149 20020809 00149 NM 2002 8 9 02FDEA00549 1 20020807 A 3260 SWITCH BOEING 727 727200 138407E NM LT MLG LACK OF LUBE A FDEA K NONE N FALSE WARNING AP APPROACH 1 SO 25 494FE 21532 LEFT MAIN GEAR DOOR INDICATED UNSAFE WHEN GEAR WAS LOWERED. CYCLED GEAR AND DOOR LIGHT WENT OUT PER NORMAL OPS. CLEANE D AND LUBED LEFT MAIN LANDING GEAR DOOR SWITCH CHECKED ADJUSTMENT AND TEST PER MM. OPERATED DOORS SEVERAL TIMES AND OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 2002091200073 20020912 00073 NM 2002 9 12 02FDEA00551 1 20020805 A 5753 BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT WING OUTBOARD FLAP HINGE FITTING LWR MOUNTING SIDE CORRODED AFTER SEALANT REMOVAL. REMOVED AND REPLACED BRACKET ASSY PER MM 57-53-01. 2 L 7 3 4F RT A22WE 2002091200074 20020912 00074 NM 2002 9 12 02FDEA00552 1 20020806 A 5753 HINGE FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LT WING OUTBOARD FLAP INBOARD HINGE FITTING LOWER MOUNTING SIDE CORRODED AFTER SEALANT REMOVAL. REMOVED AND REPLACED BR ACKET ASSY PER MM 57-53-01-4. 2 L 7 3 4F RT A22WE 2002091200075 20020912 00075 NM 2002 9 12 02FDEA00553 1 20020806 A 5753 HINGE FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LT WING OUTBOARD FLAP OUTBOARD HINGE FITTING LWR MOUNTING SIDE CORRODED AFTER SEALANT REMOVAL. REMOVED AND REPLACED BRA CKET ASSY PER MM 57-53-01-4. 2 L 7 3 4F RT A22WE 2002091200076 20020912 00076 NM 2002 9 12 02FDEA00554 1 20020805 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 LWR EXT FUSELAGE HAS BULGING SKIN AND SHEARED RIVET BETWEEN STR 28R AND 29R AT BS 352 AND 358. REMOVED AND REPLACED SKI N PER SRM 51-30-2, 51-30-5, 51-30-8, 51-10-2. 2 L 7 3 4F RT A3WE 2002080900150 20020809 00150 NM 2002 8 9 02FDEA00557 1 20020807 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 NR 1 TAIL FUEL TANK FIFTH BARREL NUT BORE FWD OF REAR SPAR IS CORRODED AT HORIZ STAB UPPER AFT PLANK COMMON TO LT OPERAT ING BLKHD AND CONSTANT SECTION JOINT. 2 L 7 3 4F RT A22WE 2002080900151 20020809 00151 NM 2002 8 9 AALA20020990 1 20020710 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 17B INOPERATIVE. RECONNECTED LOOSE CONNECTION AT SEAT 17B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2002080900152 20020809 00152 NM 2002 8 9 PCS2002F00000 1 20020710 A 2130 C238 SWITCH BOEING 727 727212 138407G NM WARNING LT SWITC INOPERATIVE A PCSA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 17 598AJ 21947 CREW REPORTED UNABLE TO PRESSURIZE IN-FLIGHT, DUMPED FUEL AND RETURNED. CAPTAIN FOLLOWED ABNORMAL PROCEDURES AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND E/E COMPARTMENT DOOR PARTIALLY OPEN DOOR WAS CLOSED. THE E/E DOOR WARNING LIGHT SYSTEM WAS ALSO DEFERRED. MAINTENANCE ORDERED E/E DOOR WARNING LIGHT SWITCH. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2002080900153 20020809 00153 WP 2002 8 9 WX0A02003 1 20020627 A 3350 20131A BATTERY PACK DOUG DC9 DC987 3022087 WP LOW VOLTAGE FAILED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 17 945MA 49725 DURING SCHEDULED MAINTENANCE FORWARD ENTRANCE AND GALLEY DOOR EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATED WHEN EMERGENCY LIGHT SWITCH SELECTED TO ON POSITION. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW. SYSTEM OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 2002080900154 20020809 00154 WP 2002 8 9 WX0A02004 1 20020627 A 3350 WIRE DOUG DC9 DC987 3022087 WP LOOSE CONNECTION LOOSE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 17 945MA 49725 DURING SCHEDULED MAINTENANCE FORWARD SECTION OF FLOOR TRACK LIGHTING FAILED TO ILLUMINATE WHEN EMERGENCY LIGHT SWITCH SE LECTED TO ON POSITION. FOUND LOOSE GROUND WIRE AT STA 384. RESECURED GROUND WIRE. SYSTEM OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 2002080900155 20020809 00155 NM 2002 8 9 AALA20020975 1 20020702 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 DURING OVERNIGHT MAINTENANCE LOWER LEFT HAND FORWARD EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT G3 GALLEY COAT CLOSET INOPE RATIVE. REPLACED LOWER LEFT HAND FORWARD LIGHT ASSEMBLY AT G3 GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2002080900156 20020809 00156 WP 2002 8 9 AALA20020976 1 20020709 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AA 49473 CORROSION ON SEAT NR 1. REMOVED SEAT TRACK NR 1 FROM STA 1174 TO 1307 AN INSTALLED NEW SEAT TRACK SRM. 2 L 7 2 4F A6WE 2002080900157 20020809 00157 WP 2002 8 9 AALA20020977 1 20020709 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AA 49473 GOUGES IN CUSP STA 294 RIGHT OUTBOARD OF TRACK. INSTALLED DOUBLER REPAIR IAW AARD. 2 L 7 2 4F A6WE 2002080900158 20020809 00158 WP 2002 8 9 AALA20020978 1 20020709 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AA 49473 IMPROPER FIBERGLASS REPAIR ON LEFT CUSP AT 35,251 HAS CORROSION UNDER PATCH AND BLUE WATER STAINS. REMOVED FIBERGLASS R EPAIR, REMOVED CORROSION, TREATED AND PRIMED AND INSTALLED DOUBLER PER AARD. 2 L 7 2 4F A6WE 2002080900159 20020809 00159 WP 2002 8 9 AALA20020979 1 20020709 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AA 49473 CUSP WEB CRACKED AT LIGHTING HOLE, STA 223 RIGHT OUTBOARD TRACK. INSTALLED NEW SECTION AT CUSP WEB, PER SRM. 2 L 7 2 4F A6WE 2002080900160 20020809 00160 WP 2002 8 9 AALA20020980 1 20020709 A 5310 5936038501 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AA 49473 CORROSION ON AFT CARGO DOOR JAMB LOWER CHORD ANGLE FROM STA 1155 TO 1211. REMOVED CORROSION BEYOND LIMITS. REPLACED CO MPLETE LOWER DOOR, CHORD ANGLE. 2 L 7 2 4F A6WE 2002080900161 20020809 00161 WP 2002 8 9 AALA20020981 1 20020709 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AA 49473 CORROSION ON SEAT TRACK FLANGE. CABIN SEAT TRACK NR 5. INSTALLED REPAIR STRAP TO SEAT TRACK NR 5 AT STA 200 IAW AARD. 2 L 7 2 4F A6WE 2002080900162 20020809 00162 NM 2002 8 9 AALA20020983 1 20020706 A 2612 5753669 PRESSURE SWITCH BOEING 767 767323 1385205 NM SMOKE DETECTION FAILED A AALA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 21 363AA 24044 CARGO DET AIR STATUS MSD ILLUMINATED. RESET CBS AS PER QRH. STATUS MSG REMAINED, DIVERTED. TROUBLESHOT SYSTEM, REMOVE D AND REPLACED SMOKE DETECTOR PRESS SWITCH. ALSO FOUND NR 2 BLOWER WAS EXTREMELY HOT TO TOUCH. REMOVED AND REPLACED BO TH NR 1 AND NR 2 FORWARD CARGO BLOWERS AS A PRECAUTION, PERFORMED OPS CHECK IAW MM. ALL OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2002080900163 20020809 00163 NM 2002 8 9 PCAA0208087 1 20020808 A 2910 8Z6069161 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM LEAKING A PCAA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 EA 13 829EX 146 ROC-DCA FLIGHT#3950. CREW REPORTED THAT THEY HAD INDICATION THAT #2 HYDRAULIC SYSTEM HAD LOST ALL FLUID. EMERGENCY DECLA RED, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE BY FLAP MOTOR LEAKING. LINE REPLACED WIT H AN INTERIM FLEX LINE. #2 ENGINE DRIVEN HYDRAULIC PUMP REPLACED. GROUND RUN OF ENGINE REVEALED NO LEAKS, OPERATIONAL CH ECK GOOD. AIRCRAFT RETURNED TO SERVECE. 2 H 7 2 4T RT A13NM 2002080900164 20020809 00164 NM 2002 8 9 AALA20020984 1 20020706 A 2432 5040 BATTERY BOEING 777 777223 1385213 NM E/E BAY FAULTY A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 750AN 30259 ENROUTE, STATUS MSGS BATTERY CHARGER MAIN AND MAIN BATTERY THEN BATTERY CHARGER MAIN MSG WAS REPLACED BY MAIN BATTERY OV ERHEAT MAIN BATTERY WAS NOW CHARGING AT UP TO 67 AMPS BATTERY WAS VISUALLY CHECKED AND FOUND TO BE SMOKING AS PER ALLIAN CE TECH CIRCUIT AND BREAKER P320 K-9 PULLED. SWAPPED BATTERY AND CHARGER WITH APU AS PER MM. CHARGING AND BATTERY SERV ICE CIRCUIT BEAKER AFTER FIX. 2 L 7 2 4F RT T00001SE 2002080900165 20020809 00165 NM 2002 8 9 AALA20020985 1 20020709 A 3350 BPS73 BATTERY PACK BOEING 767 767223 1385123 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 307AA 22313 DURING OVERNIGHT MAINTENANCE FOUND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECK NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2002080900166 20020809 00166 NM 2002 8 9 AALA20020986 1 20020707 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AA 22327 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING ROW 17B THROUGH 28B INOPERATIVE. SECURED EMERGENCY LI GHT POWER SUPPLY CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATIONS. 2 L 7 2 4F RT A1NM 2002080900167 20020809 00167 NM 2002 8 9 AALA20020987 1 20020705 A 3350 CONNECTOR BOEING 777 777223 1385213 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 761AJ 31478 DURING OVERNIGHT MAINTENANCE FOUND SEAT 4D EMERGENCY ESCAPE LIGHT INOPERATIVE. CONNECTED CANNON PLUG AT HARNESS. SYSTE M GROUND CHECKED NORMAL OPERATIONS. 2 L 7 2 4F RT T00001SE 2002080900168 20020809 00168 NM 2002 8 9 AALA20020988 1 20020704 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39365 24046 DURING OVERNIGHT MAINTENANCE FOUND SLIDE LIGHT AT L2 DOOR, INOPERATIVE. REPLACED BATTERY PACK FOR SLIDE LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2002080900169 20020809 00169 NM 2002 8 9 AALA20020991 1 20020710 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 396AN 29603 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE LIGHTING INOPERATIVE AT SEAT 2B. REPAIRED EMERGENCY ESCAPE LIGHTING CANNON PLUG SOCKET AT SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2002080900170 20020809 00170 NM 2002 8 9 AALA22020982 1 20020701 A 2120 SMOKE BOEING 767 767323 1385205 NM COCKPIT DETECTED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 376AN 25445 ENROUTE, EXPERIENCED STRONG ELECTRICAL SMELL WITH HAZE IN CABIN, COCKPIT AND AT OVERWING EMERGENCY EXIT. EMERGENCY DECL ARED. LANDED WITHOUT INCIDENT. PERFORMED CHECK OF ELECTRICAL SYSTEM. RAN PACKS AT FULL POWER. UNABLE TO DUPLICATE PR OBLEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2002080900171 20020809 00171 NM 2002 8 9 UPS02239016 1 20020730 A 5350 FRAME BOEING 727 72722C 138400F NM FAIRING # 3334 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C CORROSION ON FAIRING # 3334 ON FRAME AT L/H FAN INLET DOOR AFT AREA FRAME REPAIR CARRIED OUT IAW S RM 51-40-4 L/H FAN INLET DOOR REPLACED IAW MM 21-52-51 & DOOR ACTUATING ROD REP LACED IAW MM 21-52-51 2 L 7 3 4F A3WE 2002080900172 20020809 00172 NM 2002 8 9 UPS02239020 1 20020722 A 5310 DOUBLER BOEING 727 72722C 138400F NM R/H WINDOW POST CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C CRACK ON R/H WINDOW POST BETWEEN R1 & R2 WINDOWS AT UPPER CORNER REPAIR DOUBLER FABRICATED IAW SRM 53-30-3 REPAIR DOUBLER INSTALLED IAW SRM 53-30-3 FIG 8 REPAIR 2 2 L 7 3 4F A3WE 2002080900173 20020809 00173 NM 2002 8 9 UPS02239022 1 20020808 A 5330 STRINGER BOEING 727 72722C 138400F NM BS 259.5 STR19R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C MATERIAL LOSS INDICATION AT BS 259.5 AT STR.19 R/H. REMOVED FASTENERS IAW SRM 51-30-2. CORR NOT FO UND TO BE WITHIN LIMIT S IAW SRM 53-30-01. REPAIR CARRIED OUT AS REQUIRED IAW EO-B727-5310-1371 APPDX. E. 2 L 7 3 4F A3WE 2002080900174 20020809 00174 NM 2002 8 9 UPS02239025 1 20020723 A 5310 FITTING BOEING 727 72722C 138400F NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C LH WHEEL WELL BS 940 FORGING HAS A SUSPECT CRACK @ BASE OF PREVIOUS BLENDOUT FITTING REPLACED IAW UPS EO B727-5310-4501 2 L 7 3 4F A3WE 2002080900175 20020809 00175 NM 2002 8 9 SABA020080 1 20020808 A 3350 1306 BULB DHAV DHC8 DHC8103 1386005 NM N / A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 Aircraft 883 on flight 5080 from CLT to CVG the crew reported the overhead emergency would not test during Preflight. Ma intenance removed and replaced bulb, System ops checked good. Aircraft was returned to service 2 H 7 2 4T RT A13NM 2002080900176 20020809 00176 EA 2002 8 9 COMA0260469 1 20020808 A 5311 601R3402467 FRAME CNDAIR CL600 CL6002B19 1900309 EA F.S. 574 MISDRILLED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 938CA 18296 7046 THE L/H SIDE FRAME AT FS574 WAS DRILLED INTO THE RADIUS BETWEEN STRINGERS 12L AND 14L.REMOVED THE DAMAGED FRAME SECTOR A ND INSTALLED A NEW FRAME SECTOR I/A/W WVAC EO 601R-53-3413A. 2 L 7 2 4F RT A21EA 2002080900177 20020809 00177 EA 2002 8 9 COMA0260470 1 20020803 A 5300 FLANGE CNDAIR CL600 CL6002B19 1900309 EA F.S.484 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 938CA 18295 7046 THE INTERCOSTAL FLANGE AT BL36 (L/H & R/H)AND ANGLES AT BL27(L/H&R/H) ARE CRACKED AT F.S. 484.REPAIRED INTERCOSTAL FLANG E AND ANGLES AT (L/H&R/H) AT BL36 AND BL27 I/A/W WVAC E.O. 601R-53-3409 AT F.S. 484. 2 L 7 2 4F RT A21EA 2002080900178 20020809 00178 EA 2002 8 9 COMA0260471 1 20020806 A 7930 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J N WARNING INDICATION FALSE WARNING TO TAKEOFF 1 SO 01 447CA 7552 FLIGHT 6006 LEFT ENGINE OIL PRESSURE INDICATED ZERO DURING T/O.REPAIRED LOOSE WIRING AT PRESSURE TRANSDUCER. 2 L 7 2 4F RT A21EA 2002080900179 20020809 00179 NE 2002 8 9 COMA0260472 2 20020805 A 7200 5083T02P01 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT ENG WORN A COMA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 963CA 7127 FLIGHT 5542 LEFT ENGINE LOW OIL PRESSURE WARNING.REPLACED THE #6 BEARING CARBON SEAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2002080900180 20020809 00180 EA 2002 8 9 COMA0260473 1 20020806 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 868CA 7427 FLIGHT 6044 FLAPS FAIL MESSAGE DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002080900181 20020809 00181 EA 2002 8 9 COMA0260474 1 20020808 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 458CA 7613 FLIGHT 5984 LOUD HOWLING NOISE FROM NOSE AREA AFTER T/O.FOUND GROUND SERVICES PANEL LEFT OPEN. INSPECTED FOR DAMAGE AND SECURED PANEL TO CLOSED POSITION. 2 L 7 2 4F RT A21EA 2002080900182 20020809 00182 EA 2002 8 9 COMA0260475 1 20020808 A 2720 601R5122623 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A COMA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 01 821CA 7420 FLIGHT 5737 RUDDER TRIM IS INOP, NOSE RIGHT.REPLACED THE RUDDER TRIM PANEL. 2 L 7 2 4F RT A21EA 2002080900183 20020809 00183 NM 2002 8 9 SCNA02006 1 20020808 A 2613 CONNECTOR BOEING 737 7378Q8 13844BX NM OUT OF ADJUST A SCNA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 805SY 30032 Left wing to body overheat lite came on in flight at approximately 37,500 feet. Found connection between aft cargo loop s M348 & M1147. Cleaned connection and fault cleared. 2 L 7 2 4F RT A16WE 2002080900184 20020809 00184 NM 2002 8 9 USA2002F00060 1 20020715 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM ROW 1,6,9 DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1,6, AND 9 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. 2 L 7 2 4F RT A2NM 2002080900185 20020809 00185 NM 2002 8 9 USA2002F00061 1 20020713 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM ROW 6 INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 614AU 27145 FOUND THE FLOOR LEVEL EMERGENCY LIGHT AT ROW 6, INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2 L 7 2 4F RT A2NM 2002080900186 20020809 00186 NM 2002 8 9 USA2002F00062 1 20020714 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM ROWS 3,26,29 DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 616AU 27147 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROWS 3, 26 AND 29. MAINTENANCE REPLACED THE BATTERIES. 2 L 7 2 4F RT A2NM 2002080900187 20020809 00187 NM 2002 8 9 2002UALA01201 1 20020723 A 2121 EVT3454H FAN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE E/E BAY SEIZED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 806UA 788 SMOKE AND FUMES IN THE CABIN. THE EXTRACT FAN FOR THE AVIONICS COOLING SYSTEM WAS FOUND SEIZED AND CAUSE FOR THE BURNIN G SMELL IN THE CABIN. REPLACED EXTRACT FAN. 2 L 7 2 4F 4 F RT A28NM E40NE 2002080900188 20020809 00188 NM 2002 8 9 2002UALA01202 1 20020723 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 344UA 24248 BODY STATION 188 FRAME CRACKED IN RADIUS STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900189 20020809 00189 EU 2002 8 9 2002UALA01203 1 20020719 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 467UA 1359 FUSELAGE SKIN DAMAGED AT FRAME 67 TO FRAME 70 FROM STRINGER 42L TO 42R. MAJOR REPAIR ACCOMPLISHED. INSTALLED TWO DOUBL ERS AND FILLERS. 2 L 7 2 4F 4 F RT A28NM E40NE 2002080900190 20020809 00190 NE 2002 8 9 2002UALA01204 2 20020723 A 7320 ACTUATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUEL SYSTEM FAILED A UALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 310UA 23671 AIRCRAFT ABORTED TAKEOFF AT APPROXIMATELY 90 KNOTS BECAUSE ENGINE NR 1 DID NOT REACH TARGET N1. SUPPLEMENTAL DATA UPDAT E ROOT CAUSE WAS INTERNAL FAILURE OF THE FUEL SPAR SHUTOFF VALVE ACTUATOR. THE ACTUATOR WAS REPLACED AND THE ENGINE IS NOW OPERATING NORMALLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082300108 20020823 00108 NE 2002 8 23 2002UALA01205 2 20020722 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE STALLED A UALA H DEACTIVATE SYST/CIRCUITS R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 643UA 10530 10530 25093 727948 NR 2 ENGINE COMPRESSOR STALL. ENGINE RECOVERED. NR 2 ENGINE HAD A GROUP 3 (TAKEOFF) SURGE. THE ENGINE SELF RECOVERED. ENGINE WAS REPLACED AT TERMINATION OF THE FLIGHT FOR COMPRESSOR REFURBISHMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 2002080900191 20020809 00191 NM 2002 8 9 2002UALA01208 1 20020727 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 STATION 520 FUSELAGE FRAME CRACKED IN WEB AND INBOARD FLANGE RADIUS BELOW STRINGER 14R OUT OF INSULATION STANDOFF HOLE J UST BELOW FRAME SPLICE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002080900192 20020809 00192 NM 2002 8 9 AWXA200200708 1 20020729 A 5320 6546812170 FLOOR SUPPORT BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOOR SUPPORT BETWEEN BS 947.5 AND BS 967, LBL 18. MAINTENANCE REMOVED FLOOR SUPPORT BETWEEN BS 947.5 TO BS 967, LBL 18; FABRICATED A NEW FLOOR S UPPORT, AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG. 10-11. 2 L 7 2 4F RT A16WE 2002080900193 20020809 00193 NM 2002 8 9 AWXA200200709 1 20020729 A 5320 6546812170 FLOOR SUPPORT BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOOR SUPPORT BETWEEN BS 947.5 AND BS 967, RBL 8. MAINTENANCE REMOVED FLOOR SUPPORT BETWEEN BS 947.5 TO BS 967, RBL 8; FABRICATED A NEW FLOOR SUP PORT, AND INSTALLED REPAIR IAW B737-300 SRM 51-40-05, PG. 1, 2, & 4, AND SRM 51-40-02, PG. 10-11. 2 L 7 2 4F RT A16WE 2002080900194 20020809 00194 NM 2002 8 9 AWXA200200710 1 20020729 A 5315 6546812186 BEAM BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 0 0 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF DIAGONAL FLOOR SUPPORT BE TWEEN BS 986.5 AND BS 1006, RBL 8 TO RBL 17. MAINTENANCE REMOVED DIAGONAL FLOOR SUPPORT BETWEEN BS 986.5 TO BS 1006, RBL 8 TO RBL 17; FABRICATED A NEW FLOOR SUPPORT, AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG. 11-12. 2 L 7 2 4F RT A16WE 2002080900195 20020809 00195 NM 2002 8 9 AWXA200200712 1 20020725 A 5345 69366564 ANGLE BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 0 0 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK A CRACK WAS FOUND ON ATTACH ANGLE BETWEEN BS 927 AND 947, BL 0. MAINTENANCE REMOV ED CRACKED ATTACH ANGLE, FABRICATED A NEW ATTACH ANGLE, AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG.6-7. 2 L 7 2 4F RT A16WE 2002080900196 20020809 00196 NM 2002 8 9 AWXA200200713 1 20020723 A 5220 65795003 SUPPORT BOEING 737 73733A 1384673 NM R/H O/W HATCH CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 0 0 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK A CRACK WAS FOUND ON LOWER AFT ATTACH HOLE OF INTERIOR LINER SUPPORT R/H EMERGENC Y ESCAPE HATCH. MAINTENANCE CUTOUT CRACK ON INTERIOR LINER SUPPORT R/H EMERGENCY ESCAPE HATCH, FABRICATED A REPAIR DOUBL ER AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG. 2-4. 2 L 7 2 4F RT A16WE 2002080900197 20020809 00197 NM 2002 8 9 USA2002F00065 1 20020627 A 3610 7902708 VALVE BOEING 767 7672B7 1385107 NM PRV, RT ENG INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 656US 26847 ENROUTE, CREW RECEIVED THE EICAS MESSAGES (RT ENGINE PRV) AND (RT ENG BLD OVHT). SHORTLY THEREAFTER, THE RIGHT PACK BEC AME INOPERATIVE. THE FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE SHAFT AND BUTTERFLY OF THE RIGHT PRV DISCREPANT. THE VALVE WAS REPLACED. 2 L 7 2 4F RT A1NM 2002081100001 20020811 00001 SO 2002 8 11 C2XA02IA165 1 20020809 A 5610 163500111 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT CRACKED A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 14907 145468 LIT- DURING FLIGHT 3588, IN CRUISE THE CREW NOTED THAT THE LEFT WINDSHIELD OUTER PANE CRACKED,THE CREW DECLAIRED EMERGE NCY, AND, LANDED AT LIT WITHOUT INCIDENT. LIT- MAINTENANCE REMOVED AND REPLACED THE LEFT WINDSHIELD, PERFORMED A OPERA TIONAL CHECK, AND, A LEAK CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002081100002 20020811 00002 SO 2002 8 11 C2XA02IA166 1 20020809 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO TAIL INOPERATIVE A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 15910 145455 IAH- DURING TAKEOFF THE CREW NOTED THAT THE RUDDER SYST, 2 WAS INOP., AND ABORTED THE TAKEOFF WITHOUT INCIDENT. MAINTE NANCE REMOVED AND REPLACED THE RUDDER #2 PRESSURE SWITCH, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002081100003 20020811 00003 SO 2002 8 11 C2XA02IA167 1 20020809 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO TAIL INOPERATIVE A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 15910 145455 IAH- DURING TAKEOFF THE CREW NOTED THAT THE RUDDER #2 SYSTEM WAS INOPERATIVE,AND, ABORTED THE TAKEOFF. IAH- MAINTENAN CE REMOVED AND REPLACED THE RUDDER #1 PRESSURE SWITCH, PERFORMED A OPERATIONAL CHECK,NO DEFECTS NOTED,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002082700091 20020827 00091 NM 2002 8 27 DHL2002721500 1 20020805 A 5320 FLOOR SUPPORT BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK, DISCREPANCY AS FOLLOWS, CRACK IN FLOOR SUPPORT UNDER (FWD) COCKPIT ENTRY FLOOR BETWEEN DOOR AND MANUAL E XTENSION PANELS. REMOVED CRACK FLOOR SUPPORT FROM COCKPIT FLOOR BETWEEN ENTRY DOOR AND MANUAL EXT PANELS IAW B-727 SRM 51-30-2. FABRICATED NEW FLOOR SUPPORT IAW B-727 SRM 53-10-2 AND 53-40-3. INSTALLED NEW FLOOR SUPPORT IAW B-727 SRM 51- 30-2. 2 L 7 3 4F RT A3WE 2002081200001 20020812 00001 CE 2002 8 12 AUS20020772 1 20020704 A 3260 ICH16 SWITCH CESSNA 404 404CESSNA 2075901 CE CONT O520 GTSIO520M 17032 SO MCAULY 3FF32 3FF32C501 GL NLG OUT OF ADJUST W O OTHER N FALSE WARNING CL CLIMB 1 AU S (AUS) NOSE LANDING GEAR SWITCH OUT OF ADJUSTMENT. 1 L 7 2 3O 3 O A25CE E7CE 5 C P45GL 2002081200002 20020812 00002 NM 2002 8 12 AUS20020773 1 20020728 A 2730 162700100 COMPUTER BOEING 737 737800* NM GE CFM56 CFM567B24 NE ELEVATOR CONTROL CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ELEVATOR FEEL COMPUTER INTERNAL S126 SWITCH FAILED. SUSPECT CAUSED BY CONTAMINATION FROM FAILURE OF NR 1 ENGINE DR IVEN HYDRAULIC PUMP. SEE MDR 02/0732. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002081200003 20020812 00003 EA 2002 8 12 AUS20020778 2 20020720 A 8530 CYLINDER PARTEN P68 P68B 6780104 EU LYC O360 IO360A1B6 41514 EA HARTZL HCC2Y HCC2YK2 GL RT ENGINE MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) RT ENGINE NR 2 CYLINDER INLET VALVE PUSHROD BROKEN. SHROUD TUBE SEVERELY DISTORTED. METAL IN OIL FILTER. INVESTIGA TION FOUND THE FOLLOWING DEFECTS: NR 1 CYLINDER HAD ONE INLET AND ONE EXHAUST ROCKER ARM INSTALLED BUT THE INLET WAS IN STALLED IN THE EXHAUST POSITION AND VISA VERSA. NR 2 CYLINDER HAD TWO INLET ROCKER ARMS INSTALLED. NR 3 CYLINDER HAD TH E SAME SET UP AS NR 1 CYLINDER (ONE OF EACH BUT TRANSPOSED). NR 4 CYLINDER HAD TWO EXHAUST ROCKER ARMS INSTALLED. 1 H 7 2 3O 3 O A31EU 1E10 5 C P920 2002081200004 20020812 00004 NE 2002 8 12 CA020517004 2 20020516 A 7313 3038495X NOZZLE PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL FUEL SYSTEM CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) REPLACEMENT SET OF ENGINE FUEL NOZZLES WERE RECEIVED FROM P&W ACCESSORIES SERVICES TO REPLACE A PREVIOUSLY RECEIVE D U/S SET OF EXCHANGE FUEL NOZZLES. PACKING AGAIN APPEARED NORMAL. ONE FUEL NOZZLE ASSY. WAS FOUND TO BE VISIBLY CONTAM INATED AND DISCOLORED. P&W WAS AGAIN CONTACTED TO REPLACE THE NOZZLE IN QUESTION. COMPANY MAINTENANCE DIRECTOR & QA INFO RMED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002081200005 20020812 00005 EU 2002 8 12 CA020627001 1 20020608 A 6720 350A33105803 BELLCRANK SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACK FOUND AFTER INSPECTION ON T/R BELLCRANK. THE CRACK IS ON THE WEB OF THE SHORT ARM OF THE BELLCRANK. THE TS N OF THE BELLCRANK IS FROM THE AIRFRAME TIME. 1 G 7 1 3U 3 U H9EU E19EU 2002081200006 20020812 00006 SW 2002 8 12 CA020708006 1 20020524 A 6230 206010452113 SUPPORT BELL 206 206B 1181511 SW MAIN ROTOR MISMANUFACTURED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) SUPPORT FOUND TO HAVE MACHINING MARK ABOVE BASE OF SUPPORT. THIS SUPPORT WAS NEW CONDITION AND HAD NOT BEEN PLACED IN SERVICE. 1 G 7 1 3U H2SW 2002081200007 20020812 00007 SW 2002 8 12 CA020708007 1 20020524 A 6230 206010452113 SUPPORT BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL MAIN ROTOR MISMANUFACTURED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) SUPPORT FOUND TO HAVE MACHINING MARK ABOVE BASE OF SUPPORT. THISSUPPORT WAS NEW CONDITION AND HAD NOT BEEN PLACED IN SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 2002081200008 20020812 00008 SW 2002 8 12 CA020708008 1 20020524 A 6230 206010452113 SUPPORT BELL 206 206B3 1181506 SW MAIN ROTOR MISMANUFACTURED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) SUPPORT P/N 206-010-452-113 FOUND TO HAVE MACHINING MARK ABOVE BASE OF SUPPORT. THIS SUPPORT WAS NEW CONDITION AND HAD NOT BEEN PLACED IN SERVICE. 1 G 7 1 3U H2SW 2002081200009 20020812 00009 2002 8 12 CA020712002 4 20020712 A 2210 ST472 SERVO DHAV DH60 DH60G GL AUTOPILOT WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AS PART OF PRE-FLT FUNCTION AUTOPILOT IS ENGAGED & SERVOS ARE MECHANICALLY OVERRIDDEN. IT INITAILLY DISCOVERED BY MAINT PERSONNEL THAT WERE WEAR MARKS ON THE PITCH SERVO CAPSTAN COVER. MAINT TESTING DISCOVERED THAT SLACK IN PRIMAR Y PITCH CABLE CAUSED BY OVERRIDING PITCH SERVO CAUSING CABLE TO DROOP OVER CABLE GUIDE & HOOK UP ON GUIDE SCREW HEAD. C ABLE WOULD RIDE UNDER SCREW HEAD, ON CAPSTAN COVER, UNTIL SUFFICIENT FORCE MOVED CABLE BACK INTO PROPER ALIGNMENT.2 A/C WITH AUTOPILOT INST SUBSEQUENTLY HAD PITCH SERVOS REMOVED & AUTOPILOT DISABLED PENDING FURTHER INVESTIGATION. 1 Q 7 1 3I NC EXPA1Q71 2002081200010 20020812 00010 CE 2002 8 12 CA020722002 1 20020704 A 5260 5043003115 BELLCRANK BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA AIRSTAIR DOOR BENT W K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 CA (CAN) DOOR, FWD UPPER HOOK BELLCRANK FOUND TO HAVE A BENT SHAFT, AND ARMS TO BE APPROX 45 DEGREES ANGLE TO EACH OTHER - DOOR, AFT UPPER HOOK BELLCRANK FOUND TO HAVE A BENT SHAFT WITH NOT SO SEVERE ANGLE OF DIS-AUGMENT WITH ARM ANGLES APPROX 80 DEG. TO EACH OTHER. SHAFTS SHOULD BE STRAIGHT AND ARMS 90 DEG. TO EACH OTHER.THIS INSPECTION OCCURED AFTER FLIGHT CR EW REPORTED DIFFICULTY IN OPENING / CLOSING THE AIRSTAIR DOOR. 1 L 7 2 4T 4 T A24CE E4EA 2002081200011 20020812 00011 EU 2002 8 12 CA020722003 1 20020721 A 2997 BNK12F1203SD CONNECTOR AIRBUS 310 A310300 3930305 EU GE CF6 CF680C2A5 NE HYD POWER BURNED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING PREDEPARTURE CHECK, IT WAS NOTICED THAT THE NR 2 ENGINE GREEN HYDRAULIC PUMP LOW PRESSURE LIGHT ON THE OVER HEAD PANEL, WAS NOT ON. IT WAS FOUND THAT NR 2 GREEN HYDRAULIC PUMP CONNECTOR FIN DV213 WAS BADLY BURNED AND THAT THE P INS WERE HEAVILY CORRODED. THE CONNECTOR AND PINS WERE REPLACED, SYSTEM WAS TESTED PER MAINTENANCE MANUAL AND CHECKED SE RVICEABLE, AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A35EU E13NE 2002081200012 20020812 00012 NM 2002 8 12 CA020722004 1 20020709 A 3297 ACCESSORY UNIT BOEING 737 737248 1384402 NM PWA JT8 JT8D9A 52048 NE MLG FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) THE AIRCRAFT DEPARTED ON TAKE OFF THE GEAR LEVER WOULD NOT TRAVEL PAST SAFETY SOLENOID. THE AIRCRAFT DIVERTED TO Y OW AND LANDED WITHOUT INCIDENT. MAINTENANCE INVESTIGATED, AND REMOVED AND CLEANED THE EDGE CONNECTORS OF THE LANDING GEA R ACCESSORY UNIT CIRCUIT BOARDS. THE AIRCRAFT WAS SYSTEM CHECKED ON THE GROUND IAW MM REF. 32-31-31 AND FLOWN TO VERIFY SYSTEM FOR CORRECT OPERATION BEFORE RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002081200014 20020812 00014 CE 2002 8 12 CA020722006 1 20020702 A 2916 511700712 SIGHT TUBE CESSNA 414 414A 2075907 CE CONT O520 TSIO520NB 17040 SO MCAULY 3AF32C 3AF32C505 GL HYD RESERVOIR FAILED W H DEACTIVATE SYST/CIRCUITS K FLUID LOSS AP APPROACH 1 CA (CAN) SUSPECT HYDRAULIC FLUID OVERHEATED AND MELTED RESERVOIR SIGHT TUBE. HYDRAULIC RESERVOIR THEN LEAKED ALL FLUID OVER BOARD, THROUGH OPEN SIGHT TUBE PORTS. PILOT DEACTIVATED NORMAL HYDRAULIC SYSTEM, AND USED EMERGENCY BLOW DOWN SYSTEM TO LOCK LANDING GEAR DOWN AND LANDED - NORMALLY. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2002081200015 20020812 00015 GL 2002 8 12 CA020722008 1 20020708 A 5544 2055450300 SUPPORT BRACKET DIAMON DA20 DA20C1 2990001 GL CONT O240 IO240B 17063 SO SNSNCH W69EK W69EK63 EA RUDDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) RUDDER SUPPORT BRACKET DEVELOPED CRACKS ON THE WELD. 1 L 7 1 3O 3 O NT TA4CH E7SO 5 N TA4CH 2002081200016 20020812 00016 NE 2002 8 12 CA020722009 2 20020704 A 7322 25244405 FUEL CONTROL PIPER PA31T PA31T2 7103127 SO PWA PT6 PT6A135 52043 NE LT ENGINE FAILED W E ENGINE SHUTDOWN E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA (CAN) ON START UP, THE LEFT ENGINE STARTED ACCELERATING OUT OF CONTROL, REGARDLESS OF POWER LEVER POSITION. THE CONDITIO N LEVER WAS THEN PULLED AND THE ENGINE SHUT DOWN. THE FUEL CONTROL UNIT (FCU) WAS REPLACED WITH AN OVERHAULED UNIT AND A SATISFACTORY RUN UP WAS CARRIED OUT. FUEL CONTROL UNIT P/N 2524440-5, S/N A74932 1 L 7 2 3T 4 T RT A8EA E4EA 2002081200017 20020812 00017 2002 8 12 CA020722010 4 20020710 A 6122 582855 HOUSING LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE PROP VALVE DAMAGED W E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA (CAN) ENROUTE YUX FROM YUW NR 4 ENGINE WOULD NOT SYNC. PRECAUTIONARY SHUTDOWN ACCOMPLISHED. MAINTENANCE REPLACED THE PRO P VALVE HOUSING, AIRCRAFT GROUND CHECKED AND RETURNED TO SERVICE. 2 H 7 4 4T 4 T A1SO E282 6 C P906 2002081200019 20020812 00019 GL 2002 8 12 CA020722014 2 20020719 A 7210 685029 GEARBOX LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE NR 2 ENGINE MAKING METAL W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) ENROUTE THE NR 2 ENGINE REDUCTION GEARBOX CHIP LIGHT ILLUMINATED. PRECAUTIONARY SHUTDOWN ACCOMPLISHED. MAINTENANCE FOUND A SMALL METALLIC SLIVER ON SIDE MAGNETIC PLUG. MAINTENANCE CLEANED AND REINSTALLED PLUGS, GOUND RUN CARRIED OUT B EFORE RETURN TO SERVICE. 2 H 7 4 4T 4 T A1SO E282 6 C P906 2002081200021 20020812 00021 WP 2002 8 12 CA020722016 1 20020704 A 6210 500P2100101 BLADE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACK IN LOWER SKIN DISCOVERED AT STN 36.5. BLADE REMOVED FROM SERVICE. FURTHER ANALYSIS OF THE BLADE REVEALED THA T THE CRACK STARTED AT THE FIRST LIGHTENING HOLE OF THE "C" CHANNEL AND MOVED TO LOWER SKIN. THE CRACK THEN RAN LATERALL Y TO THE TE AND TOWARD THE LE. THE "V" CHANNEL AT THE TE HAD CRACKED LONGITUDINALLY FOR APPROX 2 INCHES. FURTHER ANALYSI S REVEALED SURFACE PITS WERE DETECTED ON THE INNER RADIUS OF THE LIGHTENING HOLE. THESE PITS WERE ANODIZED, INDICATING T HAT THESE PITS WERE FORMED DURING THE CONSTRUCTION PROCESS. 1 G 7 1 3U 3 U H3WE E4CE 2002081200022 20020812 00022 CE 2002 8 12 CA020722017 1 20020721 A 2612 302157 DETECTOR BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA NR 1 ENGINE MALFUNCTIONED W E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA 11506 11506 (CAN) CREW REPORTED NR 1 ENGINE FIRE WARNING ILLUMINATED IN FLIGHT. AIRCRAFT HEADING CHANGED AND WARNING STILL ILLUMINAT ED. EMERGENCY CALL MADE AND ENGINE SHUT DOWN IN FLIGHT. NR 1 ENGINE FORWARD UPPER FLAME DETECTOR REPLACED WITH NEW. GROU ND FUNCTION CHECKED. NO FURTHER FAULTS NOTED. 1 L 7 2 4T 4 T A24CE E4EA 2002081200023 20020812 00023 CE 2002 8 12 CA020723001 1 20020626 A 3211 169110001223 BRACKET BEECH 23 A24R 1151252 CE LYC O360 IO360A1A 41514 EA MCAULY 2D34C 2D34C9 GL MLG UPLOCK MECH CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON VISUAL INSPECTION OF THE LT WHEEL WELL, THE ANGLE HOLDING THE UPLOCK HOOK BRACKET WAS IDENTIFIED AS BEING HEA VILY CORRODED, SHOWING SIGNS OF ADVANCED EXFOLIATION CORROSION. UPON DISASSEMBLY, INTERGRANULAR CORROSION WAS ALSO FOUND ON THE UPLOCK HOOK BRACKET, AT THIS MATING SURFACE WITH THE ANGLE. 1 L 7 1 3O 3 O A1CE 1E10 5 C P7EA 2002081200024 20020812 00024 CE 2002 8 12 CA020723002 1 20020626 A 2750 1695240483 ARM BEECH 23 A24R 1151252 CE LYC O360 IO360A1A 41514 EA MCAULY 2D34C 2D34C9 GL TE FLAPS WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FLAPS WERE FOUND TO BE LOOSE. AFTER INVESTIGATION IT WAS FOUND THAT THE FLAP ARMS THAT JOIN THE FLAP CONTROL TUBE TO THE FLAP RODS HAD ELONGATED BOLT HOLES DUE TO WEAR. THE ELONGATED HOLES ARE THE ONES WHERE THE CLEVIS BOLTS ATTACH TH E ARMS TO THE FLAP CONTROL TUBE. BOTH FLAP ARMS WERE FOUND WITH APPROXIMATELY THE SAME CONDITION. 1 L 7 1 3O 3 O A1CE 1E10 5 C P7EA 2002081200025 20020812 00025 CE 2002 8 12 CA020723003 1 20020626 A 2750 HANDLE BEECH 23 A24R 1151252 CE LYC O360 IO360A1A 41514 EA MCAULY 2D34C 2D34C9 GL TE FLAP CONTROL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FLAP HANDLE PEDESTAL IS CRACKED AT BEND ON LOWER RT FORWARD CORNER. 1 L 7 1 3O 3 O A1CE 1E10 5 C P7EA 2002081200026 20020812 00026 NE 2002 8 12 CA020723004 2 20020630 A 7300 BRH10113 SHAFT BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE ENGINE DAMAGED W D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 CA (CAN) GATE RETURN DUE TO ENGINE AUTO-SHUTDOWN. CUSTOMER REPORTED FAULT CODES 732133&732128. DURING FAULT ISOLATION, IT N OTED THAT OVERSPEED SHUTOFF CABLE SAGGING. ROTATING FAN BY HAND DID CAUSE LP TURBINE TO ROTATE, HOWEVER, IT MADE RATCHE TY NOISE. REMOVAL OF TAIL CONE REVEALED THAT SHUTOFF CABLE WRAPPED AROUND LP TURBINE SHAFT BREAKAGE SENSING MECHANISM & THAT MECHANISM IN 35 DEG (FAILED) CONDITION. INVESTIGATION. AT RRC REVEALED THAT SHAFT, FUEL CUT OFF DRIVE SPLINES WERE MISASSEMBLED WITH TUBE REF FSO SPLINES. SPLINES WERE NOT ENGAGED & BOTH PART WERE TORQUED TOGETHER. AFTER FEW HRS OF RUN NING, SPLINES ENGAGED INTO THEIR LOCATION MAKING LP TURBINE ASSEMBLY LOOSE WHICH ACTIONED FUEL SHUTOFF MECH. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002081200027 20020812 00027 CE 2002 8 12 CA020723005 1 20020626 A 5514 MS244625 BEARING BEECH 23 A24R 1151252 CE LYC O360 IO360A1A 41514 EA MCAULY 2D34C 2D34C9 GL HORIZONTAL STAB CORRODED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) WHEN INSPECTING CONTROL SURFACES, IT WAS NOTICED THAT THE HORIZONTAL STABILATOR HAD AN ABNORMAL FORE / AFT MOVEMEN T. UPON DISINSTALLATION, THE HORIZONTAL STAB BUSHINGS AND BEARINGS WERE FOUND TO BE WORN AND THE BOLTS WERE FOUND TO BE CORRODED. 1 L 7 1 3O 3 O A1CE 1E10 5 C P7EA 2002081200028 20020812 00028 NM 2002 8 12 CA020723007 1 20020629 A 5312 BULKHEAD BOEING 727 727116C 1384046 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 51926 51926 (CAN) DURING A ROUNTINE STRUCTURAL 1500 HOUR INSPECTION THE FOLLOWING CRACKS WERE FOUND. B.S. 178 PRESSURE BULKHEAD WL 166.5 RBL 5.5. 2 L 7 3 4F 4 F RT A3WE E2EA 2002081200029 20020812 00029 WP 2002 8 12 IXXA0200044O 1 20020709 A 3230 UPLOCK DOUG DC8 DC871F 302199D WP LT MLG STICKS A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 821BX 82570 2580 45811 EN ROUTE FROM RFD TO TOL, THE LANDING GEAR UPLATCH CHECK FAILED AND THE LANDING GEAR UNSAFE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR SEVERAL TIMES BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURE S AND THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE LEFT MAIN LANDING GEAR UP LATCH MECHANISM STICKING. MAINTENANCE CLEANED AND LUBED THE MECHANISM AND PERFORMED SUCCESSFUL OP ERATIONAL CHECKS IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002081200030 20020812 00030 NE 2002 8 12 CA020724003 3 20020526 A 6111 BLADE DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE HAMSTD 2D 2D30 NE PROPELLER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PROP WAS SLOW TO CYCLE THROUGH HIGH PITCH. PROP INSPECTED & HUB FOUND CRACKED ABOUT 6 INCHES LONG AROUND NR 1 BLAD E SHANK. PROP SENT TO HOPE AERO FOR OVERHAUL. 1 H 7 1 3R 3 R A806 5E1 5 C P206 2002081200031 20020812 00031 CE 2002 8 12 CA020724004 1 20020607 A 3246 D30656 WHEEL CESSNA 172 172N 2072434 CE LYC O320 O320H2AD 41508 EA MCAULY 1C160 1C160DTM GL MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) 2 OUTBOARD WHEEL HALFS FOUND CRACKED AROUND BOLTS (CRACKS MAYBE CAUSED BY OVERTORQUE). 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 2002081200034 20020812 00034 WP 2002 8 12 IXXA0200045O 1 20020629 A 3260 0080004002 CONTROL BOX DOUG DC8 DC863 302198A WP MLG DEFECTIVE A IXXA O OTHER N FALSE WARNING CL CLIMB 1 SW 11 786AL 84148 2577 46121 EN ROUNT FROM TOL TO LAX, THE LANDING GEAR DOOR NOT LATCHED LIGHT ILLUMINATED FOLLOWING LANDING GEAR RETRACTION. THE FL IGHT CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT FOLLOWED COMPANY PROCEDURES AND CONT INUED TO LAX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED A DEFECTIVE PROXIMITY SWITCH CONTROL BOX AND SENSOR. MAINTENANCE REPLACED THE PROXIMITY CONTROL BOX AND SENSOR AND PERFORMED SUCCESSFUL OPERATIONAL CHECKS IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002081200035 20020812 00035 SO 2002 8 12 CA020724009 2 20020713 A 7322 MA45 FLOAT CESSNA 185 185 2072802 CE CONT O520 IO520D 17032 SO MCAULY 2A34C D2A34C58 GL CARBURETOR LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE CONDUCTING A ROUTINE VISUAL INSPECTION PRIOR TO COWLING INSTALLATION, A SPACE WAS NOTED BETWEEN BOTH HALVES OF THE CARBURETOR OF APPROX 1/32 INCHES. FURTHER INSPECTION REVEALED THAT ALL FLOAT BOWL ATTACHMENT SCREWS WERE FOUND L OOSE. ALL SCREWS WERE RE-TORQUED AND LOCKING TABS WERE ADJUSTED TO POSITIVELY LOCK ALL SCREW HEADS. IT IS RECOMMENDED TH AT SPECIAL ATTENTION SHOULD BE GIVEN TO THIS AREA FOR LOOSE SCREWS OR A LOOSE FLOAT BOWL, LEAKAGE, ETC. AND ALL SCREWS C HECKED FOR PROPER TORQUE AT A 50 HOUR INTERVAL. 1 H 7 1 3O 3 O NC 3A24 E5CE 5 C P3EA 2002081200038 20020812 00038 NM 2002 8 12 CA020724011 1 20020721 A 2830 DUMP VALVE DHAV DHC8 DHC8301 1386003 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE FUEL SYSTEM STICKING W K NONE O OTHER IN INSP/MAINT 1 CA 28500 28500 (CAN) AFTER REFUELLING, LT DUMP VALVE WOULD NOT CLOSE. AIRCRAFT REPOSITIONED VIA FERRY FLIGHT PERMIT TO LOCATION WHERE L T DUMP VALVE WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002081200039 20020812 00039 2002 8 12 P5CA0200686 4 20020630 A 2210 AUTOPILOT SYS BOEING 747 747249F 1384849 NM COCKPIT MALFUNCTIONED A P5CA K NONE O OTHER UK UNKNOWN 1 WP 23 806FT 21827 B-AUTOPILOT WILL NOT ACCEPT STEERING COMMANDS IN HDG OR INS MODE. ALSO INOP IN MANUAL. TRANSFERRED TO DEFERRED MX ITEM . 2 L 7 4 4F A20WE 2002081200040 20020812 00040 SW 2002 8 12 CA020724013 1 20020723 A 6230 214040125101 BEARING BELL 412040366115 BELL 412 412 1182202 SW MAST SPALLED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA A466 (CAN) MAST REMOVED FOR TRANSMISSION CHIP INDICATIONS. BEARING FOUND SPALLED ON REMOVAL. 1 G 7 2 4U H4SW 2002081200041 20020812 00041 SW 2002 8 12 CA020724014 1 20020723 A 6230 204040309101 NUT BELL 412040366115 BELL 412 412 1182202 SW MAST LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA A466 (CAN) ON REMOVAL OF MAST LOWER MAST BEARING RETENSION NUT FOUND WITH NO TORQUE. BEARING RACE NOT SEATED. 1 G 7 2 4U H4SW 2002081200042 20020812 00042 NM 2002 8 12 P5CA0200687 1 20020627 A 4910 DOOR BOEING 747 747249F 1384849 NM APU CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 A 2 INCH LONG CRACK FOUND ON APU INLET DOOR OUTSIDE LOWER FORWARD CORNER. COMPOSITE REPAIR CARRIED OUT WITH REF TO SRM 51-40-06. AREA PROTECTED WITH REF TO SRM 51-21-01. 2 L 7 4 4F A20WE 2002081200043 20020812 00043 NE 2002 8 12 P5CA0200689 2 20020629 A 7520 SHROUD BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 702225 CRACKS FOUND ON NR 1 ENG TURBINE COOLING SHROUD AT 8 & 2 O'CLOCK POSITIONS. RT (2 CRACKS) NR 1 IS 5 INCHES LONG & NR 2 IS 2 INCHES LONG. LT (4 CRACKS) NR 1 IS 3 INCHES LONG, NR 2 IS 5 INCHES LONG, NR 3 IS 1.5 INCH LONG & NR 4 IS 1.5 INCH LONG. ALSO BRACKET HAS A 1 INCH LONG CRACK. NR 1 ENG TCC MANIFOLD WELD REPAIRED IAW P&W STD PRACTICES 70-42-01 USING A MS 5832 FOR INCONEL. 2 L 7 4 4F 4 F A20WE E3NE 2002081200044 20020812 00044 EA 2002 8 12 CA020725001 1 20020713 A 2110 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ACM BAY MALFUNCTIONED W E D ENGINE SHUTDOWN RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) QUOTE FROM MAINTENANCE CONTROL LOG: "CPT REPORTS THAT ON TAXI OUT SMOKE STARTED FILLING UP CABIN, A/C WAS EVAC TH ROUGH A/S/D ON TAXIWAY, NO EXITSWERE PULLED. PER CPT NO WARNING OR FAULTS NOTED IN COCKPIT." NO FIRE EXTINGUISHERS WERE UTILIZED. LOCAL MAINTENANCE FOUND THE RIGHT PACK WAS UNCONTROLLABLE. IT WENT TO OVERTEMP CONDITION WHEN TURNED ON. THE P ACK WAS DEFERRED TO FLY THE AIRCRAFT TO ATL. IN ATL, THE RIGHT ACM WAS REPLACED. OPS CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002081200045 20020812 00045 NM 2002 8 12 P5CA0200690 1 20020629 A 4980 6513987052 ACOUSTIC PANEL BOEING 747 747249F 1384849 NM APU DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 APU EXHAUST ACOUSTIC LINER DAMAGED AT 01:30 O'CLOCK POSITION. APU LINER REMOVED & REPLACED IAW MM 49-81-02. 2 L 7 4 4F A20WE 2002081200048 20020812 00048 CE 2002 8 12 CA020725008 1 20020712 A 5346 045100336 MOUNT CESSNA 150 152 2071835 CE LYC O235 O235L2C 41505 EA ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 14169 (CAN) ON INSPECTION (100 HOUR) ENGINE MOUNT WAS FOUND CRACKED AT LOWER RIGHT TUBE AT NOSE OLEO MOUNTING. THE ENGINE WAS REMOVED AND THE MOUNT REPLACED. THE ENGINE WAS RE-INSTALLED AND GROUND RUN SERVICEABLE. THE AIRCRAFT WAS RETURNED TO SER VICE. 1 H 7 1 3O 3 O NT 3A19 E223 2002081200049 20020812 00049 NE 2002 8 12 CA020725009 2 20020602 A 7200 ENGINE BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE NR 1 FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING D E INFLIGHT SEPARATION VIBRATION/BUFFET CL CLIMB 1 CA (CAN) ON DEPARTURE FROM OTTAWA, CLIMBING THROUGH FL 270 TO 280, A LOUD BANG WAS HEARD AND A SHUDDER CAME FROM NR 1 ENG INE, POWER WAS REDUCED AND ENGINE WAS SHUT DOWN, OTHER THAN FLUCTUATING VIBRATION, OTHER PARAMETERS NORMAL.NUMBER ONE E NGINE REPLACED. MORE INFORMATION WILL FOLLOW WHEN ENGINE REPORT AVAILABLE. 2 L 7 2 4F 4 F A16WE E2EA 2002081200050 20020812 00050 CE 2002 8 12 CA020725010 1 20020712 A 2730 AN16322RS PIN CESSNA 180 180A 2072604 CE CONT O470 O470L 17026 SO MCAULY 2A34C 2A34C203 GL ELEVATOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PILOT NOTICED INCREASING VAGUENESS IN ELEVATOR CONTROL AND LANDED ASAP. UPON CLOSE EXAMINATION TURN BARREL AND PI N EYE HAD SEPARATED CAUSING VAGUENESS IN CONTROL SAFETY WIRE WAS HOLDING PARTS TOGETHER, TURN BARREL HAD FRACTURED AT BA RREL END. THE ABOVE WAS MARKED BY THE SAFETY WIRE AND THE ANTI-CORROSION MATERIAL GREASE ETC. BOTH EYES WERE CHANGED RE TENSION, CABLES, RESAFETY AND GIVEN FRESH ANTI-CORROSION TREATMENT. HIGHLY RECOMMEND THAT ALL SALT WATER OPERATORS OF C1 80, C185 REMOVED AND INSPECT THESE COMPONENTS AS SOON AS POSSIBLE. AS SALT WATER CORROSION HAPPENS SO QUICKLY. 1 H 7 1 3O 3 O 5A6 E273 5 C P3EA 2002081200051 20020812 00051 EU 2002 8 12 CA020725011 1 20020721 A 3260 404HE996 SQUAT SWITCH FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU MLG FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) T/O WAS REJECTED AT APPROX 60/70 KNOTS DUE TO T/O WARNING HORN ASSOCIATED WITH A GPW CAUTION LIGHT AND STICK SHAKE R. LT AND RT SQUAT SWITCHES REPLACED. AIRCRAFT TEST FLOWN SATISFACTORY. 2 L 7 2 4F 4 F RT A20EU E2EU 2002081200052 20020812 00052 NM 2002 8 12 CA020725012 1 20020605 A 3230 273T62013 BRACE BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE MLG ACTUATOR SHEARED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKE OFF. LT MLG WOULD NOT RETRACT, EICAS GEAR DISAGREE DOOR LIGHT AND GEAR LIGHT ON. AIRCRAFT RETURNED TO AIRPORT. FOUND LT BEAR SIDE BRACE LOCK ACTUATOR PISTON SHAFT SHEARED. REPLACED ACTUATOR AND SYSTEM CHECKED NORMAL 2 L 7 2 4F 4 F RT A1NM E3NE 2002081200053 20020812 00053 2002 8 12 P5CA0200693 4 20020702 A 3441 7886580011A2 INU BOEING 747 747283B 1384867 NM COCKPIT FAILED A P5CA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 23 921FT 21575 DOUBLE INS FAILURE WHILE EN ROUTE. NR 3 INS HAD WARNING LIGHT, ACTION CODE 02, MALFUNCTION CODE 56 - BECAME 35 MILES OF F TRACK (CODES CLEARED) NR 3 INS HAD RED WARNING LIGHT, ACTION CODE 01, MALFUNCTION CODES 13, 31, 34, 35, 36, 42, 50 & 6 2. F/O'S ADI RED FLAG. INS TURNED OFF. REMOVED & REPLACED BOTH NR 3 & 2 INS NAV UNITS. OPS CHECK ON BOTH UNITS NORMA L PER MM 34-41-03. 2 L 7 4 4F A20WE 2002081200055 20020812 00055 NM 2002 8 12 PCAA0207078 1 20020720 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST NR NOT REPORTED 1 EA 13 820EX 019 LGA-FLIGHT 3971. CREW REPORTED ALL FLOOR LEVEL EMERGENCY LIGHTS BEYOND ROW 3 ARE INOPERATIVE. MAINTENANCE RESECURED FL OOR EMERGENCY LIGHT STRIPS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081200056 20020812 00056 NM 2002 8 12 PCAA0207079 1 20020720 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST NR NOT REPORTED 1 EA 13 851EX 343 PIT-FLIGHT 3597. CREW REPORTED EMERGENCY EXIT PLACARD ABOVE FLOOR LEVEL EXIT BACK LIGHTING BURNED OUT. MAINTENANCE REC ONNECTED CANNON PLUG BEHIND SIGN AND RELAMPED 4 BULBS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081200057 20020812 00057 NM 2002 8 12 PCAA0207082 1 20020729 A 2910 O-RING DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM CUT A PCAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 13 808EX 299 MDT-FLIGHT 3963. CREW REPORTED LOSS OF HYDRAULIC SYSTEM AND NR 1 QUANTITY IN FLIGHT WITH RUDDER ISOLATION VALVE LIGHT, FOLLOWED SHORTLY AFTER NR 1 HYDRAULIC PUMP, NR 1 HYDRAULIC PRESSURE, RUDDER PRESSURE AND FULL RUDDER PRESSURE LIGHTS ILL UMINATED. ZERO QUANTITY IN SYSTEM, RAN FOR APPROXIMATELY 14 MINUTES. MAINTENANCE INSPECTED AND FOUND CUT O-RING ON NR 1 CASE DRAIN FILTER ASSEMBLY. PACKING REPLACED. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081200058 20020812 00058 SO 2002 8 12 RAIA00206178 1 20020512 A 5320 14522188003 FITTING EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 804HK 145082 BLK CK - CORROSION ON FLOORBOARD STRINGER AT CBL BETWEEN FRAMES 15 AND 18. REMOVED AND REPLACED T-SHAPE IAW SRM 51-40-0 2. 2 L 7 2 4F RT T00011AT 2002081200059 20020812 00059 EU 2002 8 12 RAIA00206192 1 20020619 A 3350 CONNECTOR AEROSP ATR42 ATR42300 8680920 EU CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 423TE 119 5619-STL- CABIN DOOR EMERGENCY EXIT LIGHT INOP. CLEANED CONNECTOR AT CABIN DOOR EMERGENCY EXIT LIGHT, OPS OK. 2 H 7 2 4T RT A53EU 2002081200061 20020812 00061 EU 2002 8 12 RAIA00207207 1 20020709 A 3350 CONNECTOR AEROSP ATR42 ATR42300 8680920 EU CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 423TE 119 MX-STL- EMERGENCY LIGHT AT BOTTOM OF STAIRS INOP. CLEANED CONNECTOR AT LIGHT ASSY, OPS CHECK OK. 2 H 7 2 4T RT A53EU 2002081200062 20020812 00062 NM 2002 8 12 SQ7A062002 1 20020126 A 5315 FLOORBEAM BOEING 727 727251 138408H NM FUSELAGE CORRODED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - DURING SCHEDULED MAINTENANCE THE FLOORBEAM AT BS 1166, WL 208.1, & LBL 11 WAS FOUND CORRODED. REPAIRED PER SRM 53 -10-8, FIG 8. 2 L 7 3 4F A3WE 2002081200064 20020812 00064 NM 2002 8 12 CA020726001 1 20020613 A 3246 32300541 TIRE BOEING 747 747433 NM PWA 4056 PW4056 NE MLG FAILED W O OTHER O OTHER LD LANDING 1 CA (CAN) ON LANDING AT FRANCFORT, NR 2 TIRE DESINTEGARATED, AND LEFT INBOARD FLAP TRAILING EDGE DAMAGED. NR 1 AND 2 WHEEL S CHANGED AND FLAP REPAIRED 2 L 7 4 4F 4 F RT A20WE E24NE 2002081200065 20020812 00065 NM 2002 8 12 CA020726003 1 20020715 A 5320 654581945 GUSSET BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) 2.5 INCH CRACK IN CENTER OF GUSSET (GUSSET TOTAL LENGTH 10.5 INCHES). VISIBLE ALONG INSIDE RADIUS. REF SDA AL-2002 -03TAT 57540.8 HRLDG 55883 2 L 7 2 4F 4 F A16WE E2EA 2002081200066 20020812 00066 NM 2002 8 12 SQ7A072002 1 20020202 A 5320 FITTING BOEING 727 727251 138408H NM FUSELAGE CORRODED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - DURING SCHEDULED MAINTENANCE CORROSION WAS FOUND ON T-EXTRUSION AT BS 820 - 850, RBL 10, WL 138.5, BELOW A/C BAY. REPAIRED PER SRM 51-10-1. 2 L 7 3 4F A3WE 2002081200067 20020812 00067 NM 2002 8 12 CA020726004 1 20020715 A 5320 654581945 GUSSET BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) 2.5 INCH IN CRACK IN CENTRE OF GUSSET (GUSSET TOTAL LENGTH 10.5 INCHES).VISIBLE ALONG INSIDE RADIUS.REF SDA AL-200 2-03TAT: 54113.9 HR. LDG: 52167 2 L 7 2 4F 4 F A16WE E2EA 2002081200068 20020812 00068 EA 2002 8 12 CA020726006 2 20020716 A 8530 72877 LIFTER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION METAL FOUND IN FILTER, LARGE PARTS FOUND IN FINGER SCREEN. CYLINDER NR 6 DIFFERENTIAL PRESSURE F OUND LOW, CYL REMOVED, FOUND LIFTER BODY FLANGE MISSING. UPON REMOVAL OF ALL CYLINDER ASSEMBLIES, IT WAS NOTED ALL PISTO N SKIRTS WERE MISSING PIECES, CONNECTING RODS SCORED AND GROOVED, CYLINDER ASSEMBLY LOWER FLANGES PEENED AND CASE DAMAGE D INTERNALLY. WHEN LOGS CHECKED AND PILOT QUESTIONED, IT WAS NOTED OIL USAGE AND ALL TEMPS WERE NORMAL FOR TYPE AND ENGI NE WAS OF NORMAL POWER AND NO VIBRATION. IT IS THE SUBMITTERS OPINION THAT THIS POWERPLANT WAS HOURS FROM SELF DESTRUCTI ON. 1 L 7 2 3O 3 O A20SO E14EA 2002081200069 20020812 00069 NM 2002 8 12 SQ7A092002 1 20020202 A 5320 STRUCTURE BOEING 727 727251 138408H NM FUSELAGE CRACKED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - DURING SCHEDULED MAINTENANCE THE UPPER CHORD WAS FOUND CRACKED BETWEEN BS 1263 & 1273 JUST BELOW THE AFT AIRSTAIR ACTUATOR. REPAIRED THE CHORD PER S/B 727-53-0129. 2 L 7 3 4F A3WE 2002081200070 20020812 00070 NM 2002 8 12 SQ7A122002 1 20020124 A 5320 SILL BOEING 727 727251 138408H NM FUSELAGE CORRODED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282 21161 YXD - DURING SCHEDULED MAINTENANCE CORROSION WAS FOUND AT THE R-1 DOOR CUTOUT, LOWER SILL, BS 380 TO 420. REPLACED LOWE R CHORD PER SRM 51-10-1. 2 L 7 3 4F A3WE 2002081200071 20020812 00071 2002 8 12 CA020726007 4 20020617 A 3442 FTN7V6748 INDICATOR BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE WX RADAR FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA (CAN) 30 MINUTES AFTER DEPARTURE, ELECTRICAL BURNING SMELL IN COCPIT, AIRCRAFT LANDED SAFELY, BURNING SMELL ORIGINATED BY WEATHER RADAR INDICATOR. INDICATOR REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 2002081200072 20020812 00072 EU 2002 8 12 CA020726009 1 20020706 A 7603 704A34130052 CONTROL CABLE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE POWER LEVER BROKEN W E ENGINE SHUTDOWN R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET LD LANDING 1 CA (CAN) PILOT MAKES NORMAL LDG AT FIRE BASE CAMP IN PELICAN NARROWS, SASK. PILOT PULLS / RETARDS THROTTLE LEVER & HEARS CL UNK. THROTTLE LEVER IS VERY LOOSE & ENGINE DOES NOT SHUTDOWN, IDLES AT 55 PERCENT NG. THROTTLE LEVER IS UNRESPONSIVE TO ANY POSITIIONS . PILOT RETARDS FUEL SHUT OFF LEVER & SHUTS DOWN ENGINE.UPON INVEST. THEY NOTICE FCU BALL CABLE INNER POR TION AT THREADED ENDS IS SHEARED OFF. ENGINEER ARRIVES & DETERMINES THAT AREA WHERE CABLE BROKE HAS BEEN 75 PERCENT CRAC KED FOR WHILE DUE TO STRESS AT UPPER HOLE OF LEVER. MWC "CAUTIONS" THAT UPPER HOLE BE USED. MWC 760000502282 FIG.2. LOW ER HOLE TESTED W/O STRESS & WERE ABLE TO RIG F.C.U. SAME. 1 G 7 1 3U 3 U H9EU E19EU 2002081200073 20020812 00073 NE 2002 8 12 SQ7A172002 2 20020310 A 7230 FAN BLADE BOEING 727 727251 138408H NM PWA JT8 JT8D17 52049 NE ENGINE CRACKED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 281 21160 IND - DURING SCHEDULED MAINTENANCE CRACKS WERE FOUND IN THE C-1 FAN BLADES NR 13 & NR 16. REMOVED AND REPLACED THE C-1 FAN ASSY. 2 L 7 3 4F 4 F A3WE E2EA 2002081200074 20020812 00074 EA 2002 8 12 CA020726010 1 20020617 A 2742 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE MACH TRIM FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) MACH AND STAB TRIM MESSAGE ON CLIMB, PROCEDED WITH STAB TRIM 1 INOPERATIVE, FAULT DISAPEARED, AUTOPILOT ENGAGED, FLT CREW DISENGAGED A/P AT 10,000 FT, FOR MANUAL LANDING, EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REPLACED HOR IZONTAL STAB TRIM ACTUATOR, OPERATION CHECKED NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2002081200075 20020812 00075 NM 2002 8 12 SWAA021695 1 20020729 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 EEPLS DAMAGED AT MID CABIN. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002081200076 20020812 00076 NM 2002 8 12 SWAA021696 1 20020726 A 2761 654456115 ACTUATOR BOEING 737 7372H4 138448C NM SPOILER FAILED A SWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 29 073SW 22673 DURING FINAL APPROACH, NR 6 SPOILER REMAINED EXTENDED. REMOVED AND REPLACED NR 6 SPOILER ACTUATOR PER MM. 2 L 7 2 4F A16WE 2002081200078 20020812 00078 NE 2002 8 12 GTIA020521 2 20020518 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE RIGHT LEAKING A GTIA O OTHER K FLUID LOSS CL CLIMB 1 GL 23 810NK 48015 696450 FLL - FLT 9810 - LEVEL AT 5000 FEET RIGHT ENGINE WENT FROM 65 PERCENT N1 TO 110 PERCENT, EPR WENT TO 2.30 EGT 670 NO CON TROL OVER ENGINE WITH POWER LEVER. DURING INITIAL RUN AFTER INSTALLING ENGINE FOUND FUEL LEAKING FROM COLD STREAM INTO REVERSER. REMOVED AND REPLACED ENGINE IAW 71-00-00 ON ENGINE RUN FOUND FUEL LEAK IN COLD STREAM. REMOVED AND REPLACED NR 2 ENGINE. RUN CHECK AND LEAK CHECK OK. (M) 2 L 7 2 4F 4 F A6WE E9NE 2002081200079 20020812 00079 NM 2002 8 12 MEX2002216 1 20020709 A 2121 731376A FAN BOEING 757 7572Q8 1384972 NM CABIN MALFUNCTIONED A ASMF C ABORTED TAKEOFF J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 23 802AM 26270 FLT 490 - MEX-LAX - CAPTAIN ABORTED TAKEOFF, RADAR FAILED, OVERHEAT LIGHT WAS ON AND BURNING SMELL WAS DETECTED. DURING CHECK RADAR AND EICAS MESSAGES WERE OK AND BURNING SMELL DISAPPEARED. AIR CONDITIONING PACKS, TRIM VALVES WERE CHECKED , ALL OK. AIRCRAFT WAS SENT TO THE HANGAR. LEFT SUPPLY FAN WAS REPLACED IAW MM 21-58-06, LOW FLOW SENSORS TS5155 AND T S5156 WERE REPLACED IAW MM 21-58-17, RADAR WAS CHECKED IAW MM 34-43-00, NO FAILS WERE FOUND. (M) 2 L 7 2 4F RT A2NM 2002081200080 20020812 00080 NM 2002 8 12 MEX2002217 1 20020711 A 7930 42D109 SWITCH DOUG MD88 MD88 3023688 NM RT ENGINE MALFUNCTIONED A ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 169PL 53175 MID-MEX - FLT 526 - CAPTAIN ABORTED TAKEOFF, OIL STRAINER CLOGGING LIGHT CAME ON. DURING REVISION WAS DETECTED CHIP DET ECTOR AND RIGHT MAIN OIL FILTER WITH CARBON RESIDUES. THEY WERE DRAINED AND CLEANED. RIGHT ENGINE RUNNING TEST WAS ACC OMPLISHED IAW MM 79-20-08/71-00-00. DURING OVERNIGHT SERVICE THE RIGHT MAIN OIL FILTER WAS CHANGED AND THE RESTRICTORS WERE CLEANED IAW MM 79-20-00. ADDITIONALLY THE SWITCH WAS CHANGED IAW MM 79-33-01 AND PERFORMANCES TESTS WAS ACCOMPLISH ED TO THE APU. (M) 2 L 7 2 4F RT A6WE 2002081200081 20020812 00081 SO 2002 8 12 SIMA200217304 1 20020617 A 5320 STRUCTURE EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - FOUND NUMEROUS SMALL GOUGES JUST INBOARD OF WASTE SERVICE ACCESS PANEL AT FRAMES 60 AND 61 AND STRINGERS 20R AND 2 1R. GOUGES BLENDED, PERFORMED NDT, NO DEFECTS, ACCEPTED AS IS IAW EMB GST-1999/02. SURFACE PROTECTION RESTORED. (M) 2 L 7 2 4T RT T00011AT 2002081200082 20020812 00082 SO 2002 8 12 SIMA200217307 1 20020617 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - THIS IS A LEVEL 2 FINDING. PASSENGER DOOR ENTRY FLOORBOARD SUPPORT HAS CORROSION. PERFORMED NDT, NO DEFECTS. FL OOR SUPPORTS FOUND TO BE WITHIN EMB 145-21-10 LIMITS. (M) 2 L 7 2 4T RT T00011AT 2002081200083 20020812 00083 SO 2002 8 12 SIMA200217308 1 20020619 A 5320 14525381003 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 THIS IS A LEVEL 2 FINDING, LAVATORY CENTER BEAM GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 S RM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002081200084 20020812 00084 SO 2002 8 12 SIMA200217309 1 20020617 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - FOUND ONE DENT MARKED NR 3 AFT OF PAX DOOR LOWER CORNER AT FRAMES 19 AND 20 AND STRINGER 15L AND 16L. ALSO FOUND CRACK. REMOVED DAMAGE BY CUT OUT, FABRICATED A REPAIR DOUBLER AND FILLER, REPAIR DONE IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 18 53-21-01, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002081200085 20020812 00085 NE 2002 8 12 CA020726013 2 20020716 A 7200 ENGINE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE LEFT FAILED W E ENGINE SHUTDOWN D INFLIGHT SEPARATION TX TAXI/GRND HDL 1 CA 12122 (CAN) DURING WALKAROUND PILOTS NOTICED GRINDING NOISE COMING FROM LT ENGINE. MAINTENANCE WAS CALLED TO INVESTIGATE. GR INDING NOISE WAS COMING FROM POWER SECTION AREA. OIL FILTER WAS CHECKED AND FOUND TO BE CONTAMINATED WITH METAL CHIPS. ENGINE WAS REMOVED AND SENT TO OVERHAUL SHOP FOR TEAR DOWN AND REPAIR. 2 H 7 2 4T 4 T A41EU E4EA 2002081200086 20020812 00086 SO 2002 8 12 SIMA200217310 1 20020617 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - FOUND ONE DENT AFT OF PASSENGER DOOR ON EMB PLACARD AT FRAME 19 AND 20 AND STRINGER 14L AND 15L. PERFORMED NDT, N O DEFECTS, DENT ACCEPTED AS IS IAW EMB GST-1999/02. (M) 2 L 7 2 4T RT T00011AT 2002081200087 20020812 00087 SO 2002 8 12 SIMA200217311 1 20020617 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - FOUND GOUGE BETWEEN FRAMES 28/29 AND STRINGERS 17R/18R. BLENDED GOUGES, PERFORMED NDT, NO DEFECTS. ACCEPTED AS I S IAW EMB GST-1999/02, SURFACE PROTECTION RESTORED. (M) 2 L 7 2 4T RT T00011AT 2002081200088 20020812 00088 SO 2002 8 12 SIMA200217312 1 20020617 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - FOUND GOUGE AT FRAME 63/64 AND STRINGERS 19L AND 20L JUST BELOW AND FORWARD OF CARGO DOOR CUTOUT. BLENDED GOUGES, PERFORMED NDT, NO DEFECTS, ACCEPTED AS IS IAW EMB GST-1997/02, SURFACE PROTECTION RESTORED. (M) 2 L 7 2 4T RT T00011AT 2002081200089 20020812 00089 SO 2002 8 12 SIMA200217313 1 20020617 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - FOUND GOUGE WITH DENT AT FRAME 66 AND 67 BELOW CARGO DOOR AREA AND STRINGERS 18L AND 20L. BLENDED GOUGE, PERFORME D NDT, NO DEFECTS. ACCEPTED AS IS IAW EMB GST-1997/02, SURFACE PROTECTION RESTORED. (M) 2 L 7 2 4T RT T00011AT 2002081200090 20020812 00090 SO 2002 8 12 SIMA200217314 1 20020617 A 5210 STRUCTURE EMB 145 EMB145LR 3260212 SO PAX DOOR GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - FOUND PASSENGER DOOR IS GOUGED IN TWO PLACES. PERFORMED NDT INSPECTION AND FOUND NO DEFECTS. REPAIR DONE IAW EMB GST-2005/02. (M) 2 L 7 2 4T RT T00011AT 2002081200091 20020812 00091 SO 2002 8 12 SIMA200217315 1 20020617 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - THIS IS A LEVEL 2 FINDING, RIGHT CENTER SILL HAS CORROSION. REMOVED CORROSION BY BLENDING, FILLED WITH EPOXY RESI N AND SANDED. FABRICATED A REPAIR DOUBLER, REPAIR DONE IAW ETN-53-036, FIG 5, AND STANDARD SRM PRACTICES. M) 2 L 7 2 4T RT T00011AT 2002081200092 20020812 00092 SO 2002 8 12 SIMA200218301 1 20020702 A 2120 ODOR EMB 145 EMB145LR 3260212 SO COCKPIT DETECTED A SIMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 649PP 145234 ORD - FLT 4334 - CREW REPORTED A RUBBER ODOR IN MAIN CABIN AND COCKPIT IN FLIGHT. SHUT OFF GASPER AND RECIRCULATION FAN S AND ODOR DECREASED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. PERFORMED GROUND OPERATIONAL CHECK OF APU AND AIRCR AFT BLEED SYSTEMS AND DETECTED NO ODOR. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002081200093 20020812 00093 SO 2002 8 12 SIMA200218401 1 20020628 A 5310 WINDOW FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - MAINTENANCE FOUND LEFT WINDSHIELD CUT OUT STRUCTURE HAS 15 CORRODED HOLES. REMOVED CORROSION BY REAMING/BOLT HOLE S. FABRICATED FREEZE PLUGS. REPAIR DONE IAW EMB GST-2022/02, ITEM 9 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002081200094 20020812 00094 SO 2002 8 12 SIMA200218402 1 20020628 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - MAINTENANCE FOUND CORROSION ON GALLEY CENTER FLOORBEAM. REMOVED CORRODED GALLEY CENTER BEAM. INSTALLED SERVICEAB LE BEAM IAW EMB 145 SRM 145/1142, CHAPTER 51, REV 18 51-40-02, AEA ETN EM-53-028 R1, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002081200095 20020812 00095 SO 2002 8 12 SIMA200218403 1 20020701 A 5311 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - DURING AN IMBV MAINTENANCE, FOUND FRAME 72 DENTED AND BENT AT SPLICE JOINT ABOVE FLOOR ON LEFT SIDE OF CARGO. REM VOED FRAME 72 SPLICE CHANNEL. RECONTOURED DENT. PERFORMED NDT AND FOUND NO DEFECTS. FABRICATED TWO DOUBLER ANGLE, REP AIR DONE IAW EMB GST-2022/02-A, ITEM 7, GST-2075/02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002081200096 20020812 00096 SO 2002 8 12 SIMA200218404 1 20020628 A 5311 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - DURING AN IMBV INSPECTION FOUND DENT ON FRAME 67 BETWEEN STRINGER 14R AND 15R. RECONTOURED DENT PERFORMED NDT AND FOUND NO DEFECTS. FABRICATED TWO DOUBLERS ANGLES, REPAIR DONE IAW EMB GST-2022/02-A ITEM 5, AND STANDARD SRM PRACTICES . (M) 2 L 7 2 4T RT T00011AT 2002081200097 20020812 00097 SO 2002 8 12 SIMA200218405 1 20020628 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - MAINTENANCE FOUND CORROSION ON FORWARD DIGITAL. REMOVED CORROSION BY CUT OUT. FABRICATED A REPLACEMENT STRAP AND TWO DOUBLERS. REPAIR DONE IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 18 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002081200098 20020812 00098 SO 2002 8 12 SIMA200218406 1 20020628 A 5320 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - MAINTENANCE FOUND CORROSION ON LEFT OMEGA BEAM PREVIOUS REPAIR AT FRAME 20. REMOVED PREVIOUS REPAIR, CORROSION LI MITED TO PREVIOUS REPAIR. FABRICATED DOUBLER, PLATE, AND SHIMS. REPAIR DONE IAW EMB 145 SRM 145/1142 CHAPTER 53, REV 1 8 53-21-01, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002081200099 20020812 00099 SO 2002 8 12 SIMA200218407 1 20020628 A 5320 14510634002 CLIP EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND SHEAR CLIP CRACKED ON FRAME 81 AT THE 2 O'CLOCK POSITION. REMOVED DAMAGE SHEAR CLIP. INSTALLED SERVICEABLE CLIP IAW EMB GST-2022/02A, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002081200100 20020812 00100 SO 2002 8 12 SIMA200218408 1 20020628 A 5310 WINDOW FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - MAINTENANCE FOUND RIGHT WINDSHIELD CUT OUT STRUCTURE HAS 25 CORRODED HOLES. REMOVED CORROSION BY REAMING BOLT HOL ES. FABRICATED FREEZE PLUGS. REPAIR DONE IAW EMB GST 2022/02, ITEM 9 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002081200101 20020812 00101 SO 2002 8 12 SIMA200218409 1 20020628 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - MAINTENANCE FOUND CARGO DOOR LOWER SILL CORRODED. REMOVED CORRODED SILL BEAM. INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 145/1142, CHAPTER 51 REV 18 51-20-03, 51-40-02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002081200102 20020812 00102 SO 2002 8 12 SIMA200218410 1 20020628 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 ABI - DURING IMBV INSPECTION MAINTENANCE, FOUND THE CARGO DOOR LOWER SILL CORRODED. REMOVED CORRODED SILL BEAM. INSTAL LED NEW BEAM IAW EMB145 SRM 145/1142, CHAPTER 51, REV 18 51-20-01, 02, 03, 04, AND 06 CPM 51-21-04 AND 05 AND STANDARD S RM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002081200103 20020812 00103 NE 2002 8 12 CA020726014 2 20020715 A 8530 356996 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE HAMSTD 43E 43E60 NE NR 4 ENGINE CRACKED W E A ENGINE SHUTDOWN UNSCHED LANDING D J INFLIGHT SEPARATION WARNING INDICATION CR CRUISE 1 CA (CAN) WHILE ENROUTE TO A FIRE THE FLIGHT CREW HAERD A LOUD BANG FROM NR 4 ENGINE. THE CREW SHUT DOWN THE ENGINE AND FEA THERED THE PROP. THE AIRCRAFT RETURNED TO YZH. MAINTENANCE CREW DISCOVERED A CRACKED EAR ON THE NR 13 CYLINDER. THE CY LINDER WAS REPPLACED WITH A SERVICEABLE ASSY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4R 4 R 6A3 5E8 6 C P871 2002081200104 20020812 00104 SW 2002 8 12 CA020726015 1 20020605 A 5320 206031314037 CHANNEL BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL FUSLEAGE CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A 100 HOUR INSPECTION UPPER LT CHANNEL LOCATED ON REAR OF FUSELAGE WHERE TAILBOOM ATTACHES TO FUSELAGE. CH ANNEL FOUND TO HAVE CRACK PRETUDING FROM A RIVET HOLE. CHANNEL WAS REMOVED AND REPLACED NEW. 1 G 7 1 3U 3 U H2SW E1GL 2002081200105 20020812 00105 EA 2002 8 12 CA020726016 2 20020708 A 7200 FADEC BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA LT ENGINE FAILED W O OTHER Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CA (CAN) WHILE EN ROUTE LT ENGINE SHUT ITSELF DOWN. AIRCRAFT CONTINUED TO DESTINATION AND MADE UNEVENTFUL SINGLE ENGINE LAN DING. TROUBLESHOOTING ISOLATED FADEC ON LT ENGINE AS BEING DEFECTIVE. FADEC IS NOW BEING INVESTIGATED. TSN 3002.4 HRS F ADEC 370.12 HRS ON LEFT HAND ENGINE, 1394:06 SINCE OVERHAUL. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002081200106 20020812 00106 SO 2002 8 12 CA020726018 2 20020708 A 8530 ST711ER CYLINDER CESSNA 180 180K 2072624 CE CONT O520 O520* SO MCAULY D3A34 D3A34C403 GL ENGINE CRACKED W A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA (CAN) AT END OF 2 RT FLT, CYL HEAD TEMP, OIL TEMP & PRESSURE ALL NORMAL. OIL TEMP SUDDENLY WENT UP ONE NEEDLE WIDTH, OIL PRESSURE WENT DOWN ONE NEEDLE WIDTH. ENGINE MADE BANGING, CLATTERING NOISE WITH WHIFF OF HOT OIL SMOKE IN COCKPIT. E NGINE RAN VERY ROUGH, SO PILOT BROUGHT POWER BACK & NOISE LESSENED WITH STILL SOME CLATTER. PILOT MADE "ALL STATIONS" CALL & LANDED IN SHEBANDOWAN LAKE. PILOT ABLE TO IDLE ENGINE TO SHORE: (AT IDLE NO BANGING OR CLATTERING NOISE.) A/C L EFT TIED UP AT PRIVATE BEACH NEAR COTTAGE & DOCK. PILOT NOTIFIED DIR. OF MAINT IMMEDIATELY BY PHONE. UPON INSP, NR 1 CYL INDER FOUND CRACKED FROM LOWER SPARK PLUG HOLE, & FOLLOWED CYLINDER FINS HALF WAY AROUND CYLINDER. 1 H 7 1 3O 3 O 5A6 E5CE 5 C P47GL 2002081200108 20020812 00108 EA 2002 8 12 CA020729007 2 20020716 A 7414 M3100 IMPULSE COUPLING SLICK 4372 ZLIN 242 Z242L 9970204 EU LYC O360 AEIO360A1B6 41514 EA MAGNETO LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 94110059 (CAN) WHILE INSPECTING A MAGNETO, THE IMPULSE COUPLING WAS REMOVED, INSPECTED AND WAS FOUND TO HAVE A LOOSE FIT BETWEEN THE IMPULSE PAWL MOUNTING PLATES AND THE IMPULSE HUB. DUE TO TWO PREVIOUS CATASTROPHIC FAILURES OF IMPULSE COUPLINGS. THE IMPULSE COUPLING WAS REMOVED FROM SERVICE. THIS IMPULSE COUPLING HAD ONLY 141.4 HRS SINCE NEW. SLICK SB1-98 AND SB 2-80C WERE CARRIED OUT ON THE IMPULSE COUPLING AND NO DEFECTS WERE EVIDENT ON THE IMPULSE PAWLS. NOTE THAT NEITHER SB1- 98 NOR SB2-80C REQUIRE A CHECK FOR CONDITION OF FIT BETWEEN IMPULSE PAWL MOUNTING PLATES AND THE IMPULSE HUB. AN EXTENS IVE REPORT WAS ATTACHED TO SDR C-FVWH (APR 15, 2002) DESCRIBING OUR FINDINGS ON THE TWO PREVIOUS FAILURES. 1 L 7 1 3O 3 O 0 A76EU 1E10 2002081200111 20020812 00111 EA 2002 8 12 CA020731011 1 20020723 A 2730 22D1174A CONTROL CABLE SCWZER SG2 SGS233A 8051606 EA ELEVATOR FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) RT ELEVATOR CABLE FOUND FRAYED AT P/N 22A148-1 FAIRLEAD. 1 K 0 0 G2EA 2002081200112 20020812 00112 EA 2002 8 12 CA020731012 1 20020723 A 2730 22D1175A CONTROL CABLE SCWZER SG2 SGS233A 8051606 EA ELEVATOR FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ELEVATOR CONTROL CABLE FOUND FRAYED AT P/N 22A148-1 FAIRLEAD. 1 K 0 0 G2EA 2002081200113 20020812 00113 GL 2002 8 12 CA020731018 1 20020716 A 8011 958856 SPRAG CLUTCH DIAMON DA20 DA20A1 2990000 GL ROTAX 912 ROTAX912S2 EU IGNITION HOUSING WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ENGINE WOULD NOT START. (100HP 912S) PROP WOULD KICK BACK AT COMPRESSION STROKE AND MAKE METALLIC NOISE AS IT DID SO. SPRAG CLUTCH WAS VISUALLY INSPECTED AND APPEARED FINE. IT WAS REPLACED ANYWAY AND PROBLEM WAS CURED. 1 L 7 1 3O 3 O NT TA4CH E00051EN 2002081200114 20020812 00114 EU 2002 8 12 CA020801012 1 20020724 A 6520 350A33020005 BEVEL GEAR SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D1 NE TAILROTOR DRIVE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) TAILROTOR GEARBOX BEVEL GEAR - LOSS OF TORQUE ATTACHING IT TO THE OUTPUT DRIVE SHAFT - ALL THE BOLTS WERE LOOSE CA USING EXTREME BACKLASH IN GEAR SET. FOUND DURING GEARBOX REMOVAL/INSTALLATION. THE INPUT PINION, OUTPUT BEVEL GEAR, OUT PUT SHAFT ALL SCRAPED. 1 G 7 1 3U 3 U H9EU E19EU 2002081200115 20020812 00115 EU 2002 8 12 CA020801013 1 20020724 A 5412 350A5801100802 FIREWALL SNIAS 350 AS350BA 8680817 EU LYC LTS101 LTS101600A3 41560 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) A CRACK WAS FOUND ON FIREWALL DURING MAINTENANCE OPERATION. LENGTH OF CRACK 3.75 PO. AN ENGINE AIR FILTER KIT HAS RECENTLY BEEN INSTALLED AS PER STC SH02-22 BASED ON FAA APPROVED STC: SR01049SE. A PART OF THIS MODIFICATION CONSIST O F INSTALLATION A DIFFERENTIAL PRESSURE SWITCH MOUNTED ON THE FIREWALL. THE CRACK IS LOCATED JUST ABOVE THIS PRESSURE SWI TCH. NOTE THAT THIS KIT HAS BEEN INSTALLED SINCE 160 HOURS AIR TIME. 1 G 7 1 3U 3 U NC H9EU E5NE 2002081200116 20020812 00116 NE 2002 8 12 CA020802002 2 20020706 A 8530 AE92181 CYLINDER HEAD DHAV DHC3 DHC3 2800202 EA PWA R1340 R134059 52016 NE HAMSTD 23D 23D40 NE ENGINE FRACTURED W A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 CA (CAN) HEAD FRACTURED AND SEPARATED AT APPROXIMATELY THE FIRST THREAD IN THE HEAD. THE CYLINDER HAS BEEN FORWARDED TO TH E MANUFACTURER OF THE CYLINDER FOR FURTHER INVESTIGATION. 1 H 7 1 3R 3 R A815 5E2 6 C P719 2002081200117 20020812 00117 EU 2002 8 12 CA020803001 1 20020731 A 6321 PISTON DUNLOP AH43881 BOLKMS 117 BK117B2 5626013 EU ROTOR BRAKE FAILED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION LD LANDING 1 CA (CAN) AT SHUT DOWN OF THE HELICOPTER THE PILOT REPORTED A SQUEALING NOISE FROM THE AREA OF THE TRANSMISSION. ON INVESTI GATION IT WAS FOUND THAT THE ROTOR DISK HAD DISCOLORED AND HAD WARPED FORWARD. FURTHER INVESTIGATION REVEALED THAT THE REAR PAD PISTON HAD NOT RETRACTED FAR ENOUGH SINCE ITS LAST APPLICATION. THE PAD SHOWED SIGNS OF HEAT BUT THERE WERE NO OTHER INDICATIONS LOCATED ON THE CALIPER 1 G 7 2 3U NC H13EU 2002081200118 20020812 00118 GL 2002 8 12 EVAS91003 2 20020105 A 7200 BLADE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2* GL COMPRESSOR DAMAGED W QOCF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 03 16107 48546 704721 DURING TAKE OFF, NR 3 ENGINE HIGH EGT & HPC STALL. REPLACED NR 3 ENGINE, ON GROUND FOUND SEVERAL BLADES & STAGE NR 6 SEV ERE DAMAGE OF COMPRESSOR. 2 L 7 3 4F 4 F RT A22WE E23EA 2002081200119 20020812 00119 NM 2002 8 12 EVAS91004 1 20020201 A 7100 HMU BOEING 747 74745E 1384947 NM GE CF6 CF680C2B2 30025 NE NR 1 ENGINE FAILED W QOCF E C ENGINE SHUTDOWN ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 WP 03 1643 27174 704102 DURING TAKE OFF, NR 1 ENGINE LOW N2 THEN FLAME OUT. ON GROUND REPLACED EEC & HMU, OPR CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E13NE 2002081200120 20020812 00120 NM 2002 8 12 EVAS91015 1 20020806 A 3250 TILLER BOEING 767 76735H 1385208 NM NLG STEERING FAILED W QOCF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 03 16605 26064 TILLER STEERING RIGHT ONLY DURING TAXI, REPLACED NLG STEERING METERING VALVE & RIGGING & OPR CHECKED NORMAL. 2 L 7 2 4F RT A1NM 2002081200121 20020812 00121 EA 2002 8 12 2002FA0000957 2 20020726 A 8530 75068 EXHAUST VALVE PIPER PA18 PA18150 7101828 SO LYC O320 O320* 41508 EA NR 3 CYLINDER FRACTURED B BIGA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 04 116BH 1961 1961 188041 RL1917427A AIRCRAFT EXPERIENCED PARTIAL LOSS OF POWER DUE TO FAILURE OF NR 3 CYLINDER EXHAUST VALVE. AIRCRAFT TERMINATED FLIGHT AND LANDED WITHOUT FURTHER INCIDENT. 1 H 7 1 3O 3 O 1A2 E274 2002081200125 20020812 00125 EU 2002 8 12 02141308 1 20020521 A 3397 PIN BAG JETSTM JETSTM4112 EU ELEC CONNECTOR INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 308UE 41023 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE PERSON NEL SECURED A LOOSE PIN IN THE CONNECTOR FOR THE EXIT SIGN. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 4T RT A196 2002081200134 20020812 00134 NM 2002 8 12 SWAA021697 1 20020728 A 2910 65C26841 FUSE BOEING 737 7373H4 1384600 NM HYD SYSTEM MALFUNCTIONED A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 29 388SW 26591 AIR TURN BACK, AFTER TAKEOFF, LEADING EDGE DEVICES FAILED TO RETRACT. RESET B-SYSTEM L/E DEVICE HYD FUSES PER MM. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2002081200135 20020812 00135 2002 8 12 SWAA021702 4 20020730 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002081200136 20020812 00136 NM 2002 8 12 SWAA021704 1 20020729 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (3 EA), BS 887 AT STR 4L, BS 727A AND STR 25L AND BS 727B AT STR 25R. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002081200137 20020812 00137 NM 2002 8 12 SWAA021705 1 20020730 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (5 EA), BS 380 AT STR 22L, BS 500D AT STR 19R, BS 500D AT STR 19L , BS 807 AT STR 26R AND BS 500D AT STR 21R. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002081200138 20020812 00138 NM 2002 8 12 SWAA021709 1 20020731 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED A1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EXIT LIGHT ASSY P ER MM. 2 L 7 2 4F A16WE 2002081200139 20020812 00139 NM 2002 8 12 SWAA021710 1 20020730 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 EEPLS LOOSE AT ROW NR 13. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002081200140 20020812 00140 NM 2002 8 12 SWAA021711 1 20020730 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 715SW 27849 DURING SCHEDULED C3 CHECK, FOUND EEPLS BROKEN AT ROW'S NR 10 AND NR 11. REMOVED AND REPLACED EEPLS AT ROW'S NR 10 AND N R 11 PER MM. 2 L 7 2 4F RT A16WE 2002081200141 20020812 00141 SO 2002 8 12 SIMA200219101 1 20020706 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 ABI - DURING INSPECTION FOUND STRINGER 19R CHAFED. BLENDED CHAFE, PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER ANGLE, AND TWO SHIMS. REPAIR DONE IAW EMB-145 SRM 145/1142, CHAPTER 53, R EV 18, 53-24-02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002081200142 20020812 00142 SO 2002 8 12 SIMA200219102 1 20020708 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 ABI - FOUND PIT ON STRINGER 4R BETWEEN FRAMES 27 AND 28 TO HAVE A .1875 INCH CRACK ON OUTER EDGE. REMOVED DAMAGE BY CUT OUT. FABRICATED A DOUBLER AND FILLER. REPAIR DONE IAW EMB145 SRM 145/1142, CHAPTER 53, REV 18 53-22-01, GST 2136/02, A ND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002081200143 20020812 00143 SO 2002 8 12 SIMA200219103 1 20020704 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 ABI - DENT BETWEEN FRAMES 20 AND 21 AND STRINGERS 3L AND 4L, 1.6 BY 3 BY .052. PERFORMED EDDY CURRENT INSPECTION, NO DE FECTS. DENT FOUND TO BE WITHIN EMB 145 SRM 53-21-10. (M) 2 L 7 2 4T RT T00011AT 2002081200144 20020812 00144 SO 2002 8 12 SIMA200219104 1 20020704 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE SCRATCHED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 ABI - FOUND SCRATCH BETWEEN FRAMES 29 AND 30, STRINGERS 21L AND 21R. BLENDED AREA, PERFORMED EDDY CURRENT AND THICKNESS , NO DEFECTS. SCRATCH FOUND TO BE WITHIN EMB 145 SRM 53-22-10 TABLE 101 LIMITS. (M) 2 L 7 2 4T RT T00011AT 2002081200145 20020812 00145 SO 2002 8 12 SIMA200219105 1 20020704 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 ABI - FOUND DENTS/SCRAPE BETWEEN FRAMES 19 AND 20 AND STRINGERS 15L AND 16L. BLENDED AREA PERFORMED EDDY CURRENT AND TH ICKNESS, NO DEFECTS. DENT FOUND TO BE WITHIN EMB 145 SRM 53-21-10 TABLES 101 AND 102 LIMITS. (M) 2 L 7 2 4T RT T00011AT 2002081200146 20020812 00146 SO 2002 8 12 SIMA200219106 1 20020704 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 ABI - TWO PROTRUSIONS BETWEEN FRAME 9 AND 10 AND STRINGERS 18L AND 20L, .3 BY .3 BY .001, AND ONE DENT .7 BY .5 BY .002. PERFORMED EDDY CURRENT INSPECTION AND FOUND NO DEFECTS. DENT FOUND TO BE WITH IN EMB145 SRM 53-12-01. (M) 2 L 7 2 4T RT T00011AT 2002081200147 20020812 00147 SO 2002 8 12 SIMA200219107 1 20020704 A 5210 SKIN EMB 145 EMB145LR 3260212 SO PAX DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 ABI - MAIN DOOR HAS ONE DENT AT APPROX 4 INCHES FORWARD OF AFT LOWER CORNER ON EDGE OF SKIN, 9 INCH BY .033 INCH. (M) 2 L 7 2 4T RT T00011AT 2002081200148 20020812 00148 SO 2002 8 12 SIMA200219108 1 20020704 A 5210 SKIN EMB 145 EMB145LR 3260212 SO PAX DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 ABI - FOUND PASSENGER DOOR HAS DENT 10 INCHES FROM TOP AND 2.5 INCHES FROM LEADING EDGE 2 INCHES BY 3 INCHES BY .021 INC H. (M) 2 L 7 2 4T RT T00011AT 2002081200149 20020812 00149 SO 2002 8 12 SIMA200219109 1 20020704 A 4910 SKIN EMB 145 EMB145LR 3260212 SO APU COWLING DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 ABI - FOUND TWO PROTRUSION ON LEFT SIDE OF APU COWL. (M) 2 L 7 2 4T RT T00011AT 2002081200150 20020812 00150 SO 2002 8 12 SIMA200219110 1 20020704 A 5500 SUPPORT EMB 145 EMB145LR 3260212 SO TAIL CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 ABI - FOUND PULLEY SUPPORT ANGLE IS CRACKED ON LEFT END BETWEEN VERTICAL SPARS 3 AND AUX SPAR 52 PERCENT AND BELOW ZV 31 45.0 MM. (M) 2 L 7 2 4T RT T00011AT 2002081200151 20020812 00151 SO 2002 8 12 SIMA200219111 1 20020704 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 ABI - THREE DENTS BETWEEN FRAMES 19 AND 20, STRINGERS 11L AND 12L. (M) 2 L 7 2 4T RT T00011AT 2002081200152 20020812 00152 EU 2002 8 12 SIMA200219301 1 20020712 A 3350 7225280527 SWITCH SAAB SF340 340B 7860101 EU CONTROL PANEL BROKEN A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 344SB 340B344 F/A EMERGENCY LIGHT ARM SWITCH BROKEN. SFP TO LAX FOR REPAIRS. REPLACED FLIGHT ATTENDANTS CONTROL PANEL IAW SAAB 340B MM CHAPTER 25-22-15, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2002081200153 20020812 00153 SO 2002 8 12 SIMA200219602 1 20020715 A 3040 163800111 ELEMENT EMB 145 EMB145LR 3260212 SO COCKPIT FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 644AE 145204 DURING CLIMB CREW REPORTED A SMOKE SMELL IN THE AIRCRAFT. CREW ELECTED TO RETURN TO ORD AND LANDED WITH NO FURTHER INCI DENTS. MAINTENANCE FOUND THE CAUSE OF THE SMELL TO BE FROM THE CAPTAINS WINDSHIELD HEATING ELEMENT. MAINTENANCE REMOVE D AND REPLACED THE CAPTAINS WINDSHIELD HEATING ELEMENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW EM B MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002081200154 20020812 00154 SO 2002 8 12 SIMA200219808 1 20020706 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 ABI - DURING MBV MAINTENANCE, FOUND DENT 3 INCHES FORWARD OF FRAME 20, BELOW STRINGERS 15L. PERFORMED EDDY CURRENT AND THICKNESS CHECK AND FOUND NO DEFECT. DENT TREATED FOR CORROSION AND ACCEPTED AS IS IAW EMB GST-2182/02. (M) 2 L 7 2 4T RT T00011AT 2002081200155 20020812 00155 SO 2002 8 12 SIMA200219809 1 20020706 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 ABI - DURING MBV MAINTENANCE, FOUND A DENT 3 INCH AFT OF FRAME 20, BELOW STRINGER 11L. PERFORMED EDDY CURRENT INSPECTIO N AND FOUND NO DEFECTS. DENT ACCEPTED AS IS IAW EMB GST-2182/02, SURFACE PROTECTION APPLIED. (M) 2 L 7 2 4T RT T00011AT 2002081200156 20020812 00156 SO 2002 8 12 SIMA200219810 1 20020706 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 ABI - DURING MBV INSPECTION MAINTENANCE FOUND A DENT 8 INCH AFT OF FRAME 20, BELOW STRINGER 11L. PERFORMED EDDY CURRENT INSPECTION AND FOUND NO DEFECTS. DENT ACCEPTED AS IS IAW EMB GST-2182/02, SURFACE PROTECTION RESTORED. (M) 2 L 7 2 4T RT T00011AT 2002081200157 20020812 00157 SO 2002 8 12 SIMA200219811 1 20020706 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 ABI - DURING MBV INSPECTION, MAINTENANCE FOUND A DENT BETWEEN FRAMES 17 AND 18 AND STRINGER 21-20L. PERFORMED EDDY CURR ENT INSPECTION AND FOUND NO DEFECTS. DENT FOUND TO BE WITHIN EMB145 SRM 53-21-10, TABLE 102 LIMITS. (M) 2 L 7 2 4T RT T00011AT 2002081200158 20020812 00158 SO 2002 8 12 SIMA200219812 1 20020706 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 ABI - DURING MBV INSPECTION, FOUND A DENT 5.5 INCH AFT OF FRAME 19 BELOW STRINGERS 15L. PERFORMED EDDY CURRENT INSPECTI ON AND THICKNESS TEST AND FOUND NO DEFECTS. (M) 2 L 7 2 4T RT T00011AT 2002081200159 20020812 00159 SO 2002 8 12 SIMA200219813 1 20020706 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 ABI - DURING MBV INSPECTION MAINTENANCE FOUND A DENT 4 INCHES FORWARD OF FRAME 20 BELOW STRINGER 15L. PERFORMED EDDY CU RRENT INSPECTION AND THICKNESS TEST AND FOUND NO DEFECTS. (M) 2 L 7 2 4T RT T00011AT 2002081200160 20020812 00160 SO 2002 8 12 SIMA200220002 1 20020716 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 FOUND STRINGER 19L CHAFED. BLENDED CHAFE, FABRICATED AND INSTALLED TWO DOUBLER ANGLES IAW EMB GST-2182/02, AEA ETN-51-- 020. (M) 2 L 7 2 4T RT T00011AT 2002081200161 20020812 00161 SO 2002 8 12 SIMA200220003 1 20020716 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 ABI - FOUND STRINGER 19R CHAFED. BLENDED CHAFED, FABRICATED AND INSTALLED A DOUBLER ANGLE, IAW EMB 145 SRM 145/1142, CH APTER 53, REV 18 53-24-02, AEA ETN-51-020. (M) 2 L 7 2 4T RT T00011AT 2002081200162 20020812 00162 NM 2002 8 12 TSAA0251066 1 20020226 A 5312 65C28106 BULKHEAD BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 REMOVED CORROSION AT 1016 SKIN BULKHEAD AND ATTACHING FRAME AFT SIDE OF BULKHEAD BETWEEN LBL 5 TO RBL 5 IAW SRM 53-10-1 FIGURE 1 DETAIL 16. CUT OUT ACCESS HOLE AFT OF BULKHEAD PER DRAWING 65C28106. DOUBLER AND FILLER COMPLETED IAW DRAWING 65C28106. CUT OUT DAMAGED PORTION OF WEB AT BULKHEAD 1016 BETWEEN STRINGER 26L AND 26R COMPLETED IAW SB 737-53A1075. ACCESS HOLE FILLER AND DOUBLER INSTALLATION COMPLETED IAW SRM 51-30-2 PAGE 2 PARAGRAPH 4 ITEM A-E. COMPLETED INSTALLATI ON OF RADIAL STIFFENERS, SPLICE AND WEB REPAIR IAW B737 SB 737-53A1075. (M) 2 L 7 2 4F RT A16WE 2002081200163 20020812 00163 NM 2002 8 12 TSAA0253059 1 20020301 A 5532 6550575508 SKIN BOEING 737 7372M6C 1384708 NM VERTICAL STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 FOUND SKIN BULGE ON RIGHT SIDE VERTICAL FIN RIGHT SPAR AT FWL 112.356. FABRICATED REPAIR ANGLE, EXTERNAL DOUBLER, TWO F S 173.10 IN SPAR RIB CLIPS, REPLACEMENT FIN REAR SPAR WEB, SOLID SINGLE GUSSET, SKIN TRIM POUT FILLER AND FLAT FILLERS I AW FIGURES 2A THROUGH 2E. INSTALL ALL REPAIR PARTS AND SHIM GAPS TO .003 INCH MAXIMUM IAW ECO 2509. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002081200164 20020812 00164 NM 2002 8 12 TSAA0253060 1 20020301 A 5531 65474156 SPAR BOEING 737 7372M6C 1384708 NM VERTICAL STAB CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 FOUND CRACK IN THE VERTICAL STABILIZER IN SPAR WEB ON THE VERTICAL STABILIZER. TRIMMED OUT CRACK IAW FIGURE 2. FABRICA TED A REPAIR DOUBLER AND A FILLER AS SHOWN IN FIGURE 2. INSTALLED REPAIR PARTS AND VERIFIED 8110-3 RECEIVED IAW ECO 327 6. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002081200165 20020812 00165 NM 2002 8 12 SWAA021714 1 20020730 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (3 EA) , BS 578 AND BS 706 AT STR 10R, AND BS 663 AT STR 10R. RE MOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002081200166 20020812 00166 NM 2002 8 12 SWAA021717 1 20020731 A 5230 BOE20030038 SEAL BOEING 737 737317 138447P NM CARGO DOOR LEAKING A SWAA G B O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 29 661SW 23173 DURING CRUISE, CABIN ALTITUDE WARNING HORN SOUNDED. DESCENDED TO 11,000 FT, MASKS DID DEPLOY AND WERE USED. REMOVED AN D REPLACED AFT CARGO DOOR PRESS SEAL. RESEALED AFT ENTRY DOOR SCUFF PLATE, RETORQUED AND RESEALED NR 1 COCKPIT WINDOW, CLEANED AFT SVC DOOR UPPER HINGE SEAL. OPS CHECKED GOOD PER MM. 2 L 7 2 4F RT A16WE 2002081200167 20020812 00167 2002 8 12 SWAA021718 4 20020801 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002081200168 20020812 00168 NM 2002 8 12 USAA020263 1 20020612 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 51663 22210 FLOORBEAM, 24 INCH CORRODED AREA. NO LEVEL OR TASK NR. STA 324, RBL 40-64. FABRICATED REPLACEMENT PER SRM AND EA. 2 L 7 2 4F RT A2NM 2002081200169 20020812 00169 NM 2002 8 12 USAA020262 1 20020605 A 5310 BEAM BOEING 767 7672B7 1385107 NM STA325,RBL24,46 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651US 50498 24764 CLT BEAM, 22 INCHES LONG, CORROSION, NO LEVEL OR TASK, STA 325, RBL 24-46. NEW T-CAP AND SPLICE PER SRM. 2 L 7 2 4F RT A1NM 2002081200170 20020812 00170 NM 2002 8 12 GAIA02072OP 1 20020720 A 2910 HYDRAULIC SYSTEM BOEING 727 727251 138408H NM A AND B SYSTEMS FAILED A GAIA K NONE K FLUID LOSS CR CRUISE 1 SW 07 278US 21157 DURING CRUISE THE AIRCRAFT STARTED TO LOOSE BOTH A AND B SYSTEM HYDRAULIC SYSTEM FLUID. BOTH SYSTEMS WERE SECURED AND T HE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED, USING MINIMUM BRAKING AND REVERSE THRUST. THE AIRCRAFT WAS STOPPED ON THE RUNWAY, THE LANDING GEAR WAS PINNED BY MAINTENANCE AND THE AIRCRAFT WAS TOWED CLEAR OF THE RUNWAY. 2 L 7 3 4F A3WE 2002081200171 20020812 00171 NM 2002 8 12 QXEA0201141 1 20020809 A 5270 BUTTON BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 FAILED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 410QX 4053 SEA - DURING CLIMB THROUGH 19K FEET, FUSELAGE DOOR WARNING LIGHT CAME ON. ON DESCENT THROUGH 14K FEET, CABIN PRESSURIZAT ION WAS LOST. CABIN PRESSURE WENT FROM 4 PSI TO O PSI IN A FEW SECONDS. EMERGENCY CHECKLISTS WERE PERFORMED AND THE LAND ING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE REAR CARGO DOOR "PRESS TO RELEASE" BUTTON AND A TTACHED THE SPRING ON THE DOOR LATCHING MECHANISM. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081200172 20020812 00172 SO 2002 8 12 C2XA02BT039 1 20020810 A 3350 AML1317 LIGHT EMB 145 EMB145LR 3260212 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 21537 145523 BTV---CO3389, DURING ROUTINE INSPECTION/CHECK, MAINTENANCE FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHT TO BE INOPERATIV E.....REMOVED AND REPLACED MAIN DOOR FORWARD CABIN CEILING/OVERHEAD EMERGENCY LIGHT IAW EMB145 AMM 33-50-06. OPS. CHECKE D GOOD. 2 L 7 2 4T RT T00011AT 2002081200173 20020812 00173 SO 2002 8 12 C2XA02BT040 1 20020812 A 3350 GE1317 LIGHT EMB 145 EMB145LR 3260212 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 13994 145291 BTV---CO3389, MAINTENANCE FOUND , DURING SERVICE/ROUTINE INSPECTION/CHECK, LEFTHAND WING AFT EMERGENCY LIGHT TO BE INOPE RATIVE IN ALL MODES.....REMOVED AND REPLACED LEFTHAND WING AFT EMERGENCY LIGHT IAW EMB145 AMM 33-50-12. OPS.CHECKED GOOD . 2 L 7 2 4T RT T00011AT 2002081200174 20020812 00174 SO 2002 8 12 C2XA02CL163 1 20020808 A 7933 23073715 SENSOR EMB 145 EMB145ER 3260211 SO #1 ENGINE DEFECTIVE A C2XA A E UNSCHED LANDING ENGINE SHUTDOWN J N WARNING INDICATION FALSE WARNING CL CLIMB 1 SW 27 15941 145035 CLE FLIGHT# 3033 THE CREW REPORTED #1 ENGINE OIL TEMPERATURE WAS HIGH DURING CLIMB.THE ENGINE WAS SHUT DOWN BY THE CREW AND THE AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE #1 ENGINE OIL PRESSURE/TEMPERATURE SENS OR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002081200175 20020812 00175 NM 2002 8 12 SABA020081 1 20020811 A 3350 6104789 BATTERY DHAV DHC8 DHC8103 1386005 NM A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 801WP 086 Flight 5004 on Aircraft 801 From CLT to OAJ : During Pre-Flight the Aircrew could not get the emergency floor lights to test. Maintenance removed and replaced the battery pack and system ops checked good. Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002081200176 20020812 00176 NM 2002 8 12 COOSDR020216 1 20020801 A 5312 BULKHEAD BOEING 727 727232 1384082 NM FUSELAGE CRACKED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 511PE 20634 AFT CARGO COMPARTMENT PRESSURE BULKHEAD, CRACKED. 2 L 7 3 4F A3WE 2002081200177 20020812 00177 NM 2002 8 12 COOSDR020217 1 20020801 A 5751 652176633 SKIN BOEING 727 727232 1384082 NM AILERON DELAMINATED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 511PE 20634 LEFT WING OUTBOARD AILERON TRAILING EDGE DELAMINATED. 2 L 7 3 4F A3WE 2002081200178 20020812 00178 NM 2002 8 12 COOSDR020218 1 20020801 A 5280 65382178 SKIN BOEING 727 727232 1384082 NM NLG DOOR DELAMINATED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 511PE 20634 NOSE LANDING GEAR LEFT AFT DOOR DELAMINATED SKIN. 2 L 7 3 4F A3WE 2002081200179 20020812 00179 EU 2002 8 12 YENA200222 1 20020811 A 2750 ABS012130 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DEFECTIVE A YENA O OTHER J WARNING INDICATION LD LANDING 1 EA 15 531JB 2783 1650 Upon configuration for landing, slats operated normally. Flaps locked at 1. Landed at flap 1 configured slats 3 per FCOM Maintenance removed and replaced interconnecting struct Prox Sensor 39CV IAW MM 27-51-44-400-002 and Ops Tested IAW MM 2 7-51-00-710-002, Ops check normal. 2 L 7 2 4F 4 F RT A28NM E40NE 2002081200180 20020812 00180 NM 2002 8 12 QXEA0201142 1 20020810 A 7930 54273618010 INDICATOR DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 348PH 4144 484 PDX-IN CLIMB NOTICED OIL PRESSURE #2 ENGINE AT 45 PSI. REDUCED NP TO 1050. OIL PRESSURE WENT UP TO 55 PSI. A MINUTE LATE R DROPPED TO 50 PSI. REDUCED POWER TO FLIGHT IDLE. NH WAS STILL ABOVE 75%. CREW DECIDED TO RETURN TO PDX. REMOVED AND RE PLACED #2 OIL PRESSURE TRANSMITTER AND OIL PRESSURE/TEMPERATURE INDICATOR. GROUND RAN ENGINES FOR 10 MINUTES HIGH TO CRU ISE SETTING. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081200181 20020812 00181 NM 2002 8 12 AWXA200200715 1 20020809 A 3350 BMS13311122 WIRE BOEING 757 757225 1384959 NM SEAT ROW 22 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 0 0 22207 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH SEAT LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 22 L/H. MAINTENANCE REPAIRED A BROKEN WIRE SPLICE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 L/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002081200182 20020812 00182 NM 2002 8 12 AWXA200200720 1 20020728 A 5315 654681138 TEE CHORD BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 0 0 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR BEAM (TEE CHORD) BS 986 , RBL 20 - 40. MAINTENANCE REMOVED UPPER TEE CHORD OF FLOOR BEAM BS 986, RBL 3 - 49, FABRICATED 2 EACH SUPPORT ANGLES, 2 EACH STRAPS, 2 EACH SHEAR TIES, 6 CLIPS, AND A NEW UPPER TEE CHORD, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5365-02219 -TB3. 2 L 7 2 4F RT A16WE 2002081200183 20020812 00183 NM 2002 8 12 AWXA200200721 1 20020729 A 5315 654681138 TEE CHORD BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 0 0 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR BEAM (TEE CHORD) BS 986 .5, RBL 3 - RBL 49. MAINTENANCE REMOVED UPPER TEE CHORD OF FLOOR BEAM BS 986.5, RBL 3 - LBL 49, FABRICATED 2 EACH SUPPOR T ANGLES, 2 EACH STRAPS, 2 EACH SHEAR TIES, 6 CLIPS, AND A NEW UPPER TEE CHORD, AND INSTALLED REPAIR PARTS IAW AWA ER 03 -5365-02219-TB3. 2 L 7 2 4F RT A16WE 2002081200184 20020812 00184 NM 2002 8 12 AWXA200200722 1 20020729 A 5315 65468101 TEE CHORD BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 0 0 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR BEAM (TEE CHORD) BS 967 , LBL 18. MAINTENANCE CUTOUT DAMAGED AREA OF UPPER TEE CHORD BS 967, LBL 18, FABRICATED 2 EACH SUPPORT ANGLES, 2 EACH ST RAPS, AND A NEW SECTION OF UPPER TEE CHORD, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-51, PG. 207-211, FIG 202. 2 L 7 2 4F RT A16WE 2002081200185 20020812 00185 NM 2002 8 12 AWXA200200726 1 20020723 A 5330 65457788 SKIN BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 0 0 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1/8" CRACK WAS FOUND ON UPPER FUSELAGE HINGE CUTOUT OF THE R-2 DOOR BS 947, STR 12 R/H. MAINTENANCE CUTOUT DAMAGED SECTION OF SKIN ON R-2 DOOR UPPER FUSELAGE HINGE CUTOUT BS 947, STR 12 R/H. FABRICA TED A DOUBLER AND FILLER, AND INSTALLED REPAIR IAW B737-300 SRM 53-60-01, PG. 210-212. 2 L 7 2 4F RT A16WE 2002081200186 20020812 00186 NM 2002 8 12 02081204 1 20020812 A 5200 PUSHROD BOEING BOEING 757 757236 1384971 NM A N8TA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 19 521NA 25592 Left Center Door EICAS Message/Light appeared in flight. Handle popped up, out of locked position.Adjusted cocking pushr od in accordance with M/M 52-11-00 and 52-11-13. Handle torque test as per M/M 52-11-00 was good. 2 L 7 2 4F RT A2NM 2002081200187 20020812 00187 NM 2002 8 12 02081202 1 20020810 A 2613 CLAMP BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE LOOSE A N8TA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 549NA 24544 30752 Climbing through FL19.0, Left Engine Overheat Message; Reduced Thrust light out. Troubleshoot per F.I.M. 26-11-00, found loose clamp on PRSOV, secured per M/M 20-11-00, All Operations checked per F.I.M. 26-11-00 2 L 7 2 4F 4 F RT A2NM E12EU 2002081200188 20020812 00188 2002 8 12 02081203 4 20020812 A 2565 LANYARD AIRCRUISERS BOEING 757 757236 1384971 NM DISPLACED A N8TA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 19 521NA 25592 Left Entry Door light came on in flight. Visual inspection showed door not fully closed. Interior handle would pop out o f closed detent repeatedly.Found L2 Door Slide Girt/Girt Bar assy. unsecured, reinstalled Girt/Girtbar Assy per M/M 25-6 6-01. L2 Door ops check normal per M/M 52-11-00. Investigation revealed slide lanyard was tangled around Girt bar assy. 2 L 7 2 4F RT A2NM 2002081300021 20020813 00021 SW 2002 8 13 2002FA0000922 1 20020718 A 6230 269A21725 TUBE HUGHES 269 269C1 8059504 SW LYC O360 HO360C1A 41514 EA M/R MAST CRACKED B HIAR K NONE K FLUID LOSS IN INSP/MAINT 1 WP 27 6151L 2629 0087 3617236A TUBE APPEARED TO HAVE A PAINT FLAW. REMOVAL OF PAINT REVEALED A CRACKED TUBE WELD. TUBE REMOVED FROM SERVICE FOR TESTI NG/ INSPECTION BY MANUFACTURER. 1 G 7 1 3O 3 O O 4H12 E286 2002081300022 20020813 00022 SW 2002 8 13 2002FA0000923 1 20020718 A 6230 269A21725 TUBE HUGHES 269 269C1 8059504 SW LYC O360 HO360C1A 41514 EA M/R MAST CRACKED B HIAR K NONE O OTHER IN INSP/MAINT 1 WP 27 20256 1609 0099 L3769536A TUBE APPEARED TO HAVE HAD A CRACK UNDERNEATH THE LUG WELD PRIOR TO COMPLETE FAILURE. THE FAILURE OF THIS TUBE ASSEMBLY CAUSED SEVERE VIBRATION IN AIRCRAFT, RESULTING IN DAMAGE TO MAIN ROTOR BLADES, TAIL ROTOR BLADES, DRIVETRAIN, TAILBOOM A ND CANOPY. 1 G 7 1 3O 3 O O 4H12 E286 2002081300023 20020813 00023 2002 8 13 MWEA020428 4 20020626 A 3160 DISPLAY DOUG DC9 DC981 3022081 WP COCKPIT MALFUNCTIONED A MWEA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 804ME 48030 CAPTAIN REPORTED LOSING BACKGROUND COLORS (BLUE/BROWN) ON CAPTAIN'S PFD & THEN ON FIRST OFFICER'S PFD. CHECKED LEFT AND RIGHT AIR CONDITIONING PACKS FOR LOOSE DUCTS, NONE NOTED. PRESSURIZED CABIN TO CHECK PACK FLOW, EACH PACK WOULD PRESSU RE CABIN ABOVE GPSID SEPARATELY. CLEANED DIVERTED VALVE ASSY. REMOVED, CLEANED AND REINSTALLED COOLING FAN DIVERTER RE F MD80 MM 21-50. 2 L 7 2 4F A6WE 2002081300024 20020813 00024 SW 2002 8 13 2002FA0000924 1 20020722 A 2432 MS24185D1 RELAY GULSTM 690TP 690B 7630516 SW NR 2 BATTERY FAILED B MV5R O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 GL 11 771BA 8624 11429 NR 2 BATTERY MAIN RELAY FAILED CLOSED. THE FAILURE CREATED HEAT DISTRESS AND MELTED THE CONTACTORS WITHIN THE RELAY. 1 H 7 2 3T 2A4 2002081300025 20020813 00025 NE 2002 8 13 SWIA200211067 2 20020725 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RIGHT MALFUNCTIONED A SWIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 NM 07 214SW 120280 RIGHT ENGINE AUTO FEATHERED ON THE TAKEOFF ROLL. ABORTED THE TAKEOFF. PERFORMED TWO TAKEOFF POWER RUNS, ALL CHECKS NOR MAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2002081300026 20020813 00026 2002 8 13 SWIA200211070 4 20020722 A 6122 GOVERNOR EMB 120 EMB120ER 3260203 SO NR 2 ENGINE LEAKING A SWIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 301YV 120301 DURING CRUISE, GOT A TRIPLE CHIME OIL WARNING WITH CORRESPONDING OIL PRESSURE BETWEEN 40-55 PSI ON ENGINE NR 2. COMPLIE D WITH QRH AND FEATHERED ENGINE NR 2. OIL PRESSURE THEN FELL TO APPROXIMATELY 20-30 PSI AND ENGINE NR 2 WAS SHUTDOWN PE R QRH. ALL OTHER ENGINE INDICATIONS WERE NORMAL. FOUND OIL LEAK COMING FROM OVERSPEED GOVERNOR SWITCH ON NR 2 ENGINE. REPLACED OVERSPEED GOVERNOR PER MEL 61-22-01. ALSO REPLACED BAD BREATHER SEAL PER MM 72-20-00. ALL RUNS AND LEAK CHEC K GOOD. OIL LEVEL GOOD AFTER ENGINE RUNS. 2 L 7 2 4T RT A31SO 2002081300027 20020813 00027 2002 8 13 SWIA200211072 4 20020719 A 2216 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 498SW 7483 AFTER LANDING, AILERON TRIM WOULD NOT TRIM TO RWD. TRIMS OK TO LWD. REMOVED AND REPLACED THE AILERON AND RUDDER TRIM C ONTROL PANEL. BOTH SYSTEMS OPERATE NORMALLY. 2 L 7 2 4F RT A21EA 2002081300028 20020813 00028 SO 2002 8 13 SWIA200211073 1 20020718 A 5610 1636004 WINDOW EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 215SW 120281 RIGHT DV WINDOW CRACKED. REMOVED AND REPLACED RIGHT DV WINDOW. PERFORMED LEAK CHECK TO 6 PSI. NO LEAKS NOTED. SERVIC EABLE AT THIS TIME. 2 L 7 2 4T RT A31SO 2002081300029 20020813 00029 2002 8 13 SWIA200211074 4 20020719 A 2210 8220044001 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 597SW 2471 2149 7293 NR 2 YAW DAMPER INOP. REMOVED AND REPLACED FCP IAW 22-11-07. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002081300031 20020813 00031 SO 2002 8 13 SWIA200211075 1 20020718 A 3320 BALLAST EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CABIN DEFECTIVE A SWIA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 235SW 120310 WHILE ON THE GROUND WITH APU ON, SMELLED STRONG SMOKE FROM AFT GALLEY AREA (NO VISUAL SMOKE). SMELLED LIKE BURNING PLAS TIC. SMELL ISOLATED TO GALLEY LIGHT WHICH HAD APPARENTLY BURNED OUT. REMOVED AND REPLACED BALLAST WITH SERVICEABLE UNI T. OPS CHECK GOOD. WHILE ON GROUND WITH APU RUNNING, BURNED WIRE SMELL AND WHITE SMOKE SEEN COMING FROM GALLEY AREA. REPLACED AFT GALLEY LIGHT REACTOR. 2 L 7 2 4T 4 T RT A31SO E20NE 2002081300032 20020813 00032 2002 8 13 SWIA200211078 4 20020719 A 3416 28704E2101 ALTIMETER EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A SWIA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 NM 07 293SW 3039 1070 120320 ON CLIMBOUT, CAPTAIN'S ALTIMETER STUCK AT 1,000 FT, VSI STUCK AT 100 FPM CLIMB, RED FLAGS ON ALTIMETER AND ALTITUDE SELE CTOR, LOST THE TCAS AND MODE C. RETURNED TO PDX. REPLACED CAPTAIN'S ALTIMETER IAW MM 34-11-00. OPS CHECKS/LEAK CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002081300033 20020813 00033 EA 2002 8 13 SWIA200211079 1 20020727 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT DIRTY A SWIA O OTHER N FALSE WARNING DE DESCENT 1 NM 07 916SW 7634 DESCENDING THROUGH 12,000 FT, RECEIVED A RIGHT EMERGENCY DOOR CAUTION MESSAGE. CAUTION SELF CLEARED AT ABOUT 7000 FT (N O CABIN PRESSURE LOSS). CLEANED AND INSPECTED RIGHT EMERGENCY EXIT DOOR PROXIMITY SENSOR. RESECURED DOOR. OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 2002081300034 20020813 00034 EU 2002 8 13 2002FA0000926 1 20020625 A 2150 31552E01 TURBINE AMD FALCON FALCON20 2730103 EU GARRTT TFE731 TFE731* 01518 WP COOLING FAILED D NVIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 15 227WE 29 344 PILOT REPORTED SMOKE IN CABIN MADE EMERGENCY LANDING. MAINTENANCE REPLACED COOLING TURBINE WITH OVERHAULED UNIT. 2 L 7 2 4F 4 F RT A7EU E6WE 2002081300035 20020813 00035 EA 2002 8 13 SWIA200211080 1 20020724 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 589SW 1906 1906 7072 RECEIVED STAB TRIM CH 1 MESSAGE IN FLIGHT. REMOVED AND REPLACED HSTA IAW 27-42-01 AND REMOVED AND REPLACED MOTOR CONTRO L UNIT IAW 27-47-00. 2 L 7 2 4F RT A21EA 2002081300036 20020813 00036 SO 2002 8 13 SWIA200211081 1 20020726 A 3242 BRAKE EMB 120 EMB120ER 3260203 SO RT MLG SEIZED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 190SW 120050 ON TAXI OUT THE OUTBOARD RIGHT MAIN TIRE POPPED. FOUND NR 4 BRAKE LOCKED UP. REMOVED AND REPLACED NR 4 BRAKE IAW MM 32 -41-05. LEAK CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002081300037 20020813 00037 WP 2002 8 13 AALA20020864 1 20020603 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND GOUGE IN RIGHT CUSP FORWARD OF STATION 427 FRAME. INSTALLED DOUBLER RIGHT CUSP STATION 427 AS PER SRM 53-01 FIG 4-3. (M) 2 L 7 2 4F A6WE 2002081300038 20020813 00038 WP 2002 8 13 AALA20020865 1 20020604 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND CORROSION ON LOWER SIDE OF RIGHT CUSP AT STATION 544. REMOVED CORROSION, INSTALLED DOUBLER PER AARD 53-00-0 0-02. (M) 2 L 7 2 4F A6WE 2002081300039 20020813 00039 WP 2002 8 13 AALA20020867 1 20020608 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND FORWARD CARGO LOWER JAMB THRESHOLD PAN IS CORRODED STATION 370 TO 427. REMOVED AND REPLACED THRESHOLD PAN A SSEMBLY PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002081300040 20020813 00040 WP 2002 8 13 AALA20020868 1 20020530 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND FRAME AT STATION 1456 CRACKED WHERE L3L IS ATTACHED TO IT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AAR D 53-10-00-17. (M) 2 L 7 2 4F A6WE 2002081300041 20020813 00041 WP 2002 8 13 AALA20020869 1 20020605 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND CORROSION ON T-ANGLE STATION 1219 L28R OUTBOARD SIDE. REPLACED T-ANGLE PER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2002081300042 20020813 00042 WP 2002 8 13 DHL2002802007 1 20020809 A 2500 SEAT DOUG DC8 DC873 302199C WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 1) SECOND OBSERVERS SEAT WILL NOT ADJUST LATERALLY ALONG SEAT TRACKS SECOND OFFICER CHAIR NEEDS LUBRICATION IN ALL DIRE CTIONS2) PERFORMED OPERATIONAL CKECK OF SECOND OBSERVERS SEAT PER MM 25-11-2. REMOVED PEN FROM TRACKS. LUBED TRACKS PE R MM 12-80-0 NO DEFECTS NOTED OPS CHECKED GOOD. 2 L 7 4 4F RT 4A25 2002082300073 20020823 00073 NM 2002 8 23 02FDEA00565 1 20020807 A 5310 DOOR FRAME BOEING 727 72725 1384006 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 AFT FRAME OF FWD CARGO DOOR CUT OUT CRACK AT THE TIP DOOR STOP FITTING BETWEEN STR 19R - 20R. REMOVED AND REPLACED AN GLE & FILLER ON AFT FRAME PER EA 7-5310-65859. 2 L 7 3 4F A3WE 2002091200078 20020912 00078 NM 2002 9 12 02FDEA00567 1 20020806 A 5330 SKIN BOEING 727 72725 1384006 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 NUMEROUS NICKS IN LWR EXTERNAL FUSELAGE SKIN BETWEEN BS 580 & 600, STR 23R TO STR 26R. 2 L 7 3 4F A3WE 2002081300044 20020813 00044 WP 2002 8 13 AALA20020870 1 20020611 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND CORROSION ON SUPPORT ANGLE BLENDED CUT OUT OF LIMITS. INSTALLED NEW Z-ANGLE FLOORBOARD SUPPORT FROM STATION 1117-1155 IAW SRM 51-10-03. (M) 2 L 7 2 4F A6WE 2002082000143 20020820 00143 NM 2002 8 20 SABA020082 1 20020812 A 3350 1305 LIGHT DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 AIRCRAFT 883 ON FLIGHT 5057 FROM CLT TO TLH: DURING PREFLIGHT INSPECTION CREW REPORTED THE NUMBER ONE ROW EMERGENCY LIG HT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED BULB AND SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2002081300047 20020813 00047 WP 2002 8 13 AALA20020871 1 20020611 A 5320 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND CORROSION ON DOOR BEAM STATION 1155-1212 L28R. FOUND CORROSION BLENDED OUT OF LIMITS. INSTALLED NEW DOOR B EAM STATION 1117 TO 1250 IAW AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2002081300049 20020813 00049 WP 2002 8 13 AALA20020872 1 20020605 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND NR 3 SEAT TRACK CORRODED IN CHANNEL. REPAIRED PER AARD 53-20-00-10 FIG 4A. (M) 2 L 7 2 4F A6WE 2002081300053 20020813 00053 WP 2002 8 13 AALA20020874 1 20020605 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND HFEC INDICATES CRACKS EMITTING FROM DEEP SCRATCHES AT LOWER FUSE SKIN ANTENNAS AT STATION 390 AND 402. CUT OUT TWO DAMAGE AREA'S AND INSTALLED REPAIR DOUBLER 13 INCH BY 36 INCH PER SRM 53-04 FIG 170. (M) 2 L 7 2 4F A6WE 2002081300055 20020813 00055 WP 2002 8 13 AALA20020919 1 20020523 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 73444 49470 TUL - FOUND RIGHT CUSP CORRODED AFT OF LIGHTENING HOLE STATION 558 LOWER SIDE. INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002081300057 20020813 00057 WP 2002 8 13 AALA20020920 1 20020524 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 73444 49470 TUL - FOUND CORROSION ON NR 6 SEAT TRACK IN CHANNEL AND ON LUGS. REMOVED DAMAGED AREA FROM SEAT TRACK. INSTALLED REPAI R PLUG PER AARD 53-20-00-10 PAGE 1 REPAIR NR 10. (M) 2 L 7 2 4F A6WE 2002081300060 20020813 00060 WP 2002 8 13 AALA20020921 1 20020605 A 5730 SKIN DOUG DC9 DC982 3022082 WP WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 73444 49470 TUL - FOUND 3 INCH CRACK IN FIXED LEADING EDGE SKIN ABOVE NR 8 SLAT TRACK. REPAIRED CRACK PER SRM 57-01 FIG 3 SHEET 2 P AGE 8. (M) 2 L 7 2 4F A6WE 2002081300072 20020813 00072 CE 2002 8 13 AMTA200200921 1 20020806 A 3233 1540275121 ACTUATOR CESSNA 337 T337G 2075726 CE MLG MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 11 186 P3370207 IN TRANSIT DOOR AND FE'S LT GEAR DOOR LIGHTS CAME ON IN CLIMB. 1 H 7 2 3O A6CE 2002081300074 20020813 00074 EU 2002 8 13 B3OR20020012 1 20020529 A 6320 350A35101820 PULLEY SNIAS 350 AS350B2 8680813 EU M/R GEARBOX SCORED B U0SM K NONE O OTHER IN INSP/MAINT 1 SW 03 5204X 986 3099 AIRCRAFT WAS IN FOR 500 HOUR INSPECTION. WHILE INSPECTING THE MAIN GEAR BOX COUPLING THAT DRIVES THE HYDRAULIC PUMP VIA A BELT AND PULLEY, THE PULLEY SURFACE WHERE THE BELT CONTACTS IT WAS FOUND TO BE UNUSUALLY ROUGH. THE BELT WAS ALSO INS PECTED AND FOUND TO HAVE AN ABNORMAL TEXTURE. IT IS SUSPECTED THAT DIRT AND DEBRIS MAY HAVE GOTTEN ON THE BELT AND DAMAG ED THE PULLEY SURFACE. REPLACED PULLEY AND BELT. 1 G 7 1 3U H9EU 2002081300075 20020813 00075 SO 2002 8 13 C2XA02CL165 1 20020809 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16987 145261 DURING A 4A INSPECTION THE AFT AISLE EMERGENCY LIGHT WAS FOUND INOPERATIVE.MAINTENANCE REPLACED THE LAMP.OPERATIONAL CHE CKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002081300076 20020813 00076 EU 2002 8 13 B3OR20020013 1 20020517 A 6310 350A35110500 GIMBAL RING SNIAS 350 AS350B2 8680813 EU MGB COUPLING LOOSE B U0SM K NONE O OTHER IN INSP/MAINT 1 SW 03 5204X 986 3099 SEVERAL HOURS BEFORE THE AIRCRAFT CAME IN FOR IT'S 500 HOUR INSPECTION, IT WAS NOTED THAT THE ENGINE TO MAIN GEAR BOX GI MBAL JOINT , WHICH HOUSES THE DRIVE SHAFT, HAD EXCESSIVE PLAY. UPON INSPECTION AT THE 500 HOUR, THE GIMBAL RING AND HOUS ING WERE MEASURED AND FOUND TO BE OUT OF LIMITS AT THE GIMBAL PINS. THE PINS THEMSELVES NORMALLY GET SOME WEAR BUT THIS WEAR WAS IN THE BUSHINGS IN THE GIMBAL AND RING. A TECH REP WAS CONTACTED DUE TO THE FACT THAT THESE PARTS WERE FOUND OU T TO BE NON-REPAIRABLE. HE SUGGESTED THAT WE LOOK AT THE LEFT FOWARD MAIN GEAR BOX CROSSBEAM SUPPORT SHOCK MOUNT FOR THE CAUSE OF THIS PROBLEM. HE WAS CORRECT. THE LAMINATED MOUNT WAS DETERIORATED. WHEN THE CROSSBEAM WAS REMOVED IT WAS FOUN 1 G 7 1 3U H9EU 2002081300078 20020813 00078 EU 2002 8 13 B3OR20020015 1 20020529 A 6330 579069G MOUNT SNIAS 350 AS350B2 8680813 EU M/R GEARBOX DETERIORATED B U0SM K NONE O OTHER IN INSP/MAINT 1 SW 03 5204X 986 3099 THE ENGINE TO M/R GEARBOX GIMBAL JOINT , WHICH HOUSES THE DRIVE SHAFT, HAD EXCESSIVE PLAY. UPON INSPECTION AT THE 500 HO UR, THE GIMBAL RING AND HOUSING WERE MEASURED AND FOUND TO BE OUT OF LIMITS AT THE GIMBAL PINS. THE PINS THEMSELVES NORM ALLY GET SOME WEAR BUT THIS WEAR WAS IN THE BUSHINGS IN THE GIMBAL AND RING. A TECH REP WAS CONTACTED. AND SUGGESTED THA T WE LOOK AT THE LEFT FOWARD MAIN GEAR BOX CROSSBEAM SUPPORT SHOCK MOUNT FOR THE CAUSE OF THIS PROBLEM. HE WAS CORRECT. THE LAMINATED MOUNT WAS DETERIORATED. WHEN THE CROSSBEAM WAS REMOVED IT WAS FOUND THAT THE LAMINATED MOUNT HAD BEEN MOVI NG AND CAUSED FRETTING CORROSION ON THE BEAM. THE RUBBER PORTION OF THE MOUNT APPEARS TO HAVE BEEN DAMAGED BY OILS. 1 G 7 1 3U H9EU 2002081300079 20020813 00079 EU 2002 8 13 B3OR20020016 1 20020529 A 6210 STOP SNIAS 350 AS350B2 8680813 EU STARFLEX CORRODED B U0SM K NONE O OTHER IN INSP/MAINT 1 SW 03 5204X 3099 DURING 500 HOUR INSPECTION OF THE MAIN ROTOR COMPONENTS, CORROSION WAS FOUND ON THE MATING SURFACE OF THE SPHERICAL STOP WHERE IT ATTACHES TO THE STARFLEX. ALL THREE SPHERICAL STOPS WERE REPLACED DUE THE FACT THAT THEY ALL HAD 500 HOURS ON THEM AND CHANGING ONLY ONE IS NOT RECOMMENDED. 1 G 7 1 3U H9EU 2002081300080 20020813 00080 EU 2002 8 13 B3OR20020017 1 20020529 A 6220 BEARING SNIAS 350 AS350B2 8680813 EU MAIN ROTOR CORRODED B U0SM K NONE O OTHER IN INSP/MAINT 1 SW 03 5204X 3099 DURING A 500 HOUR INSPECTION IT IS NECESSARY TO DISSASSEBLE THE MAIN ROTOR FREQUENCY ADAPTER TO INSPECT FOR CORROSION. T HE BEARING THAT IS IN THE ADAPTER IS SUPPOSED TO BE EASILY REMOVABLE. VARIOUS EFFORTS WERE MADE TO REMOVE THE BEARING. T HE BEARING WAS REMOVED BY EXCESSIVE FORCE TO TRY TO FIND OUT WHY IT WAS FROZEN IN PLACE. AIRCRAFT'S ADAPTERS WERE ASSE MBLED WITH MINIMAL AMOUNTS OF A COMPOUND CALLED "MASTINOX" I.A.W. THE M/M. WHEN THE BEARING WAS REMOVED, CORROSION WAS FOUND IN THE BEARING BORE AND ON THE RETAINING RING. ALL THREE FREQUENCY ADAPTERS WERE IN THE SAME CONDITION AND ALL THR EE REPLACED. 1 G 7 1 3U H9EU 2002081300081 20020813 00081 CE 2002 8 13 B3OR20020018 1 20020807 A 2731 10161000013 RIVET BEECH 200 A200 1152921 CE PWA PT6 PT6A41 52043 EA TRIM TAB MISSING B U0SM K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 7074G 16 16 BC17 TRIM TAB WAS REPLACED DUE TO CORROSION, WHEN PART WAS INSTALLED IT WAS NOT NOTICED THAT THE RIVETS ALONG THE LEADING EDG E AND AROUND THE PITCH HORN WERE NOT INSTALLED. 1 L 7 2 4T 4 T A24CE E4EA 2002081300082 20020813 00082 NE 2002 8 13 EGR2002F00005 1 20020708 A 7930 CHIP DETECTOR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL NR 2 ENGINE ACTIVATED E EGRA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 17 764LF 4891 760264 CAE890821 NR 2 ENGINE CHIP LIGHT ILLUMINATED WHEN INITIATING APPROACH, LIGHT COULD NOT BE RESET PER SMSP. AIRCRAFT LANDED AT NEAR BY AIRPORT. NO FAILURE OF SYSTEMS OR COMPONENTS FOUND. MAINTENANCE REMOVED UPPER CHIP PLUG ON NR 2 ENGINE AND FOUND 1 SMALL FLAKE. CLEANED AND GROUND RUN ENGINE FOR 20 MINUTES. THEN RAN ADDITIONAL 10 MINUTES AT HOVER. DO DISCREPANCIES NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2002081300083 20020813 00083 SW 2002 8 13 EHA2002F0000A 1 20020508 A 2550 212072915103 CARGO HOOK BELL 212 212 1181420 SW WATER BUCKET MALFUNCTIONED E EHAA O OTHER O OTHER FF FIRE FIGHTING 1 AL 03 5017H 30930 UTILIZING A BAMBI BUCKET FOR WATER BOMBER, AC EXPERIENCED 2 UNCOMMANDED LOAD RELEASES. MAINT SUSPECTED A PROBLEM WITH D -RING COMPATIBILITY WAS CONDUCTED WITH NO ANOMILIES NOTED. ELEC AND MANUAL LOAD JETTISON SYS WERE TESTED, NO ANOMILIES NOTED. SEVERAL LOAD HOOKUP AND LOAD RELEASE FUNCTIONAL TESTS WERE PERFORMED, NO ANOMILIES NOTED. POSSIBILITY THAT CARGO HOOK HAD NOT BEEN PROPERLY LOCKED IN CLOSED POSITION. OPERATIONS WERE RESUMED. ANOTHER UNCOMMANDED LOAD RELEASE WAS E XPERIENCED, MAINT ONSITE PERFORMED RIGGING OPER ON MAN RELEASE SYSTEM AND DETAILED INSPECTION OF KNOWN PROBLEM AREAS OF CARGO HOOK WIRING. MINOR DISCREP IN MANUAL RELEASE SYS RIGGING WHICH WERE RATIFIED AND THE AC WAS RETURNED TO SERVICE. 1 G 7 1 4U H4SW 2002081300084 20020813 00084 SO 2002 8 13 C2XACL167 1 20020809 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14945 145049 CLE FLIGHT#2979 THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE.MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT INVERTER.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002081300085 20020813 00085 SW 2002 8 13 EHA2002F00001 1 20020522 A 6730 212001720003 CONTROL SERVO BELL 212 212 1181420 SW TAIL ROTOR INOPERATIVE E EHAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 827MS 31205 AFTER REPLACING THE TAIL ROTOR SERVO WITH A TESTED, (TIME CONTINUED), SERVICEABLE UNIT, A MAINTENANCE OPERATIONAL CHECK FLIGHT WAS CONDUCTED. DURING THE MOC FLIGHT, THE UPPER SEAL FOR THE SERVO FAILED, CAUSING LOSS OF NR1 HYDRAULIC PRESS. THE AIRCRAFT RETURNED TO BASE, ANOTHER SERVICEABLE TAIL ROTOR SERVO WAS INSTALLED, MOC FLIGHT CONDUCTED WITHOUT INCIDEN T, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 4U H4SW 2002101000016 20021010 00016 SW 2002 10 10 EHA2002F00002 1 20020721 A 2822 CIRCUIT BREAKER BELL 205 205A1 1181414 SW LYC T53 T53* 41549 NE RT FUEL BOOST FAILED B EHAR O OTHER O OTHER NR NOT REPORTED 1 AL 03 4750R 30009 LE07587 RIGHT FUEL BOOST PUMP INOPERATIVE. REPLACED CIRCUIT BREAKER. 1 G 7 1 4U 4 U H1SW E1EA 2002081300086 20020813 00086 SW 2002 8 13 EHA2002F00003 1 20020524 A 7720 3024304 THERMOCOUPLE BELL 212 212 1181420 SW NR 2 ENGINE FAILED E EHAA O OTHER N FALSE WARNING NR NOT REPORTED 1 AL 03 16974 30886 AFTER SEVERAL FLIGHTS AND SUBSEQUENT CHANGE OF PILOTS, THERE WAS NO T5 INDICATION DURING ENGINE START ON NR 2 ENGINE. D URING VISUAL INSPECTION IT WAS NOTED THAT A STUD HAD BROKEN OFF OF THE THERMAL COUPLE TERMINAL BLOCK TO WHICH EXTERNAL W IRING HARNESS CONNECTS. THE ENGINE WAS REMOVED, DISASSEMBLED, AND THE T5 THERMAL COUPLE HARNESS REPLACED, WITHOUT FURTH ER INCIDENT. 1 G 7 1 4U H4SW 2002081300087 20020813 00087 SW 2002 8 13 EHA2002F00004 1 20020526 A 2550 204072915103 CARGO HOOK BELL 212 212 1181420 SW WATER BUCKET INOPERATIVE E EHAA O OTHER O OTHER FF FIRE FIGHTING 1 AL 03 5017H 30930 DURING WORK WITH THE FORREST SERVICE USING BAMBI BUCKETS FOR WATER BOMBER OPERATIONS, THE AIRCRAFT EXPERIENCED AN UNCOMM ANDED EXTERNAL LOAD RELEASE. THE AIRCRAFT WAS FLOWN TO THE MAIN BASE WHERE A COMPLETE AND THOROUGH ELECTRICAL EVALUATIO N AND, AS A PRECAUTION, REPLACED THE RELEASE RELAY FOR THE ELECTRICAL PORTION OF THE CARGO HOOK. THE MANUAL RELEASE POR TION OF CARGO HOOK RELEASE SYSTEM WAS THOROUGHLY INSPECTED AND DETERMINED TO BE IN SATISFACTORY WORKING CONDITION. THE CARGO HOOK AND SUSPENSION ASSEMBLY WAS REPLACED, MANUAL RELEASE SYSTEM WAS RIGGED, AND TESTS PERFORMED ON BOTH THE MANUA L AND ELECTRICAL RELEASE SYSTEMS OF THE CARGO HOOK. 1 G 7 1 4U H4SW 2002081300088 20020813 00088 SW 2002 8 13 EHA2002F00005 1 20020601 A 2612 872203 FIRE LOOP BELL 212 212 1181420 SW NR 1 ENGINE BROKEN E EHAA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 AL 03 398EH 30766 APPROX 0.5 HOURS AFTER TAKEOFF, ENROUTE FOR CROSS COUNTRY, THE NR 1 ENGINE FIRE (T) HANDLE ILLUMINATED IN FLIGHT. HANDL E WAS PULLED TO FIRE NR 1 ENGINE MAIN FIRE BOTTLE, NR 1 ENGINE WAS SHUT DOWN AND SECURED, AND HELICOPTER RETURNED TO BAS E. UPON INSPECTION IT WAS FOUND THAT ENGINE FIRE BOTTLE DID NOT ACTUALLY DISCHARGE. FURTHER INSPECTION FOUND THAT TOP FIRE LOOP CABLE (P101 PN 872203) ON NR 1 ENGINE WAS BROKEN AT FIRE WALL AND SHORTED TO CONNECTOR SHELL, CAUSING A FALSE FIRE INDICATION. IT WAS DETERMINED THAT MAIN BOTTLE NOT FIRING WAS CAUSED BY A BROKEN WIRE (W3A22) AT CONNECTION TO (T ) HANDLE SWITCH (E) COMMON CONNECTION. ALL DISCREPANCIES WERE CORRECTED AND A THOROUGH SYSTEM INSP/ OP CHECK PERFORMED. 1 G 7 1 4U H4SW 2002081300089 20020813 00089 SO 2002 8 13 C2XA02CL168 1 20020812 A 3350 78241 INVERTER EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 25504 145186 CLE FLIGHT#4008 THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON THE FRONT PARTITION WAS INOPERATIVE.MAINTENANCE REPLACED T HE EMERGENCY EXIT LIGHT INVERTER.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002081300090 20020813 00090 SW 2002 8 13 EOP2002F00000 1 20020807 A 6730 SERVO BELL 206 206B 1181511 SW LATERAL CYCLIC MALFUNCTIONED E EOPA H DEACTIVATE SYST/CIRCUITS E VIBRATION/BUFFET NR NOT REPORTED 1 AL 01 4847 4004 PILOT NOTICED CYCLIC STICK HAD A SLIGHT SHAKE IN THE LATERAL AXIS, TURNED OFF HYDRAULIC SYSTEM AND THE SHAKE WENT AWAY. A/C LANDED AND RIGHT SERVO WAS CHANGED, PROBLEM CORRECTED. 1 G 7 1 3U H2SW 2002081300091 20020813 00091 SW 2002 8 13 ERAA080462 1 20020710 A 5302 SKIN BELL 212 212 1181420 SW TAILBOOM CRACKED E ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 10729 ADW06072 TAILBOOM HAS CRACK ON SADDLE DOUBLER RT BASE OF VERTICAL FIN. FOUND SADDLE DOUBLER TO BOTH BE CRACKED AND LOWER SKIN BE NEATH DOUBLERS CRACKED. REMOVED BOTH SADDLE DOUBLERS AND SKIN AND FOUND LOWER SKIN TO BE CRACKED. MUST BE SENT OFF TO REPAIR IN FIXTURE. 1 G 7 1 4U H4SW 2002081300092 20020813 00092 WP 2002 8 13 CALA0200438 1 20020809 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 1079-1136 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND L/H CENTER SEAT TRACK CORRODED BETWEEN STA 1079 AND 1136. THE SEAT TRACK WAS REMOVED AND REPLACED IAW S RM 51-30-5. 2 L 7 2 4F A6WE 2002081300093 20020813 00093 EU 2002 8 13 ERAA080464 1 20020711 A 6210 10514101111 BOLT BOLKMS 105 BO105CBS 5626008 EU M/R BLADE CRACKED E ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 423EH 543 SECONDARY BLADE BOLTS CRACKED UNDER HEAD IN RADIUS. SCRAPPED 3 EA SECONDARY BLADE BOLTS FOR CRACKS IAW MBB BO-105 MAINT ENANCE MANUAL CHAPTER 13. 1 G 7 2 3U NC H3EU 2002081300094 20020813 00094 SO 2002 8 13 ASOA02373S 1 20020630 A 3297 WIRE HARNESS EMB 120 EMB120RT 3260202 SO LT MLG PINCHED A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 232AS 120036 CLIMB OUT FROM DFW, NOTICED SMOKE DEVELOPING IN THE COCKPIT WITH A HOT PACK SMELL. THE SMOKE RAPIDLY INCREASED IN VOLUM E AS THE CAPTAIN BEGAN RUNNING THE APPROPRIATE CHECKLISTS. THE SMOKE STARTED TO DECREASE AFTER CAPTAIN PERFORMED SMOKE EVACUATION CHECKLIST. AFTER CHECKLISTS WERE COMPLETED VERIFIED THAT ALL A/C SWITCHES WERE IN THE PROPER POSITION AND MO VED ACCORDINGLY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW. SMOKE WAS ALSO IN THE CABIN DURING FLIGHT . MX R&R THE LEFT MLG WOW PROXIMITY SWITCH DUE TO A PINCHED HARNESS. THE MORE LIKELY CAUSE OF THIS DISCREPANCY WAS THE RAM AIR SWITCH BEING OUT OF POSITION. AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER DISCREPANCY OF THIS NATURE. (M) 2 L 7 2 4T RT A31SO 2002081300095 20020813 00095 SO 2002 8 13 ASOA02374 1 20020630 A 5313 12006173009 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 502AS 120274 DURING C-CHECK INSPECTION IN BNA, STRINGER 18 LEFT WAS FOUND CORRODED BETWEEN FRAME 13A AND SPLICE JUST FORWARD OF FRAME S 15 AND 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER IAW SRM'S 51-25-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002081300096 20020813 00096 SO 2002 8 13 ASOA02375 1 20020630 A 5313 12005744013 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 502AS 120274 DURING C-CHECK INSPECTION IN BNA, FOUND CORROSION OUT OF LIMITS ON STRINGER 19 LEFT BETWEEN FRAMES 13A AND 18A. MAINTEN ANCE REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002081300097 20020813 00097 SO 2002 8 13 ASOA02376 1 20020630 A 5330 12019230003 DOUBLER EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 502AS 120274 DURING C-CHECK INSPECTION IN BNA, THE FUSELAGE EXTERNAL SKIN DOUBLER AT FRAME 21 HAD SEVERAL BULGES AND CRACKED RIVET HE ADS BETWEEN STRINGERS 20 LEFT AND 21 RIGHT. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SKIN DOUBLER IAW ASA EO 120-52 -0178. THIS EO CONTAINS REPAIR SPECIFICATIONS FOR ASA EO120-53-0096, EST 246/95, 226/96, 283/96, 3431/00, SRM 51-00-00, AND SRM 53-00-00 AS REF. (M) 2 L 7 2 4T RT A31SO 2002081300098 20020813 00098 EA 2002 8 13 ASOA02377 1 20020620 A 5320 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 847AS 7335 DURING HANGAR MAINTENANCE IN MCN, FRAME 718 LEFT WAS FOUND TO BE CRACKED. FRAME 718 RIGHT WAS FOUND ONLY TO HAVE A DOUB LER CRACKED NOT THE ACTUAL FRAME ITSELF. MAINTENANCE REMOVED AND REPLACED THE CRACKED DOUBLER IAW SRM 51-00. MAINTENAN CE REPAIRED THE CRACKED LEFT FRAME IAW ASA EO 600-53-0067. THIS EO INCLUDES REPAIR SPECIFICATIONS FOR FS 718 CRACKS ON CRJ200 AIRCRAFT USING REO 601R-53-61-193, REO 601R-53-61-492, SRM 51-00 REV 14, AND SRM 53-00 REV 14 AS REF. (M) 2 L 7 2 4F RT A21EA 2002081300099 20020813 00099 EA 2002 8 13 ASOA02378 1 20020629 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 847AS 7335 DURING HANGAR MAINTENANCE IN MCN, LEFT SIDE ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED CRACKED E NGINE SUPPORT BEAM IAW ASA EO 600-53-0073. THIS EO INCLUDES REPAIR SPECIFICATIONS FOR ENGINE SUPPORT BEAM CRACKS AT BL 36.20 FOR CRJ200 AIRCRAFT. THIS EO REFERENCES ASA EO 600-53-0043. REO 601R-53-61-366 REV E, SERVICE BULLETIN A601R-53- 059, AND SRM'S 51-00 REV 14 AND 53-00 REV 14. (M) 2 L 7 2 4F RT A21EA 2002081300100 20020813 00100 EA 2002 8 13 ASOA02379 1 20020701 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 838AS 7276 DURING A SCHEDULED INSPECTION IN XNA, THE AFT OVERHEAD CABIN EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002081300101 20020813 00101 EU 2002 8 13 ASOA02380 1 20020701 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A ASOA K NONE O OTHER CR CRUISE 1 SO 11 634AS 3199 370 FLT 4125 - DURING FLIGHT FROM MGM TO ATL, THE FORWARD PART OF THE EMERGENCY LIGHTS CAME ON WHEN THE EMERGENCY LIGHTS WER E SWITCHED TO THE ARM POSITION. AIRCRAFT CONTINUED AND LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE EMER GENCY LIGHT POWER SUPPLY IN THE 61WL POSITION. AN ENGINE GROUND MAINTENANCE RUN WAS PERFORMED AND THE OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WAS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002081300102 20020813 00102 EA 2002 8 13 ASOA02381 1 20020702 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 860AS 7433 DURING A SCHEDULED INSPECTION IN XNA, THE SECOND FROM FORWARD CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE BURNED OUT CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002081300103 20020813 00103 SO 2002 8 13 ASOA02382 1 20020702 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 273AS 120222 DURING GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS COULD NOT BE TURNED OFF. MAINTENANCE CHARGED THE EMERGENCY LIGHTI NG BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002081300104 20020813 00104 SO 2002 8 13 ASOA02383 1 20020702 A 3350 3071BPE LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 275AS 120234 DURING A HANGAR INSPECTION IN MCN, SEVERAL EMERGENCY LIGHTS ON THE CABIN FLOOR WERE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED ALL INOPERATIVE EMERGENCY LIGHT BULBS ON THE CABIN FLOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002081300105 20020813 00105 SO 2002 8 13 ASOA02384 1 20020703 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DEFECTIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 267AS 120198 DURING HANGAR MAINTENANCE IN TXK, THE EMERGENCY LIGHT CIRCUIT BREAKER POPPED WHEN THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH WAS TURNED ON. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK IN THE NR 2 POSITION. OPERA TIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002081300106 20020813 00106 SO 2002 8 13 ASOA02385 1 20020704 A 3350 12021299501 LIGHT EMB 120 EMB120RT 3260202 SO EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 281AS 120224 DURING GROUND INSPECTION IN ATL, THE RIGHT UPPER EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE INOPERATIVE EXTERNAL EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002081300107 20020813 00107 EU 2002 8 13 UPS02138892 1 20020724 A 2120 ODOR AIRBUS A300 A300F4622R 3930360 EU CABIN DETECTED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 01 144UP 0827 INSPECTION TYPE:N/A DURING LANDING PHASE OF PREV FLT & DURING T/O ROLL OF THIS LEG OBSERVED A HIGHLY OBNOXIOUS ODOR, NOT SURE OF SOURCE. THE SMELL WENT AWAY 10 MIN INTO FLIGHT. IT DID NOT SMELL LIKE ELECTRICAL FIRE, MORE LIKE SOMETHING BU RNING IN A STOVE. NO SMOKE PRESENT. SAME ODOR ON LANDING. RAN ENGINES, IDLED FOR SEVERAL MINUTES AND NO SMELL WAS OBS ERVED. ALL CONDITIONS WERE NORMAL. 2 L 7 2 4F RT A35EU 2002081300109 20020813 00109 NM 2002 8 13 UPS02238850 1 20020618 A 5313 STRINGER BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI AFT STR END AT BS 950 STR 9 RT CRACKED. REPLACED STR END IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2002081300110 20020813 00110 NM 2002 8 13 UPS02238852 1 20020618 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C+SI, NLG W/W RIGHT CEILING PANEL CORRODED. REMOVED AND REPLACED AFT CORNER . MATERIAL REMOVED IAW SRM 51-10-01. CARRIED OUT REPAIR OF AFFECTED AREA IAW SMRO EO 2002-035-016. 2 L 7 3 4F A3WE 2002081300111 20020813 00111 NM 2002 8 13 UPS02238875 1 20020722 A 3350 BATTERY BOEING 727 72731C 1384011 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:PFLT FORWARD ENTRY EMERGENCY EXIT LIGHT INOP. FORWARD ENTRY EMERGENCY EXIT LIGHT BATTERIES REPLACED. I NSPECTED/TESTED SERVICEABLE IAW B727 MM 33-50-01. 2 L 7 3 4F A3WE 2002081300112 20020813 00112 NM 2002 8 13 UPS02238919 1 20020729 A 3350 BATTERY BOEING 727 72730C 1384009 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:N/A, EMERGENCY LIGHT WEAK AT COCKPIT. REPLACED BATTERIES, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002081300113 20020813 00113 NM 2002 8 13 UPS02238920 1 20020729 A 3350 BATTERY BOEING 727 72730C 1384009 NM CABIN DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:N/A, EMERGENCY LIGHT WEAK AT L1 DOOR. REPLACED BATTERIES, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002081300114 20020813 00114 NM 2002 8 13 UPS02238974 1 20020803 A 5210 LATCH BOEING 727 72725C 138400H NM ENTRY DOOR OUT OF ADJUST A IPXA K NONE O OTHER LD LANDING 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, ENTRY DOOR HANDLE UNLATCHED ON LANDING FOUND DOOR ENTRYWAY PARTIALLY OPENED. ALSO ACFT SUFFICIENT TO MAINTAIN PRESSURIZATION IN AUTO/MAN. PERFORMED FWD ENTRY DOOR ADJ FOR SOFT UNLATCHING PER MM 52-11-00. 2 L 7 3 4F A3WE 2002081300115 20020813 00115 NM 2002 8 13 UPS02238980 1 20020731 A 3210 YOKE BOEING 727 72722C 138400F NM LT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, LT BS 940 SWING LINK REMOVAL YOKE ASSY FOUND TO BE CORRODED. YOKE ASSY REPLACED IAW MM 57-15-01. 2 L 7 3 4F A3WE 2002081300116 20020813 00116 NM 2002 8 13 UPS02238984 1 20020724 A 5320 STRAP BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, FLOORBOARD SUPPORT STRAP CRACKED BS 850 LBL 45.5. FLOORBOARD SUPPORT STRAP REPLACED BS 850 LBL 45.5 IAW SRM 53-20-2. 2 L 7 3 4F A3WE 2002081300117 20020813 00117 NM 2002 8 13 SWAA021773 1 20020806 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 EEPLS COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002081300118 20020813 00118 2002 8 13 SWAA021777 4 20020806 A 2565 6949956 CABLE BOEING 737 7372H4 138448C NM FWD ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002081300119 20020813 00119 NM 2002 8 13 UPS02239009 1 20020723 A 5320 STIFFENER BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, MAIN CARGO DECK COMPARTMENT BS 1183 STIFFENER TIE CRACKED AT RBL 361 UPPER TIE BETWEEN VERT BEAM AT R BL 26.83 & RBL 36.83. NEW STIFFENER INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2002081300120 20020813 00120 NM 2002 8 13 SWAA021763 1 20020806 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED PM CHECK, FOUND EEPLS COVERS LOOSE (7 EA) IN CABIN. SECURED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2002081300121 20020813 00121 NM 2002 8 13 SWAA021764 1 20020806 A 3350 6104289 BATTERY BOEING 737 7373Q8 1384670 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INTERMITTENT. REMOVED AND REPLACED B ATTERY PER MM. 2 L 7 2 4F RT A16WE 2002081300122 20020813 00122 NM 2002 8 13 SWAA021766 1 20020806 A 3350 311500 LENS BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002081300123 20020813 00123 NM 2002 8 13 SWAA021770 1 20020806 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, WL 207 AND RBL 56. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002081300124 20020813 00124 NM 2002 8 13 SWAA021771 1 20020806 A 5312 6547978 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 AND BS 420, WL 208 AND RBL 65. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002081300125 20020813 00125 NM 2002 8 13 UPS02239010 1 20020723 A 5311 FRAME BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, LEFT WHEEL WELL, BS 930 FRAME IS CRACKED ON INNER FLANGE UPPER HOLE. REPAIR CARRIED OUT IAW UPS EO B 727-5310-2611-B. 2 L 7 3 4F A3WE 2002081300126 20020813 00126 NM 2002 8 13 UPS02239013 1 20020626 A 5754 STRUCTURE BOEING 727 72722C 138400F NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C PLS CARRY OUT PERMANENT REPAIR TO NR 2 L/E SLAT DENT (APPROX 1.5 FT O/B OF ACTUATOR). PERMANENT REPAI R CARRIED OUT ON NR 2 L/E SLAT IAW SRM 57-50-03 FIG 1. 2 L 7 3 4F A3WE 2002081300127 20020813 00127 NM 2002 8 13 UPS02239017 1 20020725 A 5414 PANEL BOEING 727 72722C 138400F NM NR 1 PYLON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, ENGINE NR 1 PYLON PANEL 5408 IS DELAMINATED INNER, SURFACE FWD END. REPAIRED IAW SRM 51-40-5. 2 L 7 3 4F A3WE 2002081300128 20020813 00128 NM 2002 8 13 UPS02239018 1 20020725 A 5414 PANEL BOEING 727 72722C 138400F NM NR 3 PYLON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, ENGINE NR 3 PYLON PANEL 5508 IS DELAMINATED, INNER SURFACE FWD END. REPAIRED IAW SRM 51-40-5. 2 L 7 3 4F A3WE 2002081300129 20020813 00129 NM 2002 8 13 UPS02239021 1 20020726 A 3210 LINK BOEING 727 72722C 138400F NM LT MLG DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, LEFT MLG BEAM SWING LINK BOLT HOLE HAS MECHANICAL DAMAGE. REPAIR CARRIED OUT IAW SMRO EO 2002-040-00 4 UPS ENGINEERING FILE 727-57-20059. 2 L 7 3 4F A3WE 2002081300130 20020813 00130 SO 2002 8 13 LR7A02064 1 20020812 A 5312 WEB LKHEED 382 382G 526414U SO FS 880 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2340 4606 DURING SCHEDULED C4 INSPECTION PER JOB CARD HSP5336 FOUND RH FS 880 BULKHEAD WEB CRACKED AT RBL 80, WL 230.REPLACED WEB IAW SRM SMP 583 53-50-04, 51-60 AND 51-70. NR 2023. 2 H 7 4 4T A1SO 2002081300131 20020813 00131 SO 2002 8 13 LR7A02065 1 20020812 A 5312 WEB LKHEED 382 382G 526414U SO FS 900 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2340 4606 DURING SCHEDULED C4 INSPECTION PER JOB CARD HSP5336 FOUND LH FS 900 BULKHEAD WEB CRACKED AT LBL 70, WL 245.REPAIRED IAW SRM SMP 583 51-140-17. NR 2024. 2 H 7 4 4T A1SO 2002081300132 20020813 00132 SO 2002 8 13 LR7A02067 1 20020812 A 5311 FRAME LKHEED 382 382G 526414U SO FS 617 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2340 4606 DURING SCHEDULED C4 INSPECTION PER JOB CARD HSP5335 FOUND LH FS 617 FRAME CRACKED AT SPLICE FITTING, LBL 20, WL 282.REPA IRED IAW LAC MEA 382-53-02-046. NR 2032. 2 H 7 4 4T A1SO 2002081300133 20020813 00133 SO 2002 8 13 LR7A02068 1 20020812 A 5321 FLOOR PANEL LKHEED 382 382G 526414U SO FS 245-588 WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2340 4606 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC05297 FOUND FS 245 TO 588 CENTER FLOOR PANELS WARPED, RBL 20 TO LBL 20, WL 146.REPLACED FLOOR PANELS IAW SRM SMP 583 53-40-05 AND 51-60. NR 2036. 2 H 7 4 4T A1SO 2002081300134 20020813 00134 SO 2002 8 13 LR7A02069 1 20020812 A 5321 FLOOR PANEL LKHEED 382 382G 526414U SO FS 588-817E WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2340 4606 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC05297 FOUND FS 588 TO 657 & 737E TO 817E 3 EA. CENTER FLOOR PANELS WARPED, RBL 20 TO LBL 20, WL 146.REPLACED FLOOR PANELS IAW SRM SMP 583 53-40-05 AND 51-60. NR 2037. 2 H 7 4 4T A1SO 2002081300135 20020813 00135 SO 2002 8 13 LR7A02070 1 20020812 A 5343 3884828 BEAM LKHEED 382 382G 526414U SO FS 577 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2340 4606 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC3209 FOUND FS 577 RMLG BEAM CRACKED AT RBL 62, WL 240.REPLACED RMLG BEAM I AW SRM SMP 583 51-60, 51-70 AND ED02-014-3. NR 2072. 2 H 7 4 4T A1SO 2002081300136 20020813 00136 SO 2002 8 13 LR7A02072 1 20020812 A 5343 BEAM LKHEED 382 382G 526414U SO FS 528 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2340 4606 DURING SCHEDULED C4 INSPECTION PER JOB CARD HST5316 FOUND FS 528 LMLG BEAM CORRODED AT LBL 63, WL 247.REPAIRED IAW LAC M EA 382-53-02-25. NR 2132. 2 H 7 4 4T A1SO 2002081300137 20020813 00137 SO 2002 8 13 LR7A02073 1 20020812 A 5313 ANGLE LKHEED 382 382G 526414U SO FS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2340 4606 DURING SCHEDULED C4 INSPECTION NR 2026 ACCOMPLISHMENT FOUND FS 477 'L' ANGLE CRACKED AT LBL 60, WL 270.REPLACED ANGLE IA W SRM SMP 583 51-10, PG. 4. NR 2182. 2 H 7 4 4T A1SO 2002081300138 20020813 00138 SO 2002 8 13 LR7A02074 1 20020812 A 5321 FLOOR PANEL LKHEED 382 382G 526414U SO FS 796-809 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2340 4606 DURING SCHEDULED C4 INSPECTION PER JOB CARD HSP53161 FOUND FS 796 TO 809 RAMP LH AND RH FLOOR PANELS WITH CRACKED HAT SE CTIONS, LBL 60 AND RBL 60, WL 146.REPLACED FLOOR PANELS IAW SRM SMP 583 51-10 PG 4, 51-60 AND 51-70. NR 2183. 2 H 7 4 4T A1SO 2002081300139 20020813 00139 NM 2002 8 13 UPS02239023 1 20020722 A 5330 SKIN BOEING 727 72722C 138400F NM B521 S1R-S4R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, MATERIAL LOSS INDICATIONS AT BS 521 AFT SKIN FROM STR 1 TO STR 2 OF 15 - 20 PERCENT AND FROM STR 3R T O STR 4R OF 20 PERCENT AND ON FWD SKIN AT BS 521 BETWEEN STR 3R AND STR 4R OF 15 PERCENT. AREA INSP AND CORROSION FOUND ON SKIN AND TEAR STRAP AT INDICATED AREAS OF SKIN. CORRODED AREA OF SKIN AND TEAR STRAP OUT OF LIMITS AND CUT AWAY IAW SRM 53-30-3. FURTHER CORROSION FOUND ON SKIN AND REINFORCING STRAP AT BUTT JOINT SPLICE AT S2L. REPAIR CARRIED OUT IA W SRM 53-30-3 FIG 21 UPS EO-B727-5330-0815. 2 L 7 3 4F A3WE 2002081300140 20020813 00140 2002 8 13 ERAA080466 4 20020711 A 3442 40008330208 INDICATOR SKRSKY S61 S61N 8142104 NE RADAR SYS CONTAMINATED E ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 563EH 1273 61808 RADAR INOPERABLE, HAS BLANK SCREEN. UNIT ALSO INTERMITTANT; HAD MODERATE WATER DAMAGE. REMOVED CORROSION, REPLACED R39 , REPAIRED BLOWN TRACES, ALIGNED AND TESTED. 2 G 7 2 4U 1H15 2002081300141 20020813 00141 2002 8 13 ERAA080467 4 20020712 A 3442 40008330208 INDICATOR SKRSKY S61 S61N 8142104 NE WX RADAR CONTAMINATED E ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 562EH 758 61257 UNIT WORKS ONLY IN WX MODE. UNIT WOULD NOT COME ON. FOUND CORROSION CAUSED BY WATER DAMAGE. FOUND BLOWN RESISTOR ON HV SWEEP CARD. FOUND BAD TRACKS AND CONNECTIONS ON MAIN CONNECTOR. FOUND BAD FLYBACK. ACTION TAKEN: REPLACED ALL BAD PA RTS, ALIGNED & TESTED UNIT 2 G 7 2 4U 1H15 2002081300142 20020813 00142 2002 8 13 ERAA080468 4 20020715 A 3442 40008330208 INDICATOR BELL 412 412 1182202 SW WX RADAR CONTAMINATED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 419EH UNIT DROPS OFF LINE, SLOW TO COME ON. WATER DAMAGE, BAD LOW VOLTAGE, VIDEO SWEEP; DATA PROCESSING ON CONTROL LOGIC CART S. ACTION TAKEN: REMOVED CORROSION, REPLACED BAD COMPONENTS ON ALL BAD CARDS, ALIGNED AND TESTED. 1 G 7 2 4U H4SW 2002081300144 20020813 00144 NM 2002 8 13 UPS02239029 1 20020722 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, 15 TO 20 PERCENT MATERIAL LOSS INDICATION AT BS 1080 STR 4R. REPAIR CARRIED OUT IAW UPS EO B727-5330 -1177 & SMRO EO 2002-040-005 UPS ENGINEERING FILE B727-5330-17277. 2 L 7 3 4F A3WE 2002081300145 20020813 00145 NM 2002 8 13 UPS02438796 1 20020713 A 2612 FIRE WARNING BOEING 747 747123 1384873 NM COCKPIT INTERMITTENT A IPXA K NONE N FALSE WARNING CL CLIMB 1 SO 01 675UP 20390 INSPECTION TYPE:N/A, ON CLIMBOUT GOT A BTB TRIP ON NR 2 WITH MOMENTARY FLASH OF FIRE WARNING HAD GCU LT ON GEN PARALLEL SHOWED MOMENTARY FLUX ON AC VOLT. RESET PWR AOM OPS NORMAL REMAINDER OF FLIGHT. NOTED TO MMOC INFM NR 2 BTB OK WITH AP U PWR AND FIRE WARNING SYS TEST NORMAL. RAN ENG NR 2 FOR GCU OPR. CHECKED ALL OK BY FLT CREW. 2 L 7 4 4F A20WE 2002081300146 20020813 00146 NM 2002 8 13 UPS02438816 1 20020702 A 5330 PANEL BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX KEELBEAM BOX LWR EXTERIOR LWR FIXED PANEL UPPER SURFACE FOUND SURFACE CORRODED AT LT SIDE STA 1440 TO 1460 LBL 7 TO 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. FIXED PANEL REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300147 20020813 00147 NM 2002 8 13 UPS02438817 1 20020703 A 5320 69B118571 BRACKET BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - KEELBEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1000 LBL 9. CORROSION BLEND OUT EX CEEDS SRM LIMITS. SUPPORT BRACKET REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300148 20020813 00148 NM 2002 8 13 UPS02438818 1 20020702 A 5320 SUPPORT BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX KEELBEAM BOX LWR EXTERIOR LWR PANEL SUPPORT LWR CHORD FOUND SURFACE CORROSION AT STA 1276 TO 1353 R BL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300149 20020813 00149 NM 2002 8 13 UPS02438819 1 20020702 A 5320 SUPPORT BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX KEEL BEAM BOX LWR EXTERIOR LWR SUPPORT LWR CHORD FOUND SURFACE CORROSION AT STA 1329 RBL 16 TO LBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300150 20020813 00150 NM 2002 8 13 UPS02438820 1 20020702 A 5320 SUPPORT BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX KEELBEAM BOX LWR EXTERIOR PANEL SUPPORT LWR CHORD FOUND SURFACE CORROSION AT STA 1353 RBL 16 TO LBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300151 20020813 00151 NM 2002 8 13 UPS02438821 1 20020702 A 5320 SUPPORT BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - KEELBEAM BOX LOWER EXTERIOR PANEL SUPPORT LOWER CHORD FOUND SURFACE CORROSION AT STA 1470 LBL 16 TO RBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300152 20020813 00152 NM 2002 8 13 UPS02438822 1 20020703 A 5320 69B118751 BRACKET BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - KEELBEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1227 LT SIDE LBL 9. CORROSION BLEN D OUT EXCEEDS SRM LIMITS. BRACKET REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300153 20020813 00153 NM 2002 8 13 UPS02438823 1 20020703 A 5320 69B118571 BRACKET BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - KEELBEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1183 RT SIDE RBL 9. CORROSION BLEN D OUT EXCEEDS SRM LIMITS. KEELBEAM PANEL SUPPORT BRACKET REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300154 20020813 00154 NM 2002 8 13 UPS02438824 1 20020702 A 5320 65B138626 SUPPORT BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:N/A FX KEELBEAM BOX LWR EXTERIOR PANEL SUPPORT LWR CHORD SURFACE FOUND SURFACE CORROSION AT STA 1276 RBL 16 TO LBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300155 20020813 00155 NM 2002 8 13 UPS02438826 1 20020702 A 5320 65B140561 SUPPORT BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - KEELBEAM BOX LOWER EXTERIOR PANEL SUPPORT LOWER CHORD FOUND SURFACE CORROSION AT STA 1405 LBL 16 TO RBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300156 20020813 00156 NM 2002 8 13 UPS02438828 1 20020702 A 5320 65B15085U886 SUPPORT BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - KEELBEAM BOX LOWER SURFACE LOWER PANEL SUPPORT LOWER CHORD SURFACE FOUND SURFACE CORROSION AT STA 1480 RBL 16 TO LBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300157 20020813 00157 NM 2002 8 13 UPS02438829 1 20020702 A 5320 65B140632 SUPPORT BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX KEELBEAM BOX LWR EXTERIOR LWR PANEL SUPPORT LOWER CHORD FOUND SURFACE CORROSION AT STA 1392 TO 1440 LBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300158 20020813 00158 NM 2002 8 13 UPS02438831 1 20020703 A 5330 PANEL BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - KEELBEAM BOX LOWER EXTERIOR KEELBEAM FIXED PANEL UPPER SURFACE AND HINGE FITTING AREA FOUND SURFA CE CORROSION AT STA 1440 TO STA 1470 RBL 7 TO RBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. WEB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300159 20020813 00159 NM 2002 8 13 UPS02438833 1 20020703 A 5320 65B15069132 RIB BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - KEELBEAM BOX LOWER EXTERIOR LOWER CHORD ATT RIB FOUND SURFACE CORROSION AT STA 1360 RBL 7 TO LBL 7. CORROSION BLEND OUT EXCEEDS SRM LIMITS. RIB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300160 20020813 00160 NM 2002 8 13 UPS02438834 1 20020703 A 5320 69B118571 BRACKET BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - KEELBEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1122 RBL 9. CORROSION BLEND OUT EX CEEDS SRM LIMITS. BRACKET REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081300161 20020813 00161 WP 2002 8 13 MWEA020474 1 20020813 A 5753 99575793 WING DOUG DC9 DC932 3022066 WP FLAP PANEL DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 LEFT WING AFT SIDE OF WING FLAP TRAILING EDGE PANEL IS DELAMINATED AT FORWARD OUTBOARD CORNER DOT.18. -- FABRICATED AN D INSTALLED SKIN. 2 L 7 2 4F A6WE 2002081300162 20020813 00162 WP 2002 8 13 MWEA020475 1 20020813 A 5755 3913194505 SPOILER DOUG DC9 DC932 3022066 WP TAG #1 RH WING CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 INBOARD FLIGHT SPOILER OUTBOARD HINGE SUPPORT IS CHAFED. TAG #1 RIGHT WING. -- SUPPORT IS CHAFED TO LIMITS. LOCATED AN D DRILLED NEW FITTINGS. 2 L 7 2 4F A6WE 2002081300163 20020813 00163 WP 2002 8 13 MWEA020476 1 20020813 A 5313 5910163191 BRACKET DOUG DC9 DC914 3022034 WP RADIAL #6 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 SUPPORT BRACKET 5910163-191 LOCATED ON LEFT SIDE OF APB AT RADIAL 6 INBOARD END DAMAGED. -- LOCATED AND DRILLED INBOAR D AND OUTBOARD END OF NEW 191 AND REMOVED AND INSTALLED BRACKET. 2 L 7 2 4F A6WE 2002081300164 20020813 00164 WP 2002 8 13 MWEA020480 1 20020813 A 5740 99116033 STRINGER DOUG DC9 DC914 3022034 WP STRINGER 16&17 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGERS 16 AND 17 ALSO EXT ENDING UNDER STRINGERS 16 AND 17. 2 L 7 2 4F A6WE 2002081300165 20020813 00165 WP 2002 8 13 MWEA020486 1 20020813 A 5740 99116033 STRINGER DOUG DC9 DC914 3022034 WP STRINGER 11&12 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 11 AND 12 ALSO EXTE NDING UNDER STRINGER 11. -- REMOVED CORRORION. 2 L 7 2 4F A6WE 2002081300166 20020813 00166 WP 2002 8 13 MWEA020478 1 20020813 A 5313 5910163173 ANGLE DOUG DC9 DC914 3022034 WP RADIAL 6 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 ANGLE AT RADIAL 6 LEFT IS CRACKED. -- DRILLED UP ANGLE AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2002081300167 20020813 00167 WP 2002 8 13 MWEA020487 1 20020813 A 5740 99116033 STRINGER DOUG DC9 DC914 3022034 WP STRINGER 12&13 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 12 AND 13 ALSO EXTE NDING UNDER STRINGER 12 AND 13. -- FABRICATED SHIMS FOR STRINGER AND REMOVED CORROSION. 2 L 7 2 4F A6WE 2002081300168 20020813 00168 EU 2002 8 13 AWXA200200718 1 20020811 A 7720 ENGINE IAE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 MALFUNCTIONED A AWXA C ABORTED TAKEOFF J S M WARNING INDICATION AFFECT SYSTEMS OVER TEMP TO TAKEOFF 1 WP 28 635AW V0042 092 V0042 ON TAKEOFF FROM FLL EN ROUTE FOR PHX NR 1 ENGINE HAD LOW EPR, EPR AT 1.32 CHARTED EPR WAS 1.40, ABORTED TAKEOFF. CONTRAC T MAINTENANCE AT FLL PERFORMED TEST OF BOTH ENGINES, TESTS WERE NORMAL. PLACED NR 1 ENGINE ON MEL 73-20-04, COND. 1, EPR MODE INOP. MAINTENANCE FERRIED AIRCRAFT BACK TO PHX AND REPLACED ENGINE. 2 L 7 2 4F 4 F RT A28NM E311NE 2002081300169 20020813 00169 NM 2002 8 13 AWXA200200727 1 20020812 A 2560 P20700012015 FLASHLIGHT AIRBUS A319 A319132 3930340 NM ZONE 220 INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 817AW 0 0 1373 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT HAS A BLINKING LITE. MAINTENANCE REMO VED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002081300170 20020813 00170 NM 2002 8 13 AWXA200200729 1 20020807 A 5345 65B57839 FITTING BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 0 0 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON L/H AFT LAVATORY OUTBOARD MOUNT FITTING BS 1010, LBL 65. M AINTENANCE REMOVED AND REPLACED L/H AFT LAVATORY OUTBOARD MOUNT FITTING BS 1010, LBL 65, IAW B737-300 SRM 51-40-02, PG. 6-10, AND SRM 53-60-51, PG. 106-113. 2 L 7 2 4F RT A16WE 2002081300171 20020813 00171 NM 2002 8 13 AWXA200200730 1 20020801 A 5320 65C326779 FLOOR SUPPORT BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOOR SUPPORT AT BS 994, RBL 20.70 - RBL 33.80. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT BS 994, RBL 20.70 - RBL 33.80. FABRICATED A NEW FLOOR SUPPORT, AND INSTALLED REPAIR IAW B737-300 SRM 51-40-05, PG. 4-5. 2 L 7 2 4F RT A16WE 2002081300172 20020813 00172 NM 2002 8 13 AWXA200200731 1 20020725 A 5311 6517684 DOUBLER BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 0 0 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND ON BELT FRAME DOUBLER BS 303, BETWEEN STRINGERS 16 AND 17 L/H. MAINTENANCE REMOVED CRACKED DOUBLER, FABRICATED A NEW DOUBLER, AND INSTALLED REPAIR IAW DWG 65-17684, AND B737-200 SRM 51-10-1, PG. 8. 2 L 7 2 4F RT A16WE 2002081300173 20020813 00173 NM 2002 8 13 AWXA200200735 1 20020729 A 5320 69374024 ANGLE BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 0 0 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND ON ANGLE AT THE FORWARD GALLEY DOOR LOWER SILL, BS 294.5. MAINTENANCE REMOVED CRACKED ANGLE AT BS 294.5, FABRICATED A NEW ANGLE PER DWG 69-37402-4, AND INSTALLED REPAIR IAW B737- 200 SRM 51-10-01, PG. 8. 2 L 7 2 4F RT A16WE 2002081300174 20020813 00174 NM 2002 8 13 AWXA200200737 1 20020729 A 5345 65B578393 FITTING BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 0 0 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON L/H AFT LAVATORY INBOARD FORWARD MOUNT FITTING BS 967, LBL 50. MAINTENANCE REMOVED AND REPLACED L/H AFT LAVATORY INBOARD FORWARD MOUNT FITTING BS 967, LBL 50, IAW B737-300 SRM 51 -40-02, PG. 10-11, AND SRM 53-40-05, PG. 4. 2 L 7 2 4F RT A16WE 2002081300175 20020813 00175 NM 2002 8 13 AWXA200200738 1 20020729 A 5345 65B578393 FITTING BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 0 0 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON R/H AFT LAVATORY INBOARD FORWARD MOUNT FITTING BS 967, RBL 50. MAINTENANCE REMOVED AND REPLACED R/H AFT LAVATORY INBOARD FORWARD MOUNT FITTING BS 967, RBL 50, IAW B737-300 SRM 51 -40-02, PG. 6-10, AND SRM 53-60-51, PG. 106-113. 2 L 7 2 4F RT A16WE 2002081300176 20020813 00176 NM 2002 8 13 AWXA200200739 1 20020729 A 5345 65B578393 FITTING BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 0 0 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON L/H AFT LAVATORY OUTBOARD FORWARD MOUNT FITTING BS 967, LB L 60. MAINTENANCE REMOVED AND REPLACED L/H AFT LAVATORY OUTBOARD FORWARD MOUNT FITTING BS 967, LBL 60, IAW B737-300 SRM 51-40-02, PG. 6-10, AND SRM 53-60-51, PG. 106-113. 2 L 7 2 4F RT A16WE 2002081300177 20020813 00177 NM 2002 8 13 AWXA200200740 1 20020729 A 5345 65B578393 FITTING BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 0 0 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON R/H AFT LAVATORY OUTBOARD FORWARD MOUNT FITTING BS 967, RB L 60. MAINTENANCE REMOVED AND REPLACED R/H AFT LAVATORY OUTBOARD FORWARD MOUNT FITTING BS 967, RBL 60, IAW B737-300 SRM 51-40-02, PG. 6-10, AND SRM 53-60-51, PG. 106-113. 2 L 7 2 4F RT A16WE 2002090300145 20020903 00145 NE 2002 9 3 02081301 2 20020813 A 7320 44A2562 SWITCH BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE NR 2 ENGINE FAILED A N8TA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 19 543NA 28161 31426 IN FLIGHT: RIGHT ENGINE SPOOLED BACK OVER A PERIOD OF ABOUT 5 MINUTES. ABOUT 3 INCH SPLIT IN THRUST LEVERS TO SYNC N1'S . ADVISED BY MAINTENANCE CONTROL TO SWITCH OFF ELC ON NR 2 ENGINE. APPEARED TO RETURN TO NORMAL. PRECAUTIONARY LANDIN G MADE. TROUBLESHOOTING IN PROGRESS AT THIS TIME. REMOVED AND REPLACED ALTITUDE SWITCH, RIGHT ENGINE, AS PER M/M 75-32 -07. AIRBORNE SYSTEM TEST OF EEC AND ENG LIMITER CONDUCTED AS PER M/M 71-00-00, ALL SYSTEMS CHECK GOOD. AIRCRAFT RELEAS ED FOR RETURN TO SERVICE 2 L 7 2 4F 4 F RT A2NM E12EU 2002081400001 20020814 00001 NM 2002 8 14 PCAA0208093 1 20020813 A 7931 PW120A ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RIGHT LEAKING A PCAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 13 842EX 23417 15696 341 121088 SCE-PIT FLIGHT#3825. CREW REPORTED LOSS OF OIL PRESSURE ON #2 ENGINE. ENGINE SHUT DOWN AND EMERGENCY DECLARED. MAINTENAN CE FOUND A CUT O RING ON TRANSFER TUBE BETWEEN OIL PRESSURE REGULATOR AND MAIN OIL FILTER. O RING REPLACED. MAIN AND SCA VANGE OIL FILTERS REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL. NO FLAGS NOTED ON ENGINE CONDITION PANEL. GROUND RAN A IRCRAFT FOR TEN MINUTES, LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002081400002 20020814 00002 NE 2002 8 14 ERAA080473 1 20020716 A 6510 S613564003 DRIVE SHAFT SKRSKY S61 S61N 8142104 NE TAIL ROTOR VIBRATION H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 562EH 12360 61257 T/R DRIVESHAFT HAS EXCESSIVE VIBRATIONS. SENT TO ACRO FOR REPAIR TWO COLLARS/BUSHINGS FOUND OUT OF CONCENTRICITY BY .00 65 INCH MAX ALLOWABLE - 002 INCH. SHAFT STRAIGHTENED TO WITHIN TOLERANCE WAS .95 INCH IS NOW .006 INCH TWO COLLARS RE PLACED. 2 G 7 2 4U 1H15 2002081400003 20020814 00003 GL 2002 8 14 ERAA080474 2 20020717 A 7320 252466714 SHAFT BOLKMS 105 BO105A EU ALLSN 250C 250C18 03011 GL GOVERNOR STIFF H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 291EH 4620 S842 THROTTLE SHAFT STIFF. THROTTLE BUSHING, REPLACED WITH NEW, AND GOVERNOR WAS RE-CALIBRATED TO FINAL CALIBRATION LIMI TS. 1 G 7 2 3U 3 U H3EU E4CE 2002081400004 20020814 00004 GL 2002 8 14 ERAA080475 2 20020717 A 7320 252466715 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C18 03011 GL ENGINE MALFUNCTIONED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 130EH 5322 558 TORQUE SPLITS - SPEEDS UP AND ADJ MAX BEEP TO 99 PERCENT N2. THEN WAS TEST FLOWN - CHECKED MAX BEEP AT 96 PERCENT - ADJ TO 99 PERCENT AND HOVER A/C MAX BBEP FELL AGAIN TO 95 PERCENT. SENT TO ACRO FOR REPAIR. FOUND EXCESSIVE DROOPING, BEYO ND SERVICE LIMITS, ROUGH BEARINGS INTERNALLY, THROTTLE SHAFT BUSHING LOOSE. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-1095A. 1 G 7 2 3U 3 U H3EU E4CE 2002081400005 20020814 00005 GL 2002 8 14 ERAA080476 2 20020717 A 7320 SHAFT BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C18 03011 GL GOVERNOR STIFF H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 131EH 10572 595 STIFF THROTTLE SHAFT. ROUGH/ DRY INTERNAL BEARINGS. ACTION TAKEN: SENT TO ACRO FOR REPAIR. REPAIRED AND TESTED IAW HO NEYWELL OHM FORM 15-1095A. 1 G 7 2 3U 3 U H3EU E4CE 2002081400006 20020814 00006 SW 2002 8 14 ERAA080477 1 20020717 A 6230 412040366105 MAST BELL 412 412 1182202 SW MAIN ROTOR MAKING METAL H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 418EH 1451 MAKING METAL. MAST BEARING BREAKING DOWN. REMOVED MAST BEARING VISUALLY INSPECTED, EXPOSED COMPONENTS. INSTALLED SWIT CH, BEARING, NEW SEAL AND SLEEVE, REASSEMBLED. MAST ASSY REPAIRED IAW BHT 412 CR&O 63. COMPLIED WITH TB 412-98-150 1 G 7 2 4U H4SW 2002081400007 20020814 00007 GL 2002 8 14 ERAA080478 2 20020718 A 7320 252466715 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C18 03011 GL ENGINE MALFUNCTIONED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 130EH 11502 558 TORQUE SPLITS UP TO 30% IN CRUISE FLIGHT. GOVERNOR REPAIRED AND TESTED SERVICEABLE IAW HONEYWELL OHM FORM 15-1095A. CE B'S A-1353R2 AND 1384 FOUND N/A BY UNIT S/N. 1 G 7 2 3U 3 U H3EU E4CE 2002081400008 20020814 00008 GL 2002 8 14 ERAA080479 2 20020718 A 7250 6898735 TURBINE WHEEL BOLKMS 105 BO105A EU ALLSN 250C 250C18 03011 GL ENGINE DAMAGED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 135EH 11342 S675 UNIT HAS LOW POWER. NR 4 NOZZLE AND NR 3 WHEEL CRACKED. INSTALLED NEW NR 3 & 4 WHEEL AND NEW NR 4 NOZZLE. C/W CEB-136 0; RE-COAT INNER SHAFT. 1 G 7 2 3U 3 U H3EU E4CE 2002081400009 20020814 00009 GL 2002 8 14 ERAA080480 2 20020718 A 7230 6870811 DIFFUSER BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C18 03011 GL COMPRESSOR DAMAGED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 131EH 595 ALUMINUM DAMAGED BY IMPELLER. REMOVED AND RE-APPLIED PLASMA SPRAY ON CONTOUR. (OVERHAULED). 1 G 7 2 3U 3 U H3EU E4CE 2002081400010 20020814 00010 EU 2002 8 14 FF62002F00000 1 20020611 A 7710 39957213 INDICATOR SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT READS HIGH B FF6R K NONE O OTHER IN INSP/MAINT 1 NM 11 407EM 266 1906 N/R INDICATOR READS TOO HIGH. 1 G 7 1 3U 3 U H9EU E19EU 2002081400011 20020814 00011 SO 2002 8 14 FPI2002F00009 2 20020729 A 7414 6310 IMPULSE COUPLING CESSNA 210 210L 2073448 CE CONT O520 IO520* 17032 SO MAGNETO FAILED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 7874J 1119 21060597 295086R IMPULSE COUPLING FAILED ON MAGNETO. MAGNETO SEPARATED FROM ENGINE, RESULTING IN METAL CONTAMINATION OF ENGINE. ENGINE REMOVED FOR INSPECTION AND OVERHAUL. 1 H 7 1 3O 3 O 3A21 E5CE 2002081400012 20020814 00012 EA 2002 8 14 GIK2002F00000 1 20020424 A 5511 C2TP183 RIB DHAV DHC2 DHC2MK3 2800107 EA HORIZONTAL STAB CRACKED B GIKR K NONE O OTHER IN INSP/MAINT 1 NM 01 227N 332 1686TB54 BOTH HORIZONTAL STABILIZER END CAP RIBS LT AND RT WERE FOUND CRACKED DURING ANNUAL INSPECTION. THIS RIB HAD BEEN MODIFI ED UNDER STC SA456NW ON JAN 25-2000. TOTAL TIME ON PART IS 332 HOURS. AIRCRAFT HAS BEEN OPERATING UNDER NORMAL CONDITI ONS. 1 H 7 1 3T A806 2002081400013 20020814 00013 EU 2002 8 14 IO5R080457 1 20020806 A 6730 L673M40A1001 ACTUATOR UROCOP EC135 EC135P1 8680990 EU TAIL ROTOR DEFECTIVE H IO5R K NONE O OTHER IN INSP/MAINT 1 FS 01 552BA 255 190 SERVO UNIT LEAKING INTO FENESTRON GEARBOX OIL REMOVED AND REPLACED RMA RO38197 1 G 7 2 3U O H88EU 2002081400014 20020814 00014 EU 2002 8 14 IO5R080458 1 20020807 A 6330 L633M2010101 MOUNT UROCOP EC135 EC135P1 8680990 EU MAIN ROTOR DEFECTIVE H IO5R K NONE O OTHER IN INSP/MAINT 1 FS 01 552BA 270 190 Z-ARIS MOUNT COLLAPSED REMOVED AND REPLACED 1 G 7 2 3U O H88EU 2002081400015 20020814 00015 SW 2002 8 14 JJW2002F00000 1 20020712 A 5320 206031106017S STIFFENER BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUSELAGE CRACKED E JJWA K NONE O OTHER IN INSP/MAINT 1 SO 17 281CB 10354 3303 FOUND STIFFNER CRACKED DURING INSPECTION - CRACK ORIGINATED IN LOWEST HI-LOCK FASTENER POSITION 2.875 INCH BELOW TOP OF PART. ALSO SPLICED NEW WEB (PN 206031106349S) DUE TO CRACK IN WEB FROM SAME LOCATION. REPLACED STIFFNER. ALL WORK I AW SRM. 1 G 7 1 3U 3 U H2SW E4CE 2002081400018 20020814 00018 GL 2002 8 14 PG92002F00002 2 20020626 A 7250 23031493 SEAL BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL TURBINE DAMAGED B PG9R K NONE O OTHER IN INSP/MAINT 1 WP 19 178PA 45319 CAE890697 TURBINE REMOVED AND REPLACED DUE TO SMOKING DURING SHUTDOWN. 1 G 7 1 3U 3 U H2SW E1GL 2002081400019 20020814 00019 GL 2002 8 14 PG92002F00003 2 20020701 A 7321 23065147 FUEL CONTROL BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL ENGINE SURGES B PG9R K NONE O OTHER IN INSP/MAINT 1 WP 19 5743C 45474 CAE890697 ENGINE FUEL CONTROL REMOVED AND REPLACED DUE TO COMPRESSOR SURGE FROM 62 PERCENT TO 100 PERCENT. 1 G 7 1 3U 3 U H2SW E1GL 2002081400020 20020814 00020 WP 2002 8 14 PHA2002F00000 1 20020523 A 6320 369A5358 LOCKWASHER HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL CLUTCH ASSY CRACKED D PHAA K NONE O OTHER IN INSP/MAINT 1 NM 13 69PF 1425 1060012D CAE830354 DURING 100 HOUR INSPECTION CLUTCH (PN 369A5350-51) WAS REMOVED FOR SERVICE. LOCK WASHER (PN369A5358) WAS FOUND TO HAVE CRACKED IN 3 PLACES, THIS ALLOWED THESE FRAGMENTS TO SLING OUT FROM THE CLLUTCH WHICH TURNS AT 6200 RPM AND RIDE AGAINS T THE INTERIOR OF THE CLUTCH SUPPORT HOUSING (PN 369A5351). THE LOCK WASHER FRAGMENTS CUT A GROOVE .7500 OF THE TOTAL W ALL THICKNESS OF THE HOUSING AWAY. THIS IMBALANCE CAUSED THE CARRIER BEARING (PN 369A5361 TO BE OUT OF BALANCE AND IT R EQUIRED REPLACEMENT. THE LOCKWASHER WAS REPLACED 181.9 HOURS PRIOR TO FAILURE DURING A SCHEDULED 300 HOUR CLUTCH INSPEC TION. 1 G 7 1 3U 3 U H3WE E4CE 2002081400021 20020814 00021 CE 2002 8 14 RNV2002F00000 1 20020719 A 3230 MS24665153 COTTER PIN CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO LT MLG MISSING E RNVA O OTHER O OTHER LD LANDING 1 WP 13 816PW 402C0261 ON LANDING THE LT MAIN GEAR LOWER AND UPPER TORQUE LINKS SEPARATED AT THE CONNECTING BOLT. I FEEL THAT THE COTTER PIN C AME OUT, WHICH ALLOWED THE NUT TO UNSCREW FROM THE BOLT, LETTING THE BOLT TO FALL OUT OF THE TORQUE LINKS. I WOULD RECO MMEND CLOSER INSPECTION BY MAINTENANCE PERSONNEL AND PILOTS ON PREFLIGHTS. PLUS REPLACEMENT OF COTTER PINS AT ONE YEAR INTERVALS. 1 L 7 2 3O 3 O A7CE E8CE 2002081400026 20020814 00026 EU 2002 8 14 TI12002F00001 1 20020513 A 2997 85106RT1419P CONNECTOR BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101600A 41560 NE HYD SYSTEM CORRODED B TI1R A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 05 117TX 7177 INTERMITTENT ILLUMINATION OF MASTER CAUTION LIGHT ALONG WITH HYD 2 WARNING LIGHT. NO FEEDBACK OR FLIGHT CONTROL ABNORMA LITIES WEAR NOTED. HYDRAULIC PRESSURE WAS NORMAL AND STEADY. MASTER CAUTION WAS RESET AND HYD 2 LIGHT ILLUMINATED AGAI N, WITH PRESSURE FLUCTUATION. PROBLEM CORRECTED ITSELF WITHIN A FEW SECONDS. ABOUT 10 MINUTES LATER MASTER CAUTION HYD 2 LIGHTS ILLUMINATED AGAIN, ACCOMPANIED WITH BOTH HYDRAULIC SYSTEM PRESSURE DOWN TO 50 BARS. NO FEED BACK IN FLIGHT CO NTROLS WERE NOTED. A PRECAUTIONARY LANDING WAS MADE. HYD SYSTEM WAS INSPECTED AND CORROSION WAS FOUND ALONG WITH MOIST URE, ON BOTH HYD SYSTEM. PRESSURE TRANSDUCER CONNECTOR PLUGS. THEY WERE CLEANED AND NO FURTHER DISCREPANCIES WERE NOTE 1 G 7 2 3U 3 U H13EU E5NE 2002081400027 20020814 00027 SW 2002 8 14 TI12002F00002 1 20020522 A 6220 407310102101 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR SEPARATED B TI1R A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SW 05 2022Y 2224 53281 AN ABNORMAL INTERMITTENT VIBRATION WAS FELT DURING CRUISE FLIGHT. THE CAUSE WAS DETERMINED TO BE THE OUTBOARD MAIN ROTO R GRIP ELASTOMERIC BEARING ON ONE BLADE GRIP TO HAVE SEPARATED. THE OTHER THREE ELASTOMERIC BEARING WERE INSPECTED, AND FOUND TO HAVE VARIOUS STAGES OF SEPARATION. ALL FOUR OUTBOARD ELASTOMERIC BEARING WERE REPLACED. THE MAIN ROTOR HUB A SSEMBLY HAD ONLY 275 HOURS REMAINING UNTIL THE FIRST SCHEDULED OVERHAUL. THE INBOARD ELASTOMERIC BEARING WERE ALSO CHAN GED DURING THIS MAINTENANCE EVENT DUE TO DETERIORATION OF THE RUBBER BONDING. 1 G 7 1 3U 3 U O H2SW E1GL 2002081400029 20020814 00029 EU 2002 8 14 MALA020439 1 20020729 A 7931 83465 SENSOR SAAB SF340 340B 7860101 EU LT ENGINE MALFUNCTIONED A MALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 447XJ 340B447 DURING TAXI OUT ON FLIGHT 2943, LT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. PRESSURE AND TEMPERATURE NORMAL. AFTER R ETURNING, MAINTENANCE REPLACED LT ENGINE OIL PRESSURE SENSOR, OPS CHECK GOOD AMM 79-30-05-4. 2 L 7 2 4T RT A52EU 2002081400030 20020814 00030 EU 2002 8 14 USOM103282 1 20020514 A 6220 35A31190703 STARFLEX SNIAS 350 AS350B2 8680813 EU MAIN ROTOR CRACKED C U0SM K NONE O OTHER IN INSP/MAINT 1 SW 03 5204X 3099 UPON INSPECTING PART DURING (T) 500 HOUR INSPECTION, FOUND CRACKED PAINT 2 INCHES FROM ONE END OF STARFLEX. INVESTIGAT ION REVEALED A 20 MM LONG X 4 INCH HIGH VOID IN THE FIBERGLASS. VOID APPEARS TO HAVE BEEN A MANUFACTURING DEFECT. 1 G 7 1 3U H9EU 2002081400031 20020814 00031 EU 2002 8 14 USOM117002 1 20020606 A 6510 350A34021006 DRIVE SHAFT SNIAS 350 AS350B2 8680813 EU TAIL ROTOR SLIPPED C U0SM K NONE O OTHER IN INSP/MAINT 1 SW 03 5204Y 981 3101 INSTALLED SHAFT IN AIRCRAFT AND COMPLIED WITH INITIAL BALANCE RUN, AFT BEARING SLIPPED ON SHAFT AND EXCESSIVE HEAT ON AL L BEARINGS. CLEANED AND REINDEXED BEARING, ON SECOND RUN, 3 BEARINGS SLIPPED EXCESSIVELY AND COPIUS AMOUNTS OF GREASE S LUNG FROM ALL BEARING AND ALL WERE VERY HOT. 1 G 7 1 3U H9EU 2002081400033 20020814 00033 NM 2002 8 14 DL767020785 1 20020710 A 2910 272T4500387 LINE BOEING 767 767232 1385132 NM RT W/W SPLIT A DALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 27 101DA 22213 ON CLIMBOUT, 'C' SYS HYD QTY MSG ACTIVATED. 'C' SYS QTY CK'D AT 0.31 FOUND BROKEN LINE IN RT UPPER OUTBD W/W. RPLD SAME 2 L 7 2 4F RT A1NM 2002081400034 20020814 00034 NM 2002 8 14 DL757020816 1 20020713 A 5330 146N37506 SKIN BOEING 757 757232 1384965 NM FS 1670, S-18R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 607DL 22814 FUSELAGE / SKIN / FS 1661-1680 / STRG. 18R-19R : DENT REPAIR THE FUSELAGE SKIN BETWEEN FS 1661 & 1680 AND BETWEEN STRINGERS 18R & 19R WAS FOUND DENTED. THE DENT WAS REMOVED WITH A CUTOUT AND REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 383296-14, REV A. 2 L 7 2 4F RT A2NM 2002081400035 20020814 00035 NM 2002 8 14 DL757020817 1 20020713 A 5330 141N38517 SKIN BOEING 757 757232 1384965 NM FS 280, WL 205 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 607DL 22814 FUSELAGE / SKIN / FS 278-288 / WL 200-208 : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED BETWEEN FS 278 & 288 AND BETWEEN WL 200 & 208. THE DENT WAS REMOVED WITH A 5" X 5.2" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383331-14, REV A. 2 L 7 2 4F RT A2NM 2002081400036 20020814 00036 NM 2002 8 14 DLM88020822 1 20020716 A 2700 UNK AILERON DOUG MD88 MD88 3023688 NM WINGS STIFF A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 935DL 49722 DURING CLB-OUT EWR PILOT NOTED AILERONS FELT VERY STIFF. AILERON REPONSE WAS NORMAL. FLIGHT RETURNED TO EWR. PILOT REPO RTED AILERON FELT NORMAL ON APPROACH TO EWR. MTC INSPECTED AILERON SYSTEM WITH NO OBVIOUS DEFECTS NOTED. LUBRICATED AIL ERON MECHANISM IN MAIN WHEEL WELL. FLT CONTROL CHECK NORMAL. 2 L 7 2 4F RT A6WE 2002081400037 20020814 00037 NM 2002 8 14 DL72S020831 1 20020718 A 5700 UNK ANGLE BOEING 727 727232 1384082 NM RT WING 5 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND ON E1 L/C 1.25 INCH CRACK NBR 5 SLAT COVE SKIN ATTACH ANGLE AT INBD END REPAIRED PER M/M57-54-000-8 FIG 805A 2 L 7 3 4F A3WE 2002081400038 20020814 00038 NM 2002 8 14 DL72S020832 1 20020718 A 5700 UNK ANGLE BOEING 727 727232 1384082 NM NBR 6 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND ON E1 LETTER CK. 1 INCH CRACK AT COVE SKIN ATTACH ANGLE NBR 6 SLAT BELOW ACTUATOR ROD REPAIRED PER M/M 57-54-000-8 FIG 805A, 2 L 7 3 4F A3WE 2002081400039 20020814 00039 NM 2002 8 14 DL757020838 1 20020716 A 5330 146N34102 SKIN BOEING 757 757232 1384965 NM FS 1617, S-17R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 607DL 22814 FUSELAGE / SKIN / FS 1617 / STRG. 17R : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED AT FS 1617 JUST BELOW STRINGER 17R. THE DENT WAS REMOVED WITH A CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 383406-14, REV A. 2 L 7 2 4F RT A2NM 2002081400040 20020814 00040 NM 2002 8 14 DL757020839 1 20020716 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FS 598, S-14L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 607DL 22814 FUSELAGE / SKIN / FS 598 / STRG. 14L-15L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS DENTED AT FS 598 BELOW THE STRINGER 14L SKIN LAP JOINT. THE DENT WAS REMOVED WITH A CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 383418-14, REV A. 2 L 7 2 4F RT A2NM 2002081400041 20020814 00041 NM 2002 8 14 DL76S020842 1 20020718 A 5330 141T3230 SKIN BOEING 767 767332 1382001 NM FS 290, S-37R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 124DE 23438 FUSELAGE / SKIN / FS 287-303 / STRG. 37R : DENT REPAIR THE FUSELAGE SKIN WAS DENTED AT THE STRINGER 37R SKIN LAP JOINT BETWEEN FS 287 & 303. THE LAPJOINT WAS CUTOUT IN THE AREA TO REMOVE THE DENT. THE CUTOUT WAS REPAIRED WITH 2 ALUMINUM EXTERNAL DOUBLERS PER ER/A 383469-14. 2 L 7 2 4F RT A1NM 2002081400042 20020814 00042 NM 2002 8 14 DL72S020844 1 20020719 A 5700 UNK ANGLE BOEING 727 727232 1384082 NM #6 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 546DA 22677 FOUND ON F1 LETTER CK LOWER COVE SKIN ATTACH ANGLE IS CRACKED AT NUMBER 6 SLAT BELOW ACTUATOR. REPAIRED PER MM 57-54-000-8 2 L 7 3 4F A3WE 2002081400043 20020814 00043 NM 2002 8 14 DL72S020845 1 20020719 A 5700 UNK RIB BOEING 727 727232 1384082 NM #4 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 546DA 22677 AT F-1 LETTER CK FOUND DOUBLER CRACKED #4 SLAT INBD ACTUATOR ATTACH NOSE RIB FOUND DOUBLER INCORRECTLY SHIMMED, RESHIMED AND REPLACED DOUBLER PER M/M 57-54-000-8 FIG 804 2 L 7 3 4F A3WE 2002081400044 20020814 00044 NM 2002 8 14 DL738020856 1 20020722 A 3320 8200048701 SIGN BOEING 737 737832 13844CF NM AFT GALLEY LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 386DA 30373 REAR GALLEY CENTER OVERHEAD EMERGENCY SIGN LOOSE. SECURED EMERGENCY EXIT SIGN. CKS OK. 2 L 7 2 4F RT A16WE 2002081400045 20020814 00045 NM 2002 8 14 DL73K020868 1 20020726 A 5310 654653949 FRAME BOEING 737 737247 138448D NM STA 616 WL202 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 375DL 23602 FUSELAGE FRAME AT STA 616 LH/RH WERE CRACKED IN IN BD/OUTBD FLANGEAT LOCATION ATTACHING TO FLOOR STUB BEAM. D AMAGE WAS FOUND DURING INSPECTION PER SI 3-85751-12. CORRECTIVE ACTION: DAMAGE WAS REPAIRED PER ER/A 383607-14. 2 L 7 2 4F A16WE 2002081400046 20020814 00046 NM 2002 8 14 DL733020869 1 20020726 A 5330 6545774594 SKIN BOEING 737 737347 1384647 NM STA 727D+15 S22R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 DURING INSPECTION PER OPN 57512 CRACK WAS FOUND IN THE SKIN AT STATION 727D+15 AND STR-22R. CORRECTIVE ACTION: REPAIRED PER ER/A 383586-14. 2 L 7 2 4F RT A16WE 2002081400047 20020814 00047 NM 2002 8 14 DL733020870 1 20020726 A 5330 6545774575 SKIN BOEING 737 737347 1384647 NM STA727E+15 S22L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 DURING INSPECTION PER OPN 57512 SKIN CRACK WAS FOUND AT STATION 727E+15 AND STRINGER 23L. CORRECTIVE ACTION: REPAIRED PER ER/A 383585-14. 2 L 7 2 4F RT A16WE 2002081400048 20020814 00048 2002 8 14 DL767020872 4 20020726 A 3420 INDICATOR 6227998003 BOEING 767 767232 1385132 NM CAPTAIN/LEFT OVERHEATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 102DA 2002 22214 CAPTAIN EADI WENT BLANK. SELECTED ALT EFI AND INDICATOR REMAINED BLANK. ABOUT 5 MINUTES LATER SMOKE WAS SEEN COMING FROM CAPTAIN EADI. PULLED C/B E3 AND SMOKE STOPPED. REMOVED LEFT ADI INSPECTED CONNECTORS NO DAMAGE FOUND. REPLA LEFT ADI WITH SEVISBLE UNIT PER MM 34-22-03-04. OPERATION NORMAL. 2 L 7 2 4F RT A1NM 2002081400049 20020814 00049 NM 2002 8 14 DL757020875 1 20020726 A 3300 767 BULB BOEING 757 757232 1384965 NM EXTERIOR L1 DOOR BURNED OUT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 6712B 30484 ON LAYOVER FOUND DOOR L1 EXTERIOR EMERGENCY LIGHT BURNED OUTREPLACED BULB. LIGHT OPERATES NORMAL 2 L 7 2 4F RT A2NM 2002081400050 20020814 00050 NM 2002 8 14 DL76S020887 1 20020729 A 2900 000AE968D0165 LINE BOEING 767 767332 1382001 NM RT ACMP TO FLTR LEAKING A DALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 27 127DL 24077 RT HYD QUANITY SYSTEM TO ZERO RETURN TO LAS VEGAS CA FND LINE TO RT ACMP LEAKING, RPLD SAME. 2 L 7 2 4F RT A1NM 2002081400051 20020814 00051 NM 2002 8 14 DL757020891 1 20020730 A 7100 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE #2 ENGINE FAILED A DALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE TO TAKEOFF 1 SO 27 677DL 4241 0 25982 727054 RT ENG FAIL AT APPROX 500FT ON T/O FROM SNA ACFT. WT. 213000 FLAPS 20 DEG CA BOROSCOPED ENG FOUND 15TH-17TH STG HPC DAMAGED BEYOND LILIMITS. ENGINE CHG REQUIRED. RIILAX029439. REPL RT ENG. RAN PER PFHB. ALL CKS NML 2 L 7 2 4F 4 F RT A2NM E17NE 2002081400052 20020814 00052 NM 2002 8 14 DLM88020909 1 20020805 A 2780 59388301 CASTING 59388301 DOUG MD88 MD88 3023688 NM L/E WING 0 SLAT BROKEN A DALA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SO 27 995DL NA 53362 LEFT WING PULLEY SUPPORT CASTING BROKEN AFT OF 0 SLAT STA XCW 121. CABLE FRAYED SAME LOCATION CABLE 209 SEG B ZERO SLAT EXTEND CABLE. N/R CARD 70 FOUND DURING LETTER CK J-1 CA RPLD SUPPORT CASTING AND CABLE. 2 L 7 2 4F RT A6WE 2002081400053 20020814 00053 NM 2002 8 14 DLM88020911 1 20020805 A 5330 5920323249 SKIN DOUG MD88 MD88 3023688 NM STA 437 @ L-20R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 963DL 49982 DURING HMV-2, INSPECTION FOUND A DENT IN THE FUSELAGE SKIN FROM STA 435 TO STA 439 @ L-20R. THE C1 DOOR INTERNAL SURROUN D DOUBLER WAS NOT DAMAGED. THE DENT WAS REMOVED RESULTING IN A CUTOUT MEASURING 4.375 INCHES (FWD/AFT) X 2.125 INCHES (U P/DOWN). A DOUBLER REPAIR WAS ACCOMPLISHED PER MD-88 SRM 53-04, FIGURE 12B, SHEET 4 (CLASS 1 EXTERNAL REPAIR), EXCEPT TH E UPPER & LOWER FINGER DOUBLERS WERE ENDED AT THE C1 DOOR INTERNAL DOUBLER. 2 L 7 2 4F RT A6WE 2002081400054 20020814 00054 NM 2002 8 14 DL76S020915 1 20020805 A 7100 332T12296 DUCT BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE #2 ENGINE WORN A DALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 27 139DL 25984 580398 AIR TURN BACK RT ENG OVERHEAT MSG AFTER TAKEOFF. FOUND 8TH STAGE DUCT SEPERATED ON NO.2 ENG. REPLCD DUCT BETWEEN CK VLV AND PRECOOLER. 2 L 7 2 4F 4 F RT A1NM E13NE 2002081400055 20020814 00055 NM 2002 8 14 DL72S020916 1 20020806 A 5314 655848826 STRINGER BOEING 727 727232 1384082 NM S-18A, FS 950 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 FUSELAGE / STRINGER / 18A / FS 920-950 : FATIGUE CRACK REPAIR STRINGER 18A WAS FOUND WITH A 4" TYPICAL FATIGUE CRACK AT FS 950. THE STRINGER WAS CUT AT FS 921 AND THE AFT END REMOVED TO ELIMINATE ALL CRACKS. A NEW SECTION OF STRINGER WAS SPLICED IN PER BAC S/B 727-053-0172 AND ER/A 383648-14. 2 L 7 3 4F A3WE 2002081400056 20020814 00056 NM 2002 8 14 DLM88020939 1 20020809 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM FS 650, L-30 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DL 49542 FUSELAGE / SKIN / FS 650 / L29-30 : CORROSION NEAR ANTENNA CUTOUT THE FUSELAGE SKIN WAS FOUND WITH A CORROSION BULGE AT AN EXISTING ANTENNA CUTOUT AT FS 655 AND LONG. 30. THE CORROSION WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383678 -14, REV A. 2 L 7 2 4F RT A6WE 2002081400057 20020814 00057 SO 2002 8 14 WVBA2002014 1 20020710 A 2140 A23D04 REGULATOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HEATER LEAKING E WVBA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 4082T 959 318152089 DURING INSPECTION EVENT FUEL WAS OBSERVED COMING OUT OF THE DRAIN FOR THE COMBUSTION HEATER. THE FUEL PRESSURE REGULATO R WAS REMOVED AND FOUND TO LEAKING FROM PARTING SURFACE. PART WAS REPLACED PER SB. RECOMMEND MACHING THE HOUSING AND U SING AN (ORING TYPE SEAL). 1 L 7 2 3O 3 O A20SO E14EA 2002081400058 20020814 00058 EA 2002 8 14 WVBA2002015 2 20020724 A 7314 RG9080J4AM PUMP PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA FUEL SYSTEM INOPERATIVE E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 4082T 677 318152089 DURING POST INSPECTION GROUND RUN, IT WAS OBSERVED THAT THE RIGHT ENGINE WOULD NOT RUN WITH OUT BOOST PUMP ASSISTANCE. WHEN REMOVED IT WAS NOTED THAT THE SHAFT ROTATED WITH ROUGHNESS. PUMP WAS REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 2002081400059 20020814 00059 EU 2002 8 14 MALA020440 1 20020730 A 3230 HP848430621 CONTROL VALVE SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION LD LANDING 1 GL 15 425XJ 340B425 ON FINAL APPROACH ON FLIGHT 3167, LANDING GEAR WOULD NOT EXTEND. ON ARRIVAL SELECTED GEAR DOWN, NO LIGHTS (GREEN) ILLUM INATED, INTRANSIT LIGHT ILLUMINATED. PERFORMED QRH, DIRECTED TO PULL EMERGENCY GEAR EXTENSION HANDLE. PULLED HANDLE AN D GOT THREE GREEN. MAINTENANCE REPLACED LANDING GEAR CONTROL VALVE IAW CHAP 32. REPLACED BOTH LT & RT SEPARATION BOLTS ALL IAW SF340 CHAPTER 32. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2002081400060 20020814 00060 2002 8 14 MALA020441 4 20020801 A 3442 6227337001 TRANSPONDER SAAB SF340 340B 7860101 EU WEATHER RADAR FAILED A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 425XJ 340B425 DURING FLIGHT 3016, WEATHER RADAR INOP. AIR TURNBACK TO DTW. MAINTENANCE REMOVED AND REPLACED WEATHER RADAR TRANSPONDE R. OPS CHECK GOOD IAW THE SF340 MM. 2 L 7 2 4T RT A52EU 2002081400061 20020814 00061 NE 2002 8 14 MALA020442 2 20020803 A 7323 GOVERNOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A1 30030 NE LT ENGINE MALFUNCTIONED A MALA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 GL 15 76XJ 340A076 LEFT ENGINE BOTTOM GOVERNORS WOULD NOT ENGAGE ON FLIGHT 2790. A/C RETURNED TO GATE. MAINTENANCE PERFORMED TEST OF LT G EN AND LT BOTTOMING GOVERNOR IAW SAAB AMM 71-00-00-5. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2002081400062 20020814 00062 2002 8 14 MEX2002225 4 20020718 A 3443 TRANSCEIVER DOUG MD88 MD88 3023688 NM RADAR UNIT OVERHEATED W ASMF K NONE L M NO TEST OVER TEMP IN INSP/MAINT 1 SW 23 158PL 49761 RADAR OUT OF SERVICE. TESTED ON GROUND AND CONFIRMED FAILURE. TRANSCEIVER WAS CHECKED AND AN OVER TEMPERATURE INDICATI ON WAS FOUND. TRANSCEIVER WAS REMOVED AND REINSTALLED WHEN IT REACHED A COOLER TEMPERATURE, THE OVER TEMPERATURE INDICA TOR WAS RESET BUT THOSE ACTIONS DID NOT CORRECT PROBLEM. 2 L 7 2 4F RT A6WE 2002081400063 20020814 00063 EU 2002 8 14 MALA020444 1 20020805 A 3010 BOOT SAAB SF340 SF340A 7850100 EU DE-ICE SYS WILL NOT TEST A MALA D RETURN TO BLOCK L NO TEST NR NOT REPORTED 1 GL 15 48XJ DURING TAXI ON FLIGHT 3182, DEICE BOOTS WILL NOT TEST. MAINTENANCE INSPECTED AND DEFERRED. 2 L 7 2 4T RT A52EU 2002081400064 20020814 00064 EU 2002 8 14 MALA020445 1 20020805 A 3150 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A1 30030 NE COCKPIT ACTIVATED A MALA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 GL 15 106XJ 340A106 DURING TAXI OUT ON FLIGHT 3064, LT AIR VALVE LIGHT ILLUMINATED AFTER TAXI. A/C RETURNED TO GATE. MAINTENANCE DEFERRED. NO OTHER INFORMATION AVAILABLE NOW. 2 L 7 2 4T 4 T RT A52EU E8NE 2002081400065 20020814 00065 EU 2002 8 14 RAIA00207216 1 20020715 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 421TE 102 STL- EMERGENCY LIGHT ON STAIRS IS OUT. MAINTENANCE REPAIRED BROKEN WIRE ON PAX DOOR EMERGENCY LIGHT. 2 H 7 2 4T RT A53EU 2002081400066 20020814 00066 NE 2002 8 14 MEX2002230 2 20020719 A 7230 COMPRESSOR WHEEL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RT ENGINE DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 1003X 48067 DURING PREFLIGHT CHECK, FOUND SEVERAL DAMAGED BLADES OF RIGHT ENGINE DUE TO ADVERSE METOROLOGICAL CONDITION ON ROUTE. DISK C1 WAS REPLACED IAW MM, NOSE COWLING IAW MM AND BULLET ASSY. TESTED OK. 2 L 7 2 4F 4 F A6WE E9NE 2002081400067 20020814 00067 EU 2002 8 14 RAIA00207223 1 20020721 A 7712 BRIDGE JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE MALFUNCTIONED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 553HK 41066 ROC- RIGHT ENGINE WILL NOT MAKE TORQUE. MAINTENANCE CHANGED TORQUE BRIDGE FROM POSITION NR 1 TO 2, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002081400068 20020814 00068 EU 2002 8 14 RAIA00207224 1 20020721 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY EXIT OUT OF ADJUST A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 564HK 41081 RIC- EMERGENCY EXIT WARNING ILLUMINATED. MAINTENANCE ADJUSTED REAR EMERGENCY EXIT MICROSWITCH, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002081400069 20020814 00069 NE 2002 8 14 MEX2002237 2 20020724 A 7321 76960615 FUEL CONTROL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D217 52053 NE LT ENGINE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 169PL 26591 53175 AIRCRAFT RETURNED TO PLATFORM DURING TAXI DUE TO AN INDICATION OF 500 DEGREES IN EGT ON THE LEFT ENGINE. FCU WAS ADJUST ED IAW MM AND TESTED OK. FCU WAS REPLACED BY N1, N2 AND EPR OSCILATIONS. TESTS WERE PERFORMED IAW MM. 2 L 7 2 4F 4 F RT A6WE E9NE 2002081400070 20020814 00070 WP 2002 8 14 MEX2002238 1 20020724 A 4920 3812761 ENGINE DOUG DC9 DC987 3022087 WP APU FAILED W ASMF O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 23 214AM 22596 49585 CREW REPORTED THE PRESENCE OF SMOKE IN CABIN DUE TO AN OIL LEAK IN THE LT A/C PACK. THE MAGNETIC CAP OF THE COOLING TU RBINE HAD METAL CHIPS, A/C PACK WAS INOPERATIVE PER MEL. APU WAS REPLACED IAW MM, FOR LACK OF OIL AND LEAKAGE THROUG TH E LOAD CONTROL VALVE. THE CHIP DETECTOR OF THE COOLING TURBINE WAS VERIFIED AND FOUND IT OK. AFTER APU REPLACEMENT, BO TH PACKAGES WERE WORKING OK. 2 L 7 2 4F RT A6WE 2002081400071 20020814 00071 EU 2002 8 14 RAIA00207225 1 20020721 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 572HK 41091 BWI- FLOOR PATH LIGHTS INOPERATIVE. SECURED CONNECTOR, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002081400072 20020814 00072 EU 2002 8 14 RAIA00207227 1 20020729 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 563HK 41079 BWI- EMERGENCY PATH LIGHTS INOPERATIVE. SECURED CONNECTOR ON ESCAPE PATH LIGHTS, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002081400073 20020814 00073 WP 2002 8 14 AALA20020822 1 20020603 A 7830 B-NUT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LT ENGINE LOOSE A AALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 285AA 49297 LAS - FLT 1236 - WHILE TAXIING AT LAS, CABIN AND COCKPIT FILLED WITH SMOKE, PERFORMED EMERGENCY EVACUATION. TURNED OFF APU SMOKE STOPPED. SECURED LOOST B-NUT AT LEFT THRUST REVERSER. CLEANED ACCUMULATOR AREA. ACCOMPLISHED PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 2002081400074 20020814 00074 EU 2002 8 14 RAIA00207230 1 20020730 A 2520 INSULATION AEROSP ATR42 ATR42300 8680920 EU FUSELAGE OUT OF POSITION A RAIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CE 03 426TE 228 STL - RIGHT SIDE PITCH YOKE BINDING. SECURED INSULATION THAT WAS DROOPING DOWN ON ELEVATOR CABLES, OPS CHECK OK. 2 H 7 2 4T RT A53EU 2002081400075 20020814 00075 WP 2002 8 14 AALA20020889 1 20020616 A 4920 PACKING DOUG DC9 DC982 3022082 WP APU LEAKING A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 426AA 49338 MEX - FLT 1156 - EN ROUTE MEX-DFW, NOTICED HEAVY SMOKE IN CABIN RIGHT AFTER TAKEOFF AT MEX. RAN CABIN FIRE AND SMOKE CH ECKLIST, SMOKE DISSIPATED WHEN PACKS AND RECIRCULATION FAN TURNED OFF. RETURNED AND LANDED MEX WITHOUT INCIDENT. REPLA CED PACKING AT APU MASTER CHIP DETECTOR. RAN APU, NO OIL LEAKS NOTED. PERFORMED AIRCRAFT PACKS AND HIGH PRESSURE PNEUM ATIC DUCTING BURN OUT. REPLACED BOTH PACKS COALESCERS BAGS. RAN UP AIRCRAFT PACKS, NO SMOKE OR ODOR NOTED. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002081400076 20020814 00076 EU 2002 8 14 RAIA00208232 1 20020805 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 565HK 41082 STL - EMERGENCY PATH LIGHTS INOP. SECURED LOOSE BULB, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002081400077 20020814 00077 EU 2002 8 14 RAIAOO207219 1 20020717 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 550HK 41039 STL- EMERGENCY ESCAPE PATH LIGHTS OUT AT ROWS 3, 4, AND 5. MAINTENANCE RECONNECTED LIGHT STRIP, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002081400078 20020814 00078 2002 8 14 SWAA021719 4 20020731 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002081400079 20020814 00079 NM 2002 8 14 SWAA021720 1 20020801 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 EEPLS WIRES EXPOSED AT MID CABIN. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002081400080 20020814 00080 NM 2002 8 14 SWAA021728 1 20020801 A 2612 894093 FIRE LOOP BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAULTY A SWAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 29 095SW 23054 687797 DECLARED EMERGENCY, IN FLIGHT SHUT DOWN, NR 2 ENGINE FIRE BELL WARNING LIGHT ILLUMINATED. SHUT DOWN ENGINE AND DISCHARG ED BOTH FIRE EXTINGUISHER BOTTLES. REMOVED AND REPLACED NR 2 ENGINE LOWER FIRE DETECTOR LOOP PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2002081400081 20020814 00081 NM 2002 8 14 SWAA021730 1 20020801 A 3350 BR2013 COVER BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 EEPLS WIRES EXPOSED AT MID CABIN. REPAIRED COVER PER MM. 2 L 7 2 4F RT A16WE 2002081400082 20020814 00082 NM 2002 8 14 SWAA021731 1 20020802 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 EEPLS LOOSE IN CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002081400083 20020814 00083 NM 2002 8 14 SWAA021732 1 20020801 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 EEPLS LOOSE AND DISCONNECTED AT ROW NR 12. SECURED AND CONNECTED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002081400084 20020814 00084 2002 8 14 SWAA021733 4 20020802 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER WHILE OPENING DOOR. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002081400085 20020814 00085 NM 2002 8 14 SWAA021735 1 20020803 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 081SW 22730 DURING SCHEDULED PM CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002081400086 20020814 00086 2002 8 14 SWAA021736 4 20020804 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM . 2 L 7 2 4F A16WE 2002081400087 20020814 00087 NM 2002 8 14 SWAA021738 1 20020802 A 5312 6546568 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED C4 CHECK, FOUND AFT PRESSURE BULKHEAD HAS OIL CANNING AT 2 O'CLOCK POSITION. REPAIRED BULKHEAD PER SAW EA. 2 L 7 2 4F RT A16WE 2002081400088 20020814 00088 NM 2002 8 14 SWAA021739 1 20020801 A 3350 100031 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED C2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT AT ROW NR 3 INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2002081400089 20020814 00089 NM 2002 8 14 SWAA021748 1 20020804 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED ST BS 360, STR 5L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002081400090 20020814 00090 2002 8 14 SWAA021750 4 20020805 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002081400091 20020814 00091 2002 8 14 SWAA021751 4 20020805 A 2565 D31355105 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLID E PER MM. 2 L 7 2 4F A16WE 2002081400092 20020814 00092 NM 2002 8 14 SWAA021752 1 20020804 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 105SW 23249 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002081400093 20020814 00093 NM 2002 8 14 SWAA021755 1 20020801 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002081400094 20020814 00094 NM 2002 8 14 SWAA021758 1 20020805 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002081400095 20020814 00095 NM 2002 8 14 SWAA021759 1 20020805 A 5314 6545866 KEELBEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND KEEL BEAM CORRODED AT BS 540, WL 149 AND RBL 7. REPAIRED KEEL BEAM PER BFG ER. 2 L 7 2 4F RT A16WE 2002081400096 20020814 00096 WP 2002 8 14 AALA20020893 1 20020608 A 4920 PLUG DOUG DC9 DC982 3022082 WP APU DAMAGED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 488AA 49681 AUS - FLIGHT 1592 - EN ROUTE AUS-ORD, ON TAKEOFF AT AUS A RUBBER / INSULATION / ELECTRICAL ODOR WAS NOTED. IT INCREASED TO A VISIBLE HAZE IN THE CABIN. RETURNED AUS, HAZE DISSIPATED, LANDED AUS WITHOUT INCIDENT. REPLACED APU OIL DRAIN PL UG, LEFT AND RIGHT AUGMENTATION VALVES, AND COALESCERS BAGS. PERFORMED AIRCRAFT PACK BURN OUT. NO ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002081400097 20020814 00097 2002 8 14 SWAA021765 4 20020805 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002081400098 20020814 00098 2002 8 14 SWAA021767 4 20020806 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002081400099 20020814 00099 2002 8 14 SWAA021768 4 20020805 A 2565 D31354418 SLIDE BOEING 737 7373Q8 1384670 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED RON, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER M M. 2 L 7 2 4F RT A16WE 2002081400100 20020814 00100 2002 8 14 AALA20020922 4 20020618 A 2565 D29982125 SLIDE DOUG DC9 DC982 3022082 WP PAX DOOR DISLODGED A AALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 513AA 49890 IND - FLT 2076 - FIRST CLASS GALLEY DOOR SLIDE FELL OUT AND DID NOT DEPLOY SUCCESSFULLY. AIRCRAFT HAS BEEN INSPECTED AN D FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM IND TO DFW FOR REPAIRS. REPLACED FIRST CLASS GALLEY DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002081400101 20020814 00101 NM 2002 8 14 SWAA021769 1 20020804 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002081400102 20020814 00102 NM 2002 8 14 SWAA021772 1 20020806 A 2133 322684004 OUTFLOW VALVE BOEING 737 7373H4 1384600 NM CABIN PRESSURE FAILED A SWAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 29 373SW 26581 DECLARED EMERGENCY, DIVERSION, AT FL310, ALTITUDE WARNING HORN CAME ON. CABIN ALT AT 10,000 FEET CLIMBING. REMOVED AND REPLACED FWD AND AFT OUT FLOW VALVES, DELTA P MODULE, OVERHEAD MODULE, A/C ACCESSORY UNIT, CABIN PRESS CONTROLLER AND L OWER SAFETY RELIEF VALVE PER MM. 2 L 7 2 4F RT A16WE 2002081400103 20020814 00103 NM 2002 8 14 SWAA021774 1 20020806 A 3350 BR2013 LIGHT BOEING 737 7373G7 1384595 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP WORN AT ROW NR 8. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2002081400104 20020814 00104 NM 2002 8 14 SWAA021775 1 20020807 A 3350 PH22300L LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 EEPLS STRIP LOOSE AT ROW NR 9 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2002081400105 20020814 00105 NM 2002 8 14 SWAA021776 1 20020806 A 3350 BR2013 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED C4 CHECK, FOUND EEPLS FWD END CAP MISSING AND WIRES EXPOSED IN SEVERAL AREAS. INSTALLED END CAP AND SE CURED EXPOSED WIRES PER MM. 2 L 7 2 4F A16WE 2002081400106 20020814 00106 EU 2002 8 14 SIMA200220502 1 20020723 A 5300 ALCLAD2024T3 FASTENER SAAB SF340 340B 7860101 EU RT HORZ STAB ELONGATED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 FOUND RIGHT HORIZONTAL STABILIZER UPPER FORWARD SPAR CAP FASTENERS HOLE AT THE INBOARD END WAS FOUND TO BE ELONGATED. R EMOVED HORIZONTAL STAB. LEADING EDGE RIB AND MOUNTING ANGLE ON THE SPAR WEB. FABRICATED A REPLACEMENT SECTION SPAR WEB, TWO DOUBLER, ANGLE AND SHIMS. REPAIR DONE IAW SRM. 2 L 7 2 4T RT A52EU 2002081400107 20020814 00107 NM 2002 8 14 SWAA021778 1 20020807 A 3230 FCA410 RELAY BOEING 737 737317 138447P NM E/E BAY FAILED A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 29 693SW 23174 NOSE GEAR RED UNSAFE LIGHT DID NOT EXTINGUISH AFTER TAKEOFF. REMOVED AND REPLACED NOSE GEAR LATCHING RELAY R 374 PER MM . 2 L 7 2 4F RT A16WE 2002081400108 20020814 00108 NM 2002 8 14 SWAA021779 1 20020806 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 EEPLS LOOSE AT ROWS NR 9 AND NR 10. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002081400109 20020814 00109 NM 2002 8 14 UPS02438836 1 20020703 A 5320 69B118571 BRACKET BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - KEELBEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1122 RBL 9. CORROSION BLEND OUT EX CEEDS SRM LIMITS. BRACKET REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002081400110 20020814 00110 NM 2002 8 14 UPS02438837 1 20020715 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:SP STA 720 STR 44L SHEAR TIE IS CRACKED. REMOVED DAMAGED SECTION OF SHEAR TIE, NDT VERIFIED NO CRACKS. AFTER DAMAGE REMOVAL, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 53-10-04. 2 L 7 4 4F A20WE 2002081400111 20020814 00111 NM 2002 8 14 UPS02438859 1 20020720 A 5753 WEDGE BOEING 747 747123 1384873 NM T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:PFLT LT INBOARD MID FLAP IS CRACKED IN TWO PLACES. REPAIRED DAMAGED AREAS OF MID FLAP T/E WEDGE IAW EO B747-5750-17190A. ACCOMPLISH PERM REPAIR OF PART REPLACEMENT NO LATER THAN C-CHECK. 2 L 7 4 4F A20WE 2002081400112 20020814 00112 NM 2002 8 14 UPS02438861 1 20020702 A 5320 RIB BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX KEELBEAM BOX LWR EXTERIOR LWR CHORD SUPPORT LWR RIB FOUND SURFACE CORROSION AT STA 1308 RBL 2 AFT S URFACE. CORROSION BLEND OUT EXCEEDS SRM LIMIT. RIB REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002081400113 20020814 00113 SO 2002 8 14 SIMA200220503 1 20020712 A 5300 AL7075T6511 WINDSHIELD EMB 145 EMB145LR 3260212 SO PILOT WINDSHIELD CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 FOUND PILOT WINDSHIELD CUTOUT LOWER STRIP HAS 6 CORRODED HOLES. REMOVED CORROSION BY REAMING HOLES 2 AND 4 TO ALLOWABLE LIMITS. REAMED HOLES 1 AND 4 TO .313 TO REMOVE CORROSION. FABRICATED TO FREEZE PLUGS. REPAIR DONE IAW SRM. (B8349) 2 L 7 2 4T RT T00011AT 2002081400114 20020814 00114 NM 2002 8 14 UPS02438863 1 20020703 A 5320 65B1054266 SUPPORT BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - KEELBEAM PANEL SUPPORT LOWER CHORD SURFACE FOUND SURFACE CORROSION AT STA 1112 LBL 9 TO RBL 9. C ORROSION BLEND OUT EXCEEDS SRM LIMIT. PANEL SUPPORT REPLACED A PER SRM 5101 PG 8. 2 L 7 4 4F A20WE 2002081400115 20020814 00115 WP 2002 8 14 AALA20020924 1 20020617 A 3620 SENSOR DOUG DC9 DC982 3022082 WP FLAPPER DOORS DIRTY A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 429AA 49341 TUS - FLT 590 - EN ROUTE TUS-DFW - AFTER TAKEOFF RECEIVED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT WITH MASTER WARNING LI GHT. EMEREGNCY PROCEDURES WERE COMPLIED WITH AND AIRCRAFT RETURNED TO TUS. DOWNWIND TO LANDING, LIGHT EXTINGUISHED, BU T ON SHORT FINAL LIGHT BEGAN TO FLICKER ON AND OFF. PASSENGERS IN THE REAR OF THE AIRCRAFT, NEAR THE ENGINES, REPORTED ODD ODORS AND BURNING SMELL. LANDED TUS WITHOUT INCIDENT. CLEANED BOTH LEFT AND RIGHT TEMPERATURE SENSOR FLAPPER DOORS . ALSO, INSPECTED TAIL COMPARTMENT DUCTING AND FOUND NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002081400116 20020814 00116 NM 2002 8 14 ASAA0210118 1 20020513 A 5311 6546555 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 867, STRINGER 24R-25R DENTED. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F A16WE 2002081400117 20020814 00117 NM 2002 8 14 ASAA0210120 1 20020513 A 5311 6546549 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BODY STATION 767, STRINGER 22L DENTED. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F A16WE 2002081400118 20020814 00118 NM 2002 8 14 ASAA0210121 1 20020513 A 5311 6546549 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BODY STATION 767, STRINGER 24L DENTED. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F A16WE 2002081400119 20020814 00119 NM 2002 8 14 ASAA0210122 1 20020513 A 5310 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 827, RIGHT BUTTOCK LINE 8 CORRODED. REPAIRED SHEAR TIE PER SRM. (M) 2 L 7 2 4F A16WE 2002081400120 20020814 00120 NM 2002 8 14 ASAA0210123 1 20020513 A 5311 6546550 FAILSAFE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND STUB FRAME FAIL/SAFE AT BS 791, RIGHT BUTTOCK LINE 8 CORRODED. REMOVED AND REPLAC ED STUB FRAME FAIL/SAFE PER SRM. (M) 2 L 7 2 4F A16WE 2002081400121 20020814 00121 NM 2002 8 14 ASAA0210124 1 20020515 A 5740 6545320 FITTING BOEING 737 737290C 138448V NM LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND LT MLG BEAM TO SPAR FITTING AT WING STATION 150-162 CRACKED. REPAIRED FITTING PER EA AND SERVICE BULLETING. (M) 2 L 7 2 4F A16WE 2002081400122 20020814 00122 NM 2002 8 14 ASAA0210130 1 20020518 A 5315 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 1006, LEFT BUTTOCK LINE 10 CORRODED. REPAIRED FLOORBEAM PER SRM. (M) 2 L 7 2 4F RT A16WE 2002081400123 20020814 00123 NM 2002 8 14 ASAA0210131 1 20020520 A 5313 65457697 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 26R AT BS 536 CORRODED. REPAIRED STRINGER PER SRM. (M) 2 L 7 2 4F RT A16WE 2002081400124 20020814 00124 NM 2002 8 14 ASAA0210132 1 20020526 A 5315 6545810 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 312, WATERLINE 208 CORRODED. REPAIRED FLOORBEAM PER SRM. (M) 2 L 7 2 4F RT A16WE 2002081400125 20020814 00125 NM 2002 8 14 ASAA0210134 1 20020528 A 5315 6545808 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 294, LEFT BUTTOCK LINE 20, RIGHT BUTTOCK LINE 60 CORRODED. REPAIR ED FLOORBEAM PER SRM. (M) 2 L 7 2 4F RT A16WE 2002081400126 20020814 00126 NM 2002 8 14 ASAA0210136 1 20020529 A 5315 BAC1505100186 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 328, RIGHT BUTTOCK LINE 15, RIGHT BUTTOCK LINE 29 CORRODED. REPAI RED FLOORBEAM PER SRM. (M) 2 L 7 2 4F RT A16WE 2002081400127 20020814 00127 NM 2002 8 14 ASAA0210137 1 20020529 A 5320 654587546 SILL BOEING 737 7372X6C 1384552 NM BS 290-328 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND FORWARD GALLEY DOOR MOPSILL AT BS 290-328, RIGHT BUTTOCK LINE 54 CORRODED. REPAIR ED MOPSILL PER SRM. (M) 2 L 7 2 4F RT A16WE 2002081400128 20020814 00128 NM 2002 8 14 ASAA0210146 1 20020607 A 5342 FITTING BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND SPAR LUGS AT BS 1104, LEFT BUTTOCK LINE 45, RIGHT BUTTOCK LINE 45 CORRODED. REPAI RED REAR SPAR LUGS PER EA. (M) 2 L 7 2 4F RT A16WE 2002081400129 20020814 00129 NM 2002 8 14 ASAA0210147 1 20020607 A 5311 6545813501 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 332, RIGHT BUTTOCK LINE 68.4 CORRODED. REPAIRED REAR FRAME PER SRM. (M) 2 L 7 2 4F RT A16WE 2002081400130 20020814 00130 NM 2002 8 14 ASAA0210148 1 20020607 A 5511 SPAR BOEING 737 7372X6C 1384552 NM HORIZONTAL STAB CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND FORWARD SPAR AT HORIZONTAL STABILIZER STATION 57.93 CORRODED. REPAIRED REAR FORWA RD SPAR PER EA. (M) 2 L 7 2 4F RT A16WE 2002081400131 20020814 00131 NM 2002 8 14 ASAA0210149 1 20020608 A 5315 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 967, LEFT BUTTOCK LINE 18 CORRODED. REPAIRED FLOORBEAM PER EA. ( M) 2 L 7 2 4F RT A16WE 2002081400132 20020814 00132 NM 2002 8 14 ASAA0240053 1 20020518 A 5311 6546560 FAILSAFE BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 PAE - DURING C-CHECK, FOUND CORROSION ON FAIL/SAFE AT BS 946 RBL 18, AND WL 175. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002081400133 20020814 00133 WP 2002 8 14 GTIA020652 1 20020510 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND MID PIT. LONGERON 29L CORRODED/GOUGE STATION 579-598. REMOVED LONGERON 29L STATION 589-664. LOCATED AND DR ILLED HOLES IN REPAIR LONGERON 29L. FABRICATED AFT LONGERON 29 SPLICE USING MATERIAL. INSTALLED MID PIT LONGERON 29L S PLICE COMMON TO STATION 674. (M) 2 L 7 2 4F A6WE 2002081400134 20020814 00134 WP 2002 8 14 GTIA020654 1 20020510 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 NM 01 816NK 49140 FTW - FOUND MID PIT, CORRODED AT RT AFT FLOOR SUPPORT, STATION 693. FORMED NEW FLOOR SUPPORT. INSTALLED NEW SUPPORT. REMOVED FLOOR SUPPORT FRONT PAGE. (M) 2 L 7 2 4F A6WE 2002081400135 20020814 00135 WP 2002 8 14 GTIA020655 1 20020515 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND MID B/B LONGERON 30 AT STATION 775 IS CORRODED. REMOVED LONGERON 30 FROM Y STATION 741 TO Y STATION 775. F ABRICATED LONGERON 30 SECTION FROM STATION 741. FABRICATED LONGERON 30 SPLICE. INSTALLED SPLICE. INSTALLED LONGERON P RIOR TO STEP 8. (M) 2 L 7 2 4F A6WE 2002081400136 20020814 00136 WP 2002 8 14 GTIA020656 1 20020509 A 5310 STRAP DOUG DC9 DC982 3022082 WP DOOR FRAME CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 NM 01 816NK 49140 FTW - FOUND AFT PIT STATION 1155-1212 L28R, REPAIR STRAP ON OUTBOARD AND INBOARD SIDE DOOR JAMB BEAM IS CORRODED, EVIDEN CE OF CORROSION BETWEEN STRAP AND BEAM. REMOVED STRAPS STATION 1150 AND 1220. REMOVED JAMB BEAM. LOCATED AND DRILLED AND NEW JAMB BEAM. INSTALLED DOOR JAMB BEAM. FLOOR SUPPORT AT STATION 1193. FOUND TO BE OUT OF LIMITS. LOCATED AND D RILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT AT STATION 1193. (M) 2 L 7 2 4F A6WE 2002081400137 20020814 00137 NM 2002 8 14 UPS02438864 1 20020703 A 5320 65B117915 WEB BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - KEELBEAM BOX LOWER EXTERIOR LOWER KEELBEAM FIXED PANEL UPPER SURFACE AND HINGE FITTING AREA FOUND SURFACE CORROSION AT STA 1255 TO STA 1275 LBL 7 TO LBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMIT. WEB REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002081400138 20020814 00138 WP 2002 8 14 GTIA020792 1 20020624 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND FORWARD PIT HAS CRACKED AT BRACKET SUPPORT AFT 2 ANGLE RBL IN INCHES. REMOVED CRACKED BRACKET SUPPORT. FA BRICATED NEW BRACKET. INSTALLED BRACKET. (M) 2 L 7 2 4F A6WE 2002081400139 20020814 00139 NM 2002 8 14 UPS02438865 1 20020703 A 5320 65B117916 FITTING BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C FX - KEELBEAM BOX LOWER EXTERIOR LOWER FIXED PANEL UPPER SURFACE AND HINGE FITTING AREA FOUND SURFACE CORROSION AT STA 1255 TO 1275 RBL 7 TO RBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMIT. FITTING REPLACED AS PER SRM 51-1 0-01 PG 8. 2 L 7 4 4F A20WE 2002081400140 20020814 00140 WP 2002 8 14 GTIA020793 1 20020701 A 7120 ISOLATION MOUNT DOUG DC9 DC982 3022082 WP NR 1 ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - NR 1 ENGINE AFT MOUNT ISOLATOR, INNER CONICAL SURFACE HAS NICKS, SCRATCHES AND WORN PLATING. REMOVED NR 1 ENGINE AFT MOUTN ISLOATOR. INSTALLED SVC, NR 1 ENGINE AFT MOUNT ISOLATER. (M) 2 L 7 2 4F A6WE 2002081400141 20020814 00141 WP 2002 8 14 GTIA020794 1 20020623 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND MID PIT HAS CORROSION AT BRACKETS ATTACH TO INBOARD BEAM STATION 617 RBL 8 INCHES BOTH SIDES, TWO EACH. REM OVED BRACKETS FROM STATION 617 RBL 8. FABRICATED BRACKETS FROM 7075-T6511. INSTALLED NEW FABRICATED BRACKETS AT STATIO N 617 RBL 8. (M) 2 L 7 2 4F A6WE 2002081400142 20020814 00142 NM 2002 8 14 UPS02438866 1 20020707 A 5320 654U6624227 FITTING BOEING 747 747123F NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, LT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING FOUND NR 2, 3, 4, 5, 6, 7, 8, 9, 11 HOLES ELONGATED AF TER FITTING REMOVED. LT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING CHANGED AS PER BOEING SB 747-53A2390. 2 L 7 4 4F A20WE 2002081400143 20020814 00143 WP 2002 8 14 GTIA020795 1 20020621 A 7120 ISOLATION MOUNT DOUG DC9 DC982 3022082 WP LT ENGINE WRONG PART A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND LEFT ENGINE FORWARD UPPER AND LOWER VIBRATION ISOLATORS MISMATCH. REMOVED LEFT ENGINE FORWARD UPPER AND LOW ER VIBRATION ISOLATORS. INSTALLED NEW UPPER AND LOWER ISOLATORS. (M) 2 L 7 2 4F A6WE 2002081400144 20020814 00144 NM 2002 8 14 UPS02438871 1 20020701 A 5320 FLOOR SUPPORT BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, M/D - BS 1320 RBL 75-97 FLOOR SUPPORT ATT PLATE CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. FL OOR SUPPORT ATT PLATE AT M/D BS 1320 RBL 75-97 REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002081400145 20020814 00145 WP 2002 8 14 GTIA020796 1 20020627 A 5320 CHANNEL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND ANGLE CRACKED AT FS 937 RBL 7 INCHES STRUCTURE BELOW CENTER WING, KEEL BEAM AREA, NEAR AUX HYD PUMP. REMOVE D CHANNEL DAMAGED. FABRICATED CHANNEL. LOCATED AND DRILLED ANGLE TWO REPAIR SPLICE AND 1 STRAP. INSTALLED ANGLE TWO R EPAIR SPLICE AND 1 SPLICE. (M) 2 L 7 2 4F A6WE 2002081400146 20020814 00146 WP 2002 8 14 GTIA020797 1 20020623 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND L1 DOOR THRESHOLD FLOOR SUPPORT HAS CORRODED. REMOVED FLOOR SUPPORT DAMAGED. FORMED FLOOR SUPPORT. INSTAL LED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002081400147 20020814 00147 WP 2002 8 14 GTIA020798 1 20020623 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND MID PIT HAS CORROSION LEFT ANGLE FORWARD FACE BULKHEAD STATION 788, BOTH SIDES. REMOVED ANGLE. DRILLED AND LOCATED HOLES, INSTALLED. (M) 2 L 7 2 4F A6WE 2002081400148 20020814 00148 NM 2002 8 14 UPS02438873 1 20020722 A 2910 65B801293 HYDRAULIC LINE BOEING 747 747256B 1384865 NM HYD SYSTEM RUPTURED A IPXA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 01 528UP 24071 INSPECTION TYPE:N/A, AIR TURNBACK FOR LOSS OF NR 1 HYD QTY. FOUND RT BODY GEAR DOWNLOCK ACTUATOR FLEX LINE BUSTED. INS TALLED T/E MP FLEX LINE IAW MM 32-30-00. LEAK CHECK GOOD ON GROUND. 2 L 7 4 4F RT A20WE 2002081400149 20020814 00149 WP 2002 8 14 GTIA020799 1 20020630 A 5340 ATTACH FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND PASSENGER CABIN HAS CRACK AT LEFT BRACKET ATTACH TO THE FRAME AND LONGERON 3L STATION 218. REMOVED ATTACH B RACKET. FORMING BRACKET. INSTALLED BRACKET. (M) 2 L 7 2 4F A6WE 2002081400150 20020814 00150 WP 2002 8 14 GTIA020800 1 20020624 A 5340 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND MID LOWER COMPARTMENT CARGO DOOR HAS CORROSION AT 3RD ANGLE ATTACH TO INTERCOSTAL. REMOVED ANGLE. HOLES DR ILLED AND LOCATED ON NEW ANGLE. INSTALLED NEW ANGLE. (M) 2 L 7 2 4F A6WE 2002081400151 20020814 00151 WP 2002 8 14 GTIA020801 1 20020702 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND DENT AT PREVIOUS REPAIR AT FS 1206 BETWEEN LONGERON 27 AND 29L REQUIRES REPAIR TO BE REACCOMPLISHED TO INCLU DE DENT. REMOVED PREVIOUS REPAIR STATION 1206 LONGERON 27-29L. CUT OUT SKIN FOR REPAIR. FABRICATED FILLER AND DOUBLER , EXTERNAL AND FINGER DOUBLRS. INSTALLED REPAIR. (M) 2 L 7 2 4F A6WE 2002081400152 20020814 00152 NM 2002 8 14 UPS02438876 1 20020722 A 3350 LIGHT BOEING 747 747121 1384871 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:PFLT FWD EMERGENCY EXIT LIGHT OUT MAIN ENTRY DOOR IS INOP. REMOVED AND REPLACED M415 ERF 33-15-05. 2 L 7 4 4F A20WE 2002081400153 20020814 00153 WP 2002 8 14 GTIA020802 1 20020710 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND L1 DOOR FRAME HAS CRACK STATION 195 Z67. STOP DRILLED CRACK. (M) 2 L 7 2 4F A6WE 2002081400154 20020814 00154 WP 2002 8 14 GTIA020803 1 20020622 A 5730 PANEL DOUG DC9 DC982 3022082 WP LT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND LEFT WING LOWER L/E PANEL 1166C APPROX 2 INCH CRACK AND TOOL MARKS ON SIN, BARE METAL ON BACK. DAMAGE CUT O UT, FORMED DOUBLER REPAIR AND FILLER. INSTALLED DOUBLER REPAIR AND FILLER. (M) 2 L 7 2 4F A6WE 2002081400155 20020814 00155 WP 2002 8 14 GTIA020804 1 20020624 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 245 LBL 47-52, CRACK IN EDGE OF LIGHTENING HOLE INBOARD SIDE, PUNCTURE IN FLOOR WEB OUTBOARD OF LIGH TENING HOLE. REMOVED CRACK. FORMING DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2002081400156 20020814 00156 NE 2002 8 14 UPS02438877 2 20020720 A 7200 JT9D ENGINE BOEING 747 747123 1384873 NM PWA JT9 JT9D* NE NR 1 MALFUNCTIONED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 674UP 20100 662936 INSPECTION TYPE:N/A, WHEN PACK LAND 3 WAS TURNED ON AFTER TAKEOFF OILY SMOKE FILLED THE FLIGHT DECK. PACK 1 AND 3 WAS T URNED OFF AND PACK 2 TURNED ON. SMOKE CLEARED AND FLIGHT CONTINUED TO PHL. REMOVED AND CLEANED NR 1 PACK COALESCER BAG . RAN PACKS FROM APU, OPS CHECK GOOD. RAN PACKS FROM ENG 1 & 4, SMELL OF SMOKE AGAIN FROM NR 1 ENG. NR 1 ENGINE REQUI RES CHANGE DUE TO RUMBLING AND OIL CONSUMPTION. 2 L 7 4 4F 4 F A20WE E20EA 2002081400157 20020814 00157 NM 2002 8 14 UPS02438883 1 20020628 A 5320 FLOOR SUPPORT BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, FWD CARGO COMPARTMENT STA 560 RBL 45 PALLET LOCK FLOOR SUPPORT CORROSION. CORROSION BLEND OUT EXCEED S SRM LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2. 2 L 7 4 4F A20WE 2002081400159 20020814 00159 EA 2002 8 14 COMA0260476 1 20020808 A 5300 601R52065 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA F.S.574 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 938CA 18296 7046 WHILE ACCOMPLISHING THE REPLACEMENT OF FRAME 574 THE INTERCOSTAL FOR THE CARGO DOOR SUPPORT STRUCTURE WAS DAMAGED. THE I NBOARD FLANGE WAS BENT AND TWO CRACKS DEVELOPED.THE DAMAGED FLANGE WAS CUT OFF AND A REPAIR ANGLE WAS FABRICATED AND INS TALLED I/A/W WVAC EO 601R-53-3416. 2 L 7 2 4F RT A21EA 2002081400160 20020814 00160 EU 2002 8 14 SIMA200216403 1 20020624 A 5347 S53375001204 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 DURING CPCP-2 INSPECTION, SEAT TRACKS, LEFT FORWARD OUTBOARD, LEFT FORWARD INBOARD, RIGHT FORWARD INBOARD, RIGHT FORWARD OUTBOARD, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MID INBOARD, WERE FOUND TO BE CORRODED. RAID SEAT TRACKS, RIGHT MIDDLE INBOARD, RIGHT AFT INBOARD, LEFT FORWARD OUTBOARD, RIGHT FORWARD OUTBOARD, LEFT MID OUTBOARD IAW E1. 2 H 7 2 4T RT A53EU 2002081400161 20020814 00161 EA 2002 8 14 COMA0260477 1 20020812 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS CR CRUISE 1 SO 01 473CA 141 7668 FLIGHT 5761 FLAPS FAIL MESSAGE.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2002081400162 20020814 00162 EA 2002 8 14 COMA0260478 1 20020809 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 446CA 7546 FLIGHT 5760 OVERHEAD EMERGENCY EXIT LIGHT IS INOP AT ROW 1.REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2002081400166 20020814 00166 EU 2002 8 14 SIMA200217101 1 20020616 A 5347 7253799383 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 375AE 340B375 DISC-PAX SEAT TRACK ON RIGHT INBOARD SIDE HAS CORROSION IN VARIOUS SPOTS THE ENTIRE LENGTH OF CABIN. MAINTENANCE REMOVE D AND REPLACED THE RIGHT INBOARD SEAT TRACK IAW MM. 2 L 7 2 4T RT A52EU 2002081400167 20020814 00167 EU 2002 8 14 SIMA200218701 1 20020706 A 2120 ODOR SAAB SF340 340B 7860101 EU COCKPIT DETECTED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 304AE 340B304 DURING CRUISE FLIGHT THE CREW NOTED AN ELECTRICAL/WOOD SMOKE SMELL IN COCKPIT. AIRCRAFT WAS LANDED WITH NO OTHER PROBLE MS NOTED. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. GROUND RUN OF AIRCRAFT WAS SATISFACTORY. ISOLATED BOTH BLE ED SYSTEMS DURING RUNS AND FOUND NO SMELL AT ANY TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2002081400168 20020814 00168 EA 2002 8 14 COMA0260480 1 20020811 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 473CA 7668 FLIGHT 5961 FLAPS FAIL MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002081400169 20020814 00169 EA 2002 8 14 COMA0260481 1 20020811 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 420CA 7451 FLIGHT 5968 FLAPS FAILED AT 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002082000160 20020820 00160 EA 2002 8 20 COMA0260479 1 20020809 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 ENGINE LACK OF LUBE A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 735CA 7267 FLIGHT 5299 NR 2 IDG CAUTION MESSAGE DURING T/O. SERVICED THE IDG OIL TO PROPER LEVEL. 2 L 7 2 4F RT A21EA 2002081400170 20020814 00170 EU 2002 8 14 SIMA200219130 1 20020705 A 5347 7253725193 CARGO TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 DISC-CARGO AREA SEAT TRACK AT 18.3L HAS AREA CORROSION MEASURED BELOW LIMITS. REMOVED SECTION AND INSTALLED REPAIR EXTR USION IAW SRM. 2 L 7 2 4T RT A52EU 2002081400171 20020814 00171 EU 2002 8 14 SIMA200219201 1 20020711 A 2913 4018502 PUMP SAAB SF340 340B 7860101 EU HYD SYSTEM FAILED A SIMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 350CF 340B350 DISC LOST ALL HYDRAULIC POWER INBOARD, OUTBOARD, MAIN INDICATOR SHOWS ZERO ON TAXI OUT. REMOVED AND REPLACED HYDRAULIC MOTOR DRIVEN PUMP IAW MM. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2002081400172 20020814 00172 EU 2002 8 14 SIMA200219801 1 20020711 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 DURING MBV MAINTENANCE FOUND A DENT IN FRAME IN CARGO BAY AT STATION 677. DENT WAS RECOUNTED, NDT INSPECTED WITH NO DEF ECTS NOTED. A REPAIR DOUBLER WAS INSTALLED IAW RS AND STANDARD PRACTICES. 2 L 7 2 4T RT A52EU 2002081400173 20020814 00173 EU 2002 8 14 SIMA200219802 1 20020711 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 DURING MBV INSPECTION MAINTENANCE FOUND FRAME IN CARGO BAY DENTED AT STATION 686.888. DENT WAS RECONTOURED AND AN NDT I NSPECTION WAS COMPLIED WITH NO DEFECTS WERE NOTED. A REPAIR DOUBLER WAS INSTALLED IAW REPAIR STATEMENT AND STANDARD PRA CTICES. 2 L 7 2 4T RT A52EU 2002081400174 20020814 00174 EU 2002 8 14 SIMA200219803 1 20020711 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 DURING MBV MAINTENANCE FOUND THE RIGHT CARGO BAY FRAME AT STATION 668.888 DENTED. RECONTOURED DENT BACK TO NORMAL CONTO UR. PERFORMED AN NDT INSPECTION AND FOUND NO DEFECTS. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SDS AND SRM PRACTI CES. 2 L 7 2 4T RT A52EU 2002081400175 20020814 00175 2002 8 14 SWAA021811 4 20020812 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002081400176 20020814 00176 NM 2002 8 14 SWAA021815 1 20020811 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKS (2 EA) AT STR 22L, BS 767 AND BS 787. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002081400177 20020814 00177 NM 2002 8 14 SWAA021816 1 20020811 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKS (2 EA) AT STR 23L, BS 727E AND BS 747. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002081400178 20020814 00178 NM 2002 8 14 SWAA021817 1 20020811 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 500D, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002081400179 20020814 00179 NM 2002 8 14 SWAA021818 1 20020811 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002081400180 20020814 00180 NM 2002 8 14 SWAA021819 1 20020812 A 5510 6547985 RIB BOEING 737 7373H4 1384600 NM RT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STABILIZER LOWER RIB CHORD CRACKED AT STA 120.3, 24 AFT OF FWD LOWER SPAR. REMOVED AND REPLACED LOWER RIB CHORD PER SRM. 2 L 7 2 4F RT A16WE 2002081400181 20020814 00181 NM 2002 8 14 SWAA021821 1 20020812 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT LOWER STOP FITTING, BS 440 AT STR 27R. REPAIRED FRAME PER SRM . 2 L 7 2 4F RT A16WE 2002081400182 20020814 00182 NM 2002 8 14 SWAA021822 1 20020812 A 5311 6945815 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED (2 EA) AT BIN ATTACH POINTS, BS 360, STR 8R AND 9R AND BS 380, STR 8L AND 9L. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2002081400183 20020814 00183 NM 2002 8 14 SWAA021823 1 20020812 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, WL 208 AND RBL 15. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002081400184 20020814 00184 NM 2002 8 14 SWAA021824 1 20020810 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A+2, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002081400185 20020814 00185 NM 2002 8 14 SWAA021825 1 20020810 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 13R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002081400186 20020814 00186 NM 2002 8 14 SWAA021826 1 20020810 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 18L, BS 753 AND BS 749. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002081400187 20020814 00187 2002 8 14 SWAA021791 4 20020808 A 2565 6949956 CABLE BOEING 737 7372H4 138448C NM FWD ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 086SW 22827 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002081400188 20020814 00188 NM 2002 8 14 SWAA021792 1 20020810 A 5314 BAC1503 STIFFENER BOEING 737 7373Q8 1384670 NM LT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED PM CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663.75, LBL 4. REPAIRED STIFFENER PER SWA EA. 2 L 7 2 4F RT A16WE 2002081400189 20020814 00189 NM 2002 8 14 SWAA021793 1 20020810 A 5314 BAC1508 STIFFENER BOEING 737 7373Q8 1384670 NM LT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED PM CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 727, LBL 16. REPAIRED STIFFENER PER SWA EA. 2 L 7 2 4F RT A16WE 2002081400190 20020814 00190 NM 2002 8 14 SWAA021794 1 20020810 A 5520 65C25746141A ELEVATOR BOEING 737 7373H4 1384600 NM LT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 1/2D CHECK, FOUND LT ELEVATOR DELAMINATED AT FWD CENTER UPPER SKIN. REMOVED AND REPLACED LEFT ELEVATOR AND TAB PER MM. 2 L 7 2 4F RT A16WE 2002081400191 20020814 00191 NM 2002 8 14 SWAA021795 1 20020810 A 5330 6545768 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 341, ABOVE STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F A16WE 2002081400192 20020814 00192 NM 2002 8 14 SWAA021796 1 20020809 A 5755 654645170A SPOILER BOEING 737 7372H4 138448C NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED 1/4D CHECK, FOUND NR 1 SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED NR 1 SPOILER PER MM. 2 L 7 2 4F A16WE 2002081400193 20020814 00193 NM 2002 8 14 SWAA021798 1 20020808 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002081400194 20020814 00194 NM 2002 8 14 SWAA021799 1 20020809 A 3242 40817 TRANSDUCER BOEING 737 7372T4 1384492 NM LT INBD WHEEL BROKEN A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 29 722WN 22698 LT BRAKE GRABS AT LOW SPEED. FOUND,LT INBD ANTI-SKID TRANSDUCER FLYWHEEL BROKEN OFF. REMOVED AND REPLACED LEFT INBD TR ANSDUCER PER MM. 2 L 7 2 4F A16WE 2002081400195 20020814 00195 NM 2002 8 14 SWAA021800 1 20020807 A 2710 65C259271 BEARING BOEING 737 7373H4 1384600 NM RT MLG W/W WORN A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 385SW 26600 NOTICABLE BINDING IN AILERON CONTROL WHEEL. MX FERRY TO PHX. REMOVED AND REPLACED BEARINGS AT AILERON FEEL CENTERING U NIT AND F/O'S CONTROL YOKE ASSY PER MM. 2 L 7 2 4F RT A16WE 2002081400196 20020814 00196 2002 8 14 SWAA021801 4 20020809 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002081400197 20020814 00197 NM 2002 8 14 SWAA021802 1 20020810 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, ABOVE STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002081400198 20020814 00198 NM 2002 8 14 SWAA021803 1 20020810 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 EEPLS COVER MISSING AT ROW NR 14. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002081400199 20020814 00199 NM 2002 8 14 SWAA021804 1 20020811 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 716SW 27850 EEPLS COVER LOOSE IN FWD CABIN. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2002081400200 20020814 00200 NM 2002 8 14 SWAA021806 1 20020808 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM CRACKED CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207 AND RBL 39. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002081400201 20020814 00201 NM 2002 8 14 SWAA021807 1 20020810 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002081400202 20020814 00202 NM 2002 8 14 SWAA021808 1 20020810 A 2781 65C26686 SLAT BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED D CHECK, FOUND NR 1 SLAT CRACKED BELOW INBD AUX TRACK CUTOUT. REPAIRED NR 1 SLAT PER SRM. 2 L 7 2 4F RT A16WE 2002081400203 20020814 00203 2002 8 14 SWAA021809 4 20020810 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM BOTH FWD DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED C1 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PE R MM. 2 L 7 2 4F RT A16WE 2002081400204 20020814 00204 NM 2002 8 14 FX72002F00001 1 20020726 A 2900 HYDRAULIC LINE BOEING 727 727231 1384079 NM PWA JT8 JT8D217 52053 NE LOOSE A FX7A A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 19 54348 21967 DURING CRUISE SYSTEM (A) HYDRAULICS FAILED, PRESSURE WENT TO (O) A/C DIVERTED TO SAP AND LANDED SAFELY FOUND SYSTEM (A) PRESSURE LINE (B) NUT LOOSE TIGHTENED SAME SERVICED HYDRAULIC AND OPS CHECK GOOD PER MM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E9NE 2002081400205 20020814 00205 NM 2002 8 14 UIEA200200029 1 20020807 A 5411 65B941071 TEE CHORD BOEING 747 7472D7B 1384803 NM CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 80028 22337 Internal inspection of #4 pylon found aft horizontial flange of R/H Tee Chord cracked at NC 270 Bulkhead in area of uppe r link fitting. Crack is located at the end fastener hole. 2 L 7 4 4F RT A20WE 2002081400206 20020814 00206 NM 2002 8 14 UIE2002F00008 1 20020722 A 3397 8906K1563 SWITCH BOEING 747 7472D3B 1384805 NM WING ILL LTS INOPERATIVE A UIEA G H O2 MASK DEPLOYED DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 EA 15 506MC 21252 ON DESCENT A STRONG ELECTRICAL ODOR COMING OUT OF GASPERS. ELECTRICAL SMOKE OR FIRE CHECK LIST INITIATED. AFTER ITEM N R 6, SMOKE STOPPED. AIRCRAFT REMAINED IN THIS CONFIGURATION AND LANDED. C/A: FOUND MELTED INSULATION AT WING ILLUMINA TION LIGHT SWITCH TERMINAL. LIGHT INTERMITTENTLY INOPERATIVE, PULLED CIRCUIT BREAKER. TRANSFERRED. REPLACED SWITCH A ND WIRE ATTACHED TO TERMINAL NR 1 ON SWITCH FOR THE WING ILLUMINATION LIGHTS IAW MM. 2 L 7 4 4F RT A20WE 2002081400207 20020814 00207 WP 2002 8 14 MWEA020494 1 20020814 A 5740 4912003512 STRINGER CLIP DOUG DC9 DC914 3022034 WP XRS 111 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TEMPORARY STRINGER CLIP INSTALLED AT XRS 111 BETWEEN STRINGER 21&22 RIGHT WING. -- DRILLED UP CLIP AND INSTALLED NEW C LIP. 2 L 7 2 4F A6WE 2002081400208 20020814 00208 WP 2002 8 14 MWEA020507 1 20020814 A 5740 4912005512 STRINGER DOUG DC9 DC914 3022034 WP XRS 111 #11 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 TEMPORARY STRINGER CLIP INSTALLED AT XRS 111 BETWEEN STRINGER 11 AND AFT SPAR RIGHT WING. -- DRILLED UP CLIP AND INSTA LLED NEW CLIP. 2 L 7 2 4F A6WE 2002081400209 20020814 00209 NM 2002 8 14 UPS02439046 1 20020804 A 5310 BAC15048196 STIFFENER BOEING 747 747212B 1384886 NM M/D CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C M/D- BS 2300 RBL 10 WL 190 FLR BEAM ATT VERTICAL STIFFENER CRK. STIFFENER REPLACED AS PER SRM 51-1 0-01. 2 L 7 4 4F A20WE 2002081400210 20020814 00210 NM 2002 8 14 UPS02439047 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C LH BS 1480 B/H HOLE #15 CRACK FOUND AT SPLICE PLATE RUNNING UP & DOWN, BOTH CRACKS APPROX 0.020", REFE R ATTACH SKETCH. LH B/H BOLT HOLE #15 REAMED TO 0.500" AS PER SB 747-53A2390 FIG.11 CRACK TEST DONE NO CRACK FOUND A S PER NTM PT6 51-00-00 FIG 4 AND BUSHING INSTALLED AS PER SB 747-53A2390 R1 2 L 7 4 4F A20WE 2002081400211 20020814 00211 NM 2002 8 14 UPS02439048 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C LH BS 1480 B/H MOD HOLE #14 CRACK FOUND AT SPLICE PLATE AFT SURFACE RUNNING UP APPROX 1/16" LONG. REFE R ATTACH SKETCH. (STR L33 TO L34) LH BS 1480 B/H SPLICE PLATE BOLT HOLE #14 REAMED TO 0.500" AND BUSHING INSTALLED A S PER SB 747-53A2390 R1 CRACK TEST DONE AS PER NTM 51-00-00 FIG 4 NIL CRACK REVEALED. 2 L 7 4 4F A20WE 2002081400212 20020814 00212 NM 2002 8 14 UPS02439049 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C LH BS 1480 B/H HOLE #23 CRACK FOUND AT SPLICE PLATE RUNNING CRACK FOUND AT SPLICE PLATE RUNNING UP APP ROX 0.040" REFER ATTACHED SKETCH. (STR L33 TO L34) LH BS 1480 B/H HOLE #23 AT SPLICE PLATE REAMED TO 0.500" AND BUSH ING INSTALLED AS PER SB 747-53A2390 R1 HOLE CRACK FREE CONFIRMED AS PER NTM 51-00-00 FIG 4 2 L 7 4 4F A20WE 2002081400213 20020814 00213 NM 2002 8 14 UPS02439050 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C LH BS 1480 B/H #11 HOLE 2EA CRACK FOUND AT OUTER CHORD SPLICE FTG RUNNING FWD AT 8 O/C POSN & 7 O/C PO SN (LOOKING I/B),CRACK AT 8 O/C POSN 3/16" LONG, CRACK AT 7 O/C POSN 0.040" LONG (CRACK AT O/B FACE) (STR L33 TO L34) LH BS 1480 B/H OUTER CHORD SPLICE FTG BOLT HOLE #11 REAMED TO 0.660" AS PER SB 747-53A2390 R1 AND BUSHING REINSTALLED CRACK FREE CONFIRMED AS PER NDT NTM PT 6 51-00-00 FIG 4. 2 L 7 4 4F A20WE 2002081400214 20020814 00214 NM 2002 8 14 UPS02439051 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C LH BS 1480 B/H #7 HOLE 3EA CRACK FOUND AT OUTER CHORD SPLICE FTG RUNNING AFT 0.020" , 0.030" & 0.040" LONG (COUNT FROM UPPER TO LOWER ) (CRACK AT O/B FACE). STR L33 TO L34 LH BS 1480 B/H OUTER CHORD SPLICE FTG BOLT HOL E #7 REAMED TO 0.625" AND BUSHING INSTALLED AS PER SB747-53A2390 R1 HOLE CRACK FREE CONFIRMED AS PER NTM PT6-51-00-00. 2 L 7 4 4F A20WE 2002081400215 20020814 00215 NM 2002 8 14 UPS02439052 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C BS 1480 B/H LH #4 HOLE CRACK FOUND AT OUTER CHORD SPLICE FTG, RUNNING FWD APPROX 0.030" LONG. (CRACK A T O/B FACE). STR L33 TO L34 LH BS 1480 B/H LH #4 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.625 AND BUSHING INSTALLE D AS PER SB 747-53A2390 R1 HOLE CRACK FREE CONFIRMED AS PER NTM PT6-51-00-00 FIG 4 2 L 7 4 4F A20WE 2002081400216 20020814 00216 NM 2002 8 14 UPS02439053 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C LH BS 1480 B/H HOLE #5 CRACK FOUND 1EA AT FASTENER FITTING 1/16" IN LENGTH APPROX. REFER TO ATTACHED D WG FOR LOCATION. (STR L33 TO L34). LH BS 1480 B/H EXTENSION FITTING BOLT HOLE #5 REAMED TO 0.625" AND BUSHING INSTAL LED AS PER SB 747-53A2390 R1 REWORK HOLE CRACK FREE CONFIRMED AS NTM PT6-51-00-00 FIG 4. 2 L 7 4 4F A20WE 2002081400217 20020814 00217 NM 2002 8 14 UPS02439054 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C RH BS 1480 B/H HOLE #5 CRACK FOUND 2EA AT EXTENSION FITTING 1/16" IN LENGTH APPROX AND 1EA AT HOLE #5 SKIN 1/16" IN LENGTH APPROX. REFER ATTACHED DWG FOR LOCATION. (STR R33 TO R34). RH BS1480 B/H HOLE #5 AT EXTENSION FITTING AND SKIN REAMED TO 0.625" AND BUSHING INSTALLED AS PER SB 747-53A2390. REWORKED HOLE CRACK FREE CONFIRMED AS P ER NTM PART 6 51-00-00 FIG.1 2 L 7 4 4F A20WE 2002081400218 20020814 00218 NM 2002 8 14 UPS02439056 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C RH BS 1480 B/H #3 HOLE CRACK FOUND AT EXTENSION FITTING APPROX 1/16" LONG RUNNING FWD & 0.040" LONG R UNNING AFT. REFER ATTACHED SKETCH. (STR R33 TO R34). RH BS 1480 B/H #3 HOLE AT EXTENSION FITTING REAMED TO 0.625" AN D BUSHING INSTALLED AS PER SB 747-53A2390.AS PER NTM PART 6 51-00-00 FIG 1 2 L 7 4 4F A20WE 2002081400219 20020814 00219 NM 2002 8 14 UPS02439058 1 20020804 A 5330 SKIN BOEING 747 747212B 1384886 NM BS1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C RH BS 1480 B/H 33 HOLE CRACK FOUND AT SKIN THROUGH THICKNESS RUNNING FWD. REFER ATTACHED SKETCH. (STR R33 TO R34 ) RH BS 1480 B/H #3 HOLE AT SKIN REAMED TO 0.625" AND BUSHING INSTALLED AS PER SB 747-53A2390 REWORKED H OLE INSPECTED NIL CRACK FOUND AS PER NTM PART 6 51-00-00 FIG 1. 2 L 7 4 4F A20WE 2002081400220 20020814 00220 NM 2002 8 14 UPS02439060 1 20020804 A 5330 SKIN BOEING 747 747212B 1384886 NM BS1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C RH BS 1480 BULKHEAD CHROD AREA #11 HOLE CRACK FOUND AT SKIN, APPROX 1/16" RUNNING FWD. REFER ATTACHED SKETCH. (STR R34 ) RH BS 1480 B/H #11 HOLE AT SKIN REAMED TO 0.625" AND BUSHING INSTALLED AS PER SB 747-53A2390 REWO RKED HOLE INSPECTED NIL CRACK FOUND AS PER NTM PART 6 51-00-00 FIG 1. 2 L 7 4 4F A20WE 2002081400221 20020814 00221 NM 2002 8 14 UPS02439061 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C RH BS 1480 #16 HOLE CRACK FOUND AT SPLICE PLATE AFT SURFACE RUNNING UP 1/8" AND RUNNING DOWN 3/16" LON G. REFER ATTACH SKETCH. (STR R33 TO R34) RH BS 1480 B/H SPLICE PLATE REPLACED DUE HOLE CRACK EXCCEED 'D' MAX LIMIT A S PER SB 747-53A2390 FIG 11. 2 L 7 4 4F A20WE 2002081400222 20020814 00222 NM 2002 8 14 UPS02439062 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C RH BS 1480 B/H #14 HOLE CRACK AT B/H WEB AFT SURFACE RUNNING UP APPROX 3/16" LONG. REFER ATTACHED SKET CH. ( STR R33 TO R34) RH BS 1480 B/H #14 HOLE AT B/HEAD WEB REAMED TO 0.500" AND BUSHING INSTALLED AS PER SB747-53A2 390 REWORKED HOLE CRACK FREE CONFIRMED AS PER NTM PART 6 , 51-00-00 FIG 1 2 L 7 4 4F A20WE 2002081400223 20020814 00223 NM 2002 8 14 UPS02439063 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C BS 1480 RH B/H #18 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG, RUNNING O/B APPROX 0.030" LONG. (STR R3 3 TO R34) RH BS 1480 B/H #10 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.625" AND BUSHING INSTALLED AS PER SB 747-53A 2390 REWORKED HOLE INSPECTED NIL CRACK FOUND AS PER NTM PART 6 51-00-00 FIG 1. 2 L 7 4 4F A20WE 2002081400224 20020814 00224 NM 2002 8 14 UPS02439064 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C BS 1480 RH B/H #16 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG, RUNNING I/B APPROX 1/16" & O/B APPROX 1 /8" LONG.(STR R33 TO R34). RH BS 1480 B/H #16 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.562" AND BUSHING INSTALLED AS PER SB 747-53A2390 REWORKED HOLE INSPECTED ,NIL CRACK FOUND AS PER NTM PART 6 51-00-00 FIG 1 2 L 7 4 4F A20WE 2002081400225 20020814 00225 NM 2002 8 14 UPS02439065 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C BS 1480 RH B/H #14 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG, RUNNING O/B APPROX 1/16" LONG. (STR R33 TO R34) RH BS 1480 B/H #14 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.500" AND BUSHING INSTALLED AS PER SB 747-53A2 390 REWORKED HOLE INSPECTED NIL CRACK FOUND AS PER NTM PART 6 51-00-00 FIG 1 2 L 7 4 4F A20WE 2002081400226 20020814 00226 NM 2002 8 14 UPS02439066 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C BS 1480 RH B/H #7 HOLE FOUND CORROSION AROUND AND INSIDE HOLE BORE OF OUTER CHORD SPLICE FTG. (STR R33 TO R34). RH BS 1480 B/H #7 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.660 AND BUSHING INSTALLED AS PER B747-53A239 0 REWORKED HOLE INSPECTED NIL CRACK FOUND AS PER NTM PART 6 51-00-00 FIG 1 2 L 7 4 4F A20WE 2002081400227 20020814 00227 NM 2002 8 14 UPS02439067 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C BS 1480 RH B/H #9 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG. RUNNING AFT APPROX 1/16" LONG. (STR R33 TO R34) RH BS 1480 B/H #9 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.660" AND BUSHING INSTALLED AS PER SB747-53A2390 . REWORKED HOLE INSPECTED, NIL CRACK FOUND AS PER NTM PART 6 51-00-00 FIG 1. 2 L 7 4 4F A20WE 2002081400228 20020814 00228 NM 2002 8 14 UPS02439068 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C BS 1480 RH B/H #6 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG RUNNING AFT APPROX 1/16" LONG.(STR R33 T O R34). RH BS 1480 B/H #6 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.660" AND BUSHING INSTALLED AS PER SB 747-53A239 0 REWORKED HOLE INSPECTED NIL CRACK FOUND AS PER NTM PART 6 51-00-00 FIG 1. 2 L 7 4 4F A20WE 2002081400229 20020814 00229 NM 2002 8 14 UPS02439069 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C BS 1480 RH B/H #5 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG, RUNNING FWD APPROX 1/8" AND AFT APPROX 1 /16" LONG. (STR R33 TO R34). RH BS 1480 B/H #5 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.660" AND BUSHING INSTALLED AS PER SB747-53A2390. REWORKED HOLE CRACK FREE CONFIRMED AS PER NTM PART 6 51-10-00 FIG 1. 2 L 7 4 4F A20WE 2002081400230 20020814 00230 NM 2002 8 14 UPS02439070 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C BS 1480 RH B/H #3 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG, RUNNING FWD APPROX 1/16" & AFT APPROX 0. 040" LONG. (STR R33 TO R34) RH BS 1480 B/H #3 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.625" AND BUSHING INSTALLED AS PER SB 747-53A2390 REWORKED HOLE CRACK FREE CONFIRMED AS PER NTM PART 6 51-00-00 FIG 1. 2 L 7 4 4F A20WE 2002081400231 20020814 00231 NM 2002 8 14 UPS02439071 1 20020809 A 5310 FITTING BOEING 747 747212B 1384886 NM BS1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C RH BS 1480 BULKHEAD EXTENSION FITTING BOLT HOLE #11 FOUND CRACK. RH BS 1480 BULKHEAD #11 HOLE AT EXTENSION FITTING REAMED TO 0.625" AND BUSHING INSTALLED AS PER SB 747-53A2390 REWORKED HOLE INSPECTED NIL CRACK FOUND A S PER NTM PART 6 51-00-00 FIG 1. 2 L 7 4 4F A20WE 2002081400232 20020814 00232 NM 2002 8 14 UPS02439072 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C RH BS 1480 B/H #16 HOLE CRACK AT B/H WEB AFT SURFACE RUNNING UP APPROX 0.040" LONG. REFER ATTACHED SKE TCH. (STR R34) RH BS 1480 B/H HOLE AT WEB PNL REAMED TO 0.500" AND BUSHING INSTALLED AS PER SB 747-53A2390 REWORKED HOLE INSPECTED. NIL CRACK FOUND AS PER NTM PART 6 51-00-00 FIG 1. 2 L 7 4 4F A20WE 2002081400233 20020814 00233 WP 2002 8 14 MWEA020508 1 20020814 A 5740 99116033 STRINGER DOUG DC9 DC914 3022034 WP 15&16 I/B&O/B DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REPAIRED CLIPS REQUIRED INSTALL BETWEEN STRINGER 15&16 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLE D UP AND INSTALLED CLIPS. 2 L 7 2 4F A6WE 2002081400234 20020814 00234 WP 2002 8 14 MWEA020509 1 20020814 A 5740 99110633 STRINGER DOUG DC9 DC914 3022034 WP 17&16 I/B&O/B DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REPAIR CLIPS REQUIRED INSTALL BETWEEN STRINGER 17&16 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS. 2 L 7 2 4F A6WE 2002081400235 20020814 00235 WP 2002 8 14 MWEA020510 1 20020814 A 5310 5910163119 SEAL DOUG DC9 DC914 3022034 WP LH&RH APB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LEFT AND RIGHT AFT PRESSURE BULKHEAD SEAL RETAINERS ARE CRACKED. -- DRILLED UP AND INSTALLED SEAL RETAINERS. 2 L 7 2 4F A6WE 2002081400236 20020814 00236 WP 2002 8 14 MWEA020491 1 20020814 A 5740 99116033 STRINGER DOUG DC9 DC914 3022034 WP STRINGER 14&15 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 14&15 ALSO EXTENDIN G UNDER STRINGER 14&15 AND ONE SPOT ON VERTICAL LEG. -- FABRICATED AND INSTALLED SHIM 2 L 7 2 4F A6WE 2002081400237 20020814 00237 WP 2002 8 14 MWEA020492 1 20020814 A 5312 59101639 DOUBLER DOUG DC9 DC914 3022034 WP DOT 31 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT PRESSURE BULKHEAD PLUG DOOR STOP RECEPTACLE AT LOWER LEFT CORNER HAS A CRACK EMANATING FROM CUT OUT HOLE TO DOOR JAM B EGDE DOT 31. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002081400238 20020814 00238 WP 2002 8 14 MWEA020499 1 20020814 A 5312 59101639 DOUBLER DOUG DC9 DC914 3022034 WP APBJAMB DOT30 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT PRESSURE BULKHEAD PLUG DOOR STOP RECEPTACLE AT UPPER RIGHT CORNER HAS A CRACK EMANATING FROM CUTOUT HOLE TO THE DOOR JAMB EDGE DOT 30. -- FABRICATED AND INSTALLED DOUBLER, FABRICATED AND INSTALLED 8 FASTENERS. 2 L 7 2 4F A6WE 2002081400239 20020814 00239 WP 2002 8 14 MWEA020500 1 20020814 A 5312 5910163195 ANGLE DOUG DC9 DC914 3022034 WP APB RADIAL #2 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT PRESSURE BULKHEAD RIGHT HAND RADIAL #2 LOWER ANGLE THAT ATTACHES TO JAMB GUSSET HAS A CRACKED ATTACH HOLE. -- FABR ICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2002081400240 20020814 00240 WP 2002 8 14 MWEA020503 1 20020814 A 5310 59101639 STIFFENER DOUG DC9 DC914 3022034 WP 2&16 LEFT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 2 EACH DOUBLE DRILLED HOLES ON AFT PRESSURE BULKHEAD RADIAL STIFFNERS 2&6 LEFT. -- REAMED HOLE UP AND INSTALLED 2 EACH BUSHINGS. 2 L 7 2 4F A6WE 2002081400241 20020814 00241 WP 2002 8 14 MWEA02504 1 20020814 A 5310 59101639 STIFFENER DOUG DC9 DC914 3022034 WP 18&20 LEFT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 1 EACH DOUBLE DRILLED HOLES ON AFT PRESSURE BULKHEAD BETWEEN RADIAL STIFFENER 18&20 LEFT. -- REAMED HOLES AND INSTALLE D BUSHING. 2 L 7 2 4F A6WE 2002081400242 20020814 00242 WP 2002 8 14 MWEA02505 1 20020814 A 5740 99116033 STRINGER DOUG DC9 DC914 3022034 WP 14,15 & 16 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REQUESTING BOEING AGREEMENT OF FASTENER PLACEMENT IN UPPER PORTION OF REPAIR CLIPS BETWEEN STRINGER 14,15&16 THERE ARE T WO CLIPS AND TWO FASTENERS PER CLIP. -- BOEING APPROVES OF THE PLACEMENT OF THE FASTENERS. 2 L 7 2 4F A6WE 2002081400243 20020814 00243 WP 2002 8 14 MWEA020485 1 20020814 A 5740 99116033 STRINGER DOUG DC9 DC914 3022034 WP 13&12 I/B&O/B DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REPAIR CLIP REQUIRED INSTALL BETWEEN STRINGERS 13&12 ON THE INBOARD AND OUTBOARD SIDES OF XCW 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS. 2 L 7 2 4F A6WE 2002081400244 20020814 00244 WP 2002 8 14 MWEA020484 1 20020814 A 5740 99116033 STRINGER DOUG DC9 DC914 3022034 WP 14&13 I/B&O/B DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REPAIR CLIPS REQUIRED INSTALL BETWEEN STRINGERS 14&13 ON THE INBOARD AND OUTBOARD SIDE OF XCW 58 WING. 2 L 7 2 4F A6WE 2002081400245 20020814 00245 WP 2002 8 14 MWEA020483 1 20020814 A 5740 99116033 STRINGER DOUG DC9 DC914 3022034 WP 15&14 I/B&O/B DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REPAIR CLIPS REQUIRED BETWEEN STRINGERS 15&14 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS. 2 L 7 2 4F A6WE 2002081400246 20020814 00246 WP 2002 8 14 MWEA020495 1 20020814 A 5740 99116033 STRINGER DOUG DC9 DC914 3022034 WP STRINGER 18&19 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 18&19 ALSO EXTENDIN G UNDER STRINGER 18 FORWARD AND AFT. -- FABRICATED AND INSTALLED SHIM. 2 L 7 2 4F A6WE 2002081400247 20020814 00247 WP 2002 8 14 MWEA020501 1 20020814 A 5312 591016321 STIFFENER DOUG DC9 DC914 3022034 WP APB 10 O'CLOCK CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 AFT PRESSURE BULKHEAD RADIAL STIFFENER ON AFT SIDE AT 10 O'CLOCK POSSITION HAS A SMALL CRACK AT THE RIGHT SIDE. -- FAB RICATED AND INSTALLED STIFFENER. 2 L 7 2 4F A6WE 2002081400248 20020814 00248 WP 2002 8 14 MWEA020511 1 20020814 A 5312 5910163199 STIFFENER DOUG DC9 DC914 3022034 WP #6 LEFT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RECEPTACLE UNDER RADIAL STIFFENER AT 10 O'CLOCK POSITION #6 LEFT FOUND TO BE CRACKED IN 2 PLACES. -- DRILLED UP AND IN STALLED RECEPTACLE. 2 L 7 2 4F A6WE 2002081400249 20020814 00249 WP 2002 8 14 MWEA020513 1 20020814 A 7110 595873161 STIFFENER DOUG DC9 DC914 3022034 WP 5 O'CLOCK POS. CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 RADIAL STIFFENER AT 5 O'CLOCK POSITION IS CRACKED AT ATTACH FASTNER LEFT ENGINE. -- REMOVED AND REPLACED STIFFENER. 2 L 7 2 4F A6WE 2002081400250 20020814 00250 NM 2002 8 14 AWXA200200736 1 20020725 A 5320 7075T6040 WEB BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 0 0 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND ON THE LOWER WEB OF THE AFT CARGO DOOR FORWARD FUSELAGE FR AME, BS 787. MAINTENANCE REMOVED DAMAGED WEB AT AFT CARGO DOOR FORWARD FUSELAGE FRAME, FABRICATED A NEW WEB, AND INSTALL ED REPAIR IAW B737-200 SRM 51-10-01, PG. 8. 2 L 7 2 4F RT A16WE 2002081400251 20020814 00251 NM 2002 8 14 AWXA200200747 1 20020724 A 5311 6545507 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 0 0 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND ON THE FORWARD GALLEY DOOR CUTOUT FORWARD UPPER FRAME, BS 291.5. MAINTENANCE CUTOUT DAMAGED AREA OF FRAME AT FORWARD GALLEY DOOR CUTOUT, BS 291.5. FABRICATED 3 EACH REPAIR ANGLES , 2 EACH CHANNELS, AND A FILLER, AND INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-3, FIG 1. 2 L 7 2 4F RT A16WE 2002081400252 20020814 00252 NM 2002 8 14 AWXA200200749 1 20020724 A 5311 6545807 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 0 0 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND AT FASTENER HOLE ON THE FORWARD GALLEY DOOR CUTOUT, FORWAR D LOWER FRAME SECTION, INBOARD LOWER ATTACHMENT, BS 291.5. MAINTENANCE CUTOUT DAMAGED AREA OF FRAME AT FORWARD GALLEY DO OR CUTOUT, FORWARD LOWER FRAME SECTION, BS 291.5. FABRICATED 3 EACH REPAIR ANGLES, 2 EACH CHANNELS, AND A FILLER, AND IN STALLED REPAIR PARTS IAW B737-200 SRM 51-40-3, FIG 1. 2 L 7 2 4F RT A16WE 2002081400253 20020814 00253 NM 2002 8 14 AWXA200200750 1 20020731 A 5315 69353654 ANGLE BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1" CRACK WAS FOUND ON FLOOR BEAM SUPPORT ANGLE BS 400, BL 0. MAINTENANCE REMOVE D DAMAGED FLOOR BEAM SUPPORT ANGLE AT BS 400, BL 0. FABRICATED A NEW FLOOR BEAM SUPPORT ANGLE, AND INSTALLED REPAIR IAW B737-200 SRM 51-30-2, PG. 2-3. 2 L 7 2 4F RT A16WE 2002081500001 20020815 00001 WP 2002 8 15 866060702 1 20020606 A 3234 14180 SELECTOR VALVE CVAC 640 640340D 2422814 WP NLG LEAKING A JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 866TA 12318 283 NOSE LANDING GEAR WOULD NOT EXTEND AND LOCK IN THE DOWN POSITION. NOSE GEAR OPERATED NORMALLY AFTER SEVERAL CYCLES. JA CKED AIRCRAFT AND INSPECTED NOSE LANDING GEAR DURING SEVERAL CYCLES. FOUND NO MECHANICAL BINDING OR OBSTRUCTIONS. NOTE D SMALL HYDRAULIC SEEP ON NOSE GEAR ACTUATING CYLINDER, REPLACED NOSE GEAR ACTUATOR AND AGAIN INSPECTED NOSE GEAR DURING SEVERAL CYCLES. NO DEFECTS WERE NOTED. AS A PRECAUTIONARY MEASURE, THE LANDING GEAR SELECTOR VALVE IS TO BE CHANGED. A LANDING GEAR SELECTOR VALVE IS ON ORDER AT THIS TIME. AFTER REPLACING THE LANDING GEAR SELECTOR VALVE AND RECHECKIN G NOSE GEAR UPLOCK RIGGING, THE AIRCRAFT WAS GIVEN SEVERAL GEAR RETRACTION WITH SYSTEMS OPERATING NORMALLY. 2 L 7 2 4T RT A793 2002081500002 20020815 00002 EU 2002 8 15 A6WA200260032 1 20020706 A 2497 H6921H1837000 J-BOX BAC 146 146300A 1500267 EU GENERATOR SMOKE A A6WA F ACTIVATE FIRE EXT. O OTHER NR NOT REPORTED 1 GL 31 614AW 27614 E3132 PILOTS REPORT THE FORWARD CARGO SMOKE WARNING LIGHT ILLUMINATED, FIRE BOTTLE WAS FIRED. MAINTENANCE INSPECTED AND FOUND THE SOFT START RESISTOR BOX SMOLDERING. REMOVED AND REPLACED THE RESISTOR BOX ASSEMBLY. 2 H 7 4 4F RT A49EU 2002081500003 20020815 00003 WP 2002 8 15 AMTA200200895 1 20020629 A 5210 SKIN LKHEED 1011 10113851 5265010 WP PAX DOOR BENT A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 186AT 193C1074 LT NR 1 DOOR WOULD NOT CLOSE. LT CORNER OUTER SKIN BENT. REPAIRED UPPER FORWARD CORNER PER ERA. 2 L 7 3 4F A23WE 2002081500004 20020815 00004 WP 2002 8 15 AMTA200200920 1 20020702 A 5210 SKIN LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122* 54555 NE PAX DOOR BENT A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 186AT 193C1074 LEFT NR 1 DOOR UPPER FORWARD CORNER OUTER SKIN BENT. REPAIRED DOOR PER ER/A. 2 L 7 3 4F 4 F A23WE A12EU 2002081500005 20020815 00005 EU 2002 8 15 BMAC020006 1 20020620 A 7797 WIRE BAG JETSTM JETSTM3101 1500215 EU EGT DISCONNECTED A B16A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 536PA 681 DURING CRUISE FLIGHT, THE LT ENGINE EGT BEGAN TO FLUCTUATE BETWEEN 630 DEGREES AND 600 DEGREES. THE TTL WAS TURNED OFF PER THE EMERGENCY CHECKLIST, AND FLUCTUATION CONTINUED BETWEEN 580 DEGREES AND 600 DEGREES. SOME FLUCTUATION IN ENGINE SOUND WAS OBSERVED. THE SRL WAS TURNED OFF AND ALL INDICATIONS RETURNED TO NORMAL. FLIGHT DIVERTED. ALL INDICATIONS R EMAINED NORMAL. NR 1 AIRFRAME CONNECTOR PLUG AT ENGINE EGT SOFT LEAD TO HAVE BARE WIRES INTERNALLY AND IN CLOSE PROXIMI TY TO CONNECTOR PLUG INNER SHELL. REPAIRED IAW AC AND WIRING. PERFORMED ENGINE GROUND RUN, NO EGT FLUCTUATION AT THIS TIME. 2 L 7 2 4T RT A21EU 2002081500006 20020815 00006 CE 2002 8 15 CJ62002F00000 1 20020701 A 2910 651710562 LINE CESSNA 500 560CESSNA 2076750 CE HYD SYSTEM CHAFED E CJ6A K NONE K FLUID LOSS IN INSP/MAINT 1 GL 03 314QS 5600441 NOTICED HYDRAULIC FLUID LEAKING ON NOSE STRUT. FOUND NOSE GEAR EXTEND HYDRAULIC LINE SEVERELY CHAFED AND LEAKING FLUID. LINE WAS POSITIONED SUCH THAT EVERY TIME THE GEAR WAS RETRACTED THE GEAR CONTACTED THE LINE, THEREBY CAUSING THE CHAFI NG. IF LEAK IS SERIOUS ENOUGH, HYDRAULIC FLUID COULD BE DEPLETED FROM SYSTEM. SUGGEST INSPECTING ALL HYDRAULIC LINES I N THE NOSE WHEEL WELL AREA FOR IMPROPER ROUTING AND CHAFING. 2 L 7 2 4F RT A22CE 2002081500007 20020815 00007 CE 2002 8 15 CNQ2002F0000A 1 20020712 A 3297 620803230 WIRE CESSNA 650 650 2076802 CE UPLOCK SWITCH BROKEN B CNQR K NONE O OTHER IN INSP/MAINT 1 CE 07 70DJ 5889 6500058 THE LT MLG FAILED TO RETRACT AFTER TAKEOFF. FOUND TWO BROKEN WIRES ON THE LT MLG UPLOCK SWITCH. THE WIRES APPEARED TO BE OLD AND BRITTLE. REPAIRED THE TWO BROKEN WIRES AND ALL OTHER WIRES AT THE UPLOCK SWITCH. PERFORMED A FUNCTIONAL TES T OF THE LANDING GEAR SYSTEM. 2 L 7 2 4F A9NM 2002081500008 20020815 00008 NM 2002 8 15 COOSDR020221 1 20020801 A 5753 652919510 FLAP TRACK BOEING 727 727232 1384082 NM TE FLAPS BROKEN B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 511PE 20634 RT WING, INBOARD FLAP, NR 5 MOVABLE FAIRING INBOARD FAIRING TRACK, BROKEN. 2 L 7 3 4F A3WE 2002081500009 20020815 00009 WP 2002 8 15 COOSDR020222 1 20020801 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 602AL 45991 PAX CABIN AT STA Y781.500 CRACKED FITTING. 2 L 7 4 4F RT 4A25 2002081500010 20020815 00010 WP 2002 8 15 COOSDR020225 1 20020801 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 602AL 45991 LOWER FUSELAGE STA Y640 CRACKED FITTING. 2 L 7 4 4F RT 4A25 2002081500011 20020815 00011 WP 2002 8 15 COOSDR020226 1 20020801 A 5210 FITTING DOUG DC8 DC873F 302199F WP AFT PAX DOOR CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 602AL 45991 AFT ENTRANCE DOOR HAS A CRACKED FITTING. 2 L 7 4 4F RT 4A25 2002081500012 20020815 00012 WP 2002 8 15 COOSDR02219 1 20020801 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 815US 48095 IN THE PASSENGER CABIN AT THE MAIN ENTRY DOOR AT STA 160.0, LONGERON 18 LT LOWER CUSP WEB HAS CORROSION. 2 L 7 2 4F A6WE 2002081500013 20020815 00013 EA 2002 8 15 DAT2002F00001 2 20020626 A 7250 3029303 BLADE STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45 52043 EA LT ENGINE BROKEN E DATA K NONE O OTHER IN INSP/MAINT 1 GL 13 167RC 17206 SH3038 LT ENGINE STARTED TO SHAKE AFTER START UP. THE CREW SHUTDOWN THE ENGINE AND EXITED THE AIRCRAFT. MAINTENANCE INSPECTED THE LT ENGINE AND FOUND 2 BROKEN PT BLADES WHICH CAUSED BINDING OF THE POWER SECTION. THE POWER SECTION IS BEING REMOV ED AND REPLACED. 2 H 7 2 4T 4 T A41EU E4EA 2002081500014 20020815 00014 WP 2002 8 15 DSJ2002F00000 1 20020522 A 7931 CONNECTOR CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL OIL PRESS XMITER CORRODED B VGCA K NONE N L FALSE WARNING NO TEST IN INSP/MAINT 1 GL 23 151FL 51 INSPECT NR 1 ENGINE FOR EXCESSIVE OIL USEAGE / CONSUMPTION. INSTALLED NEW SEAL ON ENGINE. LT ENGINE OIL PRESSURE LIGH T CAME ON VERY DIM. FEATHERED LT ENGINE (PRECAUTIONARY) CORRECTION. FOUND CORROSION ON OIL PRESSURE TRANSMITTER CONNEC TOR PLUG FOR GEARBOX. CLEANED AND GROUND CHECK, NORMAL. 2 L 7 2 4R 4 T 6A6 E282 2002081500015 20020815 00015 NE 2002 8 15 EAS2002F00000 2 20020704 A 7321 5002T94G33 FUEL CONTROL LEAR 24 24D 5170311 CE GE CJ610 CJ6106 30006 NE LT ENGINE MALFUNCTIONED E EASA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 EA 23 701SC 8415 24D235 251240A LT ENGINE FLAMED OUT AT 45,000 FT WITH NO PRIOR ABNORMAL INDICATIONS NOTED. LT ENGINE RESTARTED AT 19,000 FT AND A/C LA NDED SAFELY. INSPECTED THE LT ENGINE FUEL SYS, REMOVED FUEL PUMP FILTER. NO DEFECTS OR NOTED. REINSTALLED. REMOVED LT ENGINE FUEL CONTROL FILTER. NO DEFECTS OR FOUND. REINSTALLED FILTER. REMOVED HIGH PRESS FUEL FILTER, NO DEFECTS F OUND. REASSEMBLED AND REINSTALLED. LOW POWER ENGINE RUN AND LEAK CHECK SATISFACTORY. HIGH POWER PERFORMANCE ENGINE RU N ACCOMPLISHED. FUEL SAMPLES PRIOR TO AND AFTER FLIGHT SHOWED NO SIGNS OF WATER. IT WAS DETERMINED THAT LT ENGINE FUEL CONTROL MIGHT BE OF CONCERN AND SHOULD BE REPLACED. 2 L 7 2 4J 4 J A10CE 1E16 2002081500016 20020815 00016 NM 2002 8 15 EIA2002087 1 20020722 A 2432 BATTERY BOEING 747 747212B 1384886 NM MAIN ELECTRICAL SMOKE A EIAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 482EV 20713 3 HOURS INTO FLIGHT, AIRCRAFT BATTERY BEGAN TO VENT SMOKE AND HAD AN ELECTRICAL ODOR. A FLIGHT TURN BACK WAS DONE. 2 L 7 4 4F A20WE 2002081500017 20020815 00017 WP 2002 8 15 GTIA020830 1 20020717 A 2780 833702 SWITCH DOUG DC9 DC982 3022082 WP FLAPS AND SLATS FAILED A GTIA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 23 803NK 48087 ON FINAL, FLAPS 28 DEGREES, SLATS LANDING AT VREF PLUS 10, SLAT DISAGREEMENT AND LANDING LIGHT STARTED CYCLING BACK AN D FORTH RECEIVED A STICK SHAKER AND EXECUTED GO AROUND. LEVEL AT 200 KIAS, 15 DEGREE FLAPS, THE SLAT INDICATION WAS C YCLING BETWEEN TAKEOFF, DISAGREEMENT. FOUND NO CHECK LIST ON Q/H APPLICABLE. COME BACK AROUND, FLAPS 40 DEGREE WITH REF PLUS 20, SLATS STAY IN LANDING UNTIL SLOWED IN FLAIR AND THEN CYCLED AGAIN. FOUND BAD LT WING SLAT "D" SWITCH. R/R LT WING SLAT "D" PROX SENSOR AND R/R RT WING SLAT "D" SWITCH AS PRECAUTIONARY. OPS CHECK GOOD PER MM. PERFORMED BIT CHECK ON BOTH STALL WARNING COMPUTERS. PER MM. OPS CHECKED GOOD. PERFORMED TEST ON PROX ELECT UNIT PER MM. OPS 2 L 7 2 4F A6WE 2002081500018 20020815 00018 NE 2002 8 15 GTIA020846 2 20020714 A 7230 JT8D217C BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE NR 1 COMPRESSOR NICKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 33705 48048 NR 1 ENGINE C1 FAN BLADES ARE ROUGH AND HAVE NICKS. NR 1, SN 718528, FAILED BORESCOPE INSPECTION , C-7 DISK 10 BLADES W ITH NICKS AND MISSING MATERIAL. 2 BLADES DAMAGED NEAR TIP (1) MEASURES .140 INCH LONG (2) MEASURES .165 INCH LONG WITH A CRACK PROPAGATING UPWARD FROM UPPER EDGE OF NICK. ENGINE REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 2002081500019 20020815 00019 WP 2002 8 15 GTIA020857 1 20020708 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 DENT AT FS 69 ABOVE RT NLG DOOR. REQUIRES PAINT REMOVAL, DYE PENETRANT INSPECTION FOR CRACKS, EVALUATION, REPAINT AND C ARRY OVER LOG ITEM FOR FURTHER INSPECTION. UPON FURTHER INVESTIGATION FOUND SKIN TO BE GOUGED AT DENT LOCATION. AREA FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER, INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2002081500020 20020815 00020 CE 2002 8 15 HMG2002F00002 1 20020708 A 5414 13091003140 DOOR BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE NACELLE DEPARTED A HMGA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SW 15 224CR FL60 PCE95609 LT INBOARD NACELLE DOOR DEPARTED AIRCRAFT IN FLIGHT AND PUNCTURED THE FUSELAGE. 2 L 7 2 4T 4 T A24CE E4EA 2002081500021 20020815 00021 GL 2002 8 15 IUEA02016 1 20020508 A 5420 015U127525 PIN BOEING 747 747300 GL GE CF6 CF650E2 30018 NE NR4 PYLON MISALIGNED A IUEA K NONE O OTHER IN INSP/MAINT 1 EA 15 24837 24837 530277 DURING WALK AROUND DAILY CHECK, INSPECTION FOUND NR 4 ENGINE PYLON MIDSPAR FUSE PIN ALIGNMENT STRIPES MISALIGNED BY 0.5 INCH. CLOSER INVESTIGATION POINTS TO POSSIBLE FUSE PIN FAILURE. THIS AS PER MM. FURTHER INSPECTION FOUND SPRING BEA MS CRACKED, REPLACEMENT REQUIRED. REPLACED SPRING BEAMS (PN 65B9413931 AND PN 65B9413932) PER MM. REPLACED FUSE PINS (PN 015U127525) PER MM. PERFORMED HARD LANDING INSPECTION PER MM. ENGINE RUN CHECKS, OK. DETAILED REPAIR SERVICE PACK AGE ON FILE AT MFG HDG PURCHASE. 2 L 7 4 4F 4 F RT A20WE E23EA 2002081500022 20020815 00022 EU 2002 8 15 JGV2002F00005 1 20020628 A 5730 FASTENER AMD FALC50 FALCON50MYST 2730106 EU RT WING WRONG PART B JGVR K NONE K FLUID LOSS IN INSP/MAINT 1 CE 09 78LT 75 LEAKING FASTENERS LOCATED ON THE RIGHT WING LOWER SURFACE REMOVABLE PLANK, CAME UPON INCORRECT FASTENER INSTALLED. FAST ENER WAS A 6 MM DIAMETER RATHER THAN A 5 MM DIAMETER AND SHORT IN LENGTH. FOUND THAT NUTPLATE, LOCATED INSIDE WING FUE L TANK, WAS MISSING OR BROKEN. AFTER REMOVAL OF PR SEALANT INSIDE THE FASTENER HOLE, DISCOVERED THE HOLE TO BE OVERSIZE D AND TAPPED. VISUAL INSPECTION REVEALED THAT FASTENERS WERE NOT INSTALLED IN THEIR EXACT LOCATION, NUMEROUS FASTENERS, ON THE REMOVABLE PLANK, NOT LOCKED INTO THE NUT PLATES LOCATED INSIDE THE WING TANK. IMPROPER FASTENER INSTALLATION AN D UNAUTHORIZED MODIFICATION TO THE WING PLANK, COULD SERIOUSLY JEOPARDIZE THE SAFETY OF THE CREW AND PASSENGERS. 2 L 7 3 4F A46EU 2002081500023 20020815 00023 EU 2002 8 15 JGV2002F00006 1 20020628 A 5730 PANEL AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP RT WING DAMAGED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 347K 46 PERFORMING FASTENER LEAKAGE REPAIR ON THE RIGHT WING LOWER REMOVABLE PLANK AND DISCOVERED AND INCORRECT FASTENER LOCATED IN THE FORWARD/INBOARD CORNER OF THE PLANK. UPON REMOVAL OF THE FASTENER, THE MECHANIC DISCOVERED THE FASTENER TO BE I NCORRECT IN LENGTH AND DIAMETER. FASTENER HOLE AND COUNTERSINK WERE CLEANED AND INSPECTED. DISCOVERED THE FASTENER HOL E HAD BEEN ENLARGED AND TAPPED. NUT PLATE INSIDE THE WING TANK WAS BROKEN AND MISSING. PERFORMED PLANK REMOVAL AND REP AIR ON THE PLANK, RIB, AND NUT PLATE. CUSTOMER HAD CONCERNS OF THE CONDITION OF THE LEFT WING LOWER REMOVABLE PLANK. H OLE WAS ENLARGED, THE PLANK TAPPED, AND THE NUT PLATE INSIDE THE TANK WAS DAMAGED AND MISSING. PERFORMED REPAIR. 2 L 7 3 4F 4 F A46EU E6WE 2002081500024 20020815 00024 CE 2002 8 15 JGV2002F00007 1 20020723 A 1100 PLACARD LEAR 45 45LEAR 5170805 CE SEAT BELT WORN B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 828CA 159 (TSO TABS ON CABIN BELTS) LOW GRADE IN USED FOR TSO INFORMATION, CABIN SEAT BELTS, RUBS OFF TOO EASY, CAN NOT READ TSO INFORMATION. (PAC-SCI BELTS) 2 L 7 2 4F RT T00008WI 2002081500025 20020815 00025 EU 2002 8 15 JGV2002F00008 1 20020628 A 1430 FASTENER ISRAEL 1125 ASTRASPX 4500205 EU WINDOW FRAME INTERFERENCE B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 100GA 139 RIVET BUCK TAIL INTERFEARENCE WITH CABIN WINDOW FLANGES ON THE PERIMETER OF WINDOW FRAME. WINDOW SEALS CUT AT FACTORY. REPAIRED PER EO DDA0825W342121 REVD. INSTALLED NEW SEALS, ALL CABIN WINDOWS. 2 L 7 2 4F RT A16NM 2002081500026 20020815 00026 CE 2002 8 15 JGV2002F00009 1 20020725 A 2497 5511301 RESISTOR BFGOODRICH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE POWER SUPPLY DELAMINATED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 118RK 8416 5600389 BURNED CIRCUIT TRACES ON CELL HEATING RESISTOR (HR1). HEATING RESISTOR IS DELAMINATING AT ONE OF BURNED AREAS. FOUND D URING ROUTINE INSPECTION OF UNIT. ALTHOUGH THESE HEATING RESISTORS BURN AT RANDOM SERIES AREAS, MOST COMMON AREA IS BET WEEN CELLS NR 9 AND NR 12. 2 L 7 2 4F 4 F RT A22CE E25EA 2002081500027 20020815 00027 NE 2002 8 15 KBMA119534 2 20020801 A 7421 IGNITER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 2273A 2273 IGNITER INOPERATIVE. REPLACED WITH REPAIRED IGNITER. 1 G 7 1 3U 3 U NC H9EU E19EU 2002081500028 20020815 00028 SO 2002 8 15 LD22002F00001 1 20020624 A 2913 1159SCH5057 PUMP GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE HYD SYSTEM FAILED B LD2R K NONE O OTHER IN INSP/MAINT 1 GL 15 83M 1468 557 11225 FLUID SAMPLE TAKEN AT 100 HOUR INTERVAL SHOW THAT THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP AND BLED SYSTEM WITH SIG HT GAUGE INSTALLED IN RETURN LINE OF HYDRAULIC RIG TO HELP EVALUATE AIR REMOVAL FROM SYSTEM. WE WILL CONTINUE TO MONITO R FLUID SAMPLES. FAILED THEIR FLUID SAMPLES (WEAR IN THE PUMP) PER 3M. 2 L 7 2 4F 4 F RT A12EA E00057EN 2002081500029 20020815 00029 SO 2002 8 15 LD22002F00002 1 20020624 A 2913 3029091 PUMP GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE HYD SYSTEM FAILED B LD2R K NONE O OTHER IN INSP/MAINT 1 GL 15 83M 1468 557 11225 FLUID SAMPLE TAKEN AT 100 HOUR INTERVAL SHOW THAT THE PUMP NEEDS TO BE REPLACED. REPLACE PUMP AND BLED SYSTEM WITH SIGH T GAUGE INSTALLED IN RETURN LINE OF HYDRAULIC RIG TO HELP EVALUATE AIR REMOVAL FROM SYSTEM. WE WILL CONTINUE TO MONITOR FLUID SAMPLES. FAILED THEIR FLUID SAMPLES. (WEAR IN THE PUMP) PER 3M. 2 L 7 2 4F 4 F RT A12EA E00057EN 2002081500030 20020815 00030 WP 2002 8 15 MEX2002236 1 20020722 A 2150 A/C PACK DOUG DC9 DC982 3022082 WP LEFT FAILED A ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 1003X 48067 AIRCRAFT ABORTED TAKE OFF AS DUE TO INOPERATIVE RT A/C PACK AND THE LT ONE WAS DEFICIENT. BOTH AIRCRAFT PACKS WERE CHEC KED FOR LEAKS, EVERYTHING WAS OK. PERFORMED AN AUTO TEST ON BOTH PRESSURIZATION CONTROLLERS, CHECKED OK. OPERATIONAL T ESTS TO BOTH A/C PACKS, OK. 2 L 7 2 4F A6WE 2002081500031 20020815 00031 2002 8 15 MEX2002245 4 20020729 A 3441 2587794 FLOW VALVE DOUG DC9 DC982 3022082 WP COMPASS FAILED A ASMF O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 23 491SH 49150 PILOT REPORTED A DIFFERENCE OF 6 DEGREES BETWEEN COMPASS AND RADAR WITH AN INDICATION FAILURE AND FLIGHT DIRECTORS OUT O F SERVICE IN TAKE OFF. DUE TO SUCH A FAILURE, A CHANGE OF EQUIPMENT WAS REQUESTED. THE FLOW VALVE OF THE COMPASS SYST EM WAS REPLACED, IAW MM, TEST OK. 2 L 7 2 4F A6WE 2002081500033 20020815 00033 EU 2002 8 15 MALA020447 1 20020718 A 3260 CONNECTOR BAC 146 AVRO146RJ85A 1500097 EU RT MLG LOOSE A MALA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 GL 15 513XJ E2329 FLT ATTEMPTED AN APPROACH BUT ENDED UP GOING MISSED DUE TO WIND SHEER. THEN RECEIVED AN INDICATION THAT THE GEAR WAS NO T UP AND LOCKED. ELECTED TO DIVERT THE FLIGHT TO CVG DUE TO THE FACT THAT IT IS A MAINTENANCE BASE. THE FLIGHT LANDED IN CVG WITH NO PROBLEMS. MAINTENANCE FOUND RT MLG UPLOCK SENSOR CANNON PLUG LOOSE. REMOVED AND CLEANED CANNON PLUG AND REINSTALLED. REMOVED AND CLEANED DOOR UPLOCK SENSOR CANNON PLUG AND REINSTALLED. PERFORMED GEAR SWING IAW AMM 32-30-0 0, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2002081500034 20020815 00034 EU 2002 8 15 MALA020450 1 20020805 A 5210 BRACKET BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR OUT OF RIG A MALA K NONE O OTHER TX TAXI/GRND HDL 1 GL 15 503XJ E2310 ON FLIGHT 3476, MAIN CABIN DOOR DIFFICULT TO OPERATE. MAINTENANCE FOUND GAP BETWEEN BAULK BLADE AND BRACKET OUT OF RIG. ADJUSTED AS REQUIRED, IAW AVRO AMM 52-11-00. OPS CHECK GOOD, OK FOR SERVICE. 2 H 7 4 4F RT A49EU 2002081500035 20020815 00035 NM 2002 8 15 QXEA0200968 1 20020715 A 7120 SUPPORT DHAV DHC8 DHC8202 2809007 NM LT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LT NACELLE LOWER INBOARD ENGINE SUPPORT TUBE IS CHAFED APPROXIMATELY 22 INCHES FROM FORWARD END. REPAIRED IAW RD 8-54-036 AND HORIZON AIR EA 2-54-147. 2 H 7 2 4T RT A13NM 2002081500036 20020815 00036 WP 2002 8 15 MEX2002246 1 20020729 A 2611 SMOKE DETECTOR DOUG DC9 DC987 3022087 WP LAVATORIES MALFUNCTIONED A ASMF O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 23 204AM 49404 THE THREE LAVATORY SMOKE DETECTOR ALARMS WERE FLASHING AND DID NOT TURN OFF. THE SYSTEM WAS RESET BUT THE ALARM CONTINU ED RINGING. DUE TO SUCH A FAILURE, A CHANGE OF EQUIPMENT WAS REQUESTED. THE SYSTEM AND THE SMOKE DETECTOR CONNECTORS WERE CHECKED, AUTO TEST WAS PERFORMED AND IT WAS OK. 2 L 7 2 4F RT A6WE 2002081500037 20020815 00037 NM 2002 8 15 QXEA0200969 1 20020715 A 7120 SUPPORT DHAV DHC8 DHC8202 2809007 NM LT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LT NACELLE UPPER INBOARD ENGINE SUPPORT TUBE IS CHAFED WHERE WIRE BUNDLE IS IN CONTACT APPROXIMATELY 12 INCHES FRO M AT END OF TUBE. REPAIRED IAW RD 8-54-036 AND HORIZON AIR EA 2-54-147. 2 H 7 2 4T RT A13NM 2002081500038 20020815 00038 NM 2002 8 15 QXEA0200972 1 20020708 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX- FUSLEAGE SKIN BELOW UPPER TCAS ANTENNA HAS PITTING CORROSION. REPAIRED IAW DHC-8 SRM 51-20-11 AND 51-20-16. 2 H 7 2 4T RT A13NM 2002081500039 20020815 00039 NM 2002 8 15 QXEA0200973 1 20020712 A 5720 SUPPORT DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX- LEFT HAND WING TOP TRAILING EDGE SUPPORT STRUCTURE HAS CHAFE DAMAGE FROM CONTACTING OUTBOARD FLAP WHILE IN THE UP P OSITION. REPAIRED IAW DHC-8 RD 8-57-1549. 2 H 7 2 4T RT A13NM 2002081500040 20020815 00040 NM 2002 8 15 QXEA0200986 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LT OUTBOARD SEAT TRACK X546 HAS TWO GOUGES IN CHANNEL AND SEVERAL ON TOP FLANGE. REPAIRED IAW DHC-8-202 SRM 51-20 -16 AND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2002081500041 20020815 00041 NM 2002 8 15 QXEA0200987 1 20020708 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LT INBOARD SEAT TRACK X230 TO X235 HAS CORROSION PITS IN RADIUS OF OUTBOARD FLANGE. REPAIRED IAW DHC-8-202 SRM 51 -40-11 AND SRM 51-40-16. 2 H 7 2 4T RT A13NM 2002081500042 20020815 00042 NM 2002 8 15 QXEA0200988 1 20020705 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM NACELLE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - FRETTING CORROSION ON AFT ALUMINUM LAND UNDER PANEL 422DT NEAR CENTER NUT PLATE. REPAIRED IAW DHC-8-200 SRM 51-00 -26, TABLE 2 ON PAGE 2. 2 H 7 2 4T RT A13NM 2002081500043 20020815 00043 NM 2002 8 15 QXEA0200989 1 20020705 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM NACELLE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - FRETTING CORROSION ON AFT ALUMINUM LAND UNDER PANEL 422DT NEAR CENTER NUT PLATE. REPAIRED IAW DHC-8-202 SRM 54-00 -16, TABLE 1 ON PAGE 2. 2 H 7 2 4T RT A13NM 2002081500044 20020815 00044 NM 2002 8 15 QXEA0200990 1 20020708 A 2701 CONTROL COLUMN DHAV DHC8 DHC8202 2809007 NM COCKPIT EXCESS PLAY A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - COPILOT CONTROL COLUMN HAS .1875 INCH OF FREE PLAY FOR AND AFT RELATIVE TO CAPTAINS CONTROL COLUMN IN MIDDLE OF TR AVEL. REPAIRED IAW HORIZON AIR EA 2-27-61. 2 H 7 2 4T RT A13NM 2002081500045 20020815 00045 NM 2002 8 15 QXEA0200991 1 20020713 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LEFT HAND INBOARD SEAT TRACK X438.5 HAS A CORROSION PIT IN THE CHANNEL. REPAIRED IAW RD 8-53-4472, RD 8-53-4473, RD 8-53-1102 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002081500046 20020815 00046 NM 2002 8 15 QXEA0200992 1 20020708 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - RT WING FRONT SPAR TOP CAP SCRATCHED APPROXIMATELY 10 INCHES LONG AT YW225. REPAIRED IAW RD 8-57-1119. 2 H 7 2 4T RT A13NM 2002081500047 20020815 00047 NM 2002 8 15 QXEA0200993 1 20020708 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - RT WING FRONT SPAR TOP CAP SCRATCHED APPROXIMATELY 10 INCHES LONG OUTBOARD OF YW279. REPAIRED IAW RD 8-57-1119. 2 H 7 2 4T RT A13NM 2002081500048 20020815 00048 NM 2002 8 15 QXEA0200994 1 20020708 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - RT WING FRONT SPAR BOTTOM CAP SCRATCHED BETWEEN YW207 AND YW279. REPAIRED IAW RD 8-57-1119. 2 H 7 2 4T RT A13NM 2002081500049 20020815 00049 NM 2002 8 15 QXEA0200995 1 20020712 A 5720 SUPPORT DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - RT WING TOP TRAILING EDGE SUPPORT STRUCTURE HAS CHAFE DAMAGE FROM CONTACTING FLAP WHILE IN UP POSITION, AT YW174. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-57-1549, PAGE 3, STEPS 1, 3, AND 4. 2 H 7 2 4T RT A13NM 2002081500050 20020815 00050 NM 2002 8 15 QXEA0200996 1 20020708 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - CENTER FORWARD CARGO FLOOR AFT FLOOR FLANGE ANGLE BETWEEN LEFT AND RIGHT INBOARD SEAT RAILS AT X600.00 HAS CORROSI ON. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002081500051 20020815 00051 NM 2002 8 15 QXEA0200999 1 20020707 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - THERE IS CORROSION ON FUSELAGE SKIN SURFACE UNDER LOWER TRANSPONDER ANTENNA. REPAIRED IAW DHC-8 SRM 51-20-16, PAG E 3 AND SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002081500052 20020815 00052 NM 2002 8 15 QXEA0201002 1 20020710 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - PITTING CORROSION ON RIGHT HAND INBOARD SEAT TRACK NR 8 AT STATION 500. REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40 -11. 2 H 7 2 4T RT A13NM 2002081500053 20020815 00053 NM 2002 8 15 QXEA0201003 1 20020707 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM CENTER WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - CENTER, AFT WING SPAR FLANGE HAS CHAFING FROM LEFT HAND WING YW48.00 TO RIGHT WING YW48.00. REPAIRED IAW RD 8-57- 1434. 2 H 7 2 4T RT A13NM 2002081500054 20020815 00054 NM 2002 8 15 QXEA0201004 1 20020717 A 5753 DOUBLER DHAV DHC8 DHC8202 2809007 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - RIGHT HAND OUTBOARD FLAP REPAIR PATCH ON TOP SIDE AT INBOARD END IS CHAFED FROM CONTACTING UNDERSIDE OF WING TRAIL ING EDGE. REPAIRED IAW RD 8-57-122 AND DHC-8 SRM 51-20-26. 2 H 7 2 4T RT A13NM 2002081500055 20020815 00055 NM 2002 8 15 QXEA0201005 1 20020706 A 1430 BOLT DHAV DHC8 DHC8202 2809007 NM RT WING FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - RIGHT WING TO FUSELAGE ATTACHMENT BOLT FAILED ULTRA SONIC INSPECTION. REPLACED BOTH IAW HORIZON AIR EA 2-57-167. 2 H 7 2 4T RT A13NM 2002081500056 20020815 00056 NM 2002 8 15 QXEA0201006 1 20020702 A 5730 PLATE DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LADDER PLATE FOR PANEL 622AT HAS FRETTING CORROSION AROUND ONE BOLT HOLE. REPAIRED IAW DHC-8-200 RD 8-57-1471. 2 H 7 2 4T RT A13NM 2002081500057 20020815 00057 NM 2002 8 15 QXEA0201007 1 20020709 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - RIGHT SIDE FRAME 4 STRINGER 3, STRAIGHT UP LOOKING THROUGH PANEL 311AB HAS APPROXIMATELY 1 INCH CRACK. REPAIRED I AW RD 8-55-199. 2 H 7 2 4T RT A13NM 2002081500058 20020815 00058 NM 2002 8 15 QXEA0201009 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LEFT HAND OUTBOARD SEAT TRACK X317 HAS LIGHT SURFACE CORROSION. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20 -41. 2 H 7 2 4T RT A13NM 2002081500059 20020815 00059 NM 2002 8 15 QXEA0201010 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LEFT HAND OUTBOARD SEAT TRACK LIGHT CORROSION FROM X332 TO X334. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-2 0-41. 2 H 7 2 4T RT A13NM 2002081500060 20020815 00060 NM 2002 8 15 QXEA0201011 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LEFT HAND OUTBOARD SEAT TRACK X391.45 HAS LIGHT SURFACE CORROSION. REPAIRED IAW DHC-8200 SRM 51-20-16 AND SRM 51- 20-41. 2 H 7 2 4T RT A13NM 2002081500061 20020815 00061 NM 2002 8 15 QXEA0201012 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LEFT HAND OUTBOARD SEAT TRACK X375 HAS LIGHT SURFACE CORROSION. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20 -41. 2 H 7 2 4T RT A13NM 2002081500062 20020815 00062 NM 2002 8 15 QXEA0201013 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION IN CHANNEL AT X424. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2002081500063 20020815 00063 NM 2002 8 15 QXEA0201014 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LEFT HAND OUTBOARD SEAT TRACK AT X438 HAS LIGHT CORROSION IN THE CHANNEL. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2002081500064 20020815 00064 NE 2002 8 15 MEX2002247 2 20020730 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE RIGHT MALFUNCTIONED A ASMF D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 838AM 49397 AIRCRAFT RETURNED TO PLATFORM DUE TO THE RT ENGINE DID NOT ACCELERATE AND ALSO IT HAD A LOW INDICATION OF N2. DURINE TH E FAILURE VERIFICATION, THERE WERE OSCILATIONS IN THE INDICATIONS OF N2, EPR AND FUEL FLOW. ENGINE TOOK 20 SECONDS IN A CCELERATE. THE THROTTLE CHAMBER WAS LUBRICATED AND PERFORMED TRIM IAW MM. ACCELERATION TEST OK. 2 L 7 2 4F 4 F RT A6WE E2EA 2002081500066 20020815 00066 2002 8 15 372PA0011 4 20020803 A 2230 AUTOTHRUST SYS BOEING 737 737306 13844BG NM COCKPIT INTERMITTENT A PIDA K NONE O OTHER CR CRUISE 1 SO 05 372PA 23546 AUTO THROTTLE INTERMITTENTLY INOP, T/S SYSTEM. NO FAULTS FOUND ON A/T BITE TEST & SERVO/LRU'S. OPS CHECK OK, REF TO MM 22-04-10. 2 L 7 2 4F RT A16NE 2002081500067 20020815 00067 WP 2002 8 15 ARWA20020801 1 20020803 A 3240 AE2460000G024 HYDRAULIC LINE DOUG DC8 DC863F 302198F WP LT MLG BLOWN A ARWA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 19 441J 45988 LOST ALL HYDRAULIC ON LANDING. CHECK HYDRAULIC QUANTITY AND TO BOC AT STANDARD PIPE. REPLACED BLOWN BRAKE HYDRAULIC LI NE AT LT GEAR, SERVICED MAIN HYDRAULIC SYSTEM; RUN UP ENGINES AND CHECK HYDRAULIC PUMPS OFR OPS AND FOUND NORMAL. OPERA TED ALL FLIGHT CONTROLS AND ALL NORMAL; NO HYDRAULIC LEAKS DETECTED IAW MM 20-12-0 AND MM 12-31-1. INSTALLED TEMP FLEX LINE LT GEAR. 2 L 7 4 4F 4A25 2002081500068 20020815 00068 WP 2002 8 15 AT0200072 1 20020806 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN NOT SEATED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 821AT 47284 EMERGENCY LIGHTING OVERWING EXIT MARKERS INOPERATIVE (LEFT FORWARD AND AFT AND RIGHT FORWARD). SEATED EMERGENCY LIGHTIN G BATTERIES IN PACK B5-33, AND RESERVICED GROUND AT AFT RIGHT HAND OVERWING EXIT MARKER ASSY. OPS CHECK GOOD PER DC9 MM 33-50. 2 L 7 2 4F A6WE 2002081500069 20020815 00069 WP 2002 8 15 MEX2002248 1 20020730 A 2910 LINE DOUG DC9 DC982 3022082 WP HYD SYSTEM DAMAGED A ASMF A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 23 505MD 49149 ON DEPARTURE, CAPTAIN REPORTED THE PRESENCE OF SMOKE IN THE PASSENGER CABIN. THE HYDRAULIC SYSTEM WAS VERIFIED TO BE L EAKING AND THE APU WAS SHUTDOWN DUE TO HYDRAULIC FLUID IN IT, AND THE A/C PACK WAS CONTAMINATED. HYDRAULIC LINE OF THE RT REVERSE FILTER WAS DAMAGED. A HIGH PRESSURE HOSE WAS INSTALLED AS PROVISIONAL OPTION AND WATER SEPARTORS OF BOTH A/C PACKS WERE REPLACED, DUCTS CONTAMINATED BY HYDRAULIC FLUID WERE CLEANED, TEST OK. THE HOSE WAS REPLACED WITH THE RIGHT LINE IAW MM AND OPERATIONAL TEST TO THE APU AND A/C PACKS. EVERYTHING OK. 2 L 7 2 4F A6WE 2002081500070 20020815 00070 WP 2002 8 15 NQ52002F00000 1 20020709 A 5320 340331025221 INTERCOSTAL CVAC 440 440 2422902 WP ALLSN 501D 501D13 03004 GL FUSELAGE CRACKED B NQ5R K NONE O OTHER IN INSP/MAINT 1 GL 23 51255 18207 383 501554 SLIGHT SURFACE CRACKING DETECTED IN THE RADIUS OF INTERCOSTAL (TEE) PN3403310252-21 (FORWARD RIGHT ESCAPE HATCH FRAME). INTERCOSTAL IS PART OF FUSELAGE BELTFRAME ASSEMBLY AT FS 334.749 AND PROVIDES THE FORWARD, VERTICAL SEATING SURFACE FOR THE ESCAPE HATCH. 2 L 7 2 4R 4 T 6A6 E282 2002081500071 20020815 00071 2002 8 15 O2G2002F00000 4 20020716 A 2213 70608 CONTROL UNIT CNDAIR CL604 CL604 1900301 EA PITCH TRIM FAILED E O2GA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NE 03 1DG 71 5516 MACH TRIM FAILURE BY AUTOPILOT PITCH TRIM. SHORTLY AFTER THE STABILIZER CHANNEL NR1 TRIM FAILED RESULTING IN A LOSS OF ALL PITCH TRIM. REMOVED AND REPLACED HSTCU BOX, SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2002081500072 20020815 00072 SO 2002 8 15 C2XA02CL157 1 20020802 A 2741 3621001007 CONTROL UNIT EMB 135 EMB135LR 3260305 SO HORIZ STAB INOPERATIVE A C2XA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 27 27523 7054 145389 CLE - THE CREW REPORTED A PITCH TRIM 1 INOP MESSAGE DURING CLIMBOUT. BOTH TRIM SWITCHES ON YOKE WERE INOPERATIVE. THE BACKUP TRIM WAS OPERATIONAL. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HSC U. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002081500073 20020815 00073 SO 2002 8 15 C2XA02CL158 1 20020803 A 2710 41012130103 DAMPER EMB 145 EMB145LR 3260212 SO AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 1365 145557 DURING A 3A INSPECTION THE LEFT AILERON DAMPER ROD END BEARING WAS FOUND LOOSE. THIS ROD END CONNECTS TO THE AILERON FI TTING. FURTHER INSPECTION REVEALED DAMAGE TO THE AILERON DAMPER FITTING. THE LEFT AILERON WAS REPLACED ALONG WITH THE AILERON DAMPER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002081500074 20020815 00074 SO 2002 8 15 C2XA02CL159 1 20020802 A 3350 74441 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 15973 145159 CLE - FLIGHT 3284, THE CREW REPORTED THE EXIT SIGN AT SEAT 12A WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBL Y. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002081500075 20020815 00075 NM 2002 8 15 OZI2002F00000 1 20020617 A 5730 SKIN BOEING 737 737* NM LT & RT WING CHAFED A OZIA K NONE O OTHER IN INSP/MAINT 1 CE 05 461LF 30635 DURING SCHEDULED INSPECTION CHECK, WING LOWER SURFACE OF BOTH THE LT AND RT WING SKINS, WERE SEVERLY CHAFED AT EACH FLAP TRACK FAIRING. ALL THE DAMAGE APPEARS TO BE CAUSED BY CONTACT BETWEEN THE WING LOWER SKIN AND THE (BLADE SEAL), WHICH IS ATTACHED TO THE ENGINE AFT POSITION FAIRING. 2 L 7 2 4F RT A16WE 2002081500076 20020815 00076 CE 2002 8 15 RU32002F00000 1 20020724 A 2120 SMOKE BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE CABIN DETECTED E RU3A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 15 78 FF13 ON TURN FOR NDB APPROACH, TECH REPORTED (ELECTRONIC BURNING SMELL). NOTED BY ALL CREW. DECLARED EMERGENCY AND LANDED I CT. ON EVAC, NOTED LIGHT BLUE SMOKE FROM PORT SIDE EQUIPMENT RACK. FIRE DEPT UNABLE TO PINPOINT SOURCE. AN FBO, INVES TIGATED BUT FOUND NOTHING. MAINTENANCE LOOKED EVERYTHING OVER AND FOUND NO EVIDENCE OF SMOKE. OPERATED ALL SYSTEMS AND EVERYTHING WAS OPERATING PROPERLY. 2 L 7 2 4T 4 T A24CE E4EA 2002081500077 20020815 00077 EU 2002 8 15 SIMA200219804 1 20020711 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 DURING MBV INSPECTION, MAINTENANCE FOUND THE CARGO BAY RT FRAME AT STA 658.5 DENTED. RECONTOURED DENT BACK TO NORMAL CO NTOUR. PERFORMED NDT INSPECTION AND FOUND NO DEFECT. FABRICATED AND INSTALLED A REPAIR DOUBLER. REPAIR DONE IAW REPAI R STATEMENT AND STANDARD SRM PRACTICES. 2 L 7 2 4T RT A52EU 2002081500078 20020815 00078 EU 2002 8 15 SIMA200219805 1 20020710 A 5311 ALCLAD2024T3 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 DURING MBV INSPECTION, MAINTENANCE FOUND THE CARGO BAY RT FRAME AT STATION 640, DENTED. RECONTOURED DENT BACK TO NORMAL CONTOUR PERFORMED NDT INSPECTION AND FOUND NO DEFECTS. FABRICATED AND INSTALLED A REPAIR DOUBLER. REPAIR DONE IAW SD S AND STANDARD SRM PRACTICES. 2 L 7 2 4T RT A52EU 2002081500079 20020815 00079 EU 2002 8 15 SIMA200219806 1 20020709 A 5311 ALCLAD2024T3 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 DURING MBV INSPECTION MAINTENANCE FOUND FRAME 258 IN GALLEY AREA HAS CORROSION (FROM PREVIOUS REPAIR). REMOVED PREVIOUS REPAIR AND ADDITIONAL CORROSION BY CUT OUT. MAINTENANCE FABRICATED AND INSTALLED A DOUBLER. REPAIR DONE IAW SRM. 2 L 7 2 4T RT A52EU 2002081500080 20020815 00080 EU 2002 8 15 SIMA200219807 1 20020709 A 5410 ALCLAD2024T3 FRAME SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 DURING MBV INSPECTION MAINTENANCE FOUND LT NACELLE INBOARD FILLET AREA, CHAFED. BLENDED CHAFED AREA. PERFORMED NDT INS PECTION AND FOUND NO DEFECTS. MAINTENANCE FABRICATED AND INSTALLED AN REPAIR DOUBLER REPAIR DONE IAW SRM. 2 L 7 2 4T RT A52EU 2002081500081 20020815 00081 EU 2002 8 15 SIMA200220001 1 20020716 A 5414 CRES301ANNL SKIN SAAB SF340 340B 7860101 EU RT NACELLE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 FOUND RT NACELLE INBOARD FORWARD SKIN HAS THREE RIVETS RECESSED THROUGH SKIN. PERFORMED CUT TO INNER SKIN TO GAIN ACCES S TO DAMAGED AREA. FABRICATED AN INNER SKIN SPLICE DOUBLER. REPAIR DONE IAW SRM PRACTICES. 2 L 7 2 4T RT A52EU 2002081500082 20020815 00082 EU 2002 8 15 SIMA200220004 1 20020719 A 3350 6013211 BATTERY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 266AE 340B266 EMERGENCY FLOOR LIGHTS, INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY SUPPLY IAW MM. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002081500083 20020815 00083 EU 2002 8 15 SIMA200220303 1 20020722 A 2120 SMOKE SAAB SF340 340B 7860101 EU CABIN DETECTED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 340RC 340B340 FLIGHT ATTENDENT REPORTED SMOKE IN CABIN AT ROW 11 WITH FAINT BURNED SMELL IN CABIN CREW ELECTED TO RETURN. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. NO SOURCE OF SMOKE WAS FOUND. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2002081500084 20020815 00084 EU 2002 8 15 SIMA200220501 1 20020717 A 5414 ALCLAD2024T3 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 FOUND RT NACELLE OUTBOARD FORWARD SKIN HAS POSSIBLE CRACK AT RIVET. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND I NDICATION OF A CRACK. PERFORMED CUT TO INNER SKIN TO GAIN ACCESS TO DAMAGE AREA. REMOVED DAMAGED SKIN BY CUTOUT AND PE RFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO ADDITIONAL REJECTABLE INDICATIONS. FABRICATED AN EXTERNAL DOUBLER AN D INNER SPLICE DOUBLER. REPAIR DONE IAW SRM. 2 L 7 2 4T RT A52EU 2002081500085 20020815 00085 SO 2002 8 15 C2XA02CL160 1 20020807 A 3230 355022002 CONTROL UNIT EMB 145 EMB145ER 3260211 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15941 3949 3533 145035 CLE - FLIGHT 3218, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT DURING CLIMB. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WER E GOOD. THE AIRCRAFT WAS TEST FLOWN AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002081500086 20020815 00086 SO 2002 8 15 SIMA200220504 1 20020720 A 5310 14525480003 BEAM EMB 145 EMB145LR 3260212 SO DOOR FRAME CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 FOUND CARGO DOOR CUTOUT LOWER SILL BEAM CORRODED. REMOVED CORRODED SILL (BEAM). INSTALLED NEW BEAM IAW SRM. (B8349) 2 L 7 2 4T RT T00011AT 2002081500087 20020815 00087 SO 2002 8 15 SIMA200220505 1 20020717 A 5311 ALCLAD2024T3 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 FOUND FRAME 72 DENTED AT STRINGERS 14 RT AND 16 RT IN CARGO COMPARTMENT. RECONTOURED DENT. FABRICATED A REPAIR DOUBLER . REPAIR DONE IAW SRM. (B8349) 2 L 7 2 4T RT T00011AT 2002081500088 20020815 00088 SO 2002 8 15 SIMA200220506 1 20020717 A 5311 14522371003 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 FOUND FRAME 72 DENTED AT STRINGERS 14 LT AND 15 LT IN CARGO COMPARTMENT. RECONTOURED DENT. FABRICATED A REPAIR DOUBLER USING CHANNEL FRAME. REPAIR DONE IAW SRM. (B8349) 2 L 7 2 4T RT T00011AT 2002081500089 20020815 00089 SO 2002 8 15 SIMA200220507 1 20020720 A 5320 ALCLAD2024T3 CHANNEL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 FOUND CORROSION ON RT HAT CHANNEL AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED A CHANNEL REPAIR DOUBLER AND F ILLER. REPAIR DONE IAW SRM. 2 L 7 2 4T RT T00011AT 2002081500090 20020815 00090 SO 2002 8 15 SIMA200220508 1 20020717 A 5311 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 FOUND FRAME 71 DENTED AT STRINGER 16R IN CARGO COMPARTMENT. RECONTOURED DENT. FABRICATED A REPAIR DOUBLER. REPAIR DON E IAW SRM. (B8349) 2 L 7 2 4T RT T00011AT 2002081500091 20020815 00091 SO 2002 8 15 SIMA200220509 1 20020721 A 5311 ALCLAD2024T3 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 FOUND NUMEROUS UNDOCUMENTED BLENDED AREAS ON FORWARD DIGITAL. REMOVED BLENDED AREAS BY CUT OUT. FABRICATED A REPLACEME NT STRAP ALSO FABRICATED TWO DOUBLERS AND SHIMS. REPAIR DONE IAW SRM. 2 L 7 2 4T RT T00011AT 2002081500092 20020815 00092 SO 2002 8 15 C2XA02CL161 1 20020805 A 7333 23052613 TRANSMITTER EMB 145 EMB145LR 3260212 SO NR 1 ENGINE INOPERATIVE A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 16951 3624 145063 CLE - FLIGHT 3171, THE CREW REPORTED THE NR 1 ENGINE FUEL FLOW INDICATION SHOWED 0 IN FLIGHT. THE ENGINE OPERATED NORM ALLY. MAINTENANCE REPLACED THE NR 1 ENGINE FUEL FLOW TRANSMITTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002081500093 20020815 00093 SO 2002 8 15 SIMA200220510 1 20020719 A 5315 2024T3 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 FOUND CORROSION ON GALLEY CENTER FLOORBEAM AT FRAME 20. REMOVED CORROSION BY CUTOUT. FABRICATED A REPAIR DOUBLER AND F ILLER. REPAIR DONE IAW SRM. 2 L 7 2 4T RT T00011AT 2002081500094 20020815 00094 SO 2002 8 15 SIMA200220511 1 20020722 A 5310 14525175001 SHEAR TIE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 FOUND FRAME 65 SHEAR TIE CORRODED. REMOVED CORROSION BY CUT OUT. FABRICATED A REPLACEMENT SPLICE. REPAIR DONE IAW SRM . 2 L 7 2 4T RT T00011AT 2002081500095 20020815 00095 SO 2002 8 15 SIMA200220512 1 20020713 A 5310 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 FOUND UNDOCUMENTED BLENDED AREAS ON LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20. REMOVED PREVIOUS REPAIR AND FABRICAT ED A DOUBLER, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW SRM. (B8349) 2 L 7 2 4T RT T00011AT 2002081500096 20020815 00096 SO 2002 8 15 C2XA02CL162 1 20020804 A 2530 CBC16707 RECEPTACLE EMB 135 EMB135LR 3260305 SO GALLEY BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 15527 145413 SLP - FLIGHT 4153, THE CREW REPORTED A STRONG SMELL OF BURNING RUBBER FROM THE NR 2 COFFEE JUG. THE AIRCRAFT WAS RELEA SED IAW 25-60-02/3D. MAINTENANCE REPLACED THE COFFEE POT RECEPTACLE IN THE GALLEY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002081500097 20020815 00097 SO 2002 8 15 SIMA200220513 1 20020712 A 5310 SILL EMB 145 EMB145LR 3260212 SO DOOR FRAME DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 145115 FOUND NUMEROUS UNDOCUMENTED BLENDED AREAS ON SERVICE DOOR CENTER SILL. FILLED BLENDED AREAS WITH EPOXY RESIN, SANDED AR EA SMOOTH. FABRICATED REPAIR DOUBLER. REPAIR DONE IAW SRM. 2 L 7 2 4T RT T00011AT 2002081500098 20020815 00098 EU 2002 8 15 SIMA200220514 1 20020717 A 5311 ALCLAD2024T3 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 352SB 340B352 NO DOCUMENTATION COULD BE FOUND FOR DOUBLER REPAIR ON LT AFT FUSELAGE, FORWARD OF CARGO DOOR. REMOVED PREVIOUS INSTALLE D REPAIR DOUBLER AND PERFORMED A CUT OUT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. 2 L 7 2 4T RT A52EU 2002081500099 20020815 00099 EU 2002 8 15 SIMA20215501 1 20020604 A 3350 601321 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 174AE 340B174 DURING PREFLIGHT THE FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHTS WOULD NOT STAY ON. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2002081500100 20020815 00100 2002 8 15 C2XA02CL164 4 20020809 A 2330 8211500513 ENTERTAIN SYS EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 27 22909 145459 CLE - FLIGHT 3248, THE CREW REPORTED A LAV SMOKE WARNING MESSAGE IN FLIGHT. A BURNING SMELL WHILE THE LIGHT WAS ON. R EPORTED THE SMELL COMING FROM THE CD PLAYER COMPARTMENT. MAINTENANCE INSPECTED AND REPLACED THE CD PLAYER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002081500101 20020815 00101 SO 2002 8 15 C2XA02CL166 1 20020810 A 3350 74441 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 28529 145512 DURING A SERVICE/ROUTINE CHECK, THE EMERGENCY EXIT LIGHT ABOVE THE SERVICE DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPL ACED THE EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002081500102 20020815 00102 NM 2002 8 15 QXEA0201211 1 20020813 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 867 502 PSC-EMERGENCY LIGHTS LEFT OUTSIDE AFT, #1 AND #3 AISLE OVERHEAD IS INOPERATIVE. REMOVED AND REPLACED PS 3 BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081500103 20020815 00103 SO 2002 8 15 C2XA02IA155 1 20020803 A 2750 3635001001 BRAKE EMB 145 EMB145LR 3260212 SO T/E FLAP FAILED A C2XA B EMER. DESCENT F FLT CONT AFFECTED AP APPROACH 1 SW 27 11565 145621 CREW REPORTED THAT ON DESCENT THE FLAPS WOULD NOT EXTEND. THE AIRCRAFT ACCOMPLISHED AN EMERGENCY DESCENT AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT FLAP TRANSMISSION BRAKE TO HAVE FAILED. THE AFFECTED FLAP BRAKE WAS R EMOVED AND REPLACED, THE SYSTEM OPERATIONALLY CHECKED, AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002081500104 20020815 00104 SO 2002 8 15 C2XA02IA157 1 20020804 A 4920 4501968D APU EMB 145 EMB145LR 3260212 SO APU BAY LEAKING A C2XA K NONE B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TX TAXI/GRND HDL 1 SW 27 13994 145291 EWR - WHEN STARTING THE APU THE CREW NOTED THAT A FUEL SMELL WAS PRESENT IN THE COCKPIT. MAINTENANCE REMOVED AND REPLA CED THE APU PERFORMED A OPERATIONAL CHECK AND A LEAK CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 L 7 2 4T RT T00011AT 2002081500105 20020815 00105 EU 2002 8 15 C2XA02IA158 1 20020805 A 3260 D22878000 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU RT MLG MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SW 27 14821 160 IAH- THE CREW NOTED THAT THE LANDING GEAR MASTER WARNING DISAGREE ILLUMINATED AND RETURNED TO IAH WITHOUT INCIDENT. MA INTENANCE REMOVED AND REPLACED THE RIGHT INBOARD WEIGHT ON WHEELS PROX SWITCH, PERFORMED A OPERATIONAL CHECK OF THE LAND ING GEAR SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002081500106 20020815 00106 SO 2002 8 15 C2XA02IA161 1 20020805 A 3260 WARNING SYSTEM EMB 145 EMB145ER 3260211 SO COCKPIT MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 17928 145007 IAH- AFTER TAKEOFF THE LEFT MAIN LANDING GEAR, LANDING GEAR DISAGREE MESSAGE APPEARED, THE CREW RETURNED THE AIRCRAFT T O IAH WITHOUT INCIDENT. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002081500107 20020815 00107 SO 2002 8 15 C2XA02IA162 1 20020805 A 3260 23092900401 UPLOCK EMB 145 EMB145ER 3260211 SO RT MLG FAULTY A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 17928 145007 IAH- DURING A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM THE MECHANIC NOTED THAT THE RIGHT HAND MLG WAS NOT SHOWING T HE CORRECT INDICATION UPON RETRACTION. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND MLG UPLOCK BOX, PERFORMED A OPER ATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002081500108 20020815 00108 SO 2002 8 15 C2XA02IA163 1 20020802 A 3350 74441 SIGN EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15973 145159 CLE- DURING POST FLIGHT INSPECTION THE CREW NOTED THAT THE EMERGENCY SIGN LIGHT AT SEAT 12A DID NOT ILLUMINATE. MAINTE NANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO D EFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002081500109 20020815 00109 EU 2002 8 15 C2XA02IA164 1 20020805 A 2131 CONTROLLER AEROSP ATR42 ATR42320 8680930 EU CABIN PRESSURE MALFUNCTIONED A C2XA B EMER. DESCENT O OTHER CR CRUISE 1 SW 27 14822 163 LRD- DURING FLIGHT 3929 THE CREW NOTED THAT EXCESS CABIN ALTITUDE IN CRUISE AT 18,000 FEET. DECLARED EMERGENCY AND DID AN EMERGENCY DESCENT TO 10,000 FEET AND LANDED AT LDR WITHOUT INCIDENT. CONTRACT MAINTENANCE PERFORMED A OPERATIONAL C HECK OF THE PRESSURIZATION SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002081500110 20020815 00110 SO 2002 8 15 C2XA02TY118 1 20020802 A 5311 14523509403 FRAME EMB 135 EMB135LR 3260305 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24517 145332 TYS DURING A SCHEDULED 1-C INSPECTION, A CHAFE MARK WAS FOUND ON FRAME 70 NEXT TO THE BLEED AIR DUCT. BLENDED OUT THE AREA, PERFORM A DYE INSPECTION, ALODINED AND PAINTED. NO DEFECTS WERE FOUND AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002081500111 20020815 00111 CE 2002 8 15 SO12002F00000 1 20020701 A 2821 173779601 FILTER LEAR 24 24B 5170306 CE GE CJ610 CJ6106 30006 NE LT & RT ENGINE FAILED B SO1R K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 19 233W 211 251150 FILTERS, LT AND RT ENGINE LOW FUEL PRESSURE LIGHT CAME ON DURING ENGINE POWER RUN. REPLACED LOW PRESSURE FUEL FILTERS A ND REMOVED CUSTOMER FURNISHED FILTER FROM MFG NOTIFIED CUSTOMER OF MALFUNCTION AND RECOMMENDED NOT TO USE FUEL FILTERS F ROM CERTAIN MFG. BOTH ENGINES OPS AND LEAK CHECKED GOOD ON ENGINE PERFORMANCE RUN. 2 L 7 2 4J 4 J A10CE 1E16 2002081500112 20020815 00112 WP 2002 8 15 T192002F00000 2 20020715 A 7532 HTE49029A SEAL BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE731* 01518 WP BLEED VALVE DEFECTIVE E T19A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 217AL 258177 AFTER TAKEOFF, DURING CLIMBOUT, REPORTED AFT EQUIPMENT BAY OVERHEAT LIGHT ON MASTER CAUTION WARNING PANEL ILLUMINATED. RETURNED TO PLACE OF ORIGIN. AFTER TROUBLESHOOTING FOUND DETERIORATED BLEED VALVE SEAL ON RT ENGINE BLEED AIR SHUTOFF VALVE IN AFT EQUIPMENT BAY. REPLACED DEFECTIVE SEAL WITH NEW SEAL. RAN BOTH ENGINES AT POWER AND PERFORMED OPERATIONAL AND LEAK CHECK. NO DISCREPANCIES NOTED. SUSPECT CAUSE OF DEFECTS SHRINKAGE OF SEAL OVER PERIOD OF TIME. RECOMMEND PE RIODIC BLEED AIR LEAK CHECKS AND TORQUE CHECKS OF BLEED AIR MARMON CLAMPS. 2 L 7 2 4F 4 F RT A3EU E6WE 2002082800084 20020828 00084 NM 2002 8 28 TSAA0233153 1 20020629 A 3350 9221009 BATTERY PACK BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D NE CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED FORWARD ENTRY DOOR IDENTIFIER POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002082800088 20020828 00088 NM 2002 8 28 TSAA0233158 1 20020617 A 3350 9221009 BATTERY PACK BOEING 737 737230 1384401 NM PWA JT8 JT8D NE CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED FORWARD SERVICE DOOR IDENT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002082800089 20020828 00089 NM 2002 8 28 TSAA0233159 1 20020617 A 3350 1000679 LIGHT BOEING 737 737230 1384401 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 36905 23155 REPLACED FORWARD SERVICE DOOR IDENT LIGHT ASSEMBLY DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002082800090 20020828 00090 NM 2002 8 28 TSAA0233160 1 20020629 A 3350 86210066 BATTERY PACK BOEING 737 737230 1384401 NM PWA JT8 JT8D NE CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED NR FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002090600229 20020906 00229 NM 2002 9 6 TSAA0253151 1 20020617 A 5330 6546529 SKIN BOEING 727 7272Q9 138448M NM PWA JT8 JT8D9 52048 NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 FOUND SKIN CRACK BELOW STRINGER 19 LAP JOINT AT BS 440. TRIMMED OUT DAMAGE AND VERIFIED USING HFEC. FABRICATED REPAIR DOUBLER, STRUCTURAL FILLER. REPAIR COMPLETED IAW WITH ECO 3288. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2002090600230 20020906 00230 NM 2002 9 6 TSAA0253152 1 20020617 A 5330 65C37526 SKIN BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 24031 FOUND CRACK ON FUSELAGE SKIN, STRINGER 21L AT BS 985.5. TRIMMED OUT DAMAGED AREA AND VERIFIED USING HFEC METHOD NO DEFE CTS NOTED. FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4U 4 F RT A16WE E2EA 2002081500113 20020815 00113 SO 2002 8 15 C2XA02TY119 1 20020802 A 5512 14521906003 SKIN EMB 135 EMB135LR 3260305 SO HORIZ STAB GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24517 145332 TYS - DURING A SCHEDULED 1-C INSPECTION, THE CENTER WING BOX OF THE HORIZONTAL STAB HAS SOME SCRATCHES AND GOUGES. MAI NTENANCE BLENDED DAMAGE, PERFORMED DYE-PENETRANT INSPECTION. WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002081500114 20020815 00114 CE 2002 8 15 UG82002F00004 1 20020626 A 8012 9914433 START VALVE CESSNA 750 750 2076810 CE RT ENGINE STUCK E UG8A O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 5115 2660 7500018 RT ENGINE START VALVE OPEN LIGHT REMAINED ILLUMINATED AFTER ENGINE START. START REGULATOR VALVE FOR RT ENGINE, FAILED. REPLACED AND OPERATIONALLY CHECKED RIGHT ENGINE START REGULATOR VALVE PER MFG MM. 2 L 7 2 4J RT T00007WI 2002081500115 20020815 00115 NM 2002 8 15 C8GA20020008 1 20020709 A 3260 WARNING SYSTEM BOEING 727 727227 1384078 NM COCKPIT MALFUNCTIONED A C8GA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 15 308AS 22002 FLT 713 FROM SAN TO DEN. ON APPROACH TO DEN, LEFT MAIN GEAR INDICATE UNSAFE BOTH INSTRUMENT PANEL AND SECONDARY. CYCLE D GEAR, NO LUCK. EXECUTED GO-AROUND THEN CYCLED GEAR AND GOT GOOD INDICATIONS AND LANDED WITHOUT INCIDENT. INSPECT THE MAIN GEAR ASSEMBLY AND FOUND NO DEFECTS, RE-RACKED THE LANDING GEAR MODULE AS PRECAUTIONARY, SYSTEM OPS CHECKED GOOD IA W MM 32-31. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2002081500116 20020815 00116 NE 2002 8 15 CNMA200200004 2 20020708 A 7200 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 MALFUNCTIONED A CNMA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 07 540AX 46595 455256 NR 2 ENGINE OR ACFT SHUTTERED, MADE A POP, THEN WENT QUIET. NR 2 ENGINE'S EGT WENT TO 945. REDUCED THROTTLE TO 740 N1 AND N2. CLIMBING TO 2100 FT EGT STABILIZED AROUND 915 - 925 AND OIL FILTER CLOG LIGHT CAME ON NR 2 ENGINE. SHUT DOWN N R 2 ENGINE. RETURNED TO AIRPORT. 2 L 7 3 4F 4 F A22WE E23EA 2002081500117 20020815 00117 CE 2002 8 15 UG82002F00005 1 20020719 A 2741 COMPUTER CESSNA 750 750 2076810 CE PITCH TRIM MALFUNCTIONED E UG8A O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 5114 7500017 PITCH FEEL FAIL LIGHT CAME ON, COULD NOT EXTINGUISH. SYSTEM LOCKUP. RESET PITCH FEEL SYSTEM, CLEARED EICAS FAIL MESSAG E. OPERATION RETURNED TO NORMAL. 2 L 7 2 4J RT T00007WI 2002081500118 20020815 00118 NM 2002 8 15 UIE2002000026 1 20020722 A 3340 8906K1563 SWITCH BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE LIGHT PANEL INTERMITTENT A UIEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 15 506MC 21252 ON DESCENT A STRONG ELECTRICAL ODOR COMING OUT OF GASPERS. ELECTRICAL SMOKE OR FIRE CHECK LIST INITIATED. AFTER NR 6, SMOKE STOPPED. AIRCRAFT IN THIS CONFIGURATION AND LANDED. FOUND MELTED INSULATION AT WING ILLUMINATION LIGHT SWITCH TE RMINAL. LIGHT INTERMITTENTLY INOPERATIVE. PULLED CIRCUIT BREAKER. REPLACED SWITCH AND WIRE ATTACHED TO TERMINAL NR 1 ON SWITCH FOR THE WING ILLUMINATION LIGHTS. 2 L 7 4 4F 4 F RT A20WE E23EA 2002081500119 20020815 00119 NM 2002 8 15 UIEA200200026 1 20020722 A 3397 8906K1563 SWITCH BOEING 747 7472D3B 1384805 NM LIGHT PANEL INOPERATIVE A UIEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 15 506MC 21252 ON DESCENT A STRONG ELECTRICAL ODOR COMING OUT OF GASPERS. ELECTRICAL SMOKE OR FIRE CHECK LIST INITIATED. AFTER ITEM N R 6, SMOKE STOPPED. AIRCRAFT REMAINED IN THIS CONFIGURATION AND LANDED. C/A: FOUND MELTED INSULATION AT WING ILLUMINAT ION LIGHT SWITCH TERMINAL. LIGHT INTERMITTENTLY INOPERATIVE, PULLED CIRCUIT BREAKER. TRANSFERRED TO DMI, MEL. REPLACE D SWITCH AND WIRE ATTACHED TO TERMINAL NR1 ON SWITCH FOR THE WING ILLUMINATION LIGHTS IAW MM. 2 L 7 4 4F RT A20WE 2002081500120 20020815 00120 EU 2002 8 15 USA2002F00058 1 20020625 A 2150 87292325V04 COMPUTER AIRBUS 320 A320211 3930320 EU E/E BAY FAILED A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 188US 621 1724 AFTER TAKEOFF, CAPTAIN DETECTED SMOKE IN THE COCKPIT ALONG WITH AN ECAM MESSAGE OF (AVNCS SMOKE). THE FLIGHT RETURNED T O AIRPORT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE AVIONICS EQUIPEMENT VENTILATION COMPUTER DUE TO A FAILED BITE CHECK. BITE CHECKED OK AFTER REPLACEMENT OF THE AVIONICS EQUIPEMENT VENTILATION COMPUTER. 2 L 7 2 4F RT A28NM 2002081500121 20020815 00121 NM 2002 8 15 F3LA200200196 1 20020715 A 2121 8012404 FAN BOEING 737 73736E 138443A NM E/E BAY INOPERATIVE A F3LA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 314FL 223 25256 FLIGHT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO DEN. REPLACED TURBOFAN, PERFORMED PRESSURIZAT ION SYSTEM OPERATIONAL TEST AND CHECKED OKAY. 2 L 7 2 4F RT A16WE 2002081500123 20020815 00123 2002 8 15 F3LA200200198 4 20020724 A 3460 1689L50701 FMC BOEING 737 7373L9 1384470 NM E/E BAY FAULTY A F3LA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 312FL 24569 AIR TURNBACK. ON CLIMBOUT, THE FLIGHT CREW REPORTED THE ONLY MODE CONTROL WAS N1. NO AUTO-PILOT, NO AUTO THROTTLE OR M ODE CONTROL. MAINTENANCE REMOVED AND REPLACED AIR DATA COMPUTER, FMCS AND OPERATIONS CHECK WAS NORMAL. 2 L 7 2 4F RT A16WE 2002081500126 20020815 00126 NM 2002 8 15 F3LA200200201 1 20020726 A 2613 OVERHEAT LOOP BOEING 737 7372Y5 1384554 NM CARGO BAY OUT OF POSITION A F3LA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 118RW 23040 DURING CLIMBOUT, THE FLIGHT CREW DISCOVERED A WIND/BODY OVERHEAT LIGHT ON. QRH ITEMS ACCOMPLISHED AND LIGHT EXTINGUISHE D. AIR TURNBACK ACCOMPLISHED. UPON INSPECTION BY MAINTENANCE, AFT CARGO PIT HAD TWO AREAS WHERE THE OVERHEAT DETECTOR WAS TOUCHING THE BLEED DUCT. MAINTENANCE CORRECTED THE PROBLEM AND THE SYSTEM CHECKED NORMAL. CORRECTIONS MADE IN ACCO RDANCE WITH MM 26-18-0, PAGE 501. 2 L 7 2 4U RT A16WE 2002081500127 20020815 00127 NM 2002 8 15 F3LA200200203 1 20020723 A 5330 SKIN BOEING 737 737317 138447P NM FUSELAGE CANNING A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION FOUND THE FUSELAGE SKIN AT BS 928, STR 21 LT, OIL CANNED (BUCKLED). MAINTENANCE REMOVED SE CTION OF SKIN, FABRICATED REPAIR DOUBLER AND TRIPLER. PARTS WERE INSTALLED IN ACCORDANCE WITH SRM 51-40-02 2 L 7 2 4F RT A16WE 2002081500128 20020815 00128 NM 2002 8 15 F3LA200200204 1 20020723 A 5320 CROSSBEAM BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION NOTED CABIN FLOOR EXPANSION JOINT CROSS MEMBERS CRACKED AT FASTENER STATION 540 RBL 44, UND ER THE FLOOR. MAINTENANCE REPAIRED THE EXPANSION IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-40-2 AND 51-10-2. 2 L 7 2 4F RT A16WE 2002081500129 20020815 00129 NM 2002 8 15 F3LA200200207 1 20020723 A 5330 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION FOUND A CRACK IN FUSELAGE SKIN AT STA 727E, STR 22 R. MAINTENANCE REMOVED THE DAMAGE, BLEN DED THE AREA. A DOUBLER WAS FABRICATED AND INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-00-01 FIGURE 201 AND SRM 53-60-01. 2 L 7 2 4F RT A16WE 2002081500130 20020815 00130 NM 2002 8 15 F3LA200200208 1 20020723 A 5330 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION NOTED A CRACK IN THE RIGHT HAND FUSELAGE SKIN AT STA 727E, BETWEEN STR 22 R AND 23 R. MAIN TENANCE REMOVED THE DAMAGE, FABRICATED A DOUBLER AND INSTALLED THE DOUBLER IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53 -00-01, FIGURE 201 AND SRM 53-60-01. 2 L 7 2 4F RT A16WE 2002081500131 20020815 00131 NM 2002 8 15 F3LA200200210 1 20020723 A 5330 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION NOTED A CRACK IN THE FUSELAGE SKIN AT STA 727E STR 21 R. MAINTENANCE REMOVED THE DAMAGE. A DOUBLER WAS FABRICATED AND INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-00-01 FIGURE 201 AND SRM 53-60-01. 2 L 7 2 4F RT A16WE 2002081500132 20020815 00132 NM 2002 8 15 F3LA200200213 1 20020723 A 5315 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION NOTED LIGHT SURFACE CORROSION IN FORWARD ENTRY AT STA 344. MAINTENANCE FOUND THE STA 344 F LOORBEAM TO BE OUT OF LIMITS IAW SRM 53-10-51. MAINTENANCE REMOVED AND REPLACED THE UPPER CHORD OF STA 344 FLOORBEAM, W L 208, RBL 17 THROUGH LBL 65, IAW SRM 53-10-51, 50-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002081500133 20020815 00133 NM 2002 8 15 F3LA200200214 1 20020723 A 5315 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION NOTED CORROSION ON STA 328 FLOORBEAM, NEAR PREVIOUS REPAIR NEAR L1 DOOR SILL. MAINTENANCE FOUND THE BEAM TO BE OUT OF LIMITS IN ACCORDANCE WITH SRM 53-10-51. MAINTENANCE REMOVED AND REPLACED THE UPPER CHORD OF STA 328 FLOORBEAM, WL 208, LBL 33 TO LBL 64 IAW SRM 53-10-51, 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002081500135 20020815 00135 SO 2002 8 15 LR7A02045 1 20020707 A 5320 386681 ANGLE LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION FOUND RBL 62 CHINE ANGLE CRACKED AT FS 588 TO 597, WL 144. REPLACED CHINE ANGLE IAW SRM SMP 583 51-70 AND DWG 386681. 2 H 7 4 4T A1SO 2002081500136 20020815 00136 SO 2002 8 15 LR7A02046 1 20020707 A 5320 386681 ANGLE LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION FOUND LBL 62 CHINE ANGLE CRACKED AT FS 573 TO 597, WL 144. REPLACED CHINE ANGLE IAW SRM SMP 583 51-70 AND DWG 386681. 2 H 7 4 4T A1SO 2002081500137 20020815 00137 NM 2002 8 15 QXEA0201213 1 20020809 A 2910 FLEX LINE DHAV DHC8 DHC8202 2809007 NM ZONE 700 LEAKING A QXEA K NONE K FLUID LOSS DE DESCENT 1 NM 09 357PH 504 SEA- AFTER GEAR EXTENSION, LOST NO.2 HYDRAULIC WITH ASSOCIATED CAUTION LIGHTS ILLUMINATED. ZERO HYDRAULIC FLUID AND ZERO HYDRUALIC PRESSURE WERE NOTED 5 MINUTES PRIOR TO ENGINE SHUTDOWN. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AND FOUND MAIN LANDING GEAR DOWNLOCK ACTUATOR HYDRAULIC LINE LEAKING. REMOVED AND REPLACED FLEX LINE. OPERATIONAL CHECKS GOOD. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091100073 20020911 00073 NM 2002 9 11 F3LA200200216 1 20020810 A 3397 WIRE BOEING 737 737301 1384611 NM CABIN BROKEN A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 578US 21 23257 INSPECTION REPORTED ROW 3 ABC SINGLE LAMP SEAT MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT 3 ABC PER MM 33-19-00, PERFORMED OPERATIONAL TEST AND CHECKED OKAY. 2 L 7 2 4F RT A16WE 2002081500138 20020815 00138 NM 2002 8 15 PCAA0208095 1 20020813 A 5315 85310380 FLOORBEAM DHAV DHC8 DHC8102 2809003 NM X97 CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 851EX 343 DURING ROUTINE MAINTENANCE VISIT NOSE WHEELWELL FLOOR BEAM P/N 85310380 (STATION X97) FOUND CRACKED AT AIRCRAFT CENTERLI NE. DAMAGED AREA CUT OUT, EDDY CURRENT INSPECTED, AND REPAIRED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-53-1336 . AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081600007 20020816 00007 2002 8 16 KBMA119521 4 20020801 A 2312 0641051130K4196A RADIO SNIAS 350 AS350BA 8680817 EU VHF SYSTEM INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 1188P 2347 RADIO IS TRANSMITTING BUT TOTALLY UNREADABLE BY PILOTS AND TOWER. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2002081600008 20020816 00008 EU 2002 8 16 KBMA119523 1 20020801 A 2150 0500847 MOTOR SNIAS 350 AS350BA 8680817 EU CONDENSOR INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 1188P 1840 2347 AIR CONDITIONER INOPERATIVE. REPLACED WITH SERVICEABLE CONDENSOR MOTOR. 1 G 7 1 3U NC H9EU 2002081600009 20020816 00009 EU 2002 8 16 KBMA119524 1 20020806 A 6420 350A33215001 SPIDER SNIAS 350 AS350BA 8680817 EU TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 2300 TAIL ROTOR SPIDER BALL END WORN. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2002081600010 20020816 00010 EU 2002 8 16 KBMA119525 1 20020807 A 2150 420800001 BLOWER SNIAS 350 AS350BA 8680817 EU A/C BLOWER INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 1188P 1254 2347 REAR AIR CONDITIONER BLOWER, INOPERATIVE. REPLACED WITH SERVICEABLE AIRCRAFT EVAPORATOR BLOWER. 1 G 7 1 3U NC H9EU 2002081600011 20020816 00011 EU 2002 8 16 KBMA119526 1 20020801 A 6730 AC67244 SERVO SNIAS 350 AS350BA 8680817 EU MAIN ROTOR LEAKING E KBMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 37SH 546 2300 MAIN ROTOR SERVO WAS LEAKING. REPLACED WITH OVERHAULED SERVO. 1 G 7 1 3U NC H9EU 2002081600012 20020816 00012 EU 2002 8 16 KBMA119527 1 20020731 A 2842 647510033 PROBE SNIAS 350 AS350BA 8680817 EU FUEL SYSTEM STICKING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 2273A 1384 2273 (FUEL PROBE) FUEL GAUGE INDICATOR STICKS INTERMITTENTLY. REPLACED WITH OVERHAULED UNIT. 1 G 7 1 3U NC H9EU 2002081600013 20020816 00013 EU 2002 8 16 KBMA119528 1 20020731 A 2150 050008 COMPRESSOR SNIAS 350 AS350B2 8680813 EU AIR CONDITIONER INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 977 3141 AIR CONDITIONER BLOWING HOT AIR. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U H9EU 2002081600014 20020816 00014 EU 2002 8 16 KMBA119522 1 20020801 A 2150 59008 COMPRESSOR SNIAS 350 AS350BA 8680817 EU AIR CONDITIONER INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 1188P 11659 2347 AIR CONDITIONER COMPRESSOR INOPERATIVE. REPLACED WITH NEW COMPRESSOR. 1 G 7 1 3U NC H9EU 2002081600015 20020816 00015 EU 2002 8 16 USA2002F00059 1 20020604 A 5610 WINDSHIELD AIRBUS A319 A319112 3930323 EU COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 758US 1348 DURING CRUISE FLIGHT, THE WINDSHIELD CRACKED IN A SPIDER WEB PATTERN. FLIGHT RETURNED TO FIELD IN PIT. MAINTENANCE ACT ION PENDING. 2 L 7 2 4F RT A28NM 2002081600016 20020816 00016 NE 2002 8 16 USA2002F00063 2 20020421 A 7250 1499M62G09 SHROUD BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE HP TURBINE BURNED A USAA A UNSCHED LANDING B M J SMOKE/FUMES/ODORS/SPARKS OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 511AU 23594 724694 AFTER TAKEOFF, CREW NOTED AN OVERTEMP CONDITION ON THE RIGHT ENGINE. THE TOWER INFORMED THE CREW THAT BLACK SMOKE WAS P OURING FROM THE ENGINE. THE CREW REDUCED POWER ON THE RIGHT ENGINE. THE FLIGHT RETURNED TO FIELD AND LANDED WITH NO FU RTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REPORTED METAL IN THE TAILPIPE. THE ENGINE WAS REMOVED AND REP LACED. OPERATIONAL CHECK AND LEAK CHECK GOOD. TEARDOWN OF THE ENGINE REVEALED TEN HIGH PRESSURE TURBINE SHROUDS BURNED . ONE OF THESE SHROUDS DROPPED INTO THE GAS PATH CAUSING SOME SECONDARY DAMAGE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002081600017 20020816 00017 2002 8 16 USA2002F00064 4 20020601 A 2565 D31041146 SLIDE BOEING 757 757225 1384959 NM L3 DOOR TORN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 27454 22199 DURING A SLIDE INFLATION OPERATIONAL CHECK ON THE LEFT 3 DOOR, THE SLIDE TORE IN THE THRESHOLD AREA. THE TEAR EMINATED FROM THE CENTER OFT HE MATERIAL AND PROGRESSED OUT TOWARD THE EDGES. THE EDGES OF THE SLIDE REMAINED INTACT. THE SLIDE INFLATED PROPERLY AND REMAINED ATTACHED TO THE AIRCRAFT. EVALUATION PENDING. 2 L 7 2 4F RT A2NM 2002081600018 20020816 00018 NM 2002 8 16 USA2002F00066 1 20020417 A 4980 9769871 TAILPIPE BOEING 737 7374B7 1384702 NM APU LOOSE A USAA F ACTIVATE FIRE EXT. J WARNING INDICATION TX TAXI/GRND HDL 1 EA 19 440US 24811 APU WAS STARTED ON FINAL AND UPON TOUCHDOWN, CREW RECEIVED AN APU FIRE WARNING BELL AND INDICATION LIGHT. AS AIRCRAFT C LEARED THE RUNWAY, CREW PULLED AND ROTATED THE APU FIRE HANDLE, DISCHARGING THE BOTTLE. FIRE LIGHT EXTINGUISHED AS CREW SWITCHED THE APU OFF. CREW ASKED TOWER IF THEY OBSERVED AND SMOKE. TOWER RESPONDED NO SMOKE WAS NOTED. FLIGHT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE APU TAILPIPE LOOSE AND SEAL DE TERIORATED ON LOWER SHROUD EXHAUST OPENING. REMOVED AND REPLACED APU ASSEMBLY AND SEAL, ALSO, APU FIRE EXTINGUISHER AND YELLOW INDICATOR DISCHARGE DISC. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2002081600019 20020816 00019 CE 2002 8 16 WC72002F00002 1 20020715 A 2750 BEARING CESSNA 650 650 2076802 CE TE FLAPS SEIZED B WC7R O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 25 398CW 6500098 THE FLAPS WERE STUCK AT 20 DEGREES. ANY ATTEMPT TO RAISE OR LOWER THEM CAUSED THE 40 AMP FUSE TO BLOW. SUBSEQUENT INVE STIGATION REVEALED THAT THE FLAP MOTOR HAD A SEIZED BEARING AT THE TELEFLEX DRIVE ON ONE END. IT WAS NOTED THAT A FUSEL AGE DRAIN WAS LOCATED ABOVE THE MOTOR AND FOILET WATER HAD BEEN LEAKING ONTO THE MOTOR AND WAS ALLOWED TO ENTER THE BEAR ING CAUSING SEVERE CORROSION. 2 L 7 2 4F A9NM 2002081600020 20020816 00020 CE 2002 8 16 WIB2002F00004 1 20020626 A 2150 66082484 MOTOR LEAR 35 31A 5170531 CE GARRTT TFE731 TFE731* 01518 WP AIR CONDITIONER FAILED B WIBR K NONE O OTHER IN INSP/MAINT 1 SW 11 77PY 089 AIR CONDITIONER COMPRESSOR DRIVE MOTOR FAILED. FOUND TO BE INTERNALLY BURNED UP. CURRENT LIMITER DID NOT BLOW. POSSIB LY CAUSED BY BEARING FAILURE. 2 L 7 2 4F 4 F RT A10CE E6WE 2002081600021 20020816 00021 CE 2002 8 16 WIB2002F00005 1 20020531 A 5340 262501569570 BRACKET LEAR 35 31 5170530 CE GARRTT TFE731 TFE731* 01518 WP FUSELAGE CRACKED B WIBR K NONE O OTHER IN INSP/MAINT 1 SW 11 90WA 028 NOSE ROLLER ATTACH BRACKETS INBOARD AND OUTBOARD ON LEFT AND RIGHT FLAPS CRACKED. 2 L 7 2 4F 4 F RT A10CE E6WE 2002081600022 20020816 00022 CE 2002 8 16 WIB2002F00006 1 20020801 A 2742 31355402 ACTUATOR LEAR 35 31 5170530 CE HORIZONTAL STAB FAILED B WIBR O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SW 11 90WA 028 STAB ACTUATOR BAD FROM STOCK. DAMAGED ANOTHER COMPONENT. NOT THE FIRST TIME. PITCH TRIM WOULD FAIL IN PRIMARY MODE AF TER OVERHAULED UNIT WAS INSTALLED. 2 L 7 2 4F RT A10CE 2002081600023 20020816 00023 CE 2002 8 16 WIB2002F00007 1 20020807 A 2730 BELLCRANK LEAR 35 31 5170530 CE GARRTT TFE731 TFE731* 01518 WP ELEVATOR CRACKED B WIBR K NONE O OTHER IN INSP/MAINT 1 SW 11 19LT 019 THE ELEVATOR BELLCRANK WAS CRACKED WHERE THE THRU BOLTS CONNECT IT TO THE TORQUE TUBE ON THE ELEVATOR. THE BELLCRANK IS A CAST PIECE. 2 L 7 2 4F 4 F RT A10CE E6WE 2002081600024 20020816 00024 CE 2002 8 16 WVE2002F00016 1 20020724 A 3230 60411050037 BEARING LEAR 60 60LEAR 5170707 CE LT & RT MLG CORRODED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 223FX 124 DURING 3000 LANDING INSPECTION, CORROSION WAS DISCOVERED ON THE LEFT AND RIGHT MAIN LANDING GEAR LOWER BEARINGS. PROBAB LE CAUSE: MOISTURE INTRUSION. RECOMMENDATION: REQUEST ENGINEERING ASSISTANCE TO DEVELOP A PROCEDURE FOR SEALING THE L OWER STRUT AREA. 2 L 7 2 4F RT A10CE 2002081600025 20020816 00025 CE 2002 8 16 WVG2002F00000 1 20020722 A 5311 5410557 FRAME LEAR 60 60LEAR 5170707 CE FUSELAGE CORRODED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 223FX 3813 124 DURING 3000 LANDING INSPECTION, LIGHT CORROSION WAS DISCOVERED ON THE FORWARD AND AFT PASSENGER/CREW DOOR FUSELAGE FRAME S WHEN REMOVING THE DOOR TENSION PLATES (TWO FORWARD & THREE AFT) FOR NDT. 2 L 7 2 4F RT A10CE 2002081600026 20020816 00026 CE 2002 8 16 XO72002F00000 1 20020711 A 2910 MS287784 O-RING CESSNA 650 650 2076802 CE ACTUATOR FILTER NICKED B I97R A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CE 07 660AA 388 6500059 PERFORMED EMER LANDING DUE TO LOSING NORMAL HYD PRESSURE AND QUANTITY. AC WAS 1100 LBS OVER MAX LANDING WEIGHT WHEN EME R LANDING WAS PERFORMED. LEFT LOW FUEL PRESSURE LIGHT ILLUMINATED BRIEFLY BEFORE LOST HYD PRESSURE. REMOVED INSP PANE LS FROM AC BELLY AND FOUND THAT HYD FLUID WAS LEAKING OUT OF WEEP HOLE ABOVE ACCESSED AREA. ACCESSED AILERON BELLCRANK AREA BY REMOVING AFT CABIN FLOORBOARD. FOUND AREA FULL OF HYD FLUID. PRESSURIZED HYD SYST AND FOUND FLUID LEAKING FROM AILERON BOOST ACTUATOR FILTER O-RING. REMOVED O-RING AND FOUND O-RING WAS NICKED. REPLACED WITH NEW O-RING. OPS AND LEAK CHECKED GOOD. PERFORM ENG RUN. MAINT TEST FLIGHT. ALL SYS CHECKED GOOD. 2 L 7 2 4F A9NM 2002081600027 20020816 00027 NM 2002 8 16 UPS02438884 1 20020725 A 5315 FLOORBEAM BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, CRACK FOUND AT 1 FASTENER HOLE AT BS 340 LT SIDE UPPER DECK FLOORBEAM UPPER CHORD AREA (VERTICAL FLA NGE). CHORD REPAIRED AS PER RS R-53-25-34834 & UPS REPAIR/ALTERATION AUTHORIZATION 747-53-20085. 2 L 7 4 4F A20WE 2002081600028 20020816 00028 NM 2002 8 16 UPS02438891 1 20020724 A 3350 MODULE BOEING 747 747121 1384871 NM CABIN MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: PFLT, EMERGENCY LIGHTS SYSTEM UNARMED LIGHT WILL NOT TEST USING OVERHEAD IND LIGHTS TEST SWITCH. NOTE : LIGHT WILL ILLUMINATE WITH EMERGENCY LIGHTS SWITCH IN ON POSITION. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL MODU LE PER 33-51-09, OPS CKS NORMAL AND UNARMED LIGHT ILLUMINATED WITH TEST SWITCH WHEN ON SELECTED. 2 L 7 4 4F A20WE 2002081600029 20020816 00029 NM 2002 8 16 UPS02438894 1 20020702 A 5310 PRESSURE PANEL BOEING 747 747123F NM WHEEL WELL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RT BLG W/W AT BS 1416 RBL 6 - 9 TOP CEILING / CHORD MATING SURFACE CORRODED AS RED MARKED. CORROSI ON BLEND OUT 0.050 X 1 X 2 INCH EXCEED SRM LIMIT. PRESSURE DECK WEB REPAIRED AS PER SRM 53-10-07 FIG 15. 2 L 7 4 4F A20WE 2002081600030 20020816 00030 NM 2002 8 16 UPS02438895 1 20020702 A 5310 PRESSURE PANEL BOEING 747 747123F NM WHEEL WELL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RT BLG W/W AT BS 1410, RBL 0 - 3 TOP CEILING / CHORD MATING SURFACE CORROSION FOUND AS RED MARKED. CORROSION BLEND OUT 0.016 X .5 X 1 INCH EXCEED SRM LIMIT. PRESSURE WEB REPAIRED AT RT BLG W/W BS 1402 - 1422 BL 0 TO RB L 33 AS PER SRM 53-10-07 FIG 15. (REFER HAECO NON ROUTINE CARD NR 7522). 2 L 7 4 4F A20WE 2002081600031 20020816 00031 NM 2002 8 16 UPS02438898 1 20020728 A 3350 LIGHT BOEING 747 747256B 1384865 NM COURIER BAY INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 528UP 24071 COURIER COMPT MOST AFT EMERGENCY LIGHTS INOP. RELAMPED COURIER COMPT AFT EMERGENCY LIGHTS OPS NORMAL. 2 L 7 4 4F RT A20WE 2002081600032 20020816 00032 NM 2002 8 16 UPS02438914 1 20020704 A 5230 SKIN BOEING 747 747123F NM CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, DURING THE REPAIR ASSESSMENT PROGRAM INSPECTION - BS 560 - 566 STR 38R - 39R EXISTING REPAIR DOUBLER THICKNESS AT FWD CARGO DOOR FWD LOWER CORNER AREA OUT OF SRM REPAIR LIMITS. FWD CARGO DOOR FWD LOWER CORNER AREA REPAI RED AS PER SRM 52-00-03 FIG 4 REFER RAP - SEQUENCE 42 - 17 FOR DETAIL INSTRUCTION. 2 L 7 4 4F A20WE 2002081600033 20020816 00033 NM 2002 8 16 UPS02438916 1 20020701 A 5330 SKIN BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C M/D - R3 DOOR LWR HINGE CUTOUT SKIN CRACKED. SKIN REPAIRED AS PER SRM 52-10-02 FIG 11. 2 L 7 4 4F A20WE 2002081600034 20020816 00034 NM 2002 8 16 UPS02438918 1 20020702 A 5330 SKIN BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C LT BS 1480 BULKHEAD AREA, HOLE NR 11 CRACK FOUND AT SKIN RUNNING FWD AND AFT, CRACK THROUGH THICKNESS , PLS REFER ATT FIG. SKIN REPAIRED AS PER SB 53A2390 FIG 28 STEP 13 - 17. 2 L 7 4 4F A20WE 2002081600035 20020816 00035 NM 2002 8 16 UPS02438921 1 20020703 A 5310 PRESSURE PANEL BOEING 747 747123F NM WHEEL WELL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C RT WLG W/W PRESSURE DECK LWR BONDED SKIN CORRODED AT BS 1375 O/B AREA AS MARKED. CORROSION BLEND OUT 0.050 X 1 X 2 INCH EXCEED SRM LIMIT. BS 1315 TO 1380 RBL 94 TO RBL 128 PRESSURE DECK WEB REPAIRED AS PER SRM 53-10-07 FIG 2. 2 L 7 4 4F A20WE 2002081600036 20020816 00036 NM 2002 8 16 UPS02438923 1 20020707 A 5312 BULKHEAD BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C M/D - BS 1241 LBL 40 CANTED BULKHEAD FOUND CORRODED CRACKED, DUE SEALANT REMOVED FOUND. M/D - BS 124 1 CANTED BULKHEAD REPAIRED FROM BL 0 - LBL 45 AS PER RS R53-48-34842 AND REFER NRC 7643 FOR WORK DETAIL. 2 L 7 4 4F A20WE 2002081600037 20020816 00037 NM 2002 8 16 UPS02438924 1 20020704 A 5330 SKIN BOEING 747 747123F NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C DURING THE REPAIR ASSESSMENT PROGRAM INSPECTION - BS 960 - 980 STR 3L - 4L EXISTING REPAIR DOUBLER TH ICKNESS AT THAT AREA OUT OF SRM REPAIR LIMIT. BS 960 - 980 STR 3L - 4L NEW REPAIR DOUBLER REPLACED AS PER SRM 51-30-02 AND 53-30-03 FIG 1. 2 L 7 4 4F A20WE 2002081600038 20020816 00038 NM 2002 8 16 UPS02438925 1 20020707 A 5312 BULKHEAD BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, M/D - BS 1241 LBL 30 CANTED BULKHEAD FOUND CORRODED CRACKED DUE SEALANT REMOVED FOUND. M/D BS 1241 CANTED BULKHEAD REPAIRED FROM BL 0 - LBL 45 AS PER RS R53-48-34842 AND REF NRC 7643 FOR WORK DETAIL. 2 L 7 4 4F A20WE 2002081600039 20020816 00039 NM 2002 8 16 UPS02438926 1 20020703 A 5310 PRESSURE PANEL BOEING 747 747123F NM WHEEL WELL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RIGHT WLG W/W PRESSURE DECK O/B AFT CORNER ABOVE BRAKE METERING V/V AREA CORRODED AS MARKED. CORROS ION BLEND OUT 0.030 X 1 X 2 INCH EXCEED SRM LIMIT. BS 1315 TO 1380 RBL 98 TO RBL 128 PRESSURE DECK WEB REPAIRED AS PER 53-10-07 FIG 2 REFER NRC 7774. 2 L 7 4 4F A20WE 2002081600040 20020816 00040 NM 2002 8 16 UPS02438927 1 20020701 A 5320 65B1525679 ANGLE BOEING 747 747123F NM LT MLG DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, LEFT BLG W/W - O/B STRUT DOOR ATTACHMENT FAIRING ANGLES INNER FACE SURFACE CORRODED AT FS 1438 TO 14 80 LBL 120. CORROSION BLEND OUT 0.050 X 1 X 2 INCH EXCEED SRM LIMIT. FAIRING CHORD REPLACED IAW SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002081600041 20020816 00041 NM 2002 8 16 UPS02438928 1 20020801 A 2433 241804 TRU BOEING 747 747200 1384847 NM E/E BAY BURNED A IPXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 522UP 21936 MOMENTARY HEAVY SMOKE FROM BEHIND S/O PANEL. T/R-2 C/B POPPED, SMOKE RAPIDLY DISSIPATED. SMOKE WAS NOT OBSERVED COMING FROM TRU. REMOVED AND REPLACED NR 2 TRU IAW MM 24-32-01. ALL INDICATIONS NORMAL. OK FOR SERVICE. 2 L 7 4 4F RT A20WE 2002081600042 20020816 00042 NM 2002 8 16 UPS02438929 1 20020628 A 5740 65B172236 FITTING BOEING 747 747123F NM CENTER WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, CRACK REVEALED AT RT OF BS 1241 REAR SPAR TO WING CENTER SECTION SPLICE FITTING SIGNAL INDICATION GR EATER THAN 50 PERCENT FSH. RIGHT BS 1241 WING REAR SPAR TO WING CENTER SECTION SPLICE FITTING REPLACED AS PER UPS EO B7 47-5740-4366-F APPENDIX A, C, D, F, H AND I. 2 L 7 4 4F A20WE 2002081600043 20020816 00043 NM 2002 8 16 UPS02438931 1 20020717 A 5740 FITTING BOEING 747 747123F NM CENTER WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RIGHT BS 1241 WING REAR SPAR UPPER SPLICE FITTING NR 8 HOLE CRACK FOUND APPROX 0.030 INCH, RUNNING I/ B AND NR 3 HOLE CRACK FOUND AT FWD AND AFT DIRECTION. RIGHT BS 1241 WING REAR SPAR TO WING CENTER SECTION SPLICE FITTIN G REPLACED AS PER UPS EO B747-5740-4366-F APPENDIX A, C, D, F, H AND I. 2 L 7 4 4F A20WE 2002081600044 20020816 00044 NM 2002 8 16 UPS02438932 1 20020704 A 5310 PRESSURE PANEL BOEING 747 747123F NM LT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, LEFT BLG W/W - CEILING PRESSURE DECK CORRODED AT LBL 55, FS 1350 - 1370. LEFT BLG W/W CEILING PRESS URE DECK WEB REPAIRED AT BS 1335 - 1375 LBL 55 - 80 REFER NRC 7975. CORROSION BLEND OUT 0.060 X 1 X 2 INCH EXCEED SRM L IMIT. 2 L 7 4 4F A20WE 2002081600045 20020816 00045 NM 2002 8 16 UPS02438934 1 20020717 A 5230 FITTING BOEING 747 747123F NM ROTARY ACTUATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, FWD ROTARY ACTUATOR SUPPORT FITTING FOUND CRACK AT HOLE NR 8 (LOOKING FWD) APPROX 0.030 INCH LONG AS MARKED. CRACKED HOLE OVERSIZED TO 0.688 INCH AND CRACK / CORROSION FREE. BUSHING FABRICATED AND INSTALLED AS PER RS R 53-65-34855 WITH ENGINEERING FILE NUMBER : 747-53-20096. 2 L 7 4 4F A20WE 2002081600046 20020816 00046 NM 2002 8 16 UPS02438935 1 20020717 A 5230 FITTING BOEING 747 747123F NM ROTARY ACTUATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C FWD ROTARY ACTUATOR SUPPORT FITTING FOUND CRACK AT HOLES NR 6 (LOOKING FW) APPROX 0.030 INCH LONG AS MARKED. CRACKED HOLE OVERSIZED TO 0.541 INCH AND CRACK / CORROSION FREE. BUSHING FABRICATED AND INSTALLED AS PER RS R5 3-65-34855 WITH ENGINEERING FILE NUMBER : 747-53-20096. 2 L 7 4 4F A20WE 2002081600047 20020816 00047 NM 2002 8 16 UPS02438936 1 20020628 A 5310 STRAP BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, CRACK FOUND AT BS 800 RT SIDE ABOVE S17R FWD FASTENER HOLE, THE CRACK FOUND 1 INCH LONG AT THE STRAP . BS 800 RT SIDE ABOVE STR 17R THE STRAP REPAIRED AS PER HX RS R53-22-34839 AND REFER NRC 5908 FOR WORK DETAIL. (UPS E O B747-5310-17165-A). 2 L 7 4 4F A20WE 2002081600048 20020816 00048 NM 2002 8 16 UPS02438937 1 20020628 A 5310 STRAP BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, CRACK FOUND AT BS 800 RT SIDE ABOVE S16R AFT FASTENER HOLE CRACK FOUND AT STRAP .125 INCH AT FWD AND .0625 INCH RUNNING AFTWARD. BS 800 RT BETWEEN STR 15 TO STR 17 AREA STRAP REPAIRED AS PER RS R-53-22-34839 (UPS EO B74 7-5310-17165-A). 2 L 7 4 4F A20WE 2002081600049 20020816 00049 NM 2002 8 16 UPS02438944 1 20020628 A 5310 REVEAL BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C M/D - R5 DR FWD CUTOUT REVEAL CRACKED. REVEAL REPAIRED AT BS 2231 S25R AREA AS PER RS R-53-61-34845, (UPS EO B747-5310-17209-A, APPENDIX A) REFER HAECO NRC 6215 FOR DETAIL. 2 L 7 4 4F A20WE 2002081600050 20020816 00050 NM 2002 8 16 UPS02438945 1 20020628 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, CRACK REVEALED AT BS 800 LT SIDE S16L FWD FASTENER HOLE, CRACK FOUND THRU THICKNESS AT FRAME BS 800 LT S16L FRAME REPAIRED AS PER RS R-53-22-34840. (UPS EO 13747-5310-17235-A & EO B747-5310-17198-A). 2 L 7 4 4F A20WE 2002081600051 20020816 00051 NM 2002 8 16 UPS02438948 1 20020703 A 5310 PRESSURE PANEL BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RT WLG PX DECK AT O/B BS 1340 AREA HEAVY CORROSION FOUND AS MARKED. CORROSION BLEND OUT 0.060 INCH X 1 INCH X 1 INCH EXCEED SRM LIMIT, BS 1315 - 1380 RBL 94 - 128. PRESSURE DECK WEB REPAIRED AS PER SRM 53-10-07 FIG 2. UPS MPI 15830 RAISED FOR EXTERNAL INSPECTION AS PER SRM 53-10-07 PG 5. 2 L 7 4 4F A20WE 2002081600052 20020816 00052 NM 2002 8 16 UPS02438950 1 20020702 A 5313 LONGERON BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RT BLG W/W AT BS 1416 RBL 110 ON TOP OF OVERWING LONGERON VERTICAL SUPPORT FRAME MATING SURFACE CORR OSION FOUND AS RED MARKED AND ON TOP OF THIS DEFECT THE CROSS-OVER STRINGER CORROSION FOUND AS RED MARKED. CORROSION BL END OUT DEPTH THROUGH THICK, WIDTH .25 INCH, LENGHT 2.125 INCH EXCEED SRM LIMIT. BS 1350 - 1480 RT OVERWING LONGERON RE PAIRED IAW RS R-53-43-34843, (UPS EO B747-5310-17206-A). 2 L 7 4 4F A20WE 2002081600053 20020816 00053 NM 2002 8 16 UPS02438952 1 20020701 A 5313 LONGERON BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, LT BLG W/W - OVERWING LONGERON AT W/W CORRODED AT MULTI SPOTS FROM FS 1360 - 1470 LBL 123 - 109. CO RROSION BLEND OUT DEPTH THROUGH THICK, WIDTH .25 INCH, LENGTH 3.625 INCH EXCEED SRM LIMIT. BS 1350 - 1480 RT OVERWING L ONGERON REPAIRED IAW RS R-53-43-34843 (UPS EO B747-5310-17206-A). 2 L 7 4 4F A20WE 2002081600054 20020816 00054 NM 2002 8 16 UPS02438953 1 20020705 A 5313 LONGERON BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT BLG W/W AT BS 1438 RBL 110 ON TOP OF OVERWING LONGERON AND VERT SUPPORT FRAME CORROSION REVEALED. CORROSION BLEND OUT 0.168 INCH X .5 INCH X 2.5 INCH EXCEED SRM LIMIT. BS 1350 - 1480 RT OVERWING LONGERON REPAIRED IAW RS R-53-43-34843, (UPS EO B747-5310-17206-A). 2 L 7 4 4F A20WE 2002081600055 20020816 00055 NM 2002 8 16 UPS02438955 1 20020715 A 5730 SKIN BOEING 747 747123F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C RIGHT WING - FRONT SPAR LOWER CHORD FOUND CORROSION AT WS 1100 - 1110 AFTER LOWER PANEL, REMOVED JUST AT NR 4 PYLON AREA. CORROSION BLEND OUT 0.104 INCH X 2 INCH X 4 INCH EXCEED SRM LIMIT. WING LOWER SKIN REPAIRED AS PE R HX RS R-57-26-34853 (UPS RA ENGINEERING FILE NUMBER 747-57-20030). 2 L 7 4 4F A20WE 2002081600056 20020816 00056 NM 2002 8 16 UPS02438957 1 20020702 A 5310 PRESSURE PANEL BOEING 747 747123F NM MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, LT WLG W/W - FS 1241 CANTED BULKHEAD CORROSION FOUND AT LBL 21 - 23. CORROSION BLEND OUT 0.050 INCH X 1 INCH X 2 INCH EXCEED SRM LIMIT. BS 1241 - 1265 BL 0 TO LBL 45 CANTED BULKHEAD WEB REPAIRED IAW RS R-53-48-34842 (U PS RA ENGINEERING FILE NUMBER: 747-53-20092). 2 L 7 4 4F A20WE 2002081600057 20020816 00057 NM 2002 8 16 UPS02438958 1 20020629 A 5712 65B101495 RIB BOEING 747 747123F NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C LT WING L/E RIB AT ILES 802.5 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR C/OUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAI RS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. COR ROSION BLEND OUT 0.022 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. 2 L 7 4 4F A20WE 2002081600058 20020816 00058 NM 2002 8 16 UPS02438959 1 20020629 A 5712 65B101485 RIB BOEING 747 747123F NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, LT WING LEADING EDGE RIB AT ILES 842.05 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.024 INCH X 0.5 INCH X 0.5 INCH, EXCEED SRM LIMIT. WING LEADING EDGE RIB INTE RIM CORROSION REPAIR CUTOUT AS PER EO B747-5740--17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. 2 L 7 4 4F A20WE 2002081600059 20020816 00059 NM 2002 8 16 UPS02438960 1 20020629 A 5712 65B078365 RIB BOEING 747 747123F NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, LT WING L/E RIB AT OLES 1308.15 FOUND CORROSION AT ROTARY ACTUTOR MOUNTING BOLT HOLES BORE AND CUTOU T SURFACE. CORROSION BLEND OUT 0.017 INCH X 0.5 INCH X 1 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSI ON REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIR TO BE DETAIL VISUALLY INSPECTION AT EVERY C-C HECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. 2 L 7 4 4F A20WE 2002081600060 20020816 00060 NM 2002 8 16 UPS02438961 1 20020629 A 5712 65B101406 RIB BOEING 747 747123F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C RT WING L/E RIB AT ILES 1014.95 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOU T SURFACE. CORROSION BLEND OUT 0.017 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORRO SION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C -CHECK NOT EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. 2 L 7 4 4F A20WE 2002081600061 20020816 00061 NM 2002 8 16 UPS02438962 1 20020629 A 5712 65B078346 RIB BOEING 747 747123F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RT WING L/E RIB AT OLES 1277.15 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTO UT SURFACE. CORROSION BLEND OUT 0.050 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORR OSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-.. 2 L 7 4 4F A20WE 2002081600062 20020816 00062 NM 2002 8 16 UPS02438963 1 20020629 A 5712 65B078466 RIB BOEING 747 747123F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT WING L/E RIB AT OLES 1421.35 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOU T SURFACE. CORROSION BLEND OUT 0.031 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORRO SION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C -CHECK NOT EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. 2 L 7 4 4F A20WE 2002081600063 20020816 00063 NM 2002 8 16 UPS02438964 1 20020629 A 5712 65B078546 RIB BOEING 747 747123F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RT WING L/E RIB AT ILES 1523.45 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTO UT SURFACE. CORROSION BLEND OUT 0.032 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORR OSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. 2 L 7 4 4F A20WE 2002081600064 20020816 00064 NM 2002 8 16 UPS02438965 1 20020629 A 5712 65B101519 RIB BOEING 747 747123F NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, LT WING L/E RIB AT ILES 765.45 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOU T SURFACE. CORROSION BLEND OUT 0.018 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORRO SION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C -CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX B. 2 L 7 4 4F A20WE 2002081600065 20020816 00065 NM 2002 8 16 USA2002F00067 1 20020702 A 4960 38762594 SWITCH BOEING 737 7374B7 1384702 NM UP CEILING FDR FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 434US 24556 ENROUTE, THE APU EXPERIENCED AN OVERSPEED CONDITION RESULTING IN AN AUTO SHUTDOWN OF THE APU. THE NR 1 ENGINE GENERATOR /CSD WAS ALREADY ON MEL (DUE TO LEAKING), SO THE FLIGHT DIVERTED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE APU ELECTRONIC 3 SPEED SWITCH. OPERATIONAL CHECK GOOD. ACCOMPLISH ED SUCCESSFUL INFLIGHT START OF APU. CLEARED AND REMOVED MEL ON NR 1 ENGINE GENERATOR/ CSD BY REPLACING THE NR 1 ENGINE CSD (PN 735511A). OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2002081600066 20020816 00066 NM 2002 8 16 UPS02438966 1 20020630 A 5712 65B078345 RIB BOEING 747 747123F NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, LT W L/E RIB AT OLES 1277.15 FOUND CORROSION AT ROTARY ACTUATOR MOUNT BOLT HOLES BORE AND CUTOUT SUR FACE. CORROSION BLEND OUT 0.022 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHEC K NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. 2 L 7 4 4F A20WE 2002081600067 20020816 00067 NM 2002 8 16 UPS02438967 1 20020701 A 5712 65B101529 RIB BOEING 747 747123F NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, LT WING L/E RIB AT ILES 755.05 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOU T SURFACE. CORROSION BLEND OUT 0.008 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORRO SION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C -CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. 2 L 7 4 4F A20WE 2002081600068 20020816 00068 NM 2002 8 16 UPS02438968 1 20020702 A 5712 65B078526 RIB BOEING 747 747123F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RT WING L/E RIB AT OLES 1493.45 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTO UT SURFACE. CORROSION BLEND OUT 0.038 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORR OSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. 2 L 7 4 4F A20WE 2002081600069 20020816 00069 NM 2002 8 16 UPS02438969 1 20020702 A 5712 65B078406 RIB BOEING 747 747123F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RT WING L/E RIB AT OLES 1349.29 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTO UT SURFACE. CORROSION BLEND OUT 0.026 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORR OSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. 2 L 7 4 4F A20WE 2002081600070 20020816 00070 NM 2002 8 16 UPS02438970 1 20020702 A 5712 65B078426 RIB BOEING 747 747123F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RT WING L/E RIB AT OLES 1381.25 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTO UT SURFACE. CORROSION BLEND OUT 0.030 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORR OSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. 2 L 7 4 4F A20WE 2002081600071 20020816 00071 NM 2002 8 16 UPS02438971 1 20020702 A 5712 65B078366 RIB BOEING 747 747123F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RT WING L/E RIB AT OLES 1308.15 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTO UT SURFACE. CORROSION BLEND OUT 0.020 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORR OSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. 2 L 7 4 4F A20WE 2002081600072 20020816 00072 NM 2002 8 16 UPS02438972 1 20020702 A 5712 65B101476 RIB BOEING 747 747123F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT WING L/E RIB AT ILES 852.45 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.065 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROS ION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C- CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. 2 L 7 4 4F A20WE 2002081600073 20020816 00073 NM 2002 8 16 UPS02438988 1 20020701 A 5310 FITTING BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RT BS 1480 BULKHEAD LONGERON EXTENSION FITTING FOUND CRACK AT NR 5 AT 8 O'CLOCK POSITION (VIEW LOOKI NG I/B), .0625 INCH IN LENGTH APPROX. RT BS 1480 BULKHEAD LONGERON EXTENSION FITTING AT HOLE NR 5 CRACK, HOLE FINAL SIZ E 0.6875 INCH & PLAN B REPAIR BUSHING INSTALL PER SB 53A2390 R1 FIG 14. HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TI ME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06. 2 L 7 4 4F A20WE 2002081600074 20020816 00074 NM 2002 8 16 UPS02438991 1 20020805 A 5313 STRINGER BOEING 747 747123F NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, BS 1480 BULKHEAD TOTAL 6 STRINGER FOUND SHORT EDGE MARGIN S34L, S35L , S36L, S34R, S35R & S36R. BS 1480 BULKHEAD STRINGER SHORT EDGE MARGIN CONDITION AT S34L, S35L, S36L , S34R, S35R & S36R ARE CONSIDERED AS STRUCTUALLY ACCEPTABLE AS PER HX RS R-53-43-34841 ITEM 4 PER FIG 5 & 6. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LI MIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06. 2 L 7 4 4F A20WE 2002081600075 20020816 00075 NM 2002 8 16 UPS02438994 1 20020701 A 5310 FITTING BOEING 747 747123F NM FUSLEAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RT OF BS 1480 BULKHEAD LONGERON EXTENSION FITTING FOUND CORROSION AT HOLE NR 11 BORE SURFACE SURFACE .0625 INCH IN DEPTH APPROX. RT BS 1480 BULKHEAD LONGERON EXTENSION FITTING AT HOLE NR 11 FINAL SIZE 0.6875 INCH & PLAN B REPAIR BUSHING INSTALL PER SB 53A2390 R.1 FIG 14. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAI R FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06. 2 L 7 4 4F A20WE 2002081600076 20020816 00076 2002 8 16 UIEA200200028 4 20020801 A 3410 A4321710016 INDICATOR BOEING 747 747243B 1384830 NM AIR SPEED IND STOPPED A UIEA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 EA 15 518MC 23476 AIR TURN BACK: F/OS AIR SPEED INDICATOR STOPPED AT 138 KTS. MACH OK. ALL OTHER FLIGHT INDICATONS OK. SWITCHED TO ALTE RNATE STATIC-NO HELP. RETURNED TO ORD. C/A: REPLACED F/OS AIR SPEED INDICATOR AND ACCOMPLISHED FULL PITOT STATIC CHECK WITH 500 TESTER. CHECKS OK PER MM. MAINTENANCE ALSO ACCOMPLISHED CONDITIONAL OVER WEIGHT LANDING INSPECTION PER MM. NO DISCREPANCIED NOTED. 2 L 7 4 4F A20WE 2002081600077 20020816 00077 NM 2002 8 16 UIEA200200027 1 20020727 A 2610 69B4650620 MODULE BOEING 747 747230B 1384889 NM CONTROL MODULE FAULTY A UIEA A B G J UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED DUMP FUEL J N WARNING INDICATION FALSE WARNING CR CRUISE 1 EA 15 508MC 21644 IN CRUISE, FL 290 MAIN DECK CARGO FIRE WARN LTS ILLUM STEADY. EMER ACTION AND LANDING CARRIED OUT. FUEL JETTISONED IAW CHECKLIST. MAIN DECK CARGO SMOKE DET LTS ILLUMINATED STEADY ON DESCENT, WENT OUT AND CAME ON INTERMITTENTLY THROUGHOUT DESCENT UNTIL THEY REMAINED OUT AFTER 10,000 FEET. DIVERTED, FUEL DUMPED +/- 40.8 TONS. C/A: MAIN DECK CARGO FIRE DET ECTION A AND B CONDITION CHECKED OK. FLIGHT, DPS/MEL ITEM REPEATED ON DESCENT. MAIN DECK CNTRL PANEL CHECKED AND TESTE D OK. ALL SMOKE DETECTORS ON MAIN DECK CHECKED, OK. FIRE WARNING LIGHTS ILLUM ON TAXI IN. UNABLE TO DUP DEFECT ON GRO UND REPLACED CONTROL MODULE IAW MM AS PRECAUTION. ALL SMOKE DETECTORS ON MAIN DECK CHECKED AND SYS TESTED OK IAW MM. 2 L 7 4 4F A20WE 2002081600078 20020816 00078 SW 2002 8 16 3RL072502 1 20020725 A 7930 WARNING LIGHT BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL COCKPIT ILLUMINATED E YTRA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 3RL 396 CAE800131 ON START-UP, ENGINE CHIP LIGHT CAME ON. 1 G 7 1 3U 3 U H2SW E4CE 2002081600079 20020816 00079 SW 2002 8 16 510RT062702 1 20020627 A 6240 206076373001 TACH GENERATOR BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ROTOR FAILED E YTRA K NONE O OTHER CR CRUISE 1 SW 03 510RT 51078 CAE860171 HYDRAULIC FAILURE DURING CRUISE FLIGHT. 1 G 7 1 3U 3 U H2SW E1GL 2002081600080 20020816 00080 NM 2002 8 16 AALA20021085 1 20020722 A 2560 101651303 SLIDE BOEING 767 767323 1385205 NM GE CF6 CF680 30025 NE CABIN DEPLOYED A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 39365 24046 DURING TAXI TO THE GATE, FLIGHT ATTENDENT INADVERTENTLY DEPLOYED THE RIGHT NR 1 DOOR SLIDE. SLIDED DEPLOYMENT WAS SUCCE SSFUL. REPLACED RIGHT NR 1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2002081600081 20020816 00081 WP 2002 8 16 ARWA20020802 1 20020804 A 2450 50128011 CONTROL PANEL DOUG DC8 DC85F54 3021926 WP COCKPIT MALFUNCTIONED A ARWA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 19 426FB 45667 AFTER STARTING ENGINE NR 2 AND ENGINE NR 3 HAD SMOKE IN COCKPIT. CREW EVACUATED AIRCRAFT. FOUND NR 2 AC CONTROL PANEL BURNT OUT. REMOVED AND REPLACED NR 2 AC CONTROL PANEL IAW MM 24-5-7, ALSO REMOVED AND REPLACED GENERATOR RELAY IAW MM 2 4-5-3. OPERATIONS CHECK NORMAL IAW MM 24-00. 2 L 7 4 4F RT 4A25 2002090900145 20020909 00145 NE 2002 9 9 ARWA20020803 2 20020813 A 7200 JT3D7 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 POWER LOSS A ARWA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 19 441J 53767 1377 45988 671378 AFTER BRAKE RELEASE, LOST PARTIAL POWER ON NR 4 ENGINE. ABORTED TAKEOFF AND RETURNED TO RAMP. REMOVED AND REPLACED NR 4 ENGINE, OPS CHECK AND LEAK CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2002081600082 20020816 00082 NM 2002 8 16 CALA0200406 1 20020718 A 5743 BEAM BOEING 737 7373T0 1384582 NM LT & RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND THE LT AND RT MLG SUPPORT BEAM O/B ATTACH POINTS CORRODED BETWEEN BUSHINGS. REPAIRED THE LT AND RT MLG BEAM IAW ECRA 5741-01025 AND 5741-01026. 2 L 7 2 4F RT A16WE 2002081600083 20020816 00083 WP 2002 8 16 CALA0200416 1 20020718 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND L2 DOOR JAMB CUSP ANGLE CORRODED AT STA 1089-1221, LBL 54. THE CORROSION WAS REMOVED IAW SRM 53-01, FI GURE 1. REPAIR WAS INSTALLED IAW SRM 51-10-4 AND 51-30-05. 2 L 7 2 4F A6WE 2002081600084 20020816 00084 NM 2002 8 16 CALA0200420 1 20020719 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND DIAGONAL FLOOR SUPPORT CORRODED AT BS 1016, LBL 8 AND RBL 8. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2002081600085 20020816 00085 NM 2002 8 16 CALA0200425 1 20020720 A 5414 PANEL BOEING 737 7373T0 1384582 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND A 1 INCH CRACK AT EDGE OF ACCESS HOLE IN NR 1 ENGINE PYLON PANEL 5724L. INSTALLED REPAIR DOUBLER IAW E CRA 5430-01204. 2 L 7 2 4F RT A16WE 2002081600086 20020816 00086 NM 2002 8 16 CALA0200426 1 20020722 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND CARGO FLOOR SUPPORT CORRODED AT STA 792-815, L27R. A NEW CARGO FLOOR SUPPORT WAS INSTALLED IAW SRM 53- 00-53. 2 L 7 2 4F RT A16WE 2002081600087 20020816 00087 WP 2002 8 16 CALA0200428 1 20020724 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND CUSP WEB CORRODED AT FS 1174-1250, LBL 44-58. THE CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2 AN D 51-30-1. 2 L 7 2 4F A6WE 2002081600088 20020816 00088 NM 2002 8 16 CALA0200431 1 20020726 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE FRETTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND RT KEEL BEAM TOP OF LOWER CHORD HAD WASHER MILLED INTO IT AT STA 720-727, RBL 6. INSTALLED REPAIR IAW ECRA 5310-03740. 2 L 7 2 4F RT A16WE 2002081600089 20020816 00089 EU 2002 8 16 AALA20021079 1 20020723 A 2740 ERLM8504413 RUDDER FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE COCKPIT FAULTY A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 1427A 11412 AFTER TAKEOFF BOTH STABILIZER TRIM FAULTED, BOTH YAW DAMPER AND NR 2 RUDDER SYSTEM FAULTED. STABILIZER TRIM AND YAW DAM PER WERE RESET. LANDED WITHOUT INCIDENT. REPLACED RUDDER LIMITER MONITOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT E25NE 2002081600090 20020816 00090 WP 2002 8 16 CALA0200437 1 20020809 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND E&E COMPARTMENT SUBFLOOR CORRODED AT VENTRAL STAIR MECHANISM, STA 162-168, X = 54.000. A DOUBLER WAS I NSTALLED IAW SRM 51-70-4. 2 L 7 2 4F A6WE 2002081600091 20020816 00091 SO 2002 8 16 LR7A02047 1 20020707 A 5320 BEAM LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION FOUND LT FS 557 UPPER BOW BEAM LOWER END CRACKED AND EXISTING REPAIR NOT PER SRM AT LBL 6 3, WL 150. REPAIRED IAW SRM SMP 583 53-40-14. 2 H 7 4 4T A1SO 2002081600092 20020816 00092 SO 2002 8 16 LR7A02061 1 20020707 A 5320 BEAM LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2322 4763 DURING SCHEDULED C3 INSPECTION FOUND LT FS 557 LOWER BOW BEAM CRACKED AT LOWER END AT LBL 63, WL 146. REPAIRED IAW LAC MEA 382-53-02-034. 2 H 7 4 4T A1SO 2002081600093 20020816 00093 SO 2002 8 16 LR7A02063 1 20020727 A 5320 3530428R TEE FITTING LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 343 5025 DURING SCHEDULED A-CHECK INSPECTION FOUND RT FS 990 BULKHEAD TEE AND WEB CRACKED AT RBL 63, WL 257. REPLACED TEE AND WE B IAW SRM SMP 583-53-50-04 AND 51-70. 2 H 7 4 4T A1SO 2002081600094 20020816 00094 SO 2002 8 16 LR7A02066 1 20020812 A 5320 RING ASSEMBLY LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2340 4606 DURING SCHEDULED C4 INSPECTION FOUND LT FS 477 RING SEGMENT CRACKED AT LBL 49, WL 267. REPAIRED IAW SB 382-53-50, DWG K S382-53-184 R1. 2 H 7 4 4T A1SO 2002081600095 20020816 00095 SO 2002 8 16 LR7A02071 1 20020812 A 5343 CAP LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2340 4606 DURING SCHEDULED C4 INSPECTION FOUND FS 528 RT MLG BEAM CAP CRACKED AT RBL 67, WL 236. REPAIRED IAW SRM SMP 583 53-40-1 9. 2 H 7 4 4T A1SO 2002081600096 20020816 00096 2002 8 16 OZIA200243003 4 20020506 A 3425 HG2010AC02 COMPUTER DORNER DO32 DO328300 NM E/E BAY FAILED A OZIA K NONE J WARNING INDICATION AP APPROACH 1 CE 05 430Z 4691 3127 GLIDESLOPE ON CAPTAIN'S SIDE FAILED. 2 H 7 2 4T RT A55NM 2002081600097 20020816 00097 NM 2002 8 16 OZIA200243005 1 20020520 A 7330 WARNING SYSTEM DORNER DO32 DO328300 NM PWA 306 PW306B NE COCKPIT ACTIVATED A OZIA K NONE J WARNING INDICATION DE DESCENT 1 CE 05 430Z 3628 3127 CD0019 INTERMITTENT RT FUEL FILTER BYPASS INDICATION. 2 H 7 2 4T 4 F RT A55NM E35NE 2002081600098 20020816 00098 SO 2002 8 16 PNSA020704 1 20020704 A 8011 MZ6222 STARTER PIPER PA32 PA32301 7103207 SO ENGINE MALFUNCTIONED E PNSA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 AL 03 8212H 328006046 DURING CLIMB AFTER OPENING HEATER VENT DETECTED SMOKE AND ODOR OF ELECTRICAL FIRE AND AMP METER SHOWED PEGGED AT 70 AMPS . ELECTRICAL SYSTEM SHUT OFF AND SMELL WENT AWAY. MAINTENANCE FOUND STARTER SOLENOID STUCK AND OVERHEATED. 1 L 7 1 3O A3SO 2002081600099 20020816 00099 NM 2002 8 16 QXEA0201015 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS CORROSION PITS IN ITS CHANNEL AT X467. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2002081600100 20020816 00100 NM 2002 8 16 QXEA0201016 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LEFT HAND OUTBOARD SEAT TRACK AT X484 HAS NICKS IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2002081600101 20020816 00101 NM 2002 8 16 QXEA0201017 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LEFT HAND OUTBOARD SEAT TRACK X504 HAS NICKS IN TOP FLANGE. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2002081600102 20020816 00102 NM 2002 8 16 QXEA0201018 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT PITS IN TOP FLANGE X520. REPAIRED IAW DHC-8-202 SRM 51-20-16 AND SRM 51-2 0-41. 2 H 7 2 4T RT A13NM 2002081600103 20020816 00103 NM 2002 8 16 QXEA0201021 1 20020702 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - MATING AREA FOR PANEL 144HZ HAS LIGHT CORROSION AROUND PERIMETER. REPAIRED IAW DHS-8-200 SRM 51-20-11, PAGE 7 AND CPC MANUAL CHAPTER 5, PAGE 5. 2 H 7 2 4T RT A13NM 2002081600104 20020816 00104 NM 2002 8 16 QXEA0201022 1 20020710 A 5420 SHIM DHAV DHC8 DHC8202 2809007 NM RT NACELLE OUT OF POSITION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - SHIM OUT OF POSITION AT FORWARD END OF CHANNEL, LOCATED AT OUTBOARD SIDE OF RIGHT MAIN WHEEL WELL ZN15.00 AND XN17 0.60, IN RIGHT NACELLE. REPAIRED IAW HORIZON AIR EA 2-564-144. 2 H 7 2 4T RT A13NM 2002081600105 20020816 00105 NM 2002 8 16 QXEA0201023 1 20020703 A 7120 STRUT DHAV DHC8 DHC8202 2809007 NM RT ENGINE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LIGHT SURFACE CHAFING ON INBOARD SIDE OF LOWER RIGHT ENGINE STRUT, ON RIGHT NACELLE. REPAIRED IAW DHC-8 RD 8-54-0 36. 2 H 7 2 4T RT A13NM 2002081600106 20020816 00106 NM 2002 8 16 QXEA0201024 1 20020712 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - PITTING CORROSION ON RIGHT OUTBOARD SEAT TRACK AT STATION 309-312. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002081600107 20020816 00107 NM 2002 8 16 QXEA0201025 1 20020705 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LIGHT CORROSION ON RIGHT OUTBOARD SEAT TRACK (NR 11) AT STATION 438. REPAIRED IAW DHC-8-202 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002081600108 20020816 00108 NM 2002 8 16 QXEA0201026 1 20020705 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - SCRATCH ON RIGHT HAND OUTBOARD SEAT TRACK NR 11 AT STATION 450. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20 -36. 2 H 7 2 4T RT A13NM 2002081600109 20020816 00109 NM 2002 8 16 QXEA0201027 1 20020705 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - SCRATCH ON RIGHT HAND OUTBOARD SEAT TRACK NR 11 AT STATION 470. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20 -36. 2 H 7 2 4T RT A13NM 2002081600110 20020816 00110 NM 2002 8 16 QXEA0201028 1 20020705 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LIGHT CORROSION ON RIGHT HAND OUTBOARD SEAT TRACK NR 11 AT STATION 485. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002081600111 20020816 00111 NM 2002 8 16 QXEA0201029 1 20020705 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - SCRATCH ON RIGHT HAND OUTBOARD SEAT TRACK NR 11 AT STATION 490. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002081600112 20020816 00112 NM 2002 8 16 QXEA0201030 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LIGHT CORROSION ON RIGHT HAND OUTBOARD SEAT TRACK NR 11 AT STATION 515. REPAIRED IAW RD 8-53-3644 DHC-8-200 SRM 5 1-20-16 AND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2002081600113 20020816 00113 NM 2002 8 16 QXEA0201031 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - CORROSION ON RIGHT HAND OUTBOARD SEAT TRACK NR 12 AT STATION 528. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51- 20-41. 2 H 7 2 4T RT A13NM 2002081600114 20020816 00114 NM 2002 8 16 QXEA0201032 1 20020714 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - SCRATCH ON RIGHT HAND OUTBOARD SEAT TRACK NR 12 AT STATION 540. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20 -41. 2 H 7 2 4T RT A13NM 2002081600115 20020816 00115 NM 2002 8 16 QXEA0201033 1 20020705 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LIGHT CORROSION ON RIGHT HAND INBOARD SEAT TRACK NR 9 AT STATION 531. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002081600116 20020816 00116 NM 2002 8 16 QXEA0201034 1 20020709 A 5510 FRAME DHAV DHC8 DHC8202 2809007 NM HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LEFT HAND SIDE FRAME 4 STRINGER 3, LOOK UP FROM PANEL 331AB OVER SUPPORT BRACKET, HAS .5 INCH CRACK. REPAIRED IAW RD 8-55-199. 2 H 7 2 4T RT A13NM 2002081600117 20020816 00117 NM 2002 8 16 QXEA0201035 1 20020716 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM NACELLE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - DENT IN NACELLE SKIN, INBOARD SIDE OF NACELLE, AT APPROXIMATELY STATION XN121.2, ZN20.25, JUST FORWARD OF DRAIN MA ST. REPAIRED IAW HORIZON AIR EA 2-54-146. 2 H 7 2 4T RT A13NM 2002081600118 20020816 00118 NM 2002 8 16 QXEA0201036 1 20020717 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - OUTBOARD FLAP HAS TWO AREAS OF CHAFE DAMAGE ON THE UPPER INBOARD SURFACE. REPAIRED IAW DHC-8-200 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002081600119 20020816 00119 NM 2002 8 16 QXEA0201037 1 20020717 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - INBOARD FLAP HAS CHAFE DAMAGE ON UPPER SURFACE AT THE PREVIOUS PATCH. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2002081600120 20020816 00120 NM 2002 8 16 QXEA0201039 1 20020715 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - FLOORBEAM SEAT TRACK NR 7 ATTACH HOLE IS OVERSIZED. REPAIRED IAW HORIZON AIR EA 2-53-405. 2 H 7 2 4T RT A13NM 2002081600121 20020816 00121 NM 2002 8 16 AALA20021062 1 20020718 A 2900 LINE BOEING 757 757223 1384957 NM RROYCE RB211 RB211* 54555 NE PRESSURE LINE BROKEN A AALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 21 657AM 24615 ENROUTE, CUN-JFK ON DEPARTURE, LEFT HYDRAULIC SYSTEM QUANTITY LOSS. RETURNED AIRCRAFT TO CUN AND LANDED WITHOUT INCIDEN T. REPLACED RIGHT GEAR MAIN DOOR SEQUENCE VALVE PRESSURE LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM A12EU 2002081600122 20020816 00122 NM 2002 8 16 AALA20021084 1 20020724 A 3350 LIGHT BOEING 767 767223 1385123 NM GE CF6 CF680 30025 NE CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 305AA 22311 DURING OVERNIGHT MAINTENANCE FOUND CENTER GALLEY EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR E MERGENCY ESCAPE PATH LIGHT CENTER GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2002081600123 20020816 00123 NM 2002 8 16 AALA20021083 1 20020724 A 3350 CONNECTOR BOEING 767 767223 1385123 NM GE CF6 CF680 30025 NE CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AA 22327 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 32H INOPERATIVE. SECURED CONNECTOR AT SEAT LEG F OR 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2002081600125 20020816 00125 NM 2002 8 16 AWXA200200670 1 20020729 A 3150 WARNING SYSTEM BOEING 737 7373G7 1384595 NM COCKPIT FALSE ACTIVATION A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 309AW 24711 PHX - ABORTED TAKEOFF - FLT 0137 - WHEN PREPARING TO TAKEOFF FROM PHX EN ROUTE TO LAS THE TAKEOFF WARNING CONFIGURATION HORN SOUNDED WITH SPOILERS, FLAPS, TRIM AND BRAKES ALL IN THE PROPER POSITION. MAINTENANCE PERFORMED A WARNING SYSTEM T EST, CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002081600126 20020816 00126 NM 2002 8 16 AALA20021082 1 20020725 A 3350 LIGHT BOEING 767 767323 1385205 NM GE CF6 CF680 30025 NE CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 383AN 26995 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 34H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT A SSEMBLY AT SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2002081600127 20020816 00127 NE 2002 8 16 AWXA200200675 2 20020729 A 7261 4A7120 SCAVENGE PUMP AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 ENGINE LEAKING A AWXA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 WP 28 646AW 271 PHX - FLT 0536 - WHILE AIRCRAFT WAS TAXIING TO GATE, THE AIRCRAFT TAXIING BEHIND REPORTED SEEING A TAILPIPE FIRE AT NR 1 ENGINE TAILPIPE. MAINTENANCE PERFORMED A HOT SECTION BORESCOPE PER T/C 15M72304, NO DEFECTS WERE NOTED. AS A PRECAUT ION THE NR 1 ENGINE OIL SCAVAGE PUMP WAS REMOVED AND REPLACED IAW T/C R5M79301, ENGINE RUN OPERATIONAL CHECK WAS GOOD. OIL PRESSURE AND TEMPERATURE WAS NORMAL, NO LEAKS WERE NOTED. 2 L 7 2 4F 4 F RT A28NM E311NE 2002081600128 20020816 00128 NM 2002 8 16 AWXA200200676 1 20020728 A 3350 6104789 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 186AW 22653 PHX - DURING INSPECTION THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E LT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002081600129 20020816 00129 NM 2002 8 16 AWXA200200677 1 20020728 A 3350 6104789 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 186AW 22653 PHX - DURING INSPECTION THE LT EXTERIOR EMERGENCY EXIT LIGHT ON BELLY OF AIRCRAFT, AFT OF THE WING WAS FOUND INOPERATIVE . MAINTENANCE REMOVED AND REPLACED THE LT EXTERIOR EMERGENCY EXIT LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002081600130 20020816 00130 NM 2002 8 16 AWXA200200678 1 20020729 A 3397 D9299200900200 WIRE AIRBUS A319 A319132 3930340 NM CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 LAS - EMERGENCY LIGHT HARNESS SEAT ROW 9 RT HAS A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH L IGHT HARNESS AT SEAT ROW 9 RT, OPERATIONAL CHECK OF LIGHTING SYSTEM CHECKED GOOD. 2 L 7 2 4F RT A28NM 2002081600131 20020816 00131 NM 2002 8 16 AWXA200200682 1 20020725 A 5310 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 307AW 24634 MCN - MAJOR REPAIR - DURING C-12 CHECK A .5 INCH CRACK WAS FOUND ON THE SUPPORT ANGLE AT THE FORWARD LOWER CUTOUT OF THE R1 DOOR, BS 294.5. MAINTENANCE REMOVED THE DAMAGED SUPPORT ANGLE AND DOOR STOP FITTING, FABRICATED A NEW REPAIR ANGLE AND FRAME, AND INSTALLED REPAIR PARTS IAW DWG 69-37402, AND B737-300 SRM 51-40-02, PG 3-4, 10-11, & 38. 2 L 7 2 4F RT A16WE 2002081600132 20020816 00132 NM 2002 8 16 AWXA200200683 1 20020730 A 3350 RPS1B POWER SUPPLY BOEING 737 73733A 1384673 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 175AW 23634 DFW - FLT 0548 FLIGHT CREW REPORTED THAT EMERGENCY ESCAPE PATH LIGHTING SEAT ROWS 1 - 5 LT ARE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHTING POWER SUPPLY AT FORWARD CEILING ABOVE SEAT ROW 1, OPERATIONAL CHEC K WAS GOOD. 2 L 7 2 4F RT A16WE 2002081600133 20020816 00133 EU 2002 8 16 AWXA200200684 1 20020727 A 2560 P4010021 BATTERY AIRBUS 320 A320231 3930325 EU FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 643AW 315 YWG - DURING C-08 CHECK, THE EMERGENCY FLASHLIGHTS AT BOTH THE FORWARD AND AFT FLIGHT ATTENDANT POSITIONS WERE FOUND TO HAVE UNSERVICEABLE BATTERIES. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN BOTH THE FORWARD AND AFT FLIGHT ATTEND ANT POSITIONS, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002081600134 20020816 00134 NM 2002 8 16 AWXA200200686 1 20020731 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 184AW 22651 LAS - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 6 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 6 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002081600135 20020816 00135 NM 2002 8 16 AWXA200200688 1 20020802 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 154AW 23776 LAS - FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AT THE AFT LT FLIGHT ATTENDANT JUMPSEAT WAS INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFT LT FLIGHT ATTENDANT JUMPSEAT EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002090900154 20020909 00154 NM 2002 9 9 AWXA200200689 1 20020803 A 2913 3508807 PUMP BOEING 757 757225 1384959 NM NR 2 ENGINE FAILED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 913AW 19567 2528 22207 PHX - AIR TURN BACK - FLT 0081 - AFTER TAKEOFF FROM PHX EN ROUTE TO BWI DURING INITIAL CLIMB A RT HYD QUANTITY EICAS MES SAGE ILLUMINATED FOLLOWED BY A RT HYD SYSTEM PRESSURE EICAS MESSAGE, QUANTITY INDICATED .26, TURNED BACK TO PHX AND LAND ED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE HYD PUMP IAW T/C R5M29601, LEAK AND OPERATIONAL CHECK WAS GOOD. VENDOR CONFIRMED FAILURE OF NR 2 ENGINE HYD PUMP. BENCH TEST WAS NOT PERFORMED DUE TO THICK BLACK BURNT SLUDG E FOUND AT INLET PORT DURING ACCEPTANCE INSPECTION. 2 L 7 2 4F RT A2NM 2002081600136 20020816 00136 EU 2002 8 16 AALA20020064 1 20020620 A 5312 BULKHEAD FOKKER F28 F28MK0100 4990807 EU FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 NM 01 1425A 11408 TUL - FOUND SCRATCHES AND GOUGES ON INBOARD BULKHEAD IN RIGHT A/C BAY. REPAIRED DAMAGE BY INSTALLING DOUBLERS PER ESO 5 1000 DATED 6-19-02. (M) 2 L 7 2 4F RT 2002081600137 20020816 00137 EU 2002 8 16 AALA20020082 1 20020621 A 5312 BULKHEAD FOKKER F28 F28MK0100 4990807 EU FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1425A 11408 TUL - FOUND LARGE DENT ON INBOARD BULKHEAD IN RIGHT A/C BAY. REPAIRED DAMAGE BY INSTALLING DOUBLER PER ESO 51000. (M) 2 L 7 2 4F RT 2002081600138 20020816 00138 EU 2002 8 16 AALA20020135 1 20020621 A 5312 BULKHEAD FOKKER F28 F28MK0100 4990807 EU FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1425A 11408 TUL - FOUND SCRATCHES AND GOUGES ON INBOARD BULKHEAD IN LEFT AC BAY. REPAIRED DAMAGE BY INSTALLING DOUBLER PER ESO 5100 0. (M) 2 L 7 2 4F RT 2002081600139 20020816 00139 EU 2002 8 16 AALA20020148 1 20020621 A 5312 BULKHEAD FOKKER F28 F28MK0100 4990807 EU FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1425A 11408 TUL - FOUND DENT IN INBOARD BULKHEAD IN LEFT AC BAY. REPAIRED DAMAGE BY INSTALLING DOUBLER PER ESO 51000. (M) 2 L 7 2 4F RT 2002081600140 20020816 00140 EU 2002 8 16 AALA20020201 1 20020621 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 NM 01 1425A 11408 TUL - FOUND CORROSION AROUND HOLE IN FUSELAGE FOR EXHAUST DUCT AND UNDER MOUNTING FRAME FOR OUTER HEAT SHIELD. INSTALLE D DOUBLER AND DOUBLER SHIMS AROUND IN FUSE FOR APU EXHAUST PER ESO 5100. (M) 2 L 7 2 4F RT 2002081600141 20020816 00141 EU 2002 8 16 AALA20020381 1 20020617 A 5320 ANGLE FOKKER F28 F28MK0100 4990807 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 NM 01 1425A 11408 TUL - FOUND OBLIQUE FRAME FORWARD SIDE ANGLE CRACKED AND STOP DRILLED OR ROUTED OUT ABOVE STRINGERS 50/40. INSTALLED NE W OBLIQUE ANGLE AT FRAME 50-2 BETWEEN STRINGERS 50/48 PER ESO 51000 AND SRM 53-00-02. (M) 2 L 7 2 4F RT 2002081600142 20020816 00142 NM 2002 8 16 AALA20020707 1 20020512 A 5245 DOOR BOEING 767 767223 1385123 NM A/C BAY MISSING A AALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 21 317AA 22319 MIA - FLT 207 - EN ROUTE MIA-LAX, RUMBLING NOISE AND VIBRATIONS IN BUSINESS CLASS SECTION OF AIRCRAFT. AIRCRAFT RETURNE D TO MIA LANDED WITHOUT INCIDENT. NO OVERWEIGHT LANDING. RIGHT PACK BAY DOOR MISSING FROM AIRCRAFT. REPAIR EVALUATION IN PROGRESS. (M) 2 L 7 2 4F RT A1NM 2002081600143 20020816 00143 WP 2002 8 16 AALA20020821 1 20020531 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND CARGO CUT OUT LOWER FRAME HAS CORROSION ON OUTBOARD FACE STATION 1155-1211, SEVERAL AREAS. INSTALLED NEW FR AME PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002081600144 20020816 00144 NM 2002 8 16 AALA20020849 1 20020512 A 5245 DOOR BOEING 767 767223 1385123 NM A/C BAY MISSING A AALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 21 317AA 22319 MIA - FLT 207 - EN ROUTE MIA-LAX, RUMBLING NOISE AND VIBRATIONS IN BUSINESS CLASS SECTION OF AIRCRAFT. AIRCRAFT RETURNE D TO MIA LANDED WITHOUT INCIDENT. NO OVERWEIGHT LANDING. RIGHT PACK BAY DOOR MISSING FROM AIRCRAFT. AIRCRAFT REMOVED FROM SERVICE AND FERRIED TO AFW ON SPOTTING MESSAGE. DURING MBV AT AFW ALL PANELS WERE REPAIRED AND/OR REPLACED AS REQU IRED. (M) 2 L 7 2 4F RT A1NM 2002081600145 20020816 00145 NM 2002 8 16 AALA20021025 1 20020714 A 2420 GEN3014 IDG BOEING 777 777223 1385213 NM RROYCE RB211 RB211* 54555 NE LEFT ENGINE FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 772AN 29580 FOUR HOURS INTO FLIGHT, LEFT GENERATOR FAILED. REPLACED LEFT GCU PER MM. REPLACEMENT TEST PASSED MESSAGE CLEARED. LEFT GEN SYS STILL INOPERATIVE ON ENGINE RUN MESSAGE AND NO VOLT OUTPUT. REPLACED LEFT IDDG PER MM. LEAK AND GEN SYS OPS T EST OK. 2 L 7 2 4F 4 F RT T00001SE A12EU 2002081600146 20020816 00146 NE 2002 8 16 AALA20020801 2 20020601 A 7200 ENGINE BOEING 737 737823 13844BZ NM CFMINT CFM56 CFM567B26US NE RIGHT MALFUNCTIONED A AALA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 21 927AN 30077 MSY - FLT 978 - MIA-IAH - EN ROUTE IAH AT CRUISE, RT ENGINE LOST POWER ASSOCIATED WITH VIBRATION. PILOT DECLARED EMERGE NCY AND LANDED MSY WITHOUT INCIDENT. TOWER REPORTED RIGHT ENGINE ON FIRE. EMERGENCY EVACUATION INITIATED. THERE WERE NO ENGINE FIRE WARNING LIGHTS IN COCKPIT. FIRE CREWS DETERMINED THERE WAS NO ENGINE FIRE. EMERGENCY EVACUATION CANCELE D. REMOVED AND REPLACED RIGHT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A16WE E00055EN 2002081600147 20020816 00147 NM 2002 8 16 AALA20020881 1 20020609 A 2781 SENSOR BOEING 767 767323 1385205 NM L/E SLAT MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 366AA 25193 MIA - FLT 1772 - EN ROUTE SJU-JFK, AIRCRAFT EXPERIENCED L/E ASYMMETRIC MESSAGE ON EICAS. DIVERTED FLIGHT TO MIA LANDING WITHOUT INCIDENT, NON-OVERWEIGHT. MIA ACCOMPLISHED FIM TASK 32-09-03 FAULT CODE 10 AND 285 WAS DETECTED. REPLACED PSE U DUE TO CODE 10 PROCEDURES AND INSPECTED LEFT NR 4 SLAT PROP SENSORS. NO FAULTS NOTED. OPERATIONAL CHECK PERFORMED ON FLAP/SLATS. SYSTEM CHECKED NORMAL. (M) 2 L 7 2 4F RT A1NM 2002081600148 20020816 00148 NM 2002 8 16 ASAA0210062 1 20020317 A 5320 6546554 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BS 847, STRINGER 26L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002081600149 20020816 00149 NM 2002 8 16 ASAA0210063 1 20020317 A 5320 6546548 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BS 747, STRINGER 26L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002081600150 20020816 00150 NM 2002 8 16 ASAA0210064 1 20020318 A 5320 6546548 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BS 747, STRINGER 22R CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002081600151 20020816 00151 NM 2002 8 16 ASAA0210114 1 20020513 A 5311 6546596 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 727B, STRINGER 24R-25R DENTED. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F A16WE 2002081600152 20020816 00152 NM 2002 8 16 ASAA0210115 1 20020513 A 5311 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 500B, STRINGER 21L-25L DENTED. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F A16WE 2002081600153 20020816 00153 SO 2002 8 16 C2XA02IA168 1 20020811 A 2742 3621001007 CONTROL UNIT EMB 135 EMB135LR 3260305 SO FAILED A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 27523 145389 Crew reported a pitch trim fail indication inflight. The aircraft returned to IAH without further incident. A reset of t he system was performed along with an operational check of the stab trim. The aircraft was returned to service. The prob lem reocurred and returned to IAH. Maintenance removed and replaced the Horizontal Stabilizer Control Unit. The aircraft operationally checked good and was returned to service. 2 L 7 2 4F RT T00011AT 2002081600154 20020816 00154 EA 2002 8 16 COMA0260482 1 20020813 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 958CA 7111 FLIGHT 5295 EMERGENCY FLOOR PATH LIGHTS, ROWS 2-9, ARE INOPERABLE.SECURED LOOSE WIRE CONNECTOR, OPERATION SATISFACTORY. 2 L 7 2 4F RT A21EA 2002081600155 20020816 00155 NM 2002 8 16 UPS02439077 1 20020803 A 5310 WEB BOEING 747 747212B 1384886 NM STA 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C FX- LOWER FUSELAGE PRESSURE BULKHEAD ATT WEB FOUND CRACKED AT STA 1480 RH SIDE O/B RBL 95. CLOSE OF SP LICE FITTING STRG 33R. WEB PANEL REPAIRED AS PER SRM 51-40-02 FIG 1 2 L 7 4 4F A20WE 2002081600156 20020816 00156 SO 2002 8 16 C2XA02IA169 1 20020812 A 2742 3622009015 ACTUATOR EMB 135 EMB135LR 3260305 SO VERTICAL STABILI FAULTY A C2XA K NONE O OTHER CL CLIMB 1 SW 27 27523 3683 3683 145389 Crew reported pitch trim failure during cruise. The aircraft returned to IAH and landed without incident. Maintenance re moved and replaced the horizontal stabilizer actuator. The aircraft was operationally checked, test flown satisfactorily , and returned to service. 2 L 7 2 4F RT T00011AT 2002081600157 20020816 00157 NM 2002 8 16 CA020726021 1 20020726 A 5754 651722419 BRACKET BOEING 727 727116C 1384046 NM PWA JT8 JT8D7B 52053 NE SLAT ACTUATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 51926 51926 (CAN) DURING A ROUTINE STRUCTURAL INSPECTION A CRACK WAS FOUND IN THE NR 3 LEADING EDGE SLAT ACTUATOR INBOARD WING ATTAC H FITTING. THE CRACK WAS FOUND ON A VISUAL INSPECTION AND CONFIRMED TO BE 3/4 OF A INCH USING NDT. THERE IS NO ALLOWABLE REPAIRS FOR THIS BRACKET. THE BRACKET WAS REPLACED WITH A NEW UNIT FROM BOEING. THE BRACKET IS A ON CONDITION PART AND HAS NOT BEEN A PROBLEM FOR US IN THE PAST. 2 L 7 3 4F 4 F RT A3WE E2EA 2002081600159 20020816 00159 NM 2002 8 16 CA020731016 1 20020713 A 2782 65446516 ACTUATOR BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE LE SLATS FAILED W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CA (CAN) L/E FLAP TRANSIT ON AFTER T/O. NR 5 RT WING SLAT FULLY EXTENDED FOR APPROX 2 MIN. WHEN IT RETRACTED AND BEFORE WE RECYCLED THE FLAPS. REPLACED NR 5 SLAT ACTUATOR AS PER AMM. SYSTEM CHECKED SERVICEABLE AND CERTIFIED. 2 L 7 2 4F 4 F A16WE E2EA 2002081600160 20020816 00160 EU 2002 8 16 CA020801004 1 20020708 A 2730 3945122506 COMPUTER AIRBUS A321 A321211 3930370 EU IAE V2530 V2530A5 NE ELEVATOR CONTROL FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) ELAC (ELEVATOR AILERON COMPUTER) 1 FAULT INBOUND TO YYZ ACCOMPANIED BY A MILD ELECTRICAL BURNING SMELL. SMELL DISP ATED AFTER ELAC WAS SELECTED OFF. ELAC REPLACED AND CHECKED SERVICEABLE PER AMM 27-93-34-400 2 L 7 2 4F 4 F RT A28NM E40NE 2002081600161 20020816 00161 EU 2002 8 16 CA020801005 1 20020716 A 2721 ACTUATOR AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE RUDDER TRIM FAILED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA (CAN) AUTO FLT RUDDER TRIM FAULT ON ECAM. RESET DID NOT FIX. RUDDER TRIM ACTUATOR REPLACED AS PER AMM 27-22-51 AND OPER ATION CHECKED. 2 L 7 2 4F 4 F RT A28NM E37NE 2002081600162 20020816 00162 NM 2002 8 16 CA020801008 1 20020725 A 5280 NAS6706D26 BOLT BOEING 767 7673S1 1385211 NM GE CF6 CF680C2B6F 30025 NE LT MLG DOOR SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AT TRIP CHECK DAMAGE FOUND TO LT WING TO FLAP FAIRING, MLG SHOCK STRUT DOOR, AND JURY STRUT DOOR. INVESTIGATION FOUND SHOCK STRUT DOOR MID ATTACH BOLD HAD SHEARED ALLOWING SEPERATION OF DOOR FROM STRUT. NEW FAIRING PANEL FABRICATE D, JURY STRUT DOOR TEMPORARY REPAIRED AND SHOCK STRUT DOOR REMOVED FOR REPAIRS AIRCRAFT IS PRESENTLY FLYING UNDER MEL 32 -12-01A. 2 L 7 2 4F 4 F RT A1NM E13NE 2002081600164 20020816 00164 NE 2002 8 16 CA020807003 2 20020804 A 7250 804319 SEAL BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE NR 1 ENGINE LEAKING W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 CA (CAN) ON DESCENT ODOR OF SMOKE VERY STRONG. SMOKE ALARM SOUNDED IN FRONT AND BACK OF AIRCRAFT. ODOR PERSISTED FOR AP PROX 10 MINUTES. QRH DRILL CARRIED OUT. ALL PARAMETERS NORMAL. SMOKE ODOR APPEARS TO COME FROM AIR CONDITIONING. OIL FOUND IN THE NR 1 ENGINE LPT SHAFT CREATING SMOKE THROUGH THE FRONT. REAR CONE REMOVED FOR ACCESS. LPT REAR PLUG SEAL R EPLACED. WORK COMPLETED AS PER ENGINE MANUAL 72-00-53. 2 L 7 2 4F 4 F RT A1NM E3NE 2002081600165 20020816 00165 NM 2002 8 16 QXEA0201214 1 20020813 A 2120 GASKET DHAV DHC8 DHC8202 2809007 NM ZONE 400 LEAKING A QXEA K NONE O OTHER CR CRUISE 1 NM 09 348PH 484 PDX-BLEED AIRFLOW INADEQUATE, MAIN CABIN NEVER COOLED AT ALTITUDE. DUCT TEMPERATURE NEVER DROPPED BELOW 20 DEGREES WITH OUTSIDE AIR TEMP -10 AT FLIGHT LEVEL 220. DIRTY SOCK SMELL. INSPECTED AND FOUND #1 NACELLE SHUTOFF VALVE LEAKING. REPLAC ED GASKET AND CLAMP. AIRFLOW INDICATOR NORMAL, AUTO/TEMP CONTROL OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081600166 20020816 00166 NM 2002 8 16 QXEA0201215 1 20020815 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 548 548 528 PDX-RIGHT HAND FUSELAGE AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081600167 20020816 00167 EU 2002 8 16 C2XA02IA170 1 20020812 A 3350 0341516 FUSE AEROSP ATR42 ATR42320 8680930 EU CABIN BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15827 175 Emergency lights at station 25WL did not test when selected. Maintenance removed and replaced the fuse at station 3wl. T he system operationally checked good and the aircraft was approved for return to service. 2 H 7 2 4T RT A53EU 2002081600168 20020816 00168 NM 2002 8 16 ASAA0210116 1 20020513 A 5320 65516985 SPLICE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER SPLICE AT BS 907, STRINGER 25L CORRODED. REPAIRED STRINGER SPLICE PER SR M. (M) 2 L 7 2 4F A16WE 2002081600169 20020816 00169 NM 2002 8 16 ASAA0210117 1 20020513 A 5311 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 500A, STRINGER 20L-24L DENTED. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F A16WE 2002081600170 20020816 00170 EU 2002 8 16 C2XA02IA171 1 20020812 A 3350 3011151 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15827 175 The emergency light battery at station 30WL was found to have low voltage. Maintenance removed and replaced the affected battery and the emergency light system was operationally checked. 2 H 7 2 4T RT A53EU 2002081600171 20020816 00171 NM 2002 8 16 ASAA0210119 1 20020513 A 5311 6546551 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 867, STRINGER 24L-25L DENTED. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F A16WE 2002081600172 20020816 00172 NM 2002 8 16 ASAA0210125 1 20020515 A 5310 6546650 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 787, RIGHT BUTTOCK LINE 9 CORRODED. REMOVED AND REPLACED SHEAR TI E PER SRM. (M) 2 L 7 2 4F A16WE 2002081600173 20020816 00173 NM 2002 8 16 ASAA0210126 1 20020515 A 5330 BEAR STRAP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND BEAR STRAP AT BS 360, WATERLINE 300 CRACKED. REPAIRED BEAR STRAP PER EA. (M) 2 L 7 2 4F A16WE 2002081600174 20020816 00174 NM 2002 8 16 ASAA0240025 1 20020303 A 5313 STRINGER BOEING 737 737490 1384715 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 703AS 28893 PAE - DURING C-CHECK, FOUND DAMAGED STRINGER AT BS 486. REPAIRED STRINGER 1 AT BS 486 PER SRM. (M) 2 L 7 2 4F RT A16WE 2002081600175 20020816 00175 NM 2002 8 16 ASAA0240032 1 20020315 A 5330 65C32358 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 762AS 25099 PAE - DURING C-CHECK, FOUND CREASE IN FUSELAGE SKIN 17 INCHES LONG AT BS 399-416 AND STRINGER 20 RT. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002081600176 20020816 00176 NM 2002 8 16 ASAA0240075 1 20020707 A 3350 8100022608 LIGHT BOEING 737 7374Q8 138447Q NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 774AS 25107 PDX - DURING LINE CHECK, FOUND FORWARD 2 EMERGENCY TRACK LIGHTS INOPERATIVE. RELAMPED AND RECONNECTED LIGHTS, OPS CHECK ED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002081600177 20020816 00177 NM 2002 8 16 ASAA0240076 1 20020708 A 3350 8100022608 LIGHT BOEING 737 7374Q8 138447Q NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 FAI - DURING LINE CHECK, FOUND NUMEROUS TRACK LIGHTS INOPERATIVE. RELAMPED AND RECONNECTED LIGHTS, OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002081600178 20020816 00178 NM 2002 8 16 ASAA0240077 1 20020710 A 3350 8100022608 LIGHT BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 SEA - DURING LINE CHECK, FOUND TRACK LIGHTS INOPERATIVE AT ROW 20. RECONNECTED LIGHTS, OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002081600179 20020816 00179 NM 2002 8 16 ASAA0240078 1 20020711 A 3350 8100022608 LIGHT BOEING 737 7374Q8 138447Q NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 774AS 25107 PDX - DURING LINE CHECK, FOUND TRACK LIGHTS INOPERATIVE AT ROW 21-24. REPLACED LIGHT ASSEMBLY, OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002081600180 20020816 00180 WP 2002 8 16 ASAA0280216 1 20020629 A 3397 0105610 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS FOUND DISCONNECTED AT ROW 28. RECONNECTED WIRING AT 28. LIG HTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002081600181 20020816 00181 NM 2002 8 16 AWXA200200693 1 20020805 A 3397 BR963180 WIRE BOEING 737 73733A 1384673 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 175AW 23634 PHX - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A BR OKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT ROW 14 LT. REMOVED AND REPLACED HARNESS, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002081700001 20020817 00001 SO 2002 8 17 C2XA02BT041 1 20020817 A 3350 1317 LAMP EMB 145 EMB145ER 3260211 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14939 145030 BTV---CO3398, DURING SERVICE CHECK MAINTENANCE FOUND THE AFT OVERHEAD AISLE EMERGENCY LIGHT TO BE INOPERATIVE.....REMOVE D AND REPLACED THE LAMP IN THE AISLE OVERHEAD EMERGENCY LIGHT. OPS.CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2002081700002 20020817 00002 SO 2002 8 17 C2XA02BT043 1 20020815 A 2100 AE3007 ENGINE EMB 145 EMB145LR 3260212 SO #1 ENGINE ODOR A C2XA O A OTHER UNSCHED LANDING B O SMOKE/FUMES/ODORS/SPARKS OTHER CL CLIMB 1 SW 27 11551 145411 EWR---CO3516, CREW REPORTED, "VERY ACRID ODOR AND SMALL AMOUNT OF SMOKE FROM #1 PACK AFTER ENGINE BLEED SELECTED ON CLIM BOUT" MAINTENANCE FOUND EVIDENCE OF ENGINE COMPRESSOR WASH FLUID CAUSING ACRID SMELL RAN ENGINES IAW EMB145 MM 72-00-00. OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVCIE. CO3121, CREW REPORTED, "AIR RETURN DUE TO SMOKE IN CABIN AND COCKPIT AND LAV FIRE INDICATION." EWR MAINTENANCE INSPECTED ENGINES #1 AND #2 FOR OIL LEAKAGE AT ENGINE "0" BEARING NO LEAKS NO TED. RAN BOTH ENGINES AT POWER WITH BLEEDS ON FOR ONE HOUR. NO SMOKE IN CABIN OR COCKPIT AND NO LAV SMOKE INDICATION. RE FERENCE EMB145 MM 72-00-00. AIRCRAFT RELEASED FOR TEST FLIGHT PURPOSES. CO4366, AIRCRAFT TEST FLOWN SATISFACTORY. AIRCR 2 L 7 2 4T RT T00011AT 2002081900001 20020819 00001 NM 2002 8 19 S02425005 1 20020320 A 2500 7A146723 SLIDE RAFT BOEING 747 747400 NM PWA 4056 PW4056 NE 4L DOOR DAMAGED W SAJF O OTHER O OTHER IN INSP/MAINT 1 WP 03 28709 B18201 T/S CHK FOUND 4L DOOR SLIDE/RAFT LOOSEN NOT IN NORMAL POSITION. CHK FOUND SLIDE/RAFT UNTIED AND PNEUMATIC BOTTLE WAS NOT BEEN DISCHARGED.C/A:1.RPLD 4L DOOR SLIDE/RAFT IAW AMM 25-69-01. 2.PARTS LOAN FROM ANA. 3.RPLD LOANED PART WITH C AL SLIDE/RAFT AND PFMED DOOR OPER CHK OK. 4.INFORMED GRD AGENCY PAY MORE ATTENTION WHEN WORKING. 2 L 7 4 4F 4 F RT A20WE E24NE 2002081900002 20020819 00002 NM 2002 8 19 ANCF200200017 1 20020812 A 2781 TARGET BOEING 767 767284 1385184 NM PWA 4056 PW4056 NE LE SLATS OUT OF ADJUST W ANCF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 988AN 24742 EICAS MESSAGE LE SLAT ASYM, LEADING EDGE LIGHT ILLUMINATED WITH THE FLAP LEVER IN UP, BOTH FLAP POINTERS WERE IN 1/2. DU RING FLAP/SLAT RETRACTION ON CLIMB-OUT PHASE. PERFORMED PROCEDURE IAW FIM 27-81-00 PAGE 134 AND WAS ADJUSTED CLEARANCE AT SENSOR TARGET S-281 IAW AMM 27-88-01 PAGE 201. TEST WITH SATISFACTORY RESULTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002081900003 20020819 00003 NE 2002 8 19 CA020607013 2 20020607 A 7210 GEARBOX DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENG REDUCTION GB MAKING METAL W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 29094 13838 (CAN) LT ENGINE REDUCTION GEAR BOX REPLACED DUE TO INTERNAL COMPONENT MAKING METAL. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002081900004 20020819 00004 EA 2002 8 19 CA020715001 1 20020712 A 5341 2153103658 STRUCTURE CNDAIR CL215 CL2151A10 1900320 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACK FOUND AT UPPER ATTACH FASTENER HOLE DURING NDT REQUIRED BY AD 1997-07R2 WHOSE REQUIREMENTS ARE EVERY 415 FLI GHT HOURS OR 1500 WATER DROPS, WHICHEVER COMES FIRST. THIS AIRCRAFT HAD 1011 WATER DROPS SINCE THE LAST COMPLIANCE OF TH IS AD. IT WAS ACCOMPLISHED EARLY AS OTHER CL-215'S OF THE OPERATION WERE APPROACHING THE 1500 WATER DROP LIMIT OF THE AD AND IT WAS DECIDED TO ACCOMPLISH THE ADS ON ALL OF THE AIRCRAFT TO "ZERO" THE AD TO GET US THROUGH THE SUMMER FIRE SEAS ON. AN ALTERNATE MEANS OF COMPLIANCE(AMOC) TO THIS AD FOR THIS AIRCRAFT HAS BEEN REQUESTED. 2 H 7 2 4R RT A14EA 2002081900006 20020819 00006 EU 2002 8 19 CA020718005 1 20020707 A 3221 A1029E BOLT BAG JETSTM JETSTM3212 1500217 EU GARRTT TPE331 TPE33110U 01514 WP MCAULY 4HFR34 4HFR34C652 NE NLG SHEARED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) CAA AD 024-05-87 REQUIRES COMPLIANCE WITH BAE SB 53-A-JA870510. PART C OF THIS BULLETIN REQUIRES A 1600 CYCLE TOR QUE CHECK OF THE NLG RETRACT JACK ATTACH BOLTS. DURING THE CHECK AT THIS TIME ONE OF THE BOLTS SHEARED. ALL BOLTS WERE REPLACED WITH NEW. GOING BACK THROUGHT THE RECORDS IT APPEARS THAT THIS BOLT MAY BE AN ORIGINAL. AIRCRAFT TSN IS 1493 7.4 AND CSN 16568 2 L 7 2 4T 4 T RT BA15CAA E4WE 6 C 3PNE 2002081900008 20020819 00008 CE 2002 8 19 GLBA2002123 1 20020815 A 5600 SEALANT BEECH 1900 1900D 1154162 CE A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 257GL UE257 LOUD CRACKLING NOISE IN FLIGHT. DIVERTED A/C TO CYS / REMOVED EXCESSIVE SEALANT FROM FO.'S WINDSHIELD, AS REQUIRED 2 L 7 2 4T RT A24CE 2002111800012 20021118 00012 EU 2002 11 18 AWXA200200691 1 20020804 A 2910 S4340161001 SOLENOID VALVE AIRBUS 320 A320232 3930326 EU HYD SYSTEM LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 649AW 17193 803 PHX - AIR TURNBACK - FLT 0081 - AFTER TAKEOFF FROM PHX EN ROUTE TO BWI DURING CLIMB ECAM INDICATED LOSS OF YELLOW HYDRAU LIC PRESSURE AND FLUID. AIRCRAFT TURNED BACK TO PHX. MAINTENANCE FOUND THE 3150GP HYDRAULIC SOLENOID VALVE LEAKING AND REPLACED VALVE IAW 29-19-51-401. SERVICED YELLOW HYDRAULIC SYSTEM, PERFORMED ENGINE RUN, OPERATED BOTH HYDRAULIC SYSTE MS, LEAK AND OPERATIONAL CHECKS WERE GOOD. VENDOR TEARDOWN OF 3-2 WAY VALVE FOUND A DAMAGED SEAL ON THE PISTON CONFIRMI NG FAILURE OF UNIT. REPLACED SEALS, O-RINGS, PACKINGS, AND BACK-UP RINGS, RE-CERTIFIED UNIT IAW CMM 29-10-14. 2 L 7 2 4F RT A28NM 2002081900009 20020819 00009 NM 2002 8 19 AWXA200200692 1 20020802 A 2910 50606 SHUTTLE VALVE BOEING 737 737277 1384570 NM HYD SYSTEM FAULTY A AWXA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 28 188AW 22655 SLC - EMERGENCY LANDING - FLT 0454 - ON SHORT FINAL APPROACH AT SLC EN ROUTE FROM PHX LOST A-SYSTEM HYDRAULIC QUANTITY A ND PRESSURE. AIRCRAFT SHUT DOWN AND TOWED TO GATE. MAINTENANCE FOUND THE NR 1 THRUST REVERSER SHUTTLE VALVE HAD A BLOW N PLUG, REMOVED AND REPLACED THE NR 1 THRUST REVERSER SHUTTLE VALVE IAW BMM 78-34-22. SERVICED A-SYSTEM HYDRAULICS AND RAN ENGINE OPERATING THE NR 1 THRUST REVERSER AND FLIGHT CONTROLS, LEAK AND OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002081900011 20020819 00011 NM 2002 8 19 AALA20020899 1 20020616 A 2780 3941001003 SOLENOID VALVE BOEING 737 737823 13844BZ NM L/E SLAT MALFUNCTIONED A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 908AN 29510 MIA - FLT 1343 - MIA-HOU - EN ROUTE HOU, UPON FLAP RETRACTION FROM 1 TO UP LEADING EDGE FLAPS TRANSIT AND SLED RED LIGHT REMAINED ILLUMINATED. EMERGENCY DECLARED. LANDED MIA WITHOUT INCIDENT. AFTER LANDING UPON FLAP RETRACTION L/E FLAPS TRANSIT AND SLAT LED'S 2, 3, 5, 6 REMAINED DOWN. REMOVED AND REPLACED UNCOMMANDED MOTION VALVE SOLENOID. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2002081900012 20020819 00012 NM 2002 8 19 AALA20020900 1 20020616 A 2780 SLAT BOEING 737 737823 13844BZ NM WING MALFUNCTIONED A AALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 21 921AN 29522 MIA - FLT 2127 - MIA-CUN - EN ROUTE CUN, AFTER TAKEOFF AND FLAP RETRACTION, LE FLAPS TRANSIT LIGHT REMAINED ON. ACCOMPL ISHED LE FLAPS TRANSIT ABNORMAL PROCEDURE. LIGHT WOULD NOTE EXTINGUISH ACCOMPLISHED (ASYMMETRICAL OR NO LEADING EDGE DE VICES) AND MADE UNEVENTFUL FLAPS 15 DEGREES LANDING. ALL HYDRAULIC PRESSURES AND QUANTITIES NORMAL. TROUBLESHOOTING IN PROGRESS. (M) 2 L 7 2 4F RT A16WE 2002081900014 20020819 00014 NM 2002 8 19 ASAA0210040 1 20020115 A 5210 69101402 BRACKET BOEING 737 737290C 138448V NM L1 DOOR BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, FOUND UPPER HINGE COVER BRACKET BROKEN CAUSING THE L1 DOOR TO BE DIFFICULT TO CLOSE. RE MOVED AND REPLACED BRACKET, THEN DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2002081900015 20020819 00015 NM 2002 8 19 ASAA0210065 1 20020318 A 5320 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BS 792, STRINGER 19L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2002081900016 20020819 00016 NM 2002 8 19 ASAA0210104 1 20020511 A 5310 6546551 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 807, RBL 8, RBL 15 CORRODED. REPAIRED SHEAR TIE PER SRM. (M) 2 L 7 2 4F A16WE 2002081900017 20020819 00017 NM 2002 8 19 ASAA0210105 1 20020511 A 5313 BAC1498158 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 26L AT BS 907 CORRODED. REPAIRED STRINGER PER SRM. (M) 2 L 7 2 4F A16WE 2002081900018 20020819 00018 NM 2002 8 19 ASAA0210106 1 20020513 A 5311 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 500, STRINGER 22L-23L DENTED. REPAIRED FRAME DENT PER SRM. (M) 2 L 7 2 4F A16WE 2002081900019 20020819 00019 NM 2002 8 19 ASAA0210107 1 20020513 A 5522 6576782 SKIN PANEL BOEING 737 737290C 138448V NM ELEVATOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT ELEVATOR STATION 135.79, DENTED. REPAIRED ELEVATOR SKIN DENT PER SR M. (M) 2 L 7 2 4F A16WE 2002081900020 20020819 00020 NM 2002 8 19 ASAA0210108 1 20020513 A 5311 6546596 FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 727B, STRINGER 20L-22L CORRODED. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F A16WE 2002081900021 20020819 00021 NM 2002 8 19 ASAA0210109 1 20020513 A 5311 6546559 FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 927, STRINGER 22L-25L CORRODED. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F A16WE 2002081900022 20020819 00022 NM 2002 8 19 ASAA0210110 1 20020513 A 5313 65C25124 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 28L AT BS 375 CORRODED. REPAIRED STRINGER PER SRM. (M) 2 L 7 2 4F A16WE 2002081900023 20020819 00023 NM 2002 8 19 ASAA0210111 1 20020513 A 5311 65622061 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 400, STRINGER 20L-24L DENTED. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F A16WE 2002081900024 20020819 00024 NM 2002 8 19 ASAA0210112 1 20020513 A 5311 6546555 FRAME BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 867, STRINGER 24L DENTED. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F A16WE 2002081900025 20020819 00025 NM 2002 8 19 ASAA0210113 1 20020514 A 5313 6573743 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 27L AT BS 1009 CORRODED. REPAIRED STRINGER PER SRM. (M) 2 L 7 2 4F A16WE 2002081900026 20020819 00026 NM 2002 8 19 ASAA0210135 1 20020528 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING SCHEDULED MAINTENANCE CHECK, FOUND EMERGENCY EXIT SIGN ABOVE L2 DOOR ILLUMINATED. REMOVED AND REPLACED REM OTE ASSEMBLY BATTERY, THEN SIGN TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002081900027 20020819 00027 NM 2002 8 19 ASAA0210138 1 20020601 A 5315 6546568114 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 1016, LBL 6, LBL 10 CORRODED. REPAIRED FLOORBEAM PER SRM. (M) 2 L 7 2 4F RT A16WE 2002081900028 20020819 00028 NM 2002 8 19 ASAA0210139 1 20020601 A 5330 SKIN PANEL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 378, STRINGER 28L-28R CRACKED. REPAIRED SKIN PANEL PER EA. (M) 2 L 7 2 4F RT A16WE 2002081900029 20020819 00029 NM 2002 8 19 ASAA0240005 1 20020111 A 5330 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 783AS 25114 PAE - FOUND SCRATCHES ON EXTERNAL SKIN BS 917-938 BETWEEN STRINGER 17R AND STRINGER 18R. REPAIRED IAW ASA EA. (M) 2 L 7 2 4F RT A16WE 2002081900030 20020819 00030 NM 2002 8 19 ASAA0240014 1 20020214 A 5320 654795710 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 PAE - DURING C-CHECK, FOUND AFT CARGO BAY DOOR CUTOUT STRUCTURE U-CHANNEL HAS AREAS OF CORROSION BS 796-847, RBL 28 AND WL 155. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002081900031 20020819 00031 NM 2002 8 19 ASAA0240015 1 20020212 A 5330 65C32359 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 PAE - DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED ON INTERIOR SKIN AT BS 500F, WL 149 AND STRINGER 27R. REPAIRED IAW S RM. (M) 2 L 7 2 4F RT A16WE 2002081900032 20020819 00032 NM 2002 8 19 ASAA0240016 1 20020214 A 5315 6546811 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 PAE - DURING C-CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 45 TO RBL 25 AND WL 207. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002081900033 20020819 00033 NM 2002 8 19 ASAA0240033 1 20020319 A 5320 65479573 THRESHOLD BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 762AS 25099 PAE - DURING C-CHECK, FOUND THRESHOLD AT AFT CARGO DOOR HAS CORROSION ON WEB AT STATION 794-847 AND RBL 21-28. REMOVED AND REPLACED WEB IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002081900034 20020819 00034 NM 2002 8 19 ASAA0240054 1 20020522 A 3397 8100022601 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 764AS 25101 SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTING AT ROW 18 INOPERATIVE. RECONNECTED WIRE, OPERATIONAL CHECKED NORMAL . (M) 2 L 7 2 4F RT A16WE 2002122000009 20021220 00009 CE 2002 12 20 GLBA2002124 1 20020816 A 7797 A20495M SHIELD BEECH 1900 1900D 1154162 CE FF XMITTER WIRE DAMAGED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 254GL UE254 LT ENGINE TORQUE FLUCTUATION, FUEL FLUCTUATION, FLT CREW ADVISED TO RETURN TO DEN, MX DETERMINED LT FUEL FLOW TRANSMITTE R CAUSING INDICATION FLUCUATIONS, PLACED BOTH ON MEL A/C RETURNED TO SERVICE, R&R WIRE SHIELD OPS CHECK OK 2 L 7 2 4T RT A24CE 2002081900035 20020819 00035 NM 2002 8 19 C1HA200292030 1 20020817 A 3350 900835A BATTERY BOEING 727 727212 138407G NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 292AS 21458 L-2 DOOR EMERGENCY LIGHT INOPREMOVED AND REPLACED BATTERY IAW M/M 33-50-00 OPS CHECK GOOD 2 L 7 3 4F A3WE 2002081900036 20020819 00036 CE 2002 8 19 GLBA2002125 1 20020817 A 3110 6226137001 TRANSMITTER BEECH 1900 1900D 1154162 CE A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 NM 03 219GL UE219 NAV 2 FAILED / DIVERTED A/C TO CYS, MX R&R #2 NAV RECEIVER, OPS CKD. GOOD A/C RETURNED TO SERVICE 2 L 7 2 4T RT A24CE 2002081900038 20020819 00038 NM 2002 8 19 ASAA0240058 1 20020527 A 3233 65C330325 ARM BOEING 737 737490 1384715 NM LT MLG DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 703AS 28893 SEA - DURING LINE CHECK, FOUND LEFT MAIN LANDING GEAR ACTUATOR BEAM ARM ASSEMBLY TO HAVE A DISCONTINUITY. REMOVED AND R EPLACED LEFT MLG ACTUATOR BEAM ARM ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 2002081900039 20020819 00039 NM 2002 8 19 ASAA0240059 1 20020531 A 5730 SKIN BOEING 737 7374Q8 138447Q NM LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 769AS 25103 SEA - DURING CHECK, FOUND LEFT WING FIXED LEADING EDGE CRACKED JUST INBOARD OF PYLON AT K-FLAP LOCATION. REPAIRED IAW W ITH EA. (M) 2 L 7 2 4F RT A16WE 2002081900040 20020819 00040 NM 2002 8 19 ASAA0240060 1 20020601 A 2810 65C267143 SKIN BOEING 737 737490 1384715 NM CENTER TANK GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 792AS 28887 JNU - DURING CHECK, FOUND GAUGE IN CENTER FUEL TANK SKIN ABOVE RIGHT PACK TURBO FAN VALVE. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2002081900041 20020819 00041 NM 2002 8 19 ASAA0240061 1 20020603 A 5311 654795576 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 32235 PAE - DURING SI CHECK, FOUND CORROSION ON AFT CARGO BAY FRAME AT BS 787 RBL 20 AND WL 160. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002081900042 20020819 00042 NM 2002 8 19 ASAA0240062 1 20020603 A 5210 50794594 DOOR FRAME BOEING 737 7374S3 1384711 NM L1 DOOR CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 PAE - DURING SI CHECK, FOUND L1 DOOR FORWARD FRAME CHAFED JUST ABOVE 4TH STOP PIN FROM THE TOP. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2002081900043 20020819 00043 NM 2002 8 19 ASAA0240063 1 20020603 A 5330 6545866711 SKIN BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 PAE - DURING SI CHECK, FOUND SKIN BENEATH MARKER BEACON ANTENNA IS CORRODED AT BS 625, WL 148.5 AND BL 00. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2002081900044 20020819 00044 NM 2002 8 19 ASAA0240064 1 20020603 A 5330 SKIN BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 PAE - DURING SI CHECK, FOUND SKIN BENEATH MARKER BEACON ANTENNA IS CORRODED AT BS 510, WL 148.5 AND BL 00. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2002081900045 20020819 00045 NM 2002 8 19 ASAA0240067 1 20020603 A 5230 654692110 SKIN BOEING 737 7374S3 1384711 NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 PAE - DURING SI CHECK, FOUND FORWARD CARGO DOOR REQUIRED RESKIN DUE TO NUMEROUS OUT OF LIMIT DENTS. REMOVED AND REPLACE D FORWARD CARGO DOOR EXTERNAL SKIN IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002081900046 20020819 00046 WP 2002 8 19 ASAA0280069 1 20020311 A 2597 D29982107 WIRE HARNESS DOUG DC9 DC983 3022083 WP R1 DOOR FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 977AS 32719 53453 OAK - DURING C-CHECK, FOUND FORWARD SERVICE R1 DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLI DE. SYSTEM CHECKED OK. (M) 2 L 7 2 4F RT A6WE 2002081900047 20020819 00047 WP 2002 8 19 GTIA020805 1 20020623 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND MID PIT HAS CORROSION AT FORWARD CARGO FITTING STATION 636 RBL 6 INCHES. REMOVED DAMAGED CARGO FITTING. HO LES LOCATED AND DRILLED ON NEW FITTING. INSTALLED NEW FITTING. (M) 2 L 7 2 4F A6WE 2002081900048 20020819 00048 WP 2002 8 19 GTIA020806 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 160-196 LBL 45, FLOORBOARD SUPPORT IS CORRODED. REMOVED FLOORBOARD SUPPORT. FABRICATED FLOOR SUPPO RT. INSTALLED FLOOR BOARD SUPPORT. (M) 2 L 7 2 4F A6WE 2002081900049 20020819 00049 WP 2002 8 19 GTIA020807 1 20020624 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 160 LBL 14-42 1 INCH ABOVE SUB FLOOR, LOWER PANEL ANGLE HAS EXFOLIATION CORROSION. REMOVED LOWER PA NEL ANGLE AT STATION 160 LBL 14-42. FABRICATED NEW ANGLE. INSTALLED FABRICATED ANGLE. (M) 2 L 7 2 4F A6WE 2002081900050 20020819 00050 WP 2002 8 19 GTIA020808 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 160 LBL 7 TO LBL 56 FLOORBOARD SUPPORT HAS AREAS OF CORROSION. REMOVED FLOOR BOARD SUPPORT FROM STA TION 160 LBL 7 TO LBL 56. FABRICATED FLOOR BOARD SUPPORT STATION 160 LBL 7 TO LBL 56. INSTALLED FLOOR SUPPORT AT STATI ON 160 LBL 7 LBL 56. (M) 2 L 7 2 4F A6WE 2002081900051 20020819 00051 WP 2002 8 19 GTIA020809 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 196 LBL 14-43 FLOORBOARD SUPPORT IS CORRODED. REMOVED FLOOR BOARD SUPPORT. FABRICATED FLOOR BOARD SUPPORT. INSTALLED FABRICATED SUPPORT. (M) 2 L 7 2 4F A6WE 2002081900052 20020819 00052 WP 2002 8 19 GTIA020810 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 196-256 LBL 14, FLOOR BOARD SUPPORT IS CORRODED. REMOVED FLOOR BOARD SUPPORT. LOCATED AND DRILLED. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002081900053 20020819 00053 WP 2002 8 19 GTIA020811 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 160-200 LBL 7, FLOOR BOARD SUPPORT IS CORRODED. REMOVED FLOOR BOARD SUPPORT FABRICATED NEW TRACK, F LOOR BOARD SUPPORT. (M) 2 L 7 2 4F A6WE 2002081900054 20020819 00054 WP 2002 8 19 GTIA020812 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 256 LBL 14-20 FLOOR BOARD SUPPORT IS CORRODED. REMOVED FLOOR SUPPORT. FABRICATED FLOOR BOARD SUPPO RT. INSTALLED SUPPORT. (M) 2 L 7 2 4F A6WE 2002081900055 20020819 00055 WP 2002 8 19 GTIA020813 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 160-200 RBL 45 FLOOR BOARD SUPPORT IS CORRODED. REMOVED FLOOR BOARD SUPPORT ANGLE FROM STATION 160- 200 RBL 45. FORMED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT ON STATION 160-200 RBL 45. (M) 2 L 7 2 4F A6WE 2002081900056 20020819 00056 WP 2002 8 19 GTIA020814 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 170 BL 0 FLOOR BOARD SUPPORT CORRODED. REMOVED CORRODED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT FR OM EXTRUSION. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002081900057 20020819 00057 WP 2002 8 19 GTIA020815 1 20020624 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 200-256 RBL 45 RIGHT OUTBOARD SEAT TRACK HAS AREAS OF CORROSION, NICKS AND BARE METAL. REMOVED AND INSTALLED SEAT TRACK AND SPLICE. (M) 2 L 7 2 4F A6WE 2002081900058 20020819 00058 WP 2002 8 19 GTIA020816 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 160-200 RBL 7, FLOOR BOARD SUPPORT IS CORRODED. REMOVED DAMAGED SUPPORT. FABRICATED SUPPORT TRACK. INSTALLED NEW FABRICATED TRACK ON STATION 160-200 RBL 7. (M) 2 L 7 2 4F A6WE 2002081900060 20020819 00060 NM 2002 8 19 CA020726012 1 20020725 A 2910 82910010195 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) HYDRAULIC LEAK IN NOSE AREA.NOSE LANDING GEAR DOOR SOLENOID VALVE LINE FOUND LEAKING. LINE REPLACED 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002081900061 20020819 00061 GL 2002 8 19 C2XA02IA172 2 20020814 A 7200 AE3007A1 ENGINE EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL POWER LOSS A C2XA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 27 14940 7824 149 145033 CAE310127 Flight 3927 - Crew reported that the #1 engine lost power in flight. The crew shut the engine down and had experienced n oticeable vibration after shutdown. The crew diverted to AUS and landed without incident. Maintenance removed and replac ed the affected engine, and the aircraft was returned to service. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002081900062 20020819 00062 SO 2002 8 19 C2XA02IA173 1 20020818 A 8011 35059105 STARTER ALLSN AE3007 EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FAILED A C2XA A UNSCHED LANDING Z SIGNIFICANT FAILURE REPORT CR CRUISE 1 SW 27 17984 10059 1376 CAE311029 145246 311029 Crew reported a momentary #2 engine fire indication. The aircraft returned to IAH and landed without incident. Maintenan ce inspected the right engine and found that the air turbine starter had failed causing heat damage to the engine outer bypass duct and lower cowling. Maintenance removed and replaced the #2 engine, #2 air turbine starter, and performed rep airs to the right lower cowl. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002081900067 20020819 00067 WP 2002 8 19 GTIA020817 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 200 RBL 8-45 FLOOR BOARD SUPPORT CORRODED. REMOVED FLOOR BOARD SUPPORT. LOCATED AND DRILLED. INST ALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002081900068 20020819 00068 WP 2002 8 19 GTIA020818 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - FOUND STATION 166 RBL 10, FLOOR BOARD SUPPORT CORRODED. REMOVED SUPPORT. FABRICATED NEW SUPPORT. INSTALLED SUPP ORT. (M) 2 L 7 2 4F A6WE 2002081900069 20020819 00069 WP 2002 8 19 GTIA020819 1 20020624 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 218-237 LBL 43 SUPPORT ANGLE CORRODED 1 EACH, FIGURE 8 HOLE. REMOVED SUPPORT ANGLE. HOLES LOCATED AND DRILLED ON NEW SUPPORT ANGLE. INSTALLED SUPPORT ANGLE. (M) 2 L 7 2 4F A6WE 2002081900071 20020819 00071 NM 2002 8 19 PCAA0207083 1 20020731 A 2910 O-RING DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM DAMAGED A PCAA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 13 810EX 308 PHL - FLIGHT 3957 CREW REPORTED NR 2 HYDRAULIC CONTENTS DROPPED TO ZERO AND NR 2 HYDRAULIC PRESSURE DROPPED TO ZERO AFTE R 5 MINUTES IN FLIGHT. NO PRESSURE FOR 10 MINUTES. MAINTENANCE INSPECTED NR 2 HYDRAULIC PUMP AND FOUND O-RING ON PRESS URE UNION DAMAGED. CASE DRAIN FILTERS WERE ALSO INSPECTED, WITH NO DEFECTS NOTED. O-RING WAS REPLACED. GROUND RUN-UP GOOD. NO LEAKS FOUND. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081900072 20020819 00072 EU 2002 8 19 PNSA020706 1 20020728 A 1430 FASTENER SAAB SF340 340B 7860101 EU TAIL CONE LOOSE A PNSA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 AL 03 675PA 340B206 ON CLIMBOUT FROM ANC AN UNUSUAL VIBRATION WAS FELT IN CONTROL YOKE AND RUDDER PEDALS. AIRCRAFT RETURNED TO ANC. MAINTE NANCE FOUND TAIL CONE ACCESS PANEL 317AB FORWARD TWO CAM LOCK FASTENERS LOOSE AND HANDLE FOR PANEL WAS STOWED WHICH MADE PANEL APPEARED INSTALLED CORRECTLY TO FLIGHT CREW ON PREFLIGHT. PANEL WAS RESECURED AND AIRCRAFT INSPECTED FOR DAMAGE WITH NONE FOUND FROM LOOSE PANEL. 2 L 7 2 4T RT A52EU 2002081900073 20020819 00073 NM 2002 8 19 DHL2002705011 1 20020816 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 705DH 19191 1) #1 ENGINE FIRE LOOP WILL NOT TEST. 2) R&R #1 ENG FIRE LOOP PER M/M 26-11-00. 2 L 7 3 4F A3WE 2002081900074 20020819 00074 NM 2002 8 19 QXEA0201059 1 20020724 A 6120 78249017 PCU DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE MALFUNCTIONED A QXEA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 09 359PH * 514 PDX- NR 2 ENGINE LOST 20 PERCENT TORQUE ON CLIMBOUT. NO CAUTION LIGHTS ILLUMINATED. ALL ENGINE PARAMETERS APPEARED NOR MAL WITH THE EXCEPTION OF NL WHICH WAS ABOUT 7 PERCENT LOWER THAN NR 1. RETURNED TO FIELD. AIRCRAFT LANDED WITHOUT INC IDENT. REMOVED AND REPLACED NR 2 PCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081900075 20020819 00075 NM 2002 8 19 QXEA0201061 1 20020724 A 3397 WIRE DHAV DHC8 DHC8202 2809007 NM CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 349PH 486 SEA- EMERGENCY FLOOR PATH LIGHTS ARE INOPERATIVE AT ROW 7. INSPECTED AND FOUND BROKEN WIRE AT PLUG 3352-P9. REPAIRED W IRE WITH SEAL SPLICE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081900076 20020819 00076 NM 2002 8 19 QXEA0201093 1 20020727 A 2611 SMOKE WARNING DHAV DHC8 DHC8202 2809007 NM COCKPIT FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 374PH 528 SEA- ON TAXI OUT SMOKE WARNING LIGHT ILLUMINATED WITH NO MASTER WARNING LIGHTS. RETURNED TO GATE. NO SMOKE PRESENT IN AFT CARGO BAY AFTER SHUTDOWN. NR 1 & 2 SMOKE DETECTORS TEST GOOD. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081900077 20020819 00077 NM 2002 8 19 UPS02439096 1 20020804 A 5340 BAC15201545 SEAT TRACK BOEING 747 747212B 1384886 NM M/D CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C M/D- BS2278 LBL 33 SEAT TRACK CROWN CORR. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040" X 1" X 2" EXCEED SRM 53-10-01 FIG 1 LIMITS. FOR REPLACEMENT REFER TO SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002081900078 20020819 00078 NM 2002 8 19 UPS02439097 1 20020804 A 5310 WEB BOEING 747 747212B 1384886 NM FWD CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C FWD CARGO - STA 900 (LBL 46", BELOW FLOOR 6") FRAME WEB FOUND CRACK AS MARKED. REPAIRED WEB AT FWD CARGO STA 900 LBL 46" AS PER SRM 51-40-02. 2 L 7 4 4F A20WE 2002081900079 20020819 00079 NM 2002 8 19 UPS02439101 1 20020804 A 5310 141U11074 WEB BOEING 747 747212B 1384886 NM BS 320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C RH BS 320 NOSE W/W VERTICAL BEAM WEB ONE INSULATION BLANKET STANDOFF HOLE CRACK FOUND APPROX 7/8" LON G AS MARKED. (WL 160 TO 170) VERTICAL BEAM WEB REPLACED AS PER DWG 624U0005 SHEET 4 AND SRM 51-10 -01 PG 8. 2 L 7 4 4F A20WE 2002081900080 20020819 00080 EA 2002 8 19 CA020729010 1 20020717 A 5320 21531036 ANGLE CNDAIR CL215 CL2151A10 1900320 EA HAMSTD 43E 43E60 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ACCOMPLISHMENT OF AD CF-97-07R2 CRACKS WERE NOTED ON BOTH THE LT AND RT AFT OUTBD WING TO FUSELAGE ATTACH A NGLES. TOTAL DOOR DROPS WERE 11655 AND TOTAL LANDINGS WERE 1711. 2 H 7 2 4R RT A14EA 6 C P871 2002081900081 20020819 00081 NE 2002 8 19 QXEA0201094 2 20020727 A 7320 VALVE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 ENGINE DIRTY A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 359PH 514 PSC- WHILE NR 2 ENGINE RUNNING AND STARTING NR 1 ENGINE WHITE SMOKE BEGAN TO FILL THE COCKPIT. CLEANED DIRTY DEPOSITS F ROM P2.5/P3 SWITCHING VALVE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002081900082 20020819 00082 EU 2002 8 19 QXEA0201097 1 20020727 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 BOI- EXIT SIGN AT PASSENGER CABIN LINTEL HAS SEVERAL LAMPS INOPERATIVE. REPLACED EXIT SIGN. OPERATIONAL CHECK GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002081900083 20020819 00083 EU 2002 8 19 QXEA0201100 1 20020730 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 PDX- FORWARD EVACUATION EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REMOVED AND REPLACED FORWARD CABIN EXIT SIGN ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002081900084 20020819 00084 NM 2002 8 19 QXEA0201102 1 20020803 A 5210 85210263101 STRUT DHAV DHC8 DHC8202 2809007 NM PAX DOOR DEFECTIVE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 360PH 515 SEA- PASSENGER CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. REMOVED AND REPLACED LOWER GAS SPRING STRUT. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081900086 20020819 00086 EA 2002 8 19 QXEA0201105 1 20020803 A 5730 ACCESS PANEL CNDAIR CL600 CL6002C10 1390015 EA LT WING DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 10041 PDX - DENT NOTED AT FIXED ACCESS PANEL 521AT, LEFT HAND WING. INSTALLED LEADING EDGE 521AT ON THE LEFT HAND WING IAW CR J-700 MM 57-41-05, PAGES 426-428. 2 L 7 2 4F RT A21EA 2002081900088 20020819 00088 SO 2002 8 19 C2XA02CL171 1 20020814 A 2530 CBC16707 RECEPTACLE EMB 145 EMB145LR 3260212 SO GALLEY MELTED A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 13550 145575 CLE FLIGHT# 2950 THE CREW REPORTED A STRONG BURNING RUBBER ODOR NEAR THE FRONT OF THE AIRCRAFT.MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND HOT JUG RECEPTACLE.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002081900089 20020819 00089 GL 2002 8 19 C2XA02CL172 2 20020815 A 7200 AE3007AIP ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LEFT PYLON ODOR A C2XA O OTHER O OTHER CL CLIMB 1 SW 27 22909 2776 145459 CAE311887 CLE FLIGHT#4387 THE CREW REPORTED SMOKE IN CABIN DURING TEST FLIGHT FOR A CHRONIC SMOKE ODOR IN CABIN.A EMERGENCY WAS DE CLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE #1 ENGINE.OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002081900090 20020819 00090 NM 2002 8 19 QXEA0201106 1 20020804 A 6123 SWITCH DHAV DHC8 DHC8202 2809007 NM COCKPIT DIRTY A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 355PH 500 LWS- ABORTED TAKEOFF DUE TO AUTOFEATHER FAILED TO ARM. BULB CHECKED OKAY. CLEANED POWER LEVER SWITCHES. NO PARTS REPL ACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081900091 20020819 00091 NM 2002 8 19 QXEA0201107 1 20020805 A 6123 954215B653323 SWITCH DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS MALFUNCTIONED A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 355PH 500 LWS- ABORTED TAKEOFF DUE TO NR 1 AUTOFEATHER DOES NOT TEST. REMOVED AND REPLACED ALT FEATHER MICRO SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081900092 20020819 00092 NM 2002 8 19 QXEA0201108 1 20020804 A 2422 DH103024600CS INVERTER DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTIONED A QXEA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION IN INSP/MAINT 1 NM 09 351PH 11160 11160 490 PDX- AUX INVERTER CAUTION LIGHT IS ILLUMINATED WITH SMOKE IN THE FLIGHT DECK. REMOVED AND REPLACED AUX INVERTER. OPERA TIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081900093 20020819 00093 2002 8 19 QXEA0201110 4 20020805 A 2210 WARNING SYSTEM BOMBDR DHC8 DHC8401 1390041 NM COCKPIT ACTIVATED A QXEA K NONE J WARNING INDICATION CR CRUISE 1 NM 09 406QX 4048 SEA- AUTO TRIM FAIL. INFLIGHT FAILURE OF PITCH TRIM. CLEARED CAUTION LIGHT. OPERATIONAL CHECKED GOOD. NO FURTHER DEF ECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081900094 20020819 00094 NM 2002 8 19 QXEA0201111 1 20020806 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 374PH 7569 7569 528 SEA- SMOKE WARNING LIGHT ILLUMINATED IN CARGO HOLD. NO SIGN OF SMOKE WHEN OPENED CARGO DOOR. NO BLEED SMOKE, NO ELECTR ICAL OVERLOAD INDICATED, DC/AC METER. REMOVED AND REPLACED NR 1 CARGO SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002081900095 20020819 00095 EA 2002 8 19 QXEA0201143 1 20020809 A 3620 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ACTIVATED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 610QX 10033 FAT - CREW RETURNED TO FIELD WHEN A RIGHT BLEED DUCT WARNING WAS RECEIVED. MAINTENANCE INSPECTED THE AIRCRAFT AND COMPL IED WITH S/L CRJ700-SL-36-002. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 2 4F RT A21EA 2002081900096 20020819 00096 2002 8 19 SWAA021789 4 20020808 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002081900097 20020819 00097 NM 2002 8 19 SWAA021790 1 20020809 A 3350 604222 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY P ER MM. 2 L 7 2 4F A16WE 2002081900098 20020819 00098 NM 2002 8 19 SWAA021797 1 20020811 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICES CRACKED AT BS 360, STR 4R AND STR 4L. REMOVED AND REPLACED STR SPLI CES PER SRM. 2 L 7 2 4F RT A16WE 2002081900099 20020819 00099 NM 2002 8 19 SWAA021805 1 20020809 A 2530 4160001 COFFEEMAKER BOEING 737 7372H4 138448C NM GALLEY MALFUNCTIONED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 091SW 22963 SMOKE COMING FROM AFT GALLEY COFFEEMAKER. REMOVED AND REPLACED COFFEEMAKER PER MM. 2 L 7 2 4F A16WE 2002081900100 20020819 00100 NM 2002 8 19 SWAA021813 1 20020811 A 3350 65C34691 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW NR 19 ABC. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002081900101 20020819 00101 NM 2002 8 19 VNAA0207025 1 20020718 A 3240 BRAKE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MLG INOPERATIVE A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 462PS 3084 THE CREW REPORTED THAT THE FIRST OFFICER'S BRAKES WERE INEFFECTIVE. MAINTENANCE INSPECTED AND BLED THE FIRST OFFICER'S BRAKES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS R ELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002081900102 20020819 00102 NM 2002 8 19 VNAA0207028 1 20020721 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 439JS 15605 60 3057 THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN AT ROW 11A WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIR CRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002081900103 20020819 00103 NM 2002 8 19 AWXA200200761 1 20020818 A 3350 BMS13311122 WIRE BOEING 737 7373B7 1384580 NM SEAT ROW 4 & 6 L BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 PHX - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 4 AND 6 L/H WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES AT SEAT ROWS 4 AND 6 L/H, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002081900104 20020819 00104 NM 2002 8 19 VNAA0207031 1 20020722 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 472PS 15141 86 3008 THE CREW REPORTED THAT THE FIRST ROW OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLAC ED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002081900105 20020819 00105 NM 2002 8 19 VNAA0207033 1 20020722 A 3250 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 3056 DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL MESSAGE AND ABORTED TAKEOFF. THE CREW CALLED MAINTENANCE C ONTROL AND WERE ABLE TO RESET THE SYSTEM. FLIGHT 4147 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURT HER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002081900106 20020819 00106 NM 2002 8 19 SABA020083 1 20020816 A 3350 6104789 BATTERY DHAV DHC8 DHC8103 1386005 NM A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 880CC 277 Flight 8680 from GSP to CLT : During post flight inspection the crew reported that the overhead emergency lights would n ot test. maintenance removed and replaced the batteres and system ops checked good. Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002082000001 20020820 00001 NE 2002 8 20 HEEA080507 2 20020729 A 7532 3043023 BLEED VALVE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE OSCILLATES E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 6559Z 36019 BLEED VALVE HAS INTERMITTENT OSCILLATION. 1 G 7 2 4U 4 U H4SW E22EA 2002082000002 20020820 00002 NE 2002 8 20 HEEA080508 2 20020729 A 7532 3043023 BLEED VALVE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE OSCILLATES E HEEA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SW 03 3893N 33010 BLEED VALVE DELIVERS ENGINE OSCILLATIONS. 1 G 7 2 4U 4 U H4SW E22EA 2002082000003 20020820 00003 NE 2002 8 20 HEEA080509 2 20020729 A 7532 3043023 BLEED VALVE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE FAILED E HEEA O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 SW 03 2258F 33073 BLEED VALVE PRODUCING HIGH ITT (100 DEGREES HIGHER) AND ENGINE N1 FLUCTUATIONS. 1 G 7 2 4U 4 U H4SW E22EA 2002082000004 20020820 00004 NE 2002 8 20 HEEA080510 2 20020729 A 7532 3043023 BLEED VALVE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE MALFUNCTIONED E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 2148K 36001 BLEED VALVE PRODUCING ENGINE SURGE. 1 G 7 2 4U 4 U H4SW E22EA 2002082000005 20020820 00005 NE 2002 8 20 HEEA080511 2 20020729 A 7532 312320301 BLEED VALVE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE MALFUNCTIONED E HEEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 03 2148K 36001 BLEED VALVE PRODUCING CONSTANT TORQUE SURGES IN FLIGHT. 1 G 7 2 4U 4 U H4SW E22EA 2002082000006 20020820 00006 NE 2002 8 20 HEEA080512 2 20020729 A 7532 312320301 BLEED VALVE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE MALFUNCTIONED E HEEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION HO HOVERING 1 SW 03 2148K 36001 BLEED VALVE PRODUCING OSCILLATION IN HOVER. 1 G 7 2 4U 4 U H4SW E22EA 2002082000007 20020820 00007 GL 2002 8 20 HEEA080513 2 20020730 A 7250 6899081 LINER BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL TURBINE SECTION BENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4180F CAE895574 DURING HOT SECTION INSPECTION THE LINER WAS FOUND BENT. 1 G 7 1 3U 3 U H2SW E1GL 2002082000008 20020820 00008 GL 2002 8 20 HEEA080514 2 20020731 A 7260 23063438 SEAL 6894171 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL HYDRODYNAMIC FAILED E HEEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 03 2270G CAG23167 3610 CAE836413 ENGINE REMOVED DUE TO SMOKE AND OIL COMING FROM GEARBOX VENT. UPON INSPECTION OF GEARBOX PARTS NOTED SEAL FAILED WITH L ARGE PIECE BROKEN AWAY FROM SPRING AREA. SCRAPPED SEAL. 1 G 7 1 3U 3 U H2SW E4CE 2002082000009 20020820 00009 GL 2002 8 20 HEEA080515 2 20020731 A 7260 23063371 SEAL BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL OIL SEPARATOR LEAKING E HEEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 03 3116P 639 51530 CAE890177 ENGINE REMOVED DUE TO FLUCTUATING OIL PRESSURE, SMOKE ON SHUTDOWN AND OIL BLOWING FROM GEARBOX. UPON INSPECTION OF GEAR BOX PARTS NOTED AIR OIL SEPERATOR HYDRODYNAMIC SEAL LEAKING. SCRAPPED SEAL. 1 G 7 1 3U 3 U H2SW E1GL 2002082000010 20020820 00010 NE 2002 8 20 HEEA080516 1 20020808 A 5310 7620323031541 BUSHING SKRSKY S76 S76A 8143006 NE PANEL OVERSIZED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 LT CABIN ROOF PANEL HAS OVERSIZED BUSHINGS. 1 G 7 2 3U H1NE 2002082000011 20020820 00011 SW 2002 8 20 HEEA080517 1 20020729 A 7910 3006084 OIL CAP BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE OIL STICKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 OIL FILLER CAP DIFFICULT TO REMOVE. SCRAPPED. 1 G 7 2 4U 4 U H4SW E22EA 2002082000012 20020820 00012 SW 2002 8 20 HEEA080518 1 20020729 A 2432 30126001 BATTERY BELL 412 412 1182202 SW MAIN DISCHARGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 107X 33113 MAIN BATTERY DEAD. REPLACED WITH SERVICEABLE BATTERY. 1 G 7 2 4U H4SW 2002082000013 20020820 00013 SW 2002 8 20 HEEA080519 1 20020729 A 2432 30126002 BATTERY BELL 412 412 1182202 SW MAIN DISCHARGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 MAIN BATTERY WEAK. WON'T CHARGE. REPLACED WITH SERVICEABLE BATTERY. 1 G 7 2 4U H4SW 2002082000014 20020820 00014 SW 2002 8 20 HEEA080521 1 20020729 A 7130 3016957 FIRESEAL BELL 412 412 1182202 SW ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 ENGINE FIRESEAL CRACKED. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002082000015 20020820 00015 SW 2002 8 20 HEEA080522 1 20020729 A 7160 3017393 TUBE BELL 412 412 1182202 SW AIR PRESSURE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 AIR PRESSURE TUBE IS DAMAGED AT FLARE. SCRAPPED. 1 G 7 2 4U H4SW 2002082000016 20020820 00016 SW 2002 8 20 HEEA080524 1 20020729 A 7722 3030083 COMPENSATOR BELL 412 412 1182202 SW ENGINE TRIM FLUCTUATES E HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 2149S 36002 ITT FLUCTUATING. SENT TO SEMCO INSTRUMENT COMPANY FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 2002082000018 20020820 00018 SW 2002 8 20 HEEA080526 1 20020729 A 7722 3030083 COMPENSATOR BELL 412 412 1182202 SW ENGINE TRIM DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 ENGINE TRIM COMPENSATOR WILL NOT ADJUST. 1 G 7 2 4U H4SW 2002082000019 20020820 00019 SW 2002 8 20 HEEA080527 1 20020729 A 7722 3030083A COMPENSATOR BELL 412 412 1182202 SW ENGINE TRIM INACCURATE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 TRIM COMPENSATOR GIVING INACCURATE READING. 1 G 7 2 4U H4SW 2002082000020 20020820 00020 SW 2002 8 20 HEEA080528 1 20020729 A 7722 3030083A COMPENSATOR BELL 412 412 1182202 SW ENGINE TRIM FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2149S 36002 TRIM COMPENSATOR GIVES NO ITT INDICATION. 1 G 7 2 4U H4SW 2002082000021 20020820 00021 NM 2002 8 20 VNAA0208018 1 20020812 A 5200 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 458PS 3068 DURING TAKE OFF, THE CREW RECEIVED A DOOR SWITCH FAIL AND A PROXI SYSTEM FAIL CAS MESSAGE AND ABORTED TAKE OFF. MAINTEN ANCE INSPECTED AND CLEANED THE PROXI SENSOR AND RERACKED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00 . OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000022 20020820 00022 NM 2002 8 20 VNAA0208024 1 20020818 A 3200 870004MODB PSEU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 440JS 16394 1731 3058 ENROUTE, THE CREW RECEIVED A PROXY SYSTEM AND A PROXY SYSTEM WEIGHT ON WHEELS MESSAGE. THE CREW CALLED MAINTENANCE AND THE DECISION WAS MADE TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENA NCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000023 20020820 00023 NM 2002 8 20 SWAA021835 1 20020814 A 5230 6547952524 DOOR BOEING 737 737301 1384611 NM AFT CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED C3 CHECK, FOUND AFT CARGO DOOR CRACKED AT FWD END BETWEEN 2ND AND 3RD STOPS. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 2002082000024 20020820 00024 2002 8 20 SWAA021837 4 20020813 A 2565 D31354 SLIDE BOEING 737 737301 1384611 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED BC3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE NYLON CORD HANGING OUT OF GIRT AREA. STOWED NYLON C ORD PER MM. 2 L 7 2 4F RT A16WE 2002082000025 20020820 00025 2002 8 20 SWAA021838 4 20020814 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 416WN 32453 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002082000026 20020820 00026 NM 2002 8 20 SWAA021840 1 20020813 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 890, BETWEEN STR 24R AND STR 25R. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2002082000027 20020820 00027 NM 2002 8 20 SWAA021841 1 20020814 A 5314 6545866 KEELBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED SERVICE CHECK, FOUND RT KEEL BEAM LOWER CHORD CORRODED AT BS 500A PLUS 8, STR 28R. REPAIRED KEEL BEAM LOWER CHORD PER SWA EA. 2 L 7 2 4F A16WE 2002082000028 20020820 00028 NM 2002 8 20 SWAA021842 1 20020814 A 5315 65C345371 FLOORBEAM BOEING 737 7375H4 138449D NM MID CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2002082000029 20020820 00029 NM 2002 8 20 SWAA021843 1 20020814 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR 8R AND STR 9R, BS 360 AND BS 827. REPAIRED F RAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2002082000030 20020820 00030 NM 2002 8 20 SWAA021844 1 20020814 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR 8L AND STR 9L, BS 380 AND BS 867. REPAIRED F RAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2002082000031 20020820 00031 2002 8 20 SWAA021828 4 20020812 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM AFT ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002082000032 20020820 00032 NM 2002 8 20 SWAA021829 1 20020812 A 5230 6547952 SKIN BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR OUTER SKIN CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002082000033 20020820 00033 NM 2002 8 20 SWAA021830 1 20020813 A 5753 6546435336 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED BC4 CHECK, FOUND RT AFT INBD T/E FLAP DELAMINATED AT INBD AFT END. REMOVED AND REPLACED RT AFT INBD T/ E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002082000034 20020820 00034 NM 2002 8 20 SWAA021832 1 20020813 A 5330 6545765 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002082000035 20020820 00035 NM 2002 8 20 SWAA021833 1 20020813 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 770SA 30589 EEPLS WIRES EXPOSED AT OVERWING EXIT. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002082000036 20020820 00036 SW 2002 8 20 HEEA080529 1 20020729 A 7920 3032247B FILTER BELL 412 412 1182202 SW P3 DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 P3 FILTER HAS A BENT BYPASS SPRING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002082000037 20020820 00037 SW 2002 8 20 HEEA080530 1 20020729 A 6310 3034508WFC ELEMENT BELL 412 412 1182202 SW C-BOX FILTER DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 CAUSED C-BOX FILTER TO BYPASS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002082000038 20020820 00038 SW 2002 8 20 HEEA080531 1 20020729 A 6310 3034508WFC ELEMENT BELL 412 412 1182202 SW C-BOX FILTER DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 CAUSING BYPASS TO POP. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002082000039 20020820 00039 SW 2002 8 20 HEEA080533 1 20020729 A 6310 3034508WFC FILTER BELL 412 412 1182202 SW COMB BOX CONTAMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 WHITE GLUE LIKE SUBSTANCE IN FILTER. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002082000040 20020820 00040 SW 2002 8 20 HEEA080534 1 20020729 A 6310 310893901 FILTER BELL 412 412 1182202 SW COMB BOX DIRTY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 COMBINING GEARGOX FILTER DIRTY. REPLACED WITH SERVICEABLE FILTER. 1 G 7 2 4U H4SW 2002082000041 20020820 00041 SW 2002 8 20 HEEA080537 1 20020729 A 7714 32005007 TACH GENERATOR BELL 412 412 1182202 SW ENGINE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 TACH GENERATOR FAILED TO FUNCTION. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002082000042 20020820 00042 SW 2002 8 20 HEEA080538 1 20020729 A 6700 3214M228 ARM BELL 412 412 1182202 SW FLIGHT CONTROLS BINDING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 FLIGHT CONTROL ARM BINDING AND CANNOT SET. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002082000043 20020820 00043 NE 2002 8 20 HEEA080539 2 20020729 A 7321 SERVO VALVE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE TCU LEAKING E HEEA K NONE K L FLUID LOSS NO TEST IN INSP/MAINT 1 SW 03 2148K A8414 36001 TORQUE SPLIT. TESTED UNIT AND FOUND SERVO VALVES LEAKING. REPLACED SERVO VALVE AND SERVO LEVER WITH REWORKED PART. UNI T TESTED SATISFACTORY. 1 G 7 2 4U 4 U H4SW E22EA 2002082000044 20020820 00044 NE 2002 8 20 HEEA080540 2 20020729 A 7321 32447066 CONTROL UNIT BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE TORQUE OSCILLATES E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 2148K 36001 BOTH ENGINES OSCILLATING TOGETHER 3 TO 4 PERCENT. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U 4 U H4SW E22EA 2002082000045 20020820 00045 NE 2002 8 20 HEEA080541 2 20020729 A 7321 SERVO VALVE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE TCU LEAKING E HEEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 03 3893N A31793 33010 LARGE TORQUE OSCILLATION. FOUND SERVO VALVES AND LEVER LEAKING AIR. CLEANED VALVES AND LEVER, RESET UNIT AND TESTED SAT ISFACTORY. 1 G 7 2 4U 4 U H4SW E22EA 2002082000046 20020820 00046 NE 2002 8 20 HEEA080542 2 20020729 A 7321 SERVO VALVE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE TCU LEAKING E HEEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 03 6559Z A65840 36019 ENGINE SURGE. FOUND SERVO VALVES LEAKING. PERFORMED 2500 HOUR INSPECTION. POLISHED SERVO VALVES AND RE-CALIBRATED UNIT . TESTED SATISFACTORY. 1 G 7 2 4U 4 U H4SW E22EA 2002082000047 20020820 00047 NE 2002 8 20 HEEA080543 2 20020729 A 7321 SERVO VALVE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE TCU LEAKING E HEEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 03 2148K A65985 36001 CAUSES TORQUE SPLITS AND ERRATIC CONTROL. ENGINES SURGING. FOUND SERVO VALVES LEAKING. REPLACED SERVO VALVES AND SERVO VALVE LEVERS. UNIT TESTED SATISFACTORY. 1 G 7 2 4U 4 U H4SW E22EA 2002082000048 20020820 00048 NE 2002 8 20 HEEA080544 2 20020729 A 7320 324473514 FUEL CONTROL BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE DAMAGED E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2148K 36001 LEAKING AT DOME WEEP HOLE. SPLIT UNIT AND INSPECTED TORQUE TUBE BORE. FOUND TORQUE TUBE BORE COATING FLAKING OFF. SENT MAIN BODY TO VENDOR FOR REPAIR. REASSEMBLED UNIT AFTER REPAIR AND FOUND NO LEAKING. UNIT TESTED SATISFACTORY. 1 G 7 2 4U 4 U H4SW E22EA 2002082000049 20020820 00049 SW 2002 8 20 HEEA080545 1 20020729 A 2840 384178103 SWITCH BELL 412 412 1182202 SW FUEL SYSTEM READS LOW E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 READS LOWER THAN IS ACTUALLY IN FUEL TANKS WHEN TESTING LEFT OR RIGHT. 1 G 7 2 4U H4SW 2002082000050 20020820 00050 SW 2002 8 20 HEEA080546 1 20020729 A 2841 384178103 SWITCH BELL 412 412 1182202 SW FUEL INDICATOR MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 WHEN SELECTING RIGHT POSITION GAUGE WILL NOT ALWAYS RETURN TO THE PREVIOUS GAUGE READING. IT MAY BE 100 LBS. LESS THEN IT MAY BE 50 LBS. LESS. SOMETIMES IT WILL SLOWLY CREEP BACK TO THE PREVIOUS FUEL INDICATION. IT CAUSES THE GAUGE TO RE AD 300 LBS. LOW. SENT TO MASCO FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 2002082000051 20020820 00051 SW 2002 8 20 HEEA080547 1 20020729 A 2841 393008040 INDICATOR BELL 412 412 1182202 SW FUEL QTY FLUCTUATES E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893N 33010 FLUCTUATES ABOUT 50 POUNDS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002082000052 20020820 00052 SW 2002 8 20 HEEA080548 1 20020729 A 7714 39433339002 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH READS LOW E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 ALL NEEDLES ON TRIPLE TACH READ 200 LOW. 1 G 7 2 4U H4SW 2002082000053 20020820 00053 SW 2002 8 20 HEEA080549 1 20020729 A 2432 39563001 BATTERY PACK BELL 412 412 1182202 SW MAIN DISCHARGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 7128R 36007 MAIN AIRCRAFT BATTERY PACK WEAK. 1 G 7 2 4U H4SW 2002082000054 20020820 00054 SW 2002 8 20 HEEA080550 1 20020729 A 2432 39563001 BATTERY PACK BELL 412 412 1182202 SW MAIN DISCHARGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893L 33006 MAIN AIRCRAFT BATTERY PACK DEAD. 1 G 7 2 4U H4SW 2002082000055 20020820 00055 SW 2002 8 20 HEEA080551 1 20020729 A 2432 39563001 BATTERY PACK BELL 412 412 1182202 SW MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 107X 33113 MAIN AIRCRAFT BATTERY PACK SLOW TO CHARGE. 1 G 7 2 4U H4SW 2002082000056 20020820 00056 SW 2002 8 20 HEEA080552 1 20020729 A 2432 39563001 BATTERY PACK BELL 412 412 1182202 SW MAIN DISCHARGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22608 33075 MAIN AIRCRAFT BATTERY PACK DEAD. REPAIRED. 1 G 7 2 4U H4SW 2002082000057 20020820 00057 SW 2002 8 20 HEEA080553 1 20020729 A 2432 39563001 BATTERY PACK BELL 412 412 1182202 SW MAIN DISCHARGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22608 33075 MAIN AIRCRAFT BATTERY PACK WEAK. REPAIRED. 1 G 7 2 4U H4SW 2002082000058 20020820 00058 SW 2002 8 20 HEEA080554 1 20020729 A 2432 39563001 BATTERY PACK BELL 412 412 1182202 SW MAIN DISCHARGED E HEEA K NONE L G NO TEST MULTIPLE FAILURE IN INSP/MAINT 1 SW 03 2148K 36001 DISCHARGED MAIN AIRCRAFT BATTERY PACK CAUSED STANDBY ATTITUDE INDICATOR NOT TO TEST. REPAIRED. 1 G 7 2 4U H4SW 2002082000059 20020820 00059 2002 8 20 HEEA080555 4 20020729 A 3442 4000035 RADAR BELL 412 412 1182202 SW WX SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 107X 33113 WEATHER RADAR UNIT HAS A RANGE OF ONLY 3 MILES. FOUND OVEN INOPERATIVE. REPLACED OSCILLATOR CARD. ALIGNED, INSPECTED A ND BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002082000060 20020820 00060 2002 8 20 HEEA080556 4 20020729 A 3442 4000035 RADAR BELL 412 412 1182202 SW WX SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2148K 36001 WEATHER RADAR UNIT HAS NO SIDE TONE ON CHANNELS 1 & 2. FOUND UNIT HAS INTERMITTENT AUDIO ON CHANNEL NR 2. REPLACED POT R441. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002082000061 20020820 00061 2002 8 20 HEEA080557 4 20020729 A 3442 4000035 RADAR BELL 412 412 1182202 SW WX SYSTEM WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1202T 33112 WEATHER RADAR UNIT IS WEAK RECEIVING AND TRANSMITTING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002082000062 20020820 00062 2002 8 20 HEEA080558 4 20020729 A 3442 4000035010 RADAR BELL 412 412 1182202 SW WX SYSTEM DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893N 33010 LOOSE ITEM (RESISTOR) FOUND INSIDE OF WEATHER RADAR UNIT. REINSTALLED LOOSE RESISTOR R328. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 2002082000063 20020820 00063 2002 8 20 HEEA080560 4 20020729 A 3422 4020936903 GYRO BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2258F 33073 DIRECTIONAL GYRO WON'T SLAVE. 1 G 7 2 4U H4SW 2002082000064 20020820 00064 2002 8 20 HEEA080561 4 20020729 A 2211 4025008918 COMPUTER BELL 412 412 1182202 SW AFCS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2148K 36001 NR 1 AFCS KICKING IN PITCH, ROLL AND YAW. 1 G 7 2 4U H4SW 2002082000065 20020820 00065 2002 8 20 HEEA080562 4 20020729 A 2212 4030182901 SENSOR BELL 412 412 1182202 SW ALTITUDE CONTROL INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 107X 33113 ALTITUDE HOLD MODE INOPERATIVE. 1 G 7 2 4U H4SW 2002082000066 20020820 00066 2002 8 20 HEEA080563 4 20020729 A 2211 4033089901 COMPUTER BELL 412 412 1182202 SW AFCS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 142PH 33150 AFCS COMPUTER CAUSES AIRCRAFT TO CLIMB INSTEAD OF DESCENDING WHEN CAPTURING GLIDE SLOPE ON ILS. 1 G 7 2 4U H4SW 2002082000067 20020820 00067 2002 8 20 HEEA080564 4 20020729 A 2211 4033089901 COMPUTER BELL 412 412 1182202 SW AFCS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1202T 33112 AFCS COMPUTER MALFUNCTIONED, FLIGHT DIRECTOR WON'T HOLD HEADING. REPAIRED. 1 G 7 2 4U H4SW 2002082000068 20020820 00068 SW 2002 8 20 HEEA080565 1 20020729 A 6710 412001300105 BELLCRANK BELL 412 412 1182202 SW M/R GEARBOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 MAIN ROTOR GEARBOX BELLCRANK HAS WORN BEARINGS. REPAIRED. 1 G 7 2 4U H4SW 2002082000069 20020820 00069 SW 2002 8 20 HEEA080566 1 20020729 A 6320 412010182101 BEARING BELL 412 412 1182202 SW M/R GEARBOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 MAIN ROTOR GEARBOX HAS WORN BEARINGS. SCRAPPED. 1 G 7 2 4U H4SW 2002082000070 20020820 00070 SW 2002 8 20 HEEA080567 1 20020729 A 6320 412010182101 BEARING BELL 412 412 1182202 SW M/R GEARBOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 MAIN ROTOR GEARBOX HAS WORN BEARINGS. SCRAPPED. 1 G 7 2 4U H4SW 2002082000071 20020820 00071 SW 2002 8 20 HEEA080568 1 20020729 A 6320 412010182101 BEARING BELL 412 412 1182202 SW M/R GEARBOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 MAIN ROTOR GEARBOX HAS WORN BEARINGS. SCRAPPED. 1 G 7 2 4U H4SW 2002082000072 20020820 00072 SW 2002 8 20 HEEA080569 1 20020729 A 6320 412010182101 BEARING BELL 412 412 1182202 SW M/R GEARBOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 MAIN ROTOR GEARBOX HAS WORN BEARINGS. REPAIRED. 1 G 7 2 4U H4SW 2002082000073 20020820 00073 SW 2002 8 20 HEEA080570 1 20020729 A 6220 412010216105 BEARING BELL 412 412 1182202 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 9688 36001 MAIN ROTOR HAS WORN BEARINGS. REPAIRED. 1 G 7 2 4U H4SW 2002082000074 20020820 00074 SW 2002 8 20 HEEA080571 1 20020729 A 6710 BEARING BELL 412 412 1182202 SW BELLCRANK ASSY SEIZED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 BEARING SEIZED. REPAIRED. 1 G 7 2 4U H4SW 2002082000075 20020820 00075 SW 2002 8 20 HEEA080572 1 20020729 A 6220 412010100193FM HUB BELL 412 412 1182202 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 MAIN ROTOR HUB RED BLADE DAMPER UNSERVICEABLE. REPAIRED. 1 G 7 2 4U H4SW 2002082000076 20020820 00076 SW 2002 8 20 HEEA080573 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW SWASHPLATE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L RE0002 33006 SWASHPLATE GIMBAL RING BEARING WORN. REPAIRED. 1 G 7 2 4U H4SW 2002082000077 20020820 00077 SW 2002 8 20 HEEA080574 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW SWASHPLATE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 20493 RE0025 33073 SWASHPLATE GIMBAL RING BEARING WORN. REPAIRED. 1 G 7 2 4U H4SW 2002082000078 20020820 00078 SW 2002 8 20 HEEA080575 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK UNSTAKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N A1870 33002 MAIN ROTOR SHASHPLATE DRIVE LINK LOWER BEARING UNSTAKED. REPAIRED. 1 G 7 2 4U H4SW 2002082000079 20020820 00079 SW 2002 8 20 HEEA080576 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z A1917 36019 MAIN ROTOR SWASHPLATE DRIVE LINK BEARING WORN. REPAIRED. 1 G 7 2 4U H4SW 2002082000080 20020820 00080 SW 2002 8 20 HEEA080577 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S A2070 36002 MAIN ROTOR SWASHPLATE DRIVE LINK BEARING WORN. REPAIRED. 1 G 7 2 4U H4SW 2002082000081 20020820 00081 SW 2002 8 20 HEEA080578 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z A2071 36019 MAIN ROTOR SWASHPLATE DRIVE LINK BEARING WORN. REPAIRED. 1 G 7 2 4U H4SW 2002082000082 20020820 00082 SW 2002 8 20 HEEA080579 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 2479 A2257 33113 MAIN ROTOR SWASHPLATE DRIVE LINK BEARING WORN. REPAIRED. 1 G 7 2 4U H4SW 2002082000083 20020820 00083 SW 2002 8 20 HEEA080580 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z A2292 36019 MAIN ROTOR SWASHPLATE DRIVE LINK BEARING WORN. REPAIRED. 1 G 7 2 4U H4SW 2002082000084 20020820 00084 SW 2002 8 20 HEEA080581 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK UNSTAKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T A2363 33112 MAIN ROTOR SWASHPLATE DRIVE LINK LOWER BEARING UNSTAKED. REPAIRED. 1 G 7 2 4U H4SW 2002082000085 20020820 00085 SW 2002 8 20 HEEA080582 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D A2528 33076 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000086 20020820 00086 SW 2002 8 20 HEEA080583 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S A2607 36002 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000087 20020820 00087 SW 2002 8 20 HEEA080584 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D A2612 33076 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000088 20020820 00088 SW 2002 8 20 HEEA080585 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z A2615 36019 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000089 20020820 00089 SW 2002 8 20 HEEA080586 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z A2616 36019 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000090 20020820 00090 SW 2002 8 20 HEEA080587 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S A2718 36002 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000091 20020820 00091 SW 2002 8 20 HEEA080588 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S A2732 36002 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000092 20020820 00092 SW 2002 8 20 HEEA080589 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T A2932 33112 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000093 20020820 00093 SW 2002 8 20 HEEA080590 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T A2934 33112 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000094 20020820 00094 SW 2002 8 20 HEEA080591 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N A1340 33002 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000095 20020820 00095 SW 2002 8 20 HEEA080592 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z A1876 36019 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000096 20020820 00096 SW 2002 8 20 HEEA080593 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 A1944 33075 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000097 20020820 00097 SW 2002 8 20 HEEA080594 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N A1952 33002 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000098 20020820 00098 SW 2002 8 20 HEEA080595 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 A1956 33075 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000099 20020820 00099 SW 2002 8 20 HEEA080596 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S A1987 36002 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000100 20020820 00100 SW 2002 8 20 HEEA080597 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z A2025 36019 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000101 20020820 00101 SW 2002 8 20 HEEA080598 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z A2045 36019 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000102 20020820 00102 SW 2002 8 20 HEEA080599 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X A2158 33113 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000103 20020820 00103 SW 2002 8 20 HEEA080600 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z A2167 36019 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000104 20020820 00104 SW 2002 8 20 HEEA080601 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X A2191 33113 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000105 20020820 00105 SW 2002 8 20 HEEA080602 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 2642 A2311 33023 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000106 20020820 00106 SW 2002 8 20 HEEA080603 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D A2771 33076 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000107 20020820 00107 SW 2002 8 20 HEEA080604 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T A2825 33112 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. 1 G 7 2 4U H4SW 2002082000108 20020820 00108 SW 2002 8 20 HEEA080605 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T A2876 33112 BOLT STUCK IN LOWER BEARING OF MAIN ROTOR SWASHPLATE DRIVE LINK. REPAIRED. 1 G 7 2 4U H4SW 2002082000109 20020820 00109 SW 2002 8 20 HEEA080606 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW DRIVE LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T A2913 33112 MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARINGS. REPAIRED. 1 G 7 2 4U H4SW 2002082000110 20020820 00110 NM 2002 8 20 AWXA200200706 1 20020730 A 5320 65C320747 FLOOR SUPPORT BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOOR SUPPORT BETWEEN BS 986.5 AND BS 1006, RBL 21, LOCATION OF RT AFT LAVATORY INBOARD FORWARD MOUNT. MAINTENANCE REMOVED FLOOR SUPPORT BETWEEN BS 986.5 TO BS 1006, RBL 2; FABRICATED A NEW FLOOR SUPPORT, AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02 PG 10-11 AND SRM 51-40-05 PG 4-5. 2 L 7 2 4F RT A16WE 2002082000111 20020820 00111 SW 2002 8 20 HEEA080607 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW PITCH LINK TUBE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z A3439 36019 MAIN ROTOR PITCH LINK TUBE HAS WORN BEARINGS. REPAIRED. 1 G 7 2 4U H4SW 2002082000112 20020820 00112 NM 2002 8 20 AWXA200200707 1 20020801 A 5320 65C320747 FLOOR SUPPORT BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOOR SUPPORT BETWEEN BS 986.5 AND BS 1006, LBL 34. MAINTENANCE REMOVED FLOOR SUPPORT BETWEEN BS 986.5 TO BS 1006, LBL 34; FABRICATED A NEW FLOO R SUPPORT AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02 PG 10-11 AND SRM 51-40-05 PG 4-5. 2 L 7 2 4F RT A16WE 2002082000113 20020820 00113 SW 2002 8 20 HEEA080608 1 20020729 A 6230 BEARING BELL 412 412 1182202 SW PITCH LINK TUBE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z A3671 36019 MAIN ROTOR PITCH LINK TUBE HAS WORN BEARINGS. REPAIRED. 1 G 7 2 4U H4SW 2002082000114 20020820 00114 SW 2002 8 20 HEEA080609 1 20020729 A 6210 412015300109 BLADE BELL 412 412 1182202 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 9139 36003 MAIN ROTOR BLADE LOWER EROSION SHIELD PEELING OFF BEYOND LIMITS. 1 G 7 2 4U H4SW 2002082000115 20020820 00115 SW 2002 8 20 HEEA080610 1 20020729 A 6210 412015300109 BLADE BELL 412 412 1182202 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 800Y 5181 33134 MAIN ROTOR BLADE EROSION SHIELD ON LOWER SURFACE IS SEPARATED BEYOND LIMITS. 1 G 7 2 4U H4SW 2002082000116 20020820 00116 NM 2002 8 20 AWXA200200711 1 20020729 A 5310 6545855101 CREASE BEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF RT CREASE BEAM (INNER CHO RD) AT R-2 DOORWAY BS 950 - BS 986.5, RBL 66. MAINTENANCE REMOVED RT CREASE BEAM BETWEEN BS 950 TO BS 986.5, RBL 66; FA BRICATED A NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02 PG 3-4 AND DWG 65-45855. 2 L 7 2 4F RT A16WE 2002082000117 20020820 00117 SW 2002 8 20 HEEA080611 1 20020729 A 6320 412040006101 GEARBOX BELL 412 412EP 1182205 SW MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 412PH 2715 36140 CORROSION FOUND ON MAIN ROTOR GEARBOX. REPAIRED. 1 G 7 2 4U H4SW 2002082000118 20020820 00118 SW 2002 8 20 HEEA080612 1 20020729 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW NR 1 TORQUE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 107X 33113 TORQUE INDICATOR DOES NOT HAVE A NR 1 ENGINE INDICATION. 1 G 7 2 4U H4SW 2002082000119 20020820 00119 EU 2002 8 20 AWXA200200714 1 20020809 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 642AW 1929 584 LAS - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHTS WERE FOUND INOPERATIVE AT SEAT ROWS 13, 17, 19, AND 24. MAIN TENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (13WL) IAW AMM 33-51-38-401 AND MID CABIN POWER SUPPLY (11WL) B ATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002091000115 20020910 00115 NM 2002 9 10 AWXA200200716 1 20020812 A 2130 VFT300B00 VALVE AIRBUS A319 A319132 3930340 NM CABIN PRESSURE MALFUNCTIONED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 808AW 606 1088 EWR - ABORTED TAKEOFF - FLT 0688 - DURING TAKEOFF ROLL AT EWR EN ROUTE PHX ECAM INDICATED A VENT SKIN VALVE FAULT, WITH ASSOCIATED AVIONICS SYSTEM FAULT. REJECTED TAKEOFF AT 70 KTS. MAINTENANCE PERFORMED PROCEDURES FOR MEL 21-26-04, COND 1, EXTRACT VALVE INOPERATIVE. PARTS ORDERED. VENDOR BENCH TEST OF SKIN AIR VALVE WAS NO FAULT FOUND, UNIT WAS FUNCTION AL TESTED AND RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002082000120 20020820 00120 NM 2002 8 20 AWXA200200719 1 20020730 A 5320 65C320747 FLOOR SUPPORT BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT (INTERCOSTAL) B ETWEEN BS 986.6 AND BS 1006, RBL 33, AT LOCATION OF RT AFT LAVATORY OUTBOARD FORWARD MOUNT. MAINTENANCE REMOVED DAMAGED INTERCOSTAL BETWEEN BS 986.6 AND BS 1006, RBL 33. FABRICATED A NEW INTERCOSTAL AND INSTALLED REPAIR IAW B737-300 SRM 5 1-40-02 PG 11-12. 2 L 7 2 4F RT A16WE 2002082000121 20020820 00121 NM 2002 8 20 AWXA200200723 1 20020728 A 5310 655287846 CREASE BEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK HEAVY EXFOLIATION CORROSION WAS FOUND ON CREASE BEAM (INNER CHORD) AT L2 DOOR FRO M LT AFT LAVATORY TO DOORWAY DRAIN BS 967 - BS 986.5, LBL 66. MAINTENANCE REMOVED DAMAGED CREASE BEAM, LT AFT DRAIN PAN , 2 EACH STIFFENERS, AND 1 ATTACH ANGLE AT BS 967 - BS 986.5, LBL 66. FABRICATED AND INSTALLED A NEW CREASE BEAM, REINS TALLED LT AFT DRAIN PAN, 2 EACH STIFFENERS, AND 1 ATTACH ANGLE IAW B737-300 SRM 51-40-02 PG 3-4, 11 & 38. 2 L 7 2 4F RT A16WE 2002082000122 20020820 00122 NM 2002 8 20 AWXA200200724 1 20020728 A 5320 673535511 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER CLIP AT BS 947, STRINGER 12 LT. MAINTENAN CE REMOVED CRACKED STRINGER CLIP AT BS 947, STRINGER 12 LT. FABRICATED A NEW STRINGER CLIP, AND INSTALLED REPAIR IAW B7 37-300 SRM 51-40-02, PG 3-4, 10-11. 2 L 7 2 4F RT A16WE 2002082000123 20020820 00123 NM 2002 8 20 AWXA200200725 1 20020725 A 5347 655384420 CARGO TRACK BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK A CRACK WAS FOUND ON THE OUTBOARD SIDE OF AFT CARGO FLOOR TRACK FLANGE, BS 767, R BL 15. MAINTENANCE REMOVED DAMAGED SECTION OF FLOOR TRACK, FABRICATED A NEW SECTION OF FLOOR TRACK, AND INSTALLED REPAI R IAW B737-300 SRM 51-40-02, PG 2-4, 10-11, 16-19, 38, AND SRM 51-40-05 PG 4-5. 2 L 7 2 4F RT A16WE 2002082000124 20020820 00124 NM 2002 8 20 02231414 1 20020819 A 3350 2LA00593435 LIGHT DORNER DO32 DO328300 NM A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 414FJ 3169 During preflight inspection, the crew reported that the emergency exit sign above the aft service door was cracked in ha lf. The aircraft was ferried to a station where the required part was available. Maintenance personnel removed and rep laced the aft service door emergency exit sign. An operational check was satisfactory and the aircraft was returned to service. 2 H 7 2 4T RT A55NM 2002082000125 20020820 00125 NM 2002 8 20 AWXA200200728 1 20020812 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 325AW 23260 PHX - EEL - FLIGHT CREW REPORTED THAT THE EMERGENCY FLOOR PROXIMITY ESCAPE PATH LIGHT AT SEAT ROW 6 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 6 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002082000126 20020820 00126 NM 2002 8 20 AWXA200200732 1 20020725 A 5320 6517684642 INTERCOSTAL BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A .375 INCH CRACK WAS FOUND ON INTERCOSTAL BS 294, STR 8 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 294, STR 8 LT. FABRICATED A NEW INTERCOSTAL AND INSTALLED REPAIR IAW DWG 65-17684, AND B737- 200 SRM 51-10-01 PG 8. 2 L 7 2 4F RT A16WE 2002082000127 20020820 00127 NM 2002 8 20 AWXA200200733 1 20020725 A 5320 6517684688 INTERCOSTAL BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A .75 INCH CRACK WAS FOUND ON INTERCOSTAL BS 294, STR 15 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 294, STR 15 LT. FABRICATED A NEW INTERCOSTAL AND INSTALLED REPAIR IAW DWG 65-17684 AND B737- 200 SRM 51-10-01 PG 8. 2 L 7 2 4F RT A16WE 2002082000128 20020820 00128 NM 2002 8 20 AWXA200200734 1 20020725 A 5320 651768552 INTERCOSTAL BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A .5 INCH CRACK WAS FOUND ON INTERCOSTAL INNER CHORD BS 360, STR 14 LT. MAINTENA NCE REMOVED CRACKED INNER CHORD ANGLE AT BS 360, STR 14 LT. FABRICATED A NEW INNER CHORD ANGLE, AND INSTALLED REPAIR IA W DWG 65-17685-52, AND B737-200 SRM 51-10-01 PG 8. 2 L 7 2 4F RT A16WE 2002082000129 20020820 00129 NM 2002 8 20 AWXA200200741 1 20020725 A 5320 6547690 ANGLE BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK CRACKS WERE FOUND IN THE LOWER RADIUS OF THE AFT CARGO RT OUTBOARD CAP SUPPORT (Z EE ANGLE) AT RBL 21, BS 727C, 727D, 727E, 747, AND 767. MAINTENANCE REMOVED THE OUTBOARD CAP SUPPORT SECTION AT RBL 21, BS 727C TO 767. FABRICATED A NEW CAP SUPPORT SECTION, AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG 3, 38, SRM 51 -40-05, PG 4, BMM 51-21-99, PG 701-703, AND DWG 65-47690. 2 L 7 2 4F RT A16WE 2002111800013 20021118 00013 NE 2002 11 18 AWXA200200742 2 20020810 A 7530 1685MK6 ACTUATOR AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE LEAKING A AWXA F ACTIVATE FIRE EXT. A B P FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION TX TAXI/GRND HDL 1 WP 28 633AW 26404 14079 082 V0351 DTW - FIRE - FLT 0239 - WHILE AT GATE, POST FLIGHT, A FIRE OCCURRED AT THE NR 2 ENGINE ON SHUTDOWN, NO ECAM WARNING JUS T A LOT OF SMOKE, PUSHED NR 2 ENGINE FIRE BUTTON DISCHARGING BOTH FIRE EXTINGUISHER BOTTLES, FIRE WAS PUT OUT. MAINTENA NCE TROUBLESHOT PROBLEM TO VARIABLE STATOR VANE ACTUATOR, REMOVED AND REPLACED ACTUATOR IAW T/C R5M75303, PERFORMED POWE R ASSURANCE ENGINE RUN PER T/C F5M71302, NO DEFECTS WERE NOTED. VENDOR PERFORMED EXTENSIVE BENCH TEST AND TEARDOWN OF VARIABLE STATOR VANE ACTUATOR, FINDING REASON FOR REMOVAL NOT CONFIRMED. WHILE ON TEST PLATFORM UNIT WAS FOUND TO BE LE AKING FROM A DRY DRAIN. THIS LEAK WAS DETERMINED TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LEAKAGE IN THAT AREA AUTHORIZE 2 L 7 2 4F 4 F RT A28NM E311NE 2002082000130 20020820 00130 NM 2002 8 20 AWXA200200743 1 20020813 A 3350 1012621 LIGHT BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 PHX - EEL - DURING INSPECTION THE LT OVERWING EMERGENCY EXIT DOOR LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY EXIT DOOR LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002082000131 20020820 00131 EU 2002 8 20 AWXA200200744 1 20020813 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 66 PHX - EEL - FLIGHT CREW REPORTED OVERWING EXIT LIGHTS ILLUMINATED AND THE RT OVERWING EXIT SLIDE LIGHT DOES NOT INDICATE S ARMED. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING BATTERY PACK AT POWER SUPPLY (11WL), AND RESEATED THE RT OVER WING DOOR WARNING PLUNGER, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002111800014 20021118 00014 EU 2002 11 18 AWXA200200745 1 20020812 A 7500 LINE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE CRUSHED A AWXA E C ENGINE SHUTDOWN ABORTED TAKEOFF A J FLAME/FIRE WARNING INDICATION TO TAKEOFF 1 WP 28 633AW 082 V0351 PREPARING TO TAKEOFF, WHEN STARTING TO APPLY TAKEOFF POWER PRIOR TO 1.05 EPR, THE NR 2 ENGINE MADE A COMPRESSOR STALL SO UND. IMMEDIATELY MOVED THRUST LEVERS TO IDLE AND ECAM INDICATED, ENGINE 2 COMPRESSOR VANE FAULT. EIGHT PASSENGERS ALSO REPORTED SEEING FLAMES COMING FROM NR 2 ENGINE WHEN POWER WAS FIRST APPLIED ON RUNWAY. REJECTED TAKEOFF, SHUTDOWN NR 2 ENGINE ON TAXI IN TO GATE. MX BORESCOPED NR 2 ENGINE HPC PER T/C I5M72305, NO DEFECTS NOTED. FOUND HIGH PRESSURE FUEL LINE TO VARIABLE STATOR VANE ACTUATOR CRUSHED, REPLACED LINE AND VARIABLE STATOR VANE ACTUATOR IAW T/C R5M75303, PERFOR MED VIBRATION CHECK AND HIGH POWER ASSURANCE ENGINE RUN PER T/C'S F5M71310 AND F5M71302, NO FAULTS WERE NOTED. VENDOR 2 L 7 2 4F 4 F RT A28NM E311NE 2002082000132 20020820 00132 NE 2002 8 20 AWXA200200746 2 20020812 A 7314 5009913F PUMP AIRBUS A319 A319132 3930340 NM IAE V2527 V2527A5 NE NR 2 ENGINE FAILED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 660AW 1234 ORD - ABORTED TAKEOFF - FLT 0060 - ON TAKEOFF FROM ORD EN ROUTE FOR PHX RECEIVED ECAM INDICATION FOR NR 2 ENGINE COMPRES SOR VANE FAULT. ABORTED TAKEOFF AT 60 KTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2002082000133 20020820 00133 WP 2002 8 20 CALA0200439 1 20020818 A 3222 VALVE DOUG DC9 DC982 3022082 WP NOSE STRUT DEFECTIVE A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 18833 49493 THE NOSE GEAR DID NOT RETRACT AND WAS ACCOMPANIED BY THE RED GEAR UNSAFE LIGHT REMAINING ILLUMINATED AFTER TAKEOFF FROM MIA. THE GEAR WAS CYCLED, BUT THE HANDLE WOULD NOT COME UP. THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED WITHOUT INC IDENT. MAINTENANCE FOUND THE NOSE STRUT SCHRADER VALVE DEFECTIVE. THE SCHRADER VALVE WAS REMOVED AND REPLACED. THE NOSE GEAR WAS SWUNG SEVERAL TIMES WITH NO DEFECTS NOTED. A VISUAL INSPECTION OF THE GEAR FOUND NO OTHER DEFECTS. 2 L 7 2 4F A6WE 2002082000134 20020820 00134 NM 2002 8 20 AWXA200200748 1 20020729 A 5310 6545507 DOOR FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A .125 INCH CRACK WAS FOUND ON THE FORWARD ENTRY DOOR CUTOUT FRAME AT BS 312, STR 6 LT. MAINTENANCE BLENDED OUT CRACK ON FORWARD ENTRY DOOR CUTOUT FRAME AT BS 312, STR 6 LT. HFEC INSPECTION VERIFIED CRACK NO LONGER EXISTS. 2 L 7 2 4F RT A16WE 2002091000116 20020910 00116 EU 2002 9 10 AWXA200200751 1 20020814 A 2530 1238B OVEN AIRBUS 320 A320232 3930326 EU GALLEY SMOKE A AWXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 28 652AW 953 PHX - SMOKE - FLT 0504 - BOTH OVENS IN FORWARD GALLEY SMOKE WHEN OVEN IS HEATED. REMOVED AND REPLACED BOTH OVENS IN THE FORWARD GALLEY, OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT A28NM 2002082000135 20020820 00135 NM 2002 8 20 AWXA200200752 1 20020814 A 3150 WARNING SYSTEM BOEING 737 7373G7 1384595 NM COCKPIT ACTIVATED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 307AW 24634 PHX - ABORTED TAKEOFF - FLT 0495- INFO ONLY- T/O WARNING HORN SOUNDED ON T/O AT THRUST LEVERS ADVANCED. REJECTED T/O FL APS AT 1 DEGREE WITH A GREEN LIGHT, FLAP HANDLE AT 1 STAB TRIM 4.5 UNITS, SPEED BRAKE HANDLE STOWED NO CIRCUIT BREAKERS TRIPPED. SUBSEQUENT TAKEOFF NORMAL. 2 L 7 2 4F RT A16WE 2002082000137 20020820 00137 EA 2002 8 20 QXEA0201144 1 20020809 A 2613 LOOP CNDAIR CL600 CL6002C10 1390015 EA OVERHEAT SYS OUT OF POSITION A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 610QX 1237 1237 10033 FAT - CREW RETURNED TO FIELD WHEN PASSING THROUGH 10,500 FEET AFTER A RIGHT BLEED DUCT WARNING WAS RECEIVED. MAINTENANC E LEAK CHECKED THE RIGHT BLEED DUCT. NO LEAKS WERE DETECTED. THE MDC WAS INTERROGATED AND SHOWED THE RIGHT BLEED LOOP- B FAILED, OPEN CIRCUIT. REPOSITIONED BLEED LOOP. PERFORMED TEST OF BLEED LEAK DETECTION AND WARNING SYSTEM AND REPLACE D AILC. OPERATIONAL CHECK WAS GOOD, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002082000138 20020820 00138 NM 2002 8 20 QXEA0201145 1 20020808 A 6123 M390166150L RELAY DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS INOPERATIVE A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 355PH 500 PDX- ABORTED TAKEOFF, DURING TAKEOFF ROLL AT 70 KIAS ON TAKEOFF POWER SET, NOTED THAT AUTO-FEATHER ARM LIGHT WAS NOT ON. LIGHT TESTED GOOD. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED 6121-K5 RELAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002082000139 20020820 00139 EA 2002 8 20 QXEA021060 1 20020723 A 3234 9752661 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 609QX 1392 1392 10031 BOI- GEAR DISAGREE WARNING WITH ALL UP INDICATIONS. DECLARED AN EMERGENCY WITH AIR TRAFFIC CONTROL. PERFORMED EMERGENC Y CHECKLIST AND GEAR DEPLOYED MANUALLY. AIRCRAFT LANDED WITHOUT INCIDENT AND AIRCRAFT WAS TOWED TO THE GATE. REMOVED A ND REPLACED MAIN LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002082000140 20020820 00140 EA 2002 8 20 QXEA021095 1 20020727 A 2824 L92B13602 CARTRIDGE CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 602QX 1795 1795 10010 BOI - ON CLIMBOUT AT 18000 FEET, THE LEFT TRANSFER SHUTOFF VALVE MESSAGE ILLUMINATED. CENTER FUEL TANK QUANTITY INCREAS ED WITH FUEL BURN. CREW COMPLIED WITH EMERGENCY PROCEDURES AND THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED T HE AIRCRAFT AND REPLACED THE LEFT FUEL TRANSFER SHUTOFF VALVE CARTRIDGE. TRANSFER SYSTEM, FQGC AND VALVE SYSTEM TESTS W ERE COMPLIED WITH. OPERATIONAL CHECKS WERE GOOD, AN RII WAS COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002082000141 20020820 00141 EU 2002 8 20 QXEA021098 1 20020727 A 5220 A26839003 CABLE FOKKER F28 F28MK4000 4990810 EU EMERGENCY EXIT BROKEN A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 499US 11182 SEA - FLIGHT ATTENDANT REPORTS THAT THE EMERGENCY DOOR HANDLE FOR THE GALLEY EMERGENCY EXIT IS STUCK. MAINTENANCE INSPE CTED AND FOUND THE FORWARD TENSION CABLE BROKEN. THE DOOR WAS REMOVED, CABLE WAS REPLACED, THE DOOR WAS REINSTALLED. OP ERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002082000144 20020820 00144 NM 2002 8 20 SWAA021827 1 20020813 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 EEPLS WIRES EXPOSED IN CABIN. SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 2002082000145 20020820 00145 NM 2002 8 20 SWAA021831 1 20020812 A 3350 604222 BATTERY BOEING 737 7372T4 1384492 NM CARGO BAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED A2 CHECK, FOUND RT AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002082000146 20020820 00146 NM 2002 8 20 SWAA021834 1 20020812 A 3350 604222 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 AFT GALLEY AREA EMERGENCY EXIT LIGHTS ARE INTERMITTENT. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002082000147 20020820 00147 2002 8 20 SWAA021836 4 20020813 A 2565 D31354 SLIDE BOEING 737 737301 1384611 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002082000148 20020820 00148 2002 8 20 SWAA021839 4 20020813 A 2565 61621469 SLIDE BOEING 737 7373Y0 1384671 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED RON, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER M M. 2 L 7 2 4F RT A16WE 2002082000149 20020820 00149 NM 2002 8 20 SWAA021845 1 20020814 A 5523 183A42111 FITTING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB NR 2 ATTACH LUG WORN. REMOVED AND REPLACED RT EL EVATOR ATTACH LUG PER MM. 2 L 7 2 4F RT A16WE 2002082000150 20020820 00150 NM 2002 8 20 SWAA021846 1 20020814 A 5523 183A42111 FITTING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED PM CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB NR 2, NR 3 AND NR 4 ATTACH LUGS WORN. REMOVED AND REP LACED RT ELEVATOR TAB ATTACH LUGS PER SWA EA 2 L 7 2 4F RT A16WE 2002082000151 20020820 00151 NM 2002 8 20 SWAA021847 1 20020814 A 5523 183A42111 FITTING BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED PM CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB NR 1, NR 2 AND NR 3 ATTACH LUGS WORN. REMOVED AND REP LACED LEFT ELEVATOR ATTACH LUGS PER MM. 2 L 7 2 4F RT A16WE 2002082000152 20020820 00152 NM 2002 8 20 AWXA200200690 1 20020804 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 801AW 10275 54 889 PHX - THE L1 DOOR, R1 DOOR, AND SEAT ROW 1 LT EMERGENCY LIGHTS WERE FOUND INOPERATIVE DURING EMERGENCY LIGHTING TEST. M AINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) AND BATTERY IAW AMM 33-51-38-401, OPERATIONAL CHECK W AS GOOD. 2 L 7 2 4F RT A28NM 2002082000153 20020820 00153 NM 2002 8 20 AWXA200200695 1 20020725 A 5320 655429623 SPLICE BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF AFT CARGO FLOOR SUPPORT BS 773, LBL 21 TO RBL 21. MAINTENANCE REMOVED CORROSION FROM AFT CARGO FLOOR TEE SPLICE, MATERIAL LOSS OUT OF LIMITS. FABRICATED NEW TEE SPLICE AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02 PG 3-4. 2 L 7 2 4F RT A16WE 2002082000154 20020820 00154 NM 2002 8 20 AWXA200200696 1 20020806 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 801AW 889 PHX - FLIGHT CREW REPORTED EMERGENCY FLASHLIGHT UNDER THE FORWARD FLIGHT ATTENDANT SEAT IS INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002082000155 20020820 00155 NM 2002 8 20 AWXA200200697 1 20020807 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 DFW - DURING INSPECTION THE SEAT MOUNTED EMERGENCY LIGHT WAS FOUND BROKEN AT SEAT ROW 4 LT. MAINTENANCE REMOVED AND REP LACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002082000156 20020820 00156 NM 2002 8 20 AWXA200200698 1 20020807 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 PHX - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002082000157 20020820 00157 NM 2002 8 20 AWXA200200705 1 20020808 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 801AW 2627 889 PHX - EEL - DURING INSPECTION THE EMERGENCY EXIT LIGHTS ABOVE THE L1, R1, AND SEAT ROW 1 WERE FOUND INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) IAW AMM 33-51-04, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002082000161 20020820 00161 EU 2002 8 20 CX7A194J10 1 20020703 A 2613 1734362450 TERMINAL SAAB SF340 340B 7860101 EU LT ENGINE LOOSE A CX7A K NONE L NO TEST IN INSP/MAINT 1 GL 03 306CE 340B203 LEFT TAILPIPE HOT, WILL NOT TEST. RECRIMPED TERMINAL RING ON SENSOR IAW SAAB AMM. 2 L 7 2 4T RT A52EU 2002082000162 20020820 00162 EU 2002 8 20 CX7A194J11 1 20020717 A 2613 1734362450 TERMINAL SAAB SF340 340B 7860101 EU RT ENGINE BROKEN A CX7A K NONE L NO TEST TX TAXI/GRND HDL 1 GL 03 303CE 340B194 RIGHT TAILPIPE HOT, DOES NOT TEST. REPLACED BROKEN TAILPIPE SENSOR TERMINAL RING. 2 L 7 2 4T RT A52EU 2002082000163 20020820 00163 EU 2002 8 20 CX7A194J6 1 20020612 A 2613 OVERHEAT LOOP SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A CX7A E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 03 305CE 340B202 APPROX 1 MINUTE AFTER TO, THE TAILPIPE HOT LIGHT RT CAME ON. RAN CHECK LIST AND DID NOT GO OUT. SHUT DOWN ENGINE. RET URNED TO IND. THE LIGHT WENT OUT ABOUT THREE MINUTES AFTER SHUT DOWN. IT CAME ON AGAIN FOR ABOUT 5 SECONDS AND THEN WE NT OUT AGAIN A FEW SECONDS LATER. 2 L 7 2 4T RT A52EU 2002082000164 20020820 00164 EU 2002 8 20 CX7A194J8 1 20020621 A 2697 1734362450 WIRE SAAB SF340 340B 7860101 EU LT ENGINE DAMAGED A CX7A K NONE L NO TEST IN INSP/MAINT 1 GL 03 304CE 340B198 LEFT TAILPIPE HOT AND TRIPLE CHIME DOES NOT TEST. FOUND DURING PREFLIGHT. REPLACED WIRES IN 5 O'CLOCK SENSOR. 2 L 7 2 4T RT A52EU 2002082000165 20020820 00165 EU 2002 8 20 CX7A194J9 1 20020703 A 2613 1734362450 OVERHEAT LOOP SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A CX7A K NONE L NO TEST IN INSP/MAINT 1 GL 03 303CE 340B194 RIGHT TAILPIPE HO,T DOES NOT TEST. NO CWP LIGHT. NO TRIPLE CHIME. REMOVED TAIL SECTION OF COWLING AND CHECKED ALL SEN SOR WIRES. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002082000166 20020820 00166 NE 2002 8 20 MWEA020472 2 20020804 A 7200 7202 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LEFT VIBRATION A MWEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 31 601ME 49762 MECHANICS PERFORMED ENGINE VIBRATION ANALYSIS INSPECTED CI FAN BLADES COMPONENTS VISIBLE THROUGH PYLON ACCESSORY PANEL W ITH NO DEFECTS NOTED. REMOVED AND REPLACED LEFT ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2002082000167 20020820 00167 WP 2002 8 20 MWEA020482 1 20020814 A 5720 4911484501 CLIP DOUG DC9 DC914 3022034 WP LT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 REMOVED LEFT FUEL TANK SHEAR CLIP AT 69 BULKHEAD BETWEEN STRINGER 12 & 13. DRILLED UP CLIP AND INSTALLED FASTENERS. 2 L 7 2 4F A6WE 2002082000168 20020820 00168 WP 2002 8 20 MWEA020488 1 20020813 A 5720 99116033 FITTING DOUG DC9 DC914 3022034 WP LT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 LEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 13 AND 14, ALSO EXT ENDING UNDER STRINGER 14 AND 13. ALSO FOUND CRACK ON OUTBOARD LEG. BLENDED OUT CRACK AND REMOVED CORROSION AROUND AND UNDER STRINGER. 2 L 7 2 4F A6WE 2002082000169 20020820 00169 WP 2002 8 20 MWEA020493 1 20020814 A 5320 591016315 STIFFENER DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 STIFFENER AFT SIDE OF AFT PRESSURE BULKHEAD AT RADIAL 20 LEFT IS CRACKED AND DENTED. FABRICATED AND INSTALLED STIFFENER . 2 L 7 2 4F A6WE 2002082000170 20020820 00170 NM 2002 8 20 PCAA0208084 1 20020803 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST NR NOT REPORTED 1 EA 13 819EX 016 PHL - FLIGHT 3882 CREW REPORTED FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE FOUND RIGHT REAR EMERGENCY EXI T FLOOR STRIP DETACHED. FLOOR STRIP WAS RESECURED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002082000171 20020820 00171 NM 2002 8 20 PCAA0208088 1 20020808 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 810EX 308 DURING ROUTINE MAINTENANCE VISIT ONE FLOOR LEVEL EMERGENCY LIGHT WAS FOUND INOPERATIVE. BAD WIRE FOUND TO LIGHTS SOCKET . SOCKET ASSEMBLY REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002082000172 20020820 00172 NM 2002 8 20 PCAA0208089 1 20020808 A 5210 STOP DHAV DHC8 DHC8102 2809003 NM PAX DOOR DAMAGED A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 832EX 280 DCA - FLIGHT 3963 CREW REPORTED MAIN PASSENGER DOOR WILL NOT OPEN FROM OUTSIDE. MAINTENANCE PERFORMED AN INTERIM REPAI R TO DOOR HANDLE STOP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002082000173 20020820 00173 NM 2002 8 20 PCAA0208090 1 20020808 A 3350 PIN DHAV DHC8 DHC8102 2809003 NM CONNECTOR BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 849EX 337 DURING ROUTINE MAINTENANCE VISIT, SECOND CEILING AISLE EMERGENCY LIGHT FOUND TO BE INOPERATIVE. LIGHT WAS RELAMPED, BAT TERIES AT POSITIONS 300, 400, 500 AND 600 WERE REPLACED WITH NO FIX. AFTER FURTHER TROUBLESHOOTING A PIN WAS FOUND BROK EN IN CONNECTOR HOUSING. PIN WAS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002082000174 20020820 00174 NM 2002 8 20 PCAA0208091 1 20020809 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN CRUSHED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 835EX 289 DURING ROUTINE MAINTENANCE VISIT FIRST FLOOR LEVEL EMERGENCY LIGHT FOUND INOPERATIVE. CRUSHED WIRE FOUND AND REPAIRED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002082000175 20020820 00175 NM 2002 8 20 PCAA0208092 1 20020809 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 836EX 297 DURING ROUTINE MAINTENANCE VISIT EMERGENCY FLOOR LIGHTING HAD A BROKEN WIRE, 4TH LIGHT BACK FROM FRONT OF ROW. LIGHT AS SEMBLY REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002082000176 20020820 00176 NM 2002 8 20 PCAA0208094 1 20020814 A 3350 FUSE DHAV DHC8 DHC8102 2809003 NM POWER SUPPLY BLOWN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT RIGHT AFT EMERGENCY LIGHT FOUND INOPERATIVE. BULB WAS REPLACED WITH NO FIX. AFTER TRO UBLESHOOTING IT WAS DISCOVERED THAT BOTH FORWARD AND AFT POWER SUPPLIES HAD BLOWN FUSES. FUSES WERE REPLACED, OPERATION AL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002082000177 20020820 00177 NM 2002 8 20 SWAA021810 1 20020811 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 RT OVERWING EMERGENCY EXIT LIGHT BROKEN. REPAIRED WIRING AND REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002082000178 20020820 00178 NM 2002 8 20 SWAA021812 1 20020811 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 080SW 22675 DURING SCHEDULED RON, FOUND FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2002082000179 20020820 00179 NM 2002 8 20 SWAA021814 1 20020811 A 3350 D2964 PIN BOEING 737 7375H4 138449D NM CONNECTOR BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED RON, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. FOUND BROKEN PIN IN CONNECTOR D2964. REPAIRED CON NECTOR PER MM. 2 L 7 2 4F RT A16WE 2002082000180 20020820 00180 NM 2002 8 20 SWAA021820 1 20020812 A 2752 569670 MOTOR BOEING 737 737317 138447P NM T/E FLAP FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 693SW 23174 AIR TURNBACK, AFTER TAKEOFF T/E FLAPS WOULD NOT RETRACT HYDRAULICALLY. REMOVED AND REPLACED T/E FLAP HYDRAULIC MOTOR PE R MM. 2 L 7 2 4F RT A16WE 2002082000181 20020820 00181 NM 2002 8 20 VNAA0207030 1 20020722 A 3350 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN INOPERATIVE A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 437JS 3055 THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHT AT SEAT 9A WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLA CED THE EMERGENCY LIGHT STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002121300014 20021213 00014 EU 2002 12 13 AWXA200200753 1 20020815 A 7810 TAILPIPE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE FIRE A AWXA E ENGINE SHUTDOWN A FLAME/FIRE TX TAXI/GRND HDL 1 WP 28 633AW 082 V0351 AFTER ENG SHUTDOWN, RT TAIL PIPE FIRE, MOTORED ENG AND FIRE OUT. PERFORMED EXHAUST INSP & CHECK, NORM, ENG RUN ACCOMPLI SHED, NORM SHUTDOWN. RETURN TO PHX, AT ENG SHUTDOWN, SMOKE COMING FROM NR 2. PERFORMED DYE PEN AND AND ENG RUN, COMPLET ED, NO DEFECT NOTED. REMOVED OIL TUBE BETWEEN DIFFUSER AND TURBINE EXHAUST CASE FOR BLOCKAGE, NONE FOUND. LEAK AT FUEL D IST VALVE COVER, FUEL LINE AT FUEL VALVE. THE COVER AND FUEL LINE REPLACED. NR 2 ENG LOW PRESS BLEED SLAVE ACTUATOR LEAK ING, REPLACED LP BLEED SLAVE ACTUATOR, LEAK AND OPS CHECKS GOOD. TEST FLT DONE PRIOR TO RETURNING TO SERVICE, TEST FLT GOOD, NO SMOKE AT ENG SHUTDOWN. FLT 0576 AT ENG SHUTDOWN A TAILPIPE FIRE REPORTED AT NR 2 ENG. MAINT REMOVED NR 2 ENG. 2 L 7 2 4F 4 F RT A28NM E311NE 2002082000182 20020820 00182 EU 2002 8 20 AWXA200200754 1 20020815 A 3320 BALLAST AIRBUS 320 A320232 3930326 EU CABIN DEFECTIVE A AWXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 642AW 584 FWD F/A'S REPORT SMELLING AN ACRID, BURNING ELEC SMELL WHILE SEATED AT STATION VARIOUS PHASES OF FLIGHT. FOUND INOP BAL LAST IN FWD LAV, REPLACED LIGHT BALLAST, OPS NORMAL. 2 L 7 2 4F RT A28NM 2002082000183 20020820 00183 NE 2002 8 20 AWXA200200755 2 20020816 A 7200 SMOKE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE DETECTED A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 633AW 082 AFTER SHUTDOWN OF THE NR 2 ENG, EXCESSIVE SMOKE COMING FROM ENGINE. 2 L 7 2 4F 4 F RT A28NM E311NE 2002082000184 20020820 00184 NM 2002 8 20 AWXA200200756 1 20020816 A 2560 P4010021 BATTERY BOEING 737 7373Y0 1384671 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 331AW 23747 SNA - EMERGENCY EQUIPMENT - DURING INSPECTION THE FORWARD EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE BATTERIES IN THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002082000185 20020820 00185 NM 2002 8 20 AWXA200200757 1 20020816 A 3350 1721601 CONNECTOR AIRBUS A319 A319132 3930340 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 801AW 889 CMH - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED CONNECTOR AT SEAT ROW 4 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002082000186 20020820 00186 NM 2002 8 20 AWXA200200759 1 20020816 A 3350 65C2702921 LIGHT BOEING 737 7373S3 1384711 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 28 313AW 23712 PHX - EEL - FLIGHT ATTENDANT REPORTED THAT EMERGENCY EXIT LIGHT IN FIRST CLASS WAS INOPERATIVE. REPLACED BULLNOSE LIGHT ASSEMBLY PER BMM 33-51-21-201, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002082000187 20020820 00187 EU 2002 8 20 AWXA200200760 1 20020817 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 657AW 10995 1003 PHX - EEL - EMERGENCY LIGHTS SYSTEM WILL NOT TEST ON PRESS AND TEST PANEL (110RT). MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (13WL) IAW AMM 33-51-38-000-001, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002082000188 20020820 00188 NM 2002 8 20 VNAA0207034 1 20020724 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 442JS 14774 123 3060 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING AT ROW 10A. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AN D THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000189 20020820 00189 NM 2002 8 20 VNAA0207035 1 20020724 A 2432 DTSP400L BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY OVERHEATED A VNAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 07 470PS 13786 330 3006 DURING CLIMBOUT, THE CREW RECEIVED A BATTERY OVERHEAT MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED T HE NUMBER TWO BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000190 20020820 00190 NM 2002 8 20 VNAA0207036 1 20020725 A 3510 OXYGEN SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT LOW A VNAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 439JS 3057 EN ROUTE THE OXYGEN HAD GONE DOWN AND THE CREW SUSPECTED AN OXYGEN LEAK. THE FLIGHT DESCENDED TO 10,000 FEET AND DIVERT ED TO PIT. MAINTENANCE INSPECTED AND SERVICED THE OXYGEN IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 35-00-00. OPERA TIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000191 20020820 00191 NM 2002 8 20 VNAA0207038 1 20020725 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 431JS 3028 DURING TAKEOFF, THE CAPTAIN HEARD A CHIME. THE CREW LOOKED DOWN AND SAW A MESSAGE FLASH BUT COULD NOT TELL CLEARLY WHAT THE MESSAGE WAS AND ABORTED TAKEOFF. FLIGHT 9423 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000192 20020820 00192 NM 2002 8 20 VNAA0207039 1 20020726 A 5270 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EMERGENCY EXIT DIRTY A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 471PS 3007 IMMEDIATELY FOLLOWING TURBULENCE, THE CREW SEEN THE 9A EMERGENCY DOOR LIGHT FLASH ON THE RED WARNING PANEL. MAINTENANCE INSPECTED AND CLEANED THE EMERGENCY DOOR TARGET AND PROXI SENSOR IN ACCORDANCE WITH 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000193 20020820 00193 NM 2002 8 20 VNAA0207040 1 20020728 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 439JS 14819 73 3057 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 3 TO 4 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000194 20020820 00194 NM 2002 8 20 VNAA0207042 1 20020729 A 2750 FCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE T/E FLAP MALFUNCTIONED A VNAA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 GL 07 439JS 3057 DURING TAKEOFF, THE CREW RECEIVED A FLAP CONTROL FAIL CAS MESSAGE. MAINTENANCE INSPECTED AND RESET THE FLAP CONTROL UNI T IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEAS ED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000195 20020820 00195 NM 2002 8 20 VNAA0207044 1 20020729 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 457PS 15628 1090 3048 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 4 AND 5 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AN D THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000196 20020820 00196 2002 8 20 VNAA0207045 4 20020730 A 3425 FLIGHT DIR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 434JS 3051 DURING TAKEOFF, THE CREW RECEIVED A FLIGHT DIRECTOR FAIL IN THE HORIZONTAL MODE AND ABORTED TAKEOFF. ON THE TAXI WAY TH E CREW CALLED MAINTENANCE CONTROL AND RESET THE SYSTEM. FLIGHT 4168 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIG HT 4168 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000197 20020820 00197 WP 2002 8 20 ZW0A0207601 1 20020703 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 980TW 53630 THE FUSELAGE SKIN WAS DAMAGED AT 6 O'CLOCK, STATION 110 TO 113. TRIMMED OUT DAMAGED SKIN AND REPAIRED PER SRM 53-04, FI G 12B, SHEET 22. 2 L 7 2 4F RT A6WE 2002082000198 20020820 00198 WP 2002 8 20 ZW0A0207602 1 20020703 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 980TW 53630 THE FUSELAGE SKIN WAS DAMAGED UNDER THE FWD DRAIN MAST. REPAIRED DAMAGED SKIN UNDER THE FWD DRAIN MAST PER ARA 18254 AN D SRM 53-04, FIG 12B. 2 L 7 2 4F RT A6WE 2002082000199 20020820 00199 WP 2002 8 20 ZW0A0207603 1 20020703 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP FUSELAGE BENT A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 980TW 53630 THE Y-CHORD WAS BENT AT STA 110, LONGERON 28L TO 28R. INSTALLED NEW Y-CHORD PER ARA 18257, BETWEEN LONGERON 26L AND 26R . 2 L 7 2 4F RT A6WE 2002082000200 20020820 00200 WP 2002 8 20 ZW0A0207604 1 20020703 A 5320 SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 980TW 53630 THE FORWARD BULKHEAD SUPPORT ANGLE WAS DAMAGED AT STA 110, RBL 2. REPAIRED PER ARA 18260. 2 L 7 2 4F RT A6WE 2002082000201 20020820 00201 WP 2002 8 20 ZW0A0207605 1 20020703 A 5320 SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 980TW 53630 THE FWD BULKHEAD SUPPORT ANGLE WAS DAMAGED AT STA 110, LBL 2. REPAIRED PER ARA 18260. 2 L 7 2 4F RT A6WE 2002082000202 20020820 00202 NM 2002 8 20 ZW0A0207702 1 20020724 A 3397 WIRE BOEING 767 7673Y0 NM CABIN DISCONNECTED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 632TW 24953 THE EGRESS LIGHTS WERE INOPERATIVE ON RT SIDE OF CABIN, ROWS 4 TO 6. RECONNECTED WIRE IN TRACK AT ROW 4. 2 L 7 2 4F RT A1NM 2002082000203 20020820 00203 WP 2002 8 20 ZW0A0208002 1 20020723 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9619V 53566 DURING CHECK-C, SKIN DAMAGED FUSELAGE STATION 110 TO APPROX FUSELAGE STATION 129 LONGERON 28 RIGHT TO LONGERON 27 RIGHT. REPAIRED SKIN DAMAGE FS 110 TO APPROX FS 129 L28R-L27R PER ARA18213 AND SRM 53-02. NO CRACKS FOUND PER PART 6-51-00-0 3. 2 L 7 2 4F RT A6WE 2002082600097 20020826 00097 NM 2002 8 26 2002UALA01296 1 20020812 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 RIGHT HAND FUSELAGE SKIN AT STATION 532 STRINGER 17R, HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082600099 20020826 00099 NM 2002 8 26 2002UALA01298 1 20020812 A 5312 BULKHEAD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 APU FIREWALL BULKHEAD REPAIR AT STATION 1885 WORN DUE TO CONTACT WITH RIGHT HAND DOOR HOOK. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082600101 20020826 00101 NM 2002 8 26 2002UALA01304 1 20020813 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 AFT PIT FRAME HAS CORROSION STATION 1480 RBL 25. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME CAP STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082600102 20020826 00102 NM 2002 8 26 2002UALA01305 1 20020813 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 CABIN FLOOR STRUCTURE INTERCOSTAL SUPPORT AT STATION 720 TO 740 RBL 62 STRINGER 17R HAD EXCESSIVE CORROSION ON UPPER SUR FACE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082600103 20020826 00103 NM 2002 8 26 2002UALA01306 1 20020813 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 CABIN FLOOR STRUCTURE OUTER CREASE BEAM HAD EXCESSIVE CORROSION ON UPPER SURFACE AT STATION 736 RBL 64 STRINGER 17R. MA JOR REPAIR ACCOMPLISHED. REMOVED COMPLETE SECTION OF CREASE BEAM AND INSTALLED NEW SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082600106 20020826 00106 NM 2002 8 26 2002UALA01312 1 20020815 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHTS AT 3L BLINKS ON & OFF. ALSO, FLOOR LIGHTS AT 32-34C BLINK. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2002082600109 20020826 00109 NM 2002 8 26 2002UALA01317 1 20020816 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 FUSELAGE SKIN DENTED AT STA 1485, STR 45L AND 46L. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN DENT WAS REWORKED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002082000204 20020820 00204 SO 2002 8 20 C2XA02CL173 1 20020816 A 3260 852701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO NOSE GEAR FAILED A C2XA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SW 27 13990 145277 CLE FLIGHT#3222 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF.A EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.AFTER EXITING RUNWAY THE MESSAGE DISAPPEARED.THEY ALSO REPORTED ENGINE 1 AND 2 THRUST REVERSER DISAGREE MESSAGE.MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR WOW PROXIMITY SENSOR AND SERVICED THE NOSE LANDING GEAR SHOCK ABSORBER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002082000205 20020820 00205 2002 8 20 SWAA021863 4 20020817 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM FWD ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002082000206 20020820 00206 NM 2002 8 20 SWAA021867 1 20020818 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 EEPLS COVER MISSING AT ROW NR 2. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002082000207 20020820 00207 2002 8 20 SWAA021868 4 20020818 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002082000208 20020820 00208 NM 2002 8 20 SWAA021870 1 20020818 A 3350 6042221 BATTERY BOEING 737 737317 138447P NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED PM CHECK, FWD CABIN EMERGENCY EXIT LIGHTS NOT TURNING OFF. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002082000209 20020820 00209 NM 2002 8 20 SWAA021871 1 20020812 A 2701 BACB10B28PLT BEARING BOEING 737 7373H4 1384600 NM CONTROL COLUMN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED RON, FOUND AILERONS BINDING DURING PREFLIGHT CONTROL CK. REMOVED AND REPLACED CONTROL COLUMN BEARINGS PER MM. 2 L 7 2 4F RT A16WE 2002082000210 20020820 00210 NM 2002 8 20 SWAA021872 1 20020816 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002082000211 20020820 00211 NM 2002 8 20 SWAA021873 1 20020817 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 360, STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002082000212 20020820 00212 NM 2002 8 20 SWAA021874 1 20020817 A 5330 6545768 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 103SW 23109 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 344, STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F A16WE 2002082000213 20020820 00213 NM 2002 8 20 SWAA021875 1 20020816 A 5320 BAC1503 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED SERVICE CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663.5, RBL 6.15. REPAIRED STIFFENER PER SWA EA. 2 L 7 2 4F RT A16WE 2002082000214 20020820 00214 NM 2002 8 20 SWAA021876 1 20020817 A 5330 589357 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED PM CHECK, FOUND CAPTIAN'S UPPER WINDOW POST SKIN CRACKED IN UPPER RADIOUS. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002082000215 20020820 00215 NM 2002 8 20 SWAA021877 1 20020815 A 2612 894092 FIRE LOOP BOEING 737 7372H4 138448C NM NR 2 ENGINE MALFUNCTIONED A SWAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 29 083SW 22732 INFLIGHT SHUTDOWN, DECLARED EMERGENCY, ON BASE LEG TO FINAL NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED. BOTH BOTTLES WE RE DISCHARGED. REMOVED AND REPLACED NR 2 ENG UPPER FIRE DETECTION ELEMENT PER MM. 2 L 7 2 4F A16WE 2002082000216 20020820 00216 NM 2002 8 20 SWAA021880 1 20020818 A 5712 6545445 RIB BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND RT WING RIB CRACKED AT WBL 135.5, BETWEEN STR 2R AND STR 3R. REPAIRED RIB PER BFG ER. 2 L 7 2 4F RT A16WE 2002082000217 20020820 00217 NM 2002 8 20 SWAA021881 1 20020818 A 5553 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING, LT AFT, LT FWD AND RT FWD LUGS CORRODED. REPAIRED LUGS PE R BFG ER. 2 L 7 2 4F RT A16WE 2002082000218 20020820 00218 NM 2002 8 20 SWAA021851 1 20020815 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 EEPLS COVER LOOSE IN CABIN. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002082000219 20020820 00219 NM 2002 8 20 SWAA021856 1 20020815 A 3260 MS2538 SWITCH BOEING 737 7373H4 1384600 NM COCKPIT OUT OF ADJUST A SWAA K NONE O OTHER AP APPROACH 1 SW 29 336SW 23940 AFTER GEAR EXTENSION, THREE GREEN AND THREE RED LIGHTS ILLUMINATED, RECYCLED GEAR AND THREE GREEN LIGHTS ILLUMINATED. A DJUSTED S78 SWITCH PER MM. 2 L 7 2 4F RT A16WE 2002082000220 20020820 00220 NM 2002 8 20 SWAA021857 1 20020815 A 5210 6547952 STRUCTURE BOEING 737 7373H4 1384600 NM ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR CRACKED AT LOWER HINGE AREA, BS 316 AND WL 236. REPAIRED DOOR PER BOE ING SB. 2 L 7 2 4F RT A16WE 2002082000221 20020820 00221 NM 2002 8 20 SWAA021858 1 20020815 A 5315 65C345371 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED (4 EA), BETWEEN BS 662 AND BS 675 AT LBL 25. REPAIRED FL OORBEAMS PER BFG ER. 2 L 7 2 4F RT A16WE 2002082000222 20020820 00222 NM 2002 8 20 SWAA021859 1 20020815 A 5315 65C345371 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED (2 EA), BETWEEN BS 666 AND BS 670 AT RBL 25. REPAIRED FL OORBEAM PER BFG ER. 2 L 7 2 4F RT A16WE 2002082000223 20020820 00223 SO 2002 8 20 C2XA02BT044 1 20020817 A 2520 500064001 PUMP EMB 145 EMB145 3260210 SO INTERMITTENT A C2XA O OTHER O OTHER UK UNKNOWN 1 SW 27 16961 145103 EWR---CO3426, CREW REPORTED, "BURNING SMELL DETECTED FROM COFFEE POTS." MAINTENANCE REMOVED AND REPLACED RIGHTHAND PUMP ASSEMBLY IAW EMB145 MM 25-22-01. OPS.CHECKED GOOD. NO ODORS DETECTED AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002082000224 20020820 00224 2002 8 20 C2XA02BT045 4 20020820 A 2350 7511001939 AUDIO PANEL EMB 135 EMB135ER 3260203 SO COCKPIT FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 27506 145206 EWR---CO3742, WHILE SITTING AT THE GATE, CREW REPORTED, "SMOKE IN THE COCKPIT".....MAINTENANCE FOUND SMOKE TO BE COMING FROM AUDIO CONTROL PANEL. REMOVED AND REPLACED AUDIO CONTROL PANEL IAW EMB135/145 MM 23-51-01. OPS.CHECKED GOOD. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002082000225 20020820 00225 EA 2002 8 20 COMA0260483 1 20020815 A 3350 59465 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 FLIGHT 5778 EMERGENCY LIGHTS ARE INOP ROWS 8 TO 13.REPAIRED LOOSE CONNECTION AT ROW 13. 2 L 7 2 4F RT A21EA 2002082000226 20020820 00226 EA 2002 8 20 COMA0260484 1 20020813 A 3231 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA NLG MISRIGGED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 958CA 15695 7111 FLIGHT 5296 AND 5703 BANGING AND THUMPING NOISE FROM NLG WITH GEAR RETRACTED; WITH GEAR DOWN NOSE DOORS OPEN WARNING.ADJ USTED THE NLG DOORS ACTUATING MECHANISM. 2 L 7 2 4F RT A21EA 2002082000227 20020820 00227 EA 2002 8 20 COMA0260485 1 20020815 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF S J AFFECT SYSTEMS WARNING INDICATION TO TAKEOFF 1 SO 01 978CA 7158 FLIGHT 5770 T/O ABORTED DUR TO REVERSE UNLOCK WARNING.SECURED THE R/H ENGINE T/R AND DEFERRED MAINTENANCE PER MEL. 2 L 7 2 4F RT A21EA 2002082000228 20020820 00228 EA 2002 8 20 COMA0260486 1 20020814 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 473CA 604 7668 FLAPS FAILED WHEN SELECTED TO 8 DEGREES AT GATE.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2002082000229 20020820 00229 EA 2002 8 20 COMA0260487 1 20020814 A 3260 172825 TARGET CNDAIR CL600 CL6002B19 1900309 EA R/H MLG LOOSE A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 956CA 7105 FLIGHT 5787 GEAR DISAGREE MESSAGE, R/H MLG DID NOT INDICATE UPLOCK.TIGHTENED LOOSE PROXIMITY SENSOR TARGET ON R/H MLG UP LOCK. 2 L 7 2 4F RT A21EA 2002082000230 20020820 00230 WP 2002 8 20 ABXA020069 1 20020729 A 3350 5708458503 BATTERY PACK DOUG DC8 DC861 3021952 WP CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 162 45891 LOST EXTERNAL POWER AND NO EMERGENCY EXIT LIGHT ILLUMINATED WITH SWITCH IN ARMED POSITION. REPLACED THE EMERGENCY BATTE RY PACK. OPS CHECKED GOOD IAW DC-8 MM. 2 L 7 4 4F 4A25 2002082000231 20020820 00231 WP 2002 8 20 ABXA020070 1 20020731 A 3230 LANDING GEAR DOUG DC9 DC941 302207N WP NLG MALFUNCTIONED A ABXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 23 975AX 47512 UPON GEAR EXTENSION FOR APPROACH, NOSE GEAR DID NOT EXTEND (NO GREEN LIGHT/NOSE LIGHT DID NOT SHOW). GEAR RECYCLED AFTE R GO-AROUND. NOSE GEAR EXTENDED NORMALLY. INSPECTED NOSE LANDING GEAR DOWNLOCK SWITCH WIRING, NO DEFECTS NOTED. LUBED NOSE LANDING GEAR. REPLACED THE NOSE LANDING GEAR DOWN AND LOCK BULBS. PERFORMED EXTENSION AND RETRACTION TEST. NO D EFECTS NOTED IAW DC-9 AMM 32-20-00-2-0001. 2 L 7 2 4F A6WE 2002082000232 20020820 00232 NM 2002 8 20 ABXA020071 1 20020726 A 5753 113T13227 LINK BOEING 767 767200 1385120 NM T/E FLAP WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 785AX 23018 LINK ON INBOARD FITTING OF THE LEFT OUTBOARD FLAP HAD EXCESSIVE MOVEMENT. REPLACED LINK IAW B767 AMM 27-51-27. 2 L 7 2 4F RT A1NM 2002082000233 20020820 00233 WP 2002 8 20 ABXA020072 1 20020730 A 3233 4771392501 PIN DOUG DC8 DC863F 302198F WP MLG ACTUATOR SHEARED A ABXA K NONE O OTHER AP APPROACH 1 GL 23 828AX 45999 PLACED LANDING GEAR LEVER DOWN, HAD LOUD BANG WITH GREENLIGHT ON NOSE GEAR. FOUND RIGHT MAIN LANDING GEAR ACTUATOR LOWE R PIVOT PIN SHEARED. REPLACED THE RETRACT PIN AND ACTUATOR. REWORKED THE RIGHT MAIN LANDING GEAR RETRACT PIN BOSS HOLE . OVERSIZED TO REMOVE CORROSION IAW NEA 32130001-003. WORK COMPLETED IAW D832-44721-MR. BOEING COMMERCIAL AIRCRAFT GR OUP CONTACTED BY ENGINEERING FOR EVALUATION. 2 L 7 4 4F 4A25 2002082000234 20020820 00234 WP 2002 8 20 ABXA020073 1 20020802 A 5610 WINDOW DOUG DC9 DC932F 3022067 WP COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 FIRST OFFICER'S WINDOW WOULD NOT OPEN. INSPECTED, CLEANED AND LUBRICATED IAW DC-9 AMM 56-10-03. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002082000235 20020820 00235 WP 2002 8 20 ABXA020074 1 20020811 A 3260 WARNING SYSTEM DOUG DC8 DC863F 302198F WP COCKPIT MALFUNCTIONED A ABXA K NONE N FALSE WARNING CR CRUISE 1 GL 23 811AX 46113 GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR, LIGHT WENT OUT. LOUD GRINDING NOISE HEARD ON 2ND ROT ATION. 2 L 7 4 4F 4A25 2002082000236 20020820 00236 NM 2002 8 20 VNAA0208004 1 20020805 A 2750 FCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE T/E FLAP MALFUNCTIONED A VNAA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 GL 07 439JS 3057 DURING TAKEOFF, THE CREW RECEIVED A FLAP CONTROL FAILURE CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND RES ET THE FLAP CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000237 20020820 00237 NM 2002 8 20 VNAA0208005 1 20020805 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 442JS 12275 80 3060 THE CREW REPORTED THAT THE EMERGENCY BATTERY AT THE 7LK LOCATION WAS NOT WORKING PROPERLY. MAINTENANCE INSPECTED AND RE PLACED THE EMERGENCY BATTERY AT THE 7LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CH ECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000238 20020820 00238 NM 2002 8 20 VNAA0208006 1 20020805 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 460PS 14386 751 3061 THE CREW REPORTED THAT THE EMERGENCY LIGHT AT ROW 11A WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMER GENCY BATTERY AT THE 7LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFO RMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082000239 20020820 00239 EU 2002 8 20 YENA200218 1 20020730 A 2810 L95F50603 SEAL AIRBUS 320 A320232 3930326 EU RELIEF VALVE CRACKED A YENA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 524JB 3968 3968 1528 FLT 106, IAD TO LGB, A/C DEVELOPED FUEL MIGRATION FROM LEFT MAIN TO CTR TANK. LEVELED OFF AT FL280, DID AN EMERGENCY LA NDING AT PITTSBURG. A/C TOUCHDOWN V/S WAS LESS THAN 100 FPM. FOUND OVERPRESSURE PROTECTOR 96QM SEAL CRACKED ON VALVE. REPLACED OVERPRESSURE PROTECTOR 96QM REF AMM 28-12-41, INSP CK PER 28-12-47, LEAK CHECK TANK PLATES 147AZ AND 548AB REF AMM 57-17-11 OK. 2 L 7 2 4F RT A28NM 2002082000240 20020820 00240 NM 2002 8 20 HNAA020054 1 20020813 A 3350 6040681LF BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST UK UNKNOWN 1 EA 07 917HA 27873 126 075 TWO OF THE FOUR RED EMERGENCY FLOOR LIGHT FORWARD END ARE INOP. REMOVED AND REPLACED EMERGENCY BATTERY 3352 PS1. 2 H 7 2 4T RT A13NM 2002082000241 20020820 00241 NM 2002 8 20 AWXA200200763 1 20020730 A 5313 69416803 ATTACH ANGLE BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 1/2" CRACK WAS FOUND ON WEB UPPER CHORD (ATTACH ANGLE) AT FASTENER HOLES BS 5 00B TO BS 520, BL 0, WL 208.1. MAINTENANCE REMOVED WEB UPPER CHORD BS 500B TO BS 520, FABRICATED A REPAIR ANGLE AND INST ALLED REPAIR IAW DWG 69-41680, AND B737-200 SRM 51-30-2, FIG 7, PG. 32, SRM 51-10-2, FIG 2, PG. 7 & 32, AND SRM 51-10-1, PG. 10. 2 L 7 2 4F RT A16WE 2002082000242 20020820 00242 NM 2002 8 20 AWXA200200764 1 20020731 A 5330 507945164 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4" CRACK WAS FOUND ON L-1 DOOR INTERNAL SKIN AT THE AFT UPPER CORNER DOOR STO P ADJUSTMENT CUTOUT, BS 346. MAINTENANCE CUTOUT CRACK AT L-1 DOOR AFT UPPER CORNER DOOR STOP ADJUSTMENT CUTOUT, BS 346. FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR IAW B737-200 SRM 51-40-2, FIG. 1, PG. 1-3. 2 L 7 2 4F RT A16WE 2002082000243 20020820 00243 NM 2002 8 20 AWXA200200766 1 20020730 A 5330 6545871132 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4" CRACK WAS FOUND ON R-1 DOOR EXTERNAL SKIN AT UPPER AFT CORNER OF HINGE CUT OUT, CONFIRMED BY HFEC INSPECTION. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN AT R-1 DOOR UPPER AFT CORNER OF HINGE CUTOUT AND PERFORMED HFEC INSPECTION TO ENSURE NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND INSTALLED REPAIR IAW AWA ER 15- 5241-02221-TB1. 2 L 7 2 4F RT A16WE 2002082000244 20020820 00244 NM 2002 8 20 AWXA200200767 1 20020802 A 5313 BAC1498156 STRINGER BOEING 737 737277 1384570 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON BOTH SIDES OF STRINGER 26 R/H BETWEEN BS 887 A ND BS 927. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED STRINGER 26 R/H FROM BS 885 TO BS 917, REMOVED TO FOM 1 EACH STRINGER CLIP & SPLICE BS 907, AND 1 EACH STRINGER CLIP BS 927. FABRICATED A FILLER, A REPAIR SPLICE, AND 4 EACH SHIMS; REINSTALLED STRINGER CLIPS AND SPLICE AT BS 907 AND BS 927, AND INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-3, FIG 1, PG. 3-10. 2 L 7 2 4F RT A16WE 2002082000245 20020820 00245 NM 2002 8 20 AWXA200200770 1 20020810 A 5313 BAC1498158 STRINGER BOEING 737 737277 1384570 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON THE UPPER AFT END OF STRINGER 26 R/H, BS 380 (E&E COMPARTM ENT). MAINTENANCE REMOVED 1 EACH STRINGER SPLICE BS 360, 2 EACH STRINGER CLIPS BS 360 & BS 380, AND CUTOUT DAMAGED SECT ION OF STRINGER BS 363 TO BS 387. FABRICATED A NEW SECTION OF STRINGER, 2 EACH SPLICES, 2 EACH SHIMS, AND INSTALLED REPA IR PARTS AND 2 EACH (REMOVED) STRINGER CLIPS IAW B737-200 SRM 53-10-3, FIG. 1, PG. 3-9. 2 L 7 2 4F RT A16WE 2002082000246 20020820 00246 NM 2002 8 20 AWXA200200771 1 20020813 A 5754 114N300252 SLAT BOEING 757 7572S7 1384962 NM DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 0 0 23568 LCQ - MAJOR REPAIR - APPROXIMATELY 12" OF TRAIL EDGE WEDGE HAS SKIN AND CORE DAMAGE ON # 6 LEADING EDGE SLAT. REMOVED # 6 LEADING EDGE SLAT; CLEANED, PREPARED, AND REPLACED TRAILING EDGE WEDGE IAW E.O. 57-55-10. REINSTALLED # 6 LEADING EDGE SLAT IAW BMM 27-81-01, PG. 401-422. 2 L 7 2 4F RT A2NM 2002082000247 20020820 00247 NM 2002 8 20 AWXA200200772 1 20020723 A 5330 6573746 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 0 0 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND ON FORWARD UPPER CORNER OF SKIN CUTOUT AT THE L-2 DOOR BS 951. MAINTENANCE REMOVED DAMAGED AREA OF SKIN AND BONDED DOUBLER, FABRICATED A DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW B737-200 SRM 53-30-3, FIG. 21A, PG 78. 2 L 7 2 4F RT A16WE 2002082100001 20020821 00001 SW 2002 8 21 HEEA080613 1 20020729 A 7712 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 N/R AND NR 2 NEEDLES INOPERATIVE. 1 G 7 2 4U H4SW 2002082100002 20020821 00002 SW 2002 8 21 HEEA080614 1 20020729 A 2840 473203003 SIGNAL COND UNIT BELL 412 412 1182202 SW FUEL INDICATOR MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 TRANSFER LIGHT COMES ON AND STAYS ON FOR 20 MINUTES. 1 G 7 2 4U H4SW 2002082100003 20020821 00003 SW 2002 8 21 HEEA080615 1 20020729 A 2800 475C61NSX DRAIN VALVE BELL 412 412 1182202 SW FUEL SYSTEM LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2148K 36001 FUEL DRAIN VALVE LEAKS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2002082100004 20020821 00004 SW 2002 8 21 HEEA080616 1 20020729 A 2510 501836401 RESTRAINT BELL 412 412 1182202 SW COCKPIT FRAYED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 SHOULDER RESTRAINT FRAYED. SCRAPPED. 1 G 7 2 4U H4SW 2002082100005 20020821 00005 2002 8 21 HEEA080617 4 20020729 A 3421 5040017901 INDICATOR BELL 412 412 1182202 SW ATTITUDE MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 142PH 33150 ATTITUDE INDICATOR WON'T PULL FLAG - WORKS INTERMITTENTLY. REPAIRED. 1 G 7 2 4U H4SW 2002082100006 20020821 00006 2002 8 21 HEEA080618 4 20020729 A 3421 504001790116 GYRO BELL 412 412 1182202 SW COCKPIT OSCILLATES E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 ADI OSCILLATES INTERMITTENTLY. REPAIRED. 1 G 7 2 4U H4SW 2002082100008 20020821 00008 EU 2002 8 21 UHL2002F00002 1 20020610 A 3230 AE7064588 HOSE AIR864141 SAAB SF340 SF340A 7850100 EU GE CT7TS CT71 30030 NE NOSE GEAR CHAFED A UHLA A D UNSCHED LANDING RETURN TO BLOCK J K O WARNING INDICATION FLUID LOSS OTHER TO TAKEOFF 1 NE 03 340SZ LK8607041 340A004 AFTER DEPARTURE, UPON SELECTING GEAR UP HYDRAULIC WARNING LIGHT ILLUMINATED WITH ASSOCIATED (2620) PRESSURE READING ON G AUGE LANDING GEAR EXTENDED RETRUNED TO FIELD, MAINTENANCE INSPECTED, FOUND NOSE RETRACT CYLINDER HOSE CHAFFED THROUGH. REPLACED HOSE, SERVICED RESERVOIR. AIRCRAFT JACKED AND CYCLED ALL CHECKS PERFORMED NORMALLY IAW MM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 U RT A52EU E8NE 2002082100009 20020821 00009 2002 8 21 HEEA080620 4 20020729 A 3421 504001790116 GYRO BELL 412 412 1182202 SW COCKPIT UNRELIABLE E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 3893N 33010 INDICATOR PRECESSES RIGHT UNTIL CARD REACHES INTERNAL STOPS, UNRELIABLE. REPAIRED. 1 G 7 2 4U H4SW 2002082100010 20020821 00010 2002 8 21 HEEA080621 4 20020729 A 3421 504001790116 GYRO BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893N 33010 LIGHT INOPERATIVE. REPAIRED. 1 G 7 2 4U H4SW 2002082100011 20020821 00011 2002 8 21 HEEA080622 4 20020729 A 3421 504001790116 GYRO BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 INSTRUMENT LIGHTING INOPERATIVE. REPAIRED. 1 G 7 2 4U H4SW 2002082100013 20020821 00013 2002 8 21 HEEA080624 4 20020729 A 3421 504001790116 GYRO BELL 412 412 1182202 SW COCKPIT OSCILLATES E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 ADI OSCILLATES INTERMITTENTLY. REPAIRED. 1 G 7 2 4U H4SW 2002082100014 20020821 00014 2002 8 21 HEEA080625 4 20020729 A 3421 504001790116 GYRO BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893N 33010 HORIZON GYRO LIGHT INOPERATIVE. REPAIRED. 1 G 7 2 4U H4SW 2002082100015 20020821 00015 2002 8 21 HEEA080626 4 20020729 A 3421 5040017928 INDICATOR BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 107X 33113 STANDBY ATTITUDE INDICATOR WON'T ERECT. REPAIRED. 1 G 7 2 4U H4SW 2002082100016 20020821 00016 2002 8 21 HEEA080627 4 20020729 A 3421 5040017928 INDICATOR BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 107X 33113 STANDYBY ATTITUDE INDICATOR TUMBLES. REPAIRED. 1 G 7 2 4U H4SW 2002082100017 20020821 00017 2002 8 21 HEEA080628 4 20020729 A 3421 504001790116 GYRO BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 142PH 33150 HORIZON GYRO WON'T PULL FLAG WITH STANDBY BATTERY OUTPUT OF 22.4 VOLTS. REPAIRED. 1 G 7 2 4U H4SW 2002082100018 20020821 00018 SW 2002 8 21 HEEA080629 1 20020729 A 2421 51509001R CONTROL BOX BELL 412 412 1182202 SW GENERATOR FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22608 33075 GENERATOR DROPS OFF LINE INTERMITTENTLY. 1 G 7 2 4U H4SW 2002082100019 20020821 00019 SW 2002 8 21 HEEA080630 1 20020729 A 2421 51509002R CONTROL UNIT BELL 412 412 1182202 SW GENERATOR FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1202T 33112 CONTROL UNIT WON'T ALLOW GENERATOR TO COME ON LINE. 1 G 7 2 4U H4SW 2002082100020 20020821 00020 SW 2002 8 21 HEEA080631 1 20020729 A 2421 51509002R CONTROL UNIT BELL 412 412 1182202 SW GENERATOR FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 GENERATOR WOULD NOT COME ON LINE. SENT TO MASCO FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 2002082100021 20020821 00021 SW 2002 8 21 HEEA080632 1 20020729 A 2421 51509002R CONTROL UNIT BELL 412 412 1182202 SW NR 2 GENERATOR FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6559Z 36019 NR 2 GENERATOR WILL NOT COME ON LINE. 1 G 7 2 4U H4SW 2002082100023 20020821 00023 2002 8 21 HEEA080634 4 20020729 A 3416 6221205004 INDICATOR BELL 412 412 1182202 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1202T 33112 INDICATOR ALTERNATES BETWEEN SELF TEST AND NORMAL INDICATION DURING FLIGHT REGIMES ONLY. 1 G 7 2 4U H4SW 2002082100024 20020821 00024 2002 8 21 HEEA080635 4 20020729 A 3416 6223201001 INDICATOR BELL 412 412 1182202 SW RADIO ALTIMETER MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1202T 33112 ABOVE 2500 FEET INDICATOR READS 50 FEET AND FLAG APPEARS. SENT TO BROKER TO BE SOLD AS IS. 1 G 7 2 4U H4SW 2002082100025 20020821 00025 NM 2002 8 21 0202646743 1 20020808 A 5313 STRINGER BOEING 747 747249F 1384849 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 643NW 22245 During "M" check found crack on stringer 42L at BS 1730. Repaired per EA 67-191497. 2 L 7 4 4F A20WE 2002082100026 20020821 00026 NM 2002 8 21 0202656743 1 20020802 A 5712 RIB BOEING 747 747249F 1384849 NM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 643NW 22245 During "M" check found corrosion on the upper surface of left wing leading edge rib at wing station 1339.75. Repaired pe r EA 67-191214. 2 L 7 4 4F A20WE 2002082100027 20020821 00027 SW 2002 8 21 HEEA080637 1 20020729 A 2913 SEAL BELL 412 412 1182202 SW HYD PUMP LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 107X AU30D14333F 33113 HYDRAULIC PUMP DRIVE SEAL LEAKING. 1 G 7 2 4U H4SW 2002082100028 20020821 00028 EU 2002 8 21 02232320 1 20020820 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 320UE 41043 During preflight inspection, the crew reported that the emergency floor track lights at seat row 6 and 7 were inoperativ e. Maintenance personnel secured the connector for the emergency floor track lights. An operational check was satisfac tory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002082100029 20020821 00029 EA 2002 8 21 HEEA080638 2 20020729 A 7240 6854255 DRAIN VALVE BELL 412 412 1182202 SW PWA PT6T PT6T3 52045 EA ENGINE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 ENGINE BURNER DRAIN VALVE WILL NOT CLOSE - CORROSION. REPAIRED. 1 G 7 2 4U 4 U H4SW E22EA 2002082100031 20020821 00031 SW 2002 8 21 HEEA080640 1 20020730 A 2820 70009H015C152A SLEEVE BELL 206 206L3 1182108 SW HOSE ASSY CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 979BH 51403 HOSE ASSY SLEEVE CORRODED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002082100032 20020821 00032 NE 2002 8 21 2002F00806 2 20020802 A 7200 ENGINE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LEFT POWER LOSS G AMTA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 11 514AT 27971 31749 FLIGHT NUMBER 935. LEFT ENGINE EPR LAGGING ON TAKEOFF, WILL NOT PRODUCE REQUIRED EPR. UNLATCHED BOTH EEC'S AND TAKEOFF EPR WAS ACHIEVED. MAINTENANCE TROUBLESHOT PER FIM 73-21-00 BITE EEC (LT) NO FAULTS NOTED AT THIS TIME. PER FIM RETURNE D AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002082100033 20020821 00033 NE 2002 8 21 2002F00807 2 20020802 A 7200 ENGINE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LEFT POWER LOSS G AMTA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 11 514AT 27971 31749 FLIGHT NUMBER 935. LEFT ENGINE EPR LAGGING ON TAKEOFF, WILL NOT PRODUCE REQUIRED EPR. UNLATCHED BOTH EEC'S AND TAKEOFF EPR WAS ACHIEVED. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE TROUBLESHOT PER FIM 73-21-00 BITE EEC (LT) NO FAULTS NOT ED AT THIS TIME. PER FIM RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002082100034 20020821 00034 NE 2002 8 21 2002F00808 2 20020803 A 7200 ENGINE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LEFT POWER LOSS G AMTA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 GL 11 514AT 27971 31749 DURING SCHEDULED MAINTENANCE LEFT ENGINE WOULD NOT MAKE TAKEOFF POWER WITH EEC'S ON. ENGINE MAKES TAKEOFF POWER WITH EE C'S OFF. AIR CARRIER INVESTIGATING SINCE THIS IS A REPETITIVE DISCREPANCY. 2 L 7 2 4F 4 F RT A2NM E12EU 2002082100035 20020821 00035 WP 2002 8 21 ABXA020076 1 20020812 A 2120 DUCT DOUG DC9 DC932 3022066 WP A/C BAY DISCONNECTED A ABXA O OTHER S AFFECT SYSTEMS CR CRUISE 1 GL 23 982AX 47317 AT FL 350, CABIN ALTITUDE INCREASED TO 9,500 ALONG WITH THE RIGHT GENERATOR TRIPPING OFF LINE. RESET GENERATOR. PERFOR MED DESCENT TO 14,000 CABIN ALTITUDE WAS REGAINED AT APPROXIMATELY 17,000 TO 18,000. PACK PRESSURE NORMAL AS WELL AS EL ECTRICAL PARAMETERS AT TIME OF THE PRESSURIZATION PROBLEM. PERFORMED LEAK CHECK OF THE LEFT AND RIGHT AC PACKS AND DUCT S. FOUND RIGHT AC DUCT JUST AFT OF COALESCER BAG DISCONNECTED AND COALESCER BAG MISSING. INSTALLED NEW COALESCER AND R ECONNECTED DUCT. PERFORMED ENGINE RUN AND OPS CHECK OF RIGHT GENERATOR. NO DEFECTS NOTED. ALSO PRESSURIZED AIRCRAFT W ITH RIGHT PACK. NO FURTHER LEAKS OR DEFECTS NOTED IAW DC9 MM 21-20-02 AND 21-00-00. 2 L 7 2 4F A6WE 2002082100036 20020821 00036 WP 2002 8 21 AMTA200200992 1 20020805 A 5320 BEAM LKHEED 1011 1011385115 5265015 WP FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 194AT 193B1230 LOWER GALLEY BOXBEAM IN FRONT OF LIFTS CORRODED, LEVEL TWO (2) CORROSION. 2 L 7 3 4F A23WE 2002082100037 20020821 00037 WP 2002 8 21 AMTA200200994 1 20020806 A 3350 110049 CHARGER LKHEED 1011 10113851 5265010 WP CABIN FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 186AT 193C1074 ZONE A LEFT HAND SIDE ROW 1-7 AND RIGHT SIDE 2-7 EGRESS LIGHTS OUT. 2 L 7 3 4F A23WE 2002082100038 20020821 00038 WP 2002 8 21 AMTA200200997 1 20020806 A 5754 RIB LKHEED 1011 1011385115 5265015 WP L/E SLAT CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 194AT 193B1230 6R SLAT 4TH RIB OUTBOARD FROM INBOARD END CRACKED. 2 L 7 3 4F A23WE 2002082100039 20020821 00039 WP 2002 8 21 AMTA200200998 1 20020806 A 5754 RIB LKHEED 1011 1011385115 5265015 WP L/E SLAT CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 194AT 193B1230 6R SLAT 4TH RIB OUTBOARD FROM INBOARD END CRACKED. 2 L 7 3 4F A23WE 2002082100040 20020821 00040 WP 2002 8 21 AMTA200201016 1 20020807 A 2780 472085119 COMPARATOR LKHEED 1011 1011385115 5265015 WP L/E SLAT FAILED A AMTA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 GL 11 198AT 193B1111 ON FLAP EXTENSION, FLAP/SLAT LOCK LIGHT CAME ON, SLAT STAYED RETRACTED. 2 L 7 3 4F A23WE 2002082100041 20020821 00041 WP 2002 8 21 AMTA200201018 1 20020809 A 5754 RIB LKHEED 1011 1011385115 5265015 WP L/E SLAT CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 194AT 193B1230 6R SLAT INBOARD RIB CRACKED AT AFT END CRACK LENGTH 0.500. 2 L 7 3 4F A23WE 2002082100042 20020821 00042 WP 2002 8 21 AMTA200201058 1 20020814 A 3350 LIGHT LKHEED 1011 10113853 5265020 WP EXTERIOR INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 162AT 1220 R3 + P4A EMERGENCY EXTERIOR EXIT LIGHTS INOP. 2 L 7 3 4F A23WE 2002082100043 20020821 00043 NM 2002 8 21 AMTA200201059 1 20020809 A 5310 DOOR FRAME LKHEED 1011 1011 N/A-SDR NM FUSELAGE CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 195AT 193C1041 FWD FUSELAGE SECTION, RT ECS BAY CUTOUT FRAME FOR ACCESS DOOR CRACKED WITH CORROSION AT STAND OFF ATTACH POINT JUST FORW ARD OF FORWARD HINGE ARM ATTACH POINT, TOP FWD OF O/B FRAME FORMER, TM3. REMOVED AND REPLACED CRACKED AND CORRODED CHOR D ON O/B SIDE OF RT ECS BAY CUTOUT. 2 L 7 3 4F RT A23WE 2002082100044 20020821 00044 SW 2002 8 21 HEEA080641 1 20020730 A 2820 70009H145C272A HOSE BELL 206 206L3 1182108 SW FUEL DIST LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 6251X 51552 FUEL HOSE LEAKS. SCRAPPED. 1 G 7 1 3U H2SW 2002082100045 20020821 00045 SW 2002 8 21 HEEA080642 1 20020730 A 2820 SLEEVE BELL 206 206L3 1182108 SW FUEL HOSE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 979BH 51403 FUEL HOSE ASSY SLEEVE CORRODED. SCRAPPED. 1 G 7 1 3U H2SW 2002082100046 20020821 00046 SW 2002 8 21 HEEA080643 1 20020730 A 2820 70009J000V570A HOSE BELL 206 206L3 1182108 SW FUEL DIST CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 979BH 51403 CORROSION WHERE BRAIDED LINE GOES INTO SLEEVE. REPLACED WITH SERVICEABLE HOSE. 1 G 7 1 3U H2SW 2002082100047 20020821 00047 SW 2002 8 21 HEEA080644 1 20020730 A 2820 70030J000D465 HOSE BELL 206 206L3 1182108 SW FUEL DIST COLLAPSED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4835 51131 FUEL HOSE COLLAPSED. SCRAPPED. 1 G 7 1 3U H2SW 2002082100048 20020821 00048 SW 2002 8 21 HEEA080645 1 20020730 A 2910 70053H000A100A HOSE BELL 206 206L3 1182108 SW HYD SYSTEM FAILED E HEEA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 03 8590X 51494 PRESSURE HOSE FROM THE HYD PUMP TO AN AIRFRAME HAND LINE FAILED INTERNALLY IN FLIGHT CAUSING LOSS OF HYD FLUID. SCRAPPED . 1 G 7 1 3U H2SW 2002091200146 20020912 00146 NM 2002 9 12 AWXA200200762 1 20020818 A 3234 114079010AB SELECTOR VALVE AIRBUS A319 A319132 3930340 NM LANDING GEAR FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 802AW 17410 7502 924 AFTER TAKEOFF WITH GEAR RETRACTED, ECAM IND L/G NOT UPLOCKED & L/G DOOR NOT CLOSED MESSAGE. RECYCLED, RECEIVED MESSAGE, RECYCLED AGAIN & GEAR RETRACTED NORMALLY, TURNED BACK. PFR FAILURES IND NLG UPLOCK PROXIMITY SENSORS (12GA & 13GA), DO WNLOCK (18GA & 19GA), FOLLOWED BY TARGET POSITION ON ALL SENSORS. T/S MANUAL WARNINGS PLUS FAILURES LED TO 32-31-00-810 -808, SELECTOR VALVE (40GA) FAULTY. R&R L/G SELECTOR VALVE (40GA). T/S FOUND L/G DOOR SELECTOR VALVE (41GA) HOT, REPLA CED L/G DOOR SELECTOR VALVE (41GA). LEAK & OPS CHECK GOOD. VENDOR BENCH TEST OF L/G DOOR SELECTOR VALVE, NO FAULT FOUN D. L/G SELECTOR VALVE, CONFIRMED FAILURE AS INTERNAL LEAKAGE. UNIT RESEALED. 2 L 7 2 4F RT A28NM 2002082100049 20020821 00049 SW 2002 8 21 HEEA080646 1 20020730 A 6320 70061G000X116A HOSE BELL 206 206B3 1181506 SW M/R GEARBOX LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2268V 3605 FWU RETURN LINE FROM TRANSMISSION TO FIREWALL LEAKING. SCRAPPED. 1 G 7 1 3U H2SW 2002082100050 20020821 00050 2002 8 21 HEEA080647 4 20020730 A 3442 80510800001 CONTROL HEAD BELL 206 206L3 1182108 SW WX RADAR SYS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 31077 51520 WX RADAR CONTROL HEAD HAS A FATAL ERROR CODE FOR THE POWER SUPPLY. 1 G 7 1 3U H2SW 2002082100051 20020821 00051 NM 2002 8 21 USA2002F00068 1 20020727 A 3241 426412 CONTROL UNIT BOEING 757 7572B7 1384964 NM ANTISKID CU FAULTY A USAA K NONE O OTHER LD LANDING 1 EA 19 620AU 19412 27199 UPON LANDING, CREW REPORTED THE NORMAL BRAKES WERE VERY SOFT AS THE ANTISKID SYSTEM WAS ON MEL. BRAKE PEDALS HAD TO BE COMPLETELY DEPRESSED TO MAKE TURNOFF. FLIGHT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPL ACED THE ANTISKID CONTROL UNIT AND PERFORMED OPERATIONAL CHECK OF ANTISKID SYSTEM. NO FAULTS FOUND. REMOVED ANTISKID M EL. 2 L 7 2 4F RT A2NM 2002082100052 20020821 00052 2002 8 21 HEEA080648 4 20020730 A 3442 80510800001 CONTROL HEAD BELL 206 206L3 1182108 SW WX RADAR SYS WILL NOT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 31801 51074 WX RADAR CONTROL HEAD WILL NOT TEST OR PAINT TARGETS. 1 G 7 1 3U H2SW 2002082100053 20020821 00053 2002 8 21 HEEA080649 4 20020730 A 3445 80511400003 CONTROL UNIT BELL 206 206L3 1182108 SW WX RADAR DAMAGED E K NONE L NO TEST IN INSP/MAINT 1 SW 03 ANTI COLLISION AVOIDANCE SYSTEM CONTROL HEAD HAS IT`S FAN RUBBING INSIDE OF UNIT. 1 G 7 1 3U H2SW 2002082100054 20020821 00054 2002 8 21 HEEA080650 4 20020730 A 3422 843676 INDICATOR BELL 206 206L3 1182108 SW COCKPIT INOPERATIVE E HEEA O OTHER L NO TEST NR NOT REPORTED 1 SW 03 6251X 51552 VSI WILL NOT RESPOND TO ALTITUDE CHANGES. 1 G 7 1 3U H2SW 2002082100055 20020821 00055 SW 2002 8 21 HEEA080651 1 20020730 A 7921 8534998 OIL COOLER BELL 206 206B3 1181506 SW ENGINE MALFUNCTIONED E O OTHER M OVER TEMP NR NOT REPORTED 1 SW 03 2753F 2729 OIL TEMPERATURE AT 100 DEGREES NEAR RED LINE IN FLIGHT. 1 G 7 1 3U H2SW 2002082100056 20020821 00056 SW 2002 8 21 HEEA080652 1 20020730 A 7921 8543909 OIL COOLER BELL 206 206L3 1182108 SW ENGINE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 31077 51520 ENGINE OIL COOLER LEAKING. 1 G 7 1 3U H2SW 2002082100057 20020821 00057 SW 2002 8 21 HEEA080653 1 20020730 A 7921 8543909 OIL COOLER BELL 206 206L3 1182108 SW ENGINE MALFUNCTIONED E HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 21497 51518 ENGINE OIL TEMPERATURE NEEDLE INDICATES JUST BELOW THE "HIGH SIDE" RED LINE IN CRUISE FLIGHT. 1 G 7 1 3U H2SW 2002082100058 20020821 00058 NM 2002 8 21 C1HA200282015 1 20020812 A 2410 O-RING BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE NR 3 ENGINE LEAKING A C1HA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 15 682CA 22019 688091 ENGINE NR 3 OIL QUANTITY DROPPED TO 1.5 GALLONS. ENGINE OIL TEMPERATURE WAS 90 DEGREES, OIL PRESSURE WAS 44 AND OIL QUA NTITY CONTINUED TO DROP TO .5 GALLONS. TEMPERATURE BEGAN TO RISE AND PRESSURE BEGAN TO DROP, EXECUTED A PRECAUTIONARY S HUTDOWN. FOUND O-RING ON CSD FRONT FLANGE LEAKING. REINSTALLED CSD ASSEMBLY IAW MM. OPERATIONAL AND LEAK CHECK OF CSD NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2002082100059 20020821 00059 SW 2002 8 21 HEEA080654 1 20020730 A 7921 8543909 OIL COOLER BELL 206 206L3 1182108 SW ENGINE FAILED E HEEA O OTHER M OVER TEMP NR NOT REPORTED 1 SW 03 31077 51520 ENGINE OIL TEMPERATURE NEAR RED LINE. 1 G 7 1 3U H2SW 2002082100060 20020821 00060 SW 2002 8 21 HEEA080655 1 20020730 A 7921 8543909 OIL COOLER BELL 206 206L3 1182108 SW ENGINE FAILED E HEEA O OTHER M OVER TEMP NR NOT REPORTED 1 SW 03 81SP 51029 ENGINE OIL TEMPERATURE RUNNING AT UPPER SCALE AND ABOVE NORMAL. 1 G 7 1 3U H2SW 2002082100061 20020821 00061 NM 2002 8 21 DL72S020819 1 20020716 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM T/E FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 NR 2 MID FLAP REMOVED FROM AC 533 DURING HMV. AFT SPAR RAIL REPAIRED PER M/M 57-52-0 FIG 802. 2 L 7 3 4F A3WE 2002082100062 20020821 00062 SW 2002 8 21 HEEA080656 1 20020730 A 7921 8534998 OIL COOLER BELL 206 206B3 1181506 SW ENGINE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 22743 3624 OIL COOLER LEAKING. 1 G 7 1 3U H2SW 2002082100063 20020821 00063 SW 2002 8 21 HEEA080657 1 20020730 A 7921 8543909 OIL COOLER BELL 206 206L3 1182108 SW ENGINE FAILED E HEEA O OTHER M OVER TEMP NR NOT REPORTED 1 SW 03 42EA 51542 OIL COOLER PRODUCING HIGH ENGINE OIL TEMPERATURE. 1 G 7 1 3U H2SW 2002082100064 20020821 00064 SW 2002 8 21 HEEA080658 1 20020730 A 7921 8543909 OIL COOLER BELL 206 206L3 1182108 SW ENGINE FAILED E HEEA O OTHER M OVER TEMP NR NOT REPORTED 1 SW 03 6603X 51412 OIL COOLER PRODUCING HIGH ENGINE OIL TEMPERATURE. 1 G 7 1 3U H2SW 2002082100065 20020821 00065 NM 2002 8 21 DL72S020828 1 20020718 A 5532 SKIN BOEING 727 727232 1384082 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND ON E-1 LETTER CK SKIN CRACKED AT BASE OF VERTICAL STAB RT SIDE ABOVE FWD END OF NUMBER 2 ENG CUTOUT AT STR 10. RE PAIR PER MM 55-30-000-8. 2 L 7 3 4F A3WE 2002082100066 20020821 00066 SW 2002 8 21 HEEA080659 1 20020730 A 7921 8543909 OIL COOLER BELL 206 206L3 1182108 SW ENGINE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 4835 51131 ENGINE OIL COOLER LEAKING. 1 G 7 1 3U H2SW 2002082100067 20020821 00067 GL 2002 8 21 HEEA080660 2 20020730 A 7420 9048222105 LEAD BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL IGNITER CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 42EA 51542 INGNITER LEAD CHAFED. REPAIRED. 1 G 7 1 3U 3 U H2SW E1GL 2002082100068 20020821 00068 2002 8 21 HEEA080661 4 20020730 A 2312 9710831 RADIO BELL 206 206B3 1181506 SW VHF SYSTEM FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 VHF INOPERATIVE. FOUND UNIT WON'T TRANSMIT IN VHF MODE AND RECEIVER CUTS OUT WHEN VARYING FROM 3-5KHZ IN VHF AND UHF MOD ES. 1 G 7 1 3U H2SW 2002082100069 20020821 00069 SW 2002 8 21 HEEA080662 1 20020730 A 3340 A490ATSDF1428 POWER SUPPLY BELL 206 206L4 1182110 SW ANTI COLLISION FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 7074W 52033 ANTI COLLISION LIGHT INOPERATIVE. REPLACED POWER SUPPLY WITH SERVICEABLE PART. 1 G 7 1 3U NC H2SW 2002082100070 20020821 00070 NM 2002 8 21 DL72S020846 1 20020719 A 5754 SPAR BOEING 727 727232 1384082 NM L/E SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 546DA 22677 AT F-I LETTER CK FOUND .375 INCH CRACK NR 2 SLAT AT TAI DUCT CUTOUT, INBOARD CORNER. REPAIRED PER M/M 57-54-000-8 FIG 8 02A. 2 L 7 3 4F A3WE 2002082100071 20020821 00071 SW 2002 8 21 HEEA080663 1 20020730 A 3340 A490ATSDF1428 POWER SUPPLY BELL 206 206L3 1182108 SW ANTI COLLISION INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6748D 51106 ANTI COLLISION LIGHT POWER SUPPLY INOPERATIVE. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002082100072 20020821 00072 SW 2002 8 21 HEEA080664 1 20020730 A 3340 A490ATSDF1428 POWER SUPPLY BELL 206 206L3 1182108 SW ANTI COLLISION FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6251X 51552 ANTI COLLISION LIGHT POWER SUPPLY WILL NOT CHARGE UP OR DISCHARGE. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002082100073 20020821 00073 NM 2002 8 21 DL72S020860 1 20020720 A 5532 65174631 SKIN BOEING 727 727232 1384082 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 THE LT BOX SKIN OF THE VERTICAL STABILIZER WAS FOUND WITH A CRACK EMANATING FROM A FASTENER COMMON TO THE REAR SPAR LOCA TED 1 INCH ABOVE THE FUSELAGE SKIN INTERFACE. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383575-14, REV A. 2 L 7 3 4F A3WE 2002082100074 20020821 00074 2002 8 21 HEEA080665 4 20020730 A 2350 AA34200 RADIO BELL 206 206L3 1182108 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4835 51131 INTERGRATED AUDIO SYSTEM HAS NO MIC AUDIO. 1 G 7 1 3U H2SW 2002082100076 20020821 00076 NM 2002 8 21 DL72S020865 1 20020723 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 523DA 21583 EMERGENCY EXIT LIGHT OVER AFT RT DOOR INOP. REPLACED BATTERY AND RACK. ALSO SECURED GROUND. 2 L 7 3 4F A3WE 2002082100077 20020821 00077 2002 8 21 HEEA080667 4 20020730 A 2350 AA38300 AMPLIFIER BELL 206 206L1 1182107 SW COCKPIT INTERFERENCE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5014V 45217 ICS AMPLIFIER CAUSES LOUD BUZZ IN HEADSET. 1 G 7 1 3U H2SW 2002082100078 20020821 00078 SW 2002 8 21 HEEA080668 1 20020730 A 3246 206053184114 SKID BELL 206 206L3 1182108 SW MLG CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251X 51552 MLG SKID TUBE HAS CORROSION. SCRAPPED. 1 G 7 1 3U H2SW 2002082100079 20020821 00079 NM 2002 8 21 DL72S020866 1 20020723 A 3350 6012541 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 523DA 21583 LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY RACK. 2 L 7 3 4F A3WE 2002082100080 20020821 00080 SW 2002 8 21 HEEA080669 1 20020730 A 7714 AG44A202 TACH GENERATOR BELL 206 206L3 1182108 SW N2 INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3116P 51530 N2 INDICATOR INOPERATIVE. REPAIRED. 1 G 7 1 3U H2SW 2002082100081 20020821 00081 NM 2002 8 21 DL72S020890 1 20020727 A 5330 65C139131 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 DURING LAYOVER, MAINTENANCE FOUND A 1 INCH LONG CRACK IN THE FUSELAGE SKIN BETWEEN TWO FASTENERS AT S-30 BETWEEN FS 990 AND 1009. THE SUBJECT CRACK WAS REMOVED AND AN EXTERNAL DOUBLER INSTALLED. THE REPAIR INCORPORATED AN EXISTING REPAIR INSTALLED PER PREVIOUS ER/A 331904-14 AT S-29L. 2 L 7 3 4F A3WE 2002082100082 20020821 00082 SW 2002 8 21 HEEA080670 1 20020730 A 7920 AN8334J FITTING BELL 206 206L1 1182107 SW ENGINE OIL CRACKED E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 27766 45312 OIL LEAKING FROM ELBOW JAMB NUT. FOUND FITTING CRACKED AT JAMB NUT FLANGE. CRACK RUNS AROUND RADIUS AND MEASURES APPRO XIMATELY 1/4 IN LENGTH. REPLACED FITTING. 1 G 7 1 3U H2SW 2002082100084 20020821 00084 NM 2002 8 21 DL72S020895 1 20020801 A 3350 S106 BATTERY BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8890Z 21859 EMERGENCY LIGHT OVER 1L DOOR WILL NOT LIGHT. REPLACED BATTERIES, OP CHECKS NORMAL. 2 L 7 3 4F RT A3WE 2002082100085 20020821 00085 GL 2002 8 21 HEEA080671 2 20020730 A 7261 B4093 CHIP DETECTOR BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 31801 51074 CHIP DETECTOR DID NOT PASS INSPECTION REQUIREMENT. SCRAPPED. 1 G 7 1 3U 3 U H2SW E1GL 2002082100086 20020821 00086 SW 2002 8 21 HEEA080672 1 20020730 A 2432 BD131 CONNECTOR BELL 206 206L1 1182107 SW BATTERY BURNED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5019F 45244 BATTERY CONNECTOR BURNED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002082100087 20020821 00087 SW 2002 8 21 HEEA080673 1 20020730 A 2840 BSE20630G TRANSDUCER BELL 206 206L1 1182107 SW FUEL PRESSURE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5007N 45184 WHEN SWITCH IS TURNED ON, THE FUEL PRESSURE WILL GO UP EVEN WITH THE BOOST PUMPS OFF. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002082100088 20020821 00088 SW 2002 8 21 HEEA080674 1 20020730 A 2840 BSE20630G TRANSDUCER BELL 206 206L3 1182108 SW FUEL PRESSURE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4835 51131 FUEL PRESSURE GAUGE SHOWS FUEL PRESSURE WITH BOOST PUMPS OFF. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002082100089 20020821 00089 GL 2002 8 21 HEEA080675 2 20020730 A 7421 CH34168 IGNITER BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL ENGINE DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22743 3624 IGNITER PRODUCING A WEAK SPARK. ERODED INSULATOR. SCRAPPED. 1 G 7 1 3U 3 U H2SW E4CE 2002082100090 20020821 00090 2002 8 21 HEEA080677 4 20020730 A 3120 CK726424 CLOCK BELL 206 206B3 1181506 SW COCKPIT INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2268V 3605 CLOCK IS INTERMITTENTLY INOPERATIVE. SCRAPPED. 1 G 7 1 3U H2SW 2002082100091 20020821 00091 NE 2002 8 21 DL72S020917 2 20020806 A 7510 320115DALFH VALVE BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE WORN A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 519DA 21470 687679 AIR RETURN TO CVG FOR HIGH OIL TEMP NUMBER 1 ENG. REPLACED FUEL HEAT VALVE, OP CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2002082100092 20020821 00092 2002 8 21 HEEA080678 4 20020730 A 3423 C2300DL4B COMPASS BELL 206 206L1 1182107 SW COCKPIT LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 5007Q 45187 COMPASS LEAKING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 2002082100093 20020821 00093 2002 8 21 HEEA080679 4 20020730 A 3423 C2300DL4B COMPASS BELL 206 206L3 1182108 SW COCKPIT LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 6748D 51106 COMPASS LEAKING FLUID. 1 G 7 1 3U H2SW 2002082100094 20020821 00094 NE 2002 8 21 DL72S020920 2 20020807 A 7321 7436025 FUEL CONTROL BOEING 727 727225A 1384077 NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CL CLIMB 1 SO 27 805EA 54504 82237 22436 700639 ON CLIMBOUT AUS NUMBER 3 ENGINE SLOWLY ROLLED BACK TO IDLE. ENGINE SHUTDOWN ON FINAL DFW. REPLACED FUEL PUMP AND FUEL CONTROL RIGGED AND TRIMMED ENGINE, ALL OPS CHECK NORMAL. 2 L 7 3 4F 4 F RT A3WE E2EA 2002082100095 20020821 00095 2002 8 21 DL72W020784 4 20020710 A 3442 TRANSCEIVER BOEING 727 727247 138408F NM WEATHER RADAR FAILED A DALA O OTHER O OTHER CR CRUISE 1 SO 27 295WA 22532 WX RADAR PAINTS NO RETURNS NEITHER GROUND NOR PRECIP. REPLACED WX TRANSCEIVER. 2 L 7 3 4F A3WE 2002082100096 20020821 00096 2002 8 21 HEEA080680 4 20020730 A 3423 WIRE BELL 206 206B3 1181506 SW COMPASS BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2268V 33293M 3605 ONE WIRE MISSING FOR LIGHT AND OTHER WIRE BROKEN. 1 G 7 1 3U H2SW 2002082100097 20020821 00097 NM 2002 8 21 DL72W020852 1 20020721 A 3350 1000677REV LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 295WA 22532 EMERGENCY LIGHT ABOVE 2R DOOR FAILED TO OPERATE DURING EMERGENCY LIGHT SYSTEM TEST DURING LAYOVER CHECK. REPLACED EMERG ENCY LIGHT ASSY AND BATTERIES, OP CHECKS NORMAL. 2 L 7 3 4F A3WE 2002082100101 20020821 00101 2002 8 21 HEEA080685 4 20020730 A 3120 CK726424 CLOCK BELL 206 206B3 1181506 SW COCKPIT INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2268V 3605 CLOCK INTERMITTENTLY STOPS AND RUNS SLOW. SCRAPPED. 1 G 7 1 3U H2SW 2002082100102 20020821 00102 2002 8 21 HEEA080686 4 20020730 A 3120 CK726424 CLOCK BELL 206 206B3 1181506 SW COCKPIT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22743 3624 UNABLE TO ADJUST TIME ON CLOCK. ADJUSTMENT KNOB KEEPS COMING LOOSE. TIGHTENED KNOB, BUT IT KEEPS COMING LOOSE. SCRAPPE D. 1 G 7 1 3U H2SW 2002082100103 20020821 00103 2002 8 21 HEEA080687 4 20020730 A 3120 CK726424 CLOCK BELL 206 206L3 1182108 SW COCKPIT INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 31801 51074 CLOCK INTERMITTENTLY INOPERATIVE. SCRAPPED. 1 G 7 1 3U H2SW 2002082100104 20020821 00104 NE 2002 8 21 DL72W020883 2 20020728 A 7200 ENGINE BOEING 727 727247 138408F NM PWA JT8 JT8D15A 52051 NE NR 1 OUT OF TRIM A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 292WA 75827 22110 687607 REJECTED TAKEOFF. AIRSPEED APPROX 130 KIAS LIGHT BRAKING. EVERYTHING ELSE NORMAL WITH ABORT. COULD NOT GET NORMAL POW ER EPR OF 2.06 OUT OF NUMBER 1 ENGINE. N1 AND EGT NORMAL. FIRE DEPT INSPECTED BRAKES, CHECKED OK. REMOVED AND REPLACE D EPR TRANSMITTER NR 1 LEAK CKS GOOD. NO HELP, EPR STILL LOW, ALONG WITH ALL OTHER ENGINE INDICATIONS. TRIMMED NR 1, 2 , 3 ENGINE. RAN ENGINE PER PFHB TO T/O PWR. CHECKS OK. ALL ENGINES INDICATE NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2002082100105 20020821 00105 NM 2002 8 21 DL72W020905 1 20020803 A 3350 RPS1 POWER SUPPLY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 295WA 22532 ON LAYOVER FOUND F/C EMERGENCY TRACK LIGHTS INOP. REPLACED F/C EMERGENCY TRACK LIGHT POWER SUPPLY. TRACK LIGHTS CHECK NORMAL. 2 L 7 3 4F A3WE 2002082100106 20020821 00106 NM 2002 8 21 DL733020812 1 20020715 A 2910 AS11608026 HYDRAULIC LINE BOEING 737 737347 1384647 NM HYD SYSTEM RUPTURED A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 3301 23181 LOSS OF B-SYSTEM PRESSURE IN FLIGHT. REPLACED B-PUMP HYD SUPPLY LINE IN RT WHEEL WELL . ALSO REPLACED NR 2 ENGINE HYD PUMP AND CASE DRAIN FILTER SYSTEM, OPS AND LEAKS CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2002082100107 20020821 00107 NM 2002 8 21 DL733020861 1 20020720 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952WP 23378 THE BONDED SKIN AND UNDERLYING BEARSTRAP WERE FOUND DENTED AND GOUGED AT THE FWD EDGE OF THE C1 CARGO DOOR OPENING AT FS 440 NEAR STRINGER 23R. THE DAMAGE WAS REMOVED IN ALL LAYERS. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL DOUBLERS PER ER/ A 383504-14, REV A. 2 L 7 2 4F RT A16WE 2002091100074 20020911 00074 NM 2002 9 11 F3LA200200217 1 20020820 A 5512 SKIN BOEING 737 737317 138447P NM HORIZ STAB DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 46438 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED DENT IN RT HORIZONTAL STAB LEADING EDGE AT BS 121.59. CUT OUT DAMAGE, AND FABRICA TED AND INSTALLED REPAIR DOUBLER PER SRM 55-10-01. 2 L 7 2 4F RT A16WE 2002082100108 20020821 00108 NM 2002 8 21 DL733020874 1 20020726 A 2751 1817389 TRANSMITTER BOEING 737 737347 1384647 NM T/E FLAP MALFUNCTIONED A DALA O OTHER O OTHER AP APPROACH 1 SO 27 2310 23596 DURING FLAP EXTENSION RIGHT FLAP IND REMAINED NEAR ZERO AND LEFT INDICATED NEAR ONE DEGREE. L/E INDICATIONS NORMAL. FO LLOWED QRH PROCEDURES AND LANDED AT 170 KIAS. REPLACED RIGHT T/E FLAP POSITION TRANSMITTER, OPS NORMAL. 2 L 7 2 4F RT A16WE 2002082100109 20020821 00109 EA 2002 8 21 COMA0260488 1 20020819 A 3230 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 805CA 6036 7354 FLIGHT 5232 GEAR DISAGREE WARNING AFTER T/O.REPLACED THE MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002082100110 20020821 00110 EA 2002 8 21 COMA0260489 1 20020818 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER O OTHER CL CLIMB 1 SO 01 708CA 6564 928 7235 FLIGHT 5322 GEAR DISAGREE MESSAGE - NLG SLOW TO RETRACT.REPLACED NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002082100111 20020821 00111 EA 2002 8 21 COMA0260490 1 20020818 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 954CA 7100 FLIGHT 6008 FLAPS FAILED AT 8 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002091100075 20020911 00075 NM 2002 9 11 F3LA200200218 1 20020820 A 5315 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION 1 FT LEFT OF CENTER LINE FLOORBEAM AT BS 294.5. FOUND CORROSION ON FLOO RBEAM AT BS 294.5 TO BE OUT OF LIMITS FROM LBL 19.5 TO RBL 60 PER SRM 53-10-51. REMOVED THIS SECTION OF THE TOP CHORD, FABRICATED REPLACEMENT CHORD AND INSTALLED PER SOPM 26-41-02 AND SRM 53-10-51. 2 L 7 2 4F RT A16WE 2002082100112 20020821 00112 EA 2002 8 21 COMA0260491 1 20020719 A 5414 SKIN CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 959CA 7116 FASTENER HOLE ON PNL 422EB IS DAMAGED.REAMED HOLE TO .4045" AND INSTALLED A FREEZE PLUG FABRICATED FROM AMS 5659 PO #232 83/1 AND REPLACED PROTECTIVE FINISH. WORK WAS PERFORMED I/A/W WVAC 601R-54-3374B APPROVED BY 8110-3 DATED 07/19/02. REF COMAIR W/O 29767 MAINT LOG PAGE 520539 AND C/O 7116902. 2 L 7 2 4F RT A21EA 2002091100076 20020911 00076 NM 2002 9 11 F3LA200200219 1 20020820 A 5420 DOUBLER BOEING 737 737317 138447P NM NR 1 PYLON CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED NR 1 ENGINE PYLON HOCKEY STICK DOUBLER CRACKED AT AFT LOWER END. FABRICATED AND I NSTALLED NEW DOUBLER PER SRM 51-70-13 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002082100113 20020821 00113 NE 2002 8 21 DL733020877 2 20020727 A 7200 CFM563 ENGINE BOEING 737 737347 1384647 NM GE CFM56 CFM563B1 13802 NE NR 1 OVERTEMP A DALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 27 2310 23596 D00864 ON TAKEOFF (NORMAL POWER) CLIMBOUT BOTH ENGINE INDICATIONS SHOWED RED LIGHT ILLUMINATED ON DIGITAL READOUT AT 970 DEGREE S (C) PLUS ON BOTH ENGINES AT LEAST 5 SECONDS. N1 INDICATES AT ABOUT 96.6. PULLED BACK THROTTLES, RED LIGHT EXTINGUISH ED. REMOVED AND REPLACED BOTH ENGINES DUE TO OVERTEMP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082100114 20020821 00114 NM 2002 8 21 DL733020892 1 20020730 A 2611 72130001008 SMOKE DETECTOR BOEING 737 737347 1384647 NM LAVATORY FAULTY A DALA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 27 2310 23596 LAV SMOKE AMBER LIGHT AND CHIME CAME ON DURING CRUISE FLIGHT. ALL LAVS CHECKED WITH NO SIGN OF SMOKE, FUMES, EXCESSIVE HEAT. CIRCUIT BREAKER PULLED TO SILENCE CHIME. FOUND AFT RT DETECTOR INOP. REPLACED DETECTOR, OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 2002082100115 20020821 00115 NM 2002 8 21 2002F00802 1 20020715 A 2697 UL27185 WIRE HARNESS BOEING 757 75733N 1384931 NM LT ENGINE FAULTY G AMTA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 551TZ 32585 FLIGHT NUMBER 762, DURING GROUND HANDLING EICAS MESSAGE ON STATUS PAGE L ENG FIRE LP 2 RECEIVED. MAINTENANCE REPLACED E NGINE HARNESS FROM D40158P TO DETECTORS TS5032 & TS5030. L ENG FIRE LOOP 2 EXTINGUISHED. 2 L 7 2 4F RT A2NM 2002082100116 20020821 00116 NM 2002 8 21 2002F00803 1 20020715 A 3610 312N53217 DUCT BOEING 757 75723N 1384973 NM BLEED AIR DAMAGED G AMTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 517AT 21286 21286 27973 FLIGHT NUMBER 579, DURING CLIMB RECEIVED R STRUT OH DET 1 FOLLOWED BY R ENG OVERHEAT. AIRCRAFT RETURNED TO DEPARTURE AI RPORT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE HP6 DUCT IN ACCORDANCE WITH MM 36-11-01. 2 L 7 2 4F RT A2NM 2002082100117 20020821 00117 NM 2002 8 21 2002F00804 1 20020725 A 3397 WIRE BOEING 757 75723N 1384973 NM CABIN LOOSE G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 526AT 30735 DURING SCHEDULED MAINTENANCE EMERGENCY EGRESS LIGHTING OUT AT ROW 4ABC TO 10ABC. MAINTENANCE FOUND LOOSE WIRES ON WIRE ASSY AT ROW 4ABC AND RECONNECTED WIRES. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002082100118 20020821 00118 NM 2002 8 21 2002F00805 1 20020721 A 7714 TRANSDUCER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE MALFUNCTIONED G AMTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 11 550TZ 32584 31792 FLIGHT NUMBER 935. DURING TAKEOFF ROLL RIGHT ENGINE LIMITS EXCEEDED. LEFT ENGINE N2-104, N3-100; RIGHT ENGINE N2-101 N O ENGINE SURGES DURING THIS EVENT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE PLA TRANSDUCER IN ACCORDANCE WITH MM 75-32-14. OPERATIONAL CHECK AND ENGINE RUNS GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2002082100119 20020821 00119 NM 2002 8 21 2002F00809 1 20020804 A 3397 WIRE BOEING 757 75723N 1384973 NM CABIN LOOSE G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 519AT 27975 DURING SCHEDULED MAINTENANCE FIRST FIVE EMERGENCY EGRESS LIGHTS WOULD NOT TEST IN THE FORWARD CABIN. MAINTENANCE RECONN ECTED LOOSE WIRE AT ROW 5DEF. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002082100120 20020821 00120 NM 2002 8 21 2002F00810 1 20020806 A 3397 WIRE BOEING 757 75723N 1384973 NM CABIN DISCONNECTED G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 527AT 30886 DURING SCHEDULED MAINTENANCE EGRESS LIGHTS WOULD NOT LIGHT UP AT ROW 15 THROUGH 19. MAINTENANCE RECONNECTED EGRESS LIGH T WIRING AT ROW 15. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002082100121 20020821 00121 NM 2002 8 21 2002F00811 1 20020809 A 3350 LIGHT BOEING 757 75723N 1384973 NM CABIN INOPERATIVE G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 515AT 27598 DURING SCHEDULED MAINTENANCE EMERGENCY EGRESS FLOOR LIGHTS INOP AT AFT LAVS. 2 L 7 2 4F RT A2NM 2002082100122 20020821 00122 NE 2002 8 21 2002F00812 2 20020815 A 7310 FUEL FILTER LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 3 ENGINE DIRTY G AMTA O OTHER J X WARNING INDICATION ENGINE FLAMEOUT DE DESCENT 1 GL 11 188AT 193C1078 10528 ON DESCENT NR 3 ENGINE FUEL PRESSURE LIGHT ON, THROTTLES AT IDLE, ENGINE FLAMED-OUT. PERFORMED EMERGENCY RESTART, OK. REMOVED AND REPLACED NR 3 ENGINE LP FUEL FILTER IAW M/M 73-11-02, PERFORMED LP FUEL PUMP DRIVE TEST 19 OF M/M 71-00-00, OK. 2 L 7 3 4F 4 F A23WE E12EU 2002082100123 20020821 00123 NM 2002 8 21 2002F00813 1 20020809 A 3397 WIRE BOEING 757 75723N 1384973 NM CABIN LOOSE G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 515AT 27598 DURING SCHEDULED MAINTENANCE THE EMERGENCY EGRESS FLOOR LIGHTS WERE INOPERATIVE AT AFT LAVS. MAINTENANCE REPAIRED LOOSE WIRING, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002082100124 20020821 00124 NM 2002 8 21 2002F00814 1 20020721 A 7714 N14FF104 TRANSDUCER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FAULTY G AMTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 11 550TZ 32584 31792 FLIGHT NUMBER 935. DURING TAKEOFF ROLL ENGINE LIMITS EXCEEDED, LEFT ENGINE N2-104, N3-100; RIGHT ENGINE N2-101. NO ENGI NE SURGES DURING THIS EVENT. MAINTENANCE REMOVED AND REPLACED THE PLA TRANSDUCER PER MM 75-32-14 ON THE NR 2 ENGINE. O PERATIONAL CHECKS AND ENGINE RUNS GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2002082100125 20020821 00125 NE 2002 8 21 2002F00815 2 20020813 A 7530 AC67760 SOLENOID BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE MALFUNCTIONED G AMTA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 11 522AT 14000 14000 29330 31604 FLIGHT NUMBER 217. DURING GO-AROUND AT LAS, RIGHT ENGINE WENT TO EGT 858. MAINTENANCE REMOVED AND REPLACED LEFT IP BLE ED VALVE SOLENOID IN ACCORDANCE WITH MM 75-32-03. 2 L 7 2 4F 4 F RT A2NM E12EU 2002082100126 20020821 00126 NE 2002 8 21 2002F00816 2 20020814 A 7200 ENGINE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RIGHT OVERTEMP G AMTA K NONE M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 GL 11 522AT 29330 31605 FLIGHT NUMBER 710. ON TAKEOFF AT LAS THE RIGHT ENGINE EGT REACHED 863 BEFORE PULLING BACK. 2 L 7 2 4F 4 F RT A2NM E12EU 2002082100127 20020821 00127 WP 2002 8 21 2002F00817 1 20020528 A 5320 STRUCTURE LKHEED 1011 1011385115 5265015 WP FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 198AT 193B1111 C3 CARGO PIT HAS CORRODED NUT PLATES ON LOWER AFT FLOOR FRAME. REMOVED AND REPLACED RT TEE CAP IAW SRM 51-40-01. CORRO SION LEVEL 2. 2 L 7 3 4F A23WE 2002082100128 20020821 00128 NE 2002 8 21 2002F00818 2 20020817 A 7200 ENGINE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RIGHT OVERTEMP G AMTA K NONE M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 GL 11 522AT 29330 31605 FLIGHT NUMBER 716. DURING TAKEOFF AT LAS RIGHT ENGINE EGT 855C FOR 15 SECONDS WITH ELC ON, EGT RETURNED TO WITHIN LIMIT S WHEN THRUST REDUCED. ENGINE WAS NOT SHUTDOWN. 2 L 7 2 4F 4 F RT A2NM E12EU 2002082100129 20020821 00129 NM 2002 8 21 2002F00819 1 20020816 A 2612 710127 FIRE LOOP BOEING 757 75733N 1384931 NM LT ENGINE FAULTY G AMTA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 553TZ 32587 FLIGHT NUMBER 455. DURING GROUND HANDLING RECEIVED EICAS MESSAGE ENG FIRE LP 2. MAINTENANCE REMOVED AND REPLACED LEFT FIRE DETECTION ELEMENT (TS 5032), TB12 CONNECTOR. REF M/M 26-11-01-4, WD 71-51-11, PAGE 1 SHEET 6. 2 L 7 2 4F RT A2NM 2002082100130 20020821 00130 NM 2002 8 21 AALA20020824 1 20020607 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 392AN 29429 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SYSTEM AT 17B INOPERATIVE. RESEATED CONNECTOR UNDER SEAT 17B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082100131 20020821 00131 NM 2002 8 21 AALA20020825 1 20020607 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 389AA 27449 LAX - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 22AB INOPERATIVE. RESEATED LOOSE PUSHED P IN IN CONNECTOR AT SIDEWALL FOR SEAT 22AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082100132 20020821 00132 NM 2002 8 21 AALA20020826 1 20020607 A 3350 PIN BOEING 767 767323 1385205 NM CONNECTOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 389AA 27449 LAX - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 31AB INOPERATIVE. RESEATED LOOSE PUSHED P IN IN CONNECTOR AT SIDEWALL FOR SEAT 31AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082100133 20020821 00133 NM 2002 8 21 AALA20020827 1 20020607 A 3350 BATTERY BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 389AA 27449 JFK - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 16D INOPERATIVE. INSTALLED BATTERY FOR ES CAPE PATH LIGHTING SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082100134 20020821 00134 NM 2002 8 21 AALA20020829 1 20020604 A 3350 POWER SUPPLY BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING FOR BUSINESS CLASS INOPERATIVE. REPLACED POWER SUPPLY M33098 FOR EMERGENCY ESCAPE PATH LIGHTING IN BUSINESS CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002082100135 20020821 00135 NM 2002 8 21 AALA20020875 1 20020613 A 2910 RELIEF VALVE BOEING 757 757223 1384957 NM HYD SYSTEM MALFUNCTIONED A AALA K NONE N FALSE WARNING DE DESCENT 1 SW 21 630AA 24588 DFW - FLT 389 - EN ROUTE SAT-DFW - DURING DESCENT, LEFT HYDRAULIC QUANTITY EICAS MESSAGE CAME ON. LEFT RESERVOIR LIGHT ALSO CAME WITH ZERO PRESSURE SHOWING. AIRCRAFT LANDED AT DFW WITHOUT INCIDENT. INSPECTION OF AIRCRAFT FOUND NO LEAKS. REPLACED LEFT RESERVOIR PRESSURIZATION MODULE FILTER. REPLACED LEFT HYDRAULIC RESERVOIR PRESSURE RELIEF VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002082100136 20020821 00136 NM 2002 8 21 AALA20020876 1 20020613 A 2913 PUMP BOEING 757 757223 1384957 NM HYD SYSTEM FAILED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 677AN 29427 BDL - FLT 623 - EN ROUTE BDL-SJU, AFTER TAKEOFF, LEFT ENGINE DRIVEN HYDRAULIC PUMP FAILED. AIRCRAFT LOST ALL LEFT SYSTE M HYDRAULIC FLUID. PERFORMED AN ALTERNATE GEAR EXTENSION. AIRCRAFT RETURNED TO BDL AND LANDED WITHOUT INCIDENT. REPLA CED LEFT ENGINE HYDRAULIC PUMP AND ALL LEFT SYSTEM FILTERS. SERVICED HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OP ERATION. (M) 2 L 7 2 4F RT A2NM 2002082100137 20020821 00137 NM 2002 8 21 AALA20020879 1 20020612 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 381AN 25450 ORD - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT 24B INOPERATIVE. RECONNECTED LOOSE CONNECTO R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082100138 20020821 00138 NM 2002 8 21 AALA20020880 1 20020612 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AA 22327 JFK - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT 32H INOPERATIVE. RECONNECTED LOOSE CONNECTO R AT SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082100139 20020821 00139 NM 2002 8 21 AALA20020896 1 20020617 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 396AN 29603 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING ROWS 19B, 20B, 21B AND 22B INOPERATIVE. REINST ALLED CANNON PLUG AT SEATS 19B, 20B, 21B, AND 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082100140 20020821 00140 NM 2002 8 21 AALA20021086 1 20020721 A 3350 COVER BOEING 777 777223 1385213 NM RROYCE RB211 RB211* 54555 NE CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 780AN 29956 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHT LENS COVER MISSING AT SEAT 3D. REPLACED EMERGENCY EXIT L IGHT LENS COVER FOR SEAT 3D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT T00001SE A12EU 2002082100141 20020821 00141 NM 2002 8 21 AALA20021087 1 20020722 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM RROYCE RB211 RB211* 54555 NE CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT T00001SE A12EU 2002082100142 20020821 00142 NM 2002 8 21 AALA20021089 1 20020722 A 2421 COO5010 OIL COOLER BOEING 767 767223 1385123 NM GE CF6 CF680 30025 NE NR 1 ENGINE LEAKING A AALA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 323AA 22324 LEFT GEN DRIVE LIGHT AND GEN DRIVE EICAS MESSAGE DISPLAYED AFTER LANDING LIGHT WENT OUT IN LESS THAN 1 MINUTE. DID NOT DISCONNECT. T/S AND FOUND IDG OIL COOLER LEAKING IN NR 1 ENG. REMOVED AND REPLACED IDG OIL COOLER AS PER MM. RECONNECT ED IDG. OPS CHECKED AND LEAK CHECKED NR 1 IDG ALL CHECKED GOOD. INSPECTED FILTERS AND POPPETS. ALL NORMAL. OK FOR SE RVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 2002082100143 20020821 00143 NM 2002 8 21 AALA20021102 1 20020727 A 3350 CONNECTOR BOEING 767 767323 1385205 NM GE CF6 CF680 30025 NE CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 351AA 24032 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 30H, INOPERATIVE. TIGHTENED LOOSE CONNECTOR A T SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2002082100144 20020821 00144 NM 2002 8 21 AALA20021105 1 20020728 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 DURING OVERNIGHT MAINTENANCE FOUND MID GALLEY RIGHT HAND SIDE EMERGENCY LIGHT INOPERATIVE. REPLACED MID GALLEY RIGHT HA ND SIDE EMERGENCY LIGHTING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2002082100145 20020821 00145 NM 2002 8 21 AALA20021107 1 20020730 A 3350 HOUSING BOEING 767 767323 1385205 NM GE CF6 CF680 30025 NE CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 366AA 25193 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE LIGHTS AT SEAT 22A INOPERATIVE. REPLACED EMERGENCY LIGHT HOUSING AS SEMBLY AT SEAT 22A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2002082100146 20020821 00146 NM 2002 8 21 DL73K020788 1 20020711 A 2560 61020 BATTERY BOEING 737 737232 1384475 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 321DL 23093 FORWARD OUTBOARD F/A FLASHLIGHT BATTERY LOW. REPLACED BATTERY, CHECKS OK. 2 L 7 2 4F RT A16WE 2002082100147 20020821 00147 NM 2002 8 21 DL73K020796 1 20020712 A 2170 COALESCER BAG BOEING 737 737232 1384475 NM A/C BAY DIRTY A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 307DL 27548 23079 000000 ON PUSHBACK AND ENGINE START, F/A'S SMELLED SMOKE IN AFT GALLEY AREA. RETURNED TO GATE FOR MTC. INSPECTED AFT GALLEY, LT & RT A/C BAYS, LT & RT ENGINES, AFT LAV SMOKE DETECTOR. REPLACED RT A/C COALESCER BAG, RAN ENGINES AND PACKS, NO SME LL OR SMOKE NOTED. OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2002082100148 20020821 00148 SO 2002 8 21 C2XA02IA175 1 20020815 A 2770 KPD2611 CARTRIDGE EMB 145 EMB145LR 3260212 SO WEAK A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 29906 2614 2614 145472 Crew reported that the gustlock indication illuminated during flight. The aircraft diverted and landed at CRP without in cident. Maintenance inspected the gustlock system and the aircraft was dispatched under an MEL. Maintenance later remove d and replaced the gust lock spring cartridge, operationally checked the gustlock system, cleared the MEL and the aircra ft was returned to service. 2 L 7 2 4T RT T00011AT 2002090600166 20020906 00166 SO 2002 9 6 C2XA02IA174 1 20020815 A 7830 83990166 SWITCH EMB 145 EMB145 3260210 SO THRUST REVERSER FAULTY A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 12967 145133 CREW REPORTED A NR 1 ENGINE THRUST REVERSER FAIL MESSAGE ILLUMINATED DURING FLIGHT. THE CREW SHUTDOWN THE NR 1 ENGINE A ND THE AIRCRAFT LANDED AT GSO WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NR 1 THRUST REVERSER ON MEL. AFTER TROUBLESHOOTING THE NR 4 STOW AND TRANSIT, SWITCH WAS FOUND TO BE FAULTING. THE AFFECTED SWITCH WAS REMO VED AND REPLACED, THE AIRCRAFT WAS OPERATIONALLY CHECKED, THE MEL CLEARED, AND THEN RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002082100149 20020821 00149 NM 2002 8 21 DL73K020811 1 20020715 A 2910 BACH8A06EE02 HYDRAULIC LINE BOEING 737 737232 1384475 NM HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 320DL 23092 ON DEPARTURE, PLACED LANDING GEAR CONTROL HANDLE UP AND HAD FOLLOWING INDICATIONS: 3 RED GEAR LIGHTS, HYDRAULIC QUANTIT Y DROPPED TO .5 GAL, HYD MASTER CAUTION WITH BOTH OVERHEAD A-SYSTEM LOW PRESSURE LIGHTS ILLUMINATED. FOUND RETRACT PRES S LINE ON LEFT MAIN GEAR LEAKING. REPLACED RETRACT PRESS LINE, REPLACED BOTH A-SYSTEM CASE DRAIN AND PRESS FILTERS. AL L SYSTEMS AND LEAK CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2002082100150 20020821 00150 NM 2002 8 21 DL73K020827 1 20020718 A 3350 20131A BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 301DL 23073 EMERGENCY LIGHT SWITCH OFF, AFT SEAT EMERGENCY LIGHTS STAY ON. REPLACED BATTERY PACK, OPS NORMAL. 2 L 7 2 4F RT A16WE 2002090900151 20020909 00151 NM 2002 9 9 F3LA200200220 1 20020820 A 5754 SKIN BOEING 737 737317 138447P NM L/E SLAT CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED LT WING NR 1 SLAT LOWER SKIN CRACKED AT LAST ROW OF RIVETS I/B OF CENTER AUX TRACK . FABRICATED AND INSTALLED REPAIR PER SRM 57-43-01. 2 L 7 2 4F RT A16WE 2002082100151 20020821 00151 NM 2002 8 21 USA2002F00075 1 20020726 A 2133 7110033 OUTFLOW VALVE BOEING 737 7373B7 1384580 NM AFT FUSELAGE LEAKING A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 531AU 43421 24478 ON CLIMB OUT, ENROUTE, CABIN ALT WARNING HORN SOUNDED. CREW REPORTED OUTFLOW VALVE WAS FULLY CLOSED IN AUTO, STANDBY, A ND MANUAL PRESS MODES BUT THEY WERE NEVER ABLE TO GET CABIN PRESS. EMER DESCENT WAS ACCOMPLISHED. FLIGHT LANDED WITHOU T FURTHER INCIDENT. NO EMER WAS DECLARED. MAIN FOUND APU BLEED AIR DUCT PRESS SEAL BOOT IN AFT KEEL BEAM DISLODGED. R ESECURED CLAMP AND BOOT. FOUND CABIN PRESS OUTFLOW VALVE BLADE SEALS LEAKING. REMOVED AND REPLACED CABIN PRESS OUTFLOW VALVE. OPS CHECK GOOD. PRESS A/C TO 6.5 PSI. NO LEAKS NOTED. CLEARED MEL ON LEFT PACK BY REPLACING LEFT PACK WATER SEPARATOR 35 DEGREE SENSOR (PN 6275701). LEFT PACK OUTPUT READS 4 DEGREES CENTIGRADE IN FULL COLD. A/C OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2002091100080 20020911 00080 NM 2002 9 11 F3LA200200224 1 20020820 A 5320 FLOOR SUPPORT BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON UNDERSIDE OF CARGO FLOORBEAM AROUND NUT PLATE, BS 727E +2, RBL 8. RE MOVED DAMAGED AREA, FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 51-41-02, 53-00-53, AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002082100152 20020821 00152 NM 2002 8 21 GAIA02079OP 1 20020809 A 3350 1000679 LIGHT B727251 BOEING 727 727251 138408H NM EMER EXIT LT ASY DISCHARGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 255US 19974 DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. C/A: RECHARGED EME RGENCY LIGHT ASSEMBLY FROM THE GROUND POWER UNIT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2002082100153 20020821 00153 WP 2002 8 21 WXOA02006 1 20020806 A 3350 60030431 POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN SIDEWALL DISCHARGED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 945MA 49725 DURING SCHEDULED MAINTENANCE, FOUND AFT LT OVERWING EMERGENCY LIGHT FIXTURE TO NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT. SYSTEM OPERATIONAL CHECK NORMAL IAW MM. 2 L 7 2 4F RT A6WE 2002082100154 20020821 00154 NM 2002 8 21 HALA0200385 1 20020804 A 2421 GEARBOX BOEING 717 717200 1383700 NM ACCY GEARBOX FAILED A HALA K NONE J WARNING INDICATION AP APPROACH 1 WP 13 476HA 55118 RIGHT ENGINE SYSTEM FAIL ILLUMINATED PRIOR TO LANDING. C/A: REPLACED RIGHT ENGINE GEN STATOR AND ROTOR ASSY. CONDITION SAME. REMOVED ACCESSORY GEARBOX IAW MM. INSTALLED AGB PER MM. LEAK AND POWER ASSURANCE CHECK, OK. 2 L 7 2 4F TR A6WE 2002091100081 20020911 00081 NM 2002 9 11 F3LA200200225 1 20020820 A 5330 SKIN BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FUSELAGE SKIN, BS 469-487, BETWEEN STR 25-R AND 26-R. REPAIRED PER E A 53-737-177 AND SRM 53-30-03. 2 L 7 2 4F RT A16WE 2002082100155 20020821 00155 NE 2002 8 21 MALA020469 2 20020816 A 7320 230349306 ECU BAC 146 AVRO146RJ85A 1500097 EU LF507 LF5071F NE DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 15 508XJ E2318 DURING TAKEOFF ON FLIGHT #3686, AFTER V1 AND #2 ENGINE EGT FLUCTUATED FROM -5 DEGREES CEL. TO APPROXIMATELY 643 DEGREES CEL. THEN TO ALL DASHES THEN BACK TO NORMAL. ALL OTHER ENGINES WERE GOOD EGT WAS STABLE FOR A WHILE THEN EGT INDICATED DASHES. MAINTENANCE REPLACED #2 ECU PN 2-303-493-06, SN/ON 9ALG716, SN/OFF 9ALG786. ALL IAW AVRO MM CHAPTER 24, ALL CHE CKS GOOD AT THIS TIME. 2 H 7 4 4F 4 F RT A49EU E6NE 2002082100156 20020821 00156 EU 2002 8 21 MALA020471 1 20020820 A 2910 HE152581 PRESSURE SWITCH BAC 146 AVRO146RJ85A 1500097 EU A MALA O OTHER J WARNING INDICATION LD LANDING 1 GL 15 532XJ E2366 DURING LANDING ROLLOUT ON FLIGHT #3526, LOSS OF GREEN HYDRAULIC SYSTEM UPON LANDING ROLLOUT AND TAXI INTO GATE. MAINTEN ANCE FOUND #3 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE SWITCH PN HE15258-1, SN 3704, FAILED INTERNALLY AT CANNON PLUG ATTAC HMENT POINT. NEW SWITCH INSTALLED. 2 H 7 4 4F RT A49EU 2002082100157 20020821 00157 NM 2002 8 21 AWXA200200775 1 20020820 A 3350 BMS13311122 WIRE BOEING 737 737277 1384570 NM SEAT ROW 10 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 0 0 22655 PHX - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHT SEAT ROW 10 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT SEAT ROW 10 L/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002082100158 20020821 00158 NM 2002 8 21 AWXA200200777 1 20020731 A 5347 140N25022 TIE CLIP BOEING 757 7572S7 1384962 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 0 0 23566 LCQ - MAJOR REPAIR - DURING C-08 CHECK A 3/4" CRACK WAS FOUND ON FLOOR BEAM SUPPORT TIE CLIP BS 1280, AFT CARGO COMPARTM ENT. MAINTENANCE REMOVED CRACKED FLOOR BEAM SUPPORT TIE CLIP BS 1280, FABRICATED A NEW FLOOR SUPPORT TIE CLIP, AND INST ALLED REPAIR IAW B757-200 SRM 51-20-00, PG. 1, AND SRM 51-40-05, PG. 1. 2 L 7 2 4F RT A2NM 2002082100159 20020821 00159 NM 2002 8 21 AWXA200200778 1 20020731 A 5347 140N2502 TIE CLIP BOEING 757 7572S7 1384962 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 0 0 23566 LCQ - MAJOR REPAIR - DURING C-08 CHECK A 5/8" CRACK WAS FOUND ON FLOOR BEAM SUPPORT TIE CLIP BS 1320, AFT CARGO COMPARTM ENT. MAINTENANCE REMOVED CRACKED FLOOR BEAM SUPPORT TIE CLIP BS 1320, FABRICATED A NEW FLOOR SUPPORT TIE CLIP, AND INST ALLED REPAIR IAW B757-200 SRM 51-40-02, PG. 1. 2 L 7 2 4F RT A2NM 2002082100160 20020821 00160 NM 2002 8 21 AWXA200200779 1 20020730 A 5320 146N83261 CREASE BEAM BOEING 757 7572S7 1384962 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 0 0 23566 LCQ - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON THE LOWER SIDE OF CREASE BEAM AND FLOOR PAN AT BS 1348, LB L 66. MAINTENANCE CLEANED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS, CUTOUT DAMAGED AREA OF FLOOR PAN AND PERFORME D HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW B757 -200 SRM 51-70-13, PG. 1-2. REMOVED CREASE BEAM FROM BS 1290 TO BS 1400, FABRICATED A NEW CREASE BEAM AND INSTALLED REPA IR IAW B757-200 SRM 51-40-02, PG. 4-7. 2 L 7 2 4F RT A2NM 2002082100161 20020821 00161 NM 2002 8 21 AWXA200200780 1 20020801 A 5315 146N83262 CREASE BEAM BOEING 757 7572S7 1384962 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 0 0 23566 LCQ - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON CREASE BEAM AT ATTACHMENT HOLE BS 1340, RBL 65. MAINTENANC E CLEANED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS, REMOVED CREASE BEAM CHORD FROM BS 1290 TO BS 1400, FABRICATED A NEW CREASE BEAM AND INSTALLED REPAIR IAW B757-200 SRM 51-40-02, PG. 11-12, & 39. 2 L 7 2 4F RT A2NM 2002082200001 20020822 00001 2002 8 22 HEEA080688 4 20020730 A 2300 DMC633A ANTENNA BELL 206 206L3 1182108 SW FM SYSTEM FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 42EA 51542 FM SYSTEM HAS LIMITED RANGE. SCRAPPED. 1 G 7 1 3U H2SW 2002082200002 20020822 00002 2002 8 22 HEEA080689 4 20020730 A 2312 DMC631A ANTENNA BELL 206 206L3 1182108 SW VHF SYSTEM FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 42EA 51542 NO RANGE ON VHF. SCRAPPED. 1 G 7 1 3U H2SW 2002082200003 20020822 00003 2002 8 22 HEEA080690 4 20020730 A 2300 DMC633A ANTENNA BELL 206 206L3 1182108 SW COMMS SYSTEM CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 42EA 51542 ANTENNA IS CRACKED AND CORRODED. SCRAPPED. 1 G 7 1 3U H2SW 2002082200004 20020822 00004 2002 8 22 HEEA080691 4 20020730 A 3140 DPUA0101 COMPUTER BELL 206 206L4 1182110 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 7077F 52038 PROCESSOR FAULT LIGHT, INTERNAL BATTERY FAILURE. 1 G 7 1 3U NC H2SW 2002082200005 20020822 00005 2002 8 22 HEEA080692 4 20020730 A 3140 DPUA0101 COMPUTER BELL 206 206L3 1182108 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 31077 51520 LIGHT STAYS ON, UNABLE TO DOWNLOAD. 1 G 7 1 3U H2SW 2002082200006 20020822 00006 2002 8 22 HEEA080693 4 20020730 A 3140 DPUA0101 COMPUTER BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 129MR 51129 INTELLASTAR PROCESSOR INTERNAL BATTERY DEAD. 1 G 7 1 3U H2SW 2002082200007 20020822 00007 2002 8 22 HEEA080694 4 20020730 A 3140 DPUA0101 COMPUTER BELL 407 407 1182206 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 436PH 51436 INTELLASTART PROCESSOR HAS AN INTERMITTENT LIGHT ON FAULT LAMP. 1 G 7 1 3U O H2SW 2002082200008 20020822 00008 2002 8 22 HEEA080695 4 20020730 A 3140 DPUA0101 COMPUTER BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4835 51131 INTELLASTART PROCESSOR INTERNAL BATTERY DEAD. 1 G 7 1 3U H2SW 2002082200009 20020822 00009 2002 8 22 HEEA080696 4 20020730 A 3140 DPUA0101 COMPUTER BELL 206 206L4 1182110 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 7077B 52037 INTELLASTART PROCESSOR INTERNAL BATTERY VOLTAGE. 1 G 7 1 3U NC H2SW 2002082200010 20020822 00010 2002 8 22 HEEA080697 4 20020730 A 3140 DPUA0101 COMPUTER BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2777D 45299 CANNOT COMMUNICATE TO PROCESSOR. 1 G 7 1 3U H2SW 2002082200011 20020822 00011 2002 8 22 HEEA080698 4 20020730 A 3140 DPUA0101 COMPUTER BELL 206 206L4 1182110 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 7074W 52033 INTELLASTART PROCESSOR INTERNAL BATTERY FAULT. 1 G 7 1 3U NC H2SW 2002082200012 20020822 00012 2002 8 22 HEEA080699 4 20020730 A 3140 DPUA0101 COMPUTER BELL 206 206L3 1182108 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 31073 51519 INTELLISTART LIGHT FLASHING. 1 G 7 1 3U H2SW 2002082200013 20020822 00013 SW 2002 8 22 HEEA080700 1 20020730 A 7740 DPUA0101 COMPUTER BELL 206 206L3 1182108 SW ENGINE MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3116P 51530 INTELLASTART PROCESSOR MALFUNCTION, CANNOT DOWNLOAD DATA LOG. 1 G 7 1 3U H2SW 2002082200014 20020822 00014 SW 2002 8 22 HEEA080701 1 20020730 A 7740 DPUA0101 COMPUTER BELL 206 206L3 1182108 SW ENGINE MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6251X 51552 WILL NOT COMMUTE WITH COMPUTER AND INTELLISTART LIGHT STAYS ON. 1 G 7 1 3U H2SW 2002082200015 20020822 00015 SW 2002 8 22 HEEA080702 1 20020730 A 7740 DPUA0101 COMPUTER BELL 206 206L3 1182108 SW ENGINE MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 53119 51575 HAD SOLENOID FAULT WITH NO LAMP ILLUMINATED CAUSING ENGINE TO OVERTEMP.. 1 G 7 1 3U H2SW 2002082200016 20020822 00016 WP 2002 8 22 ABXA020078 1 20020810 A 3260 25878263 COMPUTER DOUG DC9 DC932F 3022067 WP ELEC. COMP. DEFECTIVE A ABXA K NONE F FLT CONT AFFECTED CL CLIMB 1 GL 23 904AX 47040 DURING CLIMB THROUGH FL 180, AUTOPILOT GAVE AN UNCOMMANDED RIGHT RUDDER INPUT. AN UNCOMMANDED RIGHT RUDDER INPUT OCCURRE D WITH AUTOPILOT DISENGAGED, USED MANUAL RUDDER WITH YAW DAMPER ON AND SERVO ON. REPLACED THE STABILITY AUGMENTATION COM PUTER IAW DC-9 MM 22-11-01-2. 2 L 7 2 4F A6WE 2002082200017 20020822 00017 SW 2002 8 22 HEEA080703 1 20020730 A 7740 DPUA0101 COMPUTER BELL 206 206L3 1182108 SW ENGINE MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 41128 51134 INTELLASTART PROCESSOR INTERNAL BATTERY FAULT. 1 G 7 1 3U H2SW 2002082200018 20020822 00018 SW 2002 8 22 HEEA080705 1 20020731 A 5320 206031201249S ANGLE BELL 206 206L3 1182108 SW FUSELAGE MISMARKED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 RECEIVED P/N 206-031-201-250S RT ANGLE, MISIDENTIFIED AS 206-031-201-249S. 1 G 7 1 3U H2SW 2002082200019 20020822 00019 2002 8 22 HEEA080706 4 20020731 A 2210 214074301105 AMPLIFIER BELL 214 214ST 1182106 SW SCAS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 AMPLIFIER ROLLS CHANNEL AND KICKS OFF LINE. 2 G 7 2 4U H10SW 2002082200020 20020822 00020 SW 2002 8 22 HEEA080707 1 20020731 A 6320 406340100101 PUMP BELL 407 407 1182206 SW XMSN OIL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 TRANSMISSION OIL PUMP FOUND LEAKING. 1 G 7 1 3U O H2SW 2002082200021 20020822 00021 2002 8 22 HEEA080709 4 20020802 A 2210 412074030101 AMPLIFIER BELL 412 412 1182202 SW ADI ERRATIC E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 ADI HAD ERRATIC MOVEMENT. 1 G 7 2 4U H4SW 2002082200022 20020822 00022 SW 2002 8 22 HEEA080710 1 20020807 A 5610 206033600018 WINDOW BELL 206 206L3 1182108 SW COCKPIT SEPARATED E HEEA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SW 03 3108E 51498 PILOTS SLIDING WINDOW DEPARTED AIRCRAFT IN FLIGHT. NO DAMAGE TO AIRCRAFT. REPLACED SLIDING WINDOW. 1 G 7 1 3U H2SW 2002082200023 20020822 00023 SW 2002 8 22 HEEA080711 1 20020807 A 2840 473203003 SIGNAL COND UNIT BELL 412 412 1182202 SW FUEL INDICATOR MALFUNCTIONED E HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 SIGNAL COND UNIT MALFUNCTIONED ILLUMINATING FUEL LOW LIGHT. 1 G 7 2 4U H4SW 2002082200024 20020822 00024 SW 2002 8 22 HEEA080712 1 20020807 A 2840 473203003 SIGNAL COND UNIT BELL 412 412 1182202 SW FUEL INDICATOR MALFUNCTIONED E HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 SIGNAL COND UNIT MALFUNCTIONED ILLUMINATING FUEL LOW LIGHT. 1 G 7 2 4U H4SW 2002082200025 20020822 00025 SW 2002 8 22 HEEA080713 1 20020807 A 2840 473203003 SIGNAL COND UNIT BELL 412 412 1182202 SW FUEL INDICATOR FAILED E HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 FUEL INDICATOR READS ZERO. 1 G 7 2 4U H4SW 2002082200027 20020822 00027 SW 2002 8 22 HEEA080715 1 20020807 A 2840 473203003 SIGNAL COND UNIT BELL 412 412 1182202 SW FUEL INDICATOR MALFUNCTIONED E HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 SIGNAL COND UNIT PRODUCING INTERMITTENT LOW FUEL LIGHT WITH FUEL IN AIRCRAFT. 1 G 7 2 4U H4SW 2002082200028 20020822 00028 SW 2002 8 22 HEEA080716 1 20020807 A 6710 214001423109 ACTUATOR BELL 214 214ST 1182106 SW MAIN ROTOR INOPERATIVE E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 MAIN ROTOR ACTUATOR INOPERATIVE. 2 G 7 2 4U H10SW 2002082200029 20020822 00029 SW 2002 8 22 HEEA080717 1 20020807 A 3340 214175140103 POWER SUPPLY BELL 214 214ST 1182106 SW EXTERIOR LIGHTS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 LIGHTS WOULD NOT COME ON. REPLACED POWER SUPPLY. 2 G 7 2 4U H10SW 2002082200030 20020822 00030 NE 2002 8 22 CA020729012 2 20020714 A 7421 9550168760 IGNITER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING MAINTENANCE, ENGINEER REMOVED IGNITERS FOR INSPECTION, ONE ELECTRODE WAS MISSING. CARRIED OUT SL. 2170 (BO RESCOPE INSPECTION ) FOUND INTERNAL DAMAGE TO ENGINE. ENGINE WAS REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2002082200031 20020822 00031 EU 2002 8 22 CA020729013 1 20020726 A 5610 9598110112 WINDOW PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL COCKPIT BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING REMOVAL OF THE MAIN RT WINDSCREEN, IT WAS NOTICED THAT ONE OF THE SCREW ATTACHMENT LUGS ON THE TOP SECTION OF THE RT SIDE WINDOW WAS CRACKED. THE SIDE WINDOW REQUIRED REPLACEMENT. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002082200033 20020822 00033 EA 2002 8 22 CA020730001 1 20020726 A 3234 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) A/C WAS SITTING AT THE GATE WITH AC EXTERNAL POWER SELECTED ON AND HYDRAULIC SYSTEM NR 3 PRESSURIZED. AC POWER H AS BEEN SELECTED OFF WITH HYDRAULIC NR 3 SYSTEM STILL PRESSURIZED WHICH CAUSED THE NLG TO COLLAPSE. DUE TO CHOCKS BEIN G INSTALLED, NLG DID NOT COLLAPSE COMPLETELY AND NO DAMAGE OCCURRED TO THE A/C. NO PASSENGERS WERE ONBOARD AND NO PERSO NAL WERE INJURED. NOSE LANDING GEAR SELECTOR VALVE REPLACED, GEAR SWINGS PERFORMED AND LANDING GEAR OPS CHECKED SERVIC EABLE IN ACCORDANCE WITH THE AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002082200034 20020822 00034 CE 2002 8 22 CA020730002 1 20020725 A 5312 50440014595 ANGLE BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL PRESSURE BLKHD DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 16102 (CAN) THE REAR PRESSURE BULKHEAD WAS FOUND CRACKED. WE BELIEVE THE CRACK WAS CAUSED BY A ANGLE THAT DID NOT HAVE ENOUGH CLEARENCE BETWEEN IT AND THE PRESSURE BULKHEAD. WHEN THE AFT BULKHEAD FLEXES THE ANGLE DIGS INTO THE BULKHEAD CAUSING A STRESS RISER AND EVENTUALLY A CRACK. THE OTHER KING AIRS IN OUR FLEET ARE ALSO SHOWING SIGNS OF THIS STRESS RISER BUT NO CRACKS HAVE SHOWN UP. THE CRACK WAS REPAIRED. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 2002082200035 20020822 00035 NM 2002 8 22 CA020730003 1 20020728 A 2150 ACM BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE ACM BAY FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) CREW REPORTED "BURNING SMELL IN FLIGHT DECK AND CABIN. MIX VALVES CYCLED FULL COLD SMELL DISSIATED". MAINT REPLACE D PACK CONTROL VALVE INITIALIALY, THEN ON SUBSEQUENT FLIGHT THE PACK TRIPPED IN AUTO. ACM REPLACED SNAG CLEARED. ACM OUT FOR OVERHAUL. 2 L 7 2 4F 4 F A16WE E2EA 2002082200036 20020822 00036 EU 2002 8 22 CA020730004 1 20020726 A 7600 7303989 CONTROL CABLE BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU ROTOL R4304 R2124304 EU WHEEL WELL FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A B-4 INSPECTION, THE MECHANIC NOTED THE HP CABLE FRAYED WITH ONLY 10 STRANDS LEFT HOLDING THE CABLE TOGETH ER. THE AREA IN THE VICINITY OF THE DAMAGED CABLE WAS INSPECTED AND THERE WAS NO SIGN WHERE THE CABLE COULD HAVE BEEN RU BBING. THE AIRCRAFT WAS OPERATED FROM GRAVEL STRIPS THE WEEK PRIOR AND THE MECHANIC SUSPECTS THAT THE CABLE MAY HAVE BEE N DAMAGED FROM ROCKS COMING OFF THE TIRES DURING GEAR RETRACTION. THE CABLE WAS REPLACED AND THE AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 3T 4 T A24EU A196 6 C P899 2002082200039 20020822 00039 NM 2002 8 22 CA020730007 1 20020627 A 5330 SKIN BOEING 737 737296 1384486 NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 56297 (CAN) TWO FATIGUE CRACKS FOUND IN RT FUSELAGE SKIN BETWEEN STA. 727A & 727B AND BETWEEN STR 14R & 19R ABOVE EXISTING REP AIR AT SAME LOCATION. ONE CRACK IS HORIZONTAL 1.5 INCHES AND OTHER VERTICAL 1 INCH LONG. EXISTING DOUBLER REMOVED AND RE PAIR CARRIED OUT AS PER SRM 53-30-3 AND BOEING 737-100/200 PRELIMINARY COPY GENERAL FUSILAGE SKIN REPAIR FIGURE 48 DETAI LS 1 THRU 9. 2 L 7 2 4F 4 F RT A16WE E2EA 2002082200040 20020822 00040 EA 2002 8 22 CA020731001 1 20020724 A 4930 WE38304862 FUEL NOZZLE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE APU ENGINE CRACKED W H DEACTIVATE SYST/CIRCUITS K FLUID LOSS NR NOT REPORTED 1 CA (CAN) THE INITIAL PROBLEM REPORTED WAS THAT, WITH APU BLEED ON & BOTH PACKS OPERATING, DUCT PRESSURE WOULD DROP TO APPRO X 20 PSI & APU BLEED CAUTION MESSAGE WAS POSTED. APU RPM ALSO DROPPED AND, DURING ENGINE START, APU GEN DROPPED OFF LIN E. 1ST ACTION TAKEN WAS TO MEL APU BLEED AIR, BUT THEN A FUEL LEAK WAS NOTICED. A FUEL PIPE AT FCU WAS TIGHTENED BUT FUE L WAS STILL LEAKING. APU WAS PLACED ON MEL AS THERE WAS INSUFFICIENT TIME TO TROUBLESHOOT FURTHER. CLH ENGINEERING SENT A COPY OF AOM 700-062 TO HAMBURG MAINT & REQUIRED THAT FUEL NOZZLES BE INSP FOR CRACKS. THIS WAS DONE & A CRACK FOUND. CRACKED NOZZLE WAS REPLACED & APU WAS TESTED & REINSTATED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002082200042 20020822 00042 EA 2002 8 22 CA020731004 1 20020724 A 2800 79888311 CONTROL PANEL CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE REFUEL/DEFUEL FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA (CAN) DURING TRANSIT REFUELLING, SMOKE NOTICED FROM FLIGHT DECK REFUEL/DEFUEL PANEL. MAINTENANCE PERSONNEL WERE SENT AND THE PANEL WAS REPLACED. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002082200044 20020822 00044 WP 2002 8 22 AALA20020382 1 20020620 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 415AA 49326 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE LIGHTING FOR ROWS 21-31 INOPERATIVE. REPLACED EMERGENCY EXIT L IGHT BATTERY PACK FOR ROWS 21-31. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200045 20020822 00045 WP 2002 8 22 AALA20020383 1 20020620 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7522A 49899 MAI - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRING FOR FORWARD EMER GENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200046 20020822 00046 WP 2002 8 22 AALA20020432 1 20020621 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 255AS 49287 DFW - DURIG OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 20-31 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE FOR SEAT 21-31. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200047 20020822 00047 WP 2002 8 22 AALA20020494 1 20020621 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 255AA 49287 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED FORWARD EMERGENCY EXIT LIGHT WI RE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200048 20020822 00048 WP 2002 8 22 AALA20020502 1 20020621 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 255AA 49287 DFW - DURING OVERNIGHT MAINTENANCE, FOUND RIGHT AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED RIGHT AFT EMERGENCY EXI T LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200049 20020822 00049 WP 2002 8 22 AALA20020800 1 20020622 A 3350 SWITCH DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 483A 49676 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ARM/ON SWITCH AT ATTENDANT STATION INOPERATIVE. REPLACED EMERG ENCY EXIT LIGHT ARM/ON SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200050 20020822 00050 NM 2002 8 22 AALA20020834 1 20020529 A 2421 766088 IDG BOEING 767 767223 1385123 NM RT ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 313AA 22316 JFK - FLT 679 - EN ROUTE JFK-AUA - RIGHT ENGINE IDG FAILED. RETURNED JFK LANDING WITHOUT INCIDENT. REPLACED RIGHT ID G ENERATOR. PERFORMED OPERATIONS CHECKED PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082200051 20020822 00051 WP 2002 8 22 AALA20020882 1 20020614 A 3350 CONTACTOR DOUG DC9 DC983 3022083 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 591AA 53254 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS AT ROW 23 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002082200052 20020822 00052 WP 2002 8 22 AALA20020883 1 20020614 A 3350 CONTACTOR DOUG DC9 DC983 3022083 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 591AA 53254 DFW - DURING OVERNIGHT MAINTENANCE OVERHEAD EMERGENCY EXIT LIGHTS AT ROW 24 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT B ATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002082200053 20020822 00053 WP 2002 8 22 AALA20020884 1 20020616 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 245AA 49257 DFW - FOUND DURING MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS AT ROW 23-26 DIM. CLEANED EMERGENCY EXIT LIGHT BATTERY C ONTACTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200054 20020822 00054 WP 2002 8 22 AALA20020885 1 20020616 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 469AA 49599 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS AT ROW 13-16 INOPERATIVE. RESEATED EMERGENCY EXIT LI GHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200055 20020822 00055 WP 2002 8 22 AALA20020886 1 20020613 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 440AA 49459 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT TAIL SECTION INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BAT TERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200056 20020822 00056 WP 2002 8 22 AALA20020887 1 20020613 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 458AA 49563 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT ROW 19 INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGHT B ATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200057 20020822 00057 WP 2002 8 22 AALA20020888 1 20020616 A 3350 LIGHT DOUG DC9 DC982 3022082 WP TAIL CONE BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 DFW - DURING OVERNIGHT MAINTENANCE, AFT TAIL CONE EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REPLACED AFT TAIL CONE EMERGENC Y EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200058 20020822 00058 WP 2002 8 22 AALA20020890 1 20020612 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 291AA 49303 DFW - DURING OVERNIGHT MAINTENANCE, FOUND L1 ENTRY DOOR EMERGENCY EXIT CEILING LIGHT DIM. REPLACED L1 ENTRY DOOR EMERGE NCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200059 20020822 00059 WP 2002 8 22 AALA20020891 1 20020612 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7540A 49994 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR SIDEWALL FORWARD EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED AFT STAIR SI DEWALL FORWARD EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200060 20020822 00060 NM 2002 8 22 AALA20020902 1 20020319 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 ORD - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 34B INOPERATIVE. SECURED CONNECTOR AT WALL FOR SEAT 34B EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082200061 20020822 00061 WP 2002 8 22 AALA20020923 1 20020618 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7530 49922 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 24-26 INOPERATIVE. SECURED OVERHEAD EMERGENC Y EXIT LIGHT BATTERY CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082200062 20020822 00062 NM 2002 8 22 AALA20020927 1 20020622 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 192AN 32386 DFW - FOUND EMERGENCY LIGHT AT ROW 18D INOPERATIVE. RECONNECTED CANNON PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002082200063 20020822 00063 NM 2002 8 22 AALA20020928 1 20020623 A 3350 CONTACTOR BOEING 757 757223 1384957 NM EXTERIOR DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 693AA 26973 MIA - FOUND AFT LEFT FUSELAGE EMERGENCY LIGHT NEXT TO PRESSURE RELIEF VALVE IS INOPERATIVE. CLEANED BULB ASSEMBLY CONTA CT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002082200064 20020822 00064 NM 2002 8 22 AALA20020929 1 20020622 A 3340 LIGHT BOEING 757 757223 1384957 NM NLG BROKEN A AALA O OTHER S AFFECT SYSTEMS LD LANDING 1 SW 21 653A 24611 SJU - FLT 1470 - EN ROUTE ORD-SJU - DURING LANDING, NOSE GEAR INDICATION FAILED TO INDICATE DOWN AND LOCKED UPON EXTENSI ON. AIRCRAFT LANDED AT SJU WITHOUT INCIDENT. INSPECTION FOUND DAMAGED NOSE LANDING LIGHT ASSEMBLY. BROKEN GLASS FROM LANDING LIGHT FOUND EMBEDDED IN NOSE GEAR TARGETS. ALSO, FOUND BROKEN DOWNLOCK SENSOR AND GLASS INSIDE GEAR PIN HOLE AT BRACE. REPLACED LIGHT ASSEMBLY AND DOWNLOCK SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002082200065 20020822 00065 NM 2002 8 22 ASAA0210060 1 20020314 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT ON THE SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED REMOT E ASSEMBLY BATTERY THEN LIGHT OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002082200066 20020822 00066 NM 2002 8 22 ASAA0210061 1 20020317 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS WOULD NOT TEST IN THE AFT CABIN. REMOVED AND REPLACE D THE TWO MOST AFT REMOTE ASSEMBLY BATTERY THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002082200067 20020822 00067 NM 2002 8 22 ASAA0210077 1 20020403 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT SEAT PALLET 3-3 INOPERATIVE. REMOVED AND REPLAC ED REMOTE ASSEMBLY BATTERY AND RECEIVER AT SEAT PALLET 3-3, THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002082200068 20020822 00068 NM 2002 8 22 ASAA0210078 1 20020409 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROWS 14 AND 15 INOPERATIVE. REMOVED AND REPLACE D REMOTE ASSEMBLY BATTERY, THEN FLOOR TRACK LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002082200069 20020822 00069 NM 2002 8 22 ASAA0240030 1 20020313 A 3350 S283T0143 BATTERY BOEING 737 7374Q8 138447Q NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 709AS 28896 PHX - DURING LINE CHECK, THE EMERGENCY AISLE LIGHTS AT ROWS 18 AND 21 WERE INOPERATIVE. REPLACED EMERGENCY BATTERY ASSE MBLY. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2002082200070 20020822 00070 NM 2002 8 22 ASAA0240041 1 20020409 A 3350 8100022602 LIGHT BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 769AS 25103 SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTING AT ROW 18 AND 25 DISCONNECTED. RECONNECTED TRACK LIGHTS, OPS CHECKE D NORMAL. (M) 2 L 7 2 4F RT A16WE 2002082200071 20020822 00071 WP 2002 8 22 ASAA0280071 1 20020315 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING PREFLIGHT CHECK, FOUND TWO INOPERATIVE EMERGENCY TRACK LIGHTS AT ROWS 29 AND 33. REPLACED BROKEN LIGHT MOD ULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002082200072 20020822 00072 WP 2002 8 22 ASAA0280217 1 20020701 A 3350 0105610 MODULE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 07 943AS 53018 SEA - DURING LINE MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE AT ROW 30. REPLACED EMERGENCY TRACK LIGHT MODULE AT ROW 30. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002082200074 20020822 00074 CE 2002 8 22 CA020731005 1 20020722 A 5342 23320192 FITTING LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP HORIZONTAL STAB LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING HUMP INSPECTION THE FOLLOWING DISCREPANCY WERE FOUND. THE HORIZONTAL STAB CENTER HINGE FITTING HAD LOOSE AN D MISSING RIVETS. A TOTAL OF 14 RIVETS WERE AFFECTED AND CONSEQUENTLY REPLACED BY HI-LOK AS PER STRUCTURAL REPAIR MANUAL . 2 L 7 2 4F 4 F A10CE E6WE 2002082200075 20020822 00075 NM 2002 8 22 CA020731006 1 20020717 A 5220 MS276463839 BEARING DHAV DHC8 DHC8201 2809001 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE EMERGENCY EXIT CORRODED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) TRAINING CAPTAIN CARRYING OUT EVACUATION TRAINING WAS UNABLE TO OPEN FWD EMERGENCY EXIT. ON INVESTIGATION BY LINE ENGINEERS, THE DOOR HANDLE WOULD NOT FULLY EXTEND. AFTER DISASSEMBLY OF TRIM AROUND DOOR AND DOOR PANEL. THE DOOR OPENIN G MECHANISM BEARINGS WERE FOUND TO BE CORRODED AND SEIZED. THE DOOR WAS ALSO FOUND TO HAVE WATER COLLECTING AT THE BOTTO M AND ALL INSULATION WITHIN THE DOOR WAS FOUND WET. BEARINGS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002082200076 20020822 00076 CE 2002 8 22 CA020731007 1 20020723 A 2730 233151116 BOLT LEAR 243400014 LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP RT ELEVATOR LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING HUMP INSPECTION THE RT ELEVATOR BELLCRANK ATTACHMENT BOLT HAD VERTICAL FREE PLAY BETWEEN THE BELLCRANK AND THE ELEVATOR INPUT SHAFT. THE RT ELEVATOR TORQUE TUBE AND BELLCRANK ATTACHMENT HOLES WERE ELONGATED.AS PER LEARJET ENG INEERING REPORT. THE ELONGATED HOLES WERE OPEN GOOD AND ROUND TO ACCOMODATE FOR NEW BOLTS P/N NAS6604-32Y. 2 L 7 2 4F 4 F A10CE E6WE 2002082200078 20020822 00078 EU 2002 8 22 CA020731008 1 20020623 A 2530 92023695 OVEN AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE GALLEY OVERHEATED W F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) OVEN NR 1 IN Y CLASS GALLEY, OVERHEATED AND SPARKED THEN STARTED SMOKING.C/B PULLED AND 2 SHOTS OF HALON FIRED IN IT. OVEN COOLED DOWN AND REMAINED DEACTIVATED FOR REMANDER OF FLIGHT. OVEN REPLACED ,WIRING AND CONNECTOR INSPECTED FOR DAMAGE. NO FAULTS FOUND.OVEN OPEATION CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E29NE 2002082200079 20020822 00079 CE 2002 8 22 2002131 1 20020821 A 3200 114800121 WHEEL BEECH 1900 1900D 1154162 CE A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 210GL UE210 AFTER TAKE OFF,NOSE WHEEL VIBRATION, R&R NOSE WHEEL ASSY. 2 L 7 2 4T RT A24CE 2002082200081 20020822 00081 NM 2002 8 22 CA020731009 1 20020630 A 3040 5893543110 CONTROLLER BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE WINDSCREEN MALFUNCTIONED W B EMER. DESCENT O OTHER CR CRUISE 1 CA (CAN) OUTER PANE OF F/O,S NR 1 FORWARD WINDOW CRACKED AND DELAMINATED WHILE CRUSING AT 330. ALTITUDE REDUCED, DIFFERENTI AL REDUCED AS PRECAUTION. F/O,S WINDOW AND HEAT CONTROLLER REPLACED AS PER AMM. 2 L 7 2 4F 4 F A16WE E2EA 2002082200082 20020822 00082 EA 2002 8 22 A6WA200240023 1 20020716 A 2620 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA INOPERATIVE A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 423AW 622 622 7636 SMOKE CARGO FIRE WARNING DURING CLIMB C/W QRH FOR SMOKE CARGO, DISCHARGED BOTH CARGO FIRE BOTTLES. MAINTENANCE REMOVED AND REPLACED CARGO SMOKE DETECTOR, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2002082200084 20020822 00084 EU 2002 8 22 CA020731010 1 20020703 A 3260 201122006 UPLOCK AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE LT MLG FAILED W L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 CA (CAN) LT MLG DOOR NOT CLOSING ON GEAR EXTENSION 200 KTS. GO AROUND AND RE-CYCLED . NO JOY, DOOR NOT CLOSING. LT MLG DOO R UPLOCK ASSY. CHANGED AS PER AMM TASK 21-31-33-400-002. 2 L 7 2 4F 4 F RT A28NM E29NE 2002082200085 20020822 00085 NM 2002 8 22 SABA020084 1 20020820 A 3350 1306 LIGHT DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 AIRCRAFT 883 ON FLIGHT 5080 FROM AGS TO CLT, ON POST-FLIGHT THE CREW COULD NOT GET THE FLOOR EMERGENCY LIGHTS TO TEST. M AINTENANCE REPAIRED A WIRE AND REPLACED BULBS. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002082200089 20020822 00089 2002 8 22 CA020731015 4 20020710 A 3460 B546BAM0206 COMPUTER AIRBUS A319 A319114 3930350 NM CFMINT CFM56 CFM565A1 NE FLT MANAGEMENT MALFUNCTIONED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) AT 7000 FEET, 250 KTS. WITH AUTOPILOT NR 1 ENGAGED AIRCRAFT SUDDENLY ROLLED LEFT (UNCOMMANDED) A/P DISCONNECTED AND ROLL ARRESTED AT 20 DEGREES. NOT WAKE TURBULANCE. FLIGHT MANAGEMENT COMPUTER REPLACED AND SYSTEM CHECKED SERVICABLE . 2 L 7 2 4F 4 F RT A28NM E29NE 2002082200094 20020822 00094 EU 2002 8 22 CA020801006 1 20020724 A 7600 1519M83P14 CONTROL UNIT AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 1 ENGINE FAILED W O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA (CAN) DURING CRUISE NR 1 ENGINE FADEC A FAULT, FADEC B FAULT. ENGINE CONTINUED TO OPERATE NORMAL EXCEPT IN DESCENT NR 1 ENGINE HAD MOMENTARILY SMALL EXCURSIONS TOWARD IDLE (APROX 21. N1 DROP) AND IDLE WOULD ANNUNCIATE EVEN WHEN IDLE NOT RE QUIRED. REPLACE ECU NR 1 ENGINE AS PER AMM 73-21-60-400 ENGINE RUN-UP C/O NO FAULTS, CONSIDERED SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E29NE 2002082200096 20020822 00096 NM 2002 8 22 CA020801007 1 20020630 A 5610 WINDOW AIRBUS A319 A319114 3930350 NM COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA (CAN) CAPT'S LATERAL FIXED OUTER WINDOW OUTER SHIELD CRACKED CAPT'S LATERAL FIXED WINDOW REPLACED PER AMM 56-11-12 2 L 7 2 4F RT A28NM 2002082200097 20020822 00097 NE 2002 8 22 CA020801009 2 20020731 A 8510 519587 CASE CNDAIR CL215 CL2151A10 1900320 EA PWA R2800 CA3 52026 NE HAMSTD 43E 43E60 NE RT ENGINE DAMAGED W E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CA (CAN) FLIGHT CREW OBSERVED OIL LEAKING FROM RIGHT ENGINE AND INITIATED A PRECAUTIONARY ENGINE SHUTDOWN. AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NOSE CASE PLUG INSERT THREADS HAD STRIPPED IN CASE. NOSE CASE WAS REP LACED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4R 4 R RT A14EA E231 6 C P871 2002082200101 20020822 00101 CE 2002 8 22 CA020802003 1 20020731 A 3231 DOOR BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA LT MLG OBSTRUCTED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) CREW REPORTS ON CLIMB WHEN LANDING GEAR WAS SELECTED UP, RETRACTION / EXTENSION MOTOR SOUNDED SLOW AND THEN STOPPE D COMPLETELY PART OF THE WAY UP. EMERGENCY EXTENSION WAS CARRIED OUT AND A SAFE LANDING OCCURRED. VISUAL INSPECTION FOUN D LT INBOARD MAIN LANDING GEAR DOOR HAD CAUGHT THE INBOARD WHEEL DURING RETRACTION CAUSING THE CIRCUIT BREAKER TO TRIP. GEAR DOORS RERIGGED AND PARTS ORDERED. GROUND AND FLIGHT FUNCTION CHECKS CARRIED OUT. NO FURTHER FAULTS. 1 L 7 2 3T 4 T A14CE E4EA 2002082200102 20020822 00102 EA 2002 8 22 CA020802004 1 20020731 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ACM BAY SEIZED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) COCKPIT PACK TEMP STARTED CLIMBING UNCONTROLLABLY IN AUTOMATIC AND MANUAL MODE. PACK PSI NORMAL. FAULT TRACED TO S EIZED AIR CYCLE MACHINE. ACM REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002082200103 20020822 00103 NM 2002 8 22 02233409 1 20020821 A 3350 321430 BATTERY PACK DORNER DO32 DO328300 NM A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 409FJ 3161 During preflight inspection, the crew reported that the first row of emergency floor track lights were inoperative. Mai ntenance personnel removed and replaced an emergency exit light battery pack. An operational check was satisfactory and the aircraft was returned to service. 2 H 7 2 4T RT A55NM 2002082200104 20020822 00104 NM 2002 8 22 DL73K020871 1 20020725 A 2910 BACH6P0263CC HYDRAULIC LINE BOEING 737 737232 1384475 NM NLG BLOWN A DALA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 312DL 23084 LOSS OF A-HYD SYS WHEN LANDING GEAR HANDLE WAS LOWERED. BOTH LOW PRESS A-SYS LIGHTS ILLUM AND HYD QTY GAUGE WENT TO ZER O. LOUD BANG WAS HEARD WHEN GEAR WAS LOWERED. FOUND NOSE GEAR MAIN ACTUATOR PRESS LINE BLOWN. INSTALLED REPLACEMENT H YD LINE PER MM, HYD SERVICED TO FULL. CYCLED GEAR HANDLE. NO LEAKS, PRESS GOOD. 2 L 7 2 4F RT A16WE 2002082200105 20020822 00105 NE 2002 8 22 CA020806001 2 20020803 A 7250 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT SEIZED W E A ENGINE SHUTDOWN UNSCHED LANDING E Y J VIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CA (CAN) "WHILE IN CRUISE FLIGHT, THE LEFT ENGINE DEVELOPED A HIGH FREQUENCY VIBRATION, REGISTERING ABOUT 1.5 ON THE VIBRAT ION METER. ABOUT 30 SECONDS LATER THE N2 WENT TO ZERO. ELECTED TO DIVERT TO IND AND LANDED ABOUT 20 MINUTES LATER. FOUND THE N2 SECTION OF THE LT ENGINE WILL NOT TURN. AN ENGINE CHANGE HAD BEEN INITIATED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002082200106 20020822 00106 EA 2002 8 22 CA020806002 1 20020719 A 2822 NPN CONNECTOR CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A NE PUMP FILTER FAILED W O OTHER J WARNING INDICATION IN INSP/MAINT 1 CA (CAN) AS A RESULT OF REPORTED "PUMP INOP" LIGHT AND ADAPTER OIL "HI TEMP" LIGHT, REPLACED THE APU BOOST PUMP. OPERATED NORMALLY FOR THE FIRST FEW TESTS BUT QUIT AGAIN. DISCOVERED NO POWER AT THE CONNECTOR INSIDE THE BOOST PUMP CANNISTER. THE FUEL WAS DRAINED AND THE CONNECTOR WAS FOUND BURNED. THIS IS LOCATED INSIDE THE FUEL TANK AS PART OF A SUBMERGED C ANNISTER/PUMP ASSEMBLY AND IT APPEARS THAT FUEL GOT INSIDE THE PLUG OR HOSE CAUSING THE PINS TO SHORT OUT. ALL PARTS REP LACED AND SYSTEM FUNCTIONS NORMAL. 2 L 7 2 4F 4 F RT A21AE E15NE 2002082200108 20020822 00108 NM 2002 8 22 DL73K020922 1 20020807 A 2910 HYDRAULIC LINE BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 243WA 45622 23517 709162 NR 2 ENGINE HYD PUMP RUPTURED THE PRESS LINE AND LOST ALL HYD QTY. FOUND RIGHT ENGINE HYD PUMP PRESS LINE LEAKING. REP LACED LINE. PULLED AND INSPECTED ALL SYSTEM AND CASE DRAIN FILTERS, NO TROUBLE FOUND. SERVICED HYD TO FULL. RAN ENGIN E AND ELEC PUMPS. CYCLED ALL FLT CONT. LEAK CHECKS GOOD. ALL CHECKS NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 2002082200110 20020822 00110 EA 2002 8 22 CA020806005 1 20020802 A 2121 FAN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE GALLEY EXAHAUST FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) AFTER T/O STRONG ACRID SMELL ON THE FLIGHT DECK, SIMILAR TO ELECTRICAL BURNING. SOURCE OF ODOR WAS NOT LOCATED BUT LIMITED TO THE FLIGHT DECK. ODOR WAS SUSTAINED. GALLEY EXHAUST FAN CHANGED, AIRCRAFT GROUND. RUN AND PNEUMATICS CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002082200111 20020822 00111 EA 2002 8 22 CA020806006 1 20020805 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT & RT FAILED W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CA (CAN) FLAP FAILED AT 8 DEGREES. LT AND RT BPSU REPLACED AND ADJUSTED AS PER AMM 27-51-10 2 L 7 2 4F 4 F RT A21EA E15NE 2002082200112 20020822 00112 NM 2002 8 22 DL73K020934 1 20020809 A 2560 BATTERY BOEING 737 737247 138448D NM MEGAPHONE DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 377DL 23604 AFT MEGAPHONE INOP. REPLACED BATTERIES. 2 L 7 2 4F A16WE 2002082200113 20020822 00113 NE 2002 8 22 CA020806007 2 20020723 A 7230 JA804373 SEAL BOEING 767 767209 1385127 NM PWA JT9 JT9D7R4D 52054 NE ENGINE BEARING FAILED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) THIS ENGINE WAS REMOVED DUE TO HIGH OIL CONSUMPTION, REFURBISHED AND WITH BELOW 2000 HRS ON WING . BEARING SEALS FAILED. SEALS HAD JAMMED IN THEIR HOUSINGS IN REARWARD POSITION RENDERING THEM USELESS. 2 L 7 2 4F 4 F RT A1NM E3NE 2002082200114 20020822 00114 NE 2002 8 22 CA020806008 2 20020727 A 7200 ENGINE BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE NR 2 FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) WHEN ADDING THRUST FOR T/O, HEARD LOUD BANG AND NOTICED PARAMETERS DROPPING. SHUT DOWN AND SECURED NR 2 ENGINE. NR 2 ENGINE AND T/R REPLACED AS PER AMM 2 L 7 2 4F 4 F A16WE E2EA 2002082200115 20020822 00115 NM 2002 8 22 DL757020813 1 20020713 A 5330 146N37305 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 607DL 22814 THE FUSELAGE SKIN WAS FOUND WITH A DENT AND GOUGE AT THE STRINGER 14L LAP JOINT AT FS 1691. THE DAMAGE WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383291-14, REV A. 2 L 7 2 4F RT A2NM 2002082200116 20020822 00116 NM 2002 8 22 CA020806010 1 20020806 A 3242 BRAKE ASSY BOEING 727 727217 1384061 NM PWA JT8 JT8D17 52049 NE MLG FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) NR 4 MAIN LANDING GEAR BRAKE ASSY FOUND DRAGGING DURING PUSHBACK. NR 4 MAIN BRAKE ASSEMBLY AND MAIN WHEEL REPLACED DUE TO DAMAGE. TOTAL TIME OF BRAKE ASSY ARE 381 CYCLES SINCE OVERHAUL. THE LIFE OF THESE BRAKES PRIOR TO OVERHAUL ARE APPROXIMATELY 450 CYCLES. 2 L 7 3 4F 4 F RT A3WE E2EA 2002082200117 20020822 00117 GL 2002 8 22 CA020806011 2 20020802 A 7260 GEARBOX BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) OIL METAL CONTAMINATION IN ENGINE GEARBOX AND GEARBOX SEND FOR INSPECTION AND REPAIR. 1 G 7 1 3U 3 U H2SW E4CE 2002082200118 20020822 00118 WP 2002 8 22 IXXA0200051O 1 20020820 A 2820 TANK DOUG DC8 DC871F 302199D WP #4 MAIN AND ALT UNCALIBRATED A IXXA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 11 820BX 82065 2138 46065 AFTER TAKE OFF FROM LRD, THE FLIGHT CREW NOTICED A SIGNIFICANT AIRCRAFT ROLL TO THE RIGHT WHICH REQUIRED HALF LEFT AILER ON TO MAINTAIN LEVEL FLIGHT. THE FLIGHT RETURNED TO LRD FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE #4 MAIN AND #4 ALTERNATE TANKS READING LOW. MAINTENANCE RECALIBRATED THE TANKS AND PERFORMED SUCCESS FUL OPERATIONAL CHECKS IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002082200119 20020822 00119 WP 2002 8 22 A4J2002F00001 1 20020802 A 3230 H50002125268 LATCH DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE BYPASS DOOR WORN A A4JA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS TO TAKEOFF 1 SO 35 932MJ 48156 AFTER TAKEOFF, LAND GR LVR WAS PLACED IN UP POSITION, FLT DECK CREW REPORTED NO RESPONSE TO GR HNDL (UP) SELECTION, WITH GR REMAINING IN DOWN AND LOCKED POS AND MN GR DOORS OPEN. RECYCLING OF THE GR HNDL WAS NO HELP. MAINT WAS NOTIFIED AN D A/C RETURNED. MAINT RECOVERED A/C AND DURING POST FLIGHT INSPECTION MAINT BYPASS DOOR WAS FOUND IN DOWN POSITION. WH EN MAINT BYPASS DOOR WAS CLOSED AND WITH HYDR PRESSURE APPLIED MAIN GR DOORS CLOSED. A/C WAS TOWED TO HANGER, LT GR DO OR WAS REPLACED IAW MM AND A GR SWING WAS PERFORMED IAW MM WITH ALL GR SYS OPERATING NORMAL. BYPASS DOOR LATCH WAS REPL ACED DUE TO UNSERVICEABLE SPRING AND WAS DETERMINED TO BE PRIMARY CAUSE OF AIR TURN BACK. A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2002082200120 20020822 00120 NM 2002 8 22 CA020806012 1 20020802 A 2740 56019P003 MOTOR BOEING 737 7372T2 1384491 NM PWA JT8 JT8D17 52049 NE STAB TRIM BINDING W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) ON APPROACH STAB TRIM REPORTED TO HAVE JAMMED.THE FLT LANDED W/O EVENT.RECTIFICATION UPON LANDING ENGINEER CONTACT ED.THE STAB TRIM SYS BRAKE FOUND APPLIED.STAB TRIM SYS THEN FUNCTIONED IN BOTH DIRECTIONS W/O FAULT. TRIM SYS THEN INSPE CTED PER AMM WITH NO FAULTS FOUND. A/C FLOWN TO YEA WITHOUT FURTHER FAULT. UPON INSPECTING AUTOPILOT TRIM MOTOR, IT AP PEARED TO RUN ROUGH. AUTOPILOT TRIM ACTUATOR REPLACED. MAIN DRIVE MOTOR ALSO REPLACED FOR TROUBLESHOOTING. 2 L 7 2 4F 4 F RT A16WE E2EA 2002082200122 20020822 00122 NM 2002 8 22 DL757020815 1 20020713 A 5315 146N51114 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 607DL 22814 THE UPPER CAP OF THE FS 1681 PASSENGER FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION. THE UPPER CAP FLANGE WAS TR IMMED OFF ALONG THE ENTIRE LENGTH OF THE BEAM TO REMOVE ALL OF THE CORROSION. A NEW ALUMINUM EXTRUSION CAP WAS FABRICAT ED AND INSTALLED PER ER/A 383326-14, REV A. 2 L 7 2 4F RT A2NM 2002082200123 20020822 00123 NM 2002 8 22 DL757020818 1 20020713 A 5330 146N361010 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 607DL 22814 THE FUSELAGE SKIN WAS FOUND WITH 2 TIME-LIMITED SKIN REPAIRS FWD AND AFT OF THE FS 1720 BULKHEAD AND BETWEEN STRINGERS 2 9L & 29R. THE PREVIOUS REPAIR AREAS WERE CUTOUT TO COMPLETELY REMOVE ALL EXISTING FASTENER HOLES. THE CUTOUTS WERE REP AIRED WITH 2 EXTERNAL DOUBLERS EACH PER ER/A 383392-14, REV A. 2 L 7 2 4F RT A2NM 2002082200124 20020822 00124 NM 2002 8 22 DL757020841 1 20020718 A 5320 143N8512 SILL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 607DL 22814 THE OUTER CHORD OF THE C1 DOOR LOWER SILL WAS FOUND CORRODED. TO REPLACE THE CHORD, THE FS 620 FRAME OUTER CHORD AND WE B WERE CUT AND LOWER ENDS REMOVED. A NEW SILL CHORD WAS INSTALLED AND LOWER FRAME SECTION REINSTALLED WITH REPAIR ANGLE SPLICES. THE WORK WAS ACCOMPLISHED PER ER/A 383339-14, REV A. 2 L 7 2 4F RT A2NM 2002082200125 20020822 00125 NM 2002 8 22 DL757020847 1 20020719 A 3350 LIGHT BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 604DL 22811 EMERGENCY LIGHT OUTSIDE OF L-2 DOOR INOP. RELAMPED EMERGENCY LIGHT, CHECK GOOD. 2 L 7 2 4F RT A2NM 2002082200126 20020822 00126 NM 2002 8 22 DL757020864 1 20020724 A 2150 32024422 CHECK VALVE BOEING 757 757232 1384965 NM A/C BAY OUT OF POSITION A DALA O OTHER O OTHER CL CLIMB 1 SO 27 626DL 22916 RIGHT PACK ON PREV MCO AS BEING INOP. DURING CLIMBOUT OF JAX CABIN TEMPS RAN HOT. UNABLE TO DECREASE CABIN TEMPS BELOW 90 DEGREES. FOUND RIGHT PACK TRIM AIR CHECK VALVE IMPROPERLY POSITIONED WHICH WAS ALLOWING LEFT PACK AIR TO PASS THROU GH THE RIGHT ACM. RIGHT PACK IS INOP AND CAUSED THE HI CABIN TEMPS. REPOSITIONED CHECK VALVE AND NO RIGHT PACK REMAINS ISOLATED FROM LEFT. 2 L 7 2 4F RT A2NM 2002082200127 20020822 00127 NM 2002 8 22 DL757020888 1 20020729 A 3230 RELAY BOEING 757 757232 1384965 NM LANDING GEAR FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 637DL 23760 WHILE PERFORMING 757 ACJIC 6017 GEAR DOORS FAILED TO OPERATE AS REQUIRED. TROUBLESHOOTING REVEALED POWERPACK MOTOR HAD BAD INTERNAL WINDING DUE TO CONSTANT VOLTAGE APPLICATION. RELAY K10369 AND POWERPACK ASSY WERE CHANGED AND TESTED PER 7 57ACJIC OP 6017 WITH NO FURTHER PROBLEMS. AC WAS RETURNED TO SERVICE AFTER COMPLETING SCHEDULED MTC. FAILURE OF RELAY K10369 IN CLOSED POSITION CAUSED FAILURE OF POWERPACK ASSY. 2 L 7 2 4F RT A2NM 2002082200128 20020822 00128 NM 2002 8 22 DL757020904 1 20020730 A 5320 146N85125 SILL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 605DL 22812 CORROSION FOUND ON THE C2 DOOR LOWER SILL WHICH REQUIRES REPLACEMENT OF OUTER CHORD. REPLACEMENT OF CHORD REQUIRES SPLI CE OF THE STA 1440 FRAME OUTER CHORD AND WEB. CORRECTIVE ACTION, ER/A 383444-14 R.B. 2 L 7 2 4F RT A2NM 2002082200129 20020822 00129 NM 2002 8 22 DL757020906 1 20020804 A 1420 324049 TERMINAL BOEING 757 757232 1384965 NM COCKPIT BROKEN A DALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 27 679DA 26955 SHORTLY AFTER T/O LOST LEFT FMC FOLLOWED RAPIDLY BY LOSS OF NUMEROUS LEFT AC POWERED EQUIPMENT. LOA PROBE, L AFT FUEL P UMP, CTR L FUEL PUMP, L FMC FAIL, L IRS ON DC, ANTISKID - NUMEROUS STATUS MESSAGES. ADVISED FLT CNTRL, MTC AND ATL. DE CLARED EMERGENCY DUE TO OVERWEIGHT LANDING. FOUND CAPT INST XFER ON EICAS. REPLACED CAPT IBVSU, NO HELP. FOUND BROKEN TERMINAL ON C901 CIRCUIT BREAKER IN P31 PANEL. INSTALLED NEW TERMINAL, ALL OPS GOOD. 2 L 7 2 4F RT A2NM 2002082200130 20020822 00130 NE 2002 8 22 CA020807002 2 20020717 A 7250 CF343B1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT FAILED W E C ENGINE SHUTDOWN ABORTED TAKEOFF E Y J VIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 CA 10462 (CAN) ON PASSING 400 FT ABOVE GROUND AFTER TAKEOFF, A SEVERE 4.5 VIBRATION WAS FELT AND CONFIRMED. ITT INCREASED TO 935 DEGREES CENTIGRADE WITH OIL PRESSURE MASTER WARNING LIGHT. ENGINE SEVERE/FIRE DRILL CARRIED OUT AND RETURN TO ELS. MET AL CHIPS FOUND ON THE ENGINE CHIP DETECTOR. ENGINE CHANGED WAS CARRIED OUT ON THE LT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002082200131 20020822 00131 NM 2002 8 22 DL757020910 1 20020804 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 605DL 22812 THE FUSELAGE SKIN WAS FOUND DENTED AT FS 1624 ABOVE STRINGER 18L. THE DENT WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL DOUBLER PER ER/A 383531 -14, REV A. 2 L 7 2 4F RT A2NM 2002082200132 20020822 00132 NM 2002 8 22 DL757020913 1 20020604 A 5330 146N35317 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 605DL 22812 WHILE ACCOMPLISHING A REINFORCEMENT MODIFICATION TO THE AFT VHF ANTENNA CUTOUT AT FS 1473 AND RBL 3.2 AND EXISTING REPAI R DOUBLER WAS REMOVED. THE NEW CUTOUT WAS REPAIRED WITH 2 EXTERNAL DOUBLERS PER ER/A 383467-14, REV A. 2 L 7 2 4F RT A2NM 2002082200133 20020822 00133 NM 2002 8 22 DL757020921 1 20020807 A 3350 767 LIGHT BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 618DL 22908 ON LAYOVER FOUND EXTERIOR EMERGENCY LIGHT AT L2 DOOR DID NOT ILLUMINATE. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A2NM 2002082200134 20020822 00134 NM 2002 8 22 DL757020929 1 20020808 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 6706Q 30422 LEFT OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS INOP. REPLACED BATTERY POWER SUPPLY, OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2002082200135 20020822 00135 NM 2002 8 22 DL757020933 1 20020809 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 626DL 22916 FOUND ON LAYOVER SEVERAL EMERGENCY LIGHTS INOP IN AFT CABIN OVERHEAD INBOARD OF PSU CLOSEOUT PANEL. REPLACED BASE M737 AND BATTERY PACK. NOW CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002082200136 20020822 00136 NM 2002 8 22 DL757020942 1 20020813 A 5320 143N852210 SILL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 611DL 22818 THE OUTER CHORD OF THE C1 DOOR CUTOUT LOWER SILL WAS FOUND WITH SEVERAL AREAS OF CORROSION. THE CHORD WAS REMOVED AND A NEW REPLACEMENT CHORD INSTALLED. THE WORK WAS ACCOMPLISHED PER ER/A 383664-14. 2 L 7 2 4F RT A2NM 2002082200137 20020822 00137 NE 2002 8 22 UHL2002F00003 2 20020715 A 7230 6044T42P10 DISK SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE 5TH STG COMP FAILED A UHLA E ENGINE SHUTDOWN J X WARNING INDICATION ENGINE FLAMEOUT CR CRUISE 1 NE 03 149SZ 340A149 GEE367503 CREW HEARD (CLUNKING NOISE) FROM NR 1 ENGINE FOLLOWED BY FAILURE OF NR 1 ENGINE. TORQUE NOSE GEAR AND FF DROPPED TO ZER O. (AUTO SHUTDOWN) EVENT OCCURRED AT APPROX 7000 FT MSL. 15 MINUTES PRIOR TO FAILRE, CREW ACCOMPLISHED NORMAL TREND MO NITORING. EMERGENCY DECLARED AIRCRAFT LANDED. INVESTIGATION WITH BOROSCOPE DISCOVERED FOREIGN OBJECT DAMAGE OF 5TH STA GE COMPRESSOR AND BACK. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002082200138 20020822 00138 GL 2002 8 22 DL764020792 2 20020706 A 7200 ENGINE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL LEFT VIBRATION A DALA K NONE E VIBRATION/BUFFET CL CLIMB 1 SO 27 832MH 29704 FAILED VERIFICATION FLIGHT FROM FAN LUBE (BOTH ENGINES). LEFT ENGINE VIBES TO 4.3. PERFORMED AVM TRIM BALANCE. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E23EA 2002082200139 20020822 00139 NM 2002 8 22 DL764020862 1 20020723 A 1430 114T41457 BOLT BOEING 767 767432ER 1385134 NM L/E SLAT FAILED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 833MH 29706 EICAS MSG L/E SLAT ASSYM ILLUMINATED WHILE EXTENDING FLAPS TO 15 DEGS. T/E FLAPS INDICATE 15 DEG L/E SLATS YELLOW. PSE U TEST SHOWS SENSOR TARGET 285. FOUND TARGET MISSING AND BOLT SHEARED. REPLACED BOLT AND TARGET TO INBOARD AUX TRACK N R 4 SLAT PER AMM NO RII PER TOPP 40-30-05. L/E SLAT OPS CK OK. EICAS MSG CLEARED. 2 L 7 2 4F RT A1NM 2002082200140 20020822 00140 WP 2002 8 22 ZW0A0208001 1 20020729 A 2410 325753 O-RING DOUG DC9 DC983 3022083 WP RT CSD DETERIORATED A ZW0A A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CE 13 931TW 49527 DURING CRUISE OIL QTY IN RT ENGINE DROPPED FROM 9 QTS TO 5 QTS, OIL PRESSURE REMAINED NORMAL. REDUCED POWER AND MADE UN SKD LANDING. CSD TRA553 WET SPLINE CAVITY O-RING LEAKING DUE TO DETERIORATION. REPLACED CSD AND PACKING PER MM D9-24-0 3. 2 L 7 2 4F RT A6WE 2002082200141 20020822 00141 WP 2002 8 22 ZW0A0208003 1 20020723 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9619V 53566 DURING CHECK-C LONGERON 28R DAMAGED AT FUSELAGE STATION 110 TO FUSELAGE STATION 129. REPAIRED LONGERON 28A FUSELAGE STA TION 110 TO FUSELAGE STATION 129 PER SRM 53-02 FIG 18. NO CRACKS FOUND PART 6-51-00-03. 2 L 7 2 4F RT A6WE 2002082200142 20020822 00142 WP 2002 8 22 ZW0A0208004 1 20020723 A 5320 CHANNEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9619V 53566 DURING CHECK-C TEE CHANNEL BELOW LONGERON 28R FUSELAGE STATION 110 TO APPROX FUSELAGE STATION 129 DAMAGED. REPLACED TEE CHANNEL 9911597-502 AND SEAL PER ARA18213. 2 L 7 2 4F RT A6WE 2002082200143 20020822 00143 WP 2002 8 22 ZW0A0208005 1 20020723 A 5320 TEE CHORD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9619V 53566 DURING CHECK-C BULKHEAD CHORD DAMAGED FUSELAGE STATION 110 LONGERON 27R AND 28R AND TEE CHANNEL AFT SIDE OF BULKHEAD. C OLD WORKED TEE CHORD NDT INSPECTED PER ARA 18213 ITEM 3 SHOT PEENED, NO CRACK FOUND PER 6-51-00-03. 2 L 7 2 4F RT A6WE 2002082200144 20020822 00144 NM 2002 8 22 ZW0A0208202 1 20020801 A 3350 LIGHT BOEING 757 7572Q8 1384972 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST UK UNKNOWN 1 CE 13 702TW 28162 EGRESS LIGHTS OUT ROW 14 AND 15 DUE TO WEAR. RELAMPED AT ROW 14. OPS CHECKED NORMAL. LAST CHECK-C LAX 6/12/01. 2 L 7 2 4F RT A2NM 2002082200145 20020822 00145 WP 2002 8 22 ZW0A0208203 1 20020803 A 3610 B-NUT DOUG DC9 DC982 3022082 WP A/C BAY LOOSE A ZW0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 13 914TW 49185 DURING TAKEOFF HIGH TEMP LIGHT IN TAIL COMPARTMENT RESULT IN UNSCHEDULED LANDING/RETURN TO STL. PNEUMATIC PRESS REGULAT OR RELIEF LINE LOOSE HEAT EXCHANGE VENTING TO TAIL COMPARTMENT RT HEAT EXCHANGE PERRY SEAL LEAKING. TIGHTENED B-NUT ON LT PRESS REGULATOR RELIEF LINE REPOSITIONED HEAT EXCHANGER SEALS REPLACED RT PAC PERRY SEAL. LEAK CHECK TAIL COMPARTMEN T WITH ENGINES AT HI POWER PER MD 9-36-07. LEAK CHECK ALL NORMAL. 2 L 7 2 4F A6WE 2002082200146 20020822 00146 WP 2002 8 22 DHL2002806535 1 20020727 A 2720 5644210 RUDDER DOUG DC8 DC873F 302199F WP WORN A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 81567 46002 N/R 2473 RUDDER OUTER PLATING AROUND ZR101.000 RH SIDE(MAJOR REPAIR)CORR: PERFORMED MAJOR REPAIR IAW EO DHL020626 , ED-3 111, EO SEMAN 2002725. REMOVED FASTNERS WITHIN REPAIR AREA IAW SRM51-1-21 PG. 1, TRIMMED OUT DAAGED SHIMN AREA IAW EO DH L 020626, ED3111, EO SEMANS 20022725. CLEANED , TREATED AND PRIMED AREA IAW SRM51-1-8B , FABRICATED REPAIR DOUBLER (2024 T3AL.040) IAW DHL 020626 ED-3111, EO SEMAN SEMAN 20022725, CLEANED, TREATED AND PRIMED REPAIR DOUBLER WITH NEW FASTNERS ON RUDDER OUTER PLATING AROUND STA. ZR101.000 , IAW SRM51-1-21 PG.1. 2 L 7 4 4F RT 4A25 2002082200147 20020822 00147 NE 2002 8 22 ZW0A0208204 2 20020805 A 7250 TURBINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE LT ENGINE FAILED A ZW0A E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 CE 13 939AS 49657 DURING CLIMB LEFT ENG TURBINE FAILURE. FLT CREW DECLARED EMERGENCY SHUT ENG DOWN PER QRH RESULTING IN UNSCHEDULED LANDI NG. REPLACED NR 1 ENG, OPS AND LEAK CHECKED NR 1 ENG. 2 L 7 2 4F 4 F RT A6WE E9NE 2002082200148 20020822 00148 WP 2002 8 22 ZW0A0208301 1 20020801 A 2910 HYDRAULIC SYSTEM DOUG DC9 DC983 3022083 WP APU BAY LEAKING A ZW0A O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 CE 13 967TW 53617 HYD FLUID LEAK INTO APU INLET RESULTING IN SMOKE IN THE CABIN. RETURNED AIRCRAFT TO THE GATE. CHANGED WATER SEPARATORS AND PERFORMED MD9-49-06. PAC BURNOUT OP CHECK. 2 L 7 2 4F RT A6WE 2002082200149 20020822 00149 EA 2002 8 22 M02115 1 20020807 A 2700 3833001009 DAMPER CNDAIR CL600 CL6002B19 1900309 EA YAW DAMPER FAILED A MASA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SW 07 17156 7156 YAW DAMPNER NR 2 WILL NOT ENGAGE. MECHANIC T/S SYSTEM. REMOVED AND REPLACED NR 2 YAW DAMPNER ACTUATOR NO FURTHER DEFEC T. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002082200150 20020822 00150 EU 2002 8 22 MALA020491 1 20020821 A 2710 CABLE SAAB SF340 340B 7860101 EU A MALA K NONE E VIBRATION/BUFFET NR NOT REPORTED 1 GL 15 446XJ 340B446 ON FLIGHT #2727, WHEN FLAPS SELECTED 15 DEGREES,CAPT AND FO'S YOKE VIBRATE UNTIL FLAPS SELECTED TO 20 DEGREES CAPT YOKE ALSO HAS RATTLE THAT ONLY STOPS WHEN HOLDING YOKE WITH PRESSURE. MAINTENANCE PERFORMED AILERON SYSTEM CABLE CHECK. NOT ED LHOB AFT CABLE CIRCUIT TENSION INCORRECT. ADJUSTED TENSION AS REQURIED. REF SAAB AMM CH 27-110-002. 2 L 7 2 4T RT A52EU 2002082200151 20020822 00151 EU 2002 8 22 MALA020492 1 20020818 A 5320 SEAT TRACK SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 DURING 4K INSPECTION IN CWA, RH CENTER AISLE SEAT TRACK HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-7 0-40. REF 409 #138103 FOR DETAIL. A/C RELEASE DATE: 8/20/02. 2 L 7 2 4T RT A52EU 2002082200152 20020822 00152 EU 2002 8 22 MALA020501 1 20020819 A 5320 PLATE SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 DURING 4K INSPECTION IN CWA, PLATE FOR PANEL 122DZ TO 121EZ AND 122EZ TO 121FZ ARE CORRODED. MAINTENANCE REMOVED AND RE PLACED BOTH PLATES. REF TO 409 #138121 FOR DETAIL. A/C RELEASE DATE 8/20/02 2 L 7 2 4T RT A52EU 2002091000098 20020910 00098 WP 2002 9 10 ARWA20020807 1 20020820 A 2612 CA326051002 CONNECTOR DOUG DC8 DC861 3021952 WP NR 1 ENGINE DAMAGED A ARWA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 19 30UA 45888 NR 1 ENGINE FIRE WARNING IN-FLIGHT. PERFORMED EMERGENCY CHECK LIST AND DIVERTED TO SAN JUAN (TJST). CHECK NR 1 ENGINE FOR EVIDENCE OF FIRE OR PNEUMATIC LEAK, NONE FOUND. FOUND BOTTOM LOOP SENSOR CANNON PLUG DAMAGED; REMOVED AND REPLACED CANNON PLUG. REMOVED AND REPLACED FIRE DETECTOR AMP; REMOVED AND REPLACED LT INBOARD FIRE EXT CONTAINER WITH NEW SQUIBS . ENGINE RAN AT HIGH POWER AND SYSTEM CHECKED NORMAL IAW MM REF 26-4-1, MM 20-50-1 AND MM 26-10-2. 2 L 7 4 4F 4A25 2002091100082 20020911 00082 NM 2002 9 11 F3LA200200226 1 20020821 A 5320 WEB BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED WEB AT BS 927, STR 21L, CORRODED. FABRICATED AND INSTALLED REPLACEMENT WEB PER SR M 51-10-02. 2 L 7 2 4F RT A16WE 2002091100083 20020911 00083 NM 2002 9 11 F3LA200200227 1 20020821 A 5315 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON UNDERSIDE OF CARGO FLOORBEAM AROUND NUT PLATES, BS 772 TO 513, LBL 2. 5. 2 L 7 2 4F RT A16WE 2002082200153 20020822 00153 NM 2002 8 22 F3LA200200228 1 20020820 A 5414 SKIN BOEING 737 737317 138447P NM NO. 2 ENG DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED NO. 2 ENGINE PYLON TOP FWD SKIN DELAMINATED AT FWD INBD CORNER. REPAIRED AND REFI NISHED PER SRM 51-70-17. 2 L 7 2 4F RT A16WE 2002082200154 20020822 00154 NM 2002 8 22 F3LA200200229 1 20020820 A 5320 STRAP BOEING 737 737317 138447P NM CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED FORE AND AFT FUSELAGE STRAP ON RT. SIDE AT STA. 540 CRACKED AT AFT END ABOVE RT. P ACK INLET DUCT. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-30-71, 51-40-2 AND 51-7-77 2 L 7 2 4F RT A16WE 2002082200155 20020822 00155 EU 2002 8 22 SIMA200219132 1 20020708 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU 21LN/23LN INOPERATIVE A SIMA K NONE O OTHER CR CRUISE 1 SW 21 384AE 340B384 CREW REPORTED EMERGENCY LIGHT CONTROL CIRCUIT BREAKER POPED DURING FLIGHT. C/A: REMOVED AND REPLACED BATTERY SUPPLY 21L N AND 23LN IAW MM. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002082200156 20020822 00156 NM 2002 8 22 F3LA200200230 1 20020820 A 5313 STRINGER CLIP BOEING 737 737317 138447P NM BS 597 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CRACKED TIE CLIP TO STRINLGER AT BS 597, STR. 8-R. REPLACED STRINGER CLIP PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002082200157 20020822 00157 2002 8 22 AWXA200200787 4 20020818 A 3441 HG1050AD04 IRU BOEING 737 737301 1384611 NM ZONE 100 - FUSEL FAILED A AWXA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 WP 28 324AW 54149 999 23261 PHX - AIR TURN BACK - FLT 0646 - ON CLIMB FROM PHX EN ROUTE FOR ONT THE #2 INERTIAL REFERENCE SYSTEM LIGHT ILLUMINATED, DUE TO WEATHER AT ONT AIRCRAFT TURNED BACK TO PHX. MAINTENANCE REMOVED AND REPLACED THE #2 INERTIAL REFERENCE UNIT, FUNC TIONAL CHECK OF NEW UNIT WAS GOOD. 2 L 7 2 4F RT A16WE 2002082200158 20020822 00158 NM 2002 8 22 AWXA200200788 1 20020731 A 5410 6552263353 ANGLE BOEING 737 737277 1384570 NM BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A "T" ANGLE CLIP WAS FOUND BROKEN ON INBOARD SIDE OF THE #2 ENGINE FIXED FAIRING BETWEEN 2ND AND 3RD ATTACH FITTINGS FROM THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE "T" ANGLE CLIP ON INBOARD SIDE OF THE #2 ENGINE FIXED FAIRING IAW B737-200 SRM 51-30-2, FIG. 7, PG. 2-3, & 32. 2 L 7 2 4F RT A16WE 2002082200159 20020822 00159 NM 2002 8 22 AWXA200200789 1 20020731 A 5410 6552263353 ANGLE BOEING 737 737277 1384570 NM BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A "T" ANGLE CLIP WAS FOUND BROKEN ON INBOARD SIDE OF THE #1 ENGINE FIXED FAIRING BETWEEN 2ND AND 3RD ATTACH FITTINGS FROM THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE "T" ANGLE CLIP ON INBOARD SIDE OF THE #1 ENGINE FIXED FAIRING IAW B737-200 SRM 51-30-2, FIG. 7, PG. 2-3, & 32. 2 L 7 2 4F RT A16WE 2002082200160 20020822 00160 NM 2002 8 22 AWXA200200790 1 20020731 A 5410 65522633806 LONGERON BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK THE #1 ENGINE FIXED FAIRING LOWER END "Z" ANGLE WAS FOUND CRACKED BETWEEN 1ST AND 2ND ATTACH FITTINGS FROM THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE LOWER END "Z" ANGLE ON THE #1 ENGINE FIX ED FAIRING IAW B737-200 SRM 51-30-2, FIG. 7, PG. 2-3, 5, 8-11, & 32. 2 L 7 2 4F RT A16WE 2002091100084 20020911 00084 NM 2002 9 11 F3LA200200231 1 20020820 A 5311 FRAME BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FRAME AT BS 967, LBL 14. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2002082200161 20020822 00161 NM 2002 8 22 F3LA200200232 1 20020820 A 5315 51057009 CHANNEL BOEING 737 737317 138447P NM BS 827 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON UNDERSIDE OF CARGO FLOORBEAM AROUND NUTPLATE, BS 827, RBL 25. INSTAL LED CHANNEL FOR FLOOR SUPPORT REPAIR PER 53-00-53. 2 L 7 2 4F RT A16WE 2002082200162 20020822 00162 EU 2002 8 22 C2XA02SH043 1 20020814 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 25811 094 SHV-DURING MAINTENANCE CHECK, MAINTENANCE FOUND THE AFT LOWER LEFT AND RIGHT EMERGENCY EXIT DOOR LIGHTS WILL NOT ILLUMIN ATE. MAINTENANECE REMOVED AND REPLACED EMERGENCY POWER SUPPLY 30WL IAW ATR AMM/JIC 33-51-21 AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002082300001 20020823 00001 EU 2002 8 23 CA020807004 1 20020730 A 2500 RDAV709101 MONITOR AIRBUS 330 A330342 EU RROYCE RB211 RB211TRENT77 NE CABIN FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) DURING FLIGHT THE LCD MONITOR AT L2 DOOR STOPPED WORKING AND EMITTED A BURNING SMELL. ON ARRIVAL IN CDG, MAINTENAN CE INSPECTED THE MONITOR AND ITS ASSOCIATED WIRING AND FOUND NO DAMAGE. THE SYSTEM WAS DEACTIVATED (CONNECTOR REMOVED AN D THE C/B PULLED) AND PUT ON MEL 25-20-01. THE VIDEO WAS REPLACED AT A LATER DATE AND SYSTEM CHECKED SERVICEABLE. 1 L 7 2 4F 4 F RT A46NM E39NE 2002082300002 20020823 00002 NM 2002 8 23 CA020808002 1 20020413 A 3260 PROXIMITY SENSOR BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA ROTOL R320 CR3204123F1 GL MLG MALFUNCTIONED W O OTHER J WARNING INDICATION DE DESCENT 1 CA (CAN) UNCOMMANDED GEAR EXTENSION: DURING DESCENT AT SPEED 275 WE COULD FEEL THAT THE GEAR / GEAR DOOR WENT DOWN MOMENTAR ILY WITH AN INTERMITTENT UNSAFE INDICATION. REDUSED SPEED AND LANDED WITHOUT ANY FURTHER INDICATIONS. INVESTIGATION / A CTION PROXIMITY SENSOR ELECTRONIC UNIT REPLACED ACCORDING AMM 32-61-01. 2 H 7 2 4T 4 T RT A13NM E00062EN 6 C P5NE 2002082300006 20020823 00006 NM 2002 8 23 CA020809002 1 20020808 A 2910 1121S11072 LIMITER BOEING 727 72751C 1384015 NM PWA JT8 JT8D7B 52053 NE HYD FLOW CRACKED W O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA (CAN) SYSTEM "A" HYDRAULIC FAILURE ON SHORT FINAL. MAINTENANCE FOUND OUTBOARD FLAP FLOW LIMITING VALVE CRACKED. REPLACE D. 2 L 7 3 4F 4 F A3WE E2EA 2002082300007 20020823 00007 EU 2002 8 23 CA020812001 1 20020806 A 2752 5275212154 ARM PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL FLAP DRIVE CRACKED W D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) DURING TAXI, AIRCRAFT CREW RECEIVED A FLAP WARNING FAULT. THE COMPUTER AUTOMATICALLY DISABLES THE SYSTEM WHEN A W ARNING OCCURS SO NO FLAP SELECTION WAS AVAILABLE. ON INSPECTION THE RT INBOARD FLAP DRIVE ARM WAS FOUND CRACKED AT THE WING ATTACHMENT. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002082300008 20020823 00008 NM 2002 8 23 CA020812002 1 20020810 A 2612 894093 FIRE LOOP BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE CHAFED W E B ENGINE SHUTDOWN EMER. DESCENT N FALSE WARNING DE DESCENT 1 CA (CAN) CREW EXPERIENCED A FIRE INDICATION ON NR 2 ENGINE DURING DESCENT INTO YXE. NR 1 FIRE BOTTLE WAS DISCHARGED & ENGIN E WAS SHUTDOWN. FIRE INDICATION RETURNED A SHORT TIME LATER. CREW DISCHARGED SECOND BOTTLE. EMERGENCY DECLARED & CREW REQUIRED EMERGENCY VEHICLES FOR A/C INSPECTION UPON LANDING. A/C LANDED WITHOUT INCIDENT. MAINT FOUND CHAFED WIRE ON NR 1 & 2 ENGINE FIRE DETECT LOWER ELEMENTS. REPLACED FIRE LOOP & GROUND TESTED SYSTEM AS SERVICEABLE. A/C RETURNED TO SE RVICE WITH NO FURTHER INCIDENTS TO REPORT. 2 L 7 2 4F 4 F A16WE E2EA 2002082300009 20020823 00009 NM 2002 8 23 CA020812003 1 20020810 A 4997 941D3352 CONNECTOR BOEING 737 7372Q9 138448M NM PWA JT8 JT8D9A 52048 NE APU SYSTEM BURNED W H DEACTIVATE SYST/CIRCUITS G J MULTIPLE FAILURE WARNING INDICATION IN INSP/MAINT 1 CA (CAN) ON TURNAROUND, WHEN FLT CREW SELECTED APU GENERATOR ON LINE, SEVERAL C/B,S TRIPPED. GENERATOR VOLTAGE LOW UNDER LOAD,BUT DID NOT TRIP OFF BUS. FOUND BTB TERMINAL CONNECTOR BOLT BURNED & LOOSE. BTB REPLACED. CHECKED SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 2002082300010 20020823 00010 NM 2002 8 23 CA020812004 1 20020810 A 2121 5007024260 GASPER FAN BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE CARGO BAY SMOKE W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) AT GATE, ODOR OF SMOKE IN COCKPIT. INVESTIGATION FOUND ODOR COMING FROM GASPER FAN. C/B PULLED AND AIRCRAFT DIS PATCHED UNDER MEL 21-24. 2 L 7 2 4F 4 F A16WE E2EA 2002082300012 20020823 00012 NM 2002 8 23 CA020813001 1 20020708 A 2844 7G980 PRESSURE SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FUEL SYSTEM INTERMITTENT W O OTHER N FALSE WARNING DE DESCENT 1 CA 36084 36084 (CAN) DURING DECENT NR 2 ENGINE FUEL PRESSURE CAUTION LIGHT FLICKERED. AFTER ARRIVAL NR 2 ENGINE FUEL PRESSURE SWITCH R EPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002082300013 20020823 00013 EA 2002 8 23 CA020813002 1 20020628 A 2910 82970009113 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 24468 24468 (CAN) DURING WALK-AROUND FOUND HYDRAULIC LEAK IN NR 1 NACELLE, HYDRAULIC LINE REPLACED WITH TEMP FLEX LINE. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002082300014 20020823 00014 EU 2002 8 23 CA020813003 1 20020803 A 6510 1053025136 BRACKET BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL T/R DRIVEBEARING LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE 2 BOLTS THAT HOLD THE TAIL ROTOR SHAFT OUTER RING BEARING TO THE BEARING BRACKET AT FRAME 9 LT BECAME LOOSE O VER A PERIOD OF 40 HOURS FROM LAST INSPECTION AND ELONGATED THE HOLES. THE BEARING ASSEMBLY STARTED TO SPIN AND HIT THE TAIL ROTOR SHAFT COVER. THE MARKS ON THE COVER WERE NOTICED ON THE NEXT SERVICEABILITY CHECK BY THE TECHNICIAN. THE TAIL ROTOR STIFFNER AND THE TAILBOOM SKIN WERE ALSO HIT BY THE BEARING OUTER RING. 1 G 7 2 3U 3 U H3EU E4CE 2002082300015 20020823 00015 NM 2002 8 23 CA020813004 1 20020708 A 6120 CONTROL UNIT DHAV DHC8 DHC8201 2809001 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE PROPELLER BINDING W E ENGINE SHUTDOWN E VIBRATION/BUFFET IN INSP/MAINT 1 CA (CAN) WHILE CARRYING OUT POST-ENGINE CHANGE GROUND RUNS. THE NR 1 ENGINE SUFFERED AN OVER TORQUE OF 149 PERCENT WHEN MO VING THE POWER LEVER FROM DISCING TO FLIGHT IDLE. THE CAUSE OF THE OVER TORQUE WAS DETERMINED TO BE FROM A BINDING PCU. THE PCU WAS REPLACED, THE PROPELLER ASSY WAS REPLACED DUE TO THE OVER TORQUE, AND THE ENGINE WAS INSPECTED IAW DASH 8 AMM ATA 71-00-00, AND PW-123 ENGINE MM ATA 5-10-00. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002082300017 20020823 00017 EU 2002 8 23 CA020813006 2 20020606 A 7230 PC72366610 COMPRESSOR GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY5118 54523 EU ENGINE FAILED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 CA (CAN) CREW REPORTED 3. MILS VIBRATION AT DECENT AT 70 PERCENT. LATER A LOUD BUZZ AT CRUISE, AND VIBRATION WAS 1.8 MILS. BOROSCOPED ENGINE, A GROUND RUN VIBRATION WAS WITHIN LIMITS. A ONE HOUR FLT AND A BUZZING COULD BE HEARD FROM A/C. AC/D C GENERATORS & HYDRAULIC PUMPS FROM LT ENGINE INSTALLED ON RT ENGINE WITH NO CHANGE. VIBRATION SURVEY IAW MAINT MANUAL C ARRIED OUT AND RESULTS POINTED OUT TO HP COMPRESSOR. ENGINE REVIEW AT RRC CONFIRMED VIBRATION. ENGINE STRIP REVEALED HP COMPRESSOR ROTOR STAGE 11 TO 12 FAILED. SPACER HAS A TEAR APPROX 6 INCHES AND HEAVY RUB. 2 L 7 2 4F 4 F RT A12EA E2EU 2002082300018 20020823 00018 EU 2002 8 23 CA020813009 1 20020813 A 5620 M105233027 TRACK BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL WINDOW DEBONDED W O OTHER D INFLIGHT SEPARATION CR CRUISE 1 CA (CAN) LT AFT SLIDING WINDOW TRACK BONDING FAILURE TO WINDOW PANEL. WHEN TRACK BONDING FAILED, THE SLIDING WINDOW FLEW A WAY FROM THE AIRCRAFT. HELICOPTER LANDED WITH NO FURTHER DAMAGE. 1 G 7 2 3U 3 U H3EU E4CE 2002082300019 20020823 00019 NM 2002 8 23 CA020813010 1 20020806 A 5320 69144681 FITTING BOEING 727 72725C 138400H NM FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 66295 66295 (CAN) DURING C3 CHECK FOUND STRINGER END FITTING CORRODED AT BS 740 AT STRINGER 9 LT, REMOVED CORRODED FITTING AND INSTA LLED NEW FITTING AT BS 740 AT STRINGER 9 LT IAW SRM 51-30-2 2 L 7 3 4F A3WE 2002082300020 20020823 00020 NM 2002 8 23 CA020813011 1 20020806 A 5320 65453132 STRINGER CLIP BOEING 727 72725C 138400H NM FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING C3-CHECK FOUND STRINGER CLIP CRACKED AT BS 1070 AT STRINGER 7 RT. REMOVED AND REPLACED WITH A NEW STRINGER CLIP AT 7R IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2002082300021 20020823 00021 NM 2002 8 23 CA020813012 1 20020806 A 5320 65453132 STRINGER CLIP BOEING 727 72725C 138400H NM FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING C3-CHECK FOUND STRINGER CLIP CRACKED AT BS 1050 AT STRINGER 6 LT. REMOVED AND REPLACED WITH A NEW STRINGER CLIP IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2002082300022 20020823 00022 NM 2002 8 23 CA020813013 1 20020806 A 5320 65453132 STRINGER CLIP BOEING 727 72725C 138400H NM FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING C3-CHECK FOUND STRINGER CLIP CRACKED AT BS 1050 AT STRINGER 8 LT. REMOVED AND REPLACED STRINGER CLIP WITH A NEW CLIP IAW SRM 51-30-2 2 L 7 3 4F A3WE 2002082300024 20020823 00024 NM 2002 8 23 CA020813015 1 20020806 A 5320 65453132 STRINGER CLIP BOEING 727 72725C 138400H NM FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING C3-CHECK FOUND STRINGER CLIP CRACKED AT BS 1030 AT STRINGER 8 LT. REMOVED AND REPLACED STRINGER CLIP WITH N EW CLIP IAW SRM 51-30-2 2 L 7 3 4F A3WE 2002082300025 20020823 00025 NM 2002 8 23 CA020814002 1 20020813 A 3234 656021132 ACCESSORY UNIT BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE MLG FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKE-OFF, CREW SELECTED GEAR HANDLE TO THE RETRACT POSITION. NO JOY UNTIL OVERRIDE TRIGGER INITIATED. A IRCRAFT RETURNED TO BASE & LANDED WITHOUT INCIDENT. LANDING GEAR ACCESSORY UNIT REPLACED & CHECKED SERVICEABLE IAW MM 3 2-10.4. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2 L 7 3 4F 4 F A3WE E2EA 2002082300026 20020823 00026 SW 2002 8 23 CA020814004 1 20020813 A 6320 407040050101 CASE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL M/R GEARBOX MISMANUFACTURED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) MAIN ROTOR GEARBOX HAS A CASTING FLAW IN CASE. 1 G 7 1 3U 3 U O H2SW E1GL 2002082300028 20020823 00028 GL 2002 8 23 CA020815001 2 20020808 A 7323 DRIVE SHAFT AEROSP AS355 AS355F2 8680812 EU ALLSN 25OC 250C20R GL GOVERNOR SHEARED W E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) IN CRUISE FLT, NR 2 ENGINE TORQUE DROPPED BELOW ENGINE TRIM ADJUSTMENT WITH POWER FLUXS. NR 2 ENGINE THROTTLED BA CK FROM FLT TO IDLE. RETURNED TO GATE AS A PRECAUTION. ENGINE DECELED FROM POINT TO ACTIVATE REIGNITION SYS, & CONTINUE D TO SPOOL DOWN TO APPROX 30 PERCENT N1, THROTTLE MOVED TO CUTOFF. A/C CONTINUED FLT IN OEI CONDITION FOR 30 MINUTES. PRELIMINARY INVEST SHOWED NO SIGNS OF EXTERNAL DAMAGE, FUEL, OIL, & AIR LINES INTACT, FUEL QUALITY CLEAN & CLEAR, FUEL FILTERS & SCREENS W/O MEASURABLE AMOUNT OF DIRT, & NO AIR IN FUEL SYS. NR 2 ENGINE ATTEMPTED START BUT WOULD NOT ACCELE RATE PAST 31 PERCENT MARK ON TWO OCCASIONS. 1 G 7 2 3U 3 U H11EU E4CE 2002082300029 20020823 00029 EA 2002 8 23 CA020815002 2 20020601 A 7250 311196501 CASE BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA COMBUST SECTION CRACKED W O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 CA 30901 (CAN) POWER SECTION WAS REMOVED DUE LOW POWER. 1 G 7 1 4U 4 U H4SW E22EA 2002082300030 20020823 00030 2002 8 23 WRNA200200004 4 20020822 A 2213 7876639001 COMPUTER LKHEED 1011 10113851 5265010 WP UNSERVICEABLE A WRNA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 05 311EA 326 193A1012 During Climb to cruise altitude Both Mach Feel Fail Lights came on. Fuel dump procedures carried out for Max landing wt (26K lbs dumped). Aircraft landed normal and returned to base.Corrective Action: Removed and replaced Trim Augmentation Computer. Op's check satisfactory I/A/W 22-13-01. Aircraft returned to service. 2 L 7 3 4F A23WE 2002082300031 20020823 00031 EA 2002 8 23 02234703 1 20020822 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 703BR 7467 During preflight inspection, the crew reported that the L/H overwing exterior emergency exit light was inoperative. Mai ntenance personnel removed and replaced the lamp in the L/H overwing exterior emergency exit light. An operational chec k was satisfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002082300032 20020823 00032 NM 2002 8 23 MDAS091012 1 20020819 A 2740 10622336 ACTUATOR BOEING 737 737800* NM TAIL CONE MALFUNCTIONED W Q0MF A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 WP 03 4168 28236 ON AUG19TH, AE 857 FLIGHT (A/C B-16802, S/N 28236) EXPERIENCED THAT "SPEED TRIM FAIL" LIGHT CAME ON DURING CLIMBED THROU GH 2500 FEET. BY 10 SECONDS, THE LIGHT WENT OFF. WHILE CLIMBED THROUGH 5000 FEET AND THE CREW ENGAGED THE "AUTO-PILOT", THE "STAB OUT OF TRIM" WARNING LIGHT CAME ON. THE CREW FOLLOWED QRH PROCEDURE, AND FOUND THAT THE CONDITION REMAINED UNC HANGED. DUE TO THE ROUTE NEED RNP AND RVSM OPERATION, IT HAD TO HAVE "AUTO-PILOT". IF NOT, THE CRUISE HEIGHT HAD TO DES CENT BELOW FL290. CONSIDERATION OF FUEL QUANTITY IN THAT SITUATION, THE CREW ASK ATC FOR AIR TURNED BACK TO CKS AIRPORT. AIRCRAFT LANDED SAFELY. IAW AMM PART 2 27-41-71, REPLACED STAB TRIM MOTOR. FUNCTION CHECK NORMAL. PER AMM 22-11-8 2 L 7 2 4F RT A16WE 2002082300033 20020823 00033 WP 2002 8 23 MEX2002257 1 20020608 A 3222 5910448541 STRUT DOUG DC9 DC982 3022082 WP NLG BROKEN W ASMF O OTHER O OTHER TX TAXI/GRND HDL 1 SW 23 1003X 54079 48067 DURING PUSH BACK THE NOSE LANDING GEAR WAS OVER-ROTATED MORE THAN 180 DEGREES. DURING REVISION IN PLATFORM THE FOLLOWIN G DAMAGES WERE DETECTED: RIGHT ACTUATORS BROKEN, LEFT ACTUATOR BLOCKADED IN LATERAL WALL, STEERING CONTROL CABLES BROKE N. AIRCRAFT WAS REPAIRED IN HANGER. 2 L 7 2 4F A6WE 2002082300034 20020823 00034 2002 8 23 MEX2002258 4 20020708 A 3418 9650449002 COMPUTER DOUG MD80 MD83 3023681 NM STALL WARNING FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 945AS 7267 49643 AIRCRAFT RETURNED TO PLATFORM AS DUE TO AUTO SLAT FAIL LIGHT ON, BOTH STALL WARNING COMPUTERS WERE FOUND WITH FAILURES, PROXIMITY SWITCH AND "C" AND "D" SENSORS WERE TESTED AND FAIL CONTINUE. EXCESSIVE GREASE WAS DETECTED IN OUTBOARD SLATS ACTUATORS. ACTUATORS WERE CLEANED AND STALL WARNING COMPUTER WAS REPLACED IAW MM. TEST OK. 2 L 7 2 4F RT 2002082300035 20020823 00035 WP 2002 8 23 MEX2002259 1 20020809 A 3250 S49166E9AS04012 CONTROL CABLE DOUG DC9 DC982 3022082 WP NLG STEERING BROKEN W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 1003X 48067 AIRCRAFT RETURNED TO PLATFORM DUE TO LACK OF STEERING CONTROL. SYSTEM WAS CHECKED AND A CONTROL CABLE WAS FOUND BROKEN. CABLE WAS REPLACED IAW MM. TESTS OK. 2 L 7 2 4F A6WE 2002082300036 20020823 00036 NE 2002 8 23 S02172025 2 20020710 A 7200 ENGINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 FAILED W SAJF A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 03 48469 NR 3 ENGINE A BANG DURING ROTATION, EGT PEAK 661 DEGREE C FOR SHORT TIME, THEN BACK TO NORMAL. EEC BITE NO FAULT MESS AGE FOUND. ENGINE INLET AND EXHAUST VISUALLY CHECKED NORMAL. BLEED VALVE SYS CHECKED NORMAL. BORESCOPE INSPECTION OF LP COMPRESSOR, HP COMPRESSOR, LP TURBINE & HP TURBINE NORMAL. VSV SYS RIG CHECKED FOUND IGV STAGE MISRIGGED ABOUT HALF RIG PIN HOLE. CHIP DETECTOR & OIL FILTER CHECKED NORMAL. GROUND ACTUATOR TEST NORMAL. ENG PERFORMANCE TEST NORMAL. EXC EPT AT EPR 1.3 N1 HIGHER THAN LIMIT. ENG RETURN TO SERVICE. A/C BACK TO TPE M/L REMOVED ENG. TEST CELL PERFORMED ENG WA TER WASH, FOUND PT4.95 TUBE DAMAGED, REPLACED. TEST CELL PERFORMED TEST 21 "PASSED". 2 L 7 3 4F 4 F RT A22WE E24NE 2002082300037 20020823 00037 WP 2002 8 23 2002FA0000988 1 20020820 A 6420 BEARING HUGHES 369 369E 4470707 WP SWASHPLATE LOOSE C K NONE O OTHER IN INSP/MAINT 1 WP 05 522PD 998 0373E TAIL ROTOR SWASHPLATE BEARING LOOSE, EXCESS PLAY 1 G 7 1 3U H3WE 2002082300038 20020823 00038 EU 2002 8 23 HCM2002F00001 1 20020718 A 6320 WARNING LIGHT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE M/R GEARBOX ILLUMINATED E HCMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 13 982BH 2876 9339 WHILE ON A SIGHTSEEING FLIGHT, PILOT EXPERIENCED A MAIN GEARBOX CHIP LIGHT INDICATION. THE PILOT MADE A PRECAUTIONARY L ANDING. UPON INSPECTION OF THE MAIN GEARBOX CHIP PLUGS BY MAINTENANCE PERSONNEL, NO METAL WAS FOUND. CLEANED MAGNETIC CHIP PLUGS AND CONNECTORS. OPERATIONAL CHECK AND LEAK CHECK FOUND TO BE SATISFACTORY. 1 G 7 1 3U 3 U H9EU E19EU 2002082300039 20020823 00039 EU 2002 8 23 HCM2002F00002 1 20020718 A 2434 RMR54302410 RELAY SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE MASTER ELEC BOX FAILED E HCMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 197BH 2666 WHILE ON ROUTINE SIGHTSEEING TRIP, THE PILOT EXPERIENCED A FLICKERING GENERATOR FAILURE WARNING LIGHT WHILE TAKING OFF F ROM THE AIRPORT. CONTINUED FLIGHT UNTIL RECEIVED A STEADY GENERATOR FAILURE WARNING LIGHT. RETURN TOT AIRPORT. UPON I NSPECTION BY MAINTENANCE PERSONNEL IT WAS DETERMINED THAT THERE WAS A FAILURE OF THE REX-K1 GENERATION EXCITATION RELAY LOCATED IN THE MASTER ELECTRICAL BOX. THE RELAY AND THE BATTERY WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO RECOMMENDATIONS TO PREVENT RECURRENCE OF THIS RELAY FAILURE. 1 G 7 1 3U 3 U H9EU E19EU 2002082300040 20020823 00040 2002 8 23 KBMA119505 4 20020814 A 3422 5050031904 GYRO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT FAILED E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 313LV 1683 3296 DIRECTIONAL GYRO LOOSES POWER AFTER ABOUT 30 MINUTES. REPLACE WITH OVERHAUL UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2002082300041 20020823 00041 EU 2002 8 23 KBMA119510 1 20020730 A 2110 590008 COMPRESSOR SNIAS 350 AS350BA 8680817 EU AIR CONDITIONER INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 270SH 6226 1864 AIR CONDITIONER, INOPERATIVE. REPLACED WITH NEW COMPRESSOR. 1 G 7 1 3U NC H9EU 2002082300042 20020823 00042 EU 2002 8 23 KBMA119511 1 20020730 A 2497 350A31185100 STRAP SNIAS 350 AS350BA 8680817 EU GROUND BRAID BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 10946 2300 BONDING BRAID WAS BROKEN. REPLACED WITH NEW BRAID. 1 G 7 1 3U NC H9EU 2002082300043 20020823 00043 2002 8 23 KBMA119514 4 20020814 A 3120 AT420000 CLOCK SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 350SH 6230 2957 NO DISPLAY ON CLOCK. REPLACED WITH NEW CLOCK. 1 G 7 1 3U 3 U NC H9EU E19EU 2002082300046 20020823 00046 EU 2002 8 23 KBMA119537 1 20020809 A 6510 350A2310534451 BRACKET SNIAS 350 AS350BA 8680817 EU T/R DRIVE SHAFT CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 1188P 11702 2347 TAIL ROTOR DRIVE SHAFT BRACKET IS CRACKED. REPLACED WITH NEW BRACKET. 1 G 7 1 3U NC H9EU 2002082300047 20020823 00047 EU 2002 8 23 KBMA119538 1 20020811 A 2150 350A6011 MOTOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE AIR CONDITIONER INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 313LV 1665 3296 AIR CONDITIONER BLOWS HOT AIR. REPLACED CONDENSOR MOTOR WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2002082300048 20020823 00048 EU 2002 8 23 KBMA119540 1 20020812 A 2912 806966 FILTER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE HYD SYSTEM CLOGGED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 792 3141 HYDRAULIC FILTER IS CLOGGING. REMOVED AND REPLACED WITH NEW FILTER. 1 G 7 1 3U 3 U H9EU E19EU 2002082300049 20020823 00049 EU 2002 8 23 KBMA119543 1 20020813 A 3340 SWITCH SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE ANTI COLLISION INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 350SH 6224 2957 ANTI COLLISION LIGHT INOPERATIVE. REPLACED WITH NEW SWITCH. 1 G 7 1 3U 3 U NC H9EU E19EU 2002082300050 20020823 00050 EU 2002 8 23 KBMA119544 1 20020813 A 6730 AC67244 SERVO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE SERVO SYS BINDING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3865 3141 SERVO CONTROLS BINDING WHEN INPUTS TO THE LEFT ARE REQUIRED. REPLACED WITH OVERHAUL UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2002082300051 20020823 00051 NM 2002 8 23 SWAA021892 1 20020819 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 731SA 27863 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED THOUGHT OUT CABIN. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002082300052 20020823 00052 NM 2002 8 23 SWAA021893 1 20020820 A 3350 311500 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW NR 13 DEF. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002082300053 20020823 00053 NM 2002 8 23 SWAA021897 1 20020817 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED 1/2D CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT T/E OTBD END. REPAIRED NR 5 L/E SLAT PER SRM. 2 L 7 2 4F RT A16WE 2002082300054 20020823 00054 NM 2002 8 23 SWAA021898 1 20020817 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, LBL 11. REMOVED AND REPLACED FLOORBEAM SECTION PER S RM. 2 L 7 2 4F RT A16WE 2002082300055 20020823 00055 NM 2002 8 23 SWAA021899 1 20020820 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD CRACKED AT BS 178, WL 188 AND RBL 1.0. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2002082300056 20020823 00056 NM 2002 8 23 SWAA021900 1 20020820 A 5753 6546435274 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 ON WALK AROUND INSPECTION, FOUND RT WING OTBD T/E FLAP DELAMINATED ON LOWER SIDE. REMOVED AND REPLACED RT OTBD T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002082300057 20020823 00057 NM 2002 8 23 SWAA021903 1 20020820 A 5754 65C26687 SLAT BOEING 737 737317 138447P NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED C2 CHECK, FOUND NR 1 L/E SLAT CRACKED AT INBD MAIN TRACK CUTOUT ON T/E ROW OF RIVETS. REPAIRED SLAT PE R SRM. 2 L 7 2 4F RT A16WE 2002082300058 20020823 00058 NM 2002 8 23 SWAA021884 1 20020819 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 718SW 27852 EEPLS LENS MISSING AT ROW NR 11. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002082300059 20020823 00059 NM 2002 8 23 SWAA021885 1 20020819 A 5523 65C25798 HINGE FITTING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 29 321SW 23342 AIRFRAME VIBRATION FELT ABOVE 280 KNOTS. REMOVED AND REPLACED LEFT INBD ELEVATOR TAB HINGE FITTING PER MM. 2 L 7 2 4F RT A16WE 2002082300060 20020823 00060 NM 2002 8 23 SWAA021887 1 20020818 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, ABOVE STR 14R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002082300061 20020823 00061 NM 2002 8 23 SWAA021888 1 20020818 A 5753 6546435278 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED C2 CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED OTBD T/E AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2002082300062 20020823 00062 NM 2002 8 23 SWAA021889 1 20020818 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 484, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002082300063 20020823 00063 NM 2002 8 23 SWAA021891 1 20020818 A 5330 6545768 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 102SW 23108 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 340, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F A16WE 2002082300065 20020823 00065 NM 2002 8 23 02FDEA00556 1 20020808 A 2612 WARNING SYSTEM BOEING 727 727200 138407E NM COCKPIT FALSE ACTIVATION A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 149FE 19087 ON T/O ROLL, FIRE BELL SOUNDED WITH NO OTHER FIRE INDICATIONS. BELL WOULD NOT SILENCE WITH APU BELL CUTOUT BUTTON, BELL SILENCED WITH GLARESHIELD BELL SHUTOFF BUTTON, ABORTED AT 110 KTS. PERFORMED FIRE TEST ON BOTH LOOPS & APU ALL NORMAL NO ABNORMAL ENGINE INDICATIONS NOTED. PERFORMED TEST OF APU, ENGINE, WHEEL WELL, CARGO DETECTION FOR BELLS IAW MM 26-11 -000-1, 26-11-000-5 26-11-000-0. NO DEFECTS NOTED. VISUALLY CHECKED MAIN AND NOSE WHEEL HEAT DETECTORS OK, RAN ALL THR EE ENGINES AT TAKEOFF, MAX POWER, FLT IDLE AND VARIOUS OTHER SETTINGS FOR LONG PERIODS OF TIMES ALL INDICATIONS NORMAL. PRECAUTIONARY REMOVED AND REPLACED FIRE DET DETECTOR MODULE, OPS CK GOOD IAW MM 26-11-000-5. A/C RELEASED FOR SERVICE. 2 L 7 3 4F RT A3WE 2002082300066 20020823 00066 NM 2002 8 23 02FDEA00558 1 20020806 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 NUMEROUS NICKS IN LWR EXTERNAL FUSELAGE SKIN BETWEEN BS 368, STR 19L TO 20L. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 1. 2 L 7 3 4F RT A3WE 2002082300067 20020823 00067 NM 2002 8 23 02FDEA00559 1 20020806 A 5320 STRINGER CLIP BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19717 CRACKED STR CLIP BS 1070, STR 7R. 2 L 7 3 4F RT A3WE 2002082300068 20020823 00068 NM 2002 8 23 02FDEA00560 1 20020806 A 5320 STRINGER CLIP BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CRACKED STR CLIP AT BS 1050, STR 6 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002082300069 20020823 00069 NM 2002 8 23 02FDEA00561 1 20020812 A 5320 STRINGER CLIP BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 STRINGER CLIP CRACKED AT BS 1050, STR 8 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2. 2 L 7 3 4F A3WE 2002082300070 20020823 00070 NM 2002 8 23 02FDEA00562 1 20020806 A 5320 STRINGER CLIP BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CRACKED STRINGER CLIP AT BS 1030, STR 4 RT. 2 L 7 3 4F RT A3WE 2002082300071 20020823 00071 NM 2002 8 23 02FDEA00563 1 20020806 A 5320 STRINGER CLIP BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CRACKED STRINGER CLIP AT BS 1030, STR 8 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2. 2 L 7 3 4F A3WE 2002082300072 20020823 00072 NM 2002 8 23 02FDEA00564 1 20020806 A 5320 69144691 FITTING BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 STRINGER END FITTING CORRODED AT BS 740, STR 9L. REMOVED AND REPLACED FITTING PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002082300074 20020823 00074 NM 2002 8 23 02FDEA00566 1 20020806 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 SKIN IS CHAFED AT BS 475, 2 INCHES ABOVE STR 21R. REMOVED AND REPLACED SKIN PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 2002082300075 20020823 00075 NM 2002 8 23 02FDEA00568 1 20020804 A 5320 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CRACK STRINGER CLIP AT BS 700, STR 2 L. *S/D* REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002082300076 20020823 00076 NM 2002 8 23 02FDEA00570 1 20020802 A 5312 BULKHEAD BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CRACK ON WEB AT BS 178, RBL 10, WL 235. REMOVED AND REPLACED WEB PER SRM 53-10-9. 2 L 7 3 4F RT A3WE 2002082300077 20020823 00077 NM 2002 8 23 02FDEA00571 1 20020803 A 5320 STRINGER CLIP BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CRACKED STRINGER CLIP AT BS 1000, STR 9 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2, 51-30-5. 2 L 7 3 4F RT A3WE 2002082300078 20020823 00078 NM 2002 8 23 02FDEA00572 1 20020803 A 5320 STRINGER CLIP BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CRACKED STRINGER CLIP AT BS 1030, STR 9 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2, 51-30-5. 2 L 7 3 4F RT A3WE 2002082300079 20020823 00079 NM 2002 8 23 02FDEA00573 1 20020803 A 5320 STRINGER CLIP BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CRACKED STRINGER CLIP AT BS 1030, STR 7 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2, 51-30-5. 2 L 7 3 4F RT A3WE 2002082300080 20020823 00080 NM 2002 8 23 02FDEA00574 1 20020810 A 3020 DUCT DOUG MD11 MD11 3023602 NM NR 2 ENGINE FAILED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 25 623FE 48794 RECEIVED ENG 2-ICE OFF ALERT, CONSEQUENCE ENG 2A-ICE DUCT FAILED. SHUT DOWN NR 2 ENG IN FLIGHT. 2 L 7 3 4F RT A22WE 2002082300081 20020823 00081 EU 2002 8 23 02FDEA00575 1 20020812 A 3231 A254310012 UPLOCK AIRBUS 300 A300F4605R 3930327 EU NLG DOOR BROKEN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 659FE 817 817 757 NOSE LANDING GEAR UNSAFE INDICATIONS ON TAKEOFF. DECLARED EMERGENCY RETURN TO KMEM. FOUND THE RIGHT NLG DOOR UPLOCK HO OK BROKEN. REMOVED AND REPLACED NLG DOOR UPLOCK ASSY, LEAK CK C/W. OP CHECKS NORMAL. 2 L 7 2 4F RT A35EU 2002091200080 20020912 00080 NM 2002 9 12 02FDEA00577 1 20020810 A 5320 WEB BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CRACKED WEB BS 613 BETWEEN STR 1 & 2 LT. 2 L 7 3 4F RT A3WE 2002091200081 20020912 00081 NM 2002 9 12 02FDEA00578 1 20020810 A 5320 WEB BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CRACKED WEB BS 600 BETWEEN STR 1 & 2 LT. REMOVED AND REPLACED WEB PER SRM 51-30-2, 51- 30-5, 51-20-1. 2 L 7 3 4F RT A3WE 2002091200082 20020912 00082 NM 2002 9 12 02FDEA00579 1 20020810 A 5313 STRINGER BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 STRINGER 8R CRACKED AT BS 600. REMOVED AND REPLACED STRINGER PER SRM 53-10-01, 51-40-4. 2 L 7 3 4F RT A3WE 2002091200083 20020912 00083 NM 2002 9 12 02FDEA00580 1 20020812 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 208FE 22930 DENT IN SKIN AT BS 1072, RBL 60, WL 200. REMOVED AND REPLACED SKIN PER SRM 53-30-1. 2 L 7 3 4F RT A3WE 2002082300082 20020823 00082 NM 2002 8 23 02FDEA00581 1 20020810 A 2613 355944255 LOOP BOEING 727 727200 138407E NM OVERHEAT SYS OUT OF POSITION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 282FE 22349 LOWER AFT BODY HEAT WARNING LIGHT CAME ON IN CLIMB. RAN LOWER AFT HEAT CHECKLIST. AFTER TURNING OFF NR 3 BLEED, LOWER AFT BODY HEAT LIGHT WENT OUT. TESTED SYSTEM, TEST OK. RETURNED TO MEM. FOUND ONE LOOP TOUCHING STRUCTURE. REPOSITION ED LOOP. RAN ENGINES AND OPS CHECKED SYSTEM. CHECKS OK. NO LEAKS NOTED. REPLACED LOOP M365 SECTION 48R. OPS AND LEA K CHECK OK. 2 L 7 3 4F RT A3WE 2002082300083 20020823 00083 NM 2002 8 23 02FDEA00582 1 20020813 A 2780 SWITCH BOEING 727 727200 138407E NM COCKPIT FAULTY A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 25 241FE 20979 DURING INITIAL TAKEOFF, AS FLAPS WERE BROUGHT FROM 5' TO 2' THE L/E FLAP INDICATOR REMAINED AMBER (DID NOT SHOW GREEN). L/E FLAPS POSITION TEST ON S/O PANEL INDICATED 2, 3, 5, 6 & 7 STILL EXTENDED (IN GREEN). QRH (RED TABS) PROCEDURE ACCO MPLISHED. UNEVENTFUL LANDING BACK AT SAN. PILOTS REPORTED NO ABNORMAL ROLLING TENDENCIES DURING ENTIRE FLIGHT. CYCLED L/E TEST SWITCH S1010. NR 5 SLAT INDICATION, OPS CHECKS OK. RAN L/E DEVICES SEVERAL TIMES. ALL CHECKS OK PER M/M 27- 82-011-4. 2 L 7 3 4F RT A3WE 2002082300085 20020823 00085 EU 2002 8 23 02FDEA00583 1 20020813 A 5310 TORQUE BOX AIRBUS 310 A310 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 CORROSION AROUND FASTENER HEADS IN AVIONICS COMPT NOSE GEAR WHEEL WELL TOP TORQUE BOX (FROM FRAME 13 TO 15A). 2 L 7 2 4F RT A35EU 2002082300086 20020823 00086 NM 2002 8 23 02FDEA00584 1 20020814 A 3260 694710566 MODULE BOEING 727 727200 138407E NM COCKPIT DEFECTIVE A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 478FE 21395 NOSE GEAR LIGHT (GREEN) DID NOT ILLUMINATE WITH GEAR HANDLE DOWN. PUSHED PRESS TO TEST GREEN LIGHT ILLUMINATED. MANUAL LY EXTENDED THE GEAR. CHECKED ALIGNMENT STRIPE ON NOSE, INDICATED DOWN AND LOCKED BUT STILL NO GREEN LIGHT. REPUSHED P RESS TO TEST AND GREEN LIGHT REMAINED ILLUMINATED AFTER RELEASE BUT NO SPRING TENSION ON NOSE GEAR LIGHT. FOUND THE NOS E GEAR GREEN LIGHT ASSY BAD; PRESS TO TEST FEELS SOLID (NO SPRING TENSION) AS COMPARED TO OTHERS AND FX 727-200 M/M 33-1 0-051-2. REMOVED AND REPLACED THE LANDING GEAR CONTROL PANEL MODULE IAW FX 727-200 M/M 25-10-052-4. LIGHT PRESS TO TE ST OPERATES NORMAL. 2 L 7 3 4F RT A3WE 2002082300088 20020823 00088 NM 2002 8 23 02FDEA00585 1 20020812 A 5314 KEELBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 208FE 22930 CORROSION (C53-113-01) ON KEELBEAM FLANGE AT BS 950B - 950B+11, LBL 7, WL 149. REMOVED AND REPLACED KEELBEAM FLANGE PER DWG 27-53-023. 2 L 7 3 4F RT A3WE 2002091200084 20020912 00084 NM 2002 9 12 02FDEA00586 1 20020813 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 EXTERNAL SKIN CHAFED AT STR 19 LT, BS 720D+13. 2 L 7 3 4F RT A3WE 2002082300091 20020823 00091 NM 2002 8 23 02FDEA00587 1 20020811 A 3242 211473 BRAKE ASSY BOEING 727 727200 138407E NM MLG FIRE A FDEA K NONE A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 462FE 4219 704 22550 FIRE IN RIGHT MAIN LANDING GEAR BRAKE AFTER SHUTDOWN CLEARED TO LAND ON 19R AT ICT. WINDS 020/8. TOOK LONGER THEN NORM AL TO SLOW DOWN TO TAXI SPEED. EVERYTHING ELSE WAS OTHERWISE NORMAL. FIRE STARTED AFTER BLOCK IN. FIRE WAS AT NR 3 BR AKE ASSEMBLY. INSPECTED RIGHT MAIN GEAR ASSEMBLY PER M/M 05-51- 121-2 AND REMOVED & REPLACED NR 3 BRAKE AND TIRE PER M/ M 32-41-032-4 & 32-45-001-4. NO DAMAGE WAS NOTED TO RIGHT GEAR STRUT ASSEMBLY. 2 L 7 3 4F RT A3WE 2002082300094 20020823 00094 WP 2002 8 23 02FDEA00588 1 20020813 A 5743 ARB0642501 FRAME DOUG DC10 DC1030 3023501 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 LEFT MAIN LANDING GEAR RETRACT CYLINDER SUPPORT FRAME IS CRACKED AT APEX LUG TO THE RADIUS AFT SIDE. REMOVED AND REPLAC ED SUPPORT BRACKET RETRACT ACTUATOR REF 8-5740-7-4312. 2 L 7 3 4F A22WE 2002082300095 20020823 00095 NM 2002 8 23 CA020808004 1 20020729 A 2421 700842A CSD BOEING 727 727171C 1384057 NM PWA JT8 JT8D7A 52053 NE NR 3 GENERATOR FAILED W E A H ENGINE SHUTDOWN UNSCHED LANDING DEACTIVATE SYST/CIRCUITS H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE NR 3 ENGINE GENERATOR TRIPPED - CSD OIL PRESSURE WAS LOW AND TEMP HIGH, DISCONNECT FAILED. ENGINE SH UTDOWN AS A PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT, YEG AIRPORT RESCUE WAS IN ATTENDANCE BUT NO ACTION WAS TAKEN OR REQUIRED. CSD WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002091200086 20020912 00086 NM 2002 9 12 02FDEA00590 1 20020811 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 208FE 22930 BULGE IN SKIN AT STR 28L, BS 1030. REMOVED AND REPLACED SKIN PER SRM 53-10-3 & 53-30-3, 53-30-1 FIG 2. 2 L 7 3 4F RT A3WE 2002082300096 20020823 00096 NM 2002 8 23 02FDEA00591 1 20020815 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 208FE 22930 SKIN GOUGED AT BS 720D+13, STR 10L. 2 L 7 3 4F RT A3WE 2002091100086 20020911 00086 NM 2002 9 11 F3LA200200235 1 20020820 A 5330 BEAR STRAP BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON BEAR STRAP AT BS 465-477, OUTBOARD OF STR 25-R. REPAIRED PER EA 53-7 37-177 AND SRM 53-30-03. 2 L 7 2 4F RT A16WE 2002091100087 20020911 00087 NM 2002 9 11 F3LA200200236 1 20020820 A 5320 FLOOR SUPPORT BOEING 737 737317 138447P NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CARGO FLOOR SUPPORT DAMAGED AT BS 460-540, LBL 10. REMOVED DAMAGED SECTION OF CAR GO FLOOR SUPPORT FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-00-53, 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002091100138 20020911 00138 NM 2002 9 11 F3LA200200237 1 20020820 A 5210 WEB BOEING 737 737317 138447P NM L1 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON L1 ENTRY DOOR WEB, BS 312 TO BS 351. REMOVED L1 DOOR WEB AND DOUBLER S, FABRICATED AND INSTALLED NEW WEB AND DOUBLERS PER SRM 51-30-05, 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002082300097 20020823 00097 NM 2002 8 23 02FDEA00593 1 20020816 A 3610 1843801 COOLER BOEING 727 727200 138407E NM BLEED AIR LEAKING A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 492FE 21530 ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. NO PACK TAKEOFF, ALL BLEED AIR SWITCHES CLOSED, 0 P SI MANIFOLD PRESSURE PRIOR TO TAKEOFF. LIGHT WENT OUT AS THRUST LEVERS RETARDED AND NR 1 BLEED AIR VALVE WAS OPENED. O VERHEAT SYSTEM TESTED GOOD. LIGHT REMAINED OUT FOR REMAINDER OF FLIGHT. ABNORMAL PROCEDURES COMPLETED. REMOVED AND RE PLACED NR 1 PRECOOLER IAW 36-11-051-4. LEAK AND OP CHECKS GOOD. 2 L 7 3 4F RT A3WE 2002082300098 20020823 00098 NM 2002 8 23 02FDEA00594 1 20020818 A 5320 BEAM BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 TWO HOLES WITH PILOT HOLES ADJACENT TO THEM AND 1 ELONGATED HOLE IN STUB BEAM WEB AT BS 783, WL 204-207, LBL 65. REMOVE D AND REPLACED STUB BEAM PER EA 7-5310-65851. 2 L 7 3 4F RT A3WE 2002091200028 20020912 00028 NM 2002 9 12 02FDEA00595 1 20020816 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 208FE 22930 COMPLY WITH EA 7-5330-65843 FUSELAGE SKIN REPAIR BS 304 & STR 22R/23R. COMPLIED WITH EA 7-5330-65843. 2 L 7 3 4F RT A3WE 2002091100139 20020911 00139 NM 2002 9 11 F3LA200200238 1 20020820 A 5320 STIFFENER BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED STIFFENER AT BS 328, LBL 28, CRACKED AT TOP HOLE OF FLOORBEAM. FABRICATED AND INS TALLED REPLACEMENT STIFFENER PER SRM 51-40-2. 2 L 7 2 4F RT A16WE 2002082300099 20020823 00099 NM 2002 8 23 02FDEA00599 1 20020820 A 2613 WARNING SYSTEM BOEING 727 727200 138407E NM COCKPIT FALSE ACTIVATION A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 268FE 21674 AT FL 280 DURING CLIMB THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. P ROCEDURE WAS ACCOMPLISHED. WHEN ENG NR 3 BLEED VALVE AND THE RIGHT PACK WERE CLOSED AND TURNED OFF, THE LIGHT WENT OUT IN 2 MINUTES. SYSTEM CHECKED OK. INSPECTED DUCTING FOR LEAKS. NONE FOUND AT THIS TIME. RAN ALL 3 ENGINES TO TAKEOFF POWER WITH PACKS ON FOR SEVERAL MINUTES. LOWER AFT BODY OVERHEAT LIGHT DID NOT COME ON. OVERHEAT DETECTION SYSTEM, OP S CKS NORMAL PER BMM 26-14-000-0. 2 L 7 3 4F RT A3WE 2002091200087 20020912 00087 NM 2002 9 12 02FDEA00600 1 20020821 A 5320 WEB BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CORROSION ON BOTTOM SIDE OF SHEAR WEB AT BS 1136, RBL 64, WL 208. 2 L 7 3 4F RT A3WE 2002082300100 20020823 00100 NM 2002 8 23 02FDEA00601 1 20020810 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 208FE 22930 CORROSION ON BS 344 FLOORBEAM TOP CHORD AT NUT PLATE LOCATIONS UPPER AND LWR FLANGES LBL 57 TO RBL 12, WL 208. R&R UPPE R CHORD ON FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 2002082300102 20020823 00102 SO 2002 8 23 SIMA200222107 1 20020805 A 5100 14521725001 SILL EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 734EK 145371 THIS IS LEVEL TWO FINDING ON CRIC NR 23854. LEFT SILL IN GALLEY AREA HAS CORROSION. C/A: INSTALLED SERVICEABLE SILL IA W SRM. 2 L 7 2 4F RT T00011AT 2002082300106 20020823 00106 EA 2002 8 23 COMA0260492 1 20020821 A 2410 IDG CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 01 436CA 7482 FLIGHT 5196 LEFT IDG CAUTION MESSAGE DURING T/O.DEFERRED MAINTENANCE PER MEL 2 L 7 2 4F RT A21EA 2002082300110 20020823 00110 NM 2002 8 23 BJNA020816 1 20020805 A 5315 FLOORBEAM BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 CORROSION AT 3 EACH SCREW HOLES ON BEAM AT BS 947.5 BETWEEN LBL 20 TO LBL 40. LEVEL 2 CORROSION SECTION OF FLOORBEAM. FABRICATED AND INSTALLED SECTION IAW SRM. 2 L 7 2 4F RT A16WE 2002082300113 20020823 00113 NM 2002 8 23 2002UALA01249 1 20020730 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 FORWARD CABIN FLOORBEAM UPPER T-CAP AT BODY STATION 365.25 RBL 09 TO RBL 60 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. RE PLACED T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082300114 20020823 00114 NM 2002 8 23 2002UALA01251 1 20020730 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 CABIN FLOOR CREASE BEAM I/B CHORD EXCESSIVE MATERIAL REMOVED FROM CORROSION, STATION 755 STRINGER 17L. MAJOR REPAIR ACC OMPLISHED. INSTALLED CREASE BEAM SPLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082300115 20020823 00115 NM 2002 8 23 2002UALA01252 1 20020730 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 FORWARD CABIN FLOOR INTERCOSTAL STATION 369 RBL 58 STRINGER 17R, HAS CORROSION AROUND FASTENER HOLE. MAJOR REPAIR ACCOM PLISHED. REPLACED WITH NEW INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082300116 20020823 00116 NM 2002 8 23 2002UALA01253 1 20020730 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 FORWARD CABIN FLOOR INTERCOSTAL STATION 368, RBL 10.5 UPPER SURFACE CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082300117 20020823 00117 NM 2002 8 23 2002UALA01254 1 20020730 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 FORWARD CABIN FLOORBEAM UPPER CAP CORRODED, STATION 324 RBL 42. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082300118 20020823 00118 NM 2002 8 23 2002UALA01258 1 20020731 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 AFT CABIN LEFT HAND SIDE FLOORBEAM UPPER SURFACE CORRODED AROUND NUT PLATE HOLES STATION 927 BETWEEN LBL 14 AND LBL 44. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED ANGLE DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082300119 20020823 00119 NM 2002 8 23 2002UALA01259 1 20020801 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 CABIN BODY FRAME INBOARD CHORD IS CRACKED BODY STATION 294, RBL 53, WL 209. MAJOR REPAIR ACCOMPLISHED. SPLICED FRAME I NBOARD CHORD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082300120 20020823 00120 WP 2002 8 23 DHL2002806840 1 20020712 A 5730 SKIN DOUG DC8 DC873F 302199F WP A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 46002 N/R:2477 LH WING UPPER SURFACE SHIN SHOWS CORROSION STRINGER 9 XRS396.000 ( MAJOR REPAIR)CORR: PERFORMED MAJOR REPAIR IA W SRM 57-2-1 SHEET 1.BLENDED OUT LH WING UPPER SKIN FOUND OUT OF LIMITS IAW SRM57-2-0 PG. 16 CUT CORRODED AREA IAW SRM 5 7-2-1 FIG. 32 CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED FILLER AND DOUBLER IAW SRM51-1-8B, APPLIED P RC SEALANT ON SLICE SURFACE IAW SRM 51-1-15 PG.1 , INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG. 32 AND SRM 51-1-2OD PG. 9 FOR LEAK CHECK SEE J/C 8-28-11-024 2 L 7 4 4F RT 4A25 2002082300121 20020823 00121 NM 2002 8 23 2002UALA01260 1 20020731 A 2751 INDICATOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE TE FLAPS FAILED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 903UA 25003 LANDED UNDER AMBER ALERT AFTER FLAPS WOULD NOT DEPLOY. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED THE FLAP POSITION INDICATOR 2 L 7 2 4F 4 F RT A16WE E2GL 2002082300122 20020823 00122 NM 2002 8 23 2002UALA01261 1 20020731 A 3260 CIRCUIT CARD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MLG FAILED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 336UA 24240 FLIGHT LANDED UNDER AMBER ALERT DUE TO NOSE GEAR SAFE LIGHT NOT ILLUMINATED AND UNSAFE LIGHT IS ILLUMINATED WITH GEAR HA NDLE DOWN. SUPPLEMENTAL DATA UPDATE NOSE LANDING GEAR M1214 GEAR DOWN SWITCH (CARD) FAILED. REPLACED THE NOSE GEAR DOWN SWITCH M1214 (LOGIC CARD). 2 L 7 2 4F 4 F RT A16WE E2GL 2002082300123 20020823 00123 NM 2002 8 23 BJNA020806 1 20020806 A 5311 FRAME BOEING 737 737282 13844AT NM RBL8, BS967 CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 CORROSION ON FRAME RBL 8 NEAR BEAM BS 967. REMOVED 18.8750 INCH SECTION, FABRICATED AND INSTALLED REPAIR SECTION OF FRA ME IAW SRM. 2 L 7 2 4F RT A16WE 2002082300124 20020823 00124 NM 2002 8 23 2002UALA01262 1 20020801 A 5512 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 942UA 26679 AIRCRAFT LEFT HAND HORIZONTAL STABILIZER LEADING EDGE AT OUTBOARD END IS DAMAGED. DENT IS APPROXIMATELY 5 INCHES FROM O UTBOARD END, STAB BL 240 TO BL 249. MAJOR REPAIR ACCOMPLISHED. LEADING EDGE PARTIAL SKIN REPLACEMENT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082300125 20020823 00125 EU 2002 8 23 2002UALA01263 1 20020731 A 2810 195F50603 DISK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CENTER TANK BURST A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 479UA 1538 RETURN TO FIELD WITH A FUEL IMBALANCE PROBLEM. OVER PRESSURE BURST DISC BETWEEN THE LEFT INNER WING FUEL TANK AND THE C ENTER FUEL TANK RUPTURED. FUEL TRANSFERRED FROM THE LEFT WING TO THE CENTER CAUSING AN IMBALANCE BETWEEN THE INNER WING TANKS. 2 L 7 2 4F 4 F RT A28NM E40NE 2002082300126 20020823 00126 NM 2002 8 23 2002UALA01264 1 20020731 A 2913 4205401 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 550UA 25398 LEFT ENGINE HYDRAULIC PUMP FAILED. TOWED TO THE GATE WITHOUT INCIDENT. REPLACED PUMP, CHANGED FILTERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082300127 20020823 00127 NM 2002 8 23 2002UALA01267 1 20020730 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EEL EXIT SIGN UNDER VIDEO MONITOR NEXT TO NUMBER 3 MAIN ENTRY DOOR ON LEFT HAND SIDE OF AIRCRAFT INOP. EXIT SIGN WIRING SHOWED OPEN WIRE IN EXIT SIGN ASSEMBLY. MAJOR REPAIR ACCOMPLISHED. REPLACED CONNECTOR ON EXIT SIGN ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2002082300128 20020823 00128 NM 2002 8 23 2002UALA01268 1 20020801 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 942UA 26679 STATION 178 BULKHEAD WEB CRACKED AT RIGHT HAND LOWER RADAR MOUNT INBOARD SIDE UPPER END. MAJOR REPAIR ACCOMPLISHED. RE PAIR DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082300129 20020823 00129 NM 2002 8 23 2002UALA01269 1 20020801 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 CABIN, STATION 294, FUSELAGE STUB FRAME CRACKED AT UPPER DOOR STOP FITTING, AT STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STUB FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082300130 20020823 00130 NM 2002 8 23 BJNA020815 1 20020805 A 5311 FRAME BOEING 737 737282 13844AT NM SCREW HOLE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 CORROSION UNDER 1 EACH SCREW HOLE AT FRAME BS 961 BETWEEN RBL 28-20 LEVEL 2 CORROSION. REMOVED CORRODED SECTION OF FRAM E, FABRICATED AND INSTALLED REPAIRED SECTION OF FRAME IAW SRM. 2 L 7 2 4F RT A16WE 2002082300131 20020823 00131 NM 2002 8 23 2002UALA01270 1 20020731 A 2120 SMOKE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DETECTED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 339UA 24243 CREW REPORTED ELECTRICAL SMELLING SMOKE FIRST SEEN AT CENTER AISLE DROP CEILING PANEL JUST FWD OF AFT GALLEY. OPERATED ALL EQUIPMENT, LIGHTS, LAV FLUSH ETC AND OBSERVED AREA DURING FERRY FLIGHT. NO ODOR OR VISIBLE SMOKE DETECTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700010 20021017 00010 NM 2002 10 17 2002UALA01271 1 20020801 A 2120 DUCT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 527UA 24995 LOUD BANGING NOISE FROM LEFT PACK, MAIN DISTRIBUTION DUCT CAME LOOSE FROM CEILING AND WAS HANGING DOWN 4-6 INCHES BETWEE N ROWS 9-11. FOUND OVERHEAD DISTRIBUTION DUCT SEALANT SPLIT AT ROW 8 THROUGH 10. FOUND MISSING FASTENERS USED TO SECUR E OVERHEAD DUCT TO CENTER OVERHEAD SLOT. REPLACED AIR DUCT AT ROW 8-10 PER MM21-23-01. CLEANED AIR NOZZLES AND RESTRIC TOR PLATES AND INSTALLED. OPS CHECKD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082300132 20020823 00132 NM 2002 8 23 DL764020787 1 20020710 A 2752 256T63102 ACTUATOR BOEING 767 767432ER 1385134 NM T/E FLAP TRIPPED A DALA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 SO 27 830MH 29701 T/E FLAP DISAGREE MSG ON T/O FROM LAX. DUE TO LIMITED FLAPS 20 LANDING AND SHORT RUNWAY IN OGG, DIVERTED TO HNL. FOUND NR 6 FLAP ROTARY ACTUATOR TRIPPED. RESET SAME FLAPS/SLATS, OPS NORMAL. 2 L 7 2 4F RT A1NM 2002082300133 20020823 00133 NM 2002 8 23 DL764020821 1 20020716 A 2752 256T63102 ACTUATOR BOEING 767 767432ER 1385134 NM T/E FLAP TRIPPED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 839MH 29712 AFTER DEPARTING HNL, FLAPS LOCKED AT 6 DEGS AND EICAS MSG T/E FLAP DISAGREE APPEARED. C/W QRH PROCEDURE AND RAISED FLAP S USING ALTERNATE MODE BUT FLAPS WOULD NOT COME UP BEYOND 2 DEGS. INITIATED AIR TURNBACK TO HNL. LANDED OVERWEIGHT, MT C IN PROGRESS. NO FAULTS ON FSEU. CHECKING OVER TORQUE TRIP INDICATORS. NO HISTORY. FOUND T/E FLAP ROTARY ACTUATORS 2 - 3 - 4 AND 6 OVER TORQUE IND TRIPPED. RESET SAME, ALL OPS NORMAL. 2 L 7 2 4F RT A1NM 2002082300134 20020823 00134 NM 2002 8 23 DL764020830 1 20020718 A 2752 356T63102 ACTUATOR BOEING 767 767432ER 1385134 NM T/E FLAP TRIPPED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 838MH 29711 ON DEPARTURE, T/E FLAPS DISAGREE LIGHT CAME ON WHEN RETRACTING FLAPS FROM 15 DEG TO 5 DEG. RETRACTED FLAPS USING ALT FL APS PER PROCEDURE. EXT FLAPS USING ALT MEANS PER PROCEDURE. DIVERTED TO TPA FOR MTC ACTION. TPA MTC-RAN FLAPS USING N ORMAL POWER. FOUND NR 3 ROTARY ACT TRIPPED. RESET SAME AND RAN FLAPS SEVERAL TIMES. NO FURTHER DEFECTS NOTED. BITE O F FSEU SHOWS NO CURRENT FAULTS. 2 L 7 2 4F RT A1NM 2002082300135 20020823 00135 NM 2002 8 23 DL767020849 1 20020720 A 3150 285T025919 MODULE BOEING 767 767232 1385132 NM E/E BAY FAULTY A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 105DA 22217 ABORTED TAKEOFF IN BOS FOR SPOILERS WARNING. RECYCLED SPEED BRAKE HANDLE PER BOS MTC. THROTTLED UP ON TAXIWAY WITH NO WARNING LIGHT. ATTEMPTED ANOTHER TAKEOFF. ABORTED FOR SPOILERS AGAIN. BOTH ABORTS LESS THAN 15 KNOTS. T/S PER FIM 31 -51-00 FIG 108. REPLACED T/O CONFIG WARNING MODULE. PERFORMED CONFIG T/O TEST. CHECKS OK PER M/M. 2 L 7 2 4F RT A1NM 2002082300136 20020823 00136 NM 2002 8 23 DL76G020786 1 20020710 A 2120 ODOR BOEING 767 767332 1382001 NM CABIN DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1604R 30180 FLIGHT ATTENDANTS REPORTED SMELLING BURNING RUBBER IN THE AREA OF ROW 27 WHILE AT CRUISE ALTITUDE. NO SMOKE WAS VISIBL E. LEFT AND RIGHT RECIRC FANS WERE TURNED OFF AND THE SMELL DISAPPEARED. INSPECTED FLOOR DUCTING AND CEILING IN AREA O F ROW 27. INSPECTED RECIR FANS AND FILTERS IN CARGO COMP. RECIR FANS AND AIRFLOW NORMAL. NO ODORS PRESENT. 2 L 7 2 4F RT A1NM 2002082300137 20020823 00137 WP 2002 8 23 DHL2002806844 1 20020706 A 5712 FORMER DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 81567 46002 N/R: 1696 RH WING OUTBD L/E UPPER PART FORMER CRACKED .250 XFS647.500CORR: STOP DRILLED CRACK IAW SRM 57-2-0 PG. 9-10 FA BRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B INSTALLED REINFORCING ANGLE IAW SRM57-2-0 PG. 9-10 , SRM 51-1-21 PG. 1 2 L 7 4 4F RT 4A25 2002082300138 20020823 00138 NE 2002 8 23 DL76G020791 2 20020712 A 7320 441789 HYDROMECH UNIT BOEING 767 767332 1382001 NM GE CF6 CF680 30025 NE NR 1 ENGINE MALFUNCTIONED A DALA E ENGINE SHUTDOWN M OVER TEMP CL CLIMB 1 SO 27 1605 30198 051899 NR 1 ENG IFSD ON CLIMB APPROX 8,000 FT. NR 1 ENGINE HAD N1 OVERSPEED AND EGT EXCEED. PERFORMED OVERSPEED AND OVERTEMP INSPECTION AND FOUND OK. REPLACED HMU. PERFORMED EEC TEST AND HIGH POWER RUN-UP AND ALL OK. ENGINE TO BE REPLACED WIT HIN 10 FLT CYCLES DUE N1 WENT TO 117.6. 2 L 7 2 4F 4 F RT A1NM E13NE 2002082300139 20020823 00139 WP 2002 8 23 AALA20020995 1 20020711 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 473AA 49648 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS BETWEEN ROWS 7 AND 11 INOPERATIVE. REPLACED EMERGENCY EXIT LI GHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300140 20020823 00140 WP 2002 8 23 AALA20020999 1 20020711 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 560AA 53090 PHL - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPAIRED WIRES ON BATTERY SUPPLY UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300141 20020823 00141 WP 2002 8 23 AALA20021000 1 20020710 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 289AA 49301 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT C EILING LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300142 20020823 00142 WP 2002 8 23 AALA20021001 1 20020711 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 214AA 49162 DFW - DURING OVERNIGHT MAINTENANCE, TAILCONE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED TAIL CONE EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300143 20020823 00143 WP 2002 8 23 AALA20021005 1 20020711 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 516AM 49893 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ON SEAT 2EF INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT LIGH T SEAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300144 20020823 00144 WP 2002 8 23 AALA20021006 1 20020713 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33502 49739 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT STAIRWAY INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300145 20020823 00145 WP 2002 8 23 AALA20021007 1 20020712 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP COCKPIT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 475AA 49650 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD PANEL COCKPIT EMERGENCY EXIT LIGHTS INOPERATIVE. RESECURED EMERGENCY EXIT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300146 20020823 00146 WP 2002 8 23 AALA20021008 1 20020712 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 475AA 49650 DFW - DURING OVERNIGHT MAINTENANCE OVERHEAD PANEL 1L DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. RESECURED EMERGENCY EXIT B ATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300147 20020823 00147 WP 2002 8 23 AALA20021009 1 20020712 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 475AA 49650 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD PANEL 1R DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. RESECURED EMERGENCY EXIT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300148 20020823 00148 WP 2002 8 23 AALA20021010 1 20020713 A 3350 PIN DOUG DC9 DC982 3022082 WP CONNECTOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 516AM 49893 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 21D INOPERATIVE. RESECURED EMERGENCY EXIT PIN IN CANN ON PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300149 20020823 00149 WP 2002 8 23 AALA20021011 1 20020713 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 287AA 49299 DFW DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 21 DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300150 20020823 00150 WP 2002 8 23 AALA20021012 1 20020713 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 287AA 49299 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300151 20020823 00151 WP 2002 8 23 AALA20021013 1 20020712 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7527A 49919 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ABOVE FLIGHT ATTENDANT SEATS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300152 20020823 00152 NM 2002 8 23 AALA20021016 1 20020714 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AA 25200 MIA - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT AT 30H INOPERATIVE. REPINNED BROKEN EMERGEN CY ESCAPE PATH LIGHTING WIRES TO CONNECTOR AT SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082300153 20020823 00153 WP 2002 8 23 AALA20021017 1 20020715 A 3350 WIRE DOUG DC9 DC983 3022083 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 563AA 49345 DFW - DURING OVERNIGHT MAINTENANCE, AFT OVERHEAD EMERGENCY EXIT LIGHT BY L2 FLIGHT ATTENDANT SEAT INOPERATIVE. TIGHTENE D AFT OVERHEAD EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002082300154 20020823 00154 NM 2002 8 23 AALA20021018 1 20020713 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 DFW - DURING OVERNIGHT MAINTENANCE, FOUND SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEAT 38H INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEAT 38H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F RT A1NM 2002082300155 20020823 00155 NM 2002 8 23 AALA20021019 1 20020713 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 308AA 22314 LAX - DURING OVERNIGHT MAINTENANCE, FOUND MID GALLEY LEFT EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPAIRED WIRING F OR MID GALLEY LEFT EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082300156 20020823 00156 NM 2002 8 23 AALA20021020 1 20020713 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 DFW - DURING OVERNIGHT MAINTENANCE, FOUND SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEAT 28H INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SET 28H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082300157 20020823 00157 WP 2002 8 23 AALA20021022 1 20020716 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 216AA 49167 AUS - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY ESCAPE P ATH LIGHTING BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300158 20020823 00158 WP 2002 8 23 AALA20021023 1 20020716 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 442AA 49468 ORD - DURING OVERNIGHT MAINTENANCE, LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY LIGHTING INOPERATIVE. REPLACED EXTERIOR EMERGENCY LIGHTING BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082300159 20020823 00159 EA 2002 8 23 SWIA200211083 1 20020615 A 2710 CONTROL CABLE CNDAIR CL600 CL6002B19 1900309 EA AILERON CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 592SW 7279 RIGHT WING AILERON CABLES FROM THE TENSION REGULATOR INBOARD TO THE WHEEL WELL ARE CORRODED. RIGHT WING AILERON CABLES REPLACED IAW CRJ MM 27-00-00-960-802. 2 L 7 2 4F RT A21EA 2002082300160 20020823 00160 EA 2002 8 23 SWIA200211084 1 20020615 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 592SW 7279 FLOOR SUPPORT ANGLES AT FS 621 ON LEFT AND RIGHT SIDES ARE CRACKED. REPAIR CARRIED OUT IAW CRJ REO 601R-53-61-117, REV A. 2 L 7 2 4F RT A21EA 2002082300161 20020823 00161 SO 2002 8 23 SWIA200211085 1 20020705 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 582SW 120350 LEFT NACELLE OUTBOARD AND INBOARD FRAME NR 17 CRACKED. INSTALLED REPAIR DOUBLER ON FRAMES IAW EMB SRM 51-70-05 AND 51-4 0-02. 2 L 7 2 4T RT A31SO 2002082300162 20020823 00162 SO 2002 8 23 SWIA200211086 1 20020705 A 5320 1200444901 BEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 582SW 120350 EXCESSIVE CORROSION ON BEAM IN FRONT OF LAV BETWEEN FRAMES 38 AND 40. REMOVED AND REPLACED BEAM AND RIVETED IAW ASM 51- 40-02. 2 L 7 2 4T RT A31SO 2002082300163 20020823 00163 SO 2002 8 23 SWIA200211087 1 20020705 A 5310 DOOR FRAME EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 582SW 120350 FRAME 13 RIGHT SIDE CRACKED ON INSIDE AND OUTSIDE OF VERTICAL BRACE, AT COCKPIT DOOR OPENING. REMOVED AND REPLACED INSI DE L-BRACKET AND FABRICATED AND INSTALLED DOUBLER IAW SRM 51-70-05 AND 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 2002082300164 20020823 00164 SO 2002 8 23 SWIA200211089 1 20020719 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO CARGO DOOR OUT OF ADJUST A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 218SW 120287 FORWARD DOOR LIGHT WITH TRIPLE CHIME ON BEGINNING OF TAKEOFF ROLL. ABORTED TAKEOFF. ADJUSTED FORWARD DOOR MICROSWITCH. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002082300165 20020823 00165 EA 2002 8 23 SWIA200211090 1 20020725 A 2760 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA SPOILER SHORTED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 430SW 7523 I/B GND SPOILER CAUTION MESSAGE APPEARS DURING GROUND FFOD TESTS, ACCOMPANIED BY INTERMITTENT I/B GND SPOILER FAULT STAT US MESSAGE. REPLACED CANNON PLUG 2P6CN ON INBOARD SPOILERS MANIFOLD. PERFORMED OPS CHECK OF SPOILER SYSTEM PER MM 27-6 4-00 & 27-65-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002082300166 20020823 00166 SO 2002 8 23 SWIA200211091 1 20020714 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 291SW 120318 RIGHT SIDE LOWER FORWARD SEAT TRACK HAS CORROSION. REPLACED RIGHT SIDE LOWER FORWARD SEAT TRACK IAW 53-01-05. 2 L 7 2 4T RT A31SO 2002082300167 20020823 00167 SO 2002 8 23 SWIA200211092 1 20020714 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 291SW 120318 RIGHT NACELLE FRAME NR 1 CRACKED INBOARD & OUTBOARD OF TORSION BAR MOUNT POINTS. REPLACED RIGHT FRAME NR 1 IAW SB 120- 54-0036 AND SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002082300168 20020823 00168 NE 2002 8 23 SWIA200211093 2 20020730 A 7200 PW118B ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LEFT MALFUNCTIONED A SWIA E ENGINE SHUTDOWN R F PARTIAL RPM/PWR LOSS FLT CONT AFFECTED CR CRUISE 1 NM 07 393SW 5856 5856 120330 115098 WHILE EN ROUTE FROM SAN TO LAX, NR 1 ENGINE TORQUE BEGAN TO SURGE AND AIRCRAFT BEGAN TO YAW BACK AND FORTH. FOLLOWED QR H AND SELECT EEC MANUAL PER QRH. FOUR TO FIVE MINUTES LATER NR 1 ENGINE BEGAN TO SURGE AGAIN WITH WIDER PARAMETER SWING S. ELECTRONIC FUEL CONTROL FAILURE. CHECKLIST CALLED FOR ENGINE SHUTDOWN. SHUTDOWN & SECURED ENGINE PER THE QRH. DEC LARED AN EMERGENCY AND PROCEEDED TO LAX. REMOVED & REPLACED LEFT ENGINE ASSEMBLY IAW MM 71-00-00 & 61-10-03. 2 L 7 2 4T 4 T RT A31SO E20NE 2002082300169 20020823 00169 NM 2002 8 23 F3LA200200239 1 20020820 A 5320 STRINGER CLIP BOEING 737 737317 138447P NM BS 767 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED STRINGER CLIP AT BS 767, STR 6-L, CRACKED. FABRICATED AND INSTALLED REPLACEMENT S TRINGER CLIP PER SRM 51-30-02, SRM 57-40-02 AND BOEING DRAWING 69-35352. 2 L 7 2 4F RT A16WE 2002082300170 20020823 00170 NM 2002 8 23 02082201 1 20020819 A 5310 SKIN BOEING BOEING 757 757256 1384925 NM GOUGED A N8TA O OTHER O OTHER IN INSP/MAINT 1 WP 19 508NA 26244 Gouge in outer skin, STA. 755, STR. 15L. Cut out damaged area, installed fillers and doubler Per E.O. 02-0887. To be R einspected every 12000 Flight Cycles 2 L 7 2 4F RT A2NM 2002082300171 20020823 00171 2002 8 23 SWAA021905 4 20020820 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002082300172 20020823 00172 NM 2002 8 23 SWAA021906 1 20020817 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED 1/2D CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHT LENSES BROKEN. REMOVED AND REPLACE D LENSES PER MM. 2 L 7 2 4F RT A16WE 2002082300173 20020823 00173 2002 8 23 SWAA021908 4 20020821 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 092SW 22964 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F A16WE 2002082300174 20020823 00174 NM 2002 8 23 SWAA021910 1 20020820 A 5320 BAC1503 STIFFENER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663.75, LBL 6.15. REPAIRED STIFFENER PER SWA EA. 2 L 7 2 4F RT A16WE 2002082300175 20020823 00175 NM 2002 8 23 SWAA021911 1 20020821 A 5315 BAC1509 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 825, RBL 3. REPAIRED FLOORBEAM PER SRM AND SWA RA. 2 L 7 2 4F RT A16WE 2002082300176 20020823 00176 NM 2002 8 23 SWAA021912 1 20020820 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED C3 CHECK, FOUND LT HORIZ STAB CRACKED ON LOWER SKIN AT AFT SPAR, 6 FT FROM ROOT. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 2002082300177 20020823 00177 NM 2002 8 23 SWAA021914 1 20020821 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR FUSELAGE SKIN AND BEARSTRAP CRACKED AT BOTH UPPER AND LOWER DOOR HINGE CUT OUTS. REPAIRED SKIN AND BEARSTRAP PER SRM AND SWA EA. 2 L 7 2 4F RT A16WE 2002082300178 20020823 00178 NM 2002 8 23 CA020815003 1 20020807 A 2150 ACM DHAV DHC8 DHC8301 1386003 NM ACM BAY SEIZED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) PRIOR TO DECENT A STRONG ODOR WAS EMITTED FROM THE AIR-CONDITIONING SYSTEM. SHORTLY AFTERWARDS ONE OF THE FLIGHT ATTENDANTS ADVISED THE FLIGHT CREW THAT SMOKE WAS FILLING THE REAR CABIN AREA. THE AIRCRAFT WAS DIVERTED AND LANDED WIT HOUT FURTHER INCIDENT. ENGINEERING INVESTIGATION REVEALED THAT THE NR 1 AIR-CONDITIONING PACK ACM HAD FAILED WITH THE AC M TURBINE SEIZED. THE ODOR AND SMOKE IN THE CABIN WERE DUE TO LEAKAGE AND HEATING OF THE ACM LUBRICATING OIL DURING THE ACM FAILING AND PRIOR TO AIR-CONDITIONING PACK SHUTDOWN. THE ACM WAS CHANGED AND THE AIRCRAFT WAS RETURNED TO SERVICE WI THOUT FURTHER INCIDENT. 2 H 7 2 4T RT A13NM 2002082300179 20020823 00179 NM 2002 8 23 CA020815004 1 20020801 A 7930 APT761000100DW TRANSMITTER DHAV DHC8 DHC8301 1386003 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE OIL PRESSURE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE, ENGINE NR 2 OIL PRESSURE WAS OBSERVED TO BE DROPPING BELOW 45 PSI. ENGINE POWER WAS REDUCED AND THE PROPELLER FEATHERED. THE OIL PRESSURE CONTINUED TO DROP BELOW 40 PSI AND THE ENGINE WAS SHUTDOWN AS A PRECAUTION. NO OI L PRESSURE WARNING WAS ILLUMINATED DURING THE EVENT UNTIL THE ENGINE WAS SHUTDOWN. AIRCRAFT LANDED WITHOUT FURTHER INC IDENT. INVESTIGATION BY MAINTENANCE REVEALED THAT THE NR 2 ENGINE OIL PRESSURE TRANSMITTER WAS DEFECTIVE. THE OIL PRESS URE TRANSMITTER WAS REPLACED, AND AN OPERATIONAL CHECKOUT OF THE ENGINE WAS PERFORMED SATISFACTORILY. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002082300180 20020823 00180 NE 2002 8 23 CA020815005 2 20020808 A 7421 9550168760 IGNITER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE UNSERVICEABLE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A 100 HR INSPECTION AN IGNITOR WAS FOUND UNSERVICEABLE. UPON REMOVAL IT WAS NOTICED THAT THE CENTER ELECTRO DE WAS ERODED BEYOND LIMITS. IT WAS ALSO NOTED THAT THE CERAMIC ISOLATOR / INSULATOR WAS LOOSE RESULTING IN THE CERAMIC ISOLATOR FALLING INTO THE COMBUSTION CHAMBER. 1 G 7 1 3U 3 U NC H9EU E19EU 2002082300181 20020823 00181 NE 2002 8 23 CA020815006 2 20020812 A 7200 ENGINE BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE NR 1 MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING DEPARTURE, NR 1 ENGINE CHIP INDICATION LIGHT ILLUMINATED, PILOT PULSED SYSTEM, LIGHT EXTINGUISHED. A/C LA NDED LOAD PASSENGERS AND CONTINUE MISSION, DURING SECOND DEPARTURE NR 1 ENGINE CHIP INDICATION LIGHT ILLUMINATED, PILOT PULSED SYSTEM AND LIGHT EXTINGUISHED. WHILE IN CRUISE NR 1 ENGINE CHIP INDICATION LIGHT ILLUMINATED, PILOT PULSED SYST EM, LIGHT EXTINGUISHED, A/C RETURNED TO BASE. NR 1 ENGINE SCAVENGE FILTER CHIP DETECTOR INSPECTED. LIGHT FERROUS CHIPS FOUND. SCAVENGE OIL FILTER INSPECTED AND OIL SCREENED AND INSPECTED, NO MATERIAL FOUND. NR 1 ENGINE REMOVED AND SENT FOR REPAIR. 1 G 7 2 3U 3 U NC H13EU E5NE10 2002082300182 20020823 00182 NM 2002 8 23 UPS02239119 1 20020814 A 5310 WEB BOEING 727 72731C 1384011 NM BS 1243 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C LIGHTENING HOLE IN AFT AIRSTAIR TORQUE BOX AT BS 1243 RHS IS CRACKED WEB REPAIR CARRIED OUT IAW SR M 51-10-4 2 L 7 3 4F A3WE 2002082300183 20020823 00183 NM 2002 8 23 UPS02239121 1 20020812 A 5310 INTERCOSTAL BOEING 727 72731C 1384011 NM BS 1130 BBL6R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C CRACK ON INTERCOSTAL AT BS 1130 BBL 6 R INTERCOSTAL REMOVED IAW SRM 51-30-02 INTERCOSTAL FABRICATE D IAW SRM 51-20-1 FIG 7 AND INSTALLED IAW SRM 51-30-2 2 L 7 3 4F A3WE 2002082300184 20020823 00184 NM 2002 8 23 SABA020085 1 20020821 A 3350 6104789 BATTERY DHAV DHC8 DHC8103 1386005 NM A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 801WP 086 AIRCRAFT 801 ON FLIGHT 5098 FROM CLT to LEX : During preflight the aircrew could not get the aft ceiling interior and ex terior emergency lights to test. Maintenance removed and replaced the battery packs and resequred a loose connection at the Power Supply. System ops checked good and aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002082300185 20020823 00185 2002 8 23 CA020816001 4 20020810 A 3418 0861CAG SENSOR LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE ANGLE OF ATTACK MISSING W O OTHER D J INFLIGHT SEPARATION WARNING INDICATION CR CRUISE 1 CA (CAN) LEFT ALPHA AIR DATA SENSOR HEAT OFF LEGEND CAME ON IN FLIGHT. ON ARRIVAL IT WAS FOUND THAT THE AOA VANE WAS MISSIN G. AN INSPECTION OF THE WING AND STABILIZERS WAS C/O, NO DAMAGED WAS FOUND. THE AOA SENSOR WAS REPLACED, AND TESTED SERV ICEABLE. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 2002082300186 20020823 00186 NE 2002 8 23 CA020816002 2 20020707 A 7250 MODULE51 BLADE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE ENGINE FAILED W D RETURN TO BLOCK E J VIBRATION/BUFFET WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) PHYSICAL VIBRATION REPORTED AT 35 PERCENT N1, 70 PERCENT N2, AND FELT IN THE COCKPIT. GATE RETURN TRIM BALANCE R EDUCED N1 EMV FROM 2.2 TO 1.2 BUT DID NOT FIX COCKPIT VIBRATION. MCD FOUND CLEAN. BOROSCOPE INSPECTION REVEAL LP 1 TUR BINE BLADE FAILURE. ENGINE AT RRC FOR REPAIR, FAILED BLADE WILL BE RETURNED TO RRD FOR INVESTIGATION. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002082300187 20020823 00187 WP 2002 8 23 CA020816003 1 20020812 A 5230 1613510103 FAIRING LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE CARGO DOOR MISSING W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON ARRIVAL, THE CREW NOTICED THAT THE C2 CARGO DOOR FAIRING ASSY. WAS MISSING. FURTHER INVESTIGATION REVEALED T HAT C2 CARGO PANEL ASSY DOOR FAIRING , TOP AFT FAIRING CUT OUT PANEL CRACKED 1 INCH LONG AND PART OF AFT LIP IS MISSING . MAINTENANCE REPLACED THE MISSING PANEL IAW AMM 53-52-00 AND REPAIRED THE PANEL ASSY. IAW SRM 51-50-07. 2 L 7 3 4F 4 F A23WE E12EU 2002082300188 20020823 00188 EU 2002 8 23 CA020816006 1 20020816 A 3340 MS16562234 STOP PIN HUGHES 030040 BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE LIGHT GIMBLE MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 040000011 (CAN) PILOT DOING DAILY INSPECTION NOTICED SX5 TURNED BEYOND 90 DEGREE LEFT POSITION WHERE NORMAL STOP OCCURS. FURTHER V ISUAL INSPECTION REVEALED ROLL PIN MISSING THEREFORE NOTHING TO MECHANICALLY STOP THE 360 DEGREE ROTATION OF SEARCHLIGHT . PIN REPLACED,LIGHT TESTED AND RETURNED TO SERVICE. 1 G 7 2 3U 3 U NC H13EU E5NE10 2002082300189 20020823 00189 EA 2002 8 23 CA020819001 1 20020706 A 7500 32895902 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE FAILED W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 CA 19755 (CAN) RIGHT 14TH STAGE DUCT WARNING MESSAGE APPEARED DURING FLIGHT. QRH PROCEDURE APPLIED AND RETURNED TO DEPARTURE AIRP ORT. RIGHT 14TH STAGE SOV REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002082300190 20020823 00190 EA 2002 8 23 CA020819002 1 20020812 A 5610 601R330331 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13071 (CAN) LT WINDSHIELD CRACKED. REPLACED LT WINDSHIELD IAW 56-11-01. 2 L 7 2 4F RT A21EA 2002082300191 20020823 00191 EA 2002 8 23 CA020819003 1 20020731 A 5610 601R3303312 WINDOW CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) IN FLIGHT, THE RT SIDE WINDOW CRACKED. WINDOW WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002082300192 20020823 00192 EA 2002 8 23 CA020819004 1 20020725 A 5610 601R3303312 WINDOW CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA (CAN) IN FLIGHT, THE RT SIDE WINDOW CRACKED. WINDOW WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002082300193 20020823 00193 SO 2002 8 23 CA020820003 1 20020724 A 2435 SHAFT PIPER PA46 PA46500TP 7104622 SO STARTER GEN CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LIGHT SURFACE CORROSION FOUND ON STARTER-GEN SHAFT AT ITS BASE, BETWEEN SPLINE O-RING AND BASE. MOST PROBABLE CAU SE OF CORROSION IS WATER INGRESSION DUE TO IMPROPER SEALING SURFACES NEAR COOLING AIR EXHAUST OF STARTER/GEN. SHAFT APP EARS TO BE MADE OF STRAIGHT CARBON STEEL WITH NO COATING. 1 L 7 1 3O RT A25SO 2002082300195 20020823 00195 NM 2002 8 23 CA020820005 1 20020819 A 5270 BULB BOEING 727 727231 1384079 NM PWA JT8 JT8D9A 52048 NE DOOR INDICATOR BURNED OUT W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) AFTER TAKE OFF, A/C FAILED TO PRESSURIZE. A RUMBLING SOUND WAS HEARD FROM BENEATH COCKPIT FLOOR. FUEL DUMP OF 400 0 LBS CARRIED OUT AND RETURNED FOR NORMAL LANDING. E/E BAY DOOR WAS NOT LATCHED PROPERLY & COCKPIT INDICATOR LIGHTS WER E UNSERVICEABLE. VERBAL FROM F/E, DOOR SECURED / LATCHED PROPERLY, LIGHT BULBS REPLACED, WARNING SYSTEM TEST NORMAL 2 L 7 3 4F 4 F A3WE E2EA 2002082300196 20020823 00196 NM 2002 8 23 CA020820006 1 20020819 A 2150 A/C PACK BOEING 727 727231 1384079 NM PWA JT8 JT8D9A 52048 NE ACM BAY TRIPPED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) ON SECOND T/O, PRESSURISATION WAS LOST ON ROLL. RTO INITIATED AT 70KTS. RT PACK TRIPPED. A/C RE-CONFIGURED & NO RMAL T/O 7 FLIGHT CARRIED OUT. 2 L 7 3 4F 4 F A3WE E2EA 2002082300197 20020823 00197 GL 2002 8 23 CA020821003 3 20020814 A 6111 83272 CLAMP HARTZL HCB3R302E GRUMAV G21 G21A 3951204 SO PWA R985 R985* 52008 NE HARTZL HCB3R HCB3R302 GL PROP BLADE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 202N (CAN) DURING A SCHEDULED INSPECTION, THE NR 3 REAR BLADE CLAMP WAS FOUND TO HAVE A 2 INCH CRACK ACROSS IT. THE PROPELLE R WAS REMOVED AND SENT IN FOR OVERHAUL. 1 H 7 2 3R 3 R TC654 5E1 5 C P28EA 2002091100140 20020911 00140 NM 2002 9 11 F3LA200200240 1 20020820 A 5313 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON STR 21R UNDER FRAME AT BS 727. FABRICATED AND INSTALLED NEW STRINGER SECTION AND REPAIR SPLICES PER SRM 53-00-03, FIG 201 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002082300198 20020823 00198 NM 2002 8 23 AWXA200200795 1 20020812 A 5311 6545807530 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A 3/4" CRACK WAS FOUND ON THE R-1 DOOR FRAME AT INBOARD LOWER END, BS 300, RBL 55 . MAINTENANCE REMOVED DAMAGED SECTION OF R-1 DOOR LOWER FORWARD STUB BEAM FRAME AND FOUND SILL CLIP ALSO CRACKED. REMOVE D SILL CLIP, FABRICATED 2 EACH REPAIR ANGLES AND NEW SILL CLIP, AND INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-3, PG. 1-6, FIG. 1. 2 L 7 2 4F RT A16WE 2002082300199 20020823 00199 NM 2002 8 23 AWXA200200798 1 20020728 A 5320 65465347 SHEAR TIE BOEING 737 737277 1384570 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 0 0 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK CORROSION WAS FOUND ON BELT FRAME SUPPORT ANGLE (SHEAR TIE) IN FORWARD CARGO COMP ARTMENT, BS 520, BL 0. MAINTENANCE REMOVED BELT FRAME SUPPORT ANGLE BS 520, BL 0. FABRICATED A NEW BELT FRAME SUPPORT AN GLE, AND INSTALLED REPAIR IAW DWG 65-46534-7, AND B737-200 SRM 51-10-1, PG. 8. 2 L 7 2 4F RT A16WE 2002082300200 20020823 00200 EA 2002 8 23 SWIA200211139 1 20020820 A 3030 PITOT TUBE CNDAIR CL600 CL6002B19 1900309 EA #2 MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 588SW 7069 AMBER CAUTION MESSAGE FOR PITOT BASE HEAT ILLUMINATED @ 10,000. RETURNED TO SLC. REMOVED AND REPLACED #2 PITOT TUBE IA W CRJ MM 34-11-01. PERFORMED OPS CHEAK & LEAK CHECK IAW 34-11-00. OPS CHECKS GOOD. PN 667-0658 SN 201354. 2 L 7 2 4F RT A21EA 2002082600018 20020826 00018 NM 2002 8 26 0202682287 1 20020820 A 3350 M9015 POWER SUPPLY BOEING 727 727251 138408H NM AFT CABIN A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 287US 21375 AFT CABIN SECTIO OF EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 2002082600019 20020826 00019 NM 2002 8 26 02FDEA00550 1 20020805 A 5753 BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING LWR MOUNTING SIDE, FOUND HINGE FITTING & WASHERS CORRODED AFTER SEALANT R EMOVAL. R&R BRACKET ASSY PER MM 57-53-01. 2 L 7 3 4F RT A22WE 2002082600020 20020826 00020 NM 2002 8 26 2002UALA01275 1 20020804 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 942UA 26679 STATION 986.5 CABIN FLOORBEAM HAS SMALL SPOT OF CORROSION TWO PLACES AT RBL 17 AND RBL 24. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLES. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082600021 20020826 00021 NM 2002 8 26 2002UALA01276 1 20020804 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 943UA 26680 BODY STATION 420 FUSELAGE FRAME INBOARD FLANGE DENTED AT STRINGER 25 LT. MAJOR REPAIR ACCOMPLISHED. REPLACED SPLICE PL ATE WHERE DENT WAS LOCATED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600054 20021126 00054 EU 2002 11 26 2002UALA01277 1 20020804 A 2120 SMOKE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY DETECTED A UALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 448UA 842 ON DESCENT, FLIGHT ATTENDANT RELEASED HALON EXTINGUISHER IN AFT LAV DUE TO LIGHT HAZE/SMOKE AND HEAT. EMERGENCY PROCEDU RES WERE PUT INTO EFFECT. SMOKE/HEAT HAD DISSIPATED ON LANDING. RAN ENGINES AND APU. CHECKED AFT FWD LAV FOR SIGNS OF SMOKE, ELECTRICAL SMELL NONE NOTED. CHECKED LAV WATER HEATER, OPEN UP PANEL IN AFT PIT AND CHECK APU DUCTING FOR POSSIB LE LEAK, NONE NOTED. REPLACED BOTH THE LEFT AND RIGHT PACK OZONE FILTERS. RAN PACKS FOR FIVE HOURS. ALSO RAN GALLEY CH ILLERS, OVENS, COFFEEPOT, HEATERS AND COFFEEMAKERS. CHECKED THE HOT WATER HEATERS UNDER SINK CHECKED GOOD. UNABLE TO P OSITIVELY IDENTIFY HAZE/SMOKE/HEAT SOURCE. 2 L 7 2 4F 4 F RT A28NM E40NE 2002082600025 20020826 00025 NM 2002 8 26 2002UALA01274 1 20020802 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 EXTERNAL FUSELAGE GOUGED STATION 299 BETWEEN STRINGER 25R AND 26R. ALSO GOUGED STATION 305 BETWEEN STRINGER 25R AND 26R . LIGHTNING STRIKES STATION 313 AT STRINGER 25R, AND STATION 308 STRINGER 25R AND 26R. FUSELAGE DENTED STATION 288 BET WEEN STRINGER 24R AND 23R. MAJOR REPAIR ACCOMPLISHED. ONE PIECE FUSELAGE DOUBLER REPAIR MANUFACTURED AND INSTALLED ENC OMPASSING ALL DAMAGE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082600026 20020826 00026 WP 2002 8 26 AALA20010933A 1 20020607 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND CUSP CORRODED AT STATION RIGHT 712. INSTALLED REPAIR DOUBLER PER AARD 53-00-00-02 PAGES 1-3. (M) 2 L 7 2 4F A6WE 2002082600027 20020826 00027 WP 2002 8 26 AALA20010934A 1 20020610 A 5320 SILL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND CORROSION ON ENTRY PLATE AT FORWARD SERVICE DOOR. REMOVED AND REPLACED ENTRY PLATE SRM 51-01. (M) 2 L 7 2 4F A6WE 2002082600028 20020826 00028 WP 2002 8 26 AALA20020935 1 20020606 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE LIGHTNING STRIKE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND STATIC DISCHARGE AFT OF ANTENNA CUT OUT AT STATION 380 BETWEEN L29L-L30. DUE PENNED, NO CRACKS FOUND, POLIS HED AREA, APPLIED ALODINE PER SRM 53-04-00 FIG 38 TABLE B SHEET 5 COND 1. (M) 2 L 7 2 4F A6WE 2002082600029 20020826 00029 WP 2002 8 26 AALA20020936 1 20020606 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND CORROSION AROUND ANTENNA CUTOUT ON FUSELAGE SKIN AT STATION 380 BETWEEN L29L-L30. BLENDED CORROSION PER SRM 51-01 AND SRM 53-04 FIG 38 TREATED WITH ALODINE, TABLE A COND 2. (M) 2 L 7 2 4F A6WE 2002082600030 20020826 00030 WP 2002 8 26 AALA20020937 1 20020615 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND CORROSION ON CUSP ABOVE DOOR CUTOUT STATION 1180. REPAIRED CUSP AS PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002082600031 20020826 00031 WP 2002 8 26 AALA20020938 1 20020607 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND DEEP SCRATCHES IN FUSELAGE SKIN AT ANTENNA EDGES. BLENDED OUT SCRATCHES PER SRM 53-04 FIG 38 SHEET 3 CONDIT ION 2 ALODINED AREA. (M) 2 L 7 2 4F A6WE 2002082600032 20020826 00032 WP 2002 8 26 AALA20020939 1 20020617 A 5553 ATTACH ANGLE DOUG DC9 DC982 3022082 WP VERTICAL STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND VERTICAL FIN ATTACH ANGLE CRACKED STATION 1408 RIGHT. REPLACED CHORD ANGLE STATION 1408 PER AARD 55-30-00-7 . (M) 2 L 7 2 4F A6WE 2002082600034 20020826 00034 WP 2002 8 26 AALA20020940 1 20020617 A 5553 ATTACH ANGLE DOUG DC9 DC982 3022082 WP VERTICA STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND VERTICAL FIN ATTACH ANGLE CRACKED STATION 1428 LEFT. REPLACED CHORD ATTACH ANGLE STATION 1428 PER AARD 55-3 0-00-1. (M) 2 L 7 2 4F A6WE 2002082600035 20020826 00035 WP 2002 8 26 AALA20020941 1 20020617 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND CABIN FLOOR WEB CRACKED STATION 1300 RIGHT SIDE 9 INCH INBOARD OF CUSP WEB. INSTALLED REPAIR PER ESO80559/6 -12-02. (M) 2 L 7 2 4F A6WE 2002082600036 20020826 00036 WP 2002 8 26 AALA20020942 1 20020620 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND CRACK EMITTING FROM FASTENER HOLE STATION 1380 LONGERON 14R. CUTOUT DAMAGE AND INSTALLED DOUBLER PER SRM 53 -04. (M) 2 L 7 2 4F A6WE 2002082600037 20020826 00037 WP 2002 8 26 AALA20020943 1 20020621 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND DENT IN FUSELAGE SKIN AT RED STRIPE ABOVE MIDDLE OF FORWARD CARGO DOOR. CUT OUT DAMAGE AND INSTALLED FILLER AND INTERNAL AND EXTERNAL DOUBLERS PER SRM 53-04. (M) 2 L 7 2 4F A6WE 2002082600038 20020826 00038 WP 2002 8 26 AALA20020944 1 20020612 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND SEVERAL SMALL SCRATCHES AND SLIGHT DENT ON LEFT SIDE STATION 237 1 INCH ABOVE CUSP LINE. INSTALLED REPAIR D OUBLER PER SRM 53-04 FIG 12B AND AARD 53-30-00-9. (M) 2 L 7 2 4F A6WE 2002082600039 20020826 00039 WP 2002 8 26 AALA20020945 1 20020610 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND FLOOR SUPPORT CORRODED STATION 1211 ABOVE LONGERON 28L TO 29R. REPLACED FLOOR SUPPORT PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 2002082600040 20020826 00040 WP 2002 8 26 AALA20020946 1 20020610 A 5320 TAB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 TUL - FOUND TAB CRACKED ON DOOR JAMB BOX WEB AT INTERCOSTAL STATION 207 LONGERON 15L. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-11 PAGE 1 AND 2. (M) 2 L 7 2 4F A6WE 2002082600041 20020826 00041 WP 2002 8 26 AALA20021004 1 20020619 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 554AA 53084 TUL - FOUND NR 1 SEAT TRACK CORRODED AT STATION 1236. MACHINED OUT DAMAGED AREA AND INSTALLED PLUG PER SRM 53-05-00 PAG E 8C PAGE 8D. (M) 2 L 7 2 4F A6WE 2002082600042 20020826 00042 NM 2002 8 26 AALA20021024 1 20020715 A 3350 1000679 SIGN BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 321AA 22322 LAX - DURING OVERNIGHT MAINTENANCE, FOUND FLIGHT DECK EMERGENCY EXIT SIGN INOPERATIVE. REPLACED FLIGHT DECK EMERGENCY E XIT SIGN LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082600044 20020826 00044 NE 2002 8 26 AALA20021028 2 20020715 A 7321 76960612 FUEL CONTROL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE MALFUNCTIONED A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 21 568AA 49349 IAD - FLT 1395 - EN ROUTE PHL-ORD, LEFT ENGINE THROTTLE RETARDED AT 10,000 FEET AND THEN REGAINED POWER UNCOMMANDED. DI VERTED AIRCRAFT TO IAD LANDING WITHOUT INCIDENT. AIRCRAFT NOT OVERWEIGHT. REPLACED LEFT ENGINE FUEL CONTROL AND FUEL P UMP. TRIMMED ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002082600045 20020826 00045 WP 2002 8 26 AALA20021029 1 20020716 A 3350 AAP3274A CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 295AA 49307 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS IN CEILING ROW 23 THROUGH 26 INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082600046 20020826 00046 WP 2002 8 26 AALA20021030 1 20020625 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14551 53033 TUL - FOUND AFT EDGE OF FLOORBOARD CORRODED UNDER F/O'S SEAT. REPLACED FLOORBOARD TOP SKIN SHEET AND INSTALLED FLOORBOA RD PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002082600048 20020826 00048 WP 2002 8 26 AALA20021031 1 20020703 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14551 53033 TUL - FOUND CORROSION STATION 1149-1212. REMOVED CORROSION, INSTALLED DOUBLER PER ESO 80559. (M) 2 L 7 2 4F A6WE 2002082600049 20020826 00049 WP 2002 8 26 AALA20021032 1 20020601 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14551 53033 TUL - FOUND CORROSION FORWARD LOWER DOOR CORNER CUTOUT BRACKET. INSTALLED NEW SERVICEABLE FORWARD LOWER DOOR CORNER CAS TING AT STATION 1145-1146. (M) 2 L 7 2 4F A6WE 2002082600050 20020826 00050 WP 2002 8 26 AALA20021033 1 20020717 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427AA 49339 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS BETWEEN ROWS 4-7 INOPERATIVE. TIGHTENED WIRE ON BATTE RY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082600051 20020826 00051 WP 2002 8 26 AALA20021034 1 20020716 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 443AA 49469 DTW - DURING OVERNIGHT MAINTENANCE EMERGENCY ESCAPE PATH SEAT MOUNTED LIGHTING AT SEAT 11DEF INOPERATIVE. REPLACED CANN ON PLUG TO SEAT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082600052 20020826 00052 WP 2002 8 26 AALA20021035 1 20020718 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7546A 53028 TUL - FOUND LONGITUDINAL FLOOR SUPPORT AT RBL 52 HAS AREA OF CORROSION AT STATION 172 AND 195. INSTALLED NEW LONGITUDIN AL FLOORBOARD SUPPORT AT RBL 52 STATION 172-195 SRM 51-01. (M) 2 L 7 2 4F A6WE 2002082600053 20020826 00053 WP 2002 8 26 AALA20021036 1 20020708 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7546A 53028 TUL - FOUND FLOOR WEB HAS CORROSION STATION 190-200, RBL 49-52. CUT OUT CORROSION INSTALLED DOUBLER PER SRM 51-01 FIG 2 SHEET 1. (M) 2 L 7 2 4F A6WE 2002082600054 20020826 00054 WP 2002 8 26 AALA20021037 1 20020708 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7546A 53028 TUL - FOUND FLOOR WEB HAS CORROSION STATION 178-180 RBL 50 TO 52. CUT OUT CORROSION INSTALLED DOUBLER PER SRM 51-01 FIG 2 SHEET 1. (M) 2 L 7 2 4F A6WE 2002082600055 20020826 00055 WP 2002 8 26 AALA20021038 1 20020711 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7546A 53028 TUL - FOUND GOUGE IN NR 2 SEAT TRACK APPROX STATION 1250. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 1240-1309 PE R SRM 51-01. (M) 2 L 7 2 4F A6WE 2002082600056 20020826 00056 WP 2002 8 26 AALA20021039 1 20020718 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7546A 53028 TUL - FOUND HORIZONTAL FLOORBOARD SUPPORT AT STATION 200 HAS AREA OF CORROSION AT RBL 49. INSTALLED NEW FLOOR SUPPORT A T STATION 200 RBL 49 SRM 51-01. (M) 2 L 7 2 4F A6WE 2002082600058 20020826 00058 WP 2002 8 26 AALA20021040 1 20020711 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7546A 53028 TUL - FOUND LEFT CUSP CORRODED STATION 1306. INSTALLED NEW CUSP SECTION FROM LEFT 1250 TO 1306 AS PER SRM 53-05 FIG 97. (M) 2 L 7 2 4F A6WE 2002082600059 20020826 00059 WP 2002 8 26 AALA20021041 1 20020708 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7546A 53028 TUL - FOUND LEFT CUSP HAS FOUR PUNCTURE HOLES AT NR 1 SEAT TRACK, STATION 1200 TO 1214. INSTALLED DOUBLER AS PER AARD 5 3-00-00-02 SRM 53-01. (M) 2 L 7 2 4F A6WE 2002082600060 20020826 00060 WP 2002 8 26 AALA20021042 1 20020702 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7546A 53028 TUL - FOUND THREE SMALL AREAS SURFACE CORROSION LEFT CUSP STATION 526. CUT OUT CORROSION, FABRICATE DOUBLER ALODINED, A ND PRIMED. REPAIR AREA AND DOUBLER, INSTALLED DOUBLER AS PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002082600061 20020826 00061 WP 2002 8 26 AALA20021044 1 20020710 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 21 7546A 53028 TUL - FOUND CORROSION ON LEFT CUSP, UNDER NR 1 SEAT TRACK STATION 1175. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002082600062 20020826 00062 WP 2002 8 26 AALA20021045 1 20020710 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7546A 53028 TUL - FOUND CORROSION ON AFT CARGO DOOR CUT OUT LOWER DOOR BEAM. REMOVED AND REPLACED AFT CARGO CUT OUT LOWER DOOR BEAM PER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2002082600063 20020826 00063 WP 2002 8 26 AALA20021046 1 20020627 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND SHEAR TIE CRACKED STATION CANT 1437 STR 2R. INSTALLED NEW SHEAR TIE PER SRM 51-00. (M) 2 L 7 2 4F A6WE 2002093000006 20020930 00006 NM 2002 9 30 2002UALA01278 1 20020804 A 2425 7077604 INVERTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE E/E BAY MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 643UA 25093 EICAS STATUS MESSAGE OF STANDBY INVERTER DISPLAYED. UNABLE TO CLEAR MESSAGE. SUPPLEMENTAL DATA UPDATE FOUND INVERTER P OWER TRU CB OPEN, REPLACED STATIC INVERTER. OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2002082600067 20020826 00067 2002 8 26 2002UALA01279 4 20020802 A 2565 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 829UA 1211 DURING NR 3 SERVICE CHECK OF EMERGENCY LIGHTING SYSTEM FOUND EPSU EXT LOAD AFT L FAULT. POWER SUPPLY SHOWS EXT LOAD FAU LT. SUSPECT SLIDE LIGHTS BAD. BOTH SLIDES REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002082600069 20020826 00069 NM 2002 8 26 2002UALA01280 1 20020806 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 HOLE IN FUSELAGE NEAR BOTTOM OF AFT LEFT ENTRY DOOR. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND TRIPLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082600070 20020826 00070 NM 2002 8 26 2002UALA01282 1 20020806 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 943UA 26680 178 BULKHEAD WEB CRACKED AT RIGHT HAND LOWER WL 200 RBL 5. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112500107 20021125 00107 NM 2002 11 25 2002UALA01283 1 20020805 A 7312 51A346 FUEL HEATER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ENGINE FAILED A UALA O OTHER M J OVER TEMP WARNING INDICATION DE DESCENT 1 WP 29 773UA 26929 777002 ENG OIL TEMP R EICAS AND AMBER TEMP DISPLAY, TEMP DISPLAY WENT RED ON GROUND DURING TAXI. REPLACED THE SERVO FUEL HEATE R. SHOP TEARDOWN OF THE REMOVED HEATER REVEALED FAILED TUBES IN THE FUEL/OIL HEAT EXCHANGER. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002082600071 20020826 00071 NM 2002 8 26 2002UALA01284 1 20020807 A 5330 DOUBLER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 EXTERNAL EXISTING FUSELAGE SKIN REPAIR STATION 845, 1 INCH BELOW STR 22R GOUGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082600072 20020826 00072 NM 2002 8 26 2002UALA01285 1 20020808 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE LIGHTNING STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 943UA 26680 FUSELAGE SKIN ALONG LEFT HAND SIDE OF A/C AT STRINGER 22L & BODY STATION 407.75 HAS A FASTENER & SKIN AROUND FASTENER WI TH EXTENSIVE DAMAGE DUE TO LIGHTNING STRIKE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED REPAIRED BY FREEZE PLUG AND INSTALLED NEW FASTENER WITH STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082600073 20020826 00073 SO 2002 8 26 AQF2002F00000 2 20020706 A 8530 CYLINDER CESSNA 150 150B 2071806 CE CONT O200 O200A 17020 SO NR 4 CRACKED D AQFA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 11 1128Y 15059528 29391A LOOKING FOR OIL LEAK. FOUND CRACK INSIDE CYLINDER ABOUT MIDWAY. CIRCULAR COVERING APPROXIMATELY 30 PERCENT OF RADIUS. 1600 HOURS SMOH 1 H 7 1 3O 3 O 3A19 E252 2002082600074 20020826 00074 SO 2002 8 26 BTH2002F00003 1 20020813 A 3243 6846400 FITTING PIPER PA32 PA32260 7103206 SO LYC O540 O540* 41532 EA BRAKE RESERVOIR CRACKED E BTHA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 7748J 14777 321152 BRAKE RESERVOIR (PN 6846400) HAD A CRACKED HOSE ATTACH FITTING LEAKING HYDRAULIC FLUID ON TO DEFROSTER HOSE, CAUSING SMO KE IN COCKPIT. REPLACED BRAKE RESERVOIR WITH A SERVICEABLE PART. 1 L 7 1 3O 3 O A3SO E295 2002082600075 20020826 00075 CE 2002 8 26 FFK2002F00000 1 20020722 A 8010 642083A5 ADAPTER BEECH 58 58 1152740 CE LT ENGINE INOPERATIVE B FFKR K NONE O OTHER IN INSP/MAINT 1 SO 05 11HW 59 TH271 LEFT ENGINE STARTER ADAPTER ACCESSORY, INOPERATIVE. ENGINE WILL NOT TURN OVER, SUSPECT BROKEN SPRING, IN CLUTCH ACCESSO RY UNIT HAS 59 HOURS. 1 L 7 2 3O 3A16 2002082600076 20020826 00076 SO 2002 8 26 J4P2002F00000 1 20020802 A 2822 SEAL PIPER PA34 PA34220T 7103420 SO CONT O360 LTSIO360KB 17025 SO BOOST PUMP FAILED E J4PA K NONE O OTHER IN INSP/MAINT 1 SO 13 9257X 1083 3447002 319277 SHAFT SEAL FAILURE ALLOWING FUEL TO ENTER BOOST PUMP MOTOR INCREASING POTENTIAL FOR AIRCRAFT FIRE. 1 L 7 2 3O 3 O A7SO E9CE 2002082600077 20020826 00077 CE 2002 8 26 KZ52002F00001 1 20020815 A 8011 MHJ3151S GEAR BEECH 65 65 1152802 CE LYC O720 IO720A1B 41546 EA ARMATURE BROKEN B KZ5R K NONE O OTHER IN INSP/MAINT 1 GL 15 5078N 222 LF16 RL123954A A NEW STARTER NEEDS TO BE DESIGNED. ENGINE DID NOT KICK BACK DURING START. 1 L 7 2 3O 3 O 3A20 1E15 2002082600078 20020826 00078 SO 2002 8 26 SO52002F00000 1 20020805 A 2840 6770051 LINE PIPER PA32 PA32RT300 7103215 SO LYC O540 IO540* 41532 EA FUEL GAUGE CORRODED B SO5R O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NE 03 319SF 32R7885140 PILOT REPORTED STRONG SMELL OF FUEL (AVGAS) IN COCKPIT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FUEL LINE FROM FUEL PRESSURE GAUGE TO FORWARD BULKHEAD AT STA 53.60 LEAKING. LINE WAS SEVERLY CORRODED IN A 1.5000 IN LONG SECTIO N APPROX. 3 INCHES FROM BULKHEAD FITTING. TUBE ASSEMBLY WAS UNAVAILABLE FROM PIPER. FABRICATED AND INSTALLED A NEW LI NE PER AC. OPERATIONAL AND LEAK CHECK SATISFACTORY. SUBMITTER SUSPECTS WATER LEAKAGE FROM WINDSHIELD OR DEFROSTER DUCT S DRIPPING ON TUBING AS CAUSE OF CORROSION. 1 L 7 1 3O 3 O A3SO 1E4 2002082600079 20020826 00079 NM 2002 8 26 2002UALA01286 1 20020808 A 2131 CONTROLLER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 29 203UA 24718 FORWARD ENTRY DOOR LIGHT ILLUMINATED. AIRCRAFT DID NOT PRESSURIZE, AND DOOR WAS NOISY. THE DOOR LIGHT WAS CAUSED BY TH E DOOR STRIKER BEING OUT OF ADJUSTMENT. ADJUSTED STRIKER PLATE AND LIGHT OPS GOOD. THE PRESSURIZATION PROBLEM WAS NOT CAUSED BY THE DOOR. PRESSURE CONTROLLER REPLACED AND NO ADDITIONAL PROBLEMS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700011 20021017 00011 NE 2002 10 17 2002UALA01287 2 20020808 A 7230 500170702TYP BLADE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE FAILED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 611UA 21872 715854 RIGHT ENGINE COMPRESSOR STALL - HIGH EGT ON CLIMB OUT. SEVENTH STAGE COMPRESSOR BLADE FAILURE. ON TEARDOWN, FIVE EACH BLADES WERE COMPLETELY MISSING FROM THE DISK. 2 L 7 2 4F 4 F RT A1NM E3NE 2002100200017 20021002 00017 NM 2002 10 2 2002UALA01288 1 20020808 A 3830 VALVE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LAVATORY FAILED A UALA A UNSCHED LANDING K FLUID LOSS UK UNKNOWN 1 WP 29 620UA 21880 MID CABIN LAV TOILET OVERFLOWED, WATER SHUTOFF. RINSE VALVE ON TOILET ASSY FAILED IN THE OPEN POSITION. REPLACED TOILE T ASSEMBLY. 2 L 7 2 4F 4 F RT A1NM E3NE 2002100200018 20021002 00018 2002 10 2 2002UALA01289 4 20020807 A 2565 416T281229 BRACKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE LOOSE A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 656UA 25394 'L WING SLIDE' EICAS MESSAGE DISPLAYED INTERMITTENTLY WITH EMERGENCY DOOR OVERHEAD LIGHTS FLICKERING. TARGET ASSY BRACK ET FOUND LOOSE IN OFF WING SLIDE COMPARTMENT. SECURED BRACKET. 2 L 7 2 4F 4 F RT A1NM E24NE 2002082600080 20020826 00080 NM 2002 8 26 2002UALA01290 1 20020809 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 942UA 26679 CABIN FLOORBEAM AT STATION 986.5 HAS A STRAP REPAIR INSTALLED AT RIGHT HAND SIDE WALL, REQUIRES ANGLE REPAIR. MAJOR REP AIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082600081 20020826 00081 NM 2002 8 26 SROM200200018 1 20020815 A 3020 320115 VALVE BOEING 737 737205 1384456 NM ANTI ICE SYS SHORTED I SROM A UNSCHED LANDING O OTHER CR CRUISE 1 AL 03 733PA 58140 12482 23466 "ANTI-ICE ENG 2 & WING VALVE CIRCUT BREAKER POPS WHEN ANTI-ICE IS TURNED ON". AIRCRAFT RETURNED TO DEPARTURE AIRPORT DU E TO WEATHER CONDITIONS AT DESTINATION AIRPORT. "T/S TO #2 ENGINE COWL VALVE. REPLACED SAME. REF MM 75-11-11. OPS & LEAK CHECK GOOD". 2 L 7 2 4F RT A16WE 2002082600082 20020826 00082 CE 2002 8 26 VJ32002F00058 1 20020806 A 2710 3552431422 CONTROL CABLE BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO AILERON FRAYED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 8101C 2552 CE1538 825785R CABLE FRAYED WHERE IT PASSES THROUGH A PULLEY ASSEMBLY. CAUSE MAY BE DUE TO PULLEY NOT ROTATING WHEN CABLE IS EXERCISED . RECOMMEND TO INSTALL SEALED BEARING TYPE PULLEY IN THESE AREAS. 1 L 7 1 3O 3 O 3A15 E5CE 2002082600083 20020826 00083 EA 2002 8 26 VJ32002F00059 2 20020805 A 8530 115TA601004 BAFFLE GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA ENGINE CYCLINDER CRACKED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 861AF 47 85001 L2802348A ENGINE BAFFLE CRACKED ON NUMBER 3 CYLINDER FROM NORMAL ENGINE VIBRATION. 1 L 7 1 3O 3 O RT A49CE 1E4 2002082600084 20020826 00084 EA 2002 8 26 VJ32002F00060 2 20020805 A 8530 115TA601003 BAFFLE GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA ENGINE CYLINDER CRACKED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 864AF 146 85004 L2826348A ENGINE BAFFLE CRACKED ON NUMBER 1 CYLINDER FORM NORMAL ENGINE VIBRATION. RECOMMEND FOR FACTORY TO REINVESTIGATE ENGINEE RING DRAWING TO COME UP WITH A STRONGER PIECE OF BAFFLING TO INSTALL. 1 L 7 1 3O 3 O RT A49CE 1E4 2002082600085 20020826 00085 EA 2002 8 26 VJ32002F00061 2 20020805 A 8530 115TA601009 BAFFLE GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA ENGINE CYLINDER CRACKED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 864AF 85004 L2826348A ENGINE BAFFLE CRACKED ON NUMBER 4 CYLINDER FROM NORMAL ENGINE VIBRATION. 1 L 7 1 3O 3 O RT A49CE 1E4 2002082600086 20020826 00086 NM 2002 8 26 QXEA0201275 1 20020822 A 3230 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 OUT OF ADJUST A QXEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 09 410QX 4053 SEA - CREW RETURNED TO FIELD WHEN AFTER TAKEOFF THE RIGHT GEAR DOOR AND GEAR UPLOCK LIGHTS ILLUMINATED FOR APPROXIMATELY 2 TO 3 MINUTES. GEAR EXTENSION WAS NORMAL. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE MAIN GEAR UPLOCK PROXIMITY SENSOR IN THE FAR CONDITION. MAINTENANCE ADJUSTED THE MAIN LANDING GEAR UPLOCK PROXIMITY SENSOR ON THE RIGHT GEAR IAW WI TH THE MAINTENANCE MANUNAL. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002082600087 20020826 00087 NM 2002 8 26 2002UALA01291 1 20020809 A 5320 ANGLE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 943UA 26680 CABIN RIGHT HAND CREASE BEAM INBOARD SUPPORT ANGLE AT STATION 294 RBL 55 HAS CORROSION AND BARE METAL EXPOSED. MAJOR RE PAIR ACCOMPLISHED. REPLACED Z-ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082600088 20020826 00088 NM 2002 8 26 2002UALA01292 1 20020811 A 5310 DOOR FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 943UA 26680 FORWARD GALLEY DOOR CUTOUT FORWARD FRAME IS CRACKED AT TOP INBOARD CORNER. MAJOR REPAIR ACCOMPLISHED. REPLACED STUB FR AME. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082600089 20020826 00089 NM 2002 8 26 2002UALA01293 1 20020811 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 AFT PIT DOOR SILL VERTICAL WEB GOUGED BETWEEN STATION 793 - 821 RBL 23 (APPROX) BELOW FLOOR TRACK. MAJOR REPAIR ACCOMPL ISHED. INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800113 20021018 00113 NM 2002 10 18 2002UALA01294 1 20020811 A 2611 21198356 SMOKE DETECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CARGO BAY DEFECTIVE A UALA B F A EMER. DESCENT ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 210UA 8200 30216 COCKPIT HAD AFT CARGO PIT FIRE INDICATION ON EICAS. DISCHARGED BOTH FIRE BOTTLES AS PRECAUTION. FALSE FIRE ALARM CAUSE D BY DEFECTIVE AFT CARGO COMPARTMENT SMOKE DETECTOR. SMOKE DETECTOR WAS REPLACED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002082600090 20020826 00090 SO 2002 8 26 C2XA02CL175 1 20020825 A 7931 23070401 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL OUT OF TOLERANCE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 11544 1498 145557 CAE312023 CLE FLIGHT# 3198 THE CREW REPORTED THE #1 ENGINE OIL PRESSURE EXCEEDED LIMITS IN CLIMBOUT.MAINTENANCE INSPECTED AND REMO VED AND REPLACED THE #1 ENGINE.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002082600091 20020826 00091 WP 2002 8 26 DHL2002806846 1 20020704 A 5712 FORMER DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 81567 46002 ITEM REF N/R 1317 LT. WING OUTBD L/E FORMER CRACKED AT STA. XFS691.000CORR: STOP DRILLED CRACK IAW SRM 57-2-0 PG. 9-10 FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED AND PRIMED AREA IAW SRM 51-1-8B INSTALLED REINFOR CING ANGLE ON OUTBD L/E FORMER , XFS691.000 IAW SRM57-2-0 PG. 9-10 2 L 7 4 4F RT 4A25 2002082600092 20020826 00092 WP 2002 8 26 DHL8062002847 1 20020705 A 5712 FORMER DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 81567 46002 ITEM N/R 1964 RH WING OUTBOARD LEADING EDGE UPPER PART FORMER CRACKED 3/4 " XFS616.250CORR: REMOVEED FASTNERS IAW SRM 51 -1-21 PG1 PERFORMED STOP DRILL IAW SRM 57-2-0 PG 9-10 FABRICATED DOUBLER IAW 57-2-0 PG 9-10 CLEANED , TREATED , AND PRIM ED IAW SRM 51-1-8B , INSTALLED DOUBLER ON RH WING OUTBD LEADING EDGE UPPER PART FORMER WITH NEW FASTNERS IAW SRM 57-2-0 PG. 9-10 AND SRM 51-1-21 PG 1 2 L 7 4 4F RT 4A25 2002082600093 20020826 00093 WP 2002 8 26 DHL2002806848 1 20020703 A 5712 FORMER DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 81567 46002 ITEM REF N/R 2233 LH WING CTR. LEADING EDGE LOWER SURFACE FORMER WITH 1" CRACK IN IT STA XFS 335.220 CORR: REMOVED FASTN ERS IAW SRM 51-1-21 PG. 1 STOP DRILLED CRACK IAW SRM57-2-0 PG. 9-10FABRICATED REINFORCING ANGLE IAW SRM57-2-0 PG. 9-10 , CLEANED , TREATED , AND PRIMED IAW SRM51-1-8B , INSTALLED REINFORCING ANGLEAND NEW FASTNERS IAW SRM 57-2-0 PG. 9-10 , S RM 51-1-21 PG.1 2 L 7 4 4F RT 4A25 2002082600094 20020826 00094 WP 2002 8 26 DHL2002806849 1 20020704 A 5712 FORMER DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 81567 46002 ITEM REF N/R 2286 RH WING CTR L/E LOWER FORMER 1" CRACK , STA. XFS360.250CORR: PERFORMED STOP DRILL ON 1" CRACK , STA XF S360.250 IAW SRM 57-2-0 PG. 9-10 FABRICATED DOUBLER IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1- 8B INSTALLED DOUBLER ON CTR L/E LOWER FORMER IAW SRM 57-2-0 PG 9-10 2 L 7 4 4F RT 4A25 2002082600095 20020826 00095 WP 2002 8 26 DHL2002806850 1 20020704 A 5712 FORMER DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 81567 46002 ITEM REF. N/R RH WING CTR L/E FORMER .500 CRACKED XFS329.000CORR: STOP DRILLED CRACK ON RH WING CTR L/E UPPER FORMER , S TA. XFS329.000 , IAW SRM57-2-0 PG. 9-10 FABRICATED DOUBLER IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SR M 51-1-8B, INSTALLED DOUBLER ON RH WING CTR L/E UPPER FORMER IAW SRM 57-2-0 PG. 9-10 2 L 7 4 4F RT 4A25 2002082600096 20020826 00096 WP 2002 8 26 DHL2002806851 1 20020704 A 5712 FORMER DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 81567 46002 ITEM REF N/R 2282 RH WING CTR LEADING EDGE UPPER FORMER .500 CRACK @ STA XFS 322.750CORR: REMOVED FASTNER IAW SRM 51-1-2 1 PG 1 , FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B INSTALLED R EINFORCING ANGLE AND NEW FASTNERS IAW SRM 57-2-0 PG. 9-10 SRM 51-1-21 PG. 1 2 L 7 4 4F RT 4A25 2002101700012 20021017 00012 NM 2002 10 17 2002UALA01295 1 20020811 A 2822 5006286F PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUEL SYSTEM FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 655UA 25393 INDICATION OF A LEFT CENTER BOOST PUMP FAILURE WITH POSSIBLE FUEL IMBALANCE. THE LEFT CENTER FUEL TANK OVERRIDE PUMP WA S REPLACED AND OPS CHECKED OK. SYSTEM OPERATION NORMAL THROUGH 8/25/2002. SHOP TEST OF THE REMOVED PUMP WAS PERFORMED WITH NO DEFECTS NOTED. 8/26/02 THE LT OVERRIDE PUMP AGAIN EXHIBITED THE SAME SYMPTOM. THE PUMP WAS REMOVED AND A PUMP WITH MACHINED DIFFUSER WAS INSTALLED AND SYSTEM OPERATION HAS BEEN NORMAL TO DATE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002082600098 20020826 00098 NM 2002 8 26 2002UALA01297 1 20020812 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 RIGHT HAND CABIN FLOOR FRAME, STATION 1640, RBL 55, WL 208 HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INS TALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082600100 20020826 00100 NM 2002 8 26 2002UALA01299 1 20020812 A 5310 CREASE BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 942UA 26679 CABIN AFT RIGHT HAND GALLEY DOOR CREASE BEAM INBOARD CHORD CORRODED ALONG DOOR OPENING AREA STATION 947 - 1006 RBL45 - R BL 47. MAJOR REPAIR ACCOMPLISHED. REPLACED CHORD ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700013 20021017 00013 NE 2002 10 17 2002UALA01300 2 20020812 A 7200 810641 BEARING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 615UA 24639 85 21876 709628 RIGHT ENGINE OIL FILTER MESSAGE DISPLAYED. RIGHT ENGINE SHUTDOWN BEFORE LANDING. FAILURE OF THE NUMBER THREE BEARING. ENGINE WAS 85 HOURS TSO. FAILURE BEING INVESTIGATED BY ENGINE OVERHAUL OSV AND BEARING OSV. 2 L 7 2 4F 4 F RT A1NM E3NE 2002101700014 20021017 00014 NE 2002 10 17 2002UALA01301 2 20020808 A 7320 3352615000 B-NUT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE LOOSE A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 310UA 23671 724330 NR 2 ENGINE ROLLED BACK TO IDLE AT 800 FT AGL. AIRCRAFT RETURNED TO FIELD. ROLLBACK WAS ATTRIBUTED TO A LOOSE CDP B-NU T AIR SIGNAL LINE AT THE MAIN ENGINE CONTROL, 9 O'CLOCK POSITION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800114 20021018 00114 NM 2002 10 18 2002UALA01302 1 20020812 A 2612 47348707 CIRCUIT CARD BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FIRE WARNING FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 793UA 26946 INTERMITTENT PROBLEM WITH LEFT ENGINE FIRE DETECTION SYSTEM. THE NR 1 ENGINE OVERHEAT MESSAGE WAS A FALSE INDICATION. BOTH OF THE NR 1 ENGINE FIRE LOOPS WERE INSPECTED AND OPS CK'D WITH NO DISCREPANCIES FOUND. DUE TO LEFT CARD FAULT INDI CATION FROM CMC, THE NR 1 ENGINE FIRE DETECTION CARD WAS REPLACED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002100200019 20021002 00019 EU 2002 10 2 2002UALA01303 1 20020813 A 2810 L95F50603 DISK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CENTER TANK RUPTURED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 481UA 1559 FLIGHT DIVERTED UNDER AMBER ALERT DUE TO FUEL IMBALANCE. FOUND BURST DISC BETWEEN LEFT INNER AND CENTER FUEL TANKS BROK EN. REPLACED DISC. 2 L 7 2 4F 4 F RT A28NM E40NE 2002082600104 20020826 00104 NM 2002 8 26 2002UALA01307 1 20020813 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 942UA 26679 RIGHT HAND STATION 188 FRAME CRACKED AT WL 207. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100200020 20021002 00020 2002 10 2 2002UALA01308 4 20020812 A 2397 WIRE BOEING 777 777222 1385219 NM CABIN DAMAGED A UALA O OTHER O OTHER UK UNKNOWN 1 WP 29 229UA 30557 FOUND ARCED WIRES IN BUNDLE. ONE WIRE IS BROKEN, OTHER WIRES ARE DAMAGED, LOCATED AT STATION 731 ABOVE VIDEO CONTROL CE NTER. DAMAGE WAS CAUSED BY THE WIRE BUNDLE CHAFFING AGAINST THE EDGE OF THE VIDEO CONTROL CENTER PANEL. WIRE BUNDLE WAS REPAIRED, ROUTED AND SECURED AWAY FROM ANY AIRCRAFT STRUCTURE. 2 L 7 2 4F RT T0001SE 2002100200021 20021002 00021 NM 2002 10 2 2002UALA01309 1 20020813 A 5330 141W2315 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 27786 27786 26947 FUSELAGE SKIN DAMAGED AT STA 390, STR 32R. MAJOR REPAIR ACCOMPLISHED. EXTERNAL DOUBLER APPLIED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002082600105 20020826 00105 NM 2002 8 26 2002UALA01310 1 20020815 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 AFT PIT DOOR CUTOUT SKIN BEAR STRAP BLENDED BEYOND LIMITS AT STATION 796 STR 21-24R. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100200022 20021002 00022 NM 2002 10 2 2002UALA01311 1 20020814 A 5313 STRINGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 DAMAGE TO FUSELAGE STRINGER 43L FOUND, STA 1520 TO 1540. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR PERFORMED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002100200023 20021002 00023 NE 2002 10 2 2002UALA01313 2 20020814 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE STALLED A UALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 643UA 41448 2628 25093 724378 COMPRESSOR STALL ON LEFT ENGINE AT TAKEOFF. ENGINE EXPERIENCED A GROUP 3 (TAKEOFF) SURGE. REMOVED ENGINE FOR HIGH COMP RESSOR OVERHAUL. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101700015 20021017 00015 NM 2002 10 17 2002UALA01314 1 20020814 A 2750 215016001 INDICATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT LOOSE A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 504UA 24625 RIGHT TRAILING EDGE FLAP WILL NOT EXTEND BEYOND 15 DEGREES. THE FLAP POSITION INDICATOR WAS IMPROPERLY TORQUED DURING I NSTALLATION. INDICATOR WAS RETORQUED AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082600107 20020826 00107 NM 2002 8 26 2002UALA01315 1 20020815 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 345UA 24249 DENT FOUND IN RIGHT HAND SIDE OF FUSELAGE BELOW FWD LAV SERVICE PANEL AND ABOUT 3 INCHES AFT OF RED STEERING LIMIT STRIP E. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082600108 20020826 00108 NM 2002 8 26 2002UALA01316 1 20020816 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 FUSELAGE SKIN, STA 1520 TO 1540, STR 42L, IS DENTED AND GOUGED. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND TRIPLER APPLIED . 2 L 7 4 4F 4 F RT A20WE E24NE 2002082600110 20020826 00110 NM 2002 8 26 SABA020086 1 20020823 A 3350 1306 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 882CC 168 FLIGHT 5098 FROM CINCINNATI TO CHARLOTTE : DURING POST FLIGHT INSPECTION IN CHARLOTTE, THE AIRCREW REPORTED THE EMERGENC Y LIGHT AT ROW FIVE INOP. MAINTENANCE REMOVED AND REPLACED BULB AND SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2002082600111 20020826 00111 NM 2002 8 26 UPS02239164 1 20020812 A 5340 SEAT TRACK BOEING 727 72731C 1384011 NM BS 960 BBL18 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C CRACK ON SEAT TRACK IN LWR AFT CARGO COMP. AT BS 960 BBL 18L REPAIR CARRIED OUT IAW SRM 53-10-5 FI G 5 2 L 7 3 4F A3WE 2002082600112 20020826 00112 NM 2002 8 26 UPS02439162 1 20020804 A 5310 FITTING BOEING 747 747212B 1384886 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C RH BS 1480 B/H EXTENSION FITTING #9 HOLE CRACK FOUND, APPROX 1/16", RUNNING FWD & AFT REFER ATTACHED S KETCH. ( STR R33 TO R34) RH BS 1480 B/H EXTENSION FITTING #9 HOLE REAMED TO 0.850" DIAMETER AND BUSHING REPAIR CARR IED OUT AS PER RS #R-53-43-34874. NOTE: REPEAT INSPECTIONS PER UPS EO -B747-10732 APPENDIX 'C' MUST BE ACCOMPLISHED EVE RY 48,00 CYCLES. 2 L 7 4 4F A20WE 2002082600113 20020826 00113 NM 2002 8 26 UPS02439163 1 20020804 A 5310 SKIN BOEING 747 747212B 1384886 NM BS1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C RH BS 1480 B/H #12 HOLE CRACK FOUND AT SKIN THROUGH THICKNESS RUNNING FWD & AFT REFER ATTACHED SKETCH. (STR R33 TO R34) RH BS 1480 B/H #12 HOLE AT SKIN REAMED TO 0.710 " DIAMETER AND BUSHING REPAIR CARRIED OUT AS PER R S # R-53-43-34784. NOTE: REPEAT INSPECTIONS PER UPS EO-B747-10732 APPENDIX 'C' MUST BE ACCOMPLISHED EVERY 4,800 CYCLES. 2 L 7 4 4F A20WE 2002082600115 20020826 00115 WP 2002 8 26 AALA20021047 1 20020625 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND 4 INCH CRACK AT LEFT CUSP AT STATION 224. INSTALLED NEW CUSP SHEET STATION 218 TO 237 LEFT SIDE PER SRM 51- 01. (M) 2 L 7 2 4F A6WE 2002082600116 20020826 00116 WP 2002 8 26 AALA20021048 1 20020626 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND NR 5 SEAT TRACK CORRODED FROM STATION 200-218, AND STATION 235-238. INSTALLED NEW NR 5 SEAT TRACK FROM STAT ION 200-240 PER SRM 53-05 FIG 4. (M) 2 L 7 2 4F A6WE 2002082600117 20020826 00117 WP 2002 8 26 AALA20021049 1 20020625 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND CORROSION ON RIGHT CUSP STATION 725-728. REMOVED CORROSION. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002082600118 20020826 00118 WP 2002 8 26 AALA20021050 1 20020626 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND CORROSION ON SUBFLOOR UNDER SEAT TRACK NR 5 STATION 200-219 AT SEAT TRACK FASTENER HOLES. CUT OUT CORROSION 3 INCH BY 4 INCH INSTALLED DOUBLER PER SRM 53-01 IN SUBFLOOR. (M) 2 L 7 2 4F A6WE 2002082600119 20020826 00119 WP 2002 8 26 AALA20021051 1 20020703 A 5320 STRAP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND CORROSION ON STRAP, LONGERON 28R STATION 1155. INSTALLED FREEZE PLUG PER ESO 80559. (M) 2 L 7 2 4F A6WE 2002082600120 20020826 00120 WP 2002 8 26 AALA20021052 1 20020702 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND CORROSION ON LOWER DOOR JAMB. INSTALLED DOUBLER REPAIR PER ESO 8055907-02-02. (M) 2 L 7 2 4F A6WE 2002082600121 20020826 00121 WP 2002 8 26 AALA20021053 1 20020626 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND L4L HAS A CRACK AROUND FASTENER AT STATION 156 ABOVE EDC PANEL. SPLICED IN LONGERON AND INSTALLED DOUBLER P ER SRM 53-02. (M) 2 L 7 2 4F A6WE 2002082600122 20020826 00122 WP 2002 8 26 AALA20021055 1 20020627 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND SKIN CRACKED AT STATION 1380, LONGERON 14L. INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002082600123 20020826 00123 WP 2002 8 26 AALA20021056 1 20020621 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND CORROSION ON NR 2 SEAT TRACK IN AFT GALLEY AREA. CUT OUT CORRODED AREA INSTALLED PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2002082600124 20020826 00124 WP 2002 8 26 AALA20021057 1 20020624 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND CORROSION ON NR 1 SEAT TRACK AT TIE DOWN STATION 1236. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2002082600125 20020826 00125 WP 2002 8 26 AALA20021058 1 20020702 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE LIGHTNING STRIKE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND STATIC DISCHARGES ON FUSE SKIN FROM STATION 350 TO 370 BETWEEN LONGERON 23R AND LONGERON 24R. BLENDED AREAS , DYE CHECKED, INSTALLED DOUBLER PER SRM 53-04 AND AARD 53-30-00-03. (M) 2 L 7 2 4F A6WE 2002082600126 20020826 00126 WP 2002 8 26 AALA20021059 1 20020702 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE LIGHTNING STRIKE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL- FOUND STATIC DISCHARGES ON FUSELAGE SKIN BETWEEN STATION 427 TO STATION 446 BETWEEN LONGERON 23R AND 25R. BLENDED AREAS, BYE CHECKED, INSTALLED DOUBLER PER PER SRM 53-04 AND AARD 53-30-00-07. (M) 2 L 7 2 4F A6WE 2002082600127 20020826 00127 WP 2002 8 26 AALA20021060 1 20020625 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND DENT IN FUSELAGE SKIN STATION 224 BETWEEN LONGERON 1 AND 2R. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-0 4-00 FIG 38. (M) 2 L 7 2 4F A6WE 2002082600128 20020826 00128 WP 2002 8 26 AALA20021061 1 20020626 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 TUL - FOUND SMOOTH DENT IN FUSELAGE APPROX 12 INCHES ABOVE CUSP LINE, APPROX SIX FEET AFT OF FORWARD ENTRY DOOR. INSTAL LED DOUBLER AND REPAIRED PER AARD 53-30-00-9. (M) 2 L 7 2 4F A6WE 2002082600129 20020826 00129 NM 2002 8 26 AALA20021063 1 20020718 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 366AA 25193 MIA - DURING OVERNIGHT MAINTENANCE, FOUND LEFT SIDE EMERGENCY ESCAPE LIGHTS AT ROW 2 THROUGH ROW 8 INOPERATIVE. REPLACE D EMERGENCY ESCAPE LIGHTS AT ROW 2 THROUGH ROW 8 BATTERY PACK AND POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082600130 20020826 00130 NM 2002 8 26 AALA20021064 1 20020718 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 DFW - DURING OVERNIGHT MAINTENANCE, FOUND FRONT COAT CLOSET EMERGENCY LIGHT BROKEN. REPLACED FRONT COAT CLOSET EMERGENC Y LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002082600131 20020826 00131 WP 2002 8 26 DHL2002806852 1 20020705 A 5712 FORMER DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 81567 46002 ITEM N/R 2281 RH WING CTR L/E UPPER FORMER 1/2" CRACKED , STA XFS 316.000CORR: PERFORMED STOP DRILL IAW SRM 57-2-0 PG. 9 -10 FABRICATED DOUBLER WITH 2024T3 AL O.063 IAW SRM57-2-0 PG9-10 , CLEANED , TREATED , AND PRIMED. IAW SRM51-1-8B , INST ALLED DOUBLER ON R/H WING CTR. L/E UPPER FORMER, XFS316.000 IAW SRM 57-2-0 PG. 9-10 2 L 7 4 4F RT 4A25 2002082600132 20020826 00132 WP 2002 8 26 AALA20021065 1 20020719 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 467AA 49597 DFW - DURING OVERNIGHT MAINTENANCE, LEFT OVERHEAD EMERGENCY CEILING EXIT LIGHTS FADE FROM DIM TO INOPERATIVE. REPLACED LEFT OVERHEAD EMERGENCY CEILING EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082600133 20020826 00133 WP 2002 8 26 AALA20021066 1 20020719 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 428AA 49340 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD OVERWING EMERGENCY EXIT LIGHTS ON BOTH SIDES ARE INOPERATIVE. CLEANED FORWA RD OVERWING EMERGENCY EXIT LIGHTS BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M 2 L 7 2 4F A6WE 2002082600134 20020826 00134 WP 2002 8 26 AALA20021067 1 20020719 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 432AA 49350 DFW - DURING OVERNIGHT MAINTENANCE, AFT COMPARTMENT TAIL EXIT DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. SECURED BATTERY W IRE CONNECTIONS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002082600135 20020826 00135 EU 2002 8 26 DHL2002363502 1 20020806 A 5400 A5461025600101 RIB AIRBUS 300 A300B4203 3930306 EU CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 0 85 C-check/#2 pylon rib #22, rib is cracked at lower otb. corner.Corrective action/ reference pg. 2 rib removed & replaced, item #4.Fairing attach structure not required to remove & replace rib # 22 ref. pg. 2 item #4.Removal of angle not requi red for r&r of rib #22. Ref. pg. 2 item # 4. Removed rib # 22 IAW A300 SRM 51-30-30,located & drilled rib #22 IAW A300 S RM 51-30-30,ok to install,installed rib # 22 IAW A300 SRM 51-30-30. 2 L 7 2 4F RT A35EU 2002082600136 20020826 00136 EU 2002 8 26 MALA020502 1 20020811 A 2611 CRAB120101 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU CARGO BAY MALFUNCTIONED A MALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 31XJ 340A031 DURING PUSHBACK OF FLIGHT 3102 CARGO SMOKE. MAINTENANCE REMOVED AND REPLACED CARGO SMOKE DETECTOR PN ON/OFF CRAB1201-01 , SN/OFF 781, SN/ON 1116. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002082600137 20020826 00137 NM 2002 8 26 AWXA200200801 1 20020731 A 5343 654581951 WEB BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A 3/8" CRACK WAS FOUND ON THE NOSE LANDING GEAR ACTUATOR SUPPORT BEAM WEB EXTENDI NG FROM UPPER CENTER RIVET HOLE, HFEC INSPECTION CONFIRMED CRACK. MAINTENANCE REMOVED NOSE LANDING GEAR ACTUATOR SUPPORT BEAM AND WEB, FABRICATED A NEW WEB, AND INSTALLED SUPPORT BEAM AND WEB IAW 737-200 SRM 51-30-2, PG. 8-9, FIG. 7, 11, & 13. 2 L 7 2 4F RT A16WE 2002082600138 20020826 00138 NM 2002 8 26 AWXA200200803 1 20020806 A 5315 6545815 ANGLE BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/2" CRACK WAS FOUND ON TOP OF CABIN FLOOR BEAM SUPPORT ANGLE BS 344, LBL 12, W L 206. MAINTENANCE REMOVED DAMAGED FLOOR BEAM SUPPORT ANGLE BS 344, LBL 12. FABRICATED A NEW FLOOR BEAM SUPPORT ANGLE, AND INSTALLED REPAIR IAW 737-200 SRM 51-30-2, PG. 2-3, AND DWG 65-45815. 2 L 7 2 4F RT A16WE 2002082600139 20020826 00139 NM 2002 8 26 AWXA200200807 1 20020724 A 5230 65C161458 STOP FITTING BOEING 737 737277 1384570 NM GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 0 0 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK THE FORWARD CARGO DOOR BOTTOM AFT DOOR STOP SHOWS EVIDENCE OF WEAR FROM CONTACTIN G DOOR STOP FITTING BOLTS. MAINTENANCE REMOVED DAMAGED FORWARD CARGO DOOR BOTTOM AFT DOOR STOP; FABRICATED A NEW BOTTOM AFT DOOR STOP, AND 2 EACH CLIP ANGLES; AND INSTALLED REPAIR PARTS IAW E.O. 52-30-04. 2 L 7 2 4F RT A16WE 2002082600140 20020826 00140 NM 2002 8 26 AWXA200200810 1 20020806 A 5320 6549649 BRACKET BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 0 0 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND ON THE L-1 DOOR LINER LOWER PAN FORWARD SUPPORT BRACKET AT BS 3 12. MAINTENANCE REMOVED DAMAGED LOWER PAN FORWARD SUPPORT BRACKET AT BS 312, FABRICATED A NEW BRACKET PER DWG 65-49649, AND INSTALLED REPAIR IAW B737-200 SRM 51-30-2, PG. 2. 2 L 7 2 4F RT A16WE 2002082600141 20020826 00141 NM 2002 8 26 AWXA200200812 1 20020723 A 5320 6549649 ATTACH ANGLE BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 0 0 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND ON THE L-1 DOOR LINER LOWER AFT SUPPORT BRACKET ATTACH ANGLE AT BS 344. MAINTENANCE REMOVED DAMAGED LOWER AFT SUPPORT BRACKET ATTACH ANGLE AT BS 344, FABRICATED A NEW ATTACH ANGLE PER DWG 65-49649, AND INSTALLED REPAIR IAW B737-200 SRM 51-10-1, PG. 8. 2 L 7 2 4F RT A16WE 2002082600142 20020826 00142 EU 2002 8 26 DHL2002363508 1 20020806 A 5540 RUDDER AIRBUS 300 A300B4203 3930306 EU DEBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-check/Rudder t/e @ upper end has debonded area on L/H side and material missing (sealant missing) (1 sq. inch) on R/H side.Corrective action/area smoothed an blend IAW A300 SRM 51-4-10. Both areas alodine prepped IAW A300 SRM 51-40-12. Ar ea resealed IAW A300 SRM 51-40-20. Protected all exposed areas IAW A300 SRM 51-40-12. 2 L 7 2 4F RT A35EU 2002082600143 20020826 00143 EU 2002 8 26 DHL2002363509 1 20020802 A 5300 SKIN AIRBUS 300 A300B4203 3930306 EU CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-check/R/H aft upper fuselage ext. skin has areas of corr. @ FR. 80 between STR. 4R to 11RCorrective action/Removed cor r. IAW A300 SRM 51-40-11. UT thickness checked per NTM 51-20-00, minimum remaining1.75 mm before 1.85 mm within limits p er SRM A300 53-10-00. Treated an protected area IAW A300 SRM 51-40-12. 2 L 7 2 4F RT A35EU 2002082600144 20020826 00144 EU 2002 8 26 DHL2002363510 1 20020802 A 5300 SKIN AIRBUS 300 A300B4203 3930306 EU CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-check/R/H aft upper fuselage ext. skin has areas of corr. @ fr80 between STR. 12R to 17R.Corrective action/removed cor rosion IAW A300 SRM 51-40-11. UT thickness checked per NTM 51-20-00 before 2.04 mm minimum after 1.97 mm. Treated an pro tected area IAW A300 SRM 51-40-12. 2 L 7 2 4F RT A35EU 2002082700001 20020827 00001 WP 2002 8 27 DHL2002806854 1 20020718 A 5711 3757850 SKIN PANEL DOUG DC8 DC873F 302199F WP CORRODED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 81567 46002 ITEM N/R 0762 RH WING CTR SPAR SKIN CORRODED AROUND STA. XRS 34.500CORR: PERFORMED MAJOR REPAIR IAW EO DHL020609 ED-3094 , EO SEMAN 2002683 REMOVED CORROSION ON RH WING IAW SRM 51-1-8 PG. 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG. 16 REMO VED FASTNERS IAW SRM 51-1-21 PG. 1 BLENDED OUT DAMAGED SKIN AREA IAW EO DHL020609 , ED-3094 , EO SEMAN 2002683, FABRICAT ED REPAIR DOUBLER 7075T6.125 IAW EO DHL020609 , ED-3094 , EO SEMAN 2002683. CLEANED,TREATED , AND PRIMED AREA IAW SRM 51 -1-8B INSTALLED DOUBLER ON RH WING CTR. SPAR UPPER SKIN , XRS34.5000 IAW EO DHL020609 , ED-3094 , EO SEMAN 2002683. SEE J/C 8-28-12-029M FOR LEAK CK. 2 L 7 4 4F RT 4A25 2002082700003 20020827 00003 NM 2002 8 27 2002F00820 1 20020725 A 3260 161N50211 SPRING BOEING 757 757225 1384959 NM MLG UPLOCK BROKEN A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 618AU 22210 ON APPROACH, WHEN THE GEAR WAS EXTENDED, THE CREW RECEIVED THE EICAS MESSAGE AND THE GEAR AMBER LIGHT ILLUMINATED. CREW RECYCLED THE GEAR. ALL INDICATIONS WERE NORMAL AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A BROKEN UPLOCK ACTUATOR SPRING. 2 L 7 2 4F RT A2NM 2002082700011 20020827 00011 NM 2002 8 27 A6WA200230014 1 20020710 A 5320 FLOOR SUPPORT DORNER DO32 DO328100 2996000 NM FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 340PH 3064 CARGO DOOR SUPPORT FRAME 38 HAS 3 EA CRACK CLIPNUT HOLE THAT MEASURE APPROX. .40 INCH LONG. REPAIRED CARGO FLOORBOARD SUPPORT FRAME 38 CROSSBEAM IAW DO SPR 39507 BY INSTALLING REPAIRED DOUBLERS. 2 H 7 2 4T RT A45NM 2002082700012 20020827 00012 EA 2002 8 27 A6WA200240024 1 20020716 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A A6WA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 424AW 7656 PASSENGER ENTRY DOOR JAMBED CLOSED. MAINTENANCE LUBED LOWER DOOR CAMS AND REPOSITIONED AIRCRAFT TO RELIEVE DOOR FRAME S TRESS. 2 L 7 2 4F RT A21EA 2002082700013 20020827 00013 EA 2002 8 27 A6WA200260033 2 20020717 A 7321 77390020 FUEL CONTROL BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA NR 2 ENGINE MALFUNCTIONED A A6WA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 GL 31 614AW 14985 E3132 LF05467AC NR 2 ENGINE WENT SUB-IDLE ON APPROACH, HUNG AT 39-40 PERCENT NR 2 AND WOULD NOT ACCELERATE. CREW SHUT DOWN ENGINE. MAI NTENANCE REMOVED AND REPLACED FUEL CONTROL. 2 H 7 4 4F 4 F RT A49EU E6NE 2002082700014 20020827 00014 EU 2002 8 27 A832002F00000 1 20020807 A 5610 MY2026610 WINDOW AMD FALC20 FALCON20D5 2730003 EU COCKPIT CRACKED B A83R K NONE O OTHER IN INSP/MAINT 1 SO 17 339TG 9105 198 COCKPIT SIDE WINDOWS WERE REMOVED FOR REPAIR OF CRAZING. AT TIME OF REMOVAL IT WAS FOUND CRACKED 95 PERCENT AROUND OUTE R PANEL ASSEMBLY. CRACKS EXTENDED THROUGH BOLT MOUNTING HOLES. THESE CRACKS CANNOT BE DETECTED WHILE WINDOW IS INSTALL ED DUE TO SPACER INSTALLED BETWEEN PANELS. (AGEING PLASTIC AND CYCLES OF THE PART MAY BECAUSE OF CRACKS. 2 L 7 2 4F RT A7EU 2002082700015 20020827 00015 NM 2002 8 27 AALA20021076 1 20020726 A 4997 CONNECTOR BOEING 767 767323 1385205 NM GE CF6 CF680 30025 NE APU LOOSE A AALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 21 361AA 24042 APU FAULT LIGHT CAME ON AT FL320. ACCOMPLISHED APU FAULT PROCEDURE WITH RESTART AND LIGHT REMAINED ILLUMINATED. RESEAT ED ELECTRICAL CONNECTOR ON APU LOW OIL PRESSURE SWITCH SERVICED APU TO FULL ACCOMPLISHED GROUND CHECKS AND OIL CONSUMPT ION CHECK ALL OK INSPECTED OIL FILTERS AND MAGNETIC CHIP DETECTORS ALL CLEAN APU OK FOR FURTHER SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 2002082700016 20020827 00016 CE 2002 8 27 ACE0155021 1 20020515 A 2701 1185210249 YOKE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE COCKPIT CRACKED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 1553C 30175 UC24 WHILE PERFORMING A SCHEDULED AILERON YOKE INSPECTION. FOUND THE RT AILERON YOKE CRACKED ON ONE SIDE OF THE TAPER PIN HO LE. ALONG THE GRAIN OF THE METAL. 2 L 7 2 4T 4 T RT A24CE E4EA 2002082700017 20020827 00017 CE 2002 8 27 ACE0206021 1 20020206 A 3260 P624003 DOWNLOCK SWITCH AIRIGHT BEECH 1900 1900C 1154161 CE NLG ACTUATOR INOPERATIVE E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 45GL 7023 387 UC45 PILOT REPORTED THAT ON APPROACH TO ANCHORAGE, WHEN THE LANDING GEAR WAS SELECTED DOWN. THE NOSE GEAR, GREEN DOWN AND LO CK LAMP FAILED TO ILLUMINATE (THE GEAR UNSAFE LIGHTS WERE NOT ILLUMINATED). THE GEAR WAS CYCLED AND AFTER A 30 SECOND D ELAY, THE NOSE GEAR DOWN AND LOCK LAMP ILLUMINATED. AN UNEVENTFUL LANDING WAS MADE AND MAINTENANCE REPLACED THE NOSE GE AR ACTUATOR. 2 L 7 2 4T RT A24CE 2002082700018 20020827 00018 CE 2002 8 27 ACE0220021 1 20020220 A 3260 LIGHT BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE MLG INDICATOR BROKEN E YADA O OTHER N FALSE WARNING LD LANDING 1 AL 03 5632C 33350 UC81 UPON LANDING GEAR RETRACTION AFTER TAKEOFF, LANDING GEAR DOWN AND LOCK GREEN LIGHTS REMAINED ILLUMINATED. GEAR WARNING HANDLE LIGHTS CONTINUED TO WORK CORRECTLY. AIRCRAFT MADE UNEVENTFUL LANDING IN ANCHORAGE AND MAINTENANCE REPLACED THE D EFECTIVE LAMP MODULE. 2 L 7 2 4T 4 T RT A24CE E4EA 2002082700019 20020827 00019 CE 2002 8 27 ACE0319021 1 20020320 A 5210 SHAFT BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE PAX DOOR HANDLE SHEARED E YADA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 1566C 6156 UC36 AFTER LANDING, PILOT REPORTED INTERIOR CABIN DOOR HANDLE INOPERATIVE. MAINTENANCE REMOVED THE HANDLE AND FOUND THE DRIV E SHAFT SHEARED. MAINTENANCE REPLACED THE HANDLE ASSEMBLY AND FOUND NO OTHER PROBLEMS. 2 L 7 2 4T 4 T RT A24CE E4EA 2002082700020 20020827 00020 NE 2002 8 27 ACE0425021 2 20020426 A 7314 RA5326 DIAPHRAGM LEARSIEGLER RG37060A BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE FUEL PUMP LEAKING E YADA O OTHER K FLUID LOSS IN INSP/MAINT 1 AL 03 1566C 1364 B107014019 UC36 ON THE RAMP, THE PILOT REPORTED FUEL LEAKING FROM THE INBOARD NR 1 ENGINE DRAIN LINE. MAINTENANCE DISCOVERED THE LOW PR ESSURE FUEL PUMP WAS REPLACED. DISASSEMBLY OF THE PUMP REVEALED THAT THE DIAPHRAGM IN THE PRESSURE ADJUSTING VALVE HAD A HOLE IN IT. FURTHER INSPECTION DETERMINED THAT THE PN RA531 DIAPHRAGM CONTROL PLATE, THAT CONTACTS THE DIAPHRAGM, DID NOT CONFORM TO THE LEAR SIEGLER/ ROMEC PLATE DESIGN DRAWING FOR FINAL FINISH OF THE OUTER CIRCUMFERENCE OF THE PLATE. SHARP EDGES THAT REMAIN ON THIS PLATE HAVE THE CAPACITY TO CAUSE A HIGH RATE OF WEAR ON THE RUBBER DIAPHRAGM, CAUSING EA RLY FAILURE OF THE DIAPHRAGM AND RESULTING IN FUEL LEAKAGE. 2 L 7 2 4T 4 T RT A24CE E4EA 2002082700021 20020827 00021 CE 2002 8 27 ACE0509021 1 20020509 A 3230 1018100903 BOLT BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE MLG LACK OF LUBE E YADA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 5632C UC81 AT CAMP INSPECTION, WHILE PERFORMING A SPECIAL INSPECTION AS DIRECTED BY MFG. FOUND RT MLG DRAG BRACE CENTER BOLT TO B E MISSING GREASE PASSAGES. THIS IS THE EXACT CONDITION THAT REQUIRED THE SPECIAL INSPECTION. REPLACED THE (PN 10181009 03) BOLT WITH A NEW INSPECTED BOLT OF THE SAME PART NUMBER. THIS IS THE FIRST DEFECTIVE BOLT LOCATED OUT OF FOUR INSPEC TED. 2 L 7 2 4T 4 T RT A24CE E4EA 2002082700022 20020827 00022 NM 2002 8 27 373PA0005 1 20020825 A 2910 HYDRAULIC LINE BOEING 737 7373Y0 1384671 NM A PIDA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 05 373PA 23749 After departure, A/C experienced total loss of "A" system hydraulics, both quantity and pressure. A/C diverted, normal landing. Found hydraulic line to uplock actuator on Lt. gear broken. R&R hydraulic line. 2 L 7 2 4F RT A16WE 2002082700023 20020827 00023 CE 2002 8 27 ACE0510021 1 20020510 A 5610 11450432S WINDSHIELD BEECH 1900 1900C 1154161 CE COCKPIT CRACKED E YADA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 45GL 5767 UC45 ON CLIMB OUT, RT WINDSHIELD CRACKED. AIRCRAFT IMMEDIATELY RETURNED TO THE AIRPORT AND MADE AN UNEVENTFUL LANDING. WIND SHIELD REPLACED. 2 L 7 2 4T RT A24CE 2002082700024 20020827 00024 CE 2002 8 27 ACE0515021 1 20020515 A 2710 1185210249 YOKE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE TAPER PIN HOLE CRACKED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 1553C 30175 UC24 WHILE PERFORMING A SCHEDULED AILERON YOKE INSPECTION, FOUND THE RT AILERON YOKE CRACKED ON ONE SIDE OF THE TAPER PIN HOL E. ALONG THE GRAIN OF THE METAL. THIS COMPONENT WAS INSPECTED AT LEAST ONCE WITHIN THE PREVIOUS 2000 FLIGHT HOURS. 2 L 7 2 4T 4 T RT A24CE E4EA 2002082700025 20020827 00025 EU 2002 8 27 BMAC020005 1 20020614 A 5280 137581C DOOR BAG JETSTM JETSTM3101 1500215 EU NLG ANIMAL STRIKE A B16A O OTHER F FLT CONT AFFECTED LD LANDING 1 NE 05 536PA 681 NOSE LANDING GEAR CENTER DOOR DAMAGED DUE TO DEER STRIKE ON LANDING JUST AFTER TOUCHDOWN. REPLACED NOSE LANDING GEAR CE NTER DOOR. COMPLIED WITH ANIMAL STRIKE INSPECTION, NOSE GEAR CENTER DOOR WAS ONLY DAMAGE NOTED. COMPLIED WITH NOSE LA NDING GEAR SWING. RT OF GEAR DOOR INSTALLATION AND SWING. 2 L 7 2 4T RT A21EU 2002082700026 20020827 00026 EU 2002 8 27 BMAC020009 1 20020723 A 3310 LTS2A RHEOSTAT BAG JETSTM JETSTM3101 1500215 EU CABIN LIGHT FAILED A B16A D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NE 05 529PA 771 BRIEF FAINT ODOR OF SMOKE IN COCKPIT OR STRANGE ODOR ON TAXI. VISUALLY INSPECTED STA 130. FORWARD AVIONICS, PERFORMED LT & RT ENGINE RUN COMPLIED WITH. NO DAMAGED OR DEFECTIVE WIRING FOUND. NO SMOKE DETECTED. PROBLEM COULD NOT BE DUPLI CATED. THE ROOF PANEL BACK LIGHTING WAS FOUND INOPERATIVE BY PILOT REPORT. THE LIGHT DIMMER SUPPLY WAS REMOVED AND REP LACED. IAW MM AND THE OPERATIONAL CHECK WAS GOOD. IT IS BELIEVED THAT THIS FAILED PART WAS THE CAUSE OF THE BRIEF SMEL L OF SMOKE/WEIRD SMELL NOTED ON 07/23/2002. NO ADDITIONAL OCCURRANCE HAVE BEEN REPORTED. 2 L 7 2 4T RT A21EU 2002082700027 20020827 00027 2002 8 27 BMAC020010 4 20020729 A 3197 WIRE BAG JETSTM JETSTM3101 1500215 EU COCKPIT BROKEN A B16A C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NE 05 538PA 751 ON TAKE OFF ROLL, RT ENGINE POWER WAS SET TO 90 PERCENT TORQUE. AS POWER WAS BEING ADVANCED TO CHARTED TAKE OFF TORQUE, THE RT TORQUE CAME BACK TO 80 PERCENT TO 85 PERCENT TORQUE. ALL OTHER INDICATIONS NORMAL. REPAIRED BROKEN WIRE COMING FROM NR 2 SRL, COMPUTER CONNECTOR PLUG BACK SHELL IAW WDM. OPS CHECK GOOD ON STATIC AND HIGH SPEED RUN UP IAW MM. 2 L 7 2 4T RT A21EU 2002082700028 20020827 00028 EA 2002 8 27 BSY2002F00014 2 20020809 A 7310 MS295128 O-RING PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA NR 2 ENGINE FAILED E BSYA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 525AA 318052111 AIRCRAFT ABORTED TAKE OFF BECAUSE LT ENGINE 200 RPM LOW. FOUND O-RINGS ON LEFT FUEL MANIFOLD IN WING ROOT SUCKING AIR, REMOVED AND REPLACED O-RINGS. OPS GOOD. 1 L 7 2 3O 3 O A20SO E14EA 2002082700029 20020827 00029 2002 8 27 BSY2002F00015 4 20020809 A 3197 CONNECTOR PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA INSTRUMENT PANEL LOOSE E BSYA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 4UE 318152061 LT GEAR DOWN AND LOCK INTERMITTENT. FOUND CONNECTOR LOOSE IN INSTRUMENT PANEL, TIGHTENED CONNECTOR. CYCLED GEAR SEVERA L TIMES. OPS CHECKED GOOD. 1 L 7 2 3O 3 O A20SO E14EA 2002082700030 20020827 00030 CE 2002 8 27 BSY2002F00016 1 20020809 A 5230 LATCH CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE CARGO DOOR FAILED E BSYA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 242CS 208B0239 PCE19112 TOP AFT CARGO DOOR CAME OPEN AFTER TAKEOFF. REBUILT UPPER CABIN LATCH ASSEMBLY OPS CHECK GOOD. 1 H 7 1 3T 3 T A37CE E4EA 2002082700031 20020827 00031 EA 2002 8 27 BSY2002F00017 2 20020809 A 8550 HOSE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA RT ENGINE LOOSE E BSYA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 35871 318052123 RL199468A RT ENGINE SURGING ON TAKEOFF RETURNED TO AIRPORT. FOUND UPPER DECK HOSE LOOSE AT TURBO DISCHARGE HOUSING. TIGHTENED HO SE. RUN UP, OK. 1 L 7 2 3O 3 O A20SO E14EA 2002082700032 20020827 00032 2002 8 27 BSY2002F00018 4 20020809 A 2563 660018 DRAG CHUTE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP AFT DEPLOYED E BSYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 81FR 081 ON CLIMB OUT, AT 15,000 FEET, DRAG CHUTE DEPLOYED AND SEPARATED FROM AIRCRAFT. INSTALLED DOOR AND DRAG CHUTE. OPS CHEC KED GOOD. CAUSE FOR DEPLOYMENT UNKNOWN AT THIS TIME. 2 L 7 2 4F 4 F A10CE E6WE 2002082700033 20020827 00033 CE 2002 8 27 BSY2002F00019 1 20020814 A 3230 SWITCH BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO MLG BENT E BSYA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 58TA TH596 LANDING GEAR WOULD NOT EXTEND EITHER ELECTRICALLY OR MANUALLY, FEATHERED ENGINES AND LANDED GEAR UP. FOUND UP LIMIT SWI TCH ACTUATING TAB BENT, NOT ALLOWING TAB TO HIT. UP LIMIT SWITCH GEAR BOX WENT PAT UP LIMITS. JAMMING GEAR BOX, COULD NOT CRANK GEAR DOWN. CAUSE UNKNOWN AT THIS TIME. WHY TAB WAS BENT. 1 L 7 2 3O 3 O 3A16 E5CE 2002082700034 20020827 00034 WP 2002 8 27 COOSDR020223 1 20020801 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 602AL 45991 LOWER FUSELAGE AT STA Y798 CRACKED FITTING. 2 L 7 4 4F RT 4A25 2002082700035 20020827 00035 WP 2002 8 27 COOSDR020224 1 20020801 A 5740 STIFFENER DOUG DC8 DC873F 302199F WP LT WING CRACKED B EE4Y K NONE O OTHER IN INSP/MAINT 1 SO 23 602AL 45991 LEFT WING TRAILING EDGE AREA AT XRS407.000 CRACKED STIFFENER. 2 L 7 4 4F RT 4A25 2002082700036 20020827 00036 GL 2002 8 27 EGR2002F00006 2 20020718 A 7261 CHIP DETECTOR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 ENGINE ILLUMINATED E EGRA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 17 3122G 760232 CAE8906345 ENROUTE, AT 2000 FEET, NR 2 ENGINE CHIP LIGHT ILLUMINATED COMPLIED WITH ENGINE CHECK LIST, LANDED AT EMERGENCY AIRPORT. REMOVED FORWARD AND AFT CHIP PLUGS, FOUND 2 SMALL FLAKES ON FORWARD PLUG, AFT PLUG FOUND 1 SMALL HAIR. CLEANED PLUGS AND INSTALLED. REMOVED INTERNAL OIL FILTER, INSPECTED AND INSTALLED SAME. DRAINED AND RESERVICED NR 2 ENGINE OIL . GR OUND RUN AIRCRAFT FRO 30 MINUTES, LIGHT STAYED OUT. 1 G 7 2 3U 3 U H1NE E1GL 2002082700037 20020827 00037 SO 2002 8 27 ENH2002F00000 1 20020726 A 2913 BUSHING PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA HYD PUMP WORN E ENHA K NONE O OTHER IN INSP/MAINT 1 AL 03 77HV 125 318152193 REMOVED FOR LOW PRESURE OUTPUT. DISASSEMBLY SHOWS DRIVEN GEAR SHAFT BUSHINGS WORN EXCESSIVELY. 1 L 7 2 3O 3 O A20SO E14EA 2002082700038 20020827 00038 NM 2002 8 27 FX72002F00002 1 20020711 A 3230 69553479 LINK BOEING 727 727231 1384079 NM PWA JT8 JT8D217 52053 NE MLG INOPERATIVE A FX7A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 54348 21967 AFTER TAKEOFF, GEAR HANDLE WOULD NOT MOVE BEYOND OFF POSITION AIRCRAFT RETURNED TO AIRPORT, REMOVED AND REPLACED THE GRO UND SHIFT LINK IN LEFT WHEEL WELL PER MM. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E9NE 2002082700039 20020827 00039 CE 2002 8 27 IBU2002F00000 1 20020802 A 3510 510010937 LINE CESSNA 421 421C 2076016 CE OXYGEN SYSTEM CHAFED E IBUA K NONE O OTHER IN INSP/MAINT 1 WP 07 763CA 421C1019 OXYGEN SUPPLY LINE WAS FOUND TO HAVE A HOLE RUBBED INTO IT FROM RAM AIR DUCT (THE DUCT SUPPORT COIL). A VISUAL INSPECTI ON OF THE AREA, WHEN ON GROUND, APPEARS TO HAVE CLEARANCE. BUT OUT BELIEF IS THAT IN THE AIR WITH RAM AIR COMING IN IT BOTH EXPANDS AND MOVES THE DUCT TO RUB THE OXYGEN LINE. 1 L 7 2 3O A7CE 2002082700040 20020827 00040 NM 2002 8 27 KPVA200216 1 20020808 A 3350 CONNECTOR DHAV DHC8 DHC8103 1386005 NM COCKPIT DAMAGED A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808WP 026 COCKPIT EMERGENCY LIGHT WILL NOT COME ON WHEN SELECTED (ON). STRAIGHTENED BENT CONTACT ON CONNECTOR AND OPS CHECK OF EM ERGENCY LIGHTS SYSTEM GOOD IAW MM. 2 H 7 2 4T RT A13NM 2002082700041 20020827 00041 WP 2002 8 27 ABXA020094 1 20020627 A 5300 LONGERON DOUG DC8 DC863 302198A WP FS 36 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 AIR COND/PRESS COMPARTMENT AT FS 36, LONGERON 31 RIGHT, AT OUTBOARD SIDE WAS CORRODED AROUND FASTENERS. FABRICATED REPAI R STRAP AND REPAIRED AREA IAW REA D853-43733-MR, SRM 53-2-0, 51-1-8, 51-1-20D. 2 L 7 4 4F 4A25 2002082700042 20020827 00042 WP 2002 8 27 ABXA020095 1 20020705 A 5315 FLOORBEAM DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 AFT CARGO AT STA. 1300, RBL 16, FLOORBEAM WAS CORRODED. FABRICATED NEW REPAIR PARTS AND FLOORBEAM IAW ABX REA D853-43926 -MR, 51-1-8, 53-2-0, 51-1-20D, 51-3-0, AND 51-1-21. 2 L 7 4 4F 4A25 2002082700043 20020827 00043 WP 2002 8 27 ABXA020097 1 20020708 A 5300 WEB DOUG DC8 DC863 302198A WP FS 960 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 MAIN CABIN STATION 960, CORROSION UNDER BEAM AND SHEAR WEB BY LEFT BUTT LINE 68. REPAIRED AREA IAW ABX REA D853-43930-MR . 2 L 7 4 4F 4A25 2002082700044 20020827 00044 WP 2002 8 27 ABXA020100 1 20020708 A 5300 BEAM DOUG DC8 DC863 302198A WP STA. 940 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 MAIN CABIN STATION 940, RIGHT BUTT LINE 68, CORROSION UNDER BEAM AND SHEAR WEB PANEL, LOWER SIDE CORNER. REPAIRED AREA I AW REA D853-43931-MR. 2 L 7 4 4F 4A25 2002082700045 20020827 00045 NM 2002 8 27 KPVA200218 1 20020810 A 5260 NAS5625R16 CAM FOLLOWER DHAV DHC8 DHC8103 1386005 NM AIRSTAIR DOOR DAMAGED A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 806WP 357 A LOUD BINDING & GRINDING IN AIRSTAIR DOOR WHEN OPENING OR CLOSING. INSTALLED CAM FOLLOWER ON FORWARD HANDRAIL UPPER AS SEMBLY. OPS CHECK GOOD, NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2002082700046 20020827 00046 NM 2002 8 27 MAS2002F00008 1 20020406 A 6123 454215B653323 SWITCH DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER FAILED A MASA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 456YV 456 RETURNED TO THE GATE DUE TO THE AUTOFEATHER SWITCH (SELECT) WOULD NOT MECHANICALLY ENGAGE. MECHANIC WAS CALLED AND REPL ACED THE AUTOFEATHER SWITCH, OPS CHECK GOOD AND WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002082700047 20020827 00047 2002 8 27 MEX2002256 4 20020508 A 3418 106010 SWITCH DOUG DC9 DC982 3022082 WP STALL COMPUTER FAILED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 491SH 49150 AIRCRAFT RETURNED TO PLATFORM AS DUE TO AUTO SLAT FAIL LIGHT, THE STALL COMPUTER WAS REPLACED AND FAILURE CONTINUED, THE CONNECTORS OF STALL COMPUTER WERE CLEANED AND BOTH ACTUATOR CONNECTORS WERE RESEATED, TESTS WERE PERFORMED OK. DURING TAXI THE SAME LIGHT ILLUMINATED. THE ACTURATORS WERE FOUND WITH EXCESSIVE GREASE IN SLAT DRUM CAUSING FAILURE. SENSOR S D1-55 AND D1-56 IN THE DRUM WERE CLEANED. SYSTEM WORKING CORRECTLY. 2 L 7 2 4F A6WE 2002082700048 20020827 00048 NM 2002 8 27 NOM2002F00000 1 20020807 A 3232 69141019 ACTUATOR BOEING 727 727200RE 1384071 NM RT MLG DOOR FAILED I NOMB A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 727M 27530 22541 AFTER TAKE OFF, AMBER DOOR WARNING LIGHT ON CENTER PANEL AND RIGHT MAIN LANDING GEAR DOOR WARNING F/E PANEL REMAINED ON. RECYCLED GEAR AND ALL LIGHTS OUT AND OPS NORMAL. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR ACTUATOR IAW MM. OPS NORMAL. 2 L 7 3 3F RT A3WE 2002082700049 20020827 00049 SO 2002 8 27 SIMA200222105 1 20020802 A 5522 SKIN EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007C GL LT ELEVATOR DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 733KR 145368 DURING INSPECTION FOUND DAMAGE ON THE LOWER LT ELEVATOR SKIN. PERFORMED TWO CUSTS TO REMOVE DAMAGE. FABRICATED A REPAI R DOUBLER. REPAIR DONE IAW STATEMENT AND SRM PRACTICES. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002082700050 20020827 00050 SO 2002 8 27 SIMA200222106 1 20020809 A 5330 ALCLAD2024T3 SKIN EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 734EK 145371 DURING INSPECTION, FOUND CORROSION ON LT OMEGA BEAM AT FRAME 20. CUT OUT CORRODED AREA AND FABRICATED DOUBLER ANGLE AND FILLER AND PLATE AND TWO SHIMS. REPAIR DONE IAW SRM PRACTICES. 2 L 7 2 4F RT T00011AT 2002082700051 20020827 00051 SO 2002 8 27 SIMA200222108 1 20020805 A 5321 14500222001 FLOORBOARD EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 734EK 145371 THIS IS A LEVEL TWO FINDING ON CRIC NR 23858. GALLEY AREA FLOORBOARD EXTENSIONS HAVE CORROSION. GALLEY AREA FLOORBOARD EXTENSIONS HAVE CORROSION. REMOVED AND INSTALLED EXTENSION IAW SRM. 2 L 7 2 4F RT T00011AT 2002082800083 20020828 00083 2002 8 28 TSAA0225160 4 20020711 A 2565 D31355427 SLIDE BOEING 737 73725A 1384481 NM PWA JT8 JT8D17 52049 NE CABIN DEFECTIVE A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 DURING A ROUTINE TRAINING EXERCISE AND AFTER SUCCESSFUL SLIDE DEPLOYMENT, THE SLIDE ASSEMBLY EXPLODED AT THE SEAM. NO H ARM TO PERSONNEL. REMOVED AND REPLACED SLIDE; CONTINUED WITH EXERCISE. SLIDE SENT TO VENDOR FOR EVALUATION. 2 L 7 2 4F 4 F RT A16WE E2EA 2002082700052 20020827 00052 NM 2002 8 27 TSAA0231174 1 20020811 A 3150 4081600930 DISPLAY BOEING 737 73773A 1384606 NM COCKPIT FAILED A TSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 739AL 28500 DURING CLIMB TO CRUISE ALTITUDE THE ALTIMETER INDICATION, SPEED INDICATION, FLIGHT MODE ANNUNCIATOR, VOR 1, AND DME 1 AN NUNCIATOR FLAGS ILLUMINATED ON THE FIRST OFFICERS DISPLAY UNIT. BOTH ENGINES NR 1 AND NR 2 EEC LIGHT ILLUMINATED. AIRC RAFT DIVERTED AND LANDED IN HNL WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 DISPLAY ELECTRONICS UNIT. THE OPC SOFTWARE WAS LOADED AND BITE CHECKS WERE COMPLETED IAW MM. OVERWEIGHT LANDING INSPECTION WAS ACCOMPLISHED AND THE A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002082700053 20020827 00053 NE 2002 8 27 TSAA0271172 2 20020811 A 7200 LINE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D* NE NR 1 ENGINE OBSTRUCTED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 817AL 23292 DURING CLIMB THE NR 1 ENGINE EGT INDICATED 600 DEGREES C WITH THRUST LEVER 4 INCHES AHEAD OF THE NR 2 ENGINE THRUST LEVE R. THE NR 1 ENGINE EPR WAS 1.73 AND THE NR 2 ENGINE EPR WAS 1.83. THE FLIGHT RETURNED AND LANDED WITH NO FURTHER INCID ENT. (ETOPS A/C ON NON ETOPS FLIGHT) MAINTENANCE INSPECTED THE NR 1 ENGINE AND REMOVED AN OBSTRUCTION IN THE PT2. POWER ASSURANCE CHECK WAS COMPLETED AT BOTH TAKEOFF AND CLIMB POWER SETTINGS. NO DEFECTS WERE NOTED AND THE AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002082700054 20020827 00054 NM 2002 8 27 TSAA0277173 1 20020811 A 7711 LG80A6 TRANSMITTER BOEING 737 737200 1384453 NM NR 1 ENGINE INOPERATIVE A TSAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 13 817AL 23292 NR 1 ENGINE EPR DROPPED OFF ON CLIMB OUT OF 7,000 FEET. NR 1 ENGINE EPR WAS 1.73 AND NR 2 ENGINE EPR WAS 1.85. BOTH TH E NR 1 AND NR 2 ENGINES NR 1 WAS 89 PERCENT AND NR 2 WAS 92 PERCENT. THE AIRCRAFT RETURNED AND LANDED IN HNL WITH NO FU RTHER INCIDENT. (ETOPS A/C OR NON ETOPS FLIGHT) MAINTENANCE INSPECTED THE NR 1 ENGINE AND PURGED THE PT2 AND PT7 LINES . THE NR 1 ENGINE EPR TRANSMITTER WAS REPLACED IAW MM. A HIGH POWER RUN AND POWER ASSURANCE CHECK WAS COMPLETED ON THE NR 1 ENGINE. NO DISCREPANCIES WERE NOTED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A16WE 2002082700055 20020827 00055 SO 2002 8 27 UG82002F00006 1 20020802 A 3150 7013348924 DAU GULSTM GV GULFSTREAMGV 3980116 SO CHANNEL 1A FAILED A UG8A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 5102 551 FAIL AMBER LIGHT CAME ON DURING CLIMB OUT AT 12,000 FEET. DAU 1A CHANNEL FAILURE. NEEDS FURTHER TROUBLESHOOTING. (REP ORT NR G02-32) 2 L 7 2 4F RT A12EA 2002082700056 20020827 00056 EU 2002 8 27 UO22002F00015 1 20020731 A 5230 FGFB295001462A2 SLEEVE AMD FALC90 FALCON900EX 2730009 EU CARGO DOOR WORN B UO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 8100E 04 UPON INSPECTION DURING C CHECK, FOUND THAT HINGE SLEEVE WAS WORN ALMOST COMPLETELY THROUGH IF THIS PART FAILS, THE MED W ILL NO LONGER BE COUNTER BALANCED AND COULD OPEN WITH GREAT FORCE AND CAUSE INJURY AND DAMAGE. CAUSE IS FROM ALL OF THE LOAD OF THE DOOR BEING ON THIS ONE SLEEVE. 2 L 7 3 4F RT A46EU 2002082700057 20020827 00057 NM 2002 8 27 USA2002F00069 1 20020718 A 5230 10608211 SEAL BOEING 737 737401 1384701 NM CARGO DOOR OUT OF POSITION A USAA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 417US 23984 ENROUTE, THE CABIN ALTITUDE BEGAN TO CLIMB. PRESSURIZATION SYSTEM AUTO FAILED TO STANDBY MODE WITH NO HELP AND CREW WAS UNABLE TO CONTROL CABIN IN MANUAL MODE. CREW DECLARED AN EMERGENCY AND QUICKLY DECENDED. CAPTAIN MANUALLY DEPLOYED TH E OXYGEN MASKS TO ENSURE THAT OXYGEN WAS AVAILABLE TO THE PASSENGERS. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDE NT. MAINTENANCE FOUND 18 INCHES OF THE FORWARD CARGO DOOR SEAL OUT OF POSITION AT THE AFT EDGE OF DOOR. REPOSITIONED D OOR SEAL AND PERFORMED SATISFACTORY PRESSURIZATION LEAK CHECK IAW MM. REPLACED ALL OXYGEN MASKS AND OXYGEN GENERATORS. FORWARD CARGO DOOR SEAL HAS BEEN PROGRAMMED FOR REPLACEMENT. 2 L 7 2 4F RT A16WE 2002082700058 20020827 00058 NM 2002 8 27 USA2002F00070 1 20020722 A 5210 CONTROL ROD BOEING 737 737401 1384701 NM PAX DOOR OUT OF ADJUST A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 412US 23881 AFTER TAKEOFF, ENROUTE, CABIN PRESSURE BEGAN TO CLIMB WITH ALTITUDE. FLIGHT WAS LEVELED OFF AT 2500 FEET WHEN A FLIGHT ATTENDANT REPORTED THAT THE AFT ENTRY DOOR HAD POPPED OPEN. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDEN T. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE AFT ENTRY DOOR CONTROL ROD OUT OF ADJUSTMENT. ADJUSTED CONTROL RO D AND RESENT DOOR LOCKING PRESSURE. OPERATIONAL CHECK OF DOOR GOOD. 2 L 7 2 4F RT A16WE 2002082700059 20020827 00059 NM 2002 8 27 USA2002F00071 1 20020723 A 3260 CIRCUIT BREAKER BOEING 737 7373B7 1384580 NM MLG TRIPPED A USAA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 EA 19 517AU 23703 ON DESCENT, CREW DID NOT RECEIVE THREE GREEN LANDING GEAR LIGHTS WHEN LOWERING THE LANDING GEAR. CREW ACCOMPLISHED GO-A ROUND, AND WHILE PERFORMING CHECKLIST, THEY FOUND THE SECTION 5 CIRCUIT BREAKER POPPED. CREW RESET CIRCUIT BREAKER AND RECEIVED NORMAL GEAR INDICATION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. CREW REPORTED TO MAINTENANCE THAT THE FIRST OFFICERS SHOULDER HARNESS PROBABLY GOT HOOKED ON THE CIRCUIT BREAKER CAUSING IT TO POP. MAIN TENANCE CHECKED ALL LANDING GEAR POSITIONS SENSORS AS PRECAUTIONARY. ALL SENSORS CHECKED GOOD. AIRCRAFT OK FOR SERVIC E. 2 L 7 2 4F RT A16WE 2002082700060 20020827 00060 NM 2002 8 27 USA2002F00072 1 20020730 A 2612 659401 MODULE BOEING 737 7373B7 1384580 NM FIRE CONTROL FAULTY A USAA O OTHER N FALSE WARNING DE DESCENT 1 EA 19 371US 38915 22950 ON DESCENT, THE FIRE WARNING ANNUNCIATOR ON THE GLARESHIELD ILLUMINATED. CREW COULD NOT CANCEL THE LIGHT. NO OTHER IND ICATIONS OF FIRE WAS NOTED. FIRE DETECTION TESTS NORMAL OTHERWISE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANC E REMOVED AND REPLACED THE FIRE CONTROL MODULE. SYSTEM TESTS NORMAL IN COCKPIT AND E & E COMPARTMENT. 2 L 7 2 4F RT A16WE 2002082700061 20020827 00061 NM 2002 8 27 USA2002F00073 1 20020719 A 3810 8921082G5 WATER HEATER BOEING 737 7373B7 1384580 NM AFT RT LAVATORY OVERHEATED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 525AU 8700 23860 ENROUTE, FLIGHT ATTENDANT REPORTED A SLIGHT ELECTRICAL ODOR IN THE AFT GALLEY AREA THAT TENDED TO BE INTERMITTENT. ODOR DISSIPATED DURING FLIGHT. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED THE AFT GALLEY AR EA INCLUDING CONNECTOR PLUGS FOR BOTH AFT COFFEEMAKERS. NO DEFECTS NOTED. FOUND THE AFT RIGHT LAVATORY WATER HEATER OV ERHEAT TRIPPED. REMOVED AND REPLACED AFT RIGHT LAVATORY WATER HEATER. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2002082700062 20020827 00062 NM 2002 8 27 USA2002F00074 1 20020802 A 3234 HANDLE BOEING 737 7373B7 1384580 NM MLG HANDLE LACK OF LUBE A USAA O OTHER O OTHER AP APPROACH 1 EA 19 384US 22957 ON APPROACH, CREW RECEIVED A GEAR INDICATION OF 3 RED UNSAFE LIGHTS ALONG WITH 3 GREEN DOWN AND LOCKED LIGHTS WHEN FLAPS 30 WAS SELECTED. THE (TOO LOW, GEAR) WARNING SOUNDED SEVERAL TIMES UNTIL AFTER THE GEAR WAS RETRACTED DURING GO AROUND . CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND DROPPED THE GEAR FOR INSP. SYSTEM OPERATED NORMAL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LANDING GEAR POSITION HANDLE STICKING OUT (NOT FULLY RETRACTED) IN THE DOWN POSITION. CLEANED AND LUBRICATED HANDLE AS REQUIRED. CHECKED CONDITION AND WIRING OF THE LEVER POSITION S WITCH. CHECKS OK. OPERATIONAL CHECK OF SWITCH GOOD IAW MM. 2 L 7 2 4F RT A16WE 2002082700063 20020827 00063 CE 2002 8 27 WIB2002F00008 1 20020727 A 2150 66082484 MOTOR LEAR 35 31A 5170531 CE GARRTT TFE731 TFE731* 01518 WP AIR CONDITIONER SHORTED B WIBR K NONE O OTHER IN INSP/MAINT 1 SW 11 261SC 061 AIR CONDITIONER COMPRESSOR DRIVE MOTOR FAILED. FOUND TO BE INTERNALLY BURNED. CURRENT LIMITER DID BLOW. POSSIBLY CAUS ED BY BEARING FAILURE. 2 L 7 2 4F 4 F RT A10CE E6WE 2002082700064 20020827 00064 EU 2002 8 27 Z972002F00000 1 20020520 A 3241 40921 TRANSDUCER ISRAEL 1124 1124A 4500103 EU GARRTT TFE731 TFE731* 01518 WP ANTI SKID SYSTEM FAILED E Z97A O OTHER O OTHER NR NOT REPORTED 1 SW 09 118MP 340 ANTI-SKID TRANSDUCER FAILED (LOCK UP) CAUSING THE MAIN WHEEL BEARING TO HEAT-UP INTURN CAUSED LEFT MAIN WHEEL BEARING FA ILURE CAUSING SEVERE DAMAGE TO AXLE, LOWER FORK, WHEEL HALVES. ALL NEW PARTS INSTALLED. 2 M 7 2 4F 4 F A2SW E6WE 2002082700065 20020827 00065 WP 2002 8 27 ZIA2002F00000 1 20020514 A 2432 GE50C BATTERY LKHEED 188 188A 5262602 WP MAIN DISCHARGED A ZIAA B A EMER. DESCENT UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 GL 23 346HA 188A1043 IN CRUISE, EN-ROUTE, LOST (A) BUS IN FLIGHT. LOST ALL RADIOS BOTH COMMS AND BOTH NAVS. OVERWEIGHT LANDING. RESET ALL MAIN FEEDER C/BS OPS. CHECKED GOOD ON GROUND RUN-UP. REMOVED MAIN AC BATTERY AND REPAIRED BATTERY CONNECTOR, OPS CHECKE D GOOD COMPLIED WITH ONE -119C, NO DEFECTS NOTED. 2 L 7 4 4T RT 4A22 2002082700069 20020827 00069 EU 2002 8 27 DHL2002363511 1 20020808 A 5300 SKIN AIRBUS 300 A300B4203 3930306 EU CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-check/Sta.1380 STR. 48L interior of skin has 3 SQ" of moderate corrosion.Corrective action/ Smoothed an blended area o f corrosion IAW A300 SRM 51-40-11. Material removed is .022" max allowable material loss is .047" area within limits IAW A300 SRM 53-12-00 Fig. 605 pg. 611. Treated an primed area IAW A300 SRM 51-40-12. 2 L 7 2 4F RT A35EU 2002082700070 20020827 00070 SO 2002 8 27 000187 1 20020806 A 5270 SWITCH EMB 145 EMB145 3260210 SO CARGO DOOR DIRTY A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 277 CARGO DOOR SHOWS OPEN ON EICAS. NO LOSS OF PRESSURIZATION. CLEANED CARGO DOOR SWITCHES. 2 L 7 2 4F RT T00011AT 2002082700071 20020827 00071 NE 2002 8 27 02070901 2 20020709 A 7532 C8E389 CONTROL UNIT BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E4 54555 NE BLEED VALVE MALFUNCTIONED A N8TA D RETURN TO BLOCK Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 WP 19 526NA 24794 30746 AFTER DISCONNECT, BEGAN TO TAXI, HEARD MUFFLED POPPING NOISE. LEFT ENGINE QUIT. RETURNED TO GATE. BVCU BITE FAILED, BV CU REMOVED AND REPLACED. FUNCTIONAL CHECK GOOD AS PER M/M. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002082700072 20020827 00072 NE 2002 8 27 02080601 2 20020805 A 7530 C8E3812 CONTROL UNIT BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE NR 2 ENGINE INOPERATIVE A N8TA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 WP 19 517NA 66 24260 30677 AT 16000 FEET, COMPRESSOR STALL; AT 14000 FEET, 3 BANGS, AT 10000 FEET, NO BANGS, AT 7000 FEET, NO RESPONSE IN RT ENGIN E UPON POWER UP, AT 7000 FEET, OIL PRESSURE LOSS INDICATED (2PSI) AT 7000 FEET, LOSS RT. ENG. IDG, SHUTDOWN RT ENGINE. AIRCRAFT CONTINUED DESCENT TO DESTINATION, AN UNEVENTFUL LANDING WAS ACCOMPLISHED. BORESCOPED ENGINE NO DEFECTS NOTED, REPLACED BVCU(BLEED VALVE CONTROL UNIT) AS PER M/M., FOUND ORIGINAL UNRESPONSIVE. PERFORMED ENGINE RUN TEST 3 AND TEST 4 AS PER M/M, RIGHT ENGINE OPS CHECK GOOD, NO DEFECTS NOTED, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002082700073 20020827 00073 NM 2002 8 27 02215404 1 20020803 A 2120 ODOR DORNER DO32 DO328300 NM COCKPIT DETECTED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 404FJ 3150 DURING CLIMB, THE CREW REPORTED THAT THEY WERE EXPERIENCING (HAZE AND FUMES) IN THE CABIN. THE FLIGHT RETURNED TO CAE A ND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL FOUND THAT THE FUMES WERE CAUSED BY RESIDUAL ENGINE COMPRESSO R WASH FLUID. THE ENGINES WERE RUN WITH THE BLEEDS OPEN FOR THIRTY MINUTES. NO SMOKE OR HAZE WAS NOTED AND THE FUMES D ISSIPATED AFTER APPROXIMATELY. FIFTEEN MINUTES. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002082700074 20020827 00074 EU 2002 8 27 02219317 1 20020207 A 3030 PH1001BJ PITOT HEAD JETAIR JETSTM JETSTM4101 1500501 EU NR 2 INOPERATIVE A VTZA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 27 317UE 41031 DURING DESCENT, THE CREW REPORTED A STRONG ODOR AND THE P2 CAPTION ILLUMINATED. THE CREW COMPLETED THE QRH PROCEDURES, DECLARED AN EMERGENCY, AND TURNED OFF THE AIR CONDITIONERS AND FLOWS. THE APPROACH AND LANDING WERE COMPLETED WITHOUT F URTHER INCIDENT. MAINTENANCE PERSONNEL FOUND BURNED WIRING TO THE NR 2 PITOT HEAD. THE WIRING WAS REPAIRED AND THE NR 2 PITOT HEAD AND CURRENT SENSOR WERE REMOVED AND REPLACED. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS R ETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002082700075 20020827 00075 NM 2002 8 27 02FDEA00513 1 20020723 A 7930 OIL FILTER BOEING 727 727100 1384036 NM NR 1 ENGINE DAMAGED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 107FE 19202 NR 1 ENGINE, HIGH OIL TEMP (OFF SCALE HIGH) FOUND BAD CONNECTION AT OIL TEMP SENSOR. PER CREW INFO WINDMILLING WAS LESS THAN 30 MIN. FOUND BROKEN WIRE AT C/P ON NR 1 ENG OIL TEMP BULB. REMOVED AND REPLACED C/P D530 IAW SWPM. PERFORMED E NGINE WINDMILLING INSPECTION IAW M/M. NO DEFECTS FOUND. REPLACED NR 1 ENGINE MAIN OIL FILTER P/N AC-9806F-65, LEAK CK S GOOD. NR 1 ENG OIL TEMPERATURE INDICATOR, OPS CHECK GOOD IAW JRH. 2 L 7 3 4F RT A3WE 2002082700076 20020827 00076 NM 2002 8 27 UIEA200200025 1 20020717 A 5414 65B9405314 SKIN BOEING 747 747230B 1384889 NM PYLON WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 88570 21644 DURING CURRENT (C) CHECK, INSPECTION OF NR 3 PYLON ACCESS PLATE (473AR) CUTOUT, FOUND HEAVY WEAR AT ONE OF THE LATCH POS ITIONS. WEAR AREA TRIMMED AWAY FROM SKIN AND DOUBLER. DOOR ACCESS SIZE INCREASED ON RETAINING LIP. FABRICATED REPAIR DOUBLER AND FILLERS. ALL HOLES AND ACCESS CUTOUT NDT INSPECTED FOR CRACKS. NO CRACKS FOUND. SKIN AND REAIR FILLERS BO NDED TO EXISTING STRUCTURE PER SRM. NR 1 FASTENERS INSTALLED IAW SRM. AREA SEALED IAW SRM WITH BMS SEALANT. 2 L 7 4 4F A20WE 2002082700077 20020827 00077 NM 2002 8 27 AALA20021068 1 20020720 A 3350 LIGHT BOEING 757 757223 1384957 NM FUSELAGE DEPARTED A AALA A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 SW 21 637AM 24595 DFW - FLT 2075 - EN ROUTE MCO-DFW, EMERGENCY EXIT LIGHT FOR L-3 DOOR FELL OFF IN FLIGHT. AIRCRAFT LANDED IN DFW WITHOUT INCIDENT. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002082700078 20020827 00078 EU 2002 8 27 DHL2002363513 1 20020806 A 3213 C6538710 AXLE AIRBUS 300 A300B4203 3930306 EU GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-check/#8 axle has worn nickel plating and gouged.Corrective action/Smooth an blended out area to a .2 mm radius in ref . to repair approval sheet from Messier-Dowty OE-085-08-02-003,NDT inspected per CMM 32-09-01 section 42 no cracks found . See NDT report see page 2. Cadmium plated reworked surface IAW CMM 32-09-01. 2 L 7 2 4F RT A35EU 2002082700079 20020827 00079 EU 2002 8 27 DHL2002366008 1 20020625 A 2612 RELAY AIRBUS 300 A300B4203 3930306 EU FIRE DETECTION FAILED A DHLA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 01 366DH 249 THE ENG 1 LOOP LIGHT ILLUMINATED WITH A SINGLE SOUND CHIME (SSC) AND THE LOOP LT ON THE MWP. AFTER 30 SEC THE LIGHT WEN T OUT. A NORMAL TEST OF THE SYSTEM YIELDED A SSC AND THE LOOPS LIGHT ON THE MWP, BUT THE ENGINE 1 LOOP LIGHT WOULD NOT ILLUMINATE. LOOP-B WAS SELECTED AND A SUCCESSFUL TEST WAS PERFORMED. REMOVED AND REPLACED A-LOOP TEST RELAY 31WD. TES TED NR 1 AND NR 2 A-LOOPS AS PER MM 26-12-00. BOTH CHECKED GOOD. 2 L 7 2 4F RT A35EU 2002082700080 20020827 00080 NE 2002 8 27 DHL2002367008 2 20020821 A 7200 ENGINE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 1 MALFUNCTIONED A DHLA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 01 367DH 265 517513QEC AS THROTTLES WERE ADVANCED FOR TAKEOFF WITH THROTTLE POSITION EQUAL, ENGINE NR 1 N1 HUNG BACK AT 20 PERCENT WITH ENG NR 2 AT 70 PERCENT. UNABLE TO MAINTAIN RUNWAY CENTER LINE. REJECTED TAKEOFF AT LESS THAN 10 KTS. PERFORMED MAX POWER AS SURANCE RUN PER JRH 18.1 PG 5. PERFORMED ACCEL CHECK, FROM FLT IDLE TO T/O POWER WAS 6 SEC, THIS IS WITHIN LIMITS ALL I AW A300 M/M 71-00-00 PG 565. 2 L 7 2 4F 4 F RT A35EU E23EA 2002082700081 20020827 00081 NM 2002 8 27 DHL2002705009 1 20020718 A 2612 FIRE WARNING BOEING 727 72722C 138400F NM COCKPIT MALFUNCTIONED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705DH 19191 FIRE BELL DID NOT SOUND DURING ENGINE, APU, OR LOWER CARGO FIRE TEST. PERFORMED AURAL WARN FIRE DETECTION TEST ON ENGIN ES, APU, W/W AND LOWER CARGO SMOKE IAW 31-26-00, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002082700082 20020827 00082 NM 2002 8 27 DHL2002708009 1 20020712 A 2611 BUTTON BOEING 727 72725 1384006 NM COCKPIT BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 SMOKE DETECTION SYSTEM NR 2 TEST BUTTON BROKE OFF DURING TEST. REPAIRED TEST BUTTON COVER IAW BMM 20-60-01. 2 L 7 3 4F A3WE 2002082700083 20020827 00083 NM 2002 8 27 DHL2002709004 1 20020626 A 3350 1000679 LIGHT BOEING 727 72782C 1384026 NM COCKPIT INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 COCKPIT EMERGENCY EXIT LIGHT WILL NOT HOLD A CHARGE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY SYST, OPS C HECKED GOOD IAW B727 MM 33-50-00. 2 L 7 3 4F A3WE 2002082700084 20020827 00084 NM 2002 8 27 DHL2002715009 1 20020619 A 3150 SWITCH BOEING 727 727155C 138404Z NM NLG DIRTY A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 715DH 19618 T/O WARNING HORN SOUNDED ON T/O ROLL. CLEANED CONTACTS ON AIRBRAKE POSITION SWITCH IN FWD NOSE BAY. OPS CHECK GOOD IAW 31-26-00. 2 L 7 3 4F A3WE 2002082700085 20020827 00085 NM 2002 8 27 DHL2002720002 1 20020620 A 2611 SMOKE DETECTOR BOEING 727 727228 1384083 NM NR 1 WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 720DH 19544 COCKPIT TEST SMOKE NR 1 LEFT INOP. REMOVED AND REPLACED NR 1 LEFT SMOKE DETECTOR IAW B727 MM 26-16-01, OPS CHECKS NORMA L. 2 L 7 3 4F RT A3WE 2002082700086 20020827 00086 NM 2002 8 27 DHL2002720003 1 20020703 A 2612 CONNECTOR BOEING 727 727228 1384083 NM APU DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 720DH 19544 ON PREFLIGHT, APU WILL NOT FIRE TEST. CLEANED ELECTRICAL CONNECTOR SENSOR/RESPONDER OPS. CHECKS NORMAL IAW DHL B727A M M 26-15-0. 2 L 7 3 4F RT A3WE 2002082700087 20020827 00087 NM 2002 8 27 DHL2002721004 1 20020717 A 5220 PANEL BOEING 727 727228 1384083 NM EMERGENCY EXIT BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 OVERWING EMERGENCY EXIT DOOR PANEL IS BENT AT LOWER AFT CORNER. RESECURED INTERIOR EMERGENCY EXIT PANEL WITH GILLINER T APE IAW B727 M/M 52-21-00, CHECKS GOOD. 2 L 7 3 4F RT A3WE 2002082700088 20020827 00088 NM 2002 8 27 DHL2002721005 1 20020721 A 3350 BATTERY BOEING 727 727228 1384083 NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 721DH 19545 EMERGENCY EXIT LIGHT OVER AIRCRAFT ENTRY DOOR INOP DURING STANDBY POWER CHECK. REMOVED AND REPLACED EMERGENCY EXIT LIGH T BATTERIES, OPS CHECKS GOOD IAW B727 MM 33-50-71. 2 L 7 3 4F RT A3WE 2002082700089 20020827 00089 NM 2002 8 27 DHL2002721006 1 20020725 A 3350 LIGHT BOEING 727 727228 1384083 NM CABIN OUT OF POSITION A DHLA K NONE O OTHER NR NOT REPORTED 1 SO 01 721DH 19545 EMERGENCY EXIT LIGHT ABOVE ENTRY DOOR FELL OFF. REINSTALLED EMERGENCY EXIT LIGHT AS PER MAINTENANCE MANUAL 33-50-71. O PS CHECK GOOD. 2 L 7 3 4F RT A3WE 2002082700090 20020827 00090 NM 2002 8 27 DHL2002721007 1 20020725 A 3310 10602041 LIGHT BOEING 727 727228 1384083 NM COCKPIT DEFECTIVE A DHLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 721DH 19545 S/O`S OVERHEAD TABLE LIGHT INOP, WHEN ADJUSTED SPARKS CAME OUT OF SOCKET. FOUND S/O'S FWD TABLE LIGHT SOCKET BROKEN. R EPLACED S/O'S FWD TABLE LIGHT ASSEMBLY. OPS CHECK NORMAL. DURING START UP SMOKE APPEARED COMING FROM TABLE LIGHT AREA. TURNED OFF TABLE LIGHT & FLUORESCENT LIGHTS, SMOKE CONTINUED DEFERRED S/O'S TABLE LIGHTS. C/B PULLED AND COLLARED. I NSP WIRING ASSOCIATED W/ TABLE LIGHTS & FLUORESCENT LIGHTS PER BWDM 33-15-21, NO DEFECTS. INSP LIGHT ASSY'S, NO DEFECTS . OPS CK NORMAL. NO SMOKE IN 4 HRS. 2 L 7 3 4F RT A3WE 2002082700092 20020827 00092 NM 2002 8 27 DHL2002721501 1 20020805 A 5313 STRINGER BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK DISCREPANCY AS FOLLOWS, IN FWD CARGO AFT 640, STR 23R HAS CORROSION. REMOVED SECTION OF STRINGER. FABRI CATED A NEW SECTION OF STRINGER IAW B-727 SRM 53-10-3 FIG 1 AND SRM 53-10-2. INSTALLED NEW STRINGER AND SPLICE IAW B-72 7 SRM 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 2002082700093 20020827 00093 NM 2002 8 27 2002UALA01318 1 20020815 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 CABIN FLOORBEAM AT STATION 365 STRINGER 17R HAD EXCESSIVE MATERIAL REMOVED DURING CORROSION CLEAN UP BETWEEN RBL 10 OUT TO 64 RBL ON THE UPPER T-CAP SURFACE. MAJOR REPAIR ACCOMPLISHED. REPLACEMENT T-CAP INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082700097 20020827 00097 EU 2002 8 27 DHL2002362003 1 20020619 A 2840 MODULE AIRBUS 300 A300B4203 3930306 EU COCKPIT FAULTY A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 362DH 84 RAN BEFORE T/O CHECKLIST, HIT RECALL BUTTON AND GOT FUEL LIGHT. TAXI CLEAR OF RUNWAY, CONTACTED MAINT & FLT CONTROL. F UEL ILLUMINATED DUE TO NR 2A RES LIGHT MODULE BEING BROKEN. REMOVED AND REPLACED MODULE. TESTED, NO DEFECTS NOTED. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2002082700098 20020827 00098 EU 2002 8 27 DHL2002362004 1 20020801 A 2612 WARNING SYSTEM AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 362DH 84 NUMBER 2 ENGINE FIRE DET LOOP-A LIGHT ALWAYS ON. MXC NOTIFIED. PERFORMED OPERATIONAL CHECK OF FIRE DETECTION LOOPS (FO R ENGINES) IAW M/M 26-12-12. OPS CHECKED GOOD. 2 L 7 2 4F RT A35EU 2002082700099 20020827 00099 EU 2002 8 27 DHL2002362005 1 20020814 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 362DH 84 SMOKE DETECTOR M/I AMBER, SMOKE DETECTORS WILL NOT TEST. REINITIALIZED ELECT SMOKE DETECTION BOX AND OPS CHECKS GOOD IA W M/M 26-11-11. 2 L 7 2 4F RT A35EU 2002082700100 20020827 00100 EU 2002 8 27 DHL2002363008 1 20020625 A 5270 WARNING SYSTEM AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 363DH 85 UPON TAKEOFF AFT CARGO LIGHT AND MWP LIGHT ILLUMINATED. OPS CHECKED AFT PIT CARGO DOOR INDICATION IAW 52-34-00. OPS CH ECKED GOOD. 2 L 7 2 4F RT A35EU 2002082700101 20020827 00101 EU 2002 8 27 DHL2002363009 1 20020721 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA K NONE N FALSE WARNING NR NOT REPORTED 1 SO 01 363DH 85 CABIN SMOKE DETECTOR LIGHT ILLUMINATED. (RIGHT UPPER MID SECTION SMOKE LIGHT WAS ILLUMINATED). COOLED INSIDE OF A/C SY STEM CHECKS SERVICEABLE PER A300 MM 26-16-00. 2 L 7 2 4F RT A35EU 2002082700102 20020827 00102 EU 2002 8 27 DHL2002363010 1 20020723 A 2612 CONNECTOR AIRBUS 300 A300B4203 3930306 EU FIRE WARNING DIRTY A DHLA K NONE L NO TEST UK UNKNOWN 1 SO 01 363DH 85 ENG 1 LOOP-A ANNUNCIATOR NOT ILLUMINATED WHEN TESTING. CLEANED CONNECTOR ON NACELLE A-LOOP. LOOP-A TESTS GOOD IAW A300 MM 26-12-00. 2 L 7 2 4F RT A35EU 2002082700103 20020827 00103 EU 2002 8 27 DHL2002364008 1 20020728 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 01 364DH 141 ONE CABIN SMOKE DETECTOR ILLUMINATED WHILE PARKED ON RAMP. COOLED A/C, CABIN SMOKE DETECTOR OPS CHECK SERVICEABLE PER A 300 MM 26-16-00. 2 L 7 2 4F RT A35EU 2002082700104 20020827 00104 EU 2002 8 27 DHL2002364009 1 20020728 A 2613 3500813 CONTROLLER AIRBUS 300 A300B4203 3930306 EU OVERHEAT SYS DEFECTIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 364DH 141 B-LOOP SYSTEM OF MANIFOLD FAULT DETECTION DOES NOT TEST PROPERLY. APU MANIFOLD FAULTS B-LOOP. NR 2 WINGS MANIFOLD FAUL TS B-INOP. APU BLEED VALVE SECURED CLOSED. REMOVED AND REPLACED NR 2 SYS CFD CONTROL UNIT PER MM REF 26-16-10. SYS OP S CHECKS GOOD. OK TO CONTINUE. 2 L 7 2 4F RT A35EU 2002082700105 20020827 00105 EU 2002 8 27 DHL2002365007 1 20020721 A 2612 CONTROL UNIT AIRBUS 300 A300B4203 3930306 EU FIRE DETECTION MALFUNCTIONED A DHLA K NONE N FALSE WARNING CR CRUISE 1 SO 01 365DH 149 DURING CRUISE FLT SSC (SINGLE STROKE CHIME) AND MWP (MASTER WARNING PANEL) LOOPS LIGHT ILLUMINATED FIRE DET PANEL BOTH A & B LOOPS TESTED OK. MWP LOOPS AND CHIMES CONTINUE INTERMITTENT. RERACKED FIRE CONTROL UNIT AN OPS CHECK OK PER MM 26 -00. 2 L 7 2 4F RT A35EU 2002082700106 20020827 00106 EU 2002 8 27 DHL2002366007 1 20020622 A 2612 CONNECTOR AIRBUS 300 A300B4203 3930306 EU FIRE DETECTION LOOSE A DHLA K NONE N FALSE WARNING CL CLIMB 1 SO 01 366DH 249 LOOPS LIGHT ENGINE NR 2 SYSTEM-A CAME ON AT FLIGHT LEVEL 200 AND WENT BACK OUT AT FLIGHT LEVEL 210, RAN ABNORMAL CHECK L IST OPS CHECK OK IN FLIGHT. FOUND LOOSE CONNECTION TO LOOP-A, UNDER PYLON AFT LOOP AREA. SECURED CONNECTION. OPS CHEC K NORMAL PER MM 26-12-00. 2 L 7 2 4F RT A35EU 2002082700107 20020827 00107 EU 2002 8 27 DHL2002366010 1 20020629 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE DEFECTIVE A DHLA K NONE N FALSE WARNING CL CLIMB 1 SO 01 366DH 249 DURING CLIMBOUT THROUGH 23,000 FT, ENGINE NR 2 LOOP-A LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE. LIGHT WENT OUT AFTER ONE MINUTE. REPLACED NR 2 ENGINE A-LOOP SENSING ELEMENT AS PER MM 26-12-12. OPS CHECKED NORMAL AS PER MM 26-12-0 0. 2 L 7 2 4F RT A35EU 2002082700108 20020827 00108 EU 2002 8 27 DHL2002366012 1 20020730 A 2612 CONNECTOR AIRBUS 300 A300B4203 3930306 EU NR 1 ENGINE DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 366DH 249 ON PREFLIGHT CHECK FOUND NR 1 ENGINE A-LOOP WILL NOT TEST. CLEANED CONNECTORS ON NR 1 ENGINE A-FIRE LOOP PER A300 MM RE F 26-12-12. SYSTEM OPS CHECKS GOOD. OK TO CONTINUE. 2 L 7 2 4F RT A35EU 2002082700109 20020827 00109 EU 2002 8 27 DHL2002367004 1 20020623 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 01 367DH 265 SMOKE LIGHTS ILLUMINATED IN AFT MAIN DECK. COOLED MAIN DECK AREA. SMOKE DETECTION SYSTEM OPS CHECK SERVICEABLE. 2 L 7 2 4F RT A35EU 2002082700110 20020827 00110 EU 2002 8 27 DHL2002367005 1 20020404 A 5311 FRAME AIRBUS 300 A300B4203 3930306 EU FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH 265 FRAME 19 HAS OUTER FLANGE CRACK ABOUT ONE INCH LONG. INSTALLED DOUBLER REPAIR PER SRM 53-10-10 FIG 713. 2 L 7 2 4F RT A35EU 2002082700111 20020827 00111 EU 2002 8 27 DHL2002367006 1 20020629 A 2611 SMOKE WARNING AIRBUS 300 A300B4203 3930306 EU COCKPIT FALSE ACTIVATION A DHLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 367DH 265 DURING TAXI OUT, CARGO SMOKE LIGHT ILLUMINATED. AIRCRAFT TAXIED BACK IN. NO INDICATION OF SMOKE OR FIRE, CARGO COMPART MENT EMPTY. RESET C/B. TESTED SYSTEM; OPS CHECKED OK IAW MM 26-16. 2 L 7 2 4F RT A35EU 2002082700112 20020827 00112 EU 2002 8 27 DHL2002367007 1 20020713 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CARGO BAY MALFUNCTIONED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 367DH 265 FORWARD CARGO COMPARTMENT SMOKE DETECTOR SYSTEM NR 2 WILL NOT TEST. PERFORMED OPS CHECK OF LOWER CARGO SMOKE DETECTOR S YSTEM IAW M/M 26-14-00. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A35EU 2002082700113 20020827 00113 2002 8 27 DL76G020833 4 20020718 A 3425 6227999003 INDICATOR BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1603 29695 F/O HSI SCREEN SHORTED OUT WITH ELECTRICAL SMELL. PULLED C\B. REPLACED HSI. 2 L 7 2 4F RT A1NM 2002082700114 20020827 00114 NE 2002 8 27 DL76G020836 2 20020718 A 7250 FRAME BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 1 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 37358 24984 695374 ON MTC CHECK FOUND 6.75 INCH CRACK AT TURBINE REAR FRAME. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 2002082700115 20020827 00115 NM 2002 8 27 DL76G020857 1 20020721 A 2450 CIRCUIT BREAKER BOEING 767 767332 1382001 NM COCKPIT TRIPPED A DALA O OTHER O OTHER CR CRUISE 1 SO 27 1602 29694 WHILE IN CRUISE C/B RIGHT DC BUS AND RAM AIR TURBINE POWER C/B BOTH POPPED, ALL EMERGENCY EXIT LIGHTS IN CABIN ILLUMINAT ED. ALSO RIGHT REC FAN AFT CABIN TEMP EICAS MSG AFT EQUIP COOLING EXHAUST FAN 1 AND FWD EQUIP EXHAUST FAN MSG. RESET C /B C/W RAT MANUAL EXT. NO DEFECTS NOTED. RAN FANS AND PACKS BOTH C/B STAYED IN. INSPECTED WIRING BEHIND P6 AND P11 PAN ELS, NO CHAFING OR DAMAGE NOTED. 2 L 7 2 4F RT A1NM 2002082700116 20020827 00116 NM 2002 8 27 DL76K020886 1 20020729 A 3240 S283T00127 CONTROL UNIT BOEING 767 767332 1382001 NM BRAKE SYSTEM FAULTY A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 175DZ 29696 ANTI SKID MSG ON EICAS NORMAL AND ALTERNATE ANTISKID STATUS MSG. INTERROGATED ANTISKID/AUTOBRAKE CONTROL UNIT, FAULTED NR 4 TRANSDUCER. INSPECTED WIRING ON NR 4 TRANSDUCER AND HUB CAP ATTACHED HARDWARE, CKS GOOD. PER FIM REPLACED CONTROL UNIT, RAN FULL AUTOBRAKE/ANTISKID CK PER FIM, CKS OK. OK TO RETURN TO SERVICE. 2 L 7 2 4F RT A1NM 2002082700117 20020827 00117 NM 2002 8 27 VNAA0207046 1 20020730 A 3610 DRAIN LINE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE BLEED AIR BROKEN A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 461PS 3075 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND BLEED SHUT OFF VALVE FAIL MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPEC TED AND FOUND A BROKEN DRAIN TUBE ON THE PACK. MAINTENANCE REPLACED THE DRAIN TUBE IN ACCORDANCE WITH DORNIER MAINTENAN CE MANUAL 36-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082700118 20020827 00118 NM 2002 8 27 VNAA0207048 1 20020731 A 2150 5729C000002 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A/C BAY FAILED A VNAA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 07 423JS 150 3032 THE CREW REPORTED THAT THE CABIN TEMPERATURE WOULD NOT GO BELOW 35 DEGREES CELSIUS AND RETURNED TO DCA. THE AIRCRAFT WA S FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED THE ENVIRONMENTAL CONTROL UNIT IN ACCORDANCE WITH DORNIER MA INTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082700119 20020827 00119 NM 2002 8 27 VNAA0208003 1 20020801 A 7712 311694201 PROBE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 430JS 13846 3229 3044 DURING CLIMB, THE CREW EXPERIENCED A LEFT HAND ENGINE TORQUE INDICATION THAT WAS READING ERRATIC AND RETURNED TO TYS. T HE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE THEN INSPECTED AND REPLACED THE LEFT HAND TORQUE PROBE IN ACCORDANCE WITH D ORNIER MAINTENANCE MANUAL 77-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082700120 20020827 00120 NE 2002 8 27 VNAA0208008 2 20020807 A 7321 311888804 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 431JS 10707 3028 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INS PECTED AND REPLACED THE LEFT HAND ENGINE CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATION AL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082700121 20020827 00121 2002 8 27 VNAA0208009 4 20020807 A 3425 7013270934 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NR 1 FAILED A VNAA O OTHER G MULTIPLE FAILURE DE DESCENT 1 GL 07 328JS 3600 3030 DURING DESCENT, THE CAPTAIN REPORTED LOSING THE TRANSPONDER, RADIO MANAGEMENT UNITS 1 AND 2, FLIGHT MANAGEMENT SYSTEM, T CAS, AUTOMATIC DIRECTION FINDER, AND LOCALIZERS. WHEN THE AIRCRAFT LANDED IN PIT, MAINTENANCE INSPECTED AND REPLACED TH E NR 1 RADIO MANAGEMENT UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082700122 20020827 00122 NM 2002 8 27 VNAA0208010 1 20020807 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 438JS 15652 93 3056 THE CREW REPORTED THAT THE FIRST SECTION OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND RE PLACED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFOR MED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082700123 20020827 00123 NM 2002 8 27 VNAA0208011 1 20020808 A 3241 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 470PS 3006 DURING TAKEOFF, THE CREW RECEIVED A BLUE ANTI-SKID CAS MESSAGE AND ABORTED TAKEOFF. THE CREW RECYCLED THE AIRCRAFT POWE R AND THE MESSAGE CLEARED. FLIGHT 4181 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITHOUT ANY FURTHER INCIDEN TS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082700124 20020827 00124 NM 2002 8 27 VNAA0208012 1 20020809 A 3241 AE20768 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ANTI-SKID SYS FAULTY A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 437JS 7613 2601 3055 DURING THE CLIMBOUT, THE CREW RECEIVED MULTIPLE ERRATIC BRAKE TEMPERATURE INDICATIONS AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE ANTI SKID CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL C HECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082700125 20020827 00125 NM 2002 8 27 VNAA0208013 1 20020809 A 2730 RELAY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ELEVATOR FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 439JS 3057 DURING CLIMBOUT, THE CREW EXPERIENCED AN ELEVATOR TRIM FAST CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE 55CC RELAY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND T HE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082700126 20020827 00126 NM 2002 8 27 VNAA0208015 1 20020810 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 458PS 1322 3068 THE CREW REPORTED THAT THE FLIGHT ATTENDANTS EXIT SIGN WAS NOT ILLUMINATING. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAI NTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082700127 20020827 00127 NM 2002 8 27 VNAA0208016 1 20020811 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 458PS 14405 3068 THE CREW REPORTED THAT THE FIRST SET OF EMERGENCY FLOORING LIGHTING WAS NOT ILLUMINATING. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK POSITION IN ACCORDANCE WITH DORNIER MAINTE NANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082700128 20020827 00128 NM 2002 8 27 VNAA0208017 1 20020812 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN MALFUNCTIONED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 439JS 3057 THE CREW REPORTED THAT THE EMERGENCY FLOORING LIGHTING AT ROWS 4, 5, AND 6 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND RERACKED THE EMERGENCY BATTERY AT THE 5LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATI ONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002082700129 20020827 00129 WP 2002 8 27 02FDEA00596 1 20020817 A 5514 STRUCTURE DOUG DC10 DC1010 3022110 WP HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 550FE 46521 RUST EMITTING FROM 40 EACH BARREL NUT HOLES ON RT AND LT HORIZ STAB LWR PLANK ATTACHMENT TO CENTER TORQUE BOX. R&R RUST Y BARREL NUTS & CLEANED HOLES MID PLANK AND BOLTS WITH PLI WASHERS PER MM 52-22-02-1. 2 L 7 3 4F A22WE 2002082700130 20020827 00130 NM 2002 8 27 DHL2002721502 1 20020807 A 5311 FRAME BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK DISCREPANCY AS FOLLOWS, CRACK IN MAIN FRAME, STA 540, STR 24R. STOP DRILL OF CRACK IN MAIN FRAME IAW B-7 27 SRM 51-10-1 FIG 1. FABRICATED DOUBLER IAW B-727 SRM 52-90-1 PAGE 207-215. 2 L 7 3 4F RT A3WE 2002091100141 20020911 00141 NM 2002 9 11 F3LA200200241 1 20020823 A 5320 INTERCOSTAL BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION FWD LAVATORY AT BS 294.5, STR 4L CORRODED. FABRICATED AND INSTALLED NEW INTERCOSTAL T-CHORD AND SHIM PER SRM 51-40-02, SOPM 20-41-02 AND EA 53-737-178. 2 L 7 2 4F RT A16WE 2002082700131 20020827 00131 NM 2002 8 27 DHL2002721503 1 20020808 A 5347 SEAT TRACK BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN SEAT TRACK BETWEEN STA 870-848, AFT FLANGE CORRODED AT LBL 24. REMOVED COR ROSION FROM CABIN SEAT TRACK, BEYOND ALLOWABLE LIMITS IAW B-727 SRM 53-10-1 FIG 1. REMOVED CORRODED SEAT TRACK. FABRIC ATED NEW SECTION IAW B-727 SRM 51-30-2. INSTALLED NEW SECTION OF SEAT TRACK IAW B-727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002082700132 20020827 00132 NM 2002 8 27 DHL2002721504 1 20020808 A 5347 SEAT TRACK BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK DISCREPANCY AS FOLLOWS, CABIN, SEAT TRACK AT STA 760 IS CORRODED AT RBL 24. REMOVED CORROSION FROM CABIN SEAT TRACK AND FOUND CORROSION TO BE BEYOND ALLOWABLE LIMITS IAW B-727 SRM 53-10-1 FIG 3. REMOVED CORRODED SEAT TRACK I AW B-727 SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW B-727 SRM 53-10-2. INSTALLED NEW SECTION OF SEAT TRACK IAW B-727 S RM 51-30-2. 2 L 7 3 4F RT A3WE 2002082700133 20020827 00133 NM 2002 8 27 DHL2002721505 1 20020806 A 5330 SKIN BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN CRACKED SECTION 41 LEFT SIDE BS 243 WL 215. CUTOUT CRACKED SECTION OF FUSELAGE SKIN IAW B-727 SRM 53-30-3. FABRICATED REPAIR DOUBLER IAW B-727 SRM 53-30-3 FIG 3 AND S/B 53-0183. INSTAL LED DOUBLER AND FILLER REPAIR IAW B-727 SRM 53-30-3 FIG 3 AND S/B 727-53-0183. 2 L 7 3 4F RT A3WE 2002082700134 20020827 00134 NM 2002 8 27 DHL2002726002 1 20020703 A 2611 SMOKE DETECTOR BOEING 727 727228 1384083 NM NR 3 INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 726DH 20409 NR 3 LEFT SMOKE DETECTOR WILL NOT TEST. RELAMPED DETECTOR TEST LOOP. OPS CHECK OK 26-16-0. 2 L 7 3 4F RT A3WE 2002082700135 20020827 00135 NM 2002 8 27 DHL2002726003 1 20020724 A 2611 SMOKE DETECTOR BOEING 727 727228 1384083 NM CABIN WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 726DH 20409 NR 5 CABIN SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED LAMP TEST BULB OF DETECTOR 5R. OPS TEST GOOD IAW MM 26-1 7-00. 2 L 7 3 4F RT A3WE 2002082700136 20020827 00136 NM 2002 8 27 DHL2002741001 1 20020123 A 2612 LIGHT BOEING 727 7272Q9 138448M NM COCKPIT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 741DH 21931 NR 1 ENG FIRE TEST WILL NOT ILLUMINATE A OR B. RELAMPED NR 1 ENGINE FIRE TEST LIGHT BULBS. NR 1 ENGINE FIRE TEST OK IN BOTH A & B PER M/M 26-11-01. 2 L 7 3 4F RT A3WE 2002082700137 20020827 00137 NM 2002 8 27 DHL2002741009 1 20020621 A 2611 LIGHT BOEING 727 7272Q9 138448M NM COCKPIT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 741DH 21931 NR 6 SMOKE DETECTOR LIGHT WILL NOT TEST. RELAMPED LIGHT BULBS FOR NR 6 SMOKE DETECTOR, OPS CHECK NORMAL AS PER MM 26-17 -0. 2 L 7 3 4F RT A3WE 2002082700138 20020827 00138 NM 2002 8 27 DHL2002741010 1 20020627 A 2611 WARNING LIGHT BOEING 727 7272Q9 138448M NM COCKPIT FALSE INDICATION A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 741DH 21931 AT FL 370 THE MAIN CARGO SMOKE LIGHT CAME ON. THE LIGHT REMAINED ON UNTIL AFTER LANDING IN IAH. REMOVED AND REPLACED L AMPS ON NR 1 & 5 SMOKE DETECTOR IAW AEI 26 TEST NORMAL. 2 L 7 3 4F RT A3WE 2002082700139 20020827 00139 NM 2002 8 27 DHL2002741012 1 20020822 A 2611 SMOKE WARNING BOEING 727 7272Q9 138448M NM COCKPIT MALFUNCTIONED A DHLA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 741DH 21931 DURING DESCENT THE CARGO SMOKE LIGHT CAME ON FOR FIVE MINUTES THEN WENT OUT DURING APPROACH AT 8,000 FT. PERFORMED EMER GENCY CHECKLIST FOR CARGO SMOKE CONTROL AND EMERGENCY EVACUATION CHECKLIST. TESTED MAIN CARGO SMOKE DETECTION SYSTEM IA W AEI CARGO CONVERSION MANUAL CH 26. OPS CHECK OK OF SMOKE DETECTION SYSTEM. 2 L 7 3 4F RT A3WE 2002082700140 20020827 00140 NM 2002 8 27 DHL2002742003 1 20020730 A 3350 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 742DH 21290 PREFLIGHT, EMERGENCY EXIT LIGHTS - MAIN ENTRY AND CABIN INOP. REMOVED AND REPLACED BATTERIES, OPS CHECKED GOOD IAW M/M 33-50-0. 2 L 7 3 4F A3WE 2002082700141 20020827 00141 NM 2002 8 27 DHL2002742004 1 20020730 A 7711 JG298A4 INDICATOR BOEING 727 727225 1384077 NM COCKPIT DEFECTIVE A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 742DH 21290 NR 2 EPR GAUGE INOP ON TAKEOFF ROLL. ABORTED TAKEOFF, RETURNED TO BLOCKS. CHECKED COMPRESSOR & TURBINE; LOOKED GOOD. REPLACED NR 2 EPR IND IAW M/M 77-10, SYSTEM CHECKS NORMAL. 2 L 7 3 4F A3WE 2002082700142 20020827 00142 NM 2002 8 27 DHL2002743007 1 20020706 A 2612 SENSOR BOEING 727 727225 1384077 NM NR 3 ENGINE FAULTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 743DH 22438 NR 3 ENG FIRE WARNING TEST OF FIREWALL POS WON'T TEST. NR 3 ENG LWR PYLON PANEL REMOVED & FIREWALL LOOP CONNECTOR DISCO NNECTED FOR T/S. REMOVED AND REPLACED SENSOR C/P IAW BWPM 20-62-14 AND SYSTEM OPS CHK GOOD IAW BMM 26-11-12. 2 L 7 3 4F A3WE 2002082700143 20020827 00143 NM 2002 8 27 DHL2002743008 1 20020708 A 2612 ELEMENT BOEING 727 727225 1384077 NM NR 3 ENGINE MALFUNCTIONED A DHLA K NONE N FALSE WARNING UK UNKNOWN 1 SO 01 743DH 22438 NR 3 ENG DET CIRCUIT GROUND LIGHT ON. DEFERRED NR 3 ENG FIRE DETECTOR GROUND FAULT LIGHT PER MEL 26-9-1 CAT C. FOUND A ND CORRECTED ELEMENT CONNECTION ON STRUT ON ENG NR 3 NOW OK PER M/M 26124. 2 L 7 3 4F A3WE 2002082700144 20020827 00144 NM 2002 8 27 DHL2002743009 1 20020717 A 5250 6570375927B DOOR BOEING 727 727225 1384077 NM COCKPIT DEFECTIVE A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 743DH 22438 COCKPIT DOOR WILL NOT OPEN FROM THE INSIDE. REMOVED AND REPLACED COCKPIT DOOR IAW M/M 52-50-0. OPS CHECKS NORMAL. 2 L 7 3 4F A3WE 2002082700145 20020827 00145 NM 2002 8 27 DHL2002743010 1 20020724 A 2780 FLAP BOEING 727 727225 1384077 NM WING MALFUNCTIONED A DHLA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 SO 01 743DH 22438 DURING APPROACH NR 5 L/E FLAP FAILED TO EXTEND. ACCOMPLISHED ABNORMAL FLAP LANDING CHECK LIST. INSPECTED NR 5 L/E FLAP AND CYCLED FLAPS 4 TIMES IAW DHL MM 27-81. NO FAULTS OR PROBLEMS OBSERVED. 2 L 7 3 4F A3WE 2002082700146 20020827 00146 NM 2002 8 27 DHL2002743011 1 20020812 A 3350 1000679 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 743DH 22438 MAIN ENTRY DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY AND EMERGENCY EXIT LIGHT OPS CHECK GOOD M/M 33-50-00 . 2 L 7 3 4F A3WE 2002082700147 20020827 00147 NM 2002 8 27 DHL2002745007 1 20020816 A 3150 WARNING SYSTEM BOEING 727 727224 1384076 NM COCKPIT MALFUNCTIONED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 745DH 20665 AT KSAN T/O WARNING HORN SOUNDED WHEN THRUST ADVANCED FOR T/O. T/O ABORTED. CYCLED CONTROL SURFACES AND STAB TRIM INDI VIDUALLY. NO HORN AFTER SPEED BRAKE WAS CYCLED. THEN OPS NORMAL. DEPARTURE UNEVENTFUL. OPS CHECK T/O WARNING PER 31- 26-00. OPS CHECK SATISFACTORY. 2 L 7 3 4F A3WE 2002091100142 20020911 00142 NM 2002 9 11 F3LA200200242 1 20020823 A 5330 SKIN BOEING 737 737317 138447P NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED C2 DOOR CUTOUT FRAME SKIN DAMAGED AT BS 847, STR 23R. REMOVED DAMAGED AREA, FABRI CATED AND INSTALLED REPLACEMENT PARTS PER EA 53-737-179. 2 L 7 2 4F RT A16WE 2002082700148 20020827 00148 NM 2002 8 27 DHL2002745502 1 20020619 A 5730 SKIN BOEING 727 727224 1384076 NM LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING C-CHECK, LT WING LWR WING SKIN AT STR 9 FROM WING STA 519 TO STA 421.50 IS CORRODED. REMOVED CORROSION ON LT WIN G LWR IN SPAR SKIN, FOUND TO BE BEYOND ALLOWABLE LIMITS IAW B-727 SRM 57-30-1 FIG 1. FABRICATED AND INSTALLED DOUBLER A ND TRIPLER IAW DWG FASI-026D-1 AND FORM 8110-3. LEAK CHECKED GOOD IAW B-727 MM 28-11-00. 2 L 7 3 4F A3WE 2002091100144 20020911 00144 NM 2002 9 11 F3LA200200243 1 20020823 A 5313 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON STR 21L UNDER FRAME AT BS 927. FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 53-00-3, 51-40-02 AND 51-20-01. 2 L 7 2 4F RT A16WE 2002082700149 20020827 00149 NM 2002 8 27 UIEA200200030 1 20020813 A 3040 60B100785 WINDOW BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE L1 INOPERATIVE A UIEA G H O2 MASK DEPLOYED DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 507MC 21380 L1 WINDSHIELD LOWER AFT ELECTRICAL CONNECTION WAS PRODUCING SMOKE. SYSTEM TURNED OFF. SMOKE EV AC CHECKLIST COMPLETED. C/A: REPLACED L1 WINDOW PER MM 56-11-01 REPLACED LEFT WINDOW HEAT CONTROLLER PER MM. WINDOW HEAT CONTROLLER (PN 65715 4-5). 2 L 7 4 4F 4 F A20WE E23EA 2002091200088 20020912 00088 NM 2002 9 12 F3LA200200244 1 20020823 A 5320 INTERCOSTAL BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON UPPER FLANGE OF INTERCOSTAL AT STA 727A TO 727B. FABRICATED AND INST ALLED NEW INTERCOSTAL PER SRM 51-30-01 AND 53-60-04. 2 L 7 2 4F RT A16WE 2002082700150 20020827 00150 NM 2002 8 27 USA2002F00076 1 20020730 A 3350 1012721 LIGHT BOEING 737 7373B7 1384580 NM SEAT ROW 10ABC FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 23385 PILOT REPORTED THE EMERGENCY LIGHTS AT SEAT ROW 10ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2002091200089 20020912 00089 NM 2002 9 12 F3LA200200245 1 20020823 A 5320 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED STRINGER CLIP AT BS 727D, STR 4L CRACKED. FABRICATED AND INSTALLED REPLACEMENT ST RINGER CLIP PER BOEING DRAWING 69-35352, SRM 51-30-02 AD SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002082700151 20020827 00151 NM 2002 8 27 USA2002F00077 1 20020803 A 3397 WIRE BOEING 737 737301 1384611 NM RROYCE TAY TAY65015 54557 NE SEAT ROW 13ABC BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 23930 MAINTENANCE FOUND THE EMERGENCY LIGHT ON SEAT ROW 13 ABC INOPERATIVE. MAINTENANCE REPAIRED WIRING AT SEAT ROW 13 ABC. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E25NE 2002091200090 20020912 00090 NM 2002 9 12 F3LA200200246 1 20020823 A 5330 SKIN BOEING 737 737317 138447P NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED C-2 DOOR CUTOUT AFT FRAME SKIN DAMAGED AT STA 847, STR 23R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER EA 53-737-179. 2 L 7 2 4F RT A16WE 2002082700152 20020827 00152 NM 2002 8 27 USA2002F00079 1 20020808 A 3260 655825029806002 CARD BOEING 737 737401 1384701 NM GE CFM56 CFM56* 13802 NE E11 SHELF,LWR N FAULTY A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 407US 23877 ON CLIMB OUT FROM PIT, CREW REPORTED THE LEFT MAIN LANDING GEAR RED AND GREEN LIGHTS ILLUMINATED WHEN THE GEAR WAS RETRA CTED. CREW CYCLED GEAR WITH SAME RESULTS. WHEN GEAR WAS EXTENDED, INDICATIONS IS NORMAL. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED LOGIC CARDS M986 AND M988 AND LUBRICATED THE LANDING GEAR ASSEMBLY. PERFORMED OPERATIONAL CHECK OF MAIN LANDING GEAR IN ASSOCIATION WITH MM WITH HYDRAULIC MULE AND AIRCRAFT HYDRAULIC SYSTEM. OPERATIONAL CHECK NORMAL ON GROUND. 2 L 7 2 4F 4 F RT A16WE E2GL 2002091200091 20020912 00091 NM 2002 9 12 F3LA200200247 1 20020823 A 5315 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON UNDERSIDE OF CARGO FLOORBEAMS AROUND NUT PLATES AT BS 727, LBL 7.5; B S 826, LBL 7.5; BS 727, LBL 12; BS 813, LBL 12; AND BS 945, LBL 12. REPLACED FLOORBEAMS FROM STA 727 - 947, LBL 12 PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002091200092 20020912 00092 NM 2002 9 12 F3LA200200248 1 20020823 A 3210 BUSHING BOEING 737 737317 138447P NM RT MLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-7 CHECK, INSPECTION REPORTED RT MLG OUTER CYLINDER B-LUG (OUTBOARD SIDE) CORRODED. REMOVED CORROSION, FABRICAT ED AND INSTALLED NEW BUSHING PER SOPM 20-50-03 AND OHM 32-11-1. 2 L 7 2 4F RT A16WE 2002091200093 20020912 00093 NM 2002 9 12 F3LA200200249 1 20020823 A 5320 CHANNEL BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED FWD LAVATORY WALL ATTACH CHANNEL CORRODED AND CRACKED, BS 308, LBL 41.25 TO LBL 10 .75. FABRICATED AND INSTALLED NEW HAT CHANNEL ATTACH ANGLE PER SRM 51-10-02, 51-40-02, BOEING DRAWING 65-77488-211 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002100200026 20021002 00026 NM 2002 10 2 2002UALA01322 1 20020817 A 5312 BULKHEAD BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 PRESSURE BULKHEAD ABOVE PANEL 193BL HAS TWO LARGE DENTS. MAJOR REPAIR ACCOMPLISHED. NEW PANEL INSTALLED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002100200027 20021002 00027 NM 2002 10 2 2002UALA01323 1 20020816 A 2720 654486112 PCU BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RUDDER FAILED A UALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 29 307UA 23668 WHILE ON FINAL APPROACH, AIRCRAFT EXPERIENCED AN UNCOMMANDED RUDDER DEFLECTION. REPLACED RUDDER PCU AND STANDBY RUDDER PCU DUE TO FAILURE TO RETURN TO NEUTRAL CONSISTENTLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100200029 20021002 00029 NM 2002 10 2 2002UALA01325 1 20020819 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 CENTER AC DISTRIBUTION BAY LWR BILGE LWR FRAME AT STATION 880 AT STRINGER 30 HAS HEAVY CORROSION. MAJOR REPAIR ACCOMPLI SHED.REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200031 20021002 00031 NM 2002 10 2 2002UALA01327 1 20020820 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 CAB BODY STATION 297 FRAME HAS A DEEP GOUGE IN INNER FLANGE RADIUS NEAR STRINGER 4L. MAJOR REPAIR ACCOMPLISHED. FRAME DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200038 20021002 00038 NM 2002 10 2 2002UALA01335 1 20020822 A 3397 WIRE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN PINCHED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 220UA 30223 SEAT EMERGENCY PATH LIGHTS ON BOTH SIDES OF ZONE 3 DO NOT COME ON. THERE IS A SHORTED WIRE BETWEEN ROWS 31 AND 34. FO UND PINCHED WIRE UNDER SEAT 33F. CLEARED AND REPAIRED WIRE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002100200039 20021002 00039 NM 2002 10 2 2002UALA01337 1 20020822 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 EXTERNAL FUSELAGE SKIN DENTED STATION 610 BETWEEN STRINGER 17L AND STRINGER 18L. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002082700153 20020827 00153 WP 2002 8 27 DHL2002806858 1 20020726 A 3231 56489321 DOOR DOUG DC8 DC873F 302199F WP DELAMINATED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 81567 46002 ITEM N/R 0072 LH MLG OUTER DOOR SKIN DELAMINATEDCORR:R/R LH MLG OUTER DOOR IAW MM 32-12-1 PG 401 OPS CHECKED GOOD IAW M/ M 32-30-0 PG 201 2 L 7 4 4F RT 4A25 2002082700154 20020827 00154 EU 2002 8 27 MALA020510 1 20020823 A 3230 HP84843072 CONTROL VALVE SAAB SF340 340B 7860101 EU DEFECTIVE A MALA O OTHER O OTHER LD LANDING 1 GL 15 457XJ 340B457 DURING FLIGHT #3309 LANDING GEAR WOULD NOT EXTEND INFLIGHT. RESET F7 C/B WAS RESET PER QRH AND GEAR EXTENDED SUCCESSFUL LY. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL VALVE, PERFORMED GEAR SWINGS, AND LEAK CHECK GOOD. IAW AMM 3 2-31-15-4 PN HP848430-72 SN/ON 1213, SN/OFF 2102 A/C OK FOR SERVICE 2 L 7 2 4T RT A52EU 2002082700155 20020827 00155 NM 2002 8 27 AWXA200200820 1 20020810 A 5320 65826711 WEB BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK HFEC INSPECTION INDICATED A 7/8" CRACK ON VERTICAL PRESSURE BEAM AT BS 663, RBL 3 2, WL 199. MAINTENANCE TRIMMED OUT DAMAGE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED 2 EACH R EPAIR DOUBLERS, AND 3 EACH FILLERS, AND INSTALLED REPAIR PARTS IAW AWA E.R. 15-5702-02235-GF1. 2 L 7 2 4F RT A16WE 2002082700156 20020827 00156 NM 2002 8 27 AWXA200200821 1 20020803 A 5330 65737421 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/16" CRACK WAS FOUND ON EXTERNAL FUSELAGE SKIN EXTENDING FROM FASTENER HOLE AT BS 303, STR 17 R/H, WL 210. MAINTENANCE CUTOUT DAMAGED SKIN AND BONDED DOUBLER AND PERFORMED A HFEC INSPECTION TO VERIF Y NO CRACKS EXIST. FABRICATED 3 EACH REPAIR DOUBLERS, A STRAP, A FILLER, AND TAPERED FILLER, AND INSTALLED REPAIR PARTS IAW AWA E.R. 15-5300-02236-ES2. 2 L 7 2 4F RT A16WE 2002082700157 20020827 00157 NM 2002 8 27 AWXA200200822 1 20020805 A 5313 6552928576 STRINGER BOEING 737 737277 1384570 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON CENTER INBOARD SIDE OF STRINGER 22 L/H, AFT OF DOME PLATE NUT AND ABOVE EMERGENCY LIGHT ASSEMBLY AT BS 776. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. CUTOUT DAMAGED SECTION OF STRINGER 22 L/H; FABRICATED 2 EACH ANGLES AND A SPLICE CHANNEL; AND INSTALLED REPAI R PARTS IAW B737-200 SRM 53-10-3, PG. 3-10. 2 L 7 2 4F RT A16WE 2002082700158 20020827 00158 NM 2002 8 27 AWXA200200823 1 20020805 A 5315 66232541 SHEAR TIE BOEING 737 737277 1384570 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON THE AFT CARGO PIT FLOOR FRAME ON TOP OF THE FORWARD LEG OU TBOARD SIDE, INBOARD OF STR 27 L/H, WL 149, BS 807. MAINTENANCE REMOVED STIFFNER, STRINGER CLIP, AND CUTOUT DAMAGED SKIN ATTACHMENT (SHEAR TIE) BS 807, WL 149. FABRICATED REPAIR ANGLE AND NEW CLIP, AND INSTALLED STIFFNER AND REPAIR PARTS IA W B737-200 SRM 53-10-4, PG. 24 A, B, C, AND FIG. 9A. 2 L 7 2 4F RT A16WE 2002082700159 20020827 00159 NM 2002 8 27 AWXA200200824 1 20020820 A 5320 65689183 WEB BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A 2" CRACK WAS FOUND ON TORQUE BOX WEB AT BS 1138 L/H. MAINTENANCE CUTOUT DAMAGE AT TORQUE BOX WEB, FABRICATED A REPAIR DOUBLER, AND INSTALLED REPAIR IAW B737-200 SRM 51-40-2, PG. 1-3, FIG. 1, SRM 51-1 0-2, PG.7 & 32, FIG. 2, SRM 53-10-2, PG. 53, FIG. 6, AND SRM 51-30-02, PG. 2. 2 L 7 2 4F RT A16WE 2002082700160 20020827 00160 NM 2002 8 27 AWXA200200825 1 20020819 A 5313 6545767512 STRINGER BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1/4" CRACK WAS FOUND ON STRINGER 16 L/H AT FASTENER HOLE BS 500C+16. MAINTENANC E TRIMMED OUT DAMAGE ON STRINGER 16 L/H AT BS 500C+16 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICA TED A REPAIR CHANNEL AND RADIUS FILLER, AND INSTALLED REPAIR PARTS IAW AWA E.R. 035-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2002082700161 20020827 00161 NM 2002 8 27 AWXA200200826 1 20020820 A 5313 6545767512 STRINGER BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK A 3/4" CRACK WAS FOUND ON STRINGER 16 L/H AT FASTENER HOLE BS 500C+4. MAINTENANCE TRIMMED OUT DAMAGE ON STRINGER 16 L/H AT BS 500C+4 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATE D A REPAIR CHANNEL AND RADIUS FILLER, AND INSTALLED REPAIR PARTS IAW AWA E.R. 035-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2002082700162 20020827 00162 NM 2002 8 27 AWXA200200827 1 20020821 A 5313 6545767512 STRINGER BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1/2" CRACK WAS FOUND ON STRINGER 16 R/H AT FASTENER HOLE BS 500C+4. MAINTENANCE TRIMMED OUT DAMAGE ON STRINGER 16 R/H AT BS 500C+4 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATE D A REPAIR CHANNEL AND RADIUS FILLER, AND INSTALLED REPAIR PARTS IAW AWA E.R. 035-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2002082700163 20020827 00163 NM 2002 8 27 AWXA200200828 1 20020821 A 5313 6545767512 STRINGER BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK A 7/8" CRACK WAS FOUND ON STRINGER 16 R/H AT FASTENER HOLE BS 500C+16. MAINTENANC E TRIMMED OUT DAMAGE ON STRINGER 16 R/H AT BS 500C+16 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICA TED A REPAIR CHANNEL AND RADIUS FILLER, AND INSTALLED REPAIR PARTS IAW AWA E.R. 035-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2002082700164 20020827 00164 NM 2002 8 27 AWXA200200829 1 20020819 A 5320 654957325 ANGLE BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1 1/2" CRACK WAS FOUND ON L/H AIR CONDITIONING BAY HEAT EXCHANGER COMPOSITE DUC T SUPPORT RETAINER AT BS 619, LBL 53. MAINTENANCE FABRICATED A DOUBLER FOR L/H AIR CONDITIONING BAY HEAT EXCHANGER COMPO SITE DUCT SUPPORT RETAINER AT BS 619, LBL 53, IAW B737-300 SRM 51-70-13, PG. 1-5, TREATED & PRIMED DOUBLER IAW B737-300 SRM 51-70-13, PG.1, FIG.1, INSTALLED DOUBLER IAW BOEING DWG 65-49573, AND B737-300 SRM 51-70-13, PG.1-5, FIG. 1. 2 L 7 2 4F RT A16WE 2002082700165 20020827 00165 NM 2002 8 27 AWXA200200830 1 20020813 A 5315 65317876 CHANNEL BOEING 737 7373B7 1384580 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF L-1 ENTRY WAY CHANNEL (LOWER SCUFF PLATE ATTACHMENT INBOARD SIDE) BS 312 - 344, LBL 61. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER B 737-300 SRM 53-10-15, PG. 101 & 106. REMOVED DAMAGED CHANNEL BS 312 - 344, LBL 61, FABRICATED A NEW CHANNEL, AND INSTALL ED REPAIR IAW B737-300 SRM 53-40-02, PG. 3-4, 10-11, 26, 29, 32, 36, 38, 45, & 63, FIG. 3-4, 6-8, 12, & 14, AND DWG 65-3 1787-6. 2 L 7 2 4F RT A16WE 2002082700166 20020827 00166 NM 2002 8 27 AWXA200200832 1 20020825 A 5320 654583469 STRAP BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1 1/4" CRACK WAS FOUND ON LOWER FRAME TO FRAME STRAP BS 312 - 328, LBL 11. MAIN TENANCE REMOVED PREVIOUSLY INSTALLED REPAIR, FABRICATED A REPAIR PLATE, AND INSTALLED REPAIR IAW B737-300 SRM 53-10-51, PG. 213-219, FIG. 204. 2 L 7 2 4F RT A16WE 2002082700167 20020827 00167 NM 2002 8 27 AWXA200200834 1 20020801 A 5311 6547959502 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/2" CRACK WAS FOUND IN THE AFT CARGO DOORWAY FORWARD DOOR CUTOUT FRAME BS 827, RBL 43, WL 164. MAINTENANCE REMOVED THE THRESHOLD WEB, CLIP FROM STRINGER 27 R/H, INTERCOASTAL ASSEMBLY, 3 EACH STIFFN ERS, AND THE CRACKED FRAME AT BS 827, RBL 43, WL 164. FABRICATED REPAIR FRAME, 2 EACH SPLICE ANGLES, INNER DOUBLER, 2 EA CH TEE ANGLES, AND A SUPPORT ANGLE, AND INSTALLED REPAIR PARTS IAW AWA E.O. 53-10-01 (REV H). 2 L 7 2 4F RT A16WE 2002082700168 20020827 00168 NM 2002 8 27 AWXA200200835 1 20020731 A 5320 654581945 GUSSET BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1" CRACK WAS FOUND ON GUSSET AT AFT END OF NOSE GEAR ACTUATOR SUPPORT FITTING B S 240, BL 0, WL 190. MAINTENANCE REMOVED NOSE GEAR ACTUATOR SUPPORT FITTING AND THE CRACKED GUSSET BS 240, BL 0, WL 190 . FABRICATED A NEW GUSSET, AND INSTALLED GUSSET AND NOSE GEAR ACTUATOR SUPPORT FITTING IAW B737-200 SRM 51-30-2, PG. 8-9 . 2 L 7 2 4F RT A16WE 2002082800001 20020828 00001 WP 2002 8 28 DHL2002806527 1 20020626 A 5522 SKIN DOUG DC8 DC873F 302199F WP ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK, FOUND RT ELEVATOR UPPER SKIN WITH SEVERAL DENTS STA XE 132.750 TO 242.187. REMOVED DETERIORATED SKIN. FABRICATED AND INSTALLED NEW SKIN PER EO DHL020602 DWG EO 3084 EO SEMAN 2002687. 2 L 7 4 4F RT 4A25 2002082800002 20020828 00002 WP 2002 8 28 DHL2002806528 1 20020628 A 5753 RIB DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FOUND LT WING I/B JOINT FLAP LINK RIB SHOWS 4 CRACKS 1 INCH XW 138.000. REMOVED CRACKED RIB PER SRM 51-1-21 PAGE 1. FABRICATED AND INSTALLED PER ATM 00111590, DWG 5652796, EA SEMAN 2002729, SRM 57-7-1 PG 6 AND SRM 51-1-21 PG 1 . 2 L 7 4 4F RT 4A25 2002082800003 20020828 00003 WP 2002 8 28 DHL2002806529 1 20020626 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK, FOUND .5 INCH CRACK IN NR 3 CROSS SLIDE DOOR INNER EDGE. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1B. FAB RICATED DOUBLER PER SRM 51-1-8B FIG 1B. INSTALLED DOUBLER PER SRM 53-2-0 FIG 7B. 2 L 7 4 4F RT 4A25 2002082800004 20020828 00004 WP 2002 8 28 DHL2002806530 1 20020630 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FOUND DURING C-CHECK, FUSELAGE EXTERIOR OVERLAP REPAIR DOUBLER EDGE GAUGED AND DENTED AT STA 1440.000 L-31R AFT CARGO DO OR FRAME. REMOVED DAMAGED REPAIR DOUBLER. FABRICATED AND INSTALLED DOUBLER PER EO DHL 020618, EO3108, EO SEMAN 2002722 . 2 L 7 4 4F RT 4A25 2002082800005 20020828 00005 WP 2002 8 28 DHL2002806532 1 20020703 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 RT WING OUTBOARD LEADING EDGE UPPER SURFACE SKIN CORRODED XFS 566.000 TO XFS 660.000. REMOVED CORROSION, FOUND OUT OF L IMITS IAW SRM 57-2-0 PG 16 ,CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 PG 2 FIG 38. 2 L 7 4 4F RT 4A25 2002082800006 20020828 00006 WP 2002 8 28 DHL2002806533 1 20020723 A 5711 97510821 SPAR CAP DOUG DC8 DC873F 302199F WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 LT WING INBOARD LEADING EDGE UPPER CAP SHOWS CORROSION AND CRACK BETWEEN XFS 20.000 AND XFS 195.000. REMOVED CRACKED UP PER CAP IAW SRM 51-1-20D PAGE 21 AND SRM 51-1-21. INSTALLED NEW UPPER CAP IAW SRM 57-3-3 PAGE 5 DRAWING 9750482, SRM 51 -1-21 PAGE 1, SRM 51-1-20D PAGE 9 AND SRM 51-1-5 PAGE 1. 2 L 7 4 4F RT 4A25 2002082800007 20020828 00007 WP 2002 8 28 DHL2002806534 1 20020717 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 RT WING L/E SHOWS SPOT OF CORROSION AT STA XW257. REMOVED CORROSION ON RT WING L/E, FOUND OUT LIMITS IAW SRM 57-2-0 PG 16. TRIMMED OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW EO DHL 020615 , ED3091, EO SEMAN 2002678. 2 L 7 4 4F RT 4A25 2002082800008 20020828 00008 WP 2002 8 28 DHL2002806536 1 20020718 A 5730 56434111 PANEL DOUG DC8 DC873F 302199F WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 LT WING T/E SKIN UPPER PANEL SHOWS POINTS OF CORROSION XW47.000 - XW75.312. REMOVED CORROSION IAW SRM 57-1-8 PG 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. REMOVED DAMAGED PANEL IAW SRM 51-3-0, INSTALLED NEW PANEL ON LT WING T/E UPPE R SKIN IAW SRM 51-3-0 PAGE 1. 2 L 7 4 4F RT 4A25 2002082800009 20020828 00009 WP 2002 8 28 CALA0200443 1 20020827 A 5330 SKIN DOUG DC9 DC982 3022082 WP STA 275 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 275 LONGERON 30 AFT OF LOWER ADF ANTENNA. THE SKIN SECTION WAS REMOVED AN D REPLACED IAW SRM 51-30-02. 2 L 7 2 4F A6WE 2002082800010 20020828 00010 NM 2002 8 28 CALA0200444 1 20020827 A 5311 FRAME BOEING 737 7373T0 1384582 NM STA 867 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 23589 INSPECTION FOUND FRAME CORRODED AT STA 867 BETWEEN STRINGERS 27L AND 27R. THE CORRODED SECTION OF FRAME WAS REMOVED AND A SHEAR TIE AND FILLER WERE INSTALLED IAW SRM 53-00-07, FIGURE 208. 2 L 7 2 4F RT A16WE 2002082800011 20020828 00011 NM 2002 8 28 CALA0200445 1 20020827 A 5754 SKIN BOEING 737 7373T0 1384582 NM #6 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 23589 INSPECTION FOUND A 2" CRACK IN #6 LEADING EDGE SLAT SKIN AT EDGE OF RIVET HOLE ON SLAT LOWER SIDE BY I/B AUX TRACK. A RE PAIR WAS INSTALLED IAW SRM 57-43-01, FIGURE 206. 2 L 7 2 4F RT A16WE 2002082800012 20020828 00012 NM 2002 8 28 CALA0200447 1 20020828 A 5320 SPLICE PLATE BOEING 737 7373T0 1384582 NM STA 858 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 23589 INSPECTION FOUND AFT CARGO PIT CENTER FLOOR SPLICE PLATE CORRODED AT STA 858. THE CENTER FLOOR SPLICE WAS REMOVED AND RE PLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002082800013 20020828 00013 WP 2002 8 28 DHL2002806537 1 20020718 A 5730 5769859505 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 LT WING STUB WING LEADING EDGE LWR SKIN CRACKED .5 INCH XFS 207.000. FABRICATED AND INSTALLED DOUBLER IAW EO DHL020622, ED-3100, EO SEMAN 2002688, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002082800014 20020828 00014 WP 2002 8 28 DHL2002806838 1 20020701 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 RT WING CENTER LEADING EDGE UPPER SURFACE SKIN SHOWS CORROSION XFS 304.000 - 335.250. REMOVED CORROSION FOUND OUT OF LI MITS IAW SRM 57-2-0 PG 16. CUT CORRODED AREA IAW SRM 57-2-1 PG 2 FIG 38. FABRICATED AND INSTALLED FILLER AND DOUBLER I AW SRM 57-21-1 PG 2 FIG 38 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002082800015 20020828 00015 WP 2002 8 28 DHL2002806839 1 20020703 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 REMOVED CORROSION FROM RT WING OUTBOARD L/E UPPER SURFACE IAW SRM 51-1-8 PG 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT DAMAGED AREA IAW SRM 57-2-1 PG 2 FIG 38. FABRICATED AND INSTALLED FILLER & DOUBLER IAW SRM 57-2-1 PG 2 FI G 38, SRM 51-1-21 PG 1, SRM 51-1-15 PG 1. 2 L 7 4 4F RT 4A25 2002082800016 20020828 00016 WP 2002 8 28 DHL2002806841 1 20020721 A 5730 57695891 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 LT WING CENTER L/E LWR SKIN SHOWS CORROSION XFS 420.000. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. TRIMMED OUT AFFECTED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER ON LT WING CENTER L/E LWR SKIN. 2 L 7 4 4F RT 4A25 2002082800017 20020828 00017 WP 2002 8 28 DHL2002806842 1 20020716 A 5730 576989504 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 RT STUB WING UPPER SURFACE SKIN CORRODED AROUND XILD42.000 - 257.000. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57 -2-0 PG 16. CUT AFFECTED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW EO DHL 020613, ED-3083 & EO SEMAN 200268 0 SRM 51-1-21 PG 1, SRM 51-1-15 PG 1 & SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002082800018 20020828 00018 WP 2002 8 28 DHL2002806843 1 20020716 A 5730 576989504 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 RT STUB WING UPPER SURFACE SKIN CORRODED AROUND XILD42.000 - 257.000. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57 -2-0 PG 16. CUT AFFECTED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW EO DHL 020613, ED-3083 & EO SEMAN 200268 0 SRM51-1-21 PG 1, SRM 51-1-15 PG 1 & SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002082800019 20020828 00019 WP 2002 8 28 DHL2002807008 1 20020627 A 3260 STRIKER DOUG DC8 DC873F 302199F WP LT MLG DOOR DEFECTIVE A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 807DH 45990 GEAR DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION, CYCLED GEAR SEVERAL TIMES PER ABNORMAL PROCEDURES. LIGHT STAYED ILLU MINATED. MAIN GEAR DOOR LIGHT SWITCH NEXT TO F/E'S PANEL HAD NO EFFECT ON DETERMINING WHICH DOOR. REPLACED LT GEAR DOO R STRIKER AND PERFORMED TEST OF DOOR WARNING PER DACO M/M 32-60-00. OP CHECKS GOOD. 2 L 7 4 4F RT 4A25 2002082800020 20020828 00020 WP 2002 8 28 DHL2002807009 1 20020628 A 3260 CONNECTOR DOUG DC8 DC873F 302199F WP COCKPIT LOOSE A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 807DH 45990 DOOR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. PERFORMED ABNORMAL, CYCLED 4 TIMES AND NO EFFECTS. CONTINUED FLIGHT WITH 230 KIAS/ .65M LIMITATION. FOUND LIGHT SOCKET CONNECTIONS LOOSE. CLEANED AND SECURED CONNECTION. RELAMPE D, PERFORMED GEAR SWING AND OPS CK'D OK IAW MM 32-60-00. OK FOR CONTINUED SERVICE. 2 L 7 4 4F RT 4A25 2002082800021 20020828 00021 WP 2002 8 28 DHL2002807010 1 20020719 A 2612 CONNECTOR DOUG DC8 DC873F 302199F WP FIRE LOOP FAULTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807DH 45990 NR 4 B-FIRE LOOP WILL NOT TEST. REPLACED B-LOOP CONNECTOR ON LT SIDE OF CORE LOOP. SYSTEM CHECKS OK IAW 26-10. 2 L 7 4 4F RT 4A25 2002082800022 20020828 00022 EU 2002 8 28 DHL2003366012 1 20020730 A 2612 CONNECTOR AIRBUS 300 A300B4203 3930306 EU NR 1 ENGINE DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 366DH 249 ON PRE-FLT CHECK, FOUND NR 1 ENGINE A-LOOP WILL NOT TEST. CLEANED CONNECTORS ON NR 1 ENGINE A-FIRE LOOP PER A300 MM REF 26-12-12. SYSTEM OPS CHECKS GOOD. OK TO CONTINUE. 2 L 7 2 4F RT A35EU 2002082800023 20020828 00023 EA 2002 8 28 COMA0260493 1 20020824 A 7910 OIL TANK CNDAIR CL600 CL6002B19 1900309 EA LT ENG OVERSERVICED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 934CA 7042 FLIGHT 5596 LEFT ENGINE OIL WARNING MESSAGE.FOUND ENGINE OIL OVER FILLED - DRAINED TO PROPER LEVEL AND RETURNED TO SERVI CE. 2 L 7 2 4F RT A21EA 2002082800024 20020828 00024 EA 2002 8 28 COMA0260494 1 20020822 A 5230 DOOR LATCH CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 956CA 7105 FLIGHT 5622 CARGO DOOR OPEN CAUTION MESSAGE.FOUND HANDLE UNLATCHED - CLOSED AND LATCHED HANDLE. 2 L 7 2 4F RT A21EA 2002082800025 20020828 00025 NM 2002 8 28 DL76L020825 1 20020717 A 2760 O-RING BOEING 767 767332 1382001 NM SPOILER FAILED A DALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 197DN 28454 DURING CRUISE AT FL350 GOT R HYD QTY EICAS MSG AND R HYD RVSR LT ON OVERHEAD PANEL. R HYD QTY AT .47. FOLLOWED PROCEDU RE AND TURNED OFF R ENG HYD PUMP AND R DEMAND PUMP. R HYD QTY STAB AT .37 REST OF FLIGHT. FOUND O-RING ON PLUG AT NR 1 3 SPOILER BLOWN OUT. REPLACED O-RING ON NR 13 SPOILER ACR PLUG. SERVICED HYD SYSTEM. RAN FLT CONTROLS. NO FURTHER LE AKS NOTED. CHECKS OK. 2 L 7 2 4F RT A1NM 2002082800026 20020828 00026 NM 2002 8 28 DL76L020843 1 20020719 A 2432 425404 CHARGER BOEING 767 767332 1382001 NM E/E BAY MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 188DN 27583 MAIN BATTERY CHARGER MESSAGE WHILE INFLIGHT. MTC IN PROGRESS. REPLACED BATTERY CHARGER AND BATTERY SYSTEM, NOW OPS NOR MAL. MSG CLEARED. 2 L 7 2 4F RT A1NM 2002082800027 20020828 00027 EA 2002 8 28 COMA0260495 1 20020823 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 784CA 7319 FLIGHT 5429 GEAR DISAGREE WARNING WHEN GEAR SELECTED DOWN.COULD NOT DUPLICATE EXTENSION AND RETRACT CHECKS WERE NORMAL. 2 L 7 2 4F RT A21EA 2002082800028 20020828 00028 NM 2002 8 28 DL76S020783 1 20020707 A 2121 6066223 FAN BOEING 767 767332 1382001 NM CARGO BAY DAMAGED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 122DL 23436 ON APPROACH, BURNING SMELL IN COCKPIT ALL THE WAY BACK TO ROW 4. SMELL DISSIPATED WITHIN 2 MINUTES. ISOLATED PROBLEM T O LEFT RECIRC FAN. FOUND FAN DAMAGED BY DEBRIS. REMOVED AND REPLACED LT RECIRC FAN. 2 L 7 2 4F RT A1NM 2002082800029 20020828 00029 EA 2002 8 28 COMA0260496 1 20020824 A 3150 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 973CA 7146 FLIGHT 5642 AILERON TRIM CONFIG WARNING DURING T/O.COULD NOT DUPLICATE. CONFIG WARNING SYSTEM FUNCTIONS NORMALLY. 2 L 7 2 4F RT A21EA 2002082800030 20020828 00030 EA 2002 8 28 COMA0260497 1 20020825 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 979CA 7159 FLIGHT 5270 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002082800031 20020828 00031 EA 2002 8 28 COMA0260498 1 20020825 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 708CA 19535 7235 FLIGHT 5699 GEAR DISAGREE WARNING - NLG DID NOT RETRACT.REPLACED THE MLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002082800032 20020828 00032 NM 2002 8 28 DL76S020889 1 20020727 A 5714 111T20053 STIFFENER BOEING 767 767332 1382001 NM CENTER WING BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 116DL 23275 CRACKS WERE FOUND IN THE LBL 10 VERTICAL STIFFENER OF THE CENTER SECTION FRONT SPAR, IN THE WEB OF THE STIFFENER AT THE OVERWING FLOORBEAM TO STIFFENER JOINT. A SPLICE REPAIR WAS ACCOMPLISHED. 2 L 7 2 4F RT A1NM 2002082800033 20020828 00033 NM 2002 8 28 DHL2002745503 1 20020604 A 5320 STIFFENER BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING C-CHECK DISCREPANCY AS FOLLOWS, AFT PRESS BULKHEAD BS 1183 VERTICAL BEAM LBL 17.81 CRACKED AT FWD FLANGE PASSING RADIOS TO LATERAL SIDE WL 273 (NDT FINDING). REMOVED AND REPLACED FRAME IAW B-727 S/B 53-210. INSTALLED PREVENT MOD IA W B-727 S/B 53-210. 2 L 7 3 4F A3WE 2002082800034 20020828 00034 NM 2002 8 28 DHL2002745504 1 20020604 A 5310 SHEAR TIE BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING C-CHECK, IN FWD CARGO SHEAR TIE HAS CORROSION AT BS 720R STR 28R. DAMAGE BEYOND LIMITS IAW B-727 SRM 53-10-1 AND 51-10-1. FABRICATED REPAIR IAW B-727 SRM 53-10-4 FIG 15. INSTALLED SHEAR TIE REPAIR IAW B-727 SRM 53-10-4 FIG 15. 2 L 7 3 4F A3WE 2002082800035 20020828 00035 NM 2002 8 28 DHL2002745505 1 20020604 A 5320 STIFFENER BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING C-CHECK, AFT PRESS BULKHEAD BS 1183 VERTICAL BEAM LBL 36 CRACKED WL 250 APPROX (NDT CONFIRMED). STOP DRILLED CRA CK ON PRESSURE BULKHEAD BEAM IAW B-727 SRM 51-10-1. INSTALLED KIT 65C344406-13 REPAIR MOD IAW B-727 S/B 53-192. 2 L 7 3 4F A3WE 2002082800036 20020828 00036 NM 2002 8 28 DHL2002746007 1 20020620 A 2612 CONNECTOR BOEING 727 727224 1384076 NM NR 3 ENGINE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 ON PERFORMING FURTHER MX CONCERNING ITEM 1P LOG PAGE 270926 FOUND NR 3 ENG FIRE LOOP BROKEN FROM WIRING HARNESS. REPLAC ED CONNECTOR IAW DHL B-727 M/M 20-11-11. NR 3 ENG FIRE WARNING CHECKS GOOD IAW B-727 M/M 26-11-00. 2 L 7 3 4F A3WE 2002082800037 20020828 00037 NM 2002 8 28 DHL2002752002 1 20020726 A 3350 BATTERY BOEING 727 727223 1384074 NM CABIN DISCHARGED A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 752DH 22466 EMERGENCY EXIT LIGHTS BATTERIES LOW. INSTALLED NEW EMERGENCY EXIT LIGHT BATTERIES PER MM 34-50-00. 2 L 7 3 4F A3WE 2002082800039 20020828 00039 NM 2002 8 28 DHL2002754001 1 20020703 A 5754 SLAT BOEING 727 727223 1384074 NM WINGS BIRD STRIKE A DHLA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SO 01 754DH 22008 RTO DUE TO MULTIPLE BIRD STRIKES, RETURN TO BLOCKS FOR INSPECTION. PERFORMED BIRD STRIKE INSPECTION PER MM 05-51-41. N O DAMAGE OR STRIKE IN ENGINES. SOME STRIKES ON LEADING EDGE. NO DAMAGE A/C. OKAY FOR SERVICE. 2 L 7 3 4F A3WE 2002082800040 20020828 00040 NM 2002 8 28 DHL2002754002 1 20020723 A 2420 902F2425 CONTROL PANEL BOEING 727 727223 1384074 NM COCKPIT DEFECTIVE A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 754DH 22008 UPON APPLYING TAKEOFF THRUST AND INITIAL ROLL, NR 2 FIELD & GB OPENED WITH DIFF FAULT SYSTEM 2 INDICATION ON S/O SECONDA RY PANEL ABORTED T/O AND RETURNED TO PARKING. REMOVED AND REPLACED GEN CONTROL PANEL GROUND RAN ALL ENGINES OPS CHECKED GOOD PER 24-20-0. 2 L 7 3 4F A3WE 2002082800041 20020828 00041 NM 2002 8 28 DHL2002755001 1 20020802 A 3350 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 887MA 21857 EXIT LIGHT OVER MAIN FWD ENTRY DOOR DOES NOT WORK. INSTALLED SERVICEABLE BATTERIES ON EXIT LIGHT OVER MAIN FWD ENTRY DO OR, OPS CHECKED GOOD PER MM 33-50-71. 2 L 7 3 4F A3WE 2002082800042 20020828 00042 NM 2002 8 28 DHL2002755002 1 20020814 A 2697 GROUND WIRE BOEING 727 727225 1384077 NM FIRE BOTTLE LOOSE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 887MA 21857 RT FIRE BOTTLE DISCHARGE LT PTT INOP. SECURED GROUND WIRE W438-033-22 IAW WDM 33-19-02. DISCHARGE LIGHT PTT CHECKS GOO D. 2 L 7 3 4F A3WE 2002082800043 20020828 00043 NM 2002 8 28 DHL2002755003 1 20020816 A 2120 ODOR BOEING 727 727225 1384077 NM CABIN DETECTED A DHLA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 887MA 21857 STRONG FUEL LIKE ODOR NOTED WHEN REQUESTING A WARMER TEMP FROM LEFT PACK. OPERATED PACKS THROUGH ALL TEMP RANGES NO FUE L FUMES NOTED. 2 L 7 3 4F A3WE 2003021000143 20030210 00143 NM 2003 2 10 DHL2002780001 1 20021218 A 2781 CONTROL UNIT BOEING 727 727223 1384074 NM LE FLAPS MALFUNCTIONED A DHLA L ABORTED APPROACH O OTHER AP APPROACH 1 SO 01 780DH 22006 WHEN FLAPS FIVE SELECTED THE NR 2 LE FLAP VERY SLOW TO EXTEND. GO AROUND ACCOMPLISHED. NR 2 LE FLAP EXTENDED PROPERLY ON CE GO AROUND INITIATED. OPERATED FLAPS SEVERAL TIMES, COULD NOT DUPLICATE ON GROUND, OPS CHECKED NORMAL IAW M/M 27-81-00 . 2 L 7 3 4F A3WE 2002082800044 20020828 00044 WP 2002 8 28 DHL2002801014 1 20020723 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 STANDBY EMERGENCY CHECK INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW 33-50-1 ,TESTED OK. 2 L 7 4 4F RT 4A25 2002082800045 20020828 00045 WP 2002 8 28 DHL2002801015 1 20020717 A 2510 INERTIA REEL DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 SECOND OFFICER'S SHOULDER STRAP STUCK. VERIFIED TO BE STUCK. REMOVED AND REPLACED INERTIA ASSY. OPS CHECKS GOOD IAW D C8 MM 25-11-2. 2 L 7 4 4F RT 4A25 2002082800046 20020828 00046 WP 2002 8 28 DHL2002802008 1 20020810 A 5270 SWITCH DOUG DC8 DC873 302199C WP CABIN DOOR MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 802DH 46076 CABIN DOOR OPEN LIGHT ILLUMINATED INFLIGHT. ACCOMPLISHED ABNORMAL PROCEDURE AND CONTINUED PRESSURIZED FLIGHT. REMOVED AND REPLACED CABIN DOOR MICRO SWITCH. PERFORMED OPS CK. FOUND NORMAL IAW MM 33-20 & 52-70-0. 2 L 7 4 4F RT 4A25 2002082800047 20020828 00047 EA 2002 8 28 COMA0260499 1 20020823 A 2150 CAGE CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 920CA 7022 FLIGHT 5461 CARGO OVERHEAT CAUTION MESSAGE.REPOSITIONED ANIMAL CAGE THAT WAS BLOCKING AIR VENT. 2 L 7 2 4F RT A21EA 2002082800048 20020828 00048 WP 2002 8 28 DHL2002802009 1 20020810 A 2510 5641031519 SEAT DOUG DC8 DC873 302199C WP COCKPIT DEFECTIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 324 127 46076 CAPT SEAT WILL NOT ADJUST VERTICALLY. REMOVED AND REPLACED CAPT'S SEAT, OPS CHECK GOOD IAW DC8 MM 25-11-1. 2 L 7 4 4F RT 4A25 2002082800049 20020828 00049 WP 2002 8 28 DHL2002805050 1 20020731 A 7712 8DJ324WAC1 INDICATOR DOUG DC8 DC873F 302199F WP COCKPIT FAULTY A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 805DH 46125 NR 1 ENGINE UNABLE TO DEVELOP THRUST ON TAKEOFF ABOVE 69 PERCENT. REMOVED AND REPLACED NR 1 ENG N1 IND PER 77-12-1, OPS CHECK GOOD PER JRH CHAP 11. 2 L 7 4 4F RT 4A25 2002082800050 20020828 00050 WP 2002 8 28 DHL2002806500 1 20020630 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK FOUND FUSELAGE EXTERIOR, AFT CARGO COMPARTMENT DOOR JAMB SHOWS DAMAGED SKIN REPAIR STA FS 1400.000 AND L- 31R. FABRICATED A NEW REPAIR DOUBLER PER EO DHL 020619, EO 3109, EO SEMAN 2002723. INSTALLED NEW DOUBLER PER EODHL0206 19, EO 3109, EO SEMAN 2002723. 2 L 7 4 4F RT 4A25 2002082800051 20020828 00051 WP 2002 8 28 DHL2002806504 1 20020710 A 5720 FLANGE DOUG DC8 DC873F 302199F WP WING BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK, FOUND LT FWD AUX TANK UPPER CAP FLANGE 2 BROKEN AT STA XFS 20.000. FABRICATED DOUBLER PER SRM 57-2-0 FI G 2. INSTALLED DOUBLER PER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002082800052 20020828 00052 WP 2002 8 28 DHL2002806506 1 20020630 A 5710 FORMER DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK FOUND RT WING CTR L/E LOWER FORMER 1 INCH CRACK STA XFS 329.000. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2 . FABRICATED DOUBLER PER SRM 57-2-0 FIG 2. INSTALLED DOUBLER PER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002082800053 20020828 00053 WP 2002 8 28 DHL2002806507 1 20020629 A 5710 FORMER DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED 1 INCH AT XFS 603.750. STOP DRILLED CRACK PER S RM 57-2-0 FIG 2. FABRICATED DOUBLER PER SRM 57-2-0 FIG 2. INSTALLED NEW DOUBLER PER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002082800054 20020828 00054 WP 2002 8 28 DHL2002806508 1 20020702 A 5522 SKIN DOUG DC8 DC873F 302199F WP ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FOUND AT C-CHECK RT ELEVATOR T/E SKIN HAS A .5 INCH CRACK AT STA XE 136.000. STOP DRILLED CRACK PER SRM 55-2-0 FIG 2. FABRICATED DOUBLER PER SRM 55-2-0 FIG 2. INSTALLED DOUBLER PER SRM 55-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002082800055 20020828 00055 WP 2002 8 28 DHL2002806509 1 20020624 A 5330 5706675402 PANEL DOUG DC8 DC873F 302199F WP FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK FOUND FUSELAGE LWR FILLET 728 RT EXTERNAL SKIN DELAMINATED. REMOVED DELAMINATED FILLET PANEL PER SRM 51- 3-0 PG 1. INSTALLED NEW FILLET PANEL PER SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2002082800056 20020828 00056 WP 2002 8 28 DHL2002806510 1 20020626 A 5730 56488962 PANEL DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK FOUND RT WING T/E UPPER PANEL SKIN DELAMINATED STA XA 681.000-613.000. REMOVED AND REPLACED PANEL PER SR M 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2002082800057 20020828 00057 WP 2002 8 28 DHL2002806511 1 20020624 A 5730 56110102 PANEL DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK FOUND RT WING T/E LWR PANEL INNER AND EXTERNAL SKIN DELAMINATED BETWEEN XW 5.000 TO XW 33.000. REMOVED A ND REPLACED DELAMINATED PANEL PER SRM 51-3-0 PG 7 AND SRM 51-31 PG 1. 2 L 7 4 4F RT 4A25 2002082800058 20020828 00058 WP 2002 8 28 DHL2002806512 1 20020625 A 5280 56489321 SKIN DOUG DC8 DC873F 302199F WP LT MLG DOOR DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FOUND DURING C-CHECK, LT WING MLG DOOR LWR SKIN DELAMINATED. REMOVED OUTER DOOR FROM MLG PER SRM 51-3-0 PG 1. INSTALLE D NEW OUTER DOOR ON MLG PER SRM 51-3-0 PG 1 AND SRM 51-3-1 PG 1. 2 L 7 4 4F RT 4A25 2002082800059 20020828 00059 WP 2002 8 28 DHL2002806513 1 20020701 A 5754 SKIN DOUG DC8 DC873F 302199F WP L/E SLOT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FOUND AT C-CHECK, LT INBOARD SLOT L/E INTERNAL SKIN CRACKED 4 INCHES AT STA XFS 250.000. PERFORMED MAJOR REPAIR PER SRM 57-3-3 PG 9-11. REMOVED DAMAGED SKIN PER SRM 51-1-21 PG 1. FABRICATED NEW SKIN PER SRM 57-3-3 PG 9-11. INSTALLED NEW INTERNAL SKIN PER SRM 57-3-3 PG 9-11. 2 L 7 4 4F RT 4A25 2002082800060 20020828 00060 WP 2002 8 28 DHL2002806514 1 20020626 A 5754 STRUCTURE DOUG DC8 DC873F 302199F WP L/E SLOT DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK, FOUND RT INBOARD SLOT WITH ELONGATED HOLES AT STA XFS 250.000. TRIMMED OUT DAMAGED AREA. FABRICATED DO UBLERS AND A FILLER PER EODHL020620, EO3093, EO SEMAN 2002682. INSTALLED FILLER AND DOUBLER PER EODHL020620, EO3093, EO SEMAN 2002682. 2 L 7 4 4F RT 4A25 2002082800061 20020828 00061 WP 2002 8 28 DHL2002806515 1 20020626 A 5320 47723591 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK, FOUND MAIN CARGO COMPARTMENT FLOOR PANEL CENTER TRACK FITTING CRACKED STA 200.000. REMOVED CRACKED FITT ING PER SRM 51-1-20D PG 21. INSTALLED NEW FITTING PER SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002082800062 20020828 00062 WP 2002 8 28 DHL2002806516 1 20020627 A 5710 FORMER DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK, FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED .625 INCH AT XFS 641.250. STOP DRILLED CRACK P ER SRM 57-2-0 PG 9. FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10. INSTALLED NEW ANGLE AND FASTENERS PER SRM 57- 2-0 PG 9-10 AND SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002082800063 20020828 00063 WP 2002 8 28 DHL2002806517 1 20020607 A 5710 FORMER DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK, FOUND LT WING O/B LEADING EDGE FORMER CRACKED .5 INCH. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABR ICATED DOUBLER PER SRM 57-2-0 PG 9-10. INSTALLED DOUBLER WITH NEW FASTENERS PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1 . 2 L 7 4 4F RT 4A25 2002082800064 20020828 00064 WP 2002 8 28 DHL2002806518 1 20020626 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK, FOUND RT WING T/E UPPER SKIN DEFECT XW 761.695. REMOVED DAMAGED SKIN PANEL. FABRICATED AND INSTALLED N EW SKIN PANEL PER EODHL 020601, EO3082, EO SEMAN2002679. 2 L 7 4 4F RT 4A25 2002082800065 20020828 00065 WP 2002 8 28 DHL2002806519 1 20020627 A 5754 STRUCTURE DOUG DC8 DC873F 302199F WP L/E SLOT DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK, FOUND LT WING I/B SLOT UPPER SURFACE SKIN HOLES ELONGATED XS 250.000. CUT OUT DAMAGED AREA. FABRICATED DOUBLERS AND FILLER PER EODHL020606, EO-3088, EO SEMAN2002671. INSTALLED FILLERS AND DOUBLERS PER EODHL020606, EO-3088 , EO SEMAN2002671. 2 L 7 4 4F RT 4A25 2002082800066 20020828 00066 WP 2002 8 28 DHL2002806520 1 20020630 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FOUND DURING C-CHECK, RT WING O/B LEADING EDGE LWR SURFACE .375 INCH CRACK STA XFS 597.000. STOP DRILLED CRACK. FABRIC ATED AND INSTALLED DOUBLER PER EO DHL020608, DWG EO3104 EO SEMAN2002693. 2 L 7 4 4F RT 4A25 2002082800067 20020828 00067 WP 2002 8 28 DHL2002806521 1 20020630 A 5710 FORMER DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FOUND DURING C-CHECK, RT WING CTR L/E LWR FORMER 1 INCH CRACK STA XFS347.750. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10 . FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10. INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10. 2 L 7 4 4F RT 4A25 2002082800068 20020828 00068 WP 2002 8 28 DHL2002806522 1 20020629 A 5710 FORMER DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK, FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED .5 INCH XFS 622.500. STOP DRILLED CRACK PER SR M 57-2-0 PG 9-10. FABRICATED AND INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002082800069 20020828 00069 WP 2002 8 28 DHL2002806523 1 20020629 A 5710 FORMER DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK, FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED .25 INCH XFS 691.250. STOP DRILLED CRACK PER S RM 57-2-0 PG 9-10. FABRICATED AND INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002082800070 20020828 00070 WP 2002 8 28 DHL2002806524 1 20020630 A 5710 FORMER DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FOUND RT WING CTR L/E FORMER 1 INCH CRACK STA XFS 310.250. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. FABRIC ATED AND INSTALLED DOUBLER PER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002082800071 20020828 00071 WP 2002 8 28 DHL2002806525 1 20020629 A 5710 FORMER DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 DURING C-CHECK, FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED .5 INCH AT STA XFS 697.500. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED AND INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 7. 2 L 7 4 4F RT 4A25 2002082800072 20020828 00072 WP 2002 8 28 DHL2002806526 1 20020627 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FOUND AT C-CHECK, D BELLY DOOR INTERCOSTAL THAT SUPPORTS HINGES SHOWS DOUBLER CRACKED .5 INCH. REMOVED CRACKED DOUBLER PER SRM 53-2-0. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2002082800073 20020828 00073 EA 2002 8 28 COMA0260500 1 20020823 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 708CA 7235 FLIGHT 5288 GEAR DISAGREE WARNING AFTER T/O.COULD NOT DUPLICATE - FOUND NO DISCREPANCIES DURING GEAR RETRACT AND EXTEND CHECKS. 2 L 7 2 4F RT A21EA 2002082800075 20020828 00075 NM 2002 8 28 DL777020789 1 20020711 A 3150 WARNING SYSTEM BOEING 777 777232 1385232 NM COCKPIT FALSE ACTIVATION A DALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 860DA 29951 STATUS MSG LEFT EQUIP COOLING FAN. PULLED AND SECURED EQUIP COOLING SUPPLY C/B P110 PANEL. DISCONNECTED AND STOWED CON NECTOR DB21581. 2 L 7 2 4F RT T00001SE 2002082800076 20020828 00076 NM 2002 8 28 DL777020908 1 20020805 A 3350 D71702001 POWER SUPPLY BOEING 777 777232 1385232 NM CABIN UNSERVICEABLE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 877DA 29739 AFT GALLEY EMERGENCY LIGHTS INOP. FOUND POWER SUPPLY BAD. REPLACED POWER SUPPLY. 2 L 7 2 4F RT T00001SE 2002082800077 20020828 00077 NM 2002 8 28 UIEA200200033 1 20020819 A 5310 65B150745 BEAM BOEING 747 747243B 1384830 NM GE CF34 CF34* NE BS1344,1354 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURING CURRENT (C) CHECK AT SIAEC FOUND LOWER KEEL BEAM CHORD INBOARD VERTICAL FLANGE CRACKED 10 INCH FROM BS 1344 TO 13 54 AT LBL 9.0. LEVEL 1 CORROSION PRESENT IN CRACKED AREA OF VERTICAL WEB THROUGH ABOUT 50 PERCENT OF THE ORIGINAL THIC KNESS. CRACKED/ CORRODED AREA TRIMMED AWAY. AREA VISUALLY INSPECTED FOR ADDITIONAL CRACKS/CORROSION. NONE FOUND. FAB RICATED FILLER AND REPAIR DOUBLER. INSTALLED IAW SRM. 2 L 7 4 4F 4 F A20WE E15NE 2002082800078 20020828 00078 NM 2002 8 28 DLM11020682 1 20020618 A 2910 HYDRAULIC LINE DOUG MD11 MD11 3023602 NM HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 815DE 48624 FLUID LOSS NR 1 SYSTEM. QTY DOWN TO 1.0 WITH HYD 1 FAIL / ALERT. RETURNED TO ATL. FOUND FLUID LEAKING NEAR O/B LEFT W ING FLAP O/B ACT. NEW SECTION OF LINE ON O/B LEFT WING FLAP O/B ACT PER MM 20-0-07. LINE NEEDS LEAK CHECK. PERFORMED CAVITATION PER MM. OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2002082800079 20020828 00079 NM 2002 8 28 DLM11020850 1 20020721 A 2530 411000137 COFFEEMAKER DOUG MD11 MD11 3023602 NM GALLEY MALFUNCTIONED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 810DE 48565 DURING TAXI OUT, F/A REPORTS HEARING LOUD POP AND SEEING SPARKS FLY OUT OF COFFEEMAKERS IN AFT GALLEY. F/A`S REPORT SME LLING ELECTRICAL SMOKE. INSPECTED COFFEEMAKERS AND COMPARTMENT WIRING, NO TROUBLE FOUND OR EVIDENCE OF ELECTRICAL ARCIN G. REPLACED AFT GALLEY COFFEEMAKERS 3 AND 4. 2 L 7 3 4F RT A22WE 2002082800080 20020828 00080 NM 2002 8 28 UIEA200200034 1 20020819 A 5510 65B036202 SKIN BOEING 747 747243B 1384830 NM GE CF34 CF34* NE RH STAB STA343 CORRODED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 517MC 66399 23300 DURING CURRENT (C) CHECK AT SIAEC FOUND RIGHT HORIZONTAL STABILIZER BOTTOM SKIN AT STA 343 OUTER SURFACE CORRODED (LEVEL 2). FASTENERS REMOVED IN THE AFFECTED AREA. ALL HOLES CHECKED FOR CORROSION, OVER-SIDED AND HFEC INSPECTED FOR CRACKS. NO ADDITIONAL CORROSION ON CRACKING FOUND. CORROSION AREA BLENDED, MEASURED, FLAP PEENED, ALODINE TREATED AND PRIME P AINTED. ORIGINAL SKIN MEASURED 0.120, AFTER BLENDING 0.091 REMAINS. REPAIRS CARRIED OUT IAW SRM. REPAIR IS TIME LIMIT ED WITH PERMANENT REPAIRS TO BE CARRRIED OUT WITHIN 18 MONTHS OR NEXT (C) CHECK. 2 L 7 4 4F 4 F A20WE E15NE 2002082800081 20020828 00081 NM 2002 8 28 DLM11020863 1 20020723 A 4930 FUEL CONTROL DOUG MD11 MD11 3023602 NM APU MALFUNCTIONED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 801DE 15615 48472 1 SMOKE AND ACRID SMELL IN THE AFT CABIN WITH ENGINE SHUT DOWN AND USING APU PNEUMATICS. REMOVED AND REPLACED APU FUEL CO NTROL UNIT. NO LEAKS FROM FUEL CONTROL. CHECKS GOOD. APU CHECKS GOOD. REMOVED MCO. 2 L 7 3 4F RT A22WE 2002101800045 20021018 00045 NM 2002 10 18 371PA0010 1 20020826 A 3350 FUSE BOEING 737 737306 13844BG NM BATTERY CHARGER BLOWN A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 371PA 23543 AFT LT BULLNOSE EMERGENCY EXIT AISLE LIGHT OUT. REPLACED PICO FUSE IN RT AFT BATTERY PACK CHARGER IAW 737MM 33-51-21. 2 L 7 2 4F RT A16NE 2002082800082 20020828 00082 NM 2002 8 28 TSAA0221175 1 20020817 A 2131 7638101 CONTROLLER BOEING 737 737230 1384401 NM PWA JT8 JT8D9 52048 NE CABIN PRESSURE MALFUNCTIONED A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 820AL 22138 ON CLIMB OUT, AIRCRAFT WAS UNABLE TO MAINTAIN PRESSURIZATION. AIRCRAFT RETURNED AND MADE AN UNEVENTFUL LANDING. MAINT ENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. BITE AND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS R ETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002082800085 20020828 00085 NM 2002 8 28 TSAA0233154 1 20020629 A 3350 1000629 LIGHT BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D NE CABIN DAMAGED A TSAA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED FORWARD ENTRY DOOR IDENTIFIER LIGHT ASSEMBLY DUE TO DAMAGE. OPS CHECK, OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002082800086 20020828 00086 NM 2002 8 28 TSAA0233156 1 20020627 A 3350 8621006 BATTERY PACK BOEING 737 737282C 13844AU NM PWA JT8 JT8D NE CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR1 AND NR2 EMERGENCY FLOOR LIGHT BATTERIES DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002082800087 20020828 00087 NM 2002 8 28 TSAA0233157 1 20020627 A 3350 9221009 BATTERY PACK BOEING 737 737282C 13844AU NM PWA JT8 JT8D NE CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED LEFT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT BATTERY DUE TO INOPERATIVE. OPS CHECK, OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002082800091 20020828 00091 SO 2002 8 28 SWIA200211094 1 20020729 A 2750 3471001001 FCU EMB 120 EMB120ER 3260203 SO T/E FLAP MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 581SW 6159 6159 120349 FLAP DISAGREEMENT ON INBOARD PAIR. CYCLED 3 TIMES AFTER TAKEOFF. RETURNED TO DENVER. INSTALLED SERVICEABLE FLAP CONTR OL UNIT. REMOVED AND REPLACED FLAP ANNUNCIATOR. CLEANED CANNON PLUGS & TRACKS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002082800092 20020828 00092 SO 2002 8 28 SWIA200211095 1 20020714 A 5753 12040327001 STRUCTURE EMB 120 EMB120ER 3260203 SO FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 291SW 120318 LEFT HAND NACELLE FLAP NEEDS TO BE REPLACED DUE TO NUMEROUS INTERNAL CRACKS. REPLACED LEFT NACELLE FLAP WITH SERVICEABL E PART. 2 L 7 2 4T RT A31SO 2002082800093 20020828 00093 EA 2002 8 28 SWIA200211096 1 20020711 A 5755 FITTING CNDAIR CL600 CL6002B19 1900309 EA SPOILERON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 RIGHT SPOILERON INBOARD ANTI-ROTATION FITTING IS BENT AND CRACKED. RIGHT SPOILERON INBOARD ANTI-ROTATION FITTING REPLAC ED IAW CRJ MM 27-64-01-420-801. 2 L 7 2 4F RT A21EA 2002082800094 20020828 00094 SO 2002 8 28 SWIA200211097 1 20020630 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT & LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 270YV 120270 LEFT ENGINE FRAME NR 1 CRACKED AT I/B TORSION MOUNT. RIGHT ENGINE FRAME NR 1 CRACKED AT OUTBOARD TORSION MOUNT. REMOV ED AND REPLACED BOTH ENGINES FRAME 1 PER SB 120-54-0036 REV 02. 2 L 7 2 4T RT A31SO 2002082800095 20020828 00095 SO 2002 8 28 SWIA200211098 1 20020630 A 5420 BRACKET EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 270YV 120270 LEFT HYDRAULIC PACK OUTBOARD LOWER MOUNT BRACKET CRACKED. REPLACED LEFT HYDRAULIC PACK OUTBOARD LOWER MOUNT BRACKET WIT H SERVICEABLE UNIT. 2 L 7 2 4T RT A31SO 2002082800096 20020828 00096 SO 2002 8 28 SWIA200211099 1 20020630 A 5320 SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 270YV 120270 HORIZONTAL SUPPORT BETWEEN FRAMES 12 & 13, JUST AFT OF PILOT'S DV WINDOW, IS CRACKED. REPLACED SUPPORT BETWEEN FRAMES 1 2 & 13 JUST AFT OF PILOT'S DV WINDOW PER SRM 51-40-00. 2 L 7 2 4T RT A31SO 2002082800097 20020828 00097 SO 2002 8 28 SWIA200211100 1 20020630 A 5320 12006144003 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 270YV 120270 CENTER FLOOR PROP BUCKLED AND CRACKED AT FRAME 45. ALSO SKIN SUPPORT CLIP JUST BELOW IT BENT. REPLACED CARGO CENTER FL OOR PROP AT FRAME 45 AND SKIN SUPPORT CLIP BELOW IT PER SRM 51-4-00. 2 L 7 2 4T RT A31SO 2002082800098 20020828 00098 SO 2002 8 28 SWIA200211101 1 20020714 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 291SW 120318 CRACKED FRAME BEHIND CAPTAIN'S DV WINDOW. REPLACED FRAME IAW 120 SRM 51-10-02. 2 L 7 2 4T RT A31SO 2002082800099 20020828 00099 SO 2002 8 28 SWIA200211102 1 20020729 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 563SW 120338 EMERGENCY EXIT SIGNS AND FLOOR EMERGENCY FLOOR LIGHTS ON BATTERY NR 2 INOP. REPLACED MIDDLE BATTERY PACK. OPS CHECK GO OD ON CABIN EMERGENCY LIGHT. 2 L 7 2 4T RT A31SO 2002082800100 20020828 00100 EA 2002 8 28 SWIA200211103 1 20020729 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA RUDDER CONTROL DISCONNECTED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 432SW 7548 RUDDER TRIM WILL ONLY GO NOSE RIGHT. SOLDERED WIRE BACK ON CONTROL POTENTIOMETER. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002082800101 20020828 00101 EA 2002 8 28 SWIA200211104 1 20020730 A 3241 ANTI-SKID SYS CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 07 431SW 7536 UPON LANDING GEAR EXTENSION AT SBA RECEIVED ANTI-SKID INBOARD AND OUTBOARD EICAS MESSAGES. FOLLOWED QRH PROCEDURE. FOU ND THAT AVAILABLE LANDING DISTANCE WAS VERY NEAR BOOK LIMIT WITH BOTH ANTI-SKID INOP. DIVERTED TO LAX. PULLED AND RESE T BOTH ANTI-SKID CB'S. TURNED ON HYDRAULICS, SET ANTI-SKID TO ARM AND OPERATED SYSTEM SEVERAL TIMES. NO MESSAGES. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2002082800102 20020828 00102 SO 2002 8 28 SWIA200211105 1 20020801 A 5720 STRUCTURE EMB 120 EMB120ER 3260203 SO LT WING LEAKING A SWIA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 NM 07 188SW 5918 1412 120039 LEFT OUTBOARD FLAP ACTUATOR REMOVED DUE TO FUEL CONTAMINATION ON FLAP FROM FUEL LEAK. REPAIRED LEAK IN FUEL CELL & INST ALLED ACTUATOR IAW 28-10-00 & 27-50-00. 2 L 7 2 4T RT A31SO 2002082800103 20020828 00103 EA 2002 8 28 SWIA200211106 1 20020731 A 2421 755469D IDG CNDAIR CL600 CL6002B19 1900309 EA NR 1 ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 905SW 5105 5105 7437 GENERATOR NR 1, LEFT WINDSHIELD HEAT AND LEFT WINDOW HEAT CAUTION MESSAGES ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAK EOFF AND COMPLIED WITH QRH. COULD NOT RESET GENERATOR NR 1. REMOVED AND REPLACED LEFT IDG IAW CRJ MM 24-11-01. OPS CH ECK GOOD. 2 L 7 2 4F RT A21EA 2002082800104 20020828 00104 NE 2002 8 28 SWIA200211107 2 20020801 A 7200 CF34 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF341A NE LEFT OVERTEMP A SWIA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 NM 07 588SW 1738 1738 7069 807261 DURING TAKEOFF, LEFT ENGINE ITT WENT TO 907 DEGREES, FLASHING RED. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE I AW MM 71-00-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2002082800105 20020828 00105 SO 2002 8 28 SWIA200211108 1 20020727 A 2752 3430001005 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 NM 07 561SW 6017 6017 120335 LEFT INBOARD FLAP WILL NOT RETRACT EVEN WITH OVERRIDE. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-07. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002082800106 20020828 00106 EA 2002 8 28 SWIA200211110 1 20020808 A 2433 MS179762 TRU CNDAIR CL600 CL6002B19 1900309 EA NR 1 FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 588SW 7069 ESSENTIAL TRU 1 FAILED ON CLIMBOUT. PERFORMED QRH PROCEDURE. RETURNED TO AIRPORT. REMOVED & REPLACED ESSENTIAL TRU 1 AND NR 1 ESS TRU SHUNT. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002082800107 20020828 00107 EA 2002 8 28 SWIA200211111 1 20020808 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 594SW 4785 4785 7285 ON TAXI IN WITH FLAPS TO 20 DEGREES, FLAPS FAIL CAUTION. REMOVED & REPLACED FCU WITH SERVICEABLE UNIT. ALSO COMPLIED W ITH AD 98-20-01. 2 L 7 2 4F RT A21EA 2002082800108 20020828 00108 SO 2002 8 28 SWIA200211112 1 20020806 A 3150 WARNING SYSTEM EMB 120 EMB120RT 3260202 SO COCKPIT FALSE ACTIVATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 269UE 120194 ON TAKEOFF GOT TRIPLE CHIME EEC WARNING. ABORTED TAKEOFF. SUSPECT LEFT EEC THE CULPRIT, LOWER NP THAN RT ON FFOD. INS PECTED CANNON PLUGS AND WIRING FOR CHAFING ON LT ENGINE EEC. RAN ENGINE FOR TRIM CHECK AND TAXIED AIRCRAFT. COULD NOT DUPLICATE. OPS CHECK GOOD. NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2002082800109 20020828 00109 EA 2002 8 28 SWIA200211113 1 20020808 A 2720 SWITCH CNDAIR CL600 CL6002B19 1900309 EA RUDDER CONTAMINATED A SWIA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 NM 07 906SW 7510 ABORTED T/O DUE TO A RUDDER MISCONFIG. RUDDER TRIM CONTROL KNOB MIS-RIGGED. REPLACED RUDDER AND AILERON TRIM PANEL. R UDDER TRIM OPS CHECK GOOD. FOUND FAULTY RUDDER SWITCH. 2 L 7 2 4F RT A21EA 2002082800110 20020828 00110 SO 2002 8 28 SWIA200211114 1 20020801 A 3350 D36604001 BATTERY EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 196CA 5726 5726 120196 DURING TAXI FOR TAKEOFF, FLOOR LEVEL EMERGENCY LIGHTING FROM ROW 6 TO AFT OF AIRCRAFT ILLUMINATED. COULD NOT BE EXTINGU ISHED. REPLACED EMERGENCY LIGHT BATTERY AT ROW 8. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002082800111 20020828 00111 2002 8 28 SWIA200211115 4 20020802 A 3455 6222362001 RECEIVER EMB 120 EMB120ER 3260203 SO ADF FAILED A SWIA A UNSCHED LANDING O OTHER DE DESCENT 1 NM 07 190SW 5189 5189 120050 WHILE HOLDING AT WYS, ADF FAILED IN FLIGHT. DIVERTED TO IDA. REPLACED ADF RECEIVER. OPS CHECKS GOOD IAW MM 34-53-00. 2 L 7 2 4T RT A31SO 2002082800112 20020828 00112 SO 2002 8 28 SWIA200211116 1 20020805 A 2752 3430001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP DEFECTIVE A SWIA O OTHER F FLT CONT AFFECTED LD LANDING 1 NM 07 393SW 6131 6131 120330 INBOARD FLAPS ARE CYCLING IN AND OUT 1 TO 2 LIGHT BARS AFTER LANDING WHEN FLAPS ARE RETRACTED. REMOVED & REPLACED RIGHT INBOARD FLAP ACTUATOR. OPS CHECK GOOD AND NO LEAKS NOTED. 2 L 7 2 4T RT A31SO 2002082800113 20020828 00113 2002 8 28 SWIA200211117 4 20020801 A 3414 320AS1 INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 290SW 6038 6038 120317 ON TAKEOFF ROLL AT 30 KNOTS, GOT AURAL WARNING HIGH SPEED. ABORTED TAKEOFF. REPLACED NR 2 AIR SPEED INDICATOR. CHECKE D SYSTEM WITH PITOT/STAT TESTER. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002082800114 20020828 00114 NM 2002 8 28 DHL2002743012 1 20020826 A 2612 105080037506 FIRE LOOP BOEING 727 727225 1384077 NM A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 743DH 22438 1) APU FIRE TEST INOP. 2) DEFFERED APU FIRE DETECTION SYSTEM AS PER DHL MEL 26-11. CAT."C" CONTROL NO. 10225. PLACARD INSTALLED.3) REF. DMI #10225 APU FIRE DETECTION INOP. 4) CHECKED AND SWAPPED APU CONTROL PANEL, FIRE DETECT. POWER UNI T R-51 R-97 NO HELP. RETURNED ORIGINAL PARTS. DMI #10225 STILL OPEN. (WITH APU RUNING TEST FIRE DET. OPS GOOD)5) REF. D MI #10225. APU FIRE DET. INOP. 6) REMOVED & REPLACED APU SENSOR/RESPONDER PER M/M 26-15-2. SYS. OPS CKS NORMAL - DMI #1 0225 CLEARED. 2 L 7 3 4F A3WE 2002082800115 20020828 00115 NM 2002 8 28 UPS02239190 1 20020813 A 5330 SKIN BOEING 727 72731C 1384011 NM BS418-441,S2L-4L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C CORROSION FOUND AT LAP JOINT S4L. LFEC INSPECTION CARRIED OUT FROM B S 360 TO BS 440. MATERIAL LOSS IN DICATION FROM BS 440 TO BS 411 APPR OX. 20% - 30%. CORRODED INTERNAL DOUBLER ALSO FOUND TO BE DISBONDED. DOUBLER REMOVE D IAW SRM 51-30-2. REPAIR CARRIED OUT IAW SMRO EO 2002-044-003, REF. UPS EO B727-5330-1 7405-A. 2 L 7 3 4F A3WE 2002082800116 20020828 00116 NM 2002 8 28 UPS02239191 1 20020815 A 5310 WEB BOEING 727 72731C 1384011 NM BS 235 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C CRACK FOUND IN NLG FWD L/H PRESSURE WEB AT BS 235 APPROX. CRACK REMOVED IAW SRM 51-40-2. HFEC INSP ECTION CONFIRMED CRACK REMOV AL. REPAIR PARTS FABRICATED AND REPAIR INSTALLED IAW SRM 51-40-2, FI G. 1. 2 L 7 3 4F A3WE 2002082800117 20020828 00117 NM 2002 8 28 UPS02239194 1 20020817 A 5710 651620112 STIFFENER BOEING 727 72731C 1384011 NM LOWER END CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C LOWER END OF STIFFENER AT WS 210, R/H WING REAR SPAR, IS CORRODED STIFFENER REPLACED IAW SMRO EO 2 002-044-006, REF. UPS ENGINEERING FI LE NO. 727-57-20060. 2 L 7 3 4F A3WE 2002082800118 20020828 00118 NM 2002 8 28 ABXA020088 1 20020409 A 5300 140T21202249 SHEAR TIE BOEING 767 767200 1385120 NM FWD LWR CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 DEEP CORROSION ON SHEAR TIES AT STATION 742, BETWEEN STRINGERS 36 LEFT - 39 RIGHT. REPLACED SHEAR TIES INAW B767 AMM. 2 L 7 2 4F RT A1NM 2002082800119 20020828 00119 NM 2002 8 28 UPS02239197 1 20020813 A 5310 WEB BOEING 727 72731C 1384011 NM BS 269.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C CRACKS FOUND IN NLG W/WELL PRESSURE WEB AT BS 269.5, 4" BELOW THE CE ILING ON THE R/H PRESSURE WEB ARE A. NEW WEB AND DOUBLERS FABRICATED AND INSTALLED IAW DRAWING 65-18414 2 L 7 3 4F A3WE 2002082800120 20020828 00120 NM 2002 8 28 ABXA020090 1 20020605 A 5300 143T3213U3 ANGLE BOEING 767 767200 1385120 NM FWD LWR CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 CORRODED ANGLE BETWEEN STATIONS 632 - 654 AND BETWEEN STRINGERS 34 - 35. REPLACED ANGLE IAW B767 AMM. 2 L 7 2 4F RT A1NM 2002082800121 20020828 00121 NM 2002 8 28 ABXA020091 1 20020409 A 5300 140T2102245 SHEAR TIE BOEING 767 767200 1385120 NM FWD LWR CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 DEEP CORROSION ON SHEAR TIE AT STATION 764 BETWEEN STRINGERS 36 - 37. REPLACED SHEAR TIE IAW B767 AMM. 2 L 7 2 4F RT A1NM 2002082800122 20020828 00122 NM 2002 8 28 UPS02239198 1 20020812 A 5310 SKIN BOEING 727 72731C 1384011 NM CROWN, BS 1183 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C CORROSION FOUND ON FUSELAGE SKIN AT BS 1181, BETWEEN S-5L AND S-6L. TO REMOVE CORROSION COMPLETELY , SKIN CUT-OUT WAS MADE FROM BS 1145 T O BS 1180, BETWEEN S-5L AND S-10L. REPAIR WAS CARRIWED OUT IAW SMRO EO 2002-044-0 02 R2. REF. UPS EO B727-5330-17442-A 2 L 7 3 4F A3WE 2002082800123 20020828 00123 NM 2002 8 28 ABXA020092 1 20020409 A 5300 140T2102264 SHEAR TIE BOEING 767 767200 1385120 NM FWD LWR CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 CORRODED SHEAR TIE AT STATION 720 BETWEEN STRINGERS 37 RIGHT - 37 LEFT. REPLACED SHEAR TIE IAW B767 AMM. 2 L 7 2 4F RT A1NM 2002082800124 20020828 00124 WP 2002 8 28 ABXA020112 1 20020617 A 5310 TRACK DOUG DC8 DC863 302198A WP STA. 1440 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 AFT CARGO COMPARTMENT STATION 1440 TO 1540, RIGHT BUTT LINE 60, CORROSION UNDER FLOOR BOARD CLIP NUTS. FABRICATED 8 EACH SPLICES AND REPAIR TRACK, INSTALLED AND REPAIRED AREA IAW DC-8 SRM 51-3-0, 53-2-0, 53-2-3, AND 51-1-8. 2 L 7 4 4F 4A25 2002082800125 20020828 00125 NM 2002 8 28 UPS02439171 1 20020804 A 5410 WEB BOEING 747 747212B 1384886 NM #3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C #3 PYLON REAR MOUNT BULKHEAD FOUND CRACKED AT FWD & AFT WEB AT THREE FASTENER HOLE LOCATIONS AS PER A TTACHED FIGURE.(STA 221.9 TO 222, WL 170 TO 180). #3 PYLON REAR ENG MOUNT BULKHEAD REPAIR CARRIED OUT AS PER HX RS # R-54-53-34870. 2 L 7 4 4F A20WE 2002082800126 20020828 00126 WP 2002 8 28 ABXA020113 1 20020822 A 3040 4TL1593 SWITCH DOUG DC9 DC932 3022066 WP DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 902AX 47426 AFTER TURNING ON WINDSHIELD HEAT, A BURNING SMELL WAS NOTED IN THE COCKPIT. THE SMELL WENT AWAY AFTER TURNING OFF WINDSH IELD HEAT. REPLACED THE WINDSHIELD HEAT SWITCH. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2002082800127 20020828 00127 WP 2002 8 28 ABXA020114 1 20020822 A 3040 4TL1593 SWITCH DOUG DC9 DC932 3022066 WP DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 902AX 47426 WITH ANTI-FOG CIRCUIT BREAKERS PULLED, NO BURNING SMELL NOTED. WITH ANTI-FOG CIRCUIT BREAKERS IN, A BURNING SMELL WAS NO TED. REPLACED THE WINDSHIELD HEAT SWITCH. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2002082800128 20020828 00128 NM 2002 8 28 UPS02439172 1 20020803 A 5410 WEB BOEING 747 747212B 1384886 NM #2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C #2 PYLON REAR MOUNT B/H. FWD. AND AFT. WEB FOUND CRACKS. #2 PYLON REAR ENG MOUNT BULKHEAD REPAIR C ARRIED OUT AS PER HX RS# R-54-53-34872 2 L 7 4 4F A20WE 2002082800129 20020828 00129 WP 2002 8 28 ABXA020103 1 20020621 A 5700 5644972502N FITTING DOUG DC8 DC863 302198A WP XRS 408 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 #4 ALT HAD A CRACKED STRINGER END FITTING AT XRS 408. SPLICE - STRINGER 59 AFT SIDE. INSTALLED NEW END FITTING AND BOOST PUMP BRACKET IAW DC-8 SRM 51-1-24, 51-1-8, AND 51-1-20D. 2 L 7 4 4F 4A25 2002082800130 20020828 00130 WP 2002 8 28 ABXA020104 1 20020617 A 5400 FLAP TRACK DOUG DC8 DC863 302198A WP RIGHT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 RIGHT WING INBOARD FLAP, INBOARD FLAP TRACK SHOWED EVIDENCE OF WEAR AND CORROSION. REPLACED THE RIGHT WING INBOARD FLAP, INBOARD FLAP TRACKS IAW DC-8 MM 27-51-03. 2 L 7 4 4F 4A25 2002082800131 20020828 00131 WP 2002 8 28 ABXA020105 1 20020702 A 5300 FITTING DOUG DC8 DC863 302198A WP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 CABIN UNDER FLOOR FRAME STIFFENER WAS CRACKED AT FS 780, LEFT BUTT LINE 47.0. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20 D, 51-3-2 AND 51-3-0. 2 L 7 4 4F 4A25 2002082800132 20020828 00132 WP 2002 8 28 ABXA020107 1 20020618 A 5310 FRAME DOUG DC8 DC863 302198A WP FS 1140 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 AFT CARGO FRAME HAD CORROSION AROUND NUTPLATE AT FS 1140, LONGERON 30 LEFT. CORROSION WAS OUT OF LIMITS. TRIMMED OUT DA MAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-20D, AND REA D853-43923-MR. 2 L 7 4 4F 4A25 2002082800133 20020828 00133 WP 2002 8 28 ABXA020108 1 20020616 A 5310 LONGERON DOUG DC8 DC863 302198A WP FS 24 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 AIR COND/PRESS COMPARTMENT AT FS 24, LONGERON 31 RIGHT WAS CORRODED AT ATTACH ANGLE ATTACHING FASTENERS. REMOVED CORRODE D CLIP LONGERON TO FRAME. INSTALLED NEW ATTACH P/N 2643619-1 IAW DC-8 SRM 51-1-21A AND 51-1-24. 2 L 7 4 4F 4A25 2002082800134 20020828 00134 WP 2002 8 28 ABXA020110 1 20020616 A 5740 SPAR CAP DOUG DC8 DC863 302198A WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 RIGHT WING FORWARD LOWER SPAR CAP HAD CRACK INDICATIONS IN FASTENER HOLES #2 AND #4 FROM THE INBOARD SIDE. FABRICATED RE PAIR PARTS AND REPAIRED AREA IAW ABX DC-8 JOB CARD J060232, DC-8 SRM 51-1-8, 51-1-20D, AND 51-1-25. 2 L 7 4 4F 4A25 2002082800135 20020828 00135 NM 2002 8 28 UPS02439173 1 20020803 A 5410 WEB BOEING 747 747212B 1384886 NM #1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C #1 PYLON REAR MOUNT B/H FWD & AFT WEB FOUND CRACKS. #1 PYLON REAR ENG MOUNT BULKHEAD REPAIR CARRIE D OUT AS PER HX RS # R-54-53-34873. 2 L 7 4 4F A20WE 2002082800136 20020828 00136 NM 2002 8 28 UPS02439174 1 20020803 A 5410 WEB BOEING 747 747212B 1384886 NM #4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C #4 PYLON REAR MOUNT B/H AFT WEB FOUND CRACKS. #4 PYLON REAR ENG MOUNT BULKHEAD REPAIR CARRIED OUT AS PER HX RS # R-54-53-3487. 2 L 7 4 4F A20WE 2002082800137 20020828 00137 NM 2002 8 28 UPS02439175 1 20020804 A 5410 65B904472 STIFFENER BOEING 747 747212B 1384886 NM #2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C #2 PYLON REAR ENGINE MOUNT BULKHEAD UPPER STIFFENER 2EA FASTENER HOLES CRACK FOUND AT O/B SIDE OF PYLO N THROUG THICKNESS REFER TO ATTACHED DRAWING FOR LOCATION. #2 PYLON REAR ENGINE B/H UPPER STIFFENER REPLACED AS PER SRM 51-10-01 PAGE 8. 2 L 7 4 4F A20WE 2002082800138 20020828 00138 NM 2002 8 28 UPS02439176 1 20020804 A 5410 65B903662 STIFFENER BOEING 747 747212B 1384886 NM #1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C #1 PYLON REAR ENGINE MOUNT B/H UPPER STIFFENER FOUND 2EA FASTENER HOLE CRACKED REFER ATTACHED SKETCH F OR DETAILS. #1 PYLON REAR ENGINE MOUNT B/H UPPER STIFFENER REPLACED AS PER SRM 51-10-01 PAGE 8. 2 L 7 4 4F A20WE 2002082800139 20020828 00139 SO 2002 8 28 C2XA02IA178 1 20020824 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11547 145563 During a postflight inspection the emergency lighting system was found to be inoperative. Maintenance inspected the airc raft and found the #2 battery pack to be inoperative. The affected pack was removed and replaced and the emergency light ing system was operationaly tested. 2 L 7 2 4T RT T00011AT 2002082800140 20020828 00140 SO 2002 8 28 C2XA02IA179 1 20020824 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11547 145563 During a postflight inspection the emergency lighting system was found to be inoperative. Maintenance inspected the airc raft and found the #3 battery pack to be inoperative. The affected pack was removed and replaced and the emergency light ing system was operationaly 2 L 7 2 4T RT T00011AT 2002082800141 20020828 00141 SO 2002 8 28 C2XA02IA180 1 20020824 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11547 145563 During a postflight inspection the emergency lighting system was found to be inoperative. Maintenance inspected the airc raft and found the #4 battery pack to be inoperative. The affected pack was removed and replaced and the emergency light ing system was operationaly 2 L 7 2 4T RT T00011AT 2002082800142 20020828 00142 EU 2002 8 28 C2XA02IA181 1 20020824 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 86842 286 During scheduled maintenance the passenger door emergency light was found to be inoperative. Maintenance inspected the a ircraft and found the passenger door emergency light assmebly to be faulty. The affected light assembly was removed and replaced, the system operationally tested, and the aircraft was approved for return to service. 2 H 7 2 4T RT A53EU 2002082800143 20020828 00143 NE 2002 8 28 C2XA02IA182 2 20020825 A 7200 PW121 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE SMOKE A C2XA C ABORTED TAKEOFF B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SW 27 99838 25296 12795 259 120813 During takeoff the crew noticed a smoke smell in the cockpit and aborted takeoff. A smoke warning illuminated after abor ting the takeoff. The aircraft returned to the gate without incident. Maintenance inspected the aircraft and found the s ource of smoke to be coming from the #1 engine. The affected engine was removed and replaced and the aircraft was approv ed for return to service. 2 H 7 2 4T 4 T RT A53EU E20NE 2002091200095 20020912 00095 NM 2002 9 12 F3LA200200251 1 20020823 A 5311 FRAME BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FRAME AT BS 847, RBL 6 TO LBL 6. REMOVED DAMAGE, FABRICATED AND INST ALLED REPAIR PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2002082800144 20020828 00144 EU 2002 8 28 C2XA02IA183 1 20020826 A 2422 559012B INVERTER AEROSP ATR42 ATR42320 8680930 EU FAULTY A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 27 86842 286 DURING TAXI THE CREW REPORTED ELECTRICAL SMELL IN COCKPIT, MAINTENANCE INSPECTED A/C AND FOUND #2 INVERTER TO BE FAULTY. THE INVERTER WAS REMOVED AND REPLACED AND OPERATIONALY CHECKED GOOD. 2 H 7 2 4T RT A53EU 2002090900155 20020909 00155 WP 2002 9 9 ARWA20020808 1 20020827 A 3213 57583304 CYLINDER DOUG DC8 DC863F 302198F WP RT MLG CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 24127 IAC2775 45969 DURING DAILY INSPECTION FOUND RIGHT HAND CYLINDER CRACKED AT LOWER OUTBOARD SIDE. REMOVED AND REPLACED RT MLG STRUT ASS EMBLY. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F 4A25 2002082800145 20020828 00145 NM 2002 8 28 AWXA200200817 1 20020826 A 3260 BACC18Z3R CIRCUIT BREAKER BOEING 737 7373G7 1384595 NM ZONE 200 - FUSEL DEFECTIVE A AWXA O OTHER J N WARNING INDICATION FALSE WARNING AP APPROACH 1 WP 28 157AW 0 0 23779 PHX - EMERGENCY LANDING - FLT 0337 - EN ROUTE FRON DEN TO PHX, AFTER INITIAL LANDING GEAR EXTENSION WITH NO GREEN LIGHTS , THE MAIN GEAR VIEWING WINDOW WAS CHECKED AND REVEALED THAT THE R/H MAIN LANDING GEAR WAS NOT FULLY DOWN. THE LANDING G EAR WAS CYCLED ONE MORE TIME AND MAIN GEAR WINDOW REVEALED THAT THE LANDING GEAR WAS DOWN AND LOCKED, BUT STILL HAD NO G REEN LIGHTS. FLY BY AT PHX AND IWA TOWERS ALSO VERIFIED LANDING GEAR WAS DOWN. AN EMERGENCY WAS DECLARED AND AIRCRAFT LA NDED WITHOUT EVENT. MAINTENANCE TROUBLESHOT PER BMM 32-32-00 AND PERFORMED VISUAL INSPECTION OF R/H MAIN GEAR, NO FAULTS FOUND. THE LANDING GEAR WAS CYCLED NUMEROUS TIMES WITH OPERATION AND INDICATIONS NORMAL EACH TIME. AS A PRECAUTIONARY M 2 L 7 2 4F RT A16WE 2002082800146 20020828 00146 NM 2002 8 28 AWXA200200838 1 20020724 A 5753 6546486510 WEDGE BOEING 737 737277 1384570 NM WBL 175.5 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 0 0 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A CRACK WAS FOUND IN THE R/H INBOARD MID FLAP TRAILING EDGE WEDGE OUTBOARD END PO TTING COMPOUND, SKIN WAS ALSO FOUND DEBONDING FROM THE WEDGE AT THE INBOARD TRACK CUTOUT. MAINTENANCE REMOVED DAMAGED WE DGE, FITTED AND INSTALLED A NEW WEDGE PER DWG 65-46486, AND BMM 57-51-31, PG. 506. 2 L 7 2 4F RT A16WE 2002082900001 20020829 00001 NM 2002 8 29 2002F00822 1 20020528 A 5260 WEB BOEING 727 727222 1384073 NM AIRSTAIR CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CRACK AT VENTRAL STAIRWAY, RIGHT TORQUE BOX VERTICAL WEB, .5 INCH LONG, AT STATION 1223. (M) 2 L 7 3 4F A3WE 2002082900002 20020829 00002 NM 2002 8 29 2002F00823 1 20020527 A 5730 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION ON RIGHT WING SKIN TOP SIDE, AROUND THE OVERWING FILLER. (M) 2 L 7 3 4F A3WE 2002082900003 20020829 00003 NM 2002 8 29 2002F00824 1 20020527 A 5730 SKIN BOEING 727 727222 1384073 NM FS 251-357 CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION AT TOP OF RIGHT WING TRAILING EDGE SEAM, BETWEEN THE TRAILING EDGE OF THE WEB SKIN, AND LEAD ING EDGE, OF THE TRAILING EDGE SKIN PANELS, AT APPROXIMATELY WING STATION 251 TO 357. (M) 2 L 7 3 4F A3WE 2002082900004 20020829 00004 NM 2002 8 29 2002F00825 1 20020527 A 5730 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION ON RIGHT WING SKIN TOP SPAR, AT APPROXIMATELY WING STATION 200-330. (M) 2 L 7 3 4F A3WE 2002082900005 20020829 00005 NM 2002 8 29 2002F00826 1 20020527 A 5700 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION ON RIGHT WING TOP SKIN TRAILING EDGE SPAR, AT APPROXIMATELY WING STATION 600. (M) 2 L 7 3 4F A3WE 2002082900006 20020829 00006 NM 2002 8 29 2002F00827 1 20020527 A 5730 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION AT RIGHT WING TOP SKIN LEADING EDGE SPAR, AT APPROXIMATELY WING STATION 464. (M) 2 L 7 3 4F A3WE 2002082900007 20020829 00007 NM 2002 8 29 2002F00828 1 20020527 A 5730 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION ON RIGHT WING TOP SKIN LEADING EDGE SPAR, AT APPROXIMATELY WING STATION 519. (M) 2 L 7 3 4F A3WE 2002082900008 20020829 00008 NM 2002 8 29 2002F00829 1 20020527 A 5700 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION IN MIDDLE OF RIGHT WING TOP SKIN, AT APPROXIMATELY WING STATIN 320. (M) 2 L 7 3 4F A3WE 2002082900009 20020829 00009 NM 2002 8 29 2002F00830 1 20020527 A 5730 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION ON RIGHT WING TOP SIDE SKIN, AT APPROXIMATELY WING STATION 235. (M) 2 L 7 3 4F A3WE 2002082900010 20020829 00010 NM 2002 8 29 2002F00831 1 20020527 A 5730 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION ON RIGHT WING TOP SPAR SKIN, AT APPROXIMATELY WING STATION 357-383. (M) 2 L 7 3 4F A3WE 2002082900011 20020829 00011 NM 2002 8 29 2002F00832 1 20020527 A 5700 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION ON TOP OF RIGHT WING REAR SPAR, AT APPROXIMATELY WING STATION 251 TO 357. (M) 2 L 7 3 4F A3WE 2002082900012 20020829 00012 NM 2002 8 29 2002F00833 1 20020527 A 5730 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION AT TOP SIDE OF RIGHT WING SKIN, ON TRAILING EDGE OF SPAR, AT APPROXIMATELY WING STATION 570. (M) 2 L 7 3 4F A3WE 2002082900013 20020829 00013 NM 2002 8 29 2002F00834 1 20020527 A 5730 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION ON RIGHT WING TOP SKIN LEADING EDGE SPAR, AT STATION 655. 2 L 7 3 4F A3WE 2002082900014 20020829 00014 NM 2002 8 29 2002F00835 1 20020527 A 5730 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION AT RIGHT WING TOP SIDE, ON TRAILING EDGE SKIN, AT APPROXIMATELY WING STATION 505. (M) 2 L 7 3 4F A3WE 2002082900015 20020829 00015 WP 2002 8 29 2002F00836 1 20020514 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON AFT WASTE SYSTEM COMPARTMENT FRAMES, AT STATION 1964, BACKSIDE, 1975, 1986, AND 1997.75, BETWEEN LONGERONS 48L AND 48R. (M) 2 L 7 3 4F A22WE 2002082900016 20020829 00016 WP 2002 8 29 2002F00837 1 20020512 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK FOUND CORROSION IN AFT CARGO BAY, AT LONGERON TO FRAME INTERFACE, AT STATION 1953, L47R TO L51L. (M) 2 L 7 3 4F A22WE 2002082900017 20020829 00017 NM 2002 8 29 AALA20021069 1 20020720 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 621AM 24579 MIA - FOUND EMERGENCY LIGHT AT SEAT 25D IS INOPERATIVE. CLEANED AND RESEATED EMERGENCY LIGHT POWER CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002082900018 20020829 00018 EU 2002 8 29 AALA20021070 1 20020720 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 JFK - FOUND SEAT MOUNTED EMERGENCY LIGHT AT 33G IS INOPERATIVE. SECURED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERAT ION. (M) 2 L 7 2 4F RT A35EU 2002082900019 20020829 00019 NM 2002 8 29 AALA20021071 1 20020722 A 2910 LINE BOEING 757 757223 1384957 NM HYD SYSTEM CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 695AN 26975 DFW - FLT 760 - EN ROUTE DFW-LGA - LEFT HYDRAULIC SYSTEM QUANTITY LOSS. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. R EPLACED LEFT GEAR DOWNLOCK ACTUATOR RETURN LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002082900020 20020829 00020 NM 2002 8 29 AALA20021073 1 20020723 A 3350 BATTERY BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 335AA 22333 LAX - DURING OVERNIGHT MAINTENANCE, FOUND EXTERIOR EMEGENCY ESCAPE LIGHTING AT DOOR R2 INOPERATIVE. REPLACED EXTERIOR E MERGENCY ESCAPE LIGHTING BATTERY ASSEMBLY AT DOOR R2. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082900021 20020829 00021 NM 2002 8 29 AALA20021074 1 20020718 A 3230 SEQUENCE VALVE BOEING 767 767223 1385123 NM MLG INOPERATIVE A AALA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 305AA 22311 JFK - EN ROUTE JFK-MIA, LEFT MAIN LANDING GEAR COMES DOWN WHEN GEAR HANDLE IS PLACED IN OFF POSITION. RETURNED TO JFK L ANDED WITHOUT INCIDENT. REPLACED LEFT MAIN GEAR DOOR LATCH AND GEAR OPERATED SEQUENCE VALVE. PERFORMED OPS AND LEAK CH ECK PER MM REF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082900022 20020829 00022 NM 2002 8 29 AALA20021075 1 20020724 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 369AA 25196 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE LIGHT AT SEAT 30H INOPERATIVE. REPAIRED EMERGENCY ESCAPE LIG HTING PUSH BACK PINS AT SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002082900023 20020829 00023 NM 2002 8 29 ASAA0210057 1 20020308 A 3350 883200312 BATTERY BOEING 737 7372Q8C 138448S NM AFT CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS IN THE AFT PORTION OF THE PASSENGER CABIN INOPERATIVE . REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY (P/N 86210144) AND RECEIVER (P/N 883200312) THEN LIGHTS OPERATED NORMAL . (M) 2 L 7 2 4F A16WE 2002082900024 20020829 00024 NM 2002 8 29 ASAA0210058 1 20020309 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM AFT CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS ON THE AFT SEAT PALLET INOPRATIVE. REMOVED AND REPLA CED REMOTE ASSEMBLY BATTERY THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002082900025 20020829 00025 NM 2002 8 29 ASAA0210059 1 20020312 A 3350 883200312 RECEIVER BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS ON THE SEAT PALLET 4-2 WILLNOT EXTINGUISH. REMOVED A ND REPLACED REMOTE ASSEMBLY RECEIVER THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002082900026 20020829 00026 NM 2002 8 29 ASAA0210127 1 20020515 A 5343 658276415 BEAM BOEING 737 737290C 138448V NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND MAIN LANDING GEAR BEAM AT WING STATION 110 CHAFED. REPAIRED BEAM PER EA. (M) 2 L 7 2 4F A16WE 2002082900027 20020829 00027 NM 2002 8 29 ASAA0210128 1 20020515 A 5330 654577456 SKIN BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 727-908, STRINGER 20L-25L DENTED. REPAIRED SKIN PANEL PER EA. ( M) 2 L 7 2 4F A16WE 2002082900028 20020829 00028 NM 2002 8 29 ASAA0210129 1 20020515 A 5314 65621251 KEELBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM AT BS 675-727, LEFT BUTTOCK LINE 6.5 CORRODED. REPAIRED KEEL BEAM PER E A. (M) 2 L 7 2 4F A16WE 2002082900029 20020829 00029 NM 2002 8 29 ASAA0210133 1 20020527 A 5310 654587511 BEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND CREASE BEAM WEB AT BS 332-344, RIGHT BUTTOCK LINE 61-64 CORRODED. REPAIRED CREASE BEAM WEB PER SRM. (M) 2 L 7 2 4F RT A16WE 2002082900030 20020829 00030 NM 2002 8 29 ASAA0210140 1 20020604 A 5330 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AFT SERVICE DOOR, BS 967, RIGHT BUTTOCK ILNE 59 CRACKED. REPAIRED SKIN PANEL PER SRM. (M) 2 L 7 2 4F RT A16WE 2002082900031 20020829 00031 NM 2002 8 29 ASAA0210141 1 20020604 A 5210 507945 SKIN BOEING 737 7372X6C 1384552 NM PAX DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL ON L1 DOOR, BODY STATION 342, LEFT BUTTOCK LINE 63.3 CRACKED. REPAIRED SKIN PANEL PER SRM. (M) 2 L 7 2 4F RT A16WE 2002082900032 20020829 00032 NM 2002 8 29 ASAA0210142 1 20020606 A 5511 6573781 SPAR BOEING 737 7372X6C 1384552 NM HORIZONTAL STAB CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND REAR SPAR AT RIGHT HORIZONTAL STABILIZER 67.54 CORRODED. REPAIRED REAR SPAR PER E A. (M) 2 L 7 2 4F RT A16WE 2002082900033 20020829 00033 NM 2002 8 29 ASAA0210143 1 20020606 A 5511 6573781 SPAR BOEING 737 7372X6C 1384552 NM HORIZONTAL STAB CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND REAR SPAR AT LEFT HORIZONTAL STABILIZER 67.54 CORRODED. REPAIRED REAR SPAR PER EA . (M) 2 L 7 2 4F RT A16WE 2002082900034 20020829 00034 NM 2002 8 29 ASAA0210144 1 20020606 A 5711 654784177 FRAME BOEING 737 7372X6C 1384552 NM LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT LEFT WING STATION 126 CRACKED. REPAIRED REAR CHORD PER SRM. (M) 2 L 7 2 4F RT A16WE 2002082900035 20020829 00035 NM 2002 8 29 ASAA0210145 1 20020607 A 5314 6545866688 KEELBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING SCHEDULED C-CHECK, FOUND KEELBEAM AT BS 677-727, LEFT BUTTOCK LINE 8 CORRODED. REPAIRED REAR KEELBEAM PER EA. (M) 2 L 7 2 4F RT A16WE 2002082900036 20020829 00036 NM 2002 8 29 ASAA0240026 1 20020305 A 3350 8100022601 LIGHT BOEING 737 737490 1384715 NM AFT CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 799AS 29270 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT IN AFT CABIN INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY OPER ATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002082900037 20020829 00037 NM 2002 8 29 ASAA0240029 1 20020312 A 3397 8100022607 WIRE BOEING 737 7374Q8 138447Q NM CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 785AS 27628 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 14-15. RECONNECTED LOOSE WIRES, OPS CHECK NORM AL. (M) 2 L 7 2 4F RT A16WE 2002082900038 20020829 00038 NM 2002 8 29 ASAA0240070 1 20020612 A 5240 6545871521 MECHANISM BOEING 737 7374Q8 138447Q NM SERVICE DOOR OUT OF ADJUST A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - DURING LINE CHECK, FOUND R-1 DOOR HARD TO OPEN. ADJUSTED R-1 DOOR GUIDE ARM PER MM. OPERATIONAL CHECKED GOOD. ( M) 2 L 7 2 4F RT A16WE 2002082900039 20020829 00039 NM 2002 8 29 ASAA0240071 1 20020530 A 5300 654795961 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 4S3 PAE - DURING SI CHECK, FOUND FRAME AT BS 794, RBL 20 WL 153 IS CORRODED. REMOVED AND REPLACED FRAME IAW SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2002082900040 20020829 00040 NM 2002 8 29 ASAA024031 1 20020315 A 3397 WIRE BOEING 737 7374Q8 138447Q NM MID CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 755AS 25096 PDX - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 13-15. RECONNECTED WIRES. TRACK LIGHTS THEN OPER ATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2002082900041 20020829 00041 NM 2002 8 29 ASAA0270003 1 20020305 A 3397 WIRE BOEING 737 737790 13844CN NM FWD CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 619AS 30164 SEA - DURING LINE MAINTENANCE CHECK, FOUND TWO TRACK ILGHTS WERE INOPERATIVE AT ROW 6. REATTACHED WIRES CONNECTING LIGH T ASSEMBLY. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2002082900042 20020829 00042 NM 2002 8 29 ASAA0280066 1 20020308 A 3397 CONNECTOR DOUG MD80 MD83 3023681 NM FWD CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 53473 PDX - DURING LINE CHECK, FOUND 5 EMERGENCY TRACK LIGHTS INOPERATIVE, ROWS 6 TO 8. RESECURED ELECTRICAL CONNECTORS. LIG HTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT 2002082900043 20020829 00043 WP 2002 8 29 ASAA0280067 1 20020307 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP AFT CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE, AT ROW 29. RESECURED ELECTRICAL CONNECTORS. LI GHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002082900044 20020829 00044 WP 2002 8 29 ASAA0280068 1 20020309 A 3397 WIRE DOUG DC9 DC983 3022083 WP AFT CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 SEA - DURING LINE CHECK, FOUND BROKEN WIRE IN EMERGENCY TRACK LIGHTS AT ROW 20-31. REPLACED BROKEN WIRE. LIGHTS THEN O PERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002082900045 20020829 00045 WP 2002 8 29 ASAA0280070 1 20020314 A 3350 MODULE DOUG DC9 DC983 3022083 WP FWD CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING LINE CHECK, FOUND THREE INOPERATIVE EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN. REPLACED BROKEN LIGHT MODUL E. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002082900046 20020829 00046 WP 2002 8 29 ASAA0280072 1 20020315 A 3350 MODULE DOUG DC9 DC983 3022083 WP FWD CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING PREFLIGHT CHECK, FOUND INOPERATIVE EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN. RECONNECTED LIGHT MODULE. L IGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002082900047 20020829 00047 WP 2002 8 29 ASAA0280131 1 20020404 A 3350 2550325 BATTERY DOUG DC9 DC983 3022083 WP FWD PAX ENTRANCE INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 PDX - DURNG LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT BATTERY, OP TESTED OK . (M) 2 L 7 2 4F RT A6WE 2002082900048 20020829 00048 WP 2002 8 29 ASAA0280132 1 20020408 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP FWD CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING PREFLIGHT CHECK, FOUND FIRST TWO FEET OF EMERGENCY TRACK LIGHTS INOPERATIVE. REINSTALLED, RECONNECTED, LOO SE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002082900049 20020829 00049 WP 2002 8 29 ASAA0280133 1 20020408 A 3350 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 PHX - DURING PREFLIGHT CHECK, DETERMINED THAT THE EMERGENCY TRACK LIGHTS AT ROW 1 WERE INOPERATIVE. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002082900050 20020829 00050 EA 2002 8 29 ASOA02386 1 20020704 A 7120 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 837AS 7271 DURING HANGAR MAINTENANCE IN MCN, A CRACK WAS FOUND IN THE BOX BEAM AREA OF THE LOWER RIGHT ACCESS PANEL ON THE INBOARD SIDE AS VIEWED THROUGHT THE LIGHTENING HOLE. MAINTENANCE REPAIRED THE CRACKED ENGINE SUPPORT BEAM IAW ASA EO 600-53-007 0. (M) 2 L 7 2 4F RT A21EA 2002082900051 20020829 00051 EA 2002 8 29 ASOA02387 1 20020704 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SW 21 837AS 7271 DURING HANGAR MAINTENANCE IN MCN, THE LEFT AND RIGHT SIDES OF FRAME 718 WERE FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE CRACKED FRAME IAW ASA EO 600-53-0066. (M) 2 L 7 2 4F RT A21EA 2002082900052 20020829 00052 SO 2002 8 29 ASOA02388 1 20020705 A 3232 WTC22461 ACTUATOR EMB 120 EMB120RT 3260202 SO LT MLG DOOR LEAKING A ASOA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 238AS 120053 FLT 4064 - DURING CRUISE FLIGHT FROM CRW TO ATL, THE CAPTAIN RECEIVED A GREEN HYDRAULIC RESERVOIR LOW LEVEL LIGHT. THE CAPTAIN STARTED TO MONITOR THE HYDRAULIC QUANTITY, AND AFTER 15-20 MINUTES THE QUANTITY DROPPED SIGNIFICANTLY. AIRCRAFT DIVERTED AND LANDED SAFELY IN AVL. MAINTENANCE INSPECTED AND FOUND THE LEFT INBOARD GEAR DOOR ACTUATOR LEAKING HYDRAUL IC FLUID. MAINTENANCE REMOVED AND REPLACED THIS DOOR ACTUATOR. OPERATIONAL CHECKS NORMAL WITH NO LEAKS NOTED. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2002082900053 20020829 00053 SO 2002 8 29 ASOA02389 1 20020705 A 3350 1317 BULB EMB 120 EMB120ER 3260203 SO CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 262AS 120146 DURING GROUND INSPECTION IN DFW, THE LEFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002082900054 20020829 00054 EA 2002 8 29 ASOA02390 1 20020706 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 880AS 7606 DURING GROUND INSPECTION, THE LEFT FORWARD MOST EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002082900055 20020829 00055 SO 2002 8 29 ASOA02391 1 20020707 A 3350 BULB EMB 120 EMB120RT 3260202 SO CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 281AS 120224 DURING A GROUND INSPECTION IN DFW, THE LEFT UPPER EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002082900056 20020829 00056 NE 2002 8 29 EIAA2002088 2 20020723 A 7200 ENGINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7J 52054 NE NR 1 STALLED A EIAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 09 481EV 19896 689487 FLT 481 - PANC - WHILE CRUISING AT FL35.0, NR 1 ENGINE COMPRESSOR STALLED, N1 RPM DECREASED AND EGT INCREASED RETARDED T HROTTLE NO RESPONSE, SHUTDOWN NR 1 ENGINE. DURING WINDMILLING ATTEMPTED RESTART, EGT OUT OF LIMITS, RETURN TO ANC. (M) 2 L 7 4 4F 4 F A20WE E20EA 2002082900057 20020829 00057 NM 2002 8 29 GAIA02074OP 1 20020723 A 3350 1000679 LIGHT BOEING 727 727224 1384076 NM L1 DOOR WILL NOT TEST A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 01 69739 20667 DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE LEFT FORWARD ENTRY DOOR, EMEREGNCY EXIT LIGHT WOULD NOT TEST. RE MOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 L 7 3 4F A3WE 2002082900058 20020829 00058 NM 2002 8 29 GAIA02075OP 1 20020724 A 2612 FIRE LOOP BOEING 727 727287 1384020 NM NR 1 ENGINE GROUNDED A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 916PG 21690 FLT 705 - DFW-FWA - AFTER TAKEOFF, THE FLIGHT CREW NOTICE THE NR 1 ENGINE FIRE LIGHT WAS ON INTERMITTENTLY. THE AIRCRAF T RETURNED TO DFW AND AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED THAT THE NR 1 ENGINE FIRE LOOP GROUNDING ON A MOUNTING BRACKET. THE FIRE LOOP WAS REPOSITIONED. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2002082900059 20020829 00059 NM 2002 8 29 GAIA02076OP 1 20020724 A 2611 CG7PT2 SMOKE DETECTOR BOEING 727 727251 138408H NM NR 1 MALFUNCTIONED A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 255US 19974 FLT 3706 - FWA-ELP - AFTER TAKEOFF, THE NR 1 SMOKE DETECTOR LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO FWA AND AN UNEV ENTFUL LANDING WAS MADE. REMOVED AND REPLACED NR 1 SMOKE DETECTOR. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETUR END TO SERVICE. (M) 2 L 7 3 4F A3WE 2002082900060 20020829 00060 NM 2002 8 29 GAIA02077OP 1 20020723 A 2760 SPOILER BOEING 727 727243 138408D NM WINGS OUT OF RIG A GAIA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 07 579PE 21662 FLT 705 - DFW-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THE AIRCRAFT SHUDDER AT .78 MACH. THE SHUDDER STOPPED WHEN T HE AIRCRAFT SLOWED TO KIAS. THE CREW ELECTED TO DIVERT TO MEM. AN UNEVENTFUL LANDING WAS MADE. THE NR 1, NR 5, NR 6, NR 10 AND NR 11 SPOILERS WERE RIGGED PER THE B727 AIRCRAFT MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 L 7 3 4F RT A3WE 2002082900061 20020829 00061 NE 2002 8 29 GAIA02078OP 2 20020726 A 7510 MF4582273 DUCT BOEING 727 727287 1384020 NM PWA JT8 JT8D17 52049 NE NR 1 ENGINE BROKEN A GAIA O OTHER J WARNING INDICATION DE DESCENT 1 SW 07 916PG 21690 FLT 863 - EWR-FWA - AT THE BEGINNING OF DESCENT TO FWA, THE NR 1 ENGINE FIRE WARNING CAME ON INTERMITTENTLY. POWER WAS REDUCED TO IDLE AND THE WARNING CEASED. THE AIRCRAFT CONTINUED TO FWA AND AN UNEVENTFUL LANDING WAS MADE. INSPECTION R EVEALED THAT THE RIGHT ANTI-ICE DUCT BLEED TUBE WAS BROKEN. REMOVED AND REPLACED BLEED DUCT. OPERATIONALLY CHECKED GOO D. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F RT A3WE E2EA 2002082900062 20020829 00062 WP 2002 8 29 GTIA020748 1 20020617 A 5320 SUPPORT DOUG DC9 DC981 3022081 WP CARGO BAY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND AFT CARGO STATION 1322 CENTER L30 POST SUPPORT CORRODED. MATERIAL LOSS FOUND TO BE OUT OF LIMITS. FABRICAT ED NEW POST. POST SUPPORT WAS PREVIOUS REMOVED ON CARD B-3418NN00055. INSTALLED NEW POST. (M) 2 L 7 2 4F A6WE 2002082900063 20020829 00063 WP 2002 8 29 GTIA020749 1 20020617 A 7120 YOKE DOUG DC9 DC981 3022081 WP RT ENGINE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND RIGHT MOUNT YOKE WITH CORROSION (PIT) ON THE BACK SIDE UPPER AND LOWER. REPAIRED YOKE ON BACKSIDE, UPPER AN D LOWER AREAS PER SPIRIT AIRLINES EA 5410-0204, ORIGINAL ISSUE DATED 6-20-02. (M) 2 L 7 2 4F A6WE 2002082900064 20020829 00064 WP 2002 8 29 GTIA020750 1 20020617 A 7120 YOKE DOUG DC9 DC981 3022081 WP RT ENGINE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND RIGHT MOUNT YOKE UPPER AND LOWER COVER PLATES WITH CORROSION AND TOOL MARKS. REPAIRED UPPER AND LOWER ENGIN E MOUNT YOKE COVER PLATED PER SPIRIT AIRLINES EA 54-10-0204 ORIGINAL ISSUE DATED 6-20-02. (M) 2 L 7 2 4F A6WE 2002082900065 20020829 00065 WP 2002 8 29 GTIA020751 1 20020615 A 5320 SPLICE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND TWO FRAME SPLICES CORRODED. FABRICATED TWO SPLICES. DRILLED UP AND LOCATED NEW SPLICES. (M) 2 L 7 2 4F A6WE 2002082900066 20020829 00066 WP 2002 8 29 GTIA020752 1 20020610 A 5311 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND STATION 1322 ABOUT 4 INCHES AWAY FROM L22L, FRAME EXFOLIATED. AREA ON FRAME FOUND TO BE OUT OF LIMITS. AFT ER FUTHER EVALUATION FOUND 2 INTERCOSTALS AT STATION 1322 L22L CORROSION OUT OF LIMITS. REMOVED FRAME DAMAGED SECTION F ROM LONGERON 18L TO LONGERON 28R. FABRICATED TWO INTERCOSTAL, DRILLED AND LOCATED NEW FRAME SECTION. INSTALLED NEW FRA ME SECTION AND STRUT DOUBLER TWO INTERCOSTAL AT STATION 1322. INSTALLED REPAIR SPLICE FOUD, TWO INTERCOSTALS AT STATION 1322 LONGERON 27L, THREE FROM ANGLES FROM L23L TO LONGERON 27R AT STATION 1322. (M) 2 L 7 2 4F A6WE 2002082900067 20020829 00067 WP 2002 8 29 GTIA020753 1 20020604 A 5310 BEAM DOUG DC9 DC981 3022081 WP DOOR FRAME CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - AFT PIT LOWER DOOR CUT OUT HAS CORROSION AT OUTBOARD BEAM SURFACE ANGLE ALONG EDGE BEAM. BEAM OUT OF LIMITS AT ST ATION 1188 AND STATION 1171. FABRICATED DOUBLER AND SPACER. INSTALLED DOUBLER AND SPACER. (M) 2 L 7 2 4F A6WE 2002082900068 20020829 00068 WP 2002 8 29 GTIA020754 1 20020604 A 5340 FITTING DOUG DC9 DC981 3022081 WP FUSLEAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND AFT PIT CORRODED AT LONGERON 30 STATION 1007 TO STATION 1022. FABRICATED BATHTUB FITTING PER SPIRIT AIRLINE S EA 5310-0231. INSTALLED BATHTUB FITTING. (M) 2 L 7 2 4F A6WE 2002082900069 20020829 00069 WP 2002 8 29 GTIA020755 1 20020531 A 7120 ISOLATION MOUNT DOUG DC9 DC981 3022081 WP NR 2 ENGINE WRONG PART A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 818NK 48018 FOUND ENGINE NR 2 LOWER VIBRATION ISOLATOR, INDEX YACK MISMATCH. REMOVED ENGINE NR 2 LOWER VIBRATOR ISOLATOR. INSTALLE D NR 2 ENGINE LOWER VIBRATION ISOLATOR. (M) 2 L 7 2 4F A6WE 2002082900070 20020829 00070 WP 2002 8 29 GTIA020756 1 20020601 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FORWARD LIGHT CORROSION BARE METAL AT LONGERON 29L STATION 503, 484. MATERIAL LOSS OUT OF LIMITS. FABRICATRED -3 STRAP PER DWG NO 53100228-1 9SH 2 OF 2) EA 5310-0228. INSTALLED -3 STRAP. (M) 2 L 7 2 4F A6WE 2002082900071 20020829 00071 WP 2002 8 29 GTIA020757 1 20020602 A 5311 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND MID PIT HAS CORROSION AT THE FRAME STATION 636. REMOVED FRAME AT STATION 636 BETWEEN L29R-L26L. FABRICATED NEW FRAME. INSTALLED NEW REPAIR PART. (M) 2 L 7 2 4F A6WE 2002082900072 20020829 00072 WP 2002 8 29 GTIA020758 1 20020602 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND MID PIT CORRODED AT LONGERON 30 STATION 788. MATERIAL LOSS OUT OF LIMITS. FABRICATED -3 STRAP. REV 0 DATE D JUNE 19, 2002 AND EA 5310-0230. INSTALLED 3 STRAP. (M) 2 L 7 2 4F A6WE 2002082900073 20020829 00073 WP 2002 8 29 GTIA020759 1 20020602 A 5340 ATTACH ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND L1 DOOR LOWER THRESHOLD ATTACH ANGLE HAS CORROSION PLUS X60 INCH STATION 200 TO STATION 168. CUT OUT DAMAGE D AREA. FORMED NEW REPAIR ANGLE. INSTALLED REPAIR ANGLE. (M) 2 L 7 2 4F A6WE 2002082900074 20020829 00074 WP 2002 8 29 GTIA020760 1 20020611 A 5730 PANEL DOUG DC9 DC981 3022081 WP LT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND LEFT TRAPEZOID PANEL DELAMINATED, LEFT WING. REMOVED DELAMINATED PANEL. REPAIRED LEFT TRAPEZOID PANEL USIN G 181 GLASS CLOTH. INSTALLED TRAPEZOID PANEL. (M) 2 L 7 2 4F A6WE 2002082900075 20020829 00075 WP 2002 8 29 GTIA020761 1 20020529 A 3397 WIRE DOUG DC9 DC981 3022081 WP CONTROL PANEL BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND WITH EMERGENCY POWER ON SOME FORWARD PANEL LIGHTS WENT OUT. FOUND WIRE BROKEN. REPAIR WIRING. REMOVED WIR ING. REMOVED AND REPLACE LAMP. (M) 2 L 7 2 4F A6WE 2002082900076 20020829 00076 WP 2002 8 29 GTIA020762 1 20020529 A 5320 WEB DOUG DC9 DC981 3022081 WP FS 160-180 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND CUSP WEB CORRODED FROM STATION Y150 TO STA Y160 PLUS X57 (L1 JAMB AREA. MATERIAL OUT OF LIMITS. REMOVED WE B STATION 160 TO STATION 180 PLUS 59. CUSP WEB WAS INSTALLED ON W/O B-34 PLUS 0. (M) 2 L 7 2 4F A6WE 2002082900077 20020829 00077 WP 2002 8 29 GTIA020763 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 200 LBL 7 - RBL 7 FLOORBOARD SUPPORT CORRODED. REMOVED FLOOR SUPPORT. FABRICATED DRILLED AND LOCAT ED NEW SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002082900078 20020829 00078 WP 2002 8 29 GTIA020764 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 160-168 AND 186-194 LBL 54 TWO FLOORBOARD SUPPORTS ARE CORRODED. REMOVED FLOORBOARD SUPPORTS TWO FA BRICATED AND LOCATE AND DRILL NEW PARTS TWO EACH. INSTALLED FLOOR BOARD SUPPORTS TWO EACH. (M) 2 L 7 2 4F A6WE 2002082900079 20020829 00079 WP 2002 8 29 GTIA020765 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 200 LBL 9-13 FLOORBOARD SUPPORT IS CORRODED. REMOVED SUPPORT. FABRICATED NEW SUPPORT. INSTALLED N EW SUPPORT. (M) 2 L 7 2 4F A6WE 2002082900080 20020829 00080 WP 2002 8 29 GTIA020766 1 20020624 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 180 LBL 14-39 FLOORBOARD SUPPORT IS CORRODED. REMOVED SUPPORT. FABRICATED NEW SUPPORT. INSTALLED NEW SUPPORT. (M) 2 L 7 2 4F A6WE 2002082900081 20020829 00081 2002 8 29 GTIA020768 4 20020705 A 3460 4034241972 COMPUTER DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A GTIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 803NK 48087 FLL - FLT 380 - NR 2 DFGS SELECTED, AUTO THROTTLE INOPERATIVE, FRO FD INTERMITTENTLY INOPERATIVE. REMOVED AND REPLACED NR 2 DFGC PER MM 22-01-01 SYSTEM TESTS NORMAL PER MM 22-01-05. AUTO THROTTLE TEST NORMAL PER MM 22-31-00. (M) 2 L 7 2 4F A6WE 2002082900082 20020829 00082 NE 2002 8 29 DLM11020924 2 20020806 A 7200 PW44603 ENGINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 2 MALFUNCTIONED A DALA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 805DE 33845 48476 723870 LOUD NOISE AFTER T/O FROM AFT PORTION OF A/C POSSIBLE COMP STALL OR CARGO SHIFT NO IRREGULAR ENGINE PARAMETERS NOTICED. RETURNED TO BASE AFTER CONSULTING OCC DUMPED FUEL FROM 520-480 LANDING AT APPROX 474000 FLAPS 50. REPLACED NR 2 ENGINE PER TRANS 8T201AD ON R/C 1 THROUGH 33. 2 L 7 3 4F 4 F RT A22WE E24NE 2002082900083 20020829 00083 NM 2002 8 29 DLM11020927 1 20020808 A 2530 ODOR DOUG MD11 MD11 3023602 NM GALLEY DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 809DE 48480 FLT ATTENDANTS SMELLED AN ODOR IN AFT GALLEY CHILLER CONTROL PANEL. TURNED OFF ALL THREE CHILLER SWITCHES AND SMELL WEN T AWAY. SMELL DID NOT SEEM TO BE ELECTRICAL. UNABLE TO FAULT ANYTHING IN AFT GALLEY AREA. 2 L 7 3 4F RT A22WE 2002082900084 20020829 00084 NM 2002 8 29 DLM88020810 1 20020715 A 2560 61020 BATTERY DOUG MD88 MD88 3023688 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 979DL 53266 FWD FLASHLIGHT IN AFT CABIN INOP. REMOVED AND REPLACED BATTERY, OPS GOOD. 2 L 7 2 4F RT A6WE 2002082900085 20020829 00085 NM 2002 8 29 DLM11020855 1 20020722 A 2120 3983965 VALVE DOUG MD11 MD11 3023602 NM CABIN FAULTY A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 804DE 48475 DURING CLIMBOUT OF DFW COCKPIT CREW SMELLED SMOKE. SUBSEQUENTLY HAD AN LAVATORY SMOKE EAD ALERT. SMOKE PERSISTED FOR 3 -4 MIN, THEN WENT OUT. F/A'S REPORT DENSE SMOKE ESCAPE FROM CREW REST MODULE WHEN DOOR WAS OPENED AFTER LANDING. RETUR NED TO DFW. REPLACED FWD CABIN TRIM AIR VALVE. PERFORMED AIR CONDITION PACK AND DISTRIBUTION DUCT CLEANING PER M/M. R AN ENGINES, OPERATIONAL CHECK NORMAL. DURING PACK AND DISTRIBUTION DUCT CLEAN FOUND NR 3 TURBINE BYPASS VALVE INOP. RE PLACED SAME. 2 L 7 3 4F RT A22WE 2002082900086 20020829 00086 NM 2002 8 29 DLM11020873 1 20020726 A 2120 3989462 BYPASS VALVE DOUG MD11 MD11 3023602 NM A/C BAY MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 804DE 48475 LAV SMOKE WITH RESIDUAL SMELL IN CREW REST AREA AND HOT SMELL IN COCKPIT LASTED A FEW MINUTES. RAN ENGINES PER PFHB AT HIGH PWR SETTINGS. ISOLATED PACKS, NO SMOKE OR UNUSUAL HEAT NOTICED IN CREW REST MODULE. REMOVED AND REPLACED PACK 1 T URBINE BYPASS VALVE AND WATER SEPARATOR BAG AS PER MM. REMOVED AND REPLACED PACK 1 RAM AIR DOOR ACTUATOR AS PER MM. RE PLACED ALL 3 PACK WATER SEPARATOR BAGS. INSPECTED E/E AND AVIONICS COOLING FANS. NO DEFECTS NOTED. ALL 3 PACK INDICAT IONS NORMAL. 2 L 7 3 4F RT A22WE 2002082900087 20020829 00087 NM 2002 8 29 SWAA021848 1 20020814 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE AT ROW 9. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002082900088 20020829 00088 NM 2002 8 29 SWAA021849 1 20020815 A 2560 P2070001 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED A2 CHECK, FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002082900089 20020829 00089 NM 2002 8 29 SWAA021850 1 20020815 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 772SW 27880 AFT SVC DOOR EMERGENCY SIDE LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002082900090 20020829 00090 2002 8 29 SWAA021852 4 20020815 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT AS DOOR WAS OPENED. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002082900091 20020829 00091 2002 8 29 SWAA021853 4 20020815 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 092SW 22964 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002082900092 20020829 00092 NM 2002 8 29 SWAA021854 1 20020815 A 2731 6545166 ROD END BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND LT AND RT ELEVATOR TAB AFT ROD ENDS WORN. REMOVED AND REPLACED ROD ENDS PER MM. 2 L 7 2 4F RT A16WE 2002082900093 20020829 00093 NM 2002 8 29 SWAA021855 1 20020815 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002082900094 20020829 00094 NM 2002 8 29 SWAA021860 1 20020817 A 3350 604222 BATTERY BOEING 737 7373L9 1384470 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED RON, FOUND AFT OVERHEAD EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002082900095 20020829 00095 2002 8 29 SWAA021861 4 20020817 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED BC4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002082900096 20020829 00096 NM 2002 8 29 SWAA021862 1 20020817 A 3350 20121 BATTERY BOEING 737 7372H4 138448C NM CARGO BAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 105SW 23249 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY IN AFT CARGO INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002082900097 20020829 00097 NM 2002 8 29 SWAA021864 1 20020816 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED C1 CHECK, FOUND EXTERIOR EMERGENCY LIGHT INOP AFT OF AFT SVC DOOR. RELAMPED EMERGENCY LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002082900098 20020829 00098 2002 8 29 SWAA021865 4 20020818 A 2565 63550101 SLIDE BOEING 737 7373G7 1384595 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002082900099 20020829 00099 2002 8 29 SWAA021866 4 20020818 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 414WN 29820 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002082900100 20020829 00100 2002 8 29 SWAA021869 4 20020817 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002082900101 20020829 00101 NM 2002 8 29 SWAA021878 1 20020818 A 3211 6959886 SUPPORT BOEING 737 7372K6 1364440 NM RT MLG CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 129SW 22340 DURING SCHEDULED SPECIAL VISIT, FOUND RT MLG SIDE STRUT SUPPORT FORGING CRACKED AT BS 685, BELOW STR 18R. REMOVED AND R EPLACED RT MLG SIDE STRUT SUPPORT PER SRM AND BAC DRAWING. 2 L 7 2 4F RT A16WE 2002082900102 20020829 00102 NM 2002 8 29 SWAA021879 1 20020815 A 2782 654465116 ACTUATOR BOEING 737 7372H4 138448C NM L/E SLAT FAILED A SWAA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 29 073SW 22673 NR 3 L/E SLAT TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 SLAT ACTUATOR PER MM. 2 L 7 2 4F A16WE 2002082900103 20020829 00103 NM 2002 8 29 SWAA021882 1 20020818 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT OVERWING EXIT. RESECURED WIRES PER MM. 2 L 7 2 4F RT A16WE 2002082900104 20020829 00104 2002 8 29 SWAA021883 4 20020818 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 414WN 29820 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002082900105 20020829 00105 NM 2002 8 29 SWAA021886 1 20020819 A 5754 65C26686 SKIN BOEING 737 7375H4 138449D NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED 1/4D CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED AT AFT FASTENERS NEAR OTBD END. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2002082900106 20020829 00106 NM 2002 8 29 SWAA021890 1 20020819 A 3240 26066724 BRAKE ASSY BOEING 737 7372T4 1384492 NM RT MLG CONTAMINATED A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 29 722WN 22698 RT MLG BRAKES GRABBING, DIFFICULT TO BRAKE EVENLY. BLED NR 3 AND NR 4 BRAKE ASSY PER MM. 2 L 7 2 4F A16WE 2002082900107 20020829 00107 NM 2002 8 29 SWAA021894 1 20020820 A 3350 1064783201 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 702ML 22054 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT AT MID CABIN OVERHEAD INOP AND LENS BROKEN. REMOVED AND REPLACED BATTERY AND LENS PER MM. 2 L 7 2 4F A16WE 2002082900108 20020829 00108 2002 8 29 SWAA021895 4 20020819 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002082900109 20020829 00109 2002 8 29 SWAA021896 4 20020820 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002082900110 20020829 00110 NM 2002 8 29 SWAA021901 1 20020815 A 2752 MS9391130ZE4C MOTOR BOEING 737 7373A4 1384585 NM T/E FLAP FAILED A SWAA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SW 29 679AA 23291 AFTER LANDING, T/E FLAPS WOULD NOT RETRACT. REMOVED AND REPLACED FLAP DRIVE MOTOR PER MM. 2 L 7 2 4F RT A16WE 2002082900111 20020829 00111 NM 2002 8 29 SWAA021902 1 20020820 A 2761 654456114 ACTUATOR BOEING 737 7373A4 1384585 NM SPOILER FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED C4 CHECK, NR 2 FLIGHT SPOILER WILL NOT RETRACT. REMOVED AND REPLACED SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2002082900112 20020829 00112 NE 2002 8 29 SWAA021904 2 20020819 A 7260 340050 BEARING BOEING 737 7377H4 1384404 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED A SWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 29 412WN 29818 888582 INFLIGHT SHUTDOWN, NR 1 ENGINE OIL BYPASS LIGHT ILLUMINATED, RETARDED THROTTLE, LIGHT STAYED ILLUMINATED. REMOVED AND R EPLACED NR 1 ENGINE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082900113 20020829 00113 NM 2002 8 29 SWAA021907 1 20020820 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 303SW 22943 AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002082900114 20020829 00114 NM 2002 8 29 SWAA021909 1 20020820 A 3350 20121 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT AFT OVERHEAD BIN BULLNOSE. REMOVED AND REPLACED BATTERY P ER MM. 2 L 7 2 4F RT A16WE 2002082900115 20020829 00115 NM 2002 8 29 SWAA021913 1 20020820 A 3240 65C268591 AUGMENTOR TUBE BOEING 737 7373K2 13844BA NM MLG FAULTY A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 29 340LV 23738 BRAKE TRAVEL IS SIGNIFICANT WITHOUT ANY BRAKING ACTION. BRAKES GRABBING SUDDENLY. REMOVED AND REPLACED LEFT AND RIGHT BRAKE METERING VALVES AND LT AND RIGHT BRAKE FEEL AUGMENTORS PER MM. 2 L 7 2 4F RT A16WE 2002082900116 20020829 00116 NM 2002 8 29 DLM88020820 1 20020716 A 5330 5920323249 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 960DL 49979 AIRCRAFT ARRIVED FOR HMV WITH A TIME-LIMITED SKIN REPAIR, SCHEDULED FOR PERMANENT TO OCCUR AT HMV, PER ERA 379153-14. E RA 379153-14 WAS REVISED TO REVISION -A- TO INCORPORATE PERMANENT REPAIR INSTRUCTIONS. 2 L 7 2 4F RT A6WE 2002082900117 20020829 00117 NM 2002 8 29 DLM88020824 1 20020717 A 3411 PITOT LINE DOUG MD88 MD88 3023688 NM E/E BAY LOOSE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 935DL 49722 F/O AIRSPEED WENT TO ZERO, A/T AND A/P DISCONNECTED, OVERSPEED WARNING CONTINUOUS, F/D FAILED, F/O AIRSPEED WENT FROM 0 KTS TO 350 KTS. CADC BOTH ON 1 AIRSPEED, RETURNED TO NORMAL. FOUND PITOT LINE AT NR 2 CADC NOT SECURED. AS PRECAUTION REPLACED NR 2 CADC PER M/M 34-16-01-2. RAN RTS BOTH NR 1 AND 2 DFGC SYSTEMS GO. 2 L 7 2 4F RT A6WE 2002082900118 20020829 00118 NM 2002 8 29 DLM88020848 1 20020720 A 2133 INDICATOR DOUG MD88 MD88 3023688 NM COCKPIT OBSTRUCTED A DALA I G A CABIN DEPRESSURIZATION O2 MASK DEPLOYED UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 935DL 49722 CABIN ALTITUDE CONTROL JAMMED INFLIGHT. CABIN ALTITUDE EXCEEDED 14,000 FEET. MASKS DEPLOYED. EMERGENCY RETURN TO DFW. FOUND LOOSE HARDWARE OBSTRUCTING MOVEMENT OF OUTFLOW VALVE INDICATOR ON PEDESTAL. REMOVED HARDWARE. RAN BITE OF AUTO PRESSURIZATION CONTROLLERS. BITE CHECKS NORMAL. REPLACING OXYGEN GENERATORS AND MASKS. 2 L 7 2 4F RT A6WE 2002082900119 20020829 00119 NE 2002 8 29 DLM88020853 2 20020722 A 7261 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ACTIVATED A DALA E ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 SO 27 929DL 27799 49716 726826 IN FLIGHT SHUT DOWN, LOSS OFF OIL PRESSURE AND QTY. PRESSURE WENT TO ZERO AT PWR FOR APPROX 30 SEC. WINDMILL AT ZERO P SI FOR 10 MIN. RETURN TO CVG. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2002082900120 20020829 00120 NM 2002 8 29 DLM88020854 1 20020722 A 3610 PACKING DOUG MD88 MD88 3023688 NM A/C BAY LEAKING A DALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 987DL 53338 THE TAIL COMPARTMENT TEMP HI LIGHT ON DURING CLIMB. EXTINGUISHED TEMPORARILY WITH HP BLEED OFF, THEN RE-ILLUMINATED. C OMPLIED WITH CHECK LIST, PULLED LEFT THROTTLE TO IDLE AND LIGHT EXTINGUISHED, LEFT PACK OFF AND LEFT THROTTLE BACK TO NO RMAL. POWER AND LIGHT REMAINED EXTINGUISHED. FOUND 2 PACKINGS LEAKING AT RT ANTICIPATOR AND THERMOSTAT. REPLACED PACK INGS. REPLACED RT AND LT TAIL COMPT TEMP HIGH TEMP SENSORS, PRECAUTIONARY. FOUND 2 LOOSE PACK CLAMPS ON LT PACK. TIG HTENED SAME. LEAK CHECKS GOOD. ENGINE RUN TO PWR CHECKS GOOD. 2 L 7 2 4F RT A6WE 2002082900121 20020829 00121 NM 2002 8 29 DLM88020859 1 20020722 A 3350 UNK FUSE DOUG MD88 MD88 3023688 NM CABIN BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 996DL 53363 EMERGENCY EXIT LIGHTS INOP SEAT ROWS 1-4 AND 10-12, ALSO FWD ENTRY DOOR EXIT IDENTIFIER RIGHT SERVICE DOOR EXIT IDENTIFI ER AND G2 GALLEY. FOUND BLOWN FUSE ON POWER SUPPLY B5-211. REPLACED FUSE. LIGHTS NOW CHECK NORMAL. 2 L 7 2 4F RT A6WE 2002082900122 20020829 00122 NM 2002 8 29 DLM88020881 1 20020727 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 989DL 53341 FOUND EMERGENCY LIGHT INOP AT 14 D/E. RELAMPED LIGHT, CHECKS GOOD. 2 L 7 2 4F RT A6WE 2002082900123 20020829 00123 NM 2002 8 29 DLM88020884 1 20020728 A 3350 41B004AD073 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 980DL 53267 THREE CENTER AISLE EMERGENCY LIGHTS INOP IN F/C CABIN. REPLACED BATTERIES IN POWER SUPPLY B5-100. LIGHTS NOW OP NORMAL . 2 L 7 2 4F RT A6WE 2002082900124 20020829 00124 NM 2002 8 29 DLM88020901 1 20020802 A 2424 GCU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 968DL 29871 53161 725768 LEFT GENERATOR OFF MESSAGE ILLUMINATED AT 7000 FT ON CLIMBOUT NO VOLTS OR FREQS. FOUND NR 1 GCU FAULT LIGHT ILLUMINATED . REPLACED NR 1 GCU. REPLACED NR 1 CSD AND GEN PER AMM. NR 1 GEN, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A6WE E9NE 2002082900125 20020829 00125 NM 2002 8 29 DLM88020903 1 20020802 A 5711 SPAR DOUG MD88 MD88 3023688 NM LT WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DL 49542 PERMANENT REPAIR FOR DAMAGE TO THE LT WING FRONT SPAR. DAMAGE RESULTED IN SPLICING IN NEW SECTION OF LOWER WING SKIN AT XRS540, SPLICING LOWER SPAR CHORD AT XFS 563 AND LEADING EDGE REPAIR AT XFS 596. 2 L 7 2 4F RT A6WE 2002082900126 20020829 00126 NM 2002 8 29 DLM88020914 1 20020806 A 5330 5920323249 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 963DL 49982 DURING HMV-2, THE DENT IN THE SKIN BETWEEN STA 218 & STA 256 JUST ABOVE L-25R. TRIMMED OUT SKIN TO REMOVE A GOUGE. REP AIRED IAW MD-88 SRM 53-04, FIGURE 12B. 2 L 7 2 4F RT A6WE 2002082900127 20020829 00127 NM 2002 8 29 DLM88020937 1 20020811 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 915DE 53420 EMERGENCY LIGHTS ROWS 31 AND AFT WOULD NOT TEST. REPLACED POWER SUPPLY, OP CHECK NORMAL. 2 L 7 2 4F RT A6WE 2002082900128 20020829 00128 NM 2002 8 29 DLM88020938 1 20020811 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 910DL 49541 FOUND ALL SEAT EMERGENCY LIGHTS AND DOOR IDENTIFIERS NOT WORKING WITH COCKPIT SWITCH. FOUND AFT SEAT ROW POWER SUPPLY B AD SENDING POWER BACK TO SWITCH. REPLACED AFT POWER SUPPLY FOR SEATS, EMERGENCY LIGHTS CHECK NORMAL. 2 L 7 2 4F RT A6WE 2002082900129 20020829 00129 NE 2002 8 29 DLM90020823 2 20020716 A 7200 V2528D5 ENGINE DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 OVERTEMP A DALA O OTHER Y ENGINE STOPPAGE CL CLIMB 1 SO 27 907DA 14541 020079 53387 020079 ON CLIMBOUT EGT ROSE PAST RED LINE AFTER THROTTLE RETARDED TO DECREASE EGT. ENG AUTO SHUTDOWN. REPLACED ENG DUE TO EGT EXCEEDANCE. 2 L 7 2 4F 4 F RT A6WE E40NE 2002082900130 20020829 00130 NE 2002 8 29 DLM90020837 2 20020719 A 7200 ENGINE DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE NR 1 POWER LOSS A DALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS AP APPROACH 1 SO 27 907DA 18456 53387 071602 LEFT ENGINE POWER ROLLED BACK AND EGT 625. CREW FOLLOWED POM AND SHUT ENGINE DOWN. REPLACED NR 1 ENG PER M/M. 2 L 7 2 4F 4 F RT A6WE A40NE 2002082900131 20020829 00131 NM 2002 8 29 QXEA0201281 1 20020827 A 2720 2379003001 REGULATOR DHAV DHC8 DHC8202 2809007 NM ZONE 300 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 09 360PH 7869 7869 515 PDX - CREW RETURNED TO FIELD WHEN AFTER TAKEOFF AND PASSING 140KTS, THEY RECEIVED CAUTION LIGHTS FOR "RUDD FULL PRESS" A ND "RUDD PRESS". BELOW 14O KTS THE LIGHT WENT OUT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RUDDER DUAL PRESS REGULATOR IAW THE MAINTENANCE MANUAL. OPERATIONAL CHECKS AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2002082900132 20020829 00132 NM 2002 8 29 DLM90020900 1 20020802 A 2421 GENERATOR DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 2 ENGINE LACK OF LUBE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 902DA 17458 53382 020042 RT AC POWER FAULT WITH R GEN OIL PRESS LIGHT DURING CLIMBOUT. FOUND RT GEN OIL LEVEL LOW. SERVICED SAME. RUN ENG PER PFHB AND NO LEAK. GEN OPS OK. 2 L 7 2 4F 4 F RT A6WE E40NE 2002082900133 20020829 00133 NM 2002 8 29 DLM90020907 1 20020805 A 1430 SCREW DOUG MD90 MD9030 3023690 NM E/E BAY LOOSE A DALA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 27 904DA 53384 AIR TURNBACK, 2L DOOR HAD A LARGE AIRLEAK AUTO CONTROLLER DID NOT HAVE OUTFLOW VALVE FULL CLOSED. GOT CABIN ALT WARN LI GHT CABIN WAS AT 10000 FT/BIT AUTO CONTROLLER 1 FAULTED GROUND SWITCH. PRESSURIZED A/C PER M/M, NO DOOR LEAKS NOTED. F OUND LOOSE SCREW HAD FALLEN INTO RELAY R2-4 SHORTING TERMINALS D1 AND D2. REPLACED RELAY. PERFORMED BIT TEST PER PER M /M. ALL CKS GOOD. PERFORMED TEST OF SYS AND FOUND SYS TESTS NORMAL. 2 L 7 2 4F RT A6WE 2002082900134 20020829 00134 NM 2002 8 29 DLM90020935 1 20020810 A 3242 50121934 BRAKE ASSY DOUG MD90 MD9030 3023690 NM MLG FIRE A DALA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 902DA 53382 NR 2 BRAKE OVERHEAT ON ARRIVAL SOME FLAMES. COOLED BRAKES, NO FLAMES. REPLACED BRAKE ASSY AND NR 2 MAIN WHEEL ASSY. P ERFORMED BRAKE TEMP SENSOR TEST, TESTS OK. NO LEAKS FOUND. 2 L 7 2 4F RT A6WE 2002082900135 20020829 00135 NM 2002 8 29 DLM90020936 1 20020811 A 5240 DOOR SEAL DOUG MD90 MD9030 3023690 NM L2 DOOR DIRTY A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 911DA 53391 2L DOOR LEAK, CABIN ALTITUDE REACHED 10K FT. CHECKED 2L DOOR SEAL AND MATING SURFACE. NO DEFECTS NOTED. CLEANED 2L DO OR SEAL AND MATING SURFACE. PRESSURIZED ACFT TO 7 PSID. NO LEAKS/SQUEALS NOTED AT 2L. 2 L 7 2 4F RT A6WE 2002082900136 20020829 00136 NE 2002 8 29 NACA20020034 2 20020803 A 7421 URHB32E SPARK PLUG DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE NR 2 ENGINE SHORTED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 99330 113 113 43576 P33688 FEATHERED THE NR 2 ENGINE AT 2041Z DUE TO BACKFIRING IN CLIMB, AND DOUBLE SHORTED SECONDARY ON THE NR 10 CYLINDER. REMO VED AND REPLACED THE NR 10 LT & RT SPARK PLUGS. 2 L 7 4 4R 4 R 6A3 5E8 2002082900137 20020829 00137 NE 2002 8 29 NACA20020035 2 20020807 A 8530 356994 CYLINDER DOUG DC6 C118A 3021710 WP PWA R2800 R2800* 52026 NE NR 3 ENGINE CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 1377K 1939 1939 44596 P33192 FEATHERED THE NR 3 ENGINE AT 1841Z DUE TO RUNNING ROUGH AND LOW COMPRESSION INDICATED, NR 6 OR NR 17. REMOVED AND REPLA CED THE NR 17 CYLINDER ON THE NR 3 ENGINE. 2 L 7 4 4R 4 R 6A3 5E8 2002082900138 20020829 00138 EA 2002 8 29 SWIA200211109 1 20020804 A 3610 9799982 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 597SW 7293 AFTER TAKEOFF, SET 10TH STAGE VALVES PER SOP AND LEFT 10TH ARM OPEN APPEARED ON EICAS NR 2. FIRST OFFICER'S SYNOPTIC SH OWED LEFT 10TH VALVE WAS CLOSED, BUT LEFT 10TH SWITCH WAS PUSHED IN. RETURNED TO SLC. LANDED OVERWEIGHT BY 70 LBS. RE PLACED LEFT 10TH STAGE SOV. OPS CHECK GOOD. COMPLIED WITH OVERWEIGHT INSPECTION. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2002082900139 20020829 00139 SO 2002 8 29 SWIA200211118 1 20020807 A 5230 DOOR FRAME EMB 120 EMB120ER 3260203 SO CARGO DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 268UE 120207 C-CHECK, CRACK FOUND ON CARGO DOOR SIDE FRAME BEHIND LATERAL SUPPORT. REPLACED FRAME IAW 120 SRM 51-10-02 AND RII CARD 52-301. 2 L 7 2 4T RT A31SO 2002082900140 20020829 00140 SO 2002 8 29 SWIA200211119 1 20020811 A 2611 SENSOR EMB 120 EMB120ER 3260203 SO LAVATORY MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 292UX 120292 ON TAKOFF, AT 90 KAIS, TRIPLE CHIME SMOKE ALARM MAP SMOKE LIGHT ON MAP. ABORTED TAKEOFF. REPLACED LAV SMOKE SENSOR WIT H A SERVICEABLE UNIT. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002082900141 20020829 00141 SO 2002 8 29 SWIA200211120 1 20020810 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 583SW 5647 5647 120351 EMERGENCY LIGHTS AFT OF ROW 7 ARE INOP. REPLACED BATTERY PACK. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002082900142 20020829 00142 WP 2002 8 29 AAL2002F00000 1 20020728 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE EMER EXIT SYSTEM RESTRICTED A AALA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SW 21 476AA 49651 DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT OVER TAIL CONE WALKWAY, INOPERATIVE. RESET OVER EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2002082900143 20020829 00143 WP 2002 8 29 AALA20021096 1 20020728 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE EMER EXIT SYST INOPERATIVE A AALA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SW 21 476AA 49651 DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT OVER TAIL CONE WALKWAY, INOPERATIVE. RESET OVER EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2002082900144 20020829 00144 2002 8 29 DHL2002740004 4 20020827 A 3410 HG480B20 ADC BOEING 727 7272Q9 138448M NM A DHLA C D O ABORTED TAKEOFF RETURN TO BLOCK OTHER O OTHER TO TAKEOFF 1 SO 01 740DH 21930 1) WARNING FLAGS APPEAR IN AIRSPEED, ALTIMETER & VERTICAL SPEED INDICATOR WHEN TAKING RUNWAY FOR TAKEOFF. 2)R&R #2 ADC AND PERFORMED PITOT STATIC LEAK CHECK IAW B727 M/M 34-12-11 AND 34-11-0. NO LEAKS NOTED OPS CHECK NORMAL. TAPE REMOVED. 2 L 7 3 4F RT A3WE 2002082900145 20020829 00145 WP 2002 8 29 AALA20021095 1 20020728 A 3350 WIRE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE EMER EXIT SYST INOPERATIVE A AALA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SW 21 73444 49470 DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT ABOVE AFT FLIGHT ATTENDANT SEAT INOPERATIVE. SPLICED WIRES OVER AFT L AVATORY EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2002082900146 20020829 00146 WP 2002 8 29 AALA20021077 1 20020722 A 3350 WIRE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE TAIL LOOSE A AALA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SW 21 571AA 49353 DURING OVERNIGHT MAINTENANCE TAIL CONE EMERGENCY EXIT BATTERY WIRE LOOSE. TIGHTENED SCREW ON TAIL CONE EMERGENCY EXIT B ATTERY FOR WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E2EA 2002082900147 20020829 00147 NM 2002 8 29 AALA20021138 1 20020808 A 2410 GE5103 GENERATOR BOEING 767 767323 1385205 NM GE CF6 CF680 30025 NE RIGHT GENERATOR INOPERATIVE A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 376AN 25445 GENERATOR , POSN RIGHT GENERATOR. ENGINE DRIVEN GENERATOR SYSTEMS, INOPERATIVE. DELTA P TRIP AND HIGH OIL TEMPERATURE. 2 L 7 2 4F 4 F RT A1NM E13NE 2002082900148 20020829 00148 NM 2002 8 29 AALA20021137 1 20020805 A 2410 GEN3014 GENERATOR BOEING 777 777223 1385213 NM RROYCE RB211 RB211* 54555 NE LEFT FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 795AN 30257 ON DEPARTURE, LEFT GENERATOR, OFF LIGHT ALONG WITH THE DRIVE LIGHT ILLUMINATED. THE DRIVE WAS DISCONNECTED AS PER THE C HECKLIST. REMOVED AND REPLACED LEFT IDG OPS 2 LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT T00001SE A12EU 2002082900149 20020829 00149 NE 2002 8 29 SWIA200211121 2 20020813 A 7320 3035659 HMU EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 235SW 120310 ON TAKEOFF ROLL, RIGHT ENGINE TORQUE WAS OBSERVED TO FLUCTUATE FROM 95 PERCENT DOWN TO 85 PERCENT AND BACK A NUMBER OF T IMES. TAKEOFF WAS ABORTED. REPLACED RIGHT ENGINE HMU WITH A SERVICEABLE UNIT. NO LEAKS NOTED AT THIS TIME. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002082900150 20020829 00150 EA 2002 8 29 SWIA200211122 1 20020809 A 3222 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG BENT A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 417SW 7400 ON DEPARTURE OUT OF DFW, DURING GEAR RETRACTION, WARNING MESSAGES GEAR DISAGREE AND NOSE DOOR ANNUNCIATED. THE NOSE GEA R INDICATED DOWN AND LOCKED WITH GEAR SELECTED UP. COMPLETED QRH PROCEDURES AND AFTER BURNING OFF EXCESS FUEL, A NORMAL LANDING WAS MADE BACK AT DFW. STRAIGHTENED NOSE GEAR TORQUE LINK BRACKET AND CALIBRATED PROX SENSOR GAP. SWUNG GEAR 3 TIMES WITH NORMAL OPERATION. 2 L 7 2 4F 4 F RT A21EA E15NE 2002082900151 20020829 00151 EA 2002 8 29 SWIA200211123 1 20020813 A 2742 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE HORIZ STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 595SW 2472 2472 7292 STAB TRIM CH 2 WILL NOT ENGAGE. REPLACED HSTA AND MOTOR CONTROL UNIT. STAB TRIM OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002082900152 20020829 00152 EA 2002 8 29 SWIA200211124 1 20020809 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN DETECTED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 594SW 7285 ELECTRICAL SMOKE SMELL IN COCKPIT JUST AFTER TAKEOFF. FLIGHT ATTENDANT REPORTED THE SAME SMELL IN THE CABIN WITH A VERY LIGHT SMOKE IN THE REAR OF THE CABIN. VISUALLY INSPECTED CABIN LIGHTING AND BALLAST FOR EVIDENCE OF OVERHEAT. NO FAUL TS FOUND. RAN LEFT AND RIGHT ECS, DID DETECT SLIGHT ODOR. RAN PACKS IN HOT, NO SMOKE OCCURRED AND AFTER SEVERAL MINUTE S ODOR WAS NOT DETECTABLE. SELECTED PACKS BACK TO COLD, NO ODOR PRESENT AND PACK OPERATION NORMAL. UNABLE TO DUPLICATE ANY SMOKE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002082900153 20020829 00153 NM 2002 8 29 AALA20021130 1 20020803 A 3350 CONNECTOR BOEING 777 777223 1385213 NM RROYCE RB211 RB211* 54555 NE EMER EXIT SYSTEM UNSECURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 37C. RESECURED EMERGENCY PATH LIGHTING CONNE CTOR AT SEAT 37D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT T00001SE A12EU 2002082900154 20020829 00154 EA 2002 8 29 SWIA200211125 1 20020814 A 3030 7858062 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE PITOT HEAT MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 588SW 3140 3140 7069 CRUISE FLT AT 310 RECEIVED A CAUTION (PITOT BASE HEAT) FOLLOWED BY A (ESSN TRU 1) CAUTION. CB 3-A2 POPPED ON IT'S OWN. REMOVED & REPLACED NR 3 AIR DATA SENSOR HEAT CONTROLLER. OPS CHECKED FOR 30 MIN. REMOVED AND REPLACED ESS TRU CB3-A2. CHECKS GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 2002082900155 20020829 00155 SO 2002 8 29 SWIA200211126 1 20020815 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 199SW 7742 1562 120237 NACELLE FLAPS WOULD NOT GO PAST 4 ROWS OF LIGHTS WHEN 25 DEGREES OF FLAPS SELECTED. FLAP DISAGREEMENT WARNING. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB120 MM 27-50-09. LEAK CHECK GOOD. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2002082900156 20020829 00156 SO 2002 8 29 SWIA200211127 1 20020815 A 5753 12037299002 STRUCTURE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE T/E FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 199SW 120237 RIGHT NACELLE FLAP FOUND CRACKED. REMOVED AND REPLACED RIGHT NACELLE FLAP IAW MM 27-50-03. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002082900157 20020829 00157 NM 2002 8 29 AALA20021129 1 20020803 A 3350 CONNECTOR BOEING 777 777223 1385213 NM RROYCE RB211 RB211* 54555 NE EMER EXIT SYSTEM UNSECURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 37G. RESECURED EMERGENCY PATH LIGHTING CONNEC TOR AT SEAT 37D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT T00001SE A12EU 2002082900158 20020829 00158 EA 2002 8 29 SWIA200211128 1 20020814 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE MLG MALFUNCTIONED A SWIA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 07 416SW 7089 AFTER TAKEOFF ON GEAR UP RECEIVED GEAR DISAGREE AURAL AND AIRCRAFT BUFFETING. RAN QRH, AND PROBLEM REMAINED. AT SAME T IME NOTICED THE NR 1 BTMS INDICATION INOP. RETURNED TO SLC. REMOVED AND REPLACED MLG PRIORITY VALVE PER CRJ MM 32-32-1 5. OPERATIONAL CHECK GOOD. LEAK CHECK GOOD. REMOVED AND REPLACED NR 1 BTM SENSOR. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002082900159 20020829 00159 NE 2002 8 29 SWIA200211129 2 20020815 A 7320 78639010 HMU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE FAILED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 581SW 2553 2553 120349 LEFT ENGINE EEC FAILURE ON TAKEOFF ROLL. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE HMU IAW RII 73-301 & MM 73- 21-00. OPS & LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002082900160 20020829 00160 2002 8 29 SWIA200211130 4 20020815 A 2213 8220044001 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 430SW 2733 2661 7523 YAW DAMPER 2 WILL NOT ENGAGE. REMOVED AND REPLACED FCP 4002 IAW CRJ MM 22-11-07. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002082900161 20020829 00161 EA 2002 8 29 SWIA200211131 1 20020814 A 2720 601R122623 POTENTIOMETER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT TWISTED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 432SW 7548 RUDDER TRIM WILL NOT TRIM TO THE LEFT. FOUND RUDDER TRIM POTENTIOMETER TWISTED IN THE MOUNTS, AND A WIRE LOOSE. REPLAC ED RUDDER TRIM PANEL WITH SERVICEABLE UNIT. OPS CHECKS GOOD IAW CRJ MM 27-00-00. 2 L 7 2 4F RT A21EA 2002082900162 20020829 00162 NM 2002 8 29 USAASB02152 1 20020813 A 3233 ACTBEAMLINK400 ACTUATOR BOEING 737 737401 1384701 NM GE CFM56 CFM56* 13802 NE LT MLG FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 407US 36467 23877 ON CLIMB OUT, ENROUTE, CREW REPORTED THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT AFTER PLACING GEAR LEVER TO THE UP POS ITION. THE LEFT MAIN LANDING GEAR UNSAFE LIGHT WAS ALSO ILLUMINATED. CREW RECEIVED NORMAL GEAR INDICATION OF THREE GRE EN LIGHTS WHEN GEAR WAS EXTENDED. FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAI NTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR RETRACT ACTUATOR PER MM. ALSO, REMOVED AND REPLACED LEFT MAIN LANDING GEAR UPLOCK SENSOR (PN 189929). OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082900163 20020829 00163 NM 2002 8 29 USAASB02154 1 20020816 A 2930 693731768 PANEL BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE OVHD HYDR PANEL ILLUMINATED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 510AU 23385 DURING CRUISE, ENROUTE, THE NR1 ENGINE DRIVEN HYDRAULIC PUMP (A) SYSTEM LOW PRESSURE LIGHT ILLUMINATED. FIVE MINUTES LA TER, THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP (B) SYSTEM LOW PRESSURE LIGHT ILLUMINATED. HYDRAULIC SYSTEM QUANTITY WAS OK AND HYDRAULIC SYSTEM PRESSURE REMAINED AT 3,000 PSI WIGHT ELECTRIC PUMPS. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT F URTHER INCIDENT. NO EMERGENCY WAS DECLARED. COULD NOT DUPLICATE PROBLEM. ALL HYDRAULIC SYSTEMS OPERATE NORMAL. REMOV ED AND REPLACED THE P5-8 OVERHEAD HYDRAULIC PANEL AS PRECAUTIONARY. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082900164 20020829 00164 NM 2002 8 29 USAASB02155 1 20020817 A 3397 WIRE BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE EMR LIGHT WIRE BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 517AU 23703 MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT 17, INOPERATIVE. REPAIRED WIRING AT SEAT 17. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082900165 20020829 00165 NM 2002 8 29 USAASB02156 1 20020817 A 3397 WIRE BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE EMERGENCY LT BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 526AU 23861 FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHT AT SEAT ROW 10, LEFT HAND SIDE, HAS A BROKEN WIRE. MAINTENANCE REPAIRED B ROKEN WIRE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002082900166 20020829 00166 2002 8 29 USAASA02065 4 20020721 A 2565 D31517113 SLIDE AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE ESCAPE SLIDE BULGED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 716UW 8248 1055 THE AFT LEFT SLIDE COVER WILL NOT STAY ON. MAINTENANCE FOUND THE AFT LEFT SLIDE LACING LOOSENED UP AND SLIDE BULGING, N OT ALLOWING SLIDE COVER TO STAY ON. REPLACED THE AFT LEFT SLIDE ASSEMBLY. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E2GL 2002082900167 20020829 00167 2002 8 29 MWEA020518 4 20020829 A 2312 SBA53188 ANTENNA DOUG DC9 DC981 3022081 WP STA 474 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FORWARD LEFT VHF ANTENNA INTERCOSTAL HAS A 6" CRACK RUNNING FORWARD AND AFT AT FUSELAGE STATION 474. -- INSTALLED 5&6 ANGLES TO INTERCOSTALS AND 3 DOUBLER TO SKIN. 2 L 7 2 4F A6WE 2002082900168 20020829 00168 WP 2002 8 29 MWWA020519 1 20020829 A 5241 592081423 DOOR DOUG DC9 DC932 3022066 WP GALLEY DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 GALLEY DOOR SILL DRAIN SKIN DOUBLER CORRODED BEYOND LIMITS. -- LOCATED AND DRILLED NEW 23 DOUBLER. 2 L 7 2 4F A6WE 2002082900169 20020829 00169 WP 2002 8 29 MWEA020520 1 20020829 A 5310 5910130391 SPLICE DOUG DC9 DC932 3022066 WP LONG.11L&12L CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 APB TEE CRACKED NOTED BETWEEN LONGERON 11L & 12L APPROX. 2" LONG. -- CUT AND SPLICE SECTION OF APB TEE PER SRO 953001 2 L 7 2 4F A6WE 2002082900170 20020829 00170 WP 2002 8 29 MWEA020521 1 20020829 A 5753 59121551TE WING DOUG DC9 DC932 3022066 WP OUTBD FLAP DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LEFT OUTBOARD FLAP TRAILING EDGE DAMAGED AND AFT TRAILING EDGE CHANNEL. -- REMOVED AND REPLACED TRAILING EDGE. 2 L 7 2 4F A6WE 2002082900171 20020829 00171 2002 8 29 USAASA02068 4 20020808 A 2565 D30664105 SLIDE AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE PASSENGER CABIN MALFUNCTIONED A USAA K NONE J W WARNING INDICATION INADEQUATE Q C CR CRUISE 1 EA 19 110UW 1112 ENROUTE, DURING FLIGHT, THE SERVICE DOOR BECAMED DISARMED. THE RED WARNING LIGHT FLASHES CONTINUOUSLY IN CABIN DOORS AN D CABIN INTERCOM DATA SYSTEM. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FORWARD SERVICE DOOR SL IDE ASSEMBLY. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2002082900172 20020829 00172 EA 2002 8 29 COMA0260502 1 20020827 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 708CA 7192 7235 FLIGHT 5611 GEAR DISAGREE MESSAGE DURING RETRACTION ANFD EXTENSION.REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002082900173 20020829 00173 EA 2002 8 29 COMA0260501 1 20020829 A 5330 CART CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER C F.O.D. IN INSP/MAINT 1 SO 01 949CA 7080 A/C FUSELAGE STRUCK BY BAGGAGE CART AND SUSTAINED MAJOR DAMAGE BETWEEN F.S. 654 AND 672, AND STRINGERS 21L TO 23L.C/W RE PAIR TO SKIN AND STRINGERS I/A/W SRM 53-00-31 AND 53-00-03 AND REO 601R 53-61-577 AND 579. 2 L 7 2 4F RT A21EA 2002082900174 20020829 00174 EU 2002 8 29 AWXA200200842 1 20020826 A 3350 ABS0374A24 CABLE AIRBUS 320 A320231 3930325 EU SEAT ROW 26 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 0 0 271 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPA IRED A BROKEN WIRE AND REPLACED CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 L/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002082900175 20020829 00175 NM 2002 8 29 AWXA200200846 1 20020825 A 5311 654583470 STRAP BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 MCN- MAJOR REPAIR - DURING C-16 CHECK A 1 1/4" CRACK WAS FOUND ON THE LOWER FRAME TO FRAME STRAP AT BS 312 - 328, LBL 0 1, WL 201. MAINTENANCE REMOVED 2 EACH PREVIOUSLY INSTALLED REPAIRS AT BS 312 - 328, LBL 01. FABRICATED A REPAIR PLATE, A ND INSTALLED REPAIR IAW B737-300 SRM 53-10-51, PG. 213 - 219, FIG. 204. 2 L 7 2 4F RT A16WE 2002082900176 20020829 00176 NM 2002 8 29 AWXA200200847 1 20020820 A 5320 65479573 WEB BOEING 737 7373B7 1384580 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON WEB IN AFT CARGO COMPARTMENT AT BS 845, RBL 22, WL 155. M AINTENANCE REMOVED CORROSION ON WEB IN AFT CARGO COMPARTMENT AT BS 845, RBL 22, AND FOUND MATERIAL LOSS OUT OF LIMITS. R EMOVED DAMAGED WEB, FABRICATED A NEW -3 WEB, AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG. 5, AND SRM 51-20-05, PG . 3-4. 2 L 7 2 4F RT A16WE 2002083000001 20020830 00001 SO 2002 8 30 ASOA02264 1 20020509 A 3350 FUSE EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 503AS 120275 FLT 4336 - DURING GROUND INSPECTION IN ATL, THE FORWARD STRIP OF EMERGENCY FLOOR LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE FOR THE FORWARD SECTION OF EMERGENCY STRIP LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT O K FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002083000002 20020830 00002 SO 2002 8 30 ASOA02265 1 20020509 A 3350 FILTER EMB 120 EMB120RT 3260202 SO CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 237AS 120051 DURING A HANGAR INSPECTION IN MCN, THE FORWARD FLOOR EMERGENCY LIGHT, IN FRONT OF THE PASSENGER DOOR WAS MISSING THE RED LAMP FILTER. MAINTENANCE INSTALLED A NEW RED LAMP FILTER WHERE THE MISSING ONE WAS DISCOVERED. AIRCRAFT OK FOR SERVIC E. (M) 2 L 7 2 4T RT A31SO 2002083000003 20020830 00003 EU 2002 8 30 ASOA02266 1 20020509 A 3350 167006 BULB AEROSP ATR72 ATR72212 8680945 EU CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 634AS 370 DURING A HANGAR INSPECTION IN MCN, THE EMERGENCY FLOOR LIGHT BETWEEN ROW 7B AND 8B WAS FOUND TO BE INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED A BURNED OUT LIGHT BULB IN EMERGENCY FLOOR TRACK BETWEEN ROWS 7B AND 8B. OPERATIONAL CHECK GO OD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002083000004 20020830 00004 SO 2002 8 30 ASOA02267 1 20020511 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT 3260202 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 265AS 120170 DURING A HANGAR INSPECTION IN MCN, THE AFT SECTION OF EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE EMERGENCY LIGHTING BATTERY PACK IN THE NR 3 POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002083000005 20020830 00005 EA 2002 8 30 ASOA02268 1 20020512 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 886AS 7531 DURING GROUND INSPECTION IN ATL, THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE BURNED OUT LIGHT BULB IN THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRA FT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002083000006 20020830 00006 EA 2002 8 30 ASOA02269 1 20020512 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 843AS 7310 FLT 4787 - DURING A SCHEDULED INSPECTION IN XNA, THE AFT CEILING EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE BURNED OUT CEILING EMERGENCY LIGHT BULB. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002083000007 20020830 00007 SO 2002 8 30 ASOA02270 1 20020430 A 5310 12046163001 STRAP EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP BETWEEN FRAMES 35 AND STATION 13056 WAS FOUND CORRODED BEYOND LIMI TS. MAINTENANCE REMOVED AND REPLACED THE CORRODED LEFT BUTT STRAP IAW SRM'S 51-25-00, 51-40-05, AND 51-40-06. (M) 2 L 7 2 4T RT A31SO 2002083000008 20020830 00008 SO 2002 8 30 ASOA02271 1 20020430 A 5347 12015995003 SEAT TRACK EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C-CHECK INSPECTION IN BNA, THE LEFT FORWARD FLOOR SEAT TRACK WAS FOUND CORRODED BEYOND LIMITS BETWEEN FRAMES 15 A ND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM'S 51-25-00, 51-40-06, 51-10-00. MAINTENANCE AL SO COMPLIED WITH ASA EO 120-25-0007C WHICH FACILITATES SEAT TRACK SPLICING INSTRUCTIONS AND ESTABLISHES WEAR LIMITS USIN G EST-381/93, DATED 30 AUGUST 1993, AS A REFERENCE. (M) 2 L 7 2 4T RT A31SO 2002083000009 20020830 00009 SO 2002 8 30 ASOA02272 1 20020430 A 5347 12015997003 SEAT TRACK EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C-CHECK INSPECTION, THE RIGHT FORWARD WALL SEAT TRACK WAS CORRODED OUT OF LIMITS BETWEEN FRAMES 15 AND 32. MAINT ENANCE REMOVED AND REPLACED THE CORRODED WALL SEAT TRACK IAW ASA EO 120-25-0007C, WHICH USES EST-381/93, DATED 30 AUGUST 1993, AS A REFERENCE TO FACILITATE SEAT TRACK SPLICING INSTRUCTIONS AND ESTABLISH WEAR LIMITS. MAINTENANCE ALSO USED S RM'S 51-40-02 AND 51-21-00 AS REFERENCE. (M) 2 L 7 2 4T RT A31SO 2002083000010 20020830 00010 SO 2002 8 30 ASOA02273 1 20020430 A 5311 12002545002 FRAME EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C-CHECK INSPECTION IN BNA, THE SKIN SUPPORT AT FRAME 22, BETWEEN STRINGERS 18 LEFT AND 19 LEFT, WAS CORRODED OUT OF LIMITS AND ALSO HAD A CRACK MIGRATING FROM A RIVET HOLE. MAINTENANCE REMOVED AND REPLACED TEH CORRODED AND CRACKED S IN SUPPORT IAW SRM'S 51-25-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002083000011 20020830 00011 SO 2002 8 30 ASOA02274 1 20020513 A 3397 MS3476L2255P CONNECTOR EMB 120 EMB120ER 3260203 SO LEFT WING MISREPAIRED A ASOA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 11 505AS 120279 DURING GROUND INSPECTION IN TXK, THE LEFT AFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE FOUND THE CON NECTOR P0949 HAD PINS A AND B REVERSED. MAINTENANCE REPINNED A AND B AND ALSO REPLACED THE IN LINE FUSE. OPERATIONAL C HECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002083000012 20020830 00012 EA 2002 8 30 ASOA02275 1 20020513 A 3350 58351 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 837AS 7271 DURING GROUND INSPECTION IN FAY, THE FIRST FOUR FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWA RD ORANGE EMERGENCY LIGHTING STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002083000013 20020830 00013 EU 2002 8 30 ASOA02276 1 20020514 A 3350 7012210 BULB AEROSP ATR72 ATR72 EU PAX DOOR BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 630AS 336 DURING A HANGAR INSPECTION IN MCN, THE EMERGENCY LIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE INOPERATIVE LIGHT BULB ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE . (M) 2 H 7 2 4T RT 2002083000014 20020830 00014 EU 2002 8 30 ASOA02277 1 20020509 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 640AS 405 DURING C-CHECK INSPECTION IN BNA, THE UPPER FLOORBEAM WAS FOUND CORRODED AT FRAME 36, FROM THE RIGHT TO THE LEFT SIDE OF THE FUSELAGE. MAINTENANCE REPAIRED THE CORRODED FLOORBEAM IAW ASA EO 72-53-0131. THIS EO REF FAA FORM 8110-3, REPORT NR 02-041, WHICH INCLUDES REPAIR SPECIFICATIONS FOR AIRCRAFT N640AS. (M) 2 H 7 2 4T RT 2002083000015 20020830 00015 EU 2002 8 30 ASOA02278 1 20020509 A 5313 STRINGER AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 640AS 405 DURING C-CHECK INSPECTION IN BNA, FRAMES 38, 39 AND 40 WERE ALL FOUND CORRODED THE ENTIRE LENGTH FROM STRINGER 16 LEFT T O 16 RIGHT. MAINTENANCE REPAIRED ALL THREE CORRODED FRAMES IAW ASA EO 72-53-0131. THIS EO REFERENCE FAA FORM 8110-3, R EPORT NUMBER 02-041, WHICH INCLUDES REPAIR SPECIFICATIONS FOR AIRCRAFT N640AS. (M) 2 H 7 2 4T RT 2002083000016 20020830 00016 EU 2002 8 30 ASOA02279 1 20020509 A 5330 SKIN AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 640AS 405 DURING C-CHECK INSPECTION IN BNA, THE RIGHT FUSELAGE SKIN WAS FOUND DENTED BEYOND LIMITS BETWEEN FRAMES 23A AND 23B AS W ELL AS BETWEEN STRINGERS 13 RIGHT AND 14 RIGHT. MAINTENANCE REPAIRED THE DENTED FUSELAGE SKIN IAW ASA EO 72-53-0131. T HIS EO REF FAA FORM 8110-3, REPORT NR 02-041, WHICH INCLUDES REPAIR SPECIFICATIONS FOR AIRCRAFT NR 640AS. (M) 2 H 7 2 4T RT 2002083000017 20020830 00017 EU 2002 8 30 ASOA02280 1 20020515 A 3350 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 634AS 370 FLT 4134 - DURING GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE LIGHTED EXIT SIGN OVER THE FORWARD FLIGHT ATTENDANT SEAT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING POWER SUPPLY IN THE 61WL POSITI ON. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002083000018 20020830 00018 WP 2002 8 30 GTIA020716 1 20020626 A 2731 ACTUATOR DOUG DC9 DC982 3022082 WP TRIM INOPERATIVE A GTIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 821NK 49508 MYR - FLT 1751 - PRIMARY TRIM INOPERATIVE, WILL NOT MOVE FORE OR AFT WITH EITHER YOKE MOUNTED CONTROLS OR LONG TRIM HAND LES. REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR PER MD80 MM 27-40-05. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002083000019 20020830 00019 WP 2002 8 30 GTIA020717 1 20020610 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - MID CARGO INTERCOSTAL STATION 541-560 LONGERON 26L CRACKED TWO PLACES. FORMED NEW INTERCOSTAL AND ATTACHING L-ANG LE. (M) 2 L 7 2 4F A6WE 2002083000020 20020830 00020 WP 2002 8 30 GTIA020718 1 20020622 A 3201 DEFLECTOR DOUG DC9 DC981 3022081 WP NLG CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND RIGHT SIDE OF NOSE GEAR SPRAY DEFLECTOR CRACKED. REPLACED RIGHT SIDE OF NOSE GEAR SPRAY DEFLECTOR. NO DEFE CTS NOTED. (M) 2 L 7 2 4F A6WE 2002083000021 20020830 00021 WP 2002 8 30 GTIA020720 1 20020625 A 2750 SWITCH DOUG DC9 DC982 3022082 WP TE FLAPS OUT OF POSITION A GTIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 800NK 49144 DTW - FLT 503 - RECEIVED TAKEOFF WARNING, RETURN TO GATE, DIAL A FLAP WAS STOWED. ADJUSTED FLAP HANDLE POSITION SWITCH PER MM 27-51-00. TAKEOFF WARNING, OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4F A6WE 2002083000022 20020830 00022 WP 2002 8 30 GTIA020721 1 20020625 A 2731 COMPUTER DOUG DC9 DC982 3022082 WP TRIM MALFUNCTIONED A GTIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 23 800NK 49144 MCO - FLT 506 - TAKEOFF CONDITION LONG TRIM COMPUTER HAS EXCESSIVE PLAY, CAN ROLL CG WHEEL UP TO TWO UNITS AND THE INDIC ATOR WILL NOT MOVE. FOUND LONG TRIM COMPUTER POINTER STICKING FREED POINTER, OPS CHECK GOOD IAW MD80 MM 27-41-00. (M) 2 L 7 2 4F A6WE 2002083000023 20020830 00023 WP 2002 8 30 GTIA020722 1 20020626 A 2731 ARM DOUG DC9 DC982 3022082 WP ELEVATOR TRIM LACK OF LUBE A GTIA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 23 820NK 49126 LGA - FLT 1765 - ALT TRIM INOPERATIVE UP, OPERATED NORMALLY DOWN POSITION. LUBED ATTACHING ARM TO S10-7 ALT SWITCH. SY STEM OPS CHECKS OK PER MM 27-40-01. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 2002083000024 20020830 00024 WP 2002 8 30 GTIA020723 1 20020626 A 2731 561349 SWITCH DOUG DC9 DC982 3022082 WP ELEVATOR TRIM INTERMITTENT A GTIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 23 820NK 49126 LGA - FLT 1765 - ALT TRIM SWITCHES STOP OPERATING INTERMITTENT. REMOVED AND REPLACED ALT LONG TRIM MOTOR CONTROL SWITCH IAW MM 27-40-09, OPS NORMAL. (M) 2 L 7 2 4F A6WE 2002083000025 20020830 00025 NM 2002 8 30 GTIA020724 1 20020625 A 3397 WIRE DOUG MD80 MD83 3023681 NM TAIL CONE CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 DTW - FOUND WIRES CHAFED IN AFT ACC COMPARTMENT AT TAILCONE JETTISON HANDLE LIGHT ASSEMBLY. SECURED CHAFING WIRES AFT A CC COMPARTMENT IAW MD80 MM 20-50-02 AND REPLACED CHAFFED WIRES. OPS CHECK GOOD. (M) 2 L 7 2 4F RT 2002083000026 20020830 00026 2002 8 30 GTIA020725 4 20020625 A 2565 SLIDE DOUG DC9 DC983 3022083 WP CABIN DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 827NK 49793 FLL - FLT 258 - SLIDE PACK SEPARATED FROM HOUSING. INSTALLED SLIDE PACK IAW MD80 MM 25-62-00. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 2002083000027 20020830 00027 2002 8 30 GTIA020726 4 20020626 A 3460 4034241973 COMPUTER DOUG DC9 DC983 3022083 WP COCKPIT MALFUNCTIONED A GTIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 23 827NK 49793 FLL - FLT 258 - AUTOPILOT DISCONNECTS IN RIGHT TURNS DFGS NR 2 POSITION. REMOVED AND REPLACED NR 2 DFGC IAW MD80 MM 22- 01-01, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2002083000028 20020830 00028 WP 2002 8 30 GTIA020727 1 20020626 A 3397 WIRE DOUG DC9 DC941 302207N WP EXIT SIGN CUT A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 47605 ACY - AFT EMERGENCY EXIT SIGN INOPERATIVE. FOUND AFT EMERGENCY EXIT SIGN WIRE DISCONNECTED AND CUT ON TERMINAL STRIP. CONNECTED AND SPLICED WIRE FOR AFT EMERGENCY EXIT SIGN, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002083000029 20020830 00029 2002 8 30 GTIA020728 4 20020627 A 2210 4034242934 CONTROL PANEL DOUG DC9 DC983 3022083 WP COCKPIT FAILED A GTIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 808NK 9541 49504 FLT 706 - LGA - IAS/MACH BUTTON WILL NOT SWITCH TO MACH ON DFGS NR 2, OK ON NR 1. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL PANEL. PERFORMED OPS HECK IAW MM 22-01-05. OPS CHECKS NORMAL. (M) 2 L 7 2 4F RT A6WE 2002083000030 20020830 00030 2002 8 30 GTIA020729 4 20020630 A 3460 4034241972 COMPUTER DOUG DC9 DC983 3022083 WP COCKPIT MALFUNCTIONED A GTIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 23 808NK 3819 49504 LGA - FLT 706 - WITH DFGC SELECTED TO POSITION 2 WHEN MACH VERTICAL SPEED SELECTED WILL NOT ENGAGE MACH BUT REMAINS IN I AS WHEN DFGC NR 1 SELECTED WORKS FINE. REMOVED AND REPLACED DFGC PER MD80 MM 22-01-01, SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2002083000031 20020830 00031 2002 8 30 GTIA020730 4 20020702 A 3460 4034241971 COMPUTER DOUG DC9 DC981 3022081 WP COCKPIT MALFUNCTIONED A GTIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 23 806NK 48051 FLT 1453 - ORD - AUTO PILOT WILL NOT ENGAGE ON NR 1 OR NR 2 DFGC. FOUND A/P HEAR BEAT FAILS ON BOTH NR 1 AND NR 2 DFGC. REMOVED AND REPLACED NR 1 AND NR 2 DFGC. OPS CHECKED GOOD PER MD80 MM 22-01-05. NO OTHER DISCREPANCIES NOTED. (M) 2 L 7 2 4F A6WE 2002083000032 20020830 00032 2002 8 30 GTIA020732 4 20020629 A 2565 SLIDE DOUG DC9 DC982 3022082 WP CABIN DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FLL - FLT 1751A - FOUND ESCAPE SLIDE AT L2 DOOR CAME LOOSE. REINSTALLED ESCAPE SLIDE AT L2 DOOR IAW MD80 MM 25-62-00. (M) 2 L 7 2 4F A6WE 2002083000033 20020830 00033 2002 8 30 GTIA020733 4 20020628 A 3460 4034242923 CONTROL PANEL DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A GTIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 23 803NK 48087 MCO - FLT 594A - AUTO THROTTLE TURNED OFF ON APPROACH WHEN SPEED WAS CHANGED AUTO PILOT 2. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROLLER IAW MD80 MM 22-13-00. OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4F A6WE 2002083000034 20020830 00034 WP 2002 8 30 GTIA020769 1 20020702 A 2913 624372 CASE DOUG DC9 DC982 3022082 WP HYD PUMP SPLIT A GTIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 820NK 49126 FLT 1863 - LGA - RIGHT HYDRAULIC PRESSURE LOW AND RUDDER CONTROL MANUAL LIGHTS ILLUMINATED IN FLIGHT. RIGHT HYD PRESS ' 0' RIGHT HYD QUANTITY 2 QUARTS LANDING MANUAL EXTENSION USD. PROBLEM OCCURRED AT FL240 WITH ENGINE PUMPS ON LOW XFER AU X PUMP OFF. FOUND RIGHT AUX HYD PUMP CASE SPLIT APART. REMOVED AND REPLACED SAME PER MM 29-10-06. REMOVED AND REPLACE D RIGHT SYSTEM RETURN FILTERS PER MM 29-10-14. SERVICED RIGHT HYD SYSTEM PER MM 12-13-02. OPS AND LEAK CHECK GOOD. (M ) 2 L 7 2 4F A6WE 2002083000035 20020830 00035 WP 2002 8 30 GTIA020770 1 20020704 A 2750 CONTROL HANDLE DOUG DC9 DC982 3022082 WP TE FLAPS LACK OF LUBE A GTIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 23 820NK 49126 LGA - FLT 197 - FLAP TAKEOFF SELECTOR DOES NOT LOCK FLAPS IN THE 'OPTIUM FLAP' POSITION, ALTHOUGH THE DETENT CAN BE SEEN THE FLAP HANDLE DOES NOT 'LOCK' INTHE DETENT AND CAN BE BUMPED AND CHANGE POSITION FOR TAKEOFF. INSPECTED, LUBED AND O PERATED DIAL A FLAP MECH SEVERAL TIMES, FOUND TO WORK NORMAL IAW MM 27-50-00. (M) 2 L 7 2 4F A6WE 2002083000036 20020830 00036 2002 8 30 GTIA020771 4 20020705 A 3414 4057800906 INDICATOR DOUG DC9 DC983 3022083 WP COCKPIT MALFUNCTIONED A GTIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 23 825NK 3135 53012 DTW - DURING TAKEOFF, CAPTAINS AIRSPEED READ 75 KNOTS WHEN F/O'S READ 80 KTS WHEN F/O'S AIRSPEED READ 115KTS, CAPTAINS R EAD 100KTS, TAKEOFF ABORTED. MAX BRAKE TEMPS 20 DEGREES. REMOVED AND REPLACED F/O'S AIRSPEED INDICATOR, SYSTEM GROUND CHECKED GOOD. (M) 2 L 7 2 4F RT A6WE 2002083000037 20020830 00037 WP 2002 8 30 GTIA020772 1 20020614 A 5320 DOUBLER DOUG DC9 DC981 3022081 WP STRUT CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND STRUT DOUBLERS CORRODED. DOUBLER FOUND TO BE OUT OF LIMITS. FABRICATED NEW DOUBLER PER SRM MD80. (M) 2 L 7 2 4F A6WE 2002083000038 20020830 00038 WP 2002 8 30 GTIA020773 1 20020531 A 5743 STRAP DOUG DC9 DC981 3022081 WP MLG CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND LEFT WING LOWER SURFACE MLG STRAP HAS CRACK. PERFORMED HFEC INSPECTION OF SUSPECTED CRACKED HOLES IN STRAP AND LOWE WING SKIN PLANK. REPAIR DAMAGED AREA IAW MD80 SRM 57-03 AND SPIRIT AIRLINE DRAWING NR 57300206-1. (M) 2 L 7 2 4F A6WE 2002083000039 20020830 00039 WP 2002 8 30 GTIA020774 1 20020610 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND PASSENGER CABIN WEB CORRODED AT THE STATION 180 PLUS X57 INCHES. CUT OUT DAMAGED WEB SECTION AND FABRICATE D NEW WEB SECTION AND DOUBLER, INSTALLED WEB SECTION. (M) 2 L 7 2 4F A6WE 2002083000040 20020830 00040 WP 2002 8 30 GTIA020775 1 20020625 A 2760 CONTROL CABLE DOUG DC9 DC981 3022081 WP SPOILERS LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND SPOILER SURFACE POSITION INPUT FAILED DFDR GROUND CHECKED. T/S SYSTEM FLIGHT SPOILERS ONLY DEPLOY TO 37 USI NG SPEED BRAKE HANDLE. CHECK TENSION ON BODY CONTROL CABLE OF SPEED BRAKE CABLES RN 159 AND 160. FOUND TENSION LOW, RE TENSION CABLES. (M) 2 L 7 2 4F A6WE 2002083000041 20020830 00041 WP 2002 8 30 GTIA020776 1 20020601 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP CARGO BAY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND FORWARD PIT HAS CORROSION AT INTERCOSTAL STATION 465 TO STATION 484. SKIN CRACKED TO BE REPAIRED PER S/B 53 -188. FABRICATED -85 DOUBLER. FABRICATED -79 DOUBLER AND -7 SKIN. FORMED PARTS -11, -13, -15, -17, -19, -21, -23, -25 , -26, -27, -29, -31, -33, -149, -37, -39, -41, -43, -35, -103 IAW MD80 SRM 51-10-2. FORMED PARTS -3, -5, -6 INTERCOSTA L IAW MD80 SRM 51-10-2. FABRICATED -45 FITTING. INSTALLED ALL S/B NR 53-188 PARTS. (M) 2 L 7 2 4F A6WE 2002083000042 20020830 00042 2002 8 30 GTIA020777 4 20020704 A 2210 4034237915 DRIVE UNIT DOUG DC9 DC983 3022083 WP AILERON SERVO CHATTERING A GTIA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 23 827NK 153 49793 FLT 594 - MCO - WITH AUTO PILOT ENGAGED, THE YOLK CHATTERS IN RIGHT TURNS. REMOVED AND REPLACED AILERON SERVO DRIVE. P ERFORMED SYSTEM CHECK SYSTEM GROUND CHECKED GOOD. ALL IAW MD80 MM SECTIONS 22-11-01 AND 22-01-05. (M) 2 L 7 2 4F RT A6WE 2002083000043 20020830 00043 WP 2002 8 30 GTIA020778 1 20020703 A 2730 ELEVATOR DOUG DC9 DC982 3022082 WP HORIZONTAL STAB MALFUNCTIONED A GTIA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 23 823NK 48020 FLL - FLT 1754 - DISCONTINUED TAKEOFF AT 90 KNOTS. AIRCRAFT SEEMED TO BE TAIL HEAVY AND ABNORMAL FORWARD YOKE PRESSURE WAS REQUIRED TO MAINTAIN WEIGHT ON THE NOSE TIRE. INSPECTED HORIZONTAL STAB AND ELEVATORS FOR PROPER OPERATION. MD80 M M 27-31-0 AND 27-41-0. COMPLIED WITH HIGHT ENERGY STOP INSPECTION PER MD80 MM 05-57-00. AIRCRAFT FOUND TO BE MECHANICA LLY SOUND. (M) 2 L 7 2 4F A6WE 2002083000044 20020830 00044 2002 8 30 GTIA020779 4 20020706 A 2210 4034237915 SERVO DOUG DC9 DC983 3022083 WP AILERON DRIVE NOISY A GTIA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 GL 23 827NK 36 49793 ACY - RIGHT TURN WHEN AUTO PILOT ENGAGED AILERON SERVO MAKES GROUND NOISE FROM 0-25. REMOVED AND REPLACED AILERON SERVO DRIVE IAW MM 22-10-01. OPS CHECK NORMAL RTS CHECK PERFORMED IAW MM 22-01-05, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2002083000045 20020830 00045 WP 2002 8 30 GTIA020781 1 20020625 A 3397 WIRE DOUG DC9 DC981 3022081 WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 818NK 48018 FTW - PORTABLE EMERGENCY LIGHT (L-1) NEON BULB INOPERATIVE. SPLICED BROKEN WIRE. LIGHT OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002083000046 20020830 00046 WP 2002 8 30 GTIA020782 1 20020625 A 3350 CHARGER DOUG DC9 DC981 3022081 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND SEVERAL EMERGENCY LIGHTS IN TAIL SECTION INOPERATIVE. FOUND BAD BATTERY CHARGER SUPPLY, AFTER FURTHER TROUB LESHOOTING FOUND DEFECTIVE WIRING, REPAIRED WIRING, OPERATION CHECKS GOOD. (M) 2 L 7 2 4F A6WE 2002083000047 20020830 00047 WP 2002 8 30 GTIA020783 1 20020625 A 3397 WIRE DOUG DC9 DC981 3022081 WP EXIT SIGN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND EXITS SIGNS AT L1, R1 AND L2 DOORS INOPERATIVE. TROUBLESHOT EXITS SIGNS, FOUND WIRES BROKEN ON L1, R1, AND L2 EXIT SIGNS. REMOVED L1, R1, AND L2 EXIT SIGNS. INSTALLED EXIT SIGNS, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002083000048 20020830 00048 2002 8 30 GTIA020784 4 20020709 A 2210 7446120 RHEOSTAT DOUG DC9 DC983 3022083 WP COCKPIT FAILED A GTIA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 GL 23 827NK 49793 LAX - FLT 709 - FOUND AUTO PILOT NR 1 AND NR 2 DISCONNECTS DURING RIGHT TURNS. ALSO PULSES IN ROLL. OK STRAIGHT AND LE VEL AND LEFT TURNS. TROUBLESHOT AUTOPILOT SYSTEM. FOUND AILERON SERVO RHEOSTAT BAD. CHECKED WITH METER LEFT SIDE GOOD RIGHT SIDE BAD. REMOVED AND REPLACED RHEO STAT AND AILERON SERVO DRIVE PER MD-80 MM 22-11-01. SYSTEM OPS CHECKED GOOD PER MD80 MM 22-11-01 AND RTS PER 22-01-05. (M) 2 L 7 2 4F RT A6WE 2002083000049 20020830 00049 NM 2002 8 30 GTIA020785 1 20020710 A 5414 COWLING DOUG MD80 MD83 3023681 NM NR 2 ENGINE PEELING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 DTW - NR 2 ENGINE NOSE COWL, INLET LINER, METAL MESH PEELING AT 12 O'CLOCK POSITION. REPAIRED WIRE MESH ON NR 2 ENGINE, INLET COWL IAW MD80 SRM 54-04. (M) 2 L 7 2 4F RT 2002083000050 20020830 00050 2002 8 30 GTIA020786 4 20020710 A 2565 LANYARD DOUG DC9 DC982 3022082 WP ESCAPE SLIDE MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FLL - LS DOOR EVACUATION SLIDE LANYARD ASSEMBLY MISSING. INSTALLED LANYARD ASSY ON L2 EVACUATION SLIDE IAW MD80 MM 25-6 2-00. (M) 2 L 7 2 4F A6WE 2002083000051 20020830 00051 WP 2002 8 30 GTIA020788 1 20020711 A 3260 WARNING SYSTEM DOUG DC9 DC981 3022081 WP COCKPIT OUT OF ADJUST A GTIA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 811NK 48017 FLL - AT SPEEDS BELOW 210 KTS WITH THROTTLES PULLED BACK, NO GEAR WARNING HORN. TEST OK ON GROUND. FOR ALL TROUBLE SHO OTING AND TESTING OF THE LANDING GEAR AURAL WARNING, REF MD80 MM 32-60-00. INSPECTED 3 MAIN LANDING GEAR DOWN AND LOCKE D PROXIMITY SWITCHES AND DETERMINED OK. PERFORMED AN AST ON THE PROXIMITY S/W ELECTRONICS UNIT. OPS CHECK GOOD IAW MM 32-60-04. VERIFIED BOTH THROTTLE GEAR WARNING SWITCHES AND FLAP, 26 DEGREES S/W OPERATE NORMALLY. VERIFIED THE 'HORN C UT OUT SWITCH'. OPERATED NORMALLY AT BOTH, WITH FLAPS MORE THAN OR LESS THAN 26 DEGREES. INSTALLED PITOT EQUIP ON THE NR 1 SYSTEM AND DETERMINED THE LANDING GEAR AURAL WARNING IS OFF AT MORE THAN 210 KTS AND AURAL WARNING ON AT 210 KTS OR 2 L 7 2 4F A6WE 2002083000052 20020830 00052 WP 2002 8 30 GTIA020789 1 20020711 A 5270 WARNING SYSTEM DOUG DC9 DC983 3022083 WP PAX DOOR FALSE ACTIVATION A GTIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 23 827NK 49793 DTW - FLT 777 - FOUND DOOR LIGHT MASTER CAUTION ON TAKEOFF ROLL REJECTED TAKEOFF AT 70 KTS. SELF-TESTED PROXIMITY UNIT AS REQUIRED OPS CHECK GOOD. NO FAULTS DETECTED. INSPECTED DOORS EXTERIOR DOORS, FOR SECURITY, NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2002083000053 20020830 00053 SO 2002 8 30 SIMA200214402 1 20020524 A 2131 22250N030201 CONTROLLER EMB 145 EMB145LR 3260212 SO CABIN PRESSURE MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 616AE 145092 JAN - FLT 3479 - FLIGHT CREW REPORTED CABIN PRESSURE UNCONTROLABLE AT FL350. EMERGENCY WAS DECLARED AND AIRCRAFT WAS LA NDED SAFELY. MAINTENANCE REMOVED AND REPLACED DIGITAL CONTROLLER AND RESECURED THE RAM AIR DUCT IAW EMB MM. PERFORMED FCF WHICH WAS FOUND TO BE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002083000054 20020830 00054 SO 2002 8 30 SIMA200214901 1 20020524 A 5310 1452548003 SILL EMB 145 EMB145LR 3260212 SO CARGO DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 ABI - DURING AN IMBV INSPECTION MAINTENANCE, FOUND THE CARGO DOOR CUT OUT LOWER SILL CORRODED. REMOVED CORRODED SILL BE AM. INSTALLED NEW BEAM IAW EMB 145 SRM 145/1142, CHAPTER 51, REV 17 51-40-02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002083000055 20020830 00055 SO 2002 8 30 SIMA200214902 1 20020507 A 5310 14521725001 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36123, LEFT SILL IN GALLEY AREA HAS CORROSION. INSTALLED NEW SERVICEABLE SIL L IAW EMB145 SRM 51-20-03, 51-40-06, AND 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002083000056 20020830 00056 SO 2002 8 30 SIMA200214903 1 20020507 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36118, GALLEY CENTER BEAM GUSSET HAS CORROSION. INSTALLED NEW GALLEY CENTER BEAM GUSSET IAW EMB145 SRM 51-40-02, 51-20-03, 51-40-06. (M) 2 L 7 2 4T RT T00011AT 2002083000057 20020830 00057 SO 2002 8 30 SIMA200214904 1 20020507 A 5320 14522459003 SUPPORT EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36119, GALLEY RAMP SUPPORT HAS CORROSION. INSTALLED NEW RAMP SUPPORT IAW EMB 145 SRM 51-20-02, 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002083000058 20020830 00058 SO 2002 8 30 SIMA200214905 1 20020507 A 5310 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36120, GALLEY FORWARD RIGHT SILL HAS CORROSION. INSTALLED NEW SERVICEABLE SI LL IAW EMB145 SRM 51-40-02, 51-20-03. (M) 2 L 7 2 4T RT T00011AT 2002083000059 20020830 00059 SO 2002 8 30 SIMA200214906 1 20020507 A 5310 14521725615 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36122, GALLEY RIGHT FAT SILL HAS CORROSION. INSTALLED NEW SERVICEABLE SILL I AW EMB145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002083000060 20020830 00060 SO 2002 8 30 SIMA200214907 1 20020508 A 5310 14529603003 CROSSBEAM EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36125, GALLEY CROSSBEAM AND PROFILE CORRODED. INSTALLED NEW CROSSBEAM AND PR OFILE IAW EMB145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002083000061 20020830 00061 SO 2002 8 30 SIMA200214908 1 20020508 A 5310 14522461003 GUSSET EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36126, GALLEY FORWARD DIAMOND GUSSET HAD CORROSION. INSTALLED NEW FORWARD DI AMOND GUSSET IAW EMB145 SRM 51-20-03, 51-40-02 AND 51-40-06. (M) 2 L 7 2 4T RT T00011AT 2002083000062 20020830 00062 SO 2002 8 30 SIMA200214909 1 20020508 A 5310 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36127, GALLEY AFT DIAMOND GUSSET HAS CORROSION. INSTALLED NEW GUSSET IAW EMB 145 SRM 51-20-03 AND 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002083000063 20020830 00063 SO 2002 8 30 SIMA200214910 1 20020508 A 5310 14522461003 BEAM EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - THIS IS FROM A LEVEL 2 FINDING ON CRIC NR 36128, LEFT OMEGA BEAM HAS CORROSION FROM FRAME 23 TO 26. INSPECTED AND ACCEPTED AS IS IAW EMB GST-1552/02. RESTORED PROTECTIVE COAT IAW CPM 51-21-06. (M) 2 L 7 2 4T RT T00011AT 2002083000064 20020830 00064 SO 2002 8 30 SIMA200214911 1 20020508 A 5310 14529603003 BEAM EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36129, RIGHT CENTER OMEGA BEAM HAS CORROSION FROM FRAME 23 TO 26. BLENDED CO RROSION AND ACCEPTED AS IS IAW EMB GST-1552/02. (M) 2 L 7 2 4T RT T00011AT 2002083000065 20020830 00065 SO 2002 8 30 SIMA200214912 1 20020510 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO LAVATORY CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - THIS IS A LEVEL 2 FINDING IN CRIC NR 36131, RIGHT BEAM GUSSET UNDER LAVATORY CORRODED. BLENDED CORROSION AND ACCE PTED AS IS IAW EMB GST-1552/02. (M) 2 L 7 2 4T RT T00011AT 2002083000066 20020830 00066 SO 2002 8 30 SIMA200214913 1 20020510 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO LAVATORY CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 616AE 145092 ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36132, CENTER BEAM GUSSET UNDER LAVATORY CORRODED. BLENDED CORROSION, ACCEPT ED AS IS IAW EMB GST-1552/02. RESTORED PROTECTIVE FINISH IAW EMB145 CPM 51-21-04, 51-21-05, AND 51-21-06. (M) 2 L 7 2 4T RT T00011AT 2002083000067 20020830 00067 EU 2002 8 30 SIMA200218901 1 20020708 A 6120 COMPUTER AEROSP ATR72 ATR72212A 8680902 EU RT PROPELLER MALFUNCTIONED A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 536AT 536 MCO - FLT 5016 - DURING CLIMB-OUT, WHEN CREW SELECTED CLIMB ON POWER MANAGEMENT RIGHT PROPELLER STAYED AT 100 PERCENT. CREW RETURNED TO MCO AND DECLARED EMERGENCY UPON LANDING. AIRCRAFT WAS LANDED SAFELY WITH NO FURTHER INCIDENTS. MAINTE NANCE FOUND THE EEC/PEC SWITCH SELECTED TO THE EEC SIDE. REPOSITIONED SWITCH TO GUARDED SIDE WHICH IS THE NORMAL CONDITI ON. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RELEASED FOR AN FUNCTIONAL CHECK FLIGHT. FUNCTIONAL CHECK FLIGHT WAS S ATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002083000068 20020830 00068 SO 2002 8 30 SIMA200219701 1 20020716 A 3350 20131A SIGN EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 716AE 145264 BOS - FLT 4642 - CREW REPORTED THE EMERGENCY EXIT SIGNS BY THE PASSENGER DOOR TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THR NR 2 BATTERY PACK IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2002083000069 20020830 00069 EU 2002 8 30 SIMA200220301 1 20020718 A 3397 3011210 CONTACTOR AEROSP ATR42 ATR42300 8680920 EU CABIN DIRTY A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 135MQ 135 MIA - MAINTENANCE REPORTED THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE FOUND THE ELECTRICAL CONTA CTS IN THE LIGHT ASSEMBLY TO BE DIRTY. CONTACTS WERE CLEANED ANDBULB WAS REPLACED. OPERATIONAL CHECK WAS GOOD AND AIRC RAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002083000070 20020830 00070 EU 2002 8 30 SIMA200220302 1 20020722 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 269AT 269 MIA - MAINTENANCE REPORTED LOW VOLTAGE ON EMERGENCY LIGHT BATTERIES. MAINTENANCE REMOVED AND REPLACED THREE EMERGENCY L IGHT POWER SUPPLY UNIT BATTERY PACKS (S/N 19877, 26676, 6488) IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS R ETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002083000071 20020830 00071 NE 2002 8 30 SIMA200220401 2 20020723 A 7314 B-NUT AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE FUEL PUMP LOOSE A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 135MQ 135 MIA - FLT 9305 - DURING CLIMB-OUT, CREW NOTED NR 2 FUEL PUMP RUN LIGHT ON AND NR 2 LOW PRESSURE LIGHT ON. CREW RETURNED TO MIA ON REQUEST FROM MOC DU TO HISTORY OF FUEL PROBLEM. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. MAINTENAN CE FOUND B-NUT ON FUEL JET PUMP VERY LOOSE. B-NUT WAS TIGHTENED. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2002083000072 20020830 00072 NM 2002 8 30 USAA020206 1 20020417 A 5550 65537447 ANGLE BOEING 737 7373B7 1384580 NM EMPENNAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND DRAG ANGLE CRACKED .25 INCH, SECT 48 DRAG ANGLE LIGHT SIDE 10 INCH BEHIND ATTACH LUG. REPAIRED FILLER AND S TRAPS ON OUTSIDE AND INSIDE OF DRAG ANGLE PER TYPICAL REPAIR 53-80-03. (M) 2 L 7 2 4F RT A16WE 2002083000073 20020830 00073 NM 2002 8 30 USAA020207 1 20020604 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND SKIN CRACKED 7.875 INCH BY 6.75 INCH, BETWEEN STRINGER 16/17, OUTER SKIN STATION 178. DOUBLER INSTALLED PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2002083000074 20020830 00074 NM 2002 8 30 USAA020208 1 20020604 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND SKIN CRACKED 1.125 INCH BY 6.625 INCH CRACK, BETWEEN STRINGER 16 AND 17 OUTERSKIN STATION 178. DOUBLER INST ALLED PER EO 5300V157. (M) 2 L 7 2 4F RT A16WE 2002083000075 20020830 00075 NM 2002 8 30 USAA020209 1 20020605 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND CHORDS AND WEBS CORRODED 5 INCH BY 6 INCH AREA, FORWARD SIDE AFT PRESSURE BULKHEAD BS 1018 BL 00 4 INCH BY 5 INCH. CORROSION LEVEL 2. BULKHEAD WEB AND CHORDS INSTALLED DOUBLERS PER EA 74025. (M) 2 L 7 2 4F RT A16WE 2002083000076 20020830 00076 NM 2002 8 30 USAA020210 1 20020605 A 5320 STIFFENER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND STIFFENER CORRODED 3 INCH BY 3 INCH AREA, AFT PRESS BULKHEAD STIFFENER BS 1018 BL 00. INSTALLED DOUBLER, SP LICED SECTION OF STIFFENER PER BOEING DRAWING 65C28106. (M) 2 L 7 2 4F RT A16WE 2002083000077 20020830 00077 NM 2002 8 30 USAA020211 1 20020601 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 48991 22950 TPA - FOUND FRAME CORRODED 3 INCH BY 1.5 INCH AREA, STATION 251.6 RIGHT SIDE NOSE W/W AREA. CORROSION LEVEL 2, TASK NR C53-100-01. FABRICATED NEW PARTS PER SRM, REPLACED OLD CHORD ANGLE PER SRM 53-00-7 FIG 204. (M) 2 L 7 2 4F RT A16WE 2002083000078 20020830 00078 NM 2002 8 30 USAA020212 1 20020531 A 5753 65908541 FITTING BOEING 737 737401 1384701 NM FLAP TRACK CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 CLT - SHOP VISIT FOUND TRACK FITTING CRACKED 2 INCHES, RIGHT INBOARD FORE FLAP BETWEN MOUNT HOLES. DEFECTIVE PART REPLA CED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2002083000079 20020830 00079 NM 2002 8 30 USAA020213 1 20020531 A 5753 65908541 FITTING BOEING 737 737401 1384701 NM FLAP TRACK CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 CLT - SHOP VISIT, FOUND TRACK FITTING CRACKED 2 INCHES, LEFT INBOARD FORE FLAP BETWEEN MOUNT HOLES. DEFECTIVE PART REPL ACED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2002083000080 20020830 00080 NM 2002 8 30 USAA020214 1 20020602 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 23317 CLT - FOUND SKIN CRACKED STATION 727 AND 727A STRINGER 23L. REPAIRED, INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2002083000081 20020830 00081 NM 2002 8 30 USAA020215 1 20020604 A 5754 SKIN BOEING 737 7374B7 1384702 NM NR 2 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 785AU 31532 25024 PIT - FOUND SKIN CRACKED 4 INCH BY 8 INCH, UNDERSIDE OF NR 2 SLAT 24 INCHES FROM OUTBOARD END. INSTALLED 4 INCH BY 8 IN CH DOUBLER PER SRM 57-43-01 FIG 206. (M) 2 L 7 2 4F RT A16WE 2002083000082 20020830 00082 NM 2002 8 30 USAA020216 1 20020521 A 5310 DOUBLER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 23316 PIT - FOUND ANTENNA DOUBLER CORRODED SIX .25 INCH BY .25 INCH AREAS, ANTENNA MOUNT NUTPLATE BRACKETS BETWEEN STATION 727 D. REMOVED CORROSION AND REPLACED CHANNEL PER SRM 53-30-53, 51-40-05. CORROSION LEVEL 1, TASK NR C53-208-01. (M) 2 L 7 2 4F RT A16WE 2002083000083 20020830 00083 NM 2002 8 30 USAA020217 1 20020506 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 783AU 31714 25022 PIT - FOUND FRAME CRACKED .25 INCH, AT STATION 400 B/W S8L AND S9L. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002083000084 20020830 00084 NM 2002 8 30 USAA020218 1 20020508 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 783AU 25022 PIT - FOUND SKIN CHAFED 1 INCH AREA, LEFT AIR CONDITION BAY STRUCTURE AT DOOR LATCH STATION BS 5. FABRICATED STRAP, TRE ATED, INSTALLED PER SRM 51-70-12 WITH EA 73950. (M) 2 L 7 2 4F RT A16WE 2002083000085 20020830 00085 NM 2002 8 30 C8GA20020011 1 20020829 A 2611 100064901 SMOKE DETECTOR BOEING 727 727223 1384074 NM CARGO BAY DEFECTIVE A C8GA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 15 715AA 22470 FLT 713 FROM DEN TO TOL. DURING CRUISE LEVEL, THE LOWER AFT CARGO FIRE WARNING LIGHT CAME ON INFLIGHT. APPROPRIATE CHECK LIST WERE ACCOMPLISHED, NOTIFIED ATC, DECLARED EMERGENCY AND AIR TURNBACK TO DEN AND LANDED WITHOUT INCIDENT. UPON LAND ING INSPECTED THE LOWER AFT CARGO COMPARTMENT AND FOUND NO INDICATION OF FIRE. MEL THE LOWER AFT CARGO COMPARTMENT AREA DETECTION SYSTEM PER 26-19-1A. AIRCRAFT RETURNED TO SERVICE. MEL 26-19-1 WAS CLEARED UPON ARRIVAL IN TOL 8/29/2002 BY RE PLACING A SMOKE DETECTOR AND TWO SMOKE DETECTOR BATTERIES. 2 L 7 3 4F A3WE 2002083000086 20020830 00086 NM 2002 8 30 C1HA200286005 1 20020829 A 3350 POWER SUPPLY BOEING 727 7272S7 138407Z NM CABIN INOPERATIVE A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 686CA 22021 LT OVERWING FLOOR TRACK LIGHT POWER SUPPLY INOP. REMOVED AND REPLACED FLOOR TRACK LIGHT POWER SUPPLY. 2 L 7 3 4F A3WE 2002083000087 20020830 00087 NM 2002 8 30 UPS02239187 1 20020813 A 5320 STIFFENER BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C SUSPECT CRACK ON AFT PRESSURE BULKHEAD VERTICAL BEAM LT AT W/L 264 APPROX LBL 26.83. HFEC INSPECTION CONFIRMED CRACK. CRACK STOP DRILLED IAW EO B727-5311-0631 STEP 3. HEFC INSPECTION CONFIRMED CRACK CONTAINED. AREA REP AIRED IAW B727-5311-0631. 2 L 7 3 4F A3WE 2002083000088 20020830 00088 NM 2002 8 30 USAA020219 1 20020508 A 5245 SKIN BOEING 737 7374B7 1384702 NM A/C BAY DOOR CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 783AU 25022 PIT - FOUND SKIN CHAFED 1 INCH AREA, LT AIR CONDITIONING BAY STRUCTURE AT DOOR LATCH STATION 590. FABRICATED ANGLE, TRE ATED, INSTALLED PER SRM 51-70-12 WITH EA 73950. (M) 2 L 7 2 4F RT A16WE 2002083000089 20020830 00089 NM 2002 8 30 USAA020220 1 20020523 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 23876 PIT - FOUND SKIN CRACKED .25 INCH, FUSELAGE FRAME AT STATION 867 B/W STRINGER 8R AND 9R. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002083000090 20020830 00090 NM 2002 8 30 USAA020221 1 20020603 A 5347 SEAT TRACK BOEING 737 737401 1384701 NM CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 23876 PIT - FOUND TRACK CORRODED 2 INCHES BY .5 INCH, RIGHT INBOARD FLOOR TRACK AND FLANGE AT STATION 360. REPLACED FLOOR TRA CK (APPROX 20 INCHES) PER SRM 53-00-52, REPAIR NR 1, FIG 202. CORROSION LEVEL 1, TASK NR C53500-C. (M) 2 L 7 2 4F RT A16WE 2002083000091 20020830 00091 NM 2002 8 30 USAA020222 1 20020603 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND FRAME CRACKED .75 INCH, STATION 747 FRAME BETWEEN STRINGER 8 & 9 LEFT. DOUBLER INSTALLED PER TYPICAL REP 53 -10-14A. (M) 2 L 7 2 4F RT A16WE 2002083000092 20020830 00092 NM 2002 8 30 USAA020223 1 20020603 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND FRAME CRACKED .75 INCH DIAMETER, STATION 867 FRAME BETWEEN STRINGER 8 & 9 LEFT. DOUBLER INSTALLED PER TYPIC AL REPAIR 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002083000093 20020830 00093 NM 2002 8 30 USAA020224 1 20020531 A 5320 1123579 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND SUPPORT CORRODED ENTIRE SURFACE, DIAGONAL FLOOR SUPPORT RBBL 12, STATION 987-1016. FOUND DEFECTIVE PART REP LACED WITH IDENT PART NR. CORRODED LEVEL 1, TASK NR C53-107-02. (M) 2 L 7 2 4F RT A16WE 2002083000094 20020830 00094 NM 2002 8 30 SWAA021958 1 20020826 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 765SW 29805 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2002083000095 20020830 00095 2002 8 30 SWAA021959 4 20020826 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT CABIN DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 764SW 27878 DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED GIRT ASSY 'S PER MM. 2 L 7 2 4F RT A16WE 2002083000096 20020830 00096 NM 2002 8 30 SWAA021963 1 20020826 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB HARDWARE AND BUSHINGS ON ALL 4 HINGE ATTACH POINTS PER MM. 2 L 7 2 4F RT A16WE 2002083000097 20020830 00097 NM 2002 8 30 SWAA021964 1 20020826 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 774SW 27882 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB HARDWARE AND BUSHINGS AT NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM. 2 L 7 2 4F RT A16WE 2002083000098 20020830 00098 NM 2002 8 30 SWAA021965 1 20020827 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000099 20020830 00099 NM 2002 8 30 SWAA021966 1 20020826 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000100 20020830 00100 NM 2002 8 30 SWAA021967 1 20020825 A 5312 6547978 WEB BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 616 AND BS 639, STR 17L. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2002083000101 20020830 00101 NM 2002 8 30 SWAA021969 1 20020825 A 5753 6546435278 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED C3 CHECK, FOUND RT T/E OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT T/E OTBD AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2002083000102 20020830 00102 NM 2002 8 30 SWAA021970 1 20020826 A 5330 6545768 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 DURING SCHEDULED SERVICE CHECK, FOUND SKIN AND TEAR STRAP CRACKED AT AIR STAIR AFT LOWER CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F A16WE 2002083000103 20020830 00103 NM 2002 8 30 SWAA021971 1 20020827 A 5755 6546452 SPOILER BOEING 737 7375H4 138449D NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING WALK AROUND INSPECTION, FOUND NR 5 L/E GROUND SPOILER CRACKED. REMOVED AND REPLACED NR 5 L/E GROUND SPOILER PER MM. 2 L 7 2 4F RT A16WE 2002083000104 20020830 00104 NM 2002 8 30 SWAA021972 1 20020827 A 5330 6545785 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED 1/2D CHECK, FOUND WINDOW CUTOUTS CRACKED AT BS RT 777 LT, BS 837 LT, BS 500A + 10 RT AND BS 857 RT. RE PAIRED FRAMES PER SWA EA. 2 L 7 2 4F RT A16WE 2002083000105 20020830 00105 2002 8 30 SWAA021940 4 20020825 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM ENTRY DOORS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED C4 CHECK, FOUND BOTH CABIN ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS LOOSE. SECURED FITTINGS P ER MM. 2 L 7 2 4F RT A16WE 2002083000106 20020830 00106 NM 2002 8 30 SWAA021941 1 20020825 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2002083000107 20020830 00107 NM 2002 8 30 SWAA021942 1 20020826 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 751SW 29803 EEPLS COVER MISSING IN CABIN. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002083000108 20020830 00108 NM 2002 8 30 SWAA021944 1 20020826 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, ABOVE STR 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000109 20020830 00109 NM 2002 8 30 SWAA021945 1 20020826 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT GROUND AIR CONDITIONING DOOR CUTOUT AT FWD CORNER. REPAIRED S KIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000110 20020830 00110 NM 2002 8 30 SWAA021946 1 20020826 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000111 20020830 00111 NM 2002 8 30 SWAA021947 1 20020823 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000112 20020830 00112 NM 2002 8 30 SWAA021949 1 20020826 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000113 20020830 00113 NM 2002 8 30 SWAA021950 1 20020826 A 5754 65C26603 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED C4 CHECK, FOUND NR 3 L/E SLAT CRACKED IN AFT ROW OF RIVETS. REMOVED AND REPLACED NR 3 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2002083000114 20020830 00114 NM 2002 8 30 SWAA021953 1 20020826 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM MID CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2002083000115 20020830 00115 NM 2002 8 30 SWAA021954 1 20020826 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM MID CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2002083000116 20020830 00116 NM 2002 8 30 SWAA021955 1 20020826 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 40 TO RBL 40. REMOVED AND REPLACED FLOORBEAM SEC TION PER SRM. 2 L 7 2 4F RT A16WE 2002083000117 20020830 00117 NM 2002 8 30 SWAA021956 1 20020825 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT RT FWD EDGE OF GROUND AIR CONDITIONING CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000118 20020830 00118 NM 2002 8 30 SWAA021957 1 20020823 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C1 CHECK, FOUND SKIN CRACKED AT BOTH UPPER AND LOWER HINGE ATTACH POINTS ON FWD ENTRY DOOR. REPAIRED S KIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000119 20020830 00119 2002 8 30 SWAA021927 4 20020824 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002083000120 20020830 00120 NM 2002 8 30 SWAA021930 1 20020823 A 5330 6545776 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000121 20020830 00121 NM 2002 8 30 SWAA021932 1 20020822 A 3350 07912 COVER BOEING 737 7372T4 1384492 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER MISSING BETWEEN ROW 15 AND ROW 16. INSTALLED COVER PER MM. 2 L 7 2 4F A16WE 2002083000122 20020830 00122 NM 2002 8 30 SWAA021933 1 20020824 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000123 20020830 00123 NM 2002 8 30 SWAA021935 1 20020821 A 3350 604222 BATTERY BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INTERMITENT. REMOVED AND REPLACED B ATTERIES PER MM. 2 L 7 2 4F RT A16WE 2002083000124 20020830 00124 NM 2002 8 30 SWAA021936 1 20020825 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 827, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000125 20020830 00125 NM 2002 8 30 SWAA021937 1 20020823 A 5315 BAC1509 FLOORBEAM BOEING 737 7373Q8 1384670 NM AFT CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 727D + 6, LBL 8. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002083000126 20020830 00126 NM 2002 8 30 SWAA021918 1 20020822 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 17R AT FWD SVC DOOR AFT LOWER CORNER CUTOUT. RE PAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000127 20020830 00127 NM 2002 8 30 SWAA021921 1 20020822 A 5520 65C26384 TAB BOEING 737 7373Q8 1384670 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK, (NR 1 HINGE WORN ). REMOVED AN D REPLACED RT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002083000128 20020830 00128 NM 2002 8 30 SWAA021922 1 20020816 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000129 20020830 00129 NM 2002 8 30 SWAA021923 1 20020819 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED C4 CHECK, FOUND 1016 BULKHEAD CRACKED (3 EA) BETWEEN STR 6L AND STR 7L. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F A16WE 2002083000130 20020830 00130 NM 2002 8 30 SWAA021925 1 20020821 A 3230 654611321 TRUNNION PIN BOEING 737 7373H4 1384600 NM RT MLG SHEARED A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 29 639SW 27712 DURING DEPARTURE RT MLG WOULD NOT RETRACT. FOUND LANDING GEAR ACTUATOR TRUNNION PIN SHEARED. REMOVED AND REPLACED RT M LG TRUNNION PIN PER MM. 2 L 7 2 4F RT A16WE 2002083000131 20020830 00131 2002 8 30 SWAA021973 4 20020827 A 2565 6949956 CABLE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002083000132 20020830 00132 2002 8 30 SWAA021977 4 20020828 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD CABIN DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 752SW 29804 DURING SCHEDULED C2 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PE R MM. 2 L 7 2 4F RT A16WE 2002083000133 20020830 00133 2002 8 30 SWAA021978 4 20020827 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002083000134 20020830 00134 NM 2002 8 30 SWAA021979 1 20020828 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 4, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000135 20020830 00135 2002 8 30 SWAA021980 4 20020828 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002083000136 20020830 00136 NM 2002 8 30 SWAA021981 1 20020828 A 5330 589357 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ON CAPT'S NR 1 WINDOW UPPER OTBD POST. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002083000137 20020830 00137 NM 2002 8 30 SWAA021982 1 20020826 A 5740 65C3291818 FITTING BOEING 737 7373H4 1384600 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED SERVICE CHECK, FOUND RT MLG BEAM STABILIZER BAR FWD ATTACH FITTING ON REAR SPAR AT WBL 113.895 CORRODED IN BUSHING BORE. REPAIRED LUG BORE PER SWA EA. 2 L 7 2 4F RT A16WE 2002083000138 20020830 00138 NM 2002 8 30 VNAA0208034 1 20020823 A 3300 501122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 471PS 15829 140 3007 THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWE R SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002083000139 20020830 00139 NM 2002 8 30 VNAA0208039 1 20020825 A 3397 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 424JS 3033 THE CREW REPORTED THAT THE 9A EMERGENCY FLOOR LIGHT STRIP WAS LOOSE AND INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED A WIRE ON THE LIGHT STRIP AND RESECURED THE LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OP ERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002083000140 20020830 00140 NM 2002 8 30 USAABB020108 1 20020705 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 1, 4 AND 6 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002083000141 20020830 00141 NM 2002 8 30 USAABB02105 1 20020602 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM R3 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 SFO - FOUND R3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002083000142 20020830 00142 NM 2002 8 30 USAABB02106 1 20020602 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 SFO - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 6 AND 13 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002083000143 20020830 00143 NM 2002 8 30 USAABB02109 1 20020704 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 1 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002083000144 20020830 00144 NM 2002 8 30 USAABB02110 1 20020703 A 3200 849701 PSEU BOEING 767 767201 1385125 NM MLG FAILED A USAA L ABORTED APPROACH G J MULTIPLE FAILURE WARNING INDICATION AP APPROACH 1 EA 19 649US 6924 23901 CLT - FLT 1659 - ON APPROACH TO CLT, THE CREW RECEIVED THE CONFIGURATION WARNING, ALONG WITH THE EICAS MESSAGES 'FLAPS' AND 'GEAR NOT DOWN'. CREW HAD THREE GREEN GEAR INDICATIONS. CREW PERFORMED A MISSED APPROACH AND THEN LANDED. CREW RE PORTED NOT HAVING THRUST REVERSERS, SPEED BRAKES OR AUTO BRAKES. MAINTENANCE REPLACED THE PSEU. (M) 2 L 7 2 4F RT A1NM 2002083000145 20020830 00145 NM 2002 8 30 USAABB02111 1 20020705 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 9, 13, 18, 23, 26, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BAT TERIES. (M) 2 L 7 2 4F RT A2NM 2002083000146 20020830 00146 NM 2002 8 30 UPS02239199 1 20020814 A 5711 SPAR BOEING 727 72731C 1384011 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C SUSPECT CRACK ON RT WING REAR SPAR UPPER CHORD AT APPROX WS 198 AND WS 194. UPPER CHORD HORIZONTAL FL ANGE BLENDED TO REMOVE DAMAGE AT WS 196, WS 201 AND WS 205 IAW SRM 51-10-6. ADDITIONAL CORROSION FOUND AT 3 FASTENER LO CATION BETWEEN WS 173 AND WS 175. REPAIR CARRIED OUT IAW SMRO 2002-044-004. 2 L 7 3 4F A3WE 2002083000147 20020830 00147 NM 2002 8 30 USAABB02115 1 20020714 A 3150 WARNING SYSTEM BOEING 767 7672B7 1385107 NM COCKPIT FALSE ACTIVATION A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 653US 24894 PHL - FLT 48 - EN ROUTE PIT-CDG - CREW RECEIVED AURAL WARNINGS AND MASTER CAUTION LIGHTS. THE LEFT EICAS COMPUTER SHOWE D INDICATIONS RELATED TO THE AURAL WARNING AND MASTER CAUTION,WHILE THE RIGHTE EICAS COMPUTER SHOWED ADDITIONAL ENGINE W ARNINGS. FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH EICAS COMPUTERS. ON TH E SUBSEQUENT FLIGHT TO CLT (9280/15/JUL), THE CREW RECEIVED THE AMER ALT ALERT WITH NO APPARENT ALTITUDE CONDITION. MAI NTENANCE RESET THE WARN ELEX CIRCUIT BREAKER AND TESTED THE SYSTEM. ON FLIGHT 192, CLT-FRA, THE FLIGHT RETURNED TO CLT DUE TO THE ALT ALERT, MASTER CAUTION AND EICAS WARNINGS. MAINTENANCE REPLACED THE ALTITUDE ALERT MODULE (M617). (M) 2 L 7 2 4F RT A1NM 2002083000148 20020830 00148 NM 2002 8 30 UPS02439099 1 20020805 A 5414 A1S13010020IN SKIN BOEING 747 747212B 1384886 NM NR 1 PYLON DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C NR 1 PYLON RT LOWER EDGE AREA FROM NAC STA 180- REAR DRAG FIXED FAIRING INTERIOR METAL SKIN DEFORMED A S MARK. NR 1 PYLON RT LOWER EDGE AREA FROM NAC STA 180- REAR DRAG FIXED FAIRING INTERIOR METAL SKIN REPLACED AS PER SRM 54-34-03 FIG 25. 2 L 7 4 4F A20WE 2002083000149 20020830 00149 NM 2002 8 30 UPS02439100 1 20020804 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C RIGHT BS 1480 BULKHEAD NR 6 HOLE CORROSION FOUND AT SKIN AROUND BORE STR 33R TO 34R. HOLE REAMED AND BUSHING INSTALLED AS PER SB 747-53A2390. REWORKED HOLE INSPECTED - SATISFACTORY AS PER NTM PART 6 51-00-00 FIG 1. 2 L 7 4 4F A20WE 2002083000150 20020830 00150 NM 2002 8 30 UPS02439107 1 20020806 A 5320 2024T300501N SHIM BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C FX-KEEL BEAM BOX EXTERIOR LOWER CHORD TO PANEL SUPPORT ATT SHIM FOUND CORROSION AT RT SIDE STA 1328 RB L 6 TO RBL 9. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 53-10-01 FIG 1 LIMITS, REPLACED IAW SRM FIG 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002083000151 20020830 00151 NM 2002 8 30 UPS02439108 1 20020805 A 5320 654U6625886 SUPPORT BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C FX- KEEL BEAM PNL SUPPORT LOWER CHORD FOUND SURFACE CORROSION AT STA 1480 LBL 16 TO RBL 16. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT EXCEEDS SRM 53-10-01 LIMITS, REPLACED IAW SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002083000152 20020830 00152 NM 2002 8 30 UPS02439109 1 20020806 A 5330 PANEL BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C FX- KEEL BEAM FIXED PANEL UPPER SURFACE FOUND SURFACE CORROSION AT LT SIDE STA 1438 TO STA 1460 LBL 9 TO LBL 16. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 53-10-01 LIMITS, REPLACED IAW SRM FIG 5 1-10-01. 2 L 7 4 4F A20WE 2002083000153 20020830 00153 NM 2002 8 30 UPS02439110 1 20020806 A 5320 SHIM BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C FX-KEEL BEAM BOX EXTERIOR LOWER CHORD TO PANEL SUPPORT ATT SHIM FOUND CORROSION AT LT SIDE STA 1308 LB L 6 TO LBL 9. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 53-10-01 FIG 1 LIMITS, REPLACED IAW SRM FIG 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002083000154 20020830 00154 NM 2002 8 30 UPS02439111 1 20020806 A 5320 WEB BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C FX- AIR CONDITIONING BAY REAR FIXED FAIRING LT SIDE. GROUND PNEUMATIC AIR CONNECTOR SERVICE BOX INTER IOR REAR WEB FOUND SURFACE CORROSION AT STA 1255 LBL 34 TO LBL 36. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 53-10-01 LIMITS, REPAIR WEB IAW SRM FIG 51-40-02. 2 L 7 4 4F A20WE 2002083000155 20020830 00155 NM 2002 8 30 UPS02439112 1 20020802 A 5350 WEB BOEING 747 747212B 1384886 NM FAIRING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C FX- AIR CONDITIONING BAY REAR FIXED FAIRING INTERIOR REAR SURFACE FOUND SURFACE CORROSION AT STA 1255 RBL 9 TO RBL 30. REAR FIXED FAIRING REAR WEB AND SUPPORT CHORD REPAIRED AS PER SRM 51-40-02 FIG 1, 51-40-03 FIG 2 AND F IXED PNL REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002083000156 20020830 00156 NM 2002 8 30 UPS02439113 1 20020806 A 5330 65B117916 PANEL BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C FX- KEEL BEAM FIXED PANEL UPPER SURFACE FOUND SURFACE CORROSION AT STA 1255 TO STA 1275 RBL 9 TO RBL 1 6. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 53-10-01 LIMITS, REPLACED IAW SRM FIG 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002083000157 20020830 00157 EA 2002 8 30 SWIA200211132 1 20020815 A 2711 601R5122623 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 438SW 7574 AILERON TRIM WILL NOT MOVE TO THE LEFT. REPLACED AILERON TRIM PANEL WITH SERVICEABLE UNIT IAW CRJ MM 27-21-00. OPS CHE CKS GOOD. 2 L 7 2 4F RT A21EA 2002083000158 20020830 00158 EA 2002 8 30 SWIA200211133 1 20020817 A 2741 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 443SW 839 839 7638 SHORTLY AFTER ROTATION, STAB TRIM NR 2 AND MACH TRIM WENT INOP AND WOULD NOT RESET. PERFORMED QRH AND RETURNED TO DFW. REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR AND MOTOR CONTROL UNIT IAW 27-42-01 AND 27-42-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002083000159 20020830 00159 EA 2002 8 30 SWIA200211134 1 20020819 A 3297 WIRE CNDAIR CL600 CL6002B19 1900309 EA ANTI SKID SYS BROKEN A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 432SW 7548 ON TAKEOFF ROLL, RECEIVED AN ANTI-SKID INBOARD CAUTION MESSAGE. ABORTED THE TAKEOFF. FOUND BROKEN WIRES ON THE TRANSDU CER CANNON PLUG RIGHT INBOARD PLUG. REMOVED AND REPLACED WITH A NEW HARNESS IAW 32-44-01. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002083000160 20020830 00160 EA 2002 8 30 SWIA200211135 1 20020818 A 2760 4916405 ECU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 903SW 3072 2135 7425 SPOILER FAULT STATUS MESSAGE AND INBOARD GROUND SPOILER FAULT STATUS MESSAGE ON TAXI OUT. RESET CIRCUIT BREAKERS 1N8, 2 N8, 4A3 AND 4A2. DID NOT RESET. RETURNED TO THE GATE. REPLACED SECU IAW 27-61-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002083000161 20020830 00161 EA 2002 8 30 SWIA200211136 1 20020817 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 416SW 5056 3492 7089 AFTER TAKEOFF AND UPON RETRACTING LANDING GEAR, RECEIVED A NOSE GEAR UP DISAGREE WARNING. EXTENDED THE LANDING GEAR AND THE WARNING DID NOT PERSIST. ATTEMPTED TO RETRACT GEAR AGAIN. WARNING RETURNED. RETURNED TO BIL. REMOVED AND REPLAC ED THE NOSE LANDING GEAR SOLENOID VALVE IAW CRJ MM 32-33-10. PERFORMED SEVERAL GEAR SWINGS. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002083000162 20020830 00162 NM 2002 8 30 UPS02239091 1 20020815 A 2612 FIRE WARNING BOEING 727 72725C 138400H NM COCKPIT FALSE INDICATION A IPXA K NONE N FALSE WARNING CL CLIMB 1 SO 01 951UP 19850 INSPECTION TYPE:N/A CLIMBING THROUGH 20K GOT WHEEL WELL FIRE LIGHT. LOWERED GEAR AND LIGHT IMMEDIATELY WENT OUT. INSP NOSE AND MAIN GEAR LOOPS, NO DEFECTS FOUND. SYS CHECKS NORMAL. FIRE DET CONTROL PANEL REPLACED REF LP 653351 ITEM 2 M2 43137. 2 L 7 3 4F A3WE 2002083000163 20020830 00163 NM 2002 8 30 UPS02239105 1 20020818 A 3350 BATTERY PACK BOEING 727 72751C 1384015 NM COCKPIT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:N/A BOTH EMERGENCY LIGHT BATTERY PACKS LOW. REMOVED AND REPLACED BATTERY, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2002083000164 20020830 00164 NM 2002 8 30 UPS02239114 1 20020808 A 5320 STIFFENER BOEING 727 72731C 1384011 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C, RT WHEEL WELL BS 870 BULKHEAD VERT STIFFENER CORRODED AT UPPER END AT RBL 50 APPROX JUST FWD OF L/E C ONTROL VALVE. NEW VERT STIFFENER FABRICATED IAW DRAWING 65-16330, VERT STIFFENER INSTALLED IAW DRAWING 65-16330 & SMRO EO 2002-044-005 UPS ENGINEERING FILE B727-53-20071. 2 L 7 3 4F A3WE 2002083000165 20020830 00165 NM 2002 8 30 UPS02239115 1 20020813 A 5350 STIFFENER BOEING 727 72731C 1384011 NM FAIRING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C WING TO BODY FAIRING 3409 HAS A CRACKED FWD FRAME STIFFENER ANGLE. FABRICATED AND INSTALLED NEW STIFF ENER IAW SRM 53-50-1 FIG 4 AND SRM 51-2 0-1 FIG 7. 2 L 7 3 4F A3WE 2002083000166 20020830 00166 NM 2002 8 30 UPS02239118 1 20020812 A 5320 SUPPORT BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C ON REMOVAL OF FAIRING 3610, CRACK FOUND ON FAIRING 3608 SUPPORT FRAME AT BS 1010 STR 25 RBL 64. HFEC CARRIED OUT POST CUT OUT IAW B727 NDTM PT 6 51-00-00 FIG 4. SUPPORT FRAME REPAIRED IAW SRM 51-40-3 FIG 1 & SRM 53-50-1 FIG 9. 2 L 7 3 4F A3WE 2002083000167 20020830 00167 NM 2002 8 30 UPS02239120 1 20020815 A 5312 PRESSURE PANEL BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C SUSPECT CRACK IN NLG FWD LT PRESS WEB AT BS 243.7. CRACKED AREA REMOVED IAW SRM 51-40-2 FIG 1. HFEC C/O ON THE ABOVE AREA INSP CARRIED OUT IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT CRACK REMOVED BY CUT OUT, FABRICATED D OUBLER & FILLER IAW SRM 51-40-2, INSTALLED FILLER & DOUBLER IAW SRM 51-40-2 FIG 2. 2 L 7 3 4F A3WE 2002083000168 20020830 00168 NM 2002 8 30 UPS02438998 1 20020701 A 5320 FITTING BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT OF BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING FOUND CRACK AT HOLE NR 9 RUNNING FWD AT O/B SURFACE .0625 INCH IN LENGTH APPROX. 2 L 7 4 4F A20WE 2002083000169 20020830 00169 NM 2002 8 30 UPS02438999 1 20020701 A 5320 FITTING BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT BS 1480 BULKHEAD AT HOLE NR 3 FOUND 3 CRACKS AT EXTENSION FITTING RUNNING FWD AND AFT. 2 L 7 4 4F A20WE 2002083000170 20020830 00170 NM 2002 8 30 UPS02439000 1 20020701 A 5320 FITTING BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, RT BS 1480 BULKHEAD AT HOLE NR 1, 3 CRACKS FOUND AT EXTENSION FITTING RUNNING FWD AND AFT DIRECTION. 2 L 7 4 4F A20WE 2002083000171 20020830 00171 NM 2002 8 30 UPS02439002 1 20020702 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, LT BS 1480 BULKHEAD AREA, HOLE NR 11 CORROSION FOUND AT BULKHEAD CHORD, LOCATED AT HOLE FWD O/B. 2 L 7 4 4F A20WE 2002083000172 20020830 00172 NM 2002 8 30 UPS02439003 1 20020704 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, CORROSION AND CRACK REVEALED ON LT BS 1480 BULKHEAD CHORD AT STR 36 END FITTING AREA BY APPROX 0.040 INCH AND .1875 INCH LONG. 2 L 7 4 4F A20WE 2002083000173 20020830 00173 NM 2002 8 30 UPS02439006 1 20020712 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, LT BS 1480 BULKHEAD S35L FOUND CRACK AT CHORD I/B SURFACE, RUNNING FWD .0625 INCH, RUNNING .25 INCH L ONG, AND CRACK AT STRINGER END FITTING O/B SURFACE RUNNING FWD .125 INCH LONG. 2 L 7 4 4F A20WE 2002083000174 20020830 00174 NM 2002 8 30 UPS02439007 1 20020704 A 5311 FRAME BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C, CRACK REVEALED ON LT BS 1480 BULKHEAD CHORD AT STR 34 STRINGER END FITTING AREA BY APPROX .125 INCH R UNNING AFT AS PER FIGURE ATTACHED. 2 L 7 4 4F A20WE 2002083000175 20020830 00175 NM 2002 8 30 UPS02439008 1 20020806 A 2750 TERMINAL BOEING 747 747259B 1384804 NM T/E FLAP LOOSE A IPXA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 01 527UP 21730 INSPECTION TYPE:N/A OUTBOARD FLAPS WOULD NOT EXTEND. SECURED TERMINALS 6 & 7 OF TB 258 AND TERMINAL 11 OF TB 259 IN J42 , REPLACED S1404 GL 51752, S329, S339, PER MM 27-51-07. CYCLED FLAPS, NO MALFUNCTIONS FOUND. 2 L 7 4 4F RT A20WE 2002083000176 20020830 00176 NE 2002 8 30 UPS02439043 2 20020809 A 7200 ENGINE BOEING 747 747283B 1384867 NM PWA JT9 JT9D* NE NR 1 FLAMED OUT A IPXA A UNSCHED LANDING X M ENGINE FLAMEOUT OVER TEMP CL CLIMB 1 SO 01 523UP 22381 INSPECTION TYPE:N/A, NR 3 ENGINE WHEN ON T/O POWER CHECK 1-57 EPR ENGINE SURGED AND FLAMED OUT. ENGINE SHUT PROC CARRIE D OUT PICK EGT 713 DEGS C FOR 2 SEC ALL OTHER IND WERE NORMAL. A/C DIVERTED. REMOVED AND REPLACED NR 1 ENG. OK FOR SE RVICE. 2 L 7 4 4F 4 F A20WE E20EA 2002083000177 20020830 00177 NM 2002 8 30 UPS02439045 1 20020812 A 3350 SWITCH BOEING 747 747123F NM CABIN FAULTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:PFLT EMERGENCY LIGHT SWITCH WILL NOT STAY IN ARMED POSITION WITH GUARD CLOSED. GUARD PUSHES SWITCH INTO ON POSITION. REPLACED EMERGENCY LIGHT CONTROL MODULE IAW MM 33-51-09 PG 401/402. 2 L 7 4 4F A20WE 2002083000178 20020830 00178 NM 2002 8 30 UPS02439055 1 20020804 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C RIGHT BS 1480 BULKHEAD NR 3 HOLE CRACK FOUND AT BULKHEAD CHORD, APPROX .0625 INCH LONG, RUNNING FWD ST R 33R TO 34R. RIGHT BS 1480 BULKHEAD NR 3 HOLE AT BULKHEAD CHORD REAMED AND BUSHING INSTALLED AS PER SB 747-53A2390. 2 L 7 4 4F A20WE 2002083000179 20020830 00179 NM 2002 8 30 UPS02439057 1 20020804 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C, RIGHT BS 1480 BULKHEAD NR 6 HOLE CORROSION FOUND AT EXTENSION FITTING AROUND BORE STR 33R TO 34R. RI GHT BS 1480 BULKHEAD NR 6 HOLE AT EXTENSION FITTING REAMED AND BUSHING INSTALLED AS PER SB 747-53A2390. 2 L 7 4 4F A20WE 2002083000180 20020830 00180 NM 2002 8 30 UPS02439073 1 20020814 A 2170 COALESCER BAG BOEING 747 747200 1384847 NM A/C BAY CONTAMINATED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 521UP 21944 INSPECTION TYPE:N/A BLEED AIR SMOKE REPORTED IN UPPER DECK BY MAINTENANCE JUMPSEATERS AND NOTICEABLE BY FLIGHT CREW AT T OP OF DESCENT. ISOLATED NR 3 PACK AND SMOKE DISSIPATED. RAN 1 & 2 PACKS ONLY. VERIFIED ACM OIL SERVICED TO PROPER LEV EL. FOUND OIL RESIDUE IN COALESCER BAG. NO PART AVAIL. DEFERRED NR 3 PACK. 2 L 7 4 4F RT A20WE 2002083000181 20020830 00181 NM 2002 8 30 UPS02439076 1 20020815 A 3610 ODOR BOEING 747 747200 1384847 NM COCKPIT DETECTED A IPXA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 521UP 21944 INSPECTION TYPE:N/A OIL SMELL AND HAZE IN COCKPIT AT TOP OF DESCENT WHEN THROTTLES RETARDED. VERIFIED SOURCE OF OIL SME LL FROM NR 3 ENGINE PNEUMATICS. LOCKED OUT NR 3 ENGINE PYLON VALVE TO ISOLATE PNEUMATICS FROM AIRFRAME. 2 L 7 4 4F RT A20WE 2002083000182 20020830 00182 NM 2002 8 30 UPS02439078 1 20020804 A 5320 BAC1509100312 CHANNEL BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C M/D- BS 2315 - LBL 11 HAT SECTION CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION EXCEEDS SR M 53-10-01 FIG 1 LIMITS, REPLACEMENT REFER SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002083000183 20020830 00183 NM 2002 8 30 UPS02439079 1 20020804 A 5320 BAC1509100312 CHANNEL BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C M/D- BS 2280 - 2300 RBL 11 HAT SECTION CORRODED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION EXCEED S SRM 53-10-01 FIG 1 LIMITS, REPLACEMENT REFER SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002083000184 20020830 00184 NM 2002 8 30 UPS02439080 1 20020804 A 5320 BAC150529061 FLOOR SUPPORT BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C M/D- BS 2350 - 2360 RBL 16 FLOOR SUPPORT CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION EXC EEDS SRM 53-10-01 FIG 1, LIMITS REPLACEMENT REFER SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002083000185 20020830 00185 NM 2002 8 30 UPS02439081 1 20020804 A 5320 LS308 FLOOR SUPPORT BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C M/D- BS 2320 - 2340 RBL 2 FLOOR SUPPORT CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION EXCE EDS SRM 53-10-01 FIG 1 LIMITS, FOR REPLACEMENT REFER SRM FIG 51-10-01. 2 L 7 4 4F A20WE 2002083000186 20020830 00186 NM 2002 8 30 UPS02439098 1 20020807 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 2 PYLON DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C NR 2 PYLON I/B REAR MOUNT PYLON SKIN LOWER EDGE DOUBLER NONSTANDARD REPAIR IS FOUND AS MARKED. NR 2 P YLON I/B LOWER EDGE SKIN REPAIRED AS PER SRM 54-34-03 FIG 24 AND SRM 54-34-03 FIG 25. 2 L 7 4 4F A20WE 2002083000187 20020830 00187 NM 2002 8 30 UPS02439161 1 20020816 A 5320 ATTACH ANGLE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C COCKPIT BS 340 - 360 CTR INTERCOSTAL WEB ATT ANGLE CRACKED. ATT ANGLE REPLACED AS PER SRM 51-10-01 PA GE 8. 2 L 7 4 4F A20WE 2002083000188 20020830 00188 NM 2002 8 30 UPS02439170 1 20020826 A 3350 LIGHT BOEING 747 747SR46 1384816 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:N/A FORWARD MOST LEFT SIDE EMERGENCY LIGHT IN COURIER COMPARTMENT IS INOP. REMOVED AND REPLACED LEFT SI DE EMERGENCY LIGHT. 2 L 7 4 4F RT A20WE 2002083000189 20020830 00189 NM 2002 8 30 UPS02439178 1 20020807 A 5312 PRESSURE PANEL BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C BS RIGHT 1241 CANTED BULKHEAD OF WEB PNL HAS TWO CRACKS BETWEEN RBL 76 TO 80 AT THE AREA ADJACENT TRIM AIR DUCTS. WEB REPAIRED AS PER SRM 53-10-07 FIG 6. 2 L 7 4 4F A20WE 2002083000190 20020830 00190 WP 2002 8 30 UPS02838653 1 20020529 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 AFT PIT FS 1160 C3 DOOR RAMP PANEL SUPPORT FITTING AT L27L L36 IS CRACKED. REMOVED SUPPORT FITTING L OCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002083000191 20020830 00191 WP 2002 8 30 UPS02838655 1 20020612 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 R1 DOOR AFT DOOR JAMB CRACKED AT FASTENER HOLE APPROX LENGTH .375 INCH LONG ON FUSELAGE SKIN. ROUTED OUT CRACK IN EXTERIOR SKIN VERIFIED CRACK REMOVAL IAW HFEC NDT SPM 06-16-01-001. FABBED FILLER DOUBLER AND TRIPLER IAW DC8 SRM 53-2-0 FIG 14. INSTALLED DOUBLER AND TRIPLER REPAIR IAW 5 3-2-0 FIG 14, 51-1-20C, 51-1-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 2002083000192 20020830 00192 WP 2002 8 30 UPS02838657 1 20020526 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZ STAB DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 DENT IN RT HORIZ STAB LE 35 INCHES O/B AT ROOT. REMOVED DAMAGED AREA DENT FOUND TO BE OUT OF LIMITS. FABBED REPAIR DOUBLER IAW SRM 55-2-1. INSTALLED DOUBLER IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002083000193 20020830 00193 WP 2002 8 30 UPS02838658 1 20020525 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 AFT PIT FS 1480 L34L LONGERON IS CRACKED. REMOVED CRACKED LONGERON AND REPLACED LONGERON SECTION IAW DC8 SRM 53- 2-2 FIS 4A & 51-4-20D. 2 L 7 4 4F RT 4A25 2002083000194 20020830 00194 WP 2002 8 30 UPS02838659 1 20020525 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 LONGERON 36 CRACKED UNDER FLANGE AT APPROX FS 1272. REMOVED LONGERON SECTION (2) LONGERON SPLICES, S PLICES FOUND TO BE IN LIMITS IAW SRM 53-2-0. LOCATED & DRILLED NEW LONGERON SECTION, INSTALLED NEW LONGERON SECTION AND 2 LONGERON SPLICES IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002083000195 20020830 00195 WP 2002 8 30 UPS02838660 1 20020524 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 AFT CARGO BAY FRAME CAP IS CORRODED STA 1060 STRINGER 36. CORROSION OUT OF LIMITS IAW 53-2-0. REMOV ED FRAME CAP. FAB REPAIR ANGLE IAW UPS EO DC8-5310-11728-A. INSTALLED FRAME CAP REPAIR IAW DC8 SRM 51-1-20D & 51-1-21E . 2 L 7 4 4F RT 4A25 2002083000196 20020830 00196 WP 2002 8 30 UPS02838673 1 20020522 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 POS 13 O/B SEAT TRACK DAMAGED AT SPLICE INTERIM REPAIR C/W PER EO DC8 -5310-15957A. CUT OUT DAMAGED TRACK IAW DC8 SRM 53-2-3. LOCATED AND DEBURRED SPLICE, ALODINED & PRIMED, FABBED, LOCATED, DRILLED & INSTALLED. 2 L 7 4 4F RT 4A25 2002083000197 20020830 00197 WP 2002 8 30 UPS02838674 1 20020607 A 5230 DOOR FRAME DOUG DC8 DC873F 302199F WP CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 RT FWD DOOR UPPER FWD ELONGATED HOLE ON FRAME. FABBED DOUBLER IAW DAC DWG 5615762 AND INSTALLED SAME IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002083000198 20020830 00198 WP 2002 8 30 UPS02838675 1 20020602 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 MAIN CABIN 680 S11L LONGERON FITTING CRACKED. REMOVED FITTING, ALODINED, PRIMED AND INSTALLED NEW FI TTING IAW DC8 SRM 51-1-8, 51-1-20D, 51-1-24. 2 L 7 4 4F RT 4A25 2002083000199 20020830 00199 WP 2002 8 30 UPS02838676 1 20020614 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 L31L STA 620-650 HAS EXFOL CORROSION. FABBED NEW LONGERON IAW DAC DWG 3750575. FABBED LONGERON CLIP IAW DAC DWG 5610416. LOCATE NEW SPLICE FITTING, DRILLED EXISTING FASTENER HOLES, INSTALLED NEW LONGERON SPLICE FITTING . 2 L 7 4 4F RT 4A25 2002083000200 20020830 00200 WP 2002 8 30 UPS02838678 1 20020612 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 AC COMPT FS 24 L35R STRAP UNDER SHEAR TIE SKIN UNDER STRAP IS CORRODED. REMOVED AND REPLACED DOUBLER 2 SHEAR TIES STRAP LONGERONS L36, L35 AND L35R IAW DC8 SRM 53-2-1 PG 113, 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2002083000201 20020830 00201 WP 2002 8 30 UPS02838679 1 20020615 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1, L1 DOOR UPPER FWD DOOR JAMB CORNER CRACKED, FOUND BY X-RAY INSPECTION. ROUTED OUT CRACKED SKIN IAW DC8 SRM 53-2-0 FIG 15. VERIFIED CRACK REMOVAL IAW HFEC WPM 06-10-01.001. REMOVED EXISTING DOUBLER, TRIPLER DOOR SILL, OVERHEAD WEB AND DOOR CORNER PAN, FABBED FILLER DOUBLER TRIPLER IAW 53-2-0 FIG 15. INSTALLED REPAIR PARTS IAW 51-1-20 D AND 51-1-21. 2 L 7 4 4F RT 4A25 2002083000202 20020830 00202 NE 2002 8 30 UPS02838684 2 20020619 A 7310 FITTING DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 3 ENGINE LOOSE A IPXA K NONE K X FLUID LOSS ENGINE FLAMEOUT CR CRUISE 1 SO 01 818UP 46108 INSPECTION TYPE:N/A, AT 1 HOUR AND 35 MIN AFTER TAKEOFF, NR 3 ENGINE FLAMED OUT IN MODERATE TURBULENCE AND RAIN. FLAME- OUT OCCURRED AT 35,000 FEET AND MUCH .80. ATTEMPTED INFLIGHT ENGINE START AT 35,000, WAS UNSUCCESSFUL. PERFORMED FLAME -OUT INSP PER M/M 71-00-00, FOUND FUEL LEAKING AT MAIN FUEL INLET. TIGHTENED FITTING. RAN ENG AT VARIOUS PWR SETTINGS WITH NO PROBLEMS NOTED. A/C OK FOR SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2002083000203 20020830 00203 WP 2002 8 30 UPS02838686 1 20020525 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 AFT PIT FS 1480 L34L LONGERON IS CRACKED. REMOVED CRACKED LONGERON AND REPLACED LONGERON SECTION IAW DC8 SRM 53-2-2 FIG 4A & 51-1-20D. 2 L 7 4 4F RT 4A25 2002083000204 20020830 00204 WP 2002 8 30 UPS02838687 1 20020525 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1, LONGERON 36 IS CRACKED UNDER FLANGE AT APPROX FS 1272. REMOVED LONGERON SECTION, 2 LONGERON SPLICES , SPLICES FOUND IN LIMITS IAW 53-2-0. LOCATED & DRILLED NEW LONGERON SECTION, INSTALLED NEW LONGERON SECTION AND 2 LONG ERON SPLICE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002083000205 20020830 00205 WP 2002 8 30 UPS02838707 1 20020626 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN NOT SEATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:N/A, EMERGENCY LIGHT REMAIN ON AND CANNOT BE EXTINGUISHED. RESET EMERGENCY LIGHTS BATTERY PACK, OPS CHE CKS GOOD. 2 L 7 4 4F RT 4A25 2002083000206 20020830 00206 WP 2002 8 30 UPS02838709 1 20020627 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:N/A, 1 BULB INOP CREW ENTRY EMERGENCY LIGHT. RELAMPED AS REQUIRED. 2 L 7 4 4F RT 4A25 2002083000207 20020830 00207 WP 2002 8 30 UPS02838711 1 20020628 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2, RIGHT WING CENTER LEADING EDGE LOWER SKIN IS CRACKED INBOARD OF XW408. STOP-DRILLED CRACKED, NDT VE RIFIED CRACK TERMINATES AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087 FIG 1 APPX C. 2 L 7 4 4F RT 4A25 2002083000208 20020830 00208 WP 2002 8 30 UPS02838712 1 20020618 A 5414 SKIN DOUG DC8 DC871F 302199D WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2, NR 1 PYLON OUTBOARD SIDE SKIN IS CRACKED AT YN 343. NDT VERIFIED CRACK TERMINATES AT END OF PART. FABRICATED AND INSTALLED DOUBLER IAW DC8 70 SERIES SRM 54-2-0 FIG 6. 2 L 7 4 4F RT 4A25 2002083000209 20020830 00209 WP 2002 8 30 UPS02838713 1 20020618 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 REMOVE STAINLESS DOUBLER ON THE R2 DOOR UPPER AFT CORNER AND REPAIR FUSELAGE SKIN CRACKED AT STA 1660 LONG 10R AT UPPER CORNER. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT AREA, FABRICATED AN D INSTALLED REPAIR DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 16. 2 L 7 4 4F RT 4A25 2002083000210 20020830 00210 WP 2002 8 30 UPS02838714 1 20020618 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2, REMOVE STEEL DOUBLER ON L-1 DOOR UPPER AFT CORNER AND REPAIR IAW SRM 53-2-0 FIG 15. REMOVED EXISTIN G DOUBLER, NDT VERIFIED NO CRACKS AT EXISTING CUTOUT, FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG 15 . 2 L 7 4 4F RT 4A25 2002083000211 20020830 00211 WP 2002 8 30 UPS02838715 1 20020621 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 STATION 940 LONGERON 24L IS CRACKED. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED AT STOP DR ILL, FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-2-2 FIG 5. 2 L 7 4 4F RT 4A25 2002083000212 20020830 00212 WP 2002 8 30 UPS02838732 1 20020620 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 360.25. STOP-DRILLED CRACK, NDT VERIFIED STOPDRILLS TERMI NATES CRACK. INSTALLED CONICAL WASHERS, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-7767-A AND SRM 51-1-26. 2 L 7 4 4F RT 4A25 2002083000213 20020830 00213 WP 2002 8 30 UPS02838733 1 20020619 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON R-1 DOOR UPPER FWD CORNER AND REP AIR PER DC8 SRM 53-2-0 FIG 14, SK IN IS CRACKED STA 160 LONG 10R. REMOVED STEEL DOUBLER, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICAT ED DOUBLER,TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 14 REF TEMP REVISION 53-109. 2 L 7 4 4F RT 4A25 2002083000214 20020830 00214 NM 2002 8 30 CALA0200448 1 20020829 A 5414 SKIN BOEING 737 7373T0 1384582 NM #1 ENG PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 23589 INSPECTION FOUND A 1" CRACK IN UPPER SURFACE OF #1 ENGINE PYLON PANEL 5727L CUTOUT. REPAIRED CRACK IAW ECRA 5430-01230, REV B. 2 L 7 2 4F RT A16WE 2002083000215 20020830 00215 WP 2002 8 30 UPS02838734 1 20020620 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 REMOVE EXISTING REPAIR DOUBLER ON L-1 DOOR LOWER FWD TO AFT CORNER TO EVALUATE DAMAGE, INTERNAL DOUBL ER CRACKED AT LONG 21L, AND SKIN DAMAGED STA 31-70 BETWEEN LONG 21L TO 14L. REMOVED EXISTING REPAIR, CUTOUT DAMAGE AREA S AND SKIN SEGMENT BETWEEN STA 31 TO 70 BETWEEN LONG 21L TO 14L, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTAL LED DOUBLERS, TRIPLERS, FILLERS, AND SKIN SEGMENT IAW 8110-3 APPROVED SAA SK730-509, EO DC8-5330-17087-A, SRM 53-2-0 FIG 15. 2 L 7 4 4F RT 4A25 2002083000216 20020830 00216 WP 2002 8 30 UPS02838747 1 20020705 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A EMERGENCY LIGHTS DO NOT TEST. REPLACED EMERGENCY BATTERY PACK. 2 L 7 4 4F RT 4A25 2002083000217 20020830 00217 WP 2002 8 30 UPS02838753 1 20020707 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: N/A SKIN CRACK L/T FUSELAGE STATION 1500 ITEM DEFERRED D240904. INSTALLED REPAIR DOUBLER PER EO DC8-53 30-17101A. 2 L 7 4 4F RT 4A25 2002083000218 20020830 00218 WP 2002 8 30 UPS02838767 1 20020710 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS STAY ON WITH AC POWER ON GENERATORS. REMOVED EMERGENCY EXIT LIGHT BATTERY PAC K, OPS OK. 2 L 7 4 4F RT 4A25 2002083000219 20020830 00219 WP 2002 8 30 UPS02838768 1 20020627 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 C PIT DOOR JAMB T-ANGLE HAS CORROSION FROM STA 1250 L33R. REMOVED CORRODED T-ANGLE, LOCATED & DRILLE D NEW ANGLE IAW DC8 SRM 51-1-24. INSTALLED NEW T-ANGLE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002083000220 20020830 00220 WP 2002 8 30 UPS02838769 1 20020625 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 R3 DOOR LOWER FORWARD CORNER HAS CRACK INDICATION FOUND BY RADIOGRAPHIC INSPECTION. REPAIRED DOOR JA MB CORNER IAW DC8 SRM 53-2-0 FIG 17. 2 L 7 4 4F RT 4A25 2002083000221 20020830 00221 WP 2002 8 30 UPS02838770 1 20020625 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 R3 DOOR UPPER AFT CORNER HAS CRACK INDICATION FOUND BY RADIOGRAPHIC INSPECTION. REPAIRED DOOR JAMB C ORNER IAW DC8 SRM 53-2-0 FIG 16. 2 L 7 4 4F RT 4A25 2002083000222 20020830 00222 SO 2002 8 30 C2XA02BT046 1 20020830 A 3350 1317 LIGHT EMB 145 EMB145ER 3260211 SO BLOWN A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 15926 145005 BTV---DURING SERVICE/ROUTINE OVERNIGHT CHECK MAINTENANCE FOUND AISLE OVERHEAD EMERGENCY LIGHT AT EMERGENCY EXIT ROW TO B E INOPERATIVE. REMOVED AND REPLACED LIGHT BULB AT EMERGENCY EXIT OVERHEAD LIGHT IAW EMB145 AMM 33-50-00. OPS. CHECKED LI GHT GOOD. 2 L 7 2 4F RT T00011AT 2002083000223 20020830 00223 NM 2002 8 30 02082901 1 20020829 A 2913 3508807 PUMP RROYCE 535E4 BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E4 54555 NE #1 ENGINE FAILED A N8TA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 19 545NA 10115 3326 31658 29944 31658 Crew called with Left Engine Driven Hyd. pump overheat and later with Left Hyd. Qty. loss. Aircraft returned to LAS, an uneventful landing was accomplished. Further investigation revealed that the #1 Engine E.D.P. had suffered mechanical fa ilure, causing loss of hydraulic fluid. Replaced Hydraulic pump and filters, flushed per m/m 29-11-00, leak check okay. A/C was then returned to service. 2 L 7 2 4F 4 F RT A2NM E12EU 2002083000224 20020830 00224 WP 2002 8 30 UPS02838771 1 20020622 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 L1 DOOR CORNER UPPER FWD DOUBLER DOES NOT MEET SRM REQUIREMENTS. REPAIRED DOOR JAMB CORNER IAW DC8 S RM 53-2-0 FIG 15. 2 L 7 4 4F RT 4A25 2002083000225 20020830 00225 SO 2002 8 30 C2XA02BT047 1 20020828 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO DISCHARGED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14916 145415 EWR---CO3419, CREW REPORTED "EMERGENCY LIGHT INOPERATIVE". MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PAC KS AND RECHARGED EMERGENCY LIGHT BATTERIES. OPS.CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002083000226 20020830 00226 WP 2002 8 30 UPS02838772 1 20020626 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 C3 CROSS SLIDE DOOR LWR T-BOLT BACK UP FITTING CORRODED AT STA 1242. REMOVED CORRODED FITTING LOCATE D, DRILLED UP MODIFIED FITTING AND CLIPS IAW DC8 SRM 53-2-0 FIG 2D. INSTALLED FITTING AND 2 CLIPS IAW DC8 SRM 53-2-0 FI G 2D & 51-1-20D. 2 L 7 4 4F RT 4A25 2002083000227 20020830 00227 WP 2002 8 30 UPS02838774 1 20020626 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 C3 CROSS SLIDE DOOR JAMB HAS CRACKED BANANA FITTING AT STA 1260 LONGERON L33R. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002083000228 20020830 00228 WP 2002 8 30 UPS02838778 1 20020707 A 5320 3754914501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 FITTING IN TORQUE BOX AT STA 1150 IS CORRODED BEYOND LIMITS AT LONG 31R. REMOVED AND REPLACED FITTIN G IAW DWG 3754914, AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002083000229 20020830 00229 WP 2002 8 30 UPS02838781 1 20020621 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 STA 1400 FRAME IS CRACKED BELOW LONG 34R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, AND FILL ER IAW DC8-5310-11728-A, AND DWG DC8-53A-011. 2 L 7 4 4F RT 4A25 2002092000089 20020920 00089 SO 2002 9 20 C2XA02BT048 1 20020828 A 3320 BR9000 BALLAST EMB 145 EMB145ER 3260211 SO GALLEY DEFECTIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 15941 145035 EWR---CO3869, ON POSTFLIGHT INSPECTION, CREW REPORTED SMOKE IN THE GALLEY. BAD GALLEY BALLAST. MAINTENANCE REMOVED AND REPLACED BALLAST FOR GALLEY LIGHT. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002083000230 20020830 00230 SO 2002 8 30 C2XA02BT049 1 20020828 A 3350 78812 LIGHT EMB 145 EMB145LR 3260212 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 13566 145622 BDL---CO3368, CREW REPORTED EMERGENCY FLOOR EXIT LIGHTING PROXIMITY STRIP NEAR EXIT INOPERATIVE....CONTRACT MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT STRIP AND OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002083000231 20020830 00231 NM 2002 8 30 UPS02439214 1 20020802 A 5330 SKIN BOEING 747 747212B 1384886 NM AFT CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C AFT CARGO DOOR CUTOUT UPPER FWD CORNER 1EA FASTENER HOLE CRACK FOUND AT SKIN, APPROX 1/2" RUNNING DOW NWARD AND 5/16" RUNNING UPWARD PLS REFER ATT FTG. (BS1810 TO 1810, STR R28 TO R28) WASHER AND DOUBLER INSTALLED AT U PPER FWD CUTOUT AS PER SRM 53-30-03 FIG 62 WORK DETAIL REFER ATTACHED CWS. AND EO B747-5330-14013-B REPEAT INSPECTION I S REQUIRED AT INTERVAL 3000 CYCLES AS PER SRM 53-30-03 FIG 62 TABLE 3. 2 L 7 4 4F A20WE 2002100700067 20021007 00067 NM 2002 10 7 UPS02439228 1 20020827 A 5347 SEAT TRACK BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 528UP 1 INSPECTION TYPE:N/A F/O OUTBOARD AFT SEAT TRACK CRACKED 2 PLACES. REMOVED AND REPLACED F/O OUTBOARD AFT SEAT TRACK. 2 L 7 4 4F RT A20WE 2002083000232 20020830 00232 NM 2002 8 30 UPS02439229 1 20020827 A 5340 SEAT TRACK BOEING 747 747200 1384847 NM CAPT SEAT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 528UP 1 INSPECTION TYPE:N/A CAPTS SEAT TRACK DAMAGED ***MRR FILED AS OPEN*** 2 L 7 4 4F RT A20WE 2002083000235 20020830 00235 NM 2002 8 30 ABXA020124 1 20020712 A 5700 SKIN BOEING 767 767200 1385120 NM LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 A 0.06" LONG CRACK WAS FOUND IN ONE FASTENER HOLE IN THE UPPER LEFT WING SKIN PANEL AS SHOWN IN REF. (5) - SB 767-54-008 1. REPAIRED AREA IAW REA B657-43511-MR. 2 L 7 2 4F RT A1NM 2002083000236 20020830 00236 NM 2002 8 30 ABXA020125 1 20020712 A 5700 SKIN BOEING 767 767200 1385120 NM RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 A 0.06" LONG CRACK WAS FOUND IN ONE FASTENER HOLE IN THE RIGHT UPPER WING WHILE ACCOMPLISHING SERVICE BULLETIN SB 767-54 -0081. REPAIRED AREA IAW REA B657-43512-MR. 2 L 7 2 4F RT A1NM 2002083000237 20020830 00237 NM 2002 8 30 ABXA020126 1 20020724 A 5700 112T4101 SKIN BOEING 767 767200 1385120 NM RIGHT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 CORROSION AT RIGHT WING LOWER SKIN PANEL NO. 1 AT REAR SPAR, BETWEEN STRINGER 230 AND 277. REPAIRED AREA IAW REA B657-43 583-MR. 2 L 7 2 4F RT A1NM 2002083000238 20020830 00238 NM 2002 8 30 ABXA020137 1 20020611 A 5300 96FS667743101 SEAT TRACK BOEING 767 767200 1385120 NM A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 SEAT TRACK P/N 96FS667743-101 LOWER HORIZONTAL OUTBOARD FLANGE AT STATION 753-45, LEFT BUTT LINE 86.38, DRILLED BY MISTA KE. REPAIRED AREA IAW REA B653-43514-DE. 2 L 7 2 4F RT A1NM 2002083000239 20020830 00239 NM 2002 8 30 ABXA020138 1 20020712 A 5700 1143170 RIB BOEING 767 767200 1385120 NM A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 LEFT WING LEADING EDGE SLAT #6 AUXILIARY RIB ASSEMBLY P/N 1143170, AUXILIARY RIB HAD MISDRILLED HOLE. REPAIRED AREA IAW REA B657-43455-MR. 2 L 7 2 4F RT A1NM 2002083000240 20020830 00240 NM 2002 8 30 ABXA020140 1 20020712 A 5300 96FS667831135 SHEAR TIE BOEING 767 767200 1385120 NM A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 SHEAR TIE INSTALLED AT STATION 1417, BETWEEN STRINGER 20 LEFT TO STRINGER 21 LEFT, HAD SHORT EDGE MARGIN TO FASTENER. RE PAIRED AREA IAW REA B653-43456-DE. 2 L 7 2 4F RT A1NM 2002083000241 20020830 00241 NM 2002 8 30 ABXA020143 1 20020425 A 5700 113T11106 SUPPORT FITTING BOEING 767 767200 1385120 NM RIGHT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 MIGRATED BUSHING, RIGHT MAIN LANDING GEAR SIDE STRUT SWIVEL SUPPORT FITTING, AFTER REMOVAL OF PART 113T1108-25, FOUND DE EP CORROSION ON FITTING. REPAIRED AREA IAW REA B657-43443-MR. 2 L 7 2 4F RT A1NM 2002083000242 20020830 00242 NM 2002 8 30 ABXA020144 1 20020730 A 5500 182T32002 SKIN BOEING 767 767200 1385120 NM CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 RIGHT HORIZONTAL STABILIZER, UPPER SKIN P/N 182T3200-2, AT STRINGER 3, RSS 42, WAS CORRODED OUT OF LIMITS. REPAIRED AREA IAW REA B655-43586-MR. 2 L 7 2 4F RT A1NM 2002083000243 20020830 00243 WP 2002 8 30 ABXA020148 1 20020829 A 3260 801801 SENSOR DOUG DC9 DC941 302207N WP DEFECTIVE A ABXA O OTHER O OTHER CL CLIMB 1 GL 23 954AX 47612 AFTER GEAR RETRACTION, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON. RIGHT HYDRAULIC PUMPS ON HIGH. AT GEAR UPLATCH CHECK , THE LIGHT WENT OUT. GEAR RECYCLED ONE TIME BEFORE UPLATCH CHECK WITH THE LIGHT STILL ON. REPLACED THE LEFT GEAR DOWN S ENSOR IAW DC-9 MM 32-60-01-2 AND PERFORMED ADJUSTMENT AND TEST. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 2002091600033 20020916 00033 NM 2002 9 16 DHL2002721513 1 20020803 A 5311 FRAME BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK, RT WHEEL WELL CASTING FRAME BS 930 CRACKED TO O/B FWD FLANGE, O/B AFT FLANGE ALSO I/B FLANGE. REMOVED C RACKED STA 930 FRAME RT. LOCATED AND DRILLED-UP NEW STA 930 FRAME R. INSTALLED NEW STA 930 FITTING RT. 2 L 7 3 4F RT A3WE 2002083100001 20020831 00001 EU 2002 8 31 DHL2002363515 1 20020808 A 5310 SKIN AIRBUS 300 A300B4203 3930306 EU CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-check/STA. 1415 STR. 49R and STA. 49L on the interior of the skin there is 4SQ" of moderate corrosion at STR. 49R and 7SQ" of moderate corrosion at STR. 49LCorrective action/Removed corrosion IAW A300 SRM 51-40-11. UT thickness checked p er NTM 51-20-00 49L before 3.20mm,49L after 2.48mm,49R before 2.23mm,49R after 1.52mm. Engineering dispo on page 2.White light/magnifying glass inspected damaged area. Rototested holes per NTM 51-30-10,no cracks found. Smooth rework damage area for proper nut sitting IAW A300 SRM 51-30-30. Eddy current inspected reworked area per NTM 51-31-05 no cracks found . Reamed holes to dia. listed 4.723 to 4.758 mm. Installed fastners IAW A300 SRM 51-30-30. Alodined and primed IAW A 2 L 7 2 4F RT A35EU 2002083100002 20020831 00002 EU 2002 8 31 DHL2002363517 1 20020801 A 5311 SKIN AIRBUS 300 A300B4203 3930306 EU CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-check/ Popped rivet at frame 100 at the 3 oclock position(suspected corrosio) (exterior).corrective action/ Removed an replaced butt joint IAW A300 SRM 53-10-00 pg. 701 an A300 SRM 51-30-30.Performed repair IAW Airbus repair solution by i nstalling doubler an filler in ref. to 942-019963/005/2002 IAW A300 SRM 51-30-30 See RAS form # ref. RAS/DAHAM/4015720/2 002.Cutout area of skin 6.5"x2.5". Removed crack IAW Airbus repair 942-019963/005/2002. Eddy current inspected cutout ar ea per NTM 51-31-05 no cracks found. 2 L 7 2 4F RT A35EU 2002083100003 20020831 00003 EU 2002 8 31 DHL2002363518 1 20020827 A 5753 TAB AIRBUS 300 A300B4203 3930306 EU DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-check/Rt. wing O/B flap @ rib 25,repair on the upper surface of O/B end of aft flap is delaminated. Lower surface also has a small area of delamination on existing repair.Corrective action/ Repaired tab using new core material an bonded n ew skin to 15"x15" of upper tab IAW A300 SRM 51-42-20 para 2.4 an 57-50-00 para 601. Removed R/H wing outer flap outboar d tab IAW A300MM 27-51-52. Painted tab R/H IAW A300 SRM 51-40-12. 2 L 7 2 4F RT A35EU 2002083100004 20020831 00004 EU 2002 8 31 DHL2002363519 1 20020809 A 3222 D520181 SLEEVE AIRBUS 300 A300B4203 3930306 EU CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-check/#3 protective axle sleeve has worn nickel plating,gouged an corrosion.Corrective action/Replaced protective slee ve IAW A300 MM 32-42-27. Installation of # 3 brake an tire assy. accomplished on NRC DHL-085-904 Seq. 0019 (and bleed an leak ck) 2 L 7 2 4F RT A35EU 2002090100001 20020901 00001 EU 2002 9 1 DHL2002363521 1 20020802 A 5300 DOUBLER AIRBUS 300 A300B4203 3930306 EU A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-check/R/H aft. fuselage external doubler is bulging @ Fr. 72,str. 46R to 44R.Corrective action/ Removed 5 ea. hilocks from fr. 72 IAW A300 SRM 51-30-30.Inspected holes for corr. or seperation of doubler found no defect.Installed 5 ea. hil ocks in fr. 72 IAW A300 SRM 51-30-30. 2 L 7 2 4F RT A35EU 2002090100002 20020901 00002 EU 2002 9 1 DHL2002363522 1 20020812 A 5300 COVER AIRBUS 300 A300B4203 3930306 EU CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-check/web between fr. 25 an fr. 26 above str. 45R has 10 sq. in. of corrosion.Corrective action/ Removed corroded web IAW A300 SRM 51-30-30. Went for engineering support.Fabricated new cover plate from 0.025" 2024-T3 clad. Cutout cover pl ate per Fig. 1. Treated,primed an topcoat on cover plate an cutout per A300 SRM 51-41-12.OK to install new cover plate I AW A300 SRM 51-30-30. Installed cover plate per A300 SRM 51-30-30. 2 L 7 2 4F RT A35EU 2002090100003 20020901 00003 EU 2002 9 1 DHL2002363524 1 20020821 A 5540 RUDDER AIRBUS 300 A300B4203 3930306 EU DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-check/EADS responsibility during DFDR system test,rudder damaged at lower t/e wedge 19" longx 4.5" wide %' up from low er edge of rudder.Corrective action/area repaired IAW A300 SRM 55-40-00 page 740 see page 2 an 3 fpr detrail instruction am NDT requirements c/w. Prepped an painted IAW A300 SRM 51-40-12 2 L 7 2 4F RT A35EU 2002090300001 20020903 00001 NM 2002 9 3 ANCF200200018 1 20020828 A 2120 DUCT DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE CABIN PRESSURE LEAKING W ANCF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 583AN 53183 DURING CLIMB AT FL180, THE FLOW LIGHT CAME ON AND THE CABIN ALTITUDE WAS INCREASING. IMMEDIATELY DESCENT WAS PERFORMED T O FL100, BUT THE FLOW LIGHT REMAINED ON UNTIL FL100 WAS REACHED. THE AIR LEAK FOUND IN LT DUCT THERMOSTAT WAS CORRECT ED. SOME CLAMPS IN LT / RT DUCTS THAT WERE FOUND LOOSEN WERE ADJUSTED AND THE WATER TANK PRESSURIZATION LINE WAS ADJUSTE D IAW AMM 36-00-00 PAGES 201-206 AND 223. PNEUMATIC SYSTEM TEST WITH SATISFACTORY RESULTS. 2 L 7 2 4F 4 F RT E9NE 2002090300002 20020903 00002 2002 9 3 CA020801010 4 20020616 A 3442 INDICATOR BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE WX RADAR FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA (CAN) FLIGHT WAS DIVERTED DUE TO BURNING SMELL IN COCKPIT FROM WEATHER RADAR INDICATOR. UNIT WAS REPLACED AND SHOP REPO RT INDICATED CAUSE OF PROBLEM WAS BURNED OUT DIODES ON RECTIFIER AND FILTER ASSY. 2 L 7 2 4F 4 F A16WE E2EA 2002090300003 20020903 00003 NM 2002 9 3 CA020802001 1 20020801 A 5754 6521630173 SLAT BOEING 727 727231 1384079 NM PWA JT8 JT8D9A 52048 NE LT WING SEPARATED W O OTHER D INFLIGHT SEPARATION DE DESCENT 1 CA (CAN) ON APPROACH, LT INBD. FORE FLAP SEPARATED FROM A/C. AFTER LANDING,DISCOVERED THE A/C HAD LOST THE LT FOREFLAP TRA ILING EDGE. (APPROX. 8FT) THE SEPARATED SECTION TRAVELLED AFT, AND CONTACTED THE NR 1 ENGINE INLET COWL AND FORWARD PYL ON LEADING EDGE. SCUFF MARKS ON THE FUSELAGE FORWARD OF THE PYLON WERE ALSO FOUND. 2 L 7 3 4F 4 F A3WE E2EA 2002090300004 20020903 00004 NM 2002 9 3 CA020807001 1 20020707 A 3150 WARNING SYSTEM BOEING 767 767209 1385127 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT ACTIVATED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) REJECTED TAKE OFF RTO. AT 145 KTS. DUE CONFIGURATION WARNING. 2 L 7 2 4F 4 F RT A1NM E3NE 2002090300005 20020903 00005 EA 2002 9 3 CA020808001 1 20020806 A 2710 600908002 PULLEY CNDAIR CL600 CL6002B19 1900309 EA AILERONS FROZEN W B A EMER. DESCENT UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CA 15113 (CAN) FROZEN AILERONS AT FL280 CLIMBING TO FL300. A/C WAS STILL CONTROLLABLE BUT ONLY WITH A BANK ANGLE OF 5 DEG. DECI DED TO START A STRAIT DESCENT DOWN TO FL70 TO GET OUT OF FREEZING LEVEL. AT FL70 AILERON OPERATION WAS REGAINED. LANDIN G IN DUS WAS NORMAL. BEFORE FLIGHT, HAD HEAVY RAIN SHOWERS. FDR REPLACED. FOUND 'GEL' ON AILERON FLT CONTROL CABLE PU LLEYS. CLEANED PULLEYS AND APPLIED LPS 3 TO CABLES IAW MM 20-23-00. 2 L 7 2 4F RT A21EA 2002090300006 20020903 00006 EA 2002 9 3 CA020809001 1 20020725 A 2710 CONTROL CABLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE AILERONS FROZEN W A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CA 18261 (CAN) PILOT REPORTED THAT THE AILERON TRIM MESSAGE WAS DISPLAYED ON EICAS WHILE IN CRUISE AND THAT AILERONS WERE VERY ST IFF. AIRCRAFT DECENDED TO A LOWER ALTITUDE AND PROBLEM CLEARED. CREW REPORTED THAT THERE WAS HEAVY RAIN ON TAKE OFF. A IRCRAFT LANDED WITHOUT INCIDENT.AILERON CONTROL CIRCUIT INSPECTED AND NO ANOMALIES NOTED. AFT QUADRANTS AND CONTROL PUL LEYS CLEANED AND LUBRICATED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002090300007 20020903 00007 SW 2002 9 3 CA020815007 1 20020611 A 7160 6890550 INTAKE DUCT BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL ENGINE SEPARATED W B A EMER. DESCENT UNSCHED LANDING D F E INFLIGHT SEPARATION FLT CONT AFFECTED VIBRATION/BUFFET DE DESCENT 1 CA (CAN) ONE NUT PLATE HOLDING THE INTAKE BELL MOUTH TO THE FIRE WALL DEPARTED FROM ITS MOUNTING AND WAS INGESTED BY THE CO MPRESSOR. THIS CAUSED A VIOLENT YAW AND PARTIAL LOSS OF POWER. THE PILOT ENTER AN AUTO-ROTATION AND LANDED SUCCESFULLY W ITH MINIMAL DAMAGE TO THE AIRCRAFT. 1 G 7 1 3U 3 U H2SW E4CE 2002090300008 20020903 00008 GL 2002 9 3 CA020819006 2 20020817 A 7323 206062721011 ACTUATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED W O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) THE PILOT WAS IN CRUISE FLIGHT WHEN THE ROTOR TACH NEEDLE MOVED TO 98 PERCENT. THE PILOT TRIED TO INCREASE ROTOR S PEED BY USING THE INCREASE BUTTON ON THE GOVERNOR BEEP RANGE SWITCH, BUT NO REACTION. THE PILOT BEGAN DESCENT INTO THE WELL SITE AND ON PULLING UP ON THE COLLECTIVE, THE ROTOR RPM DROPPED TO 95 PERCENT ON THE TACH. LANDED NORMALLY. THE PILOT LOOKED INTO THE ENGINE COMPARTMENT, THE LINEAR ACTUATOR ARM WAS ABLE TO MOVE IN AND OUT FREELY. FLEW UP WITH A NEW ACTUATOR AND SET IT UP, THE PILOT CONTINUE. 1 G 7 1 3U 3 U H2SW E4CE 2002090300009 20020903 00009 EA 2002 9 3 CA020820001 1 20020805 A 2710 600911915153 MIXER BOX CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE AILERONS CONTAMINATED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 CA 12272 (CAN) WHILE EN-ROUTE AT 29,000 FT, THE FLIGHT CREW EXPERIENCED AILERON CONTROL LOCKUP. A/P TRIM CAUTION MSG. AIRCRAFT DESCENDED TO 15,000 FT FOR 5 MIN. CONTROL RETURNED. AIRCRAFT CONTINUED TO DESTINATION WITHOUT INCIDENT. AIRCRAFT TOOK O FF IN HEAVY RAIN AND STANDING WATER ON THE RUNWAY. MORE INFO TO FOLLOW WHEN AVAILABLE.AILERON CONTROL SYSTEM WAS INSPECT ED. FOUND THAT THE LT AND RT AILERON MIXER ASSY. HAD A SMALL AMOUNT OF ROTATIONAL RESISTANCE . BOTH LT AND RT AILERON M IXER ASSY WERE REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002090300010 20020903 00010 EA 2002 9 3 CA020820002 1 20020805 A 2710 6009119153 MIXER BOX CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AILERON DAMAGED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 CA (CAN) WHILE ENROUTE, FLIGHT CREW EXPERIENCED AILERON CONTROL STIFFNESS AND JAM AT 25,000 FT. AUTO-PILOT DISSCONNECTED AND THE CREW WAS ABLE TO FREE THE JAM AND CONTINUED ON WITHOUT FURTHER INCIDENT. THE AIRCRAFT TOOK OFF IN HEAVY RAIN AND THERE WAS STANDING WATER ON THE RUNWAY AT THE TIME OF DEPARTURE. AILERON CONTROL SYSTEM WAS INSPECTED. FOUND THAT THE LT AND RT AILERON MIXER ASSY. HAD SOME ROTATIONAL RESISTANCE. BOTH LT AND RT AILERON MIXER ASSY WHERE REPLACED. AIRCRA FT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002090300011 20020903 00011 EA 2002 9 3 CA020820008 1 20020717 A 5610 601R3303310 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 16897 (CAN) RT WINDSHIELD OUTER PLY CRACKED DURING TAXI. A/C RETURNED TO BLOCKS. WINDSHIELD REPLACED. WINDSHIELD HAD BEEN INSTALLED SINCE NEW. 2 L 7 2 4F 4 F RT A21EA E15NE 2002090300012 20020903 00012 WP 2002 9 3 CA020820009 1 20020818 A 2530 331216 TUBE 2671 LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE EVAPORATOR CRACKED W O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 062 (CAN) CREW REPORTED AFT CABIN BURNING ODOR WITH WHITE SMOKE NEAR AFT GALLEY LT CABIN DOOR AREA. THE AFT GALLEY POWER WA S TURNED OFF IN FLIGHT BY CREW AND THE SITUATION WAS BACK TO NORMAL. UPON ARRIVAL, AFT GALLEY CHILLER WAS REPLACED. T HE EVAPORATOR WAS REMOVED FROM ORIGINAL UNIT AND FURTHER LEAK CHECK WAS CARRIED OUT AND REVEALED THAT AN EXTERNAL TUBIN G OF THE EVAPORATOR WAS CRACKED AT A WELDING POINT WHICH PERMITTED THE FREON TO ESCAPE CAUSING THE WHITE SMOKE. 2 L 7 3 4F 4 F A23WE E12EU 2002090300013 20020903 00013 WP 2002 9 3 CA020820010 1 20020818 A 3230 740845103 MANIFOLD LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE MLG CONTROL MOD CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING NORMAL MAINTENANCE OPERATION, THE MAIN LANDING GEAR CONTROL MODULE IN THE HYDRAULIC SERVICE CENTER, WAS FOU ND LEAKING BECAUSE THE MAIN LANDING GEAR CONTROL MODULE MANIFOLD WAS CRACKED. MAINTENANCE REPLACED THE MLGCM IAW THE AMM 32-31-01 2 L 7 3 4F 4 F A23WE E12EU 2002090300015 20020903 00015 NM 2002 9 3 UPS02439179 1 20020816 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BS 380 UPPER DECK FLOORBEAM UPPER CHORD, 1 FASTENER HOLE CRACK REVEALED AT RBL 60, RUNNING AFT APPROX .0625 INCH LENGTH. UPPER DECK BS 380 FLOORBEAM RBL 60 CRACKED HOLE REPAIRED AS PER EO B747-5320-12407-C APPENDIX D PLAN A. 2 L 7 4 4F A20WE 2002090300016 20020903 00016 NM 2002 9 3 UPS02439180 1 20020816 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BS 340 UPPER DECK FLOORBEAM UPPER CHORD, THREE FASTENER HOLES CRACKED, REVEALED AT LBL 18, RBL 15 & RB L 46 RESPECTIVELY. UPPER DECK BS 300 FLOORBEAM LBL 18 & RBL 15 CRACKED HOLE REF NRC 7305 SECTIONAL REPLACED FROM RBL 20 TO LBL 40 AS PER SRM 53-10-07 FIG 23, RBL 46 CRACKED FASTENER HOLE REPAIRED AS PER EO B747-5320-12407-C APPENDIX D, PLA N C. 2 L 7 4 4F A20WE 2002090300017 20020903 00017 NM 2002 9 3 UPS02439181 1 20020816 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BS 360 UPPER DECK FLOORBEAM UPPER CHORD, 2 FASTENER HOLES CRACK REVEALED AT RBL 28 & RBL 43 RESPECTIVE LY. UPPER DECK BS 360 RBL 28 CRACKED HOLE CRACK REMOVED AS PER EO B747-5320-12407-C APPENDIX D. NO NECESSARY REPAIR. RBL 43 CRACKED FASTENER HOLE REPAIRED AS PER EO B747-5320-12407-C APPENDIX D PLAN C. 2 L 7 4 4F A20WE 2002090300018 20020903 00018 NM 2002 9 3 UPS02439182 1 20020817 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C, UPPER DECK BS 400 RBL 80 FLOOR SUPPORT FOUND CRACKED. FLOOR SUPPORT REPAIRED PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 2002090300019 20020903 00019 NM 2002 9 3 UPS02439183 1 20020816 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C UPPER DECK BS 520 - 540 LBL 65 SEAT TRACK CROWN FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMI T. SEAT TRACK REPAIR AS PER SRM 53-10-05 FIG 6. 2 L 7 4 4F A20WE 2002090300020 20020903 00020 NM 2002 9 3 UPS02439186 1 20020826 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C UPPER DECK BS 520 - 570 RBL 50 SEAT TRACK CROWN FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMI T. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002090300021 20020903 00021 WP 2002 9 3 UPS02838911 1 20020702 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 AIR COND PRESS COMPT AT FS 56 BETWEEN L32R - 34R BETWEEN, UNDER AND AROUND SHEAR TIE SKIN IS CORRODED . REMOVED CORROSION FROM FUSELAGE SKIN, FAB NEW SECTION OF INNER DOUBLER, FAB SPLICE PLATE DOUBLER IAW DC8 53-2-0, INST ALLED INNER DOUBLER IAW DAC DWG 5613862. 2 L 7 4 4F RT 4A25 2002090300022 20020903 00022 WP 2002 9 3 UPS02838912 1 20020623 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN CRACKED FS 1724 L15R. REPAIRED AREA IAW DC8 SRM 53-2-1. 2 L 7 4 4F RT 4A25 2002090300023 20020903 00023 WP 2002 9 3 UPS02838913 1 20020725 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:N/A CRACK AT PIT 34 UPPER FWD CORNER FUSELAGE SKIN. INSTALLED REPAIR DOUBLERS PER EO DC-8 53-10-17222-A . 2 L 7 4 4F RT 4A25 2002090300024 20020903 00024 WP 2002 9 3 UPS02838975 1 20020726 A 5320 3750257U1 SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 STA 440-460 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002090300025 20020903 00025 WP 2002 9 3 UPS02838976 1 20020722 A 5511 RIB DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 LEFT HORIZONTAL STAB L/E UPPER RIB IS CRACKED AT FASTENER END AT XFS 166.250. STOP DRILLED CRACK, ND T VERIFIED NO CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 55-3-0 FIG 8. 2 L 7 4 4F RT 4A25 2002090300026 20020903 00026 WP 2002 9 3 UPS02838977 1 20020726 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 LONG 24L IS CRACKED AT STA 978. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATES AT STOP DRILL, FAB RICATED AND INSTALLED DOUBLER IAW SRM 53-2-2 FIG 5. 2 L 7 4 4F RT 4A25 2002090300027 20020903 00027 WP 2002 9 3 UPS02838978 1 20020720 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 R-1 DOOR UPPER FWD CORNER HAS A REPAIR THAT DOES NOT CONFORM TO THE SRM AT STA 160 AT LONG 11R. REMO VED DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 14. 2 L 7 4 4F RT 4A25 2002090300028 20020903 00028 WP 2002 9 3 UPS02838979 1 20020723 A 5320 5612298 FINGER DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 AFT SIDE OF STA -99 FINGER DOUBLER IS CORRODED BEYOND LIMITS AT RBL 60. REMOVED, FABRICATED AND INST ALLED DOUBLER DWG 5612298. 2 L 7 4 4F RT 4A25 2002090300029 20020903 00029 WP 2002 9 3 UPS02838985 1 20020725 A 5330 577991641 FINGER DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 INTERNAL FINGER DOUBLER IS CORRODED BEYOND LIMITS STA 70-210 AT LONG 31R. REMOVED, FABRICATED, AND R EPLACED DOUBLER IAW DWG 5779916, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2002090300030 20020903 00030 WP 2002 9 3 UPS02839015 1 20020807 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, LIGHTS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2002090300031 20020903 00031 WP 2002 9 3 UPS02839024 1 20020725 A 5330 577992541 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 STA 190 DOUBLER CORRODED BEYOND LIMITS BETWEEN LONGERONS 31L & 31R. REMOVED, FABRICATED & INSTALLED REPLACEMENT DOUBLER IAW DWG 5779925 & SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002090300032 20020903 00032 WP 2002 9 3 UPS02839028 1 20020809 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT FAILED DURING PREFLIGHT. REMOVED AND REPLACED LIGHT ASSY. 2 L 7 4 4F RT 4A25 2002090300033 20020903 00033 WP 2002 9 3 UPS02838782 1 20020618 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLERS ON L2 DOOR LOWER FWD CORNER AND REPAIR IAW SRM 53-2-0 FIG 18, STA 162 0 LONG 21L SKIN IS CRACKED. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND IN STALLED DOUBLER, TRIPLER, FILLER, AND REPAIR BUSHINGS IAW SRM 53-2-0 FIG 18 AND EO DC8-5330-17068-A. 2 L 7 4 4F RT 4A25 2002090300034 20020903 00034 WP 2002 9 3 UPS02838794 1 20020618 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON L1 DOOR UPPER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 15 AT STA 25 LONG 10L AREA. REMOVED EXISTING REPAIR, CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOU BLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15. 2 L 7 4 4F RT 4A25 2002090300035 20020903 00035 WP 2002 9 3 UPS02838795 1 20020622 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 CORROSION BETWEEN LONGERON AND FRAME ATTACH PLATE AFT OF TORQUE BOX STA 1160 AT LONG 35R TO 33R WEB I S CORRODED BEYOND LIMITS. REMOVED EXISTING DOUBLER, CUT OUT CORRODED SECTION OF WEB, FABRICATED AND INSTALLED WEB SECTI ON, SPLICE PLATES, FRAME REPAIR ANGLES, CLIPS, INTERCOSTAL, AND UPPER TORQUE BOX WEB IAW DWG 9754949, 3753772, 9754947, 5753893, AND SRM 53-2-0 FIG 1B, DC8-5310-11728-A APPX A. 2 L 7 4 4F RT 4A25 2002090300036 20020903 00036 WP 2002 9 3 UPS02838797 1 20020714 A 3350 6012235 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 EMERGENCY EXIT LIGHTS FAILED OPS CHECK. RANG OUT WIRING PER WDM 33-50-01, WIRING CHECKED OUT GOOD. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, AND OPS CHECKED GOOD IAW DC8 M/M 33-50-01. 2 L 7 4 4F RT 4A25 2002090300037 20020903 00037 WP 2002 9 3 UPS02838812 1 20020717 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 852UP 46052 INSPECTION TYPE:N/A AFTER ENG START, WENT DARK, EMERGENCY LIGHTS CAME ON, WENT TO DISARM, THEN DISARM CHECK, DISARM, THE N BACK TO ARM. LIGHTS CAME BACK ON. PULLED AND RESET EMERGENCY LIGHTS CONTROL CB AND EMERGENCY LIGHTS CB TO GET THEM T O WORK NORMALLY. REMOVED, REPLACED AND TESTED EMERGENCY LIGHTS BATTERY PACK IAW MM 33-50-01. 2 L 7 4 4F RT 4A25 2002090300038 20020903 00038 2002 9 3 UPS02838815 4 20020716 A 2565 SLIDE DOUG DC8 DC873F 302199F WP ENTRY DOOR OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:N/A ESCAPE SLIDE GIRT BAR WOULD NOT ENGAGE. REPACKED AND INSTALLED EVACUATION SLIDE ON MAIN CABIN DOOR IAW DC8-MM 25-60-01. 2 L 7 4 4F RT 4A25 2002090300039 20020903 00039 WP 2002 9 3 UPS02838848 1 20020719 A 3240 CONTROL VALVE DOUG DC8 DC873F 302199F WP LT MLG MALFUNCTIONED A IPXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 803UP 46073 INSPECTION TYPE:N/A ON TAXI OUT A/C FELT LIKE LEFT BRAKES WERE DRAGGING. REMOVED AND REPLACED WHEEL BRAKE CONTROL VALVE S PER MM 32-42-02. PERFORMED ADJ /TEST OF SYSTEM, ALL BRAKES OPERATE NORMALLY. A/C OK TO SERVICE. 2 L 7 4 4F RT 4A25 2002090300040 20020903 00040 WP 2002 9 3 UPS02838853 1 20020622 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 STA 540 SHEAR TIE IS CRACKED BETWEEN LONG 35R AND 36. CUT OUT DAMAGE, FABRICATED AND INSTALLED SHEAR TIE REPAIR IAW SRM 53-2-0 FIG 2B. 2 L 7 4 4F RT 4A25 2002090300041 20020903 00041 WP 2002 9 3 UPS02838854 1 20020622 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 STA 540 SHEAR TIE IS CRACKED BETWEEN LONG 31L AND 32L. CUT OUT DAMAGE, FABRICATED AND INSTALLED SHEA R TIE IAW SRM 53-2-0 FIG 2B. 2 L 7 4 4F RT 4A25 2002090300042 20020903 00042 WP 2002 9 3 UPS02838855 1 20020621 A 5320 575072673 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 STA 90 INTERCOSTAL IS CRACKED AT LONG 33L. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5750 726 AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2002090300043 20020903 00043 WP 2002 9 3 UPS02838856 1 20020621 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 STA 90 INTERCOSTAL IS CRACKED AT LONG 33R. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 575 0726, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002090300044 20020903 00044 WP 2002 9 3 UPS02838857 1 20020620 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 STA 1660 LONG 11R IS CRACKED. STOP DRILLED CRACK NDT VERIFIED CRACK IS TERMINATED AT STOP DRILL, FAB RICATED AND INSTALLED REPAIR STRAP ALONG WITH SKIN DOUBLER AND TRIPLER AND FILLER. 2 L 7 4 4F RT 4A25 2002090300045 20020903 00045 WP 2002 9 3 UPS02838858 1 20020626 A 5711 SPAR CAP DOUG DC8 DC871F 302199D WP RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C2 RIGHT WING REAR SPAR UPPER CAP HAS ELONGATED HOLES BETWEEN XRS 456 AND XA 500. OVERSIZED HOLES, NDT VERIFIED NO CRACKS AT HOLES, FABRICATED AND INSTALLED BUSHINGS IAW 8110-3 APPROVED SAA SK 730-143, AND UPS ENGINEERING F ILE NUMBER DC8-57-20051. 2 L 7 4 4F RT 4A25 2002090300046 20020903 00046 WP 2002 9 3 UPS02838879 1 20020625 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 AT O/B SIDE OF LONG 24L STA 857 POSSIBLE CRACK ON LWR FLAT OF BATHTUB FITTING. NDT TO VERIFY REMOVED LONG 24 AND TRAP FITTING IAW DC8 SRM 51-1-20D. DRILLED LOCATED NEW LONG 24 IAW DC8 SRM 51-1-24. INSTALLED NEW LONGERO N AND TRAP FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002090300047 20020903 00047 WP 2002 9 3 UPS02838880 1 20020626 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 MAIN CABIN LONGERON END FITTING CRACKED AT FS 1690 L26RT. REMOVED FITTING, CLEANED, ALODINED & PRIM ED IAW DC8 SRM 51-1-8. LOCATED, DRILLED & DEBURRED NEW FITTING IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SRM 51-1- 21, 51-1-20D & 51-1-17. 2 L 7 4 4F RT 4A25 2002090300048 20020903 00048 WP 2002 9 3 UPS02838881 1 20020709 A 5320 CLIP DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 FWD PIT STA 380 INTERCOSTAL ATTACH CLIP IS CRACKED L33L. REMOVED CLIP, FABBED CLIP IAW DAC DWG 57507 26-93, AND INSTALLED CLIP IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002090300049 20020903 00049 WP 2002 9 3 UPS02838882 1 20020710 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 R1 AFT LOWER DOOR JAMB CORNER HAS CRACKED EXT FUSELAGE SKIN AT FASTENER HOLE FOUND BY EDDY CURRENT IN SP. CUT OUT DAMAGE, PERFORMED EDDY CURRENT INSP AFTER DAMAGE REMOVAL IAW DOUGLAS NDT SPM 06-10-01.001, NO CRACKS NOTED. FABBED DOUBLER TRIPLER & FILLER IAW DC8 SRM 53-2-0 FIG 14. 2 L 7 4 4F RT 4A25 2002090300050 20020903 00050 WP 2002 9 3 UPS02838890 1 20020724 A 3350 BATTERY DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED TEST BATTERY & RELAY UNIT MM 33-50-01. 2 L 7 4 4F RT 4A25 2002090300051 20020903 00051 WP 2002 9 3 UPS02838896 1 20020724 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:PFLT SHEET METAL CRACK ON PIT 34 FWD UPPER DOOR CUTOUT AREA. A/C FERRIED TO SDF 9146. ACCOMPLISHED PER MANENT REPAIR PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 2002090300052 20020903 00052 WP 2002 9 3 UPS02838900 1 20020702 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 ACP SRM REPAIR TO SEAT TRACK AT POS 2L/3L SUPERLOCK INSTALLED IAW EO M-2550-4101. CUT OUT DAMAGED SE AT TRACK SECTION, FABBED AND DRILLED NEW SEAT TRACK SECTION AND 2 SPLICES IAW DC8 SRM 53-2-3. INSTALLED NEW SEAT TRACK SECTION, SPLICES IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002090300053 20020903 00053 WP 2002 9 3 UPS02838901 1 20020702 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 CABIN STA 70 SEAT TRACK-E IS WORN. BLEND GOUGE IAW SRM 53-2-0 FIG 14. FOUND OUT OF LIMITS IAW 53-2- 3. REMOVED DAMAGED SECTION AND FABBED NEW SEAT TRACK IAW DC8 SRM 53-2-3. INSTALLED NEW SEAT TRACK IAW DC8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2002090300054 20020903 00054 WP 2002 9 3 UPS02838902 1 20020703 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 MAIN CABIN LONG 32R END FITTING CORRODED AT FS 1760. REMOVED CORRODED FITTING IAW DC8 SRM 51-1-21, L OCATED DRILLED DEBURRED NEW FITTING IAW 53-2-0, INSTALLED FITTING IAW DC8 SRM 51-1-21 & 51-1-20D, 51-1-17. 2 L 7 4 4F RT 4A25 2002090300055 20020903 00055 WP 2002 9 3 UPS02838903 1 20020626 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 MAIN CABIN FRAME CORRODED AT FS 1740 BETWEEN L33L TO L33R. REMOVED DAMAGED SECTION OF FRAME AND SPLI CED IN NEW SECTION IAW DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2002090300056 20020903 00056 WP 2002 9 3 UPS02838904 1 20020625 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 AFT CARGO CORRODED INTERCOSTAL STR 35R AT LIGHTENING HOLE STA 1085. REMOVED CORRODED INTERCOSTAL IAW DC8 SRM 51-1-21, FABBED NEW INTERCOSTAL IAW DAC DWG 9758507, INSTALLED INTERCOSTAL IAW 51-1-21. 2 L 7 4 4F RT 4A25 2002090300057 20020903 00057 WP 2002 9 3 UPS02838905 1 20020625 A 5320 CLIP DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 AFT SIDE OF FS 683 WEB LWR CHORD CRACKED BETWEEN LONGERON 30L AND 32L LOCATED BETWEEN WING CENTER SEC TION LWR SURFACE AND FUSELAGE LWR LOBE VIEWED THROUGH REMOVED STRESS PNLS. REMOVED 1 CLIP STA 683 L30L AND 2 CLIP L30L & 31L RCD LOCATED AND DRILLED 2 NEW CLIP IAW DC8 SRM 51-1-24, INSTALLED ALL THREE CLIP IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002090300058 20020903 00058 WP 2002 9 3 UPS02838906 1 20020625 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 AFT PIT AFT SIDE OF Z-FITTING CORRODED AT PREV GROUND AREA. REMOVED CORRODED Z-FITTING, LOCATED DRIL LED NEW FITTING AND FABBED 2 SPLICE REPAIR ANGLES. INSTALLED NEW FITTING AND SPLICE REPAIR ANGLES IAW DC8 SRM 53-2-0 FI G 2D & 51-1-20D. 2 L 7 4 4F RT 4A25 2002090300059 20020903 00059 WP 2002 9 3 UPS02838907 1 20020625 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 AFT PIT STA 1220 AT L27L Z-FITTING CRACK. REMOVED FITTING, FABBED REPAIR ANGLES, LOCATED DRILLED ANG LES & FITTINGS IAW DC8 SRM 53-2-0 FIG 20. INSTALLED FITTING ANGLES IAW DC8 SRM 53-2-0 FIG 20. 2 L 7 4 4F RT 4A25 2002090300060 20020903 00060 WP 2002 9 3 UPS02838908 1 20020627 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 L17L END FITTING CRACKED FS 1769. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002090300061 20020903 00061 WP 2002 9 3 UPS02838909 1 20020627 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 L17R END FITTING CRACKED AT FS 1769. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002090300062 20020903 00062 WP 2002 9 3 UPS02838910 1 20020626 A 5350 FITTING DOUG DC8 DC873F 302199F WP TAILCONE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 TAIL CONE ATTACH FITTING HAS CRACK AT L10L. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002090300063 20020903 00063 NM 2002 9 3 UPS02439188 1 20020816 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C, UPPER DECK BS 560 - 580 LBL 30 SEAT TRACK CROWN FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIM IT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 6. 2 L 7 4 4F A20WE 2002090300064 20020903 00064 NM 2002 9 3 UPS02439189 1 20020818 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C, UPPER DECK BS 670-710 LBL 8 SEAT TRACK FOUND CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 4. 2 L 7 4 4F A20WE 2002090300065 20020903 00065 EA 2002 9 3 CA020821001 1 20020820 A 4920 22853401101 FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COMBUSTER DRAIN BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOUND COMBUSTOR DRAIN FITTING BROKEN ON TWO EXHAUST NOZZLE FAIRINGS DURING "C" CHECK. THIS HAS OCCURED TWICE ON T WO DIFFERENT AIRCRAFT. THE ENGINE SIDE WAS NOT SPECIFIED. INSPECTION OF THE INSIDE OF THE FAIRINGS SUGGESTS THAT UNDRA INED FUEL HAS PRODUCED SMALL FIRES. 2 L 7 2 4F 4 F RT A21EA E15NE 2002090300067 20020903 00067 NM 2002 9 3 CA020821004 1 20020819 A 2910 SHUTTLE VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM STUCK W O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 CA (CAN) DOUBLE HYDRAULIC FAILURE PRIOR TO LANDING. AIRCRAFT STOPPED USING PARKING BRAKE JUST OFF END OF RUNWAY, WITH NO DAMAGE OR INJURY. NR 1 BRAKE UNIT FOUND LEAKING. NR 1 HYDRAULIC SYSTEM SHUTTLE VALVE FOUND STUCK OPEN ALLOWING DOUBLE HYDRAULIC SYSTEM FAILURE. BOTH BRAKE UNITS AND SHUTTLE VALVES REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002090300068 20020903 00068 NM 2002 9 3 UPS02439192 1 20020813 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D - FLOOR SUPPORT FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 4. 2 L 7 4 4F A20WE 2002090300069 20020903 00069 EA 2002 9 3 CA020821005 1 20020819 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE PAX DOOR OUT OF ADJUST W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) PASSENGER DOOR WOULD NOT OPEN. ( SECOND OCCURANCE IN TWO WEEKS). DOOR HANDLE LOADS FOUND HIGH. INNER HANDLE TEN SION ADJUSTED. UPPER PIVOTS FOUND GOING SLIGHTLY OVER CENTER. UPPER STOP BOLT ADJUSTED. LATCH CAM TORQUE TUBE ROD SHORTE NED TO ACHIEVE ALIGNMENT OF GREEN WITNESS MARKS. DOOR CYCLED AND TESTED SEVERAL TIMES. 2 L 7 2 4F 4 F RT A21EA E15NE 2002090300070 20020903 00070 NM 2002 9 3 UPS02439193 1 20020814 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D - STA 506 LBL 70 SEAT TRACK FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM LIMIT. O/B SPLICE ANGLE REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002090300072 20020903 00072 EA 2002 9 3 CA020822001 1 20020817 A 4930 WE38304862 NOZZLE HONEYWELL WE38007702 CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE APU FUEL SYS CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA P123 (CAN) DURING ROUTINE MAINTENANCE, APU WOULD NOT START. APU BAY DOORS OPENED AND FUEL LEAK NOTED. FOUND THE FUEL NOZZLE AT THE 6 O'CLOCK POSITION CRACKED. APU INOPERATIVE IAW MEL 49-10-01, AND FUEL NOZZLE ORDERED. FUEL NOZZLE REPLACED AND AIRCRAFT RETURNED IN SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002090300073 20020903 00073 EA 2002 9 3 CA020822002 1 20020819 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W B EMER. DESCENT O OTHER DE DESCENT 1 CA (CAN) RT SIDE WINDOW CRACKED DURING DESCENT AT APPROX 5000FT. THE WINDOW WAS PRE SERVICE BULLETIN. RT WINDOW REPLACED A ND AIRCRAFT RETURNED IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002090300074 20020903 00074 NM 2002 9 3 UPS02439200 1 20020813 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D - BS 260 LBL 30 SEAT TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SE AT TRACK I/B FLANGE REPAIRED AS PER SRM 53-10-05 FIG 16. 2 L 7 4 4F A20WE 2002090300075 20020903 00075 CE 2002 9 3 CA020822006 1 20020808 A 3297 WIRE HARNESS LEAR 45 45LEAR 5170805 CE MLG SQUAT SWITCH FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) LT OUTBOARD SQUAT SWITCH FAILED CAUSING EICAS MESSAGES, T/O TRIM, PRI TRIM, SEC TRIM, LT ENG BUG STUCK. REPLACED S QUAT SWITCH HARNESS 44EN2R 2 L 7 2 4F RT T00008WI 2002090300076 20020903 00076 NM 2002 9 3 UPS02439201 1 20020814 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D - SEAT TRACK FLANGE FOUND CORRODED AT STA 480-500 RBL 85. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002090300077 20020903 00077 EA 2002 9 3 CA020822007 1 20020530 A 2752 853D10012 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAPS FAILED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 CA 13636 (CAN) FLAP FAIL MSG DURING EXTENSION ON DESCENT. FLAPS SHOWED 20 DEG. NO EMERGENCY DECLARED AND LANDED AT GRR. RT NR 3 ACTUATOR FAILED AND FLAP SURFACE TWISTED BADLY. ROAD TRIP SET UP AND MECHANICS DESPATCHED WITH PARTS. PARTS REPLACED IAW AMM. A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002090300078 20020903 00078 NE 2002 9 3 CA020822008 2 20020820 A 7261 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE NACELLE FAILED W G O2 MASK DEPLOYED B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 CA (CAN) DURING APPROACH, CREW NOTED ODOR AND PUFF OF SMOKE THRU VENTS. LAV SMOKE ALARM ILLUMINATED SHORTLY AFTER. ENVIRO NMENTAL SYSTEMS WERE ISOLATED AND THE LANDING COMPLETED WITH OXYGEN SYSTEMS DONNED. DURING FINAL STAGES OF LANDING, OIL PRESSURE WARNING ANNUNCIATOR ILLUMINATED AND VERIFED AT 30 -35 PSI. FOUND BLACK OIL AND HEAVY CARBON DEPOSITS ON ALL IN TERNAL SURFACES. SCAVENGE SCREEN INTAKE PLUGGED SOLID WITH CONTAMINATION. ATTEMPTS TO CLEAN THE SCREEN FAILED AS THE EN GINE CONTINUED TO EXPEL OIL FROM THE INTAKE 'PICOLO' HOLES, INTO THE COMPRESSOR SECTION OF THE ENGINE. ENGINE REPLACED AND SENT IN FOR INVESTIGATION. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002090300079 20020903 00079 EA 2002 9 3 CA020823001 1 20020519 A 2761 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE GROUND SPOILERS FAILED W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CA (CAN) LT INBOARD GROUND SPOILER DEPLOYED WHILE CLIMBING THROUGH 29,000 FT. CLIMB DECREASED AND BUFFET NOTICED. LT INBO ARD GROUND SPOILER SHOWED DEPLOYED AND LT OUTBOARD GROUND SPOILER SHOWED AMBER. MESSAGE CLEARED SHORTLY. MAINTENANCE R EMOVED AND REPLACED SSCU NR 1 AND LT INBOARD GROUND SPOILER ACTUATOR. ALSO ADJUSTED ALL GROUND SPOILER PROX. SENSORS. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002090300080 20020903 00080 NM 2002 9 3 CA020823002 1 20020823 A 3230 1022851 HAND PUMP BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA HYD SYSTEM FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) DURING MAINT, INSPECTORS FOUND ALT GEAR EXTENSION NOT WORKING. CARRIED OUT GEAR CHECKS & DOING ALT RELEASE, AL L FAILED. HAND PUMP WAS NOT BUILDING UP PRESSURE TO LOCK MLG'S. THEY REPLACED SELECTOR VALVE WITH A PRE MOD SUM 4D0134 14. SELECTOR VALVE DUE TO NO STOCK OF POST MOD VALVE. DIDN'T RECTIFY THE PROBLEM, STILL NO HANDPUMP PRESSURE: CHANGED HANDPUMP & THAT SOLVED PROBLEM. THE FOLLOWING OP TEST OF ALT LDG GEAR EXTENSION HYDRAULIC SYS WAS CARRIED OUT SUCCESSFUL . SINCE FLUID FOUND HEAVILY CONTAMINATED, EMERG SYS HAS BEEN BLEED & REFILLED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002090300082 20020903 00082 NM 2002 9 3 UPS02439202 1 20020814 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D - STA 476-480 LBL 32 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. BS 460-510 LBL 32 SEAT TRACK REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002090300083 20020903 00083 NM 2002 9 3 UPS02439203 1 20020816 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C UPPER DECK STA 420-440 BL 0 FLOOR SUPPORT CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOOR SUP PORT REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002090300084 20020903 00084 NM 2002 9 3 UPS02439204 1 20020818 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C UPPER DECK BS 480 BL 0 - RBL 35 FLOORBEAM CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOOR SUP PORT UPPER BEAM REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002090300085 20020903 00085 2002 9 3 VNAA0208020 4 20020812 A 3460 COMPUTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 461PS 3075 DURING TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE CONTROL FAIL MESSAGE AND ABORTED TAKEOFF. WHEN THE FLIGHT TAXIED ON TO THE TAXIWAY, THE MESSAGE CLEARED. THE CREW CALLED MAINTENANCE CONTROL AND WAS ADVISED TO MAKE ANOTHER TAKEOFF ATTEMP T. FLIGHT 4031 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300086 20020903 00086 NM 2002 9 3 VNAA0208021 1 20020813 A 2450 230GC02Y02 PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 426JS 130 31 3038 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERA TIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300087 20020903 00087 NM 2002 9 3 VNAA0208023 1 20020815 A 5300 STRUCTURE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE VIBRATION A VNAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 437JS 3055 DURING CLIMBOUT, THE CREW REPORTED A VIBRATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND PERFORMED A FUNCTIONAL CH ECK FLIGHT WITH THE CREW AND COULD NOT DUPLICATE THE VIBRATION. AFTER THE SATISFACTORY FUNCTIONAL CHECK FLIGHT, THE AIR CRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300088 20020903 00088 NM 2002 9 3 VNAA0208025 1 20020818 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 439JS 16264 953 3057 THE CREW REPORTED THAT THE FIRST ROW OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLAC ED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300089 20020903 00089 NM 2002 9 3 VNAA0208026 1 20020819 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 438JS 16893 350 3056 THE CREW REPORTED THAT THE ROW 4 TO 6 OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLA CED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300090 20020903 00090 NM 2002 9 3 VNAA0208027 1 20020819 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 459PS 14897 122 3070 THE CREW REPORTED THAT THE ROW 6 TO 9 OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLA CED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300091 20020903 00091 NM 2002 9 3 VNAA0208028 1 20020819 A 2843 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 442JS 3060 DURING TAKEOFF, THE CREW RECEIVED A FUEL FEED TEMPERATURE CAS MESSAGE AND ABORTED TAKEOFF. WHEN FLIGHT 4150 CLEARED TH E RUNWAY THE MESSAGE CLEARED. THE CREW CALLED MAINTENANCE CONTROL AND THE DECISION WAS MADE TO TRY ANOTHER TAKEOFF ATTE MPT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300092 20020903 00092 NM 2002 9 3 VNAA0208029 1 20020819 A 2843 1060K SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUEL SYSTEM MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 442JS 17166 3060 DURING TAKEOFF, THE CREW RECEIVED A FUEL FEED TEMPERATURE CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE CONTROL DISPATCH ED DAY MAINTENANCE. MAINTENANCE IN PHL INSPECTED AND REPLACED THE FUEL FEED TEMPERATURE SENSOR IN ACCORDANCE WITH DORNI ER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091700008 20020917 00008 WP 2002 9 17 DHL2002806012 1 20020826 A 2697 WIRE DOUG DC8 DC873F 302199F WP SMOKE DETECTION SHORTED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806DH 46002 SMOKE DET SYS NOT TESTING PROPERLY. FOUND NR 3 SDU AT FAULT, NEW SDU INSTALLED, NO HELP. NR 3 SDU CONNECTOR STOWED SYS TEM OPS CHECK NORMAL. NR 3 SMOKE DETECTOR INOP. PULLED AND STOWED NR 3 SDU CONNECTOR DEFERRED. REMOVED AND REPLACED N R 3 MAIN DECK SMOKE DETECTOR, OPS CHECKS SERVICEABLE. T/S WIRING AND FOUND WIRES C AND D SHORTED TOGETHER BETWEEN SMOK E DET AND COCKPIT. REPAIRED WIRE W242B24 AT POS 3 AND 6 AND WIRE W143C24 AT POS 3. SYS CK OK IAW 26-10-5. 2 L 7 4 4F RT 4A25 2002090300093 20020903 00093 NM 2002 9 3 VNAA0208031 1 20020821 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 460PS 965 131 3061 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 9 TO 12 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK POSITION. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE . 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300094 20020903 00094 EU 2002 9 3 CA020823004 1 20020816 A 7920 5002T27P01 TUBE AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE ENGINE CRACKED W E A ENGINE SHUTDOWN UNSCHED LANDING D J INFLIGHT SEPARATION WARNING INDICATION CL CLIMB 1 CA (CAN) A/C DEPARTED. DURING CLIMB OUT THROUGH FL250, FLT CREW HEARD ABNORMAL SOUND FROM REAR OF A/C. ALL ENGINE PARAMETE RS WERE NORMAL EXCEPT FOR RISE IN EGT. FLT CREW REQUESTED TO RETURN. APPROXIMATELY 30 NAUTICAL MILES FROM LANDING, EN GINE BEGAN TO MAKE ABNORMAL SOUNDS, SECURED ENGINE. A/C LANDED SUCCESSFULLY. CONTRACTED AMO AND ADVISED OF CONDITION OF ENGINE AS DAMAGE TO REAR FAN AREA & EXCESSIVE OIL LEAK. BY REMOVING ENGINE TAIL CONE, IT HAS BEEN OBSERVED THAT AFT OIL PRESSURE LINE TO AFT FAN BEARING NR 5 FOUND CRACKED. ALTHOUGH SERVICE DIFFICULTY REPORT IDENTIFIES CRACKED TUBE ASS Y P/N 5002T27P01, WE SHOULD NOT DISREGARD POSSIBILITY OF BEARING FAILURE. 2 L 7 2 4F 4 F RT A7EU E7EA 2002090300095 20020903 00095 NM 2002 9 3 VNAA0208032 1 20020821 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 434JS 15262 759 3051 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT THE REAR EXIT SIGN WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REP LACED THE EMERGENCY BATTERY AT THE 7LK POSITION. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SE RVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300096 20020903 00096 NM 2002 9 3 VNAA0208033 1 20020821 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 458PS 15230 89 3068 THE CREW REPORTED THAT THE SECOND SECTION OF EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACE D THE EMERGENCY BATTERY AT THE 5LK POSITION. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVIC E. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300097 20020903 00097 EA 2002 9 3 CA020826001 1 20020819 A 2910 CN6272003001 LINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE HYD SYSTEM CRACKED W O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) DURNING FLIGHT, PILOT REPORTED A HYD. SYSTEM NR 1 FAILURE. FLUID AND PRESSURE WENT TO ZERO. AFTER FURTHER INVE STIGATION IT WAS DISCOVERED THAT THE PRESSURE LINE FROM THE EDP WAS THE CAUSE OF THE LOSS OF FLUID. A/C TAT IS 2,110.6 AND TAC IS 1,809.HYD. LINE LOOKS TO BE IN GOOD CONDITION BUT WAS STATED THAT THE FLUID WAS LEAKING OUT FROM THE WELDED AREA ON THE END OF THE LINE. ALSO STATED THAT IT JUST WASN`T LEAKING AT ONE POINT BUT AROUND THE WHOLE WELDED AREA. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002090300098 20020903 00098 NM 2002 9 3 VNAA0208035 1 20020824 A 3244 TIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG VIBRATION A VNAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 438JS 3056 AFTER TAKEOFF, THE CREW REPORTED A SEVERE NOSE GEAR VIBRATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED T HE NOSE WHEEL TIRE ASSEMBLIES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300099 20020903 00099 NE 2002 9 3 CA020826002 2 20020821 A 7261 667486S FITTING BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE GEARBOX LEAKING W E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA (CAN) FLIGHT CREW REPORTED LOSS OF NR 1 ENGINE OIL AND LOW OIL PRESSURE WARNING LIGHT ON FINAL APPROACH. PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED AND NORMAL LANDING CONDUCTED. NO FURTHER INCIDENTS TO REPORT. MAINTENANCE INSPECTION REVE ALED BANJO FITTING ON THE OIL FILTER BYPASS SYSTEM LEAKING. ENGINEERS REPLACED THE NR 1 ENGINE ACCESSORY GEARBOX, S/N:' ON'KF3586, S/N:'OFF'DE5935 AND COMPLETED SYSTEM LEAK CHECK. NO FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE WITH NO FURT HER INCIDENTS TO REPORT. 2 L 7 2 4F 4 F A16WE E2EA 2002090300100 20020903 00100 NM 2002 9 3 CA020826003 1 20020815 A 2121 732591C COOLING FAN BOEING 767 76735H 1385208 NM GE CF6 CF680C2B6F 30025 NE E/E BAY FAILED W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA (CAN) INTERMITTENT LOUD SQUEEL IN FRONT CABIN AND GALLEY WAS FOLLOWED BY MOMENTARY SMOKE IN FLIGHT DECK AND FWD EQUIPMEN T BAY FAN STATUS MESSAGE WITH ASSOCIATED CB POPPING.FORWARD EQUIPMENT COOLING FAN REPLACED AS PER AMM. 2 L 7 2 4F 4 F RT A1NM E13NE 2002090300101 20020903 00101 NM 2002 9 3 VNAA0208036 1 20020824 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 461PS 3075 DURING TAKEOFF, THE CREW RECEIVED A TAKE OFF CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. THE MESSAGE THEN EXTINGUISH ED BY ITSELF AND FLIGHT 4102 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4102 THEN DEPARTED WITH NO FURTHER INCIDEN TS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300102 20020903 00102 NM 2002 9 3 VNAA0208037 1 20020824 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 438JS 12318 42 3056 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING A ROWS 1 TO 6 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPL ACED THE EMERGENCY BATTERIES AT THE 4LK AND 5LK POSITIONS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERA TIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300103 20020903 00103 NM 2002 9 3 VNAA0208038 1 20020824 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 457PS 13693 3048 THE CREW REPORTED THAT THE EMERGENCY BATTERY AT THE 4LK POSITION NEEDS REPLACED. MAINTENANCE INSPECTED AND REPLACED TH E EMERGENCY BATTERY AT THE 4LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WER E PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300104 20020903 00104 NM 2002 9 3 VNAA0208040 1 20020825 A 3234 7178011 CONTROL HANDLE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 462PS 9184 3084 AFTER TAKEOFF, THE CREW COULD NOT GET THE LANDING GEAR TO RETRACT. FLIGHT 4141 RETURNED TO PIT AND LANDED SAFELY. MAIN TENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. O PERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300105 20020903 00105 NM 2002 9 3 VNAA0208041 1 20020827 A 3240 AC69965 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MLG FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 458PS 12288 3068 THE CREW REPORTED A EMERGENCY PARKING BRAKE CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS R ELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300106 20020903 00106 NM 2002 9 3 VNAA0208043 1 20020829 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 470PS 17453 3006 THE CREW REPORTED THAT THE EMERGENCY LIGHTING A ROW 9 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIR CRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300107 20020903 00107 NM 2002 9 3 VNAA0208044 1 20020829 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 457PS 14808 26 3048 THE CREW REPORTED THAT THE LAST TWO EMERGENCY FLOOR TRACK LIGHTS WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLA CED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002090300108 20020903 00108 WP 2002 9 3 DHL2002801017 1 20020902 A 2611 BULB DOUG DC8 DC873F 302199F WP A DHLA O OTHER J L WARNING INDICATION NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 1) #7 MAIN DECK CARGO SMOKE DET. WONT TEST2) ENTERED ON DMI #10282 IAW DHL MEL 26-6 (1) PLACARD INSTALLED G.MARTIN 21 1513) REF DMI #10282 #7 MAIN DECK CARGO SMOKE DET. WON'T TEST.4) RE-LAMPED TEST BULB AND OP CHECKS GOOD IAW DACO M/M 2 6-00. DMI 10282 CLEARED, PLACARD REMOVED. 2 L 7 4 4F RT 4A25 2002090300110 20020903 00110 NE 2002 9 3 WRNA200200002 2 20020725 A 7321 FUEL CONTROL AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 2 ENGINE OUT OF ADJUST A WRNA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 821SC 211 DURING CLIMB NR 2 ENGINE BLEED VALVE REG FAULT LIGHT CAME ON. TEMP INCREASE TO 230 DEGREES AND TEMP HI LIGHT CAME ON FO LLOWED BY A/C PACK FAULT LIGHT. UNABLE TO CONTROL PRESSURIZATION DUE TO NR 1 BLEED VALVE CURRENTLY ON MEL (LOCKED OUT) NR 2 HP BLEED FAULT LIGHT CAME ON. AIRCRAFT RETURNED TO AIRPORT. FUEL DUMP PROCEDURES USED FOR LANDING WEIGHT AND AIRC RAFT RETURNED WITH NORMAL LANDING. CLEARED BY ADJUSTING SPECIFIC GRAVITY PER 73-21-02. RUN UP CHECKS COMPLIED WITH, AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A35EU E23EA 2002090300111 20020903 00111 2002 9 3 WRNA200200003 4 20020807 A 3418 STALL WARNING AIRBUS 300 A300B4203 3930306 EU COCKPIT ACTIVATED A WRNA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 05 501TR 53 IN CLIMBOUT, CLEAN CONFIGURATION ABOVE 250 KTS VIOLENT SHUDDER WITH STALL WARNING AND STICK SHAKER. A/C WT 335 ALT FL 2 00, ENGINE PARAMETERS AND FLT CONTROL INDICATION NORMAL. SYS PARAMETERS NORMAL. AIRCRAFT RETURNED TO AIRPORT. PERFORM OP'S CK OF AOA SENSOR'S, NO FAULT FOUND. INSP AOA SENSORS, NO FAULT FOUND. RAN ENGINES AT PART PWR, NO VIBRATIONS NOT ED. INSP ENGINE FAN BLADES, NO FAULT FOUND. CHECKED FLAP, SLAT AND FLT CONTROL MOVEMENT AND INSP FLAP, SLATS, AND FLT CONTROLS, NO DEFECTS NOTED ALL IAW 27-10-00, 27-20-00 AND 27-50-00. AIRCRAFT RETURNED TO SERVICE. TEST FLT PERFORMED A ND OPERATED SATISFACTORY. 2 L 7 2 4F RT A35EU 2002090300112 20020903 00112 EU 2002 9 3 YENA200219 1 20020805 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU BLUE SYSTEM LACK OF LUBE A YENA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 517JB 1327 AT JFK FLT 17, JFK TO FLL, ON TAKEOFF, B-HYDRAULIC SYSTEM LOW ECAM MESSAGE. ABORTED TAKEOFF AT APPROX 75 KTS, RETURNED TO GATE. FOUND BLUE SYSTEM LOW, FOUND NO EVIDENCE OF LEAK. SERVICED TO FULL, OPERATED ALL FLIGHT CONTROLS, UNABLE TO F IND LEAK AS PER AMM 27-50-00. LEAK CHECK GOOD, NO FAULT NOTED, OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2002090300113 20020903 00113 EU 2002 9 3 YENA200223 1 20020810 A 3350 CONNECTOR AIRBUS 320 A320232 3930326 EU CABIN NOT SEATED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 505JB 1173 DURING EMERGENCY LIGHT TEST, PER WEEKLY CHECK DOC, STEP 5&7 EMERGENCY TEST FAILED. RESET CANNON PLUG ON ESPU FIN 10WL. PERFORMED OPS CK OF EMERGENCY LIGHT SYSTEM AS PER AMM 33-51-00. OPS CKS GOOD. 2 L 7 2 4F RT A28NM 2002090300114 20020903 00114 NM 2002 9 3 ZW0A0208401 1 20020811 A 3397 WIRE BOEING 767 767300 1385204 NM CABIN BROKEN A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 691LF 25137 THE EGRESS LIGHTS WERE INOPERATIVE ON THE LEFT SIDE OF THE CABIN AT SECTION 5-6 AND RT SIDE SECTION 3-6. FOUND BROKEN W IRE AND SPLICED SAME. 2 L 7 2 4F RT A1NM 2002090300115 20020903 00115 NM 2002 9 3 ZW0A0208402 1 20020811 A 5313 LONGERON BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 423TW 55090 LONGERON 24L WAS DAMAGED AT STA 136. REPAIRED LONGERON 24L PER SRM 53-00-05, FIG 201. 2 L 7 2 4F TR A6WE 2002090300116 20020903 00116 WP 2002 9 3 ZW0A0208601 1 20020812 A 2750 CONTROL HANDLE DOUG DC9 DC983 3022083 WP COCKPIT DIRTY A ZW0A A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 13 978TW 53628 THE FLAP/SLAT SELECTOR HANDLE WAS DIFFICULT TO MOVE. FLIGHT RETURNED TO STL. FOUND THE HANDLE MECHANISM WAS DIRTY. CL EANED AND LUBRICATED THE FLAP/SLAT HANDLE MECHANISM. 2 L 7 2 4F RT A6WE 2002090300117 20020903 00117 NE 2002 9 3 ZW0A0208602 2 20020811 A 7261 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217A 52053 NE RIGHT LEAKING A ZW0A A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 13 9405T 53141 3261 SMOKE APPEARED IN THE CABIN AND COCKPIT. FLIGHT MADE AN UNSCHEDULED LANDING AT ICT. EXTENSIVE CHECKS OF THE WATER SEPA RATOR FILTERS, ENGINE END CAPS, ETC. FOUND NO CAUSE FOR THE SMOKE. THE AIRCRAFT OPERATED TO STL WHERE BOTH ENGINES WER E BORESCOPED PRECAUTIONARY. THE RT ENGINE HAD OIL IN THE EIGHTH STAGE SO THE ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A6WE E9NE 2002090300118 20020903 00118 WP 2002 9 3 ZWOA0207801 1 20020727 A 2913 AS66411LS666 PUMP DOUG DC9 DC983 3022083 WP HYD SYSTEM FAILED A ZW0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 13 978TW 53628 LOST HYDRAULIC PRESSURE FROM NUMBER TWO HYDRAULIC PUMP DUE TO SHEARED SHAFT. REPLACED NUMBER TWO HYDRAULIC PUMP. 2 L 7 2 4F RT A6WE 2002090300119 20020903 00119 NM 2002 9 3 DL777020880 1 20020724 A 3150 WARNING SYSTEM BOEING 777 777232 1385232 NM COCKPIT FALSE ACTIVATION A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 877DA 29739 ON DESCENT PASSING FL270 AFT CARGO HEAT LIGHT CAME ON ALONG WITH THE FOLLOWING STATUS MSG. ELMS P110 PANEL¥ IFE COOLING FAN EQUIPMENT VENT FAN AIR/GND L¥ L AND R RECIRC FAN. T/S PER FIM MAINT MSG FAULT CODE 24-18801. PERFORMED ELMS P110 EU INITIALIZE SELF TEST. TEST PASSED. ALL MSG CLEARED AND SHOWN NOT ACTIVE ON MAT. 2 L 7 2 4F RT T00001SE 2002090300120 20020903 00120 NM 2002 9 3 DLM11020923 1 20020808 A 3610 11501266 COMPUTER DOUG MD11 MD11 3023602 NM PWA 4060 PW4060 52119 NE BLEED AIR MALFUNCTIONED A DALA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 809DE 48480 723923 AIR SYS 02 PRESS LO LIGHT ILLUMINATED IN FLT 5 PSI, FOLLOWED BY AIR SYS 2/3 PRESS LO LIGHTS, RESULTING IN TOTAL PRESSURI ZATION FAILURE. RECOVERED AIR SYS 01/03 IN MANUAL MODE. REVIEWED CFDS, SYS SHOWS NO CURRENT FAULTS. PERF RTS OF ACC, ALL TEST PASSED. PERF RTS OF ESC AND MANIFOLD FAILURE CONTROLLER, ALL TEST PASSED. PERF RTS OC CPC, ALL TEST PASSED. PERF RTS OF PSC. RAN ALL THREE ENGINES AND PERF PNEU CHECK OUT OF ENG BLEED SYS IN MAN/AUTO, ALL ENG PNEU CHECKS GOOD. PSC 02 FAILED PM3 SENSOR. REPLACED 1 PSC, PERF ADJ TEST PER AMM CKS GOOD. PERF 2 PSC, RETURN TO SERVICE. 2 L 7 3 4F 4 F RT A22WE E24NE 2002090300121 20020903 00121 WP 2002 9 3 MWEA020522 1 20020827 A 5313 SBA531887001 INTERCOSTAL DOUG DC9 DC981 3022081 WP STA 465-484 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FOUND 7 CRACKS IN FUSELAGE SKIN BETWEEN LONGERON 29LEFT AND 30. STATION 465-484. -- INSTALLED 5 AND 6 ANGLES TO INTERC OSTAL AND 3 DOUBLER TO SKIN. 2 L 7 2 4F A6WE 2002090300122 20020903 00122 NM 2002 9 3 HNAA0200056 1 20020831 A 2612 VC1165 CLAMP DHAV DHC8 DHC8201 2809001 NM #1 NACELLE DETACHED A HNAA E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 EA 07 997HA 8862 507 DURING TAXI, NUMBER 1 ENGINE FIRE INDICATION, FIRED ONE BOTTLE. INSPECTED AREA, FOUND JET PIPE SEPERATED FROM NUMBER ON E ENGINE. REATTACHED JET PIPE WITH NEW CLAMP AND INSPECTED AREA FOR COLLATERAL DAMAGE, NONE FOUND. FERRIED AIRCRAFT TO ROA. 2 H 7 2 4T RT A13NM 2002090300123 20020903 00123 NM 2002 9 3 UPS02439209 1 20020822 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C, COCKPIT BS 340 RBL 10 - 20 FLOOR BEAM UPPER CHORD CORRODED. CORROSION REMOVED IAW 51-10-01 EXCEED SR M LIMIT 53-10-07 FIG 16. 2 L 7 4 4F A20WE 2002090300124 20020903 00124 NM 2002 9 3 UPS02439210 1 20020816 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C, COCKPIT - BS 340 LBL 100 FLOORBEAM UPPER CHORD FOUND CORRODED. CORROSION REMOVED IAW 51-10-01, CORRO SION BLEND OUT EXCEEDS SRM LIMIT. FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 23. 2 L 7 4 4F A20WE 2002090300125 20020903 00125 NM 2002 9 3 UPS02439211 1 20020817 A 5320 ATTACH ANGLE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C, UPPER DECK BS 420 RIGHT STR S9AR, S8AR AND S6AR FRAME INNER CHORD ATTACH ANGLE FOUND CRACK AS MARKED. UPPER DECK BS 420 RIGHT STR S9AR, S8AR AND S6AR FRAME INNER CHORD ATTACH ANGLES REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002090300126 20020903 00126 NM 2002 9 3 UPS02439224 1 20020813 A 5320 DOUBLER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C, M/D BS 360 S-24A FRAME DOUBLER FOUND CRACKED. M/D BS 360 STR 24AL FRAME DOUBLER REPLACED AS PER SRM 51-10-01 PAGE 8. 2 L 7 4 4F A20WE 2002090300127 20020903 00127 WP 2002 9 3 UPS02839033 1 20020809 A 3350 BATTERY DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS DO NOT STAY ON. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UN IT PER MM 33-50-01, OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2002090300128 20020903 00128 NM 2002 9 3 UPS02439207 1 20020818 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C, UPPER DECK BS 700-710 LBL 28 SEAT TRACK CROWN FOUND CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 6. 2 L 7 4 4F A20WE 2002090300129 20020903 00129 WP 2002 9 3 UPS02839034 1 20020723 A 5720 36433191 STIFFENER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 LEFT WING T/E INBOARD VERTICAL STIFFENER AT FLAP HINGE 98 IS CRACKED AT BOTTOM. REMOVED, FABRICATED, AND INSTALLED STIFFENER IAW DWG 3643320, AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002090300130 20020903 00130 WP 2002 9 3 UPS02839035 1 20020802 A 5541 5656223515 RIB DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 RUDDER RIB CRACKED AT STA ZR 140. REMOVED, FABRICATED, AND REPLACED RIB IAW DWG 5656223 AND SRM 51-1 -21. 2 L 7 4 4F RT 4A25 2002090300131 20020903 00131 WP 2002 9 3 UPS02839036 1 20020802 A 5541 565622317 RIB DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 RUDDER RIB CRACKED STA ZR 135. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 5656223 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002090300132 20020903 00132 WP 2002 9 3 UPS02839037 1 20020803 A 5320 57550583 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 STA 780 LONG 35R END FITTING CRACKED. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 5755058 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002090300133 20020903 00133 WP 2002 9 3 UPS02839038 1 20020724 A 5230 DOOR FRAME DOUG DC8 DC871F 302199D WP CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 CARGO PIT C DOOR CORNER CLIPS CRACKED INSIDE LIGHTENING HOLES FS STA 1170 TO 1210 AT LONG 22R APPROX. FOUND DOOR PAN/FRAME CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED CLIPS, DOUBLERS, AND DOOR PAN SECTION IAW DWG 5894025 AND SRM 52-2-0 FIG 2, 52-4-1. 2 L 7 4 4F RT 4A25 2002090300134 20020903 00134 WP 2002 9 3 UPS02839039 1 20020725 A 5320 37558451N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 STA 1152 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 34L TO 35L. REMOVED AND REPLACED FIT TING IAW DWG 3755845, AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002090300135 20020903 00135 WP 2002 9 3 UPS02839040 1 20020723 A 5320 559799213 GUSSET DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 STA 131 TO 121 AT LBL 45 ANGLE FITTING/GUSSET IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND RE PLACED GUSSET IAW DWG 5597992, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002090300136 20020903 00136 WP 2002 9 3 ABXA020150 1 20020829 A 2530 A061681 BRACKET DOUG DC8 DC863F 302198F WP DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 826AX 46061 HOT CUP CAUSED A BURNING ODOR AND SMOKE FROM PRONGS ON THE HOT CUP. REPLACED HOT CUP AND BRACKET ASSEMBLY. OPS CHECKED G OOD IAW DC-8 MM. 2 L 7 4 4F 4A25 2002090300137 20020903 00137 NM 2002 9 3 ZW0A0209101 1 20020901 A 3350 767 LAMP BOEING 757 757231 1384950 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 720TW 30319 THE AFT CABIN EGRESS AND EXTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED SHORTED BULB IN EXTERIOR EMERGENCY LIGHT AFT OF THE L4 CABIN DOOR. CHECK-C 1-26-01 LAX. --CLOSED-- 2 L 7 2 4F RT A2NM 2002090300139 20020903 00139 EA 2002 9 3 CA020826005 1 20020819 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT FAILED W O OTHER O OTHER CR CRUISE 1 CA (CAN) 1ST OFFICER`S SIDE WINDOW SHATTERED AT FL 330 PRIOR TO DECENT, LATER HEAT AND CAUTION MESSAGE ILLUMINATED. CABIN P RESS/ALT NORMAL AND QRH PROCEDURES CARRIED OUT. F/O'S SIDE WINDOW REPLACED AND LEAK CHECKED AS PER AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002090300140 20020903 00140 WP 2002 9 3 0202771221 1 20020821 A 2530 806740409 COFFEEMAKER DOUG DC10 DC1030 3023501 WP A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 221NW 46579 ENROUTE FROM AMS TO MIA, CREW USED HALON EXTINGUISHER INTO FORWARD GALLEY NBR 1 GALLEY COFFEEMAKER. SMOKE DIMINISHED. FL IGHT DIVERTED TO SNN AND LANDED WITHOUT INCIDENT. REPLACED COFFEEMAKER. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 2002090300141 20020903 00141 NM 2002 9 3 UPS02239165 1 20020814 A 5754 SKIN BOEING 727 72731C 1384011 NM #4 KRUEGAR FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C RIVET PULLED THROUGH ANTI-ICE SKIN AT #4 KRUEGER FLAP AT 8TH BAY O/B SKIN REPAIRED IAW SRM ADDENDU M EO # B727-5750-3082 2 L 7 3 4F A3WE 2002090300142 20020903 00142 NM 2002 9 3 UPS02239166 1 20020814 A 5754 SKIN BOEING 727 72731C 1384011 NM #3 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C #3 LE FLAP ANTI-ICE SKIN CRACKED AT MIDDLE O/B RIVET 3RD BAY FROM O/ B REPAIR CARRIED OUT IAW SRM ADDENDUM EO # B727-5750-3082 2 L 7 3 4F A3WE 2002090300143 20020903 00143 NM 2002 9 3 UPS02239167 1 20020813 A 5310 DOUBLER BOEING 727 72731C 1384011 NM BS 269.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C SUSPECT CRACK AT FASTNER BESIDE REPAIR AT NLG WHEEL WELL LEFT FWD PR ESS WEB AT BS 269.5 REPAIR DO UBLER REMOVED IAW SRM 51-30-2 NDT CARRIED OUT CRACK CONFIRM ED & END OF CRACK MARKED. DOUBLER AND FILLERS FABRICATED AND INSTALL ED IAW SRM 51-40-2 FIG 2 2 L 7 3 4F A3WE 2002090300144 20020903 00144 NM 2002 9 3 UPS02239168 1 20020814 A 5754 SKIN BOEING 727 72731C 1384011 NM NO.4 KRUGER FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C CRACK IN ANTI-ICE SKIN AT 5TH BAY O/B ON NO.4 KRUEGER FLAP. ANTI-ICE SKIN FOUND TO BE OUT OF LIMIT S IAW SRM ADDENDIUM EO NO. B72 7-5750-3082-D. ANTI ICE SKIN REPLACED IAW DRAWING NO.65-16225 + SRM 51-30-02. 2 L 7 3 4F A3WE 2002090300146 20020903 00146 NM 2002 9 3 AWXA200200853 1 20020828 A 5230 65479532 SKIN BOEING 737 7373B7 1384580 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON LOWER SECTION OF INNER SKIN ON AFT CARGO DOOR 18" FROM FO RWARD EDGE AT INSULATION BLANKET RETAINER SNAP BS 815, STR 23 R/H. MAINTENANCE CUTOUT CORRODED SECTION OF SKIN, FABRICAT ED A REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13, PG. 1-5, FIG. 1. 2 L 7 2 4F RT A16WE 2002090300147 20020903 00147 NM 2002 9 3 AWXA200200854 1 20020825 A 5230 65917001053 FRAME BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON AFT CARGO DOOR FORWARD UPPER FRAME BETWEEN THE 3RD AND 4 TH STOP FITTINGS, BS 802, RBL 46. MAINTENANCE REMOVED AFT CARGO DOOR FORWARD UPPER FRAME, FABRICATED A NEW SECTION OF FR AME, AND INSTALLED REPAIR IAW SRM 52-30-02, PG. 106, FIG. 101, SRM 51-40-02, PG. 2-4, & 10, AND SRM 51-10-02, PG. 12, 15 -16. 2 L 7 2 4F RT A16WE 2002090300148 20020903 00148 NM 2002 9 3 AWXA200200855 1 20020812 A 5230 65917001050 FRAME BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK A 3/4" CRACK WAS FOUND ON AFT CARGO DOOR FORWARD LOWER FRAME BETWEEN THE 1ST AND 2ND STOP FITTINGS, BS 802, RBL 42. MAINTENANCE REMOVED AFT CARGO DOOR FORWARD LOWER FRAME, FABRICATED A NEW SECTION OF FRAME, AND INSTALLED REPAIR IAW SRM 52-30-02, PG. 106, FIG. 101, SRM 51-40-02, PG. 2-4, & 10, AND SRM 51-10-02, PG. 12, 15-16. 2 L 7 2 4F RT A16WE 2002090300149 20020903 00149 NM 2002 9 3 AWXA200200856 1 20020815 A 5412 313A1355213 ATTACH ANGLE BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 0 0 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK 2 EACH CRACKS WERE FOUND ON ATTACH ANGLES OF #1 PYLON, JUST AFT OF LOWER HEATSHI ELD BLANKET. MAINTENANCE REMOVED CRACKED ATTACH ANGLES JUST AFT OF LOWER HEATSHIELD BLANKET, FABRICATED 2 EACH REPLACEME NT ATTACH ANGLES, AND INSTALLED REPAIR PARTS IAW AWA E.R. 03-5400-02241-TB1. 2 L 7 2 4F RT A16WE 2003012200100 20030122 00100 NE 2003 1 22 AWXA200200774 2 20020818 A 7230 V2524A5 BEARING AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 2 ENGINE FAILED A AWXA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 28 822AW 5839 1410 V10888 STL - DIVERSION - FLT 0695 - EN ROUTE FROM CMH TO LAX THE NR 2 ENGINE COMPRESSOR STALLED TWO TIMES AT FL 370, EGT RED LI NED AND OIL PRESSURE PEAKED AT 330 PSI THEN SLOWLY DROPPED TO -0- PSI, SHUTDOWN ENGINE PER ECAM INSTRUCTIONS AND DIVERTE D TO STL. ENGINE IS BEING REPLACED. ENGINE REPLACED IAW T/C R5M71302 AND F5M71301, OPERATIONAL CHECK WAS GOOD. VENDOR TEARDOWN INSPECTION OF ENGINE CONFIRMED FAILURE OF ENGINE. FAILURE DUE TO FRACTURED OUTER RACE OF NR 3 BEARING, AND NR 3 BEARING FAILURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2002090300150 20020903 00150 NM 2002 9 3 02090301 1 20020901 A 2780 114N300220 SLAT BOEING BOEING 757 757236 1384971 NM DELAMINATED A N8TA A UNSCHED LANDING O OTHER TO TAKEOFF 1 WP 19 506NA 33959 24771 skin delamination and honeycomb missing trailing edge of slat inboard right wing. An uneventful landing was accomplished . Further investigation revealed delamination of fixed leading edge wing panel (aft of #6 leading edge slat) approx. 10' X24", and hole in upper L/H corner of most I/B fixed panel approx. 1 1/4" X 3/4", thru panel. Aircraft was inspected for ferry flight and transported to repair station 2 L 7 2 4F RT A2NM 2002090300151 20020903 00151 NM 2002 9 3 S02832022 1 20020605 A 3200 LANDING GEAR BOEING 737 737800* NM CFMINT CFM56 CFM567B26US NE RH MAIN GEAR W SAJF O OTHER O OTHER DE DESCENT 1 WP 03 21011464 30173 B18612 DRG APPR RH GEAR READ LT ILLUM. WHILE L/G HANDLE DOWN. GND CK FND RH L/G COULD NOT FULL DOWN AND LOCKED. RECYCLIN G L/G HANDLE SUSPECTED RH L/G RET ACT INTERNAL LEAKS. BENCH CH RH RET ACT CONFIRMED INTERNAL. LEAKAGE OVER LIMIT. PER MM 32-32-11 RPLD RET ACT. PER MM 32-33-00 MAIN GR EXT & RET TESTED NML.C/A:1.PER CMM 32-32-37 INTERNAL LEAKAGE TEST. RECYC LING THE INTERNAL LEAKAGE TEST FND LEAKS OCCURRED DRG EXT & NO LEAKS FOR RET. 2. THE ROOT CAUSE IS AN ONE-WAY LEAKAGE UN DER EXT, WHICH SUGGESTS AN INTERIOR VALVE/SEAL FAILURE. 3.THIS FIRST OCCURRENCE IS AN ISOLATED CASE, AND THE ACT RELIABI LITY IS COVERED BY AMP 32-215-01/-02 OF F2 CK FOR MLG EXT SYS. 4.THE WARRANTY REMEDY WAS CLAIMED. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002090400001 20020904 00001 EU 2002 9 4 CA020826006 1 20020820 A 3230 664700500A4D CONTROL UNIT AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE MLG FAILED W O OTHER J WARNING INDICATION CL CLIMB 1 CA (CAN) LDG LGCIU 2 FAULT AFTER GEAR SELECTED UP AND DOORS CLOSED (APPROX 1000 AGL0. TWO LOUD THUMPS HEARED AND FELT ON CO CKPIT FLOOR. ECAM CARRIED OUT MESSAGE CLEARED AND LATER RETURNED. CHANGED NR 2 LGCIU PER AMM. 2 L 7 2 4F 4 F RT A28NM E29NE 2002090400002 20020904 00002 NE 2002 9 4 CA020826007 2 20020816 A 7321 7436024 FUEL CONTROL BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED W O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION LD LANDING 1 CA (CAN) ON LANDING ENGINE 1 AND 2 ONLY GO INTO IDLE REVERSE. UNABLE TO PULL ANY REVERSE POWER. NR 1 ENGINE FCU REPLACED AN D CHECKED SERVICEABLE AS PER AMM. 2 L 7 2 4F 4 F A16WE E2EA 2002090400004 20020904 00004 EA 2002 9 4 CA020827001 1 20020822 A 2730 8220260001 BOLT 6225027101 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SERVO MOUNT SHEARED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA D38T (CAN) ON FINAL APPROACH FOR LANDING, CAPTAIN REPORTED THAT HIS YOKE STUCK AT ABOUT MID-TRAVEL & WAS UNABLE TO MOVE IT I N BOTH DIRECTIONS. CAPTAIN TRIED TO YANK YOKE BACK IN ATTEMPT TO FREE IT, PROCESS THE STICK SHAKER CAME ON. THE CREW FINALLY SUCCEEDED TO LAND AIRCRFAT WITHOUT INCIDENT. WITH A/C ON GROUND, EXTENSIVE TROUBLESHOOTING CARRIED OUT ON ELEV ATOR SYSTEM. MAINT UNABLE TO DUPLICATE YOKE BEING STUCK AT ANY POSSITION. 2 L 7 2 4F 4 F RT A21EA E15NE 2002090400005 20020904 00005 EA 2002 9 4 CA020827005 1 20020805 A 2710 MIXER BOX CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE AILERONS STIFF W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 17839 17839 (CAN) WHILE EN-ROUTE THE FLIGHT CREW EXPERIENCED AILERON CONTROL STIFFNESS & JAM. THE CREW DECLARED AN EMERGENCY AND LA NDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT TOOK OFF IN HEAVY RAIN AND STANDING WATER ON THE RUNWAY. LT AILERON CABLE SYSTEM WAS INSPECTED. THE LT AILERON MIXER ASSY. AND RT AILERON MIXER ASSY. WHERE FOUND TO HAVE SOME RESISTANCE IN THE ROTATING MOVEMENT SO BOTH ASSY WHERE REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002090400006 20020904 00006 EA 2002 9 4 CA020828001 1 20020822 A 2910 MM67075293001 LINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE HYD SYSTEM CRACKED W D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) LOSS OF PRESSURE ON HYDRAULIC SYSTEM NR 2. HYDRAULIC LEAK LOCATED IN AFT EQUIPMENT BAY ONE DP NR 2 PRESSURE LINE T O PRESSURE MANIFOLD. FOUND LINE CRACKED. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002090400007 20020904 00007 CE 2002 9 4 CA020828006 1 20020809 A 2913 710501 MOTOR BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60 52043 NE HYD PACK FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) ELECTRIC MOTOR ON HYDRAULIC PACK - DRAWS TOO MUCH AMPENAGE. THE SYSTEM IS PROTECTED BY A 60 AMP CIRCUIT BREAKER. T HIS ASSY IS OPERATING AT BELOW OR AT THE CIRCUIT BREAKER CAPACITY. THE CB TRIPPED AND THE GEAR WOULD NOT EXTEND. GEAR HA D TO BE HAND PUMPED DOWN. 2 L 7 2 4T 4 T A24CE E4EA 2002090400008 20020904 00008 CE 2002 9 4 CA020828010 1 20020821 A 2842 509215821 GASKET BEECH B300 B300B350C CE PWA PT6 PT6A60A 52043 NE FUEL QTY PROBE SPLIT W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA (CAN) A/C RETURNED SHORTLY AFTER DEPARTURE WITH FUEL LEAK IN LT NACELLE AREA. ON REMOVAL OF TOP COVER, MECHANIC FOUND FU EL STREAMING FROM NACELLE FUEL QUANTITY PROBE FLANGE AREA. TANK DRAINED & PROBE REMOVED. GASKET WHICH HAD BEEN REPLACED PREVIOUS DAY FOUND TO BE SPILT. A/C HAD BEEN SERVICED WITH FUEL TO LEAK CHECK TANK AFTER REPLACING GASKET, MECHANIC RE LIED ONLY ON GRAVITY FEEDTO FILL IT. COMPLETELY FILLING NACELLE TANK REQUIRES RUNNING ENGINE TO PROVIDE FUEL FLOW TO JET PUMP WHICH KEEPS TANK FULL. ENGINES WERE NOT RUN UNTIL DEPARTURE FLT. PASSENGER NOTICED LEAK IN FLT & REPORTED IT TO P ILOTS. 2 L 7 2 4T 4 T RT A24CE E4EA 2002090400011 20020904 00011 WP 2002 9 4 CA020829012 1 20020625 A 2910 LINE VICKERS PF143911252G DOUG DC4 C54EDC 3021528 WP PWA R2000 R20004 52023 NE HYD PUMP RUPTURED W E D ENGINE SHUTDOWN RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA X233142 (CAN) DURING TAXI THE FLIGHT CREW NOTICED A LOSS IN HYDRAULIC PRESSURE. FLUID WAS ADDED WITH NO EFFECT. THE PILOT NOTICE D A HYDRAULIC LEAK FROM NR 2 ENGINE. THE ENGINE WAS THEN SHUTDOWN. THE PILOT DECIDED TO RETURN AND PARK. AT THIS TIME MA INTENANCE WAS CONTACTED AND NOTICED THAT THE PRESSURE LINE FROM THE HYDRAULIC PUMP HAD RUPTURED. 2 L 7 4 4R 4 R A762 5E5 2002090400014 20020904 00014 2002 9 4 MEX2002264 4 20020813 A 3418 COMPUTER DOUG MD88 MD88 3023688 NM STALL WARNING FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 23 162PL 49765 AIRCRAFT RETURNED TO PLATFORM DUE TO AUTO SLAT FAIL LIGHT ON. IN THE EOAP APPEARED A MESSAGE OF AUTO SLAT FAIL. PERFOR MED A BITE CHECK TO THE STALL COMPUTERS, BOTH OF THEM RECORDED THE SAME FAILURE. AIRCRAFT WAS SHUT DOWN TO DISCONNECT B OTH AUTO-ACTURATORS AND RESET COMPUTERS. IAW MM. TEST, OK. 2 L 7 2 4F RT A6WE 2002090400015 20020904 00015 NM 2002 9 4 MEX2002266 1 20020814 A 2612 3460001321 WARNING SYSTEM BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE RT ENGINE ACTIVATED W ASMF F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 SW 23 806AM 26273 AT START OF RT ENGINE, ALL THE FIRE ALARMS ACTIVATED. FUEL CONTROL WAS DISCONNECTED AND MASTER WARNING WAS ADJUSTED, CR EW REQUESTED TO PERFORM A VISUAL INSPECTION TO CONFIRM FIRE PRESENCE. FIRE HANDLE WAS PULLED AND FIRE ALARM CONTINUED A FTER 30 SEC. THE FIRST EXTINGUISHER BOTTLE WAS DISCHARGED, AFTER ONE MINUTE THE ENGINE STARTER WAS SELECTED ON AUTOMAT IC MODE, AFTER 20 SEC. THE SECOND BOTTLE WAS DISCHARGED AND THE FIRE ALARMS STOPPED. THE RIGHT FIRE LOOP SYSTEM WAS CH ECKED IAW FIM, TEST OK, EXTINGUISHER BOTTLES WERE REPLACED IAW MM, TESTS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2002090400016 20020904 00016 WP 2002 9 4 MEX2002268 1 20020818 A 2131 CONTROLLER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 23 1003X 48067 AIRCRAFT MADE A TECHNICAL STOP IN TRC DUE TO PRESSURIZATION TROUBLES. CABIN PRESSURE CONTROLLER WAS RESEATED, TESTS OK. 2 L 7 2 4F 4 F A6WE E2EA 2002090400017 20020904 00017 EU 2002 9 4 3W2324 1 20020807 A 6410 355A12004008 BLADE SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE TAIL ROTOR CRACKED E XCHA K NONE O OTHER IN INSP/MAINT 1 AL 05 6080D 686 2054 TAIL ROTOR BLADE ASSEMBLY HAS CRACK IN SKIN. ORDER NEW TAIL ROTOR BLADE. 1 G 7 1 3U 3 U H9EU E19EU 2002090400018 20020904 00018 NM 2002 9 4 GFV2002F00000 1 20020815 A 7810 369D28630501 DUCT DOUG 600N 600N 3027377 NM ALLSN 250C 250C47B GL ENGINE EXHAUST CRACKED B GFVR K NONE O OTHER IN INSP/MAINT 1 NM 02 613BP 286 RN045 EXHAUST DUCT CONTINUALLY CRACKS FROM THE FLANGE, RUNNING TO THE END OR OUTLET OF THE DUCT. DUCT ALSO EXHIBITS BLUING FR OM EXCESS HEAT. 1 G 7 1 3U 3 U NC H3WE E1GL 2002090400019 20020904 00019 EU 2002 9 4 KBMA115445 1 20020825 A 2797 350A31185100 BONDING JUMPER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ELECTRICAL WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 345SH 1841 3345 BONDING BRAID WORN, BEYOND LIMITS. (BROKEN) REPLACED WITH NEW BONDING BRAID. 1 G 7 1 3U 3 U H9EU E19EU 2002090400020 20020904 00020 EU 2002 9 4 KBMA115446 1 20020824 A 6730 SEAL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE LT LATERAL SERVO LEAKING E KBMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 313LV 1732 3296 LEFT LATERAL SERVO WAS LEAKING FROM SHAFT SEAL. REPLACED WITH SERVICEABLE SERVO. 1 G 7 1 3U 3 U H9EU E19EU 2002090400021 20020904 00021 SW 2002 9 4 KBMA115447 1 20020825 A 7714 206075681105 INDICATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL DUAL TACH FLUCTUATES E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 73DP 12575 2513 TACH NEEDLE FLUCTUATES BETWEEN 2 PERCENT TO 15 PERCENT WHILE AT GROUND IDLE. (DUAL TACH, NR 2 SIDE) REPLACED TACH WITH OVERHAULED UNIT. (INDICATOR) 1 G 7 1 3U 3 U H2SW E4CE 2002090400022 20020904 00022 EU 2002 9 4 KBMA115448 1 20020826 A 7921 95092 FAN SNIAS 350 AS350BA 8680817 EU OIL COOLER BINDING E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 558 2957 OIL COOLER FAN IS BINDING AND TURNS ROUGH. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2002090400023 20020904 00023 NE 2002 9 4 KBMA115449 2 20020826 A 7321 0164248850 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE LEAKING E KBMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 313LV 1730 3296 DECEL LEAKING CONTINUOUSLY. REPLACED FUEL CONTROL. 1 G 7 1 3U 3 U H9EU E19EU 2002090400024 20020904 00024 SW 2002 9 4 KBMA115451 1 20020826 A 7714 8DJ81WBS4 INDICATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL COCKPIT MALFUNCTIONED E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 667JM 23 3444 GAS PRODUCER GAUGE BACKLIGHTING, INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U H2SW E4CE 2002090400025 20020904 00025 EU 2002 9 4 KBMA115452 1 20020827 A 2930 DSQ201 SWITCH SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE HYD TEST STICKING E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 345SH 1849 3345 HYDRAULIC TEST SWITCH IS STICKY. REPLACED SWITCH WITH NEW. 1 G 7 1 3U 3 U H9EU E19EU 2002090400026 20020904 00026 EU 2002 9 4 KBMA115453 1 20020827 A 2420 350A08291500 ECU SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE GENERATOR BURNED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 9461 1864 GENERATOR INOPERATIVE. (REX RELAY SOCKET BURNED) REPLACED MASTER ELECTRICAL BOX WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002090400027 20020904 00027 2002 9 4 KBMA115454 4 20020828 A 3422 103002201 GYRO SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT ERRATIC E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 9467 1864 DIGITIAL GYRO DOES NOT HOLD READING DURING TURNS. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002090400028 20020904 00028 EU 2002 9 4 KBMA115455 1 20020828 A 7921 9691 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE OIL COOLER INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 270SH 300 1864 OIL COOLER MOTOR INOPERATIVE. REPLACED OIL COOLER MOTOR. 1 G 7 1 3U 3 U NC H9EU E19EU 2002090400029 20020904 00029 EU 2002 9 4 KBMA115476 1 20020822 A 5270 SP381200 SWITCH SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE PAX DOOR SHORTED E KBMA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 19 345SH 1831 3345 DOOR LIGHT FLICKERS CONSTANTLY IN CRUISE FLIGHT. INSTALLED NEW SWITCH. 1 G 7 1 3U 3 U H9EU E19EU 2002090400030 20020904 00030 NE 2002 9 4 KBMA119506 2 20020808 A 7421 0307048520 BRACKET SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE IGNITER CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 1188P 11699 2347 ENGINE IGNITER SUPPORT BRACKET CRACKED. REPLACED WITH NEW BRACKET. 1 G 7 1 3U 3 U NC H9EU E19EU 2002090400031 20020904 00031 EU 2002 9 4 KBMA119507 1 20020808 A 6420 350A33214501 LINK SNIAS 350 AS350BA 8680817 EU TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 1188P 1128 2347 TAIL ROTOR PITCH CONTROL LINKS WORN. REPLACED WITH SERVICE LINKS. 1 G 7 1 3U NC H9EU 2002090400032 20020904 00032 2002 9 4 KBMA119515 4 20020817 A 3422 RCA15BK1 GYRO SNIAS 350 AS350B1 8680811 EU COCKPIT INOPERATIVE A KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 53SH 7 2009 DIRECTIONAL GYRO, INOPERATIVE. FLAG WILL NOT GO AWAY. REPLACED WITH SERVICEABLE DIRECTIONAL GYRO. 1 G 7 1 3U H9EU 2002090400033 20020904 00033 EU 2002 9 4 KBMA119516 1 20020817 A 2400 102149 METER SNIAS 350 AS350B1 8680811 EU COCKPIT MALFUNCTIONED E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 53SH 2009 HOUR METER STARTS COUNTING WHEN BATTERY POWER IS APPLIED. REPLACED HOUR METER WITH NEW UNIT. 1 G 7 1 3U H9EU 2002090400034 20020904 00034 EU 2002 9 4 KBMA119517 1 20020816 A 2110 BRUSHES SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE EVAP MOTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 1696 3296 FORWARD EVAPORATOR MOTOR BRUSHES ARE WORN AND HOLDER IS BROKEN. REPLACED WITH NEW MOTOR. 1 G 7 1 3U 3 U H9EU E19EU 2002090400035 20020904 00035 EU 2002 9 4 KBMA119518 1 20020815 A 7160 350A54108421 SEAL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE AIR INTAKE WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 3882 3141 AIR INTAKE SEAL IS WORN. REPLACED WITH NEW SEAL. 1 G 7 1 3U 3 U H9EU E19EU 2002090400036 20020904 00036 EU 2002 9 4 KBMA119519 1 20020815 A 6720 350A27119120 BUSHING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE T/R CONTROL WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 3882 3141 TAIL ROTOR CONTROL TUBE BUSHINGS ARE WORN. REPLACED WITH NEW BUSHINGS. 1 G 7 1 3U 3 U H9EU E19EU 2002090400037 20020904 00037 EU 2002 9 4 KBMA119520 1 20020815 A 6510 704A33698027 SLEEVE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE DRIVESHAFT WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 3141 DRIVESHAFT BEARING INNER SLEEVES ARE WORN AND BRITTLE. REPLACED SLEEVES WITH NEW SLEEVES. 1 G 7 1 3U 3 U H9EU E19EU 2002090400038 20020904 00038 EU 2002 9 4 KBMA119536 1 20020810 A 2121 0500847 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE COOLING FAN INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 350SH 1279 2957 FAN MOTOR INOPERATIVE, POPS CIRCUIT BREAKER. REPLACED WITH NEW MOTOR. 1 G 7 1 3U 3 U NC H9EU E19EU 2002090400039 20020904 00039 EU 2002 9 4 KBMA119541 1 20020813 A 2121 0500847 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE COOLING FAN FAULTY E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 270SH 113 1864 MOTOR MAKING ODD NOISE AND POPS CIRCUIT BREAKER. REPLACED MOTOR WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002090400040 20020904 00040 EU 2002 9 4 KBMA119549 1 20020819 A 2121 420800006 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE A/C FAN INOPERATIVE A KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 230SH 2337 AIR CONDITIONER INOPERATIVE, NO AIR BLOWING. REPLACE MOTOR WITH SERVICE MOTOR. 1 G 7 1 3U 3 U NC H9EU E19EU 2002090400041 20020904 00041 EU 2002 9 4 KBMA119550 1 20020819 A 3340 A490ATS STROBE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE EXTERIOR INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 345SH 1814 3345 ANTI COLLISION LIGHT INOPERATIVE. REPLACE WITH SERVICEABLE STROBE BOX. 1 G 7 1 3U 3 U H9EU E19EU 2002090400042 20020904 00042 EU 2002 9 4 KBMA119551 1 20020818 A 6220 BUSHING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE STARFLEX DEBONDED E KBMA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 19 345SH 1811 M1256 3345 AIRCRAFT HAS VERTICAL VIBRATION. FOUND BUSHINGS DEBONDED. REPLACE WITH SERVICE STARFLEX. 1 G 7 1 3U 3 U H9EU E19EU 2002090400043 20020904 00043 EU 2002 9 4 KBMA119552 1 20020818 A 6220 BUSHING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE STARFLEX DEBONDED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 345SH 3345 AIRCRAFT HAS VERTICAL VIBRATION FOUND BUSHINGS, DEBONDED. REPLACED STARFLEX AND BALL JOINTS. 1 G 7 1 3U 3 U H9EU E19EU 2002090400050 20020904 00050 CE 2002 9 4 GLAB2002120 1 20020813 A 3150 PIN BEECH 1900 1900D 1154162 CE WARNING SYS DISCONNECTED A GLBA O OTHER N FALSE WARNING CR CRUISE 1 NM 03 228GL UE228 ANNUNCIATOR POWER SOURCE ILLUMINATED. RECONNECTED PIN TO CONNECTOR FOR PCB A144. 2 L 7 2 4T RT A24CE 2002090400051 20020904 00051 CE 2002 9 4 GLBA2002116 1 20020803 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE MLG OUT OF ADJUST A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 220GL UE220 INTRANSIT LIGHT ILLUMINATED WITH GEAR RETRACTED. INSPECTED AND ADJUSTED UPLOCK SWITCH, OPS CHECKED SYSTEM SATISFACTORY. 2 L 7 2 4T RT A24CE 2002122000008 20021220 00008 CE 2002 12 20 GLBA2002117 1 20020806 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE MLG FAILED A GLBA O OTHER J WARNING INDICATION AP APPROACH 1 NM 03 254GL 11544 4969 UE254 LEFT MAIN LANDING GEAR WOULD NOT EXTEND ELECTRICALLY, EXTENDED MANUALLY. REMOVED AND REPLACED ACTUATOR. 2 L 7 2 4T RT A24CE 2002090400052 20020904 00052 2002 9 4 GLBA2002118 4 20020807 A 3418 TRANSDUCER BEECH 1900 1900D 1154162 CE STALL WARNING FAULTY A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 208GL UE208 STALL WARNING HORN SOUNDED SEVERAL TIMES DURING CLIMB. REMOVED AND REPLACED STALL TRANSDUCER, PERFORMED CALIBRATION TES T FLT OP/C GOOD. 2 L 7 2 4T RT A24CE 2002090400053 20020904 00053 CE 2002 9 4 GLBA2002119 1 20020811 A 3610 PRINTED CKT BOAR BEECH 1900 1900D 1154162 CE BLEED AIR MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 226GL UE226 DUAL ENVIRO FAIL AFTER TAKEOFF, RESET BLEED AIR MANAGEMENT PCB. 2 L 7 2 4T RT A24CE 2002090400054 20020904 00054 CE 2002 9 4 GLBA2002121 1 20020813 A 3150 WARNING SYSTEM BEECH 1900 1900D 1154162 CE COCKPIT FALSE ACTIVATION A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 184UX UE184 DUAL ENVIRO FAIL ON TAKEOFF ROLL, PERFORMED GROUND RUNS AND P-TEST AND OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2002090400055 20020904 00055 WP 2002 9 4 CALA0200449 1 20020831 A 5311 FRAME DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 49488 INSPECTION FOUND A 2" CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, LONGERON 2R AND 2L. REPAIRED BELTFRAME IAW SRM 53 -03-31A. 2 L 7 2 4F A6WE 2002090400056 20020904 00056 WP 2002 9 4 CALA0200450 1 20020831 A 5313 LONGERON DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 49488 INSPECTION FOUND A 1.5" CRACK IN LONGERON 2R AT STA 1418. REPAIRED LONGERON IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 2002090400057 20020904 00057 NM 2002 9 4 PCAA0209100 1 20020903 A 3350 61047811 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM POSITION #2 WEAK A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 979HA 373 DURING ROUTINE MAINTENANCE VISIT RIGHT FORWARD EXTERIOR EMERGENCY LIGHT AND SECOND CEILING EMERGENCY LIGHT FOUND INOPERA TIVE. POSITION #2 EMERGENCY LIGHT BATTERY PACK REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002090400058 20020904 00058 SO 2002 9 4 C2XA02CL167 1 20020809 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14945 145049 CLE FLIGHT#2979 THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE.MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT INVERTER.OPERATIONAL CHECKS WERE GOOD.Original Control number was incomplete. Corrected 9/4/02 2 L 7 2 4F RT T00011AT 2002090400059 20020904 00059 WP 2002 9 4 MWEA020524 1 20020903 A 5313 59114481 SPLICE DOUG DC9 DC982 3022082 WP STA 351 20&21R DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FRAME DAMAGED STATION 351 LONGERON 20 RIGHT-21 RIGHT. -- FABRICATED AND INSTALLED FRAME REPAIR SPLICES. 2 L 7 2 4F A6WE 2002090400060 20020904 00060 WP 2002 9 4 MWEA020525 1 20020903 A 5313 99124574 FRAME DOUG DC9 DC982 3022082 WP STA 362 20&21R DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FRAME DAMAGED AT STATION 362 LONGERON 20 RIGHT AND 21 RIGHT. -- DRILLED FRAME REMOVED AND INSTALLED FRAME. 2 L 7 2 4F A6WE 2002090400061 20020904 00061 WP 2002 9 4 MWEA020526 1 20020903 A 5313 59203235 LONGERON DOUG DC9 DC982 3022082 WP STATION 351 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 LONGERON 20 RIGHT DAMAGED AT STATION 351. -- FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 2002090400062 20020904 00062 WP 2002 9 4 MWEA020527 1 20020903 A 5313 59203235 LONGERON DOUG DC9 DC982 3022082 WP STATION 351 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 LONGERON 21 RIGHT DAMAGED AT STATION 351. -- FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 2002090400063 20020904 00063 WP 2002 9 4 MWEA020528 1 20020903 A 5313 49127981 CLIP DOUG DC9 DC982 3022082 WP STATION 351 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 SHEAR CLIP DAMAGED AT LONGERON 21 RIGHT AT STATION 351. -- FABRICATED AND INSTALLED SHEAR CLIP AND SPLICE. 2 L 7 2 4F A6WE 2002090400065 20020904 00065 CE 2002 9 4 GLBA2002122 1 20020814 A 2422 INVERTER BEECH 1900 1900D 1154162 CE E/E BAY FAILED A GLBA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 NM 03 254GL UE254 RIGHT AC BUS LIGHT CAME ON. REMOVED AND REPLACED NR 2 INVERTER. 2 L 7 2 4T RT A24CE 2002090400067 20020904 00067 2002 9 4 GLBA2002126 4 20020818 A 6122 GOVERNOR BEECH 1900 1900D 1154162 CE LT ENGINE OUT OF ADJUST A GLBA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 NM 03 204GL UE204 LEFT PROP LIMITED TO 1650 ON TAKEOFF ROLL. ADJUSTED LEFT HAND PROP GOV. 2 L 7 2 4T RT A24CE 2002122000010 20021220 00010 CE 2002 12 20 GLBA2002127 1 20020819 A 2160 SOLENOID BEECH 1900 1900D 1154162 CE RT ENVIRONMENTAL FAILED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 208GL UE208 RT ENVIRONMENTAL FAIL ON TAKE OFF / CHANGED P-TEST SOLENOID OPS CHECK OK 2 L 7 2 4T RT A24CE 2002122000011 20021220 00011 CE 2002 12 20 GLBA2002129 1 20020819 A 5610 10138402517 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 261GL UE261 CAPTAIN'S WINDSHIELD CRACKED IN FLIGHT, DIVERTED A/C TO FMN, FERRY TO CYS. REMOVED AND REPLACED WINDSHIELD 2 L 7 2 4T RT A24CE 2002090400069 20020904 00069 CE 2002 9 4 GLBA2002131 1 20020821 A 3246 114800121 WHEEL BEECH 1900 1900D 1154162 CE NLG VIBRATION A GLBA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 03 210GL UE210 AFTER TAKEOFF, NOSE WHEEL VIBRATION. REMOVED AND REPLACED NOSE WHEEL ASSY. 2 L 7 2 4T RT A24CE 2002090400072 20020904 00072 NE 2002 9 4 GLBA2002132 2 20020823 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT OVERTEMP A GLBA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 NM 03 100UX UE100 114224 LEFT ENGINE OVERTEMPED ON TAKEOFF ROLL, PERFORMED FULL POWER PERFORMANCE RUN UP TQ WITHIN LIMITS. 2 L 7 2 4T 4 T RT A24CE E26NE 2002090400073 20020904 00073 CE 2002 9 4 GLBA2002133 1 20020823 A 5210 SEAL BEECH 1900 1900D 1154162 CE DOOR DIRTY A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 245GL UE245 MASSIVE DOOR SEAL SQUEAL IN CLIMB. CLEANED DIRT FROM DOOR SEAL. 2 L 7 2 4T RT A24CE 2002090400074 20020904 00074 2002 9 4 GLBA2002134 4 20020824 A 3460 COMPUTER BEECH 1900 1900D 1154162 CE E/E BAY MALFUNCTIONED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 170GL UE170 F/O'S FLIGHT DIRECTOR FROZE, ALL FCP LIGHTS LIT UP, AP FAIL ILL THEN FD FLAGGED ON EHSI. RERACKED DPU. 2 L 7 2 4T RT A24CE 2002122000012 20021220 00012 CE 2002 12 20 GLBA2002135 1 20020826 A 3610 PLUG BEECH 1900 1900D 1154162 CE EVA TUBE MISSING A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 211GL UE211 RT BLEED FAIL ON TAKE OFF, REPLACED EVA TUBE PLUG OPS CHECK OK. 2 L 7 2 4T RT A24CE 2002090400075 20020904 00075 CE 2002 9 4 GLBA2002136 1 20020827 A 2150 A/C PACK BEECH 1900 1900D 1154162 CE A/C BAY FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 210GL UE210 RIGHT ENVIRO FAIL. 2 L 7 2 4T RT A24CE 2002122000013 20021220 00013 CE 2002 12 20 GLBA2002137 1 20020828 A 7712 1143800653 INDICATOR BEECH 1900 1900D 1154162 CE RT TORQUE MALFUNCTIONED A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 150GL 5660 3351 UE150 RT TORQUE INDICATOR FLUCTUATES BETWEEN 1500-2800, REMOVED AND REPLACED INDICATOR 2 L 7 2 4T RT A24CE 2002122000014 20021220 00014 CE 2002 12 20 GLBA2002138 1 20020830 A 7931 CONNECTOR BEECH 1900 1900D 1154162 CE OIL PRESS IND FAILED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 249GL UE249 RT ENGINE OIL PRESSURE FLUCTUATED 70 PSI TO 120 PSI,CHANGED CONNECTOR OPS CHECK GOOD 2 L 7 2 4T RT A24CE 2002090400076 20020904 00076 GL 2002 9 4 BSY2002F00020 3 20020809 A 6197 WIRE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE HARTZL H3B3M HCB3M GL PROP DEICE SYS LOOSE E BSYA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 1026V 208B0319 PCE19195 ON TAKE OFF OUT OF BOSTON, SPARKS WERE FLYING OUT FROM UNDERNEATH PILOTS PANEL, RETURNED TO BASE. FOUND EXPOSED WIRE OU T OF CONNECTOR P160 ON WIRE NR HA20 ON PROPELLER DEICE CIRCUIT, SHORTED ON SIDE PANEL REPAIRED CONNECTOR, OPS GOOD. 1 H 7 1 3T 3 T A37CE E4EA 5 C P9NE 2002090400077 20020904 00077 2002 9 4 HNAA0200052 4 20020807 A 3460 101741111SCN60 COMPUTER DHAV DHC8 DHC8201 2809001 NM COCKPIT FAILED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 07 996HA 17153 514 497 SMOKE CAME FROM FMS THEN UNIT WENT BLANK. FMS INSPECTED AND DEACTIVATED IAW EO8-34-02-0872. 2 H 7 2 4T RT A13NM 2002090400078 20020904 00078 CE 2002 9 4 CUX2002F00000 1 20020711 A 5720 501200737 FITTING BEECH 90 E90 1152914 CE PWA PT6 PT6A27 52043 EA LT WING SCRATCHED E CUXA K NONE O OTHER IN INSP/MAINT 1 WP 17 111TC LW305 LEFT WING LOWER FORWARD INBOARD WING BOLT ATTACH FITTING (PN 50-120073-7) WAS DISCOVERED TO HAVE 3 SMALL SCRATCHES DURIN G A REPETITIVE INSPECTION OF AD. THE SCRATCHES WERE LOCATED ON THE ATTACH BOLT WASHER SEARING FACE RADIUS IN AN AXIAL D IRECTION AND WERE APPROXIMATELY .001 INCH DEEP. IT IS BELIEVED THAT PREVIOUS IMPROPER CLEANING TOOLS OR INSTALLATION PR OCEDURES MAY HAVE CAUSED THE SCRATCHING. THE DAMAGED PART WAS BLENDED AND REINSPECTED IAW FR. 1 L 7 2 3T 4 T 3A20 E4EA 2002090400079 20020904 00079 CE 2002 9 4 CUX2002F00001 1 20020711 A 5523 5061001722 SKIN BEECH 90 E90 1152914 CE PWA PT6 PT6A27 52043 EA ELEV TRIM TAB CRACKED E CUXA K NONE O OTHER IN INSP/MAINT 1 WP 17 111TC 6557 LW305 RIGHT ELEVATOR TRIM TAB OUTER SKIN WAS DISCOVERED CRACKED AT THE UPPER INBOARD AFT CORNER DURING A ROUTINE PHASE 1 INSPE CTION. THE CRACK BEGAN AT A SKIN ATTACH COUNTER SUNK RIVET AND EXTENDED FORWARD AND FAT APPROXIMATELY .350 INCH IN EACH DIRECTION. THE TAB WAS REPAIRED BY INSTALLING A NEW SKIN ASSEMBLY. 1 L 7 2 3T 4 T 3A20 E4EA 2002090400080 20020904 00080 NM 2002 9 4 HNAA0200053 1 20020814 A 2920 CIRCUIT BREAKER DHAV DHC8 DHC8102 2809003 NM COCKPIT TRIPPED A HNAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 07 914HA 53 BOTH STANDBY HYDRAULIC PUMP CIRCUIT BREAKERS TRIPPED AND NORMAL BRAKES FAILED WHEN NR 1 ENGINE WAS SHUTDOWN DURING TAXI. MAINTENANCE RESET CIRCUIT BREAKERS AND PERFORMED ASSOCIATED OP CHECKS AND COULD NOT DUPLICATE PROBLEM. 2 H 7 2 4T RT A13NM 2002090400081 20020904 00081 CE 2002 9 4 CUX2002F00002 1 20020711 A 5720 501200687 STIFFENER BEECH 90 E90 1152914 CE PWA PT6 PT6A27 52043 EA RT WING CRACKED E CUXA K NONE O OTHER IN INSP/MAINT 1 WP 17 111TC 6557 LW305 RIGHT WING UPPER FORWARD STIFFENER (PN 50-120068-7) WAS DISCOVERED CRACKED DURING A ROUTINE PHASE 1 INSPECTION. THE CRA CK BEGAN AT THE INBOARD EDGE, EMANATING OUTWARD THROUGH THE FIRST 2 RIVET HOLES FOR A TOTAL LENGTH OF 1.55 INCHES. THE DAMAGED PART WAS REMOVED AND REPLACED WITH A NEW ONE. 1 L 7 2 3T 4 T 3A20 E4EA 2002090400082 20020904 00082 SO 2002 9 4 ECWR200201 1 20020625 A 7160 561020 SCREEN PIPER PA46 PA46310P 7104605 SO CONT O550 TSIOL550C SO AIR BOX FAILED B ECWR K NONE O OTHER IN INSP/MAINT 1 SO 15 2138C 100 468608020 814513R INDUCTION AIR FILTER METAL PROTECTIVE SCREEN FAILED AND THE METAL FROM THE SCREEN WAS INDUCTED INTO THE TURBOCHARGER ASS EMBLY AND INTAKE AIR OF THE ENGINE. THE ENGINE OIL FILTER WAS REMOVED AND IT WAS DISCOVERED TO HAVE MAJOR METALLIC CONT AMINATION AS A RESULTED OF THE AIR FILTER SCREEN FAILURE. THE AIRCRAFT WAS IN FOR AN ANNUAL INSPECTION WHEN THE TECHNIC IAN, UPON INSPECTION OF THE AIR BOX AND FILTER, DISCOVERED THE DAMAGE. THE TURBOCHARGER TURBINE SUFFERED SEVERE EROSION AND IS IN AN UNSERVICEABLE STATE REQUIRING MAJOR OVERHAUL. THE FILTER HAD 100 HOUR TIS FROM NEW INSTALLATION 05/11/01. CHECK FOR BAD LOT OF FILTERS FORM OEM. 1 L 7 1 3O 3 O RT A25SO E4SO 2002092500086 20020925 00086 NM 2002 9 25 HNAA0200055 1 20020821 A 3040 TERMINAL DHAV DHC8 DHC8102 2809003 NM WINDSCREEN HEAT LOOSE A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 938HA 26022 152 AFTER SELECTION OF WINDSHIELD WARM-UP, NOTICED SMOKE FROM FIRST OFFICERS WINDSCREEN AREA. SELECTED TO OFF AND SMOKE DIS APPEARED. INSPECTED ALL WINDSCREEN TERMINALS, TEMP MONITOR IN COAT CLOSET AND WIRES UNDER GLARESHIELD. FOUND ONE LOOSE TERMINAL (L2) ON THE FIRST OFFICERS SIDE. RESECURED L2 AND OPS CHECKED WIND SCREEN HEAT. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2002090400083 20020904 00083 CE 2002 9 4 R2J2002F00009 1 20020820 A 5512 010A21001103 SKIN MTSBSI MU2 MU2B40 5780440 CE GARRTT TPE331 TPE331* 01514 WP HORIZONTAL STAB CRACKED B R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 361MA 3553 429SA DURING RIGHT HORIZONTAL STABILIZER DEICE BOOT REPLACEMENT, INSPECTORS FOUND 8 INCH CRACK UNDER DEICE BOOT ON HORIZONTAL STABILIZER LEADING EDGE SKIN. PROCEDURE FOR REPAIR FOUND IN MU2 STRUCTURAL SRM. FIELD APPROVAL OF DATA C/W AND REPAIR MADE. INSPECTION OF THIS AREA RECOMMENDED WHERE DEICE BOOT REMOVED OR USE (SQUEEZE TEST) TO FIND SOME DEFECTS WITH DEIC E BOOT ON. 1 H 7 2 3T 3 T RT A10SW E2WE 2002090400085 20020904 00085 EU 2002 9 4 MALA020451 1 20020810 A 8010 HC921H1879002 MONITOR BAC 146 AVRO146RJ85A 1500097 EU COCKPIT MALFUNCTIONED A MALA K NONE N FALSE WARNING CR CRUISE 1 GL 15 523XJ E2348 DURING FLIGHT 3685, STARTER OPERATING ANNUNCIATION VERY DIM AND INTERMITTENT DURING ENGINE STARTS ON ENGINE 3 AND 4. WO RKS NORMALLY ON ENGINES 1 AND 2. MAINTENANCE REPLACED RT VOLTAGE MONITOR IAW 80-10-27. OPS CHECK GOOD. A/C GOOD FOR C ONTINUED SERVICE, REPAIRED WIRES BEHIND STARTER OVERHEAD PANEL. 2 H 7 4 4F RT A49EU 2002090400086 20020904 00086 EU 2002 9 4 MALA020452 1 20020806 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K-CHECK IN CWA, FRAME ANGLE AT STA 225 HAS LIGHT SURFACE CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70 -40. 2 L 7 2 4T RT A52EU 2002090400087 20020904 00087 CE 2002 9 4 RJ22002F00000 1 20020820 A 2435 BEARING LUCAS CESSNA 500 S550 2076607 CE PWA JT15 JT15D4 52112 NE STARTER GEN FAILED B RJ2R A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 EA 21 1VA 2249 S5500143 INFLIGHT, CREW NOTICED NOISE IN LT ENGINE, FOLLOWED BY NR 1 GENERATOR FAILURE. INSPECTORS FOUND AFT BEARING ON LT START ER GENERATOR HAD COMPLETELY FAILED ALLOWING ARMATURE TO HIT FIELD POLES. S/G HAD APPROXIMATELY 500 HOURS SINCE LAST OVE RHAUL. EXCHANGE STARTER-GENERATOR AND GENERATOR CONTROL UNIT INSTALLED SYSTEM CHECKED, OK. CAUSE OF BEARING FAILURE UN KNOWN. SENT FOR CORE EVALUATION. SUSPECTED CAUSE OF FAILURE, MANUFACTURING DEFECT IN BEARING. 1 L 7 2 4F 4 F RT A22CE E1NE 2002090400088 20020904 00088 2002 9 4 MALA020453 4 20020812 A 2565 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EVAC SLIDE FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 AFTER PREVIOUS FLIGHT 3624, RT AFT EVACUATION SLIDE BATTERY PACK FAILED. DURING TASK CARD 0437 INSPECTION. MAINTENANCE INSTALLED SLIDE ASSEMBLY. 2 H 7 4 4F RT A49EU 2002090400090 20020904 00090 EU 2002 9 4 MALA020454 1 20020715 A 5315 FLOORBEAM BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 515XJ E2333 DURING C-CHECK IN CVG, CORROSION AND CRACKS WERE FOUND ON THE FRAME 18 FLOORBEAM. MAINTENANCE REMOVED DAMAGE IAW BAE AP PROVED FAX BARA/AVR/5973/02-MN AND MESABA EO A53080. 2 H 7 4 4F RT A49EU 2002090400091 20020904 00091 EU 2002 9 4 VJ32002F00062 1 20020816 A 7800 120A641402 CLAMP GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA HEAT SHIELD CRACKED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 861AF 293 85001 L2802348A DURING PROGRESSIVE INSPECTION FOUND CLAMP CRACKED AND ROLL RIVET SHEARED OFF. PROBABLE CAUSE IS ENGINE VIBRATION. 1 L 7 1 3O 3 O RT A49CE 1E4 2002090400092 20020904 00092 EU 2002 9 4 MALA020455 1 20020705 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 515XJ E2333 DURING C-CHECK IN CVG, RIGHT O/B SEAT RAIL HAS 6 AREAS OF CORROSION. SEAT RAIL REPAIRED IAW EO A53026. 2 H 7 4 4F RT A49EU 2002090400093 20020904 00093 EU 2002 9 4 MALA020456 1 20020705 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 515XJ E2333 DURING C-CHECK IN CVG, RIGHT I/B SEAT RAIL NR 3, HAS 7 AREAS OF CORROSION. SEAT RAIL REPAIRED IAW EO A53026. 2 H 7 4 4F RT A49EU 2002090400094 20020904 00094 NM 2002 9 4 SWAA021915 1 20020821 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 717SA 27851 DURING SCHEDULED RON, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002090400095 20020904 00095 2002 9 4 SWAA021916 4 20020821 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM AFT CABIN DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2 L 7 2 4F A16WE 2002090400096 20020904 00096 2002 9 4 SWAA021917 4 20020822 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN DOOR WAS OPENED. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002090400097 20020904 00097 2002 9 4 SWAA021919 4 20020821 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002090400098 20020904 00098 NM 2002 9 4 SWAA021920 1 20020821 A 2730 6545166 ROD BOEING 737 7373H4 1384600 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED C2 CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR PUSH ROD AFT END ROD AS SY PER MM. 2 L 7 2 4F RT A16WE 2002090400099 20020904 00099 NM 2002 9 4 SWAA021924 1 20020822 A 5311 6546576 FRAME BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C CHECK, FOUND OTBD LOWER CHORD HORIZ FLANGE CRACKED AT BS 1156, STR 20. REPAIRED HORIZ FLANGE PER SWA EA. 2 L 7 2 4F A16WE 2002090400100 20020904 00100 2002 9 4 SWAA021926 4 20020825 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002090400101 20020904 00101 2002 9 4 SWAA021928 4 20020823 A 2565 D31591475 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED S LIDE PER MM. 2 L 7 2 4F RT A16WE 2002090400102 20020904 00102 NM 2002 9 4 SWAA021929 1 20020824 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 EEPLS LOOSE AT ROW NR 9. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002090400103 20020904 00103 2002 9 4 SWAA021931 4 20020822 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002090400104 20020904 00104 NM 2002 9 4 SWAA021934 1 20020824 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED A2 CHECK, FOUND EEPLS INOP AT FWD CABIN. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002090400105 20020904 00105 NM 2002 9 4 SWAA021938 1 20020825 A 3230 A42006028305 SOLENOID BOEING 737 7373H4 1384600 NM COCKPIT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 355SW 25250 AIR TURNBACK, AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. FOUND GEAR LEVER CONTROL LOCK SOLENOID INOP. REMOVED AND R EPLACED SOLENOID PER MM. 2 L 7 2 4F RT A16WE 2002090400106 20020904 00106 NM 2002 9 4 SWAA021939 1 20020823 A 3233 654610079 PIN BOEING 737 7373H4 1384600 NM RT MLG SHEARED A SWAA K NONE E VIBRATION/BUFFET AP APPROACH 1 SW 29 637SW 27710 DURING APPROACH CREW HEARD LOUD BANG AND AIRCRAFT SHUTTER WHEN GEAR WAS LOWERED. FOUND RT MLG ACTUATOR TRUNNION PIN SHE ARED. MX FERRY TO HOU, REMOVED AND REPLACED RT MLG PER MM. 2 L 7 2 4F RT A16WE 2002090400107 20020904 00107 NM 2002 9 4 SWAA021943 1 20020826 A 3260 1061226 DOWNLOCK SENSOR BOEING 737 7372T4 1384492 NM NLG FAILED A SWAA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SW 29 721WN 22697 DECLARED EMERGENCY, DURING APPROACH NOSE GEAR INDICATED UNSAFE, MADE UNEVENTFUL LANDING. MX FERRY TO HOU. FOUND DOWN L OCK SENSOR INOP, REMOVED AND REPLACED NOSE GEAR DOWN LOCK SENSOR PER MM. 2 L 7 2 4F A16WE 2002090400108 20020904 00108 NM 2002 9 4 SWAA021951 1 20020826 A 2782 65446519 ACTUATOR BOEING 737 7372H4 138448C NM L/E SLAT FAILED A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 29 086SW 22827 AIR TURNBACK, DURING FLAP RETRACTION AFTER TAKEOFF, NR 3 L/E SLAT FAILED TO RETRACT. REMOVED AND REPLACED NR 3 L/E SLAT ACTUATOR PER MM. 2 L 7 2 4F A16WE 2002090400109 20020904 00109 NM 2002 9 4 SWAA021952 1 20020826 A 5312 6545409306 PRESSURE PANEL BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 33 AND LBL 39. REPAIRED BEADED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2002090400110 20020904 00110 NM 2002 9 4 SWAA021960 1 20020826 A 3350 604222 BATTERY BOEING 737 7375H4 138449D NM CARGO BAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED RON, FOUND AFT SVC DOOR AND RIGHT EXTERIOR LOWER FUSELAGE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPL ACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002090400111 20020904 00111 NM 2002 9 4 SWAA021961 1 20020825 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED SPECIAL VISIT, FOUND LT OVERWING EMERGENCY EXIT LIGHTS INOP. CHARGED BATTERIES PER MM. 2 L 7 2 4F A16WE 2002090400112 20020904 00112 NM 2002 9 4 UPS02439205 1 20020816 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C UPPER DECK BS 550 LBL 50 SEAT TRACK CROWN FOUND CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEA T TRACK REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002090400113 20020904 00113 NM 2002 9 4 UPS02439206 1 20020818 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C UPPER DECK BS 680 LBL 28 SEAT TRACK LIP FOUND CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPAIRED. 2 L 7 4 4F A20WE 2002090400114 20020904 00114 NM 2002 9 4 UPS02439212 1 20020814 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C, M/D - FLOOR SUPPORT FOUND CORRODED AT STA 240 LBL 4 - LBL 5. CORROSION REMOVED IAW 51-10-01, CORROSI ON BLEND OUT EXCEEDS SRM LIMIT. FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 8. 2 L 7 4 4F A20WE 2002090400115 20020904 00115 NM 2002 9 4 UPS02439213 1 20020803 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C, M/D BS 460 RBL 58 - RBL 70 FLOORBEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01, CORROSI ON BLEND OUT EXCEEDS SRM 53-10-01 FIG 1 LIMITS, REPAIRED BS 460 RBL 70 FLOORBEAM WEB IAW SRM FIG 53-10-07 FIG 11. 2 L 7 4 4F A20WE 2002090400116 20020904 00116 NM 2002 9 4 UPS02439215 1 20020806 A 5320 SPLICE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C, RIGHT BS 1241 BULKHEAD SPLICE STRAP FWD HOLE FOUND CRACK AT 12 O/C POSN WL 190. HOLE REWORKED IAW EO 5310-0323 APP F LIMIT. REF EO 5310-0323 PARA 4D ITEM 3 FOR SPLICE STRAP CRACK FINDING NO FURTHER ACTION IS REQUIRED. 2 L 7 4 4F A20WE 2002090400117 20020904 00117 NM 2002 9 4 UPS02439216 1 20020805 A 5312 BULKHEAD BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C LEFT BS 1241 BULKHEAD FWD HOLE CRACKED AT BULKHEAD FRAME FORGING SPLICE STRAP & SKIN WL 170 TO 180. R EWORKED HOLE AS PER EO 5310-0323 APP F TABLE 1, REWORKED HOLE NDT INSPECTED NIL CRACK FOUND AS PER NTM PART 6 51-00-00 F IG 1. 2 L 7 4 4F A20WE 2002090400118 20020904 00118 NM 2002 9 4 UPS02439217 1 20020814 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C, M/D BS 540 S24L FRAME FOUND CRACKED. M/D BS 540 S24L FRAME REPAIRED AS PER SRM 53-10-04 FIGURE 15. 2 L 7 4 4F A20WE 2002090400119 20020904 00119 NM 2002 9 4 UPS02439220 1 20020810 A 5312 BULKHEAD BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C, CORROSION REVEALED ON BS 1480 BULKHEAD WEB LEFT I/B CORNER AREA, AREA INSP AFTER BATHTUB FITTING REMO VED INSIDE KEEL BEAM BOX. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 53-10-01 LIMITS, REPAIRE D IAW HX RS R53-49-34878. 2 L 7 4 4F A20WE 2002090400120 20020904 00120 NM 2002 9 4 UPS02439223 1 20020806 A 5314 KEELBEAM BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C, FX-KEEL BEAM BOX INTERIOR RIGHT SIDE LOWER CHORD FOUND CORROSION AT STA 1460-1468 RBL 6 TO RBL 8. CO RROSION REMOVED IAW SRM 51-10-01 CORROSION BLEND OUT EXCEEDS SRM 53-10-01 LIMITS, REPAIRED IAW HX RS R53-49-34878. 2 L 7 4 4F A20WE 2002090400121 20020904 00121 NM 2002 9 4 UPS02439225 1 20020807 A 5720 STIFFENER BOEING 747 747212B 1384886 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:C, RIGHT WLG BS 1241 BULKHEAD STIFFENER FOUND CORROSION AT WL 150 RBL 4-10. CORROSION REMOVED IAW SRM 5 1-10-01. CORROSION BLEND OUT EXCEEDS SRM 57-10-01 FIG 1 LIMITS FOR REPAIR REFER TO HX RS R57-12-34875. 2 L 7 4 4F A20WE 2002090400122 20020904 00122 WP 2002 9 4 UPS02839030 1 20020808 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:N/A, CORROSION FOUND AT FUSELAGE STATION 1680 STRINGER 28L IN FUSELAGE SKIN. REPAIRED CORROSION PER EO DC8-5330-17295-A IN SKIN PANEL. 2 L 7 4 4F RT 4A25 2002090400123 20020904 00123 WP 2002 9 4 UPS02839041 1 20020723 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 STA 89 DOUBLER, FINGER DOUBLER AND WEB ARE CORRODED BEYOND LIMITS AT RBL 30. CUT OUT CORRODED AREA O N WEB, FABRICATED AND INSTALLED FILLER, DOUBLER, AND FINGER DOUBLER IAW DWG 5612298, AND SR08530026. 2 L 7 4 4F RT 4A25 2002090400126 20020904 00126 SO 2002 9 4 AK62002F00001 2 20020823 A 8520 BEARING CESSNA 421 421B 2076014 CE CONT O520 GTSIO520H 17032 SO ENGINE FAILED B AK6R K NONE O OTHER IN INSP/MAINT 1 SW 19 5448J 421B0906 231537R THE RT ENGINE APPEARS TO HAVE SUFFERED FROM OIL STARVATION AT THE NR 5 ROD JOURNAL. THIS CAUSED THE ROD TO SEPARATE AND PROTRUDE THRU THE TOP OF THE CRANKCASE. 1 L 7 2 3O 3 O A7CE E7CE 2002090400127 20020904 00127 2002 9 4 ALG2002F00062 4 20020816 A 3442 M15853001 RADAR SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL COCKPIT FAILED E ALGR O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 03 703AL 760266 IN CRUISE FLIGHT, RADAR WORKING INTERMITTENTLY FOLLOWED BY SMOKE IN THE COCKPIT. 1 G 7 2 3U 3 U H1NE E1GL 2002090400128 20020904 00128 SW 2002 9 4 ALG2002F00063 1 20020710 A 6340 SPLINE ADAPTER BELL 206 206L1 1182107 SW TACH GEN WORN E ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 3899C 45596 DURING FLIGHT PILOT NOTED ROTOR TACH WENT TO ZERO. TACH GENERATOR SPLINES WORN. 1 G 7 1 3U H2SW 2002090400129 20020904 00129 EU 2002 9 4 MALA020457 1 20020705 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 515XJ E2333 DURING C-CHECK IN CVG, LEFT I/B SEAT RAIL NR 2, HAS 12 AREAS OF CORROSION. SEAT RAIL REPAIRED IAW EO A53026. 2 H 7 4 4F RT A49EU 2002090400130 20020904 00130 GL 2002 9 4 ALG2002F00064 2 20020508 A 7210 6893672 PINION GEAR ALLSN BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX FAILED E ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 647AL 1675 CAG47389 53357 CAE847389 UPON DISASSEMBLY OF GEARBOX DUE TO CHIP LIGHT. FOUND EXCESSIVE GALLIN ON PINION AND T/M GEARS. T/M GEAR HAD ROUGH EDGE S CAUSING PINION GEAR TO GALL. ASSURE PROPER MACHINING AND MESHING OF GEAR TEETH AT FACTORY. 1 G 7 1 3U 3 U O H2SW E1GL 2002090400131 20020904 00131 EU 2002 9 4 MALA020458 1 20020806 A 5260 CHANNEL SAAB SF340 340B 7860101 EU AIRSTAIRS CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K-CHECK IN CWA, AIRSTAIR U-CHANNEL HAS CORROSION. MAINTENANCE REMOVED CORROSION SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090400132 20020904 00132 EU 2002 9 4 MALA020459 1 20020806 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN CWA, I/B GALLEY SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED CORROSION AND APPLIED PROTECTIVE TREATMENTS AND COATINGS IAW SAAB SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090400133 20020904 00133 EU 2002 9 4 MALA020460 1 20020806 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN CWA, FRAME ANGLE AT STA 258 HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION AND APPLIED PROT ECTIVE TREATMENTS AND COATINGS IAW SAAB SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090400134 20020904 00134 EU 2002 9 4 MALA020461 1 20020806 A 5320 SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN CWA, SUPPORT AT LBL 11 BETWEEN STA 225 AND 236 HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSI ON AND APPLIED PROTECTIVE TREATMENTS AND COATINGS IAW SAAB SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090400135 20020904 00135 EU 2002 9 4 MALA020462 1 20020806 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN CWA, FRAME ANGLE STA 272 HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION AND APPLIED PROTECT IVE TREATMENTS AND COATINGS. 2 L 7 2 4T RT A52EU 2002090400136 20020904 00136 EU 2002 9 4 MALA020463 1 20020807 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN CWA, LBL 18.3 SEAT TRACK HAS CORROSION AT FWD SECTION AND CENTER SECTION. MAINTENANCE REMOVED C ORROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090400137 20020904 00137 EU 2002 9 4 MALA020464 1 20020807 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN CWA, LBL 18.3 SEAT TRACK HAS CORROSION ON SIDE IN CARGO INFILL PANEL AREA. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090400138 20020904 00138 WP 2002 9 4 MWEA020529 1 20020903 A 5313 59203235 LONGERON DOUG DC9 DC982 3022082 WP STATION 351 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 LONGERON 22 RIGHT IS DAMAGED AT STATION 351. -- LOCATED AND DRILLED NEW LONGERON AND REINSTALLED LONGERON. 2 L 7 2 4F A6WE 2002090400139 20020904 00139 WP 2002 9 4 MWEA020530 1 20020903 A 5313 99115264 CLIP DOUG DC9 DC982 3022082 WP STATION 294 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 SHEAR CLIP DAMAGED AT STATION 294 LONGERON 21 RIGHT. -- FABRICATED AND INSTALLED SHEAR CLIP. 2 L 7 2 4F A6WE 2002090400140 20020904 00140 WP 2002 9 4 MWEA020531 1 20020903 A 5313 49127981 CLIP DOUG DC9 DC982 3022082 WP STATION 362 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 SHOVEL CLIP DAMAGED AT STATION 362 LONGERON 20 RIGHT. -- LOCATED AND DRILLED SHOVEL CLIP AND REINSTALLED CLIP. 2 L 7 2 4F A6WE 2002090400141 20020904 00141 WP 2002 9 4 MWEA020532 1 20020903 A 5313 49127981 CLIP DOUG DC9 DC982 3022082 WP STATION 362 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 SHOVEL CLIP DAMAGED AT STATION 362 LONGERON 21 RIGHT. -- LOCATED AND DRILLED HOLES IN NEW SHOVEL AND REINSTALLED CLIP. 2 L 7 2 4F A6WE 2002090400142 20020904 00142 WP 2002 9 4 MWEA020533 1 20020903 A 5313 SKIN DOUG DC9 DC982 3022082 WP STATION 392 TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 MISDRILLED HOLES IN NEW SKIN AT STATION 392 ABOVE LONGERON 19 RIGHT. -- PLUGED MISDRILLED HOLES. 2 L 7 2 4F A6WE 2002090400143 20020904 00143 WP 2002 9 4 MWEA020535 1 20020904 A 5313 49127981 SHEAR TIE DOUG DC9 DC982 3022082 WP STATION 332 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 SHEAR CLIP DAMAGED AT LONGERON 20 RIGHT STATION 332. -- LOCATED AND DRILLED SHEAR TIE. REMOVED AND INSTALLED SHEAR TIE AND SPLICE. 2 L 7 2 4F A6WE 2002090400144 20020904 00144 WP 2002 9 4 MWEA020536 1 20020904 A 5313 9912455505 DOUBLER DOUG DC9 DC982 3022082 WP STATION 362 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FORWARD CARGO DOOR DOUBLER DAMAGED AT STATION 362 LONGERON 20&21 RIGHT. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002090400145 20020904 00145 CE 2002 9 4 DYM2002F00000 1 20020718 A 2150 1015552117 COMPRESSOR BEECH 200 B200 1152922 CE PWA PT6 PT6* 52043 EA AIR CONDITIONING DAMAGED E DYMA O OTHER O OTHER NR NOT REPORTED 1 SW 05 457TC BB1458 ON TRAINING FLIGHT COPILOT NOTICED HOLE IN RIGHT INBOARD COWLING. UPON INSPECTION THE (FREON COMPRESSOR) HAD A SILVER DOLLAR SIZED HOLE IN THE SIDE. IT HAD A FLASH FIRE AND TORCHED A HOLE IN THE SIDE OF THE COWLING. SEVERAL COMPONENTS W ERE ALSO DAMAGED. 1 L 7 2 4T 3 T A24CE E2NE 2002090400146 20020904 00146 EU 2002 9 4 MALA020465 1 20020807 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN CWA, BL 0 SEAT TRACK HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION, TREATED, PRIMED AND PA INTED SEAT TRACK IAW E SF340 SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090400147 20020904 00147 EU 2002 9 4 MALA020466 1 20020806 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN CWA, RIGHT O/B FLOORBOARD ANGLE FROM STA 258-294 HAS CORROSION. REMOVED CORROSION AND APPLIED P ROTECTIVE TREATMENTS AND COATINGS IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090400148 20020904 00148 EU 2002 9 4 MALA020467 1 20020814 A 2432 POWER SUPPLY SAAB SF340 340B 7860101 EU E/E BAY LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 366PX 340B267 DURING FLIGHT 2756 EMERGENCY POWER SUPPLY CAUTION LIGHT ILLUMINATED. AIR TURNBACK TO MSP. MAINTENANCE RESECURED EMERGE NCY POWER SUPPLY (JET PACK) IN AVIONICS RACK. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002090400149 20020904 00149 EU 2002 9 4 MALA020468 1 20020814 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU RT MLG NOT SEATED A MALA A UNSCHED LANDING O OTHER AP APPROACH 1 GL 15 441XJ 340B441 DURING FLIGHT 3247, EN ROUTE TO CMX, RIGHT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE UPON GEAR DOWN SELECTION. PILOT TRI ED TO RELAMP, THIS DID NOT HELP. OVERFLEW CMX WENT ON TO MSP AND LANDED. UPON LANDING IN MSP CREW HAD NO GREEN INDICAT ION. DIVERSION TO MSP. MAINTENANCE RESEATED RIGHT MLG DOWNLOCK SWITCH HARNESS CONNECTOR. ALL LANDING GEAR INDICATIONS NORMAL, GEAR SWING AMM 32-30-00. 2 L 7 2 4T RT A52EU 2002090400150 20020904 00150 NM 2002 9 4 375PA0004 1 20020902 A 3350 BULB BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 375PA 23812 SEVERAL EMERGENCY FLOOR LOCATOR LIGHTS ARE INOP. RELAMPED SEVERAL LIGHTS IN FWD TRACK. ALL E-PATH OPS CHECK OK PER MM 33-51-81. 2 L 7 2 4F RT A16WE 2002100200040 20021002 00040 NM 2002 10 2 2002UALA01342 1 20020824 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 FUSELAGE HAD MULTIPLE DENTS ON EXISTING REPAIR DOUBLER AND ADJACENT TO THE REPAIR DOUBLER BETWEEN STATION 615 AND 645 AN D STRINGER 15L TO 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER AND FILLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200042 20021002 00042 NM 2002 10 2 2002UALA01344 1 20020825 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 MID CABIN CREASE BEAM INNER CHORD IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED INNER CHORD CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200043 20021002 00043 NM 2002 10 2 2002UALA01345 1 20020825 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 CABIN FLOOR SUPPORT STATION 680 TO 700 RBL 60 JUST FORWARD OF FLOOR DRAIN DR. 2R SUPPORT IS CORRODED. MAJOR REPAIR AC COMPLISHED. REPLACED SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200044 20021002 00044 NM 2002 10 2 2002UALA01346 1 20020825 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 CABIN FLOOR SUPPORT STATION 720-740 IS CORRODED ON TOP SURFACE. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200045 20021002 00045 NM 2002 10 2 2002UALA01347 1 20020825 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 CABIN FLOOR SUPPORT STATION 720-740 RBL 60 IS CORRODED ON TOP SURFACE. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200046 20021002 00046 NM 2002 10 2 2002UALA01348 1 20020825 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 CABIN SUPPORT STATION 710-720 RBL 60 JUST INBOARD OF DOOR 2R IS CORRODED ON TOP SURFACE. MAJOR REPAIR ACCOMPLISHED. RE PLACED SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200047 20021002 00047 NM 2002 10 2 2002UALA01349 1 20020825 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 STATION 700 RBL CREASE BEAM INNER ANGLE CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WITH NEW. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200048 20021002 00048 NM 2002 10 2 2002UALA01351 1 20020823 A 2560 BATTERY PACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 620UA 21880 NUMBER 1 SPOILER SQUIB AND NUMBER 2 ESCAPE SLIDE WILL NOT TEST. FOUND EMERGENCY ESCAPE BATTERY PACK ON RIGHT SIDE M962 DISCONNECTED. THE CONNECTOR WAS RECONNECTED AND THE SYSTEM OPERATED OK. 2 L 7 2 4F 4 F RT A1NM E3NE 2002100200049 20021002 00049 NM 2002 10 2 2002UALA01352 1 20020816 A 5311 FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 FUSE FRAME WEB AT STA 1540 BETWEEN STR 43L AND 45L NEED TO BE REPAIRED. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECT ION OF WEB. 2 L 7 4 4F 4 F RT A20WE E24NE 2002100200050 20021002 00050 NM 2002 10 2 2002UALA01353 1 20020816 A 5311 FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 FUSE FRAME WEB AT STA 1500 BETWEEN STR 43L AND 44L NEEDS REPAIR. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECTION OF WEB. 2 L 7 4 4F 4 F RT A20WE E24NE 2002100200051 20021002 00051 NM 2002 10 2 2002UALA01354 1 20020816 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 FUSE SKIN DENTED AT STA 1485, STR 45L AND 46L. MAJOR REPAIR ACCOMPLISHED. FUSE SKIN DENT REWORKED AND REFORMED. NO DO UBLER, SPLICE NEEDED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002100200052 20021002 00052 NM 2002 10 2 2002UALA01355 1 20020824 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE LIGHTNING STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 UPPER RT EXTERIOR FUSELAGE SKIN AT BS 435, STR 2R HAS EXCESSIVE MATERIAL REMOVED AFTER LIGHTNING STRIKE REWORK. MAJOR R EPAIR ACCOMPLISHED. DOUBLER REPAIR WAS INSTALLED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002100200059 20021002 00059 NM 2002 10 2 2002UALA01363 1 20020828 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 CABIN CREASE BEAM WEB CORRODED STATION 960-980 STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. CABIN CREASE BEAM WEB REPLACED . 2 L 7 2 4F 4 F RT A2NM E17NE 2002101700028 20021017 00028 NM 2002 10 17 2002UALA01374 1 20020829 A 5347 SEAT TRACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 MID CABIN RIGHT HAND SIDE SEAT TRACK INBOARD FLANGE HAS LIGHT CORROSION AT STATION 680 TO 690 RBL 30. MAJOR REPAIR ACCO MPLISHED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101700029 20021017 00029 NM 2002 10 17 2002UALA01375 1 20020830 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 FORWARD CABIN FLOOR RIGHT HAND CREASE BEAM INNER CHORD RBL 65 UPPER SURFACE HAS LOCALIZED MATERIAL LOSS. MAJOR REPAIR A CCOMPLISHED. REPLACED CREASE BEAM INNER CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002090400151 20020904 00151 WP 2002 9 4 MWEA020534 1 20020904 A 5313 99124512 STRAP DOUG DC9 DC982 3022082 WP STATION 362 MISALIGNED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 RIGHT FRAME AT STATION 362 HAS 3 EXISTING PILOT HOLES NOT LINING UP WITH EXISTING FASTENER HOLES PATTERN. -- LOCATED A ND DRILLED STRAP FABRICATED AND INSTALLED STRAP. 2 L 7 2 4F A6WE 2002090400152 20020904 00152 WP 2002 9 4 MWEA020523 1 20020903 A 5313 5920323187 DOUBLER DOUG DC9 DC982 3022082 WP FWD CARGO DR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 WHILE AIRCRAFT PARKED AT GATE, BAGGAGE CART STRUCK AIRCRAFT ON RIGHT HAND SIDE FORWARD OF THE FORWARD CARGO DOOR JAMB. -- LOCATED AND DRILLED HOLES REMOVED AND INSTALLED SKIN. 2 L 7 2 4F A6WE 2002090400153 20020904 00153 EU 2002 9 4 MALA020533 1 20020903 A 2150 7769106 ACM SAAB SF340 SF340A 7850100 EU A MALA K NONE O OTHER CR CRUISE 1 GL 15 991XJ 340A091 DURING FLIGHT #3249, CREW SMELLED SOMETHING BURNING AND THEN THE ACM STARTED BLOWING HOT AIR. MAINTENANCE REPLACED RH A CM PN 776910-6, SN/ON 9703055, SN/OFF 9806175 IAW SAAB JOB CARD 215181 ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002090400154 20020904 00154 NE 2002 9 4 MALA020534 2 20020829 A 7220 230004015 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LF507 LF5071F NE A MALA K NONE Y ENGINE STOPPAGE CR CRUISE 1 GL 15 532XJ E2366 #2 ENGINE FAILED INFLIGHT. MAINTENANCE REPLACED #2 ENGINE SN/OFF P07686, SN/ON P07672 IAW TASK CARD 7100-502 ALSO COMPL ETED WORK PACKAGE DATED 08282000. ALL OPS AND LEAK CHECKS ARE GOOD. REF WORK PACKAGE FOR DETAILS. 2 H 7 4 4F 4 F RT A49EU E6NE 2002090400156 20020904 00156 WP 2002 9 4 ARWA20020810 1 20020830 A 2700 40581 TRANSDUCER DOUG DC8 DC85F54 3021926 WP A ARWA O OTHER J O WARNING INDICATION OTHER TO TAKEOFF 1 SO 19 426FB 45667 LOG PAGE # 110608. DISCREPANCY: NEAR END OF TAKEOFF ROLL PTY MAIN GEAR SPOILER INOPERATIVE LIGHT CAME ON. CORRECTIVE ACTION:REMOVED AND REPLACED #5 ANTISKID TRANSDUCER OPERATIONAL CHECK NORMAL IAW 27-35-0. 2 L 7 4 4F RT 4A25 2002091100059 20020911 00059 SO 2002 9 11 C2XA02TY128 1 20020904 A 5311 1452563003 FRAME EMB 145 EMB145 3260210 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED 2-C INSPECTION, MAINTENANCE FOUND CHAFING ON FRAME 70 AT STRINGER 13R. MAINTENANCE INSPECTED AN D BLENDED AREA,THEN ALODINE, PRIME AND PAINTED IAW EMB 135/145 SRM 51-102. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEAS ED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002090500001 20020905 00001 NM 2002 9 5 S02832028 1 20020711 A 3200 GOODYR MWT BOEING 737 737800* NM CFMINT CFM56 CFM567B26US NE #3/4 M/W/T, RH I W SAJF O OTHER O OTHER TX TAXI/GRND HDL 1 WP 03 30173 B18612 GRD CHK FOUND THROWN TREAD ON #4 TIRE. RH I/B AFT FLAP GOT DENTS DUE TO DEBRIS STRIKEN.C/A:1.RPLD #3 & #4 TIRE IA W AMM 32-45-1. 2.CHK FOUND DENTS WERE WITHIN LIMIT IAW SRM 57-53-01 THEN C/F TO D/D, FLAP SSYS TESTED NML. 3 TEMPORARY R EPAIR DENTS ON RH I/B T/E AFT FLAP IAW SRM 57-53-01, 51-70-10 & EON 738-57-00-0006. ON JUL 11 2002. 4.RPLD RH I/B AFT FL AP ASSY IAW AMM 27-51-12 AND D/D CLEAR ON JUL 14 2002. 5.EON MUL -32-636630-0009 IS ISSUED FOR PEELED RID OF TIRE RPLD I NFO. 6.PER BOEING 737-SL-57-080R0, EO 738-57-00-0009 IS USSUED FOR INBD AFT FLAP LOWER SURFACE FOD DEBRIS PROTECTION. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002090500002 20020905 00002 NM 2002 9 5 2002F00838 1 20020716 A 3350 SIGN BOEING 727 727225 1384077 NM AFT AIRSTAIR INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 DURING PREFLIGHT TRANSIT, FOUND AFT AIRSTAIR STAIRWELL EMERGENCY EXIT LIGHT SIGN INOPERATIVE. REMOVED AND REPLACED AFT AIRSTAIR STAIRWELL EMEREGNCY EXIT LIGHT ASSEMBLY AND OPS CHECKED SATISFACTORY AS PER MM 33-50-0. (M) 2 L 7 3 4F A3WE 2002090500013 20020905 00013 SW 2002 9 5 2002F00849 1 20020327 A 5270 SWITCH FRCHLD SA227 SA227DC 3377521 SW CARGO DOOR CONTAMINATED A BSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 05 453LS DC852B DFW - FLT 1316 - FOUND CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB. CREW RETURNED TO BASE. LIGHT WENT OUT ON LANDING . STICKY HANDLE OR CLICK CLACKS, OR DOOR CLOSING PROCEDURES. CLEANED AND LUBED CARGO DOOR LIGHT SWITCHES AND CLICK CLA CKS. CARGO DOOR LIGHT OPS CHECK NORMALLY. TEST FLIGHT WAS COMPLETED WITH NO PROBLEMS NOTED ON THE TEST FLIGHT. (M) 2 L 7 2 4T RT A18SW 2002090500014 20020905 00014 SW 2002 9 5 2002F00850 1 20020331 A 2120 20475546 ACM FRCHLD SA227 SA227DC 3377521 SW LEFT FAILED A BSAA O OTHER J WARNING INDICATION DE DESCENT 1 NM 05 60NE 5902 AC760B FLT 2591 - GEG - DURING DESCENT, CO-PILOT NOTICED THE CABIN TEMP DIDN'T RESPOND TO TEMP CONTROLLER IN AUTO OR MANUAL MOD E. THE CABIN TEMP KEPT ON RISING, AND PEAKED AT 90F UPON PARKING ON THE RAMP. THE CREW NOTICED A LIGHT HAZE IN THE CAB IN WHEN DEPLANING, ALONG SLIGHT OIL SMELL. THE CREW RAN THE ENGINES AFTER PASSENGERS HAD DEPLANED AND VERIFIED THE PROB LEM TO BE THE LEFT SIDE BLEED. IT WAS SUSPECTED THE LT ACM HAD FAILED. REPLACED ACM, SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A18SW 2002090500015 20020905 00015 WP 2002 9 5 2002F00851 1 20020521 A 2560 P4010021 FLASHLIGHT DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND EMERGENCY FLASHLIGHT INOPERATIE IN AFT GALLEY, RIGHT FLIGHT ATTENDANTS SEAT. (M) 2 L 7 3 4F A22WE 2002090500016 20020905 00016 WP 2002 9 5 2002F00852 1 20020514 A 5320 STANCHION DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT WASTE SYSTEM COMPARTMENT, IN THE AREA OF ALL THREE BULKHEAD STANCIONS WHERE THEY ATTA CH TO THE INTERCOSTALS, AT STATION 1977. (M) 2 L 7 3 4F A22WE 2002090500017 20020905 00017 WP 2002 9 5 2002F00853 1 20020521 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON LONGERON 44L, AT STATION 879, APPROXIMATELY 13 INCHES LONG. (M) 2 L 7 3 4F A22WE 2002090500018 20020905 00018 NM 2002 9 5 2002F00854 1 20020529 A 5347 SEAT TRACK BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND SEAT TRACK WITH CORROSION AROUND NUTPLATES, AT STATION 780-846, LBL 48. (M) 2 L 7 3 4F A3WE 2002090500019 20020905 00019 WP 2002 9 5 AALA20020142 1 20020622 A 2613 SENSOR DOUG DC9 DC982 3022082 WP TAIL SECTION MALFUNCTIONED A AALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 483A 49676 DFW - FLT 1039 - EN ROUTE DFW-PHX - AFTER TAKEOFF DFW TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. COMPLETED CH ECKLIST AND LIGHT EXTINGUISHED THEN RE-ILLUMINATED AND FINALLY EXTINGUISHED. RETURNED AND LANDED DFW WITHOUT INCIDENT. INSPECTED TAIL COMPARTMENT AREA FOR LEAKS. NO LEAKS NOTED, PRECAUTIONARY REPLACED LEFT AND RIGHT TEMPERATURE SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002090500020 20020905 00020 EU 2002 9 5 MALA020472 1 20020818 A 2120 ODOR BAC 146 AVRO146RJ85A 1500097 EU CABIN DETECTED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 535XJ E2371 DURING FLIGHT 3520 AFT F/A SMELLED SULPHUR BURNING SMELL IN AFT CABIN FOLLOWED BY MELTED PLASTIC SMELL. FLIGHT CREW SME LLED IT BRIEFLY BUT SMELL LINGERED IN AFT CABIN. MAINTENANCE INSPECTED ELECTRICAL COMPONENTS. ABOVE AFT CEILING PANELS AND ALL LIGHTING, PA SYSTEM, AIR SYSTEMS AND CIRCUIT BREAKERS. NO DEFECTS NOTED. ALL ASSOCIATED SYSTEMS OPERATED NORM ALLY. COULD NOT DUPLICATE DISCREPANCY. 2 H 7 4 4F RT A49EU 2002090500021 20020905 00021 WP 2002 9 5 AALA20020176 1 20020627 A 3350 60030451 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 409AA 49320 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD OVERHEAD EMERGENCY EXIT LIGHTS IN TAIL CONE INOPERATIVE. RESEATED FORWARD O VERHEAD EMERGENCY EXIT LIGHTS IN TAIL CONE BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002090500022 20020905 00022 WP 2002 9 5 AALA20020804 1 20020521 A 5510 STRUCTURE DOUG DC9 DC982 3022082 WP HORIZONTAL STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 232AA 49179 TUL - FOUND RIGHT HORIZONTAL STABILIZER, MID LOWER SECTION, MIDDLE PLANK HAS APPROX 6 INCHES DAMAGED AREA WITH CRACK. R EPAIRED PER ESO 80559 DATED 5/20/02. (M) 2 L 7 2 4F A6WE 2002090500023 20020905 00023 WP 2002 9 5 AALA20020805 1 20020521 A 5511 STRINGER DOUG DC9 DC982 3022082 WP HORIZONTAL STAB DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 232AA 49179 TUL - FOUND STRINGER IS DENTED FROM SKIN DAMAGE AT INSIDE, FORWARD AREA OF HORIZONTAL L/E, RIGHT SIDE MIDDLE LOWER SECTI ON MIDDLE PLANK. REPAIRED PER ESO 80559 DATED 5/20/02. (M) 2 L 7 2 4F A6WE 2002090500024 20020905 00024 WP 2002 9 5 AALA20020806 1 20020530 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7540A 49994 TUL - FOUND NR 3 AFT CABIN SEAT TRACK CORRODED FROM STATION 1145-1309. REMOVED DAMAGED SECTION OF NR 3 SEAT TRACK. SPLI CED IN NEW SECTION OF TRACK FROM STATION 1145 TO 1309 PER SRM 53-05 FIG 4F, SHEET 1. (M) 2 L 7 2 4F A6WE 2002090500025 20020905 00025 WP 2002 9 5 AALA20020807 1 20020510 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND SEAT TRACK NR 6 CORRODED STATION 451-458. INSTALLED SLAT TRACK REPAIR PER SRM 53-05 FIG 4A SHEET 1 AND 2. (M) 2 L 7 2 4F A6WE 2002090500026 20020905 00026 WP 2002 9 5 AALA20020808 1 20020516 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1236 AND 1208. REPAIRED DAMAGED AREAS PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2002090500027 20020905 00027 WP 2002 9 5 AALA20020809 1 20020516 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND SHEAR TIE CRACKED AFT SIDE OF 1437 FRAME BETWEEN L1 AND L2R. INSTALLED NEW SHEAR TIE SRM 51-01. (M) 2 L 7 2 4F A6WE 2002090500028 20020905 00028 WP 2002 9 5 AALA20020810 1 20020501 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND STATION 1306 ABOVE LONGERON 19R SKIN GOUGED. CUT OUT GOUGED AREA AND INSTALLED INTERNAL DOUBLER AND PLUG PE R SRM 53-04 FIG 38 SHT 24 AND INSTALLED SCUFF PLATE PER AARD 53-30-00-8. (M) 2 L 7 2 4F A6WE 2002090500029 20020905 00029 EU 2002 9 5 MALA020473 1 20020819 A 2613 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 142XJ ON TAKEOFF OF FLIGHT 3001, RECEIVED RIGHT TAILPIPE HOT CWP AND MASTER WARNING AFTER GEAR RETRACTION. REDUCED POWER TO 3 0 PERCENT TORQUE, COMPLETED QRH, LIGHT WENT OFF AFTER APPROXIMATELY 5 MINUTES. DID NOT SHUT ENGINE DOWN. AIR RETURN TO FWA. MADE AND EMERGENCY LANDING IN FWA. MAINTENANCE ACCOMPANIED CREW FOR HIGH POWER RUN-UP. RAN ENGINES UP TWICE TO FULL POWER AND COULD NOT DUPLICATE TAIL PIPE PROBLEM. AIRCRAFT OK FOR RETURN TO SERVICE. 2 L 7 2 4T RT A52EU 2002090500030 20020905 00030 WP 2002 9 5 AALA20020811 1 20020531 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND CORROSION UNDER FASTENERS ON INSIDE FRAME AT STATION 1463. INSTALLED DOUBLER PER ESO DATED 5-30-02, SPOT FA CED CORROSION AREAS. STRAP INSTALLED, 2 ROWS OF FASTENERS. (M) 2 L 7 2 4F A6WE 2002090500031 20020905 00031 EU 2002 9 5 MALA020483 1 20020816 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING 4K/2Y/4Y INSPECTION IN CWA, FRAME ANGLES STA 258 HAS CORROSION. MAINTENANCE REMOVED CORROSION AND REPAIRED FRAME IAW EO NR S53108. 2 L 7 2 4T RT A52EU 2002090500032 20020905 00032 EU 2002 9 5 MALA020484 1 20020816 A 5321 FLOORBOARD SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING 4K/2Y/4Y INSPECTION IN CWA, FLOOR BOARD WEB STA 288 HAS SEVERAL RIVETS, CORRODED AND CORROSION FWD OF SEAT 1A, C/ D. MAINTENANCE REMOVED AND REPLACED STA 288 WEB IAW SRM 51-00-00. 2 L 7 2 4T RT A52EU 2002090500033 20020905 00033 EU 2002 9 5 MALA020485 1 20020816 A 1430 RIVET SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING 4K/2Y/4Y INSPECTION IN CWA, RIVETS ON FRAME ANGLE AT STA 236 HAVE CORROSION. MAINTENANCE REMOVED CORROSION AND R EPLACED RIVETS AS REQUIRED IAW SRM 51-70-40 AND 51-40-21. 2 L 7 2 4T RT A52EU 2002090500034 20020905 00034 EU 2002 9 5 MALA020486 1 20020816 A 5260 CHANNEL SAAB SF340 340B 7860101 EU AIRSTAIRS CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING 4K/WY/4Y INSPECTION IN CWA, AIRSTAIR U-CHANNEL HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090500035 20020905 00035 WP 2002 9 5 AALA20020812 1 20020517 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FLOORBEAM CRACKED, STATION 927, LBL 56. REMOVED AND INSTALLED NEW FLOORBEAM PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002090500036 20020905 00036 EU 2002 9 5 MALA020487 1 20020816 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING 4K/2Y/4Y INSPECTION IN CWA, GALLEY I/B SEAT TRACK PROFILE HAS CORROSION AT AFT PORTION. MAINTENANCE REMOVED CORR OSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090500037 20020905 00037 WP 2002 9 5 AALA20020813 1 20020513 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND NR 2 SEAT TRACK CORRODED STATION 1193. INSTALLED PLUG REPAIR AS PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2002090500038 20020905 00038 WP 2002 9 5 AALA20020814 1 20020522 A 5310 THRESHOLD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND CORROSION ON FORWARD CARGO DOOR FRAME, LOWER THRESHOLD AT STATION 405. REMOVED AND REPLACED SECTION OF PAN (THRESHOLD) PER SRM 53-05 FIG 44. (M) 2 L 7 2 4F A6WE 2002090500039 20020905 00039 WP 2002 9 5 AALA20020815 1 20020520 A 5553 ATTACH ANGLE DOUG DC9 DC982 3022082 WP EMPENNAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND CRACK BETWEEN RIVETS ON VERTICAL STABILIZER TO FUSELAGE RIGHT ATTACH ANGLE 8 INCHE FORWARD OF VERTICAL REAR SPAR ATTACH POINT. CUT OUT DAMAGED AREA. INSTALLED DOUBLER ANGLE PER AARD 53-10-00-2. (M) 2 L 7 2 4F A6WE 2002090500040 20020905 00040 WP 2002 9 5 AALA20020816 1 20020514 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - ROUTED FRAME PREVIOUSLY WITHOUT REPAIR. INSTALLED STRAP REPAIR PER AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2002090500041 20020905 00041 WP 2002 9 5 AALA20020817 1 20020514 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND CORROSION ON BOTTOM SIDE OF LEFT CUSP STATION 617-622. REMOVED CORROSION AND INSTALLED DOUBLER AS PER SRM 5 3-01 PAGE 18. (M) 2 L 7 2 4F A6WE 2002090500042 20020905 00042 WP 2002 9 5 AALA20020818 1 20020514 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND CORROSION TOP CUSP STATION 549-533, LEFT SIDE. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01 PAGE 1 8. (M) 2 L 7 2 4F A6WE 2002090500043 20020905 00043 WP 2002 9 5 AALA20020819 1 20020529 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND TOP FLANGE OF INTERCOSTAL CRACKED AT TWO FASTENER HOLES BELOW CABIN FLOOR, BL0. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002090500044 20020905 00044 EU 2002 9 5 MALA020488 1 20020820 A 7997 WIRE SAAB SF340 340B 7860101 EU RT ENGINE PULLED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 442XJ 340B442 DURING CLIMBOUT ON FLIGHT 3251, RIGHT PROP OIL TEMP READ 100 DEGREES CELSIUS, FOR APPROXIMATELY 15 MINUTES WITH CLIMB PO WER SET. PROP PRESSURE NORMAL, PROP FUNCTION NORMAL. AIR RETURN TO MSP. MAINTENANCE WITH ENGINE STATIC FOUND RIGHT PR OP OIL TEMP INDICATOR PEGGED TO MAX TEMP FOUND ONE WIRE PULLED OUT OF PIN ON CANNON PLUG AT TEMP BULB. REPLACED PIN SYS TEM, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002090500045 20020905 00045 WP 2002 9 5 AALA20020820 1 20020531 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND WEB CORRODED SEVERAL AREAS FS 1213-1215 ABOVE L28R WEB BLOWN OUT. INSTALLED NEW WEB PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002090500046 20020905 00046 WP 2002 9 5 AALA20020840 1 20020516 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7532A 49924 TUL - FOUND STATION 1160-1165 CUSP CORRODED, RIGHT SIDE OF CABIN. DOUBLER REPAIRED CUSP STATION 1160-1165 RIGHT SIDE PE R AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002090500047 20020905 00047 EU 2002 9 5 MALA020489 1 20020820 A 2932 HE152581 PRESSURE SWITCH BAC 146 AVRO146RJ85A 1500097 EU HYD SYSTEM LEAKING A MALA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 532XJ E2366 DURING LANDING FLIGHT NR 3526 LOST GREEN HYDRAULIC SYSTEM UPON LANDING ROLLOUT AND TAXI INTO GATE. MAINTENANCE INSPECTE D HYDRAULIC BAY FOR LEAKS, FOUND GREEN SYSTEM EDP PRESSURE SWITCH LEAKING. REPLACED PRESSURE SWITCH IAW AMM 29-37-11-20 2. NO LEAKS NOTED. SERVICED GREEN SYSTEM WITH 4 QTS OF FLUID REF AMM 12-10-29. A/C OK FOR SERVICE. 2 H 7 4 4F RT A49EU 2002090500048 20020905 00048 WP 2002 9 5 AALA20020841 1 20020520 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND CREASE IN SKIN ALONG FRAME AND SEVERAL DENTS IN SKIN STATION 277 ABOVE LONGERON 18L. INSTALLED REPAIR DOUBL ER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2002090500049 20020905 00049 WP 2002 9 5 AALA20020843 1 20020524 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND TWO DEEP DENTS IN SKIN STATION 452 BETWEEN LONGERON 22 AND 23L. INSTALLED PERMANENT EXTERNAL REPAIR PER SRM 53-04 FIG 12B SHEET 4, 5, 6 95 AND 96. (M) 2 L 7 2 4F A6WE 2002090500050 20020905 00050 WP 2002 9 5 AALA20020844 1 20020603 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7541A 49995 TUL - FOUND DOOR BEAM HAS NUMEROUS AREAS OF CORRSOSION. DOUBLER INSTALLED PER AARD 53-10-03. (M) 2 L 7 2 4F A6WE 2002090500051 20020905 00051 EU 2002 9 5 MALA020490 1 20020821 A 3350 COVER SAAB SF340 340B 7860101 EU CABIN LOOSE A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 407XJ 340B407 ON FLIGHT 3301, FLOOR TRACK EMERGENCY LIGHTING COVER FROM ROW 2-3 NOT SECURE. MAINTENANCE RESECURED EMERGENCY FLOOR TRA CK LIGHTING. OPERATION AND SECURITY CHECK GOOD. 2 L 7 2 4T RT A52EU 2002090500052 20020905 00052 WP 2002 9 5 AALA20020845 1 20020529 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7541A 49995 TUL - FOUND CRACK IN RADIUS OF LONGERON 4L AT STATION 160. REMOVED CRACKED SECTION OF 4L LONG AT STATION 160 OF INSTALL ED NEW SECTION PER SRM 53-02-00. (M) 2 L 7 2 4F A6WE 2002090500053 20020905 00053 WP 2002 9 5 AALA20020846 1 20020528 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7541A 49995 TUL - FOUND HOLE IN OUTBOARD FLANGE OF NR 5 SEAT TRACK AT STATION 205. INSTALLED STRAP ON OUTBOARD FLANGE OF NR 5 SEAT TRACK STATION 205 PER 53-20-00-13, TREATED AND PRIMED. (M) 2 L 7 2 4F A6WE 2002090500054 20020905 00054 WP 2002 9 5 AALA20020847 1 20020603 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7541A 49995 TUL - FOUND CORROSION ON NR 6 SEAT TRACK NR 2 GALLEY AREA. REPAIRED PER AARD 53-20-00-04. (M) 2 L 7 2 4F A6WE 2002090500055 20020905 00055 EU 2002 9 5 MALA020493 1 20020818 A 5320 BEAM SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 DURING 4K INSPECTION IN CWA, LT ANGLE BEAM BETWEEN FRAMES 258 AND 236.5 (LBL 10) HAS CORROSION. MAINTENANCE REMOVED COR ROSION IAW 51-20-41. 2 L 7 2 4T RT A52EU 2002090500056 20020905 00056 WP 2002 9 5 AALA20020848 1 20020523 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7540A 49994 TUL - FOUND CORROSION ON NR 4 SEAT TRACK AT STATION 234. REMOVED AND REPLACED SEAT TRACK NR 4 FROM STATION 265 TO STATI ON 200 WITH NEW SEAT TRACK PER MD-80 SRM 53-05 SRM 53-05 PAGE 106 FIG 4F. (M) 2 L 7 2 4F A6WE 2002091200096 20020912 00096 NM 2002 9 12 F3LA200200252 1 20020828 A 5330 SKIN BOEING 737 73736Q 1384409 NM FUSELAGE GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 307FL 3196 28760 DURING C-5 CHECK, INSPECTION REPORTED SMALL GOUGE IN OUTER FUSELAGE SKIN AT BS 203, STR 18R. REPAIRED DAMAGE PER SRM 53 -00-01 FIG 202. 2 L 7 2 4F RT A16WE 2002090500057 20020905 00057 WP 2002 9 5 AALA20020852 1 20020604 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND NR 1 SEAT TRACK HAS CORRODED AT GALLEY BOLT HOLE STATION 1174. INSTALLED NEW NR 1 SEAT TRACK STATION 1174-1 309 SRM 51-01. (M) 2 L 7 2 4F A6WE 2002090500058 20020905 00058 WP 2002 9 5 AALA20020853 1 20020531 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND CRACK IN SHEAR TIE. REMOVED AND REPLACED SHEAR TIE SRM 51-01. (M) 2 L 7 2 4F A6WE 2002090500059 20020905 00059 EU 2002 9 5 MALA020494 1 20020819 A 5320 BEAM SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 DURING 4K INSPECTION IN CWA, LT GALLEY BEAM STA 258 LBL 15 HAS CORROSION. MAINTENANCE REMOVED CORROSION ON GALLEY BEAM STA 258 IAW SRM 51-70-40. FOUND ATTACHING ANGLE TO BE CORRODED. REMOVED AND REPLACED ANGLE. 2 L 7 2 4T RT A52EU 2002090500060 20020905 00060 WP 2002 9 5 AALA20020854 1 20020603 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND CUSP BETWEEN SEAT TRACK 1 AND 2 CORRODED. INSTALLED NEW CUSP FROM 1279-1309 PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002090500061 20020905 00061 EU 2002 9 5 MALA020495 1 20020818 A 5260 CHANNEL SAAB SF340 340B 7860101 EU AIRSTAIRS CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 DURING 4K INSPECTION IN CWA, AIRSTAIR SLIDE CHANNEL HAS CORROSION. MAINTENANCE REPAIRED CORROSION IAW SRM CHAP 51. 2 L 7 2 4T RT A52EU 2002090500062 20020905 00062 WP 2002 9 5 AALA20020894 1 20020609 A 4990 O-RING DOUG DC9 DC982 3022082 WP APU FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 577AA 53154 BOS - FLT 1835 - EN ROUTE BOS-DFW, AFTER TAKEOFF A HOT MISTY ODOR WAS PRESENT IN COCKPIT FOLLOWED BY FLIGHT ATTENDANTS R EPORTING SMOKE FILLING THE CABIN, SOME IN COCKPIT, FLIGHT ATTENDANTS REPORTED SMOKE WAS ORIGINATING AROUND ROWS 17 AND 1 8. DECLARED EMERGENCY, RETURNED TO TO BOS AND LANDED WITHOUT INCIDENT. SMOKE DISSIPATED DURING DESCENT AND LANDING. T AXI TO GATE WAS UNEVENTFUL. REPLACED APU O-RING AT MAGNETIC DRAIN PLUG. REPLACED LEFT COALESCERS BAG. ACCOMPLISHED PA CK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002090500063 20020905 00063 EU 2002 9 5 MALA020496 1 20020818 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 DURING 4K INSPECTION IN CWA, RT GALLEY I/B SEAT TRACK PROFILE HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-2 0-91. 2 L 7 2 4T RT A52EU 2002090500064 20020905 00064 WP 2002 9 5 AALA20020906 1 20020623 A 2613 SENSOR DOUG DC9 DC983 3022083 WP TAIL DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 594AA 53284 LAS - FLT 1598 - EN ROUTE LAS-ORD, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF FROM LAS. RETURNED LAS AND LAND WITHOUT INCIDENT. REPLACED BOTH LEFT AND RIGHT TAIL COMPARTMENT TEMPERATURE SENSORS. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002090500065 20020905 00065 NM 2002 9 5 AALA20020907 1 20020624 A 3350 LIGHT BOEING 767 767323 1385205 NM AFT CARGO INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 381AN 25450 SFO - DURING OVERNIGHT MAINTENANCE, EXTERNAL EMERGENCY EXIT LIGHT FORWARD OF AFT CARGO PIT DOOR INOPERATIVE. ADJUSTED E XTERNAL EMERGENCY EXIT LIGHT SOCKET FORWARD OF AFT CARGO PIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002090500066 20020905 00066 WP 2002 9 5 AALA20020908 1 20020623 A 2613 SENSOR DOUG DC9 DC982 3022082 WP TAIL MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 585AA 53248 DFW - FLT 1682 - EN ROUTE DFW-TPA - WHILE CLIMBING THROUGH 14,000 FEET TAIL COMPARTMENT TEMPERATURE HIGH ILLUMINATED ON DEPARTURE. THE LIGHT EXTINGUISHED SHORTLY AFTER THE EMERGENCY PROCEDURES WERE ACCOMPLISHED, BUT RE-ILLUMINATED AGAIN SE VERAL TIMES. AN EMERGENCY RETURN TO DFW WAS ACCOMPLISHED. LANDED DFW WITHOUT INCIDENT. REPLACED TAIL COMPARTMENT TEMP ERATURE SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002090500067 20020905 00067 EU 2002 9 5 MALA020497 1 20020819 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 DURING 4K INSPECTION IN CWA, FRAME AND ANGLE AT STA 258 HAS CORROSION. MAINTENANCE REMOVED CORROSION ON FRAME IAW SRM 5 1-70-40. REMOVED AND REPLACED ANGLE IAW SRM CHAP 51. 2 L 7 2 4T RT A52EU 2002090500068 20020905 00068 EU 2002 9 5 MALA020498 1 20020819 A 5320 BEAM SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 DURING 4K INSPECTION IN CWA, RT BEAM AND ANGLE BETWEEN STA 272 AND 288 HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED ANGLE, REMOVED CORROSION AND REPAIRED BEAM IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090500069 20020905 00069 EU 2002 9 5 MALA020499 1 20020819 A 1430 RIVET SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 DURING 4K INSPECTION IN CWA, WEB AT STA 294 HAS CORRODED FASTENERS. MAINTENANCE REMOVED AND REPLACED RIVETS. 2 L 7 2 4T RT A52EU 2002090500070 20020905 00070 EU 2002 9 5 AALA20020909 2 20020620 A 7310 LINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU LT ENGINE LEAKING A AALA E A ENGINE SHUTDOWN UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 1460A 11480 MEM - FLT 2069 - EN ROUTE CVG-DFW, CREW NOTED 500 POUND FUEL IMBALANCE DURING CLIMB-OUT. ALSO NOTED DIFFERENCE IN FUEL FLOW IN LEFT ENGINE. IN-FLIGHT FUEL CHECKLIST COMPLETED. SHUT DOWN LEFT ENGINE, AND TOOK EMERGENCY DIVERSION TO MEM. LANDED MEM WITH FUEL ODOR IN COCKPIT. ACCOMPLISHED EMERGENCY EVACUATION USING SLIDES. REPAIRED FUEL INTAKE COOLING LIN E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT 2002090500071 20020905 00071 NM 2002 9 5 AALA20020910 1 20020627 A 3350 LIGHT BOEING 767 767223 1385123 NM L1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 317AA 22319 SFO - DURING OVERNIGHT MAINTENANCE, EXTERIOR EMEREGNCY EXIT LIGHT AT L1 DOOR INOPERATIVE. CLEANED EXTERIOR EMERGENCY EX IT LIGHT SOCKET AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002090500072 20020905 00072 NM 2002 9 5 AALA20020913 1 20020629 A 3350 LIGHT BOEING 767 767323 1385205 NM L1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 387AM 27184 SFO - DURING OVERNIGHT MAINTENANCE, EXTERIOR EMERGENCY L1 DOOR LIGHT INOPERATIVE. REPLACED EXTERIOR EMERGENCY LIGHT SOC KET AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002090500073 20020905 00073 NM 2002 9 5 AALA20020948 1 20020628 A 3397 CONNECTOR BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 368AA 25195 ORD - FOUND SEAT 28AB EMERGENCY LIGHTS INOPERATIVE. RECONNECTED EMEREGNCY LIGHT CONNECTOR PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002090500074 20020905 00074 EU 2002 9 5 MALA020500 1 20020819 A 1430 FASTENER SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 DURING 4K INSPECTION IN CWA, LT AND RT CENTER AISLE SEAT TRACK CLIPS ARE CORRODED. MAINTENANCE REMOVED AND REPLACED COR ROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090500075 20020905 00075 WP 2002 9 5 AALA20020950 1 20020628 A 2613 GASKET DOUG DC9 DC982 3022082 WP ACM BAY FAILED A AALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 21 208AA 49159 LAS - FLT 322 - EN ROUTE LAS-DFW TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING ROTATION. TEMPERATURE LIGHT EXTINGUISHED WHEN POWER WAS REDUCED, ILLUMINATED WITH HIGHER POWER SETTING. RETURNED LAS AND LANDED WITHOUT INCIDENT. REPLACED RIGHT AIR CONDITIONING SUPPLY HIGH TEMPERATURE SENSOR GASKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002090500076 20020905 00076 WP 2002 9 5 AALA20020951 1 20020629 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 426AA 49338 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN OVERHEAD BETWEEN AFT LAVATORIES INOPERATIVE. TIGHTENED EME RGENCY EXIT LIGHTS BATTERY IN PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002090500077 20020905 00077 WP 2002 9 5 AALA20020952 1 20020629 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7541A 49995 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM SEAT 20 FORWARD INOPERATIVE. REPLACED EMERGENCY EXIT LIG HTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002090500078 20020905 00078 NM 2002 9 5 AALA20020953 1 20020702 A 3397 CONNECTOR BOEING 777 777223 1385213 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 ORD - DURING OVERNIGHT MAINTENANCE, EMEREGNCY EXIT PATH LIGHTS AT SEATS 4D AND 4G INOPERATIVE. SECURED EMERGENCY EXIT P ATH LIGHTING CONNECTOR AT SEAT 4D AND 4G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002090500079 20020905 00079 EU 2002 9 5 MALA020503 1 20020821 A 2612 LOOP SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A MALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 41XJ 340A041 AFTER PUSHBACK FOR FLIGHT 3085, RT TAILPIPE HOT LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. LT ENGINE HAD NOT YET BEEN STARTED. MAINTENANCE REMOVED AND REPLACED RT NACELLE PANEL 464AT AS REQUIRED FOR OHMS CHECK. OHM/OPS CHECK GOOD PER AM M 26-12-05. 2 L 7 2 4T RT A52EU 2002090500080 20020905 00080 NM 2002 9 5 AALA20020958 1 20020702 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 192AN 32386 MIA - EMERGENCY LIGHT AT ROW 24 AND L4 DOOR INOPERATIVE. SECURED LOOSE CONNECTION AT ROW 24. RELAMPED L4 DOOR EMERGENC Y LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002090500081 20020905 00081 NM 2002 9 5 AALA20020959 1 20020701 A 3397 HARNESS BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 392AN 29429 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT SEAT 20C INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHTING WIRE HARNESS AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002090500082 20020905 00082 WP 2002 9 5 AALA20020960 1 20020701 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP LIGHT BATTERY DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7521A 49898 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS BETWEEN ROW 13-16 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHTS BATTERY CONTACTS. SYTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002090500083 20020905 00083 WP 2002 9 5 AALA20020961 1 20020701 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7531A 49923 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD LEFT OVERWING EMERGENCY EXIT LIGHT SIGN INOPERATIVE. TIGHTENED WIRE ON CONN ECTOR TO FORWARD LEFT OVERWING EMEGENCY EXIT LIGHT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002090500084 20020905 00084 WP 2002 9 5 AALA20020962 1 20020702 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 283AA 49296 DFW - DURING OVERNIGHT MAINTENANCE, EMEREGNCY EXIT LIGHTS IN TAIL INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002090500085 20020905 00085 WP 2002 9 5 AALA20020963 1 20020702 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 440AA 49459 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS FROM ROW 23-26 INOPERATIVE. RESEATED EMERGENCY EXIT L IGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. 9M) 2 L 7 2 4F A6WE 2002090500086 20020905 00086 NM 2002 9 5 AALA20020964 1 20020704 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 632AA 24590 FOUND SEAT 9D EMERGENCY PATH LIGHTS INOPERATIVE. FOUND BAD CONNECTOR AT MUX COVER UNDERSEAT. REPLACED CONNECTOR. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002090500087 20020905 00087 WP 2002 9 5 AALA20020965 1 20020704 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 248AA 49259 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROW 8 THROUGH 11 DIM. RESEATED CEILING EMEREGNCY E XIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002090500088 20020905 00088 WP 2002 9 5 AALA20020966 1 20020704 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 203AA 49145 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT TAIL CONE DIM. CLEANED EMERGENCY EXIT LIGHTS SOCKET. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002090500089 20020905 00089 WP 2002 9 5 AALA20020967 1 20020704 A 2432 AAP3274A CHARGER DOUG DC9 DC982 3022082 WP E/E COMPT FAILED A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 271AA 49293 DTW - FLT 1281 - EN ROUTE PVED-ORD, BATTERY CHARGER OFF LIGHT ILLUMINATED, CIRCUIT BREAKER REPORTED OPEN. CREW DECLARED EMERGENCY AND COMPLIED WITH PROCEDURES. DIVERTED AND LANDED DTW WITHOUT INCIDENT. REPLACED MAIN BATTERY CHARGER. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002091200097 20020912 00097 NM 2002 9 12 F3LA200200253 1 20020828 A 5754 SKIN BOEING 737 7372P6 1C84609 NM L/E SLAT CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 272 3197 21613 DURING C-2 CHECK, INSPECTION REPORTED LT WING NR 1 SLAT LOWER SKIN CRACKED AT LAST ROW OF RIVETS, OUTBOARD OF MAIN TRACK . REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER SRM 57-43-01. 2 L 7 2 4F RT A16WE 2002090500090 20020905 00090 NE 2002 9 5 AALA20020969 2 20020705 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 2 FAILED A AALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 21 477AA 49652 IND - FLT 772 - EN ROUTE DFW-LGA - DURING CRUISE AT 37,000 FEET, RIGHT ENGINE FAILED. N2 SUDDENLY WENT TO ZERO AND OIL PRESSURE WENT TO ZERO. OIL QUANTITY WAS OVER 12 QUARTS. NO FIRE INDICATIONS. DIVERTED AND LANDED IND WITHOUT INCIDENT . REPLACED NR 2 ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 2002090500091 20020905 00091 2002 9 5 MALA020506 4 20020824 A 3425 6227713004 COMPUTER SAAB SF340 340B 7860101 EU NR 2 FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 439XJ 340B439 DURING CLIMBOUT OF FLIGHT 3108, F/O'S EADI AND EHSI SHOWED XXSIDE DATA ON INITIAL CLIMBOUT. HEADING BUG WOULD SHOW LEFT AND RIGHT 15 DEGREES. CAPT SIDE DATA WOULD CHANGE BETWEEN VOR AND LRN MODE. AIR RETURN TO MSP. MAINTENANCE REPLACED N R 2 DPU. NR 2 DPU OPS CHECKS GOOD IAW SF340 MM CHAP 34. 2 L 7 2 4T RT A52EU 2002090500092 20020905 00092 2002 9 5 MALA020508 4 20020826 A 2565 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU CABIN UNSERVICEABLE A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 518XJ E2337 LEFT REAR EVAC SLIDE READS ZERO PSI. MAINTENANCE REPLACED LT REAR ESCAPE SLIDE IAW AVRO JOB CARD 0437, ALL CHECKS GOOD IAW AVRO AMM 25-60-11. 2 H 7 4 4F RT A49EU 2002090500093 20020905 00093 EU 2002 9 5 MALA020509 1 20020826 A 2750 HP14161005 CONTROL VALVE SAAB SF340 SF340A 7850100 EU T/E FLAP FAULTY A MALA L A ABORTED APPROACH UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 15 119XJ 340A119 INBOUND ON FLIGHT 3089, FLAPS WOULD NOT EXTEND. OVERFLEW MCW DIVERTED TO MSP. A/C LANDED WITHOUT INCIDENT. MAINTENANC E REMOVED AND REPLACED FLAP CONTROL VALVE, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002090500094 20020905 00094 EU 2002 9 5 MALA020511 1 20020804 A 5315 FLOORBEAM BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 517XJ E2335 DURING C-CHECK INSPECTION IN CVG, FOUND EVIDENCE OF CORROSION ON FLOORBEAM 18 BETWEEN SEAT RAILS 3/4, 29 INCHES FROM A/C CENTERLINE ON RIGHT SIDE OF A/C. DAMAGE REPAIRED IAW BARA/ARV/6005/02-DC AND EO NR A53090. 2 H 7 4 4F RT A49EU 2002090500095 20020905 00095 EU 2002 9 5 MALA020512 1 20020802 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 517XJ E2335 DURING C-CHECK INSPECTION IN CVG, NR 3 SEAT RAIL SHOWS EVIDENCE OF CORROSION BETWEEN FRAME 18 & 20. MAINTENANCE DAMAGED REPAIRED BY REPLACING SECTION IAW EO A53026, AND SRM 53-00-32. 2 H 7 4 4F RT A49EU 2002090500096 20020905 00096 EU 2002 9 5 MALA020513 1 20020802 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 517XJ E2335 DURING C-CHECK INSPECTION IN CVG, NR 4 SEAT RAIL SHOWS EVIDENCE OF CORROSION BETWEEN FRAME 18 AND 20. MAINTENANCE REPAI RED DAMAGE BY REPLACING SECTION IAW EO NR A53026 AND SRM 53-00-32. 2 H 7 4 4F RT A49EU 2002090500097 20020905 00097 EU 2002 9 5 MALA020470 1 20020816 A 2923 520831 PUMP BAC 146 AVRO146RJ85A 1500097 EU HYD SYSTEM FAILED A MALA K NONE J WARNING INDICATION CR CRUISE 1 GL 15 534XJ E2370 EN ROUTE ON FLIGHT 3566, YELLOW HYDRAULIC LIGHT TEMP ILLUMINATED. MAINTENANCE REPLACED AC PUMP IAW AMM 29-20-11 AND REP LACED YELLOW ISOLATION VALVE. OPS AND LEAK CHECKS, NO DEFECTS NOTED. 2 H 7 4 4F RT A49EU 2002090500098 20020905 00098 EU 2002 9 5 MALA020474 1 20020813 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING 4K/2Y-4Y INSPECTION IN CWA, CARGO AREA SEAT TRACK LBL 18.3 HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION IA W SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090500099 20020905 00099 EU 2002 9 5 MALA020475 1 20020814 A 5320 CHANNEL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING 4K/2Y/4Y INSPECTION IN CWA, LBL 11 CHANNELS BETWEEN FRAMES 236 AND 258 HAVE CORROSION. MAINTENANCE REMOVED CORRO SION, REPLACED BEAM AND ANGLE IAW SRM 51-40-20. 2 L 7 2 4T RT A52EU 2002090500100 20020905 00100 EU 2002 9 5 MALA020476 1 20020814 A 5320 STRUCTURE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING 4K/2Y/4Y INSPECTION IN CWA, CORROSION ON GALLEY FLOOR INTERCONNECTS. MAINTENANCE REMOVED CORROSION IAW SRM 51-20 -42. 2 L 7 2 4T RT A52EU 2002090500101 20020905 00101 EU 2002 9 5 MALA020477 1 20020814 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING 4K/2Y-4Y INSPECTION CARGO AREA SEAT TRACK SIDES HAVE CORROSION AT INFILL PANEL AREA. MAINTENANCE REMOVED CORROSI ON IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090500102 20020905 00102 EU 2002 9 5 MALA020478 1 20020814 A 5320 STRUCTURE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING 4K/2Y/4Y INSPECTION IN CWA, LEFT FWD SEAT TRACK WRAP AROUND HAS CORROSION. MAINTENANCE REMOVED AND REPLACED WRAP AROUND. 2 L 7 2 4T RT A52EU 2002090500103 20020905 00103 EU 2002 9 5 MALA020479 1 20020814 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING 4K/2Y/4Y INSPECTION IN CWA, GALLEY AREA SEAT RAIL HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090500104 20020905 00104 EU 2002 9 5 MALA020480 1 20020814 A 2150 11341041 MOTOR SAAB SF340 340B 7860101 EU A/C BAY MALFUNCTIONED A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 407XJ 340B407 DURING FLIGHT 3297 AT 18,000 FT, SMOKE INFLIGHT DECK AND CABIN. CREW HAD SMOKE GOGGLE ON, SUPPLEMENTAL A/C WAS TURNED O FF AND CONDITIONS IMPROVED. AIR RETURN TO MEM. MAINTENANCE INVESTIGATED AND FOUND SUPPLEMENTAL A/C COMPRESSOR MOTOR AT FAULT. EXCESSIVELY ARCING. MAINTENANCE REMOVED AND REPLACED SUPPLEMENTAL A/C COMPRESSOR MOTOR IAW ARR 8/8/2. 2 L 7 2 4T RT A52EU 2002090500105 20020905 00105 EU 2002 9 5 MALA020481 1 20020815 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING 4K/2Y/4Y INSPECTION IN CWA, ANGLE AT FRAME STA 225 HAS CORROSION. MAINTENANCE REMOVED CORROSION AND REPAIRED ANG LE IAW SRM 51-70-20. 2 L 7 2 4T RT A52EU 2002090500106 20020905 00106 EU 2002 9 5 MALA020482 1 20020815 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING 4K/2Y/4Y INSPECTION IN CWA, NOTED LT CENTER AISLE SEAT TRACK LBL 18.3 CORROSION OUT OF LIMITS AT APPROXIMATELY ST A 300. MAINTENANCE COMPLETED REPAIR IAW EO NR S53060 FROM STA 297 TO 329. 2 L 7 2 4T RT A52EU 2002090500107 20020905 00107 NM 2002 9 5 N8TA02080801 1 20020801 A 5315 BAC1518338 FLOORBEAM BOEING 757 757256 1384925 NM FUSELAGE CORRODED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 508NA 21797 26244 CORROSION ON FLOORBEAM BODY STATION 377.7, LBL 17, WL 208. FLOORBEAM UPPER CHORD FOUND TO BE CORRODED OUT OF LIMITS AT LBL 6, LBL 11, AND LBL 17 PER SRM 53-00-51 FIG 101. FLOORBEAM REPAIRED PER SRM 53-00-51 FIG 205, M/M 51-21-04, AND SRM 51-40-02. 2 L 7 2 4F RT A2NM 2002090500108 20020905 00108 NM 2002 9 5 N8TA02081201 1 20020810 A 5320 146N524607 SILL BOEING 757 757256 1384925 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 508NA 21792 26244 CORROSION ON MOP SILL BS 1647, WL 208, LBL 57. REPLACED PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E12EU 2002090500109 20020905 00109 NM 2002 9 5 N8TA02081901 1 20020729 A 5330 SKIN BOEING 757 757256 1384925 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE GOUGED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 508NA 26244 GOUGE IN OUTER SKIN STA 758, 2 INCHES ABOVE STR 16L. AFTER BLEND, GOUGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-01. IN TERIM REPAIR DOUBLER, DETAILED PER ER 02-0887 PG 1-14. 2 L 7 2 4F 4 F RT A2NM E12EU 2002090500110 20020905 00110 2002 9 5 SWAA021962 4 20020826 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002090500111 20020905 00111 NM 2002 9 5 SWAA021968 1 20020827 A 2731 65C26384 TAB BOEING 737 7373A4 1384585 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED PM CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TA B PER MM. 2 L 7 2 4F RT A16WE 2002090500112 20020905 00112 NM 2002 9 5 SWAA021974 1 20020825 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 EEPLS LOOSE AT ROW NR 2. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002090500113 20020905 00113 2002 9 5 SWAA021975 4 20020828 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002090500114 20020905 00114 NM 2002 9 5 SWAA021976 1 20020824 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 EEPLS LOOSE AT ROW NR 9. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002090500115 20020905 00115 WP 2002 9 5 UPS02839044 1 20020810 A 3350 LIGHT DOUG DC8 DC871F 302199D WP ENTRY DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:N/A, ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. OPS CHECK NORMAL, NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 2002090500116 20020905 00116 WP 2002 9 5 UPS02839074 1 20020813 A 5753 WEB DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:PFLT RT WHEEL WELL FLAP SUPPORT WEB ANGLE CRACKED. FERRIED TO SDF FOR REPAIR PERMIT 9151, D243076. REM OVED FASTENERS IN DAMAGED WEB & SUPPORT BRACKET. REPAIRED WEB PER SRM 57-2-0 FIG 2A. REINSTALLED WEB. 2 L 7 4 4F RT 4A25 2002090500117 20020905 00117 WP 2002 9 5 UPS02839075 1 20020813 A 3233 MOUNT DOUG DC8 DC871F 302199D WP NLG BROKEN A IPXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 748UP 45948 INSPECTION TYPE:N/A ATB - NLG RETRACT CYLINDER AFT MOUNT ASSY BROKE CAUSING DAMAGE TO FUSELAGE SKIN. A/C FERRIED TO TCO FOR REPAIR 9150. TRIMMED DAMAGE ON BULKHEAD IAW REO G08732 STEP NR 1, DYE PENETRATE INSP IAW MIL-271F, NO CRACK NOTED IN CUTOUT. FABBED, DRILLED FASTENER HOLES IN DOUBLER, TRIPLER & FILLERS IAW REO G08732. OK TO ALODINE. FABBED NEW LOW ER STIFFENER IAW DWG 5615530. INSTALLED UPPER & LOWER STIFFENERS FINGER DOUBLER & TRIPLER IAW DC8 SRM 51-1-21 & REOG087 32. 2 L 7 4 4F RT 4A25 2002090500118 20020905 00118 WP 2002 9 5 UPS02839087 1 20020726 A 5320 3755822511 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 STA 340 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 36 AND 35R. REMOVED AND REPLACED FITT ING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002090500119 20020905 00119 WP 2002 9 5 UPS02839089 1 20020726 A 5320 9754020523 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 STA 272 TO 280 LONG 35R INTERCOSTAL LOWER FLANGE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9754020 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002090500120 20020905 00120 WP 2002 9 5 UPS02839090 1 20020807 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1746 AT LONG 35R AND 34R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER, AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2002090500121 20020905 00121 WP 2002 9 5 UPS02839092 1 20020814 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:PFLT RT W/W UPPER INBOARD STIFFENER CRACKED. REMOVED ANGLE, INSTALLED NEW ANGLE IAW SRM 51-1-20. 2 L 7 4 4F RT 4A25 2002090500122 20020905 00122 WP 2002 9 5 UPS02839093 1 20020814 A 5712 PRESSURE PANEL DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:PFLT RT W/W UPPER WEB CRACKED STA XW 5.00 FERRY 9151 TO SDF REF D243078. REPAIRED WEB PER SRM 57-2-0 FI GURE 2A. 2 L 7 4 4F RT 4A25 2002090500123 20020905 00123 WP 2002 9 5 UPS02839094 1 20020814 A 5320 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:PFLT RIGHT W/W AFT OPENING ATTACH ANGLE CRACKED. REMOVED ANGLE, DRILLED NEW ANGLE, INSTALLED NEW ANGLE IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002090500124 20020905 00124 WP 2002 9 5 UPS02839095 1 20020814 A 5720 ANGLE DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:PFLT RIGHT W/W CORROSION FLAP WELL AREA. REPLACED ANGLE. 2 L 7 4 4F RT 4A25 2002090500125 20020905 00125 WP 2002 9 5 UPS02839103 1 20020816 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:N/A EMERGENCY LIGHTS DISARMED, WILL NOT ILLUMINATE. SUSPECT INOP BULB. RELAMPED EMERGENCY LIGHTS, DISA RMED LIGHT. OPS CHECKS OK. 2 L 7 4 4F RT 4A25 2002090500126 20020905 00126 WP 2002 9 5 UPS02839106 1 20020813 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:LNSV NLG BULKHEAD DAMAGED. TRIMMED OUT DAMAGE ON BULKHEAD IAW REO G08732. DYE PENETRANT CHECKED FOR CR ACKS, NONE NOTED. FABRICATED NEW STIFFENER, FILLERS, TRIPLER, AND FINGER DOUBLER PER DAC DWG 5615530 & REO G08732. INS TALLED IAW REO G08732, DC8 SRM 51-1-21, & 51-1-20D. 2 L 7 4 4F RT 4A25 2002090500127 20020905 00127 EU 2002 9 5 MALA020514 1 20020828 A 3230 CONNECTOR SAAB SF340 SF340A 7850100 EU RIGHT FAULTY A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 119XJ 340A119 RIGHT EMERGENCY SEPARATION BOLT CANNON PLUG BAD. MAINTENANCE REMOVED AND REPLACED CANNON PLUG IAW SAAB SRM 20-30-15. 2 L 7 2 4T RT A52EU 2002090500128 20020905 00128 EU 2002 9 5 MALA020515 1 20020828 A 3230 CONNECTOR SAAB SF340 SF340A 7850100 EU LEFT DAMAGED A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 119XJ 340A119 LEFT EMERGENCY SEPARATION BOLT CANNON PLUG DAMAGED. MAINTENANCE REPLACED CANNON PLUG IAW SAAB 340 SRM 20-30-15. 2 L 7 2 4T RT A52EU 2002090500129 20020905 00129 NE 2002 9 5 MALA020516 2 20020818 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT FLAMED OUT A MALA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 GL 15 114XJ 340A114 DURING FLIGHT 3310, LT ENGINE FLAMED OUT WHEN CONDITION LEVER PUT INTO THE MIN/MAX POSITION. ENGINE HUNG UP, THEN GOT I T TO MIN/MAX THE ENGINE FLAMED OUT. MAINTENANCE PERFORMED START ATTEMPT ON LT ENGINE THE LT ENGINE STARTED AND RAN AS R EQUIRED. NO FLAME-OUTS NOTED. NOTED THAT THE LT CONDITION LEVER IS TOUCHY NEAR THE START GATE SUSPECT THAT THE PILOT S LIGHTLY WENT BELOW THE START DETENT WHEN TRYING TO UNSTICK THE CONDITION LEVER, ALL ENGINE PARAMETERS WERE NORMAL AT ALL TIME OF RUNNING. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002090500130 20020905 00130 EU 2002 9 5 MALA020517 1 20020827 A 7931 IPTE1191000200 TRANSDUCER SAAB SF340 SF340A 7850100 EU LT ENGINE FAULTY A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 68XJ 340A068 DURING FLIGHT 3205, LEFT MASTER WARNING ILLUMINATED NOTICED LT ENGINE OIL TEMP AND PRESSURE WENT TO THE BOTTOM OF GAUGE, NOTICED NO ERRATIC ENGINE INDICATIONS. MAINTENANCE REPLACED LT PROP GEARBOX OIL PRESSURE TRANSDUCER IAW SAAB AMM 79-30 -05-4, OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002090500131 20020905 00131 EU 2002 9 5 MALA020518 1 20020826 A 2750 HP14161005 CONTROL VALVE SAAB SF340 340B 7860101 EU T/E FLAP FAILED A MALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 15 411XJ 340B411 DURING FLIGHT 3697, FLAPS WOULD NOT EXTEND. MAINTENANCE CONNECTED BREAKOUT BOX AND FOUND FLAP VALVE INOP. REPLACED VAL VE IAW SAAB AMM 27-51-15-2. ALL CHECKS GOOD, OPS CHECK GOOD IAW SAAB AMM 27-51-00. 2 L 7 2 4T RT A52EU 2002090500132 20020905 00132 EU 2002 9 5 MALA020519 1 20020827 A 2913 4018502 PUMP SAAB SF340 340B 7860101 EU HYD SYSTEM FAILED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 424XJ 340B424 ON FINAL INTO DTW ON FLIGHT 3315, WITH SELECTED GEAR DOWN, HYDRAULIC CAUTION ILLUMINATED ONLY THE NOSE GEAR WAS DOWN. N OTED MAIN HYDRAULIC PRESSURE LOW AND ALL OTHER NORMAL. RAN QRH CHECK LIST, GOT THREE GREEN NORMAL LANDING FOLLOWED HYDR AULIC PUMP DOES NOT RUN IN AUTO OR OVRD. MAINTENANCE REMOVED AND REPLACED HYDRAULIC PUMP ASSEMBLY. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2002091200098 20020912 00098 NM 2002 9 12 F3LA200200254 1 20020824 A 2612 655280915 MODULE BOEING 737 7372L9 1384497 NM FIRE DETECTION MALFUNCTIONED A F3LA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 271FL 77 22734 AIR TURNBACK. FLIGHT CREW REPORTED NR 2 ENGINE FIRE WARNING ILLUMINATED APPROXIMATELY 5 MINUTES AFTER TAKEOFF. FIRE WA RNING WENT OUT WHEN THRUST REDUCED, ALL INDICATIONS NORMAL. WHEN MORE THRUST ADDED, FIRE WARNING ILLUMINATED AGAIN. RE DUCED THRUST TO IDLE THROUGHOUT LANDING, NO FURTHER FIRE WARNING. RAN ENGINE AT IDLE AND AT TAKEOFF POWER. INSPECTED E NGINE FOR LEAKS, NONE NOTED. DETERMINED WHEN SWITCH WAS PLACED IN FIRE FROM NORMAL, ALL INDICATIONS WERE NORMAL AND TES TED OKAY. UPON ARRIVAL IN DEN, REPLACED FIRE CONTROL MODULE AND CHECKED OKAY. REMOVED PLACARD. 2 L 7 2 4F RT A16WE 2002090500133 20020905 00133 EU 2002 9 5 MALA020520 1 20020827 A 3240 BRAKE ASSY SAAB SF340 340B 7860101 EU LT MLG SMOKE A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 444XJ 340B444 DURING FLIGHT 3302, RAMP AGENT CALLED FIRETURCK IN MLI, WHEN IT WAS DISCOVERED DURING TAXIING IN, SMOKE IN LT MAIN BRAKE AREA. MAINTENANCE REPLACED BOTH LT I/B, LT O/B WHEEL ASSEMBLIES AND BRAKES. 2 L 7 2 4T RT A52EU 2002090500134 20020905 00134 EU 2002 9 5 MALA020521 1 20020830 A 7997 WIRE SAAB SF340 340B 7860101 EU LT ENGINE LOOSE A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 364PX 340B262 DURING FLIGHT 3151, CREW REPORTED LT PROP OIL PRESSURE FLUCTUATING. PROP OIL PRESSURE GAUGE GIVES ERRATIC READING FROM 0-200 PSI FOR A MINUTE OR SO, THEN CONTINUES TO GIVE ERRATIC READING. QRH COMPLETE AND MX HAS US TRIP AND RESET C/B J11 . CONDITION CONTINUES. AIR RETURN TO MSP. MAINTENANCE FOUND LOOSE WIRE IN SPLICE. REPLACED SPLICE, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002090500135 20020905 00135 EU 2002 9 5 MALA020522 1 20020830 A 3260 801801 PROXIMITY SENSOR BAC 146 AVRO146RJ85A 1500097 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 517XJ E2335 DURING FLIGHT 3436, GEAR WOULD NOT RETRACT EVEN USING GEAR OVERRIDE. USED RETRACT POSITION SPOILER LIGHT ALSO ILLUMINATE D. MAINTENANCE REMOVED AND REPLACED PROX SENSOR GA11, ON SYSTEM 2 RIGHT LEG OLEO REF AVRO AMM, ALL SYSTEMS NOW CHECK GO OD AT THIS TIME. 2 H 7 4 4F RT A49EU 2002090500136 20020905 00136 EU 2002 9 5 MALA020523 1 20020823 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING 4K-INSPECTION IN CWA, FRAME 225 HAS LIGHT CORROSION ON UPPER FLANGE. MAINTENANCE REMOVED CORROSION IAW SRM 51-70 -41. 2 L 7 2 4T RT A52EU 2002090500137 20020905 00137 EU 2002 9 5 MALA020524 1 20020823 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING 4K-INSPECTION IN CWA, FRAME 236 HAS LIGHT CORROSION ON UPPER FLANGE. MAINTENANCE REMOVED CORROSION IAW SRM 51-70 -40. 2 L 7 2 4T RT A52EU 2002090500138 20020905 00138 EU 2002 9 5 MALA020525 1 20020823 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING 4K-INSPECTION IN CWA, FRAME 258 HAS LIGHT CORROSION ON UPPER FLANGE. MAINTENANCE REMOVED CORROSION IAW SRM 51-70 -40. 2 L 7 2 4T RT A52EU 2002090500139 20020905 00139 EU 2002 9 5 MALA020526 1 20020823 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING 4K-INSPECTION IN CWA, FRAME 272 HAS LIGHT CORROSION ON UPPER FLANGE. MAINTENANCE REMOVED CORROSION IAW SRM 51-70 -40. 2 L 7 2 4T RT A52EU 2002090500140 20020905 00140 EU 2002 9 5 MALA020527 1 20020823 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING 4K-INSPECTION IN CWA, PILOTS AND COPILOTS FLOOR HAS LIGHT CORROSION ON THE FLOOR AND RIVET HEADS. MAINTENANCE RE MOVED CORROSION FROM COCKPIT FLOOR IAW SRM 51-20-43. 2 L 7 2 4T RT A52EU 2002090500141 20020905 00141 EU 2002 9 5 MALA020528 1 20020823 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING 4K-INSPECTION IN CWA, FWD AISLE SEAT TRACKS LT AND RT HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002091200099 20020912 00099 NM 2002 9 12 F3LA200200255 1 20020824 A 2612 CONNECTOR BOEING 737 7372L9 1384497 NM FIRE DETECTOR DIRTY A F3LA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 271FL 77 22734 AIR TURNBACK. FLIGHT CREW REPORTED NR 2 FIRE WARNING HANDLE ILLUMINATED MOMENTARILY ON THREE OCCASIONS DURING DEPARTURE . CLEANED CONNECTORS A AND B ON LOWER FIRE DETECTOR ELEMENT AND CHECKED OKAY. 2 L 7 2 4F RT A16WE 2002091200100 20020912 00100 NM 2002 9 12 F3LA200200256 1 20020829 A 2612 894092 SENSING ELEMENT BOEING 737 7372L9 1384497 NM NR 2 ENGINE FAULTY A F3LA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 271FL 110 22734 AIR TURNBACK. FLIGHT CREW REPORTED NR 2 FIRE WARNING BELL SOUNDED AND LIGHT ILLUMINATED. LIGHT EXTINGUISHED WITH THRUS T REDUCED TO IDLE. ALL ENGINE INDICATIONS APPEARED NORMAL. REPLACED NR 2 ENGINE UPPER FIRE SENSING ELEMENT. REMOVED P LACARD. 2 L 7 2 4F RT A16WE 2002090500142 20020905 00142 EU 2002 9 5 QXEA0201332 1 20020902 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 7184 222 11159 PDX-AFT LOWER EGRESS LIGHTS WON'T EXTINGUISH. REMOVED AND REPLACED POWER SUPPLY BATTERY FOR AFT LOWER EGRESS LIGHTS. OPE RATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002090500143 20020905 00143 NM 2002 9 5 AALA20020970 1 20020704 A 3350 LIGHT BOEING 777 777223 1385213 NM L1 DOOR INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT GALLEY L1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT A SSEMBLY AT GALLEY L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002090500144 20020905 00144 EA 2002 9 5 COMA0260503 1 20020902 A 3220 UPLOCK CNDAIR CL600 CL6002B19 1900309 EA A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 784CA 7319 FLIGHT 5646 GEAR DISAGREE MESSAGE WHEN GEAR SELECTED DOWN.ADJUSTED THE NLG UPLOCK ASSY. 2 L 7 2 4F RT A21EA 2002090500145 20020905 00145 EA 2002 9 5 COMA0260504 1 20020902 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 965CA 7131 FLIGHT 5789 FLAS FAIL MESSAGE WHEN SELECTED TO 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002090500146 20020905 00146 EA 2002 9 5 COMA0260505 1 20020830 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 708CA 5760 7235 FLIGHT 5466 STEERING INOP CAUTION MESSAGE.REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002090500147 20020905 00147 EA 2002 9 5 COMA0260506 1 20020902 A 3231 622EN1436 SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 708CA 7235 FLIGHT 5009 GEAR DISAGREE WARNING AND NOSE DOOR OPEN MESSAGE.REPLACED THE NLG DOORS MICRO SWITCH S2GA. 2 L 7 2 4F RT A21EA 2002090500148 20020905 00148 EA 2002 9 5 COMA0260507 1 20020829 A 7930 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 991CA 7216 FLIGHT 5736 R/H ENGINE OIL PRESSURE WARNING DURING T/O.COULD NOT DUPLICATE. OIL PRESSURE INDICATIONS NORMAL DURING MAIN T. RUNS. 2 L 7 2 4F RT A21EA 2002090500149 20020905 00149 EA 2002 9 5 COMA0260508 1 20020902 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 965CA 7131 FLIGHT 5789 FLAPS FAIL MESSAGE WHEN SELECTED 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002090500150 20020905 00150 EA 2002 9 5 COMA0260509 1 20020902 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 796CA 7338 FLAPS FAIL MESSAGE DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002090500151 20020905 00151 EA 2002 9 5 COMA0260510 1 20020903 A 3620 355924400 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA L/H PYLON MALFUNCTIONED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 964CA 7129 FLIGHT 5983 L/H 14TH STAGE BLEED AIR DUCT WARNING. IFSD.REPLACED THE BLEED AIR LEAK SENSOR ELEMENT IN L/H ENGINE PYLON. 2 L 7 2 4F RT A21EA 2002090500152 20020905 00152 WP 2002 9 5 AT0200076 1 20020905 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP B5-24, B5-32 A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 CEILING EMERGENCY LIGHTS OUT ROWS 1-15. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERIES IN B5-24 AND B5-32, OPS CHECK GOOD PER MM 33-50. 2 L 7 2 4F A6WE 2002090500153 20020905 00153 NM 2002 9 5 AALA20020971 1 20020705 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 20 H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002090500154 20020905 00154 WP 2002 9 5 MWEA020537 1 20020905 A 2730 99184501 ELEVATOR DOUG DC9 DC914 3022034 WP STATION XE200 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LEFT ELEVATOR LOWER FORWARD SPAR FLANGE IS CRACKED APPROXIMATELY 2" AT STATION XE200. -- FABRICATED AND INSTALLED REPA IRED PART. 2 L 7 2 4F A6WE 2002090500155 20020905 00155 WP 2002 9 5 MWEA020539 1 20020905 A 2910 7920135575 HYDRAULIC LINE DOUG DC9 DC932 3022066 WP RIGHT WHEEL LEAKING A MWEA O OTHER K FLUID LOSS AP APPROACH 1 GL 31 302ME 47102 LOST ALL HYDRAULIC QUANTITY ON RIGHT SIDE. -- REMOVED LINES REPLACED WITH TEMPORARY FLEX LINE AND PLACED ON MAINTENACE CARRY OVER FOR REPLACEMENT OF TEMPORARY FLEX LINE. 2 L 7 2 4F A6WE 2002090500156 20020905 00156 SO 2002 9 5 C2XA02BT042 1 20020816 A 2530 HEATER EMB 145 EMB145 3260210 SO GALLEY DIRTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 16961 145103 BWI---CO3404, CREW REPORTED, ELECTRICAL BURNING ODOR IN GALLEY AREA. MAINTENANCE INSPECTED GALLEY AND FIRST THREE ROWS OF THE CABIN AFT OF THE GALLEY AND FOUND BURNT COFFEE ON COFFEEMAKER HEAT PAD. CLEANED HEAT PAD, NO FURTHER MAINTENANCE REQUIRED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002090500157 20020905 00157 SO 2002 9 5 C2XA02TY130 1 20020905 A 5321 14522460015 GUSSET EMB 145 EMB145 3260210 SO GALLEY FLOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED 2-C INSPECTION MAINTENANCE FOUND THE GALLEY GUSSET CORRODED. MAINTENANCE R/R NEW GUSSET IAW EMB 135/145 SRM 51-40-02. COUNTERSUNK HOLES IAW EMB 135/145 SRM 51-40-06,PAINTED TOP GUSSET IAW CPM 51-21-06. ALL WORK WAS A CCOMPLISHED AND WIL BE REL. UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002090600001 20020906 00001 NM 2002 9 6 2002F00855 1 20020528 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND FLOORBEAM EXFOLIATED IN SEVERAL AREAS, FROM LBL 60 TO RBL 60 UPPER CHORD, AT STATION 1130. (M) 2 L 7 3 4F A3WE 2002090600002 20020906 00002 WP 2002 9 6 AALA20020855 1 20020611 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND CORROSION IN INTERCOSTAL STATION 1309-1322 BETWEEN LONGERON 28R AND 27R. REPLACED INTERCOSTAL PER SRM 51-10 -03. (M) 2 L 7 2 4F A6WE 2002090600003 20020906 00003 WP 2002 9 6 AALA20020856 1 20020611 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND SEAT TRACK NR 5 CORRODED ON OUTBOARD FLANGE STATION 204. REMOVED SECTION OF TRACK AND SPLICED IN NEW SECTIO N OF SEAT TRACK STATION 200-247 PER SRM 53-05 FIG 4F. (M) 2 L 7 2 4F A6WE 2002090600004 20020906 00004 WP 2002 9 6 AALA20020857 1 20020611 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND DENT AND SCRATCH IN FUSELAGE SKIN LEFT SIDE L26 STATION 162 JUST FORWARD AND BELOW FLAP AIRSTAIR DOOR. INST ALLED DOUBLER PER SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 2002090600005 20020906 00005 WP 2002 9 6 AALA20020858 1 20020528 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND CORROSION ON RIGHT CUSP STATION 280. ROUTED DAMAGE AND INSTALLED DOUBLER PER SRM 53-01 FIG 43. (M) 2 L 7 2 4F A6WE 2002090600006 20020906 00006 WP 2002 9 6 AALA20020859 1 20020531 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND CORROSION ON LEFT CUSP STATION 1174 AFT OF SERVICE DOOR AT SEAT TRACK MOUNT. CUT OUT CORROSION AND INSTALLE D REPAIR DOUBLER PER SRM 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002090600007 20020906 00007 WP 2002 9 6 AALA20020860 1 20020605 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND SEAT TRACK NR 6 CORRODED STATION 213-218. INSTALLED NEW SEAT TRACK FROM STATION 213-303 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002090600008 20020906 00008 WP 2002 9 6 AALA20020861 1 20020530 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND HOLE PUNCHED THROUGH RIGHT CUSP AT STATION 484 AND 485. CUT OUT DAMAGED AREA AND INSTALLED A DOUBLER ON CUS P PER SRM 53-01, FIG 4. (M) 2 L 7 2 4F A6WE 2002090600009 20020906 00009 WP 2002 9 6 AALA20020862 1 20020530 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TUL - FOUND CORROSION ON RIGHT CUSP AT STATION 288-305. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2002090600010 20020906 00010 NM 2002 9 6 AALA20020914 1 20020605 A 2820 ADAPTER BOEING 777 777223 1385213 NM FUEL MANIFOLD CRACKED A AALA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 21 772AN 29580 AFW - FOUND ADAPTER CRACKED DURING DEFUELING. SMALL FUEL SPILL OCCURRED. REMOVED CRACK MANIFOLD ADAPTER AND INSTALLED NEW ITEM, LEAK CHECK OK. (M) 2 L 7 2 4F RT T00001SE 2002090600011 20020906 00011 NM 2002 9 6 AALA20020915 1 20020611 A 5320 WEB BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 317AA 22319 AFW - FOUND WEB AT STATION 742 HAS CORROSION REQUEST ENGINEERING APPROVAL TO REMOVE SECTION OF WEB AND REPAIR AS PER SKE TCH. REPAIR USING REF/A/ AS GUIDELINES AND USE BACB30M Y6K OR EQUIVALENT REPAIR DOUBLER .040 IN 7075-TC ALODINED USE TA PERED SHIMS AS REQUIRED. (M) 2 L 7 2 4F RT A1NM 2002090600012 20020906 00012 NM 2002 9 6 AALA20020918 1 20020621 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 AFW - FOUND EMERGENCY EXIT SIGNS AT R/2 AND L/2 DID NOT ILLUMINATE DURING SYSTEM TEST. REMOVED AND REPLACED BATTERY PAC K. (M) 2 L 7 2 4F RT A1NM 2002090600013 20020906 00013 NM 2002 9 6 AALA20020955 1 20020702 A 2120 SMOKE BOEING 757 757223 1384957 NM CABIN DETECTED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 690AA 25696 ELECTRICAL SMOKE AREA SEATS 9 THROUGH 13 AREA, REQUEST INSPECTION. INSPECT INSEAT HARNESSES, POWERPORTS, LIGHT BALLASTS IN AREA. PERFORM OPERATION CHECK OF SYSTEMS PER MM. REPAIR FOR FINDINGS. ELECTRICAL SMOKE AREA SEATS 9-13, ACC CABIN FIRE/SMOKE CHECKLIST SMOKE STOPPED. VISUAL INSPECTED ALL ELECTRICAL WIRE CABLE ROWS 9 THROUGH13 LEFT AND RIGHT CHECK A LL NORMAL. NO VISUAL EVIDENCE IF SMOKE AND ELECTRICAL ODOR. (M) 2 L 7 2 4F RT A2NM 2002090600014 20020906 00014 NM 2002 9 6 AALA20020956 1 20020624 A 2410 GEN5013 IDG BOEING 767 767223 1385123 NM RIGHT FAILED A AALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 21 316AA 22318 RIGHT GENERATOR OFF LIGHT ANNUNCIATION QRH PROCEDURE CAME BACK ON LINE FOR SHORT TIME. BITE ON BPCU SHOWED UNDER VOLTAG E TRIP AND REPLACED GCU, ON RIGHT GENERATOR SYSTEM. REMOVED AND REPLACED RIGHT GCU. RAN ENGINE AND FOUND VOLTAGE WANDE RING. PLACED THE RIGHT IDG AS INOPERATIVE REF MEL MAN 24-01 PER MEL AUTH 6 560DC-A. ENT INTO MIC ACCOMPLISHED MPM PROC EEDING NR 24-01 AND CHECKS OK. REPLACED RIGHT IDG ASSY LEAK CEHCK OPS CHECK NORMAL CLEARED MEL 06-560DC-A CLEARED MIC R EMOVED PLACARD. (M) 2 L 7 2 4F RT A1NM 2002090600015 20020906 00015 NM 2002 9 6 AALA20020957 1 20020620 A 2822 PUMP BOEING 767 767323 1385205 NM FUEL SYSTEM CONTAMINATED A AALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 21 382AN 25451 ALL FUEL BOOST PUMPS ON, X-FEEDS CLOSED. FUEL FED FROM BOTH THE MAIN TANKS AND CENTER TANKS. TURNED OFF WD PUMPS, ON M AINS, CENTER TANK PROVIDED ALL FUEL REF ITEMS 62. A/C HAS BEEN INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FL IGHT FROM ORD TO AFW FOR FURTHER EVALUATION OF FUEL SYSTEM. THIS FERRY FLIGHT IS AUTHORIZED BY SPOTTING MESSAGE 6-974 D ATED 6/15/02. REMOVED DEBRIS FROM CENTER TANK FUEL PUMP PICKUP SCREENS. ACCOMPLISHED ON AFW DROP IN BOW. OPS CHECK AND LEAK CHECKS OF CENTER TANK SYSTEM, CHECKS GOOD. (M) 2 L 7 2 4F RT A1NM 2002090600016 20020906 00016 WP 2002 9 6 AALA20020968 1 20020703 A 2120 ODOR DOUG DC9 DC982 3022082 WP CABIN DETECTED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 488AA 49681 ABQ - FLT 11287 - EN ROUTE PHX-DFW, DURING CRUISE AT 33,000 FEET, A STRONG ELECTRICAL FIRE SMELL ENTER THE COCKPIT FOLLO WED BY REPORTS FROM CABIN OF BURNING ELECTRICAL SMELL. EMERGENCY PROCEDURE WERE FOLLOWED AND THE FLIGHT ATTENDANTS REPO RTED THE SMELL SEVERE. DIVERTED ABQ AND LANDED WITHOUT INCIDENT. THE ODOR REMAINED WITH THE AIRCRAFT UNTIL ON THE GROU ND AND THEN STARTED TO DISSIPATE. THE FLIGHT ATTENDANTS REPORTED THAT THE ODOR WOULD CHANGE WHEN THE PACKS WERE SHUT OF F, BUT THE SMELL REMAINED. THE SMELL WAS A VERY PRONOUNCED ELECTRICAL BURNING SMELL. PRECAUTIONARY REPLACED NR 1 ENGIN E AND WATER SEPARATOR COALESCER BAGS, LEAK CHECKED NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. NO FUMES NOTED. (M 2 L 7 2 4F A6WE 2002090600017 20020906 00017 WP 2002 9 6 AALA20020972 1 20020702 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 16545 53027 TUL - FOUND CORROSION ON DOOR PAN HORIZONTAL AND VERTICAL LEGS. SPLICED IN NEW SECTION OF DOOR PAN PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002090600018 20020906 00018 WP 2002 9 6 AALA20020973 1 20020703 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 16545 53027 TUL - FOUND NR 2 TRACK HAS CORROSION AT STATION 1200. REMOVED AND REPLACED SEAT TRACK NR 2 FROM STATION 1180-1309 PER S RM 53-05, PAGE 10G, FIG 4F. (M) 2 L 7 2 4F A6WE 2002090600019 20020906 00019 WP 2002 9 6 AALA2002842 1 20020516 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND DENT IN FUSELAGE SKIN RUNNING PARALLEL TO LONGERON 23L FROM STATION 387-395. INSTALLED PERMANENT REPAIR (CL AS 1) PER SRM 53-04 FIG 12B SHEET 4, 5, 6 AND 95, 96. (M) 2 L 7 2 4F A6WE 2002090600020 20020906 00020 EA 2002 9 6 ASOA020397 1 20020713 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA ACM BAY FAILED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 872AS 2236 7542 ON TAXI OUT OF GSP THE CABIN FILLED WITH SMOKE. THE AIRCRAFT WS EVACUATED ON THE TAXIWAY THROUGH THE PASSENGER DOOR AND THE OVERWING EMERGENCY EXITS. THE CAPTAIN DID NOT RECEIVE ANY FAULT WARNINGS OR MESSAGES. MAINTENANCE REMOVED AND REP LACED THE RIGHT ACM. THE FAILED ACM HAD NO ROTATION OF THE COMPRESSOR OR TURBINE. THIS ALLOWED HOT BLEED AIR TO ENGER THE CABIN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002090600021 20020906 00021 EA 2002 9 6 ASOA02393 1 20020710 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 854AS 7382 FLT 4505 - DURING A SCHEDULED INSPECTION IN XNA, THE AFT OVERHEAD CABIN EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MA INTENANCE REMOVED AND REPLACED THE BURNED OUT OVERHEAD EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002090600022 20020906 00022 SO 2002 9 6 ASOA02394 1 20020710 A 3350 D36604001 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SW 21 275AS 120234 FLT 4243 - DURING GROUND INSPECTION IN ATL, THE AFT SECTIONS OF EMERGENCY FLOOR LIGHTING WERE FOUND TO ILLUMINATE WHEN T HE COCKPIT SWITCH WAS IN THE ARM POSITION AND THE CABIN SWITCH IN NORMAL. MAINTENANCE REMOVED AND REPLACED THE EMERGENC Y BATTERY PACK IN THE NR 3 POSITION. OPERATIONAL CHECKS GOOD. AIRCRAF OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002090600023 20020906 00023 EA 2002 9 6 ASOA02395 1 20020710 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 880AS 7606 FLT 4713 - DURING GROUND INSPECTION IN DFW, THE LEFT FORWARD MOST EXTERNAL EMEREGNCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVI CE. (M) 2 L 7 2 4F RT A21EA 2002090600024 20020906 00024 EA 2002 9 6 ASOA02396 1 20020712 A 3234 533405 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG INOPERATIVE A ASOA O OTHER J WARNING INDICATION DE DESCENT 1 SO 11 701EV 10020 FLT 4592 - DURING DESCENT INTO ISP, THE CAPTAIN RECEIVED A GEAR DISAGREEMENT AND A PROXIMITY SYSTEM NR 1 FAULT MESSAGE O N THE EICAS AFTER HE LOWERED THE GEAR HANDLE. AN EMERGENCY WAS DECLARED AND A MANUAL GEAR EXTENSION WAS PERFORMED. AIR CRAFT LANDED SAFELY IN ISP. CAPTAIN DID REPORT THE LOSS OF NOSEWHEEL STEERING ON LANDING ROLLOUT BUT WAS ABLE TO MANEUV ER THE AIRCRAFT OFF ON THE RUNWAY. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECK S GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002090600025 20020906 00025 NE 2002 9 6 GAIA02027AOP 2 20020324 A 7230 772761 COMPRESSOR WHEEL BOEING 727 727223 1384074 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A GAIA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SW 07 6833 20186 6533657B FLT 2713 - MCO-FWA - DURING CRUISE AT 31,000 FEET, THE NR 2 ENGINE COMPRESSOR STALLED. THE CREW SHUT DOWN NR 2 ENGINE A ND DECLARED AN EMERGENCY. THE FLIGHT DIVERTED TO JAX AND THE LANDING WAS UNEVENTFUL. REMOVED AND REPLACED C-1 DISK ON NR 2 ENGINE. PERFORMED OPERATIONAL CHECKS AND NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2002090600026 20020906 00026 NM 2002 9 6 GAIA02069OP 1 20020607 A 3230 ACCESSORY UNIT BOEING 727 727232 1384082 NM E/E COMPT FAILED A GAIA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 77780 20635 DURING APPROACH OF FLIGHT NR 1849 FROM MSP TO SEA, THE RIGHT MAIN LANDING GEAR INDICATED UNSAFE. CREW DID A 'GO AROUND' AND ON SECOND APPROACH GOT ALL GREEN LIGHTS. SECONDARY INDICATIONS WERE NORMAL. CREW DECLARED AN EMERGENCY INTO SEA. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT GEAR SWITCH AND LANDING GEAR ACCESSORY UN IT AS A PRECAUTIONARY PROCEDURE. PERFORMED OPERATIONAL CHECK PER BOEING 727 MM 32-61-91 PAGE 401. ALL INDICATIONS NORM AL. (M) 2 L 7 3 4F A3WE 2002090600027 20020906 00027 2002 9 6 GTIA020736 4 20020630 A 2210 4034242923 CONTROL PANEL DOUG DC9 DC982 3022082 WP COCKPIT FAILED A GTIA O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 803NK 48087 MCO - FLT 506 - INTERMITTENT AUTOTHROTTLE DISCONNECT ON APPROACH. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL PANEL, S YSTEM OPS CHECKS GOD IAW MD80 MM 22-01-05. (M) 2 L 7 2 4F A6WE 2002090600028 20020906 00028 WP 2002 9 6 GTIA020737 1 20020701 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG DISCHARGED A GTIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 823NK 48020 MYR - FLT 1572 - NOSE WHEEL WOULD NOT RETRACT AFTER TAKEOFF, FOLLOWED QRH PROCEDURES RETURNED TO KMYR FOR MX. SERVICED NOSE STRUT TO PROPER LEVEL IAW MD80 MM 32-21-02 AND PERFORMED GEAR SWING IAW MD80 MM 32-30-00. NO DEFECTS NOTED, NOSE GE AR RETRACTION. OPS CHECKS GOOD. (M) 2 L 7 2 4F A6WE 2002090600029 20020906 00029 WP 2002 9 6 GTIA020738 1 20020628 A 2780 SWITCH DOUG DC9 DC981 3022081 WP SLATS OUT OF ADJUST A GTIA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 23 810NK 48015 FLL - FLT 470 - FOUND AUTO SLAT FAIL ON TAKEOFF, DID NOT COME ON DURING LANDING. ADJUSTED FLAP/SLAT SWITCH IAW MM 27-84 -02. (M) 2 L 7 2 4F A6WE 2002090600030 20020906 00030 WP 2002 9 6 GTIA020739 1 20020630 A 5270 SENSOR DOUG DC9 DC983 3022083 WP CARGO DOOR LOOSE A GTIA D RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 23 827NK 49793 LGA - FLT 1865 - IMMEDIATELY INTO TAKEOFF ROLL, AFT CARGO DOOR LIGHT ILLUMINATED IT WENT OUT, THEN FLICKERED WHILE TAXI ING. TRANSFERRED TO DIM, AFT CARGO DOOR INDICATION INOP. DOOR FOUND CLOSED AND LOCKED, CREW STATED AIRCRAFT WAS ROLLIN G AT 40 KNOTS NORMAL BRAKING APPLIED. FOUND HARDWARE LOOSE ON STRIKER TIGHTENED AND ADJUSTED IAW MM CH 52-31-00. (M) 2 L 7 2 4F RT A6WE 2002090600031 20020906 00031 WP 2002 9 6 GTIA020740 1 20020703 A 5730 PANEL DOUG DC9 DC982 3022082 WP LT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 ACY - FOUND LEFT WING LOWER TRAILING EDGE PANEL CRACKED BOTTOM SIDE. PERFORMED MULTIPLE LAMINATION REPAIR ON LEFT LOWER TRAILING EDGE PANEL BOTTOM INBOARD IAW DC9/MD80 SRM 57-70-1. (M) 2 L 7 2 4F A6WE 2002090600032 20020906 00032 WP 2002 9 6 GTIA020741 1 20020703 A 5730 PANEL DOUG DC9 DC982 3022082 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 ACY - RIGHT WING LOWER TRAILING EDGE PANEL CRACKED BOTTOM SIDE INBOARD. PERFORMED MULTIPLE LAMINATION REPAIR ON RIGHT L OWER TRAILING EDGE PANEL BOTTOM INBOARD IAW 57-70-1 OF THE DC9/MD80 SRM. (M) 2 L 7 2 4F A6WE 2002090600033 20020906 00033 WP 2002 9 6 GTIA020742 1 20020602 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - PASSENGER CABIN HAS CORROSION AT THE WEB STATION 168.7 STATION 180 PLUS X57 INCHES. PASSENGER CABIN HAS CORROSION AT THE WEB FORWARD LEFT LOWER CORNER DOOR STATION 160 TO STATION 148.5 PLUS X55 INCHES. PASSENGER CABIN HAS CORROSION AT THE WEB STATION 218 PLUS X59 INCHES. REMOVED CUSP FROM STATION 155 TO 225 LEFT SIDE. FABRICATE CUSP. FABRICATED TW O DOUBLERS STATION 154 AND 180. INSTALLED TWO DOUBLER ON CUSP. INSTALLED CUSP FROM STATION 150 TO 230, PLUS 59. (M) 2 L 7 2 4F A6WE 2002090600034 20020906 00034 WP 2002 9 6 GTIA020743 1 20020614 A 5340 ATTACH ANGLE DOUG DC9 DC981 3022081 WP TAIL DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 FTW - FOUND REPLACED DORSAL FIN ATTACH ANGLE PER EA 5310-208A. REMOVED 5939711-501 AND 502 ANGLES. LOCATED AND DRILLED NEW. INSTALLED -3 AND -4 ANGLES. EA 5310-208A SIGN OFFS PERFORMED AND DOCUMENTED ON EOA W/C B00034-11R-00006. (M) 2 L 7 2 4F A6WE 2002090600035 20020906 00035 WP 2002 9 6 GTIA020745 1 20020625 A 5753 SKIN DOUG DC9 DC941 302207N WP TE FLAP DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 47605 ACY - DELAMINATION OF TRAILING EDGE OF RIGHT INBOARD FLAP. REF TO ITEM 32787-3 DELAMINATION OF TRAILING EDGE OF RIGHT I NBOARD FLAP. STOP DRILLED TRILINE EDGE CRACK AND FILLED AREA WITH PR22B1/2 SEALANT IAW DC9 MM 78-30-0. (M) 2 L 7 2 4F A6WE 2002090600036 20020906 00036 2002 9 6 GTIA020747 4 20020628 A 2210 4034242923 CONTROLLER DOUG DC9 DC982 3022082 WP AUTOTHROTTLE FAILED A GTIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 23 803NK 626 48087 MCO - FLT 594A - AUTO THROTTLE TURNED OFF ON APPROACH WHEN SPEED WAS CHANGED AUTO PILOT 2. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROLLER, OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4F A6WE 2002090600037 20020906 00037 WP 2002 9 6 GTIA020859 1 20020805 A 2120 ODOR DOUG DC9 DC982 3022082 WP CABIN DETECTED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 23 800NK 49144 TPA - FLT 632 - ON APPROACH INTO DTW 'BURING' RUBBER SMELL FROM ROW 19-23 DISSIPATED QUICKLY. PERFORMED AN INSPECTION O N THE LIGHTING SYSTEM INCLUDING BALLASTS ON ROW 19 TO 23, BOTH SIDES. NO DEFECTS WERE NOTED. (M) 2 L 7 2 4F A6WE 2002090600038 20020906 00038 WP 2002 9 6 GTIA020860 1 20020801 A 5414 SKIN DOUG DC9 DC983 3022083 WP NR 2 NACELLE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 DTW - NR 2 ENGINE INLET COWL WIRE MESH LINER TORN. REPAIRED TORN LINER WIRE MESH NR 2 ENGINE INLET COWL. (M) 2 L 7 2 4F RT A6WE 2002090600039 20020906 00039 WP 2002 9 6 GTIA020866 1 20020712 A 5753 SKIN DOUG DC9 DC981 3022081 WP TE FLAP DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND LEFT FLAP UNDERSIDE HAS METAL FILLER FALLING OUT. REMOVED DAMAGED SKIN. MATERIAL SUBSTITUTED FROM 2014-T6 TO 7075-T6. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2002090600040 20020906 00040 WP 2002 9 6 GTIA020872 1 20020719 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND LONGERON 25L AT STATION 160 IN E/E COMPARTMENT IS CRACKED. REMOVED DAMAGED SECTION OF LONGERON. LOCATED AN D DRILLED LONGERON SPLICE. INSTALLED LONGERON AND SPLICES. (M) 2 L 7 2 4F A6WE 2002090600041 20020906 00041 WP 2002 9 6 GTIA020873 1 20020719 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND LONGERON END FITTING 29L HAS CORROSION AROUND FASTENERS ON FITTING. MATERIAL LOSS FOUNDED OUT LIMITS. REMO VED FITTING. INSTALLED NEW FITTING. (M) 2 L 7 2 4F A6WE 2002090600042 20020906 00042 WP 2002 9 6 GTIA20020839 1 20020517 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 TUL - FOUND TWO DEEP GOUGES STATION 387-395 LONGERON 23L, STATION 369-374 STATION 370. INSTALLED PERMANENT REPAIR PER S RM 5304 FIG 12B SHEET 4, 5, 6 AND 95, 96. (M) 2 L 7 2 4F A6WE 2002090600043 20020906 00043 NM 2002 9 6 MEX2002243 1 20020726 A 7920 699151 STRAINER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE ENGINE OIL CLOGGED A ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 169PL 53175 FLT 416 - AIRCRAFT ABORTED TAKEOFF DUE TO OIL STRAINER CLOGGING TURNED ON. OIL MAIN FILTER WAS REPLACED. RESTRICTORS W ERE CLEANED AND THE CLOGGING FILTER ALARM WAS REPLACED IAW MM 79-35. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002090600044 20020906 00044 NE 2002 9 6 USAABB02089 2 20020607 A 7300 ODOR BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT DETECTED A USAA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 629AU 27807 SFO - FLT 197 - AFTER TAKEOFF FROM PHL, CREW RECEIVED THE EICAS MESSAGES 'LT ENG EEC' AND 'RT ENG EEC' AND THE ASSOCIATE D LIGHTS. CREW ALSO NOTED AN ELECTRICAL SMELL. THE EEC'S WERE SELECTED OFF AND THE SMELL DISSIPATED. FLIGHT CONTINUED TO SFO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED BITE ON BOTH EEC'S, ADC'S AND BVCU'S. BOTH ENGINES WERE RUN WITH NO PROBLEMS NOTED. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2002090600045 20020906 00045 2002 9 6 USAASA02061 4 20020707 A 2565 SLIDE AIRBUS A319 A319112 3930323 EU ESCAPE SLIDE MALFUNCTIONED A USAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 19 724UW 1122 DCA - THE RIGHT OVERWING EMERGENCY EXIT SLIDE INDICATES DISARMED. MAINTENANCE ARMED THE RIGHT OVERWING EMERGENCY EXIT S LIDE. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2002090600046 20020906 00046 EU 2002 9 6 USAASA02062 1 20020707 A 3260 848401 UPLOCK SWITCH AIRBUS A319 A319112 3930323 EU MLG FAILED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 716UW 1055 PIT - FLT 74 - EN ROUTE SFO-PIT, UPON GEAR EXTENSION, THE LEFT MAIN LANDING GEAR RED UNLOCK LIGHT STAYED ON AND THE GEAR DOORS SHOWED OPEN. AFTER THE LANDING GEAR WAS CYCLED, ALL INDICATIONS BECAME NORMAL. MAINTENANCE REPLACED THE LEFT ML G UPLOCK PROXIMITY SWITCH 9FIN 9GA). SYTEM CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2002090600047 20020906 00047 WP 2002 9 6 WXOA02005 1 20020708 A 2910 7936907715 FITTING DOUG DC9 DC987 3022087 WP GROUND SPOILER LOOSE A WXOA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 17 948MA 49778 COS - RIGHT SYSTEM HYDRAULIC FLUID QUANTITY INDICATION DECREASED FROM 12 QUARTS TO 1 QUART DURING DESCENT FOR ARRIVAL TO STATION. AIRCRAFT LANDED AT STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED RIGHT HYDRAULIC SYSTEM AND FOUND FLUID LE AK AT 'GROUND SPOILER DOWN' HYDRAULIC LINE FITTING. REMOVED AND INSPECTED FITTING. NO DEFECTS NOTED. RESECURED FITTIN G AND SERVICED RIGHT HYDRAULIC SYSTEM TO REQUIRED LEVEL. PERFORMED LEAK CHECK OF FITTING WITH SYSTEM PERSSURIZED. NO L EAKS DETECTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 2002090600159 20020906 00159 NM 2002 9 6 CA020828004 1 20020819 A 7931 CH48108 OIL FILTER ROBSIN R22 R22BETA 7640110 NM LYC O320 O320B2C 41508 EA ENGINE SEPARATED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) AIRCRAFT HAD OIL PRESSURE FLUCTUATIONS IN CRUISE AND RETURNED TO BASE. GROUND RUNS CONFIRMED LOW OIL PRESSURE AT I DLE. OIL FILTER WAS CUT OPEN & THE RUBBER FLAPPER VALVE WAS FOUND LOOSE AND MISSING AT 3/8 X 3/8 INCH PIECE. MISSING PAR T WAS FOUND IN OIL PRESSURE REGULATOR. ALL PARTS OF RUBBER WERE FOUND. OIL FILTER REPLACED AND AIRCRAFT RETURNED TO SERV ICE. 1 G 7 1 3O 3 O H10WE E274 2002090600161 20020906 00161 EA 2002 9 6 CA020903008 1 20020829 A 3234 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE MLG FAILED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA (CAN) GEAR DISAGREE UPON SELECTION OF GEAR HANDLE DOWN NOSE GEAR DID NOT DROP, NOSE DOOR DID NOT OPEN, RECYCLED HANDLE W ITH NO SUCCESS AS PER QRH, MANUAL EXTENSION CARRIED OUT WITH NO FURTHER INCIDENT. 2 L 7 2 4F 4 F RT A21EA E15NE 2002090600162 20020906 00162 NM 2002 9 6 CA020903009 1 20020825 A 3244 997LH457 TIRE BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE MLG FAILED W C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 CA (CAN) DEPARTING YEG CREW HEARD A LOUD BANG AND ABORTED TAKE-OFF. TIRE APPEARED TO HAVE BURST WITHOUT TREAD SEPARATION. BRAKE HEAT FROM THE RTO ALSO FLATTENED 1 AND 4. AIRPORT AUTHORITY REPORTED NO FOREIGN OBJECTS ON THE RUNWAY. TIRE WAS OPERATING AFTER THIRD RECAP. NO OTHER AIRCRAFT DAMAGE WAS OBSERVED. INSPECTIONS REQUIRED WERE ACCOMPLISHED, BRAKES AN D WHEEL/TIRE ASSYS. WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2002090600163 20020906 00163 SO 2002 9 6 C2XA02CL176 1 20020901 A 3260 80069424 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A C2XA K NONE N FALSE WARNING CL CLIMB 1 SW 27 14916 3518 145415 CLE FLT 3274 THE CREW REPORTED THAT DURING LANDING GEAR RETRACTION THE AURAL WARNING LANDING GEAR SOUNDED. NO OTHER IN DICATIONS NOTED. AIRCRAFT LANDED IN CLE WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE AU RAL WARNING UNIT. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002090600164 20020906 00164 SO 2002 9 6 C2XA02CL177 1 20020903 A 2750 FLAP EMB 135 EMB135LR 3260305 SO WING MALFUNCTIONED A C2XA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 27 14516 145323 CLT FLT 3061 CREW REPORTED THAT THE FLAPS FAILED TO EXTEND. GOT SPS ADVANCED AND FLAP FAIL ON EICAS. CREW DECLARED EMER GENCY, AND LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM, PULLED AND RESET THE FLAP CIRCUIT BREAKER. AL L OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002090600165 20020906 00165 SO 2002 9 6 C2XA02CL178 1 20020903 A 2752 3632001003 DRIVE UNIT EMB 135 EMB135LR 3260305 SO T/E FLAP FAILED A C2XA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 27 14516 4052 145323 CLE FLT 3187 CREW REPORTED THAT THE FLAPS EXTENDED NORMALLY TO 45 DEGREES. AFTER EXTENSION FLAP FAIL ON EICAS APPEARED AND FLAP INDICATOR DISPLAYED AMBER DASH. FLAPS WOULD NOT RETRACT. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLAC ED THE FLAP POWER DRIVE UNIT. ALL SYSTEM OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002090600167 20020906 00167 EU 2002 9 6 C2XA02IA176 1 20020821 A 2121 EVTA1925B FAN AEROSP ATR42 ATR42320 8680930 EU E/E BAY MALFUNCTIONED A C2XA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SW 27 99838 12764 12764 259 CREW REPORTED THAT UPON APPROACH TO LCH, AN ELEC SMK MASTER WARNING INDICATION ILLUMINATED. THE CREW PERFORMED THE NECE SSARY CHECKLIST FOR AN ELEC SMK INDICATION AND THE WARNING EXTINGUISHED. THE AIRCRAFT LANDED AT LCH WITHOUT INCIDENT. A GROUND RUN OF THE AIRCRAFT DID NOT REVEAL ANY DISCREPANCIES AND THE AIRCRAFT WAS RETURNED TO SERVICE WITHOUT ANY FURTH ER INDICATIONS ON THE FOLLOWING FLIGHT. MAINTENANCE AT IAH INSPECTED THE AIRCRAFT AND FOUND AN ODOR COMING FROM THE ELE CTRONIC EXHAUST FAN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FAN AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2002090600168 20020906 00168 SO 2002 9 6 C2XA02IA177 1 20020824 A 5524 14539965401 HINGE FITTING EMB 145 EMB145LR 3260212 SO ELEVATOR WORN A C2XA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 27 15910 145455 DURING UNSCHEDULED MAINTENANCE TO IDENTIFY A SOURCE OF INFLIGHT VIBRATION AT OR ABOVE 290 KTS, MAINTENANCE FOUND THE LEF T ELEVATOR TO HAVE WORN HINGE FITTINGS. THE FITTINGS WERE WORN TO THE POINT OF THAT ALLOWED MIGRATION OF A BUSHING INSE RT CAUSING PLAY IN THE HINGE POINT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ELEVATOR AND THE AIRCRAFT WAS TEST FL OWN SATISFACTORILY WITH NO ABNORMAL VIBRATION BEING NOTED. 2 L 7 2 4T RT T00011AT 2002090600169 20020906 00169 EU 2002 9 6 C2XA02IA184 1 20020828 A 3297 WIRE AEROSP ATR42 ATR42320 8680930 EU NLG DAMAGED A C2XA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 93840 271 IAH- LANDING GEAR WILL NOT RETRACT. MEL ATA32-31-03C NR 031643. MAINTENANCE REPAIRED WIRES AT CANNON PLUG 5004 VC, PE RFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. 2 H 7 2 4T RT A53EU 2002090600170 20020906 00170 SO 2002 9 6 C2XA02IA185 1 20020829 A 4930 4504113 APU EMB 145 EMB145 3260210 SO APU BAY LEAKING A C2XA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SW 27 13956 145078 HRL- THE CREW NOTED THAT THE APU HAS A STRONG FUEL SMELL WHEN RUNNING. MAINTENANCE INSPECTED THE APU AND THE AIRCRAFT WAS RELEASED IAW MEL. MAINTENANCE REMOVED AND REPLACED THE APU, PERFORMED A OPERATIONAL CHECK AND A LEAK CHECK. NO DEF ECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002090600171 20020906 00171 SO 2002 9 6 C2XA02IA186 1 20020830 A 5524 14527811401 HINGE EMB 145 EMB145LR 3260212 SO ELEVATOR WORN A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 27 13978 145180 LIT- THE CREW NOTED SEVERE VIBRATIONS IN BOTH YOKES IN FLIGHT. DECLARED EMERGENCY AND THE FLIGHT WAS DIVERTED TO LIT AN D LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ELEVATOR IAW EMB145 AMM 27-30-00, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002090600172 20020906 00172 SO 2002 9 6 C2XA02IA187 1 20020830 A 5524 14527811401 HINGE EMB 145 EMB145LR 3260212 SO ELEVATOR WORN A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 27 13978 145180 LIT- THE CREW NOTED SEVERE VIBRATIONS IN BOTH YOKES IN FLIGHT. DECLARED EMERGENCY, THE FLIGHT WAS DIVERTED TO LIT, LAN DED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ELEVATOR IAW EMB145 AMM 27-30-00, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002090600173 20020906 00173 NM 2002 9 6 UPS02M37974 1 20020402 A 5310 DOOR FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP INSPECTION TYPE:N/A, FWD LOWER CARGO DOOR FRAME CORROSION AT STA 895.700 LONG 41R & 43R. ACCOMPLISHED INTERIM REPAIR AS PER EO MD11-5310-16522-A, PERMANENT REPAIR AT C-CHECK ITEM DEFERRED. 2 L 7 3 4F RT A22WE 2002090600174 20020906 00174 NM 2002 9 6 UPS02M38775 1 20020605 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 253UP INSPECTION TYPE:C CABIN SEAT TRACK AT STA 612 RBL 8.5 FOUND CORRODED. CORROSION REMOVED FOUND EXCEEDED LIMIT PER SRM 53 -70-00 FIG 3 VOL 1 REV 31. SEAT TRACK REMOVED AND REPLACED FROM STA 605-645 RBL 8.5 AS PER SRM 53-70-00 FIG 1 VOL 1 REV 31. 2 L 7 3 4F RT A22WE 2002090600175 20020906 00175 NM 2002 9 6 UPS02M38776 1 20020530 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM STA870-899 LBL=8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 253UP INSPECTION TYPE:C CABIN SEAT TRACK AT STA 870-899 LBL 8 FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS P ER SRM 53-70-00 FIG 3 REV 31. SEAT TRACK REMOVED AND REPLACED AT STA 816-929 AS PER SRM 53-70-00 FIG 1 VOL 1 REV 31. 2 L 7 3 4F RT A22WE 2002090600176 20020906 00176 NM 2002 9 6 UPS02M38777 1 20020530 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 253UP INSPECTION TYPE:C CABIN SEAT TRACK AT STA 806-840 RBL 8 FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT PER SRM 53-70-00 FIG 3 VOL 1. SEAT TRACK REMOVED AND REPLACED AT STA 799-869 RBL 8 AS PER SRM 53-70-00 FIG 1 VOL 1 REV 31. 2 L 7 3 4F RT A22WE 2002090600177 20020906 00177 2002 9 6 372PA0012 4 20020905 A 2565 SLIDE BOEING 737 737306 13844BG NM A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 R-2 door emergency exit slide out of green band. Inspected and found OK, gage needle is less than one-half of green ban d to the left, per MM 25-61-35 Pg. 215. R&R R-2 emergy. exit slide IAW 737-300 MM 25-61-35 for convenience. 2 L 7 2 4F RT A16NE 2002090600178 20020906 00178 NM 2002 9 6 UPS02M38946 1 20020530 A 5315 FLOORBEAM DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 253UP INSPECTION TYPE:C, FLOORBEAM AT STA 1841 LBL 27 FOUND CORRODED. FLOORBEAM WEB AT STA 1841 LT REMOVED AND REPLACED AS PE R DWG:AGA7170 AND INSTALLED AS PER SRM 51-35-01 VOL II REV 31. 2 L 7 3 4F RT A22WE 2002090600179 20020906 00179 NM 2002 9 6 UPS02M38949 1 20020619 A 5315 FLOORBEAM DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 253UP INSPECTION TYPE:C, CTR CARGO STA 1841, BL 0 - RBL 60 FLOORBEAM WEB FOUND CORRODED. FLOORBEAM WEB REMOVED AND REPLACED A S PER DWG AGA7170 AND INSTALLED AS PER SRM 51-35-01 VOL II REV 31. 2 L 7 3 4F RT A22WE 2002090600180 20020906 00180 NM 2002 9 6 UPS02M38951 1 20020529 A 5350 FRAME DOUG MD11 MD11F 3023600 NM TAIL CONE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 253UP INSPECTION TYPE:C, EXTENDED TAIL CONE AFT CONE GUIDE PIN LOCATING BLOCK ATTACHMENT FRAME AT CANT STA 2258.846 FOUND CRAC KED. EXTENDED TAIL CONE CRACKED AREA TRIMMED AND REPAIR CHANNELS AND ANGLES FABRICATED AS PER SRM 53-00-01 FIG 9 VOL I REV 31. REPAIR CHANNEL AND ANGLES INSTALLED AND EXTENDED TAIL CONE FRAME INSTALLED AS PER SRM 51-35-01 VOL II REV 31. 2 L 7 3 4F RT A22WE 2002090600181 20020906 00181 NM 2002 9 6 UPS02M39031 1 20020630 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 253UP INSPECTION TYPE:C, AFT CARGO CORROSION ON SEAT TRACK BETWEEN STA 1841 - 1887 LBL 20. CORROSION FOUND EXCEEDING LIMIT PE R SRM 53-70-00 FIG 3 VOL I REV 31. SEAT TRACK REMOVED, REWORKED IAW DWG AGA3855 AND INSTALLED AS PER SRM 51-31-01 VOL I I REV 31. 2 L 7 3 4F RT A22WE 2002090600182 20020906 00182 NM 2002 9 6 UPS02M39082 1 20020617 A 5320 INTERCOSTAL DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 253UP INSPECTION TYPE:C, FWD CARGO COMPT LT INTERCOSTAL BETWEEN STA 840-859 LONGERON 32 FOUND CORRODED. CORROSION FOUND EXCEE DING LIMIT AT STA 840-859 LONGERON 32 IAW SRM 53-00 -01 FIG 4 VOL 1 REV 31. INTERCOSTAL REMOVED, FABRICATED NEW INTERCO STAL IAW DWG ACA7043 AND NEW INTERCOSTAL INSTALLED IAW SRM 51-35-01 VOL II REV 31. 2 L 7 3 4F RT A22WE 2002090600183 20020906 00183 NM 2002 9 6 UPS02M39083 1 20020630 A 5315 FLOORBEAM DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 253UP INSPECTION TYPE:C, AFT CARGO CORROSION ON FLOORBEAM UPPER CHORD AT STA 1902 0-20 RBL. CORROSION TRIMMED OUT IAW SRM 53- 00-01 FIG 9. HFEC INSPECTION CARRIED OUT, NO CRACKS FOUND ON TRIMMED AREA. REPAIR ANGLE & FILLER, FAB & INSTALLED IAW SRM 53-00-01 VOL I & VOL II. 2 L 7 3 4F RT A22WE 2002090600184 20020906 00184 NM 2002 9 6 UPS02M39084 1 20020624 A 5310 SHEAR TIE DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 253UP INSPECTION TYPE:C, AFT WASTE COMPARTMENT STA 1974 BETWEEN LONGERON 50L - LONGERON 50R FOUND CORROSION ON SHEAR TIE. COR ROSION FOUND EXCEEDING ON SHEAR TIE AS PER SRM 53-00-01 VOL I REV 31. SHEAR TIE & SURROUNDING PARTS REMOVED IAW SRM 51- 35-01 & SRM 51-33-01 VOL II REV 31. NEW SHEAR TIE FABRICATED IAW DWG AGA8002 AND FABRICATED SHEAR TIE AND SURROUNDING P ARTS WET INSTALLED AS PER DWG AGA8002. 2 L 7 3 4F RT A22WE 2002090600185 20020906 00185 NM 2002 9 6 UPS02M39085 1 20020701 A 5310 SHEAR TIE DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 253UP INSPECTION TYPE:C, AFT CARGO BILGE AREA FRAME SHEAR TIE FOUND WITH CORROSION AT STA 1953 LONG 51 RT - 52 RT. CORROSION FOUND EXCEEDING LIMIT ON SHEAR TIE AT STA 1953 LONG 51 RT - 52 RT AS PER SRM 53-00-01 VOL I REV 31. SHEAR TIE & SURROUN DING PARTS REMOVED IAW SRM 51-35-01 VOL II & 51-33-01 VOL II. NEW SHEAR TIE FABRICATED AND INSTALLED AS PER DWG AGA7133 . 2 L 7 3 4F RT A22WE 2002090600186 20020906 00186 NM 2002 9 6 UPS02M39086 1 20020530 A 5320 AGA71705N SUPPORT DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 253UP INSPECTION TYPE:C, CENTER CARGO PANEL SUPPORT STRUCTURE AT STA 1841, LBL 30 TO RBL 30 CORRODED. SUPPORT REMOVED AT STA 1841 IAW SRM 51-35-01 VOL II REV 31. NEW SUPPORT INSTALLED IAW SRM 51-35-01 VOL II REV 31. 2 L 7 3 4F RT A22WE 2002090600187 20020906 00187 NM 2002 9 6 UPS02M39177 1 20020605 A 5347 AFA7789547 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 253UP INSPECTION TYPE:C, CABIN SEAT TRACK AT STA 1964 LBL 76 FOUND CORRODED. SEAT TRACK CORROSION BLEND OUT FOUND EXCEED SRM LIMIT PER SRM 53-70-00 FIG 3 VOL I REV 31. SEAT TRACK REPAIR CARRIED OUT AT STA 1831-2007 X=107.25 PER SRM 53-70-00 FIG 1 VOL I REV 31. 2 L 7 3 4F RT A22WE 2002090600188 20020906 00188 NM 2002 9 6 UPS02M39218 1 20020809 A 2810 DOUBLER DOUG MD11 MD11F 3023600 NM FUEL TANK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP INSPECTION TYPE:C, UPPER AUX TANK UPPER EXTERNAL SKIN HAS SLIGHT SURFACE CORROSION AT STA 1375 X=-47 TO X=-90. UPPER AU X TANK UPPER EXTERNAL SKIN CORROSION REMOVED BY HAND, CLEAN AND TREATED IAW SRM 51-21-01 VOL II REV 31. CORROSION FOUND WITHIN LIMIT EXCEPT 3 DOUBLERS BADLY CORRODED AT STA 1375 X=-47 TO X=-75, FOUND EXCEED LIMIT. DOUBLER FABRICATED AND R EPLACED AS PER SRM 51-35-01 VOL II REV 31. 2 L 7 3 4F RT A22WE 2002090600189 20020906 00189 NM 2002 9 6 UPS02M39219 1 20020805 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP INSPECTION TYPE:C, CABIN FLOOR SEAT TRACK HAS CORROSION AT STA 800 TO 805 X=8.5. SEAT TRACK CROWN CORROSION REMOVED, FO UND EXCEEDED LIMIT PER SRM 53-70-00 FIG 3 VOL I REV 31. SEAT TRACK SECTIONAL REPLACED FROM STA 783 TO STA 909 X=8.5. 2 L 7 3 4F RT A22WE 2002090600190 20020906 00190 EU 2002 9 6 XNOA01061 1 20020807 A 2780 GEARBOX AIRBUS 300 A300B4203 3930306 EU L/E SLAT MALFUNCTIONED A XN0A A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 23 372PC 196 AFTER T/O, SLAT WOULD NOT RETRACT BEYOND 16 DEGREES. REMOVED AND REPLACED NR 11 STEP BACK GEARBOX IAW A300 MM CHAP 27-8 1-16, OPS CHECKS GOOD. INSPECTED SLAT SYSTEM FOUND LEFT WING SLAT NR 3 AND NR 4 MISRIGGED. RIGGED NR 3 AND NR 4 SLATS IAW A300 MM 27-81-35. ADJUSTED SLAT CONTROL INSP LIMIT GUIDE ROD IAW MM 27-81-00, PERFORMED FUNCTIONAL TEST OF SLAT CON TROL AND SLAT SYSTEM IAW A300 27-81-00, NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 2002090600191 20020906 00191 EU 2002 9 6 XNOA01062 1 20020808 A 2780 SLAT AIRBUS 300 A300B4203 3930306 EU WING OUT OF ADJUST A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 372PC 196 DURING TAXI OUT FLIGHT CONTROL CHECK FOUND SLATS WOULD NOT RETRACT BEYOND 16 DEGREES. ADJUSTED LEFT SLAT ASYMMETRY PICK OFF IAW A300 MM 27-83-00. RAN SLATS SEVERAL TIMES. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2002090600192 20020906 00192 EU 2002 9 6 XNOA01063 1 20020809 A 2780 SLAT AIRBUS 300 A300B4203 3930306 EU WING MALFUNCTIONED A XN0A D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 372PC 196 DURING TAXI, FLIGHT CONTROL CHECK FAILED DUE TO SLATS FAILED TO RETRACT. CYCLED SLATS, NO HELP. INSP ALL SLATS, NO DEF ECTS NOTED. RAN SLATS SEVERAL TIMES. OPS CHECK NORMAL IAW A300 MM 27-81-00. 2 L 7 2 4F RT A35EU 2002090600193 20020906 00193 EU 2002 9 6 XNOA01065 1 20020820 A 2913 PUMP AIRBUS 300 A300B4203 3930306 EU HYD SYSTEM FAILED A XN0A O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 GL 23 224KW 073 LOST FLUID IN GREEN HYD SYS LANDING GEAR MANUALLY EXTENDED. REMOVED AND REPLACED NR 2 ENG GREEN SYS HYD PUMP AS REQ, LE AK & OPS CHECK GOOD. SERVICED GREEN SYSTEM AS REQ IAW A300 MM 29-11-32. RESTORED LANDING GEAR ACT SYS TO NORMAL IAW A3 00 MM 32-30-00. 2 L 7 2 4F RT A35EU 2002090600194 20020906 00194 EU 2002 9 6 DHL2002365009 1 20020831 A 2621 35200002 BOTTLE AIRBUS 300 A300B4203 3930306 EU A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 365DH 149 FOUND CARGO COMPARTMENT FIRE BOTTLES #1 AND #2 MI AMBER. SQUIB TEST GOOD. TRANSFERRED TO DMI #10280 AS PER MEL 26-23-01 , CAT C. NOTIFIED MXC, PLACARD INSTALLED.REPLACED CARGO COMPARTMENT FIRE BOTTLES (S/N'S OFF: 00056K1 & 00101K1) & DISCHA RGE CARTRIDGES IAW M/M26-23-11 AND M/M 26-23-12; OPS CHECKED GOOD. THIS CLEARS DMI# 10280. PLACARDS REMOVED. 2 L 7 2 4F RT A35EU 2002090600195 20020906 00195 WP 2002 9 6 MWEA020540 1 20020906 A 5340 5910814 FLOORBOARD DOUG DC9 DC914 3022034 WP STA 200&218 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FLOOR BOARD ATTACH FASTENER HOLES AND FORWARD EDGE LIGHTLY CORRODED ON SEAT TRACK #3 BETWEEN STATIONS 200 AND 218. -- REMOVED CORROSION, LOCATED AND DRILLED NEW SEAT TRACK, INSTALLED NUTPLATES. 2 L 7 2 4F A6WE 2002090600196 20020906 00196 NE 2002 9 6 XNOA01066 2 20020827 A 7240 CASE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 2 ENGINE DAMAGED A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 371PC 157 NR 2 ENGINE FIRE WARNING AFTER TAKEOFF. AFTER PULLING THROTTLE TO IDLE, INDICATION WENT OUT. ELECTED TO RETURN FOR OVE RWEIGHT LANDING. T/S AND FOUND NR 12 LP FUEL NOZZLE FLANGE BURN HOLE IN ENG CASE. REPLACE NR 2 ENG ASSY PER ENA AMM A3 00-71-00-00 PERFORMED GROUND RUNS PER ENA A300 AMM 71-00-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A35EU E23EA 2002090600197 20020906 00197 CE 2002 9 6 2002F00781 1 20020703 A 2820 101389011105 FITTING RAYTHN 390 390 CE FUEL SYSTEM BROKEN B BWVA K NONE O OTHER IN INSP/MAINT 1 CE 07 460AS 211 RB8 THE FITTING IS PLASTIC WITH A .8750 INCH FUEL HOSE ATTACHED, THE HOSE IS AT AN ANGLE WHICH PUTS A SIDE LOAD ON THE FITTI NG AND THE FITTING BROKE WHERE THREADS END THAT SCREW IN TO THE CHECK VALVE. 1 7 2 3F RT A00010WI 2002090600200 20020906 00200 WP 2002 9 6 AALA20021098 1 20020727 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 294AA 49306 DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT CEILING LIGHT FROM ROW 19-21, INOPERATIVE. RESET OVER EMERGENCY EXIT LIGHT BATTERIES CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2002090600201 20020906 00201 NM 2002 9 6 AALA20021127 1 20020807 A 3350 CONNECTOR BOEING 767 767323 1385205 NM GE CF6 CF680 30025 NE CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AN 29606 EMERGENCY LIGHT INOPERATIVE AT SEATS 31HJ, 30HJ, 29HJ, AND 27HJ ARE INOPERATIVE. RECONNECTED PLUG AT 27HJ. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2002090600202 20020906 00202 NM 2002 9 6 AALA20021131 1 20020808 A 3350 BATTERY BOEING 767 767223 1385123 NM GE CF6 CF680 30025 NE CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 321AA 22322 DURING OVERNIGHT MAINTENANCE EMERGENCY ESCAPE PATH LIGHTING SEATS 20H THROUGH 29H FADE/EXTINGUISHED AFTER 1MIN 10 SEC. REPLACED EMERGENCY ESCAPE PATH LIGHTING BATTERY ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2002090600203 20020906 00203 NE 2002 9 6 ACE0805021 2 20020806 A 7314 1143890425 PUMP BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE LT ENGINE LEAKING E YADA O OTHER K FLUID LOSS IN INSP/MAINT 1 AL 03 5632C 269 UC81 PILOT REPORTED FUEL LEAKING FROM LEFT COWLING AFTER SHUT DOWN ON THE RAMP, MAINTENANCE REPLACED THE LOW PRESSURE FUEL PU MP DUE FUEL LEAKING FROM PRESSURE RELIEF COVER GASKET. THIS PUMP WAS IN COMPLIANCE WITH CRANE SB. CONCERNING RELIEF CO VER SCREW TORQUES AND LEAKS. 2 L 7 2 4T 4 T RT A24CE E4EA 2002090600206 20020906 00206 CE 2002 9 6 CGH2002F00001 1 20020816 A 5320 97430000150 CROSSBEAM BEECH B300 B300 1159232 CE PWA PT6 PT6* 52043 EA FUSELAGE CRACKED B CGHR K NONE O OTHER IN INSP/MAINT 1 GL 19 470MN 3362 FL156 THIS CROSS TIE IS RIVETED TO THE FUSELAGE IMMEDIATELY AFT OF THE LEFT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSS TIE ADJACENT TO THE AFT, LOWER CORNER OF THE EMERGENCY EXIT OPENING. 2 L 7 2 4T 3 T RT A24CE E2NE 2002090600207 20020906 00207 CE 2002 9 6 CGH2002F00002 1 20020816 A 5320 1304300462 CROSSBEAM BEECH B300 B300 1159232 CE FUSELAGE CRACKED B CGHR K NONE O OTHER IN INSP/MAINT 1 GL 19 470MN 3362 FL156 THIS CROSS TIE IS RIVETED TOT HE FUSELAGE IMMEDIATELY FORWARD OF THE RIGHT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATE D ON THE CROSS TIE ADJACENT TOT HE FORWARD, LOWER CORNER OF THE EMERGENCY EXIT OPENING. 2 L 7 2 4T RT A24CE 2002090600208 20020906 00208 CE 2002 9 6 CGH2002F00003 1 20020816 A 5320 97430000149 CROSSBEAM BEECH B300 B300 1159232 CE FUSELAGE CRACKED B CGHR K NONE O OTHER IN INSP/MAINT 1 GL 19 470MN 3362 FL156 THIS CROSS TIE IS RIVETED TO THE FUSELAGE IMMEDIATELY AFT OF THE RIGHT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSS TIE ADJACENT TO THE AFT, LOWER CORNER OF THE EMERGENCY EXIT OPENING. 2 L 7 2 4T RT A24CE 2002090600209 20020906 00209 CE 2002 9 6 CGH2002F00004 1 20020816 A 5320 97430000149 CROSSBEAM BEECH B300 B300 1159232 CE FUSELAGE CRACKED B CGHR K NONE O OTHER IN INSP/MAINT 1 GL 03 711VN 4122 FL7 THIS CROSS TIE IS RIVETED TO THE FUSELAGE IMMEDIATELY AFT OF THE RIGHT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSS TIE ADJACENT TO TE AFT, LOWER CORNER OF THE EMERGENCY EXIT OPENING. 2 L 7 2 4T RT A24CE 2002090600210 20020906 00210 NM 2002 9 6 CW12002F00002 1 20020812 A 2932 7G9781 PRESSURE SWITCH AMD FALC50 FALCON2000 2730170 NM HYD SYSTEM FAILED B CW1R O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 EA 11 790L 4340 15 WHILE AIRCRAFT WAS WAITING TO DEPART, WITH BOTH ENGINES RUNNING, THE HYDRAULIC PRESSURE SWITCH INTERNALLY FAILED CAUSING ALL NR 2 SYSTEM HYDRAULIC FLUID TO EMPTY INTO THE AIRCRAFT AND ONTO THE GROUND. THE FLUID ESCAPED THROUGH A RELIEF HOL E ON THE BODY OF THE SWITCH. THE NR 2 HYDRAULIC SYSTEM FLUID EMPTIED VERY RAPIDLY. 2 K 7 3 4F RT A50NM 2002090600211 20020906 00211 CE 2002 9 6 CWQ2002F00003 1 20020805 A 2730 676031217 BUSHING CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL PUSH/PULL TUBE FROZEN B CWQR O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 05 971QS 3161 7500071 ELEVATOR FEELS ABNORMALLY STIFF. AILERON CONTROL FEELS NORMAL. CONTROL CHECKS NORMAL. ELEVATOR FEELS SIMILAR TO MANUA L REVISION MADE IN SIMULATOR. TROUBLESHOOT ELEVATOR SYSTEM. FOUND COPILOT PUSH/PULL TUBE AFT/BELOW COCKPIT PEDESTAL, B USHINGS FROZE, REPLACED BUSHINGS. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2002090600212 20020906 00212 2002 9 6 DEL2002F00000 4 20020719 A 2310 15ARM30021 RETAINER LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP FUSELAGE BROKEN E DELA O OTHER O OTHER NR NOT REPORTED 1 CE 03 723CC 8194 036 HF ANTENNA SHACKLE. ASSEMBLY BROKE IN HALF. SOME PAINT WAS CHIPPED ON THE LEFT VERTICAL STABILIZER. NO OTHER DEFECTS FOUND. 2 L 7 2 4F 4 F A10CE E6WE 2002090600213 20020906 00213 EU 2002 9 6 KBMA115439 1 20020819 A 6720 704A34130184 CONTROL CABLE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR DAMAGED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 1710 3296 TAIL ROTOR CONTROL CABLE IS ROUGH AND BINDS IN SPOTS. REPLACED WITH NEW CABLE. 1 G 7 1 3U 3 U H9EU E19EU 2002090600214 20020906 00214 EU 2002 9 6 KBMA115440 1 20020819 A 2150 350A6011 HOUSING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE AIR CONDITIONER CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 1710 3296 AFT EVAPORATOR MOTOR BRUSH HOUSING IS CRACKED AND BROKEN. REPLACED MOTOR WITH NEW UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2002090600215 20020906 00215 EU 2002 9 6 KBMA115456 1 20020829 A 7922 9696 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE OIL COOLER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 270SH 2 1864 OIL COOLER MOTOR, INOPERATIVE. REPLACED WITH OVERHAULED UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002090600216 20020906 00216 EU 2002 9 6 KBMA115457 1 20020829 A 3310 704A46814049 TRANSISTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 11070 2300 INSTRUMENT LIGHTS ARE INOPERATIVE. (1 EACH TRANSISTOR TRACE BAD) REPLACED WITH OVERHAUL UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002090600217 20020906 00217 CE 2002 9 6 KC82002F00003 1 20020826 A 2133 2419249 OUTFLOW VALVE LEAR 24 24D 5170311 CE GE CJ610 CJ6101 30006 NE CABIN PRESSURE OBSTRUCTED E KC8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 80CK 309 CREW HAD DIFFICULTY MAINTAINING CABIN ALTITUDE. FOUND DEBRIS ON SEAT OF OUTFLOW VALVE. CLEANED OUTFLOW VALVE, CLEANED JET PUMP FILTER, AND PERFORMED OPERATIONAL CHECKS OF PRESSURIZATION SYSTEM PER MFG MM. 2 L 7 2 4J 4 J A10CE 1E16 2002090600218 20020906 00218 CE 2002 9 6 LX52002F00001 1 20020812 A 5280 5082017933 SKIN BEECH B300 B300 1159232 CE PWA PT6 PT6* 52043 EA NLG DOOR CRACKED B LX5R K NONE O OTHER IN INSP/MAINT 1 GL 19 961LL 1390 FL264 INNER DOOR SKIN CRACKS, FITTING SUPPORT CRACKS LOCATED AT DOOR LINK ATTACHMENT. LEFT NOSE LANDING DOOR. THIS IS THE TH IRD AIRCRAFT WITH THIS SAME DAMAGE, SAME LOCATION. PROBABLE CAUSE IMPROPER RIGGING FROM MANUFACTURE. 2 L 7 2 4T 3 T RT A24CE E2NE 2002090600219 20020906 00219 WP 2002 9 6 MCC2002F00000 2 20020801 A 7200 ENGINE SWRNGN SA226 SA226AT 8780405 SW GARRTT TPE331 TPE331* 01514 WP LEFT & RIGHT FLAMED OUT E MCCA A UNSCHED LANDING X ENGINE FLAMEOUT NR NOT REPORTED 1 SW 11 120SC AT067 PILOT STARTED TO ENCOUNTER ICE AND TURNED ON THE ENGINE ANTI-ICE. BOTH ENGINES FLAMED OUT DUE TO CLEAR ICE THAT WAS UNK NOWN TO PILOT. PILOT RESTARTED BOTH ENGINES AND MADE A PRECAUTIONARY LANDING. GROUND CHEEKS WERE MADE OF THE DEICE SYS TEM, ENGINE ANIT ICE SYSTEM, AND IGNITION SYSTEM. ALL CHECKED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A5SW E2WE 2002090600220 20020906 00220 CE 2002 9 6 TIMR74 1 20020709 A 5512 146200231 SKIN BEECH 1900 1900C 1154161 CE HORIZ STAB CRACKED A TIMR K NONE O OTHER IN INSP/MAINT 1 GL 03 172GA UB11 LEADING EDGE OF STABILIZER DISBONDED ON LOWER SIDE AND A CRACK FORMED JUST OFF THE END CAP AND COMPOSITE JOINT. (CONTRO L NR 74) 2 L 7 2 4T RT A24CE 2002090600221 20020906 00221 NM 2002 9 6 TSAA0228165 1 20020723 A 2842 TERMINAL BOEING 737 73776N 13844CH NM FUEL SYSTEM LOOSE A TSAA O OTHER N FALSE WARNING CL CLIMB 1 WP 13 741AL 28641 CLIMB TO CRUISE ALTITUDE, NR 2 FUEL QUANTITY GAUGE DROPPED 1200 POUNDS FOR ABOUT 2 MINUTES. A/C DIVERTED AND LANDED WIT H NO FURTHER PROBLEMS. MAINT PERFORMED TESTS ON INSPECTED WING TO BODY AND SPAR CONNECTORS WITH NO DEFECTS NOTED. SUMP ED TANKS AND MOISTURE TESTED ALL SAMPLES, NO DISC WERE NOTED. DURING VERIF FLT NR2 TANK INDICATED A 1500 LB DIFF IN REA DING. INSULATION/ CAP TEST WAS COMPLETED ON PROBES AND COMPENSATOR, ALL WERE FOUND TO BE IN LIMITS. DURING NR 2 FUEL T ANK AND COMPENSATOR UNIT TEST, PROB TERMINAL WAS FOUND TO BE LOOSE. DISC WAS CORRECTED AND FUEL TANK CAPACITANCE CHECK WAS COMPLETED. A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002090600222 20020906 00222 NM 2002 9 6 TSAA0232176 1 20020816 A 3260 LIGHT BOEING 737 73776N 13844CH NM GE CFM56 CFM56* 13802 NE COCKPIT INOPERATIVE A TSAA O OTHER O OTHER AP APPROACH 1 WP 13 743AL 28654 RT LANDING GEAR GREEN LIGHT FAILED TO ILLUMINATE AFTER GEAR WAS SELECTED DOWN DURING APPROACH. SECONDARY GEAR INDICATOR IN OVERHEAD PANEL SHOWED NORMAL GREEN LIGHTS. CIRCUIT BREAKERS WERE CHECKED. AIRCRAFT MADE A PASS BY TOWER TO CONFIRM GEAR DOWN. A NORMAL LANDING WAS MADE WITH NO FURTHER PROBLEMS. TROUBLESHOT LANDING SYSTEM IAW FIM. LIGHT BULB FOR RI GHT MAIN GEAR INDICATOR WAS FOUND BURNT OUT. LIGHT BULB ON CENTER INSTRUMENT PANEL WAS REPLACED AND BOTH PRIMARY AND SE CONDARY GEAR INDICATORS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002090600223 20020906 00223 NM 2002 9 6 TSAA0251177 1 20020815 A 5330 6545769 SKIN BOEING 737 7372T4 1384492 NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 36847 23443 SKIN CRACK AT BS 380 BETWEEN STRINGER 28L AND 28R. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2002090600224 20020906 00224 NM 2002 9 6 TSAA0251178 1 20020816 A 5313 6978188 STRINGER BOEING 737 7372T4 1384492 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 FOUND CORROSION ON BS 500 AT STRINGER 26R. CUT AND REMOVED DAMAGED PORTION OF FORMED SECTION. FABRICATED REPAIR ANGLES AND DOUBLER IAW SRM. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2002090600225 20020906 00225 NM 2002 9 6 TSAA0234166 1 20020725 A 3411 PITOT TUBE BOEING 737 73773A 1384606 NM PITOT/STATIC SYS OBSTRUCTED A TSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 738AL 28499 DURING TAKEOFF ROLL THE CAPTAINS AIRSPEED INDICATOR ACCELERATED SLOWER THAN THE FIRST OFFICERS AIRSPEED INDICATOR. AFTE R LIFT-OFF, THE AIRCRAFT EXPERIENCED AN ENGINE WARNING LIGHT AND STICK SHAKER WARNING. RETURNED WITH NO FURTHER INCIDEN T. MAINTENANCE PERSONNEL FOUND A WASPS NEST (MUD DOBBER) IN THE CAPTAINS PITOT PROBE. THE PITOT PROBE WAS CLEANED. LE AK AND OPERATIONAL CHECKS WERE GOOD. OVERWEIGHT LANDING INSPECTION WAS COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVI CE. 2 L 7 2 4F RT A16WE 2002090600226 20020906 00226 NM 2002 9 6 TSAA0251179 1 20020617 A 5313 6546877 STRINGER BOEING 737 7372T4 1384492 NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 CRACKS BS 739, S-18R AND BS 745, S-19R. REMOVED DAMAGED AREA, VERIFIED CRACK REMOVAL USING HFEC METHOD, FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F A16WE E2EA 2002090600227 20020906 00227 NM 2002 9 6 TSAA0251180 1 20020815 A 5313 6546549 STRINGER BOEING 737 7372T4 1384492 NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 CRACK LOCATED AT BS 767, S-14L. TRIMMED OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND REPAIR ANGLES. 2 L 7 2 4F 4 F A16WE E2EA 2002090600228 20020906 00228 NM 2002 9 6 TSAA0251181 1 20020819 A 5320 6545866 STRAP BOEING 737 7372T4 1384492 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 36847 23443 KEEL BEAM VERTICAL STRAP CORRODED AT BS 532. BLENDED AND FLAP PEENED REPAIR AREA, FABRICATED TWO FILLER STRAPS, INSTALL ED FILLERS AND STRAP. 2 L 7 2 4F 4 F A16WE E2EA 2002090600231 20020906 00231 NM 2002 9 6 TSAA0253161 1 20020708 A 5330 6545800 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 IDENTIFIED A TWO INCH CRACK ON FUSELAGE SKIN AT BS274 STRINGER 15R. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002090600232 20020906 00232 NM 2002 9 6 TSAA0253162 1 20020708 A 5330 6545800 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 IDENTIFIED ONE INCH CRACK ON FUSELAGE SKIN AT BS 277 STRINGER 11L. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED A FILLER AND DOUBLER. INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002090600233 20020906 00233 NM 2002 9 6 TSAA0253163 1 20020708 A 5330 6573748 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 IDENTIFIED A TWO INCH CRACK ON FUSELAGE SKIN AT BS962 STRINGER 21L. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED A FILLER AND DOUBLER. INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002090600234 20020906 00234 NM 2002 9 6 TSAA0253164 1 20020708 A 5330 6573748 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 IDENTIFIED A TWO AND A HALF INCH CRACK ON FUSELAGE SKIN AT BS 942 STRINGER 24R. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED TWO EACH FILLER AND TWO EACH DOUBLER. INSTALLED REPAIR PARTS IAW SRM. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002090600235 20020906 00235 NM 2002 9 6 TSAA0253182 1 20020816 A 5711 654549816 SPAR BOEING 737 7372S5C 1384499 NM PWA JT8 JT8D17 52049 NE RT WING CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 RIGHT WING FRONT SPAR CRACK AND CORRODED AT FSS124.79 AND FSS134.80. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002090600236 20020906 00236 NM 2002 9 6 0202805534 1 20020830 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM MID CABIN DEFECTIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 534US 24265 DURING EMERGENCY LIGHT TEST, MID CABIN AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002090900076 20020909 00076 SO 2002 9 9 C2XA02BT050 1 20020904 A 2621 FIRE BOTTLE EMB 145 EMB145LR 3260212 SO CARGO BAY DEFECTIVE A C2XA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 27 13908 145465 EWR---CO3491, CREW REPORTED, BAGG EXT BTL INOP MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED BAGGAGE COMPARTMENT F IRE BOTTLES IAW EMB145 MM 26-03-01. OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT T00011AT 2002090600237 20020906 00237 NM 2002 9 6 UPS02239287 1 20020827 A 5210 BRACKET BOEING 727 72722C 138400F NM DOOR PULL HANDLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C DOOR PULL HANDLE SUPPORT BRACKET REPAIR CARRIED OUT IAW SRM 51-30-3 2 L 7 3 4F A3WE 2002090600238 20020906 00238 SO 2002 9 6 C2XA02BT051 1 20020905 A 3220 852701 SWITCH EMB 135 EMB135LR 3260305 SO FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 24517 145332 EWR---CO3181, CREW REPORTED, "AIR RETURN DUE TO LDG AIR GND FAILURE AND THRUST REVERSER #1 DISAGREE" MESSAGES AFTER R OTATION. RUMBLING HEARD FROM NOSE ON CLIMBOUT. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT AND REMOVED AND REPLACE D NOSE LANDING GEAR PROXIMITY SWITCH. TEST FLEW AIRCRAFT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002090600239 20020906 00239 NE 2002 9 6 ARWA20020902 2 20020903 A 7532 563883 BLEED VALVE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE A ARWA D RETURN TO BLOCK E J R VIBRATION/BUFFET WARNING INDICATION PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SO 19 1804 46711 1238 45896 644073 LOG PAGE # 112879. DISCREPANCY: DURING TAXI NOTICED # 3 ENGINE COMPRESSOR STALLING ACCELERATION OF ENGINE. CORRECTIVE ACTION: REMOVED AND REPLACED # 3 ENGINE SURGE BLEED VALVE IAW DC-8 MM 75-30-3. OPERATIONS CHECKED OK; RUNUP FOUND NORM AL IAW DC-8 MM 71-00. 2 L 7 4 4F 4 F 4A25 1E8 2002090600240 20020906 00240 EU 2002 9 6 QXEA0201337 1 20020902 A 3350 900835A BATTERY PACK FOKKER F28 F28MK4000 4990810 EU ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX- EVACUATION LIGHTS ON SEATS 12,13, AND 14AB ARE INOPERATIVE. REMOVED AND REPLACED EVACUATION BATTERY PACK. OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002090700001 20020907 00001 SO 2002 9 7 C2XA02TY134 1 20020906 A 5100 14522461003 DOUBLER EMB 145 EMB145 3260210 SO FRAME 20 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS During a scheduled inspection, corrosion was found on a doubler at the right hand beam hat section at frame 20. Ma intenance accomplished a blend-out repair IAW EMB GST #1927/02A and EMB145 CPM 51-21-04,05 and 06. The repair was satis factory, the aircraft will be released upon completion of inspection. 2 L 7 2 4F RT T00011AT 2002090800001 20020908 00001 SO 2002 9 8 RAIA00209233 1 20020702 A 4910 4501968B APU EMB 145 EMB145ER 3260211 SO SMOKE A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 808HK 9829 4223 145157 5311-PIT- SMOKE IN CABIN DURING CLIMB. MAINTENANCE DEFERRED APU IAW MEL. SUBSEQUENTLY MAINTENANCE REMOVED AND REPLACED A PU, OPS AND LK CK GOOD. 2 L 7 2 4F RT T00011AT 2002090800002 20020908 00002 EU 2002 9 8 RAIA00209234 1 20020807 A 2731 311078 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU ELEVATOR TRIM INOPERATIVE A RAIA O OTHER J WARNING INDICATION CR CRUISE 1 CE 03 553HK 41066 FLIGHT CREW REPORTED PITCH TRIM INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FO'S PITCH TRIM SWITCH, OPS CHECKED O K. 2 L 7 2 4T RT A41NM 2002090800003 20020908 00003 SO 2002 9 8 RAIA00209236 1 20020811 A 3350 HG2010AC02 INDICATOR EMB 145 EMB145 3260210 SO OVERHEATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 804HK 6764 145082 5256-PIT- CAPTAIN AHRS OVER HEAT INDICATION. MAINTENANCE REMOVED AND REPLACED #1 AHRS, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002090800004 20020908 00004 SO 2002 9 8 RAIA00209237 1 20020813 A 3350 1317 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 806HK 145112 MX-RIC - COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002090800005 20020908 00005 NE 2002 9 8 RAIA00209238 2 20020815 A 7200 TPE33114HR ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE FOD A RAIA O OTHER O OTHER DE DESCENT 1 CE 03 561HK 12531 41077 75107 5563-SPI - CREW REPORTED POSSIBLE BIRD INGESTION DURING DECENT INTO STL. MAINTENANCE FOUND DAMAGE BEYOND ON-WING REPAIR AND REMOVED AND REPLACED THE #2 ENGINE, LK AND OPS CK OK. 2 L 7 2 4T 4 T RT A41NM E18NE 2002090800006 20020908 00006 SO 2002 9 8 RAIA00209239 1 20020819 A 8011 35059104C STARTER EMB 145 EMB145 3260210 SO SEIZED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 804HK 4558 145082 5288-PIT - RIGHT ENGINE WILL NOT START, NO ROTATION. MAINTENANCE REMOVED AND REPLACED THE #2 AIR TURBINE STARTER, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002090800007 20020908 00007 EU 2002 9 8 RAIA00209243 1 20020824 A 3350 1819 LIGHT AEROSP ATR72 ATR72202 8680940 EU CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 721TE 217 MX-STL - MAIN CABIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED CABIN DOOR EMERGENCY LIGHT BULB, OPS CK OK. 2 H 7 2 4T RT A53EU 2002090800008 20020908 00008 EU 2002 9 8 RAIA00209245 1 20020830 A 3350 6134051 BATTERY PACK JETAIR JETSTM JETSTM4101 1500501 EU DISCHARGED A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 573HK 9597 347 41092 MX-STL - EMERGENCY LIGHT BATTERY #1 INOPERATIVE. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY, OPS CK OK 2 L 7 2 4T RT A41NM 2002090900002 20020909 00002 EU 2002 9 9 AUS20020783 1 20020724 A 2597 F0N91862UR12 WIRE FOKKER F27 F27MK50 EU PWA PWA120 PW125B NE GALLEY SHORTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S 23295 (AUS) NR 1 GALLEY WIRING SHORT CIRCUITED IN AREA UNDER THE REAR GALLEY. SUSPECT CAUSED BY MOISTURE ON THE WIRES. 2 H 7 2 4T 4 T RT A817 E20NE 2002090900003 20020909 00003 NM 2002 9 9 AUS20020785 1 20020730 A 2131 7110025 CONTROL PANEL BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU CABIN PRESSURE FAULTY W O OTHER O OTHER DE DESCENT 1 AU S 91030938 (AUS) PRESSURISATION SELECTOR PANEL FAULTY. 2 L 7 2 4F 4 F RT A16WE E21EU 2002090900004 20020909 00004 NM 2002 9 9 AUS20020786 1 20020801 A 7931 APT761000100DW TRANSMITTER DHAV DHC8 DHC8315 2809010 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE ENG OIL PRESS UNSERVICEABLE W O OTHER E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION DE DESCENT 1 AU S (AUS) NR 2 ENGINE OIL PRESSURE TRANSMITTER FAULTY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002090900005 20020909 00005 NM 2002 9 9 AUS20020787 1 20020725 A 2710 69B826571 BOLT BOEING 747 747338 NM AILERON FRACTURED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT AILERON PCU RODEND BOLT HEAD BROKEN. 2 L 7 2 4F RT A20WE 2002090900006 20020909 00006 GL 2002 9 9 AUS20020791 3 20020802 A 6197 189894001 WIRE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4MP3 GL STOP SOLENOID FAILED W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 AU S (AUS) LT PROPELLER GROUND IDLE STOP SOLENOID FAILED. BROKEN CONDUCTOR AT WIRING ENTRY INTO SOLENOID BODY. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 2002090900007 20020909 00007 CE 2002 9 9 AUS20020792 1 20020716 A 8012 96487 VALVE CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP HARTZL HCB3T HCB3TN3 GL START VALVE FAILED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) RT ENGINE PRIMARY FUEL SOLENOID VALVE FAULTY. INVESTIGATION FOUND THE OPERATING COIL SHORT CIRCUITED TO EARTH. 1 L 7 2 3T 4 T RT A28CE E4WE 6 C P15EA 2002090900009 20020909 00009 SW 2002 9 9 AUS20020794 1 20020729 A 5753 DW4K2H BEARING SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL TE FLAPS FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FLAP WALKING BEAM CENTRE BEARING DISINTEGRATED. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002090900010 20020909 00010 EU 2002 9 9 AUS20020795 1 20020731 A 5610 NP1701012 WINDSHIELD BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE COCKPIT CRACKED W O OTHER O OTHER CL CLIMB 1 AU S 3895 (AUS) RT COPILOTS "A" WINDSHIELD CRACKED ON FIRST LAYER. WINDSHIELD HEATING SYSTEM CHECKED SERVICEABLE. 2 H 7 4 4F 4 F A49EU E6NE 2002090900011 20020909 00011 NM 2002 9 9 AUS20020796 1 20020718 A 7312 MS990204 PLUG DHAV DHC8 DHC8201 2809001 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE FUEL HEATER MISSING W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) NR 2 ENGINE FUEL HEATER FOUND TO HAVE A YELLOW PLASTIC MS BLANKING PLUG FITTED IN PLACE OF THE CORRECT STAINLESS S TEEL PLUG PN MS9902-04. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002090900012 20020909 00012 EU 2002 9 9 AUS20020802 1 20020503 A 5280 DOOR FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU MLG CHAFED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) RT NOSE LANDING GEAR DOOR RUBBING ON RT NOSE WHEEL. LT NOSE WHEEL RUBBING ON WHEEL CUTOUT. NOSE WHEEL CENTERING OUT OF ADJUSTMENT. 2 L 7 2 4F 4 F RT A20EU E2EU 2002090900013 20020909 00013 EU 2002 9 9 AUS20020803 1 20020506 A 3230 SEQUENCE VALVE FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU NLG MALFUNCTIONED W O OTHER J WARNING INDICATION CL CLIMB 1 AU S (AUS) NOSE LANDING GEAR RETRACTION SYSTEM FAULTY. NLG SEQUENCE VALVE ADJUSTED. NLG DOOR SELECTOR VALVE AND NLG DOOR ACT UATOR RESTRICTOR REPLACED. 2 L 7 2 4F 4 F RT A20EU E2EU 2002090900014 20020909 00014 EU 2002 9 9 AUS20020805 1 20020515 A 2841 INDICATOR FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU FUEL QUANTITY OUT OF ADJUST W K NONE N FALSE WARNING IN INSP/MAINT 1 AU S (AUS) FUEL QUANTITY INDICATOR OUT OF CALIBRATION. 2 L 7 2 4F 4 F RT A20EU E2EU 2002090900015 20020909 00015 NE 2002 9 9 AUS20020808 3 20020806 A 6111 BLADE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE PROPELLER BIRD STRIKE W O OTHER C F.O.D. TO TAKEOFF 1 AU S (AUS) AIRCRAFT SUFFERED A BIRDSTRIKE ON TAKEOFF. INSPECTION COULD FIND NO IMPACT DAMAGE ON AIRFRAME OR ENGINE. EVIDENCE OF SUPERFICIAL DAMAGE TO RT PROPELLER BLADES. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002090900016 20020909 00016 NM 2002 9 9 AUS20020810 1 20020802 A 2150 200103091 TURBINE DHAV DHC8 DHC8315 2809010 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE CABIN COOLING SEIZED W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 AU S (AUS) NR 1 AIR CONDITIONING PACK AIRCYCLE MACHINE TURBINE SEIZED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002090900017 20020909 00017 NM 2002 9 9 AUS20020811 1 20020801 A 2910 65C268093172 LINE BOEING 737 73733A 1384673 NM CFMINT CFM56 CFM563B2 13802 EU MLG HYD SYS FAILED W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) MAIN LANDING GEAR ACTUATOR HYDRAULIC LINE PN 65C26809-3172 RUBBING ON SPOILER HYDRAULIC LINE PN 65C26809-3072. SPO ILER LINE LEAKING. LINES ARE LOCATED IN THE LT UNDERCARRIAGE BAY ABOVE THE MAIN LANDING GEAR. 2 L 7 2 4F 4 F RT A16WE E21EU 2002090900018 20020909 00018 NE 2002 9 9 AUS20020812 2 20020805 A 7200 ENGINE BAC 146 AVRO146RJ70A 1500095 EU LYC ALF520 ALF520* 41580 NE NR 4 FAILED W E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 AU S (AUS) NR 4 ENGINE INFLIGHT SHUTDOWN. LIMITED INFORMATION PROVIDED. 2 H 7 4 4F 4 F RT A49EU E6NE 2002090900019 20020909 00019 GL 2002 9 9 AUS20020814 2 20020805 A 7230 702887 COMPRESSOR WHEEL BOEING 747 747400 NM GE CF6 CF680C2* GL NR 2 ENGINE DAMAGED W E A ENGINE SHUTDOWN UNSCHED LANDING E F J VIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 AU S 12122 (AUS) NR 2 ENGINE N2 VIBRATION LEVELS HIGH. BORESCOPE INSPECTION FOUND DAMAGE TO THE FIFTH STAGE HIGH PRESSURE COMPRESS OR. 2 L 7 4 4F 4 F RT A20WE E23EA 2002090900020 20020909 00020 NM 2002 9 9 AUS20020815 1 20020805 A 4920 380029817 OIL COOLER BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL APU ENGINE FAILED W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S 5503 (AUS) APU AUTO SHUTDOWN. APU OIL COOLER AND BYPASS VALVE CHANGED TO RECTIFY DEFECT. 2 L 7 2 4F 4 F RT A1NM E23EA 2002090900021 20020909 00021 EU 2002 9 9 AUS20020816 2 20020804 A 7200 BEARING BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU NR 1 ENGINE MAKING METAL W O OTHER J WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) NR 1 ENGINE FORWARD SUMP CHIP DETECTOR CONTAINED METAL PARTICLES. NDT ANALYSIS FOUND THE PARTICLES TO BE M50 BEAR ING MATERIAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2002090900022 20020909 00022 NM 2002 9 9 AUS20020817 1 20020803 A 2722 3860061102 PCU BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE RUDDER ACTUATOR LEAKING W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 AU S 47703 0652 (AUS) UPPER RUDDER LOWER PCA LEAKING. LOSS OF HYDRAULIC FLUID. 2 L 7 4 4F 4 F RT A20WE E30NE 2002090900026 20020909 00026 NM 2002 9 9 AUS20020856 1 20020803 A 5753 65B1594511 FITTING BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE TE FLAPS FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) OUTBOARD TRAILING EDGE FLAP NR 2 BOAT FAIRING REAR ATTACHMENT FITTING SHEARED. 2 L 7 4 4F 4 F RT A20WE E30NE 2002090900029 20020909 00029 EU 2002 9 9 AUS20020862 1 20020531 A 2150 3269B0102 ACM AMD FALC50 FALCON900 2700160 EU GARRTT TFE731 TFE7315BR WP AC BAY LEAKING W C ABORTED TAKEOFF K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 AU S 1304 207 (AUS) TURBOCOOLER LEAKING OIL. SUSPECT CAUSED BY INTERNAL SEAL FAILURE. 2 L 7 3 4F 4 F RT A46EU E6WE 2002090900030 20020909 00030 EU 2002 9 9 AUS20020872 1 20020614 A 5754 ANV12SP21C ROLLER AMD FALC50 FALCON900 2700160 EU GARRTT TFE731 TFE7315BR WP LE FLAPS WORN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LEADING EDGE SLAT ROLLERS WORN. 2 L 7 3 4F 4 F RT A46EU E6WE 2002090900031 20020909 00031 CE 2002 9 9 AUS20020873 1 20020805 A 3230 4532103045001 BELLCRANK LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP MLG DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT MAIN LANDING GEAR OUTBOARD DOOR BELLCRANK BROKEN AND UPPER PUSHROD BENT. SUSPECT CAUSED BY INCORRECT RIGGING DU RING PRODUCTION. RT GEAR NOT DAMAGED BUT ALSO MISRIGGED. 2 L 7 2 4F 4 F RT T00008WI E6WE 2002090900032 20020909 00032 SW 2002 9 9 AUS20020874 1 20020809 A 2820 9000924 RESTRICTOR VALVE GULSTM 500 500S 0141107 SW LYC O540 IO540E1B5 41532 EA HARTZL HCC3Y HCC3YR2 NE FUEL DIST BLOCKED W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 AU S (AUS) FUEL VAPOR SEPARATOR / FILTER ASSEMBLY RESTRICTOR BLOCKED. THE RESTRICTOR IS LOCATED IN THE RETURN LINE FROM THE F UEL DISTRIBUTOR VALVE. 1 H 7 2 3O 3 O 6A1 1E4 5 C P25EA 2002090900033 20020909 00033 SW 2002 9 9 AUS20020882 1 20020413 A 2435 303001383 BRUSHES BELL 206 206L3 1182108 SW STARTER-GEN WORN W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S 5053 (AUS) STARTER-GENERATOR BRUSHES SEVERELY WORN. BURNING AND ARCING BETWEEN BRUSHES AND COMMUTATOR. 1 G 7 1 3U H2SW 2002090900034 20020909 00034 NE 2002 9 9 AUS20020883 2 20020807 A 7200 6058T83G01 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R375 R3754123F21 NE LEFT FAILED W E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 AU S (AUS) LT ENGINE FAILURE. LIMITED INFORMATION PROVIDED. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P17NE 2002090900035 20020909 00035 2002 9 9 AUS20020884 4 20020809 A 3425 CONNECTOR FOKKER F27 F27MK50 EU PWA PWA120 PW125B NE AHRU DIRTY W O OTHER O OTHER CL CLIMB 1 AU S 27793 (AUS) NR 2 ATTITUDE HEADING REFERENCE UNIT (AHRU) FAULTY. SUSPECT FAULT CAUSED BY DIRTY CONNECTOR. 2 H 7 2 4T 4 T RT A817 E20NE 2002090900036 20020909 00036 NM 2002 9 9 AUS20020887 1 20020810 A 2597 WIRE HARNESS BOEING 747 747 UTILSYS NM GALLEY CHILLER BURNED W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 AU S (AUS) CHILLER BOOST FAN WIRING LOOM BURNED. CARGO BAY INSULATION BLANKETS ALSO BURNED. 2 L 7 4 4F RT A20WE 2002090900037 20020909 00037 NM 2002 9 9 AUS20020888 1 20020812 A 2731 6355B000103 MOTOR BOEING 737 737800* NM GE CFM56 CFM567B24 NE ELEVATOR TAB FAILED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 AU S 270 1630C (AUS) STABILIZER TRIM MOTOR FAULTY. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002090900038 20020909 00038 2002 9 9 AUS20020889 4 20020812 A 2330 6456701 COOLING FAN BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL ENTERTAIN SYS FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) INFLIGHT ENTERTAINMENT SYSTEM COOLING FAN FAILED. 2 L 7 2 4F 4 F RT A1NM E23EA 2002090900040 20020909 00040 EU 2002 9 9 AUS20020893 1 20020809 A 2910 HTE400005 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP MCAULY 4HFR34 4HFR34C653 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) HYDRAULIC SYSTEM NON-RETURN VALVE LEAKING. SUSPECT LEAK EMANATING FROM ENGRAVED PART NUMBER IN CASE. 2 L 7 2 4T 4 T RT A56EU E4WE 6 C 3PNE 2002090900041 20020909 00041 CE 2002 9 9 AUS20020894 1 20020812 A 3260 BULB BEECH 200 B200C 1152924 CE PWA PT6 PT6A42 52043 NE MCAULY 4HFR34 4HFR34C754 NE MLG INDICATOR BURNED OUT W O OTHER N FALSE WARNING LD LANDING 1 AU S (AUS) LANDING GEAR INDICATOR GLOBES (4OFF) UNSERVICEABLE. 1 L 7 2 4T 4 T A24CE E4EA 6 C 3PNE 2002090900042 20020909 00042 NM 2002 9 9 AUS20020895 1 20020812 A 4940 38007021 STARTER BOEING 737 737800* NM GE CFM56 CFM567B24 NE APU FAILED W O OTHER O OTHER NR NOT REPORTED 1 AU S (AUS) APU FAILED TO START. STARTING SYSTEM INOPERATIVE. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002090900043 20020909 00043 NE 2002 9 9 AUS20020896 2 20020811 A 7200 ENGINE BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE NR 3 & 4 SURGES W A UNSCHED LANDING E F J VIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 AU S (AUS) NR 3 AND NR 4 ENGINES SUFFERED MULTIPLE SURGES. 2 L 7 4 4F 4 F RT A20WE E30NE 2002090900044 20020909 00044 NE 2002 9 9 AUS20020897 3 20020809 A 6111 A1633115 O-RING MCAULY 4HFR34C652 SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UHR WP MCAULY 4HFR34 4HFR34C652 NE PROPELLER LEAKING W A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 AU S 222 (AUS) RT PROPELLER BLADE O-RING SEAL STICKING. OIL LEAKING PAST THE SEAL ENTERED THE ENGINE AIR INTAKE AND FLOWED THROUG H THE RT BLEED AIR SYSTEM INTO THE CABIN. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002090900045 20020909 00045 NE 2002 9 9 AUS20020900 3 20020809 A 6111 7943051 PLUG HAMSTD 14SF23 DHAV DHC8 DHC8315 2809010 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE PROPELLER BLADE CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) LT PROPELLER NR 2 BLADE BUTT PLUG CRACKED ALLOWING OIL TO LEAK INTO THE BLADE CAVITY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002090900046 20020909 00046 NE 2002 9 9 AUS20020902 2 20020818 A 7200 BEARING BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 4 FAILED W O OTHER E VIBRATION/BUFFET CL CLIMB 1 AU S (AUS) ENGINE SURGED FOLLOWED BY FAILURE WITH VIBRATION. FIRE BOTTLE FIRED. SUSPECT NR 4 BEARING PACKAGE FAILURE. 2 H 7 4 4F 4 F A49EU E6NE 2002090900047 20020909 00047 NE 2002 9 9 AUS20020904 2 20020728 A 7260 39737801 BEARING BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE DDG FAILED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 AU S (AUS) LT ENGINE DEDICATED DRIVE GENERATOR (DDG) LINE 12 BEARING FAILED. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002090900048 20020909 00048 EU 2002 9 9 AUS20020905 1 20020818 A 6410 109813201111 BLADE AGUSTA A109 A119 0261102 EU PWA PT6 PT6B36 52043 EA TAIL ROTOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) TAIL ROTOR BLADE PAINT CRACKED. 1 G 7 2 3U 4 U H7EU E4EA 2002090900049 20020909 00049 NE 2002 9 9 AUS20020906 2 20020815 A 7250 3039300 MODULE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A67R 52043 NE HARTZL HCA6A HCA6A3 NE POWER SECTION LEAKING W K NONE O OTHER IN INSP/MAINT 1 AU S 3013 (AUS) RT ENGINE POWER SECTION MODULE INTERNAL OIL LEAK. 2 H 7 2 4T 4 T A41EU E26NE 6 C P14NE 2002090900050 20020909 00050 CE 2002 9 9 AUS20020907 1 20020815 A 2424 51538001 GCU BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA AC REGULATOR OUT OF ADJUST W O OTHER J WARNING INDICATION CL CLIMB 1 AU S 757 342A (AUS) RT GENERATOR CONTROL UNIT (GCU) OUT OF ADJUSTMENT. 2 L 7 2 4T 4 T RT A24CE E4EA 2002090900051 20020909 00051 2002 9 9 AUS20020919 4 20020821 A 3416 AA300 INDICATOR DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE ALTIMETER FAULTY W O OTHER N FALSE WARNING CR CRUISE 1 AU S (AUS) RADIO ALTITUDE SYSTEM FAULTY GIVING INCORRECT GPWS WARNINGS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002090900052 20020909 00052 EU 2002 9 9 AUS20020920 1 20020821 A 2435 BRUSHES PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL STARTER GEN WORN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) STARTER GENERATOR BRUSHES WORN. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002090900053 20020909 00053 2002 9 9 AUS20020921 4 20020314 A 3418 9754421421 TRANSMITTER PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL STALL WARNING FAULTY W O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 AU S (AUS) ANGLE OF ATTACK TRANSMITTER VANE BEARING CORRODED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002090900054 20020909 00054 2002 9 9 AUS20020922 4 20020619 A 3418 9754421421 TRANSMITTER PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL STALL WARNING CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ANGLE OF ATTACK TRANSMITTER VANE BEARING CORRODED AND STICKING. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002090900055 20020909 00055 EU 2002 9 9 AUS20020923 1 20020813 A 2435 BRUSHES LUCAS PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL STARTER GEN WORN W K NONE O OTHER IN INSP/MAINT 1 AU S 985 YO236 (AUS) STARTER-GENERATOR BRUSHES WORN EXCESSIVELY. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002090900056 20020909 00056 2002 9 9 AUS20020924 4 20020722 A 3418 9754421421 TRANSMITTER PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL STALL WARNING CORRODED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 AU S (AUS) ANGLE OF ATTACK TRANSMITTER VANE BEARINGS CORRODED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002090900057 20020909 00057 2002 9 9 AUS20020925 4 20020814 A 3418 BEARING PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL ANGLE OF ATTACK STICKING W O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 AU S (AUS) ANGLE OF ATTACK TRANSMITTER VANE BEARINGS STICKING. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002090900058 20020909 00058 GL 2002 9 9 AUS20020929 1 20020810 A 4920 ENGINE AEROVD L39 L39C 05620RN GL APU FAILED W O OTHER E T VIBRATION/BUFFET ENGINE CASE PENETRATION NR NOT REPORTED 1 AU S (AUS) APU SUFFERED A CATASTROPHIC FAILURE DURING ENGINE START. SUSPECTCAUSED BY FATIGUE FAILURE OF IMPELLER OR FAILURE O F TURBINE BEARING. 1 M 7 1 4U RT EXPA1M71 2002090900061 20020909 00061 SO 2002 9 9 AUS20020932 1 20020606 A 3245 6006 TUBE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL NLG TIRE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NOSE WHEEL TIRE FLAT. INVESTIGATION FOUND TIRE TUBE HOLED. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2002090900062 20020909 00062 SO 2002 9 9 AUS20020934 1 20020813 A 5711 6244802 FITTING PIPER PA28 PA28RT201 7102818 SO LYC O360 IO360C1C6 41514 EA MCAULY 2D34C 2D34C215 GL WING SPAR CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT AND RT REAR SPAR ATTACHMENT PLATES CORRODED. ATTACHMENT ANGLEFLOOR PLATE ATTACHMENT RIVETS CORRODED AND RIVET H EADS MISSING. 1 L 7 1 3O 3 O 2A13 1E10 5 C P7EA 2002090900063 20020909 00063 NM 2002 9 9 AUS20020936 1 20020810 A 2750 65B8112716 TRANSMISSION BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE TE FLAPS FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 7 FLAP TRANSMISSION ASSEMBLY FAULTY WITH A LOUD CLICKING NOISE BEING HEARD. EXCESSIVE AXIAL PLAY ALSO FOUND IN OUTPUT SHAFT. 2 L 7 4 4F 4 F RT A20WE E30NE 2002090900064 20020909 00064 EU 2002 9 9 AUS20020939 1 20020822 A 3230 F8553048401 HOSE FOKKER F27 F27MK50 EU PWA PWA120 PW125B NE MLG HYD SYS FAILED W O OTHER K F FLUID LOSS FLT CONT AFFECTED CL CLIMB 1 AU S 1585 (AUS) LT MAIN LANDING GEAR RETRACTION HOSE BURST. LOSS OF HYDRAULIC FLUID. 2 H 7 2 4T 4 T RT A817 E20NE 2002090900066 20020909 00066 GL 2002 9 9 AUS20020941 2 20020818 A 7261 CHIP DETECTOR BOEING 767 76733A 1385209 NM GE CF6 CF680C2* GL NR 1 ENGINE CONTAMINATED W K NONE J WARNING INDICATION IN INSP/MAINT 1 AU S (AUS) NR 1 ENGINE CHIP DETECTOR CONTAINED METAL PARTICLES. METALLURGICAL INVESTIGATION FOUND THAT THE METAL WAS NOT FROM ANY ENGINE COMPONENT AND IT IS SUSPECTED TO BE BUILD SWARF. 2 L 7 2 4F 4 F RT A1NM E23EA 2002090900067 20020909 00067 CE 2002 9 9 AUS20020943 1 20020819 A 3010 27S7D510903 BOOT CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP DEICE SYSTEM SPLIT W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LEADING EDGE DE-ICE BOOT SPLIT LONGITUDINALLY. 1 L 7 2 3T 4 T RT A28CE E4WE 2002090900068 20020909 00068 SW 2002 9 9 AUS20020946 1 20020823 A 2913 246006 VALVE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL HYD POWER PACK FAULTY W O OTHER J WARNING INDICATION TO TAKEOFF 1 AU S 4805 (AUS) POWER PACK MOUNTED HYDRAULIC GEAR VALVE ASSEMBLY FAULTY. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002090900069 20020909 00069 NM 2002 9 9 AUS20020947 1 20020823 A 4920 380029815 GEARBOX BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL APU ENGINE CONTAMINATED W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S (AUS) APU AUTO SHUTDOWN. INSPECTION FOUND CONTAMINATION ON THE GEARBOX MAGNETIC PLUG. 2 L 7 2 4F 4 F RT A1NM E23EA 2002090900070 20020909 00070 NE 2002 9 9 AUS20020953 2 20020826 A 7220 BLT5371 BOLT BOEING 767 767338 1385151 NM RROYCE RB211 RB211524* NE LT ENGINE MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT ENGINE NOSE CONE SUPPORT RING BOLTS MISSING. 2 L 7 2 4F 4 F RT A1NM E12EU 2002090900071 20020909 00071 CE 2002 9 9 AUS20020954 1 20020824 A 3230 LANDING GEAR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4MP3 GL MAINS MALFUNCTIONED W O OTHER J WARNING INDICATION AP APPROACH 1 AU S (AUS) LANDING GEAR EXTENSION SYSTEM FAULTY. GEAR EXTENDED MANUALLY. INVESTIGATION AND GROUND TESTING COULD FIND NO FAU LTS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 2002090900072 20020909 00072 SO 2002 9 9 AUS20020956 1 20020828 A 5220 HANDLE PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA HARTZL HCE2Y HCE2YK2 GL EMERGENCY EXIT BENT W K NONE O OTHER IN INSP/MAINT 1 AU S 6678 (AUS) EMERGENCY EXIT DOOR HANDLE BENT. 1 L 7 2 3O 3 O A20SO E14EA 5 C P9EA 2002090900073 20020909 00073 WP 2002 9 9 ABXA020154 1 20020904 A 2120 1808491 COALESCER BAG DOUG DC9 DC941 302207N WP DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 23 973AX 47511 STRONG SMELL WHILE AT TAKE-OFF POWER. PERFORMED ENGINE RUN, OPERATED BOTH PACKS FROM APU AND ENGINES. NO SMELL NOTED. VI SUALLY INSPECTED PNEUMATIC DUCTING, NO DEFECTS NOTED. CHECKED ACM OILS AND REPLACED COALESCER BAGS IAW DC-9 MM PROCEDURE S. 2 L 7 2 4F A6WE 2002090900074 20020909 00074 NM 2002 9 9 C1HA200285013 1 20020908 A 3350 900835A BATTERY PACK BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 685CA 22492 Overhead emergency exit light inoperative at row 20. Removed and replaced emergency exit light battery pack per MM. Oper ational checks good. 2 L 7 3 4F A3WE 2002090900075 20020909 00075 NM 2002 9 9 DHL2002720004 1 20020906 A 2613 1014A POWER UNIT BOEING 727 727228 1384083 NM A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 720DH 19544 1) APU FIRE WARNING SYSTEM WILL NOT TEST ON PREFLIGHT. 2) DEFERRED APU FIRE WARNING PER MEL 26-11 CAT. "C" DMI #10316 ASSIGNED. PLACARD INSTALLED.3) REF. DMI #10316 APU FIRE WARNING SYSTEM WILL NOT TEST. 4) REMOVED AND REPLACED APU OPER ATING POWER UNIT. RELAY OPS CHECK GOOD IAW B727 M/M 26-15-00. THIS CLEARS DMI #10316. PLACARD REMOVED. 2 L 7 3 4F RT A3WE 2002090900077 20020909 00077 WP 2002 9 9 GTIA010874A 1 20020719 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND LONGERON END FITTING 29R STATION 1338 HAS CORROSION AROUND FASTENERS ON FITTING. MATERIAL LOSS FOUNDED OUT OF LIMITS. REMOVED FITTINGS. INSTALLED NEW FITTING 29R. (M) 2 L 7 2 4F A6WE 2002090900078 20020909 00078 WP 2002 9 9 GTIA020875 1 20020730 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP BATTERY PACK BENT A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND LEFT AND RIGHT OVERWING EXIT SIGNS INOPERATIVE, UPPER SIGNS ONLY. FOUND BATTERY PACK CONTACT BENT. REALIGN ED CONTACT. (M) 2 L 7 2 4F A6WE 2002090900079 20020909 00079 WP 2002 9 9 GTIA020876 1 20020707 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND DENT AT FS 69 ABOVE RIGHT NOSE GEAR DOOR REQUIRES PAINT REMOVAL, DYE PENETRANT INSPECTION, FOR CRACK EVALUAT ION. AREA FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER. INSTALLED DOUBLER AND FILL ER. (M) 2 L 7 2 4F A6WE 2002090900080 20020909 00080 WP 2002 9 9 GTIA020877 1 20020628 A 7160 5930645509 NOSE COWL DOUG DC9 DC982 3022082 WP NR 2 ENGINE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND NR 2 ENGINE, NOSE COWL 4 O'CLOCK TO 8 O'CLOCK POSITION SOUND SUPPRESSION MATERIAL DELAMINATED. REPLACED DAM AGED NOSE COWL. (M) 2 L 7 2 4F A6WE 2002090900081 20020909 00081 WP 2002 9 9 GTIA020878 1 20020621 A 5730 PANEL DOUG DC9 DC982 3022082 WP RT WING DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND RIGHT WING HAD DENT/DAMAGE AT OUTER SKIN FUELING PANEL. STOP DRILLED CRACK FOUND IN DENT. FABRICATED DOUBL ER. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2002090900082 20020909 00082 WP 2002 9 9 GTIA020879 1 20020706 A 5522 SKIN DOUG DC9 DC982 3022082 WP ELEVATOR SCRATCHED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND LEFT ELEVATOR UPPER SURFACE HAS DEEP SCRATCH. FABRICATED NEW SKIN, DOUBLER AND SPLICE. INSTALLED SKIN, DOU BLER AND SPLICE. (M) 2 L 7 2 4F A6WE 2002090900083 20020909 00083 WP 2002 9 9 GTIA020881 1 20020628 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND CRACK UNDER FORWARD RIGHT SIDE OF LOWER VHF ANTENNA, SKIN, DURING EDDY CURRENT INSPECTION FOUND 2.5 INCH CRA CK. FABRICATED SKIN AND DOUBLER. INSTALLED SKIN AND DOUBLER. (M) 2 L 7 2 4F A6WE 2002090900084 20020909 00084 WP 2002 9 9 GTIA020882 1 20020704 A 5280 DOOR FRAME DOUG DC9 DC982 3022082 WP LT MLG DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND LEFT MLG DOOR HAS CRACKED AT FORWARD AFT INBOARD FRAME, ANGLE PREVIOUS REPAIR. CUT OUT DAMAGE. FORMED DOUB LER AND FRAME. INSTALLED NEW FRAME AND DOUBLER. (M) 2 L 7 2 4F A6WE 2002090900085 20020909 00085 WP 2002 9 9 GTIA020883 1 20020625 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - REMOVAL OF SUPPORT ANGLE SUB FLOOR WAS FOUND TO HAVE EXFOLIATION. CUT OUT DAMAGED AREA. FABRICATED NEW SUB FLOOR SECTION AND DOUBLER. INSTALLED NEW SUB FLOOR AND DOUBLER. (M) 2 L 7 2 4F A6WE 2002090900086 20020909 00086 WP 2002 9 9 GTIA020884 1 20020623 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND FLOORBOARD CORRODED. REMOVED FLOOR SUPPORT. FABRICATED, DRILLED AND LOCATED NEW SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002090900087 20020909 00087 WP 2002 9 9 GTIA020885 1 20020623 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND MID PIT HAS CORROSION AT LONGERON. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2002090900088 20020909 00088 WP 2002 9 9 GTIA020886 1 20020811 A 2530 112253 COFFEEMAKER DOUG DC9 DC982 3022082 WP GALLEY MALFUNCTIONED A GTIA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 820NK 49126 DTW - FLT 313 - FOUND FORWARD GALLEY-LOW POT SMELLED SMOKE, SMELLED LIKE PLASTIC BURNING. PULLED C/B'S AND TURNED OFF G ALLEY POWER SMELL STOPPED. REMOVED AND REPLACED FORWARD GALLEY LOWER COFFEE MAKER. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2002090900089 20020909 00089 WP 2002 9 9 GTIA020887 1 20020717 A 5320 ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - BELT FRAME LOWER ATTACH ANGLE CRACKED FS 529 STATION 28L AND 27L. CUT OUT CRACKED ATTACH ANGLE. FABRICATED REPAI R. INSTALLED REPAIR. (M) 2 L 7 2 4F A6WE 2002090900090 20020909 00090 CE 2002 9 9 AUS20020957 1 20020825 A 5210 1013840961 HANDLE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A42 52043 NE PAX DOOR SHEARED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) AIRSTAIR DOOR INTERNAL HANDLE SHAFT SHEARED PREVENTING THE DOOR FROM BEING OPENED FROM THE INSIDE. 1 L 7 2 4T 4 T A24CE E4EA 2002090900091 20020909 00091 WP 2002 9 9 GTIA020888 1 20020717 A 5320 ATTACH ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND MID CARGO FORWARD BULKHEAD LOWER ATTACH ANGLE CORRODED FS 541 LBL 15 INCHES TO RBL 15 INCHES. REMOVED ATTAC H ANGLE. FABRICATED A NEW SUPPORT ANGLE. INSTALLED SUPPORT ANGLE. (M) 2 L 7 2 4F A6WE 2002090900092 20020909 00092 WP 2002 9 9 GTIA020889 1 20020803 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CUT A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND ONE AFT STAIRWAY EMERGENCY LIGHT IS INOPERATIVE. TROUBLESHOT FOUND EMERGENCY LIGHT WIRES CUT AT SPLICE POIN TS. RESPLICED WIRES. (M) 2 L 7 2 4F A6WE 2002090900093 20020909 00093 WP 2002 9 9 GTIA020890 1 20020714 A 5730 PANEL DOUG DC9 DC981 3022081 WP WING DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND PANEL 1120C HAS A DENT, BARE METAL. DENT OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR DOUBLER. (M ) 2 L 7 2 4F A6WE 2002090900094 20020909 00094 WP 2002 9 9 GTIA020891 1 20020714 A 5730 PANEL DOUG DC9 DC981 3022081 WP WING DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND PANEL 1171C BARE METAL ON BACK SIDE, NUMEROUS OXIDIZED SCREW HEADS AND SCREW HOLES, EXFOLIATION CORROSION IN TWO PLACES. FOUND MATERIAL TO BE OUT OF LIMITS IN 2 PLACES. FABRICATED TWO DOUBLERS. INSTALLED TWO DOUBLERS. (M) 2 L 7 2 4F A6WE 2002090900095 20020909 00095 WP 2002 9 9 GTIA020892 1 20020716 A 5730 PANEL DOUG DC9 DC981 3022081 WP WING CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND PANEL 1220C, EXFOLIATION CORROSION NEAR CORNER, SEVERAL OXIDIZED SCREW HOLES AND HEADS. MATERIAL LOSS OUT O F LIMITS. REPAIR DOUBLER FABRICATED. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2002090900096 20020909 00096 WP 2002 9 9 GTIA020893 1 20020724 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - SUBFLOOR AT STATION LBL 26 TO LBL 56 STATION 200-219 HAS 2 CRACKS. DRILLED AND LOCATED FLOOR WEB. (M) 2 L 7 2 4F A6WE 2002090900097 20020909 00097 WP 2002 9 9 GTIA020894 1 20020717 A 5230 FITTING DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PIT STATION 1155 L25R-L26R DOOR LATCH FITTING ON FORWARD DOOR FRAME IS CRACKED. REMOVED OLD DOOR LATCH FITTING FROM FRAME DRILLED NEW DOOR LATCH. INSTALLED DOOR LATCH FITTING. (M) 2 L 7 2 4F A6WE 2002090900098 20020909 00098 WP 2002 9 9 GTIA020895 1 20020718 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FORWARD CARGO FS 427 FLOOR SUPPORT CORRODED AND DOUBLER DRILLED STATION 29R-29L. REMOVED DAMAGED FLOOR SUPP ORT. LOCATED AND DRILLED NEW PART. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002090900099 20020909 00099 WP 2002 9 9 GTIA020896 1 20020718 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FORWARD CARGO FS 427 FLOOR SUPPORT CORRODED AND DOUBLE DRILLED STATION 29R-28R. REMOVED FLOOR SUPPORT STATI ON 427 RBL 29 TO LBL 28. FABRICATED NEW SUPPORT. INSTALLED SUPPORT. (M) 2 L 7 2 4F A6WE 2002090900100 20020909 00100 WP 2002 9 9 GTIA020897 1 20020718 A 7120 ISOLATOR DOUG DC9 DC981 3022081 WP RT ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND RIGHT ENGINE FORWARD LOWER VIBRATION ISOLATOR INNER CORE ASSEMBLY CONTACTING OUTER RETAINER AND SLIPPAGE MAR KS MORE THEN .5 INCH. REMOVED RIGHT ENGINE FORWARD LOWER VIBRATION ISOLATOR INNER CORE ASSEMBLY. INSTALLED RIGHT LOWER VIBRATION ISOLATOR. (M) 2 L 7 2 4F A6WE 2002090900101 20020909 00101 WP 2002 9 9 GTIA020898 1 20020716 A 5320 ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - AFT PIT STATION 1212 CORNER ANGLE, DOOR FRAME TO SKIN, IS CORRODED. REMOVED CORNER ANGLE. DRILLED AND LOCATED NE W ANGLE. INSTALLED NEW ANGLE. (M) 2 L 7 2 4F A6WE 2002090900102 20020909 00102 WP 2002 9 9 GTIA020899 1 20020716 A 5320 ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PIT STATION 1155 CORNER ANGLE, DOOR FRAME TO SKIN, IS CORRODED. REMOVED CORNER ANGLE. DRILLED AND LOCA TED NEW ANGLE. INSTALLED NEW ANGLE. (M) 2 L 7 2 4F A6WE 2002090900103 20020909 00103 WP 2002 9 9 GTIA020900 1 20020716 A 5330 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND ANTENNA INNER DOUBLER CORRODED. REMOVED ANTENNA DOUBLER. LOCATED AND DRILLED ANTENNA DOUBLER. INSTALLED D OUBLER. (M) 2 L 7 2 4F A6WE 2002090900104 20020909 00104 WP 2002 9 9 GTIA020901 1 20020716 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - AFT PIT STATION 1155-1212 L29R, THRESHOLD/FLOORBOARD SUPPORT HAS AREAS OF BARE METAL/LT CORROSION. REMOVED FLOOR SUPPORT. INSTALLED NEW FLOOR BOARD SUPPORT. (M) 2 L 7 2 4F A6WE 2002090900105 20020909 00105 WP 2002 9 9 GTIA020902 1 20020716 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PIT STATION 1212-1220 BETWEEN L29R-L30, INTERCOSTAL IS CORRODED. REMOVED DAMAGED PARTS. FORMED PARTS. INSTALLED PARTS. (M) 2 L 7 2 4F A6WE 2002090900106 20020909 00106 WP 2002 9 9 GTIA020903 1 20020716 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PIT STATION 1322-1338 L226, LOWER FLANGE OF INTERCOSTAL IS CORRODED AROUND ATTACH FASTENERS. REMOVED IN TERCOSTAL. FORMED INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002090900107 20020909 00107 WP 2002 9 9 GTIA020904 1 20020717 A 5330 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FORWARD CARGO FS 263 STATION 23L-24L PREVIOUS REPAIR HAS CRACKS ON DOUBLER. REMOVED EXISTING DOUBLER, SPLIC ES AND STRAP. FABRICATED DOUBLER, SPLICES AND STRAP. INSTALLED NEW DOUBLER, SPLICES AND STRAPS. (M) 2 L 7 2 4F A6WE 2002090900108 20020909 00108 GL 2002 9 9 C2XA02CL169 2 20020814 A 7313 3035060 FUEL NOZZLE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE COKED A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 22909 145459 CAE311887 CLE FLIGHT 4004 THE CREW REPORTED A LAV SMOKE WARNING INDICATION DURING CLIMB ACCOMPANIED BY A STRONG ODOR. MAINTENANCE REPLACED THE NR 1 ENGINE FUEL NOZZLES. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002090900109 20020909 00109 SO 2002 9 9 C2XA02CL170 1 20020815 A 3230 23092900001 UPLOCK EMB 145 EMB145LR 3260212 SO RT MLG FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 13949 10369 145057 CLE FLIGHT 3092 THE CREW REPORTED WHEN THE GEAR WAS RETRACTED RECEIVED A LANDING GEAR LEVER DISAGREE WARNING MESSAGE ALO NG WITH A RIGHT MAIN GEAR UNLOCK LIGHT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT M AIN GEAR UPLOCK BOX. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002090900110 20020909 00110 SO 2002 9 9 C2XA02CL174 1 20020820 A 5610 163500111 WINDSHIELD EMB 135 EMB135LR 3260305 SO COCKPIT CRACKED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 12528 1737 145504 CLE FLIGHT 3237 THE CREW REPORTED THE CAPTAINS WINDSHIELD SHATTERED DURING CLIMBOUT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002090900111 20020909 00111 EU 2002 9 9 MALA020529 1 20020823 A 5260 TRACK SAAB SF340 340B 7860101 EU AIRSTAIRS CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING 4K-INSPECTION IN CWA, AIRSTAIR MAIN TRACK HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002090900112 20020909 00112 EU 2002 9 9 MALA020530 1 20020823 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING 4K-INSPECTION IN CWA, GALLEY I/B SEAT TRACK HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-41. 2 L 7 2 4T RT A52EU 2002090900113 20020909 00113 EU 2002 9 9 MALA020531 1 20020823 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING 4K-INSPECTION IN CWA, FRAME 288 AND 294 UPPER WEBBING HAS LIGHT CORROSION. MAINTENANCE REMOVED WEBBING FOR BOTH FRAMES IAW SRM 51-20. 2 L 7 2 4T RT A52EU 2002090900114 20020909 00114 EU 2002 9 9 MALA020532 1 20020903 A 2560 SEAL BAC 146 AVRO146RJ85A 1500097 EU FLASHLIGHT BROKEN A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 529XJ E2363 FWD F/A FLASHLIGHT EMERGENCY SEAL BROKEN. MAINTENANCE REPLACED SEAL ON FWD EMERGENCY FLASHLIGHT. 2 H 7 4 4F RT A49EU 2002090900115 20020909 00115 2002 9 9 P5CA0200694 4 20020805 A 3417 78031055 ADC BOEING 747 747300 GL NR 1 FAILED A P5CA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 WP 23 354MC 23394 DUAL CADC FAILURE CAUSING FAILURE IN TRANSPONDER ALTITUDE REPORTING & INACCURATE ALTIMETER & AIRSPEED INDICATIONS. NR 1 & NR 3 INS WOULD NOT UPDATE. REMOVED AND REPLACED NR 1 CADC. CHECKED ALL DRAINS FOR MOISTURE; NONE FOUND. PURGED PIT OT/STATIC LINES AND FITTINGS WITH DRY NITROGEN ON BOTH SYSTEMS. RERACKED NR 2 CADC. PERFORMED FULL PITOT STATIC CHECK FOR ALL ASSOCIATED AIR DATA INSTRUMENTS AND LEAKS IN THE SYSTEM. NO LEAKS NOTED. 2 L 7 4 4F RT A20WE 2002090900116 20020909 00116 NM 2002 9 9 P5CA0200696 1 20020810 A 5350 65B067327 PANEL BOEING 747 747341 13848AM NM FAIRING DAMAGED A P5CA K NONE O OTHER UK UNKNOWN 1 WP 23 355MC 23395 FOUND 6 INCH CRACK IN HONEYCOMB OF PANEL 193 AFT OF LT BODY GEAR FAIRING PANEL. REPAIRED PANEL AFT OF LT BODY GEAR BS 1 620 TO BS 1660 AS PER B747 SRM 51-40-07. LT BODY GEAR O/B STRUT DOOR DAMAGED. DOOR REMOVED, INSTALLED NEW DOOR ASSY. REINSTALLED LEFT BODY GEAR SHOCK STRUT USING ORIG ROD IAW MM 32-14-00. INSTALLED PUTTY TO DOOR STOPS. REQ CHK & MEASUR E ON NEXT LEG IAW MM 32-14-00, PG 519, CHAP H. FOUND HOLE IN WING TO BODY FAIRING BEHIND LEFT GEAR STRUT. REMOVED & RE PLACED BODY GEAR FAIRING PANEL JUST AFT OF LEFT BODY GEAR AS PER B747 SRM 51-10-01. ALL DAMAGE OCCURRED DUE TO FOD ON R UNWAY DURING TAKEOFF OR LANDING. 2 L 7 4 4F RT A20WE 2002090900117 20020909 00117 NE 2002 9 9 P5CA0200697 2 20020816 A 7200 JT9D7J ENGINE BOEING 747 747200 1384847 NM PWA JT9 JT9D7 52054 NE LT WING MAKING METAL A P5CA E B ENGINE SHUTDOWN EMER. DESCENT R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 23 524UP 21446 685971 COMPRESSOR STALL & ENGINE FAILURE AT FL 37.0. SECURED ENGINE PER PAC ABNORMAL PROCEDURE & CHECKLIST. EGT INCREASING PA ST 910 DEGREES WHEN SHUTDOWN INITIATED. UPON INSPECTION, FOUND METAL IN TAILPIPE & LR 3.5 BLEED. ENGINE CHANGE REQUIRE D. REMOVED & REPLACED ENGINE. 2 L 7 4 4F 4 F RT A20WE E20EA 2002090900118 20020909 00118 NM 2002 9 9 SWAA021948 1 20020825 A 3350 PH22300L TRACK BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTO LUMINESCENT TRACK STRIP CRACKED FROM ROW NR 7 TO OVERWING EXIT. REMOVED AN D REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2002090900119 20020909 00119 WP 2002 9 9 UPS02839122 1 20020726 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 FLOORBEAM STA 879 RBL 60 IS CRACKED AT O/B LIGHTENING HOLE. SPLICED IN NEW SECTION OF FLOORBEAM IAW REO G08713. 2 L 7 4 4F RT 4A25 2002090900120 20020909 00120 WP 2002 9 9 UPS02839123 1 20020809 A 5720 FITTING DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 RT WING STR 51 I/B SIDE STA 74 IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D, LOCATED DRILLED AND DEBURRED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRM 51-1-20D, TORQUED BOLT IAW DC8 SRM 51-1-23. 2 L 7 4 4F RT 4A25 2002090900121 20020909 00121 WP 2002 9 9 UPS02839124 1 20020730 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 REPAIR DOUBLER 715-3L-12 STA 1690-1698 AND LONG 28L IS CLASSIFIED AS CAT D ONLY 2 ROWS OF FASTENERS B EYOND CUTOUT AND 3 OF 4 CORNERS OF CUTOUT ARE SQUARE. REMOVED EXISTING REPAIRS AND FITTINGS, FABBED, LOCATED & DRILLED DOUBLER & FILLER IAW DC8 SRM 53-2-0 FIG 7 SHT 5. INSTALLED DOUBLER FILLER & END FITTING IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002090900122 20020909 00122 WP 2002 9 9 UPS02839125 1 20020730 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB, LONGERON 11 CRACKED APPROX 2 INCHES, FOUND BY X-RAY INSPECTION. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2002090900123 20020909 00123 WP 2002 9 9 UPS02839126 1 20020730 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB LONGERON 11 CRACKED APPROX 2 INCHES, FOUND BY X-RAY INSPECTION. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2002090900124 20020909 00124 WP 2002 9 9 UPS02839129 1 20020806 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 RT MLG DOOR CUTOUT AREA AFT WEB PNL OF UPLATCH CUTOUT IS CRACKED. FABBED NEW WEB IAW DAC DWG 5651021 & NEW ATTACH ANGLE IAW DAC DWG 56 51221. INSTALLED ASSY IAW DC8 SRM 51-1-21, 51-3-0 & 51-1-20D. 2 L 7 4 4F RT 4A25 2002090900125 20020909 00125 WP 2002 9 9 UPS02839132 1 20020725 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 LT AFT PRESSURE BULKHEAD CRACKED AT FS 1766 L11L. REPAIRED AREA IAW DC8 SRM 53-2-5 FIG 14A AND DAC D WG SRO8530007. 2 L 7 4 4F RT 4A25 2002090900126 20020909 00126 WP 2002 9 9 UPS02839134 1 20020813 A 5414 SKIN DOUG DC8 DC871F 302199D WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 NR 1 PYLON O/B SIDE AT PNL 199A UPPER SKIN IS CRACKED. FABBED DOUBLER IAW DC8 SRM 54-2-0, INSTALLED DOUBLER IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002090900127 20020909 00127 WP 2002 9 9 UPS02839135 1 20020809 A 5320 FITTING DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 RT WING STR 51 I/B SIDE AT STA 74 IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRM 51-1-20D, TORQUED BOLT IAW DC8 SRM 51-1-23. 2 L 7 4 4F RT 4A25 2002090900128 20020909 00128 WP 2002 9 9 UPS02839136 1 20020806 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 RT MLG DOOR CUTOUT AREA AFT WEB PNL OF UPLATCH CUTOUT IS CRACKED. FABBED NEW WEB IAW DAC DWG 5651021 & NEW ATTACH ANGLE IAW DAC DWG 56 51221. INSTALLED ASSY IAW DC8 SRM 51-1-21 & 51-3-0 AND 51-120D. 2 L 7 4 4F RT 4A25 2002090900129 20020909 00129 WP 2002 9 9 UPS02839138 1 20020730 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB LONGERON 11 CRACKED APPROX 2 INCHES, FOUND BY X-RAY INSPECTION. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2002090900130 20020909 00130 WP 2002 9 9 UPS02839142 1 20020729 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FUSELAGE DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 FLOOR PANEL STA 759-879 PANEL A DELAMINATED. FABBED NEW PANEL IAW UPS EO DC8 5320-9691C. 2 L 7 4 4F RT 4A25 2002090900131 20020909 00131 WP 2002 9 9 UPS02839144 1 20020815 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 INT CABIN CRACKED FRAME TO FORMER FITTING STA 12 RT STA 220. REMOVED AND REPLACED CRACKED FITTING. 2 L 7 4 4F RT 4A25 2002090900132 20020909 00132 WP 2002 9 9 UPS02839147 1 20020727 A 5220 SKIN DOUG DC8 DC871F 302199D WP EMERGENCY EXIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 LT SIDE FWD OVERWING EMERGENCY EXIT DOOR HAS CRACK INDICATION AT LOWER AFT CORNER, FOUND BY NDT INSPE CTION. REPAIRED AREA IAW REO G08714. 2 L 7 4 4F RT 4A25 2002090900133 20020909 00133 WP 2002 9 9 UPS02839148 1 20020727 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 CABIN INTERCOSTAL ATTACH FITTING HAS CRACK STA 902 L19L. REMOVED AND REPLACED FITTING IAW DC8 SRM 51 -1-24 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2002090900134 20020909 00134 WP 2002 9 9 UPS02839149 1 20020727 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 FWD PIT STA 278 ABOVE LONGERON 31R LOWER SURFACE OF FITTING CORRODED. REMOVED FITTING FOUND CORROSIO N OUT OF LIMITS IAW DC8 SRM 51-1-8 AND 51 -1-21 AND INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002090900135 20020909 00135 WP 2002 9 9 UPS02839151 1 20020726 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 FLOORBEAM STA 879 RBL 60 IS CRACKED AT O/B LIGHTENING HOLE. SPLICED IN NEW SECTION OF FLOORBEAM IAW REO G08713. 2 L 7 4 4F RT 4A25 2002090900136 20020909 00136 WP 2002 9 9 UPS02839152 1 20020726 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 FWD CARGO AFT DOOR FRAME FWD LWR INNER SURFACE AT LIGHTENING HOLE MULTIPLE CRACKS, DOUBLER IS UNTREAT ED METAL AND FASTENERS ARE IMPROPERLY INSTALLED. REPAIRED WEB IAW DAC DWG 5616520. 2 L 7 4 4F RT 4A25 2002090900137 20020909 00137 WP 2002 9 9 UPS02839154 1 20020725 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 RT APB CRACKED STA 1766 L11R OUTBOARD OF EXISTING DOUBLER. REPAIRED AREA IAW REO-G08719. 2 L 7 4 4F RT 4A25 2002090900138 20020909 00138 WP 2002 9 9 UPS02839155 1 20020809 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 L1 LWR FWD DOOR JAMB CORNER CRACKED AT FASTENER HOLE. INTERNAL DOUBLER CRACKED PER X-RAY INSP FOUND OX AND DOUBLE DRILLED HOLES, INSTALLED BUSHINGS IAW DAC DWG 47099818, FABBED REPAIR BUSHINGS IAW DAC DWG 4709987B, BLEND ED GOUGES WITHIN LIMITS IAW DC8 SRM 553-2-0. ALODINED, PRIMED & INSTALLED DOUBLERS IAW 53-2-0 FIG 15. 2 L 7 4 4F RT 4A25 2002090900139 20020909 00139 EU 2002 9 9 000188 1 20020815 A 7720 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU COCKPIT ACTIVATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 140 RIGHT ENGINE O/T WARNING. GROUND RAN AT T/O POWER AND ALL OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002090900140 20020909 00140 SO 2002 9 9 000189 1 20020821 A 3230 CONTROL UNIT EMB 145 EMB145 3260210 SO LANDING GEAR MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 267 AC RTF FOR LG AIR/GND FAIL ON EICAS. REMOVED AND REPLACED LGEU. 2 L 7 2 4F RT T00011AT 2002090900141 20020909 00141 2002 9 9 000192 4 20020901 A 3452 TRANSPONDER EMB 145 EMB145 3260210 SO COCKPIT INOPERATIVE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 381 CREW REPORTS BOTH TRANSPONDERS INOP ON WAY TO YYZ. ALSO HAS FLAP LOW SPEED MSG. 2 L 7 2 4F RT T00011AT 2002090900142 20020909 00142 SO 2002 9 9 000193 1 20020902 A 7830 THRUST REVERSER EMB 145 EMB145 3260210 SO NR 2 ENGINE MALFUNCTIONED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 291 ON TAKEOFF CREW GOT E AT TR DISAGREE MSG ON EICAS. MEL'D NR 2 ENGINE TR. 2 L 7 2 4F RT T00011AT 2002090900143 20020909 00143 SO 2002 9 9 000194 1 20020905 A 2612 FIRE WARNING EMB 145 EMB145 3260210 SO COCKPIT ACTIVATED A CHQA K NONE J WARNING INDICATION UK UNKNOWN 1 GL 11 295 APU FIRE WARNING WENT OFF WHEN STARTED APU. INSPECTED AND OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2002090900144 20020909 00144 EU 2002 9 9 000195 1 20020908 A 3260 LIGHT SAAB SF340 SF340A 7850100 EU COCKPIT MALFUNCTIONED A CHQA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 108 LOWERED LANDING GEAR AND DID NOT GET ANY OF 3 GREEN DOWN LOCK LIGHTS. CONT MTX T/S. 2 L 7 2 4T RT A52EU 2002090900146 20020909 00146 NM 2002 9 9 HNAA0200057 1 20020815 A 5311 85321002 FRAME DHAV DHC8 DHC8102 2809003 NM PWC HAMSTD CORRODED A HNAA O OTHER O OTHER IN INSP/MAINT 1 EA 07 940HA 156 During 40k insp. frame leg was found with corrosion at station X370 between stringers 31s and 32s. A new frame section was spliced in as per EO8-53-02-943. 2 H 7 2 4T RT A13NM 2002090900147 20020909 00147 NM 2002 9 9 HNAA0200058 1 20020815 A 5311 85320086 FRAME DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA O OTHER O OTHER IN INSP/MAINT 1 EA 07 940HA 156 During 40k insp. corrosion was found on frame leg at station X312 between stringer 31s and 30s. A new frame section was spliced in as per. EO8-53-02-0943. 2 H 7 2 4T RT A13NM 2002090900148 20020909 00148 NM 2002 9 9 HNAA0200059 1 20020815 A 5311 85320103107 FRAME DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA O OTHER O OTHER IN INSP/MAINT 1 EA 07 940HA 156 During 40k insp. corrosion was found on frame leg at station X242 between stringers 31s and 30s. A new section of frame leg was spliced in as per EO8-53-02-0943 2 H 7 2 4T RT A13NM 2002090900149 20020909 00149 NM 2002 9 9 HNAA0200060 1 20020815 A 5311 85320086 FRAME DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA O OTHER O OTHER IN INSP/MAINT 1 EA 07 940HA 156 During 40k insp. corrosion was found on frame leg at station X312 between stringers 31s and 32s. A new section of frame was spliced in as per EO8-53-02-0943. 2 H 7 2 4T RT A13NM 2002090900150 20020909 00150 NM 2002 9 9 02090901 1 20020905 A 3241 AS11506K0540 HYDRAULIC LINE BOEING 757 7572T7 1384914 NM RROYCE RB211 RB211535E4 54555 NE BURST A N8TA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 WP 19 513NA 53430 23895 Just prior to takeoff, the "R Hyd Press" EICAS Msg. came on and right hyd qty had dropped to "0.45RF". Aircraft returned to the gate. further investigation revealed the right aft outboard (#8) Brake flex line had ruptured. Line was removed and replaced as per M/M 20-10-10, and Ops checked as per M/M 32-41-00. Aircraft was released for return to service. 2 L 7 2 4F 4 F RT A2NM E12EU 2002090900152 20020909 00152 NM 2002 9 9 UPS02239382 1 20020828 A 5310 ANGLE BOEING 727 72722C 138400F NM BS 870 S18A WEB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C LEFT MLG WHEEL WELL, ATTACH ANGLE LOCATED BETWEEN FITTING BS 870 & S TR. 18A WEB IS CRACKED REPLAC ED ANGLE IAW SRM 51-30-2 2 L 7 3 4F A3WE 2002090900153 20020909 00153 NM 2002 9 9 UPS02239383 1 20020829 A 5310 WEB BOEING 727 72722C 138400F NM BS 285 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C NOSE WHEEL WELL L/H SIDEWALL WEB HAS SUSPECT CRACK AROUND RIVETS @ B S 285, 3" ABOVE SILL WEB REPA IRED IAW SRM 51-40-2 FIG 1 2 L 7 3 4F A3WE 2002102100126 20021021 00126 NM 2002 10 21 UPS02439389 1 20020907 A 5753 PANEL BOEING 747 747212B 1384886 NM T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE:N/A LT WING OTBD MID T/E FLAP 4 FT CRACK ON TRAILING EDGE. INSTALLED COVE PANEL REF SRM 51-30-02. 2 L 7 4 4F A20WE 2002090900156 20020909 00156 EU 2002 9 9 MALA020539 1 20020902 A 5320 ANGLE SAAB SF340 340B 7860101 EU A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 416XJ 340B416 DURING 4K-INSPECTION IN CWA, CARGO FLOOR ANGLE BETWEEN AFT CENTER AISLE SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED A ND REPLACED NEW ANGLE IAW SRM CHAP 51. RELEASE DATE 9/4/02. REF 409 # 138436 FOR DETAIL. 2 L 7 2 4T RT A52EU 2002090900157 20020909 00157 EU 2002 9 9 MALA020547 1 20020901 A 5320 SEAT TRACK SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 416XJ 340B416 DURING 4K-INSPECTION IN CWA, RH CENTER AISLE SEAT TRACK FWD PORTION AND CLIP HAS CORROSION AT APPROXIMATELY STA 294. MA INTENANCE REMOVED CORROSION IAW SRM 51-70-40. RELEASE DATE 9/4/02. REF 409 # 141859 FOR DETAIL. 2 L 7 2 4T RT A52EU 2002091000001 20020910 00001 EU 2002 9 10 IO5R080905 1 20020903 A 6710 L673M40A1001 ACTUATOR UROCOP EC135 EC135P1 8680990 EU FENESTRON DEFECTIVE H IO5R K NONE K FLUID LOSS IN INSP/MAINT 1 FS 01 552BA 247 190 SERVO LEAKING EXCESSIVE OUT PITCH CONTROL SHAFT REMOVED AND REPLACED 1 G 7 2 3U O H88EU 2002091000002 20020910 00002 NE 2002 9 10 AUS20020958 2 20020821 A 7210 PCE17463 CHIP DETECTOR CESSNA 208 208 2073702 CE PWA PT6 PT6A114 52043 NE MCAULY 3AF34C 3GFR34C703 GL ENGINE GEARBOX CONTAMINATED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 AU S (AUS) PROPELLER REDUCTION GEARBOX CHIP DETECTOR CONTAINED A SMALL AMOUNT OF METAL PARTICLES. 1 H 7 1 3T 3 T NT A37CE E4EA 5 C P60GL 2002091000004 20020910 00004 NM 2002 9 10 AUS20020964 1 20020808 A 5310 FRAME BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT OUTBOARD FRAME CRACKED. FRAME IS LOCATED AT BS727 STRINGER NO18. 2 L 7 2 4F 4 F RT A16WE E21EU 2002091000005 20020910 00005 EU 2002 9 10 AUS20020966 1 20020823 A 2910 MS21902W6 FITTING BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE MLG HYD SYS SHEARED W O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 AU S (AUS) BRAKE SYSTEM MANIFOLD FITTING SHEARED. LOSS OF YELLOW' HYDRAULIC SYSTEM FLUID. 2 H 7 4 4F 4 F RT A49EU E6NE 2002091000006 20020910 00006 NE 2002 9 10 CA020826008 1 20020821 A 5711 21610063 DOUBLER CONAER LA4 LA4200 5110310 NE LYC O360 IO360A1B 41514 EA LT WING SPAR CAP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LT WING LOWER SPAR CAP DOUBLER CRACKED AT OUTER BOLT HOLE. 1 H 7 1 3O 3 O 1A13 1E10 2002091000007 20020910 00007 SW 2002 9 10 CA020827006 1 20020628 A 6310 3032641 BEARING BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA COMB GEARBOX SPALLED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) THE PILOT WAS FLYING WHEN THE MASTER CAUTION LIGHT ACTIVED. THE ENGINE CHIP LIGHT ON THE NR 1 SIDE ALSO ACTIVED. THE PILOT LANDED AS SOON AS PRACTICAL. THE REDUCTION GEARBOX AND BOTH POWER SECTIONS WERE REMOVED. THE SOURCE OF METAL WAS LOCATED. IT WAS THE NR 5 BEARING, SPALLING ON THE NR 1 ENGINE SIDE OF THE REDUCTION GEARBOX. THE TSO AND TSN FRO M BOXES (F) AND (G) ARE THE REDUCTION GEARBOX HOURS. THE BEARING TSN UNKNOWN. THE BEARING INSTALLATION WAS POST MOD. S B 5035. 1 G 7 1 4U 4 U H4SW E22EA 2002091000008 20020910 00008 NE 2002 9 10 CA020827007 2 20020722 A 7250 9609000408 BEARING SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE TURBINE SECTION SPALLED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING FLIGHT AN ENGINE CHIP LIGHT OCCURRED. PILOT LANDED AS SOON AS PRACTICAL. ENGINEER FOUND THAT ALL THE ENGIN E CHIP PLUGS HAD METAL. ENGINE CHIP PLUGS WERE CLEANED AND THE ENGINE WAS RUNUP AGAIN. ENGINE WAS RUN AND SHUT DOWN TO INSPECT THE CHIP PLUGS, MORE METAL WAS FOUND AND THE ENGINE WAS REMOVED AND SENT TO A REPAIR FACILITY. FOUND THE ENGIN E CHIPS WAS FROM THE REAR BEARING OF THE MO3. THE REAR BEARING HAD ONLY 739.6 HOURS SINCE NEW. 1 G 7 1 3U 3 U H9EU E19EU 2002091000009 20020910 00009 GL 2002 9 10 CA020827009 3 20020820 A 6114 HUB CONAER LA4 LA4200 5110310 NE LYC O360 IO360A1B 41514 EA HARTZL HCC2Y HCC2YK1 GL PROPELLER CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CORROSION ON HUB IN O-RING SEAL AREA. BALL WEAR ON BLADE BEARING. CHROME WORN THRU TO BASE METAL ON PITCH CH ANGE ROD. 1 H 7 1 3O 3 O 1A13 1E10 5 C P920 2002091000010 20020910 00010 NM 2002 9 10 CA020828003 1 20020821 A 3397 RAX5301A CONTROL UNIT BOEING 767 767333 1385301 NM GE CF6 CF680C2B6F 30025 NE CABIN FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 321965 (CAN) CABIN CREW REPORTED 'PASSENGER READING LIGHT NOT WORKING IN Y CLASS.' THE 1ST OBSERVATION BY MAINT NOTED THAT IN CENTER SECTION OF AFT CABIN, ROWS 19DEF TO 36DEF, CALL LIGHT ILLUMINATED AT SEAT 36DEF, 26DEF & APPROXAMITELY ROW 20 OR 21DEF. CALL LIGHT AT SEAT 26DEF UNUSUAL ORANGE COLOR. PSU SEAT ROW 26DEF INDICATED EVIDENCE OF EXTREME FAILURE AS INDICATED BY SMOKE REMAINS ON & AROUND PAX SERVICE UNIT DECODER (PSUD). A/C WIRING CONNECTOR PINS 2 & 3 TO PSUD J2 CON NECTOR WERE BURNED. NO EVIDENCE OF PIN OR SOCKET CONTACTS REMAINED REPLACED PSUD AT ROW 26DEF & CONNECTOR. ALSO CHANGE D AREA SERVICE BOX & THE PSUD AT 27DEF. 2 L 7 2 4F 4 F RT A1NM E13NE 2002091000011 20020910 00011 EU 2002 9 10 CA020828005 1 20020809 A 6510 350A2310534551 BEARING AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20F 03013 GL T/R DRIVE SHAFT ELONGATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) NOISE WAS HEARD FROM OIL COOLER FAN AREA ON SHUTDOWN. INSPECTION REVEALED NR 6 T/R DRIVESHAFT SUPPORT BEARING BOL T HOLES HAD ELONGATED AND ALLOWED THE T/R DRIVESHAFT AND FAN SHAFT TO MOVE OUT OF ALIGNMENT. NR 6 BEARING SUPPORT, BEAR ING AND BEARING TRANSMISSION WERE REPLACED. OIL COOLER FAN WAS REMOVED, INSPECTED AND REINSTALLED. FAN SHAFT BALANCE CHE CK WAS CARRIED OUT AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H11EU E4CE 2002091000012 20020910 00012 WP 2002 9 10 CA020828007 1 20020618 A 6520 369D25146 BEARING HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL TAIL ROTOR CRACKED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) M/R CHIP LIGHT WAS REPORTED. CHIP PLUGS INSPECTED AND FOUND TO HAVE LARGE AMOUNT OF DEBRIS. SOURCE FOUND TO BE THE T/R O/P PINION ROLLER BEARING. THE INNER RACE WAS FOUND TO BE CRACKED AND HEAVY SPALLING WAS ALSO OCCURRING. THIS INNER RACE IS PRESSED ONTO THE PINION WITH AN INTERFERENCE FIT. 1 G 7 1 3U 3 U H3WE E4CE 2002091000013 20020910 00013 WP 2002 9 10 CA020828008 1 20020420 A 6520 369D25146 BEARING HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A SEAL CHANGE A CRACK WAS DETECTED ON THE INNER RACE OF THE T/R O/P PINION ROLLER BEARING. THIS INNER RACE IS PRESSED ONTO THE PINION WITH AN INTERFERENCE FIT. 1 G 7 1 3U 3 U H3WE E4CE 2002091000014 20020910 00014 WP 2002 9 10 CA020828009 1 20020701 A 6520 369D25146 BEARING HUGHES 369 369E 4470707 WP ALLSN 250C 250C20B 03013 GL TAIL ROTOR CRACKED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) M/R TRANSMISSION CHIP LIGHT WAS REPORTED. CHIP PLUGS INSPECTED AND FOUND TO HAVE LARGE AMOUNT OF DEBRIS. SOURCE FO UND TO BE THE T/R O/P PINION ROLLER BEARING. THE INNER RACE WAS FOUND TO BE CRACKED AND HEAVY SPALLING WAS ALSO OCCURRIN G. THIS INNER RACE IS PRESSED ONTO THE PINION WITH AN INTERFERENCE FIT. 1 G 7 1 3U 3 U H3WE E4CE 2002091000015 20020910 00015 EA 2002 9 10 CA020829001 2 20020806 A 7321 252444076 FUEL CONTROL DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA NR 2 ENGINE OUT OF ADJUST W O OTHER R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 CA (CAN) - FUEL CONTROL UNIT INSTALLED IN NR 2 POSITION. - MAINTENANCE RUN, ENGINE WOULD NOT COME OFF 'MIN FLOW' OR DEVELOP POWER. UNIT HAD BEEN OVERHAULED WITHIN 30 DAYS, RETURNED TO OVERHAUL SHOP FOR TESTING AND REPORT. 1 H 7 2 3T 4 T RT A9EA E4EA 2002091000016 20020910 00016 EA 2002 9 10 CA020829003 2 20020806 A 7321 25244405 FUEL CONTROL DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA RT ENGINE FAILED W D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 CA (CAN) - DURING STARTUP, RT ENGINE WOULD ONLY PRODUCE 8 LBS OF TORQUE.- FUEL CONTROL UNIT FOUND FAULTY. UNIT REPLACED W ITH OVERHAUL, THIS UNIT ALSO 'FAILS', RETIRMED TO OVERHAUL SHOP. SECOND OVERHAUL UNIT INSTALLED, AIRCRAFT RETURNED TO S ERVICE. ORIGINAL FCU SENT TO OVERHAUL SHOP FOR TESTING AND STRIP REPORT. 1 H 7 2 3T 4 T RT A9EA E4EA 2002091000017 20020910 00017 SO 2002 9 10 CA020829004 1 20020814 A 7714 4708869002R CONTROLLER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA LT ENGINE INTERMITTENT W O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CA (CAN) - DURING TAKEOFF ROLL PILOT NOTICED THE LT RPM STUCK AT 2000 RPM 'MOMENTARILY'. ALL OTHER ENGINE PARAMETERS NORMAL . CREW PROCEEDED TO BASE WITH NO PROBLEMS. TROUBLESHOOTING FOUND DIFFERENTIAL CONTROLLER AT FAULT. UNIT REPLACED WIT H OVERHAUL AND AIRCRAFT RETURNED TO SERVICE. FAULTY UNIT RETURNED TO OVERHAUL SHOP AND STRIP REPORT REPAIR. 1 L 7 2 3O 3 O A20SO E14EA 2002091000019 20020910 00019 SW 2002 9 10 CA020829007 1 20020813 A 5600 36004313SS WINDSHIELD GULSTM 690TP 690A 0141722 SW GARRTT TPE331 TPE33110T WP COCKPIT CRACKED W O OTHER O OTHER CL CLIMB 1 CA (CAN) PILOTS WINDSHIELD CRACKED AFTER TAKEOFF, CLIMBING THROUGH 2,000 FEET. AIRCRAFT FLOWN TO HOME BASE UNPRESSURIZED. 1 H 7 2 3T 4 T 2A4 E4WE 2002091000021 20020910 00021 GL 2002 9 10 CA020829009 2 20020819 A 7240 6870992 CASE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL COMBUST CHAMBER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ENGINE ASSEMBLY HAD HIGH TOT. UPON INSPECTION ENGINEER DISCOVERED CRACK IN ARMPIT AREA. 1 G 7 1 3U 3 U H3WE E4CE 2002091000023 20020910 00023 EA 2002 9 10 CA020829011 2 20020722 A 7414 10357424 DISTRIBUTOR BLK CONT 101530456 ROBSIN R22 R22BETA 7640110 NM LYC O360 O360J2A 41514 EA MAGNETO CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA I138902F (CAN) CRACK FOUND IN THE MAGNETO DISTRIBUTOR BLOCK UPON INSPECTION NEXT TO BUSHING. 1 G 7 1 3O 3 O H10WE E286 2002091000024 20020910 00024 GL 2002 9 10 CA020829013 2 20020717 A 7323 SPLINE ADAPTER BENDIX 23065121 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL DRIVE SHAFT WORN W K NONE O OTHER IN INSP/MAINT 1 CA 9268 (CAN) DRIVE SPLINE RETAINING CLIP AND WASHER FOUND DEPARTED FROM SHAFT. EPOXY PLUG DEPARTED. 1 G 7 1 3U 3 U H2SW E4CE 2002091000027 20020910 00027 NM 2002 9 10 CA020830005 1 20020830 A 3310 LIGHT BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT MISWIRED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) FIRST OFFICERS UTILITY LIGHT FOUND MISWIRED AT TERMINAL BLOCK. PROBLEM WAS FOUND WHILE CARRYING OUT ROUTINE MAINT ENANCE AND BULB SOCKET CAME IN CONTACT WITH GROUND PRODUCING LOTS OF SPARKS. FLEET CAMPAIGN ISSUED AND TERMINAL BLOCK W IRED CORRECTLY. 2 L 7 2 4F 4 F RT A1NM E3NE 2002091000028 20020910 00028 NM 2002 9 10 CA020830007 1 20020830 A 3310 LIGHT BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT MISWIRED W K NONE W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) SECOND OBSERVERS UTILITY LIGHT FOUND MISWIRED AT TERMINAL BLOCK. THIS WAS A FINDING RESULTING FROM A FLEET CAMPAI GN TO CHECK FOR SIMILAR PROBLEMS ON OTHER AIRCRAFT. LIGHT SOCKET PRODUCED SPARKS IF INADVERTENTLY TOUCHED BY A GROUNDIN G OBJECT. TERMINAL BLOCK WIRING CORRECTED 2 L 7 2 4F 4 F RT A1NM E3NE 2002091000029 20020910 00029 NM 2002 9 10 CA020830009 1 20020830 A 3310 LIGHT BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT MISWIRED W K NONE B W SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) FIRST OFFICERS UTILITY LIGHT MISWIRED AT TERMINAL BLOCK. THIS FINDING WAS RESULT OF A FLEET CAMPAIGN TO CHECK FOR SIMILAR PROBLEMS FOUND ON OTHER AIRCRAFT. LIGHT SOCKET PRODUCES SPARKS IF INADVERTENTLY TOUCHED BY A GROUNDING OBJECT. TERMINAL BLOCK CORRECTLY WIRED. 2 L 7 2 4F 4 F RT A1NM E3NE 2002091000031 20020910 00031 NM 2002 9 10 CA020830011 1 20020830 A 3310 LIGHT BOEING 767 767375 1385217 NM GE CF6 CF680C2B6F 30025 NE COCKPIT MISWIRED W K NONE B W SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) SECOND OBSERVERS UTILITY LIGHT FOUND MISWIRED AT TERMINAL BLOCK. THIS FINDING WAS RESULT OF A CAMPAIGN TO CHECK FOR SIMILAR PROBLEM ON 767 FLEET. LIGHT SOCKET PRODUCES SPARKS IF INADVERTENTLY TOUCHED BY A GROUNDING OBJECT. TERMINA L BLOCK REWIRED CORRECTLY. 2 L 7 2 4F 4 F RT A1NM E13NE 2002091000034 20020910 00034 NM 2002 9 10 CA020830015 1 20020830 A 3310 LIGHT BOEING 767 7673Y0 NM PWA 4060 PW4060 52119 NE COCKPIT MISWIRED W K NONE B W SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) CAPTAINS UTILITY LIGHT FOUND MISWIRED AT TERMINAL BLOCK.THIS FINDING WAS RESULT OF A CAMPAIGN TO CHECK FOR SIMILAR PROBLEMS ON 767 FLEET. TERMINAL BLOCK REWIRED CORRECTLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2002102100032 20021021 00032 NM 2002 10 21 372PA0013 1 20020909 A 2760 CONTROL CABLE BOEING 737 737306 13844BG NM SPOILER BROKEN A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 ON WALK AROUND INSPECTION, FOUND NR 2 FLT SPOILER CABLE WSA1-3 BROKEN. R&R CABLE AND OPERATIONAL CHECKED PER MM 27-61-0 0. 2 L 7 2 4F RT A16NE 2002091000035 20020910 00035 NM 2002 9 10 0202846730 1 20020829 A 5311 SHEAR TIE BOEING 747 7472J9F 1384806 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 During "H" check found crack in shear tie t-chord at BS 400 RBL 80. Repaired per EA 67-192355. 2 L 7 4 4F RT A20WE 2002091000036 20020910 00036 2002 9 10 SWAA021999 4 20020901 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091000037 20020910 00037 2002 9 10 SWAA022000 4 20020902 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091000038 20020910 00038 NM 2002 9 10 SWAA022007 1 20020831 A 3350 1010427 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 OVERHEAD BIN EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW NR 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002091000039 20020910 00039 2002 9 10 SWAA022008 4 20020831 A 2565 6557463 FITTING BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING LOOSE. SECURED FITTING PER MM. 2 L 7 2 4F RT A16WE 2002091000040 20020910 00040 NM 2002 9 10 SWAA022010 1 20020831 A 3350 6104789 BATTERY BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED WHEN SW IS IN OFF POS. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2002091000041 20020910 00041 2002 9 10 SWAA022017 4 20020829 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM FWD ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002091000042 20020910 00042 NM 2002 9 10 SWAA022019 1 20020829 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED C1 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED AT Y-CHORD AREA, STR 6L. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F A16WE 2002091000043 20020910 00043 NM 2002 9 10 SWAA022020 1 20020902 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002091000044 20020910 00044 NM 2002 9 10 SWAA022021 1 20020902 A 5330 6545800 DOUBLER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED SPECIAL VISIT, FOUND SEVERAL CRACKS AT FWD AIRSTAIR LOWER CUTOUT BEAR STRAP. REPAIRED DOUBLER PER SWA EA. 2 L 7 2 4F A16WE 2002091000045 20020910 00045 NM 2002 9 10 SWAA022023 1 20020830 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 915, STR 24R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F A16WE 2002091000046 20020910 00046 NM 2002 9 10 SWAA022024 1 20020830 A 5330 6545768 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 372, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002091000047 20020910 00047 NM 2002 9 10 SWAA022025 1 20020902 A 5753 6571909 FLAP BOEING 737 7372H4 138448C NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED C1 CHECK, FOUND LT OTBD T/E MID FLAP CRACKED ON THE AFT SPAR UPPER CHORD. REMOVED AND REPLACED LT OTBD T/E MID FLAP PER MM. 2 L 7 2 4F A16WE 2002091000048 20020910 00048 NM 2002 9 10 SWAA022026 1 20020831 A 5753 6473731 SKIN BOEING 737 7373Q8 1384670 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED 1/4D CHECK, FOUND RT T/E INBD FORE FLAP DELAMINATED ON UPPER SKIN. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091000049 20020910 00049 NM 2002 9 10 SWAA022027 1 20020903 A 5753 6546430 FLAP BOEING 737 7373H4 1384600 NM LT WING PEELING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING WALK AROUND INSPECTION, FOUND PREVIOUS REPAIR PEELING OFF AT LT T/E INBD FORE FLAP. REMOVED AND REPLACED LT T/E INBD FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2002091000050 20020910 00050 NM 2002 9 10 SWAA022028 1 20020901 A 5330 6545800 DOUBLER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED 1/4D CHECK, FOUND AIRSTAIR DOOR CUTOUT CRACKED AT BS 344, STR 21L. REPAIRED DOUBLER PER SWA EA. 2 L 7 2 4F RT A16WE 2002091000051 20020910 00051 NM 2002 9 10 SWAA022029 1 20020901 A 5755 65C25251 SPOILER BOEING 737 7373Q8 1384670 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED 1/4D CHECK, FOUND LT T/E SPOILERS, NR 0, NR 1, NR 2 AND NR 3 DELAMINATED. REMOVED AND REPLACED LT T/ E SPOILERS, NR 0, NR 1, NR 2 AND NR 3 PER MM. SERIAL NUMBERS, 2825Y AT NR 0, 2857Y AT NR 1, 2779Y AT NR 2 AND 2885Y AT NR 3. 2 L 7 2 4F RT A16WE 2002091000052 20020910 00052 NM 2002 9 10 SWAA022030 1 20020829 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091000053 20020910 00053 NM 2002 9 10 SWAA022032 1 20020830 A 5320 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND CORROSION ON CREASE BEAM WEB (2 EA) BETWEEN BS 887 TO BS 907, WL 208 AND RBL 64 AND BS 8 67, WL 208 AND LBL 65. REPAIRED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2002091000054 20020910 00054 NM 2002 9 10 SWAA022033 1 20020830 A 5510 65C25727 STABILIZER BOEING 737 7373H4 1384600 NM RT STABILIZER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED ALONG REAR SPAR, NEAR MID POINT. REPAIRED STABILIZER PER SRM. 2 L 7 2 4F RT A16WE 2002091000055 20020910 00055 NM 2002 9 10 SWAA022034 1 20020902 A 2781 6552807 MODULE BOEING 737 7373H4 1384600 NM E/E COMP FAULTY A SWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 29 654SW 28399 ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED AND L/E FLAP TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED FLAP/SLAT MO DULE PER MM. 2 L 7 2 4F RT A16WE 2002091000056 20020910 00056 NM 2002 9 10 SWAA022050 1 20020904 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091000057 20020910 00057 NM 2002 9 10 SWAA022051 1 20020905 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091000058 20020910 00058 NM 2002 9 10 SWAA022053 1 20020905 A 5312 6546568 BULKHEAD BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND PRESSURE BULKHEAD CRACKED (2 EA) AT BS 1016, STR 6R AND STR 6L. REPAIRED BULKHEAD PER S RM. 2 L 7 2 4F RT A16WE 2002091000059 20020910 00059 NM 2002 9 10 SWAA022054 1 20020904 A 5330 6545800 DOUBLER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED A2 CHECK, FOUND CRACKS AT THE LOWER CORNER OF THE AIRSTAIR CUTOUT. REPAIRED DOUBLER PER SWA EA AND SRM . 2 L 7 2 4F A16WE 2002091000060 20020910 00060 NM 2002 9 10 SWAA022056 1 20020905 A 5320 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIES CRACKED (2 EA) AT BS 360, STR 14L AND STR 14R. REMOVED AND REPLACED SH EAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2002091000061 20020910 00061 NM 2002 9 10 SWAA022058 1 20020904 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) ABOVE STR 10L, BS 500D + 16, BS 500A + 12, BS 500C + 5 AND BS 500A + 2. REPAIRED SKIN PER SWA EA AND SRM. 2 L 7 2 4F RT A16WE 2002091000062 20020910 00062 NM 2002 9 10 SWAA022059 1 20020904 A 5330 589357 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND SKIN CRACKED ON BOTH CAPTAIN'S AND FIRST OFFICER'S WINDOW POSTS. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2002091000063 20020910 00063 NM 2002 9 10 SWAA022060 1 20020904 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 12L, BS 500D + 2 AND BS 500D + 18. REPAIRED S KIN PER SRM. 2 L 7 2 4F RT A16WE 2002091000064 20020910 00064 NM 2002 9 10 SWAA022061 1 20020904 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 487, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091000065 20020910 00065 2002 9 10 SWAA022036 4 20020903 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091000066 20020910 00066 NM 2002 9 10 SWAA022037 1 20020904 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 EEPLS COVER LOOSE IN FWD CABIN. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002091000067 20020910 00067 NM 2002 9 10 SWAA022038 1 20020904 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091000068 20020910 00068 NM 2002 9 10 SWAA022039 1 20020904 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091000069 20020910 00069 NM 2002 9 10 SWAA022040 1 20020904 A 5330 6545768 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER AFT CUTOUT, BS 350 AND ABOVE STR 17L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2002091000070 20020910 00070 NM 2002 9 10 SWAA022041 1 20020904 A 5330 589358 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED 1/4D CHECK, FOUND R-1 COCKPIT WINDOW FRAME SKIN CRACKED AT UPPER OTBD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091000071 20020910 00071 NM 2002 9 10 SWAA022042 1 20020904 A 5330 6545767 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 430, BL 0. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002091000072 20020910 00072 NM 2002 9 10 SWAA022043 1 20020831 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED A1 CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TA B HINGE BUSHINGS AT NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM. 2 L 7 2 4F RT A16WE 2002091000073 20020910 00073 NM 2002 9 10 SWAA022044 1 20020831 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED A1 CHECK, SWA SI 11038-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TA B HINGE BUSHING AT NR 4 ELEVATOR TAB HINGE ATTACH POINT PER MM. 2 L 7 2 4F RT A16WE 2002091000074 20020910 00074 NM 2002 9 10 SWAA022045 1 20020901 A 5330 6545800 DOUBLER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 DURING SCHEDULED SPECIAL VISIT, FOUND SEVERAL SKIN CRACKS AT FWD AIRSTAIR LOWER CUTOUT BEAR STRAP. REPAIRED DOUBLER PER SWA EA. 2 L 7 2 4F A16WE 2002091000075 20020910 00075 NM 2002 9 10 SWAA022046 1 20020901 A 5330 6545767 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 DURING SCHEDULED SPECIAL VISIT, FOUND SKIN CRACKED AT FWD CARGO DOOR OPENING LOWER STOP FITTING. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002091000076 20020910 00076 NM 2002 9 10 SWAA022047 1 20020901 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002091000077 20020910 00077 NM 2002 9 10 SWAA022048 1 20020902 A 2751 NAS561P3 BUSHING BOEING 737 7375H4 138449D NM COCKPIT WORN A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 29 510SW 24187 T/E FLAP HANDLE WOULD NOT MOVE PAST 5 DEGREES. REMOVED AND REPLACED T/E FLAP HANDLE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2002091000078 20020910 00078 NM 2002 9 10 VNAA0209008 1 20020907 A 3200 BRAKE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 328JS 3030 DURING TAKE OFF, THE CREW RECEIVED A HIGH BRAKE TEMPERATURE INDICATION AND ABORTED TAKE OFF. THE CREW TAXIED OFF THE RU NWAY AND WAITED FOR THE BRAKE TEMPERATUES TO COOL. THE DECISION WAS THEN MADE TO ATTEMPT ANOTHER TAKE OFF. FLIGHT 4048 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091000079 20020910 00079 2002 9 10 SWAA022063 4 20020908 A 2565 D31591 SLIDE BOEING 737 7375H4 138449D NM FWD ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED WHEN OPENING DOOR. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091000080 20020910 00080 NM 2002 9 10 SWAA022065 1 20020907 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2002091000081 20020910 00081 2002 9 10 SWAA022066 4 20020906 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 767SW 29807 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091000082 20020910 00082 NM 2002 9 10 SWAA022068 1 20020905 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED AT ROW NR 3, 4, 5, 11 AND 23. REMOVED AND REPLACED EEPLS COVERS P ER MM. 2 L 7 2 4F RT A16WE 2002091000083 20020910 00083 2002 9 10 SWAA022069 4 20020905 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 778SW 27883 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091000084 20020910 00084 2002 9 10 SWAA022071 4 20020907 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM AFT SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW AND SLIDE GIRT CABLE MISROUTED. REPOSITIONED SLIDE AND REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002091000085 20020910 00085 2002 9 10 SWAA022072 4 20020907 A 2565 65C19901 CABLE BOEING 737 7373Q8 1384670 NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002091000086 20020910 00086 2002 9 10 SWAA022073 4 20020907 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091000087 20020910 00087 NM 2002 9 10 SWAA022074 1 20020908 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C PLUS 5, STR 15R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091000088 20020910 00088 NM 2002 9 10 SWAA022075 1 20020908 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727 PLUS 14, ABOVE STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091000089 20020910 00089 NM 2002 9 10 SWAA022076 1 20020905 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 20 DEF. SECURED LENS PE R MM. 2 L 7 2 4F RT A16WE 2002091000090 20020910 00090 NM 2002 9 10 SWAA022078 1 20020907 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 14L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091000091 20020910 00091 NM 2002 9 10 SWAA022079 1 20020905 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FWD CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 24 TO RBL 54. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2002091000092 20020910 00092 NM 2002 9 10 CALA0200453 1 20020907 A 5347 SEAT TRACK BOEING 757 757224 1384958 NM STA 1080-1180 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18112 27302 INSPECTION FOUND A 1" CRACK AND CORROSION IN SEAT TRACK AT STA 1080-1180, LBL 45.5. THE SEAT TRACK SECTION WAS REMOVED A ND REPLACED IAW BOEING DRAWING #144N5001. 2 L 7 2 4F RT A2NM 2002091000093 20020910 00093 NM 2002 9 10 CALA0200455 1 20020909 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, LBL 34. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT. A CHORD AND SPLICE A NGLE REPAIR WAS INSTALLED IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 2002091000094 20020910 00094 WP 2002 9 10 0202759759 1 20020825 A 2780 CONTROL CABLE DOUG DC9 DC941 302207N WP L/E SLAT OUT OF RIG A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 01 759NW 47287 ON TAKEOFF, THE CREW HAD A STALL INDICATOR ACCOMPANIED WITH A STICK SHAKER. ONCE IN THE AIR, A LOUD POP WAS HEARD AND T HE AIRCRAFT ROLLED TO THE RIGHT. AFTER ROLL CORRECTION, THE STALL INDICATION CLEARED BUT THE CREW ELECTED TO RETURN TO MSP. LANDING WAS UNEVENTFUL AND MAINTENANCE FOUND THE SLAT EXTEND CABLE LOOSE AND THE TURNBUCKLE BINDING AS IT MOVED TH ROUGH A LIGHTENING HOLE. REPLACED THE AOA TRANSDUCERS, BOTH STALL WARNING COMPUTERS, AND TONE GENERATORS. RIGGED SLATS . OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002091000095 20020910 00095 NM 2002 9 10 CA020830018 1 20020824 A 3230 273T453010 SEQUENCE VALVE BOEING 767 767275 1385155 NM PWA JT9 JT9D7R4D 52054 NE MLG DOOR FAILED W A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CA (CAN) FLIGHT RETURN TO TORONTO WITH GEAR WARNING WHEN GEAR LEVER SEL TO NEUTRAL AFTER RETRACTION, GEAR CYCLED & THEN RT GEAR LIGHTS REMAINED ON. ALT GEAR EXTENSION CARRIED OUT. REPLACED DOOR SEQUENCE VALVE AT POSITION NR 1. 2 L 7 2 4F 4 F RT A1NM E3NE 2002091000096 20020910 00096 EA 2002 9 10 CA020830019 1 20020817 A 3242 60485123101 KEY 501233MH CNDAIR CL604 CL604 1900301 EA CENTRE ROTOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) BRAKE UNIT WAS APPROACHING WEAR LIMIT IAW AMM, AND AS A RESULT ELECTED TO CHANGE THE ASSEMBLY. UPON REMOVAL OF TH E ASSOCIATED MAIN WHEEL, 5 OF THE CENTRE ROTOR DRIVE KEYS WERE FOUND SHEARED FROM THE ROTOR ITSELF. MINOR DAMAGE WAS NOT ED ON THE MAIN WHEEL HEAT SHIELD SUBASSEMBLIES. 2 L 7 2 4F RT A21EA 2002091000097 20020910 00097 CE 2002 9 10 CA020830020 1 20020816 A 5711 122005112 SPAR CESSNA 206 U206E 2073350 CE RT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) - INSPECTION REVEALED CRACK AT BOTTOM ANGLE OF AILERON HINGE. FURTHER INSPECTION REVEALED CRACKED REAR SPAR AT HI NGE ATTACH POINT AND CRACKED RIB STA 109. INSPECTION OF RIB AND REAR SPAR IS DIFFICULT BECAUSE OF LACK OF INSPECTION PA NELS. THE INSPECTION CAN BE ACCOMPLISHED WITH A LIGHT AND MIRRORS THROUGH OTHER INSPECTION PANELS. 1 H 7 1 3O A4CE 2002091000099 20020910 00099 EU 2002 9 10 CA020830021 1 20020730 A 3251 Z24242170001 SPRING ZLIN 242 Z242L 9970204 EU LYC O360 AEIO360A1B6 41514 EA NLG STEERING SYS BROKEN W O OTHER O OTHER TX TAXI/GRND HDL 1 CA (CAN) DURING TAXI, A STUDENT NOTICED PLAY IN THE NOSE WHEEL STEERING OF THE AIRCRAFT. MAINTENANCE WAS NOTIFIED AND THE LT STEERING SPRING WAS FOUND TO BE BROKEN. THE SPRING WAS REPLACED USING THE MINIMUM COIL DISTANCE SETTING ON THE LT A ND RT STEERING SPRINGS. 1 L 7 1 3O 3 O 0 A76EU 1E10 2002091000100 20020910 00100 SW 2002 9 10 CA020830023 1 20020820 A 2810 STRUCTURE BBAVIA 8 8GCBC 1220803 SW LYC O360 O360C2E 41514 EA FUEL TANK CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) FUEL FITTING BOSS FOUND CRACKED AROUND WELD APPROXIMATELY 1 INCH IN LENGTH. THE CRACK IS IN THE LOWER AFT RT THREA DED NIPPLE. 1 H 7 1 3O 3 O A21CE E286 2002091000101 20020910 00101 NM 2002 9 10 CA020830024 1 20020827 A 2910 82950010115 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) PILOTS REPORTED HYDRAULIC LEAK FROM LT NACELLE.LEAK TRACED TO NR 2 SYSTEM FLIGHT SPOILER UNLOADING HYDRAULIC LINE ON LT SIDE UNDER WING AREA. LINE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002091000102 20020910 00102 CE 2002 9 10 CA020903004 1 20020822 A 2434 530406 HUB FORD DOFF10300F CESSNA 150 150M 2071830 CE CONT O200 O200A 17020 SO ALTERNATOR WORN W O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 1101534 (CAN) IN FLIGHT ALTERNATOR FAILURE. DURING TROUBLESHOOTING, FOUND THE HUB COMPLETELY WORN OUT, THEREFORE THE GEAR COULD NO LONGER ROTATE THE ALTERNATOR. 1 H 7 1 3O 3 O 3A19 E252 2002091000104 20020910 00104 NE 2002 9 10 ARWA20020809 2 20020828 A 7261 OIL SYSTEM DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 3 ENGINE LACK OF LUBE A ARWA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 19 441J 45988 NR 3 ENGINE OIL QUANTITY INDICATING ZERO; WITH OIL PRESSURE FLUCTUATING AND LOW OIL PRESSURE, LIGHT ILLUMINATED. PERFOR MED IN-FLIGHT ENGINE SHUTDOWN AT 1920Z. NOTE WINDMILLING OIL PRESSURE 20 PSI TURNED ON START LEVER AT 2020Z AS PER AFM. SERVICED NR 3 ENGINE OIL TANK WITH 17 QUARTS OF 2380 OIL. IDLE RAN NR 3 ENGINE, NO LEAKS NOTED. SERVICED TWO MORE QU ARTS AFTER ENGINE SHUTDOWN. ACCOMPLISHED ENGINE RUN CHECK IAW MM 71-00 AND PERFORMED OPS CHECK OF OIL SYSTEM IAW MM 79- 00, NO LEAKS NOTED ENGINE OPERATION NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 2002091000106 20020910 00106 NM 2002 9 10 CA020903010 1 20020830 A 2910 82950010109 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) PILOT NOTICED HYDRAULIC FLUID LEAKING FROM LT REAR SPAR I/B OF ENGINE. LIFT DUMP PRESSURE LINE FOUND LEAKING. LIN E REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002091000107 20020910 00107 WP 2002 9 10 ARWA20020901 1 20020902 A 3230 56165545503 CYLINDER DOUG DC8 DC862 3021970 WP LT MLG LEAKING A ARWA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 SO 19 802BN 45909 AFTER LANDING IN SKCL LOSS OF HYDRAULICS PRESSURE AND QUANTITY. FOUND HYDRAULIC LEAK IN LEFT BOGIE TRIM CYLINDER. REMO VED AND REPLACED LEFT HYDRAULIC BOGIE TRIM CYLINDER AS PER ALTERNATE METHOD MM REF 32-33-1. SERVICED HYDRAULIC IAW MM 1 2-30-1 AND BLEED SYSTEMS IAW MM 29-00, NO LEAKS NOTED. 2 L 7 4 4F 4A25 2002091000108 20020910 00108 EA 2002 9 10 CA020903011 1 20020822 A 2150 GG670950011 PRECOOLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AIR CONDITIONING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE TROUBLESHOOTING THE RT BLEED OVERHEAT PROBLEM HORIZON FOUND THAT THE RT PRE-COOLER HAD TWO CRACKS ONE ON EAC H SIDE. THE CRACKS ARE IN THE WELDED AREAS OF THE INLET AND THE OUTLET. 2 L 7 2 4F 4 F RT A21EA E15NE 2002091000109 20020910 00109 NM 2002 9 10 AWXA200200512 1 20020608 A 2751 1817389 TRANSMITTER BOEING 737 7373Y0 1384671 NM T/E FLAP FAILED A AWXA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 28 323AW 20339 3276 23684 DECLARED EMERGENCY LANDING AFTER MISSED APPROACH DUE RT T/E FLAP LOCKING OUT. MX R&R FLAP POSITION INDICATOR & RT WING FLAP POSITION TRANSMITTER. C/W INTERFACE & FLAP POSITION INDICATING TEST. RT T/E FLAP POSITION TRANSMITTER WAS CONFIRM ED FAILURE BY VENDOR BENCH TEST FOR STALL WARNING SYNCHRO BEARING BINDING. FLAP POSITION INDICATOR WAS CONFIRMED FAILUR E W/BENCH TEST FINDING POINTERS SPLIT DUE TO DEFECTIVE REED SWITCH. UNIT CALIBRATED. 2 L 7 2 4F RT A16WE 2002091000110 20020910 00110 EU 2002 9 10 CA020903016 1 20020830 A 2822 2060B PUMP AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE FUEL BOOST FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA (CAN) DURING TAKEOFF ROLL, PILOT NOTICED FUEL PRESSURE ENUNCIATOR LIGHT ILLUMINATION. PILOT IN COMMAND INITIATED REJEC TED TAKEOFF. AT TIME FLT CREW ADVISED ATC & RETURNED TO APRON. FURTHER EXAMINATION REVEALED THAT THE NR 1 FUEL BOOST P UMP CIRCUIT BREAKER HAD TRIPPED. MAINT ORGANIZATION CONTACTED. DISCUSSIONS BETWEEN FLT CREW & MAINT PERSONNEL DETERMIN ED MALFUNCTION OF NR 1 FUEL BOOST PUMP. OP & MAINT PROCEDURES WERE COMPLIED IN ACCORD WITH CO MIN EQUIP LIST 28-01-1. N O ABNORMALITIES WERE NOTED & FLT RESUMED ITS INTENDED ROUTE. OUR MAINT ORGANIZATION REPLACED DEFECTIVE BOOST PUMP. 2 L 7 2 4F 4 F RT A7EU E7EA 2002091000111 20020910 00111 NM 2002 9 10 EVA2002091001 1 20020906 A 5753 FLAP TRACK BOEING 767 767300 1385204 NM TE FLAPS CORRODED W QOCF K NONE O OTHER IN INSP/MAINT 1 WP 03 16603 26064 .DURING B-16603 C10 CHECK FOUND RT MAIN FLAP INBOARD TRACK BEAM FASTENER HOLE CORRODED. 2 L 7 2 4F RT A1NM 2002091000118 20020910 00118 NM 2002 9 10 AWXA200200765 1 20020803 A 5315 6546810501 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF TEE CHORD BS 967, RBL 27 - 41, WL 208. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED TEE CHORD BS 967 FROM BL 0 TO RBL 43. FABRICATED A NEW TEE CHORD, 4 REPAIR ANGLES, 4 STRAPS, AND INSTALLED REPAIR PARTS IAW B737-200 SRM 51-30- 2, PG 8-9, & 13, AND SRM 53-10-9, FIG 2, PG 7-11. 2 L 7 2 4F RT A16WE 2002091000119 20020910 00119 NM 2002 9 10 AWXA200200768 1 20020801 A 5320 694147310 INTERCOSTAL BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON INTERCOSTAL AT BS 500A, STRINGER 25 RT. MAINTENANCE REMOVED INTERCOSTAL FROM BS 500A, STRINGER 25 RT, FABRICATED A NEW INTERCOSTAL PER DWG 69-41473, AND INSTALLED REPAIR I AW B737-200 SRM 51-30-2 PG 8-9 & 32. 2 L 7 2 4F RT A16WE 2002091000120 20020910 00120 NM 2002 9 10 AWXA200200769 1 20020731 A 5320 651862110 PLATE BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FORWARD CORNER SCUFF PLATE. MA INTENANCE PREPARED, TREATED, AND WELDED THE CRACK ON FORWARD CORNER SCUFF PLATE IAW AWA ER 15-5333-01016-JS2. 2 L 7 2 4F RT A16WE 2002091000121 20020910 00121 NM 2002 9 10 AWXA200200773 1 20020724 A 5230 6546821528 SKIN BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 YVR - MAJOR REPAIR - DURING C-20 CHECK A .5 INCH CRACK WAS FOUND 10 INCHES UP ON THE AFT END OF THE FORWARD CARGO DOOR, JUST FORWARD OF LIGHTENING HOLE BS 485. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC INSPECTION TO VERIFY THE CRAC K WAS CONTAINED, FABRICATED A DOUBLER, AND INSTALLED REPAIR IAW AWA ER 15-5234-02225-TB2. 2 L 7 2 4F RT A16WE 2002091000126 20020910 00126 NM 2002 9 10 AWXA200200776 1 20020810 A 5320 143N52601 ANGLE BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 LCQ - MAJOR REPAIR - DURING C-08 CHECK A 1.25 INCH CRACK WAS FOUND ON FLOORBEAM SUPPORT ANGLE BETWEEN BS 660 - 680. MAI NTENANCE REMOVED CRACKED FLOORBEAM SUPPORT ANGLE, FABRICATED A NEW FLOOR SUPPORT ANGLE, AND INSTALLED REPAIR IAW B757-20 0 SRM 51-10-02, PG 15 AND SRM 51-40-02, PG 8, 11-12. 2 L 7 2 4F RT A2NM 2002091000127 20020910 00127 NM 2002 9 10 AWXA200200781 1 20020820 A 5330 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 SJC - MAJOR REPAIR - DURING ROUTINE INSPECTION RAMPER FOUND A 4.25 INCH CRACK 8 FT AFT OF THE AFT CARGO DOOR, APPROXIMAT ELY 20 INCHES UP FROM RT SIDE OF CENTER BELLY, BS 940, STR 18 RT. MAINTENANCE CUT OUT DAMAGED AREA OF SKIN AND PERFORME D A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER AND SPLICE PLATE AND INSTALLED REPAIR PARTS IAW B737 -200 SRM 53-30-3, FIG 16. 2 L 7 2 4F RT A16WE 2002091000128 20020910 00128 NM 2002 9 10 0202606637 1 20020812 A 2530 COFFEEMAKER BOEING 747 747251B 1384892 NM GALLEY MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 637US 23548 DURING CRUISE, A BURNING SMELL EMITTED NEAR THE NR 3 GALLEY. DEACTIVATED THE NR 3 GALLEY, GASPER FAN AND RECIRCULATION FAN AND THE SMELL DISSIPATED. DECLARED AN EMERGENCY AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDE NT. REPLACED THE LEFT FORWARD COFFEEMAKER IN THE NR 3 GALLEY. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002091000129 20020910 00129 NM 2002 9 10 0202616310 1 20020810 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK (TPE), FOUND -A- ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE ON THE RIGHT SIDE. RECONNECTED THE LIGH T CONNECTOR AT DOOR 1R. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002091000130 20020910 00130 NM 2002 9 10 0202626626 1 20020812 A 2910 FITTING BOEING 747 747251B 1384892 NM HYD SYSTEM LOOSE A NWAA A UNSCHED LANDING K F FLUID LOSS FLT CONT AFFECTED CL CLIMB 1 GL 01 626US 21708 DURING CLIMB, LOST FLUID FROM THE NR 4 HYDRAULIC SYSTEM AND THE OUTBOARD FLAPS DID NOT RETRACT. DECLARED AN EMERGENCY A ND THE AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. TIGHTENED A FLEXIBLE HYDRAULIC PRESSURE LINE FITTING ON AF T SIDE OF THE ENGINE DRIVEN HYDRAULIC PUMP IN THE NR 4 PYLON. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002091000131 20020910 00131 NM 2002 9 10 0202635527 1 20020811 A 2910 271N61192 HYDRAULIC LINE BOEING 757 757251 1384970 NM HYD SYSTEM LEAKING A NWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 01 527US 23842 JUST AFTER DEPARTURE FROM MSP, THE AIRCRAFT EXPERIENCED A COMPLETE LOSS OF HYDRAULIC FLUID FROM THE LEFT HYDRAULIC SYSTE M. AN EMERGENCY WAS DECLARED WITH ATC AND THE AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED FROM THE RUNWAY. REPLACED THE HYDRAULIC LINE AT THE LEFT MAIN LANDING GEAR DOWNLOCK ACTUATOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002091000132 20020910 00132 WP 2002 9 10 0202669942 1 20020813 A 5220 591015931 DOOR DOUG DC9 DC932 3022066 WP EMERGENCY EXIT OUT OF RIG A NWAA K NONE O OTHER LD LANDING 1 GL 01 3991C 47175 RIGHT FORWARD OVERWING EXIT DOOR FELL OPEN DURING LANDING. NO PASSENGERS WERE ON THE AIRCRAFT. THE PLASTIC TRIM PANEL ON THE DOOR CRACKED WHEN THE DOOR FELL OUT. MAINTENANCE FOUND THE DOOR DAMAGED AND OUT OF RIG. REPLACED THE DOOR AND P LASTIC INNER LINER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002091000133 20020910 00133 EU 2002 9 10 0202673214 1 20020812 A 3320 LIGHT AIRBUS 320 A320211 3930320 EU CABIN DEFECTIVE A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 314US 00160 EN ROUTE TO SPOKANE, THE LEAD FLIGHT ATTENDANT NOTICED AN ELECTRICAL ODOR FROM THE AREA OF ROW 10DEF. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. RELAMPED AND INSPECTED AREA. NO ODOR PRESENT. 2 L 7 2 4F RT A28NM 2002091000134 20020910 00134 WP 2002 9 10 0202699975 1 20020827 A 2915 RELIEF VALVE DOUG DC9 DC931 3022065 WP HYD SYSTEM LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 9339 47382 DURING GEAR UPLATCH CHECK AFTER TAKEOFF, THE RIGHT HYDRAULIC SYSTEM FLUID QUANTITY WENT TO ZERO. GEAR DOOR OPENED AND M AIN LANDING GEAR EXTENDED AS THE HYDRAULIC SYSTEM FAILED. CREW ENSURED GEAR WAS PROPERLY EXTENDED PER COM. FLIGHT RETU RNED TO MDT AND LANDED SAFELY. MAIN GEAR DOORS WERE DAMAGED ON LANDING. MAINTENANCE FOUND THE PRESSURE RELIEF VALVE IN THE RIGHT WHEEL WELL LEAKING. REPLACED THE PRESSURE RELIEF VALVE, BOTH THE ELECTRIC AND ENGINE DRIVEN HYDRAULIC PUMPS AND ASSOCIATED FILTERS, AND GEAR DOORS. RESERVICED THE SYSTEM. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002091000135 20020910 00135 NM 2002 9 10 0202706309 1 20020820 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN NOT SEATED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51-60. RESEATED CONNECTOR AT ROW 51. OPERAT IONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002091000136 20020910 00136 NM 2002 9 10 0202716304 1 20020820 A 2913 3508806 PUMP BOEING 747 747451 1384940 NM NR 3 ENGINE FAILED A NWAA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS CL CLIMB 1 GL 01 664US 37686 22 23819 DURING CLIMB, LOST HYDRAULIC FLUID FROM THE NR 3 HYDRAULIC SYSTEM. TURNED NR 3 HYDRAULIC PUMPS OFF AND AIRCRAFT CONTINU ED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE NR 3 ENGINE DRIVEN HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002091000137 20020910 00137 NM 2002 9 10 0202726311 1 20020814 A 2530 COFFEEMAKER BOEING 747 747451 1384940 NM GALLEY BURNED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 671US 26477 DURING FLIGHT, SMOKE EMITTED FROM THE NR 3 GALLEY COFFEEMAKER. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INC IDENT. FOUND WIRE BURNT AT BOTTOM OF COFFEEMAKER. REPLACED THE COFFEEMAKER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002091000138 20020910 00138 WP 2002 9 10 0202739860 1 20020808 A 2780 DUCT DOUG DC9 DC951 3022051 WP L/E SLAT SLOW A NWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 01 769NC 47757 WHEN SLATS WERE DEPLOYED AT 250 KTS, THE AIRCRAFT ROLLED TO THE RIGHT AND THERE WAS NO BLUE SLAT EXTEND LIGHT. CREW CYC LED THE SLATS BACK UP NORMALLY, RE-DEPLOYED AND THE AIRCRAFT ROLLED AGAIN. AFTER A FEW SECONDS THE BLUE LIGHT ILLUMINAT ED AND THERE WAS LESS TENDENCY TO ROLL. LANDING AT MCI WAS UNEVENTFUL. MAINTENANCE FOUND THE LEFT T-DUCT SLOW. REPLAC ED THE LEFT -T- DUCT. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002091000139 20020910 00139 WP 2002 9 10 0202749937 1 20020827 A 2722 59140665569 POWERPACK DOUG DC9 DC931 3022065 WP RUDDER FAULTY A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 908H 47517 DURING CLIMB THROUGH 8000 FEET, THE AIRCRAFT WOULD YAW LEFT AND RIGHT. COMPLIED WITH COM PROCEDURES AND YAW ACTION STOP PED WHEN MANUAL RUDDER WAS SELECTED. AIRCRAFT RETURNED TO A NORMAL LANDING AT CLT. MAINTENANCE REPLACED THE RUDDER POW ER PACKAGE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002091000140 20020910 00140 NM 2002 9 10 0202766631 1 20020816 A 3320 SOCKET BOEING 747 747251B 1384892 NM GALLEY BURNED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 631US 23111 DURING FLIGHT, SMOKE EMITTED FROM THE NR 3 RIGHT GALLEY CENTER LIGHT. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITH OUT INCIDENT. REPLACED LIGHT SOCKET, BALLAST, AND FUSE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002091000141 20020910 00141 NE 2002 9 10 0202789150 2 20020822 A 7200 JT8D7 ENGINE DOUG DC9 DC914 3022034 WP PWA JT8 JT8D7 52053 NE RIGHT FAILED A NWAA C F ABORTED TAKEOFF ACTIVATE FIRE EXT. T A ENGINE CASE PENETRATION FLAME/FIRE TO TAKEOFF 1 GL 01 8908E 74552 3439 45749 657287 DURING TAKEOFF ROLL, THE RIGHT ENGINE EXPERIENCED AN UNCONTAINED FAILURE AND RELATED ENGINE FIRE. CREW ABORTED TAKEOFF AND DISCHARGED THE RIGHT ENGINE FIRE BOTTLE. MAINTENANCE REPLACED THE FIRE BOTTLE AND RIGHT ENGINE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2002091000142 20020910 00142 2002 9 10 0202796315 4 20020902 A 2330 ELECTRICAL BOX BOEING 747 747451 1384940 NM CABIN ODOR A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 575NW 33001 AT FL370, A STRONG ELECTRICAL ODOR IN THE AREA OF SEAT 10AB WAS OBSERVED BY THE FLIGHT ATTENDANT AND PILOT. ODOR DISSIP ATED AFTER 15 MINUTES AND FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED SEAT 10A CONSOLE AND SEB. OPER ATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 2002091000143 20020910 00143 NM 2002 9 10 0202816310 1 20020829 A 3350 TERMINAL BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM DOOR 3R - SEAT 38H. RECONNECTED TERMINAL AT SEAT 38. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002091000144 20020910 00144 NM 2002 9 10 0202826310 1 20020831 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK (TPE), FOUND RIGHT SIDE ZONE -A- FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REINSTALLED WIRE. OPERATIO NAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002091000145 20020910 00145 NM 2002 9 10 0202836310 1 20020903 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK (TPE), FOUND RIGHT SIDE ZONE -A- FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED WIRE. OPERATIO NAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002091000146 20020910 00146 WP 2002 9 10 ARWA20020804 1 20020701 A 5312 BULKHEAD DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, AFT PRESSURE BULKHEAD UPPER RIGHT SIDE WITH 1.5 INCH CRACK STA 1766. CUT OUT DAMAGE AREA AND FABRICATED FILLER, FINGER DOUBLER AND DOUBLER IAW DRAWING SR08530007; INSTALLED PARTS IAW DRAWING SR08530007. 2 L 7 4 4F 4A25 2002091000147 20020910 00147 WP 2002 9 10 ARWA20020805 1 20020701 A 5312 BULKHEAD DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, AFT PRESSURE BULKHEAD UPPER LEFT SIDE WITH 0.125 INCH, 0.050 INCH, 0.375 INCH, & 0.580 INCH CRACKS, STA 1766. CUT OUT DAMAGE AREA AND FABRICATED FILLER, DOUBLER AND FINGER DOUBLER IAW DRAWING SRO8530007; INSTALLED PARTS IAW DRAWING SRO8530007. 2 L 7 4 4F 4A25 2002091000148 20020910 00148 WP 2002 9 10 ARWA20020806 1 20020705 A 5711 SPAR DOUG DC8 DC863F 302198F WP LT WING CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, LEFT WING FRONT LOWER SPAR WITH CRACKS, STA XFS 526.7 (0.125 INCH) AND STA XFS 518 (1.25 INCH). ACCOMPL ISHED REPAIR OF LEFT WING FRONT SPAR LOWER OUTBOARD CAP IAW RED SKETCH 02-07-11-001 SHEET 1 TO 6. BOEING MESSAGE ARW-MI A-02-00016H. THIS REPAIR HAS BEEN FAA APPROVED AS A TEMPORARY REPAIR THROUGH FAA 8110-3 FORM. 2 L 7 4 4F 4A25 2002091000149 20020910 00149 NE 2002 9 10 ARWA20020811 2 20020831 A 7532 563883 BLEED VALVE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 3 ENGINE MALFUNCTIONED A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 661AV 64283 3841 45969 670978 WHILE SPOOLING ENGINES FOR TAKEOFF, NR 3 ENGINE MADE A LOUD NOISE AT 1.1 EPR 80 PERCENT N2 BLEEDS OFF. REMOVED AND REPL ACED PRESSURE RATIO BLEED CONTROL IAW DC-8 MM 75-30-0. CHECKED ENGINE RUN UP NORMAL IAW 71-00. 2 L 7 4 4F 4 F 4A25 1E8 2002091000150 20020910 00150 SO 2002 9 10 C2XA02CL179 1 20020902 A 3350 SIGN EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 15941 145035 CLE FLT 3292 CREW REPORTED THAT THE EMERGENCY EXIT IDENTIFIER SIGN IN THE CENTER CABIN CEILING IS INOP. 2 L 7 2 4F RT T00011AT 2002091000151 20020910 00151 SO 2002 9 10 C2XA02IA188 1 20020907 A 8012 23075454 B-NUT EMB 145 EMB145LR 3260212 SO NR 2 ENGINE LOOSE A C2XA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 27 13978 145180 IAH- DURING TAKEOFF THE CREW NOTED THAT E2 ATTCS NO MARGIN, REJECTED TAKEOFF. MAINTENANCE INSPECTED THE ENGINE AND FOU ND A LOOSE B-NUT ON THE START CONTROL VALVE. MAINTENANCE TIGHTENED THE B-NUT AND PERFORMED A ENGINE RUN ON THE NR 2 ENG INE. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002091000152 20020910 00152 SO 2002 9 10 C2XA02SH041 1 20020806 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 SHV- DURING C-CHECK INSPECTION, FRAME 22 RIGHT HAND OUTBOARD SILL AFT OF SERVICE DOOR WAS FOUND TO HAVE FOUR AREAS OF CO RROSION. MAINTENANCE OUT OF LIMITS RIGHT HAND OUTBOARD SILL IAW EMB 145-SRM 53-21-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002091000153 20020910 00153 SO 2002 9 10 C2XA02SH042 1 20020806 A 5320 14521725013 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 SHV- DURING C-CHECK INSPECTION, FRAME 18-19 RIGHT HAND OUTBOARD SILL FORWARD OF SERVICE DOOR HAD THREE AREAS OF CORROSIO N. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND OUTBOARD SILL BETWEEN FRAMES 18 AND 19 IAW EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002091000154 20020910 00154 SO 2002 9 10 C2XA02TY061 1 20020407 A 5544 12007254007 BRACKET EMB 145 EMB145 3260210 SO RUDDER CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 TYS DURING A SCHEDULED INSPECTION THE RUDDER II MID-BEARING BRACKET WAS FOUND TO BE CHAFED AT THE CONNECTING ROD ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE BRACKET IAW EMB-145 SRM 51-40-02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091000155 20020910 00155 SO 2002 9 10 C2XA02TY062 1 20020407 A 5310 14532604001 STOP FITTING EMB 145 EMB145 3260210 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 TYS DURING A SCHEDULED INSPECTION THE LEFT HAND OVERWING EMERGENCY EXIT UPPER STOP WAS FOUND GOUGED BEYOND MANUFACTURER S LIMITS. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT UPPER STOP IAW EMB-145 MM 20-10-01. 2 L 7 2 4F RT T00011AT 2002091000156 20020910 00156 SO 2002 9 10 C2XA02TY065 1 20020408 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 TYS DURING A SCHEDULED INSPECTION THE FORWARD CENTER OMEGA BEAM TOP CAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-145 SRM 51-20-03, 51-40-06 AND 51-40-02. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WIL L BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091000157 20020910 00157 SO 2002 9 10 C2XA02TY066 1 20020408 A 5315 14522226003 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 TYS DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM UNDER THE LAVATORY WAS FOUND TO BE CORRODED. MAINTENANCE REMOVE D AND REPLACED THE CENTER FLOORBEAM IAW EMB-SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UP ON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091000158 20020910 00158 NM 2002 9 10 AWXA200200783 1 20020821 A 2761 654456115 ACTUATOR BOEING 737 73733A 1384673 NM SPOILER LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 28 174AW 47650 13140 23633 PHX - EMERGENCY LANDING - FLT 0644 - ON DESCENT INTO PHX EN ROUTE FROM ELP LOST A-HYDRAULIC SYSTEM PRESSURE. MAINTENANC E FOUND THE NR 6 FLIGHT SPOILER ACTUATOR LEAKING. REMOVED AND REPLACED NR 6 FLIGHT SPOILER ACTUATOR IAW T/C R3M27021, L EAK AND OPERATIONAL CHECK WERE GOOD. 2 L 7 2 4F RT A16WE 2002091000159 20020910 00159 NM 2002 9 10 AWXA200200784 1 20020730 A 5320 149N7523 SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 LCQ - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND UNDER NUT PLATES FOR LOWER FASTENERS ON FLAP CUTOUT SUPPORT C HORD AT RT UPPER WHEEL WELL, BS 1147 TO BS 1180. MAINTENANCE REMOVED FLAP CUTOUT SUPPORT CHORD BS 1147 TO BS 1180. FAB RICATED A NEW CUTOUT SUPPORT CHORD AND INSTALLED REPAIR IAW B757-200 SRM 51-40-02, PG 4 & 11. 2 L 7 2 4F RT A2NM 2002091000160 20020910 00160 NM 2002 9 10 PCAA0209102 1 20020908 A 2910 82910009159 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM NOSE GEAR AREA LEAKING A PCAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 13 831EX 160 ROC-LGA FLIGHT#3905. CREW REPORTED #2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED IN FLIGHT DURING CLIMBOUT. AIR CRAFT DIVERTED TO SYR WITHOUT INCIDENCE. MAINTENANCE REPLACED A HYDRAULIC LINE IN NOSE GEAR AREA, AND SERVICED #2 HYDRAU LIC SYSTEM. OPERATIONAL AND LEAK CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091000161 20020910 00161 EU 2002 9 10 AWXA200200785 1 20020821 A 2560 P20700012015 FLASHLIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 645AW 238 SAN - EMERGENCY EQUIPMENT - DURING INSPECTION THE AFT FLIGHT ATTENDANTS FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFT FLIGHT ATTENDANTS FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002091000162 20020910 00162 EU 2002 9 10 AWXA200200786 1 20020821 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 642AW 1214 584 PHX - EEL - THE EMERGENCY LIGHT SYSTEM WON`T TEST. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY U NIT BATTERIES, AND LT AFT EMERGENCY POWER SUPPLY UNIT (13WL) AND BATTERIES IAW AMM 33-51-38, EMERGENCY LIGHT TEST WAS GO OD. 2 L 7 2 4F RT A28NM 2002091000163 20020910 00163 NM 2002 9 10 AWXA200200791 1 20020731 A 5310 6517684133 DOOR FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND L-1 DOOR FRAME CUTOUT FORWARD LOWER STOP FITTING ATTACH PLATE WEB DOUBLER, BS 294.5, STR 16 LT. MAINTENANCE REMOVED THE L-1 DOOR FORWARD LOWER STOP FITTING ATTACH PLATE; REMO VED CLOSE OUT ANGLE AND FRAME STIFFENER PLATE TO FOM; CUT AND REMOVED DAMAGED SECTION OF WEB; FABRICATED A REPAIR DOUBLE R, FILLER, AND LOWER STOP FITTING ATTACH PLATE AND INSTALLED ALL REMOVED PARTS AND REPAIR PARTS IAW B737-200 SRM 51-40-2 , FIG 1 PG 3. 2 L 7 2 4F RT A16WE 2002091000165 20020910 00165 SW 2002 9 10 CYX2002F00000 1 20020726 A 5400 20603220027 STRAP AROFAL OH58 OH58C 1181580 SW LT PYLON CRACKED A CYXR K NONE O OTHER IN INSP/MAINT 1 CE 01 9263Y 8908 6916239 DURING A 300 HOUR INSPECTION THE LEFT HAND AFT PYLON SUPPORT STRAP WAS FOUND CRACKED. THIS SUPPORT STRAP IS RIVETED TO THE UNDER SIDE OF THE UPPER CABIN ROOF BEAM LEFT HAND AFT CORNER. CRACK IS APPROXIMATELY 1.750 INCHES IN LENGTH AND OR IGINATED IN A BEND RADIUS. OUT OF THE FOUR SUPPORT STRAPS THE LEFT REAR IS THE MOST CRITICALLY LOADED. 1 G 7 1 3U NC H22NM 2002091000166 20020910 00166 SW 2002 9 10 CYX2002F00001 1 20020726 A 5400 20603220027 STRAP AROFAL OH58 OH58C 1181580 SW LT PYLON CRACKED A CYXR K NONE O OTHER IN INSP/MAINT 1 CE 01 82791 8810 6816965 DURING A 300 HOUR INSPECTION THE LEFT HAND AFT PYLON SUPPORT STRAP WAS FOUND CRACKED. THIS SUPPORT STRAP IS RIVETED TO THE UNDER SIDE OF THE UPPER CABIN ROOF BEAM LEFT HAND AFT CORNER. CRACK IS APPROXIMATELY 2.250 INCH IN LENGTH AND ORIGI NATED IN A BEND RADIUS. OUT OF THE FOUR SUPPORT STRAPS THE LEFT REAR IS THE MOST CRITICALLY LOADED. 1 G 7 1 3U NC H22NM 2002091000167 20020910 00167 SW 2002 9 10 CYX2002F00002 1 20020822 A 6340 407375021103 SENSOR BELL 407 407 1182206 SW ROTOR RPM FAULTY A CYXR O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 01 407LG 53143 ROTOR RPM ANNUNCIATOR LIGHT CAME ON AND STAYED ON IN FLIGHT. ROTOR RPM WAS IN THE NORMAL RANGE. INSTALLED A NEW ROTOR RPM SENSOR SWITCH AND SYSTEM OPERATED NORMALLY. CAUSE OF FAILURE UNKNOWN. 1 G 7 1 3U O H2SW 2002091000168 20020910 00168 NM 2002 9 10 EWC2002F00001 1 20020821 A 7160 STRUCTURE PIPER PA60 PA60700P 7106023 NM LYC O540 TIO540* 41532 EA FLAPPER VALVE BROKEN B EWCR K NONE O OTHER IN INSP/MAINT 1 SO 05 41MV 2102 608423009 MANIFOLD VALVE INSTRUMENT AIR OUTLET PORT BLOCKED BY FLAPPER VALVE. HINGE MATERIAL FLEXED UNTIL IT CRACKED AND SEPARATE D LEAVING LOOSE FLAPPER VALVE IN HOUSING. 1 M 7 2 3O 3 O RT A17WE E14EA 2002091000169 20020910 00169 SW 2002 9 10 FSP2002F00001 1 20020605 A 7921 407340339101 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C* GL COOLER BLOWER FAILED E FSPA K NONE O OTHER IN INSP/MAINT 1 NE 05 407NN 242 53250 FOUND BLACK GREASE COMING FROM BOTH BEARINGS ON THE OIL COOLER BLOWER, THESE WERE THE NEW STYLE REQUIRED BY ASB407-01-44 . 1 G 7 1 3U 3 U O H2SW E4CE 2002091000170 20020910 00170 EU 2002 9 10 KBMA115472 1 20020819 A 6720 350A27119120 BUSHING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE T/R CONTROL TUBE WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 1710 3296 TAIL ROTOR TUBE BUSHINGS WORN. REPLACED WITH 1 EACH NEW BUSHINGS. 1 G 7 1 3U 3 U H9EU E19EU 2002091000171 20020910 00171 SO 2002 9 10 LAB2002F00002 1 20020824 A 5753 SPRING PIPER PA32 PA32300 7103212 SO LYC O540 TIO540* 41532 EA FLAP RETURN BROKEN E LABA O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 05 6117J 6130 327640095 FAILURE OF FLAP TO RETRACT. INVESTIGATED AND FOUND SPRING BROKEN. 1 L 7 1 3O 3 O A3SO E14EA 2002091000172 20020910 00172 NE 2002 9 10 MMS2002F00000 2 20020828 A 8520 288935 BEARING AIRTRC AT300 AT301 0390103 SW PWA R1340 R134053 52016 NE ENGINE WORN C MMSG A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 03 316OT 828 3010478 ENGINE OIL CHIP LIGHT CAME ON AFTER TAKE OFF. RETURNED AND LANDED. FOUND METAL IN OIL AND FILTER. REMOVED PROP AND TH RUST BEARING COVER. FOUND THRUST BEARING BALLS SEVERLY WORN AND BALL CAGE BROKEN. REMOVED GEAR REDUCTION CASE AND REWO RKED BY OVERHAUL FACILITY. 1 L 7 1 3R 3 R A9SW 5E2 2002091000173 20020910 00173 CE 2002 9 10 SD23102001 1 20020818 A 3230 508103961 LINK BEECH 99 C99 1154006 CE MLG BROKEN E MGDA O OTHER J WARNING INDICATION LD LANDING 1 NM 03 223CA U200 ROUTINE FLIGHT, PREPARING AIRCRAFT FOR LANDING, SELECTED GEAR DOWN AND DIDN'T GET RIGHT MAIN GEAR DOWN AND LOCKED LIGHT. ATTEMPTED MANUAL GEAR EXTENSION WITH NO CHANGE IN GEAR INDICATION. REQUESTED FLY BY FOR VISUAL CHECK OF GEAR EXTENSION . GROUND REPORT ALL GEAR TO DOWN. CONFIGURED AIRCRAFT FOR MINIMUM SPEED LANDING. LANDED ON LEFT MAIN AND NOSE GEAR, S LOWED DOWN AND ALLOWED RIGHT MAIN TO CONTACT GROUND. RIGHT MAIN DID NOT HOLD AIRCRAFT WEIGHT, RIGHT ENGINE SHUTDOWN PRI OR TO PROPELLER CONTACTING GROUND. MINIMAL DAMAGE TO AIRCRAFT DUE TO HIGH FLOATATION LANDING GEAR. 1 L 7 2 3T A14CE 2002091000174 20020910 00174 2002 9 10 TC42002F00000 4 20020903 A 6122 9696001119 LINE BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO PROP GOVERNOR CHAFED B TC4R O OTHER K FLUID LOSS NR NOT REPORTED 1 SO 03 1888W TH340 299494R LUBRICATION LINE FROM PROPELLER UNFEATHERING ACCUMULATOR IS RUBBED BY FUEL LINE AT THROTTLE SERVO. RUBBED HOLE IN LINE CAUSING PROPELLER TO FEATHER. 1 L 7 2 3O 3 O 3A16 E5CE 2002091000175 20020910 00175 NM 2002 9 10 AWXA200200792 1 20020813 A 5320 65C320747 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON THE UPPER SURFACE OF THE OUTBOARD FORWARD RT AFT LAV FLOOR SUPPORT BS 991, RBL 32, WL 208. MAINTENANCE CLEANED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED FLOOR SUP PORT BS 991, RBL 32. FABRICATED A NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW B737-300 SRM 51-40-05, FIG 2-3, PG 4-5, AN D SRM 51-40-02, PG 10-11. 2 L 7 2 4F RT A16WE 2002091000176 20020910 00176 NM 2002 9 10 AWXA200200793 1 20020813 A 5320 65C326779 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON THE UPPER SURFACE OF RT AFT LAV FLOOR SUPPORT BS 992, RBL 29.5, WL 208. MAINTENANCE CLEANED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED FLOOR SUPPORT BS 992, RBL 29 .5. FABRICATED A NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW B737-300 SRM 51-40-05, FIG 2-3 PG 4-5, AND SRM 51-40-02, PG 10-11. 2 L 7 2 4F RT A16WE 2003062500119 20030625 00119 NM 2003 6 25 AWXA200200794 1 20020822 A 5754 STRUCTURE BOEING 737 7373S3 1384711 NM LE FLAP BROKEN A AWXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 28 312AW 24060 UNCOMMANDED FLT INPUT - ON APPROACH AFTER FLAPS SELECTED TO 30 DEG ACFT ROLLED HARD LT, REQUIRED ALMOST FULL RT AILERON TO KEEP STRAIGHT & LEVEL. SELECTED FLAPS TO 40 DEG & PROBLEM REMAINED, LANDED UNEVENTFULLY. MX PERFORMED VISUAL INSPE CTION OF WINGS AND FOUND LT INBOARD FORE FLAP AT INBOARD END BROKEN OFF FROM ATTACH POINT. FORE FLAP WAS SEIZED INTO MI D FLAP. MX REMOVED & REPLACED LT INBOARD FORE FLAP. ALSO REPLACED LT MID FLAP INBOARD CARRIAGE CAM TRACKS, OPS CHECK G OOD. VENDOR REPLACED 2 INBOARD END TORQUE TUBE RIBS (P/N'S 69-37814-2, AND 6937814-3). PERFORMED BOND REPAIR OF LEADIN G EDGE SKIN AT EXTREME INBOARD END WHERE SKIN WAS TORN 6 X 3.5 INCH AREA. ENTIRE FORE FLAP OVERHAULED. 2 L 7 2 4F RT A16WE 2002091000177 20020910 00177 NM 2002 9 10 AWXA200200796 1 20020801 A 5320 65468222 WEB BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN CLOSE OUT WEB AT BS 1005, RBL 43, CORROSION WAS ALSO FOUND ON LOWER SIDE OF SAME WEB AT RBL 44. MAINTENANCE REMOVED THE DAMAGED CLOSE OUT WEB BS 986.5 TO 1016, RBL 44. FA BRICATED A NEW CLOSE OUT WEB, AND INSTALLED REPAIR IAW B737-200 SRM 51-30-2, PG 2-3, 8-9, & 32, FIG 7, 11, &13 AND SRM 5 1-30-5, PG 4, FIG 2, 51-10-2, PG 1-2. 2 L 7 2 4F RT A16WE 2002091000178 20020910 00178 NM 2002 9 10 AWXA200200797 1 20020729 A 5330 654577452 SKIN BOEING 737 737277 1384570 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK FUSELAGE SKIN WAS FOUND TO REQUIRE REPLACEMENT DUE TO NUMEROUS REPAIR PATCHES, BS 727 - 908, STR 14 - 20 LT. MAINTENANCE CUT OUT SKIN BS 727 - 908, STR 14 - 20 LT. AFTER THE SKIN WAS REMOVED FOUND 2 CRACKED TIE CLIPS AT BS 727B, 747, AND 1 CRACKED SHEAR TIE ANGLE. FABRICATED A NEW SECTION OF SKIN, FILLERS, A REPAIR A NGLE, 9 TAPER SHIMS, 2 TIE CLIP, AND INSTALLED REPAIR PARTS IAW AWA ER 15-5361-02229-ES1. 2 L 7 2 4F RT A16WE 2002091000179 20020910 00179 NM 2002 9 10 AWXA200200799 1 20020723 A 5730 6546419 SKIN BOEING 737 737277 1384570 NM RT WING DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - MAJOR REPAIR - DURING C-20 THE RT WING LOWER SURFACE NR 5 SLAT TROMBONE CUTOUT HAS SMALL PIECE OF SKIN MISSING AT OUTBOARD END. MAINTENANCE REMOVED DAMAGED AREA OF SKIN RT WING LOWER SURFACE NR 5 SLAT TROMBONE CUTOUT, FABRICATED A NE W SECTION OF SKIN, AN INTERNAL SPLICE, AND WEB, AND INSTALLED REPAIR PARTS IAW AWA ER 15-5741-02221-SS1. 2 L 7 2 4F RT A16WE 2002091000180 20020910 00180 EU 2002 9 10 AWXA200200800 1 20020823 A 3350 341430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 643AW 315 PHX - EEL - EMERGENCY ESCAPE PATH LIGHTING WILL NOT TEST PER T/C I8M05319. MAINTENANCE REMOVED AND REPLACED THE AFT BAT TERY PACK AT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002091000181 20020910 00181 NM 2002 9 10 AWXA200200802 1 20020802 A 5315 6545409602 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A 2.7 INCH CRACK WAS FOUND ON THE LOWER SIDE OF FLOORBEAM UPPER CHORD AT BS 663, RBL 24, WL 202; VERIFIED BY HFEC INSPECTION. MAINTENANCE REMOVED CRACKED SECTION OF UPPER CHORD BS 663, RBL 24, WL 202. FABRICATED 2 REPAIR ANGLES, A STRAP, AND NEW SECTION OF CHORD. HFEC OF CHORD AND VERTICAL WEB IDENTIFIED 4 CRACKS PRO TRUDING FROM UPPER AND LOWER HOLES ON VERTICAL WEB AT RBL 19 & 20.5 UPPER ROW, AND RBL 20.5 & 28 LOWER ROW. OVERSIZED C RACKED HOLES ON VERTICAL WEB TO .200 AND RE-ACCOMPLISHED HFEC INSPECTION TO VERIFY CRACKS CONTAINED. INSTALLED REPAIR P ARTS FOR UPPER CHORD REPAIR IAW AWA ER 15-5715-02229-ES2. 2 L 7 2 4F RT A16WE 2002091000184 20020910 00184 NM 2002 9 10 AWXA200200804 1 20020731 A 5730 6546419 SKIN BOEING 737 737277 1384570 NM RT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK .25 INCH CRACKS WERE FOUND ON RT WING LEADING EDGE AT THE NR 6 SLAT CENTER STOP F ITTING CUTOUT, WS 557. MAINTENANCE BLENDED OUT CRACKS ON RT WING LEADING EDGE NR 6 SLAT CENTER STOP CUTOUT IAW AWA ER 1 5-5741-02232-SS1. 2 L 7 2 4F RT A16WE 2002091000186 20020910 00186 NM 2002 9 10 AWXA200200805 1 20020807 A 5210 654656113 WEB BOEING 737 737277 1384570 NM R2 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON R-2 DOOR INTERCOSTAL WEB AT BS 954, WL 252. MAINTEN ANCE REMOVED 3 STRAPS AND CRACKED INTERCOSTAL WEB AT BS 954, WL 252. FABRICATED A NEW INTERCOSTAL WEB, AND INSTALLED NE W WEB AND 3 STRAPS IAW 737-200 SRM 51-30-2 PG 4, 33-34, FIG 8. 2 L 7 2 4F RT A16WE 2002091000187 20020910 00187 NM 2002 9 10 AWXA200200806 1 20020815 A 5320 65429596 INTERCOSTAL BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON INTERCOSTAL IN THE AFT CARGO COMPARTMENT AT BS 800, RBL 43, WL 164. MAINTENANCE REMOVED DAMAGED INTERCOSTAL AT BS 800, RBL 43, WL 164. FABRICATED A NEW REPLACEMENT INTERC OSTAL, AND INSTALLED REPAIR IAW 737-200 SRM 51-20-1, PG 10-11, 14 & 18A, FIG 3 & 7, SRM 51-30-5, PG 4-5, FIG 2 & 3, AND SRM 51-10-2, PG 32, FIG 32. 2 L 7 2 4F RT A16WE 2002091000188 20020910 00188 NM 2002 9 10 AWXA200200809 1 20020725 A 5312 65841002 PRESSURE PANEL BOEING 737 737277 1384570 NM FUSELAGE CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK CHAFING WAS FOUND ON THE RT WHEEL WELL CEILING WEB CAUSED BY CONTACT WITH THE SPO ILER RATION MIXER. MAINTENANCE BLENDED OUT DAMAGE PER B737-200 SRM 51-10-6 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER AND TRIPLER, AND INSTALLED REPAIR PARTS IAW AWA ER 15-5702-02221-TB2. 2 L 7 2 4F RT A16WE 2002091000189 20020910 00189 NM 2002 9 10 AWXA200200811 1 20020724 A 5753 6546486 WEDGE BOEING 737 737277 1384570 NM T/E FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK THE LT INBOARD MIDFLAP TRAILING EDGE WEDGE END WAS FOUND TO HAVE CRACKS AND DELAM INATION IN POTTING COMPOUND AT THE 1ST, 2ND, AND 3RD INBOARD TRACK CUTOUTS AND OUTBOARD BLOCK. MAINTENANCE REMOVED DAMA GED LT INBOARD MIDFLAP TRAILING EDGE WEDGE, FABRICATED A NEW WEDGE PER DWG 65-46486, AND INSTALLED REPAIR. 2 L 7 2 4F RT A16WE 2002091000190 20020910 00190 NM 2002 9 10 AWXA200200813 1 20020820 A 5753 6546431 SKIN BOEING 737 737277 1384570 NM T/E FLAP GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK THE RT OUTBOARD TRAILING EDGE FOREFLAP FAILED CONDUCTIVITY TEST AFTER REPAIR OF 5 INCH LONG GOUGE FROM A CHAFING PANEL BOLTHEAD. MAINTENANCE REMOVED DAMAGED RT OUTBOARD TRAILING EDGE FOREFLAP SKIN, FA BRICATED NEW REPLACEMENT SKIN, AND INSTALLED REPAIR IAW AWA ER 2-57-52-17. 2 L 7 2 4F RT A16WE 2002091000191 20020910 00191 WP 2002 9 10 ABXA020155 1 20020708 A 5300 SR095301513 DOUBLER DOUG DC9 DC931 3022065 WP EXT. FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 CRACK IN FUSELAGE SKIN AT STATION 994, LONGERON 12 RIGHT, BETWEEN 2 RIVETS AND EXTENDING 1/4" PAST BOTH RIVETS. REPAIRED CRACK IAW DC-9 DWG SR09530151 AND E.A. 5311005-034. 2 L 7 2 4F A6WE 2002091000192 20020910 00192 WP 2002 9 10 ABXA020156 1 20020621 A 5300 SR095301513 DOUBLER DOUG DC9 DC931 3022065 WP EXT. FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 5" CRACK TOP OF FUSELAGE AT #1 LONGERON IN AFT PRESSURE BULKHEAD AREA. REPAIRED CRACK IAW DC-9 DWG SR0953151 AND E.A. 53 11005-034. 2 L 7 2 4F A6WE 2002091000193 20020910 00193 WP 2002 9 10 ABXA020158 1 20020624 A 5700 99193392 DOUBLER DOUG DC9 DC931 3022065 WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 ANGLED DOUBLER COMMON TO #7 SLAT TRACK RIB INBOARD AND FRONT SPAR CRACKED. REPAIRED AREA IAW DC-9 SRM 57-09. 2 L 7 2 4F A6WE 2002091000194 20020910 00194 WP 2002 9 10 ABXA020162 1 20020702 A 5330 29114065 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 FUSELAGE SKIN CRACKED AT UPPER AFT CORNER OF MAIN ENTRY DOOR CUTOUT. LOCATED AT UPPER AFT DOOR STOP. REPAIRED CRACKED FU SELAGE SKIN AT UPPER AFT CORNER OF MAIN ENTRY DOOR CUTOUT IAW DC-9 REWORK DWG SR0953252-7001. 2 L 7 2 4F A6WE 2002091000195 20020910 00195 WP 2002 9 10 ABXA020163 1 20020702 A 5315 49125401 SPLICE DOUG DC9 DC931 3022065 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 BULKHEAD 965 CABIN FLOOR, LOWER FITTING WAS CRACKED AT LEFT BUTT LINE 33. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002091000196 20020910 00196 WP 2002 9 10 ABXA020168 1 20020904 A 5300 591015824 DOUBLER DOUG DC9 DC931 3022065 WP STA. 872 - 940 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING ROUTINE LINE OPERATIONS AT ILN, MAINTENANCE DISCOVERED CORROSION ON THE FUSELAGE SKIN RESULTING IN THE DISCOVERY OF CORROSION ON THE INTERNAL DOUBLER P/N 5910158-24. THE DAMAGE TO THE INTERNAL DOUBLER WAS TRIMMED OUT AND A NEW SECTIO N SPLICED IN IAW DC-9 SRM 53-04, FIG. 12 C. THE INTERNAL DOUBLER WAS FABRICATED FROM 7075-T6 X .063". OTHER PERTINENT DE TAILS OF THIS REPAIR CAN BE FOUND IN W.O. 2002908. REF: REA D953-45018-MR. 2 L 7 2 4F A6WE 2002091000197 20020910 00197 WP 2002 9 10 ABXA020169 1 20020904 A 5300 2024T3X063 SKIN DOUG DC9 DC931 3022065 WP STA. 872 - 940 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING ROUTINE LINE OPERATIONS AT ILN, MAINTENANCE DISCOVERED CORROSION ON THE FUSELAGE SKIN, LOCATED AT THE LOWER CARGO DOOR JAMB, FORWARD LOWER CORNER. THE DAMAGE TO THE SKIN WAS TRIMMED OUT AND A NEW SECTION OF SKIN WAS SPLICED IN, IAW D C-9 SRM 53-04, FIG. 12 C. THIS SKIN WAS FABRICATED FROM 2024-T3 X .063". OTHER PERTINENT DETAILS OF THIS REPAIR CAN BE F OUND IN W.O. 2002908. REF: REA D953-45018-MR. 2 L 7 2 4F A6WE 2002091000198 20020910 00198 NM 2002 9 10 01645 1 20020903 A 2810 TANK BOEING 737 737230C 1384472 NM OVERSERVICED A MJYA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 SW 07 737TW 98909 63909 20257 On departure aircraft was notified by the Tower that aircraft was streaming fuel out of left wing tip area, Fuel stream was verified and called for immediate return to YIP. Declared an emergency. Landed normal not high energy stop or overwe ight. Maitenance determined that center wing tank had been overfueled. Sumped Surge tanks on both wings and inspected fo r leaks. System checked normal. 2 L 7 2 4F A16WE 2002091000199 20020910 00199 EU 2002 9 10 000191 1 20020824 A 2425 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU COCKPIT ACTIVATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 140 NO LEFT TORQUE INDICATION, NO LEFT PROP RPA INDICATION, LEFT GENERATOR LIGHT CAME ON. NO C/A STATED IN RPA. 2 L 7 2 4T RT A52EU 2002091000200 20020910 00200 NM 2002 9 10 AWXA200200814 1 20020725 A 5751 6546456 RIB BOEING 737 737277 1384570 NM AILERON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK CRACKS WERE FOUND ON THE LT AILERON LEADING EDGE RIBS AT THE OUTBOARD END, AND IN BOARD OF THE NR 2 HINGE FITTING. MAINTENANCE REMOVED OUTBOARD RIB OF LT AILERON, FABRICATED A NEW RIB, AND INSTALLED RE PAIR PER DWG 65-46456. MAINTENANCE DRESSED OUT CRACKS AT INBOARD OF THE NR 2 HINGE FITTING IAW B737-200 SRM 57-50-1 FIG 4, PG 6 H. PERFORMED HFEC INSPECTION TO VERIFY CRACKS WERE CONTAINED, NO CRACKS NOTED. 2 L 7 2 4F RT A16WE 2002091000201 20020910 00201 SO 2002 9 10 C2XA02TY063 1 20020407 A 3213 1456711540 HOUSING EMB 145 EMB145 3260210 SO RT MLG GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND MAIN LANDING GEAR FORWARD SIDE-BRACE BEARING HOUSING WAS FOUND GOUGED ON THE INNER SURFACE. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB GST-113/02. THE DYE PENETRANT INSPECTION WAS SATISFACTORY AFTER REPAIR. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091000202 20020910 00202 SO 2002 9 10 C2XA02TY064 1 20020407 A 3220 14521680003 CAP EMB 145 EMB145 3260210 SO NLG GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 TYS DURING A SCHEDULED INSPECTION THE NOSE LANDING GEAR FORWARD UPPER BEARING CAP WAS FOUND TO BE DAMAGED ON THE MATING SURFACE. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB GST-1126/02. THE DYE PENETRANT INSPECTION WAS SATISFACTO RY AFTER THE REPAIR. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091000203 20020910 00203 SO 2002 9 10 C2XA02TY067 1 20020408 A 5320 12043404003 STRAP EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 TYS DURING A SCHEDULED INSPECTION THE BELLY DRAIN GUSSET STRAP AT FRAME 53 WAS FOUND TO BE CORRODED. MAINTENANCE REMOV ED AND REPLACED THE GUSSET STRAP IAW EMB-145 SRM 51-40-02 AND EMB-145 CPM 51-21-04 AND 05. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091000204 20020910 00204 SO 2002 9 10 C2XA02TY122 1 20020816 A 5330 14521890005 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE NICKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 TYS DURING A SCHEDULED INSPECTION A NICK WAS FOUND ABOVE THE AFT AVIONICS DOOR. MAINTENANCE MEASURED AND BLENDED THE D AMAGE, PERFORMED DYE PENETRANT INSPECTION IAW-GST2491/02 AND CMP-51-21-02,05 AND 06. THE REPAIR WAS SATISFACTORY AND TH E AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. 2 L 7 2 4T RT T00011AT 2002091000205 20020910 00205 SO 2002 9 10 C2XA02TY124 1 20020816 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 20 AND 23. MAINTENANC E REMOVED AND REPLACED THE DAMAGED AREA AND FABRICATED NEW ANGLE SHIM AND FILLER IAW EMB-145 SRM 63-21-10, THE REPAIR WA S SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002091000206 20020910 00206 SO 2002 9 10 C2XA02TY123 1 20020816 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD CENTER TOP CAP BETWEEN FRAMES 20 AND 23. MAINTEN ANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002091000207 20020910 00207 SO 2002 9 10 C2XA02TY125 1 20020829 A 5320 14522459003 ANGLE EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD RAMP ANGLE AT FRAME 19 AND 20. MAINTENANCE REMOV ED AND REPLACED THE RAMP ANGLE IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091000208 20020910 00208 SO 2002 9 10 C2XA02TY126 1 20020904 A 5315 14000450001 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS, DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM WAS FOUND CORRODED AROUND SEVERAL FASTENERS IN LAV. MAINTENANC E REMOVED AND REPLACED THE CENTER TOP CAP IAW-EMB-135/145-SRM-51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WI LL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091000209 20020910 00209 EA 2002 9 10 COMA0260511 1 20020906 A 5300 601R3117215 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA F.S.460 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 18689 7044 INTERCOSTAL CRACKED AT F.S. 460 OUTBOARD OF LBL9.REPAIRED F.S. 460 INTERCOSTAL I/A/W WVAC EO 601R-53-3440B. 2 L 7 2 4F RT A21EA 2002091000210 20020910 00210 EA 2002 9 10 COMA0260512 1 20020906 A 5347 601R38312115 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FS 449.85 TO 499 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 18689 7044 RIGHT SIDE SEAT RAIL CORRODED FROM FS 449.85 TO 499.REMOVED AND REPLACED I/A/W CRJ AMM 20-21-00-910-801. 2 L 7 2 4F RT A21EA 2002091000211 20020910 00211 EA 2002 9 10 COMA0260513 1 20020906 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA F.S.449.85 TO 49 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 18689 7044 LEFT SIDE SEAT RAIL CORRODED FROM FS 449.85 TO 499REMOVED AND FABED SEAT RAIL FROM 20276-144-1-1IAW CRJ SRM 53-41-49 AND REPLACED I/A/W CRJ AMM 20-21-00-910-801. 2 L 7 2 4F RT A21EA 2002091000212 20020910 00212 EA 2002 9 10 COMA0260514 1 20020906 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 981CA 7163 FLIGHT 5084 - DURING CRUISE FLIGHT TO MCO RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY, AIRCRAFT LAN DED SAFELY AT MCO.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3, (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2002091000213 20020910 00213 EA 2002 9 10 COMA0260515 1 20020907 A 3240 750005000 VALVE CNDAIR CL600 CL6002B19 1900309 EA CTR FUSELAGE SEC FAILED A COMA K NONE J WARNING INDICATION TO TAKEOFF 1 SO 01 783CA 7585 7315 FLIGHT 6688. AFTER T/O DURING GEAR RETRACTION RECEIVED AN ANTI-SKID O/B AND PARKING BRAKE CAUTION MESSAGE, AIRCRAFT RETU REND TO THE FIELD.REPLACED THE MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002091000214 20020910 00214 EA 2002 9 10 COMA0260516 1 20020907 A 7930 TANK CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 934CA 7042 FLIGHT 5879 DURING CRUISE FLIGHT RECEIVED A LEFT ENGINE OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY AND DIV ERTED TO ATL, AIRCRAFT LANDED SAFELY.PERFORMED OPERATIONAL TEST OF THE ENGINE OIL REPLENISHING SYSTEM, SERVICED ENGINE W ITH OIL TO PROPER LEVEL. PERFORMED ENGINE RUNS, DISCREPANCY COULD NOT BE DUPLICATED. 2 L 7 2 4F RT A21EA 2002091000215 20020910 00215 EA 2002 9 10 COMA0260517 1 20020908 A 2930 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 984CA 973 7171 FLIGHT 5310. DURING CRUISE FLIGHT RECEIVED A #2 HYDRAULIC SYSTEM LOW RESSURE CAUTION MESSAGE, UNSCHEDULED LANDING AT CLE , AIRCRAFT LANDED SAFELY.REPLACED THE #2 ENGINE DRIVEN HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 2002091000216 20020910 00216 EA 2002 9 10 COMA0260518 1 20020905 A 3260 STRUT CNDAIR CL600 CL6002B19 1900309 EA A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 958CA 7111 FLIGHT 5517. WHEN THE GEAR HANDLE WAS RAISED AFTER T/O A "GEAR DISAGREE" AND "NOSE DOOR OPEN" WARNING MESSAGE ACTIVATED. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD LANDING SAFELY.SERVICED THE NOSE LANDING GEAR STRUT. 2 L 7 2 4F RT A21EA 2002091000217 20020910 00217 NM 2002 9 10 C1HA200286006 1 20020902 A 3350 BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 686CA 22021 Cockpit emergency exit light is INOP.Replaced 1 battery and cleaned contact. 2 L 7 3 4F A3WE 2002091000218 20020910 00218 EA 2002 9 10 COMA0260519 1 20020904 A 3230 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 929CA 927 7035 FLIGHT 5984 GEAR DISAGREE MESSAGE.REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2002091000219 20020910 00219 NM 2002 9 10 AWXA200200872 1 20020903 A 5313 69353521 STRINGER CLIP BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A 1/2" CRACK WAS FOUND ON STRINGER CLIP AT BS 559, STRINGER 10 R/H. MAINTENANCE R EMOVED DAMAGED STRINGER CLIP AT BS 559, STRINGER 10 R/H, FABRICATED A NEW STRINGER CLIP, AND INSTALLED REPAIR IAW DWG 69 -35352, AND B737-200 SRM 51-30-2, PG. 8, 9, FIG. 11, 13. 2 L 7 2 4F RT A16WE 2002091000220 20020910 00220 NM 2002 9 10 AWXA200200873 1 20020903 A 5313 69353521 STRINGER CLIP BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A 1/2" CRACK WAS FOUND ON STRINGER CLIP AT BS 597, STRINGER 9 R/H. MAINTENANCE RE MOVED DAMAGED STRINGER CLIP AT BS 597, STRINGER 9 R/H, FABRICATED A NEW STRINGER CLIP, AND INSTALLED REPAIR IAW DWG 69-3 5352, AND B737-200 SRM 51-30-2, PG. 8, 9, FIG. 11, 13. 2 L 7 2 4F RT A16WE 2002091000221 20020910 00221 NM 2002 9 10 AWXA200200874 1 20020903 A 5313 69353521 STRINGER CLIP BOEING 737 737277 1384570 NM A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A 1/2" CRACK WAS FOUND ON STRINGER CLIP AT BS 663, STRINGER 10 R/H. MAINTENANCE R EMOVED DAMAGED STRINGER CLIP AT BS 663, STRINGER 10 R/H, FABRICATED A NEW STRINGER CLIP, AND INSTALLED REPAIR IAW DWG 69 -35352, AND B737-200 SRM 51-30-2, PG. 8, 9, FIG. 11, 13. 2 L 7 2 4F RT A16WE 2002091100001 20020911 00001 SO 2002 9 11 C2XA02SH044 1 20020830 A 5300 14522226003 BUTT STRAP EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV-DURING C-CHECK INSPECTION, THE LEFT LATERAL BEAM AND CENTER FLOOR BEAM NUTPLATE HOLES WERE FOUND TO BE CORRODED AT B ETWEEN FRAMES 59 AND 61.MAINTENANCE REMOVED AND REPLACED BOTH THE LEFT HAND AND CENTER BUTT STRAP'S BETWEEN FRAMES 59 AN D 61 IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002091100002 20020911 00002 SO 2002 9 11 C2XA02SH045 1 20020830 A 5300 14526437001 BUTT STRAP EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV-DURING C-CHECK INSPECTION, THE RIGHT HAND LATERAL FLOOR BEAM WAS FOUND TO HAVE CORROSION AROUND THE NUTPLATE HOLES B ETWEEN FRAMES 59 AND 61.MIANTENANCE REMOVED AND REPLACED THE RIGHT HAND BUTT STRAP BETWEEN FRAMES 59 AND 61 IN ACCORDANC E WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002092000098 20020920 00098 SO 2002 9 20 C2XA02SH048 1 20020831 A 5320 14522461011 DOUBLER EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV- DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON NUT PLATE HOLES ON DOUBLER AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CORRODED DOUBLER AT FRAME 20 IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002091100003 20020911 00003 SO 2002 9 11 2002F00864 1 20020722 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR FOD A MASA O OTHER C F.O.D. TX TAXI/GRND HDL 1 SW 07 833MJ 145327 FLT 5847 - CLT-XNA - ON ARRIVAL IN XNA, THE MAIN CABIN DOOR COULD NOT BE OPENED FROM THE INSIDE. THE OUTSIDE HANDLE WOR KED NORMALLY. MAINTENANCE FOUND FOD JAMMING THE INNER HANDLE LINKAGE. REMOVED IT AND LUBRICATED DOOR. DOOR OPS NORMAL LY. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002091100004 20020911 00004 SO 2002 9 11 2002F00865 1 20020807 A 5210 14540853405 STOP EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 837MJ 145367 ASH - FLT 5897 - CLT-BTR - PAX DOOR WILL NOT CLOSE MAINTENANCE ADJUSTED DOOR STOPS IAW EMB AMM 52-18-02. OPS CHECKS GOO D. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002091100005 20020911 00005 SO 2002 9 11 2002F00866 1 20020811 A 3110 MR10042N INDICATOR EMB 145 EMB145LR 3260212 SO COCKPIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 833MJ 145327 ASH - FLT 5728 - CLT-ROA - COCKPIT PBE HAS LOST VACUUM. PBE WAS INSPECTED AND FOUND TO BE IN A SERVICEABLE CONDITION AS THE HUMIDITY INDICATOR WAS STILL BLUE. (M) 2 L 7 2 4T RT T00011AT 2002091100006 20020911 00006 SO 2002 9 11 2002F00867 1 20020805 A 3150 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO PITCH TRIM ACTIVATED A MASA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 07 839MJ 145416 FLT 5756 - CLT-MDW - RETURNED TO FIELD DUE TO A PITCH TRIM 1 EICAS MESSAGE. MAINTENANCE CURRENTLY TROUBLESHOOTING. RES ET C/B OPS CHECK GOOD. TRIM 3 SEC OR ABOVE 250K'S TRIPS SYSTEM. (M) 2 L 7 2 4T RT T00011AT 2002091100007 20020911 00007 NM 2002 9 11 2002F00868 1 20020727 A 2710 CONTROL CABLE DHAV DHC8 DHC8202 2809007 NM AILERONS DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 446YV 446 DURING AN A15 CHECK ON AIRCRAFT, NOTICED THAT CABLES WERE JUST WITHIN LIMITS. MAINTENANCE REMOVED AND REPLACED AILERON CABLES, PULLY, OUTBOARD ROLL SPOILER CABLE, RIGHT UPPER INBOARD AILERON CABLE, AN FCD WAS ISSUED TO INSPECT THE DHC8 FLEET. RESULTS PENDING. (M) 2 H 7 2 4T RT A13NM 2002091100012 20020911 00012 CE 2002 9 11 2002F00863 1 20020215 A 5410 1189100359 ANGLE BEECH 1900 1900C 1154161 CE NACELLE CRACKED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 198GA UB5 ANGLE LOCATED ABOVE THE ICE DOOR HINGE, THIS ANGLE HOLDS THE LOWER FIRE SEAL BULKHEAD. WHEN THIS ANGLE CRACKS, IT ALLOW S THE OUTSIDE COWL RIVETS TO WORK LOOSE, AND THIS CAUSES THE COWL SIDE SKIN TO CRACK. (M) 2 L 7 2 4T RT A24CE 2002100300014 20021003 00014 NM 2002 10 3 BJNA020801 1 20020804 A 5311 FRAME BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FORWARD CARGO COMPARTMENT STA 480 MAIN FRAME IS CORRODED AT STRINGER 26R UNDER TRANSITION PANEL. LEVEL 2 CORROSION. RE MOVED CORROSION. FABRICATED AND INSTALLED FRAME REPAIR IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002091100013 20020911 00013 NM 2002 9 11 BJNA020802 1 20020801 A 5712 RIB BOEING 737 737282 13844AT NM LT WING CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND LEFT WING LEADING EDGE RIB AT NR 2 SLAT ACTUATOR INBOARD CORRODED. (M) 2 L 7 2 4F RT A16WE 2002100300015 20021003 00015 NM 2002 10 3 BJNA020803 1 20020805 A 5330 SKIN BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 LAP SEAM RIVETS PULLING SKIN BULGING SEPARATING BS 1088 AT AFT FUSELAGE JACK POINT, LEVEL 2 CORROSION. REMOVED CORROSIO N, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW REO. PERMANENT REPAIR. 2 L 7 2 4F 4 F RT A16WE E2EA 2002100300016 20021003 00016 NM 2002 10 3 BJNA020804 1 20020805 A 5313 STRINGER BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 EACH STRINGER 26L AND 27L AT STA 957 AND 976 HAS CORRODED THROUGH STRINGERS, LEVEL 2 CORROSION. REMOVED CORRODED SECTIO NS OF STRINGERS 26L AND 27L, FABRICATED REPAIR SECTIONS FROM BAC1498.163 24 INCHES AND BAC1448-117 12.5 INCHES AND INSTA LLED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002100300017 20021003 00017 NM 2002 10 3 BJNA020805 1 20020803 A 5753 SKIN BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE T/E FLAP CHAFED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 LEFT WING OUT BOARD MID AND AFT FLAPS LOWER TRAILING EDGE SKIN HAVE CHAFED AREA JUST OUT BOARD OF NR 2 FLAP TRACK FAIRIN G. BLENDED AREA ON LEFT WING OUTBOARD MID AND AFT FLAPS LOWER TIE SKIN OUTBOARD OF NR 2 FLAP TRACK FAIRING. 2 L 7 2 4F 4 F RT A16WE E2EA 2002100300018 20021003 00018 NM 2002 10 3 BJNA020807 1 20020802 A 5320 BEAM BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 CORROSION IN AFT PIT AT STA 727 T CAP SPAR BETWEEN STR 24L 27L CORROSION AT STR 20 AND 21L BETWEEN STA 727 TO 727A. COR ROSION LEVEL 2. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR SECTION. REMOVED CORRODED VERTICAL BEAM AT BS 737 5 24-256. FABRICATED AND INSTALLED VERTICAL BEAM REPAIR PART IAW SRM, PERMANENT REPAIR. 2 L 7 2 4F 4 F RT A16WE E2EA 2002100300020 20021003 00020 NM 2002 10 3 BJNA020808 1 20020805 A 5320 FLOOR SUPPORT BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND CORROSION AT SCREW HOLES (7 EACH AT FRAME LBL 20 BETWEEN BS 947.5 TO BS 986.5. REMOVED AND REPLACED 2 EACH FLOOR SUPPORTS IAW SRM. PERMANENT REPAIR. 2 L 7 2 4F 4 F RT A16WE E2EA 2002091100014 20020911 00014 NM 2002 9 11 BJNA020809 1 20020806 A 5310 STRUCTURE BOEING 737 73728 138448R NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM FOUND CORROSION ON 4 SCREW HOLES AT RBL 20 BETWEEN BS 986.5 TO BS 967, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 2002091100015 20020911 00015 NM 2002 9 11 BJNA020810 1 20020808 A 5347 SEAT TRACK BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 SURFACE CORROSION ON SEAT TRACK AT RBL 32 AT BS 328, LEVEL 2 CORROSION. FOUND CORROSION ON SEAT TRACK OUT OF LIMITS, CU T NEW TRACK FROM BAC1520-792 16 INCH INSTALLED IAW 727 SRM 51-10-2, 51-10-1 AND 51-30-2. (M) 2 L 7 2 4F RT A16WE 2002100300021 20021003 00021 NM 2002 10 3 BJNA020811 1 20020806 A 5310 SHEAR TIE BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND CORROSION IN FORWARD PIT AT STA 500 LBL 2 TO RBL 2 FRAME LOWER LEG, LEVEL 2 CORROSION. CUT AND REMOVED CORROSION FROM SHEAR TIE LEG. FABRICATED AND INSTALLED SHEAR TIE REPAIR AND DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002091100016 20020911 00016 WP 2002 9 11 ABXA020172 1 20020724 A 5300 591326266 ANGLE DOUG DC9 DC941 302207N WP EXT. FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LOWER RIGHT PYLON ATTACH ANGLE WAS CRACKED AT STATION 1072. INSTALLED SECTION OF ATTACH ANGLE IAW DC-9 SRM 54-04. 2 L 7 2 4F A6WE 2002100300022 20021003 00022 NM 2002 10 3 BJNA020812 1 20020806 A 5320 TIE CLIP BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND TENSION TIE FITTING AT STA 104 STR 19L AND 20L CRACKED ON CORNER. LEVEL 2 CORROSION. REMOVED SECTION OF STATION 19L AT FS 104 FABRICATED REPAIR SECTION OF STATION AND TIE CLIP AT 19L AND 1104 TREATED, PRIMED AND INSTALLED STRINGER, SPLICES SECTION AND TIE CLIP IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002091100017 20020911 00017 NM 2002 9 11 BJNA020813 1 20020809 A 5310 DOOR FRAME BOEING 737 737282 13844AT NM FUSELAGE GOUGED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND RIGHT SIDE FORWARD EDGE OF AFT CARGO DOOR OPENING IS GOUGED AND TORN. CUT OUT DAMAGED AREA AND FABRICATED STACKED DOUBLER REPAIR PER B737 SRM 53-30-3 FIG 46. INSTALLED REPAIR PER B737 SRM 31-30-2, 51-20-4, 53-30-3 FIG 46. (M) 2 L 7 2 4F RT A16WE 2002091100018 20020911 00018 NM 2002 9 11 BJNA020814 1 20020802 A 5330 SKIN BOEING 737 737282 13844AT NM FUSELAGE GOUGED A BJNA K NONE O OTHER IN INSP/MAINT 1 NM 01 344TM 23044 FORWARD CARGO DOOR CUT OUT FUSELAGE SKIN GOUGED CRACKED BS 491 APPROX 5-23R AFT EDGE. BLENDED GOUGE AND CRACK PERFORMED NDT OF AREA NO CRACK REMAINING. FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIRED IAW B737 SRM 53-30-3, 51-10-2, AN D 51-20-4. (M) 2 L 7 2 4F RT A16WE 2002091100019 20020911 00019 WP 2002 9 11 GTIA020905 1 20020718 A 5320 STRUCTURE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFTER REMOVAL OF THRESHOLD TO FOM ENTRY WAY SUB FLOOR WAS FOUND CORRODED AT APPROX STATION 200. REMOVED COR RODED SECTION SUBFLOOR. FABRICATED REPAIR SPLICE. INSTALLED SPLICE, FLOOR SUPPORT AND WEB. (M) 2 L 7 2 4F A6WE 2002091100020 20020911 00020 WP 2002 9 11 GTIA020906 1 20020724 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND DENT AT FS 640 BETWEEN LONGERONS 15R AND 16R REQUIRES REPAIR. FABRICATED DOUBLER AND FILLER. INSTALLED REP AIR DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2002091100021 20020911 00021 WP 2002 9 11 GTIA020907 1 20020724 A 5330 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND EXISTING REPAIR AT FORWARD VHF ANTENNA CUT OUT REQUIRES REPLACEMENT. REMOVED EXISTING REPAIR DOUBLER. FABR ICATED DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2002091100022 20020911 00022 WP 2002 9 11 GTIA020908 1 20020724 A 5330 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND EXISTING REPAIR AT FS 237 BETWEEN LONGERON 30 AND 29L REQUIRES REPLACEMENT. REMOVED EXISTING FILLER AND DOU BLER. FABRICATED NEW DOUBLER AND FILLER. INSTALLED NEW REPAIR DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2002091100023 20020911 00023 WP 2002 9 11 GTIA020909 1 20020707 A 7830 THRUST REVERSER DOUG DC9 DC981 3022081 WP NR 1 ENGINE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND THREE DENTS ON FORWARD PART OF LOWER T/R 1 ENGINE. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. ( M) 2 L 7 2 4F A6WE 2002091100024 20020911 00024 WP 2002 9 11 GTIA020910 1 20020724 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND DENT ON FUSELAGE SKIN STATION 20 LONGERON 13L. DENT AND GOUED OUT OF LIMITS. FABRICATED REPAIR PARTS. INS TALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2002091100025 20020911 00025 NM 2002 9 11 HALA0200413 1 20020811 A 2130 DUCT BOEING 717 717200 1383700 NM COMPRESSOR CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 486HA 55131 HNL - FOUND LEFT COMPRESSOR OUTLET DUCT CRACKED. REPLACED DUCT. OPS CHECK OK. (M) 2 L 7 2 4F TR A6WE 2002091100026 20020911 00026 NM 2002 9 11 RIVA020716 1 20020716 A 3350 110049 CHARGER BOEING 727 727225 1384077 NM CABIN INOPERATIVE A RIVA K NONE L NO TEST IN INSP/MAINT 1 NE 05 361PA 20623 PSM - INTERIOR EMERGENCY EXIT LIGHTS AT DOOR L1 AND R1 INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER IAW MM 33-50-1 81. OPERATIONAL CHECKS GOOD. (M) 2 L 7 3 4F A3WE 2002091100027 20020911 00027 EU 2002 9 11 SIMA200222701 1 20020809 A 5347 7253799381 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 334AE 340B334 MBV - FOUND PREVIOUS REPAIR ON FORWARD END OF SEAT TRACK 18.3L CORRODED. PREPARED AND INSTALLED EXTRUSION (P/N 72537993 81) AND U-BEAM (P/N 7253799379) IAW SAAB 340 SRM 72LKS 3079 REV 40 53-70-60 PG 204/205. (M) 2 L 7 2 4T RT A52EU 2002091100028 20020911 00028 EU 2002 9 11 SIMA200222801 1 20020711 A 5220 DOOR SAAB SF340 340B 7860101 EU EMERGENCY EXIT MISINSTALLED A SIMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 386AE 340B386 ON PREFLIGHT, FOUND OVERWING EMERGENCY EXIT DOORS INSTALLED ON WRONG SIDES OF A/C. INSTALLED EMERGENCY EXIT DOORS IN TH E CORRECT POSITIONS. (M) 2 L 7 2 4T RT A52EU 2002091100029 20020911 00029 NM 2002 9 11 PCAA0209104 1 20020904 A 7120 87110021003 STRUT DHAV DHC8 DHC8102 2809003 NM OBL BROKEN A PCAA K NONE Z SIGNIFICANT FAILURE REPORT IN INSP/MAINT 1 EA 13 845EX 344 DURING A LEVEL INSPECTION LEFT OUTBOARD AFT ENGINE STRUT WAS FOUND BROKEN. ENGINE STRUT WAS REPLACED IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 71-20-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091100031 20020911 00031 EU 2002 9 11 AWXA200200717 1 20020809 A 5730 D5744358301300Z PANEL AIRBUS 320 A320232 3930326 EU RT WING MISSING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 653AW 1003 A 6 X 8 INCH PORTION OF PANEL 621FB FOUND MISSING AFT OF L/E O/B END, JUST I/B OF NR 2 ENG PYLON. A 4 INCH GOUGE TO HON EY COMB OF NR 2 ENG NOZZLE AT 10 O'CLOCK POSITION. UPON REMOVAL OF PANEL 621FB DAMAGE FOUND TO RT I/B L/E SLAT O/B TRAC K FAIRING, I/B & MIDDLE LANDING ASSEMBLIES, FORWARD O/B L/E ACCESS PANEL ATTACH BRACKET, AND GENERATOR FEEDER CABLES. O /B LANDING ASSY MISSING. MX REMOVED AND REPLACED NR 2 ENG NOZZLE, RT I/B L/E SLAT O/B TRACK FAIRING, I/B, MIDDLE, O/B L ANDING ASSEMBLIES, AND FORWARD O/B L/E ACCESS PANEL ATTACH BRACKET. SPLICED GENERATOR FEEDER CABLES I/B OF NR 2 ENG PYL ON IAW STANDARD PRACTICE MANUAL CHAP 20, CONTINUITY CHECK GOOD. ENG OPS CHECK OUT GOOD. 2 L 7 2 4F RT A28NM 2002091100032 20020911 00032 NM 2002 9 11 TSAA0253114 1 20020404 A 5310 654578832 STRUCTURE BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 PERFORMED WINDOW CORNER FASTENERS HOLE INSPECTION PER S/B 737-53A1177R 6 AND DISCOVERED DEFECTS IN WINDOW CORNERS WITH C RACK INDCIATION AT BS 440 RT WINDOW UPPER FORWARD CORNER USING HFEC METHODS. REPAIRED IAW SRM, AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 2002091100033 20020911 00033 EU 2002 9 11 USAABA02017 1 20020813 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 673UW 0337 PHL - EPSU 2L, 2R, 3L, AND 4R FAILED BATTERY CAPACITY TEST. MAINTENANCE REPLACED THE EPSU'S. GROUND OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A46NM 2002091100034 20020911 00034 NM 2002 9 11 USAABB02117 1 20020718 A 3350 20121 BATTERY BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 PHL - FOUND RIGHT AFT EMERGENCY DOOR GROUND ILLUMINATION LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGE R. (M) 2 L 7 2 4F RT A1NM 2002091100035 20020911 00035 EU 2002 9 11 USAABB02118 1 20020722 A 3350 321430 POWER SUPPLY AIRBUS 330 A330323 3930335 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 672UW 0333 PHL - DURING A-CHECK, FOUND THE 2R DOOR EPSU INOPERATIVE. MAINTENANCE REPLACED THE EPSU. (M) 2 L 7 2 4F RT A46NM 2002091100036 20020911 00036 2002 9 11 USAABB02122 4 20020722 A 2210 THROTTLE BOEING 767 7672B7 1385107 NM AUTO THROTTLE MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 656US 26847 PHL - FLT 11 - APPROXIMATELY THREE HOURS INTO THE FLIGHT, AT FL350, THE AUTO THROTTLES WENT TO IDLE DETENT. MAINTENANCE PERFORMED A FUNCTIONAL CHECK OF THE AUTO THROTTLE SYSTEM. NO FAULTS WERE FOUND. (M) 2 L 7 2 4F RT A1NM 2002091100037 20020911 00037 2002 9 11 USAABB02130 4 20020803 A 3422 6228000006 SIGNAL COND UNIT BOEING 767 767201 1385125 NM COCKPIT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 648US 53293 23900 AMS - FL 43 - AFTER TAKEOFF, CREW REPORTED THAT THE CAPTAINS ADI AND HSI WERE BLANK AND THE 'SG FAIL' WAS DISPLAYED. SE LECTING ALTERNATE EFI CORRECTED THE FAULT. THE FLIGHT RETURNED TO AMS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACE D THE LEFT SIGNAL GENERATOR. (M) 2 L 7 2 4F RT A1NM 2002091100038 20020911 00038 NM 2002 9 11 USAABB02131 1 20020807 A 3350 8731002511REV15 SIGN BOEING 757 7572B7 1384964 NM L4 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 615AU 27146 LAX - FOUND L4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002091100039 20020911 00039 EU 2002 9 11 USAASA02064 1 20020719 A 3350 321430 BATTERY PACK AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 764US 1369 PIT - THE FORWARD DOOR EXIT LIGHTS BLINK INTERMITTENTLY, STAYED ON, AND THEN LIGHT UNDER EMERGENCY EXIT STAYS ON. MAINT ENANCE REPLACED A BATTERY PACK ON EMERGENCY POWER SUPPLY UNIT 10WL. (M) 2 L 7 2 4F RT A28NM 2002091100040 20020911 00040 EU 2002 9 11 USAASA02066 1 20020722 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 738US 1254 TPA - THE EMEREGNCY LIGHT TEST SHOWS 'L EPSU LOAD FAULT FORWARD'. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002091100041 20020911 00041 NM 2002 9 11 USAASB02135 1 20020717 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM AFT ENTRY DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 337US 23235 PHL - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ABOVE THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002091100042 20020911 00042 NM 2002 9 11 AWXA200200815 1 20020724 A 5753 6546435236 SKIN BOEING 737 737277 1384570 NM T/E FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 11579 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK THE RT OUTBOARD AFT FLAP WAS FOUND TO EVIDENCE OF DEBONDING ON THE LOWER SURFACE INBOARD END. MAINTENANCE REMOVED AND REPLACED THE RT OUTBOARD AFT FLAP ASSEMBLY IAW T/C R3R27001. 2 L 7 2 4F RT A16WE 2002091100043 20020911 00043 NM 2002 9 11 USAASB02140 1 20020725 A 3350 WIRE BOEING 737 7373B7 1384580 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 511AU 23594 ORD - MAINTENANCE FOUND THE EMERGENCY EXIT AISLE LIGHT AT SEAT 6C INOPERATIVE. MAINTENANCE RESPLICED THE WIRE CONNECTIO N AT THE INBOARD ARMREST ASSEMBLY AT SEAT 6C. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002091100044 20020911 00044 NM 2002 9 11 AWXA200200816 1 20020724 A 5751 6546454504 SKIN BOEING 737 737277 1384570 NM AILERON DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 11579 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK DELAMINATION WAS FOUND ON THE LOWER OUTBOARD END OF THE RT AILERON. MAINTENANCE REMOVED AND REPLACED THE RT AILERON PER T/C R3M27015. 2 L 7 2 4F RT A16WE 2002091100045 20020911 00045 NM 2002 9 11 AWXA200200818 1 20020723 A 2823 60127 SHUTOFF VALVE BOEING 737 737277 1384570 NM FUEL SYSTEM FAILED A AWXA O OTHER X ENGINE FLAMEOUT IN INSP/MAINT 1 WP 28 182AW 11579 22649 YVR - ENGINE FLAMEOUT - DURING C-20 CHECK ENGINE PERFORMANCE DETERIORATION TEST THE NR 2 ENGINE EXPERIENCED IMPENDING FL AME-OUT WITHIN 40 SECONDS OF SHUTTING OFF THE NR 2 FUEL TANK BOOST PUMPS, ENGINE RECOVERED NORMALLY WITH BOOST PUMPS WER E RESELECTED TO THE ON POSITION. NR 1 ENGINE OPERATION WAS NORMAL. MAINTENANCE PERFORMED FUEL FEED SYSTEM VACUUM TEST PER AWA T/C F3L28001, NO LEAKAGE WAS NOTED. REMOVED AND REPLACED FUEL SHUTOFF VALVE RT WING IAW BMM 28-23-11, PG 401. RE-ACCOMPLISHED PERFORMANCE DETERIORATION CHECK PER AWA T/C F3B28001, TEST WAS GOOD. 2 L 7 2 4F RT A16WE 2002091100046 20020911 00046 NM 2002 9 11 USAASB02141 1 20020726 A 3350 CHARGER BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 504AU 23379 IND - MAINTENANCE FOUND THE AFT LEFT ESCAPE SLIDE EMERGENCY LIGHT AT THE AFT RIGHT SERVICE DOOR EMERGENCY EXIT LIGHT INO PERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1197 BATTERY CHARGER ASSEMBLY AT STATION 960L. OPERATIONAL CHECK OF EM ERGENCY LIGHTS GOOD. (M) 2 L 7 2 4F RT A16WE 2002091100047 20020911 00047 NM 2002 9 11 USAASB02142 1 20020726 A 3397 WIRE BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 522AU 23857 SYR - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTS AT SEAT ROWS 8, 9 AND 10L LEFT SIDE, INOPERATIVE. MAINTENANCE R EPAIRED A BROKEN WIRE. OPERATIONAL CHECK OF EVACUATION LIGHTS GOOD. (M) 2 L 7 2 4F RT A16WE 2002091100048 20020911 00048 NM 2002 9 11 2002UALA01395 1 20020831 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 AFT CABIN #4R DOOR CUT OUT AFT FRAME BODY STATION 1681 LOWER AREA AT FLOOR LEVEL IS CORRODED. MAJOR REPAIR ACCOMPLISHED .NESTED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002091100049 20020911 00049 NM 2002 9 11 2002UALA01396 1 20020901 A 5313 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 CABIN CREASE BEAM IB CHORD BODY STATION 734 TO BODY STATION 740 LBL 65 UPPER SURFACE HAS EXCESS MAT LOSS. MAJOR REPAIR ACCOMPLISHED.CREASE BEAM INNER CHORD REPLACED. PARTS SEALED AND FASTENERS INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002091100050 20020911 00050 NM 2002 9 11 2002UALA01400 1 20020903 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 AFT CARGO COMPARTMENT BODY STATION 1480 CIRCUMFERENTIAL FRAME AT STRINGER 24L TO 26L HAS CORROSION ON FORWARD SURFACE OF WEB AND UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED.NESTED ANGLE REPAIR AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002091100051 20020911 00051 NM 2002 9 11 2002UALA01404 1 20020905 A 5313 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 CABIN FLOOR STATION 773, RBL 62, INBOARD CREASE BEAM HAS CORROSION AT FLOOR BOARD FASTENER HOLE. MAJOR REPAIR ACCOMPLIS HED. CORROSION CUT OUT AND DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002091100052 20020911 00052 NM 2002 9 11 USAASB02144 1 20020727 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM FWD CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 517AU 23703 SYR - MAINTENANCE FOUND THE EVACUATION LIGHTS BY THE FORWARD ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002101800028 20021018 00028 NM 2002 10 18 2002UALA01412 1 20020905 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 AFT PIT FLOOR CUTOUT LOWER FRAME UPPER ANGLE CORRODED STA 1410 TO STA 1440. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMP LISHED. REPLACED UPPER ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002091100053 20020911 00053 NM 2002 9 11 AWXA200200819 1 20020803 A 5315 654681135 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION WAS FOUND ON THE UPPER SURFACE OF TEE CHORD AT BS 986, LBL 21 TO RBL 40, WL 208. MAINTENANCE BLENDED DAMAGED SECTION OF TEE CHORD, MATERIAL LOSS OUT OF LIMITS. REMOVED FLOOR SUPPORTS BS 9 66 TO BS 986.5, AND TEE CHORD BS 986, LBL 21 TO RBL 48. FABRICATED -2 & -3 FLOOR SUPPORT ANGLES, A NEW SECTION OF TEE C HORD, 2 FRAME CLIPS, AND -4 & -5 STRAPS, AND INSTALLED REPAIR PARTS IAW AWA ER 15-5300-02234-TB4. 2 L 7 2 4F RT A16WE 2002091100054 20020911 00054 NM 2002 9 11 AWXA200200831 1 20020812 A 5315 6545410554 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND IN THE UPPER FLANGE OF LONGITUDINAL FLOORBEAM AT RBL 4 5 APPROXIMATELY 2 INCHES FROM BS 727B, WL 208.1. MAINTENANCE CUT OUT CRACK IN UPPER FLANGE OF LONGITUDINAL FLOORBEAM RB L 45 AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A NEW TIE STRAP AND SHIM, AND INSTALLED REPAIR PARTS IAW AWA ER 15-5702-02234-TB5. 2 L 7 2 4F RT A16WE 2002091100055 20020911 00055 NM 2002 9 11 AWXA200200833 1 20020814 A 5320 654583469 STRAP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1.25 INCH CRACK WAS FOUND ON LOWER FRAME TO FRAME STRAP BS 312, RBL 26. MAINTE NANCE FABRICATED A REPAIR DOUBLER, AND INSTALLED REPAIR TO LOWER FRAME TO FRAME STRAP BS 312, RBL 26 IAW B737-300 SRM 53 -10-51 PG 213-219 FIG 204, SRM 51-40-02 PG 3 & 4 FIG 3-4, 6-8. 2 L 7 2 4F RT A16WE 2002091100056 20020911 00056 NM 2002 9 11 AWXA200200836 1 20020812 A 3350 1012621 LIGHT BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - EEL - DURING C-20 CHECK THE AFT SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND BROKEN. REPLACED AFT SERVICE DOOR EME RGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002091100057 20020911 00057 NM 2002 9 11 AWXA200200837 1 20020827 A 5314 6545866688 KEELBEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK A .5 INCH CRACK WAS FOUND ON LT KEEL BEAM BETWEEN BS 727 & BS 727A UNDER A PREVIO US REPAIR. MAINTENANCE TRIMMED OUT DAMAGED AREA OF KEEL BEAM AT BS 727 & BS 727A AND PERFORMED A HFEC INSPECTION TO VER IFY NO CRACKS EXIST. FABRICATED A STRAP, SHEAR TIE, ANGLE, AND 6 FILLERS, AND INSTALLED REPAIR PARTS IAW B737-200 SRM 5 3-10-6 FIG 2 - 3, PG 6-27 AND AWA ER 15-5369-02236-GF1. 2 L 7 2 4F RT A16WE 2002091100058 20020911 00058 SO 2002 9 11 C2XA02TY127 1 20020904 A 5240 000248 BUSHING EMB 145 EMB145 3260210 SO SERVICE DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED 2-C INSPECTION MAINTENANCE FOUND THE DAMPER BUSHING ON THE SERVICE DOOR SIDE SHOWING SIGN'S OF C ORROSION. MAINTENANCE REMOVED AND REPLACED THE DAMPER, CLEANED AND INSPECTED AREA IAW EMB 145 AMM 52-43-00. ALL WORK W AS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002091100060 20020911 00060 SO 2002 9 11 C2XA02TY129 1 20020905 A 5320 14521721009 STRAP EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS FOUND FWD DIGITAL PLATE AT GALLEY CORRODED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED NEW FWD STRAP IAW EMB 14 5 SRM 53-21-10; SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002091100061 20020911 00061 SO 2002 9 11 C2XA02TY131 1 20020906 A 5320 14521725013 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED INSPECTION THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED AT THE AFT SECTION. MAINTENANCE ACCOM PLISHED THE BLEND-OUT REPAIR IAW EMB GST 1927/02A AND EMB145 CPM 51-21-05, THE REPAIR WAS FOUND TO SATISFACTORY. THE AI RCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091100062 20020911 00062 SO 2002 9 11 C2XA02TY132 1 20020906 A 5315 14522460009 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED INSPECTION THE TOP CAP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A BLEND-O UT REPAIR IAW EMB GST 1927/02A AND EMB145 CPM 51-21-04, 51-21-05 AND 51-21-06. THE REPAIR WAS FOUND TO BE SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091100063 20020911 00063 SO 2002 9 11 C2XA02TY133 1 20020906 A 5315 14521700001 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED INSPECTION THE LEFT HAND OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLIS HED A BLEND-OUT REPAIR IAW EMB GST 1927/02A, EMB145 CPM 51-21-04, 05 AND 06. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091100064 20020911 00064 SO 2002 9 11 C2XA02TY135 1 20020906 A 5730 14565100406 SKIN EMB 145 EMB145 3260210 SO RT WING GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED INSPECTION A GOUGE WAS FOUND ON THE RIGHT HAND NR 1 LEADING EDGE. MAINTENANCE ACCOMPLISHED A BL END-OUT REPAIR IAW EMB GST 2512/02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL RELEASED UPON COMPLETION OF INSPECTI ON. 2 L 7 2 4F RT T00011AT 2002091100065 20020911 00065 SO 2002 9 11 C2XA02TY136 1 20020906 A 5730 14555101401 SKIN EMB 145 EMB145 3260210 SO RT WING GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED INSPECTION A GOUGE WAS FOUND ON THE RIGHT HAND LEADING EDGE NR 2. MAINTENANCE ACCOMPLISHED A BL END-OUT REPAIR IAW EMB GST 2649/02 AND EMB145 AMM 57-41-00. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091100066 20020911 00066 SO 2002 9 11 C2XA02TY137 1 20020907 A 5320 14521725001 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED INSPECTION THE PASSENGER DOOR SILL WAS TO BE CORRODED ON THE LEFT HAND AFT SECTION. MAINTENANCE REMOVED AND REPLACED THE SILL SECTION IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEA SED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091100067 20020911 00067 SO 2002 9 11 C2XA02TY138 1 20020907 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED INSPECTION THE SERVICE DOOR SILL WAS TO HAVE CORROSION ON THE FORWARD SECTION. MAINTENANCE REMO VED AND REPLACED THE SILL SECTION IAW EMB145 SRM 53-21-10, 51-20-03 AND 51-40-02. THE REPAIR WAS SATISFACTORY, THE AIRC RAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002091100068 20020911 00068 WP 2002 9 11 CALA0200440 1 20020818 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG LEAKING A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 18833 49493 THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF FROM MCO. THE GEAR WAS CYCLED, BUT THE HANDLE WOULD N OT RAISE PAST HALF WAY. THE AIRCRAFT WAS RETURNED TO MCO. MAINTENANCE FOUND THE NOSE STRUT DEFLATED DUE TO AN INTERNAL LEAK. A FULL NOSE STRUT REPACK WAS PERFORMED IAW MM 32-21-02. THE GEAR WAS CYCLED SEVERAL TIMES WITH NO DEFECTS NOTED . 2 L 7 2 4F A6WE 2002091100069 20020911 00069 NM 2002 9 11 CALA0200441 1 20020818 A 2432 18550 BATTERY BOEING 767 767224 1385170 NM E/E BAY OVERHEATED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 09 68155 30434 SMOKE AND BURNING ODOR ENTERED THE COCKPIT ON DESCENT INTO BRU. THE BATTERY CHARGER CIRCUIT BREAKER WAS PULLED AND THE SMOKE AND ODOR CEASED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE MAIN BATTERY HAD OVERHEATED AND BUB BLED OVER. THE MAIN BATTERY AND CHARGER WERE REMOVED AND REPLACED IAW MM 24-31-01. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A1NM 2002091100070 20020911 00070 2002 9 11 CALA0200442 4 20020826 A 2565 D31591478 SLIDE BOEING 737 737524 1384721 NM L1 DOOR UNSERVICEABLE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59630 44082 27534 THE L1 DOOR EMERGENCY ESCAPE SLIDE PRESSURE WAS OUT OF GREEN BAND. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-35. 2 L 7 2 4F RT A16WE 2002091100071 20020911 00071 NM 2002 9 11 CALA0200446 1 20020827 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 23589 INSPECTION FOUND FORWARD BAGGAGE BIN FLOOR NUT PLATE STRIP CORRODED AT STA 500D. A NEW ANGLE WAS INSTALLED IAW SRM 51-1 0-02. 2 L 7 2 4F RT A16WE 2002091100072 20020911 00072 EU 2002 9 11 CX7A194J17 1 20020816 A 2750 POTENTIOMETER SAAB SF340 340B 7860101 EU T/E FLAP OUT OF ADJUST A CX7A A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 03 308CE 340B210 DURING INITIAL CLIMBOUT FLAPS BEGAN UNCOMMANDED DEPLOYMENT TO LESS THAN 7 DEGREES, THEN RETRACTED. CYCLE REPEATED APPRO X EVERY 20 SEC W/PITCH UP MOVEMENT. NO AUTOPILOT ENGAGED, YAW DAMPER ENGAGED. FLAPS NOT SPLIT AND HANDLE AT FLAPS 0 DE G. FOUND LT FLAP POTENTIOMETER OUT OF ADJUSTMENT. ADJUSTED POTENTIOMETER IAW SAAB MM. 2 L 7 2 4T RT A52EU 2002091100077 20020911 00077 NM 2002 9 11 F3LA200200221 1 20020820 A 5320 ANGLE BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON MOP SILL SUPPORT ANGLE, BS 349, AT BOTTOM OF NUT PLATE HOLE ON L1 ENT RY DOOR. REMOVED MOP SILL SUPPORT ANGLE AND WEB PER SRM 51-30-2, LOCATED FASTENER HOLES ON MOP SUPPORT ANGLE PER SRM 51 -10-2 AND INSTALLED NEW MOP SILL SUPPORT ANGLE PER SRM 51-40-2. 2 L 7 2 4F RT A16WE 2002091100078 20020911 00078 NM 2002 9 11 F3LA200200222 1 20020820 A 5420 ANGLE BOEING 737 737317 138447P NM NR 1 PYLON CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED NR 1 PYLON SUPPORT ANGLE CRACKED IN AFT PORTION OF PYLON FWD OF CASTING, ADJACENT TO FLAP DOOR. REPLACED NR 1 PYLON SUPPORT ANGLE PER SRM 51-40-02 AND 51-40-05. 2 L 7 2 4F RT A16WE 2002091100079 20020911 00079 NM 2002 9 11 F3LA200200223 1 20020820 A 5230 DOOR FRAME BOEING 737 737317 138447P NM CARGO DOOR DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT LOWER AFT DOOR FRAME WEB CHIPPED AND PIECES MISSING. CUT OU T DAMAGED AREA, FABRICATED AND INSTALLED NEW SECTION OF FRAME WEB PER SRM 51-70-13 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002091100085 20020911 00085 NM 2002 9 11 F3LA200200233 1 20020820 A 5320 CHANNEL BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED L1 DOOR MOP SILL FLOOR ANGLE AND STANDS FOR THRESHOLD CORRODED. REPLACED THRESHOL D ATTACH CHANNEL AND ZEE ANGLE PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002091100092 20020911 00092 SO 2002 9 11 FFS2002F00006 1 20020902 A 2913 54001AA PUMP PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA HYD SYSTEM FAILED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 820FS 121 317952185 RL267268A GEAR HANDLE NOT RETURNING TO NEUTRAL. REMOVED PUMP AT 121.9 HOURS TSN. 1 L 7 2 3O 3 O A20SO E14EA 2002091100093 20020911 00093 GL 2002 9 11 HBK2002F00000 1 20020813 A 3220 MS178268 NUT CIRRUS SR SR22 2130001 GL CONT O550 IO550* SO FORK RETAINER MISSING E HBKA K NONE O OTHER IN INSP/MAINT 1 SW 11 808CD 494 0114 WHILE INSPECTING AIRCRAFT NOSE GEAR, FOUND NOSE FORK RETAINER NUT AND WASHER STACK MISSING. NO EVIDENCE OF HARDWARE EVE R BEING INSTALLED. NO SHEARED COTTER PIN. POSSIBLE NOSE FORK SEPARATION COULD HAVE OCCURRED CIRRUS SB HAD NOT BEEN ACC OMPLISHED. 1 L 7 1 3O 3 O NT A00009CH E3SO 2002091100094 20020911 00094 NM 2002 9 11 USAA020201 1 20020605 A 5542 65C2584151 SKIN BOEING 737 737401 1384701 NM RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 46636 23876 PIT - FOUND RUDDER WITH SEVERAL AREAS OF SKIN DAMAGE, STATION 196.46 TO STATION 0.00. WET LAY UP REPAIR PER EA 73884. (M) 2 L 7 2 4F RT A16WE 2002091100095 20020911 00095 NM 2002 9 11 USAA020282 1 20020723 A 7120 310A10201635403 MOUNT BOEING 737 737301 1384611 NM ENGINE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 1343 23228 PIT - FOUND ENGINE MOUNT STRUT WORN BEYOND LIMITS, ENGINE MOUNT MAIN SLEEVE REPAIR. REAMED, CHAMFERED, BLENDED AND ROTO PEENED THE FITTING BORE PER TYPICAL 54-50-10 REV A. (M) 2 L 7 2 4F RT A16WE 2002091100096 20020911 00096 NM 2002 9 11 USAA020284 1 20020724 A 5512 65C25746131A SKIN BOEING 737 7373B7 1384580 NM HSTAB LE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 42286 24515 PIT - FOUND LOWER SURFACE DELAMINATED 5 INCHES BY 5 INCHES, 74.5 INCHES FROM INBOARD END AND 10.5 INCHES FROM LEADING ED GE. REPAIRED PER SRM 55-20-01, 51-70-17 AND EA 74407. (M) 2 L 7 2 4F RT A16WE 2002091100097 20020911 00097 NM 2002 9 11 USAA020289 1 20020708 A 5320 STIFFENER BOEING 737 737301 1384611 NM BULKHEAD CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 44212 23510 TPA - FOUND STIFFENER CORRODED, STATION 1016, BL 0, AFT PRESS BULKHEAD STIFFENER. SPLICED IN LOWER SECTION OF STIFFENER PER EA 94326A, SB 737-53, 1075 REV A. (M) 2 L 7 2 4F RT A16WE 2002091100098 20020911 00098 NM 2002 9 11 AWXA200200839 1 20020724 A 5753 6546481251 FLAP BOEING 737 737277 1384570 NM LT WING DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK DELAMINATION OF THE L OUTBOARD FOREFLAP WAS FOUND AT THE INBOARD TRAILING EDGE. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARD FOREFLAP IAW T/C M3M57004. 2 L 7 2 4F RT A16WE 2002091100099 20020911 00099 NM 2002 9 11 AWXA200200840 1 20020723 A 5755 654645161B SKIN BOEING 737 737277 1384570 NM SPOILER DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 YVR - MAJOR REPAIR - DURING C-20 CHECK DELAMINATION ON THE UPPER SURFACE OF THE NR 7 FLIGHT SPOILER WAS FOUND AT THE 3 I NCH FOLD OF THE TRAILING EDGE AT INBOARD SIDE. MAINTENANCE REMOVED AND REPLACED THE NR 7 FLIGHT SPOILER PANEL IAW BMM 2 7-61-11 PG 401. 2 L 7 2 4F RT A16WE 2002091100100 20020911 00100 NM 2002 9 11 AWXA200200843 1 20020827 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM CABIN DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS FOUND DAMAGED. MAINTENANCE REMOVED A ND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002091100101 20020911 00101 NM 2002 9 11 AWXA200200844 1 20020827 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 150AW 23218 PHX - EEL - FLIGHT CREW REPORTED THAT THE EMERGENCY ESCAPE PATH LIGHT WAS LOOSE AND INOPERATIVE AT SEAT ROW 5 LT. MAINT ENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002091100102 20020911 00102 NE 2002 9 11 AWXA200200845 2 20020828 A 7532 BLEED VALVE AIRBUS A319 A319132 3930340 NM IAE V2527 V2527A5 NE NR 2 ENGINE LACK OF LUBE A AWXA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 WP 28 660AW 1234 V10732 PHX - ABORTED TAKEOFF - FLT 0014 - ON TAKEOFF FROM PHX EN ROUTE FOR JFK THE NR 2 ENGINE EGT EXCEEDED LIMITATIONS, ABORTE D TAKEOFF AT APPROXIMATELY 80 KTS. MAINTENANCE DOWNLOADED PREFLIGHT REPORT AND PERFORMED TROUBLESHOOTING TASKS 77-00-00 -810-844 INSPECTION OF EXHAUST SYSTEM, AND 77-00-00-810-818A / 75-32-42-200-010 INSPECTION OF VARIABLE STATOR VANE MECHA NISM, NO DEFECTS WERE NOTED. PERFORMED BITE TEST OF FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) ON CHANNELS A & B, BO TH CHANNELS FAULTED B25TK, LUBRICATED LOW PRESSURE COMPRESSOR (LPC) BLEED VALVE MECHANISM PER AMM TASK 72-00-00-600-011. 2 L 7 2 4F 4 F RT A28NM E40NE 2002091100103 20020911 00103 NM 2002 9 11 AWXA200200848 1 20020731 A 5230 143A61175 WEB BOEING 737 737277 1384570 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN THE FORWARD END OF LOWER WEB ON FORWARD CARGO DOOR BS 446, STR 23 RT. MAINTENANCE REMOVED CRACKED SECTION OF WEB, FABRICATED 2 FILLERS, AND INSTALLED REPAIR PARTS IAW EO 52-31-04, FIG 2, PG 26, 36-37. 2 L 7 2 4F RT A16WE 2002091100104 20020911 00104 EU 2002 9 11 AWXA200200849 1 20020828 A 3220 LANDING GEAR AIRBUS 320 A320231 3930325 EU NLG COLLAPSED A AWXA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 28 635AW 092 PHX - LANDING GEAR - FLT 0794 - AFTER LANDING AT PHX EN ROUTE FROM IAH AT LATER STAGE OF LANDING ROLL; THE NOSE LANDING GEAR COLLAPSED CAUSING SEVERE DAMAGE TO AIRFRAME, ENGINES, AND NOSE LANDING GEAR. 2 L 7 2 4F RT A28NM 2002091100105 20020911 00105 NM 2002 9 11 AWXA200200851 1 20020901 A 2560 P4010021 BATTERY PACK BOEING 737 7373B7 1384580 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 328AW 23377 TUS - EMERGENCY EQUIPMENT - DURING INSPECTION THE 2 FORWARD GALLEY EMERGENCY FLASHLIGHTS WERE FOUND INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE BATTERY PACKS IN THE 2 FORWARD GALLEY EMERGENCY FLASHLIGHTS, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002091100106 20020911 00106 EU 2002 9 11 AWXA200200852 1 20020902 A 2560 P4010021 BATTERY AIRBUS 320 A320231 3930325 EU FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 627AW 66 LAS - EMERGENCY EQUIPMENT - DURING INSPECTION THE AFT CABIN EMERGENCY FLASHLIGHT WAS FOUND TO NEED NEW BATTERIES. MAINT ENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002091100107 20020911 00107 NM 2002 9 11 AWXA200200857 1 20020831 A 5210 4507945178 SKIN BOEING 737 737277 1384570 NM L1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A .5 INCH CRACK WAS FOUND ON L1 DOOR INNER SKIN AT UPPER CORNER ACCESS HOLE FOR FOR UPPER END OF VERTICAL TORQUE TUBE. MAINTENANCE REMOVED DAMAGED AREA OF SKIN, FOUND MATERIAL LOSS TO BE WITHIN LIMIT S PER B737-200 SRM 52-00-2 PG 16, 21-24, FIG. 6. 2 L 7 2 4F RT A16WE 2002091100108 20020911 00108 NM 2002 9 11 AWXA200200858 1 20020825 A 5320 BAC5975 PLATE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK A .375 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FORWARD SCUFF PLATE, BS 807 , RBL 34. MAINTENANCE REMOVED AFT CARGO COMPARTMENT FORWARD SCUFF PLATE AT BS 807, RBL 34. WELDED CRACKED AREA OF SCUF F PLATE PER AWA ER 03-5333-99348-JS2B, RE-INSTALLED SCUFF PLATE IAW BMM 25-52-51 PG 402. 2 L 7 2 4F RT A16WE 2002091100109 20020911 00109 NM 2002 9 11 AWXA200200859 1 20020903 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM COCKPIT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 183AW 22650 PHX - EEL - DURING INSPECTION OF EMERGENCY LIGHT SYSTEM THE COCKPIT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT THE COCKPIT EMERGENCY LIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002091100110 20020911 00110 NM 2002 9 11 USAA020286 1 20020705 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 47222 23380 PIT - FOUND STRINGER CRACKED .5 INCH, BS 787 BETWEEN S8 AND S9 AT RIVET HOLE ON SUPPORT BRACKET. INSTALLED DOUBLER ON S UPPORT BRACKET FRAME AREA. (M) 2 L 7 2 4F RT A16WE 2002091100111 20020911 00111 EU 2002 9 11 AWXA200200860 1 20020904 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 19866 091 PHX - EEL - DURING INSPECTION EMERGENCY LIGHTS FAILED TEST AT PRESS TO TEST PANEL, STEP 5, T/C I8M05319. MAINTENANCE RE MOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (13WL), BITE TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2002091100112 20020911 00112 NM 2002 9 11 AWXA200200861 1 20020814 A 5320 6545815568 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON THE LOWER TEE CHORD REPAIR SPLICE ANGLE AT BS 344 FORWARD SIDE, LBL 53, WL 207.5. MATERIAL LOSS OUT OF LIMITS PRIOR TO BLEND. MAINTENANCE REMOVED EXTRUDED ANGLE, WEB PANEL AND DAMAGED SPLICE ANGLE AT BS 344 FORWARD SIDE LBL 53 WL 207.5. FABRICATED AND INSTALLED THE NEW REPAIR SPLICE ANGLE, AND RE-INSTALLED EXTRUDED ANGLE & WEB PANEL IAW DWG 65-45815, B737-300 SRM 53-10-15, PG 113, FIG 101, SRM 51-20-01, PG 10 & 47, FIG 2, SRM 51-40-02, PG 10-11, 16, 38, FIG 8, SRM 51-40-05, PG 4, FIG 2 AND SRM 51-20-05 PG 1-4 FIG 1. 2 L 7 2 4F RT A16WE 2002091100113 20020911 00113 NM 2002 9 11 USAA020290 1 20020712 A 5312 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 44212 23510 TPA - FOUND WEB CORRODED 3 SQUARE INCH AREA, BL 0, AFT PRESS BULKHEAD WEB, STATION 1016. CORROSION LEVEL 2, TASK NR C53 -107-02. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER PER EA 94326A AND SB 737-53A 1075 REV 3. (M) 2 L 7 2 4F RT A16WE 2002091100114 20020911 00114 NM 2002 9 11 USAA020291 1 20020720 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 48430 23311 PIT - FOUND INTERCOSTAL/ANGLE CORRODED 1 INCH BY 1 INCH AND .5 INCH BY .33 INCH, STATION 219.8 BELOW CAPTAIN NR 2 WINDOW . REMOVED CORROSION FROM INTERCOSTAL AND RIB ANGLE PER BOEING DWG 65-16305. (M) 2 L 7 2 4F RT A16WE 2002091100115 20020911 00115 NM 2002 9 11 USAA020292 1 20020714 A 5320 65516982 SPLICE BOEING 737 7373B7 1384580 NM STRINGER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 47222 23380 PIT - FOUND STRINGER SPLICE CRACKED .5 INCH, STATION 907 AT S-R4. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2002091100116 20020911 00116 NM 2002 9 11 USAA020293 1 20020730 A 5340 1131253 ATTACH ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 46973 23315 PIT - FOUND ANGLE CRACKED .75 INCH, INT ATTACH ANGLE FORWARD STATION 291.5, S12R AND S13R. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2002091100117 20020911 00117 NM 2002 9 11 USAA020294 1 20020730 A 5320 1131198 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 46873 23315 PIT - FOUND ANGLE CRACKED .5 INCH, INT ATTACH ANGLE FORWARD OF STATION 291.5, S11R AND S12R. DEFECTIVE PART REPLACED WI TH IDENT PART NR PER BOEING DWG 65-45807-31. (M) 2 L 7 2 4F RT A16WE 2002091100118 20020911 00118 NM 2002 9 11 USAA020296 1 20020730 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 46973 23315 PIT - FOUND FRAME CRACKED .25 INCH, INT DOOR FRAME ON FUSELAGE AT FORWARD UPPER CORNER. FABRICATED NEW ANGLE PER EA. ( M) 2 L 7 2 4F RT A16WE 2002091100119 20020911 00119 NM 2002 9 11 USAA020299 1 20020730 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 46973 23315 PIT - FOUND STRINGER CRACKED .125 INCH, AT RIVET STATION 927 AT STRINGER 8R AND 9R. REMOVED CRACK AND INSTALLED OVERSIZ ED FASTENER PER 51-40-05. (M) 2 L 7 2 4F RT A16WE 2002091100120 20020911 00120 NM 2002 9 11 USAA020300 1 20020730 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 46973 23315 PIT - FOUND STRINGER CRACKED .25 INCH, STATION 907, STRINGER 8L-9L AT RIVET. REMOVED CRACKED AND INSTALLED A REPAIR ANG LE PER TYPICAL REPAIR 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002091100121 20020911 00121 NM 2002 9 11 USAA020301 1 20020720 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 48430 23311 PIT - FOUND KEEL BEAM CORRODED, 3-4 INCHES, EXFOLIATION THROUGH BEAM S-28R AT STATION 540. CORROSION LEVEL 2, TASK NR C 53-208-01. REPLACED KEEL BEAM SECTION PER EA 74111. (M) 2 L 7 2 4F RT A16WE 2002091100122 20020911 00122 NM 2002 9 11 USAA020303 1 20020626 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND FRAME CRACKED .125 INCH, STATION 727F BETWEEN STRINGER 8/9R. REMOVED CRACKED AND INSTALLED DOUBLER PER TYPI CAL REPAIR 53-10-14 REV A. (M) 2 L 7 2 4F RT A16WE 2002091100123 20020911 00123 NM 2002 9 11 USAA020304 1 20020626 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND ANGLE CRACKED .5 INCH, STATION 294 BETWEEN STRINGER 12 AND 13 RIGHT. REMOVED CRACKED ANGLE AND INSTALLED NE W PER BOEING DWG 65-45807. (M) 2 L 7 2 4F RT A16WE 2002091100124 20020911 00124 NM 2002 9 11 USAA020305 1 20020626 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND FRAME CRACKED .125 INCH, STATION 827 BETWEEN STRINGER 8R AND 9R. REMOVED CRACKED FRAME AND INSTALLED DOUBLE R PER TYPICAL REPAIR 53-10-14 REV A. (M) 2 L 7 2 4F RT A16WE 2002091100125 20020911 00125 NM 2002 9 11 USAA020306 1 20020730 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND BEAM CORRODED 1 INCH BY 2 INCH AREA, FLOOR SUPPORT RBBL 8.10 AFT OF STATION 767. CORROSION LEVEL 1, TASK NR C53-208-01. REMOVED DAMAGE AT JOGGLE AND INSTALLED REPAIR PER TYPICAL REPAIR 53-10-06B. (M) 2 L 7 2 4F RT A16WE 2002091100126 20020911 00126 NM 2002 9 11 USAA020307 1 20020730 A 5315 1713200 FLOORBEAM BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND BEAM CORRODED 1 INCH BY 2 INCH AREA, FLOORBEAM LBBI 3.00 AFT OF STATION 767. CORROSION LEVEL 1, TASK NR C53 -202-01. SPLICE REPAIR, JOGGLE KIT, PER SRM 53-00-53 FIG 202 AND TYPICAL REPAIR 53-10-06B. (M) 2 L 7 2 4F RT A16WE 2002091100127 20020911 00127 NM 2002 9 11 USAA020310 1 20020702 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 23315 PIT - FOUND SKIN CRACKED 3 INCHES, ABOVE LEFT NLG DOOR JUST FORWARD OF STATION 259.5. TRIMMED OUT DAMAGE AND INSTALLED DOUBLER PER EA 61654B. (M) 2 L 7 2 4F RT A16WE 2002091100128 20020911 00128 NM 2002 9 11 AWXA200200862 1 20020813 A 5320 65C326772 WEB BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 MCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON THE LOWER SURFACE OF HORIZONTAL WEB AT BS 988, RBL 45, WL 208 (AFT OF 986.5 FLOORBEAM AND INBOARD OF CREASE BEAM). MAINTENANCE REMOVED DAMAGED WEB, FABRICATED A NEW WEB, AND INS TALLED REPAIR IAW DWG 65C32677, B737-300 SRM 53-60-51 PG 101-104, FIG 104, SRM 51-20-01 PG 10 & 47 FIG 2, SRM 51-40-02 P G 10-11, SRM 51-40-05 PG 4 FIG 2 AND BMM 51-21-99 PG 701-703. 2 L 7 2 4F RT A16WE 2002091100129 20020911 00129 EU 2002 9 11 AWXA200200864 1 20020905 A 3350 ABS0374A24 CONNECTOR AIRBUS 320 A320232 3930326 EU CABIN DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 640AW 448 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT WAS FOUND INOPERATIVE. MAINTENANCE REMO VED AND REPLACED DAMAGED CONNECTOR AT LOWER BULKHEAD SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD IAW T/C F1C33301. 2 L 7 2 4F RT A28NM 2002091100130 20020911 00130 EU 2002 9 11 AWXA200200865 1 20020905 A 2560 P4010021 BATTERY AIRBUS 320 A320231 3930325 EU FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 629AW 076 SEA - EMERGENCY EQUIPMENT - DURING INSPECTION THE EMERGENCY FLASHLIGHT AT THE AFT FLIGHT ATTENDANT SEAT WAS FOUND INOPER ATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN EMERGENCY FLASHLIGHT AT THE AFT FLIGHT ATTENDANT SEAT, OPERATI ONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002091100131 20020911 00131 NM 2002 9 11 AWXA200200866 1 20020905 A 3350 1010731 SIGN BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 158AW 23780 PHX - EEL - EMERGENCY EXIT SIGN AT THE L1 DOOR HAS 3 BULBS INOPERATIVE, RELAMP DID NOT HELP. MAINTENANCE REMOVED AND R EPLACED THE L1 DOOR EMERGENCY EXIT SIGN, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002091100132 20020911 00132 NM 2002 9 11 AWXA200200867 1 20020901 A 5320 69353521 STRINGER CLIP BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK THE OUTBOARD UPPER LEG OF STRINGER CLIP WAS FOUND CRACKED ON THE AFT SIDE OF FRAM E 663, STR 11 LT, ABOVE CABIN WINDOW. MAINTENANCE REMOVED DAMAGED STRINGER CLIP AT BS 663, STR 11 LT, FABRICATED A NEW STRINGER CLIP AND INSTALLED REPAIR IAW B737-200 SRM 51-30-5, PG 8-9 AND SRM 51-30-5 PG 4-5. 2 L 7 2 4F RT A16WE 2002091100133 20020911 00133 NM 2002 9 11 AWXA200200868 1 20020907 A 3350 100865 POWER SUPPLY BOEING 737 73733A 1384673 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 PHX - EEL - EMERGENCY ESCAPE EXIT LIGHTS AT L1 DOOR, R-1 DOORS, AND SEAT ROWS 1-4 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD POWER SUPPLY IAW BMM 33-51-51-962-016, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002091100134 20020911 00134 NM 2002 9 11 AWXA200200870 1 20020907 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 821AW 5891 1406 PHX - EEL - DURING INSPECTION THE FORWARD CABIN EMERGENCY LIGHTS WOULD NOT COMES ON. MAINTENANCE REMOVED AND REPLACED E MERGENCY POWER SUPPLY UNIT (11WL) AND BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002091100135 20020911 00135 NM 2002 9 11 AWXA200200871 1 20020903 A 5320 69353521 STRINGER CLIP BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A .75 INCH CRACK WAS FOUND ON STRINGER CLIP AT BS 706, STRINGER 3 LT. MAINTENANC E REMOVED DAMAGED STRINGER CLIP AT BS 706, STRINGER 3 LT, FABRICATED A NEW STRINGER CLIP, AND INSTALLED REPAIR IAW DWG 6 9-35352, AND B737-200 SRM 51-30-2 PG 8, 9 FIG 11, 13. 2 L 7 2 4F RT A16WE 2002091100136 20020911 00136 EU 2002 9 11 AWXA200200875 1 20020909 A 2530 416100123 COFFEEMAKER AIRBUS 320 A320232 3930326 EU GALLEY SHORTED A AWXA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 649AW 4571 2442 803 DURING CLIMBOUT FLIGHT CREW OBSERVED AN ELECTRICAL BURNING SMELL AND SMOKE COMING FROM FORWARD GALLEY, UPON INVESTIGATIO N THE F/A NOTICED ARCING AT THE NR 1 COFFEEMAKER. THE AIRCRAFT TURNED BACK TO PHX AND THE NR 1 COFFEEMAKER CIRCUIT BREA KER WAS PULLED. ARCING AND SMOKE STOPPED AT THIS TIME. AIRCRAFT LANDED AT PHX WITHOUT FURTHER EVENT. MAINTENANCE PERF ORMED VISUAL INSPECTION OF THE NR 1 COFFEEMAKER FINDING A SHORTED WIRE AND CIRCUIT BOARD DAMAGE. REMOVED AND REPLACED T HE NR 1 COFFEEMAKER AND PERFORMED OPERATIONAL CHECK, COFFEEMAKER CHECKED GOOD. MAINTENANCE ALSO PERFORMED A GALLEY SHED AND POWER TRANSFER, THIS CHECK WAS ALSO GOOD. CONFIRMED COFFEMAKER AS PROBLEM. A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002091100137 20020911 00137 NM 2002 9 11 F3LA200200234 1 20020820 A 5320 STRUCTURE BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 3372 23177 DURING C-7 CHECK, INSPECTION REPORTED CRACK IN SURROUNDING DOOR STRUCTURE TRIM AT BS 294.5, WL 208.1. REMOVED DAMAGED S ECTION, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-70-13. 2 L 7 2 4F RT A16WE 2002091100143 20020911 00143 WP 2002 9 11 MWEA020541 1 20020911 A 5330 59122851 WINDOW FRAME DOUG DC9 DC914 3022034 WP STATION 218 RH TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 WINDOW FRAME RETAINER FOR THE MOST FORWARD RIGHT PLUG WINDOW LOWER FORWARD CORNER HAS TOOL MARKS STATION 218 RIGHT -- BLENDED TOOL MARKS FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2002091100145 20020911 00145 NM 2002 9 11 UPS02239396 1 20020831 A 5700 6516201188 BRACKET BOEING 727 72722C 138400F NM WS192 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C R/H WING REAR SPAR LWR CHORD T BRACKET CORRODED WS 192 TO GAIN ACCESS #2 TANK FRONT SPAR PANELS RE MOVED. NEW BRACKET INSTAL LED IOAW BOEING DWG 65-16201, WING PANELS CLOSED. 2 L 7 3 4F A3WE 2002091100146 20020911 00146 NM 2002 9 11 UPS02239398 1 20020830 A 5710 WEB BOEING 727 72722C 138400F NM R/H WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C CRACK ON WEB ABOVE NO5 L/E FLAP I/B CORNER. CRACK STOP DRILLED IAW 727 SRM 51-10-01 NDT CARRIED OU TIAW NDT MAN 5 1-00-00 PT 6 FIG 4, CRACK CONTAINED. REPAIR CARRIED OUT IAW SRM REF 51-40-02. 2 L 7 3 4F A3WE 2002091100147 20020911 00147 NM 2002 9 11 UPS02239402 1 20020827 A 5330 BUTT JOINT BOEING 727 72722C 138400F NM BS 441 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C SUSPECT CORROSION FOUND AT BUTT JOINT BS 441, AREA DERIVETED BETWEEN S17 AND S21 R. COROSION FOUND OUTSIDE LIMITS BETWEEN 18R AND 21R IAW SRM 53-30-01. REPAIRED IAW UPS EO B727-5310- 1371 APPENDIX E. 2 L 7 3 4F A3WE 2002091100148 20020911 00148 EA 2002 9 11 COMA0260520 1 20020906 A 5320 6003106819 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FS460 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 18690 7044 FLOOR SUPPORT CRACKED AT F.S. 460 ON RBL9.INSTALLED NEW FLOOR SUPPORT P/N 600-31068-19 I/A/W WVAC E.O. 601R-53-34-3437A 2 L 7 2 4F RT A21EA 2002091100149 20020911 00149 EA 2002 9 11 COMA0260521 1 20020906 A 5300 60131171 ANGLE CNDAIR CL600 CL6002B19 1900309 EA F.S.484 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 18690 7044 RIGHT SIDE F.S. 484 ANGLE CRACKED ON OUTBOARD SIDE AT RBL 36.FABED AND INSTALLED NEW ANGLE ON F.S. 484 OUTBOARD SIDE AT RBL 36 IAW WVAC EO 601R-53-3438A. 2 L 7 2 4F RT A21EA 2002091100150 20020911 00150 EA 2002 9 11 COMA0260522 1 20020910 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA K NONE J WARNING INDICATION LD LANDING 1 SO 01 983CA 7169 FLIGHT 5922 DURING LANDING AT CVG RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREE FLAP POSITION.COMPLIED WITH AD 98-20 -01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3, (A,B,C AND E). FLAP SYSTEM WAS RESET WIT H NO FURHTER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2002091100151 20020911 00151 EA 2002 9 11 COMA0260523 1 20020910 A 3250 17300233 WIRE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 956CA 7105 FLIGHT 5975. AFTER DEPARTING CVT RECEIVED A STEERING IMPERATIVE MESSAGE AFTER GEAR RETRACTION. FLIGHT RETURNED TO THE FI ELD.REPLACED THE STEERING WIRING HARNESS. 2 L 7 2 4F RT A21EA 2002092000101 20020920 00101 SO 2002 9 20 C2XA02SH051 1 20020831 A 5320 14521725013 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV- DURING C-CHECK INSPECTION THE RIGHT SILLS FORWARD AND AFT OF SERVICE DOOR WERE FOUND TO HAVE SURFACE CORROSION. MA INTENANCE REMOVED AND REPLACED RIGHT SILLS FORWARD AND AFT OF SERVICE DOOR IAW EMB 145 SRM 51-20-01, SRM 51-40-02, SRM 5 1-20-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002092000100 20020920 00100 SO 2002 9 20 C2XA02SH050 1 20020831 A 5320 14522460011 BUTT STRAP EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV- DURING C-CHECK INSPECTION CORRODED NUT PLATE HOLES WERE FOUND ON CENTER FLOORBEAM BUTT STRAP AT FRAME 18. MAINTENA NCE REMOVED AND REPLACED BUTT STRAP BETWEEN FRAMES 17 AND 19 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RET URN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002091200001 20020912 00001 NM 2002 9 12 USAA020311 1 20020730 A 5320 CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 48430 23311 PIT - FOUND CORROSION ON CLIP 1 INCH BY 4 INCH, AT STATION 500D S28L-S28R. CORROSION LEVEL 1. CORROSION REMOVED, TREAT ED, PRIMED PER SRM 53-00-07, 51-10-02, 51-20-01. (M) 2 L 7 2 4F RT A16WE 2002091200002 20020912 00002 NM 2002 9 12 USAA020312 1 20020723 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 48430 23311 PIT - FOUND FRAME CORRODED 4 INCHES BY 8 INCHES, STATION 500C BETWEEN STRINGER 28R AND 29L FORWARD SIDE OF FRAME. CORRO SION REMOVED, TREATED, PRIMED, PAINTED PER SRM 51-20-04, 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002091200003 20020912 00003 NM 2002 9 12 USAA020313 1 20020619 A 5510 FRAME BOEING 737 7373B7 1384580 NM HORIZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 42286 24515 PIT - FOUND X-FRAME CORRODED .5 INCH BY 2 INCH AREA, FORWARD SPAR UPPER RIGHT BOLT HEAD TERMINAL FITTING. CORROSION LEV EL 1. CLEANED CORROSION, TREATED, AND PRIMED PER SRM 51-20-04 AND 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002091200004 20020912 00004 NM 2002 9 12 USAA020314 1 20020721 A 5320 1123578 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 42286 24515 PIT - FOUND FLOOR SUPPORT CORRODED 2 INCHES BY 6 INCHES, STATION 967-986 RBL 19 TOP BOTTOM. REMOVED FLOOR SUPPORT WITH IDENT PART NR PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002091200005 20020912 00005 NM 2002 9 12 USAA020316 1 20020731 A 5320 65516982 TIE CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 47222 23380 PIT - FOUND TIE CLIP CRACKED .125 INCH, STATION 908 S-4R. MANUFACTURED AND REPAIRED SPLICE PER DWG 65-45772 AND SRM 51- 10-02. (M) 2 L 7 2 4F RT A16WE 2002091200006 20020912 00006 NM 2002 9 12 USAA020317 1 20020731 A 5311 9V53261481 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 47222 23380 PIT - FOUND FRAME CRACKED .25 INCH, FRAME ATTACH BRACKET HOLE AT STATION 887-S9L. MANUFACTURED REPAIR IAW TYPICAL REPAI R 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002091200007 20020912 00007 NM 2002 9 12 USAA020318 1 20020731 A 5320 654583470 CHANNEL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 47222 23380 PIT - FOUND CHANNEL CRACKED .25 INCH, STATION 223 136-0 BELOW FLOOR. REPLACED ASSEMBLY WITH IDENT PART PER SRM 51-10-02 . (M) 2 L 7 2 4F RT A16WE 2002091200008 20020912 00008 NM 2002 9 12 USAA020319 1 20020731 A 5320 654581246 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 47222 23380 PIT - FOUND INTERCOSTAL CRACKED .25 INCH, STATION 340 BOTTOM OF VERTICL L. MANUFACTURED FROM BOEING DRAWING NR 65-45912 -46. (M) 2 L 7 2 4F RT A16WE 2002091200009 20020912 00009 NM 2002 9 12 USAA020321 1 20020731 A 5320 654581292 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 47222 23380 PIT - FOUND L-SUPPORT CRACKED .5 INCH, STATION 328 LBL 47 FLOORBEAM VERTICAL L. MANUFACTURED AND HEAT TREATED FROM PERF ORMED STOCK PER SRM 51-10-02 AND 20-30-06. (M) 2 L 7 2 4F RT A16WE 2002091200010 20020912 00010 NM 2002 9 12 USAA020322 1 20020731 A 5320 CHANNEL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 47222 23380 PIT - FOUND CHANNEL CRACKED .5 INCH, BELOW FLOOR STATION 328 LBL 4 INCHES. REPLACED ASSEMBLY PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002091200011 20020912 00011 NE 2002 9 12 AALA20021078 2 20020723 A 7250 BEARING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE NR 2 ENGINE LEAKING A AALA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 21 558AA 53088 AFTER SHUTDOWN, NR 2 ENGINE HAD NUMBER 6 BEARING OIL LEAK CAUSING A FIRE. FIRE BOTTLES 1 AND 2 WERE DISCHARGED. NUMBER 2 OIL QUANTITY WAS OBSERVED TO BE 8 QUARTS. REPLACED NUMBER 2 ENGINE. INSTALLED SERVICEABLE NUMBER 1 AND 2 FIRE EXTIN GUISHER BOTTLES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2002091200012 20020912 00012 WP 2002 9 12 AALA20021080 1 20020723 A 2130 A/C PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE A/C BAY FAILED A AALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 21 407AA 49318 ENROUTE, AFTER TAKEOFF TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED, FOLLOWED BY LOUD RUMBLING IN TAIL COMPARTMEN T. RETURNED, WHEN LIGHT FAILED TO EXTINGUISH. EXTINGUISHED OF SHORT FINAL. LANDED WITHOUT INCIDENT. REPLACED RT PACK AND CROSSOVER WYE DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2002091200013 20020912 00013 WP 2002 9 12 AALA20021094 1 20020726 A 2613 60714811 SENSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE TAIL COMPARTMENT DEFECTIVE A AALA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 21 203AA 49145 ENROUTE, TAIL COMPARTMENT HIGHT TEMPERATURE LIGHT ILLUMINATED WHILE CLIMBING THROUGH 17,000 FEET. TURNED HIGHT PRESSURE BLEED OF AIR CONDITIONING. CLOSING OF LEFT THROTTLE AND LEFT PACK EXTINGUISHED LIGHT. RETURNED AND LANDED WITHOUT INC IDENT. REPLACED TAIL COMPARTMENT HIGH TEMPERATURE SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2002091200014 20020912 00014 WP 2002 9 12 AALA20021144 1 20020810 A 2613 SENSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE TAIL COMPARTMENT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 593AA 53256 ENROUTE, AFTER TAKEOFF ON CLIMBOUT TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. STAYED ON FOR SEVERAL MINUTES. RETURNED RDU, WITH POWER REDUCED LIGHT EXTINGUISHED. LANDED RDU WITHOUT INCIDENT. REPLACED RT TAIL COMPARTMENT OVERHE AT SENSOR. RAN ENGINES TO ALL POWER SETTINGS WITH NO LEAKS NOTED, ALL INDICATIONS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E2EA 2002091200015 20020912 00015 WP 2002 9 12 AALA20021145 1 20020812 A 2150 CLAMP DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE ACM BAY LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70404 49315 ENROUTE, TAIL COMPARTMENT TEMPERATURE HIGH ANNUNCIATOR LIGHT ILLUMINATED ON TAKEOFF. RETURNED AND LANDED WITHOUT INCIDE NT. INSTALLED NEW CLAMP ON LEFT ACM DUCT SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2002091200016 20020912 00016 WP 2002 9 12 AALA20021146 1 20020807 A 2150 39271012 VALVE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE ACM BAY DEFECTIVE A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 486AA 49679 IMMEDIATELY AFTER TAKE OFF THE CABIN FILLED WITH NOTICEABLE AMOUNT OF SMOKE. DISSIPATED AFTER 3-5 MINUTES. RETURNED AN D LANDED WITHOUT INCIDENT. REPLACED LIGHT AND RIGHT AIR CONDITIONING PRESSURE REGULATOR VALVES. BOTH COALESCERS BAGS, AND LEAKING APU MAGNETIC DRAIN PLUG. ACCOMPLISHED PACK BURNOUT. NO SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2002091200017 20020912 00017 EU 2002 9 12 AALA20021175 1 20020816 A 2150 23409401 SEPARATOR FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE ACM BAY CRACKED A AALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 1417D 11396 ON TAKEOFF ROLL ORD, PACK ONE TEMPERATURE WENT TO 145 DEGREES. FLIGHT ATTENDANT AND PASSENGER REPORTED SMOKE IN CABIN. PACK ONE FAULTED ON OVERHEAD. RETURNED ORD AND LANDED WITHOUT INCIDENT. REPLACED LEFT PACK SEPARATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT E25NE 2002091200020 20020912 00020 CE 2002 9 12 CA020906001 1 20020824 A 3246 3A056518001 LINK CESSNA 206 TU206G 2073357 CE CONT O550 IO550F 17042 SO MCAULY D3A34 D3A34C402 GL AMPHIB FLOAT SEVERED W L ABORTED APPROACH O OTHER LD LANDING 1 CA (CAN) AMPHIB FLOATS SELECTED TO DOWN POSITION AND AIRCRAFT LANDED ON RUNWAY. THE PILOT FELT THE RT AFT FLOAT CONTACT PA VEMENT AND IMMEDIATELY INITIATED A GO-AROUND. SELECTED GEAR UP AND LANDED WITH NO INCIDENT ON THE WATER. INSPECTION FOU ND THE RT MLG ACTUATOR LINK BROKEN OFF AT THE END OF THE THREADED SHANK. WHEN THE ACTUATOR RUNS TO THE END OF ITS TRAVEL , THE JAM NUT AT THE END OF THE THREADED SHANK RESTS AGAINST THE STOP AND THE OVER CENTRE TRAVEL THEN MAKES THE JAM NUT ACT AS THEFULCRUM AND CAUSES A SLIGHT BENDING MOMENT ON THE LINK. THE NUMEROUS CYCLES CAUSED THE LINK TO CRACK AND FINAL LY BREAK. 1 H 7 1 3O 3 O A4CE E3SO 5 C P47GL 2002091200021 20020912 00021 EU 2002 9 12 AALA20021176 1 20020815 A 3397 CONNECTOR FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1430D 11415 DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTING AT 11 AND 12 DIM. REPLACED EMERGENCY EXIT FLOOR PATH LI GHTING CONNECTOR AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT E25NE 2002091200022 20020912 00022 WP 2002 9 12 AALA20021179 1 20020813 A 2170 21D101 COALESCER BAG DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE ACM BAY CONTAMINATED A AALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 466AA 49596 EN ROUTE, DAY-ORD UNKNOWN SMOKE IN CABIN AND IN COCKPIT DURING TAKEOFF. DISSIPATED AFTER APPROXIMATELY 5 MINUTES. RETU RNED AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM DAY TO ORD. REPLACED BOTH COALESCER BAGS AND ACCOMPLISHED PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2002091200023 20020912 00023 NM 2002 9 12 AALA20021199 1 20020817 A 2432 CHA5035 CHARGER BOEING 767 767323 1385205 NM GE CF6 CF680 30025 NE E/E BAY FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 AIRCRAFT MAIN BATTERY CHARGER FAILED DURING FLIGHT. REMOVED AND REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER. ACCOMP LISHED ALL REQUIRED CHECKS IAW MM. ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2002091200024 20020912 00024 EU 2002 9 12 AALA20021204 1 20020821 A 5340 FITTING FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE GIRT BAR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1436A 11426 FORWARD GIRT BAR BLOCK FITTING CORRODED AT FORWARD ENTRY. STA3850 FLOORBEAM 1420L. REMOVED AND REPLACED GIRT BAR BLOCK FITTING IAW SRM. 2 L 7 2 4F 4 F RT E25NE 2002091200025 20020912 00025 EU 2002 9 12 AALA20021205 1 20020821 A 5315 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1436A 11426 FLOORBEAM CAP CORRODED BLO, STA 4610-4710. CUTOUT CORROSION, INSTALLED STRAP AND DOUBLER IAW AARD. 2 L 7 2 4F 4 F RT E25NE 2002091200026 20020912 00026 EU 2002 9 12 AALA20021206 1 20020821 A 5315 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1436A 11426 FLOORBEAM, BL600R, CAP CORRODED, STA 3845-4850. CUTOUT CORROSION, INSTALLED FLOORBEAM CAP 3845-4850 PER SRM. 2 L 7 2 4F 4 F RT E25NE 2002091200027 20020912 00027 EU 2002 9 12 AALA20021207 1 20020821 A 5315 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1436A 11426 FLOORBEAM CAP CORRODED. (PL600L, STA 3845-4850). CUTOUT CORROSION, INSTALLED FLOORBEAM CAP STA 4175-4575 PER AARD. 2 L 7 2 4F 4 F RT E25NE 2002091200029 20020912 00029 WP 2002 9 12 02FDEA00602 1 20020802 A 5511 SPAR CAP DOUG DC10 DC1010 3022110 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 550FE 46521 HORIZONTAL STAB, CONSTANT SECTION, REAR SPAR UPPER CAP HAS A 2.5 INCH CRACK IN RT END OF VERTICAL TANG CRACK IS VERTICAL . REMOVED AND REPLACED PER EO 8-5510-7-4318. 2 L 7 3 4F A22WE 2002091200030 20020912 00030 NM 2002 9 12 02FDEA00603 1 20020826 A 2612 65249203 CONTROLLER BOEING 727 727200 138407E NM E/E BAY FAULTY A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 268FE 21674 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT AT FL250. ENG A/ICE HAD BEEN ON FOR SEVERAL MINUTES PRIOR AND TURNE D OFF PRIOR TO GOING TO QRH. LIGHT EXTINGUISHED PER QRH PROCEDURE, REPEAT WRITE-UP. REMOVED AND REPLACED FIRE DETECTIO N CONTROLLER PER MM 26-14. OPS CHECK NORMAL. WOULD NOT DUPLICATE. 2 L 7 3 4F RT A3WE 2002091200031 20020912 00031 NM 2002 9 12 02FDEA00604 1 20020823 A 2612 CONNECTOR BOEING 727 727100 1384036 NM FIRE WARNING FAULTY A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 149FE 19087 DURING TAKEOFF MSY RWY 19 AT V1 APPROXIMATELY 100 KNOTS, WARN BELL SOUNDED WITH NO OTHER LIGHTS OR INDICATIONS IN COCKPI T ATOGW 131.4 - ABORT INITIATED BELL W/N SILENCE ON INITIAL ATTEMPTS. MAIN CARGO SMOKE DET IS INOP. FOUND PTT SW ON TH E MAIN CARGO SMOKE DET SYSTEM CONTROL PANEL INTERMITTENT. LIGHTLY TAPPING SW CAUSES BELL TO SOUND BUT NO LIGHTS. REMOV ED CANNON PLUG ON MAIN CARGO SMOKE DETECTOR PNL TO PREVENT NUISANCE BELL. R&R AURAL WARNING BOX AS PRECAUTION PER MM 31 -26-000-4, OP CKS GOOD. TROUBLESHOOT PER WDM 26-16-01 PG 7, FOUND PIN 14 ON CONNECTOR D3828 CAUSING INTERMITTENT ALARM BELL. R&R CANNON PLUG CONNECTOR PER B727-100 WIRING DIAGRAM 26-16-01, OPS CK GOOD. 2 L 7 3 4F RT A3WE 2002091200032 20020912 00032 GL 2002 9 12 02FDEA00605 2 20020825 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 3 FAILED A FDEA F ACTIVATE FIRE EXT. X ENGINE FLAMEOUT DE DESCENT 1 SO 25 368FE 46606 451426 NR 3 ENGINE FAILED APPROX 45 MIN INTO FLIGHT AT FL310 FELT VIBRATION, HEARD NOISE AND MONITORED ALL ENGINE GAUGES WINDIN G DOWN. NO FIRE LIGHT, FOLLOWED RED TABS AND SHUTDOWN AND FIRED ONE FIRE BOTTLE. COULD NOT DUMP FUEL ( BELOW DUMPABLE LIMIT) SO LANDED OVERWEIGHT 35DEG FLAPS AT 368,000 POUNDS GW. REPLACED THE NR 3 ENGINE 2 L 7 3 4F 4 F A22WE E23EA 2002091200033 20020912 00033 NM 2002 9 12 02FDEA00606 1 20020825 A 2750 FLAP BOEING 727 727200 138407E NM WING FAILED A FDEA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 25 465FE 21289 OUTBOARD FLAPS DID NOT EXTEND PAST 23 ALTERNATE FLAP MOTOR USED TO EXTEND FLAPS. 2 L 7 3 4F RT A3WE 2002091200034 20020912 00034 NM 2002 9 12 02FDEA00607 1 20020827 A 5511 RIB BOEING 727 727100 1384036 NM HORIZ STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 LEFT HORIZONTAL STAB T/E RIB AT ELEVATOR BS 209, I/B SIDE HAS CHAFING DAMAGE. REMOVED AND REPLACED RIB PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002091200035 20020912 00035 NM 2002 9 12 02FDEA00609 1 20020825 A 5710 STRUCTURE DOUG MD11 MD11 3023602 NM RT WING SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FUSELAGE RIGHT SIDE LWR SURFACE OF WING ROOT AT WING TO BODY FILLET (154AB) SCRATCHED. REMOVED & REPLACED SKIN PER EA . 1-5330-66000. 2 L 7 3 4F RT A22WE 2002091200036 20020912 00036 EU 2002 9 12 02FDEA00610 1 20020831 A 4990 B-NUT AIRBUS 300 A300F4605R 3930327 EU APU LOOSE A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 682FE 3362 3362 800 NR 1 GEN FAULT ILLUMINATED IN FLIGHT. FOLLOWED ECAM PROCEDURES. UNABLE TO RESET NR 1 GEN STARTED APU. ACN RELEASED PE R MEL/CDL: 24-11-01GEN NR 1 - INOP. APU GEN MUST BE USED TO PWR 1 AFFECTED BUS THROUGHOUT FLIGHT. VERIFY AND RECORD IN EAML THAT OIL QTY OF IDG IN DISC MODE, REMAINING OPERATIVE IDG, & APU GEN ARE CHECKED ONCE EACH FLIGHT DAY. GPCU BITE INDICATED MPU/WIRING IN FLT APU AUTO-SHUTDOWN. APU INOP. FOLLOWED ECAM AND TURNED APU MSR SW OFF. DIVERTED TO RNO DUE TO NR 1 GEN + APU INOP, REF WRI 24-20/2038. APU SHOWED NO INDICATION OF OIL AT TANK. SERVICED APU TO FULL AND FOUND S EVERAL B-NUTS LOOSE. TIGHTENED B-NUTS WIPED DOWN AREA AND RAN APU WITH NO LEAKS DETECTED. 2 L 7 2 4F RT A35EU 2002091200037 20020912 00037 NM 2002 9 12 02FDEA00611 1 20020810 A 5315 FLOORBEAM BOEING 727 7272S2F 1384O81 NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 208 22930 BS 740 FLOORBEAM IS CHAFED RBL 43 TO LBL 56 WL 208 UPPER AFT FLANGE. REMOVED AND REPLACED FLOORBEAM PER EA 7-5310-65351 . 2 L 7 3 4F A3WE 2002091200038 20020912 00038 WP 2002 9 12 02FDEA00612 1 20020828 A 5314 KEELBEAM DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 322 47908 CENTER W/W LEFT WEB CORRODED AT FWD INSP PLATE ON KEELBEAM CORROSION IS STILL EVIDENT. CORROSION MAY ALSO BE UNDER ACCE SS PLATE. REMOVED AND REPLACED KEELBEAM PER EA 8-5310-65917. 2 L 7 3 4F RT A22WE 2002091200039 20020912 00039 WP 2002 9 12 02FDEA00614 1 20020904 A 2822 CONNECTOR DOUG DC10 DC1010 3022110 WP BOOST PUMP BURNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 385FE 46619 NR 1 FUEL TANK AFT BOOST PUMP POS, CONNECTOR IS BURNED. R&R WIRE HARNESS & BOOST PUMP HOUSING PER MM 28-22-01-02. 2 L 7 3 4F A22WE 2002091200040 20020912 00040 WP 2002 9 12 02FDEA00615 1 20020904 A 2822 60847 CONNECTOR DOUG DC10 DC1010 3022110 WP BOOST PUMP BURNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 385FE 46619 NR 1 FUEL TANK AFT BOOST PUMP CONNECTOR IS BURNED. R&R BOOST PUMP PER MM 28-22-01-2, OPS CHECK NORMAL. 2 L 7 3 4F A22WE 2002091200041 20020912 00041 EA 2002 9 12 02255633 1 20020911 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 633BR 7274 During the preflight inspection, the crew reported that the L/H aft exterior emergency light was inoperative. Maintenan ce personnel removed and replaced the lamp in the L/H aft exterior emergency light assembly. An operational check was s atisfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002091200042 20020912 00042 WP 2002 9 12 ABXA020080 1 20020821 A 2120 ODOR DOUG DC9 DC932 3022066 WP COCKPIT DETECTED A ABXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 902AX 47426 STRONG ELECTRICAL BURNING SMELL IN COCKPIT. VERIFIED SMELL. INSPECTED EPC, RELAY PANEL, E&E COMPARTMENT AND THE GYRO C OMPARTMENT. OPERATED PACK ONE AT A TIME. NO SMELL NOTED. 2 L 7 2 4F A6WE 2002091200043 20020912 00043 WP 2002 9 12 ABXA020081 1 20020819 A 7933 M057271 INDICATOR DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE COCKPIT DEFECTIVE A ABXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 847AX 46031 669243 NR 1 ENGINE OIL TEMP WENT TO 150 DEG CELSIUS FOR APPROXIMATELY 20 MINUTES. SECURED THE NR 1 ENGINE. ALL OTHER INDICATI ONS WERE NORMAL. REPLACED THE NR 1 ENGINE OIL TEMP BULB IAW DC-8 AMM 79-34-01-2 AND THE NR 1 ENGINE OIL TEMP GAUGE IAW DC-8 AMM 31-00-00-2. PERFORMED GROUND RUN OF THE NR 1 ENGINE IAW P/W MM 72-00. OPS CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 2002091200044 20020912 00044 NM 2002 9 12 ABXA020082 1 20020811 A 5320 145T8692 BRACKET BOEING 767 767200 1385120 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 767AX 22785 PANEL SPLICE TEE BRACKETS UNDER PANELS 139CL AND 139DL WERE FOUND TO BE CORRODED BEYOND LIMITS. REPAIRED AREA IAW REA B 653-44780. 2 L 7 2 4F RT A1NM 2002091200045 20020912 00045 WP 2002 9 12 ABXA020083 1 20020820 A 3210 57591015038N LANDING GEAR DOUG DC8 DC863 302198A WP RT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 RIGHT MAIN LANDING GEAR WAS CORRODED IN THE FORWARD ATTACH LUG. REPLACED THE RIGHT MAIN LANDING GEAR. 2 L 7 4 4F 4A25 2002091200046 20020912 00046 NM 2002 9 12 ABXA020084 1 20020409 A 5320 451T2504U22 PANEL BOEING 767 767281 1385109 NM FUSLEAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 CORRODED SHEAR PANEL BETWEEN STATIONS 544-610, LEFT BUTT LINE - RIGHT BUTT LINE - 20. REPLACED PANEL IAW B767 AMM. 2 L 7 2 4F RT A1NM 2002091200047 20020912 00047 NM 2002 9 12 ABXA020085 1 20020516 A 5311 143T106013 FRAME BOEING 767 767200 1385120 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 DEEP CORROSION ON UPPER CHORD AT STATION 544. REPLACED UPPER CHORD IAW B767 AMM. 2 L 7 2 4F RT A1NM 2002091200048 20020912 00048 NM 2002 9 12 ABXA020086 1 20020516 A 5311 143T1060U15 FRAME BOEING 767 767200 1385120 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 DEEP CORROSION ON UPPER CHORD AT STATION 720, BETWEEN RIGHT BUTT LINE 45 - LEFT BUTT LINE 45. REPLACED UPPER CHORD IAW B767 AMM. 2 L 7 2 4F RT A1NM 2002091200049 20020912 00049 NM 2002 9 12 ABXA020087 1 20020409 A 5311 143T1060U1 FRAME BOEING 767 767200 1385120 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 CRACK AND DEEP CORROSION ON UPPER CHORD AT STATION 676, RIGHT BUTT LINE 45. REPLACED T-CHORD IAW B767 AMM. 2 L 7 2 4F RT A1NM 2002091200050 20020912 00050 NM 2002 9 12 ABXA020089 1 20020408 A 5320 451T250441 PANEL BOEING 767 767200 1385120 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 CORRODED SHEAR PANEL BETWEEN STATIONS 566 - 610, LEFT BUTT LINE 35 - 45. REPLACED PANEL IAW B767 AMM. 2 L 7 2 4F RT A1NM 2002091200051 20020912 00051 WP 2002 9 12 ABXA020093 1 20020617 A 5312 56453325 DOUBLER DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 RIGHT WHEEL WELL UPPER PRESSURE DECK REPAIR DOUBLER EXFOLIATED ABOVE LONGERON 24, FS 879. REPAIRED AREA IAW ABX REA D85 3-43932-MR. 2 L 7 4 4F 4A25 2002091200052 20020912 00052 WP 2002 9 12 ABXA020096 1 20020618 A 5312 56453325 PRESSURE PANEL DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 MAIN CABIN, STATION 857 TO 880, BUTT LINE 0, CORROSION FOUND UNDER FINGER DOUBLER AND UNDER CABLE SUPPORT BRACKET. REPA IRED AREA IAW REA D853-43928-MR. 2 L 7 4 4F 4A25 2002091200053 20020912 00053 WP 2002 9 12 ABXA020098 1 20020708 A 5720 FITTING DOUG DC8 DC863 302198A WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 RIGHT WING STATION 219, FLAP LINK SUPPORT (CANOE) WAS CORRODED AND PITTED UNDER AFT TRACK PLATES. REMOVED CORROSION FRO M FLAP LINK SUPPORT FITTING AND FABRICATED REPAIR FILLERS IAW DC-8 SERVICE BULLETIN 27-164. REMOVED CORROSION FROM LEFT AND RIGHT SIDE SUPPORT HOLES, FABRICATED AND INSTALLED REPAIR BUSHINGS IAW REA D827-43940-MR. 2 L 7 4 4F 4A25 2002091200054 20020912 00054 WP 2002 9 12 ABXA020099 1 20020711 A 5330 SKIN DOUG DC8 DC863 302198A WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 L1 DOOR FORWARD LOWER AND AFT CORNER REPAIRS. REPAIRED AREA IAW ABX REA D853-43922-MR, DC-8 SRM 53-2-0, 51-1-20D, 51-1- 21, AND 51-3-0. 2 L 7 4 4F 4A25 2002091200055 20020912 00055 NM 2002 9 12 ABXA020101 1 20020720 A 3213 161T20041 BUSHING BOEING 767 767200 1385120 NM RT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784AX 41044 23017 RIGHT MAIN LANDING GEAR LOWER AFT SIDE STRUT, LOWER FORWARD BUSHING WAS CORRODED. REPLACED THE RIGHT MAIN LANDING GEAR LOWER AFT SIDE STRUT IAW BOEING B767 MM 32-11-05. 2 L 7 2 4F RT A1NM 2002091200056 20020912 00056 WP 2002 9 12 ABXA020102 1 20020617 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 RIGHT NOSE TUNNEL STATION 32, FRAME WAS CRACKED. FABRICATED NEW FRAME AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 53-3-1, 53-2-0, AND 51-1-8. 2 L 7 4 4F 4A25 2002091200057 20020912 00057 WP 2002 9 12 ABXA020106 1 20020618 A 5320 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 AFT ACCESSORY COMPARTMENT LONGERON END FITTING CRACKED AT FS 1690, LONGERON 32 LEFT. FABRICATED LONGERON AND FRAME REPA IRS, INSTALLED REPAIRS IAW DC-8 SRM 53-2-0, 53-2-2, 51-1-8, 51-1-20D, 51-3-0, AND REA D853-43934-MR. 2 L 7 4 4F 4A25 2002091200058 20020912 00058 WP 2002 9 12 ABXA020109 1 20020616 A 5320 4610355 FITTING DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 AIR COND/PRESS COMPARTMENT BETWEEN FS 56-70, LONGERON 36, END FITTING WAS CORRODED. REPLACED END FITTING IAW DC-8 SRM 5 1-1-20D. 2 L 7 4 4F 4A25 2002091200059 20020912 00059 WP 2002 9 12 ABXA020111 1 20020617 A 5315 FLOORBEAM DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 FORWARD CARGO TEE CHORD AT FS 70 WAS CORRODED BETWEEN LONGERON 29 LEFT - LONGERON 31 LEFT. FABRICATED REPAIR DOUBLER AN D REPAIRED AREA IAW DC-8 SRM 51-1-27 AND REA D853-43935-MR. 2 L 7 4 4F 4A25 2002091200060 20020912 00060 2002 9 12 ABXA020115 4 20020820 A 2565 101623303 SLIDE BOEING 767 767200 1385120 NM L1 DOOR UNSERVICEABLE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 790AX 582 23140 EMERGENCY ESCAPE SLIDE ON L1 DOOR HAD NO PRESSURE. REPLACED THE EMERGENCY ESCAPE SLIDE ON L1 DOOR IAW B767 AMM 25-66-01 -4. 2 L 7 2 4F RT A1NM 2002092400060 20020924 00060 NM 2002 9 24 CALA0200458 1 20020911 A 5320 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 INSPECTION FOUND A .5 INCH CRACK IN STIFFENER ACROSS BOTTOM OF FLOORBEAMS AT STA 328, RBL 45, WL 201. A DOUBLER WAS INS TALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2002092400061 20020924 00061 NM 2002 9 24 CALA0200459 1 20020911 A 5320 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 INSPECTION FOUND A .5 INCH CRACK IN STIFFENER ACROSS BOTTOM OF FLOORBEAMS AT STA 312, RBL 36, WL 201. THE CRACK WAS STO P DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2002092400062 20020924 00062 NM 2002 9 24 CALA0200460 1 20020911 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 INSPECTION FOUND A .5 INCH CRACK IN CABIN FLOOR VERTICAL WEB AT STA 1016, LBL 26 BELOW STRAP. A REPAIR WAS INSTALLED IA W SRM 51-40-00. 2 L 7 2 4F RT A16WE 2002091200061 20020912 00061 NM 2002 9 12 02FDEA00617 1 20020830 A 5313 STRINGER BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 FOUND STR 27 RT CRACKED IN INBOARD RADIUS AT BS 1111-1116. REMOVED AND REPLACED STRINGER PER SRM 51-40-4. 2 L 7 3 4F RT A3WE 2002091200062 20020912 00062 NM 2002 9 12 02FDEA00618 1 20020830 A 5230 STRUCTURE BOEING 727 727100 1384036 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CRACK AT AFT CARGO AFT LWR CORNER 4TH FASTENER FROM CORNER OF DOOR CUTOUT. REMOVED AND REPLACED CARGO DOOR PER SRM 51 -10-7. 2 L 7 3 4F RT A3WE 2002091200063 20020912 00063 NM 2002 9 12 02FDEA00619 1 20020830 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CRACKS NOTED IN FASTENER HOLES 5 EA AT BS 610-614, STR 3L IN ALL LAYERS EXCEPT INNERMOST AND FILTER. REMOVED AND REPLAC ED FASTENER HOLES PER EA 7-5330-65875. 2 L 7 3 4F RT A3WE 2002091200064 20020912 00064 NM 2002 9 12 02FDEA00620 1 20020830 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CRACKS NOTED IN FASTENER HOLE AT BS 488, STR 3L, AFT HOLE OF FILLER IN ALL LAYERS INCLUDING FILLER, EXCEPT INNERMOST SKI N CRACKS ENDS MARKED. REMOVED AND REPLACED FASTENER HOLES PER EA 7-5330-65875. 2 L 7 3 4F RT A3WE 2002091200065 20020912 00065 2002 9 12 ABXA020116 4 20020822 A 2565 SPRING BOEING 767 767200 1385120 NM PAX DOOR OUT OF POSITION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 790AX 23140 DOOR SLIDE ARMING HANDLE WAS DIFFICULT TO ARM. TOOK THREE ATTEMPTS TO RECYCLE MAIN DOOR TWO TIMES. FOUND EVACUATION SL IDE GIRT BAR AFT SPRING OUT OF POSITION. REPOSITIONED SPRING AS REQUIRED. OPS CHECKED NUMEROUS TIMES IAW B767 AMM. OP S CHECKED GOOD. 2 L 7 2 4F RT A1NM 2002091200066 20020912 00066 NM 2002 9 12 ABXA020117 1 20020822 A 2560 GIRT BAR BOEING 767 767200 1385120 NM PAX DOOR OBSTRUCTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 GIRT BAR WOULD NOT ARM ON MAIN CABIN DOOR. REMOVED TAPE FROM THE MAIN ENTRANCE DOOR GIRT BAR. OPS CHECKED GOOD IAW B76 7 AMM CHAPTER 52. 2 L 7 2 4F RT A1NM 2002091200067 20020912 00067 NM 2002 9 12 ABXA020119 1 20020826 A 3231 LATCH BOEING 767 767281 1385109 NM NLG DOOR DIRTY A ABXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 23 784AX 23017 UPON DEPARTURE, WHEN LANDING GEAR WAS RAISED, A LOUD NOISE WAS HEARD AND A LARGE AMOUNT OF VIBRATION WAS FELT. LANDING GEAR WAS EXTENDED AND THREE GREEN INDICATED. AIRCRAFT LANDED UNEVENTFULLY. FOUND LEFT FORWARD NOSE LANDING GEAR DOOR O PEN. MANUALLY CLOSED DOOR AND DISCOVERED DOOR NOT LATCHING PROPERLY. INSPECTED DOOR CLEARANCE AND FORWARD STOP CLEARAN CE. FOUND TO BE WITHIN LIMITS. DISCOVERED EXCESSIVE DIRT AND LUBRICANT ON DOOR LATCHING MECHANISM. CLEANED AND LUBED DOOR MECHANISM. MANUALLY OPENED AND CLOSED DOOR AND GOT POSITIVE LOCK EACH TIME IAW B767 AMM 32-22-02. 2 L 7 2 4F RT A1NM 2002091200068 20020912 00068 WP 2002 9 12 ABXA020120 1 20020826 A 3350 5708458503 BATTERY PACK DOUG DC8 DC863F 302198F WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 814AX 1114 46041 EMERGENCY LIGHTS WERE VERY DIM. REPLACED EMERGENCY LIGHTS BATTERY PACK IAW DC-8 AMM 33-50-01-2. 2 L 7 4 4F 4A25 2002091200069 20020912 00069 WP 2002 9 12 ABXA020121 1 20020827 A 3260 LIGHT DOUG DC9 DC932 3022066 WP COCKPIT CORRODED A ABXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 986AX 47543 UPON GEAR EXTENSION, NOSE LANDING GEAR LIGHT WOULD NOT ILLUMINATE. AFTER GEAR WAS RECYCLED, THE NOSE GEAR LIGHT ILLUMIN ATED. FOUND MINOR CORROSION ON THE NOSE LANDING GEAR INDICATION LIGHT. REPLACED THE NOSE LANDING GEAR INDICATION LIGHT BULBS. PERFORMED GEAR SWING IAW DC-9 MM 32-60-00. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002091200070 20020912 00070 WP 2002 9 12 ABXA020122 1 20020827 A 3397 WIRE DOUG DC9 DC932 3022066 WP COCKPIT DISCONNECTED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 981AX 47273 CAPTAIN'S YOKE CLIPBOARD LIGHT WAS INOPERATIVE. SHORTED OUT WITH SPARKING AND THEN THE LIGHT BLEW. RECONNECTED THE CEN TER WIRE ON THE CLIPBOARD RHEOSTAT. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2002091200071 20020912 00071 WP 2002 9 12 ABXA020123 1 20020823 A 7830 5958782503 LINK DOUG DC9 DC914 3022034 WP THRUST REVERSER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 2469 45728 NR 2 LOWER AFT LEFT THRUST REVERSER DRIVER LINK WAS CRACKED. REPLACED THE NR 2 LOWER LEFT DRIVE LINK IAW DC-9 MM 78-31- 05-2-0001, NEA 7830001, TASK NEA 13435, AD 75-14-06, AD 96-10-11, AND SERVICE BULLETIN 78-66. 2 L 7 2 4F A6WE 2002091200077 20020912 00077 NM 2002 9 12 02FDEA00555 1 20020805 A 5311 FRAME BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 CORROSION CIRCUMFERENTIAL CHORD CORRODED AT BS 351 BETWEEN STR 26L AND 26R. 2 L 7 3 4F RT A3WE 2002091200079 20020912 00079 NM 2002 9 12 02FDEA00576 1 20020812 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE LIGHTNING STRIKE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 LIGHTNING STRIKE LWR FUSELAGE AT BS 181, STR 19R. 2 L 7 3 4F RT A3WE 2002091200085 20020912 00085 NM 2002 9 12 02FDEA00589 1 20020813 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE LIGHTNING STRIKE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 LIGHTNING STRIKE ON OUTER SKIN AT BS 401, STR 10R. REMOVED AND REPLACED SKIN PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 2002091200094 20020912 00094 NM 2002 9 12 F3LA200200250 1 20020821 A 3610 32145525 SHUTOFF VALVE BOEING 737 73736N 1384408 NM NR 2 ENGINE FAILED A F3LA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 306FL 17260 2535 28563 AIR TURNBACK. FLIGHT CREW REPORTED WING/BODY OVERHEAT ILLUMINATED IN FLIGHT. COMPLIED WITH CHECKLIST AND LIGHT REMAINE D ILLUMINATED. PRESSURE IN RT DUCT 10 PSI, WHICH DECREASED TO 5 PSI WHEN THRUST LEVER REDUCED IN POWER. SHUT DOWN NR 2 ENGINE AND MONITORED OIL PRESSURE. REPLACED M237 MODULE AND NR 2 ENGINE PRSOV. PERFORMED OVERWEIGHT LANDING INSPECTIO N PER MM 05-51-74, PHASE I. NO DAMAGE NOTED. PERFORMED OPERATIONAL TESTS AND CHECKED OKAY. 2 L 7 2 4F RT A16WE 2002091200102 20020912 00102 WP 2002 9 12 IXXA0200050O 1 20020819 A 2910 O-RING DOUG DC8 DC862 3021970 WP HYD SYSTEM DAMAGED A IXXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 11 21CX 70934 1300 45955 AFTER TAKEOFF FROM COF, THE FLIGHT CREW NOTICED A DROP IN THE HYDRAULIC QUANTITY AND THE OIL LOW LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND RETURNED TO COF FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCR AFT AND LOCATED A DAMAGED O-RING ON THE LEFT HAND AILERON PACK FILTER BOWL CHIP PLUG. MAINTENANCE REPLACED THE O-RING A ND PERFORMED A SUCCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SER VICE. 2 L 7 4 4F 4A25 2002091200103 20020912 00103 GL 2002 9 12 P5CA0200695 1 20020807 A 5330 SKIN BOEING 747 747300 GL FUSELAGE DAMAGED A P5CA K NONE O OTHER TO TAKEOFF 1 WP 23 354MC 23394 UPON WALKAROUND IN ANC, FOUND THAT AIRCRAFT TAIL HAD APPARENTLY MADE GROUND CONTACT DURING TAKEOFF FROM ICN, CAUSING DAM AGE TO APU ACCESS DOORS TO BULKHEAD 2764. APPARENT CAUSE: TAKEOFF SPEED LOWER THAN THAT REQUIRED FOR ACTUAL TOGW. PERF ORMED INTERIM REPAIR TO FUSELAGE BOTTOM TAIL SECTION & INTERIOR FUSELAGE SKIN PER EDA 5161E001. 2 L 7 4 4F RT A20WE 2002091200104 20020912 00104 NM 2002 9 12 ABXA020127 1 20020703 A 5311 146T138447 FRAME BOEING 767 767200 1385120 NM FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 FUSELAGE STATION 1540 FRAME OUTER CHORD DAMAGE BETWEEN STRINGER 10 LEFT AND STRINGER 11 LEFT AT HORIZONTAL FLANGE. REPA IRED DAMAGED AREA IAW REA B653-43564-MR. 2 L 7 2 4F RT A1NM 2002091200105 20020912 00105 NM 2002 9 12 ABXA020129 1 20020712 A 5320 STRAP BOEING 767 767200 1385120 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 FUSELAGE SKIN TEAR STRAP WAS CORRODED AT STATION 742, BUTT LINE 0, BETWEEN STRINGER 39 LEFT TO STRINGER 39 RIGHT, UNDER SHEAR TIE, AFTER BLENDED OUT, FOUND REMAINING THICKNESS OUT OF LIMITS. REPAIRED AREA IAW REA B653-43559-MR. 2 L 7 2 4F RT A1NM 2002091200106 20020912 00106 NM 2002 9 12 ABXA020133 1 20020712 A 5311 143T15902 FAILSAFE BOEING 767 767200 1385120 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 FAIL-SAFE STRAP LOCATED AT STATION 539, BETWEEN STRINGER 31 RIGHT TO STRINGER 32 RIGHT FORWARD CARGO DOOR. CORROSION WA S FOUND ON FAIL-SAFE. REPAIRED AREA IAW REA B653-43524. 2 L 7 2 4F RT A1NM 2002091200107 20020912 00107 NM 2002 9 12 DHL2002727010 1 20020909 A 3350 1000679 LIGHT BOEING 727 727228 1384083 NM A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 727DH 20204 1) MAIN ENTRY EMERGENCY EXIT LT. INOP. 2) REMOVED AND REPLACED LT. ASSY PER B-727 M/M 33-50-101. OP CHECKS GOOD. 2 L 7 3 4F RT A3WE 2002091200108 20020912 00108 NM 2002 9 12 ABXA020141 1 20020714 A 5230 146T63341 SKIN BOEING 767 767200 1385120 NM CARGO DOOR GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 GOUGE IN 146T6334-1 BULK CARGO DOOR INNER SKIN, STATION 1439, WATER LINE 131. REPAIRED AREA IAW REA B652-43447-MR. 2 L 7 2 4F RT A1NM 2002091200109 20020912 00109 NM 2002 9 12 ABXA020142 1 20020712 A 2710 251T15154 CONTROL QUADRANT BOEING 767 767200 1385120 NM AILERON DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 AILERON CONTROL QUADRANT ASSEMBLY, FOUND DAMAGE AT BEARING SEAT. REPAIRED AREA IAW REA B627-43542-MR. 2 L 7 2 4F RT A1NM 2002091200110 20020912 00110 WP 2002 9 12 ABXA020145 1 20020828 A 3260 SWITCH DOUG DC9 DC931 3022065 WP LT MLG DOOR FAULTY A ABXA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 23 924AX 47403 ON FINAL APPROACH, GEAR DOOR OPEN LIGHT WOULD NOT EXTINGUISH. RECYCLED GEAR AND LIGHT STILL DID NOT GO OUT. EXTENDED G EAR LIGHT ON AT FLAPS 15 DEGREES. WHEN FLAPS 25 DEGREES SELECTED, LIGHT WENT OUT. EXECUTED MISSED APPROACH. CONFIGURE D TO EXT/15 DEGREES GEAR UP WITH NORMAL INDICATIONS. ON NEXT APPROACH, ALL INDICATIONS WERE NORMAL. FOUND LEFT MAIN LA NDING GEAR DOOR SWITCH BAD. REPLACED THE DOOR SWITCH. OPS CHECKED GOOD IAW DC-9 MM 32-60-03. 2 L 7 2 4F A6WE 2002091200111 20020912 00111 WP 2002 9 12 ABXA020146 1 20020828 A 3230 BRACKET DOUG DC9 DC931 3022065 WP RT MLG OUT OF ADJUST A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 908AX 47008 AFTER TAKEOFF WITH GEAR HANDLE UP, THE RIGHT GEAR RED UNSAFE LIGHT ILLUMINATED. RECYCLED THE GEAR WITH NO CHANGE. THE GEAR UPLATCH CHECK ALSO FAILED. ADJUSTED THE TENSION ON THE RIGHT MAIN GEAR DOOR ROLLER BRACKET AND SPRING ASSEMBLY IAW DC-9 MM 32-31-04-2-0103. ALSO CHECKED AND RIGGED THE RIGHT LANDING GEAR DOOR LATCH TORQUE TUBE IAW DC-9 MM 32-31-04-2- 1003. CYCLED THE GEAR THREE TIMES. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002091200112 20020912 00112 WP 2002 9 12 ABXA020149 1 20020828 A 2710 2642425 BEARING DOUG DC8 DC861 3021952 WP AILERON BROKEN A ABXA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 23 853AX 46037 AILERONS WERE VERY DIFFICULT TO TURN TO THE LEFT WITH HYDRAULIC POWER ON. REPLACED THE RIGHT AILERON REVERSION MECHANIS M BEARING ASSEMBLY FOR TAB LOCKOUT IAW DC-8 OVERHAUL MANUAL 27-6-2. PERFORMED TEST OF REVERSION MECHANISM IAW DC-8 MM 2 7-11-08. NO DISCREPANCIES NOTED. OPS CHECKED GOOD. MANUAL REVERSION ROLLER BEARING WAS BROKEN IN HALF ON THE RIGHT AI LERON POWER PACK. 2 L 7 4 4F 4A25 2002091200113 20020912 00113 WP 2002 9 12 ABXA020151 1 20020829 A 3260 DOWNLOCK SWITCH DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A ABXA O OTHER O OTHER AP APPROACH 1 GL 23 986AX 47543 INITIAL LANDING GEAR EXTENSION, NOSE GEAR GREEN LIGHT EXTINGUISHED. RECYCLED GEAR FOR DOWN AND LOCKED. NOSE GEAR GREEN LIGHT ILLUMINATED AS NORMAL. REPLACED THE NOSE LANDING GEAR DOWNLOCK SWITCH AND THROTTLE TRANSFER RELAY, NO HELP. REP LACED THE NOSE LANDING GEAR DOWNLOCK LIGHT ASSEMBLY. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2002091200114 20020912 00114 WP 2002 9 12 ABXA020152 1 20020830 A 3260 LATCH DOUG DC9 DC931 3022065 WP RT MLG OUT OF ADJUST A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 908AX 47008 RIGHT GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. UPLATCH CHECK FAILED (GEAR DOOR OPEN LIGHT CAME ON AND GEAR EXTENDED). WHEN THE GEAR HANDLE WAS PLACED IN UP POSITION, RIGHT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT WENT OUT. RIGHT GEAR RETRACTED NORMALLY. ADJUSTED AND TESTED RIGHT MAIN GEAR DOOR LATCH MECHANISM IAW DC-9 MM 32-31-04. OPS CHEC KED GOOD. 2 L 7 2 4F A6WE 2002091200115 20020912 00115 NE 2002 9 12 ABXA020153 2 20020903 A 7200 JT3D7 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 MALFUNCTIONED A ABXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 814AX 541 46041 669191 NR 4 ENGINE LOW OIL PRESSURE LIGHT CAME ON ACCOMPANIED BY AN OIL PRESSURE FLUCTUATION AND QUANTITY DECREASING. ENGINE W AS SECURED AND OIL PRESSURE WAS BELOW 5 PSI WITH ENGINE WINDMILLING AT 30 PERCENT N2 FOR REMAINED OF FLIGHT. REPLACED T HE NR 4 ENGINE. RUN UP/TRIM CHECK IAW DC-8 A/B. 2 L 7 4 4F 4 F 4A25 1E8 2002091200116 20020912 00116 WP 2002 9 12 ABXA020157 1 20020624 A 5712 SS0957000318 RIB DOUG DC9 DC931 3022065 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 NR 8 SLAT TRACK INBOARD LEADING EDGE RIB ANGLE COMMON TO ROLLERS CRACKED AT AFT LOWER VERTICAL LEG. REPLACED RIB IAW DC -9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002091200117 20020912 00117 WP 2002 9 12 ABXA020159 1 20020625 A 5312 SB09530166285 BULKHEAD DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 AFT PRESSURE BULKHEAD SIDE SKIN SPLICED AT Z 14.00. SPLICE NOT IAW DOUGLAS AFT PRESSURE BULKHEAD RE-WORK. SPLICED NEW SECTION (LOWER) OF RIGHT AFT PRESSURE BULKHEAD WEB IAW REA D953-44534-MR AND DOUGLAS DWG J060088. 2 L 7 2 4F A6WE 2002091200118 20020912 00118 WP 2002 9 12 ABXA020160 1 20020706 A 5320 49125151 CAP DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 LONGERON END CAP CRACKED NR 11 RIGHT. INSTALLED NEW END CAP NR 11 RIGHT IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002091200119 20020912 00119 WP 2002 9 12 ABXA020161 1 20020702 A 5320 99105033 ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 LONGERON 18L CUSP ANGLE FS 980, CORRODED AND CRACKED. REPAIRED CUSP ANGLE IAW REA D953-44535. 2 L 7 2 4F A6WE 2002091200120 20020912 00120 WP 2002 9 12 ABXA020164 1 20020702 A 5320 991050315 WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 RIGHT CUSP CRACKED AT STATION 937. REPAIRED AREA IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002091200121 20020912 00121 WP 2002 9 12 ABXA020165 1 20020702 A 5310 591008515 ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 BOTTOM OF SERVICE DOOR CUTOUT, INNER JAMB ANGLE EXFOLIATED, LONGERON 18 RIGHT. REPLACED JAM ANGLE AND REPAIRED AREA IAW DC-9 SRM 51-30-5 AND 51-10-3. 2 L 7 2 4F A6WE 2002091200122 20020912 00122 WP 2002 9 12 ABXA020166 1 20020717 A 5753 5910041503 VANE DOUG DC9 DC941 302207N WP T/E FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 LARGE AREA OF DELAMINATION IN LEFT FIXED VANE ABOVE INBOARD FLAP HINGE. SKIN INSIDE THE SAME AREA HAD A DEEP CHAFE AT A PPROXIMATELY STATION 137.7. REPLACED LEFT INBOARD FLAP FIXED VANE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002091200123 20020912 00123 WP 2002 9 12 ABXA020167 1 20020718 A 5313 592480215 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 LONGERON 17 CRACKED AT FS 256. REPLACED SECTION OF LONGERON 17 RIGHT, STATION 230 - 268 IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2002091200124 20020912 00124 WP 2002 9 12 ABXA020170 1 20020723 A 5280 5910557503 DOOR DOUG DC9 DC941 302207N WP LT MLG CHAFED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LEFT MAIN LANDING GEAR OUTBOARD DOOR CHAFED ON INNER FORWARD LIP AND UNDER ARTICULATING DOOR COUNTER BALANCE ARM. REPLA CED THE LEFT MAIN LANDING GEAR OUTBOARD DOOR AIW DC-9 MM. 2 L 7 2 4F A6WE 2002091200125 20020912 00125 WP 2002 9 12 ABXA020171 1 20020723 A 2761 59242731 BRACKET DOUG DC9 DC941 302207N WP SPOILER CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 SPOILER - ACTUATOR MIXER BRACKET WAS CORRODED AND PITTED IN NUMEROUS PLACES. REPLACED MIXER BRACKET IAW DC-9 MM. 2 L 7 2 4F A6WE 2002091200126 20020912 00126 WP 2002 9 12 ABXA020173 1 20020724 A 5521 5910412523 SPAR DOUG DC9 DC941 302207N WP ELEVATOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 UNREPAIRED CRACKS NOTED ON LEFT ELEVATOR FRONT SPAR .625 INCH LONG AT XE 174.5 AND .75 INCH AT XE 172.5. INSTALLED NEW ELEVATOR IAW DC-9 MM. 2 L 7 2 4F A6WE 2002091200127 20020912 00127 WP 2002 9 12 ABXA020174 1 20020814 A 5280 4925884201 HINGE DOUG DC9 DC941 302207N WP RT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 RIGHT MAIN LANDING GEAR INBOARD DOOR HINGE WAS CRACKED. REMOVED AND REINSTALLED RIGHT MAIN LANDING GEAR DOOR FOR HINGE CHANGE IAW DC-9 MM 32-12-01-2-02-01 AND SRM 51-30-1, 51-30-5, AND 52-05. 2 L 7 2 4F A6WE 2002091200128 20020912 00128 WP 2002 9 12 ABXA020175 1 20020814 A 5320 39248461 ANGLE DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 EXFOLIATED ANGLE ON OUTBOARD END OF SLANT PANEL. REPLACED ANGLE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002091200129 20020912 00129 WP 2002 9 12 ABXA020176 1 20020814 A 5320 991150060AX INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 INTERCOSTAL JUST BELOW RIGHT RADOME HINGE WAS CRACKED AT CUTOUT. REPLACED INTERCOSTAL AND INSTALLED FASTENERS IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002091200130 20020912 00130 WP 2002 9 12 ABXA020177 1 20020816 A 5320 99107555 WEB DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 CUSP WEB WAS CRACKED AT STATION 1041, LONGERON 18 LEFT. REPLACED CUSP WEB IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002091200131 20020912 00131 NM 2002 9 12 02FDEA00621 1 20020904 A 2781 SWITCH BOEING 727 727200 138407E NM L/E FLAP FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 479FE 21461 DURING FLAP RETRACTION FROM 15 TO 5 L/E FLAP INDICATOR WENT FROM GREEN TO AMBER. S/O LED POSITION INDICATORS SHOWED NR 6 LED RETRACTED. CYCLING FLAPS CHANGED NOTHING. LANDED WITH FLAPS 30 WITH A L/E FLAP AMBER WITH NR 6 INDICATING RETRAC TED. REPLACED NR 6 LEADING EDGE FLAP POSITION INDICATING SWITCH IAW M/M 27-82-001-4. OPS CHECKS GOOD. 2 L 7 3 4F RT A3WE 2002091200132 20020912 00132 NM 2002 9 12 02FDEA00622 1 20020904 A 3260 656021127 MODULE BOEING 727 727200 138407E NM LANDING GEAR FAULTY A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 275FE 22040 LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED ON TAKEOFF AFTER GEAR RETRACTION. CYCLED GEAR PER QRH. ALL GEAR EXTENDED N ORMALLY, BUT LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER RETRACTION. FLIGHT CONTINUED PER QRH WITH GEAR HANDLE IN THE UP POSITION. PERFORMED NORMAL GEAR RETRACTION FOR LANDING GEAR INDICATING AND WARNING SYSTEM PER 727-200 MM 32-61- 001-5 COULD NOT DUPLICATE THE PROBLEM. REMOVED AND INSTALLED THE LANDING GEAR ELECTRICAL/ELECTRONIC MODULE PER 727-200 MM 32-09-121-4. OPS CHECKED SAME PER 727-200 MM 32-09-121-5 AND 32-61-001-5, NO DEFECTS NOTED. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2002091200133 20020912 00133 NM 2002 9 12 02FDEA00623 1 20020905 A 5270 BZ2RQ18A2 SWITCH BOEING 727 727100 1384036 NM CARGO DOOR FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 189FE 19082 AIRPLANE DIVERTED TO TPA. MAIN CARGO DOOR WARNING ON S/O'S ANNUNCIATOR CAME ON IN FLIGHT. REPLACED LOCK BAR CLOSED SWI TCH PER M/M 52-34-009-5. OPS CHECK OK. 2 L 7 3 4F RT A3WE 2002091200134 20020912 00134 NM 2002 9 12 02FDEA00624 1 20020906 A 7710 WARNING LIGHT BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 495FE 21669 LOUD BOOM & AIRFRAME SHUDDER EXPERIENCED ON CLIMBOUT, AUTOPACK TRIP ACTIVATED. ENGINE FAIL LIGHT BLINKED MOMENTARILY, B UT STAYED OUT. SUSPECT COMPRESSOR STALL BUT UNABLE TO IDENTIFY ENG. ALL ENG INSTRUMENTS NORM. BORESCOPED ENGINES 1, 2 , 3 PER MM 72-00-00-1. NO DAMAGE BEYOND MM LIMITS WAS NOTED. ENG RUN WAS COMPLIED WITH, ALL CHECK OK. 2 L 7 3 4F 4 F RT A3WE E2EA 2002091200135 20020912 00135 NM 2002 9 12 02FDEA00625 1 20020905 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 SKIN CHAFED AT BS 720D+10, STR 19R. 2 L 7 3 4F RT A3WE 2002091200136 20020912 00136 NM 2002 9 12 02FDEA00626 1 20020905 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 CHAFING ON SKIN LAP BS 720D PLUS 10 STR 19L. R&R SKIN PER SRM 53-30-3 FIG 14 & DWG SR 27-57-056. 2 L 7 3 4F RT A3WE 2002102800125 20021028 00125 NM 2002 10 28 02FDEA00627 1 20020905 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 STR 15L IS CRACKED AT BS 720B+16. R&R STRINGER PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 2002091200137 20020912 00137 NM 2002 9 12 02FDEA00628 1 20020904 A 5320 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 STR CLIP CRACKED AT BS 660, STR 7L. R&R STRINGER CLIP PER SRM 51-30-2, 51-30-5. 2 L 7 3 4F RT A3WE 2002091200138 20020912 00138 NM 2002 9 12 02FDEA00629 1 20020904 A 5320 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 STRINGER CLIP CRACKED AT BS 660, STR 9L. R&R STRINGER CLIP PER SRM 51-30-2, 51-30-5. 2 L 7 3 4F RT A3WE 2002091200139 20020912 00139 NM 2002 9 12 02FDEA00630 1 20020904 A 5320 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 STRINGER CLIP CRACKED AT BS 660, STR 6L. R&R STRINGER CLIP PER SRM 51-30-2, 51-30-5. 2 L 7 3 4F RT A3WE 2002091200140 20020912 00140 WP 2002 9 12 02FDEA00631 1 20020905 A 5743 ARB06421 SUPPORT DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FOUND HFEC DISCONTINUITY IND ON MLG RETRACT CYLINDER SUPPORT FRAME. R/R FRAME PER E.O. 8-5740-7-4312C PART 4 (REF N 6 S EQ 0009). 2 L 7 3 4F A22WE 2002091200141 20020912 00141 NM 2002 9 12 02FDEA00632 1 20020904 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 208FE 22930 GOUGE IN FRAME BS 348, LBL 44, WL 281. 2 L 7 3 4F RT A3WE 2002091200142 20020912 00142 NM 2002 9 12 02FDEA00633 1 20020906 A 3260 189915 SENSOR BOEING 727 727200 138407E NM RT MLG FAILED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 477FE 21394 DURING TAKEOFF ROLL THE RIGHT GEAR RED LIGHT CAME ON AFTER GEAR RETRACTION THE RED GEAR LIGHT REMAINED ON WITH ALL OTHER GEAR LIGHTS EXTINGUISHED (GEAR WAS RE-CYCLED). REPLACED RT MAIN GEAR UPLOCK SENSOR PER M/M 32-61-081-4. ALSO REPLACED THE LANDING GEAR ACCESSORY UNIT PER M/M 32-09-121-4. ALL CHECKS OK. 2 L 7 3 4F RT A3WE 2002091200143 20020912 00143 NM 2002 9 12 02FDEA00634 1 20020907 A 2170 COALESCER BAG DOUG MD11 MD11 3023602 NM A/C BAY DIRTY A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 584FE 48436 AFTER FLAP RETRACTION GOT SMOKE IN THE COCKPIT, WENT ON OXYGEN, DECLARED EMERGENCY AND RETURNED TO NRT. SMOKE GRADUAL LY DISSIPATED OVER ABOUT 15 MIN. OPENED ALL 3 ENGINES AND CHECKED FOR OIL LEAKS IN PNEUMATIC SYSTEM, NO LEAKS FOUND. R EMOVED AND REPLACED ALL 3 A/COND WATER SEPARATOR BAGS MM:21-54-01. ALSO CHECKED APU BLEED SYSTEM FOR OIL LEAKS AND NONE FOUND. REMOVED ALL 6 DU`S, NO EVIDENCE FOR OVERHEATING. ALSO CHECKED AVIONICS COMPT FOR POSSIBLE SHORTS AND NONE FOUND . THEN RAN ALL 3 ENGINES WITH ALL BLEEDS ON AND NO ODOR FOUND. 2 L 7 3 4F RT A22WE 2002102800126 20021028 00126 EU 2002 10 28 02FDEA00636 1 20020911 A 5330 A5361056723500 SKIN AIRBUS 310 A310 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 INNER FACE OF FUSELAGE SKIN CORRODED IN AVIONICS COMPT BETWEEN FRAME 16, 16A AND 17 OUTBOARD OF STRINGER 44R AND BETWEEN FRAME 16A AND 17, INBD OF STR 44R. R&R SKIN DOUBLER PER EA 6-5330-65-65906. 2 L 7 2 4F RT A35EU 2002091200144 20020912 00144 EU 2002 9 12 02FDEA00637 1 20020901 A 5230 A52378014204 SKIN AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 676FE 790 TWO INCHES FROM FWD EDGE OF HANDLE OF BULK CARGO DOOR HANDLE CUTOUT GOUGED. 2 L 7 2 4F RT A35EU 2002091200145 20020912 00145 NM 2002 9 12 02FDEA00638 1 20020803 A 5711 7178T6 SPAR BOEING 727 727200 138407E NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 127FE 19719 RIGHT REAR SPAR CHORD CRACKED APPROX BS 200. 2 L 7 3 4F RT A3WE 2002091200147 20020912 00147 NM 2002 9 12 AWXA200200841 1 20020827 A 2780 65448736 SWITCH BOEING 737 737277 1384570 NM L/E SLAT DEFECTIVE A AWXA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 28 188AW 59666 13338 22655 AFTER TAKEOFF NR 5 SLAT REMAINED IN EXTENDED POSITION, DECLARED EMERGENCY, TURNED BACK. MX INSPECTED AND LUBRICATED NR 5 L/E SLAT ROD ENDS & TRACKS IAW BMM 12-22-71. CYCLED FLAPS SEVERAL TIMES, OPERATIONAL CHECK WAS NORMAL. MX WROTE A CRI TICAL FOLLOW-UP TO LUBRICATE ALL L/E DEVICES AND REPLACED NR 5 SLAT ACTUATOR. MX LUBRICATED L/E SLAT TRACKS, MAIN / AUX ILIARY TRACK ROLLERS, AND REPLACED NR 5 L/E SLAT ACTUATOR IAW R3M27020, PROBLEM STILL EXISTS. ISOLATED PROBLEM TO DEFEC TIVE NR 5 L/E SLAT ACTUATOR ROD END SWITCH, REPLACED ROD END (REED) SWITCH IAW T/C R3M27019, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002091200148 20020912 00148 NE 2002 9 12 HAEA00037 2 20020811 A 7200 ENGINE LEAR 24 24B 5170306 CE GE CJ610 CJ6106 30006 NE RIGHT DAMAGED E HAEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 233TW 24B221 251772A PILOT REPORTED NORMAL DEPARTURE FROM KSHV, DURING CLIMB RT ENGINE FIRE WARNING CAME ON AT 10,000FT. CREW SHUTDOWN ENGIN E AND RETURNED TO KSHV FOR UNEVENTFUL LANDING. DURING TROUBLESHOOTING FOR ENGINE FIRE LIGHT MAINTENANCE DISCOVERED FOD DAMAGE. REMOVED AND REPLACED ENGINE. 2 L 7 2 4J 4 J A10CE 1E16 2002091200149 20020912 00149 CE 2002 9 12 HAEA00038 1 20020827 A 2420 OH1030115 CONTROL BOX LEAR 24 24D 5170311 CE GENERATOR FAULTY E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 299TW 24D299 ACFT DEPARTED KYIP CLIMBING OUT OF 6,000 FOR 13,000 YAW DAMPER STARTED KICKING OFF, OFF FLAGS CAME IN TO VEIW ON BOTH PI LOT AND CO-PILOT SIDES AND THE SECONDARY INVERTER LIGHT FLASHED. PRIMARY VOLT METER NEEDLE WAS TICKING ALONG WITH AMP N EEDLE FOR GENERATOR. MAINTENANCE REMOVED AND REPLACED GENERATOR CONTROL BOX, OPS CHECK NORMAL. ACFT RETURNED TO SERVIC E. 2 L 7 2 4J A10CE 2002091200150 20020912 00150 EU 2002 9 12 HAEA00039 1 20020904 A 2131 133007 CONTROLLER AMD FALC20 FALCON 2720302 EU CABIN PRESSURE FAILED E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 240TW 40 AIRCRAFT DEPARTED KOKC FOR KLRD, LEAVING 5,500 FT CABIN CONTINUED TO CLIMB, DIVERTED TO KADS FOR MAINTENANCE. REMOVED A ND REPLACED CABIN ALTITUDE CONTROLLER, PERFORMED OPERATION CHECKS AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F A7EU 2002091200151 20020912 00151 CE 2002 9 12 HAEA00040 1 20020906 A 3411 STATIC LINE LEAR 24 24 5170302 CE PITOT/STATIC SYS KINKED E HAEA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 222TW 24161 AIRCRAFT DEPARTED KYIP CLIMBING THROUGH 2,000 FT ALTIMETER PILOT SIDE LOCKED UP. RETURNED TO DEPARTURE AIRPORT FOR MAIN TENANCE. FOUND STATIC LINE KINKED, REPAIRED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4J A10CE 2002091200152 20020912 00152 CE 2002 9 12 HAEA00041 1 20020909 A 3260 SQUAT SWITCH LEAR 25 25B 5170511 CE LANDING GEAR OUT OF ADJUST E HAEA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SW 05 666TW 116 AIRCRAFT DEPARTED ADS FOR MFE, CLIMBING OUT, CABIN ALTITUDE CLIMBED WITH AIRCRAFT. RETURNED TO DEPARTURE AIRPORT FOR MA INTENANCE. ADJUSTED RT SQUAT SWITCH, AIRCRAFT OPS CHECK GOOD AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4J A10CE 2002091200153 20020912 00153 WP 2002 9 12 ABXA020179 1 20020731 A 5230 593410437 CLIP DOUG DC9 DC941 302207N WP FWD. CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 BEAM #5 TEE FITTING AT FORWARD END WAS CRACKED. REPLACED THE #5 TEE IAW DC-9 SRM 51-30-5 AND 51-30-4. 2 L 7 2 4F A6WE 2002091200154 20020912 00154 WP 2002 9 12 ABXA020181 1 20020801 A 5320 991050313 WEB DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 RIGHT CUSP WEB CRACKED BEWTEEN F.S. 1021 AND 1041. REPAIRED CUSP WEB IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002091200155 20020912 00155 WP 2002 9 12 ABXA020182 1 20020801 A 5312 49125401 SPLICE DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 LEFT SIDE F.S. 1041 BULKHEAD FITTING WAS CRACKED. REPLACED FITTINGS IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2002091200156 20020912 00156 WP 2002 9 12 ABXA020184 1 20020802 A 5312 591013060 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 AFT PRESSURE BULKHEAD CRACKED ON RIGHT SIDE OF VENTRAL DOORWAY APPROXIMATELY 36" UP FROM FLOOR. REPAIRED AREA IAW DC-9 S RM 53-05. 2 L 7 2 4F A6WE 2002091200157 20020912 00157 WP 2002 9 12 ABXA020185 1 20020804 A 5312 49125391 SPLICE DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 PYLON BULKHEAD ATTACH FITTING AT STA. 1041, LEFT BUTT LINE 30, WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002091200158 20020912 00158 WP 2002 9 12 ABXA020186 1 20020806 A 5200 591412159 PAN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 CRACK IN FORWARD ENTRY DOOR ABOVE FORWARD LOWER STOP PAD. REPLACED DOOR IAW DC-9 MM. 2 L 7 2 4F A6WE 2002091200159 20020912 00159 WP 2002 9 12 ABXA020187 1 20020807 A 5400 991550032 CLIP DOUG DC9 DC941 302207N WP RT. ENG. PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 LOWER BOLT HOLE WAS CRACKED AT #2 ENGINE AFT MOUNT. REPLACED ANGLE IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002091200160 20020912 00160 WP 2002 9 12 ABXA020195 1 20020812 A 5200 59101575 PAN DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 AFT LOWER CARGO DOOR HAD CRACKED INTERIOR DOOR STOP FITTING AT AFT UPPER CORNER. REPLACED AFT LOWER CARGO DOOR ON N.R. # 0350 IAW DC-9 MM. 2 L 7 2 4F A6WE 2002091200161 20020912 00161 WP 2002 9 12 ABXA020196 1 20020812 A 5200 59101575 PAN DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 FORWARD END OF AFT LOWER CARGO DOOR HAD CRACKED PANES AT DOORSTOP CUTOUT AT BEAMS 1, 2, AND 3. REPLACED DOOR ON N.R. #03 50 AND IAW DC-9 MM. 2 L 7 2 4F A6WE 2002091200162 20020912 00162 WP 2002 9 12 ABXA020198 1 20020812 A 5200 59101575 PAN DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 AFT LOWER CARGO DOOR INNER PAN WAS CRACKED NEAR FORWARD LATCH HOOK AT ROLLER CUTOUT. REPLACED AFT LOWER CARGO DOOR ON N. R. #0350 AND IAW DC-9 MM. 2 L 7 2 4F A6WE 2002091200163 20020912 00163 WP 2002 9 12 ABXA020199 1 20020813 A 5230 3926046501 FITTING DOUG DC9 DC941 302207N WP FWD. CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 FORWARD LOWER CARGO DOOR AFT STOP FITTING AT END OF INTERCOSTAL CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30 -5. 2 L 7 2 4F A6WE 2002091200164 20020912 00164 WP 2002 9 12 ABXA020200 1 20020813 A 5300 995766437 FORMER DOUG DC9 DC941 302207N WP FWD. CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 FORWARD LOWER CARGO DOOR, LOWER FORWARD STOP INTERCOSTAL FORMER WAS CRACKED. REPLACED BRACKET IAW DC-9 SRM 51-30-1 AND 5 1-30-2. 2 L 7 2 4F A6WE 2002091200165 20020912 00165 WP 2002 9 12 ABXA020203 1 20020829 A 5400 991550032 CLIP DOUG DC9 DC941 302207N WP #1 ENG. PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 #1 PYLON ATTACH ANGLE INSIDE PANEL 8111 AT UPPER AFT ENGINE MOUNT STRAP HAD CRACK NEXT TO BOLT. REPLACED ANGLE IAW DC-9 DWG 9915500 AND DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002091200166 20020912 00166 NM 2002 9 12 AWXA200200876 1 20020902 A 5230 654795217 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A 3/8" CRACK WAS FOUND ON THE AFT CARGO DOOR INNER SKIN AT THE CENTER ACCESS OPEN ING JUST BELOW THE HANDLE, BS 787-847. MAINTENANCE BLENDED OUT CRACK ON THE AFT CARGO DOOR INNER SKIN AT THE CENTER ACCE SS OPENING JUST BELOW THE HANDLE IAW B737-200 SRM 52-00-2, FIG. 1, PG. 1-4A. HFEC ISNPECTION VERIFIED CRACK NO LONGER EX ISTS. 2 L 7 2 4F RT A16WE 2002091200167 20020912 00167 NM 2002 9 12 AWXA200200877 1 20020902 A 5320 6546544547 WEB BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A 1/2" CRACK WAS FOUND ON VERTICAL WEB AT BS 695, LBL 58-62, WL 206. MAINTENANCE REMOVED DAMAGED VERTICAL WEB AT BS 695, LBL 58-62, WL 206. FABRICATED A NEW VERTICAL WEB AND WEB SPLICE, AND INSTALLED R EPAIR PARTS IAW DWG 65-41544-547, AND B737-200 SRM 51-40-2, PG. 1-3, FIG. 1. 2 L 7 2 4F RT A16WE 2002091200168 20020912 00168 NM 2002 9 12 AWXA200200878 1 20020907 A 5220 MPP171700LH CABLE AIRBUS A319 A319132 3930340 NM ZONE 844 - DOORS MALADJUSTMENT A AWXA O OTHER L S NO TEST AFFECT SYSTEMS IN INSP/MAINT 1 WP 28 812AW 0 0 1178 MCN - EMERGENCY ESCAPE SYSTEM - DURING B-02 CHECK THE L/H OVER WING EMERGENCY ESCAPE EXIT RELEASE CABLE FAILED TEST. MAI NTENANCE ADJUSTED FLEXIBLE CONTROL CABLE ASSEMBLY IAW AMM 25-62-43-420-050, STEP A(9) B, AND STEP 11; TEST WAS GOOD IAW AWA T/C F1C52303. 2 L 7 2 4F RT A28NM 2002091200169 20020912 00169 EU 2002 9 12 AWXA200200880 1 20020911 A 3320 325070 BALLAST AIRBUS 320 A320231 3930325 EU SEAT ROW 17 L/H DEFECTIVE A AWXA K NONE O OTHER CR CRUISE 1 WP 28 624AW 0 0 55 PHX - BURNING SMELL - FLT 0534 - EN ROUTE FROM SAN TO PHX AN ACRID BURNING SMELL WAS NOTICED IN PROXIMITY OF SEAT ROW 17 L/H. MAINTENANCE FOUND CEILING LIGHT BALLAST BAD ABOVE SEAT ROW 17 L/H, REPLACED CEILING LIGHT BALLAST ASSEMBLY IAW AMM 33-21-09, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002091200170 20020912 00170 NM 2002 9 12 AWXA200200881 1 20020901 A 5330 659187912 SKIN BOEING 737 737277 1384570 NM -N/A- CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A 1" CRACK WAS FOUND ON OUTER SKIN NEAR THE R/H MAIN LANDING GEAR WHEEL WELL KEEL BEAM AREA, BETWEEN 2 REPAIR DOUBLERS, BS 707. MAINTENANCE REMOVED DAMAGED SECTION OF OUTER SKIN, FABRICATED A SECTION O F KEEL BEAM OUTER SKIN AND 3 EACH REPAIR DOUBLERS, AND INSTALLED REPAIR PARTS IAW AWA E.R. 15-5315-02247-TB2. 2 L 7 2 4F RT A16WE 2002091300001 20020913 00001 EU 2002 9 13 DHL2002262516 1 20020802 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-CHECK, LT MLG DOOR CUTOUT ON THE AFT SIDE FR 53 STR 41 HAS A GOUGE WITH A PIECE OF SKIN MISSING ON THE EDGE. TRIMMED OUT DAMAGED AREA IN THE SKIN IAW A300 SRM 51-41-10. EDDY CURRENT INSPECTED AREA PER NTM 51-31-05, NO CRACKS FOUND. FAB RICATED REPAIR DOUBLER AND FILLER IAW A300 SRM 51-41-10. INSTALLED REPAIR IAW FIG 1 AND A300 SRM 51-30-30. 2 L 7 2 4F RT A35EU 2002091300002 20020913 00002 EU 2002 9 13 DHL2002362006 1 20020830 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE OUT OF POSITION A DHLA K NONE N FALSE WARNING UK UNKNOWN 1 SO 01 362DH 84 ENGINE NR 2 LOOP-A LIGHT ILLUMINATED INTERMITTENTLY IN LIGHT TURBULENCE. OPENED NR 2 ENGINE, REPOSITIONED A-LOOP. PERF ORMED ENGINE NR 2 -A- AND -B- LOOP TEST. GROUND OPS CHECKED GOOD. UNABLE TO DUPLICATE ON GROUND. 2 L 7 2 4F RT A35EU 2002091300003 20020913 00003 EU 2002 9 13 DHL2002362007 1 20020904 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 PYLON DEFECTIVE A DHLA K NONE N FALSE WARNING UK UNKNOWN 1 SO 01 362DH 84 NR 2 ENGINE -A- FIRE LOOP FLICKERS INTERMITTENTLY ON S/O PANEL WITH LOOP FLICKERING ON THE MWP. T/S AND FOUND PYLON LOO P EXCESSIVELY HIGH OHMS. INSTALLED NEW PYLON DETECTORS AND OPS CHECKED OK PER 26-12-12. 2 L 7 2 4F RT A35EU 2002091300004 20020913 00004 EU 2002 9 13 DHL2002362008 1 20020906 A 2612 CONNECTOR AIRBUS 300 A300B4203 3930306 EU NR 3 ENGINE LOOSE A DHLA K NONE N FALSE WARNING UK UNKNOWN 1 SO 01 362DH 84 ENGINE 2 FIRE DETECTION LOOP -A- LIGHT ILLUMINATES INTERMITTENTLY. ABNORMAL PERFORMED. FOUND LOOSE CONNECTOR ON ENGINE CORE LOOP. CLEANED AND RESECURED LOOP CONNECTOR. GROUND CHECKED AS PER MM 26-12-00, OPS NORMAL. 2 L 7 2 4F RT A35EU 2002091300005 20020913 00005 WP 2002 9 13 MWEA020515 1 20020826 A 5230 99576644N INTERCOSTAL DOUG DC9 DC915 3022036 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FORWARD CARGO DOOR HAS A CRACKED INTERCOSTAL OUTBOARD OF LOWER AFT STOP FITTINGS BELOW BEAM 1. LOCATED AND DRILLED INTE RCOSTAL. REMOVED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2002091300006 20020913 00006 WP 2002 9 13 MWEA020516 1 20020827 A 5320 99155549 INTERCOSTAL DOUG DC9 DC915 3022036 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FORWARD CARGO COMPARTMENT HAS LIGHT CORROSION ON INTERCOSTAL AT STA 218-237 BETWEEN LONGERON 28R-27R. DRILLED UP NEW IN TERCOSTAL, REMOVED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2002091300007 20020913 00007 WP 2002 9 13 MWEA020538 1 20020905 A 5321 9910078170 FLOORBOARD DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FLOORBOARD ATTACH FASTENERS HOLES ARE LIGHTLY CORRODED ON J-CHANNEL BETWEEN STATIONS 160 AND 200 FORWARD OF SEAT TRACK 4 . REMOVED CORROSION AND INSTALLED FLOOR SUPPORT. 2 L 7 2 4F A6WE 2002091300008 20020913 00008 NE 2002 9 13 NACA20020037 2 20020819 A 8530 356993 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 3 ENGINE CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 779TA 1169 1169 45529 36210 FEATHERED THE NR 3 ENGINE AT 0312Z DUE TO BACKFIRING AND ROUGH RUNNING. REPLACED THE NR 4 CYLINDER. 2 L 7 4 4R 4 R A781 5E8 2002091300009 20020913 00009 NE 2002 9 13 NACA20020038 2 20020821 A 8530 356996 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE NR 3 ENGINE DEFECTIVE A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 99330 703 703 43576 P33821 SHUTDOWN THE NR 3 ENGINE DUE TO DOUBLE SHORTED SECONDARY CYLINDER NR 11 AND DOUBLE SHORTED SECONDARY CYLINDER NR 15. RE MOVED AND REPLACED THE NR 11 AND NR 15 CYLINDERS. 2 L 7 4 4R 4 R 6A3 5E8 2002091300010 20020913 00010 NE 2002 9 13 NACA20020039 2 20020828 A 8530 356993 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 4 ENGINE CRACKED A NACA E D ENGINE SHUTDOWN RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 AL 03 779TA 971 971 45529 NK510318 NR 4 ENGINE FEATHERED DUE TO BACKFIRING. REMOVED AND REPLACED THE NR 18 CYLINDER. 2 L 7 4 4R 4 R A781 5E8 2002091300011 20020913 00011 NE 2002 9 13 NACA20020040 2 20020831 A 8530 356994 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 4 ENGINE CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 779TA 235 235 45529 NK510318 FEATHERED THE NR 4 ENGINE IN CRUISE DUE TO BACKFIRED, LOW BMEP. REPLACED THE NR 3 CYLINDER. 2 L 7 4 4R 4 R A781 5E8 2002091300012 20020913 00012 NE 2002 9 13 NACA20020041 2 20020831 A 7420 IGNITION LEAD DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 3 ENGINE SHORTED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 43872 540 540 533294 P32204 PRECAUTIONARY SHUTDOWN THE NR 3 ENGINE DUE TO DOUBLE SHORTED SECONDARY ON THE NR 10 CYLINDER. REPLACED SPARK PLUGS, Y-L EAD, SHORT LEADS, AND COIL. 2 L 7 4 4R 4 R A781 5E8 2002091300013 20020913 00013 NM 2002 9 13 PCAA0208096 1 20020821 A 3350 FUSE DHAV DHC8 DHC8102 2809003 NM POWER SUPPLY BLOWN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT RIGHT AFT EMERGENCY LIGHT ON FUSELAGE AND EMERGENCY LIGHT IN CENTER CABIN CEILING FOUND INOPERATIVE. FUSE REPLACED IN AFT EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2002091300014 20020913 00014 NM 2002 9 13 PCAA0208097 1 20020821 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 DURING ROUTINE MAINTENANCE VISIT RIGHT SIDEWALL AND RIGHT FLOOR LEVEL EMERGENCY LIGHTS FOUND INOPERATIVE. RESECURED LOO SE CONNECTOR FOR RIGHT FLOOR LIGHT AND REPLACED FUSES IN BATTERY BOX FOR SIDEWALL LIGHT. OPERATIONAL CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091300015 20020913 00015 NM 2002 9 13 PCAA0208098 1 20020824 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST NR NOT REPORTED 1 EA 13 820EX 019 MHT- FLIGHT 3758. CREW REPORTED FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE FROM 4A TO 9A LEFT SIDE. MAINTENANCE RESECURE D CONNECTIONS NEAR ROW 4 AND ROW 9. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091300016 20020913 00016 NM 2002 9 13 PCAA0208099 1 20020825 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DISCONNECTED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT AFT HALF OF LEFT EMERGENCY FLOOR PATH LIGHTING FOUND INOPERATIVE. CIRCUIT FOUND DISCON NECTED AT AFT PLUG. THE CONNECTION WAS RESECURED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091300017 20020913 00017 NM 2002 9 13 PCAA0209101 1 20020906 A 2530 RECEPTACLE DHAV DHC8 DHC8102 2809003 NM GALLEY SHORTED A PCAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 13 815EX 321 ROC-LGA FLIGHT 3905. CREW REPORTED DURING DESCENT NOTICED A SMOKE ODOR IN COCKPIT AND GALLEY AREA. MAINTENANCE INSPECT ED AND FOUND NR 2 HOT JUG RECEPTACLE SHORTED OUT. RECEPTACLE AND HOT JUG REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091300018 20020913 00018 NM 2002 9 13 PCAA0209103 1 20020905 A 3350 JUMPER DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 DURING ROUTINE MAINTENANCE VISIT FLOOR LEVEL EMERGENCY LIGHTS FROM ROW 7 TO ROW 1 ON RIGHT SIDE, AND ROW 5 TO ROW 7 LEFT SIDE FOUND INOPERATIVE. EMERGENCY LIGHT BATTERIES REMOVED TO REPLACE FUSES, BATTERIES THEN REINSTALLED. ALL JUMPER LE ADS CHECKED. JUMPERS THAT WERE FOUND LOOSE WERE RESECURED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091300019 20020913 00019 NM 2002 9 13 PCAA0209105 1 20020911 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT EMERGENCY AISLE LIGHTS FOUND INOPERATIVE AT AFT LEFT SIDE OF AIRCRAFT. THREE CONNECTOR S WERE FOUND TO BE LOOSE. CONNECTORS WERE RESECURED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091300020 20020913 00020 SO 2002 9 13 SWIA200211137 1 20020819 A 5753 PLATE EMB 120 EMB120ER 3260203 SO T/E FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 291SW 120318 LEFT NACELLE FLAP HAS CRACK O/B PLATE AT STIFFENER LOWER. REPLACED NACELLE FLAP. 2 L 7 2 4T RT A31SO 2002091300021 20020913 00021 2002 9 13 SWIA200211138 4 20020819 A 3160 6229810016 DISPLAY CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 407SW 7034 CAPTAIN'S MFD FAILED INFLIGHT. RETURNED TO SLC. INSTALLED SERVICEABLE MFD SCREEN AT CAPTAIN'S POSITION. OPS CHECKS GO OD. 2 L 7 2 4F RT A21EA 2002091300022 20020913 00022 EA 2002 9 13 SWIA200211140 1 20020820 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 406SW 7030 AFTER SELECTION OF WING ANTI-ICE NORM, RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE. COMPLIED WITH QRH AND RETURNED TO SLC . RAN AIRCRAFT ANTI-ICE SYSTEM. COULD NOT DUPLICATE. SYSTEM OPERATES NORMAL. 2 L 7 2 4F RT A21EA 2002091300023 20020913 00023 SO 2002 9 13 SWIA200211141 1 20020819 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 199SW 4742 1617 120237 ON DESCENT INTO ELKO, RIGHT NACELLE WOULD NOT EXTEND PAST 15 DEGREES WITH CONTROL FAULTS. AFTER LANDING, ALL FLAPS RETR ACTED. THEREAFTER, RIGHT NACELLE FLAP WOULD NOT WORK, CAUSING FLAP ASYMMETRY. REMOVED AND REPLACED NACELLE FLAP ACTUAT OR. REMOVED AND REPLACED FLAP CONTROL BOX. OPS & LEAK CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002091300024 20020913 00024 2002 9 13 SWIA200211142 4 20020814 A 3425 6226190204 COMPARATOR EMB 120 EMB120ER 3260203 SO NR 1 MALFUNCTIONED A SWIA A UNSCHED LANDING I J FLT. ATTITUDE INST. WARNING INDICATION CL CLIMB 1 NM 07 295UX 3903 1228 120295 AT 70 PERCENT NP, CAPTAIN'S AHARS GOES BLANK, THEN RETURNS WITH HDG FLAG AND COMPASS CARD 30 DEGREES OFF THE HEADING. R ETURNED OT SAN. REPLACED NR 1 AHC-85. PERFORMED REORIENTATION PROCEDURE. RAN LEFT AND RIGHT ENGINES THROUGH 70 PERCEN T NP, AUX GENS ON AND OFF, CAPTAIN'S EHSI AND EADI CHECK GOOD. OPS CHECKS GOOD, COMPASS CARDS AND HEADING MATCH SIDE TO SIDE. 2 L 7 2 4T RT A31SO 2002091300025 20020913 00025 2002 9 13 SWIA200211143 4 20020817 A 3414 320AS1 INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 268UE 5352 5352 120207 ON THE TAKEOFF ROLL AT ABOUT 70 KIAS, RECEIVED A HI SPEED WARNING WITH A TRIPLE CHIME. ABORTED TAKEOFF. INSTALLED SERV ICEABLE AIRSPEED INDICATOR ON CAPTAIN'S SIDE. GROUND OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002091300026 20020913 00026 2002 9 13 SWIA200211144 4 20020819 A 3425 6226190204 COMPUTER EMB 120 EMB120ER 3260203 SO NR 1 MALFUNCTIONED A SWIA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 NM 07 268UE 5391 5113 120207 AUTOPILOT DID AN UNCOMMANDED ROLL TO THE LEFT WHEN SELECTED TO CAPTAIN'S SIDE. DISENGAGED AND RE-ENGAGED AUTOPILOT AND IT HAPPENED AGAIN. CAPTAIN'S FLIGHT DIRECTOR COMMANDED MULTIPLE UNWANTED PITCH CHANGES WHILE IN LEVEL FLIGHT (AUTOPILOT WAS NOT ENGAGED). TRIED TO RE-ENGAGE AUTOPILOT LATER IN FLIGHT AND IT WOULD NOT ENGAGE. REPLACED NR 1 AHRS. SYSTEM O PS CHECKS GOOD IAW 22-10-00 AND 34-21-00. 2 L 7 2 4T RT A31SO 2002091300027 20020913 00027 SO 2002 9 13 SWIA200211145 1 20020817 A 2121 COOLING FAN EMB 120 EMB120ER 3260203 SO E/E BAY SEIZED A SWIA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 196SW 120151 ON TAXI OUT THERE WAS A SMOKE SMELL IN THE CABIN AND THE LAV SMOKE DETECTOR WENT OFF. FOUND AVIONICS COOLING FAN SEIZED . REMOVED AND REPLACED FAN IAW EMB MM 21-27-02. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002091300028 20020913 00028 SO 2002 9 13 SWIA200211146 1 20020818 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 296SW 120325 ONE RED LIGHT OF FORWARD PAIR OF FLOOR EMERGENCY LIGHTS IS INOP. RELAMPED FORWARD EMERGENCY FLOOR LIGHT AS REQUIRED. O PS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002091300029 20020913 00029 EA 2002 9 13 SWIA200211147 1 20020820 A 4960 21188002 ECU CNDAIR CL600 CL6002B19 1900309 EA APU FAULTY A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 413SW 865 865 7102 ON DESCENT TO IAH DURING APU START, RECEIVED AN APU FIRE FAIL STATUS MESSAGE, FOLLOWED BY AN APU FIRE WARNING MESSAGE. PUSHED THE APU FIRE SWITCH AND RECEIVED NO FIRE INDICATIONS AFTER THAT. RAN QRH AND RECEIVED APU FAULT MESSAGE. FOUND EXCESSIVE OIL FROM THE OVERSERVICED APU. ALSO FOUND APU DOOR WILL NOT OPEN. REPLACED APU ECU. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002091300030 20020913 00030 EA 2002 9 13 SWIA200211148 1 20020819 A 3020 300013000003 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA RT COWLING FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 439SW 8 8 7578 RIGHT COWL ANTI-ICE FAILED EN ROUTE. DIVERTED TO GJT DUE TO WEATHER. REMOVED AND REPLACED RIGHT ENGINE COWL ANTI-ICE V ALVE WITH SERVICEABLE UNIT IAW MM 30-22-01. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002091300031 20020913 00031 EA 2002 9 13 SWIA200211149 1 20020818 A 3234 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A SWIA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 NM 07 416SW 23 23 7089 AFTER TAKEOFF, UPON GEAR RETRACTION, RECEIVED A GEAR DISAGREE WARNING WITH A LIGHT AERODYNAMIC BUFFET. RETURNED TO SLC. FOUND MLG NOT UPLOCKING ON UPLOCK HOOKS. REMOVED AND REPLACED MLG SELECTOR VALVE IAW MM 32-32-00. SWUNG GEAR. OPS C HECKS GOOD & LEAK CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002091300032 20020913 00032 NM 2002 9 13 P5CA0200698 1 20020828 A 7100 NONE GEARBOX BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE #1 ENGINE FAILED A P5CA E A ENGINE SHUTDOWN UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 WP 23 806FT 21827 702280 SHORTLY AFTER T/O, #1 ENG. LOW OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE DROPPED TO 10psi & WAS STEADY; OIL QTY SHOW ED FULL & WAS STEADY. PERFORMED LOSS OF OIL PRESSURE PROCEDURE IAW AFM. COULD NOT RESTORE ENG. OIL PRESSURE OR EXTINGU ISH LIGHT, THEREFORE A PRECAUTIONARY ENG. SHUTDOWN WAS PERFORMED IAW AFM. AFTER SHUTDOWN, OIL PRESSURE DROPPED TO ZERO & OIL TEMP ROSE TO 10 DEGREES ABOVE THE GREEN BAND. FLT RETURNED TO CAI WHERE ENG. PROBLEM WAS FOUND TO BE CAUSED BY GE ARBOX FAILURE. IT HAD BEGUN TO DISINTEGRATE INTERNALLY REQUIRING AN ENGINE CHANGE. 2 L 7 4 4F 4 F A20WE E3NE 2002091300033 20020913 00033 SO 2002 9 13 C2XA02CL181 1 20020912 A 2822 2C71 PUMP EMB 145 EMB145LR 3260212 SO WING FAILED A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 16981 7115 145208 CLE FLIGHT#3017 THE CREW REPORTED FUEL PUMP 1A FAILED IN FLIGHT.MAINTENANCE REPLACED THE FUEL PUMP.OPERATIONAL CHECKS WE RE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002102800129 20021028 00129 EU 2002 10 28 02FDEA00641 1 20020913 A 5330 A5361087322200 DOUBLER AIRBUS 310 A310 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 FWD LAVATORY SERVICING PANEL DOUBLER AT LEFT SIDE OF FUSELAGE BETWEEN FRAME 12 AND 12A IS CORRODED ALONG LWR EDGE. R&R FRAME DOUBLER PER EA 6-5330-65-65906. 2 L 7 2 4F RT A35EU 2002102800130 20021028 00130 EU 2002 10 28 02FDEA00642 1 20020913 A 5415 A5461175400000 FITTING AIRBUS 310 A310 EU LT PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 LT PYLON AFT MOUNT FITTING FOUND CORRODED. R&R FITTING PER SB A310-54-2021 ON PYLON STRUCTURE. 2 L 7 2 4F RT A35EU 2002091300034 20020913 00034 SO 2002 9 13 SWIA200211150 1 20020817 A 3230 12043270501 CONTROL BOX EMB 120 EMB120RT 3260202 SO LANDING GEAR MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 196CA 1216 1216 120196 LEFT LANDING RED LIGHTS REMAIN ON (A & B) WITH GEAR HANDLE SELECTED. INSTALLED SERVICEABLE LANDING GEAR RELAY BOX ASSY, SWUNG LANDING GEAR 35 PLUS TIMES. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002091300035 20020913 00035 EA 2002 9 13 SWIA200211151 1 20020819 A 3242 5010520 BRAKE ASSY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 4 MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 432SW 7548 ON TAKEOFF ROLL, RECEIVED ANTI-SKID INBOARD CAUTION MSG AND PERFORMED A LOW SPEED ABORT (60 KTS) APPLIED LITTLE BREAKING , BUT NR 4 BRAKE TEMP CLIMBED TO 7 WHILE THE REST REMAINED AT (2 OR 3 UNITS). CYCLED POWER OFF & ON. COMPLETED OPS CHE CK OF ANTI-SKID. OPS CHECK GOOD AT THIS TIME. REMOVED AND REPLACED NR 4 BRAKE. LEAK & OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002091300036 20020913 00036 SO 2002 9 13 SWIA200211152 1 20020820 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE T/E FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 199SW 5892 20 120237 ON APPROACH THE NACELLE FLAPS ARE INOP. REPAIRED WIRE W628-0007-22 BETWEEN P1869 & P0828. REMOVED AND REPLACED FLAP CO NTROL UNIT. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002091300037 20020913 00037 NE 2002 9 13 SWIA200211153 2 20020820 A 7321 FUEL CONTROL EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE OUT OF RIG A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 289YV 120289 RIGHT ENGINE EEC FAILED DURING TAKEOFF ROLL AT APPROX 100 KTS. ABORTED TAKEOFF. ADJUSTED RIGGING ON LEFT AND RIGHT ENG INES AND RETRIMMED DURING ENGINE RUNS. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002091300038 20020913 00038 EA 2002 9 13 SWIA200211154 1 20020824 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM DAMAGED A SWIA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 905SW 7437 RUDDER TRIM INOP. INSPECTED RUDDER TRIM CONTROL SWITCH PANEL. REPAIRED WIRE CONNECTION. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002091300039 20020913 00039 EA 2002 9 13 SWIA200211155 1 20020825 A 4990 1603662 OIL COOLER CNDAIR CL600 CL6002B19 1900309 EA APU FAULTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 720SW 3127 2670 7297 APU OIL TEMP INDICATION ILLUMINATED IN FLIGHT (20,000). RETURNED TO PHX. REPLACED APU OIL COOLER. OPS & LEAK CHECK GO OD. 2 L 7 2 4F RT A21EA 2002091300040 20020913 00040 2002 9 13 SWIA200211156 4 20020719 A 3451 ANTENNA EMB 120 EMB120ER 3260203 SO DME 2 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 DURING C-CHECK FOUND SEVERAL LOWER FUSELAGE ANTENNAS WITH CORROSION: MKR 1/TDR 1/ DME 2/ RADAR ALT/ TDR 2. REPLACED DM E AND MARKER BEACON ANTENNAS. FUNCTION CHECKED FOLLOWING SYSTEM: DME 1 & 2 IAW 34-51-00, ATC 1 & 2 IAW 34-52-00, MARKE R BEACON 1 & 2 IAW 34-55-00, RADIO ALTIMETER IAW 34-42-00, VHF 2 IAW 23-15-00. ALL SYSTEMS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002091300041 20020913 00041 SO 2002 9 13 SWIA200211157 1 20020719 A 5230 CABLE EMB 120 EMB120ER 3260203 SO CARGO DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 DURING C-CHECK, FOUND CABLES AND PULLEYS ON CARGO DOOR CORRODED. REMOVED AND REPLACED CABLES AND PULLEYS IAW 52-31-00. 2 L 7 2 4T RT A31SO 2002091300042 20020913 00042 SO 2002 9 13 SWIA200211158 1 20020719 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 DISCOVERED DURING C-CHECK, LEFT AND RIGHT FWD AND AFT WALL SEAT TRACKS ARE CORRODED. REMOVED AND REPLACED LEFT AND RIGH T FWD AND AFT WALL SEAT TRACKS IAW 53-01-05. 2 L 7 2 4T RT A31SO 2002091300043 20020913 00043 SO 2002 9 13 SWIA200211159 1 20020719 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 DISCOVERED DURING C-CHECK, LEFT AND RIGHT FWD FLOOR SEAT TRACKS ARE CORRODED. REMOVED AND REPLACED LEFT AND RIGHT FWD F LOOR SEAT TRACKS IAW 53-01-05. 2 L 7 2 4T RT A31SO 2002091300044 20020913 00044 SO 2002 9 13 SWIA200211160 1 20020719 A 5752 BUSHING EMB 120 EMB120ER 3260203 SO AILERON TAB CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 DISCOVERED DURING C-CHECK, LEFT AILERON TRIM TAB BUSHINGS AND HARDWARE ARE CORRODED. REMOVED AND REPLACED LEFT AILERON TRIM TAB BUSHINGS AND HARDWARE IAW 57-60-00. 2 L 7 2 4T RT A31SO 2002091300045 20020913 00045 SO 2002 9 13 SWIA200211161 1 20020719 A 5752 BUSHING EMB 120 EMB120ER 3260203 SO AILERON TAB CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 DURING C-CHECK, RIGHT AILERON TRIM TAB BUSHINGS AND HARDWARE ARE CORRODED. REMOVED AND REPLACED RIGHT AILERON TRIM TAB BUSHINGS AND HARDWARE IAW 57-60-00. 2 L 7 2 4T RT A31SO 2002091300046 20020913 00046 SO 2002 9 13 SWIA200211162 1 20020719 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 C-CHECK, LT NACELLE O/B SIDE FRAME 15 CRACKED. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON THE FRAME IAW EMB S RM 51-70-05 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002091300047 20020913 00047 SO 2002 9 13 SWIA200211163 1 20020719 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 FOUND DURING C-CHECK, LEFT NACELLE O/B SIDE FRAME 17 CRACKED. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON THE FRAME IAW EMB SRM 51-70-05 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002091300048 20020913 00048 SO 2002 9 13 SWIA200211164 1 20020719 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 FOUND DURING C-CHECK, LEFT NACELLE I/B SIDE FRAME 15 CRACKED. STOP-DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-40-02 AND 51-70-05. 2 L 7 2 4T RT A31SO 2002091300049 20020913 00049 SO 2002 9 13 SWIA200211165 1 20020719 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 FOUND DURING C-CHECK, RIGHT NACELLE I/B SIDE FRAME 16 CRACKED. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON THE FRAME IAW EMB SRM 51-70-05. 2 L 7 2 4T RT A31SO 2002091300050 20020913 00050 SO 2002 9 13 SWIA200211166 1 20020719 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 FOUND DURING C-CHECK, RIGHT SIDE NACELLE O/B SIDE FRAME 15 CRACKED. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EMB SRM 51-00-00 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002091300051 20020913 00051 SO 2002 9 13 SWIA200211167 1 20020719 A 5420 BRACKET EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 FOUND DURING C-CHECK, AT FRAME 13, THE BRACKET THAT HOLDS THE POWER POSITION PULLEY QUADRANT, RT NACELLE, I/B SIDE IS CR ACKED. REMOVED AND REPLACED THE CRACKED BRACKET AT FRAME 13, RT NACELLE IAW EMB SRM 51-00-00 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002091300052 20020913 00052 SO 2002 9 13 SWIA200211168 1 20020719 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 FOUND DURING C-CHECK, LEFT NACELLE FRAME ONE IS CRACKED AT THE I/B TORSION MOUNT. COMPLIED WITH S/B 120-54-0036 REV 2 N ACELLES - INSPECTION/REPLACEMENT OF NACELLE FRAME ONE. 2 L 7 2 4T RT A31SO 2002091300053 20020913 00053 SO 2002 9 13 SWIA200211169 1 20020719 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 FOUND DURING C-CHECK, RIGHT NACELLE FRAME NR 1 CRACKED. ACCOMPLISHED EMB S/B 120-54-0036 REV 2. C/W PART 1-2.2.1, 2.2. 2.1 THROUGH 2.2.3.8 & PART 2-2.3. 2 L 7 2 4T RT A31SO 2002091300054 20020913 00054 SO 2002 9 13 SWIA200211170 1 20020719 A 5320 INTERCOSTAL EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 FOUND DURING C-CHECK, INTERCOSTAL AFT OF PILOT'S SIDE WINDOW CRACKED. FABRICATED AND INSTALLED DOUBLER TO PART IAW EMB SRM 51-00-00 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002091300055 20020913 00055 SO 2002 9 13 SWIA200211171 1 20020719 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 FOUND DURING C-CHECK, RIGHT NACELLE FRAME -0- HAS SEVERAL CRACKS IN IT. REMOVED AND REPLACED FRAME -0- IAW SRM 51-40-02 . 2 L 7 2 4T RT A31SO 2002091300056 20020913 00056 EA 2002 9 13 SWIA200211172 1 20020824 A 5210 ROD CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 408SW 7055 AFTER DEPARTURE, AC WOULD NOT PRESSURIZE. F/A REPORTED CABIN DOOR VERY LOUD. RETURNED TO FIELD. REINSTALLED ROD ON DO OR PRESSURE VALVE IAW 52-11-15. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2002091300057 20020913 00057 EA 2002 9 13 SWIA200211173 1 20020824 A 2721 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 905SW 7437 RUDDER TRIM SWITCH STICKS NOSE RIGHT OR NOSE LEFT, DOES NOT SPRING BACK TO NEUTRAL. REMOVED AND REPLACED AILERON AND RU DDER CONTROL PANEL. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002091300058 20020913 00058 SO 2002 9 13 SWIA200211174 1 20020822 A 3231 LATCH EMB 120 EMB120ER 3260203 SO RT MLG OUT OF ADJUST A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 293SW 120320 NOTICED RIGHT MAIN GEAR INBOARD DOOR OPEN IN FLIGHT. RETURNED TO LAX. TIGHTENED AND ADJUSTED RIGHT MAIN GEAR INBOARD D OOR LATCH PIVOT BOLT. CYCLED GEAR DOORS SEVERAL TIMES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002091300059 20020913 00059 EA 2002 9 13 SWIA200211175 1 20020828 A 3260 SENSOR CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR MALFUNCTIONED A SWIA O OTHER N FALSE WARNING AP APPROACH 1 NM 07 407SW 7034 LANDING GEAR DISAGREE MESSAGE APPEARED WHEN LANDING GEAR WAS SELECTED DOWN. GEAR CAME DOWN AFTER MANUAL GEAR RELEASE WA S USED. AFTER LANDING, NOSE WHEEL STEERING WAS INOP. ADJUSTED NOSE LANDING GEAR PROX SENSORS UPLOCK, BOTH NR 1 & 2 DOW NLOCK, BOTH GEAR DOOR PROX SENSORS, NR 2 WOW SENSOR IAW CL600 MM 322-61-05. OPS CHECKED SEVERAL TIMES. OPS CHECKED GOO D. 2 L 7 2 4F RT A21EA 2002091300060 20020913 00060 SO 2002 9 13 SWIA200211176 1 20020828 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 223SW 120291 EMERGENCY LIGHTS WOULD NOT ILLUMINATE IN THE LAST THREE ROWS OF THE AIRCRAFT. REPLACED AFT EMERGENCY LIGHT BATTERY. OP S CHECKED GOOD. 2 L 7 2 4T RT A31SO 2002091300061 20020913 00061 EA 2002 9 13 SWIA200211177 1 20020828 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 594SW 7285 EMERGENCY EXIT ROW LIGHT ROW 2-5 INOP. EMERGENCY DOOR LIGHT INOP ROW 8 LEFT SIDE. REPLACED EMERGENCY LIGHT FLOOR STRIP FROM ROW 1 TO 7. ALL LIGHTS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002091300062 20020913 00062 EA 2002 9 13 SWIA200211178 1 20020827 A 2740 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT DIRTY A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 416SW 7089 PILOT'S TRIM SWITCH STICKS WHEN TRIMMING NOSE UP, WON'T TRIM. CLEANED TRIM SWITCH, OPS CHECK GOOD THROUGH SEVERAL CYCLE S. 2 L 7 2 4F RT A21EA 2002091300063 20020913 00063 EA 2002 9 13 SWIA200211179 1 20020825 A 1430 SCREW CNDAIR CL600 CL6002B19 1900309 EA WINDOW HEAT LOOSE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 417SW 7400 F/O'S WINDSHIELD HEAT IS SPARKING IN THE TERMINAL BOX. TIGHTENED UPPER TERMINAL SCREW. OPS CHECK OK. 2 L 7 2 4F RT A21EA 2002091300064 20020913 00064 SO 2002 9 13 SWIA200211180 1 20020821 A 3260 PLUNGER EMB 120 EMB120ER 3260203 SO MLG OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 561SW 120335 DEPARTING LAX ON GEAR RETRACTION, HAD INDICATION DISAGREEMENT. ALL GREEN LIGHTS OUT THEN ALL RED LIGHTS ON, THEN BOTH A &B LIGHT ON LEFT GEAR (RED) AND -B- ON RT GEAR WOULD NOT EXTINGUISH. COMPLIED WITH QRH. NO CHANGE & GEAR CYCLED DOWN W ITH 3 GREEN. RETURNED TO LAX. FOUND BOTH MAIN GEAR UPLOCK PLUNGERS OUT OF ADJUSTMENT. ADJUSTED PLUNGERS. SWUNG GEAR NUMEROUS TIMES. ALL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002091300065 20020913 00065 EA 2002 9 13 SWIA200211181 1 20020718 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 493SW 7450 DISCOVERED DURING C-CHECK, FS 625.30 STR 15L INTERCOSTAL ANGLE CRACKED. NEW INTERCOSTAL ANGLE INSTALLED IAW CRJ SRM 51- 40-11. 2 L 7 2 4F RT A21EA 2002091300066 20020913 00066 EA 2002 9 13 SWIA200211182 1 20020724 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 DISCOVERED DURING C-CHECK, FS 280.0 LBL 9.0 I/B & O/B FLOORBEAM ANGLES CRACKED. REMOVED ANGLES AND INSTALLED NEW ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21 DWG JK601R31101. 2 L 7 2 4F RT A21EA 2002091300067 20020913 00067 NM 2002 9 13 377PA0007 1 20020912 A 3350 58671 INVERTER BOEING 737 7373L9 1384470 NM A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 377PA 23718 Emergency floor path lighting inop at aprox. sta. 500C. Trouble shot & found inverter bad. R&R inverter IAW WDM 33-51- 41, Ops chk good. 2 L 7 2 4F RT A16WE 2002091300068 20020913 00068 EA 2002 9 13 SWIA200211183 1 20020724 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 DISCOVERED DURING C-CHECK, FS 280.0 RBL 9.0 I/B FLOORBEAM ANGLE CRACKED. REMOVED ANGLE AND INSTALLED NEW ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21 DWG JK601R31101. 2 L 7 2 4F RT A21EA 2002091300069 20020913 00069 SO 2002 9 13 SWIA200211184 1 20020829 A 2910 HYDRAULIC LINE EMB 120 EMB120ER 3260203 SO HYD SYSTEM CRACKED A SWIA O OTHER K FLUID LOSS AP APPROACH 1 NM 07 186SW 120034 DURING APPROACH, EXPERIENCED LOSS OF HYDRAULIC FLUID IN BLUE SYSTEM. FOLLOWED QRH, LANDED UNEVENTFULLY. FOUND CRACKED LINE IN RIGHT NACELLE. REMOVED AND REPLACED LINE. RAN ENGINES. LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2002091300070 20020913 00070 SO 2002 9 13 SWIA200211185 1 20020830 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 187SW 120037 FLOOR LIGHTING IN FRONT OF GALLEY NOT WORKING. REPAIRED BROKEN WIRE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002091300071 20020913 00071 EA 2002 9 13 SWIA200211187 1 20020827 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 408SW 7055 FLAP FAIL MESSAGE DURING PREFLIGHT. REMOVED AND REPLACED LEFT BPSU IAW 27-51-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002091300072 20020913 00072 EA 2002 9 13 SWIA200211188 1 20020831 A 2460 BUSS TIE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT DEFECTIVE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 427SW 7497 TURNING ON BATT MASTER, THE AROMA OF ELECTRICAL SMOKE EXISTED. NO CIRCUIT BREAKERS HAD POPPED. REPLACED BUSS TIE NR 2 CONTACTOR. TURNED ON BATT MASTER & RAN ALL SYSTEMS. NO SMOKE AROMA NOTED. 2 L 7 2 4F RT A21EA 2002091300073 20020913 00073 WP 2002 9 13 ABXA020205 1 20020826 A 5300 5939711502 ANGLE DOUG DC9 DC931 3022065 WP VERT STAB L/E DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 RIGHT DORSAL FIN ATTACH ANGLE HAD TOOLING DAMAGE IN THE RADIUS. REPLACED DORSAL FIN ATTACH ANGLE IAW DC-9 SRM 51-30-1, 5 1-30-2, 51-30-5, AND REA D953-44887. 2 L 7 2 4F A6WE 2002091300074 20020913 00074 2002 9 13 SWIA200211189 4 20020901 A 2210 6229968001 DAMPER CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 435SW 7555 YAW DAMPER NR 2 INOP. REMOVED AND REPLACED NR 2 YAW DAMPER IAW 22-22-01. REPLACED NR 2 FCC CARD. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002091300075 20020913 00075 EA 2002 9 13 SWIA200211190 1 20020902 A 2760 4916405 ECU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 916SW 7634 AFTER STARTING ENGINES, NOTED FLT SPOILERS, GROUND SPOILERS, CAUTION MSGS & SPOILERONS. INSTALLED SERVICEABLE SECU. OP S CHECK GOOD. 2 L 7 2 4F RT A21EA 2002091300076 20020913 00076 EA 2002 9 13 SWIA200211191 1 20020828 A 2910 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 NM 07 912SW 7595 ON DESCENT INTO PHX, HYD PUMP 1B CAUTION ILLUMINATED. CHECKED HYD SYNOPTIC PAGE. RESERVOIR 1 SHOWED WHITE WITH NO DATA (DASHED AMBER LINES) & HYD 1B PUMP AMBER, 1B THEN CYCLED FROM GREEN TO AMBER INTERMITTENTLY ON OR IN AUTO. AFTER LANDI NG, RESERVOIR READING SHOWED 5 PERCENT. POST FLIGHT FOUND HYD FLUID LEAKING FROM AFT EQUIPMENT BAY. REPAIRED CHAFED PR ESSURE LINE TO HYD SYSTEM NR 1. SERVICED FLUID LEVEL. OPERATED SYSTEM TO BLEED AND OPS CHECK GOOD. NO LEAKS NOTED. 2 L 7 2 4F RT A21EA 2002091300077 20020913 00077 EA 2002 9 13 SWIA200211192 1 20020902 A 2920 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 07 909SW 7558 HYD PUMP 2B MESSAGE ILLUMINATED ON APPROACH. HYDRAULIC SYNOPTIC PAGE SHOWED 0 PERCENT FLUID, TEMP 40 DEGREES WITH HYD P SI OF 3000. REPLACED NR 2 HYD SYSTEM TUBE ASSY, CASE DRAIN AND TUBE ASSY, PUMP PRESS LINE. SERVICED NR 2 HYD SYSTEM. NO LEAKS NOTED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002091300078 20020913 00078 EA 2002 9 13 SWIA200211193 1 20020830 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA A/C BAY SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 418SW 7446 DURING CLIMBOUT, NOTICED VISIBLE SMOKE IN COCKPIT AND CABIN. APU BLEED IN USE. RIGHT AC PACK BLOWING SMOKE. RETURNED TO FIELD. FOUND RT PACK BLOWING SMOKE. CHECKED WATER SOCK AND WAS CLEAN. REINSTALLED WATER SOCK. RAN RIGHT AC PACK W ITH ENG BLEEDS AND APU BLEEDS. NO SMOKE NOTED FROM THE RIGHT AC PACK SYSTEM. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2002091300079 20020913 00079 SO 2002 9 13 SWIA200211194 1 20020828 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT BURNED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 198SW 120227 ELECTRICAL SMELL IN COCKPIT. SMELL VERY FAINT IN CABIN. SMELL DISSIPATED WHEN W/S HEAT TURNED OFF (BOTH). FOUND RT W/ S GND AT WINDOW BURNED. COULD SMELL BURNT SMELL WITH W/S HEAT ON ONLY. REMOVED AND REPLACED RT WINDSHIELD IAW MM 56-10 -01. OPS CHECK GOOD RII 56-301. INSTALLED WINDSHIELD WIPER, OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002091300080 20020913 00080 NM 2002 9 13 USAA020230 1 20020513 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 785AU 31532 25024 PIT - FOUND FLOORBEAM CORRODED, STATION 986.5 TOP T-CAP ON FLOORBEAM, CORROSION REMOVED PER SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 2002091300081 20020913 00081 NM 2002 9 13 USAA020231 1 20020515 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 785AU 31532 25024 PIT - FOUND FLOOR SUPPORT CORRODED, STATION 986.5 TO 967 AT LBBL 16. FLOOR SUPPORT REPLACED WITH NEW PER SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 2002091300082 20020913 00082 NM 2002 9 13 USAA020232 1 20020515 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 785AU 31532 25024 PIT - FOUND FLOORBEAM CORRODED, TOP BEAM CAP STATION 967 AT LBBL 18 AT SCREW HOLE. REMOVED AND REPLACED BEAM CAP PER SR M 53-00-51. (M) 2 L 7 2 4F RT A16WE 2002091300083 20020913 00083 NM 2002 9 13 USAA020233 1 20020523 A 5320 CHANNEL BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 446US 31626 24873 PIT - FOUND ZEE CHANNEL CORRODED, RIGHT SERVICE DOOR ZEE CHANNEL. INSTALLED REPAIR PER SRM 53-10-51 FIG 206. (M) 2 L 7 2 4F RT A16WE 2002091300084 20020913 00084 NM 2002 9 13 USAA020235 1 20020523 A 5347 SEAT TRACK BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 446US 31626 24873 PIT - FOUND SEAT TRACK CORRODED, RIGHT INBOARD SEAT TRACK FORWARD END AT STATION 328. REMOVED CORROSION PER SRM 51-20-0 1. (M) 2 L 7 2 4F RT A16WE 2002091300085 20020913 00085 NM 2002 9 13 USAA020236 1 20020530 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND SUPPORT ANGLE CORRODED, INBOARD FORWARD SERVICE DOOR THRESHOLD SUPPORT ANGLE. REMOVED CORROSION PER SRM 51- 10-02. (M) 2 L 7 2 4F RT A16WE 2002091300086 20020913 00086 NM 2002 9 13 USAA020237 1 20020530 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND ZEE ANGLE CORRODED TWO AREAS, FORWARD SERVICE DOOR ZEE ANGLE. REMOVED CORROSION PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002091300087 20020913 00087 NM 2002 9 13 USAA020238 1 20020530 A 5320 SUPPORT BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND SUPPORT ZEE CORRODED 4 AREAS, FORWARD SERVICE DOOR SILL SUPPORT ZEE, 4 EACH. REMOVED CORROSION PER SRM 51-1 0-02. (M) 2 L 7 2 4F RT A16WE 2002091300088 20020913 00088 NM 2002 9 13 USAA020249 1 20020621 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND FRAME AND CLIP WITH SCATTERED CORROSION, FORWARD SIDE, FRAME AND CUP AT STATION 727G, S27L - S27R. (M) 2 L 7 2 4F RT A16WE 2002091300089 20020913 00089 NM 2002 9 13 USAA020250 1 20020614 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 784AU 31807 25023 PIT - FOUND FLOORBEAM CORRODED, STATION 967, RBL 29. FLOORBEAM UPPER CHORD REPAIR PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 2002091300090 20020913 00090 NM 2002 9 13 USAA020251 1 20020601 A 5534 ATTACH FITTING BOEING 737 7374B7 1384702 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 784AU 31807 25023 PIT - FOUND FITTING CORRODED, LEFT AFT OUTBOARD VERTICAL STABILIZER ATTACH FITTING. FITTING REPLACED, DRAG ANGLE REPAIR ACCOMPLISHED PER TYPICAL REPAIR 53-80-03. (M) 2 L 7 2 4F RT A16WE 2002091300091 20020913 00091 NM 2002 9 13 USAA020252 1 20020618 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48945 22952 PIT - FOUND Y-CHORD AND BULKHEAD CORRODED, BS 1016 AFT PRESSURE BULKHEAD AT FLOOR LINE CENTER. CORROSION LEVEL 2, REMOV ED CORROSION AND INSTALLED DOUBLERS PER EA 74025. (M) 2 L 7 2 4F RT A16WE 2002091300092 20020913 00092 NM 2002 9 13 USAA020253 1 20020508 A 5310 6517688165 CREASE BEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND CREASE BEAM CORRODED, STATION 277-360. DEFECTIVE PART REPLACED WITH IDENT PART. (M) 2 L 7 2 4F RT A16WE 2002091300093 20020913 00093 NM 2002 9 13 USAA020254 1 20020530 A 5320 65C25229 CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND CLIP CORRODED, STATION 727E BETWEEN S26R AND S27R. DOUBLER TREATED PER SRM 53-00-07 PAGES 210-212. (M) 2 L 7 2 4F RT A16WE 2002091300094 20020913 00094 NM 2002 9 13 USAA020255 1 20020501 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 IT - FOUND FLOOR SUPPORT CORRODED, STATION 727-787 AND 787-827 ABOVE S25L. SPLICED IN NEW SECTION PER SRM 53-60-53. (M ) 2 L 7 2 4F RT A16WE 2002091300095 20020913 00095 NM 2002 9 13 USAA020256 1 20020514 A 5347 SEAT TRACK BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND LEFT INBOARD SEAT TRACK, STATION 827-945 LBBL 24. CORROSION LEVEL 2. SPLICED IN SECTION OF TRACK PER SRM 5 3-00-52. (M) 2 L 7 2 4F RT A16WE 2002091300096 20020913 00096 NM 2002 9 13 USAA020268 1 20020712 A 2540 PANEL BOEING 737 737301 1384611 NM LAVATORY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 44212 23510 TPA - FOUND LAVATORY PANEL CORRODED 1 INCH BY 2 INCH, STATION 1025 AFT LEFT LAV PANEL AT TANK DRAW CUT OUT. CORROSION L EVEL 2. INSTALLED TYPICAL WEB REPAIR PER SRM 51-70-13 FIG 1. (M) 2 L 7 2 4F RT A16WE 2002091300097 20020913 00097 NM 2002 9 13 USAA020269 1 20020627 A 5320 SHIM BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 FOUND PIT INTERCOSTAL SHIM CORRODED, FS 967-987 RBL 17 WBL 208. REMOVED CORRODED SHIM AND REPLACED WITH NEW PER SRM 53- 00-04. (M) 2 L 7 2 4F RT A16WE 2002091300098 20020913 00098 NM 2002 9 13 USAA020270 1 20020625 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND INTERCOSTAL CORRODED, STATION 325 LBL 11 AT WBL 208. CORROSION LEVEL 2. REMOVED AND REPLACED INTERCOSTAL P ER SRM 53-10-04. (M) 2 L 7 2 4F RT A16WE 2002091300099 20020913 00099 NM 2002 9 13 USAA020273 1 20020625 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND SCUPPER DRAIN Z-ANGLE CORRODED, STATION 957-986.5 RBL 52 AT WBL 208. REMOVED LIGHT SURFACE CORROSION AND PR IMED PER SRM 53-10-15. (M) 2 L 7 2 4F RT A16WE 2002091300100 20020913 00100 NM 2002 9 13 USAA020274 1 20020625 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND Z-ANGLE CORRODED AT 4 LOCATIONS, STATION 957-986 RBL 54 AT WBL 208. REMOVED CORROSION PER SRM 53-10-15. (M ) 2 L 7 2 4F RT A16WE 2002091300101 20020913 00101 NM 2002 9 13 USAA020275 1 20020626 A 5347 SEAT TRACK BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND SEAT TRACK CORRODED, STATION 907 AND 908 WBL 208. REMOVED CORROSION PER SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 2002091300102 20020913 00102 NM 2002 9 13 USAA020276 1 20020626 A 5320 MOUNT BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND SEAT TRACK GABLE MOUNT CORRODED, STATION 986 AND 1016 RBL 32. REMOVED CORROSION PER SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 2002091300103 20020913 00103 NM 2002 9 13 USAA020277 1 20020701 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND Z-ANGLE CORRODED AT A FEW LOCATIONS, FS 867-947.5 STRINGER 26 RT. REMOVED SURFACE CORROSION PER SRM 51-10-0 2. (M) 2 L 7 2 4F RT A16WE 2002091300104 20020913 00104 NM 2002 9 13 USAA020285 1 20020719 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 47222 23380 PIT - FOUND SKIN CRACKED 3 INCHES, LOWER AFT CORNER OF FORWARD SERVICE DOOR CUT OUT AT BS 328. INSTALLED DOUBLERS PER S RM 53-10-01. (M) 2 L 7 2 4F RT A16WE 2002091300105 20020913 00105 NM 2002 9 13 USAA020287 1 20020704 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 51663 22210 CLT - FOUND 2 INCH AREA BULGE, FS 1458 AT S30 AT 2 RIVETS. INSTALLED DOUBLER PER EA 86441, SRM 53-00-01 FIG 203. (M) 2 L 7 2 4F RT A2NM 2002091300106 20020913 00106 NM 2002 9 13 USAA020288 1 20020703 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 51663 22210 CLT - FOUND SKIN WITH 3 INCH AREA BULGE, FS 1463 AT S28R AT 3 RIVETS. STRINGER SPLICE REPAIR DOUBLER TRIPLER PER SRM 53 -00-02, 53-00-01 AND EA 86402. (M) 2 L 7 2 4F RT A2NM 2002091300107 20020913 00107 NM 2002 9 13 USAA020295 1 20020619 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 46973 23315 PIT - FOUND SKIN CRACKED 1.5 INCHES LONG, FORWARD SERVICE DOOR AFT LOWER CORNER. INSTALLED DOUBLER PER SRM 53-10-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2002091300108 20020913 00108 NM 2002 9 13 USAA020297 1 20020730 A 5210 1131996 DOOR FRAME BOEING 737 7373B7 1384580 NM DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 46973 23315 PIT - FOUND FRAME CRACKED TWO PLACES 1 INCH EACH, UPPER FORWARD CORNER OF INTERIOR DOOR STOP FRAME. DEFECTIVE PART REPL ACED WITH IDENT PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002091300109 20020913 00109 NM 2002 9 13 USAA020298 1 20020730 A 5210 1121994 DOOR FRAME BOEING 737 7373B7 1384580 NM DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 46973 23315 PIT - FOUND FRAME CRACKED TWO PLACES 1 INCH EACH, UPPER AFT CORNER OF INTERIOR DOOR STOP FRAME. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002091300110 20020913 00110 NM 2002 9 13 USAA020302 1 20020622 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 48430 23311 PIT - FOUND SKIN CRACKED 1 INCH, STATION 328 AT S16R, LOWER CORNER OF DOOR OPENING. INSTALLED DOUBLER, FILLER REPAIR PE R SRM 53-10-01 FIG 202 AND EA 74207. (M) 2 L 7 2 4F RT A16WE 2002091300111 20020913 00111 NM 2002 9 13 USAA020308 1 20020619 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 46973 23315 PIT - FOUND SKIN CRACKED 1 INCH, CAPTAINS WINDSHIELD NR 1 UPPER LEFT CORNER OF WINDOW POST. INSTALLED EXTERIOR DOUBLER PER SRM 53-10-01 FIG 210 PAGE 233. (M) 2 L 7 2 4F RT A16WE 2002091300112 20020913 00112 NM 2002 9 13 USAA020320 1 20020731 A 5320 654583469 CHANNEL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 47222 23380 PIT - FOUND CHANNEL CRACKED 1 INCH, STATION 228, LBL 12 INCHES BELOW FLOOR. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002091300113 20020913 00113 NM 2002 9 13 USAA020323 1 20020731 A 5320 6545834551 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 PIT - FOUND INTERCOSTAL CRACKED 1 INCH, STATION 344 BELOW FLOOR LBL 45 INCHES. REPLACED ASSEMBLY WITH IDENT PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002091300114 20020913 00114 NM 2002 9 13 USAABB02116 1 20020717 A 2560 284N14206 SWITCH BOEING 757 757225 1384959 NM R4 DOOR MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 22203 PIT - R4 DOOR FOUND HARD TO OPEN. MAINTENANCE FOUND THE FORWARD GIRT BAR PROX SWITCH MISSING AND REPLACED IT. (M) 2 L 7 2 4F RT A2NM 2002091300115 20020913 00115 NM 2002 9 13 USAABB02119 1 20020722 A 2560 140N276218 GIRT BAR BOEING 757 757225 1384959 NM 4L DOOR DEFECTIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 22193 PHL - ATH THE 4L DOOR, THE GIRT BAR ENGAGEMENT LIGHT WAS EXTINGUISHED WITH THE SLIDE ARMING LEVER IN THE ARMED POSITION. MAINTENANCE REPLACED THE GIRT BAR. (M) 2 L 7 2 4F RT A2NM 2002091300116 20020913 00116 NM 2002 9 13 USAABB02120 1 20020725 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 612AU 27124 CLT - FOUND THE L4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002091300117 20020913 00117 NM 2002 9 13 USAABB02121 1 20020725 A 3350 8731002511REV15 SIGN BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 612AU 27124 CLT - FOUND THE R4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE EXIT IDENTIFIER ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002091300118 20020913 00118 NM 2002 9 13 USAABB02124 1 20020727 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 618AU 22210 BOS - FOUND THE TWO AISLE EMERGENCY LIGHTS AT SEAT ROW 4D INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 4D. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2002091300119 20020913 00119 NM 2002 9 13 USAABB02125 1 20020728 A 3350 8731002511REV15 SIGN BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 613AU 27144 BDL - FOUND THE RIGHT REAR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE EXIT IDENTIFIER. OPERATIONAL CHECK GO OD. (M) 2 L 7 2 4F RT A2NM 2002091300120 20020913 00120 NM 2002 9 13 USAABB02127 1 20020730 A 3350 8731002511REV15 SIGN BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 615AU 27146 FLL - FOUND R4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002091300121 20020913 00121 NM 2002 9 13 USAABB02128 1 20020702 A 3350 86210066 BATTERY PACK BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 633AU 27811 LAX - FOUND ALL FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AT ROWS 1, 4, 6, 9, 13 , 18, 23, 26, 29 AND 33. (M) 2 L 7 2 4F RT A2NM 2002091300122 20020913 00122 NM 2002 9 13 USAABB02129 1 20020803 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 605AU 22201 PHL - FOUND NINE FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002091300123 20020913 00123 NE 2002 9 13 SWIA200211195 2 20020902 A 7261 5083T02P01 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE DEFECTIVE A SWIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 416SW 7089 CLIMBING THROUGH FL240, 250 KTS, APPROX 5 DEGREES PITCH, CLIMB-THRUST, RIGHT ENGINE OIL LOW PRESS WARNING ILLUMINATED. QRH LED TO INFLIGHT SHUTDOWN. OIL PRESS APPROX 23-26 PSI AT 89.0 PERCENT N1. INSTALLED OVERHAULED NR 6 & NR 7 CARBON S EALS AND EXHAUST FRAME. RAN ENG FOR 10 MINUTES AT 85 PERCENT N2. NO LEAKS FOUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2002091300124 20020913 00124 EA 2002 9 13 SWIA200211196 1 20020829 A 3234 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 407SW 7034 NOSE GEAR WOULD NOT EXTEND NORMALLY ON APPROACH OKC. DID QRH PROCEDURE AND A MANUAL EMER GEAR EXT, ALL NORMAL. LOST NW S ON TAXI INTO GATE. COULD NOT RESET. AS ON FIRST EXT AT 180 KIAS, TRIED TWO MORE NORMAL EXTENSIONS (NOTE NW STEERING HAD BEEN FAIRLY SENSITIVE PRIOR LEGS). REMOVED AND REPLACED MLG SOLENOID SELECTOR VALVE PER MM 32-33-10. CYCLED LANDIN G GEAR, OPS CHECKS GOOD. NO LEAKS NOTED. NOSE WHEEL STEERING OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002091300125 20020913 00125 2002 9 13 SWIA200211197 4 20020830 A 2211 PIN EMB 120 EMB120ER 3260203 SO AUTOPILOT SYS BACKED OUT A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION UK UNKNOWN 1 NM 07 288SW 120316 CAPTAINS AUTOPILOT DOES NOT CAPTURE GS WITH APPR MODE. CAPTAIN'S AUTOPILOT FAILED WITH AILERON SERVO FAILURE. REPLACED PUSHED OUT PIN 44 ON J3 OF PILOT'S AUTOPILOT COMPUTER RACK. CAPTAIN`S AUTOPILOT OPS CHECK GOOD IAW MM 22-10-00. TESTE D AILERON SERVO WITH BOTH CAPT'S AND F/O'S AUTOPILOT. COULD NOT DUPLICATE DISCREPANCY. BOTH AUTOPILOTS AND AILERON SER VO OPS CHECKS GOOD IAW MM 22-10-00. 2 L 7 2 4T RT A31SO 2002091300126 20020913 00126 SO 2002 9 13 SWIA200211198 1 20020904 A 2121 EVAC2322C2 COOLING FAN EMB 120 EMB120ER 3260203 SO CABIN MALFUNCTIONED A SWIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 224SW 120294 ON TAXI OUT, STRONG ELECTRICAL ODOR IN FLIGHT DECK, THEN F/A REPORTS A VERY LOUD WHIPPING & CRACKING NOISE IN THE BACK O F CABIN. RETURNED TO GATE. REPLACED LEFT PACK GROUND COOLING FAN. RAN BOTH PACKS & BOTH ENGINES. ALL CHECKS NORMAL. 2 L 7 2 4T RT A31SO 2002091300127 20020913 00127 NE 2002 9 13 SWIA200211199 2 20020901 A 7321 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT EEC DIRTY A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 199SW 120237 LEFT EEC MANUAL REVERSION FAILED ON TAKEOFF. ABORTED TAKEOFF. CLEANED CONTAMINATION FROM LEFT ENG EEC P1 CONNECTOR. R AN ENG, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002091300128 20020913 00128 2002 9 13 SWIA200211200 4 20020829 A 3452 6226523205 CONTROL HEAD EMB 120 EMB120ER 3260203 SO TRANSPONDER MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 565SW 120340 AFTER TAKEOFF, ATC REPORTS NO TRANSPONDER REPORTING. TRIED BOTH ONE AND TWO TRANSPONDERS, NEITHER WORKED. RETURNED TO LAX. REPLACED TRANSPONDER CONTROL HEAD. TESTED WITH TEST BOX. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002091300129 20020913 00129 NE 2002 9 13 SWIA200211201 2 20020902 A 7200 PW118 ENGINE EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE LEFT OVERTEMP A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 196CA 120196 ON CLIMBOUT (LEFT) T6 RAISED WITH POWER REDUCTION. T6 CONTINUED TO RISE TO THE POINT OF T6 WARNING. T6 FINALLY CAME DO WN TO ABOUT 684 DEGREES, PRODUCING NO TORQUE. DID A PRECAUTIONARY ENGINE SHUTDOWN. RETURNED TO LAX. REMOVED AND REPLA CED LEFT ENGINE IAW EMB120 MM 71-00-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2002091300130 20020913 00130 EU 2002 9 13 C2XA02IA190 1 20020912 A 2422 559012A INVERTER AEROSP ATR42 ATR42320 8680930 EU FWD.ELECT.COMPT INOPERATIVE A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 86842 286 IAH- AFTER LANDING THE CREW NOTED A BURNING SMELL. IAH- MAINTENANCE REMOVED AND REPLACED THE #2 INVERTER, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002091300131 20020913 00131 EU 2002 9 13 C2XA02IA191 1 20020912 A 3350 7012210 LAMP AEROSP ATR42 ATR42320 8680930 EU PAX DOOR STEP BURNED OUT A C2XA K NONE L NO TEST HO HOVERING 1 SW 27 99838 259 IAH- DURING WEEKLY CHECK IT WAS NOTED THAT THE PAX DOOR EMERGENCY LIGHT WAS INOPERATIVE. IAH- MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002091300132 20020913 00132 EU 2002 9 13 C2XA02IA192 1 20020912 A 3350 0341516 FUSE AEROSP ATR42 ATR42320 8680930 EU CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 99838 259 IAH- DURING A WEEKLY CHECK IT WAS NOTED THAT THE AISLE PATH LIGHTING FOR POWER SUPPLY 18WL FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE FUSE AT LOCATION 18WL, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOIR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002091500001 20020915 00001 2002 9 15 RAIA00209247 4 20020908 A 3425 7003360948 CONTROL UNIT JETAIR JETSTM JETSTM4101 1500501 EU FALSE INDICATION A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 554HK 12962 1784 41067 5522-STL- #1 ELECTRONIC ADI INDICATED PITCH COMPARE ERROR. MAINTENANCE REMOVED AND REPLACED THE #1 AHRS UNIT, OPS CK OK. 2 L 7 2 4T RT A41NM 2002091500002 20020915 00002 2002 9 15 RAIA00209248 4 20020909 A 2350 APC2531 CONTROL PANEL AEROSP ATR42 ATR42300 8680920 EU A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 422TE 106 5450-STL- FO's AUDIO PANEL INOP. MAINTENANCE REMOVED AND REPLACED FO's AUDIO CONTROL PANEL, OPS CK OK. 2 H 7 2 4T RT A53EU 2002091500003 20020915 00003 EU 2002 9 15 RAIA00209249 1 20020909 A 2435 8260121 STARTER GEN AEROSP ATR42 ATR42300 8680920 EU INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 426TE 25423 667 228 5590-STL- RIGHT ENGINE WILL NOT ROTATE ON START. MAINTENANCE REMOVER AND REPLACED THE RIGHT ENGINE STARTER/GENERATOR, OP S & LK CK OK. 2 H 7 2 4T RT A53EU 2002091500004 20020915 00004 EU 2002 9 15 RAIA00209250 1 20020909 A 2730 CB50067 SIGNAL COND UNIT JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 03 552HK 17054 41057 5550-STL- STICK SHAKER WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED THE STICK SHAKER SIGNAL PROCESSOR, OPS CK OK. 2 L 7 2 4T RT A41NM 2002091600001 20020916 00001 2002 9 16 SWAA022113 4 20020910 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091600002 20020916 00002 2002 9 16 SWAA022114 4 20020910 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE LOOSE. SECURED SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2002091600003 20020916 00003 2002 9 16 SWAA022115 4 20020910 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091600004 20020916 00004 2002 9 16 SWAA022116 4 20020911 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 710SW 27844 AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091600005 20020916 00005 NM 2002 9 16 SWAA022118 1 20020910 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 885, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002091600006 20020916 00006 2002 9 16 SWAA022080 4 20020909 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM. 2 L 7 2 4F RT A16WE 2002091600007 20020916 00007 NM 2002 9 16 SWAA022081 1 20020908 A 5330 6545776 SKIN BOEING 737 7373T5 1384608 NM AFT SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD LOWER CORNER OF AFT SVC DOOR CUTOUT. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2002091600008 20020916 00008 NM 2002 9 16 SWAA022082 1 20020908 A 5320 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 195, WL 209 AND RBL 29. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002091600009 20020916 00009 NM 2002 9 16 SWAA022084 1 20020909 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER SWA T1. 2 L 7 2 4F RT A16WE 2002091600010 20020916 00010 NM 2002 9 16 SWAA022085 1 20020908 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091600011 20020916 00011 NM 2002 9 16 SWAA022086 1 20020909 A 5330 589357 SKIN BOEING 737 7373H4 1384600 NM WINDOW POST CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED ON BOTH CAPTAIN'S AND F/O WINDOW POSTS. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091600012 20020916 00012 NM 2002 9 16 SWAA022087 1 20020909 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 592, STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091600013 20020916 00013 NM 2002 9 16 SWAA022088 1 20020908 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727 PLUS 14, ABOVE STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091600014 20020916 00014 NM 2002 9 16 SWAA022089 1 20020907 A 5320 6545768 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L AND STR 14L. REMOVED AND REPLACED SH EAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002091600015 20020916 00015 NM 2002 9 16 SWAA022091 1 20020907 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091600016 20020916 00016 NM 2002 9 16 SWAA022092 1 20020907 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 525, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091600017 20020916 00017 NM 2002 9 16 SWAA022093 1 20020907 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED A2 CHECK, SWA SI 11038, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSH INGS ON NR 2, NR 3 AND NR 4 TAB HINGE ATTACH POINTS PER MM. 2 L 7 2 4F RT A16WE 2002091600018 20020916 00018 NM 2002 9 16 SWAA022095 1 20020909 A 5510 6547991 RIB BOEING 737 737317 138447P NM LT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STABILIZER UPPER RIB CHORD CRACKED (2 EA) AT STA 166.30 AND STA 193.9. RE PAIRED UPPER RIBS PER SRM. 2 L 7 2 4F RT A16WE 2002091600019 20020916 00019 NM 2002 9 16 SWAA022096 1 20020909 A 5311 6545774 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT CORRODED AT BS 847, BETWEEN STR 25R AND STR 26R. REPAIRED F RAME PER SRM. 2 L 7 2 4F RT A16WE 2002091600020 20020916 00020 NM 2002 9 16 SWAA022097 1 20020909 A 5311 6516301 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002091600021 20020916 00021 NM 2002 9 16 SWAA022098 1 20020906 A 5520 BACB28AKM07 BUSHING BOEING 737 7373H4 1384600 NM RT HORIZ STAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHING ON NR 1 TA B HINGE ATTACH POINT PER MM. 2 L 7 2 4F RT A16WE 2002091600022 20020916 00022 NM 2002 9 16 SWAA022099 1 20020906 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10L, BS 383, BS 494 AND BS 500 PLUS 15. REPAI RED SKIN PER SRM AND SWA EA. 2 L 7 2 4F RT A16WE 2002091600023 20020916 00023 NM 2002 9 16 SWAA022100 1 20020906 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091600024 20020916 00024 NM 2002 9 16 SWAA022101 1 20020907 A 5540 65C25814 RUDDER BOEING 737 7373H4 1384600 NM VERTICAL STAB DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SPECIAL VISIT, FOUND RUDDER DELAMINATED AT FIN WL 96. REMOVED AND REPLACED RUDDER PER MM. 2 L 7 2 4F RT A16WE 2002091600025 20020916 00025 EU 2002 9 16 DHL2002363512 1 20020810 A 5730 SKIN AIRBUS 300 A300B4203 3930306 EU RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-CHECK, RT WING FWD OF NR 6 FLAP TRACK ASSY HAS EXFOLIATION ON LOWER WING PLANK AT DRAIN HOLE. REMOVED CORROSION IAW A 300 SRM 51-40-11. REMOVED DAMAGED FASTENER AND COUNTERSUNK HOLE PER A300 SRM 51-30-43 AND REINSTALLED NEW FASTENER IAW A300 SRM 51-30-35. APPLIED CORROSION PREVENTATIVE IAW A300 SRM 51-40-11, OK TO PRIME. PRIMED AFFECTED AREA IAW A300 SR M 51-40-12. APPLIED TOP COAT TO AFFECTED AREA IAW A300 SRM 51-40-12. PERFORMED ABOVE APPROVAL CONTAINED IN RAS/BAE/101 /2002. 2 L 7 2 4F RT A35EU 2002091600026 20020916 00026 2002 9 16 DHL2002363526 4 20020905 A 2210 AUTOPILOT SYS AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 01 363DH 85 ACCEPTANCE FLIGHT/DURING COUPLED APPROACH WITH BOTH AUTOPILOTS ENGAGED IN CMD AND IN LAND MODE AT A PREDETERMINED ALTITU DE GO AROUND WAS SELECTED AND THE PITCH CLIMBOUT DID NOT SEEM TO BE CORRECT TO THE FLIGHT CREW, AS WELL AS THE ALTITUDE ACQUISITION. THE CHECK WAS DONE AGAIN USING ONLY AUTOPILOT 2 AND AFTER A NORMAL APPROACH GO AROUND WAS SELECTED, THE AI RCRAFT NOSED UP AND THE ENGINES ACCELERATED. AFTER A SHORT TIME THE COPILOT HAD THE YOKE FULL FORWARD AND THE AIRCRAFT WAS NOT RESPONDING, USE OF THE STABILIZER TRIM SWITCH ON THE YOKES WAS ALSO INOPERATIVE. THE PILOT THEN TURNED THE STAB TRIM WHEEL MANUALLY AND THE AIRCRAFT NOSED OVER. IT WAS IF THE AUTOPILOT WOULD NOT DISENGAGE THE GO AROUND MODE. THIS 2 L 7 2 4F RT A35EU 2002091600027 20020916 00027 NM 2002 9 16 DHL2002721008 1 20020905 A 5270 SWITCH BOEING 727 727228 1384083 NM ENTRY DOOR OUT OF ADJUST A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 721DH 19545 MAIN CARGO DOOR WARNING LIGHT S/O PANEL AND RIGHT AT ENTRY DOOR ILLUMINATED AT FL285 CABIN PSI WAS 7.0 TO 8.0 PSI NO LOS S OF PRESSURIZATION NOTED. DHL AIRWAYS EVENT REPORT STATES AN EMERGENCY WAS DECLARED. ADJUSTED AFT JAMB DRIFT PIN SWIT CH. OPS CHECKED DOOR PER MM CHAPTER 52-30-0. NO DEFECTS FOUND. PRESSURIZED AIRCRAFT TO 92 PSI, WARNING LIGHT DID NOT ILLUMINATE. 2 L 7 3 4F RT A3WE 2002091600028 20020916 00028 WP 2002 9 16 ZW0A0209502 1 20020912 A 4990 5910050ALLC0NF1 APU DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 9405T 53141 THERE WAS A SMELL OF BURNED OIL AND LIGHT HAZE IN COCKPIT AND CABIN. THE APU WAS PLACARDED INOPERATIVE PER MEL. THE AP U WAS LATER REPLACED. CHECK-C 10-01-01 MCI. --CLOSED-- 2 L 7 2 4F RT A6WE 2002091600029 20020916 00029 NM 2002 9 16 DHL2002721510 1 20020803 A 5312 PRESSURE PANEL BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK, NOSE WHEEL WELL HORIZONTAL PRESS MID CHORD CORROSION AT APPROX STA 320 & 355 RT AT DOGHOUSE TO CATWALK J UST AFT OF RT NOSE TRUNNION. FOUND RT AND N/W/W PRESSURE WEB MID CHORD TO BE CORRODED BEYOND ALLOWABLE LIMITS AND REMOV ED. LOCATED AND DRILLED UP NEW MID CHORD FITTING ON RT AND NLG WW PRESSURE WEB. INSTALLED NEW MID CHORD FITTING IN NLG WW RT. REINSTALLED RT HORIZONTAL WALKWAY WEB IN FWD E & E. 2 L 7 3 4F RT A3WE 2002091600030 20020916 00030 NM 2002 9 16 QXEA0201439 1 20020911 A 2730 3994001011 ACTUATOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 300 FAILED A QXEA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 09 402QX 1722 1722 4032 PDX - ON CLIMBOUT AT SEA, CREW RECEIVED AN AUTO PITCH TRIM FAIL MESSAGE ON THE PFD WITH AN ASSOCIATED PITCH TRIM CAUTION . AUTO PILOT WAS ENGAGED AT THE TIME. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND CDS CODES E3,E7,G3,AND G7. MAINTENANC E REPLACED THE PITCH TRIM ACTUATOR. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED OK. THE AIRCRAFT WAS RETURNED TO SERVI CE. 2 H 7 2 4T RT A13NM 2002091600031 20020916 00031 NM 2002 9 16 DHL2002721511 1 20020807 A 5720 FITTING BOEING 727 727228 1384083 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK, RT WING STRINGER LUG CRACKED AT RIB ATTACH WS 656. CRACK IN LUG TERMINATES AT FASTENER HOLE ON RT VENT BOX STRINGER AT RIB ATTACH WS 656 VERIFIED BY 10 X MAGNIFYING GLASS. DRILLED UP REPAIR PARTS AND INSTALLED. 2 L 7 3 4F RT A3WE 2002091600032 20020916 00032 NM 2002 9 16 DHL2002721512 1 20020806 A 5330 SKIN BOEING 727 727228 1384083 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK, FOUND 2 DENTS ON SECTION 41 SKIN AT 6 O'CLOCK POSITION FWD OF FWD E/E BAY DOOR. CUT OUT SECTION OF DAMA GED FUSELAGE SKIN 6 O'CLOCK POSITION AT STA 186 FWD OF FWD E & E DOOR IAW B-727 SRM 53-30-3 FIG 4. REMOVED EXISTING FLU SH REPAIR FWD OF CUT OUT IAW B-727 SRM 51-30-2. FABRICATED REPAIR DOUBLER AND FILLERS IAW B-727 SRM 53-30-2. INSTALLED REPAIR DOUBLER ON FUSELAGE SKIN AT 6 O'CLOCK POSITION IAW B-727 SRM 53-30-3 FIG 4. 2 L 7 3 4F RT A3WE 2002091600034 20020916 00034 NM 2002 9 16 DHL2002721514 1 20020805 A 5347 SEAT TRACK BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK, CABIN SEAT TRACK AT LBL 45 IS CORRODED AT STA 1148 AND STA 1156. REMOVED CABIN SEAT TRACK SECTION FROM STA 1148 TO STA 1156-LBL 45 IAW B-727 SRM 51-30-2. FABRICATED NEW SECTION OF SEAT TRACK IAW B-727 SRM 53-10-5 FIG 1. I NSTALLED NEW SEAT TRACK IAW B-727 SRM 53-10-5 FIG 1. 2 L 7 3 4F RT A3WE 2002091600035 20020916 00035 NM 2002 9 16 DHL2002721516 1 20020807 A 5711 SPAR BOEING 727 727228 1384083 NM LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK, LT WING UPPER FRONT SPAR ATTACH TO L/E WS 140/150 CORROSION UNDERNEATH L/E SKIN. REMOVED CORROSION FROM FRONT SPAR UPPER CHORD UPPER SURFACE WS 140 TO WS 150. MAT LOSS BEYOND ALLOWABLE LIMITS. FABRICATED 2 SPAR CHORD REPA IR ANGLES. INSTALLED REPAIR PARTS. 2 L 7 3 4F RT A3WE 2002091600036 20020916 00036 NE 2002 9 16 MWEA020514 2 20020820 A 7321 BELLOWS DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE LT ENGINE LOW A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 502ME 48132 CREW REPORTED LEFT ENGINE EPR, N1, N2, AND FUEL FLOW ALL FLUCTUATING. PERFORMED VISUAL INSPECTION OF ENGINE. NO DEFECT S NOTED. DRAINED EXCESS MOISTURE FROM MOISTURE TRAP AND SERVICED FCU BELLOWS. RAN ENGINE TO TAKEOFF POWER. ALL ENGINE PARAMETERS STABLE MATCHING, OK FOR SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2002091600037 20020916 00037 NM 2002 9 16 SWAA022083 1 20020907 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002091600038 20020916 00038 NM 2002 9 16 SWAA022090 1 20020907 A 5320 6545774 DOUBLER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME DOUBLER CRACKED AT BS 727, STR 10R. REPAIRED FRAME DOUBLER PER SRM . 2 L 7 2 4F RT A16WE 2002091600039 20020916 00039 NM 2002 9 16 SWAA022094 1 20020909 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE BULGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BULGED AT BS 500D TO BS 526, STR 28L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091600040 20020916 00040 NM 2002 9 16 SWAA022102 1 20020908 A 2913 849589 PUMP BOEING 737 7377H4 1384404 NM NR 2 ENGINE FAILED A SWAA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 29 700GS 27835 DECLARED EMERGENCY, DURING FLIGHT LOST B HYDRAULIC SYSTEM, QUANTITY ZERO. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRA ULIC PUMP AND NR 2 ELECTRIC PUMP PER MM. 2 L 7 2 4F RT A16WE 2002091600041 20020916 00041 NM 2002 9 16 SWAA022103 1 20020907 A 3097 W502452 WIRE BOEING 737 7373Y0 1384671 NM COCKPIT CHAFED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 699SW 23826 BURN SMELL IN COCKPIT, SMELL IMMEDIATELY DISSIPATED. C/W INSPECTION IN MCI NO DEFECTS NOTED. LATER AT LAS, DID FOLLOW UP AND FOUND CHAFFED WIRE AT L1 WINDOW HEAT UNDER GLARE SHIELD. REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 2002091600042 20020916 00042 NM 2002 9 16 SWAA022117 1 20020910 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 706SW 27840 DURING SCHEDULED PM SERVICE CHECK, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002091600043 20020916 00043 GL 2002 9 16 SWAA022119 2 20020911 A 7260 335304603 BEARING BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563B1US GL NR 2 ENGINE FAILED A SWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 29 357SW 26594 857235 DIVERSION, ON CLIMB-OUT FROM HOU, AIRFRAME LATERAL VIBRATION FELT, NR 2 ENGINE N2 IND FLUCTUATES 2.0 PERCENT. REMOVED A ND REPLACED NR 2 ENGINE DUE TO AGB SHAFT BEARING FAILURE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002091600044 20020916 00044 SO 2002 9 16 SWIA200211186 1 20020901 A 7910 CAP EMB 120 EMB120ER 3260203 SO LT ENGINE OUT OF POSITION A SWIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 301YV 120301 ON TAXI OUT TO RUNWAY, OIL PRESSURE WARNING LIGHT ILLUMINATED FOLLOWED BY OIL AURAL WARNING ON LEFT ENGINE. SHUT DOWN L EFT ENGINE IMMEDIATELY. OIL PRESSURE FELL BELOW 40 PSI D FOR LESS THAN 5 SECONDS. REASON FOR LOW OIL PRESSURE ON LEFT ENGINE WAS OIL CAP INADVERTENTLY LEFT OFF AFTER OIL SERVICE. 2 L 7 2 4T RT A31SO 2002091600045 20020916 00045 2002 9 16 U30A200200021 4 20020817 A 2211 B546CAM0103 COMPUTER AIRBUS 320 A320214 3930316 EU AUTOPILOT SYS FAULTY A U30A K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 17 262AV 1184 1184 1725 DURING PREFLIGHT FOR FLT 1371 AT ORD, ECAM MESSAGE INDICATED AP2, CAT 3 DUAL. AFS BITE CALLS FOR FMGC NR 2 REPLACEMENT. DEFERRED NR 2 FMGC PER MEL 22-83-01-2. AIRCRAFT OPERATED ORD-CUN-PHL. UPON ARRIVAL AT PHL THE NR 2 FMGC (FLIGHT MANA GEMENT GUIDANCE COMPUTER) WAS REPLACED PER AMM 22-83-34-401. OPERATIONALLY & RVSM CHECKED OK. 2 L 7 2 4F RT A28NM 2002091600046 20020916 00046 WP 2002 9 16 ZW0A0209503 1 20020909 A 3350 408822101 BATTERY DOUG DC9 DC982 3022082 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 901TW 49166 THE EMERGENCY AISLE OVERHEAD LIGHTS WERE INOPERATIVE FROM ROW 8 THRU 12. REPLACED THE BATTERIES IN THE BATTERY PACK. CH ECK-C 6-16-01 STL. --CLOSED-- 2 L 7 2 4F A6WE 2002091600047 20020916 00047 NM 2002 9 16 VNAA0208045 1 20020830 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 429JS 16282 372 3043 THE CREW REPORTED THAT THE EMERGENCY LIGHTS AT ROWS 4 AND 5 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091600048 20020916 00048 NM 2002 9 16 VNAA0209001 1 20020901 A 3242 BRAKE ASSY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT MALFUNCTIONED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 462PS 3084 THE CREW REPORTED THAT THE FIRST OFFICER'S LEFT BRAKE WAS NOT OPERATING AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND BLED THE BRAKE AND THE BRAKE METERING UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHE CKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091600049 20020916 00049 NM 2002 9 16 VNAA0209005 1 20020905 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 425JS 14378 126 3037 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 4 TO 5 WILL NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED TH E EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE A IRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091600050 20020916 00050 NM 2002 9 16 VNAA0209006 1 20020905 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 459PS 11060 135 3070 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 6 TO 9 WILL NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED TH E EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE A IRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091600051 20020916 00051 NM 2002 9 16 VNAA0209009 1 20020909 A 3250 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 439JS 3057 DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING CAS MESSAGE AND ABORTED TAKEOFF. THE CREW EXITED THE RUNWAY AND THE MESSAGE CLEARED BY ITSELF. THE CREW CALLED MAINTENANCE CONTROL AND THE DECISION WAS MADE TO ATTEMPT ANOTHER TAKEOF F. FLIGHT 4085 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091600052 20020916 00052 NM 2002 9 16 VNAA0209010 1 20020909 A 3250 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 430JS 3044 DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING CAS MESSAGE AND ABORTED TAKEOFF. THE CREW EXITED THE RUNWAY AND THE MESSAGE CLEARED BY ITSELF. THE DECISION WAS MADE TO ATTEMPT ANOTHER TAKEOFF. FLIGHT 4124 THEN DEPARTED WITH NO F URTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091600053 20020916 00053 NM 2002 9 16 VNAA0209011 1 20020909 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 458PS 14266 137 3068 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 4-7 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLAC ED THE 5LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091600054 20020916 00054 NE 2002 9 16 VNAA0209012 2 20020910 A 7530 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ENGINE DIRTY A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 439JS 3057 DURING TAKEOFF, THE CREW RECEIVED AN AC VOLT FAIL AND ECU FAIL MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND C LEANED THE CANNON PLUG ON THE IBV VALVE AND ECU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 75-00-00. OPERATIONAL CHE CKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091600055 20020916 00055 NM 2002 9 16 VNAA0209013 1 20020910 A 3251 2318000002 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG FAULTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 430JS 16 3044 DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE NOSE WHEEL STEERING ELECTRONIC CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERA TIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091600056 20020916 00056 NM 2002 9 16 VNAA0209014 1 20020910 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 439JS 3057 DURING TAKEOFF, THE CREW RECEIVED AN ECU FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CREW THEN EXITED THE RUNAWAY AND THE MESSAGE CLEARED BY ITSELF. THE CREW CALLED MAINTENANCE CONTROL AND THE DECISION WAS MADE TO TRY ANOTHER TAKEOFF ATTEMP T. FLIGHT 4123 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091600057 20020916 00057 NM 2002 9 16 VNAA0209015 1 20020910 A 4920 APU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE APU BAY DETERIORATED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 463PS 3087 THE CREW REPORTED A BURNING SMELL IN THE COCKPIT THAT SEEMS TO BE COMING FROM THE RIGHT HAND PACK. MAINTENANCE INSPECTE D AND FOUND THAT THE APU WAS FAILING THE COMPRESSION CHECK. THE APU WAS THEN DEFERRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091600058 20020916 00058 NM 2002 9 16 VTZA02225409 1 20020814 A 3350 LIGHT DORNER DO32 DO328300 NM CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 409FJ DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED FLOOR TRACK LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002091600059 20020916 00059 NM 2002 9 16 VTZA02229415 1 20020217 A 3350 LIGHT DORNER DO32 DO328300 NM CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 415FJ 3170 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANC E PERSONNEL RELAMPED THE PASSENGER DOOR EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WA S RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002091600060 20020916 00060 NM 2002 9 16 VTZA02238413 1 20020826 A 3350 CONNECTOR DORNER DO32 DO328300 NM CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 413FJ DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL SECURED LOOSE EMERGENCY CONNECTOR AT ROW 8. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR RE TURN TO SERVICE. 2 H 7 2 4T RT A55NM 2002091600061 20020916 00061 NM 2002 9 16 VTZA02239408 1 20020827 A 7732 CONNECTOR DORNER DO32 DO328300 NM PWC PW207 PW207D NE RT ENGINE DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 408FJ DURING CRUISE FROM BGR TO BOS CREW RECEIVED RT ENGINE N2 VIBRATION AND ENGINE MISCOMPARE EICAS MESSAGES. FLIGHT CREW FO LLOWED QRH PROCEDURES AND RETURNED TO POINT OF DEPARTURE. AIRCRAFT LANDED IN BGR WITHOUT ANY FURTHER INCIDENT. MAINTEN ANCE PERSONNEL CLEANED, INSPECTED AND RETIGHTENED THE CANNON PLUG. RT ENGINE VIBRATION CHECK WAS SATISFACTORY AND AIRCR AFT WAS RELEASED FOR RETURN TO SERVICE. 2 H 7 2 4T 3 U RT A55NM E42NE 2002091600062 20020916 00062 EU 2002 9 16 VTZA08282002 1 20020828 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 301UE 301UE FIRST HALF OF EMERGENCY TRACK LIGHTING OUT. 2 L 7 2 4T RT A41NM 2002091600063 20020916 00063 WP 2002 9 16 ZW0A0208701 1 20020817 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 940AS 49825 DURING CHECK-C MAINT THE FWD SERVICE DOOR HAD A .25 INCH CRACK IN THE UPPER BEAM, FWD END INSIDE RADIUS. REMOVED AND RE PLACED BEAM PER SPM 6-70-01. 2 L 7 2 4F A6WE 2002091600064 20020916 00064 WP 2002 9 16 ZW0A0208801 1 20020819 A 3350 60030451LB BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9404V 53140 THE EMERGENCY LIGHT IN UPPER RIGHT SIDE OF TAIL CONE, AND THE EMERGENCY LIGHT IN THE MID GALLEY, WERE BOTH INOPERATIVE. REPLACED THE BATTERY PACK FOR EACH OF THEM. 2 L 7 2 4F RT A6WE 2002091600065 20020916 00065 WP 2002 9 16 ZW0A0208802 1 20020816 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 940AS 49825 DURING CHECK-C MAINT THE NUMBER 2 CABIN FLOOR TRACK AT LBL 44, WAS CORRODED AT ATTACH HOLES, STA 1136 TO 1180. REMOVED CORRODED SECTION AND SPLICED IN NEW SECTION PER SRM 53-05, FIG 4 PAGE 100. 2 L 7 2 4F A6WE 2002091600066 20020916 00066 WP 2002 9 16 ZW0A0208803 1 20020819 A 5320 PLATE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 940AS 49825 DURING CHECK-C MAINT FOUND A CRACK IN PLATE AT KEEL BEAM ABOVE THE AFT EDGE OF THE LT WHEEL WELL DOOR. INSTALLED NEW PL ATE PER SRM 6-70-01, PAGE 3 ITEM 4B-1 AND DOUGLAS DRAWING 5936395, AND SRM 51-30-5. 2 L 7 2 4F A6WE 2002091600067 20020916 00067 NM 2002 9 16 ZW0A0208901 1 20020814 A 5330 SKIN BOEING 757 757231 1384950 NM FUSELAGE DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 724TW 28488 DURING CHECK C MAINT THERE WAS A PREVIOUS REPAIR TO A DENT IN THE FUSELAGE AT STA 661, BETWEEN STRINGER 17L AND 18L. TH E DENT MEASURED 3.25 INCHES BY 0.105 DEEP. MADE PERMANENT REPAIR BY INSTALLING SOLID FASTENERS PER SRM 53-00-01, FIG 20 4. 2 L 7 2 4F RT A2NM 2002091600068 20020916 00068 WP 2002 9 16 ZW0A0209001 1 20020820 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 940AS 49825 DURING CHECK-C MAINT FOUND SKIN CORRODED AT STA 693, RT OUTBOARD SIDE AT LONGERON 30. REMOVED CORROSION AND REPAIRED PE R ARA 18279. 2 L 7 2 4F A6WE 2002091600069 20020916 00069 WP 2002 9 16 ZW0A0209002 1 20020821 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 940AS 49825 DURING CHECK-C MAINT FOUND CORROSION ON FUSELAGE SKIN ON FWD SIDE OF STA 693, RT OUTBOARD SIDE OF LONGERON 30 AT SCUPPER DRAIN. REMOVED CORROSION PER SPM 6-80-01. REPAIRED AREA PER ARA 18279. 2 L 7 2 4F A6WE 2002091600070 20020916 00070 WP 2002 9 16 ZW0A0209003 1 20020823 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE BENT A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 940AS 49825 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND A BENT FORMER RING AT STA 1271, APPROXIMATELY 3 INCHES ABOVE LONGERON 30. REMOVED DAMAGED AREA AND REPAIRED PER SRM 53-3, FIG 5. 2 L 7 2 4F A6WE 2002091600071 20020916 00071 WP 2002 9 16 ZW0A0209201 1 20020909 A 5313 STRINGER DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9402W 53138 DURING CHECK-C MAINT LONGERON 2L WAS CRACKED AT STA 1418, .25 INCH LONG. INSTALLED REPAIR SPLICE PER SRM 53-02, FIG 18. 2 L 7 2 4F RT A6WE 2002091600072 20020916 00072 EU 2002 9 16 DHL2002363500 1 20020806 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-CHECK, RT SIDE OF FUSELAGE AT FRAME 6 BELOW STR 44R HAS 1 EACH DENT. DENT IS WITHIN LIMITS IAW A300 SRM 53-10-00 PG 6 15 FIG 609. NO FURTHER ACTION REQUIRED. 2 L 7 2 4F RT A35EU 2002091600073 20020916 00073 EU 2002 9 16 DHL2002363501 1 20020806 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-CHECK, LT SIDE OF FUSELAGE AT FR 21-22 BELOW LAP SEAM UNDER MAIN CARGO DOOR HAS DENT EXTENDING FROM THE INSIDE. DENT IS WITHIN LIMITS IAW A300 SRM 53-10-00 PG 615 FIGURE 609. NO FURTHER ACTION REQUIRED. 2 L 7 2 4F RT A35EU 2002091600074 20020916 00074 EU 2002 9 16 DHL2002363503 1 20020811 A 5315 FLOORBEAM AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-CHECK, CORROSION ON FLOORBEAM AT FRAME 6L BL 78 R. REMOVED SURFACE CORROSION IAW A 300 SRM 51-40-11. WITHIN LIMITS I AW A300 SRM 53-10-00 PG 602. 2 L 7 2 4F RT A35EU 2002091600075 20020916 00075 EU 2002 9 16 DHL2002363504 1 20020812 A 5230 SKIN AIRBUS 300 A300B4203 3930306 EU CARGO DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-CHECK, FWD LOWER CARGO DOOR HAS NUMEROUS GOUGES/NICKS ON SKIN EDGE AT FRAME 20 AND 25. BROKE SHARP EDGES AND SMOOTHED GOUGES WITHIN LIMITS IAW A300 SRM 52-30-30. 2 L 7 2 4F RT A35EU 2002091600076 20020916 00076 EU 2002 9 16 DHL2002363505 1 20020812 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-CHECK, LWR AFT CARGO DOOR CUTOUT HAS 1 SQUARE INCH OF LIGHT SURFACE CORROSION AT FWD LOWER CORNER. REMOVED SURFACE CO RROSION IAW A300 SRM 51-40-11, FOUND TO BE WITHIN LIMITS IAW A300 SRM 51-10-00. 2 L 7 2 4F RT A35EU 2002091600077 20020916 00077 EU 2002 9 16 DHL2002363506 1 20020815 A 5730 SKIN AIRBUS 300 A300B4203 3930306 EU LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-CHECK, BOTTOM SKIN LEFT WING BETWEEN RIB 10 AND 13 JUST OUTBOARD OF ACCESS PANEL 543BB LIGHT CORROSION ON WING PLANK. REMOVED CORROSION IAW A300 SRM 51-40-11. REMOVED CORROSION IAW A300 SRM 51-40-11, AREA WITHIN LIMITS IAW A300 SRM 57-3 3-11. 2 L 7 2 4F RT A35EU 2002091600078 20020916 00078 EU 2002 9 16 DHL2002363507 1 20020815 A 5320 DOUBLER AIRBUS 300 A300B4203 3930306 EU FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-CHECK, MAIN CABIN FRAME 21 STR 9R FRAME REPAIR HAS BEEN DENTED. REMOVED REPAIR CHANNEL IAW A300 SRM 51-30-30. HAND F ORMED DENT PER A300 SRM 51-40-40 AN 51-40-10, REFORMED TO ORIGINAL CONTOUR. EC INSPECTED PER NTM 51-31-05, NO CRACKS FO UND. REINSTALLED REPAIR IAW A300 SRM 51-30-30. 2 L 7 2 4F RT A35EU 2002091600079 20020916 00079 EU 2002 9 16 DHL2002363514 1 20020809 A 3213 D520181 SLEEVE AIRBUS 300 A300B4203 3930306 EU NR 4 AXLE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-CHECK, NR 4 AXLE PROTECTIVE SLEEVE HAS PITTING ON EXTERNAL SURFACE AND NICKEL PLATING WORN. REMOVED AND REPLACED PROT ECTIVE SLEEVE IAW A300 AMM 32-42-27. 2 L 7 2 4F RT A35EU 2002091600080 20020916 00080 EU 2002 9 16 DHL2002363520 1 20020816 A 7830 THRUST REVERSER AIRBUS 300 A300B4203 3930306 EU NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-CHECK, NR 1 INBOARD FAN REVERSER UPPER AFT CORNER INSIDE AREA IS DELAMINATED AND CRACKED AT THE CORNER AND IS BENT JUS T INBOARD ON A RETAINER. COMPLIED WITH MRAS 5T2020626JT1 AND 5T2020826JTAND GE TNSM 78-32-03 REPAIR NR 6. 2 L 7 2 4F RT A35EU 2002091600081 20020916 00081 EU 2002 9 16 DHL2002363523 1 20020809 A 3213 D520181 SLEEVE AIRBUS 300 A300B4203 3930306 EU NR 8 AXLE FLAKING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 C-CHECK, NR 8 AXLE PROTECTIVE SLEEVE HAS INTERNAL BLISTERING AND FLAKING ON NICKEL PLATING. REMOVED AND REPLACED DAMAGE D PROTECTIVE SLEEVE IAW A300 AMM 32-42-22. 2 L 7 2 4F RT A35EU 2002091600082 20020916 00082 EU 2002 9 16 DHL2002364010 1 20020902 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN MALFUNCTIONED A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 364DH 141 UPPER DECK RT NR 6 SMOKE DETECTOR LIGHT ON. COOLED AIRCRAFT. SMOKE SYSTEM OPS CHECKED NORMAL. 2 L 7 2 4F RT A35EU 2002091600083 20020916 00083 EU 2002 9 16 DHL2002365010 1 20020909 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE MALFUNCTIONED A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 365DH 149 NUMBER 2 ENGINE A-LOOP WILL NOT TEST, B-LOOP OK. PERFORMED OPERATIONAL CHECK OF NR 2 A-LOOP SYSTEM. GROUND OPS CHECKED . NORMAL IAW A-300 M/M 26-12-00. 2 L 7 2 4F RT A35EU 2002091600084 20020916 00084 EU 2002 9 16 DHL2002367009 1 20020826 A 2611 SMOKE WARNING AIRBUS 300 A300B4203 3930306 EU COCKPIT FALSE ACTIVATION A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 367DH 265 ON TAKEOFF OFF AT 120 KNOTS IAS, SMOKE INDICATION ON MASTER WARNING PANEL AND CHIMES ANNUNCIATOR CAUSING NEED TO ABORT T HE TAKEOFF. RETURNED TO RAMP. TESTED SMOKE DETECTOR SYSTEM GOOD PER AMS 26-11-00. 2 L 7 2 4F RT A35EU 2002091600085 20020916 00085 NM 2002 9 16 DHL2002721506 1 20020805 A 5320 INTERCOSTAL BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK, CABIN INTERCOSTAL AT RBL 24 IS CORRODED AT STA 1148. REMOVED INTERCOSTAL AT STA 1148 AND RBL 24 IAW B-7 27 SRM 51-30-2. FABRICATED NEW INTERCOSTAL IAW B-727 SRM 53-10-5. INSTALLED NEW INTERCOSTAL AT STA 1148 RT FROM RBL 20 TO RBL 65 IAW B-727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002091600086 20020916 00086 NM 2002 9 16 DHL2002721507 1 20020805 A 5347 SEAT TRACK BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK, CABIN SEAT TRACK AT LBL 24 IS CORRODED AT STA 1136 AND STA 1156. REMOVED CABIN SEAT TRACK SECTION IAW B 727 SRM 51-30-2. FABRICATED A NEW SECTION OF SEAT TRACK IAW B-727 SRM 57-10-5 FIG 1. INSTALLED NEW SEAT TRACK IAW B-7 27 SRM 53-10-5 FIG 1. 2 L 7 3 4F RT A3WE 2002091600087 20020916 00087 NM 2002 9 16 DHL2002721508 1 20020805 A 5347 SEAT TRACK BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK, CABIN SEAT TRACK AT RBL 45 IS CORRODED AT STA 1177. REMOVED CABIN SEAT TRACK AT STA 1177 AND RBL 45 IAW B-727 SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW B-727 SRM 53-10-5 FIG 1. INSTALLED SECTION OF SEAT TRACK IAW B-727 S RM 53-10-5 FIG 1. 2 L 7 3 4F RT A3WE 2002091600088 20020916 00088 NM 2002 9 16 SWAA021998 1 20020902 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 EEPLS LOOSE AT ROW NR 1. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002091600089 20020916 00089 NM 2002 9 16 SWAA022001 1 20020901 A 3350 57771 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 710SW 27844 EEPLS FWD END CAP LOOSE. REMOVED AND REPLACED FWD END CAP PER MM. 2 L 7 2 4F RT A16WE 2002091600090 20020916 00090 2002 9 16 SWAA022002 4 20020901 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 712SW 27846 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091600091 20020916 00091 2002 9 16 SWAA022003 4 20020829 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING DOOR. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091600092 20020916 00092 2002 9 16 SWAA022004 4 20020831 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091600093 20020916 00093 2002 9 16 SWAA022005 4 20020830 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 754SW 29849 AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING DOOR. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091600094 20020916 00094 2002 9 16 SWAA022009 4 20020831 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091600095 20020916 00095 NM 2002 9 16 SWAA022011 1 20020831 A 2612 0881031007 SWITCH BOEING 737 7373H4 1384600 NM COCKPIT INOPERATIVE A SWAA K NONE J WARNING INDICATION CR CRUISE 1 SW 29 375SW 26583 IN FLIGHT, MASTER FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED FOR NEARLY 5 MINUTES, WOULD NOT CANCEL. REMOVED AND R EPLACED FIRST OFFICER FIRE WARNING BELL CUTOUT SW PER MM. 2 L 7 2 4F RT A16WE 2002091600096 20020916 00096 NM 2002 9 16 SWAA022012 1 20020831 A 3830 AD20131A STUD BOEING 737 7373A4 1384585 NM LAVATORY LOOSE A SWAA K NONE B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CL CLIMB 1 SW 29 673AA 23251 AFTER DEPARTURE AN ELECTRICAL FUME WAS NOTICED, CABIN CREW CONFIRMED FUME. NO CB'S TRIPPED, AC AND DC LOADS ALL NORMAL. FUMES DIMMISHED BUT NOT ELIMINATED. FOUND BLUE FLUID FROM FWD LAV LEAKING AT PRESS FILL. FOUND LOWER ENTRY LIGHT SHO RTED OUT DUE TO LAV SPRAY. REMOVED AND REPLACED BULB PER MM. FOUND FWD LAV PRESS FILL ATTACHMENT STUDS ON TANK LOOSE. REMOVED AND REPLACED FWD LAV PRESS FILL ATTACHMENT SEAL AND TIGHTENED STUDS PER MM 2 L 7 2 4F RT A16WE 2002091600097 20020916 00097 EU 2002 9 16 SWAA022013 2 20020830 A 7321 9368M57P19 MEC BOEING 737 7373A4 1384585 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 ENGINE MALFUNCTIONED A SWAA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 SW 29 669SW 23752 NR 2 ENGINE FLAMED OUT ON DESCENT AT IDLE POWER. FUEL FLOW SHOWED 0, ALL OTHER ENGINE INDICATIONS (OIL PRESS, N1/N2) NO RMAL. RESTARTED ENGINE AT 15,000 FEET AND RAN NORMAL TO LANDING AND SHUTDOWN. REMOVED AND REPLACED FUEL PUMP AND MEC P ER MM. 2 L 7 2 4F 4 F RT A16WE E21EU 2002091600098 20020916 00098 NM 2002 9 16 SWAA022014 1 20020830 A 2730 6544761 PCU BOEING 737 7372T4 1384492 NM ELEVATOR LEAKING A SWAA A UNSCHED LANDING K J F FLUID LOSS WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SW 29 702ML 22054 AIR TURNBACK, AFTER TAKEOFF LOST 'B' HYDRAULIC SYSTEM QUANTITY. FOUND 'B' SYSTEM ELEVATOR PCU LEAKING. REMOVED AND REP LACED 'B' SYSTEM ELEVATOR PCU PER MM. 2 L 7 2 4F A16WE 2002091600099 20020916 00099 NM 2002 9 16 SWAA022015 1 20020902 A 3350 300432 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 415WN 29836 DURING SCHEDULED SERVICE CHECK, FOUND AFT RT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002091600100 20020916 00100 2002 9 16 SWAA022016 4 20020902 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002091600101 20020916 00101 NM 2002 9 16 SWAA022018 1 20020902 A 2782 6544551 ACTUATOR BOEING 737 7373H4 1384600 NM KRUEGER FLAP FAILED A SWAA K NONE F FLT CONT AFFECTED UK UNKNOWN 1 SW 29 636WN 27709 NR 3 KRUEGER FLAP WILL NOT RETRACT. REMOVED AND REPLACED NR 3 KRUEGER FLAP ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2002091600102 20020916 00102 NM 2002 9 16 SWAA022022 1 20020830 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002091600103 20020916 00103 NM 2002 9 16 SWAA022031 1 20020830 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002091600104 20020916 00104 NM 2002 9 16 SWAA022035 1 20020904 A 3350 6556633 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2002091600105 20020916 00105 NM 2002 9 16 SWAA022049 1 20020905 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 763SW 27877 DURING SCHEDULED RON, FOUND EEPLS INOP AND COVER MISSING AT ROW NR 1. RELAMPED AND INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002091600106 20020916 00106 2002 9 16 SWAA022052 4 20020905 A 2565 1061323468 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR DEFECTIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR WOULD NOT LATCH PROPERLY. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091600107 20020916 00107 NM 2002 9 16 SWAA022055 1 20020905 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SPECIAL VISIT, FOUND STR SPLICES CRACKED (3 EA) AT STR 4L, BS 360, BS 727 AND BS 908. REMOVED AND REPL ACED STR SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2002091600108 20020916 00108 NM 2002 9 16 SWAA022057 1 20020905 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (8 EA) AT BS 605 AT STR 2R, BS 706 AT STR 4R, BS 685 AT STR 4R, BS 360 AT STR 9R, BS 500 AT STR 4L, BS 663 AT STR 4L, BS 616 AT STR 5L AND BS 597 AT STR 9L. REMOVED AND REPLA CED STR TIE CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002091600109 20020916 00109 2002 9 16 SWAA022062 4 20020904 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091600110 20020916 00110 2002 9 16 SWAA022064 4 20020908 A 2565 61621 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091600111 20020916 00111 NM 2002 9 16 SWAA022067 1 20020906 A 3350 65C27093 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 OVERHEAD EMERGENCY EXIT SIGN LOOSE AT ROW NR 3. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2002091600112 20020916 00112 NM 2002 9 16 SWAA022070 1 20020905 A 3350 BR2013 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 712SW 27846 DURING SCHEDULED RON, FOUND EEPLS INOP AT ROW NR 1 AND NR 2. REPAIRED LOOSE CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2002091600113 20020916 00113 NM 2002 9 16 SWAA022077 1 20020907 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002091600114 20020916 00114 NM 2002 9 16 DHL2002721517 1 20020807 A 5311 FRAME BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK, BS 910 FRAME CRACKED AT STR 15 RT. REMOVE FASTENERS, BS 910 FRAME STR 15 LT IAW B-727 SRM 51-30-2. CUT OFF AND REMOVED CRACKED SECTION OF STA 910 AND STR 15 LEFT TO STR 14 LEFT IAW B-727 SRM 53-10-4. FABRICATED DOUBLER AN GLE AND FILLER ANGLE IAW B-727 SRM 53-10-4 PAGE 1 SHEET 2 DETAIL I. INSTALLED REPAIR PARTS IAW B-727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002091600115 20020916 00115 NM 2002 9 16 DHL2002721518 1 20020803 A 5311 FRAME BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK, LEFT WHEEL WELL CASTING FRAME BS 930 CRACKED. REMOVED CRACKED STA 930 FRAME LT. LOCATED AND DRILLED-UP NEW STA 930 FRAME LT. INSTALLED NEW STA 930 FRAME LT. 2 L 7 3 4F RT A3WE 2002091600116 20020916 00116 NM 2002 9 16 DHL2002721519 1 20020905 A 5270 SWITCH BOEING 727 727228 1384083 NM CARGO DOOR OUT OF ADJUST A DHLA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SO 01 721DH 19545 DURING ACCEPTANCE FLIGHT OUT OF C-CHECK HEAVY MAINTENANCE CREW DECLARED AN EMERGENCY LANDING DUE TO MAIN CARGO DOOR WARN ING LIGHT S/O PANEL AND LIGHT AT ENTRY DOOR ILLUMINATED AT FL 285 CABIN PSI WAS 7.0 TO 8.0 PSI, NO LOSS OF PRESSURIZATIO N. ADJUSTED AFT JAMB DRIFT PIN SWITCH. OPS CHECKED DOOR PER MM CHAPTER 52-30-0. NO DEFECTS FOUND. PRESSURIZED AIRCRA FT TO 92 PSI, WARNING LIGHT DID NOT ILLUMINATE. 2 L 7 3 4F RT A3WE 2002091600117 20020916 00117 NM 2002 9 16 DHL2002740003 1 20020827 A 3350 PIN BOEING 727 7272Q9 138448M NM BATTERY PACK LOOSE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 740DH 21930 MAIN ENTRY DOOR EMERGENCY LIGHT DOOR DOES NOT ILLUMINATE DURING STANDBY POWER CHECK. CLEANED AND RESECURED BATTERY PACK ELECTRIC PINS. OPS CHECKED GOOD M/M 33-50-00. 2 L 7 3 4F RT A3WE 2002091600118 20020916 00118 NM 2002 9 16 DHL2002742005 1 20020907 A 5230 MECHANISM BOEING 727 727225 1384077 NM CARGO DOOR LACK OF LUBE A DHLA I CABIN DEPRESSURIZATION J WARNING INDICATION NR NOT REPORTED 1 SO 01 742DH 21290 MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT. COMPLETED EMERGENCY CHECKLIST, DOOR LIGHT WENT OUT AT 4.0 DIFF. CLEANED A ND LUBE LOCKING MECHANISM AND MICRO SWITCH. PERFORMED OPS CHECK GOOD SEVERAL TIMES IAW B-727 MM 52-73-11. 2 L 7 3 4F A3WE 2002091600119 20020916 00119 NM 2002 9 16 DHL2002742006 1 20020910 A 1430 COTTER PIN BOEING 727 727225 1384077 NM CARGO DOOR LOOSE A DHLA I CABIN DEPRESSURIZATION J WARNING INDICATION NR NOT REPORTED 1 SO 01 742DH 21290 MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT. COMPLETED EMERGENCY CHECKLIST. FOUND AFT DOOR LOCK PIN MICRO SWITCH STRIK ER COTTER PIN LOOSE. REPLACED PIN INSURING STRIKER SECURITY IAW 727 WIRING DIAGRAM SUPPLEMENT 52-73-11 PG 1, OPS CHECK NORMAL. OK FOR CONTINUED SERVICE. 2 L 7 3 4F A3WE 2002091600120 20020916 00120 NM 2002 9 16 DHL2002742007 1 20020910 A 5270 SWITCH BOEING 727 727225 1384077 NM CARGO DOOR LACK OF LUBE A DHLA I CABIN DEPRESSURIZATION N FALSE WARNING NR NOT REPORTED 1 SO 01 742DH 21290 CARGO DOOR LIGHT ILLUMINATED IN FLIGHT. COMPLETED EMERGENCY CHECKLIST. LIGHT ILLUMINATED AT 8.0 CABIN DIFF. HOOKS UNL OCKED AND DOOR WARNING LIGHTS ILLUMINATED ON DOOR CONTROL PANEL. LIGHT OUT AT 3.0 DIFF. LUBRICATED CARGO DOOR SWITCH I AW B-M/M 20-60-2. PRESSURIZED A/C IAW JRH 6.3. ALL INDICATIONS NORMAL. DOOR OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002091600121 20020916 00121 NM 2002 9 16 DHL2002742008 1 20020912 A 5230 HOOK BOEING 727 727225 1384077 NM CARGO DOOR LACK OF LUBE A DHLA I CABIN DEPRESSURIZATION J WARNING INDICATION NR NOT REPORTED 1 SO 01 742DH 21290 MAIN CARGO DOOR LIGHT ILLUMINATED AT FL 298. COMPLETED EMERGENCY CHECK LIST. LIGHT ILLUMINATED AT 8.0 CABIN DIF. HOOK S UNLOCKED AND DOOR WARNING LIGHTS ILLUMINATED ON DOOR CONTROL PANEL. LIGHTS WENT OUT AT 3 PSI CABIN DIF. INSPECTED DO OR LATCH HOOKS & SWITCH OPERATION FOR OPERATION. LUBRICATED LATCH HOOKS. CYCLED DOOR SEVERAL TIMES IAW AE M/M CHAPTER 24 PAGE 36, CHECKS NORMAL. 2 L 7 3 4F A3WE 2002091600122 20020916 00122 NM 2002 9 16 DHL2002745009 1 20020910 A 2612 WARNING SYSTEM BOEING 727 727224 1384076 NM COCKPIT MALFUNCTIONED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 745DH 20665 NR 2 ENG FIRE WARNING WILL NOT TEST IN COCKPIT. PERFORMED OPS CHECK OF NR 2 ENGINE FIRE WARNING, OPS GOOD IAW 26-11-001 . 2 L 7 3 4F A3WE 2002091600123 20020916 00123 NM 2002 9 16 DHL2002747005 1 20020902 A 2612 LIGHT BOEING 727 727224 1384076 NM COCKPIT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 747DH 22253 ENGINE NR 1 FIRE BOTTLE DISCHARGE BUTTON IS NOT ILLUMINATED DURING TEST. RELAMPED NR 1 ENGINE FIRE BOTTLE DISCHARGE BUT TON, OPS CHECK GOOD IAW 727 M/M 33-10-00. 2 L 7 3 4F A3WE 2002091600124 20020916 00124 NM 2002 9 16 DHL2002755004 1 20020905 A 3350 1000677 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 887MA 21857 EMERGENCY EXIT LIGHT OVER FWD ENTRY DOOR WON'T TEST. REPLACED EMERGENCY EXIT LIGHT ASSY. TESTS OK PER MM 33-50-01. 2 L 7 3 4F A3WE 2002091600125 20020916 00125 NM 2002 9 16 2002F00870 1 20020601 A 5320 651593727 ANGLE BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7644U 20038 AT B-CHECK, DURING INSPECTION OF LOWER SILL BEAM, FOUND CRACK IN SUPPORT ANGLE EXTENDING FROM BOTTOM FASTENER HOLE, AT S TATION 680. (M) 2 L 7 3 4F A3WE 2002091600126 20020916 00126 NM 2002 9 16 2002F00871 1 20020531 A 5320 SPLICE BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CRACK AT FORWARD CARGO COMPARTMENT, ON LEFT STRINGER SPLICE, AT STATION 685 STRINGER 26L. (M) 2 L 7 3 4F A3WE 2002091600127 20020916 00127 NM 2002 9 16 2002F00872 1 20020527 A 5730 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION ON RIGHT WING TOP SKIN, AT LEADING EDGE SPAR, AT STATION 655. (M) 2 L 7 3 4F A3WE 2002091600128 20020916 00128 NM 2002 9 16 2002F00873 1 20020527 A 5730 SKIN BOEING 727 727222 1384073 NM RT WING CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND CORROSION AT RIGHT WING TOP SKIN, AT LEADING EDGE SPAR, AT APPROXIMATELY WING STATION 464. (M) 2 L 7 3 4F A3WE 2002091600129 20020916 00129 NM 2002 9 16 IU62002F00000 1 20020327 A 2923 654468311 HOUSING BOEING 737 737 UTILSYS NM HYD SYSTEM CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 11084 THE HOUSING IS CRACKED ON THE LEFT HAND SIDE OF PORT NR 1. 2 L 7 2 4F RT A16WE 2002091600130 20020916 00130 NM 2002 9 16 IU62002F00002 1 20020326 A 3230 65446922 HOUSING BOEING 737 737 UTILSYS NM MODULE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING IS CRACKED IN (D) PRIORITY PORT. 2 L 7 2 4F RT A16WE 2002091600131 20020916 00131 NM 2002 9 16 C7WA200200028 1 20020913 A 2782 1U1110 ACTUATOR BOEING 727 727231 1384079 NM BROKEN A C7WA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 17 54354 21986 LOST ALL OF "A" SYSTEM HYDRAULIC WHEN CLIMBING OUT OF 15,000 FEET.RETURNED TO TUS WITHOUT FURTHER INCIDENT. 2 GALLONS R EMAINING AFTER TAXI-IN.FOUND BROKEN #4 KRUEGER FLAP ACTUATOR. REMOVED AND REPLACED.OPS CHECK OK I/A/W M.M. 27-00-81 2 L 7 3 4F A3WE 2002091600132 20020916 00132 NM 2002 9 16 2002F00874 1 20020524 A 5330 SKIN BOEING 727 727222 1384073 NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7635U 19908 AT C-CHECK, FOUND DENT ON FUSELAGE SKIN AT STATION 481, BELOW STRINGER 18R. (M) 2 L 7 3 4F A3WE 2002091600133 20020916 00133 SO 2002 9 16 ASOA02285 1 20020521 A 5713 12016085002 STRINGER EMB 120 EMB120RT 3260202 SO RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 244AS 120073 DURING HANGAR MAINTENANCE IN TXK, THE RIGHT WING NR 10 STRINGER WAS FOUND CRACKED AT THE OUTBOARD FORWARD EDGE OF THE NR 1 FUEL PANEL. MAINTENANCE REPAIRED THE CRACK IN THE RIGHT WING NR 10 STRINGER BY INSTALLING A SPLICE. THIS WORK WAS A CCOMPLISHED IAW SRM 57-20-03. (M) 2 L 7 2 4T RT A31SO 2002091600134 20020916 00134 EA 2002 9 16 ASOA02286 1 20020522 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 843AS 7310 FLT 4505 - DURING A SCHEDULED INSPECTION IN XNA, THE RIGHT EXTERNAL EMERGENCY LIGHT IN THE NR 2 POSITION WAS INOPERATIVE . MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002091600135 20020916 00135 EU 2002 9 16 ASOA02287 1 20020523 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 531AS 454 DURING C-CHECK INSPECTION IN BNA, THE UPPER FLANGE OF THE FLOORBEAMS AT FRAMES 36, 39 AND 40 HAD SURFACE CORROSION BEYON D LIMITS AROUND THE NUTCLIP HOLES FROM STRINGER 14 LEFT TO STRINGER 14 RIGHT. MAINTENANCE REPAIRED THE CORRODED FLOORBE AM UPPER FLANGES IAW ASA EO 72-53-0132. (M) 2 H 7 2 4T RT A53EU 2002091600138 20020916 00138 NE 2002 9 16 MEX2002175 2 20020506 A 7412 103538754 EXCITER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LT ENGINE FAILED A ASMF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 23 838AM 49397 FLT 495 - MEX-MID - AIRCRAFT RETURNED TO GATE DUE TO IGNITION FAILING DURING LEFT ENGINE STARTING IGNITION BOC AND START VALVE WERE REPLACED IAW MM 74-10-01 AND 80-10-02. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002091600139 20020916 00139 NM 2002 9 16 USAA020131 1 20020405 A 5414 SKIN BOEING 737 7373B7 1384580 NM RT PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 48107 23311 PHL - FOUND ON WALKAROUND, SKIN CRACKED AND MISDRILLED FASTENR HOLE .375 INCH, CRACK BEYOND RIVET RIGHT ENGINE PYLON OUT BOARD. REPAIRED PER TYPICAL REPAIR 54-50-07. (M) 2 L 7 2 4F RT A16WE 2002091600140 20020916 00140 NM 2002 9 16 USAA020132 1 20020325 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 522AU 42848 23857 TPA - FOUND STRINGER HAS DEFECTIVE FASTENER HOLES, FS 616, S3L STRINGER TIE CLIP. REMOVED TEMP REPAIR, SPLICED IN NEW S ECTION OF STRINGER PER SRM 53-00-03 FIG 203. (M) 2 L 7 2 4F RT A16WE 2002091600141 20020916 00141 NM 2002 9 16 USAA020133 1 20020409 A 5210 SKIN BOEING 737 737301 1384611 NM DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 45478 23930 TPA - FOUND SKIN CRACKED .25 INCH, LOWER AFT CORNER OF LOWER HINGE CUT OUT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 52-10-12. (M) 2 L 7 2 4F RT A16WE 2002091600142 20020916 00142 NM 2002 9 16 USAA020134 1 20020411 A 5312 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 45478 23930 TPA - FOUND BULKHEAD WEB CRACKED TWO PLACES 2.5 INCH EACH, FS 663.75, RBL 45, W/W FORWARD BULKHEAD WEB. INSTALLED TWO D OUBLERS PER EA 94296A. (M) 2 L 7 2 4F RT A16WE 2002091600143 20020916 00143 NM 2002 9 16 CALA0200461 1 20020913 A 5320 STIFFENER BOEING 737 7373T0 1384582 NM BS 1016-1022 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 INSPECTION FOUND CENTER STIFFENER ON AFT PRESSURE BULKHEAD FORWARD FACE CORRODED ON R/H SIDE, IN BILGE, BS 1016-1022. RE PAIRED STIFFENER IAW SRM 51-70-11 AND 53-80-08. 2 L 7 2 4F RT A16WE 2002091600144 20020916 00144 NM 2002 9 16 CALA0200462 1 20020915 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 52 TO RBL 52. THE UPPER CAP WAS REMOVED AND A NEW "T" CHORD REPAIR WAS INSTALLED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2002091600145 20020916 00145 NM 2002 9 16 CALA0200463 1 20020916 A 5730 DOUBLER BOEING 737 7373T0 1384582 NM R/W I/B T/E CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 INSPECTION FOUND A 2" CRACK IN R/H WING UPPER I/B T/E PANEL DOUBLER, WBL 80. THE DOUBLER WAS REMOVED AND REPLACED IAW SR M 51-70-11. 2 L 7 2 4F RT A16WE 2002091600146 20020916 00146 EU 2002 9 16 02FDEA00648 1 20020913 A 2730 A27371145000000 CABLE AIRBUS 310 A310 EU N/A CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 451FE 303 ELEVATOR CONTROL CABLES AZ737114000000 (E2R1) & A2731145000000 (E2RC) AT SUPPORT PULLIES BS 4467 - FR 84 SEVERELY CORR ODED. ** S/D ** COMING 2 L 7 2 4F RT A35EU 2002091600147 20020916 00147 EA 2002 9 16 COMA0260524 1 20020913 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 THE R/H SIDE FUSELAGE SKIN WAS DENTED AT FS 674.2, WL60.CUT OUT THE DAMAGED SKIN. FABRICATED AND INSTALLED A REPAIR DOUB LER I/A/W WVAC EO 601R-53-3456. 2 L 7 2 4F RT A21EA 2002091600148 20020916 00148 SO 2002 9 16 C2XA02BT053 1 20020915 A 3200 852701 SWITCH EMB 145 EMB145ER 3260211 SO FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 27 14942 145037 EWR---CO4131, CREW REPORTED, "ON TAKEOFF GOT LND GEAR AIR/GND FAIL. THEREFORE AIRRETURNED." MAINTENANCE REMOVED AND REPL ACED LEFT HAND PROXIMITY SWITCH ON SHOCKABSORBER IAW EMB145 MM #32-63-01. EXTENDED AND RETRACTED LANDING GEAR OPS.CHECKE D GOOD IAW EMB145 MM #32-30-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002091600149 20020916 00149 EA 2002 9 16 COMA0260525 1 20020914 A 5210 RETAINER SEAL CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 THE PAX DOOR SEAL STRIKERS WERE DAMAGED AT FS 310 ADN FS 349, WL 83-85.REMOVED THE DAMAGED AREA AND FABRICATED AND INSTA LLED REPAIR STRIPS I/A/W REO 601R-52-11-008 ISSUE B. 2 L 7 2 4F RT A21EA 2002091600150 20020916 00150 EA 2002 9 16 COMA0260526 1 20020914 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 THE FUSELAGE SKIN FORWARD OF THE PAX DOOR AT FS 310, WL83 TO 85 WAS DAMAGED.(WHILE PERFORMING SKIN REPAIR THE INTERCOSTA L BEHIND THE REPAIR AREA WAS FOUND TO BE SLIGHTLY DAMAGED/GOUGED.)REMOVED THE DAMAGED AREA OF SKIN. FABRICATED AND INSTA LLED REPAIR FILLER AND DOUBLERS I/A/W REO 601R-53-21-180. (THE SLIGHTLY DAMAGED/GOUGED AREA ON THE SUPPORTING INTERCOSTA L WAS BLENDED I/A/W WVAC EO 601R-53-3461.) 2 L 7 2 4F RT A21EA 2002092000091 20020920 00091 SO 2002 9 20 C2XA02BT054 1 20020914 A 3150 80069424RW WARNING SYSTEM EMB 135 EMB135LR 3260305 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 14516 145323 EWR---CO3873, CREW REPORTED, UPON GEAR RETRACTION LANDING GEAR AURAL WARNING SOUNDED. RECYCLED GEAR WARNING SOUNDED AGA IN. AIR RETURNED TO NEWARK. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED AURAL WARNING UNIT IAW EMB145 MM 31-51-01 . OPS CHECKED AND TEST FLOWN SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002091600151 20020916 00151 EA 2002 9 16 COMA0260527 1 20020912 A 5300 601R3501252 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS 625.0 CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 962CA 15504 7123 RH OBLIQUE ANGLE IS CRACKED AT FS 625.0 P/N 601R35012-52.REPAIRED RH OBLIQUE ANGLE AT F.S. 625.0 P/N 601R35012-52 I/A/W CANADAIR REO 601R-53-61-100. 2 L 7 2 4F RT A21EA 2002091600152 20020916 00152 NM 2002 9 16 AWXA200200886 1 20020913 A 3350 3416402 CONNECTOR BOEING 757 7572S7 1384962 NM SEAT ROW 10 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 0 0 23323 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 10 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMO VED AND REPLACED A BAD WIRE HARNESS CONNECTOR AT SEAT ROW 10 L/H IAW SWPM 20-10-13, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002091600153 20020916 00153 EU 2002 9 16 MALA020559 1 20020907 A 3240 AE20612 CONTROL BOX BAC 146 AVRO146RJ85A 1500097 EU DEFECTIVE A MALA O OTHER J WARNING INDICATION LD LANDING 1 GL 15 513XJ E2329 DURING FLIGHT #3690 ENROUTE TO DTW, WITH YELLOW SYSTEM SELECTED THE ANTI-SKID INOP LIGHT ILLUMINATED. WE FOLLOWED THE QR H AND UPON SELECTION OF GREEN SYSTEM THE LIGHT EXTINUISHED.A/C LANDED IN SDF WITHOUT INCIDENT. A/C FERRIED BACK TO DTW. MAINTENANCE REMOVED AND REPLACED ANTI-SKID CONTROL BOX PN AE20612 SN/OFF 0210, SN/ON 0176 IAW AVRO MM 32-41-47-201 AL O PS CHECK GOOD. 2 H 7 4 4F RT A49EU 2002091600154 20020916 00154 NM 2002 9 16 F3LA200200259 1 20020913 A 5315 FLOORBEAM BOEING 737 737301 138447R NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED VARIOUS STAGES OF CORROSION ON AFT GALLEY/LAVATORY FLOOR BEAMS. REMOVED CORROSION ON FLOOR BEAM AT BS 986.5 PER SRM 53-60-51. CORROSION REMOVAL AT LBL 28 TO LBL 44 WAS OUT OF LIMITS AND REPAIRED PER S RM 53-00-51, FIG. 203. 2 L 7 2 4F RT A16WE 2002091600155 20020916 00155 SO 2002 9 16 C2XA02IA194 1 20020915 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO TAIL INOPERATIVE A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 13997 145298 IAH- THE CREW NOTED THAT RUDDER SYSTEM #2 FAIL ON EICAS IN FLIGHT, THE AIRCRAFT RETURNED TO IAH AND, LANDED WITHOUT INC IDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE #1 RUDDER PRESSURE SWITCH, PERFORMED A OPERATIONAL CHECK , NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002091600156 20020916 00156 SO 2002 9 16 C2XA02IA195 1 20020915 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO TAIL INOPERATIVE A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 13997 145298 IAH- THE CREW NOTED THAT RUDDER SYSTEM #2 FAIL ON EICAS IN FLIGHT, THE AIRCRAFT RETURNED TO IAH, AND, LANDED WITHOUT IN CIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE #2 RUDDER PRESSURE SWITCH, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002091600157 20020916 00157 SO 2002 9 16 C2XA02IA196 1 20020915 A 2720 M835362024M RELAY EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 13997 145298 IAH- FLIGHT 3844, THE CREW NOTED THAT RUDDER SYSTEM #2 INOPERATIVE DURING INITIAL CLIMBOUT, THE AIRCRAFT RETURNED TO IA H, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED RELAY K0378, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002091700001 20020917 00001 EU 2002 9 17 YENA200224 1 20020917 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CEILING PNL 11WL FAULTY A YENA O OTHER O OTHER UK UNKNOWN 1 EA 15 523JB 4568 1506 At LGB, Left Emergency Power Supply Unit Fault.Emergency Power Supply Unit replaced and tested OK IAW MM 33-51-38. 2 L 7 2 4F RT A28NM 2002091700003 20020917 00003 WP 2002 9 17 AT0200071 1 20020823 A 2923 AS19593C PUMP DOUG DC9 DC932 3022066 WP HYD SYSTEM FAILED A ZZDA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 15 849AT 47484 ON ROTATION NOSE WHEEL OFF GROUND AND POSITIVE RATE, THE CALLOUT FOR GEAR WAS INITIATED AND WHEN THE GEAR WAS SELECTED U P, THERE WERE CIRCUIT BREAKER'S POPPING ON AFT CIRCUIT BREAKER PANEL, RADIO FAN OFF LIGHT ILLUMINATED, CREW SMELLED SMOK E BUT THERE WAS NO VISIBLE. THE CIRCUIT BREAKERS THAT POPPED WERE RIGHT AUXILIARY HYDRAULIC PUMP, RIGHT WING MAIN TANK FORWARD (ALL 3 PHASES), LEFT WING MAIN TANK AFT-1 PHASE. REMOVED AND REPLACED RIGHT AUXILIARY HYDRAULIC PUMP AND THE RI GHT BUSS RELAY. INSPECTED SURROUNDING AIRCRAFT WIRING. 2 L 7 2 4F A6WE 2002091700004 20020917 00004 WP 2002 9 17 AT0200073 1 20020818 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 836AT 47397 HEAVY CORRODED FLOOR PANEL STA 230 TO 305, RBL 44 TO RBL 56. REMOVED AND REPLACED SKIN ON FLOOR PANEL IAW DC-9 SRM 51-3 0-2. 2 L 7 2 4F A6WE 2002091700005 20020917 00005 WP 2002 9 17 AT0200074 1 20020818 A 5320 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 836AT 47397 HEAVY CORRODED SUBFLOOR PANEL AND INCLUDING AREA BELOW SEAT TRACK AT STA 230 TO 305 RBL 44. CUT OUT CORROSION ON SUBFLO OR, AND INSTALLED REPAIR IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002091700006 20020917 00006 NM 2002 9 17 DHL2002755005 1 20020910 A 2150 A/C PACK BOEING 727 727225 1384077 NM A/C BAY OVERHEATED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 887MA 21857 ELECTRICAL SMOKE AND STRONG BURNING ODOR IN COCKPIT. THIS SITUATION OCCURRED PRIOR TO FOLLOWING WRITE UP, STICK SHAKER. INSPECTED COCKPIT WIRING, NO EVIDENCE OF BURNING. ODOR CAME FROM PACKS THAT OVERHEATED WHILE A/C WAS IN AIR MODE, OPS CHECK GOOD IAW B727 MM 21-12-0. 2 L 7 3 4F A3WE 2002091700007 20020917 00007 WP 2002 9 17 DHL2002805051 1 20020824 A 2611 LAMP DOUG DC8 DC873F 302199F WP SMOKE DETECTOR INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 805DH 46125 NR 3 SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED LAMPS IN NR 3 SMOKE DETECTOR IAW MM 26-10-6. TESTS OK NOW. 2 L 7 4 4F RT 4A25 2002091700009 20020917 00009 WP 2002 9 17 DHL2002806013 1 20020911 A 2612 FIRE WARNING DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A DHLA O OTHER N FALSE WARNING IN INSP/MAINT 1 SO 01 806DH 46002 WHEN NR 3 LOOP-B IS SELECTED MASTER FIRE WARNING LIGHT AND BELL ARE CONTINUOUSLY ACTUATED. LIGHT AND BELL ARE TERMINATE D WHEN LOOP-A IS SELECTED. T/S RANG OUT EACH SECTION OF LOOP WITH METER AND NO DEFECTS NOTED. CLEANED AND RESECURED CO NNECTORS AND SYS OPS CK'S GOOD PER MM REF 20-10-1. 2 L 7 4 4F RT 4A25 2002091700010 20020917 00010 WP 2002 9 17 DHL2002806845 1 20020705 A 5754 5769859163 FITTING DOUG DC8 DC873F 302199F WP L/E SLOT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 LT WING INBOARD SLOT ZEE PAN FITTING CRACKED 2 INCHES XS 250.000. REMOVED ZEE PAN FITTING IAW SRM 51-1-20D PG 21, PERFO RMED ANTI CORROSIVE TREATMENT AND PRIMED EFFECTED AREA IAW SRM 51-1-8B, INSTALLED ZEE PAN FITTING IAW SRM 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2002091700011 20020917 00011 WP 2002 9 17 DHL2002806853 1 20020703 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 LT MLG W/W SUPPORT ANGLE CORRODED AT STA 857.000 LBL 42. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18, FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2. REMOVED FORMER ANGLE IAW SRM 53-2-0 FIG 1F, FABRICATED ANGLE IAW SRM 53-2-0 FIG 1F, INSTALLED FOR MER ANGLE IAW SRM 53-2-0 FIG 1 F. 2 L 7 4 4F RT 4A25 2002091700012 20020917 00012 WP 2002 9 17 DHL2002806855 1 20020726 A 5512 5644330503 SKIN DOUG DC8 DC873F 302199F WP HORIZ STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 LT HORIZ STAB INBOARD L/E ELONGATED HOLES & CORRODED STA XFS 178.750. PERFORMED MAJOR REPAIRS. REMOVED CORROSION LT HO RIZ STAB L/E AT STA XFS178.750. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12-14. TRIMMED OUT DAMAGED AREA. FABRICATED A R EPAIR DOUBLER & TRIPLER AND FILLERS. INSTALLED FILLERS, DOUBLER, TRIPLER ON LT HORIZ STAB INBOARD L/E XFS178.750 WITH N EW FASTENERS EO DHL 020611 ED-3090 EO SEMAN 2002686 AND 2002686 AND SRM 51-1-20D PG 9 AND SRM 51-1-15 PG 1. 2 L 7 4 4F RT 4A25 2002091700013 20020917 00013 WP 2002 9 17 DHL2002806856 1 20020705 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 LT WING OUTBOARD L/E UPPER SKIN CORRODED (STA 578.000-603.750, 628.750-653.750). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 PG 2 FIG 38. REMOVED CORROSION FROM LT OUTBOARD LEADING EDGE UPPER SKIN IAW SRM 51-1-8 PG 17-18 FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT DAMAGED AREA IAW SRM 57-2-1 PG 2 FIG 38. FABRICATED DOUBLER. INSTALLED DOUBLER IAW SRM 57- 2-1 PG 2 FIG 38, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002091700014 20020917 00014 WP 2002 9 17 DHL2002806857 1 20020723 A 5350 5710370501 PANEL DOUG DC8 DC873F 302199F WP FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 LOWER FUS FILLET NR 742 LT EXTERNAL SKIN DELAMINATED. REMOVED FILLET NR 742 LT IAW SRM 51-3-0 PG 1. INSTALLED NEW FILL ET PANEL IAW SRM 51-3-0 PG 1, SRM 51-3-1 PG 1. 2 L 7 4 4F RT 4A25 2002091700015 20020917 00015 WP 2002 9 17 DHL2002806859 1 20020722 A 5730 57696004 SKIN DOUG DC8 DC873F 302199F WP RT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 PERFORMED MAJOR REPAIR IAW EO DHL 020621, ED-3095, EO SEMAN 2002684. BLENDED DAMAGED AREAS. FABRICATED REPAIR DOUBLER IAW EO DHL 020621, ED-3095, EO SEMANS 2002684. INSTALLED DOUBLER ON RT WING L/E LOWER SURFACE STA XFS710.000 IAW EO DHL 020621, ED-3095, EO SEMAN 2002684. 2 L 7 4 4F RT 4A25 2002091700016 20020917 00016 WP 2002 9 17 DHL2002806860 1 20020718 A 5730 57696003 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 81567 46002 LT WING OUTBOARD LEADING EDGE UPPER SKIN HOLES ELONGATED XFS710.000. PERFORMED MAJOR REPAIR IAW EO DHL 020614, ED-3086, EO SEMAN 2002675. TRIMMED OUT DAMAGED SKIN AREA. FABRICATED A REPAIR DOUBLER, A TRIPLER AND A FILLER IAW EO DHL 02061 4, ED-3086, EO SEMAN 2002675. INSTALLED FILLER, DOUBLER, TRIPLER ON LT WING OUTBOARD L/E UPPER SKIN , XFS710.00 IAW EO DHL 020614, ED-3086 EO SEMAN 2002675. 2 L 7 4 4F RT 4A25 2002091700017 20020917 00017 2002 9 17 MWEA020564 4 20020917 A 3414 4057800906 INDICATOR DOUG DC9 DC981 3022081 WP COCKPIT FAILED A MWEA O OTHER S AFFECT SYSTEMS CL CLIMB 1 GL 31 807ME 48033 CAPTAIN'S AIRSPEED INDICATOR FLAGGED AND NEEDLE STUCK AT 80 KNOTS. -- REMOVED AND REPLACED AIRSPEED INDICATOR. 2 L 7 2 4F A6WE 2002091700018 20020917 00018 NM 2002 9 17 DHL7212002515 1 20020807 A 5311 FRAME BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 DURING C-CHECK, BS 940 FRAME (LEFT) CRACKED AT AFT FLOORBEAM ATTACH FLANGE (CONFIRMED BY NDT). STOP DRILLED CRACK IAW B -727 S/B 53-190. LOCATED AND DRILLED-UP ANGLES, DOUBLERS AND RADIUS FILLERS. INSTALLED REPAIR KIT ON FRAME IAW B-727 S /B 727-53-0190. 2 L 7 3 4F RT A3WE 2002091700019 20020917 00019 NE 2002 9 17 VNAA0209007 3 20020905 A 6111 BLADE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PROPELLER OUT OF ADJUST A VNAA O OTHER O OTHER CL CLIMB 1 GL 07 441JS 3059 DURING CLIMBOUT, THE CREW REPORTED THAT THE LEFT HAND FUEL SHUT OFF VALVE IS CLOSED AND THERE WAS A TORQUE SPLIT OF 5 PE RCENT. THE CREW ELECTED TO RETURN TO YOW. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE PERFORMED OPERATIONAL CHECKS ON THE FUEL SHUT OFF VALVE WHICH WERE GOOD. MAINTENANCE THEN ADJUSTED THE BLADE ANGLE IN ACCORDANCE WITH DORNIE R MAINTENANCE MANUAL 61-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091700020 20020917 00020 NE 2002 9 17 2002F00876 2 20020814 A 7532 AC67760 BLEED VALVE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FAULTY G AMTA K NONE J WARNING INDICATION TO TAKEOFF 1 GL 11 522AT 14000 14000 29330 31605 FLIGHT NUMBER 710. ON TAKEOFF AT LAS RIGHT ENGINE EGT 863C BEFORE PULLING BACK. MAINTENANCE REMOVED AND REPLACED IP BL EED VALVE SOLENOID PER MM 75-32-03-4. 2 L 7 2 4F 4 F RT A2NM E12EU 2002091700021 20020917 00021 NE 2002 9 17 2002F00877 2 20020810 A 7532 AC69178 BLEED VALVE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FAULTY G AMTA K NONE M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 GL 11 522AT 29330 31605 FLIGHT NUMBER 716, MAX EPR T/O FROM LAS; RIGHT ENGINE EGT ROSE TO 859C FOR APPROXIMATELY 5 SECONDS. MAINTENANCE REMOVED AND REPLACED HP3 LEFT SOLENOID PER MM 75-32-05-4 AND RIGGED ENGINE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002091700022 20020917 00022 NM 2002 9 17 PCAA0209106 1 20020916 A 2611 8006223 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM FALSE ACTIVATION A PCAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 13 810EX 27612 5235 308 LGA-MHT FLIGHT#3534. CREW REPORTED DURING TAKEOFF, BAGGAGE COMPARTMENT SMOKE WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNE D TO FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE MASTER WARNING CONTROL BOX AND PERFORMED TEST OF SMOKE DETECTOR. N O FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091700023 20020917 00023 NE 2002 9 17 AT0200075 2 20020904 A 7250 EN131 TURBINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 2 ENGINE FAILED A ZZDA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 15 959AT 55021 NR 2 ENGINE FAILED IN CLIMB AT 9,600 FEET HEARD BANG AND SUDDEN YAW TO RIGHT. TURBINE GAS TEMPERATURE INDICATIONS AT 11 50 CELSIUS RIGHT ENGINE INSTRUMENTS SPOOLED DOWN TO ZERO. ENGINE RIGHT BEARING OVERHEAT ALERT AND ENGINE RIGHT SYSTEM F AIL ALERT. REMOVED AND REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002091700024 20020917 00024 WP 2002 9 17 AT0200077 1 20020810 A 5321 FLOORBOARD DOUG DC9 DC9 3022002 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 836 47397 CPCP, METALLIC FLOORBOARDS AND HONEYCOMB STRUCTURE INSPECTION. LEVEL 2 CORROSION FINDINGS. 2 L 7 2 4F A6WE 2002091700025 20020917 00025 NE 2002 9 17 SABA020087 2 20020822 A 7261 BEARING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 2 ENGINE LEAKING A SABA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 33 883CC 162 120097 AIRCRAFT 883 ON FLIGHT 5098 FROM CINCINNATI TO CHARLOTTE : DURING CRUISE FLIGHT, PILOT PULLED BACK ON POWER AND A BURNT OIL SMELL WAS REPORTED IN THE CABIN AND FLIGHT DECK. NO EMERGENCY WAS DECLARED AND AIRCRAFT CONTINUED TO CHARLOTTE. AI RCRAFT LANDED IN CHARLOTTE WITH NO OTHER PROBLEMS. MAINTENANCE FOUND THE FORWARD BEARING AREA FOR NUMBER TWO ENGINE LEA KING OIL. ENGINE WAS REMOVED AND REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 2002091700026 20020917 00026 NE 2002 9 17 2002F00821 2 20020819 A 7200 ENGINE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RIGHT MALFUNCTIONED G AMTA K NONE R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 11 528AT 30887 31743 FLIGHT NUMBER 337, RIGHT ENGINE WOULD NOT REACH MAX TAKEOFF EPR (1.73) WITH EEC AND ENGINE LIMITER ON. HOWEVER, RIGHT E NGINE REACHED REQUIRED STANDARD EPR (1.68). TAKEOFF WITH EEC AND ENGINE LIMITER OFF NOT CHECKED. RIGHT ENGINE PARAMETE RS WERE NORMAL IN CLIMB. 2 L 7 2 4F 4 F RT A2NM E12EU 2002091700027 20020917 00027 NE 2002 9 17 2002F00878 2 20020813 A 7532 AC67760 BLEED VALVE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FAULTY G AMTA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 11 522AT 14000 14000 29330 31604 FLIGHT NUMBER 217. DURING GO-AROUND AT LAS RIGHT ENGINE WENT TO EGT 858. ENGINE REMAINED 50 DEGREES APPROX WARMER THAN LEFT ENGINE. MAINTENANCE REMOVED AND REPLACED LEFT IP BLEED VALVE SOLENOID IN ACCORDANCE WITH MM 75-32-03, RAN ENGINE, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2002091700028 20020917 00028 NM 2002 9 17 2002F00879 1 20020803 A 7711 LK83104 PITOT HEAD BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE MISSING G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 31749 LEFT ENGINE WILL NOT MAKE T/O POWER WITH EEC'S ON, WILL MAKE T/O POWER WITH EEC'S OFF. MAINTENANCE FOUND LEFT PF4 EPR R AKE ASSY MISSING 1 PITOT HEAD, MADE TEMPORARY REPAIR PER MM 77-11-04-2. CHECKED ENGINE CONTROLS PER AMM 76-11-00-501, P ER FIM 71-06-00 SHEET 2, BLOCK 5. MADE ADJUSTMENT TO MICRO ADJUSTER AT ARROWHEAD DISCONNECT TO ALLOW RIG PINS TO BE INS TALLED. 2 L 7 2 4F 4 F RT A2NM E12EU 2002091700029 20020917 00029 NE 2002 9 17 2002F00880 2 20020819 A 7320 FFG022AD GOVERNOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE DEFECTIVE G AMTA K NONE R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 11 528AT 6413 6413 30887 31743 FLIGHT NUMBER 337, RIGHT ENGINE WOULD NOT REACH MAX T/O EPR (1.73) WITH EEC AND ENG LIMITER ON. HOWEVER, RIGHT ENGINE R EACHED REQUIRED STANDARD EPR (1.68). T/O WITH EEC AND ENG LIMITER OFF NOT CHECKED. RIGHT ENGINE PARAMETERS WERE NORMAL IN CLIMB. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE FFG IN ACCORDANCE WITH MM 73-21-01-4. 2 L 7 2 4F 4 F RT A2NM E12EU 2002091700030 20020917 00030 NE 2002 9 17 2002F00881 2 20020716 A 7321 356A7065G152 EEC BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAULTY G AMTA K NONE R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 11 513AT 3743 3743 32449 31795 FLIGHT NUMBER 218, LEFT EPR GAUGE WOULD NOT GO TO COMMANDED EPR DURING DESCENT/CRUISE. MAINTENANCE REMOVED AND REPLACED LEFT EEC PER M/M 73-21-07, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002091700031 20020917 00031 NM 2002 9 17 AMTA200201097 1 20020813 A 5315 FLOORBEAM LKHEED 1011 1011 N/A-SDR NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 195AT 193C1041 AT 53 - FUSELAGE, 60 - MID FUSELAGE SECTION, LOWER GALLEY FLOORBEAM FS 901, RBL 23 TO RBL 28 IS CORRODED. REPLACED COR RODED T-CAP SECTION IN EXISTING REPAIR PER SRM 51-40-02 AND 53-23-00. 2 L 7 3 4F RT A23WE 2002091700032 20020917 00032 NM 2002 9 17 AMTA200201152 1 20020809 A 5320 SPLICE LKHEED 1011 1011 N/A-SDR NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 195AT 193C1041 FUSELAGE, 10 - MAINFRAME, FWD CENTER SPLICE ANGLE AT FS 328 CAP BL 0 CORRODED. INSTALLED NEW SPLICE ANGLE AT BL 0 FWD S IDE OF FS 328 CHORD PER L-1011 SRM 51-40-0. 2 L 7 3 4F RT A23WE 2002091700034 20020917 00034 NM 2002 9 17 QXEA0201040 1 20020715 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - FLOORBEAM SEAT TRACK NR 7 ATTACH HOLE OVERSIZED AT APPROXIMATELY 405.737 AND YR9.25. REPAIRED IAW HORIZON AIR EA 2-53-405, FIGURE 4. 2 H 7 2 4T RT A13NM 2002101800030 20021018 00030 NM 2002 10 18 2002UALA01414 1 20020907 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 CABIN FLOOR SUPPORT CORRODED AT STATION 327 RBL 40-55. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH STRAP DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101800033 20021018 00033 NM 2002 10 18 2002UALA01418 1 20020909 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 AFT PIT STATION 1420 LEFT HAND FRAME ABOVE STRINGER 25L IS DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTA LLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101800040 20021018 00040 NM 2002 10 18 2002UALA01420 1 20020908 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE LIGHTNING STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 AFTER THE LIGHTNING STRIKE WAS REMOVED AT BODY STATION 1261 BETWEEN STRINGER 30-31 HAS TOO MUCH MATERIAL REMOVED FROM TH E SKIN. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800043 20021018 00043 NM 2002 10 18 2002UALA01423 1 20020909 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 UPPER FUSE SKIN REQUIRES EXCESSIVE MATERIAL REMOVAL TO ELIMINATE DAMAGE AROUND SKY RADIO ANTENNA DOUBLER, APPROX STA 727 , STR 2R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA, MANUFACTURED, AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800044 20021018 00044 NM 2002 10 18 2002UALA01424 1 20020906 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 CABIN STA 847, STR 9R FRAME WEB CRACKED AT AIR GRILL ATTACH POINT. MAJOR REPAIR ACCOMPLISHED. CUT DAMAGED AREA AND FAB RICATED NEW PART AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800118 20021018 00118 NM 2002 10 18 2002UALA01425 1 20020906 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 CABIN STRINGER CLIP AT STA 773, STR 10L WAS CRACKED. MAJOR REPAIR ACCOMPLISHED. REMOVED CRACKED CLIP AND REPLACED IT W ITH A NEW ONE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800121 20021018 00121 NM 2002 10 18 2002UALA01428 1 20020908 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 CABIN STA 907, STR 4L. FOUND 2 EA CRACKS IN STRINGER AROUND FASTENERS. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800124 20021018 00124 NM 2002 10 18 2002UALA01432 1 20020908 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 LT CABIN FRAME AT STA 400 IS CRACKED JUST ABOVE STR 9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800126 20021018 00126 NM 2002 10 18 2002UALA01434 1 20020908 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 LT CABIN FRAME IS CRACKED AT FASTENER HOLE JUST ABOVE AND INBOARD OF STR 9L. MAJOR REPAIR ACCOMPLISHED. END OF CRACK D AMAGE REMOVED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800128 20021018 00128 NM 2002 10 18 2002UALA01438 1 20020910 A 5531 SPAR CAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 VERTICAL STABILIZER FORWARD SPAR CAP DAMAGED AT APPROX FIN STA 108.00. MAJOR REPAIR ACCOMPLISHED. DAMAGED AREA REMOVED AND EXTRUSION REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800129 20021018 00129 NM 2002 10 18 2002UALA01439 1 20020910 A 5347 SEAT TRACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 AFT CABIN STATION 920, WL 208, RBL 47, END OF SEAT TRACK CORRODED AT FASTENER. MAJOR REPAIR ACCOMPLISHED. CUT OUT SEAT TRACK, INSTALLED NEW TRACK WITH DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002091700035 20020917 00035 NM 2002 9 17 2002UALA01431 1 20020908 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 FWD CABIN STR 2R IS DRILLED INTO ABOVE STRINGER CLIP AT STA 380. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SECTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002091700036 20020917 00036 NM 2002 9 17 QXEA0201041 1 20020714 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE LIGHTNING STRIKE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - LIGHTNING STRIKE BURN EXIT MARK, LEFT HAND LOWER FUSELAGE AT STATION X361.0, Z-84. REPAIRED IAW HORIZON AIR EA 2- 53-408. 2 H 7 2 4T RT A13NM 2002091700037 20020917 00037 NM 2002 9 17 QXEA0201042 1 20020716 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - RIGHT HAND FUSELAGE SKIN IS CREASED AT X446-X450, Z107.0. REPAIRED IAW HORIZON AIR EA 2-53-407. 2 H 7 2 4T RT A13NM 2002091700038 20020917 00038 NM 2002 9 17 QXEA0201062 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - NR 10 RIGHT HAND OUTBOARD SEAT TRACK BOTTOM CORROSION AT X406.0. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091700039 20020917 00039 NM 2002 9 17 QXEA0201063 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 7 RIGHT HAND INBOARD SEAT TRACK AT STATION X406 HAS CORROSION ON BOTTOM. REPAIRED IAW DHC-8 RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002091700040 20020917 00040 NM 2002 9 17 QXEA0201064 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 7 RIGHT HAND INBOARD SEAT TRACK INBOARD FLANGE AT STATION X396.0 IS PITTED. REPAIRED IAW DHC-8 RD 8-53-833. 2 H 7 2 4T RT A13NM 2002091700041 20020917 00041 NM 2002 9 17 QXEA0201065 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 4 LEFT HAND INBOARD SEAT TRACK BOTTOM CHAFED BY TRIM PIECES AT STATIONS X291.0, X320.0, X387.0 AND X410.0. REPA IRED IAW DHC-8 RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002091700042 20020917 00042 NM 2002 9 17 QXEA0201066 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 4 LEFT HAND INBOARD SEAT TRACK TOP HAS PITTING AT STATION X391.0. REPAIRED IAW DHC-8 RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002091700043 20020917 00043 NM 2002 9 17 QXEA0201067 1 20020722 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- WING TO FUSELAGE FAIRING SUPPORT STRUCTURE WEB SKIN IS CRACKED AND CHAFED ON AFT SIDE OF WEB SKIN FROM BLEED AIR T- DUCT. REPAIRED IAW DHC-8 RD 8-53-5437. 2 H 7 2 4T RT A13NM 2002091700044 20020917 00044 NM 2002 9 17 QXEA0201068 1 20020720 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- FLAP CHAFING AGAINST NACELLE FAIRING STRUCTURE. REPAIRED IAW DHC-8 RD 8-57-1549 AND RD 8-57-1734. 2 H 7 2 4T RT A13NM 2002091700045 20020917 00045 NM 2002 9 17 QXEA0201069 1 20020721 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- CORROSION ON ANGLE BELOW FLOORBOARD 145AZ AT STATION X597.5 AND Z99. REPAIRED IAW DHC-8 SRM 51-20-11, 51-20-16, 51 -40-11, AND 51-20-36. 2 H 7 2 4T RT A13NM 2002091700046 20020917 00046 NM 2002 9 17 QXEA0201070 1 20020721 A 3220 ARM DHAV DHC8 DHC8202 2809007 NM NLG GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NOSE LANDING GEAR TRAILING ARM HAS NICKS AND GOUGES ALONG LEADING EDGE. REPAIRED IAW DHC-8 RD 8-32-289. 2 H 7 2 4T RT A13NM 2002091700047 20020917 00047 NM 2002 9 17 QXEA0201071 1 20020720 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- THERE ARE GOUGES AND SCRATCHES IN UPPER SPAR CAP OF RIGHT HAND WING FROM STATION YW297 TO YW324. REPAIRED IAW DHC- 8 RD 8-57-2054. 2 H 7 2 4T RT A13NM 2002091700048 20020917 00048 NM 2002 9 17 QXEA0201072 1 20020720 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM FUSELAGE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- ONE SMOKING RIVET AT AFT WING TO FUSELAGE STRAP/FRAME ON RIGHT HAND UNDERWING. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002091700049 20020917 00049 2002 9 17 QXEA0201073 4 20020721 A 3445 ANTENNA DHAV DHC8 DHC8202 2809007 NM TCAS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- LOWER FUSELAGE TCAS ANTENNA HAS CORROSION AROUND SCREW HOLES. REPAIRED IAW DHC-8 SRM 51-20-11 AND 51-20-16. 2 H 7 2 4T RT A13NM 2002091700050 20020917 00050 NM 2002 9 17 QXEA0201074 1 20020721 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- LOWER CORNER OF BAGGAGE DOOR CUTOUT BETWEEN STATIONS 580.000 TO 597.000 HAS NUMEROUS NICKS, SMALL GOUGES, AND PAINT CHIPPING OFF. REPAIRED IAW DHC-8 SRM 51-20-11, 51-20-26 AND 51-20-51. 2 H 7 2 4T RT A13NM 2002091700051 20020917 00051 NM 2002 9 17 QXEA0201075 1 20020720 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- CARGO FLOOR NUT PLATE BRACKET AND FLOOR Z-CHANNEL CHAFED AT X545.0 AFT AND BELOW RIGHT HAND OUTBOARD SEAT TRACK. R EPAIRED IAW DHC-8 SRM 51-20-11, 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2002091700052 20020917 00052 NM 2002 9 17 QXEA0201076 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 1 LEFT HAND OUTBOARD SEAT TRACK TOP HAS CORROSION AT STATION X265.0. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091700053 20020917 00053 NM 2002 9 17 QXEA0201077 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 10 RIGHT HAND OUTBOARD SEAT TRACK TOP HAS CORROSION AT STATION X265.0. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091700054 20020917 00054 NM 2002 9 17 QXEA0201078 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 10 RIGHT HAND OUTBOARD SEAT TRACK TOP HAS CORROSION AT STATION X296.0. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091700055 20020917 00055 NM 2002 9 17 QXEA0201079 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 10 RIGHT HAND OUTBOARD SEAT TRACK BOTTOM HAS CORROSION AT STATION X328. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091700056 20020917 00056 NM 2002 9 17 QXEA0201080 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 10 RIGHT HAND OUTBOARD SEAT TRACK BOTTOM HAS CORROSION AT STATION X342.0. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091700057 20020917 00057 NM 2002 9 17 QXEA0201081 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 10 RIGHT HAND OUTBOARD SEAT TRACK BOTTOM HAS CORROSION AT STATION X374.0. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091700058 20020917 00058 NM 2002 9 17 QXEA0201082 1 20020720 A 5330 DOUBLER DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- DOUBLER GOUGED AT TOP SIDE OF CARGO DOOR APERTURE. REPAIRED IAW DHC-8 RD 8-53-5461. 2 H 7 2 4T RT A13NM 2002091700059 20020917 00059 NM 2002 9 17 QXEA0201083 1 20020720 A 5330 DOUBLER DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- DOUBLER GOUGED AT TOP SIDE OF CARGO DOOR APERTURE STATION X580.5. REPAIRED IAW DHC-8 RD 8-53-5461. 2 H 7 2 4T RT A13NM 2002091700060 20020917 00060 NM 2002 9 17 QXEA0201084 1 20020723 A 5320 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- PANEL 425AL BOTTOM FLANGE IS CHAFED. REPAIRED IAW DHC-8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002091700061 20020917 00061 NM 2002 9 17 QXEA0201085 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 6 LEFT HAND INBOARD SEAT TRACK HAS CORROSION AROUND THE NUT PLATES AT STATIONS X546.0, X565.0 AND X581.0. REPAI RED IAW DHC-8 SRM 51-40-11, 51-20-16, 51-20-36 AND RD 8-53-784. 2 H 7 2 4T RT A13NM 2002091700062 20020917 00062 NM 2002 9 17 USAA020135 1 20020328 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 778AU 31481 24980 PIT - FOUND FRAME CRACKED .25 INCH, STATION 747 BETWEEN STRINGERS L8/L9. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002091700063 20020917 00063 NM 2002 9 17 USAA020136 1 20020321 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 778AU 31481 24980 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 4 INCH AREA, LBBL 13.80 STATION 787-847. SPLICED IN NEW SECTION OF FLOOR S UPPORT FROM STATION 785-880 PER SRM 53-30-53 FIG 203. (M) 2 L 7 2 4F RT A16WE 2002091700064 20020917 00064 NM 2002 9 17 USAA020137 1 20020315 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 31974 24996 PIT - FOUND FRAME CRACKED .500 INCH, FS 867 BETWEEN S8 AND S9 RIVET HOLE IN CLIP. INSTALLED DOUBLER AND FILLER PER TYPI CAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002091700065 20020917 00065 NM 2002 9 17 USAA020138 1 20020315 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 31974 24996 PIT - FOUND FRAME CRACKED .500 INCH, FS 440 BETWEEN S8 AND S9 RIVET HOLE IN CLIP. INSTALLED DOUBLER AND FILLER. (M) 2 L 7 2 4F RT A16WE 2002091700066 20020917 00066 NM 2002 9 17 USAA020139 1 20020315 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 31974 24996 PIT - FOUND FRAME CRACKED .500 INCH, FS 727B BETWEEN S8 AND S9 RIVET HOLE CLIP. INSTALLED DOUBLER AND FILLER PER TYPICA L REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002091700067 20020917 00067 NM 2002 9 17 USAA020140 1 20020322 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 31974 24996 PIT - FOUND FRAME CRACKED .500 INCH, FS 727F BETWEEN S8-S9 RIVET HOLE CLIP. INSTALLED DOUBLER AND FILLER PER TYPICAL RE PAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002091700068 20020917 00068 NM 2002 9 17 USAA020141 1 20020322 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 31974 24996 PIT - FOUND FRAME CRACKED.500 INCH, FS 787 BETWEEN S8-S9 RIVET HOLE CLIP. INSTALLED DOUBLER AND FILLER PER TYPICAL REPA IR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002091700069 20020917 00069 NM 2002 9 17 USAA020142 1 20020322 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 31974 24996 PIT - FOUND FRAME CRACKED .500 INCH, FRAME STATION 727D BETWEEN S8-S9 RIVET HOLE CLIP. INSTALLED DOUBLER AND FILLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002091700070 20020917 00070 NM 2002 9 17 USAA020143 1 20020322 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 31974 24996 PIT - FOUND FRAME CRACKED .500 INCH, STATION 867 BETWEEN S8-S9 RIVET HOLE CLIP. INSTALLED DOUBLER AND FILLER PER TYPICA L REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002091700071 20020917 00071 NM 2002 9 17 USAA020144 1 20020326 A 5320 CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 24996 PIT - FOUND CLIP CRACKED .75 INCHES, STATION 305, NEAR MED UPPER HINGE CUT OUT. REMOVED AND REPLACED CLIP PER STANDARD PRACTICE. (M) 2 L 7 2 4F RT A16WE 2002091700072 20020917 00072 NM 2002 9 17 USAA020145 1 20020325 A 5510 6549873501 HINGE FITTING BOEING 737 7374B7 1384702 NM HORIZ STAB WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 31974 24996 PIT - FOUND SUPPORT FITTING WORN BEYOND LIMITS, HINGE PLATE MOUNTING HOLES WORN, LEFT HORIZONTAL NR 6 HINGE, HORIZ STATI ON 213.32. REMOVED AND REPLACED PART. (M) 2 L 7 2 4F RT A16WE 2002091700073 20020917 00073 NM 2002 9 17 USAA020146 1 20020326 A 5753 6546434302 SKIN BOEING 737 7374B7 1384702 NM T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 31974 24996 PIT - FOUND SKIN DELAMINATED 13.5 INCHES BY 8 INCHES, 39 INCHES OUTBOARD OF INBOARD EDGE RIGHT INBOARD AFT FLAP. VACUUM COMPOSITE REPAIR (SHOP) PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2002091700074 20020917 00074 NM 2002 9 17 USAA020147 1 20020326 A 5753 SKIN BOEING 737 7374B7 1384702 NM T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 31974 24996 PIT - FOUND SKIN DELAMINATED 13 INCHES BY 4 INCHES, LEFT OUTBOARD AFT FLAP 7 FT 8 INCHES OUTBOARD OF INBOARD EDGE. VACU UM COMPOSITE REPAIR PER 737-400 SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2002091700075 20020917 00075 NM 2002 9 17 USAA020148 1 20020326 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 31974 24996 PIT - FOUND FRAME CRACKED .500 INCH CRACK, FRAME STATION 827 BETWEEN S8 AND S9 AT RIVET ON CLIP. INSTALLED DOUBLER AND FILLER PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2002091700076 20020917 00076 NM 2002 9 17 USAA020149 1 20020322 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 31974 24996 PIT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH AREA, STATION 344 BL0 BEAM. CORROSION LEVEL 2, FABRICATED SECTION, SPLI CE ANGLES PER 53-10-51. (M) 2 L 7 2 4F RT A16WE 2002091700077 20020917 00077 NM 2002 9 17 USAA020150 1 20020410 A 5542 SKIN BOEING 737 7373B7 1384580 NM RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 44868 23862 PIT - FOUND LEADING EDGE RUDDER WORN, 1 INCH BY .25 INCH, 3 LAYERS DEEP, LE L00 SIDE, 95 INCHES FROM TOP RUDDER AND 29 I NCHES FROM TRAILING EDGE. REPAIR PER EA 73763. (M) 2 L 7 2 4F RT A16WE 2002091700078 20020917 00078 NM 2002 9 17 USAA020151 1 20020322 A 5542 SKIN BOEING 737 7374B7 1384702 NM RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 780AU 31804 24997 PIT - FOUND RUDDER WITH SKIN DAMAGE .25 INCH BY .25 INCH AND 1 INCH BY .25 INCH, WITHIN 6 INCHES OF PANEL EDGE OR FASTEN ER LINE. WET LAY UP REPAIR PER EA 73621 AND SRM 50-70-11. (M) 2 L 7 2 4F RT A16WE 2002091700079 20020917 00079 NM 2002 9 17 USAA020152 1 20020410 A 5347 CARGO TRACK BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 780AU 24997 PIT - FOUND TRACK CORRODED 1 INCH BY 2 INCH AREAS, 4 PLACES, TIE DOWN TRACK OVER 26R STATION 787-847. REPLACED WITH FAB RICATED TRACK PER SRM 53-00-53, FIG 202. (M) 2 L 7 2 4F RT A16WE 2002091700080 20020917 00080 NM 2002 9 17 USAA020153 1 20020402 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 448US 32409 24892 PIT - FOUND SKIN CRACKED .15625 CRACK AND SMALL DENT, 6 INCHES FORWARD OF MED DOOR FRAME BETWEEN DOOR HINGES. DOUBLER I NSTALLED PER SRM 53-10-01 FIG 205 AND EA 73704. (M) 2 L 7 2 4F RT A16WE 2002091700081 20020917 00081 NM 2002 9 17 USAA020154 1 20020331 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 448US 32409 24892 PIT - FOUND SKIN CRACKED .15625, LEFT SIDE STATION 306 BETWEEN STRINGER 11 LT - 12 LT. INSTALLED DOUBLER PER EA 73704 A ND SRM 53-10-01. (M) 2 L 7 2 4F RT A16WE 2002091700082 20020917 00082 NM 2002 9 17 USAA020186 1 20020510 A 5542 SKIN BOEING 737 7374B7 1384702 NM RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 446US 31626 24873 PIT - FOUND RUDDER WITH SKIN DAMAGE, 6 INCHES WIDE BY 105 INCHES LONG, AND 5.5 INCHES WIDE BY 40 INCHES LONG, BOTH SIDES OF RUDDER. WET LAY UP REPAIR PER SRM 51-70-17 FIG 18 AND 51-70-11 AND EA 73999. (M) 2 L 7 2 4F RT A16WE 2002091700083 20020917 00083 NM 2002 9 17 USAA020188 1 20020515 A 5514 FITTING BOEING 737 737401 1384701 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 39356 23881 TPA - FOUND FITTING CORRODED .625 INCH, LEFT SIDE HORIZONTAL STAB CENTER SECTION, FRONT SPAR. CORROSION LEVEL 2. REMOV ED CORROSION, BLENDED, SPOT FACE, REPAIRED PER SRM 55-10-10, FIG 103 AND EA 94305. (M) 2 L 7 2 4F RT A16WE 2002091700084 20020917 00084 NM 2002 9 17 USAA020189 1 20020514 A 5230 SKIN BOEING 737 737401 1384701 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 39356 23881 TPA - FOUND SKIN CRACKED .5 INCH, AFT CARGO DOOR SKIN, AFT UPPER CORNER. INSTALLED DOUBLER PER SRM 52-00-01. (M) 2 L 7 2 4F RT A16WE 2002091700085 20020917 00085 NM 2002 9 17 USAA020190 1 20020523 A 5542 65C2584151 SKIN BOEING 737 7374B7 1384702 NM RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 785AU 31532 25024 PIT - FOUND RUDDER DELAMINATED .5 INCH BY .5 INCH, LEFT AND RIGHT WITHIN 6 INCHES OF PANEL EDGE FOR FASTENER LINE. WET LAYUP REPAIR PER SRM 51-70-11 AND 51-70-17, EA 74066. (M) 2 L 7 2 4F RT A16WE 2002091700086 20020917 00086 NM 2002 9 17 USAA020191 1 20020521 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 23316 PIT - FOUND FRAME CRACKED 1 INCH BY 3 INCH CORRODED AREA, FS 500B, BETWEEN STRINGERS 27L AND 28L. REMOVED CORROSION PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002091700087 20020917 00087 NM 2002 9 17 USAA020192 1 20020521 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 46636 23316 PIT - FOUND FRAME CORRODED 1 INCH BY 1 INCH CORRODED AREA, STATION 500B, BETWEEN STRINGERS 28L AND 28R. INSTALLED FABRI CATED SHEAR TIE PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2002091700088 20020917 00088 NM 2002 9 17 USAA020193 1 20020521 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 46636 23316 PIT - FOUND FRAME CRACKED .5 INCH, FS 887 RIGHT AT STRINGER 9R. INSTALLED FRAME DOUBLER PER T/R 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002091700089 20020917 00089 NM 2002 9 17 USAA020194 1 20020521 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 46636 23316 PIT - FOUND FRAME CRACKED .5 INCH, FS 827 RIGHT AT STRINGER 9R. INSTALLED FRAME DOUBLER PER T/R 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002091700090 20020917 00090 NM 2002 9 17 USAA020195 1 20020521 A 5320 SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 46636 23316 PIT - FOUND ANTENNA SUPPORT ZEE 1.25 INCH CRACK, HORIZONTAL LEG OF ANTENNA ZEE SUPPORT STATION 727D AND 727C. REPLACED ZEE SUPPORT PER SRM 51-40-05. (M) 2 L 7 2 4F RT A16WE 2002091700091 20020917 00091 NM 2002 9 17 USAA020196 1 20020521 A 5330 DOUBLER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 46636 23316 PIT - FOUND DOUBLER CRACKED 1 INCH, ANTENNA DOUBLER BETWEEN STATION 727D AND 727E. REPLACED ZEE SUPPORT AND MOUNT BRACK ET PER SRM 51-40-05. (M) 2 L 7 2 4F RT A16WE 2002091700092 20020917 00092 NM 2002 9 17 USAA020197 1 20020521 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 46636 23316 PIT - FOUND FRAME CRACKED 1 INCH, FRAME 807 LEFT AT FASTENER STRINGER 9. INSTALLED ANGLES, SHIMS, STRAP PER T/R 53-10-1 4A. (M) 2 L 7 2 4F RT A16WE 2002091700093 20020917 00093 NM 2002 9 17 USAA020198 1 20020522 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 46636 23316 PIT - FOUND SHELF WITH .25 INCH CRACK ON EACH SIDE OF FASTENER, AFT END OF S18 LEFT SHELF AT AFT INBOARD FASTENER. REPL ACED 18A SHELF ASSEMBLY PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002091700094 20020917 00094 NM 2002 9 17 USAA020199 1 20020521 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 46636 23316 PIT - FOUND SHELF WITH 3 AREAS OF CORROSION, 1 INCH ROUND, 2 INCH BY 2 INCH, 2 INCH BY 3 INCH, 6 INCHES TO 8 INCHES AFT OF STATION 706 ON LEFT 18A SHELF. REMOVED CORROSION PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002091700095 20020917 00095 NM 2002 9 17 USAA020200 1 20020521 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 46636 23316 PIT - FOUND 1 INCH ROUND CORRODED AREA, BETWEEN STATION 695 AND 706 ON LEFT SIDE 18A SHELF INBOARD. REMOVED CORROSION P ER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002091700096 20020917 00096 NM 2002 9 17 USAA020225 1 20020702 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 23315 PIT - FOUND RUDDER DELAMINATED SEVERAL PLACES FROM .25 INCHES TO 6 INCHES, 1 PLY DEEP, RIGHT/LEFT RUDDER, R STATION 121. 64 TO 0.00. COMPLETED 200-230 DEGREE WET LAY UP PER SRM 51-70-17 PER EA 74241. (M) 2 L 7 2 4F RT A16WE 2002091700097 20020917 00097 NM 2002 9 17 USAA020226 1 20020706 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 48287 22959 PIT - FOUND SKIN CRACK 2 INCHES LONG, RIGHT SIDE STATION 727E AT STRINGER 24 RIGHT. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER PER EA 74290. (M) 2 L 7 2 4F RT A16WE 2002091700098 20020917 00098 NM 2002 9 17 USAA020228 1 20020514 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 785AU 31532 25024 PIT - FOUND FRAME CRACKED .25 INCHES IN LENGTH, STRINGER 9R, BS 867 AT PSU SUPPORT FITTING. CRACK CUT OUT, DOUBLER INST ALLED, FILLER ADDED PER TYPICAL REPAIR 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002091700099 20020917 00099 NM 2002 9 17 USAA020229 1 20020516 A 5311 BELTFRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 785AU 31532 25024 PIT - FOUND BELTFRAME CRACKED .25 INCH, STRINGER S9L AT FRAME 500C. REPAIRED ANGLES AND CHANNELS PER TYPICAL REPAIR 53- 10-14A. (M) 2 L 7 2 4F RT A16WE 2002091700100 20020917 00100 NM 2002 9 17 USAA020234 1 20020519 A 5320 INTERCOSTAL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 446US 31626 24873 PIT - FOUND INTERCOSTAL CRACKED 1 INCH, FORWARD UPPER CORNER INTERCOSTAL AT BL 0 STATION 344-360. INSTALLED DOUBLER PER EA 73949. (M) 2 L 7 2 4F RT A16WE 2002091700101 20020917 00101 NM 2002 9 17 USAA020239 1 20020530 A 5320 1131253 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND ANGLE CRACKED .5 INCH, FORWARD SERVICE DOOR, FORWARD FRAME UPPER ANGLE S12R-S13R. DEFECTIVE PART REPLACED W ITH IDENT PART N/R. (M) 2 L 7 2 4F RT A16WE 2002091700102 20020917 00102 NM 2002 9 17 USAA020240 1 20020530 A 5320 1131199 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND ANGLE CRACKED .5 INCH, FORWARD SERVICE DOOR FORWARD FRAME LOWER ANGLE S10R-S11R. DEFECTIVE PART REPLACED WI TH IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2002091700103 20020917 00103 NM 2002 9 17 QXEA0201086 1 20020719 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 9 RIGHT HAND INBOARD SEAT TRACK HAS CORROSION AROUND NUT PLATES AT STATIONS X598.0 AND X565.0. REPAIRED IAW DHC -8 RD 8-53-4936. 2 H 7 2 4T RT A13NM 2002091700104 20020917 00104 NM 2002 9 17 QXEA0201087 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 5 LEFT HAND INBOARD SEAT TRACK BOTTOM IS CHAFED BY TRIM PIECES AT STATIONS X448.0, X480.0 AND X510.0. REPAIRED IAW DHC-8 RD 8-53-1239. 2 H 7 2 4T RT A13NM 2002091700105 20020917 00105 NM 2002 9 17 QXEA0201088 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 5 LEFT HAND INBOARD SEAT TRACK INBOARD FLANGE IS GOUGED AT STATION X436.0. REPAIRED IAW DHC-8 RD 8-53-833. 2 H 7 2 4T RT A13NM 2002091700106 20020917 00106 NM 2002 9 17 QXEA0201089 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 9 RIGHT HAND INBOARD SEAT TRACK NEEDS TO BE CLEANED AND PRIMED AT SEAT ATTACH POINTS. GOUGES IN BOTTOM OF TRACK AT STATION X531.0 AND X542.0. REPAIRED IAW DHC-8 RD 8-53-4936. 2 H 7 2 4T RT A13NM 2002091700107 20020917 00107 NM 2002 9 17 QXEA0201090 1 20020719 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 9 RIGHT HAND INBOARD SEAT TRACK HAS CORROSION AT NUT PLATES AT STATION X533.0 AND X546.0. REPAIRED IAW DHC-8 RD 8-53-4936. 2 H 7 2 4T RT A13NM 2002091700108 20020917 00108 NM 2002 9 17 QXEA0201091 1 20020718 A 5411 FRAME DHAV DHC8 DHC8202 2809007 NM LT PYLON GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- LEFT HAND A FRAME WHERE RETRACTION ACTUATOR FITTING MOUNT, JUST BELOW TOP IS GOUGED. REPAIRED IAW DHC-8 RD 8-54-11 78. 2 H 7 2 4T RT A13NM 2002091700109 20020917 00109 NM 2002 9 17 QXEA0201092 1 20020720 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- TWO GOUGES NEXT TO EACH OTHER ON THE TOP CENTER INBOARD SIDE OF OUTBOARD WINGS. REPAIRED IAW DHC-8 RD 8-57-1734 AN D RD 8-57-1549. 2 H 7 2 4T RT A13NM 2002091700110 20020917 00110 NM 2002 9 17 QXEA02011232 1 20020813 A 2120 ODOR DHAV DHC8 DHC8202 2809007 NM COCKPIT DETECTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 354PH 498 SEA- FUMES IN COCKPIT. INSPECTED AIRCRAFT, SMELLED FOR FUMES WITH EXTERIOR POWER ON AND RAN ENGINES WITH AC GENERATORS ONLINE FOR 30 MINUTES USING VARIOUS SYSTEMS. NO EVIDENCE OF FUMES NOTICED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 2002091700111 20020917 00111 NM 2002 9 17 QXEA0201124 1 20020727 A 7810 NOZZLE DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 2 FINGERNAIL DECK UNDERSIDE HAS CHAFE DAMAGE FROM FUEL/OIL/HYDRAULIC DRAIN LINE. REPAIRED IAW DHC-8 RD 8-54-097 . 2 H 7 2 4T RT A13NM 2002091700112 20020917 00112 NM 2002 9 17 QXEA0201125 1 20020726 A 5755 BRACKET DHAV DHC8 DHC8202 2809007 NM SPOILER GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- LEFT HAND WING OUTBOARD SPOILER CENTER HINGE POINT INBOARD SIDE OF INBOARD BRACKET GOUGED AND SCRATCHED AROUND PIVO T. REPAIRED IAW HORIZON AIR EA 2-57-176. 2 H 7 2 4T RT A13NM 2002091700113 20020917 00113 NM 2002 9 17 QXEA0201126 1 20020725 A 5755 HINGE BRACKET DHAV DHC8 DHC8202 2809007 NM SPOILER SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- THERE IS A DEEP SCRATCH ON THE SURFACE OF THE LEFT HAND CENTER HINGE BRACKET ON THE LEFT HAND OUTBOARD ROLL SPOILER . REPAIRED IAW DHC-8 SRM 51-20-36 AND HORIZON AIR EA 2-57-175. 2 H 7 2 4T RT A13NM 2002091700114 20020917 00114 NM 2002 9 17 QXEA0201128 1 20020720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- NR 1 LEFT HAND OUTBOARD SEAT TRACK BOTTOM HAS CORROSION AT STATION X297.0. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091700115 20020917 00115 NM 2002 9 17 QXEA0201129 1 20020723 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- PITTING ALONG THE INBOARD SIDE OF THE NR 4 FLAP TRACK ON LEFT HAND WING. REPAIRED IAW HORIZON AIR EA 2-57-169. 2 H 7 2 4T RT A13NM 2002091700116 20020917 00116 NM 2002 9 17 QXEA0201130 1 20020726 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- CRACK IN FUSELAGE FRAME JUST BELOW PANEL 122BR ON FRAME 151.6 JUST BELOW STRINGER 27. REPAIRED IAW HORIZON AIR EA 2-53-409. 2 H 7 2 4T RT A13NM 2002091700117 20020917 00117 NM 2002 9 17 QXEA0201131 1 20020726 A 5720 MOUNT BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- TOP MOUNT BRACKET CRACKED AT STATION YW139.00 OF FORWARD SPAR LEFT HAND WING. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002091700118 20020917 00118 NM 2002 9 17 QXEA0201132 1 20020726 A 5720 MOUNT BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- BOTTOM MOUNT BRACKET IS CRACKED AT STATION YW139.000 ON FORWARD SPAR OF LEFT HAND WING. REPAIRED IAW DHC-8 SRM 51- 40-00. 2 H 7 2 4T RT A13NM 2002091700119 20020917 00119 NM 2002 9 17 QXEA0201133 1 20020726 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- Z-BRACKET IS CRACKED AT FORWARD SPAR STATION YW58.200 ON LEFT HAND WING. REPAIRED IAW HORIZON AIR EA 2-57-170 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002091700120 20020917 00120 NM 2002 9 17 QXEA0201134 1 20020727 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- UPPER END OF Z-BRACKET IS CRACKED AT FORWARD RIGHT HAND WING SPAR AT STATION Y58.20. REPAIRED IAW HORIZON AIR EA 2 -57-171 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002091700121 20020917 00121 NM 2002 9 17 QXEA0201135 1 20020723 A 5320 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- PANEL 422CT BOTTOM EDGES ARE CHAFED IN SEVERAL PLACES. REPAIRED IAW DHC-8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002091700122 20020917 00122 NM 2002 9 17 QXEA0201136 1 20020723 A 5320 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- PANEL 422BT BOTTOM EDGES ARE CHAFED IN SEVERAL PLACES. REPAIRED IAW DHC-8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002091700123 20020917 00123 NM 2002 9 17 QXEA0201137 1 20020723 A 5320 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- PANEL 422DT BOTTOM HAS CHAFED EDGES. REPAIRED IAW DHC-8 SRM 51-20-11 AND 51-20-36. 2 H 7 2 4T RT A13NM 2002091700124 20020917 00124 NM 2002 9 17 QXEA0201138 1 20020724 A 5541 RIB DHAV DHC8 DHC8202 2809007 NM RUDDER CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- FORE RUDDER CLOSING RIB OUTSIDE SURFACE HAS FRETTING CORROSION AROUND RIVET HOLES. REPAIRED IAW DHC-8 MM TASK 27-2 0-11-030-802, DHC-8 SRM 51-40-06, 51-40-11 AND 27-20-11. 2 H 7 2 4T RT A13NM 2002091700125 20020917 00125 NM 2002 9 17 QXEA0201139 1 20020723 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX- UPPER FORWARD CORNER OF CARGO DOOR SKIN IN BENT. REPAIRED IAW DHC-8 RD 8-52-029, DHC-8 SRM 51-10-21, 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2002091700126 20020917 00126 NM 2002 9 17 QXEA0201146 1 20020807 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS GOUGES AT X282.400. REPAIRED IAW DHC-82 SRM 51-20-16, PAGE 4, PARAGRAPH 4D. 2 H 7 2 4T RT A13NM 2002091700127 20020917 00127 NM 2002 9 17 QXEA0201147 1 20020807 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS GOUGES IN CENTER AT X310.000. REPAIRED IAW DHC-82 SRM 51-20-16, PAGE 4, PARAGR APH 4D. 2 H 7 2 4T RT A13NM 2002091700128 20020917 00128 NM 2002 9 17 QXEA0201148 1 20020807 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS GOUGES AT X342.300. REPAIRED IAW DHC-82 SRM 51-20-16, PAGE 4, PARAGRAPH 4D. 2 H 7 2 4T RT A13NM 2002091700129 20020917 00129 NM 2002 9 17 QXEA0201149 1 20020807 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION AT X421.000. REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 4, PARAGRAPH 4D. 2 H 7 2 4T RT A13NM 2002091700130 20020917 00130 NM 2002 9 17 QXEA0201150 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT X256.000. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091700131 20020917 00131 NM 2002 9 17 QXEA0201151 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS SURFACE CORROSION AT X295.000. REPAIRED IAW RD 8-53-1352 AND SRM 51-20-16, PAGE 4, PARAGRAPH 4D. 2 H 7 2 4T RT A13NM 2002091700132 20020917 00132 NM 2002 9 17 QXEA0201152 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS SURFACE CORROSION AT X380.000. REPAIRED IAW RD 8-53-1352 AND SRM 51-20-16, PAGE 4, PARAGRAPH 4D. 2 H 7 2 4T RT A13NM 2002091700133 20020917 00133 NM 2002 9 17 QXEA0201153 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS SURFACE CORROSION AT X405.737. REPAIRED IAW RD 8-53-1342 AND SRM 51-20-16, PAGE 4, PARAGRAPH 4D. 2 H 7 2 4T RT A13NM 2002091700134 20020917 00134 NM 2002 9 17 QXEA0201154 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS SURFACE CORROSION AT X424.124. REPAIRED IAW RD 8-53-1342 AND SRM 51-20-16, PAGE 4, PARAGRAPH 4D. 2 H 7 2 4T RT A13NM 2002091700135 20020917 00135 NM 2002 9 17 QXEA0201155 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS SURFACE CORROSION AT X438.000. REPAIRED IAW RD 8-53-1342 AND SRM 51-20-16, PAGE 4, PARAGRAPH 4D. 2 H 7 2 4T RT A13NM 2002091700136 20020917 00136 EA 2002 9 17 HNAA0200065 1 20020913 A 2560 4108703 BOTTLE DHAV DHC8 DHC8311 1386006 EA CABIN LEAKING A HNAA H DEACTIVATE SYST/CIRCUITS O OTHER UK UNKNOWN 1 EA 07 333EN 332 332 221 RIGHT HAND DITCHING DAM PREESURE AT 1200 PSI. DITCHING DAM REMOVED AND PUR IN BAG BIN. REPLACED DITCHING DAM NITROGEN B OTTLE AND REINSTALLED DITCHING DAM. 2 H 7 2 4T RT A13NM 2002091700137 20020917 00137 NM 2002 9 17 HNAA0200064 1 20020914 A 3350 66013211X BATTERY PACK DHAV DHC8 DHC8201 2809001 NM CABIN DISCHARGED A HNAA O OTHER L NO TEST UK UNKNOWN 1 EA 07 985HA 29963 770 479 EMERGENCY EXIT RED LIGHTS INOP FROM ROW 2 THROUGH 4 AND ROW 1. FOUND BROKEN WIRES IN ASSY AND DEAD BATERIES. REPLACED ALL SIX EMERGENCY LIGHT BATTERY PACKS AND REPAIRED WIRING AS NCESSARY, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2002091800007 20020918 00007 NE 2002 9 18 CA020524003 2 20020519 A 8500 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT LIGHTNING STRIKE W O OTHER Y ENGINE STOPPAGE LD LANDING 1 CA (CAN) LIGHTENING STRIKE TO NR 1 ENGINE. LT ENGINE SHUT DOWN AS A RESULT OF LIGHTENING STRIKE. CREW NEVER CALLED. MECH FOUND LIGHTENING STRIKE: LT AOA VANE, SEVERAL WINDOWS ALONG LEFT SIDE OF FUSELAGE HAD ARC MARKS AND TAILCONE HAD BURN MA RKS. MECH INSPECTED ENGINE AND FOUND NO BURNS ARCS ETC. RAN ENG AT 75 PERCENT N1 FOR 40 MIN, INSPECTED CHIP DETECTOR - NO FAULTS. FERRIED AIRCRAFT TO COMPLY WITH SECOND PART OF LIGHTENING INSEPECTION.'COMPLIED WITH INSPECTION AND REPAIRS . NO ABNORMALATIES FOUND ON THE ENGINE.AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002091800010 20020918 00010 NM 2002 9 18 CA020828002 1 20020827 A 7312 320115 SHUTOFF VALVE BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE FUEL HEAT STUCK W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) WHILE CLIMBING TO 15,000 70NM EAST OF YUL, NR 2 ENGINE OIL TEMP STARTED CLIMBING INTO YELLOW ARC. COMPLETED QRH CHECKLIST AND AFTER 15 MINUTES ACCOMPLISHED ENGINE SHUTDOWN AND DECISION WAS MADE TO RETURN TO YUL. INVESTIGATION FOUND THAT THE FUEL HEAT VALVE WAS STUCK HALF OPEN. VALVE REPLACED AND CHECKED SERVICEABLE, ALL PARAMETERS CHECKED NORMAL ON FIRST FLIGHT FROM YUL TO YYZ. 2 L 7 2 4F 4 F A16WE E2EA 2002091800011 20020918 00011 NE 2002 9 18 CA020829015 2 20020827 A 7200 ENGINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE NR 3 VIBRATION W E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKE OFF, THE NR 3 THROTTLE WAS RETARDED, THE ENGINE WAS SHUT DOWN DUE TO HIGH VIBRATIONS (2.5 2.7 UNITS) , CHANNEL A&B FROM LOW CHANNEL. THE AIRCRAFT RETURNED TO BASE (YYZ). MAINTENANCE C/OUT A BOROSCOPE AND THE FINDINGS WERE, HP COMPRESSOR STAGE 1, DAMAGE TO MOST OF THE BLADESAND ONE BLADE WAS DAMAGED BEYOUND LIMITS I.A.W. 72-00-00 P.629, THE ENGINE WAS REJECTED. MAINTENANC E WILL REPLACE THE ENGINE 2 L 7 3 4F 4 F A23WE E12EU 2002091800013 20020918 00013 GL 2002 9 18 CA020830002 2 20020715 A 7323 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE MALFUNCTIONED W O OTHER W R INADEQUATE Q C PARTIAL RPM/PWR LOSS HO HOVERING 1 CA (CAN) GOVERNOR REMOVED FOR OVERSPEEDING AND DROOPING. 1 G 7 1 3U 3 U H2SW E4CE 2002091800014 20020918 00014 GL 2002 9 18 CA020830003 2 20020728 A 7323 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE MALFUNCTIONED W O OTHER W R INADEQUATE Q C PARTIAL RPM/PWR LOSS HO HOVERING 1 CA (CAN) GOVERNOR REMOVED FOR OVERSPEEDING AND DROOPING. REMOVED AT11485.1 INSTALLED AT11393.9 DIFFERENCE 91.2 1 G 7 1 3U 3 U H2SW E4CE 2002091800018 20020918 00018 NE 2002 9 18 CA020830022 2 20020823 A 7200 ENGINE BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE NR 2 VIBRATION W O OTHER E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 CA (CAN) RT ENGINE VIBRATION FELT FROM TOP OF DESCENT TO LANDING. NR 2 FUEL LEVER VIBRATING AND DURING TAXI WHEN POWER ADDE D. TURBINE VIBRATION GOES UP TO 2.5 TO 3. 2 L 7 2 4F 4 F A16WE E2EA 2002091800019 20020918 00019 EA 2002 9 18 CA020903001 2 20020903 A 7320 25245009 FUEL CONTROL PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA MIXTURE DAMAGED W O OTHER E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 CA (CAN) PILOT REPORTED UNORTHODOX RT ENGINE PARAMETERS WITH DIFFICULTY IN LEANING IN FLIGHT. 'COKE BOTTLE' CHECK C/OUT ON AC22ES. NO DEFECT. MAGNETO TIMING CHECKED ONE BAD SPARK PLUG REPLACED. MANIFOLD INTAKES CHECKED. PERFORMANCE IMPROVED ON RUN-UP BUT NOT PERFECT. IDLE MIXTURE ADJUSTMENTS TRIED BUT IN VAIN. DISCONNECTED MIXTURE CONTROL IN VIEW OF REPLACING S ERVO. MECHANIC SENSED SOME 'GRIPPING' INTERNALLY WHEN MOVING MIXTURE FULL RANGE. REPLACEMENT OF SERVO BY RECERTIFIED REP AIRED UNIT AND ADJUSTMENT OF IDLE MIXTURE PROVED CORRECT. 1 L 7 2 3O 3 O A20SO E14EA 2002091800020 20020918 00020 EA 2002 9 18 CA020903002 2 20020812 A 7240 301474 FUEL NOZZLE EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA ENGINE FAILED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) AT TERMINATING A ROUTINE 7 DAYS INSPECTION ON THE AIRCRAFT, THE MECHANIC SPOTTED A ROUND DISCOLOURED 'DOT' ON THE ENGINE CASING, TWO FUEL NOZZLES WERE REMOVED TO INVESTIGATE WITH A BORESCOPE TO CONFIR M APPARENT DAMAGE IN THE FUEL COM BUSTION LINER. ENGINE WAS THEN 'SPLIT' FOR A HSI THE NOZZLES WERE SENT TO SAE (LAST NOZZLE OVERHAUL DONE BY ANOTHER FIR M) AND THEIR FUEL NOZZLE TEARDOWN INSPECTION REPORT. CONFIRMED FAILURE OF NR 11 NOZZLE WHICH IN TURN CAUSED DAMAGE TO T HE COMBUSTION CHAMBER LINER DECLARED SCRAP. 1 L 7 2 4T 4 T A21SO E4EA 2002091800021 20020918 00021 EU 2002 9 18 CA020903003 1 20020813 A 5630 M105233027 TRACK BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL WINDOW BROKEN W A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 CA (CAN) LT AFT SLIDING WINDOW TRACK BONDING FAILURE TO WINDOW PANEL WHEN TRACK BONDING FAIL THE SLIDING WINDOW FLEW AWAY F ROM AIRCRAFT. BONDING OF WINDOW TRACK TO PANEL FAILED. HELICOPTER LANDED AND NO FURTHER DAMAGED. 1 G 7 2 3U 3 U H3EU E4CE 2002091800022 20020918 00022 WP 2002 9 18 CA020903006 2 20020812 A 7321 GEAR BEECH 100 B100 1152919 CE GARRTT TPE331 TPE331* 01514 WP FUEL CONTROL BROKEN W A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE THE LT ENGINE QUIT AS IF NO MORE FUEL COULD REACH IT. THE PILOT TURNED AROUND AND LANDED AT ITS ORI GINAL DEPARTING POINT WITHOUT ANY PROBLEM. THE FCU GEAR THAT ENGAGES THE FCU WAS FOUND BROKEN. 1 L 7 2 4T 3 T A14CE E2WE 2002091800023 20020918 00023 EU 2002 9 18 CA020903012 1 20020803 A 6510 1053025136 BRACKET BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL T/R DRIVE DEFORMED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE TWO BOLTS THAT HOLDS THE TAIL ROTOR SHAFT OUTER RING BEARING TO THE BEARING BRACKET AT THE FRAME. BOLTS BECAM E LOOSE OVER A PERIOD OF 40 HOURS SINCE LAST INSPECTION, BOLT HOLES BECAME ELONGATED. BEARING ASSEMBLY STARTED TO SPIN AND HIT THE TAIL ROTOR SHAFT COVER. MARKS LEFT ON THE COVER WERE NOTICED ON THE NEXT CHECK BY THE TECHNICIAN. TAIL RO TOR STIFFENER AND THE TAILBOOM SKIN WERE ALSO HIT BY THE BEARING OUTER RING. 1 G 7 2 3U 3 U H3EU E4CE 2002091800024 20020918 00024 EU 2002 9 18 CA020903013 1 20020829 A 7920 MY2078810 HOSE AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE ENGINE PYLON LEAKING W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA (CAN) DURING TAKE-OFF ROLL, THE PILOT WAS UNABLE TO MAKE ADAPTED EPR ON LT ENGINE. THE PILOT INITIATED REJECTED TAKE-O FF. THE FLIGHT CREW ADVISED ATC, AND RETURNED TO THE MAINTENANCE FACILITY. AMO HAS DETERMINED THAT HOSE ASSEMBLY WAS L EAKING, GIVING A FALSE EPR INDICATION. A NEW HOSE WAS INSTALLED AND ENGINE PERFORMANCE RUN COMPLIED WITH SATISFACTORIL Y. 2 L 7 2 4F 4 F RT A7EU E7EA 2002091800026 20020918 00026 NM 2002 9 18 CA020904002 1 20020825 A 2722 112003 ACTUATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE RUDDER BYPASSING W A UNSCHED LANDING K F FLUID LOSS FLT CONT AFFECTED CL CLIMB 1 CA (CAN) 10 MINUTES AFTER TAKEOFF, RUDDER ISOLATE CAUTION LIGHT ILLUMINATED. PILOTS NOTICED A LOSS OF HYDRAULIC FLUID AND DECIDED TO RETURN TO AIRPORT. MAINTENANCE FOUND FLUID IN TAIL BUT COULD NOT ISOLATE WHERE FLUID CAME FROM. SUSPECT NR 1 RUDDER ACTUATOR MAY HAVE BYPASSED FLUID, UNIT WILL BE REMOVED AND SENT TO OVERHAUL FACILITY FOR INSPECTION. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002091800029 20020918 00029 EA 2002 9 18 CA020904008 1 20020821 A 4990 APU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU BAY FAILED W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 CA (CAN) ENGINE GEN NR 2 INOP - DISPATCHED IAW MEL 24-11-1-2 ON THE FLT. (APU GEN REQUIRED TO OPERATE CONTINUOUSLY DURING FLT) DURING FLT APU OIL TEMP CAUTION MSG APPEARED. DIVERTED. APU HAS BEEN REPAIRED AND AIRCRAFT RETURNED IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002091800033 20020918 00033 NM 2002 9 18 QXEA0201156 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS GOUGES ON OUTBOARD FLANGE AT X426.000. REPAIRED IAW RD 8-53-1352 AND SRM 51-20- 16, PAGE 4, PARAGRAPH 4D. 2 H 7 2 4T RT A13NM 2002091800034 20020918 00034 NM 2002 9 18 QXEA0201157 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS CORROSION AT X467.000. REPAIRED IAW RD 8-53-1342 AND SRM 51-20-16, PAGE 4, PARA GRAPH 4D. 2 H 7 2 4T RT A13NM 2002091800035 20020918 00035 NM 2002 9 18 QXEA0201158 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS CORROSION AT X488.500. REPAIRED IAW RD 8-53-1342 AND SRM 51-20-16, PAGE 4, PARA GRAPH 4D. 2 H 7 2 4T RT A13NM 2002091800036 20020918 00036 NM 2002 9 18 QXEA0201159 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS GOUGES ON OUTBOARD RAIL AT X456.500. REPAIRED IAW RD 8-53-1342 AND SRM 51-20-16 , PAGE 4, PARAGRAPH 4D. 2 H 7 2 4T RT A13NM 2002091800037 20020918 00037 NM 2002 9 18 QXEA0201160 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-LEFT HAND OUTBOARD NR 3 SEAT TRACK HAS SURFACE CORROSION. REPAIRED IAW RD8-53-3644 AND SRM 51-20-16, PAGE 4. 2 H 7 2 4T RT A13NM 2002091800038 20020918 00038 NM 2002 9 18 QXEA0201161 1 20020807 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-RIGHT HAND OUTBOARD NR 11 SEAT TRACK HAS CORROSION. REPAIRED IAW RD8-53-1342 AND SRM 51-20-16, PAGE 4. 2 H 7 2 4T RT A13NM 2002091800039 20020918 00039 NM 2002 9 18 QXEA0201162 1 20020807 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-RIGHT HAND OUTBOARD NR 11 SEAT TRACK IS GOUGED AND HAS SURFACE CORROSION AT X452.000. REPAIRED IAW RD8-53-1342 AND SRM 51-20-16, PAGE 4. 2 H 7 2 4T RT A13NM 2002091800040 20020918 00040 WP 2002 9 18 CA020905001 2 20020820 A 7260 31030351 BEARING 31017263 BEECH 100 B100 1152919 CE GARRTT TPE331 TPE3316252B 01514 WP TORQUE SENSOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ENGINE DISMANTLE TO FIND FAILURE CAUSE OF BEARING. FOUND DAMAGE TO TORQUE SENSOR AND ALL GEAR RELATED. BEARING L OOSENESS WAS THE CAUSE OF THE BEARING DAMAGE. 1 L 7 2 4T 4 T A14CE E2WE 2002091800041 20020918 00041 NM 2002 9 18 QXEA0201163 1 20020807 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-RIGHT HAND OUTBOARD NR 11 SEAT TRACK IS GOUGED AND HAS SURFACE CORROSION AT X467.000. REPAIRED IAW RD8-53-1342 AND SRM 51-20-16, PAGE 4. 2 H 7 2 4T RT A13NM 2002091800042 20020918 00042 NM 2002 9 18 QXEA0201164 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-LEFT HAND INBOARD NR 5 SEAT TRACK IS GOUGED IN CENTER OF TRACK AT X501.000. REPAIRED IAW RD8-53-1339 AND SRM 51-20- 16, PAGE 4. 2 H 7 2 4T RT A13NM 2002091800043 20020918 00043 NM 2002 9 18 QXEA0201165 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-LEFT HAND INBOARD NR 5 SEAT TRACK HAS SURFACE CORROSION AT X515.000. REPAIRED IAW RD8-53-1339 AND SRM 51-20-16, PAG E 4. 2 H 7 2 4T RT A13NM 2002091800044 20020918 00044 NM 2002 9 18 QXEA0201166 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-RIGHT HAND INBOARD NR 8 SEAT TRACK HAS GOUGES ON INBOARD TRACK RAIL AT X436.000. REPAIRED IAW RD8-53-1339 AND SRM 5 1-20-16, PAGE 4. 2 H 7 2 4T RT A13NM 2002091800045 20020918 00045 EA 2002 9 18 CA020905002 1 20020828 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA (CAN) IN CRUISE, THE COPILOT SIDE WINDOW CRACKED. AIRCRAFT COMPLETED THE FLIGHT AND LANDED TO THE DESTINATION AIRPORT. THE AIRCRAFT WAS THEN FERRIED WHERE THE WINDOW WAS REPLACED. THE AIRCRAFT HAD 663 FH AND 581 FC AT THE TIME OF THE EVEN T. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002091800046 20020918 00046 NM 2002 9 18 QXEA0201167 1 20020812 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-RIGHT HAND INBOARD NR 7 SEAT TRACK HAS GOUGES AT X411.000. REPAIRED IAW DHC8 SRM 51-20-16, PAGE 4, SRM 51-20-36 AND SRM 20-16-01. 2 H 7 2 4T RT A13NM 2002091800048 20020918 00048 NM 2002 9 18 QXEA0201168 1 20020811 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX- LOWER FORWARD BAG DOOR STOP AT STATION 564.5 HAS .060 WEAR INTO STOP. REPAIRED IAW RD8-53-104. 2 H 7 2 4T RT A13NM 2002091800049 20020918 00049 NM 2002 9 18 QXEA0201169 1 20020807 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-NUT PLATE CORRODED AT BAG BAY STEP BULKHEAD JUST OUTBOARD OF PULLEYS ON LEFT HAND SIDE. REPAIRED IAW DHC8 SRM 51-20 -16, PAGE 4 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002091800050 20020918 00050 EA 2002 9 18 CA020905005 1 20020830 A 2730 3094334 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB TRIM JAMMED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) CREW NOTED STAB TRIM RUNAWAY IN THE NOSE DOWN DIRECTION DURING CLIMB FROM ATL WHILE ACCELERATING TO 250 KTS. CREW DECLARED EMERGENCY AND RETURNED. MAINTENANCE CONTROL NOTIFIED. MAINTENANCE FOUND INDICATION OF PILOT'S TRIM SWITCH JAMM ED IN THE MDC. REMOVED AND REPLACED THE PILOT'S STAB TRIM SWITCH. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002091800051 20020918 00051 NM 2002 9 18 QXEA0201170 1 20020809 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-CORROSION AT AFT END OF NR 6 SEAT TRACK AT STATION Y9.250 AND X596.0. REPAIRED IAW RD8-53-4936 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002091800053 20020918 00053 NM 2002 9 18 QXEA0201171 1 20020806 A 5320 ACCESS PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-CORROSION AROUND NUT PLATES STOP AND BOTTOM, ALL AROUND CARGO BAY ACCESS PANEL 144HZ. REPAIRED IAW DHC8 SRM 51-20-1 6, PAGE 4 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002091800054 20020918 00054 NM 2002 9 18 QXEA0201172 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-RIGHT HAND INBOARD NR 7 SEAT TRACK HAS GOUGE IN CENTER OF TRACK AT X280.000. REPAIRED IAW RD8-53-1339 AND SRM 51-20 -16, PAGE 4. 2 H 7 2 4T RT A13NM 2002091800055 20020918 00055 NM 2002 9 18 QXEA0201173 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-RIGHT HAND INBOARD NR 7 SEAT TRACK HAS GOUGES ON INBOARD AND OUTBOARD RAILS AT X282.000. REPAIRED IAW RD8-53-1339 A ND SRM 51-20-16, PAGE 4. 2 H 7 2 4T RT A13NM 2002091800056 20020918 00056 NM 2002 9 18 QXEA0201174 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX- RIGHT HAND INBOARD NR 7 SEAT TRACK HAS GOUGES IN CENTER OF TRACK AT X296.000. REPAIRED IAW RD8-53-1339 AND SRM 51- 20-16, PAGE 4. 2 H 7 2 4T RT A13NM 2002091800057 20020918 00057 GL 2002 9 18 CA020905007 1 20020823 A 5750 GM12715911 SLAT TRACK BOMBDR BD700 BD7001A10 1390006 GL RROYCE BR700 BR700710A220 09500 NE WING WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A 'C' CHECK, PREMATURE WEAR OF THE SLAT TRACK PLATING WAS DISCOVERED (PLATING WORN). IT APPEARS THE WORN SU RFACE PLATING PROCESS WAS USED. TRACK AFFECTED RAIL : LT SLAT NR 1, RAIL NR 2, RT SLAT NR 1, RAIL NR 2, RT SLAT NR 3 , RAIL NR 3 2 L 7 2 4F 4 F RT T00003NY E00061EN 2002091800058 20020918 00058 NM 2002 9 18 QXEA0201175 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX- RIGHT HAND INBOARD NR 7 SEAT TRACK HAS GOUGES ON SEAT TRACK AT X372.000. REPAIRED IAW RD8-53-1339 AND SRM 51-20-16 , PAGE 4. 2 H 7 2 4T RT A13NM 2002091800059 20020918 00059 NM 2002 9 18 QXEA0201176 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-RIGHT HAND INBOARD NR 7 SEAT TRACK HAS GOUGES ON SEAT TRACK AT X409.000. REPAIRED IAW RD8-53-1339 AND SRM 51-20-16, PAGE 4. 2 H 7 2 4T RT A13NM 2002091800061 20020918 00061 NM 2002 9 18 QXEA0201177 1 20020808 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX- A 1 INCH CRACK ON EMPENNAGE FRAME NR 4 FLANGE TIE-IN TO STRINGER NR 4 AT FS 710.000 AND 716.00. REPAIRED IAW RD8-5 5-199 AND SRM 53-20-21, PAGE 6. 2 H 7 2 4T RT A13NM 2002091800063 20020918 00063 NM 2002 9 18 QXEA0201178 1 20020806 A 5542 SKIN DHAV DHC8 DHC8202 2809007 NM RUDDER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-TRAILING RUDDER HAS 2 UPPER STATIC WICKS CHAFING INTO TRAILING EDGE SKIN ON RIGHT HAND SIDE, LOCATED 5TH AND 9TH RIB FROM TOP OF RUDDER. REPAIRED IAW DHC8 SRM 55-40-16, SRM 51-20-11 AND RD8-55-042. 2 H 7 2 4T RT A13NM 2002091800064 20020918 00064 NM 2002 9 18 CA020906003 1 20020904 A 3234 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) ON APPROACH, PILOTS SELECTED THE MLG HANDLE TO DOWN POSITION. GEAR DID NOT EXTEND AND THE PILOTS OBSERVED 3 RED GEAR UNSAFE LIGHTS AND 2 AMBER LIGHTS IN THE SELECTOR HANDLE. AFTER SEVERAL ATTEMPTS, PILOTS DIVERTED WHERE COMPANY MAI NTENANCE WAS AVAILABLE. AN EMERGENCY EXTENSION FOR THE MLG AND NLG WAS CARRIED OUT AND THE GEAR EXTENDED TO THE DOWN AND LOCK POSITION. AN EMERGENCY WAS DECLARED AS A PRECAUTION AND THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON INVESTIGATION I T WAS FOUND THAT THE LANDING GEAR SELECTOR VALVE WAS AT FAULT. THE SELECTOR VALVE WAS REPLACED, GEAR SWINGS CARRIED OUT AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002091800065 20020918 00065 NM 2002 9 18 QXEA0201179 1 20020810 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX- NR 1 NACELLE AFT ALUMINUM LANDING FOR PANEL 412DT HAS A GOUGE IN THE CENTER OF LANDING. REPAIRED IAW DHC8 SRM 51-2 0-11, PAGE 7, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002091800067 20020918 00067 NM 2002 9 18 QXEA0201181 1 20020810 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX- NR 1 NACELLE FORWARD ALUMINUM LANDING FOR PANEL 412DT HAS SCRATCHES ALONG FORWARD SKIN EDGE. REPAIRED IAW DHC8 SRM 51-20-11, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002091800068 20020918 00068 NM 2002 9 18 QXEA0201182 1 20020807 A 5720 INTERCOSTAL DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-CHAFING ON INTERCOSTAL OF WING TO FUSELAGE FAIRING AT STATION YW57.000. REPAIRED IAW DHC8 SRM 51-20-11, PAGE 5. 2 H 7 2 4T RT A13NM 2002091800069 20020918 00069 NM 2002 9 18 MEX2002285 1 20020902 A 4930 O-RING DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE APU FUEL VALVE LEAKING W ASMF K NONE L K NO TEST FLUID LOSS IN INSP/MAINT 1 SW 23 169PL 33430 53175 DURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED NEAR APU FUEL FEED LINE DRAIN. APU WAS TURNED OFF, HOWEVER THE LEAK CON TINUED, THE FUEL PUMP WAS TURNED OFF AND LEAK DISAPPEARED. LINE WAS CHECKED BUT NO DAMAGE WAS FOUND. THE APU FUEL FEE D VALVE WAS DISCONNECTED AND NO LEAKS WERE DETECTED. APU WAS DEFERRED BY MEL, AND REPLACED IAW MM, AND AN O-RING OF DRA IN TUBE WAS CHANGED IAW MM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002091800070 20020918 00070 NM 2002 9 18 QXEA0201183 1 20020807 A 5720 SUPPORT DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-CHAFING ON BRIDGE SUPPORT ASSEMBLY. SUPPORTING WING TO FUSELAGE FAIRING AT STATION YW57.000. REPAIRED IAW DHC8 SRM 51-20-11, PAGE 5. 2 H 7 2 4T RT A13NM 2002091800071 20020918 00071 WP 2002 9 18 MEX2002286 1 20020903 A 3233 567865 LOCK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE NLG ACTUATOR FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 23 501AM 49188 AIRCRAFT RETURNED TO PLATFORM DUE TO A STRONG VIBRATION IN THE NOSE LANDING GEAR. MAINTENANCE CHECKED THE RT NLG DOOR WAS IN THE DOWN POSITION. THE RIGHT NOSE GEAR DOOR LINKAGE ACTUATOR LOCK WAS REPLACED IAW MM. TEST OK. 2 L 7 2 4F 4 F A6WE E2EA 2002091800072 20020918 00072 NE 2002 9 18 2002F00882 1 20020912 A 6210 761509000045 BLADE SKRSKY S76 S76 8143010 NE MAIN ROTOR CRACKED E K NONE O OTHER IN INSP/MAINT 1 SW 09 90421 6746 82 760039 DURING A PREFLIGHT INSPECTION, THE MAIN ROTOR BLADE WAS FOUND TO BE DEBONDING AT STATION 57.75 THROUGH 77.75. THERE WAS A SMALL VOID, 1.25 INCHES, AT STATION 78.25. THERE WAS A SMALL CRACK ON TOP OF THE BLADE AT STATION 187.5. 1 G 7 2 3U H1NE 2002091800074 20020918 00074 NE 2002 9 18 EGR2002F00007 1 20020821 A 3110 LIGHT SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL COCKPIT INOPERATIVE E K NONE O OTHER IN INSP/MAINT 1 EA 17 3122G 14434 760232 890634S NR 2 ENGINE FUEL PRESSURE CAUTION LIGHT, INOPERATIVE. PIN ON NR 2 FUEL PRESSURE SWITCH CONNECTOR PLUG BACKED OUT. REIN STALLED NR 2 FUEL PRESSURE SWITCH CONNECTOR PLUG PIN AND FUNCTION CHECKED GOOD. 1 G 7 2 3U 3 U H1NE E1GL 2002091800075 20020918 00075 NM 2002 9 18 QXEA0201184 1 20020806 A 7110 STRUCTURE DHAV DHC8 DHC8202 2809007 NM COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-CRACK FROM RIVET HOLE AT FORWARD RIGHT HAND CORNER OF LOWER COWL FORWARD SUMP. REPAIRED IAW RD8-54-533. 2 H 7 2 4T RT A13NM 2002091800076 20020918 00076 NM 2002 9 18 QXEA0201185 1 20020805 A 7110 STRUCTURE DHAV DHC8 DHC8202 2809007 NM NR 1 COWLING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-AFT CLOSING MEMBER HAS 4 INCH LONG CHAFE AT CENTER OF TOP FLANGE ON NR 1 LOWER COWL. REPAIRED IAW DHC8 SRM 51-40-11 . 2 H 7 2 4T RT A13NM 2002091800077 20020918 00077 NE 2002 9 18 EGR2002F00009 2 20020620 A 7320 23072726 HYDROMECH UNIT BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE ENGINE LEAKING E EGRA K NONE O OTHER IN INSP/MAINT 1 EA 17 993PA 992 49050 CAEB44106 DURING FLIGHT CREW DETECTED FUEL ODOR AFTER LANDING. PILOT SAW FUEL IN THE NR 2 ENGINE COMPARTMENT. MECHANIC PINPOINTE D FUEL LEAK TO THE AFT SIDE OF THE HMU COMING FROM A PLATE WITH AN ADJUSTOR/CONTROL. 1 G 7 2 3U 3 U RT H9SW E1GL 2002091800078 20020918 00078 EU 2002 9 18 HXSA0000370 1 20020626 A 6210 355A11003020 BLADE SNIAS 350 AS350B2 8680813 EU MAIN ROTOR DELAMINATED B HXSR K NONE O OTHER IN INSP/MAINT 1 AL 05 970TH 837 9011 REMOVED MAIN ROTOR BLADE, DUE TO DELAMINATION OF BLADE TIP. SENT TO AEC FOR INSPECTION. REPLACED. 1 G 7 1 3U H9EU 2002091800079 20020918 00079 NM 2002 9 18 QXEA0201186 1 20020809 A 5330 SKIN PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-REPLACED SKIN PANEL FORWARD OF REAR PRESSURE BULKHEAD BETWEEN STRINGER 17 AND 29 RIGHT HAND. REPAIRED IAW RD8-53-67 09 AND SRM 51-20-16, SRM 51-40-11 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002091800080 20020918 00080 EU 2002 9 18 HXSA0000372 1 20020626 A 6210 355A11003020 BLADE SNIAS 350 AS350B2 8680813 EU MAIN ROTOR DELAMINATED B HXSA K NONE O OTHER IN INSP/MAINT 1 AL 05 970TH 837 9011 REMOVED MAIN ROTOR BLADE, DUE TO DELAMINATION OF BLADE TIP. SENT FOR INSPECTION. REPLACED. 1 G 7 1 3U H9EU 2002091800081 20020918 00081 EU 2002 9 18 HXSA0000373 1 20020708 A 6210 355A11003020 BLADE SNIAS 350 AS350B2 8680813 EU MAIN ROTOR DELAMINATED B HXSA K NONE O OTHER IN INSP/MAINT 1 AL 05 970TH 837 9011 REMOVED MAIN ROTOR BLADE, DUE TO DELAMINATION OF BLADE TIP. SENT TO AEC FOR INSPECTION. REPLACED. 1 G 7 1 3U H9EU 2002091800082 20020918 00082 EU 2002 9 18 KBMA115438 1 20020820 A 6720 350A33214501 PITCH LINK SNIAS 350 AS350BA 8680817 EU TAIL ROTOR CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 925 1864 TAIL ROTOR P/C LINK HAS CRACKED BUSHINGS. REPLACED WITH REPAIRED P/C LINK. 1 G 7 1 3U NC H9EU 2002091800083 20020918 00083 NM 2002 9 18 QXEA0201187 1 20020804 A 5542 SKIN DHAV DHC8 DHC8202 2809007 NM RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-FORE RUDDER RIGHT HAND SIDE SKIN HAS CRACK AT AFT EDGE IN LINE WITH TOP HINGE. REPAIRED IAW DHC8 SRM 51-20-11, PAGE 9, SRM 51-20-36, SRM 51-40-11 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2002091800084 20020918 00084 EU 2002 9 18 KBMA115443 1 20020820 A 2821 446138604 BRACKET SNIAS 350 AS350* EU FUEL FILTER CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 9424 1864 FUEL FILTER BARAKET IS CRACKED ON CORNER. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U H9EU 2002091800085 20020918 00085 NM 2002 9 18 QXEA0201188 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-LEFT HAND INBOARD NR 4 SEAT TRACK HAS CORROSION ON OUTBOARD FLANGE AT X222.000. REPAIRED IAW RD8-53-4473 AND SRM 51 -40-11, RD8-53-1102, SRM 51-40-00, SRM 51-60-00 AND SRM 51-60-11. 2 H 7 2 4T RT A13NM 2002091800086 20020918 00086 EU 2002 9 18 KBMA115444 1 20020820 A 6420 350A33215001 BALL SNIAS 350 AS350BA 8680817 EU T/R SPIDER WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 9424 1864 TAIL ROTOR SPIDER BALL END WORN BEYOND LIMITS. REMOVED AND REPLACED WITH SERVICEABLE BALL END. 1 G 7 1 3U NC H9EU 2002091800087 20020918 00087 EU 2002 9 18 KBMA115458 1 20020901 A 5630 350120261 WINDOW SNIAS 350 AS350BA 8680817 EU CABIN DOOR SEPARATED E KBMA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 WP 19 270SH 9485 1864 CABIN DOOR WINDOW DEPARTED AIRCRAFT. REPLACED WITH SERVICEABLE WINDOW. 1 G 7 1 3U NC H9EU 2002091800088 20020918 00088 EU 2002 9 18 KBMA115459 1 20020903 A 2150 0522844 MOTOR SNIAS 350 AS350BA 8680817 EU CONDENSOR SEIZED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 5221 2337 CONDENSOR MOTOR LOCKED UP. REPLACED WITH NEW MOTOR. 1 G 7 1 3U NC H9EU 2002091800089 20020918 00089 NM 2002 9 18 QXEA0201189 1 20020811 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-CARGO DOOR APERTURE LOWER AFT DOOR STOP IS WORN. REPAIRED IAW RD8-53-104. 2 H 7 2 4T RT A13NM 2002091800090 20020918 00090 EU 2002 9 18 KBMA115463 1 20020821 A 2150 094110112 BRUSHES SNIAS 350 AS350B2 8680813 EU EVAP BLOWER INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 345SH 1824 3345 AIRCRAFT EVAPORATOR BLOWER BRUSHES (INOPERATIVE) REQUIRE REPLACEMENT. REPLACED BRUSHES WITH NEW. 1 G 7 1 3U H9EU 2002091800091 20020918 00091 EU 2002 9 18 KBMA115464 1 20020826 A 6730 350A23002065 GUIDE SNIAS 350 AS350BA 8680817 EU T/R SERVO WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 1188P 11790 11790 RIGHT SIDE TAIL ROTOR SERVO SLIDE GUIDE WORN THROUGH. REPLACED WITH NEW GUIDE. 1 G 7 1 3U NC H9EU 2002091800092 20020918 00092 NM 2002 9 18 QXEA0201190 1 20020807 A 5753 SPAR DHAV DHC8 DHC8202 2809007 NM T/E FLAP GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-GOUGES EXIST ON FLAP FRONT SPAR WEB ADJACENT TO INBOARD SIDE OF ACTUATOR BRACKET. REPAIRED IAW DHC8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002091800093 20020918 00093 NM 2002 9 18 QXEA0201191 1 20020806 A 5542 SKIN DHAV DHC8 DHC8202 2809007 NM RUDDER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-TRAILING RUDDER HAS 2 UPPER STATIC WICKS CHAFING INTO TRAILING EDGE SKIN ON RIGHT HAND SIDE, LOCATED AT 5TH AND 9TH RIB FROM TOP OF RUDDER. REPAIRED IAW DHC8 SRM 51-20-31 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2002091800094 20020918 00094 2002 9 18 KBMA115466 4 20020814 A 2300 73949 SWITCH SNIAS 350 AS350BA 8680817 EU RADIO INOPERATIVE E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 230SH 5148 2337 ICS / TRANSMIT SWITCH ON CYCLIC STICK DOES NOT ALLOW TRANSMISSION. REPLACED WITH SERVICEABLE SWITCH. 1 G 7 1 3U NC H9EU 2002091800095 20020918 00095 NM 2002 9 18 QXEA0201192 1 20020806 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-ADF BOTTOM ANTENNA HAS SURFACE CORROSION ON SKIN. REPAIRED IAW DHC8 SRM 51-20-11 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002091800096 20020918 00096 EU 2002 9 18 KBMA115468 1 20020814 A 7160 350A54108421 SEAL SNIAS 350 AS350BA 8680817 EU AIR INTAKE WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 5148 2337 AIR INTAKE SEAL WORN. REPLACED WITH NEW SEAL. 1 G 7 1 3U NC H9EU 2002091800097 20020918 00097 NM 2002 9 18 QXEA0201193 1 20020806 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-TCAS BOTTOM ANTENNA HAS SURFACE CORROSION ON SKIN. REPAIRED IAW DHC8 SRM 51-20-11 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002091800098 20020918 00098 EU 2002 9 18 KBMA115469 1 20020817 A 2150 SD508 COMPRESSOR SNIAS 350 AS350B2 8680813 EU AC SYSTEM INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 1707 3296 AIR CONDITIONER QUIT BLOWING COLD AIR, ONLY HOT AIR. REPLACED WITH SERVICEABLE COMPRESSOR. 1 G 7 1 3U H9EU 2002091800099 20020918 00099 NM 2002 9 18 QXEA0201194 1 20020806 A 5541 RIB DHAV DHC8 DHC8202 2809007 NM RUDDER DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-FORE RUDDER, LOWER RIB IS DENTED. REPAIRED IAW DHC8 SRM 51-40-11 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2002091800100 20020918 00100 EU 2002 9 18 KBMA115470 1 20020811 A 2150 350A6011 BLOWER SNIAS 350 AS350B2 8680813 EU CONDENSOR INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 1665 3296 AIR CONDITIONER BLOWS HOT AIR. REPLACE CONDENSOR BLOWER. 1 G 7 1 3U H9EU 2002091800101 20020918 00101 EU 2002 9 18 KBMA115471 1 20020812 A 2622 194543C EXTINGUISHER SNIAS 350 AS350BA 8680817 EU CABIN INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 2273A 4748 2273 FIRE EXTINGUISHER CHARGE DECREASED INTO RED ZONE. INSTALLED SERVICEABLE EXTINGUISHER. 1 G 7 1 3U NC H9EU 2002091800102 20020918 00102 2002 9 18 KBMA115473 4 20020819 A 2300 16061 BATTERY SNIAS 350 AS350BA 8680817 EU RADIO DISCHARGED E KBMA K NONE L NO TEST IN INSP/MAINT 1 WP 19 2273A 2273 RADIO SYSTEM FLICKERS, VOLT METER READS 18 VOLTS. REPLACED WEAK BATTERY WITH SERVICEABLE BATTERY. 1 G 7 1 3U NC H9EU 2002091800103 20020918 00103 2002 9 18 KBMA115474 4 20020810 A 2312 CONNECTOR SNIAS 350 AS350BA 8680817 EU COCKPIT DAMAGED E KBMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 19 1188P 11705 2347 FIRE LIGHT FLICKERS ON AFTER TAKEOFF. REPLACED EYE LET CONNECTOR ON LEFT FORWARD. 1 G 7 1 3U NC H9EU 2002091800104 20020918 00104 EU 2002 9 18 KBMA119546 1 20020729 A 7712 305731366 INDICATOR SNIAS 350 AS350BA 8680817 EU ENG TORQUE STUCK E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 270SH 268 1864 TORQUE GAUGE WAS STUCK ON 27 PERCENT. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2002091800107 20020918 00107 NM 2002 9 18 CALA0200465 1 20020916 A 5720 ANGLE BOEING 737 7373T0 1384582 NM L/W O/B AFT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 INSPECTION FOUND A 3" CRACK IN L/H WING LOWER/AFT O/B SUPPORT ANGLE. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2002091800108 20020918 00108 NM 2002 9 18 CALA0200466 1 20020918 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 927-947 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND A 2" CRACK IN WEB L-ANGLE AT STA 927-947. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002091800113 20020918 00113 EA 2002 9 18 COMA0260528 1 20020917 A 5220 601R330501 LATCH CNDAIR CNDAIR CL600 CL6002B19 1900309 EA CREW EXCAPE HATC CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 987CA 11335 7198 7199 UPON INSPECTION MECHANIC FOUND OUTHE HANDLE OF CREW EXCAPE HATCH STUCK IN THE DOWN POSITION. wOULD NOT "POP UP" WHEN OP EN BUTTON WAS DEPRESSED.REMOVED HANDLE ASSAMBLEY AND INSTALLED SERVICABLE HANDLE IAW CRJ SRM 51-42-06 pg 1-18. 2 L 7 2 4F RT A21EA 2002091800114 20020918 00114 NM 2002 9 18 QXEA0201195 1 20020803 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-CARGO DOOR APERTURE LOWER AFT EDGE PIECE HAS DEEP GOUGE ON EDGE. REPAIRED IAW DHC8 SRM 53-10-00. 2 H 7 2 4T RT A13NM 2002091800115 20020918 00115 NM 2002 9 18 QXEA0201197 1 20020807 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-FRAME IS CHAFED AT X653.0 Y29.0L Z112.5. REPAIRED IAW DHC8 SRM 51-20-11, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002091800116 20020918 00116 NM 2002 9 18 QXEA0201198 1 20020807 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-FRAME IS CHAFED AT X653.0, Y29.0 AND Z112.5. REPAIRED IAW DHC8 SRM 51-20-11, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002091800117 20020918 00117 EA 2002 9 18 COMA0260530 1 20020915 A 5220 601R330501 LATCH HANDLE CNDAIR CNDAIR CL600 CL6002B19 1900309 EA CREW EXCAPE HATC CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 435CA 3916 7474 7473 UPON INSPECTION MECHANIC FOUND OUTER HANDLE OF CREW EXCAPE HATCH STUCK IN THE DOWN POSITION. WOULD NOT "POP UP" WHEN OP EN BUTTON WAS DEPRESSED.REMOVED HANDLE ASSEMBLEY AND INSTALLED SERVICABLE HANDLE IAW CRJ SRM 51/42/06 pg 1-18. 2 L 7 2 4F RT A21EA 2002091800118 20020918 00118 NM 2002 9 18 USAA020241 1 20020621 A 5743 FITTING BOEING 737 737401 1384701 NM RT MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND AFT SUPPORT FITTING CRACKED .5 INCH, RIGHT MLG AFT SUPPORT FITTING NR 4 UPPER OUTBOARD FASTENER. OVERSIZED HOLES PER TYPICAL REPAIR 57-40-13. (M) 2 L 7 2 4F RT A16WE 2002091800119 20020918 00119 NM 2002 9 18 USAA020242 1 20020621 A 5310 DOOR FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND FRAME CRACKED .25 INCH, FORWARD SERVICE DOOR, UPPER FORWARD FRAME CORNER AT STATION 294.5. BLENDED OUT CRAC K PER EA 74071. (M) 2 L 7 2 4F RT A16WE 2002091800120 20020918 00120 NM 2002 9 18 USAA020243 1 20020613 A 5514 STIFFENER BOEING 737 737401 1384701 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND STIFFENER ANGLE CRACKED 1.5 INCHES LONG, LEFT HORIZONTAL STAB REAR SPAR ELEVATOR STATION 221.50. NEW STIFFE NER REPLACED AND DOUBLER PER SRM 55-10-10 AND EA 74155. (M) 2 L 7 2 4F RT A16WE 2002091800121 20020918 00121 NM 2002 9 18 USAA020244 1 20020608 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND FLOOR SUPPORT ANGLE 1.5 INCH LONG THROUGH RIVET HOLE, FRAME 601 LOWER END INBOARD ANGLE 5 INCHES BELOW CABIN FLOOR. CUT OUT DAMAGE AND INSTALLED DOUBLER PER EA 74131. (M) 2 L 7 2 4F RT A16WE 2002091800122 20020918 00122 NM 2002 9 18 USAA020245 1 20020614 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND SKIN CRACKED .75 INCH, FORWARD SERVICE DOOR JAMB LOWER AFT CORNER. INSTALLED DOUBLER PER SRM 53-10-01 FIG 2 02-1-5. (M) 2 L 7 2 4F RT A16WE 2002091800123 20020918 00123 NM 2002 9 18 USAA020246 1 20020621 A 5743 SUPPORT FITTING BOEING 737 737401 1384701 NM LT MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND AFT SUPPORT FITTING CRACKED .5 INCH, LEFT MLG AFT SUPPORT FITTING NR 4 UPPER OUTBOARD FASTENER. OVERSIZED H OLES PER TYPICAL REPAIR 57-40-13. (M) 2 L 7 2 4F RT A16WE 2002091800124 20020918 00124 NM 2002 9 18 USAA020247 1 20020531 A 5310 DOUBLER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND DOUBLER CRACKED .5 INCH, FORWARD SERVICE DOOR FRAME LOWER CORNER HI-LOCK IN REPAIR DOUBLER. FABRICATED AND INSTALLED DOUBLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2002091800125 20020918 00125 NM 2002 9 18 USAA020248 1 20020528 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 39819 23876 PIT - FOUND FRAME .5 INCH CRACK, FUSELAGE FRAME 827 B/W STRINGERS 8L AND 9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAI R 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002091800126 20020918 00126 NM 2002 9 18 USAA020257 1 20020504 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND FRAME CRACKED .25 INCH, STATION 767 BETWEEN S8L AND S9L AT PSU SUPPORT BRACKET. INSTALLED DOUBLER PER TYPIC AL REPAIR 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002091800127 20020918 00127 NM 2002 9 18 USAA020258 1 20020502 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND FRAME CRACKED .25 INCH, STATION 480 BETWEEN S8R AND S9R. CUT OUT CRACK, INSTALLED DOUBLER PER TYPICAL REPAI R 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002091800128 20020918 00128 NM 2002 9 18 USAA020259 1 20020515 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND INTERCOSTAL CRACKED 1 INCH, UPPER AFT FLANGE INTERCOSTAL BL 0 STATION 294.5-312. INSTALLED NEW INTERCOSTAL PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002091800129 20020918 00129 NM 2002 9 18 USAA020260 1 20020518 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND STRINGER CRACKED .25 INCH, STATION 663 STRINGER 2R. INSTALLED DOUBLERS PER SRM 53-00-07 FIG 209. (M) 2 L 7 2 4F RT A16WE 2002091800130 20020918 00130 NM 2002 9 18 USAA020261 1 20020514 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 48985 22952 PIT - FOUND FRAME CRACKED TWO PLACES .125 INCH AND .25 INCH, STATION 380 BETWEEN S8R AND S9R. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2002091800131 20020918 00131 NM 2002 9 18 USAA020264 1 20020701 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 46790 23702 CLT - FOUND SKIN CRACKED .5 INCH, BOTTOM OF FORWARD FUSELAGE AND R/B COOLING DUCT. DAMAGED REMOVED, DOUBLER INSTALLED P ER TYPICAL REPAIR 53-30-07. (M) 2 L 7 2 4F RT A16WE 2002091800132 20020918 00132 NM 2002 9 18 USAA020265 1 20020710 A 5542 65C2584151 SKIN BOEING 737 737401 1384701 NM RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND RUDDER SKIN DAMAGE, LT/RT RUDDER, CRITICAL AREAS AND 6 INCHES OF PANEL EDGE. WET LAY UP REPAIR PER SRM 55-4 0-01, 51-70-11 AND EA 74270. (M) 2 L 7 2 4F RT A16WE 2002091800133 20020918 00133 NM 2002 9 18 USAA020267 1 20020707 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 47222 23380 PIT - FOUND FRAME CRACKED .25 INCH, AT STATION 847 STRINGER 9L. DOUBLER INSTALLED PER TR 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002091800134 20020918 00134 NM 2002 9 18 USAA020271 1 20020625 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND Z-ANGLE CORRODED 3 INCHES BY 2 INCHES, STATION 294-325 WBL 208 RT. (M) 2 L 7 2 4F RT A16WE 2002091800135 20020918 00135 NM 2002 9 18 USAA020272 1 20020625 A 5347 SEAT TRACK BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND SEAT TRACK CORRODED 2 INCH BY 2 INCH CORROSION, STATION 907 RT WBL 208 RBL 51. REMOVED CORROSION. (M) 2 L 7 2 4F RT A16WE 2002091800136 20020918 00136 NM 2002 9 18 USAA020278 1 20020716 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND FRAME CRACKED .5 INCHES LONG, STATION 787 BETWEEN S1 AND S2 RIGHT SIDE. DOUBLER INSTALLED PER TYPICAL REPAI R 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002091800137 20020918 00137 NM 2002 9 18 USAA020279 1 20020626 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND FRAME CRACKED .125 INCH, STATION 827 BETWEEN STRINGER 8RT AND 9RT. REMOVED FRAME AND INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14 REV A. (M) 2 L 7 2 4F RT A16WE 2002091800138 20020918 00138 NM 2002 9 18 USAA020280 1 20020701 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND FRAME CRACKED .125 INCH, BS 747 BETWEEN STRINGER 8/9 LT. REMOVED CRACK AND INSTALLED DOUBLER PER TR 53-10-1 4A. (M) 2 L 7 2 4F RT A16WE 2002091800139 20020918 00139 NM 2002 9 18 USAA020281 1 20020701 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 40034 23879 PIT - FOUND FRAME CHAFED .5 INCH, STATION 767 BETWEEN STRINGER 8 AND 9 RT. REMOVED DAMAGED SECTION OF FRAME INSTALLED D OUBLER PER TR 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002091800140 20020918 00140 NM 2002 9 18 USAA020315 1 20020720 A 5500 1132329 ATTACH ANGLE BOEING 737 7373B7 1384580 NM THRUST BEAM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 48430 23311 PIT - FOUND ATTACH ANGLE CRACKED 6 INCHES IN RADIUS, RIGHT THRUST BEAM UPPER INBOARD ATTACH ANGLE. DEFECTIVE PART REPLA CED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2002091800141 20020918 00141 NM 2002 9 18 ZW0A0209301 1 20020907 A 3350 362624 LIGHT BOEING 757 757231 1384950 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 716TW 28484 THE EGRESS LIGHT AT SEAT 1B WAS INOPERATIVE. REPLACED THE LIGHT STRIP. 2 L 7 2 4F RT A2NM 2002091800142 20020918 00142 NM 2002 9 18 ZW0A0209302 1 20020909 A 5414 SKIN BOEING 757 7572Q8 1384972 NM NR 2 PYLON CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 702TW 28162 DURING CHECK-C MAINT THE NR 2 ENGINE PYLON, FWD ACCESS HOLE TO INTERIOR OF THE PYLON, APPROXIMATE NACELLE STA 162, THE O TBD SIDE HAD A CRACK 1.625 INCHES LONG. THE CRACK WAS LOCATED TOP FWD SECTION, AND VISIBLE ON OTBD TO INBD OF THE SKIN. ACCOMPLISHED BOEING SERVICE BULLETIN 757-54-0037 DIRECTED BY EMLR 73249. 2 L 7 2 4F RT A2NM 2002091800143 20020918 00143 WP 2002 9 18 ZW0A0209401 1 20020911 A 3350 408822101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST NR NOT REPORTED 1 CE 13 960TW 49231 BOTH COCKPIT EMERGENCY LIGHTS AT TOP OF OVERHEAD PANEL WERE INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY B5-23. 2 L 7 2 4F A6WE 2002091800144 20020918 00144 WP 2002 9 18 ZW0A0209402 1 20020909 A 2120 SMOKE DOUG DC9 DC983 3022083 WP COCKPIT DETECTED A ZW0A K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 13 9405T 53141 BLUE/GREY SMOKE IN COCKPIT AT 35,000 FEET. SMOKE DISSIPATED PRIOR TO RUNNING SMOKE REMOVAL CHECKLIST. APU WAS DEACTIVA TED PER MEL. ANOTHER STATION LATER PERFORMED PACK BURN OUT AND FOUND NO SMOKE OR OIL SMELL IN CABIN. THE APU WAS REACT IVATED. 2 L 7 2 4F RT A6WE 2002091800145 20020918 00145 NM 2002 9 18 ZW0A0209403 1 20020909 A 5414 SKIN BOEING 757 7572Q8 1384972 NM NR 2 PYLON CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 702TW 28162 DURING CHECK-C MAINT ON NUMBER 2 PYLON 1.5 INCH CRACKS GOING AFT WERE FOUND INBD AND OTBD FORWARD ACCESS HOLE AT NACELLE STA 120 BETWEEN STA 116.05 AND 128. ACCOMPLISHED EMLR 73249. 2 L 7 2 4F RT A2NM 2002091800146 20020918 00146 WP 2002 9 18 ZW0A0209501 1 20020913 A 3350 60030451LB BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9621A 53592 THE EMERGENCY EXIT SIGNS ABOVE BOTH AFT OVERWING DOORS WERE INOPERATIVE. REPLACED THE BATTERY PACK. 2 L 7 2 4F RT A6WE 2002091800147 20020918 00147 EA 2002 9 18 COMA0260531 1 20020914 A 2910 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 912CA 7011 HYDRAULIC NUMBER ONE LOW PRESSURE CAUTION.TIGHTENED LOOSE QUICK DISCONNECT FITTING ON HYDRAULIC PRESSURE LINE AT PYLON F IRE WALL. 2 L 7 2 4F RT A21EA 2002091800148 20020918 00148 EA 2002 9 18 ASOA02406 1 20020720 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 834AS 7254 DURING A HANGAR INSPECTION IN MCN, THE FORWARD MOST EXTERNAL EMERGENCY LIGHT ON THE LEFT SIDE OF THE FUSELAGE WAS INOPER ATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002091800149 20020918 00149 EU 2002 9 18 ASOA02407 1 20020721 A 3350 E0052RB15SNE CONNECTOR AEROSP ATR72 ATR72212 8680945 EU CABIN FAULTY A ASOA K NONE O OTHER CR CRUISE 1 SO 11 531AS 454 FLT 4108 - DURING FLIGHT FROM MYR TO ATL, THE FLIGHT ATTENDANT REPORTED THAT THE FIRST SEVEN ROWS OF EMERGENCY FLOOR TRA CK LIGHTS ILLUMINATED. BOTH EMERGENCY SWITCHES WERE IN THE ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE CANNON PLUG AT THE 43WL POWER SUPPLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002091800150 20020918 00150 EU 2002 9 18 ASOA02408 1 20020721 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 531AS 14112 454 FLT 4039 - DURING INCOMING RUNS IN MCN, WITH THE EMERGENCY LIGHTS ARMED, SEVERAL EMERGENCY LIGHTS WERE ILLUMINATED FROM ROWS 1-7 ON THE FLOOR, CEILING, AND SIDEWALL. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY IN THE 43WL POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002091800151 20020918 00151 SO 2002 9 18 ASOA02410 1 20020715 A 5313 12026335013 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 639AS 120283 DURING C-CHECK INSPECTION IN BNA, STRINGER 21 LEFT WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 12 AND 13. MAI NTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER IAW SRM'S 53-00-00 AND 51-21-02. (M) 2 L 7 2 4T RT A31SO 2002091800152 20020918 00152 SO 2002 9 18 ASOA02411 1 20020715 A 5313 12006173009 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 639AS 120283 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND OUT OF LIMITS ON STRINGER 18 LEFT BETWEEN FRAMES 13A AND 15A. MAI NTENANCE REMOVED AND REPLACED THE CORRODED STRINGER SECTION IAW SRM'S 51-25-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002091800153 20020918 00153 SO 2002 9 18 ASOA02412 1 20020715 A 5313 12004137005 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 639AS 120283 DURING C-CHECK INSPECTION IN BNA, STRINGER 17 LEFT WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 20 AND 22. MAI NTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002091800154 20020918 00154 SO 2002 9 18 ASOA02413 1 20020715 A 5320 12014241001 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 639AS 120283 DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND OUT OF LIMITS ON THE CROSS BEAM AT FRAME 15 NEAR THE PASSENGER ENT RY DOOR. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRM'S 51-25-00, 51-21-00 AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002091800155 20020918 00155 EA 2002 9 18 COMA0260532 1 20020914 A 2750 865D1007 PCU CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 967CA 15067 7134 FLAPS FAIL, WOULD NOT EXTEND.REPLACED THE POWER DRIVE UNIT. 2 L 7 2 4F RT A21EA 2002091800156 20020918 00156 SO 2002 9 18 ASOA02414 1 20020715 A 5320 12004149002 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 639AS 120283 DURING C-CHECK INSPECTION IN BNA, THE CROSSBEAM AT FRAME 16 WAS FOUND TO BE CORRODED BEYOND LIMITS BETWEEN THE RIGHT BUT T STRAP AND THE RIGHT FLOOR SILL. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002091800157 20020918 00157 SO 2002 9 18 ASOA02415 1 20020715 A 5320 SILL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 639AS 120283 DURING C-CHECK INSPECTION IN BNA, THE RIGHT BUTT STRAP FLOOR SILL WERE FOUND TO BE CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP AND FLOOR SILL IAW SRM'S 53-00, 51-25-00, AND 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002091800158 20020918 00158 SO 2002 9 18 ASOA02416 1 20020715 A 5320 BUTT STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 639AS 120283 DURING C-CHECK INSPECTION IN THE LEFT BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 13 AND 15. ANOTHER LEFT BUTT S TRAP WAS CORRODED BETWEEN FRAMES 14 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTIONS OF BUTT STRAP IAW SR M 51-25-00, 51-21-02, AND 51-40-02 E25. (M) 2 L 7 2 4T RT A31SO 2002091800159 20020918 00159 SO 2002 9 18 ASOA02417 1 20020715 A 5330 12019230003 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 639AS 120283 DURING C-CHECK INSPECTION IN BNA, THE FUSELAGE BELLY SKIN WAS FOUND TO BE CORRODED OUT OF LIMITS. MAINTENANCE REMOVED A ND REPLACED THE CORRODED SKIN PANEL IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002091800160 20020918 00160 EA 2002 9 18 COMA0260533 1 20020914 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 812CA 7381 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002091800161 20020918 00161 EA 2002 9 18 ASOA02418 1 20020722 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN CONTAMINATED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 844AS 7317 FLT 4542 - DURING GROUND INSPECTION IN GNV, THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND WATER THROUGH OUT THE ENTIRE FLOOR STRIP AND DRIED IT UP. MAINTENANCE REMOVED AND REPLACED THE SECTION OF FLOOR TRACK LIGHTING BETWEEN ROWS 5 AND 8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002091800162 20020918 00162 EA 2002 9 18 ASOA02419 1 20020722 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA K NONE O OTHER TX TAXI/GRND HDL 1 SO 11 843AS 8472 7310 FLT 4843 - DURING TAXI INTO DFW, THE CAPTAINS LEFT WINDSHIELD WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED WINDSHIELD. PRESSURE AND OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002091800163 20020918 00163 EA 2002 9 18 ASOA02420 1 20020724 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 903EV 7621 DURING GROUND INSPECTION IN ATL, THE LEFT OVERWING EMERGENCY LIGHT BULB WAS FOUND TO BE BURNED OUT. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002091800164 20020918 00164 EA 2002 9 18 ASOA02421 1 20020724 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA O OTHER O OTHER AP APPROACH 1 SO 11 871AS 7537 FLT 4463 - ON APPROACH INTO SHV, THE FLAPS FAILED AT 20 DEGREES. THE CAPTAIN FOLLOWED THE APPROPRIATE QRH PROCEDURES. AN EMERGENCY WAS DECLARED AS A PRECAUTION. AIRCRAFT LANDED SAFELY IN SHV. MAINTENANCE RESET THE FLAP SYSTEM AND FOUND IT TO OPERATE NORMALLY. THE FLAPS WERE RUN THROUGH SEVERAL CYCLES WITH NO DEFECTS NOTED. NO FAULTS WERE LOGGED IN THE MAINTENANCE DIAGNOSTIC COMPUTER OR THE AIR DATA COMPUTER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002091800165 20020918 00165 EA 2002 9 18 COMA0260534 1 20020914 A 3030 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 729CA 7265 TAT PROBE HEAT, RT AOA HEAT, RT STATIC HEAT, RT PITOT HEAT CAUTION MESSAGES.COULD NOT DUPLICATE, RESET SYSTEM, OPS CHECK NORMAL. 2 L 7 2 4F RT A21EA 2002091800166 20020918 00166 SO 2002 9 18 ASOA02422 1 20020725 A 5230 12023348005 DOOR SEAL EMB 120 EMB120RT 3260202 SO CARGO DOOR TORN A ASOA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SO 11 237AS 120051 DURING CRUISE FROM ILM TO ATL, AT APPROX 22,000 FT, CABIN PRESSURE STARTED TO CLIMB AT 2000 FPM. CAPTAIN ATTEMPTED TO U SE THE MANUAL CONTROLLER, NO EFFECT. DESCENT WAS INITIATED. AT 18,000 FT BOTH BLEED OVERHEAT LIGHTS ILLUMINATED BUT SO ON EXTINGUISHED AFTER QRH CHECKLIST WAS PERFORMED. AT ALTITUDE OF 16,000 FT THE CABIN OXYGEN MASKS HAD DEPLOYED. CABIN PRESSURE INDICATED 10,000. UPON REACHING FL100 THE CABIN PRESSURE DESCENDED TO 8000 WITH A DELTA P OF 1. AIRCRAFT LAN DED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR SEAL WHICH WAS FOUND TO BE RIPPED. PRESSURIZATION C HECK UP TO 4 DELTA P GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2002091800167 20020918 00167 SO 2002 9 18 ASOA02423 1 20020726 A 3350 BATTERY PACK EMB 120 EMB120RT 3260202 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 240AS 120060 DURING GROUND INSPECTION IN DFW, THE FORWARD SECTION OF FLOOR EMERGENCY LIGHTING WERE FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IN THE NR 1 AND NR 2 POSITIONS. OPERATIONAL CHECKS GOOD. AIR CRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002091800168 20020918 00168 EA 2002 9 18 ASOA02424 1 20020726 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 828AS 7213 WHILE COMPLYING WITH ASA EO600-53-0043A, INSPECTION OF THE ENGINE SUPPORT BEAM, THERE WAS A CRACK FOUND AT THE LEFT AND RIGHT ACCESS PANEL. BOTH CRACKS WERE ON THE INBOARD FORWARD SIDE OF THE PANELS. MAINTENANCE REPAIRED THE CRACKED ENGIN E SUPPORT BEAM IAW ASA EO 600-53-0073. (M) 2 L 7 2 4F RT A21EA 2002091800169 20020918 00169 EA 2002 9 18 ASOA02425 1 20020726 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 828AS 7213 DURING HANGAR INSPECTION IN MCN, FRAME STATION 718 WAS FOUND TO BE CRACKED ON BOTH THE LEFT AND RIGHT SIDE. MAINTENANCE REPAIRED THE CRACKED FRAME IAW ASA EO 600-53-0067. (M) 2 L 7 2 4F RT A21EA 2002091800170 20020918 00170 NM 2002 9 18 QXEA0201199 1 20020807 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-CORROSION AT ATTACH POINT FOR CARGO PANEL 145AZ. REPAIRED IAW DHC8 SRM 53-00-16, SRM 51-20-16, PAGE 4, SRM 51-20-36 , PAGE 6. 2 H 7 2 4T RT A13NM 2002091800171 20020918 00171 NM 2002 9 18 QXEA0201200 1 20020808 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-FRAME HAS CORROSION AT X653.0 AND Y26.0L BELOW CARGO BAY FLOOR. REPAIRED IAW DHC8 SRM 51-20-16, PAGE 4, SRM 51-20-3 6, PAGE 6 AND SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002091800172 20020918 00172 NM 2002 9 18 QXEA0201201 1 20020805 A 5230 TRACK DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-CARGO DOOR AFT GUIDE TRACK IS GOUGED ON UPPER RAIL. REPAIRED IAW RD8-52-208. 2 H 7 2 4T RT A13NM 2002091800173 20020918 00173 NM 2002 9 18 QXEA0201202 1 20020811 A 5230 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-CARGO DOOR FORWARD UPPER DOOR IS GOUGED. REPAIRED IAW RD8-53-104. 2 H 7 2 4T RT A13NM 2002091800174 20020918 00174 NM 2002 9 18 QXEA0201203 1 20020811 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-CARGO DOOR APERTURE AFT UPPER DOOR STOP IS GOUGED. REPAIRED IAW RD8-53-104. 2 H 7 2 4T RT A13NM 2002091800175 20020918 00175 NM 2002 9 18 QXEA0201204 1 20020806 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-CARGO DOOR APERTURE FORWARD UPPER DOOR STOP IS GOUGED ON FUSELAGE. REPAIRED IAW RD8-53-5461. 2 H 7 2 4T RT A13NM 2002091800176 20020918 00176 NM 2002 9 18 QXEA0201205 1 20020806 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-CARGO DOOR APERTURE AFT UPPER DOOR STOP IS GOUGED. REPAIRED IAW RD8-53-5461. 2 H 7 2 4T RT A13NM 2002092400064 20020924 00064 EA 2002 9 24 COMA0260529 1 20020916 A 7110 22850583801 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NR 1 COWLING FAILED A COMA E ENGINE SHUTDOWN S AFFECT SYSTEMS DE DESCENT 1 SO 01 716CA 7250 807248 DURING FLIGHT NUMBER ONE THROTTLE LEVER JAMMED WITH 90 PERCENT THRUST. UNABLE TO REDUCE. SHUT DOWN ENGINE WITH FIRE PU SH SW LIGHT AND LANDED SINGLE ENGINE. FOUND UPPER CORE COWL HOLD OPEN ROD DISLOCATED FROM ITS STOWAGE CLIP AND WAS JAMM ED AGAINST THE LINKAGE RUNNING BETWEEN THE FUEL CONTROL AND THE THROTTLE QUAD. REMOVED AND INSTALLED SERVICEABLE STOWAG E CLIP. INSTALLED SERVICEABLE CLIP PIN AND HOLD OPEN ROD FOR PREVENTIVE MAINTENANCE IAW SB CF34-NAC-71-013. 2 L 7 2 4F 4 F RT A21EA E15NE 2002091800177 20020918 00177 NM 2002 9 18 QXEA0201206 1 20020809 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-LEFT HAND NR 5 FLAP TRACK HAS SLIGHT PITTING ALONG OUTBOARD SIDE WHERE SIDE ROLLER MAKES CONTACT. REPAIRED IAW HORI ZON AIR EA 2-57-182. 2 H 7 2 4T RT A13NM 2002091800178 20020918 00178 NM 2002 9 18 QXEA0201207 1 20020809 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-FRAME NR 1 AT STATION 670.349 DAMAGED BETWEEN STRINGER 18L AND 22L. REPAIRED IAW DHC8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002091800179 20020918 00179 NM 2002 9 18 QXEA0201208 1 20020809 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-BOUNDRY ANGLE AT STATION X653.349 DAMAGED BETWEEN STRINGER 18L AND 22L. REPAIRED IAW HORIZON AIR EA 2-53-411. 2 H 7 2 4T RT A13NM 2002091800180 20020918 00180 NM 2002 9 18 QXEA0201209 1 20020809 A 5312 BULKHEAD DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX-AFT PRESSURE BULKHEAD PANEL DAMAGED. REPAIRED IAW HORIZON AIR EA 2-53-353, DHC8 SRM 51-40-11 AND SRM 51-30-26. 2 H 7 2 4T RT A13NM 2002091800181 20020918 00181 EU 2002 9 18 MALA020565 1 20020917 A 2560 P4010021 FLASHLIGHT SAAB SF340 SF340A 7850100 EU A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 142XJ AFTER FLIGHT #3203 PASSENGER REMOVED EMERGENCY FLASHLIGHT FROM HOLDER. CABIN EMERGENCY FLASHLIGHT INOP. MAINTENANCE REP LACED BATTERY PN P4-01-0021 OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002102100045 20021021 00045 NE 2002 10 21 OZIA200243008 2 20020910 A 7250 30B466101 TURBINE BLADES DORNER DO32 DO328300 NM PWA 306 PW306B NE ENGINE MISSING A OZIA K NONE O OTHER IN INSP/MAINT 1 CE 05 430Z 1979 495 3127 CD0022 ENGINE SHOWED SHIFT IN ITT AND N2 PARAMETERS ON ECTM. BORESCOPE FOUND HP TURBINE MISSING TWO BLADES AND OTHER BLADES WI TH CRACKS. 2 H 7 2 4T 4 F RT A55NM E35NE 2002091800182 20020918 00182 WP 2002 9 18 0202909987 1 20020912 A 4990 HONEYWELL GTCP8598DCA DOUG DC9 DC932 3022066 WP A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 987US P27486DCA 47458 DURING CLIMB, FLIGHT ATTENDANT REPORTED THE LEFT AFT LAV SMOKE ALARM SOUNDING AND BURNING SMELL IN CABIN. SMELL CLEARED BUT LAV ALARM CONTINUED UNTIL RESET. FLIGHT CONTINUED TO DESTINATION. MAINTENANCE REPLACED THE APU. OPERATIONAL CHECK OK . 2 L 7 2 4F A6WE 2002091800183 20020918 00183 NM 2002 9 18 QXEA0201469 1 20020913 A 3340 M525237387 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 200 SMOKE A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 379PH 530 SEA-SMOKE FROM NOSE GEAR LOCKED LIGHT CAPTAINS SIDE PANEL. REMOVED AND REPLACED NOSE GEAR LOCKED LIGHT. OPERATIONAL CHEC K GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092000102 20020920 00102 SO 2002 9 20 C2XA02SH052 1 20020831 A 5320 14522461011 DOUBLER EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV- DURING C-CHECK DOUBLER AT FRAME 22 WAS FOUND TO HAVE CORROSION IN NUT PLATE HOLES. MAINTENANCE REMOVED AND REPLACE D DOUBLER AT FRAME 22 IAW IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002092000103 20020920 00103 SO 2002 9 20 C2XA02SH053 1 20020831 A 5320 14522460011 BUTT STRAP EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV DURING C-CHECK INSPECTION CENTER FLOORBEAM STRAP AT FRAME 18 WAS FOUND TO HAVE CORROSION IN NUT PLATES HOLES. MAINT ENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVIC E. 2 L 7 2 4F RT T00011AT 2002092000104 20020920 00104 SO 2002 9 20 C2XA02SH054 1 20020831 A 5320 14522459003 ANGLE EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV - DURING C-CHECK CENTER FLOORBEAM REINFORCEMENT ANGLE WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 20. MAINTEN ANCE REMOVED AND REPLACED AFFECTED ANGLE IAW EMB -145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002092000106 20020920 00106 SO 2002 9 20 C2XA02SH056 1 20020831 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV- DURING C-CHECK, CENTER FLOOR SUPPORT BETWEEN FRAMES 18 AND 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP BETWEEN FRAMES 18 AND 20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002092000107 20020920 00107 SO 2002 9 20 C2XA02SH057 1 20020831 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV- DURING C-CHECK, CENTER FLOOR SUPPORT BETWEEN FRAMES 20 AND 23 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002091900001 20020919 00001 SO 2002 9 19 C2XA02TY144 1 20020918 A 5324 14526795001 STRINGER EMB 145 EMB145 3260210 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS DURING A SCHEDULED 2-C INSPECTION MAINT. FOUND GOUGES ON STRINGER 19L AND 19R AT STA. 17727.0. MAINT. BLENDED AND N DI TESTED AREA,NO CRACKS WERE FOUND. FAB.ALLODINE,PRIME AND INSTALLED REPAIR PARTS AT STRINGER 19L. MEASURED,BLENDED PER FORM NDI ,FOUND NO DEFECTS,ALLODINED,PRIME AND PAINTED 19RIAW EMB 135/145 SRM 53-24-02,CPM 51-21-04,05,06. ALL WORK WAS ACCOMPLISH AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002091900009 20020919 00009 CE 2002 9 19 EL62002F00000 1 20020827 A 3233 12810013 HOUSING CESSNA 172 172RG 2072438 CE LYC O360 O360* 41514 EA LT MLG ACTUATOR BROKEN B EL6R K NONE O OTHER IN INSP/MAINT 1 EA 23 9706B 172RG0980 PILOT HEARD LOUD BANG IN FLIGHT, ACTUATED GEAR FOR CHECK, NOTED LEFT NOT WORKING. INSPECTION FOUND LEFT MAIN GEAR ACTU ATOR HOUSING BROKEN IN HALF AROUND GEAR DRIVE SECTION. 1 H 7 1 3O 3 O 3A17 E286 2002091900010 20020919 00010 NE 2002 9 19 IUXR941L 2 20020913 A 7250 3006146 BEARING BEECH 99 99 1154002 CE PWA PT6 PT6A36 52043 NE ENGINE FAILED B K NONE L NO TEST IN INSP/MAINT 1 WP 23 BEARING CAGE SEPARATED DURING ENGINE TEST. (S/N E967). BEARING RETURNED TO BEARING REFURB FACILITY. CURRENTLY PERFORMI NG ANALYSIS, EARLY INDICATION IS LATENT DEFECTS (CRACKS) IN CAGE. 1 L 7 2 3T 4 T A14CE E4EA 2002091900011 20020919 00011 CE 2002 9 19 MNZA0207008 1 20020729 A 2820 051600918 RESERVOIR CESSNA 172 172R 2072401 CE LYC IO360 IO360L2A EA FUEL SYSTEM CRACKED A MNZA K NONE K FLUID LOSS IN INSP/MAINT 1 CE 03 5172J 313 17281095 UPON INSPECTION, IT WAS NOTED THAT A FUEL STAIN WAS EVIDENT ON THE UNDERBELLY OF THE AIRCRAFT IN THE VACINITY OF THE FUE L SELECTOR VALVE. CABIN FLOORING AND UPHOLSTERY WAS REMOVED AND THE FUEL SELECTOR AND FUEL RESERVOIR WAS REMOVED AND INS PECTED. THE RESEVOIR WAS PRUGED AND PRESSURE TESTED. THE TANK WAS THEN COVERED IN A SOAPY WATER SOLUTION AND LEAK WAS NOTED COMING FROM A WELDED SEAM. IT IS BELIEVED THAT A MINIMUM .75 INCH CRACK WAS EVIDENT IN A PART WIGH ONLY 300 HOURS . MFG WARRANTY REPLACED THE PART AND AFTER TAKIN PICTURES, WE SURRENDERED THE PART TO THEM. 1 H 7 1 3O 3 O NT 3A12 1E10 2002091900013 20020919 00013 CE 2002 9 19 RH62002F00000 1 20020620 A 2434 DOFF10300J ALTERNATOR CESSNA 177 177RG 2073709 CE LYC O360 IO360A1A 41514 EA ENGINE SHORTED B RH6A O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 NE 01 8248G 500 177RG0148 UNUSED RECTIFIER POST BECOME LOOSE AND FELL INTO BOTTOM OF ALTERNATOR CASE. VIBRATION CAUSED LOOSE BOLT TO SHORT STATOR WINDINGS AND INTERMITTENTLY CAUSE DISCHARGE SPIKE IN BUS SYSTEM SPIKE WOULD CAUSE AVIONICS TO TURN OFF AND LOOSE NAVIGA TION INFORMATION. 1 H 7 1 3O 3 O A20CE 1E10 2002091900014 20020919 00014 SO 2002 9 19 UIE2002F00009 2 20020528 A 7414 6379 MAGNETO BEECH 35 G35 1151516 CE CONT E225 E225* 17015 SO ENGINE FAILED A UIEA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 EA 15 348G 18 D4532 AIRCRAFT ENGINE RIGHT MAGNETO FAILED DURING MAGNETO CHECK. FOUND IMPULSE COUPLER SPRING IN TWO PIECES. SPRING BROKE IN TO TWO PIECE FOR UNKNOWN REASON. ALSO FOUND PREVIOUS TECHNICIAN SPLICED MAG (P) LEAD AND GROUND WIRE TOGETHER CAUSING T HE MAG TO GROUND OUT INTERMITTENT. THE REASON FOR THE INTERMITTENT WAS THE GROUND WIRE WAS POORLY CONNECTED TO THE (P) LEAD. (SW152002B0548 FSDO) 1 L 7 1 3O 3 O A777 E267 2002091900015 20020919 00015 NM 2002 9 19 2002F00883 1 20020706 A 3350 201319 BATTERY DHAV DHC8 DHC8201 2809001 NM CABIN INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 17358 7358 FLT 6900 - CMH-TUS - EMERGENCY EXIT LIGHTS DIM AT ROW 2-5. MAINTENANCE WAS CALLED. MAINTENANCE REPLACED THE BATTERY AN D THE SYSTEM OP CHECKS GOOD. AIRCRAFT DEPARTED WITHOUT ANY FURTHER INCIDENT. (M) 2 H 7 2 4T RT A13NM 2002091900016 20020919 00016 NM 2002 9 19 2002F00884 1 20020708 A 3350 6519022 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456YV 456 DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT THE 3/4 EMERGENCY PATH LIGHTS WERE INOPERATIVE. REPLACED THE LIGHT S STRIPS. OPS CHECKS GOOD. (M) 2 H 7 2 4T RT A13NM 2002091900017 20020919 00017 EA 2002 9 19 2002F00885 1 20020708 A 2560 P20700001214 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA FLIGHT DECK INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7353 7353 DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT THE CAPTAINS EMERGENCY FLASHLIGHT WAS INOPERATIVE. REPLACED THE FL ASHLIGHT. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002091900018 20020919 00018 EA 2002 9 19 2002F00886 1 20020710 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17337 7337 DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT THE FORWARD EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTEN ANCE REPLACED THE LIGHT BULB. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002091900019 20020919 00019 NM 2002 9 19 2002F00887 1 20020727 A 7500 CLAMP BOEING 727 727231 1384079 NM NR 3 ENGINE LOOSE A FX7A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 54348 21967 AFTER TAKEOFF IN MIA, NR 3 ENGINE STRUT O/H LIGHT CAME ON, WHEN REDUCING POWER LIGHT WENT OUT. FOLLOWED PROCEDURES AND RETURNED TO MIA. FOUND LOOSE 13TH STAGE MOD VALVE CLAMP AT ENGINE STRUT TIGHTENED SAME PER MM 20-80-1 AND RAN ENGINE PE R MM 71-00. OPS CHECK GOOD A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002091900020 20020919 00020 NM 2002 9 19 2002F00888 1 20020726 A 2910 B-NUT BOEING 727 727231 1384079 NM HYD SYSTEM LOOSE A FX7A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 54348 21967 DURING CRUISE SYSTEM 'A' HYDRAULICS FAILED, PRESSURE WENT TO ZERO. AIRCRAFT DIVERTED TO SAP AND LANDED SAFELY, FOUND SY STEM 'A' PRESSURE LINE B-NUT LOOSE TIGHTENED SAME SERVICED HYD AND OPS CHECK GOOD PER MM 29-11. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 3 4F A3WE 2002091900021 20020919 00021 WP 2002 9 19 AALA20020274 1 20020222 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7533A 49987 TUL - FOUND NR 2 SEAT TRACK, STATION 1170, HAS CORROSION AT FASTENER HOLE. CUT OUT DAMAGE AREA AROUND HOLE, FABRICATED STRAP FROM 7075-T6, .090. INSTALLED STRAP PER AARD 53-20-00-13. (M) 2 L 7 2 4F A6WE 2002091900022 20020919 00022 NM 2002 9 19 SWAA022141 1 20020916 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM MID CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 713SW 27847 RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REINSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002091900023 20020919 00023 2002 9 19 SWAA022142 4 20020914 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST AND SLIDE CABLE MISROUTED. A DJUSTED SLIDE AND REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002091900024 20020919 00024 NM 2002 9 19 SWAA022143 1 20020914 A 3350 07912 COVER BOEING 737 7373Y0 1384671 NM AFT GALLEY LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER LOOSE NEXT TO NR 3 GALLEY. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2002091900025 20020919 00025 NM 2002 9 19 SWAA022144 1 20020915 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS RED LENS MISSING IN AFT CABIN. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002091900026 20020919 00026 NM 2002 9 19 SWAA022148 1 20020915 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091900027 20020919 00027 NM 2002 9 19 SWAA022149 1 20020915 A 5320 6546529 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 344, ABOVE STR 21L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2002091900028 20020919 00028 NM 2002 9 19 SWAA022150 1 20020916 A 5755 65464152 SPOILER BOEING 737 7373H4 1384600 NM LT WING BULGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND NR 4 SPOILER UPPER SKIN BULGED. REMOVED AND REPLACED NR 4 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2002091900029 20020919 00029 2002 9 19 SWAA022126 4 20020913 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002091900030 20020919 00030 2002 9 19 SWAA022129 4 20020912 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002091900031 20020919 00031 NM 2002 9 19 SWAA022133 1 20020912 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED C3 CHECK, FOUND RT OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OTBD T/E AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2002091900032 20020919 00032 NM 2002 9 19 SWAA022136 1 20020913 A 5330 6545785 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED 1/4D CHECK, FOUND RT FUSELAGE SKIN CRACKED AT BS 520, UPPER WINDOW CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2002091900033 20020919 00033 NM 2002 9 19 SWAA022138 1 20020913 A 2740 MS252531 SWITCH BOEING 737 7373H4 1384600 NM TAIL COMP FAULTY A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 29 654SW 28399 ABORTED TAKEOFF, DURING TAKEOFF, WARNING HORN SOUNDED. REMOVED AND REPLACED STABILIZER TAKEOFF WARNING LIMIT SWITCH AND R274 RELAY PER MM. 2 L 7 2 4F RT A16WE 2002091900034 20020919 00034 NM 2002 9 19 SWAA022139 1 20020912 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C2 CHECK, FOUND BS 1016 AFT PRESS BULKHEAD CRACKED (2 EA) AT 6 0' CLOCK AND 9 0' CLOCK POSITION. REPAI RED BULKHEAD PER SWA EA. 2 L 7 2 4F RT A16WE 2002091900035 20020919 00035 WP 2002 9 19 AALA20020275 1 20020225 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7533A 49987 TUL - FOUND NR 3 SEAT TRACK STATION 1300-1307 HAS AREAS OF CORROSION. REMOVED SECTION OF SEAT TRACK AND INSTALLED NEW S ECTION 1265 TO 1307. (M) 2 L 7 2 4F A6WE 2002091900036 20020919 00036 NM 2002 9 19 SWAA022120 1 20020909 A 3350 311500 LENS BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY LIGHT LENS AT ROW NR 5 DEF MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002091900037 20020919 00037 NM 2002 9 19 SWAA022123 1 20020910 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002091900038 20020919 00038 NM 2002 9 19 SWAA022125 1 20020910 A 5311 6546536 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2002091900039 20020919 00039 WP 2002 9 19 AALA20020276 1 20020227 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7533A 49987 TUL - FOUND NR 6 SEAT TRACK CORRODED AT G2 TIE DOWN STATION 215. REPLACED SEAT TRACK FROM STATION 215 TO 303, APPROX SR M 53-05. (M) 2 L 7 2 4F A6WE 2002091900040 20020919 00040 NM 2002 9 19 VNAA0209024 1 20020916 A 6100 PROPELLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 07 423JS 3032 DURING CLIMB, THE CREW NOTICED A VIBRATION SUSPECTED FROM THE LEFT HAND PROPELLER AND RETURNED TO PIT. MAINTENANCE INSP ECTED AND THEN BALANCED THE LEFT HAND PROPELLER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-00-00. OPERATIONAL CHE CKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002091900041 20020919 00041 WP 2002 9 19 AALA20020277 1 20020226 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7533A 49987 TUL - FOUND TIE DOWN STATION 160 RBL 12 INCHES CORRODED. REMOVED AND REPLACED WITH NEW TIE DOWN STATION 160 RBL 12 INCH ES PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002091900042 20020919 00042 WP 2002 9 19 AALA20020284 1 20020303 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7533A 49987 TUL - FOUND STATION 636-676 CORRODED RIGHT CUSP. INSTALLED CUSP REPAIR PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2002091900043 20020919 00043 WP 2002 9 19 AALA20020291 1 20020227 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7533A 49987 TUL - FOUND CORROSION IN AFT CARGO DOOR BEAM FS 1155-1211. REMOVED CORROSION PER SRM 51-10-03 AND INSTALLED FULL LENGTH DOUBLER PER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2002091900044 20020919 00044 WP 2002 9 19 AALA20020754 1 20020527 A 2120 5953625521 DUCT DOUG DC9 DC983 3022083 WP ACM BAY DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 436AA 49454 ORD - FLT 1511 - EN ROUTE ORD-PSP - 15 MINUTES AFTER TAKEOFF TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. FOLLO WED PROCEDURES AND LIGHT EXTINGUISHED WITHIN ONE MINUTE. RETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED AIR CONDIT IONING DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002091900045 20020919 00045 NM 2002 9 19 AALA20020772 1 20020524 A 2420 IDG BOEING 767 767323 1385205 NM RT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 21 382AN 25451 LHR - FLT 109 - RIGHT GEN DRIVE LIGHT ILLUMINATED 1.5 HOURS INTO FLIGHT ACCOMPLISHED GENERATOR DRIVE DISCONNECT PROCEDUR E. REMOVED AND REPLACED RIGHT ENGINE IDG PER MM. ACCOMPLISHED REQUIRED CHECKS TEST GOOD, NO LEAKS NOTED. (M) 2 L 7 2 4F RT A1NM 2002091900046 20020919 00046 WP 2002 9 19 AALA20020783 1 20020514 A 5320 FITTING DOUG DC9 DC982 3022082 WP CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AA 49255 TUL - FOUND CORROSION ON T-FITTING AT LOWER AFT CORNER OF MID CARGO DOOR JAMB. INSTALLED NEW T-FITTING PER SRM 51-30 E5 8-4A NR 0210772. (M) 2 L 7 2 4F A6WE 2002091900047 20020919 00047 WP 2002 9 19 AALA20020784 1 20020510 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AA 49255 TUL - FOUND DEEP WORN AREA IN BOTTOM OF CABIN FLOORBEAM AT STATION 389 BL 0. REMOVED DAMAGED AREA. INSTALLED ANGLE DOU BLER FILLER AND WEAR STRIP, CLEANED AND TREATED AND PRIMED PER AARD 53-20-00-21. (M) 2 L 7 2 4F A6WE 2002091900048 20020919 00048 WP 2002 9 19 AALA20020785 1 20020501 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AA 49255 TUL - FOUND CORROSION ON FUSELAGE SKIN AROUND FORWARD ANTENNA 1 INCH HOLE STATION 380. BLENDED CORRODED FROM SKIN AND T REATED DAMAGE IS ACCEPTABLE AS IS PER SRM 53-01 FIG 1, SHEET 3, PAGE 6. (M) 2 L 7 2 4F A6WE 2002103100233 20021031 00233 WP 2002 10 31 DHL2002801018 1 20020916 A 2612 300062495 CONNECTOR DOUG DC8 DC873F 302199F WP FIRE LOOP DEFECTIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 NR 3 ENGINE B LOOP INOP. FOUND PIN B ON P1-7007 TO PIN B CONNECTOR P1-7001 GROUNDED. IT ONLY SHOWS WITH A MEGGER. REP LACED CONNECTOR P1-7007, SYS OPS CHECKS GOOD PER DC-8 M/M 26-10-0. 2 L 7 4 4F RT 4A25 2002091900049 20020919 00049 WP 2002 9 19 AALA20020786 1 20020504 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AA 49255 TUL - FOUND CRACKED FASTENER HOLES UNDER NR 2 SEAT TRACK ON CUSP AT STATION'S 1211-1213-1219. INSTALLED ONE DOUBLER STA TION 1209-1215 AND ONE DOUBLER STATION 1225-1229, PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002091900050 20020919 00050 WP 2002 9 19 AALA20020787 1 20020516 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AA 49255 TUL - FOUND SEVERAL SMALL SPOTS OF CORROSION ON WEB ALONG LOWER DOOR JAMB STATION 1155 TO STATION 1212. INSTALLED NEW D OOR AREA WEB FROM STATION 1155-AFT TO STATION 1212 PER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2002091900051 20020919 00051 WP 2002 9 19 AALA20020788 1 20020510 A 5310 PAN DOUG DC9 DC982 3022082 WP PAX DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AA 49255 TUL - FOUND FORWARD DOOR PAN IS CORRODED IN FRONT, BACK AND BOTTOM INSTALLED PAN SPLICE REPAIR PER SRM 53-05 PT 1. (M) 2 L 7 2 4F A6WE 2002091900052 20020919 00052 WP 2002 9 19 AALA20020789 1 20020516 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AA 49255 TUL - FOUND HEAVY CORROSION ON BEAM FACE AND LOWER LEG FROM STATION 1155 AFT TO STATION 1212. INSTALLED FULL LENGTH BEA M DOUBLER PER AARD 53-10-00-3 FIG 1 SHEETS 1-13. (M) 2 L 7 2 4F A6WE 2002091900053 20020919 00053 NM 2002 9 19 AALA20020795 1 20020529 A 2420 GEN5013 IDG BOEING 767 767223 1385123 NM RT GENERATOR FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 313AA 22316 JFK - FLT 679 - DURING TAKEOFF RECEIVED EICAS MESSAGES, RIGHT GEN OFF, RIGHT GEN DRIVE LT, AND RIGHT UTIL BUS RESET GE N DRIVE LIGHT ON STEADY. COMPLETED CHECKLISTS, RETURNED AND LANDED. REMOVED RIGHT IDG. INSTALLED NEW IDG OPS AND LEAK CHECK OK. (M) 2 L 7 2 4F RT A1NM 2002091900054 20020919 00054 WP 2002 9 19 DHL2002802010 1 20020917 A 2611 SMOKE DETECTOR DOUG DC8 DC873 302199C WP A DHLA K NONE J L WARNING INDICATION NO TEST IN INSP/MAINT 1 SO 01 802DH 46076 1) #6 SMOKE DETECT. WON'T TEST2) INSTALLED O/H'D DETECTOR UNIT AND OPS CK'D OK PER MM 26-10-1 2 L 7 4 4F RT 4A25 2002091900055 20020919 00055 EU 2002 9 19 AALA20021091 1 20020723 A 3201 SHIELD FOKKER F28 F28MK0100 4990807 EU NLG DAMAGED A AALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SW 21 1412A 11370 ORD - FLT 879 - EN ROUTE ORD-RST, UPON GEAR RETRACTION THE MFDU INDICATED A RIGHT MAIN LANDING GEAR INDICATINO FOLLOWED BY A ANTI-SKID ALERT ON MFDU. THE GEAR WAS RECYCLED AND BOTH ALERTS RETURNED. A SMALL BUFFET WAS FELT. RETURNED ORD A ND LANDED WITHOUT INCIDENT. REPLACED WHEEL WELL SCATTER SHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002091900056 20020919 00056 EU 2002 9 19 AALA20021092 1 20020724 A 2720 AAP2989 MANIFOLD FOKKER F28 F28MK0100 4990807 EU RUDDER FAILED A AALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 21 1427A 11412 DFW - FLT 551 - AFTER TAKEOFF, BOTH STAB TRIM FAULTED, BOTH YAW DAMPER AND NR 2 RUDDER SYSTEM FAULTED. STAB TRIM AND YA W DAMPER WERE RESET. LANDED DFW WITHOUT INCIDENT. REPLACED RUDDER MANIFOLD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M0 2 L 7 2 4F RT 2002091900057 20020919 00057 EU 2002 9 19 AALA20021093 1 20020724 A 2841 0106KIP02022 COMPUTER FOKKER F28 F28MK0100 4990807 EU FUEL TOTALIZER DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 1403M 11354 DFW - FLT 1809 - EN ROUTE DTW-DFW - HAD FUEL IMBALANCE. AIR INTERRUPTED STL AND LANDED WITHOUT INCIDENT. REPLACED FUEL TOTALIZER PROCESSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002091900058 20020919 00058 NM 2002 9 19 AALA20021108 1 20020801 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 380AN 25449 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEATS 21B AND 23B INOPERATIVE. REPAIRED PUSH P IN TO CONNECTOR AT SEATS 21B AND 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002091900059 20020919 00059 EU 2002 9 19 AALA20021110 1 20020729 A 3233 D82310403 ACTUATOR FOKKER F28 F28MK0100 4990807 EU NLG CRACKED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 1412A 11370 DFW - FLT 334 - EN ROUTE DFW-BNA, NOSE GEAR UNSAFE MESSAGE AND NR 1 HYDRAULIC SYSTEM LOSS ON MFDU AFTER GEAR RETRACTION. ACCOMPANIED WITH A LARGE BANG. RETURNED DFW AND ACCOMPLISHED EMERGENCY GEAR EXTENSION. LANDED DFW WITHOUT INCIDENT. REPLACED NOSE GEAR RETRACT ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002091900060 20020919 00060 2002 9 19 GTIA020731 4 20020628 A 3450 CONTROL PANEL DOUG DC9 DC981 3022081 WP NAVIGATION FAILED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 806NK 936 48051 FLT 1751 - SJU - DFGS 2 WHEN SELECTED WILL NOT CAPTURE VOR RADIAL COURSE BECAUSE THE SYSTEM WILL NOT ARM. IT WILL ARE T HE LOCK INSTEAD BUT THERE IS NO LOCALIZER FRQ DIALED IN. AUTOPILOT WILL DISENGAGE DFGS NR 1 WORKS FINE. REMOVED AND RE PLACED NR 2 VHF/NAV CONTROL PANEL PERFORMED RTS CHECK TEST SYSTEM GIVES 'GO' INDICATION. (M) 2 L 7 2 4F A6WE 2002091900061 20020919 00061 WP 2002 9 19 DHL2002803009 1 20020919 A 3230 PROXIMITY SWITCH DOUG DC8 DC873 302199C WP A DHLA O OTHER O OTHER CL CLIMB 1 SO 01 803DH 46123 1) AFTER GEAR RETRACTION DOORS NOT LATCHED LIGHT REMAINED ON CYCLED GEAR 4-5 TIMES IAW ABNORMAL PROCEDURE BEFORE LIGHT WENT OUT POSSIBLE REPEAT ITEM FROM AUG 8 OR 102) CLEANED GEAR DOOR PROX SWITCHED OPS CK GOOD PWE MM 32 60 0 2 L 7 4 4F RT 4A25 2002091900062 20020919 00062 NM 2002 9 19 QXEA0201248 1 20020818 A 1430 FASTENER DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - FASTENER LIFTING BELOW RIGHT HAND AFT CORNER OF VERTICAL STABILIZER LEADING EDGE PANEL 321GT. REPAIRED IAW DHC-82 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002091900063 20020919 00063 NM 2002 9 19 QXEA0201249 1 20020818 A 1430 FASTENER DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - FASTENER LIFTING BELOW RIGHT HAND AFT LOWER CORNER OF VERTICAL STABILIZER LEADING EDGE PANEL 321GT. REPAIRED IAW DHC-8 SRM 51-40-1. 2 H 7 2 4T RT A13NM 2002091900064 20020919 00064 NM 2002 9 19 QXEA0201250 1 20020820 A 5514 SUPPORT FITTING DHAV DHC8 DHC8202 2809007 NM HORIZ STAB GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND FORWARD HORIZONTAL STABILIZER SUPPORT FITTING IS GOUGED BETWEEN HORIZONTAL AND VERTICAL STABILIZERS. RE PAIRED IAW RD 8-55-847. 2 H 7 2 4T RT A13NM 2002091900065 20020919 00065 NM 2002 9 19 QXEA0201251 1 20020821 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND WING NR 4 FLAP TRACK OUTBOARD SIDE ROLLER CONTACT SURFACE ON TRACK HAS PITTING. REPAIRED IAW HORIZON AI R EA 2-57-185. 2 H 7 2 4T RT A13NM 2002091900066 20020919 00066 NM 2002 9 19 QXEA0201252 1 20020817 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - RIGHT HAND OUTBOARD NR 11 SEAT TRACK TOP AND BOTTOM CORROSION AT X437.0. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091900067 20020919 00067 NM 2002 9 19 QXEA0201253 1 20020817 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - RIGHT HAND OUTBOARD NR 11 SEAT TRACK TOP AND BOTTOM CORROSION AT X454.0. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091900068 20020919 00068 NM 2002 9 19 QXEA0201254 1 20020817 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - RIGHT HAND OUTBOARD NR 11 SEAT TRACK TOP AND BOTTOM CORROSION AT X468.0. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091900069 20020919 00069 NM 2002 9 19 QXEA0201255 1 20020817 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - RIGHT HAND OUTBOARD NR 11 SEAT TRACK TOP AND BOTTOM CORROSION AT X486.0. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091900070 20020919 00070 WP 2002 9 19 GTIA020735 1 20020630 A 7711 2047021 INDICATOR DOUG DC9 DC982 3022082 WP NR 1 EPR OSCILLATES A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 803NK 48087 FLL - FLT 380 - NR 1 EPR PERIODICALLY OSCILLATES BETWEEN .77 AND 2.2 DURING CRUISE AND DESCENT WITH IDLE POWER OSCILLATI ONS CAUSE AUTO THROTTLES TO TRIP OFF. REMOVED AND REPLACED NR 1 EPR INDICATOR, OPS CHECK GOOD PER MM 72-00-00. (M) 2 L 7 2 4F A6WE 2002091900071 20020919 00071 NM 2002 9 19 QXEA0201256 1 20020817 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - RIGHT HAND OUTBOARD NR 11 SEAT TRACK TOP AND BOTTOM CORROSION AT X499.0. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002091900072 20020919 00072 NM 2002 9 19 QXEA0201257 1 20020817 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - RIGHT HAND OUTBOARD NR 12 SEAT TRACK TOP CORROSION AT X516.0. REPAIRED IAW RD 8-53-3644. 2 H 7 2 4T RT A13NM 2002091900073 20020919 00073 NM 2002 9 19 QXEA0201258 1 20020817 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - RIGHT HAND OUTBOARD NR 12 SEAT TRACK BOTTOM WORN AND TOP INBOARD AND OUTBOARD EARS WORN AT X542.0. REPAIRED IAW R D 8-53-3644. 2 H 7 2 4T RT A13NM 2002091900074 20020919 00074 NM 2002 9 19 QXEA0201259 1 20020819 A 7120 MOUNT DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - NR 2 ENGINE NACELLE UPPER INBOARD DIAGONAL MOUNT STRUT HAS GOUGE MID SPAN ON TOP SIDE. REPAIRED IAW RD 8-54-036. 2 H 7 2 4T RT A13NM 2002091900075 20020919 00075 NM 2002 9 19 QXEA0201260 1 20020819 A 7120 MOUNT DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - NR 2 ENGINE NACELLE LOWER INBOARD DIAGONAL MOUNT STRUT HAS CIRCULAR CHAFE AT MID SPAN ON OUTBOARD SIDE. REPAIRED IAW RD 8-54-036. 2 H 7 2 4T RT A13NM 2002091900076 20020919 00076 NM 2002 9 19 QXEA0201261 1 20020819 A 5410 STRUT DHAV DHC8 DHC8202 2809007 NM NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - A LIGHT CHAFE EXISTS IN STRUT. REPAIRED IAW RD 8-54-036. 2 H 7 2 4T RT A13NM 2002091900077 20020919 00077 NM 2002 9 19 QXEA0201262 1 20020819 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM LT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND WING DRY BAY PANEL 523 AT LADDER PLATE HAS SCRATCH DAMAGE TO TOP SURFACE WHERE PANEL EDGE SEALANT GOES. REPAIRED IAW RD 8-57-499. 2 H 7 2 4T RT A13NM 2002091900078 20020919 00078 NM 2002 9 19 QXEA0201263 1 20020819 A 5720 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - CRACKED THE SUPPORT BRACKET AT TOP FORWARD SPAR FOR LEADING EDGE. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002091900079 20020919 00079 NM 2002 9 19 QXEA0201264 1 20020819 A 5720 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - CRACKED SUPPORT BRACKET BOTTOM FORWARD SPAR FOR LEADING EDGE AT YW139.000. REPAIRED IAW DHC-8 SRM 51-40-00 AND SR M 51-40-11. 2 H 7 2 4T RT A13NM 2002091900080 20020919 00080 NM 2002 9 19 QXEA0201265 1 20020819 A 5720 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - CRACKED SUPPORT BRACKET UPPER FOR LEADING EDGE AT STATION 139.000, LEFT HAND WING. REPAIRED IAW DHC-8 SRM 51-20-1 1. 2 H 7 2 4T RT A13NM 2002091900081 20020919 00081 NM 2002 9 19 QXEA0201266 1 20020820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND OUTBOARD NR 1 SEAT TRACK TOP AND BOTTOM CORROSION AT X424.0. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002091900082 20020919 00082 NM 2002 9 19 QXEA0201267 1 20020821 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - RIGHT HAND OUTBOARD NR 10 SEAT TRACK TOP AND BOTTOM CORROSION AT X342.0. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-40-10. 2 H 7 2 4T RT A13NM 2002091900083 20020919 00083 NM 2002 9 19 QXEA0201268 1 20020821 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - RIGHT HAND OUTBOARD NR 10 SEAT TRACK HAS BARE METAL. REPLACED NR 10 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002091900084 20020919 00084 NM 2002 9 19 QXEA0201269 1 20020820 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND OUTBOARD NR 2 SEAT TRACK TOP AND BOTTOM CORROSION AT X486.0. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002091900085 20020919 00085 NM 2002 9 19 QXEA0201270 1 20020817 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND OUTBOARD NR 3 SEAT TRACK TOP CORROSION AT X516.0. REPAIRED IAW RD 8-53-3644. 2 H 7 2 4T RT A13NM 2002091900086 20020919 00086 EA 2002 9 19 QXEA0201212 1 20020810 A 2612 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA LT ENGINE LOOSE A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 614QX 10049 PDX- LEFT FIRE FAIL CAUTION MESSAGE ON TWICE DURING TAXI OUT. RETURNED TO GATE. TIGHTENED LOOSE CONNECTION ON LEFT HAN D ENGINE B-LOOP. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900087 20020919 00087 NM 2002 9 19 QXEA0201216 1 20020815 A 2120 ODOR BOMBDR DHC8 DHC8401 1390041 NM COCKPIT DETECTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 411QX 4055 SEA-FAINT SMELL OF SMOKE NOTICED FOLLOWED BY CAPTAINS MAP LIGHT CIRCUIT BREAKER POPPING. INSPECTED CAPTAINS LIGHT SOCKE T, RHEOSTAT AND LOCAL WIRING. NO DEFECT NOTED OR SIGNS OF OVERHEAT. RESET CIRCUIT BREAKER. OPERATED MAP LIGHT AT ALL SETTINGS. CIRCUIT BREAKER STAYED RESET. SYSTEM CHECKS OK. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091900088 20020919 00088 NM 2002 9 19 QXEA0201217 1 20020813 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - EMPENNAGE EXTERIOR LEFT HAND SIDE SKIN HAS A DENT AT FSX803.000 AND Z172.000. REPAIRED IAW SRM 53-30-24, FIGURE 1 SHEET 4 PAGE 1. 2 H 7 2 4T RT A13NM 2002091900089 20020919 00089 NM 2002 9 19 QXEA0201218 1 20020813 A 5720 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - BLEED AIR SUPPORT Z-BRACKET CRACKED AT RIGHT HAND WING FRONT SPAR, STATION YW53.200. REPAIRED IAW DHC-8 SRM 51-40 -11 AND HORIZON AIR EA 2-57-178. 2 H 7 2 4T RT A13NM 2002091900090 20020919 00090 NM 2002 9 19 QXEA0201219 1 20020811 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LOWER FORWARD BAG DOOR STOP AT STATION 564.5 HAS WEAR TO STOP. REPAIRED IAW RD 8-53-104. 2 H 7 2 4T RT A13NM 2002091900091 20020919 00091 NM 2002 9 19 QXEA0201220 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND INBOARD SEAT TRACK HAS CORROSION ON OUTBOARD FLANGE AT X222.000. REPAIRED IAW DHC-8 SRM 51-40-00 AND SR M 51-40-11. 2 H 7 2 4T RT A13NM 2002091900092 20020919 00092 NM 2002 9 19 QXEA0201221 1 20020808 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND INBOARD SEAT TRACK HAS CORROSION ON OUTBOARD FLANGE AT X222.000. REPAIRED IAW DHC-8 SRM 51-40-00 AND SR M 51-40-11. 2 H 7 2 4T RT A13NM 2002091900093 20020919 00093 NM 2002 9 19 QXEA0201222 1 20020812 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - UPPER FUSELAGE SKIN HAS DENT AT X291.400 BETWEEN STRINGERS 13 AND 2155.550. REPAIRED IAW RD 8-53-6856. 2 H 7 2 4T RT A13NM 2002091900094 20020919 00094 NM 2002 9 19 QXEA0201223 1 20020806 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - TCAS BOTTOM ANTENNA HAS SURFACE CORROSION ON SKIN. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002091900095 20020919 00095 NM 2002 9 19 QXEA0201224 1 20020813 A 5523 ARM DHAV DHC8 DHC8202 2809007 NM ELEVATOR TAB CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - RIGHT HAND ELEVATOR SPRING TAB NR 3 HINGE ARM HAS CHAFE DAMAGE. REPAIRED IAW HORIZON AIR EA 2-55-72. 2 H 7 2 4T RT A13NM 2002091900096 20020919 00096 NM 2002 9 19 QXEA0201225 1 20020815 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND INBOARD FLAP IS CHAFED FROM INBOARD EDGE FORWARD OF TRAILING EDGE. REPAIRED IAW HORIZON AIR EA 2-57-183 . 2 H 7 2 4T RT A13NM 2002091900097 20020919 00097 NM 2002 9 19 QXEA0201226 1 20020813 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND NR 4 FLAP TRACK HAS PITTING ON OUTBOARD SIDE WHERE SIDE ROLLER MAKES CONTACT. REPAIRED IAW HORIZON AIR EA 2-57-180. 2 H 7 2 4T RT A13NM 2002091900098 20020919 00098 NM 2002 9 19 QXEA0201227 1 20020813 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - PITTING ON FLAP TRACK OF THE NR 4 TRACK BOTH SIDES ON RIGHT HAND WING. REPAIRED IAW HORIZON AIR EA 2-57-181. 2 H 7 2 4T RT A13NM 2002091900099 20020919 00099 NM 2002 9 19 QXEA0201228 1 20020813 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND NR 4 FLAP TRACK HAS SLIGHT PITTING INBOARD SIDE WHERE SIDE ROLLER MAKES CONTACT. REPAIRED IAW HORIZON A IR EA 2-57-180. 2 H 7 2 4T RT A13NM 2002091900100 20020919 00100 NM 2002 9 19 QXEA0201229 1 20020809 A 2752 ATTACH FITTING BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX- LEFT HAND INBOARD FLAP OUTBOARD ACTUATOR ATTACH BRACKET BEARING SURFACE DAMAGED BY ACTUATOR ATTACH PIN. REPAIRED I AW HORIZON AIR EA 6-57-51. 2 H 7 2 4T RT A13NM 2002091900101 20020919 00101 EU 2002 9 19 QXEA0201231 1 20020809 A 1430 FASTENER FOKKER F28 F28MK4000 4990810 EU LT WING LOOSE A QXEA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 497US 11173 PDX- CLASS THREE FUEL SEEP FROM LEFT HAND NR 5 LIFT DUMPER BELLCRANK FITTING, LOWER SIDE UPPER OUTBOARD HI-LOK. REPAIRE D IAW F-28 SRM 28-11-0-5 AND 27-50-5. 2 L 7 2 4F RT A20EU 2002091900102 20020919 00102 EA 2002 9 19 QXEA0201233 1 20020529 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 PDX- FORWARD CARGO BAY CHIMNEY ASSEMBLY AT TOP OF DOOR OPENING HAS SCREEN DAMAGE. MESH IS PULLED AWAY ON OUTBOARD SIDE. REMOVED AND REPLACED FORWARD CARGO BAY CHIMNEY ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900103 20020919 00103 EA 2002 9 19 QXEA0201234 1 20020529 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 DEN- PROTECTIVE COVERING OVER SMOKE DETECTOR IN FORWARD CARGO AREA BROKEN OPEN AND TORN. REMOVED AND REPLACED CAGE ASS EMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900104 20020919 00104 EA 2002 9 19 QXEA0201235 1 20020531 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX- FORWARD CARGO BAY SMOKE DETECTOR SCREEN DAMAGED. REMOVED AND REPLACED CENTER SMOKE DETECTOR CHIMNEY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900105 20020919 00105 EA 2002 9 19 QXEA0201236 1 20020530 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 BOI- FORWARD BAGGAGE BAY WIRE MESH CHIMNEY DAMAGED. REMOVED AND REPLACED FORWARD BAGGAGE BAY WIRE MESH CHIMNEY. OPERAT IONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900106 20020919 00106 EA 2002 9 19 QXEA0201237 1 20020530 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 TUS- CHIMNEY AT BAGGAGE DOOR DAMAGED. REMOVED AND REPLACED FORWARD PIT CENTER SMOKE DETECTOR CHIMNEY. OPERATIONAL CHEC K GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900107 20020919 00107 EA 2002 9 19 QXEA0201238 1 20020529 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 PDX- MESH CAGE AT DOOR OPENING DAMAGED. REMOVED AND REPLACED SMOKE DETECTOR CHIMNEY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900108 20020919 00108 EA 2002 9 19 QXEA0201239 1 20020530 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 MFR- FORWARD CENTER SMOKE DETECTOR MESH DAMAGED. INSTALLED NEW GUARD ASSEMBLY OVER FORWARD CENTER SMOKE DETECTOR. OPER ATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900109 20020919 00109 EA 2002 9 19 QXEA0201240 1 20020530 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 608QX 10026 PDX- DAMAGE FOUND TO THE SCREEN OF FORWARD BAGGAGE BAY CHIMNEY ASSEMBLY AT CENTER SMOKE DETECTOR. REMOVED AND REPLACED FORWARD CARGO SMOKE DETECTOR PROTECTIVE COVERING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900110 20020919 00110 EA 2002 9 19 QXEA0201241 1 20020530 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 609QX 10031 BOI- WIRE MESH CHIMNEY ASSEMBLY IS DAMAGED ABOVE DOOR ASSEMBLY. REMOVED AND REPLACED DAMAGED CHIMNEY ASSEMBLY OVER FORW ARD CARGO DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900111 20020919 00111 EA 2002 9 19 QXEA0201242 1 20020530 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 610QX 10033 BOI- COMPLIED WITH HORIZON AIR EA TO INSPECT FORWARD CARGO COMPARTMENT WIRE MESH CHIMNEY ASSEMBLY AT ENTRANCE. REMOVED AND REPLACED CHIMNEY ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900112 20020919 00112 EA 2002 9 19 QXEA0201243 1 20020530 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 10041 BOI- COMPLIED WITH HORIZON AIR EA TO INSPECT FORWARD CARGO COMPARTMENT WIRE MESH CHIMNEY ASSEMBLY AT ENTRANCE. REMOVED AND REPLACED CHIMNEY ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900113 20020919 00113 NM 2002 9 19 QXEA0201244 1 20020821 A 7931 APT7610001000D TRANSMITTER DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE MALFUNCTIONED A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 369PH 9794 9794 513 SEA- ON TAKEOFF ROLL IN SEA, NR 2 OIL PRESSURE DROPPED TO 40 PSI. ABORTED TAKEOFF. OIL PRESSURE RETURNED TO NORMAL ONE RUNWAY WAS CLEARED. NO NR 2 OIL PRESSURE WARNING LIGHT. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER. O PERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091900114 20020919 00114 EA 2002 9 19 QXEA0201245 1 20020805 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 610QX 10033 BOI- CHIMNEY SECTION IN FORWARD CARGO PIT ABOVE CARGO DOOR IS BENT. REPLACED DAMAGED UNIT WITH SERVICEABLE UNIT. OPERA TIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900115 20020919 00115 EA 2002 9 19 QXEA0201246 1 20020821 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX- FORWARD CARGO SMOKE DETECTOR CHIMNEY DAMAGED. REMOVED AND REPLACED FORWARD CARGO SMOKE DETECTOR CHIMNEY. OPERATIO NAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900116 20020919 00116 NM 2002 9 19 QXEA0201247 1 20020821 A 5720 ANGLE DHAV DHC8 DHC8202 2809007 NM LT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND WING TOP EDGE NUT PLATE ANGLE FOR LEADING EDGE PANELS 512AL AND 512DL HAS SCRATCH DAMAGE TO FORWARD SPAR TOP EDGE. REPAIRED IAW RD 8-57-1675. 2 H 7 2 4T RT A13NM 2002091900117 20020919 00117 CE 2002 9 19 2002F00889 1 20020905 A 2121 26193873 BLADES LEAR 35 31A 5170531 CE FAN BINDING E W9FA O OTHER O OTHER NR NOT REPORTED 1 EA 07 131LJ 750 063 FAN BLADES CONTACTING HOUSING. 2 L 7 2 4F RT A10CE 2002091900118 20020919 00118 SO 2002 9 19 920DM 2 20020812 A 8530 VALVE GUIDE PIPER PA28 PA28R201T 7102813 SO CONT O360 TSIO360FB 17025 SO ENGINE BROKEN B B9YR O OTHER O OTHER NR NOT REPORTED 1 GL 07 920DM 454 454 28R8231047 300099 CYLINDER WAS REMOVED FOR LEAKING EXHAUST VALVE BY CUSTOMER. UPON DISASSEMBLY AND REMOVAL OF LOWER VALVE SPRING RETAINER , THE GUIDE WAS FOUND TO BE IN TWO PIECES. THE LOWER HALF WAS STILL IN THE CYLINDER HEAD AND ID WAS EXTREMELY WORN AND OVAL SHAPED. THE FRACTURE HAD OCCURRED JUST BELOW THE FLANGE OF THE GUIDE AT THE CYLINDER HEAD BOSS. 1 L 7 1 3O 3 O 2A13 E9CE 2002091900119 20020919 00119 NM 2002 9 19 QXEA0201271 1 20020817 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND OUTBOARD NR 3 SEAT TRACK TOP EARS WORN AT X530.0. REPAIRED IAW RD 8-53-3644. 2 H 7 2 4T RT A13NM 2002091900120 20020919 00120 2002 9 19 DHL2002741013 4 20020919 A 3414 2083081 INDICATOR BOEING 727 7272Q9 138448M NM A DHLA C D O ABORTED TAKEOFF RETURN TO BLOCK OTHER O OTHER TO TAKEOFF 1 SO 01 741DH 21931 1) REJECTED TAKE OFF DUE TO FIRST OFFICER'S AIRSPEED INDICATED 40 KNOTS SLOWER THAN CAPTAINS. EMERGENCY CHECK LIST COMP LETED.2) REMOVED AND REPLACED F/O'S AIRSPEED INDICATOR PER M/M 34-12-21 INSPECTED PITOT STATIC SYSTEM, FOUND F/O PITOT TUBE PLUGGED, REMOVED DEBRIS AND CLEANED PITOT TUBE. PERFORMED PITOT STATIC SYSTEM TEST PER M/M 34-11-00. PERFORMED AIRS PEED INDICATORS TEST PER M/M 34-12-12. OPS CHECKED GOOD. A/C OK TO CONTINUE.3) CREW REJECTED TAKEOFF AT 105 KTS. INDICA TED ON CAPT.'S INDICATOR, AMBIENT AIR TEMP 28 C., PRESS. ALT. 1400', A/C WEIGHT 131.5K, REPORTED FULL REVERSE THRUST USE D WITH MODERATE BRAKING. 4) REVIEWED AOM & BMM BRAKE COOLING CHARTS. PER M/M REQUIRES 20 MIN. GROUND TIME FOR 2 L 7 3 4F RT A3WE 2002091900121 20020919 00121 NM 2002 9 19 QXEA0201272 1 20020817 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND OUTBOARD NR 3 SEAT TRACK BOTTOM CORROSION AND TOP INBOARD AND OUTBOARD EARS WORN ZT X542.0. REPAIRED IA W RD 8-53-3644. 2 H 7 2 4T RT A13NM 2002091900122 20020919 00122 NM 2002 9 19 QXEA0201273 1 20020821 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND WING NR 4 FLAP TRACK INBOARD SIDE, SIDE ROLLER CONTACT SURFACE HAS PITTING. REPAIRED IAW RD 8-57-185. 2 H 7 2 4T RT A13NM 2002091900123 20020919 00123 NM 2002 9 19 QXEA0201274 1 20020820 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND WING OUTBOARD FLAP TOP INBOARD SKIN HAS CHAFE DAMAGE AT STATION YW178.000. REPAIRED IAW RD 8-57-1734. 2 H 7 2 4T RT A13NM 2002091900124 20020919 00124 NM 2002 9 19 QXEA0201276 1 20020824 A 5532 SKIN DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 PDX- SKIN DENT DAMAGE BETWEEN FRAME NR 3, FRONT SPAR AND STRINGERS 28S-28P IN THE VERTICAL STABILIZER. REPAIRED IAW HOR IZON AIR EA 2-55-69 -A-. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091900125 20020919 00125 NM 2002 9 19 QXEA0201277 1 20020825 A 3260 CONNECTOR DHAV DHC8 DHC8202 2809007 NM LT MLG DISCONNECTED A QXEA O OTHER J WARNING INDICATION LD LANDING 1 NM 09 362PH 518 SEA - AFTER LANDING, THE GEAR HORN SOUNDED, AND THE LEFT MAIN GEAR INDICATED UNSAFE AND GEAR INTRANSIT. MAINTENANCE INS PECTED THE AIRCRAFT AND FOUND PSEU FAULT CODE AND A DISCONNECTED CANNON PLUG ON THE LEFT GEAR. THE CANNON PLUG WAS RECO NNECTED AND A GEAR FUNCTIONAL CHECK WAS PERFORMED. CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091900126 20020919 00126 NM 2002 9 19 QXEA0201278 1 20020826 A 2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8202 2809007 NM MAIN SYS CONTAMINATED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 360PH 515 PDX - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A RUDD FULL PRESS CAUTION LIGHT FOLLOWED BY A RUDD PRESS CAUTION LIGHT. BOTH LIGHTS WENT OUT WHEN FLAPS WERE AT 15 DEGREES PRIOR TO LANDING. MAINTENANCE INSPECTED THE A IRCRAFT AND FOUND AIR IN THE HYDRAULIC SYSTEM. SYSTEM WAS BLED AND SERVICED. OPERATIONAL CHECKS WERE GOOD AND THE AIRC RAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091900127 20020919 00127 EU 2002 9 19 QXEA0201279 1 20020825 A 3310 SOCKET FOKKER F28 F28MK4000 4990810 EU COCKPIT DEFECTIVE A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 493US 11161 PDX- BURNT SMELL IN COCKPIT. REMOVED AND REPLACED PILOT'S CENTER PEDESTAL. INBOARD SIDE RED LAMP SOCKET. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002091900128 20020919 00128 NE 2002 9 19 GTIA020746 2 20020618 A 7200 LINER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 726971 NR 1 ENGINE ACCOUSTIC LINE DAMAGED 7 O'CLOCK POSITION FORWARD OF THE FUEL DRAIN, 4 INCH BY 4 INCH AREA. NR 1 ENGINE ACC OUSTIC LINER DAMAGE REINSPECT. TRANSFERRED TO C/O 34708-1. REINSPECTED NR 1 ENGINE ACCOUSTIC LINER DAMAGE OK FOR CONT SERVICE. C/O STILL ACTIVE. REMOVED AND REPLACED NR 1 ENGINE IAW MD80 MM 71-10-00. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002091900129 20020919 00129 NM 2002 9 19 QXEA0201280 1 20020825 A 3610 VALVE DHAV DHC8 DHC8202 2809007 NM BLEED AIR CARBONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 367PH 511 SEA- NR 1 ENGINE BLEED AIR PRODUCES BLUE HAZE WHEN FIRST TURNING ON AFTER ENGINE START. HAZE AND ACCOMPANYING SMELL LAS T ONLY 2-4 MINUTES. CLEANED CARBON BUILDUP ON NR 1 P2.5-3 SWITCHING VALVE. NO SMOKE OR SMELL NOTED. NO PARTS REPLACED , OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091900130 20020919 00130 EA 2002 9 19 QXEA0201283 1 20020827 A 2611 96847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 BOI- FIRE DETECTION CHIMNEY IN FORWARD CARGO COMPARTMENT IN ENTRYWAY IS DAMAGED. REMOVED AND REPLACED CHIMNEY PIECE IN ENTRYWAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002091900131 20020919 00131 NM 2002 9 19 QXEA0201284 1 20020825 A 5320 WEB DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND INBOARD SEAT TRACK NR 5 HAS TWO BAD RIVETS AND DAMAGE TO WEB AROUND FIVE RIVETS BETWEEN X510.0 AND X531. 0. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002102800133 20021028 00133 EU 2002 10 28 02FDEA00655 1 20020919 A 5330 A5361206020200 SKIN AIRBUS 310 A310 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 FUSELAGE SKIN INNER SURFACE CORRODED IN AVIONICS COMPT ON RIGHT SIDE OF ENTRY HATCH BETWEEN 8 & 9. CORROSION BLENDOUT D EPTH IS BEYOND LIMITS OF SRM 53-10-00. R&R STIFFENER PER EA 6-5330-65-66446. 2 L 7 2 4F RT A35EU 2002092400068 20020924 00068 NM 2002 9 24 F3LA200200261 1 20020913 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED FRAME CRACKED AT BS 460 BETWEEN STR 26R AND 27R. REPAIRED CRACKED FRAME PER SRM 5 3-00-07. 2 L 7 2 4F RT A16WE 2002091900132 20020919 00132 NM 2002 9 19 QXEA0201286 1 20020826 A 5320 GUSSET DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - GUSSET SCRATCHED ON FRAME AT LOWER CORNER OF EMERGENCY EXIT APERTURE AT STATION X240.5, STRINGER 23S. REPAIRED IA W DHC-8 SRM 51-40-11 AND HORIZON AIR EA 2-53-419. 2 H 7 2 4T RT A13NM 2002091900133 20020919 00133 NM 2002 9 19 QXEA0201288 1 20020821 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM FUSELAGE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - TWO SMOKING RIVETS IN SKIN ABOVE RIGHT HAND EMERGENCY EXIT. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002091900134 20020919 00134 NM 2002 9 19 QXEA0201289 1 20020822 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM RT WING LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - TWO LOOSE RIVETS AT RIGHT HAND WING ROOT FAIRING SCUPPER DRAIN OUTLET AT STATION X424. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002091900135 20020919 00135 NM 2002 9 19 GTIA020861 1 20020718 A 2420 GCU DOUG MD80 MD83 3023681 NM LT GENERATOR MALFUNCTIONED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 822NK 49392 DTW - FLT 874 - AT CRUISE, RECEIVED THE AC CROSSTIE LOCKOUT LIGHT, LT FLIGHT FAULT AND LT GEN OFF LIGHT ON AFTER REINSTA LLING POWER TO THE LT AC SYSTEM WITH THE APU PER OUR QRH. UNABLE TO RESTORE LEFT GENERATOR POWER. REMOVED AND REPLACED GENERATOR CONTROL UNIT. TIGHTEN ALL FIREWALL GEN CONTROL AND POWER CONNECTORS. OPS CHECK NORMAL ENGINE. (M) 2 L 7 2 4F RT 2002091900136 20020919 00136 NM 2002 9 19 QXEA0201290 1 20020822 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM OIL COOLER MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - RIVET MISSING FROM OIL COOLER BOX STRUCTURE, OUTBOARD OF OIL COOLER. REPLACED RIVET IAW DHC-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002091900137 20020919 00137 NM 2002 9 19 QXEA0201291 1 20020823 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LIGHT CORROSION EXPOSED AROUND NUT PLATE HOLES AFTER REMOVAL OF MAIN CABIN DOOR SILL. REPAIRED IAW DHC-8 CPM, CHA PTER 5, PAGE 5-1 TO 5-5. 2 H 7 2 4T RT A13NM 2002091900138 20020919 00138 NM 2002 9 19 QXEA0201292 1 20020825 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - TWO FASTENER HOLES ARE ELONGATED FORWARD END OF NR 6 SEAT TRACK/RAIL IN THE NR 5/6 SPLICE AREA. REPAIRED IAW DHC- 8 SRM 51-40-00, TABLE 4. 2 H 7 2 4T RT A13NM 2002091900139 20020919 00139 NM 2002 9 19 QXEA0201293 1 20020826 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 [DX - SCRATCH ON TOP FLANGE OF FLOOR SUPPORT FRAME AT X242 JUST OUTBOARD OF RIGHT HAND INBOARD SEAT TRACK. REPAIRED IAW HORIZON AIR EA 2-53-418. 2 H 7 2 4T RT A13NM 2002091900140 20020919 00140 NM 2002 9 19 QXEA0201294 1 20020818 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - CORROSION ON RIGHT HAND INBOARD SEAT TRACK AT AFT LUG IN CARGO PIT AT STATION 597. REPAIRED IAW DHC-8 SRM 51-40-0 0. 2 H 7 2 4T RT A13NM 2002091900141 20020919 00141 NM 2002 9 19 QXEA0201295 1 20020822 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - CORROSION ON ANGLE BELOW PANEL 144CZ AT AFT END. REPAIRED IAW DHC-8 SRM 51-20-57. 2 H 7 2 4T RT A13NM 2002091900142 20020919 00142 NM 2002 9 19 QXEA0201296 1 20020822 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - CORROSION ON ANGLE, BELOW PANEL 144AX (AFT END). REPAIRED IAW DHC-8-200 SRM 51-20-57 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002091900143 20020919 00143 NM 2002 9 19 GTIA020862 1 20020729 A 2420 GENERATOR DOUG MD80 MD83 3023681 NM LEFT FAILED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 822NK 49392 DTW - FLT 706 - AFTER TAKEOFF OVER MILE AREA, LEFT GEN FAULT FEEDER AND GEN BUS AND X-TIE LIGHT CAME ON, QRH FOLLOWED. FOUND LEFT GENERATOR BAD. ON GENERATOR T5 TO T6 READ .5 OHMS WHICH FAIL GENERATOR. REMOVED AND REPLACED LEFT POWER REL AY FOR PRECAUTIONARY. (M) 2 L 7 2 4F RT 2002091900144 20020919 00144 NM 2002 9 19 QXEA0201297 1 20020823 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - CRACK IN LEFT HAND NACELLE AFT FIREWALL APPROXIMATELY 2 O'CLOCK POSITION. REPAIRED IAW DHC-8-200 RD 8-54-611. 2 H 7 2 4T RT A13NM 2002091900145 20020919 00145 WP 2002 9 19 GTIA020863 1 20020725 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - FOUND UPPER FUSELAGE AT STATION 313, LONGERON 1 CRACKED UNDER NR 2 VHF ANTENNA. FORMED FILLER AND DOUBLER. INSTA LLED NEW REPAIR. (M) 2 L 7 2 4F A6WE 2002091900146 20020919 00146 NM 2002 9 19 QXEA0201298 1 20020824 A 5230 DOOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - CARGO DOOR GOUGED AT UPPER EDGE. REPAIRED IAW RD 8-52-029. 2 H 7 2 4T RT A13NM 2002091900147 20020919 00147 NM 2002 9 19 QXEA0201299 1 20020824 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - MAIN CABIN DOOR SILL CORRODED. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002091900148 20020919 00148 WP 2002 9 19 GTIA020864 1 20020623 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - FOUND CABIN LBL STATION 896, INBOARD SEAT TRACK, HAS CORROSION. REMOVED SEAT TRACKS. FABRICATED NEW SEAT TRACKS. INSTALLED SEAT TRACKS. (M) 2 L 7 2 4F A6WE 2002091900149 20020919 00149 WP 2002 9 19 GTIA020865 1 20020624 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND RIGHT INBOARD SEAT TRACK HAS AREAS OF CORROSION. REMOVED SEAT TRACKS. INSTALLED SEAT TRACKS. (M) 2 L 7 2 4F A6WE 2002091900150 20020919 00150 NM 2002 9 19 2002F00890 1 20020710 A 3110 D4168P CONNECTOR BOEING 727 727225 1384077 NM COCKPIT DIRTY A MYWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 803MA 22434 AT POWER UP BEFORE TAKEOFF IN KEF, TAKEOFF WARN HORN CAME ON. AIRCRAFT WAS PROPERLY CONFIGURED. EXITED RUNWAY, CYCLED CONTROLS AND RUNUP, NO HELP. RETURN TO GATE. REMOVED CONNECTOR PLUG D4168P FOUND DIRTY. CLEANED CONNECTOR PLUG AND RE INSTALLED. OPS CHECKED SYSTEM IAW MM 31-26-0. (M) 2 L 7 3 4F A3WE 2002091900151 20020919 00151 EU 2002 9 19 A6WA200260019 1 20020619 A 7600 LINKAGE BAC 146 146200A 1500266 EU NR 1 ENGINE DAMAGED A A6WA O OTHER Y ENGINE STOPPAGE LD LANDING 1 GL 31 291UE E2084 DURING LANDING ROLL OUT, NR 1 GENERATOR FELL OFF LINE A FEW MOMENTS LATER, NR 1 ENGINE FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE UPPER AND LOWER ENGINE CONTROL LINKAGE ROD ENDS. RE-RIGGED CONTROL LINKAGE AND TMS ACTUATOR, GROUN D RAN, OPS CHECK GOOD. (M) 2 H 7 4 4F A49EU 2002091900152 20020919 00152 WP 2002 9 19 GTIA020867 1 20020701 A 5210 PIN DOUG DC9 DC982 3022082 WP PAX DOOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND DAMAGE AT FORWARD SERVICE DOOR HOLD OPEN PIN REQUIRES REPAIR. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2002091900153 20020919 00153 WP 2002 9 19 GTIA020868 1 20020703 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND EXTERNAL FUSELAGE SKIN AT STATION 451, LONGERON 22 LEFT IS DAMAGED/GOUGED. CUT OUT DAMAGED AREA. FORMED NE W REPAIR DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2002091900154 20020919 00154 WP 2002 9 19 GTIA020869 1 20020705 A 5320 PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - AFT FUSELAGE UNPRESSURED INTERNAL, HAS LIGHT CORROSION/BARE METAL AT FORWARD FACE PANEL SUPPORT HOUSING AND CANTED . REMOVED FACE PANEL. FABRICATED NEW FACE PANEL. INSTALLED FACE PANEL. (M) 2 L 7 2 4F A6WE 2002091900155 20020919 00155 WP 2002 9 19 GTIA020870 1 20020619 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND DENT ON LEFT SIDE OF FUSELAGE FORWARD OF DOOR. CUT OUT DAMAGED AREA. FORMED FILLER AND FINGER DOUBLER. IN STALLED DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2002091900156 20020919 00156 WP 2002 9 19 GTIA020871 1 20020801 A 3260 PROXIMITY SENSOR DOUG DC9 DC981 3022081 WP NLG INTERMITTENT A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 ORD - FLT 433 - NOSE GEAR UNSAFE LIGHT CAME ON AT FL330, LIGHT EXTINGUISHED AFTER PRESSURIZING HYDRAULICS. DETERMINED T HE NLG GEAR UP PROXIMITY SENSOR IS OPERATING INTERMITTENTLY. REMOVED AND REPLACED THE NOSE GEAR UP SENSOR. (M) 2 L 7 2 4F A6WE 2002091900157 20020919 00157 WP 2002 9 19 MEX2002140 1 20020605 A 2420 696233B CSD DOUG DC9 DC987 3022087 WP NR 1 ENGINE FAILED A ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 1075T 49724 FLT 307 - MEX-ACA - TECHNICAL PERSONNEL AT GATE REPORT THAT THE ENGINE NR 1 CSD HAD DAMAGE OUT OF LIMITS AND THE MASTER CAUTION LIGHT WAS ON AS A CONSEQUENCE OF OIL LOW PRESSURE. AIRCRAFT WAS SENT TO THE HANGAR AND THE CSD AND THE RADIATOR OIL WERE CHANGED IAW WITH MM 24-10-1 AND 24-10-3, TESTS OK. (M) 2 L 7 2 4F RT A6WE 2002091900158 20020919 00158 WP 2002 9 19 MEX2002144 1 20020805 A 2130 HOSE DOUG DC9 DC987 3022087 WP COOLING TURBINE LEAKING A ASMF J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 205AM 49405 FLT 602 - MEX-DFW - AIRCRAFT RETURN TO FLIGHT DUE TO PRESSURIZATION FAILURE FLOW LIGHT ON WITH A 7.5 OF CABIN DIFFERENTI AL PRESSURE AT 10000 FT. HOSE RUBBER LEFT COOLER TURBINE WERE CHANGED IAW MM 21-20-00, TESTS OK. (M) 2 L 7 2 4F RT A6WE 2002091900159 20020919 00159 NM 2002 9 19 MEX2002145 1 20020905 A 2930 WARNING SYSTEM BOEING 757 7572Q8 1384972 NM HYD SYSTEM ACTIVATED A ASMF D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 23 805AM 26272 FLT 902 - MEX-MTY - AIRCRAFT RETURN TO GATE DUE TO CENTRAL AND LEFT HYDRAULIC SYSTEM RSVR LIGHT CAME ON. SUPPLY LINES A ND DEPRESSURIZATION VALVES WERE CHECKED NO DAMAGE WAS FOUND. NITROGEN SYSTEM WAS SERVICED AND WAS TESTED IAW MM 29-11-0 0. DURING OVERNIGHT SERVICE, CHECKED THE LEFT HYDRAULIC SYSTEM IAW MM 29-30-00, TESTS OK. (M) 2 L 7 2 4F RT A2NM 2002091900160 20020919 00160 NM 2002 9 19 MEX2002171 1 20020531 A 3246 3910097 WHEEL DOUG MD88 MD88 3023688 NM NLG FAILED A ASMF D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SW 23 169PL 53175 FLT 204 - MEX-GDL - DURING TAXIING, THE STEERING CONTROL WAS LOST AND IT GOT OBSTRUCTED, NOSE LANDING GEAR. AIRCRAFT WA S SENT TO THE HANGAR. NOSE LANDING GEAR WAS INSPECTED IAW MM 32-20-00 AND STEERING WAS CHECKED IAW MM 32-50-00. NOSE L ANDING GEAR WHEELS WERE REPLACED IAW MM 32-40-02. (M) 2 L 7 2 4F RT A6WE 2002091900161 20020919 00161 WP 2002 9 19 MEX2002218 1 20020714 A 3080 39271012 VALVE DOUG DC9 DC982 3022082 WP ANTI ICE SYS FAILED A ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 505MD 32744 49149 FLT 132 - MEX-BJX - WHEN THE ANTI-ICE SYSTEM IS ON, THE LIGHT CABIN FLOW WAS TURNED ON. AT RON MEX 14/15, IT WAS PERFOR MED THE ANTI-ICE TEST IN MODE 1 AND 2. THE LEFT AUGMENTATION VALVE WAS REPLACED, TESTS OK IAW MM 21-31-021. (M) 2 L 7 2 4F A6WE 2002091900162 20020919 00162 NM 2002 9 19 MEX2002251 1 20020208 A 2150 20495056 ACM DOUG MD88 MD88 3023688 NM ACM BAY FAILED A ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 158PL 27291 5060 49761 FLT 601 - ATL-MEX - AIRCRAFT RETURNED AFTER TAKEOFF DUE TO 'FLOW' LIGHT. A/C SYSTEM WAS VERIFIED BY LEAKAGES AND FAILUR E IN PRESSURIZATION VALVES, CHECKS OK. IT WAS PERFORMED A TEST TO THE FLOW CONTROLLERS AND THEY FAILED. AIRCRAFT WAS P RESSURIZE WITH APU AND ENGINES, SYSTEM FAILED WITH ENGINES. FLOW CONTROL VALVES WAS SWAPPED, PRESSURIZATION TEST WAS PE RFORMED WITH ENGINES, CHECK OK. DURING TRANSIT CHECK THE COOLING TURBINE AND THE FLOW CONTROL VALVE WERE REPLACED. (M) 2 L 7 2 4F RT A6WE 2002091900163 20020919 00163 NE 2002 9 19 MEX2002252 2 20020408 A 7320 FUEL CONTROL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 160PL 49763 FLT 125 - GDL-DFW - AIRCRAFT RETURNED TO GATE DUE TO HIGH TEMPERATURE IN EGT ENGINE 1, N2 49, F/F 810 AND SLOW ACCELERAT ION. THROTTLE CHAMBER WAS VERIFIED AND WATER SUMP WAS DRAINED. ENGINE WAS STARTED BUT FAILURE CONTINUED. AIRCRAFT WAS CARRIED TO THE HANGAR TO REPLACE THE FCU AND PERFORMED A TRIM IAW MM 71-00-00, TESTS OK. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002091900164 20020919 00164 WP 2002 9 19 MEX2002253 1 20020408 A 5350 RADOME DOUG DC9 DC982 3022082 WP NOSE SEPARATED A ASMF O OTHER D INFLIGHT SEPARATION LD LANDING 1 SW 23 1003X 48067 FLT 477 - IAH-MEX - DURING LANDING CAPTAIN FELT A HIT TO THE AIRCRAFT. AT TRANSIT CHECK THE NOSE COWLING OF THE RIGHT E NGINE WAS FOUND WITH A DAMAGE IN ITS UPPER PART OF APPROXIMATELY 15 INCHES OF LENGTH OF 4 INCHES OF CUTTING, ALSO 5 BLAD ES WERE OUT OF LIMIT. MEX SENT SPARES AND TECHNICAL PERSONNEL TO PERFORM THE REPAIR. THREE SETS OF FAN BLADES AND NOSE COWLING WERE REPLACED, IT WAS PERFORMED A BOROSCOPE INSPECTION TO 6TH AND 7TH STAGE FAN. ENGINE WAS PROBED TO DIFFEREN T THRUST CONDITIONS, EVERYTHING OK IAW MM 72-33-21, 71-10-01 AND 72-00-00. (M) 2 L 7 2 4F A6WE 2002091900165 20020919 00165 NM 2002 9 19 MEX2002255 1 20020408 A 7500 CLAMP DOUG MD88 MD88 3023688 NM LT ENGINE BROKEN A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 168PL 53174 FLT 941 - MTY-MEX - AIRCRAFT RETURNED TO GATE, DUE TO PNEUMATIC LEAKAGE IN LEFT ENGINE. DURING REVISION IT WAS FOUND A CLAMP BROKEN OF THE 13TH STAGE AND A FOLDED PIPELINE OF THE SAME STAGE. CLAMPS AND ANTI-ICE DUCT WAS SENT TO SUCH STATI ON. PIPELINE AND CLAMPS WERE REPLACED IAW MM 75-10-05, TESTS OK. (M) 2 L 7 2 4F RT A6WE 2002091900166 20020919 00166 SO 2002 9 19 SIMA200221201 1 20020725 A 5310 ALCLAD2024T3 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 623AE 6878 145109 ABI - FOUND CORROSION ON LEFT OMEGA BEAM, PREVIOUS REPAIR, AT FRAME 20. REMVOED PREVIOUS REPAIR, CORROSION LIMITED TO P REVIOUS REPAIR. FABRICATED A DOUBLER ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 (SRM 145/1142, CHAPTER 53, R EV 18) 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002091900167 20020919 00167 SO 2002 9 19 SIMA200221202 1 20020724 A 5313 ALCLAD2024T3 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 623AE 145109 ABI - FOUND STRINGER 19R GOUGED. BLENDED GOUGE. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB-145 SRM 14 5/1142, CHAPTER 53 REV 18, 53-24-02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002091900168 20020919 00168 EU 2002 9 19 SIMA200221203 1 20020729 A 3350 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 319AM 319 MIA - FLT 5069 - FOUND EMERGENCY LIGHTS DON'T WORK WHEN AIRCRAFT IS NOT POWERED UP. LIGHT DON NOT WORK WHEN POWER IS ON IE, OR EXTERNAL POWER RAI ALL 6 BATTERY PACKS (S/N 6506, 6498, 6406, 6635, 6399, 269). (M) 2 H 7 2 4T RT A53EU 2002091900169 20020919 00169 SO 2002 9 19 SIMA200221204 1 20020727 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 623AE 145109 ABI - FOUND STRINGER 19L GOUGED. BLENDED GOUGE. FABRICATED TWO DOUBLER, FOUR SHIMS. REPAIR DONE IAW EMB145 SRM 145/11 42, CHAPTER 53, REV 18, 53-24-02, EMB GST 2298/02A, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002091900170 20020919 00170 SO 2002 9 19 SIMA200221205 1 20020727 A 5230 14525369003 CLIP EMB 145 EMB145LR 3260212 SO CARGO DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 623AE 6878 145109 ABI - FOUND CARGO DOOR SHEAR CLIP CORRODED AT FRAME 68. REMOVED CORROSION BY CUTOUT. FABRICATED A REPLACEMENT SPLICE. REPAIR DONE IAW EMB GST-2231-02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002091900171 20020919 00171 SO 2002 9 19 SIMA200221206 1 20020728 A 5310 14525480003 SILL EMB 145 EMB145LR 3260212 SO CARGO DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 623AE 145109 ABI - FOUND CARGO DOOR SILL CORRODED. REMOVED CORRODED SILL BEAM. INSTALLED NEW BEAM IAW EMB-145 SRM 145/1142, CHAPTER 51, REV 18) 51-20-03, 51-40-03 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002091900172 20020919 00172 EU 2002 9 19 SIMA200221902 1 20020807 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 277AT 277 MIA - FLT 5017 - DURING PREFLIGHT, CREW REPORTED SEVERAL FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED A BATTERY PACK IN ONE OF THE AFT POWER SUPPLY UNITS IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002091900173 20020919 00173 EU 2002 9 19 SIMA200222101 1 20020808 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 334AE 340B334 ABI - DURING INSPECTION, FOUND FRAME 686.66 DENTED. FABRICATED AND INSTALLED A DOUBLER IAW SAAB REPAIR STATEMENT 340 SD S 004197 PARA 3, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002091900174 20020919 00174 EU 2002 9 19 SIMA200222102 1 20020808 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 334AE 340B334 ABI - DUIRNG INSPECTION, FOUND FRAME 677 DENTED. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SAAB REPAIR STATEMENT 34 0SDS004197 PARA 3 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002091900175 20020919 00175 EU 2002 9 19 SIMA200222103 1 20020808 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 334AE 340B334 ABI - DURING INSPECTION, FOUND FRAME 630.112 DENTED. FABRICATED AND INSTALLED A DOUBLER IAW SAAB REPAIR STATEMENT 340SD S004197 PARA 3, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002091900176 20020919 00176 SO 2002 9 19 SIMA200222104 1 20020729 A 5310 BEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 733KR 145368 ABI - DURING INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS AND A PLATE. REPAIR DONE IAW EMB 145, SRM 145/1142, CHAPTER 53, REV 18, 53-21-10 P ARA 2, FIG 201 SHEET 1, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002091900177 20020919 00177 EU 2002 9 19 SIMA200222201 1 20020619 A 3350 301300 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 536AT 536 MIA - DURING SCHEDULED PS CHECK MAINTENANCE REPORTED A FLOOR PROXIMITY EMERGENCY LIGHT IN THE GALLEY TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT FOR THE GALLEY LIGHT IAW ATR MM. OPERATIONAL CHECK, W AS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002091900178 20020919 00178 EU 2002 9 19 SIMA200222202 1 20020702 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 550LL 550 MIA - DUIRNG SCHEDULED PS CHECK, MAINTENANCE REPORTED VERBAL FROM A PILOT, THE EMERGENCY BATTERIES (EMERGENCY LIGHTS) WE RE DEAD. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS IN EMERGENCY POWER SUPPLY UNITS 43WL AND 73WL IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002091900179 20020919 00179 EU 2002 9 19 SIMA200222203 1 20020704 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 269AT 269 MIA - DURING SCHEDULED PS CHECK, MAINTENANCE REPORTED THE AFT CABIN EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE RE MOVED AND REPLACED THE BATTERY PACK IN POWER SUPPLY UNIT 15WL IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS R ETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002091900180 20020919 00180 EU 2002 9 19 SIMA200222204 1 20020708 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 277AT 277 MIA - DURING SCHEDULED PS CHECK, MAINTENANCE REPORTED ONE BATTERY PACK FOR THE EMERGENCY TO BE INOPERATIVE, ONE SET OF L IGHTS. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002091900181 20020919 00181 SO 2002 9 19 SIMA200222401 1 20020811 A 2121 47359713 FAN EMB 135 EMB135KL 3260302 SO CARGO BAY INOPERATIVE A F A ACTIVATE FIRE EXT. UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 809AE 145521 DFW - FLT 3477 - DURING CLIMB, CREW REPORTED THE CARGO SMOKE LIGHT ILLUMINATED. CREW DECLARED AN EMERGENCY AND BLEW BOT TLES. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE FOUND THE VENTALATION FAN TO BE INOPERATIVE. FAN WAS REMOVED AND REPLACED IAW EMB MM OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2002091900182 20020919 00182 EU 2002 9 19 SIMA200222402 1 20020812 A 3350 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 269AT 269 MIA - FLT 5017 - DURING WALK AROUND CREW NOTED EMERGENCY LIGHT AT BOTTOM OF MAIN CABIN DOOR AND SOME EMERGENCY LIGHTS IN THE FORWARD CABIN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A POWER SUPPLY UNIT (P/N 301180, S/N 1374) AND A BATTERY PACK (P/N 3011151, S/N 6400) IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M ) 2 H 7 2 4T RT A53EU 2002091900183 20020919 00183 WP 2002 9 19 WXOA02002 1 20020517 A 3260 H141016 SWITCH DOUG DC9 DC987 3022087 WP NLG FAILED A WXOA O OTHER J WARNING INDICATION AP APPROACH 1 WP 17 948MA 49778 PSC - UNSAFE NOSE GEAR DOWN INDICATION REPORTED BY FLIGHT CREW ON APPROACH. CREW COMPLIED WITH AOM VOL 1 PROCEDURES. A IRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE FOUND FAILURE OF NOSE GEAR POSITION INTERLOCK SWITCH (S1-412) TO BE CAUSE OF SYSTEM MALFUNCTION. REMOVED AND REPLACED NOSE GEAR POSITION INTERLOCK SWITCH P ER MM 32-21-03. NOSE GEAR POSITION INDICATION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 2002091900184 20020919 00184 EA 2002 9 19 COMA0260535 1 20020917 A 5210 G80040 DOOR SEAL CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR LEAKING A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 940CA 7048 FLIGHT 5768 LOUD SQUEAL FROM CABIN DOOR.REPLACED THE DOOR SEAL. 2 L 7 2 4F RT A21EA 2002091900185 20020919 00185 EA 2002 9 19 COMA0260536 1 20020917 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 986CA 7174 FLIGHT 5295 CARGO DOOR CAUTION MESSAGE.DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2002091900186 20020919 00186 EA 2002 9 19 COMA0260537 1 20020917 A 2740 70608 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 01 988CA 19552 7204 FLIGHT 5824 STAB TRIM AND MACH TRIM CAUTION MESSAGE.COULD NOT DUPLICATE. REPLACED THE HSTCU. 2 L 7 2 4F RT A21EA 2002091900187 20020919 00187 NM 2002 9 19 AWXA200200897 1 20020831 A 5311 65C2511342 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A 2 1/2" CRACK WAS FOUND ON THE FORWARD CARGO COMPARTMENT FRAME BODY ABOVE STRING ER 21 L/H, BS 480. MAINTENANCE CUTOUT DAMAGED SECTION OF FRAME, REMOVED 3 EACH INTERCOASTALS FOR ACCESS, REMOVED 2 EACH STRINGER TIE CLIPS COMON TO REPAIR; FABRICATED 2 EACH REPAIR CHANNELS, 3 EACH REPAIR ANGLES, 2 EACH STRINGER CLIPS; INST ALLED REPAIR PARTS AND 3 EACH INTERCOASTALS IAW B737-200 SRM 51-40-3, PG. 1-6, FIG. 1. 2 L 7 2 4F RT A16WE 2002091900188 20020919 00188 NM 2002 9 19 QXEA0201472 1 20020917 A 2930 9604435 RESERVOIR BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 STUCK A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 412QX 1357 1357 4059 SEA - CREW PERFORMED ABNORMAL/EMERGENCY PROCEDURES WHEN DURING FLIGHT THEY RECEIVED A #1 INBOARD HYDRAULIC CAUTION AND # 1 HYDRAULIC ISOLATION VALVE LIGHTS. LIGHTS WENT OFF ON APPROACH. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE FLUID LEVEL GAUGE ON THE RESERVOIR STUCK. THE RESERVOIR WAS REPLACED AND SERVICED. OPERATIONAL AND LEAK CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002091900189 20020919 00189 SO 2002 9 19 C2XA02SH058 1 20020904 A 5315 14522461011 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV- DURING C CHECK INSPECTION, THE RT FLOORBEAM AT FRAME 22 WAS FOUND TO HAVE CORROSION. MAITENANCE REPAIRED AFFECTED AREA OF FLOORBEAM AND REMOVED AND REPLACED A DOUBLER IAW EC 5320-01073. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE . 2 L 7 2 4F RT T00011AT 2002091900190 20020919 00190 SO 2002 9 19 C2XA02SH059 1 20020902 A 5315 14525138013 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV- DURING C CHECK, SPLICE ANGLE WAS FOUND CRACKED AT LT FLOORBEAM BETWEEN FRAMES 16 AND 17. MAINTENANCE REMOVED AFFEC TED AREA AND PERFORMED A SPLICE REPAIR ON LT FLOORBEAM BETWEEN FRAMES 16 AND 17. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002091900191 20020919 00191 SO 2002 9 19 CX2A02SH60 1 20020831 A 5300 14524197005 BUTT STRAP EMB 145 EMB145ER 3260211 SO CABIN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV DURING C CHECK LEFT HAND LATERAL FLOOR BEAM STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 15 AND 19. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A SPLICE REPAIR IAW CONTINENTAL EXPRESS EC 5320-01074.THE AIRCRAFT WAS APPROVED TO RE TURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002091900192 20020919 00192 SO 2002 9 19 C2XA02SH061 1 20020831 A 5315 14590141001 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C CHECK INSPECTION, LT FLOORBEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 19 AND 21. MAINTENANCE REMOVED AFFEC TED PARTS AND REPAIRED LT FLOORBEAM IAW EMB SRM 53-21-10. THE AIRCRAFT WAS RETURN TO MAINTENANCE 2 L 7 2 4F RT T00011AT 2002092000001 20020920 00001 WP 2002 9 20 2002F00892 1 20020509 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION AT FORWARD CARGO DOOR FUSELAGE CUT OUT, FORWARD LOWER CORNER, INNER RADIUS WEB AND INNER SKI N, AT STATION 879. (M) 2 L 7 3 4F A22WE 2002092000002 20020920 00002 WP 2002 9 20 2002F00893 1 20020522 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON MAIN CABIN FLOOR SUPPORT, AT STATION 765 TO 879, LBL 47. (M) 2 L 7 3 4F A22WE 2002092000003 20020920 00003 WP 2002 9 20 2002F00894 1 20020522 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND MAIN CABIN FLOOR SUPPORT CORRODED AT STATION 840, RBL 89. (M) 2 L 7 3 4F A22WE 2002092000004 20020920 00004 WP 2002 9 20 2002F00895 1 20020514 A 5753 SKIN DOUG DC10 DC1010 3022110 WP TE FLAP GOUGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND INBOARD FAIRING OF RIGHT INBOARD FLAP GOUGED ON MIDDLE PART OF FAIRING. (M) 2 L 7 3 4F A22WE 2002092000005 20020920 00005 WP 2002 9 20 2002F00896 1 20020514 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BULKHEAD CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND AFT BULKHEAD SUPPORT ANGLE IN AFT CARGO BAY CEILING CORRODED AT STATION 1964. (M) 2 L 7 3 4F A22WE 2002092000006 20020920 00006 NM 2002 9 20 2002F00897 1 20020709 A 5343 652630023 BEAM BOEING 727 727222 1384073 NM MLG SUPPORT CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND CRACK AT LEFT MAIN LANDING GEAR SUPPORT BEAM, ON BEAM FITTING FORWARD MOUTN LUG, STATION 940. (M) 2 L 7 3 4F A3WE 2002092000007 20020920 00007 NM 2002 9 20 AALA20020898 1 20020616 A 7500 C8E3812 CONTROL UNIT BOEING 757 757223 1384957 NM LT ENG BLEED FAILED A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 636AM 24594 DFW - FLT 1873 - EN ROUTE DFW-SEA, AFTER TAKEOFF LEFT ENGINE EXHAUST TEMPERATURE WENT TO 903 FRO TWO SECONDS. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. TROUBLESHOT AND REPLACED BLEED VALVE CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002092000008 20020920 00008 NM 2002 9 20 AALA20020925 1 20020620 A 2932 211C223519 PRESSURE SWITCH BOEING 757 757223 1384957 NM HYD SYSTEM FAILED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 659AA 24617 MIA - FLT 971 - EN ROUTE MIA-MGA AT 35,000 FEET, LEFT HYDRAULIC SYSTEM FAILED. EMERGENCY DECLARED. AIRCRAFT RETURNED A ND LANDED AT MIA WITHOUT INCIDENT. TROUBLESHOT AND FOUND TO BE AN INDICATION FAULT. REPLACED PRESSURE SWITCH ON LEFT E NGINE DRIVEN PUMP. ALSO, REPLACED PRESSURE SWITCH ON POWER TURBINE UNIT AS A PRECAUTION. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002092000009 20020920 00009 NM 2002 9 20 AALA20020997 1 20020711 A 3233 AS11504K0232 HOSE BOEING 757 757223 1384957 NM MLG ACTUATOR CRACKED A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 668AA 25333 DFW - FLT 1265 - EN ROUTE SAT-DFW, COMPLETE LOSS OF LEFT HYDRAULIC SYSTEM QUANTITY. EMERGENCY DECLARED. LANDED DFW WIT HOUT INCIDENT. REPLACED RIGHT MLG LOCK ACTUATOR HOSE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002092000010 20020920 00010 NM 2002 9 20 AALA20021081 1 20020725 A 2910 5981096 SEAL BOEING 757 757223 1384957 NM FLAP CONTROL MOD LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 187AA 32382 IN CRUISE, LEFT HYD QTY LOW ON EICAS FOLLOWED PROCEED TO DEPRESS SYSTEM EXTENDED GEAR AND FLAPS USING ALTERNATE SYSTEM. REPLACED WORN SEAL ON FLAP/SLAT DEPRESSURIZATION CONTROL MODULE SOLENOID. SERVICED HYDRAULIC LT SYSTEM TO NORMAL PRESS , LT HYDRAULIC SYSTEM OPS CHECK OK, NO LEAKS NOTED. (M) 2 L 7 2 4F RT A2NM 2002092000011 20020920 00011 2002 9 20 AALA20021104 4 20020726 A 2565 D31393110 SLIDE BOEING 757 757223 1384957 NM OVERWING DEPLOYED A AALA A UNSCHED LANDING E F J VIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 21 7667A 25301 TUL - FLT 9603 - EN ROUTE TUL-DFW - AFTER TAKEOFF, RECEIVED EICAS MESSAGE FOR LEFT WING SLIDE PROBLEM. DURING LANDING, AIRCRAFT REQUIRED QUARTER WHEEL DEFLECTION FOR CONTROLLED FLIGHT. RETURNED TUL AND LANDED WITHOUT INCIDENT. REMOVED DE PLOYED OVERWING SLIDE THAT CAUSED AIRCRAFT BUFFETING AND WHEEL DEFLECTION AND REPLACED WITH SERVICEABLE UNIT. FOUND FOU R HOLES IN FILET PANEL WHICH WERE REPAIRED PER SRM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002092000012 20020920 00012 NM 2002 9 20 AALA20021106 1 20020727 A 2751 TRANSMITTER BOEING 757 757223 1384957 NM TE FLAPS INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 654A 24612 LAX - FLT 397 - EN ROUTE DFW-SNA, RECEIVED EICAS MESSAGE OF LEADING EDGE SLAT DISAGREEMENT. AIRCRAFT LANDED AT LAX WITH OUT INCIDENT. FOUND RIGHT SLAT POSITION TRANSMITTER OUT OF TOLERANCE. MADE ADJUSTMENTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002092000013 20020920 00013 NM 2002 9 20 AALA20021133 1 20020802 A 3350 CONNECTOR BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS AT 21C INOPERATIVE. TIGHTENED AND RESEATED LOOSE CONNE CTOR AT SEAT 21E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002092000014 20020920 00014 NM 2002 9 20 AALA20021134 1 20020804 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 389AA 27449 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SEAT 37B INOPERATIVE. REPAIRED WIRE ON EMERGENCY LIG HT CONNECTOR FOR SEAT 37B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002092000015 20020920 00015 NM 2002 9 20 AALA20021135 1 20020808 A 3233 271N61192 LINE BOEING 757 757223 1384957 NM MLG ACTUATOR LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 697AN 26977 SJU - FLT 1384 - EN ROUTE BGI-JFK - LEFT HYDRAULIC SYSTEM QUANTITY LOSS INDICATION IN COCKPIT. LANDED SJU WITHOUT INCID ENT. INSPECTED AND FOUND LEFT MAIN GEAR DRAG BRACE ACTUATOR LINE LEAKING. REPLACED LINE AND SERVICED SYSTEM. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002092000016 20020920 00016 NM 2002 9 20 AALA20021139 1 20020809 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT L1 CLOSET DAMAGED. REPLACED EMERGENCY ES CAPE PATH LIGHTING ASSEMBLY AT L1 CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002092000017 20020920 00017 NM 2002 9 20 AALA20021141 1 20020810 A 5210 DOOR BOEING 757 757223 1384957 NM MAIN PAX STUCK A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 650AA 24608 LAX - FLT 159 - ON ARRIVAL, L1 DOOR DIFFICULT TO OPEN. ASSIST BOTTLE FIRED AND SLIDE PARTIALLY DEPLOYED. SLIDE DID NOT FULLY DEPLOY BECAUSE OF JETBRIDGE. REPLACED DOOR SLIDE AND DOOR ASSIST BOTTLE. (M) 2 L 7 2 4F RT A2NM 2002092000018 20020920 00018 NM 2002 9 20 AALA20021147 1 20020812 A 3244 TIRE BOEING 757 757223 1384957 NM NR 3 MLG FAILED A AALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 21 688AA 25730 NR 3 MLG TIRE RECAP DEPARTED ON TAKEOFF LAX, FOUND ON RUNWAY. CREW ELECTED TO LAND IN HNL VERSUS LIH. FOUND TIRE STILL INFLATED YET RECAP DAMAGED NR 7 BRAKE LINE. REPLACED NR 3 AND NR 4 MLG TIRES AND DEACTIVATED NR 7 BRAKE PER MEL. (M) 2 L 7 2 4F RT A2NM 2002092000019 20020920 00019 NM 2002 9 20 AALA20021155 1 20020813 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT AT G3 GALLEY AREA BROKEN. REPLACED EMERGENCY ESCAPE PAT H LIGHT ASSEMBLY AT G3 GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002092000020 20020920 00020 NM 2002 9 20 AALA20021160 1 20020815 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 351AA 24032 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT LENS AT SEAT 29B IS INOPERATIVE. REPLACED SHIP TO CONNECTOR AT SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 2 4F RT A1NM 2002092000021 20020920 00021 NM 2002 9 20 AALA20021162 1 20020814 A 3350 LIGHT BOEING 777 777223 1385213 NM L1 CLOSET BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - DURING OVERNIGHT MAINTENANCE, L1 COAT CLOSET EMERGENCY LIGHT BROKEN. REPLACED L1 COAT CLOSET EMERGENCY LIGHT ASSE MBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002092000022 20020920 00022 SO 2002 9 20 SIMA200222802 1 20020816 A 3350 BATTERY PACK EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 704PG 145174 LGA - FLT 4475 - FOUND EMERGENCY BATTERY SWITCH SELECTED IN ON POSITION AND EMEREGNCY LIGHTS INOPERATIVE. REPLACED ALL FOUR EMERGENCY BATTERY PACKS, P/N'S OFF BATTERY PACKS 20131A, S/N OFF 69066, 67275, 68207, 63701. (M) 2 L 7 2 4F RT T00011AT 2002092000023 20020920 00023 SO 2002 9 20 SIMA200223301 1 20020818 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 621AE 145105 CREW REPORTED THE LAST STRIP OF FLOOR PROXIMITY EMERGENCY LIGHTING TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE ON THE STRIP LIGHT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002092000024 20020920 00024 EU 2002 9 20 USAASA0202072 1 20020813 A 3350 321430 BATTERY AIRBUS A319 A319112 3930323 EU EMERGENCY INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 701UW 890 TPA - AFT LEFT EMERGENCY BATTERY FAULTED ON TEST. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A28NM 2002092000025 20020920 00025 EU 2002 9 20 USAASA02069 1 20020811 A 3350 32145410 LIGHT AIRBUS A319 A319112 3930323 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 764US 1369 PHL - THE EMERGENCY EXIT LIGHTS AT FORWARD CENTER AND 1 LEFT AND RIGHT DOOR CEILING DO NOT ILLUMINATE WITH PERSONAL ELEC TRONIC DEVICES SIGN. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY AND BITE CHECKED GOOD . (M) 2 L 7 2 4F RT A28NM 2002092000026 20020920 00026 EU 2002 9 20 USAASA02070 1 20020811 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU PAX CABIN WILL NOT TEST A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 108UW 1061 CLT - THE AFT LEFT OVERWING EXIT EMERGENCY POWER SUPPLY UNIT FAILS TEST, INDICATING AN INTERIOR AND EXTERIOR LIGHTS FAUL T. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002092000027 20020920 00027 EU 2002 9 20 USAASA02072 1 20020813 A 3350 321430 BATTERY AIRBUS A319 A319112 3930323 EU AFT LEFT WILL NOT TEST A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 701UW 0890 TPA - AFT LEFT EMERGENCY BATTERY FAULTED ON TEST. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A28NM 2002092000028 20020920 00028 EU 2002 9 20 USAASA02073 1 20020817 A 3350 D31516113 LIGHT AIRBUS A321 A321211 3930370 EU L1 DOOR WILL NOT TEST A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 186US 1701 TPA - DURING THE EMERGENCY LIGHT TEST, THE EPSU EXTERNAL LOAD WAS FAULTED. THE L-1 DOOR SLIDE WAS REPLACED, THE R1 DOOR SLIDE CHECKED SATISFACTORY. (M) 2 L 7 2 4F RT A28NM 2002092000029 20020920 00029 NM 2002 9 20 USAASB02151 1 20020811 A 3350 20121 POWER SUPPLY BOEING 737 7374B7 1384702 NM AFT CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 776AU 24934 MIA - MAINTENANCE FOUND THE EMERGENCY LIGHT AFT OF THE R2 DOOR AND AT SEATS 24 AND 25, LEFT SIDE INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002092000033 20020920 00033 WP 2002 9 20 CALA0200467 1 20020918 A 5320 WEB DOUG DC9 DC982 3022082 WP STA 1211-1231 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 INSPECTION FOUND AFT BAGGAGE BIN SUB FLOOR STRUCTURE PLATE(WEB) CORRODED BETWEEN STA 1211 AND 1231 ABOVE LONGERON 28L-27 R. REPAIRED IAW ECRA 5311-01133. 2 L 7 2 4F A6WE 2002092000038 20020920 00038 2002 9 20 MWEA020576 4 20020918 A 3416 ALTIMETER DOUG DC9 DC932 3022066 WP COCKPIT FLUCTUATES A MWEA O OTHER S AFFECT SYSTEMS CR CRUISE 1 GL 31 209ME 47730 CAPTAIN'S STANDBY ALTIMETER FLUCTUATING. -- REMOVED AND REPLACED CAPTAIN'S STATIC SELECTOR VALVE. 2 L 7 2 4F A6WE 2002092000047 20020920 00047 EU 2002 9 20 AWXA200200882 1 20020911 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 663AW 2675 1419 PHX - EEL - DURING INSPECTION EMERGENCY EXIT LIGHTS FAILED TEST FROM PROGRAMMING AND TEST PANEL. MAINTENANCE FOUND THE RT EMERGENCY POWER SUPPLY UNIT INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY UNIT (12WL); OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002092000048 20020920 00048 EU 2002 9 20 AWXA200200883 1 20020912 A 5330 SKIN AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 645AW 238 PHX - MAJOR REPAIR - DURING INSPECTION THE FUSELAGE SKIN WAS FOUND CORRODED BENEATH AFT AIRPHONE ANTENNA. MAINTENANCE R EMOVED CORRODED SECTION OF SKIN FR 63, FABRICATED A DOUBLER, AND INSTALLED REPAIR IAW SRM 53-00-11 FIG 203. BLANKING PL ATE INSTALLED IAW AWA ER 26-2333-0056-JS4. 2 L 7 2 4F RT A28NM 2002092000049 20020920 00049 EU 2002 9 20 AWXA200200884 1 20020912 A 2497 7405869505 CABLE AIRBUS 320 A320232 3930326 EU NR 2 ENGINE ARCED A AWXA A UNSCHED LANDING J G WARNING INDICATION MULTIPLE FAILURE CR CRUISE 1 WP 28 661AW 1284 CREW RECEIVED AUTO FLT WARNINGS (FAC 2, YAW DAMPER 2, RUDDER TRAVEL LIMITER 2, RUDDER TRIM 2, SDAC 2), NO DATA FROM ALL 3 ADIRU'S. MESSAGES OCCURRED AT SAME TIME. MESSAGES NOTED & CLEARED. APPROX 20 MINS LATER ECAM MESSAGES REAPPEARED W/ NUMEROUS OTHER SYS MESSAGES; F/O`S PRIMARY FLT DISPLAY & NAVIGATION DISPLAY BEGAN TO FLICKER AS WELL AS LIGHTING & AUDIO VISUAL IN THE CABIN. DURING RAPID SEQ OF WARNING MESSAGES AN AC BUS 2 MESSAGE APPEARED, FOLLOWED BY AVIONIC VENT EXTRA CT FAN C/B TRIPPING. DECLARED AN EMERGENCY, DIVERTED TO ORD. MX FOUND NR 2 GENERATOR FEEDER CABLE CONNECTOR ARCED AT F IREWALL DISCONNECT. MX REMOVED & REPLACED NR 2 ENG IDG CABLE ASSY, OPS TEST PERFORMED AND SYS CHECKED GOOD. 2 L 7 2 4F RT A28NM 2002092000050 20020920 00050 NM 2002 9 20 AWXA200200885 1 20020914 A 2420 941D3352 CIRCUIT BREAKER BOEING 737 7373G7 1384595 NM COCKPIT DEFECTIVE A AWXA O OTHER H G ELECT. POWER LOSS-50 PC MULTIPLE FAILURE AP APPROACH 1 WP 28 309AW 24711 ON APPROACH LOST CAPT AIRSPEED INDICATION, ALTIMETER, ATTITUDE DIRECTION INDICATOR, HORIZONTAL SITUATION INDICATOR, NR 1 TRANSFORMER RECTIFIER, EQUIP COOLING C/B & NR 1 GEN FAILED. BURNING SMELL NOTICED FROM OVERWING EXIT TO AFT CABIN. MX INSPECTED WIRING ON NR 1 ENG FROM GEN TO PRESSURE FEED THROUGH, ALSO INSPECTED ALL WIRING IN THE ELECTRONIC EQUIPMENT B AY, WIRING CHECKED GOOD. FOUND NR 1 ENG GEN BAD, R&R NR 1 ENG GEN. MX DISCOVERED NR 1 ENG GEN C/B WAS DEFECTIVE NOT AL LOWING NR 1 ENG GEN TO GO OFF LINE. R&R NR 1 ENG GEN C/B (C801). OPS CHECK OF NR 1 ENG GEN SYS WAS GOOD, RAN AC PACKS ALL NIGHT, NO SMELL. 2 L 7 2 4F RT A16WE 2002092000051 20020920 00051 EU 2002 9 20 AWXA200200887 1 20020915 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 621AW 2240 053 PHX - EEL - EMERGENCY LIGHT SYSTEM TEST AT PRESS TO TEST PANEL FAILED STEP 5 OF T/C I8M05319. MAINTENANCE REMOVED AND R EPLACED THE LEFT AFT EMERGENCY POWER SUPPLY UNIT (13WL) IAW AMM 33-51-38-401, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002092000052 20020920 00052 NM 2002 9 20 AWXA200200889 1 20020915 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 PHX - EEL - DURING INSPECTION THE L2 AND R2 DOOR EMERGENCY EXIT SIDE LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT THE M1051 POWER SUPPLY, OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM WAS GOOD. 2 L 7 2 4F RT A16WE 2002092000053 20020920 00053 GL 2002 9 20 EGQ2002F00001 1 20020904 A 7810 13909002 EXHAUST PIPE CIRRUS SR SR22 2130001 GL CONT O550 IO550* SO NR 5 CYLINDER MISSING E EGQA O OTHER D INFLIGHT SEPARATION AP APPROACH 1 EA 17 344CD 107 0156 ON 9-1-2002, PILOT REPORTED A LOUD BANG WHILE ON FINAL APPROACH. POSTFLIGHTS SHOWED RIGHT LOWER ENGINE COWLING DEFORMED . MAINTENANCE REMOVED THE COWLING AND FOUND THE NR 5 EXHAUST STACK MISSING. NO OTHER DAMAGE TO THE EXHAUST SYSTEM WAS NOTED. THE SHORT EXHAUST STACK THAT BOLTS TO THE CYLINDER WAS SECURE AND INTACT WITH NO APPARENT DEFECTS. THE EXHAUST COLLECTOR WAS FOUND TO BE SECURE AND WITHOUT APPARENT DEFECT. THE RIGHT LOWER ENGINE COWLING WAS SEVERELY BURNED AND WO ULD HAVE PROBABLY BURNED THROUGH HAD THIS NOT HAPPENED ON FINAL. LANDING LIGHT ASSY WAS FOUND BROKEN AS WELL. 1 L 7 1 3O 3 O NT A00009CH E3SO 2002092000054 20020920 00054 NM 2002 9 20 AWXA200200890 1 20020914 A 2612 65528087M0DD ACCESSORY UNIT BOEING 737 7373Q8 1384670 NM E/E BAY OUT OF TOLERANCE A AWXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 28 327AW 15984 5304 23507 MZT - DIVERSION - FLT 0671 - EN ROUTE FROM PVR TO PHX AT CRUISE, WHEEL WELL FIRE WARNING LIGHT ILLUMINATED AND FIRE BELL SOUNDED. DIVERTED TO MZT AND LANDED WITHOUT FURTHER EVENT, FIRE WARNING LIGHT EXTINGUISHED AFTER 20 MINUTES WHEN LANDI NG GEAR WAS LOWERED. FLIGHT CREW PERFORMED VISUAL INSPECTION OF WHEEL WELLS AND FOUND NO EVIDENCE OF FIRE OR ANY OTHER DEFECT. MAINTENANCE WAS FLOWN DOWN TO MZT AND REPLACED THE OVERHEAT COMPARTMENT ACCESSORY UNIT M237 IAW BMM 26-17-00. VENDOR BENCH TEST OF COMPARTMENT OVERHEAT ACCESSORY UNIT WAS NO FAULT FOUND, UNIT FUNCTIONAL TESTED GOOD, TEST WAS CONDU CTED SEVERAL TIMES WITH NO DEFECTS, CLEANED CIRCUIT CARD AND WIRING, UNIT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002092000055 20020920 00055 CE 2002 9 20 FUK2002F00000 1 20020610 A 3010 M1060045144 THERMOSWITCH CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE WING WRONG PART E FUKA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NE 03 133WA 5500356 LOW TEMPERATURE SWITCH (PN M1060045144) WAS INSTALLED IN PLACE OF CORRECT HI TEMPERATURE SWITCH(PN M1165155144) AT THE T IME OF MANUFACTURE, CAUSING HEAT SYSTEM TO NOT FUNCTION AT ALL. HIGH AND LOW TEMPERATURE SWITCHES ARE IDENTICAL IN APPE ARANCE. MFG SHOULD COLOR CODE THEM TO PREVENT INSTALLING THEM IN THE WRONG LOCATION. 1 L 7 2 4F 4 F A22CE E1NE 2002092000056 20020920 00056 NM 2002 9 20 AWXA200200891 1 20020916 A 2820 COUPLING BOEING 737 737277 1384570 NM FUEL SYSTEM LOOSE A AWXA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 WP 28 189AW 22656 PHX - AIR TURNBACK - FLT 0451 - ON CLIMBOUT OF PHX EN ROUTE TO SLC THE ATC TOWER REPORTED FUEL VENTING FROM LT WING, FLI GHT ATTENDANT CONFIRMED FUEL VENT FROM LT WING, AIRCRAFT TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. AT GATE M AINTENANCE OBSERVED MINIMAL FUEL LEAK COMING FROM THE LT WING VENT. DURING TROUBLESHOOTING A FUEL FEED LINE WAS FOUND L EAKING AT COUPLING, TIGHTENED COUPLING. MAINTENANCE ALSO REPLACED FUEL VENT FLOAT VALVE; OPERATIONAL AND LEAK CHECKS WE RE GOOD. VENDOR TEARDOWN OF FUEL VENT FLOAT VALVE CONFIRMED FAILURE OF UNIT, PART WAS BEYOND REPAIR AND SCRAPPED. 2 L 7 2 4F RT A16WE 2002092000057 20020920 00057 EU 2002 9 20 GOC2002F00000 1 20020903 A 3222 STRUT BNORM BN2 BN2B26 1520350 EU LYC O540 O540* 41532 EA NLG DAMAGED E G0CA O OTHER O OTHER NR NOT REPORTED 1 NM 11 2119V 2093 1163 2105 BOLT HOLES IN TOP OF NOSE LANDING GEAR OUTER CYLINDER, (PN 46063), FAILED ALLOWING STEERING STOP TO DEPART THE AIRCRAFT IN FLIGHT. NOSE LANDING GEAR THEN SLIPPED DOWN IN MOUNTING BLOCKS RENDERING NOSE WHEEL STEERING INOPERATIVE. AIRCRAFT WAS ON FINAL LANDING FROM A CHARTER FLIGHT. 1 H 7 2 3O 3 O RT A17EU E295 2002092000058 20020920 00058 NM 2002 9 20 AWXA200200892 1 20020915 A 2751 1812996 INDICATOR BOEING 737 7373Y0 1384671 NM COCKPIT FAULTY A AWXA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 28 323AW 23684 PHX - FLIGHT CONTROL - FLT 0769 - DURING APPROACH INTO PHX EN ROUTE FROM PVR TRAILING EDGE FLAPS WOULD ONLY EXTEND TO 5 DEGREES WITH NO SPLIT ON GAUGE. WENT AROUND FOR ANOTHER APPROACH AND USED ALTERNATE FLAP PROCEDURES TO BRING FLAPS TO 15 DEGREES. LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED FLAP POSITION INDICATOR IAW BMM 27-58-41-4; O PERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002092000059 20020920 00059 SW 2002 9 20 IIF2002F00001 1 20020828 A 6220 407310102101 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR SEPARATED B IIFR K NONE O OTHER IN INSP/MAINT 1 SW 03 407JR 53245 ELASTOMERIC PORTION OF BEARING COMPLETELY DEBONDED FROM BASE. FOUND AT ROUTINE INSPECTION. BEARING IS ONE OF A BATCH OF DEFECTIVE BEARINGS MANUFACTURED BEFORE 1998. RECOMMEND THAT BEARINGS BE BONDED WITH BETTER MATERIALS OR ADHESIVE. 1 G 7 1 3U 3 U O H2SW E1GL 2002092000060 20020920 00060 NM 2002 9 20 AWXA200200893 1 20020914 A 2920 UL16539 HYDRAULIC LINE BOEING 757 7572S7 1384962 NM HYD SYSTEM LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 901AW 23321 BWI - EMERGENCY LANDING - FLT 0778 - EN ROUTE FROM LAS TO BWI AT CRUISE THE LT HYDRAULIC QUANTITY DECREASED TO ZERO AND THE SYSTEM PRESSURE LIGHT ILLUMINATED WITH AN EICAS MESSAGE FOR LT HYDRAULIC SYSTEM PRESSURE DISPLAYED. DECLARED EMERGE NCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED A HYDRAULIC LINE THAT RUNS FROM THE NR 1 ENGI NE HYDRAULIC PRESSURE MANIFOLD TO THE HYDRAULIC PRESSURE SWITCH. REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP, FLUSHED SYS TEM, AND REPLACED THE PRESSURE, RETURN, AND CASE DRAIN FILTERS IAW R5M29601; LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A2NM 2002092000061 20020920 00061 NM 2002 9 20 AWXA200200894 1 20020917 A 3397 AW252100111 WIRE HARNESS BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 309AW 24711 PHX - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 23 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002092000062 20020920 00062 EU 2002 9 20 VJ32002F00063 1 20020909 A 7160 120A6123 KNOB GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA ALT AIR CABLE DAMAGED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 865AF 6 85005 ALT. AIR KNOB BECOMES LOOSE AND INOPERATIVE WITH USE. KNOB IS PLASTIC WITH A HELI-COIL INSERT, SCREWED ONTO THREADED EN D OF CABLE. KNOB MUST BE ROTATED TO OPERATE ALTERNATE AIR AND THIS CAUSES KNOB TO WEAR AND LOOSEN ON CABLE END. A MORE SECURE METHOD OF ATTACHING KNOB TO CABLE SHOULD BE TRIED. PERHAPS A SET SCREW OR ROLL PIN. 1 L 7 1 3O 3 O RT A49CE 1E4 2002092000063 20020920 00063 NM 2002 9 20 AWXA200200895 1 20020917 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD VERTICAL EMERGENCY FLASHLIGHT WAS NOT SHOWING CHARGE. MAIN TENANCE REMOVED AND REPLACED THE FORWARD VERTICAL EMERGENCY FLASHLIGHT, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002092000064 20020920 00064 NM 2002 9 20 AWXA200200896 1 20020831 A 5240 65458493 SKIN BOEING 737 737277 1384570 NM R2 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A .25 INCH CRACK WAS FOUND ON THE R2 DOOR EXTERNAL SKIN AT THE LOWER HINGE CUTOUT UPPER AFT CORNER, BS 962. MAINTENANCE TRIMMED OUT DAMAGE AT LOWER HINGE CUTOUT UPPER AFT CORNER AND PERFORMED A HFEC I NSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW AWA ER 15-5 200-02259-TB3. 2 L 7 2 4F RT A16WE 2002092000065 20020920 00065 NM 2002 9 20 AWXA200200898 1 20020918 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN MISSING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 LAS - EEL - DURING INSPECTION IT WAS DISCOVERED THAT THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY WAS MISSING AT SEAT ROW 7 LT. MAINTENANCE INSTALLED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 7 LT; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002092000066 20020920 00066 EU 2002 9 20 AWXA200200899 1 20020918 A 2560 P20700012015 FLASHLIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 55 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THAT THE EMERGENCY FLASHLIGHT AT THE AFT FLIGHT ATTENDANT SEAT WAS INOP ERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT AT THE AFT FLIGHT ATTENDANT SEAT. 2 L 7 2 4F RT A28NM 2002092000067 20020920 00067 EU 2002 9 20 VJ32002F00064 1 20020906 A 8011 14924PM STUD GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA STARTER LOOSE B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 862AF 394 85002 DURING PROGRESSIVE INSPECTION OF ENGINE FOUND TERMINAL STUD ON STARTER SOLENOID LOOSE. 1 L 7 1 3O 3 O RT A49CE 1E4 2002092000068 20020920 00068 EU 2002 9 20 VJ32002F00065 1 20020906 A 3260 602EN16 DOWNLOCK SWITCH GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA NOSE GEAR FAILED B VJ3R O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 07 864AF 399 85004 DOWN SWITCH FAILED CAUSING NO DOWN INDICATION OF NOSE GEAR IN THE DOWN POSITION. 1 L 7 1 3O 3 O RT A49CE 1E4 2002092000069 20020920 00069 EU 2002 9 20 VJ32002F00066 1 20020906 A 3260 GH115TA HANDLE GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA MLG FAILED B VJ3R O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 07 864AF 409 85004 GEAR HANDLE EXPERIENCED INTERNAL FAILURE CAUSING MALFUNCTION OF THE HYDRAULIC GEAR PUMP. WHEN THE PUSH TO TEST BUTTON W AS PRESSED FOR THE ANNUNCIATOR PANEL, THE PUMP WOULD OPERATE. 1 L 7 1 3O 3 O RT A49CE 1E4 2002092000070 20020920 00070 EU 2002 9 20 VJ32002F00067 1 20020906 A 7921 120A6634 STRAP GROB 120 G120A 1660208 EU OIL COOLER BROKEN B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 864AF 431 85004 TERMINAL END OF OIL COOLER STRAP FOUND BROKEN DURING ROUTINE INSPECTION. APPEARS TO BE CAUSED BY FLEXING AND FATIGUE. RECOMMEND OTHER METHOD OF MOUNTING OIL COOLER. PERHAPS A RIGID MOUNT WOULD BE BETTER. 1 L 7 1 3O RT A49CE 2002092000071 20020920 00071 EA 2002 9 20 VJ32002F00068 2 20020906 A 7414 SENSOR SLICK GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA MAGNETO BROKEN B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 864AF 431 85004 RPM INDICATION SENSOR RING FOUND BROKEN DURING ROUTINE INSPECTION. THIS SENSOR RING FITS UNDER THE VENT OF THE RIGHT MA GNETO AND PROVIDES ENGINE RPM INDICATIONS. APPEARS TO BE BROKEN DUE TO FLEXING/FATIGUE. PERHAPS A DIFFERENT SENSOR OR OTHER MORE SECURE MOUNTING OF SENSOR WOULD PREVENT SUCH FAILURES. 1 L 7 1 3O 3 O RT A49CE 1E4 2002092000073 20020920 00073 2002 9 20 AALA20021003 4 20020714 A 2565 BOTTLE BOEING 757 757223 1384957 NM ESCAPE SLIDE DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 665AA 25299 ORD - R1 DOOR SLIDE BOTTLE INDICATES ZERO PSI. REPLACED SLIDE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002092000074 20020920 00074 NM 2002 9 20 AALA20021101 1 20020811 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 338AA 22335 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 27H INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT ASSEMBLY AT SEAT 27H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002092000075 20020920 00075 NM 2002 9 20 AALA20021140 1 20020810 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 378AN 25447 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE FLOOR PATH LIGHTING AT ROWS 29 INOPERATIVE. RE-SECURED CONNECTOR A T SIDE WALL FOR EMERGENCY ESCAPE FLOOR PATH LIGHTING AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002092000076 20020920 00076 WP 2002 9 20 AALA20021150 1 20020813 A 3350 SWITCH DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 249AA 49269 DFW - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHTS WOULD NOT EXTINGUISH, LIGHTS EXTINGUISH IN ARMED POSI TION. SYNCHED OVERWING EMERGENCY EXIT LIGHTS SWITCH. GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002092000077 20020920 00077 WP 2002 9 20 AALA20021152 1 20020812 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7518A 49895 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT STAIRS SECTION INOPERATIVE. RECONNECTED GROUND WIRE FO R EMERGENCY EXIT LIGHTS IN AFT STAIRS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2002092000078 20020920 00078 NM 2002 9 20 AALA20021153 1 20020806 A 3397 CONNECTOR BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 384AA 26996 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT AT SEAT 34B INOPERATIVE. INSTALLED NEW CONNECTOR ON EME RGENCY ESCAPE PATH LIGHTING HARNESS. SYSETM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002092000079 20020920 00079 NM 2002 9 20 AALA20021158 1 20020806 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AA 22327 SJU - DURING OVERNIGHT MAINTENANCE, FOUND FIRST CLASS GALLEY EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. REPLACED FIRST CL ASS GALLEY EMERGENCY ESCAPE PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002092000080 20020920 00080 NM 2002 9 20 AALA20021169 1 20020816 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 381AN 25450 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHTS AT SEAT 22H INOPERATIVE. CLEANED EMERGENCY ESCAPE LIGHT CON NECTORS AT SEAT 22H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002092000081 20020920 00081 WP 2002 9 20 AALA20021173 1 20020816 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 593AA 53256 DFW - DURING FORWARD EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002092000082 20020920 00082 CE 2002 9 20 TIM2002F00012 1 20020718 A 2820 503890348 NIPPLE BEECH 99 B99 1154004 CE PWA PT6 PT6A27 52043 EA FUEL CELL CRACKED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 99TH U155 RIGHT INBOARD BOX SECTION FUEL CELL, VENT SUPPLY NIPPLE CRACKED. 1 L 7 2 3T 4 T A14CE E4EA 2002092000083 20020920 00083 CE 2002 9 20 TIM2002F00013 1 20020809 A 2810 FLANGE BEECH 99 99A 1154003 CE PWA PT6 PT6* 52043 EA FUEL CELL CRACKED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 99CA U127 LEFT CENTER SECTION FUEL CELL CRACKED AT SUPPLY LINE FLANGE. 1 L 7 2 3T 3 T A14CE E2NE 2002092000084 20020920 00084 NM 2002 9 20 AZ5Y745M 1 20020810 A 5720 532BL PANEL BOEING 757 757200 1384950 NM WING LOOSE B K NONE K FLUID LOSS IN INSP/MAINT 1 SW 99 73724 42822 186 DURING REMOVAL OF A DRY BAY PANEL FOR TROUBLESHOOTING OF A FUEL LEAK, ONE OF THE ATTACHMENT BOLTS FELL OUT. IT LOOKED A S IF IT HAD BEEN SAWN OFF. THE DRY BAY PANEL IS NUMBER 4 AS PER 28-11-00 PG 653 (PANEL 532BL AS PER 28-11-07 PG 603). ALSO A TOTAL OF 4 ATTACH BOLTS WERE JUST HAND TIGHTENED. 2 L 7 2 4F RT A2NM 2002092000085 20020920 00085 SO 2002 9 20 C2XA02TY139 1 20020910 A 5315 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED 2-C CHECK, CORROSION WAS FOUND ON LT LAV AREA FLOORBEAM. MAINTENANCE REMOVED AND REPLACED LT LA V AREA FLOORBEAM, ALODINED, PRIMED AND PAINTED IAW EMB 135/145 SRM 53-30-01; 51-40-02; 51-21-03; 51-40-01 AND EMB 135/14 5 CPM 51-21-04, 05, 06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002092000086 20020920 00086 SO 2002 9 20 C2XA02TY140 1 20020910 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED 2-C INSPECTION, THE AFT SERVICE DOOR SILL WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF T DOOR SILL IAW EMB 135/145 SRM 53-21-10; 51-20-03; 51-40-06 AND 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEAS ED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002092000087 20020920 00087 SO 2002 9 20 C2XA02TY141 1 20020910 A 5320 14521725001 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 TYS DURING A SCHEDULED 2-C INSPECTION THE AFT PAX DOOR SILL WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT SI LL AT AFT PAX DOOR IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002111800017 20021118 00017 2002 11 18 AWXA200200879 4 20020911 A 3160 4077883960 DISPLAY AIRBUS 320 A320232 3930326 EU COCKPIT SHORTED A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 651AW 866 FLL - BURNING SMELL - FLT 0888 - EN ROUTE FROM LAS TO FLL THE NR 1 MULTI PURPOSE CONTROL DISPLAY UNIT (MCDU) WENT BLANK, AT THE SAME TIME NOTICED AN ELECTRICAL BURNING SMELL THAT LASTED APPROXIMATELY TWO MINUTES. CONTRACT MAINTENANCE AT FL L INSPECTED THE NR 1 MCDU AND FOUND THE UNIT SHORTED OUT, AIRCRAFT WIRING WAS FOUND TO BE GOOD. PLACED SYSTEM ON MEL 22 -82-01, COND 1, LT MCDU INOPERATIVE. VENDOR TEARDOWN REPORT OF MDCU CONFIRMED FAILURE UNIT FOR HARDWARE FAULT. LVPS WA S FOUND DEFECTIVE WITH AN OPEN TRACE ON A11 E79 TO A11 A1-116. LVPS REPLACED, UNIT FUNCTIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2002092000090 20020920 00090 SO 2002 9 20 C2XA02BT052 1 20020909 A 3230 355022002MOD2 CONTROL UNIT EMB 145 EMB145ER 3260211 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 12934 145019 EWR---CO3537, CREW REPORTED, AIR GROUND SENSOR FAILED AFTER TAKEOFF. AIR RETURN TO EWR. MAINTENANCE TROUBLESHOT PROBLE M, REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT IAW EMB145 AMM 32-32-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4F RT T00011AT 2002092000092 20020920 00092 SO 2002 9 20 C2XA02CL180 1 20020903 A 3350 CONNECTOR EMB 135 EMB135ER 3260203 SO CABIN LOOSE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 17507 145215 CLE FLIGHT 2904 THE CREW REPORTED THE EMERGENCY LIGHT ON THE CEILING FOR THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENAN CE INSPECTED AND RESECURED THE CANNON PLUG ON THE FORWARD CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002092000093 20020920 00093 SO 2002 9 20 C2XA02IA189 1 20020910 A 2752 3632501003 MOTOR EMB 145 EMB145LR 3260212 SO T/E FLAP FAILED A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 26549 145571 IAH- THE CREW NOTED THAT THE FLAPS FAIL IN FLIGHT. NO POSITION INDICATION OF FLAPS ON EICAS. THE CREW RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP DRIVE MOTOR UNIT, PERFORMED A OPERATIONAL CHECK , NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002092000094 20020920 00094 SO 2002 9 20 C2XA02IA193 1 20020913 A 2750 3631001007MOD3 CONTROL UNIT EMB 145 EMB145LR 3260212 SO T/E FLAP FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 26549 145571 IAH- DURING FLIGHT 3642, AT CRUISE ALTITUDE THE CREW NOTED A FLAP FAIL MESSAGE AND RETURNED TO IAH AND LANDED WITHOUT I NCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT, PERFORMED A OPERATIONAL CHECK OF THE FLAP S YSTEM AND NO DEFECTS NOTED. PERFORMED A TEST FLIGHT, WHICH WAS SATISFACTORY. THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 L 7 2 4T RT T00011AT 2002102800215 20021028 00215 SO 2002 10 28 C2XA02IA197 1 20020913 A 3234 8271013 CONTROL HANDLE EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13550 145575 COS - PILOT REPORTED THAT UPON SELECTING GEAR UP THE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED TO COS AND LAN DED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL L EVER. THE LANDING GEAR SYSTEM OPERATIONALLY TESTED SATISFACTORILY AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002102800216 20021028 00216 SO 2002 10 28 C2XA02IA198 1 20020915 A 5610 SEALANT EMB 145 EMB145LR 3260212 SO WINDOW LOOSE A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 11548 145565 IAH- ON CLIMB THE CREW NOTED THAT THE FO'S DV WINDOW SEALANT WAS FLAPPING ON THE FUSELAGE, THE AIRCRAFT RETURNED TO IAH, LANDED WITHOUT INCIDENT. MAINTENANCE IN CLE PERFORMED A REPAIR TO THE FIRST OFFICER'S DIRECT VISION WINDOW SEALANT. T HE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002092000095 20020920 00095 SO 2002 9 20 C2XA02IA199 1 20020914 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE LIGHTNING STRIKE A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 14543 145553 IAH- ON CLIMB THE CREW REPORTED A LIGHTNING STRIKE. RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORME D A LIGHTNING STRIKE INSPECTION, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002092000096 20020920 00096 SO 2002 9 20 C2XA02SH046 1 20020830 A 5320 14525422001 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV- DURING C-CHECK INSPECTION, THE LEFT SILL HAD CORROSION AROUND THE NUT PLATE HOLES BETWEEN FRAMES 60 AND 61. MAINTE NANCE REMOVED AND REPLACED THE LEFT SILL BETWEEN FRAMES 60 AND 61 IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002092000097 20020920 00097 SO 2002 9 20 C2XA02SH047 1 20020831 A 5320 14521725015 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV- DURING C-CHECK INSPECTION, THE RIGHT SILL AFT OF THE SERVICE DOOR HAD CORRODED NUT PLATE HOLES. MAINTENANCE REMOVE D AND REPLACED THE RIGHT HAND SILL AFT OF THE SERVICE DOOR IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002092000099 20020920 00099 SO 2002 9 20 C2XA02SH049 1 20020831 A 5315 14521721009 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV- DURING C-CHECK INSPECTION, CENTER FLOORBEAM STRAP FOUND TO HAVE NUT PLATES CORRODED AND SURFACE CORROSION FROM FRAM E 15 TO 17. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS IAW EMB 145 SRM 53-21-10 PG 210 ITEM 4 FIG 203, I NSTALLED REPAIR PARTS IAW EMB 145 SRM 53-21-10 AND SRM 51-40-02. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002092000105 20020920 00105 SO 2002 9 20 C2XA02SH055 1 20020902 A 5315 14521713005 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV - DURING C-CHECK, CENTER OMEGA BEAM AT AFT GALLEY MOUNTS NUT PLATE HOLES HAVE CORROSION. MAINTENANCE REMOVED AND RE PLACED AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002092000108 20020920 00108 SO 2002 9 20 C2XA02TY142 1 20020918 A 5510 14521939001 FITTING EMB 145 EMB145 3260210 SO HORIZ STAB GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 7872 145161 TYS DURING A SCHEDULED 2-C INSPECTION MAINTENANCE FOUND A GOUGED IN THE HORIZONTAL STAB LT HINGE PIN, A GST 2827/02 WAS ISSUED, WHICH STATED ALODINE, PRIME AND PAINT IAW WITH THE GST-2827-02, EMB 145 SRM 51-71-03, CPM 51-21-04-05 AND 51-21 -06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002092000109 20020920 00109 SO 2002 9 20 C2XA02TY143 1 20020918 A 5510 14521939004 FITTING EMB 145 EMB145 3260210 SO HORIZ STAB GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 7872 145161 TYS DURING A SCHEDULED 2-C INSPECTION, MAINTENANCE FOUND A GOUGE IN THE RT HORIZONTAL STAB HINGE PIN SAFETY PIN WHICH R EQUIRED A GST, ALL WORK WAS ACCOMPLISHED IAW GST WHICH STATED BLEND, ALODINE, PRIME AND PAINT SRM 51-70-03, CPM 51-21-04 , 05, 06. A/C WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002092000110 20020920 00110 WP 2002 9 20 MWEA020542 1 20020912 A 5320 99579133 INTERCOSTAL DOUG DC9 DC915 3022036 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 INTERCOSTAL AT LONGERON 29 BETWEEN FRAME STATION 313 AND 370 HAS A LARGE HOLE ON UPPER AFT END. REMOVED AND INSTALLED I NTERCOSTAL. 2 L 7 2 4F A6WE 2002092000111 20020920 00111 WP 2002 9 20 MWEA020545 1 20020912 A 5330 953023915 SKIN DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 NOSE SKIN HAS 4 POSSIBLE CRACKS AT STATION 76.6, 18 INCHES LEFT OF CENTER AREA NEEDS TO BE STRIPPED AND VERIFIED. VERIF IED CRACKS LOCATED AND DRILLED PILOT HOLES AND FABRICATED DOUBLER. 2 L 7 2 4F A6WE 2002092000112 20020920 00112 WP 2002 9 20 MWEA020546 1 20020912 A 5320 99579085 INTERCOSTAL DOUG DC9 DC915 3022036 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 INTERCOSTAL AT FRAME STATION 320 BETWEEN LONGERON 28 AND LONGERON 29 DAMAGED. FIT AND DRILLED INTERCOSTAL, REMOVED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2002092000113 20020920 00113 WP 2002 9 20 MWEA020547 1 20020912 A 5310 991224363 SHEAR TIE DOUG DC9 DC915 3022036 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 AT FRAME STATION 786 FRAME TO SKIN SHEAR TIE HAS NUMEROUS ELONGATED HOLES FROM LONGERON 30 TO 27 LEFT. LOCATED AND DRIL LED SHEAR TIE, REMOVED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2002092000114 20020920 00114 WP 2002 9 20 MWEA020548 1 20020912 A 5320 99579085 INTERCOSTAL DOUG DC9 DC915 3022036 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 INTERCOSTAL AT FRAME STATION 360 BETWEEN LONGERON 29 DAMAGED. FIT AND DRILLED INTERCOSTAL REMOVED AND INSTALLED INTERCO STAL. 2 L 7 2 4F A6WE 2002092000115 20020920 00115 WP 2002 9 20 MWEA020549 1 20020912 A 5320 99579083 INTERCOSTAL DOUG DC9 DC915 3022036 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 INTERCOSTAL AT FRAME STATION BETWEEN LONGERON 28 AND 29 DAMAGED. FIT AND DRILLED INTERCOSTAL REMOVED AND INSTALLED INTE RCOSTAL. 2 L 7 2 4F A6WE 2002092000116 20020920 00116 WP 2002 9 20 MWEA020550 1 20020913 A 5720 991175121 CLIP DOUG DC9 DC915 3022036 WP CENTER TANK CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 CENTER TANK FORWARD SPAR ACCESS WEB 8 EACH INSULATION ATTACH CLIPS REQUIRE REMOVAL TO FACILITATE OTHER MAINTENANCE. REM OVED AND INSPECTED CLIPS, FABRICATED AND INSTALLED CLIPS. 2 L 7 2 4F A6WE 2002092000117 20020920 00117 NM 2002 9 20 QXEA0201196 1 20020806 A 5410 SUMP DHAV DHC8 DHC8202 2809007 NM RIGHT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX- SUMP CRACKED AT RIGHT HAND FORWARD CORNER. REPAIRED IAW DHC8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002092000118 20020920 00118 NM 2002 9 20 QXEA0201300 1 20020823 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - CORROSION AROUND NUT PLATES UNDER MAIN CABIN DOOR SILL. REPAIRED IAW DHC-8 SRM 52-20-11 AND DHC-8 CPM, CHAPTER 5, PAGE 5-1 TO 5-5. 2 H 7 2 4T RT A13NM 2002110700018 20021107 00018 2002 11 7 PCAA0209108 4 20020919 A 3442 066308631 INDICATOR DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A PCAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 13 849EX 20670 4009 337 ALB-ISP FLIGHT 3512, CREW REPORTED THAT DURING DESCENT FLIGHT DATA RECORDER CAUTION LIGHT ILLUMINATED AND SMOKE CAME OUT OF RIGHT CORNER OF THE CENTER CONSOLE. EMERGENCY WAS DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTE D AND FOUND WEATHER RADAR INDICATOR AT FAULT. AIRCRAFT GROUND RAN WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. WEATHER RADAR INDICATOR REPLACED LATER THAT DAY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092000119 20020920 00119 NM 2002 9 20 QXEA0201301 1 20020825 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - RIGHT HAND INBOARD SEAT TRACK X470 HAS CORROSION ON INBOARD FLANGE. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002092000120 20020920 00120 NM 2002 9 20 QXEA0201302 1 20020822 A 5220 SKIN DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - COCKPIT ESCAPE HATCH SKIN HAS THREE NICKS/LIGHT SCRATCHES FORWARD PART OF HATCH. REPAIRED IAW RD 8-52-327. 2 H 7 2 4T RT A13NM 2002092000121 20020920 00121 NM 2002 9 20 QXEA0201303 1 20020825 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND INBOARD SEAT TRACK X486 HAS CORROSION PIT IN THE CHANNEL. REPAIRED IAW DHC-8-200 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002092000122 20020920 00122 NM 2002 9 20 QXEA0201304 1 20020826 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND INBOARD SEAT TRACK X543 HAS A GOUGE IN THE CHANNEL. REPAIRED IAW RD 8-53-4936. 2 H 7 2 4T RT A13NM 2002092000123 20020920 00123 NM 2002 9 20 QXEA0201305 1 20020824 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - RIGHT HAND INBOARD SEAT TRACK X209 TO X229 HAS NUMEROUS CORROSION PITS. REPAIRED IAW DHC-8-200 SRM 51-40-11 AND S RM 51-30-26. 2 H 7 2 4T RT A13NM 2002092000124 20020920 00124 NM 2002 9 20 QXEA0201306 1 20020828 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM LT WING DETERIORATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND WING TOP WING BOX SKIN AFT SURFACE COMPOSITE IS SOFT AND HAS PAINT MISSING AT STATION YW410.000. REPAIR ED IAW HORIZON AIR EA 2-57-187. 2 H 7 2 4T RT A13NM 2002092000125 20020920 00125 NM 2002 9 20 QXEA0201307 1 20020828 A 5540 BEARING DHAV DHC8 DHC8202 2809007 NM RUDDER LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - RUDDER DAMPER BEARING AT RUDDER ATTACH POINT IS LOOSE AND HAS MOVEMENT ABOUT THE HARDWARE. REPAIRED IAW RD 8-55-5 88. 2 H 7 2 4T RT A13NM 2002092000126 20020920 00126 NM 2002 9 20 QXEA0201308 1 20020828 A 2910 O-RING BOMBDR DHC8 DHC8401 1390041 NM HYD SYSTEM LEAKING A QXEA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 NM 09 400QX 4030 PDX - UPON LOWERING THE GEAR FOR LANDING, THE CREW RECEIVED AN AMBER GEAR DOOR LIGHT AND HYDRAULIC FLUID LOSS AND PRESSU RE FLUCTUATION. THE CREW COMPLIED WITH EMERGENCY PROCEDURES, SHUT DOWN AND WAS TOWED TO THE GATE. MAINTENANCE INSPECTE D THE AIRCRAFT AND FOUND A CAP ON THE HYDRAULIC MANIFOLD LEAKING. THE O-RING ON THE CAP WAS REPLACED, THE SYSTEM WAS SE RVICED, AND A OPERATIONAL CHECK WAS PERFORMED. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092000127 20020920 00127 NM 2002 9 20 QXEA0201310 1 20020830 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8401 1390041 NM LANDING GEAR FAULTY A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 408QX 4050 SEA- CREW RETURNED TO FIELD, WHEN AFTER TAKEOFF GEAR DID NOT RETRACT. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND RE PLACED NR 2 WOW HARNESS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092000128 20020920 00128 EU 2002 9 20 QXEA0201311 1 20020823 A 2612 M400D4A RELAY FOKKER F28 F28MK4000 4990810 EU FIRE WARNING FAILED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 499US 11182 PDX- ENGINE FIRE BELL DOES NOT SOUND, ALL LIGHTS ILLUMINATED. REMOVED AND REPLACED FIRE WARNING BELL RESET RELAY. OPER ATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002092000129 20020920 00129 EA 2002 9 20 QXEA0201312 1 20020828 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 611QX 10041 PDX- FORWARD CARGO BAY FIRE SUPPRESSION PROTECTION SCREEN IS DAMAGED. REMOVED AND REPLACED FIRE PROTECTION SCREEN ASSE MBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002092000130 20020920 00130 NM 2002 9 20 F3LA200200263 1 20020910 A 5330 PANEL BOEING 737 737301 1384611 NM BS 500A - 500D CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION AND PUNCTURE IN TRANSITION PANEL AT BS 500A TO 500D. FABRICATED AND INS TALLED REPLACEMENT PANEL PER SRM 51-40-02 AND SOPM 20-41-01. 2 L 7 2 4F RT A16WE 2002092000131 20020920 00131 NM 2002 9 20 QXEA0201314 1 20020830 A 3260 SENSOR BOMBDR DHC8 DHC8401 1390041 NM MLG OUT OF ADJUST A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 406QX 4048 SEA- RED GEAR UNSAFE LIGHT CAME ON MOMENTARILY FOLLOWED IMMEDIATELY THEREAFTER BY BOTH AMBER MAIN GEAR DOOR LIGHTS DURIN G CRUISE FLIGHT. ADJUSTED THE LEFT HAND UPLOCK PSU SENSOR AND LEFT AND RIGHT HAND AFT DOOR SENSOR. INSPECTED GAP OF TH E LEFT HAND UPLOCK PSU SENSOR AND FOUND TO BE WITHIN LIMITS. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2002092000132 20020920 00132 EA 2002 9 20 QXEA0201315 1 20020901 A 2612 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A QXEA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 09 604QX 10019 LAX- FIRE SYSTEM FAULT STATUS MESSAGE. PLACED ON MEL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002092000137 20020920 00137 EA 2002 9 20 COMA0260538 1 20020918 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 949CA 7080 FLIGHT 5284 1 SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP.DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2002092000138 20020920 00138 2002 9 20 MWEA020578 4 20020920 A 2565 B19867105 SLIDE DOUG DC9 DC914 3022034 WP TAILCONE DEFECTIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 TAILCONE EMERGENCY SLIDE WILL NOT DEPLOY WHEN TAILCONE IS DROPPED USING TAILCONE SLIDE. -- REMOVED TAILCONE PANEL, ADJ USTED FORWARD HOLD DOWN STRAP ON SLIDE COVER AND REINSTALLED TAILCONE. 2 L 7 2 4F A6WE 2002092000139 20020920 00139 NE 2002 9 20 COMA0260539 2 20020918 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT BLOWN A COMA E A ENGINE SHUTDOWN UNSCHED LANDING M Y OVER TEMP ENGINE STOPPAGE CL CLIMB 1 SO 01 967CA 19374 7134 807123 FLIGHT 5895 - LOUD BOOM AND YAW LEFT - LEFT ENGINE ITT 980+. IFSD.REPLACED THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002092000140 20020920 00140 EA 2002 9 20 COMA0260540 1 20020918 A 3620 355413255 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA R/H FALSE ACTIVATION A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 918CA 7018 FLIGHT 5064 R/H ANTI ICE DUCT WARNINGREPLACED FUSELAGE SECTION OF BLEED LEAK SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2002092000142 20020920 00142 NM 2002 9 20 UPS02239516 1 20020920 A 2560 SLIDE BOEING 727 72722C 138400F NM ENTRY DOOR LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:N/A FE KNOCKED THE SLIDE OFF THE DOOR WHILE CLOSING REINSTALLED SLIDE 2 L 7 3 4F A3WE 2002092000143 20020920 00143 NM 2002 9 20 AWXA200200903 1 20020906 A 5320 654957411 ANGLE BOEING 737 737301 1384611 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 0 0 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON SPAR CHORD, FORWARD SIDE OF BS 1016, BETWEEN S TR 26 L/H AND 27 L/H. MAINTENANCE REMOVED CORROSION ON FRAME SPLICE ANGLE AND FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED DAMAGED FRAME SPLICE ANGLE AND 2 EACH STRINGER CLIPS; FABRICATED A NEW FRAME SPLICE ANGLE; INSTALLED REPAIR PARTS IAW B 737-300 SRM 51-20-01, PG. 10 & 47, SRM 51-40-02, PG. 3-4. 2 L 7 2 4F RT A16WE 2002092000144 20020920 00144 WP 2002 9 20 0202869151 1 20020904 A 2131 CONTROLLER DOUG DC9 DC914 3022034 WP CABIN PRESSURE MALFUNCTIONED A NWAA B EMER. DESCENT O OTHER CR CRUISE 1 GL 01 8909E 45770 LOST PRESSURIZATION AT FL290, CABIN ALTITUDE WENT TO 12,000 FEET. CREW INITIATED A RAPID DESCENT TO 10,000 FEET. MASKS DID NOT DEPLOY. AUTO PRESSURE CONTROLLER RESTORED CABIN PRESSURE CONTROL BUT CONTINUED TO OPERATE ERRATICALLY IN AUTO. AIRCRAFT LANDED SAFELY AT DTW. MAINTENANCE FOUND THE AFT PLUG DOOR NOT SECURED PROPERLY AND SOME SOUND PROOFING INSUL ATION LODGED BETWEEN DOOR AND SEAL. REINSTALLED THE DOOR AND REPLACED THE AUTO PRESSURE CONTROLLER. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002092400070 20020924 00070 NM 2002 9 24 F3LA200200264 1 20020910 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT BS 500B - 500C AT STR 26. FABRICATED AND REPLACED INTERCOS TAL PER SRM 51-10-02, 51-40-02, AND SOPM 20-41-01. 2 L 7 2 4F RT A16WE 2002092000145 20020920 00145 WP 2002 9 20 MWEA020577 1 20020920 A 5310 591214130 ATTACH ANGLE DOUG DC9 DC914 3022034 WP STATION 951 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 RIGHT SIDE OF VERTICAL TO FUSELAGE ATTACH ANGLE HAS A CRACK AT STATION 951. -- STOP DRILLED CRACK, DRILLED HOLES IN RE PAIR ANGLE, INSTALLED REPAIR ANGLE, REMOVED HIGH AND LOW FASTENERS AND INSTALLED OVERSIZED FASTENERS. REINSTALLED HEAD KNOCKER COVER PANEL. 2 L 7 2 4F A6WE 2002092000146 20020920 00146 SO 2002 9 20 C2XA02TY146 1 20020920 A 5210 14521775013 SILL EMB 145 EMB145 3260210 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS DURING A SCHEDULED 2-C INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND CORRODED. MAINTENANCE R/R THE SERVICE FOR WARD SEAL IAW EMB 145 SRM 52-10-02 AND EMB 145 CPM 51-21-05. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002092100001 20020921 00001 SO 2002 9 21 C2XA02SH062 1 20020829 A 5210 14533395001 SKIN EMB 145 EMB145ER 3260211 SO PAX DOOR DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C CHECK INSPECTION, THE MAIN DOOR STRUCTURE WAS FOUND TO HAVE A DENT AFT OF ACTUATING LEVER. MAINTENANCE REMOVE D AND REPAIRED DAMAGED AREA IAW EMB 145 SRM 52-10-01. PERFORMED LEAK TEST. LEAK TEST GOOD. IAW EMB 145 MM 21-31-00-700-8 08-A. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002092300001 20020923 00001 WP 2002 9 23 AAL2002F00001 1 20020722 A 5311 FRAME DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AA 49269 FRAME 1322 IS CORRODED AT LONGERON 29R AND 30. REMOVED PORTION OF CORRODED FRAME AND REPLACED FRAME ALONG WITH SPLICES PER SRM. (2002-1148)(AMC 4) 2 L 7 2 4F 4 F A6WE E2EA 2002092300002 20020923 00002 WP 2002 9 23 AAL2002F00002 1 20020722 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AA 49269 WEB, AFT CARGO DOOR CUTOUT, LOWER FRAME, TOP. CORROSION ON TOP WEB OF AFT CARGO DOOR CUT OUT LOWER FRAME. REMOVED CORR ODED TOP WEB. INSTALLED NEW WEB PER SRM. (2002-1149 /AMC 4) 2 L 7 2 4F 4 F A6WE E2EA 2002092300003 20020923 00003 WP 2002 9 23 AAL2002F00003 1 20020801 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AA 49473 FLOOR MEMBRANE, 2 INCH X 4 INCH ON FLOOR MEMBRANE BELOW BRACKET AT RBL 11 STA 160 IS CORRODED AND CRACKED AT FASTENERS H OLES. INSTALLED DOUBLER PER AARD. (2002-1114/ AMC4) 2 L 7 2 4F 4 F A6WE E2EA 2002092300004 20020923 00004 WP 2002 9 23 AAL2002F00004 1 20020801 A 5320 WEB DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AA 49473 RIGHT CUSP CRACKED AT LIGHTING HOLE 2 PLACES APPROXIMATELY .5000 INCH AND 2.0 INCH STA 1265. CRACK LENGTH .500 INCH AND 2.00 INCH. INSTALLED DOUBLER PER AARD. (2002-1115) 2 L 7 2 4F 4 F A6WE E2EA 2002092300005 20020923 00005 WP 2002 9 23 AAL2002F00005 1 20020710 A 5347 5930556631 SEAT TRACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 552AA 53034 SEAT TRACK, CORROSION IN NR 2 SEAT TRACK AT STATION 1200. CUT OUT CORROSION, INSTALLED SEAT TRACK PLUG PER SRM. (2002- 1090/ AMC 4) 2 L 7 2 4F 4 F A6WE E2EA 2002092300007 20020923 00007 EU 2002 9 23 AALA20021208 1 20020821 A 5315 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1436A 11426 FLOORBEAM CAP CORRODED. BL1127L, STA 3845-4850. REMOVED AND REPLACED TEE-CAP, STA 4175-4575. 2 L 7 2 4F 4 F RT E25NE 2002092300008 20020923 00008 EA 2002 9 23 ASOA020480 1 20020901 A 3397 M2275935229 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE COCKPIT LOOSE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 909EV 475 7658 DURING GROUND INSPECTION, WHEN THE EMERGENCY LIGHT SWITCH IS IN THE OFF POSITION AND THE AIRCRAFT POWER IS TURNED OFF, E MERGENCY LIGHTS COME ON. ALSO WHEN THE AIRCRAFT POWER IS TURNED ON AND THE EMERGENCY LIGHT SWITCH IN THE COCKPIT IS TUR NED ON, THE EMERGENCY LIGHTS DO NOT COME ON. MAINTENANCE RESECURED A LOOSE WIRE ON THE EMERGENCY LIGHTS CONNECTOR. OPE RATIONS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002092300009 20020923 00009 NE 2002 9 23 ASOA020481 2 20020904 A 8550 OIL CAP AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE LT ENGINE MISSING A ASOA O OTHER D J INFLIGHT SEPARATION WARNING INDICATION DE DESCENT 1 SO 11 643AS 413 127155 DURING DECENT, THE LT ENGINE INDICATED A WARNING FOR LOW OIL PRESSURE. THE WARNING SHOWED LOW OIL PRESSURE ON THE CAP A ND LOCAL ALERT, WITH AN OIL PRESSURE FLUCTUATION IN THE CAUTION AND WARNING AREAS. THE PILOT SHUT THE ENGINE DOWN IAW T HE QRH CHECK LIST REQUIREMENTS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE ENGINE OIL CAP OFF AND THE ENGINE COVERED IN OIL. ENGINE WAS SERVICED WITH ELEVEN QUARTS OF OIL AND RAN AT 60 PERCENT TORQUE FOR FIVE MINUTES AND 35 PERCENT TORQUE FOR FIVE MINUTES. LEAK AND OPERATIONS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT E20NE 2002092300010 20020923 00010 NE 2002 9 23 ASOA020485 2 20020904 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LEFT FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 11 503AS 120275 WHILE IN FLIGHT, THE CREW REPORTED THE LT ENGINE OIL PRESSURE FLUCTUATED AND THE DECISION WAS MADE TO SHUT THE ENGINE DO WN. AN EMERGENCY WAS DECLARED AND THE FLIGHT WAS DIVERTED. THE FLIGHT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED LT ENGINE DUE TO OPERATION WITH LOW OIL PRESSURE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092300011 20020923 00011 SO 2002 9 23 ASOA020486 1 20020906 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 261AS 32469 120141 DURING GROUND INSPECTION, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE EMERGENCY LIGHT SWIT CH ON AND CHARGED THE BATTERY PACK. OPERATIONS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092300012 20020923 00012 SO 2002 9 23 ASOA020492 1 20020908 A 2150 A/C PACK EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE CABIN CONTAMINATED A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 232AS 120036 DURING CLIMBOUT, A BURNING ODOR CAME FROM THE PACKS WAS EXPERIENCED. THE CAPTAIN TURNED OFF BOTH THE LT AND RT PACKS SE PARATELY AND DETERMINED THE RIGHT PACK WAS EMITTING THE SMELL. SUBSEQUENTLY THE RIGHT PACK WAS TURNED OFF FOR THE REMAI NDER OF THE FLIGHT AND THE SMELL DISCONTINUED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE DEFERRED THE AUXILIARY POWER UN IT DUE TO SUSPECTED OIL COMING FROM THE BLEED. THIS MRR WILL REMAIN OPEN UNTIL THE DEFERRAL HAS BEEN CLEARED AND THE CA USE OF THE DISCREPANCY CAN BE DETERMINED. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092300013 20020923 00013 SO 2002 9 23 ASOA02448 1 20020812 A 3610 38E966A REGULATOR VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CENTER WING LEAKING A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 638AS 120282 115079 WHILE PERFORMING A GO AROUND PROCEDURE, CLIMBING TO 4000 FEET, THE FLIGHT CREW RECEIVED A DUCT LEAK WARNING FOR THE RT E NGINE. THE APPROPRIATE CHECKLIST WAS COMPLIED WITH, BUT THE LIGHT DID NOT EXTINGUISH. IAW THE CHECKLIST THE CAPTAIN SE CURED THE RT ENGINE, AND THE LIGHT WENT OUT. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE FO UND A LEAK AT THE RT ENGINE PRESSURE LINE PRESSURE REGULATOR. MAINTENANCE REMOVED AND REPLACED THE PRESSURE REGULATOR V ALVE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092300014 20020923 00014 SO 2002 9 23 ASOA02449 1 20020812 A 3260 922FS2A6NZ735A PROXIMITY SENSOR EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE MLG FAILED A ASOA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 232AS 120036 WHILE WAITING TO TAXI, THE CAPTAIN RECEIVED AN ELECTRONIC CAPTION WITH NO ASSOCIATED ALARM LIGHT. SHORTLY AFTER THAT TH E FIRST OFFICER REPORTED SMOKE. THE CAPTAIN ATTEMPTED TO TAXI THE AIRCRAFT TO THE GATE, BUT THE STICK SHAKER WENT OFF A ND NEITHER NOSE WHEEL NOR PEDAL STEERING WOULD RESPOND. AT THAT TIME A RIGHT PACK FAIL MESSAGE WAS RECEIVED, AND THE PA CK WAS TURNED OFF. THE SMOKE WAS NOT HEAVY BUT DID NOT CLEAR AT ALL. THE FLIGHT ATTENDANT ALSO REPORTED SMOKE IN THE C ABIN. THE AIRCRAFT WAS EVACUATED AT THAT TIME IAW QRH PROCEDURES. MAINTENANCE REMOVED AND REPLACED THE RIGHT GEAR PROX IMITY SENSOR AND ATTACHING HARNESS ASSEMBLY. OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092300015 20020923 00015 EA 2002 9 23 ASOA02456 1 20020818 A 2750 860D1008 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE TE FLAPS FAULTY A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 885AS 2284 7521 AFTER TAKEOFF, THE FLAPS DID NOT COME UP ABOVE SIX DEGREES. CAPTAIN PERFORMED APPROPRIATED CHECKLIST AND THE DECISION W AS MADE TO DIVERT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED OVERWEIGHT. MAINTENANCE COMPLIED WITH THE OVERWEI GHT LANDING INSPECTION WITH NO DEFECT NOTED. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT DUE TO I NTERNAL FAILURE FAULT CODE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002092300016 20020923 00016 NM 2002 9 23 C7WA200202001 1 20020114 A 3213 651951724 STRUT BOEING 727 727232 1384082 NM PWA JT8 JT8D9 52048 NE RT MLG FRACTURED A C7WA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 17 511PE 13664 20634 FLIGHT CREW REPORTED (RIGHT GEAR DOWN LIGHT ON IN FLIGHT) POST FLIGHT INSPECTION BY MAINTENANCE FOUND RT MLG SIDE STRUT UPPER SEGMENT FRACTURED AT WALKING BEAM ATTACH POINT. THE CAUSE OF THE FAILURE OF THIS PART REMAINS UNDER INVESTIGATION . 2 L 7 3 4F 4 F A3WE E2EA 2002092300017 20020923 00017 CE 2002 9 23 CJP2002F00003 1 20020807 A 3244 178K431 TIRE LEAR 55 55LEAR 5170702 CE RT MLG FAILED E CJPA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 03 551SC 55008 AIRCRAFT EXPERIENCED BLOW OUT OF RT MAIN TIRE ON TAKEOFF. AIRCRAFT RETURNED TO LAND AND REMAINING TIRE ON RIGHT GEAR BL EW DUE TO OVERWEIGHT CONDITION WITH ONE TIRE USEABLE. ALL TIRES REPLACED, WHEEL ASSEMBLY INSPECTED, ANTI-SKID WIRING RE PAIRED AND DAMAGED BRAKE HYDRAULIC HOSES WERE REPLACED. 2 L 7 2 4F A10CE 2002092300018 20020923 00018 EU 2002 9 23 COEA0203729 1 20020904 A 3233 AC64208 ACTUATOR FOKKER F27 F27MK600 4990706 EU NLG LEAKING A COEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 13 729FE 10385 AIRCRAFT RETURNED TO BASE AFTER IT WAS DISCOVERED THAT PNEUMATIC PRESSURE FOR OPERATION OF THE LANDING GEAR DROPPED TO Z ERO WITH GEAR IN UP POSITION. LANDING GEAR SELECTOR VALVE AND NOSE LANDING GEAR ACTUATOR FOUND LEAKING AND REPLACED. N OSE LANDING GEAR ACTUATOR PART HISTORY BEING INVESTIGATED FOR HARD TIME CONSIDERATION. 2 H 7 2 4T A817 2002092300019 20020923 00019 WP 2002 9 23 CRSJR2R936K 1 20020905 A 2822 3980001 PUMP DOUG DC9 DC982 3022082 WP FUEL BOOST FAILED B JR2R C ABORTED TAKEOFF B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SW 15 480CT 48069 DURING TAKEOFF ROLL THE AFT CENTER BOOST PUMP POPPED THE B AND C CIRCUIT BREAKERS. THE CIRCUIT BREAKERS WERE RESET AND A SHORT TIME LATER THE SAME CIRCUIT BREAKERS POPPED AGAIN. AT THE POINT THE AIRCRAFT RETURNED TO THE GROUND AND DURING THE TROUBLE SHOOTING PROCESS IT WAS FOUND THAT THE BOOST PUMP AND ITS CONDUIT HAD BEEN ARCHING. IT WAS DETERMINED THAT THE BOOST BUMP HAD BEEN INTERNALLY BURNED AS WELL AS THE RECEPTACLES ON THE CANNON PLUG OF THE BOOST PUMP. 2 L 7 2 4F A6WE 2002092300020 20020923 00020 CE 2002 9 23 CWQ2002F00004 1 20020804 A 2820 MS29513010 O-RING CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP FUEL SUMP CRACKED B CWQR K NONE K FLUID LOSS IN INSP/MAINT 1 GL 05 789QS 6507089 FOUND DURING INSPECTION FUEL LEAKING FROM SUMP DRAIN. REPLACED O-RING. O-RING APPEARS TO BE DRY ROTTED AND HAS CRACKS. O-RING MATERIAL IS NOT VERY FUEL RESISTANT. 2 L 7 2 4F 4 F A9NM E6WE 2002092300021 20020923 00021 CE 2002 9 23 CWQ2002F00005 1 20020728 A 2820 MS29513010 O-RING CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP FUEL SUMP DRAIN CRACKED B CWQR K NONE K FLUID LOSS IN INSP/MAINT 1 GL 05 792QS 6507092 DURING INSPECTION, NOTICED FUEL LEAKING ON FLOOR. FOUND SUMP DRAIN VALVE LEAKING. REMOVED AND REPLACED O-RING. THIS I S A COMMON PROBLEM. O-RING MATERIAL SEEMS TO HAVE RADIAL CRACKS AND LOOKS TO BE DRY ROTTED. NEEDS FUEL RESISTANCE MATE RIAL. 2 L 7 2 4F 4 F A9NM E6WE 2002092300022 20020923 00022 CE 2002 9 23 CWQ2002F00006 1 20020816 A 3340 68417066530 LENS CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT WING TIP CRACKED B CWQR K NONE O OTHER IN INSP/MAINT 1 GL 05 687QS 944 5605187 FOUND LT WING TIP LIGHT ASSEMBLY LENS CRACKED AROUND FORWARD AND AFT FLANGE. POSSIBLE CAUSE: OVER-TORQUE OF ATTACHING H ARDWARE. REPLACED WING TIP LIGHT ASSEMBLY LENS. 2 L 7 2 4F 4 F RT A22CE E00059EN 2002092300023 20020923 00023 CE 2002 9 23 EWC2002F00002 1 20020904 A 7500 651410227 LINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT & RT BLEED WORN B EWCR K NONE O OTHER IN INSP/MAINT 1 SO 05 560CK 3429 5600207 LEFT AND RIGHT BLEED AIR SENSE LINE WORN FROM WIRES OF DUCT (PN X2292S4-11). 2 L 7 2 4F 4 F RT A22CE E25EA 2002092300024 20020923 00024 NE 2002 9 23 FX72002F00003 2 20020810 A 7200 ENGINE BOEING 727 727231 1384079 NM PWA JT8 JT8D15 52051 NE NR 2 FLAMED OUT A FX7A O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 19 54348 21967 AFTER CRUISING AT FLIGHT LEVEL 33. IN ICE CONDITIONS, WITH ENGINE ANTI-ICE ON. NR 2 ENGINE EPR AND AND FUEL FLOW OSCILLA TED (EPR BETWEEN 1.7 AND 1.4), (FUEL FLOW 2500-1200). AFTER 20 MINUTES OUT OF ICE CONDITIONS AND COMMENCING DESCENT AFT ER POWER REDUCTION, NR2 ENGINE FLAMED OUT, FOLLOWED PROCEDURES AND ALL PARAMETERS WITHIN LIMITS, ENGINE WAS RESTARTED. ALL ENGINE PARAMETERS NORMAL AND WITHIN LIMITS UPON RESTART. AIRCRAFT CONTINUED TO ITS SCHEDULED DESTINATION OF TGU WIT H A NON-EVENTFUL LANDING. PERFORMED TROUBLESHOOTING BLEW OUT AND CLEANED WATER ON REAR P6 TUBE AND PS4 MOISTURE TRAP DR AIN PLUG, OPS CHECKED WAS FOUND TO BE SATISFACTORY IAW MM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002092300025 20020923 00025 NM 2002 9 23 GAIA02080ST 1 20020903 A 5330 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FORWARD LOWER CARGO DOOR CUTOUT FRAME AND SKIN WAS DENTED NEAR S TRINGER S23R AT THE FORWARD PORTION OF THE DOOR CUTOUT FRAME (FUSELAGE SKIN). C/A: ACCOMPLISHED REPAIR IAW REPAIR ORDE R. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002092300026 20020923 00026 NE 2002 9 23 GTIA020649 2 20020612 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE NR 2 FAILED A GTIA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 23 803NK 27212 48087 ENGINE SHUTDOWN, RIGHT ENGINE FAILURE DURING DEPARTURE. VIBRATION FOLLOWED RAPID ROLLBACK. AFTER FAILURE NR 1, 12 PER CENT, NR 2, 25 PERCENT EGT WENT OVER 800 DEGREES RETURNED TO 200 DEGREES. COMPLETED ENGINE FAILURE CHECKLIST DECLARED E MERGENCY, LANDED AT ACY EVACUATED AC ON RECOMMENDATION OF FIRE/RESCUE PERSONNEL. (QRH PROCEDURES) REMOVED AND REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 2002092300027 20020923 00027 NM 2002 9 23 IU62002F00011 1 20020530 A 2910 654494713 HOUSING BOEING 737 737500 138449E NM ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING IS CRACKED AT THE RETRACT PORT. PROBABLY CAUSED BY OVER PRESSURIZATION AND WEAKENED METAL. REPLACE WITH UPGRAD ED HOUSING ASSEMBLY. (OCN: 168497 / MECH. CB4) 2 L 7 2 4F RT A16WE 2002092300028 20020923 00028 NM 2002 9 23 IU62002F00015 1 20020716 A 2913 123412 COVER BOEING 737 737* NM SHUTOFF VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 CRACKED, STEEL SLEEVE IN THE BORE AT MANUFACTURING. (OCN: 169495) 2 L 7 2 4F RT A16WE 2002092300029 20020923 00029 NM 2002 9 23 IU62002F00016 1 20020716 A 2913 511531 HOUSING BOEING 737 737* NM SHUTTLE VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING CRACKED IN MOUNTING HOLES. OVER-TORQUE, OVER-PRESSURE, POOR DESIGN. ENGINEER A NEW DESIGN OR MATERIAL FOR HOUS ING. (OCN: 169578/ RESP:DF5/ DEPT. 1140) 2 L 7 2 4F RT A16WE 2002092300030 20020923 00030 NM 2002 9 23 IU62002F00017 1 20020730 A 2910 123412 COVER BOEING 737 737* NM VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 COVER CRACKED. 2 L 7 2 4F RT A16WE 2002092300031 20020923 00031 NM 2002 9 23 IU62002F00018 1 20020716 A 2910 S11531 HOUSING BOEING 737 737* NM SHUTTLE VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING CRACKED IN MOUNTING HOLES. 2 L 7 2 4F RT A16WE 2002092300032 20020923 00032 NM 2002 9 23 IU62002F00019 1 20020718 A 2910 654494713 HOUSING BOEING 737 737500 138449E NM ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING CRACKED AT RETRACT PORT. 2 L 7 2 4F RT A16WE 2002092300033 20020923 00033 NM 2002 9 23 IU62002F00020 1 20020718 A 2761 654494715 HOUSING BOEING BOEING 737 737500 138449E NM ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 36144 7631 GROUND SPOILER ACTUATOR HOUSING CRACKED AT RETRACT PORT. 2 L 7 2 4F RT A16WE 2002092300034 20020923 00034 NM 2002 9 23 IU62002F00021 1 20020723 A 2910 654494710 HOUSING BOEING BOEING 737 737* NM ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 3706 ACTUATOR HOUSING IS CRACKED OUT, 2ND SHOULDER ON THE RETRACT SIDE. 2 L 7 2 4F RT A16WE 2002092300035 20020923 00035 NM 2002 9 23 IU62002F00022 1 20020724 A 2913 122510 HOUSING BOEING 737 737* NM HYD VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HYD VALVE HAS A CRACKED HOUSING. 2 L 7 2 4F RT A16WE 2002092300036 20020923 00036 NM 2002 9 23 IU62002F00023 1 20020729 A 2910 S11531 HOUSING PNEUDRAULICS BOEING 737 737* NM VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 1276 VALVE HOUSING CRACKED AT MOUNTING HOLE. 2 L 7 2 4F RT A16WE 2002092300037 20020923 00037 NM 2002 9 23 IU62002F00025 1 20020731 A 2910 654494710 HOUSING BOEING BOEING 737 737* NM RETRACT PORT CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 32499 9089 ACTUATOR HOUSING IS CRACKED UNDER THE RETRACT PORT. 2 L 7 2 4F RT A16WE 2002092300038 20020923 00038 CE 2002 9 23 KC82002F00004 1 20020905 A 2797 TERMINAL LEAR 24 24D 5170311 CE GE CJ610 CJ610* 30006 NE MAIN TRIM CORRODED E KC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 588CG 304 NORMAL PITCH TRIM FAILED SHORTLY AFTER TAKE OFF. MAINTENANCE REPORTED FINDING MAIN TRIM POWER WIRE CORRODED AND LOOSE O N RELAY NR 354 LOCATED IN HELL HOLE AREA. TERMINAL END WAS CLEANED AND RESECURED. PERFORMED TRIM SYSTEMS OPERATIONAL C HECK IAW SRM. 2 L 7 2 4J 4 J A10CE 1E16 2002092300039 20020923 00039 NE 2002 9 23 C1HA200284002 2 20020922 A 7261 JT8D17 ENGINE BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE A C1HA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 GL 15 684CA 22491 688227 Shutdown #3 engine due to low oil quantity and pressure. Diverted - oil pressure went below 10psi on approach. Removed a nd replaced #3 engine. 2 L 7 3 4F 4 F A3WE E2EA 2002092300040 20020923 00040 NM 2002 9 23 KQ72002F00000 1 20020501 A 5740 651924819 FITTING BOEING 727 72723 1384004 NM TE FLAPS CRACKED B KQ7R K NONE O OTHER IN INSP/MAINT 1 SW 17 727WF 38132 20045 DURING C5 AND C6 CHECK WITH FLAPS REMOVED FOR CPCP INSPECTION FOUND THE RT INBOARD FLAP INBOARD CARRIAGE AFT TRUNION BEA RING SUPPORT CRACKED THROUGH INTIRE UPPER PART OF CASTING WHERE AFT BEARING SUPPORTS THE INBOARD FLAP CARRIAGE ASSEMBLY SPINDLE. THE FLAP CARRIAGE FITTING WAS REMOVED AND A NEW FITTING INSTALLED WITH HI-LOCS. 2 L 7 3 4F A3WE 2002092300041 20020923 00041 NM 2002 9 23 KQ72002F00001 1 20020912 A 5711 65162337 SPAR BOEING 727 72744 1384101 NM PWA JT8 JT8D* NE WINGS CORRODED B KQ7R K NONE O OTHER IN INSP/MAINT 1 SW 17 44MD 35323 19318 DURING C5 AND C6 CHECK, GPCP VISUAL INSPECTION OF WING REAR SPAR FOR CORROSION, DISCOVERED SEALANT COVERING UP SPAR. M ECH REMOVED SEALANT IN SAMPLING AREAS, FOUND PREVIOUS REPAIRS FOR CRACKING AND BLEND OUT AREAS OF CORROSION AND CRACKING . PERFORMED NDT INSP HFEC AND CONFIRM DAMAGE FOUND BY VISUAL. REMOVED WING PANEL AND INSPECTED INTERIOR OF FUEL CELL A REA, NO VISUAL DEFECTS NOTED. FOUND STACKED ANGLE REPAIRS TO SPAR. REMOVAL OF PREVIOUS REPAIRS, DISCOVERED CORROSION B ETWEEN WING SKIN PANELS AND REAR SPAR. REMOVING ALL EXISTING REPAIRS AND REPLACED ENTIRE OUTER SECTION OF UP SPAR CHORD , LESS O/B SECTION. FOUND AREAS OF CORROSION BETWEEN UPPER WING SKINS AND SPARS. REAR SPARS WERE REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 2002092300042 20020923 00042 NM 2002 9 23 MYW2002F00001 1 20020813 A 2720 3815001001 PCU BOEING 737 737800* NM RUDDER LEAKING A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 732MA DURING PREFLIGHT TRANSIT FOUND HYD FLUID LEAKING FROM TAIL AREA JUST AFT OF ELEVATORS (BOTH SIDES) FROM ABOVE AREA. (ET OPS ISSUE) TROUBLESHOOTING FOUND PCU LEAKING. REMOVED MAIN RUDDER PCU IAW MM. REPLACED RUDDER PCU IAW MM. LEAK CHECK AND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002092300043 20020923 00043 NM 2002 9 23 MYW2002F00002 1 20020803 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 DURING PREFLIGHT TRANSIT FOUND CEILING EMERGENCY EXIT LIGHTS AT ROW 19, INOPERATIVE. TROUBLE SHOT SYSTEM, REMOVED AND R EPLACED BATTERY PACK IN CEILING, OPS CHECKED SATISFACTORY IAW MM. RETURNED AIRCRAFT TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002092300044 20020923 00044 NM 2002 9 23 MYW2002F00003 1 20020805 A 3350 900542 POWERPACK BOEING 727 727243 138408D NM PWA JT8 JT8D9 52048 NE CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 521DB 21266 DURING PREFLIGHT TRANSIT FOUND CEILING EMERGENCY EXIT SIGN AFT OF SECOND OVERHEAD LIFERAFT INOPERATIVE. TROUBLE SHOT SY STEM. REMOVED AND REPLACED BATTERY PACK POWER PACK ASSEMBLY. OPERATIONAL CHECK OK, IAW MM. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 3 4F 4 F RT A3WE E2EA 2002092300051 20020923 00051 NM 2002 9 23 PCS2002F00007 1 20020214 A 3610 BACC10DU300 COUPLING BOEING 727 727212 138407G NM NR 3 PYLON LOOSE A PCSA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 17 598AJ 21947 CREW REPORTED NR 3 STRUT OVERHEAT LIGHT CAME ON. FOLLOWED AJT ABNORMAL PROCEDURE LIGHT WENT OUT. AFTER THROTTLE ADVANC EMENT LIGHT CAME BACK ON. AIRCRAFT DIVERTED BACK, DUMPED 30,000 LBS OF FUEL AND LANDED WITHOUT FURTHER INCIDENT. MAINT ENANCE FOUND A LOOSE CLAMP ON NR 3 ENGINE 13TH STAGE MODULATION VALVE. CLAMP WAS REPOSITIONED. NO LEAKS NOTED AND LIGH T REMAINED OFF AT GROUND POWER RUN. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2002092300054 20020923 00054 NE 2002 9 23 QEM2002F00000 2 20020828 A 7250 799782 VANE BOEING 747 747300 GL PWA JT9 JT9D7R4G2 52054 NE NR 2 ENGINE FRACTURED B QEMY O OTHER J WARNING INDICATION CL CLIMB 1 EA 25 4878 FGSEA 715117 SHORTLY AFTER TAKEOFF, SMOKE WAS REPORTED, SURGE OF NR 2 ENGINE FOLLOWED. INSPECTION AFTER STRIPPING, FOUND THAT 1 HPT STAGE, 2 VANE HAD BEEN LIBERATED. ALL HP AND LP TURBINE AIRFOILS WERE SUBSEQUENTLY DAMAGED. INVESTIGATION SUGGEST HPT STAGE 2 VANE FORWRD OUTER FLANGE FAILED ALLOWING VIBRATION AND FRETTING. SUPPORT TO THIS SIS EVIDANCE OF SULPHIDATION O F FORWARD OUTER FLANGE SURFACE. 2 L 7 4 4F 4 F RT A20WE E3NE 2002092300055 20020923 00055 SW 2002 9 23 R2J2002F00010 1 20020830 A 5330 2722142005 SKIN SWRNGN SA226 SA226TB 8780406 SW GARRTT TPE331 TPE331* 01514 WP FUSELAGE CRACKED B R2JR K NONE O OTHER IN INSP/MAINT 1 EA 21 193SC 9190 T300 DURING TROUBLESHOOTING OF PRESSURIZATION SYSTEM FOUND .500 INCH CRACK IN PRESSURE VESSEL F.S.190-LT-NEAR STRINGER 11. C RACK SUSPECTED TO BE CAUSED BY SKIN DENTING DURING SPAR AD COMPLIANCE SEVERAL YEARS PREVIOUS. AREA VISIBLE THROUGH WING INSPECTION PANELS AND THIS AREA NEEDS CLOSE INSPECTION. MAJOR REPAIR C/W PER SRM. FAA APPROVED PATCH. 2 L 7 2 4T 3 T RT A5SW E2WE 2002092300056 20020923 00056 NM 2002 9 23 TSAA0251185 1 20020813 A 5310 6546551 FRAME BOEING 737 7372M6C 1384708 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 CRACK LOCATED AT BS 807, S-14L. CUT AND REMOVED DAMAGED AREA, VERIFIED CRACK REMOVAL UTILIZING HFEC METHOD NO DEFECTS N OTED, FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER FROM .063 IN 2075-T6 IAW APPROVED FASTENERS WENT WITH BMS 5-95 S EALANT PER TABLE I AND TABLE V IAW SRM. APPLIED ALODINE COATING AND ONE COAT OF BMS 10-11, TYPE 1 PRIMER TO ALL REPAIR PARTS AND BARE SURFACES AND BMS 5-95 SEALANT APPLIED TO ALL FAYING SURFACES. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A16WE 2002092300057 20020923 00057 NM 2002 9 23 TSAA0251186 1 20020813 A 5330 SKIN BOEING 737 7372M6C 1384708 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 47120 21809 RT BS 1129 AND BS 1138 FUSELAGE SKIN CRACKS LOCATED AT S5R AND S12R. TRIMMED OUT CRACKS MAINTAINING A MINIMUM TRIM OUT CORNER RADIUS .050 INCHES AT A SURFACE FINISH OF 63 RMS OR SMOOTHER. PERFORMED HFEC INSPECTION AROUND TRIMOUT AREA, NO DEFECTS NOTED. FABRICATED AND INSTALLED .063 INCHES 2024T3 REPAIR DOUBLER, TWO .056 INCHES 2024T3 FILLERS AND A 2024T3 CLAD ALUMINUM TAPER SHIM WITH APPROVED FASTENERS WET WITH CORROSION INHIBITOR TO A REPAIR PARTS. APPLIED BMS 5-95 SEALA NT TO ALL FAYING SURFACES IAW ECO. RECEIVED 8110-3 APPROVAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002092300058 20020923 00058 NM 2002 9 23 TSAA0251187 1 20020813 A 5310 6545785521 WINDOW FRAME BOEING 737 7372M6C 1384708 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 RT SIDE WINDOW FRAME CORNER FASTENER HOLE CRACK AT BS 380. CRACK ON WINDOW FRAME ASSY BY UTILIZING HFEC ROTARY PROBE ME THOD, REAMED WINDOW FRAME FASTENER HOLE UNTIL REMOVAL OF CRACK, CRACK REMOVAL BY HFEC ROTARY METHOD, ENLARGED, INSTALLED FREEZE PLUG TO FASTENER HOLE TO MAINTAIN FREEZE PLUG WALL THICKNESS OF .050 INCH PER SRM. FAB AND INSTALL .032 INCH FI LLER, A .050 INCH FILLER, A .071 INCH FILLER AND .063 INCH DOUBLER FROM 2024-T3 CLAD ALUM WITH APPROVED FASTENERS, ALODI NE AND TWO COATS OF BMS 10-11 TYPE 1 PRIMER TO EXPOSED SURFACES. BMS 5-95 SEALANT APPLIED TO ALL FAYING SURFACES. BMS- 3-23 CORROSION INHIBITING COMPOUND APPLIED TO INTERNAL SURFACES OF REPAIR AREA IAW ECO. A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002092300059 20020923 00059 NM 2002 9 23 TSAA0251188 1 20020813 A 5310 6545785521 WINDOW FRAME BOEING 737 7372M6C 1384708 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 RT SIDE WINDOW FRAME CORNER FASTENER HOLE CRACK AT BS 727B. VERIFIED CRACK ON WINDOW FRAME ASSY BY UTILIZING HFEC ROTAR PROBE METHOD, REAMED WINDOW FRAME FASTENER HOLE UNTIL REMOVAL OF CRACK. VERIFIED CRACK REMOVAL BY HFEC ROTARY METHOD, ENLARGED AND INSTALLED FREEZE PLUG TO FASTENER HOLE TO MAINTAIN FREEZE PLUG WALL THICKNESS OF .050 IN PER SRM 51-10-9. FAB AND INSTALL .032 IN FILLER A .050 INCH FILLER, A .071 IN FILLER AND A .063 IN DOUBLER FROM 2024-T3 CLAD ALUM WITH AP PRVD FASTENERS, APPLIED TO ALL FAYING SURFACES. BMS 3-23 CORROSION INHIBITING COMPOUND APPLIED TO INTERNAL SURFACES OF REPAIR AREA IAW ECO. A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002092300060 20020923 00060 NM 2002 9 23 TSAA0251189 1 20020813 A 5720 6545320147 STIFFENER BOEING 737 7372M6C 1384708 NM LT WING CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 47120 21809 LT WING FRONT SPAR STIFFENER CRACK AT FSS 473.31 AND FSS 475.55. REMOVED, FABRICATED AND INSTALLED STIFFENERS. NEW STI FFENERS FABRICATED FROM 7178-T6511 EXTRUSION AND NEW SHIMS FABRICATED FROM 2024-T3, APPLIED ALODINE AND BMS 10-11 TYPE 1 PRIMER AND BMS 10-11 TYPE 2 ENAMEL TO ALL EXPOSED SURFACES, BMS 5-26 SEALANT APPLIED TO ALL FAYING SURFACES. INSTALLED .0312 INCH OVERSIZED TENSION PROTRUDING HEAD HEX DRIVE BOLTS AT EXISTING RIVET LOCATIONS AND .0156 OVERSIZED TENSION PR OTRUDING HEAD HEX DRIVE BOLTS AT EXISTING LOCK BOLT LOCATIONS WET WITH BMS 5-26 SEALANT. REPAIR COMPLETED IAW ECO. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002092300061 20020923 00061 NM 2002 9 23 TSAA0251190 1 20020813 A 5311 6546551 FRAME BOEING 737 7372M6C 1384708 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 TEAR STRAP FASTENER HOLE CRACK AT BS 777, S-20L. REMOVED FASTENER AND VERIFIED CRACK UTILIZING HFEC ROTARY HOLE PROBE M ETHOD IAW WITH NDT, REMOVED DAMAGED AREA AND HFEC INSPECTION COMPLETED NO DEFECTS NOTED. FABRICATED AND INSTALLED .032 IN 2024-T3 CLAD REPAIR FILLERS AND DOUBLERS WITH APPROVED FASTENERS, APPLIED ALODINE AND BMS 10-79 TYPE II PRIMER TO ALL REPAIR PARTS AND BARE SURFACES. APPLIED BMS 5-95 SEALANT TO ALL FAYING SURFACES. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002092300062 20020923 00062 NM 2002 9 23 TSAA0251192 1 20020826 A 5330 6554962 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 39735 BS 380 STRING 15R CRACK ON FUS SKIN. HFEC INSP EDGES ON CUTOUT, .040 IN INSUR CUT, FAB 2024-T3, CLAD SHEET .032 IN FIL LER, .050 IN FILLER, AND .050 DOUBLER, MAINTAINING 2D MIN EDGE MARGIN, 2.0 INCH MIN INSIDE CORNER AND .5 IN MIN OUTSIDE CORNER RADIUS WITH CHAMF EDGES PRE-FORMED TO MATCH CONTOUR OF FUSELAGE. SURFACES TREATED WITH CHEMICAL CONVER COATING, TWO COATS, BMS 10-79, TYPE III PRIMER. INSTALL PARTS USING BACB30FP6AAT EXIST HI-LOK LOCATIONS. BACR15BB6AD ATTACH .03 2 FILLER TO SKIN POCKET, BACR15BB6D AT FASTENER LOCATIONS WET WITH BMS 5-95 SEALANT BETWEEN FAYING SURFACES. APPLIED BM S5-95 FILLET SEAL AROUND EDGES AND APPLIED CORROSION INHIBITING COMPOUND TO INTERN SURFACES. AC RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002092600044 20020926 00044 NM 2002 9 26 VNAA0209027 1 20020919 A 3250 2318000002 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING FAILED A VNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 438JS 18249 3056 ON SHORT FINAL, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE AND DECIDED TO DO A MISSED APPROACH. THE CREW RESET THE SYSTEM IN ACCORDANCE WITH THE QUICK REFERENCE HANDBOOK AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE WHEEL STEERING CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHEC KS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002092300063 20020923 00063 NM 2002 9 23 VNAA0209028 1 20020919 A 3200 2318000002 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 438JS 18249 3056 ON SHORT FINAL, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE AND DECIDED TO DO A MISSED APPROACH. THE CREW RESET THE SYSTEM IN ACCORDANCE WITH THE QUICK REFERENCE HANDBOOK AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE WHEEL STEERING CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHEC KS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002092300064 20020923 00064 NM 2002 9 23 VNAA0209026 1 20020918 A 3200 870004MODB PSEU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 472PS 9114 486 3008 DURING CLIMB OUT, THE CREW RECEIVED A PROXY SYSTEM FAIL CAS MESSAGE AND WERE INSTRUCTED TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORM ED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002092300065 20020923 00065 NM 2002 9 23 TSAA0253183 1 20020629 A 5311 6573748 FRAME BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D17 52049 NE APU BAY CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 24031 AUXILIARY POWER UNIT COMPARTMENT CORRODED AT BS 1156 REMOVED DAMAGED SECTION OF FRAME FABRICATED AND INSTALLED REPAIR FI LLER AND DOUBLER FROM SRM, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4U 4 F RT A16WE E2EA 2002092300066 20020923 00066 2002 9 23 SWAA022151 4 20020916 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 724SW 27856 DURING SCHEDULED C1 CHECK, FOUND BOTH SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSYS OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2 L 7 2 4F RT A16WE 2002092300067 20020923 00067 NM 2002 9 23 SWAA022152 1 20020917 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM FUSELAGE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND LT EXTERIOR EMERGENCY EXIT LIGHT LENS LOOSE AT BS 727D. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002092300068 20020923 00068 NM 2002 9 23 SWAA022158 1 20020917 A 5313 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FWD CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002092300069 20020923 00069 NM 2002 9 23 SWAA022159 1 20020914 A 5330 6545775 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 867, STR 24R AND STR 25R. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2002092300070 20020923 00070 NM 2002 9 23 SWAA022160 1 20020915 A 2731 65C30878 BRACKET BOEING 737 7373Y0 1384671 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED C2 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB C ONTROL BRACKET PER MM. 2 L 7 2 4F RT A16WE 2002092300071 20020923 00071 NM 2002 9 23 SWAA022161 1 20020916 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STR 15R. REPAIRED BULKHEAD PER SWA EA. 2 L 7 2 4F A16WE 2002092300072 20020923 00072 NM 2002 9 23 SWAA022162 1 20020916 A 5311 6546529 FRAME BOEING 737 737317 138447P NM FWD CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 460, RBL 2. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002092300073 20020923 00073 NM 2002 9 23 SWAA022163 1 20020917 A 5311 6545774 FRAME BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 747, BETWEEN STR 25R AND STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002092300074 20020923 00074 NM 2002 9 23 SWAA022164 1 20020917 A 5315 6545410 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727A + 17, WL 208 AND LBL 25. REPAIRED FLOORBEAM P ER BFG ER. 2 L 7 2 4F RT A16WE 2002092300075 20020923 00075 NM 2002 9 23 SWAA022165 1 20020917 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 DURING SCHEDULED SPECIAL VISIT, FOUND BS 1016 PRESS BULKHEAD CRACKED (12 EA) ON WEBS THAT CONVERGE AT THE CENTER OF THE PRESS DOME. REPAIRED BULKHEAD PER BFG ER. 2 L 7 2 4F A16WE 2002092300076 20020923 00076 NM 2002 9 23 SWAA022166 1 20020917 A 5330 65458001115 TRIPLER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED 1/4D CHECK, FOUND CRACK AT LOWER AFT CORNER OF AIRSTAIR CUTOUT. REPAIRED TRIPLER PER SWA EA. 2 L 7 2 4F A16WE 2002092300077 20020923 00077 NM 2002 9 23 SWAA022167 1 20020917 A 5311 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND SHEAR TIES CRACKED (3 EA) BETWEEN STR 14R AND STR 15R, BS 440, BS 460 AND BS 480. REPAI RED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2002092300078 20020923 00078 NM 2002 9 23 SWAA022168 1 20020917 A 5311 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND SHEAR TIES CRACKED (2 EA) AT BS 360, BETWEEN STR 13L AND 14L AND BETWEEN STR 14R AND 14R . REPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2002092300079 20020923 00079 NM 2002 9 23 SWAA022173 1 20020913 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 765SW 29805 DURING SCHEDULED A1 CHECK, SWA SI 11038-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND B USHINGS ON NR 2, NR 3 AND NR 4 TAB HINGES PER MM. 2 L 7 2 4F RT A16WE 2002092300080 20020923 00080 NM 2002 9 23 SWAA022174 1 20020913 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 765SW 29805 DURING SCHEDULED A1 CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND B USHINGS ON NR 1, NR 3 AND NR 4 TAB HINGES PER MM. 2 L 7 2 4F RT A16WE 2002092300081 20020923 00081 NM 2002 9 23 SWAA022175 1 20020918 A 5311 6545768 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, WL 215 AND LBL 60. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002092300082 20020923 00082 NM 2002 9 23 SWAA022176 1 20020918 A 5311 6545877 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT BS 294, WL 209 AND RBL 60. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002092300083 20020923 00083 NM 2002 9 23 SWAA022179 1 20020918 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW NR 9 DEF. SECURED LIGHT PER MM . 2 L 7 2 4F RT A16WE 2002092300084 20020923 00084 NM 2002 9 23 SWAA022182 1 20020917 A 5315 6546804 FLOORBEAM BOEING 737 737317 138447P NM AFT CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, WL 208 AND RBL 2. REPAIRED FLOORBEAM PER BFG ER. 2 L 7 2 4F RT A16WE 2002092300085 20020923 00085 NM 2002 9 23 SWAA022184 1 20020918 A 5311 6545810 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 312, STR 5L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002092300086 20020923 00086 NM 2002 9 23 SWAA022186 1 20020918 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND RT FUSELAGE FRAME CRACKED AT BS 188. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002092300087 20020923 00087 NM 2002 9 23 SWAA022188 1 20020917 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 DURING SCHEDULED C4 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED (12 EA) ON WEBS THAT CONVERGE AT THE CENTER OF THE PRESS DOME AND RADIATE OUT IN ALL DIRECTIONS. MX FERRY TO PAE. REPAIRED BULKHEAD PER BFG ER. 2 L 7 2 4F A16WE 2002092300088 20020923 00088 NM 2002 9 23 TSAA0253191 1 20020816 A 5310 143A323037 DOOR FRAME BOEING 737 73776N 13844CH NM CARGO BAY GOUGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 741AL 4988 28641 GAUGE LOCATED AT FORWARD CARGO DOOR FORWARD FRAME UPPER CORNER CUTOUT. CUTOUT THE DAMAGE TO MAINTAIN WITHIN A 1 INCH DI AMETER. PERFORMED HFEC INSPECTION AT CUTOUT AREA PER NDT. APPLIED ALODINE AND PRIMERED ALL BARE SURFACES. CUTOUT FILL ED WITH BMS 5-95 SEALANT IAW ECO. RECEIVED 8110-3 APPROVAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002092300089 20020923 00089 EA 2002 9 23 02260649 1 20020917 A 2700 4918 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 649BR 7414 During flight, the crew reported that the rudder indicated full right deflection with some control problems. The aircraf t was returned to IAD and landed without incident. Maintenance personnel removed and replaced the flight control positi on indication power supply. Operational checks and a maintenance acceptance flight were satisfactory and the aircraft w as returned to service. 2 L 7 2 4F RT A21EA 2002092300090 20020923 00090 EA 2002 9 23 02262649 1 20020919 A 2700 4918 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER CR CRUISE 1 EA 27 649BR 7414 During flight, the crew reported that the rudder and aileron were self trimming and that the flap position indication os cillated regardless of the selected flap position. The flight continued to HPN and landed without incident. Maintenanc e personnel removed and replaced the flight control position indication power supply. Operational checks were satisfact ory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002102800117 20021028 00117 WP 2002 10 28 ARWA20020915 1 20020920 A 2910 37160197 HYDRAULIC LINE DOUG DC8 DC861 3021952 WP NR 2 ENGINE LEAKING A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 29UA 46159 LOSS OF HYDRAULIC FLUID IN FLIGHT, PERFORMED EMERGENCY CHECKLIST AND LANDED IN MIA WITHOUT FURTHER INCIDENT. FOUND NR 2 ENGINE HYDRAULIC CASE DRAIN LINE LEAKING. REMOVED & REPLACED LINE IAW MM 20-12-0. SERVICED HYDRAULIC FLUID IAW MM 12- 30-1, PREFORMED LEAK CHECK OF ENGINE IAW MM 71-00 & 29-00, NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002092300091 20020923 00091 EU 2002 9 23 MALA020535 1 20020904 A 5751 HINGE SAAB SF340 SF340A 7850100 EU AILERON LACK OF LUBE A MALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 15 110XJ 340A110 DURING FLIGHT 3321, WITH AUTO-PILOT OFF, A/C HARD TO TURN TO THE LEFT. MAINTENANCE PERFORMED REQUIRED AILERON CHECKS, A LL CHECKS GOOD. LUBRICATED AILERON HINGE POINTS, FREEDOM FORCE CHECK OF PILOTS AND F/O'S CONTROL COLUMN IS GOOD. 2 L 7 2 4T RT A52EU 2002092300092 20020923 00092 EU 2002 9 23 MALA020536 1 20020905 A 2120 ODOR SAAB SF340 340B 7860101 EU CABIN DETECTED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 360PX 340B220 DURING FLIGHT 2922, FWD SUPPLEMENTAL AIR CONDITIONING SMELLS HOT/ BURNT. SUSPECT MOTOR BURNT UP. NO OTHER INFORMATION AT THIS TIME. 2 L 7 2 4T RT A52EU 2002092300093 20020923 00093 EU 2002 9 23 MALA020537 1 20020901 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 416XJ 340B416 DURING 4K-INSPECTION IN CWA, LT CENTER AISLE SEAT TRACK FWD PORTION STA 297 HAS CORROSION. MAINTENANCE REMOVED CORROSIO N IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002092300094 20020923 00094 EU 2002 9 23 MALA020538 1 20020901 A 5260 CHANNEL SAAB SF340 340B 7860101 EU AIRSTAIR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 416XJ 340B416 DURING 4K-INSPECTION IN CWA, AIRSTAIR SLIDE UNIT CHANNEL HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002092300095 20020923 00095 EU 2002 9 23 MALA020540 1 20020901 A 5320 STRUCTURE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 416XJ 340B416 DURING 4K-INSPECTION IN CWA, RT SEAT TRACK FWD WRAP AROUND AT STA 294 HAS HEAVY CORROSION. MAINTENANCE INSTALLED NEW WR AP AROUND. 2 L 7 2 4T RT A52EU 2002092300096 20020923 00096 EU 2002 9 23 MALA020541 1 20020901 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 416XJ 340B416 DURING 4K-INSPECTION IN CWA, ANGLE AT FRAME STA 225 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002092300097 20020923 00097 EU 2002 9 23 MALA020542 1 20020830 A 5320 BEAM SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 416XJ 340B416 DURING 4K-INSPECTION IN CWA, LT BEAM AND ANGLE LBL 10.5 BETWEEN FRAME STA 258 & 236.5 HAS CORROSION. MAINTENANCE REMOVE D CORROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002092300098 20020923 00098 EU 2002 9 23 MALA020543 1 20020830 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 416XJ 340B416 DURING 4K-INSPECTION IN CWA, FRAME AND ANGLE TOPS AT STA 258 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70 -40. 2 L 7 2 4T RT A52EU 2002092300099 20020923 00099 EU 2002 9 23 MALA020544 1 20020901 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 416XJ 340B416 DURING 4K-INSPECTION IN CWA, RT GALLEY I/B SEAT TRACK TOP AND PROFILE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED G ALLEY SEAT TRACK IAW SRM 51. 2 L 7 2 4T RT A52EU 2002092300100 20020923 00100 EU 2002 9 23 MALA020545 1 20020901 A 5321 FLOORBOARD SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 416XJ 340B416 DURING 4K-INSPECTION IN CWA, RT O/B FLOORBOARD FLANGE HAS CORROSION AFT OF STA 288. MAINTENANCE REMOVED CORROSION IAW S RM 51-70-40. 2 L 7 2 4T RT A52EU 2002092300101 20020923 00101 EU 2002 9 23 MALA020546 1 20020903 A 5320 STRUCTURE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 416XJ 340B416 DURING 4K-INSPECTION IN CWA, LT FWD SEAT TRACK WRAP AROUND HAS HEAVY CORROSION AT STA 294. MAINTENANCE INSTALLED NEW WR AP AROUND. 2 L 7 2 4T RT A52EU 2002092300102 20020923 00102 EU 2002 9 23 MALA020548 1 20020906 A 2932 981212 TRANSMITTER BAC 146 AVRO146RJ85A 1500097 EU HYD SYSTEM LEAKING A MALA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 15 528XJ E2353 ON APPROACH FROM CVG TO DTW CREW NOTED HYDRAULIC QUANTITY (YELLOW) WAS LOW, JUST BELOW 1/4. AT THE GATE F/A'S ADVISED C REW SMOKE AND FUMES IN CABIN. NOTED LEAK UNDER CABIN ON GROUND COMING FROM HYDRAULIC BAY. MAINTENANCE NOTED YELLOW HYD RAULIC SYSTEM PRESSURE TRANSDUCER HAS A BLOWN O-RING PROTRUDING FROM ITS ATTACHED FITTING, IT WAS NOTED THAT THE FITTIN G WAS TIGHT. MAINTENANCE REPLACED PRESSURE TRANSMITTER RDI CODE 1/DN2, CLEANED RESIDUAL FLUID, SERVICED, BLED HYDRAULIC S. PERFORMED LEAK CHECK. 2 H 7 4 4F RT A49EU 2002092300103 20020923 00103 NM 2002 9 23 0202946730 1 20020815 A 5315 FLOORBEAM BOEING 747 7472J9F 13848CZ NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING "H" CHECK FOUND CORROSION ON THE TOP AFT FLANGE OF FLOORBEAM AT BS 1920 FROM BL 0 TO LBL 54 AND BL 0 TO RBL 58. REPAIRED PER EA 67-192359. 2 L 7 4 4F RT A20WE 2002092300104 20020923 00104 EU 2002 9 23 MALA020549 1 20020907 A 2910 GPP125072 PRESSURE SWITCH SAAB SF340 340B 7860101 EU HYD SYSTEM FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 451XJ 340B451 DURING CLIMBOUT OF FLIGHT 2971 MAIN AND EMERGENCY HYDRAULIC PRESSURE LIGHT ILLUMINATED. FOLLOWED MEMORY ITEMS AND NOTED MAIN AND EMERGENCY ACCUMULATORS AROUND 200 PSI. THEREFORE, CREW PLACED MAIN GEAR HANDLE DOWN AND PULLED EMERGENCY GEAR HANDLE. AIR RETURN TO MSP. MAINTENANCE REPLACED HYDRAULIC PRESSURE SWITCH 9ML IAW 29-10-45-4. REPLACED RT & LT SEPAR ATION BOLTS, PERFORMED LANDING GEAR EXT AND RETRACTION TEST, PERFORMED HYDRAULIC BLEED DOWN CHECK. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002092300105 20020923 00105 EU 2002 9 23 MALA020550 1 20020908 A 5210 AC69076 DAMPENER BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR DEFECTIVE A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 515XJ E2333 FWD MAIN CABIN DOOR HARD TO ARM SLIDE. MAINTENANCE PERFORMED ADJUSTMENT TEST OF LT FWD CABIN DOOR SLIDE HANDLE IAW AMM 52-11-00. OPERATIONAL AND FUNCTIONAL TEST CHECKS GOOD. ENGAGEMENT DISENGAGEMENT POSITIONS ARE ALL GOOD. DURING T/S OF FWD PAX DOOR FOUND FWD GUST DAMPENER NOT RESTRICTING OPENING OF DOOR. MAINTENANCE REPLACED LT FWD DOOR GUST DAMPENER I AW 52-11-14. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2002092300106 20020923 00106 WP 2002 9 23 0202959617 1 20020917 A 2150 COUPLING DOUG DC9 DC932 3022066 WP LT PACK OUTPUT BLOWN A NWAA B EMER. DESCENT O OTHER CR CRUISE 1 GL 01 617NW 47235 CABIN PRESSURE CLIMBED THROUGH 10,000 FEET AT FL330. DECLARED AN EMERGENCY AND DESCENDED TO 10,000 FEET. CABIN PRESSURE WAS NOT REGAINED AND FLIGHT CONTINUED AT LOWER ALTITUDE TO AN UNEVENTFUL LANDING AT MSP. MASKS DID NOT DEPLOY. MAINTENAN CE FOUND THE OUTPUT COUPLING ON THE LEFT PACK BLOWN OPEN. REPLACED THE OUTPUT COUPLING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002092300107 20020923 00107 EU 2002 9 23 MALA020551 1 20020909 A 3297 WIRE SAAB SF340 340B 7860101 EU RT MLG DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 DURING LANDING OF FLIGHT 3026, GEAR EMERGENCY EXTENSIONS CHECKS FOUND WIRING FOR EXPLOSIVE BOLT BAD. MAINTENANCE NOTED RT GEAR EXPLOSIVE BOLT WIRING AT CANNON PLUG SHOWING OPEN. REPAIRED DAMAGED WIRING AT CANNON PLUG FOR RT LANDING GEAR E XPLOSIVE BOLT IAW SAAB WM 20-20-00, ALL OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002092300108 20020923 00108 EU 2002 9 23 MALA020552 1 20020905 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y-INSPECTION IN CWA, ANGLE AT STA 225 HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002092300109 20020923 00109 EU 2002 9 23 MALA020553 1 20020905 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y-INSPECTION IN CWA, FRAME AND ANGLE AT STA 258 HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 5 1-70-40. 2 L 7 2 4T RT A52EU 2002092300110 20020923 00110 EU 2002 9 23 MALA020554 1 20020905 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y-INSPECTION IN CWA, RT I/B GALLEY SEAT TRACK PROFILE HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002092300111 20020923 00111 EU 2002 9 23 MALA020555 1 20020905 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y-INSPECTION IN CWA, RT SIDE OF FRAME 272 TOP AND ANGLE HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION I AW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002092300112 20020923 00112 WP 2002 9 23 0202859956 1 20020911 A 3320 NW434812 CONTROLLER DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A NWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 923RW 47183 A FAINT ELECTRICAL SMELL WAS OBSERVED NEAR ROW 4 AND DURING TAXI THE SMELL PROGRESSED TO THE MIDDLE OF THE MAIN CABIN. AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. REPLACED SEAT 3AB PSU LIGHT CONTROLLER. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 2002092300113 20020923 00113 2002 9 23 0202879883 4 20020903 A 2565 13621228 SLIDE DOUG DC9 DC951 3022051 WP TAILCONE FAILED A NWAA K NONE L NO TEST NR NOT REPORTED 1 GL 01 671MC 47660 FIRST OFFICER ATTEMPTED TO LOWER REAR STAIRWAY AND DROPPED THE TAIL CONE INSTEAD. TAIL CONE EVACUATION SLIDE DID NOT DE PLOY OR INFLATE. REPLACED THE SLIDE AND THE TAIL CONE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002092300114 20020923 00114 WP 2002 9 23 0202889876 1 20020912 A 2130 39613011 CONTROL VALVE DOUG DC9 DC951 3022051 WP A/C BAY FAILED A NWAA G B O2 MASK DEPLOYED EMER. DESCENT O OTHER CR CRUISE 1 GL 01 785NC 48110 DURING CRUISE AT FL330, THE MASTER WARNING AND RED CABIN PRESSURE LIGHTS ILLUMINATED AND CABIN PRESSURE INDICATED 1000 F EET. COMPLIED WITH COM PROCEDURES. AIRCRAFT DESCENDED TO 10,000 FEET BUT CREW COULD NOT CONTROL THE CABIN PRESSURE. M ASKS DEPLOYED AUTOMATICALLY PRIOR TO DESCENT. FLIGHT LANDED AT DTW WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT FLO W CONTROL VALVE. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 2002092300115 20020923 00115 WP 2002 9 23 0202899987 1 20020913 A 2120 SMOKE DOUG DC9 DC932 3022066 WP CABIN DETECTED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 987US 47458 DURING CLIMB, SMOKE WAS NOTICED IN THE CABIN. SMOKE DISSIPATED AFTER TURNING OFF WING AND ENGINE ANTI-ICE. RETURNED AI RCRAFT TO DEPARTURE AIRPORT AND MADE AN UNEVENTFUL LANDING. MAINTENANCE PURGED THE AC SYSTEM AND REPLACED THE COALESCER BAGS. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 2002092300116 20020923 00116 NM 2002 9 23 0202916628 1 20020906 A 2530 ODOR BOEING 747 747251B 1384892 NM GALLEY DETECTED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 628US 22389 DURING FLIGHT, AN ELECTRICAL BURNING SMELL EMITTED FROM THE NR 1 HOT PLATE IN THE NR 1 GALLEY. AIRCRAFT CONTINUED TO DE STINATION AND LANDED WITHOUT INCIDENT. RECYCLED CIRCUIT BREAKER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002092300117 20020923 00117 NM 2002 9 23 0202926309 1 20020905 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51KJH-66KH. RECONNECTED LIGHTS AT ROW 66. O PERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002092300118 20020923 00118 NM 2002 9 23 0202936633 1 20020909 A 2530 CONTROLLER BOEING 747 747227B 1384888 NM GALLEY MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 633US 21991 DURING FLIGHT, AN ELECTRICAL FUME EMITTED IN THE UPPER DECK AND FLIGHT DECK. PULLED UPPER DECK GALLEY CIRCUIT BREAKERS AND SMELL DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT UPPER DECK OVEN CONTROLLER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002102800100 20021028 00100 2002 10 28 ARWA20020903 4 20020907 A 3442 20671570157 TRANSCEIVER DOUG DC8 DC862 3021970 WP WEATHER RADAR FAILED A ARWA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 1804 45896 NR 2 RADAR ON CAPTAIN'S SIDE WILL NOT PAINT GROUND RETURNS OR WEATHER. NR 2 RADAR ON FIRST OFFICER'S SIDE WILL NOT PAIN T GROUND RETURN OR WEATHER AND RADAR SPIKES. AIRCRAFT RETURNED TO DEPARTING BASE. REMOVED AND REPLACED NR 2 RADAR TRA NSCEIVER IAW MM 34-00. PERFORMED OPERATIONAL CHECK SYSTEM IAW MM 34-41-0; FOUND NORMAL. REMOVED AND REPLACED RADAR CON TROL PANEL SELECTOR IAW MM 34-41-0. OPERATIONS CHECKED BOTH POSITIONS, FOUND NORMAL IAW MM 34-41-0. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002102800106 20021028 00106 WP 2002 10 28 ARWA20020904 1 20020907 A 2740 179913 COMPUTER DOUG DC8 DC863F 302198F WP STAB CONTROL MALFUNCTIONED A ARWA B A EMER. DESCENT UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 SO 19 441J 45988 DURING DESCEND PITCH TRIM COMPENSATOR FAILED IN EXTENDED POSITION, PERFORMED EMERGENCY CHECKLIST PHASE 1 AND 2 ITEMS; IN ITIATED A FLAP 50 LANDING AND DECLARED AN EMERGENCY IAW PHASE 2 EMERGENCY ABNORMAL CHECKLIST. REMOVED AND REPLACED PITC H COMPUTER IAW MM 27-30-12 SYSTEMS OPERATIONS AND LEAKS CHECKED NORMAL IAW MM 24-30-6 AND MM 34-11-0. AIRCRAFT RETURN T O SERVICE. 2 L 7 4 4F 4A25 2002092300119 20020923 00119 WP 2002 9 23 ARWA20020905 1 20020828 A 5344 HINGE DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 8969U 46070 DURING C-CHECK, MAIN CARGO COMPARTMENT DOOR HINGE LOBE WITH CRACK STA 460. 2 L 7 4 4F 4A25 2003011700017 20030117 00017 WP 2003 1 17 ARWA20020906 1 20020816 A 5210 36456591 HINGE DOUG DC8 DC862 3021970 WP PAX DOOR CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 8969U 46070 DURING C-CHECK, FORWARD ENTRANCE DOOR UPPER HINGE WITH 2 INCH CRACK. REMOVED FORWARD ENTRANCE DOOR IAW DC-8 MM 52-11-1, REMOVED AND REPLACED HINGE AND REINSTALLED FORWARD ENTRANCE DOOR IAW DC-8 MM 52-11-1. OPS CHECK NORMAL IAW DC-8 MM 52- 10-0. NO LEAKS NOTED IAW DC-8 MM 21-00. 2 L 7 4 4F 4A25 2003011700022 20030117 00022 WP 2003 1 17 ARWA20020907 1 20020821 A 5320 DOUBLER DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 8969U 46070 DURING C-CHECK, COCKPIT STA 133 - STA 148 RBL 63 SUB FLOOR FILLER DOUBLER WITH CORROSION & SHEARED RIVET. REMOVED CORRO SION IAW DC-8 SRM 51-1-8, FOUND TO BE WITHIN LIMITS IAW DC-8 SRM 53-2-0; REMOVED AND REPLACED RIVET IAW DC-8 SRM 51-1-21 . 2 L 7 4 4F 4A25 2003011700025 20030117 00025 WP 2003 1 17 ARWA20020908 1 20020820 A 5320 FITTING DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 8969U 46070 DURING C-CHECK, MAIN CARGO COMPARTMENT STA 840, L-22R, FITTING WITH CRACK. REMOVED AND REPLACED FITTING OF MAIN CARGO C OMPARTMENT IAW DC-8 SRM 51-1-20D AND DC-8 SRM 53-1-0. 2 L 7 4 4F 4A25 2003011700026 20030117 00026 WP 2003 1 17 ARWA20020909 1 20020820 A 5320 FITTING DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 8969U 46070 DURING C-CHECK, MAIN CARGO COMPARTMENT STA 840, L-22L, FITTING WITH CRACK. REMOVED AND REPLACED FITTINGS OF MAIN CARGO COMPARTMENT STA 840, L-22L IAW DC-8 SRM 51-1-20D AND DC-8 SRM 53-1-0. 2 L 7 4 4F 4A25 2003011700027 20030117 00027 WP 2003 1 17 ARWA20020910 1 20020819 A 5720 5753054508N SUPPORT FITTING DOUG DC8 DC862 3021970 WP RT WING CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 8969U 46070 DURING C-CHECK, RT WING L/E INTERIOR STA XW 239.743 INBOARD PYLON FRONT SPAR SUPPORT FITTING (FOOT STOOL) WITH CRACK. R EMOVED AND REPLACED FOOT STOOL FITTING IAW BOEING MESSAGE INSTRUCTIONS ARW-MIA-02-00020H DATED 08/21/02, S/B DC8-57-84, DC8-A57-84 AND DC8-A57-99. 2 L 7 4 4F 4A25 2003011700028 20030117 00028 WP 2003 1 17 ARWA20020911 1 20020816 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 8969U 46070 DURING C-CHECK, MAIN CARGO COMPARTMENT 980, L-18R FRAME WITH A 1.75 INCH CRACK. REMOVED AND REPLACED AREA, FABRICATED F ILLERS ANGLES AND DOUBLER IAW AS ELEVEN INC DRAWING AS11451 SH 1 & 2, DATED 09/10/02; PRIMED FILLERS, ANGLES & DOUBLER I AW DC-8 SRM 51-1-/ AND INSTALLED FILLERS, ANGLES AND DOUBLER IAW AS ELEVEN INC DRAWING AS11451 SH 1 & 2, DATE 09/10/02; ISSUED FAA FORM 8110-3. 2 L 7 4 4F 4A25 2002111500067 20021115 00067 WP 2002 11 15 ARWA20020912 1 20020910 A 2910 LINE DOUG DC8 DC863F 302198F WP HYD SYSTEM LEAKING A ARWA O OTHER K FLUID LOSS LD LANDING 1 SO 19 784AL 46135 AFTER LANDING, LOSS HYDRAULIC FLUID TO STANDPIPE. REMOVED AND REPLACED HYDRAULIC BRAKE LINE WITH A FLEX LINE (TEMP) IAW MM 32-42-1 AND GMM 6-6-1 OPS AND LEAK OK IAW MM 32-42-1 SERVICED HYDRAULIC SYSTEM IAW MM 12-03-0. CARRIED OVER ITEM NR 05938 WAS CLOSED ON LOG PAGE NR 113307; REINTALLED FLEX LINE IN FAK AS REQUIRED. 2 L 7 4 4F 4A25 2002092300120 20020923 00120 WP 2002 9 23 ARWA20020913 1 20020912 A 7920 LINE DOUG DC8 DC863F 302198F WP NR 1 ENGINE LOOSE A ARWA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 661AV 45969 PRECAUTIONARY SHUTDOWN NR 1 ENGINE. OIL QUANTITY DECREASING, OIL PRESSURE FLUCTUATING, OIL TEMPERATURE RISING AT 1215Z WINDMILL OIL PRESSURE 15 PSI. REMOVED AND REPLACED NR 1 ENGINE MAIN OIL FILTER ELEMENT IAW P&W MM 72-0 PG 424A.B FIGURE 40B. INSPECTED REMOVED FILTER, FOUND FILTER CLEAN, NO METAL. FOUND OIL PRESSURE LINE FROM OIL PRESSURE SWITCH AT T-FI TTING AT OIL FILTER HOUSING LOOSE, TIGHTENED. PERFORMED ENGINE RUN IAW P&W MM 72-00. ENGINE OPS AND LEAK CHECK NORMAL. NO LEAK NOTED. ENGINE WAS INSPECTED AND CHECK IAW P&W MM 72-00 PAGE 663 STEP 14A, ALL NORMAL. 2 L 7 4 4F 4A25 2002092300121 20020923 00121 WP 2002 9 23 ARWA20020914 1 20020912 A 5320 SPLICE DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 DURING C-CHECK, MAIN CARGO COMPARTMENT FLOORBEAM SPLICES CRACKED AT STA 320, 340, 360, 380, 400, 420, 440 & 460 L-21 LON GITUDE. 2 L 7 4 4F 4A25 2002092300122 20020923 00122 WP 2002 9 23 MWEA020553 1 20020913 A 5320 99579083 INTERCOSTAL DOUG DC9 DC915 3022036 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 INTERCOSTAL AT FRAME STATION 332 BETWEEN LONGERON 28 AND 29 DAMAGED. REMOVED INTERCOSTAL, FABRICATED FIT AND DRILLED CL IPS AND INTERCOSTAL, INSTALLED INTERCOSTAL AND CLIP. 2 L 7 2 4F A6WE 2002092300123 20020923 00123 WP 2002 9 23 MWEA020554 1 20020913 A 5320 4912458503 INTERCOSTAL DOUG DC9 DC915 3022036 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 AT STATION 766 LONGERON 29 RIGHT INTERCOSTAL FORWARD ATTACH CLIP HAS ELONGATED HOLE. REMOVED ATTACH CLIP, FABRICATED AN D INSTALLED CLIP. 2 L 7 2 4F A6WE 2002092300124 20020923 00124 WP 2002 9 23 MWEA020555 1 20020913 A 5320 99577099 INTERCOSTAL DOUG DC9 DC915 3022036 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 REMOVED INTERCOSTAL FROM STATION 785 TO 800 AT LONGERON 29 RIGHT TO FACILITATE MAINTENANCE. FOUND ELONGATED HOLES. LOC ATED AND DRILLED INTERCOSTAL, INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2002092300125 20020923 00125 WP 2002 9 23 MWEA020556 1 20020913 A 5310 991224361 SHEAR TIE DOUG DC9 DC915 3022036 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 REMOVED SHEAR TIE AT STATION 785 FROM LONGERON 21 LEFT TO 27 LEFT TO FACILITATE MAINTENANCE. SHEAR TIE HAS SEVERAL ELON GATED HOLES, LOCATED AND DRILLED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2002092300126 20020923 00126 WP 2002 9 23 MWEA020557 1 20020913 A 5553 591214130 ATTACH ANGLE DOUG DC9 DC915 3022036 WP VERTICAL STAB DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 STATION 930 FRAME AT THE RIGHT DORSAL FIN ATTACH ANGLE HAS A FASTENER PULLING THROUGH. REMOVED 2 HI-LOKS FROM RIGHT SID E, REAMED 2 HOLES, FABRICATED AND INSTALLED SLEEVE BUSHING. 2 L 7 2 4F A6WE 2002092300127 20020923 00127 WP 2002 9 23 MWEA020558 1 20020913 A 5553 591214129 ATTACH ANGLE DOUG DC9 DC915 3022036 WP VERTICAL STAB DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 STATION 930 AT THE LEFT DORSAL FIN ATTACH ANGLE HAS TWO FASTENERS PULLING THROUGH. REMOVED 2 HI-LOKS, FABRICATED AND IN STALLED SLEEVE BUSHINGS. 2 L 7 2 4F A6WE 2002092300128 20020923 00128 WP 2002 9 23 MWEA020560 1 20020913 A 5310 5912494501 DOOR FRAME DOUG DC9 DC915 3022036 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FORWARD CARGO COMPARTMENT LOWER DOOR JAMB HAS SEVERAL AREAS OF MODERATE CORROSION STATION 312 TO 370. REMOVED DAMAGED S ECTION FIT, DRILLED SECTION AND INSTALLED NEW SECTION. 2 L 7 2 4F A6WE 2002092300129 20020923 00129 WP 2002 9 23 MWEA020561 1 20020913 A 5320 9911520233 FLOOR SUPPORT DOUG DC9 DC915 3022036 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT STATION 218 HAS SEVERAL AREAS LIGHT CORROSION LONGERON 30 TO 28 RIGHT DOT 469 . HEAT TREATED 2 DOUBLERS, LOCATED AND DRILLED DOUBLER, INSTALLED REPAIR DOUBLER, LOCATING AND DRILLED REMAINING FLOOR LINING, INSTALLED 2 NUT PLATES. 2 L 7 2 4F A6WE 2002092300130 20020923 00130 WP 2002 9 23 MWEA020562 1 20020913 A 5720 99116032 FITTING DOUG DC9 DC915 3022036 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 RIGHT WING XCW 58 LOWER WING TEE REQUIRES REPAIR OR REPLACEMENT DUE TO CORROSION REMOVAL. REMOVED WING TEE, RECEIVED NE W WING TEE, LOCATED AND DRILLED AND INSTALLED WING TEE. 2 L 7 2 4F A6WE 2002092300131 20020923 00131 WP 2002 9 23 MWEA020566 1 20020917 A 5313 591142515 LONGERON DOUG DC9 DC915 3022036 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 AFT CARGO LONGERON 29 RIGHT HAS ELONGATED HOLES TWO EACH STATION 785 FRAME LOCATION. FABRICATED AND INSTALLED SECTION O F LONGERON. REMOVED AND INSTALLED SHOVEL CLIP. 2 L 7 2 4F A6WE 2002092300132 20020923 00132 WP 2002 9 23 MWEA020567 1 20020917 A 5311 9912243105 FRAME DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FASTENER HOLES AT FRAME STATION 785 AND LONGERON 22 LEFT IS CRACKED. FABRICATED, LOCATED AND DRILLED AND INSTALLED FRAM E SPLICE. REMOVED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2002092300133 20020923 00133 EU 2002 9 23 MALA020556 1 20020905 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y-INSPECTION IN CWA, WEB AT STA 288 AND 294 HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70 -40. 2 L 7 2 4T RT A52EU 2002092300134 20020923 00134 EU 2002 9 23 MALA020557 1 20020906 A 5347 CARGO TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y-INSPECTION IN CWA, CARGO AREA SEAT TRACKS HAVE LIGHT CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-7 0-40. 2 L 7 2 4T RT A52EU 2002092300135 20020923 00135 EU 2002 9 23 MALA020558 1 20020906 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y-INSPECTION IN CWA, AFT AISLE SEAT TRACK AT 0 BL SIDE AT STA 622 TO 630 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. 2 L 7 2 4T RT A52EU 2002092300136 20020923 00136 EU 2002 9 23 MALA020560 1 20020913 A 2750 HP14161005 CONTROL VALVE SAAB SF340 340B 7860101 EU T/E FLAP FAILED A MALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 15 449XJ 340B449 DURING FLIGHT 3264, CREW REPORTED THE FLAPS WILL NOT EXTEND ON LANDING. MAINTENANCE REPLACED FLAP CONTROL VALVE IAW SAA B AMM 27-51-15-2. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2002092300137 20020923 00137 SO 2002 9 23 C2XA02TY147 1 20020923 A 5300 14522178005 SILL EMB 145 EMB145 3260210 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS, During a scheduled inspection the service door seal was found corroded. Maintenence repaired the damage by cleaning the corrosion and installing a lateral doubler. I/A/W-EMB-135/145-SRM-53-21-02, 51-40-02, CPM-51-21-04,05 & 06 and GST- 2807/02. The repair was satisfactory and the aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002092300138 20020923 00138 2002 9 23 MALA020561 4 20020915 A 3457 COMPUTER BAC 146 AVRO146RJ85A 1500097 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 510XJ E2323 DURING FLIGHT 3541, BOTH VPU QUIT COMMUNICATING INFLIGHT. IRS'S ALSO STARTED TO DRIFT SEVERELY. LT NAV FLIGHT PLAN ON ND WAS ALSO SHOWING SEVER DEVIATION FROM COURSE. NO INDICATIONS OF BAD IR'S WERE GIVEN. AIR RETURN TO MSP. MAINTENANC E RELOADED GNS-X NAV DATABASES. NR 1 AND NR 2 GNS-X CHECK GOOD IAW AVRO MM CHAP 34. 2 H 7 4 4F RT A49EU 2002092300139 20020923 00139 EU 2002 9 23 MALA020562 1 20020915 A 3230 85106RC84SNB CONNECTOR SAAB SF340 340B 7860101 EU RT MLG BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 DURING CONTINUITY CHECK OF SEPARATION BOLT DUAL BRIDGE CIRCUITRY FOUND RT CANNON PLUG BROKEN. MAINTENANCE REPLACED CANN ON PLUG ON RT SEPARATION BOLT P/N 851-06RC8-4SNB IAW WIRING MANUAL 20-30-15. 2 L 7 2 4T RT A52EU 2002092300140 20020923 00140 NM 2002 9 23 TSAA0257184 1 20020724 A 5730 SKIN BOEING 737 737230 1384401 NM LT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 LEFT LOWER OUTBOARD WING TRAILING EDGE CORRODED AT WSL 453. BLENDOUT TO REMOVE ALL CORROSION CONFIRMED USING 10X VISUAL INSPECTION NO DEFECTS NOTED, OBTAINED A SURFACE FINISH OF 125 MICROINCHES RADIUS OR SMOOTHER, FLAT PEENED REWORKED AREA , ALODINED AND PRIMED. FILLED DEPRESSIONS WITH BMS 5-95 SEALANT REFERRING TO SRM. APPLIED ONE COAT BMS 10-79, TYPE III PRIMER OVER THE SEALANT IAW ECO. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002092300141 20020923 00141 EU 2002 9 23 MALA020563 1 20020916 A 2913 PUMP BAC 146 AVRO146RJ85A 1500097 EU ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 517XJ E2335 DURING FLIGHT 3586, CREW REPORTED THE GREEN SYSTEM HYDRAULIC TEMP LIGHT ON. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED GREEN SYSTEM EDP, ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2002092300142 20020923 00142 EU 2002 9 23 MALA020564 1 20020917 A 3350 MS274061 SWITCH SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 114XJ 340A114 ON FLIGHT 3196 EMERGENCY LIGHTS UNARMED LIGHT DID NOT ILLUMINATE WHEN EMERGENCY LIGHT TURNED OFF. MAINTENANCE CHECKED L AMPS, FOUND OK. REMOVED AND REINSTALLED THE WEU IAW SAABY MM 31-50-05-4. NO VISIBLE DEFECTS NOTED. A/C HAS BEEN INSPE CTED AND FOUND SAFE FOR THE INTENDED FERRY FLIGHT FROM INL TO MSP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHTS SW ITCH IN THE COCKPIT. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002092300143 20020923 00143 EU 2002 9 23 MALA020566 1 20020918 A 3246 BEARING SAAB SF340 340B 7860101 EU RT MLG WHEEL DEFECTIVE A MALA K NONE O OTHER TO TAKEOFF 1 GL 15 445XJ 340B445 DURING TAKEOFF OF FLIGHT 3156, A/C PULLS TO THE RIGHT ON TAKEOFF. AT 60 KTS ON TAKEOFF, AFTER RELEASE OF TILLER, THE A/ C YAWED TO THE RIGHT. A LARGE LEFT RUDDER APPLICATION WAS USED TO RETURN TO CENTER LINE. WINDS WERE CALM, AND THE BRAK ES WERE NOT TOUCHED. EN ROUTE THE LINE AP ON, THE LEFT RUDDER PEDAL APPEARS TO BE FURTHER IN THAN THE RIGHT. MAINTENAN CE CHECKED NOSE WHEEL STEERING, ALL 6 WHEELS, BRAKES, RUDDER DAMPER, FOUND DEFECTIVE BEARINGS ON RT I/B WHEEL ASSEMBLY, REPLACED RT I/B WHEEL ASSEMBLIES. PERFORMED HIGH SPEED TAXI, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002092300144 20020923 00144 EU 2002 9 23 MALA020567 1 20020918 A 3350 2LA00511520 TERMINAL SAAB SF340 340B 7860101 EU CABIN BROKEN A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 442XJ 340B442 DURING LC1, NOTED EMERGENCY LIGHT IN THE COVE OVER SEAT 10A WOULD NOT COME ON. MAINTENANCE FOUND THE POSITIVE TERMINAL BRACKET ON THE LIGHT HOUSING BROKEN. MAINTENANCE REPLACED LIGHT ASSEMBLY AND OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002092300145 20020923 00145 EU 2002 9 23 MALA020568 1 20020918 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU LT MLG CONTAMINATED A MALA K NONE N FALSE WARNING AP APPROACH 1 GL 15 422XJ 340B422 DURING APPROACH OF FLIGHT 2734 LT MAIN GEAR DOWN LOCKED INDICATION DID NOT ILLUMINATE. LIGHT TESTED OK CYCLED LANDING G EAR AND THEN GOT 3 GREEN LIGHTS ON PREVIOUS APPROACH. LT MAIN LIGHT WAS VERY LATE ILLUMINATING. MAINTENANCE DURING TRO UBLESHOOTING FOUND OIL IN CANNON PLUG CLEANED AS REQUIRED. CYCLED GEAR SEVERAL TIMES, ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2002092300146 20020923 00146 WP 2002 9 23 MWEA020568 1 20020917 A 5720 59100379 SPLICE DOUG DC9 DC915 3022036 WP WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FASTENER HOLES DAMAGED IN CENTER TANK ON STRINGER 17 AFT SPLICE PLATE APPROXIMATELY 1 INCH LEFT OF STATION 0 BULKHEAD. SPOTFACED HOLE TO REMOVE DAMAGE, FABRICATED AND INSTALLED FASTENERS IN STRAP. 2 L 7 2 4F A6WE 2002092300147 20020923 00147 NE 2002 9 23 MWEA020569 2 20020917 A 7200 SMOKE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE RT ENGINE DETECTED A MWEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 203ME 47673 SMOKE COMING FROM THE RIGHT ENGINE. INSPECTED ENGINE, NO LEAKS FOUND OR SIGNS OF FIRE IN ENGINE COWL, NO DEFECTS NOTED. 2 L 7 2 4F 4 F A6WE E2EA 2002092300148 20020923 00148 EA 2002 9 23 QXEA0201316 1 20020830 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY CRACKED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 609QX 10031 PDX- FORWARD CARGO SMOKE DETECTOR CAGE IS CRACKED. REMOVED AND REPLACED ONE OF THE FORWARD CARGO SMOKE DETECTOR CAGES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002092300149 20020923 00149 EA 2002 9 23 QXEA0201317 1 20020902 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 612QX 10042 BOI- FORWARD CARGO COMPARTMENT CHIMNEY IN ENTRYWAY DAMAGED. REMOVED AND REPLACED CARGO COMPARTMENT FIRE DETECTOR CHIMNE Y. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002092300150 20020923 00150 NM 2002 9 23 QXEA0201318 1 20020827 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND WING NR 5 FLAP TRACK OUTBOARD SIDE ROLLER CONTACT SURFACE HAS PITTING. REPAIRED IAW HORIZON AIR EA 2-57 -186. 2 H 7 2 4T RT A13NM 2002092300151 20020923 00151 NM 2002 9 23 QXEA0201319 1 20020827 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - SCRATCHES ON MATTING UPPER SURFACE FOR LEADING EDGE AT STATION YW178.00 ON RIGHT HAND WING. REPAIRED IAW DHC-8-20 0 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002092300152 20020923 00152 NM 2002 9 23 QXEA0201320 1 20020829 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - PITTING ON THE OUTBOARD SIDE OF THE NR 4 FLAP TRACK ON RIGHT HAND WING. REPAIRED IAW HORIZON AIR EA 2-57-18. 2 H 7 2 4T RT A13NM 2002092300153 20020923 00153 NM 2002 9 23 QXEA0201321 1 20020829 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - PITTING ON INBOARD SIDE OF THE 4 FLAP TRACK ON RIGHT HAND WING. REPAIRED IAW HORIZON AIR EA 2-57-184. 2 H 7 2 4T RT A13NM 2002092300154 20020923 00154 NM 2002 9 23 QXEA0201322 1 20020826 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - MAIN CABIN DOOR BOTTOM AFT STOP ON APERTURE HAS WEAR PIT IN CENTER. REPAIRED IAW RD 8-53-3933. 2 H 7 2 4T RT A13NM 2002092300155 20020923 00155 CE 2002 9 23 UG82002F00008 1 20020822 A 2700 DAMPER CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL YAW MISINSTALLED E UG8A O OTHER W J INADEQUATE Q C WARNING INDICATION NR NOT REPORTED 1 GL 23 5113 3240 7500013 AMBER YAW DAMP NOT CENTERED, MESSAGE ILLUMINATED DURING TAKEOFF. TAKEOFF WAS ABORTED. YAW DAMPER NOT CENTERED. CREW R EFERENCED AND FOLLOWED APPROVED FLIGHT MANUAL PROCEDURES OF AFM. SYSTEM RESET WAS NORMAL. CREW CONTINUED TRIP. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2002092300156 20020923 00156 NM 2002 9 23 UIEA200200032 1 20020819 A 5730 65B3925015 PANEL BOEING 747 747243B 1384830 NM GE CF34 CF34* NE LT WING CRACKED E UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 66399 23300 DURING CURRENT (C) CHECK AT SIAEC FOUND CRACKED CLOSURE PANEL ON LT WING LE NR12 KRUGER FLAP FOLDING NOSE SECTION OF THE CENTER ATTACH BRACKET AT ILES 480. TRIMMED OUT CRACKED SECTION OF CLOSURE WEB. FABRICATED NEW SECTION OF WEB AND ASSO CIATED SLICE DOUBLERS. INSTALLED PER STANDARD SRM. 2 L 7 4 4F 4 F A20WE E15NE 2002092300157 20020923 00157 SO 2002 9 23 C2XA02BT055 1 20020921 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 13988 145265 BTV---CO3389, DURING 5A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHTS DO NOT COME ON IN AUTO MODE....REMOVED AND REPLACE D #2 EMERGENCY LIGHT BATTERY POWER SUPPLY/CHARGER IAW EMB145 MM 33-50-04. OPS.CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2002102100035 20021021 00035 EU 2002 10 21 DHL2002364011 1 20020914 A 2620 30903837 SQUIB AIRBUS 300 A300B4203 3930306 EU APU FIREBOTTLE FAULTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 364DH 141 APU FIREBOTTLE SQUIB WILL NOT TEST. REMOVED & REPLACED SQUIB. OPS CHECKED OK IAW M/M 26-22-12. 2 L 7 2 4F RT A35EU 2002092300158 20020923 00158 NM 2002 9 23 UIA02007 1 20020910 A 3244 WHEEL DOUG MD90 MD9030 3023690 NM MLG DEPARTED Z D RETURN TO BLOCK D J INFLIGHT SEPARATION WARNING INDICATION TX TAXI/GRND HDL 1 TW 00 17923 53534 NR 3 MAIN WHEEL MISSING , NO DAMAGE FOUND ON MLG OR FUSELAGE DURING TRANSIT CHECK. A/C APPROCHED AND LANDED WITH NORMAL CONFIGURATION, MAIN WHEEL FOUND ADJACENT TO TAXI WAY & "ANTI-SKID FAULT" MESSAGE SHOWED IAW PILOT REPORT. CARRIED OUT M AIN WHEEL CHECK IAW BOEING'S RECOMMENDATION, ALSO REPLACE NR 3 & 4 WHEEL AND SHAFT, CHECKED NORMAL. RECHECKED ORIGINAL NR 3 WHEEL, NO DAMAGE EXCEPT RETAINER PIN WAS MISSING. 2 L 7 2 4F RT A6WE 2002092300159 20020923 00159 EA 2002 9 23 UIA02002 1 20020523 A 3231 83232013003 BELLCRANK DHAV DHC8 DHC8311 1386006 EA NLG DOOR CRACKED Z L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 TW 00 15229 407 NOSE GEAR DOOR CAUTION LIGHT ON DURING APPOARCH. CHECK FOUND NOSE GEAR DOOR BELLCRANK CRACKED. REPLACED BELLCRANK ASS Y AND VISUAL CHECKED OK IAW AMM 32-30-01, SWING DOOR CHECK NORMAL. 2 H 7 2 4T RT A13NM 2002092300160 20020923 00160 NE 2002 9 23 UIA02005 2 20020729 A 7200 ENGINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 FAILED Z B EMER. DESCENT X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 TW 00 15223 404 2123204 NR 2 ENGINE HAS AN IN FLIGHT SHUTDOWN, IAW QUICK REFERENCE HANDBOOK MADE AN EMERGENCY LANDING AT KHH. FOUND TRANSFER AC CESSORY GEARBOX TOWER SHAFT HAD FREE ROTATION DURING CHECK.THIS IS THE SECOND SIMILAR EVENT HAPPENING WITHIN A WEEK, THE ENGINE WAS REPAIRED , DUE TO CENTER COOLING RING FOUND CRACKED AND MATERIAL MISSING.TSO:3314HR TSLSV:207HR CSO:6192CYC CSLSV:405CYC, 2 H 7 2 4T 4 T RT A13NM E20NE 2002092300161 20020923 00161 EA 2002 9 23 COMA0260541 1 20020919 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 716CA 7250 FLIGHT 5283 GEAR DISAGREE WARNING, NLG SLOW TO EXTEND.COULD NOT DUPLICATE. RETRACT AND EXTENSION CHECKS WERE NORMAL. 2 L 7 2 4F RT A21EA 2002092300162 20020923 00162 SO 2002 9 23 C2XA02CL184 1 20020918 A 2822 KO122 CONTACTOR EMB 145 EMB145LR 3260212 SO A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 12540 145537 EWR FLIGHT#3764 THE CREW REPORTED WHILE IN FLIGHT DURING CROSS FEED OPERATION PUMP 1B INDICATED OFF.THE PUMP WORKED ON T HE GROUND.MAINTENANCE INSPECTED AND REPLACED THE 1B FUEL PUMP CONTACTOR.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002092300163 20020923 00163 NM 2002 9 23 02092301 1 20020920 A 7732 RB211535E4 ENGINE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE RT. ENG VIBRATES A N8TA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 19 551NA 35809 2130 25621 30828 At FL 370, Rt. Eng. indicated 2.6-2.7 vib., aircraft returned to LAS. Further inspection revealed no defects as per RB2 11 M/M 72-31-13. (A tap test, blade lube, and power run were performed as per the noted M/M ref. Ops check good as per M /M Ref. noted. No other defects were noticed, aircraft was returned to service. 2 L 7 2 4F 4 F RT A2NM E12EU 2002092400002 20020924 00002 EA 2002 9 24 UIA02006 1 20020816 A 7600 7982133007L3 EEC DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 ENGINE MALFUNCTIONED Z O OTHER J WARNING INDICATION CR CRUISE 1 TW 00 15225 3 3 405 123296 NR 2 ENGINE MANUAL WARNING LIGHT CAME ON, TQ NO INDICATION IN FLT. GROUND ENGINE RUNUP, CHECK FOUND NR 2 ENGINE EEC MAL FUNCTIONED. PFM ENG RUNNING TEST AFTER REPLACED, ENG CONDITION BACK NORMAL. 2 H 7 2 4T 4 T RT A13NM E20NE 2002092400003 20020924 00003 EA 2002 9 24 UIA02003 1 20020618 A 3230 SELECTOR VALVE DHAV DHC8 DHC8311 1386006 EA MLG FAILED Z L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 TW 00 15221 325 LANDING GEAR WILL NOT EXTENED IN FLT. USED ALTERNATE EXTENSION, A/C SAFETY LANDING. AFTER CHECKING LANDING SYS, FOUND LANDING GEAR SELECTOR VALVE MALFUNCTIONED. REPLACED SELECTOR VALVE AND PERFORMED LANDING GEAR RETRACTION AND EXTENSION OPERATIONAL CHECKED NORMAL. 2 H 7 2 4T RT A13NM 2002092400004 20020924 00004 EA 2002 9 24 UIA02004 1 20020724 A 2434 SHAFT PWC PW123 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE DC GENERATOR BROKEN Z A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 TW 00 15219 123131 381 123131 NR 1 ENGINE SHUTDOWN 15 MINS AFTER TAKING OFF, SAFE SINGLE ENGINE LANDING AT MZG. MECHANIC CREW CHECKED THE ENGINE AND THE OIL TANK CHIP DETECTOR, FOUND DEBRIS AND CHECKED THE STARTER. DC GENERATOR SHAFT BROKEN, TRANSFER ACCESSORY GEARBO X INPUT AND OUTPUT HAVE NOISE WHEN FREE ROTATION TURNING WITH HAND. TSO 456 HR, CSO 878 CYC, 2 H 7 2 4T 4 T RT A13NM E20NE 2002092400005 20020924 00005 EU 2002 9 24 KBMA113004 1 20020907 A 6510 593404 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR ROUGH E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 5244 2337 NR 5 TAIL ROTOR SHAFT BEARING ROUGH. INSTALLED NEW BEARING. 1 G 7 1 3U 3 U NC H9EU E19EU 2002092400006 20020924 00006 GL 2002 9 24 KBMA115465 2 20020831 A 7261 AS308408 O-RING BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED E KBMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 667JM 3444 ENGINE HAS A REPORTED OIL LEAK. REPLACED O-RING AT REAR BEARING PRESSURE ELBOW. 1 G 7 1 3U 3 U H2SW E4CE 2002092400007 20020924 00007 EU 2002 9 24 KBMA116001 1 20020827 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 2273A 996 2273 BEARINGS WORN BEYOND LIMITS. REPLACED WITH NEW BEARINGS. 1 G 7 1 3U 3 U NC H9EU E19EU 2002092400008 20020924 00008 EU 2002 9 24 KBMA116007 1 20020912 A 6730 AC67244 SERVO SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE FLIGHT CONTROLS INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 910 2957 LATERAL SERVO IS BINDING AND GETTING WORSE IN FLIGHT CONTROLS. REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002092400009 20020924 00009 EU 2002 9 24 KBMA116008 1 20020912 A 7921 47750 BLOWER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE OIL COOLER INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 61 2957 OIL COOLER BLOWER, INOPERATIVE. REPLACED WITH SERVICEABLE UNIT/ OVERHAULED BLOWER. 1 G 7 1 3U 3 U NC H9EU E19EU 2002092400010 20020924 00010 EU 2002 9 24 KBMA116009 1 20020912 A 2917 MA12401 PRESSURE SWITCH SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE HYD SYSTEM INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 2421 2957 HYDRAULIC WARNING LIGHT STAYS ILLUMINATED ON THE GROUND AT FLIGHT IDLE. REPLACED HYD SWITCH WITH NEW SWITCH. 1 G 7 1 3U 3 U NC H9EU E19EU 2002092400011 20020924 00011 EU 2002 9 24 KBMA116010 1 20020912 A 2435 BRUSHES SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE STARTER GEN WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 37SH 942 9010XL 2300 AIRCRAFT WILL NOT START OR CRANK. FURTHER DISASSEMBLY OF STARTER GEN FOUND BRUSHES WORN. REPLACED WITH SERVICEABLE UN IT. RETURNED AIRCRAFT TO SERVICE. 1 G 7 1 3U 3 U NC H9EU E19EU 2002092400012 20020924 00012 EU 2002 9 24 KBMA116013 1 20020901 A 6510 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR DELAMINATED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 1002 2957 LAMINATED TAIL ROTOR (BEARINGS) HALF SHELLS, DELAMINATED. REPLACED WITH NEW. 1 G 7 1 3U 3 U NC H9EU E19EU 2002092400013 20020924 00013 EU 2002 9 24 KBMA116014 1 20020901 A 6520 350A33215300 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 1360 2957 BEARINGS ARE SPLIT AND CRACKED. REPLACED WITH NEW BEARING. 1 G 7 1 3U 3 U NC H9EU E19EU 2002092400026 20020924 00026 NM 2002 9 24 UIEA200200035 1 20020829 A 2430 21B772A CONTROL UNIT BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 3 GENERATOR FAILED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 527MC 22471 ON CLIMBOUT, NR 3 AND NR 4 BUS TIES OPENED. SPLIT BUS SYSTEM OPEN. NR 3 GENERATOR WAS DISCONNECTED. NR 4 GENERATOR CH ECKED GOOD VOLTS/ FREQ. NR 3 BUS LOST POWER AND COULD NOT REPOWER. DUMPED 17.0 KGS OF FUEL PRIOR TO LANDING. REMOVED AND REPLACED RIGHT BUS PROTECTION UNIT IAW MM. ALL OPS OK DURING ENGINE RUNS AND APU GENERATORS. 2 L 7 4 4F 4 F RT A20WE E23EA 2002092400027 20020924 00027 EU 2002 9 24 UO22002F00016 1 20020910 A 3020 F10A5SEP1025 SOLENOID VALVE ISRAEL 1124 1124 4500102 EU GARRTT TFE731 TFE7313 01518 WP NACELLE HEAT FAILED B UO2R O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 19 35LH 413 HEAT INTERMITTENTLY COMES ON WITH SWITCH OFF ON LT NACELLE. REMOVED VALVE, FOUND SOLONOID VALVE SHORTED AND WRONG INLET FITTING INSTALLED. AIR INLET FITTING DOES NOT FIT AIR LINE. 2 M 7 2 4F 4 F A2SW E6WE 2002092400028 20020924 00028 NM 2002 9 24 USA2002F00078 1 20020807 A 7830 WARNING LIGHT BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE THRUST REVERSER FALSE INDICATION A USAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 524AU 23859 724580 THE NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. CAPTAIN FELT THE AIRCRAFT YAW, SO HE SHUT DOWN THE NR 1 ENGIN E. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. TOTAL SINGLE ENGIN E TIME WAS 20 MINUTES. MAINTENANCE FOUND THE NR1 ENGINE THRUST REVERSER STOWED WHEN THE AIRCRAFT ARRIVED AT THE GATE. DETERMINATION WAS MADE TO BE AN INDICATION PROBLEM. THE AIRCRAFT WAS RELEASED ON MEL. MAINTENANCE ACTION PENDING. 2 L 7 2 4F 4 F RT A16WE E2GL 2002092400029 20020924 00029 NM 2002 9 24 USA2002F00081 1 20020808 A 3260 806007 CIRCUIT CARD BOEING 737 737401 1384701 NM GE CFM56 CFM56* 13802 NE MLG FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 407US 23877 ON CLIMB OUT, CREW REPORTED THE LT MAIN LANDING GEAR RED AND GREEN LIGHTS ILLUMINATED WHEN GEAR WAS RETRACTED, CYCLED GE AR WITH SAME RESULTS. WHEN GEAR WAS EXTENDED, INDICATION WAS NORMAL. FLT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINT REMOVED AND REPLACED LOGIC CARDS M986 AND M988 AND LUBRICATED THE LANDING G EAR ASSEMBLY. PERFORMED OPER CHECK OF MLG IN ASSOC WITH MM WITH HYDRAULIC MULE AND AIRCRAFT HYDRAULIC SYSTEM. OPERATIO NAL CHECK NORMAL ON GROUND. PROBLEM REPEATED, ON CLIMB OUT, THE LT MLG RED AND GREEN LIGHTS ILLUM UPON GEAR RETRACTION. MAIN REMOVED AND REPLACED LOGIC CARD M987 (DOWN AND LOCKED). OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002092400030 20020924 00030 NM 2002 9 24 USA2002F00082 1 20020815 A 3350 71070201 BATTERY BOEING 767 767201 1385125 NM SLIDE LIGHTS DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 648US 38609 23900 DURING THE ANNUAL SLIDE OPERATIONAL DEPLOYMENT CHECK FOR THE R3 DOOR, THE SLIDE MOUNTED EMERGENCY LIGHTS DID NOT ILLUMIN ATE. MAINTENANCE REPLACED THE SLIDE. THE EMERGENCY LIGHT BATTERY WAS FOUND TO BE DISCHARGED. TWO MORE SLIDES OF THIS POSITION WILL BE DEPLOYED. 2 L 7 2 4F RT A1NM 2002092400031 20020924 00031 NM 2002 9 24 USA2002F00083 1 20020821 A 2150 11502501 SENSOR BOEING 737 7374B7 1384702 NM A/C PACK TEMP FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 442US 24841 ON CLIMB OUT, ENROUTE, THE AIRCRAFT WOULD NOT PRESSURIZE. THE RT PACK PRESSURE INDICATED ZERO AND THE LT PACK TRIP LIGH T ILLUMINATED AND TRIPPED TWICE AFTER RESET. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENC Y WAS DECLARED. MAINTENANCE FOUND THE LT PACK TEMPERATURE SENSOR BAD. REMOVED AND REPLACED LT PACK TEMPERATURE SENSOR. ALSO, REPLACED THE P5-10 AIR CONDITIONING PANEL DUE TO LT PACK SWITCH INOPERATIVE. OPERATIONAL CHECK GOOD. FOUND RT ENGINE BLEED AIR REGULATOR INOPERATIVE. REMOVED AND REPLACED RT ENGINE BLEED AIR REGULATOR ALSO, REMOVED AND REPLACED R T BLEED AIR CIRCUIT BREAKER FOR TRIPPING. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002092400032 20020924 00032 NM 2002 9 24 USA2002F00084 1 20020826 A 3260 CIRCUIT BREAKER BOEING 737 7373B7 1384580 NM GROUND RELAY TRIPPED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 DURING APPROACH, AFTER GEAR EXTENSION, CREW RECEIVED TWO INDICATIONS THAT THE NOSE LANDING GEAR WAS NOT DOWN. CREW DECL ARED AN EMERGENCY AND ACCOMPLISHED A FLYBY THE TOWER. TOWER CONFIRMED THAT ALL GEAR WERE DOWN. AFTER FOLLOWING QUICK R EFERENCE HANDBOOK PROCEDURES, NORMAL GEAR INDICATIONS ILLUMINATED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. CREW FOUND THE AIR/GROUND RELAY AND LIGHTS CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER AND RECEIVED NORMAL GEAR INDICATIONS. MA INTENANCE CHECKED LANDING GEAR INDICATION SYSTEM. SYSTEM CHECKS NORMAL. (FIRST OFFICERS SEAT BELT HARNESS SUSPECTED IN TRIPPING BREAKER). 2 L 7 2 4F RT A16WE 2002092400033 20020924 00033 EU 2002 9 24 USA2002F00085 1 20020612 A 2820 3C93012 CHECK VALVE AIRBUS A319 A319112 3930323 EU FUEL SYSTEM RUPTURED A USAA A UNSCHED LANDING K P FLUID LOSS NO WARNING INDICATION CL CLIMB 1 EA 19 717UW 1069 ENROUTE, AFTER TAKEOFF, THE TOWER NOTIFIED THE CREW THAT FUEL WAS STREAMING FROM THE RT WING. CREW OBSERVED THAT THE LT WING FUEL QUANTITY WAS 400 LBS LESS THAN THE RT WING. AFTER CRUISE ALTITUDE WAS REACHED, THE FUEL QUANTITY WAS STABILI ZED. FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RT HAND BOOST PUMP CANNISTER CHECK VALVES, AND CLEANED THE RT HAND BOOST PUMP SUCTION VALVE CLACKER AND RT HAND SCAVENGE JET PUMP (69QM). OPERATIONALLY AN D LEAK CHECKED, OK. 2 L 7 2 4F RT A28NM 2002092400034 20020924 00034 EU 2002 9 24 USA2002F00086 1 20020107 A 3222 D65519 SHOCK ABSORBER AIRBUS 320 A320214 3930316 EU NLG DISTORTED A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 19 107US 7751 1052 ENROUTE, RECEIVED AN ECAM WARNING FOR SHOCK ABSORBER FAULT. AS A RESULT, THE LANDING GEAR HANDLE WOULD NOT GO INTO THE UP POSITION AND THE LANDING GEAR WOULD NOT RETRACT. THE FLIGHT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLA CED THE NOSE LANDING GEAR ASSEMBLY. OPERATIONALLY CHECKED OK. 2 L 7 2 4F RT A28NM 2002092400035 20020924 00035 NM 2002 9 24 USA2002F00087 1 20020828 A 2197 WIRE BOEING 737 7374B7 1384702 NM CONTROL PANEL FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 426US 24548 ON CLIMB OUT, AIRCRAFT ENCOUNTERED A PRESSURIZATION PROBLEM AT 6,000 FT. CREW STOPPED THE CLIMB AT 7,000 FT AND RETURNE D TO FIELD AT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND NO OXYGEN MASKS WERE DEPL OYED. MAINTENANCE REPAIRED WIRING IN BACK OF THE OVERHEAD PRESSURIZATION PANEL. ALSO, REMOVED AND REPLACED AFT OUTFLOW VALVE AND P5-6 OVERHEAD PRESSURIZATION PANEL FOR TROUBLESHOOTING PURPOSES. ACCOMPLISHED OPERATIONAL TEST OF PRESSURIZA TION SYSTEM PER MM. OPERATIONAL TEST GOOD. 2 L 7 2 4F RT A16WE 2002092400036 20020924 00036 NM 2002 9 24 USA2002F00088 1 20020829 A 5610 5553K172 HOSE BOEING 737 7374B7 1384702 NM WATER DRAIN OUT OF POSITION A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 785AU 25024 ON CLIMB OUT, A HIGH PITCHED SQUEAL DEVELOPED FROM THE FIRST OFFICERS SLIDING WINDOW. DECISION WAS MADE BY CREW TO RETU RN TO FIELD BECAUSE NOISE WAS INTERFERING WITH RADIO COMMUNICATIONS TO ATC AND EACH OTHER. FLIGHT LANDED WITHOUT FURTHE R INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE WINDSHIELD WATER DRAIN HOSE STUCK IN THE FIRST OFFICERS S LIDING WINDOW JAMB. REPOSITIONED DRAIN HOSE AND SECURED OUT OF WAY. PRESSURIZED AIRCRAFT. LEAK CHECK GOOD. NO FURTHE R DEFECTS NOTED. 2 L 7 2 4F RT A16WE 2002092400037 20020924 00037 2002 9 24 USAASA02063 4 20020715 A 3140 350E05320303 COMPUTER AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FLT WARNING MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 119US 900 1268 DURING CRUISE, THE CREW RECEIVED AN ECAM MESSAGE MESSAGE FOR A NR 1 ENGINE FIRE, HOWEVER NO MASTER WARNING OR BELLS OPER ATED. SHORLY AFTERWARDS, RECEIVED ECAM MESSAGES FOR DUAL ENGINE FLAMEOUT AND AVIONICS SMOKE. ALL OTHER INDICATIONS WER E NORMAL, BUT A SMOKE ODOR WAS PRESENT. FOLLOWED ECAM PROCEDURES FOR AVIONICS SMOKE AND RAT DEPLOYED FLT DIVERTED TO IN D AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 FLIGHT WARNING COMPUTER. OPERATIONALLY CHECKS, OK. ALSO STOWED THE RAT. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E2GL 2002092400038 20020924 00038 EU 2002 9 24 USAASA02067 1 20020808 A 5210 DOOR AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE MAIN PAX STUCK A USAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 19 757UW 1342 AT THE GATE, THE 2L DOOR WOULD NOT OPEN. MAINTENANCE FOUND THE DOOR ASSIST ABOTTLE DISCHARGED ON CLOSED DOOR PRELOADING ON CLOSED DOOR PRELOADING DOOR MECHANISM. THE PRESSURE WAS RELIEVED AND THE DOOR WAS OPS CHECKED,OK. THE DOOR ASSIST BOTTLE WAS THEN SERVICED. 2 L 7 2 4F 4 F RT A28NM E2GL 2002092400039 20020924 00039 2002 9 24 USAASA02071 4 20020811 A 2565 LATCH AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE GIRT BAR FOD A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 701UW 0890 ENROUTE, THE 2L SLIDE DISARMS IN FLIGHT. MAINTENANCE CLEANED FOREIGN OBJECT DAMAGE FROM GIRT BAR LATCHES. OPERATIONALL Y CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E2GL 2002092400040 20020924 00040 NM 2002 9 24 USAASB02153 1 20020816 A 3350 3114981 LIGHT BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE EXTERIOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 23313 MAINTENANCE FOUND THE EXTERIOR EMERGENCY EXIT LIGHT, AT THE AFT ENTRY DOOR, INOPERATIVE. REMOVED AND REPLACED THE REFLE CTOR ASSEMBLY, WHICH WAS FOUND CORRODED, AT THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002092400041 20020924 00041 WP 2002 9 24 WRLA200219 1 20020808 A 5330 SKIN DOUG DC10 DC1030 3023501 WP GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 352WL 47838 FOUND CORROSION UNDER PRIMARY PITOT STATIC PORT PLATE LEFT SIDE OF AIRCRAFT THAT EXCEEDED STRUCTURAL REPAIR MANUAL LIMIT S BETWEEN FUSELAGE STATION 859 AND 879, BETWEEN LONGERONS 39LH AND 40LH. TRIMMED OUT DAMAGED FROM CORROSION. FABRICATE D AND INSTALLED FILLER AND DOUBLER IAW EA. REPAIRED CORROSION. 2 L 7 3 4F 4 F A22WE E2GL 2002092400042 20020924 00042 CE 2002 9 24 WVE2002F00017 1 20020819 A 3600 DUCT LEAR 60 60LEAR 5170707 CE PWA 305 PW305 NE RT ENGINE DAMAGED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 229FX 137 PCECA0109 DURING 300 HOUR INSPECTION, THE UPPER COWLING WAS REMOVED FOR MINOR INSPECTION. DAMAGE WAS NOTED TO THE UPPER BYPASS DU CT. DURING FURTHER INVESTIGATION, DAMAGE WAS ALSO NOTED ON THE RIGHT AND LEFT INNER CORE COWLS. TO BE EVALUATED BY MFG . 2 L 7 2 4F 4 F RT A10CE E35NE 2002092400043 20020924 00043 WP 2002 9 24 WVE2002F00018 2 20020819 A 7310 4573100000V500 LINE LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE731* 01518 WP FUEL SYSTEM CHAFED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 425FX 147 DURING 1200 HOUR INSPECTION, THE ENGINE FUEL FEED LINE WAS FOUND CHAFING ON THE FORWARD FIREWALL AFT OF THE INLET ASSEMB LY. INSTALLED ADDITIONAL ADEL CLAMP. NO DAMAGE OCCURRED TO FUEL LINE. LINE IMPROPERLY SECURED. (2002B1363) 2 L 7 2 4F 4 F RT T00008WI E6WE 2002092400044 20020924 00044 EU 2002 9 24 Y2PA02018 1 20020814 A 7920 5002T26P11 LINE AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D 30010 NE NR 1 ENGINE OIL FAILED A Y2PA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 23 830AA 055 304H588 UPON DESCENT INTO DRT THE NR 1 ENGINE LOST OIL PRESSURE. THE ABNORMAL CHECKLIST FOR LOSS OF OIL PRESSURE WAS EXECUTED A ND THE CREW SHUT DOWN THE LEFT ENGINE. CREW DECLARED AN EMERGENCY AND CONTINUED APPROACH. AIRCRAFT SUBSEQUENTLY LANDED WITHOUT FURTHER INCIDENT AND CREW TERMINATED EMERGENCY WITH DRT. C/A: AFTER LANDING THE CREW CHECKED THE LEFT ENGINE COWLING AND FOUND A LARGE AMOUNT OF OIL. MAINTENANCE WAS DISPATCHED TO RECTIFY PROBLEM. IT WAS DISCOVERED THAT AN OIL PRESSURE LINE HAD FAILED. OIL PRESSURE LINE WAS REPLACED. ENGINE WAS RUNAND OPERATIONAL AND LEAK CHECK WAS GOOD. NO D EFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A7EU E7EA 2002092400045 20020924 00045 CE 2002 9 24 ZOX2002F00000 1 20020825 A 2612 24409015 WARNING SYSTEM BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE ACTIVATED E Z0XA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 07 168AZ UE68 THE RT ENGINE HAD A FIRE WARNING INDICATION. DURING TAXI TO TERMINAL. THE PILOT ACTED IAW PROCEDURES AND SHUT THE ENGI NE DOWN. MAINTENANCE IS STILL TROUBLESHOOTING THE FIRE LOOP SYSTEM. 2 L 7 2 4T 4 T RT A24CE E26NE 2002092400046 20020924 00046 SO 2002 9 24 VJ32002F00069 1 20020913 A 2560 110744733 HARNESS PIPER PA28 PA28181 7102807 SO LYC O360 O360A4M 41514 EA COCKPIT FAILED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 4130W 2843204 DURING FLIGHT AND INSPECTION ON GROUND SHOULDER HARNESS KEEPS LOCKING UP BY THE INERTIAL REEL NO RECOMMENDATION AT THIS TIME. 1 L 7 1 3O 3 O 2A13 E286 2002092400047 20020924 00047 2002 9 24 VJ32002F00070 4 20020913 A 3421 102007403 INDICATOR PIPER PA28 PA28180 7102808 SO LYC O360 O360A4M 41514 EA GYRO HORIZON FAILED B VJ3R O OTHER O OTHER NR NOT REPORTED 1 WP 07 4130W 2843204 DURING FLIGHT INDICATOR SHOWS 10 DEGREE BANK PLUS 50 DEGREE PITCH DURING LEVEL FLIGHT. NO RECOMMENDATION AT THIS TIME. 1 L 7 1 3O 3 O 2A13 E286 2002092400048 20020924 00048 CE 2002 9 24 VJ32002F00071 1 20020903 A 3610 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO DRY AIR FAILED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 5599P 583 CE1344 825760R DURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT U P AND AIR PRESSURE STILL LOW AT HIGHER RPM. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP. 1 L 7 1 3O 3 O 3A15 E5CE 2002092400049 20020924 00049 CE 2002 9 24 VJ32002F00072 1 20020903 A 3610 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO DRY AIR FAILED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 1569A 379 CE1328 DURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT U P AND AIR PRESSURE STILL LOW AT HIGHER RPM. PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP. RECOMMENDAT ION FOR CORRECTIVE ACTION IS MAKE THIS A LIFE LIMIT PART AND CHANGE AT 500 HOURS. 1 L 7 1 3O 3 O 3A15 E5CE 2002092400050 20020924 00050 SO 2002 9 24 C2XA02CL186 1 20020922 A 3350 1317 LAMP EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 24517 145332 CLE FLIGHT#3309 THE CREW REPORTED ROW 9 OVERHEAD EMERGENCY EXIT LIGHT WAS INOPERATIVE.MAINTENANCE INSPECTED AND REPLACED THE LAMPS.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002092400051 20020924 00051 NM 2002 9 24 200200274 1 20020916 A 5330 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 477EV 20784 FUSELAGE BILGE SKIN REPAIR, BS 2160-2180, STR 48L TO 48R. THE CORROSION HAS BEEN REMOVED BY TRIMMING THE FUSELAGE SKIN. THE REPAIR IS APPROVED AS A TIME LIMITED REPAIR FOR A MAXIMUM OF 24 MONTHS AFTER 04 SEP 2002, PER ECRA 477-53-067-2. 2 L 7 4 4F RT A20WE 2002092400052 20020924 00052 NM 2002 9 24 200200275 1 20020916 A 5315 141U004845 FLOORBEAM BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 477EV 20784 BS 360 UPPER DECK FLOORBEAM EXISTING REPAIR STRAP, UPPER FWD FLANGE, LBL 41.7 - 65.2 DAMAGED. A FWD REPAIR ANGLE AND TW O AFT REPAIR ANGLES ALL INSTALLED ON AN UNDERSIDE OF THE BS 360 UPPER DECK FLOORBEAM CHORD. 2 L 7 4 4F RT A20WE 2002092400053 20020924 00053 NM 2002 9 24 200200276 1 20020916 A 5315 FLOORBEAM BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 477EV 20784 BS 340 UPPER DECK FLOOR BEAM - UPPER CHORD - OVERSIZED FASTENER HOLES AT LT FRAME ATTACHMENT. TWO FASTENER HOLES WERE O VERSIZED BEYOND THE LIMITS ALSO THE EDGE MARGIN IN THE FASTENER HOLE COMMON TO THE SUBJECT FLOORBEAM UPPER CHORD AND THE BS 340 FRAME INNER CHORD HAS AN EDGE MARGIN CONDITION LESS THAN THE 1.7D MINIMUM. INSTALLED OVERSIZED FASTENERS AND FA BRICATED AND INSTALLED A REPAIR STRAP ON THE BS 340 FRAME INNER CHORD PER ECRA 477-53-069-2. 2 L 7 4 4F RT A20WE 2002092400054 20020924 00054 NM 2002 9 24 200200277 1 20020917 A 5330 65B041093 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 477EV 20784 FUSELAGE SKIN AT BS 560, STR 37R DAMAGED. A TRIPLER AND DOUBLER INSTALLED PER SRM GUIDELINES. 2 L 7 4 4F RT A20WE 2002092400055 20020924 00055 NE 2002 9 24 CALA0200451 2 20020906 A 7314 3017790050 PUMP BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FAILED A CALA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 SW 09 69333 21382 23571 721272 THE NR 2 ENGINE FLAMED OUT WHILE ON DESCENT AT 10,000 FEET. AN ENGINE RESTART WAS ATTEMPTED, BUT WAS UNSUCCESSFUL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FUEL PUMP AND MEC. LEAK AND OPERATIONAL CHECKS WERE GOOD. IN ADDITION, THE SPAR VALVE WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002092400056 20020924 00056 NM 2002 9 24 CALA0200452 1 20020909 A 3150 69782143 MODULE BOEING 737 737824 13844BZ NM COCKPIT FAULTY A CALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 27205 3045 30577 THE MACH WARNING, LANDING GEAR WARNING HORN, AND FIRE WARNING BELLS ACTIVATED ON CLIMBOUT FROM LAS AT APPROXIMATELY 25,0 00 FEET. THE ASSOCIATED CIRCUIT BREAKERS WERE PULLED AND THE WARNINGS SILENCED. THE AIRCRAFT WAS DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AURAL WARNING MODULE AT FAULT. THE AURAL WARNING MODULE WAS REMOVED AND REPLACED IAW MM 31-51-00 AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2002092400057 20020924 00057 WP 2002 9 24 CALA0200454 1 20020907 A 5350 CONTROL CABLE DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 49488 THE EXTERIOR TAIL CONE RELEASE HANDLE PULLED LOW AT 10 POUNDS. THE TAIL CONE CABLE TENSION WAS ADJUSTED AND THE HANDLE CLIPS WERE REPLACED. 2 L 7 2 4F A6WE 2002092400058 20020924 00058 NM 2002 9 24 CALA0200456 1 20020910 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND LT DIAGONAL FLOOR SUPPORT CORRODED AT STA 1006 TO 1016. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002092400059 20020924 00059 NM 2002 9 24 CALA0200457 1 20020910 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND RT DIAGONAL FLOOR SUPPORT CORRODED AT STA 1006-1016. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SR M 51-40-02. 2 L 7 2 4F RT A16WE 2003032800057 20030328 00057 NE 2003 3 28 CALA0200464 2 20020915 A 7200 CONTROL UNIT BOEING 757 757224 1384958 NM RROYCE RB211 RB211535E4 54555 NE NR 1 ENGINE FAILED A CALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 SW 09 19136 29285 31628 THE AUTO THROTTLE DISCONNECTED FOLLOWED BY EEC/LIMITER AUTO DISCONNECT WHILE AT CRUISE AFTER LEAVING LIS. THERE WAS AN I NSTANT EGT RISE TO 961 WITH REPORTS OF SURGE/STALL AND FLAME FROM THE EXHAUST. THE THROTTLE WAS RETARDED TO IDLE AND ALL RETURNED TO NORMAL INCLUDING EGT. WHILE RETURNING TO LIS ON APPROACH AT 4K THE CREW EXPERIENCED SURGE, EGT RISE, AND EN GINE AUTO SHUTDOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. A NR 1 ENGINE CHANGE IS IN PROGRESS. ENGINEERING CONCLUDED THA T THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO FAILURE OF A POWER CONDITIONING CONTROL UNIT(PCCU). 2 L 7 2 4F 4 F RT A2NM E12EU 2002092400063 20020924 00063 NM 2002 9 24 CALA0200468 1 20020919 A 5311 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND LEFT AND RIGHT MAIN BS 616 FRAME INNER CHORDS CRACKED BELOW MAIN CABIN FLOOR. THE CRACKS WERE 1 INCH E ACH. THE CRACKED AREAS WERE CUT OUT AND FILLERS AND STIFFENERS WERE INSTALLED IAW ECRA 5311-01134. 2 L 7 2 4F RT A16WE 2002092400065 20020924 00065 NM 2002 9 24 F3LA200200257 1 20020905 A 5753 6546430190 SKIN BOEING 737 73736Q 1384409 NM T/E FLAP DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 307FL 3196 28760 DURING C-5 CHECK, INSPECTION REPORTED 3 CREASES ON TOP SURFACE OF RIGHT INBOARD FOREFLAP. REMOVED, REPAIRED AND REINSTA LLED RT INBOARD FOREFLAP PER MM 27-51-07, SRM 57-53-02 AND SRM 51-70-10. 2 L 7 2 4F RT A16WE 2002092400066 20020924 00066 NM 2002 9 24 F3LA200200258 1 20020910 A 2120 ODOR BOEING 737 7372Y5 1384554 NM CABIN DETECTED A F3LA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 03 118RW 23040 AIR TURNBACK. FLIGHT CREW REPORTED FWD LAVATORY SMOKE ALARM ACTIVATED WHILE CLIMBING THROUGH 8000 FT. PASSENGERS IN RO W 2 NOTED DISTINCT SMELL/ODOR OR SMOKE (OVEN/ELECTRICAL) DURING FLIGHT. NR 2 PACK TRIP OFF LIGHT ILLUMINATED IMMEDIATEL Y BEFORE SMOKE ALARM ACTIVATED. PERFORMED OPERATIONAL CHECK OF LAVATORY SMOKE DETECTOR SYSTEM, WITH NO DISCREPANCIES NO TED. PERFORMED OPERATIONAL CHECK OF FWD GALLEY OVEN FOR 30 MIN ON HIGH, WITH NO DISCREPANCIES NOTED. PERFORMED OPERATI ONAL CHECK OF RT PACK SYSTEM FOR SEVERAL HOURS, WITH NO DISCREPANCIES NOTED. REPLACED NR 2 PACK WATER SEPARATOR BAG AS PRECAUTIONARY. 2 L 7 2 4U RT A16WE 2002092400067 20020924 00067 NM 2002 9 24 F3LA200200260 1 20020913 A 5753 ROLLER BOEING 737 737317 138447P NM T/E FLAP OUT OF RIG A F3LA K NONE E VIBRATION/BUFFET AP APPROACH 1 NM 03 EICHH 65 23177 FLIGHT CREW REPORTED A LOUD VIBRATION WAS HEARD UPON FLAP EXTENSION ON APPROACH THAT APPEARED TO BE COMING FROM RT SIDE OF AIRCRAFT. PERFORMED INSPECTION PER MM 05-51-67, NO ABNORMALITIES OR DISCREPANCIES NOTED. PERFORMED TEST FLIGHT. TE ST FLIGHT UNSATISFACTORY DUE TO VIBRATION AT FLAP SETTINGS 10-30. FOUND RT INBOARD AFT FLAP DEAD WEIGHT ROLLERS OUT OF RIG. ADJUSTED DEAD WEIGHT ROLLERS PER MM 27-51-11 AND FLAP OPS CHECKED GOOD. PERFORMED ANOTHER TEST FLIGHT, WITH NO DI SCREPANCIES NOTED. 2 L 7 2 4F RT A16WE 2002092400069 20020924 00069 NM 2002 9 24 F3LA200200262 1 20020913 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C4 CHECK, INSPECTION REPORTED ELONGATED HOLE ON INTERCOSTAL AT BS 500A-500B, STR 26. FABRICATED AND INSTALLED RE PLACEMENT INTERCOSTAL PER SRM 51-10-02, 51-50-02 AND SOPM 20-41-01. 2 L 7 2 4F RT A16WE 2002092400071 20020924 00071 2002 9 24 MALA020569 4 20020918 A 3425 6226190113 COMPUTER SAAB SF340 340B 7860101 EU NR 2 MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 363PX 340B260 DURING FLIGHT 3076, NR 2 AHRS COMPUTER DROPPED OFF LINE. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS COMPUTER. 2 L 7 2 4T RT A52EU 2002092400072 20020924 00072 EU 2002 9 24 MALA020570 1 20020919 A 3010 EJECTOR VALVE SAAB SF340 SF340A 7850100 EU DE-ICE SYSTEM FAULTY A MALA D RETURN TO BLOCK O OTHER NR NOT REPORTED 1 GL 15 48XJ DE-ICE TEST FAILED ON FLIGHT 3027, STAB INBOARD & OUTBOARD LIGHTS FAIL TO ILLUMINATE. A/C RETURNED TO GATE. MAINTENANC E REPLACED DE-ICE EJECTOR VALVE IAW CHAP 30. 2 L 7 2 4T RT A52EU 2002092400073 20020924 00073 NM 2002 9 24 QXEA0201323 1 20020828 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND INBOARD SEAT TRACK X212 TO X226 OUTBOARD FLOORBOARD FLANGE HAS CORROSION IN SIXTEEN SPOTS. 2 H 7 2 4T RT A13NM 2002092400074 20020924 00074 NM 2002 9 24 QXEA0201324 1 20020826 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM NR 2 NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - NR 2 NACELLE EXHAUST DECK/SKIN IS CHAFED ON UNDERSIDE BY OIL DRAIN LINE. REPAIRED IAW RD 8-54-097. 2 H 7 2 4T RT A13NM 2002092400075 20020924 00075 NM 2002 9 24 QXEA0201326 1 20020826 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - GOUGE IN SKIN UNDER RIGHT HAND WINDSHIELD WIPER ARM. REPAIRED IAW DHC-8-200 SRM 51-20-26, SRM 51-20-16 AND SRM 51 -20-11. 2 H 7 2 4T RT A13NM 2002092400076 20020924 00076 NM 2002 9 24 QXEA0201327 1 20020826 A 5411 FRAME DHAV DHC8 DHC8202 2809007 NM LT NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - INBOARD VERTICAL FRAME AT AFT SIDE OF LEFT HAND ENGINE NACELLE BULKHEAD HAS A ELONGATED FASTENER HOLE AT TOP WHERE STIFFENER ATTACHES. REPAIRED IAW HORIZON AIR EA 2-54-153. 2 H 7 2 4T RT A13NM 2002092400077 20020924 00077 NM 2002 9 24 QXEA0201329 1 20020827 A 5720 ANGLE DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - LEFT HAND WING FRONT SPAR CONNECTION ANGLE FROM NACELLE TO WING SPAR HAS A CRACK IN CONNECTION ANGLE AT TOP AFT RI VET. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002092400078 20020924 00078 NM 2002 9 24 QXEA0201330 1 20020827 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - THERE IS A OUTWARD DENT IN THE BELLY SKIN APPROXIMATELY 6 INCHES AFT OF STATION 467, ABOUT 6 INCHES OUTBOARD OF DM E ANTENNA. REPAIRED IAW DHC-8 SRM 51-20-36, SRM 51-20-26, PARAGRAPH 5A AND RD 8-53-2181. 2 H 7 2 4T RT A13NM 2002092400079 20020924 00079 NM 2002 9 24 QXEA0201331 1 20020902 A 3230 LANDING GEAR DHAV DHC8 DHC8202 2809007 NM NLG & MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 374PH 528 SEA - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF, THE GEAR FAILED TO RETRACT. MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED EXTENSION AND RETRACTION OPERATIONAL AND FUNCTIONAL CHECKS IAW DHC MM 32-30-00-720-801. NO PARTS WERE CHANGE D AND NO DEFECTS WERE NOTED. COULD NOT DUPLICATE. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092400080 20020924 00080 NM 2002 9 24 200200278 1 20020917 A 5330 65B070174 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 477EV 20784 REPAIR OF EXISTING REPAIR AT BS 2320, STR 22R. THE EXISTING REPAIR WAS REMOVED FROM THE AIRCRAFT AND DISCARDED, AND THE EXISTING DENT WAS TRIMMED AWAY PER B747 GUIDELINES. THE FUSELAGE SKIN TRIM OUT AND EXISTING FASTENER HOLES COMMON TO T HE REPAIR AREA WERE HFEC INSPECTED TO ENSURE A CRACK FREE CONDITION AND THE DOUBLER AND TRIPLER WERE INSTALLED TO RESTOR E THE ORIGINAL SKIN PANEL. 2 L 7 4 4F RT A20WE 2002092400081 20020924 00081 NM 2002 9 24 200200279 1 20020917 A 5730 65B167634 SKIN PANEL BOEING 747 747SR46 1384816 NM RT WING CORRODED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 477EV 20784 RIGHT WING - CORROSION REPAIR AT FORWARD EDGE OF LOWER FORWARD SKIN PANEL, WS 1390-1498. THE CORROSION WAS IN THE UPPER SURFACE OF THE SUBJECT SKIN, AND IN THE LOWER SURFACE OF THE RT WING FORWARD SPAR LOWER CHORD. THE CORROSION WAS REMOV ED BY BLENDING PER B747 SRM 51-10-01. FABRICATED AND INSTALLED SHIMS AND TO ACCOMPLISH SRM REPAIRS AT ALL THREE CUTOUTS IN THE FORWARD EDGE OF THE SUBJECT WING SKIN, PER ECRA 477-57-078-2. 2 L 7 4 4F RT A20WE 2002092400082 20020924 00082 NM 2002 9 24 200200280 1 20020917 A 5311 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE GOUGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 477EV 20784 BS 1418 RT FRAME INNER CHORD SPLICE CHANNEL - GOUGE AT WL 238. A GOUGE WAS FOUND IN THE INNER CHORD SPLICE CHANNEL OF T HE RT BS 1416 FUSELAGE FRAME, BETWEEN STR - 20R AND 22R AT WL 238. THIS PROVIDES INSTRUCTIONS TO BLEND THE FRAME TO REM OVE THE DAMAGE, FLAP PEEN THE BLENDED AREA, AND INSTALL A REPAIR ANGLE, PER ECRA 477-53-079-2. 2 L 7 4 4F RT A20WE 2002092400083 20020924 00083 NM 2002 9 24 200200281 1 20020917 A 5311 65B01708505 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 477EV 20784 BS 260 FRAME - REPAIR FOR CRACK IN OUTER RADIUS ABOVE LT STR - 14D. THE AIRCRAFT CRACKS WERE FOUND IN THE OUTBOARD FLAN GE OF THE SUBJECT FRAME. THE DAMAGE IS COMMON TO ZONE 6, ZONE 6 HAS NOT BEEN ACCOMPLISHED ON THE AIRCRAFT. THIS PROVID ES INSTRUCTIONS TO FABRICATE AND INSTALL A REPAIR DOUBLER, PER ECRA 477-53-081-2. 2 L 7 4 4F RT A20WE 2002092400084 20020924 00084 NM 2002 9 24 200200282 1 20020917 A 5320 DOUBLER BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 477EV 20784 REPAIR OF OVERSIZED FASTENER HOLES COMMON TO FASTENER HOLES COMMON TO THE BS 747-53-2181 L1 AND R1 DOOR BOOMERANG DOUBLE RS. THE R1 DOUBLER IS BEING REMOVED AND REPLACED PER BSB 747-553-2181. AT THE OVERSIZED FASTENER HOLES COMMON TO THE L 1 DOUBLER, OVERSIZE FASTENERS ARE BEING INSTALLED PER BSB 747-53-2181, PER ECRA 477-71-087-2. 2 L 7 4 4F RT A20WE 2002092400085 20020924 00085 NM 2002 9 24 200200283 1 20020919 A 5315 65B1033947 FLOORBEAM BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED B EIAA K NONE O OTHER IN INSP/MAINT 1 WP 07 477EV 20784 BS 320 MAIN DECK FLOORBEAM - CRACK IN WEB AT LBL 39 AND CRACK IN LOWER CHORD AT LBL 37.5. THE CRACKED WEB IS BEING REPA IRED BY LOCALLY TRIMMING AWAY THE CRACK, HFEC INSPECTING THE EXISTING FASTENER HOLES TO ENSURE A CRACK FREE CONDITION, A ND INSTALLING A REPAIR DOUBLER. THE CRACKED FLOORBEAM LOWER CHORD IS BEING REPAIRED BY CUTTING THE FLOORBEAM LOWER CHO RD LBL 17, DISCARDING THE SECTION OF FLOORBEAM FROM THE LT SIDE OF BODY, AND SPLICING IN A NEW SECTION OF FLOORBEAM LOWE R CHORD EXTRUDED ANGLES PER ECRA 477-53-085-2 REV A. 2 L 7 4 4F RT A20WE 2002092400086 20020924 00086 SO 2002 9 24 SWIA200211202 1 20020905 A 3297 WIRE HARNESS EMB 120 EMB120RT 3260202 SO RT MLG FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 1105G 120105 ON DEPARTURE FROM SFO, LANDING GEAR WOULD NOT RETRACT. ALL GREEN REMAINED ILLUMINATED & ALL REDS EXCEPT RIGHT A WERE IL LUMINATED W/GEAR HANDLE IN UP POSITION. CYCLED GEAR - SAME RESULTS. RETURNED TO SFO. PERFORMED GEAR SWING. OPS CHECK ED GOOD BUT NOTICED RIGHT MAIN RED -A- LIGHT FLICKERS. SWAPPED RT MAIN UPLOCK A & B CONNECTORS PER SNL 120-32-0015 AND DEFERRED RED -B- SYS. SWAPPED HARNESSES BACK TO ORIGINAL POSITION, RIGHT UPLOCK AND REPLACED -A- HARNESS WITH A SERVICE ABLE UNIT. SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002092400087 20020924 00087 SO 2002 9 24 SWIA200211203 1 20020906 A 3010 BOOT EMB 120 EMB120ER 3260203 SO LT WING FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 209SW 120269 LEADING EDGE MIDDLE, RIGHT & LEFT WING BOOTS FAILED. RETURNED TO SLC. REMOVED AND REPLACED LEFT MIDDLE DEICE BOOT IAW 30-10-00. OPS & LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2002092400088 20020924 00088 SO 2002 9 24 SWIA200211204 1 20020908 A 3010 BOOT EMB 120 EMB120ER 3260203 SO DE-ICE SYSTEM FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 197SW 120186 INBOARD LEFT AND RIGHT STAB AND INBOARD LEFT AND RIGHT WING LEADING EDGE DEICERS FAILED IN FLIGHT ON BOTH TIMERS. RETUR NED TO SLC. REMOVED & REPLACED RIGHT WING OUTBOARD DEICE, LEFT OUTBOARD DEICE BOOT & RIGHT HORIZONTAL STAB DEICE BOOT W ITH SERVICEABLE UNIT. OPERATED DEICE BOOT SYSTEM. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002092400089 20020924 00089 EA 2002 9 24 SWIA200211205 1 20020906 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER DIRTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 403SW 7028 RIGHT THRUST REVERSER DEPLOY MSG ON TO ROLL. ABORTED, CLEANED RIGHT THRUST REVERSER MICROSWITCHES, CLEANED & LUBED THRU ST REVERSER TRACKS & ACTUATORS. CYCLES THRUST REVERSER NUMEROUS TIMES WITH NO FAULTS. OPS CHECK GOOD PER MM 78-30-00. 2 L 7 2 4F RT A21EA 2002092400090 20020924 00090 NM 2002 9 24 SWAA022190 1 20020922 A 2130 BACC10BN500LR DUCT CLAMP BOEING 737 7373Q8 1384670 NM MLG W/W LEAKING A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 688SW 23254 DECLARED EMERGENCY, DIVERSION, DURING CLIMB LOST CABIN PRESSURATION, MASKS DEPLOYED. FOUND DUCT AT AFT MLG W/W LEAKING. TIGHTENED CLAMP PER MM. 2 L 7 2 4F RT A16WE 2002092400091 20020924 00091 2002 9 24 SWAA022191 4 20020920 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002092400092 20020924 00092 NM 2002 9 24 SWAA022193 1 20020919 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROWS NR 11 ABC AND NR 14 ABC. SECU RED LENSES PER MM. 2 L 7 2 4F RT A16WE 2002092400093 20020924 00093 2002 9 24 SWAA022194 4 20020919 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM AFT SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002092400094 20020924 00094 NM 2002 9 24 SWAA022197 1 20020919 A 5330 6546529 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, BETWEEN STR 18R AND STR 28R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002092400095 20020924 00095 NM 2002 9 24 SWAA022199 1 20020921 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4L, BS 300 AND BS 420. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002092400096 20020924 00096 NM 2002 9 24 SWAA022201 1 20020922 A 5520 65C2638423A TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED SERVICE CHECK, FOUND LT ELEVATOR TAB CRACKED AT HINGE CUTOUTS. REMOVED AND REPLACED LT ELEVATOR TAB PE R SRM. 2 L 7 2 4F RT A16WE 2002092400097 20020924 00097 EA 2002 9 24 SWIA200211207 1 20020905 A 3010 SENSOR CNDAIR CL600 CL6002B19 1900309 EA WING FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 417SW 7400 ON CLIMBOUT, INTERMITTENT WING OVHT MSG ILLUMINATED. FOLLOWED QRH PROCEDURE. MESSAGE STAYED OUT AT LOWER POWER SETTING S. RETURNED TO SLC. REPLACED SUFFICIENT/OVERHEAT SENSOR IAW MM 30-12-23. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002092400098 20020924 00098 SO 2002 9 24 SWIA200211208 1 20020902 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 218SW 120287 EMERGENCY LIGHTS FROM ROW 9 AND AFT ARE INOP. REPLACED AFT BATTERY PACK FOR EMERGENCY LIGHTS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002092400099 20020924 00099 SO 2002 9 24 SWIA200211209 1 20020904 A 2150 22045404 ACM EMB 120 EMB120ER 3260203 SO A/C BAY MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 562SW 60 60 120336 VENTILATION SYSTEM BLOWING SMOKE INTO CABIN. REMOVED & REPLACED LEFT AND RIGHT ACM, OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002092400100 20020924 00100 EA 2002 9 24 SWIA200211210 1 20020905 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB FAILED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 433SW 7550 STAB CHANNEL NR 1 INOP. REMOVED & REPLACED STAB TRIM ACTUATOR & MOTOR CONTROL UNIT IAW 27-40-00, 27-42-01, 27-42-05. O PS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002092400101 20020924 00101 NE 2002 9 24 SWIA200211211 2 20020909 A 7261 ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RIGHT LEAKING A SWIA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 07 288SW 120316 RIGHT ENGINE SMOKES ON SHUTDOWN. FOUND ENGINE BLOWING OIL OUT FROM FRONT COMPRESSOR. REMOVED AND REPLACED RT ENGINE AS REQUIRED IAW 71-00-00. OPS CHECK GOOD. PACKS NO LONGER SMOKING. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092400102 20020924 00102 SO 2002 9 24 SWIA200211212 1 20020907 A 4950 VALVE EMB 120 EMB120RT 3260202 SO APU MALFUNCTIONED A SWIA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 137H 120137 APU CAUSES SMOKE IN COCKPIT & CABIN. FOUND LCV NOT OPENING CAUSING SMELL TO COME FROM PACKS. REPLACED APU LCV, OPS CHE CK GOOD. 2 L 7 2 4T RT A31SO 2002092400103 20020924 00103 EA 2002 9 24 SWIA200211213 1 20020912 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM BROKEN A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 594SW 7285 RUDDER TRIM INOP, WILL NOT MOVE LEFT OR RIGHT. FOUND WIRE BROKEN OFF OF RUDDER TRIM SWITCH. SOLDERED WIRE BACK ONTO SW ITCH. OPERATED RUDDER TRIM & CHECKED NORMAL. 2 L 7 2 4F RT A21EA 2002092400104 20020924 00104 SO 2002 9 24 SWIA200211214 1 20020910 A 5753 GUIDE EMB 120 EMB120ER 3260203 SO T/E FLAP BENT A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 212SW 120276 RIGHT OUTBOARD FLAP ROLLER GUIDE BENT. INSTALLED NEW BRACKET FOR INBOARD ROLLER, RT OUTBOARD FLAP MOVEABLE CHANNEL. OP ERATED FLAPS. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002092400105 20020924 00105 2002 9 24 SWIA200211215 4 20020911 A 2210 6229968001 DAMPER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AUTOPILOT SYS FAULTY A SWIA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 NM 07 439SW 2141 2141 7578 NR 1 YAW DAMPER WOULD ENGAGE UNTIL RUDDER MOVEMENT WAS INITIATED THEN NR 1 WOULD AGAIN DISCONNECT. REPLACED NR 1 YAW DA MPER LINEAR ACTUATOR IAW MM 22-22-01. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002092400106 20020924 00106 NE 2002 9 24 SWIA200211216 2 20020906 A 7200 BEARING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE OUT OF POSITION A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 442SW 7609 873269 REMOVE LEFT ENGINE FOR 8:00 VG SHAFT AND BEARING SUPPORT REPAIR (LEFT ENGINE VG SHAFT BEARING 8 O'CLOCK POSITION HAS MIG RATED OUT). REMOVED AND REPLACED LT ENGINE IAW MM 71-00-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2002092400107 20020924 00107 EA 2002 9 24 SWIA200211217 1 20020913 A 2741 70607 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 443SW 7638 STAB TRIM CH 2 AND MACH TRIM DISENGAGED CLIMBING OUT OF SLC. RAN QRH PROCEDURE. DID NOT RE-ENGAGE. RETURNED TO SLC. REMOVED AND REPLACED HORIZONTAL STABILIZER TRIM UNIT WITH SERVICEABLE UNIT. OPS CHECK SATISFACTORY IAW CRJ MM 27-41-01. 2 L 7 2 4F RT A21EA 2002092400108 20020924 00108 2002 9 24 SWIA200211218 4 20020907 A 2210 6229968001 DAMPER CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 923SW 7664 NR 2 STATUS MESSAGE DURING FLIGHT. WOULD NOT RESET. SWAPPED FCC CARDS FROM TOP TO BOTTOM. REPLACED NR 2 YAW DAMPER W/ SERVICEABLE UNIT IAW MM 22-22-01. PERFORMED EXTENSIVE FUNCTIONAL CHECKS OF BOTH NR 1 & 2 YAW DAMPER SYSTEMS. OPS CHECK GOOD ON GROUND AT THIS TIME. 2 L 7 2 4F RT A21EA 2002092400109 20020924 00109 SO 2002 9 24 SWIA200211219 1 20020912 A 2752 3430001007 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAP LEAKING A SWIA O OTHER K F FLUID LOSS FLT CONT AFFECTED AP APPROACH 1 NM 07 224SW 6703 6703 120294 ON SHORT FINAL, LOST GREEN HYD FLUID & PSI AFTER EXTENDING THE FLAPS TO 25 DEGREES. REMOVED THE RT FLAP ACTUATOR AND IN STALLED A SERVICEABLE ACTUATOR. SERVICED THE HYD SYSTEM AS NEEDED. OPS CHECK GOOD, LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092400110 20020924 00110 EA 2002 9 24 SWIA200211220 1 20020915 A 2741 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 439SW 7578 WHILE EN ROUTE TO LAS HAD A STAB TRIM RUNAWAY. PERFORMED MEMORY ITEMS FOLLOWED BY QRH. RETURNED TO SLC. REMOVED AND R EPLACED CAPTAIN'S TRIM SWITCH. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002092400111 20020924 00111 2002 9 24 BMAC020013 4 20020901 A 3457 9650686001 CPU BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE331* 01514 WP AVIONICS RACK FALSE INDICATION A B16A K NONE L NO TEST IN INSP/MAINT 1 NE 05 538PA 751 GPWS SYSTEM INOPERATIVE. TERRAIN WON`T SINK AND PULL UP CALLS MADE. AIRCRAFT WAS IN NORMAL TAKEOFF CONFIGURATION IN CLI MB. MADE TURNBACK TO PSM SYSTEM DEFERRED PER MEL. SYSTEM LATER TROUBLESHOT AND REPLACED GPWS CPU SYSTEM TESTS NORMAL O N THE DECK AT THIS TIME. 2 L 7 2 4T 3 T RT A21EU E2WE 2002092400112 20020924 00112 NM 2002 9 24 TSAA0233196 1 20020904 A 3350 861002 BATTERY PACK BOEING 737 737282C 13844AU NM PWA JT8 JT8D* NE CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED OVERWING EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( TSAA 8000.3325 DH) 2 L 7 2 4F 4 F RT A16WE E2EA 2002092400113 20020924 00113 SO 2002 9 24 SWIA200211221 1 20020911 A 2752 3203001005 ACTUATOR EMB 120 EMB120RT 3260202 SO T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 1105G 5944 5944 120105 INBOARD FLAPS CONTROL FAULT FROM 15 DEGREES TO 0 DEGREES WHEN RETRACTING THEM. REPAIRED ENVIRONMENTAL SPLICE AT LEFT I/ B FLAP ACTUATOR CANNON PLUG. INSPECTED WIRING AT CANNON PLUGS AND FCU. FOUND LEFT INBOARD FLAP ACTUATOR BAD. REPLACED LEFT FLAP ACTUATOR (I/B) WITH SERVICEABLE UNIT. CYCLED 10 TIMES. OPS CHECK AND LEAK CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002092400114 20020924 00114 NM 2002 9 24 TSAA0253195 1 20020904 A 5330 6545775 SKIN BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 EA 13 821AL 23155 TRIMMED OUT DAMAGE SKIN AT BS 749 STRINGER 18R. HFEC EDGE OF TRIMMED AREA, NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 2002102900030 20021029 00030 SO 2002 10 29 SWIA200211222 1 20020915 A 2697 WIRE EMB 120 EMB120ER 3260203 SO FIRE WARNING SYS BROKEN A SWIA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 NM 07 582SW 122 122 120350 INTERMITTENT INDICATIONS OF BAGGAGE COMPARTMENT SMOKE/FIRE OCCURRED. COMPLIED WITH MEMORY ITEM & QRH BY ACTUATING FIRE EXTINGUISHERS. REMOVED AND REPLACED BOTH SMOKE DETECTORS IN CARGO BAY IAW MM 26-15-0. REPAIRED BROKEN WIRES W11-5695-2 2 AND W110-5700-22 AT TEST PANEL. INSPECTED CARGO COMPARTMENT SMOKE DETECTORS WIRING HARNESS AND CANNON PLUGS. FOUND N O DEFECTS. PERFORMED CARGO COMPARTMENT FIRE/SMOKE WARNING TEST, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002100900117 20021009 00117 NM 2002 10 9 QXEA0201476 1 20020921 A 2913 570347 PUMP DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE FAILED A QXEA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 09 361PH 10129 10129 516 LWS - THE NR 2 ENGINE HYDRAULIC PUMP FAILED IN FLIGHT. LANDING GEAR WOULD NOT EXTEND NORMALLY, CREW USED ALTERNATE EXTE NSION. CREW PERFORMED THE ABNORMAL PROCEDURES CHECKLIST. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE DRIVEN PUMP. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092400115 20020924 00115 NM 2002 9 24 QXEA0201477 1 20020921 A 3260 860TS09Y00 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 09 410QX 1985 1985 4053 PDX - CREW RETURNED TO FIELD WHEN AFTER TAKE OFF THE RIGHT GEAR DOOR AMBER LIGHT STAYED ON AFTER RETRACTION. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LANDING GEAR CONTROL PANEL. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE RII WAS COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092400116 20020924 00116 SO 2002 9 24 SWIA200211223 1 20020913 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT CRACKED A SWIA D RETURN TO BLOCK C F.O.D. TX TAXI/GRND HDL 1 NM 07 224SW 120294 A 767 POWERED UP ACROSS A RUNWAY IN FRONT OF AIRCRAFT, BLOWING ROCKS AND CRACKING THE LEFT WINDSHIELD. INSTALLED SERVIC EABLE WINDSHIELD ON LT SIDE IAW 56-10-01. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092400117 20020924 00117 EA 2002 9 24 SWIA200211224 1 20020804 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 PAX DOOR LWR SILL VERTICAL FLOOR ANGLE CORRODED. DISCOVERED DURING C-CHECK. FITTED AND INSTALLED NEW ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13. 2 L 7 2 4F 4 F RT A21EA E15NE 2002092400118 20020924 00118 EA 2002 9 24 SWIA200211225 1 20020804 A 1430 RIVET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY EXIT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 ANCHOR NUTS FOR RT OVERWING EMERGENCY EXIT BOTTOM HINGE FITTINGS HAVE CORRODED RIVETS. DISCOVERED DURING C-CHECK. FITT INGS REMOVED FOR ACCESS. RIVETS INSTALLED IAW CRJ SRM 51-42-16. INSTALLED FITTINGS IAW MM 20-21-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2002092400119 20020924 00119 SO 2002 9 24 SWIA200211226 1 20020813 A 5541 RIB EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 207SW 120266 RIB IN RUDDER 1 DAMAGED JUST BELOW GREEN RUDDER ACTUATOR ATTACH POINT. DISCOVERED DURING C-CHECK. REPLACED DAMAGED RIB IAW 120 SRM 51-10-02. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092400120 20020924 00120 SO 2002 9 24 SWIA200211227 1 20020813 A 5754 FRAME EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT WING LE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292UX 120292 RIGHT INBOARD LEADING EDGE INBOARD FRAME CRACKED, MARKED. DISCOVERED DURING C-CHECK. REPLACED RIGHT INBOARD LEADING ED GE FRAME. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092400121 20020924 00121 SO 2002 9 24 SWIA200211228 1 20020917 A 5310 WINDOW POST EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FUSELAGE CRACKED A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 289YV 120289 PILOTS SIDE WINDOW POST CRACKED AT BOTTOM FORWARD CORNER, OVER 1 INCH LONG CRACK EXTENDS THROUGH RIVET. DISCOVERED ON P REFLIGHT INSPECTION. COMPLIED WITH SB 120-53-0072 RII CARD 53, INSTALLATION OF DOUBLER TO POST SKIN. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092400122 20020924 00122 NM 2002 9 24 VNAA0209016 1 20020914 A 2432 DTSP400L BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NR 2 OVERHEATED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 459PS 10611 865 3070 AFTER TAKEOFF, THE CREW RECEIVED A NR 2 MAIN BATTERY OVERHEAT CAS MESSAGE AND RETURNED TO BNA. MAINTENANCE WAS DISPATCH ED, INSPECTED, AND REPLACED THE NR 2 MAIN BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL C HECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002092400123 20020924 00123 NM 2002 9 24 VNAA0209017 1 20020914 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 461PS 3075 DURING TAKEOFF, THE CREW EXPERIENCED A DISPLAY UNIT 5 AND A WEIGHT ON WHEELS 1 FAIL CAS MESSAGE AND ABORTED TAKEOFF. MA INTENANCE INSPECTED AND HAD THE CREW CYCLE THE POWER THEN PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH DORNIER MAINTE NANCE MANUAL 31-00-00. THE OPERATIONAL CHECKS PRODUCED NO DEFICIENCIES AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002092400124 20020924 00124 WP 2002 9 24 MWEA020581 1 20020924 A 5313 5911429159 LONGERON DOUG DC9 DC981 3022081 WP STATION 1361 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 CORROSION ON LONGERON 24 LEFT AT STATION 1361 CORROSION IS ON WASHERS ON RIVETS AND TWO SPOTS ARE ON THE LONGERON BELOW FRAME DOT 100. -- REMOVED LONGERON 24 LEFT, FABRICATED AND DRILLED LONGERON AND SPLICE FITTINGS AND REINSTALLED 8 HI-L OCS FROM EXISTING STIFFENER AND INSTALLED LONGERON AND FITTINGS. 2 L 7 2 4F A6WE 2002092400125 20020924 00125 WP 2002 9 24 MWEA020583 1 20020924 A 5315 991556175 FLOORBEAM DOUG DC9 DC981 3022081 WP STATION 1338 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FLOOR BEAM WEB STATION 1338 LEFT OUTBOARD ENDS HAS CORROSION. -- REMOVED DAMAGED SECTION, FABRICATED AND DRILLED UP FI LLER AND DOUBLER, INSTALLED FILLER AND DOUBLER AND STAIR FITTING. 2 L 7 2 4F A6WE 2002092400126 20020924 00126 WP 2002 9 24 MWEA020584 1 20020924 A 5230 995766437 FORMER DOUG DC9 DC981 3022081 WP BEAM 5 FWD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 MID PIT CARGO DOOR HAS A CRACKED FORMER BELOW BEAM FIVE ON THE FORWARD SIDE. -- LOCATED AND DRILLED AND INSTALLED FORM ER. 2 L 7 2 4F A6WE 2002092400127 20020924 00127 WP 2002 9 24 MWEA020585 1 20020924 A 5521 9918450505 ELEVATOR DOUG DC9 DC981 3022081 WP XE 40 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 RIGHT ELEVATOR SPAR GOUGED AT XE 40 DOT 62. -- BLENDED DAMAGE AREA. 2 L 7 2 4F A6WE 2002092400128 20020924 00128 WP 2002 9 24 MWEA020587 1 20020924 A 5313 592480225 LONGERON DOUG DC9 DC981 3022081 WP STATION 389 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 LONGERON 17 CRACKED AT FRAME STATION 389 BOTH LEGS RIGHT SIDE OF AIRCRAFT. -- REMOVED DAMAGED SECTION FABRICATED AND R EPAIRED LONGERON AND SPLICE, INSTALLED LONGERON. 2 L 7 2 4F A6WE 2002092400129 20020924 00129 WP 2002 9 24 MWEA020588 1 20020924 A 5311 39129562 ATTACH FITTING DOUG DC9 DC981 3022081 WP STATION 1219 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FRAME TO FLOOR ATTACH FITTING AT FRAME STATION 219 RIGHT SIDE HAS HEAVY CORROSION AROUND FORWARD ATTACH BOLT HOLES. -- REMOVED CORROSION, LOCATED AND DRILLED AND INSTALLED NEW FITTINGS. 2 L 7 2 4F A6WE 2002092400130 20020924 00130 WP 2002 9 24 MWEA020590 1 20020924 A 5313 99367303 INTERCOSTAL DOUG DC9 DC981 3022081 WP STATION 1112 IMPROPER A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 IMPROPER PREVIOUS BLEND OUT AT FRAME STATION 1112 LONGERON 9 LEFT INTERCOSTAL. -- BLENDED DAMAGE, FABRICATED NEW PLATE , LOCATED AND DRILLLED INTERCOSTAL, INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2002092400131 20020924 00131 WP 2002 9 24 MWEA020591 1 20020924 A 5330 9910155123 SKIN DOUG DC9 DC981 3022081 WP DOT 443 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 RIGHT MAIN LANDING GEAR WHEEL CEILING SKIN CRACKED AT RIGHT AFT CORNER, JUST FORWARD OF FUEL DRAIN SHROUD COVER SUPPORT COVER BRACKET DOT 443. -- CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND EDGE SEALED DOUBLER. 2 L 7 2 4F A6WE 2002092400132 20020924 00132 WP 2002 9 24 MWEA020579 1 20020924 A 5553 591218836 STABILIZER DOUG DC9 DC981 3022081 WP STATION 1441 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 VERTICAL STABILIZER DORSAL FIN LOWER RIGHT INBOARD ATTACH ANGLE CRACKED AT FRAME STATION 1441 DOT 80. -- REMOVED ATTAC H ANGLE, LOCATED AND DRILLED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2002092400133 20020924 00133 WP 2002 9 24 MWEA020580 1 20020924 A 5533 591218835 STABILIZER DOUG DC9 DC981 3022081 WP STATION 1441 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 VERTICAL STABILIZER DORSAL FIN LOWER LEFT INBOARD ATTACH ANGLE CRACKED AT FRAME STATION 1441 DOT 79. -- REMOVED ATTACH ANGLE, LOCATED AND DRILLED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2002092400134 20020924 00134 WP 2002 9 24 MWEA020582 1 20020924 A 5315 9911595123 FLOORBEAM DOUG DC9 DC981 3022081 WP STATION 200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 WEB ON STATION 200 FLOOR BEAM UNDER OUTBOARD LEFT VERTICAL SUPPORT IS CORRODED. -- REMOVED DAMAGED AREA, FABRICATED DO UBLER AND FILLER AND INSTALLED REPAIRED DOUBLER. 2 L 7 2 4F A6WE 2002092400135 20020924 00135 EU 2002 9 24 DHL2002363011 1 20020924 A 2420 976J9313 CONTROLLER AIRBUS 300 A300B4203 3930306 EU A DHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 363DH 85 DURING TAKEOFF LOST #1 GENERATOR, #1 YAW, #1 PITCH TRIM. REJECTED TAKEOFF.DEFERRED #1 GENERATOR TO DMI 10468 IAW MEL 24- 10-01, CAT. 'B'. COMPLIED WITH SP 24-11-01. MXC NOTIFIED. PLACARD INSTALLED.REMOVED AND REPLACED #1 GENERATOR CONTROL UN IT PER MM 24-21-00. RAN ENGINE #1 PER JRH OPS CHECKED GENERATOR GOOD. THIS CLEARS DMI, MXC NOTIFIED. PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2002092400136 20020924 00136 NE 2002 9 24 TSAA0275194 2 20020905 A 7532 658385001 BLEED VALVE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D* NE NR 2 ENGINE MALFUNCTIONED A TSAA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 WP 13 816AL 23122 THE NR 2 ENGINE COMPRESSOR STALLED WHEN THE THRUST LEVERS WERE BROUGHT BACK TO IDLE AT TOP OF DECENT. THE AIRCRAFT CONT INUED THE APPROACH AND LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE PRESSURE RATIO BLEED CONTROL VALVE (PRBC). GROUN D OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002092400137 20020924 00137 EA 2002 9 24 QXEA0201333 1 20020905 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 605QX 10022 PDX- CAGE ABOVE AND JUST INSIDE FORWARD CARGO DOOR HAS SOME BROKEN MESH. REMOVED AND REPLACED CAGE IN FORWARD CARGO PI T. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002092400138 20020924 00138 2002 9 24 SWIA200211229 4 20020907 A 3425 6226198103 COMPUTER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 214SW 1634 1634 120280 CAPT'S EHIS FAILED AFTER TAKEOFF. RETURNED TO FIELD. REMOVED AND REPLACED THE NR 1 HPU WITH A SERVICEABLE UNIT. OPS C HECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092400139 20020924 00139 SO 2002 9 24 SWIA200211230 1 20020917 A 5411 FRAME EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 289YV 120289 RIGHT NACELLE FRAME NR 1 CRACKED AT INBOARD AND OUTBOARD WEB AREAS. DISCOVERED DURING C-CHECK. REPLACED RIGHT NACELLE FRAME NR 1 IAW SB 120-54-0036 RII CARD 54-301. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092400140 20020924 00140 EA 2002 9 24 SWIA200211231 1 20020915 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 426SW 7468 DURING TAKEOFF ROLL, CONFIG TRIM THEN CONFIG SPOILERS WARNING ILLUMINATED. ABORTED TAKEOFF. RESET SPOILER SYSTEM, VERI FIED AILERON TRIM AT NEUTRAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2002092400141 20020924 00141 EA 2002 9 24 SWIA200211232 1 20020915 A 5753 601R146992 FLAP CNDAIR CL600 CL6002B19 1900309 EA RT WING BIRD STRIKE A SWIA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 NM 07 446SW 395 395 7666 RIGHT OUTBOARD FLAP DAMAGED BY BIRD STRIKE. REMOVED AND REPLACED RIGHT WING OUTBOARD FLAP ASSEMBLY IAW 27-53-00. OPS C HECK GOOD. 2 L 7 2 4F RT A21EA 2002092400142 20020924 00142 WP 2002 9 24 MWEA020592 1 20020924 A 5330 5911410347 SKIN DOUG DC9 DC981 3022081 WP STATION 237 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FUSELAGE SKIN HAS A DENT AT STATION 237 BELOW LONGERON 18 LEFT DOT 206. -- COLD FORMED SKIN, FABRICATED REAPAIR DOUBLE R AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002092400143 20020924 00143 WP 2002 9 24 MWEA020594 1 20020924 A 5311 99115311 PANEL DOUG DC9 DC981 3022081 WP STA 712&731 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 WINDOW PANEL INTERIOR SURFACE ON LEFT HAND SIDE OF AIRCRAFT BETWEEN STATION 712 AND 731 HAS CORROSION AT LOWER CENTER LI P AREA. -- REMOVED CORROSION, FABRICATED AND INSTALLED WINDOW BELT DOUBLER. 2 L 7 2 4F A6WE 2002092400144 20020924 00144 SO 2002 9 24 SWIA200211234 1 20020918 A 7920 LINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE LEAKING A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 268UE 120207 LOST OIL PRESSURE AFTER TAKEOFF ON UPWIND LEG. REDUCED POWER. LANDED ON RWY 10, SHUT DOWN ENGINE AFTER LANDING. FOUND LOWER OIL COOLER HOSE ON LEFT ENGINE TO HAVE A HOLE. REMOVED AND REPLACED LEFT ENGINE OIL COOLER HOSE IAW MM 79-21-05. DOWNLOAD AND REVIEW OF FDR DATA INDICATED NO EXCEEDENCES. 2 L 7 2 4T 4 T RT A31SO E20NE 2002092400145 20020924 00145 WP 2002 9 24 MWEA020593 1 20020924 A 5311 4911383503 FRAME DOUG DC9 DC981 3022081 WP STATION 1271 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 HOLE IN FRAME AT STATION 1271 RIGHT SIDE AND LONGERON 15. -- FABRICATED,LOCATED AND DRILLED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2002101800117 20021018 00117 2002 10 18 2002UALA01406 4 20020831 A 3417 4040800906 ADC BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 671UA 30026 FIRST OFFICERS AIR DATA COMPUTER FAILED. FIRST OFFICER AIR DATA INSTRUMENT FLUCTUATING, RUDDER RATIO AND AILERON LOCKOU T EICAS MESSAGE DISPLAYED. REPLACED THE FIRST OFFICER AIR DATA COMPUTER. CONFIRMED THE FAULT, UNIT SENT TO THE MANUFAC TURER FOR EVALUATION DUE TO PREVIOUS FAILURES. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800127 20021018 00127 EU 2002 10 18 2002UALA01435 1 20020908 A 2910 AE2463921G0181 HYDRAULIC LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT MLG RUPTURED A UALA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 429UA 539 ABORTED TAKEOFF DUE TO ECAM HYDRAULIC GREEN RESERVOIR LOW LEVEL WARNING. FOUND RIGHT HAND MLG DOOR RETRACT ACTUATOR AFT FLEX LINE RUPTURED. REPLACED FLEX LINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2002101800130 20021018 00130 NM 2002 10 18 2002UALA01441 1 20020912 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 AFT CARGO PIT STATION 1520 ABOVE STRINGER 23L HAS DEEP DENT ON TOP FLANGE. MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVED A ND FRAME DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101800134 20021018 00134 NM 2002 10 18 2002UALA01448 1 20020914 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 CABIN FLOOR AREA STATION 1440 TO 1460 STRINGER 17R OUTER CREASE BEAM SPLICE HAD CORROSION AT 1452 TO 1466. ALSO WEB BET WEEN INNER AND OUTER CREASE BEAMS HAD CORROSION BETWEEN 1440 AND 1460. MAJOR REPAIR ACCOMPLISHED. REMOVED WEB AND FACT ORY SPLICE REPLACED OUTER CREASE BEAM SPLICE BETWEEN 1452 TO 1466 WITH FACTORY NEW PART ALSO INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101800140 20021018 00140 NM 2002 10 18 2002UALA01453 1 20020914 A 2560 PBE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 663UA 27160 PASSENGER BREATHING EQUIPMENT DAMAGED AT CLOSET 309. REPLACED PBE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800147 20021018 00147 NM 2002 10 18 2002UALA01460 1 20020915 A 5412 BULKHEAD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 NR 2 PYLON WEB CRACKED, ACCESS THROUGH PYLON PANELS 446BL OR 446BR. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800149 20021018 00149 NM 2002 10 18 2002UALA01462 1 20020916 A 5420 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 NR 1 ENGINE PYLON CRACKED AT FORWARD TORQUE BOX, OUTBOARD DRAIN HOLE. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB WITH DOU BLERS AND FILLERS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800156 20021018 00156 NM 2002 10 18 2002UALA01468 1 20020918 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 CABIN CREASE BEAM EXCESSIVE CORROSION STATION 690-740 STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM SE CTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2002102800082 20021028 00082 NM 2002 10 28 2002UALA01470 1 20020918 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 CABIN RIGHT HAND CREASE BEAM CORRODED STATION 970. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002102800083 20021028 00083 NM 2002 10 28 2002UALA01471 1 20020918 A 5320 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 CABIN LEFT HAND CREASE BEAM WEB CORRODED STATION 1000-1020. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002092400146 20020924 00146 SO 2002 9 24 C2XA02CL187 1 20020924 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16911 145446 CLE FLIGHT#4368 THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON THE GALLEY DOOR WAS INOPERATIVE.MAINTENANCE REPLACED THE E MERGENCY LIGHT INVERTER.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002092400147 20020924 00147 NM 2002 9 24 ANCF200200020 1 20020919 A 7100 WOODWARD BOEING 757 757236 1384971 NM RROYCE RB211 RB211535* NE W ANCF A UNSCHED LANDING X R ENGINE FLAMEOUT PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 23 951PG 1948207 22185 30046 DURING CRUISE AT 28000 FT RH ENGINE PRESENTED A POWER LOOSE OF 50%, RH ENGINE WAS REDUCED TO IDLE AND POWERED IT AS A TE ST. RIGHT AFTER, THE RH ENGINE FLAMED OUT. IN THE FIRST ATTEMPT IT DID NOT START.ADDITIONALY CABIN ALTITUDE ALARM WAS PR ESENTED. CREW DECIDED TO DIVERT TO CLO.CORRECTIVE ACTION:PERFORMED BOROSCOPE INSPECTION IAW AMM 72-00-00 PAGE 601, THE C OMPRESSOR BLADES WERE FOUND IN NORMAL CONDITION.TROUBLE SHOOTING WAS PERFORMED IAW FIM 71-05-00 FIG 116 AND FIM 71-05-00 FIG 107, REPLACED FUEL FLOW GOVERNOR IAW AMM 73-21-01 PAGE 401, PERFORMED RUN UP IAW AM 71-00-00 WITH SATISFACTORY RESU LTS. THE AIRCRAFT FLEW TO MAIN BASE IN ORDER TO READ FDR. AFTER READING WAS FOUND AN AIR LEAK FROM TUBE ASSY P1 2 L 7 2 4F 4 F RT A2NM E12EU 2002092400148 20020924 00148 2002 9 24 DHL2002804009 4 20020921 A 3414 INDICATOR DOUG DC8 DC873F 302199F WP A DHLA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SO 01 804DH 46124 1) REJECTED TAKEOFF AT APPROX. 90 KTS DUE TO NO AIRSPEED INDICATIONS ON CAPT. OR F/O'S AIRSPEED INDICATIONS. NORMAL BR AKING & REVERSE USED.2) PERFORM AISPEED INDICATOR FUNCTIONAL CK BOTH CAPT & F/O CKS GOOD IAW DC 8 MMS 34-11-00. PERFORM PITOT LEAK TEST WITH DPS 350 TESTER CHKS GOOD IAW DC 8 MMS 34-12-00 LEAK CHK CAPT. FO & ALT SYSYTEM PERFORMED ALL 2 L 7 4 4F RT 4A25 2002103100234 20021031 00234 WP 2002 10 31 DHL2002801019 1 20020923 A 2697 WIRE DOUG DC8 DC873F 302199F WP FIRE WARNING SHORTED A DHLA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 801DH 46033 DURING SERVICE CHECK NR 3 ENGINE FIRE DETECTION SHORT LIGHT ALWAYS ILLUMINATED IN B LOOP POSITION. REPLACED WIRE 4W5123 C16 FROM R5-7001 TO R5-7007 OPS CHECKED GOOD PER M/M 26-10-0. 2 L 7 4 4F RT 4A25 2002092500001 20020925 00001 SO 2002 9 25 C2XA02SH063 1 20020910 A 5310 14521725013 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 DURING C CHECK, THE SERVICE DOOR FORWARD SILL WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED FORWARD SER VICE DOOR SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002092500003 20020925 00003 EA 2002 9 25 AMY2002F00000 2 20020918 A 7323 MS3106A10SL4S PLUG PIPER PA46 PA46500TP 7104622 SO PWA PT6 PT6* 52043 EA GOVERNOR DAMAGED B AMYR K NONE O OTHER IN INSP/MAINT 1 CE 05 999RW 4697037 OVERSPEED GOVERNOR WHICH SITS ON THE FORWARD LEFT SIDE OF THE ENGINE HAS A DEFECT. THE TEST SOLENOID ELECTRICAL PLUG SI TS IN A MANNER THAT WIRES GOING TO THE PLUG ARE DAMAGED WHENEVER THE COWLING IS REMOVED OR INSTALLED. THE PRESENT PLUG IS A STRAIGHT PLUG. THE STRAIGHT PLUG SHOULD BE REPLACED WITH A 90 DEGREE PLUG TO PROVIDE CLEARANCE FOR THE WIRES AND T HE COWLING. 1 L 7 1 3O 3 T RT A25SO E2NE 2002092500004 20020925 00004 WP 2002 9 25 ABXA020217 1 20020911 A 5300 591359612 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 SHEARTIE AT F.S. 1059, LONGERON 15 RIGHT WAS CRACKED. REPAIRED SHEARTIE IAW DC-9 SRM 51-30-5 AND ABX DRAWING #K05159. 2 L 7 2 4F A6WE 2002092500005 20020925 00005 WP 2002 9 25 ABXA020218 1 20020913 A 5200 99577359 CLIP DOUG DC9 DC932 3022066 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 RIGHT AFT OVERWING EXIT DOOR HAD CRACKED ATTACH CLIP INSIDE UPPER FORWARD LIGHTENING HOLE. INSTALLED NEW ATTACH CLIP IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002092500006 20020925 00006 SO 2002 9 25 C2XA02CL188 1 20020924 A 7933 23073715 SENSOR EMB 145 EMB145ER 3260211 SO RIGHT ENGINE DEFECTIVE A C2XA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 27 14939 145030 CLE FLIGHT#3397 THE CREW REPORTED #2 ENGINE EXCEEDED THE LIMITS FOR OIL TEMPERATURE WHILE CLIMBING THRU 5000'.POWER WAS REDUCED AND THE TEMPERATURE RETURNED TO NORMAL.THE OIL TEMPERATURE EXCEEDED LIMITS AGAIN A FEW MINUTES LATER AND THE ENG INE WAS SHUTDOWN FOR PRECAUTIONARY PURPOSES.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLA CED THE #2 OIL TEMPERATURE SENSOR.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002092500007 20020925 00007 EA 2002 9 25 BSY2002F00021 2 20020910 A 8500 1068291018 MAGNETO PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA MAGNETO DEFECTIVE E BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 3590D 318052144 786461A RT ENGINE STARTED RUNNING ROUGH. REMOVED AND REPLACED DEFECTIVE MAGNETO OPS CHECKS GOOD. 1 L 7 2 3O 3 O A20SO E14EA 2002092500008 20020925 00008 NM 2002 9 25 PCAA0209111 1 20020923 A 7931 PW120A ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT FALSE INDICATION A PCAA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 EA 13 848EX 22298 8123 331 121178 SYR-BOS FLIGHT#3848. CREW REPORTED #1 ENGINE OIL PRESSURE INDICATION WENT TO ZERO, ENGINE SHUT DOWN AS A PRECAUTION. EME RGENCY DECLARED, AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND CI RCUIT BREAKER K5 POPPED. WIRING INSPECTED AND CANNON PLUG AT PRESSURE SWITCH CLEANED. AIRCRAFT RAN FOR 30 MINUTES, OPERA TIONAL CHECK GOOD.AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002092500009 20020925 00009 NM 2002 9 25 QXEA0201309 1 20020831 A 5230 ROLLER BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR OBSTRUCTED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 411QX 4055 SEA- CREW RETURNED TO FIELD DUE TO FUSELAGE DOORS WARNING LIGHT ILLUMINATED EIGHT MINUTES AFTER DEPARTURE, PASSING THROU GH 14,000 FEET. FIVE MINUTES LATER DURING DESCENT FLIGHT ATTENDANT REPORTED HEARING A BANG. AIRCRAFT LANDED WITHOUT IN CIDENT. FOUND PAINT OVER SPRAY ON RELEASE LATCH ROLLER ASSEMBLY, CAUSING RELEASE BUTTON TO STICK OPEN. CLEANED AND LUB ED ROLLER ASSEMBLY ON REAR CARGO DOOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092500010 20020925 00010 CE 2002 9 25 CG02002F00000 1 20020911 A 3246 5030001087 WHEEL BEECH 90 C90A 1152911 CE PWA PT6 PT6* 52043 EA MLG CRACKED B CGOR K NONE O OTHER IN INSP/MAINT 1 GL 03 617MM 736 LJ1587 DURING TIRE CHANGE FOUND SEVERAL BOLT HOLES CRACKED DURING ROUTINE EDDY-CURRENT INSPECTION OF BOLT HOLE AND TIRE BEAD SE AT AREAS. SUSPECT PROBABLY CAUSED BY OVERTORQUING OF TIE BOLTS DURING PAST TIRE CHANGES. 1 L 7 2 3T 3 T RT 3A20 E2NE 2002092500011 20020925 00011 CE 2002 9 25 CG02002F00001 1 20020911 A 3246 5030001087 WHEEL BEECH 90 C90A 1152911 CE PWA PT6 PT6A6 52043 EA MLG CRACKED A CGOR K NONE O OTHER IN INSP/MAINT 1 GL 03 617MM 736 LF1587 DURING TIRE CHANGE, FOUND SEVERAL BOLT HOLES CRACKED DURING ROUTINE EDDY-CURRENT INSPECTION OF BOLT HOLE AND TIRE BEAD S EAT AREAS. 1 L 7 2 3T 3 T RT 3A20 E4EA 2002092500012 20020925 00012 NM 2002 9 25 QXEA0201334 1 20020903 A 5230 HANDLE BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR OUT OF POSITION A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 409QX 4051 AIRCRAFT DIVERTED WHEN FLIGHT CREW RECEIVED A FORWARD BAG DOOR CAUTION LIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. COMPLI ED WITH HORIZON AIR TASK CARD 52-32-00-20-801. COMPLIED WITH FUNCTIONAL CHECK OF DOOR HANDLE. NO DEFECTS NOTED. DOOR HANDLE SLIGHTLY PROTRUDED ON ARRIVAL AT GEG. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2002102800211 20021028 00211 SO 2002 10 28 C2XA02CL185 1 20020920 A 4930 4504015 FUEL LINE EMB 145 EMB145 3260210 SO APU LOOSE A C2XA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 16963 145116 IAH FLIGHT NR 3922 THE CREW REPORTED A STRONG FUEL SMELL IN CABIN AND COCKPIT WHEN STARTING THE APU. MAINTENANCE INSPEC TED AND RESECURED FUEL LINE AT THE APU FUEL ACCELERATION CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002092500013 20020925 00013 CE 2002 9 25 CGO2002F00002 1 20020911 A 2150 11791006013 PLATE RAYTHN BEECH B300 B300 1159232 CE A/C COMPRESSOR FAILED B CGOR K NONE L NO TEST IN INSP/MAINT 1 GL 03 991LL 3035 FL142 DURING FREON AIR CONDITIONING SYSTEM TROUBLESHOOTING, FOUND COMPRESSOR FAILED. UPON REMOVAL OF OLD UNIT FOR REPLACEMENT , FOUND PIVOT PLATE CRACKED COMPLETELY THROUGH. 2 L 7 2 4T RT A24CE 2002092500014 20020925 00014 EU 2002 9 25 QXEA0201335 1 20020831 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DEFECTIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US * 1081 11156 PDX- GREEN EXIT AND EVACUATION LIGHTS AT MAIN CABIN DOOR AND GALLEY SERVICE DOOR ILLUMINATE WITH EMERGENCY LIGHT SWITCH IN OFF POSITION AND EXIT AIRCRAFT SWITCH TURNED OFF, REGARDLESS OF BATTERY SWITCH POSITION. REMOVED AND REPLACED BATTER Y. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002092500015 20020925 00015 NM 2002 9 25 QXEA0201374 1 20020701 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 CKB - LEFT HAND INBOARD FLAP HAS MINOR CHAFING ON THE TOP SKIN. REPAIRED IAW SRM 57-51-30-320-801. 2 H 7 2 4T RT A13NM 2002092500016 20020925 00016 EA 2002 9 25 KZ52002F00002 2 20020828 A 7320 RSA10AD1 SERVO BEECH 65 65 1152802 CE LYC O720 IO720A1B 41546 EA FUEL CONTROL FAILED B KZ5R K NONE O OTHER IN INSP/MAINT 1 GL 15 5078N 1863 LF16 L150154A PILOT REPORTED RT ENGINE TO BE LOW ON POWER, FOUND ENGINE TO BE RUNNING VERY RICH, WHICH CAUSED PLUGS TO FOUL, INSTALLED OVERHAULED FUEL SERVO AND CLEANED PLUGS, GROUND RUN AND TEST FLIGHT OK. 1 L 7 2 3O 3 O 3A20 1E15 2002092500017 20020925 00017 2002 9 25 SIMA200224901 4 20020905 A 3140 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE EICAS FALSE ACTIVATION A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 501BG 10017 AFTER CLIMBOUT LT BLEED DUCT OVERHEAT EICAS WARNING WITH CONCURRENT INDICATION ON ECS PAGE. CREW FOLLOWED AOM PROC. DE CLARED EMERGENCY AND RETURNED TO AIRPORT. ON TOUCHDOWN EICAS MESSAGE WENT OUT. CREW CALLED MOC AFTER THEY WERE ON THE GROUND. NO OTHER PROBLEMS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. LEAK TEST OF LEFT BLEED SYSTEM AND OPERATIONAL CHECK OF LEFT BLEED AIR TEMP SENSOR WERE GOOD IAW MM. MEL WAS CLEARED AND AI RCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002092500018 20020925 00018 NM 2002 9 25 QXEA0201375 1 20020701 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 CKB - RIGHT HAND INBOARD FLAP HAS MINOR CHAFING ON THE TOP SKIN. REPAIRED IAW SRM TASK 57-51-30-320-801. 2 H 7 2 4T RT A13NM 2002092500019 20020925 00019 EU 2002 9 25 SIMA200224903 1 20020906 A 6130 FE2016002 PROP BRAKE AEROSP ATR72 ATR72212A 8680902 EU PROPELLER FIRE A SIMA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SW 21 538AT 538 AIRCRAFT WAS AT THE GATE AND THE CREW HAD THE RT ENGINE IN MODE, THE READY LIGHT FOR THE PROP BRAKE WAS ON. THE CREW NO TED THAT THE PROP STARTED TO ROTATE. THEY THEN GOT THE PROP BRAKE CWP LIGHT AND THE E2 FIRE LIGHT. THEY USED THE FIRE BOTTLES, BOTH SHOTS AND THE RAMP CREW SAW FLAMES ON THE ENGINE AND THEY USED THE GROUND DRY CHEM-FIRE EXT ON THE ENGINE, INTO THE INLET AND THE TAIL PIPE. PAX WERE DEPLANED WITH NO INCEDENTS NOTED. REPLACED RT ENGINE AND REMOVED AND DEACT IVATED PROP BRAKE PER EO. 2 H 7 2 4T RT A53EU 2002092500020 20020925 00020 EA 2002 9 25 SIMA200225503 1 20020909 A 2820 CHECK VALVE CNDAIR CL600 CL6002C10 1390015 EA GE CF6 CF6* 30020 GL WING TANKS FAILED A SIMA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 503AE 10021 ON DECENT CREW NOTED CAUTION MESSAGE (FUEL IMBALANCE) WITH 1,000 LBS IN RT WING, CENTER TANK STARTED TO FILL UP AND SAW MAX IMBALANCE OF 1200 LBS WITH 1250 IN CENTER TANK. AIRCRAFT LANDED SAFELY; NO FURTHER INCIDENTWS WERE REPORTED. REMOV ED AND REPLACED LT AND RT UPPER AND LOWER CHECK VALVES AND CLAMPS. 2 L 7 2 4F 4 F RT A21EA E23EA 2002092500021 20020925 00021 EA 2002 9 25 SIMA200225701 1 20020913 A 7500 LOOP CNDAIR CL600 CL6002C10 1390015 EA GE CF6 CF650* 30018 NE BLEED SYSTEM OUT OF POSITION A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 501BG 10017 LT BLEED DUCT MASTER WARNING DECLARED EMERGENCY. INSPECTED AND FOUND BLEED LOOP SENSOR MT 202/MT203, NOTED LOOP TOUCHIN G BLEED LINE, REPOSITION BLEED SENSOR LOOP....FCF PASSED. 2 L 7 2 4F 4 F RT A21EA E23EA 2002092500022 20020925 00022 EU 2002 9 25 SIMA200226107 1 20020915 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE CABIN CORRODED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 269AT 269 MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS IN THE FORWRD CABIN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE POWER SUPPLY UNIT AT POSITION 3WL IAW ATRMM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21 2002B9782) 2 H 7 2 4T 4 T RT A53EU E20NE 2002092500023 20020925 00023 NM 2002 9 25 QXEA0201376 1 20020715 A 5230 SUPPORT BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 CKB - AFT BAGGAGE BAY DOOR FORWARD BOTTOM EDGE OF INNER SUPPORT IS DAMAGED. REPAIRED IAW HORIZON AIR EA 6-52-173 AND WV AC EO DH8S-52-0493. 2 H 7 2 4T RT A13NM 2002092500024 20020925 00024 EU 2002 9 25 UO22002F00017 1 20020912 A 2910 F50B751112 LINE AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP HYD SYSTEM CHAFED B UO2R K NONE O OTHER IN INSP/MAINT 1 GL 19 83FJ 12685 74 HYDRAULIC NR 1 PRESSURE LINE AND NR 1RETURN LINE CHAFING IN PYLON. 2 L 7 3 4F 4 F A46EU E6WE 2002092500025 20020925 00025 NM 2002 9 25 USAABB02147 1 20020903 A 2121 6067723 FAN BOEING 757 757225 1384959 NM CABIN FAULTY A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 19 607AU 22203 ON PREFLIGHT IN SJU, CREW NOTED A SLIGHT SMOKE SMELL IN THE LT WHEEL WELL. ON TAKEOFF, THE SMELL WAS NOTED AGAIN, BUT D ISSIPATED. THE SMELL RETURNED AND THE FLIGHT DIVERTED TO GSO. MAINTENANCE OPERATED THE PACKS FROM VARIOUS SOURCES THRO UGH FULL TEMPERATURE RANGE WITH NO ABNORMALITIES NOTED. INSPECTED ALL PASSENGER SEAT ELECTRONIC UNITS, ENTERTAINMENT FE ED-THROUGHS, EQUIPMENT RACKS, ELECTRICAL POWER CENTERS AND CARD FILES. NO ABNORMALITIES WERE NOTED. FOUND THE RT RECIR CULATION FAN EMITTING A FAINT ODOR. REPLACED FAN. 2 L 7 2 4F RT A2NM 2002092500026 20020925 00026 NM 2002 9 25 USAASB02167 1 20020905 A 2120 ODOR BOEING 737 737401 1384701 NM CABIN/COCKPIT DETECTED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 412US 23881 DURING CRUISE CREW REPORTED A BURNING/SMOKE ODOR IN COCKPIT. FLT ATTENDANTS REPORTED ODOR WAS OBVIOUS THROUGHOUT CABIN AS SEVERAL PASSENGERS COMPLAINED. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. ODO R WAS NOTICEABLE AFTER LANDING AND AT GATE. MAINT GROUND RAN BOTH ENGINES, AIR SYSTEMS, PACKS AND ELECTRICAL SYSTEMS. ALL CHECKED OK. INSPECTED GALLEYS, CABIN AREA, E/E COMPARTMENTS AND CARGO BAYS. ALL CHECKED OK. INSPECTED GALLEYS, CA BIN AREA, E/E COMPARTMENTS AND CARGO BAYS. ALL CHECKED OK. CHECKED AIR CYCLE MACHINES AND INSPECTED BOTH ENGINES FOR F OD AND INGESTION. ALL CHECKED OK. 2 L 7 2 4F RT A16WE 2002092500027 20020925 00027 NM 2002 9 25 USAASB02171 1 20020914 A 3260 189929 UPLOCK SENSOR BOEING 737 7373B7 1384580 NM RT MLG FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 515AU 23701 ON CLIMB OUT, ENROUTE, CREW RECEIVED A RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT AFTER GEAR RETRACTION. CREW FOLLOWED QU ICK REFERENCE HANDBOOK PROCEDURES AND CYCLED THE GEAR. THEY RECEIVED THREE GEAR GREEN LIGHTS WHEN EXTENDING GEAR BUT RE CEIVED RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT AGAIN AFTER RETRACTING THE GEAR. FLIGHT RETURNED TO FIELD AND LANDED AN D TAXIED TO GATE WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE TROUBLESHOT SYSTEM AND REMOVED AND R EPLACED THE RIGHT MAIN LANDING GEAR UPLOCK SENSOR, OPERATIONAL TEST SATISFACTORY. 2 L 7 2 4F RT A16WE 2002092500028 20020925 00028 CE 2002 9 25 VJ32002F00073 1 20020903 A 3610 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO DRY AIR FAILED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 5519A 310 CE1337 825759R DURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT U P AND AIR PRESSURE STILL LOW AT HIGHER RPM. PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP. 1 L 7 1 3O 3 O 3A15 E5CE 2002092500029 20020925 00029 CE 2002 9 25 VJ32002F00074 1 20020903 A 3610 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO DRY AIR FAILED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 8112T 609 CE1539 DURING GROUND RUN UP, OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP. 1 L 7 1 3O 3 O 3A15 E5CE 2002092500030 20020925 00030 EU 2002 9 25 VJ32002F00075 1 20020913 A 2820 201B6 METER GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA FUEL FLOW FLUCTUATES B VJ3R O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 865AF 218 85005 DURING FLIGHT THE FLIGHT CREW NOTICED THE FUEL FLOW FLUCTUATING. BELIEVED CAUSED FROM HEAT IN ENGINE BAY CAUSING FUEL T O VAPORIZE AS IS PASSES THROUGH FUEL FLOW METER. RECOMMENDATION IS MOUNT THE FUEL FLOW METER HORIZONTALLY AND WRAP IN H EAT SHIELDING. 1 L 7 1 3O 3 O RT A49CE 1E4 2002092500031 20020925 00031 SW 2002 9 25 2002F00900 1 20020218 A 2612 LIGHT BELL 214 214ST 1182106 SW INSTRUMENT PANEL CONTAMINATED A DXTA K NONE L NO TEST IN INSP/MAINT 1 SW 03 392AL 28114 DURING PREFLIGHT CHECK, NR 1 FIRE LIGHT WOULD NOT TEST, WATER CONDUCTOR. AFTER BEING DRIED OUT SYSTEM OPERATED PROPERLY . (M) 2 G 7 2 4U H10SW 2002092500032 20020925 00032 EU 2002 9 25 QXEA0201336 1 20020904 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 PDX- EXIT SIGN ABOVE GALLEY HAS SEGMENTS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ABOVE GALLEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002092500033 20020925 00033 NM 2002 9 25 QXEA0201338 1 20020902 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX- THERE ARE TWO .5 INCH LONG DENTS ON FUSELAGE, FORWARD OF LAVATORY SERVICE DOOR JUST BELOW RIGHT HAND PITOT TUBE. R EPAIRED IAW HORIZON AIR EA 2-53-424. 2 H 7 2 4T RT A13NM 2002092500034 20020925 00034 NM 2002 9 25 QXEA0201340 1 20020825 A 7110 ATTACH ANGLE BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - RIGHT HAND LOWER COWLING 87144121-101 ATTACH ANGLE IS CRACKED. REPAIRED IAW HORIZON EA 6-71-56A. 2 H 7 2 4T RT A13NM 2002092500035 20020925 00035 NM 2002 9 25 QXEA0201341 1 20020825 A 7110 BRACKET BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - RIGHT HAND LOWER COWLING 87144114-103 LEFT HAND AFT BRACKET IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-17-56A. 2 H 7 2 4T RT A13NM 2002092500036 20020925 00036 NM 2002 9 25 QXEA0201342 1 20020825 A 7110 FITTING BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - RIGHT HAND LOWER COWLING 87144 RIGHT HAND CLEAT IS CRACKED. REPAIRED IAW HORIZON AIR EA --A. 2 H 7 2 4T RT A13NM 2002092500037 20020925 00037 NM 2002 9 25 QXEA0201343 1 20020825 A 7110 SUPPORT BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - RIGHT HAND LOWER COWLING 87144117-104 SUPPORT ANGLES (2) ARE CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-56A. 2 H 7 2 4T RT A13NM 2002092500038 20020925 00038 NM 2002 9 25 QXEA0201344 1 20020830 A 5420 BRACKET BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - LEFT HAND NACELLE PANEL 414AR TRAILING EDGE SUPPORT BRACKET IS CRACKED. REPAIRED IAW WVAC EO DH85-54-0528 AND HOR IZON AIR EA 6-54-113A. 2 H 7 2 4T RT A13NM 2002092500039 20020925 00039 NM 2002 9 25 QXEA0201345 1 20020823 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - LEFT HAND CENTER WING LEADING EDGE HAS CRACKED RIBS AT FOUR PLACES, TWO ON INBOARD RIB ENDS AND TWO ON OUTBOARD RI B ENDS. REPAIRED IAW HORIZON AIR EA 6-57-55 AND WVAC EO DH8S-57-0529A. 2 H 7 2 4T RT A13NM 2002092500040 20020925 00040 NM 2002 9 25 QXEA0201346 1 20020823 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - RIGHT HAND CENTER WING LEADING EDGE HAS CRACKED RIBS AT FOUR PLACES, TWO ON INBOARD RIB ENDS AND TWO ON OUTBOARD R IB ENDS. REPAIRED IAW HORIZON AIR EA 6-57-55A AND WVAC EO DHC8S-57-0529A. 2 H 7 2 4T RT A13NM 2002092500041 20020925 00041 NM 2002 9 25 QXEA0201347 1 20020826 A 7110 FRAME BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 DKB - LEFT HAND LOWER COWLING 87144120-103 FRAME IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-56A AND WVAC EO DH8S-71-0 526. 2 H 7 2 4T RT A13NM 2002092500042 20020925 00042 NM 2002 9 25 QXEA0201348 1 20020829 A 5420 STIFFENER BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - RIGHT HAND AFT NACELLE PANEL 424AR OUTBOARD SIDE AFT END STIFFENER CRACKED. REPAIRED IAW HORIZON AIR EA 6-54-113A AND DH8S-54-0528. 2 H 7 2 4T RT A13NM 2002092500043 20020925 00043 GL 2002 9 25 C2XA02BT056 2 20020923 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SHUTDOWN A C2XA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 36915 3466 3466 145421 CAE311748 CVG---CO3395, CREW REPORTED, "SMOKE IN COCKPIT AND CABIN ASSOCIATED WITH HIGH ITT ON #1 ENGINE AND COMPLETE LOSS OF OIL PRESSURE. NO FIRE WARNINGS OR INDICATIONS OTHER THAN SMOKE. SMOKE DISSAPATED WHEN # 1 ENGINE WAS SHUTDOWN." MAINTENANCE REMOVED AND REPLACED #1 ENGINE IAW EMB145 AMM #71-00-00. OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002092500044 20020925 00044 NM 2002 9 25 QXEA0201349 1 20020830 A 5420 STIFFENER BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - RIGHT HAND AFT NACELLE INBOARD PANEL 424AL AFT END STIFFENER IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-54-113A AN D WVAC EO DH8S-54-0528. 2 H 7 2 4T RT A13NM 2002092500045 20020925 00045 NM 2002 9 25 QXEA0201350 1 20020825 A 7110 BRACKET BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - RIGHT LOWER ENGINE COWL AFT INBOARD BRACKET CRACKED. REPAIRED IAW HORIZON AIR EA 6-57-56A AND WVAC EO DH8S-71-052 6A. 2 H 7 2 4T RT A13NM 2002092500046 20020925 00046 NM 2002 9 25 QXEA0201352 1 20020828 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - LEFT HAND OUTBOARD FLAP HAS A GOUGE ON TOP SKIN. REPAIRED IAW WVAC EO DH8S-57-0534. 2 H 7 2 4T RT A13NM 2002092500047 20020925 00047 NM 2002 9 25 QXEA0201353 1 20020828 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - RIGHT HAND OUTBOARD FLAP HAS A GOUGE ON TOP SKIN AT STATION 261.119. REPAIRED IAW HORIZON AIR EA 6-57-52 AND WVAC EO DH8S-57-0534. 2 H 7 2 4T RT A13NM 2002092500048 20020925 00048 NM 2002 9 25 QXEA0201359 1 20020826 A 7110 ATTACH ANGLE BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - LEFT HAND LOWER COWL ATTACHMENT ANGLE CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-56A AND WVAC EO DH8S-71-0526A. 2 H 7 2 4T RT A13NM 2002092500049 20020925 00049 EA 2002 9 25 QXEA0201360 1 20020625 A 5730 SKIN CNDAIR CL600 CL6002C10 1390015 EA LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 CKB - LEFT HAND SIDE LEADING EDGE CHAFED AND INBOARD LOWER SIDE OF MID SLAT, INBOARD CHAFED AT WS 199.66. REPAIRED IAW WVAC EO 610R-57-4033 AND HORIZON AIR EA R-57-05. 2 L 7 2 4F RT A21EA 2002092500050 20020925 00050 NM 2002 9 25 QXEA0201362 1 20020523 A 5420 BRACKET BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 CKB - AFT LOWER BRACKET CRACKED THROUGH BOLT HOLES AND UPPER WEB CRACKED AT FIRST HOLE ON INBOARD SIDE. REPAIRED IAW HO RIZON AIR EA 6-54-79 AND RD 8/4-54-044. 2 H 7 2 4T RT A13NM 2002092500051 20020925 00051 NM 2002 9 25 QXEA0201363 1 20020523 A 7810 PLATE BOMBDR DHC8 DHC8401 1390041 NM EXHAUSTSYS CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - LEFT HAND INBOARD AND RIGHT HAND OUTBOARD AFT EXHAUST MOUNT COVER PLATES CHAFED. REPAIRED IAW Q400 AMM 78-10-16-4 00-801. 2 H 7 2 4T RT A13NM 2002092500052 20020925 00052 NM 2002 9 25 QXEA0201364 1 20020520 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 CKB - LEFT HAND CENTER LEADING EDGE HAS CRACKS ON THE END RIBS. ONE ON THE OUTBOARD RIB AND TWO ON THE INBOARD RIB. RE PAIRED IAW DHC8S-57-0394 AND HORIZON AIR EA 6-57-11. 2 H 7 2 4T RT A13NM 2002092500053 20020925 00053 NM 2002 9 25 QXEA0201365 1 20020520 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 CKB - RIGHT HAND CENTER LEADING EDGE HAS CRACKS ON THE END RIBS. ONE ON THE OUTBOARD RIB AND TWO ON THE INBOARD RIB. R EPAIRED IAW HORIZON AIR EA 6-57-11 AND EO DH8S-57-0394. 2 H 7 2 4T RT A13NM 2002092500054 20020925 00054 NM 2002 9 25 QXEA0201366 1 20020525 A 5230 FITTING BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 CKB - CARGO DOOR STRUT FITTING IS DAMAGED AND MISSING ON BUSHING. REPAIRED IAW HORIZON AIR EA 6-52-155 AND WVAC EO DH8X -52-0408B. 2 H 7 2 4T RT A13NM 2002092500055 20020925 00055 NM 2002 9 25 QXEA0201367 1 20020618 A 5753 FLAP BOMBDR DHC8 DHC8401 1390041 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 CKB - RIGHT HAND OUTBOARD FLAP HAS A CHAFE AT YW19120 TO YW230. REPAIRED IAW WVAC EO DH8S-57-0437A. 2 H 7 2 4T RT A13NM 2002092500056 20020925 00056 NM 2002 9 25 QXEA0201369 1 20020613 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 CKB - RIGHT HAND LEADING EDGE INBOARD RIB HAS A HOLE CHAFED THROUGH EDGE. REPAIRED IAW HORIZON AIR EA 6-57-36 AND WVAC EO DH8S-57-0448. 2 H 7 2 4T RT A13NM 2002092500057 20020925 00057 NM 2002 9 25 QXEA0201370 1 20020612 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 CKB - LEFT HAND CENTER LEADING EDGE INBOARD RIB IS CRACKED IN TWO PLACES AND OUTBOARD RIB HAS ONE CRACK. REPAIRED IAW H ORIZON AIR EA 6-57-28 AND WVAC EO DH8S-57-0428. 2 H 7 2 4T RT A13NM 2002092500058 20020925 00058 NM 2002 9 25 QXEA0201371 1 20020628 A 5720 INTERCOSTAL BOMBDR DHC8 DHC8401 1390041 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 CKB - LEFT HAND CENTER WING LEADING EDGE HAS THREE CRACKS ON THE CORNERS OF THE INTERCOSTALS. REPAIRED IAW HORIZON AIR EA 6-57-39 AND WVAC EO DH8S-57-0466. 2 H 7 2 4T RT A13NM 2002092500059 20020925 00059 NM 2002 9 25 QXEA0201372 1 20020628 A 7810 PLATE BOMBDR DHC8 DHC8401 1390041 NM EXHAUST SYS WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 CKB - LEFT HAND NACELLE INBOARD EXHAUST FITTING COVER PLATE HAS A HOLE WORN THROUGH IT. REPAIRED IAW HORIZON AIR EA 6-7 8-08 AND WVAC EO DH8S-78-0465. 2 H 7 2 4T RT A13NM 2002092500060 20020925 00060 NM 2002 9 25 QXEA0201373 1 20020715 A 5230 SUPPORT BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 CKB - AFT BAGGAGE BAY DOOR AFT BOTTOM CORNER INNER CORNER SUPPORT IS DAMAGED. REPAIRED IAW HORIZON AIR EA 6-52-173 AND WVAC EO DH8S-52-0493. 2 H 7 2 4T RT A13NM 2002092500061 20020925 00061 SO 2002 9 25 SWIA200211235 1 20020914 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 569SW 5651 5651 120344 DURING F/A PREFLIGHT EMERGENCY LIGHTS COME ON THEN GO DARK. TEST FAILED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT 5BC. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002092500062 20020925 00062 EA 2002 9 25 SWIA200211236 1 20020914 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 592SW 7279 ABORTED TAKEOFF FOR INBOARD OUTBOARD GROUND SPOILER FAULT. CLEARED MESSAGES BY POWER DOWN. NO FURTHER PROBLEMS. 2 L 7 2 4F RT A21EA 2002092500063 20020925 00063 CE 2002 9 25 2002F00899 1 20020220 A 3230 MODULE CESSNA 750 750 2076810 CE MLG FAILED A DXTA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 989QS 7500089 EN ROUTE TO THE US FROM MKJS THE A/C EXPERIENCED AN UNCOMMANDED EXTENSION OF THE L/G AT FL410, .89 MACH. THE L/G REMAIN ED EXTENDED FOR APPROX 1 MINUTE AND THEN RETRACTED. SEVERAL MINUTES LATER THE L/G EXTENDED AGAIN UNTIL DESCENT TO FL230 , 210 KIAS WHEN THE GEAR RETRACTED. THE L/G DEPLOYED NORMALLY ON APROACH AND THE A/C LANDED IN FLL WITHOUT INCIDENT. M AINTENANCE INSPECTED TEH A/C AND DETERMINED IT SAFE FOR FERRY TO MCO. AT MCO MAINTENANCE REMOVED AND REPLACED THE LG CO NTROL ASSY, LOGIC MODULE AND THE GEAR DOWN CONTROL WIRE BETWEEN THESE COMPONENTS. THE L/G SYSTEM OPS CHECKED GOOD PER C ES FT 750-0037 6.2. THE A/C WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4J RT T00007WI 2002092500064 20020925 00064 EA 2002 9 25 2002F00902 1 20020423 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG W/W INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 77260 7260 FLT 6451 - RETURNED TO CMH, AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT AND GEAR DISAGREE MESSAGE. MAINTENANCE REMOVED A ND REPLACED NOSE GEAR PRIORITY VALVE. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002092500065 20020925 00065 EA 2002 9 25 2002F00903 1 20020425 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG W/W INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 47202 7202 FLT 5887 - MKE-PHL, RETURNED TO FIELD WITH A GEAR DISAGREE MESSAGE WITH AN 'X' OVER THE NLG INDICATION ON THE PRIMARY PA GE. MAINTENANCE WAS CALLED, MAINTENANCE REMOVED AND REPLACED THE SELECTOR VALVE. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002092500066 20020925 00066 EA 2002 9 25 2002F00904 1 20020614 A 2741 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA VERT STABILIZER FAILED A MASA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SW 07 77331 7331 FLT 5800 - PHL-CVG, ABORTED TAKEOFF, GOT TAKEOFF CONFIG-STAB TRIM WARNING. MAINTENANCE STILL WORKING ON STAB TRIM ACTUA TOR CHANGE. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STAB TRIM ACTUATOR. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002092500067 20020925 00067 WP 2002 9 25 AALA20021097 1 20020727 A 3350 60030451 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 476AA 49651 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROWS 19-22 INOPERATIVE. REPLACED EMEREGNCY EXIT LIGHT BATTE RIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002092500068 20020925 00068 WP 2002 9 25 AALA20021109 1 20020731 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 432AA 49350 RDU - DURING OVERNIGHT MAINTENANCE, AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED AFT CABIN OVERHEAD E MERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002102900096 20021029 00096 SO 2002 10 29 C2XA02BT057 1 20020924 A 2750 3631101007 CONTROL HANDLE EMB 135 EMB135LR 3260305 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14516 145323 CREW REPORTED, "LANDING GEAR WARNING HORN WARNING CONSTANT WITH GEAR IN UP POSITION, SYSTEM CUTOUT INOPERATIVE." MAINTE NANCE REMOVED AND REPLACED FLAP SELECTOR HANDLES IAW EMB135 AMM 27-53-03. OPS CHECKED SYSTEM GOOD. TEST FLIGHT OF AIRC RAFT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002092500069 20020925 00069 WP 2002 9 25 AALA20021112 1 20020729 A 3397 WIRE DOUG DC9 DC982 3022082 WP FLOOD LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 219AA 49171 DFW - DURING OVERNIGHT MAINTENANCE, LEFT AISLE CEILING EMERGENCY EXIT FLOOD LIGHT DIM AT ROW 23. TIGHTENED SCREW ON GRO UND WIRE FOR LEFT AISLE CEILING EMERGENCY EXIT FLOOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002092500070 20020925 00070 WP 2002 9 25 AALA20021113 1 20020731 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 429AA 49341 DFW - DURING OVERNIGHT MAINTENANCE, SEAT 6E EMERGENCY EXIT PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGH TING CONNECTOR AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002092500071 20020925 00071 WP 2002 9 25 AALA20021142 1 20020810 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 402A 49313 DFW - DURING OVERNIGHT MAINTENANCE, BOTH SIDEWALL EMERGENCY EXIT LIGHTS FOR AFT STAIRS IN TAILCONE INOPERATIVE. REPLACE D WIRE RUN FROM HANDLE LIGHT CONNECTOR TO BOTH SIDEWALL LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002092500072 20020925 00072 WP 2002 9 25 AALA20021143 1 20020812 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 208AA 49159 MIA - DURING OVERNIGHT MAINTENANCE, BOTH LT AND RT FORWARD EMERGENCY EXIT ESCAPE HATCH LIGHT DIM. RECONNECTED LOOSE CON NECTION AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002092500073 20020925 00073 WP 2002 9 25 AALA20021151 1 20020813 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 227AA 49177 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT TAIL SECTION DIM. TIGHTENED GROUND WIRE FOR EMERGENCY EXIT LIGHTS IN AFT TAIL SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002092500074 20020925 00074 NM 2002 9 25 BJNA020833 1 20020812 A 5330 SKIN BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FORWARD FRAME OF THE C-2 DOOR CUT OUT ABOVE TRANSITION PANEL HAS LEVEL 2 CORROSION. REMOVED CORRODED FRAME IAW 737 SRM 51-30-2 AND REO L00 588. REPAIRED FRAME IAW REO L00 588 REV IR. FABRICATED FRAME SPLICES AND INSTALLED IAW REO L00588 AND B737 SRM 51-20-1. (M) 2 L 7 2 4F RT A16WE 2002092500075 20020925 00075 WP 2002 9 25 EIA2002089 1 20020802 A 3260 LATCH DOUG DC9 DC933F 302207A WP RT MLG OUT OF ADJUST A EIAA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 933F 47191 FLT 120 - PANC - AFTER TAKEOFF, AFT RIGHT GEAR UNSAFE LIGHT REMAINED ON, UPLATCH CHECK FAILED. PERFORMED ADJUSTMENT/TES T MAIN GEAR DOOR LATCH MECHANISM PER MM 32-31-4, SYSTEM OPS CHECK NORMAL, ALSO GREASED LATCH MECHANISM, CLEANED ELECTRIC PLUGS ON UPLATCH SWITCH, LUBRICATED DOOR LATCH. (M) 2 L 7 2 4F A6WE 2002092500076 20020925 00076 WP 2002 9 25 GTIA020510 1 20020515 A 7160 59306451 LINER DOUG DC9 DC983 3022083 WP NR 2 INLET DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 DTW - NR 2 ENGINE INLET WIRE MESH ON ACOUSTIC LINER SEPARATING. 25 INCHES REMOVED OF WIRE MESH ON NR 2 NOSE COWL. 6:30 TO 4:30 FORWARD TO AFT 25 INCHES WIDE. PLACED ON C/O 28753-3. REMOVED AND REPLACED NR 2 ENGINE INLET NOSE COWL. (M) 2 L 7 2 4F RT A6WE 2002092500077 20020925 00077 WP 2002 9 25 GTIA020653 1 20020510 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - FOUND MID PIT, CORRODED AT SUPPORT BRACKET ATTACH TO LONGERON 30. FORMED NEW PART PRIOR TO STEP 1. REMOVED BRACK ET. INSTALLED BRACKET. (M) 2 L 7 2 4F A6WE 2002092500078 20020925 00078 WP 2002 9 25 GTIA020677 1 20020515 A 7810 SUPPRESSOR DOUG DC9 DC982 3022082 WP NR 1 ENGINE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FTW - ENGINE NR 1 EXHAUST CASE NOISE SUPPRESSOR BULGED SKIN 4 TO 9 O'CLOCK POSITION AND FORWARD RING EXFOLIATED. REMOVE D T/R, 7 AREAS OF DELAMINATION IN PERFORATED SKIN 4 AREAS OF DELAMINATED IN OUTER SKIN, PIN AND PLUG REPAIRS. REMOVED A ND TREATED EXFOLIATED AREA. REINSTALLED T/R. (M) 2 L 7 2 4F A6WE 2002092500079 20020925 00079 2002 9 25 GTIA020780 4 20020707 A 2213 7446120 RHEOSTAT DOUG DC9 DC983 3022083 WP AILERON SERVO FAILED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 827NK 49793 DEN - FLT 980 - IN TURN YOKE VERY JERKY, AUTO PILOT DISENGAGES. OK IN LEVEL FLIGHT, NR 2 AUTO PILOT. TROUBLESHOT AUTOP ILOT SYSTEM. FOUND AILERON SERVO RHEOSTAT BAD. CHECKED WITH METER LEFT SIDE GOOD RIGHT SIDE BAD. REMOVED AND REPLACED RHEOSTAT AND AILERON SERVO DRIVE PER MD-80 MM 22-11-01. SYSTEM OPS CHECKED GOOD PER MD80 MM 22-11-01 AND RTS PER 22-01 -05. (M) 2 L 7 2 4F RT A6WE 2002092500080 20020925 00080 WP 2002 9 25 GTIA020820 1 20020624 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FORWARD PIT AFT BULKHEAD FORWARD FACE HAS CRACKED AT UPPER ANGLE LBL 26 INCHES. DRILLED STOP CRACK ON UPPER FLANG E STATION 541 LBL 26. DRILLED AND LOCATED, INSTALLED. (M) 2 L 7 2 4F A6WE 2002092500081 20020925 00081 WP 2002 9 25 GTIA020821 1 20020624 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - MID PIT FLOORBEAM HAS CHAFING/DAMAGE STATION 655. MATERIAL LOSS OUT OF LIMITS. FORMED ANGLES. INSTALLED ANGLES. (M) 2 L 7 2 4F A6WE 2002092500082 20020925 00082 WP 2002 9 25 GTIA020822 1 20020624 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - AFT PIT FLOORBEAM HAS CHAFING/DAMAGE THROUGH HOLE STATION 1174. FABRICATED ANGLE REPAIR AND FILLER. INSTALLED AN GLE AND SHIM. (M) 2 L 7 2 4F A6WE 2002092500083 20020925 00083 WP 2002 9 25 GTIA020823 1 20020624 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FORWARD CARGO COMPARTMENT HAS CHAFING/DAMAGE AT FLOORBEAM STATION 389. MATERIAL LOSS OUT OF LIMITS. FABRICATED D OUBLERS. INSTALLED DOUBLERS STATION 389. (M) 2 L 7 2 4F A6WE 2002092500084 20020925 00084 WP 2002 9 25 GTIA020824 1 20020624 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND FORWARD CARGO COMPARTMENT CHAFING/DAMAGE AT FLOORBEAM STATION 408. FOUND AREA TO BE OUT OF LIMITS. FABRICA TED REPAIR ANGLE. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2002092500085 20020925 00085 WP 2002 9 25 GTIA020825 1 20020626 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FS 1146 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - PASSENGER CABIN RIGHT SEAT TRACK, RBL 44, STATION 1146 HAS CORROSION, SCRATCHES AND GOUGES. REMOVED DAMAGE AREA O F SEAT TRACK FROM STATION 1126 TO 1147. DRILLED AND LOCATED HOLES IN NEW SEAT TRACK AND SPLICES. FABRICATED SEAT TRACK . INSTALLED NEW SEAT TRACK AND SPLICES. (M) 2 L 7 2 4F A6WE 2002092500087 20020925 00087 NM 2002 9 25 QXEA0201379 1 20020703 A 5411 FRAME BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 CKB - RIGHT HAND INBOARD A FRAME .25 INCH HOLE ELONGATED THROUGH FIRST 15 PERCENT OF A FRAME. REPAIRED IAW HORIZON AIR EA 6-54-99 AND WVAC EO DH8S-54-0478. 2 H 7 2 4T RT A13NM 2002092500088 20020925 00088 NM 2002 9 25 QXEA0201380 1 20020708 A 5420 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 CKB - LEFT HAND NACELLE OUTBOARD CHANNEL THIRD HOLE FROM TOP AND INBOARD HOLE ELONGATED. REPAIRED IAW HORIZON AIR EA 6- 54-100 AND WVAC EO DH8S-54-0479. 2 H 7 2 4T RT A13NM 2002092500089 20020925 00089 NM 2002 9 25 QXEA0201381 1 20020628 A 5720 INTERCOSTAL BOMBDR DHC8 DHC8401 1390041 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 CKB - INBOARD RIGHT HAND CENTER WING INTERCOSTAL CRACKED. REPAIRED IAW HORIZON AIR EA 6-57-39 AND WVAC EO DH8S-57-0466. 2 H 7 2 4T RT A13NM 2002092500090 20020925 00090 NM 2002 9 25 QXEA0201382 1 20020714 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 CKB - LEFT HAND OUTBOARD FLAP TOP SKIN HAS A CHAFE. REPAIRED IAW HORIZON AIR EA 6-57-40 AND WVAC EO DH8S-57-0475. 2 H 7 2 4T RT A13NM 2002092500091 20020925 00091 NM 2002 9 25 QXEA0201383 1 20020628 A 7810 PLATE BOMBDR DHC8 DHC8401 1390041 NM EXHAUST SYS CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 CKB - EXHAUST FITTING COVER PLATE RIGHT HAND OUTBOARD HAS A HOLE CHAFED THROUGH IT. REPAIRED IAW HROZION AIR EA 6-78-08 AND WVAC EO DH8S-78-0465. 2 H 7 2 4T RT A13NM 2002092500092 20020925 00092 NM 2002 9 25 QXEA0201384 1 20020523 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 CKB - LEFT OUTBOARD FLAP UPPER SKIN HAS CHAFE DAMAGE BETWEEN WING STATIONS YW191.200 AND YW281.019. REPAIRED IAW HORIZO N AIR EA 6-57-17 AND D-400 RD8/4-57-016. 2 H 7 2 4T RT A13NM 2002092500093 20020925 00093 NM 2002 9 25 QXEA0201385 1 20020820 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX- CRACK IN FIREWALL JUST ABOVE MAIN LANDING GEAR RETRACT ACTUATOR ATTACH FITTING UPPER ACCESS HOLE ON NR 2 RIGHT HAND ENGINE. REPAIRED IAW DHC-8 RD 8-54-806. 2 H 7 2 4T RT A13NM 2002092500094 20020925 00094 NM 2002 9 25 QXEA0201388 1 20020905 A 2422 DH103024600CSIIB INVERTER DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 358PH 12313 214 506 BOI- STRONG FISH SMELL ON FLIGHT DECK. REMOVED AND REPLACED INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2002092500095 20020925 00095 EU 2002 9 25 QXEA0201389 1 20020905 A 2440 914F5824 CONTROL UNIT FOKKER F28 F28MK4000 4990810 EU COCKPIT MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 479AU * 2432 11228 BOI- WHEN ATTEMPTING TO HOOK UP GROUND POWER SMOKE APPEARED FROM RIGHT PANEL BEHIND FIRST OFFICER. REMOVED AND REPLACED EXTERNAL GROUND POWER CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002092500096 20020925 00096 NM 2002 9 25 QXEA020139 1 20020825 A 7110 FRAME BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 CKB - RIGHT HAND LOWER COWLING 87144120-103 FRAME IS CRACKED. REPAIRED IAW HORIZON AIR EA/EO 6-71-561A. 2 H 7 2 4T RT A13NM 2002092500097 20020925 00097 NM 2002 9 25 QXEA0201390 1 20020806 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB - SUPPORT CHANNEL IS CRACKED IN THE LEFT HAND LOWER COWL. REPAIRED IAW WVAC EO DH8X-71-0503C AND HORIZON AIR EA 6-71 -50C. 2 H 7 2 4T RT A13NM 2002092500098 20020925 00098 NM 2002 9 25 QXEA0201392 1 20020806 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB - SUPPORT CHANNEL IS CRACKED ON LOWER LEFT COWL. REPAIRED IAW HORIZON AIR EA 6-71-50C AND WVAC EO DH8S-71-0503C. 2 H 7 2 4T RT A13NM 2002092500099 20020925 00099 WP 2002 9 25 GTIA020826 1 20020626 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FORWARD ENTRY STATION 196 LBL 22-45 SUBFLOOR IS CORRODED UNDER FLOOR BOARD SUPPORT, .500 INCH HOLE THROUGHT SUB FL OOR AT OUTBOARD END, HIDDEN DAMAGE. REMOVED DAMAGED SUB FLOOR SKIN, FABRICATED REPAIR SKIN AND DOUBLER. INSTALLED REPA IR SKIN AND DOUBLER ON STATION 196 LBL 22-45. (M) 2 L 7 2 4F A6WE 2002092500100 20020925 00100 NM 2002 9 25 QXEA0201393 1 20020806 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB - LEFT HAND LOWER COWL CHANNEL IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-054 AND WVAC EO DH8S-71-0503C. 2 H 7 2 4T RT A13NM 2002092500101 20020925 00101 WP 2002 9 25 GTIA020827 1 20020627 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND L2 DOOR STATION 1146 AND LBL 55 INCHES FLOOR SUPPORT HAS CORROSION AND A SHANK. REMOVED FLOOR SUPPORT. FAB RICATED FLOOR SUPPORT, INSTALLED SUPPORT. (M) 2 L 7 2 4F A6WE 2002092500102 20020925 00102 WP 2002 9 25 GTIA020828 1 20020628 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 148 LBL 7, LIGHT CORROSION ON SUB FLOOR WEB WITH SMALL HOLE THROUGH WEB. CUT OUT PUNCTURED AND CORR ODED AREA AT STATION 148 LBL 7 FLOOR WEB. FABRICATED DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER ON STATIO N 148 LBL 7 SUB FLOOR WEB. (M) 2 L 7 2 4F A6WE 2002092500103 20020925 00103 WP 2002 9 25 GTIA020829 1 20020629 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND PASSENGER CABIN HAS CRACKED AT THE WEB, UNDER TEE, LBL 14.5 INCHES, STATION 200. REMOVED DAMAGE. FABRICATE D REPAIR. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2002092500104 20020925 00104 WP 2002 9 25 GTIA020831 1 20020717 A 5753 STRUCTURE DOUG DC9 DC932 3022066 WP TE FLAPS DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DTW - FOUND RIGHT FLAP TRAILING EDGE SPLICE APPROX 1.5 INCHES INBOARD END OF FLAP AT FIRST EXPANSION JOINT. SANDED AND INSTALLED FIBERGLASS LAYUP REPAIR ON RIGHT FLAP TRAILING EDGE. (M) 2 L 7 2 4F A6WE 2002092500105 20020925 00105 WP 2002 9 25 MWEA020595 1 20020925 A 5311 991150210 FRAME DOUG DC9 DC914 3022034 WP STATION 58 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 CRACK ON FRAME AROUND FASTENER HOLE AT FRAME STATION 25 RIGHT SIDE OF NOSE WHEEL WELL AREA ABOUT 1" DOWN FROM CEILING. -- REMOVED FASTENERS, FABRICATED AND LOCATED REPAIR DOUBLER AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002092500106 20020925 00106 WP 2002 9 25 MWEA020596 1 20020925 A 5315 2912758 FLOORBEAM DOUG DC9 DC914 3022034 WP STATION 817 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 RIGHT LAV FLOOR BEAM AT FRAME STATION 817 HAS CORROSION AROUND 3 NUTPLATES APPROXIMATELY 24" RIGHT OF CENTER LINE. -- REMOVED DAMAGED AREA, FABRICATED, LOCATED AND DRILLED REPAIR ANGLE, INSTALLED REPAIR ANGLE,FILLER AND NUTPLATES. 2 L 7 2 4F A6WE 2002092500107 20020925 00107 NM 2002 9 25 AWXA200200919 1 20020911 A 5320 65163007 WEB BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 0 0 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK A 3/8" CRACK WAS FOUND ON WEB AT BS 178, WL 213, LBL 5.7. MAINTENANCE STOP DRILLE D CRACK AT BOTH ENDS, AND REPAIRED DAMAGED AREA IAW B 737-300 SRM 53-10-08, PG. 275-279, & 286, FIG. 210. 2 L 7 2 4F RT A16WE 2002092500108 20020925 00108 NM 2002 9 25 AWXA200200920 1 20020911 A 5320 65163007 WEB BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 0 0 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK A 2" CRACK WAS FOUND ON WEB AT RIVET HOLE BS 178, WL 234, RBL 8. MAINTENANCE BLEN DED OUT DAMAGE AT BS 178, WL 234, RBL 8, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG. 209, PG. 265-269. 2 L 7 2 4F RT A16WE 2002092500109 20020925 00109 NM 2002 9 25 AWXA200200921 1 20020911 A 5320 65163007 WEB BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 0 0 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK A 5/8" CRACK WAS FOUND ON WEB AT BS 178, WL 213, RBL 5.7. MAINTENANCE STOP DRILLE D CRACK AT BOTH ENDS, AND REPAIRED DAMAGED AREA IAW B 737-300 SRM 53-10-08, PG. 275-279, & 286, FIG. 210. 2 L 7 2 4F RT A16WE 2002092500110 20020925 00110 NM 2002 9 25 AWXA200200922 1 20020911 A 5320 65163007 WEB BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 0 0 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK A 2" CRACK WAS FOUND ON WEB AT RIVET HOLE BS 178, WL 234, LBL 9. MAINTENANCE BLEN DED OUT DAMAGE AT BS 178, WL 234, LBL 9, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG. 209, PG. 265-269. 2 L 7 2 4F RT A16WE 2002092600001 20020926 00001 WP 2002 9 26 GTIA020834 1 20020729 A 2420 9008D092 GENERATOR DOUG DC9 DC983 3022083 WP LEFT FAILED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 822NK 49392 FLT 706 - LGA - AFTER TAKEOFF OVER MILE AREA LT GENERATOR FAULT FEEDER AND GEN BUS AND X-TIE LIGHT CAME ON, QRH FOLLOWED . FOUND LEFT GENERATOR BAD. ON GENERATOR T5 TO T6 READ .5 OHMS WHICH FAIL GENERATOR. REMOVED AND REPLACED LEFT POWER RELAY FOR PRECAUTIONARY. REF ITEM 43556-1 FOR LEFT GEN REPLACEMENT IAW MD80 MM 24-20-00. (M) 2 L 7 2 4F RT A6WE 2002092600002 20020926 00002 WP 2002 9 26 GTIA020835 1 20020713 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - AFT ACCESSORY COMP GOUGE ON LONGERON 22L FLANGE, STATION 1380. FABRICATED REPAIR DOUBLER, INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2002092600003 20020926 00003 WP 2002 9 26 GTIA020836 1 20020624 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 218-237 LBL 18, SUPPORT ANGLE CORRODED ON FORWARD END. FABRICATED NEW SUPPORT ANGLE. INSTALLED NEW SUPPORT ANGLE. (M) 2 L 7 2 4F A6WE 2002092600004 20020926 00004 WP 2002 9 26 GTIA020837 1 20020623 A 5320 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND MID PIT CRACKED AT BRACKET ATTACH TO INTERCOSTAL AND BULKHEAD FRAME RBL 16 INCHES STATION 788. REMOVED CRAC KED BRACKET AT FRAME RBL 16 INCHES STATION 788, LOCATED AND CB DRILLED NEW FITTING, INSTALLED. (M) 2 L 7 2 4F A6WE 2002092600005 20020926 00005 WP 2002 9 26 GTIA020838 1 20020628 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND COCKPIT FLOORBOARD STATION 120-160 CENTER CORRODED AND MISSING INSERTS. FABRICATED NEW PANEL. (M) 2 L 7 2 4F A6WE 2002092600006 20020926 00006 WP 2002 9 26 GTIA020839 1 20020621 A 5730 PANEL DOUG DC9 DC982 3022082 WP LT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND LEFT WING UPPER SURFACE PANEL DELAMINATED NEXT TO INBOARD SPOILER. REMOVED PANEL. LOCATED AND DRILLED NEW PANEL. INSTALLED PANEL. (M) 2 L 7 2 4F A6WE 2002092600007 20020926 00007 WP 2002 9 26 GTIA020840 1 20020704 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - AFT CARGO FLOORBOARD STATION 1212-1234 SURFACE CORROSION, GOUGES, DRILL STARTS AND ELONGATED HOLES. REMOVED CORRO SION GOUGES, MATERIAL OUT OF LIMITS. FORMED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002092600008 20020926 00008 WP 2002 9 26 GTIA020841 1 20020801 A 7160 LINER DOUG DC9 DC983 3022083 WP NR 2 ENG INLET TORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 DTW - NR 2 ENGINE INLET COWL WIRE MESH LINER TORN. REPAIRED TORN LINER WIRE MESH NR 2 ENGINE INLET COWL IAW MD80 SRM 54 -04A. (M) 2 L 7 2 4F RT A6WE 2002092600009 20020926 00009 WP 2002 9 26 GTIA020844 1 20020623 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND PASSENGER CABIN LEFT OVERWING INTERNAL FRAME HAS CRACKS STATION 965L NR 12. STOP DRILLED CRACK. FORMED REP AIR ANGLES, ROUTED TO HEAT TREAT DEPT. INSTALLED REPAIR ANGLES -3, -5, AND -7 ON STATION 965 LONGERON NR 12. (M) 2 L 7 2 4F A6WE 2002092600010 20020926 00010 WP 2002 9 26 GTIA020845 1 20020711 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 546-552 BETWEEN LONGERON 17R AND 18R, 6 INCHES LONG CREASE IN FUSELAGE SKIN. CUT OUT DAMAGE. FORME D FINGER DOUBLER. FORMED SKIN DOUBLER. INSTALLED FINGER DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2002092600011 20020926 00011 WP 2002 9 26 GTIA020847 1 20020621 A 5730 PANEL DOUG DC9 DC982 3022082 WP LT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND LEFT LOWER WING SURFACE TRAPEZOID (SHAPE) PANEL DELAMINATED NEXT TO MLG WHEEL. REPAIRED LEFT LOWER WING SUR FACE TRAPEZOID PANEL. (M) 2 L 7 2 4F A6WE 2002092600012 20020926 00012 WP 2002 9 26 GTIA020848 1 20020621 A 5730 PANEL DOUG DC9 DC982 3022082 WP RT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND LOWER WING SURFACE TRAPEZOID (SHAPE) PANEL DELAMINATED NEXT TO MLG WHEEL. REPAIRED RIGHT LOWER WING TRAPEZO ID PANEL. (M) 2 L 7 2 4F A6WE 2002092600013 20020926 00013 WP 2002 9 26 GTIA020849 1 20020619 A 5330 SKIN DOUG DC9 DC982 3022082 WP WINDOW BELT DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - C/O CONTROL NR 0870 ON L/P 84615, FUSELAGE HAS DENT BELOW CAPTAINS CLEARVIEW WINDOW AT APPROX STATION 125. REWORK ED DENT. FORMED DOUBLER REPAIR. S/D - DENT AT FS 121 BETWEEN LONGERONS 17 AND 18L REQUIRES REPAIR. (M) 2 L 7 2 4F A6WE 2002092600014 20020926 00014 WP 2002 9 26 GTIA020850 1 20020731 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 816NK 49140 FLL - FOUND 1.75 INCH CRACK IN UNPRESSURIZED AREA OF LEFT AFT FUSELAGE AT STATION 1437 BETWEEN LONGERONS 22L AND 23L. A CCOMPLISHED REPAIR IAW MD80 SRM 53-01. (M) 2 L 7 2 4F A6WE 2002092600015 20020926 00015 WP 2002 9 26 GTIA020851 1 20020710 A 5543 SKIN DOUG DC9 DC982 3022082 WP RUDDER TAB PUNCTURED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND RUDDER TAB HAS PUNCTURE MARK (HOLE) APPROX .25 INCH DIAMETER 3 INCHES ABOVE FIXED TAB. RUDDER TRIM TAB FIXE D TAB DEBONDED. THIS TAB REPLACED. (M) 2 L 7 2 4F A6WE 2002092600016 20020926 00016 WP 2002 9 26 GTIA020852 1 20020704 A 5280 STRUCTURE DOUG DC9 DC982 3022082 WP MLG DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND LEFT MLG DOOR HAS A CRACK AT FORWARD AFT INBOARD FRAME, ANGLE PREVIOUS REPAIR. CUT OUT DAMAGE. FORMED DOUB LER AND FRAME. INSTALLED NEW FRAME AND DOUBLER. (M) 2 L 7 2 4F A6WE 2002092600017 20020926 00017 WP 2002 9 26 GTIA020853 1 20020622 A 5242 STRUCTURE DOUG DC9 DC982 3022082 WP E/E DOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - E/E DOOR INTERNAL SURFACE HAS CORROSION ALL AROUND. MATERIAL LOSS EXCEEDS THE LIMITS PRESCRIBED IN 52-01. REPAIR DUOBLERS FABBRICATED. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2002092600018 20020926 00018 WP 2002 9 26 GTIA020854 1 20020425 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 218-225 LBL 18 ON REMOVABLE OF SUPPORT ANGLE REF 18-NN-00134 SUB FLOOR WAS FOUND TO HAVE EXFOLIATION . CUT OUT DAMAGED AREA. FABRICATED NEW SUB FLOOR SECTION AND DOUBLER. INSTALLED NEW PARTS. (M) 2 L 7 2 4F A6WE 2002092600019 20020926 00019 WP 2002 9 26 GTIA020855 1 20020623 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND MID PIT HAS CORROSION AT LONGERON 30 STATION 807. REMOVED THE DEEPEST CORROSION AREA. FABRICATED REPAIR PA RTS. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2002092600020 20020926 00020 WP 2002 9 26 GTIA020856 1 20020624 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND STATION 164 LBL 14 AND LBL 42, LIGHT CORROSION ON FLOOR WEB AROUND FITTINGS. AFTER FURTHR EVAL, FOUND THREE FITTINGS CORRODED OUT OF LIMITS. AREA AT STATION 164 LBL 42 FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA. FABRICATED DO UBLER. INSTALLED DOUBLER. DRILLED THREE FITTINGS. INSTALLED THREE FITTINGS. (M) 2 L 7 2 4F A6WE 2002092600021 20020926 00021 WP 2002 9 26 GTIA020858 1 20020621 A 5730 SKIN DOUG DC9 DC982 3022082 WP RT WING DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND RIGHT WING HAS DENT/DAMAGE AT OUTER SKIN FUELING PANEL 1249C. STOP DRILLED CRACK FOUND IN DENT. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2002092600022 20020926 00022 EU 2002 9 26 SIMA200223001 1 20020817 A 3350 74441 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AE 340B386 SGF - FLT 3567 - EMERGENCY EXIT SIGN ABOVE FORWARD EMERGENCY EXIT WILL NOT ILLUMINATE. RAI RIGHT FORWARD EMERGENCY EXIT SIGN IAW AMM 33-50-35. (M) 2 L 7 2 4T RT A52EU 2002092600023 20020926 00023 EU 2002 9 26 SIMA200223303 1 20020819 A 3350 303A51 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 135MQ 135 MIA - FLT 5017 - CREW REPORTED AFTER AIRCRAFT SHUTDOWN THREE EMERGENCY LIGHTS REMAINED ON WHEN SWITCH WAS OFF. MAINTENA NCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY BATTERY PACK IAW ATR MM. OPERATINOAL CHECK WAS GOOD AND AIRCRAFT WA S RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002092600024 20020926 00024 EU 2002 9 26 SIMA200224001 1 20020823 A 3397 CONNECTOR SAAB SF340 340B 7860101 EU CABIN DISCONNECTED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AE 340B373 ACT - FLT 3764 - EXIT LIGHT OVER FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. RECONNECTED CONNECTOR P465UP1, OPS CHECK GOOD IAW WM 33-50. (M) 2 L 7 2 4T RT A52EU 2002092600025 20020926 00025 EU 2002 9 26 SIMA200224002 1 20020826 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 434AT 434 MIA - FLT 4958 - EMERGENCY EXIT LIGHT IN AIRSTAIRS DOOR IS INOPERATIVE. RAI, EMERGENCY SUPPLY POWER UNIT. (M) 2 H 7 2 4T RT A53EU 2002092600026 20020926 00026 NM 2002 9 26 TSAA0251083 1 20020226 A 5330 6545771 SKIN BOEING 737 7372X6C 1384552 NM WINDOW BELT CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS BETWEEN S10L BS 767 PLUS 10 AN D BS 827 PLUS 10 ON WINDOW NR 26 LEFT UPPER AFT HOLES NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS TO SUIT THE AREA OF SKIN/DOUBLER TRIMMED. FABRICAT ED A DOUBLER AND TRIPLER IAW SB 737-53A1177. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION E. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F RT A16WE 2002092600027 20020926 00027 WP 2002 9 26 AAL2002F00006 1 20020730 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7549A 34552 53031 FUSELAGE SKIN GOUGED AT STA 380, EXTERNAL, FOR LOWER ANTENNA MOUNT. SIZE OF DISCREPANCY .2500 X .5000 OUT OF LIMITS. L OWER FUSELAGE, STA 380 IS GENERAL LOCATION. C/A: BLENDED GOUGES IAW SRM.(2002-1164, AMC4) 2 L 7 2 4F A6WE 2002092600028 20020926 00028 WP 2002 9 26 AAL2002F00007 1 20020805 A 5320 WEB DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7549A 53031 WEB, FORWARD ENTRY DOOR JAMB WEB TANG CRACKED STA 210 AT LONGERON IS LEFT (MARKED) AFT SIDE OF DOOR CAST OUT. CRACK LEN GTH .5 INCH AT STA 210, FUSELAGE. C/A: REPAIRED DOOR JAMB INNER SKIN WEB AT LONGERON 15 BY APPLYING REPAIR STRAP. (20 02-1165, AMC4 ) 2 L 7 2 4F 4 F A6WE E2EA 2002092600029 20020926 00029 NM 2002 9 26 QXEA0201436 1 20020909 A 6120 CONTROLLER BOMBDR DHC8 DHC8401 1390041 NM AUTOFEATHER SYS MALFUNCTIONED A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 404QX 4046 YVR - AUTO FEATHER FAILED TO ARM ON TAKEOFF ROLL. COMPLIED WITH SERVICE LETTER C8 SL 31-001R9. NO PARTS REPLACED. OPE RATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092600030 20020926 00030 WP 2002 9 26 AAL2002F00008 1 20020807 A 5730 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE LT WING GROOVED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7549A 34552 53031 WING SKIN, GROVE IN BOTTOM OF WING IN BOARD AND AFT OF NR1 SLOT TRACK ON PANEL LANDING. DEPTH, OUT OF LIMITS, .5000 INC H X 10 INCHES, LEFT WING. REPAIRED IAW ESO. (2002-1167 AMC4) 2 L 7 2 4F 4 F A6WE E2EA 2002092600031 20020926 00031 NM 2002 9 26 VNAA0209018 1 20020915 A 2150 CIRCUIT BREAKER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT TRIPPED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 432JS 3045 FLIGHT 4056 WAS ON THE RUNWAY READY FOR TAKEOFF AND RECEIVED A LEFT HAND PACK OVERHEAT MESSAGE AND ABORTED TAKEOFF. MAI NTENANCE INSPECTED AND RESET THE L2 CIRCUIT BREAKER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002092600032 20020926 00032 WP 2002 9 26 AAL2002F00009 1 20020730 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7549A 34552 53031 SKIN, EXTERNAL FUSELAGE SKIN GOUGED AT STA 402 AT LOWER ANTENNA MOUNT. BLENDED GOUGES IAW SRM. (2002-1242 AMC4) 2 L 7 2 4F 4 F A6WE E2EA 2002092600033 20020926 00033 WP 2002 9 26 AAL2002F00010 1 20020828 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 446AA 49472 SKIN, STA 1380 LONGERON 14R, CRACK IN SKIN PROTRUDING FROM SHEAR - TIE AT LOWER FASTENER. CRACK LENGTH .250. C/A: INST ALLED DOUBLER IAW SRM. (2002-1242 AMC4) 2 L 7 2 4F 4 F A6WE E2EA 2002092600034 20020926 00034 WP 2002 9 26 AAL2002F00011 1 20020815 A 5347 500201 SEAT TRACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 446AA 49472 SEAT TRACK, LIGHT CORROSION TRACK NR 2 STA 1200R. C/A: ALODINED PRIMED AND INSTALLED NEW PLUG WET IAW SRM. (2002-124 3 , AMC4) 2 L 7 2 4F 4 F A6WE E2EA 2002092600035 20020926 00035 NM 2002 9 26 VNAA0209019 1 20020915 A 3250 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING MALFUNCTIONED A VNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 438JS 3056 DURING LANDING, FLIGHT 4180 EXPERIENCED A NOSE WHEEL STEERING FAIL CAS MESSAGE AND EXECUTED A MISSED APPROACH. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND TURNED OFF THE NOSE WHEEL STEERING AND ANTI-SKID. FLIGHT 4180 THEN LANDED WI TH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND RERACKED THE NOSE WHEEL STEERING CONTROL UNIT THEN PERFORMED TAXI CH ECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. THE PROBLEM COULD NOT BE DUPLICATED DURING THESE OPERATION AL CHECKS AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002092600036 20020926 00036 WP 2002 9 26 AAL2002F00012 1 20020814 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 446AA 49472 METAL FLOOR MEMBRANE, HOLE IN METAL FLOOR, STA 05, INBOARD OF NR 3 SEAT TRACK UNDER CENTER FLOORBOARD FC 10. C/A: CUT OUT DAMAGE- INSTALLED DOUBLER IAW AARD. (2002-1244, AMC4) 2 L 7 2 4F 4 F A6WE E2EA 2002092600037 20020926 00037 NM 2002 9 26 VNAA0209022 1 20020915 A 3350 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN INOPERATIVE A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 457PS 3048 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING STRIP WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRA FT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002092600038 20020926 00038 WP 2002 9 26 AAL2002F00013 1 20020814 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE CABIN SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 446AA 45129 49472 METAL FLOOR MEMBRANE, 2 INCH SCRATCH IN FLOOR, STA 212 INBOARD OF NR 5 SCAT TRACK UNDER CENTER FLOORBOARD, FC 10. INSTA LLED CUTOUT DAMAGED DOUBLER. (2002-1245 , AMC4) 2 L 7 2 4F 4 F A6WE E2EA 2002092600039 20020926 00039 WP 2002 9 26 AAL2002F00014 1 20020801 A 5310 BELTFRAME DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 34931 53284 BELTFRAME STA 1271, CORROSION ON BELTFRAME STA 1271, LONGERON 30. INSTALLED DOUBLER. (2002-1185, AMC4) 2 L 7 2 4F 4 F RT A6WE E2EA 2002092600040 20020926 00040 WP 2002 9 26 AAL2002F00015 1 20020801 A 5310 BEAM DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 34931 53284 AFT SERVICE DOOR JAMB BEAM. FOUND CORROSION ON DOOR JAMB BEAM FROM STA. 1155 TO 1212, REPLACED-OUT OF LIMITS. INSTALLE D DOOR JAMB BEAM IAW AARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2002092600041 20020926 00041 NM 2002 9 26 VNAA0209023 1 20020916 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 457PS 14993 424 3048 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROW 9 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AI RCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002092600042 20020926 00042 WP 2002 9 26 AAL2002F00016 1 20020724 A 5320 WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 53284 CUSP, STA 1261 RIGHT FUSELAGE CUSP WEB, CRACKED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2002092600043 20020926 00043 NM 2002 9 26 VNAA0209025 1 20020917 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 470PS 11458 158 3006 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROW 11 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002092600045 20020926 00045 NM 2002 9 26 VNAA0209029 1 20020920 A 3350 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN LOOSE A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 457PS 3048 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 10 TO 12 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND R ESECURED THE EMERGENCY FLOOR LIGHTING IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE P ERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002092600046 20020926 00046 NM 2002 9 26 VNAA0209030 1 20020922 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 459PS 1101 135 3070 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 7 TO 9 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REP LACED THE 6LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORM ED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002092600047 20020926 00047 NM 2002 9 26 QXEA0201443 1 20020911 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- RIGHT HAND WING FLAP TRACK NR 4 HAS PITTING ON TOP HORIZONTAL WEB TRACK. REPAIRED IAW HORIZON AIR EA 2-57-193. 2 H 7 2 4T RT A13NM 2002092600048 20020926 00048 NM 2002 9 26 QXEA0201444 1 20020911 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- RIGHT HAND WING FLAP TRACK NR 4 HAS PITTING ON BOTH SIDES OF VERTICAL WEB TRACKS. REPAIRED IAW HORIZON AIR EA 2-57 -193. 2 H 7 2 4T RT A13NM 2002092600049 20020926 00049 NM 2002 9 26 QXEA0201445 1 20020911 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- NR 4 FLAP TRACK OUTBOARD SIDE LOAD ROLLER TRACK PITTED. REPAIRED IAW HORIZON AIR EA 2-257-192. 2 H 7 2 4T RT A13NM 2002092600050 20020926 00050 CE 2002 9 26 BSY2002F00022 1 20020910 A 3260 ICH25 DOWNLOCK SWITCH BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO NLG INOPERATIVE E BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 2064V TH1004 810935R GOING INTO (DET) HAD NO NOSE GEAR DOWN AND LOCK LIGHT, LANDED OK. FOUND NOSE GEAR DOWN AND LOCK SWITCH BAD. REMOVED AN D REPLACED SWITCH OPS CHECKS GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2002092600051 20020926 00051 NM 2002 9 26 QXEA0201446 1 20020911 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- NR 4 FLAP TRACK INBOARD SIDE LOAD ROLLER TRACK PITTED. REPAIRED IAW HORIZON AIR EA 2-57-192. 2 H 7 2 4T RT A13NM 2002092600052 20020926 00052 NM 2002 9 26 QXEA0201448 1 20020911 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- RIGHT HAND OUTBOARD SEAT TRACK NR 10 HAS HEAVY CORROSION INSIDE CHANNEL AND ON TOP RAIL CUTOUTS AT STATION X342.300 . REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40-11. 2 H 7 2 4T RT A13NM 2002092600053 20020926 00053 NM 2002 9 26 QXEA0201449 1 20020913 A 5210 SKIN DHAV DHC8 DHC8202 2809007 NM CABIN DOOR NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- MAIN CABIN DOOR EXTERNAL SKIN HAS TWO NICKS 11 AND 18 INCHES FROM FUSELAGE. REPAIRED IAW DHC-8 SRM 51-20-26, 51-00 -06 AND 51-00-04. 2 H 7 2 4T RT A13NM 2002092600054 20020926 00054 NM 2002 9 26 QXEA0201450 1 20020913 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- NINETY DEGREE CONNECTION BRACKET AT STATION 600.00 CARGO STEP HAS SEVERAL AREAS OF SURFACE CORROSION. REPAIRED IAW DHC-8 SRM 51-20-11, 51-20-16, 51-20-36 AND 51-40-11. 2 H 7 2 4T RT A13NM 2002092600055 20020926 00055 NM 2002 9 26 QXEA0201451 1 20020912 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- CRACK IN RADIUS OF FORWARD CLOSING ANGLE RBL 22 AND UNDER PANEL 261JT. REPAIRED IAW DHC-8 RD 8-53-5192. 2 H 7 2 4T RT A13NM 2002092600056 20020926 00056 NM 2002 9 26 QXEA0201452 1 20020913 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND OUTBOARD SEAT TRACK NR 2 HAS PITTING CORROSION ON TOP RAIL AT STATION X500.000. REPAIRED IAW DHC-8 RD 8- 53-1342. 2 H 7 2 4T RT A13NM 2002092600057 20020926 00057 NM 2002 9 26 QXEA0201453 1 20020913 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND OUTBOARD SEAT TRACK NR 2 HAS PITTING CORROSION ON TOP RAIL AT X497.000 AND X492.000. REPAIRED IAW DHC-8 RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002092600058 20020926 00058 NM 2002 9 26 QXEA0201454 1 20020913 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND OUTBOARD SEAT TRACK NR 3 TOP RAIL HAS PITTING CORROSION AT STATION X531.000. REPAIRED IAW DHC-8 RD 8-53- 3644 AND DHC-8 SRM 51-20-16 AND 51-00-06. 2 H 7 2 4T RT A13NM 2002092600059 20020926 00059 NM 2002 9 26 QXEA0201394 1 20020806 A 7110 FRAME BOMBDR DHC8 DHC8401 1390041 NM LT COWLING BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB - LEFT HAND LOWER COWL SUPPORT FRAME IS BROKEN. REPAIRED IAW HORIZON AIR EA 6-71-504 AND WVAC EO DH8S-71-0503C. 2 H 7 2 4T RT A13NM 2002092600060 20020926 00060 NM 2002 9 26 QXEA0201395 1 20020805 A 7110 FITTING BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB - RIGHT HAND LOWER COWL CLEAT IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-17-50 AND WVAC EO DH8S-71-0503. 2 H 7 2 4T RT A13NM 2002092600061 20020926 00061 NM 2002 9 26 QXEA0201396 1 20020805 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB- SUPPORT CHANNEL IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-50 AND WVAC EO DH8S-71-0503. 2 H 7 2 4T RT A13NM 2002092600062 20020926 00062 NM 2002 9 26 QXEA0201397 1 20020805 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB- SUPPORT CHANNEL IS CRACKED AT RIGHT LOWER COWLING. REPAIRED IAW HORIZON AIR EA 6-71-50 AND WVAC EO DH8S-71-0503. 2 H 7 2 4T RT A13NM 2002092600063 20020926 00063 NM 2002 9 26 QXEA0201398 1 20020805 A 7110 ANGLE BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB- ANGLE IS CRACKED AT RIGHT LOWER COWL. REPAIRED IAW HORIZON AIR EA 6-71-50 AND WVAC EO DH8S-71-0503. 2 H 7 2 4T RT A13NM 2002092600064 20020926 00064 NM 2002 9 26 QXEA0201399 1 20020806 A 7110 BRACKET BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB- CRACKED RIB BRACKET AT BIRD CATCHER INSIDE LEFT HAND LOWER COWL. REPAIRED IAW WVAC EO DH8S-71-0503C. 2 H 7 2 4T RT A13NM 2002092600065 20020926 00065 NM 2002 9 26 QXEA0201400 1 20020728 A 5730 SKIN BOMBDR DHC8 DHC8401 1390041 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB- RIGHT HAND CENTER WING LEADING EDGE CRACKED AT 4 CORNERS. REPAIRED IAW HORIZON AIR EA 6-57-47 AND WVAC EO DH8S-57- 0506. 2 H 7 2 4T RT A13NM 2002092600066 20020926 00066 NM 2002 9 26 QXEA0201401 1 20020806 A 5730 SKIN BOMBDR DHC8 DHC8401 1390041 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB- ALL 4 CORNERS CRACKED ON LEFT HAND WING INBOARD LEADING EDGE. REPAIRED IAW HORIZON AIR EA 6-57-47A AND WVAC EO DH8 S-57-0506A. 2 H 7 2 4T RT A13NM 2002092600067 20020926 00067 NM 2002 9 26 QXEA0201404 1 20020806 A 5413 LONGERON BOMBDR DHC8 DHC8401 1390041 NM NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB- INBOARD LONGERON HAS 3 BAD FASTENER HOLES AT NACELLE STATION 141.66. REPAIRED IAW HORIZON AIR EA 6-54-108 AND WVAC EO DH8S-54-0515. 2 H 7 2 4T RT A13NM 2002092600068 20020926 00068 NM 2002 9 26 QXEA0201407 1 20020808 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB- LEFT HAND OUTBOARD FLAP HAS SKIN DAMAGE. REPAIRED IAW HORIZON AIR EA 6-57-49 AND WVAC EO DH8S-57-0516. 2 H 7 2 4T RT A13NM 2002092600069 20020926 00069 NM 2002 9 26 QXEA0201408 1 20020806 A 7810 PLATE BOMBDR DHC8 DHC8401 1390041 NM EXHAUST SYS WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB- AFT EXHAUST NOZZLE TRUNNION COVER PLATE HAS HOLE WORN THROUGH PLATE. REPAIRED IAW HORIZON AIR EA 6-78-11. 2 H 7 2 4T RT A13NM 2002092600070 20020926 00070 NM 2002 9 26 QXEA0201409 1 20020806 A 7110 PANEL BOMBDR DHC8 DHC8401 1390041 NM LT COWLING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB- SCREW PULLED THROUGH LIGHT PANEL AT LEFT HAND LOWER COWL. REPAIRED IAW HORIZON AIR EA 6-71-52 AND WVAC EO DH8S-71- 0513. 2 H 7 2 4T RT A13NM 2002092600071 20020926 00071 NM 2002 9 26 QXEA0201410 1 20020805 A 7110 FRAME BOMBDR DHC8 DHC8401 1390041 NM RT COWLING BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 CKB- SUPPORT FRAME IS BROKEN AT RIGHT HAND LOWER COWL. REPAIRED IAW HORIZON AIR EA 6-71-52C AND WVAC EO DH8S-71-0503C. 2 H 7 2 4T RT A13NM 2002092600072 20020926 00072 NM 2002 9 26 QXEA0201411 1 20020621 A 5320 ANGLE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 CKB - RIGHT HAND CLOSING ANGLE CRACKED. REPLACED IAW RD 8-53-4556. 2 H 7 2 4T RT A13NM 2002092600073 20020926 00073 NM 2002 9 26 QXEA0201412 1 20020321 A 5320 ANGLE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 CKB - LEFT HAND AFT CLOSING ANGLE CRACKED. REPLACED IAW RD 8-53-4556. 2 H 7 2 4T RT A13NM 2002092600074 20020926 00074 NM 2002 9 26 QXEA0201413 1 20020329 A 5320 ANGLE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 CKB - RIGHT HAND FORWARD CLOSING ANGLE CRACKED. REPAIRED IAW EO DH8S-53-0367A AND HORIZON AIR EA 9-53-636A. 2 H 7 2 4T RT A13NM 2002092600075 20020926 00075 NM 2002 9 26 QXEA0201414 1 20020321 A 5320 ANGLE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 CKB - LEFT HAND FORWARD CLOSING ANGLE CRACKED. REPAIRED IAW RD 8-53-4556. 2 H 7 2 4T RT A13NM 2002092600076 20020926 00076 NM 2002 9 26 QXEA0201416 1 20020228 A 1430 FASTENER DHAV DHC8 DHC8102 2809003 NM VERTICAL STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 CKB - THREE FASTENERS AT THE BOTTOM RIGHT HAND SIDE OF THE VERTICAL STABILIZER ARE LOOSE. REPAIRED IAW DHC-8 SRM 51-40- 11. 2 H 7 2 4T RT A13NM 2002092600077 20020926 00077 NM 2002 9 26 QXEA0201417 1 20020311 A 5532 SKIN DHAV DHC8 DHC8102 2809003 NM VERTICAL STAB DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 CKB - DENT ON RIGHT HAND SIDE OF VERTICAL STABILIZER BETWEEN RIBS 10 AND 11. REPAIRED IAW HORIZON AIR EA 9-55-149A AND WVAC EO DH8S-55-0357A. 2 H 7 2 4T RT A13NM 2002092600078 20020926 00078 NM 2002 9 26 QXEA0201418 1 20020205 A 5711 SPAR DHAV DHC8 DHC8102 2809003 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 CKB - RIGHT HAND WING FORWARD SPAR TOP FLANGE OUTBOARD OF NR 2 NACELLE AT 24 INCHES HAS GOUGES. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, METHOD 2. 2 H 7 2 4T RT A13NM 2002092600079 20020926 00079 NM 2002 9 26 QXEA0201419 1 20020723 A 5510 STRUCTURE DHAV DHC8 DHC8102 2809003 NM HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 CKB - HORIZONTAL STABILIZER HAS CRACK INDICATION. COMPLIED WITH SERVICE BULLETIN 8-55-22. 2 H 7 2 4T RT A13NM 2002092600080 20020926 00080 NM 2002 9 26 QXEA0201420 1 20020215 A 1430 RIVET DHAV DHC8 DHC8102 2809003 NM ELEVATOR LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 CKB - RIGHT HAND ELEVATOR TOP SIDE AT ELEVATOR MASS BALANCE TEN RIVETS IN SKID ARE LOOSE. REPAIRED IAW DHC-8 SRM 51-40- 11, PAGE 1, STEP 16. 2 H 7 2 4T RT A13NM 2002092600081 20020926 00081 NM 2002 9 26 QXEA0201422 1 20020222 A 1430 BOLT DHAV DHC8 DHC8102 2809003 NM AILERON WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 CKB - ALL THREE ATTACHMENT BOLTS FOR AILERON HINGE FITTING TO HINGE ARM REQUIRES REPLACEMENT DUE TO WEAR SIGNS. REPAIRE D IAW HORIZON AIR EA 9-57-583 AND WVAC EO DH8S-57-0364. 2 H 7 2 4T RT A13NM 2002092600082 20020926 00082 NM 2002 9 26 QXEA0201423 1 20020220 A 1430 BOLT DHAV DHC8 DHC8102 2809003 NM AILERON WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 CKB - ALL THREE ATTCHEMENT BOLTS FOR AILERON HINGE FITTING TO HINGE ARM REQUIRES REPLACEMENT DUE TO WEAR SIGNS. REPAIRE D IAW HORIZON AIR EA 9-57-583 AND WVAC EO DH8S-57-0364. 2 H 7 2 4T RT A13NM 2002092600083 20020926 00083 NM 2002 9 26 QXEA0201424 1 20020413 A 7810 EXHAUST PIPE DHAV DHC8 DHC8102 2809003 NM RT ENGINE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 CKB - RIGHT HAND ENGINE FINGERNAIL HAS 1 INCH CRACK ON THE INSIDE EXHAUST OPENING. REPAIRED IAW DHC-8 SRM 51-10-00. 2 H 7 2 4T RT A13NM 2002092600084 20020926 00084 NM 2002 9 26 QXEA0201425 1 20020802 A 5230 SKIN DHAV DHC8 DHC8102 2809003 NM CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 CKB - BAGGAGE BAY DOOR HAS A DENT WITH A SCRATCH AFT OF THE DOOR HANDLE. REPAIRED IAW WVAC EO DH8S-52-0517A AND DHC-8 M M 52-30-00, STEPS 1 TO 32. 2 H 7 2 4T RT A13NM 2002092600085 20020926 00085 EA 2002 9 26 QXEA0201437 1 20020911 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 BOI- FORWARD CARGO CENTER CHIMNEY IS TORN AND BENT. REPLACED CHIMNEY WITH SERVICEABLE ONE. OPERATIONAL CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002092600086 20020926 00086 EA 2002 9 26 QXEA0201438 1 20020910 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 BOI- FORWARD CARGO COMPARTMENT FIRE DETECTOR CHIMNEY DAMAGED. REMOVED AND REPLACED FIRE DETECTOR CHIMNEY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002092600087 20020926 00087 NM 2002 9 26 QXEA0201440 1 20020915 A 3830 ODOR BOMBDR DHC8 DHC8401 1390041 NM LAVATORY DETECTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 401QX 4031 PDX- BAD SMELL WAFTING THROUGHOUT CABIN, SEEMS TO BE COMING FROM THE LAVATORY. FLUSHED AND SERVICED LAVATORY TANK. NO WAFTING SMELL NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092600088 20020926 00088 NM 2002 9 26 QXEA0201441 1 20020911 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- FORWARD MOST BRACKET ON NR 10 SEAT TRACK HAS DISFIGURED HOLE ON TOP AFT HOLE. REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40-11. 2 H 7 2 4T RT A13NM 2002092600089 20020926 00089 NM 2002 9 26 QXEA0201442 1 20020912 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- RIGHT HAND WING FORWARD SPAR BOTTOM FLANGE IS CHAFED WITH BARE METAL AT STATION YW57.000. REPAIRED IAW DHC-8 RD 8- 57-811. 2 H 7 2 4T RT A13NM 2002092600090 20020926 00090 GL 2002 9 26 D5H2002F00000 3 20020910 A 6197 PIN CESSNA 208 208B 2073701 CE PWA PT6 PT6A45 52043 EA HARTZL H3B3M HCB3M GL CONNECTOR LOOSE E E5HA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 01 64BP 208B0604 PILOT REPORTED SMOKE IN COCKPIT 30 MINUTES INTO FLIGHT. CONNECTOR FROM PROPELLER HEAT CIRCUIT BREAKER (P-186/J-186). C ONNECTOR, 12 GAUGE WIRE(HA-36). MAINTENANCE CREW FOUND CONNECTOR FULLY ENGAGED AND STILL ATTACHED TO WIRE BUNDLE. MAIN TENANCE FOUND TERMINAL PINS INSIDE CONNECTOR LOOSE CAUSING HIGH RESISTANCE WHICH RESULTED IN HEATING AND BURNING OF PLUG . SINCE THERE IS HIGH CURRENT DRAW IN THIS CIRCUIT AND THOUGH THIS CONNECTOR IS RECOMMENDED THAT THE PINS AT THIS CONN ECTOR BE CHECKED FOR PROPER TIGHTNESS AND ENGAGEMENT. 1 H 7 1 3T 4 T A37CE E4EA 5 C P9NE 2002092600091 20020926 00091 GL 2002 9 26 SIMA200226109 2 20020916 A 7200 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL BIRD INGESTION A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 828AE 145604 AFTER TAKE OFF FROM SJC THE AIRCRAFT ENCOUNTERED ABOUT A DOZEN BIRDS WHICH WERE INGESTED INTO BOTH ENGINES. AN EMERGENC Y WAS DECLARED AND AIRCRAFT RETURNED TO SJC WITH NO FURTHER INCIDENTS REPORTED. C/A: MAINTENANCE PERFORMED A BIRDSTRIKE INSPECTION IAW AE MCM. NO DAMAGE WAS FOUND FROM THE BIRDS. THE INSPECTION WAS COMPLETED AND AIRCRAFT WAS RETURNED TO SERVICE. (PTRS SW2002B5973) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002092600092 20020926 00092 WP 2002 9 26 AALA20021116 1 20020725 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 TUL - FOUND CORROSION ON BEAM AROUND 2 FITTINGS AT CARGO DORO CUT OUT LOWER SIDE. REMOVED AND REPLACED CARGO DOOR BEAM PER SRM 51-30-00. (M) 2 L 7 2 4F A6WE 2002092600093 20020926 00093 NM 2002 9 26 QXEA0201455 1 20020910 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND CENTER SEAT TRACK NR 4 OUTBOARD FLANGE HAS A GOUGE AT STATION X234.500. REPAIRED IAW DHC-8 SRM 51-40-11 AND DHC-8 RD 8-53-1102. 2 H 7 2 4T RT A13NM 2002092600094 20020926 00094 NM 2002 9 26 QXEA0201456 1 20020913 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND OUTBOARD SEAT TRACK NR 1 HAS PITTING CORROSION ON TOP RAILS BETWEEN STATIONS X259.400 TO X270.500. REPAI RED IAW DHC-8 SRM 51-20-16, 51-00-06 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002092600095 20020926 00095 NM 2002 9 26 QXEA0201457 1 20020913 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND CENTER SEAT TRACK NR 5 HAS PITTING CORROSION ON TOP RAIL AT STATION X456.000. REPAIRED IAW DHC-8 RD 8-53 -1339. 2 H 7 2 4T RT A13NM 2002092600096 20020926 00096 NM 2002 9 26 QXEA0201458 1 20020913 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND CENTER SEAT TRACK NR 5 HAS PITTING CORROSION ON TOP RAIL AT STATION X488.000. REPAIRED IAW DHC-8 SRM 51- 20-16, 51-00-06 AND RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002092600097 20020926 00097 NM 2002 9 26 QXEA0201459 1 20020913 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND CENTER SEAT TRACK NR 6 INSIDE CENTER CHANNEL HAS PITTING CORROSION AT STATION X545.000. REPAIRED IAW DHC -8 SRM 51-20-16, 51-00-06 AND RD 8-53-3644. 2 H 7 2 4T RT A13NM 2002092600098 20020926 00098 WP 2002 9 26 AALA20021117 1 20020725 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 TUL - FOUND STATION 1212-1216 TOP OF DOOR BEAM L28R, DOOR FRAME WEB CORRODED AT TWO NUTPLATES. REMVOED AND REPLACED DOO R FRAME WEB PER SRM 51-30-00. (M) 2 L 7 2 4F A6WE 2002092600099 20020926 00099 NM 2002 9 26 QXEA0201479 1 20020924 A 3350 6038441 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM ZONE 200 BURNED OUT A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 357PH * 11054 504 PDX-1ST AND 3RD OVERHEAD EMERGENCY LIGHTS IN CABIN FAIL TO ILLUMINATE. REMOVED AND REPLACED PS-3 POWER SUPPLY. OPERATION AL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092600100 20020926 00100 WP 2002 9 26 AALA20021118 1 20020719 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 TUL - FOUND CRACK IN CUSP WEB AT STATION 248 RBL 55 AND CORROSION AT STATION 245/240 RBL 55. REMOVED CRACK AND CORROSIO N AND INSTALLED REPAIR DOUBLER PER 53-00-00-02 PAGE 1. (M) 2 L 7 2 4F A6WE 2002092600101 20020926 00101 WP 2002 9 26 AALA20021119 1 20020719 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 TUL - FOUND CRACK IN CUSP STATION 240 RBL 47-49. REMOVED DAMAGED AREA. INSTALLED DOUBLER REPAIR PER AARD 53-00-00-02 P AGE 1. (M) 2 L 7 2 4F A6WE 2002092600102 20020926 00102 WP 2002 9 26 AALA20021120 1 20020723 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 TUL - FOUND TEMP REPAIR DOUBLER ON NLG JAMB SKIN JUST AFT OF LEFT STRUT DR AFT HINGE, DUE TO CRACK ON SKIN. REMOVED AND INSTALLED NEW SECTINO OF SKIN AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2002092600103 20020926 00103 WP 2002 9 26 AALA20021121 1 20020723 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 TUL - FOUND CRACK IN FUSELAGE SKIN AT STATION 1437 BETWEEN L3R AND L4R. CUT OUT DAMAGE INSTALLED FILLER AND EXTERNAL DO UBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002092600104 20020926 00104 NM 2002 9 26 QXEA0201460 1 20020913 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND OUTBOARD SEAT TRACK NR 2 HAS SEVERAL GOUGES INSIDE CENTER CHANNEL AND ON TOP RAIL AT STATION X433.000. R EPAIRED IAW DHC-8 SRM 51-20-16, 51-00-06 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002092600105 20020926 00105 WP 2002 9 26 AALA20021122 1 20020724 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 TUL - FOUND FUSELAGE SKIN CRACKED BETWEEN TWO RIVETS, STATION 1380 BELOW LONGERON 13L. CUT OUT DAMAGE, FABRICATED FILLE R AND INSTALLED EXTERNAL DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2002092600106 20020926 00106 WP 2002 9 26 AALA20021123 1 20020722 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 TUL - FOUND STATION 1332 SIDE OF VAULT DOOR FRAME. STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 53-01 FIG 2. (M) 2 L 7 2 4F A6WE 2002092600107 20020926 00107 NM 2002 9 26 QXEA0201461 1 20020913 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND CENTER SEAT TRACK NR 5 HAS CORROSION INSIDE CENTER CHANNEL AT STATION 501.000. REPAIRED IAW DHC-8 SRM 51 -20-16, 51-00-06 AND RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002092600108 20020926 00108 NM 2002 9 26 BJNA020817 1 20020803 A 5311 FRAME BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND CORROSION AT FRAME STATION 747 AT STRINGER 27 AND AT FRAME STATION 527 STRINGER 27L AND 27R. LEVEL 2 CORROSION. REMOVED CORROSION FROM STRINGER. FABRICATED AND INSTALLED 2 EACH STIFFENERS AND 2 EACH TIE REPAIRS IAW B737 SRM 51-10-6 , 51-10-2, 51-30-2, AND 53-10-4 FIGURE 6. (M) 2 L 7 2 4F RT A16WE 2002092600109 20020926 00109 NM 2002 9 26 BJNA020818 1 20020814 A 5330 PANEL BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND CORROSION IN FORWARD PIT LEFT SIDE TRANSITION PANEL FROM STATION 500B TO 520, LEVEL 2 CORROSION. REMOVED OLD TRAN SITION PANEL, FABRICATED NEW SECTION OF PANEL, INSTALLED NEW SECTION OF TRANSITION PANEL LEFT STATION 500B TO 520 IAW B7 37 SRM 51-402 FIGURE 1 AND 51-30-2. (M0 2 L 7 2 4F RT A16WE 2002092600110 20020926 00110 NM 2002 9 26 BJNA020819 1 20020806 A 5311 ANGLE BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FORWARD PIT BS 500 RBL 28 FRAME SUPPORT LOWER LEG FORWARD AND AFT HAS LEVEL 2 CORROSION. REMOVED CORROSION FABRICATED A ND INSTALLED ANGLE REPAIR IAW B737 SRM 51-20-01, 51-10-6, AND 51-10-1. (M) 2 L 7 2 4F RT A16WE 2002092600111 20020926 00111 NM 2002 9 26 BJNA020820 1 20020806 A 5320 FLOOR SUPPORT BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FORWARD PIT FLOOR SUPPORT BS 520 LBL 17 TO LBL 20 LEVEL 2 CORROSION AROUND 4 EACH NUT CLIPS AND 1 MISSING. REMOVED CORR OSION FABRICATED AND INSTALLED FLOOR SUPPORT REPAIR IAW 737 SRM 51-10-2, 51-30-2, 51-40-4, FIGURE 1 AND 53-10-1. (M) 2 L 7 2 4F RT A16WE 2002092600112 20020926 00112 NM 2002 9 26 QXEA0201462 1 20020913 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND CENTER SEAT TRACK NR 5 HAS CORROSION INSIDE CENTER CHANNEL AT STATION X510.000. REPAIRED IAW DHC-8 SRM 5 1-20-16, 51-00-06 AND RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002092600113 20020926 00113 NM 2002 9 26 BJNA020821 1 20020806 A 5313 STRINGER BOEING 737 737282 13844AT NM TAIL GOUGED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 TAIL COMPARTMENTS BS 1044 STRINGER 26L HAS DEEP CHAFE FROM BLEED AIR DUCT. CUT OUT CHAFED SECTION OF STRINGER, FABRICAT ED AND INSTALLED STRINGER REPAIR IAW 53-10-3, 51-30-2 FIGURE 1 SHEETS 1 THROUGH 8. (M) 2 L 7 2 4F RT A16WE 2002092600114 20020926 00114 NM 2002 9 26 BJNA020822 1 20020806 A 5320 TORQUE BOX BOEING 737 737282 13844AT NM FUSELAGE GOUGED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND BS 1104 TORQUE BOX LEFT CENTER SIDE HAS DEEP GOUGE. CUT OUT GOUGED AREA. FABRICATED AND INSTALLED FILLER AND DOU BLER REPAIR IAW B737 SRM 51-40-2 FIGURE 1 PAGE 1-3. (M) 2 L 7 2 4F RT A16WE 2002092600115 20020926 00115 NM 2002 9 26 BJNA020823 1 20020806 A 5320 TORQUE BOX BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND BS 1100 LEFT TOP CORNER OF TORQUE BOX NUT PLATE HAS LEVEL 2 CORROSION. CUT OUT CORRODED AREA FABRICATED AND INSTA LLED FILLER ANGLE AND RADIUS BLOCK IAW B737 SRM 51-40-5, FIGURE 1 PAGE 1. (M) 2 L 7 2 4F RT A16WE 2002092600116 20020926 00116 NM 2002 9 26 QXEA0201463 1 20020913 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- AFT CARGO DOOR APERTURE HAS CHAFE DAMAGE FROM DOOR OPENING AND THE STOP BRACKET THAT IS HITTING IT. REPAIRED IAW D HC-8 SRM 51-20-16, 51-20-26 AND RD 8-53-5461. 2 H 7 2 4T RT A13NM 2002092600117 20020926 00117 NM 2002 9 26 BJNA020824 1 20020815 A 5311 FRAME BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND FRAME AT STATION 328 HAS SURFACE CORROSION AROUND FASTENER HOLES ON UNDER SIDE OF FRAME. LEVEL 2 CORROSION. REMO VED CORROSION AT 328 FABRICATED REPAIR ANGLES IAW B737 SRM 53-10-9 PAGE 26. (M) 2 L 7 2 4F RT A16WE 2002092600118 20020926 00118 NM 2002 9 26 BJNA020825 1 20020807 A 5313 STRINGER BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 AFT AIRCRAFT INSIDE RIGHT SIDE STRINGER 17 AT FS 986.5 UNDER CUSP LONGERON HAS LEVEL 2 CORROSION. REMOVED CORROSIN FABR ICATED AND INSTALLED NEW CUSP WEB IAW B737 SRM 51-20-1, 53-10-2, FIGURE 5, 53-10-1 FIGURE 1 AND 51-10-6. (M) 2 L 7 2 4F RT A16WE 2002092600119 20020926 00119 NM 2002 9 26 BJNA020826 1 20020804 A 5230 BEAM BOEING 737 737282 13844AT NM CARGO DOOR CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 AFT CARGO COMPARTMENT DOOR INTERNAL LOWER BEAM OUTER T-CHORD AFT END IS CRACKED .25 INCH AT 3RD FASTENER FROM AFT END. REMOVED T-CHORD FABRICATED AND INSTALLED REPAIR T-CHORD AND ANGLES IAW 52-A-1079 ITEM 6. (M) 2 L 7 2 4F RT A16WE 2002092600120 20020926 00120 NM 2002 9 26 BJNA020827 1 20020815 A 5310 BEAM BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND LEVEL 2 CORROSION 4 EACH PLACES ON UPPER SURFACE OF BEAM 294.5 BETWEEN LBL 10 TO RBL 20. REMOVED CORROSION AND TR EAT. REPAINT SURFACE CHECK LIMITS. (M) 2 L 7 2 4F RT A16WE 2002092600121 20020926 00121 NM 2002 9 26 QXEA0201464 1 20020912 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- TOP FORWARD STOP ON CARGO DOOR APERTURE IS CHAFED AND WORN BY THE STOPS CONTACTING THE FITTING. REPAIRED IAW DHC-8 SRM 51-30-26. 2 H 7 2 4T RT A13NM 2002092600122 20020926 00122 NM 2002 9 26 BJNA020828 1 20020816 A 5311 FRAME BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND LEVEL 2 CORROSION UNDER 3 EACH SCREW HOLES AT FRAME RBL 28 BETWEEN BS 955 TO BS 967. REMOVED FRAME ORDERED AND RE CEIVED NEW FRAME (BEAM) DRILLED, DEBBARRD, TREATED PRIMED AND INSTALLED IAW B737-200 SRM 51-10-6 PAGE 12, 51-30-2 PAGE 3 , AND B737 MM 51-21-51 PAGE 1. (M) 2 L 7 2 4F RT A16WE 2002092600123 20020926 00123 NM 2002 9 26 BJNA020829 1 20020802 A 5311 FRAME BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FORWARD CARGO COMPARTMENT BS 480 MAIN FRAME HAS LEVEL 2 CORROSION AT STRINGER 26R UNDER TRANSITION PANEL. REMOVED CORRO SION FABRICATED AND INSTALLED FRAME REPAIR IAW SRM 51-10-2, 51-10-6, 51-30-2, AND 53-10-4 FIGURE 5. (M) 2 L 7 2 4F RT A16WE 2002092600124 20020926 00124 NM 2002 9 26 BJNA020830 1 20020805 A 5315 FLOORBEAM BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 LEVEL 2 CORROSION ON 8 EACH SCREW HOLES ON BEAM BS 986.5 BETWEEN RBL 20 TO LBL 20. REMOVED UPPER FLOORBEAM CAP AT BS 98 6.5. FABRICATED AND INSTALLED REPAIR SECTINO 2 EACH CLIPS IAW TIMCO REO-L00584 REV. (M) 2 L 7 2 4F RT A16WE 2002092600125 20020926 00125 NM 2002 9 26 QXEA0201465 1 20020911 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- RIGHT HAND INBOARD SEAT TRACK NR 7 HAS HEAVY CORROSION ON TOP RAIL AT GALLEY/LAV LOCATION. REPAIRED IAW DHC-8 SRM 51-40-11, 51-40-00, 51-30-26, RD 8-53-4473 AND 8-53-1102. 2 H 7 2 4T RT A13NM 2002092600126 20020926 00126 NM 2002 9 26 BJNA020831 1 20020810 A 5311 FRAME BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND LEVEL 2 CORROSION FORWARD PIT STATION 500 RBL 12 FRAME LOWER LEG. CORROSION REMOVED AND FOUND REMAINING MATERIAL OUT OF LIMITS, FABRICATED, TRIMMED DRILLED, ALODINED PRIMED AND INSTALLED REPAIR IAW B737 SRM 51-10-6, 53-10-1, 53-10-4 FIGURE 6 PAGE 13-15. (M) 2 L 7 2 4F RT A16WE 2002092600127 20020926 00127 NM 2002 9 26 QXEA0201466 1 20020911 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- AFTER NR 2 DME ANTENNA REMOVED THERE WAS CORROSION FOUND ON THE FUSELAGE SKIN. REPAIRED IAW DHC-8 SRM 51-00-06, 51 -00-04, 53-00-16 AND 51-20-16. 2 H 7 2 4T RT A13NM 2002092600128 20020926 00128 NM 2002 9 26 BJNA020832 1 20020827 A 5511 SPAR BOEING 737 737282 13844AT NM HORIZONTAL STAB CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND LT HORIZONTAL STAB CENTER SECTION REAR SPAR TOP CHORD FORWARD LUG HAS LEVEL 2 CORROSION INSIDE BORE. REMOVED CORR OSION BORED I/D OF LUG TO 1.564 INCH, ROTO TREATED AND INSTALLED BUSHING. (M) 2 L 7 2 4F RT A16WE 2002092600129 20020926 00129 NM 2002 9 26 BJNA020834 1 20020805 A 5315 FLOORBEAM BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND LEVEL 2 CORROSION ON FLOORBEAM BS 328 AT EACH SCREW HOLE AT RBL 32. REMOVED EXISTING REPAIR IN AREA. REMOVED COR ROSION FOUND REMAINING MATERIAL TO BE OUT OF LIMITS, FABRICATED REPAIR ANGLES FROM BAC1490-2734 33 INCHES AND 31 INCHES. INSTALLED IAW B737 SRM 53-10-9, FIGURE 6, 53-10-2 FIGURE 7 53-10-1 FIGURE 1 AND REO-L00 591 REV 1R DATED 08/23/2002. (M) 2 L 7 2 4F RT A16WE 2002092600130 20020926 00130 WP 2002 9 26 GTIA020576 1 20020527 A 5414 SKIN DOUG DC9 DC983 3022083 WP NR NACELLE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 DTW - FOUND ON DAILY INSPECTION, FOUND NR 2 ENGINE UPPER COWL DELAMINATED MIDWAY ALONG LENGTH. SUSPECT BLEED DUCT LEAKA GE. INTERIM EXTERNAL DOUBLER REPAIR INSTALLED ON RIGHT UPPER COWL DOOR EXTERNAL SURFACE PER SPIRIT AIRLINES EA 7110-020 2 ON C/O 28664-2. (M) 2 L 7 2 4F RT A6WE 2002092600131 20020926 00131 WP 2002 9 26 GTIA020843 1 20020727 A 3260 H1410051 LIGHT DOUG DC9 DC932 3022066 WP MLG INDICATOR INOPERATIVE A GTIA O OTHER J WARNING INDICATION LD LANDING 1 GL 23 12536 47113 FLT 276 - TPA - FOUND RIGHT LANDING GEAR BUTTON INDICATOR LIGHT INOPERATIVE, GREEN LENS. REMOVED AND REPLACED GEAR DOWN LOCK SWITCH ON RIGHT MAIN GEAR AND OPS CHECKED IAW MM 32-60-01. OPS CHECK NORMAL. CLOSED AS OF 8/28/02. (M) 2 L 7 2 4F A6WE 2002092600132 20020926 00132 2002 9 26 QXEA0201467 4 20020914 A 3418 STALL WARNING BOMBDR DHC8 DHC8401 1390041 NM COCKPIT MALFUNCTIONED A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 407QX 4049 GEG - CREW ABORTED TAKEOFF, RECEIVED A AURAL WARNING BETWEEN 50 AND 70 KTS. MAINTENANCE INSPECTED THE AIRCRAFT AND PERF ORMED STALL WARNING TESTS 1 AND 2 IAW FSM P-38 AND 3-40. MAINTENANCE ALSO INTERROGATED THE ARCDU IN ALL CATEGORIES. NO DEFECTS WERE NOTED. OPERATIONAL CHECK FLIGHT WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092600133 20020926 00133 WP 2002 9 26 GTIA020915 1 20020713 A 5751 SKIN DOUG DC9 DC981 3022081 WP RT AILERON DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND RIGHT OUTBOARD AILERON TAB DELAMINATED ON LOWER SURFACE AT INBOARD END AND AT CENTER HINGE. REMOVED RIGHT A ILERON OUTBOARD TAB. DAMAGE EXCEEDS MD80 SRM REPAIR LIMITS. INSTALLED RIGHT OUTBOARD AILERON TAB. (M) 2 L 7 2 4F A6WE 2002092600134 20020926 00134 NM 2002 9 26 QXEA0201468 1 20020916 A 3260 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM COCKPIT ILLUMINATED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 410QX 4053 SEA - AIRCRAFT RETURNED TO FIELD AFTER TAKEOFF, THE RIGHT MAIN GEAR INDICATED RED AFTER RETRACTION. AIRCRAFT DOWN FOR M AINTENANCE AND INSPECTION. 2 H 7 2 4T RT A13NM 2002092600135 20020926 00135 WP 2002 9 26 GTIA020916 1 20020725 A 5315 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AT FS 236 6L LONGERON CRACKED. REMOVED LONGERON SPLICER AND DAMAGED LONGERON. FABRICATED NEW LONGERON SECT ION AND REPAIR SPLICE. INSTALLED NEW LONGERON AND SPLICES. (M) 2 L 7 2 4F A6WE 2002092600136 20020926 00136 NM 2002 9 26 QXEA0201470 1 20020916 A 5210 HANDLE DHAV DHC8 DHC8202 2809007 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 360PH 515 SEA- FLIGHT ATTENDANT REPORTS THAT MAIN CABIN DOOR IS HARD TO OPERATE. CLEANED AND LUBED HANDLE. NO PARTS REPLACED. O PERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092600137 20020926 00137 WP 2002 9 26 GTIA020917 1 20020712 A 5523 SKIN DOUG DC9 DC981 3022081 WP ELEVATOR TAB DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND LEFT ELEVATOR CONTROL TAB UPPER SURFACE DELAMINATED AT 2/3 HINGE FITTINGS. REMOVED LEFT ELEVATOR CONTROL TA B. REPAIRED LEFT ELEVATOR CONTROL TAB. INSTALLED LEFT ELEVATOR TAB. (M) 2 L 7 2 4F A6WE 2002092600138 20020926 00138 EA 2002 9 26 QXEA0201471 1 20020916 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 604QX 10019 BOI- CENTER CHIMNEY ON FORWARD CARGO BAY IS DAMAGED. REMOVED AND REPLACED FORWARD CARGO BAY CHIMNEY. OPERATIONAL CHECK S GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002092600139 20020926 00139 NM 2002 9 26 QXEA021386 1 20020819 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX- DEFORMATION DAMAGE TO STRINGER 165 AT STATION X-151. REPAIRED IAW HORIZON AIR EA 2-53-415. 2 H 7 2 4T RT A13NM 2002092600140 20020926 00140 NM 2002 9 26 QXEA021387 1 20020819 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX- SMOOTH DEFORMATION DAMAGE TO STRINGER 165 AT STATION X-151. THIS IS THE POINT OF GREATEST DEFORMATION WITH 9 INCH TAPER TO ZERO DAMAGE FORWARD AND AFT STRINGER APPEARS TO BE PUSHED IN APPROXIMATELY .25 INCH AT GREATEST POINT. REPAIRE D IAW HORIZON AIR EA 2-53-415. 2 H 7 2 4T RT A13NM 2002092600141 20020926 00141 NM 2002 9 26 QXEA021447 1 20020909 A 5410 STRUT DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- NR 2 ENGINE LOWER OUTBOARD STRUT IS CHAFED ON INNER SURFACE. REPAIRED IAW DHC-8 RD 8-54-036. 2 H 7 2 4T RT A13NM 2002092600142 20020926 00142 NM 2002 9 26 OZIA200243009 1 20020924 A 3310 OL3092 LAMP DORNER DO32 DO328300 NM BURNED OUT A OZIA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 430Z 3127 Right main gear "green down arrow" not illuminated when gear selected down. 2 H 7 2 4T RT A55NM 2002092600143 20020926 00143 WP 2002 9 26 GTIA020918 1 20020712 A 5523 SKIN DOUG DC9 DC981 3022081 WP LT ELEVATOR TAB DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND LEFT ELEVATOR GEAR TAB DELAMINATED LOWER SURFACE AT 1/B AND OUTBOARD SIDES. REMOVED GEARED TAB. REPAIRED L EFT ELEVATOR GEARED TAB. INSTALLED GEARED TAB ON LEFT ELEVATOR. (M) 2 L 7 2 4F A6WE 2002092600144 20020926 00144 WP 2002 9 26 GTIA020919 1 20020712 A 5523 SKIN DOUG DC9 DC981 3022081 WP RT ELEVATOR TAB DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND RT ELEVATOR CONTROL TAB IS DELAMINATED UPPER LOWER. REMVOED RIGHT ELEVATOR CONTROL TAB. TAB HAS CORROSION DAMAGE TO FRONT. REPLACED CONTROL TAB. INSTALLED RIGHT ELEVATOR CONTROL TAB. (M0 2 L 7 2 4F A6WE 2002092600145 20020926 00145 WP 2002 9 26 GTIA020920 1 20020712 A 5523 STRUCTURE DOUG DC9 DC981 3022081 WP ELEVATOR TAB CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND RIGHT ELEVATOR ANTI-FLOAT TAB LOWER SURFACE LE HAS CORROSIN FROM INBOARD SIDE TO OUTBOARD SIDE. MATERIAL LO SS FOUND TO BE OUT OF LIMITS. REMOVED RIGHT ELEVATOR ANTI-FLOAT TAB. INSTALLED RIGHT ELEVATOR ANTI-FLOAT TAB. (M) 2 L 7 2 4F A6WE 2002092600146 20020926 00146 WP 2002 9 26 GTIA020921 1 20020716 A 5310 BEAM DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PIT STATION 1155-1212 L28R, REPAIR STRAP ON DOOR JAMB BEAM IS CORRODED. REMOVED CORROSION AND INTERCOST AL. FABRICATED INTERCOSTAL AND ANGLES. INSTALLED CLIPS BRACKETS, ANGLES AND NEW INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002092600147 20020926 00147 WP 2002 9 26 GTIA020922 1 20020716 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND PIT STATION 1148-1220 L27R-L29R, THRESHOLD CLOSURE WEB HAS AREAS OF CORROSION ON UPPER AND LOWER SURFACES. REMOVED WEB. FABRICATED NEW WEB. INSTALLED WEB. (M) 2 L 7 2 4F A6WE 2002092600148 20020926 00148 WP 2002 9 26 GTIA020923 1 20020716 A 5310 BEAM DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CARGO DOOR JAMB BEAM CORRODED FS 636 TO 693. REMOVED JAMB BEAM MID CARGO DOOR AND BRACKETS. FABRICATED BRA CKETS AND CENTER BACK. LOCATED AND DRILLED NEW JAMB BEAM. INSTALLED JAMB BEAMS MID CARGO DOOR AND CORNER BRACKET. (M) 2 L 7 2 4F A6WE 2002092600149 20020926 00149 WP 2002 9 26 GTIA020924 1 20020716 A 5330 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - ANTENNA INNER DOUBLER CORRODED FS 675 TO 685 STRINGER 29R TO 27L. REMOVED ANTENNA DOUBLER. LOCATED AND DRILLED N EW ANTENNA DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2002092600150 20020926 00150 WP 2002 9 26 GTIA020925 1 20020716 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FUSELAGE INNER SKIN CORRODED FS 788 STRINGER 28L TO 28R. REMOVED LONGERON 30. REMOVED CORROSION ON LONGER 30 AND DAMAGED SKIN. LOCATED AND DRILLED NEW LONGERON 30. FABRICATED FILLERS, REPAIR DOUBLER, REPAIR TRIPLER AND REPAIR SECT ION OF FORMER. INSTALLED FILLERS, DOUBLERS, TRIPLERS, SECTION OF FORMER AND SPLICE. (M) 2 L 7 2 4F A6WE 2002092600151 20020926 00151 WP 2002 9 26 GTIA020926 1 20020717 A 5311 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - AFT PIT STATION 1309 L30-L23L, AREAS OF CORROSION ON FORWARD AND AFT SIDES OF FRAME. REMOVED SECTION OF DAMAGE. LOCATED AND DRILLED NEW FRAME SECTION. INSTALLED FRAME. (M) 2 L 7 2 4F A6WE 2002092600152 20020926 00152 WP 2002 9 26 GTIA020927 1 20020726 A 5320 59366711 STRAP DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PIT STATION 1212 HAS CORROSION AT THE STRAP. REMOVED STRAP. LOCATED NEW STRAP. INSTALLED NEW STRAP. (M) 2 L 7 2 4F A6WE 2002092600153 20020926 00153 WP 2002 9 26 GTIA020929 1 20020822 A 3350 SIGN DOUG DC9 DC983 3022083 WP EXIT SIGN BROKEN A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 809NK 49503 DEN - FLT 982 - RIGHT DOOR EMERGENCY 'EXIT' ILLUMINATOR BROKEN. REMOVED AND REPLACED R-1 DOOR LUMINATOR. (M) 2 L 7 2 4F RT A6WE 2002092600154 20020926 00154 WP 2002 9 26 GTIA020931 1 20020724 A 5315 FLOORBEAM DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FLOORBEAM WEB SUPPORT CORRODED STATION 1309 L23L. FABRICATED REPAIR PART. FABRICATED PART AND REINSTALLED. (M) 2 L 7 2 4F A6WE 2002092600155 20020926 00155 WP 2002 9 26 GTIA020932 1 20020718 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFTER REMOVAL OF THRESHOLD TO FOM FLOOR SUPPORT WAS FOUND TO BE EXFOLIATED AT STATION 190, APPROX LBL 54 APP ROX. REMOVED FLOOR SUPPORT. DRILLED AND LOCATED THE ANGLE SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002092600156 20020926 00156 WP 2002 9 26 GTIA020933 1 20020819 A 3397 CONNECTOR DOUG DC9 DC981 3022081 WP EXIT SIGN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND L1 DOOR EXIT MARKER INOPERATIVE. RESOLDERED CONNECTION ON L1 EXIT IDENTIFIER. (M) 2 L 7 2 4F A6WE 2002092600157 20020926 00157 WP 2002 9 26 GTIA020934 1 20020819 A 3397 CONNECTOR DOUG DC9 DC981 3022081 WP LIGHT LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 14. FOUND DEFECTIVE TERMINAL CONNECTION. REPAIRED TERMINAL. (M ) 2 L 7 2 4F A6WE 2002092600158 20020926 00158 WP 2002 9 26 GTIA020936 1 20020817 A 3350 SIGN DOUG DC9 DC981 3022081 WP CABIN CHAFED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND RIGHT OVERWING EXIT IDENTIFIERS, BOTH FORWARD AND AFT ARE INOPERATIVE. REMOVED RIGHT FORWARD AND SFT EXIT I DENTIFIERS. RESOLDERED CONNECTIONS ON FORWARD AND AFT EXIT IDENTIFIERS. (M) 2 L 7 2 4F A6WE 2002092600159 20020926 00159 WP 2002 9 26 GTIA020937 1 20020716 A 5313 SPLICE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND STRINGER 30 SPLICE FITTING CORRODED FS 579-595. DUPLICATED LONGERON SPLICE. SPLICES FS 579-FS 595 TO BE IN STALLED ON WC B00038 118 N 00108. (M) 2 L 7 2 4F A6WE 2002092600160 20020926 00160 WP 2002 9 26 GTIA020938 1 20020716 A 5313 STRINGER DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND STRINGER 30 CORRODED FS 617 TO 610, FS 617-636, 636-655, 674-655. FOUND TO BE OUT OF LIMITS. REMOVED LONGE RON REPAIR STATION. FABRICATED LONGERON SPLICES AND REPAIR STATION. INSTALLED LONGERON 30 AND SPLICES REPAIR. (M) 2 L 7 2 4F A6WE 2002092600161 20020926 00161 WP 2002 9 26 GTIA020939 1 20020716 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PIT STATION 1193 L28R-L29R, INTERCOSTAL CORRODED. REMOVED INTERCOSTAL AND SUPPORT ANGLES. FABRICATED I NTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002092600162 20020926 00162 WP 2002 9 26 GTIA020940 1 20020716 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PIT STATION 1212 L28R-L29R, INTERCOSTAL CORRODED. REMOVED INTERCOSTAL AND SUPPORT ANGLES. FABRICATED N EW INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002092600163 20020926 00163 WP 2002 9 26 GTIA020941 1 20020716 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP FS 1202 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PIT STATION 1212 L28R-L29R, INTERCOSTAL CORRODED. REMOVED INTERCOSTAL AND SUPPORT ANGLES. FABRICATED N EW INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002092600164 20020926 00164 WP 2002 9 26 GTIA020942 1 20020707 A 5230 SKIN DOUG DC9 DC981 3022081 WP CARGO DOOR DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - THREE DENTS UNDER AFT CARGO DOOR LOWER FUSELAGE TWO DENTS APPROX 4 INCHES LONG BY .125 INCHES DEEP 1 DENT APPROX 3 INCHES LONG BY .125 INCHE DEEP. REMOVED DAMAGE AREA. FABRICATED OF THE 3, 5, 7, 9, 11, 13 AND 15. INSTALLED REPAIR P ART. (M) 2 L 7 2 4F A6WE 2002092600165 20020926 00165 WP 2002 9 26 GTIA020943 1 20020707 A 5754 SKIN DOUG DC9 DC981 3022081 WP NR 5 SLAT DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - RIGHT LEADING EDGE SLAT NR 5 DAMAGED TO APPROX 6 INCHES FROM OUTBOARD TIP, TEMPORARY REPAIR INSTALLED. REMOVED RI GHT LE NR 5 SLAT. REMOVED INNER SKIN AND CRACKED RIB. FORMED NEW RIB. INSTALLED RIB AND INNER SKIN. (M) 2 L 7 2 4F A6WE 2002092600166 20020926 00166 WP 2002 9 26 GTIA020944 1 20020816 A 2820 LINE DOUG DC9 DC981 3022081 WP FUEL SYSTEM LOOSE A GTIA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FUEL IN AFT CARGO PIT AT STATION 1320 LEFT. FOUND ENGINE FUEL FEED LINE AFT SHROUD TO HAVE A LOOSE CONNECTI ON AND A BROKEN O-RING. REPLACED O-RING AND CONNECTED FUEL LINE. (M) 2 L 7 2 4F A6WE 2002092600167 20020926 00167 WP 2002 9 26 GTIA020945 1 20020823 A 3397 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 825NK 53012 DTW - L1 AND R1 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED WIRES AND OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2002092600168 20020926 00168 WP 2002 9 26 GTIA020946 1 20020824 A 3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083 WP MLG DOOR CONTAMINATED A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 824NK 53015 FLT 9824 - FTW - DOOR OPEN LIGHT CAME ON CLIMBING THROUGH 30 FT THEN WENT OUT AFTER 30 MIN DID QRH PROCEDURE. INSPECTED , CLEANED GEAR DOOR PROX SENSOR AND CHECKED FOR PROPER CLEARANCE. PERFORMED GROUND CHECK OF GEAR DOOR INDICATIONS ALL O P NORMAL NO LIGHT ON WITH DOOR CLOSED. (M) 2 L 7 2 4F RT A6WE 2002092600169 20020926 00169 EU 2002 9 26 AWXA200200923 1 20020925 A 3350 ABS0374A24 CABLE AIRBUS 320 A320232 3930326 EU SEAT ROW 19 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 0 0 953 PHX - EEL - DURING P-08 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H WAS FOUND INOPERATIVE. MAINTENANCE RE PAIRED BROKEN SPLICE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H IAW ESPM 20-25-21; OPS CHECK OF EMERGENCY CABIN L IGHTING WAS GOOD. 2 L 7 2 4F RT A28NM 2002092600170 20020926 00170 NM 2002 9 26 AWXA200200925 1 20020907 A 5414 311A14509 DOUBLER BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 0 0 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 1/8" CRACK WAS FOUND ON FLANGE OF #1 NACELLE ACCESS PANEL 5727L. MAINTENANCE STOP DRILLED HOLES AND PERFORMED A HFEC INSPECTION TO VERIFY CRACKS WERE CONTAINED; REMOVED NECESSARY FASTENERS; FABRICA TED A REPAIR DOUBLER, AND INSTALLED REPAIR PARTS IAW AWA E.R. 03-5433-00340-DL1. 2 L 7 2 4F RT A16WE 2002092600171 20020926 00171 NM 2002 9 26 AWXA200200926 1 20020910 A 5410 65C2630812 ANGLE BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 0 0 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND ON THE #2 PYLON AFT PANEL ATTACH ANGLE RADIATING FROM THE LO WER AFT NUTPLATE HOLE. MAINTENANCE REMOVED AND REPLACED THE 32 PYLON AFT PANEL ATTACH ANGLE IAW B737-300 SRM 51-40-02, P G. 38, 44-45, & 63, FIG. 8, 12, & 14., AND SRM 51-40-05, PG. 2-4, & 16, FIG. 1 & 2. 2 L 7 2 4F RT A16WE 2002092600172 20020926 00172 NM 2002 9 26 AWXA200200927 1 20020905 A 5314 65458668 SKIN PANEL BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 0 0 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND ON L/H MAIN LANDING GEAR WHEEL WELL KEEL BEAM OUTER SKIN BS 716. MAINTENANCE REMOVED KEEL BEAM OUTER SKIN PANEL; FABRICATED A NEW REPLACEMENT SKIN PANEL AND 2 EACH INNER DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5331-01025-SS1A. 2 L 7 2 4F RT A16WE 2002092600173 20020926 00173 EU 2002 9 26 MALA020575 1 20020925 A 4920 LF5071F ENGINE BAC 146 AVRO146RJ85A 1500097 EU A MALA D RETURN TO BLOCK O OTHER NR NOT REPORTED 1 GL 15 523XJ E2348 #3 ENGINE WOULD NOT START AFTER APU SHUTDOWN. STARTED OPERATING AND IGNITION LIGHTS ILLUMINATED BUT NO ENGINE ROTATION NOTED. MAINTENANCE FOUND OIL BYPASS PIN EXTENDED, AND MAIN CHIP DETECTOR CONTAMINATED, CONDITION 3. INSTALLED #3 ENGINE FERRY KIT IAW TASK CARD THREE ENGINE FERRY/ FLIGHT TO BE CONDUCTED IAW AVRO AFM APPENDIX 4. MAINTENANCE INSPECTED #3 ST ARTER SHAFT-VERIFIED SHEARED. FOUND ENGINE OIL BYPASS POPPED AND MAIN CHIP DETECTOR CONTAMINATED MSP MAINTENANCE REMOVE D AND REPLACED #3 ENGINE IAW TASK CARD 7100-502. 2 H 7 4 4F RT A49EU 2002092600174 20020926 00174 NM 2002 9 26 SWAA022155 1 20020917 A 3350 300432 LIGHT BOEING 737 7372H4 138448C NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 081SW 22730 DURING SCHEDULED A2 CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHT INOP AT BS 727D. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2002092600175 20020926 00175 EU 2002 9 26 C2XA02IA203 1 20020925 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 86842 286 IAH- THE CREW REPORTED THAT NUMEROUS EMERGENCY LIGHTS FAIL TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE E MERGENCY LIGHT BATTERY PACK, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002092700005 20020927 00005 WP 2002 9 27 AAL2002F00017 1 20020808 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 34931 53284 SEAT TRACK NR 3, CORRODED AT STA 1232, STA 1275, AND STA 1300. C/A: SPLICED IN SERVICEABLE SEAT TRACK FROM STA 1185 TO STA 1309 IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002092700006 20020927 00006 WP 2002 9 27 AAL2002F00018 1 20020731 A 5320 WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 34931 53284 CUSP WEB, CRACKED AND CORRODED AT STA 150 TO STA 170. REPLACED CUSP WEB SHEET, STA 150 TO STA 170 IAW SRM. (AMC4) 2 L 7 2 4F 4 F RT A6WE E2EA 2002092700007 20020927 00007 WP 2002 9 27 AAL2002F00019 1 20020725 A 5330 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 53284 FUSELAGE SKIN, DENT IN FUSELAGE, STA 180 L4L ABOVE MAIN ENTRY DOOR. BUMPED OUT DENT AND INSTALLED TWO ROW DOUBLER IAW S RM. DYE CHECKED, NO CRACKS FOUND. (AMC4) 2 L 7 2 4F 4 F RT A6WE E2EA 2002092700008 20020927 00008 WP 2002 9 27 AAL2002F00020 1 20020724 A 5320 WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 34931 53284 CORROSION ON CUSP WEB UNDERNEATH GALLEY TIE DOWN, INBOARD OF SEAT TRACK NR 4 AT STA 218. INSTALLED DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002092700009 20020927 00009 WP 2002 9 27 AAL2002F00022 1 20020724 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 53284 NR 1 SEAT TRACK GALLEY MOUNT CORRODED AT STA 1234. C/A: REMOVED CORROSION BY ROUTING OUT INSTALLED PLUG AS IAW SRM. TR EATED AND PRIMED. 2 L 7 2 4F 4 F RT A6WE E2EA 2002092700010 20020927 00010 WP 2002 9 27 AAL2002F00023 1 20020724 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 53284 NR 1 SEAT TRACK TOPSIDE AND GALLEY MOUNT HOLE CORRODED STA 1209. REMOVED CORROSION BY ROUTING OUT. INSTALLED PLUG REPA IR IAW SRM. TREATED AND PRIMED IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002092700011 20020927 00011 WP 2002 9 27 AAL2002F00024 1 20020725 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 53284 NR 4 SEAT TRACK CORRODED AT STA 237. INSTALLED SEAT TRACK PLUG IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002092700012 20020927 00012 SO 2002 9 27 BLIA512C8502 2 20020805 A 8500 534728 SHAFT CESSNA 421 421B 2076014 CE CONT O520 GTSIO520H 17032 SO IDLER FAILED E BLIA A UNSCHED LANDING R B PARTIAL RPM/PWR LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 17 65AE 1176 423 421B0953 817538R DURING CLIMB TO MK LEVELED AT 18K. ENGINE OPS BECAME ROUGH, THEN TACH WENT TO ZERO. PILOT OBSERVED SMOKEY MIST FROM L OUVERS. ENGINE TURNED OFF AND FEATHERED. DECLARED EMERGENCY AND LANDED. INSPECTED AND FOUND IDLER SHAFT LOOSE IN NACE LLE. AIRCRAFT IN STORAGE TIL MAINTENANCE ACTION IS ORGANIZED. LARGE AMOUNT OF OIL WAS OBSERVED IN FLIGHT, STREAMING OU T AFTER SHUTDOWN AND IS CURRENTLY ALL OVER NACELLE. ENGINE WILL BE REMOVED AND SENT FOR EVALUATION AND REPAIR. 1 L 7 2 3O 3 O A7CE E7CE 2002092700013 20020927 00013 SO 2002 9 27 MW22002F00000 2 20020715 A 8520 649898 CRANKSHAFT CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO ENGINE BROKEN A MW2R K NONE O OTHER IN INSP/MAINT 1 GL 17 3963G 3931 860 340A0246 CRANKSHAFT BROKEN IN TWO PIECES AT NR 3 ROD CHEEK. 1 L 7 2 3O 3 O 3A25 E8CE 2002092700014 20020927 00014 SW 2002 9 27 RW82002F00000 1 20020907 A 2910 70061H000A180A LINE BELL 206 206B 1181511 SW HYD SYSTEM FAILED E RW8A O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 21 894HA 3278 THE HYDRAULIC PRESSURE LINE FROM THE PUMP HAD FAILED. THE CLAMP THAT SECURES THE HOSE TO THE PYLON DECK HAD CHAFED INTO THE STEEL BRAIDING OF THE LINE, CAUSING A WEAK POINT IN THE LINE, AND THE WALL OF THE HOSE TO RUPTURE THROUGH THE BRAID ING. THUS CAUSING A TOTAL HYDRAULIC FAILURE. THE CAUSE OF THE HOSE FAILURE IS THE ALIGNMENT OF THE CLAMP ON THE HOSE. 1 G 7 1 3U H2SW 2002092700015 20020927 00015 SW 2002 9 27 Y3AR527Y 1 20020918 A 5302 2060312329103S FITTING BELL 206 206L4 1182110 SW ALLSN 250C 250C30 03013 GL TAILBOOM CRACKED B Y3AR K NONE O OTHER IN INSP/MAINT 1 SW 03 357SP 1399 52161 DURING 100 HOUR ANNUAL INSPECTION FOUND LT UPPER FITTING ON THE FUSELAGE SIDE OF THE TAILBOOM ATTACHMENT CRACKED. REMOV ED AND REPLACED FITTING (PN 206031329103S) MM. FITTING IS CRACKED ON THE OUTBOARD FLANGE BETWEEN THE 2 AFT RIVETS. 1 G 7 1 3U 3 U NC H2SW E1GL 2002092700020 20020927 00020 NE 2002 9 27 2002F00905 2 20020828 A 7320 FFG022AD GOVERNOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE INOPERATIVE G D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 522AT 4953 4953 29330 31391 (SUPP-CLOSED) FLIGHT NUMBER 108. RT EEC AND ENGINE LIMITER INOP LIGHT ILLUMINATED. EICAS MESSAGE "RT ENGINE EEC, RT ENGI NE" LIMITER DISPLAYED. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE FUEL FLOW GOVERNOR PER M.M. 73-21-01. OPS CHECK AND LEAK CHECK GOOD PER M.M. 71-00-00-5 TESTS 1,2,9, AND 10. 2 L 7 2 4F 4 F RT A2NM E12EU 2002092700021 20020927 00021 NM 2002 9 27 2002F00906 1 20020917 A 7100 B-NUT BOEING 757 75728A 1384976 NM RT ENGINE LOOSE G K NONE J WARNING INDICATION CR CRUISE 1 GL 11 521AT 24368 (ORIG-CLOSED) FLIGHT NUMBER 205. DURING CRUISE EICAS MSG RT ENG OVHT DISPLAYED. EXTINGUISHED AFTER THRUST REDUCTION. MAI NTENANCE TROUBLESHOT PER FIM 26-12-00 FOUND LOOSE B-NUT LINE ON PRSOV LINE. TIGHTENED LINE & TEST NR 4 COMPLIED WITH. SY STEM CHECKED OK. 2 L 7 2 4F RT A2NM 2002092700022 20020927 00022 NE 2002 9 27 2002F00907 2 20020919 A 7320 1853M33P06 EEC BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE NR 1 ENGINE INOPERATIVE G D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 306TZ 3121 3121 32348 889536 (ORIG CLOSED) NR 1 ENGINE CONTROL AMBER LIGHT ILLUMINATED AFTER ENGINE START. RETURNED TO GATE. REMOVED & REPLACED LT EN GINE (EEC) ELECTRONIC ENGINE CONTROL IN ACCORDANCE WITH MAINTENANCE MANUAL. SYSTEM CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002092700023 20020927 00023 WP 2002 9 27 200201206 1 20020918 A 7100 ENGINE LKHEED 1011 10113851 5265010 WP NR 2 BIRD INGESTION A AMTA E ENGINE SHUTDOWN C F.O.D. TO TAKEOFF 1 GL 11 188AT 193C1078 NR 2 ENGINE SHUTDOWN FOR HIGH VIBS, 2.6 BOTH CHANNELS. OIL PRESSURE 19 PSI, ALL PARAMETERS NORMAL. INSPECTED INLET AND EXHAUST , REMOVED EVIDENCE OF BIRD STRIKE FROM ONE BLADE, INSPECTED CHIP DETECTORS (NO DEBRIS FOUND), RAN ENGINE ANE PE RFORMED TEST NR 11. VIBS WITHIN NORMAL RANGE. 2 L 7 3 4F A23WE 2002092700024 20020927 00024 SO 2002 9 27 000197 1 20020910 A 3110 WARNING LIGHT EMB 145 EMB145 3260210 SO COCKPIT ILLUMINATED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 263 E 1-2 REV DISAGREE AND LG AIR/GND FAIL ON EICAS. FIRE DETECT FAIL. SERVICED NOSE STRUT AND RR'D FIRE LOOP 2 L 7 2 4F RT T00011AT 2002092700025 20020927 00025 SO 2002 9 27 000198 1 20020912 A 3110 WARNING LIGHT EMB 145 EMB145 3260210 SO COCKPIT ILLUMINATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 291 E2 REV DISAGREE MSG ON EICAS. DEFERRED E2 THRUST REVERSER 2 L 7 2 4F RT T00011AT 2002092700026 20020927 00026 SO 2002 9 27 000200 1 20020923 A 3150 WARNING LIGHT EMB 145 EMB145 3260210 SO COCKPIT ILLUMINATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 292 T/O FLAP CONFIG PROBLEM. RESET A/C AND OPS CHECK GOOD 2 L 7 2 4F RT T00011AT 2002092700027 20020927 00027 NE 2002 9 27 000201 2 20020925 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT FAILED A CHQA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 11 104 PILOT REPORTS ON CLIMB OUT LT ENGINE OVT TEMP LIGHT CAME ON. PILOT REDUCED POWRE TEMP. STILL STAYED AT 900 DEGREE'S LT P ROP WENT INTO AUTOCOARSENING PILOT SHUT DOWN LT ENGINE 2 L 7 2 4T 4 T RT A52EU E8NE6 2002092700028 20020927 00028 SO 2002 9 27 CHQ000196 1 20020910 A 3150 WARNING LIGHT EMB 145 EMB145 3260210 SO COCKPIT ILLUMINATED A CHQA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 GL 11 263 E 1-2 REV DISAGREE AND LG AIR/GND FAIL ON EICAS. SERVICED NOSE STRUT 2 L 7 2 4F RT T00011AT 2002092700029 20020927 00029 EU 2002 9 27 00043 1 20020918 A 3241 N2F190130 SWITCH AMD FALC20 FALCON 2720302 EU ANTI SKID TEST FAILED E HAEA O OTHER O OTHER LD LANDING 1 SW 05 165TW 65 LANDING AT KYIP AIRCRAFT HAD NO BRAKING ACTION ON SYSYTEM NR 1 , CAPT TOOK CONTROL OF AIRCRAFT AND WENT TO SYSTEM NR 2 , AIRCRAFT BEGAN TO SLOW, CAPT TURNED AIRCRAFT THRU GRASS AND BACK ON TO THE TAXI WAY TO HELP SLOW THE AIRCRAFT. NO DAMA GE TO AIRCRAFT OR AIRPORT. MAINTENANCE REMOVED AND REPLACED ANTI SKID TEST SWITCH. OPERATIONAL CHECK OF BRAKES SYSTEM NR 1 AND 2 WITH NO DEFECTS FOUND.RETURN AIRCRAFT TO SERVICE. 2 L 7 2 4F A7EU 2002092700030 20020927 00030 EU 2002 9 27 00044 1 20020924 A 7931 TRANSDUCER AMD FALC20 FALCON 2720302 EU RT ENGINE OIL FAILED E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 221TW 221 AIRCRAFT DEPARTED SDF FOR RFD AFTER REACHING 13,000 MSL THE RT ENGINE OIL PRESSURE LIGHT CAME ON AND INDICATION WAS IN T HE RED, OIL TEMP WAS NORMAL, ENGINE WAS SHUT DOWN AND SECURED, AIRCRAFT RETURNED TO SDF. MAINTENANCE SWAPPED OIL PRESS URE TRANSDUCERS AND PERFORMED ENGINE RUNS, CHECKED BOTH CHIP DETECTORS AND OIL FILTER WAS CLEANED, NO PROBLEMS FOUND OP CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE, NO OIL PRESSURE INDICATING PROBLEMS ON NEXT FLIGHT. 2 L 7 2 4F A7EU 2002092700031 20020927 00031 NM 2002 9 27 CALA0200469 1 20020920 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 500C CRACKED A CALA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND A 1/2" CRACK IN STRINGER 16R FORWARD OF ICE LIGHT AT BS 500C. THE STRINGER SECTION WAS REPLACED IAW SRM 53-00-03, FIGURE 202. 2 L 7 2 4F RT A16WE 2002092700032 20020927 00032 NM 2002 9 27 CALA0200470 1 20020922 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM STA 947.5-967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 947.5-967, LBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51- 40-02. 2 L 7 2 4F RT A16WE 2002092700033 20020927 00033 NM 2002 9 27 CALA0200471 1 20020924 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 500. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2002092700034 20020927 00034 NM 2002 9 27 CALA0200472 1 20020924 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND FORWARD PIT DOOR CUTOUT AFT JAMB R/H LOWER WEB CORRODED ON UNDERSIDE AT STA 500. A WEB SPLICE REPAIR WA S INSTALLED IAW SRM 51-70-13, FIGURE 1. 2 L 7 2 4F RT A16WE 2002092700035 20020927 00035 NM 2002 9 27 CALA0200473 1 20020925 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM STA 747-767 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND R/H INTERCOSTAL IN AFT CARGO AREA CORRODED AT STA 747-767, RBL 22. THE INTERCOSTAL WAS REMOVED AND REPL ACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002092700036 20020927 00036 NM 2002 9 27 CALA0200474 1 20020925 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 794-847 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND AFT BAG BIN THRESHOLD LOWER SUPPORT WEB CORRODED IN SEVERAL SPOTS AT STA 794-847, S26R. THE SUPPORT WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002092700037 20020927 00037 NM 2002 9 27 CALA0200475 1 20020925 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM ABB THRESHOLD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND AFT BAGGAGE BIN THRESHOLD FORWARD WEB SUPPORT CORRODED. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2002092700038 20020927 00038 WP 2002 9 27 CALA0200476 1 20020925 A 5311 FRAME DOUG DC9 DC983 3022083 WP STA 1463 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 49526 INSPECTION FOUND A 1.25" CRACK IN TAIL COMPARTMENT R/H SIDE CANTED FRAME AT STA 1463, L17R. A REPAIR DOUBLER WAS INSTALL ED IAW SRM 53-01, FIGURE 2. 2 L 7 2 4F RT A6WE 2002092700039 20020927 00039 NM 2002 9 27 CALA0200477 1 20020927 A 5320 WEB BOEING 737 7373T0 1384582 NM ABB THRESHOLD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND AFT CARGO PIT THRESHOLD WEB CORRODED AT STA 793-847. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002092700040 20020927 00040 WP 2002 9 27 0203039931 1 20020718 A 5330 SKIN DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 90S 47244 During Hck in ATL, a .125 crack was found on the RH skin adjacent to the wiper cutout area. Repaired per EA 99-190551. 2 L 7 2 4F A6WE 2002092700041 20020927 00041 WP 2002 9 27 0203049952 1 20020808 A 5710 SPAR DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 916RW 47144 During HCK in DHN, the rear spar chord was found cracked. Repaired per EA 99-131324 2 L 7 2 4F A6WE 2002092700042 20020927 00042 WP 2002 9 27 0203059951 1 20020808 A 5310 BULKHEAD DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9347 45827 During HCK in DHN, the aft pressure bulkhead web was found cracked under Z=63.5 stiffener approx. 10" outboard of the ve ntral door jamb. Repaired per EA 99-191325. 2 L 7 2 4F A6WE 2002092700043 20020927 00043 WP 2002 9 27 0203069951 1 20020812 A 5230 DOOR DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9347 45827 During HCK in DHN, crack damage was found on the lower forward cargo door inner and outer flange. Repaired per EA 99-191 322. 2 L 7 2 4F A6WE 2002092700044 20020927 00044 WP 2002 9 27 0203079952 1 20020813 A 5310 DOOR DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 916RW 47144 During Hck in DHN, aft cargo door was found to be cracked at the #2 forward doorstop. Repaired per EA 99-191323. 2 L 7 2 4F A6WE 2002092700045 20020927 00045 WP 2002 9 27 0203089912 1 20020901 A 5310 DOOR FRAME DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 While stationed in MSP during pressurization checks for squealing, the aft ventral door upper left hand corner jamb was found cracked. Repaired per EA. 99-187509. 2 L 7 2 4F A6WE 2002092700046 20020927 00046 WP 2002 9 27 0203099919 1 20020904 A 5310 LONGERON DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 941N 47450 During HCK in ATL, an existing repair had been found cracked. The repair at station 320 was repaired per EA 99-190665. 2 L 7 2 4F A6WE 2002092700047 20020927 00047 WP 2002 9 27 0203009931 1 20020709 A 5311 FRAME DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 90S 47244 During HCK in ATL, frames station 389 and 408 were found cracked at longeron 17. Repaired per EA 99-190536. 2 L 7 2 4F A6WE 2002092700048 20020927 00048 WP 2002 9 27 0203019975 1 20020709 A 5310 BULKHEAD DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9339 47382 During HCK in ATL, a crack was found on the LH portion of the APB Door cutout upper jamb. A repair of the upper jamb are a was extended to incorporate the the cracked area. Repaired per EA 99-190542. 2 L 7 2 4F A6WE 2002092700049 20020927 00049 WP 2002 9 27 0203029975 1 20020715 A 5310 ANGLE DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 90S 47244 During Hck in ATL Maintenance Base, the LH side of the verticle stabilizer attach angle (aft) was found cracked at stati on 1100. Repaired per EA 99-190557. 2 L 7 2 4F A6WE 2002092700050 20020927 00050 WP 2002 9 27 0203109876 1 20020922 A 2130 DUCT DOUG DC9 DC951 3022051 WP TAIL LOOSE A NWAA B EMER. DESCENT O OTHER CR CRUISE 1 GL 01 785NC 48110 LOST CABIN PRESSURE AT FL310 AND PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. THE OUTFLOW VALVE WAS FULLY CLOSED AND B OTH SUPPLY PRESSURES INDICATED 25 PSI. FLIGHT LANDED WITHOUT INCIDENT AT GFK. AFTER LANDING, THE CREW DETERMINED THERE W AS NO AIRFLOW FROM THE LEFT PACK AND NORMAL AIRFLOW FROM THE RIGHT PACK MAINTENANCE SECURED A LOOSE DUCT IN THE TAIL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002092700051 20020927 00051 EU 2002 9 27 0203133237 1 20020923 A 2920 ZCV67374612 CHECK VALVE AIRBUS 320 A320212 3930322 EU LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS CR CRUISE 1 GL 01 337NW 00358 RECEIVED 'HYD Y RSVR LO LVL' MESSAGE. DEACTIVATED THE YELLOW HYDRAULIC SYSTEM PER COM PROCEDURES. NOTE: LOSS OF THE YELL OW HYDRAULIC SYSTEM IN CONJUNCTION WITH THE NBR 1 YAW DAMPER BEING INOP PER MEL RESULTED IN ACTIVATION OF ALTERNATE LOW FLIGHT MODE. CONTINUED FLIGHT AND LANDED UNEVENTFULLY. FOUND THE PTU MANIFOLD CHECK VALVE LEAKING. REPLACED SEAL, SERVIC ED SYSTEM, AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002092700052 20020927 00052 NM 2002 9 27 SABA020088 1 20020828 A 5610 ODOR DHAV DHC8 DHC8103 1386005 NM COCKPIT DETECTED A SABA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 33 801WP 086 FLIGHT 5055 AIRCRAFT 801 FROM CINCINNATI TO CHARLOTTE: DURING CRUISE FLIGHT THE AIRCREW NOTICED A SLIGHT ELECTRICAL SME LL IN THE COCKPIT. NO EMERGENCY WAS DECLARED. AIRCRAFT CONTINUED TO CHARLOTTE WITH NO OTHER PROBLEMS. MAINTENANCE FOU ND THE SMELL COMING FROM PRC AROUND ONE OF THE COCKPIT WINDOWS. SEALANT WAS ALLOWED TO DRY AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092700053 20020927 00053 NM 2002 9 27 SWAA022121 1 20020911 A 3350 6104781 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002092700054 20020927 00054 NM 2002 9 27 SWAA022122 1 20020912 A 3350 PH22300L TRACK BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 EEPLS STRIP MISSING AND LOOSE AT ROW NR 9 LT. INSTALLED STRIP AND SECURED PER MM. 2 L 7 2 4F RT A16WE 2002092700055 20020927 00055 NM 2002 9 27 SWAA022124 1 20020910 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED C3 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED (2 EA) AT APPROX 3 O'CLOCK POSITION. REPAIRED BULKHEAD PER SWA EA. 2 L 7 2 4F A16WE 2002092700056 20020927 00056 2002 9 27 SWAA022127 4 20020913 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002092700057 20020927 00057 NM 2002 9 27 SWAA022128 1 20020914 A 2560 P4010021 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 334SW 23938 FWD INBD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2002092700058 20020927 00058 2002 9 27 SWAA022130 4 20020912 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002092700059 20020927 00059 NM 2002 9 27 SWAA022131 1 20020912 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED C3 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW NR 12 DEF. REMOVED AND REPLACE D LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002092700060 20020927 00060 NM 2002 9 27 SWAA022132 1 20020914 A 5311 6546529 BELTFRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED 1/4D CHECK, FOUND BELT FRAME CRACKED AT BS 500B, BETWEEN STR 20L AND STR 21L. REPAIRED BELT FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002092700061 20020927 00061 NM 2002 9 27 SWAA022134 1 20020913 A 5311 6546529 BELTFRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED 1/4D CHECK, FOUND BELT FRAME CRACKED AT BS 500C, BETWEEN STR 20L AND STR 21L. REPAIRED BELT FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002092700062 20020927 00062 NM 2002 9 27 SWAA022135 1 20020910 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STR SPLICE PER SR M. 2 L 7 2 4F RT A16WE 2002092700063 20020927 00063 NM 2002 9 27 SWAA022137 1 20020914 A 2781 F75935 SWITCH BOEING 737 7373H4 1384600 NM L/E FLAP FAILED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 333SW 23697 AIR TURNBACK, AFTER TAKEOFF WITH FLAPS SELECTED UP, L/E FLAP TRANSIT LIGHT REMAINED ILLUMINATED AND NR 2 L/E FULL EXTEND LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED NR 2 KRUEGER FLAP EXTEND SWITCH PER MM. 2 L 7 2 4F RT A16WE 2002092700064 20020927 00064 NM 2002 9 27 SWAA022140 1 20020916 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 385SW 26600 AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED AFT LOWER EMERGENCY FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2002092700065 20020927 00065 NM 2002 9 27 SWAA022145 1 20020916 A 2450 FCA410383 RELAY BOEING 737 7372K6 1364440 NM COCKPIT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 129SW 22340 AIR TURNBACK, DECLARED EMERGENCY, DURING CLIMB, ALL F/O'S INSTRUMENT LIGHTS INOP, ALSO WINDSHEAR AND RT AFT FUEL PRESS L IGHTS ILLUMINATED. REMOVED AND REPLACED R4 RELAY PER MM. 2 L 7 2 4F RT A16WE 2002092700066 20020927 00066 NM 2002 9 27 SWAA022146 1 20020915 A 2731 65C26384 TAB BOEING 737 7373H4 1384600 NM RT ELEVATOR VIBRATES A SWAA K NONE E F VIBRATION/BUFFET FLT CONT AFFECTED NR NOT REPORTED 1 SW 29 603SW 27954 AIRCRAFT VIBRATES MOMENTARILY WITH HIGH POWER SETTINGS AND/OR AERODYNAMIC LOAD. REMOVED AND REPLACED RT ELEVATOR TAB PE R MM. 2 L 7 2 4F RT A16WE 2002092700067 20020927 00067 NM 2002 9 27 SWAA022153 1 20020917 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STR SPLICE PER MM . 2 L 7 2 4F RT A16WE 2002092700068 20020927 00068 2002 9 27 SWAA022154 4 20020916 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002092700069 20020927 00069 2002 9 27 SWAA022156 4 20020916 A 2565 22D22901151 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 071SW 22358 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F A16WE 2002092700070 20020927 00070 NM 2002 9 27 SWAA022157 1 20020917 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 RT OVERWING EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002092700071 20020927 00071 2002 9 27 SWAA022169 4 20020904 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002092700072 20020927 00072 2002 9 27 SWAA022170 4 20020917 A 2565 61621469 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002092700073 20020927 00073 2002 9 27 SWAA022171 4 20020918 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002092700074 20020927 00074 2002 9 27 SWAA022172 4 20020918 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002092700075 20020927 00075 NM 2002 9 27 SWAA022177 1 20020918 A 3350 6556633 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 778SW 27883 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002092700076 20020927 00076 NM 2002 9 27 SWAA022178 1 20020917 A 3350 6574550 LIGHT BOEING 737 7373H4 1384600 NM SERVICE DOOR NOT SEATED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE LIGHT INOP. RESEATED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002092700077 20020927 00077 NE 2002 9 27 SWAA022180 2 20020918 A 7200 JT8D9A ENGINE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9 52048 NE NR 2 VIBRATION A SWAA K NONE E VIBRATION/BUFFET UK UNKNOWN 1 SW 29 074SW 22674 687782 NR 2 ENGINE VIBRATING AND N1 INDICATOR FLUCTUATING. REMOVED AND REPLACED NR 2 ENGINE AND N1 INDICATOR PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2002092700078 20020927 00078 NM 2002 9 27 SWAA022181 1 20020916 A 5320 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002092700079 20020927 00079 NM 2002 9 27 SWAA022183 1 20020918 A 5320 6551698 SPLICE BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002092700080 20020927 00080 NM 2002 9 27 SWAA022185 1 20020917 A 5320 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 20R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002092700081 20020927 00081 NM 2002 9 27 SWAA022187 1 20020917 A 3250 162A1417 COLLAR BOEING 737 7377H4 1384404 NM NLG WORN A SWAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 29 773SA 27881 AFTER PUSHBACK RUDDER PEDAL MOVEMENT CAUSED A BANG/THUMP IN THE NOSE WHEEL AREA. REMOVED AND REPLACED NLG STEERING COLL AR AND LOWER PLATE PER MM. 2 L 7 2 4F RT A16WE 2002092700082 20020927 00082 NM 2002 9 27 C1HA200284 1 20020926 A 3350 806740401 LIGHT BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 684CA 22491 Cockpit emergency light INOP.Removed and replaced emergency light. 2 L 7 3 4F A3WE 2002092700083 20020927 00083 NM 2002 9 27 SABA020090 1 20020908 A 3350 1306 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 33 883CC 162 FLIGHT 5011 FROM LEX TO CLT ; DURING POST-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE EMERGENCY LIGHT AT ROW ONE INOP . MAINTENANCE REMOVED AND REPLACED BULB AND SYSTEM OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2002092700084 20020927 00084 EA 2002 9 27 COMA0260542 1 20020925 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 918CA 7018 FLIGHT 5968 GEAR DISAGREE MESSAGE - NLG DID NOT RETRACT.SERVICED THE NLG SHOCK STRUT WITH OIL AND N2 PER AMM. 2 L 7 2 4F RT A21EA 2002092700085 20020927 00085 EA 2002 9 27 COMA0260543 1 20020925 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 472CA 445 7667 FLIGHT 5507 FLAPS FAILED WHEN SELECTED TO 30 DEGREES.REPLACED THE L/H BPSU. 2 L 7 2 4F RT A21EA 2002092700086 20020927 00086 EA 2002 9 27 COMA0260544 1 20020923 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 918CA 7018 FLIGHT 5258 FLAPS FAILED WHEN SELECTED UP AFTER T/O.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002092700087 20020927 00087 NM 2002 9 27 SABA020091 1 20020908 A 3350 1306 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A SABA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 33 881CC 294 FLIGHT 5032 FROM PGV TO CLT, DURING POST-FLIGHT INSPECTION IN CLT, THE AIR CREW REPORTED THE EMERGENCY LIGHT INOP ON ROW ONE. MAINTENANCE REMOVED AND REPLACED BULB AND SYSTEM OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2002092700088 20020927 00088 WP 2002 9 27 MWEA020600 1 20020927 A 5313 J0601385 SKIN DOUG DC9 DC932 3022066 WP STATION 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FUSELAGE SKIN IS CRACKED AT ONE RIVET HOLE FRAME STATION 996 BETWEEN LONGERON 3&4 RIGHT. -- STOP DRILLED NOTED CRACK, BLENDED 2 DRILL START. FABRICATED, LOCATED AND DRILLED DOUBLER. FABRICATED , LOCATED AND DRILLED FINGER DOUBLER. INSTALL ED FINGER DOUBLER AND REPAIR DOULBER. 2 L 7 2 4F A6WE 2002102900097 20021029 00097 SO 2002 10 29 C2XA02BT058 1 20020926 A 3230 355022002 CONTROL UNIT EMB 145 EMB145ER 3260211 SO COCKPIT FAULTY A C2XA O OTHER J WARNING INDICATION UK UNKNOWN 1 SW 27 17928 145007 CREW REPORTED, "GEAR NOT RETRACTING." MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT AND LANDING GEA R CONTROL LEVER IAW EMB145 AMM 32-32-01 AND 32-32-02. OPERATIONAL CHECKED SYSTEM GOOD. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002092700089 20020927 00089 NM 2002 9 27 SABA020092 1 20020912 A 3350 1306 LIGHT DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A SABA K NONE L NO TEST IN INSP/MAINT 1 SO 33 882CC 168 FLIGHT 5011 FROM CLT TO LEX, DURING PREFLIGHT THE AIRCREW REPORTED THE OVERHEAD EMERGENCY LIGHTS INOP. MAINTENANCE REMOV ED AND REPLACED BULBS AND SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002092700090 20020927 00090 NM 2002 9 27 SABA020093 1 20020915 A 3350 1306 BULB DHAV DHC8 DHC8103 1386005 NM A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 Flight 5011 from LEX to CLT During post-flight inspection the crew reported the emergency light at row one would not tes t. Maintenance removed and replaced bulb and system ops checked good. Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002092700091 20020927 00091 WP 2002 9 27 MWEA020601 1 20020927 A 5313 J0601389 SKIN DOUG DC9 DC932 3022066 WP STATION 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FUSELAGE SKIN IS CRACKED AT 3 RIVETS HOLES FRAME STATION 996 BETWEEN LONGERON 3&4 LEFT. -- STOPPED DRILLED 3 CRACKS, B LENDED 3 EACH DRILLED START . FABRICATED AND REPAIR AND INSTALLED DOUBLER AND FINGER DOUBLER. 2 L 7 2 4F A6WE 2002092700092 20020927 00092 WP 2002 9 27 MWEA020602 1 20020927 A 5711 3912766501 SPAR DOUG DC9 DC932 3022066 WP LH WING GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 LEFT WING, LOWER ANGLE FITTINGS ON FALSE SPAR HAS A DEEP GOUGE IN IT. DOT NS01. -- BLENDED GUAGE, REMOVED AND INSTALLE D FITTINGS FABRICATED REPAIR AND INSTALLED BUSHINGS. FIT AND DRILLED AND INSTALLED AUX SPAR FITTING. 2 L 7 2 4F A6WE 2002092700093 20020927 00093 WP 2002 9 27 MWEA020603 1 20020925 A 5210 53725 LATCH DOUG DC9 DC932 3022066 WP LAV DOOR BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 LAV SERVICE DOOR TOP AFT LATCH SURFACE BROKEN (AIRCRAFT SIDE). -- TRIMMED OUT DAMAGE TO DOUBLER, FABRICATED AND INSTAL LED DOUBLER. 2 L 7 2 4F A6WE 2002092700094 20020927 00094 NM 2002 9 27 AWXA200200933 1 20020903 A 5311 65C352431 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A 3/4" CRACK WAS FOUND ON THE AFT CARGO DOOR FORWARD FRAME AT BS 794, WL 167, RB L 44. MAINTENANCE STOP DRILLED THE CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED. FABRICATED A DOUBLER, 2 EACH SUPPORT TEE'S, 2 EACH RADIUS FILLERS, AND INSTALLED REPAIR PARTS IAW E.O. 53-10-01. 2 L 7 2 4F RT A16WE 2002092800001 20020928 00001 SO 2002 9 28 C2XA02SH065 1 20020928 A 5313 14527177006 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 DURING C CHECK A GOUGE WAS FOUND ON STRINGER 19 RT BETWEEN FRAMES 52 AND 53. MAINTENANCE BLENDED GOUGE, PERFORMED DYE PE NATRANT INSPECTION AND INSTALLED AT REINFORCEMENT AT STRINGER 19 RT BETWEEN FRAMES 52 AND 53 IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002092900001 20020929 00001 SO 2002 9 29 C2XA02SH067 1 20020927 A 5500 14568500409 STRUCTURE EMB 145 EMB145LR 3260212 SO SPEEDBRAKE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 DURING C CHECK LT SPEED BRAKE OUTER TRAILING EDGE IS WRAPED. MAINTENANCE REMOVED AND REPLACED LT SPEED BRAKE. OPERATION AL CHECK GOOD IAW EMB 145 AMM 27-63-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002092900002 20020929 00002 SO 2002 9 29 C2XA02SH068 1 20020927 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 SHV - DURING C CHECK THE GALLEY FLOORBEAM ANGLE WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AN REPLACED FLOORBEAM A NGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002093000001 20020930 00001 EU 2002 9 30 WRNA200200005 1 20020926 A 7931 9067M69601 LINE GE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE ENGINE BROKEN A WRNA A O UNSCHED LANDING OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 05 502TA 528265 075 528265 #1 engine oil qty dropped to zero (0) after flt level 27.0 #1 eng oil press flux between 40-30 psi then 30-20 psi then s teady no psi. Aircraft made unscheduled landing @ MSY. No fuel was dumped. Aircraft landed normally.Corrective Action: F ound "D" sump scavenge line leaking. Changed out scavenge line segment and gamma fitting I/A/W MM 20-00. Inspected Engin e chip detectors for signs of bearing failure. All checked satisfactory. Line leak check satisfactory. Aircraft returned to service. 2 L 7 2 4F 4 F RT A35EU E23EA 2002102800127 20021028 00127 EU 2002 10 28 02FDEA00639 1 20020912 A 5330 A5361056723500 DOUBLER AIRBUS 310 A310 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 DOUBLER ON INNER FACE OF FUSELAGE SKIN CORRODED IN AVIONIC COMPT BETWEEN FRAME 16A & 17, EXTENDING FWD OF FRAME 16A OUTB D OF STR 44L & FWD OF FRAME 17 INBD OF STR 44L. R&R SKIN DOUBLER PER EA 6-5330-65-65906. 2 L 7 2 4F RT A35EU 2002102800128 20021028 00128 EU 2002 10 28 02FDEA00640 1 20020912 A 5730 SKIN AIRBUS 310 A310 EU RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 RIGHT WING OUTER LWR SKIN PANEL NR 2 AT TRAILING EDGE OF RIB 2 CRACK. R&R WING LWR SKIN PANEL NR 2 PER EA 6-5710-65100. 2 L 7 2 4F RT A35EU 2002093000002 20020930 00002 WP 2002 9 30 MWEA020604 1 20020927 A 2100 21D101 COALESCER BAG DOUG DC9 DC932 3022066 WP UNSERVICEABLE A MWEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 31 401ME 47133 FLIGHT ATTENDANT REPORTED SMELL IN AFT CABIN. -- REMOVED AND REPLACED LEFT AND RIGHT COALESCER BAG. 2 L 7 2 4F A6WE 2002093000003 20020930 00003 NM 2002 9 30 02FDEA00643 1 20020912 A 2613 65249201 CONTROL UNIT BOEING 727 727200 138407E NM E/E BAY MALFUNCTIONED A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SO 25 288FE 21850 LOWER AFT BODY OVERHEAT LIGHT STARTED TO FLICKER ON PASSING THROUGH 27K FT. ON CLIMBOUT LIGHT WENT OUT AFTER TURNED OFF RT PACK AND CLOSED BLEED NR 3 COMPLETED QRH PROCEDURES CONTINUED AT FL280. COMPLIED WITH ADJUST AND TEST AND TROUBLE S HOOTING CHART UNABLE TO DUPLICATE. M/M 26-14-000-5 REPLACED OVER HEAT DETECTION CONTROL UNIT M/M 26-14-11. 2 L 7 3 4F RT A3WE 2002093000004 20020930 00004 EU 2002 9 30 02FDEA00644 1 20020912 A 2923 PUMP AIRBUS 300 A300F4605R 3930327 EU GREEN SYSTEM LEAKING A FDEA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS CR CRUISE 1 SO 25 679FE 793 EN ROUTE AT FL310 GREEN HYD QUANTITY WENT TO RED DOT WITH ECAM NOTIFICATION. FOLLOWED ECAM AND QRH PROCEDURES. DURING REMAINDER OF FLT GREEN HYD QTY APPEARED TO CONTINUE LEAKING BELOW THE RED DOT. GRAVITY EXT OF GEAR WAS NORMAL AND WE W ERE TOWED IN. ACFT DECLARED EMERGENCY FOR LANDING DUE TO NO NLG STEERING CAPABILITIES. DURING TROUBLE SHOOTING OF HYDR O GREEN SYSTEM FOUND GREEN SIDE OF G/Y PTU PUMP LEAKING HEAVY AT PUMP HOUSING MATING SURFACES. R/R'D GREEN AND YELLOW P TU PER MM 29-23-11-4,OPS AND IK CKED GOOD SCV BOTH RESERVOIR. INDG GEAR FREE FALL EXT SYS OK PER PER 32-33-00-0. 2 L 7 2 4F RT A35EU 2002093000005 20020930 00005 NM 2002 9 30 UPS02239169 1 20020809 A 5753 WEDGE BOEING 727 72731C 1384011 NM T/E FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C R/H I/B MIDFLAP DISBOND UPPER SURFACE T-EDGE WEDGE 10 INCHES FROM EN D APPROX. REPAIRED IAW SRM 51 -40-20 2 L 7 3 4F A3WE 2002093000007 20020930 00007 WP 2002 9 30 ABXA020178 1 20020910 A 5311 99196182N FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 NEED TO REMOVE AND REPLACE MAIN FRAME AT FS 718, DUE TO REPAIR ANGLE THAT WAS INSTALLED. REMOVED AND REPLACED MAIN FRAM E AT FS 718 IAW JC EA 53400324-001-2. 2 L 7 2 4F A6WE 2002093000008 20020930 00008 WP 2002 9 30 ABXA020180 1 20020731 A 5730 59127352 SKIN PANEL DOUG DC9 DC941 302207N WP WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DELAMINATION AREA ON OUTBOARD TRAILING EDGE BONDED PANEL LOCATED ON WING UPPER SURFACE AND FORWARD OF AILERON. REPLACED OUTBOARD TRAILING EDGE BONDED PANEL IAW DC-9 SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 2002093000009 20020930 00009 WP 2002 9 30 ABXA020183 1 20020801 A 5320 59203471 FITTING DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 FRAME FOOT AT STA 617 LEFT HAD HEAVY EXFOLIATION CORROSION. REPLACED FRAME FOOT AT STA 617 LEFT AND FASTENERS IAW DC-9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 2002093000010 20020930 00010 NM 2002 9 30 SWAA022147 1 20020915 A 2560 PH22300L TRACK BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 PHOTO LUMINESCENT STRIP LOOSE AT ROW NR 8 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2002093000011 20020930 00011 NM 2002 9 30 SWAA022192 1 20020920 A 3350 604222 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHAR GER PER MM. 2 L 7 2 4F RT A16WE 2002093000012 20020930 00012 2002 9 30 SWAA022195 4 20020920 A 2565 23022991 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED RON CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2002093000013 20020930 00013 2002 9 30 SWAA022196 4 20020919 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002093000014 20020930 00014 NM 2002 9 30 SWAA022198 1 20020922 A 5754 65C26602 WEDGE BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND NR 5 L/E SLAT WEDGE DELAMINATED AT BOTH INBD AND OTBD ENDS. REPAIRED NR 5 L/E SLAT WEDG E PER MM. 2 L 7 2 4F RT A16WE 2002093000015 20020930 00015 NM 2002 9 30 SWAA022200 1 20020921 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 4R, BS 597 AND BS 685. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002093000016 20020930 00016 NE 2002 9 30 SWIA200211233 2 20020914 A 7320 3035659 HMU EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 251YV 4953 2322 120251 ON TAKEOFF ROLL, LEFT ENGINE TQ FLUCTUATED BETWEEN 90, 100 & 80 PERCENT WHILE THE RIGHT ENGINE TQ WAS AT 90 PERCENT. A ( + -) 10 PERCENT TQ DIFFERENCE ON LEFT ENGINE WAS OBSERVED. TAKEOFF ABORTED. RAN LEFT & RIGHT ENGINES IN TAKEOFF POSI TION WHILE EEC ARE ON, PROP SYNC -ON-, AUTOFEATHER -ON-. RAN ENGINES IN VARIOUS ARRANGEMENTS. OPS CHECKS GOOD. NO DEF ECTS NOTED. RETRIMMED BOTH ENGINES. OPS CHECKS GOOD. 09/16 - UPDATE: FURTHER TROUBLESHOOTING RESULTED IN REMOVAL AND REPLACEMENT OF NR 1 HMU. OPS AND LEAKS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002093000017 20020930 00017 WP 2002 9 30 U2RB070102 1 20020730 A 5343 57500922 SUPPORT FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76397 392 46088 DURING COMPLIANCE BOEING S/B DC8-53-061R4 VISUALLY DETECTED RT MLG SUPPORT FITTING CRACKED IN TWO PLACES. UPPER AREA .8 75 INCH AND AFT UPPER AREA CRACK EXTENDING UP AND OUT INTO SUPPORT FITTING FLANGE. 2 L 7 4 4F 4A25 2002093000018 20020930 00018 WP 2002 9 30 U2RB070202 1 20020730 A 5343 57500921 SUPPORT FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76397 392 46088 DURING COMPLIANCE WITH BOEING S/B DC8-53-61 R4, VISUALLY DETECTED LEFT HAND WHEEL WELL TRAPEZOID FITTING CRACKED AND EXT ENDING FROM BOLT HOLE APPROXIMATELY 2.25 INCHES. 2 L 7 4 4F 4A25 2002093000019 20020930 00019 WP 2002 9 30 U2RB070302 1 20020731 A 5320 36410042 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76397 392 46088 DURING COMPLIANCE OF BOEING S/B 53-61 R4 DURING DISASSEMBLY FOR REPLACEMENT OF CRACKED RT MLG SUPPORT FITTING DURING DIS ASSEMBLY FOUND RT LONGERON NR 24 FUSELAGE FRAME FITTING CORRODED. 2 L 7 4 4F 4A25 2002093000020 20020930 00020 WP 2002 9 30 UPS02839227 1 20020830 A 3230 UPLOCK DOUG DC8 DC871F 302199D WP MLG OUT OF RIG A IPXA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 715UP 45915 INSPECTION TYPE:N/A, MLG DOOR UNSAFE LIGHT. PERFORMED PULL TEST, DOOR FAILED. PERFORMED TEST OF MAIN GEAR DOOR UP PROX IMITY SENSORS, GOOD IAW UPS DC8 MM 32-60-00. R&R PROXIMITY BOX IAW SRM 51-3-0. RIGGED DOOR UPLOCK CABLE RT SIDE CHECKE D GOOD IAW UPS DC8 32-31-04. TIGHTENED LOOSE GROUND ON LT DOOR PROX SWITCH. DOOR LATCH SYSTEM FOR MAIN GEAR DOORS OPS CHECK GOOD IAW DC8 MM 32-60-00 2 L 7 4 4F RT 4A25 2002093000021 20020930 00021 EU 2002 9 30 XNOA01067 1 20020904 A 2910 HYDRAULIC SYSTEM AIRBUS 300 A300B4203 3930306 EU GREEN SYSTEM DIRTY A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 473AS 203 NR 1 EDP INOP (GREEN SYSTEM). CLEANED AND RESECURED CONNECTION AT BYPASS. SOL SYS CHECKED GOOD PER A300 MM 29-11-32. 2 L 7 2 4F RT A35EU 2002093000022 20020930 00022 EU 2002 9 30 XNOA01068 1 20020917 A 3231 DOOR AIRBUS 300 A300B4203 3930306 EU NLG OUT OF RIG A XN0A D RETURN TO BLOCK J E WARNING INDICATION VIBRATION/BUFFET TX TAXI/GRND HDL 1 GL 23 224KW 073 NOSE GEAR LIGHT ILLUMINATED WITH GEAR HANDLE IN NEUTRAL POS, LIGHT VIBRATION NOSE DOORS. RIGGED LEFT HAND NOSE GEAR DOO R. OPS CHECK GOOD ON GEAR SWING IAW A300 MM 32-30-00. 2 L 7 2 4F RT A35EU 2002093000023 20020930 00023 2002 9 30 XNOA01069 4 20020918 A 2210 CIRCUIT BREAKER AIRBUS 300 A300B4203 3930306 EU AUTOPILOT SYS TRIPPED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 307FV 235 NR 2 PITCH TRIM TRIPS OFF WON'T RESET. TRANSFERRED TO DMI 2623 IAW MEL 22-11-03. PLACARDS INSTALLED. 2 L 7 2 4F RT A35EU 2002093000024 20020930 00024 NM 2002 9 30 XNOA01070 1 20020918 A 5753 ROLLER BOEING 727 727227 1384078 NM T/E FLAP FAILED A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 793A 20774 AFTER T/O DURING FLAP RETRACTION OUTBOARD FLAPS WENT TO 2 DEGREES INBOARD FLAPS REMAINED AT 5 DEGREES. MX INSPECTION FO UND FAILED ROLLERS AT LEFT OUTBOARD FORE FLAP SEQUENCING CARRIAGE. REMOVED AND REPLACED ROLLERS. OPS CHECK GOOD IAW B7 27 MM 27-51-14 & 27-51-10. 2 L 7 3 4F A3WE 2002093000025 20020930 00025 WP 2002 9 30 ABXA020188 1 20020911 A 3231 29568461 CONTROL CABLE DOUG DC9 DC933F 302207A WP NLG BROKEN A ABXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 23 934AX 47462 ON INITIAL CLIMB OUT, EXCESSIVE NOISE AND VIBRATION IN VICINITY OF NOSE GEAR. WHEN GEAR LOWERED, NOISE, VIBRATION STOPP ED. FOUND RIGHT FORWARD NOSE GEAR DOOR OPEN, AND DOOR STOP CABLE BROKEN. REPLACED LEFT AND RIGHT NOSE GEAR DOOR STOP C ABLES IAW DC-9 MM 32-22-01-2-0004. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002093000026 20020930 00026 WP 2002 9 30 ABXA020189 1 20020809 A 5531 99118315 RIB DOUG DC9 DC941 302207N WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 VERTICAL REMOVEABLE LEADING EDGE RIB WAS CRACKED, LEFT SIDE NR 12. REPAIRED AREA IAW DC-9 SSRM K05159, SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002093000027 20020930 00027 WP 2002 9 30 ABXA020190 1 20020809 A 5531 99118275 RIB DOUG DC9 DC941 302207N WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 VERTICAL REMOVABLE LEADING EDGE RIB WAS CRACKED LEFT SIDE NR 7. REPAIRED AREA IAW DC-9 ABX SSRM K05159, SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002093000028 20020930 00028 WP 2002 9 30 ABXA020191 1 20020809 A 5531 99118245 RIB DOUG DC9 DC941 302207N WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 VERTICAL REMOVABLE LEADING EDGE RIB WAS CRACKED LEFT SIDE NR 4. REPAIRED AREA IAW DC-9 ABX SSRM K05159, SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002093000029 20020930 00029 WP 2002 9 30 ABXA020192 1 20020809 A 5531 99118245 RIB DOUG DC9 DC941 302207N WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 VERTICAL REMOVABLE LEADING EDGE RIB WAS CRACKED LEFT SIDE NR 1. REPAIRED AREA IAW ABX DC-9 SSRM K05159, SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002093000030 20020930 00030 WP 2002 9 30 ABXA020193 1 20020809 A 5531 99118245 RIB DOUG DC9 DC941 302207N WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 VERTICAL REMOVABLE LEADING EDGE RIB WAS CRACKED RIGHT SIDE NR 3. REPAIRED AREA IAW DC-9 ABX SSRM K05159, SRM 51-30-2 AN D 51-30-5. 2 L 7 2 4F A6WE 2002093000031 20020930 00031 WP 2002 9 30 ABXA020194 1 20020812 A 5320 5910130391N1 TEE FITTING DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 CRACK INDICATION ON NR 6 AFT PRESSURE BULKHEAD 'T' AT LONGERON 14 LEFT AND 'P' DOME RADIAL. REPLACED NR 6 'T' CAP IAW E A 53120037-006. 2 L 7 2 4F A6WE 2002093000032 20020930 00032 WP 2002 9 30 ABXA020197 1 20020812 A 5230 59191577 PAN DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 OUTER PAN WAS CRACKED AT BEAM 3 ON AFT END OF AFT LOWER CARGO DOOR. REPLACED DOOR IAW DC-9 MM. 2 L 7 2 4F A6WE 2002093000033 20020930 00033 WP 2002 9 30 ABXA020201 1 20020828 A 5320 99577261 INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 CRACKED INTERCOSTAL AT STA. 794, LEFT BUTT LINE 22. REPAIRED INTERCOSTAL IAW DC-9 SSRM K05159. 2 L 7 2 4F A6WE 2002093000034 20020930 00034 WP 2002 9 30 ABXA020202 1 20020828 A 5320 99577262 INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 CRACKED INTERCOSTAL AT STA 794, RBL 22. REPAIRED INTERCOSTAL IAW DC-9 SSRM K05159. 2 L 7 2 4F A6WE 2002093000035 20020930 00035 EU 2002 9 30 MALA020584 1 20020926 A 5320 7253721439 WEBBING SAAB SF340 340B 7860101 EU A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 DURING 4K-INSPECTION IN CWA, MAINTENANCE FOUND WEBBING BETWEEN STA 288-294 TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED WEBBING PN 7253721-439 IAW SAAB SRM CHAP 51. RELEASE DATE IS 9/30/02. 2 L 7 2 4T RT A52EU 2002093000036 20020930 00036 WP 2002 9 30 DHL2002804010 1 20020930 A 2611 302314 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP A DHLA K NONE J L WARNING INDICATION NO TEST IN INSP/MAINT 1 SO 01 804DH 46124 1) #5 SMOKE DETECTOR WILL NOT TEST2) R&R #5 SMOKE DETECTOR IAW M/M 26-10-5. OPS CHECK GOOD 2 L 7 4 4F RT 4A25 2002093000037 20020930 00037 NM 2002 9 30 QXEA0202491 1 20020927 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 15868 450 506 PSC-FRONT 4 RED EMERGENCY FLOOR TRACK EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED PS-6 BATTERY PACK. OPERATIONAL CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002093000038 20020930 00038 WP 2002 9 30 IXXA0200076O 1 20020929 A 3210 STRIKER DOUG DC8 DC873F 302199F WP GEAR DOOR DIRTY A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 606AL 88644 396 46044 AFTER TAKE OFF FROM RMS, THE LANDING GEAR DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED FOLLOWING LANDING GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR AND THE LIGHT WAS EXTINGUISHED. THE FLIGHT CONTINUED TO GSO FOR AN UNEVENTFUL LANDING . MAINTENANCE INSPECTED THE AIRCRAFT, CLEANED THE SWITCHES AND STRICKER AND PERFORMED OPERATIONAL CHECKS WITH NO DEFECT S NOTED IN ACCORDANCE WITH THE DOUGLAS MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002093000039 20020930 00039 WP 2002 9 30 IXXA0200075O 1 20020924 A 2710 165W010045 PUMP DOUG DC8 DC863 302198A WP RUDDER LEAKING A IXXA O OTHER J WARNING INDICATION CR CRUISE 1 SW 11 786AL 84445 2908 46121 ENROUTE FROM TOL TO PDX, THE FLIGHT CREW NOTICED A DROP IN THE HYDRAULIC QUANTITY SYSTEM. THE FLIGHT CREW FOLLOWED COMP ANY PROCEDURES AND PROCEDED TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT USING ALL PUMPS AND SY STEMS AND FOUND NO DEFECTS. MAINTENANCE SERVICED THE HYDRAULIC SYSTEM. A FEW HOURS LATER MAINTENANCE NOTICED THE CASE DRAIN PLUG ON THE STANDBY RUDDER PUMP LEAKING. MAINTENANCE REPLACED THE PUMP AND PERFORMED SUCESSFUL OPERATION CHECKS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002093000040 20020930 00040 NM 2002 9 30 AWXA200200935 1 20020927 A 3350 BMS13311122 WIRE BOEING 757 7572G7 1384963 NM SEAT ROW 19 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 0 0 24233 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H WAS FOUND INOPERATIVE. MAINTENANCE SPLI CED A BROKEN WIRE AT SEAT ROW 19 L/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002093000041 20020930 00041 NM 2002 9 30 AWXA200200936 1 20020928 A 3350 BMS13311122 WIRE BOEING 757 7572S7 1384962 NM SEAT ROW 28 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 0 0 23321 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 28 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPA IRED A BROKEN WIRE AT SEAT ROW 28 L/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002093000042 20020930 00042 NM 2002 9 30 AWXA200200940 1 20020901 A 7110 65NK712501 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK EXFOLIATION CORROSION WAS FOUND ON THE FORWARD LAV PAN RING AT BS 275. MAINTENAN CE REMOVED EXTERNAL DOUBLER AND LAV PAN RING; FABRICATED A NEW EXTERNAL DOUBLER; INSTALLED REPAIR PART AND LAV PAN RING IAW B737-200 SRM 51-30-2, PG. 2-4, 8, FIG. 1, SRM 51-30-5, PG. 47, SRM 51-30-8, PG. 1-3. 2 L 7 2 4F RT A16WE 2002093000043 20020930 00043 NM 2002 9 30 AWXA200200941 1 20020911 A 5330 654580023 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A 1 1/4" CRACK WAS FOUND ON FUSELAGE SKIN 6" BELOW THE UPPER HINGE CUTOUT OF THE L-1 DOOR, BS 306, WL 236.68. MAINTENANCE REMOVED EXISTING DOUBLER AND FOUND 2 CRACKS EMANATING FROM EXISTING STOP DRILL HOLES. CUTOUT DAMAGED AREA OF SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS , A REPAIR DOUBLER, AND A GAP COVER; INSTALLED REPAIR PARTS IAW AWA E.R. 15-5300-02269-ES2. 2 L 7 2 4F RT A16WE 2002093000044 20020930 00044 NM 2002 9 30 AWXA200200942 1 20020901 A 5753 657190233 SKIN BOEING 737 737277 1384570 NM WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK THE L/H WING INBOARD MID FLAP UPPER SURFACE WAS FOUND TO HAVE A WORN SPOT AT THE INBOARD EDGE. MAINENANCE CUTOUT WORN SPOT ON MID FLAP UPPER SURFACE; FABRICATED AN EXTERNAL DOUBLER, AND INSTALLED REPA IR PART IAW AWA E.R. 15-5753-02269-ES3. 2 L 7 2 4F RT A16WE 2002093000045 20020930 00045 NM 2002 9 30 AWXA200200943 1 20020922 A 5753 657192681 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 0 0 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A 3/16" CRACK WAS FOUND ON THE L/H WING INBOARD HINGED FLAP UPPER SKIN AT THE R/ H SIDE APPROXIMATELY 7" FROM THE TRAILING EDGE GOING FORWARD. MAINTENANCE TRIMMED OUT DAMAGED AREA ON HINGED FLAP UPPER SKIN; FABRICATED AN EXTERNAL DOUBLER, AND INSTALLED REPAIR PART IAW AWA E.R. 15-5753-02269-GF3. 2 L 7 2 4F RT A16WE 2002093000046 20020930 00046 NM 2002 9 30 AWXA200200944 1 20020906 A 5313 65457768 STRINGER BOEING 737 737301 1384611 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 0 0 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON BOTH SIDES OF STRINGER 26 R/H, BS 1006-1012, A FT SIDE OF WASTE SERVICE COMPARTMENT. MAINTENANCE FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED CORRODED STRINGER 26 R/H, B S 1006-1012; FABRICATED A NEW STRINGER PER DWG 65-45776; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 3-4. 2 L 7 2 4F RT A16WE 2002093000047 20020930 00047 NM 2002 9 30 AWXA200200945 1 20020911 A 5330 65458001112 SKIN BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 0 0 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK 1/16" AND 1/32" CRACKS WERE FOUND ON THE FUSELAGE SKIN AT THE LOWER AFT CUTOUT OF THE R-1 DOOR, BS 326.5 AND BS 327.5. MAINTENANCE CUTOUT 2 EACH CRACKS AT THE LOWER AFT CUTOUT OF THE R-1 DOOR, BS 326.5 AND BS 327.5; FABRICATED -1, -2, & -5 REPAIR PLATES, -3, -7 FILLERS, AND -4, -6 TAPERED FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01, PG. 204-208, FIG. 202. 2 L 7 2 4F RT A16WE 2002093000048 20020930 00048 NM 2002 9 30 AWXA200200946 1 20020923 A 5320 654860677 FORMER BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 0 0 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND ON R/H WING TO BODY FAIRING FORMER, AFT OF R/H RAM AIR SCOOP , BS 535. MAINTENANCE REMOVED DAMAGED WING TO BODY FAIRING FORMER BS 535; FABRICATED A -2 REPAIR ANGLE; INSTALLED REPAIR PART IAW AWA E.R. 03-5300-02269-TB2. 2 L 7 2 4F RT A16WE 2002093000049 20020930 00049 NM 2002 9 30 AWXA200200947 1 20020901 A 5313 69353523 TIE CLIP BOEING 737 737375 13844BN NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 0 0 23707 YVR - MAJOR REPAIR - DURING C-03 CHECK A 5/16" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727C, STRINGER 4 L/H. MAINTEN ANCE REMOVED THE DAMAGED STINGER TIE CLIP AT BS 727C, STRINGER 4 L/H, FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED R EPAIR PART IAW B737-300 SRM 51-10-02, PG. 12, AND SRM 51-40-02, PG. 3. 2 L 7 2 4F RT A16WE 2002093000050 20020930 00050 NM 2002 9 30 AWXA200200948 1 20020901 A 5313 69353533 TIE CLIP BOEING 737 737375 13844BN NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 0 0 23707 YVR - MAJOR REPAIR - DURING C-03 CHECK A 1/2" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727B, STRINGER 4 L/H. MAINTENA NCE REMOVED THE DAMAGED STINGER TIE CLIP AT BS 727B, STRINGER 4 L/H, FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED RE PAIR PART IAW B737-300 SRM 51-40-02, PG. 6. 2 L 7 2 4F RT A16WE 2002093000051 20020930 00051 NM 2002 9 30 AWXA200200949 1 20020904 A 5313 693535214 TIE CLIP BOEING 737 737375 13844BN NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 0 0 23707 YVR - MAJOR REPAIR - DURING C-03 CHECK A 1/2" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727E, STRINGER 5 R/H. MAINTENA NCE REMOVED THE DAMAGED STINGER TIE CLIP AT BS 727E, STRINGER 5 R/H, FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED RE PAIR PART IAW DWG 69-35352, AND B737-300 SRM 51-40-02, PG. 3. 2 L 7 2 4F RT A16WE 2002093000052 20020930 00052 NM 2002 9 30 AWXA200200954 1 20020901 A 5311 69620493 SHEAR TIE BOEING 737 737375 13844BN NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 0 0 23707 YVR - MAJOR REPAIR - DURING C-03 CHECK A 1/2" CRACK WAS FOUND ON FRAME ATTACH ANGLE (SHEAR TIE) AT BS 727D, BELOW STR 1 5 R/H. MAINTENANCE REMOVED DAMAGED SHEAR TIE AT BS 727D, BELOW STR 15 R/H; FABRICATED A NEW REPLACEMENT SHEAR TIE; INSTA LLED REPAIR PART IAW DWG 69-62049, AND B737-300 SRM 51-40-02, PG. 12. 2 L 7 2 4F RT A16WE 2002093000053 20020930 00053 NM 2002 9 30 S02J30032 1 20020927 A 3000 60B100286 WINDSHIELD BOEING 747 747400 NM GE CF6 CF680C2* GL R1 MALFUNCTIONED W SAJF O OTHER O OTHER CR CRUISE 1 WP 03 30768 B18711 CREW VERBAL REPORT THROUGH SATCOM THAT AFTER 3 HRS FLT, SLIGHT WHITE FUMES COMING FROM COCKPIT R1 WINDSHIELD LOWE R END CAUSED OF 2 SHOTS OF HALON FIRE EXTINGUISHER. C/A:1. FOUND R1 WINDSHIELD BUS BAR TERMINAL A ON LWR R/S OF WINDSHIE LD LOOSE AND PLASTIC TERMINAL COVER MELTED.2. LUX STATION: R1 WINDSHIELD BUS BAR TERMINAL A RETIGHTENED AND WINDOW HEAT SYS GND TEST PASSED. PLASTIC COVER NEEDS TO BE REINSTALLED. XFRD TO DD LOG PAGE D0056501 FOR ARCING DAMAGE.TPE STATION: R1 WINDSHIELD ASSAY REPLACED FOR MAINTENANCE PREVENTION, DD ITEM CLOSED.3. THIS AIRCRAFT WAS DELIVERED FROM BOEING ON SE P 25, 2002. REPORT THE POOR QUALITY TO BOEING AND WAITING FOR INVESTIGATION RESULT FROM BOEING. 2 L 7 4 4F 4 F RT A20WE E23EA 2002100100001 20021001 00001 NM 2002 10 1 PCAA0209115 1 20020929 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM LEFT INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 811AW 14064 201 DURING ROUTINE MAINTENANCE VISIT LEFT AFT FUSELAGE EMERGENCY LIGHTS FOUND INOPERATIVE. SYSTEM WAS TROUBLESHOT AND LEFT E MERGENCY LIGHTING POWER SUPPLY BOX FOUND AT FAULT. BOX WAS REPLACED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2002100100002 20021001 00002 EU 2002 10 1 DHL2002364012 1 20020928 A 2120 B38QA6505 VALVE AIRBUS 300 A300B4203 3930306 EU A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 AFT CARGO COMPARTMENT ISOLATION VALVES CURCUIT BREAKER POPS DURING CABIN SMOKE DETECTOR TEST.DEFERRED IAW MEL 21-62-02 C AT C. ENTERED AS DMI #10510. REMOVED AND REPLACED AFT L/SIDE ISOLATION VALVE AS PER MM 21-64-32. GROUND OPS CHECKED NO RMAL. THIS CLEARS DMI #10510. 2 L 7 2 4F RT A35EU 2002100100003 20021001 00003 WP 2002 10 1 0203159154 1 20020904 A 5310 LONGERON DOUG DC9 DC914 3022034 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 During Hck in ATL, a crack was found in the forward end of longeron 29L at staion 361 under a production splice. Repaire d per EA 91-190684. 2 L 7 2 4F A6WE 2002100100004 20021001 00004 WP 2002 10 1 0203169154 1 20020913 A 5330 SKIN DOUG DC9 DC914 3022034 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 During an HCK in ATL, two areas of corrosion were found in the fuslage skin. Repaired per EA 91-190676. 2 L 7 2 4F A6WE 2002100100005 20021001 00005 WP 2002 10 1 0203179154 1 20020913 A 5310 SKIN DOUG DC9 DC914 3022034 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 During Hck in ATL, cracks have been found on the fuselage skin at sta 503 between L17 and L18 LHS. Repaired per EA 91-19 0691. 2 L 7 2 4F A6WE 2002100100006 20021001 00006 WP 2002 10 1 0203189154 1 20020922 A 5310 BULKHEAD DOUG DC9 DC914 3022034 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 During Hck in ATL, a typical crack was found in the pressure panel at sta 105 and X=35. Also, corrosion was found betwee n x=-25 and x=-35. Repaired per EA 91-190674. 2 L 7 2 4F A6WE 2002100100007 20021001 00007 WP 2002 10 1 0203199616 1 20020905 A 5330 SKIN DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 616NW 47229 During Hck in DHN, the fuselage skin was found cracked at teh forward entry door cutout lower aft corner. Repaired per E A 96-191339. 2 L 7 2 4F A6WE 2002100100008 20021001 00008 WP 2002 10 1 0203209756 1 20020913 A 5330 SKIN DOUG DC9 DC941 302207N WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 756NW 47180 While in DHN for Hck, a .44 inch crack was found in the skin at a fastener hole 5" above Longeron 18 right. Repaired per EA 97-191331. 2 L 7 2 4F A6WE 2002100100009 20021001 00009 WP 2002 10 1 0203219867 1 20020719 A 5310 BRACKET DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 47786 During Mck in ATL, 2 cracks were found on the left and right station 69 brackets X=+- 10". Repaired per EA 98-190582. 2 L 7 2 4F RT A6WE 2002100100010 20021001 00010 WP 2002 10 1 0203229867 1 20020724 A 5720 RIB DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 47786 During Mck in ATL, a crack was found in the left wing leading edge rib at station x 134.921. The crack emanates from the fastener hole and extends inbrd to the edge of the part. Repaired per EA 98-190577. 2 L 7 2 4F RT A6WE 2002100100011 20021001 00011 WP 2002 10 1 0203239863 1 20020725 A 5310 BULKHEAD DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 772NC 47774 During Mck in ATL, a crack was found in the flight compartment horizontal pressure panel at station 105. The crack is lo cated at X=35. Repaired per EA 98-190571. 2 L 7 2 4F RT A6WE 2002100100012 20021001 00012 WP 2002 10 1 0203249867 1 20020802 A 5310 ANGLE DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 47786 During Mck in ATL, corrosion was found in the left upper cusp angle at station 200. Repaired per EA 98-190596. 2 L 7 2 4F RT A6WE 2002100100013 20021001 00013 WP 2002 10 1 0203259856 1 20020802 A 5310 BULKHEAD DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 765NC 47718 During Mck in ATL, a 2" crack was found in the flight compartment horizontal pressure panel at station 105 X=35. Repaire d per EA. 98-190618. 2 L 7 2 4F RT A6WE 2002100100014 20021001 00014 WP 2002 10 1 0203269867 1 20020812 A 5310 INTERCOSTAL DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 47786 During Mck in ATL, the inbrd edge of the floor support intercostal at station 180 was found with two cracks between x=20 and x=30. 2 L 7 2 4F RT A6WE 2002100100015 20021001 00015 WP 2002 10 1 0203279856 1 20020829 A 5330 SKIN DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 765NC 47718 During Mck in ATL, a .5" skin crack was found at station 1135, 1 inch below L17. Also a dent was found at Sta 1135. Repa ired per EA 98-190648. 2 L 7 2 4F RT A6WE 2002100100016 20021001 00016 WP 2002 10 1 0203289856 1 20020830 A 5320 FLOOR PANEL DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 765NC 47718 During Mck in ATL, the galley floor panel was found with a soft condition and a 4 inch crack in the aft floor panel web edge. Repaired per EA 98-190673. 2 L 7 2 4F RT A6WE 2002100100017 20021001 00017 WP 2002 10 1 0203299852 1 20020909 A 5310 BULKHEAD DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 During Mck in ATL, a crack was found in the flight compartment horizontal pressure panel at station 105. Repaired per EA 98-190706. 2 L 7 2 4F RT A6WE 2002100100018 20021001 00018 WP 2002 10 1 0203319919 1 20020904 A 5310 LONGERON DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 941N 47450 During an Hck in ATL, an existing repair was found cracked. The crack at station 320 was repaired per EA. 99-190665. 2 L 7 2 4F A6WE 2002100100019 20021001 00019 WP 2002 10 1 0203329910 1 20020912 A 5310 PRESSURE PANEL DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 During HCK in ATL, a crack was found in the flight compartment horizontal pressure panel at station 105, X=-35. Repaired per EA 99-190722. 2 L 7 2 4F A6WE 2002100100020 20021001 00020 WP 2002 10 1 0203339910 1 20020913 A 5310 PRESSURE PANEL DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 Duirng Hck in ATL, a crack was found in the flight compartment horizontal pressure panel at station 105. The crack is lo cated at x=+35. Repaired per EA 99-190723. 2 L 7 2 4F A6WE 2002100100021 20021001 00021 NM 2002 10 1 CALA0200478 1 20020928 A 5311 FRAME BOEING 737 7373T0 1384582 NM STA 807 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND A 1" CRACK IN FRAME AND FRAME WAS BENT IN AFT PIT AT STA 807 BETWEEN STRINGER 23L AND 24L. A FRAME REPA IR WAS INSTALLED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2002100100022 20021001 00022 NM 2002 10 1 CALA0200479 1 20020929 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 270-294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 INSPECTION FOUND SEAT TRACK CORRODED BETWEEN STA 270 AND 294.5, RBL 43 UNDER G-1 GALLEY. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52 AND 51-10-02. 2 L 7 2 4F RT A16WE 2002101700019 20021017 00019 NM 2002 10 17 2002UALA01341 1 20020823 A 2160 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN TEMP FAILED A UALA B A EMER. DESCENT UNSCHED LANDING M OVER TEMP CL CLIMB 1 WP 29 540UA 25252 COCKPIT VERY HOT, TEMPERATURE UNCONTROLLABLE. NO EVAC OCCURRED. NO OVERWEIGHT LANDING IN DTW. REPLACED TRIM AIR PRESSU RE REGULATING VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100100023 20021001 00023 NM 2002 10 1 2002UALA01486 1 20020924 A 5311 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 1 RIGHT HAND MAIN ENTRY DOOR BODY TORQUE FUSE PRESSURIZED SUPPORT WEB GOUGED. MAJOR REPAIR ACCOMPLISHED. NEW WEB INST ALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100100024 20021001 00024 NM 2002 10 1 2002UALA01487 1 20020924 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 AFT CARGO FUSELAGE FRAME DENT STATION 1420 STRINGER 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100100025 20021001 00025 NM 2002 10 1 2002UALA01493 1 20020925 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 605UA 21866 AFT CARGO PIT AT BODY STATION 1080-1087, STRINGER 33L IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER. 2 L 7 2 4F 4 F RT A1NM E3NE 2002100100026 20021001 00026 EA 2002 10 1 COMA0260548 1 20020926 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS CR CRUISE 1 SO 01 472CA 1 1 7667 FLIGHT 5506 - FLAPS FAIL CAUTION MESSAGE.REPLACED THE L/H BPSU. 2 L 7 2 4F RT A21EA 2002100100027 20021001 00027 EA 2002 10 1 COMA0260547 1 20020927 A 3350 64643 LAMP CNDAIR CL600 CL6002B19 1900309 EA FLOOR INOPERATIVE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 455CA 7592 FLIGHT 5961 EMERGENCY FLOOR PATH LIGHTING INOP ROWS 3-7.REPLACED TRACK LIGHT POWER STRIPS. 2 L 7 2 4F RT A21EA 2002100100028 20021001 00028 EA 2002 10 1 COMA0260546 1 20020926 A 2710 CLREF27672768 PULLEY CNDAIR CL600 CL6002B19 1900309 EA WING BINDING A COMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 934CA 7042 AUTO PILOT LWD AND RWD CAUTION - AILERON CONTROL EXTREMELY DIFFICULT.REPLACED THE L/H AND R/H AILERON BELLCRANK ASSY IN MLG WHEEL WELLS. 2 L 7 2 4F RT A21EA 2002100100029 20021001 00029 WP 2002 10 1 ABXA020204 1 20020826 A 5330 59114065 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 FUSELAGE SKIN CRACKED AT UPPER/AFT STOP. REPAIRED UPPER AFT DOOR CUTOUT IAW DC-9 SRM 53-05. 2 L 7 2 4F A6WE 2002100100030 20021001 00030 WP 2002 10 1 ABXA020206 1 20020827 A 5313 5920319 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 LONGERON 29 LEFT FORE AND AFT OF SPLICE CRACKED AT FS 408. REPLACED SECTION OF LONGERON IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2002100100031 20021001 00031 WP 2002 10 1 ABXA020207 1 20020915 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 DURING AIRCRAFT LINE OPERATIONS AT ILN, MAINTENANCE DISCOVERED LOWER INNER SKIN CORROSION AT FS STA 380 TO STA 395, BETW EEN LONGERONS 35 LEFT TO 35 RIGHT. REMOVED CORROSION FROM SKIN AND INTERNAL DOUBLER. THE SKIN AND INTERNAL DOUBLER WER E CUT OUT. FABRICATED DOUBLER, TRIPLER, AND FILLER. INSTALLED AND IDENTIFIED IAW REA D853-45139-MR. 2 L 7 4 4F 4A25 2002100100032 20021001 00032 WP 2002 10 1 ABXA020208 1 20020814 A 5280 4925884201 HINGE DOUG DC9 DC941 302207N WP RT MLG CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 RIGHT MAIN LANDING GEAR INBOARD DOOR HINGE WAS CRACKED. REMOVED AND REINSTALLED THE RIGHT MAIN LANDING GEAR DOOR FOR HI NGE CHANGE IAW DC-9 MM 32-12-01-2-02-01, SRM 51-30-1, 51-30-5 AND 52-05. 2 L 7 2 4F A6WE 2002100100033 20021001 00033 WP 2002 10 1 ABXA020209 1 20020814 A 5320 39248461 ANGLE DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 EXFOLIATED ANGLE ON OUTBOARD END OF SLANT PANEL. REPLACED ANGLE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002100100034 20021001 00034 WP 2002 10 1 ABXA020210 1 20020814 A 5320 991150060AX INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 INTERCOSTAL JUST BELOW RIGHT RADOME HINGE WAS CRACKED AT CUTOUT. REPLACED INTERCOSTAL AND INSTALLED FASTENERS IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002100100035 20021001 00035 WP 2002 10 1 ABXA020211 1 20020816 A 5320 99107555 WEB DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 CUSP WEB WAS CRACKED AT STA 1041, LONGERON 18 LEFT. REPLACED CUSP WEB STRINGER IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002100100036 20021001 00036 NM 2002 10 1 ABXA020214 1 20020922 A 3350 CONNECTOR BOEING 767 767200 1385120 NM CABIN NOT SEATED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 775AX 22790 EMERGENCY LIGHTS WOULD NOT STAY ON. FOUND EMERGENCY BATTERIES DEPLETED. CHARGED USING AIRCRAFT POWER. TROUBLESHOT WIR ES IAW B767 WD 33-51-11. CHECKED GOOD. RESEATED PLUG D5124P. OPS CHECKED GOOD IAW B767 MM 31-51-00. EMERGENCY LIGHTS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2002100100037 20021001 00037 WP 2002 10 1 ABXA020215 1 20020920 A 3397 WIRE DOUG DC8 DC863 302198A WP CABIN BROKEN A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 822AX 46079 EMERGENCY EXIT LIGHTS DISARM CHECK WAS INOPERATIVE. FOUND WIRE NR 1 BROKEN AT EMERGENCY LIGHT SWITCH (R7-61). REPAIRED WIRE IAW DC-8 WD 33-51-01. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2002100100038 20021001 00038 WP 2002 10 1 ABXA020216 1 20020924 A 3350 60030451 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 972AX 21 47631 COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CHECKED GOOD IAW DC9 AMM 33-53-00. 2 L 7 2 4F A6WE 2002100100039 20021001 00039 WP 2002 10 1 ZW0A0209601 1 20020913 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9624T 53594 DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION IN CABIN FLOORBEAM, STATION 1155, FROM LBL 22 INCHES TO OTBD . REPLACED PART PER SRM 51-30-0 FASTENER INSTALLATION AND SRM 6-70-01 FOR PART INSTALLATION. 2 L 7 2 4F RT A6WE 2002100100040 20021001 00040 NM 2002 10 1 ZW0A0209602 1 20020912 A 5414 SKIN BOEING 757 7572Q8 1384972 NM NR 2 PYLON CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 702TW 28162 DURING CHECK-C MAINT IN THE NUMBER 2 PYLON, THE FWD ACCESS HOLE TO INTERIOR AT APPROX NAC STA 116.5, THE OTBD SIDE OF PY LON HAD CRACK 1.625 INCHES LONG. CRACK LOCATED TOP FWD SECTION OF ACCESS HOLE. CRACK IS VISIBLE ON OTBD AND INBD SIDE OF SKIN. 2 L 7 2 4F RT A2NM 2002100100041 20021001 00041 NM 2002 10 1 ZW0A0209603 1 20020912 A 5414 SKIN BOEING 757 7572Q8 1384972 NM NR2 PYLON CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 702TW 28162 DURING CHECK-C MAINT CRACKS FOUND ON NUMBER 2 PYLON THE FWD ACCESS HOLE AT NACELLE STA 116.5, OTBD AND INBD OF PYLON, CR ACKS 1.625 INCHES LONG AT TOP FWD SECTION OF ACCESS HOLE. CRACK IS VISIBLE ON OTBD AND INBD SIDE OF SKIN. ACCOMPLISHED BOEING SERVICE BULLETIN 757-54-0037 DIRECTED BY EMLR 73249 TO INCORPORATE REPAIR. 2 L 7 2 4F RT A2NM 2002100100042 20021001 00042 NM 2002 10 1 ZW0A0209604 1 20020913 A 5414 SKIN BOEING 757 7572Q8 1384972 NM PYLON CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 702TW 28162 DURING CHECK-C MAINT FOUND CRACKS IN PYLON DURING REPAIR. FWD ACCESS HOLE NACELLE STA 116.5 EMITTING FWD APPROX 1.5 INC HES, INBD AND OTBD SIDES. ACCOMPLISHED REPAIR PER EMLR 73252 AND SB 757-54-0037. 2 L 7 2 4F RT A2NM 2002100100043 20021001 00043 NE 2002 10 1 ZW0A0209701 2 20020921 A 7200 ENGINE BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE RIGHT MALFUNCTIONED A ZW0A A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 CE 13 719TW 28487 4943 ON CLIMB OUT THE RT ENGINE STALLED, EGT ROSE, AND THE ENGINE STOPPED RUNNING. THE FLIGHT RETURNED TO CUN. THE ENGINE W AS CHANGED. --OPEN-- 2 L 7 2 4F 4 F RT A2NM E17NE 2002100100044 20021001 00044 WP 2002 10 1 ZW0A0209703 1 20020917 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9624T 53594 DURING CHECK-C MAINT FOUND CORROSION ON FLOOR TRACK AT NUT PLATE HOLES FROM STA 1218 TO 1297, RBL 18. LOCATED HOLES AND INSTALLED NEW TRACK PER SRM 6-70-01. 2 L 7 2 4F RT A6WE 2002100100045 20021001 00045 WP 2002 10 1 ZW0A0209704 1 20020918 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9624T 53594 DURING CHECK-C MAINT FOUND CORROSION IN FASTENER HOLES IN LONGITUDINAL FLOOR BEAM 11 INCHES INBD OF DOOR THRESHOLD FROM STA 1155 TO 1211. REPLACED FLOOR BEAM PER SRM 6-70-01. 2 L 7 2 4F RT A6WE 2002100100046 20021001 00046 WP 2002 10 1 ZW0A0210001 1 20020925 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 925TW 49357 THE ESCAPE PATH LIGHTING IN THE FIRST CLASS SECTION CAME ON IN FLIGHT AND STAYED ON WITH SWITCH IN ARM POSITION. REPLACE D THE POWER SUPPLY FOR FIRST CLASS. 2 L 7 2 4F A6WE 2002100100047 20021001 00047 WP 2002 10 1 ZW0A0210101 1 20020926 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 925TW 49357 THE EMERGENCY ESCAPE PATH LIGHTING ILLUMINATED DURING FLIGHT IN FIRST CLASS CABIN. REPLACED EGRESS POWER SUPPLY NUMBER 2 AT ROWS 7 AND 8. 2 L 7 2 4F A6WE 2002100100048 20021001 00048 NM 2002 10 1 ZW0A0210201 1 20020928 A 2421 729825J IDG BOEING 757 757231 1384950 NM LT ENGINE MALFUNCTIONED A ZW0A A UNSCHED LANDING J B H WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC CL CLIMB 1 CE 13 705TW 28479 THE LEFT GENERATOR CONTROL OFF LIGHT AND LEFT BUS TIE ISOLATION LIGHT ILLUMINATED, ACCOMPANIED BY SMOKE IN CABIN AND COC KPIT. FLIGHT RETURNED TO TPA. CHANGED THE LEFT IDG AND LEFT GENERATOR CONTROL PANEL. 2 L 7 2 4F RT A2NM 2002100100049 20021001 00049 EA 2002 10 1 COMA0260545 1 20020927 A 3241 D3899926KA35SN CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA L/H MLG DEFECTIVE A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 959CA 7116 FLIGHT 6039 ANTI SKID CAUTION DURING T/O.REPLACED THE L/H OTB WHEEL SPEED TRANSDUCER CONNECTOR. 2 L 7 2 4F RT A21EA 2002100100050 20021001 00050 EA 2002 10 1 COMA0260549 1 20020927 A 5240 SERVICE DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 966CA 7132 FLIGHT 5804 - LOUD NOISE AFTER T/O. GROUND INTERCOM DOOR LEFT OPEN.INSPECTED FOR DAMAGE AND CLOSED DOOR. 2 L 7 2 4F RT A21EA 2002100100051 20021001 00051 EA 2002 10 1 COMA0260550 1 20020927 A 2410 WIRE CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 735CA 7267 FLIGHT 5637 IDG CAUTION MESSAGE DURING T/O.REPAIRED WIRING AT IDG TEMP PROBE. 2 L 7 2 4F RT A21EA 2002100100052 20021001 00052 EA 2002 10 1 COMA0260551 1 20020927 A 2740 TRIM MOTOR CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J N WARNING INDICATION FALSE WARNING TO TAKEOFF 1 SO 01 982CA 7168 FLIGHT 5674 STAB TRIM CAUTION MESSAGE DURING T/O.COULD NOT DUPLICATE. FOUND NO DEFECTS WITH SYSTEM. 2 L 7 2 4F RT A21EA 2002100100053 20021001 00053 EA 2002 10 1 COMA0260552 1 20020928 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 455CA 1790 7592 FLIGHT 6074 - EMERGENCY LIGHTS BATTERY IS DEAD.REPLACED BATTERIES. 2 L 7 2 4F RT A21EA 2002100100054 20021001 00054 EA 2002 10 1 COMA0260553 1 20020928 A 3350 383782 LAMP CNDAIR CL600 CL6002B19 1900309 EA FLOOR INOPERATIVE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 FLIGHT 5582 FWD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP.REPLACED FLEXIBLE LAMP SECTION. 2 L 7 2 4F RT A21EA 2002100100055 20021001 00055 EA 2002 10 1 COMA0260554 1 20020930 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 409CA 7441 FLIGHT 5706 FLAPS FAIL CAUTION.RESET FLAP SYSTEM AND DEFERRED MAINT.PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002100100056 20021001 00056 EA 2002 10 1 COMA0260555 1 20020930 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 986CA 7174 FLIGHT 5460 LANDING GEAR DISAGREE WARNING.COULD NOT DUPLICATE. LANDING GEAR EXTENSION AND RETRACTION CHECKS NORMAL. 2 L 7 2 4F RT A21EA 2002100100057 20021001 00057 NM 2002 10 1 AWXA200200957 1 20020906 A 5320 654860710 ANGLE BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 0 0 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK A 5/16" CRACK WAS FOUND ON R/H RAM AIR SCOOP SUPPORT ANGLE BS 539. MAINTENANCE CU TOUT DAMAGE ON SUPPORT ANGLE AT BS 539, FABRICATED 1 EACH REPAIR AND SPLICE ANGLE, AND INSTALLED REPAIR PARTS IAW B737-3 00 SRM 51-70-11, PG. 1-6, FIG. 1. 2 L 7 2 4F RT A16WE 2002100200001 20021002 00001 EA 2002 10 2 CA020910001 1 20020905 A 5610 WINDOW PPG NP1393221 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 15087 95310H8414 (CAN) DURING FLIGHT, LT SIDE WINDOW CRACKED. DIVERTED FLIGHT. LT SIDE WINDOW REPLACED IN ACCORDANCE WITH AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002100200003 20021002 00003 NE 2002 10 2 CA020913001 1 20020731 A 6320 S6135220173 RING GEAR SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE M/R GEARBOX CRACKED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING NORMAL OPERATION, RING GEAR CRACKED, CHIP LIGHT ILLUMINATED, AIRCRAFT RETURNED FOR LANDING. GEARBOX REMO VED FOR FURTHER INVESTIGATION. REVEALED BROKEN TOOTH ON RING GEAR, BROKEN TOOTH ON PLANETARY PINION AND DAMAGED SUN GE AR. GEARBOX REPAIRED. FULL INSPECTION FOR METAL CONTAMINATION CARRIED OUT. 2 G 7 2 4U 4 U 1H15 1E3 2002100200004 20021002 00004 NM 2002 10 2 CA020916008 1 20020914 A 2530 8650010000 OVEN BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE GALLEY ODOR W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) FLT ATT REPORTED A BURNING SMELL IN THE REAR GALLEY NR 3 OVEN FOUND AT FAULT. CB PULLED AND COLLARED. NR 3 OVEN R EPLACED PER MM AND OPERATION CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 2002100200006 20021002 00006 SW 2002 10 2 CA020918010 1 20020902 A 5302 204030749017 BULKHEAD BELL 204 204B 1181404 SW LYC T53 T5313B 41549 NE TAIL BOOM CRACKED W B A EMER. DESCENT UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) T/R FLIGHT CONTROL BELLCRANK SUPPORT ATTACHES TO BULKHEAD. THE BULKHEAD IS REINFORCED BY LOWER ANGLE AND UPPER AN GLE, SUSPECT THAT THE LOWER ANGLE CRACKED PROBABLY DUE TO CORROSION (NOT VERIFIED). THIS ALLOWED THE SUPPORT TO MOVE AN D EVENTUALLY CRACKED THE BULKHEAD. WHEN THE BULKHEAD CRACKED,IT ALLOWED FOR THE T/R CHAIN PITCH CHANGE MECHANISM TO BECO ME DISENGAGED DUE TO EXCESSIVE MOVEMENTOF THE BELLCRANK SUPPORT. THE PITCH CHANGE MECHANISM RE-ENGAGED BUT WAS NOW COMPL ETELY OUT OF RIG RESULTING IN LOSS OF T/R AUTHORITY. 1 G 7 1 4U 4 U H1SW E17EA 2002100200008 20021002 00008 SO 2002 10 2 C2XA02BT059 1 20021002 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO LOOSE A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 16911 145446 EWR---CO3039, CREW REPORTED, THE GALLEY DOOR EMERGENCY LIGHT WAS INOPERATIVE....MAINTENANCE FOUND A LOOSE CONNECTOR AND RESECURED THE CANNON PLUG. OPS.CHECKED SYSTEM GOOD. 2 L 7 2 4T RT T00011AT 2002100200009 20021002 00009 NM 2002 10 2 UPS02239250 1 20020902 A 5312 PRESSURE PANEL BOEING 727 72762C 138402C NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 913UP 19245 INSPECTION TYPE:SEG4 RIGHT WHEEL WELL FWD BULKHEAD, JUST BELOW APU LOAD CONTROL VLV, HAS A 3.5 INCH CRACK TO 4 INCH CRAC K CRACKED THROUGH. STOP DRILLED CRACK AS PER B72 7 SRM 51-10-01, ACCOMPLISHED HFEC 51-000-00 FIG 4 NDT INSP CRACK CONTA INMENT CONFIRMED. INSTALLED DOUBLERS AND FILLERS AS PER B727 SRM 53-10-9 FIG 5. REPLACED KEEL BEAM SUPPORT ANGLE AT BS 870 AS PER BOEING DRAWING NR 66-12638. 2 L 7 3 4F A3WE 2002100200010 20021002 00010 NM 2002 10 2 UPS02239282 1 20020827 A 5230 SKIN BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C LWR FWD CARGO HOLD DOOR CRACK ON INNER SKIN ADJACENT TO LWR TORQUE UBE AT LIGHTNING HOLE. REPAIR CAR RIED OUT IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2002100200011 20021002 00011 NM 2002 10 2 UPS02239283 1 20020828 A 5320 WEB BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C RT LIGHTNING HOLE SECOND AFT UPPER HOLE ON STAIRWELL SIDE WALL AT 7 O'CLOCK POSITION IS CRACKED. CRAC K STOP DRILLED IAW SRM 51-10-01, REPAIRED IAW SRM 51-40-02. 2 L 7 3 4F A3WE 2002100200012 20021002 00012 NM 2002 10 2 UPS02239284 1 20020828 A 5320 WEB BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C LT LIGHTNING HOLE, FOURTH AFT UPPER HOLE ON LT AIRSTAIR WELL SIDE WALL IS CRACKED AT 5 O'CLOCK POSITIO N. CRACK STOP DRILLED IAW SRM 51-10-01 & REPAIR CARRIED OUT IAW SRM 51-40-02. 2 L 7 3 4F A3WE 2002100200013 20021002 00013 NM 2002 10 2 UPS02239288 1 20020827 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C SUSPECT CRACK INDICATION FOUND IN NOSE WHEEL WELL SIDEWALL AT BS 276 RT SIDE 3 INCH INDICATION IS LOCA TED 24 INCHES FROM NWW CEILING. DAMAGE REMOVED IAW SRM 51-10-1 REPAIRED AREA IAW SRM 51-40-02 FIG 1. 2 L 7 3 4F A3WE 2002100200014 20021002 00014 NM 2002 10 2 UPS02239392 1 20020902 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C CRACK INDICATION FOUND IN RIGHT WALL OF NOSE WHEEL WELL LOCATED AT B S 264.5 APPROX 7 INCHES FROM CEIL ING CRACK IS APPROX 2 INCHES LONG. HFEC INSPECT IAW NDT MAN PT6 51-00-00 FIG 4, CRACK CONFIRMED AND ENDS MARKED. DAMAG E REMOVED IAW SRM 51-10-01, HFEC CARRIED OUT ON CUTOUT NDF. REPAIR CARRIED OUT IAW SRM 51-40-02 FIG 1 2 L 7 3 4F A3WE 2002100200015 20021002 00015 NM 2002 10 2 UPS02239393 1 20020903 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C NLG RT PRESSURE WEB HAS SUSPECT CRACK AT BS 286 4 INCHES FROM SILL. HFEC CARRIED OUT IAW NDT MAN PT6 51-00-00 FIG 4 CRACK CONFIRMED AND ENDS MARKED. DAMAGE REMOVED IAW SRM 51-10-01. HFEC INSPECT CUTOUT TO CONFRM DAMAGE REMOVAL. REPAIRED IAW SRM 51-40-02 FIG 1. 2 L 7 3 4F A3WE 2002100200016 20021002 00016 NM 2002 10 2 2002UALA01281 1 20020802 A 2440 RELAY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERNAL POWER INTERMITTENT A UALA K NONE N FALSE WARNING CR CRUISE 1 WP 29 529UA 25019 RIGHT HYDRAULIC QUANTITY INDICATES ZERO. RIGHT HYDRAULIC PRESS NORMAL. TROUBLESHOT TO 115 V AC GROUND SERVICE TRANSFER BUS RELAY K102. RELAY WAS INTERMITTENT, K102 RELAY WAS REPLACED AND SYSTEM CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200024 20021002 00024 NM 2002 10 2 2002UALA01320 1 20020817 A 5313 STRINGER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 943UA 26680 STATION 188 LEFT HAND STRINGER 17 CRACKED VERIFIED WITH HFEC. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE & DOUBLER REP AIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100200025 20021002 00025 EU 2002 10 2 2002UALA01321 1 20020818 A 3350 SOCKET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 445UA 826 EMERGENCY EXIT LIGHTS FLOOR LIGHT DAMAGED AT 01L. ALL TROUBLESHOOTING PROCEDURES WERE FOLLOWED AND THE LIGHT BASE WAS R EPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002100200028 20021002 00028 NM 2002 10 2 2002UALA01324 1 20020816 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 CABIN FLOOR STRUCTURE FLOOR BEAM UPPER T-CAP AT STATION 324 STRINGER 17R 38 RBL TO 63 RBL HAD EXCESSIVE MATERIAL REMOVED IN PROCESS OF CORROSION CLEAN UP. MAJOR REPAIR ACCOMPLISHED. REMOVED SECTION OF T-CAP FROM 9 LBL TO 63 RBL AND INSTAL LED REPLACEMENT T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200030 20021002 00030 NM 2002 10 2 2002UALA01326 1 20020820 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 CABIN BODY FRAME STRINGER CLIP IS CRACKED BODY STATION 380 STRINGER 2R. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER C LIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100200032 20021002 00032 NM 2002 10 2 2002UALA01328 1 20020822 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 CABIN, STRINGER 10R STRINGER CLIP CRACKED AT MOST INBOARD ATTACH FASTENER. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGE R CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100200033 20021002 00033 NM 2002 10 2 2002UALA01329 1 20020822 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 CLIP AT STATION 440 STRINGER 9 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100200034 20021002 00034 NM 2002 10 2 2002UALA01330 1 20020822 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 FORWARD CABIN STRINGER CLIP CRACKED BODY STATION 344 STRINGER 12R. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100200035 20021002 00035 NM 2002 10 2 2002UALA01331 1 20020822 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 STATION 663.75, STRINGER 9L, CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100200036 20021002 00036 NM 2002 10 2 2002UALA01333 1 20020822 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 LEFT SIDE OF AIRCRAFT APPROXIMATELY 3 FEET AFT OF FORWARD ENTRY DOOR THERE IS A DENT. MAJOR REPAIR ACCOMPLISHED. INSTA LLED REPAIR DOUBLER AND STRINGER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100200037 20021002 00037 NM 2002 10 2 2002UALA01334 1 20020821 A 5415 BRACKET BOEING 777 777222 1385219 NM NR 2 NACELLE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 783UA 26950 NR 2 ENGINE CROSS TIE INBOARD LEG UPPER BRACKET IS BENT AND FASTENER CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED UPPE R BRACKET FOR CROSS TIE. 2 L 7 2 4F RT T0001SE 2002100200041 20021002 00041 NM 2002 10 2 2002UALA01343 1 20020824 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 CABIN DOOR 2L THRESHOLD INNER CREASE BEAM ANGLE CORRODED UNDER DOOR PAN AREA. MAJOR REPAIR ACCOMPLISHED. REPLACED INNER CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200053 20021002 00053 EU 2002 10 2 MALA020591 1 20020927 A 7600 7239060503 CTOT PANEL SAAB SF340 340B 7860101 EU A MALA D RETURN TO BLOCK P NO WARNING INDICATION NR NOT REPORTED 1 GL 15 361PX 340B249 CTOT INOP LH SIDE, DID NOT MOVE ON FLIGHT #3031. RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED CTOT PANEL PN 72390 60-503 SN/ON 0274, SN/OFF 0280. IAW SAAB AMM 76-10-50-4. OPS CHECKED GOOD. 2 L 7 2 4T RT A52EU 2002100200054 20021002 00054 NM 2002 10 2 2002UALA01357 1 20020826 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 AFT PIT STATION 1420 FUSELAGE FRAME HAS DENT IN UPPER CAP ABOVE STRINGER 26L AND HAS EXCESSIVE MATERIAL LOSS AT RBL 14 A ND LBL 2 TO LBL6. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME SECTION FROM PRODUCTION SPLICE AT STRINGER 24L TO CARGO DO OR SILL AT STRINGER 26R. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200055 20021002 00055 NM 2002 10 2 2002UALA01358 1 20020826 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 CABIN PRESSURE DECK BODY STATION 1680-1681 HAS 30 PERCENT MATERIAL LOSS RBL 52.5. MAJOR REPAIR ACCOMPLISHED. REPAIR DO UBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200056 20021002 00056 NM 2002 10 2 2002UALA01359 1 20020827 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 FORWARD CABIN FUSELAGE FRAME AT STATION 400 CRACKED AT FASTENER HOLE JUST ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100200057 20021002 00057 NM 2002 10 2 2002UALA01360 1 20020827 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 FUSELAGE FRAME CRACKED AT STATION 847 JUST ABOVE STRINGER 9R AT INBOARD FASTENER FOR PASSENGER SERVICE UNIT RAIL SUPPORT . MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100200058 20021002 00058 NM 2002 10 2 2002UALA01362 1 20020827 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 AFT PIT STATION 1280 BL 0 FRAME CAP CORROSION. MAJOR REPAIR ACCOMPLISHED. FRAME CAP STRAP REPAIRED INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002100200060 20021002 00060 NM 2002 10 2 UPS02239556 1 20020917 A 5310 BRACKET BOEING 727 72722C 138400F NM BS 500 S26L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI SMALL BRACKET ATTACHING AFT END OF INTERCOSTAL TO FRAME AT BS 500 IS CRACKED, INTERCOSTAL IS LOCAT ED ABOVE STR. 26L IN LWR FWD CARGO BAY BRACKET REPLACED IAW SRM 51-20-1, FIG 7 & SRM 51-30-02 2 L 7 3 4F A3WE 2002100200061 20021002 00061 NM 2002 10 2 UPS02239557 1 20020924 A 5510 PIN BOEING 727 72722C 138400F NM HORIZ. STAB. CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI HORIZ. STAB. HINGE R/H OUTER PIN HAS EVIDENCE OF PITTING CORROSION A DJACENT TO RELIEF RADIUS H ORIZ. STAB HINGE R/H O/B PIN REPLACED IAW MM 55-10-01 2 L 7 3 4F A3WE 2002100200062 20021002 00062 NM 2002 10 2 UPS02239558 1 20020923 A 5310 INTERCOSTAL BOEING 727 72722C 138400F NM BS 294 & 284 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI COCKPIT FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 294 & 284 LBL 5 REMOVED INTERCOSTAL IAW SRM 51- 30-2 FABRICATED INTERCOSTAL IAW SRM 53-10-2 & SRM 51-20-4 INSTALLED INTERCOSTAL IAW SRM 51-30-2 2 L 7 3 4F A3WE 2002100200063 20021002 00063 NM 2002 10 2 AWXA200200959 1 20020909 A 5753 6546466 ANGLE BOEING 737 737375 13844BN NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 0 0 23707 YVR - MAJOR REPAIR - DURING C-03 CHECK A 1" CRACK WAS FOUND ON THE L/H OUTBOARD MIDFLAP REAR SPAR TO RIB ATTACH ANGLE AT WBL 305.56. MAINTENANCE REMOVED L/H OUTBOARD MIDFLAP REAR SPAR TO RIB ATTACH ANGLE AT WBL 305.56. FABRICATED A NEW REPL ACEMENT ANGLE, AND INSTALLED REPAIR PART IAW DWG 65-46466, AND B737-300 SRM 51-40-02, PG. 12. 2 L 7 2 4F RT A16WE 2002100200064 20021002 00064 NM 2002 10 2 AWXA200200960 1 20020901 A 5311 69784122 SHEAR TIE BOEING 737 737375 13844BN NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 0 0 23707 YVR - MAJOR REPAIR - DURING C-03 CHECK A 3/8" CRACK WAS FOUND ON FRAME ATTACH ANGLE (SHEAR TIE) AT BS 727D, ABOVE STR 14 R/H. MAINTENANCE REMOVED DAMAGED SHEAR TIE AT BS 727D, FABRICATED A NEW SHEAR TIE, AND INSTALLED REPAIR PART IAW AWA E. R. 03-5362-02270-ES2. 2 L 7 2 4F RT A16WE 2002100900172 20021009 00172 NM 2002 10 9 F3LA200200266 1 20020930 A 5320 PANEL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON TRANSITION PANEL AT BS 787 TO BS 707. FABRICATED AND INSTALLED REPAI R PARTS PER SRM 53-60-53, SRM 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002100300001 20021003 00001 NM 2002 10 3 CALA0200480 1 20021002 A 3230 SOLENOID BOEING 737 737524 1384721 NM LEVER INSTL INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17620 27333 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM CLE. THE GEAR OVERRIDE TRIGGER WAS USED AND THE GEAR RAISED. THE A IRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A GEAR SWING AND COULD NOT DUPLICATE THE FAILURE. THE LANDING GEAR LEVER LOCK SOLENOID WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE IAW MM 32-31-31, PAGE 401. 2 L 7 2 4F RT A16WE 2002100300002 20021003 00002 NM 2002 10 3 CALA0200482 1 20021002 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 727C CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70352 23590 A WALKAROUND INSPECTION FOUND A 3" CRACK IN L/H FUSELAGE SKIN AT STA 727C, STRINGER 25L AND 26L. THE CRACKED AREA OF SKI N WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-00, FIGURE 201. 2 L 7 2 4F RT A16WE 2002100300003 20021003 00003 EU 2002 10 3 2002F00909 1 20020906 A 3246 BEARING SAAB SF340 340B 7860101 EU NLG FAILED A NSVA O OTHER O OTHER NR NOT REPORTED 1 EA 27 294CJ 340B294 CMH - AFTER AN UNEVENTFUL LANDING CREW TAXIED TO GATE AND DISCOVERED RIGHT FRONT NOSE WHEEL ASSEMBLY HAS SEPARATED FROM AXLE. WHEEL WAS RECOVERED IN PIT. MAINTENANCE REMOVED AND REPLACED NOSE WHEEL ASSEMBLY, AXLE AND TORQUE ARM. UPON FUR THER INVESTIGATION IT WAS DETERMINED THAT THE CAUSE OF THE BEARING FAILURE WAS DUE TO THE INTRODUCTION OF WATER/CONTAMIN ANTS INTO THE BEARING CREATING A BREAK DOWN OF THE LUBRICATING PROPERTIES OF THE GREASE. (M) 2 L 7 2 4T RT A52EU 2002100300004 20021003 00004 NM 2002 10 3 ASAA0210184 1 20020831 A 5320 6546547 WEB BOEING 737 737210C 1384459 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE CRACK IN WEB AT BS 727B-747, STRINGER 14R-15R. REPAIRED CRACK PER SRM. (M) 2 L 7 2 4F A16WE 2002100300005 20021003 00005 NM 2002 10 3 ASAA0270011 1 20020909 A 5230 146A611013 SKIN BOEING 737 737790 13844CN NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 617AS 30542 SEA - DURING MAINTENANCE CHECK, FOUND A DENT IN AFT CARGO DOOR. REPAIRED DENT WITH DOUBLER PER EA 5230-01176. (M) 2 L 7 2 4F RT A16WE 2002100300006 20021003 00006 NM 2002 10 3 ASAA0270012 1 20020909 A 5330 149A7210 STRUCTURE BOEING 737 737790 13844CN NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 617AS 30542 SEA - DURING MAINTENANCE CHECK, A GOUGE WAS FOUND IN THE PNEUMATIC ACCESS DOOR SURROUND STRUCTURE. CLEANED UP GOUGE AND INSTALLED REPAIR STRAP PER EA5310-02109. (M) 2 L 7 2 4F RT A16WE 2002100300007 20021003 00007 WP 2002 10 3 GTIA020963 1 20020828 A 5330 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FOUND EXISTING EXTERNAL DOUBLER AT FS 1193 TO 1211 BETWEEN L26L AND 29L REQUIRES REPLACEMENT. REMOVED EXISTING EXTERNAL DOUBLER. FABRICATED FINGER DOUBLER, DOUBLER AND FILLER. INSTALLED FINGER DOUBLER, DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2002100300008 20021003 00008 WP 2002 10 3 GTIA020965 1 20020910 A 2120 ODOR DOUG DC9 DC932 3022066 WP CABIN DETECTED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 12536 47113 ACY - FLT 276 - FLIGHT ATTENDANTS DETECTED A FAINT ODOR DURING THE INITIAL CLIMB BUT IT DISSIPATED BY LEVEL OFF. COULD NOT DETECT ANY ODOR WITH PACKS ON AND A/C RUNNING, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002100300009 20021003 00009 NM 2002 10 3 USAA020324 1 20020812 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 42462 23559 TPA - FOUND SKIN CRACKED .25 INCH, AT AFT END OF EQUIP COOLING EXHAUST. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53- 30-07. (M) 2 L 7 2 4F RT A16WE 2002100300010 20021003 00010 NM 2002 10 3 USAA020325 1 20020820 A 5240 6545871523 SKIN BOEING 737 737301 1384611 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 48363 23513 TPA - FOUND SKIN CRACKED 1.25 INCH LONG, FORWARD SERVICE DOOR SKIN ABOVE LOWER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 52-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2002100300011 20021003 00011 NM 2002 10 3 USAA020326 1 20020814 A 5542 SKIN BOEING 737 7373B7 1384580 NM RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 43237 24411 PIT - FOUND RUDDER WITH SKIN DAMAGE, STATION 7.60, 17.70. REPAIRED PER SRM 51-70-17, 55-40-01. (M) 2 L 7 2 4F RT A16WE 2002100300012 20021003 00012 NM 2002 10 3 USAA020327 1 20020814 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 22952 PIT - FOUND SKIN CRACKED 3.5 INCH, S25R BETWEEN STATION 727E AND 747. INSTALLED DOUBLER PER SRM 53-00-01 FIG 2. (M) 2 L 7 2 4F RT A16WE 2002100300013 20021003 00013 NM 2002 10 3 USAA020328 1 20020819 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 50807 22956 CLT - FOUND SKIN CRACKED 2 INCHES, LEFT SIDE FUSELAGE STRINGER 24 BETWEEN STATION 727D AND 727E. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2002101000118 20021010 00118 NM 2002 10 10 F3LA200200267 1 20020930 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR SUPPORT AT BS 727C (-4), LBL 8, AT NUTPLATE. REMOVED DAM AGED FLOOR SUPPORT CHANNEL. FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 53-00-53, 51-40-02, AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002101000119 20021010 00119 NM 2002 10 10 F3LA200200268 1 20020930 A 5320 ATTACH ANGLE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON LT. LAVATORY WALL ATTACH ANGLE, BS 994. REPLACED ATTACH ANGLE PER S RM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002100300019 20021003 00019 NM 2002 10 3 F3LA200200270 1 20020930 A 5320 ATTACH ANGLE BOEING 737 737301 1384611 NM CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON RT. AFT LAV WALL ATTACH ANGLE. FABRICATED AND INSTALLED REPLACEMENT ATTACH ANGLE PER BOEING DRAWING 65-73223 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002100300023 20021003 00023 NM 2002 10 3 2002F00910 1 20020901 A 3350 1000677 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 DURING PREFLIGHT TRANSIT, FOUND L2 DOOR OVERHEAD EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED L2 OVERHEAD EXIT LIGHT BA TTERY PACK AND OPS CHECK OK IAW MM 33-50-31. (M) 2 L 7 3 4F A3WE 2002100300024 20021003 00024 EA 2002 10 3 2002F00911 1 20020820 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 97325 7325 FLT 6070 - PHX-EUG - MID CABIN CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE MEL'D. DURING OVERNIGHT MAINTENA NCE, THE LIGHT WAS REPLACED. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002100300025 20021003 00025 EA 2002 10 3 2002F00912 1 20020826 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77260 7260 FLT 6002 - PHL-LAX - DURING PREFLIGHT, THE CREW DISCOVERED THAT TWO OVERHEAD EMERGENCY EXIT LIGHTS WERE INOPERATIVE IN T HE MAIN CABIN. MAINTENANCE REPLACED THE BULBS. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2002100300026 20021003 00026 NE 2002 10 3 2002F00913 2 20020829 A 7200 ENGINE AIRBUS 320 A320233 3930329 EU IAE V2527 V2527EA5 NE NR 2 BIRD INGESTION A RJEF O OTHER C F.O.D. LD LANDING 1 SO 23 462TA 1334 SAP - DURING LANDING, ENGINE NR 2 EXPERIENCED A BIRD STRIKE. AFTER LANDING MAINTENANCE PERSONNEL PERFORMED INSPECTION O F THE ENGINE NR 2. AT THE MOMENT, AIRCRAFT REMAINS ON GROUND AT SAP STATION FOR INSPECTION AND MAINTENANCE. (M) 2 L 7 2 4F 4 F RT A28NM E40NE 2002101000122 20021010 00122 NM 2002 10 10 F3LA200200272 1 20020930 A 5240 DOOR BOEING 737 737301 1384611 NM LAVATORY SERVICE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED FWD LAVATORY SERVICE PANEL CORRODED. REPLACED LAVATORY SERVICE DOOR. 2 L 7 2 4F RT A16WE 2002100300027 20021003 00027 NE 2002 10 3 DL76G021003 2 20020827 A 7200 CF680C2B6F ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE #1 ENGINE FAILED A DALA J DUMP FUEL Z SIGNIFICANT FAILURE REPORT CL CLIMB 1 SO 27 169DZ 17129 17129 29689 704805 LEFT ENGINE SURGED. REPLACED #1 ENGINE. ETOPS CATEGORY 'C': UNCOMMANDED PWR CHANGES,SURGES,OR STALLS 2 L 7 2 4F 4 F RT A1NM E13NE 2002100300028 20021003 00028 NM 2002 10 3 DL738021029 1 20020903 A 5330 143A32322 SKIN BOEING 737 737832 13844CF NM FS 462, S-26R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DA 29621 FUSELAGE / SKIN / FS 462 / STRG. 26R-BL 0 : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS GOUGED AND PUNCTURED BY GROUND EQUIPMENT AT FS 462 BETWEEN STRINGERS 26R & BL 0. THE DAMAGE WAS REMOVED WITH A 20" X 8" CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER ER/A 383775-14, REV A. 2 L 7 2 4F RT A16WE 2002100300029 20021003 00029 NM 2002 10 3 DLM88021033 1 20020903 A 2910 290051518 TUBE DOUG MD88 MD88 3023688 NM LT THR REV CONT LEAKING A DALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 27 934DL 49721 ON CLIMB OUT HYD QTY ON LEFT SIDE ENGINE DROPS TO 3/4 QT FOLLOWED POM PROCEDURES AND SHUT OFF HYD PUMPS ON LEFT SIDE UNTI CONFIGURING FOR LANDING. CORR ACT. FOUND LINE LEAKING AT LEFT THRUST REVERSER MODULE. REPLACED LINE AND LEAK CHECKED. PERFORMED OPN 5089. CHECKS GOOD. 2 L 7 2 4F RT A6WE 2002100300030 20021003 00030 NM 2002 10 3 DL72S021034 1 20020903 A 5700 WEB BOEING 727 727232 1384082 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 CRACK ON O/B WEB OF #1 SLAT ACT. MOUNT BRACKET REPAIR PER M/M 57-20-021-8 2 L 7 3 4F A3WE 2002100300031 20021003 00031 NM 2002 10 3 DL73K021039 1 20020905 A 3350 WIRE UNK BOEING 737 737232 1384475 NM 8 DEF BROKEN A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 308DL 23080 AT 0700 FLT CREW REPORTED EMERGENCY LIGHT AT SEAT 8 DEF WAS INOP. FOUND BROKEN WIRE AND REPAIRED SAME. LIGHT NOW OP NML 2 L 7 2 4F RT A16WE 2002100300032 20021003 00032 NM 2002 10 3 DL73K021044 1 20020906 A 8010 1G309 SWITCH BOEING 737 737232 1384475 NM #1 ENGINE FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 306DL 23078 701140 IR - START VALVE ILLUMINATED AFTER T/O APPROX 2000' AGL. ENGINE SHUTDOWN IAW PILOTS OPERATING MANUAL. POSITIVE OIL PRESSURE ENTIRE FLIGHT. ENGINE SHUTDOWN APROX 15 MINUTES. NO OVERWIEGHT LANDING. CA - FOUND #1 ENGINE START VLV LIGHT ON WITH VALVE CLOSED. REPLACED #1 ENGINE START VALVE AND PRESSURE SW PER MM. RAN ENGINE VLV OPS AND INDICATION OK. PERFORMED WINDMILL INSP PER MM. MOS AND CHIP DETECTOR OK. LEAK CK OK. 2 L 7 2 4F RT A16WE 2002100300033 20021003 00033 NM 2002 10 3 DL72S021049 1 20020908 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN WEAK A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 532DA 22045 R1 OVERHEAD EMERGENCY LIGHT BARELY ILLUMINATES REPLACED BATTERIES OPS CK OK 2 L 7 3 4F A3WE 2002100300034 20021003 00034 NM 2002 10 3 DLM88021054 1 20020908 A 2750 3922841531 CABLE DOUG MD88 MD88 3023688 NM LT GEAR WELL BROKEN A DALA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 27 947DL 49878 DURING APPROACH THE LEFT FLAP INDICATION STUCK AT 0 DEGREES DURING FLAP EXTENSION. A/C ROLLED AND AUTO PILOT DISC A/C FLAP HANDLE RECYCLED AND FLAPS CAME DOWN NORMALLY HOWEVER A/C REQUIRED 2 UNITS OF RIGHT AILERON TRIM FOR REMAINDER OF APPROACH. C/A - INSPECTED AND FOUND FLAP BUS CABLE 34A BROKEN. REMOVED AND REPLACED FLAP BUS CABLES 34A AND 34B PER OPN 2000 RIGGEDPER M/M OPS CKS GOOD 2 L 7 2 4F RT A6WE 2002100300035 20021003 00035 NM 2002 10 3 DL738021063 1 20020911 A 2560 02031461201 LIGHT BOEING 737 737832 13844CF NM 2R DOOR BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3738B 30382 DOOR 2R EMERGENCY EXIT SIGN COVER LOOSE. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A16WE 2002100300036 20021003 00036 NM 2002 10 3 DL73K021088 1 20020916 A 3350 20131A BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 322DL 23094 EMERGENCY LIGHTS WOULD NOT TURN OFF - REPLACED BATTERY PACK 2 L 7 2 4F RT A16WE 2002100300037 20021003 00037 NM 2002 10 3 DL738021089 1 20020916 A 5610 WINDOW BOEING 737 737832 13844CF NM CAPTAINS L-1 LOOSE A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 37700 29631 ON CLIMBOUT EXCESSIVE WIND NOISE TURNED INTO EXTREME SQUEAL AT 10000 FEET AND ABOVE. PRESSURIZATION APPEARED NORMAL. ---RETORQUED CAPTS L-1 AND PRESURIZED AIRCRAFT OK FOR SVC 2 L 7 2 4F RT A16WE 2002100300038 20021003 00038 NM 2002 10 3 DL757021092 1 20020916 A 5310 143N85121 FRAME BOEING 757 757232 1384965 NM FS 620, S-25R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 FUSELAGE / C1 DOOR OPENING / LOWER SILL AND FS 620 FRAME : CORROSION REPAIR THE OUTER CHORD OF THE C1 DOOR OPENING LOWER SILL WAS FOUND DAMAGED DUE TO CORROSION. TO FACILITATE REPLACEMENT OF THE CHORD, THE FS 620 FRAME OUTER CHORD AND WEB WERE CUT BETWEEN STRINGERS 25R & 26R AND LOWER ENDS REMOVED. A NEW SILL CHORD WAS INSTALLED AND THE FRAME CHORD AND WEB SPLICED BACK IN PLACE WITH ALUMINUM REPAIR DOUBLERS AND ANGLES PER ER/A 383668-14, REV A. 2 L 7 2 4F RT A2NM 2002100300039 20021003 00039 NM 2002 10 3 DL76L021104 1 20020918 A 2120 4203651 VALVE BOEING 767 767332 1382001 NM FWD CARGO STUCK A DALA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 27 179DN 25144 WITH EQPT COOLING OPERATING IN STBY MODE DUE TO MEL 21-58-07 - AFTER TAKEOFF GOT AN OVHT LIGHT FOR THE EQPT COOLING. PLACED EQPT COOLING TO OVRD AND OVHT LIGHT WENT OUT. ELECTED TO OFF LAND TO JFK FOR FIX. CA FOUND SMOKE CLEARANCE VALVE V140 PARTIALLY OPEN AND INOPMANUALLY CYCLED VALVE SEVERAL TIMES THE VALVE STARTED TO WOR REMOVED VALVE.REPLACED OVERRIDE VALVE OPS CK OK.ALSO SPEED CKS OK ETOPS CATEGORY 'B': DIVERSION OR TURNBACK 2 L 7 2 4F RT A1NM 2002100300040 20021003 00040 NM 2002 10 3 DL733021124 1 20020923 A 5311 6546547251 FRAME BOEING 737 737347 1384647 NM FRAME CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305WA 23346 A CRACK WAS FOUND IN THE OUTER CHORD OF THE FS 727 FRAME AT STR 14L. THE .8 INCH CRACK WAS CUT OUT AND THE FRAME WAS REPAIRED WITH A .090 7075-T6 ANGLE. THE DAMAGE WAS FOUND ATHMV. 2 L 7 2 4F RT A16WE 2002100300041 20021003 00041 NM 2002 10 3 DL757021157 1 20020930 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FS 540, S-15L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 674DL 25979 FUSELAGE / SKIN ASSY / FS 520-550 / STRG. 14L-16L : GROUND DAMAGE REPAIR THE FUSELAGE WAS STRUCK BY GROUND EQUIPMENT RESULTING IN A LARGE DENTED AREA BETWEEN FS 520 & 550 FROM STRINGER 14L TO 16L. THE SKIN DAMAGE WAS REMOVED WITH A 30" X 10" CUTOUT. THE UNDERLYING STRINGERS WERE REPAIRED PER THE B757 SRM. THE SKIN CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383903-14, REV A. 2 L 7 2 4F RT A2NM 2002101000123 20021010 00123 NM 2002 10 10 F3LA200200273 1 20020930 A 5730 SKIN BOEING 737 737301 1384611 NM RT WING GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED RT WING LEADING EDGE AT INBD END OF NR 5 SLAT GOUGED. REPAIRED DAMAGE PER SRM 51- 70-17, FIGURE 19. 2 L 7 2 4F RT A16WE 2002100300042 20021003 00042 WP 2002 10 3 AALA20021163 1 20020809 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7549A 53031 TUL - FOUND CORROSION ON AFT CARGO DOOR THRESHOLD BEAM AT STATION 1163-1174. REMOVED AND REPLACED BEAM PER AARD 53-10-0 0. (M) 2 L 7 2 4F A6WE 2002100300043 20021003 00043 WP 2002 10 3 AALA20021180 1 20020815 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 549AA 53031 TUL - FOUND CORROSION ON AFT CX DOOR BEAM STATION 1163 TO 1174. INSTALLED NEW SERVICEABLE DOOR BEAM AFT CARGO PER AARD 53-10-00. (M) 2 L 7 2 4F A6WE 2002100300044 20021003 00044 WP 2002 10 3 AALA20021235 1 20020827 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 595AA 53285 TUL - FOUND DEEP WEAR ON FRAME AT STATION 1401 AT LONGERON 21R. REPAIRED FRAME AT 1401 AND LONGERON 21R PER ESO 80599. (M) 2 L 7 2 4F RT A6WE 2002100300045 20021003 00045 WP 2002 10 3 AALA20021239 1 20020815 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 595AA 53285 FOUND PITTING CORROSION IN BASE OF SEAT TRACK NR 3 FROM STATION 658 TO STATION 672. ROUTED OUT DAMAGED AREA AND INSTALL ED PLUG AS REQUIRED PER AARD 53-20-00-10. (M) 2 L 7 2 4F RT A6WE 2002100300046 20021003 00046 WP 2002 10 3 AALA20021240 1 20020816 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 595AA 53285 TUL - FOUND DENT IN FUSELAGE SKIN AT STATION 237 L19 LEFT. CUT OUT DAMAGED AREA OF SKIN AND INSTALLED REPAIR PER SRM 53 -04 FIG 12B. (M) 2 L 7 2 4F RT A6WE 2002100300047 20021003 00047 WP 2002 10 3 AALA20021241 1 20020816 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 595AA 53285 TUL - FOUND FUSELAGE SKIN CRACKED STATION 1380 LONGERON 14L. INSTALLED DOUBLER PER AARD 53-30-00-02. (M) 2 L 7 2 4F RT A6WE 2002100300048 20021003 00048 EA 2002 10 3 ASOA02434 1 20020801 A 3350 3071BPE LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 886AS 7531 FLT 4053 - DURING GROUND INSPECTION IN DFW, THE OVERHEAD EMERGENCY EXIT LIGHT BEFORE ROW 1 WAS INOPERATIVE. THE EMERGEN CY LIGHT ON THE AIRSTAIR DOOR WAS ALSO FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RESPECTIVE BURNED OUT EMERGENCY LIGHT BULBS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002100300049 20021003 00049 EA 2002 10 3 ASOA02435 1 20020801 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 853AS 7374 DURING C-CHECK INSPECTION IN MCN, A CRACK FOUND ON FRAME STATION 640 BETWEEN STRINGERS 13 RIGHT AND 14 RIGHT. MAINTENAN CE REPAIRED THE CRACKED FRAME IAW ASA EO 600-53-0076. (M) 2 L 7 2 4F RT A21EA 2002100300050 20021003 00050 SO 2002 10 3 ASOA02436 1 20020801 A 5330 12027430005 SKIN EMB 120 EMB120RT 3260202 SO FUSELAGE BIRD STRIKE A ASOA K NONE C F.O.D. NR NOT REPORTED 1 SO 11 246AS 120100 AN EMERGENCY LANDING WAS PERFORMED COMING INTO DFW DUE TO A BIRD STRIKE TO THE CAPTAINS WINDSHIELD. MAINTENANCE REMOVED AND REPLACED A DAMAGED PIECE OF SKIN IN FRONT OF THE WINDSHIELD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M ) 2 L 7 2 4T RT A31SO 2002101000125 20021010 00125 NM 2002 10 10 F3LA200200275 1 20020930 A 5320 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SPLICE PANEL AT BS 771 CORRODED. FABRICATED AND INSTA LLED REPLACEMENT PARTS PER SRM 51-10-01 AND 51-20-01. 2 L 7 2 4F RT A16WE 2002100300051 20021003 00051 SO 2002 10 3 ASOA02437 1 20020801 A 5315 12046155001 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 267AS 120198 DURING C-CHECK INSPECTION IN BNA, THE OMEGA BEAM WAS FOUND TO BE CORRODED OUT OF LIMITS AT FRAME STATION 4562. MAINTENA NCE REPAIRED THE CORRODED OMEGA BEAM IAW WITH ASA E0120-53-0181. (M) 2 L 7 2 4T RT A31SO 2002100300052 20021003 00052 SO 2002 10 3 ASOA02438 1 20020802 A 5753 12026801452 FITTING EMB 120 EMB120RT 3260202 SO T/E FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 240AS 2881 120060 DURING HANGAR MAINTENANCE IN TXK, THE RIGHT WING OUTBOARD FLAP OUTBOARD END CLOSURE FITTING WAS FOUND CRACKED. MAINTENA NCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002100300053 20021003 00053 EA 2002 10 3 ASOA02439 1 20020803 A 3350 364911 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 853AS 7374 DURING C-CHECK INSPECTION IN MCN, THE FIRST FLOOR TRACK EMERGENCY LIGHTING STRIP WAS INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE INOPERATIVE SECTION OF EMERGENCY LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002100300054 20021003 00054 NM 2002 10 3 SABA020096 1 20020919 A 3350 6104789 BATTERY DHAV DHC8 DHC8103 1386005 NM A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 880CC 277 Flight 5005 from AGS to CLT. Aircrew reported during pre-flight that the emergency floor lights would not test. Maintena nce removed and replaced the emergency battery packs and system ops checked good. Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002100300055 20021003 00055 SO 2002 10 3 ASOA02440 1 20020804 A 2520 SEAT EMB 120 EMB120RT 3260202 SO CABIN OUT OF POSITION A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 280AS 120231 DURING HANGAR INSPECTION IN MCN, THE EMERGENCY EXIT DOORS AT ROWS 5 AND 8 WERE INHIBITED FROM OPENING. MAINTENANCE FOUN D THE EXIT AT ROW 5 WAS OPENING AGAINST THE SEAT BACK AT ROW 4A. MAINTENANCE REPOSITIONED THE SEAT FOR SUFFICIENT CLEAR ANCE OF THE EXIT DOOR. MAINTENANCE RESECURED THE OVERHEAD PANEL TO THE CEILING AT ROW 8 TO ENABLE THE EXIT TO BE REMOVE D. OPERATIONAL CHECKS OF BOTH DOORS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002100300056 20021003 00056 EA 2002 10 3 ASOA02441 1 20020806 A 3350 3071BPE SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 828AS 7213 DURING HANGAR MAINTENANCE IN MCN, THE LIGHTED EMERGENCY EXIT SIGN AT THE PASSENGER DOOR ON THE FORWARD WALL WAS INOPERAT IVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR S ERVICE. (M) 2 L 7 2 4F RT A21EA 2002100300057 20021003 00057 NM 2002 10 3 HALA0200464 1 20020826 A 4910 INLET BOEING 717 717200 1383700 NM APU CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 475HA 55121 HNL - FOUND 4 INCH CRACK ON APU INLET BOX, APU INOPERATIVE. OK TO CONTINUE PER MEL 49-10-01. (M) 2 L 7 2 4F TR A6WE 2002100300058 20021003 00058 EU 2002 10 3 SIMA200224004 1 20020826 A 5347 7253742407 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 334AE 340B334 ABI - FOUND SEAT TRACK 36 L WORN ON TOP FLANGE. REMOVED AND INSTALLED SEAT TRACK IAW SAAB 340SRM (72LKS 3079 REV 40) CH APTER 51-40-21, 51-40-22, AND 51-40-25 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002100300059 20021003 00059 EU 2002 10 3 SIMA200224101 1 20020828 A 3220 LANDING GEAR SAAB SF340 340B 7860101 EU NLG BIRD STRIKE A SIMA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 21 330AE 340B330 ON ROTATION, THE AIRCRAFT HAD A BIRD STRIKE IN THE NOSE WHEEL WHEEL AREA. THE CREW DECLARED AN EMERGENCY AND RETURN TO LAX WITH NO FURTHER PROBLEMS. REMOVED BIRD REMAINS FROM UPPER NLG AND INSPECTED AREA WITH. NO DAMAGE NOTED. (M) 2 L 7 2 4T RT A52EU 2002100300060 20021003 00060 EU 2002 10 3 SIMA200224201 1 20020829 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU RT MLG DISCONNECTED A SIMA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 350CF 340B350 FSM - FLT 3535 - RIGHT MLG SAFE LIGHT FAILED TO ILLUMINATE. LAMP TEST GOOD. EMERGENCY WAS DECLARED. LANDING WAS NORMA L. FOUND CANNON PLUG ON RIGHT MLG NOT CONNECTED. INDICATION WAS REGAINED WHEN CANNON PLUG WAS RECONNECTED. AIRCRAFT W AS FERRIED TO LAW FOR LANDING GEAR EXTENSION/RETRACTION CHECKS IAW MAINTENANCE. INSPECTED DOWNLOCK ADJUSTMENT NO DEFECT S NOTED, OPS CHECK OF MLG GOOD. (M) 2 L 7 2 4T RT A52EU 2002100300061 20021003 00061 NM 2002 10 3 USA020353 1 20020906 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 45719 23595 PIT - FOUND SKIN WITH CRACKS TWO .5 INCH LONG, ONE .25 INCH LONG, STATION 380 E/E EXHAUST. CUT OUT CRACKS, INSTALLED EX TERNAL DOUBLER PER EA 74749, TR 53-30-07. (M) 2 L 7 2 4F RT A16WE 2002100300062 20021003 00062 NM 2002 10 3 USAA020283 1 20020726 A 7120 6035403 MOUNT BOEING 737 737401 1384701 NM PYLON WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 415US 18857 23883 PIT - FOUND ENGINE MOUNT WORN BEYOND LIMITS. MACHINED, CHAMFER, MPI, ROTOPEEN PER TYPICAL REP 50-50-08 REV B. (M) 2 L 7 2 4F RT A16WE 2002100300063 20021003 00063 NM 2002 10 3 USAA020329 1 20020801 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 23315 PIT - FOUND SKIN CRACKED 2.1 INCH, STATION 727E ABOVE STRINGER 24L IN AFT FUSELAGE SKIN. CRACKED AREA CUT OUT AND DOUBL ER INSTALLED PER SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2002101000126 20021010 00126 NM 2002 10 10 F3LA200200276 1 20020930 A 5320 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT FLOOR SPLICE AT BS 857. FABRICATED AND INSTALL ED REPLACEMENT FLOOR PANEL SPLICE STRIP PER SRM 51-10-01 AND 51-20-01. 2 L 7 2 4F RT A16WE 2002100300064 20021003 00064 NM 2002 10 3 USAA020330 1 20020830 A 5414 SKIN BOEING 737 7374B7 1384702 NM RT PLYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 36406 24555 PIT - FOUND PYLON SKIN CRACKED 1 INCH, RIGHT ENGINE PYLON ACCESS PANEL 5828R, STATION 196.700. STOP DRILLED CRACK, INST ALLED DOUBLER PER TYPICAL REPAIR 54-30-07. (M) 2 L 7 2 4F RT A16WE 2002100300065 20021003 00065 NM 2002 10 3 USAA020331 1 20020903 A 5313 6546877144 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 PIT - FOUND WEB BEAM CRACKED .25 INCH, FS 727, S18A RIGHT WEB BEAM FIRST INBOARD FAST HOLE. DEFECTIVE PART REPLACED WIT H IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2002100300066 20021003 00066 NM 2002 10 3 USAA020332 1 20020819 A 5314 KEELBEAM BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 42520 23555 CLT - FOUND KEEL BEAMS CORRODED, 4 AREAS, 7 CRACKS .25 INCHES, STATION 727-727A STRINGER 27L AND 27R. CORROSION REMOVED MECHANICALLY, SHIMS AND DOUBLER INSTALLED PER EA 74578. (M) 2 L 7 2 4F RT A16WE 2002100300067 20021003 00067 NM 2002 10 3 USAA020333 1 20020816 A 5511 RIB BOEING 737 7373B7 1384580 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 43323 24478 PIT - FOUND RIB CRACKED 3 INCHES LONG AND .005 INCH DEEP, RIGHT HORIZ STAB RIB, INBOARD END OF BALANCE PANEL. METAL BON D REPAIR PER TYPICAL REP 55-10-05 AND SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2002100300068 20021003 00068 NM 2002 10 3 USAA020334 1 20020815 A 5743 FITTING BOEING 737 7373B7 1384580 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 42286 24515 PIT - FOUND FITTING CRACKED .5 INCH, LEFT WING AT FASTENER HOLE MLG BEAM SUPPORT FITTING. FITTING REPLACED, MODIFIED PA RT INSTALLED PER EA 74450 AND EA 74371. (M) 2 L 7 2 4F RT A16WE 2002100300069 20021003 00069 NM 2002 10 3 USAA020335 1 20020821 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 48363 23513 TPA - FOUND 20 SQUARE INCHES OF CORROSION, AFT FRAME OF FORWARD LAVATORY DOOR, LOWER END PARTITION. REMOVED DAMAGED SEC TION AND SPLICED IN NEW SECTION PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2002100300070 20021003 00070 EA 2002 10 3 COMA0260556 1 20021001 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR BURNED OUT A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 810CA 7370 FLIGHT 5466 - 2 EXTERIOR EMERGENCY LIGHTS ARE INOP.REPLACED LIGHT BULBS. 2 L 7 2 4F RT A21EA 2002100300071 20021003 00071 EA 2002 10 3 COMA0260557 1 20020930 A 3230 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 927CA 13780 7031 FLIGHT 5214 GEAR DISAGREE WARNING, NLG INDICATED UNSAFE.REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2002101000127 20021010 00127 NM 2002 10 10 F3LA200200277 1 20021002 A 5313 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR STRINGER CORRODED AT BS 771, RBL 4. FABRICATED AND IN STALLED REPAIR PARTS PER SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002101000128 20021010 00128 NM 2002 10 10 F3LA200200278 1 20021002 A 5313 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR STRINGER CORRODED AT BS 771, RBL 8. FABRICATED AND IN STALLED REPAIR PARTS PER SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002100300072 20021003 00072 NM 2002 10 3 SABA020097 1 20020930 A 3350 1306 BULB DHAV DHC8 DHC8103 1386005 NM A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 883CC 162 Aircraft 883 Flight 5018 from CLT to PGV. During pre-flight the aircrew reported that the emergency floor lights at row six would not test. Maintenance replaced bulbs and system ops checked good. Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002101000129 20021010 00129 NM 2002 10 10 F3LA200200279 1 20021002 A 5320 THRESHOLD BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT DOOR THRESHOLD WEB CORRODED AT BS 787, RBL 25. FABRICATED A ND INSTALLED REPLACEMENT WEB PER SRM 53-60-15, 51-40-02, AND 51-10-02. 2 L 7 2 4F RT A16WE 2002101000130 20021010 00130 NM 2002 10 10 F3LA200200280 1 20021002 A 5320 PANEL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT LT TRANSITION PANEL CORRODED FROM BS 727C TO 827. FABRICATE D AND INSTALLED REPLACEMENT TRANSITION PANEL PER SRM 51-40-02, 53-60-53, 51-40-02 AND SOPM 20-41-07. 2 L 7 2 4F RT A16WE 2002101000131 20021010 00131 NM 2002 10 10 F3LA200200281 1 20021002 A 5320 BRACKET BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26302 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FWD ENTRY DOOR GIRT BAR BRACKETS. FABRICATED AND INSTALLED REPLACEME NT BRACKETS PER SRM 53-10-15, 51-20-00, 51-40-00, EO 51-00-737-001, AND BOEING DRAWING 65C16121. 2 L 7 2 4F RT A16WE 2002101000047 20021010 00047 NM 2002 10 10 F3LA200200285 1 20021002 A 5210 TORQUE TUBE BOEING 737 737301 1384611 NM AFT ENTRY DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED AFT ENTRY DOOR TORQUE TUBE CORROSION LENGTH OF TUBE. REPLACED TORQUE TUBE ASSEMBL Y PER OHM 52-16-01. 2 L 7 2 4F RT A16WE 2002100300073 20021003 00073 NM 2002 10 3 F3LA200200282 1 20021002 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM BS 947 - 967 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT BS 947 - BS 967, LBL 17. FABRICATED AND INSTALLED REP LACEMENT INTERCOSTAL PER SRM 53-60-51, 51-40-02 AND EA 53-737-181. 2 L 7 2 4F RT A16WE 2002101000048 20021010 00048 NM 2002 10 10 F3LA200200286 1 20021002 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION CARGO FLOOR SUPPORT BS727C(-4) LBL8. DETERMINED SUPPORT TO BE OUT OF LI MITS PER SRM 53-60-53. FABRICATED PARTS PER SRM 53-00-53 / SOPM 20-41-02. INSTALLED PER 737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002101000049 20021010 00049 NM 2002 10 10 F3LA200200287 1 20021002 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION FLOOR SUPPORT BS 986 TO 1006 LT. FABRICATED FLOOR SUPPORT AND INSTALLED AT BS 986-1006 LT PER SRM 53-60-51, SRM 51-40-2 MM 51-21-99 AND EA 53-737-181. 2 L 7 2 4F RT A16WE 2002100300074 20021003 00074 NM 2002 10 3 AWXA200200961 1 20020902 A 5414 311A14503 SKIN PANEL BOEING 737 737375 13844BN NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 0 0 23707 YVR - MAJOR REPAIR - DURING C-03 CHECK A 1/4" CRACK WAS FOUND ON THE # 1 ENGINE PYLON TOP FAIRING FORWARD OUTBOARD PANEL CUTOUT. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED., FABRICATED A DOUBLER, AND INSTALLED REPAIR PART IAW AWA E.R. 03-5455-02272-SS1. 2 L 7 2 4F RT A16WE 2002100300075 20021003 00075 NM 2002 10 3 AWXA200200967 1 20020904 A 5320 69784122 SHEAR TIE BOEING 737 737375 13844BN NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 0 0 23707 YVR - MAJOR REPAIR - DURING C-03 CHECK A 3/8" CRACK WAS FOUND ON SHEAR TIE ANGLE AT BS 727E, ABOVE STR 14 R/H. MAINTENAN CE REMOVED DAMAGED SHEAR TIE AT BS 727E, FABRICATED A NEW REPLACEMENT SHEAR TIE, AND INSTALLED REPAIR PART IAW AWA E.R. 03-5362-02270-ES2. 2 L 7 2 4F RT A16WE 2002100300076 20021003 00076 NM 2002 10 3 AWXA200200969 1 20020901 A 5414 311A145078 SKIN BOEING 737 737375 13844BN NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 0 0 23707 YVR - MAJOR REPAIR - DURING C-03 CHECK CORROSION WAS FOUND ON SKIN OF THE # 1 ENGINE PYLON UPPER FAIRING JUST FORWARD OF THE UPPER ATTACH POINT, SKIN BULGED BETWEEN SKIN JOINTS AS VIEW FROM UPPER SURFACE. MAINTENANCE REMOVED FASTENERS AND L IFTED SKIN ; CLEANED, BLENDED, TREATED, AND PRIMED CORRODED AREA; APPLIED MOLDABLE PLASTIC SHIM; RESECURED SKIN PER AWA E.R. 03-5455-02272-SS1. 2 L 7 2 4F RT A16WE 2002100300077 20021003 00077 NM 2002 10 3 AWXA200200970 1 20020920 A 5315 143N5140 WEB BOEING 757 757225 1384959 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 907AW 0 0 22691 LCQ - MAJOR REPAIR - DURING C-06 CHECK A 1/2" CRACK WAS FOUND EMANATING FROM LIGHTNING HOLE ON CABIN FLOOR WEB AT LBL 24 , BS 660 - 680. MAINTENANCE CUTOUT DAMAGED PORTION OF WEB, FABRICATED A REPAIR DOUBLER, AND INSTALLED REPAIR PART IAW B7 57-200 SRM 51-70-13, FIG. 1, PG. 1-2. 2 L 7 2 4F RT A2NM 2002100300078 20021003 00078 NM 2002 10 3 AWXA200200971 1 20020916 A 5315 BAC1520792 SEAT TRACK BOEING 757 757225 1384959 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 907AW 0 0 22691 LCQ - MAJOR REPAIR - DURING C-06 CHECK INTERGRANULAR CORROSION WAS FOUND ON R/H OUTBOARD SEAT TRACK BS 440. MAINTENANCE CUTOUT DAMAGED SECTION OF SEAT TRACK BS 440 TO BS 640. FABRICATED A NEW SECTION OF SEAT TRACK, AND INSTALLED REPAIR PART IAW B757-200 SRM 51-40-08, FIG. 5, PG. 13. 2 L 7 2 4F RT A2NM 2002100300079 20021003 00079 NM 2002 10 3 F3LA200200288 1 20021002 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM BS1006-1016 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT BS 1006 - 1016 RBL32.FABRICATED FLOOR SUPPORT ANDINSTAL LED FLOOR SUPPORT BS 1006 - 1016 RBL 32 PER SRM 51-40-02 & SRM 53-60-51. 2 L 7 2 4F RT A16WE 2002100300080 20021003 00080 EU 2002 10 3 C2XA02IA205 1 20020930 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 97841 280 IAH- DURING MAINTENANCE THE MECHANIC NOTED THAT NUMEROUS EMERGENCY LIGHTS FAILED TO ILLUMINATE ON THE FLOOR. IAH- MA INTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AT LOCATION 3WL, PERFORMED A OPERATIONAL CHECK OF THE EM ERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002100300081 20021003 00081 EU 2002 10 3 C2XA02IA206 1 20020930 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 97841 280 IAH- DURING MAINTENANCE THE MECHANIC NOTED THAT NUMEROUS EMERGENCY LIGHTS FAILED TO ILLUNINATE ALONG THE FLOOR. IAH- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY BATTERY AT LOCATION 18WL, PERFORMED A OPERATIONAL CHE CK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002100400001 20021004 00001 SO 2002 10 4 C2XA02SH071 1 20021004 A 5310 14521725001 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 DURING C CHECK INSPECTION CORROSION WAS FOUND ON NUTPLATE AT LT SILL BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED AND R EPLACED LT SILL BETWEEN FRAMES 18 AND 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100400002 20021004 00002 SO 2002 10 4 C2XA02SH073 1 20021004 A 5315 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 DURING C CHECK INSPECTION BUTTSRAP ON CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 23. MAINTENANCE REMOVED AND REPLACED CENTER FLOORBEAM BETWEEN FRAMES 18 AND 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED T O RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100400003 20021004 00003 SO 2002 10 4 C2XA02SH075 1 20021004 A 5315 14525991003 FLOORBEAM EMB 145 EMB145ER 3260211 SO CARGO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 SHV-DURING C CHECK FLOORBEAM DOUBLER AT FWD CARGO PARTITION WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACE D DAMAGED DOUBLER IAW EMB 145 SRM 51-20-03 AND SRM 51-04-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100400004 20021004 00004 SO 2002 10 4 C2XA02SH074 1 20021004 A 5320 14524222001 ANGLE EMB 145 EMB145ER 3260211 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 DURING C CHECK INSPECTION SPLICED ANGLE AT LT FLOORBEAM BETWEEN FRAMES 16 AND 17 WAS FOUND CRACKED. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100400005 20021004 00005 SO 2002 10 4 C2XA02SH077 1 20021004 A 5315 14522461011 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 SHV-DURING C CHECK INSPECTION DOUBLER ON RT LATERAL FLOORBEAM AT FRAME 20 WAS FOUND WITH CORROSION. MAINTENANCE REMOVED AND REPLACED DAMAGED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100400006 20021004 00006 SO 2002 10 4 C2XA02SH079 1 20021004 A 5315 14522461011 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 SHV-DURING C CHECK INSPECTION, LT LATERAL FLOORBEAM AROUND NUTPLATE HOLES WAS FOUND TO HAVE CORROSION. MAINTENANCE REMO VED DAMAGE AND PERFORMED A FLOORBEAM REPAIR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100400007 20021004 00007 SO 2002 10 4 C2XA02SH080 1 20021004 A 5310 14522226003 BUTT STRAP EMB 145 EMB145ER 3260211 SO CARGO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 DURING C CHECK INSPECTION, CORROSION AND PITTING WAS FOUND AROUND RIVETS ON BUTTSTRAP BETWEEN FRAMES 59 AND 61. MAITENA NCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100400008 20021004 00008 SO 2002 10 4 C2XA02SH081 1 20021004 A 5315 FLOORBEAM EMB 145 EMB145ER 3260211 SO CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 SHV-DURING C CHECK, LT CARGO SILL FLOORBEAM WAS FOUND TO HAVE CORROSION. MAITENANCE REMOVED AND REPLACED AFFECTED SILL FLOORBEAM IAW EMB SRM 57-220-03, SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100400009 20021004 00009 SO 2002 10 4 C2XA02SH082 1 20021004 A 5315 FLOORBEAM EMB 145 EMB145ER 3260211 SO CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 DURING C CHECK INSPECTION, RT FLOORBEAM BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO HAVE CORROSION IN NUTPLATE HOL ES. MAITENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN T O SERVICE. 2 L 7 2 4F RT T00011AT 2002100400010 20021004 00010 SO 2002 10 4 C2XA02SH084 1 20021004 A 5315 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 SHV DURING C CHECK, NUTPLATE HOLES WERE FOUND WITH CORROSION ON LT LATERAL FLOORBEAM BETWEEN FRAMES 15 AND 17. MAITENA NCE REMOVED DAMAGED SECTION AND PERFORMED FLOORBEAM REPAIR IAW EC 5320-01078. THE AIRCRAFT WAS APPROVED TO RETURN TO SE RVICE. 2 L 7 2 4F RT T00011AT 2002100400011 20021004 00011 SO 2002 10 4 C2XA02SH085 1 20021004 A 5315 14521700007 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 SHV DURING C CHECK INSPECTION, THE RT FLOORBEAM AT FRAME 20 WAS FOUND TO HAVE CORROSION AT NUTPLATE HOLES AND UNDER DOU BLER. MAINTENANCE REMOVED DAMAGED SECTION AND PERFORMED A FLOORBEAM REPAIR IAW EC 5320-01077. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100400012 20021004 00012 SO 2002 10 4 C2XA02SH086 1 20021004 A 5310 14521725001 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 DURING C CHECK CORROSION WAS FOUND ON NUTPLATE HOLES ON LT SILL BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED AND REPLA CED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100400013 20021004 00013 SO 2002 10 4 C2XA02SH087 1 20021004 A 5410 14576599004 ANGLE EMB 145 EMB145ER 3260211 SO NR 1 NACELLE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 SHV DURING C CHECK INSPECTION SUPPORT ANGLE WAS FOUND GOUGED ON NR 1 ENGINE LOWER COWLING JUST AFT OF MOST FOWARD PIVOT POINT. MAINTENACE REMOVED DAMAGED AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVE D TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100400014 20021004 00014 NM 2002 10 4 CALA0200483 1 20021003 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND A .040" CRACK AT EDGE OF LIGHTENING HOLE IN C-1 DOOR INTERIOR SKIN. SECOND ROW AFT OF LEADING EDGE, CEN TER OF DOOR INTERIOR. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01018. 2 L 7 2 4F RT A16WE 2002100400015 20021004 00015 NM 2002 10 4 CALA0200484 1 20021003 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND A 0.050" CRACK AT EDGE OF LIGHTENING HOLE IN C-2 DOOR INTERIOR SKIN. SECOND ROW FROM LEADING EDGE CENTE R OF DOOR. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01019. 2 L 7 2 4F RT A16WE 2002100400016 20021004 00016 NM 2002 10 4 USAA020337 1 20020831 A 5320 SUPPORT BRACKET BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 22192 CLT - FOUND ANGLE SUPPORT CRACKED .5 INCH, STATION 930 LBL 66 AT MLG MAIN DOOR STOP FITTING. INSTALLED NEW SUPPORT BRAC KETS PER SRM 51-10-02 AND EA 86573. (M) 2 L 7 2 4F RT A2NM 2002100400017 20021004 00017 NM 2002 10 4 USAA020338 1 20020827 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 411US 40562 23880 CLT - FOUND SKIN CRACKED 3 INCHES, STATION BS 727D STRINGER 23R. INSTALLED DOUBLER PER TR 53-60-03. (M) 2 L 7 2 4F RT A16WE 2002100400018 20021004 00018 NM 2002 10 4 USAA020339 1 20020724 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 46790 23702 CLT - FOUND SKIN CRACKED .4375 INCH STATION 380 STRINGER 00 BOTTOM FUSELAGE CENTER LINE. INSTALLED DOUBLER PER TR 53-30 -07. (M) 2 L 7 2 4F RT A16WE 2002100400019 20021004 00019 NM 2002 10 4 USAA020341 1 20020810 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 55514 22203 CLT - FOUND STRINGER CORRODED 20 INCHES, STATION 660-680 S-28L, STRINGER TO KEEL BEAM SPLICE. BLEND OUT, SHOT PEEN, FAB RICATED FILLER AND REPAIR CHANNEL PER EA 86510. (M) 2 L 7 2 4F RT A2NM 2002101000132 20021010 00132 NM 2002 10 10 F3LA200200283 1 20021002 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT BS 947-BS 967, RBL 41. REMOVED INTERCOSTAL PER SRM 51 -40-02. FABRICATED AND INSTALLED INTERCOSTAL PER SRM 51-60-02, MM 51-21-99 AND EA 53-737-181. 2 L 7 2 4F RT A16WE 2002100400020 20021004 00020 NM 2002 10 4 USAA020342 1 20020813 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 55514 22203 CLT - FOUND SKIN CRACKED 6 INCHES BY 10 INCHES, BS 555-565 STRINGER 28-29. DOUBLER INSTALLED. (M) 2 L 7 2 4F RT A2NM 2002100400021 20021004 00021 NM 2002 10 4 USAA020343 1 20020723 A 7830 SUPPORT BOEING 757 7572B7 1384964 NM THRUST REVERSER BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 621AU 30860 27200 CLT - FOUND APPROX 8 INCH SECTION BROKEN/MISSING, NR 1 ENGINE T/R 11 O'CLOCK POSITION. REMOVED AND REPLACED T/R REAR CA SCADE SUPPORT RING PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2002100400022 20021004 00022 NM 2002 10 4 USAA020348 1 20020813 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 46845 23232 PIT - FOUND STRINGER CRACKED .25 INCH, STATION 907 BETWEEN STRINGER 59L AND 58L. INSTALLED DOUBLER PER TR 53-10-14A. ( M) 2 L 7 2 4F RT A16WE 2002100400023 20021004 00023 NM 2002 10 4 USAA020349 1 20020903 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 46845 23232 PIT - FOUND INTERCOSTAL CRACKED 1 INCH, STATION 303, S4L. MANUFACTURED NEW WEB PER 53-00-03. (M) 2 L 7 2 4F RT A16WE 2002100400024 20021004 00024 NM 2002 10 4 USAA020350 1 20020903 A 5312 PRESSURE PANEL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 46845 23232 PIT - FOUND WEB CRACKED 1 INCH, STATION 672 RBL 42 W/W PRESS PANEL. DOUBLERS, STIFFENER, HEAT TREATED PER SRM 53-60-51 AND EA 74665. (M) 2 L 7 2 4F RT A16WE 2002100400025 20021004 00025 NM 2002 10 4 USAA020351 1 20020829 A 5512 SKIN BOEING 737 737301 1384611 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 46845 23232 PIT - FOUND BOTTOM SKIN WITH 2 INCH LONG CRACK, LT LOWER STAB SKIN, REAR SPAR ELEV STATION 66.54 AND 94.07. REPAIR FILL ER, DOUBLER PER TYPICAL REPAIR 55-10-07 REV B. (M) 2 L 7 2 4F RT A16WE 2002100400026 20021004 00026 NM 2002 10 4 USAA020352 1 20020820 A 5320 CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 46845 23232 PIT - FOUND SKIN CLIP CRACKED .5 INCH, AT STATION 616 AND S5R. REMOVED AND REPLACED SKIN CLIP PER 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002100400027 20021004 00027 NM 2002 10 4 USAA020354 1 20020910 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 43237 24411 PIT - FOUND BEAM CORRODED 6.5 INCHES BY .5 INCH AREA, NUT PLATE HOLES ON TOP FLANGE OF FLOORBEAM STATION 98. REMOVED CO RRODED SECTION OF FLOORBEAM AND SPLICED IN NEW PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 2002100400028 20021004 00028 NM 2002 10 4 USAA020355 1 20020910 A 5320 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 43237 24411 PIT - FOUND 40 INCH BY 1 INCH AREA OF CORROSION, ZEE ANGLE AT AFT SERVICE DOOR THRESHOLD. REMOVED CORROSION, TREATED AN D PRIMED PER SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 2002100400029 20021004 00029 NM 2002 10 4 USAA020356 1 20020810 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 43446 24412 PIT - FOUND FRAME CRACKED .25 INCH, STATION 867 AT S8L-S9L. INSTALLED DOUBLER PER TYPICAL REP 53-10-14A. (M) 2 L 7 2 4F RT A16WE 2002100400030 20021004 00030 NM 2002 10 4 USAA020357 1 20020822 A 5320 STIFFENER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 47058 23317 TPA - FOUND CHANNEL STIFFENER CORRODED 6 INCHES, STATION 0 BULKHEAD 1016. CUT AND REMOVED DAMAGED PART, SPLICED IN NEW CHANNEL STIFFENER PER SB 737-53A1075 AND EA 94341. (M) 2 L 7 2 4F RT A16WE 2002100400031 20021004 00031 NM 2002 10 4 USAA020358 1 20020831 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 46532 23235 CLT - FOUND SKIN CRACKED 1 INCH, S22L AT STATION 727D PLUS 13. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 2002100400032 20021004 00032 NM 2002 10 4 USAA020359 1 20020904 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 46532 23235 CLT - FOUND SKIN CRACKED 2.1 INCH, S23R AT STATION 727D PLUS 4. INSTALLED DOUBLER AND TRIPLER PER EA 74734. (M) 2 L 7 2 4F RT A16WE 2002100400033 20021004 00033 NM 2002 10 4 USAABB02132 1 20020815 A 3350 LIGHT BOEING 767 767201 1385125 NM EVAC SLIDE INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 648US 38609 23900 CLT - DURING THE ANNUAL SLIDE OPERATIONAL DEPLOYMENT CHECK FOR THE R3 DOOR, THE SLIDE MOUNTED EMERGENCY LIGHTS DID NOT I LLUMINATE. MAINTENANCE REPLACED THE SLIDE. THE SLIDE WILL BE ROUTED TO THE SHOP. PER US AIRWAYS POLICIES AND PROCEDUR E, TWO MORE SLIDES OF THIS POSITION WILL BE DEPLOYED. (M) 2 L 7 2 4F RT A1NM 2002100400034 20021004 00034 NM 2002 10 4 USAABB02133 1 20020820 A 2612 0205K0S600 SWITCH BOEING 757 757225 1384959 NM RT ENGINE MALFUNCTIONED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 607AU 22203 PHL - FL 1268, ON INITIAL CLIMB, CREW INTERMITTENTLY RECEIVED THE EICAS MESSAGE RIGHT ENGINE FIRE AND ASSOCIATED WARNING LIGHTS. THE FIRE TEST WAS ACCOMPLISHED AND WAS SATISFACTORY IN ALL MODES. THE WARNINGS DID NOT REOCCUR IN FLIGHT OR O N DESCENT. MAINTENANCE REPLACED BOTH OVERHEAT DETECTOR SWITCHES ON THE RIGHT ENGINE. (M) 2 L 7 2 4F RT A2NM 2002100400035 20021004 00035 NM 2002 10 4 USAABB02134 1 20020822 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 605AU 22201 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 23, 29 AND 33. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002100400036 20021004 00036 NM 2002 10 4 USAABB02135 1 20020819 A 3260 851801 SENSOR BOEING 767 767201 1385125 NM LT MLG MALFUNCTIONED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 648US 23900 PHL - FLT 894 - AFTER TAKEOFF, UPON GEAR RETRACTION, WHEN THE GEAR LEVER WAS SELECTED TO THE 'OFF' POSITION, THE LEFT MA IN LANDING GEAR EXTENDED. THE CREW POSITIONED THE GEAR LEVER TO 'UP' AND THE GEAR RETRACTED. THE LEVER WAS LEFT IN THE 'UP' POSITION, AND THE CREW HAD THE AMBER GEAR DISAGREE LIGHT. MAINTENANCE REPLACED THE LATCH SENSORS S260 AND S238. ON THE SUBSEQUENT FLIGHT, CREW RECEIVED THE GEAR DOOR LIGHT AND EICAS MESSAGE. MAINTENANCE FOUND AND SECURED A LOOSE SE NSOR S242. (M) 2 L 7 2 4F RT A1NM 2002100400037 20021004 00037 NM 2002 10 4 USAABB02136 1 20020819 A 3260 851801 SENSOR BOEING 767 767201 1385125 NM MLG LOOSE A USAA J DUMP FUEL N FALSE WARNING CL CLIMB 1 EA 19 648US 23900 PHL - FLT 894 - AFTER TAKEOFF, UPON GEAR RETRACTION, WHEN THE GEAR LEVER WAS SELECTED TO THE 'OFF' POSITION, THE LEFT ML G EXTENDED. THE CREW POSITIONED THE GEAR LEVER TO 'UP' AND THE GEAR RETRACTED. THE LEVER WAS LEFT IN THE 'UP' POSITION , AND THE CREW HAD THE AMBER GEAR DISAGREE LIGHT. MAINTENANCE REPLACED THE LATCH SENSORS S260 AND S238. ON THE SUBSEQU ENT FLIGHT, CREW RECEIVED THE GEAR DOOR LIGHT AND EICAS MESSAGE. MAINTENANCE FOUND AND SECURED A LOOSE SENSOR S242. (M ) 2 L 7 2 4F RT A1NM 2002100400038 20021004 00038 NM 2002 10 4 USAABB02138 1 20020823 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 BDL - EMERGENCY AISLE LIGHT AT SEAT 29 IS DIM. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002100400039 20021004 00039 NM 2002 10 4 USAABB02141 1 20020828 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AU 27199 LAX - FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002100400040 20021004 00040 NM 2002 10 4 USAABB02148 1 20020905 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 610AU 27122 LAX - FOUND ALL FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED ALL THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002100400041 20021004 00041 NM 2002 10 4 USAABB02149 1 20020905 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 29 INOPERATIVE AND AT ROW 23 DIM. MAINTENANCE REPLACED THE BATTERIES. ( M) 2 L 7 2 4F RT A2NM 2002100400042 20021004 00042 EU 2002 10 4 USAASA02074 1 20020821 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 105UW 0868 BOS - AFT EPSU FAILED EMERGENCY LIGHT TEST. MAINTENANCE REPLACED THE EPSU. (M) 2 L 7 2 4F RT A28NM 2002100400043 20021004 00043 NM 2002 10 4 2002UALA01365 1 20020828 A 5320 CLIP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 944UA 26683 FUSELAGE NOSE COMP CREASE BEAM CLIP IS BENT. BODY STATION 178 AFT, LBL 25-28, WL 207. MAJOR REPAIR ACCOMPLISHED. CLIP REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100400044 20021004 00044 NM 2002 10 4 2002UALA01366 1 20020828 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 FUSELAGE FRAME CRACKED AT STATION 807 JUST ABOVE STRINGER 9R AT INBOARD FASTENER FOR PASSENGER SERVICE UNIT RAIL SUPPOR T. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002100400045 20021004 00045 WP 2002 10 4 GTIA020967 1 20020823 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 MID PIT LOWER DOOR JAMB CUTOUT HAS CORROSION AT DOUBLER AT STA 522 TO STA 579. REMOVED DOUBLER AND CORRODED STRAP. FAB RICATED STRAP. INSTALLED REMOVED DOUBLER AND NEW STRAP. 2 L 7 2 4F 4 F A6WE E2EA 2002100400046 20021004 00046 NM 2002 10 4 F3LA200200284 1 20021002 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM BS 947-967 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT BS 947 - BS 967, LBL 8. REMOVED DAMAGED INTERCOSTAL P ER SRM 51-40-02. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-40-02, SRM 53-60-51 AND EA 53-737-181. 2 L 7 2 4F RT A16WE 2002100400047 20021004 00047 WP 2002 10 4 GTIA020968 1 20020901 A 5313 LONGERON DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE FUSELAGE CORRODED B GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 CORROSION HEAVY PITTING IN MID CARGO PIT F 674 AND 693 LONG 29L. REMOVED LONG 29L FROM 664.5 TO 740.5 FABRICATED LONGER ON 29L AND 2 EACH LONGERON SPLICES , INSTALLED LONGERON AND SPLICES. 2 L 7 2 4F 4 F A6WE E2EA 2002100400048 20021004 00048 WP 2002 10 4 GTIA020969 1 20020904 A 5313 LONGERON DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE FUSELAGE CORRODED B GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 MID B/B LONGERON 29L CORRODED AT STA 636, 648 AND 654. REMOVED L29L AT STA 589 TO 664.5 AND SPLICES. FABRICATED LONGER ON IAW EA. INSTALLED SPLICES AT STA 589 TO 664.5. 2 L 7 2 4F 4 F A6WE E2EA 2002101000051 20021010 00051 NM 2002 10 10 F3LA200200289 1 20021002 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION STA 947-967 LBL 30-45 ON INTERCOSTAL. FABRICATED AND INSTALLED REPLACEM ENT INTERCOSTAL PER SRM 53-60-51, 51-40-02, EA 53-737-181 AND MM 51-21-99. 2 L 7 2 4F RT A16WE 2002100400049 20021004 00049 WP 2002 10 4 GTIA020970 1 20020822 A 5210 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE L1 DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 L1 DOOR SKIN AREA AROUND HOOK CUTOUT CRACKED. REMOVED CRACK AT HOOK CUTOUT AT L1 DOOR. FABRICATED REPAIR, DOUBLER, INS TALLED REPAIRED DOUBLER. 2 L 7 2 4F 4 F A6WE E2EA 2002100400050 20021004 00050 WP 2002 10 4 GTIA020971 1 20020821 A 5754 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE L/E SLAT DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 38737 49141 FROM CARRY OVER LIST, 3 DENTS ON NR 2 SLAT R WING, 1ST DENT XOS 204 DEPTH .016, 2ND DENT XOS 235 DEPTH .039, 3RD DENT XO S 264 DEPTH .019. ALL THREE DENTS ARE OUT OF LIMITS, REPAIRED DENTS. 2 L 7 2 4F 4 F A6WE E2EA 2002100400051 20021004 00051 WP 2002 10 4 GTIA020972 1 20020909 A 5754 HORN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE L/E SLAT DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 38737 49141 RIGHT SLAT 0 HAS 2 DENTS IN LEADING EDGE. NR 1 15 INCH FROM INBOARD END. NR 2, 18 INCH FROM INBOARD END. SKIN HAS SCR ATCHES BETWEEN THE 2 DENTS. REMOVED RIGHT WING SLAT HORN. INSTALLED RIGHT WING SLAT HORN NUMBER ZERO SLAT. 2 L 7 2 4F 4 F A6WE E2EA 2002101000055 20021010 00055 NM 2002 10 10 F3LA200200290 1 20021002 A 5320 CHANNEL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO BIN LT FLOOR SUPPORT ZEE CHANNEL. FOUND TO BE OUT OF LIMIT S PER SRM 53-60-53. FABRICATED PARTS PER SRM 53-60-53 & SOPM 20-41-02. INSTALLED PART PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002100400052 20021004 00052 NM 2002 10 4 DHL2002747006 1 20021002 A 2910 596005003 SOLENOID VALVE BOEING 727 727224 1384076 NM A DHLA O OTHER K FLUID LOSS NR NOT REPORTED 1 SO 01 747DH 22253 1) IN FLIGHT, HYDRAULIC SYSTEM "A" DECREASED TO 0.2. ENGINE #1 LOW PRESSURE LIGHT ILLUMINATED INTERMITTENTLY. PERFORMED ABNORMAL PROCEDURES. "A" HYDRAULIC SYSTEM FLUID SHUTOFF SWITCHED CLOSED FOR 7 MINUTES. (NOTE: DHL INSPECTION AND SURVEI LLANCE REPORT DATED 10-02-2002 STATES THAT AN EMERGENCY WAS DECLARED.)2) FOUND LOWER RUDDER SOLENOID VALVE LEAKING, REP LACED SOLENOID VALVE & GASKET - NO FURTHER LEAKS NOTED. RUDDER PCU OPS CHECKED GOOD IAW DHL M/M 27-20-141. SERVICED "A" SYSTEM HYDRAULICS & RAN ENGINES - NO HYDRAULIC LEAKS NOTED. RESET "A" SYSTEM SWITCHES TO OPEN, SYSTEM OPS CHECKED NORMAL IAW DHL M/M 29-11-0.3) MANUAL LANDING GEAR EXTENSION PERFORMED.4) TESTED GEAR MANUAL EXTENSION SYSTEM PER 2 L 7 3 4F A3WE 2002101000056 20021010 00056 NM 2002 10 10 F3LA200200291 1 20021002 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION STA 947-967 LBL 17 INTERCOSTAL. FABRICATED NEW INTERCOSTAL PART SRM 53- 60-51 & MM 51-21-99. INSTALLED PART PER SRM 51-40-02 & EA 53-737-181. 2 L 7 2 4F RT A16WE 2002101000057 20021010 00057 NM 2002 10 10 F3LA200200292 1 20021002 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED ON CORROSION ON FLOOR INTERCOSTAL AT STA 986.5 - 1006, RBL 37. FABRICATED AND INS TALLED REPLACEMENT INTERCOSTAL PER SRM 51-40-02 AND 53-60-51. 2 L 7 2 4F RT A16WE 2002101000058 20021010 00058 NM 2002 10 10 F3LA200200293 1 20021002 A 5345 ATTACH ANGLE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CLOSET ATTACH ANGLES AT BS 1015. FABRICATED AND INSTALLED REPLACEMEN T ANGLES PER BOEING DRAWING 65-48812 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002100400053 20021004 00053 WP 2002 10 4 GTIA020973 1 20020911 A 3397 WIRE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE A/C BAY DISCONNECTED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 817NK 38737 49141 TAIL EMERGENCY AND EVACUATION LIGHTS, INOPERATIVE. FOUND WIRING NOT CONNECTED, RECONNECTED AND SECURED WIRING. 2 L 7 2 4F 4 F A6WE E2EA 2002100400054 20021004 00054 WP 2002 10 4 GTIA020974 1 20020916 A 1430 DOME NUT DOUG DC9 DC941 302207N WP PWA JT12 JT12* 52042 NE RT WING BROKEN A GTIA O OTHER K FLUID LOSS CR CRUISE 1 GL 23 131NK 47605 RIGHT TANK FUEL QUANTITY WENT DOWN FASTER THAN LEFT WHILE IN FLIGHT. LANDED WITH 5600 IN LEFT AND 4300 IN RIGHT. CONFI RMED QUANTITY WITH DRIP STICKS. FOUND MISSING BOLT ON FORWARD PANEL ON RIGHT WING. FOUND 2 DOME NUTS FOR RIGHT WING FQ PROBE NR 2 ACCESS PLATE OFF AND ONE SCREW MISSING. REPLACED TWO BROKEN DOME NUTS AND INSTALLED ACCESS PLATE WITH NEW S EAL. 2 L 7 2 4F 4 J A6WE 1E9 2002100400055 20021004 00055 WP 2002 10 4 GTIA020975 1 20020918 A 3350 LIGHT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE CABIN INOPERATIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 38745 49141 L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT 1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY. 2 L 7 2 4F 4 F A6WE E2EA 2002100400056 20021004 00056 WP 2002 10 4 GTIA020976 1 20020909 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 36447 49415 FLOOR BOARDS VERY SPONGY AT FORWARD ENTRY AREA STA 160-200, BL 0-LBL 46. FLOORBOARDS TO BE REMOVED AND REINSTALLED ON, FABBED FLOOR BOARDS. 2 L 7 2 4F 4 F RT A6WE E2EA 2002100400057 20021004 00057 WP 2002 10 4 GTIA020977 1 20020911 A 5755 4925T21502 SUPPORT FITTING DOUG DC9 DC983 3022083 WP SPOILER CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 36447 49415 RIGHT INBOARD FLIGHT SPOILER CENTER LOWER TORQUE TUBE SUPPORT FITTING IS CRACKED DOT KF036. REMOVED FITTING, DRILLED AN D LOCATED NEW FITTING, INSTALLED FITTING. 2 L 7 2 4F RT A6WE 2002100400058 20021004 00058 EU 2002 10 4 2002F00914 1 20020824 A 2720 S2728126000200 CONTROL CABLE AEROSP ATR72 ATR72212 8680945 EU RUDDER DAMAGED A TRBA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SO 21 451AT 19622 451 DURING ACCOMPLISHMENT OF A FLEET CAMPAIGN DIRECTIVE FCD, IT WAS FOUND THAT THE CAPTAINS RUDDER CABLE LOCATED AT FK 12 CO MING APART. REMOVED AND REPLACED RUDDER CABLE UNDER THE CAPTAIN SEAT AS PER MM 27-21-00. DURING ACCOMPLISHMENT OF A FC D, FOUND PRESENCE OF FOD EMBEDDED IN THE CAPTAIN RUDDER CABLE PULLEY LOCATED AT THE FRONT CABIN AREA. (M) 2 H 7 2 4T RT A53EU 2002100400059 20021004 00059 NM 2002 10 4 PCAA0210116 1 20021003 A 2910 82970010391 LINE DHAV DHC8 DHC8102 2809003 NM LEAKING A PCAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 13 804EX 227 ROC-DCA FLIGHT#3793. CREW REPORTED WHILE AT 17,000 FEET #2 HYDRAULIC ISOLATION VALVE LIGHT ILLUMINATED WITH .5 QUARTS IN DICATED ON #2 SYSTEM. FLIGHT DIVERTED TO MDT, EMERGENCY DECLARED, AIRCRAFT LANDED WITH OUT INCIDENT. MAINTENANCE FOUND H YDRAULIC LINE TO GEAR DOOR SEQUENCING VALVE IN LEFT WHEEL WELL LEAKING. HYDRAULIC LINE WAS REPLACED. LEAK AND OPERATIONA L CHECK OF LANDING GEAR GOOD. HYDRAULIC FLUID SERVICED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002100400060 20021004 00060 NM 2002 10 4 PCAA0210117 1 20021002 A 7931 PW120A ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT LEAKING A PCAA E ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 EA 13 811AW 28889 21474 201 120827 ALB-LGA FLIGHT#3543. CREW REPORTED THAT DURING CLIMB, LEFT OIL PRESSURE WARNING LIGHT ILLUMINATED. ENGINE WAS SHUT DOWN, EMERGENCY DECLARED. FLIGHT RETURNED TO ALB AND LANDED WITH OUT INCIDENT. MAINTENANCE REPLACED #1 ENGINE AND OIL COOLER IN ACCORDANCE WITH ALLEGHENY AIRLINES JOBCARD 008-7101-349. OPERATIONAL AND LEAK CHECK OF ENGINE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002100400061 20021004 00061 NM 2002 10 4 PCAA0210118 1 20021002 A 5542 85540001003 RUDDER DHAV DHC8 DHC8102 2809003 NM TAIL CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 847EX 27208 8016 333 DURING ROUTINE MAINTENANCE VISIT WHILE PERFORMING BONDING INTEGRITY INSPECTION TASK 550001 LEFT FORE RUDDER FOUND CRACKE D AT RIB #26. DAMAGED AREA WAS CUT OUT AND REPAIRED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-55-335. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002100400062 20021004 00062 EU 2002 10 4 2002F00915 1 20020821 A 2720 2728160 CONTROL CABLE AEROSP ATR72 ATR72212 8680945 EU RUDDER BROKEN A TRBA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 21 355AT 19622 355 RIGHT RUDDER PEDAL LOOSE CONTROL AFTER HEAVY STROKE, BELOW FUSELAGE. FOUND INBOARD RUDDER CABLE BROKEN LOCATED BETWEEN CAPTAIN SIDE QUADRANT AND THE FORWARD CARGO COMPARTMENT (LEFT SIDE). CABLE REMOVED AND REPLACED AS PER MM 27-21-00. IN SPECTION REVEALED PRESENCE OF METAL DEBRIS IN THE CABLE PULLEY AT FRONT CABIN AREA. (M) 2 H 7 2 4T RT A53EU 2002100400063 20021004 00063 SO 2002 10 4 ASOA02443 1 20020803 A 5313 12005744002 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 267AS 120198 DURING C-CHECK INSPECTION IN BNA, STRINGER 18 RIGHT WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 16 AND 17. MA INTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER IAW SRM'S 51-40-02 AND 51-40-00. (M) 2 L 7 2 4T RT A31SO 2002100400064 20021004 00064 SO 2002 10 4 ASOA02444 1 20020803 A 5320 1202789001 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 267AS 120198 DURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS FOUND TO BE CORRODED OUT OF LIMITS FROM FRAME 13 TO FRAME 14. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002100400065 20021004 00065 SO 2002 10 4 ASOA02445 1 20020803 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 267AS 120198 DURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED OUT OF LIMITS AT FRAMES 13 TO 16 AND FROM FRA ME 16-21. MAINTENANCE REMOVED AND REPLACED THE TWO CORRODED SECTIONS SOFT BUTT STRAP IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002100400066 20021004 00066 SO 2002 10 4 ASOA02446 1 20020803 A 5320 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 267AS 120198 DURING C-CHECK INSPECTION IN BNA, THE LEFT INBOARD AND OUTBOARD CROSSBEAMS AT FRAME 16 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS BEAMS IAW SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 2002100400067 20021004 00067 SO 2002 10 4 ASOA02447 1 20020811 A 3350 1317 LIGHT EMB 120 EMB120 3260201 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 868AS 7474 DURING GROUND INSPECTION IN DFW, A CABIN CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE BURNED OUT CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002100400068 20021004 00068 EU 2002 10 4 SIMA200219112 1 20020705 A 5512 SKIN SAAB SF340 340B 7860101 EU HORIZ STAB DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 ABI - RIGHT HORIZONTAL LOWER SKIN HAS ONE DENT. PERFORMED SONIC BOND AND EDDY CURRENT INSPECTION, NO DEFECTS. DENT WIT HIN SAAB SRM 55-10-10 AND 51-10-10 LIMITS. (M) 2 L 7 2 4T RT A52EU 2002100400069 20021004 00069 EU 2002 10 4 SIMA200219113 1 20020705 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 353SB 340B353 ABI - FOUND LEFT FUSELAGE BELOW ICE SHIELD HS TWO DENTS. PERFORMED EDDY CURRENT, NO DEFECTS. (M) 2 L 7 2 4T RT A52EU 2002100400070 20021004 00070 EU 2002 10 4 SIMA200219114 1 20020705 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 ABI - FOUND LEFT FUSELAGE AFT OF ICE SHIELD BELOW WINDOW HAS SIX DENTS. PERFORMED EDDY CURRENT INSPECTION NO DEFECTS. (M) 2 L 7 2 4T RT A52EU 2002100400071 20021004 00071 EA 2002 10 4 COMA0260558 1 20021002 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 781CA 7312 FLIGHT 5962 - FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002100400072 20021004 00072 EU 2002 10 4 SIMA200219116 1 20020705 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 ABI - FOUND LEFT FUSELAGE HAS A DENT APPROX 14 INCHES BELOW THE STATIC PORT. PERFORMED EDDY CURRENT INSPECTION, NO DEFE CTS. (M) 2 L 7 2 4T RT A52EU 2002100400073 20021004 00073 EU 2002 10 4 SIMA200219117 1 20020705 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 17454 340B352 ABI - TAIL SECTION AFT LOWER SKIN HAS A PROTRUSION FORWARD OF PANEL 318AL. PERFORMED EDDY CURRENT INSPECTION, NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A52EU 2002100400074 20021004 00074 EU 2002 10 4 SIMA200219118 1 20020705 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 TAIL SECTION RIGHT BELOW ELEVATOR HAS A DENT AT FUSELAGE. PERFORMED EDDY CURRENT INSPECTION, NO DEFECTS NOTED. DENT FO UND WITHIN SAAB 340 SRM 53-90-10 AND 51-10-10 LIMITS. (M) 2 L 7 2 4T RT A52EU 2002100400075 20021004 00075 EU 2002 10 4 SIMA200219120 1 20020705 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 ABI - RIGHT FUSELAGE AFT OF ICE SHIELD HAS 23 DENTS. PERFORMED EDDY CURRENT INSPECTION, NO DEFECTS. DENTS ACCEPTED AS IS IAW SAAB 340 STATEMENT 340SDS004141 PARA 5. (M) 2 L 7 2 4T RT A52EU 2002100400076 20021004 00076 EU 2002 10 4 SIMA200219121 1 20020705 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 RIGHT FUSELAGE HAS A DENT ABOVE AND FORWARD OF PITOT TUBE. PERFORMED EDDY CURRENT INSPECTION. NO DEFECTS NOTED. DENT FOUND TO BE WITHIN SAAB 340 SRM 51-10-10 LIMITS. (M) 2 L 7 2 4T RT A52EU 2002100400077 20021004 00077 EU 2002 10 4 SIMA200219123 1 20020705 A 5512 SKIN SAAB SF340 340B 7860101 EU HORIZ STAB DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 ABI - LEFT HORIZONTAL TOP SKIN HAS 57 DENTS. PERFORMED EDDY CURRENT AND BOND CHECK, NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A52EU 2002100400078 20021004 00078 EU 2002 10 4 SIMA200219124 1 20020705 A 5512 SKIN SAAB SF340 340B 7860101 EU HORIZ STAB DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 RIGHT HORIZONTAL TOP SKIN HAS 45 DENTS. PERFORMED EDDY CURRENT AND BOND CHECK, NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A52EU 2002100400079 20021004 00079 EU 2002 10 4 SIMA200219125 1 20020705 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 ABI - FOUND FUSELAGE TOP SKIN HAS 150 DENTS. PERFORMED EDDY CURRENT INSPECTION, NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A52EU 2002100400080 20021004 00080 EU 2002 10 4 SIMA200219126 1 20020705 A 5532 SKIN SAAB SF340 340B 7860101 EU VERTICAL STAB DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 VERTICAL STABILIZER RIGHT UPPER AREA HAS ONE DENT. PERFORMED EDDY CURRENT AND SONIC BOND CHECK. NO DEFECTS NOTED. DEN T FOUND TO BE WITHIN SAAB 340 SRM 55-70-10 AND 51-10-10 LIMITS. (M) 2 L 7 2 4T RT A52EU 2002100400081 20021004 00081 EU 2002 10 4 SIMA200219127 1 20020705 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 LEFT FUSELAGE AFT HAS 2 PROTRUSION. PERFORMED EDDY CURRENT INSPECTION. NO DEFECTS NOTED. PROTRUSIONS FOUND TO BE WITH IN SAAB 340 SRM 53-80-30 AND 51-10-10 LIMITS. (M) 2 L 7 2 4T RT A52EU 2002100400084 20021004 00084 NM 2002 10 4 UPS02239605 1 20020918 A 5310 STRINGER BOEING 727 72722C 138400F NM BS 400 STR.15R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI STR.15R FOUND CRACKED AT BS400 STRINGER REPAIRED IAW SRM 53-10-3 FIG.1 DETAIL 2 2 L 7 3 4F A3WE 2002100400085 20021004 00085 NM 2002 10 4 UPS02239607 1 20020922 A 5710 RIB BOEING 727 72722C 138400F NM BS519 LWR STR. CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI SUSPECT CRACK AT RIB BS 519 AT LWR. STR. ATTACH POINT AFT OF ACCESS PNL. STOP DRILLED CRACK IAW 51-10-1. PAGE 12. 2 L 7 3 4F A3WE 2002100400086 20021004 00086 NM 2002 10 4 UPS02239608 1 20020917 A 5310 INTERCOSTAL BOEING 727 72722C 138400F NM BS1183LBL26WL280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI CRACK ON VERT. BEAM INTERCOSTAL AT BS 1183 LBL26 AT WL 280. FABRICATED NEW INTERCOSTAL IAW SRM 53-10-2 FIG 5. INTERCOSTAL INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2002100400088 20021004 00088 EA 2002 10 4 COMA0260559 1 20021003 A 2760 4916405 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA #2 MALFUNCTIONED A COMA O H OTHER DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED DE DESCENT 1 SO 01 785CA 8949 7326 FLIGHT 5708 WHEN FLIGHT SPOILERS DEPLOYED, AIRCRAFT ROLLED TO LEFT.REPLACED THE #2 SECU. 2 L 7 2 4F RT A21EA 2002100400089 20021004 00089 EA 2002 10 4 COMA0260560 1 20021003 A 4910 APU CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 01 999CA 7230 FLIGHT 9489 APU OIL TEMP CAUTION MESSAGE.COULD NOT DUPLICATE. FOUND NO FAULTS WITH APU 2 L 7 2 4F RT A21EA 2002100400090 20021004 00090 EA 2002 10 4 COMA0260561 1 20021003 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA L/H FAILED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 781CA 798 7312 FLIGHT 5237 FLAPS FIALED AT 41 DEGREES.REPLACED THE L/H BPSU. 2 L 7 2 4F RT A21EA 2002100400091 20021004 00091 EA 2002 10 4 COMA0260562 1 20021003 A 2410 755469C IDG CNDAIR CL600 CL6002B19 1900309 EA R/H FAILED A COMA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 01 999CA 18429 7230 FLIGHT 5860 IDG #2 CAUTION MESSAGE DURING T/O.REPLACED THE R/H IDG. 2 L 7 2 4F RT A21EA 2002100400092 20021004 00092 NM 2002 10 4 C1HA200288017 1 20021003 A 3350 900835A BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 688CA 22344 L/H exterior emergency overwing light inoperative.Removed and replaced battery pack. 2 L 7 3 4F A3WE 2002101000059 20021010 00059 NM 2002 10 10 F3LA200200294 1 20021002 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT BS 947-967, LBL 45. REMOVED INTERCOSTAL PER SRM 51-40 -02. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-60-51, 51-40-02, MM 51-21-99 AND EA 53-737-181. 2 L 7 2 4F RT A16WE 2002100400093 20021004 00093 NM 2002 10 4 C1HA200684003 1 20020926 A 3350 900835A BATTERY PACK BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 684CA 22491 Emergency overhead light aft of FWD liferafts INOP.Removed and replaced battery pack. 2 L 7 3 4F A3WE 2002100400094 20021004 00094 NM 2002 10 4 C1HA200288016 1 20021003 A 3350 900542 POWER SUPPLY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 688CA 22344 R-2 Door emergency light INOP.Removed and replaced R-2 foor emergency light power supply. 2 L 7 3 4F A3WE 2002121600033 20021216 00033 NM 2002 12 16 C1HA200284004 1 20020926 A 3350 806740401 LIGHT BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE COCKPIT INOPERATIVE A C1HA K NONE L NO TEST UK UNKNOWN 1 GL 15 684CA 22491 COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT. 2 L 7 3 4F 4 F A3WE E2EA 2002100400095 20021004 00095 NM 2002 10 4 C1HA200284003 1 20020926 A 3350 900835A BATTERY PACK BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 684CA 22491 Emergency overhead light aft of FWD liferafts INOP.Removed and replaced battery pack. 2 L 7 3 4F A3WE 2002100400096 20021004 00096 NM 2002 10 4 AWXA200200977 1 20020914 A 5315 143N514038 ANGLE BOEING 757 757225 1384959 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 DURING C-06 CHECK A 1 INCH CRACK WAS FOUND ON UPPER FLOOR BEAM ANGLE IN THE FORWARD CARGO COMPARTMENT, BS 672. MAINTENAN CE REMOVED THE CRACKED ANGLE FROM BS 660 TO BS 680. FABRICATED A NEW ANGLE, AND INSTALLED REPAIR PART IAW B757-200 SRM 5 1-40-02, FIG. 8, PG. 39-40. 2 L 7 2 4F RT A2NM 2002100400097 20021004 00097 EU 2002 10 4 SIMA200224009 1 20020814 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 373AE 340B373 ABI - DURING AN MBV INSPECTION, DAMAGE WAS NOTED ON THE UPPER PORTION OF FRAME 710 OF THE CARGO FLOOR. RECONTOURED THE DAMAGED AREA OF THE WEB AND FLANGE. PERFORMED EDDY CURRENT INSPECTION OF THE AREA AND FOUND NO DEFECTS. FABRICATED A 2 9 INCH REINFORCEMENT STIFFENERS FOR THE DAMAGE PORTION OF THE FLANGE. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS00421 7 AND STANDARD SAAB 340 SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002100400098 20021004 00098 SO 2002 10 4 C2XA02SH088 1 20021004 A 5410 14576599004 ANGLE EMB 145 EMB145ER 3260211 SO NR 1 NACELLE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 SHV DURING C CHECK INSPECTION GOUGE WAS FOUND ON NR 1 ENGINE LOWER COWLING AFT OF ENGINE DRAIN. MAINTENANCE REMOVED DAMA GED SETION AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100600001 20021006 00001 SO 2002 10 6 C2XA02SH090 1 20021006 A 5315 14590082003 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 DURING C CHECK INSPECTION, LT LATERAL FLOORBEAM WAS FOUND TO HAVE CORROSION AT RE-ENFORCEMENT ANGLE BETWEEN FRAMES 19 A ND 21. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 51-30-01, SRM 51-40-02. THE AIRCRAFT WA S APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100600002 20021006 00002 SO 2002 10 6 C2XA02SH089 1 20021006 A 5330 12306513005 SKIN EMB 145 EMB145ER 3260211 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 DURING C CHECK, DENT WAS FOUND ON SKIN DOUBLER JUST BELOW PANEL 113EL. MAITENANCE REMOVED DAMAGE AND PERFORMED A DOUBLE R REPAIR IAW EMB 145 SRM 53-11-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002100600003 20021006 00003 SO 2002 10 6 RAIA00210252 1 20020826 A 4910 4501968D APU EMB 145 EMB145 3260210 SO UNSERVICEABLE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 807HK 12209 6863 145119 5302-PIT- APU WILL NOT START AIRCRAFT ENGINE. MAINTENANCE DEFERRED PER MEL 49-52-02. SUBSEQUENTLY CLEARED MEL BY REMOVIN G AND REPLACING THE APU. 2 L 7 2 4F RT T00011AT 2002100600004 20021006 00004 EU 2002 10 6 RAIA00210254 1 20020913 A 2611 CG7PT2 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU INTERMITTENT A RAIA O OTHER J WARNING INDICATION LD LANDING 1 CE 03 552HK 41057 5477-CMI- TOILET SMOKE WARNING LIGHT ILLUMINATED DURING LADING AND EXTINGUISHED A MINUTE OR SO LATER. MAINTENANCE DEFERR ED PER MEL 26-1. SUBSEQUENTLY CLEARING DMI BY REMOVING AND REPLACING THE TOILET SMOKE DETECTOR 2 L 7 2 4T RT A41NM 2002100600005 20021006 00005 EU 2002 10 6 RAIA00210255 1 20020915 A 3350 1270 LAMP AEROSP ATR42 ATR42300 8680920 EU INOPERATIVE A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 424TE 124 5535-STL- AFT EMERGENCY LIGHT MALFUNCTION. REMOVED AND REPLACED LIGHT BULB. 2 H 7 2 4T RT A53EU 2002100600006 20021006 00006 EU 2002 10 6 RAIA00210256 1 20020915 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU DISCHARGED A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 424TE 562 562 124 MX-PIA- EMERGENCY LIGHTS INOP. REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY. 2 H 7 2 4T RT A53EU 2002100600007 20021006 00007 EU 2002 10 6 RAIA00210257 1 20020916 A 3230 DHE1148 PROXIMITY SWITCH AEROSP ATR72 ATR72202 8680940 EU INOPERATIVE A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 722TE 5867 220 5462-STL- LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED MLG PRIMARY WEIGHT ON WHEEL SWITCH, OPS CK OK. 2 H 7 2 4T RT A53EU 2002100600008 20021006 00008 EU 2002 10 6 RAIA00210259 1 20020917 A 3350 6134031 POWERPACK JETAIR JETSTM JETSTM4101 1500501 EU A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 561HK 41077 5497-STL- FOUR EMERGENCY LIGHTS WILL NOT ILLUMINATE IN CABIN. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUP PLY, OPS CK OK 2 L 7 2 4T RT A41NM 2002100600009 20021006 00009 EU 2002 10 6 RAIA00210260 1 20020917 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU DISCHARGED A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 424TE 5019 929 124 5460-STL- EMERGENCY LIGHTS AT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY, OPS CK OK. 2 H 7 2 4T RT A53EU 2002100600010 20021006 00010 EU 2002 10 6 RAIA00210263 1 20020920 A 3350 LP1670 BULB AEROSP ATR72 ATR72202 8680940 EU BURNED OUT A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 723TE 283 MX - STL - EMERGENCY LIGHT INOP AT SERVICE DOOR. REMOVED AND REPLACED BULB, OPS CK OK. 2 H 7 2 4T RT A53EU 2002100600011 20021006 00011 2002 10 6 RAIA00210265 4 20020921 A 3400 272546 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 564HK 41081 5466-=STL- FOs SYMBOL GENERATOR FAILED. MAINTENANCE REMIVED AND REPLACED SYMBOL GENERATOR SWITCH, OPS CK OK. 2 L 7 2 4T RT A41NM 2002100600012 20021006 00012 SO 2002 10 6 RAIA00210266 1 20020922 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO BURNED OUT A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 812HK 145373 MX-PIT-EMERGENCY LIGHT INOP AT GALLEY. REMOVED AND REPLACED EMERGENCY LIGHT BULB AT GALLEY, OPS CK OK. 2 L 7 2 4T RT T00011AT 2002100600013 20021006 00013 EU 2002 10 6 RAIA00210268 1 20020927 A 3150 327 LIGHT AEROSP ATR42 ATR42300 8680920 EU COCKPIT MALFUNCTIONED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 422TE 106 5548-STL- FLIGHT ATTENDANT AC WILD SHIELD INDICATOR LIGHT CAME ON. MAINTENANCE REMOVED AND REPLACED INDICATOR LIGHT BULB , OPS CK OK. 2 H 7 2 4T RT A53EU 2002100600014 20021006 00014 SO 2002 10 6 RAIA00210269 1 20020929 A 3350 1317 BULB EMB 145 EMB145 3260210 SO BURNED OUT A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 802HK 145066 MX-PIT-EMERGENCY LIGHT IMOP AT GALLEY. REMOVED AND REPLACED LIGHT BULB AT GALLEY EMERGENCY LIGHT, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002100600015 20021006 00015 EU 2002 10 6 RAIA00210270 1 20020929 A 2435 5A895 LEAD JETAIR JETSTM JETSTM4101 1500501 EU DETERIORATED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 572HK 41091 5399-BWI- RIGHT GENERATOR DROPPED OF LINE. MAINTENANCE COULD NOT DUPLICATE MALFUNCTION BUT REMOVED AND REPLACED DETERIOR ATING TERMINAL LEAD, OPS CK OK. 2 L 7 2 4T RT A41NM 2002100600016 20021006 00016 EU 2002 10 6 RAIA00210273 1 20020930 A 2435 51539019E GCU JETAIR JETSTM JETSTM4101 1500501 EU FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 572HK 11960 1194 41091 9545-BWI- RIGHT GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED GCU, OPS CK OK. 2 L 7 2 4T RT A41NM 2002100600017 20021006 00017 EU 2002 10 6 RAIA00210275 1 20021002 A 2930 141910013 LINE JETAIR JETSTM JETSTM4101 1500501 EU CHAFED A RAIA O OTHER J WARNING INDICATION LD LANDING 1 CE 03 560HK 41076 5551-SBN- UPON DECENT INTO STL GOT HYD SYSTEM LOW PRESSURE WARNING. MAINTENANCE REMOVED AND REPLACED HYDRAULIC PUMP LOW PRESSURE LINE, LK AND OPS CK OK. 2 L 7 2 4T RT A41NM 2002100600018 20021006 00018 EU 2002 10 6 RAIA00210276 1 20021003 A 2435 51539019E GCU JETAIR JETSTM JETSTM4101 1500501 EU FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 561HK 10543 4296 41077 5559-SPI- LEFT GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED LEFT GCU, OPS CK OK. 2 L 7 2 4T RT A41NM 2002100600019 20021006 00019 SO 2002 10 6 C2XA02IA215 1 20021005 A 2120 M8353616022L RELAY EMB 135 EMB135LR 3260305 SO RT.RELAY PANEL INTERMITTENT A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 27 17524 145399 IAH- FLIGHT 3959,THE CREW NOTED THAT THE AIRCRAFT HAS A LIGHT TO MODERATE VIBRATION IN CLIMB (290 KIAS) THROUGH CRUISE (320KIAS). FELT IN FLOORBOARD, AND, SEAT IN COCKPIT. NO VIBRATION NOTED ON YOKE. IAH- MAINTENANCE INSPECTED THE FORW ARD INLET AIRFLOW SHUTOFF VALVE,AND, FOUND THE VALVE TO BE INTERMITTENT. REMOVED AND REPLACED RELAY K0039 FOR SHUTOFF V ALVE TEMP CONTROL. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. 2 L 7 2 4F RT T00011AT 2002100700001 20021007 00001 WP 2002 10 7 ABXA020223 1 20020916 A 5300 591140617 LONGERON DOUG DC9 DC931 3022065 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 LONGERON 4 LEFT, CRACKED AT F.S. 200. REPLACED LONGERON IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002100700002 20021007 00002 WP 2002 10 7 ABXA020224 1 20020930 A 5200 99579456 ATTACH ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 FORWARD CARGO DOOR AFT HINGE FORWARD ATTACH ANGLE ON HINGE HAD CORROSION. REPLACED ATTACH ANGLE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002100700003 20021007 00003 NM 2002 10 7 ABXA020226 1 20021004 A 5210 140T26033 CHANNEL BOEING 767 767231 1385131 NM C2 DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 787AX 23020 "T" CHANNEL CORRODED, C2 BAG BIN DOOR, BELOW DOOR VENT CUTOUTS. REPLACED "T" CHANNEL IAW BOEING SRM. 2 L 7 2 4F RT A1NM 2002100700004 20021007 00004 WP 2002 10 7 ABXA020222 1 20020916 A 5400 591326265 ATTACH ANGLE DOUG DC9 DC931 3022065 WP LEFT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 PYLON LOWER ATTACH ANGLE FORWARD END WAS CRACKED. REPAIRED PYLON LOWER ATTACH ANGLE FORWARD END IAW DC-9 SRM 54-04 AND S SRM DWG #K07439. 2 L 7 2 4F A6WE 2002101000061 20021010 00061 NM 2002 10 10 F3LA200200296 1 20021002 A 5320 SILL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON R2 MOP SILL. REPLACED MOP SILL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002101000060 20021010 00060 NM 2002 10 10 F3LA200200295 1 20021002 A 5320 SILL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR MOP SILL. REPLACED MOP SILL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002103100268 20021031 00268 WP 2002 10 31 ABXA020220 1 20021001 A 2131 10256852 CONTROLLER DOUG DC9 DC941 302207N WP CABIN PRESSURE MALFUNCTIONED A ABXA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 954AX 47612 ON CLIMBOUT, AIRCRAFT DID NOT PRESSURIZE. PERFORMED ABNORMAL, AUTO CONTROLLER WAS INOPERATIVE. UNABLE TO CONTROL PRESS URE. INSPECTED ALL ACCESS DOORS, ALL CLOSED. INSPECTED AND LUBRICATED OUTFLOW BUTTERFLY VALVE LINKAGE AND OUTFLOW NOZZ LE, NO DEFECTS FOUND. MANUALLY PRESSURIZED AIRCRAFT, ABLE TO GET UP TO 3.3 DIFF PRESSURE. REPLACED THE AUTO PRESSURIZA TION CONTROLLER IAW DC-9 MM 21-32-00-2-0601. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002100700005 20021007 00005 EU 2002 10 7 2002F00916 1 20020907 A 2720 S2728130200400 CONTROL CABLE AEROSP ATR42 ATR42300 8680920 EU RUDDER BROKEN A TRBA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SO 21 971NA 017 DURING WORK TO CLEAR A MEL, UNDER CEILING PANEL OF GALLEY AREA, FOUND RUDDER CABLE WITH BROKEN STRAND. REMOVED AND REPL ACED RUDDER CABLE ASSEMBLY LOCATED BETWEEN FRAME 38-47 AS PER MM 27-21-00. (M) 2 H 7 2 4T RT A53EU 2002100700006 20021007 00006 NM 2002 10 7 QXEA0201569 1 20020928 A 2750 85750750003 FLAP BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 WORN A QXEA D RETURN TO BLOCK J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 09 409QX 2312 2312 4051 GEG - UPON PUSHBACK, THE FLAP DRIVE CAUTION LIGHT ILLUMINATED WITH THE FLAPS SET TO 5 DEGREES. MAINTENANCE RESET THE FLA P CONTROL UNIT. THE FLAPS OPERATED NORMALLY FORM 5 DEG TO 35 BUT THE FLAP DRIVE CAUTION REMAINED ILLUMINATED. MAINTENANC E INSPECTED THE AIRCRAFT AND REPLACED THE LEFT INBOARD FLAP AND ASSOCIATED HARDWARE. OPERATIONAL CHECKS WERE PERFORMED A ND CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002100700008 20021007 00008 NM 2002 10 7 ASAA0210172 1 20020731 A 3350 07912 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHT AT ROW 19 INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY AT ROW 19, THEN LIGHT NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100700009 20021007 00009 NM 2002 10 7 ASAA0210173 1 20020801 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE O OTHER LD LANDING 1 NM 01 745AS 20794 JNU - EMERGENCY EXIT SIGN ON SMOKE BARRIER ILLUMINATED. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY, THEN SIGN TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100700010 20021007 00010 NM 2002 10 7 ASAA0210174 1 20020802 A 3350 86210144 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHT AT ROW 14 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY PACK, THEN LIGHT TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100700011 20021007 00011 NM 2002 10 7 ASAA0210178 1 20020816 A 3350 86210144 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - SMOKE BARRIER AND OVERWING EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLIES (3) AT BOTH OVERWING EX ITS AND SMOKE BARRIER, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100700012 20021007 00012 NM 2002 10 7 ASAA0240082 1 20020716 A 1420 8100022608 TERMINAL BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 FAI - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROWS 9, 10 AND 11 INOPERATIVE. RECONNECTED WIRE TERMINAL END S. LIGHTS THEN FUNCTIONED PROPERLY. (M) 2 L 7 2 4F RT A16WE 2002100700013 20021007 00013 NM 2002 10 7 ASAA0240088 1 20020806 A 3397 541N5091 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 FAI - FLOOR TRACK LIGHTING INOPERATIVE FROM ROW 22-25. RECONNECTED TRACK LIGHT WIRING, OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100700014 20021007 00014 NM 2002 10 7 ASAA0240090 1 20020813 A 3397 541N5091 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 FAI - FOUND FLOOR TRACK LIGHTING INOPERATIVE FROM ROW 18-20. RECONNECTED TRACK LIGHT WIRING, OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100700015 20021007 00015 NM 2002 10 7 ASAA0270010 1 20020806 A 3350 411A343012B LIGHT BOEING 737 737790 13844CN NM CABIN SHORTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 625AS 30792 ANC - DURING MAINTENANCE CHECK, FOUND THE L2 DOOR OVERHEAD EXIT LIGHT INOPERATIVE. REPLACED SHORTED BULB AND FUSE. EXI T LIGHT THEN FUNCTIONED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2002101000062 20021010 00062 NM 2002 10 10 F3LA200200297 1 20021002 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON STR 26R AT BS 380. REMOVED CORRODED SECTION OF STRINGER PER SRM 51-4 0-02. FABRICATED AND INSTALLED REPAIR PER SRM 53-30-03 AND 53-00-03. 2 L 7 2 4F RT A16WE 2002100700016 20021007 00016 WP 2002 10 7 ASAA0280148 1 20020428 A 5242 5910083 SKIN DOUG DC9 DC983 3022083 WP E/E BAY DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND E/E BAY DOOR EXTERIOR SKIN DENTED AT FORWARD RIGHT CORNER. REPAIRED DOOR SKIN PER SRM 52-05 , FIG 4. (M) 2 L 7 2 4F RT A6WE 2002100700017 20021007 00017 WP 2002 10 7 ASAA0280150 1 20020430 A 5310 2506195 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND SHEAR TIE CORRODED AT FS 769. INSTALLED SPLICE REPAIR PER SRM 53-03 AND 51-60. (M) 2 L 7 2 4F RT A6WE 2002100700018 20021007 00018 WP 2002 10 7 ASAA0280151 1 20020501 A 5320 99155415 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PAE - DURING C-CHECK, FOUND INTERCOSTAL UPPER FLANGE LOWER SURFACE CORRODED IN MID CARGO BAY. REPLACED INTERCOSTAL PER SRM'S 51-10-04, 51-30-02, AND 53-01. (M) 2 L 7 2 4F RT A6WE 2002100700019 20021007 00019 2002 10 7 ASAA0280221 4 20020711 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 BUR - DURING PREFLIGHT CHECK, THE L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2002100700020 20021007 00020 2002 10 7 ASAA0280223 4 20020715 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 PHX - DURING PRE-FLIGHT CHECK, THE AFT SERVICE DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYAR D. (M) 2 L 7 2 4F RT A6WE 2002100700021 20021007 00021 WP 2002 10 7 ASAA0280228 1 20020719 A 5313 527779223250 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 951AS 49111 OAK - DURING C-CHECK, FOUND CORROSION AROUND AND UNDER RIVETS ALONG LONGERON 22R AT FUSELAGE STATION 160-180. CUT OUT D AMAGED SKIN FROM STATION 150 TO 177 BETWEEN L21R AND L23R. SPLICED IN NEW L22R SECTION FROM STATION 110-229 PER SRM 53- 02 FIG 18. INSTALLED EXTERNAL SKIN DOUBLER OVER CUT OUT PER SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 2002100700022 20021007 00022 WP 2002 10 7 ASAA0280233 1 20020723 A 5313 59360531 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 951AS 49111 OAK - DURING C-CHECK, FOUND LONGERON 30, IN MID CARGO AREA, CORRODED BEYOND LIMITS FROM STATION 636 TO 655. REPLACED LO NGERON 30 FROM STATION 579-788 PER SRM 51-30-5, PAGE 3, FIG 2. (M) 2 L 7 2 4F A6WE 2002101000063 20021010 00063 NM 2002 10 10 F3LA200200298 1 20021002 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON STR 25L AT BS 500B+6. REPAIRED PER SRM 53-00-03, DETAIL VII. 2 L 7 2 4F RT A16WE 2002101000064 20021010 00064 NM 2002 10 10 F3LA200200299 1 20021002 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL IN FWD CARGO COMPARTMENT BETWEEN BS 500 AND 500A, ABOVE S TR 25L. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-30-04 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002100700023 20021007 00023 WP 2002 10 7 ASAA0280239 1 20020730 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT ASSEMBLY, OP TESTED OK. (M) 2 L 7 2 4F A6WE 2002100700024 20021007 00024 WP 2002 10 7 ASAA0280240 1 20020730 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE IN 1ST CLASS SECTION. RESECURED CONNECTORS. LIG HTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700025 20021007 00025 WP 2002 10 7 ASAA0280241 1 20020801 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE AT ROW 1. RESECURED CONNECTORS. LIGHTS THEN OPE RATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700026 20021007 00026 WP 2002 10 7 ASAA0280242 1 20020802 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING AT ROW 7 'NEEDS A CONNECTOR'. REATTACHED CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700027 20021007 00027 WP 2002 10 7 ASAA0280244 1 20020804 A 3350 0105606 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 49386 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHT AT 23D 'OUT OF SOCKET' DISCONNECTED. REPAIRED RECONNECTED SOCKET. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002100700028 20021007 00028 WP 2002 10 7 ASAA0280245 1 20020806 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE AT ROW 3. RECONNECTED MODULE. LIGHTS THEN OPERA TED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700029 20021007 00029 WP 2002 10 7 ASAA0280254 1 20020809 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING LINE CHECK, FIRST SIX EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPAIRED WIRING. LIGHTS THEN O PERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700030 20021007 00030 NM 2002 10 7 374PA0001 1 20021004 A 2780 189929 SENSOR BOEING 737 73736M 138443B NM A PIDA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 374PA 28333 Takeoff warning horn activated during T/O roll, observed LE flaps transit light illuminated, performed RTO. R&R #1&2 ti res and brakes, R&R #3&4 brakes per 32-41 & 32-45; insp anti-skid system per 32-42-00 OK; performed T/O warning test per AD 88-22-09 OK; brake seizure insp per 05-51-04 OK; high energy insp per 05-51-07 no damage found. R&R #1 kruger flap proximity sensor per MM 27-88-11, Ops chk. good. 2 L 7 2 4F RT A16WE 2002101000065 20021010 00065 NM 2002 10 10 F3LA200200300 1 20021002 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL BETWEEN BS 294.5 AND BS 312, RBL 1 AND CRACKED ON AFT END . REMOVED DAMAGED INTERCOSTAL PER SRM 51-40-02. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-40-06, SRM 51-40-02 AND SOPM 20-41-01. 2 L 7 2 4F RT A16WE 2002100700031 20021007 00031 WP 2002 10 7 ASAA0280255 1 20020808 A 2560 D29982107 HARNESS DOUG DC9 DC983 3022083 WP EVAC SLIDE FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 20320 53019 OAK - DURING C-CHECK, FORWARD PASSENGER DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLIDE. SY STEM CHECKED OK. (M) 2 L 7 2 4F RT A6WE 2002100700032 20021007 00032 WP 2002 10 7 ASAA0280256 1 20020810 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN 1ST CLASS. RECONNECTED LIGHT MODUL ES FOUND DISCONNECTED. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700033 20021007 00033 WP 2002 10 7 ASAA0280257 1 20020810 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 BUR - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 3. RECONNECTED LOOSE LIGHT MODULE CONNECTO R. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700034 20021007 00034 WP 2002 10 7 ASAA0280258 1 20020811 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 53074 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. REPLACED TWO LAMP MODULES. L IGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700035 20021007 00035 WP 2002 10 7 ASAA0280263 1 20020813 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 937AS 49364 PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE IN FORWARD, MID, AND AFT CABIN. RECHARGED POWER SU PPLIES (BATTERY PACKS). LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002100700036 20021007 00036 WP 2002 10 7 ASAA0280264 1 20020813 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 RNO - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. SPLICED BROKEN MODULE CONNECT OR WIRE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700037 20021007 00037 WP 2002 10 7 ASAA0280265 1 20020813 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. REATTACHED LOOSE LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700038 20021007 00038 WP 2002 10 7 ASAA0280266 1 20020816 A 3397 0105606 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 PDX - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 26-29. REPAIRED DAMAGED WIRING BETWEEN LIGHT MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002100700039 20021007 00039 WP 2002 10 7 ASAA0280267 1 20020816 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING PREFLIGHT CHECK, FOUND FIRST FIVE EMERGENCY TRACK LIGHTS INOPERATIVE. RECONNECTED LIGHTS. LIGHTS THEN OPE RATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700040 20021007 00040 WP 2002 10 7 ASAA0280268 1 20020816 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 28. RECONNECTED LIGHTS. LIGHTS THEN OPER ATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700041 20021007 00041 WP 2002 10 7 ASAA0280269 1 20020817 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SFO - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LIGHT. LIGHT THE N OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700042 20021007 00042 WP 2002 10 7 ASAA0280270 1 20020818 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN VARIOUS LOCATIONS THROUGH OUT CABIN. RECONNEC TED/REPAIRED LIGHTS. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100700043 20021007 00043 EU 2002 10 7 SIMA200219128 1 20020705 A 5512 SKIN SAAB SF340 340B 7860101 EU HORIZ STAB DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 ABI - RIGHT HORIZONTAL LOWER SKIN HAS ONE DENT. PERFORMED EDDY CURRENT AND SONIC BOND CHECK, NO DEFECTS NOTED. DENT FO UND TO BE WITHIN SAAB 340 SRM 55-10-10 AND 51-10-10 LIMITS. (M) 2 L 7 2 4T RT A52EU 2002100700044 20021007 00044 EU 2002 10 7 SIMA200219129 1 20020705 A 5347 CARGO TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 ABI - CARGO AREA SEAT TRACK AT BL 0 HAS AREAS MEASURED BELOW LIMITS. SEAT TRACK ACCEPTED AS IS IAW SAAB 340 STATEMENT 3 40SDS004141, PARA 6. (M) 2 L 7 2 4T RT A52EU 2002100700045 20021007 00045 EU 2002 10 7 SIMA200224005 1 20020826 A 5347 7253742409 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 334AE 340B334 ABI - FOUND SEAT TRACK 36 R WORN ON TOP FLANGE. REMOVED AND INSTALLED SEAT TRACK IAW SAAB 340 SRM CHAPTERS 51-40-21, 51 -40-22 AND 51-40-25 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002100700046 20021007 00046 EU 2002 10 7 SIMA200224006 1 20020814 A 5320 STRUCTURE SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 373AE 340B373 DURING AN MBV INSPECTION, FOUND DAMAGE NOTED ON THE RIGHT FLOOR OF THE COCKPIT OUTBOARD OF THE COPILOTS SEAT TRACK. REM OVED THE DAMAGE BY A CUT OUT. PERFORMED AN EDDY CURRENT INSPECTION OF THE CUT OUT WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS004217 REV A AND STANDARD SAB 340 SRM 72LKS 3079 REV 40 PRA CTICES. (M) 2 L 7 2 4T RT A52EU 2002100700047 20021007 00047 EU 2002 10 7 SIMA200224007 1 20020815 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 373AE 340B373 ABI - DURING MBV INSPECTION, DAMAGE WAS NOTED ON THE UPPER PORTION OF FRAME 694 OF THE CARGO FLOOR. REMOVED BUCKLED ANG LE FROM WEB. RECONTOURED THE DAMAGED AREA OF THE WEB AND PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA AND FOUND NO DEFECTS. FABRICATED A DOUBLER REPAIR. WORK DONE IAW SAAB REPAIR STATEMENT 340SDS004217 AND STANDARD SAAB 340 SRM PRACT ICES. (M) 2 L 7 2 4T RT A52EU 2002100700048 20021007 00048 EU 2002 10 7 SIMA200224008 1 20020814 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 373AE 340B373 ABI - DURING AN MBV INSPECTION, DAMAGE WAS NOTED ON THE UPPER PORTION OF FRAME 702 OF THE CARGO FLOOR. RECONTOURED THE DAMAGE AREA OF THE WEB AND FLANGE, PERFORMED AN EDDY CURRENT INSPECTION AND FOUND NO DEFECTS. FABRICATED A 13 INCH REIN FORCEMENT STIFFENER FOR THE DAMAGE PORTION. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS004217 AND STANDARD SAAB 340 SR M PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002100700049 20021007 00049 EU 2002 10 7 SIMA200224010 1 20020812 A 3211 TRUNNION SAAB SF340 340B 7860101 EU RT MLG DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 373AE 340B373 ABI - DURING INSPECTION DAMAGE WAS NOTED ON THE RIGHT MLG FORWARD TRUNNION, FORWARD OUTBOARD ATTACHMENT HOLE. THE DAMAG E WAS IN THE FORM OF THREAD MARKS OVER THE ENTIRE LENGTH OF THE HOLE. DAMAGED HOLE WAS REAMED TO .5646 DIAMETER. REAMI NG THREAD MARKS WERE BLENDED WITHOUT INCREASING THE DEPTH OF THE DAMAGE. REPAIR DONE IAW SAAB 340 REPAIR 340SDS004217, SAAB 340 AMM 57-40-05-8 AND STANDARD SAAB 340 PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002100700050 20021007 00050 EU 2002 10 7 SIMA200224011 1 20020815 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 373AE 340B373 ABI - DURING MBV INSPECTION, FOUND FRAME 258 TO HAVE A PREVIOUS REPAIR WITH ADDITIONAL CORROSION BEYOND SRM LIMITS. REM OVED PREVIOUS REPAIR AND COMPLETELY REMOVED CORROSION BY CUT OUT. PERFORMED EDDY CURRENT INSPECTION AND FOUND DEFECTS. FABRICATED A REPAIR DOUBLER, L SHAPED FILLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS004248 AND STANDARD SRM PRA CTICES. (M) 2 L 7 2 4T RT A52EU 2002100700051 20021007 00051 SO 2002 10 7 SIMA200224012 1 20020821 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 626AE 145117 ABI - DURING AN IMBV INSPECTION, MAINTENANCE FOUND CORROSION ON PREVIOUS REPAIR ON LEFT OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR AND FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB 145 9SRM 145/1142, CHAPTER 53, 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002100700052 20021007 00052 SO 2002 10 7 SIMA200224013 1 20020820 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 626AE 145117 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON THE GALLEY CENTER FLOORBEAM. REMOVED CORRODED GALLEY CENTER FLOORBE AM. INSTALLED SERVICEABLE FLOORBEAM IAW EMB 145 (SRM 145/1142, CHAPTER 51, REV 19) 51-40-02, 51-20--01, 51-20-03, 51-40 -04, AEAI ETN NR EB 53-022 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002100700053 20021007 00053 SO 2002 10 7 SIMA200224014 1 20020821 A 5315 14521721007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 626AE 145117 ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL IN THE GALLEY WAS FOUND TO BE CORRODED. CUT OUT DAMAGED PORTION OF THE DIGITAL. FABRICATED TWO DOUBLER, ONE SHIM. REPAIR DONE IAW EMB 145 SRM (145/1142, REV 18) SRM 53-21-10, AND STAND ARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002100700054 20021007 00054 SO 2002 10 7 SIMA200224015 1 20020818 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 626AE 145117 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON THE GALLEY RIGHT FLOORBEAM. REMOVED CORRODED GALLEY RIGHT BEAM. IN STALLED SERVICEABLE BEAM IAW EMB 145 (SRM 145/1142, CHAPTER 51, REV 19) 51-40-02, AEAI ETN EM 53-028 AND STANDARD SRM PR ACTICES. (M) 2 L 7 2 4T RT T00011AT 2002100700055 20021007 00055 SO 2002 10 7 SIMA200224016 1 20020817 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 626AE 145117 ABI - DURING AN IMBV INSPECTION, FOUND CARGO DOOR LOWER SILL TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL. INSTALLED SERVICEABLE SILL IAW EMB145 (SRM 145/1142, CHAPTER 51, REV 17) 51-40-02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002100700056 20021007 00056 SO 2002 10 7 SIMA200224102 1 20020827 A 2710 AILERON EMB 145 EMB145LR 3260212 SO LT WING LIGHTNING STRIKE A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 655AE 145452 DFW - FLT 3473 - DURING CLIMB-OUT, AIRCRAFT WAS STRUCK BY LIGHTNING. AFTER INSPECTION REPLACED LEFT AILERON AND RIGHT E LEVATOR TRIM TAB. (M) 2 L 7 2 4T RT T00011AT 2002100700057 20021007 00057 SO 2002 10 7 SIMA200224103 1 20020822 A 5320 CHANNEL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 ABI - FOUND CORROSION ON RIGHT HAT BEAM AT FRAME 22, LEVEL 2 FINDING. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT HAT BEAM AT FRAME 22 IAW EMB 145 SRM 53-21-10, 51-40-02 AND ETN EM 53-034. (M) 2 L 7 2 4T RT T00011AT 2002100700058 20021007 00058 SO 2002 10 7 SIMA200224104 1 20020822 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 LEVEL 2 FINDING, FORWARD DIAMOND GUSSET HAS CORROSION. REPLACED FORWARD DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002100700059 20021007 00059 SO 2002 10 7 SIMA200224105 1 20020822 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 LEVEL 2 FINDING, CENTER BEAM GUSSET HAS CORROSION. REPLACED CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002100700060 20021007 00060 SO 2002 10 7 SIMA200224106 1 20020822 A 5320 14522459003 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 ABI - LEVEL 2 FINDING, GALLEY RAMP SUPPORT CORRODED. REPLACED GALLEY RAMP SUPPORT IAW EMB 145SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002100700061 20021007 00061 SO 2002 10 7 SIMA200224107 1 20020822 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 ABI - LEVEL 2 FINDING, RIGHT FORWARD SILL HAS CORROSION. REPLACED RIGHT FORWARD SILL IAW EMB 145 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002100700062 20021007 00062 SO 2002 10 7 SIMA200224108 1 20020822 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 LEVEL 2 FINDING, RIGHT AFT SILL HAS CORROSION. REPLACED RIGHT AFT SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002100700063 20021007 00063 SO 2002 10 7 SIMA200224109 1 20020822 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 ABI - LEVEL 2 FINDING, LEFT SILL HAS CORROSION. REPLACED LEFT SILL IAW EMB145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002100700064 20021007 00064 SO 2002 10 7 SIMA200224110 1 20020822 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 LEVEL 2 FINDING, AFT DIAMOND GUSSET HAS CORROSION. REPLACED AFT DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002101000066 20021010 00066 NM 2002 10 10 F3LA200200301 1 20021002 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL IN FWD CARGO COMPARTMENT BETWEEN BS 500B AND 500C, ABOVE STR 25L. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-30-04 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002101000069 20021010 00069 NM 2002 10 10 F3LA200200302 1 20021002 A 5320 WEB BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR WEB AT BS 1016. FABRICATED AN INSTALLED REPLACEMENT WEB PER BO EING DRAWING 65-46812-109 AND SRM 53-30-01. 2 L 7 2 4F RT A16WE 2002101000070 20021010 00070 NM 2002 10 10 F3LA200200303 1 20021002 A 5320 STRAP BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR STRAP AT BS 1016. FABRICATED AND INSTALLED REPLACEMENT FLOOR S TRAP PER SRM 53-30-01 AND BOEING DRAWING 65-46812. 2 L 7 2 4F RT A16WE 2002101000071 20021010 00071 NM 2002 10 10 F3LA200200304 1 20021002 A 5320 STRAP BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR STRAP BETWEEN BS 1006 AND BS 1016, RBL 18. FABRICATED AND INST ALLED REPLACEMENT FLOOR STRAP PER BOEING DRAWING 65-46812 AND SRM 51-30-01. 2 L 7 2 4F RT A16WE 2002100700065 20021007 00065 NM 2002 10 7 F3LA200200305 1 20021002 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 947 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TO BULKHEAD ANGLE AT BS 947. REPLACED BULKHEAD ANGLE PER SRM 5 3-30-53 AND 51-40-03. 2 L 7 2 4F RT A16WE 2002100700066 20021007 00066 NM 2002 10 7 QXEA0201589 1 20021004 A 2610 PU90461R2 DETECTOR DHAV DHC8 DHC8202 2809007 NM ZONE 200 DEFECTIVE A QXEA K NONE J WARNING INDICATION CR CRUISE 1 NM 09 354PH 19 19 498 SEA-LAVATORY FIRE DETECTOR WENT OFF INFLIGHT. PRESSED RESET TO SILENCE, REMAINED QUIET REST OF FLIGHT. REPLACED LAVATORY FIRE DETECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002101000072 20021010 00072 NM 2002 10 10 F3LA200200306 1 20021002 A 5320 CHANNEL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 DURING C-4 CHECK, INSPECTION REPORTED FLOOR CHANNEL CORRODED AT BS 727D ABOVE STRINGER 28L. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-60-53. FABRICATED AND INSTALLED REPLACEMENT CHANNEL PER SRM 53-60-53, SRM 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002100700068 20021007 00068 NM 2002 10 7 UPS02439255 1 20020902 A 3350 LIGHT BOEING 747 747123F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:PFLT AFT L1 DOOR EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK NORMAL. 2 L 7 4 4F A20WE 2002100700069 20021007 00069 NM 2002 10 7 0203355515 1 20021006 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 515US 23203 DURING "L" CHECK FOUND CRACK IN FLOORBEAM UPPER CAP AT BS 700 LBL 45. REPAIRED PER EA 55-191543. 2 L 7 2 4F RT A2NM 2002100700070 20021007 00070 NM 2002 10 7 0203345527 1 20021004 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 527US 23842 DURING "L" CHECK FOUND CRACK IN FLOORBEAM UPPER CAP AT BS 700 LBL 25. REPAIRED PER EA 55-191542. 2 L 7 2 4F RT A2NM 2002100700071 20021007 00071 WP 2002 10 7 UPS02839237 1 20020723 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 COMPLY WITH MPI P 13516;PERM REPAIR TO DENT STA -80 TO -74 ON LEFT SIDE ABOVE CUSP ANGLE. REMOVED IN TERIN REPAIR, NDT VERIFIED NO CRACKS AT CUTOUT AREA, FABRICATED AND INSTALLED DOUBLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2002100700072 20021007 00072 NM 2002 10 7 UPS02239609 1 20021004 A 5310 SHEAR TIE BOEING 727 72722C 138400F NM BS1050 STR.5. CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI STR.SHEAR TIE CRACKED AT STR.5 R/H BS1050. SHEAR TIE REMOVED IAW SRM 51-30-2 SHEAR TIE REPLACED IAW 51-20-1+51-40-3 2 L 7 3 4F A3WE 2002100700073 20021007 00073 NM 2002 10 7 UPS02239610 1 20020916 A 5310 SHEAR TIE BOEING 727 72722C 138400F NM BS1010 STR.4L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI STR. SHEAR TIE CRACKED AT STR. 4 L BS 1010. SHEAR TIE REMOVED IAW SRM 51-30-2 SHEAR TIE REPLACE D IAW SRM 51-20-1+51-40-3. 2 L 7 3 4F A3WE 2002100700074 20021007 00074 NM 2002 10 7 UPS02239611 1 20020916 A 5310 SHEAR TIE BOEING 727 72722C 138400F NM BS1010 STR.6 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI STR. SHEAR TIE CRACKED AT STR.6 R/H BS 1010. SHEAR TIE REMOVED IAW SRM 51-30-2. SHEAR TIE REPLA CED IAW SRM 51-20-1+51-40-3. 2 L 7 3 4F A3WE 2002100700075 20021007 00075 NM 2002 10 7 UPS02239613 1 20020916 A 5310 SHEAR TIE BOEING 727 72722C 138400F NM BS990 STR.6 R/H CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI STR. SHEAR TIE CRACKED AT STR.6 R/H B.S.990. STRINGER SHEAR TIE REMOVED IAW SRM 51-30-2. STR.SH EAR TIE REPLACED IAW SRM 51-20-1 AND 51-40-3. 2 L 7 3 4F A3WE 2002100700076 20021007 00076 NM 2002 10 7 UPS02239614 1 20020916 A 5310 SHEAR TIE BOEING 727 72722C 138400F NM BS990 STR.5 R/H CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI STR. SHEAR TIE CRACKED AT STR.5 R/H BS 990. SHEAR TIE REMOVED IAW SRM 51-30-2 SHEAR TIE REPLACE D IAW SRM 51-20-1 AND 51-40-3. 2 L 7 3 4F A3WE 2002100700077 20021007 00077 NM 2002 10 7 UPS02239615 1 20020915 A 5310 SHEAR TIE BOEING 727 72722C 138400F NM BS 1070 STR.5 LH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI STR.5 L/H SHEAR TIE FOUND CRACKED AT BS 1070. STR. SHEAR TIE REMOVED IAW 51-30-2. STR. SHEAR TI E REPLACED IAW SRM 51-20-1 AND 51-40-3. 2 L 7 3 4F A3WE 2002100700078 20021007 00078 NM 2002 10 7 UPS02239617 1 20020916 A 5310 SHEAR TIE BOEING 727 72722C 138400F NM BS1030 STR.8 R/H CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI STR. SHEAR TIE CRACKED AT STR.8 R/H BS 1030. SHEAR TIE REMOVED IAW SRM 51-30-2. SHEAR TIE REPLA CED IAW SRM 51-20-1 AND 51-40-3. 2 L 7 3 4F A3WE 2002100700079 20021007 00079 WP 2002 10 7 UPS02839238 1 20020729 A 5730 SKIN DOUG DC8 DC873F 302199F WP LEFT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION IB OF XFS 710. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 2H. 2 L 7 4 4F RT 4A25 2002100700080 20021007 00080 WP 2002 10 7 UPS02839239 1 20020831 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:PFLT EMERGENCY LIGHTS DO NOT ILLUMINATE. FOUND ON PREDEPARTURE CK. INSTALLED NEW BATTERY PACK OPS CK G OOD. OPS CK GOOD IAW M/M CH 33-50 -01. 2 L 7 4 4F RT 4A25 2002100700081 20021007 00081 WP 2002 10 7 UPS02839240 1 20020729 A 5712 RIB DOUG DC8 DC873F 302199F WP LEFT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 616.25. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002100700082 20021007 00082 WP 2002 10 7 UPS02839241 1 20020729 A 5730 SKIN DOUG DC8 DC873F 302199F WP LEFT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN IS CRACKED AT DRAIN HOLE AT XFS 597.5. STOP DRILLED CRACK, NDT VERIFIED STO P DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-4087. 2 L 7 4 4F RT 4A25 2002100700083 20021007 00083 WP 2002 10 7 UPS02839242 1 20020729 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON L1 DOOR UPPER FWD CORNER AND REPAIR PER DC8 SRM 53-2-0 FIG 15. REM OVED EXISTING REPAIR, CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15, AND EO DC8-5320-17264-A, AND SAA SK 806-198. 2 L 7 4 4F RT 4A25 2002100700084 20021007 00084 WP 2002 10 7 UPS02839243 1 20020902 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:N/A CORRODED SHEAR TIE AT STA 1140 BETWEEN STR 35L AND 36L. REPAIRED SHEAR TIE IAW DC8 SRM 53-2-0 AS RE QUIRED. 2 L 7 4 4F RT 4A25 2002100700085 20021007 00085 NM 2002 10 7 CALA0200486 1 20021004 A 2520 417N3011402D PSU BOEING 737 737824 13844BZ NM ROW 19 SHORTED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 38257 30612 A BURNING ODOR BEGAN COMING FROM THE PASSENGER SERVICE UNIT AT R/H SIDE, ROW 19 WHILE ON APPROACH TO IAH. THE AIRCRAFT L ANDED WITHOUT INCIDENT. MAINTENANCE FOUND A CONTROL CIRCUIT CARD IN PSU HAD SHORTED. THE PSU WAS REMOVED AND REPLACED IA W MM 25-23-61. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2002100700086 20021007 00086 NM 2002 10 7 CALA0200487 1 20021005 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 INSPECTION FOUND FLOORBEAM CRACKED ON UPPER ANGLE AT STA 328, LBL 12. THE CRACKED SECTION OF FLOORBEAM WAS REMOVED AND R EPLACED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2002100700087 20021007 00087 WP 2002 10 7 UPS02839244 1 20020729 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON THE L2 DOOR LOWER FWD CORNER AND REPAIR PER DC8 53-2-0 FIG 18. REM OVED EXISTING REPAIR, NDT VERIFIED NO CRACKS AT PREVIOUS CUTOUT, FABRICATED AND INSTALLED DOUBLER TRIPLER AND FILLER IAW SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2002100700088 20021007 00088 WP 2002 10 7 UPS02839245 1 20020729 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON THE R1 DOOR LOWER AFT CORNER AND REPAIR PER DC8 SRM 53-2-0 FIG 14. REMOVED EXISTING REPAIR, NDT VERIFIED NO CRACKS AROUND EXISTING CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER, AND T RIPLER IAW SRM 53-2-0 FIG 14. 2 L 7 4 4F RT 4A25 2002100700089 20021007 00089 WP 2002 10 7 UPS02839246 1 20020729 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 BULKHEAD FWD OF RT WHEEL WELL STA 851 RBL 50 L ANGLE FITTING IS CRACKED. NDT VERIFIED CRACK TERMINAT ES AT FASTENER HOLE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002100700090 20021007 00090 WP 2002 10 7 UPS02839247 1 20020730 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 CABIN FLOOR SEAT TRACK IS WORN AND BROKEN AT LBL 45 STA 1590-1600. REMOVED DAMAGED SEAT TRACK STA 15 90 TO 1680 LBL 45, FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK SECTION IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 2002101000074 20021010 00074 NM 2002 10 10 F3LA200200308 1 20021002 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON DIAGONAL FLOOR SUPPORT BETWEEN BS 1006 AND 1016, RT. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-60-51 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002100700091 20021007 00091 NM 2002 10 7 F3LA200200309 1 20021002 A 5315 FLOOR SUPPORT BOEING 737 737301 1384611 NM BS 1006 - 1016 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON DIAGONAL FLOOR SUPPORT BETWEEN BS 1006 AND 1016, L/H. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-60-51 ANDD 51-40-02. 2 L 7 2 4F RT A16WE 2002100700092 20021007 00092 NM 2002 10 7 QXEA0201590 1 20021002 A 3230 83231014003 LINK DHAV DHC8 DHC8202 2809007 NM ZONE 700 INOPERATIVE A QXEA K NONE O OTHER CR CRUISE 1 NM 09 345PH 476 PDX-RIGHT GEAR DOORS EITHER DID NOT CLOSE ON GEAR RETRACTION OR FELL OPEN IN FLIGHT. NO COCKPIT INDICATION. REMOVED AND REPLACED RIGHT HAND REAR MAIN LANDING GEAR LEFT HAND DOOR CONNECTING LINK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002100700093 20021007 00093 NM 2002 10 7 F3LA200200311 1 20021002 A 5310 BEAR STRAP BOEING 737 737301 1384611 NM BX 441 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON C-1 DOOR BEAR STRAP AT BS 441, RBL 7.5. FABRICATED AND INSTALLED REP AIR PER PER EA 53-737-180. 2 L 7 2 4F RT A16WE 2002100700094 20021007 00094 2002 10 7 ZW0A0210301 4 20020105 A 2565 101651303 SLIDE BOEING 767 767300 1385204 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 691LF 25137 ON THE GROUND THE RIGHT SIDE NUMBER 1 CABIN DOOR ESCAPE SLIDE PARTIALLY DEPLOYED AFTER THE SLIDE WAS NOT DISARMED. THE A IRCRAFT OPERATED ONE LEG PER MEL AND THE SLIDE WAS THEN REPLACED. CHECK-C 9-23-00 LAX. --OPEN-- 2 L 7 2 4F RT A1NM 2002100700095 20021007 00095 NM 2002 10 7 AWXA200200981 1 20021004 A 5330 2024T3050 SKIN BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 0 0 23632 PHX - MAJOR REPAIR - DURING INSPECTION A 3.5" CRACK WAS FOUND ON THE R/H SIDE FUSELAGE SKIN APPROXIMATELY 30" FORWARD OF THE AFT CARGO DOOR, HEFC CONFIRMED CRACK. MAINTENANCE CUTOUT DAMAGED SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST AT CUOUT. FABRICATED A REPAIR DOUBLER, AND INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01, PG. 204-206. 2 L 7 2 4F RT A16WE 2002100700096 20021007 00096 NM 2002 10 7 AWXA200200982 1 20021004 A 5313 7075T6032 TIE CLIP BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 0 0 23632 PHX - MAJOR REPAIR - DURING INSPECTION A CRACK WAS FOUND ON THE STRINGER TIE CLIP AT BS 767, STR 19 R/H. MAINTENANCE REM OVED THE DAMAGED STRINGER TIE CLIP AT BS 767, STR 19 R/H, FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP, AND INSTALLED REPAIR PART IAW DWG 69-63707-3, AND 737-300 SRM 51-30-2. 2 L 7 2 4F RT A16WE 2002100700097 20021007 00097 NM 2002 10 7 AWXA200200985 1 20020930 A 5315 69353654 ATTACH ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 0 0 25400 MCN - MAJOR REPAIR - DURING C12 CHECK A 1/4" CRACK WAS FOUND ON FLOOR SUPPORT ATTACH ANGLE AT BS 500D TO BS 520, BL 0. MAINTENANCE REMOVED THE DAMAGED FLOOR SUPPORT ATTACH ANGLE FROM BS 500D TO BS 520, FABRICATED A NEW REPLACEMENT FLOOR SU PPORT ATTACH ANGLE, AND INSTALLED REPAIR PART IAW DWG 69-35365, AND B737-300 SRM 51-40-02, PG. 3, & 38, FIG. 8. 2 L 7 2 4F RT A16WE 2002100700098 20021007 00098 WP 2002 10 7 NACA20020042 1 20020913 A 2100 5499491 SCROLL DOUG 75372415503 DOUG DC6 DC6 3021702 WP SHEARED A NACA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 43872 1681 1348 4377 533294 Discrepancies: Smoke in Cockpit. R/H Cabin Super Charger Impellar nut sheared.Corrective Action: Replaced R/H Cabin Sup ercharger Scroll. 2 L 7 4 4R A781 2002100700099 20021007 00099 NM 2002 10 7 NACA20020043 1 20020919 A 3230 65178107 ACTUATOR 65727628 BOEING 727 72723 1384004 NM CRACKED A NACA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 AL 03 992AJ FTL03 19428 Discrepancy: On approach to ANC, loss of "A" hydraulic system.Corrective Action: Replaced nose gear lock actuator. 2 L 7 3 4F A3WE 2002100800001 20021008 00001 NE 2002 10 8 MALA020597 2 20021004 A 7530 216118216 BLEED BAND BAC 146 AVRO146RJ85A 1500097 EU LF507 LF5071F NE A MALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 GL 15 524XJ E2349 DURING CLIMBOUT OF FLIGHT #3591 #3 ENGINE WAS SHUTDOWN DUE TO EGT OVERTEMP. A SLIGHT NOISE WAS HEARD AND EGT WAS RISING RAPIDLY WITH READINGS FLASHING. THRUST LEVER WAS BROUGHT BACK RIGHT AWAY TO CONTROL EGT, AND ENGINE SUBSEQUENTLY SHUTDO WN TO PREVENT DAMAGE. OBSERVED EGT WAS 648C BY CAPT AND 680 BY FO. FLIGHT DIVERTED TO CVG. MAINTENANCE REMOVED AND RE PLACED #3 ENGINE BLEED BAND PN 2-161-182-16. OPS CHECKED PARAMETERS, PWR ASSURANCE LIMITS GOOD. IAW AMM 75-30-04 AND H ONEYWELL PVA TRACK #24-ALF-2002-0091. SPECIAL PROCEDURES CHECKS CW AND OK. 2 H 7 4 4F 4 F RT A49EU E6NE 2002100800002 20021008 00002 NE 2002 10 8 MALA020598 2 20021006 A 7220 CT75A2 ENGINE SAAB SF340 SF340A 7850100 EU CT7TP CT75A1 30030 NE A MALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 15 79XJ 340A079 DURING FLIGHT #3183, RH ENGINE STARTED TO OPERATE VERY IRRATICALLY ABOUT 15 MINUTES AFTER TO. TORQUE PEGGED TO 120, AND ITT OVERTEMPED. WITNESSED AS HIGH 977 DEGREES AND RED LIGHT. DID PRECAUTIONARY SHUTDOWN AND AIR RETURN TO MSP. MAINT ENANCE FOUND FDR PARAMETERS OUT OF LIMITS, COMPLETED WORK PACKAGE 10-71-02. ENGINE CHANGE AND ASSOCIATED TASK CARDS ENGI NE PN ON/OFF CT7-5A2, SN/OFF GE-E-367386K, SN/ON GE-E-367316 ALL CHECKS GOOD SEE CONTINUTATION CARD #070609 FOR DETAILS. 2 L 7 2 4T 4 T RT A52EU E8NE 2002100800003 20021008 00003 NM 2002 10 8 F3LA200200312 1 20021004 A 5320 DOUBLER BOEING 737 737301 1384611 NM BS 440 & 460 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON RADIO ALTIMETER ANTENNA INTERNAL DOUBLER BETWEEN BS 440 AND 460. REP LACED RADIO ALTIMETER ANTENNA INTERNAL DOUBLER PER SRM 51-10-2 AND BOEING DRAWING 69-27827. 2 L 7 2 4F RT A16WE 2002100800005 20021008 00005 NM 2002 10 8 IU6R163738 1 20021001 A 2761 654494710 HOUSING BOEING 737 737 UTILSYS NM SPOILER ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 1386 CRACK IN HOUSING. WEAK HOUSING, MAKE STRONGER HOUSING. 2 L 7 2 4F RT A16WE 2002100800006 20021008 00006 NM 2002 10 8 IU6R163916 1 20020103 A 2761 654494710 HOUSING BOEING 737 737* NM SPOILER ACTUATOR BROKEN B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 47370 HOUSING IS BROKEN. 2 L 7 2 4F RT A16WE 2002100800007 20021008 00007 NM 2002 10 8 IU6R170238 1 20020509 A 3240 511531 HOUSING BOEING 737 737 UTILSYS NM SHUTTLE VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 CRACKED IN MOUNTING HOLES. 2 L 7 2 4F RT A16WE 2002100800008 20021008 00008 NM 2002 10 8 IU6R170239 1 20020809 A 3240 511531 HOUSING BOEING 737 737* NM SHUTTLE VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING CRACKED MOUNTING HOLES. 2 L 7 2 4F RT A16WE 2002100800009 20021008 00009 NM 2002 10 8 IU6R170687 1 20020826 A 2761 654494710 HOUSING BOEING 737 737* NM SPOILER ACTUATOR BROKEN B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 52559 24699 BROKEN HOUSING. 2 L 7 2 4F RT A16WE 2002100800010 20021008 00010 NM 2002 10 8 IU6R170748 1 20020828 A 2761 654494715 HOUSING BOEING 737 737* NM SPOILER ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 36490 4910 HOUSING CRACKED. 2 L 7 2 4F RT A16WE 2002100800011 20021008 00011 NM 2002 10 8 HNAA0200069 1 20021004 A 3350 6013211X BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA O OTHER L NO TEST UK UNKNOWN 1 EA 07 917HA 8161 451 075 CENTER ISLE EXIT SIGN WHITE DOWN LIGHT AND RIGHT HAND AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGH T BATTERY AND POWER SUPPLY. 2 H 7 2 4T RT A13NM 2002100800012 20021008 00012 NM 2002 10 8 UPS02439269 1 20020818 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C U/D - BS 440-460 LBL 0 - RBL 50 FLOOR SUPPORT AND WEB FOUND CORR. BLEND OUT EXCEEDS SRM LIMIT, FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002100800013 20021008 00013 NM 2002 10 8 UPS02439270 1 20020817 A 5320 65B125831 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C RT LG W/W I/B PRESSURE DECK TO VERTICAL WEB ATTACHMENT SHEAR TIE FITTING AT BS 1416 RBL 1 AREA UPPER F LANGE CRACKED. RT LG W/W I/B PRESSURE DECK TO VERTICAL WEB AT BS 1416 RBL 1 STIFFENER ATT CRACKED FITTING REPLACED AS P ER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002100800014 20021008 00014 NM 2002 10 8 UPS02439271 1 20020818 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C U/D - BS 680-710 LBL 46 SEAT TRACK CROWN FOUND CORROSION. COR BLEND OUT EXCEEDS SRM LIMIT, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 6. 2 L 7 4 4F A20WE 2002101000077 20021010 00077 NM 2002 10 10 F3LA200200313 1 20021004 A 5753 ANGLE BOEING 737 737301 1384611 NM T/E FLAP LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED RT WING INBD TE PLATE LOOSE FASTENERS ON MID FLAP. FABRICATED AND INSTALLED REPLA CEMENT ANGLE PER SRM 51-30-01, FIGURE 7 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002100800015 20021008 00015 NM 2002 10 8 UPS02439273 1 20020813 A 5320 WEB BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D - BS 390 S-14R WEB FOUND CRACKED. M/D BS 380-400 STR 14R WEB REPAIRED AS PER SRM 53-10-04 FIG 55. 2 L 7 4 4F A20WE 2002100800016 20021008 00016 NM 2002 10 8 UPS02439274 1 20020820 A 5320 PLATE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT LG W/W STA 1241 CANTED B/H DRAIN TUBE FITTING COVER PLATE FOUND CRACK AT LBL 98. LT LG W/W STA 1241 CANTED B/H DRAIN TUBE FITTING COVER PLATE REPLACE AS PER SRM 51-10-01 PG 8 AND FASTENERS INSTALLED AS PER SRM 51-3 0-02. 2 L 7 4 4F A20WE 2002100800017 20021008 00017 NM 2002 10 8 UPS02439276 1 20020830 A 3350 70031215 CONNECTOR BOEING 747 747200 1384847 NM CABIN LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:W/E UPPER DECK CREW DOOR EMERGENCY EXIT SIGN INTERMITTENT, FAILED TO COME ON DURING MAINTENANCE TEST RETORQUED LOOSE CONNECTIONS ON LIGHT ASSY. 2 L 7 4 4F RT A20WE 2002101000078 20021010 00078 NM 2002 10 10 F3LA200200314 1 20021004 A 5753 SKIN BOEING 737 737301 1384611 NM T/E FLAP DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED L/E OF LT OTBD MID T/E FLAP DENTED AND GOUGED AT OTBD ACTUATOR. FABRICATED AND IN STALLED DOUBLER PER SRM 57-53-01, SOPM 20-41-02 AND SOPM 20-42-01. 2 L 7 2 4F RT A16WE 2002100800018 20021008 00018 NM 2002 10 8 UPS02439277 1 20020818 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C U/D - BS 440 RBL 20-40 FLOOR BEAM FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMIT, UPPER CHORD REPAIRED AS PER HAECO RS NR R53-15-34883 & UPS AUTH NR 747-53-20100. 2 L 7 4 4F A20WE 2002100800019 20021008 00019 NM 2002 10 8 UPS02439278 1 20020814 A 5414 PANEL BOEING 747 747123 1384873 NM NR 3 PYLON WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C NR 3 PYLON - O/B AFT UPPER MOUNT HALF MOON PANEL CUTOUT WORN AT FWD PORTION. NR 3 PYLON O/B AFT UPPE R MOUNT HALF MOON PANEL CUTOUT REPAIRED AS PER SRM 54-30-03 FIG 35 AND FIG 36. 2 L 7 4 4F A20WE 2002100800020 20021008 00020 NM 2002 10 8 UPS02439279 1 20020819 A 5210 SKIN BOEING 747 747123 1384873 NM L3 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D L3 DOOR UPPER HINGE SKIN CUTOUT CRACKED. SKIN REPAIRED AS PER SB 747-52-2144 FIG 5. 2 L 7 4 4F A20WE 2002100800021 20021008 00021 NM 2002 10 8 UPS02439310 1 20020815 A 5312 BULKHEAD BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FUSELAGE RT TUNNEL STA 260 CANTED BULKHEAD WEB RADIUS CRACKED AT WL 180 RBL 70. FUSELAGE RT TUNNEL ST A 260 CANTED BULKHEAD WEB RADIUS CRACKED AREA REPAIRED AS PER SRM 53-10-04 FIG 6. 2 L 7 4 4F A20WE 2002100800022 20021008 00022 NM 2002 10 8 2002F00918 1 20020818 A 2612 106087713 FIRE LOOP BOEING 727 727282 138408T NM NR 1 ENGINE OUT OF POSITION A RYNA K NONE N FALSE WARNING CR CRUISE 1 CE 07 281SC 21949 IN FLIGHT FROM MBJ-STL, NR 1 ENGINE FIRE PROTECTION GROUND FAULT LIGHT ILLUMINATED. REPOSITIONED ENGINE NR 1 FIRE LOOP. (M) 2 L 7 3 4F RT A3WE 2002100800023 20021008 00023 NE 2002 10 8 2002F00919 2 20020807 A 7200 ENGINE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 MALFUNCTIONED A RYNA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 07 54SW 21535 549376 DURING CLIMB-OUT FROM CLE, NOTED ABNORMAL HIGH OIL TEMP ON NR 1 ENGINE. ACCOMPLISHED PRECAUTIONARY ENGINE SHUTDOWN. EM ERGENCY WAS DECLARED AND AIRCRAFT LANDED IN PIT WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE. (M) 2 L 7 2 4F 4 F A16WE E2EA 2002100800024 20021008 00024 SO 2002 10 8 2002F00920 1 20020814 A 2150 8166362 A/C PACK EMB 145 EMB145LR 3260212 SO A/C BAY MALFUNCTIONED A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 845MJ 145502 FLT 5745 - HSV-CLT - RETURNED TO FIELD DUE TO SMOKE IN THE CABIN WITH PACK OPERATION. MAINTENANCE TROUBLESHOT AND ISOLA TED THE RIGHT, CAUSING THE SMOKE. MAINTENANCE REPLACED THE RIGHT PACK. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT T00011AT 2002100800025 20021008 00025 NM 2002 10 8 ASAA0210176 1 20020812 A 3350 8731002142 SIGN BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 ANC - DURING INSPECTION, FOUND EXIT IDENTIFIER AT THE SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED EXIT IDENTIFIER, THEN LIGHT TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2002100800026 20021008 00026 NM 2002 10 8 ASAA0210177 1 20020816 A 3350 873100211 SIGN BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - EMERGENCY EXIT IDENTIFIER OVER R2 DOOR INOPERATIVE. REMOVED AND REINSTALLED EMERGENCY LIGHT ASSEMBLY OVER R2 DOOR , THEN OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 2002100800027 20021008 00027 NM 2002 10 8 ASAA0240086 1 20020731 A 2422 528270047 INVERTER BOEING 737 7374Q8 138447Q NM E/E BAY FAULTY A ASAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 01 755AS 25096 SEA - DURING LINE MAINTENANCE IT WAS NOTICED THAT SMOKE WAS COMING FROM THE E/E BAY AREA. IT WAS FOUND THAT THE STATIC INVERTER HAD A COMBUSTION EVENT. CLEANED THE E3-1 RACK, REPLACED THE STATIC INVERTER, BATTERY CHARGER, BOTH TR'S, AND T HE MOISTURE SHROUD. REMOVED AND REINSTALLED SEVERAL OTHER COMPONENTS TO ALLOW THE CLEANING OF THE RACKS. OPS CHECKED AF FECTED SYSTEMS, ALL OPERATIONS WERE NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100800028 20021008 00028 NM 2002 10 8 ASAA0240089 1 20020811 A 2121 6454052 FAN BOEING 737 737490 1384715 NM RIGHT FAULTY A ASAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 01 768AS 27082 SEA - AT FLIGHT LEVEL 330, RAPID INCREASE IN ELECTRICAL BURNING SMELL FOLLOW WITH A HAZE IN THE CABIN. RIGHT CABIN AIR RECIRC FAN CIRCUIT BREAKER POPPED. SMELL AND HAZE DISSIPATED RAPIDLY ON DESCENT. REMOVED AND REPLACED RIGHT RECIRC FAN , OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100800029 20021008 00029 NM 2002 10 8 ASAA0240091 1 20020827 A 5320 655120329 FLANGE BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING C-CHECK, FOUND RIGHT EXHAUST LOUVERS, SUPPORT FLANGE CRACKED. BONDED SUPPORT FLANGE PER SRM. (M) 2 L 7 2 4F RT A16WE 2002100800030 20021008 00030 NM 2002 10 8 ASAA0240092 1 20020827 A 5315 65498854 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING C-CHECK, FOUND FLOORBEAM CORRODED AT STATION 986.5 AND LBL 29-41 CORRODED AROUND NUT PLATE HOLES. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002100800031 20021008 00031 NM 2002 10 8 ASAA0240093 1 20020827 A 5310 6552878102 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING C-CHECK, FOUND CREASE BEAM HAS SURFACE CORROSION AT STATION 540 TO 1016 L2 DOOR. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2002100800032 20021008 00032 NM 2002 10 8 ASAA0240094 1 20020829 A 5347 65C31483 SEAT TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING C-CHECK, FOUND SEAT TRACK CORROSION AT STATION 900 TO 915 AND WL 218. REPAIRED PER EA AND SRM. (M) 2 L 7 2 4F RT A16WE 2002100800033 20021008 00033 NM 2002 10 8 ASAA0240095 1 20020829 A 3397 8100022607 WIRE BOEING 737 737490 1384715 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 795AS 28890 PDX - TRACK LIGHTS INOPERATIVE AT ROWS 21-24. RECONNECTED WIRES, OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100800034 20021008 00034 NM 2002 10 8 ASAA0240096 1 20020831 A 5320 654795965 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING C-CHECK, FOUND STRAP AT BS 793.4 AND STRINGER 24R-26R CORRODED. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2002100800035 20021008 00035 NM 2002 10 8 ASAA0240097 1 20020831 A 5311 654795965 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING C-CHECK, FOUND Z-ANGLE FRAME AT BS 793R AND STRINGER 12R-20R CORRODED. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2002100800036 20021008 00036 NM 2002 10 8 ASAA0240098 1 20020905 A 3397 8100022607 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 782AS 25113 PDX - TRACK LIGHTS INOPERATIVE AT ROWS 18-20. RECONNECTED WIRES, OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100800037 20021008 00037 NM 2002 10 8 ASAA0240099 1 20020905 A 3397 8100022607 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 782AS 25113 PDX - AFT CABIN TWO RED TRACK LIGHTS INOPERATIVE. RECONNECTED WIRES, OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100800038 20021008 00038 NM 2002 10 8 ASAA0240100 1 20020905 A 3397 8100022607 WIRE BOEING 737 7374Q8 138447Q NM CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 768AS 25101 PDX - FOUND TRACK LIGHTS INOPERATIVE AT ROW 14-17. REPAIRED, WIRES OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100800039 20021008 00039 WP 2002 10 8 ASAA0280292 1 20020905 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 BUR - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT THE FIRST COUPLE OF ROWS. RE PAIRED WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100800040 20021008 00040 NM 2002 10 8 KPVA200222 1 20020901 A 3231 C54634E33C SEQUENCE VALVE DHAV DHC8 DHC8103 1386005 NM RT MLG DEFECTIVE A KPVA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 807WP 023 FLT 1146 - HNL - RIGHT MAIN GEAR DOOR LIGHT ON AFTER GEAR SELECTED UP AFTER TAKEOFF. REMOVED AND REPLACED ASSOCIATED GE AR DOOR SEQUENCING VALVE IAW DHC-8 MM 32-10-51 PAGES 201-202. FUNCTIONAL CHECK OF LANDING GEAR GOOD IAW DHC-8 MM 32-30- 00 PAGES 204-205 PARA A/B. AIRCRAFT RETURNED TO SERVICEABLE CONDITION. (M) 2 H 7 2 4T RT A13NM 2002100800041 20021008 00041 CE 2002 10 8 RU3A02006 1 20020910 A 7712 1013841863 INDICATOR BEECH 300 300BEECH 1152930 CE COCKPIT FALSE INDICATION A RU3A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 76 FF11 ON TAKEOFF ROLL AT 70KIAS, THE 1 TORQUE GAUGE JUMPED FROM 35 TO 120 WITH THROTTLES ALIGNED. RIGHT TORQUE DID NOT EXCEED 70 TAKEOFF ABORTED. REMOVED AND REPLACED NR 1 TORQUE INDICATOR. OPS CHECK SATISFACTORY. (M) 2 L 7 2 4T A24CE 2002100800042 20021008 00042 EU 2002 10 8 SIMA200210122 1 20020705 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B353 ABI - FOUND LEFT FUSELAGE HAS A DENT AFT OF ICESHIELD AREA, UPPER. PERFORMED EDDY CURRENT AND SONIC BOND CHECK IAW SAAB NDT MANUAL. NO DEFECTS WERE NOTED. DENT FOUND TO BE WITHIN SAAB 340 SRM 53-70-10 AND 51-10-10 LIMITS. (M) 2 L 7 2 4T RT A52EU 2002100800043 20021008 00043 SO 2002 10 8 SIMA200218411 1 20020701 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 651AE 145422 ABI - FOUND DENT ON FUSELAGE UNDER RIGHT ENGINE FRAME 65, 66, 57, STRINGER 14R. DENT WAS REPAIRED IAW EO NR EM-53MR-391 PART A. (M) 2 L 7 2 4T RT T00011AT 2002100800044 20021008 00044 EU 2002 10 8 SIMA200219131 1 20020705 A 5210 SKIN SAAB SF340 340B 7860101 EU PAX DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 ABI - PASSENGER DOOR HAS 23 DENTS. PERFORMED EDDY CURRENT AND SONIC BOND CHECK IAW SAAB NDT MANUAL. NO DEFECTS WERE FO UND. (M) 2 L 7 2 4T RT A52EU 2002100800045 20021008 00045 EU 2002 10 8 SIMA200224701 1 20020903 A 3350 3013000 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 540AM 540 MIA - MAINTENANCE REPORTED EMERGENCY POWER SUPPLY UNIT 61WL TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER S UPPLY UNIT 61WL IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002100800046 20021008 00046 GL 2002 10 8 SIMA200224703 2 20020901 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LEFT DAMAGED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 NM 01 634AE 145150 CAE311263 SDF - FLT 4072 - AFTER TAKEOFF FROM SDF, THE CREW HEARD A VERY LOUD 'EXPLOSION' FROM THE NR 1 ENGINE. THE CAPTAIN THEN SHUT THE ENGINE DOWN. THE CREW DECLARED EMERGENCY AND RETURNED THE AIRCRAFT SAFELY. UPON INITIAL INSPECTION BY CONTRAC T MAINTENANCE, IT APPEARS THAT THE BLEED SYSTEM ON THE ENGINE SEPARATED FROM THE ENGINE. REPLACED NR 1 ENGINE ASSY. (M ) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002100800047 20021008 00047 SO 2002 10 8 SIMA200224902 1 20020905 A 2150 8152043 ACM EMB 145 EMB145LR 3260212 SO A/C BAY MALFUNCTIONED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 623AE 145109 CLE - FLT 4204 - CREW REPORTED SMOKE IN THE CABIN, DECLARED EMERGENCY AND LANDED IN CLE WITHOUT INCIDENT. RAI RIGHT ACM IAW AMM 21-51-03. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT T00011AT 2002100800048 20021008 00048 SO 2002 10 8 SIMA200224904 1 20020905 A 2740 3094343 TRIM SWITCH EMB 135 EMB135LR 3260305 SO COCKPIT FAULTY A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 717AE 145272 PITCH TRIM 1 INOPERATIVE WARNING APPEARED ON EICAS USED STANDBY TRIM FOR REMAINDER OF THE FLIGHT. DECLARED EMERGENCY AN D RETURNED TO BOS. REMOVED AND REPLACED CAPTAIN YOKE PITCH TRIM SWITCH IAW EMB135 AMM 27-40-02-001-400-801-A, OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2002100800049 20021008 00049 SO 2002 10 8 SIMA200225401 1 20020905 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - DURING AN IMBV INSPECTION, MAINTENANCE FOUND THE CARGO DOOR LOWER CENTER SILL TO BE CORRODED BEYOND SRM LIMITS. M AINTENANCE REMOVED THE CORRODED SILL AND INSTALLED NEW CENTER SILL IAW EMB 145 SRM 145/1142, CHAPTER 51, REV 17, 51-40-0 2 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002100800050 20021008 00050 SO 2002 10 8 SIMA200225402 1 20020905 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - DURING AN IMBV INSPECTION A SCRATCH WAS DISCOVERED ON LEFT FUSELAGE FORWARD OF FRAME 26 AND BELOW STRINGER 18L. B LENDED OUT SCRATCH AND PERFORMED AN EDDY CURRENT INSPECTION AND THICKNESS INSPECTION. THICKNESS WAS DETERMINED TO BE BE LOW SRM LIMITS. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW EMB145 SRM 145/1142 REV 19 CHAPTER 53-22-01 FI G 201 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002100800051 20021008 00051 2002 10 8 SABA020098 4 20021003 A 3452 066107100 TRANSPONDER DHAV DHC8 DHC8102 2809003 NM A SABA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 33 882CC 168 Flight 5025 Aircraft 882 from CLT to TLH; After takeoff and during climb out , Pilot reported that he had lost number on e and two transponders. No emergency was declared. Aircraft returned to CLT and landed with no other problems. Maintenan ce removed and replaced both transponders and system ops checked good. Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002100800052 20021008 00052 SO 2002 10 8 SIMA200225403 1 20020909 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - DURING AN IMBV INSPECTION, MAINTENANCE FOUND AN AREA OF THE FORWARD DIGITAL CORRODED. BLENDED CORRODED AREA. FAB RICATED A DOUBLER AND INSTALLED IAW EMB GST-2721.02 PARA 1 DATED SEP 5, 2002 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002100800053 20021008 00053 EU 2002 10 8 SIMA200225404 1 20020905 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 370AM 340B370 ABI - DURING AN MBV INSPECTION, THE FRAME AT STATION 258 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. CUT OUT CORRODED A REA OF FRAME AT STATION 258. FABRICATED A FILLER, DOUBLER AND TRIPLER. REPAIR DONE IAW SAAB 340 SRM CHAPTER 53-70-30. (M) 2 L 7 2 4T RT A52EU 2002100800054 20021008 00054 EU 2002 10 8 SIMA200225405 1 20020905 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 370AM 340B370 DURING AN MBV INSPECTION, THE FRAME AT STATION 236.5 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. CUT OUT CORRODED AREA OF FRAME AT STATION 236.5. FABRICATED A FILLER, SHIMS AND DOUBLER. REPAIR DONE IAW SAAB 340 SRM CHAPTER 53-70-30. (M) 2 L 7 2 4T RT A52EU 2002100800055 20021008 00055 SO 2002 10 8 SIMA200225407 1 20020905 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 ABI - DURING AN IMBV INSPECTION, A DENT WAS DISCOVERED BETWEEN FRAMES 68 AND 70 AND BETWEEN STRINGERS 19L AND 20L. AFTE R RECONTOURING PER EMB GST-2624/02 FOUND SKIN TO BE OIL CANNED. PERFORMED EDDY CURRENT INSPECTION OF THE REWORKED AREA WITH NO DEFECTS NOTED. FABRICATED A REPAIR 'L' ANGLE. REPAIR DONE IAW EMB GST-2666/02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002100800056 20021008 00056 NM 2002 10 8 USAA020345 1 20020824 A 5320 ANGLE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 46845 23232 PIT - FOUND ANGLE CORRODED, .5 INCH BY .5 INCH THREE AREAS AROUND AREAS, ANGLE STATION 500D FROM LBL 21.8 TO RBL 3.0. R EPLACED 'L' ANGLE PER 51-40-01. (M) 2 L 7 2 4F RT A16WE 2002100800057 20021008 00057 NM 2002 10 8 USAA020346 1 20020814 A 5320 CLIP BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 23232 PIT - FOUND SKIN CLIP CORRODED 6 INCHES BY 1 INCH, STATION 285.75 STRINGER 26R TO NOSE WHEEL WHEEL. REMOVED CORROSION P ER 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002100800058 20021008 00058 NM 2002 10 8 USAA020347 1 20020825 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 46845 23232 PIT - FOUND SKIN CRACKED, .2 INCH STATION 380 LBL 2.90 INCH. REPAIRED PER EO 5300V258, EA 68269A, T/R 53-30-07. (M) 2 L 7 2 4F RT A16WE 2002100800059 20021008 00059 EU 2002 10 8 USAASA02075 1 20020828 A 3350 LIGHT AIRBUS 320 A320214 3930316 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 108UW 1061 DCA - THE EMERGENCY LIGHTS SYSTEM TEST FAILED. MAINTENANCE RELAMPED THE ESCAPE HATCH LIGHTS. SYSTEM CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2002100800060 20021008 00060 EU 2002 10 8 USAASA02077 1 20020908 A 3150 9615325040 COMPUTER AIRBUS A319 A319112 3930323 EU E/E BAY FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 708UW 0972 GCM - FLT 1093 - EN ROUTE GCM-CLT, AFTER TAKEOFF, RECEIVED AN 'AVNCS SMOKE' MESSAGE ON THE ELECTRONIC CENTRALIZED AIRCRA FT MONITORING SYSTEM. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE DISPLAY M ANAGEMENT COMPUTER IN THE NR 3 POSITION. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002100800061 20021008 00061 NM 2002 10 8 UPS02439311 1 20020813 A 5320 INTERCOSTAL BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D - BS 1220 LBL 112 BELOW FLOOR, INTERCOSTAL WEB FOUND CRACKED. M/D - BS 1220 LBL 112 BELOW FLOOR I NTERCOSTAL WEB CRACK STOP DRILLED AND REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002100800062 20021008 00062 NM 2002 10 8 UPS02439314 1 20020812 A 5210 DOUBLER BOEING 747 747123 1384873 NM R1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D R1 DOOR LOWER HINGE SKIN DOUBLER FOUND CRACKED. SKIN REPAIRED AS PER SB 747-52-2144 FIG 4. 2 L 7 4 4F A20WE 2002100800063 20021008 00063 NM 2002 10 8 UPS02439315 1 20020812 A 5210 DOUBLER BOEING 747 747123 1384873 NM L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D L1 DOOR UPPER HINGE SKIN DOUBLER FOUND CRACKED. DOOR SKIN REPAIRED AS PER SB B747-52-2144 FIG 3. 2 L 7 4 4F A20WE 2002100800064 20021008 00064 NM 2002 10 8 UPS02439317 1 20020813 A 5320 69B107713 TIE CLIP BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 320 S-13AL TIE CLIP FOUND CRACKED. CLIP REPLACED AS PER SRM 51-10-01 PG. 8. 2 L 7 4 4F A20WE 2002100800065 20021008 00065 NM 2002 10 8 UPS02439319 1 20020822 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D - BS 1000 - 1020 LBL 97 SEAT TRACK FLANGE FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMIT 53-10-01. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 34. 2 L 7 4 4F A20WE 2002100800066 20021008 00066 WP 2002 10 8 UPS02839249 1 20020730 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 LEFT WING CENTER L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 366.5. REMOVED CORROSION AND FOUN D TO BE OUT OF LIMITS IAW SRM 57-2-0 FIG 7, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2- 1 FIG 38. 2 L 7 4 4F RT 4A25 2002100800067 20021008 00067 WP 2002 10 8 UPS02839251 1 20020731 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 R2 DOOR UPPER AFT CORNER SKIN IS CRACKED AT STA 1660 AT LONG 11R. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW SRM 53-2-0 FIG 16. 2 L 7 4 4F RT 4A25 2002100800069 20021008 00069 WP 2002 10 8 UPS02839254 1 20020801 A 5320 47731461 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 STA 1660 FRAME TO CUSP FITTING IS CORRODED BEYOND LIMITS ABOVE LONG 21R. REMOVED, FABRICATED, AND RE PLACED FITTING IAW DWG 4773161, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002100800070 20021008 00070 WP 2002 10 8 UPS02839256 1 20020801 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 11. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRAC KS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FREEZE PLUGS IAW SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 2002100800071 20021008 00071 WP 2002 10 8 UPS02839257 1 20020801 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 9. CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT C UTOUT, FABRICATED AND INSTALLED FREEZE PLUG AND DOUBLER IAW SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 2002100800072 20021008 00072 NM 2002 10 8 UPS02439355 1 20020813 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D - BS 360 S23R FRAME FOUND CRACKED. M/D BS 360 S23R FRAME REPAIR CARRIED OUT AS PER HX RS NR R53-1 2-34879 AND UPS EO B747-5310-17492-A. 2 L 7 4 4F A20WE 2002100800073 20021008 00073 NM 2002 10 8 UPS02439365 1 20020815 A 5313 65B1525459 LONGERON BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT LG W/W O/B, OVERWING LONGERON BETWEEN BS 1436 AND 1446 I/B LWR SURFACE CORRODED AS MARKED. LONGERO N FOUND CORRODED AT LOCATION BS 1436 TO 1445 LBL L118 TO L122 CORROSION BLEND OUT EXCEEDEDS SRM LIMIT REPLACED AS PER SR M 51-10-01. HX RSRS NR R53-43-34882, UPS EO 747-53-20104. 2 L 7 4 4F A20WE 2002100800074 20021008 00074 NM 2002 10 8 UPS02439367 1 20020816 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C RH LG W/W BS 1241 CANTED BULKHEAD FOUND CORROSION AT RBL 75-77 WL 166-167. BULKHEAD FOUND CORRODED AT LOCATION BS 1241 TO 1241 WL 166 TO 167, RBL R75 TO R77. CORROSION BLEND OUT EXCEEDS SRM LIMIT. BULKHEAD REPLACED AS P ER SRM 51-10-01 HX RS NR R53-48-34885. UPS EO NR 747-53-20101. 2 L 7 4 4F A20WE 2002100800075 20021008 00075 NM 2002 10 8 UPS02439368 1 20020820 A 5330 65B150185 SKIN BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT LG W/W STA 1355 S33L OVERWING LONGERON UPPER FUSELAGE SKIN FOUND CORROSION. SKIN FOUND CORRODED AT LOCATION BS 1355 TO 1355, STR L33 TO L33. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SKIN REPLACED AS PER SRM 51-10-01. HX RS NR R53-41-34892, UPS EO NR M5100-2780-E. 2 L 7 4 4F A20WE 2002100800076 20021008 00076 NM 2002 10 8 AWXA200200988 1 20020930 A 5330 655298881 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 0 0 25400 MCN - MAJOR REPAIR - DURING C-12 CHECK A 7/16" CRACK WAS FOUND ON EXTERNAL FUSELAGE SKIN OF L-2 DOOR UPPER HINGE CUTOUT, BS 947.5. MAINTENANCE CUTOUT DAMAGED SECTION OF SKIN AT L-2 DOOR UPPER HINGE CUTOUT BS 947.5, AND PERFORMED A HFEC INSP ECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR PLATE (DOUBLER) AND A FILLER, AND INSTALLED REPAIR PARTS IAW B737- 300 SRM 53-60-01, PG. 210-212, FIG. 205. 2 L 7 2 4F RT A16WE 2002100800077 20021008 00077 NM 2002 10 8 2002UALA01530 1 20021002 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE UNRELIABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 193UA 26890 FLIGHT ATTENDANT REPORTED LH SIDE OF FIRST CLASS AND DOOR 1L EMERGENCY LIGHTS FLASHED ON AND OFF DURING THE ENTIRE FLIGH T, UPON LANDING AND TAXI TO GATE. BATTERY CHARGER-POWER SUPPLY AND BATTERY AT DOOR 1L. 2 L 7 4 4F 4 F RT A20WE E24NE 2002100800078 20021008 00078 NM 2002 10 8 2002UALA01533 1 20021003 A 5313 STRINGER CLIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 STA. 1480, STRINGER 27L ATTACHMENT CLIP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. STRINGER CLIP WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101000080 20021010 00080 NM 2002 10 10 F3LA200200316 1 20021004 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED LT FUSELAGE FORMER AT FWD OTBD CORNER OF OUTER AIR CONDITIONING DUCT BAY DOOR CRAC KED APPROXIMATELY 4 INCHES. DRILLED AND INSTALLED REPLACEMENT TEE CHORD PER SRM 51-40-02 AND 51-10-2. 2 L 7 2 4F RT A16WE 2002100800079 20021008 00079 NM 2002 10 8 UPS02439253 1 20020829 A 3350 BATTERY PACK BOEING 747 747200 1384847 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 528UP 1 INSPECTION TYPE:PFLT 2 EA CREW SERVICE DOOR SLIDE EMERGENCY LIGHT INOP, ACCESS PANEL FOR X327 BATTERY PACK ABOVE DOOR RE MOVED FOR ACCESS. REMOVED POWER PACK ASSEMBLY. REINSTALLED BATTERY PACK AND X327 BATTERY ACCESS PANEL. DEFERRED LIGHT S INOP PER MEL 33-13. 2 L 7 4 4F RT A20WE 2002101000081 20021010 00081 NM 2002 10 10 F3LA200200317 1 20021004 A 5320 CHANNEL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED FLOOR SUPPORT CHANNEL CORRODED AT BBL 8.1 BETWEEN BS 867 AND 847. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-53, 55-00-53, 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002100800080 20021008 00080 NM 2002 10 8 F3LA200200318 1 20021004 A 5320 INTERCOSTAL BOEING 737 7373Q8 1384670 NM BS 951 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED CORROSION AROUND FLOORBOARD HOLES ON INTERCOSTAL AT BS 951, RBL 27 TO RBL 50. 2 L 7 2 4F RT A16WE 2002101000082 20021010 00082 NM 2002 10 10 F3LA200200319 1 20021004 A 5320 65C333672 INTERCOSTAL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON INTERCOSTAL AT BS 947.5 TO BS 967, RBL 50. REM OVED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002100900001 20021009 00001 EU 2002 10 9 CA020826009 1 20020811 A 6720 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE T/R SPIDER LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ASSEMBLY REMOVED FROM A/C DUE TO LOSS OF TORQUE ON NUT AND SUBSEQUENT MISALIGNMENT OF INDEX MARK. A VISUAL INSPEC TION UPON RECEIPT CONFIRMED THAT BOTH LOCKING FEATURES FOR THE NUT WERE IN PLACE. PRIOR TO DISASSEMBLY, A TIGHTENING T ORQUE WAS APPLIED TO THE NUT. THE NUT ROTATED APPROXIMATELY 10 DEG. PRIOR TO OBTAINING THE MINIMUM TORQUE LOADING OF 9 .5 M. DAN. TORQUE LOADING THE NUT TO THE MAXIMUM OF 12.0 M.DAN, ROTATED THE NUT BY FURTHER 5 DEG. 1 G 7 1 3U 3 U NC H9EU E19EU 2002100900002 20021009 00002 EA 2002 10 9 CA020828011 2 20020809 A 7320 CONTROL ARM BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA HARTZL HCD4N3 HCD4N3A GL FUEL CONTROL OBSTRUCTED W E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION AP APPROACH 1 CA (CAN) ON APPROACH, PILOT BROUGHT BACK POWER LEVERS, NR 2 ENG REACTED NORMALLY, THE NR 1 ENG INCREASED. THE PILOT MOVED THE NR 1 ENG POWER LEVER FWD AND ENG WENT BACK TO WHAT THEY HAD BEEN BEFORE APPROACH. NR 1 POWER LEVER MOVED SEVERAL TIMES, EACH TIME THE ENGINE REACTED THE SAME, ENG WAS FEATHERED AND SHUTDOWN. AFTER LANDING, AIRCRAFT WAS TOWED OFF THE RUNWAY DUE TO PILOT COULDN`T MAINTAIN PROPER STEERAGE. THE STARTER GEN TERMINAL BLOCK COVER HAD COME OFF AND HAD FA LLEN ONTO THE ENG CONTROL LINKAGE AND LANDED IN SUCH A WAY THAT WHEN THE POWER LEVER WAS BROUGHT BACK, IT FORCED THE FCU CONTROL ARM FWD INCREASING POWER. THE TERMINAL BLOCK COVER WAS REMOVED AND AN ENGINE RUN-UP, OPS WERE NORMAL. 1 L 7 2 4T 4 T A24CE E4EA 5 C STC 2002100900003 20021009 00003 EU 2002 10 9 CA020904003 1 20020827 A 2913 704A33690004 BELT SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE HYD SYSTEM SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) HYDRAULIC BELT SEPARATED AT SPLICE. 1 G 7 1 3U 3 U H9EU E00054EN 2002100900004 20021009 00004 EU 2002 10 9 CA020904006 1 20021001 A 2741 9787314203 ACTUATOR PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL PITCH TRIM SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING HORIZONTAL STAB PITCH TRIM TEST/INSPECTION MAINTENANCE FOUND THAT PITCH TRIM ACTUATOR WOULD NOT MOVE IN ALT ERNATE TRIM MODE. ACTUATOR WOULD LOAD UP BUT NOT MOVE. AIRCRAFT GROUNDED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002100900005 20021009 00005 NE 2002 10 9 CA020906004 2 20020903 A 7230 COMPRESSOR BOEING 767 767333 1385301 NM PWA 4060 PW4060 52119 NE LT ENGINE DAMAGED W K NONE P NO WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) AFTER LANDING, SPARKS NOTICED COMING OUT BY LT ENGINE TAIL PIPE. ALL PARAMETERS NORMAL, METAL DEBRIS IN TAIL CON E. BOROSCOPE FOUND EXCESSIVE COMPRESSOR DAMAGE. ENGINE REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002100900007 20021009 00007 NM 2002 10 9 CA020909002 1 20020904 A 2932 7G772 PRESSURE SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) AIRCRAFT TURNED BACK DUE TO NR 2 RUDDER HYDRAULIC CAUTION LIGHT CAME ON IN FLIGHT. NR 2 SYSTEM RUDDER HYDRAULIC PRESSURE SWITCH WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002100900008 20021009 00008 NM 2002 10 9 CA020909003 1 20020830 A 5330 SKIN BOEING 727 72725C 138400H NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 66295 (CAN) ON HEAVY C-CHECK, CRACKS NOTED AROUND FASTENER HOLE AT BS 488, STR 3 LT, IN FUSELAGE SKIN. 2 L 7 3 4F 4 F A3WE E2EA 2002100900009 20021009 00009 NM 2002 10 9 CA020909004 1 20020830 A 5330 SKIN BOEING 727 72725C 138400H NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 66295 (CAN) ON HEAVY C-CHECK, FIVE CRACKS NOTED AROUND FASTENER HOLES AT BS 610-614, STR 3 LT, IN FUSELAGE SKIN. 2 L 7 3 4F 4 F A3WE E2EA 2002100900010 20021009 00010 EA 2002 10 9 CA020910002 1 20020908 A 5610 NP1393221 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) LT SIDE WINDOW CRACKED. DIVERTED FLIGHT, LT WINDOW REPLACED AS PER AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002100900011 20021009 00011 NM 2002 10 9 CA020910005 1 20020907 A 2910 82950010335 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM CRACKED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA 29397 29397 (CAN) CREW REPORTED COMPLETE LOSS OF NR 2 HYDRAULIC SYSTEM AFTER SELECTING GEAR DOWN ON APPROACH. AIRCRAFT LANDED WITHO UT INCIDENT . INSPECTION FOUND NR 2 HYD SYTEM LOSS OF FLUID, LT OUTBOARD ROLL SPOILER RETURN LINE CRACKED & LEAKING. TE MP LINE INSTALLED, ENGINE DRIVEN PUMP & FILTERS REPLACED & LEAK CHECKED, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002100900012 20021009 00012 EU 2002 10 9 CA020910006 1 20020829 A 3213 5321012167 LINK PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL MLG CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE WORN TRAILING LINK BUSHINGS WERE SCHEDULED TO BE REPLACED DURING THE ANNUAL INSPECTION. UPON REMOVING THE BUSH INGS FROM THE RT TRAILING LINK, SEVERAL SPOTS OF CORRORSION WERE DISCOVERED IN THE MAIN BUSHING BORE. TECH REP. DIRECTED A CHANGE OUT OF DEFECTIVE PART. THE RT MLG WAS REPLACED AS A UNIT. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002100900014 20021009 00014 WP 2002 10 9 CA020910008 1 20020906 A 6210 BLADE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING 100 HOUR INSPECTION, ENGINEER FOUND BLADE CRACKED JUST OUT BOARD OF THE ROOT FITTING. BLADE WAS REMOVED AN D REPLACED WITH NEW UNIT. 1 G 7 1 3U 3 U H3WE E4CE 2002100900015 20021009 00015 WP 2002 10 9 CA020911001 2 20020909 A 7321 89778018 FUEL CONTROL MTSBSI MU2 MU2B60 5780460 CE GARRTT TPE331 TPE33110 01514 WP RT ENGINE LEAKING W A UNSCHED LANDING R F PARTIAL RPM/PWR LOSS FLT CONT AFFECTED CL CLIMB 1 CA (CAN) AFTER TAKEOFF THE TORQUE ON THE RT ENGINE DROPPED APPROXIMATELY 10 PERCENT. PILOT ADVANCED THE THROTTLE TO COMPEN SATE. WHEN THE TORQUE DROPPED AGAIN THE PILOT ADVANCED THE THROTTLE AGAIN THEN DECIDED TO RETARD THE THROTTLES AND COME BACK TO LAND. MAINTENANCE COMPLETED THE PS3 ROLLING DIAPHRAGM TEST AND FOUND THE FCU LEAKING. THE FUEL CONTROL WAS REPL ACED AND CHECKED OK. 1 H 7 2 3T 4 T RT A10SW E4WE 2002100900016 20021009 00016 NM 2002 10 9 0203396638 1 20020917 A 5315 SEAT TRACK BOEING 747 747251B 1384892 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 638US 23549 During "L" check found corrosion on seat track at BS 492 LBL 35. Repaired per EA 66-192645. 2 L 7 4 4F A20WE 2002100900017 20021009 00017 EU 2002 10 9 CA020911002 1 20020903 A 6220 358947P BUSHING AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20F 03013 GL STARFLEX DEBONDED W K NONE O OTHER IN INSP/MAINT 1 CA M4666 (CAN) ON A DAILY INSPECTION ONE BUSHING WAS FOUND TO BE DEBONDED. THE RETAINING BOLT WAS COMPLETELY PULED OUT OF THE ST ARFLEX. PILOT REPORTED NO ABNORMAL VIBRATION. STARFLEX ASSEMBLY REPLACED BEFORE NEXT FLIGHT. 1 G 7 2 3U 3 U H11EU E4CE 2002100900018 20021009 00018 WP 2002 10 9 CA020912001 1 20020903 A 2197 WIRE HARNESS LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE NR 2 PACK CHAFED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) NR 2 PACK RAM AIR LOUVER WILL NOT POSITION PROPERLY ON GROUND, IN FLIGHT IT STAYS AT ONE O`CLOCK POSITION. C/B T RIPPED WHEN PACK NR 2 IS OPERATED IN MANUAL. NR 2 PACK CONTROLLER INOP IN AUTO AND MANUAL. FOUND NO CONTINUITY BETWEE N RAM AIR ACTUATOR LOUVERS NR 2. CONNECTOR 2162-P6 PIN 1,2,3 TO RAM AIR INLET RELAY. FOUND NR 2 HEAT EXCHANGER AT 4 FT FROM NR 2 RAM AIR ACTUATOR CONNECTOR HAD A TOTAL OF 7 WIRE INSULATORS DAMAGED TO CENTRAL CONDUCTOR, WHEN POWER WAS APP LIED, ELECTRICAL ARCING WAS PRODUCED BETWEEN THOSE WIRES CAUSING C/B TO TRIP. 2 L 7 3 4F 4 F A23WE E12EU 2002100900019 20021009 00019 WP 2002 10 9 CA020912002 1 20020824 A 4997 WIRE HARNESS LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE APU DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) APU FAILS TO START, NO ROTATION. AIRCRAFT RELEASED PER MEL 49-00-01. BLEED AIR VALVE CONFIRMED CLOSED. CHECKED CURRENT LIMITER AND FOUND SERVICEABLE. RERACKED ECU, NO FIX. AIRCRAFT REQUIRED TO HAVE A JET START AND GPU AT ALL STATIO NS. FURTHER TROUBLE SHOOTING REVEALED A DAMAGED TERMINAL LUG ON STATER HARNESS, MOST PROBABLY DUE TO THE FACT THAT THE NUTS SECURING THE TERMINAL BECAME LOOSE AND CREATED AN OVERHEAT AT THAT POINT. APU STARTER HARNESS ASSY WAS REPLACED A ND APU OPERATIONAL CHECK CARRIED OUT PER AMM 49-41-04. 2 L 7 3 4F 4 F A23WE E12EU 2002100900020 20021009 00020 EU 2002 10 9 CA020912003 1 20020908 A 3310 F15T12WW LIGHT AIRBUS 310 A310300 3930305 EU L1 DOOR BURNED OUT W O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) TEMPORARY SMOKE ODOR DURING CLIMB OUT. ONE GALLEY LIGHT BURNED OUT AT THE SAME TIME. NO ECAM WARNING. MAINTENA NCE REPLACED THE GALLEY LIGHTS AT L1 DOOR AND CHECKED SERVICEABLE PER THE AMM 33-24-11. NO SIGNS OF OVERHEAT DAMAGE ON BALLASTS. 2 L 7 2 4F RT A35EU 2002100900021 20021009 00021 WP 2002 10 9 CA020912004 1 20020907 A 7830 LJ37013 BLOCKER DOOR LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE THRUST REVERSER BENT W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ENGINE NR 3, BLOCKER DOOR AT 5 O`CLOCK POSITION BENT ACROSS ITS WIDTH. MAINTENANCE REPLACED THE BLOCKER DOOR PER AMM 78-31-16 2 L 7 3 4F 4 F A23WE E12EU 2002100900022 20021009 00022 EA 2002 10 9 CA020912005 1 20020906 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W O OTHER O OTHER AP APPROACH 1 CA (CAN) DURING APPROACH, LT SIDE WINDOW CRACKED. LT SIDE WINDOW REPLACED IN ACCORDANCE WITH AMM 2 L 7 2 4F 4 F RT A21EA E15NE 2002100900023 20021009 00023 GL 2002 10 9 CA020912006 3 20020814 A 6111 1977 CLAMP GRUMAV G21 G21A 3951204 SO PWA R985 R985AN14B 52008 NE HARTZL HCB3R HCB3R302 GL PROPELLER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PROPELLER EXPERIENCED VIBRATIONS, WENT IN FOR SCHEDULED MAINTENANCE, CRACKED CLAMP WAS FOUND. ALSO BLADES HAD SLI PPED IN CLAMPS. PROPELLER WAS SENT IN FOR OVERHAUL AND REPAIR. 1 H 7 2 3R 3 R TC654 5E1 5 C P28EA 2002100900024 20021009 00024 CE 2002 10 9 CA020912007 1 20020829 A 3233 50810354 PIN BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA HARTZL HCB4T HCB4TN3 GL DOWNLOCK GUIDE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING SCHEDULED MAINTENANCE OF THE LANDING GEAR ACTUATOR THE DOWNLOCK GUIDE PIN WAS REMOVED FOR ACCESS AND NOTICE D IT WAS BENT, CRACKED AND EXCESSIVELY WORN. 1 L 7 2 3T 4 T A14CE E4EA 6 C P40EA 2002100900025 20021009 00025 SW 2002 10 9 CA020912008 1 20020829 A 2821 FUEL FILTER BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FUEL PUMP FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING START N1 SURGED THEN OPERATED NORMALLY. AIRFRAME FUEL FILTER, ENGINE DRIVE FUEL FILTER, HIGH PRESSURE FUEL FILTER, INLET SCREEN CHANGED OR CLEANED. SOME DEBRIS FOUND IN AIRFRAME AND ENGINE DRIVEN FUEL PUMP. 1 G 7 1 3U 3 U H2SW E4CE 2002100900026 20021009 00026 NM 2002 10 9 CA020912011 1 20020830 A 5711 SPAR BOEING 727 72725C 138400H NM PWA JT8 JT8D7 52053 NE RT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) RT WING REAR SPAR CRACKED AT STA 200. 2 L 7 3 4F 4 F A3WE E2EA 2002100900027 20021009 00027 NM 2002 10 9 DHL2002755006 1 20021007 A 3350 1000679 LIGHT BOEING 727 727225 1384077 NM A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 755DH 21857 1) COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE.2) REMOVED AND REPLACED LIGHT ASSEMBLY. OPS GOOD IAW M/M 33-50-01. 2 L 7 3 4F A3WE 2002100900028 20021009 00028 NM 2002 10 9 DHL2002740005 1 20021008 A 3350 1000677 LIGHT BOEING 727 7272Q9 138448M NM A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 740DH 21930 1) EMERGENCY EXIT LIGHT OVER MAIN ENTRANCE DOOR FOUND INOPERATIVE DURING PREFLIGHT.2) REMOVED AND REPLACED EXIT LIGHT BATTERIES IAW BMM CHAPTER 33-50-71, NO HELP, REMOVED AND REPLACED EXIT LIGHT ASSEMBLY IAW BMM REF. 33-50-71, OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 2002101000084 20021010 00084 NM 2002 10 10 F3LA200200321 1 20021004 A 5320 SILL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED REAR GALLEY R2 MOP SILL CORRODED. REPLACED MOP SILL PER SRM 53-60-51 AND 51-40-02 . 2 L 7 2 4F RT A16WE 2002102800222 20021028 00222 CE 2002 10 28 GLBA2002153 1 20020924 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE RT MLG FAILED A GLBA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 03 261GL 8745 2743 UE261 GEAR WARNING RT SIDE AFTER LANDING, R&R MLG ACTUATOR. 2 L 7 2 4T RT A24CE 2002100900029 20021009 00029 NM 2002 10 9 SABA020100 1 20021006 A 2400 4011769 BATTERY DHAV DHC8 DHC8103 1386005 NM A SABA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 33 883CC 162 Aircraft 883 flight 5082 from CVG to CLT; During cruse flight the battery over-temp light illuminated. Aircraft diverted into Lexington and landed with no other problem. No emergency was declared. Maintenance from Charlotte removed and repl aced the main battery. System ops checked good and aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002101000086 20021010 00086 NM 2002 10 10 F3LA200200323 1 20021004 A 5347 CARGO TRACK BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR STRINGER CORRODED AT SCREW HOLES FROM BS 847 TO BS 787 , RBL 16. REPLACED STRINGER TIE DOWN TRACK PER SRM 57-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002101000085 20021010 00085 NM 2002 10 10 F3LA200200322 1 20021004 A 5313 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR STRINGER CORRODED AT BS 771, RBL 28. FABRICATED AND I NSTALLED REPLACEMENT PARTS PER SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002100900030 20021009 00030 NM 2002 10 9 ZW0A0210402 1 20021008 A 5210 80330035 RESERVOIR BOEING 757 757231 1384950 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 720TW 30319 THE RIGHT SIDE NUMBER 2 CABIN DOOR ASSIST BOTTLE PRESSURE WAS AT ZERO. REPLACED THE DOOR ASSIST BOTTLE. CHECK-C 1-26-0 1 LAX. --CLOSED-- 2 L 7 2 4F RT A2NM 2002101000087 20021010 00087 NM 2002 10 10 F3LA200200324 1 20021004 A 5347 CARGO TRACK BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR STRINGER CORRODED AT BS 771, RBL 14. REPLACED FLOOR S TRINGER TIE DOWN TRACK PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2002100900031 20021009 00031 NE 2002 10 9 CA020913002 2 20020815 A 7260 4002T00G013 BEARING CARSON S61 S61LSKRSKY EA GE CT58 CT581401 30011 NE ACCESSORY G/B WORN W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) BEARINGS IN ACC DRIVE & AGB WERE NEW AT OVERHAUL. ENG RUN IN TEST CELL FOR 4 HOURS. IN A/C FOR 0.2 HRS. AFTER TES T CELL RUN, CHIP DETECTORS INSPECTED, NORMAL. ACC DRIVE UNIT REMOVED & BEVEL GEAR BEARINGS WORN. AGB REMOVED. REMOVED PINION GEAR HOUSING, PINION GEAR BEARINGS WORN, CHIPS FROM PINION GEAR. AGB, ACC DRIVE & ACC DRIVESHAFT REPLACED. ENG LUBE PUMP, AUX SUMP, FUEL/OIL COOLER, ENG OIL TANK & LINES REMOVED & INSPECTED FOR CONTAMINATION. NONE FOUND. ITEMS F LUSHED PRIOR TO INSTALL. A/C DEPARTED ON 2 HOUR FLT, APPROX 25 MIN INTO FLT, CHIP DETECTOR ILLUMINATED, A/C RETURNED TO BASE. PLUGS & FILTER REMOVED & CONTAMINATION FOUND. SYS FLUSHED & A/C FLOWN APPROX 60 FLT HOURS WITHOUT INCIDENT. 2 G 7 2 4U 4 U H8EA 1E3 2002100900032 20021009 00032 SO 2002 10 9 SWIA200211237 1 20020917 A 5312 BULKHEAD EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 299SW 120329 APU BULKHEAD CRACKED BY BIG CANNON PLUG. DISCOVERED DURING A-CHECK INSPECTION. INSTALLED SERVICEABLE DOUBLER AT APU BU LKHEAD IAW SRM. NO OTHER DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2002100900033 20021009 00033 EA 2002 10 9 SWIA200211238 1 20020912 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM BROKEN A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 405SW 7029 RUDDER TRIM WILL MOVE LEFT, BUT NOT RIGHT. SOLDERED BROKEN TERMINAL/WIRE CONTACT ON RUDDER TRIM CONTROL KNOB. OPS CHEC K GOOD. 2 L 7 2 4F RT A21EA 2002100900034 20021009 00034 NE 2002 10 9 CA020913003 1 20020825 A 6320 HOUSING SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE M/R GEARBOX WORN W A UNSCHED LANDING Y ENGINE STOPPAGE HO HOVERING 1 CA (CAN) INPUTS HAVE SIGNS OF METAL TRANSFER IN FROM THE ROLLERS TO THE GEAR HOUSING BORE, ON THE RT HOUSING THE ROLLER PAT H IS BREAKING UP. OIL-LITE WASHERS ARE WORN, DEBRIS WAS IN OIL FOUND IN AND AROUND THE ROLLER AREA. LT INPUT THE UPPER OIL-LIGHT WAS REMOVED BROKEN. OTHER CRACKS WERE FOUND IN THAT OIL-LIGHT WASHER. LT INPUT FREEWHEEL UNIT SLIPPED DURING FLIGHT. CAUSE OF SLIP IS PRESENTLY UNDER INVESTIGATION. 2 G 7 2 4U 4 U 1H15 1E3 2002100900035 20021009 00035 SO 2002 10 9 SWIA200211239 1 20020918 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 270YV 120270 ''TAKEOFF TRIM'' AURAL WARNING IN ALL SETTINGS. CYCLED AURAL WARNING CIRCUIT BREAKER. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002100900036 20021009 00036 2002 10 9 CA020913004 4 20020820 A 3457 000013911 GPS CESSNA 172 172M 2072418 CE LYC O320 O320D2G 41508 EA COCKPIT FAILED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA (CAN) DURING CRUISE PHASE OF, GPS-430 NEW INSTALLATION, TEST FLIGHT, UNIT BECAME UNRESPONSIVE WHEN ENTER BUTTON PUSHE D. THE UNIT (GNS-430) AT THAT POINT WOULD NOT CHANGE PAGES. AIRCRAFT LANDED WITH NO FURTHER PROBLEMS. 1 H 7 1 3O 3 O NT 3A12 E274 2002100900037 20021009 00037 EA 2002 10 9 SWIA200211240 1 20020920 A 2740 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 910SW 7566 AFTER RUNNING A GOOD STAB & MACH TRIM TEST, STAB CH 1 DROPPED OFF LINE FOR NO APPARENT REASON AND WOULD NOT REENGAGE. P OWERED DOWN A/C AND POWERED UP. NO DEFECTS NOTED AT THIS TIME. REPLACED CAPT'S TRIM SWITCH DUE TO PREVIOUS DISCREPANC IES. HSTC SYSTEM OPERATIONAL CHECKS GOOD IAW AMM 27-41-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2002100900038 20021009 00038 CE 2002 10 9 CA020913005 1 20020906 A 1400 6147514435 WASHER BEECH 90 E90 1152914 CE PWA PT6 PT6A28 EA WING ATTACH MISMANUFACTURED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) SPECIAL 7/8 INCH DIAMETER PRELOAD INDICATING WASHER ASSY USED ON LOWER FORWARD WING ATTACH BOLTS INDICATED PROPER TORQUE PREMATURELY. ESTIMATE NORMAL TORQUE TO BE AT LEAST 300 FT LBS AND SUSPECT WASHER ASSEMBLY INIDCATED TORQUE AT AP PROX 100 FT LBS. 1 L 7 2 3T 4 T 3A20 E4EA 2002100900040 20021009 00040 SO 2002 10 9 SWIA200211242 1 20020920 A 3150 80055711 CONTROL UNIT EMB 120 EMB120ER 3260203 SO WARNING SYSTEM MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 251YV 6549 6549 120251 TO AURAL WARNING WITH TRIM IN GREEN. ABORTED TAKE OFF REMOVED AND REPLACED AURAL WARNING UNIT. OPS CHECKS GOOD ON GROU ND. 2 L 7 2 4T RT A31SO 2002100900041 20021009 00041 GL 2002 10 9 CA020913007 2 20020905 A 7323 CLIP BENDIX ALAA1 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL DRIVE GEAR DEBONDED W O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 4752 (CAN) THE EXPOXY HOLDING THE SAFETY CLIP IN PLACE BECAME UNBONDED ALLOWING THE CLIP TO MOVE AND ALLOWING THE DRIVE GEAR TO DISCONNECT FROM THE SHAFT. 1 G 7 1 3U 3 U H2SW E4CE 2002100900042 20021009 00042 SO 2002 10 9 SWIA200211243 1 20020919 A 2121 EVAC2322C2 BLOWER EMB 120 EMB120ER 3260203 SO A/C BAY FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 563SW 4553 4553 120338 RIGHT PACK FAIL ON THE GROUND. SMALL AMOUNT OF SMOKE IN CABIN. INSTALLED SERVICEABLE GROUND COOLING FAN ON RIGHT PACK. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002100900043 20021009 00043 2002 10 9 SWIA200211244 4 20020922 A 3414 320AS1 INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 212SW 6851 6851 120276 ''HIGH SPEED'' AURAL WARNING SOUNDED ON TAKEOFF ROLL AT ABOUT 80 KNOTS. ABORTED TAKEOFF & RETURNED TO GATE. REPLACED C APT'S AIRSPEED INDICATOR IAW MM 34-12-01. OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002100900044 20021009 00044 EA 2002 10 9 CA020913008 2 20020423 A 7200 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NR 1 MAKING METAL W E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 CA (CAN) ON DESCENT, NR 1 ENGINE TORQUE DROPPED BY 200 LBS. WHEN THE PILOT RETARDED THE POWER LEVER THE TORQUE DROPPED OF F ANOTHER 2000 LBS AND THE LOW OIL PRESSURE LIGHT ILLUMINATED. THE PILOT SHUTDOWN THE ENGINE AND CONTINUED THE APPROACH AND LANDING WITHOUT INCIDENT. INITIAL INVESTIGATION FOUND METAL PARTICLES ON THE CHIP DETECTOR AND IN THE OIL FILTER. E NGINE TSO APPROXIMATELY 4,400 HOURS. 2 L 7 2 4T 4 T RT A24CE E4EA 2002100900045 20021009 00045 EA 2002 10 9 SWIA200211245 1 20020920 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 418SW 7446 F/O'S WINDOW SHATTERED ON DESCENT INTO SLC. REMOVED AND REPLACED F/O'S SIDE WINDOW IAW RII 56-402. 2 L 7 2 4F RT A21EA 2002100900047 20021009 00047 SO 2002 10 9 SWIA200211247 1 20020822 A 5420 ANGLE EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 583SW 120351 ANGLE ON FIRE WALL FWD OF RT HYDRAULIC PACKAGE CRACKED JUST ABOVE GROUND SERVICE PORTS. DISCOVERED DURING C-CHECK. FAB RICATED REPAIR, STOP DRILLED CRACK, AND INSTALLED REPAIR IAW EMB SRM 51-70-06 & 51-40-02. 2 L 7 2 4T RT A31SO 2002100900048 20021009 00048 SO 2002 10 9 SWIA200211248 1 20020822 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 583SW 120351 LT OB NACELLE 1/2 FRAME CRACKED AT RIVET AT APPROX FRAME 18. DISCOVERED DURING C-CHECK. FABRICATED AND INSTALLED DOUBL ER OVER CRACK IAW EMB120 SRM 51-00-00 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002100900049 20021009 00049 EA 2002 10 9 CA020913010 1 20020909 A 2697 WIRE CNDAIR CL601 CL6012A12 1900303 EA RT FIRE BOTTLE SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON A SCHEDULED MAINTENANCE INSPECTION OF THE FIRE BOTTLES, MECHANIC FOUND ON RT BOTTLE LT SQUIB WIRING TO BE EXPOS ED AND TOUCHING EACH OTHER IN THE APU AREA. ANOTHER CL601 A/C INSPECTED AND FOUND SIMILAR PROBLEM WITH SQUIB WIRING (SA ME BOTTLE AND SQUIB). 2 L 7 2 4F RT A21AE 2002100900050 20021009 00050 SO 2002 10 9 SWIA200211249 1 20020822 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 583SW 120351 LT NACELLE IB SIDE 1/2 FRAME AT APPROX FRAME 18 IS CRACKED AT RIVET. DISCOVERED DURING C-CHECK. FABRICATED AND INSTALL ED DOUBLER TO CRACKED AREA IAW EMB SRM 51-00-00 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002100900051 20021009 00051 EU 2002 10 9 CA020913011 1 20020909 A 5414 5R0083 PANEL AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 NACELLE DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) NR 1 ENGINE SUFFERED DAMAGE TO THE FRONT ANTI ICE IMPACT PANEL IN THE LOWER HALF OF THE FAN CASE. AFTER A FERRY F LIGHT TO A MAIN BASE THE DAMAGE WAS REPAIRED. A NUMBER OF DAYS LATER, THE SAME REPAIRED PANELS WERE FOUND DELAMINATED. O NE PANEL WAS REPAIRED AND ONE PANEL REPLACED. FOLLOWING THIS, THE PANEL THAT WAS REPLACED, WAS FOUND DELAMINATED YET AGA IN. THE MANUFACTURER HAS RECOMMENDED A PROCESS, WHICH SHOULD ALLEVIATE THE PROBLEM. 2 L 7 2 4F 4 F RT A28NM E311NE 2002100900052 20021009 00052 NM 2002 10 9 C1HA200282016 1 20021004 A 3350 900835A BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 682CA 22019 Aft Ceiling emergency exit sign INOPReplaced battery cartridge ASSY. 2 L 7 3 4F A3WE 2002100900054 20021009 00054 SO 2002 10 9 SWIA200211250 1 20020822 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 583SW 120351 RT NACELLE IB SIDE 1/2 FRAME AT APPROX FRAME 18 IS CRACKED AT RIVET. DISCOVERED DURING C-CHECK. FABRICATED AND INSTALL ED DOUBLER TO CRACKED AREA IAW EMB SRM 51-00-00 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002100900055 20021009 00055 SO 2002 10 9 SWIA200211251 1 20020822 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 583SW 120351 RT NACELLE OB SIDE 1/2 FRAME AT APPROX FRAME 18 IS CRACKED AT RIVET. DISCOVERED DURING C-CHECK. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON FRAME IAW EMB SRM 51-70-05 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002100900056 20021009 00056 SO 2002 10 9 SWIA200211252 1 20020822 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 583SW 120351 AFT, MIDDLE BUTT STRAP HAS CORROSION. DISCOVERED DURING C-CHECK. REMOVED AND REPLACED BUTT STRAP IAW EMB SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002100900057 20021009 00057 SO 2002 10 9 SWIA200211253 1 20020822 A 5320 ANGLE EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 583SW 120351 LEFT AND RIGHT SIDES OF ANGLES AT FRAME 13 BELOW JUMPSEAT CUTOUT ARE CRACKED. DISCOVERED DURING C-CHECK. FABRICATED AN D INSTALLED IB & OB SIDE DOUBLERS ON LT & RT FRAME 13. CRACKS STOP-DRILLED IAW SRM 51-70-05 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002100900058 20021009 00058 EA 2002 10 9 CA020916001 1 20020914 A 3220 HYDRAULIC SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE NLG CONTAMINATED W O OTHER J R WARNING INDICATION PARTIAL RPM/PWR LOSS AP APPROACH 1 CA 21978 (CAN) DURING APPROACH, NLG DID NOT EXTEND. ALT EXTENSION ATTEMPTED APPROX SIX TIMES WITHOUT SUCCESS. AN EMERGENCY WAS DECLARED AND LANDING PERFORMED WITH THE NLG RETRACTED. NO INJURIES REPORTED. NLG WAS EXTENDED WHERE THE A/C STOPPED AND WAS TOWED TO A HANGAR. AFTER VISUALLY INSPECTING THE GEAR, SEVERAL RETRACT/EXTEND SEQUENCES WERE PERFORMED WITH NO PROB LEMS. THE HYD SYSTEM FILTERS WERE INSPECTED AND A CHIP WAS FOUND IN THE NR 3 RETURN FILTER. CHIP WILL BE ANALYSED TO IDE NTIFY ITS SOURCE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002100900059 20021009 00059 SO 2002 10 9 SWIA200211254 1 20020920 A 2731 5299 ACTUATOR EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM FAULTY A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 294SW 120321 ELEVATOR TRIM WHEEL HAS ABNORMAL RESISTANCE. DURING MANUAL MOVEMENT OF TRIM THERE IS GRINDING AND UNEVEN RESISTANCE. A FTER THOROUGH INSPECTION, FOUND BOTH LT & RT ELEVATOR TRIM ACTUATORS GRINDING. REMOVED AND REPLACED BOTH LT & RT TRIM A CTUATORS IAW EMB 120 MM 27-32-02. INSPECTED AGAIN AND RAN THROUGH MOVEMENT MULTIPLE TIMES. ALL OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002100900060 20021009 00060 SW 2002 10 9 CA020916003 1 20020912 A 3397 LANDING LIGHT SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP CENTER WING ARCED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) CREW REPORTED SMOKE IN THE CABIN DURING TAXI, AIRCRAFT WAS SHUT DOWN AND THE SMOKE DISSIPATED. A SUBSEQUENT INSPE CTION REVEALED EVIDENCE OF A FIRE ADJACENT TO THE LT LANDING LIGHT IN THE WING CENTER SECTION AND A FUEL LEAK WHEN THE L T FUEL BOOST PUMP WAS ON. FURTHER INSPECTION REVEALED THAT FUEL LINE LOCATED JUST ABOVE THE LT LANDING LIGHT HAD A HOLE AS A RESULT OF ARCING FROM THE JUMPER WIRE ON THE RETRACTABLE LANDING LIGHT. THE AFFECTED AREAS WERE CLEANED AND INSPEC TED, THE DAMAGED FUEL LINE WAS REPLACED, ALL REMAINING ADJACENT FUEL LINES WERE INSPECTED, REPLACED THE LANDING LIGHT AS SEMBLY AND REPAIRED DAMAGED WIRING. NO STRUCTURAL DAMAGE WAS EVIDENT. 2 L 7 2 4T 4 T RT A8SW E4WE 2002100900061 20021009 00061 NM 2002 10 9 SABA020101 1 20021007 A 3350 1306 BULB DHAV DHC8 DHC8103 1386005 NM A SABA O OTHER L NO TEST IN INSP/MAINT 1 SO 33 880CC 277 Aircraft 880 flight 5032 from PGV to CLT. During post-flight inspection the pilot reported the emergency lights at row 7 D&F would not test. Maintenance removed and and replaced bulbs, system ops checked good. Aircraft was returned to ser vice. 2 H 7 2 4T RT A13NM 2002100900063 20021009 00063 EA 2002 10 9 SWIA200211256 1 20020920 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY FAILED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 595SW 7292 CARGO BOTTLE TEST NR 2 INOP. NO RED LIGHTS ON THE TEST. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR WITH NEW SERVICE ABLE DETECTOR IAW 26-15-00 CRJ MM. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002100900064 20021009 00064 NM 2002 10 9 ASAA0210167 1 20020714 A 3397 07912 WIRE BOEING 737 737290C 138448V NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 11 INOPERATIVE. SPLICED BROKEN WIRE TO LIGHT ASSEMBLY AT ROW 11 THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2002100900065 20021009 00065 NM 2002 10 9 ASAA0210169 1 20020719 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 JNU - EMERGENCY EXIT SIGN ON SMOKE BARRIER ILLUMINATED. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY, THEN SIGN TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100900066 20021009 00066 NM 2002 10 9 ASAA0210171 1 20020724 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY EXIT IDENTIFIERS AT L2 AND R2 DOORS INOPERATIVE. REMOVED AND REPLACE D REMOTE ASSEMBLY BATTERIES, THEN LIGHT TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100900067 20021009 00067 EA 2002 10 9 CA020916007 1 20020904 A 2424 756654A VOLT REGULATOR CNDAIR CL601 CL6013A 8070802 EA GE CF34 CF343A 30015 NE ELECTRICAL MALFUNCTIONED W A UNSCHED LANDING H Z G ELECT. POWER LOSS-50 PC SIGNIFICANT FAILURE REPORT MULTIPLE FAILURE NR NOT REPORTED 1 CA (CAN) DURING REQUIRED ANNUAL INFLIGHT MANUAL ADG DEPLOYMENT CHECK, AN ABNORMAL SURGING IN VOLTAGE TOOK PLACE ON DEPLOYME NT. A140 STANDBY INST. LIGHTING A150 STICKPUSHER A150 L/H CHANNEL SPS. A159 & CHANNEL ANNUNCIATOR A160 10 CHANNEL ANNUN CIATOR B184 OBSERVERS AUDIO, C15 PITCH TRIM CHANNEL, AND C29 IRU NR 1 D45 EFIS SYMBOL GENERATOR CIRCUIT BREAKERS TRIPPE D. AS A PRECAUTION CREW DECLARED AN EMERGENCY AND A NORMAL LANDING WAS MADE AT BASE. THE ADG VOLTAGE REGULATOR WAS REPL ACED WITH A SERVICEABLE UNIT, AND DMAGED ELECTRICAL COMPONENTS CHANGED. ANOATHER FLIGHT TO CHECK ADG OPERATOR WAS CARRIE D OUT WITH ALL SYSTEMS NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2002100900068 20021009 00068 NM 2002 10 9 ASAA0240079 1 20020715 A 3350 8100022608 TERMINAL BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 FAI - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROWS 14, 15, 16 AND 17 INOPERATIVE. RECONNECTED WIRE TERMINA L ENDS. LIGHTS THEN FUNCTIONED PROPERLY. (M) 2 L 7 2 4F RT A16WE 2002100900069 20021009 00069 NM 2002 10 9 ASAA0240081 1 20020716 A 3397 WIRE BOEING 737 737490 1384715 NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 768AS 27082 FAI - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROW 16 INOPERATIVE. REPLACED BROKEN WIRE. LIGHTS THEN FUNCT IONED PROPERLY. (M) 2 L 7 2 4F RT A16WE 2002100900070 20021009 00070 NM 2002 10 9 ASAA0240083 1 20020717 A 3350 8100022608 TERMINAL BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 FAI - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROWS 17-23 INOPERATIVE. RECONNECTED WIRE TERMINAL ENDS. LIG HTS THEN FUNCTIONED PROPERLY. (M) 2 L 7 2 4F RT A16WE 2002100900071 20021009 00071 NM 2002 10 9 CA020916009 1 20020916 A 2530 3510001601 COFFEEMAKER BOEING 767 767375 1385217 NM GE CF6 CF680C2B6F 30025 NE GALLEY FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA (CAN) ON DECENT CREW REPORTED SMOKE IN AFT GALLEY AND LOUD POPPING SOUND, GALLEY COVERED IN WHITE DUST. NOTIFIED ATC/M AINT/DISPATCH. MTCE SUSPECTED COFFEEMAKER HOT WATER BLEW PLUG, AIRCRAFT LEFT WITH UTILITY BUSES OFF/REAR GALLEY CB'S PU LLED. AREA INSPECTED FOUND COFFEEMAKER AT FAULT. NEW COFFEEMAKER INSTALLED IN POSN 1. RUN FOR 45 MIN NO FAULT FOUND. 2 L 7 2 4F 4 F RT A1NM E13NE 2002100900072 20021009 00072 NM 2002 10 9 ASAA0240084 1 20020717 A 3397 8100022608 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROW 12 INOPERATIVE. RECONNECTED WIRES. LIGHTS THEN FUN CTIONED PROPERLY. (M) 2 L 7 2 4F RT A16WE 2002100900073 20021009 00073 NM 2002 10 9 ASAA0240085 1 20020727 A 3397 541N5091 WIRE BOEING 737 7374Q8 138447Q NM CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 JNU - FLOOR TRACK LIGHTING INOPERATIVE FROM ROW 14-17. REPLACED DAMAGED TRACK LIGHT WIRING, OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002100900074 20021009 00074 WP 2002 10 9 ASAA0280171 1 20020509 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING PREFLIGHT CHECK, DISCOVERED 'NUMEROUS EMERGENCY TRACK LIGHTS OUT'. REPLACED WIRE SECTIONS BETWEEN ROW 2 AN D 3. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900075 20021009 00075 WP 2002 10 9 ASAA0280172 1 20020510 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - DURING LINE CHECK, DISCOVERED EMERGENCY TRACK LIGHTS AT ROW 21-23 WERE INOPERATIVE. RECONNECTED LIGHTS. LIGHTS T HEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900076 20021009 00076 WP 2002 10 9 ASAA0280197 1 20020605 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING PREFLIGHT CHECK, DISCOVERED 'PART OF EMERGENCY TRACK LIGHTING INOPERATIVE'. REPLACED WIRING AT ROW 1. LIG HTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900077 20021009 00077 WP 2002 10 9 ASAA0280198 1 20020608 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING PREFLIGHT CHECK, DISCOVERED EMERGENCY LIGHTING IN FORWARD CABIN TO BE INOPERATIVE. RESECURED ELECTRICAL CO NNECTOR. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900078 20021009 00078 WP 2002 10 9 ASAA0280199 1 20020609 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING PREFLIGHT CHECK, DISCOVERED EMERGENCY LIGHTING IN FIRST CLASS TO BE INOPERATIVE. RECONNECTED LOOSE SEGMENT S. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900079 20021009 00079 WP 2002 10 9 ASAA0280200 1 20020609 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING LINE CHECK, DISCOVERED EMERGENCY LIGHTING TO BE INOPERATIVE AT ROW 1-3. SPLICED BROKEN WIRE AT SEAT FD3. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900080 20021009 00080 WP 2002 10 9 ASAA0280220 1 20020710 A 5514 5912175522 FAIRING DOUG DC9 DC983 3022083 WP HORIZ STAB DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OAK - RIGHT HORIZONTAL STABILIZER UPPER FAIRING WAS DAMAGED DURING LINE MAINTENANCE. TEMP REPAIRED FAIRING WITH CUT OUT PIECE FROM ANOTHER FAIRING AND SPEED TAPE PER EA 5510-01157. (M) 2 L 7 2 4F RT A6WE 2002100900081 20021009 00081 WP 2002 10 9 ASAA0280222 1 20020714 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE AT ROW 9. REPLACED POWER SUPPLY (BATTERY PACK). L IGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002100900082 20021009 00082 WP 2002 10 9 ASAA0280224 1 20020716 A 3350 0105606 MODULE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING LINE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE AT ROW 2. REPLACED LIGHT MODULE. LIGHTS THEN OPERATE D PROPERLY. (M) 2 L 7 2 4F A6WE 2002100900083 20021009 00083 WP 2002 10 9 ASAA0280225 1 20020716 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING LINE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE FROM ROW 22 TO 30. REPLACED FOUR LIGHT MODULES. LIGH TS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900084 20021009 00084 WP 2002 10 9 ASAA0280226 1 20020719 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 PDX - DURING PREFLIGHT CHECK, FORWARD 1ST CLASS EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900085 20021009 00085 WP 2002 10 9 ASAA0280229 1 20020721 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 SFO - DURING PREFLIGHT CHECK, FIRST FOUR EMERGENCY TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED FIRST MODULE. LIGHT S THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900086 20021009 00086 WP 2002 10 9 ASAA0280230 1 20020721 A 3397 0105606 WIRE DOUG DC9 DC982 3022082 WP CABIN FAULTY A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 PDX - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 6 THROUGH 9. REPAIRED FAULTY WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002100900087 20021009 00087 WP 2002 10 9 ASAA0280231 1 20020721 A 2611 PU90431R3 SMOKE DETECTOR DOUG DC9 DC983 3022083 WP LAVATORY FALSE ACTIVATION A ASAA K NONE N FALSE WARNING CR CRUISE 1 NM 01 949AS 53022 SEA - DURING FLIGHT 660, SMOKE DETECTOR IN LEFT AFT LAVATORY FALSELY ALARMED DESPITE NO AMBIENT SMOKE. RESET DETECTOR. SUBSEQUENT OPERATION CHECK WAS SATISFACTORY. (M) 2 L 7 2 4F RT A6WE 2002100900088 20021009 00088 WP 2002 10 9 ASAA0280232 1 20020723 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 PDX - DURING LINE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE FROM ROW 6 TO 9. RECONNECTED WIRING TO LIGHT MODULE C ONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900089 20021009 00089 WP 2002 10 9 ASAA0280234 1 20020723 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE IN 1ST CLASS SECTION. RECONNECTED WIRING TO LIGH T MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900090 20021009 00090 WP 2002 10 9 ASAA0280235 1 20020726 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 OAK - DURING LINE MAINTENANCE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE IN 1ST CLASS SECTION. RECONNECTED WIRING TO LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900091 20021009 00091 WP 2002 10 9 ASAA0280236 1 20020726 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 LAX - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE IN FORWARD CABIN. REPAIRED FLOOR TRACK LIGHTING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900092 20021009 00092 WP 2002 10 9 ASAA0280237 1 20020727 A 3350 0105606 PLUG DOUG DC9 DC983 3022083 WP CABIN OUT OF POSITION A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING LINE MAINTENANCE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE IN FORWARD CABIN. REINSTALLED PLUG IN TRA CK LIGHTING MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900093 20021009 00093 WP 2002 10 9 ASAA0280238 1 20020727 A 3350 0105606 PLUG DOUG DC9 DC983 3022083 WP CABIN OUT OF POSITION A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 PDX - DURING LINE MAINTENANCE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE ROWS 6-9. REINSTALLED PLUG IN TRACK LIGHT ING MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002100900094 20021009 00094 WP 2002 10 9 ASAA0280277 1 20020719 A 3350 0105606 SOCKET DOUG DC9 DC982 3022082 WP CABIN MISSING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING LINE CHECK, ONE EMERGENCY TRACK LIGHT AT ROW 3 WAS FOUND TO BE INOPERATIVE. REPLACED MISSING LIGHT MODULE (SOCKET). LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002100900095 20021009 00095 WP 2002 10 9 GTIA020680 1 20020623 A 2740 WARNING SYSTEM DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A GTIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 23 803NK 48087 RSW - FLT 926 - STABILIZER WARNING SOUNDED ON TAKEOFF ROLL, REJECTED TAKEOFF AT 10 KTS. PERFORMED TAKEOFF WARNING SYSTE M IAW MM 27-00-00. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2002100900096 20021009 00096 WP 2002 10 9 GTIA020681 1 20020623 A 5753 SKIN DOUG DC9 DC981 3022081 WP T/E FLAP DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 ACY - LEFT FLAP HAS DELAMINATION AND SEPARATION ON OUTBOARD SIDE. REPAIRED DELAMINATION ON LEFT FLAP TRAILING EDGE BY S TOP DRILLING CRACK AND FILLING AREA WITH PR1422 B HALF SEALANT IAW DC9/MD 80 SRM 57-03. (M) 2 L 7 2 4F A6WE 2002100900097 20021009 00097 WP 2002 10 9 GTIA020682 1 20020623 A 5753 SKIN DOUG DC9 DC981 3022081 WP T/E FLAP DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 ACY - RIGHT FLAP TRAILING EDGE HAS DELAMINATION AND SEPARATION ON OUTBOARD. REPAIRED DELAMINATION OF RIGHT OUTBOARD FLA P TRAILING EDGE BY STOP DRILLING CRACK AND FILLING AREA WITH PR1422 B1/2 SEALANT IAW SRM 57-03. (M) 2 L 7 2 4F A6WE 2002100900098 20021009 00098 WP 2002 10 9 GTIA020683 1 20020622 A 2780 CONTROL HANDLE DOUG DC9 DC983 3022083 WP COCKPIT LACK OF LUBE A GTIA O OTHER O OTHER LD LANDING 1 GL 23 815NK 49415 DTW - FLT 249 - SLATS WOULD NOT RETRACT AFTER LANDING. LUBRICATED FLAP HANDLE SECTOR QUADRANT. OPS OK IAW MM 12-21-02. (M) 2 L 7 2 4F RT A6WE 2002100900100 20021009 00100 WP 2002 10 9 GTIA020684 1 20020619 A 2740 575600015 SENSOR DOUG DC9 DC983 3022083 WP HORIZ STAB MALFUNCTIONED A GTIA O OTHER P NO WARNING INDICATION CR CRUISE 1 GL 23 827NK 49793 DTW - FLT 237 - HORIZONTAL STABILIZER AUDIO SIGNAL IS NOT SOUNDED AND NO VOCAL WARNING IN AUTO PILOT MODE, AND MANUAL IN FLIGHT AND GROUND OPS. REMOVED AND REPLACED HORIZONTAL MOTION SENSOR AND OPS NORMAL AS PER MM 27-40-11. (M) 2 L 7 2 4F RT A6WE 2002100900101 20021009 00101 NE 2002 10 9 CA020917006 1 20020904 A 6320 S613520600046 GEARBOX SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE MAIN ROTOR CONTAMINATED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) THE AIRCRAFT WAS CONDUCTING NORMAL LOGGING OPERATIONS WHEN THE OIL PUMP CHIP LIGHT ILLUMINATED. A/C RETURNED TO BA SE & SCREEN WAS REMOVED & CONTENTS INSPECTED. 5 PIECES OF ALUMINUM WERE FOUND, APPROX. 10MM LONG, ONE WAS 5MM WIDE, THE OTHER FOUR WERE 2 TO 3 MM WIDE. GEARBOX WAS REMOVED & DISASSEMBLED. A FULL INSPECTION WAS CARRIED OUT & NO DAMAGE FOUN D. ANOTHER PIECE OF MATERIAL WAS LOCATED IN THE LOWER CASE THAT HAD ESCAPED UNDAMAGED, IT IS 8MM *7MM. OBJECT, AGAIN ALU MINUM, IS A SECTION OF A DG CLAMP. THE REST OF THE CLAMP WAS NOT FOUND. IT HAS NOT BEEN DETERMINED WHERE THE CLAMP CAME FROM OR HOW IT ENTERED THE MAIN GB. GB HAS BEEN INSPECTED AND RETURNED TO SERVICE. 2 G 7 2 4U 4 U 1H15 1E3 2002100900102 20021009 00102 EA 2002 10 9 CA020917008 1 20020915 A 5220 H341931 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ESCAPE HATCH CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 7473 (CAN) ON INSPECTION, MECHANIC FOUND OUTER HANDLE OF CREW ESCAPE HATCH STUCK IN THE DOWN POSITION. WOULD NOT POP UP WHE N BUTTON IS DEPRESSED. UNABLE TO RELEASE HANDLE EVEN WHEN FORCED. REMOVED HANDLE ASSEMBLY AND INSTALLED NEW ASSEMBLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2002100900103 20021009 00103 2002 10 9 CA020918001 4 20020912 A 3140 AE0804AA1 FAN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE DISPLAY FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA 13182 (CAN) SMOKE ODOR IN COCKPIT, REPORTED BY FLIGHT CREW. DISPLAY FAN NR 2 FOUND UNSERVICEABLE. CIRCUIT BREAKER PULLED AND AIRCRAFT RETURNED TO BASE UNDER MEL. DISPLAY FAN NR 2 REPLACED IN ACCORDANCE WITH AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2002100900104 20021009 00104 EA 2002 10 9 CA020918002 1 20020917 A 5220 H341931 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ESCAPE HATCH CORRODED W K NONE L NO TEST IN INSP/MAINT 1 CA 11335 (CAN) UPON INSPECTION MECHANIC FOUND OUTER HANDLE OF CREW ESCAPE HATCH STUCK IN THE DOWN POSITION. REMOVED AND REPLACED CORRODED HANDLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002100900106 20021009 00106 SW 2002 10 9 CA020918004 1 20020830 A 5302 205032806089A LONGERON BELL 205 205A1 1181414 SW TAIL BOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE AIRCRAFT WAS IN THE HANGAR FOR SCHEDULED MAINTENANCE, IT WAS NOTED THAT THERE WAS MOVEMENT OF THE TAILBOOM S KIN AND NO MOVEMENT OF FITTING WHEN THE TAILBOOM WAS MANUALLY FLEXED. FURTHER INVESTIGATION REVEALED THE LOWER FITTING O F THE LONGERON WAS CRACKED. THIS CRACKED FITTING LEFT ONLY 3 OF THE 4 TAILBOOM ATTACHMENT BOLTS HOLDING THE TAILBOOM TO THE AIRFRAME. THE TAILBOOM WAS REPLACED AND ALL ATTACHING HARDWARE WAS REPLACED. 1 G 7 1 4U H1SW 2002100900107 20021009 00107 NM 2002 10 9 QXEA0201426 1 20020906 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- AIRCRAFT SKIN UNDERNEATH LOWER TCAS ANTENNA IS CORRODED AROUND NUTPLATE HOLES. REPAIRED IAW DHC-8 SRM 51-20-16 AND 53-00-16. 2 H 7 2 4T RT A13NM 2002100900108 20021009 00108 NM 2002 10 9 QXEA0201427 1 20020906 A 5420 PAD DHAV DHC8 DHC8202 2809007 NM RT NACELLE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- PAD ON H-MEMBER FOR RETRACT ACTUATOR HAS FRETTING CORROSION AROUND UPPER AND RIGHT HAND NACELLE. REPAIRED IAW DHC- 8 RD 8-54-1178. 2 H 7 2 4T RT A13NM 2002100900109 20021009 00109 NM 2002 10 9 QXEA0201428 1 20020906 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- RIGHT HAND OUTBOARD SEAT TRACK NR 11 HAS CORROSION AT INSIDE CHANNEL RADIUS AT STATION 436.500. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002100900110 20021009 00110 NM 2002 10 9 QXEA0201429 1 20020906 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- RIGHT HAND SEAT TRACK NR 11 HAS CORROSION INSIDE CHANNEL RADIUS AT STATION X501.000. REPAIRED IAW DHC-8 SRM 51-00- 06 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002100900111 20021009 00111 NM 2002 10 9 QXEA0201430 1 20020906 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- RIGHT HAND OUTBOARD SEAT TRACK NR 11 TOP RAIL HAS CORROSION BETWEEN FRAME STATIONS X467.000 TO X486.000. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002100900112 20021009 00112 NM 2002 10 9 QXEA0201431 1 20020905 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- RIGHT HAND OUTBOARD SEAT TRACK NR 12 HAS WEAR ON TOP RAIL CUTOUT AT STATION 521.000. REPAIRED IAW DHC-8 SRM 51-00- 05 AND RD 8-53-3644. 2 H 7 2 4T RT A13NM 2002100900113 20021009 00113 NM 2002 10 9 QXEA0201432 1 20020905 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- RIGHT HAND OUTBOARD SEAT TRACK NR 12 HAS GOUGES IN CENTER INSIDE CHANNEL AT STATION X547.500. REPAIRED IAW DHC-8 S RM 51-00-06 AND RD 8-53-3644. 2 H 7 2 4T RT A13NM 2002100900114 20021009 00114 NM 2002 10 9 QXEA0201433 1 20020906 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND OUTBOARD SEAT TRACK NR 1 HAS CORROSION ON TOP RAIL AND A GOUGE IN CENTER CHANNEL AT STATION X291.400. RE PAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002100900115 20021009 00115 NM 2002 10 9 QXEA0201434 1 20020906 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND OUTBOARD SEAT TRACK NR 1 HAS LIGHT CORROSION ON TOP RAIL AT STATION X312.350. REPAIRED IAW DHC-8 SRM 51- 00-06 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002100900116 20021009 00116 NM 2002 10 9 QXEA0201435 1 20020906 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LEFT HAND OUTBOARD SEAT TRACK NR 1 HAS CORROSION INSIDE CENTER CHANNEL AT STATION X396.150. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-53-1342. 2 H 7 2 4T RT A13NM 2002100900118 20021009 00118 NM 2002 10 9 QXEA0201480 1 20020924 A 5330 STRAP BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX- FUSELAGE SKIN STRAP AT STATION 108.0 AND STRINGER 32L HAS A NICK ON THE INBOARD EDGE OF THE STRAP. REPAIRED IAW HO RIZON AIR EA 6-53-121. 2 H 7 2 4T RT A13NM 2002100900119 20021009 00119 NM 2002 10 9 QXEA0201487 1 20020912 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- BRACKET IS CRACKED IMMEDIATELY BELOW MAIN CABIN DOOR THRESHOLD AT STATION X242.2. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002100900120 20021009 00120 NM 2002 10 9 QXEA0201488 1 20020913 A 5320 RETAINER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- MAIN CABIN DOOR LOWER SEAL RETAINER IS CORRODED AT THRESHOLD. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002100900121 20021009 00121 NM 2002 10 9 QXEA0201489 1 20020914 A 5720 STIFFENER DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- ACCESS PLATE 524AT HAS CHAFFED STIFFENER WHERE IT CONTACTED NR 1 WIGGINS FITTING. REPAIRED IAW HORIZON AIR EA 2-57 -194. 2 H 7 2 4T RT A13NM 2002100900122 20021009 00122 EU 2002 10 9 QXEA0201490 1 20020925 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 PDX-FORWARD EXIT SIGN HAS SEVERAL LIGHTS OUT. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A20EU 2002100900123 20021009 00123 SW 2002 10 9 CA020918006 1 20020906 A 5312 2040317491 BULKHEAD BELL 204 204B 1181404 SW LYC T53 T5313B 41549 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE ROTOR CONTROL BELLCRANK BULKEAD CRACKED IN MULTIPLE PLACES. 1 G 7 1 4U 4 U H1SW E17EA 2002100900124 20021009 00124 NM 2002 10 9 QXEA0201492 1 20020926 A 3222 STRUT DHAV DHC8 DHC8202 2809007 NM NLG LOW A QXEA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 NM 09 356PH 502 SEA- RETURNED TO FIELD DUE TO, ON GEAR RETRACTION, WEIGHT ON WHEELS LIGHT ILLUMINATED AND ALL THREE GEAR DOOR LIGHTS STA YED ON AND NOSE GEAR UNSAFE LIGHT WAS ILLUMINATED. DISAGREEMENT LIGHTS ON GEAR HANDLE ALSO STAYED ILLUMINATED. PERFORM ED ALTERNATE GEAR EXTENSION METHOD NR 1. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NOSE STRUT COMPRESSED. SERVICED NOSE STRUT AND CLEANED PROX SENSORS. NO LEAKS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002100900125 20021009 00125 NM 2002 10 9 QXEA0201493 1 20020928 A 2611 SMOKE WARNING DHAV DHC8 DHC8202 2809007 NM COCKPIT FALSE ACTIVATION A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 362PH 518 PDX- MASTER WARNING LIGHT AND SMOKE WARNING LIGHTS ILLUMINATED IN FLIGHT. PUSHED OFF MASTER WARNING LIGHT AND SMOKE WAR NING EXTINGUISHED. NO SMOKE VISIBLE OR ODOR DETECTED. INSPECTED SMOKE DETECTORS. NO DEFECTS NOTED. COMPLIED WITH OPE RATIONAL TEST OF SMOKE DETECTORS IAW DHC-8 AMM 26-15-00-710-801. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE . NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2002100900126 20021009 00126 NM 2002 10 9 QXEA0201495 1 20020927 A 5534 PLATE DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - VERT STAB GOUGE IN LADDER PLATE, RIGHT HAND SIDE, LEADING EDGE. REPAIRED IAW DHC-8 RD 8-55-584. 2 H 7 2 4T RT A13NM 2002100900127 20021009 00127 NM 2002 10 9 QXEA0201496 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 515 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 7 BOTTOM CHAFED APPROXIMATELY 12 INCHES BY TRACK COVER AT X418.00. REPLACED SEA T TRACK. 2 H 7 2 4T RT A13NM 2002100900128 20021009 00128 NM 2002 10 9 QXEA0201497 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND INBOARD SEAT TRACK NR 7 CHAFED APPROXIMATELY 12 INCHES BY TRACK COVER AT X387.00. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 2002100900129 20021009 00129 NM 2002 10 9 QXEA0201498 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND INBOARD SEAT TRACK NR 7 BOTTOM CHAFED APPROXIMATELY 12 INCHES BY TRACK COVER AT X354.00. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 2002100900130 20021009 00130 NM 2002 10 9 QXEA0201499 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND INBOARD SEAT TRACK NR 7 CORROSION IN SEAT ATTACH AREA APPROXIMATELY X328.00. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 2002100900131 20021009 00131 NM 2002 10 9 QXEA0201500 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND INBOARD SEAT TRACK NR 7 BOTTOM CHAFED APPROXIMATELY 12 INCHES BY TRACK COVER, AT APPROXIMATELY X322.00 2 H 7 2 4T RT A13NM 2002100900132 20021009 00132 NM 2002 10 9 QXEA0201501 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND INBOARD SEAT TRACK NR 7 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X312.00. REPLACE D SEAT TRACK. 2 H 7 2 4T RT A13NM 2002100900133 20021009 00133 NM 2002 10 9 QXEA0201502 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND INBOARD SEAT TRACK NR 7 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X298.00. REPLACE D SEAT TRACK. 2 H 7 2 4T RT A13NM 2002100900134 20021009 00134 NM 2002 10 9 UPS02439268 1 20020816 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C RT LG W/W O/B PRESSURE DECK LWR FACE AT BS 1416 LATERAL O/B NR 2 RIVET HOLE AREA CRACKED TO EDGE. SEC TION OF PRESSURE WEB AT RT LG W/W O/B FROM STA 1400 TO 1438 RBL 110 TO MOST O/B AREA REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2002100900135 20021009 00135 NM 2002 10 9 UPS02439281 1 20020807 A 5330 PANEL BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C INSPECT SPEED TAPE TWO .25 INCH HOLES LOCATED O/B & FWD OF THE WATER SERVICING PANEL PER SRM 51-40-09 FIG 1 SHT 3. FIBERGLASS REPAIRED AS PER SRM 51-40-15 FIG 7 AT EXT SURFACE. 2 L 7 4 4F A20WE 2002100900136 20021009 00136 NM 2002 10 9 UPS02439316 1 20020818 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C RT LG W/W STA 1241 CANTED PRESSURE DECK BULKHEAD 2EA TENSION BOLT HOLES FOUND CORROSION AS RBL 75. RT LG W/W STA 1241 CANTED PRESSURE DECK 2EA TENSION BOLT HOLES OVERSIZED PER SRM 51-30-05. NDT CONFIRMED NO CRACK AND NO C ORROSION. 2 L 7 4 4F A20WE 2002100900137 20021009 00137 NM 2002 10 9 UPS02439318 1 20020815 A 5412 BULKHEAD BOEING 747 747123 1384873 NM NR 4 NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C CRACKS FOUND ON NR 4 NACELLE STRUT REAR MOUNT FWD AND AFT WEBS. NR 4 NACELLE STRUT REAR MOUNT BULKHEA D REPAIRED AS PER RS R54-53-34881 & UPS ENGINEERING FILE NUMBER 747-54-20030. 2 L 7 4 4F A20WE 2002100900138 20021009 00138 NM 2002 10 9 CA020918007 1 20020916 A 7603 253T72041 CLUTCH BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE THROTTLE MALFUNCTIONED W O OTHER E VIBRATION/BUFFET DE DESCENT 1 CA (CAN) BOTH THRUST LEVERS APPEARED TO STICK (AS IF THEY WERE IN A DETENT) AT FLIGHT IDLE AT TOP OF DECENT. THEY WERE VERY STIFF TO MOVE FORWARD FROM THAT POSITION. STICKING WAS ACCOMPANIED BY AN AUTO THROTTLE DISCONNECT. THROTTLE CLUTCH ASSY REPLACED AND OPERATION CHECKED SERVICEABLE AS PER AMM. 2 L 7 2 4F 4 F RT A1NM E3NE 2002100900139 20021009 00139 SO 2002 10 9 CA020918009 1 20020806 A 7120 102460002 MOUNT PIPER PA46 PA46500TP 7104622 SO ENGINE CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOLLOWING ENGINE MOUNT REPLACEMENT FOR SB 1103, IT WAS DISCOVERED THE MOUNT CHAFED ON ONE ENGINE MOUNT TUBE BECAUS E OF A PIECE OF THE PLENUM MAKING CONTACT. CORROSION HAD STARTED TO TAKE PLACE. THE PROBLEMATIC PART (A BOOT SEALING T HE PLENUM AROUND AN ENGINE MOUNT TUBE) WAS ADJUSTED TO PREVENT CHAFING ON THE NEW ENGINE MOUNT. 1 L 7 1 3O RT A25SO 2002100900141 20021009 00141 NM 2002 10 9 CA020918013 1 20020906 A 5270 SENSOR BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA CARGO DOOR OUT OF ADJUST W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) DURING CLIMB THE DOOR WARNING CAUTION CAME ON INTERMITTENTLY. DOOR PAGE CONFIRMED THAT THE CARGO DOOR WAS GIVING U NLOCKED INDICATION INTERMITTENTLY. AIRCRAFT RETURNED TO BASE. MAINTENANCE PERSONNEL INTERROGATED THE PSEU AND THE CARG O DOOR LOCK SENSOR INDICATED UNREASONABLY FAR WHEN DOOR WAS CLOSED. THE SENSOR WAS ADJUSTED, HOWEVER DURING ADJUSTMENT I T WAS NOTED THAT THE INDU CTANCE WAS ERRATIC. REPLACEMENT SENSOR ORDERED AND REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002100900143 20021009 00143 NE 2002 10 9 CA020919002 2 20020918 A 7321 EEC200007BL EEC AIRBUS 330 A330342 EU RROYCE RB211 RB211TRENT77 NE NR 2 ENGINE FAILED W O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 CA (CAN) ON APPROACH, ENGINE NR 2 FADEC FAULT. ECAM ACTION FOLLOWED ENGINE NR 2 SHUTDOWN FOR LANDING. POST FLIGHT REPORT INDICATED ENGINE NR 2 FADAC FAULT SOURCE DMC3 IDENT EIVMU, AFS, FWS. NR 2 ENGINE EEC REPLACED AND ENGINE GROUND RUN CARR IED OUT AND CHECKED SERVICEABLE. 1 L 7 2 4F 4 F RT A46NM E39NE 2002100900144 20021009 00144 CE 2002 10 9 CA020919003 1 20020917 A 5522 115610010125 SKIN BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16030 16030 (CAN) DURING REPAIR TO AN ELEVATOR, THE SKIN HAD TO BE REMOVED, THE TRAILING EDGE SPLINE WAS FOUND CRACKED AT SEVERAL L OCATIONS, MOST OF THE CRACKS EXTENDED FROM THE RIVET HOLE TO THE TRAILING EDGE OF THE SPLINE, A FEW CRACKS EXTENDED FR OM THE RIVET HOLE TO THE LEADING EDGE. THE CRACKS WERE VISIBLE WITHOUT DISASSEMBLY OF THE SKIN, HOWEVER THEY WERE VERY SMALL AND YOU WOULD NOT NOTICE THEM IF NOT SPECIFICALLY LOOKING FOR THEM. APPROXIMATELY 1/2 TO 2/3 OF THE HOLE WERE CRAC KED. 1 L 7 2 3T 4 T A14CE E4EA 2002100900145 20021009 00145 EU 2002 10 9 CA020920001 1 20020915 A 5320 A5397822300600 LINER AIRBUS 310 A310300 3930305 EU DOOR FRAME MISSING W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING THE WALK AROUND OF AIRCRAFT, FOUND THE LOWER FWD LINING ASSY, AT AFT CARGO COMPARTMENT DOOR FRAME, WAS MI SSING. MAINTENANCE REPLACED THE LINING ASSY IAW AMM 53-17-88. 2 L 7 2 4F RT A35EU 2002100900146 20021009 00146 EA 2002 10 9 CA020920002 1 20020917 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAPS MALFUNCTIONED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CA (CAN) WHEN FLAPS 450 SELECTED A/C ROLLS LT HALFWAY OF RT, AILERON TRIM NEEDED TO LEVEL WINGS, LT FLAPINDICATION JUMPS 40 0 TO 450 REPLACED RT NR 1 ACTUATOR , FLEXSHAFT ON INBD FLAP AND LT POS TRANSMITTER, PERFORMED RIGGING OF AILERON SYS AND FLAP SYSTEM, OPS NORMAL. THE FLAP POSITION INDICATION PROBLEM IN COMBINATION WITH A MISSRIGGED FLAP PANEL & AILERON PAN EL WAS INTERPRETED BY THE PILOT AS AFLAP ASYMMETRY. AFTER LANDING, MAINTENANCE CHECKED THE FLAP SYSTEMAND FOUND RT FLAP ACTUATOR NR 1 LEAKING. DURING REPLACEMENT OF THE ACTUATOR, THEY NOTICED THE DEFECT FLEX SHAFT. TO SOLVE THE PROBLEM, FLA P AND AILERON PANEL WERE ADJUSTED AND THE POSITION TRANSMITTER WAS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002100900147 20021009 00147 NM 2002 10 9 CA020920003 1 20020915 A 3230 NA SEQUENCE VALVE DHAV DHC8 DHC8301 1386003 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE MLG MALFUNCTIONED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) ON TAKE-OFF, LANDING GEAR CAUTION LIGHT ILLUMINATED. CREW ELECTED TO RETURN, AND PERFORMED ALTERNATE GEAR EXTENSIO N, AND THE LT MLG DOOR AMBER LIGHT STAYED ILLUMINATED. LANDING WAS COMPLETED WITH NO FURTHER INCIDENT. DURING MAINTENANC E TROUBLE-SHOOT, THE PSEU WAS CHANGED, THE LT MLG DOOR SEQUENCE VALVE WAS REPLACED, AND WIRING FROM PSEU TO LT SEQUENCE VALVE WAS REPLACED. GEAR SWING AND TEST FLIGHT WERE COMPLETEDWITH NO FURTHET RE-OCCURRANCE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002100900149 20021009 00149 EA 2002 10 9 CA020923003 1 20020920 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA (CAN) 'FLAP FAIL ' MESSAGE ON EICAS IN CRUISE FECU CHANGED AND TESTED AS PER AMM 2 L 7 2 4F 4 F RT A21EA E15NE 2002100900150 20021009 00150 NM 2002 10 9 UPS02239638 1 20020917 A 3230 652163716 SUPPORT FITTING BOEING 727 72722C 138400F NM R/H MLG W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI R/H MLG WING DOOR ACTUATOR SUPPORT FITTING CRACKED FITTING REMOVED AND REPLACED IAW EO B727-321 0-2583 2 L 7 3 4F A3WE 2002100900151 20021009 00151 NM 2002 10 9 UPS02239639 1 20020920 A 5310 FRAME BOEING 727 72722C 138400F NM BS 560 STR7 R/H DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI DENT IN FRAME BS 560 STR7 R/H REPAIRED IAW SRM 53-10-4 FIG 1 2 L 7 3 4F A3WE 2002100900152 20021009 00152 NM 2002 10 9 UPS02239640 1 20020917 A 5310 STRINGER BOEING 727 72722C 138400F NM BS 1000 STR6R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI STR 6R FOUND CRACKED AT BS 1000 STRINGER REPAIRED IAW SRM 53-10-3 FIG 1 DETAIL 11 2 L 7 3 4F A3WE 2002100900153 20021009 00153 NM 2002 10 9 UPS02439622 1 20020925 A 5410 WEB BOEING 747 747SR46 1384816 NM #2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C #2 PYLON MID SPAR WEB HAS CRACK AT PREVIOUS REPAIR NAC STA 205 APPROX. #2 PYLON MID SPAR WEB CRACK AT NAC STA 205 REPAIRED REF SRM 54-10-03 FTG.12 / SRM 51-30-02. 2 L 7 4 4F RT A20WE 2002100900154 20021009 00154 NM 2002 10 9 UPS02439624 1 20020923 A 5310 WEB BOEING 747 747SR46 1384816 NM RH TUNNEL BS 260 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C RH TUNEL AREA 7 BS 260 B/H WEB INNER UPPER CORNER CRACK AROUND FASTENER HEAD AT RBL 35". BULKHEAD WEB REPAIRED AS PER SRM 53-10-04 FIG 48.. 2 L 7 4 4F RT A20WE 2002100900155 20021009 00155 NM 2002 10 9 UPS02439631 1 20020922 A 5320 SUPPORT BOEING 747 747SR46 1384816 NM FX BS 880 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C FX- BS 880 RBL 30 - LBL 30 BODY FAIRING SUPPORT SURFACE CORROISON FOUND. CORROSION BLEND OUT 0.046 "X1"X3", EXCEED SRM LIMIT, REPAIRED AS PER SRM 53-50-04 FIG.2 2 L 7 4 4F RT A20WE 2002100900156 20021009 00156 NM 2002 10 9 UPS02439632 1 20020921 A 5310 WEB BOEING 747 747SR46 1384816 NM NOSE W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C NOSE W/W BODY STRUCTURE CRACK FOUND AT LH BS 320 VERTICAL BEAM WEB, ONE EACH STAND-OFF HOLE WAS CRACKE D BTN #2 & #3 VERTICAL BEAM CLIPS AND 2 STAND-OFF HOLES CRACKED BTN #5 & #6 CLIPS REFER FIG ATTACHED. VERT BEAM WEB REPLACED PER SRM 51-10-01 P.8. 2 L 7 4 4F RT A20WE 2002100900157 20021009 00157 NM 2002 10 9 UPS02439633 1 20020923 A 5310 WEB BOEING 747 747SR46 1384816 NM BS 260 B/H WEB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C LH TUNEL AREA 7 BS 260 B/H WEB INNER UPR CORNER AROUND FASTENER HEAD AT LBL 35". B/H WEB REPAIRED AS PER SRM 53-10-04 FIG.48. 2 L 7 4 4F RT A20WE 2002100900158 20021009 00158 EU 2002 10 9 CA020923004 1 20020907 A 2742 97873014203 ACTUATOR PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL PITCH TRIM FAILED W H DEACTIVATE SYST/CIRCUITS I FLT. ATTITUDE INST. CR CRUISE 1 CA (CAN) FLIGHT CREW REPORTED AUTOPILOT FAILED IN FLIGHT, CREW SUSPECTED PITCH TRIM ACTUATOR DUE TO AN 'OUT OF TRIM' CONDIT ION WHEN AUTOPILOT FAILS. REMOVED ACTUATOR AND NOTICED THAT THE SHAFT SEAL WAS DIRTY AND WORN, SUSPECT THAT MOISTURE WAS ENTERING ACTUATOR AND CAUSED INTERNAL MALFUNCTION. PITCH TRIM ACTUATOR WAS REPLACED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002100900159 20021009 00159 EU 2002 10 9 CA020923005 1 20020909 A 2742 9787314203 ACTUATOR PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL PITCH TRIM INOPERATIVE W H DEACTIVATE SYST/CIRCUITS I FLT. ATTITUDE INST. CR CRUISE 1 CA (CAN) FLIGHT CREW REPORTED AUTOPILOT DISCONNECTED IN FLIGHT AND TRIM INDICATOR WOULD MOVE FULL DEFLECTION WHEN PITCH TRI M OPERATED. SUSPECT INTERNAL FAULT WITH ACTUATOR. ACTUATOR REPLACED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002100900160 20021009 00160 2002 10 9 CA020923007 4 20020919 A 3497 WIRE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP NAVIGATION SYS CHAFED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) DURING TAXI AFTER A UNEVENTFUL FLIGHT, SMOKE WAS DETECTED IN THE COCKPIT. THE AIRCRAFT WAS SHUTDOWN AND THE AIRCRA FT EVACUATED. THE SMOKE EVENTUALLY DISSIPATED. A SUBSEQUENT INSPECTION REVEALED THAT THE AVIONICS RELAY WIRE 2A10A HAD C HAFED THROUGH AND ARCHED ON A HYDRAULIC LINE IN THE AREA BELOW THE FLOOR JUST AFT OF THE COPILOTS SEAT.THE WIRING AND TH E LINE WERE REPAIRED AND THE AIRCRAFT RETURNED TO SERVICE. NO STRUCTURAL DAMAGE WAS DETECTED. 2 L 7 2 4T 4 T RT A8SW E4WE 2002100900161 20021009 00161 EU 2002 10 9 CA020924001 1 20020920 A 7997 4E38B24 WIRE PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL OIL INDICATOR CHAFED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) AFTER TAKEOFF, THE PILOT LOST OIL PRESSURE INDICATION, HOWEVER, THERE WAS NO MASTER CAUTION INDICATION. THE PILOT RETURNED TO BASE WITHOUT INCIDENT. INVESTIGATION REVEALED THAT THE WIRE HARNESS, BETWEEN THE OIL PRESSURE TRANSMITTER AN D THE FIREWALL CONNECTOR PLUG WAS CHAFED THROUGH APPROX.12 INCHES FROM THE FIREWALL END, IN THE AREA WHERE THE COOLING D UCT FOR THE STARTER GEN PASSES OVER THE WIRE HARNESS. THE WIRE HARNESS WAS REPLACED AND THE OIL PRESSURE INDICATING SYST EM FUNCTIONED NORMALLY. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002100900162 20021009 00162 EA 2002 10 9 CA020925001 1 20020922 A 2752 PDU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAPS FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FLAP FAIL MESSAGE FOUND ON EICAS INTEROGATION CHECK ( FOUND ON ACCOMPLISHMENT OF SERVICE CHECK.)DURING TEST FOUND PDU2 C/B POPPING AND FLAPS HALF SPEED . PDU REPLACED AS PER AMM 2 L 7 2 4F 4 F RT A21EA E15NE 2002100900163 20021009 00163 EA 2002 10 9 CA020925003 1 20020918 A 2697 WIRE HARNESS KIDDE 899486 CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A NE EXTINGUISHER EXPOSED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WIRING HARNESS FOR THE ENGINE FIRE BOTTLE SQUIBS LOCATED IN THE APU AREA HAD EXPOSED WIRES WHERE THEHARNESS ENTERS THE CONNECTOR PLUG FOR THE SQUIB. 2 L 7 2 4F 4 F RT A21AE E15NE 2002100900164 20021009 00164 CE 2002 10 9 CA020925004 1 20020920 A 2750 6046H39A RELAY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE TE FLAPS INTERMITTENT W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AIRCRAFT DEPARTED AND FLAPS WOULD NOT RETRACT FROM TAKE OFF POSITION. CREW ELECTED TO RETURN AND AN UNEVENTFULL LA NDING WAS COMPLETED. DURING TAXI FLAPS RETRACTED. FLAPS WHERE DEEMED TO BE INTERMITTENT AND WHERE DEFERRED AND CB PULLED . AT ARRIVAL TO MAINTENANCE BASE FOUND THE FLAP RELAY TO BE INTERMITTENT AND REPLACED IT. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002100900165 20021009 00165 NM 2002 10 9 CALA0200488 1 20021007 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 375 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 INSPECTION FOUND STRINGER 23L CORRODED AT STA 375 IN FORWARD CARGO PIT. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A NEW SECTION OF STRINGER WAS SPLICED IN IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2002100900166 20021009 00166 NM 2002 10 9 CALA0200489 1 20021008 A 5330 SKIN BOEING 737 737824 13844BZ NM STA 334-344 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17229 28793 A START CART STRUCK THE AIRCRAFT LEAVING A 2" X 2" HOLE IN FUSELAGE SKIN AT STA 334-344, STRINGER 19R. REPAIRED IAW ECRA 5330-03169. A DIP WAS ISSUED TO PERFORM INSPECTIONS ON THE REPAIR AREA WITHIN 12 MONTHS FROM OCTOBER 7, 2002. SEE ECRA 5330-03169, REV A FOR PERMANENT REPAIR. 2 L 7 2 4F RT A16WE 2002100900167 20021009 00167 WP 2002 10 9 CALA0200490 1 20021009 A 5330 SKIN DOUG DC9 DC982 3022082 WP AFT FWD ENTRY DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND A DENT IN L/H FUSELAGE SKIN AFT OF FORWARD ENTRY DOOR. THE DENTED SKIN WAS REMOVED AND NEW SKIN WAS INS TALLED IAW SRM 53-04. 2 L 7 2 4F A6WE 2002100900168 20021009 00168 SO 2002 10 9 C2XA02CL196 1 20021007 A 2720 15793101 SWITCH EMB 135 EMB135LR 3260305 SO TAIL INOPERATIVE A C2XA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SW 27 14514 145303 CLT FLIGHT#3177 THE CREW REPORTED A RUDDER 1/2 FAIL MESSAGE ON CLIMBOUT.THE AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE #1 AND #2 RUDDER PRESSURE SWITCHES.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT W AS RELEASED FOR SERVICES. 2 L 7 2 4F RT T00011AT 2002100900169 20021009 00169 NM 2002 10 9 QXEA0201601 1 20021002 A 2130 502213 SEAL BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 TORN A QXEA K NONE O OTHER DE DESCENT 1 NM 09 414QX 4061 SEA-LOST CABIN PRESSURE AT 10,000 FEET DESCENDING INTO SEA. RAN RAPID DEPRESSURIZATION CHECKLIST. DID NOT WORK IN MANUAL . FLIGHT ATTENDANT REPORTED HEARING POP IN REAR OF CABIN. INSPECTED AND FOUND AFT CARGO DOOR SEAL TORN. REMOVED AND REPL ACED SEAL. GROUND RAN AIRCRAFT. PRESSURIZED. PRESSURE CHECKED GOOD. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002100900170 20021009 00170 NM 2002 10 9 QXEA0201602 1 20021006 A 7930 APT761000100DW TRANSMITTER DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA D RETURN TO BLOCK P NO WARNING INDICATION CR CRUISE 1 NM 09 354PH 6898 6898 498 PDX-RETURNED TO FIELD FOR ENGINE OIL PRESSURE INDICATOR 46 PSI THEN WENT TO 55 PSI AT FLIGHT IDLE AND REMAINED FOR REST OF FLIGHT. NO MATER CAUTION OR MASTER WARNING INDICATIONS. REPLACED #1 ENGINE OIL PRESSURE INDICATOR, NO HELP. OIL PRESS URE DROPPED TO 41 PSI. REPLACED OIL PRESSURE TRANSMITTER. INDICATIONS NORMAL AND STABILIZED. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2002100900171 20021009 00171 NM 2002 10 9 QXEA0201603 1 20021007 A 2610 PU90461R2 DETECTOR DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE J WARNING INDICATION CL CLIMB 1 NM 09 358PH 506 PDX-SMOKE ALARM IN LAVATORY WENT OFF IN CLIMBOUT. RESET, FLIGHT ATTENDANT AND FIRST OFFICER VERIFIED NO SMOKE OR FUMES N OTED. INSTALLED NEW LAVATORY FIRE DETECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002100900173 20021009 00173 NM 2002 10 9 AWXA200200990 1 20021001 A 5720 654646047 ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 0 0 25400 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/4" CRACK WAS FOUND ON LOWER SURFACE L/H WING CLOSE OUT WEB SUPPORT ANGLE 33" OUTBOARD OF THE INBOARD END OF AILERON, WS 538. MAINTENANCE REMOVED THE DAMAGED ANGLE FROM CLOSE OUT WEB WS 538, FABRICA TED A NEW REPLACEMENT ANGLE, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 10. 2 L 7 2 4F RT A16WE 2002100900174 20021009 00174 NM 2002 10 9 AWXA200200991 1 20021003 A 5313 69353521 TIE CLIP BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 0 0 25400 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/4" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 420, STR 9 R/H. MAINTENANCE REM OVED CRACKED STRINGER TIE CLIP AT BS 420, STR 9 R/H, FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP, AND INSTALLED REPAI R PART IAW B737-300 SRM 51-40-02, PG. 38, FIG. 8. 2 L 7 2 4F RT A16WE 2002101000001 20021010 00001 EA 2002 10 10 CA020926001 1 20020919 A 2697 WIRE CNDAIR CL601 CL6012A12 1900303 EA FIRE BOTTLE EXPOSED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WIRING HARNESS FOR THE ENGINE FIRE BOTTLE SQUIBS LOCATED IN THE APU AREA HAD EXPOSED WIRES WHERE THEHARNESS ENTERS THE CONNECTOR PLUG FOR THE SQUIB. 2 L 7 2 4F RT A21AE 2002101000002 20021010 00002 EA 2002 10 10 CA020926002 1 20020909 A 2910 MANIFOLD DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 2 HYD SYSTEM BYPASSING W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) AIR TURNBACK DUE TO NR 2 HYDRAULIC FLUID HOT CAUTION LIGHT ON IN FLIGHT. HYDRAULIC PIPES ARE HOT TO TOUCH ON GROUN D. NR 2 HYDRAULIC PRESSURE MANIFOLD REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002101000003 20021010 00003 EU 2002 10 10 CA020926003 1 20020924 A 2750 SD3456037XA CONTROL CABLE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE TE FLAPS BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FLAP SELECTOR CONTROL CABLE WAS FOUND BROKEN AT THE POINT WHERE THE CABLE EXITS THE FUSELAGE AND CONTINUES ON TO T HE FLAP SELECTOR. A SECOND SPOT ON THE CABLE WAS ALSO ALMOST BROKEN THROUGH WHERE THE CABLE RETURNS FROM THE FLAP SELEC TOR AND REENTERS THE FUSELAGE. BOTH AREAS WERE WHERE THE CABLE GOES AROUND A PULLEY AND DOES A 90 DEGREE TURN. PULLEYS WERE FULLY SERVICEABLE. THIS AREA IS NOT PRONE TO MANY INSPECTIONS AND THIS DEFECT WAS FOUND AS A RESULT OF AN AIR COND ITIONING SNAG. A FLEET CAMPAIGN HAS BEEN INITIATED TO INSPECT OTHER AIRCRAFT. 2 H 7 2 4T 4 T A41EU E4EA 2002101000004 20021010 00004 NM 2002 10 10 CA020926005 1 20020924 A 2910 82950010207 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) HYDRAULIC LINE FOUND CRACKED FROM DRAIN ON LOWER BELLY AND RT WING FAIRING. LIFT DUMP PRESSURE TUBE ASSY IN RT WI NG REPLACED. LINE CRACKED AT FIRST ELBOW FROM I/B END OF LINE. IPC REF 29-00-00 FIG 60 ITEM 140. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002101000005 20021010 00005 NM 2002 10 10 CA020927001 1 20020913 A 2612 FIRE LOOP BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA ENGINE MALFUNCTIONED W F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING IN INSP/MAINT 1 CA (CAN) DURING AN ENGINE GROUND RUN, THAT WAS BEING PERFORMED FOR AN OIL PRESSURE INDICATION PROBLEM, THE FIRE WARNING WAS ACTIVATED. THE ENGINE WAS SHUT DOWN, BOTTLES WERE NOT TRIGGERED. THE ENGINE AND NACELLE ZONES WERE INSPECTED FOR EV IDENCE OF ANY LOCAL HOT SPOTS. NO PROBLEM EVIDENT. THE ENGINE WAS RESTARTED AND AGAIN THE FIRE WARNING WAS TRIGGERED. PEC LOOP WAS REPLACED, AND THE PROBLEM WAS SOLVED. 1946.5 HRS, 2323 CYCLES 2 H 7 2 4T 4 T RT A13NM E00062EN 2002101000006 20021010 00006 EU 2002 10 10 CA020927003 1 20020913 A 3110 972813210 LIGHT PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL OVERHEAD PANEL INTERMITTENT W O OTHER L NO TEST TX TAXI/GRND HDL 1 CA (CAN) AFTER FLIGHT CREW TURNED ON INTERNAL BATTERY POWER THEY NOTICED THAT THE OVERHEAD ELECTRICAL MANAGEMENT POWER PANE L BACKGROUND LIGHTING WAS FLICKERING. SELECTED SWITCHES WERE ALSO FLICKERING. THE CREW CONTINUED WITH NORMAL OPERATIO NS, THE OVERHEAD PANEL BACKGROUND LIGHTING FLICKERED FOR THE COMPLETE FLIGHT. WHEN INTERNAL POWER WAS SELECTED FOR TH E NEXT FLIGHT THE PANEL LIGHTING WAS NORMAL.AFTER RETURNING TO MAINTENANCE BASE THE PANEL CONNECTIONS WERE CLEANED AND I NSPECTED WITH NO FAULTS FOUND. THE FLIGHT CREW REMARKED THAT THEY HAD SEEN SIMILAR PANEL LIGHT FLICKERING ON OTHER 10TH SERIES PC12'S (MSN 401 AND UP). WEATHER CONDITIONS AT THE TIME WAS HEAVY RAIN. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002101000007 20021010 00007 EA 2002 10 10 CA020927005 1 20020924 A 4930 WE38304862 FUEL NOZZLE HONEYWELL WE38007702 CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE APU CRACKED W H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CA P124 (CAN) FUEL LEAK NOTED AT APU. FOUND CRACKED FUEL NOZZLE. APU INOP'D IAW MEL.FUEL NOZZLE AT 2 O'CLOCK POSITION REPLACED . APU OPERATIONAL. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002101000008 20021010 00008 EU 2002 10 10 CA020927006 1 20020922 A 2150 757A000010 ACM AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE AIR CONDITIONING OVERHEATED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) BURNING ODOR REPORTED IN CABIN. NR 2 PACK FOUND OVERHEATED. NR 2 AIR CYCLE MACHINE REPLACED AS PER AMM. 2 L 7 2 4F 4 F RT A28NM E29NE 2002101000009 20021010 00009 2002 10 10 CA020930004 4 20020419 A 2215 ROLL SERVO BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA AILERONS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) DURING APPROACH AUTOPILOT WAS DISCONNECTED AND MANUAL FLYING STARTED. NOTICED AN ABNORMALLY HIGH FORCE NEEDED TO MOVE AILERON CONTROL. LANDING WAS MADE NORMALLY. THE AUTOPILOT ROLL SERVO MOTOR WAS FOUND FAULTY AND WAS REPLACED IA W AMM. OPERATIONAL CHECK PERFORMED WITHOUT REMARKS. THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002101000010 20021010 00010 CE 2002 10 10 CA020930005 1 20020930 A 1430 555225056 RIVET CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE ENGINE INLET BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) INLET COWLING HAD APPROXIMATELY 1/4 OF THE RIVET HEADS MISSING ON THREE CONSECUTIVE RIVETS, PLUS 1 RIVET HEAD LIF TING. LOCATION WAS THE 3RD ROW OF RIVETS FROM THE FRONT OF THE INLET, AT THE 2 O'CLOCK POSITION. 1 L 7 2 4F 4 F A22CE E1NE 2002101000013 20021010 00013 EU 2002 10 10 AHE02062 1 20020904 A 7714 CONNECTOR AGUSTA A109 A109C 0260118 EU ALLSN 250C 250C20R1 03013 GL TACH GEN DISCONNECTED B E8UY A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 35 109TW 1914 7650 295187 NR 1 ENGINE LOW WARNING ILLUMINATED IN FLIGHT. NG DROPPED AND FLICKERED BEFORE BECOMING ZERO. ENGINE RETARDED TO GROUN D IDLE, ALL OTHER INDICATIONS NORMAL. AIRCRAFT LANDED NORMALLY ON ONE ENGINE. NR 1 ENGINE NG TACHOMETER ELECTRICAL CON NECTOR FOUND DETACHED FROM TACH. CONNECTOR RESECURED AND GROUND TEST CARRIED OUT. OPERATION FOUND TO BE NORMAL. ALL O THER ENGINE TACH GENERATORS INSPECTED FOR CONNECTOR SECURITY AND FOUND SECURE. 1 G 7 2 3U 3 U H7EU E4CE 2002101000014 20021010 00014 SW 2002 10 10 ALG2002F00065 1 20020828 A 6310 406040516101 SHAFT BELL BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FREEWHEEL UNIT WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 587AL A4747 53248 CAE847250 SHAFT ON FREEWHEEL UNIT HAS WORN SPLINES BEYOND LIMITS. 1 G 7 1 3U 3 U O H2SW E1GL 2002101000015 20021010 00015 NE 2002 10 10 EGR2002F00010 1 20020902 A 2612 7655009005100 CONNECTOR SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL FIRE DETECTOR CONTAMINATED E EGRA O OTHER N FALSE WARNING AP APPROACH 1 EA 17 5128 9270 760181 NR 1 ENGINE FIRE DETECTOR LIGHT ILLUMINATED ON SHORT FINAL FOR 4 SECONDS, IN HEAVY RAIN WITHOUT AUDIO SIGNAL DURING RUN UP. TRANSMISSION BEARING CAUTION LIGHT ILLUMINATED FOR 10 SECONDS AND SUBSEQUENTLY EXTINGUISHED. REMOVED AND CLEANED FIRE DETECTOR CONNECTOR PLUGS. REINSTALLED, OPS CHECKED GOOD. REMOVED A/C GENERATOR AND INSTALLED SERVICEABLE GENERATO R. OPS CHECK GOOD. 1 G 7 2 3U 3 U H1NE E1GL 2002101000017 20021010 00017 SW 2002 10 10 EHA2002F00006 1 20020718 A 6320 2040403763 PRESSURE SWITCH BELL 205 205A1 1181414 SW LYC T53 T53* 41549 NE TRANSMISSION OIL INTERMITTENT B EHAR O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 03 4750R 30009 LEO7587 MAIN TRANSMISSION OIL PRESSURE SWITCH LIGHT INTERMITTNETLY INOPERATIVE. REPLACED PRESSURE SWITCH. 1 G 7 1 4U 4 U H1SW E1EA 2002101000018 20021010 00018 EU 2002 10 10 EHA2002F00007 1 20020707 A 7712 305731365 INDICATOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TORQUE METER INOPERATIVE B EHAR O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 353EV 2444 TORQUE METER FOUND INOPERATIVE ON START UP. REPLACED TORQUE METER. 1 G 7 1 3U 3 U H9EU E19EU 2002101000019 20021010 00019 EA 2002 10 10 EHA2002F00009 2 20020701 A 7321 32447210 FUEL CONTROL BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA NR 2 ENGINE FAILED B EHAR K NONE O OTHER IN INSP/MAINT 1 AL 03 16974 1556 948 30886 6143 ON APPROACH TO LANDING AT A REMOTE LOCATION, THE PILOT EXPERIENCED A LOW SIDE GOVERNING FAILURE ON THE NR 2 AUTOMATION F UEL CONTROL UNIT. THE AFCU WAS PUT ON IAW MEL AND A FERRY FLIGHT PERMIT WAS ISSUED. THE AIRCRAFT RETURNED AND THE AFCU WAS CHANGED. 1 G 7 1 4U 4 U H4SW E22EA 2002101000020 20021010 00020 NE 2002 10 10 KBMA115460 2 20020905 A 7323 25491641 GOVERNOR SNIAS 350 AS350BA 8680817 EU LYC LTS101 LTS101600A 41560 NE ENGINE FAILED B KBMA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 WP 19 270SH 601 1864 GOVENOR FAILURE DURING FLIGHT. ENGINE DECELERATED TO 60 PERCENT NG. FOUND GOVERNOR BEARING ROUGH AND PHENOLIC GEAR DRI VE SHEARED DRIVE SPLINES. INSTALLED NEW UNIT, GROUND RUN AND OPS FLIGHT PREFORMED AND FOUND SATISFACTORY. 1 G 7 1 3U 3 U NC H9EU E5NE 2002101000021 20021010 00021 EU 2002 10 10 M7K2002F00000 1 20020925 A 6220 350A31191600 STARFLEX SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR DAMAGED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 92MH 1880 2898 4157 DURING MANDATED PRE-START, STAR ARM END BUSHING ADHESIVE BOND INSPECTION IAW MFG SB., BY A QUALIFIED PILOT, ONE OF THR EE STAR ARM BUSHINGS HAD A SLIPPAGE MARK MISALIGNMENT. MAINTENANCE PERSONEL CONFIRMED BUSHING BOND FAILURE. STARFLEX R EMOVED AND REPLACED WITH NEW PART. 1 G 7 1 3U 3 U NC H9EU E19EU 2002101000022 20021010 00022 NE 2002 10 10 R7M005435191 2 20020602 A 7200 ENGINE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE NACELLE MAKING METAL B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 135SJ 0054 ENGINE MAKING METAL. REPLACED WITH LOANER ENGINE. 1 G 7 2 3U 3 U O H88EU E42NE 2002101000023 20021010 00023 2002 10 10 R7M016235185 4 20020522 A 2210 41600297005 MODULE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE AUTO PILOT INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 101HN 99 0162 AUTO PILOT MODULE INOPERATIVE. YELLOW DIAGONAL SPLASH MARKS ON PFD AND AP2. CIRCUIT BREAKER POPPED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002101000024 20021010 00024 EU 2002 10 10 R7M016235278 1 20020528 A 2140 JBS8803 VALVE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE HEATER INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 101HN 396 0162 BLEED AIR HEAT, INOPERATIVE. REPLACED WITH NEW MIXING VALVE, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002101000025 20021010 00025 SW 2002 10 10 R7M5342235162 1 20020404 A 7120 406040506101 HOUSING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE MOUNT FRETTED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 1167 53422 HOUSING TO ENGINE MOUNT IS EXCESSIVELY FRETTED. HOUSING MOUNT BOLTS WERE NOT LOOSE AS THOSE FOUND IN AC. REPLACED WIT H NEW UNIT CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002101000026 20021010 00026 SW 2002 10 10 R7M5342235163 1 20020405 A 7712 407375003107 INDICATOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL COCKPIT STUCK B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 407SJ 85 53422 TORQUE INDICATOR INOPERATIVE, INDICATOR STUCK AT 82 PERCENT, THEN WENT TO FULL DEFLECTION, THEN WENT DEAD. REPLACED WI TH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002101000027 20021010 00027 SW 2002 10 10 R7M5342235164 1 20020423 A 7712 407375003107 INDICATOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL COCKPIT INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 407SJ 32 53422 TORQUE INDICATOR UNIT INOPERATIVE. WILL NOT POWER DOWN CORRECTLY AND READS 5 PERCENT HIGHER THAN ECU. REPLACED WITH NE W UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002101000028 20021010 00028 SW 2002 10 10 R7M5344635168 1 20020415 A 6220 407310101101 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR DEBONDED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 911LN 1105 53446 MAIN ROTOR BEARING DEBONDING. REPLACED WITH NEW UNIT, CORRECTED. 1 G 7 1 3U 3 U O H2SW E1GL 2002101000029 20021010 00029 EU 2002 10 10 R7MR005435256 1 20020613 A 7810 3039621 CLAMP UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE EXHAUST STUB CRACKED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 135SJ 2098 0054 EXHAUST STUB CLAMP CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002101000030 20021010 00030 EU 2002 10 10 R7MR016235263 1 20020605 A 7740 304450101 COMPUTER UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ENGINE DATA INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 101HN 412 0162 DATA COLLECTION UNIT (DCU). UNIT INOPERATIVE. LOOSES TOTAL COUNT FORWARD AND BACKWARD. REPLACED WITH NEW UNIT, CORREC TED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002101000031 20021010 00031 EU 2002 10 10 R7MR102435220 1 20020607 A 7931 704A37642042 TRANSMITTER SNIAS 350 AS350D 8680803 EU LYC LTS101 LTS101600A 41560 NE OIL PRESSURE INOPERATIVE B R7MR O OTHER O OTHER NR NOT REPORTED 1 NM 07 350RM 9314 1024 ENGINE OIL PRESSURE TRANSMITTER INOPERATIVE, NO OIL PRESSURE NDICATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E5NE 2002101000032 20021010 00032 EU 2002 10 10 02280303 1 20021007 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 303UE 41015 During preflight inspection, the crew reported that the aft section of the emergency floor track lights was inoperative. Maintenance personnel secured the connector to the aft section of emergency floor track lights. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002101000033 20021010 00033 EU 2002 10 10 R7MR102435221 1 20020607 A 7931 704A37642042 TRANSMITTER SNIAS 350 AS350D 8680803 EU OIL PRESSURE FLUCTUATES B R7MR O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 350RM 9344 1024 ENGINE OIL PRESSURE TRANSMITTER CAUSES OIL PRESSURE GAUGE TO FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2002101000034 20021010 00034 EU 2002 10 10 R7MR102435222 1 20020706 A 7931 704A37642042 TRANSMITTER SNIAS 350 AS350D 8680803 EU LYC LTS101 LTS101600A 41560 NE OIL PRESSURE INOPERATIVE B R7MR O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 350RM 9362 1024 ENGINE OIL PRESSURE TRANSMITTER INOPERTIVE. NO OIL PRESSURE INDICATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E5NE 2002101000035 20021010 00035 EU 2002 10 10 R7MR103535241 1 20020415 A 6420 704A33633116 BEARING SNIAS 350 AS350B 8680801 EU LYC LTS101 LTS101600A 41560 NE TAIL ROTOR WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 792LF 167 1035 ELASTOMERICS OF BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, FROM EACH KIT CORRECTED PROBLEM. 4 HAL F SHELLS EQUAL 1 KIT. 1 G 7 1 3U 3 U H9EU E5NE 2002101000036 20021010 00036 NE 2002 10 10 R7MR136935223 2 20020610 A 7210 70BM055030 FLANGE SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE REDUCTION GEAR WORN B R7MR K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 5771C 11456 1369 REDUCTION GEAR, LEAKING OIL AT MO4 CONNECTION GROOVE. WORN FLANGE. BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS , CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002101000037 20021010 00037 EU 2002 10 10 R7MR324935154 1 20020423 A 6730 SC5083 CONTROL SERVO SNIAS 350 AS350B3 8680954 EU MAIN ROTOR LEAKING B R7MR K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 52281 918 3249 SERVO CONTROL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2002101000038 20021010 00038 EU 2002 10 10 R7MR324935236 1 20020612 A 6220 LINER SNIAS 350 AS350B3 8680954 EU TMECA ARRIUS ARRIU2F NE STARFLEX WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 105LN 1157 3249 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E34NE 2002101000039 20021010 00039 NE 2002 10 10 R7MR325135212 2 20020607 A 7261 350A54113800 VENT LINE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE OIL CRACKED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 106LN 1024 3251 OIL TUBE AIR VENT CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002101000040 20021010 00040 EU 2002 10 10 R7MR325135237 1 20020612 A 6220 LINER SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE STARFLEX WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 106LN 149 3251 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002101000041 20021010 00041 EU 2002 10 10 R7MR325135247 1 20020227 A 6410 704A33633116 BEARING SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 106LN 271 3251 TAIL ROTOR BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, FROM 1 EACH KIT CORRECTED PROBL EM. 4 HALF SHELLS EQUALS 1KIT. 1 G 7 1 3U 3 U H9EU E19EU 2002101000042 20021010 00042 EU 2002 10 10 R7MR325235214 1 20020607 A 3340 356H2802 POWER SUPPLY SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE EXTERIOR LIGHTS INOPERATIVE B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 392LG 1015 3252 POWER SUPPLY BOX INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002101000043 20021010 00043 EU 2002 10 10 R7MR325235248 1 20020218 A 6420 704A33633116 BEARING SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 392LG 536 3252 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACING WITH NEW UNIT FROM 1 EACH KIT CORRECTED PROBLEMS. 4 HALF SHELLS EQUALS 1 KIT. 1 G 7 1 3U 3 U H9EU E19EU 2002101000044 20021010 00044 2002 10 10 R7MR333635206 4 20020531 A 3452 066011410101 TRANSPONDER SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE CABIN ERRATIC B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 396LG 199 3336 TRANSPONDER INOPERATIVE, GIVES ERRATIC READINGS. REPLACED WITH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002101000045 20021010 00045 EA 2002 10 10 COMA0260563 1 20021003 A 3230 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 927CA 20427 7031 GEAR DISAGREE WARNING, NOSE LANDING GEAR DID NOT INDICATE SAFE ON 1ST GEAR EXTENSION.REPLACED THE NOSE LANDING GEAR SELE CTOR VALVE. 2 L 7 2 4F RT A21EA 2002101000046 20021010 00046 NM 2002 10 10 F3LA200200265 1 20020925 A 2150 A/C PACK BOEING 737 7372Y5 1384554 NM A/C BAY MALFUNCTIONED A F3LA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 118RW 23040 AIR TURN BACK. FLIGHT CREW REPORTED SMOKE IN CABIN, LT WING/BODY OVERHEAT ILLUMINATED AND RT PACK TRIPPED OFF. DECLARE D AN EMERGENCY AND RETURNED TO DEN. AIRCRAFT LANDED WITHOUT INCIDENT. ON APPROACH, AILERONS WERE DIFFICULT TO MOVE AND HAD A SHUDDER BELOW 180 KNOTS. REPOSITIONED DETECTION LINE FOUND TOUCHING BLEED DUCT IN FWD LT AFT CARGO COMPARTMENT. PLACARDED RT PACK PER MEL 21-1. PERFORMED A FLIGHT CONTROL MOVEMENT CHECK WITH NO DISCREPANCIES NOTED. PERFORMED VISU AL INSPECTION OF AILERON CONTROL SYSTEM, WITH NO DEFECTS NOTED. COMPLIED WITH FLAP MOVEMENT CHECK, WITH NO DEFECTS NOTE D. 2 L 7 2 4U RT A16WE 2002101000050 20021010 00050 EU 2002 10 10 R7MR340235216 1 20020607 A 2910 MA12401 PRESSURE SWITCH SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE HYD SYSTEM INTERMITTENT B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 385LR 202 3402 PRESSURE SWITCH OPERATES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002101000052 20021010 00052 EA 2002 10 10 COMA0260567 1 20021005 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 467CA 7637 CARGO DOOR CAUTION MESSAGE.INSPECTED CARGO DOOR, NO DEFECTS NOTED, DOOR WARNING SYSTEM WAS PREVIOUSLY ON DEFERRED MAINTE NANCE LIST. 2 L 7 2 4F RT A21EA 2002101000053 20021010 00053 EA 2002 10 10 COMA0260569 1 20021005 A 2420 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA LEFT FAILED A COMA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 01 973CA 13711 7146 NUMBER ONE GENERATOR AND INTEGRATED DRIVE GENERATOR WARNING DURING TAKE OFF.REPLACED THE LEFT INTEGRATED DRIVE GENERATOR . 2 L 7 2 4F RT A21EA 2002101000054 20021010 00054 SW 2002 10 10 R7MR534223515 1 20020418 A 6410 406016100119 BLADE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR OUT OF BALANCE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 1186 53422 TAIL ROTOR BLADE HAS AN OUT OF BALANCE CONDITION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002101000067 20021010 00067 EA 2002 10 10 COMA0260574 1 20021006 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 403CA 7428 GEAR DISAGREE MESSAGE.COULD NOT DUPLICATE, FOUND NO FAULTS WITH GEAR EXTENSION OR RETRACTION SYSTEM. 2 L 7 2 4F RT A21EA 2002101000068 20021010 00068 EA 2002 10 10 COMA0260575 1 20021005 A 2420 755469D IDG CNDAIR CL600 CL6002B19 1900309 EA RIGHT FAILED A COMA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 01 927CA 8798 7031 NUMBER TWO GENERATOR FAILED ATER TAKE OFF.REPLACED THE RIGHT INTEGRATED DRIVE GENERATOR. 2 L 7 2 4F RT A21EA 2002101000073 20021010 00073 NM 2002 10 10 F3LA200200307 1 20021002 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR BEAM UPPER CHORD AT BS 294.5. FABRICATED REPLACEMENT PARTS AND INSTALLED REPAIR PER SRM 53-10-51, SRM 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002101000075 20021010 00075 NM 2002 10 10 F3LA200200310 1 20021002 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON 312 FLOOR BEAM UPPER CHORD. FABRICATED AND INSTALLED REPLACEMENT UPP ER CHORD PER SRM 51-40-02, 51-40-06 AND SOPM 20-41-01. 2 L 7 2 4F RT A16WE 2002101000076 20021010 00076 EA 2002 10 10 COMA0260577 1 20021008 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 420CA 7451 FLAPS FAIL MESSAGE AFTER LANDING.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002102300114 20021023 00114 NM 2002 10 23 F3LA200200325 1 20021006 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT, BS 294.5 TO 312, LBL 12. REPLACED FLOOR SUPPORT PER S RM 53-10-51, 51-40-02 AND EA 53-737-181. 2 L 7 2 4F RT A16WE 2002101000079 20021010 00079 NM 2002 10 10 F3LA200200315 1 20021004 A 5320 THRESHOLD BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SILL PLATE IN FRONT OF C2 DOOR CORRODED. REPLACED THR ESHOLD WEB PER SRM 51-40-02 AND 51-30-01. 2 L 7 2 4F RT A16WE 2002101000083 20021010 00083 NM 2002 10 10 F3LA200200320 1 20021004 A 5315 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED CORROSION BY SCREW HOLES IN REAR GALLEY FLOOR BEAMS AT BS 986. FABRICATED AND INS TALLED REPLACEMENT T CAP PER SRM 53-00-01, 53-30-01 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002102300115 20021023 00115 NM 2002 10 23 F3LA200200326 1 20021006 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT, BS 328 TO 344, LBL 12. REPLACED FLOOR SUPPORT PER SRM 53-10-51, 51-40-02 AND EA 53-737-181. 2 L 7 2 4F RT A16WE 2002102300116 20021023 00116 NM 2002 10 23 F3LA200200327 1 20021006 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT, BS 312 TO 328, LBL 12. FABRICATED AND INSTALLED REPLA CEMENT FLOOR SUPPORT PER SRM 51-40-02, 51-40-02, SOPM 20-41-02 AND EA 53-737-181. 2 L 7 2 4F RT A16WE 2002102300117 20021023 00117 NM 2002 10 23 F3LA200200328 1 20021006 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT, BS 328 TO 344, RBL 11. REPLACED FLOOR SUPPORT PER SRM 53-10-01, FIG. 101, 51-40-02 AND EA 53-737-181. 2 L 7 2 4F RT A16WE 2002101000089 20021010 00089 WP 2002 10 10 GTIA020685 1 20020621 A 2697 WIRE DOUG DC9 DC981 3022081 WP COCKPIT OUT OF POSITION A GTIA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 810NK 48015 MCO - FLT 927 - LEFT ENGINE FIRE DETECT LOOP 'B' LIGHT ILLUMINATED WITHOUT FIRE WARNING. COMPLETE QRH PROCEDURE. SWITC HED TO NR 1 'A' LOOP ONLY ON PANEL. TESTED A/B LOOP NR 2 ENGINE, OPS OK. INSPECTED ENTIRE LEFT ENGINE LOOP SYSTEM AND PERFORM BITE. FOUND LOOP B LEFT ENGINE (AMBER) LIGHT SWITCH ASSY IN COCKPIT ON OVERHEAD PANEL WIRES MAKING CONTACT WITH FRAME. ADJUSTED WIRE POST ON SWITCH IAW MD80 MM 26-11-00 OPERATION CHECK OK. (M) 2 L 7 2 4F A6WE 2002102300118 20021023 00118 NM 2002 10 23 F3LA200200329 1 20021006 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR BEAM UPPER CHORD, BS 344. REPAIRED FLOORBEAM PER SRM 53-10-51 AND EA 53-737-184. 2 L 7 2 4F RT A16WE 2002101000090 20021010 00090 2002 10 10 GTIA020687 4 20020622 A 2565 SLIDE DOUG DC9 DC983 3022083 WP L2 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 827NK 49793 DTW - FOUND L2 DOOR SLIDE PACK FELL OFF DOOR AND GOT DAMAGED. REMOVED AND REPLACED L2 DOOR SLIDE PACK IAW MD80 MM 25-62 -00. (M) 2 L 7 2 4F RT A6WE 2002101000091 20021010 00091 WP 2002 10 10 0203401225 1 20021002 A 2822 608473 PUMP DOUG DC10 DC1030 3023501 WP AUX FUEL TANK INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 225NW 11595 4075 46582 PUMP WAS INSTALLED IN THE LOWER AUXILIARY FUEL TANK. IT WAS REMOVED AS PART OF EO 2815-01008 WHICH DEACTIVATES THE LOWER AUXILIARY FUEL TANK. PUMP FAILED THE STANDARD MEGGAR BENCH TEST. THE PUMP WAS DASSEMBLED AND FOUND TO HAVE CHAFING ON T HE WIRING HARNESS. 2 L 7 3 4F A22WE 2002101000092 20021010 00092 WP 2002 10 10 GTIA020688 1 20020619 A 2797 WIRE DOUG DC9 DC982 3022082 WP COCKPIT BROKEN A GTIA O OTHER N FALSE WARNING TO TAKEOFF 1 GL 23 820NK 49126 DEN - FLT 980A - SETTING MAX POWER FOR DEPARTURE GOT THE FLAP AURAL WARNING WITH FLAPS SELECTOR 4.5 OPTIUM. TROUBLE SHO T SYSTEM FOUND FLAP TAKEOFF SETTING WARNING S/W AT CONNECTOR AT D-1 1194 PINE BROKEN WIRE REPAIRED IAW MM CH 20 TAKEOFF WARNING SYSTEM. OPS CHECKED GOOD IAW MD MM 27-52-00 OK TO CONTINUE. (M) 2 L 7 2 4F A6WE 2002101000093 20021010 00093 2002 10 10 GTIA020950 4 20020906 A 2565 SLIDE DOUG DC9 DC982 3022082 WP SERVICE DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 AFT SERVICE DOOR SLIDE CAME OFF OF DOOR. NEED TO BE REINSTALLED. AFT SERVICE DOOR SLIDE REINSTALLED. (M) 2 L 7 2 4F A6WE 2002101000094 20021010 00094 WP 2002 10 10 GTIA020951 1 20020828 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND SCRATCH AT FS 398.500 BETWEEN L17 AND L18L REQUIRES REPAIR. REMOVED DAMAGED AREA. FABRICATED DOUBLER, FILL ER, FINGER DOUBLER. INSTALLED DOUBLERS AND FILLER. (M) 2 L 7 2 4F A6WE 2002101000095 20021010 00095 WP 2002 10 10 GTIA020952 1 20020829 A 7830 THRUST REVERSER DOUG DC9 DC982 3022082 WP NR 2 ENGINE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 NR 2 ENGINE T/R HAS SHARP DENT AT 7 O'CLOCK POSITION, OUTER SURFACE. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILL ER. INSTALLED REPAIR. (M) 2 L 7 2 4F A6WE 2002101000096 20021010 00096 EU 2002 10 10 SIMA200219115 1 20020705 A 5240 DOOR SAAB SF340 340B 7860101 EU ELECTRICAL POWER DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 FOUND LEFT ELECTRICAL POWER PANEL HAS 2 DENTS. PERFORMED EDDY CURRENT INSPECTION, NO DEFECTS. DENT WITHIN SAAB 340 SRM 55-70-10 AND 51-10-10 LIMITS. (M) 2 L 7 2 4T RT A52EU 2002101000098 20021010 00098 NE 2002 10 10 R7MR706335141 2 20020509 A 7250 410106701 SEAL RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SECTION WORN B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 163BK 594 7063 FIRST TURBINE SHROUD SEAL RING WORN BEYOND SERVICE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002101000100 20021010 00100 2002 10 10 DHL2002805052 4 20021009 A 2397 WIRE DOUG DC8 DC873F 302199F WP A DHLA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 805DH 46125 1) DURING TAXI IN, NOTED ELECTRICAL BURNING SMELL IN CABIN ENTRY AREA2) REPAIRED BROKEN WIRE AT RADIO RACK C/B PER MM 20-50-1. FUEL FLOW C/B REPLACED, LOOSE CONTACTS, AND OPS CK'D PER MM 73-30-1 OK. INSTALLED NEW WATER SEPERATOR BAGS & L EAK CK'D PER MM 21-55-3, OK 2 L 7 4 4F RT 4A25 2002102300121 20021023 00121 NM 2002 10 23 F3LA200200332 1 20021008 A 5320 ANGLE BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 2050 22733 DURING C-2 CHECK, INSPECTION REPORTED RT AFT WING TO BODY FAIRING SUPPORT ANGLE CRACKED AT STRINGER 20, BS 727-727B. FA BRICATED AND INSTALLED REPLACEMENT SUPPORT ANGLE PER SRM 51-10-02, SRM 51-30-00 AND BOEING DRAWING 65-48657. 2 L 7 2 4F RT A16WE 2002101000101 20021010 00101 EU 2002 10 10 SIMA200219119 1 20020705 A 5240 DOOR SAAB SF340 340B 7860101 EU ELECTRICAL POWER DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 ABI - RIGHT ELECTRICAL POWER PANEL HAS ONE DENT. PERFORMED EDDY CURRENT INSPECTION, NO DEFECTS NOTED. DENTS FOUND WITH IN SAAB 340 SRM 52-40-12 AND 51-10-10 LIMITS. (M) 2 L 7 2 4T RT A52EU 2002101000102 20021010 00102 2002 10 10 R7MR707735204 4 20020606 A 3442 78805192008 ANTENNA BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101600A 41560 NE WX RADAR INOPERATIVE B R7MR O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 420MB 9054 7077 WEATHER RADAR ANTENNA INOPERATIVE, HEADING ERROR MESSAGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002101000103 20021010 00103 NM 2002 10 10 USAA020340 1 20020723 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 43569 23739 CLT - FOUND SKIN CRACKED 2 INCHES, ABOVE S24L FORWARD OF FS 727E. DAMAGE REMOVED, INSTALLED EXTERNAL DOUBLER 10 INCHES BY 8 INCHES PER SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2002101000104 20021010 00104 NM 2002 10 10 USAA020344 1 20020822 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 778AU 32594 24980 CLT - FOUND HORIZONTAL STABILIZER CRACKED 1.5 INCH, LEFT LOWER HORIZ STAB SKIN STATION 118 AT REAR SPAR. INSTALLED DOUB LER PER TR 55-10-07 REV B AND EA 74663. (M) 2 L 7 2 4F RT A16WE 2002101000105 20021010 00105 NM 2002 10 10 USAA020360 1 20020906 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 44561 23510 CLT - FOUND SKIN CRACKED 2.5 INCHES, BELOW RIGHT LIGHT AFT OF FLAP TO FUSELAGE FAIRING. INSTALLED DOUBLER AND TRIPLER P ER EA 86586. (M) 2 L 7 2 4F RT A16WE 2002101000106 20021010 00106 NM 2002 10 10 USAA020362 1 20020912 A 7120 310A102016 MOUNT BOEING 737 737401 1384701 NM PYLON WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 38733 23984 PIT - FOUND BEARING BORE .005 INCH BEYOND LIMITS, UNIT HAS ONLY ONE BEARING FORWARD HOLE. OVERSIZED 0.005 INCH, MACHINE D TO 1.445-1.4430 PER TYPICAL REPAIR 54-50-08 REV B. (M) 2 L 7 2 4F RT A16WE 2002101000107 20021010 00107 NM 2002 10 10 USAA020363 1 20020912 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 45766 23595 CLT - FOUND SKIN CRACKED 2 INCHES, LOWER EDGE STRINGER 23L BETWEEN STATION 727D AND 727E. INSTALLED DOUBLER PER TR 53-6 0-0. (M) 2 L 7 2 4F RT A16WE 2002101000108 20021010 00108 EU 2002 10 10 USAASA02076 1 20020908 A 3350 321430 BATTERY AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 720US 1089 PHL - DURING WEEKLY CHECK, FOUND THE RIGHT BATTERY AT THE RIGHT OVERWING EXIT INOPERATIVE. MAINTENANCE REPLACED THE EME RGENCY POWER SUPPLY UNIT BATTERIES. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002101000109 20021010 00109 SW 2002 10 10 YBM2002F00000 1 20020912 A 2433 801002 CONVERTER BELL 47 47G 1181002 SW FRNKLN 6AV350 6V350* 27043 EA ELECTRICAL FAILED E YBMA K NONE O OTHER IN INSP/MAINT 1 NE 05 950B 1500 693 E6003 VOLTAGE CONVERTER (28V TO 14V) FAILED IN FLIGHT AND PASSED 28V TO RADIO CAUSING RADIO FAILURE DUE TO BLOWN ZEMOR DIODE. RADIO AND VOLTAGE CONVERTER WERE EXCHANGED AS CORES FOR NEW. 1 G 7 1 3O 3 O H1 E9EA 2002101000110 20021010 00110 EU 2002 10 10 YT22002F00000 1 20020812 A 6520 350A33020005 GEARBOX SNIAS 350 AS350B 8680801 EU MAKING METAL B YT2R K NONE O OTHER IN INSP/MAINT 1 WP 01 5806B 1836 1924 GEARBOX MAKING METAL. 1 G 7 1 3U H9EU 2003020500105 20030205 00105 2003 2 5 USAASA02078 4 20020909 A 2565 D39011101 SLIDE AIRBUS A319 A319112 3930323 EU LEFT SHORTED A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 716UW 2389 1055 CLT - THE FORWARD EMERGENCY POWER SUPPLY UNIT INDICATED AN EXTERNAL LIGHT FAULT. MAINTENANCE REPLACED AN EMERGENCY POWE R SUPPLY UNIT, HOWEVER, THE EXTERNAL LIGHT FAULT CONTINUED. THE FORWARD ESCAPE SLIDES WERE THEN REPLACED. SYSTEM OPERA TIONALLY CHECKED OK. SUBSEQUENT REPAIR TO THE SLIDE, S/N 0A3629, WAS THE REPLACEMENT OF THE LAMP HARNESS'. (M) 2 L 7 2 4F RT A28NM 2002101000111 20021010 00111 EU 2002 10 10 YT2R110924 1 20020812 A 6520 350A33020005 GEARBOX SNIAS 350 AS350B 8680801 EU TAIL ROTOR MAKING METAL B YT2R K NONE O OTHER IN INSP/MAINT 1 WP 01 5806B 1836 1924 GEARBOX MAKING METAL. 1 G 7 1 3U H9EU 2002101000114 20021010 00114 EU 2002 10 10 USAASA02079 1 20020912 A 3350 321430 BATTERY PACK AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 725UW 1135 CLT - THE EMERGENCY LIGHT TEST INDICATED A 'L FWD LT' FAULT. MAINTENANCE REPLACED THE BATTERY PACK FOR THE LEFT FORWARD LIGHT. OPERATIONALLY CHECKED AND TESTED OK. (M) 2 L 7 2 4F RT A28NM 2002101000115 20021010 00115 NM 2002 10 10 USAASB02172 1 20020916 A 3260 189929 SENSOR BOEING 737 737301 1384611 NM NLG OUT OF ADJUST A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 356US 23559 CLT - FLT 565 - IN PREPARATION FOR LANDING AT CLT, CREW ADVISED THEY DID NOT RECEIVE A NOSE LANDING GEAR GREEN SAFE LIGH T AFTER GEAR EXTENSION. CREW RECYCLED GEAR WITH NO HELP. QUICK REF HANDBOOK PROCEDURES WERE THEN FOLLOWED AND NORMAL G EAR INDICATIONS WERE RECEIVED ONCE GEAR HANDLE WAS CYCLED THROUGH 'OFF' POSITION. FLIGHT LANDED WITHOUT FURTHER INCIDEN T. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NOSE LANDING GEAR DOWNLOCK SENSOR GAP OUT OF LIMITS. SHIMMED DOWN LOCK SENSOR CORRECTLY PER MM 32-61-51. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002101000116 20021010 00116 NM 2002 10 10 USAASB02173 1 20020916 A 3260 189929 DOWNLOCK SENSOR BOEING 737 737401 1384701 NM RT MLG MALFUNCTIONED A USAA O OTHER N FALSE WARNING DE DESCENT 1 EA 19 422US 23989 PHL - FLT 26 - AFTER TAKEOFF, EN ROUTE TO PHL, CREW REPORTED THE RT MLG GREEN LIGHT FLICKERED ON FOR APPROXIMATELY ONE M INUTE WHEN GEAR HANDLE WAS PLACED TO THE OFF POSITION. UPON GEAR EXTENSION IN PHL, THE RIGHT MLG RED UNSAFE LIGHT REMAI NED ILLUMINATED WITH GREEN LIGHT EXTINGUISHED. CREW RECYCLED GEAR WITH NO HELP. A TOWER FLYBY WAS ACCOMPLISHED AND GEA R WAS VERIFIED DOWN AND LOCKED THROUGH VIEWPORTS. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED AT PHL WITHOUT FURTHE R INCIDENT. AIRCRAFT STOPPED AT THE END OF THE RUNWAY AND WAS TOWED TO THE GATE. MAINTENANCE CONFIRMED FAULT AND REMOV ED AND REPLACED THE RIGHT MAIN LANDING GEAR DOWNLOCK SENSOR. OPERATIONAL CHECK OF INDICATION SYSTEM CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2002101000120 20021010 00120 NM 2002 10 10 F3LA200200269 1 20020929 A 5320 CHANNEL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED LT. AFT LAVATORY WALL HAT CHANNEL, BS 992, CORRODED BEYOND LIMITS PER SRM 53-60-5 1. FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 51-40-02, 51-4-05 AND SOPM 20-44-04. 2 L 7 2 4F RT A16WE 2002101000121 20021010 00121 NM 2002 10 10 F3LA200200271 1 20020930 A 5320 CHANNEL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3063 23257 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON RT LAVATORY HAT CHANNEL FOR WALL ATTACH ANGLE, RBL 20. FABRICATED AN D INSTALLED HAT SECTION PER BOEING DRAWING 65-73223 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002101000124 20021010 00124 NM 2002 10 10 F3LA200200274 1 20020930 A 5320 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 3230 26301 DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL SPLICE STRIP CORRODED AT BS 727D +4. FABRICATED AND INSTALLED REPLACEMENT PART PER SRM 51-10-01 AND 51-20-01. 2 L 7 2 4F RT A16WE 2002101000133 20021010 00133 WP 2002 10 10 UPS02839258 1 20020801 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 MAIN CABIN FLOORBEAM IS CORRODED BEYOND LIMITS AT STA 920 AT RBL 65. CUTOUT CORRODED SECTION OF FLOO RBEAM, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL, FABRICATED AND INSTALLED FLOORBEAM SECTION IAW UPS ENGINEERING FILE NUM BER DC8-53-20237, AND SAA SK806-663. 2 L 7 4 4F RT 4A25 2002101000135 20021010 00135 WP 2002 10 10 UPS02839259 1 20020802 A 5320 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 STA -52 TO -67 FINGER DOUBLER AND WEB ARE CORRODED BEYOND LIMITS AT LBL 60. REMOVED FINGER DOUBLER, CUTOUT DAMAGE ON WEB, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER, DOUBLER, AND FINGER DOUBLER IAW SR08530036. 2 L 7 4 4F RT 4A25 2002102300122 20021023 00122 NM 2002 10 23 F3LA200200333 1 20021008 A 5330 SKIN BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED CRACKED SKIN AT AFT ENTRY DOOR CUTOUT FWD LOWER CORNER, APPROX .25 INCH IN LENGTH. REPAIRED PER SRM 53-30-3, FIGURE 24. 2 L 7 2 4F RT A16WE 2002102300123 20021023 00123 NM 2002 10 23 F3LA200200334 1 20021008 A 5330 SKIN BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED FWD SERVICE DOOR CUTOUT SKIN CRACKED AT AFT LOWER CORNER. REPAIRED SKIN PER SRM 5 3-30-3. 2 L 7 2 4F RT A16WE 2002102300125 20021023 00125 NM 2002 10 23 F3LA200200335 1 20021008 A 5210 STRUCTURE BOEING 737 7372L9 1384497 NM ENTRY DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED FWD ENTRY DOOR AFT LOWER THRESHOLD CRACKED AT FWD EDGE. REPAIRED PER SRM 52-30-3 AND BOEING DRAWING 65-02938. 2 L 7 2 4F RT A16WE 2002101000140 20021010 00140 SO 2002 10 10 RAIA00210277 1 20021004 A 2742 3621001007 CONTROL UNIT EMB 145 EMB145 3260210 SO FAILED A RAIA O OTHER J WARNING INDICATION DE DESCENT 1 CE 03 809HK 4001 3935 145187 5324-RIC- UPON DESCENT INTO PIT PITCH TRIM 1&2 FAILED. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTRO L UNIT, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002101000141 20021010 00141 2002 10 10 RAIA00210278 4 20021006 A 3425 7003360948 COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 550HK 13688 1902 41039 5607-STL- LEFT SIDE AHRS SHOWS 6 DEGREES NOSE DOWN. MAINTENANCE REMOVED AND REPLACED THE AHRS COMPUTER, OPS CK OK. 2 L 7 2 4T RT A41NM 2002101000142 20021010 00142 2002 10 10 RAIA00210279 4 20021006 A 3425 1FC8 RELAY JETAIR JETSTM JETSTM4101 1500501 EU FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 550HK 41039 5607-STL- LEFT SIDE AHRS SHOWS 25 DEGREES NOSE DOWN. MAINTENANCE REMOVED AND REPLACED THE 1FC8 RELAY SWITCHING UNIT, OPS CK OK. 2 L 7 2 4T RT A41NM 2002102300126 20021023 00126 NM 2002 10 23 F3LA200200336 1 20021008 A 5311 FRAME BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FRAME AT BS 747, RBL 6, WL 148. FABRICATED AND INSTALLED REPAIR PART S PER SRM 53-10-4, 53-10-1 AND 51-30-02. 2 L 7 2 4F RT A16WE 2002102300133 20021023 00133 NM 2002 10 23 F3LA200200340 1 20021008 A 5320 STRAP BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SPLICE, BS 504, WL 155. REPLACED STRAP PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 2002102300134 20021023 00134 NM 2002 10 23 F3LA200200341 1 20021008 A 5320 STRAP BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOORBOARD SPLICE STRAP, BS 772, WL 157. REPLACED STRAP PER SRM 51-3 0-2. 2 L 7 2 4F RT A16WE 2002101000143 20021010 00143 NM 2002 10 10 F3LA200200342 1 20021008 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM 813 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM, BS 813, LBL 12, WL 157. FABRICATED AND INSTALLED RE PLACEMENT PARTS PER SRM 53-10-5 AND 51-30-02. 2 L 7 2 4F RT A16WE 2002101000144 20021010 00144 NM 2002 10 10 F3LA200200343 1 20021008 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 813 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR BEAM, BS 813, LBL 8, WL 157. REPAIRED DAMAGED AREA PER S RM 53-10-1 AND 53-10-5. 2 L 7 2 4F RT A16WE 2002102300135 20021023 00135 NM 2002 10 23 F3LA200200344 1 20021008 A 5241 SKIN BOEING 737 7372L9 1384497 NM GALLEY DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED FWD GALLEY DOOR INNER DOOR SKIN CRACKED AT ATTACH RIVET, FWD EDGE, CENTER SPAN. R EMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-30-02, 51-10-02 AND 51-21-0. 2 L 7 2 4F RT A16WE 2002101000145 20021010 00145 NM 2002 10 10 F3LA200200345 1 20021008 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 813 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM, BS 813, RBL 8, WL 157. REMOVED DAMAGED AREA, FABRIC ATED AND INSTALLED REPAIR PARTS PER SRM 53-10-5 AND 51-30-02. 2 L 7 2 4F RT A16WE 2002102300136 20021023 00136 NM 2002 10 23 F3LA200200346 1 20021008 A 5730 SKIN BOEING 737 7372L9 1384497 NM LT WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED LT WING FIXED LE CRACKED ON INBD SIDE OF NR 2 SLAT, INBD AUX TRACK CUTOUT. REPAIR ED CRACK PER SRM 57-20-L1 AND MM 51-21-021. 2 L 7 2 4F RT A16WE 2002101100007 20021011 00007 NM 2002 10 11 SWAA022307 1 20020930 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 724SW 27856 EEPLS COVER LOOSE AT FWD CABIN. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2002101100008 20021011 00008 2002 10 11 SWAA022310 4 20021002 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED BC4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002101100009 20021011 00009 2002 10 11 SWAA022311 4 20021002 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002101100010 20021011 00010 NM 2002 10 11 SWAA022312 1 20021002 A 5754 6546421 SLAT BOEING 737 7372H4 138448C NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 092SW 22964 DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT DELAMINATED AT INBD T/E. REMOVED AND REPLACED NR 1 L/E SLAT PER MM. 2 L 7 2 4F A16WE 2002101100011 20021011 00011 NM 2002 10 11 SWAA022313 1 20021003 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 440, STR 4R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2002101100012 20021011 00012 NM 2002 10 11 SWAA022314 1 20021003 A 5330 6545765 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, ABOVE STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002101100013 20021011 00013 NM 2002 10 11 SWAA022315 1 20021003 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 12L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002101100014 20021011 00014 NM 2002 10 11 SWAA022316 1 20021003 A 5313 6527314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 727E AT STR 9R AND BS 597 AT STR 9L. REMO VED AND REPLACED TIE CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002101100015 20021011 00015 NM 2002 10 11 SWAA022317 1 20021002 A 5230 6545871 SKIN BOEING 737 7373H4 1384600 NM FWD CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR FWD LOWER FRAME CRACKED ABOVE LOWER STOP FITTING. REMOVED AND REPLACE D LOWER FRAME SECTION PER CCO. 2 L 7 2 4F RT A16WE 2002101100016 20021011 00016 NM 2002 10 11 SWAA022319 1 20021003 A 5330 6545785 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED SPECIAL VISIT, FOUND WINDOW CUTOUTS CRACKED AT RT WINDOWS NR 2, NR 3, NR 4, NR 5, NR 8, NR 9, NR 10 AND NR 25. REPAIRED FRAMES PER SWA EA AND SRM. 2 L 7 2 4F A16WE 2002101100017 20021011 00017 NM 2002 10 11 SWAA022202 1 20020922 A 3350 101073 LENS BOEING 737 7372H4 138448C NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EXIT LIGHT LENS PER MM. 2 L 7 2 4F A16WE 2002101100018 20021011 00018 NM 2002 10 11 SWAA022204 1 20020919 A 5755 65C25242 SPOILER BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED BC2 CHECK, FOUND NR 4 GROUND SPOILER INBD HINGE FITTING CRACKED. REMOVED AND REPLACED NR 4 GROUND SPOI LER PER MM. 2 L 7 2 4F RT A16WE 2002101100019 20021011 00019 NM 2002 10 11 SWAA022205 1 20020920 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CRACKED AT BS 190, WL 208 AND RBL 29. REPAIRED CREASE BEAM PER BFG ER. 2 L 7 2 4F RT A16WE 2002101100020 20021011 00020 NM 2002 10 11 SWAA022206 1 20020920 A 5520 65C25778 HINGE BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 751SW 29803 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB NR 1, NR 2, NR 3 AND NR 4 HINGES PER BOEING SB. 2 L 7 2 4F RT A16WE 2002101100021 20021011 00021 NM 2002 10 11 SWAA022207 1 20020920 A 5520 65C25798 HINGE BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 751SW 29803 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB NR 2, NR 3 AND NR 4 HINGES PER BOEING SB. 2 L 7 2 4F RT A16WE 2002101100022 20021011 00022 NM 2002 10 11 SWAA022208 1 20020923 A 5610 2315MODB WINDOW BOEING 737 7373Q8 1384670 NM COCKPIT CRACKED A SWAA A UNSCHED LANDING P NO WARNING INDICATION NR NOT REPORTED 1 SW 29 689SW 23387 DIVERSION, DURING FLIGHT R-1 COCKPIT WINDOW CRACKED. REMOVED AND REPLACED R-1 COCKPIT WINDOW AND CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2002101100023 20021011 00023 NM 2002 10 11 SWAA022209 1 20020923 A 5315 6545410 FLOORBEAM BOEING 737 737317 138447P NM MID CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAMS CRACKED (2 EA) BETWEEN BS 706 AND BS 711, WL 202 AT RBL 25 AND L BL 25. REPAIRED FLOORBEAMS PER BFG ER. 2 L 7 2 4F RT A16WE 2002101100024 20021011 00024 NM 2002 10 11 SWAA022211 1 20020923 A 5311 6546543 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND STR 9L, BS 480, BS 727, BS 807, BS 847 , BS 867 AND BS 887. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2002101100025 20021011 00025 NM 2002 10 11 SWAA022212 1 20020923 A 5311 6546543 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND STR 9R, BS 440, BS 480, BS 747 AND BS 827. REPAIRED FRAMES PER BFG ER. 2 L 7 2 4F RT A16WE 2002101100026 20021011 00026 NM 2002 10 11 SWAA022213 1 20020923 A 5311 6546529 FRAME BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, STR 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002101100027 20021011 00027 NM 2002 10 11 SWAA022214 1 20020920 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 926 AND BS 928, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002101100028 20021011 00028 NM 2002 10 11 SWAA022215 1 20020922 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED C1 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED (3 EA) AT 12 0' CLOCK POSITION ABOVE PRESS DOME. REPAIR ED BULKHEAD PER SWA EA. 2 L 7 2 4F A16WE 2002101100029 20021011 00029 NM 2002 10 11 SWAA022218 1 20020923 A 5530 6547450 FITTING BOEING 737 7373H4 1384600 NM VERT STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND VERTICAL STABILIZER AFT SPAR PRIMARY LUG FACE FITTINGS CORRODED. REPAIRED FITTINGS PER BFG ER. 2 L 7 2 4F RT A16WE 2002101100030 20021011 00030 NM 2002 10 11 SWAA022220 1 20020923 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT AT ROW NR 1 LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002101100031 20021011 00031 2002 10 11 SWAA022221 4 20020924 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002101100032 20021011 00032 NM 2002 10 11 SWAA022223 1 20020924 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E PLUS 10, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002101100033 20021011 00033 2002 10 11 SWAA022224 4 20020924 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F A16WE 2002101100034 20021011 00034 NM 2002 10 11 SWAA022226 1 20020924 A 5313 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPECIAL VISIT, FOUND TIE CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002101100035 20021011 00035 NM 2002 10 11 SWAA022228 1 20020924 A 5311 6557463 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIES CRACKED (3 EA) AT BS 360, BETWEEN STR 13L AND STR 15L. REPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2002101100036 20021011 00036 NM 2002 10 11 SWAA022229 1 20020924 A 5311 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 380, BETWEEN STR 14L AND STR 15L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002101100037 20021011 00037 NM 2002 10 11 SWAA022230 1 20020923 A 2130 40631997201AA CONTROLLER BOEING 737 7373H4 1384600 NM COCKPIT ERRATIC A SWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 29 634SW 27937 AT 28,000 FT, CABIN PRESS WARNING INDICATION DISPLAYED. C/W EMERGENCY DESCENT. OUTFLOW VALVE INDICATED CLOSED. REMOVE D AND REPLACED NR 1 PRESS CONTROLLER AND OUTFLOW VALVE PER MM. 2 L 7 2 4F RT A16WE 2002101100038 20021011 00038 NM 2002 10 11 SWAA022231 1 20020925 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 778SW 27883 DURING SCHEDULED A1 CHECK, FOUND EEPLS LENS MISSING AT ROW NR 1. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002101100039 20021011 00039 NE 2002 10 11 SWAA022235 2 20020924 A 7200 1668M23P BLADE BOEING 737 7373H4 1384600 NM CFM56 CFM563B1 13802 NE NR 2 ENGINE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 427748 DURING SCHEDULED SERVICE CHECK, (MTSI) FOUND 7 EA HPT BLADES WITH T/E AXIAL CRACKS ON NR 2 ENG. REMOVED AND REPLACED NR 2 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101100040 20021011 00040 NM 2002 10 11 SWAA022248 1 20020927 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 EEPLS COVER MISSING BETWEEN ROW NR 9 AND NR 10. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002101100041 20021011 00041 NM 2002 10 11 SWAA022249 1 20020929 A 5313 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FWD CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002101100042 20021011 00042 NM 2002 10 11 SWAA022250 1 20020929 A 5313 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT STR 4L, BS 616 AND BS 639. REMOVED AND REPLA CED STR TIE CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002101100043 20021011 00043 NM 2002 10 11 SWAA022251 1 20020929 A 5320 6546543 SHEAR TIE BOEING 737 7373H4 1384600 NM MID CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIES CRACKED (2 EA) AT BS 616, STR 7L AND STR 8L AND STR 7R AND STR 8R. REM OVED AND REPLACED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2002101100044 20021011 00044 NM 2002 10 11 SWAA022252 1 20020925 A 3350 101073 LENS BOEING 737 737301 1384611 NM FWD ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED BC3 CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2002101100045 20021011 00045 NM 2002 10 11 SWAA022253 1 20020929 A 5320 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 787, WL 148 AND BL O. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002101100046 20021011 00046 NM 2002 10 11 SWAA022254 1 20020929 A 5311 6546529 FRAME BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500D, STR 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002101100047 20021011 00047 2002 10 11 SWAA022255 4 20020927 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002101100048 20021011 00048 NM 2002 10 11 SWAA022257 1 20020928 A 7603 208005 CABLE BOEING 737 7372H4 138448C NM NR 1 ENGINE STIFF A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 NR 1 ENGINE THRUST LEVER DIFFICULT TO MOVE. REMOVED AND REPLACED NR 1 ENG THROTTLE TELEFLEX CABLE PER MM. 2 L 7 2 4F A16WE 2002101100049 20021011 00049 NM 2002 10 11 SWAA022258 1 20020928 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 14R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002101100050 20021011 00050 NM 2002 10 11 SWAA022259 1 20020928 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 4R, BS 626, BS 578 AND BS 626. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002101100051 20021011 00051 NM 2002 10 11 SWAA022260 1 20020929 A 5330 6545785 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED SPECIAL VISIT, FOUND WINDOW CUTOUTS CRACKED AT LT WINDOWS NR 4, NR 5, NR 6, NR 7, NR 24 AND NR 31. REP AIRED FRAMES PER SWA EA AND SRM. 2 L 7 2 4F A16WE 2002101100052 20021011 00052 NM 2002 10 11 SWAA022261 1 20020929 A 5330 6545785 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED SPECIAL VISIT FOUND WINDOW CUTOUTS CRACKED AT RT WINDOWS NR 12, NR 26, NR 28, NR 29, NR 30 AND NR 31. REPAIRED FRAMES PER SWA EA AND SRM. 2 L 7 2 4F A16WE 2002101100053 20021011 00053 NM 2002 10 11 SWAA022263 1 20020929 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 751SW 29803 FWD OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002101100054 20021011 00054 NM 2002 10 11 VNAA0210006 1 20021009 A 2800 FUEL FILTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH HP A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 471PS 3007 ENROUTE, THE CREW RECEIVED A RIGHT HAND ENGINE HIGH PRESSURE BYPASS CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CONTACTED MAINTENANCE CONTROL. THE CREW WAS THEN INSTRUCTED TO RETURN TO DAY. MAINTENANCE INSPECTED AND R EPLACED THE RIGHT HAND HIGH PRESSURE FUEL FILTER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CH ECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002101100055 20021011 00055 NM 2002 10 11 VNAA0209031 1 20020922 A 2400 GENERATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 424JS 3033 DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND DC GENERATOR FAIL CAS MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTE D AND CLEANED THE GENERATOR CANNON PLUG AND SWAPPED GENERATOR CONTROL UNITS FROM SIDE TO SIDE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002101100056 20021011 00056 NM 2002 10 11 VNAA0209037 1 20020929 A 3200 PSEU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 433JS 3047 DURING TAKE OFF, THE CREW RECEIVED A PROXY SYSTEM CAS MESSAGE AND A DOOR SWITCH FAIL AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND RERACKED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORM ED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002101100057 20021011 00057 NM 2002 10 11 801DM0007 1 20021008 A 3350 20131A BATTERY PACK BOEING 757 757200 1384950 NM A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 801DM 26240 Emergency light battery pack for overwing lights requires replacing. R&R over wing exit battery paack at sta. 990 left for emergency lights. Ops. check good per MM 33-51-07. 2 L 7 2 4F RT A2NM 2002101100058 20021011 00058 SO 2002 10 11 C2XA02CL197 1 20021010 A 3350 WIRE EMB 145 EMB145LR 3260212 SO SERVICE DOOR LOOSE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 16911 145446 CLE FLIGHT#3194 THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT THE GALLEY SERVICE DOOR WAS INOPERATIVE.MAINTENANCE INSPEC TED AND RESECURED LOOSE WIRE ON THE EMERGENCY EXIT LIGHT.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002101100059 20021011 00059 EU 2002 10 11 2002F00925 1 20020926 A 7931 SENSE LINE AIRBUS 320 A320233 3930329 EU NR 2 ENGINE LOOSE A SOKF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 23 981LR 558 SAL - FLT TA315 - DURING CLIMB, THE CAPTAIN REPORTED LOW OIL PRESS INDICATION FROM ENGINE NR 2. THE AIRCRAFT RETURNED T O EL SALVADOR STATION FOR MAINTENANCE. AFTER LANDING, MAINTENANCE PERSONNEL PERFORMED AMM 79-31-00-810-816 OIL LEAK CHE CK, AND FOUND A LEAK AT NR 4 BEARING PRESSURE TRANSDUCER (4005EN) SENSE LINE. THE LINE WAS TIGHTENED PER AMM 79-33-16 A ND THE ENGINE WAS SERVICED WITH 10 QUART OF ENGINE OIL. ENGINE TEST WAS PERFORMED ACCORDING TO AMM 71-00-00. NO DISCRE PANCIES WERE FOUND AND THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2002101100065 20021011 00065 NM 2002 10 11 C1HA200293008 1 20021004 A 3350 BATTERY PACK BOEING 727 727212 138407G NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 293AS 21348 BATTERT PACK POWER SUPPLY FOR L/H & R/H AFT SERVICE DOORS INOP ESCAPE SLIDE LIGHTREMOVED AND CHARGED AND REINSTALLED SLI DE LIGHT EMERGENCY BATTERY PACK 2 L 7 3 4F A3WE 2002101100066 20021011 00066 EU 2002 10 11 2002F00928 1 20020615 A 2711 S5367139201251 CONTROL CABLE AEROSP ATR72 ATR72212 8680945 EU AILERON TAB DAMAGED A TRBA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 21 407AT 14726 407 AFTER FAILURE OF A FUNCTIONAL CHECK FLIGHT DUE TO EXCESSIVE USAGE OF AILERON TRIM TO MAINTAIN A STRAIGHT AND LEVEL FLIGH T, THE AIRCRAFT WAS INSPECTED AND FOUND A DAMAGE CABLE UNDER THE FLOOR PANELS LOCATED AFT OF THE COCKPIT AREA. REMOVED AND REPLACED AILERON TRIM TAB CABLE ASSEMBLY. (M) 2 H 7 2 4T RT A53EU 2002101100067 20021011 00067 EU 2002 10 11 2002F00929 1 20020821 A 6120 8088777 CONTROL UNIT AEROSP ATR72 ATR72212 8680945 EU LT ENGINE MALFUNCTIONED A TRBA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS AP APPROACH 1 SO 21 438AT 438 WHEN TURNING BASE IS FINAL, BOTH ENGINES POWER LEVELS WERE ADVANCED FROM IDLE TO NORMAL. THE LEFT ENGINE NR 1 DID NOT R ESPOND TO ANY POWER LEVEL SETTING. WITH THE POWER LEVELS IN THE NOTCH, THE LEFT ENGINE NP WAS AT 103.9 BUT THE TORQUE W AS AT ZERO PERCENT. ENGINE SHUTDOWN AS PRECAUTIONARY PROCEDURE. REMOVED AND REPLACED PROPELLER CONTROL UNIT AS PER MM 61-21. (M) 2 H 7 2 4T RT A53EU 2002101100068 20021011 00068 EU 2002 10 11 2002F00930 1 20020915 A 2611 CG7G0 SMOKE DETECTOR AEROSP ATR72 ATR72212 8680945 EU CARGO BAY MALFUNCTIONED A TRBA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 21 471AT 417 UPON ARRIVAL TO THE AIRPORT, THE CAPTAIN REPORTED ELECTRIC SMOKE WARNING AND SMOKE ODOR IN THE COCKPIT AREA. REMOVED AN D REPLACED THE FORWARD CARGO SMOKE DETECTOR UNIT IAW COMPANY MM 26-15-21. (M) 2 H 7 2 4T RT A53EU 2002101100069 20021011 00069 EU 2002 10 11 2002F00931 1 20020913 A 5730 S5391007501000 PANEL AEROSP ATR42 ATR42300 8680920 EU CTR WING BOX LOOSE A TRBA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 21 351AT 354 VIBRATION FELT AND AIRSPEED STARTED TO DECREASE. FLIGHT RETURNED TO THE AIRPORT. UPON ARRIVAL A WALK-AROUND INSPECTION REVEALED THAT THE FORWARD WING BOX PANEL WAS LOOSE, NOT FLUSH. REPLACED FORWARD WING BOX PANEL. (M) 2 H 7 2 4T RT A53EU 2002101100070 20021011 00070 EU 2002 10 11 2002F00932 1 20020829 A 2611 SMOKE WARNING SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A NSVA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 252CJ 340B252 WHILE EN ROUTE TO CMH, THE LAVATORY SMOKE WARNING LIGHT ILLUMINATED DURING FLIGHT. CREW PERFORMED REQUIRED CHECKLIST. UPON LANDING THE SYSTEM WAS INSPECTED WITH NO INDICATIONS OF FIRE OR SMOKE. THE AIRCRAFT WAS RETURNED TO SERVICE UNDER THE MEL. MAINTENANCE TROUBLESHOT THE SYSTEM IAW AMM 26-13-00-05 WITH NO FAULTS FOUND. SYSTEM OPS CHECK NORMAL. THE AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002101100071 20021011 00071 NM 2002 10 11 2002F00922 1 20020922 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 DURING PREFLIGHT TRANSIT FOUND R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED R2 DOOR BATTERY PACK. OP S CHECKED OK IAW 33-50-01. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100072 20021011 00072 NM 2002 10 11 2002F00923 1 20020919 A 3350 582214 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 803MA 22434 DURING PREFLIGHT TRANSIT, FOUND EMERGENCY PATH LIGHTING INOPERATIVE BETWEEN ROWS 21/30. REMOVED AND REPLACED E PATH BAT TERY PACK ON LEFT ROW 27 IAW 33-50-00. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100076 20021011 00076 NM 2002 10 11 2002F00924 1 20020922 A 3610 89812621 VALVE BOEING 727 727231 1384079 NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE INTERMITTENT A FX7A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 64346 21633 OUT OF SVMC, DURING CLIMB AT 26,000 FEET, THE CABIN STARTED TO CLIMB AT MAXIMUM RATE THE CABIN WAS UNCONTROLLABLE, FOLLO WED THE CHECKLIST AND RETURNED TO SVMC WITHOUT INCIDENT. AIRCRAFT WAS PRESSURIZED USING ENGINE 1 AND 3 BLEEDS. THE PRO BLEM WAS THE NR 3 ENGINE 13TH STAGE MOD VALVE WAS INTERMITTENT. THE SAME WAS PLACED ON DMI PER MEL 36-11-1. AIRCRAFT W AS RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2002101100078 20021011 00078 CE 2002 10 11 2002F00927 1 20020919 A 3297 67083245 WIRE CESSNA 750 750 2076810 CE ANTI-SKID SYS DAMAGED A UG8A O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 5113 7500013 BWG - FLT 436 - AMBER ANTI-SKID FAIL MESSAGE ILLUMINATED ON START UP AND WOULD NOT EXTINGUISH. DAMAGED ANTI-SKID WIRING ON RIGHT MLG. THE WIRING WAS REPAIRED PER CESSNA CITATION X MAINTENANCE MANUAL PROCEDURES, THE SYSTEM TESTED AND THE A IRCRAFT DISCREPANCY CLEARED. (M) 2 L 7 2 4J RT T00007WI 2002101100079 20021011 00079 EA 2002 10 11 COMA0260571 1 20021006 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA IMBOARD FLAP MALFUNCTIONED A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 781CA 7870 7312 FLAPS FAILED AT 36 DEGREES.REPLACED ALL FOUR INBOARD FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 2002101100082 20021011 00082 WP 2002 10 11 AALA20021201 1 20020801 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 555AN 53085 TUL - FOUND CORROSION ON NR 2 SEAT TRACK. REPLACED NR 2 TRACK SECTION PER SRM 53-05 FIG 4. (M) 2 L 7 2 4F A6WE 2002101100083 20021011 00083 WP 2002 10 11 AALA20021209 1 20020821 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 560AA 53090 TUL - FOUND DENT WITH 3 INCH GOUGE IN SKIN AT STATION 300, BETWEEN L20R AND L21R. INSTALLED INTERNAL DOUBLER AT STATION 300 BETWEEN LONGERON 20R AND L21R PER SRM 53-04, FIG 38 VIEW I. (M) 2 L 7 2 4F A6WE 2002101100084 20021011 00084 WP 2002 10 11 AALA20021236 1 20020822 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 595AA 53285 TUL - FOUND AFT CARGO DOOR, LOWER FRAME CORRODED FROM STATION 1155 TO 1216. BLENDED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00. (M) 2 L 7 2 4F RT A6WE 2002101100085 20021011 00085 EA 2002 10 11 ASOA02450 1 20020814 A 3350 MS277891A SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INTERMITTENT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 909AS 4658 FLT 4321 - DURING GROUND INSPECTION IN ATL, THE COCKPIT EMERGENCY LIGHT SWITCH WAS ACTIVATING THE EMERGENCY LIGHTS INTER MITTENTLY WHEN IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED THE COCKPIT EMERGENCY LIGHT SWITCH. OPERATIONAL C HECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002101100086 20021011 00086 SO 2002 10 11 ASOA02451 1 20020815 A 3350 1317 LIGHT EMB 120 EMB120RT 3260202 SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 244AS 120073 DURING A HANGAR INSPECTION IN MCN, THE CEILING EMERGENCY LIGHT AT ROW 2 WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE BURNED OUT CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002101100087 20021011 00087 EA 2002 10 11 ASOA02452 1 20020815 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 901AS 7616 DURING GROUND INSPECTION IN ATL, THE CEILING EMERGENCY LIGHT OVER ROW 10 WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE BURNED OUT CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002101100088 20021011 00088 EA 2002 10 11 ASOA02453 1 20020815 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 866AS 7517 DURING GROUND INSPECTION IN DFW, THE FORWARD MOST EXTERNAL EMERGENCY LIGHT ON THE RIGHT SIDE OF THE FUSELAGE WAS INOPERA TIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAF T OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002101100089 20021011 00089 EA 2002 10 11 ASOA02454 1 20020818 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 834AS 7254 DURING C-CHECK INSPECTION IN MCN, LEFT AND RIGHT FRAME STATION 718 WAS FOUND TO BE CRACKED BETWEEN STRINGERS 10 AND 12. MAINTENANCE REPAIRED THE CRACKED FRAME IAW ASA E0600-53-0067A. (M) 2 L 7 2 4F RT A21EA 2002101100090 20021011 00090 EA 2002 10 11 ASOA02455 1 20020818 A 5346 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 834AS 7254 WHILE COMPLYING WITH ASA EO600-53-0043A, INSPECTION OF THE ENGINE SUPPORT BEAM, CRACKS WERE FOUND AT THE LEFT AND RIGHT ACCESS PANEL LOWER WEB AND THE UPPER WEB AT THE CENTER AFT SIDE. MAINTENANCE WILL REPAIR THE CRACKED ENGINE SUPPORT BEA M IAW ASA EO 600-53-0070. (M) 2 L 7 2 4F RT A21EA 2002101100091 20021011 00091 EA 2002 10 11 ASOA02457 1 20020819 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 825AS * 7207 FLT 4766 - DURING GROUND INSPECTION AT DFW, THE FORWARD SEGMENT OF EMERGENCY LIGHTS WERE SLOW TO ILLUMINATE. MAINTENANC E REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK NORMAL. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002101100092 20021011 00092 SO 2002 10 11 ASOA02458 1 20020821 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 638AS 120282 DURING HANGAR MAINTENANCE IN TXK, TRACK EMERGENCY LIGHTING AT GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED NR 1 EMERGENCY BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002101100093 20021011 00093 EA 2002 10 11 ASOA02459 1 20020822 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 834AS 7254 WHILE COMPLYING WITH ASA EO NR 600-53-0069, FOUND RIGHT ANGLE IN FRAME CRACKED BETWEEN STRINGER 9/10 AND AT RADIUS BETWE EN STRINGERS 13/14. REPAIRED CRACKED FRAMES IAW SRM 51-00 AND REO NR 601R-53-61-576. (M) 2 L 7 2 4F RT A21EA 2002101100094 20021011 00094 EA 2002 10 11 COMA0260573 1 20021006 A 7933 5018T48P03 SEAL CNDAIR CL600 CL6002B19 1900309 EA L/H ENGINE LEAKING A COMA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 995CA 7229 LEFT ENGINE OIL PRESSURE WARNING.REPLACED THE INTEGRATED DRIVE GENERATOR 2 L 7 2 4F RT A21EA 2002101100096 20021011 00096 EA 2002 10 11 COMA0260578 1 20021009 A 2410 INTEGRATED CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 447CA 7552 INTEGRATED DRIVE GENERATOR CAUITON MESSAGE DURING TAKE OFF.SERVICED LTH LEFT ENGINE INTEGRATED DRIVE GENERATOR TO PROPER OIL LEVEL. 2 L 7 2 4F RT A21EA 2002101100098 20021011 00098 EA 2002 10 11 ASOA02460 1 20020822 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SO 11 871AS 7537 FLT 4450 - ON DESCENT INTO VPS, CAPTAIN RECEIVED A FLAP FAIL MESSAGE. AN EMERGENCY WAS DECLARED AND A 0 FLAP LANDING WA S MADE. AIRCRAFT LANDED SAFELY IN VPS. REVIEWED HISTORY AND NO FLAP FAILURE HISTORY WAS FOUND. INTERROGATED FECU. SY STEM TEST PASSED. RESET C/B'S AND FLAP SYSTEM. NO DEFECTS NOTED THROUGH FIVE COMPLETE FLAP CYCLES. AIRCRAFT OK FOR SE RVICE. (M) 2 L 7 2 4F RT A21EA 2002101100099 20021011 00099 EA 2002 10 11 ASOA02461 1 20020823 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 855AS 4648 7395 EMERGENCY LIGHTS WILL ARM BUT WHEN SELECTED 'ON' THE LIGHTS WILL NOT ILLUMINATE AND THE STATUS MESSAGES DOES NOT APPEAR. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002101100100 20021011 00100 NE 2002 10 11 EIA2002098 2 20020911 A 7200 ENGINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 4 FLAMED OUT A EIAA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 NM 09 481EV 19896 KJFK - FOUND ENGINE NR 4 FLAMED OUT DURING DESCENT. (M) 2 L 7 4 4F 4 F A20WE E20EA 2002101100101 20021011 00101 NM 2002 10 11 EIA2002100 1 20020915 A 2750 BACR13CE2 RELAY BOEING 747 747132 1384882 NM FLAP SYSTEM FAILED A EIAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 09 481EV 19896 KJFK - GROUND SAFE RELAY ON LIGHT STAYED ILLUMINATED AFTER TAKEOFF, INBOARD FLAPS WOULD NOT RETRACT NORMALLY AFTER LANDI NG. REPLACED RELAYS, R952 AND R226 IN P14 EPR MM 32-09-02. (M) 2 L 7 4 4F A20WE 2002101100102 20021011 00102 NM 2002 10 11 EIAA2002099 1 20020912 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 485EV 20712 DURING A-CHECK, FOUND R5 EMERGENCY EXIT SIGN, L5 DOOR EMERGENCY EXIT FLOOD LIGHT, EMERGENCY EXIT CEILING LIGHT INOPERATI VE AT STATION 2125 LT, EMERGENCY EXIT CREW DOOR SILL LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY`S, O PS CHECKED OK, PER MM 33-01-00. (M) 2 L 7 4 4F A20WE 2002101100103 20021011 00103 NM 2002 10 11 GAIA020129ST 1 20020919 A 5712 RIB BOEING 727 727251 138408H NM WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE RIB CHORD AT FUSELAGE BS 760.95 LEFT WAS CRACKED AT THE FIRST TWO FO RWARD HOLES. ACCOMPLISHED REPAIR IAW BOEING 727 SERVICE BULLETIN 727-57-0112, REV 4. THE AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 L 7 3 4F A3WE 2002101100104 20021011 00104 NM 2002 10 11 GAIA02081ST 1 20020903 A 5310 DOOR FRAME BOEING 727 727224 1384076 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT AT THE E/E ACCESS, THE AFT DOOR LOCKING FRAME HAD CORROSION AT THE F RAME TO SKIN AT BS 460, STRINGER S29L TO S28L. REMOVED FRAME DAMAGE, AND REPAIRED PER BOEING SRM 51-10-2 FIGURE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100106 20021011 00106 EA 2002 10 11 COMA0260580 1 20021010 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR INOPERATIVE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 941CA 7050 EMERGENCY LIGHTS ROWS 2 THUR 5 ARE INOPERABLE.REPLACED FLEXIBLE LAMP ASSEMBLY. 2 L 7 2 4F RT A21EA 2002101100107 20021011 00107 NM 2002 10 11 GAIA02082ST 1 20020903 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THERE WAS A DENT IN THE SKIN AT BS 1090, STRINGER S15R. CUT OUT DAM AGED AREA FABRICATED DOUBLER IAW B727 SRM 53-30-3, FIGURE 1, SHEET 2, PATE 6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M ) 2 L 7 3 4F A3WE 2002101100110 20021011 00110 NM 2002 10 11 GAIA02083ST 1 20020903 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SO 11 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE EXTERIOR NOSE SECTION AT BS 310 THROUGH 330 BETWEEN STR INGERS 21R TO STRINGER 22R SKIN WAS DENTED. CUT OUT DAMAGED AREA. FABRICATED DOUBLER AND FILLER TREATED AND PRIMED ARE A IAW SRM 53-30-3 FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100112 20021011 00112 NM 2002 10 11 GAIA02084ST 1 20020903 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THERE WAS A DENT IN THE SKIN AT BS 1130, STRINGER 27L. REMOVED OLD REPAIR CUT OUT DAMAGED AREA INSTALLED FILLER, DOUBLER AND TRIPLER PER BOEING SRM 53-30-3, FIGURE 5. THE AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100114 20021011 00114 NM 2002 10 11 GAIA02085ST 1 20020903 A 5313 STRINGER BOEING 727 727224 1384076 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT IN THE MAIN CARGO COMPARTMENT INTERIOR AT BS 720B HAD A CRACK AT STR INGER S15L FORWARD OF WING LIGHT SUPPORT. CUT OUT DAMAGED AREA, FABRICATED NEW PART IAW B727 SRM 53-10-3, FIG 5. THE A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100116 20021011 00116 NM 2002 10 11 GAIA02086ST 1 20020903 A 5313 STRINGER BOEING 727 727224 1384076 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE MAIN CARGO COMPARTMENT INTERIOR BS 720B HAD A CRACK AT STRINGER S15R END, FORWARD OF WING LIGHT SUPPORT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED NEW PART IAW B727 SRM 53-10-3, FIGURE 5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100117 20021011 00117 NM 2002 10 11 GAIA02087ST 1 20020903 A 5730 PLENUM BOEING 727 727224 1384076 NM WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT AFT PLENUM LOWER SKIN HAS CORROSION IN TWO PLACES. FOUND C ORROSION OUT OF LIMITS. INSTALLED DOUBLER AND TRIPLER IAW B727 SRM 57-30-3 FIGURE 8. THE AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 L 7 3 4F A3WE 2002101100121 20021011 00121 NM 2002 10 11 GAIA02088ST 1 20020903 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FORWARD CARGO COMPARTMENT, THE FRAME AT BS 680 HAS THREE DENTS I NTO THE RADIUS OF STRINGERS S25L TO S23L. COLD WORKED DENTS, NDT FOUND NO CRACKS, FABRICATED DOUBLER REPAIR IAW B727 SR NM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100128 20021011 00128 NM 2002 10 11 GAIA02089ST 1 20020903 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE BS 360, FRAME INBOARD FLANGE WAS DENTED AND CRACKED IN THE AREA OF STRINGER 16 LEFT. CUT OUT DAMAGED AREA IAW B727 SRM 51-40-3, FIG 1 FABRICATED DOUBLER IAW B727 SRM 51-20-1 AND 51-40 -3 FIG 1. THE AIRCAFT WAS RETURNED TO SERVICE. (M0 2 L 7 3 4F A3WE 2002101100129 20021011 00129 NM 2002 10 11 GAIA02090ST 1 20020903 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME DENTED JUST ABOVE FLOOR LEVEL RIGHT CABIN BS 540. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3 FIGURE 1. FABRICATED DOUBLER IAW B727 SRM 51-40-3, FIGURE 1 AND 53 -10-2 FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100131 20021011 00131 NM 2002 10 11 GAIA02091ST 1 20020903 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SO 11 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME WAS DENTED JUST ABOVE FLOOR LEVEL AT THE RIGHT SI DE MAIN CARGO COMPARTMENT BS 560. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3, FIGURE 1. FABRICATED DOUBLER IAW B727-SRM 51-40-3, FIGURE 1 AND 53-10-2 FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100132 20021011 00132 NM 2002 10 11 GAIA02092ST 1 20020903 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME WAS DENTED JUST ABOVE FLOOR LEVEL AT THE RIGHT MA IN CARGO COMPARTMENT BS 580. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3, FIGURE 1. FABRICATED DOUBLER IAW B727 SRM 51-40-3 AND 53-10-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100133 20021011 00133 NM 2002 10 11 GAIA02093ST 1 20020903 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME WAS DENTED JUST ABOVE FLOOR LEVEL RIGHT MAIN CARG O COMPARTMENT BS 600. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3 FIGURE 1, FABRICATED REPAIR DOUBLER IAW B727 S RM 51-40-3 AND 53-10-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100134 20021011 00134 NM 2002 10 11 GAIA02094ST 1 20020827 A 5311 BACB1517705 FRAME BOEING 727 727222 1384073 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE MAIN FRAME LOCATED AT BS 420, STRINGER 8R WAS CRACKED. MAINTENANC E REPAIRED CRACKED FRAME PER BOEING 727 STRUCTURAL REPAIR MANUAL CHAPTER 53-10-4 FIGURE 1. (M) 2 L 7 3 4F A3WE 2002101100136 20021011 00136 NM 2002 10 11 GAIA02095ST 1 20020827 A 5311 BACB1517705 FRAME BOEING 727 727222 1384073 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE MAIN FRAME LOCATED AT BS 440 STRINGER 8R WAS CRACKED. MAINTENANCE REPAIRED CRACKED FRAME PER BOEING 727 STRUCTURAL REPAIR MANUAL CHAPTER 53-10-4 FIGURE 1. (M) 2 L 7 3 4F A3WE 2002101100138 20021011 00138 NM 2002 10 11 GAIA02096ST 1 20020827 A 5330 SKIN BOEING 727 727251 138408H NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING SEVERE WEATHER IN PHOENIX, THE FUSELAGE BELLY SKIN WAS GOUGED FROM STATION 950C TO 990 BETWEEN STRINGER 28L-29. MAINTENANCE REPAIRED THE GOUGE PER FLIGHT VEHICLES CONSULTING, INC DRAWING NR 53-02463-3 DATED 8/01/02. (M) 2 L 7 3 4F A3WE 2002101100139 20021011 00139 NM 2002 10 11 GAIA02097ST 1 20020827 A 5330 SKIN BOEING 727 727251 138408H NM FUSELAGE DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING SEVERE WEATHER IN PHOENIX, THE FUSELAGE BELLY SKIN WAS DAMAGED FROM STATION 950C TO 990 BETWEEN STRINGER 26L-28L. MAINTENANCE REPAIRED THE DAMAGE PER FLIGHT VEHICLES CONSULTING, INC DRAWING NR 53-02463-1 DATED 8/01/02. (M) 2 L 7 3 4F A3WE 2002101100140 20021011 00140 GL 2002 10 11 CNM009ADM902 2 20020823 A 7250 6898735 TURBINE WHEEL HUGHES 369 369E 4470707 WP ALLSN 250C 250C20B 03013 GL ENGINE CRACKED A YRR4 K NONE O OTHER IN INSP/MAINT 1 WP 07 142MK 0187E CAE835702 NR 1 LOCKUP WAS FOUND, HEAVY RUB OF THE 29-34 AIR SEAL OF THE 2ND STAGE TURBINE NOZZLE AND SEAL KNIVES OF THE 1ST STAGE TURBINE WHEEL. 1ST STAGE TURBINE WHEEL FOUND CRACKED IF NOT FOUND WOULD HAVE BEEN CATASTROPHIC, TURBINE WHEEL WOULD OF EXITED THE ENGINE. 1 G 7 1 3U 3 U H3WE E4CE 2002101100141 20021011 00141 NM 2002 10 11 GAIA02098ST 1 20020827 A 5330 SKIN BOEING 727 727251 138408H NM FUSELAGE GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING SEVERE WEATHER IN PHOENIX, THE FUSELAGE BELLY SKIN WAS DENTED AND GOUGED FROM STATION 970C TO 1009 BETWEEN STRING ER 26L-29L. MAINTENANCE REPAIRED THE DAMAGE PER FLIGHT VEHICLES CONSULTING INC DRAWING NR 53-02463-2 DATED 8/01/02. (M ) 2 L 7 3 4F A3WE 2002101100142 20021011 00142 CE 2002 10 11 CSA2002F00000 1 20020816 A 3240 9980035 BRAKE ASSY BEECH 99 C99 1154006 CE PWA PT6 PT6* 52043 EA MLG DESTROYED E CSAA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 AL 01 207CS 262 U207 PCE38156 AIRCRAFT LANDED, PILOT REPORTED A TOTAL FAILURE OF THE LT BRAKE SYSTEM. THE AIRCRAFT WAS ABLE TO STOP USING PROPELLER R EVERSE WITHOUT INCIDENT, AND WAS TOWED OFF OF THE RUNWAY. INSPECTION OF THE BRAKES REVEALED THAT THE BOTTOM OF BOTH CAL IPERS ON THE LEFT GEAR HAD BROKEN. IT WAS APPARENT THAT A PIECE OF FOD HAD GOTTEN BETWEEN THE TWO WHEELS AND BROKE BOTH CASTINGS. THIS CAUSED THE LOSS OF THE HYDRAULIC FLUID FOR THE BRAKE SYSTEM. THE AIRCRAFT HAD LANDED, THIS IS GRAVEL R UNWAY, THE PILOTS REPORTED NOTHING OUT OF ORDINARY AT THAT STOP. SPECULATE THAT LARGE ROCK HAD GOTTEN IN AND CAUSED THE DAMAGE, NO DAMAGE WAS FOUND ON TIRES OR WHEELS. 1 L 7 2 3T 3 T A14CE E2NE 2002101100143 20021011 00143 NM 2002 10 11 GAIA02100ST 1 20020904 A 5230 MS2000116 HINGE BOEING 727 727224 1384076 NM CARGO DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FORWARD MAIN CARGO DOOR HINGE WAS CRACKED. INSTALLED NEW HINGE SECTION PER AEI SERVICES BULLETIN 01-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100144 20021011 00144 CE 2002 10 11 CSA2002F00001 1 20020827 A 5550 1154400315 PIVOT ASSY BEECH 99 C99 1154006 CE PWA PT6 PT6A60A 52043 NE EMPENNAGE CRACKED E CSAA K NONE O OTHER IN INSP/MAINT 1 AL 01 995SB U179 PCE38103 USING VISABLE DYE PENTRANT INSPECTION, FOUND CRACKS IN STRUCTURAL WEBBING OF PIVOT POINT EXTENSIONS OF BOTH LEFT AND RIG HT HAND BRACKETS. CRACK ON LEFT BRACKET MEASURED APPROXIMATELY .5 INCHES. CRACK IN RIGHT BRACKET EXTENDED ENTIRE LENGT H OF WEB. TOTAL TIME ON PARTS UNKNOWN, THIS INSPECTION IS DUE EVERY 20K HOURS. 1 L 7 2 3T 4 T A14CE E4EA 2002101100145 20021011 00145 NM 2002 10 11 GAIA02101ST 1 20020903 A 5230 MS2000116 HINGE BOEING 727 727224 1384076 NM CARGO DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 79748 22450 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE AFT MAIN CARGO DOOR HINGE WAS CRACKED. INSTALLED NEW HINGE SECT ION AEI SERVICE BULLETIN 01-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101100146 20021011 00146 NM 2002 10 11 GAIA02130ST 1 20020919 A 5720 STIFFENER BOEING 727 727251 138408H NM LT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IN WAS DISCOVERED THAT THE LEFT WING LEADING EDGE AT WS 62.4 HAS A BOTTOM STIFFENER CRACKED. A CCOMPLISHED REPAIR IAW BOEING 727 SRM 57-10-2, FIGURE 3 AND 51-40-4, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 L 7 3 4F A3WE 2002101100147 20021011 00147 NE 2002 10 11 GAIA02132OP 2 20020905 A 7200 ENGINE BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE NR 1 MALFUNCTIONED A GAIA E ENGINE SHUTDOWN K FLUID LOSS AP APPROACH 1 SW 07 69740 20668 665348 FLT 2834 - PHL-CLT - DURING APPROACH TO CLT, THE CREW NOTICED THE NR 1 ENGINE OIL QUANTITY DECREASING. THE CREW DECIDED TO MAKE A PRECAUTIONARY SHUTDOWN OF THE ENGINE AND DECLARE AN EMERGENCY. AN UNEVENTFUL LANDING WAS MADE. THE AIRCRAFT WAS MAINTENANCE FERRIED TO DFW FOR AN ENGINE CHANGE. THE NR 1 ENGINE WAS REMOVED, REPLACED, AND OPERATIONALLY CHECK GO OD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2002101100148 20021011 00148 CE 2002 10 11 DF22002F00000 1 20020918 A 2840 S35941 SENSOR CESSNA 172 172R 2072401 CE LYC O360 IO360A1A 41514 EA FUEL TANK INOPERATIVE A DF2S K NONE O OTHER IN INSP/MAINT 1 SW 15 870CP 1742 17280666 NUMEROUS PILOT REPORTS OF LOW FUEL WARNING LIGHT FLICKERING IN FLIGHT, OFTEN TWO FAST TO DETERMINE IF LEFT OR RIGHT LIGH T. MAINTENANCE PERSONNEL UNABLE TO DUPLICATE ON GROUND. REMOVED LT FUEL QUANTITY SENDER FROM TANK AND MOVED FLOAT ARM BY HAND TO APPROX. 24 GALLON LEVEL AND OBSERVED LEFT LOW FUEL LIGHT ILLUMINATE AND LEFT FUEL INDICATOR NEEDLE DROP TO Z ERO. PILOTS HAVE REPORTED ERRONEOUS FUEL WARNING LIGHTS IN NINE OUT OF TEN A/C. THE PROBLEM IS ALMOST ALWAYS SO INTERM ITTENT THAT IT CANNOT BE DUPLICATED BY MAINTENANCE. THIS SENDER HAS 1584 HOURS IN SERVICE. 1 H 7 1 3O 3 O NT 3A12 1E10 2002101100149 20021011 00149 SO 2002 10 11 DF22002F00001 1 20021003 A 7160 86245834 AIR BOX PIPER PA44 PA44180 7104402 SO LYC O360 O360* 41514 EA CARBURETOR CRACKED A DF2S K NONE O OTHER IN INSP/MAINT 1 SW 15 355AB 299 4496093 DURING 100 HR INSPECTION, THE TECHNICIAN FOUND LEFT ENGINE CARBURETOR HEAT AIRBOX CRACKED. THE LEFT AIRBOX WAS CRACKED AT THE HOT AIR INLET AND EXTENDED ALMOST ALL THE WAY AROUND THE TUBE, RESULTING IN ALMOST COMPLETE SEPARATION OF THE TUB E FROM THE AIRBOX. A POSSIBLE CAUSE MIGHT BE POOR DESIGN OF THE AIRBOX AND WEAK WELDS AT BOTH COLD AND HOT AIR TUBES. THIS AIRBOX WAS INSTALLED NEW 299.0 HOURS AGO TO REPLACE ANOTHER BORKEN BOX. THE PREVIOUS BOX HAD 198.6 HOURS TOTAL. N EW AIRBOXES SELDOM LAST MORE THAN A FEW HUNDRED HOURS BEFORE CRACKS ARE DETECTED. 1 L 7 2 3O 3 O A19S0 E286 2002101100150 20021011 00150 NM 2002 10 11 02283418 1 20021010 A 7921 3DB316605 HEAT EXCHANGER DORNER DO32 DO328300 NM A VTZA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 418FJ 3176 During cruise of the flight from RDU to LGA, the crew reported R?H engine oil pressure fail. The engine was shutdown as a precaution and the flight diverted to RIC where it landed without incident. Maintenance personnel found the fuel/oil heat exchanger cracked. The heat exchanger was removed and replaced, operational and leak checks were satisfactory and the aircraft was returned to service. 2 H 7 2 4T RT A55NM 2002101100151 20021011 00151 WP 2002 10 11 MWEA020612 1 20021011 A 5313 995789929 INTERCOSTAL DOUG DC9 DC981 3022081 WP STATION 47 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 INTERCOSTAL CRACKED FORWARD ACCESSORY STATION 47 RIGHT OF CENTER. -- FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2002101100152 20021011 00152 NM 2002 10 11 UPS02439643 1 20020920 A 5310 PANEL BOEING 747 747SR46 1384816 NM NOSE W/W CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C NOSE W/W TOP PNL WEB FOUND CRACK AT BS 291 LBL 15 JUST FWD OF INTER- COSTAL. NOSE W/W TOP PANEL RE PAIRED AS PER SRM 53-10-04 FIG.117. 2 L 7 4 4F RT A20WE 2002101100153 20021011 00153 EA 2002 10 11 02283630 1 20021010 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 630BR 7255 During preflight inspection, the crew reported that the L/H exterior overwing emergency exit light was inoperative. Mai ntenance was initially deferred iaw the MEL. Later, maintenance personnel removed and replaced the lamp in the L/H exte rior overwing emergency exit light. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002101100154 20021011 00154 EU 2002 10 11 02283321 1 20021010 A 2422 PC125123B INVERTER JETAIR JETSTM JETSTM4101 1500501 EU A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 321UE 41045 During climb, the crew reported that they had lost a portion of their avionics systems. The flight returned to CRW and landed without incident. Maintenance personnel removed and replaced the r/h static inverter. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002101100155 20021011 00155 NM 2002 10 11 C1HA200288018 1 20021006 A 3350 900835A BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 688CA 22344 ON L2 DOOR, OVER THE DOOR EMERGENCY EXIT SIGN INOPR&R BATTERY PACK, DOOR EMERGENCY EXIT SIGN OP CHECKS GOOD 2 L 7 3 4F A3WE 2002101100156 20021011 00156 SO 2002 10 11 C2XA02IA218 1 20021009 A 3200 852701 PROXIMITY SWITCH EMB 145 EMB145ER 3260211 SO NLG WHEEL WELL INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14940 145033 IAH- THE CREW NOTED THAT THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH, AND, LANDED WITHOUT IN CIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE PROX SWITCH, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, 2 L 7 2 4F RT T00011AT 2002101100157 20021011 00157 SO 2002 10 11 C2XA02IA220 1 20021009 A 3200 8527001 PROXIMITY SWITCH EMB 145 EMB145ER 3260211 SO NLG WHEEL WELL INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14940 145033 IAH- THE CREW NOTED THAT THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH, AND, LANDED WITHOUT IN CIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR PROX SWITCH, PERFORMED A OPERATIONAL CHECK, NO DEF ECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002101100158 20021011 00158 SO 2002 10 11 C2XA02IA222 1 20021007 A 7830 14577751613 THRUST REVERSER EMB 145 EMB145 3260210 SO ENGINE DEFECTIVE A C2XA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 27 13970 145146 IAH- DURING TAKEOFF THE CREW NOTED THAT THE #1 THRUST REVERSER DISAGREE MESSAGE APPEARED ON THE EICAS, THE CREW ABORTED THE TAKEOFF. IAH- MAINTENANCE RELEASED THE AIRCRAFT IAW MEL. IAH- MAINTENANCE REMOVED AND REPLACED THE #1 THRUST R EVERSER, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002101200001 20021012 00001 SO 2002 10 12 C2XA02SH094 1 20021012 A 5410 14576599004 STIFFENER EMB 145 EMB145ER 3260211 SO NR 2 ENG NACELLE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 DURING C CHECK INSPECTION, NR 2 LOWER ENGINE NACELLE WAS FOUND TO HAVE A GOUGE ON AFT STIFFENER NEAR CENTER. MAINTENANC E REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SER VICE. 2 L 7 2 4F RT T00011AT 2002101200002 20021012 00002 SO 2002 10 12 C2XA02SH095 1 20021012 A 5411 14576518002 RIB EMB 145 EMB145ER 3260211 SO NR 2 ENG NACELLE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 DURING C CHECK INSPECTION, NR 2 ENGINE LOWER NACELLE OUTBOARD RIB WAS FOUND TO HAVE A GOUGE APPROXIMATE 4 INCHES AFT OF AFT HINGE. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS A PPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002101200003 20021012 00003 SO 2002 10 12 C2XA02SH096 1 20021012 A 5410 14576010001 STIFFENER EMB 145 EMB145ER 3260211 SO NR 1 ENG NACELLE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 DURING C CHECK, NR 1 ENGINE TOP NACELLE AFT STIFFENER 10 INCHES INBOARD OF CENTER WAS FOUND TO HAVE A GOUGED. MAINTENAN CE REMOVED DAMAGED AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002101300001 20021013 00001 SO 2002 10 13 C2XA02SH099 1 20021008 A 5410 14576608003 SKIN EMB 145 EMB145ER 3260211 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 SHV-DURING C CHECK #1 ENGINE LOWER COWLING WAS FOUND TO HAVE A GOUGE ON INERIOR SKIN 24 INCHES AFT CENTER OF COWLING. M AINTENANCE REMOVED DAMAGE AREA AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 54-10-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002101300002 20021013 00002 SO 2002 10 13 C2XA02TY151 1 20021013 A 5210 14521725003 SILL EMB 145 EMB145LR 3260212 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS, During a scheduled inspection, the service door aft sill was found corroded. Maintenance removed the corroded area, fabricated doublers, installed and restored finish. I/A/W-EMB-GST-1927/02A. The repair was satisfactory and the aircraf t will be released upon complection of inspection. 2 L 7 2 4T RT T00011AT 2002101300003 20021013 00003 SO 2002 10 13 C2XA02TY152 1 20021013 A 5330 14521725013 SILL EMB 145 EMB145LR 3260212 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS, During a scheduled inspection, the service door forward sill was found corroded. Maintenance removed the corroded a rea, fabricated doublers, installed and restored finish. I/A/W-EMB-GST-1927/02A. The repair was satisfactory and the air craft will be released upon complection of inspection. 2 L 7 2 4T RT T00011AT 2002101400001 20021014 00001 NM 2002 10 14 CALA0200491 1 20021012 A 3230 273A12011 ACTUATOR BOEING 737 737824 13844BZ NM NLG INOPERATIVE A CALA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 18220 13527 28929 THE NLG WOULD NOT RETRACT AFTER TAKEOFF FROM LAX. THE AIRCRAFT WAS RETURNED TO LAX WHERE IT LANDED WITHOUT INCIDENT. THE NLG LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-21-400. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2002101400002 20021014 00002 NM 2002 10 14 CALA0200492 1 20021011 A 2560 ACREM1A MEGAPHONE BOEING 737 7373T0 1384582 NM AFT CABIN WEAK A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14335 23573 INSPECTION FOUND AFT PORTABLE MEGAPHONE WEAK. THE MEGAPHONE WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 2002101400003 20021014 00003 NM 2002 10 14 CALA0200493 1 20021011 A 5730 SKIN BOEING 737 7373T0 1384582 NM R/W FIXED L/E CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 INSPECTION FOUND AN 8" CRACK IN R/H WING FIXED L/E SKIN PANEL ABOVE #4 SLAT ACTUATOR. THE SKIN PANEL WAS REMOVED AND REP LACED IAW ECRA 5720-01894. 2 L 7 2 4F RT A16WE 2002101400004 20021014 00004 WP 2002 10 14 CALA0200494 1 20021012 A 5311 FRAME DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND A 2" CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, L2R. REPAIRED FRAME IAW SRM 53-03, FIGURE 31A. 2 L 7 2 4F A6WE 2002101400005 20021014 00005 WP 2002 10 14 CALA0200495 1 20021012 A 5313 LONGERON DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND A 1" CRACK IN TAIL COMPARTMENT LONGERON 2R AT STA 1418. REPAIRED LONGERON IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 2002101400006 20021014 00006 EA 2002 10 14 02287622 1 20021012 A 3350 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER CR CRUISE 1 EA 27 622BR 7187 During cruiseof the flight from SFG to ORD, the crew reported emergency lights in cabin came on with switch in armed pos ition. Upon arrival maintenance personnel found cicruit breaker for emergency lights open. Closed circuit breaker, Ops ck'd emergency light system. No defects noted, aircraft returned to service. 2 L 7 2 4F RT A21EA 2002101400007 20021014 00007 NM 2002 10 14 PCAA0210121 1 20021011 A 3350 6104789 BATTERY DHAV DHC8 DHC8102 2809003 NM BURNED OUT A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 846EX 326 DURING ROUTINE MAINTENANCE VISIT RIGHT SIDE FUSELAGE AFT EMERGENCY LIGHT FOUND INOPERATIVE. EMERGENCY LIGHT BATTERY AT P OSITION 600 REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002101400008 20021014 00008 NM 2002 10 14 QXEA0201672 1 20021011 A 2610 PU90461R2 DETECTOR DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER CR CRUISE 1 NM 09 368PH 512 SEA-OUT OF 2000 FEET ON DEPARTURE FROM PDX, LAVATORY SMOKE DETECTOR ACTIVATED. FLIGHT ATTENDANT CHECKED, NO SMOKE/FUMES. PUSHED RESET/TEST, ALARM STOPPED. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2002101400009 20021014 00009 NM 2002 10 14 QXEA0201671 1 20021011 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 4203 106 504 PDX-LEFT HAND FUSELAGE EMERGENCY EGRESS LIGHT AFT OF AIRSTAIR WON'T ILLUMINATE. REMOVED AND REPLACED #3 EMERGENCY POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002101400010 20021014 00010 NM 2002 10 14 UPS02239715 1 20020924 A 5310 PANEL BOEING 727 72722C 138400F NM BS 250 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI CRACK ON NLG WHEEL WELL SIDE PANEL RH SIDE ALONG ROW OF FASTENERS AF T OF FWD RH PANEL BS 250 F ASTNERS REMOVED IAW SRM 51-30-02. CRACK CUT OUT IAW SRM 51-40-02. REPAIRS TO CRACKED AREA CARRIED OUT IAW SRM 51-40-2 2 L 7 3 4F A3WE 2002101400011 20021014 00011 NM 2002 10 14 UPS02239716 1 20020924 A 5310 PANEL BOEING 727 72722C 138400F NM BS 239 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI CRACK ON NLG WHEEL WELL PANEL RH SIDE ALONG ROW OF FASTNERS BELOW FW D RH PRESSURE PANEL BS 239 FASTENERS REMOVED IAW SRM 51-30-02. CRACK CUT OUT IAW SRM 51-40-2. REPAIRS TO CRACKED AREA CARRIED OUT IAW SRM 51-40- 2 & SRM 51-30-2 2 L 7 3 4F A3WE 2002101400012 20021014 00012 NM 2002 10 14 UPS02239718 1 20020924 A 5260 RISER BOEING 727 72722C 138400F NM RISER #8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI CORROSION ON RISER #8 ON AFT AIRSTAIRS DOOR FOUND TO BE OUTSIDE LIMI TS REF. NRC 480122 RISER R EPLACED IAW SRM ADDENDUM B727-5260-7551-A 2 L 7 3 4F A3WE 2002101400013 20021014 00013 NM 2002 10 14 UPS02239719 1 20020924 A 5260 RISER BOEING 727 72722C 138400F NM #6 RISER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI CORROSION ON RISER #6 ON AFT AIRSTAIRS FOUND TO BE OUTSIDE LIMITS RE F. NRC 480122 #6 RISER REP LACED IAW SRM ADDENDUM B727-5260-7551-A 2 L 7 3 4F A3WE 2002101400014 20021014 00014 NM 2002 10 14 UPS02239721 1 20020919 A 5310 FRAME BOEING 727 72722C 138400F NM BS 1030 S25-26LH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI LWR AFT CARGO BAY, FRAME (BS1030)TO FUSELAGE SKIN ATTACH POINT IS CR ACKED IN BEND RADIUS BETWEEN S TR 25 AND STR. 26L/H FRAME REPAIRED IAW SRM 53-10-4 FIG 11 2 L 7 3 4F A3WE 2002101400015 20021014 00015 NM 2002 10 14 UPS02239722 1 20020918 A 5260 STRINGER BOEING 727 72722C 138400F NM VENTRAL STAIRWAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI VENTRAL STAIRWAY MID STRINGER CORRODED UNDER #1 TREAD STRINGER REPAIRED IAW SRM 53-10-3 FIG 1 2 L 7 3 4F A3WE 2002101400016 20021014 00016 NM 2002 10 14 UPS02239724 1 20020917 A 5310 STRINGER BOEING 727 72722C 138400F NM S5L BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI STR. 5L FOUND CRACKED AT BS 1030 REPAIR CARRIED OUT IAW SRM 53-10-3 FIG 2 2 L 7 3 4F A3WE 2002101400017 20021014 00017 NM 2002 10 14 UPS02439727 1 20020917 A 5310 FRAME BOEING 747 747SR46 1384816 NM M/D BS 380 S24AR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C M/D BS 380 S24AR FRAME CRACKED. RH FRAME AT BS 380 S24AR REPAIRED AS PER HX RS R53-12-34913 & UPS EO B747-5310-17674-A. TO BE CONTINEOUS TO INSPECT THE REPAIR AREA UNTIL SB 747-53-2272 MOD IS COMPLETED. 2 L 7 4 4F RT A20WE 2002101400018 20021014 00018 NM 2002 10 14 UPS02439728 1 20020919 A 5730 SKIN BOEING 747 747SR46 1384816 NM LHW LWR SURFACE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C LHW LWR SKIN SURFACE CORROSION IS FOUND AT FUEL TANK ACCESS DR 522BB CUTOUT. CORROSION BLEND OUT 0 .06"X0.5"X8"EXCEED SRM LIMIT 57-30-03. CORROSION REMOVED REFER SOPM 20-20-02. 2 L 7 4 4F RT A20WE 2002101400019 20021014 00019 NM 2002 10 14 SABA020102 1 20021011 A 3350 1306 BULB DHAV DHC8 DHC8102 2809003 NM A SABA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 33 883CC 162 Flight5025 from TLH to CLT, During post-flight inspection in Charlotte the air crew reported the emergency lights were i nop at row one. Maintenance removed and replaced bulbs and system ops checked good. Aircraft was returned to service. 2 H 7 2 4T RT A13NM 2002101400020 20021014 00020 NM 2002 10 14 02101401 1 20021011 A 2913 3508806 PUMP RROYCE 535E4 BOEING 757 757236 1384971 NM #1 ENGINE FAILED A N8TA K NONE M OVER TEMP CR CRUISE 1 WP 19 522NA 2609 30800 25133 Left engine hyd. pump overheat, overheat light out ten minutes later. Loss of Hyd. Qty.. Left elec. pump turned off. Hyd press. 600 P.S.I. PTU could be heard cycling, followed by total loss of pressure and PTU lower EICAS Msg. illuminated. An uneventful landing was accomplished. Investigation revealed EDP Failure. R&R Lt. Eng. EDP and EDP Depress. Sw. as per M/M 29-11-05, ops and leak check good. Hyd. sys. (L) flushed and serviced, A/C released for return to service. 2 L 7 2 4F RT A2NM 2002101400021 20021014 00021 EU 2002 10 14 AWXA200200999 1 20021004 A 5280 D5337062220400 FITTING AIRBUS 320 A320231 3930325 EU CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 645AW 0 0 238 MCN - MAJOR REPAIR - DURING C-01 CHECK A 1 1/2" CRACK WAS FOUND ON THE R/H MAIN LANDING GEAR DOOR FORWARD HINGE FITTING. MAINTENANCE REMOVED DAMAGED R/H MAIN LANDING GEAR DOOR FORWARD HINGE FITTING, FABRICATED A NEW REPLACEMENT FITTING, AND INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 29, 39, AND SRM 51-44-11, PG. 1, 14, 16, 20. 2 L 7 2 4F RT A28NM 2002101400022 20021014 00022 NM 2002 10 14 AWXA200201000 1 20021003 A 5720 65C2630929 ANGLE BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 0 0 23261 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 1/2" CRACK WAS FOUND ON THE L/H UPPER WING PANEL ATTACH ANGLE OUTBOARD OF THE PYLON, WS 204.40. MAINTENANCE REMOVED CRACKED L/H UPPER WING PANEL ATTACH ANGLE AT WS 204.40, FABRICATED A NEW REPLACEM ENT ATTACH ANGLE, AND INSTALLED REPAIR PART IAW DWG 65C26309, B737-300 SRM 51-40-02, PG. 11, AND SRM 51-40-05, PG. 4-5, FIG. 2 & 3. 2 L 7 2 4F RT A16WE 2002101400023 20021014 00023 NM 2002 10 14 AWXA200201001 1 20021004 A 5315 69353654 ANGLE BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 0 0 23261 MCN - MAJOR REPAIR - DURING C-17 CHECK 3 EACH 1 1/2" CRACKS WERE FOUND ON FLOOR SUPPORT ANGLE FROM BS 500D TO BS 520, BL 0. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT UPPER ATTACH ANGLE FROM BS 500D TO BS 520, FABRICATED A NEW REPLACEMENT UP PER ATTACH ANGLE, AND INSTALLED REPAIR PART IAW DWG 69-35365, B737-300 SRM 51-40-02, PG. 10-11, 45, 48-49, 63, FIG. 12, 14. 2 L 7 2 4F RT A16WE 2002101400024 20021014 00024 NM 2002 10 14 AWXA200201002 1 20021005 A 5720 654962156 SUPPORT BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 0 0 23261 MCN - MAJOR REPAIR - DURING C-17 CHECK A 3" CRACK WAS FOUND ON THE INTERCOASTAL FOR AFT CARGO COMPARTMENT DOOR LATCH SUP PORT, BS 787. MAINTENANCE REMOVED THE CRACKED AFT CARGO COMPARTMENT DOOR LATCH SUPPORT AT BS 787, FABRICATED A NEW REPLA CEMENT SUPPORT, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05, PG. 4, FIG. 2, AND SRM 51-40-04, PG. 2, FIG. 1. 2 L 7 2 4F RT A16WE 2002101400025 20021014 00025 WP 2002 10 14 DHL2002873503 1 20020913 A 2730 564420507 ELEVATOR DOUG DC8 DC873F 302199F WP DENTED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 873SJ 83065 46091 ITEM N/R: 0693 RT. ELEVATOR UPPER EXTERNAL SKIN SHOWS SEVERAL DENTS ( XE132.000 TO XE141.250) ( MAJOR REPAIR) CORR: PERF ORMED MAJOR REPAIR IAW E.O. DHL020902 ED-3122, EO SEMAN 2002736 REMOVED FASTNERS IAW SRM51-1-21A PG. 4. TRIMMED OUT DAMA GED SKIN SEGMENT IAW EO DHL020902 , ED-3122 , EO SEMAN 2002736. CLEANED , TREATED , AND PRIMED AREA IAW SRM 51-1-8B FABR ICATED A NEW SKIN SEGEMENT ( 2024T3AL.032) AN INNERSPLICE ( 2024T3AL.040) AND A FILLER ( 2024T3 AL .016) IAW EO DHL02090 2, ED-3122, EO SEMAN 2002736. CLEANED , TREATED , AND PRIMED NEW SKIN , INTERIOR SURFACE, INNER SPLICE AND FILLER IAW SR M 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM51-1-15 PAGE 1. INSTALLED NEW SKIN , INNER SPLICE AND FILLER O 2 L 7 4 4F RT 4A25 2002101400026 20021014 00026 WP 2002 10 14 DHL2002873504 1 20020913 A 2730 564420507 ELEVATOR DOUG DC8 DC873F 302199F WP DENTED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 873SJ 83065 46091 ITEM N/R: 0632 RT ELEVATOR LOWER EXTERNAL SKIN DEFLECTED (DENTED) XAR 0 TO XE 83.500 ( MAJOR REPAIR) CORR: PERFORMED MAJ OR REPAIR IAW EO DHL 020901 , ED-3123 , AND EO SEMAN 2002735. REMOVED FASTNERS WITHIN REPAIR AREA IAW SRM51-1-21 PG. 1. TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL02091 , ED-3123 , EO SEMAN 20022735 . CLEANED , TREATED , AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEW SKIN SEGMENT , (2024T3AL.032)N, AN INNER SPLICE (2024T3AL.040) AND A FILLER (2024T3AL.016 ) IAW EO DHL020901, ED-3123 ,, EO SEMANS 2002735. CLEANED , TREATED AND PRIMED NEW SKIN INTERIOR SURFACE , SPLICE , AND FILLER IAW SRM 51-1-8B APPLIED PRC SEALANT ON ALL FAYING SURFACES IAW SRM 51-1-15 PG. 1. INSTALLED NEW SKIN , INNER SPLI 2 L 7 4 4F RT 4A25 2002101500009 20021015 00009 SO 2002 10 15 CQ92002F00000 2 20020920 A 7322 242514 METERING VALVE CESSNA 150 150M 2071830 CE CONT O200 O200* 17020 SO CARBURETOR BOWL SCORED B CQ9T O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 23 714GM 42 15079165 255682 A/C WAS ON TRAINING FLIGHT, AT 4000 FT, INSTRUCTOR DEMONSTRATED LEANING PROCESS BY PULLING OUT MIXTURE CONTROL UNTIL EN GINE ROUGHNESS JUST OCCURRED. ENRICHENING MIXTURE HAD NO EFFECT, AND A EMERGENCY LANDING WAS MADE WITHOUT POWER. INITI AL INSP SHOWED THAT MIXTURE CONTROL WAS OPERATING PROPERLY. INSP OF CARBURETOR SHOWED THAT MIXTURE CONTROL LEVER WAS AB LE TO MOVE BUT VALVE INSIDE WAS NOT AND APPEARED TO BE SEIZED. INTERNAL INSP SHOWED SCORE MARKS ON VALVE ASSY. NO EVID ENCE OF ANY FOD CONTAMINATION. IT WAS DIFFICULT TO SEPARATE BOWL FROM THROTTLE BODY DUE TO TIGHT FIT OF VALVE ASSY. T 1 H 7 1 3O 3 O 3A19 E252 2002101500010 20021015 00010 CE 2002 10 15 CQ92002F00001 1 20020923 A 3230 583800901 MOTOR BEECH 58 58 1152740 CE CONT O550 IO550* SO MLG BURNED B CQ9T K NONE O OTHER IN INSP/MAINT 1 WP 23 584MW 1774 TH1615 GEAR MOTOR FAILED ON EXTENSION CYCLE. HAD DIFFICULTY MANUALLY EXTENDING LANDING GEAR. A/C WAS SLOWED MUCH AS POSSIBLE AND PLACED ON AUTOPILOT. AFTER SEVERAL ATTEMPTS, PILOT WAS ABLE TO GET GEAR DOWN SAFE. UPON INSP OF A/C, IT WAS FOUND THAT EMERGENCY EXTEN HANDLE HAD BEEN DEFORMED BY PILOT TRYING TO LOWER GEAR. AFTER PLACING A/C ON JACKS, FOUND THAT GEA R HANDLE WOULD ONLY OPERATE WHEN DEFECTIVE MOTOR WAS REMOVED FROM GEARBOX. INTERNAL INSP OF MOTOR REVEALED A MELTED COM MUTATOR AND WINDING INSULATION. THIS HAD CAUSED ENOUGH INTERNAL FRICTION OF MOTOR AS TO IMPEDE MANUAL EXTENSION OF GEAR . GEARBOX WORM DRIVE GEAR HAD TO BE REPLACED DUE TO SLOT FOR GEAR HANDLE COMING OUT DURING EMERGENCY EXTENTION ATTEMPTS 1 L 7 2 3O 3 O 3A16 E3SO 2002101500011 20021015 00011 CE 2002 10 15 DF22002F00002 1 20020927 A 5510 MS210783 NUT PLATE CESSNA 172 172R 2072401 CE LYC O360 IO360A1A 41514 EA HORIZONTAL STAB BROKEN A DF2S K NONE O OTHER IN INSP/MAINT 1 SW 15 23675 2355 17280651 DURING 100 HOUR INSPECTION, TECHNICIAN FOUND LOWER ELEVATOR STOP NUTPLATE BROKEN AND FIBER LOCK PORTION OF PART SEPARATE D FROM THE REST OF NUTPLATE. STOP BOLT COULD MOVE FREELY. 1 H 7 1 3O 3 O NT 3A12 1E10 2002101500012 20021015 00012 EU 2002 10 15 FF6R112442 2 20020812 A 7210 350A32314306 GEAR SNIAS 350 AS350B2 8680813 EU TMECA ARTST2 ARTOUSTE2B1 60002 EU RGB DAMAGED B FF6R K NONE O OTHER IN INSP/MAINT 1 NM 01 115SH 3141 FROSTING ON FACE OF GEAR TEETH. UNABLE TO ESTABLISH STATIC GEAR PATTERN. 1 G 7 1 3U 3 U H9EU E300 2002101500014 20021015 00014 EU 2002 10 15 FF6R112448 1 20020801 A 6420 3160S333006001 BEARING AEROSP SA316 SA315B 8680615 EU TMECA ARTST2 ARTOUSTE2B1 60002 EU TAIL ROTOR ROUGH B FF6R K NONE O OTHER IN INSP/MAINT 1 NM 11 315SH 265 2577 BEARINGS ARE NOTCHY. PILOT CANNOT MOVE TAIL ROTOR PEDAL, SMOOTHLY. 1 G 7 1 4U 3 U H1IN E300 2002101500015 20021015 00015 SO 2002 10 15 GFV2002F00001 2 20020919 A 8530 FUEL NOZZLE CESSNA 210 T210N 2073456 CE CONT O520 TSIO520R 17040 SO ENGINE CYLINDER DIRTY B GFVR K NONE O OTHER IN INSP/MAINT 1 NM 02 1974U 21064760 294117R FUEL NOZZLE THREADS AND ROCKER SHAFT BOLTS GRITTY. 1 H 7 1 3O 3 O 3A21 E8CE 2002101500016 20021015 00016 SO 2002 10 15 GFV2002F00002 2 20020919 A 8530 FUEL NOZZLE CESSNA 210 T210N 2073456 CE CONT O520 TSIO520R 17040 SO ENGINE CYLINDER STRIPPED B GFVR K NONE O OTHER IN INSP/MAINT 1 NM 02 1974U 21064760 294117R FUEL NOZZLE THREADS NO GOOD. ROCKER SHAFT BOLTS STRIPPED. 1 H 7 1 3O 3 O 3A21 E8CE 2002101500017 20021015 00017 SO 2002 10 15 GFV2002F00003 2 20020919 A 8530 FUEL NOZZLE CESSNA 210 T210N 2073456 CE CONT O520 TSIO520R 17040 SO ENGINE CYLINDER DIRTY B GFVR K NONE O OTHER IN INSP/MAINT 1 NM 02 1974U 21064760 294117R FUEL NOZZLE THREADS AND ROCKER SHAFT BOLT GRITTY. 1 H 7 1 3O 3 O 3A21 E8CE 2002101500018 20021015 00018 SO 2002 10 15 GFV2002F00004 2 20020919 A 8530 FUEL NOZZLE CESSNA 210 T210N 2073456 CE CONT O520 TSIO520R 17040 SO ENGINE CYLINDER DAMAGED B GFVR K NONE O OTHER IN INSP/MAINT 1 NM 02 1974U 21064760 294117R FUEL NOZZLE THREADS, NO GOOD. ROCKER SHAFT BOLTS GRITTY. 1 H 7 1 3O 3 O 3A21 E8CE 2002101500019 20021015 00019 SO 2002 10 15 GFV2002F00005 2 20020919 A 8530 FUEL NOZZLE CESSNA 210 T210N 2073456 CE CONT O520 TSIO520R 17040 SO ENGINE CYLINDER DAMAGED B GFVR K NONE O OTHER IN INSP/MAINT 1 NM 02 1974U 21064760 ROCKER COVER MATING SURFACE UN-EVEN AT WELD. FUEL NOZZLE THREADS, GRITTY. 1 H 7 1 3O 3 O 3A21 E8CE 2002101500020 20021015 00020 SO 2002 10 15 GFV2002F00006 2 20020919 A 8530 ROCKER COVER CESSNA 210 T210N 2073456 CE CONT O520 TSIO520R 17040 SO ENGINE CYLINDER DAMAGED B GFVR K NONE O OTHER IN INSP/MAINT 1 NM 02 1974U 21064760 DAMAGE TO ROCKER COVER MATING SURFACE. GRIT IN ROCKER SHAFT BOLT THREADS. 1 H 7 1 3O 3 O 3A21 E8CE 2002101500021 20021015 00021 SO 2002 10 15 GJR2002F00000 1 20020826 A 2810 DC1804924632L FUEL TANK PIPER PA18 PA18150 7101828 SO LYC O360 O360* 41514 EA FUSELAGE CRACKED E GJRR K NONE O OTHER IN INSP/MAINT 1 NM 01 390CC 181 9944CC CRACK WAS FOUND ALONG THE LOWER SEAM ON THE INBOARD SIDE. APPLICATION 180HP FLOAT PLANE. INSUFFICIENT AMOUNT OF MATERI AL ALONG WELDED SEAMS. 1 H 7 1 3O 3 O 1A2 E286 2002101500022 20021015 00022 SO 2002 10 15 GJR2002F00001 1 20020725 A 2810 DC1804924625R FUEL TANK PIPER PA18 PA18150 7101828 SO LYC O360 O360* 41514 EA FUSELAGE CRACKED E GJRR K NONE O OTHER IN INSP/MAINT 1 NM 01 390CC 97 9944CC CRACK WAS FOUND ALONG THE LOWER SEAM ON THE OUTBOARD SIDE. 1 H 7 1 3O 3 O 1A2 E286 2002101500023 20021015 00023 2002 10 15 HYI2002F00014 4 20020830 A 3421 KG102 GYRO CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO HSI FAILED E HYIA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 NE 01 781EA 402C0310 CREW LOST HEADING INFORMATION IN CRUISE AT 5000 FT. DECLARED EMERGENCY AND RECEIVED NON GYRO VECTORS TO ISL 15 HYA. AT TEMPTED TO RESET GYRO C/B- WOULD NOT RESET. LANDED WITHOUT INCIDENT. MECHANIC CHANGED REMOTE GYRO (UG102). AIRCRAFT R ETURNED TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2002101500025 20021015 00025 CE 2002 10 15 JOU2002F00002 1 20020926 A 3397 WIRE CESSNA 208 208B 2073701 CE PWA PT6 PT6A11 52043 NE FUSELAGE CHAFED B J0UR O OTHER O OTHER NR NOT REPORTED 1 SO 09 125AR 489 208B0925 PILOT REPORTED FLASHING BEACON TRIPPED CIRCUIT BREAKER INTERMITTENTLY. TROUBLESHOT BEACON CIRCUIT AND FOUND WIRE INSULA TION CHAFING ON RIB LOCATED IN RUDDER FIN TIP ASSEMBLY. CONVELEX TUBING WAS FOUND INSTALLED ON WIRE HARNESS, IT WAS NO T SECURED TO PREVENT MOVEMENT. MOVEMENT OF TUBING ALLOWED WIRE TO CHAFE AND SHORT TO RIB IN RUDDER TIP ASSEMBLY. INSTA LLATION OF EXPAND-O-SLEEVING THE LENGTH OF WIRE BUNDLE (LOCATED IN FIN TIP ASSEMBLY) AND SECURING WITH TY-WRAP SHOULD P REVENT A SHORTED CIRCUIT. 1 H 7 1 3T 3 T A37CE E4EA 2002101500026 20021015 00026 CE 2002 10 15 KZ52002F00003 1 20021001 A 2750 GEAR BEECH BEECH 80 6580 1152806 CE LYC O540 IGSO540B1A 41532 EA FLAP MOTOR STRIPPED B KZ5R K NONE O OTHER IN INSP/MAINT 1 GL 15 135BA G270 LD68 GEAR ON END OF ARMATURE STRIPPED CAUSING FLAPS TO BE INOPERATIVE, ALSO CAUSED CONTAMINATION TO FLAP GEARBOX. 1 L 7 2 3O 3 O 3A20 1E7 2002101500027 20021015 00027 EU 2002 10 15 LC12002F00000 1 20020827 A 3220 TB2042068100 RING SOCATA TB20 TB20TRINIDAD 8680695 EU LYC O540 IO540* 41532 EA NLG WORN B LC1R K NONE O OTHER IN INSP/MAINT 1 EA 07 163GT 438 2000 DURING INSPECTION THE NLG STRUT, HAD FORE AND AFT AND SIDE TO SIDE PLAY BETWEEN THE HOUSING AND INNER STRUT. DISASSEMB LED STRUT. TECH REP ADVISED THAT THERE WERE NO PARAMETERS FOR THIS, REASSEMBLE AND CHECK THE STEERING ARM DIMENSIONS PE R SM. IF GOOD THEN THERE IS NO PROBLEM WITH THE NLG. ALL CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. AFTER WARRANTY DENIAL, ANOTHER MFG REP ADVISED THAT THERE IS A PROBLEM AND WOULD CONTACT FOR A SOLUTION. ADVISED TO REMOVE T HE STRUT AND SHIP TO MFG FOR REPAIR. MFG ASKED WHY RINGS IN THE STRUT HOUSING WERE NOT CHANGED. NO TECH DATA FOR REPAI R OF THAT COMPONENT FOUND. NLG STRUT WAS REPAIRED AND RETURNED BY MFG. 1 L 7 1 3O 3 O RT A51EU 1E4 2002101500028 20021015 00028 CE 2002 10 15 TXH2002F00000 1 20020815 A 3260 ISE13 DOWNLOCK SWITCH CESSNA 402 402A 207590M CE CONT O520 GTSIO520C 17032 SO MLG FAILED E TXHA K NONE O OTHER IN INSP/MAINT 1 WP 13 4544Q 402A0044 PILOT REPORTED LT MAIN GEAR DOWN AND LOCKED BUT NO GEAR DOWN INDICATION. FOUND DOWN LOCK SWITCH FAULTY. REPLACED SWITC H AND COPLETED RETRACTION TEST SATISFACTORY. 1 L 7 2 3O 3 O A7CE E7CE 2002101500029 20021015 00029 CE 2002 10 15 UAO2002F00000 1 20020827 A 7120 102910026131 TRUSS BEECH 58 58P 1152744 CE CONT O520 TSIO520* 17040 SO ENGINE MOUNT BROKEN C UA0M K NONE O OTHER IN INSP/MAINT 1 NM 07 145Z 7448 TJ289 DURING A PHASE INSPECTION IT WAS NOTED THAT THE EXHAUST HEATSHIELD FORWARD OF THE TURBO COMPRESSOR HAD CHAFED AN AREA .1 875 INCH X .3125 INCH THROUGH THE ENGINE MOUNT TRUSS. THIS WAS CAUSED BY THE HEATSHIELD MOUNT BREAKING ALLOWING THE HEA TSHIELD TO DROP ONTO THE TRUSS. WE HAVE INCORPORATED AN INSPECTION OF THIS AREA INTO OUR INSPECTION PROGRAM. 1 L 7 2 3O 3 O A23CE E8CE 2002101500030 20021015 00030 GL 2002 10 15 V5S2002F00000 3 20020910 A 6110 660706608 SLEEVE GULSTM 690TP 695 7630518 SW GARRTT TPE331 TPE331* 01514 WP ROTOL R306 R306382F7 GL PROPELLER LOOSE B V5SR K NONE O OTHER IN INSP/MAINT 1 SW 15 980GR 95049 DURING NORMAL CRUISE FLT, PILOT NOTICED AN UNUSUAL VIBRATION COMING FROM THE RT ENGINE. SHUT DOWN ENGINE AS A PRECAUT ION AND MADE A SINGLE ENGINE LANDING. MAINTENANCE REMOVED SPINNER FROM THE RT PROPELLER AND FOUND THAT THE REVERSE CONT ACT SLEEVE HAD BACKED OUT APPROX. .2500 INCH. PROP CYLINDER WAS REMOVED AND REVERSE CONTACT SPRING WAS INSPECTED AND FO UND TO BE OK. CYLINDER WAS REINSTALLED AND AIRCRAFT WAS GROUND RUN TO OPS CHECK, FOUND ALL INDICATIONS AND OPERATIONS N ORMAL. AIRCRAFT WAS RETURNED TO SERVICE AND TEST FLOWN AND NO VIBRATIONS WERE DETECTED. 1 H 7 2 3T 3 T 2A4 E2WE 6 C P8EU 2002101500031 20021015 00031 CE 2002 10 15 VJ32002F00076 1 20020920 A 3600 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO DRY AIR FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 8268T 573 CE1547 825755R DURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT U P AND AIR PRESSURE STILL LOW AT HIGHER RPM. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP. 1 L 7 1 3O 3 O 3A15 E5CE 2002101500032 20021015 00032 CE 2002 10 15 VJ32002F00077 1 20020920 A 3600 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO DRY AIR FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 5544A 1089 CE1343 DURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT U P AND AIR PRESSURE STILL LOW AT HIGHER RPM. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP. 1 L 7 1 3O 3 O 3A15 E5CE 2002101500033 20021015 00033 SO 2002 10 15 VJ32002F00078 2 20020920 A 7414 6310 MAGNETO BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO ENGINE FAILED B VJ3R O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 WP 07 8252T 117 CE1545 825834R DURING FLIGHT, CREW REPORTED ROUGH ENGINE. TROUBLESHOOTING BY MECHANIC BELIEVE RELATED TO MAGNETO NOT FIRING AT ATTITUD E. RETURNED TO MANUFACTURE FOR WARRANTY AND INSPECTION OF INTERNAL PARTS FOR POSSIBLE FAILURE. 1 L 7 1 3O 3 O 3A15 E5CE 2002101500034 20021015 00034 EU 2002 10 15 VJ32002F00079 1 20020925 A 3260 BAO10500 UPLOCK SENSOR GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA LT MLG FAILED B VJ3R O OTHER J WARNING INDICATION LD LANDING 1 WP 07 864AF 444 85004 L2826348A DURING LANDING GEAR INSPECTION GEAR ON LT MAIN WOULD NOT RELEASE FROM UP POSITION UNLESS USING EMERGENCY SYSTEM. TROUBL E SHOOTING THE GEAR SYSTEM FOUND THE LEFT UPLOCK SWITCH WAS NOT RELEASING WHEN GEAR SELECTED TO DOWN POSITION. PROBABLE CAUE COULD BE THE WIRES TO THE UP LOCK ASSEMBLY RELAY HAVE FAILED. UPLOCK ASSEMBLY WAS REMOVED AND INSTALLED A NEW UPL OCK ASSEMBLY. OPERATION CHECK OF THE GEAR SYSTEM CHECKED NORMAL. 1 L 7 1 3O 3 O RT A49CE 1E4 2002101500035 20021015 00035 EU 2002 10 15 VJ32002F00080 1 20020925 A 7810 BRACKET GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA TAILPIPE SUPPORT CRACKED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 862AF 445 85002 L2802448A TAILPIPE SUPPORT BRACKET CRACKED AT WELD FROM ENGINE HEAT AND USE AFTER 445 HOURS OF OPERATION. REMOVED MUFFLER AND INS TALLED NEW MUFFLER ASSEMBLY. RECOMMENDATION IS TO BUILD UP THE WELD AREA BETTER. PART SENT IN FOR WARRANTY. 1 L 7 1 3O 3 O RT A49CE 1E4 2002101500036 20021015 00036 EA 2002 10 15 VJ32002F00081 2 20020925 A 7310 75283 MANIFOLD GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA FUEL FLOW INOPERATIVE B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 864AF 446 85004 L2826348A ENGINE WILL NOT SHUT DOWN IN IDLE CUT OFF. RPM JUMPS FROM 250 RPM TO 400 RPM. BELIEVE DIAPHRAM DOES NOT SEAT TO CUT OF F FUEL FLOW. 1 L 7 1 3O 3 O RT A49CE 1E4 2002101500037 20021015 00037 NM 2002 10 15 F3LA200200347 1 20021014 A 5310 SHEAR TIE BOEING 737 737300 1384610 NM CORRODED A F3LA O OTHER O OTHER IN INSP/MAINT 1 NM 03 578US 23257 CORROSION FOUND ON FRAME AND SHEAR TIE FORWARD AND AFT SIDES AT BS 500D, LBL 9 TO 22 2 L 7 2 4F RT A16WE 2002101500040 20021015 00040 CE 2002 10 15 CER2002F00000 1 20020916 A 7500 GASKET LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE731* 01518 WP BLEED AIR SYS CRACKED E CERA K NONE O OTHER IN INSP/MAINT 1 EA 05 31DP 062 BLEED AIR GASKET CRACKED AFTER 25 HOURS INSTALLED. FOUND GASKET TO BE EXCESSIVELY BRITTLE. AGE OF GASKET OR INSTALL UN KNOWN. 2 L 7 2 4F 4 F A10CE E6WE 2002101500041 20021015 00041 NE 2002 10 15 ESY2002F00000 2 20020815 A 7200 CJ6108A ENGINE LEAR 25 25D 5170514 CE GE CJ610 CJ6108 30006 NE RIGHT FAILED E ESYA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 11 947TC 6207 5488 233 211147A FIFTEEN MINUTES AFTER TAKE-OFF, EXPERIENCED FAILURE OF RT ENGINE, WHILE CLIMBING, LEAVING, EVERYTHING WAS NORMAL. NO P REVIOUS ENG ABNORMALITY HAD BEEN NOTED. AT APPROX 20,000 FEET, HEARD LOUD BANG AND EXPERIENCED VIBRATIONS FROM RT ENGIN E. ENGINE LOST POWER, VERIFIED AFFECTED ENGINE, SHUT IT DOWN. CONTINUED WITH APPROPRIATE CHECKLIST. HAVING TIME AND ALTITUDE, ATTEMPTED A WINDMILLING AIR-START. (SINCE NO FIRE OR APPARENT DAMAGE WAS NOTED). ENGINE RESTARTED AND AFTER A FEW SECONDS, SHUT ITSELF OFF AGAIN. SECURED ENGINE PER CHECKLIST AND RETURNED FOR UNEVENTFUL LANDING. UPON LANDING, M ADE VISUAL INSPECTION. FORWARD AND AFT TURBINES WERE UNABLE TO BE MOVED BY HAND. NO VISIBLE DAMAGE OR FLUID LEAKS. 2 L 7 2 4J 4 J A10CE 1E16 2002101500042 20021015 00042 2002 10 15 ET32002F00000 4 20020906 A 2565 RETAINER BOEING 737 737* NM ESCAPE SLIDE MISSING B ET3D K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 DURING INSPECTION FOUND 1 OF 2 SWIVEL NUTS ON THE INFLATION HOSE SEPARATED FROM HOSE AT ASPIRATOR END. INSPECTION REVEA LED CAUSE OF SEPARATION, RETAINING RING WAS MISSING. RETAINING RING WOULD HAVE BEEN TRAPPED INSIDE ASPIRATOR INLET. A SEARCH FOR MISSING RETAINING RING WAS UNSUCCESSFUL, WITH SWIVEL NUT REINSTALLED ONTO HOSE AND PUSHED SNUG AGAINST TEFLON TAPE, NOT SUFFICIENT ROOM TO INSTALL, OR REMOVE RETAINING RING. EVIDENCE SUGGESTS RETAINING RING WAS NOT IN PLACE WHEN TELFON TAPE. IF SLIDE EVAC SYS WOULD HAVE BEEN DEPLOYED, HOSE WOULD HAVE SEPARATED PREVENTING INFLATION, RENDERING SLI DE EVAC SYS UNUSABLE. 2 L 7 2 4F RT A16WE 2002101500043 20021015 00043 CE 2002 10 15 GMZ2002F00001 1 20020912 A 3260 MS243311 SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE NLG FAILED B GMZ2 O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 01 800SD 66 RK270 LANDING GEAR WOULD NOT EXTEND WITH NORMAL SYSTEM. EMERGENCY EXTENSION SYSTEM WAS USED TO EXTEND GEAR. NOSE LANDING DOW NLOCK INDICATOR SWITCH / NOT LOCK SWITCH FAILED IN NOT LOCK POSITION WHICH PREVENTED SIGNAL FOR GEAR DOWN OPERATION. SW ITCH FAILED CONTINUITY TEST. NEW SWITCH WAS INSTALLED, GEAR OPERATED CORRECTLY. 2 H 7 2 4F 4 F RT A16SW E25EA 2002101500044 20021015 00044 NM 2002 10 15 IU6R170555P 1 20020820 A 3230 69B800021 PISTON BOEING BOEING 747 747* NM ACTUATOR BENT B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 379 PISTON IS BENT. UNIT WAS ASSEMBLED IN INCORRECT OR PER PREVENTING FULL RETRACT AND ALLOWING PISTON TO HAVE EXCESSIVE SI DE PLAY. ASSEMBLE UNIT CORRECTLY IAW HM. 2 L 7 4 4F RT A20WE 2002101500045 20021015 00045 NM 2002 10 15 F3LA200200348 1 20020929 A 5320 HFAB53AN011 FLOOR SUPPORT BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A F3LA O OTHER O OTHER IN INSP/MAINT 1 NM 03 270FL 22733 DURING C 2 CHECK, CORROSION FOUND IN AFT CARGO BAY FLOOR SUPPORT AT LBL 8. REMOVED DAMAGED SECTION OF FLOOR SUPPORT, FA BRICATED AND INSTALLED REPAIR PER SRM 53-10-5, FIGURE 6 2 L 7 2 4F RT A16WE 2002101500046 20021015 00046 NM 2002 10 15 F3LA200200349 1 20020929 A 5310 SKIN BOEING 737 7372L9 1384497 NM BS470, EXTERIOR CORRODED A F3LA O OTHER O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 DURING C 2 CHECK, CORROSION WAS FOUND ON THE SKIN AT BS 470, ON THE EXTERIOR, UNDER THE DME ANTENNAE. REPAIR WAS PERFOR MED IN ACCORDANCE WITH SRM 53-30-3, FIGURE 2 2 L 7 2 4F RT A16WE 2002101500047 20021015 00047 CE 2002 10 15 JEM2002F00003 1 20020816 A 5310 97430000150 TIE BEECH B300 B300 1159232 CE FUSELAGE CRACKED E JEMA K NONE O OTHER IN INSP/MAINT 1 CE 01 350KG FL156 THIS CROSS TIE IS RIVETED TO THE FUSELAGE IMMEDIATELY AFT OF THE LT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON TH E CROSS TIE ADJACENT TO THE AFT, LOWER CORNER OF THE EMERGENCY EXIT OPENING. 2 L 7 2 4T RT A24CE 2002101500048 20021015 00048 CE 2002 10 15 JEM2002F00004 1 20020816 A 5310 97430000149 CROSSBEAM BEECH B300 B300 1159232 CE PWA PT6 PT6* 52043 EA FUSELAGE CRACKED E JEMA K NONE O OTHER IN INSP/MAINT 1 CE 01 350KG FL156 THE CROSSBEAM IS RIVETED TO THE FUSELAGE IMMEDIATELY AFT OF THE RIGHT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSSBEAM ADJACENT TO THE AFT, LOWER OF THE EMERGENCY EXIT OPENING. 2 L 7 2 4T 3 T RT A24CE E2NE 2002101500049 20021015 00049 CE 2002 10 15 JEM2002F00005 1 20020816 A 5310 974304300462 CROSSBEAM BEECH B300 B300 1159232 CE PWA PT6 PT6* 52043 EA FUSELAGE CRACKED E JEMA K NONE O OTHER IN INSP/MAINT 1 CE 01 350KG FL156 CROSSBEAM IS RIVETED TO THE FUSELAGE IMMEDIATELY FORWARD OF THE RIGHT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSSBEAM ADJACENT TO THE FORWARD, LOWER CORNER OF THE EMERGENCY EXIT OPENING. 2 L 7 2 4T 3 T RT A24CE E2NE 2002101500050 20021015 00050 CE 2002 10 15 2002F00933 1 20020911 A 3230 991446110 CONTROL VALVE CESSNA 750 750 2076810 CE LANDING GEAR FAILED A DXTA K NONE J WARNING INDICATION AP APPROACH 1 GL 07 986QS 1162 7500086 DESCENDING THROUGH 18,000 FEET LIGHT THUMP AND LANDING GEAR UNLOCK LIGHT ILLUMINATED. THIS HAPPENED TWICE MORE AT 10,00 0 FEET AND 6,000 FEET. AIRCRAFT LANDED WITHOUT INCIDENT IN PBI. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL VALVE AND APPROVED THE A/C FOR RETURN TO SERVICE. (M) 2 L 7 2 4J RT T00007WI 2002101500051 20021015 00051 CE 2002 10 15 JEM2002F00006 1 20020816 A 5310 97430000149 CROSSBEAM BEECH B300 B300 1159232 CE FUSELAGE CRACKED B JEMA K NONE O OTHER IN INSP/MAINT 1 CE 01 711VN FL7 CROSSBEAM IS RIVETED TO THE FUSELAGE IMMEDIATELY AFT OF THE RIGHT EMERGENCY EXIT OPENING. THE CRACK WAS LOCATED ON THE CROSSBEAM ADJACENT TO THE AFT, LOWER CORNER OF THE EMERGENCY EXIT OPENING. 2 L 7 2 4T RT A24CE 2002101500052 20021015 00052 NM 2002 10 15 ASAA0210182 1 20020829 A 3350 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING PREFLIGHT CHECK, FOUND FOUR EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 12-14. REMOVED AND REPLACED R EMOTE RECEIVER AND BATTERY AT ROW 12 AND BATTERY ONLY AT ROW 14. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A16WE 2002101500053 20021015 00053 NM 2002 10 15 ASAA0210183 1 20020831 A 3350 86210144 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS WOULD NOT TEST AT ROW 15. REMOVED AND REPLACED THE B ATTERY PACK. THE TRACK LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2002101500054 20021015 00054 WP 2002 10 15 ASAA0280276 1 20020822 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING LINE CHECK, NUMEROUS EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FORWARD CABIN. REPLACED INOPER ATIVE MODULES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002101500055 20021015 00055 WP 2002 10 15 ASAA0280283 1 20020828 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FIRST CLASS CABIN. REASSEMBLED (RE CONNECTED) TRACK LIGHT MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002101500056 20021015 00056 WP 2002 10 15 ASAA0280284 1 20020827 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 1 THROUGH 7. RECONNECTED TRA CK LIGHT MODULE CONNECTORS. LIGHTS THE OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002101500057 20021015 00057 WP 2002 10 15 ASAA0280287 1 20020829 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 PDX - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FORWARD OF ROW 3. RECONNECTED DISCONN ECTED LIGHT MODULE AND REPLACED ANOTHER. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002101500058 20021015 00058 NM 2002 10 15 ASAA0280289 1 20020831 A 3350 1001191 LIGHT DOUG MD80 MD83 3023681 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 18072 12774 53473 SEA - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY (INC LUDING BATTERY PACK). LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT 2002101500059 20021015 00059 CE 2002 10 15 JOU2002F00001 1 20020926 A 7500 45A635141 VENTURI MTSBSI MU300 MU300 5780602 CE PWA JT15 JT15D4 52112 NE BLEED AIR CRACKED B J0UR O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 09 600GW 5627 A044SA PILOT REPORTED DURING A ROUTINE MAINTENANCE CHECK FLIGHT AT 10,000 FT., WHEN RIGHT OR LEFT (ONLY) BLEED AIR SUPPLY WAS S ELECTED, CABIN PRESSURIZATION COULD NOT BE MAINTAINED. THE CRACKS WERE FOUND IN RIGHT AND LEFT VENTURI ASSEMBLY LOCATED IMMEDIATELY AFT OF PRESSURE REGULATING AND SHUT-OFF VALVES. THE CRACK IN THE RIGHT AND LEFT VENTURI ASSEMBLY OCCURRED (AT THE WELD IN THE AFT END) WHERE THE VENTURI AND SLEEVE ARE JOINED. THE CAUSE OF CRACKS IS POSSIBLY AGE AND OR TEMPER ATURE RELATED. A PERIODIC INSPECTION SCHEDULE COULD POSSIBLY DETECT CRACKS BEFORE PROGRESSION CAUSED PART FAILURE. A P ERIODIC REPLACEMENT INTERVAL COULD POSSIBLY PREVENT PART FAILURE. 2 H 7 2 4F 4 F RT A14SW E1NE 2002101500060 20021015 00060 WP 2002 10 15 ASAA0280290 1 20020901 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SAN - DURING PREFLIGHT CHECK, FOUND 1ST CLASS CABIN EMERGENCY TRACK LIGHTING INOPERATIVE. RESECURED LOOSE CONNECTOR. L IGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002101500061 20021015 00061 WP 2002 10 15 ASAA0280291 1 20020903 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE AT ROWS 18-22. REPLACED ASSOCIATED POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002101500062 20021015 00062 WP 2002 10 15 ASAA0280293 1 20020906 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE NEAR AFT LAVATORIES. REPLACED ASSOCIATED POWER SUP PLY. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002101500063 20021015 00063 NM 2002 10 15 L1O2002F00000 1 20020911 A 4930 001A282A5100006 LINE DORNER DO32 DO328300 NM PWA 306 PW306B NE APU FUEL CHAFED I L1OM K NONE O OTHER IN INSP/MAINT 1 EA 21 328PM 889 3184 WHILE PERFORMING A POSTFLIGHT CHECK, FOUND APU FUEL PRESSURE LINE CHAFED. IT WAS CHAFING THE APU HIGH OIL TEMPERATURE SWITCH CONNECTOR PLUG P-12. THE FUEL LINE WAS CHAFED APPROXIMATELY 60 PERCENT OF THE WALL THICKNESS. 2 H 7 2 4T 4 F RT A55NM E35NE 2002101500064 20021015 00064 NM 2002 10 15 MEX2002300 1 20020917 A 7921 WARNING SYSTEM BOEING 757 7572Q8 1384972 NM LT ENGINE FALSE ACTIVATION B ASMF A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 23 804AM 26271 AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF THE LIGHT (OIL FILTER CLOGGING) TURNED ON DURING LT ENGINE STARTING. TE CH PERFORMED AN ERASER PROCEDURE AND THE ENGINES WERE STARTED AGAIN, MESSAGE DID NOT APPEAR AGAIN AND PARAMETERS WERE, O K. 2 L 7 2 4F RT A2NM 2002101500065 20021015 00065 WP 2002 10 15 MEX2002301 1 20020917 A 2760 R2241 RELAY DOUG DC9 DC987 3022087 WP SPOILERS FAILED B ASMF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 23 751RA 49779 AIRCRAFT ABORTED TAKEOFF AND RETURNED TO PLATFORM DUE TO WARNING LIGHT (SPOILER DEPLOYED) ON. AT PLATFORM TECH VERIFIED SENSORS AND SPOILER PANELS, ALL WERE OK. THERE WAS PERFORMED A BITE TO THE PSU AND NO FAULT CODE APPEARS. AIRCRAFT WA S DISPATCHED BY MEL. THE RELAY (PN R2-241 WAS REPLACED IAW WDM, SPOILERS WERE TESTED IAW MM. 2 L 7 2 4F RT A6WE 2002101500066 20021015 00066 NM 2002 10 15 MEX2002302 1 20020917 A 8012 START VALVE DOUG MD88 MD88 3023688 NM RT ENGINE FAILED B ASMF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 23 160PL 49763 AIRCRAFT RETURNED TO PLATFORM DUE TO THE STARTING VALVE OF THE RT ENGINE DID NOT OPEN. AT PLATFORM, TECH PERFORMED A MA NUAL STARTING. WIRE BUNDLE AND THE STARTING VALVE CONNECTOR WERE CHECKED, ALL WAS OK. STARTING TEST WERE PERFORMED IAW MM, ALL WAS OK. 2 L 7 2 4F RT A6WE 2002101500067 20021015 00067 WP 2002 10 15 ASAA0280304 1 20020912 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FIRST CLASS CABIN. REP LACED LIGHT MODULE AND WIRING. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002101500068 20021015 00068 NM 2002 10 15 GAIA02133OP 1 20020919 A 7830 WARNING LIGHT BOEING 727 727287 1384020 NM COCKPIT ILLUMINATED A GAIA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SW 07 916PG 21690 FLT 736 - BWI-CLT - AT TOP OF DESCENT, THE NR 2 ENGINE THRUST REVERSER LIGHT ILLUMINATED. THE NR 2 ENGINE THROTTLE WAS RETARDED, THE ENGINE WAS SHUTDOWN, AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT CONTINUED TO CLT AND LANDED WITHOUT FURT HER OCCURRENCE. THE NR 2 THRUST REVERSER WAS LOCKED OUT AND DEFERRED PER KHA MEL. THE AIRCRAFT WAS RETURNED TO SERVICE . (M) 2 L 7 3 4F RT A3WE 2002101500069 20021015 00069 NM 2002 10 15 GAIA02134OP 1 20020925 A 3350 100679 LIGHT BOEING 727 727251 138408H NM COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 255US 19974 DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101500070 20021015 00070 WP 2002 10 15 GTIA020953 1 20020822 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND CATERGORY II REPAIR INSTALLED WITHIN CONTROLLED AREA OF RIGHT PRIMARY STATIC PORT. REMOVED DOUBLER. FORMED NEW DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2002101500071 20021015 00071 WP 2002 10 15 GTIA020954 1 20020826 A 5320 PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - AFT CARGO FS 1155 DOOR FRAME CLOSE OUT PANEL CRACKED. REMOVED AFT CARGO DOOR FRAME CLOSE OUT PANEL. FABRICATED R EPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2003031900081 20030319 00081 NE 2003 3 19 RU3A02008 2 20020924 A 7532 BLEED VALVE LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE RT ENGINE STICKING A RU3A A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 21 57 3318 039 AFTER TAKEOFF, CREW FELT VIBRATION IN AIRCRAFT. SUSPECT COMPRESSOR STALLS ON NR 2 ENGINE. ADVANCED AND RETARDED THROTT LE ON NR 2 ENGINE AND NOTICED ENGINE POPPING AND VIBRATION. NR 2 ENGINE SET AT 88 PERCENT N2, WHERE IT RAN SMOOTH. RET URNED KOKC. ON LANDING, BOTH ENGINES IN REVERSE (IDLE) AT 40 KTS. ITT RISING THROUGH 900 DEG CELSIUS AND ENGINE POPPIN G. SECURED ENGINE. THE TEARDOWN REPORT INDICATES THE REPORTED OVER TEMPERATURE CONDITION CAN MOST LIKELY BE ATTRIBUTED TO THE FAULTY BLEED VALVES AND SOLENOID. (M) 2 L 7 2 4F 4 F RT A10CE E35NE 2002101500072 20021015 00072 CE 2002 10 15 RU3A02009 1 20020926 A 3230 POWERPACK BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE HYD SYSTEM MALFUNCTIONED E RU3A O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 15 74 FF9 PUT GEAR HANDLE DOWN, NOTHING HAPPENED, NO LIGHTS, NO LANDING GEAR EXTENDED. EXECUTED MANUAL EXTENSION PROCEDURE, THREE GREEN LIGHTS, NO RED, LANDED UNEVENTFUL. PREVIOUS TO ABOVE, ELECTRICAL (SURGE). FAILED AUTOPILOT AND TECHS PANEL. RE SET PANEL AND AUTOPILOT. RETURNED TO NORMAL OPS. AFTER LANDING, TURNED AIRCRAFT OVER TO MAINTENANCE TO TROUBLESHOOT PR OBLEM. JACKED AIRCRAFT, APPLIED 20 PSI SHOP AIR TO POWER PACK, RAN GEAR FOR 5 FAULT FREE CYCLES. APPLIED ELECTRICAL LO AD ON AIRCRAFT TO SIMULATE FLIGHT CONDITIONS FOR 2 HOURS, RAN GEAR FOR 5 FAULT FREE CYCLES AND PLACED AIRCRAFT ON GROUND . RAN ENGINES TO CHECK BLEED AIR AT HYD POWER PACK. ALL FUNCTIONS OPERATIONAL, CHECKED GOOD. 2 L 7 2 4T 4 T A24CE E4EA 2002101500073 20021015 00073 CE 2002 10 15 RY3A02007 1 20020918 A 2810 66003462 FLOAT VALVE LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE FUEL VENT LEAKING E RU3A O OTHER O OTHER AP APPROACH 1 SW 15 58 2926 057 DURING APPROACH, CONTROL TOWER ADVISED THAT A VAPOR TRAIL WAS OBSERVED FROM LT WING. AIRBORNE TECH CONFIRMED FUEL COMIN G FROM UNDER LT WING. FLT WAS DEVIATED TO AND LANDING MADE, WITH FIRE EQUIPMENT STANDING BY. FUEL FROM LT WING AND LEA K STOPPED. NORMAL LANDING/ NO PROBLEMS. REMOVED AND REPLACED LT FUEL VENT FLOAT VALVE IAW MFG MM. REFUELED, LEAK CHEC KED GOOD. RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A10CE E35NE 2002101500074 20021015 00074 NM 2002 10 15 UIEA200200036 1 20020907 A 2432 401767 BATTERY BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE MAIN OVERHEATED A UIEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 15 518MC 23476 DURING PREFLIGHT, THERE WAS STRONG BURNING SMELL IN COCKPIT. TROUBLESHOT, NR 3 ACM MAKING A NOISE, DEFERRED. DURING CR UISE AFTER 2.5 HOURS OF FLIGHT, BURNING ODOR RETURNED IN COCKPIT. AFTER SEARCHING FOR SOURCE IT WAS NOTICED NR 1 GEN KV AR/KW METER WAS READING -10KW+/-15KVR. ELECTED TO TURN GEN OFF BY TRIPPING FIELD, ODOR DISSIPATED AND DID NOT RETURN. ALL CSD LIGHTS ON MAIN GEN ANNUNCIATOR PANEL WERE ON . AFTER 6 HRS AND 43 MINUTES THERE WAS A LOUD SQUEALING SOUND UNDE R F/E PANEL AND STRONG ODOR AGAIN. BATTERY VOLTAGE DROPPED 30V-25V. PULLED C/B FOR BATTERY CHARGER. C/A: BAD SMELL C OMING FROM OVERHEATED BATTERY. BATTERY SMOLDERING DURING CHARGE. REMOVED AND REPLACED MAIN BATTERY, OPS CHECKED GOOD. 2 L 7 4 4F 4 F A20WE E23EA 2002101500075 20021015 00075 NM 2002 10 15 USAASB02157 1 20020820 A 2100 11502501 SENSOR BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE PACK TEMP FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 A/C NOT PRESS. RT PACK PRESSURE INDICATED ZERO AND LT PACK TRIP LT ILLUM AND TRIPPED. FLT RETURNED, LANDED W/O INCIDEN T. NO EMERG WAS DECLARED. MAINT FOUND LEFT PACK TEMP SENSOR BAD. R / R LT PACK TEMP SENSOR. REP P5-10 AC PANEL DUE TO LT PACK SWITCH INOP. OPS CK GOOD. RT ENG BLEED AIR REG INOP. R / R RT ENG BLEED AIR REG. R / R RT BLEED AIR CIRCU IT BREAKER FOR TRIPPING. OPS CK GOOD. PROBLEM, RT PACK PRESSURE INDICATING ZERO, RT BLEED AIR CIRCUIT BREAKER TRIPPED , REPEATED. MAINT R / R RT M1455 AC ACCY UNIT ON E2-3 SHELF IN E / E COMPT, R / R ENG FIRE CONT PANEL, CONNECTOR D3304 AT RT ENG DISCONNECT BRACKET AND REPAIRED WIRES. OPS CK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101500076 20021015 00076 CE 2002 10 15 WIB2002F00009 1 20020917 A 2740 3135540009 ACTUATOR LEAR 35 31A 5170531 CE GARRTT TFE731 TFE731* 01518 WP STABILIZER MALFUNCTIONED C WIBR O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 11 31TK 451 059 PITCH TRIM LIGHT CAME ON DURING TAKEOFF. PITCH TRIM INDICATOR MOVES RAPIDLY UP AND DOWN. INSPECTION AND OVERHAULED EVE RY 600 HOURS. RARELY MAKES 600 HOURS. 2 L 7 2 4F 4 F RT A10CE E6WE 2002101500077 20021015 00077 CE 2002 10 15 WIB2002F00010 1 20020917 A 2740 31355402 INDICATOR LEAR 35 31 5170530 CE PITCH TRIM INOPERATIVE B WIBR K NONE O OTHER IN INSP/MAINT 1 SW 11 90WA 87 028 PITCH TRIM INDICATOR INOPERATIVE, OPEN FROM RHEOSTAT ON STAB JACK ACTUATOR. INSPECTION AND OVERHAULED EVERY 600 HOURS. 2 L 7 2 4F RT A10CE 2002101500078 20021015 00078 CE 2002 10 15 ZOX2002F00001 1 20020819 A 2612 24409015 FIRE LOOP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE OUT OF POSITION E Z0XA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 07 168AZ UE68 THE RT ENGINE, DURING GROUND RUN, TAXIING TO THE TERMINAL, HAD A FIRE INDICATION. THE PILOT SHUT DOWN THE ENGINE. THE AIRCRAFT WAS LOOKED AT BY MAINTENANCE. THE RIGHT AFT FIRE LOOP WAS OUT OF POSITION FROM PREVIOUS MAINTENANCE. THE LOOP WAS PROPERLY POSITIONED, AIRCRAFT WAS TEST RUN AND NO FURTHER DEFECTS NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 2002101500079 20021015 00079 WP 2002 10 15 UPS02839260 1 20020803 A 5320 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 STA. 8 TO -25 FINGER DOUBLER IS CORRODED BEYOND LIMITS AT RBL 60. REMOVED, FABRICATED, AND REPLACED FINGER DOUBLER IAW DWG 5612298, AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2002101500080 20021015 00080 WP 2002 10 15 UPS02839261 1 20020804 A 5320 3755822505N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 STA 320 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 29L AND 30L. REMOVED AND REPLACED FIT TING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002101500081 20021015 00081 WP 2002 10 15 UPS02839262 1 20020804 A 5320 37558413 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 BATHTUB FITTING IS CRACKED AT STA 1160 AT LONG 34R. REMOVED, FABRICATED, AND REPLACED FITTING IAW DW G 3755841, AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002101500082 20021015 00082 WP 2002 10 15 UPS02839263 1 20020820 A 5320 3642974501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 STA 680 AT LBL 63 CENTER WING BOX TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3642974, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002101500083 20021015 00083 WP 2002 10 15 UPS02839264 1 20020731 A 5544 PAN DOUG DC8 DC873F 302199F WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:C2 LOWER RUDDER PANS ARE CRACKED AT 2ND AND 3RD HINGE FROM BOTTOM AT XE 77 AND XE 149. REMOVED, FABRICA TED, AND REPLACED PANS IAW DWG 5656233, AND SRM 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 2002101500084 20021015 00084 WP 2002 10 15 UPS02839289 1 20020820 A 5730 576958927 DOUBLER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 RIGHT WING CENTER L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335.25. REMOVED, FABRICATED AND REPLA CED DOUBLER IAW DWG 5769589, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002101500085 20021015 00085 WP 2002 10 15 UPS02839290 1 20020820 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 610. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATE D AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 2002101500086 20021015 00086 WP 2002 10 15 UPS02839291 1 20020821 A 5320 3779659U501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 857 LONG 3L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-2 0D. 2 L 7 4 4F RT 4A25 2002101500087 20021015 00087 WP 2002 10 15 UPS02839292 1 20020821 A 5320 3779978U1 ATTACH FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 700 LONG 18R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978 , AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002101500088 20021015 00088 WP 2002 10 15 UPS02839293 1 20020821 A 5320 3779659U501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 850 LONG 9R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-2 0D. 2 L 7 4 4F RT 4A25 2002101500089 20021015 00089 WP 2002 10 15 UPS02839294 1 20020825 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 640 SHEAR TIE IS CRACKED BETWEEN LONG 26R TO 27R. TRIMMED SHEAR TIE IAW SRM 53-2-0 FIG 2A, FABRI CATED AND INSTALLED SHEAR TIE IAW SRM 53-2-0 FIG 2A, AND 53-4-1 FIG 10. 2 L 7 4 4F RT 4A25 2002101500090 20021015 00090 WP 2002 10 15 UPS02839295 1 20020825 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 640 SHEAR TIE IS CRACKED BETWEEN LONG 26L TO 27L. REMOVED SHEAR TIE, FABRICATED AND INSTALLED RE PAIR IAW SRM 52-2-0 FIG 2A. 2 L 7 4 4F RT 4A25 2002101500091 20021015 00091 WP 2002 10 15 UPS02839296 1 20020826 A 5320 3755842505N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1180 BATHTUB FITTING CRACKED LONG 28L. REMOVED AND REPLACED FITTING IAW DWG 3755842 AND SRM 53-2 -0 FIG 2D. 2 L 7 4 4F RT 4A25 2002101500092 20021015 00092 WP 2002 10 15 UPS02839297 1 20020826 A 5320 475851452ON FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1230 LONG 33R INTERCOSTAL TO FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002101500093 20021015 00093 WP 2002 10 15 UPS02839299 1 20020826 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 INTERNAL SPLICE DOUBLER IS CORRODED AND CRACKED STA 1690 TO 1766 AT LONG 28R. REMOVED, FABRICATED AN D REPLACED DOUBLER IAW DWG 5644130, AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2002101500094 20021015 00094 WP 2002 10 15 UPS02839300 1 20020821 A 5320 3779659U501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 850 LONG 7R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-2 0D. 2 L 7 4 4F RT 4A25 2002101500095 20021015 00095 WP 2002 10 15 UPS02839301 1 20020821 A 5320 3779659U501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 850 LONG 8R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-2 0D. 2 L 7 4 4F RT 4A25 2002101500096 20021015 00096 WP 2002 10 15 UPS02839302 1 20020826 A 5320 37508651 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1745 BETWEEN LONG 35R AND 35L FWD BACKUP FITTING FOR TAILSKID SHOCK ABSORBER IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750865, AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002101500097 20021015 00097 WP 2002 10 15 UPS02839303 1 20020819 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 REMOVED DOUBLER ON R1 DOOR FWD UPPER CORNER AND REPAIR PER SRM 53-2-0 FIG 14 AT STA 160 LONG 10R. RE MOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND F ILLER IAW SRM 53-2-0 FIG 14. 2 L 7 4 4F RT 4A25 2002101500098 20021015 00098 WP 2002 10 15 UPS02839304 1 20020824 A 5320 47752621 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 KEEL BEAM FITTING 2ND FROM FRONT IS CRACKED BETWEEN WHEEL WELLS STA 902 APPROX LBL4 TO RBL 4. REMOVE D AND REPLACED FITTING IAW DWG 4775262-1, AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2002101500099 20021015 00099 WP 2002 10 15 UPS02839305 1 20020826 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 INTERNAL SPLICE DOUBLER IS CRACKED AND CORRODED STA 1690 TO 1766 AT LONG 28L. REMOVED, FABRICATED AN D INSTALLED DOUBLER IAW DWG 5644130, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002101500100 20021015 00100 WP 2002 10 15 UPS02839306 1 20020827 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1460 LONG 30L EXTERNAL DOUBLER. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2002101500101 20021015 00101 WP 2002 10 15 UPS02839307 1 20020822 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 FINGER DOUBLER IS CORRODED BEYOND LIMITS STA 960-980 AT RBL 63. REMOVED, FABRICATED AND INSTALLED DO UBLER IAW DWG 5646674, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002101500102 20021015 00102 WP 2002 10 15 UPS02839308 1 20020826 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1746 LONG 34R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 56493 29, AND SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2002101500103 20021015 00103 WP 2002 10 15 UPS02839309 1 20020826 A 5313 564932946 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 LONG 34L IS CRACKED AND CORRODED BEYOND LIMITS STA 1746 LONG 34L. REMOVED AND REPLACED LONGERON SECT ION IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2002101500104 20021015 00104 WP 2002 10 15 UPS02839320 1 20020827 A 5313 4772397U1 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1772 LONG 17R AND END FITTING ARE CRACKED. REMOVED LONGERON 17R AND END FITTING, FABRICATED LONG ERON SECTION AND REPLACED END FITTING, AND INSTALLED END FITTING AND LONGERON SECTION IAW DWG 4772397 AND 5649327, AND S RM 51-1-20D. 2 L 7 4 4F RT 4A25 2002101500105 20021015 00105 WP 2002 10 15 UPS02839321 1 20020821 A 5320 47504221N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 857 LONG 19R INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AFT SIDE. REMOVED AND REPLACED FITTI NG IAW DWG 4750422, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002101500106 20021015 00106 WP 2002 10 15 UPS02839322 1 20020821 A 5320 3779978U1 ATTACH FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 781 FWD SIDE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DW G 3779978, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002101500107 20021015 00107 WP 2002 10 15 UPS02839323 1 20020826 A 5320 37585702N1 ATTACH FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1230 LONG 35R INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW D WG 3758570, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002101500108 20021015 00108 WP 2002 10 15 UPS02839324 1 20020821 A 5320 4750418U2 ATTACH FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1220 LONG 19R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING I AW DWG 4750418, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002101500109 20021015 00109 EU 2002 10 15 RAIA00209235 1 20020807 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 555HK 41072 ESCAPE PATH LIGHTING INOPERATIVE. RE-SECURED CONNECTOR TO EMERGENCY ESCAPE PATH LIGHTING STRIP, OPS CK OK. 2 L 7 2 4T RT A41NM 2002101500110 20021015 00110 EU 2002 10 15 RAIA00209240 1 20020819 A 2612 WARNING SYSTEM AEROSP ATR72 ATR72202 8680940 EU RT ENGINE FALSE INDICATION A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 723TE 283 RIGHT ENGINE FIRE INDICATION. MAINTENANCE INSPECTED ENGINE, NO DEFECTS NOTED. ENGINE FIRE DETECTION SYSTEM TESTED, OK. 2 H 7 2 4T RT A53EU 2002101500111 20021015 00111 EU 2002 10 15 RAIA00209241 1 20020821 A 7910 M832481111 O-RING AEROSP ATR42 ATR42300 8680920 EU RT ENG OIL DAMAGED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 423TE 119 RIGHT ENGINE OIL PRESSURE INDICATED LOW. MAINTENANCE REMOVED AND REPLACED FAULTY RIGHT ENGINE OIL CAP O-RING, OPS AND LE AK CHECK OK. 2 H 7 2 4T RT A53EU 2002101500112 20021015 00112 EU 2002 10 15 RAIA00209242 1 20020821 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 551HK 41040 ESCAPE PATH LIGHTS OUT AT ROWS 9 & 10. RE-SECURED CONNECTOR TO ESCAPE PATH LIGHTS, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002101500113 20021015 00113 NE 2002 10 15 RAIA00209244 2 20020828 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE NR 2 OUT OF ADJUST A RAIA D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 CE 03 561HK 41077 75109 RIGHT ENGINE FLAMED OUT DURING TAXI. MAINTENANCE INSPECTED ENGINE, NO DEFECTS NOTED. ADJUSTED NR 2 ENGINE DECELERATIO N SCHEDULE, OPS CHECK OK. 2 L 7 2 4T 4 T RT A41NM E18NE 2002101500114 20021015 00114 EU 2002 10 15 RAIA00209246 1 20020905 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 553HK 41066 EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. RE-SECURED EMERGENCY PATH LIGHT STRIP CONNECTOR, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002101500115 20021015 00115 EU 2002 10 15 RAIA00209251 1 20020911 A 2120 ODOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DETECTED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 558HK 41071 REPORTED SMOKE ODOR IN CABIN DURING TAXI. MAINTENANCE GROUND RAN AIRCRAFT AT NUMEROUS POWER SETTINGS WITH AC PACKS ON A ND OFF WITH NO DEFECTS NOTED. 2 L 7 2 4T RT A41NM 2002101500116 20021015 00116 EU 2002 10 15 RAIA00210253 1 20020913 A 2611 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU LAV FALSE ACTIVATION A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 552HK 41057 LAV SMOKE LIGHT ILLUMINATED IN-FLIGHT AND EXTINGUISHED A FEW MINUTES LATER. MAINTENANCE INSPECTED CABIN AND LAV AREA F OR SMOKE - NONE NOTED. COULD NOT DUPLICATE SMOKE WARNING. 2 L 7 2 4T RT A41NM 2002101500117 20021015 00117 EU 2002 10 15 RAIA00210258 1 20020901 A 7931 AS3209222 O-RING AEROSP ATR42 ATR42300 8680920 EU OIL CAP DAMAGED A RAIA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 421TE 102 OIL PRESSURE LOW NR 2 ENGINE. MAINTENANCE REMOVED AND REPLACED OIL CAP O-RING, OPS AND LEAK CHECK OK. 2 H 7 2 4T RT A53EU 2002101500118 20021015 00118 EU 2002 10 15 RAIA00210262 1 20020919 A 2612 FIRE LOOP JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE DISCONNECTED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 573HK 41092 RIGHT FIRE LOOP LIGHT CAME ON DURING TAXI. MAINTENANCE RE-SECURED FIRE DETECTOR UNIT, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002101500119 20021015 00119 EU 2002 10 15 RAIA00210264 1 20020921 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 558HK 41071 EMERGENCY LIGHTS A ROWS 3 AND 4 INOPERATIVE. RE-CONNECTED PATH LIGHT STRIP CONNECTOR, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2002101500120 20021015 00120 NE 2002 10 15 RAIA00210267 2 20020924 A 7261 O-RING AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE LT ENGINE DETERIORATED A RAIA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 721TE 217 LEFT ENGINE HAS FLUID LEAK. MAINTENANCE REMOVED AND REPLACED THE NR 5 BEARING LINE O-RING, LEAK AND OPS CHECK OK. 2 H 7 2 4T 4 T RT A53EU E2ONE 2002101500121 20021015 00121 2002 10 15 RAIA00210271 4 20020926 A 3421 HG2010AC02 INDICATOR EMB 145 EMB145 3260210 SO COCKPIT INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 806HK 6626 2650 145112 RIGHT AHRS FAILED. MAINTENANCE REMOVED AND REPLACED THE 32 ATTITUDE HEEDING REFERENCE UNIT, OPS CHECK OK. 2 L 7 2 4F RT T00011AT 2002101500122 20021015 00122 2002 10 15 RAIA00210272 4 20020927 A 3421 HG2010AC02 INDICATOR EMB 145 EMB145 3260210 SO COCKPIT INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 806HK 5467 5467 145112 FO'S HEADING AND ATTITUDE FAULT. MAINTENANCE REMOVED AND REPLACED THE AHRU, OPS CHECK OK. 2 L 7 2 4F RT T00011AT 2002101500123 20021015 00123 EU 2002 10 15 RAIA00210274 1 20021001 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 553HK 41066 MX-STL- ESCAPE PATH LIGHTS INOPERATIVE. RE-SECURED CONNECTOR AT EMERGENCY ESCAPE PATH LIGHTS, OPS CK OK. 2 L 7 2 4T RT A41NM 2002101500124 20021015 00124 EU 2002 10 15 RAIA00210280 1 20021008 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 557HK 41074 EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE ROW 6 TO BACK. RE-SECURED CONNECTOR AT EMERGENCY ESCAPE PATH LIGHT STRIP, OP C HECK OK. 2 L 7 2 4T RT A41NM 2002101500125 20021015 00125 EU 2002 10 15 RAIA00210281 1 20021008 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 564HK 41081 MX-STL- EMERGENCY ESCAPE PATH LIGHTS INOP AT ROWS 3 & 4. RE-SECURED CONNECTOR AT ESCAPE PATH LIGHTING STRIP, OPS CHECK O K. 2 L 7 2 4T RT A41NM 2002101700024 20021017 00024 NM 2002 10 17 2002UALA01370 1 20020828 A 3232 60B80029 ACTUATOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT MLG DOOR FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 RT WING GEAR FAILED ALTERNATE EXTENSION TEST. NEITHER DOORS NOR GEAR WOULD EXTEND. FAILED ALTERNATE EXTEND ACTUATOR. R EPLACED ACTUATOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2002110400104 20021104 00104 NM 2002 11 4 2002UALA01449 1 20020923 A 3241 140025 TRANSDUCER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG FAILED A UALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 29 178UA 24385 AIRCRAFT RECEIVED ANTI SKID EICAS MSG ON TAKEOFF ROLL. REPLACED NR 5 ANTI-SKID TRANSDUCER. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002110400108 20021104 00108 NM 2002 11 4 2002UALA01480 1 20020921 A 3260 189915 SWITCH BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LANDING GEAR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 203UA 24718 AIRCRAFT RETURNED TO FIELD DUE TO LANDING GEAR FAILED TO RETRACT. REPLACED S106 SWITCH. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112500114 20021125 00114 NM 2002 11 25 2002UALA01488 1 20020924 A 2612 S332T10135 FIRE LOOP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU BAY SHORTED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 331UA 24192 AIRCRAFT RETURNED TO FIELD DUE TO AN APU FIRE WARNING INDICATION. AIRCRAFT EXPERIENCED APU FIRE WARNING WITH APU OFF D URING CLIMB. CREW DISCHARGED APU FIRE BOTTLE AND RETURNED TO THE FIELD. MAINTENANCE INSPECTED APU OVERHEAT DETECTION S YSTEM AND FOUND A HIGH RESISTANCE SHORT TO GROUND AT CONNECTOR D1000, PINS 20 & 26. REPLACED APU FIRE DETECTION LOOP M3 34. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101500126 20021015 00126 NM 2002 10 15 2002UALA01543 1 20021005 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 JETWAY DAMAGE FORWARD OF DOOR 2L JUST BELOW FLOOR LEVEL. DAMAGE IS 10" BY 5" PUNCTURE. SUPPLEMENTAL DATA UPDATE MAJOR R EPAIR ACCOMPLISHED.INSTALLED DOUBLER AND TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101500127 20021015 00127 NM 2002 10 15 2002UALA01548 1 20021008 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 FORWARD PIT FRAME STATION 600 LBL 35 DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVED. INSTALL ED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101500128 20021015 00128 NM 2002 10 15 2002UALA01549 1 20021008 A 5313 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 RIGHT HAND AFT CABIN BETWEEN STATION 1500 TO 1600 CREASE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED DAMAGED SEC TION AND INSTALLED DOUBLER AND TRIPLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101500129 20021015 00129 NM 2002 10 15 2002UALA01555 1 20021007 A 5753 FLAP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 606UA 21867 RIGHT WING INBOARD FLAP HINGE FITTING FLANGE IS CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED HI NGE. 2 L 7 2 4F 4 F RT A1NM E3NE 2002101500130 20021015 00130 NM 2002 10 15 HNAA0200061 1 20020916 A 6120 CONNECTOR DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE NR 2 ENGINE DIRTY A HNAA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 07 908HA 20766 1582 015 NR 2 PROP ATTEMPTED TO FEATHER WHILE ADVANCING POWER FOR TAKE OFF. CAPTAIN RAN ENGINE WITH FEATHER SYSTEN OFF, OPS NORMA L. SELECTED AUTO FEATHER ON OPS NORMAL. CALLED CONRACT MAINTENANCE, CLEANED BOTH TSEU CONNECTOR PLUGS AND NR 2 PROP FE ATHER SOLENOID CONNECTOR PLUG. REPLACED NR 2 TSEU. 2 H 7 2 4T RT A13NM 6 C P7NE 2002101500131 20021015 00131 WP 2002 10 15 ABXA020234 1 20020924 A 5312 99115007 ANGLE DOUG DC9 DC941 302207N WP RADOME CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 SKIN CRACKED ON F.S. 37 BULKHEAD, RIGHT SIDE AT UPPER RADOME ALIGNMENT PIN. REPAIRED AREA IAW ABX DRAWING 05159 AND DC-9 SRM. 2 L 7 2 4F A6WE 2002101500132 20021015 00132 WP 2002 10 15 ABXA020236 1 20020924 A 5700 3923255503 SUPPORT DOUG DC9 DC941 302207N WP REAR SPAR T/E CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 INBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING WAS CRACKED. REPLACED SUPPORT IAW DC-9 SRM 51-10-4 AND 51-30-5. 2 L 7 2 4F A6WE 2002101500133 20021015 00133 WP 2002 10 15 ABXA020237 1 20020925 A 5312 99122439 ANGLE DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 LEFT PYLON BULKHEAD ANGLE CRACKED IN RADIUS ADJACENT TO LOWER SPAR CRACK. REPLACED LEFT BULKHEAD ANGLE IAW REA D953-4530 5-MR. 2 L 7 2 4F A6WE 2002101500134 20021015 00134 WP 2002 10 15 ABXA020238 1 20020925 A 5320 991555047 INTERCOSTAL DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 CRACKED INTERCOSTAL F.S. 1072 AND LONGERON 28 LEFT. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002101500135 20021015 00135 WP 2002 10 15 ABXA020240 1 20020925 A 5313 591142375 SHIM DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 EXFOLIATION IN 2 PLACES, LONGERON 23 LEFT BETWEEN F.S. 973 AND 993. REPLACED LONGERON STIFFENER STRIP IAW DC-9 SRM 51-30 -2. 2 L 7 2 4F A6WE 2002101500136 20021015 00136 WP 2002 10 15 ABXA020241 1 20020925 A 5313 3914677501 SPLICE DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 LONGERON SPLICE AT LONGERON 30, STA. 870 - 880 WAS CRACKED. REPLACED SPLICE IAW DC-9 SRM 53-02 AND 51-30-5. 2 L 7 2 4F A6WE 2002101500137 20021015 00137 WP 2002 10 15 ABXA020243 1 20020925 A 5320 991050313 WEB DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 CUSP WEB CRACKED IN 2 PLACES AT STA. 1040, RIGHT BUTT LINE 54. REPAIRED FLOOR PANEL IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002101500138 20021015 00138 WP 2002 10 15 ABXA020244 1 20020925 A 5320 991050313 WEB DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 CUSP WEB CRACKED AT STA. 1019, RIGHT BUTT LINE 54. FOUND CRACK TO BE MINOR. TRIMMED OUT CRACK IAW DC-9 SRM 53-01. (WITHI N LIMITS) 2 L 7 2 4F A6WE 2002101500139 20021015 00139 WP 2002 10 15 ABXA020245 1 20020928 A 5320 99101516 WEB DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 CUSP WEB AT F.S. 636 - 696, RIGHT SIDE CRACKED. REPLACED WEB IAW DC-9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 2002101500140 20021015 00140 NM 2002 10 15 AWXA200201004 1 20021004 A 5312 65163007 WEB BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 0 0 23261 MCN - MAJOR REPAIR - DURING C-17 CHECK MULTIPLE CRACKS (8 EACH) WERE FOUND ON BULKHEAD BS 178 AT LBL 1.25 AND RBL 1.5 WL 206, LBL 11 AND RBL 11 WL 213, LBL 4.7 WL 198 & 201, RBL 4.7 WL 198 & 210. MAINTENANCE CUTOUT DAMAGE ON WEB BS 178 AT L BL 1.25 AND RBL 1.5 WL 206, LBL 11 AND RBL 11 WL 213, LBL 4.7 WL 198 & 201, RBL 4.7 WL 198 & 210; PERFORMED HFEC INSPECT ION OF CUTOUT AREAS TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND 3 EACH FILLERS; INSTALLED REPAIR PARTS IA W B737-300 SRM 53-10-08, FIG. 211, PG. 287-288D. 2 L 7 2 4F RT A16WE 2002101500141 20021015 00141 NM 2002 10 15 AWXA200201005 1 20021006 A 5320 654581246 STIFFENER BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 DURING C-17 CHECK A 1 1/4 INCH CRACK WAS FOUND ON THE FORWARD SIDE OF STIFFENER IN THE ELECTRONIC EQUIPMENT BAY BS 328, LBL 31, WL 205. MAINTENANCE REMOVED THE DAMAGED STIFFENER AT BS 328, LBL 31, WL 205, FABRICATED A NEW REPLACEMENT STIFFE NER, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 38, FIG. 8, SRM 51-30-01, PG. 19, FIG. 3, PG. 23-29, FIG 7 , 8, & 9, SRM 51-40-05, PG. 4, FIG. 3, AND SRM 51-20-01, PG. 10 & 47, FIG. 2. 2 L 7 2 4F RT A16WE 2002101500142 20021015 00142 NM 2002 10 15 AWXA200201006 1 20021007 A 5720 69737595 STIFFENER BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 DURING C-17 CHECK A 1 3/4 INCH CRACK WAS FOUND ON THE LOWER AFT END OF STIFFENER AT LT WING NR 3 FLAP FAIRING, WS 184.4 0 TO WS 191.00. MAINTENANCE REMOVED THE DAMAGED STIFFENER AT WS 184.40 TO WS 191.00, FABRICATED A NEW REPLACEMENT STIFFE NER, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 16-17, 38, FIG. 8, SRM 51-40-04, PG. 2, FIG. 1, AND SRM 51 -40-05, PG. 7, FIG. 4. 2 L 7 2 4F RT A16WE 2002101500143 20021015 00143 NM 2002 10 15 AWXA200201007 1 20021002 A 5311 651630087 FRAME BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 0 0 25400 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/16" CRACK WAS FOUND ON THE AFT SIDE OF CENTER RADIUS OF THE R/H FRAME AT BS 1 78, WL 208. MAINTENANCE REMOVED THE CRACKED FRAME AND BULKHEAD WEB AT BS 178, WL 208; FABRICATED A NEW REPLACEMENT FRA ME; INSTALLED REPAIR PART AND REINSTALLED BULKHEAD WEB IAW B737-300 SRM 51-40-02, PG. 3-4, 38, FIG. 4. 2 L 7 2 4F RT A16WE 2002101500144 20021015 00144 SW 2002 10 15 PNSA020904 1 20020916 A 2910 2781032682 HYDRAULIC LINE SWRNGN SA227 SA227AC 8780603 SW CRACKED A PNSA K NONE K FLUID LOSS AP APPROACH 1 AL 03 2719H AC713B After selecting gear down on arrival to ANC (flaps were set to 1/2) LH hydraulic warning came on, 2 seconds later RH hyd warning came on. Performed required checklists and declared emergency. Landing was normal without nosewheel steering an d flaps at 1/2. Maintenance found Hydraulic line cracked at bend. 2 L 7 2 4T RT A8SW 2002101600001 20021016 00001 NM 2002 10 16 HNAA0200062 1 20020216 A 2910 82970010301 LINE DHAV DHC8 DHC8201 2809001 NM HYD SYSTEM MALFUNCTIONED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 987HA 1 1 425 NR 2 HYDRAULIC CAUTION LIGHT CAME ON AND REMAINED ON AT GEAR RETRACTION, LANDING GEAR REMAINED IN TRANSIT. PREFORMED A LTERNATE EXTENSION. ON LANDING NR 2 HYDRAULIC PRESSURE RETURNED TO NORMAL. BLED AND SERVICED NR 2 HYDRAULIC SYSTEM. A IRCRAFT RELEASED FOR EVALUATION FLIGHT. 2 H 7 2 4T RT A13NM 2002101600002 20021016 00002 2002 10 16 HNAA0200063 4 20020915 A 3442 MI5853505 RADAR DHAV DHC8 DHC8201 2809001 NM FUSELAGE FALSE INDICATION A HNAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 07 965HA 2269 1999 450 RADAR WOULD NOT PAINT, CYCLED ON/OFF AND WORKS NORMAL. RETURNED TO AIRPORT 2 H 7 2 4T RT A13NM 2002101600003 20021016 00003 NM 2002 10 16 HNAA0200066 1 20020929 A 7931 3014397ASSY GARLOCK SEAL DHAV DHC8 DHC8201 2809001 NM PWA PW120 PW123 NE NR 1 ENGINE LEAKING A HNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 07 968HA 6980 6980 465 AG0010 NR 1 ENGINE OIL PRESSURE FLUX INFLIGHT CAUSING NUMEROUS ILLUMINATION OF THE MASTER CAUTION PANEL, NR 1 ENGINE SHUT DOWN AT 40 PSI. 2 H 7 2 4T 4 T RT A13NM E20NE 2002101600004 20021016 00004 2002 10 16 HNAA0200067 4 20020929 A 2215 7002260722 SERVO DHAV DHC8 DHC8201 2809001 NM AUTOPILOT DEFECTIVE A HNAA O OTHER J WARNING INDICATION LD LANDING 1 EA 07 983HA 16239 3243 478 ON APPROACH INTO CLT DURING THE FLARE ELEVATOR CONTROL WAS EXTREMELY HEAVY AND FELT LIKE THERE WAS NO AIR LOAD ON IT. TH IS PRODUCED AN OVER CONTROL OF THE PITCH ATTITUEUDE AND AIRCRAFT BEGAN TO OSCILLATE DURING THE FLARE ALMOST TO THE POINT OF UNCONTROLLABILTY. MAINTENANCE FOUND THE ELEVATOR AUTOPILOT SERVO BINDING CAUSING ELEVATOR CONTROL SYSTEM BINDING. REMOVED AND REPLACED THE ELEVATOR SERVO. EVALUATION FLIGHT SATISFACTORY. 2 H 7 2 4T RT A13NM 2002101600005 20021016 00005 NM 2002 10 16 HNAA0200068 1 20021004 A 3150 V319 SWITCH DHAV DHC8 DHC8102 2809003 NM COCKPIT DEFECTIVE A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 908HA 45102 45102 015 TAKE OFF WARNING HORN SOUNDED ON TAKE OFF. ABORTED TAKEOFF. COULD NOT SILENCE HORN. THOROUGHLY CLEANED AND INSPECTED M ICRO SWITCHES, FOUND 3151-S3, (TAKE OFF WARNING HORN ON NR 1 PCL) DEFECTIVE - REPLACED MICRO SWITCH. TAKE OFF WARNING HORN SOUNDED WITH TAKE OFF POWER, ABORTED TAKE OFF, RE CHECKED ALL TAKEOFF ITEMS, ALL OK. FOUND SWITCH 3151-S3 ACTUATO R TAB BENT. ADJUSTED TAB OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2002101600006 20021016 00006 NM 2002 10 16 HNAA0200070 1 20021008 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 914HA 53 CREW REPORTED THAT THE FIRST TWO RED FLOOR EMERGENCY ESCAPE PATH LIGHTS AT FWD EXIT AND ALL FOUR RED LIGHTS AT ROW 4 EXI T WERE INOPERATIVE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS SYSTEM. COULD NOT DUPLICATE THE DISCREPANCY 2 H 7 2 4T RT A13NM 2002101600007 20021016 00007 NM 2002 10 16 A6WA200230029 1 20020910 A 5320 FLOOR SUPPORT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 FLOOR SUPPORT AT FRAME 38 HAS MINOR SURFACE CORROSION MAINTENANCE REMOVED CLIP NUTS FROM AFFECTED HOLES ON FRAME 38 FLOO R SUPPORT, REMOVED CORROSION FROM AREA BY MECHANICAL MEANS, ETCHED, ALODINED, PRIMED, TOPCOAT AFFECTED AREAS. REINSTALL ED CLIP NUTS. 2 H 7 2 4T 4 T RT A45NM E20NE 2002101600008 20021016 00008 NM 2002 10 16 AASA0240108 1 20020917 A 5320 WEB BOEING 737 7374Q8 138447Q NM CARGO BAY CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 DURING C CHECK FOUND AFT CARGO BAY WEB CRACKED AT BS 794.5 AND STR 25R. 2 L 7 2 4F RT A16WE 2002101600009 20021016 00009 NM 2002 10 16 ASA2002F00002 1 20020917 A 5711 6545320 SPAR BOEING 737 7374Q8 138447Q NM RT WING LE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 28954 25112 DURING C CHECK FOUND RT LEADING EDGE INBOARD OF NR 2 ENGINE HAS 2 INCH CRACK ON PRIMARY STRUCTURE. REPAIRED CRACK PER E A. 2 L 7 2 4F RT A16WE 2002101600010 20021016 00010 NM 2002 10 16 ASAA0210185 1 20020915 A 5330 6546547 SKIN BOEING 737 737290C 138448V NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 740AS 59271 22578 DURING SCHEDULED SERVICE CHECK FOUND SKIN PANEL AT BODY STATION 539-540, STRINGER 17 CRACKED. REPAIRED CRACK PER SRM. 2 L 7 2 4F 4 F A16WE E2EA 2002101600011 20021016 00011 NM 2002 10 16 ASAA0240101 1 20020916 A 5712 6563439 RIB BOEING 737 7374S3 1384711 NM GE CFM56 CFM56* 13802 NE WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 33152 24795 DURING CHECK FOUND RIB CRACKED AT WBL 135.5 AND BETWEEN STR 2 AND 3. REPAIRED IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101600012 20021016 00012 NM 2002 10 16 ASAA0240103 1 20020917 A 5310 6546921 DOOR FRAME BOEING 737 7374Q8 138447Q NM CARGO BAY CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 28954 25112 DURING C CHECK FOUND FORWARD CARGO DOOR FRAME CRACKED. REPAIRED IAW EA. 2 L 7 2 4F RT A16WE 2002101600013 20021016 00013 NM 2002 10 16 ASAA0240104 1 20020917 A 5230 6546921 STRUCTURE BOEING 737 7374Q8 138447Q NM CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 28954 25112 DURING C CHECK FOUND FORWARD CARGO DOOR CRACKED AT FASTENER HOLE ON LOWER AFT FRAME. REPAIRED IAW SRM. 2 L 7 2 4F RT A16WE 2002101600014 20021016 00014 NM 2002 10 16 ASAA0240105 1 20020917 A 5320 65C2672023 RUB STRIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 DURING C CHECK, FOUND PANEL 6301 RUB STRIP CRACKED. REMOVED AND REPLACED RUB STRIP. 2 L 7 2 4F RT A16WE 2002101600015 20021016 00015 NM 2002 10 16 ASAA0240106 1 20020917 A 5230 6546921172 FRAME BOEING 737 7374Q8 138447Q NM CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 28954 25112 DURING C CHECK FOUND FORWARD CARGO DOOR CRACKED AT FASTENER HOLE ON LOWER CENTER FRAME. REMOVED AND REPLACED LOWER CENT ER FRAME. 2 L 7 2 4F RT A16WE 2002101600016 20021016 00016 NM 2002 10 16 ASAA0240107 1 20020917 A 5330 6546559 SKIN BOEING 737 7374Q8 138447Q NM BS 934.1 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 20507 25096 DURING C CHECK FOUND FUSELAGE SKIN GOUGED AT BS 934.1INCH BELOW STRINGER 16R. REMOVED AND FABRICATED NEW SKIN IAW SRM. 2 L 7 2 4F RT A16WE 2002101600017 20021016 00017 NM 2002 10 16 ASAA0240109 1 20020917 A 5320 SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM562AFR 13802 EU SIDE WALL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 DURING C CHECK FOUND AFT CARGO BAY LEFT HAND FLOOR TO SIDE WALL SUPPORT PLATE AT BS 727 TO 947 IS CORRODED. REMOVED AND FABRICATED NEW IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2002101600018 20021016 00018 NM 2002 10 16 ASAA0270004 1 20020510 A 2612 218A43107 FIRE DETECTOR BOEING 737 737790 13844CN NM GE CFM56 CFM56* 13802 NE FWD CARGO BAY MALFUNCTIONED A ASAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 02 617AS 30542 DURING CLIMB, THE FORWARD CARGO FIRE WARNING LIGHT CAME ON. PILOT FIRED FIRE EXTINGUISHER BOTTLE AND RETURNED TO AIRPOR T. INSPECTED FORWARD CARGO COMPARTMENT, THERE WERE NO SIGNS OF A FIRE. DUST FROM A LIVE SHIPMENT OF BIRDS WAS THE LIKE LY CAUSE OF THE FIRE WARNING. REPLACED THE FIRE EXTINGUISHER BOTTLE. PERFORMED SYSTEMS TESTS. NO PROBLEMS WERE NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101600019 20021016 00019 WP 2002 10 16 I7W2002F00000 2 20020905 A 7310 VALVE SWRNGN SA227 SA227BC 3377519 SW GARRTT TPE331 TPE331* 01514 WP FUEL BYPASS STUCK E I7WA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 05 770ML BC770B ENGINE FUEL BY-PASS ACTUATED CAUSING POWER FLUCTUATION AND NTS ACTUATION. VALVE STUCK OPEN. FOUND FAULT IN AIRCRAFT WI RE BUNDLE NEXT TO CONNECTOR PLUG. 2 L 7 2 4T 3 T RT A8SW E2WE 2002101600020 20021016 00020 SW 2002 10 16 I7W2002F00001 1 20020904 A 2612 FIRE WARNING FRCHLD SA227 SA227CC 3377522 SW GARRTT TPE331 TPE331* 01514 WP NR 2 ENGINE FALSE INDICATION E I7WA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 05 378PH 575 FALSE NR 2 ENGINE FIRE WARNING. FIRE DETECTOR, REMOVED AND REPLACED UNIT. DID NOT SOLVE PROBLEM. STILL TROUBLESHOOTIN G. 2 L 7 2 4T 3 T RT A18SW E2WE 2002101600021 20021016 00021 CE 2002 10 16 IMJ2002F00001 1 20020923 A 2612 99120363 FIRE LOOP CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE NR 1 ENGINE CHAFED E IMJA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 25 15SK 3420 5600395 FIVE MINUTES AFTER DEPARTURE, LT FIRE LIGHT ILLUMINATED. DECLARED EMERGENCY, ACCOMPLISHED CHECKLIST, (DISCHARGED BOTH F IRE BOTTLES AND SECURED NR 1 ENGINE). DIVERTED AND MADE AN UNEVENTFUL LANDING. INVESTIGATION REVALED NO ACTUAL FIRE. SUBSEQUENT INSPECTION REVEALED CHAFED FIRE WARNING SENSOR (FIRE LOOP). 2 L 7 2 4F 4 F RT A22CE E25EA 2002101600080 20021016 00080 EU 2002 10 16 CA021007001 1 20021002 A 2424 51634002 GCU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE RT GENERATOR INOPERATIVE W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) DURING TAXI TO POSITION FOR DEPARTURE, THE CREW NOTED ILLUNINATION OF THE RT AC GENERATOR FAULT LIGHT. TROUBLESHOO TING OF THE SYSTEM DETERMINED THAT THE RT GENERATOR CONTROL UNIT WAS AT FAULT. THE ASSEMBLY WAS REPLACED, THE SYSTEM TES TED SERVICEABLE, AND THE AIRCRAFT RELEASED. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002101600081 20021016 00081 EU 2002 10 16 CA021008002 1 20021005 A 3230 S434013100 VALVE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE MLG FAILED W O OTHER O OTHER CL CLIMB 1 CA (CAN) AFTER T/O LANDING GEAR LEVER TOOK 2-3 ATTEMPS TO MOVE FROM DOWN TO UP.AS PER T.S.M. SAFTY VALVE 49GA FAILED TEST. REPLACED AIRSPEED INTERLOCK VALVE PER AMM 32-31-17 AND OPERATIONAL CHECK CARRIED OUT. PASSED. 2 L 7 2 4F 4 F RT A28NM E29NE 2002101600082 20021016 00082 NE 2002 10 16 CA021009002 2 20020929 A 7230 6047T63P04 CARBON SEAL GENELC CF343B1 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE LEAKING W A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 CA 873358 (CAN) SMOKE IN COCKPIT IMMEDIATELY AFTER TAKEOFF. MOSTLY COMING FROM CAPTAIN'S VENT. DONNED O2 MASKS. SMOKE LAV MESSA GE FOLLOWED. PERFORMED EMERGENCY PROCEDURE. FA NOTICED SMOKE IN CABIN AS WELL.NO FIRE IN LAV. PERFORMED EVACUATION AT GATE.LANDED OVERWEIGHT (50,000 LBS). REMOVED AND REPLACED NR 1 CARBON SEAL IAW GE MM. RAN PACKS WITH ENGINES. NO SMOK E IN CABIN OR COCKPIT. ALL CHECKS GOOD 2 L 7 2 4F 4 F RT A21EA E15NE 2002101600083 20021016 00083 EA 2002 10 16 CA021009003 1 20021005 A 7830 32725706 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RT ENGINE SHEARED W D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA (CAN) RT REV UNLOCKED MESSAGE POSTED. THRUST REVERSER CYCLED SEVERAL TIMES BUT UNSUCCESSFULL. RETURNED TO GATE. AT GATE, SEVERE DAMAGE FOUND TO THRUST REVERSER TRANSLATING COWL. FOUND ACTUATOR AT 11 O'CLOCK POSITION SHEARED. ACTUATOR REPL ACED IN ACCORDANCE WITH AMM.B. 2 L 7 2 4F 4 F RT A21EA E15NE 2002101600084 20021016 00084 NE 2002 10 16 MEX2002299 2 20020916 A 7321 77910010 FUEL CONTROL BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE RT ENGINE FAILED A ASMF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 23 803AM 26268 FLT 600 - MEX-ATL - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF AN STARTING FAILED OF THE RIGHT ENGINE. AT POSITION 24, TECHNICIANS TRIED STARTING AGAIN AND ENGINE REACHED 52 PERCENT OF N2 BUT EGT'S WERE HIGH. AT HANGAR, THE FMC WAS R EPLACED IAW MM 73-21-01, TESTS IAW MM 71-01-02, ALL CORRECT. AT RON, TESTS WERE PERFORMED AGAIN, EVERYTHING WAS CORRECT . (M) 2 L 7 2 4F 4 F RT A2NM E17NE 2002101600085 20021016 00085 NE 2002 10 16 MEX2002309 2 20020924 A 7200 ENGINE BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE LEFT BIRD INGESTION A ASMF O OTHER C F.O.D. CL CLIMB 1 SW 23 301AM 30045 FLT 490 - MID-MEX - DURING TAKEOFF AFTER THE ROTATION MOVEMENT, LEFT ENGINE HAD A BIRD STRIKE, THE ENGINE MOMENTARILY ST ALLED BUT IT RECOVERED ALL PARAMETERS ITSELF. AT MEX, PERFORMED BORESCOPE INSPECTION TO SUCH ENGINE IAW MM 71-05-00 FIG 103. ENGINE WAS FOUND WITHOUT DAMAGED IN HPC INLET AND OUTLET. ENGINE CHIPS AND OIL MAIN FILTER WERE OK. JUST A FIRS T STAGE FAN BLADE WAS BENDED AND TWO FAN BLADES WERE REPLACED IAW MM 72-31-02. (M) 2 L 7 2 4F 4 F RT A2NM E17NE 2002101600086 20021016 00086 NM 2002 10 16 UIEA200200037 1 20020919 A 5414 65B940521 SKIN BOEING 747 747230B 1384889 NM NR 2 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING CURRENT C-CHECK AT SIAEC, FOUND NR 2 PYLON LEFT ACCESS PLATE CUTOUT (463CL) AT NAC STATION 332 TO 350 CRACKED AT LOWER FORWARD CORNER APPROX .5 INCH. TRIMMED OUT CRACKED AREA. HFEC INSPECTED THE TRIMMED OUT AREA AND ALL FASTENER HO LES IN THE REPAIR AREA FOR ADDITIONAL CRACKING. NO CRACKS FOUND. OVERSIZED EXISTING HOLES. FABRICATED FILLER AND REPA IR DOUBLERS. BONDED REPAIR FILLER AND DOUBLERS IN PLACE. (M) 2 L 7 4 4F A20WE 2002101600087 20021016 00087 NM 2002 10 16 UIEA200200038 1 20020919 A 5314 KEELBEAM BOEING 747 747230B 1384889 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING CURRENT C-CHECK, AT SIAEC, FOUND KEEL BEAM CHORD, INBOARD LOWER FLANGE UPPER SURFACE CORRODED, AT BS 1330/1337 AN D 1397, LBL 6. REMOVED CORROSION BY BLENDING. HFEC INSPECTED AREAS OF BLEND OUT AND FASTENER HOLES FOR ADDITIONAL CORR OSION/CRACKS. NO ADDITIONAL CORROSION/CRACKS FOUND. MEASURED BS 1330/37, NO MORE THAN 20 PERCENT OF THICKNESS REMOVED TO A DEPTH OF .088 REMAINING AFTER BLEND OUT. MEASURED BS 1397, ORIGINAL THICKNESS .235, AFTER BLENDING .135 REMAINING. (M) 2 L 7 4 4F A20WE 2002101600088 20021016 00088 NM 2002 10 16 UIEA200200039 1 20020919 A 5314 KEELBEAM BOEING 747 747230B 1384889 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING CURRENT C-CHECK AT SIAEC, FOUND KEEL BEAM BOX, LOWER CHORD, INNER VERTICAL SURFACE CORRODED LEVEL 1, AT BS 1267 R BL 10. CORROSION REMOVED BY BLENDING. HFEC INSPECTED AREA FOR ADDITIONAL CORROSION. NO CORROSION FOUND. ORIGINAL THI CKNESS BEFORE BLENDING WAS .300, AFTER BLENDING .220 REMAINING. (M) 2 L 7 4 4F A20WE 2002101600089 20021016 00089 NM 2002 10 16 UIEA200200040 1 20020905 A 5414 65B940535 SKIN BOEING 747 747230B 1384889 NM NR 2 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING CURRENT C-CHECK AT SIAEC, FOUND NR 2 PYLON TOP CAP SKIN CRACKED AT NAC STATION 264 INBOARD SIDE. CUTOUT CRACKED SKIN AND DOUBLER. SURFACE CORROSION LEVEL 1 REVEALED TO SANDWICHED STIFFENER. REMOVED AFT SECTION OF STIFFENER FOR COR ROSION BLEND REPAIRS. HFEC INSPECTED FOR CRACKS/CORROSION IN TRIMMED AREAS, CUT OUTS AND FASTENER HOLES OF THE REPAIR A REAS. NO CRACKS, CORROSION FOUND. FABRICATED ANGLES, SPLICES, FILLERS AND DOUBLERS. (M) 2 L 7 4 4F A20WE 2002101600090 20021016 00090 NM 2002 10 16 USAABB02160 1 20020914 A 2910 271N61191 HYDRAULIC LINE BOEING 757 757225 1384959 NM LT MLG LEAKING A USAA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 19 607AU 22203 CLT - FLT 1892 - ON GEAR EXTENSION FOR LANDING, CREW NOTED LOSS OF HYDRAULIC QUANTITY ON THE LEFT SYSTEM. CREW PERFORME D A TOWER FLYBY TO ENSURE THE GEAR DOWN AND LOCKED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE L EFT MAIN LANDING GEAR OVER CENTER DOWN LOCK LINE, THE EDP AND THE ACMP. (M) 2 L 7 2 4F RT A2NM 2002101600091 20021016 00091 EU 2002 10 16 USAASA02081 1 20020919 A 3350 1013101 SIGN AIRBUS 320 A320214 3930316 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 111US 1114 LGA - THE EMERGENCY LIGHT SYSTEM FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE RIGHT CABIN EMERGENCY EXIT LIGHT SIGN. FUNCTIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002101600092 20021016 00092 EU 2002 10 16 USAASA02082 1 20020922 A 3260 201117017 UPLOCK SENSOR AIRBUS A319 A319112 3930323 EU LT MLG INOPERATIVE A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 716UW 1055 IAH - FLT 775 - EN ROUTE PHL-IAH, WHEN THE LANDING GEAR WAS EXTENDED, RECEIVED THREE GREEN, DOWN AND LOCKED, INDICATIONS AND ONE RED, UNLOCKED, INDICATION FOR THE LEFT MAIN GEAR, WITH AN ASSOCIATED AMBER 'X' ECAM INDICATION. THE GEAR WAS C YCLED AND THE SAME INDICATIONS OCCURRED. THE LANDING GEAR WAS VERIFIED DOWN, AND JUST BEFORE LANDING, THE GEAR INDICATI ONS BECAME NORMAL. LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT GEAR UPLOCK. OPERATIONALLY CHE CKED OK. (M) 2 L 7 2 4F RT A28NM 2002101600093 20021016 00093 NE 2002 10 16 SWAA022189 2 20020917 A 7200 CFM567 ENGINE BOEING 737 7377H4 1384404 NM GE CFM56 CFM567B24 NE RIGHT FLAMED OUT A SWAA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 29 711HK 27845 874171 INFIGHT SHUTDOWN, DECLARED EMERGENCY, AIR TURNBACK, DURING CLIMB NR 2 ENGINE FLAMED OUT. REMOVED AND REPLACED NR 2 ENGI NE PER MM. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002101600094 20021016 00094 NM 2002 10 16 SWAA022203 1 20020923 A 3350 604222 BATTERY BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BAT TERY PER MM. 2 L 7 2 4F RT A16WE 2002101600095 20021016 00095 NM 2002 10 16 SWAA022210 1 20020923 A 5320 6551698 SPLICE BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002101600096 20021016 00096 NM 2002 10 16 SWAA022216 1 20020921 A 5712 6545445 RIB BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 AND STR 3. REPAIRED RIB LOW ER CHORD PER BFG ER. 2 L 7 2 4F RT A16WE 2002101600097 20021016 00097 NM 2002 10 16 SWAA022217 1 20020925 A 5534 6550222 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED D CHECK, FOUND VERTICAL STABILIZER REAR SPAR LT AND RT DRAG BRACE FITTINGS CORRODED. REPAIRED FITTINGS PER SRM. 2 L 7 2 4F RT A16WE 2002101600098 20021016 00098 NM 2002 10 16 SWAA022219 1 20020923 A 5534 6546874 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULE D CHECK, FOUND VERTICAL STABILIZER FAILSAFE LUG FITTINGS CORRODED. REPAIRED FITTINGS PER BFG ER. 2 L 7 2 4F RT A16WE 2002101600099 20021016 00099 NM 2002 10 16 SWAA022222 1 20020923 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 AFT ENTRY DOOR EMERGENCY EXIT LIGHT FELL LOOSE. REINSTALLED EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2002101600100 20021016 00100 2002 10 16 SWAA022225 4 20020924 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002101600101 20021016 00101 NM 2002 10 16 SWAA022227 1 20020924 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM FWD ENTRY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPECIAL VISIT, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR MOUNT SUPPORT BRACKET CORRODED. REMOVED AND REPLACED BRACKET PER SRM. 2 L 7 2 4F RT A16WE 2002101600102 20021016 00102 2002 10 16 SWAA022232 4 20020925 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002101600103 20021016 00103 NM 2002 10 16 SWAA022233 1 20020924 A 3350 57771 CAP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 EEPLS END CAP LOOSE AT FWD END. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 2002101600104 20021016 00104 NM 2002 10 16 SWAA022234 1 20020926 A 5320 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002101600105 20021016 00105 NM 2002 10 16 SWAA022256 1 20020928 A 3350 BR2013 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 740SW 29276 EEPLS COVERS LOOSE AND WIRES EXPOSED. SECURED COVERS AND WIRES PER MM. 2 L 7 2 4F RT A16WE 2002101600106 20021016 00106 2002 10 16 SWAA022262 4 20020927 A 2565 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM . 2 L 7 2 4F RT A16WE 2002101600107 20021016 00107 NM 2002 10 16 SWAA022308 1 20021002 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 092SW 22964 DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING AT AFT CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2002101600108 20021016 00108 2002 10 16 SWAA022309 4 20021002 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 092SW 22964 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002101600109 20021016 00109 NM 2002 10 16 SWAA022318 1 20021002 A 5230 BAC1490 TEE CHORD BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR LOWER T-CHORD CRACKED AT AFT END. REMOVED AND REPLACED T-CHORD PER CC O. 2 L 7 2 4F RT A16WE 2002101600110 20021016 00110 NM 2002 10 16 VNAA0209032 1 20020923 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 437JS 15938 1212 3055 THE CREW REPORTED THAT THE LAST ROW OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACE D THE 7LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED A ND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002101600111 20021016 00111 NM 2002 10 16 VNAA0209033 1 20020923 A 3350 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN LOOSE A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 425JS 3037 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROW 4 TO 6 WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND RESEC URED THE EMERGENCY FLOOR LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WE RE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002101600112 20021016 00112 NM 2002 10 16 VNAA0209034 1 20020924 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 460PS 15201 69 3061 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGEN CY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT W AS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002101600113 20021016 00113 NM 2002 10 16 VNAA0209035 1 20020926 A 3350 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN LOOSE A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 425JS 3037 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND RESECURED THE EMERGENCY F LOOR LIGHTING IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAF T WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002101600114 20021016 00114 NM 2002 10 16 VNAA0209036 1 20020926 A 3350 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN LOOSE A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 425JS 3037 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND RESECURED THE EMERGENCY F LOOR LIGHTING IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAF T WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002101600115 20021016 00115 NM 2002 10 16 VNAA0209038 1 20020930 A 2820 ZCV171 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUEL SYSTEM FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 471PS 17371 3007 EN ROUTE, THE CREW RECEIVED A FEEDER TANK LOW CAS MESSAGE AND DECIDED TO RETURN TO DAY. MAINTENANCE INSPECTED AND REPLA CED THE MOTIVE FLOW NON RETURN VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PE RFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002101600116 20021016 00116 NM 2002 10 16 VNAA0210002 1 20021002 A 3260 PROXIMITY SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT MLG OUT OF ADJUST A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 458PS 3068 DURING CLIMB OUT, THE CREW DISCOVERED THAT THE GEAR WOULD NOT RETRACT AND RETURNED TO PIT. MAINTENANCE INSPECTED AND FO UND THE RIGHT HAND MAIN LANDING GEAR PROXIMITY SENSOR OUT OF ALIGNMENT. MAINTENANCE ADJUSTED THE SENSOR IN ACCORDANCE W ITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002101600117 20021016 00117 NM 2002 10 16 ANCF200200019 1 20021014 A 5610 S141T4871 SEAL BOEING 767 767259 1385136 NM WINDOW DAMAGED W ANCF A UNSCHED LANDING O OTHER CR CRUISE 1 SO 23 986AN 24835 DURING CRUISE WITH A DIFFERENTIAL PRESSURE OVER 4.5, THERE IS A LOUDLY NOISE COMING OUT OF 2L WINDOW. MASKING CREW AND A TC COMMUNICATIONS IMPOSSIBLE, CREW DECIDED TO RETURN TO EDR. FOUND 2L WINDOW SEAL DAMAGED, CAUSING A PRESSURIZATION LE AK, REMOVED AND REPLACED 2L WINDOW SEAL IAW AMM 56-11-11 PAG 401, PERFORMED PRESSURIZATION LEAK TEST IAW AMM 05-51-24 PA G 201 TO 209, WITH SATISFACTORY RESULTS. 2 L 7 2 4F RT A1NM 2002101600118 20021016 00118 NM 2002 10 16 VNAA0210003 1 20021003 A 2120 CLAMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A/C BAY LOOSE A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 438JS 3056 THE FLIGHT ATTENDANT REPORTED SMELLING SMOKE IN THE CABIN. THE CREW PERFORMED THE SMOKE REMOVAL CHECK LIST AND THE SMOK E CLEARED. AS A PRECAUTION THE CREW DECLARED AN EMERGENCY AND REQUESTED PRIORITY HANDLING. AFTER LANDING THE FLIGHT AT TENDANT AGAIN REPORTING A SMOKE SMELL IN THE CABIN. THE CREW THEN EVACUATED THE PASSENGERS. MAINTENANCE INSPECTED, REP OSITIONED, AND RESECURED THE LEFT HAND PACK CLAMPS AT THE HEAT EXCHANGER. OPERATIONAL CHECKS WERE PERFORMED AND THE AIR CRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002101600119 20021016 00119 NM 2002 10 16 VNAA0210004 1 20021004 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 460PS 14349 82 3061 THE CREW REPORTED THAT THE LAST ROW OF EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002101600120 20021016 00120 NM 2002 10 16 VNAA0210005 1 20021007 A 3250 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING DIRTY A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 472PS 3008 ON THE TAKEOFF ROLL, THE AIRCRAFT MADE A UNCOMMANDED SWERVE TO THE LEFT. THE CREW THEN ABORTED TAKEOFF. MAINTENANCE IN SPECTED AND CLEANED AND RESEATED THE FEEDBACK POTS CANNON PLUG TO THE NOSE WHEEL STEERING CONTROL MANIFOLD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002101600121 20021016 00121 NM 2002 10 16 QXEA0201677 1 20021014 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM ZONE 200 FAULTY A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 14257 354 488 PDX-AFT EMERGENCY OVERHEAD LIGHT INOPERATIVE. FOUND AFT EMERGENCY LIGHT BATTERY BAD. REMOVED AND REPLACED BATTERY PACK A SSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002101600122 20021016 00122 NM 2002 10 16 AALA20021197 1 20020820 A 2730 5579816 TRANSDUCER BOEING 757 757223 1384957 NM ELEVATOR FAILED A AALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SW 21 192AN 32386 AFTER TAKEOFF AT ALTITUDE WHEN THE AUTOPILOT WAS TURNED ON THE TRIM WOULD RUN NOSE UP IMMEDIATELY. EACH AUTOPILOT WAS T RIED WITH SAME RESULTS, RETURN TO DFW. REPLACED RIGHT ELEVATOR NEUTRAL SHIFT TRANSDUCER, OPS CHECK GOOD. PERFORMED ALL REQUIRED CHECKS. (M) 2 L 7 2 4F RT A2NM 2002101600123 20021016 00123 WP 2002 10 16 AALA20021202 1 20020820 A 3397 WIRE DOUG DC9 DC982 3022082 WP A/C BAY DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 478AA 49653 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SIDEWALL CATWALK EMERGENCY EXIT LIGHT IN TAIL COMPARTMENT INOPERATIVE. REPA IRED FORWARD SIDEWALL CATWALK EMERGENCY EXIT LIGHT WIRE AT QUICK DISCONNECT TERMINAL. SYSTEM GROUND CHECKED NORMAL OPERA TION. (M) 2 L 7 2 4F A6WE 2002101600124 20021016 00124 WP 2002 10 16 AALA20021203 1 20020819 A 2150 591012169 ACM DOUG DC9 DC982 3022082 WP A/C BAY MALFUNCTIONED A AALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SW 21 205AA 49155 RDU - FLT 735 - EN ROUTE RDU-ORD, CLIMBING THROUGH 27,000 FEET TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. LIG HT EXTINGUISHED AFTER ACCOMPLISHING CHECKLIST AFTER APPROXIMATELY 1 MINUTE LIGHT ILLUMINATED AGAIN. RETURNED RDU AND LA NDED WITHOUT INCIDENT. REPLACED RIGHT ACM AND AUGMENTATION VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600125 20021016 00125 NM 2002 10 16 AALA20021211 1 20020815 A 2421 GEN3014 IDG BOEING 777 777223 1385213 NM RT ENGINE FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 778AN 29587 DFW - RIGHT GENERATOR DRIVE SHAFT DISCONNECTED IN FLIGHT. DEFERRED RIGHT IDG DUE TO NS AT LGW OF OIL PRESS CANNON PLUGS MEL REF 24-03. RIGHT ENGINE IDG WAS REPLACED 8-16-02 LEAK AND OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT T00001SE 2002101600126 20021016 00126 NM 2002 10 16 AALA20021212 1 20020814 A 2421 GEN5103 IDG BOEING 767 767323 1385205 NM RT ENGINE FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 374AA 25201 RIGHT GENERATOR DRIVE LEFT ILLUMINATED, IDG DISCONNECTED AS PER OM. UNABLE TO REMOVED QAD RING FOR IDG. REPLACEMENT, P LACARDED RIGHT IDG AS PER MEL 24-01 AUTH LGWA-354DC-A. REMOVED AND REPLACED RIGHT IDG PER MM. OPS CHECK GOOD. NO LEAK S NOTED REMOVED MEL 24-01. (M) 2 L 7 2 4F RT A1NM 2002101600127 20021016 00127 NM 2002 10 16 AALA20021219 1 20020727 A 3350 1317 LIGHT BOEING 767 767323 1385205 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 396AN 29603 AFW - FOUND EXTERIOR EMERGENCY LIGHT FORWARD OF AFT CARGO DOOR INOPERATIVE. REPLACED AND RESEATED LAMP, OPS CHECKS GOOD . (M) 2 L 7 2 4F RT A1NM 2002101600128 20021016 00128 WP 2002 10 16 AALA20021223 1 20020826 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 577AA 53154 MIA - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT PATH LIGHT FROM SEAT 20D AFT INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY EXIT PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600129 20021016 00129 WP 2002 10 16 AALA20021224 1 20020825 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 466AA 49596 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS FROM ROW 8-11 INOPERATIVE. SECURED EMERGENCY EXIT PAT H LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600130 20021016 00130 WP 2002 10 16 AALA20021225 1 20020825 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 241AA 49254 DFW - DURING OVERNIGHT MAINTENANCE, SEAT 11D EMERGENCY EXIT PATH LIGHT INOPERATIVE. REPLACED SEAT 11D EMERGENCY EXIT PA TH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600131 20021016 00131 WP 2002 10 16 AALA20021226 1 20020824 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 73444 49470 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AFT TAIL CONE LIGHT LEFT SIDE INOPERATIVE. SECURED EMERGENCY EXIT PA TH LIGHT GROUND WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600132 20021016 00132 WP 2002 10 16 AALA20021227 1 20020824 A 3397 GROUND WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 73444 49470 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT FLIGHT ATTENDANT SEAT. RESECURED EMERGENCY EXIT LIGHT FI XTURE GROUND WIRE IN TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600133 20021016 00133 WP 2002 10 16 AALA20021228 1 20020823 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAILCONE CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 491AA 49684 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE HANDLE LOWER EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED TAIL CONE HANDLE LOWER EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600134 20021016 00134 2002 10 16 AALA20021229 4 20020827 A 3454 VOR SYSTEM BOEING 767 767323 1385205 NM COCKPIT MALFUNCTIONED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 379AA 25448 COPILOTS VOR HAS OFF FLAG NEEDLE DOES NOT POINT TO STATION NO COURSE ON CDI. DME WORKS ONLY WITHIN 25 MILES OR LESS FRO M STATIONS. RIGHT VOR RECEIVER BITE TEST CARRIED OUT, NO FAULTS SHOWN TEST PASS OK. (M) 2 L 7 2 4F RT A1NM 2002101600135 20021016 00135 WP 2002 10 16 AALA20021246 1 20020830 A 3350 BATTERY DOUG DC9 DC982 3022082 WP A/C BAY LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 292AA 49304 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN TAIL CONE SECTION INOPERATIVE. SECURED EMERGENCY EXIT LIGH TS BATTERY IN TAIL CONE SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600136 20021016 00136 WP 2002 10 16 AALA20021247 1 20020830 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7531A 49923 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM SEAT 22D THROUGH 26D INOPERATIVE. SECURED EMERGENCY EXIT LIGHTS BATTERY AT SEAT 22-26. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600137 20021016 00137 WP 2002 10 16 AALA20021248 1 20020831 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 456AA 49561 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 19 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BATTER Y. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600138 20021016 00138 WP 2002 10 16 AALA20021249 1 20020827 A 3397 WIRE DOUG DC9 DC982 3022082 WP A/C BAY DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 251AA 49270 DFW - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT LIGHTS OVER CATWALK INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGH TS WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600139 20021016 00139 WP 2002 10 16 AALA20021250 1 20020829 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 271AA 49293 DFW - DURING OVERNIGHT MAINTENANCE, AFT CEILING EMERGENCY EXIT LIGHTS MISSING CONNECTORS. REPLACED EMERGENCY EXIT LIGHT S CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600140 20021016 00140 WP 2002 10 16 AALA20021251 1 20020902 A 2120 COUPLING DOUG DC9 DC982 3022082 WP A/C BAY BLOWN A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 408AA 49319 ORD - FLT 2099 - EN ROUTE ORD-MCO, TAIL COMPARTMENT TEMPERATURE HIGH RED CAME ON AT 25,000 FEET. DURING CLIMB LIGHT EXT INGUISHED 20 SECONDS AFTER RED BOX PROCEDURES COMPLIED WITH. LIGHT CAME BACK ON IN 1 MINUTE AND WAS ON FOR ABOUT 2 MINU TES BEFORE EXTINGUISHING FOR REMINDER OF FLIGHT. RETURNED ORD AND LANDED WITHOUT INCIDENT. REPLACED RIGHT PACK TRIM DU CT COUPLING. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600141 20021016 00141 WP 2002 10 16 AALA20021252 1 20020829 A 7830 B-NUT DOUG DC9 DC983 3022083 WP THRUST REVERSER LOOSE A AALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 562AA 49344 ORD - FLT 460 - FLIGHT ATTENDANT REPORTED ABNORMALLY HEAVY SMOKE/HAZE IN MAIN CABIN APPROXIMATELY 3 MINUTES AFTER TAKEOF F. WENT TO HIGH PRESSURE BLEED OFF, RETURNED TO ORD AND LANDED WITHOUT INCIDENT. TIGHTEN B NUT CONNECTION ON LEFT THRUS T REVERSER CONTROL VALVE AND APU. LEAK CHECK GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002101600142 20021016 00142 NM 2002 10 16 AALA20021263 1 20020905 A 2421 GEN5103 IDG BOEING 767 767323 1385205 NM NR 2 ENGINE FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 358AA 24039 LAX - GENERATOR OFF LIGHT ILLUMINATED ACCOMPANIED BY A RIGHT GENERATOR DRIVE DISCONNECT. REMOVED AND REPLACED NR 2 ENGI NE IDG AS REQUIRED, OPS CHECK GOOD. LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A1NM 2002101600143 20021016 00143 WP 2002 10 16 AALA20021265 1 20020908 A 3350 LIGHT DOUG DC9 DC982 3022082 WP A/C BAY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 227AA 49177 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED TAIL CONE CEILING EMER GENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600144 20021016 00144 WP 2002 10 16 AALA20021266 1 20020908 A 3350 LIGHT DOUG DC9 DC982 3022082 WP A/C BAY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 266AA 49291 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD TAIL CONE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED OVERHEAD TAIL CONE EM ERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600145 20021016 00145 WP 2002 10 16 AALA20021267 1 20020905 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 557AN 53087 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS AT SEATS 20D THROUGH 17D INOPERATIVE. ADJUSTED EMERG ENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600146 20021016 00146 EA 2002 10 16 COMA0260581 1 20021014 A 2610 24403615 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA R/H MLG DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 964CA 7129 FLIGHT 5071 - MLG BAY OVERHEAT WARNING.REPLACED OVERHEAT SENSING ELEMENT R/H WHEEL WELL. 2 L 7 2 4F RT A21EA 2002101600147 20021016 00147 EA 2002 10 16 COMA0260582 1 20021012 A 3220 16040101 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NLG DAMAGED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 917CA 21661 7017 FLIGHT 6088 GEAR DISAGREE MESSAGE. NLG FAILED TO RETRACT.REPLACED THE NLG ASSY. 2 L 7 2 4F RT A21EA 2002101600148 20021016 00148 EA 2002 10 16 COMA0260583 1 20021011 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR INOPERATIVE A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 989CA 7215 FLIGHT 5675 FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOPERATIVE.REPLACED STRIP LAMP. 2 L 7 2 4F RT A21EA 2002101600149 20021016 00149 EA 2002 10 16 COMA0260584 1 20021013 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS UK UNKNOWN 1 SO 01 967CA 7134 FLAPS FAILED AT 17 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002101600150 20021016 00150 EA 2002 10 16 COMA0260585 1 20021014 A 2720 6229815704 CIRCUIT BOARD CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA K NONE F E FLT CONT AFFECTED VIBRATION/BUFFET CR CRUISE 1 SO 01 458CA 3977 7613 FLIGHT 5649 RUDDER FLUCTUATING DURING FLIGHT AND VIBRATING REPLACED THE #2 FCC-4000 2 L 7 2 4F RT A21EA 2002101600151 20021016 00151 EA 2002 10 16 COMA0260586 1 20021014 A 3230 7179015 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA INST PANEL MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 914CA 3391 7012 FLIGHT 5537 LANDING GEAR CONTROL HANDLE CANNOT BE SELECTED TO UP.REPLACED THE LANDING GEAR CONTROL HANDLE ASSY. 2 L 7 2 4F RT A21EA 2002101600152 20021016 00152 WP 2002 10 16 AALA20021295 1 20020909 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 464AA 49594 DTW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY REMOVABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD ENTRY EM ERGENCY EXIT LIGHTING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101600153 20021016 00153 NM 2002 10 16 GAIA02108OP 1 20020919 A 3610 CLAMP BOEING 727 727232 1384082 NM NR 1 STRUT LOOSE A GAIA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 77780 20635 FLT 778 - FWA-BOS - DURING CRUISE, THE NR 1 ENGINE STRUT LIGHT ILLUMINATED. ACCOMPLISHED AOM PROCEDURE AND THE LIGHT EX TINGUISHED. THE AIRCRAFT CONTINUED TO BOS AND LANDED WITHOUT FURTHER OCCURRENCE. FOUND A LOOSE CLAMP AT THE SIXTH STAG E CHECK VALVE IN THE NR 1 STRUT COMPARTMENT AND TIGHTENED THE SAME. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETUR NED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101600154 20021016 00154 NM 2002 10 16 GAIA02110ST 1 20020919 A 5320 TORQUE BOX BOEING 727 727251 138408H NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE VENTRAL STAIRS RIGHT LOWER TORQUE BOX HAS A CRACKED REPAIR CHANNEL A T BS 1263. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-2, FIGURE 6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101600155 20021016 00155 NM 2002 10 16 GAIA02112ST 1 20020919 A 5347 BAC1520729 SEAT TRACK BOEING 727 727251 138408H NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE SEAT TRACK WAS CRACKED AT BS 720D, RBL 45.5. ACCOMPLISHED REPAIR IA W BOEING 727 SRM 53-10-5, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101600156 20021016 00156 NM 2002 10 16 GAIA02114ST 1 20020919 A 5315 651627910 FLOORBEAM BOEING 727 727251 138408H NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT A FLOORBEAM AT BS 783, LBL 45.5 HAS CORROSION AT UPPER T-CAP. ACCOMPLIS HED REPAIR IAW BOEING 727 SRM 53-10-8, FIGURE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101600157 20021016 00157 NM 2002 10 16 GAIA02115ST 1 20020919 A 5320 65C3440613 BEAM BOEING 727 727251 138408H NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE AFT PRESSURE BULKHEAD VERTICAL BEAM AT BS 1183, WL 240, RBL 36 IS CR ACKED AT THE INBOARD CHORD. ACCOMPLISHED REPAIR IAW BOEING SERVICE BULLETIN 727-53-0192, REV 1. THE AIRCRAFT WAS RETUR NED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101600158 20021016 00158 NM 2002 10 16 GAIA02116ST 1 20020919 A 5311 FRAME BOEING 727 727251 138408H NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT A FRAME AT BS 344, STRINGER S2L WAS CRACKED. ACCOMPLISHED REPAIR IAW BO EING 727 SRM 53-10-2, FIGURE 3 AND 53-10-4, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101600159 20021016 00159 NM 2002 10 16 GAIA02117ST 1 20020919 A 5347 BAC1520792 SEAT TRACK BOEING 727 727251 138408H NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE SEAT TRACK AT BS 520, RBL 45.5 IS CORRODED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-5, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101600160 20021016 00160 NM 2002 10 16 GAIA02118ST 1 20020919 A 5230 SKIN BOEING 727 727251 138408H NM CARGO DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE MAIN CARGO DOOR INNER SKIN IS CRACKED AROUND NR 3 LATCH HOOK ASSEMBL Y FROM AFT CENTER ATTACH BOLT. ACCOMPLISHED REPAIR IAW COTNEY EDR03-1, 8110-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101600161 20021016 00161 NM 2002 10 16 GAIA02119ST 1 20020919 A 5311 FRAME BOEING 727 727251 138408H NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 380 WAS DENTED AT STRINGER S5L. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-4, FIGURE 2. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101600162 20021016 00162 NM 2002 10 16 GAIA0211ST 1 20020919 A 5315 FLOORBEAM BOEING 727 727251 138408H NM FUSELAGE DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE FLOORBEAM AT BS 560, LBL 3 HAVE NUMEROUS HOLES THROUGH THE UPPER FLA NGE AND RADIUS. ACCOMPLISHED A REPAIR IAW BOEING 727 SRM 51-40-4, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101600163 20021016 00163 WP 2002 10 16 GTIA020956 1 20020826 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND MID PIT STATION 769 LBL 16 INCHES IS CORRODED AT FORWARD BRACKET SUPPORT INTERCOSTAL AND AREA NUTS PLATES RU STED. REMOVED FASTENERS/INTERCOSTAL. FABRICATED NEW INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002101600164 20021016 00164 WP 2002 10 16 GTIA020957 1 20020829 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - MID CARGO PIT CORROSION ON FLOOR SUPPORT, LBL 16 INCHES, FS 769. REMOVED PART. LOCATED AND DRILLED REPLACEMENT S UPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002101600165 20021016 00165 WP 2002 10 16 GTIA020958 1 20020904 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FORWARD B/B AT STATION 218, LONGERON 18L HAS CORROSION AT CUSP. REMOVED CORRODED FIRST WEB. FABRICATED REPAIR FO R FIRST WEB. INSTALLED FIRST WEB REPAIR AND SPLICES. (M) 2 L 7 2 4F A6WE 2002101600166 20021016 00166 WP 2002 10 16 GTIA020959 1 20020826 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND MID PIT STATION 788 RBL 27 INCHES INTERCOSTAL IS CRACKED. REMOVED INTERCOSTAL. FABRICATED NEW INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002101600167 20021016 00167 WP 2002 10 16 GTIA020960 1 20020821 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND FORWARD CARGO DOOR CUT OUT AFT OUTER SKIN DAMAGED. CUT AWAY DAMAGED AREA. FABRICATED FILLER, INSIDE/EXTERN AL DOUBLER. INSTALLED INT/EXT DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2002101600168 20021016 00168 WP 2002 10 16 GTIA020961 1 20020823 A 5310 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND PIT DOOR JAMB CUT OUT HAS CORROSION ON DOUBLER. REMOVED DOOR JAMB DOUBLER AND DOUBLER ANGLE. FABRICATED DO UBLER. INSTALLED DOOR JAMB DOUBLER AND ANGLE. (M) 2 L 7 2 4F A6WE 2002101600169 20021016 00169 WP 2002 10 16 GTIA020962 1 20020829 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND RIGHT HPV COMPARTMENT AFT BULKHEAD WEB CRACKED RBL 20 INCHES NEAR DOOR OPENING. FABRICATED DOUBLER REPAIR. INSTALLED THE DOUBLER REPAIR. (M) 2 L 7 2 4F A6WE 2002101600170 20021016 00170 NM 2002 10 16 KPVA200225 1 20020917 A 3350 10005511 LIGHT DHAV DHC8 DHC8103 1386005 NM COCKPIT INOPERATIVE A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805WP 353 PORTABLE EMERGENCY LIGHT ABOVE COCKPIT DOOR INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT ABOVE COCKPIT DO OR. OPS CHECK GOOD IAW DHC MM 33-51-00 PAGE 201-202. NO DEFECTS NOTED. (M) 2 H 7 2 4T RT A13NM 2002101600171 20021016 00171 NM 2002 10 16 KPVA200226 1 20020918 A 3230 83200500003 CONTROL CABLE DHAV DHC8 DHC8103 1386005 NM COCKPIT FRAYED A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 807WP 023 NOSE GEAR ALTERNATE RELEASE CABLE FRAYED WHERE IT COMES OUT OF RELEASE HANDLE. REMOVED AND REPLACED NLG ALTERNATE RELEA SE CABLE, TURNBUCKLE TO HANDLE. (M) 2 H 7 2 4T RT A13NM 2002101600172 20021016 00172 NM 2002 10 16 KPVA200227 1 20020918 A 1430 85210276101 BOLT DHAV DHC8 DHC8103 1386005 NM AIRSTAIRS LOOSE A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 806WP 357 HNL - A BOLT ON FORWARD SIDE OF AIRSTAIR SUPPORT FOR IS LOOSE AND INHIBITS DOOR FROM OPENING. INSTALLED THREADED BUSHIN G ON UPPER STAY STRUT IAW DHC 8MM 52-10-00 PATE 219 PARAGRAPH C. NO DEFECTS NOTED. (M) 2 H 7 2 4T RT A13NM 2002101600173 20021016 00173 NM 2002 10 16 MEX2002297 1 20020913 A 2910 316N310032 HYDRAULIC LINE BOEING 757 7572Q8 1384972 NM HYD SYSTEM LEAKING A ASMF D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SW 23 805AM 26272 FLT 405 - JFK - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF AN HYDRAULIC LEAKAGE IN THE RIGHT SYSTEM. TECHNICIAN RE VIEWED SUCH SYSTEM AND FOUND LEAKAGE IN A PIPELINE FROM THE FILTERS TO THE WHEELS. PIPELINE WAS REPLACED IAW MM 29-11-1 7, TESTS OK. (M) 2 L 7 2 4F RT A2NM 2002101600174 20021016 00174 WP 2002 10 16 MEX2002298 1 20020913 A 2560 COVER DOUG DC9 DC982 3022082 WP SERVICE DOOR DETACHED A ASMF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 23 1003Y 48068 FLT 509 - MEX-VSA - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF THAT THE SLIDE RAFT COVER OF THE REAR SERVICE DOOR W AS DETACHED. THE TECHNICIANS DETECTED THE COVER OUT OF ITS RESPECTIVE RECEPTACLE. THE COVER WAS REINSTALLED IAW MM 25- 62-01, AND THE DOOR WAS CLOSED IN A CORRECT WAY. (M) 2 L 7 2 4F A6WE 2002101600175 20021016 00175 EU 2002 10 16 USAA020336 1 20020818 A 5320 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 718UW 9754 1077 TPA - FOUND FLOOR SUPPORT CORRODED 1 SQUARE INCH, UPPER SURFACE OF DUMMY RAIL FLOOR SUPPORT. BLENDED CORROSION AREA, HF EC INSPECTED PER EA 94338. (M) 2 L 7 2 4F RT A28NM 2002101600176 20021016 00176 EU 2002 10 16 USAABA02019 1 20020910 A 3350 32146210 CONNECTOR AIRBUS 330 A330323 3930335 EU CABIN DIRTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 672UW 0333 PHL - FOUND EPSU BATTER FAULT ON EPSU 2. MAINTENANCE CLEANED THE CONNECTOR ON EPSU 2. (M) 2 L 7 2 4F RT A46NM 2002101600177 20021016 00177 NM 2002 10 16 USAABB02150 1 20020906 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 18 AND 26 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002101600178 20021016 00178 NM 2002 10 16 USAABB02151 1 20020907 A 3397 WIRE BOEING 757 757225 1384959 NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 600AU 22192 CLT - FOUND EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. MAINTENANCE REPAIRED WIRING AND REPLACED THE BATTERY PACK AT M370. (M) 2 L 7 2 4F RT A2NM 2002101600179 20021016 00179 NM 2002 10 16 USAABB02152 1 20020910 A 3350 86210066 BATTERY PACK BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AU 27807 LAX - FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 13, 23 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. (M) 2 L 7 2 4F RT A2NM 2002101600180 20021016 00180 NM 2002 10 16 USAABB02153 1 20020911 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 652US 24765 LAX - FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. (M) 2 L 7 2 4F RT A1NM 2002101600181 20021016 00181 NM 2002 10 16 USAABB02154 1 20020911 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 613AU 27144 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 10. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002101600182 20021016 00182 NM 2002 10 16 USAABB02155 1 20020915 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 608AU 22204 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002101600183 20021016 00183 NM 2002 10 16 USAABB02156 1 20020913 A 3350 86210066 BATTERY PACK BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 628AU 27806 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4 AND 9 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. (M) 2 L 7 2 4F RT A2NM 2002101600184 20021016 00184 NM 2002 10 16 USAABB02157 1 20020914 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 651US 24764 LAX - FOUND LEFT AFT FLOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY. (M) 2 L 7 2 4F RT A1NM 2002101600185 20021016 00185 NM 2002 10 16 USAABB02158 1 20020914 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 652US 24765 CDG - FOUND OVERWING EXIT IDENTIFIERS AND ASSOCIATED AISLE LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY. (M) 2 L 7 2 4F RT A1NM 2002101600186 20021016 00186 NM 2002 10 16 USAABB02159 1 20020915 A 3397 SPLICE BOEING 767 7672B7 1385107 NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 653US 24894 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS FROM ROWS 6 THROUGH 12 INOPERATIVE. MAINTENANCE REPAIRED A WIRING SPLICE AT RO W 12. (M) 2 L 7 2 4F RT A1NM 2002101600187 20021016 00187 NM 2002 10 16 USAABB02161 1 20020918 A 2421 739515 IDG BOEING 767 7672B7 1385107 NM GE CF6 CF680C2B2 30025 NE RT ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 653US 24894 695424 LAX - FLT 48 - FLIGHT DEPARTED LAX WITH THE LEFT IDG ON MEL. DURING CLIMB, THE CREW NOTED THE EICAS MESSAGE 'R GEN DRIV E' AND THE 'DRIVE' LIGHT FLICKERING. FLIGHT RETURNED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH IDG'S. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 2002101600188 20021016 00188 NM 2002 10 16 USAABB02162 1 20020922 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 630AU 27808 MCO - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002101600189 20021016 00189 NM 2002 10 16 USAABB02163 1 20020922 A 3233 273N2006 ACTUATOR BOEING 757 757225 1384959 NM RT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 603AU 22198 PHL - FLT 1535 - UPON GEAR RETRACTION, CREW RECEIVED THE EICAS MESSAGES 'GEAR DISAGREE' AND 'GEAR DOORS', AND THE ASSOCI ATED AMBER LIGHTS. CREW RECYCLED THE GEAR, AND HAD THE SAME INDICATIONS. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FUR THER INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR ACTUATOR. (M) 2 L 7 2 4F RT A2NM 2002101600190 20021016 00190 NM 2002 10 16 USAABB02164 1 20020924 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 BOS - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4, 9, 23 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002101600191 20021016 00191 NM 2002 10 16 USAABB02165 1 20020924 A 3350 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 623AU 27244 BOS - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4, 9, 18 AND 26 INOPERATIVE. (M) 2 L 7 2 4F RT A2NM 2002101600192 20021016 00192 NM 2002 10 16 USAABB02167 1 20020927 A 3350 873100251REV15 SIGN BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 608AU 22204 BDL - FOUND THE L4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002101600193 20021016 00193 NM 2002 10 16 UPS02239739 1 20020918 A 5260 SKIN BOEING 727 72722C 138400F NM VENTRAL STAIRWAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI VENTRAL STAIRWAY INNER SKIN UNDER #1 TREAD HAS SURFACE CORROSION CORROSION REMOVED IAW SRM 51-1 0-06. REPAIR CARRIED OUT IAW SRM 52-1 0-2 FIG 5. PAINTED IAW SRM 51-20-91 2 L 7 3 4F A3WE 2002101600194 20021016 00194 NM 2002 10 16 UPS02239741 1 20020930 A 5310 FRAME BOEING 727 72722C 138400F NM S5 - 6R DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI DURING REPAIR OF FRAME BS 560 STR. 7R DAMAGE WAS FOUND ON EXISTING R EPAIR ABOVE AT S5R - 6R RE PAIR TO FRAME CARRIED OUT IAW SRM 53-10-4 FIG 2 2 L 7 3 4F A3WE 2002101600195 20021016 00195 NM 2002 10 16 UPS02239742 1 20020916 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1178 - 1181 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI CORROSION EVIDENT ON FUSELAGE SKIN EXTERNALLY AT BS 1178 STR. 10L & 9L, BS 1181 BETWEEN STR 9L & 8L , BS 1179 BETWEEN STR. 7L & 6L REPAIR CARRIED OUT IAW SMRO EO 2002-052-012. UPS ENGINEERING FILE N O. 727-53-20081 2 L 7 3 4F A3WE 2002101600196 20021016 00196 NM 2002 10 16 UPS02239745 1 20020919 A 5310 FRAME BOEING 727 72722C 138400F NM BS 930 R/H CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI CRACK ON LWR AFT FLANGE OF FRAME BS 930 R/H AT MLG PRESS. WEB REPAIRS TO S15 & S16 CARRIED OUT IAW SRM 53-10-3. FRAME REPAIR BS 9 20 SPLICE FABRICATED IAW SRM 51-10-3 NEW 930 FITTING INSTALLED IAW D RG 65-16336 &65 -18383 SRM 51-30-3 & SMRO EO 2002-052-021 UPS ENG. FI LE NO. 727-53-20080. FRAME BS 920 REPAIR CARRIED OUT IAW SRM 51-40 -3 2 L 7 3 4F A3WE 2002101600197 20021016 00197 NM 2002 10 16 UPS02239747 1 20020916 A 5310 SHEAR TIE BOEING 727 72722C 138400F NM S5L BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI STR. SHEAR TIE CRACKED AT S5L BS 990 SHEAR TIE REPLACED IAW SRM 51-20-1 & 51-40-3 2 L 7 3 4F A3WE 2002101600198 20021016 00198 NM 2002 10 16 UPS02239748 1 20020912 A 5310 FRAME BOEING 727 72722C 138400F NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI EVIDENCE OF CORROSION ON L/H BS 740 FRAME O/B WEB FLANGE REFER TO FI G 2 ITEM 3 (WEB SEPERATION) BS 740 FITTING REPLACED IAW SRM 51-30-2 DRG 65C13724 & EO B727-5310- 7477-E 2 L 7 3 4F A3WE 2002101600199 20021016 00199 NM 2002 10 16 UPS02239755 1 20020917 A 2760 65237995 CONTROL QUADRANT BOEING 727 72722C 138400F NM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI NO. 5 SPOILER CONTROL QUADRANT CRACKED. NEW QUADRANT FITTED IAW MM 27-61-91 2 L 7 3 4F A3WE 2002101600200 20021016 00200 NM 2002 10 16 UPS02239763 1 20020915 A 5210 SUPPORT BRACKET BOEING 727 72722C 138400F NM AFT ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C&SI CRACK ON AFT ENTRY DOOR LONGITUIDINAL SUPPORT BRACKET AT RBL 8 WL 23 8 DOOR REMOVED IAW MM 52-1 3-00. SUPPORT BRACKET REMOVED IAW SRM 51-30- 2. NEW BRACKET FABRICATED IAW SRM 51-20-1 & 52-10-1.AFT ENTRY RE-INS TALLED IAW MM 52-13-00 FUNCTION CHECKED IAW MM 52-13-00. LEAK CHECKE D IAW MM 21-30-00 - NO LEAKS 2 L 7 3 4F A3WE 2002101600201 20021016 00201 NM 2002 10 16 CALA0200497 1 20021015 A 3350 276005 FUSE BOEING 757 757224 1384958 NM BATTERY PACK BLOWN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13113 27555 THE EMERGENCY ESCAPE PATH LIGHTING ON SEATS FROM ROW 15ABC TO 25ABC WERE FOUND INOPERATIVE. MAINTENANCE FOUND THAT THE L OAD FUSE HAD RUPTURED AT BATTERY PACK M10699. THE LOAD FUSE WAS REPLACED AND EMERGENCY ESCAPE PATH LIGHTING TEST WAS GOO D IAW MM 33-51-00. 2 L 7 2 4F RT A2NM 2002101600202 20021016 00202 NM 2002 10 16 CALA0200498 1 20021016 A 3350 D71702030 CHARGER BOEING 737 737824 13844BZ NM STA 727C + 13 INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17245 28955 THE EMERGENCY INTERIOR LIGHTS AT ROW 15 T0 24 AND LEFT AFT OVER WING EXTERIOR LIGHTS DID NOT PASS THE 10 MINUTE TEST PER WORK CARD 29-3350-1-7100. THE EMERGENCY LIGHT BATTERY CHARGER AT STA 727C + 13 WAS REMOVED AND REPLACED IAW MM 33-51-06 AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2002101600203 20021016 00203 NM 2002 10 16 AWXA200201009 1 20021003 A 5313 693535214 TIE CLIP BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 0 0 25400 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/8" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 520, STR 7 R/H. MAINTENANCE REM OVED DAMAGED STRINGER TIE CLIP AT BS 520, STR 7 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PA RT IAW B737-300 SRM 51-40-02, PG. 10-11, 38, FIG. 8. 2 L 7 2 4F RT A16WE 2002101600204 20021016 00204 NM 2002 10 16 AWXA200201010 1 20021008 A 5313 693535214 TIE CLIP BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 0 0 25400 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/8" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 360, STR 9 R/H. MAINTENANCE REM OVED DAMAGED STRINGER TIE CLIP AT BS 360, STR 9 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PA RT IAW B737-300 SRM 51-40-02, PG. 10-11, 38, FIG. 8. 2 L 7 2 4F RT A16WE 2002101600205 20021016 00205 NM 2002 10 16 AWXA200201011 1 20021003 A 5313 693535214 TIE CLIP BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 0 0 25400 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/8" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 500D, STR 7 R/H. MAINTENANCE RE MOVED DAMAGED STRINGER TIE CLIP AT BS 500D, STR 7 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 10-11, 38, FIG. 8. 2 L 7 2 4F RT A16WE 2002101600206 20021016 00206 NM 2002 10 16 AWXA200201012 1 20021004 A 5411 313A1355650 CHANNEL BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 0 0 23261 MCN - MAJOR REPAIR - DURING C-17 CHECK A 2 1/2" CRACK WAS FOUND ON THE LOWER WEB OF R/H PYLON STRUT FAIRING BETWEEN NAC STA. 345 TO 363, WL 117. MAINTENANCE REMOVED 1 EACH CHANNEL AND FRAME AT R/H PYLON STRUT FAIRING BETWEEN NAC STA. 345 TO 363, WL 117; FABRICATED 1 EACH REPLACEMENT FRAME AND CHANNEL; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PG. 10- 11, PG. 45, FIG. 12, AND PG. 62, FIG. 14. 2 L 7 2 4F RT A16WE 2002101600207 20021016 00207 EA 2002 10 16 SWIA200211317 1 20020821 A 5315 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 718 CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 595SW 7292 AT LEFT AND RIGHT FS 718.00 THE FRAME IS CRACKED AT THE PYLON FITTING. FOUND DURING C CHECK INSPECTION. REPAIRED CRACK ED FRAME IAW CRJ REO 601R-53-61-193. ANGLE P/N: 600-36030-31, 2024T3-040. 2 L 7 2 4F RT A21EA 2002101600208 20021016 00208 EA 2002 10 16 SWIA200211320 1 20020821 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS 484, RBL 27.0 CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 595SW 7292 FOUND INTERCOSTAL ATTACH ANGLE AT FS 484 RBL 27.00 CRACKED. FOUND DURING C CHECK INSPECTION. NEW ANGLE FITTED AND INS TALLED IAW REO 601R-53-41-059 REV ''A''.P/N: 601R31171-9. 2 L 7 2 4F RT A21EA 2002101700001 20021017 00001 SO 2002 10 17 C2XA02SH105 1 20021017 A 5320 14524131009 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 DURING C CHECK, SUPPORT UNDER PASSENGER DOOR THRESHOLD WAS FOUND WITH CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACE D SUPPORT IAW EMB SRM 51-20-03. THE AIRCRAFT WAS APPROVED TO RETURN SERVICE. 2 L 7 2 4F RT T00011AT 2002101700002 20021017 00002 NM 2002 10 17 02091101 1 20020911 A 3350 417N5091 PIN BOEING 757 75728A 1384976 NM CONNECTOR BROKEN A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 551NA 46451 25621 CABIN EMERGENCY EGRESS LIGHTS INOP AT ROWS 22 AND 23. TROUBLESHOOTING REVEALED A BROKEN PIN IN THE FLOOR TRACK CONNECTO R. PIN WAS REPLACED, OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A2NM 2002101700003 20021017 00003 NM 2002 10 17 02FDEA00645 1 20020913 A 3233 ACTUATOR BOEING 727 727100 1384036 NM MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 124FE 19360 ON TAKEOFF, UPON GEAR RETRACTION, THE RED DOORS LT, RED RIGHT GEAR UNSAFE LT, AND RT MAIN GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. FOLLOWED QRH PROCEDURES. WITH GEAR HANDLE OFF, THE RED DOORS LT, GREEN RT GEAR SAFE LT, AND RT MAIN GEAR DOOR OPEN LT ON. PLACED GEAR DOWN, AND LANDED IN ORD WITH 3 DOWN & LOCKED INDICATION. VERIFIED PRESSURIZATION OF HYDRO LINES AT LOCK ACTUATOR AND MAIN GEAR ACTUATOR. R&R MG LOCK ACT & MG DOOR ACT PER MM 32-32-061-4, 32-32-081-4, OPS & LE AK GOOD. 2 L 7 3 4F RT A3WE 2002101700004 20021017 00004 NM 2002 10 17 02FDEA00646 1 20020912 A 2730 COMPUTER BOEING 727 727200 138407E NM ELEVATOR FAULTY A FDEA J A DUMP FUEL UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 285FE 22622 ON CLIMB OUT EXCESSIVE PITCH FORCE NEEDED TO ROTATE. ELEVATOR FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED WITH ASSOCIA TED SLOW A SYSTEM LEAK. PERFORMED HYD SYS LEAK OR LOSS CHECKLIST AND ISOLATED LEAK TO ELEVATOR SYSTEM A. DUMPED FUEL A ND RETURNED FOR LANDING WITH A SYS QTY STABILIZED AT ONE GALLON. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER PER 727 MM 27-30-101-2, OPERATIONAL AND LEAK CHECK GOOD OF FEEL COMPUTER. 2 L 7 3 4F RT A3WE 2002101700005 20021017 00005 WP 2002 10 17 ABXA020248 1 20020930 A 5300 9915501 FITTING DOUG DC9 DC931 3022065 WP LEFT WHEEL WELL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 47065 FITTING CRACKED, FORWARD OF INBOARD GEAR DOOR ACTUATOR. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002101700006 20021017 00006 WP 2002 10 17 ABXA020249 1 20020930 A 5700 99193412 FITTING DOUG DC9 DC931 3022065 WP RT. WHEEL WELL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 47065 SLAT TRACK X0S 429.1, INBOARD SUPPORT FITTING TO FRONT SPAR ATTACH ANGLE CRACKED. REPLACED AREA IAW REA D957-45321 AND D C-9 SRM. 2 L 7 2 4F A6WE 2002101700007 20021017 00007 WP 2002 10 17 ABXA020250 1 20021002 A 5300 49125401N SPLICE DOUG DC9 DC931 3022065 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 47065 INBOARD AFT FITTING, FLOOR BEAM STA. 965 LEFT, WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2002101700008 20021017 00008 CE 2002 10 17 090214 1 20020914 A 5240 DOOR LEAR 24 24 5170302 CE OXYGEN SERVICE OPEN E ESUA B EMER. DESCENT E VIBRATION/BUFFET CL CLIMB 1 CE 03 105GA 116 AFTER DEPARTURE FOR CYVR, PASSING THROUGH 13000 FEET PILOT HEARD A LOUD BANG FOLLOWED BY A NOTICEABLE VIBRATION. PILOT D ECLARED AN EMERGENCY, TO RETURN TO CYVR. MAINTENANCE WAS CALL TO INVESTIGATE THE PROBLEM. IT WAS DISCOVERED THAT THE OXY GEN SERVICE DOOR ON THE RIGHT FORWARD SIDE OF THE AIRCRAFT OPENED DURING FLIGHT. NO DAMAGE TO THE DOOR OCCURRED. THE AIR CRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4J A10CE 2002101700009 20021017 00009 CE 2002 10 17 091302 1 20020913 A 2910 2419151317 HYDRAULIC LINE LEAR 25 25D 5170514 CE HYD SYSTEM LOOSE E ESUA O OTHER K FLUID LOSS AP APPROACH 1 CE 03 81AX 6387 279 PILOT DECLARED AN EMERGENCY ON APPROACH INTO DALLAS LOVE FIELD. IT WAS DISCOVERED THAT THE HYDRAULIC PRESSURE INDICATED O. THE GEAR WAS ABLE TO BE PLACED IN THE DOWN AND LOCKED POSITION WITH NO EMERGENCY PROCEDURES. THE AIRCRAFT WAS STOP PED ON THE RUNWAY BY THE USE OF THE EMERGENCY BRAKE SYSTEM. THE AIRCRAFT WAS THEN TOWED FROM THE RUNWAY, FOR THE DETERM INATION OF THE LOSS OF HYDRAULIC FLUID. 2 L 7 2 4J A10CE 2002101700016 20021017 00016 NE 2002 10 17 2002UALA01332 2 20020821 A 7200 ENGINE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 1 BIRD INGESTION A UALA A UNSCHED LANDING C R F.O.D. PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 603UA 21864 707527 AT TAKEOFF COMPRESSOR STALL ON NR 1 ENGINE. BIRD STRIKE CONFIRMED. COMPRESSOR BORESCOPED PER MM. NO DAMAGE. ENGINE C ONTINUED IN SERVICE. 2 L 7 2 4F 4 F RT A1NM E3NE 2002101700017 20021017 00017 NM 2002 10 17 2002UALA01339 1 20020825 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 MAIN LANDING GEAR WHEEL WELL CEILING CRACKED OUTBOARD AND FORWARD OF AILERON TOWER SHAFT. CRACKS AT BOTH FORWARD CORNER S OF CEILING PANEL PILLOW AND BETWEEN FASTENERS TO CHORD FORWARD OF PILLOW. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLE R AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700018 20021017 00018 NM 2002 10 17 2002UALA01340 1 20020824 A 2450 BACC63CD28A22P CONNECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 GENERATOR BURNED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 321UA 23953 SHORTLY AFTER TAKEOFF AIRCRAFT TR 3 CIRCUIT BREAKER POPPED, AND COULD NOT BE RESET. AIRCRAFT RETURNED TO FIELD. FOUND BURNED PINS ON GEN FIREWALL CONNECTOR. REPLACED NR 2 GENERATOR HARNESS AND FIREWALL RECEPTACLE PINS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700020 20021017 00020 NM 2002 10 17 2002UALA01350 1 20020806 A 2450 PIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT BURNED A UALA K NONE I J FLT. ATTITUDE INST. WARNING INDICATION DE DESCENT 1 WP 29 662UA 27159 POWER LOST TO FIRST OFFICERS PRIMARY INSTRUMENT BUSS. FLAGS IN VIEW ON FO AIRSPEED INDICATOR, RDMI, VERTICAL SPEED INDI CATOR, EHSI AND EADI BLANK. FOUND PIN 4 OF D6430P BURNT, REPLACED PIN. THIS IS 'A' PHASE FROM FIRST OFFICER'S INSTRUME NT BUS VOLTAGE SENSE UNIT COMMON TO FIRST OFFICER'S INDICATORS. REPLACED D6430J DUE TO INSULATION DAMAGE. ALL SYSTEMS AND INDICATORS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101700021 20021017 00021 NM 2002 10 17 2002UALA01361 1 20020828 A 5270 CIRCUIT CARD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DOOR WARNING FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 656UA 25394 FORWARD CARGO DOOR EICAS AND OVERHEAD CAUTION LIGHT ILLUMINATED INTERMITTENTLY. REPLACED PROXIMITY SENSOR CARDS 2 L 7 2 4F 4 F RT A1NM E24NE 2002101700022 20021017 00022 NM 2002 10 17 2002UALA01367 1 20020828 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 RIGHT HAND CABIN FLOOR Z ANGLE CORRODED AT STATION 277-360 FORWARD GALLEY DOOR. MAJOR REPAIR ACCOMPLISHED. REPLACED Z ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700023 20021017 00023 NM 2002 10 17 2002UALA01368 1 20020828 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 STRINGER CLIP AT STRINGER 1 BODY STRINGER 380 IS GOUGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700025 20021017 00025 NM 2002 10 17 2002UALA01371 1 20020829 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 RIGHT HAND AFT CABIN STRINGER CLIP IS CRACKED AND RIVET IS WORKING AT STATION 500B. MAJOR REPAIR ACCOMPLISHED. REPLACE D STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700026 20021017 00026 NM 2002 10 17 2002UALA01372 1 20020829 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 FUSELAGE LEFT CREASE BEAM WEB UPPER SURFACE HAS CORROSION AROUND LIGHTNING HOLES STATION 964 AND 969. MAJOR REPAIR ACCO MPLISHED. REMOVED AND REPLACED DAMAGED WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101700027 20021017 00027 NM 2002 10 17 2002UALA01373 1 20020829 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 FORWARD CABIN FLOOR BEAM BODY STATION 365 BL 0 TO RBL 65 HAS EXCESSIVE CROSS SECTIONAL AREA AND DEPTH OF MATERIAL REMOVE D. MAJOR REPAIR ACCOMPLISHED. REPAIRED SPLICE TO FLOOR BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101700030 20021017 00030 NM 2002 10 17 2002UALA01376 1 20020829 A 3350 60252 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 341UA 24245 EMERGENCY FLOOR LIGHTING SYSTEM INOPERATIVE. DEFECTIVE EEL LIGHT ASSEMBLY. REPLACED EEL STRIP. OPERATIONAL CHECK GOOD . 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700031 20021017 00031 NM 2002 10 17 2002UALA01377 1 20020830 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 FUSELAGE FRAME STATION 188 IS CRACKED AT STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME WEB REPAIR ANGLE AND SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700032 20021017 00032 NM 2002 10 17 2002UALA01378 1 20020830 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 FUSELAGE FRAME STATION 188 IS CRACKED AT STRINGER 17R. INSTALLED FRAME WEB REPAIR ANGLE & SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700033 20021017 00033 NM 2002 10 17 2002UALA01379 1 20020830 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 AFT CARGO PIT FUSELAGE FRAME UPPER CAP DENTED AT STATION 727B BETWEEN STRINGER 24R AND STRINGER 25R. MAJOR REPAIR ACCOM PLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700034 20021017 00034 NM 2002 10 17 2002UALA01380 1 20020831 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 944UA 26683 FUSELAGE 188 RIGHT HAND FRAME CRACKED IN OB CHORD ANGLE IN RADIUS JUST ABOVE FLOOR LINE. MAJOR REPAIR ACCOMPLISHED. IN STALLED DOUBLER ON CHORD ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700035 20021017 00035 NM 2002 10 17 2002UALA01381 1 20020831 A 5320 CLIP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 944UA 26683 FUSELAGE NOSE COMP CREASE BEAM CLIP IS BENT AT BODY STATION 178. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700036 20021017 00036 NM 2002 10 17 2002UALA01382 1 20020831 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 CABIN STATION 987 LEFT HAND SIDE FLOOR BEAM CAP IS DAMAGED. AFTER REWORK HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACC OMPLISHED. INSTALLED FLOORBEAM UPPER CAP SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700037 20021017 00037 NM 2002 10 17 2002UALA01383 1 20020831 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 AFT CABIN MAIN ENTRYWAY SCUFF PLATE LONGITUDINAL Z ANGLE IS CORRODED FROM STA 954 TO STA 987. MAJOR REPAIR ACCOMPLISHED . REPLACED Z ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101700038 20021017 00038 NM 2002 10 17 AALA20020508 1 20020421 A 3397 WIRE HARNESS BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 627AA 24585 LAX - SEAT 1EF EMERGENCY LIGHT HARNESS DISCONNECTED. RECONNECTED HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002101700039 20021017 00039 NM 2002 10 17 AALA20020577 1 20020501 A 3350 BATTERY BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 602AN 27053 LAX - FOUND EMERGENCY SEAT MOUNTED LIGHTS RIGHT SIDE FROM ROWS 15 TO 23 ARE INOPERATIVE. REPLACED BATTERY AND CHARGED P ER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002101700040 20021017 00040 NE 2002 10 17 NACA20020044 2 20020917 A 7230 356994 CYLINDER PWA R2800CB3 DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE #3 ENGINE CRACKED A NACA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 99330 759 759 P33821 43576 P33821 DISCREPANCIES: #3 ENGINE BACKFIRE, LOW BMEP @ 0010Z.CORRECTIVE ACTION: REPLACED #3 ENGINE, #5 CYLINDER. 2 L 7 4 4R 4 R 6A3 5E8 2002101700041 20021017 00041 NM 2002 10 17 AALA20020584 1 20020501 A 3350 SIGN BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 614AA 24490 DFW - RIGHT SIDE FORWARD EMERGENCY EXIT SIGN AT ROW 16 INOPERATIVE. UNRAVELED EMERGENCY LIGHT WIRES FROM SIDEWALL AND C ONNECTED TO EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002101700042 20021017 00042 NM 2002 10 17 AALA20020793 1 20020602 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 652AA 24610 DFW - FOUND EMERGENCY EXIT SIGN AT LEFT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR LEFT OVERWING EMERGENCY EX IT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002101700043 20021017 00043 NM 2002 10 17 AALA20020799 1 20020603 A 3350 SOCKET BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 191AN 32385 SFO - FOUND EMERGENCY LIGHT AT SEAT 19D AISLE INOPERATIVE. REPAIRED LIGHT SOCKET BACK PIN. SYSTEM GROUND CHECKED NORMA L OPERATION. (M) 2 L 7 2 4F RT A2NM 2002101700044 20021017 00044 NM 2002 10 17 AALA20020802 1 20020604 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 666A 25300 BOS - FOUND ROW 15-24 SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK OVER ROW 19 IAW MM. SYSTEM GROUND CHECK ED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002101700045 20021017 00045 NM 2002 10 17 AALA20020823 1 20020605 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 614AA 24490 SNA - L1 DOOR SLIDE LIGHT INOPERATIVE ON EMERGENCY LIGHT TEST. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPE RATION. (M) 2 L 7 2 4F RT A2NM 2002101700046 20021017 00046 NM 2002 10 17 AALA20020833 1 20020530 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 614AA 24490 MIA - FOUND L1 DOOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REPLACED BATTERY PACK TO L1 DOOR. SYSTEM GROUND CHECKED NOR MAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002101700047 20021017 00047 NM 2002 10 17 AALA20020947 1 20020624 A 3350 SWITCH BOEING 757 757223 1384957 NM NLG WW FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 603AA 27054 DFW - RIGHT WING FORWARD, LEFT WING AFT, L3 DOOR AND R3 DOOR EMERGENCY LIGHTS INOPERATIVE AT EXTERNAL SWITCH. REPLACED EMERGENCY LIGHT NOSE GEAR CONTROL SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002101700048 20021017 00048 SO 2002 10 17 C2XA02CL203 1 20021016 A 3231 852701 SENSOR EMB 135 EMB135LR 3260305 SO NOSE GEAR FAULTY A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 14522 145383 CLT FLIGHT# 3187 THE CREW REPORTED DURING CLIMB AFTER SLECTING GEAR UP THEY HEARD A LOUD RUMBLEIN THE NOSE SECTION.THE A IRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS DID NOT CLOSE.T HE NOSE GEAR UPLOCK PROXIMITY SENSOR WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002101700049 20021017 00049 NM 2002 10 17 AALA20021100 1 20020727 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 BOS - FOUND FLOOR PATH EMERGENCY LIGHTING BETWEEN SEATS 4E AND 6E INOPERATIVE. REPAIR SPLICED WIRING BETWEEN SEATS 4E A DN 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002101700050 20021017 00050 NM 2002 10 17 AALA20021157 1 20020814 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 183AN 29593 LAX - EMERGENCY FLOOR PATH LIGHTS INOPERATIVE FROM SEAT 3E TO 63. REPLACED BROKEN AT SEAT 6E. SYSTEM GROUND CHECKED NO RMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002101700051 20021017 00051 NM 2002 10 17 AALA20021159 1 20020815 A 3350 BATTERY BOEING 757 757223 1384957 NM CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 698AN 26980 JFK - FOUND EMERGENCY LIGHT INOPERATIVE ON FUSELAGE AFT OF L1 DOOR. RESEATED BATTERY. SYSTEM GROUND CHECKED NORMAL OPE RATION. (M) 2 L 7 2 4F RT A2NM 2002101700052 20021017 00052 NM 2002 10 17 AALA20021161 1 20020814 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 679AN 29589 DFW - A FLOOR MOUNTED EMERGENCY LIGHT IN MID GALLEY INOPERATIVE. REPLACED LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OP ERATIONS. (M) 2 L 7 2 4F RT A2NM 2002101700053 20021017 00053 NM 2002 10 17 AALA20021174 1 20020816 A 5270 WARNING SYSTEM BOEING 767 767223 1385123 NM COCKPIT MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 325AA 22326 IAD 0 FLT 133 - EN ROUTE JFK-LAX, AFTER TAKEOFF R-1 DOOR INDICATION LIGHT ON. EMERGENCY DECLARED. LANDED IAD WITHOUT I NCIDENT. PERFORMED PRESSURIZATION CHECK, UNABLE TO DUPLICATE PROBLEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002101700054 20021017 00054 NM 2002 10 17 AALA20021222 1 20020825 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHTING ASSEMBLY AT FORWARD GALLEY L1 DOOR BROKEN. REPLACED EMERG ENCY ESCAPE LIGHTING ASSEMBLY AT FORWARD GALLEY L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002101700055 20021017 00055 NM 2002 10 17 AALA20021230 1 20020824 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 335AA 22333 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE SEAT LIGHTING AT ROW 27 INOPERATIVE. REPLACED WIRE ON ONE PIN OF T HE CONNECTOR FOR EMERGENCY ESCAPE SEAT LIGHTING AT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002101700056 20021017 00056 NM 2002 10 17 AALA20021231 1 20020827 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTING ASSEMBLY AT FIRST CLASS LEFT SIDE GALLEY WALL BROKEN. REPLACED E MERGENCY LIGHTING ASSEMBLY AT FIRST CLASS LEFT SIDE GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002101700057 20021017 00057 EU 2002 10 17 AALA20021253 1 20020827 A 5610 PPGD20543406 WINDOW FOKKER F28 F28MK0100 4990807 EU COCKPIT ARCED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 1450A 11459 DFW - FLT 1424 - FIRST OFFICERS SIDE WINDOW AREA BETWEEN WINDOW RAIL AND LATCHING MECHANISM KEPT ARCING EVEN AFTER THE W INDOW HEAT SWITCH WAS TURNED OFF. LANDED DFW WITHOUT INCIDENT. REPLACED FIRST OFFICERS SLIDING WINDOW. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002101700058 20021017 00058 WP 2002 10 17 AALA20021254 1 20020826 A 2613 SWITCH DOUG DC9 DC982 3022082 WP A/C BAY DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 585AA 53248 EWR - FLT 353 - EN ROUTE LGA-ORD, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT AND MASTER WARNING LIGHT ILLUMINATED ON CLIMB- OUT FROM LGA. ACCOMPLISHED RED BOX ITEMS, WAITED TWO MINUTES, LIGHT DID NOT GO OUT. DECLARED EMERGENCY AND LANDED AT E WR. LIGHT WENT OUT AS POWER WAS REDUCED DURING DESCENT. LANDED EWR WITHOUT INCIDENT. REPLACED BOTH TAIL COMPARTMENT T EMPERATURE OVERHEAT SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002101700059 20021017 00059 NM 2002 10 17 AALA20021257 1 20020901 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHTING AT SEAT 23B BROKEN. REPLACED EMERGENCY ESCAPE LIGHTING AS SEMBLY AT SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002101700060 20021017 00060 NM 2002 10 17 AALA20021260 1 20020903 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 315AA 22317 LAX - DURING OVERNIGHT MAINTENANCE, RIGHT MID GALLEY FLOOR EMERGENCY ESCAPE LIGHTING INOPERATIVE. REPLACED RIGHT MID GA LLEY FLOOR EMERGENCY ESCAPE LIGHTING ASSEMBLY. (M) 2 L 7 2 4F RT A1NM 2002101700061 20021017 00061 NM 2002 10 17 AALA20021261 1 20020905 A 3350 SIGN BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 MIA - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY ESCAPE EXIT SIGN HOUSING AT 4L DOOR BROKEN. REPLACED EMERGENCY E SCAPE LIGHTING ASSEMBLY OVER CEILING AT 4L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002101700062 20021017 00062 NM 2002 10 17 AALA20021264 1 20020902 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 377AN 25446 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHTS AT ROW 2H THROUGH 8H INOPERATIVE. REPLACED EMERGENCY ESCAPE LIGHTING ASSEMBLY AT ROW 2H THROUGH 8H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002101700063 20021017 00063 NM 2002 10 17 AALA20021292 1 20020910 A 3350 SIGN BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT INDICATOR LIGHT AT DOOR 1R AFT BROKEN. REPLACED LIGHT ASSEMBLY AT 1R AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 2 4F RT T00001SE 2002101700064 20021017 00064 WP 2002 10 17 ASAA0280294 1 20020906 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SAN - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED LIG HT MODULE AT ROW 3. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002101700065 20021017 00065 WP 2002 10 17 ASAA0280295 1 20020907 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FIRST CLASS CABIN. RECONNECT ED LOOSE MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002101700066 20021017 00066 WP 2002 10 17 ASAA0280296 1 20020907 A 3350 POWER SUPPLY DOUG DC9 DC982 3022082 WP A/C BAY DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE IN TAIL AREA AFT OF BULKHEAD. REPLACED ASSOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2002101700067 20021017 00067 SO 2002 10 17 C2XA02CL204 1 20021016 A 3600 14542872401 LINE EMB 145 EMB145LR 3260212 SO BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 27 19554 145587 CLE FLIGHT#3296 THE CREW REPORTED AFTER TAKEOFF THEY RECEIVED A #1 BLEED LEAK MESSAGE ON THE EICAS AND THE OVERHEAD PANE L.THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #1 ENGINE DIRR ERENTIAL PRESSURE SENSOR LINE.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002101700068 20021017 00068 EU 2002 10 17 02160317 1 20021016 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE O OTHER TX TAXI/GRND HDL 1 EA 27 317UE 41031 DURING TAXI OF THE FLIGHT FROM CHS TO IAD, THE CREW REPORTED EMERGENCY LIGHTS CAME WHEN ARMED. RECYCLE AND LIGHTS WENT OUT. MAINTENANCE PERSONNEL TIGHTENED LOOSE CONNECTION ON LT PDU. OPS CK'D GOOD. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T RT A41NM 2002101700069 20021017 00069 NM 2002 10 17 GAIA02120ST 1 20020919 A 5311 FRAME BOEING 727 727251 138408H NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THE THE FUSELAGE FRAME AT BS 400, STRINGER S6R WAS DENTED. ACCOMPLISHED REPA IR IAW BOEING 727 SRM 53-10-4, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101700070 20021017 00070 NM 2002 10 17 GAIA02121ST 1 20020919 A 5752 652172642 SKIN BOEING 727 727251 138408H NM AILERON TAB DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE RIGHT WING OUTBOARD AILERON TAB HAS A SHARP DENT. REMOVED AND REPLA CED THE RIGHT OUTBOARD AILERON TAB IAW BOEING MM 27-10-41. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101700071 20021017 00071 NM 2002 10 17 GAIA02122ST 1 20020919 A 5311 FRAME BOEING 727 727251 138408H NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 540, STRINGER S9R WAS DENTED. ACCOMPLISHED REPAIR IAW B OEING 727 SRM 53-10-4, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101700072 20021017 00072 NM 2002 10 17 GAIA02123ST 1 20020919 A 5311 FRAME BOEING 727 727251 138408H NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT A PREVIOUS REPAIR TO A FRAME AT BS 540, STRINGER S17R HAD BEEN DENTED. ACCOMPLISHED REPAIR TO FRAME IAW 727 SRM 53-10-4, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101700073 20021017 00073 NM 2002 10 17 GAIA02124ST 1 20020919 A 5311 FRAME BOEING 727 727251 138408H NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING LTC INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 560, STRINGER S7R IS DENTED. ACCOMPLISHED REPAIR IAW BOEI NG 727 SRM 53-10-4, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101700074 20021017 00074 NM 2002 10 17 GAIA02125ST 1 20020919 A 5311 FRAME BOEING 727 727251 138408H NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE PREVIOUS REPAIR AT FRAME BS 600, STRINGER S17R. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-4, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101700075 20021017 00075 NM 2002 10 17 GAIA02126ST 1 20020919 A 5313 STRINGER BOEING 727 727251 138408H NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT STRINGER S15R WAS CRACKED AT BS 730. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-3, FIGURE 5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101700076 20021017 00076 NM 2002 10 17 GAIA02127ST 1 20020919 A 5313 STRINGER BOEING 727 727251 138408H NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT STRINGER S15L WAS CRACKED AT BS 730. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-3, FIGURE 5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101700077 20021017 00077 NM 2002 10 17 GAIA02128ST 1 20020919 A 5347 BAC1520792 SEAT TRACK BOEING 727 727251 138408H NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE SEAT TRACK AT BS 520, RBL 25 WAS CORRODED OUT OF LIMITS. ACCOMPLISH ED REPAIR IAW BOEING 727 SRM 51-30-5, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002101700078 20021017 00078 WP 2002 10 17 ASAA0280297 1 20020908 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 OAK - DURING PREFLIGHT CHECK, VARIOUS EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED LOOSE MODU LE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002101700079 20021017 00079 NM 2002 10 17 CALA0200500 1 20021016 A 5320 BEAM BOEING 777 777224 1385225 NM STA 1790 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57016 28679 INSPECTION FOUND A 6" CRACK IN AFT CARGO BEAM IN DOOR AREA AFT SIDE LOWER PART OF BEAM, STA 1790. A NEW STANCHION BEAM W AS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT T00001SE 2002101700080 20021017 00080 NM 2002 10 17 AWXA200201013 1 20021003 A 5320 6545833U468 ATTACH ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 0 0 25400 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/16" CRACK WAS FOUND ON ATTACH ANGLE AT BS 178, WL 207, RBL 29. MAINTENANCE RE MOVED CRACKED ATTACH ANGLE AT BS 178, WL 207, RBL 29; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART I AW B737-300 SRM 51-40-02, PG.38, FIG.8, PG. 10-11. 2 L 7 2 4F RT A16WE 2002101700081 20021017 00081 SO 2002 10 17 C2XA02SH107 1 20021017 A 5300 14522460013 BUTT STRAP EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 SHV-DURING C CHECK THE CENTER FLOOR BEAM STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 23. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002101800001 20021018 00001 SO 2002 10 18 C2XA02SH109 1 20021018 A 5300 14522226003 BUTT STRAP EMB 145 EMB145ER 3260211 SO LAVARATORY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 SHV-DURING C CHECK LAVARATORY'S FLOOR BEAMS WERE FOUND WITH CORROSION BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED DAMA GE AND REPLACED AFFECTED BUTT STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002101800002 20021018 00002 WP 2002 10 18 ASAA0280298 1 20020909 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 7. RECONNECTED LOOSE MODULE CONNECT OR. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002101800003 20021018 00003 WP 2002 10 18 ASAA0280299 1 20020909 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SJC - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FORWARD CABIN. RECONNECTED L OOSE MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002101800004 20021018 00004 2002 10 18 ASAA0280300 4 20020911 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DETACHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 PDX - DURING PREFLIGHT CHECK, THE FORWARD DOOR EMERGENCY SLIDE 'ACTIVATION CABLE' LANYARD WAS FOUND TO BE LOOSE. REATTA CHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2002101800005 20021018 00005 WP 2002 10 18 ASAA0280301 1 20020912 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 OAK - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY, INC LUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2002101800006 20021018 00006 WP 2002 10 18 ASAA0280303 1 20020912 A 3350 MISC060C LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 SEA - DURING PREFLIGHT CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERIES. LI GHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002101800007 20021018 00007 WP 2002 10 18 ASAA0280307 1 20020913 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SJC - DURING PREFLIGHT CHECK, FIRST COUPLE OF FEET OF EMERGENCY FLOOR TRACK LIGHTS IN FIRST CLASS CABIN WERE FOUND TO BE INOPERATIVE. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002101800008 20021018 00008 NM 2002 10 18 02FDEA00649 1 20020914 A 2613 OVERHEAT LOOP BOEING 727 727200 138407E NM RT MLG WW OUT OF POSITION A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 288FE 21850 FL 280 LOWER AFT BODY OVERHEAT LIGHT CAME ON. BLEED 3 OPEN, RIGHT PACK OPEN. CARGO HEAT OUTFLOW NORMAL. FOLLOWED QRH PROCEDURE. DESCENDED TO FL 250, RIGHT NR 2 BLEED OPEN, RIGHT PACK ON. CARGO HEAT OUTFLOW NORMAL. INCREASED THRUST ON NR 3 ENGINE TO 85.5 N1. LIGHT STAYED OUT. REMOVED KEEL BEAM ACCESS PANEL IN RT WHEEL WELL. FOUND AFT BODY O/H DETECTO R LOOP IN KEEL BEAM AREA ALMOST TOUCHING PNEUMATIC SUPPLY DUCT. REROUTED LOOP AS REQUIRED. NO OTHER FAULTS FOUND. CLOS ED ACCESS PANELS & RESTORED A/C TO NORMAL. PERFORMED TEST IAW MAINTENANCE MANUAL 26-14-00-5, NO FAULTS. 2 L 7 3 4F RT A3WE 2002101800009 20021018 00009 WP 2002 10 18 02FDEA00652 1 20020913 A 5743 ARBQ4621 SUPPORT DOUG DC10 DC1030 3023501 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 302FE 46801 FOUND CRACK INDICATION ON MLG RETRACT CYLINDER SUPPORT FRAME AFT HANGER SUPPORT. R&R SUPPORT FRAME ON LT MLG PER EO 8-5 740-7-4312 P3 SEQ NR 00009. 2 L 7 3 4F A22WE 2002101800010 20021018 00010 NM 2002 10 18 2002UALA01384 1 20020831 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 CABIN STATION 616R, FRAME CHORD CRACKED AT LOWER FASTENER, STUB FRAME. MAJOR REPAIR ACCOMPLISHED. STUB FRAME REPAIR AN GLE INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800011 20021018 00011 NM 2002 10 18 2002UALA01385 1 20020901 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE BUCKLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 BODY STATION 277 FRAME IS BUCKLED CREASED ABOVE STRINGER 19R, JUST OUTBOARD OF FAILSAFE CHORD ANGLE. MAJOR REPAIR ACCOM PLISHED. INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800012 20021018 00012 NM 2002 10 18 2002UALA01386 1 20020901 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 FORWARD ENTRY DOOR FLOOR CREASE BEAM Z ANGLE HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPLACED Z ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800013 20021018 00013 NM 2002 10 18 2002UALA01387 1 20020901 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 CABIN STATION 727A, STRINGER 16R, STRINGER CLIP CRACK FASTENER. MAJOR REPAIR ACCOMPLISHED. STRINGER CLIP REPLACEMENT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800014 20021018 00014 NM 2002 10 18 2002UALA01388 1 20020902 A 3350 362624 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 955UA 26703 EMERGENCY FLOOR LIGHTING SYSTEM INOPERATIVE FROM ROWS 13 TO 19. REPAIRED EEL STRIPS. FOUND AFT SECTION OPERATES NORMAL LY WITH THE EXCEPTION OF 1 EACH STRIP AT ROW 5 AND ROW 14 INOP. REPLACED MISSING EEL LAMPS AT ROWS 5 AND 14. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800015 20021018 00015 NM 2002 10 18 2002UALA01390 1 20020831 A 5320 SILL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 CABIN RIGHT HAND AFT OVER WING EXIT CUTOUT LOWER SILL OUTER T-CHORD CRACKED ON FORWARD END BODY STATION 997 STRINGER 15R . MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLES INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101800016 20021018 00016 NM 2002 10 18 2002UALA01391 1 20020830 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 CABIN FLOOR BEAM BODY STATION 297 RBL 42 HAS MATERIAL LOSS DUE TO CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. ANGLE REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101800017 20021018 00017 NM 2002 10 18 2002UALA01392 1 20020830 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 FORWARD CABIN FLOOR BEAM T-CAP BODY STATION 324 FROM RBL 40 TO RBL 46 HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPL ISHED.INSTALLED FLOOR BEAM T-CAP DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101800018 20021018 00018 NM 2002 10 18 2002UALA01394 1 20020830 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 AFT PIT STATION 1468 STRINGER 29L UPPER INBOARD FLANGE HAS EXCESSIVE MATERIAL LOSS AFTER CORROSION REMOVAL. MAJOR REPAI R ACCOMPLISHED. CUT OUT DAMAGE AND EXTENDED PRODUCTION STRINGER SPLICE AS REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101800019 20021018 00019 NM 2002 10 18 2002UALA01397 1 20020901 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 FLOORBEAM FLANGE CORRODED STA 1640 RBL 53, WL 208. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101800020 20021018 00020 NM 2002 10 18 2002UALA01402 1 20020904 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 944UA 26683 LEFT HAND STATION 188 FUSELAGE FRAME OUTBOARD CHORD ANGLE CRACKED IN RADIUS JUST ABOVE WL 207.5. MAJOR REPAIR ACCOMPLIS HED. MANUFACTURED & INSTALLED ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800021 20021018 00021 2002 10 18 2002UALA01403 4 20020826 A 3442 6225125001 DRIVE UNIT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WEATHER RADAR FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 642UA 25092 WEATHER RADAR FAILED. THE ANTENNA DRIVE UNIT AND FLAT PLATE WERE REPLACED AND SYSTEM OPERATION RESTORED. SHOP TEST OF THE FLAT PLATE FOUND THE UNIT WITHIN SPECS. THE ANTENNA DRIVE UNIT FAILED SHOP TEST. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800022 20021018 00022 NM 2002 10 18 2002UALA01405 1 20020802 A 5270 CIRCUIT CARD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WARNING SYSTEM FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 656UA 25394 FORWARD CARGO DOOR EICAS MESSAGE AND OVERHEAD CAUTION LIGHT ILLUMINATED INTERMITTENTLY. REPLACED PROXIMITY SENSOR CARDS 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800023 20021018 00023 NM 2002 10 18 2002UALA01407 1 20020905 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 CABIN STATION 887 AT STRINGER 9L FRAME WEB CRACKED AT AIR GRILL ATTACH POINT. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRA ME DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800024 20021018 00024 NM 2002 10 18 2002UALA01408 1 20020905 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 CABIN BODY FRAME WEB IS CRACKED BODY STATION 847 STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. SPLICED BODY FRAME WEB . 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800025 20021018 00025 NM 2002 10 18 2002UALA01409 1 20020905 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 STATION 178 BULKHEAD WEB CRACKED AT WL 187 RBL 1 INCH. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800026 20021018 00026 NM 2002 10 18 2002UALA01410 1 20020905 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 STATION 178 BULKHEAD CRACKED VERTICAL CHORD ANGLE LBL 5.7 INCHES WL 184. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBL ER ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800027 20021018 00027 NM 2002 10 18 2002UALA01411 1 20020905 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 STATION 178 BULKHEAD WEB CRACKED AT RIGHT HAND LOWER RADAR MOUNT OUTBOARD UPPER SIDE RBL 7 INCHES WL 200. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800029 20021018 00029 WP 2002 10 18 ARWA20021006 1 20021016 A 3240 305323001 VALVE DOUG DC8 DC863 302198A WP MLG FROZEN A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 345JW 46042 ON PUSH BACK (SAP), BRAKES DID NOT RELEASE. UNABLE TO MOVE AIRCRAFT UNDER NORMAL POWER. RETURNED TO BLOCK. AFTER TROU BLESHOOTING AND SYSTEM TEST FOUND BAD DUAL PWR.BRAKE VALVE. REPLACED VALVE. REPLACED AS PRECAUTIONARY MEANS BOTH THE LT MLG SHUTTLE VALVE, AND LT BRAKE CONTROL VALVE. PREFORMED SYSTEM FUNCTIONAL TEST, ANTI SKID FUNCTIONAL TEST, AIRCRAFT T AXIED WITH NO FURTHER INCIDENTS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002101800031 20021018 00031 NM 2002 10 18 2002UALA01415 1 20020907 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 AFT PIT LEFT HAND SIDE STATION 1480 STRINGER 26 FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL REPAIR DOU BLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101800032 20021018 00032 NM 2002 10 18 2002UALA01417 1 20020908 A 5320 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 CABIN BODY STATION 1680 AT APPROXIMATELY LBL 52 UPPER DECK PLATE HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED . INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101800037 20021018 00037 SO 2002 10 18 2002F00934 2 20021001 A 8530 FLANGE PIPER PA34 PA34220T 7103420 SO CONT O360 LTSIO360RB SO MANIFOLD TUBE FAILED W R82Y K NONE O OTHER IN INSP/MAINT 1 EA 25 95D 3449060 321697 THE ATTACHMENT FLANGE OF THE INDUCTION MANIFOLD (NR2 CYLINDER) FAILED CAUSING ROUGH RUNNING OF THE ENGINE. 1 L 7 2 3O 3 O A7SO E9CE 2002101800039 20021018 00039 NM 2002 10 18 2002UALA01419 1 20020908 A 3397 WIRE HARNESS BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 606UA 21867 ONE EEL LIGHT INOP ON RIGHT SIDE OF SEAT 1F. ALSO, DOOR 1R LOWER EXIT LIGHT INOP. MAJOR REPAIR ACCOMPLISHED. REPLACED POWER LEAD CABLE, END CAPS, AND COVER. 2 L 7 2 4F 4 F RT A1NM E3NE 2002101800042 20021018 00042 NM 2002 10 18 2002UALA01422 1 20020907 A 5270 SENSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OVERWING DOOR OUT OF TOLERANCE A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 656UA 25394 LEFT HAND OVER WING SLIDE DOOR LIGHT FLICKERING IN CONJUNCTION WITH EICAS MESSAGE. ACCOMPLISHED PROXIMITY SENSOR CHECK ON LT OVERWING SLIDE DOOR IAW MM 52-71-00/501. FOUND SENSORS OUT OF TOLERANCE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800046 20021018 00046 NM 2002 10 18 ANCF200200021 1 20021010 A 2150 20495054 ACM DOUG MD80 MD83 3023681 NM AIR CONDITIONING DAMAGED W ANCF A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 23 190AN 8571 192 53190 FIVE MINUTES AFTER TAKE OFF IT WAS FELT SMOKE SMELL FROM AIR CONDITIONING TUBES. AIRCRAFT RETURNED BACK TO BOGOTA. FLIG HT PERFORMED ON EI-CCC. AIRCRAFT WAS LEFT ON GROUND FOR WORKING ON IT AT NIGHT. THE RIGHT PACK AIR CYCLE MACHINE WAS F OUND BINDING. THE AIRCYCLE MACHINE WAS REPLACED IAW AMM. ALSO WERE REPLACED WET SEPARATORS IAW AMM. TEST SATISFACTORY I AW AMM. 2 L 7 2 4F RT 2002101800047 20021018 00047 2002 10 18 ANCF200200022 4 20021014 A 3414 HOSE DOUG MD80 MD83 3023681 NM CADC LOOSE W ANCF C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 23 632CT 49632 RT AIRSPEED INDICATOR INOPERATIVE. IT WAS FOUND LOOSEN HOSE IN CADC. IT WAS ADJUSTED PROPERLY AND PERFORMED TEST IAW AMM. 2 L 7 2 4F RT 2002101800048 20021018 00048 EU 2002 10 18 AUS20020967 1 20020830 A 2913 42011 PUMP FOKKER F27 F27MK50 EU PWA PWA120 PW125B NE HYDRAULIC SYS MALFUNCTIONED W D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 AU S 1583 (AUS) RT HYDRAULIC PUMP UNABLE TO MAINTAIN PRESSURE. A REPLACEMENT PUMP HAD THE SAME PROBLEM. A THIRD PUMP WAS FITTED WH ICH RECTIFIED THE DEFECT. 2 H 7 2 4T 4 T RT A817 E20NE 2002101800049 20021018 00049 CE 2002 10 18 AP48200222808 1 20020815 A 7160 63526002 INLET CESSNA 525 525A 2076615 CE WILINT FJ44 FJ44 66000 GL LT ENGINE CRACKED B T0DR K NONE O OTHER IN INSP/MAINT 1 CE 03 172CJ 668 525A0017 LEFT ENGINE INLET BARREL CRACKED AT 12 O'CLOCK POSITION FROM INLET RING RIVETS TO BARREL EDGE. 1 L 7 1 4F 4 F RT A1WI E3GL 2002101800050 20021018 00050 NM 2002 10 18 AUS20020969 1 20020827 A 3233 65B1300213 FITTING BOEING 747 747400 NM GE CF6 CF680C2* GL MLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) MAIN LANDING GEAR BODY GEAR DOOR ACTUATOR ROD FITTING FORWARD LUG BROKEN OFF. 2 L 7 4 4F 4 F RT A20WE E23EA 2002101800052 20021018 00052 EU 2002 10 18 AUS20020973 1 20020828 A 5730 HZ010H4073202 SEAL BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE ACCESS PANEL LEAKING W O OTHER K FLUID LOSS NR NOT REPORTED 1 AU S (AUS) RT WING ACCESS PANEL LOCATED INBOARD OF THE NR 3 NACELLE LEAKING FUEL DUE TO A FAULTY SEALING RING. 2 H 7 4 4F 4 F A49EU E6NE 2002101800053 20021018 00053 NM 2002 10 18 C1HA200286007 1 20020902 A 3350 CONTACTOR BOEING 727 7272S7 138407Z NM BATTERY PACK DIRTY A C1HA K NONE L NO TEST UK UNKNOWN 1 GL 15 686CA 22021 AFT AIRSTAIR EMERGENCY AREA LIGHT IS INOP. CLEANED CONTACTS ON BATTERY PACK. 2 L 7 3 4F A3WE 2002101800054 20021018 00054 SO 2002 10 18 LR7A02076 1 20020831 A 2150 20343041 ACM LKHEED 382 382G 526414U SO AIR CONDITIONING MALFUNCTIONED A LR7A K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 401LC 531 4606 FLIGHT CREW REPORTED OILY SMELL FROM FLIGHT DECK AIR CONDITIONING SYSTEM. REPLACED FLIGHT DECK AIR CONDITIONING COOLING TURBINE IAW SMP 581 21-50-00. OPS CHECK GOOD. 2 H 7 4 4T A1SO 2002101800055 20021018 00055 SO 2002 10 18 LR7A02077 1 20020904 A 2170 18084942 COALESCER BAG LKHEED 382 382G 526414U SO AIR CONDITIONING DIRTY A LR7A K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 401LC 88 4606 FLIGHT CREW REPORTED SMELL FROM FLIGHT DECK AIR CONDITIONING SYSTEM. REPLACED FLIGHT DECK AIR CONDITIONING WATER SEPARA TOR CONDENSER SOCK IAW SMP 581 21-50-00 PG 201 & 222. OPS CHECK GOOD. 2 H 7 4 4T A1SO 2002101800056 20021018 00056 NM 2002 10 18 OZIA200243007 1 20020831 A 2730 840932 ACTUATOR DORNER DO32 DO328300 NM ELEVATOR CONTAMINATED A OZIA K NONE J WARNING INDICATION DE DESCENT 1 CE 05 430Z 1852 3127 ELEVATOR MISTRIM CAS MESSAGE. ELEVATOR TRIM MOTOR FAIL MESSAGE ON SYC MAINT PAGE. NORMAL OR STANDBY PITCH TRIM WOULD N OT WORK ON DESCENT. RETURNED BELOW FREEZING LEVEL. 2 H 7 2 4T RT A55NM 2002101800057 20021018 00057 NE 2002 10 18 AUS20020979 2 20020903 A 7261 ENGINE BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE NR 2 LACK OF LUBE W O OTHER E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION CR CRUISE 1 AU S (AUS) NR 2 ENGINE HAD NO OIL QUANTITY. 2 H 7 4 4F 4 F RT A49EU E6NE 2002101800058 20021018 00058 EU 2002 10 18 AUS20020980 1 20020809 A 3233 C494004X8 SCREW AMD FALC20 FALCON200 2730150 EU GARRTT ATF3 ATF36A4 29002 WP MLG ACTUATOR MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) LT MAIN LANDING GEAR ACTUATOR HAD EXCESSIVE INTERNAL END PLAY. INVESTIGATION FOUND THAT THE THREADED RING HAD WORK ED LOOSE. THE REASON FOR THE RING WORKING LOOSE WAS THE SET SCREW WAS NOT CORRECTLY LOCKED IN PLACE DUE TO BECOMING THR EAD-BOUND BEFORE LOCKING THE RING. 2 L 7 2 4F 4 F RT A7EU E7WE 2002101800059 20021018 00059 WP 2002 10 18 UPS02839325 1 20020822 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 LT WING L/E LOWER SKIN IS CRACKED AT XFS 347.75. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATED A T STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-4087 APPROX C. 2 L 7 4 4F RT 4A25 2002101800060 20021018 00060 NM 2002 10 18 AUS20020981 1 20020818 A 2822 609891004 PUMP BOEING 737 737800* NM GE CFM56 CFM567B24 NE FUEL BOOST FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S 020204721 (AUS) RT CENTER FUEL TANK BOOST PUMP FAULTY. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002101800061 20021018 00061 EU 2002 10 18 AUS20020982 1 20020829 A 2932 9738114306 PRESSURE SWITCH PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL HYD SYSTEM FAILED W O OTHER O OTHER LD LANDING 1 AU S (AUS) HYDRAULIC PRESSURE SWITCH FAILED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002101800062 20021018 00062 WP 2002 10 18 UPS02839326 1 20020826 A 5320 4758514505 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1240 AFT INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT LONG 33R. REMOVED AND REPLACED FITTIN G IAW DWG 4758514, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002101800063 20021018 00063 SO 2002 10 18 AUS20020986 1 20020905 A 3230 9515339 LINE PIPER PA34 PA34220T 7103420 SO CONT O360 TSIO360RB 17025 CE MLG HYD SYSTEM CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NOSE LANDING GEAR, DOWN HYDRAULIC LINE CORRODED. SUSPECT CAUSED BY LACK OF CORROSION PREVENTION DURING MANUFACT URE. 1 L 7 2 3O 3 O A7SO E9CE 2002101800064 20021018 00064 SO 2002 10 18 AUS20020987 1 20020905 A 3230 9515340 LINE PIPER PA34 PA34220T 7103420 SO CONT O360 TSIO360RB 17025 CE MLG HYD SYSTEM CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NOSE LANDING GEAR UP HYDRAULIC LINE CORRODED. SUSPECT CAUSED BY LACK OF CORROSION PREVENTION DURING MANUFACTURE. 1 L 7 2 3O 3 O A7SO E9CE 2002101800065 20021018 00065 NM 2002 10 18 AUS20020988 1 20020815 A 2450 BACC184D5 CIRCUIT BREAKER BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE AC POWER DISTRIB FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 AU S (AUS) COCKPIT CIRCUIT BREAKER FAILED. CB WAS FOR ATC R ON P7. 2 L 7 4 4F 4 F RT A20WE E30NE 2002101800066 20021018 00066 GL 2002 10 18 AUS20020989 3 20020904 A 6114 660709608 HUB SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL PROPELLER CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S 1458 (AUS) PROPELLER HUB CRACKED IN AREA ADJACENT TO THE BOTTOM OF THE MOUNTING BOLT INSERT. CRACK DEPTH APPROXIMATELY 13MM ( 0.51IN) TO 15MM (0.59IN). FOUND USING ULTRASONIC INSPECTION. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002101800067 20021018 00067 SO 2002 10 18 AUS20020990 1 20020830 A 2434 A111084 COMMUTATOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL DC ALTERNATOR UNAPPROVED PART W O OTHER H W ELECT. POWER LOSS-50 PC INADEQUATE Q C CR CRUISE 1 AU S (AUS) ALTERNATOR FAULTY. INVESTIGATION FOUND INCORRECT COMMUTATOR FITTED. UNAPPROVED PART. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2002101800068 20021018 00068 CE 2002 10 18 AUS20020992 1 20020904 A 2434 C061452 BEARING CESSNA 210 210L 2073448 CE CONT O520 IO520L 17032 SO MCAULY 2A34C E2A34C73 GL DC ALTERNATOR FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ALTERNATOR BEARING FAILED. SUSPECT UNAPPROVED PART. 1 H 7 1 3O 3 O 3A21 E5CE 5 C P3EA9 2002101800069 20021018 00069 NE 2002 10 18 AUS20020994 2 20020905 A 7200 12728 ENGINE BOEING 747 747338 NM RROYCE RB211 RB211524D419 54555 NE NR 1 FAILED W C ABORTED TAKEOFF E F VIBRATION/BUFFET FLT CONT AFFECTED TO TAKEOFF 1 AU S (AUS) NR 1 ENGINE FAILED. EXCESSIVE VIBRATION INDICATIONS. INSPECTION FOUND METAL IN TAILPIPE. 2 L 7 2 4F 4 F RT A20WE E12EU 2002101800070 20021018 00070 EU 2002 10 18 AUS20020999 1 20020803 A 5230 FGFB29900141OA2 BELLCRANK AMD FALC50 FALCON900 2700160 EU CARGO DOOR FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S BZ67 (AUS) BAGGAGE COMPARTMENT DOOR BELLCRANK BROKEN. LOWER FUSELAGE PANEL TORN BY BROKEN BELLCRANK. 2 L 7 3 4F RT A46EU 2002101800071 20021018 00071 EU 2002 10 18 AUS20021000 1 20020811 A 2530 50413100 COFFEEMAKER AMD FALC50 FALCON900 2700160 EU GALLEY FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S 234 (AUS) COFFEEMAKER FAILED. SMOKE AND FUMES EMANATING FROM COFFEE MAKER. 2 L 7 3 4F RT A46EU 2002101800072 20021018 00072 NE 2002 10 18 AUS20021003 2 20020907 A 7261 PLATE BOEING 747 747238B 1384828 NM RROYCE RB211 RB211524D419 54555 NE NR 2 ENGINE LEAKING W O OTHER E K VIBRATION/BUFFET FLUID LOSS CR CRUISE 1 AU S (AUS) NR 2 ENGINE HYDRAULIC PUMP BLANKING PLATE LEAKING ENGINE OIL. THE HYDRAULIC PUMP HAD BEEN REMOVED FROM THE ENGINE AND THE BLANKING PLATE FITTED. 2 L 7 4 4F 4 F A20WE E12EU 2002101800073 20021018 00073 NM 2002 10 18 AUS20021004 1 20020906 A 2913 6506605 PUMP BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL HYD SYSTEM FAILED W O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AU S (AUS) LT ENGINE DRIVEN HYDRAULIC PUMP FAULTY. 2 L 7 2 4F 4 F RT A1NM E23EA 2002101800074 20021018 00074 2002 10 18 AUS20021006 4 20020830 A 3414 WL106AMA20 INDICATOR BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE AIRSPEED WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S 20954 (AUS) CAPTAIN'S MACH/ASI INDICATOR WAS INCORRECT PART. 2 H 7 4 4F 4 F RT A49EU E6NE 2002101800075 20021018 00075 WP 2002 10 18 UPS02839327 1 20020819 A 5330 577992541 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 EXTERIOR SKIN BULGING STA 190 BETWEEN LONG 35L TO 35R, INTERNAL DOUBLER IS CORRODED BEYOND LIMITS REM OVED, FABRICATED AND REPLACED INTERNAL DOUBLER IAW DWG 5779925 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2002101800076 20021018 00076 WP 2002 10 18 UPS02839328 1 20020823 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1660 LONG 24L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON IAW SRM 53-4- 1 FIG 43, AND 53-2-2 FIG 8. 2 L 7 4 4F RT 4A25 2002101800077 20021018 00077 EU 2002 10 18 AUS20021007 1 20020819 A 5510 5510111 STRUCTURE GIPPLD GA8 GA8 EU LYC O540 IO540K1A5 41532 EA HARTZL HCC2Y HCC2YR1 GL HORIZONTAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) HORIZONTAL STABILIZER CRACKED. 1 H 7 1 3O 3 O NT 1E4 5 C P920 2002101800078 20021018 00078 SW 2002 10 18 AUS20021010 1 20020903 A 6220 412010147105 BEARING BELL 412 412 1182202 SW MAIN ROTOR HEAD DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) MAIN ROTOR HEAD SPINDLE ASSEMBLY ELASTOMETRIC BEARING DELAMINATED. 1 G 7 2 4U H4SW 2002101800079 20021018 00079 NM 2002 10 18 AUS20021011 1 20020906 A 2520 COVER BOEING 747 747400 NM RROYCE RB211 RB211524* NE PASSENGER SEAT MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) PASSENGER SEAT FIRE BLOCKING COVER MISSING. A CHECK OF ALL SEATS FOUND A TOTAL ELEVEN COVERS MISSING. COVERS REQUI RED FORCOMPLIANCE WITH AD/GEN/63. 2 L 7 4 4F 4 F RT A20WE E12EU 2002101800083 20021018 00083 NE 2002 10 18 BA2002139 2 20020906 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT POWER LOSS A GLBA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 03 260GL UE260 LT ENG WOULD NOT MAKE TORQUE ON TAKE OFF, PENDING CORRECTIVE ACTION. 2 L 7 2 4T 4 T RT A24CE E26NE 2002101800084 20021018 00084 GL 2002 10 18 AUS20021021 2 20020910 A 7321 PLUG BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL FUEL CONTROL WRONG PART W C ABORTED TAKEOFF E R W VIBRATION/BUFFET PARTIAL RPM/PWR LOSS INADEQUATE Q C TO TAKEOFF 1 AU S (AUS) RT ENGINE RATING PLUG ON THE ENGINE EEC WAS INCORRECT PART NUMBER. PERSONNEL/MAINTENANCE ERROR. 2 L 7 2 4F 4 F RT A1NM E23EA 2002101800085 20021018 00085 NE 2002 10 18 GLBA2002139 2 20020906 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT POWER LOSS A GLBA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 03 260GL UE260 LT ENG WOULD NOT MAKE TORQUE ON TAKE OFF, PENDING CORRECTIVE ACTION. 2 L 7 2 4T 4 T RT A24CE E26NE 2002101800086 20021018 00086 2002 10 18 AUS20021022 4 20020906 A 6122 89741016 GOVERNOR SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UHR WP MCAULY 4HFR34 4HFR34C652 NE PROPELLER FAULTY W C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 AU S 610 (AUS) RT ENGINE PROPELLER GOVERNOR SUSPECT FAULTY. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002101800087 20021018 00087 CE 2002 10 18 GLBA2002141 1 20020909 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE BIRD STRIKE A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 170GL UE170 BIRD STRIKE RT ENG ON ROLL, INSP A/C NO DAMAGE FOUND 2 L 7 2 4T RT A24CE 2002101800088 20021018 00088 SW 2002 10 18 AUS20021023 1 20020911 A 5510 2743000229 STRUCTURE SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UHR WP MCAULY 4HFR34 4HFR34C652 NE HORIZONTAL STAB BIRD STRIKE W O OTHER C F.O.D. LD LANDING 1 AU S 13043 (AUS) BIRDSTRIKE ON RH HORIZONTAL STABILISER. EXTENSIVE DAMAGE CAUSED TO LEADING EDGE AND UPPER AND LOWER SKINS. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002101800089 20021018 00089 EU 2002 10 18 AUS20021024 1 20020907 A 3320 126039MS BALLAST BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE CABIN FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 AU S (AUS) REAR GALLEY WORK-LIGHT BALLAST FAILED. 2 H 7 4 4F 4 F A49EU E6NE 2002101800090 20021018 00090 NM 2002 10 18 AUS20021030 1 20020814 A 3411 BACR13CG2A RELAY BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL PITOT/STATIC SYS FAULTY W K NONE J WARNING INDICATION CL CLIMB 1 AU S (AUS) AIR/GROUND RELAY K522 SUSPECT FAULTY. 2 L 7 2 4F 4 F RT A1NM E23EA 2002101800091 20021018 00091 NM 2002 10 18 UPS02439344 1 20020816 A 5312 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C RT BS 1480 BULKHEAD NR 23 HOLE FOUND CRACKED AT WEB SPLICE PLATE RUNNING I/B APPROX 0.06. THE WEB SPL ICE PLATE REPLACED DUE TO HOLE OVERSIZED AND EXCEEDED LIMIT AS PER SB 747-53A2390 FIG 11. 2 L 7 4 4F A20WE 2002101800092 20021018 00092 NM 2002 10 18 AUS20021035 1 20020704 A 5712 BAC1505100794 RIB BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE WING LE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S 61831 (AUS) WING RIB CONTAINED GALVANIC CORROSION IN AREA OF LE WS 277.5. FOUND DURING CPCP INSPECTION. 2 L 7 3 4F 4 F RT A3WE E2EA 2002101800093 20021018 00093 EU 2002 10 18 AUS20021037 1 20020910 A 3242 5008744 DISK 50079961 FOKKER F27 F27MK50 EU PWA PWA120 PW125B NE BRAKE BROKEN W K NONE O OTHER IN INSP/MAINT 1 AU S MAR87128 (AUS) DURING REPOSITIONING OF AIRCRAFT, ENGINEERS DETECTED A STRANGE NOISE COMING FROM THE LT MAIN LANDING GEAR. INVESTI GATION FOUND THAT ONE OF THE ROTATING BRAKE DISCS HAD CRACKED AND FALLEN APART. AS A RESULT OF THIS FAILURE, THE ADJACEN T BRAKE ASSEMBLY THAT HAD BEEN FITTED FOR THE SAME AMOUNT OF CYCLES WAS REMOVED/CHECKED AND FOUND TO HAVE THE SAME PROBL EM. 2 H 7 2 4T 4 T RT A817 E20NE 2002101800094 20021018 00094 NM 2002 10 18 UPS02439345 1 20020816 A 5320 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C RT BS 1480 BULKHEAD NR 5 HOLE FOUND CRACK AT EXTENSION FITTING RUNNING AFT APPROX 0.06. RT BS 1480 BU LKHEAD LONGERON EXTENSION FITTING NR 5 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11. 2 L 7 4 4F A20WE 2002101800095 20021018 00095 CE 2002 10 18 AUS20021041 1 20020905 A 2731 CONTROL CABLE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO MCAULY 3AF32C 3AF32C505 GL ELEVATOR TAB MISRIGGED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) ELEVATOR TRIM CABLES IN THE HORIZONTAL STABILIZER WERE FOUND TO BE TWISTED. WHEN THE TWIST WAS TAKEN OUT IT WAS FO UND THAT THE ELEVATOR TRIM OPERATED IN THE REVERSE. FURTHER INVESTIGATION FOUND THAT THE FORWARD TRIM CABLES AT THE TURN BUCKLES WERE REVERSED. PERSONNEL/MAINTENANCE ERROR. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2002101800096 20021018 00096 NM 2002 10 18 AUS20021042 1 20020913 A 7830 BLOCKER DOOR BOEING 767 767300 1385204 NM RROYCE RB211 RB211524* NE THRUST REVERSER MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT ENGINE THRUST REVERSER NR 11 BLOCKER DOOR AND LINKAGE MISSING.PARTS WERE LATER LOCATED ON THE RUNWAY. COLD AIR DUCT ACOUSTIC LINING DAMAGED. 2 L 7 2 4F 4 F RT A1NM E12EU 2002101800097 20021018 00097 NM 2002 10 18 AUS20021043 1 20020831 A 6310 A1902 BELT ROBSIN R22 R22BETA 7640110 NM LYC O320 O320B2C 41508 EA ENGINE/XMSN SPLIT W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ENGINE TO TRANSMISSION AFT DRIVE BELT FOUND SPLIT FOR APPROXIMATELY 203.2CM (8INS) AND HAD BADLY WORN. 1 G 7 1 3O 3 O H10WE E274 2002101800098 20021018 00098 NM 2002 10 18 UPS02439346 1 20020816 A 5312 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C RT BS 1480 BULKHEAD NR 24 HOLE FOUND CRACK AT OUTER CHORD SPLICE FITTING RUNNING I/B AFT APPROX 0.09. RT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING NR 24 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 7 47-53A2390 FIG 11. 2 L 7 4 4F A20WE 2002101800100 20021018 00100 NM 2002 10 18 UPS02439347 1 20020816 A 5320 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 10 FOUND CRACK AT EXTENSION FITTING, APPROX 0.09 RUNNING FWD. LT BS 1480 BULKHEAD LONGERON EXTENSION FITTING NR 10 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2 390 FIG 11. 2 L 7 4 4F A20WE 2002101800102 20021018 00102 CE 2002 10 18 AUS20021052 1 20020910 A 5210 1013840961 HANDLE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A42 52043 NE PAX DOOR SHEARED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) PRIOR TO FLIGHT THE PILOT WAS CLOSING THE AIRSTAIR DOOR. WHEN THE INTERNAL DOOR HANDLE REACHED THE LOCKING POINT T HE HANDLE SHAFT SHEARED. THE DOOR HANDLE HAD BEEN INSTALLED ONLY 49 HOURS (76 CYCLES) PREVIOUS DUE TO THE SAME DEFECT. 1 L 7 2 4T 4 T A24CE E4EA 2002101800103 20021018 00103 NM 2002 10 18 UPS02439348 1 20020816 A 5312 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 18 FOUND CRACK AT WEB SPLICE PLATE, APPROX 0.030 RUNNING O/B. LT BS 1480 BULKHEAD WEB SPLICE PLATE NR 18 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11 . 2 L 7 4 4F A20WE 2002101800104 20021018 00104 WP 2002 10 18 AUS20021054 2 20020916 A 7200 ENGINE SWRNGN SA227 SA227AT 8780610 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL LEFT FIRE W O OTHER E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AU S 1872 (AUS) LT ENGINE FIRE ON START UP. A BURST OF FLAME EXITED FROM EXHAUST AND COMPRESSOR. A SMALL FIRE IN THE TAILPIPE SELF EXTINGUISHED. THE TURBINE GLOWED RED FOR APPROXIMATELY TWO TO THREE MINUTES.THE ENGINE LOCKED UP AND WOULD NOT ROTATE. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C P61GL 2002101800105 20021018 00105 EU 2002 10 18 AUS20021055 2 20020913 A 7200 ENGINE BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU RIGHT MALFUNCTIONED W C ABORTED TAKEOFF E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 AU S (AUS) RT ENGINE WOULD NOT ACCELERATE ABOVE 87 PERCENT N1. 2 L 7 2 4F 4 F RT A16WE E21EU 2002101800106 20021018 00106 NM 2002 10 18 UPS02439353 1 20020815 A 5312 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C RT BS 1480 BULKHEAD NR 24 HOLE FOUND CRACK AT WEB SPLICE PLATE RUNNING I/B APPROX 0.09 AND O/B APPROX .125. THE WEB SPLICE PL ATE CHANGED AS PER SB 747-53A2390. REFER HX RS R-53-43-34884 AND UPS EO B747-5310-17499-A. 2 L 7 4 4F A20WE 2002101800107 20021018 00107 NM 2002 10 18 UPS02439366 1 20020816 A 5712 RIB BOEING 747 747123 1384873 NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT WING L/E RIB AT L/E SLAT 1309.15 ROTARY ACTUATOR MOUNTING HOLES NR 1, 7 BORE CORROSION FOUND. RIB FOUND CORRODED AT LOCATION L/E SLAT 1309.15 TO 1309.15. CORROSION BLEND OUT EXCEEDED SRM LIMIT RIB REPLACED PER SRM 51- 10-01, 57-41-34886, UPS EO NR 747-5740-17509. 2 L 7 4 4F A20WE 2002101800108 20021018 00108 NM 2002 10 18 UPS02439369 1 20020817 A 5320 65B133462 ANGLE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C RT MLG W/W PRESSURE DECK LWR SPLICE ANGLE FWD TIP BETWEEN BS 1402 & 1403 , RBL 74 & 77. CORRODED AROU ND 2EA HI-LOCK HEADS. SPLICE ANGLE REPLACED AS PER 51-10-01. 2 L 7 4 4F A20WE 2002101800109 20021018 00109 NM 2002 10 18 UPS02439370 1 20020817 A 5320 65B133462 ANGLE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C RT MLG W/W PRESSURE DECK LWR SPLICE ANGLE TIP BETWEEN BS 1402 & 1403, RBL 56 & 59. CORRODED AROUND 2E A HI-LOCK HEADS. SPLICE ANGLE REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002101800110 20021018 00110 CE 2002 10 18 AUS20021060 1 20020923 A 7160 CPN1167 KNOB CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO MCAULY 3AF32C 3AF32C505 GL ENG AIR INTAKE UNAPPROVED PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S 14201 (AUS) ALTERNATE AIR CONTROL KNOB INCORRECT PART. KNOB APPEARS TO BE HOME MADE. PLACARDING ALSO INCORRECT. UNAPPROVED PAR T.PERSONNEL/MAINTENANCE ERROR. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2002101800111 20021018 00111 NE 2002 10 18 AUS20021064 2 20020920 A 7321 1853M56P08 HMU BOEING 737 737800* NM GE CFM56 CFM567B24 NE NR 2 ENGINE FAULTY W O OTHER E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 AU S 1575 (AUS) NR 2 ENGINE HYDROMECHANICAL UNIT (HMU) FAULTY. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002101800112 20021018 00112 NE 2002 10 18 AUS20021065 2 20020923 A 7200 ENGINE BOEING 747 747238B 1384828 NM RROYCE RB211 RB211524D419 54555 NE NR 4 VIBRATES W O OTHER E F J VIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 AU S (AUS) NR 4 ENGINE VIBRATION CAUSED INFLIGHT SHUTDOWN. 2 L 7 4 4F 4 F A20WE E12EU 2002101800115 20021018 00115 NE 2002 10 18 2002UALA01336 2 20020822 A 7261 21SN04413A SWITCH BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 796UA 26931 222061 NR 1 ENGINE OIL FILTER LT STATUS MESSAGE. ALSO RIGHT PACK FCV STATUS MESSAGE. REPLACED THE OIL FILTER DIFFERENTIAL PRE SSURE SWITCH. THE REMOVED SWITCH WAS A PRE PW SERVICE BULLETIN PW4G-112-79-12 CONFIGURATION. MESSAGE WAS DUE TO FAILED PROX SWITCH ON LWR RT FLOW CONTROL VALVE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002101800116 20021018 00116 EU 2002 10 18 2002UALA01389 1 20020830 A 2150 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E/E BAY MALFUNCTIONED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 463UA 1282 ABORTED TAKEOFF AT 90 KNOTS DUE TO AN AVIONICS VENT MESSAGE. THE AVIONIC EQUIPMENT COOLING COMPUTER WAS RESET AND THE A IRCRAFT FLEW FUTURE FLIGHTS WITH NO INCIDENCE. 2 L 7 2 4F 4 F RT A28NM E40NE 2002101800119 20021018 00119 NM 2002 10 18 2002UALA01426 1 20020907 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 CABIN STA 827, STR 9R, FRAME WEB CRACKED AT AIR GRILL ATTACH POINT. MAJOR REPAIR ACCOMPLISHED. DAMAGED AREA REMOVED AN D REPAIRED WITH HFEC, REPAIRED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800120 20021018 00120 NM 2002 10 18 2002UALA01427 1 20020907 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 CABIN STA 867, STR 9L, FRAME WEB IS CRACKED AT AIR GRILL ATTACH POINT. MAJOR REPAIR ACCOMPLISHED. DAMAGED AREA REMOVED AND VERIFIED WITH HFEC, REPAIRED AND STALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800122 20021018 00122 NM 2002 10 18 2002UALA01429 1 20020908 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 CABIN STA 827, STR 9L, FRAME WEB IS CRACKED AT AIR GRILL ATTACH POINT. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER MFG A ND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800123 20021018 00123 NM 2002 10 18 2002UALA01430 1 20020908 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 CABIN STA 867, STR 9R, FRAME WEB IS CRACKED AT AIR GRILL ATTACH POINT. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER MFG A ND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800125 20021018 00125 NM 2002 10 18 2002UALA01433 1 20020908 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 FWD GALLEY DOOR CUTOUT STOP PAD FITTING, INTERCOSTAL OUTBOARD L ANGLE, CRACKED AT STA 291.5, JUST ABOVE BOTTOM HINGE POI NT. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW L ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800131 20021018 00131 NM 2002 10 18 2002UALA01442 1 20020912 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 945UA 26684 STATION 178, RBL 5, WL 198 AND WL 201, BULKHEAD CRACKED AT ANTENNA MOUNT. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800132 20021018 00132 NM 2002 10 18 2002UALA01443 1 20020912 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 FORWARD NOSE STATION 188 FUSELAGE FRAME CRACKED AT STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. ANGLE DOUBLER REPAIR AND S KIN DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800133 20021018 00133 NM 2002 10 18 2002UALA01445 1 20020913 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 FORWARD CABIN FLOOR SUPPORT CORRODED BS 335 RBL 51 WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT CHANNEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112500113 20021125 00113 NE 2002 11 25 2002UALA01447 2 20020914 A 7230 COMPRESSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE STALLED A UALA O OTHER R PARTIAL RPM/PWR LOSS LD LANDING 1 WP 29 581UA 26701 726678 COMPRESSOR STALL INCURRED DURING REVERSE THRUST. SURGE INSPECTION/CHECK WAS PERFORMED, WITH NO DISCREPANCY FOUND. THE 14TH STAGE CONVERTER VALVE WAS REPLACED AS A PRECAUTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101800135 20021018 00135 NM 2002 10 18 UPS02239766 1 20020919 A 3210 65999091726 SUPPORT FITTING BOEING 727 72722C 138400F NM CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI CORROSION ON INNER FACE OF RH MLG TRUNNION SUPPORT FITTING. RH MLG TRUNNION SUPPORT FITTING REP LACED. 2 L 7 3 4F A3WE 2002101800136 20021018 00136 NM 2002 10 18 UPS02239774 1 20020924 A 5260 RISER BOEING 727 72722C 138400F NM AFT AIRSTAIR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C+SI CORROSION ON RISER #5 FOUND TO BE OUTSIDE LIMITS- REF NRC 480122.(AI RSTAIR DOOR) RISER REPLACE D IAW SRM ADDENDIUM EO B727-5260-1551-A. 2 L 7 3 4F A3WE 2002101800137 20021018 00137 NM 2002 10 18 2002UALA01450 1 20020916 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 CABIN FLOORBEAM UPPER CAP AFT FLANGE STATION 1640 HAS EXCESSIVE MATERIAL LOSS FROM CORROSION REMOVED AT RBL 51 TO RBL 52 . MAJOR REPAIR ACCOMPLISHED. BEAM CAP STRAP REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002101800138 20021018 00138 NM 2002 10 18 2002UALA01451 1 20020914 A 3350 BATTERY PACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 606UA 21867 EXIT PATH LIGHTING FLICKERING OFF AND ON. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A1NM E3NE 2002101800139 20021018 00139 NM 2002 10 18 2002UALA01452 1 20020914 A 5315 FLOORBEAM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 210UA 30216 FLOORBEAM MIDCHORD CRACKED AT LBL 38, STA 246. MAJOR REPAIR ACCOMPLISHED. DOUBLER ANGLE INSTALLED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002101800141 20021018 00141 NM 2002 10 18 2002UALA01454 1 20020915 A 5412 BULKHEAD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 NR 2 PYLON IDG WIRE HARNESS UPPER WEB CUTOUT HAS SEVERAL CRACKS. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER PYLON WEB W ITH REPAIR DOUBLER SPLICE L ANGLE AND STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800142 20021018 00142 NM 2002 10 18 2002UALA01455 1 20020915 A 5412 BULKHEAD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 NR 2 PYLON WIRE HARNESS CUTOUT AT UPPER WEB CRACKED ACCESS THROUGH INBOARD PANEL 442BL. MAJOR REPAIR ACCOMPLISHED. REPA IRED UPPER WEB WITH REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800143 20021018 00143 NM 2002 10 18 2002UALA01456 1 20020915 A 5412 BULKHEAD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 NR 1 PYLON PNEUMATIC DUCT CUTOUT, UPPER WEB CRACKED AT INBOARD AFT CORNER WHERE FIRE PROTECTION LINES ATTACHES. MAJOR R EPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800144 20021018 00144 NM 2002 10 18 2002UALA01457 1 20020915 A 5412 BULKHEAD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 NR 1 PYLON UPPER WEB CRACKED AT MAIN ENGINE WIRE HARNESS CUTOUT. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DO UBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800145 20021018 00145 NM 2002 10 18 2002UALA01458 1 20020915 A 5412 BULKHEAD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 NR 1 PYLON UPPER WEB CRACKED AT IDG CABLE CUTOUT. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800146 20021018 00146 NM 2002 10 18 2002UALA01459 1 20020915 A 5412 BULKHEAD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 NR 2 PYLON AFT UPPER SPAR WEB, AFT INBOARD CORNER CRACKED FOR PNEUMATIC DUCT, ACCESS THROUGH RT WING PANEL 611PT. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800148 20021018 00148 NM 2002 10 18 2002UALA01461 1 20020915 A 5420 FITTING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 NR 1 PYLON INBOARD MID SPAR FITTING LOWER ANGLE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED LOWER HORIZONTAL ANGLE . 2 L 7 2 4F 4 F RT A1NM E24NE 2002101800150 20021018 00150 SO 2002 10 18 C2XA02BT061 1 20021016 A 3300 LIGHT EMB 145 EMB145LR 3260212 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14916 145415 EWR---CO3489, CREW REPORTED THAT THERE WAS AN ELECTRICAL SMELL IN THE AFT CABIN (AT SEATS 17A AND 18A) AIRCRAFT PLACED O N MEL #33-20-00 CATEGORY "C" CONTROL NUMBER 031926. ....MAINTENANCE REMOVED AND REPLACED CEILING LIGHT ASSEMBLY AT SEAT 17A AREA. OPS.CHECKED GOOD. MEL ITEM CLEARED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002101800151 20021018 00151 NM 2002 10 18 2002UALA01463 1 20020916 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 945UA 26684 STATION 827, BELOW AFT PIT DOOR, FUSELAGE SKIN HAS EXCESSIVE MATERIAL REMOVED DURING REPAIR. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800152 20021018 00152 EU 2002 10 18 2002UALA01464 1 20020917 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 INTERIM REPAIR INSTALLED BETWEEN FRAME 73 AND FRAME 75. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002101800153 20021018 00153 NM 2002 10 18 2002UALA01465 1 20020917 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 945UA 26684 CABIN FLOORBEAM, BODY STATION 947, RBL 48, UPPER SURFACE HAS EXCESSIVE MATERIAL REMOVED DURING REWORK. MAJOR REPAIR ACC OMPLISHED. FLOORBEAM FLANGE DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002101800154 20021018 00154 EU 2002 10 18 2002UALA01466 1 20020917 A 3242 216001 BRAKE ASSY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 402UA 439 RETURNED TO FIELD UNDER AMBER ALERT DUE TO LEFT BRAKE WOULD NOT COOL. REPLACED NR 1 BRAKE ASSEMBLY. NO PREVIOUS HISTOR Y OF HIGH TEMPS. NO FURTHER DEFECTS ON SUBSEQUENT FLIGHTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2002101800155 20021018 00155 NM 2002 10 18 2002UALA01467 1 20020918 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 CABIN FLOOR BEAM INBOARD CHORD EXFOLIATED AT STATION 681 LBL 62. MAJOR REPAIR ACCOMPLISHED. REPLACED CHORD ANGLE WITH NEW. 2 L 7 2 4F 4 F RT A2NM E17NE 2002102900098 20021029 00098 SO 2002 10 29 C2XA02BT060 1 20021014 A 2530 CONNECTOR EMB 145 EMB145LR 3260212 SO GALLEY SHORTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 19538 STRONG ELECTRICAL SMELL IN GALLEY. MAINTENANCE FOUND SHORTED NUMBER ONE COFFEE POT CONNECTOR. MAINTENANCE REMOVED AND REPLACED COFFEE POT CONNECTOR AND REPLACED COFFEE POT UNIT. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002101800158 20021018 00158 SO 2002 10 18 AUS20021069 1 20020918 A 2910 OAS29305 POWERPACK PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA HARTZL HCE3Y HCE3YR2 GL HYD SYSTEM CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 AU S 454 (AUS) HYDRAULIC POWER PACK CONTAMINATED BY UNKNOWN BIOLOGICAL GROWTH. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2002101800159 20021018 00159 NE 2002 10 18 042655 2 20020825 A 7200 PT6A67DGG GAS GENERATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67 52043 NE Zone 500 FAILED A AMWA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 07 5YV * 9559 UE5 WHILE INFLIGHT FROM PANAMA CITY, FLORIDA THE LEFT ENGINE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED. THE OIL PRESSURE WAS BELOW 60 PSI. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO FIELD WITH NO FURTHER INCIDENT. THE CORRECTIVE A CTION WAS THE THE LEFT GAS GENERATOR AND THE POWER SECTION WAS REPLACED. TEARDOWN REPORT WILL BE AVAILABLE AT A LATER DA TE. 2 L 7 2 4T 4 T RT A24CE E26NE 2002101800160 20021018 00160 WP 2002 10 18 DHL2002806014 1 20021017 A 2612 R27024 RELAY DOUG DC8 DC873F 302199F WP A DHLA O OTHER L NO TEST IN INSP/MAINT 1 SO 01 806DH 46002 1) #3 ENG "B" LOOP FAILS TO TEST #3 ENG "B" LOOP SELECTED, FIRE WARNING LIGHT WILL START TO LIGHT AND WILL FAIL TEST2) INSTALLED RELAY R2-7003. XFERRED TO DMI 10693 PER MEL 26-2-3 CAT C XFERRED TO DMI 10693 ON LG PG 3193773) REF DMI # 1 0693 (# 3 ENG. "B" FIRE LOOP FAILS TO TEST)4) REMOVED AND REPLACED FIRE WARNING RESET RELAY R2-7024 OPS CHECKS GOOD IAW DC-8 M/M 26-10-1 THIS CLEARS DMI#10693 PLACARD REMOVED 2 L 7 4 4F RT 4A25 2002101800161 20021018 00161 WP 2002 10 18 WRNA200200006 1 20021018 A 2130 1519930105 DUCT LKHEED L10111 LKHEED 1011 10113851 5265010 WP DETACHED A WRNA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CR CRUISE 1 SO 05 311EA 193A1012 193A1012 Aircraft at F/L 280 outflow valves full closed cabin climbing at 2,000 ft/min. Manual and stby control no help. Aircraft returned to departing airport. Fuel dumped (42K lbs.) to make max landing wt. Aircraft landed normal.Corrective Action: Mx found duct out of position at ATM compartment. Repositioned and secured duct. Pressurized A/C. System check satisfac tory on ground I/A/W 36-14-02 and 21-31-00 of MM. Aircraft returned to service. 2 L 7 3 4F A23WE 2002110100105 20021101 00105 EA 2002 11 1 COMA0260587 1 20021012 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 01 915CA 4403 7013 FLIGHT 5748 EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY LIGHTS BATTERY. 2 L 7 2 4F RT A21EA 2002110100093 20021101 00093 EA 2002 11 1 COMA0260564 1 20021004 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B16 1900305 EA T/E FLAP FAILED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 781CA 3476 7312 FLAPS FAILED AT 30 DEGREES. REPLACED THE RIGHT BRAKE AND POSITION SENSOR UNIT. 2 L 7 2 4F RT A21EA 2002110100094 20021101 00094 EA 2002 11 1 COMA0260565 1 20021004 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 781CA 3476 7312 FLAPS FAILED AT 30 DEGREES. REPLACED THE RIGHT BRAKE POSITION UNIT. 2 L 7 2 4F RT A21EA 2002110100100 20021101 00100 EA 2002 11 1 COMA0260570 1 20021005 A 2710 CONTROL CABLE CNDAIR CL600 CL6002B19 1900309 EA AILERON LACK OF LUBE A COMA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 01 713CA 7245 AILERON CONTROLS SEEMED STIFFENER THEN NORMAL. LUBRICATED THE LEFT AND RIGHT AILERON CONTROL ASSEMBLY PER EO 27-069RB. 2 L 7 2 4F RT A21EA 2002110100102 20021101 00102 EA 2002 11 1 COMA0260572 1 20021006 A 2910 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LOOSE A COMA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 914CA 7012 HYDRAULIC RESERVOIR NUMBER ONE IS AT 40 PERCENT. TIGHTENED LOOSE HYDRAULIC LINE AT ENGINE DRIVE PUMP. 2 L 7 2 4F RT A21EA 2002110100103 20021101 00103 EA 2002 11 1 COMA0260576 1 20021005 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 781CA 3476 7312 FLAPS FAILED AT 40 DEGREES. REPLACED THE RIGHT BRAKE AND POSITION SENSOR UNIT. 2 L 7 2 4F RT A21EA 2002110100104 20021101 00104 EA 2002 11 1 COMA0260579 1 20021009 A 2750 860D10018ABC FCU CNDAIR CL600 CL6002B19 1900309 EA E/E BAY MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 987CA 4888 7199 FLAPS FAILED AT 13 DEGREES. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 2002101800162 20021018 00162 EA 2002 10 18 COMA0260588 1 20021017 A 3610 9799981 BLEED VALVE CNDAIR CL600 CL6002B19 1900309 EA R/H INOPERATIVE A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 987CA 15479 7199 FLIGHT 5973 R/H 10TH STAGE BLEED VALVE INOP.REPLACED BLEED AIR SHUT OFF VALVE 2 L 7 2 4F RT A21EA 2002101800163 20021018 00163 EA 2002 10 18 COMA0260589 1 20021017 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA R/H SMOKE A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 931CA 15954 7037 FLIGHT 5319 THICK SMOKE IN CABIN.REPLACED THE R/H ACM. 2 L 7 2 4F RT A21EA 2002101800164 20021018 00164 EA 2002 10 18 COMA0260590 1 20021016 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA K NONE O OTHER AP APPROACH 1 SO 01 967CA 7134 FLIGHT 5975 FLAPS INDICATED 43 DEGREES WHEN SELECTED TO 45 DEGREES.2 DEGREES INDICATION ERROR IS WITHIN LIMITS - NO MAIN T. PERFORMED. 2 L 7 2 4F RT A21EA 2002101800165 20021018 00165 EA 2002 10 18 COMA0260591 1 20021015 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 949CA 7080 FLIGHT 5480 EMERGENCY FLOOR LIGHT AT ROW 3 IS INOP.DEFERRED MAINT PER MEL 2 L 7 2 4F RT A21EA 2002101900001 20021019 00001 WP 2002 10 19 DHL2002803506 1 20020924 A 5700 5769859164 PAN DOUG DC8 DC873 302199C WP A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 R/H WING L/E ZEE PAN UPPER PART CRACKED 2 IN AT STA XFS 245.000.REMOVED ZEE PAN PER SRM 51-1-21 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW ZEE PAN PER SRM 51-1-21 PG 2,51-3-0 PG 1 2 L 7 4 4F RT 4A25 2002101900002 20021019 00002 WP 2002 10 19 DHL2002873507 1 20020903 A 5712 56488932 PANEL DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 873SJ 83065 46091 ITEM N/R 0767: RT. WING T/E UPPER PANEL CRACKED 4" STA. XRS436.000 TO STA. XA475.000CORR: REMOVED AND REPLACED RT. WING T/E UPPER PANEL , STA XRS 436 TO XA475.000 IAW SRM 51-3-0 2 L 7 4 4F RT 4A25 2002101900003 20021019 00003 WP 2002 10 19 DHL2002873508 1 20020904 A 5712 FORMER DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 873SJ 83065 46091 ITEM N/R 0716: LH WING OUTBD. LEADING EDGE .500 CRACK IN FORMER UPPER PART STA. XFS885.000CORR: REMOVED DAMAGED FORMER I AW SRM51-1-21 PG.1 FABRICATED NEW FORMER IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B INSTALLE D FORMER IAW SRM 57-2-0 PG. 9-10 2 L 7 4 4F RT 4A25 2002102000001 20021020 00001 EU 2002 10 20 RAIA00210282 1 20021010 A 3244 AHA1837 TIRE JETAIR JETSTM JETSTM4101 1500501 EU FLAT A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 568HK 41086 5564-STL- RIGHT INBOARD MLG TIRE WENT FLAT DURING TAXI. MAINTENANCE REMOVED AND REPLACED #3 AND #4 WHEEL AND TIRE, IAW A MM. 2 L 7 2 4T RT A41NM 2002102000002 20021020 00002 2002 10 20 RAIA00210283 4 20021015 A 3414 7002860909 INDICATOR AEROSP ATR72 ATR72202 8680940 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 723TE 29981 22002 283 5562-STL- CAPTAIN'S AIRSPEED INDICATOR DISPLAYS OFF FLAG. MAINTENANCE REMOVED AND REPLACED CAPTAINS AIRSPEED INDICATOR, OPS CK OK. 2 H 7 2 4T RT A53EU 2002102000003 20021020 00003 EU 2002 10 20 RAIA00210286 1 20021017 A 3060 7826892 BRUSH BLOCK AEROSP ATR42 ATR42300 8680920 EU INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 421TE 102 5596-STL-LEFT PROP HEAT FAILED. MAINTENANCE REMOVED AND REPLACED #1 PROPELLER BRUSH BLOCK, OPS CK OK. 2 H 7 2 4T RT A53EU 2002102100002 20021021 00002 NM 2002 10 21 VNAA0210019 1 20021017 A 3000 851003 EJECTOR VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 437JS 15499 52 3055 THE CREW RECEIVED AN AIRFOIL DE-ICE FAIL CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EJECTO R FLOW CONTROL VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002102100005 20021021 00005 NM 2002 10 21 751PA0004 1 20021016 A 3350 LIGHT BOEING 757 757200 1384950 NM A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 751PA 23928 Floor path emergency lights inop at mid lavatory. Relamped emergency path lights. ops check ok. 2 L 7 2 4F RT A2NM 2002102100006 20021021 00006 NM 2002 10 21 751PA0005 1 20021016 A 3350 LAMP BOEING 757 757200 1384950 NM A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 751PA 23928 R1 door exterior emergency exit light out. Replaced lamp for R1 door emergency exit light. Ops chk. normal. 2 L 7 2 4F RT A2NM 2002102100007 20021021 00007 NM 2002 10 21 SWAA022419 1 20021012 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500A PLUS 11, STR 14R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102100008 20021021 00008 NM 2002 10 21 SWAA022420 1 20021014 A 5311 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, WL 148 AND RBL 8. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002102100009 20021021 00009 NM 2002 10 21 SWAA022421 1 20021014 A 5311 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 747, WL 148 AND RBL 8.5. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002102100010 20021021 00010 NM 2002 10 21 SWAA022424 1 20021015 A 5330 65C20843 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF AIRSTAIR CUTOUT, AT BS 347 BETWEEN STR 1 9L AND 20L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F A16WE 2002102100011 20021021 00011 NM 2002 10 21 SWAA022425 1 20021015 A 5714 6545409 BEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND TRANSVERSE BEAM CRACKED (2 EA) AT BS 706, BL O AND LBL 25. REPAIRED TRANSVERSE BEAM PER SWA EA. 2 L 7 2 4F A16WE 2002102100012 20021021 00012 NM 2002 10 21 SWAA022427 1 20021015 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 392 AT STR 10R AND BS 460 AT STR 14R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102100013 20021021 00013 NM 2002 10 21 SWAA022428 1 20021015 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 500A PLUS 11 AT STR 14L, BS 380 AT STR 10L AND BS 495 AT STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102100014 20021021 00014 NM 2002 10 21 SWAA022430 1 20021012 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND LBL 10. REPAIRED WEB PER SRM. 2 L 7 2 4F A16WE 2002102100015 20021021 00015 2002 10 21 SWAA022405 4 20021013 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002102100016 20021021 00016 NM 2002 10 21 SWAA022406 1 20021013 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, BELOW STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102100017 20021021 00017 NM 2002 10 21 SWAA022407 1 20021010 A 5320 6547978 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 747 AND BS 827, WL 208 AND LBL 67. REPAIRED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2002102100018 20021021 00018 NM 2002 10 21 SWAA022408 1 20021012 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 809, ABOVE STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102100019 20021021 00019 NM 2002 10 21 SWAA022409 1 20021013 A 5330 589357 SKIN BOEING 737 7372H4 138448C NM COCKPIT WINDOW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND WINDOW POST SKIN CRACKED AT PILOT'S SLIDING WINDOW ON LOWER CORNER. REPAIRED SKIN PE R SRM. 2 L 7 2 4F A16WE 2002102100020 20021021 00020 NM 2002 10 21 SWAA022410 1 20021014 A 5210 507945 SKIN BOEING 737 7372H4 138448C NM FWD ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR OUTER SKIN CRACKED BELOW DOOR HANDLE CUTOUT. REPAIRED DOOR SKIN PER S RM. 2 L 7 2 4F A16WE 2002102100021 20021021 00021 NM 2002 10 21 SWAA022416 1 20021013 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 440 AND BS 448, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102100022 20021021 00022 2002 10 21 SWAA022437 4 20021015 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM FWD ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 102SW 23108 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002102100023 20021021 00023 2002 10 21 SWAA022438 4 20021015 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002102100025 20021021 00025 NM 2002 10 21 CALA0200502 1 20021021 A 5754 114N3002128 SLAT BOEING 757 757224 1384958 NM #6 POSITION DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13113 29230 27555 INSPECTION FOUND #6 SLAT WEDGE SKIN DELAMINATED. THE #6 SLAT WAS REMOVED AND REPLACED IAW MM 27-81-01. 2 L 7 2 4F RT A2NM 2002102100026 20021021 00026 SO 2002 10 21 000202 1 20020927 A 7830 WARNING SYSTEM EMB 145 EMB145 3260210 SO COCKPIT ACTIVATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 272 NR 2 THRUST REVERSER DISAGREE MESSAGE ON TAKEOFF ROLL. MEL'D NR 2 THRUST REVERSER. 2 L 7 2 4F RT T00011AT 2002102100029 20021021 00029 NM 2002 10 21 02FDEA00650 1 20020914 A 3260 SWITCH BOEING 727 727200 138407E NM RT MLG FAULTY A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 241FE 20979 DURING GEAR RETRACTION DURING TAKEOFF A RED DOOR WARNING LIGHT ON THE GEAR WARNING PANEL AND ASSOCIATED RIGHT GEAR DOOR LIGHT ON SECOND OFFICERS PANEL ILLUMINATED AFTER PLACING THE GEAR HANDLE TO THE OFF POSITION. QRH WAS REFERENCED. LIGH T WENT OUT AFTER PLACING HANDLE TO UP POSITION. REMOVED AND REPLACED THE RT GEAR DOOR WARNING SWITCH PER M/M 32-62 011- 4. ACCOMPLISHED GEAR SWING OPS CK NORMAL FOR SERVICE. 2 L 7 3 4F RT A3WE 2002102100030 20021021 00030 NM 2002 10 21 02FDEA00651 1 20020914 A 3260 DOWNLOCK SWITCH BOEING 727 727100 1384036 NM RT MLG LOOSE A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 124FE 19360 ON TAKEOFF, UPON GEAR RETRACTION RED RT GROUND UNSAFE LIGHT AND RT MAIN GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED, FOLLO WED QRH PROCEDURES WITH GEAR HANDLE OFF, GREEN RT GEAR SAFE LT, AND RT MAIN GROUND DOOR OPEN LIGHT ON, AFTER RECYCLING GEAR IAW QRH, GEAR UP AND LOCKED WITH SAFE INDICATIONS. FOUND RT GEAR DOWNLOCK SWITCH LOOSE AND INTERMITTENT R&R RT ML G DOWN LOCK SWITCH IAW 727 MM 32-61-021-4. COMPLIED WITH ADJ TEST OF POSITION SWITCHES IAW 727 MM 32-61-021-5 ALL INDIC ATIONS NORMAL, OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2002102100031 20021021 00031 NM 2002 10 21 02FDEA00664 1 20020919 A 2750 FLAP BOEING 727 727200 138407E NM WING LOOSE A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 25 461FE 22548 AIRFRAME BUFFET OCCURRED DURING CLIMB OUT AT .65 MACH, SLOWING THE AIRCRAFT DECREASED THE BUFFET. NO BUFFET AT .58 MACH . INSPECTED FLAPS AND AILERONS FOR SECURITY. FOUND THE RT OUTBD AFT FLAP HAD EXCESSIVE PLAY. DROPPED FLAPS AND CHECKE D THE AFT FLAP AFT ROLLER ECCENTRIC MEASUREMENT. FOUND ALL OF THEM OUT OF LIMITS. ADJUSTED ALL RT OUTBD AFT FLAP ECC ENTRICS PER M/M 27-51-012-4. CYCLED FLAPS SEVERAL TIMES. OPS CHECK IS NORMAL. ALSO FOUND RT OUTBD FLAP, OUTBD JACKSCR EW FAIRING SLIGHTLY LOOSE. SECURED ALL MOUNT BOLTS PER M/M 27-51-023-4. 2 L 7 3 4F RT A3WE 2002102100033 20021021 00033 NM 2002 10 21 C1HA200281007 1 20020902 A 2830 CONNECTOR BOEING 727 7272S7 138407Z NM FUEL DUMP SYS LOOSE A C1HA J DUMP FUEL O OTHER CL CLIMB 1 GL 15 681CA 22020 DURING FUEL DUMP, LEFT DUMP NOZZLE VALVE IN TRANSIT LIGHT ILLUMINATED BUT DID NOT EXTINGUISH. FUEL DUMP WAS OBSERVED FR OM THE COCKPIT AT RIGHT WING BUT NOT AT LEFT WING. CLEANED AND RESECURED LEFT FUEL DUMP NOZZLE VALVE CANNON PLUG. OPER ATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 2002102100034 20021021 00034 NM 2002 10 21 C1HA200297008 1 20020913 A 3230 656021123 ACCESSORY UNIT BOEING 727 727270 138408P NM E/E BAY DEFECTIVE A C1HA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 697CA 23052 ON TAKEOFF THE GEAR HANDLE WOULD NOT GO BEYOND THE OFF POSITION. AT THE OFF POSITION THE RED AND GREEN GEAR LIGHTS WERE ILLUMINATED. REPLACED LANDING GEAR ACCESSORY UNIT AND OPERATIONALLY CHECKED PER MM. OPS NORMAL. 2 L 7 3 4F RT A3WE 2002102100036 20021021 00036 CE 2002 10 21 GLBA2002142 1 20020901 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE BIRD STRIKE A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 226GL UE226 BIRD STRIKE ON TAKE OFF ROLL, BIRD STRIKE INSP CHECKS GOOD. 2 L 7 2 4T RT A24CE 2002102100037 20021021 00037 CE 2002 10 21 GLBA2002143 1 20020912 A 2435 23078019 STARTER GEN BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 219GL UE219 RT GEN FAILED DC GEN ILLUM ON T/R, R&R RIGHT START GEN. 2 L 7 2 4T RT A24CE 2002122000016 20021220 00016 NE 2002 12 20 GLBA2002145 2 20020913 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67A 52043 NE LEFT MALFUNCTIONED A GLBA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 153GL 13226 UE153 PS0095 LT ENGINE LOW OIL PRESSURE ANNUNCIATOR WITH MASTER WARNING, REMOVED AND REPLACED LT ENGINE. 2 L 7 2 4T 4 T RT A24CE E26NE 2002102100040 20021021 00040 WP 2002 10 21 ABXA020255 1 20021018 A 7931 42D491C PRESSURE SWITCH DOUG DC8 DC863F 302198F WP DAMAGED A ABXA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 GL 23 828AX 0 45999 #1 OIL PRESSURE LIGHT ILLUMINATED. PRESSURE/TEMP. GOOD. #1 THROTTLE TO IDLE. LIGHT REMAINED ON. SECURED ENGINE. RAN ENGI NE, NO DISCREPANCY, DISCONNECTED BOTH OIL MAIN WARNING SWITCHES. MEGGED WIRE FROM DIM BOX, NO DISCREPANCY. ON INSPECTION , FOUND DIFFERENTIAL OIL PRESSURE SWITCH DAMAGED EXTERNALLY. HOLE IN CASE. REPLACED SWITCH IAW DC-8 MM 79-33-01-2. OPS A ND LEAK CHECKED GOOD ON ENGINE RUN. 2 L 7 4 4F 4A25 2002102100041 20021021 00041 CE 2002 10 21 GLBA2002146 1 20020913 A 5610 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT CRACKED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 226GL UE226 CAPT'S WINDSHIELD CRACKED IN FLT, R&R CAPT'S WINDSHIELD. 2 L 7 2 4T RT A24CE 2002102100042 20021021 00042 2002 10 21 GLBA2002149 4 20020918 A 3422 6226136002 GYRO BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 NM 03 253GL 1512 UE253 NR 1 EHSI HDG RED FLAG, R&R NR 1 DIRECTIONAL GYRO. 2 L 7 2 4T RT A24CE 2002102100043 20021021 00043 WP 2002 10 21 IXXA0200068O 1 20020912 A 3260 WARNING SYSTEM DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A IXXA O OTHER N FALSE WARNING CL CLIMB 1 SW 11 606AL 88549 302 46044 AFTER TAKE OFF FROM BRO, THE LANDING GEAR DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED FOLLOWING LANDING GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR AND THE LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO MEM FOR AN UNEVENTFUL LANDING. M AINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED IN ACCORDANCE WITH THE DOUGLAS MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002102100046 20021021 00046 NE 2002 10 21 P5CA0200699 2 20020912 A 7230 COMPRESSOR BOEING 747 747300 GL GE CF6 CF650E2 30018 NE NR 3 ENGINE STALLED A P5CA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 23 354MC 23394 517897 CLIMBING THROUGH 15,000 FT NR 3 ENGINE COMPRESSOR STALLED. EGT WAS 100 DEGREES CELCIUS. LOWER THAN OTHER MOTOR & N2 WA S LOWER WITH NACELLE ANTI-ICE ON. TROUBLESHOT ENGINE PER MM 71-00-43, PERFORMED INSPECTION PER MM 72-00-00 & BORESCOPE OF ENGINE IAW MM 72-30-00. ALL INDICATIONS NORMAL. PERFORMED ENGINE RUN IAW 71-00-00. ALL OPERATIONS NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 2002102100050 20021021 00050 CE 2002 10 21 CA021001008 1 20020930 A 5730 65210008 PANEL CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE STUB WING CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FWD OUTBOARD CORNER OF BONDED DOUBLER. PANEL WAS BEING REPLACED DO TO OIL CANNING FROM DATE OF MANUFACTURE WHEN T HE CORROSION WAS FOUND AT THE FWD OUTBOARD CORNER WHERE THE PANEL CONTACTS A MONEL DOUBLER SPLICE PLATE. THIS IS NOT AN AREA THAT CAN BE INSPECTED UNLESS THE THE PANEL IS REMOVED OR UNTIL THE CORROSION MIGRATES BEYOND THE MONEL DOUBLER. 1 L 7 2 4F 4 F A22CE E1NE 2002102100053 20021021 00053 NM 2002 10 21 PCAA0209107 1 20020916 A 3350 FUSE DHAV DHC8 DHC8102 2809003 NM POWER SUPPLY BLOWN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT RIGHT AFT EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE. FUSES REPLACED IN AFT EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002102100055 20021021 00055 CE 2002 10 21 RK270 1 20020909 A 3260 MS24331 DOWNLOCK SWITCH BEECH MU300 400A 1155402 CE NLG FAULTY E ERYA O OTHER J WARNING INDICATION AP APPROACH 1 CE 07 800SD RK270 MLG DID NOT EXTEND WITH NORMAL SYSTEM. EXTENDED GEAR WITH AUX SYSTEM. INSTALLED NEW NLG DOWNLOCK/NOT LOCKED SWITCH. 2 H 7 2 4F RT A16SW 2002102100057 20021021 00057 NM 2002 10 21 CA021002004 1 20021001 A 5280 AN960616L HINGE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG DOOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 40042 40042 (CAN) THE AFT HINGE OF THE LT/ MIDDLE MLG DOOR WAS FOUND TO HAVE THE BEARING ATTACHMENT POINT FALLING APART. THE IPC CAL LS FOR A WASHER THAT CAN PASS THROUGH THE HINGE BEARING FITTING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002102100058 20021021 00058 CE 2002 10 21 CA021002006 1 20020924 A 5741 8178610 BOLT BEECH 100 B100 1152919 CE LT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WING BOLTS INSPECTED AS PER BEECH S.I.R.M. 57-16 INDEX 10. INDEX 1-11 DONE IN CONJUNCTION WITH CF-1981-25R6. CRACK FOUND IN LT UPPER AFT WING BOLT. CRACK FOUND WHERE SHAFT CONNECTS TO BOLT HEAD. WING BOLT REPLACED WITH NEW. CRACK FOUN D 1 YEAR/324 HOURS AFTER WING BOLT INSPECTION COMPLETED, SEPT 24/2001. BEECH S.I.R.M. 57-16-01 INDEX 10 CALLS FOR WING B OLT INSPECTION OF 3 YEARS/1000 HOURS. COMPANY WILL BE DOING ALL INSPECTIONS AS PER S.I.R.M. 57-16-01 INDEX 1-11 IN CONJU NCTION WITH AD CF-1981-25R6 EVERY 500 HOURS/12 MONTHS. 1 L 7 2 4T A14CE 2002102100059 20021021 00059 NM 2002 10 21 UPS02239394 1 20020826 A 2822 HOUSING BOEING 727 72722C 138400F NM RT WING CRACKED A IPXA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C FUEL LEAKING FROM NR 3 TANK O/B BOOST PUMP CAVITY. FUEL LEAK TRACED TO BOOST PUMP HOUSING FWD I/B ARE A AT ATTACH FLANGE, SEALANT REMOVED FROM SUSPECT AREA IAW SRM 51-20-4, SUSPECT CRACKS FOUND ON BOOST PUMP ATTACH FLANGE, HFEC CONFIRMS CRACKS. CRACKED BOOST PUMP HOUSING FLANGE CUTOUT IAW SRM 51-10-01. HFEC PERFORMED ON CUTOUT NDF. HOUSI NG REPAIRED IAW SRM 57-10-3, SEALED IAW SRM 51-20-04. 2 L 7 3 4F A3WE 2002102100060 20021021 00060 NM 2002 10 21 UPS02239395 1 20020831 A 5330 STRAP BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C TEAR STRAP DISBONDED AT BS 640 BETWEEN S4R AND S5R. DURING REPAIR IAW SRM CORROSION NOTED BETWEEN FAY ING SURFACES. TEAR STRAP REMOVED IAW SRM 51-30-02, CORROSION FOUND OUTSIDE LIMITS, NEW TEAR STRAP FABRICATED IAW SRM 5 3-30-04 PARA 2C METHOD V AND INSTALLED. 2 L 7 3 4F A3WE 2002102100061 20021021 00061 NM 2002 10 21 UPS02239397 1 20020903 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C SUSPECT CRACK IN NOSE WHEEL WELL RT PRESSURE WEB BS 258. HFEC CONFIRMS CRACKS IAW 727 NDT MAN PT6 51- 00-00 FIG 4. DAMAGE AREA REMOVED IAW SRM 51-10-01. HFEC CARRIED OUT AND CONFIRMS DAMAGE REMOVAL. REPAIR CARRIED OUT I AW SRM 51-40-02 FIGURE 1. 2 L 7 3 4F A3WE 2002102100062 20021021 00062 NM 2002 10 21 UPS02239399 1 20020903 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C SUSPECT CRACK AT BS 246, NLG WHEEL WELL RT PRESSURE WEB 6 INCHES ABOVE SILL CHORD. HFEC IAW NDT MAN 5 1-00-00 PT 6 FIG 4 CRACK CONFIRMED, DAMAGE CUTOUT IAW SRM 51-10-01, HFEC IAW NDT MAN 51-00-00 PT 6 FIG 4 NDF. REPAIR CA RRIED OUT IAW SRM 51-40-02 FIGURE 1. 2 L 7 3 4F A3WE 2002102100063 20021021 00063 NM 2002 10 21 UPS02239400 1 20020830 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C NOSE WHEEL WELL RT SIDE WALL WEB HAS SUSPECT CRACK 3 INCHES ABOVE SILL AT BS 243 APPROX. HFEC CARRIED AND CONFIRMS CRACKS. DAMAGE REMOVED IAW SRM 51-10-01, HFEC C/W ON CUTOUT NDF. REPAIRED IAW SRM 51-40-02 FIGURE 1. 2 L 7 3 4F A3WE 2002102100064 20021021 00064 NM 2002 10 21 UPS02239401 1 20020905 A 5311 65224972 FRAME BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C DURING INSTALLATION OF REPAIR PARTS TO LOWER SECTION OF BS 930 FITTING, CRACKS FOUND ON AFT HORIZONTAL FLANGE AT WL 201. FRAME REPLACED IAW DWG 65-16336 AND SRM 51-30-3. FRAME REPAIR IAW SRM 53-10-4 FIG 1 FRAME REINFORCI NG ANGLE REPAIRED IAW SRM 51-40-4 FIG 1. 2 L 7 3 4F A3WE 2002102100065 20021021 00065 NM 2002 10 21 UPS02239403 1 20020829 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C CRACK CONFIRMED AT MID GALLEY DOOR LWR HINGE LWR CUTOUT. CRACK CONTAINED WITH STOP DRILL CONFIRMED BY NDT HFEC. REPAIR DOUBLER FABRICATED IAW UPS EO B727-5330-1036 AND BOEING DWG 65-73484. 2 L 7 3 4F A3WE 2002102100066 20021021 00066 NM 2002 10 21 UPS02239404 1 20020902 A 2710 65532055 CONTROL QUADRANT BOEING 727 72722C 138400F NM AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C LT I/B AILERON BUS QUADRANT FOUND TO HAVE CORROSION ON BEARING SEAT ON REMOVAL OF BEARINGS. REMOVED L OWER QUADRANT IAW MM 27-10-56, QUADRANT REPLACED IAW MM 27-10-56. 2 L 7 3 4F A3WE 2002102100067 20021021 00067 NM 2002 10 21 UPS02239405 1 20020828 A 5755 ATTACH FITTING BOEING 727 72722C 138400F NM SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C NR 13 SPOILER SUPPORT CASTING O/B CASTING ATTACH BRACKET IS CRACKED AT LOWER ATTACH HOLE. REMOVED NR 13 SPOILER AND FWD ATTACH CASTING IAW MM 27-62-01, REPLACED O/B SUPPORT CASTING IAW DWG 65-17351 AND 65-16201, AND SRM 5 1-30-20. REINSTALLED SPOILER AND SPOILER SUPPORT IAW MM 27-61-01, 27-61-81. 2 L 7 3 4F A3WE 2002102100068 20021021 00068 NM 2002 10 21 UPS02439333 1 20020816 A 5312 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 15 FOUND CRACK AT WEB SPLICE PLATE , APPROX 0.02 INCH RUNNING O/B. L T 1480 BULKHEAD WEB SPLICE PLATE NR 15 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG1 1. 2 L 7 4 4F A20WE 2002102100069 20021021 00069 NM 2002 10 21 UPS02439334 1 20020816 A 5312 BULKHEAD BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 1 FOUND CRACK AT BULKHEAD CHORD, APPROX 0.06 INCH RUNNING FWD. LT BS 1480 BULKHEAD CHORD NR 1 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11. 2 L 7 4 4F A20WE 2002102100070 20021021 00070 NM 2002 10 21 UPS02439335 1 20020816 A 5312 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 15 FOUND CRACK AT OUTER CHORD SPLICE FITTING, APPROX 0.030 INCH. LT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING NR 15 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 74753 A2390 FIG 11. 2 L 7 4 4F A20WE 2002102100071 20021021 00071 NM 2002 10 21 UPS02439336 1 20020816 A 5312 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 16 FOUND CRACK AT WEB SPLICE PLATE, APPROX .125 INCH, RUNNING O/B. LT BS 1480 BULKHEAD WEB SPLICE PLATE NR 16 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-3A2390 F IG 11. 2 L 7 4 4F A20WE 2002102100072 20021021 00072 NM 2002 10 21 UPS02439337 1 20020816 A 5312 BULKHEAD BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 15 FOUND CRACK AT BULKHEAD WEB APPROX 0.03 INCH RUNNING O/B. LT BS 1 480 BULKHEAD WEB NR 15 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11. 2 L 7 4 4F A20WE 2002102100073 20021021 00073 NM 2002 10 21 UPS02439338 1 20020816 A 5312 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 1 FOUND CRACK AT OUTER CHORD SPLICE FITTING, APPROX 0.04 INCH RUNNING FWD. LT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING NR 1 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11. 2 L 7 4 4F A20WE 2002102100074 20021021 00074 NM 2002 10 21 UPS02439339 1 20020816 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 1480 BULKHEAD HOLE NR 1 FOUND CRACK AT FUSE SKIN APPROX 0.06 INCH RUNNING FWD. LT BS 1480 BULKH EAD FUSE SKIN NR 1 BOLT HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11. 2 L 7 4 4F A20WE 2002102100075 20021021 00075 NM 2002 10 21 UPS02439340 1 20020816 A 5320 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 8 FOUND CRACK AT EXTENSION FITTING APPROX 0.06 INCH RUNNING FWD. LT BS 1480 BULKHEAD LONGERON EXTENSION FITTING NR 9 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53 A2390 FIG 11. 2 L 7 4 4F A20WE 2002102100076 20021021 00076 NM 2002 10 21 UPS02439341 1 20020816 A 5320 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 1 FOUND CRACK AT EXTENSION FITTING. LT BS 1480 BULKHEAD LONGERON EXT ENSION FITTING NR 1 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER BS 747-53A2390 FIG 11. 2 L 7 4 4F A20WE 2002102100077 20021021 00077 NM 2002 10 21 UPS02439342 1 20020816 A 5312 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 16 FOUND CRACK AT OUTER CHORD SPLICE FITTING APPROX 0.02 INCH RUNNING I/B. LT BS 1480 BULKHEAD OUTER CHORD FITTING NR 16 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 74 7-53A2390 FIG 11. 2 L 7 4 4F A20WE 2002102100078 20021021 00078 NM 2002 10 21 UPS02439343 1 20020816 A 5312 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 17 FOUND CRACK AT WEB SPLICE PLATE, APPROX 0.020 INCH RUNNING O/B. L T BS 1480 BULKHEAD WEB SPLICE PLATE NR 17 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 F IG 11. 2 L 7 4 4F A20WE 2002102100079 20021021 00079 NM 2002 10 21 UPS02439371 1 20020817 A 5314 65B15069287 KEELBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FUSELAGE KEEL BEAM TOP PANEL INTERNAL HEAVY CORROSION FOUND AT BS 1250-1330. WEB FOUND CORRODED AT LO CATION BS 1250 TO 1330, RBL 8. CORROSION BLEND OUT EXCEEDED SRM LIMIT. WEB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002102100080 20021021 00080 NM 2002 10 21 UPS02439373 1 20020815 A 5412 BULKHEAD BOEING 747 747123 1384873 NM NR 3 NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C CRACK FOUND ON NR 3 NACELLE STRUT REAR MOUNT BULKHEAD AFT O/B WEB APPROX .5 INCH LONG AND STOPPED AT F ASTENER HOLE. NR 3 NACELLE STRUT REAR MOUNT BULKHEAD REPAIRED AS PER RS R54-53-34880 UPS EO NR 747-54-20029. 2 L 7 4 4F A20WE 2002102100081 20021021 00081 NM 2002 10 21 UPS02439374 1 20020814 A 5320 REVEAL BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C RT BS 2231 FRAME Y STR 24 & STR 25 FOUND 2EA FASTENER HOLES CRACKED AT REVEAL. RT BS 2231 FRAME BETWE EN STR 24R TO STR 25R 2EA FASTENER HOLES CRACKED AT REVEAL REPAIRED AS PER SRM 53-10-04 FIGURE 115. 2 L 7 4 4F A20WE 2002102100082 20021021 00082 NM 2002 10 21 2002F00947 1 20020703 A 5320 65453132 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED, AT STATION 950E, RIGHT SIDE AT STRINGER 8R. (M) 2 L 7 3 4F A3WE 2002102100083 20021021 00083 NM 2002 10 21 2002F00948 1 20020703 A 5320 65453132 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CLIP CRACKED, AT STATION 950F, RIGHT SIDE AT STRINGER 2R. (M) 2 L 7 3 4F A3WE 2002102100084 20021021 00084 NM 2002 10 21 2002F00949 1 20020703 A 5753 6521631143 STRUCTURE BOEING 727 727222 1384073 NM T/E FLAP GOUGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND LEFT WING OUTBOARD FORE FLAP INBOARD UPPER SKIN GOUGED AND PUNCTURED, AT WBL 307. (M) 2 L 7 3 4F A3WE 2002102100085 20021021 00085 NM 2002 10 21 2002F00950 1 20020703 A 5753 6521631143 SKIN BOEING 727 727222 1384073 NM T/E FLAP CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND LEFT OUTBOARD FORE FLAP LEADING EDGE SKIN CRACKED, EXTENDING FROM A PREVIOUS REPAIR DOUBLER, AT WLB 44 5. (M) 2 L 7 3 4F A3WE 2002102100086 20021021 00086 NM 2002 10 21 2002F00951 1 20020703 A 5753 SKIN BOEING 727 727222 1384073 NM T/E FLAP GOUGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND LEFT WING INBOARD FORE FLAP UPPER SKIN DEEPLY GOUGED, AT WBL 230. (M) 2 L 7 3 4F A3WE 2002102100087 20021021 00087 NM 2002 10 21 2002F00952 1 20020703 A 5753 6521631143 PAN BOEING 727 727222 1384073 NM T/E FLAP CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND LEFT WING OUTBOARD FORE FLAP LOWER SURFACE PAN CRACKED, AT OUTBOARD SEQUENCE CARRIAGE ATTACH FITTING, WLB 445. (M) 2 L 7 3 4F A3WE 2002102100088 20021021 00088 NM 2002 10 21 2002F00953 1 20020703 A 5730 FAIRING BOEING 727 727222 1384073 NM LT WING CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND LEFT WING OUTBOARD MID FLAP, OUTBOARD JACK SCREW FAIRING CRACKED. (M) 2 L 7 3 4F A3WE 2002102100089 20021021 00089 WP 2002 10 21 2002F00954 1 20020514 A 5320 TIE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND FORWARD CARGO COMPARTMENT LOWER GALLEY (BELOW FRAME LEVEL) FRAME TIE CORRODED, BOTH SIDES FORWARD AND AFT, BETWEEN LONGERONS 43R AND 44R, STATION 840. (M) 2 L 7 3 4F A22WE 2002102100090 20021021 00090 WP 2002 10 21 2002F00955 1 20020522 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CABIN SEAT TRACK CORRODED AT STATION 840 TO 879, LBL 28. (M) 2 L 7 3 4F A22WE 2002102100091 20021021 00091 WP 2002 10 21 2002F00956 1 20020603 A 5320 102512RN3 WEB DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND WEB UNDER RIGHT OUTBOARD SEAT TRACK CORRODED AT STATION 1902, ON THE UNDERSIDE. (M) 2 L 7 3 4F A22WE 2002102100092 20021021 00092 WP 2002 10 21 2002F00957 1 20020513 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND FORWARD CARGO COMPARTMENT MAIN CABIN SEAT TRACK CORRODED. AS VIEWED FROM FORWARD CARGO COMPARTMENT, S TATION 808 TO 824, RBL 28. (M) 2 L 7 3 4F A22WE 2002102100093 20021021 00093 WP 2002 10 21 2002F00958 1 20020521 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON LONGERON 44L, AT STATION 879, APPROXIMATELY 13 INCHES LONG. (M) 2 L 7 3 4F A22WE 2002102100094 20021021 00094 NM 2002 10 21 USAABB02139 1 20020822 A 3350 232T41052 LIGHT BOEING 767 7672B7 1385107 NM COCKPIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 651US 24764 PHL - COCKPIT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A1NM 2002102100095 20021021 00095 NM 2002 10 21 USAABB02140 1 20020823 A 3350 8100022601 LIGHT BOEING 767 7672B7 1385107 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 656US 26847 PHL - FOUND EMERGENCY FLOOR LIGHTS ON LEFT SIDE FROM ROW 18 THROUGH 26 INOPERATIVE. MAINTENANCE FOUND THE FLOOR PATH LI GHTING DISCONNECTED AT ROW 25 AND RECONNECTED IT. (M) 2 L 7 2 4F RT A1NM 2002102100096 20021021 00096 NM 2002 10 21 USAABB02145 1 20020830 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002102100097 20021021 00097 NM 2002 10 21 USAABB02146 1 20020829 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 602AU 22196 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002102100098 20021021 00098 NM 2002 10 21 USAASB02159 1 20020824 A 3350 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 350US 23553 SYR - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHT, ON SEAT 5C, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE E VACUATION LIGHT ASSEMBLY ON SEAT 5C. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002102100099 20021021 00099 NM 2002 10 21 USAASB02160 1 20020824 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 780AU 24997 CLE - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHTS, AT THE FORWARD SERVICE AND MAIN ENTRY DOOR, WOULD NOT DISARM/RESET . MAINTENANCE REMOVED AND REPLACED THE FORWARD LEFT CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002102100100 20021021 00100 NM 2002 10 21 USAASB02165 1 20020829 A 3350 1012623 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 504AU 23379 PHL - MAINTENANCE FOUND THE AISLE EMERGENCY EXIT LIGHT AT SEAT ROW 10, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002102100101 20021021 00101 NM 2002 10 21 UPS02439375 1 20020816 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FUSELAGE - AFT CARGO DOOR AFT CUTOUT FOUND PREVIOUSLY TRIMMED SKIN AT STA 1920 BETWEEN S39R-S40R. FUS ELAGE AFT CARGO DOOR AFT CUTOUT AT STA 1920 BETWEEN S39R-S40R SKIN REPAIR AS PER SRM 53-30-03 FIG 17. 2 L 7 4 4F A20WE 2002102100102 20021021 00102 NM 2002 10 21 UPS02439376 1 20020815 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT LG W/W O/B BS 1438 WEB LWR END ADJACENT OVERWING LONGERON I/B AREA HEAVY CORROSION FOUND. CORROSIO N BLEND OUT EXCEEDED SRM LIMIT, FRAME WEB REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2002102100103 20021021 00103 NM 2002 10 21 UPS02439377 1 20020816 A 5330 SKIN PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C W/W KEEL BEAM RT ATTACHED FIXED PANEL AT BS 1438-1464 WL 91 FOUND PANEL OUTER SKIN SURFACE HAS CORRODE D SURROUNDING PANEL EDGE AREA AND PANEL DOOR HINGE CUTOUT AREA. CORROSION BLEND OUT EXCEEDED SRM LIMIT, FIXED PANEL REP LACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2002102100104 20021021 00104 NM 2002 10 21 QXEA0201515 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX- LEFT HAND INBOARD SEAT TRACK NR 4 BOTTOM CHAFED APPROXIMATELY 12 INCHES BY TRACK COVER AT X291.00. REPLACED SEAT T RACK. 2 H 7 2 4T RT A13NM 2002102100105 20021021 00105 NM 2002 10 21 QXEA0201516 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 CORROSION IN TOP AND BOTTOM AT SEAT ATTACH AREA APPROXIMATELY X280.00. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100106 20021021 00106 NM 2002 10 21 QXEA0201517 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA APPROXIMATELY X267.00. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100107 20021021 00107 NM 2002 10 21 QXEA0201518 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND INBOARD SEAT TRACK NR 7 DRIP FACE RECEPTACLE HOLE DAMAGED PIECES BROKEN OUT AT X312.00. REPLACED NR 7 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100108 20021021 00108 NM 2002 10 21 QXEA0201519 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 OUTBOARD FLANGE CORROSION AROUND TWO FASTENER RECEPTACLES AT X312. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100109 20021021 00109 NM 2002 10 21 QXEA0201520 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 OUTBOARD FLANGE CORROSION AROUND FASTENER RECEPTACLE, APPROXIMATELY X297.00. RE PLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100110 20021021 00110 NM 2002 10 21 QXEA0201521 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 OUTBOARD FLANGE CORROSION AROUND FASTENER RECEPTACLE, APPROXIMATELY X285.00. RE PLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100111 20021021 00111 NM 2002 10 21 QXEA0201522 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 OUTBOARD FLANGE CORROSION AROUND FASTENER RECEPTACLE AT APPROXIMATELY X270.00. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100112 20021021 00112 NM 2002 10 21 QXEA0201523 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 OUTBOARD FLANGE CORROSION AROUND TWO FASTENER RECEPTACLES AT APPROXIMATELY X252. 00. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100113 20021021 00113 NM 2002 10 21 QXEA0201524 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 OUTBOARD FLANGE CORROSION AROUND FASTENER RECEPTACLE AT APPROXIMATELY X240.00. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100114 20021021 00114 NM 2002 10 21 QXEA0201525 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 OUTBOARD FLANGE CORROSION AROUND FASTENER RECEPTACLE AT APPROXIMATELY X228.00. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100115 20021021 00115 NM 2002 10 21 QXEA0201526 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 BRACKET ON OUTBOARD FLANGE CORRODED FROM X201.00 TO X222.00. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100116 20021021 00116 NM 2002 10 21 QXEA0201527 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 OUTBOARD FLANGE CORROSION AROUND RIVETS FROM X201.00 TO X222.00. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100117 20021021 00117 NM 2002 10 21 QXEA0201528 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 OUTBOARD FLANGE CORROSION AT X198.00. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100118 20021021 00118 NM 2002 10 21 QXEA0201529 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 5 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X518.00. REPLACED NR 5 SEAT TRA CK. 2 H 7 2 4T RT A13NM 2002102100119 20021021 00119 NM 2002 10 21 QXEA0201530 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 5 BOTTOM CHAFED APPROXIMATELY 12 INCHES BY FLOOR TRIM AT X510.00. REPLACED NR 5 S EAT TRACK. 2 H 7 2 4T RT A13NM 2002102100120 20021021 00120 NM 2002 10 21 QXEA0201531 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 5 TOP CORROSION APPROXIMATELY 12 INCHES AT X488.00. REPLACED NR 5 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100121 20021021 00121 NM 2002 10 21 QXEA0201532 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 5 BOTTOM CHAFED APPROXIMATELY 12 INCHES BY FLOOR TRIM AT X475.00. REPLACED NR 5 S EAT TRACK. 2 H 7 2 4T RT A13NM 2002102100122 20021021 00122 NM 2002 10 21 QXEA0201533 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 5 BOTTOM CORROSION AT SEAT ATTACH AREA APPROXIMATELY X469.00. REPLACED NR 5 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100123 20021021 00123 NM 2002 10 21 QXEA0201534 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 5 APPROXIMATELY 12 INCHES OF BOTTOM CHAFED BY FLOOR TRIM AT X445.00. REPLACED NR 5 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102100124 20021021 00124 NM 2002 10 21 UPS02439378 1 20020831 A 5320 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT LG W/W OVERWING LONGERON SPLICE FITTING ATTACH SIX MOUNT BOLTS, NUTS AND BOLTS FOUND CORROSION AFT ER FITTING REMOVE AT STA 1355. LT LG W/W OVERWING LONGERON SPLICE FITTING ATTACH SIX MOUNT BOLT HOLE OVERSIZED. NDT IN SPECTED NO CRACK & NO COR. ALL SIX BOLTS & NUTS REPLACED AS PER BOEING DWG 65B15254 SHT 2, SRM 51-30-03 FIG 1. 2 L 7 4 4F A20WE 2002102100125 20021021 00125 NM 2002 10 21 UPS02439379 1 20020812 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FUSELAGE - AFT CARGO DOOR FWD CUTOUT SKIN PORTION TRIMMED OFF AT BS 1810 STR 39R-40R. FUSELAGE SKIN R EPAIRED AS PER SRM 53-30-03 FIG 19. 2 L 7 4 4F A20WE 2002102100127 20021021 00127 NE 2002 10 21 UPS02439437 2 20020913 A 7230 PLUG BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE NR 3 ENGINE LOOSE A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 SO 01 525UP 21939 702279 INSPECTION TYPE:N/A AIR TURNBACK ENG FIRE NR 3 ENGINE. FOUND BORESCOPE PLUG AT 2 O'CLOCK POSITION ON DIFFUSER CASE LOOS E. REINSTALLED PLUG AND SAFETIED IAW 72-00-00. RAN NR 3 ENGINE WITH NO RISE IN TEMP. A/C RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 2002102100128 20021021 00128 NM 2002 10 21 UPS02439485 1 20020909 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 320 BL 0 - RBL 1 FLOORBEAM LOWER CHORD CRACKED. FLOORBEAM LOWER CHORD CRACKED AREA REPAIRED AS PER SRM 51-40-04 FIG 2. 2 L 7 4 4F A20WE 2002102100141 20021021 00141 NM 2002 10 21 DHL2002741015 1 20021016 A 2910 401605682 CAP BOEING 727 7272Q9 138448M NM A DHLA A O UNSCHED LANDING OTHER K FLUID LOSS CL CLIMB 1 SO 01 741DH 21931 1) "A" SYSTEM HYDRAULIC FAILURE AFTER TAKE-OFF, "0" QUANTITY FOLLOWED ABNORMAL PROCEDURE.2) INSPECTED & FOUND ELEVATOR FEEL COMPUTER "A" SYSTEM FILTER CAP CRACKED. R & R "A" SYSTEM CAP & SEAL PER M/M 27-30-101. INSPECTED #1 & #2 ENGINE HY DRAULIC PUMP CASE DRAIN FILTERS IAW M/M 29-41-11. NO PARTICLES FOUND OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2002102100144 20021021 00144 WP 2002 10 21 CA021007011 1 20020913 A 5610 34031103017 WINDSHIELD CVAC 440 440 2422902 WP ALLSN 501D 501D13 03004 GL COCKPIT FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) ON CLIMB OUT OF YUL, LT WINDSHIELD SHATTERED. AIRCRAFT DEPRESSURIZED AND CAME BACK TO MONTREAL. UNABLE TO ESTABLI SH THE REASON FOR WINDSHIELD SHATTERED. WINDSHIELD REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4R 4 T 6A6 E282 2002102100145 20021021 00145 WP 2002 10 21 CA021007012 1 20020918 A 2910 7936907530 LINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE HYD SYSTEM CRACKED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) ON A TURN AROUND IN THE MECHANIC FOUND AN HYDRAULIC LEAK IN THE WHEEL WELL. HE DECIDED TO REPLACE THE RIGID LINE W ITH A TEMPORARY FLEX HYDRAULIC LINE AS PER M.M. 20-12-04. THE MECHANIC CHOOSE THE WRONG TYPE OF LINE (MEDIUM PRESS LINE INSTEAD OF HIGH PRESS LINE).THE AIRCRAFT LEFT WITHOUT ANY PROBLEM. ON DEPARTURE FOR THE FLIGHT FROM YYZ TO YVR ON CLIMB THE PILOT REMARKS A TOTAL LOST OF HYDRAULIC QUANTITY ON THE LT SYSTEM. TURN AROUND AND LAND BACK IN YYZ. THE MECHANIC FO UND THE FLEX LINE BURST. PROPER FLEX LINE INSTALLED AIRCRAFT RETURN TO SERVICE. THE FLEX LINE WAS REPLACED WITH RIGID LI NE ON SEPTEMBER 19, 2002. 2 L 7 2 4F 4 F RT A6WE E9NE 2002102100146 20021021 00146 WP 2002 10 21 UPS02839329 1 20020901 A 5720 97532937 ANGLE DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 LEFT WING L/E VERTICAL ATTACH ANGLE IS CRACKED AT LOWER END AT XS 250. REMOVED, FABRICATED AND REPLA CED ANGLE IAW DWG 9753293, AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2002102100148 20021021 00148 WP 2002 10 21 UPS02839330 1 20020905 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XS 484.895. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMIN ATES CRACK, FABRICATED AND INSTALLED ANGLE DOUBLERS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002102100149 20021021 00149 WP 2002 10 21 UPS02839331 1 20020819 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 REMOVE DOUBLER ON THE L2 DOOR LOWER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 18 AT LONG 21L. REMOVED EXISTING DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW DC8-5330-17427-A, SRM 53-2-0 FIG 18, AND SAA SK 708-146. 2 L 7 4 4F RT 4A25 2002102100150 20021021 00150 WP 2002 10 21 UPS02839332 1 20020819 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 REMOVE DOUBLER ON THE L2 DOOR LWR AFT CORNER AND REPAIR PER DC8 SRM 53-2-0, FIG18 AT STA 1660 LONG 21 L. REMOVED EXISTING DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACK AT CUT OUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER , AND FILLER IAW SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2002102100151 20021021 00151 EA 2002 10 21 CA021008001 1 20020915 A 3244 0274380 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT MLG NR 3 FAILED W A L UNSCHED LANDING ABORTED APPROACH D INFLIGHT SEPARATION CL CLIMB 1 CA (CAN) AT APPROXIMATELY VR, HEARD AND FELT A LOUD BANG IN THE NOSE AREA. DURING CLIMB CALLED TOWER AND ASKED TO CHECK THE RUNWAY. SENT AN INSPECTION VEHICLE OUT AND FOUND TIRE REMENANTS. NOTIFIED THE F/A AND PAX. ASKED THE EMERGENCY EQ UIMPMENT STANDING BY. DURING APPROACH, PUT GEAR DOWN AND RECEIVED A DISAGREE MESSAGE. MISSED APPROACH. MESSAGE CLEARED AFTER 30 SEC, LANDING WAS UNEVENTFUL. 2 L 7 2 4F 4 F RT A21EA E15NE 2002102100152 20021021 00152 NM 2002 10 21 CA021008003 1 20021003 A 2121 732591D FAN BOEING 767 7673Y0 NM PWA 4060 PW4060 52119 NE CABIN FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) STRONG ELECTRICAL BURNING ODOR NOTICED NEAR RT SIDE OF P5 OVERHEAD PANEL. LOST LOWER EICAS PANEL APPROX 1 MIN LATE R. F/A ALSO NOTICED BURNING ODOR IN FRONT GALLEY. CHANGED EQUIPMENT COOLING EXT. FAN PER AMM. 2 L 7 2 4F 4 F RT A1NM E24NE 2002102100153 20021021 00153 WP 2002 10 21 UPS02839349 1 20020822 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 RT T-1 DOOR AFT LOWER CORNER HAS A DOUBLER AT STA 440.000. REMOVED DOUBLER, NDT HFEC NO CRACK NOTED AROUND CUTOUT. FABRICATED DOUBLER, TRIPLER, AND FILLER IAW EO DC8-5330-17436-A AND SK-708-650. INSTALLED DOUBLER, TRIP LER, AND FILLER AT RT STA 440.0 IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102100154 20021021 00154 WP 2002 10 21 UPS02839350 1 20020827 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1400 LONG 30L EXTERNAL DOUBLER, CLASSIFIED CATERGORY D, IAW DC8-5330. REMOVED EXTERNAL DOUBLER A T STA 1400 LONG 30L. FABRICATED INTERNAL AND EXTERNAL DOUBLERS IAW SRM 53-2-1 FIG 7, INSTALLED INTERNAL AND EXTERNAL DO UBLERS IAW SRM 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002102100155 20021021 00155 WP 2002 10 21 UPS02839357 1 20020819 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 FRAME STA 55 CRACKED AT SUPPORT ROD ATTACH FITTING LONG 24R. CUT OUT DAMAGED FRAME IAW SRM 53-2-0 FI G 2. FABRICATED FRAME AND ANGLE REPAIR IAW SRM 53-2-0 FIG2, INSTALLED FRAME ANGLE DOUBLER IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102100156 20021021 00156 WP 2002 10 21 UPS02839359 1 20020905 A 5730 TRIPLER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 LEFT WING CENTER L/E LOWER INTERNAL TRIPLER IS CRACKED AT STA XOLDI 6.225. REMOVED INTERNAL DOUBLER AND TRIPLER AT WING STA XOLDI 6.225 IAW SRM 51-1-21, FABRICATED REPAIR DOUBLER AND TRIPLER IAW DC8 DRAWING 5769589. INS TALLED REPAIR DOUBLER AND TRIPLER AT STA XOLDI 6.225 IAW SRM 51-1-20D, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002102100157 20021021 00157 WP 2002 10 21 UPS02839361 1 20020819 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 FRAME STA 55 CRACKED AT SUPPORT ROD BRACKET LONG 24L. CUT OUT DAMAGED AREA, REMOVED CRACKED SHEAR TI E AT STA 55 LONG 24L. FABRICATED AND INSTALLED FRAME REPAIR SECTION AND SHEAR TIE IAW SRM 53-2-0, SRM 53-2-0 FIG 2, AND SRM 53-3-1. 2 L 7 4 4F RT 4A25 2002102100158 20021021 00158 WP 2002 10 21 UPS02839362 1 20020821 A 5730 576960035 DOUBLER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 597.5. REMOVED, FABRICATED AND REPLAC ED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2002102100159 20021021 00159 WP 2002 10 21 UPS02839364 1 20020825 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 C-PIT DOOR SKIN IS CRACKED AND GOUGED NEAR LOWER FWD CORNER APPROX STA 1180 AT LONG 32R. CUTOUT DAMA GED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 52-2-0 FIG 4, 52-4-1. 2 L 7 4 4F RT 4A25 2002102100160 20021021 00160 WP 2002 10 21 UPS02839385 1 20020906 A 5320 DC85780071 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:N/A UPPER INBD ANGLE CRACKED LT MLG WW. REMOVED ANGLE SENT TO MANUFACTURING WP 70050 LOCATED AND DRILLE D NEW ANGLE W/CREF 18126 9-5-02 INSTALLED PER DC8 SRM 51-1-20 & 51-1-21. 2 L 7 4 4F RT 4A25 2002102100162 20021021 00162 EA 2002 10 21 CA021009001 1 20021008 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 11621 (CAN) CREW REPORTED THE LEFT WINDSHIELD SHATTERED WHILE AIRCRAFT WAS ON GROUND, AT GATE.MAINTENANCE SENT TEAM TO ELP. RE MOVED AND REPLACED THE LT WINDSHIELD. TSN/CSN/TSO AIRCRAFT HOURS: 11621.9 AIRCRAFT CYCLES: 10677 COMPONENT DATA THE SAME . DATA I HAVE INDICATES THIS IS ORIGINAL EQUIPMENT. 2 L 7 2 4F 4 F RT A21EA E15NE 2002102100164 20021021 00164 EA 2002 10 21 SWIA200211333 1 20020831 A 5415 BRACKET CNDAIR CL600 CL6002B19 1900309 EA PYLON LE CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 FOUND LEFT ENGINE PYLON LEADING EDGE LOWER ATTACH BRACKET CRACKED DURING C CHECK INSPECTION. FITTED AND INSTALLED NEW R IB IAW CRJ SRM 51-40-11, 51-42-06. 2 L 7 2 4F RT A21EA 2002102100165 20021021 00165 EU 2002 10 21 MALA020611 1 20021020 A 3350 6104789 BATTERY PACK SAAB SF340 SF340A 7850100 EU A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 106XJ 340A106 DURING LC1, EMERGENCY LIGHTS 41LN, 42LN, 43LN, 4LN, AND 3LN WOULD NOT TURN ON. MAINTENANCE REPLACED 24LN, EMERGENCY BA TTERY PACK pn 610478-9 SN/OFF 1948, SN/ON ELB018 IAW TASK CARD 335002 AND OPS CHECKED GOOD. 2 L 7 2 4T RT A52EU 2002102100166 20021021 00166 NM 2002 10 21 AWXA200201019 1 20021005 A 5315 69434771 CHANNEL BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 0 0 25400 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/2" CRACK WAS FOUND ON FLOOR SUPPORT IN THE AFT CARGO COMPARTMENT AT BS 767 T O BS 787, STR 25 R/H. MAINTENANCE REMOVED THE CRACKED FLOOR SUPPORT AT BS 767 TO BS 787, STR 25 R/H; FABRICATED A NEW RE PLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 5, 10, AND SRM 51-40-05, PG. 4, FIG. 5. 2 L 7 2 4F RT A16WE 2002102100167 20021021 00167 NM 2002 10 21 AWXA200201022 1 20021020 A 2120 69715591 FILTER BOEING 737 7373G7 1384595 NM BS 261 CONTAMINATED A AWXA K NONE O OTHER LD LANDING 1 WP 28 155AW 0 0 23777 LAX - FUMES - FLT 0702 - UPON LANDING AT LAX EN ROUTE FROM PHX THE FLIGHT ATTENDANT IN THE AFT CABIN REPORTED SMELLING F UMES WHEN THRUST REVERSERS WERE DEPLOYED. FUMES WERE BAD ENOUGH TO CAUE A BURNING SENSATION OF THE EYES. AFT CABIN IS AL SO VERY HOT, EVEN WITH BOTH PACKS IN HIGH CABIN WOULD NOT COOL DOWN. MAINTENANCE TROUBLESHOT AND FOUND THE PASSENGER CAB IN SENSE FILTER CONTAMINATED WITH DEBRIS. CLEANED FILTER AND OPERATED BOTH PACKS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002102100168 20021021 00168 NM 2002 10 21 AWXA200201023 1 20021002 A 5312 65C375903 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 0 0 25400 MCN - MAJOR REPAIR - DURING C-12 CHECK MULTIPLE CRACKS (5 EACH) WERE FOUND ON BULKHEAD WEB BS 178 AT RBL 4.7 WL 200.375 - WL 201.5, LBL 4.7 WL 200.375 - WL 201, RBL 6.7 WL 212 - WL 212.675, RBL 4.7 WL 212 - WL 212.375, LBL 6.7 WL 211.75 - W L 212.5. MAINTENANCE CUTOUT DAMAGE ON WEB BS 178 AT RBL 4.7 WL 200.375 - WL 201.5, LBL 4.7 WL 200.375 - WL 201, RBL 6.7 WL 212 - WL 212.675, RBL 4.7 WL 212 - WL 212.375, LBL 6.7 WL 211.75 - WL 212.5; PERFORMED HFEC INSPECTION OF CUTOUT AREA S TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER, A FILLER, AND 6 EACH SHIMS; INSTALLED REPAIR PARTS IAW B737-30 0 SRM 53-10-08, FIG. 211, PG. 287-288. 2 L 7 2 4F RT A16WE 2002102100169 20021021 00169 NM 2002 10 21 AWXA200201025 1 20021004 A 5320 65176846 ATTACH ANGLE BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 0 0 22651 YVR - MAJOR REPAIR - DURING C-20 CHECK A 3/4" CRACK WAS FOUND ON ATTACH ANGLE AT BS 360, STR 11 L/H, JUST AFT OF L-1 DOO R. MAINTENANCE REMOVED THE DAMAGED ATTACH ANGLE AT BS 360, STR 11 L/H; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTAL LED REPAIR PART IAW DWG 65-17684, AND SRM 51-30-2, PG. 5. 2 L 7 2 4F RT A16WE 2002102100170 20021021 00170 NM 2002 10 21 AWXA200201026 1 20021004 A 5311 654581011 FRAME BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 0 0 22651 YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/4" CRACK WAS FOUND ON FRAME AT BS 312, BETWEEN STR 5 - STR 6 L/H. MAINTENANCE STOP DRILLED CRACK AT BS 312, BETWEEN STR 5 - STR 6 L/H; PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FAB RICATED A FRAME REPAIR DOUBLER; AND INSTALLED REPAIR PART IAW B737-200 SRM 51-40-3, FIG. 1. 2 L 7 2 4F RT A16WE 2002102100171 20021021 00171 NM 2002 10 21 AWXA200201028 1 20021003 A 5330 2024T3063 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 0 0 22651 YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/4" CRACK WAS FOUND ON FUSELAGE SKIN OF R-2 DOOR UPPER HINGE CUTOUT AT FORWARD UPPER CORNER BS 957.5, WL 240. MAINTENANCE TRIMMED OUT R-2 DOOR UPPER HINGE CUTOUT AT FORWARD UPPER CORNER BS 957.5, WL 240 BY .040" AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALL ED REPAIR PARTS IAW B737-200 SRM 53-30-3, FIG. 21A. 2 L 7 2 4F RT A16WE 2002102100173 20021021 00173 SO 2002 10 21 C2XA02TY153 1 20021021 A 5510 14521904412 SUPPORT EMB 145 EMB145LR 3260212 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 TYS DURING A SCHEDULED 2-C INSPECTION THE R/H HORIZ. STAB HINGE SUPPORTS WERE FOUND GOUGED INSIDE THE PIVET BUSHING MOU NTS. MAINT. MEASURED INBD/OTBD PIVOT BUSHING HOLES,REAMED BOTH TO 1.640" ALLODINED BOTH HOLES AND INSTALL BUSHINGS IAW E MB 135/145 CPM 51-21-04,EC 5510-01043 AND GST 3018/02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2 L 7 2 4T RT T00011AT 2002102200001 20021022 00001 NM 2002 10 22 CA021009024 1 20021007 A 5330 SKIN BOEING 737 7372Q9 138448M NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) A 4 INCH CRACK,RUNNING FORE & AFT WAS FOUND DIRECTLY ABOVE STRINGER 16L AT STATION 520. CRACK REPAIR ACCOMPLISHED AS PER 737 SRM 53-30-3. 2 L 7 2 4F 4 F A16WE E2EA 2002102200002 20021022 00002 CE 2002 10 22 CA021009025 1 20020930 A 3260 CONNECTOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA DOWNLOCK SWITCH LOOSE W A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 CA (CAN) WHILE EXTENDING THE LANDING GEAR DURING AN APPROACH THE FLIGHT CREW NOTICED NO GREEN INDICATION FOR THE NOSE LANDI NG GEAR TO BE IN THE DOWN AND LOCKED POSITION. AFTER 2 MORE APPROACHES AND HAVING THE SAME RESULTS, THE AIRCRAFT WAS THE N RETURNED TO AND LANDED SAFELY. UPON INSPECTION MAINTENANCE FOUND A LOOSE WIRE AT THE NOSE GEAR DOWN LOCK SWITCH CONNEC TOR PLUG. THE WIRE WAS RE-SECURED, GEAR SWINGS CARRIED OUT AND THE SYSTEM TESTED SERVICEABLE. 2 L 7 2 4T 4 T RT A24CE E4EA 2002102200003 20021022 00003 SW 2002 10 22 CA021009029 1 20020918 A 6120 CONNECTOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL SRL COMPUTER DIRTY W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER DEPARTURE FROM AIRPORT THE PILOT OBSERVED ABNORMAL/FLUCTUATING TORQUE AND EGT INDICATIONS FOR LT ENGINE. THE AIRCRAFT RETURNED TO BASE. WIRING CONNECTOR PLUG FOR SRL COMPUTER WAS CLEANED AND SRL COMPUTER WAS RE-CALIBRATED PER DA TA SHEET, RUN-UP AND TEST FLIGHT CARRIED OUT AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002102200004 20021022 00004 SW 2002 10 22 CA021009030 1 20020927 A 3251 CIRCUIT BREAKER SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL NLG STEERING FAILED W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) AFTER LANDING THE NOSE WHEEL STEERING FUNCTION FAILED WHILE ATTEMPTING TO TAXI. THE AIRCRAFT WAS INSPECTED AND THE PROBLEM WAS TRACED TO A FAULTY CIRCUIT BREAKER WHICH HAD FAILED TO SUPPLY POWER TO POWER STEERING UNIT. CIRCUIT BREAKER WAS REPLACED AND SYSTEM FUNCTIONED NORMALLY ON GROUND TEST. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002102200005 20021022 00005 EA 2002 10 22 CA021010001 1 20021007 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WINDSHIELD FOUND CRACK AFTER FLIGHT. A/C HAD ACCUMULATED 18778 HOURS AND 14803 CYCLES. WINDHIELD WAS REMOVED AND R EPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002102200006 20021022 00006 EU 2002 10 22 CA021010002 1 20021009 A 3246 AHA1481 WHEEL BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACK FOUND ON INNER WHEEL HALF BELOW ONE TENNON APPROXIMATELY 2 INCHES IN LENGTH AROUND BOTTOM OF TENNON. (CRACK NOT NEAR A FUSE PLUG HOLE) RECTIFICATION: INNER WHEEL HALF WAS SCRAPPED. THIS INFORMATION HAS BEEN SENT TO DUNLOP. SUPPL EMENTAL INFO WILL BE ADDED WHEN THE RESPONSE FROM DUNLOP IS RECEIVED. 2 H 7 4 4F 4 F A49EU E6NE 2002102200009 20021022 00009 NM 2002 10 22 S02427035 1 20020606 A 2700 65B1018918 CARRIAGE BOEING 747 747400 NM PWA 4056 PW4056 NE TE FLAPS CRACKED W SAJF O OTHER O OTHER TX TAXI/GRND HDL 1 WP 03 28710 CRACKS WERE FOUND IN NR 4 AND NR 7 CARRIAGES DURING THE OVERHAUL. THE CARRIAGE WERE REPAIRED AS PER BOEING'S SUGGESTI ON AND OHM. THE DETAILED OF SHOP FINDINGS AND REPAIRED PROCEDURES WILL BE PROVIDED BY MB SHOP. 2 L 7 4 4F 4 F RT A20WE E24NE 2002102200010 20021022 00010 GL 2002 10 22 2002FA0001185 3 20020925 A 6114 83410 COLLAR BEECH 35 G35 1151516 CE CONT E225 E2258 17015 SO HARTZL HCA2V HCA2V* GL PROPELLER CRACKED B LU4R O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SO 17 34TT D4737 AK1299 GUIDE COLLAR CRACKED DUE TO VIBRATION FROM PROPELLER. BOTH BLADES SLIPPED IN CLAMP CREATING A SPLIT IN ANGLES. 1 L 7 1 3O 3 O A777 E267 5 C P24EA 2002102200021 20021022 00021 EU 2002 10 22 ASOA02246 1 20020423 A 3350 3011001 SIGN AEROSP ATR72 ATR72212 8680945 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 633AS 12918 344 DURING A HANGER INSPECTION, THE LT FORWARD LOWER EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. THE RT EXTERNAL EMERGENCY L IGHT AT THE SERVICE DOOR WAS ALSO FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE EMERGENCY EXIT SI GN ASSEMBLY AND THE EMERGENCY LIGHTING POWER SUPPLY AT ROW 11AB. OPERATIONAL CHECKS GOOD AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A53EU 2002102200022 20021022 00022 SO 2002 10 22 ASOA02247 1 20020425 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE TE FLAP INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 246AS 10271 120100 DURING FLIGHT, CAPTAIN RECEIVED A FLAP CONTROL FAULT. AN EMERGENCY WAS DECLARED AND THE A/C RETURNED, FOR UNEVENTFUL LA NDING. MAINT RANG OUT WIRING AND MEGGED THE WIRING ON THE ENTIRE FLAP SYSTEM, ANNUNCIATOR CIRCUIT AND STALL WARNING CIR CUIT, FROM THE FLAP CONTROL UNIT TO THE ACTUATOR AND FROM THE ANNUNCIATOR TO THE FLAP CONTROL UNIT. NO DEFECTS NOTED. MAINT THEN JACKED UP A/C, INPUT DIFFERENT IN FLIGHT CONFIGURATIONS, AND RAN FLAPS WITH PITOT TEST BOX HOOKED UP. ONLY D EFECT NOTED WAS A VARIANCE IN THE RT OB ACTUATOR WHEN IN THE PARKED POSITION. MAINT REMOVED AND REPLACED THE RT OB FLAP ACTUATOR AND ALSO THE FLAP CONTROL UNIT. AIRCRAFT HAS RETURNED TO SERVICE. THE ACTUATOR WAS DECIDEDLY THE CAUSE OF TH 2 L 7 2 4T 4 T RT A31SO E20NE 2002102200023 20021022 00023 SW 2002 10 22 BSA2002F00000 1 20020917 A 2150 2047556 ACM FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE331* 01514 WP IMPELLER FAILED A BSAA K NONE O OTHER IN INSP/MAINT 1 NM 05 847LS 5521 DC847B AFTER LANDING, SMOKE/OIL MIST FILLED THE CABIN. CREW SHUT DOWN AIRCRAFT AND EVACUATED THE PASSENGER ON THE TAXI WAY. A CM FAILURE. IMPELLER WAS FOUND LOOSE IN THE HOUSING. INITIALLY DEFERRED THE RIGHT BLEED SYSTEM IAW MEL. THE ACM WAS NO T SERVICED ON THE LAST INSPECTION, NOR WERE ANY DEFECTS NOTED DURING THE ROUTINE WING INSP IS A GENERAL VISUAL INSPECTIO N WITH NO DISASSEMBLY REQUIRED. REPLACED ACM, FOUND IMPELLER AND TURBINE END LOOSE IN THE SCROLL HOUSING. 2 L 7 2 4T 3 T RT A18SW E2WE 2002102200024 20021022 00024 SW 2002 10 22 BSA2002F00001 1 20020910 A 5230 HANDLE FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE331* 01514 WP CARGO DOOR OUT OF ADJUST A BSAA K NONE O OTHER IN INSP/MAINT 1 NM 05 160MC 21251 AC733B DURING CRUISE THE ANNUNCIATOR PANEL WARNING LIGHT CAME ON. CREW FOLLOWED EMERGENCY PROCEDURES, DEPRESSURIZED THE A/C AN D CONTINUED TO DESTINATION AT A LOWER ALTITUDE. THE DESTINATION CITY WAS THE CLOSEST AIRPORT. THE CARGO DOOR WARNING L IGHT WENT OUT AFTER APPROXIMATELY 7 MINUTES. STICKING DOOR HANDLE OR CLICK CLACKS, OR INDICATION/ MICROSWITCH ADJUSTME NT. CREW FOUND HANDLE NOT IN THE FULLY CLOSED POSITION. HANDLE WAS CYCLED AND FOUND TO OPERATE NORMALLY. MAINTENANCE INSPECTED, CLEANED AND LUBRICATED CLICK CLACKS AND DOOR HANDLE MECHANISM. 2 L 7 2 4T 3 T RT A18SW E2WE 2002102200025 20021022 00025 CE 2002 10 22 CYM2002F00000 1 20021010 A 3210 21A04503003 PIN CESSNA 206 206H 2073301 CE LYC O540 IO540* 41532 EA MLG CORRODED E CYMA K NONE O OTHER IN INSP/MAINT 1 SO 19 7270C 744 20608051 RETAINING PIN FAILED CAUSING THE SPACER SUPPORTS, AND SHOCK STRUT ASSEMBLIES (RUBBER DONUTS) TO FALL OFF OF THE YOKE ASS EMBLY AS A RESULT OF THE RETAINING PIN FAILURE THE WHEEL WAS PERMITTED TO ENTER THE WHEEL WELL BEYOND ALLOWABLE LIMITS R ESULTING IN THE FLOAT ASSEMBLY TO CONTACT THE SURFACE OF THE RUNWAY. INVESTIGATION REVEALED THE RETAINING PIN TO BE IN A CORRODED/FATIGUED CONDITION. THE MANUFACTURER/HOLDER OF THIS STC SA01185CH HAS STATED THIS PROBLEM HAS PREVIOUSLY OCC URRED AND IS CURRENTLY ADDRESSING THIS PROBLEM. 1 H 7 1 3O 3 O RT A4CE 1E4 2002102200026 20021022 00026 SO 2002 10 22 DF22002F00003 1 20021009 A 7160 554545 CONTROL CABLE PIPER PA44 PA44180 7104402 SO LYC O360 O360* 41514 EA CARB HEAT BROKEN B DF2S K NONE O OTHER IN INSP/MAINT 1 SW 15 187TX 576 4496099 PILOT REPORTED NO RPM DROP WHEN CHECKING RT ENGINE CARBURETOR HEAT DURING RUN UP. TECH FOUND THE CARBURETOR HEAT CONTRO L, BROKEN AT THE CARBURETOR HEAT AIRBOX. THE CABLE WAS BROKEN AT THE POINT WHERE THE THREADED SHAFT IS SWAGED TO THE CA BLE. THE SHROUD THAT GOES AROUND SHAFT WAS NO WERE TO BE FOUND. REPLACED CONTROL CABLE. AIRCRAFT TT: 576.7. ON PREVI OUS 100 HOUR INSPECTION, BOTH ENGINE THROTTLE CONTROLS AND THE RIGHT ENGINE MIXTURE CONTROL WERE REPLACED FOR SIMILAR PR OBLEMS. WHILE THEY HAD NOT FAILED COMPLETELY, THE SHROUDS HAD COME LOOSE AND WERE FLOATING FREELY ALONG THE THREADED SH AFT. AIRCRAFT TT: 424.9. NEED MFG EVALUATION. 1 L 7 2 3O 3 O A19S0 E286 2002102200027 20021022 00027 CE 2002 10 22 DP02002F00000 1 20020904 A 7603 640791A5 CONTROL UNIT BEECH 58 58P 1152744 CE CONT O520 TSIO520WB 17040 SO THROTTLE FAILED B DPOR K NONE O OTHER IN INSP/MAINT 1 NM 07 146Z TJ426 822553R NEW ENGINE INSTALLED FROM FACTORY. ENGINE DRIVER PUMP PRESSURES ADJUSTED IAW MFG MM. ENGINE FUEL FLOWS WOULD NOT REACH SPECIFIED VALUE OF 32.4 TO 34.1 GPH. IAW SD. ENGINE CHT AND TLT HOT. MFG RECOMMEDED INCREASING UNMETERED PRESSURE 5 P SI BEYOND THEIR PUBLISHED VALUES. NO AFFECT, MFG STATED NOT THEIR PROBLEM, TO CALL THEIR SUPPLIER. SUPPLIER SAID FLY A C TO SUPPLIER DESTINATION FOR REPAIR (FIRE FIGHTING AIRCRAFT) NOT FEASIBLE. 1 L 7 2 3O 3 O A23CE E8CE 2002102200028 20021022 00028 CE 2002 10 22 FPI2002F00010 1 20021001 A 3233 98820154 ACTUATOR CESSNA 210 T210N 2073456 CE CONT O520 TSIO520* 17040 SO MLG CRACKED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 6622N 11564 21063125 BOTH MAIN GEAR ACTUATORS FOUND CRACKED. IAW SB ACTUATOR INSPECTION. 1 H 7 1 3O 3 O 3A21 E8CE 2002102200029 20021022 00029 CE 2002 10 22 FPI2002F00011 1 20021001 A 3233 98820154 ACTUATOR CESSNA 210 210N 2073453 CE CONT O520 IO520* 17032 SO MLG CRACKED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 5229A 14625 21063320 RT MAIN GEAR ACTUATOR CRACKED IN FLIGHT. LANDING GEAR WOULD NOT EXTEND OR RETRACT. LANDED AIRCRAFT, GEAR UP. 1 H 7 1 3O 3 O 3A21 E5CE 2002102200030 20021022 00030 WP 2002 10 22 GTIA021029 1 20020915 A 5310 WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE DOOR JAMB CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 PAX CABIN, STA 200 LBL 58 INCHES HAS CORROSION ON SURFACE WEB (AFT LOWER DOOR JAMB ARE L-1 DOOR) REMOVED WEB STA 200 TO 213 (FOUND TO OUT OF LIMITS) AND CORRODED SECTION OF CUSP FABRICATED NEW WEB, UPPER CUSP AND UPPER CUSP SPLICER INSTALL ED WEB, CUSP AND CUSP SPLICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102200031 20021022 00031 WP 2002 10 22 GTIA021030 1 20020915 A 5320 ANGLE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE THRESHOLD CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 38447 49415 PASSENGER FORWARD ENTRANCE (L1 DOOR) THRESH HOLE SUPPORT ANGLE IS CORRODED. REMOVED DAMAGED SECTION. FABRICATED REPAIR FILLER AND ANGLE INSTALLED REPAIR FILLER AND ANGLE. 2 L 7 2 4F 4 F RT A6WE E2EA 2003021400133 20030214 00133 WP 2003 2 14 GTIA021031 1 20020917 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - AFT FUSELAGE UNPRESSURIZED AREA, RIGHT SIDE, FRAME AT STATION CANT 1463. CRACKED AT APPROX LONGERON 18R. STOP DR ILLED CRACK, FABRICATED DOUBLER AND INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A6WE 2002102200032 20021022 00032 WP 2002 10 22 GTIA021032 1 20020930 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 MAIN CABIN FLOOR STA 1287-1039 BL 0, INTERCOASTAL IS CRACKED FROM AFT EDGE FORWARD INTO LIGHTENING HOLE. REMOVED DAMAGE D INTERCOSTAL. FABRICATED A NEW INTERCOSTAL. INSTALLED INTERCOSTAL. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102200033 20021022 00033 EA 2002 10 22 SWIA200211342 1 20020913 A 5420 PYLON CNDAIR CL600 CL6002B19 1900309 EA LEFT, FS 605 CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 LEFT PYLON AT FS 605 IS CRACKED AT THE BOTTOM SIDE. FOUND DURING A C CHECK INSPECTION. REMOVED BLEED AIR LINES AND WIR ING. FIT AND INSTALLED RIB IAW CRJ SRM 51-40-11, 51-42-06 & SRM 51-23-00. REINSTALL BLEED AIR DUCT IAW CRJ MM 30-21-01 . 2 L 7 2 4F RT A21EA 2002102200034 20021022 00034 NM 2002 10 22 DL72S021198 1 20021015 A 5330 65545826 SKIN BOEING 727 727232 1384082 NM FS 1080, S-4R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 FUSELAGE / SKIN / FS 1070-1090 / STRG. 4R / SKIN LAP JOINT: CRACK REPAIR LFEC INSPECTIONS OF THE STRINGER 4R SKIN LAP JOINT REVEALED A CRACK INDICATION. INTERNAL MFEC INSPECTION DETERMINED A SINGLE CRACK IN THE LOWER SKIN AT THE LOWER FASTENER ROW BETWEEN FS 1070 & 1090. THE CRACK WAS REMOVED WITH A CUTOUT IN THE LAP JOINT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG. 5 AND ER/A 383975-14AD. 2 L 7 3 4F A3WE 2002102200035 20021022 00035 NM 2002 10 22 DL73K021205 1 20021017 A 5700 SKIN BOEING 737 737247 138448D NM NO 2 FOREFLAP GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 UPPER SKIN WORN THROUGH AT NO 2 T/E FOREFLAP REPAIRED PER SRM 51-40-20 FIG 12 2 L 7 2 4F A16WE 2002102200036 20021022 00036 NM 2002 10 22 DL72S021207 1 20021016 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM S-4R,FS481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 FUSELAGE / SKIN / FS 481-681 / STRG. 4R / SKIN LAP JOINT : CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP JOINT REVEALED CRACK INDICATIONS BETWEEN FS 481 & 681. INTERNAL MFEC INSPECTION REVEALED 8 CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL ALONG THE PANEL LENGTH. THE ENTIRE LAP JOINT WAS CUTOUT FROM FS 481-681 AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 383969-14AD. 2 L 7 3 4F A3WE 2002102200037 20021022 00037 NM 2002 10 22 DL72S021208 1 20021016 A 5330 655456716 SKIN BOEING 727 727232 1384082 NM S-4R,FS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 FUSELAGE / SKIN / FS 681-740 / STRG. 4R / SKIN LAP SPLICE : CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 & 740 REVEALED CRACK INDICATIONS. INTERNAL MFEC INSPECTION REVEALED SEVERAL CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN ALONG THE LENGTH OF THE PANEL. THE ENTIRE LAP JOINT ALONG THE PANEL LENGTH WAS CUTOUT TO REMOVE ALL CRACKS. THE AREA WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383973-14AD. 2 L 7 3 4F A3WE 2002102200038 20021022 00038 NM 2002 10 22 DL75A021210 1 20021018 A 3320 059341 BALLAST BOEING 757 757212 1384951 NM FORWARD CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 752AT 23128 APPROXIMATELY 3 PLUS HOURS FROM ATL DURING FLT ELECTRICAL ODOR IN FIRST CLASS CABIN - REPLACED 2CD BALLAST AND LAMPS 2 L 7 2 4F RT A2NM 2002102200039 20021022 00039 NM 2002 10 22 DL78K021214 1 20021019 A 3350 767 BULB BOEING 737 737832 13844CF NM LT FUSELAGE BLOWN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3731T 30775 IR-LT EXTERIOR EMERGENCY LIGHT JUST AFT OF WING INOP CA-RELAMPED SAME. OPS CKS NML. 2 L 7 2 4F RT A16WE 2002102200040 20021022 00040 NM 2002 10 22 DLM11021216 1 20021021 A 2530 831620405 OVEN DOUG MD11 MD11 3023602 NM AFT GALLEY UNSERVICEABLE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 810DE 48565 OVEN 326 AFT GALLEY SPARKS CAME OUT ABOVE THE WORD OFF ON THE TIMER - REPLACED OVEN 2 L 7 3 4F RT A22WE 2002102200041 20021022 00041 2002 10 22 751PA0006 4 20021017 A 2565 D31041147 SLIDE BOEING 757 757200 1384950 NM A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 751PA 23928 R3 door slide bottle pressure is low. R&R R3 door slide IAW 757MM 25-66-03. 2 L 7 2 4F RT A2NM 2002102200042 20021022 00042 WP 2002 10 22 MWEA020619 1 20021022 A 5230 5910141123 PAN DOUG DC9 DC981 3022081 WP NS18 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 FORWARD PIT DOOR INNER PAN IS GOUGED BETWEEN THE #2 AND #3 FORWARD STOP PAD FITTING NS18. -- BLENDED OUT GOUGE REMOVED 6 RIVETS, INSTALLED REPAIR. 2 L 7 2 4F A6WE 2002102500094 20021025 00094 WP 2002 10 25 MWEA020621 1 20021022 A 5753 5912125501 SPAR CAP DOUG DC9 DC981 3022081 WP T/E FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 LEFT FLAP AFT BOTTOM SPAR CAP IS CRACKED AT STATION XFLS 150. CUT OUT DAMAGE SPAR CAP, DRILLED UP SPAR AND SPLICE, INST ALLED REPAIR AND REINSTALLED INSPECTION PANEL AT LOWER LEFT SIDE OF FLAP. 2 L 7 2 4F A6WE 2002102800135 20021028 00135 WP 2002 10 28 MWEA020622 1 20021022 A 5310 SR095200089 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 AFT CARGO DOOR JAMB LOWER PORTION LONGERON 28 RIGHT MODERATE CORROSION ON AND UNDER DOUBLER PLATE. REMOVED DOUBLER, FAB RICATED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 2002102200043 20021022 00043 WP 2002 10 22 MWEA020623 1 20021022 A 5311 592480295 DOUBLER DOUG DC9 DC981 3022081 WP STATION 446 ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 DURING INSTALLATION OF 2 NACA RIVETS THROUGH SKIN LAP JOINT FINGER DOUBLERS AND SUBSEQUENT REMOVAL OF RIVETS THE FASTNER HOLES WERE ENLARGED JUST AFT OF FRAME STATION 446 AT LONGERON 15 LEFT. -- REAMED HOLES FABRICATED 2 EACH BUSHINGS FOR EXTERNAL SKIN. INSTALLED EXTERNAL BUSHINGS, HARDWARE AND 2 EACH RIVETS. 2 L 7 2 4F A6WE 2002102200044 20021022 00044 WP 2002 10 22 MWEA020624 1 20021022 A 5230 3926046505N INTERCOSTAL DOUG DC9 DC981 3022081 WP FWD CARGO DR TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 FORWARD CARGO DOOR FORWARD LOWER INTERCOSTAL HAS AN ATTACH FITTING THAT IS MISDRILLED. -- PLUGGED MISDRILLED HOLE IN P AN AND ANGLE, LOCATED AND DRILLED NEW FITTING AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2002102800136 20021028 00136 WP 2002 10 28 MWEA020625 1 20021022 A 5230 59101A1125 PAN DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 AFT CARGO DOOR DOOR PAN HAS GOUGE AROUND LOWER AFT STOP PAD. AFTER FURTHER EVALUATION FOUND CRACK AROUND DOOR JAMB. STO P DRILLED CRACK, FABRICATED DOUBLER REAPIR, INSTALLED REPAIR DOUBLER AND AFT DOOR SUPPORT. 2 L 7 2 4F A6WE 2002102800137 20021028 00137 WP 2002 10 28 MWEA020627 1 20021022 A 5320 991556317 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 JUST AFT OF FRAME STATION 1380 AT APPROXIMATELY LONGERON 28 LEFT, INTERCOSTAL HAS CORROSION ON FORWARD LOWER CORNER AROU ND FASTENER HOLE. REMOVED INTERCOSTAL, DRILLED UP AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2002102200045 20021022 00045 CE 2002 10 22 AMW2002F00002 1 20020914 A 2751 1015210243 LINK BEECH 1900 1900D 1154162 CE PWA PT6 PT6A11 52043 NE FLAP TRANSMITTER BROKEN A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 166YV 16634 UE166 AFTER DEPARTURE, THE FLAPS STILL INDICATED 17 DEGREES AFTER SELECTED UP. WHILE TRYING TO RECYCLE THE FLAPS, THE INDICAT OR MOVED TO 35 DEGREES. THE FLAP INDICATOR HAD BECOME STUCK. THE CREW ASKED TO RETURN TO THE FIELD, BUT DID NOT DECLAR E AN EMERGENCY. THE AIR TRAFFIC CONTROL TOWER DECLARED THE EMERGENCY INSTEAD. THE CORRECTIVE ACTION WAS THAT THEY REMO VED AND REPLACED THE BROKEN FLAP INDICATOR LINKAGE. NO TEARDOWN REPORT IS REQUIRED. 2 L 7 2 4T 3 T RT A24CE E4EA 2002102200046 20021022 00046 NM 2002 10 22 QXEA0201692 1 20021020 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 8171 76 511 PSC-FORWARD AND CENTER CEILING AISLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PS3 BATTERY PACK. OPERATIONAL TES T GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002102200047 20021022 00047 NM 2002 10 22 QXEA0201691 1 20021019 A 3350 6138001 BATTERY BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 818 818 4048 PDX-RIGHT HAND FORWARD EMERGENCY EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT SYSTEM BATTERY IN THE CA BIN CEILING AT STATION 083.00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002102200048 20021022 00048 NE 2002 10 22 AMW2002F00003 2 20020916 A 7310 1143890425 PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A11 52043 NE LP FUEL SYSTME FAILED A AMWA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CE 07 244YV UE244 WHILE FLIGHT WAS ENROUTE, THE LT LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CREW THEREFORE RETURNED THE A IRCRAFT TO THE FIELD WITHOUT ANY FURTHER INCIDENT. THE CORRECTIVE ACTION WAS THAT REPLACED THE LT LOW PRESSURE ENGINE D RIVEN FUEL PUMP. 2 L 7 2 4T 3 T RT A24CE E4EA 2002102200049 20021022 00049 CE 2002 10 22 AMW2002F00004 1 20020911 A 5270 MS250081 SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A11 52043 NE PAX DOOR DIRTY A AMWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 231YV 14559 UE231 DURING THE INITIAL CLIMB, THE CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CREW THEN RETURNED TO THE FIELD WITHOUT ANY FURTHER INCIDENT. NO TEARDOWN REPORT IS REQUIRED. THE CORRECTIVE ACTION WAS THAT THE DOOR SWITCH WAS CLEANED. 2 L 7 2 4T 3 T RT A24CE E4EA 2002102200050 20021022 00050 WP 2002 10 22 GTIA021033 1 20021001 A 2560 CLIP DOUG DC9 DC941 302207N WP FLASHLIGHT MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK FORWARD EMERGENCY FLASHLIGHT LOCK CLIP MISSING AND LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F A6WE 2002102200051 20021022 00051 WP 2002 10 22 GTIA021034 1 20020930 A 3220 DEFLECTOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE NLG CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 321NK 49508 RIGHT NOSE GEAR SPRAY DEFLECTOR HAS CRACK ON HUB PART. REPLACED BROKEN SPRAY DEFLECTOR ON THE RIGHT SIDE OF NOSE GEAR, OK. 2 L 7 2 4F 4 F A6WE E2EA 2002102200052 20021022 00052 SW 2002 10 22 JJWA0049154 1 20020925 A 3246 206321004 SKID BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MLG CORRODED D JJWA K NONE O OTHER IN INSP/MAINT 1 SO 17 281CB 1996 3303 HIGH SKID GEAR TUBE DISSIMILAR METAL CORROSION CRACK FOUND STARTING WITH SKID SHOE INSERT NUT UNDER AFT CROSSTUBE TITTIN G, ONLY 3 YEARS OLD, CRACK MAY HAVE BEEN MISSED FOR A WHILE ON INSPECTIONS. 1 G 7 1 3U 3 U H2SW E4CE 2002102200053 20021022 00053 SW 2002 10 22 JJWA0049155 1 20020925 A 3246 206321003 SKID BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MLG CRACKED D JJWA K NONE O OTHER IN INSP/MAINT 1 SO 17 281CB 1996 3303 SKID GEAR LANDING TUBE FOUND DISSIMILAR METAL CORROSION CRACK STARTING WITH SKID SHOE INSERT NUT AFT CROSSTUBE FITTING, NON-REPAIRABLE AREA. TUBE ONLY 3 YEARS OLD, CRACK MAY HAVE BEEN MISSED ON PAST INSPECTORS. 1 G 7 1 3U 3 U H2SW E4CE 2002102200054 20021022 00054 NE 2002 10 22 JK12002F00000 1 20020806 A 3213 20712 CYLINDER SKRSKY S76 S76B 8143007 NE PWA PT6 PT6* 52043 EA STRUT CRACKED B JK1R K NONE O OTHER IN INSP/MAINT 1 EA 25 212C 2872 760363 UPON ROUTINE RESEALING OF THE STRUT, A SMALL CRACK WAS FOUND ON LOWER END OF THE SHOCK STRUT CYLINDER. THIS HELICOPTER IS USED FOR CORPORATE TRANSPORTATION AND ENTERED INTO SERVICE ON DEC. 1990, CURRENTLY HAS 12,110 LANDINGS. THERE HAVE B EEN NO HARD OR OVERWEIGHT LANDINGS AND NO CORROSION WAS FOUND IN THE AREA OF THE CRACK. THE CYLINDER HAS LIFE LIMIT OF 108,000 CYCLES, (LANDINGS) AND THERE IS NO PERIODIC INSPECTION THAT WOULD REQUIRE DISASSEMBLY OF THE STRUT DOWN TO A LEV EL THAT WOULD EXPOSE THIS AREA. SUBMITTER RECOMMENDS A ONE TIME INSPECTION BE CONDUCTED ON OLDER HELICOPTERS TO INVESTI GATE THE SCOPE OF THIS CONDITION. 1 G 7 2 4U 3 T H1NE E2NE 2002102200055 20021022 00055 NM 2002 10 22 LI32002F00000 1 20021002 A 4930 LINE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE APU BROKEN B LI3R K NONE O OTHER IN INSP/MAINT 1 WP 09 908UA 25008 REPAIRED THE FOLLOWING APU AUTO SHUTDOWN WITH LARGE AMOUNT OF FUEL COMING OUT OF APU AREA. FUEL FOUND TO BE FROM FUEL L INE NOZZLE NEAR TOP ON LEFT SIDE OF APU, FUEL DID NOT IGNITE. MAIN FUEL MANIFOLD HAS ONE BROKEN TUBE BETWEEN THE FLEXIB LE FIRE SLEEVE AND THE B-NUT TO THE FUEL INJECTOR. MANIFOLD HAS 14 FUEL TUBES MANIFOLD IS UNDERGOING DETAILED ANALYSIS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102200056 20021022 00056 WP 2002 10 22 MEX2002305 1 20020918 A 2130 S1296S1297 SWITCH DOUG DC9 DC983 3022083 WP CABIN PRESSURE FAILED B ASMF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 23 583MD 49659 AIRCRAFT RETURNED OF FLIGHT AS CONSEQUENCE OF PRESSURIZATION FAILURE. AT PLATFORM TECH DETECTED THAT THE LIGHT (FLOW) T URNED ON IN PRESSURIZATION SELECTOR AND TRANSFER LOCK OUT. WITH ENGINES OPERATING, THERE WAS PERFORMED AT BITE AND CONT ROLLER 2 FAILED, IT WAS REPLACED ANS LIGHTS OF FLOW AND TRANSFER LOCKOUT TURNED OFF. AFTER, THERE WAS AN AIR CONDITIONI NG FAILURE. THE C/B OF FLOW CONTROL VALVE AND PRESSURE REGULATOR VALVE WERE CHECKED AND THE FCV DID NOT OPEN. THE SWIT CHES S1-296 AND S1-297 WERE REPLACED AND THE WIRE H324E20 WAS REPAIRED IAW MM, TESTS OK. 2 L 7 2 4F RT A6WE 2002102200057 20021022 00057 NE 2002 10 22 MEX2002306 2 20020920 A 7412 103538754 EXCITER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE ENGINE FAILED B ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 214AM 12703 49585 AIRCRAFT RETURNED TO PLATFORM DUE TO AN IGNITION FAILURE IN RT ENGINE. AT PLATFORM THE TECH TRIED TO START THE ENGINE B UT THERE WAS TROUBLE WITH THE EXCITER IGNITION BOX. UNIT WAS REPLACED IAW MM. 2 L 7 2 4F 4 F RT A6WE E9NE 2002102200058 20021022 00058 WP 2002 10 22 MWEA020570 1 20020920 A 5280 5910557135 HINGE DOUG DC9 DC915 3022036 WP LT MLG DOOR WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 LT MLG OUTBOARD FLYING DOOR. THE ARTICULATING DOOR HINGE HAS A FAIR AMOUNT OF MOVEMENT VERTICALLY. REMOVED, LOCATED AN D DRILLED WORN HINGE SECTION AND INSTALLED HINGE SECTION AND FLYING DOOR. 2 L 7 2 4F A6WE 2002102200059 20021022 00059 WP 2002 10 22 MWEA020571 1 20020920 A 5712 99116024 RIB DOUG DC9 DC915 3022036 WP WING TORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 AFT END OF XCW 42 RIBS IS TORN ABOUT MIDWAY UPPER WEB. FABRICATED FILLER AND REPAIRED DOUBLER, LOCATED AND DRILLED FILL ER AND DOUBLER, INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F A6WE 2002102200060 20021022 00060 WP 2002 10 22 MWEA020573 1 20020920 A 5320 99577093 INTERCOSTAL DOUG DC9 DC915 3022036 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 AFT CARGO COMPARTMENT INTERCOSTAL AT LONGERON 29 RIGHT HAS GOUGES ALONG AFT END AT STATION 785. REMOVED INTERCOSTAL, DR ILLED UP AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2002102200061 20021022 00061 WP 2002 10 22 MWEA020586 1 20020924 A 5320 9936534199 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 SUBFLOOR AT FRAME STATION 168 20 INCHES INBOARD OF PAX DOOR CUTOUT CORRODED. DRILLED OUT RIVETS, REMOVED CORROSION DAMA GE REPAIRED SUBFLOOR. 2 L 7 2 4F A6WE 2002102200062 20021022 00062 WP 2002 10 22 MWEA020589 1 20020924 A 5320 993053865 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 SUBFLOOR AT STATION 294 LEFT SIDE BY LONGERON 18 HAS INTERGRANULAR CORROSION. REMOVED FRAME AND DAMAGED AREA, FABRICATE D WEB AND DOUBLER, DRILLED AND INSTALLED FASTENERS, DOUBLER AND REINSTALLED FRAME. 2 L 7 2 4F A6WE 2002102200063 20021022 00063 WP 2002 10 22 MWEA020605 1 20021002 A 5311 27779305 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD PIT FRAME 446 CORRODED AFT SIDE BETWEEN LONGERON 30 AND 29. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER, DO UBLER AND REPAIR ANGLE. 2 L 7 2 4F A6WE 2002102200064 20021022 00064 WP 2002 10 22 MWEA020606 1 20021004 A 5311 995823837 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD PIT FRAME 484 CORRODED AROUND FASTENERS AT EACH LONGERON FROM 27 LEFT TO 27 RIGHT. REMOVED DAMAGED SECTION, LOC ATED AND DRILLED, FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2002102200065 20021022 00065 WP 2002 10 22 MWEA020607 1 20021008 A 5522 991848041 DOUBLER DOUG DC9 DC932 3022066 WP ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 SKIN DOUBLER CRACKED AT STATION XE156 FORWARD OF LOWER SPAR CAP. TRIMMED OUT DAMAGE, FABRICATED AND INSTALLED FILLERS, REMOVED AND INSTALLED FASTENERS. 2 L 7 2 4F A6WE 2002102200066 20021022 00066 WP 2002 10 22 MWEA020610 1 20021011 A 5311 995823837 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD PIT FRAME 503 CORRODED BEYOND LIMITS ON THE AFT SIDE AT LONGERON 30. REMOVED DAMAGED SECTION OF FRAME, FABRICAT ED REPAIR PLATES, DRILLED UP NEW FRAME SECTION AND REPAIR PLATES. INSTALLED REPAIR PLATES AND NEW FRAME SECTION. 2 L 7 2 4F A6WE 2002102200067 20021022 00067 WP 2002 10 22 MWEA020611 1 20021011 A 5310 9958231501 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 AFT CARGO DOOR JAMB BEAM FROM STATION 897-935 AT LONGERON 29 RIGHT HAS CORROSION AT NUTPLATE HOLES. BLENDED CORROSION, REMOVED, FABRICATED AND INSTALLED INTERCOSTAL, REMOVED AND FABRICATED BEAM, LOCATED FASTENER HOLES. 2 L 7 2 4F A6WE 2002102200068 20021022 00068 WP 2002 10 22 MWEA020613 1 20021014 A 5330 591142838 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FUSELAGE SKIN IS DENTED AT STATION 1080 AND LONGERON 22R. FABRICATED AND INSTALLED REPAIR DOUBLER, SMOOTHED OUT TOOL MA RKS. 2 L 7 2 4F A6WE 2002102200069 20021022 00069 WP 2002 10 22 MWEA020614 1 20021014 A 5310 591015849 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 AFT CARGO DOOR JAMB WEB HAS SURFACE CORROSION AT SEVERAL LOCATIONS. BLENDED CORROSION, LOCATED FASTENER HOLES IN NEW WE B AND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2002102200070 20021022 00070 WP 2002 10 22 MWEA020615 1 20021014 A 5310 J0602289 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 CORROSION ON LOWER END OF DOOR JAMB BETWEEN STATION 987-935 IN AFT CARGO BAY. BLENDED CORROSION, REMOVED FASTENERS IN L OWER JAMB SECTION, REMOVED DAMAGED SECTION OF JAMB PAN, TRIMMED LOCATED AND DRILLED UP NEW SECTION. INSTALLED NEW PAN S ECTION AND NEW WEB. 2 L 7 2 4F A6WE 2002102200071 20021022 00071 WP 2002 10 22 MWEA020616 1 20021014 A 5320 595606543 PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 CABIN OVERWING RIGHT SLANT PANEL HAS CORROSION IN THE LOWER RIGHT OUTBOARD PANEL AREA. FABRICATED AND INSTALLED NEW SLA NT PANEL. 2 L 7 2 4F A6WE 2002102200072 20021022 00072 WP 2002 10 22 MWEA020617 1 20021014 A 5310 591014249 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD CARGO DOOR JAMB PAN AT LONGERON 28 HAS LIGHT CORROSION ALONG ENTIRE LENGTH. REMOVED CORROSION, REMOVED LOWER DO OR JAMB PAN, LOCATED AND DRILLED NEW JAMB PAN, INSTALLED LOWER STOP FITTINGS AND SCUFF PLATE. 2 L 7 2 4F A6WE 2002102200073 20021022 00073 WP 2002 10 22 MWEA020618 1 20021017 A 7711 LINE DOUG DC9 DC932 3022066 WP RT ENGINE DISCONNECTED A MWEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 206ME 47791 RIGHT ENGINE PRESSURE RATIO GAUGE REMAINED AT 10. FOUND PT7 LINE DISCONNECTED AT LOWER AFT ATTACH FITTING. RECONNECTED PT7 LINE. 2 L 7 2 4F A6WE 2002102200074 20021022 00074 WP 2002 10 22 MWEA02574 1 20020920 A 5320 9957908501 INTERCOSTAL DOUG DC9 DC915 3022036 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 INTERCOSTAL AT FRAME STATION 340 BETWEEN LONGERON 28 AND 29 DAMAGED. REMOVED INTERCOSTAL, FIT AND DRILLED UP AND INSTAL LED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2002102200079 20021022 00079 NM 2002 10 22 SWAA022411 1 20021012 A 3211 656174010 CYLINDER BOEING 737 7373H4 1384600 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED RON, FOUND LT MLG AFT TRUNNION, AFT FACE CORRODED. REMOVED AND REPLACED LT MLG OUTER CYLINDER ASSY PER MM. 2 L 7 2 4F RT A16WE 2002102200080 20021022 00080 NM 2002 10 22 SWAA022412 1 20021012 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2002102200081 20021022 00081 NM 2002 10 22 SWAA022413 1 20021012 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2002102200082 20021022 00082 NM 2002 10 22 SWAA022414 1 20021011 A 3350 6404789 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED PM CHECK, FOUND LT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002102200083 20021022 00083 NM 2002 10 22 SWAA022415 1 20021012 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER M M. 2 L 7 2 4F RT A16WE 2002102200084 20021022 00084 NM 2002 10 22 SWAA022417 1 20021012 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED RON, FOUND AFT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002102200085 20021022 00085 NM 2002 10 22 SWAA022418 1 20021011 A 5312 BAC1505 TEE CHORD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH INBOARD AND OUTBOARD T-CHORDS CRACKED AT BS 178 WL 184 AND LBL 5.7. REPAIRED T-CHORDS PER SRM. 2 L 7 2 4F RT A16WE 2002102200086 20021022 00086 NM 2002 10 22 SWAA022422 1 20021015 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 713SW 27847 DURING SCHEDULED A2 CHECK, FOUND EEPLS INOP AT ROW NR 1 AND LENS MISSING AT ROW NR 5. RELAMPED AND INSTALLED LENS PER M M. 2 L 7 2 4F RT A16WE 2002102200087 20021022 00087 NM 2002 10 22 SWAA022423 1 20021013 A 5512 6573782 PANEL BOEING 737 7373Q8 1384670 NM HORIZ STAB BULGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED 1/4D CHECK, FOUND RT HORIZ STAB UPPER OUTBOARD SURFACE PANEL BULGING ON BOTH INBOARD AND OUTBOARD FWD C ORNERS. REPAIRED RT HORIZ STAB PER SWA EA'S. 2 L 7 2 4F RT A16WE 2002102200088 20021022 00088 CE 2002 10 22 043636 1 20020929 A 5270 V3101D8 SWITCH BEECH 1900 1900D 1154162 CE PAX DOOR LOOSE A AMWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 3199Q UE213 AFTER DEPARTURE ON FLIGHT 5637, THE CABIN DOOR ANNUNCIATOR ILLUMINATED. THE AIRCRAFT WAS THEN DIVERTED TO PANAMA CITY, F LORIDA WHERE MAINTENANCE INSPECTED THE DOOR AND DEFERRED THE ANNUNCIATOR SYSTEM. THE CORRECTIVE ACTION WAS THAT AFTER TH E INSPECTION OF THE DOOR, THE LATCH SWITCH ARM WAS FOUND TO BE LOOSE. MAINTENANCE REPLACED THE AFT LATCH SWITCH AND THE AIRCRAFT WAS THEN RETURNED TO SERVICE. NO TEARDOWN REPORT REQUIRED. 2 L 7 2 4T RT A24CE 2002102200089 20021022 00089 NM 2002 10 22 SWAA022426 1 20021012 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2002102200090 20021022 00090 NM 2002 10 22 DHL2002705012 1 20021021 A 3350 1000677 LIGHT BOEING 727 72722C 138400F NM A DHLA K O NONE OTHER O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 1) MAIN ENTRANCE DOOR EMERGENCY LIGHT WILL NOT CHARGE.2) REPLACED EMERGENCY LIGHT ASSEMBLY PER M/M 33-50-00. OPS CHECK ED GOOD. 2 L 7 3 4F A3WE 2002102200091 20021022 00091 NM 2002 10 22 SWAA022429 1 20021015 A 5512 657378211 SKIN BOEING 737 7373Q8 1384670 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED 1/4D CHECK, FOUND LT HORIZ STAB UPPER OUTBOARD SURFACE SKIN CORRODED. REPAIRED LT HORIZ STAB PER SWA E A. 2 L 7 2 4F RT A16WE 2002102200092 20021022 00092 NM 2002 10 22 SWAA022431 1 20021012 A 5312 BAC1505 TEE CHORD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED SPECIAL VISIT, FOUND T-CHORD CRACKED AT BS 178, WL 182 AND RBL 5.7. REPAIRED T-CHORD PER SRM. 2 L 7 2 4F A16WE 2002102200093 20021022 00093 2002 10 22 SWAA022432 4 20021016 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002102200094 20021022 00094 2002 10 22 SWAA022433 4 20021016 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002102200095 20021022 00095 NM 2002 10 22 SWAA022434 1 20021016 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED A1 CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASS Y PER MM. 2 L 7 2 4F A16WE 2002102200096 20021022 00096 NM 2002 10 22 SWAA022435 1 20021015 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 102SW 23108 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2002102200097 20021022 00097 SO 2002 10 22 AY52002F00001 1 20020911 A 5520 14527811401 FLANGE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RT ELEVATOR WORN B AY55 K NONE O OTHER IN INSP/MAINT 1 SO 03 278SK 4265 145370 DURING "C" CHECK INSPECTION, THE RIGHT ELEVATOR WAS NOTED TO HAVE PLAY AT THE CENTER HINGE POINT. FURTHER INVESTIGATION REVEALED THE INBOARD HAT BUSHING HAD BACKED OUT OF THE FLANGE ALLOWING THE ELEVATOR TO HAVE 0.122 INCH PLAY AT THE HING E. THE END OF THE HAT BUSHING SUBSEQUENTLY CAUSED 0.017 INCH WEAR INTO THE FLANGE. THE FLANGE WAS REPLACED AND THE AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002102200098 20021022 00098 NM 2002 10 22 SWAA022436 1 20021015 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 102SW 23108 DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT FWD CABIN. RELAMPED PER MM. 2 L 7 2 4F A16WE 2002102200099 20021022 00099 NM 2002 10 22 SWAA022439 1 20021016 A 5320 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, BETWEEN STR 16R AND STR 17R. REMOVED AND REPLACED S TRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002102200100 20021022 00100 2002 10 22 UPS02139736 4 20021013 A 2565 D31023101 SLIDE AIRBUS A300 A300F4622R 3930360 EU CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 120UP 0805 DURING ESCAPE SLIDE FUNCTIONAL TEST, BATTERY CAPACITY AND BULB CONTINUITY FAILED TO PASS TEST REQ. REMOVED AND REPLACED EMERGENCY EVACUATION SLIDE PER A300 AMM 25-61-2 1-4. 2 L 7 2 4F RT A35EU 2002102200101 20021022 00101 WP 2002 10 22 MEX2002307 1 20020922 A 2913 AS66411LS666 PUMP DOUG DC9 DC983 3022083 WP HYDRAULIC SYS FAILED B ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 583MD 23447 49659 AIRCRAFT RETURNED FROM FLIGHT AS CONSEQUENCE OF THE LIGHT (RT HYD PRESS LOW) AT PLATFORM, TECH SUPPLIED 14 QTS OF HYDRAU LIC FLUID. RIGHT ENGINE WAS STARTED BUT THE PRESSURE INDICATION OF MAIN PUMP WAS NOT SHOWN. SUCH PUMP WAS REPLACED AND DURING THE TESTS A PIPELINE WAS FOUND WITH DAMAGES IAW MM. THE PIPELINE WAS REPLACED WITH A FLEXIBLE HOSE, TESTS OK. THE WATER SEPARATORS AND THE PUMP FILTERS WERE REPLACED AS CONSEQUENCE OF AN HYDRAULIC SMELL IN CABIN AND FILTER OBSTRUC TION INDICATION. HYDRAULIC PUMP WAS REPLACED IAW MM, THE PIPELINE TO THE FILTERS RETURN LINE WAS CHANGED IAW MM, TESTS OK. 2 L 7 2 4F RT A6WE 2002102200102 20021022 00102 NE 2002 10 22 MEX2002315 2 20020309 A 7250 CLAMP DOUG MD88 MD88 3023688 NM PWA JT8 JT8D NE ENGINE LOOSE B ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 162PL 49765 DURING ENGINE STARTING RT ENGINE REACHED 14 PERCENT OF N2. AIRCRAFT WAS MOVED TO ANOTER PLATFORM POSITION WHERE THE ENG INE ONLY REACHED 14 PERCENT OF NR 2. TECHNICAL PERSONNEL VERIFIED THE SYSTEM BY LEAKAGES BUT NOTHING WAS CARRIED TO MAI NTENANCE HANGAR TO ATTEND THE FAILURE, PERSONNEL FOUND A LEAKAGE IN THE LOWER CLAMP OF THE STAGE 8TH VALVE. IT WAS TIGH TENED, AND A ENGINE RUN TEST WAS PERFORMED IAW MM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102200103 20021022 00103 NE 2002 10 22 MEX2002317 2 20020110 A 7200 ENGINE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE LEFT MALFUNCTIONED B ASMF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 23 1075T 49724 AIRCRAFT RETURNED TO PLATFORM DUE TO LEFT ENGINE DID NOT ACCELERATE. PARAMETERS WERE ON RIGHT ENGINE 56.5 AND ON LEFT E NGINE 51.0 ENGINE 51.0. ENGINES WERE ADJUSTED ON IDLE, TESTS OK. DURING OVERNIGHT, SERVICE WAS PERFORMED A TRIM TO BOT H ENGINES IAW MM, TESTS AND PARAMETERS WERE OK. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102200104 20021022 00104 NM 2002 10 22 MEX2002321 1 20020510 A 8012 START VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE RT ENGINE FAILED B ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 162PL 49765 STARTING OF THE ENGINE NR 2, THERE WAS NOT NR 2 TURNING AND START VALVE LIGHT DID NOT TURN ON. SUCH VALVE WAS OPENED MA NUALLY. CAPTAIN INDICATES THAT THE LIGHT TURNED ON BUT THERE IS NOT TURNING. A PIPELINE TO THE STARTING VALVE WAS TIGH TENED IAW MM AND THE ENGINE WAS STARTING MANUALLY. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102200105 20021022 00105 NM 2002 10 22 P9R2002F00005 1 20020912 A 3232 731412 ACTUATOR BOEING 727 727231 1384079 NM PWA JT8 JT8D9 52048 NE RT MLG BYPASSING A P9RA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SO 11 54344 21631 AFTER TAKEOFF, WHEN PLACING THE GEAR LEVER TO OFF. THE RED DOOR WARNING INDICATOR AND RIGHT GEAR DOOR INDICATOR ILLUMIN ATED. AIRCRAFT VEERS RIGHT. FOUND RIGHT GEAR DOOR ACTUATOR BYPASSING. REMOVED AND REPLACED RIGHT MAIN GEAR DOOR ACTUA TOR IAW MM. LK OPS CHECK, GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2002102200106 20021022 00106 2002 10 22 PG22002F00000 4 20021001 A 3421 6343560012 SWITCH BEECH B300 B300 1159232 CE PWA PT6 PT6A11 52043 NE INDICATOR SHORTED B PG2R O OTHER O OTHER NR NOT REPORTED 1 GL 11 200VC FL316 PILOTS HEADING SYSTEM CONTINUOUSLY ROTATED COUNTER CLOCKWISE. TROUBLESHOT PROBLEM TO A2S2 IN THE CCU65 CONTROL UNIT. F OUND SPRING INTERNAL TO SWITCH SHORTED TO OPPOSITE TERMINAL. REPLACEMENT OF SWITCH CURED PROBLEM. A HEIGHT QUALITY SWI TCH, OR INSULATION AROUND SPRING INSIDE SWITCH WOULD PREVENT FUTURE PROBLEMS. (HEADING SYSTEM WORKED FINE THE DAY BEFOR E PROBLEM APPEARED). 2 L 7 2 4T 3 T RT A24CE E4EA 2002102200107 20021022 00107 CE 2002 10 22 QTVA901U 1 20020926 A 2750 50000084 CONTROL CABLE CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO TE FLAPS BROKEN E QTVA O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED AP APPROACH 1 NM 11 7947Q 402B0397 ON SHORT FINAL, HEARD A THUD IN FLOORBOARDS. JUST AFTER PUTTING GEAR DOWN. AIRCRAFT HAD A SLIGHT YAW AND ROLL AND LAND ED UNEVENTFULLY. TAXIED IN, SELECTED FLAPS UP AND SHUTDOWN AIRCRAFT. DURING POSTFLIGHT NOTICED FLAPS WERE STILL FULLDO WN. MAINTENANCE INSPECTION FOUND BROKEN FLAP CONTROL CABLE. REMOVED AND REPLACED FLAP CABLE. 1 L 7 2 3O 3 O A7CE E8CE 2002102200108 20021022 00108 2002 10 22 R7M015934349 4 20020916 A 3400 MOUNT LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE731* 01518 WP MAGNETOMETER BROKEN B CERA K NONE O OTHER IN INSP/MAINT 1 NM 07 31DP 062 MAGNETOMETER MOUNTS (ELASTOMERIC) BROKEN WHICH MAY HAVE CAUSED BAD DATA TO BE SENT TO THE PRIMARY FLIGHT GENERATOR WHICH CAUSED A MISALIGNMENT WITH NUMBER TWO AHRU. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 2 L 7 2 4F 4 F A10CE E6WE 2002102200109 20021022 00109 WP 2002 10 22 AT0200085 1 20021020 A 7730 JT8D9 ENGINE DOUG DC9 DC932 3022066 WP #2 ENGINE A ZZDA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 15 830AT 47723 #2 ENGINE LOST POWER ON CLIMB OUT-ROLLED BACK TO 70% N1 WITH SIGNIFICANT VIBRATION. ALL OTHER PARAMETERS WITHIN LIMITS WITH POWER AT IDLE VIBE CEASED. CORRECTIVE ACTION: REMOVED AND REPLACED #2 ENGINE IAW P.P. TASK CARDS 99-LEAK AND OPERATIONAL NORMAL. 2 L 7 2 4F A6WE 2002102200110 20021022 00110 NM 2002 10 22 2002UALA01582 1 20021013 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 AFT CABIN FLOOR SUPPORT UPPER FRAME SURFACE IS CORRODEDSTATION 1640 AND RBL 58. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR AC COMPLISHED. REPAIRED WITH REPLACEMENT CORD, REPAIR STRAP, REPAIR ANGLE AND SPLICE ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002102200111 20021022 00111 NM 2002 10 22 2002UALA01584 1 20021013 A 5315 STIFFENER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 FLOOR BEAM VERTICAL STIFFENER CRACKED AT STATION 246, LBL40. MAJOR REPAIR ACCOMPLISHED. REPLACED STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002102200112 20021022 00112 NM 2002 10 22 2002UALA01590 1 20021015 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 AFT EXT FUSELAGE SKIN DENT OUT OF LIMITS AT STATION 1617 STRINGER 20L SKIN LAP AND PRODUCTION JOINT. SUPPLEMENTAL DATA U PDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002102200113 20021022 00113 GL 2002 10 22 29521121 1 20021022 A 3350 110049 POWER SUPPLY BOMBDR BD700 BD7001A10 1390006 GL A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 648BR DURING INSPECTION AFT EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED # 4 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00003NY 2002102200114 20021022 00114 NM 2002 10 22 AWXA200201030 1 20021015 A 5315 654581217 STIFFENER BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 0 0 22651 YVR - MAJOR REPAIR - DURING C-20 CHECK A 1/2" CRACK WAS FOUND ON AFT SIDE OF CABIN FLOOR BEAM INTERCOASTAL ATTACH ANGLE (STIFFENER) BS 328, LBL 47. MAINTENANCE REMOVED DAMAGED INTERCOASTAL ATTACH ANGLE AT BS 328, LBL 47; FABRICATED A NEW RE PLACEMENT ATTACH ANGLE; AND INSTALLED REPAIR PART IAW DWG 65-45812, AND B737-200 SRM 51-10-1, PG. 8. 2 L 7 2 4F RT A16WE 2002102200115 20021022 00115 NM 2002 10 22 AWXA200201035 1 20021001 A 5320 654795711 STRAP BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND AROUND SCREW HOLES IN AFT CARGO COMPARTMENT DOOR OPENING LOWER STRAP, BS 794-847, RBL 22. MAINTENANCE REMOVED CORROSION AT AFT CARGO DOOR OPENING LOWER STRAP AND FOUND MATERIAL LOSS OUT OF L IMITS; REMOVED LOWER STRAP BETWEEN BS 794-847, RBL 22; FABRICATED A NEW REPLACEMENT STRAP; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 3-4, 8, 10-11. 2 L 7 2 4F RT A16WE 2002102300001 20021023 00001 WP 2002 10 23 GTIA021046 1 20020929 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FLOORBOARDS, STA 160 TO STA 190 RIGHT CENTER PANEL IS CRACKED AND DELAMINATED, CORRODED. FABRICATED NEW FLOORBOARD, IN STALLED NEW FLOORBOARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300002 20021023 00002 WP 2002 10 23 GTIA021047 1 20020923 A 5313 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 32562 49504 AFT PIT STA 1287-1309 L25L, LONGERON SPLICE IS CRACKED ALONG RADIUS AT LONGERON TO SKIN FASTENERS. REMOVED SPLICE, LOCA TED AND DRILLED NEW SPLICE/ INSTALLED NEW SPLICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300003 20021023 00003 WP 2002 10 23 GTIA021048 1 20020924 A 5320 CLIP DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FLOOR SUPPORT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FORWARD CARGO FS 427 FLOOR SUPPORT CLIP, CRACKED. REMOVED FLOOR SUPPORT CLIP, FABRICATED SUPPORT CLIP, INSTALLED FLOOR SUPPORT CLIP. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300004 20021023 00004 WP 2002 10 23 GTIA021049 1 20020925 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FLOORBOARD SUPPORT STA 218 LBL4, CORRODED. C/A: FABRICATED NEW EXTRUSION FLOORBOARD SUPPORT. INSTALLED FLOORBOARD SUP PORT. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300005 20021023 00005 WP 2002 10 23 GTIA021050 1 20020925 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FLOOR SUPPORT CORRODED LBL63 STA 160-200. REMOVED FLOOR SUPPORT, FABBED NEW FLOOR SUPPORT, INSTALLED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300006 20021023 00006 WP 2002 10 23 GTIA021051 1 20020925 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FLOORBOARD SUPPORT CORRODED, LBL45, STA200. REMOVED FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT, INSTALLED FLOOR SUPPOR T. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300007 20021023 00007 WP 2002 10 23 GTIA021052 1 20020925 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FLOORBOARD SUPPORT CORRODED, RBL16, STA 200. REMOVED FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPP ORT. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300008 20021023 00008 WP 2002 10 23 GTIA021053 1 20020917 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 PAX CABIN STA 200 TO STA 256 FLOOR PANEL HAS DELAMINATED AT THE HAT SECTION. REPAIRED PAX CABIN FLOOR PANEL. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300009 20021023 00009 WP 2002 10 23 GTIA021054 1 20020917 A 5230 3926046503 SUPPORT BRACKET DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 AFT LOWER CARGO, CARGO DOOR HAS CRACKED AT INBOARD AFT BRACKET SUPPORT STRAP. REMOVED CRACKED AFT BRACKET LOCATED AND R EMOVED FITTING. INSTALLED NEW FITTING. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300010 20021023 00010 WP 2002 10 23 GTIA021055 1 20020919 A 5230 SUPPORT BRACKET DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 MID CARGO, CARGO DOOR HAS CRACKED AT FORWARD UPPER INBOARD BRACKET SUPPORT STRAP. REMOVED CRACKED BRACKET. AFTER REMOV AL OF CRACKED BRACKET FOUND DOOR PAN TO BE CRACKED. STOP DRILLED CRACK IN PAN. LOCATED AND DRILLED HOLES IN FITTING, F ABRICATED DOUBLER. INSTALLED DOUBLER AND FITTING. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300011 20021023 00011 WP 2002 10 23 GTIA021056 1 20020909 A 5230 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE CARGO DOOR DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 MID PIT CARGO DOOR HAS DENT & DAMAGE AT AROUND HANDLE EDGES. FABRICATED REPAIR DOUBLER, TRIMED DAMAGE OUT OF DOOR, INS TALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300012 20021023 00012 WP 2002 10 23 GTIA021057 1 20020911 A 5754 99375681 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE NR 5 SLAT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 LEFT WING, NR 5 SLAT, EXTREME OUTBOARD END CAP, UPPERSIDE CRACKED NEXT TO RIVETS. LOCATED, DRILLED AND DEBURRED REPAIR PART INSTALLED REPAIR PART. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300013 20021023 00013 WP 2002 10 23 GTIA021058 1 20020911 A 5754 RIB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE NR 3 SLAT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 LT WING UNDERSIDE OF NR 3 SLAT ACCESS AREA, RIB CRACKED AT FIXED LEADING EDGE, STA XRS 267. FABRICATED FILLERS AND REPA IR ANGLES/DOUBLERS STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER ON RIB. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300014 20021023 00014 WP 2002 10 23 GTIA021059 1 20020912 A 5330 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 CRACKED AND DAMAGE AROUND L1 DOOR HOLD OPEN PIN CUT OUT. LOCATED, DRILLED AND DEBURRED REPAIR DOUBLER INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300015 20021023 00015 WP 2002 10 23 GTIA021060 1 20020912 A 5313 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE DAMAGED DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 CREASE OVER FRAME AT FS 220 BETWEEN LONGERONS 17L AND 18L. LOCATED, FABRICATED AND DRILLED DOUBLER INSTALLED REPAIR DOU BLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300016 20021023 00016 WP 2002 10 23 GTIA021061 1 20020912 A 5330 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 GOUGE AT FS 1312 BETWEEN LONGERON 20R AND 21R. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUB LER AND FILLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102300017 20021023 00017 EA 2002 10 23 REX02020 1 20020929 A 7921 O-RING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE OIL COOLER CUT A REXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 8506C 7506 GEE872002 ENROUTE, IN CRUISE CONFIGURATION AT FL290, AT A POSITION 80 MILES NORTH, THE RT ENG OIL PRESSURE BEGAN TO FLUCTUATE BETW EEN 28 AND 42 PSI, FOLLOWED BY INTERMITTENT ILLUMINATION OF LOW OIL PRESSURE WARNING. FLIGHT CREW DECLARED EMERGENCY AN D SHUT DOWN THE ENGINE USING APPROVED CHECKLIST. FLIGHT CREW CONTACTED ATC AND WAS APPROVED TO DIVERT. AN OTHERWISE UN EVENTFUL APPROACH AND LANDING WAS MADE. C/A: MAINT FOUND A LOSS OF ENG OIL CAUSED BY A CUT O-RING ON OIL COOLER INLET TUBE. TUBE HAD BEEN REMOVED TO FACILITATE OTHER MAINT ON A PREVIOUS MAINT HANGER VISIT, BUT HAD BEEN LEAK CHECKED FOLLO WING INSTALL OF TUBE. O-RING WAS REPLACED AND ENGINE SERVICED WITH OIL. THE A/C WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002102300018 20021023 00018 GL 2002 10 23 RMM2002F00000 1 20020819 A 8011 STARTER DIAMON DA40 DA40 GL ENGINE MALFUNCTIONED E RMMA K NONE O OTHER IN INSP/MAINT 1 CE 01 607DS 58 40207 OPERATOR REPORTED AFTER LONG CRANKING OPERATION ALL WARNING AND INSTRUMENT LIGHTING DIMMED AND WENT OUT. BATTERY NEARLY 0 VOLTS WHEN CHECKED. CHARGED BATTERY, WHEN INSTALLING BATTERY. NEGATIVE TERMINAL, SOLENOIDS ACTIVATED AND STARTER SO LENOID ENGAGED. (AIRCRAFT HAS NEW LIGHT STARTER WITH A SOLENOID ON THE STARTER). SWITCHES ALL IN (OFF) POSITION. 1 L 7 1 3O NT A47CE 2002102300019 20021023 00019 CE 2002 10 23 RU32002F00004 1 20021003 A 2612 37702833 CONTROL BOX LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE RT ENG FIRE WARN FAILED E RU3A O OTHER N FALSE WARNING CL CLIMB 1 SW 15 58 3047 057 ON DEPARTURE, CLIMBING THROUGH 11,000 MSL, RIGHT ENGINE FIRE LIGHT ILLUMINATED. ENGINE FIRE IN FLIGHT CHECKLIST ACCOMPL ISHED. ADVISED PDX ATC, REQUESTED IMMEDIATE RECOVERY, EMERGENCY DECLARED. RIGHT ENGINE FIRE LIGHT REILLUMINATED THREE TIMES DURING APPROACH AND LANDING FOR APPROXIMATELY 5 SECONDS EACH TIME. REMOVED AND REPLACED RT ENGINE FIRE DETECTION CONTROL BOX. 2 L 7 2 4F 4 F RT A10CE E35NE 2002102300020 20021023 00020 2002 10 23 RU3A0210 4 20020103 A 3120 COMPUTER BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE COCKPIT BURNED E RU3A K NONE O OTHER IN INSP/MAINT 1 SW 15 68 FF3 SMOKE ACCOMPANIED BY ACRID FUMES, WAS DETECTED IN THE AIRCRAFT CABIN, MISSION POWER CIRCUIT BREAKER SWITCH ON GENERATOR CONTROL PANEL WAS USED TO TURN OFF POWER. CREW DONNED OXYGEN MASKS, CABIN WAS DEPRESSURIZED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. WHILE TROUBLESHOOTING KEYBOARD AT TECH POSITION WAS FOUND TO HAVE INTERNAL HEAT DAMAGE AND EMITTED S MOKE. 2 L 7 2 4T 4 T A24CE E4EA 2002102300021 20021023 00021 SO 2002 10 23 SIM2002F00000 1 20020926 A 5311 ALCLAD2024T3 FRAME EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 DURING AN INSPECTION OF AN EXISTING REPAIR TO FRAME 73 AT STRINGER 15L ADDITIONAL DAMAGE IN THE FORM OF A .75 INCH LONG CRACK, WAS FOUND. REMOVED THE EXISTING REPAIR PERFORMED AN EDDY CURRENT INSPECTION TO CONFIRM CRACK ENDED AT A RIVET HO LE. FABRICATED AN L-SHAPE REINFORCEMENT AND INSTALLED INTO FIR AIRCRAFT. REPAIR DONE IAW MM REPAIR STATEMENT AND STAND ARD MFG SRM PRACTICES. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002102300022 20021023 00022 SO 2002 10 23 SIMA200227918 1 20020915 A 5311 FRAME EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 DURING AN MFG INSPECTION, MAINTENANCE FOUND CORROSION ON LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20. REMOVED PREVIOU S REPAIR (CORROSION LIMITED TO PREVIOUS REPAIR ONLY). FABRICATED A DOUBLER ANGLE, FILLER, PLATE, AND TWO SHIMS. REPAIR DONE IAW MFG SRM AND STANDARD SRM PRACTICES. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002102300023 20021023 00023 SO 2002 10 23 SIMA200227920 1 20020917 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 DURING AN IMBV INSPECTION, STRINGER 19R WAS FOUND TO BE CHAFED. BLENDED CHAFED AREA. PERFORMED AN NON DESTRUCTIVE TEST ING INSPECTION WITH NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE AND TWO SHIMS. REPAIR DONE IAW MFG SRM AND STANDARD S RM PRACTICES. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002102300024 20021023 00024 SO 2002 10 23 SIMA200227921 1 20020920 A 5310 14525480003 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL CARGO DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 DURING AN IMBV INSPECTION, CARGO DOOR LOWER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING CARGO DOOR LOWER SILL. INSTALLED SERVICEABLE SILL IAW MFG SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002102300025 20021023 00025 CE 2002 10 23 TIM2002F00014 1 20020924 A 5740 501200743 ATTACH FITTING BEECH 99 99A 1154003 CE PWA PT6 PT6* 52043 EA RT WING CRACKED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 326CA U135 CRACK FOUND IN RIGHT WING, CENTER SECTION UPPER FORWARD ATTACH FITTING. 1 L 7 2 3T 3 T A14CE E2NE 2002102300026 20021023 00026 NM 2002 10 23 TSAA0253201 1 20021002 A 5230 6545769 STRUCTURE BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE CARGO DOOR GOUGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 40176 24031 CUTOUT DAMAGE, PERFORMED A DETAILED VISUAL AND HFEC INSPECTION OF THE CUTOUT AND ALL LAP SPLICE FASTENERS HOLES IN THE R EPAIR AREA, NO DEFECTS NOTED. FABRICATED A DOUBLER, TRIPLER STRUCTURAL FILLER. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4U 4 F RT A16WE E2EA 2002102300027 20021023 00027 NM 2002 10 23 TSAA0253202 1 20020925 A 5753 FLAP TRACK BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D15 52051 NE TE FLAPS DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 41352 39735 FLAP TRACK ATTACHMENT FITTING HOLE ELONGATED. REPAIRED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002102300028 20021023 00028 NM 2002 10 23 TSAA0253203 1 20021001 A 5330 6545769 SKIN BOEING 737 73725A 1384481 NM PWA JT8 JT8D17 52049 NE FUSELAGE GOUGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 37519 23791 REMOVED DAMAGE ON FWD CARGO DOOR CUT OUT. PERFORMED A DETAILED VISUAL AND HFEC INSPECTION OF THE CUTOUT AND ALL LAP SPL ICE FASTENERS HOLES IN THE REPAIR AREA, NO DEFECTS NOTED. INSTALLED REPAIR IAW SRM. AIRCRAFT RETURNED TO SERVICE.(TSAA80 03321) 2 L 7 2 4F 4 F RT A16WE E2EA 2002102300029 20021023 00029 NM 2002 10 23 TSAA0253204 1 20020926 A 5330 6545818 SKIN BOEING 737 737230 1384401 NM FUSELAGE GOUGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 823AL 36729 23154 23 INCH LONG GOUGE AND .5000 INCH TO 3 INCH DEEP DENT NOTED ON FUSELAGE EXISTING REPAIR AT BS344 - BS360+7. INSTALLED REPAIR PARTS REPAIR COMPLETED IAW SRM. AIRCRAFT OF FOR SERVICE. 2 L 7 2 4F RT A16WE 2002102300030 20021023 00030 NM 2002 10 23 TSAA0278199 1 20021003 A 7830 BRACKET BOEING 737 737230 1384401 NM THRUST REVERSER CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 22117 THE NUMBER ONE REVERSER UNLOCK LIGHT ILLUMINATED IN-FLIGHT. THE AIRCRAFT RETURNED TO AND LANDED AT AIRPORT WITH NO FURT HER INCIDENT. MAINTENANCE FOUND THE UPPER LOCK ACTUATOR SENSOR BRACKET CRACKED. MAINTENANCE REPLACED THE SENSOR BRACKE T AND AS A PRECAUTIONARY BOTH UPPER AND LOWER PROXIMITY SENSOR CIRCUIT CARDS. GROUND OPERATIONAL CHECKS WERE GOOD AND T HE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002103100252 20021031 00252 NM 2002 10 31 UIEA200200048 1 20020907 A 3260 UPLOCK SWITCH BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL RT MLG OUT OF ADJUST A UIEA O OTHER N FALSE WARNING CL CLIMB 1 EA 15 497MC 29258 AFTER TAKE OFF THE RIGHT GEAR DID NOT RETRACT. INDICATED INTRANSIT. GEAR EXTENDED DOWN OK BUT DID NOT RETRACT AGAIN. STATUS MESSAGE GEAR DISAGREE, GEAR MONITOR. T/S BOTH RIGHT GEAR UPLOCK SWITCHES S402 AND S1637. ADJUSTMENT OUT OF LIMI T, READJUSTED BOTH SWITCHES IAW MM. PERFORMED GROUND CHECK AND FOUND ALL, OK. 2 L 7 4 4F 4 F RT 1384945 E23EA 2002102300031 20021023 00031 NM 2002 10 23 UIEA200200049 1 20020929 A 3260 SENSOR BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NLG DOOR MALFUNCTIONED A UIEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 15 527MC 22471 NOSE GEAR DOOR LIGHT (RED) AND GEAR LIGHT REMAINED ON AFTER GEAR LEVER WAS RAISED. ATTEMPTED TO CORRECT PER FHB PROCEDU RES TO NO AVAIL. AIR TURN BACK REQUIRED. JETTISONED APPROXIMATELY 70,000 KGS OF FUEL. LIFTED THE AIRCRAFT AND TROUBLE SHOT PER MM. ALL GEAR VISUAL INSPECTIONS AND OPS NORMAL. TROUBLESHOT LANDING GEAR WARNING LOGIC CARD AND SENSOR PER MM AND CLEANED SAME. INSPECTED AND ADJUSTED NOSE GEAR DOOR WARNING SENSOR PER MM. LUBRICATED NOSE GEAR AS REQUIRED. SWI NG CHECK OPS AND INDICATION NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 2002102300032 20021023 00032 2002 10 23 UIEA200200050 4 20020929 A 2210 2736005015 MODULE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE AUTOPILOT LEAKING A UIEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 15 512MC 21220 NR 1 HYDRAULIC LOW QUANTITY LIGHT CAME ON AFTER TAKEOFF. HYDRAULIC QUANTITY DROPPED TO ZERO. APPROXIMATELY 30 SECONDS LATER THE EDP AND ADP PRESSURE LIGHTS BEGAN TO FLASH. SHUT SYSTEM DOWN IAW PROCEDURES. EDP PUMP SWITCH PLACED TO SUPPL Y OFF POSITION AT 0800. FOUND A/P PITCH MODULE LEAKING. CHANGED A/P PITCH MODULE ACC MM. FOUND PRESSURE AND RETURN LI NE INTERCHANGED. CORRECTED THE SAME. PERFORMED OPS AND LEAK CHECK. ALL SATISFACTORY. 2 L 7 4 4F 4 F A20WE E23EA 2002102300033 20021023 00033 2002 10 23 USA2002F00092 4 20020930 A 2565 D31591478 SLIDE BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE RT SERVICE DOOR FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 394US 42418 3865 23316 DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE APPEARED TO HAVE PREMATURELY I NFLATED AND BECAME TWISTED 90 DEGREES. DOOR BECAME DIFFICULT TO OPEN FULLY ONCE SLIDE BEGAN TO INFLATE. SLIDE OPERATIO NAL CHECK FAILED. MAINTENANCE DETERMINED THE FORWARD RIGHT SERVICE DOOR WAS NOT OPENED BRISKLY ENOUGH TO PROPERLY DEPLO Y ESCAPE SLIDE. MAINTENANCE REMOVED AND REPLACED THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE ASSEMBLY. TWO ADDITIONAL OPERATIONAL CHECKS ARE SCHEDULED TO BE PERFORMED AT THE FORWARD RIGHT SERVICE DOOR POSITION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102300034 20021023 00034 NM 2002 10 23 USAA020366 1 20020924 A 5330 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 24411 SKIN HAS A 1 INCH CRACK, STA 727D AT S-23 RT. INSTALLED DOUBLER IAW T/R. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102300035 20021023 00035 NM 2002 10 23 USAA020367 1 20020917 A 5751 65C2591113A SKIN BOEING 737 737301 1384611 NM RT AILERON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 27291 23228 RIGHT AILERON, CRACKED 2 LOCATIONS. LOWER SKIN FLANGE AT NR 3 HINGE AND NR 2 HINGE. REMOVED ALL DAMAGE PLUS COMPLETED WET LAYUP REPAIR IAW SRM AND EA. 2 L 7 2 4F RT A16WE 2002102300036 20021023 00036 NM 2002 10 23 USAA020368 1 20020924 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 447US 33372 24874 FUSELAGE SKIN CRACKED, STA 727D AT STRINGER 23L, 2.2500 CRACK. INSTALLED EXTERIOR DOUBLER IAW SRM. 2 L 7 2 4F RT A16WE 2003062500138 20030625 00138 EU 2003 6 25 USAASA02080 1 20020913 A 5410 DOOR AIRBUS A321 A321211 3930370 EU RT NACELLE UNSECURE A USAA A UNSCHED LANDING E D VIBRATION/BUFFET INFLIGHT SEPARATION CL CLIMB 1 EA 19 167US 1442 EN ROUTE DURING CLIMB, AT 6,000 FEET AGL, FLIGHT CREW NOTICED SOME VIBRATION. AT FL100, A FLIGHT ATTENDANT NOTIFIED COC KPIT CREW THAT A LARGE PIECE OF DEBRIS WAS LAYING OVER THE LEADING EDGE OF THE RGHT WING. THE FIRST OFFICER WENT BACK T O CABIN AND VERIFIED THE DEBRIS AND INDENTIFIED IT AS THE RIGHT ENGINE COWLING. THE FLIGHT RETURNED TO PHL AND PERFORME D A ZERO FLAP LANDING. NO EMERGENCY WAS DECLARED, HOWEVER, EMERGENCY EQUIPMENT WAS REQUESTED TO STANDBY. MX REPLACED T HE NR 2 ENGINE COWLINGS, AND REPAIRED THE ASSOCIATED DAMAGE CAUSED BY THE COWLINGS COMING OPEN IN FLIGHT. A SUBSEQUENT INVESTIGATION OF THE EVENT FOUND TWO POSSIBILITIES FOR THE COWLING TO COME UNLATCHES, EITHER THE COWLING LATCH MECHANISM 2 L 7 2 4F RT A28NM 2002102300037 20021023 00037 EU 2002 10 23 USAASA02083 1 20021002 A 2121 EVT3454H FAN AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE AVIONICS FAN VIBRATES A USAA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 19 742US 1275 ENROUTE, DURING CRUISE, A NOISE AND VIBRATION WERE NOTICED AROUND THE COCKPIT DOOR AREA. THIS WAS FOLLOWED BY AN ELECTR ICAL ODOR. THE CABIN FANS WERE TURNED OFF, AND THE BLOWER AND EXTRACT FANS WERE PLACED INTO OVER-RIDE. THE VIBRATION S TOPPED AND THE ODOR DISSIPATED. AN ECAM MESSAGE OF BLOWER FAULT ILLUMINATED. THE FLIGHT CONTINUED AND LANDED, WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE AVIONICS BLOWER FAN. OPERATIONALLY CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2002102300038 20021023 00038 2002 10 23 USAASB02158 4 20020820 A 2210 10622532 COUPLER BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE YAW DAMPER FAULTY A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 346US 6702 23515 ENROUTE, CLIMBING THROUGH FL210, AIRCRAFT EXPERIENCED A PULSING LEFT/RIGHT YAWING CONDITION. ONCE AUTOPILOT, AUTOTHROTT LE AND YAW DAMPER WERE OFF, YAWING STOPPED. CREW WAS UNABLE TO DUPLICATE CONDITION. PRIOR FLIGHT OF THIS AIRCRAFT WAS UNEVENTFUL. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED BITE CHECK OF A AND B AUTOP ILOTS, AUTOTHROTTLE AND YAW DAMPER SYSTEMS. NO FAULTS FOUND. YAW DAMPER COUPLER SHOWS PREVIOUS INTERMITTNET FAULT. RE MOVED AND REPLACED YAW DAMPER COUPLER PER MM. OPERATIONAL CHECK GOOD PER WORK CARD. FLIGHT DATA RECORDER WAS REMOVED A ND SENT TO SHOP FOR EVALUATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102300039 20021023 00039 NM 2002 10 23 USAASB02176 1 20020921 A 3234 HANDLE BOEING 737 737301 1384611 NM MLG LACK OF LUBE A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 574US 23739 IN PREPARATION FOR LANDING, CREW REPORTED THEY RECEIVED THREE GREEN AND THREE RED GEAR LIGHTS UPON GEAR EXTENSION. CREW RECYCLED GEAR WITH SAME SIX LIGHTS ILLUMINATING. GEAR HANDLE WAS THEN PULLED OUT AND PUSHED IN AND THE THREE RED GEAR LIGHTS EXTINGUISHED WITH THREE GREEN GEAR LIGHTS REMAINING ILLUMINATED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTE NANCE CLEANED AND LUBED THE LANDING GEAR HANDLE ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002102300040 20021023 00040 NM 2002 10 23 USAASB02177 1 20020922 A 5720 SEAL BOEING 737 7374B7 1384702 NM WING TO BODY TORN A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 433US 24555 DURING CLIMB OUT, ENROUTE, AIRCRAFT DEVELOPED A MODERATE LATERAL AIRFRAME VIBRATION. VIBRATION OCCURRED AT ALL SPEEDS B ETWEEN 235 AND 335 KNOTS, WITH OR WITHOUT AUTOPILOT. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED LEVEL 1 GENERAL INSPECTION IAW SL. ACCOMPLISHED BITE TEST OF YAW DAMP ER COUPLER. NO FAULTS NOTED. CHECKED ELEVATOR TAB HINGES AND ROD ENDS FOR EXCESSIVE WEAR. NO WEAR NOTED. ACCOMPLISHE D VISUAL INSPECTION OF AIRCRAFT AND FOUND A TORN WING TO BODY FAIRING SEAL. ALSO, FOUND LEFT WING TIP SEALANT BLOWN OUT AND MISSING AROUND LEADING EDGE. APPLIED SEALANT TO BOTH AREAS AND RESEALED. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2002102300041 20021023 00041 NM 2002 10 23 USAASB02182 1 20020927 A 4900 GTCP85129E APU BOEING 737 7373B7 1384580 NM APU BAY FAILED A USAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 19 530AU 43840 92 24412 DURING CRUISE, ENROUTE, NR 2 GEN OFF BUS BLUE LIGHT ILLUMINATED. NR 2 BUS OFF YELLOW LIGHT DID NOT ILLUMINATE. NO POWE R WAS BEING PRODUCED FROM NR 2 GENERATOR. CREW STARTED APU AND POWERED RIGHT BUS. APU LOW OIL QUANTITY LIGHT ILLUMINA TED FOLLOWED BY LOW OIL PRESSURE LIGHT AND HIGH OIL TEMPERATURE LIGHT, RESULTING IN AN APU AUTO SHUTDOWN. FLIGHT DIVERT ED, LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED APU ASSEMBLY. OPERAT IONAL CHECK AND LEAK CHECK GOOD. REMOVED AND REPLACED NR 2 GENERATOR CONTROL UNIT, NR 2 GENERATOR AND BUS TIE CIRCUIT BREAKER C802 AND TRANSFER BUS CONTROL RELAY R350. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002102300042 20021023 00042 2002 10 23 USAASB02186 4 20020930 A 2565 D31591478 SLIDE BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE ESCAPE SLIDE MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 394US 42418 3865 23316 DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE APPEARED TO HAVE PREMATURELY I NFLATED AND BECAME TWISTED 90 DEGREES. DOOR BECAME DIFFICULT TO OPEN FULLY ONCE SLIDE BEGAN TO INFLATE. SLIDE OPERATIO NAL CHECK FAILED. MAINTENANCE DETERMINED THE FORWARD RIGHT SERVICE DOOR WAS NOT OPENED BRISKLY ENOUGH TO PROPERLY DEPLO Y ESCAPE SLIDE. MAINTENANCE REMOVED AND REPLACED THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE ASSEMBLY. TWO ADDITIONAL OPERATIONAL CHECKS ARE SCHEDULED TO BE PERFORMED AT THE FORWARD RIGHT SERVICE DOOR POSITION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102300043 20021023 00043 EA 2002 10 23 VJ32002F00082 2 20021004 A 7310 75283 VALVE GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA MANIFOLD FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 864AF 447 85004 L2826348A DURING FLIGHT THE CHT IS CONSISTENTLY HIGH DURING ALL LEVELS OF FLIGHT. PROBABLE CAUSE IS INTERNAL FAILURE OF MANIFOLD VALVE NOT ALLOWING FUEL FLOW PROPERLY. 1 L 7 1 3O 3 O RT A49CE 1E4 2002102300044 20021023 00044 CE 2002 10 23 VJ32002F00083 1 20021004 A 3610 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO DRY AIR FAILED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 5609S 765 CE1454 825756R DURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT U P AND AIR PRESSURE STILL LOW AT HIGHER RPM. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP. 1 L 7 1 3O 3 O 3A15 E5CE 2002102300045 20021023 00045 EU 2002 10 23 VJ32002F00084 1 20021004 A 8097 14924PM TERMINAL BLOCK GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA STARTER LOOSE B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 864AF 448 85004 L2826348A DURING PROGRESSIVE INSPECTION OF ENGINE FOUND TERMINAL STUD ON STARTER SOLENOID LOOSE. 1 L 7 1 3O 3 O RT A49CE 1E4 2002102300046 20021023 00046 CE 2002 10 23 VJ32002F00085 1 20021004 A 3210 LANDING GEAR BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MALFUNCTIONED B VJ3R O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 5544A 753 CE1343 825767R LANDING GEAR WOULD NOT RETRACT DURING A FLIGHT. 1 L 7 1 3O 3 O 3A15 E5CE 2002102300047 20021023 00047 CE 2002 10 23 VJ32002F00086 1 20021004 A 5500 0024400237 BULKHEAD BEECH 33 F33A 1151425 CE CONT O520 IO520* 17032 SO EMPENNAGE CRACKED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 38071 21177 CE935 DURING PROGRESSIVE INSPECTION OF THE EMPENNAGE SECTION OF THIS AIRCRAFT, A MECHANIC FOUND A CRACK IN THE RADIUS BEND ARE A UPPER LEFT CORNER OF THE BULKHEAD. 1 L 7 1 3O 3 O 3A15 E5CE 2002102300048 20021023 00048 CE 2002 10 23 VJ32002F00087 1 20021004 A 5500 0024400237 BULKHEAD BEECH 33 F33A 1151425 CE CONT O520 IO520* 17032 SO ENPENNAGE CRACKED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 6311Z 19291 CE997 DURING A PROGRESSIVE INSPECTION OF THE EMPENNAGE SECTION OF THIS AIRCRAFT A MECHANIC FOUND A CRACK IN THE RADIUS BEND AR EA UPPER LEFT CORNER OF THE BULKHEAD. 1 L 7 1 3O 3 O 3A15 E5CE 2002102300049 20021023 00049 EA 2002 10 23 WRLA200211 1 20020527 A 2710 ARH7057515 ACTUATOR WACO GXE GXE 9600702 EA AILERONS INOPERATIVE A WRLA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 11 2710 1252 LEVEL 2 AILERON DEFLECT DISAGREE. (AIRCRAFT RETURNED TO DEPARTING STATION) TROUBLESHOOTING CARRIED OUT. GENERAL VISUA L INSPECTION OF ALL AILERON DEFLECTION ACTUATOR CONNECTORS AND PINS CARRIED OUT. NO DEFECTS NOTED. LEVEL 2 MESSAGE CLE ARED. SYSTEM OK, OPS CHECK CARRIED OUT SATISFACTORY. REPLACED LEFT HAND OUTBOARD DEFLECTED AILERON ACTUATOR. 1 Q 7 1 3V 2363 2002102300051 20021023 00051 NM 2002 10 23 WRLA200213 1 20020614 A 3020 32138683 ANTI-ICE VALVE DOUG MD11 MD11 3023602 NM NR 2 ENGINE INOPERATIVE A WRLA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 278WA 48746 ENGINE 2 ANTI-ICE DUCT, LEVEL 3 ALERT DISPLAYED ON CLIMB OUT. FOLLOWED VOL 1. DUMPED FUEL, RETURNED TO LAND. NR 2 MAN IFOLD FAILED. NR 2 ENGINE SHUT DOWN. INSPECTED A-ICE DUCT FROM 15TH STAGE FORWARD. FOUND NO PHYSICAL DEFECTS IN DUCKI NG. REPLACED TEMPERATURE SENSOR. REPLACED GCU. REPLACED EPCU. REPLACED RELAYS. REPLACED DUCT FAIL SENSORS. REPLACE D ANTI-ICE VALVE. REPLACED TEMPERATURE SENSOR. REPLACED EPCU. REPLACED GCU. REPLACED RELAYS FOR ANTI-ICE VALVE. REP LACED DUCT FAILED SENSORS. REPLACED ANTI-ICE VALVE. ANTI-ICE VALVE AND PRESSURE SWITCH. 2 L 7 3 4F RT A22WE 2002102300052 20021023 00052 WP 2002 10 23 WRLA200214 1 20020701 A 5230 SEAL DOUG DC10 DC1030F 3023504 WP CARGO DOOR LOOSE A WRLA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 11 304WL 47928 CABIN ALTITUDE WENT TO 11,000 FEET UNABLE TO MAINTAIN CABIN PRESSURE. (RETURNED TO STATION.) FOUND FORWARD AND CENTER LOWER CARGO DOOR SEAL PUSHED OUT. REINSTALLED DOOR SEAL, PRESSURE CHECKED AIRCRAFT, AIRCRAFT PRESS CHECK GOOD. REINSTA LLED DOOR SEAL. LOOSE DOOR SEAL. 2 L 7 3 4F RT A22WE 2002102300053 20021023 00053 NM 2002 10 23 WRLA200215 1 20020702 A 2710 ARH705454515 ACTUATOR DOUG MD11 MD11 3023602 NM AILERON INOPERATIVE A WRLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 272WA 48437 AILERON DEFLECT DISAGREE LEVEL ALERT AFTER TAKE OFF AND AT SLAT RETRACT. SLATS AND FLAPS (15) RECYCLED WITH ALERT REMAI NING. CONFIG. PAGE AND VISUAL SCAN CONFIRMED LEFT OUTBOARD AILERON WAS DEFLECTED. CHECK LIST PREFORMED AND RETURNED TO STATION. ENTERED INOT DMI, COMPLIED WITH MAINTENANCE PROCEDURES. NOTED: FOUND AILERON ACTUATOR OPERATING NORMAL PROCE DURES, ALL OTHER AILERON PARAMETERS SHOW NORMAL AT THIS TIME. REMOVED AND REPLACED AILERON ACTUATOR WITH FIXED PUSH ROD . 2 L 7 3 4F RT A22WE 2002102300054 20021023 00054 NE 2002 10 23 WRLA200216 2 20020703 A 7532 1115V07006 BLEED VALVE DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE NR 2 ENGINE INOPERATIVE A WRLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 11 278WA 48746 HIGH EGT NR 2 ENGINE 655 DEGREE C, REJECTED TAKE OFF AT 90 KNOTS. FOUND LHS 2.9 BLEED VALVE, INOPERATIVE REMOVED AND RE PLACED 2.9 BLEED PREFORMED ENGINE RUN TO 1.6 EPR MAX EGT REACHED WAS 633 DEGREE IN TRANSITION. IT CORRECTED AND STABILI ZED AT 627 DEGREE. N1 102 PERCENT, N2 101 PERCENT, FF 23160 PART NUMBER ON/OFF 1115V07006, SERIAL NUMBER ON 134 SERIAL NUMBER OFF 2428 TAT +29 DEGREE C. REMOVED AND REPLACED 2.9 BLEED VALVE. 2 L 7 3 4F 4 F RT A22WE E24NE 2002102300055 20021023 00055 WP 2002 10 23 WRLA200217 1 20020707 A 7714 47327 SENSOR DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 1 ENG N1 ERRATIC A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 304WL 47928 ENGINE FAIL CAUTION LIGHT ILLUMINATED DURING TAKE OFF DUE TO NR 1 ENGINE N1 TACH GIVING ERRATIC INDICATIONS. (REJECTED TAKE OFF AT 70 KNOTS.) REMOVED AND REPLACED NR 1 ENGINE FAN SPEED SENSOR , RAN ENGINE NR 1 UP TO 85 PERCENT NR 2, FOUN D NO ERRATIC FLUCTUATION ON N2 INDICATOR, BOTH NR 1 AND NR 2 STABILIZED ON INDICATORS. OPS CHECK NORMAL. 2 L 7 3 4F 4 F RT A22WE E23EA 2002102300056 20021023 00056 NM 2002 10 23 WRLA200218 1 20020727 A 5312 BULKHEAD DOUG MD11 MD11 3023602 NM FUSELAGE DENTED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 FOUND DENT WITH .375 INCH CRACK DURING C4 CHECK AT FUSELAGE STATION 2007.00 ON AFT. PRESSURE BULKHEAD. OUTBOARD OF X = 10.0 AND BELOW Z = 10.0. CUT OUT DAMAGED AREA, DIMENSION L = 1.25 X W = 0.75. ALL JOB ACCOMPLISHED. REPAIRED CRACK O N AFT PRESSURE BULKHEAD AT STA 2007. 2 L 7 3 4F RT A22WE 2002102300057 20021023 00057 NM 2002 10 23 WRLA200220 1 20020816 A 5751 NRC6043502M STRUCTURE DOUG MD11 MD11 3023602 NM RT AILERON TE DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 279WA 48756 RT INBOARD AILERON IS DAMAGED. TRAILING EDGE IS MISSING FOUND ON WALK AROUND. REMOVED AND REPLACED RT INBOARD AILERON. 2 L 7 3 4F RT A22WE 2002102300058 20021023 00058 WP 2002 10 23 WRLA200221 1 20020829 A 2497 TERMINAL DOUG DC10 DC1030 3023501 WP GE CF6 CF645A2 30020 NE ACCY BAY BURNED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 14075 46922 DURING PREFLIGHT SERVICING, AC BUS NR 1 CIRCUIT BREAKERS POPPED. FURTHER NOTED TERMINAL STRIP BURNED IN CENTER ACCESSOR Y COMPARTMENT. ACCOMPLISHED ALL NECESSARY REPAIRS. REPLACED THE FOLLOWING COMPONENTS REPAIRED TERMINAL STRIP S3521, LU GS ON FEEDER TO THE TERMINAL STRIP AND DATA PLATE FOR TERMINAL STRIP. WITH INSPECTION OF THE FEEDERS AND INSULATION. T HE FOLLOWING OTHER COMPONENTS WERE REPLACED DC BUS TIE C/B NR 1 (B15), AC BUS NR1 B PHASE C/B (B17) AND AC BUS NR 1 C PH ASE C/B (B18). REPLACED COMPONENTS, TERMINAL STRIP. 2 L 7 3 4F 4 F A22WE E23EA 2002102300059 20021023 00059 NE 2002 10 23 WRLA200223 2 20020916 A 7200 ENGINE DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE NR 2 FAILED A WRLA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION NR NOT REPORTED 1 SO 11 271WA 13733 48518 P733792 NR 2 ENGINE COMPRESSOR STALLS OR HIGH VIBRATION AT TOP OF CLIMB FL320 - FL330. SHUT DOWN PER CHECK LIST PARAMETERS. EV M TURB 1.6, N1 VARIABLE, EPR (DOWN) .7, N2 VARIABLE, EGT (ABOVE) 550, FUEL FLOW HIGH VIBRATION STOPPED WITH POWER BACK T O IDLE (AFTER APPROXIMATELY 2 MINUTES) ACCOMPLISHED BORESCOPE INSPECTION OF NR 1 AND 3 ENGINES AT ANC AND NO DEFECTS NO TED ON BOTH ENGINES. (AIRCRAFT REPOSITIONED TO XNA FOR ENGINE CHANGE). NR 2 ENGINE REMOVED AND REPLACED AT XNA. INSTA LLATION, OPS CHECK, LEAK CHECK AND RII ACCOMPLISHED. ENGINE INTERNAL FAILURE. 2 L 7 3 4F 4 F RT A22WE E24NE 2002110100097 20021101 00097 EA 2002 11 1 COMA0260566 1 20021005 A 5512 6002113345 FAIRING CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB VIBRATES A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 932CA 7038 CONSTANT VIBRATION IN CONTROL COLUMN. REPLACED THE RIGHT LOWER AND THE LEFT UPPER HORIZONTAL STAB VISOR FAIRINGS. 2 L 7 2 4F RT A21EA 2002102300065 20021023 00065 NM 2002 10 23 UPS02239561 1 20020917 A 5320 FORK BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 STRINGER TIE CRACKED BS 870 STRINGER 1 FWD SIDE. NEW STRINGER TUNING FORK INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2002102300066 20021023 00066 NM 2002 10 23 UPS02239762 1 20020915 A 5230 651862587 DOOR FRAME BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 SUSPECT CRACK ON AFT LWR CARGO DOOR, CRACK IS LOCATED ON LOWER AFT CORNER JUST INSIDE NR 1 AFT DOOR STOP. HFEC CONFORMS CRACK, CARGO LOWER AFT FRAME REPLACED IAW DWG 65-18625. 2 L 7 3 4F A3WE 2002102300067 20021023 00067 NM 2002 10 23 UPS02239767 1 20020930 A 5743 BEAM BOEING 727 72722C 138400F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 DURING REMOVAL OF T/E PANEL ATTACHED TO LOWER SURFACE OF RT MLG SUPPORT BEAM, CORROSION NOTED AROUND MLG SUPPORT BEAM FA STENER HOLE. CORROSION REMOVED AROUND HOLE IAW SRM 51-10-06. HFEC C/O ON FASTENER HOLE AND COUNTER BORE IN THE ABOVE A REA IAW B727 N DTM PT 6 51-00-00 FIG 4 AND FIG 16 - NDF. FREEZE PLUG INSTALLED IAW SRM 51-10-019 AND SMRO EO 2002-052-0 19. UPS ENGINEERING FILE NR 727-57-20063. 2 L 7 3 4F A3WE 2002102300069 20021023 00069 NM 2002 10 23 UPS02239768 1 20020923 A 5314 KEELBEAM BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 CRACKS RT KEEL BEAM VERTICAL WEB FWD OF APU CUT OUT. REPAIR IAW EO B727-5330-1995-B. 2 L 7 3 4F A3WE 2002110100107 20021101 00107 NE 2002 11 1 COMA0260592 2 20021018 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RIGHT MALFUNCTIONED A COMA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 931CA 14905 7037 807324 FLIGHT 5847 SMOKE IN CABIN. REPLACED THE RT ENGINE. EVIDENCE OF OIL AROUND VG ACTUATOR SPINDLE, SUSPECT NR 3 CARBON SE AL FAILURE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002102300070 20021023 00070 NM 2002 10 23 UPS02239769 1 20021003 A 5711 SPAR BOEING 727 72722C 138400F NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 DURING PREPARATION FOR CENTER SECTION REAR SPAR WEB SPLICE REPAIR, ADDITIONAL CORROSION WAS NOTED ON UPPER CHORD INBOARD OF LBL 34.20. WEB, CHORD, SPLICE AND STIFFENERS FABRICATED IAW DRG NR 65C21531 REPAIR COMPLETED IAW SMRO EO 2002-052-0 13. UPS ENG FILE NR B727-5710-177 09-A. 2 L 7 3 4F A3WE 2002102300071 20021023 00071 NM 2002 10 23 UPS02239770 1 20020918 A 5542 65727889 SKIN BOEING 727 72722C 138400F NM RUDDER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 LWR RUDDER LEFT SKIN CORRODED AT TS 141.6. CORROSION AND DELAMINATION FOUND ON LOWER RUDDER, LEFT SIDE, UPPER PANEL, A FT UPPER CORNER. REPLACED RUDDER IAW MM 27-20-01. 2 L 7 3 4F A3WE 2002102300072 20021023 00072 NM 2002 10 23 UPS02239773 1 20020924 A 5514 HINGE PIN BOEING 727 72722C 138400F NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 HORIZONTAL STAB HINGE LEFT OUTER PIN HAS EVIDENCE OF PITTING CORROSION ADJACENT TO RELIEF RADIUS. HORIZONTAL STABILIZER HINGE PIN LEFT OUTER REPLACED IAW MM 55-10-01 STEPS 3 AND 4. 2 L 7 3 4F A3WE 2002102300073 20021023 00073 NM 2002 10 23 UPS02439517 1 20020907 A 5320 BRACKET BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 LEFT BLG W/W O/B SIDEWALL BELOW LOWER CHORD ATTACH BRACKET CORROSION REVEALED AT STA 1394 LBL 122-130. CORROSION REMOVE D IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDED SRM 53-10-01 FIG 1 LIMITS. BRACKET REPLACED PER SRM 51-10 -01. 2 L 7 4 4F A20WE 2002102300074 20021023 00074 NM 2002 10 23 UPS02439518 1 20020907 A 5320 WEB BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 U/D FLOOR WEB FOUND CORRODED AT FLANGE AREA. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT EXCEEDED SRM 53-10 -01 LIMITS WEB REPAIR REFER SRM 51-40-03 FIG 3. 2 L 7 4 4F A20WE 2002102300075 20021023 00075 NM 2002 10 23 UPS02439519 1 20020907 A 5312 654U6624227 SPLICE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 RT BS 1480 BULKHEAD AREA HOLE NR 23 CRACK FOUND AT OUTER CHORD SPLICE FITTING APPROX .125 INCH RUNNING INBOARD AND OUTBO ARD STR R33 TO R34, RT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING HOLE NR 23 REWORKED AND CRACK FREE, OUT OF SB 'D' MAX LIMIT. NEW OUTER CHORD SPLICE FITTING REPLACED AS PER SRM 51-30-04. 2 L 7 4 4F A20WE 2002102300076 20021023 00076 NM 2002 10 23 UPS02439520 1 20020907 A 5312 65B152476 SPLICE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RT BS 1480 BULKHEAD AREA HOLE 23 CRACK FOUND AT WEB SPLICE PLATE APPROX .125 INCH RUNNING I/B AND O/B STR R33 TO R34. RT BS 1480 BULKHEAD WEB SPLICE PLATE REPLACED AS PER SRM 51-30-04 DUE CRACKED HOLE REWORKED AND OUT OF SB 747-53A2390 'D' MAX LIMIT. 2 L 7 4 4F A20WE 2002102300077 20021023 00077 NM 2002 10 23 UPS02439523 1 20020906 A 5312 PRESSURE PANEL BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RT WLG W/W KEEL BEAM TOP PANEL CORROSION REVEALED AT STA 1275-1350 RBL 0-10. CORROSION REMOVED IAW S RM 51-10-01, CORROSION BLEND OUT EXCEEDED SRM 53-10-01 FIG 1 LIMITS. WEB REPAIRED AT STA 1345 RBL 8. 2 L 7 4 4F A20WE 2002102300078 20021023 00078 NM 2002 10 23 UPS02439527 1 20020912 A 5320 65B150381 SPLICE BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RT OVERWING LONGERON LWR INBOARD SPLICE FITTING AT BS 1460 - 1480 FOUND CORRODED AFTER SPLICE FITTING REMOVED FOR CORROSION CLEAN UP ACCESS (RBL 113). SPLICE FITTING REPLACED AS PER SRM 51-30-04 DUE CORROSION EXCEED SRM 5 3-10-01. 2 L 7 4 4F A20WE 2002102300079 20021023 00079 NM 2002 10 23 PCAA0210123 1 20021021 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM POWER LOSS A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 805EX 25807 24809 228 DURING ROUTINE MAINTENANCE VISIT RIGHT LOWER FORWARD EMERGENCY EGRESS LIGHT (EXTERIOR) AND ONE EMERGENCY OVERHEAD AISLE LIGHT (2ND AFT) AND ENTRY WAY EXIT LIGHT FOUND INOPERATIVE. BATTERY AND POWER SUPPLY AT POSITION 200 REPLACED ALONG WITH ALL ASSOCIATED LIGHT BULBS. OPERATIONAL CHECK GOOD.AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002102300080 20021023 00080 NM 2002 10 23 UPS02439528 1 20020909 A 5320 REVEAL BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D- BS 2230 - 2240, S17-18L, 5L CUTOUT FWD STOP FITTING REVEAL FOUND CRACK. REVEAL PANEL REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2002102300081 20021023 00081 NM 2002 10 23 UPS02439531 1 20020921 A 3350 LIGHT BOEING 747 747200 1384847 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 528UP 1 INSPECTION TYPE AS, EMERGENCY LIGHT FWD OF MAIN ENTRY DOOR INOP. RELAMPED, OPS CHECK GOOD. 2 L 7 4 4F RT A20WE 2002102300082 20021023 00082 2002 10 23 BAQA081097 4 20021003 A 3160 L316M30C1002 DISPLAY UROCOP EC135 EC135P1 8680990 EU COCKPIT INOPERATIVE H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 577LF 189 0140 NUMEROUS SEGMENTS INOPERATIVE. WEIGHT/VNE INOPERATIVE. NO HARD CARD AVAILABLE. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U O H88EU 2002102300083 20021023 00083 NM 2002 10 23 VNAA0210007 1 20021010 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 432JS 3045 DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION MESSAGE AND ABORTED TAKEOFF. WHEN EXITING THE RUNWAY, THE MES SAGE CLEARED. FLIGHT 4140 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4140 DEPARTED WITH NO FURTHER INCIDENTS . 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002102300084 20021023 00084 SW 2002 10 23 BAQA081139 1 20021014 A 2422 SPS1307 INVERTER BELL 222 222U 1182140 SW AC SYSTEM INOPERATIVE H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 219HM 47573 INVERTER INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H9SW 2002102300085 20021023 00085 NM 2002 10 23 VNAA0210008 1 20021010 A 2425 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 433JS 3047 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR AND ECU FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE MESSAGE CLEARED. FLIGHT 4064 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGH T 4064 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002102300086 20021023 00086 NM 2002 10 23 VNAA0210009 1 20021011 A 3242 BRAKE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT MLG MALFUNCTIONED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 463PS 3087 THE CREW REPORTED THERE WAS NO BRAKING ACTION FROM THE RIGHT HAND BRAKES. MAINTENANCE INSPECTED AND BLED THE BRAKES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FO R SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002102300087 20021023 00087 2002 10 23 BAQA081143 4 20021016 A 3421 5040035921 GYRO UROCOP EC135 EC135P1 8680990 EU ATTITUDE INOPERATIVE H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 135ME 80 0009 INOPERATIVE AND CONNECTOR PLUG PULLED OUT. INSTALLED SERVICEABLE UNIT. 1 G 7 2 3U O H88EU 2002102300088 20021023 00088 EA 2002 10 23 COMA0260594 1 20021021 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS CL CLIMB 1 SO 01 914CA 7012 FLIGHT 5850 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT. I/A/W AD 98-20-01. 2 L 7 2 4F RT A21EA 2002102300089 20021023 00089 EA 2002 10 23 COMA0260595 1 20021021 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 807CA 7364 FLIGHT 5420 EMERGENCY LIGHT ON CEILING IS INOP.DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2002102300090 20021023 00090 WP 2002 10 23 IXXA0200090O 1 20021023 A 3610 D51P581119 DUCT DOUG DC8 DC871F 302199D WP 9TH STAGE DAMAGED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 827BX 83816 2348 45971 AFTER TAKE OFF FROM ANC, THE FIRE WARNING LIGHT ILLUMINATED AND THE AUDIO WARNING SOUNDED FOR THE NUMBER THREE ENGINE. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND SECURED THE ENGINE. THE FLIGHT RETURNED TO ANC FOR AN UNEVENTFUL LANDIN G. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE DUCT ASSEMBLY FOR THE NINTH STAGE BLEED AIR RUPTURED. ADDITIONA L INSPECTION FOUND THE THRUST REVERSER INNER HEAT SHIELD WITH NOMINAL DAMAGED. MAINTENANCE REPLACED THE DUCTS AND PERFOR MED SUCESSFUL OPERATIONAL CHECKS IN ACCORDANCE WITH THE DOUGLAS MAINTENANCE MANUAL. CFMI SUGGESTED MAINTENANCE PLACED TH E THRUST REVERSER ON DEFERRAL IN INCORDANCE WITH COMPANCY PROCEDURES FOR REPAIRS AT THE NEXT MAINTENANCE STATION. MAINTE 2 L 7 4 4F RT 4A25 2002102300091 20021023 00091 NM 2002 10 23 VNAA0210010 1 20021012 A 2160 5413C000 CONTROL VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN TEMP FAILED A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 471PS 17466 3007 EN ROUTE TO BNA, THE CAPTAIN REPORTED THAT THE TEMPERATURE WAS RISING IN THE CABIN AND FLIGHT 4094 WAS DIVERTING TO PIT. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND TEMPERATURE CONTROL VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANU AL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002102300092 20021023 00092 NM 2002 10 23 VNAA0210012 1 20021013 A 3350 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN INOPERATIVE A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 434JS 3051 THE CREW REPORTED THAT THE EMERGENCY LIGHTING STRIP AT ROW 9A WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE LIGHTING STRIP AT ROW 9A IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002102300093 20021023 00093 NM 2002 10 23 VNAA0210014 1 20021014 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 431JS 119 3028 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 4, 5, AND 6 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPL ACED THE 5LK EMERGENCY BATTERY AND POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CH ECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002102300094 20021023 00094 NM 2002 10 23 VNAA0210015 1 20021015 A 3150 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 432JS 3045 DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. THE CREW EXITED THE RUNWAY A ND RECONFIGURED THE AIRCRAFT AND WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4078 THEN DEPARTED WITH NO FURTHER INC IDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002102300095 20021023 00095 NM 2002 10 23 VNAA0210016 1 20021015 A 2450 230GC02Y02 CONTROL PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAULTY A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 470PS 9111 51 3006 THE FLIGHT ATTENDANT REPORTED A BURNING SMELL IN THE CABIN WHILE INBOUND TO PIT. THE CAPTAIN THEN REPORTED THE BURNING SMELL WAS INTO THE COCKPIT BY THE TIME FLIGHT 4014 REACHED THE GATE. MAINTENANCE INSPECTED AND FOUND THE EXTERNAL POWER CABLE LEADING TO THE 1VE PANEL VERY HOT AND CREATING THE BURNING SMELL. MAINTENANCE THEN REPLACED THE 1VE PANEL IN ACC ORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR S ERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002102300096 20021023 00096 NM 2002 10 23 VNAA0210018 1 20021017 A 3350 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN BROKEN A VNAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 470PS 3006 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING STRIP WAS BROKEN. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY FLOOR LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002102300097 20021023 00097 NM 2002 10 23 UPS02239765 1 20020917 A 5330 6561611 PLUG BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 CORROSION FOUND ON 3RD WINDOW PANEL BLANK FROM AFT END LEFT SIDE EXTERIOR SURFACE LOWER ENDS AND 7TH FRAME FROM AFT END ABOVE STR 14L. WINDOW PLUG REPLACED IAW MM 56-20-00. WINDOW PLUG REPLACED DUE TO CORROSION EXCESSIVE, HOWEVER NO LIMIT S EXIST PER SRM. CORROSION EXCEEDS 10 PERCENT MATERIAL THICKNESS IAW STANDARD PRACTICES. 2 L 7 3 4F A3WE 2002102300098 20021023 00098 WP 2002 10 23 UPS02839384 1 20020906 A 5312 9887427150 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:N/A LEFT WHEEL WELL AFT FLAP ENCLOSURE, WEB ASSY ON AFT PORTION WHERE ACT RETRACTS IS CRACKED IN UPPER R ADIUS. LOCATED & DRILLED NEW WEB FABRICATED NEW STIFFENER FOR SPOILER A PULLEY BRACKET ON I/B WEB PANEL, FABRICATED PER DC-8 SRM 51 W 18126. INSTALLED NEW WEB & STIFFENER PER DC8 SRM 51-1-21 2 L 7 4 4F RT 4A25 2002102300099 20021023 00099 WP 2002 10 23 UPS02839386 1 20020906 A 5320 564340219 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:N/A VERTICAL ANGLE CRACKED LT MLG WHEEL WELL. LOCATED & DRILLED NEW ANGLE WA 18126. INSTALLED PER DC-8 SRM 51-1-20 & 51-1-21. 2 L 7 4 4F RT 4A25 2002102300100 20021023 00100 WP 2002 10 23 UPS02839390 1 20020826 A 5320 4758514507 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1240 LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758 514, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102300101 20021023 00101 WP 2002 10 23 UPS02839391 1 20020820 A 5330 564932975N2 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 AFT LOWER FUSELAGE SKIN IS CRACKED AT STA 1800 LONG 33. REMOVED AND REPLACED SKIN BETWEEN STA 1690 T O 1890 LONG 28L TO 28R IAW DWG 5649329, SRM 51-1-21, 51-1-20D, 53-1-0. 2 L 7 4 4F RT 4A25 2002102300102 20021023 00102 WP 2002 10 23 WRNA200200007 1 20021022 A 2612 47226001 FIRE LOOP RROYCE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE #1 ENGINE SHORTED A WRNA E F J A ENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 311EA 10598 193A1012 10598 Enroute to BDL @ approx. 270fl, A&B fire loop on #1 engine came on. Engine fire lights came on and fire bell. Bell silen ced, #1 engine shutdown per procedures. Alt fire bottle discharged, light remained in handle, Main bottle discharged lig ht remained on. Fuel dumped, returned to BQN, landed normal. Red fire handle light remained on thru landing and taxi to gate.Corrective Action: Inspected and found A loop engine gear case sensor (loop) shorted. R&R'd loop I/A/W 26-11-01. Re placed engine firex bottles. Run up Engine checks satisfactory. Aircraft returned to service. 2 L 7 3 4F 4 F A23WE E12EU 2002102300103 20021023 00103 EU 2002 10 23 BAQA081170 1 20021018 A 6730 L673M40A1001 ACTUATOR UROCOP EC135 EC135T1 5620026 EU TAIL ROTOR LEAKING H BAQA K NONE K FLUID LOSS IN INSP/MAINT 1 FS 01 575ME 387 0157 ACTUATOR LEAKING. BEARINGS WORN IN INPUT LEVER. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2002102300104 20021023 00104 WP 2002 10 23 UPS02839408 1 20020820 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 DENT IN FUSELAGE SKIN AFT OF L4 DOOR. COLD WORKED AND BLENDED IAW DC-8 SRM 53-2-0, WITHIN LIMITS. N O CRACK NOTED IAW DAC NDT SRM 06-10-01.001. FABBED IAW DC-8 SRM 53-2-1 FIG 10. REPAIRED DENT IAW DC-8 SRM 53-2-1 FIG 1 0. 2 L 7 4 4F RT 4A25 2002102300105 20021023 00105 EU 2002 10 23 XNOA01082 1 20021022 A 3230 A25199 VALVE AIRBUS 300 A300B4203 3930306 EU A XN0A O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 370PC 2423 134 ON FINAL APPROACH INTO KMCO LANDING GEAR WOULD NOT EXTEND WHEN GEAR HANDLE WAS PLACED IN EXTEND POSITION. FOLLOWED QRH & PERFORMED MANUAL EXTENSION. AIRCRAFT HAS BEEN INSPECTED AND FOUND SAFE FOR INTENDED FERRY FLIGHT TO KMIA. GEARS TO REMA IN EXTENDED DOWN THROUGHOUT FLIGHT. ACTION TAKEN: REMOVED & REPLACED LANDING GEAR ELECTRO VALVE IAW AMM 32-31-12. PERFOR MED NORMAL EXTENSION AND RETRACTION TEST IAW AMM 32-30-00 PG. 501. VALVE OPS & LEAK CHECKS GOOD. GEAR EXTENSION & RETRAC TION TESTS GOOD. 2 L 7 2 4F RT A35EU 2002102300106 20021023 00106 EA 2002 10 23 COMA0260596 1 20021020 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA #3 MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS UK UNKNOWN 1 SO 01 987CA 11567 7199 FLIGHT 9450 GEAR DISAGREE WHILE OPERATING ON A.D.G.REPLACED THE #3 HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A21EA 2002102300107 20021023 00107 EA 2002 10 23 COMA0260597 1 20021020 A 4990 APU CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 918CA 7018 FLIGHT 5502 APU OIL PRESSURE CAUTION MESSAGE.COULD NOT DUPLICATE. OPERATIONAL CHECK OF APU WAS NORMAL. 2 L 7 2 4F RT A21EA 2002102300108 20021023 00108 EA 2002 10 23 COMA0260598 1 20021020 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 409CA 7441 FLIGHT 5079 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.COULD NOT DUPLICATE. DOOR OPERATION WAS NORMAL. 2 L 7 2 4F RT A21EA 2002102300109 20021023 00109 EA 2002 10 23 COMA0260599 1 20021019 A 3350 6464 POWER CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR INOPERATIVE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 821CA 7420 FLIGHT 5576 EMERGENCY LIGHTS INOP AT ROWS 6,7, AND 8REPLACED CABLE ASSY AT ROWS 6 THRU 8. 2 L 7 2 4F RT A21EA 2002102300110 20021023 00110 NM 2002 10 23 UPS02439550 1 20020905 A 5320 ANGLE BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LT WLG W/W FWD BULKHEAD UPPER AREA BELOW DRAIN V/V CORROSION REVEALED AT STA 1241 LBL 103. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDED SRM 57-10-01 LIMITS, WEB ANGLE REPAIR CARRIED OUT PER HX RS NR R 53-43-34905, AND RA NR 747-53-20107. 2 L 7 4 4F A20WE 2002102300111 20021023 00111 EA 2002 10 23 COMA0260600 1 20021018 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING E O VIBRATION/BUFFET OTHER CL CLIMB 1 SO 01 929CA 7035 FLIGHT 5063 LOUD WHISTLING COMING FROM R/H FORWARD SIDE OF AIRCRAFT.FOUND GROUND INTERPHONE DOOR OPEN - INSPECTED FOR DA MAGE AND CLOSED DOOR. 2 L 7 2 4F RT A21EA 2002110100109 20021101 00109 EA 2002 11 1 COMA0260593 1 20021021 A 5610 NP1393221 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 786CA 17364 7333 FLIGHT 5571 LT WINDOW HEAT CAUTION MESSAGE. REPLACED LT SIDE WINDOW. 2 L 7 2 4F RT A21EA 2002102300112 20021023 00112 NM 2002 10 23 UPS02439552 1 20020905 A 5320 REVEAL BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D- BS 2231, STR 24L REVEAL PANEL FOUND CRACK. M/D BS 2231 LT FRAME DOOR REVEAL AT S24L AREA REPAIR CARRIED OUT AS PER HX RS NR R-53-62-34896, AND EO B747-5310-17606-A. 2 L 7 4 4F A20WE 2002102300113 20021023 00113 NM 2002 10 23 UPS02439576 1 20020909 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RT BLG W/W STA 1360 TO STA 1372 S33R OVERWING LONGERON UPPER BONDED SKIN FOUND CORRODED. CORROSION RE MOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDED SRM 53-30-01 FIG 1 LIMITS, SKIN REPAIR CARRIED OUT AS PER HX RS NR R53-41-34906 AND RA NR 747-53-20110. 2 L 7 4 4F A20WE 2002102300119 20021023 00119 NM 2002 10 23 F3LA200200330 1 20021008 A 5753 SKIN BOEING 737 7372L9 1384497 NM T/E FLAP GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 2050 22733 DURING C-2 CHECK, INSPECTION REPORTED RT. WING INBD FOREFLAP, INBD UPPER SURFACE, GOUGED IN 2 AREAS. FABRICATED AND INS TALLED DOUBLER PER SRM 51-40-20. 2 L 7 2 4F RT A16WE 2002102300120 20021023 00120 NM 2002 10 23 F3LA200200331 1 20021008 A 5753 SKIN BOEING 737 7372L9 1384497 NM T/E FLAP GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 2050 22733 DURING C-2 CHECK, INSPECTION REPORTED RT. WING OTBD FOREFLAP UPPER SURFACE GOUGED AT WBL 314. REMOVED EXISTING REPAIR D OUBLER, FABRICATED AND INSTALLED REPLACEMENT DOUBLER PER SRM 51-40-20. 2 L 7 2 4F RT A16WE 2002102300124 20021023 00124 WP 2002 10 23 ZW0A0210601 1 20021021 A 3350 7732 BULB DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9629H 53599 A CABIN EGRESS LIGHT WAS INOPERATIVE. REPLACED THE BULB. CHECK-C 1-5-02 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2002102300127 20021023 00127 NM 2002 10 23 F3LA200200337 1 20021008 A 5320 SUPPORT BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 786, RBL 21, WL 157. REPLACED SIDEWA LL SUPPORT PER SRM 51-30-02, FIG. 1, AND SRM 51-30-02, FIG. 9. 2 L 7 2 4F RT A16WE 2002102300128 20021023 00128 NM 2002 10 23 F3LA200200338 1 20021008 A 5320 SUPPORT BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TO SIDEWALL SUPPORT, BS 500A - BS 520, RBL 25, WL 156. FABRICA TED AND INSTALLED REPLACEMENT SIDEWALL SUPPORT PER SRM 53-10-1, 53-10-2. 51-21-21 AND 51-30-2. 2 L 7 2 4F RT A16WE 2002102300130 20021023 00130 WP 2002 10 23 IXXA0200069S 1 20020521 A 5210 DOOR DOUG DC8 DC862 3021970 WP AFT PASSENGER CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AT FUSELAGE STATION 15OO, AFT PASSENGER DOOR FRAME AT THE LOWE R AFT CORNER. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGE AREA, FABRICATION AND INSTALLATION OF A NEW INTERNAL REPAIR ANG LE AND FRAME IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002102300131 20021023 00131 WP 2002 10 23 IXXA0200071S 1 20020531 A 5711 WING DOUG DC8 DC862 3021970 WP LEADING EDGE CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING UPPER LEADING EDGE OUTBOARD OF NUMBER FOUR PYL ON. REPAIR ACCOMPLISHED REOMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERMAL DOUB LER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002102300132 20021023 00132 WP 2002 10 23 IXXA0200067S 1 20020517 A 5200 DOOR DOUG DC8 DC862 3021970 WP FWD ENTRANCE CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED UNDER A TEMPORARY REPAIR OF THE FORWARD ENTRANCE DOOR CUT OUT FO RWARD UPPER CORNER. REPAIR ACCOMPLISHED, REMOVAL OF THE TEMPORARY REPAIR AND DAMAGED AREA, FABRICATION AND INSTALLATIN OF A REPAIR FILLER, EXTERNAL DOUBLER AND TRIPLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REAPIR MANUAL. 2 L 7 4 4F 4A25 2002102300137 20021023 00137 NM 2002 10 23 F3LA200200350 1 20021004 A 5347 CARGO TRACK BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 DURING C 4 CHECK, CORROSION WAS FOUND ON CARGO TRACK AT BS 947, RBL 14 AT THE TIE DOWN SOCKET. CARGO TRACK SECTION WAS REPLACED IN ACCORDANCE WITH SRM 53-00-53, FROM BS 867 TO BS 947. 2 L 7 2 4F RT A16WE 2002102300138 20021023 00138 NM 2002 10 23 UPS02239530 1 20020920 A 3350 CONTACTOR BOEING 727 72730C 1384009 NM CABIN DIRTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 919UP 19012 EMERGENCY EXIT LIGHTS INOP. REMOVED LIGHT ASSY OVER CREW CABIN DOOR, CLEANED CONTACTS, OPS CK OK IAW MM 33-50-01. 2 L 7 3 4F A3WE 2002102300139 20021023 00139 NM 2002 10 23 UPS02239549 1 20020930 A 3350 S106 BATTERY BOEING 727 72730C 1384009 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 919UP 19012 COCKPIT EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACED BATTERIES, OPS CHECKS GOOD, BATTERIES IAW MM 33-50-01. 2 L 7 3 4F A3WE 2002102300140 20021023 00140 NM 2002 10 23 UPS02239553 1 20020917 A 5753 CARRIAGE BOEING 727 72722C 138400F NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 NR 1 FLAP CARRIAGE HAS EVIDENCE OF CORROSION IN SPINDLE BORE HOLE. NR 1 FLAP CARRIAGE REPLACED IAW MM 27-51-13. 2 L 7 3 4F A3WE 2002102300141 20021023 00141 NM 2002 10 23 UPS02239554 1 20020917 A 5753 CARRIAGE BOEING 727 72722C 138400F NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 NR 3 FLAP CARRIAGE HAS EXCESSIVE CORROSION ON SPINDLE SHAFT SURFACE. NR 3 FLAP CARRIAGE REPLACED IAW MM 27-51-03. 2 L 7 3 4F A3WE 2002102300142 20021023 00142 NM 2002 10 23 UPS02239555 1 20020915 A 5320 FITTING BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 TAILSKID COMPT LEFT UPPER TENSION TIE AFT FITTING CRACKED. REPLACED TENSION TIE FITTING IAW DRAWING 65-25992 AND SRM 51 -30-02. 2 L 7 3 4F A3WE 2002102300143 20021023 00143 NM 2002 10 23 UPS02239560 1 20020916 A 5753 BALLSCREW BOEING 727 72722C 138400F NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 NR 4 BALLSCREW AND NUT ASSY ARE BADLY CORRODED AT YOKE ATTACH POINT. NR 4 BALLSCREW AND NUT ASSY REPLACED AS REQ`D IAW MM 27-51-36 AND OHM 57- 54-04. 2 L 7 3 4F A3WE 2002102300144 20021023 00144 NM 2002 10 23 UPS02239603 1 20020918 A 5260 RISER BOEING 727 72722C 138400F NM AFT AIRSTAIRS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 VENTRAL STAIRWAY NR 1 TREAD RIZER LOWER CHORD EVIDENCE OF CORROSION. CORROSION REMOVED IAW SRM 51-10-06 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-06. REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2002102300145 20021023 00145 NM 2002 10 23 UPS02239604 1 20020916 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 CRACK ON NLG WHEEL WELL CEILING AT BS 284 BBL 6L. CRACKED AREA TRIMMED OUT IAW SRM 51-40-2 FIG 1. HFEC AROUND THE EDGE OF CUTOUT CARRIED OUT IAW SRM 51-40-2 PT 6 51-00-00 FIG 4, RESULTS NDF. 2 L 7 3 4F A3WE 2002102300146 20021023 00146 NM 2002 10 23 UPS02239606 1 20020916 A 5310 SHEAR TIE BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 STRINGER SHEAR TIE CRACKED AT STR 5 RT BS 1010. SHEAR TIE REPLACED IAW SRM 51-20-1, 51-40-3. 2 L 7 3 4F A3WE 2002102300147 20021023 00147 NM 2002 10 23 UPS02239612 1 20020918 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 AREA OF LIGHT SURFACE CORROSION ON UPPER CHORD OF FLOORBEAM BS 312 AT LBL 4. CORROSION REMOVED IAW SRM 51-10-06 AND FOU ND TO BE OUSIDE LIMITS. REPAIR THEN CARRIED OUT IAW SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 2002102300148 20021023 00148 NM 2002 10 23 UPS02239616 1 20020916 A 5310 SHEAR TIE BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 STRINGER SHEAR TIE CRACKED AT STRINGER 6 RT BS 1050. SHEAR TIE REMOVED IAW SRM 51-30-2. SHEAR TIE REPLACED IAW SRM 51- 20-1 AND 51-40-3. 2 L 7 3 4F A3WE 2002102300149 20021023 00149 NM 2002 10 23 UPS02239628 1 20021006 A 3350 LIGHT BOEING 727 727172C 1384058 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 916UP 19808 COCKPIT EMERGENCY LIGHT 1 BULB INOP. RELAMPED COCKPIT EMERGENCY LIGHT BULB. 2 L 7 3 4F A3WE 2002102300150 20021023 00150 NM 2002 10 23 UPS02239645 1 20021010 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN NOT SEATED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 937UP 19302 EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR INOPERATIVE. RESEATED FWD ENTRY DOOR EMERGENCY EXIT LIGHT OPERATIONAL CKS GOO D. 2 L 7 3 4F A3WE 2002102300151 20021023 00151 NM 2002 10 23 UPS02239708 1 20020918 A 5260 RIB BOEING 727 72722C 138400F NM VENTRAL STAIRS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 EXFOLIATION CORROSION AND CRACK ON NR 10 VENTRAL STAIRWAY RISER LWR RIB CRACKED. LOWER RIB WEB REMOVED IAW SRM 51-30-2. CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 52-00-02. RIB WEB FABRICATED AS PER DRG NR 65-19809. RIB WEB INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2002102300152 20021023 00152 NM 2002 10 23 UPS02239709 1 20020919 A 5320 STRUCTURE BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 ON INVESTIGATION OF BS 360 BOLTS AND BOLT HOLES, BOLT HOLE IMMEDIATELY BELOW STR 24L HAS EXCESSIVE CORROSION INSIDE HOLE BORE. REPAIR CARRIED OUT IAW SRM 51-10-06, SRM 51-30-02 AND SMRO EO 2002-052-004 UPS ENGINEERING FILE NR 727-53-20077. 2 L 7 3 4F A3WE 2002102300153 20021023 00153 NM 2002 10 23 UPS02239710 1 20020916 A 5310 SHEAR TIE BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 STRINGER SHEAR TIE CRACKED AT S3L BS 990. CRACKED STRINGER SHEAR TIE REPLACED IAW SRM 51-20-1 AND 51-30-2. 2 L 7 3 4F A3WE 2002102300154 20021023 00154 NM 2002 10 23 UPS02239711 1 20020917 A 5753 CARRIAGE BOEING 727 72722C 138400F NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 NR 6 FLAP CARRIAGE SPINDLE BOLT HOLE AND UPPER AIR LOAD ROLLER BOLT HOLES ARE CORRODED. INSTALLED FABRICATED BUSHINGS I N CARRIAGE IAW SPOM 20-50-03. CORROSION REMOVED FROM HOLES IAW OHM 57-58-02. BUSHINGS FOR HOLES FABRICATED IAW OHM 57- 58-02. NR 6 FLAP CARRIAGE REPAIRED IAW OHM 57-58-02. 2 L 7 3 4F A3WE 2002102300155 20021023 00155 NM 2002 10 23 UPS02239712 1 20020917 A 5753 CARRIAGE BOEING 727 72722C 138400F NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 NR 7 FLAP CARRIAGE AFT DEAD WEIGHT ROLLER BRACKET BOLT HOLE AND CARRIAGE SPINDLE BOLTS HOLE IS CORRODED. CORROSION REMO VED FOR BOLT HOLES IAW OHM 57-58-01. BUSHINGS FOR HOLES IN CARRIAGES FABRICATED IAW OHM 57-58-01. INSTALLED BUSHINGS I AW OHM 57-58-01. NR 7 FLAP CARRIAGE REPAIRED IAW OHM 57-58-01. 2 L 7 3 4F A3WE 2002102300156 20021023 00156 NM 2002 10 23 UPS02239713 1 20020917 A 5753 CARRIAGE BOEING 727 72722C 138400F NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 NR 8 FLAP CARRIAGE LEFT AFT DEAD WEIGHT ROLLER BRACKET BOLT HOLE IS CORRODED. CORROSION REMOVED IAW OHM 57-58-01. BUSH INGS FABRICATED AND INSTALLED IAW OHM 57-58-01. NR 8 FLAP CARRIAGE REPAIRED IAW OHM 57-58-01. 2 L 7 3 4F A3WE 2002102300157 20021023 00157 NM 2002 10 23 UPS02239714 1 20020920 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 CORROSION AROUND NUT BS 380 LBL 45.5 ON SEAT TRACK. REMOVED DAMAGED SECTION IAW SRM 51-30-2, REPAIRED IAW SRM 53-10-5. 2 L 7 3 4F A3WE 2002102300158 20021023 00158 NM 2002 10 23 UPS02239717 1 20020923 A 5311 FRAME BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 BS 740 BULKHEAD LWR CHORD FOUND CORRODED DURING REMOVAL TO FACILITATE FITTING REPLACEMENT. SECTION OF CHORD REPLACED IA W DRAWING 65C13724. 2 L 7 3 4F A3WE 2002102300159 20021023 00159 NM 2002 10 23 UPS02239720 1 20020919 A 5320 SUPPORT BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 LWR AFT CARGO BAY, FRAME SUPPORT IS CRACKED AT STR 25 ATTACH POINT FRAME IS LOCATED AT BS 1093 LEFT. FRAME SUPPORT ANGL E REPAIRED IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2002102300160 20021023 00160 NM 2002 10 23 UPS02239723 1 20020917 A 5751 HINGE FITTING BOEING 727 72722C 138400F NM AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 SUSPECT CRACK ON LEFT O/B AILERON NR 3 HINGE FITTING ON WING. LEFT O/B AILERON REMOVED IAW MM 27-10-10. HINGE FITTING NR 3 REMOVED IAW SRM 51-30-02. NEW HINGE FITTING INSTALLED IAW DRAWING 65-19275. 2 L 7 3 4F A3WE 2002102300161 20021023 00161 NM 2002 10 23 UPS02239740 1 20020930 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 PRESS WEB AT BS 740 BULKHEAD DAMAGED AT LWR END WHERE IT ATTACHS TO 740 RT FITTING. DAMAGE BLENDED OUT AND REPAIRED PER SRM 53-10-9 FIG 4. 2 L 7 3 4F A3WE 2002102300162 20021023 00162 NM 2002 10 23 UPS02239746 1 20020918 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 AREAS OF LIGHT SURFACE CORROSION ON UPPER CHORD OF FLOORBEAM BS 344 BETWEEN LBL 15 TO RBL 35. FLOORBEAM SECTION REPLAC ED IAW SRM 53-10-8 FIG 7 WITH REF TO BOEING DRG 65-16316. 2 L 7 3 4F A3WE 2002102300163 20021023 00163 NM 2002 10 23 UPS02239750 1 20021015 A 3350 LIGHT BOEING 727 727180C 138406G NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 921UP 19874 EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED CREW ENTRY DOOR EMERGENCY EXIT LIGHT ASSY. OPS CHECK GOOD MM 33-50-01. 2 L 7 3 4F A3WE 2002102300164 20021023 00164 NM 2002 10 23 UPS02239751 1 20020912 A 5311 65159682 FRAME BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 CORROSION ON RT BS 740 FRAME O/B WEB FLANGE. CORROSION REMOVED WAS OUTSIDE OF LIMITS OF EO B727-5310-7477. FITTING REP LACED IAW EO B727-5310-7477-E. 2 L 7 3 4F A3WE 2002102300165 20021023 00165 NM 2002 10 23 UPS02239756 1 20020919 A 5714 651620253 STIFFENER BOEING 727 72722C 138400F NM WING CENTER BOX CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 BULGING EVIDENT ON WING CENTER SECTION REAR SPAR WEB AT BS 870, 3RD VERTICAL STIFFENER FROM LEFT SIDE. CORROSION FOUND ON VERTICAL STIFFENER AT LBL 24.70. STIFFENER REPLACED IAW SRM 51-30-2 AND DRAWING 65-16202. 2 L 7 3 4F A3WE 2002102300166 20021023 00166 NM 2002 10 23 UPS02239758 1 20021010 A 5210 65257294 HINGE BOEING 727 72722C 138400F NM AFT ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 UPPER HINGE ARM OF AFT ENTRY DOOR CRACKED. HINGE REPLACED. FUNCTION AND OPERATION CHECK CARRIED OUT IAW MM 52-13-02 AN D 52-13-00. 2 L 7 3 4F A3WE 2002102300167 20021023 00167 NM 2002 10 23 UPS02239761 1 20020917 A 5330 65423709 SKIN BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 CORROSION ON INNER SURFACE OF INTERNAL DOUBLER (SUSPECT CORROSION BETWEEN SKIN AND DOUBLER) BETWEEN BS 481 AND 475 BETWE EN STINGERS 7L AND 6L. REPAIR CARRIED OUT IAW UPS AUTHORIZATION 727-53-20082. 2 L 7 3 4F A3WE 2002102300168 20021023 00168 NM 2002 10 23 UPS02439539 1 20020925 A 3350 LIGHT BOEING 747 747200 1384847 NM CREW STAIRS INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:AS EMERGENCY ENTRY LIGHT IN CEILING AT BOTTOM OF CREW STAIRS INOP. INSTALLED LIGHT BULBS OPS CHECK NORM AL. 2 L 7 4 4F RT A20WE 2002102300169 20021023 00169 NM 2002 10 23 QXEA0201503 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND INBOARD SEAT TRACK NR 7 BOTTOM CHAFED APPROXIMATELY 12 INCHES BY TRACK COVER AT APPROXIMATELY X291.00. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102300170 20021023 00170 NM 2002 10 23 QXEA0201504 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND INBOARD SEAT TRACK NR 7 BOTTOM CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X280.00. REPLACED SEAT TR ACK. 2 H 7 2 4T RT A13NM 2002102300171 20021023 00171 NM 2002 10 23 QXEA0201505 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND INBOARD SEAT TRACK NR 7 BOTTOM CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X270.00. REPLACED SEAT T RACK. 2 H 7 2 4T RT A13NM 2002102300172 20021023 00172 NM 2002 10 23 QXEA0201506 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 AFT OUTBOARD END CORRODED AROUND 7 RIVETS AND RECEPTACLE AT APPROXIMATELY X418.0 0. DAMAGE FOUND TO BE OUT OF LIMITS IAW RD 8-53-1339. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102300173 20021023 00173 NM 2002 10 23 QXEA0201507 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 BOTTOM CHAFED APPROXIMATELY 12 INCHES AT TRACK COVER, APPROXIMATELY X418.00. RE PLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102300174 20021023 00174 NM 2002 10 23 QXEA0201508 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 BOTTOM CHAFED APPROXIMATELY 12 INCHES AT TRACK COVER, APPROXIMATELY X387.00. RE PLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102300175 20021023 00175 NM 2002 10 23 QXEA0201509 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 BOTTOM CHAFED APPROXIMATELY 12 INCHES BY TRACK COVER AT APPROXIMATELY X354.00. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102800138 20021028 00138 2002 10 28 MWEA020628 4 20021020 A 2350 6027664 MICROPHONE DOUG DC9 DC981 3022081 WP COCKPIT MALFUNCTIONED A MWEA O OTHER O OTHER DE DESCENT 1 GL 31 803ME 48029 CREW TEMPORARILY LOST COMMUNICATION. REMOVED AND REPLACED HAND MICROPHONE. 2 L 7 2 4F A6WE 2002102300176 20021023 00176 NM 2002 10 23 AWXA200201042 1 20021003 A 5320 654656841 BULKHEAD BOEING 737 737301 1384611 NM CANNING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 0 0 23261 MCN - MAJOR REPAIR - DURING C-17 CHECK OIL CANNING WAS DISCOVERED ON THE AFT PRESSURE BULKHEAD BS 1016, RBL 54, BETWEEN STR 11 R/H AND STR 13 R/H, CANNING CONCAVED FORWARD. MAINTENANCE REMOVED BOLTS FROM STR 11 R/H TO STR 14 R/H, FABRICATED AND INSTALLED SHIMS AT STR 11 - 13 R/H. REINSTALLED AND TORQUED BOLTS, CANING NO LONGER EXISTS. REPAIR ACCOMPLISHED IAW AWA E.R. 03-5383-02291-ES1. 2 L 7 2 4F RT A16WE 2002102300177 20021023 00177 NM 2002 10 23 AWXA200201043 1 20021022 A 5320 65535954 REVEAL BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 0 0 23261 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND ON THE R-1 DOOR UPPER FORWARD INTERIOR REVEAL AT BS 309, RBL 47. MAINTENANCE REMOVED DAMAGED REVEAL AT BS 309, RBL 47; FABRICATED A NEW REPLACEMENT REVEAL AND -9 STRAP; INSTALLED R EPAIR PARTS IAW B737-300 SRM 51-40-02, PG. 3-4, 26, 29, 32, & 35, FIG. 3, 4, 6, & 7. 2 L 7 2 4F RT A16WE 2002102300178 20021023 00178 NM 2002 10 23 AWXA200201044 1 20021022 A 5320 65535954 REVEAL BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 0 0 23261 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND ON THE R-1 DOOR UPPER AFT INTERIOR REVEAL AT BS 320, RBL 47. MAINTENANCE REMOVED DAMAGED REVEAL AT BS 320, RBL 47; FABRICATED A NEW REPLACEMENT REVEAL AND -9 STRAP; INSTALLED REPAI R PARTS IAW B737-300 SRM 51-40-02, PG. 3-4, 26, 29, 32, & 35, FIG. 3, 4, 6, & 7. 2 L 7 2 4F RT A16WE 2002102300179 20021023 00179 WP 2002 10 23 NACA20020049 1 20021003 A 3200 5333660500 DOWNLOCK SWITCH DOUG DC6 C118A 3021710 WP INTERMITTENT A NACA L ABORTED APPROACH O OTHER LD LANDING 1 AL 03 1377K 44596 DISCREPANCY: LEFT MAIN LANDING GEAR INDICATED AN UNSAFE CONDITION FOR 5 GEAR CYCLES. LAST CYCLE DOWN INDICATED NORMAL. C ORRECTIVE ACTION: REPLACED LMG DOWN LOCK SWITCH. 2 L 7 4 4R 6A3 2002102300180 20021023 00180 NM 2002 10 23 F3LA200200362 1 20021023 A 5310 6546921528 DOOR FRAME BOEING 737 7372L9 1384497 NM CARGO BAY CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 52094 22733 DURING C 2 CHECK, A CRACK WAS FOUND IN THE LOWER, FORWARD AND AFT CORNERS OF THE DOOR FRAME ON THE FORWARD BAGGAGE COMPA RTMENT DOOR. THE LOWER, FORWARD AND AFT FRAMES OF THE FORWARD BAGGAGE COMPARTMENT DOOR WERE REPLACED IAW SB 737-52A1100 , FIGURE 2, AND COMPLIANCE WITH AD 2000-07-06 WAS ACCOMPLISHED IAW SB 737-52A1100 THROUGH ER 02-1527. 2 L 7 2 4F RT A16WE 2002102300181 20021023 00181 SO 2002 10 23 C2XA02SH115 1 20021023 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14933 145018 SHV DURING C CHECK THE CENTER OMEGA BEAM STRAP BETWEEN FRAMES 18 AND 23 WAS FOUND HAVE CORROSION. MAINTENANCE REMOVED DA MAGE AND REPLACED THE AFFECTED OMEGA BEAM STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002102400001 20021024 00001 CE 2002 10 24 2002F00959 1 20021023 A 8120 4709089013 WASTEGATE VALVE CESSNA 414 414A 2075907 CE CONT O520 TSIO520N 17040 SO RT ENGINE STUCK E C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 13 4837A 414A0101 R519028 UNABLE TO OBTAIN TAKEOFF POWER ON RIGHT ENGINE. 1 L 7 2 3O 3 O A7CE E8CE 2002102400003 20021024 00003 SW 2002 10 24 ERAA081149 1 20020925 A 6210 412015300109 BLADE BELL 412 412 1182202 SW MAIN ROTOR CRACKED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 412EH 9573 33001 CRACK TOP SIDE ABRASION STRIP INBOARD OF MIDSCRAP JOINT. INSPECTED, PERFORMED 2500 HOUR INSPECTIONS; TRIMMED REFLEX DOU BLER, REPLACED INBOARD AND CENTER TRIM TABS WITH FIBERGLASS REPAIR AND REPLACED OUTBOARD ABRASION STRIP. 1 G 7 2 4U H4SW 2002102400004 20021024 00004 SW 2002 10 24 ERAA081150 1 20020925 A 6210 412015300104 BLADE BELL 412 412 1182202 SW MAIN ROTOR CRACKED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 422EH 9549 33068 NUMEROUS SMALL CRACKS IN SKIN AROUND MID SECTION. INSPECTED, PERFORMED 2500 HOUR INSPECTIONS REPAIRED SKIN ON BOTH SUR FACES AT STA 98 TO STA 151. REPLACED ROOT TAPE. REPLACED OUTBOARD TRIM TAB AND, REFINISHED APPLIED HIGH VIS PER CUSTO MER REQUIREMENT; STATIC BALANCED 1 G 7 2 4U H4SW 2002102400005 20021024 00005 SW 2002 10 24 ERAA081151 1 20020925 A 6210 412015300104 BLADE BELL 412 412 1182202 SW MAIN ROTOR CRACKED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 9428 SUSPECT ONE SKIN CRACK. INSPECTED, PERFORMED 2500 HOUR INSPECTION; REPLACED CENTER AND INBOARD TRIM TAB AND REPAIRED SK IN ON UPPER SURFACE AT STA 135 AND STA 104 TO STA 111. REPLACED ROOT TAPE. REFINISHED. APPLIED HIGH VIS PER CUSTOM ER REQUIREMENT; STATIC BALANCED 1 G 7 2 4U H4SW 2002102400006 20021024 00006 SW 2002 10 24 ERAA081152 1 20020925 A 6210 412015300104 BLADE BELL 412 412 1182202 SW MAIN ROTOR CRACKED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 164EH 8480 33004 BLADE HAS CRACKED LEADING EDGE. INSPECTED, PERFORMED 2500 HR INSPECTIONS ; REPLACED OUTBOARD ABRASION STRIP. REPLACE D INBOARD AND OUTBOARD SPLICE COVERS AND REBOND TRIM TAB TANGS. TRIM REFLEX DOUBLER. REPLACED ROOT TAPE; REPLACED TI P CAP, AND REFINISHED. STATIC BALANCED. 1 G 7 2 4U H4SW 2002102400007 20021024 00007 SW 2002 10 24 ERAA081153 1 20020925 A 5310 205030280139 STRUCTURE BELL 205 205A 1181413 SW SERVICE DECK DAMAGED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 LT SERVICE DECK HAS 5 X 8 INCH VOID FORWARD INBOARD SIDE OF DECK. REPAIRED DECK. 1 G 7 1 4U H1SW 2002102400008 20021024 00008 NM 2002 10 24 VNAA0210021 1 20021019 A 2600 SD947022 FIRE DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CARGO FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 457PS 3336 422 3048 DURING CLIMB, THE CARGO FIRE LIGHT ILLUMINATED ON THE RED WARNING PANEL INTERMITTENTLY. THE CREW FOLLOWED THE QUICK REF ERENCE HANDBOOK AND RELEASED THE CARGO COMPARTMENT EXTINGUISHING AGENTS. FLIGHT 4102 THEN RETURNED TO PIT AND LANDED WI TH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF A FIRE. MAINTENANCE THEN REPLACED THE CARGO CO MPARMENT FIRE BOTTLES AND THE CARGO FIRE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL C HECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. AS A PRECAUTION, MAINTENANCE WILL ALSO BE REPLACING THE CARGO FIRE PANEL. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002102400009 20021024 00009 NM 2002 10 24 SWAA022462 1 20021018 A 5330 6545776 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED 4 AFT OF BS 927, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102400010 20021024 00010 2002 10 24 SWAA022464 4 20021020 A 2565 65C16820 BRACKET BOEING 737 7373H4 1384600 NM FWD SVC DOOR SHEARED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK BRACKET HAS 1 ATTACH RIVET SHEARED. RE MOVED AND REPLACED RIVET PER SRM. 2 L 7 2 4F RT A16WE 2002102400011 20021024 00011 NM 2002 10 24 SWAA022465 1 20021019 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 4L, BS 807, BS 797 AND BS 908. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102400012 20021024 00012 NM 2002 10 24 SWAA022469 1 20021020 A 5330 6545769 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 448, FWD OF THE NR 2 RADIO ALT ANTENNA. REPAIRED SKIN PER SRM AND SWA EA. 2 L 7 2 4F A16WE 2002102400013 20021024 00013 NM 2002 10 24 SWAA022470 1 20021018 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 632SW 27707 DURING SCHEDULED C1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002102400014 20021024 00014 2002 10 24 SWAA022476 4 20021017 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD CABIN DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED C4 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PE R MM. 2 L 7 2 4F RT A16WE 2002102400015 20021024 00015 2002 10 24 SWAA022477 4 20021017 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002102400016 20021024 00016 NM 2002 10 24 SWAA022461 1 20021019 A 3320 059341 BALLAST BOEING 737 7373L9 1384470 NM CABIN SHORTED A SWAA O OTHER M OVER TEMP CR CRUISE 1 SW 29 658SW 23332 BEFORE DESCENT INTO LAX, ELECTRICAL SMELL DETECTED BETWEEN ROWS 17 AND 22. FOUND SIDEWALL LIGHT BALLAST SHORTED AT ROWS 20 AND 21 RT. REMOVED AND REPLACED BALLAST PER MM. 2 L 7 2 4F RT A16WE 2002102400017 20021024 00017 NM 2002 10 24 SWAA022386 1 20021010 A 5311 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIES CRACKED (3 EA) BETWEEN STR 13L AND STR 14L, BS 460, BS 727E AND BS 727B . REPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2002102400018 20021024 00018 NM 2002 10 24 SWAA022389 1 20021010 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS COVER PER MM 2 L 7 2 4F RT A16WE 2002102400019 20021024 00019 2002 10 24 SWAA022390 4 20021010 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2002102400020 20021024 00020 2002 10 24 SWAA022391 4 20021010 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM CABLE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002102400021 20021024 00021 2002 10 24 SWAA022392 4 20021010 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW AND CABLE MISROUTED. REPOSITIO NED SLIDE AND REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002102400022 20021024 00022 NM 2002 10 24 SWAA022394 1 20021013 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 EEPLS COVER LOOSE BETWEEN ROW NR 7 AND ROW NR 9. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2002102400023 20021024 00023 NM 2002 10 24 SWAA022396 1 20021012 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CRACKED AT BS 500C, STR 10L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2002102400024 20021024 00024 NM 2002 10 24 SWAA022398 1 20021012 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4L, BS 510C AND BS 510D. MX FERRY TO CYXX, C/ W SKIN LAP JOINT MOD PER SWA ACO. 2 L 7 2 4F RT A16WE 2002102400025 20021024 00025 NM 2002 10 24 SWAA022399 1 20021012 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) AT STR 4R, BS 639, BS 688, BS 700 AND BS 712. MX FER RY TO CYXX, C/W SKIN LAP JOINT MOD PER SWA ACO. 2 L 7 2 4F RT A16WE 2002102400026 20021024 00026 NM 2002 10 24 SWAA022400 1 20021012 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) AT STR 14L, BS 476, BS 510, BS 510B AND BS 518B. MX FERRY TO CYXX, C/W SKIN LAP JOINT MOD PER SWA ACO. 2 L 7 2 4F RT A16WE 2002102400027 20021024 00027 NM 2002 10 24 SWAA022401 1 20021012 A 5311 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002102400028 20021024 00028 NM 2002 10 24 SWAA022402 1 20021012 A 5330 65C20843 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED SPECIAL VISIT FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF AIRSTAIR CUTOUT, BS 348 AND STR 20L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F A16WE 2002102400029 20021024 00029 NM 2002 10 24 SWAA022403 1 20021010 A 5610 5893543130 WINDOW BOEING 737 7375H4 138449D NM COCKPIT CRACKED A SWAA K NONE O OTHER CL CLIMB 1 SW 29 508SW 24185 DURING CLIMB R-1 COCKPIT WINDOW CRACKED. REMOVED AND REPLACED R-1 COCKPIT WINDOW AND WINDOW HEAT CONTROLLER (CONTROLLER P/N 231-2 ON, S/N OFF 4171) 2 L 7 2 4F RT A16WE 2002102400030 20021024 00030 NM 2002 10 24 SWAA022404 1 20021013 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 18L, BS 485 AND BS 492. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102400031 20021024 00031 2002 10 24 SWAA022441 4 20021016 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM FWD SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 081SW 22730 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002102400032 20021024 00032 NM 2002 10 24 SWAA022442 1 20021016 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 711HK 27845 DURING SCHEDULED RON, FOUND EEPLS COVER MISSING AT ROW NR 6. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002102400033 20021024 00033 NM 2002 10 24 SWAA022445 1 20021015 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 511 AT STR 4R AND BS 430 AT STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102400034 20021024 00034 NM 2002 10 24 SWAA022446 1 20021017 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 14R, BS 500A AND BETWEEN BS 373 AND BS 374. R EPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102400035 20021024 00035 NM 2002 10 24 SWAA022449 1 20021017 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED A1 CHECK, FOUND RT ELEVATOR TAB HINGE NR 2, NR 3 AND NR 4 BUSHINGS WORN. REMOVED AND REPLACED TAB HING E BUSHINGS AND HARDWARE PER MM. 2 L 7 2 4F RT A16WE 2002102400036 20021024 00036 NM 2002 10 24 SWAA022450 1 20021017 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM LEFT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED A1 CHECK, FOUND LT ELEVATOR TAB HINGE NR 2, NR 3 AND NR 4 BUSHINGS WORN. REMOVED AND REPLACED TAB HING E BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002102400037 20021024 00037 NM 2002 10 24 SWAA022451 1 20021017 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED (17 EA) AT STR 4R, BS 716, BS 685, BS 577, BS 694, BS 706, BS 700, BS 837, BS 818, BS 727A, BS 797, BS 777, BS 757, BS 440, BS 727E + 10, BS 727E AND BS 727B. MX FERRY TO CYXX, C/W SKIN LAP JOINT MOD PER SWA ACO. 2 L 7 2 4F RT A16WE 2002102400038 20021024 00038 NM 2002 10 24 SWAA022452 1 20021017 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED (19 EA) AT STR 4L, BS 563, BS 628, BS 578, BS 606, BS 570, BS 696, BS 685, BS 639, BS 609, BS 600, BS 588, BS 595, BS 787, BS 727E + 10, BS 727B, BS 500C + 10, BS 500, BS 450 AND BS 757. MX FERRY TO CYXX, C/W SKIN LAP JOINT MOD PER SWA ACO. 2 L 7 2 4F RT A16WE 2002102400039 20021024 00039 NM 2002 10 24 SWAA022453 1 20021017 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 14L, BS500 + 10, BS 500C + 10 AND BS 380. MX FERRY TO C YXX, C/W SKIN LAP JOINT MOD PER SWA ACO. 2 L 7 2 4F RT A16WE 2002102400040 20021024 00040 NM 2002 10 24 SWAA022454 1 20021017 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 14R, BS 380 AND BS 500D. MX FERRY TO CYXX, C/W SKIN LAP JOINT MOD PER SWA ACO. 2 L 7 2 4F RT A16WE 2002102400041 20021024 00041 2002 10 24 SWAA022351 4 20021007 A 2565 D31354 GIRT BAR BOEING 737 7373H4 1384600 NM ESCAPE SLIDE OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002102400042 20021024 00042 NM 2002 10 24 SWAA022354 1 20021006 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 789, ABOVE STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102400043 20021024 00043 NM 2002 10 24 SWAA022355 1 20021007 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, ABOVE STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102400044 20021024 00044 NM 2002 10 24 SWAA022356 1 20021007 A 2130 BACC10BN500LR DUCT CLAMP BOEING 737 7377H4 1384404 NM MLG W/W DISCONNECTED A SWAA A C UNSCHED LANDING ABORTED TAKEOFF J WARNING INDICATION CL CLIMB 1 SW 29 714CB 27848 AIR TURNBACK, DURING CLIMB AIRCRAFT FAILED TO PRESSURIZE, WARNING HORN SOUNDED. FOUND AFT KEEL BEAM AREA BOOT ON BLEED DUCT DISCONNECTED. RECONNECTED BOOT PER MM. 2 L 7 2 4F RT A16WE 2002102400045 20021024 00045 NM 2002 10 24 SWAA022359 1 20021008 A 5330 6545785 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUTS CRACKED AT RT WINDOWS NR 7, NR 13 AND NR 21. REPAIRED FRAMES P ER SWA EA AND SRM. 2 L 7 2 4F A16WE 2002102400046 20021024 00046 NM 2002 10 24 SWAA022360 1 20021008 A 5330 6545785 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUTS CRACKED AT LT WINDOW NR 23. REPAIRED FRAMES PER SWA EA AND SRM . 2 L 7 2 4F A16WE 2002102400047 20021024 00047 NM 2002 10 24 SWAA022362 1 20021006 A 5740 65C32918 FITTING BOEING 737 7373H4 1384600 NM BOTH MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG FWD STABILIZER BAR SUPPORT FITTINGS CORRODED. REPAIRED FITTING S PER SWA EA'S. 2 L 7 2 4F RT A16WE 2002102400048 20021024 00048 NM 2002 10 24 SWAA022363 1 20021006 A 3210 6582770 FITTING BOEING 737 7373H4 1384600 NM BOTH MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG WALKING BEAM FITTINGS CORRODED. REMOVED AND REPLACED BOTH LT A ND RT WALKING BEAMS PER MM. 2 L 7 2 4F RT A16WE 2002102400049 20021024 00049 NM 2002 10 24 SWAA022365 1 20021008 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002102400050 20021024 00050 NM 2002 10 24 SWAA022366 1 20021009 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW NR 7 ABC. INSTALLED LEN S PER MM. 2 L 7 2 4F RT A16WE 2002102400051 20021024 00051 NM 2002 10 24 SWAA022368 1 20021009 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 EEPLS COVER MISSING AT ROW NR 16. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002102400052 20021024 00052 NM 2002 10 24 SWAA022369 1 20021009 A 5330 6552873 SKIN BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT DOUBLER AND BEAR STRAP CRACKED. REPAIRED SKIN PER SW A EA AND SRM. 2 L 7 2 4F RT A16WE 2002102400053 20021024 00053 NM 2002 10 24 SWAA022370 1 20021008 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED C4 CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED INBD AFT T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002102400054 20021024 00054 NM 2002 10 24 SWAA022372 1 20021009 A 5330 65C20843 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF AIR STAIR CUTOUT, BS 344 AND STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F A16WE 2002102400055 20021024 00055 NM 2002 10 24 SWAA022377 1 20021009 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM MID CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002102400056 20021024 00056 NM 2002 10 24 SWAA022380 1 20021010 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM AFT CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 EEPLS COVER MISSING AT AFT CABIN. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002102400057 20021024 00057 NM 2002 10 24 SWAA022381 1 20021010 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 749SW 29801 EEPLS COVER MISSING AT ROW NR 20. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002102400058 20021024 00058 NM 2002 10 24 SWAA022382 1 20021010 A 3230 65446104 ACTUATOR BOEING 737 7373H4 1384600 NM NLG CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 632SW 27707 NOSE GEAR HYDRAULIC LEAK, DUE TO CRACKED NLG DOWN LOCK HYD ACTUATOR. REMOVED AND REPLACED NOSE GEAR DOWN LOCK ACTUATOR. 2 L 7 2 4F RT A16WE 2002102400059 20021024 00059 NM 2002 10 24 SWAA022384 1 20021010 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 748, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002102400095 20021024 00095 NM 2002 10 24 SWAA022385 1 20021010 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727A AND BS 727B, WL 188 AND RBL 66. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002102400060 20021024 00060 SW 2002 10 24 ERAA081154 1 20020925 A 5310 205030280139 STRUCTURE BELL 205 205A 1181413 SW DECK ASSY DAMAGED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 VOID FOUND NEAR EXCITER BOX BRACKET 1 X 3 INCH APPROX. VOIDED UNDER STIFFNESS ON LT FIREWALL 2 INCH IN DIAMETER. REMOV ED 2 1/2 X 4 INCH APPROXIMATELY FOR GOOD BONDING AND PANEL REPAIR. REMOVED BAD CORE & REPAIRED & INSPECTED. 1 G 7 1 4U H1SW 2002102400061 20021024 00061 EU 2002 10 24 ERAA081155 1 20020925 A 6520 4619003003 GEARBOX BOLKMS 105 BO105C 5626005 EU TAIL ROTOR MISREPAIRED H ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 FS 01 6440 HOUSING RECEIVED WITHOUT THREAD SEALANT. CHECKED GEARBOX OUT ON HOLD BOARD, C/W PRELIMINARY INSPECTION. NO DEFECTS NOTED , DRILLED OUT LOCKS ON 2 STUDS, APPLIED LOCKTITE AND REINSTALLED ORIGINAL STUDS WITH NEW LOCKS. ATTACHED ORIGINAL YELLO W TAG TO GEARBOX REPAIRED. 1 G 7 2 3U H3EU 2002102400062 20021024 00062 EU 2002 10 24 ERAA081156 1 20020925 A 6520 4619003003 GEARBOX BOLKMS 105 BO105C 5626005 EU TAIL ROTOR MISREPAIRED H ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 FS 01 13048 TAILROTOR GEARBOX HAS NO THREAD SEALANT ON STUDS. C/W PRELIMINARY INSPECTION AND FOUND NO OBVIOUS DEFECTS. SIGNED T/R G/B OUT ON HOLD BOARD. DRILLED OUT LOCKS ON 2 EA STUDS, APPLIED LOCTITE AND REINSTALLED BOTH STUDS WITH NEW LOCKS. ATT ACHED ORIGINALYELLOW TAG TO G/B. REPAIRED. 1 G 7 2 3U H3EU 2002102400063 20021024 00063 EU 2002 10 24 ERAA081157 1 20020926 A 2435 23032027 STARTER GEN BOLKMS 105 BO105S 5626006 EU ENGINE FAILED H ERAA O OTHER O OTHER NR NOT REPORTED 1 FS 01 128EH 7345 572 STARTER GENERATOR WOULD NOT ENGAGE ON START SIDE. BRUSHES DAMAGED BY ARCING. NR 1 & 3 BRUSH HOLDERS HAD MECHANICAL DAMA GE & ARC DAMAGE NOT ALLOWING FULL SEATING. COMMUTATOR HAS SEVERE PITTING & ARC DAMAGE. STATOR FAILED HY POT . TERMINA L BLOCK FAILED CAPACITANCE CHECK. DAMPNER BACK PLATE WAS WORN. DUE TO EXTENT OF DAMAGE TO NUMEROUS PARTS OF THE UNIT, O/H WAS REQUIRED (VER) DISASSEMBLED, CLEANED AND INSPECTED UNIT. CLEARED ALL DISCREPANCIES LISTED ABOVE. OVERHAULED & TESTED. INST'D NEW O RING AND HARDWARE. 1 G 7 2 3U H3EU 2002102400064 20021024 00064 EU 2002 10 24 ERAA081158 1 20020926 A 2435 23032027 STARTER GEN BOLKMS 105 BO105S 5626006 EU ENGINE FAILED H ERAA O OTHER L NO TEST NR NOT REPORTED 1 FS 01 134EH 3474 635 ARMATURE SENT OUT FOR REWORK. STATOR FAILED HY POT TEST. ARMATURE WAS RUBBING. STATOR BURNED DURING TEST. ARMATURE B URNED DURING TEST. 1 G 7 2 3U H3EU 2002102400065 20021024 00065 GL 2002 10 24 ERAA081159 2 20020926 A 7321 252464430N FUEL CONTROL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE MALFUNCTIONED H ERAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 FS 01 298EH 10681 S845 FUEL CONTROL CAUSES HOT STARTS AND SLOW ACCELERATION. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15 602E CEB 1382 EMBODI ED. 1 G 7 2 3U 3 U H3EU E4CE 2002102400066 20021024 00066 GL 2002 10 24 ERAA081160 2 20020926 A 7321 2524644 FUEL CONTROL BOLKMS 105 BO105A EU ALLSN 250C 250C20B 03013 GL ENGINE MALFUNCTIONED H ERAA K NONE L NO TEST IN INSP/MAINT 1 FS 01 135EH 13403 S675 FUEL CONTROL CAUSES ROTOR DROOP, UNIT OVERHAULED IAW HONEYWELL OHM FOR 15 602E. 1 G 7 2 3U 3 U H3EU E4CE 2002102400067 20021024 00067 GL 2002 10 24 ERAA081161 2 20020926 A 7321 252464429 FUEL CONTROL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 2 ENGINE MALFUNCTIONED H ERAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 FS 01 124EH 9622 S559 NR 2 ENGINE HANGS AT 50 PERCENT N1 FOR 3-5 SECONDS THEN RAPIDLY ACCELS TO 537 DEGREES N1. REPLACEMENT FIXED PROBLEM. F UEL CONTROL OVERHAULED, CLOSE TO TX REQUIRES MODS, CEB'S. OVERHAULED IAW HONEYWELL OHM FOR 15-602E. 1 G 7 2 3U 3 U H3EU E4CE 2002102400068 20021024 00068 WP 2002 10 24 UPS02839411 1 20020828 A 5720 FITTING DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 LT WING NR 2 MAIN XRS 74.000 STRINGER END FITTING CRACKED AFT FITTING. REMOVED AND REPLACED END FITT ING IAW DC8 SRM 51-1-20D AND 51-1-23 2 L 7 4 4F RT 4A25 2002102400069 20021024 00069 WP 2002 10 24 UPS02839413 1 20020826 A 5320 3758496U2 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1140 LONG 35R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758 496, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102400070 20021024 00070 WP 2002 10 24 UPS02839414 1 20020826 A 5320 4758514503 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 AFT SIDE STA 1240 FRAME INTERCOSTAL TO FRAME FITTING IS CRACKED AT LONG 33R. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102400071 20021024 00071 NE 2002 10 24 ERAA081162 1 20020926 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE MISSING H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 577EH 1685 760222 DOUBLER MISSING ON BOTTOM SIDE. INSPECTED & REPLACED BOTH FORWARD INTERNAL DOUBLERS AND REBONDED CHANNEL. MODIFIED EXTE RNAL DOUBLERS INSTALLED STAINLESS STEEL TIP COVER & REPLACED ABRAISION STRIP REPAIRED KEVLAR AT ZONE A,B & D & STATIC BA LANCED 1 G 7 2 3U H1NE 2002102400072 20021024 00072 NE 2002 10 24 ERAA081163 2 20020926 A 7310 4005T01P03 GASCOLATOR SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE ENGINE CORRODED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 561EH 13959 61471 INTERGRANULAR CORROSION WITHIN HOUSING. NDT AND VISUAL INSPECTION SHOWED NO INTERGRANULAR CORROSION. SHOWED ABNORMAL CA RBON SEAL WEAR. NORMAL OVERHAUL 2 G 7 2 4U 4 U 1H15 1E3 2002102400073 20021024 00073 WP 2002 10 24 UPS02839416 1 20020826 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C-1 C BAG BIN, BATH TUB FITTING CRACKED AT STA 1160 LONG 34R, INSIDE TORQUE BOX. REMOVED CRACKED BATH T UB FITTING IAW 53-2-0. FABRICATED REPAIR ANGLES AND FABRICATED REPAIR PARTS IAW SRM 53-2-0 FIG 2D, INSTALLED REPAIR ANG LES AND BATH TUB FITTING AT STA 1160 LONG 34R IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102400074 20021024 00074 EU 2002 10 24 UVVR200200002 1 20021022 A 5712 MY20142165 RIB AMD FALC20 FALCON20C5 2730107 EU WING CORRODED B K NONE O OTHER IN INSP/MAINT 1 CE 03 405JW 12744 54 RIB HAS CRACK RADIATING THROUGH FASTENERS ATTACHING RIB TO SPAR AND A PIECE IS MISSING APPROX 6 INCHES LONG AND 1/4 INCH WIDE. CORROSION EVIDENT, POSSIBLY DUE TO INSULATION BEING WET. THIS DEFECT CAN ONLY BE SEEN IF LEADING EDGE IS DISASSEM BLED. 2 L 7 2 4F RT A7EU 2002102400075 20021024 00075 WP 2002 10 24 GTIA020955 1 20020826 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE CARGO BAY CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 AFT CARGO DOOR FRAME CLOSE OUT PANEL FS 1212, CRACKED. REMOVED PANEL, FABRICATED REPAIR DOUBLER, INSTALLED REPAIR DOUBL ER. 2 L 7 2 4F 4 F A6WE E2EA 2002102400076 20021024 00076 WP 2002 10 24 GTIA021062 1 20020912 A 5330 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 DENT AT F.S.1332 BETWEEN LONGERONS 18R AND 19R REQUIRED TO BE INSPECTED FOR CRACKS. FABRICATED INTERNAL REPAIR DOUBLER AND REPAIR SKIN PLUG. INSTALLED REPAIR DOUBLER AND REPAIR SKIN PLUG. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102400077 20021024 00077 WP 2002 10 24 GTIA021063 1 20020912 A 5313 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 MID PIT STA 768 LONGERON 29 LT CORROSION ON LONGERON INBOARD FLANGE/LOWER SURFACE AT LONGERON TO FRAME FASTENER. REMOVE D DAMAGED SECTION, FABRICATED NEW LONGERON REPAIR SECTION/SPLICE INSTALLED LONGERON AND SPLICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102400078 20021024 00078 NM 2002 10 24 CALA0200504 1 20021023 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39343 23581 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 967, LBL 6 TO RBL 6. A STRAP DOUBLER WAS INSTALLED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2002102400079 20021024 00079 WP 2002 10 24 GTIA021064 1 20020913 A 5313 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 AFT PIT, STA 1174 TO STA 1155 HAVE CORROSION AT LONGERON 30. MATERIAL LOSS OUT OF LIMITS COMPLIED WITH E.A. 5310-0252. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102400080 20021024 00080 WP 2002 10 24 GTIA021066 1 20020917 A 5523 TAB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE RT ELEVATOR DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 RT ELEVATOR ANTI-FLOAT TAB IS DELAMINATED ON UPPER SURFACE (2 PLACES). REMOVED RIGHT ELEVATOR ANTI-FLOAT TAB, REPAIRED DELAMINATED AREAS, INSTALLED ELEVATOR TAB. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102400081 20021024 00081 WP 2002 10 24 GTIA021067 1 20020922 A 5313 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 STA 1194-1212 L30, LOWER SURFACE OF LONGERON FLANGE IS CORRODED AT FASTENER LOCATIONS IN SPLICE. REMOVED DAMAGED SECTIO N OF LONG 30. FABRICATED NEW LONGERON SECTION AND SPLICE, INSTALLED NEW SPLICE LONGERON 30. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102400082 20021024 00082 WP 2002 10 24 UPS02839417 1 20020821 A 5320 3779762US01 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C-1 LONG 10R END FITTING CRACKED AT STA 675. REMOVED CRACKED END FITTING AT LONG 10R, STA 675 IAW SRM 5 1-1-20 REPLACED IAW SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2002102400083 20021024 00083 WP 2002 10 24 UPS02839419 1 20020826 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C-1 LIGHT CORROSION BETWEEN LONG 35L AND 35R STA 260 EXTENDING UNDER SHEAR TIES. CORROSION OUT OF LIMIT S ON SHEAR TIE AT STA 260, LONG 35L. REMOVED SHEAR TIE IAW SRM 51-1-20. FABRICATED SHEAR TIE IAW SRM 53-4-1, INSTALLED SHEAR TIE IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102400084 20021024 00084 EU 2002 10 24 MALA020616 1 20021023 A 7600 CTOT PANEL SAAB SF340 SF340A 7850100 EU CT7TP CT75A1 30030 NE A MALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 15 89XJ 340A089 DURING CLIMBOUT OF MSP ON FLIGHT #3038, RH ENGINE SURGED TO 108% AND ITT AT 955 WHILE CLIMBING THROUGH 11,700 MDL. A/C YAWED SEVERELY. CREW WAS NOT IN ICING CONDITIONS. FOLLOWED QRH AND LOCKED OUT TO MGR. NO FURTHER FAULTS NOTED. TEMP AN D TORQUE FLUCTUATIONS WERE FOR LESS AND 5 SECONDS. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED CTOT PANEL ALL CHECKS GOOD. FDR DOWNLOAD INFO READ BY MIKE DONAHUE INDICATES NO FURTHER ACTION REQUIRED FOR ITT EXCEEDANCE OF 955.8 FO R 3 SECONDS. 2 L 7 2 4T 4 T RT A52EU E8NE 2002102400085 20021024 00085 WP 2002 10 24 UPS02839423 1 20020912 A 2612 CONTROL UNIT DOUG DC8 DC871F 302199D WP FIRE DETECTION MALFUNCTIONED A IPXA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 01 701UP 45938 INSPECTION TYPE:N/A DIV TO SBN. EN ROUTE TO ORD AFT CARGO COMPARTMENT FIRE WARNING LIGHT ON IN FLIGHT. CREW DECLARED EM ERGENCY. R&R CENTRAL CONTROL UNIT. OPS CHECK GOOD PER MM26-18-01. 2 L 7 4 4F RT 4A25 2002102400086 20021024 00086 NM 2002 10 24 DHL2002748003 1 20021022 A 2611 160117301 BATTERY BOEING 727 727225 1384077 NM SMOKE DETECTOR DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 748DH 22440 CARGO SMOKE DETECTOR FAULT F16421-8. BOTH BATTERIES REPLACED IAW M/M T/R 26-16-01. OPS TESTED IAW M/M T/R 26-16-00. S ERVICEABLE. 2 L 7 3 4F A3WE 2002102400087 20021024 00087 WP 2002 10 24 GTIA021068 1 20020927 A 5313 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 AFT CARGO COMPARTMENT, STA 1297, LONGERON 23R HAS CORROSION THROUGH THE METAL. REMOVED CORRODED LONGERON, CUT NEW LONGE RON. FABRICATED SPLICES, INSTALLED LONGERON SECTION AND SPLICES. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102400088 20021024 00088 NE 2002 10 24 GTIA021071 2 20021001 A 7240 COMBUST CHAMBER DOUG DC9 DC941 302207N WP PWA JT8 JT8D17 52049 NE ENGINE WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 BOROSCOPE RECORD, FOUND IGNITER GUIDE NR 4 COMBUSTION CHAMBER WORN AND OUT OF CHAMBER RESTING IN OUTER COMBUSTION CASE I GNITER PORT NR 4. BURNER CANS HAVE BEEN REPACED DURING SHOP VISIT. 2 L 7 2 4F 4 F A6WE E2EA 2002102400089 20021024 00089 WP 2002 10 24 UPS02839426 1 20020826 A 5320 3755842505 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C-1 C-BAG BIN, BATHTUB FITTING CRACKED AT STA 1200, LONG-28L. REMOVED BATH TUB FITTING, FABRICATED REPA IR DOUBLER IAW SRM 53-2-0 FIG 2D. INSTALLED REPAIR DOUBLER INSTALLED NEW FITTING IAW SRM 53-2-0 FIG2D, AND SRM 51-1-20D . 2 L 7 4 4F RT 4A25 2002102400090 20021024 00090 WP 2002 10 24 GTIA021072 1 20020913 A 5313 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 AFT PIT STA 1136, HAS CORROSION AT LONGERON 28R. FABRICATED LONGERON AND LONGERON SPLICE. REMOVED DAMAGED LONGERON SEC TION, INSTALLED NEW SPLICE AND NEW LONGERON SECTION. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102400091 20021024 00091 WP 2002 10 24 GTIA021073 1 20020917 A 5320 WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 PAX CABIN FS 200 UPPER CUSP CORRODED AT R1 DOOR SCUFF PLATE AREA. CUT OUT AND REMOVED R1 DOOR AFT LOWER CORNER PAN AND CUSP FABBED CUSP. SPLICE, DOUBLER AND FILLER INSTALLED SPLICES, FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102400092 20021024 00092 WP 2002 10 24 GTIA021074 1 20020917 A 5320 WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE PUNCTURED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FORWARD CABIN RBL 8, STA 148.8 HOLE ON THE WEB/PUNCTURE. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND FILLER. INSTALL ED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102400093 20021024 00093 WP 2002 10 24 GTIA021076 1 20020914 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 PAX CABIN STA 200 TO STA 256 LEFT OUTBOARD SEAT TRACK EXFOLIATION. REMOVED DAMAGED SEAT TRACK. LOCATED, DRILLED AND FA BBED SEAT TRACK, INSTALLED SEAT TRACK. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102400094 20021024 00094 2002 10 24 MEX2002322 4 20020710 A 3443 HG1103BA01 IRU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D NE RADAR SYS FAILED B ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 158PL 49761 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AN INDICATION OF NAV AND INERTIAL FAILURE. AFTER THREE ATTEMPTS THE I NERTIA SYSTEM WAS ALIGNED CONTINUING ITS FLIGHT, ENGINES WERE NOT SHUTDOWN DURING THIS ACTIONS. AT OVERNIGHT SERVICE, A S A PREVENTATIVE ACTION, THE IRU NR 1 WAS CHANGED IAW MM, TESTS OK. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102400096 20021024 00096 NM 2002 10 24 SWAA022352 1 20021008 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 360, STR 4R AND BS 908, STR 10R. REMOVED AND REPLACED TIE CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002102400097 20021024 00097 NM 2002 10 24 SWAA022353 1 20021006 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 4R, BS 616 AND BS 639. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002102400098 20021024 00098 NM 2002 10 24 SWAA022357 1 20021006 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 213 AND RBL 5.7 AND WL 200 AND LBL 5.7. REPAI RED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2002102400099 20021024 00099 NM 2002 10 24 SWAA022358 1 20021007 A 5314 6545866 KEELBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND KEEL BEAM CORRODED FROM BS 690 TO BS 722, RBL 8. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2002102400100 20021024 00100 NE 2002 10 24 SWAA022361 2 20021005 A 7200 1663M24P BLADE BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE SHINGLED A SWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 29 365SW 26576 AIR TURNBACK AFTER TAKEOFF, NR 2 ENGINE NOISE WAS NOTICED ALONG WITH ENGINE VIBRATION METER FLUCTUATIONS. FOUND (4 EA) BLADES SHINGLED NR 38, NR 1, NR 2 AND NR 3. UNSHINGLED BLADES PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102400101 20021024 00101 NM 2002 10 24 SWAA022364 1 20021009 A 3350 65C34691 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED BC3 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW NR 9 ABC. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002102400102 20021024 00102 NM 2002 10 24 SWAA022367 1 20021009 A 3350 BR2013 TRACK BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK LOOSE AT ROW NR 9. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002102400103 20021024 00103 NM 2002 10 24 SWAA022371 1 20021009 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND LBL 12.5. REPAIRED WEB PER SRM. 2 L 7 2 4F A16WE 2002102400104 20021024 00104 NE 2002 10 24 SWAA022373 2 20021008 A 7320 658385 VALVE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE MALFUNCTIONED A SWAA K NONE O OTHER CR CRUISE 1 SW 29 083SW 22732 ON LEVEL OFF TWO LOUD BANGS WERE AUDIBLE ON LT SIDE OF AIRCRAFT (SUSPECTED COMPRESSOR STALL). REMOVED AND REPLACED NR 1 ENGINE P AND D VALVE PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2002102400105 20021024 00105 NM 2002 10 24 DHL2002741016 1 20021023 A 2710 1225P61 SWITCH BOEING 727 7272Q9 138448M NM A DHLA C O ABORTED TAKEOFF OTHER J WARNING INDICATION TO TAKEOFF 1 SO 01 741DH 21931 1) AILERON "B" SYSTEM LOW PRESSURE LIGHT ILLUMINATED ON FORWARD PANEL. RTO AT 20 KTS, SL, 174.3 K LBS, 27 DEGREE C. BE C NORMAL SEE DISCREPANCY 1P FOR RTO REASON.2) ENTERED ON DMI #10731 AS PER MEL 27-16 CAT "C". PLACARD INSTALLED. FOR IN FORMATION ONLY.3) REF. DMI #10731 (AILERON "B" SYSTEM LOW PRESSURE LIGHT ILLUMINATED ON FORWARD PANEL. 4) REMOVED AND REPLACED AILERON "B" SYSTEM HYDRAULIC LOW PRESSURE WARNING SWITCH IAW B-727 M/M 27-10-144. OPS CHECKED SERVICEABLE. THIS CLEARS DMI #10731. 2 L 7 3 4F RT A3WE 2002102400106 20021024 00106 NM 2002 10 24 SWAA022374 1 20021010 A 3350 20121 BATTERY BOEING 737 737317 138447P NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED C3 CHECK, FOUND FWD RT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002102400107 20021024 00107 NM 2002 10 24 SWAA022375 1 20021009 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT ASSY BROKEN AT FWD WALL OUTBOARD OF F/A'S SEAT. REMOVED AND REPLA CED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002102400108 20021024 00108 NM 2002 10 24 SWAA022376 1 20021009 A 3350 BR2013 TRACK BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE AT MOST FWD CABIN. REMOVED AND REPLACED EEPLS TRACK SECTION PER MM. 2 L 7 2 4F RT A16WE 2002102400109 20021024 00109 NM 2002 10 24 SWAA022378 1 20021010 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 648SW 27718 FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2002102400110 20021024 00110 NM 2002 10 24 SWAA022379 1 20021010 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPECIAL VISIT, FOUND AFT UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2002102400111 20021024 00111 NM 2002 10 24 SWAA022383 1 20021009 A 5314 6545866 KEELBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED D CHECK, FOUND KEEL BEAM CORRODED AT BS 727, STR 27L. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2002102400112 20021024 00112 NM 2002 10 24 SWAA022387 1 20021007 A 5320 6935928 ANGLE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C1 CHECK, FOUND NLG UPPER SUPPORT ANGLE CRACKED JUST FWD OF A FRAME. REMOVED AND REPLACED SUPPORT ANGL E PER SRM. 2 L 7 2 4F RT A16WE 2002102400113 20021024 00113 NE 2002 10 24 SWAA022388 2 20021003 A 7200 CASE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 674247 DURING SCHEDULED C2 CHECK, FOUND HOLE IN OVER CASING AFT OF J FLANGE BEHIND IGNITION BOX AT NR 1 ENGINE. REMOVED AND RE PLACED ENGINE PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2002102400114 20021024 00114 NM 2002 10 24 SWAA022393 1 20021012 A 3350 6504789 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM . 2 L 7 2 4F A16WE 2002102400115 20021024 00115 NM 2002 10 24 SWAA022395 1 20021011 A 2781 65445519 ACTUATOR BOEING 737 7373H4 1384600 NM L/E FLAP FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 616SW 27699 AIR TURNBACK, DURING CLIMB NR 2 KRUEGER FLAP WOULD NOT RETRACT. REMOVED AND REPLACED NR 2 KRUEGER FLAP ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2002102400116 20021024 00116 NM 2002 10 24 SWAA022397 1 20021012 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 360, STR 14L AND STR 15L. REPAIRED STR SPLI CES PER SRM. 2 L 7 2 4F RT A16WE 2002102400117 20021024 00117 NM 2002 10 24 SWAA022440 1 20021017 A 3397 WIRE BOEING 737 7372T4 1384492 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AND DAMAGED AT OVERWING EXIT. REMOVED AND REPLACED BATTERY AND RESPLIC ED WIRES PER MM. 2 L 7 2 4F A16WE 2002102400118 20021024 00118 2002 10 24 SWAA022443 4 20021017 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHILE OPENING DOOR. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002102400119 20021024 00119 2002 10 24 SWAA022444 4 20021017 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 751SW 29803 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002102400120 20021024 00120 NM 2002 10 24 SWAA022447 1 20021017 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (4 EA) AT STR 4R, BS 727D, BS 727C, BS 847 AND BS 827. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002102400121 20021024 00121 NM 2002 10 24 SWAA022448 1 20021017 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (4 EA) AT STR 5R, BS 727E, BS 727E, BS 727B AND BS 667. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002102400122 20021024 00122 2002 10 24 SWAA022455 4 20021020 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002102400123 20021024 00123 2002 10 24 SWAA022456 4 20021020 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002102400124 20021024 00124 2002 10 24 SWAA022457 4 20021019 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 713SW 27847 AFT SVC DOOR EMERGENCY EVAC PRESS IND OUT OF VIEW AND VIEWING WINDOW LOOSE. REPOSITIONED SLIDE AND SECURED WINDOW PER M M. 2 L 7 2 4F RT A16WE 2002102400125 20021024 00125 NM 2002 10 24 SWAA022458 1 20021019 A 3350 65C27093 LIGHT BOEING 737 7373T5 1384608 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002102400126 20021024 00126 NM 2002 10 24 SWAA022459 1 20021019 A 2560 PH22300L TRACK BOEING 737 7373H4 1384600 NM CABIN DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 PHOTO LUMINESCENT STRIP DISLODGED IN CABIN. REATTACHED STRIP PER MM. 2 L 7 2 4F RT A16WE 2002102400127 20021024 00127 NM 2002 10 24 SWAA022460 1 20021019 A 2822 8311002 PUMP BOEING 737 7373H4 1384600 NM NR 1 FUEL TANK INTERMITTENT A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 656SW 28401 DIVERSION, DURING CLIMB NR 1 FUEL TANK FWD BOOST PUMP LOW PRESS LIGHT ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED NR 1 FUEL TANK FWD BOOST PUMP AND P-5 PANEL PER MM. 2 L 7 2 4F RT A16WE 2002102400128 20021024 00128 NM 2002 10 24 SWAA022463 1 20021019 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 360, STR 3L AND STR 6L. REMOVED AND REPLACE D STR SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2002102400129 20021024 00129 NM 2002 10 24 SWAA022466 1 20021019 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 908, STR 4R AND STR 5L. REMOVED AND REPLACE D STR SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2002102400130 20021024 00130 NM 2002 10 24 SWAA022467 1 20021019 A 5523 HINGE BOEING 737 7377H4 1384404 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB NR 4 HINGE WORN. REMOVED AND REPLACED HARDWARE O N NR 4 HINGE PER SRM. 2 L 7 2 4F RT A16WE 2002102400131 20021024 00131 NM 2002 10 24 SWAA022468 1 20021019 A 5523 183A300 HINGE BOEING 737 7377H4 1384404 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB NR 2, NR 3 AND NR 4 HINGES WORN. REMOVED AND REP LACED HARDWARE PER SRM. 2 L 7 2 4F RT A16WE 2002102400132 20021024 00132 2002 10 24 SWAA022471 4 20021016 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 FWD ENTRY DOOR EMERGENCY EXIT EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002102400133 20021024 00133 NM 2002 10 24 SWAA022472 1 20021019 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 EEPLS LOOSE AT OVERWING EXIT. SECURED EEPLS PER MM. 2 L 7 2 4F A16WE 2002102400134 20021024 00134 NM 2002 10 24 SWAA022473 1 20021017 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 071SW 22358 DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT ROW NR 9. RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2002102400135 20021024 00135 NM 2002 10 24 SWAA022474 1 20021017 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 071SW 22358 DURING SCHEDULED C2 CHECK, FOUND EEPLS END CAP MISSING IN FWD CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2002102400136 20021024 00136 2002 10 24 SWAA022475 4 20021018 A 2565 63562101 SLIDE BOEING 737 7377H4 1384404 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 774SW 27882 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002102400137 20021024 00137 NE 2002 10 24 VNAA0210022 2 20021020 A 7321 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAULTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 439JS 3057 DURING TAKEOFF, THE CREW RECEIVED CHIP DETECT LIGHT AND HAD A RIGHT HAND ENGINE SURGE. MAINTENANCE INSPECTED AND REPLAC ED THE CANNON PLUG AT THE ECU. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002102400138 20021024 00138 SO 2002 10 24 DYM2002F00001 1 20021006 A 3220 400106 BOLT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA NLG MISSING D DYMA K NONE O OTHER IN INSP/MAINT 1 SW 05 35890 318052139 THE PILOT EXPERIENCED A NOSE GEAR NOT EXTENDING. AFTER SEVERAL EXTENSION TRIES WITH NO SUCCESS, HE LAND WITH NOSE GEAR IN NOSE WHEEL WELL. THE NLG J HOOK WAS FOUND TO BE MISSING THE NUT AND COTTER KEY, ALLOWING THE J CONTROL ROD TO DISENG AGE FROM THE J HOOK BOLT. THE J HOOK WAS DISENGAGED AND GEAR EXTENDED NORMALLY. 1 L 7 2 3O 3 O A20SO E14EA 2002102400139 20021024 00139 SW 2002 10 24 EAT2002F00001 1 20020225 A 5610 2621126905 WINDSHIELD FRCHLD SA227 SA227CC 3377522 SW GARRTT TPE331 TPE331* 01514 WP COCKPIT CRACKED B EATR A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 09 592BA AC592 THE RT COPILOTS HEATED WINDSHIELD CRACKED AT APPROX. 20,000 FEET WITH THE AIRCRAFT PRESSURIZED TO APPROXIMATELY 4.5 PSI. THE WINDSHIELD IS SPIDER CRACKED ACROSS THE ENTIRE SURFACE. THE WINDSHIELD SHOWS NO EVIDENCE OF IMPACT CAUSING THE CR ACKING. 2 L 7 2 4T 3 T RT A18SW E2WE 2002102400140 20021024 00140 CE 2002 10 24 GNB2002F00003 1 20021010 A 8120 4772400004 WASTEGATE VALVE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO TURBOCHARGER WARPED E GNBA K NONE O OTHER IN INSP/MAINT 1 SW 01 402MQ 1138 402C0095 816162R FOUND WASTEGATE BUTTERFLY VALVE WARPED, DURING ROUTINE INSPECTION. 1 L 7 2 3O 3 O A7CE E8CE 2002102400141 20021024 00141 2002 10 24 MEX2002326 4 20021012 A 3418 92743642 RELAY DOUG DC9 DC987 3022087 WP STALL WARNING DAMAGED B ASMF A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 23 753RA 49587 AIRCRAFT RETURN TO PLATFORM AS DUE TO RIGHT STALL LIGHT ON. DURING CHECK WAS DETECTED THAT THE RELAY R2-58 DAMAGED. IT WAS CHANGED AND TESTS WERE PERFORMED IAW MM. 2 L 7 2 4F RT A6WE 2002102400142 20021024 00142 NM 2002 10 24 MEX2002328 1 20021013 A 8012 VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D NE RT ENG STARTER FAILED B ASMF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 23 162PL 49765 AIRCRAFT RETURNED TO PLATFORM DUE TO RIGHT ENGINE STARTER VALVE DID NOT OPEN. THE PLUG WAS CLEANED AND THE CROSSBLEED R IGHT SIDE WAS RESET, TESTS OK. TESTED SUCH VALVE, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2002102400143 20021024 00143 EU 2002 10 24 NSV2002F00001 1 20021013 A 3350 16013211 POWER SUPPLY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN INOPERATIVE A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 237MJ 340B237 EMERGENCY LIGHTING, INOPERATIVE, FOUND PRIOR TO FIRST FLIGHT OF THE DAY. MAINTENANCE REMOVED AND REPLACED ALL POWER SUP PLIES. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RELEASED FOR SERVICE. SUSPECT LIGHTS WERE INADVERTENTLY LEFT ON AFTER POW ER WAS REMOVED. 2 L 7 2 4T 4 T RT A52EU E8NE 2002102400144 20021024 00144 NM 2002 10 24 P9R2002F00007 1 20020916 A 3397 WIRE BOEING 757 757236 1384971 NM CABIN DAMAGED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 958PG 24118 LAST 4 WHITE LIGHTS OF EMERGENCY FLOOR PATH LIGHTING INTERMITTENT. FOUND WIRE PULLED OUT OF LIGHT SOCKET. SECURED WIRE LIGHTS CHECK, OK. 2 L 7 2 4F RT A2NM 2002102400145 20021024 00145 NM 2002 10 24 P9R2002F00008 1 20020930 A 3350 LIGHT BOEING 727 727231 1384079 NM PWA JT8 JT8D9 52048 NE CABIN LOOSE A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 54344 21631 GALLEY EMERGENCY EXIT FLOOR GLOW STRIP NOT ATTACHED TO FLOOR. RESECURED EMERGENCY EXIT FLOOR LIGHTING. 2 L 7 3 4F 4 F A3WE E2EA 2002102400146 20021024 00146 CE 2002 10 24 S2Y2002F00000 1 20020904 A 3244 TIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MLG FAILED A S2YA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 13 92SK UE92 DURING TAKEOFF THE CREW NOTED AN EXTRA JUMP OFF THE RUNWAY. THE CREW DID AN AIR TURN BACK BUT UPON LANDING THE AIRCRAFT BLEW ALL FOUR TIRES. MECHANIC INSPECTED THE BRAKE SYSTEM AND FOUND NO DEFECTS. MECHANIC REPLACED ALL THE TIRE AND RET URNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T 3 T RT A24CE E2NE 2002102400147 20021024 00147 CE 2002 10 24 S2YA02029 1 20020725 A 2120 ODOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA COCKPIT DETECTED A S2YA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 13 81SK UE81 DURING PREFLIGHT, NOTICE OF A STRONG ODOR WITH THE BATTERY SWITCH ON AND USING THE RADIO FOR GROUND COMMUNICATION. MECH ANIC THOROUGHLY INSPECTED THE AIRCRAFT BUT NOTED NO DISCREPANCIES. 2 L 7 2 4T 3 T RT A24CE E2NE 2002102400148 20021024 00148 NE 2002 10 24 S2YA02030 2 20020805 A 7200 ENGINE DORNER DO32 DO328300 NM PWA 306 PW306B NE RIGHT FAILED A S2YA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 13 352SK 3164 CD0204 SHORTLY AFTER TAKEOFF, THE CREW HEARD A THUD ON THE SIDE OF THE PLANE. THIS WAS FOLLOWED BY A RISE IN ITT AND FUEL FLOW BUT A DROP IN OIL PRESSURE. THE CREW MADE AN AIR TURN BACK. MECHANIC INSPECTED THE RIGHT ENGINE AND FOUND DAMAGE TO T HE HP TURBINE. MECHANIC REPLACED THE ENGINE. 2 H 7 2 4T 4 F RT A55NM E35NE 2002102400149 20021024 00149 NE 2002 10 24 S2YA02031 3 20020808 A 6110 PROPELLER BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA HARTZL HCE4A HCE4A3I NE RIGHT LEAKING A S2YA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 13 85SK UE85 SHORTLY AFTER TAKEOFF OF FLIGHT, THE CREW NOTICED OIL ON THE RIGHT NACELLE. THE MADE AND AIR TURN BACK. MECHANIC INSPE CTED THE ENGINE AND REPLACED THE PROP FOR LEAKING. 2 L 7 2 4T 3 T RT A24CE E2NE 5 C P10NE 2002102400150 20021024 00150 CE 2002 10 24 S2YA02032 1 20020809 A 3230 MS24171D1 RELAY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA POWER PACK INOPERATIVE A S2YA O OTHER J WARNING INDICATION AP APPROACH 1 GL 13 901SK UE90 ON APPROACH, THE CREW SELECTED GEAR DOWN BUT THE GEAR FAILED TO EXTEND. THE CREW MANUALLY EXTENDED THE GEAR AND MADE AN UNEVENTFUL LANDING. THE A/C WAS FERRIED BACK. MECHANIC INSPECTED THE SYSTEM AND REPLACED THE POWER PACK RELAY. 2 L 7 2 4T 3 T RT A24CE E2NE 2002102400151 20021024 00151 CE 2002 10 24 S2YA02033 1 20020816 A 3260 MS252531 WARNING SYSTEM BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MLG INOPERATIVE A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 91SK UE91 AFTER TAKEOFF, THE CREW SELECTED GEAR UP BUT GO A RED GEAR UNSAFE LIGHT. THE CREW CONSULTED WIGH MECHANIC AND CYCLED TH E GEAR BUT STILL HAD AN RED IN TRANSIT LIGHT. THE CREW DID AIR TURN BACK AND MADE AN UNEVENTFUL LANDING. MECHANIC INSP ECTED THE SYSTEM AND REPLACED THE POWER LEVER LANDING GEAR WARNING HORN CONTROL. THE A/C DID A TEST FLIGHT WITH NO FURT HER DEFECTS. 2 L 7 2 4T 3 T RT A24CE E2NE 2002102400152 20021024 00152 NM 2002 10 24 S2YA02034 1 20020822 A 4990 4068B000002 ECU DORNER DO32 DO328300 NM RIGHT INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 353SK 2218 3122 DURING ENGINE START UP, SMOKE WAS OBSERVED IN THE CABIN AND A CAS MESSAGE FOR LT ENVIRO APPEARED. MECHANIC REPLACED THE ECS FLOW CONTROL AND SHUTOFF VALVE AND RELEASED THE AIRCRAFT. THE NEXT DAY IT NOTED THERE WAS OIL SMELL IN THE AIRCRAF T. MECHANIC INSPECTED THE SYSTEM AND FOUND THE APU TO LEAKING OIL. REPLACED THE APU. 2 H 7 2 4T RT A55NM 2002102400153 20021024 00153 NE 2002 10 24 S2YA02035 2 20020903 A 7321 8063005 FUEL CONTROL BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE INOPERATIVE A S2YA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 GL 13 145SK 126 UE145 DURING FLIGHT, DURING INITIAL DECENT INTO THE RIGHT ENGINE STARTED LOSING POWER. THE CREW DIVERTED AND MADE AN UNEVENTF UL LANDING. MECHANIC INSPECTED THE AIRCRAFT AND REPLACE THE RIGHT ENGINES HIGH PRESSURE FUEL PUMP FOR TROUBLE SHOOTING BUT IT DID NOT FIX THE PROBLEM. MECHANIC REPLACED THE FUEL CONTROL UNIT (FCU) AND OPS CHECKED THE SYSTEM WITH NO FURTHE R DEFECTS NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 2002102400154 20021024 00154 NM 2002 10 24 USAABB02172 1 20021006 A 2597 G899314 CONNECTOR BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE ESCAPE SLIDE DEFORMED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 645US 23897 DURING AN OPERATIONAL CHECK OF THE RIGHT OVERWING SLIDE (AIRCRAFT IS IN A HEAVY MAINTENANCE VISIT), THE SLIDE DID NOT DE PLOY NORMALLY DUE TO THE FAILURE OF THE INBOARD SPOILER TO RETRACT. MAINTENANCE FOUND TWO BENT PINS IN THE CONNECTOR FO R THE SPOILER OVERRIDE SQUIB. THE PINS WERE BENT AS A RESULT OF IMPROPER INSTALLATION OF A BLANKING PLUG. A CHANGE HAS BEEN SUBMITTED TO THE MAINTENANCE PROGRAM CARD TO CAUTION MECHANICS CONCERNING THE INSTALLATION AND REMOVAL OF THE BLAN KING PLUG. THE AIRCRAFT IS PROGRAMMED FOR REPAIR AND OPERATIONAL RETEST OF THE OVERWING SLIDE. 2 L 7 2 4F 4 F RT A1NM E13NE 2002102400155 20021024 00155 NM 2002 10 24 USAABB02173 1 20021008 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE ROW 6 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 605AU 22201 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 6, INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A2NM A12EU 2002102400156 20021024 00156 NM 2002 10 24 USAASB02184 1 20021002 A 3260 189929 UPLOCK SENSOR BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE LT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 507AU 23382 ON CLIMB OUT, CREW RECEIVED A LT MAIN LANDING GEAR UNSAFE LIGHT AFTER GEAR RETRACTION. CREW RECYCLED GEAR WITH SAME RES ULTS. FLIGHT RETURNED TO FIELD AT PI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMO VED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK SENSOR IAW MM. SWUNG GEAR SEVERAL TIMES. OPERATIONAL CHECK AND INDI CATION CHECK TEST GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110500132 20021105 00132 NM 2002 11 5 WRLA200222 1 20020913 A 2710 PIN DOUG MD11 MD11F 3023600 NM CONNECTOR BACKED OUT A WRLA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 27 275WA 48631 AILERON DEFLECT DISAGREE UPON FLAP RETRACTION, AIRCRAFT RETURNED TO DEPARTING STATION PANC. REPAIRED CONNECTOR PIN AT P 1-1667. PIN E AND ALL FCC FLAP SYSTEMS PASSED RETURN TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2002102400157 20021024 00157 NM 2002 10 24 QXEA0201483 1 20020912 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- 524BT ATTACH HOLE AT CORNER IS SLIGHTLY ELONGATED WITH DISPLACED METAL. REPAIRED IAW DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002102400158 20021024 00158 NM 2002 10 24 QXEA0201484 1 20020913 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- 524CT HAS SEVERAL HOLES WITH RAISED METAL ON LOWER SURFACE. REPAIRED IAW DHC-8 SRM 51-20-11 AND 51-20-16. 2 H 7 2 4T RT A13NM 2002102400159 20021024 00159 NM 2002 10 24 QXEA0201485 1 20020912 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- 524BT HAS LIGHT SURFACE CORROSION ON UNDER SIDE. REPAIRED IAW DHC-8 SRM 51-20-11, 51-20-16 AND 51-00-06. 2 H 7 2 4T RT A13NM 2002102400160 20021024 00160 NM 2002 10 24 QXEA0201486 1 20020912 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- 524CT HAS LIGHT SURFACE CORROSION ON INTERIOR SIDE ALONG INBOARD END OF FASTENER HOLES. REPAIRED IAW DHC-8 SRM 51- 20-11, 51-20-16 AND 51-00-06. 2 H 7 2 4T RT A13NM 2002102400161 20021024 00161 NM 2002 10 24 QXEA0201510 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 TOP AND BOTTOM CORROSION IN AREA OF SEAT ATTACH AT APPROXIMATELY X343.00. REPLA CED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400162 20021024 00162 NM 2002 10 24 QXEA0201511 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 TOP CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X38.00. REPLACED NR 4 SEAT T RACK. 2 H 7 2 4T RT A13NM 2002102400163 20021024 00163 NM 2002 10 24 QXEA0201512 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 BOTTOM CHAFED APPROXIMATELY 12 INCHES BY TRACK COVER AT APPROXIMATELY X322.00. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400164 20021024 00164 NM 2002 10 24 QXEA0201513 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 CORROSION TOP AND BOTTOM OF SEAT ATTACH AREA AT APPROXIMATELY X312.00. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400165 20021024 00165 NM 2002 10 24 QXEA0201514 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 4 CORROSION ON TOP IN AREA OF SEAT ATTACH AT APPROXIMATELY X298.00. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400166 20021024 00166 NM 2002 10 24 QXEA0201535 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 5 FORWARD OUTBOARD FLANGE CORROSION AROUND EIGHT RIVETS AT X426. REPLACED NR 5 SE AT TRACK. 2 H 7 2 4T RT A13NM 2002102400167 20021024 00167 NM 2002 10 24 QXEA0201536 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND INBOARD SEAT TRACK NR 9 INBOARD FLANGE CORROSION AT X530.00. REPLACED NR 9 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400168 20021024 00168 NM 2002 10 24 QXEA0201537 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 10 TOP CORROSION IN SEAT ATTACH AREA AT X424.00. REPLACED NR 10 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400169 20021024 00169 NM 2002 10 24 QXEA0201538 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 10 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X407.00. REPLACED NR 10 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400170 20021024 00170 NM 2002 10 24 QXEA0201539 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 10 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X393.00. REPLACED NR 10 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400171 20021024 00171 NM 2002 10 24 QXEA0201540 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 10 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X377.00. REPLACED NR 10 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400172 20021024 00172 NM 2002 10 24 QXEA0201541 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 10 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X363.00. REPLACED NR 10 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400173 20021024 00173 NM 2002 10 24 QXEA0201542 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 10 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X343.00. REPLACED NR 10 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400174 20021024 00174 NM 2002 10 24 QXEA0201543 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 10 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X328.00. REPLACED NR 10 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400175 20021024 00175 NM 2002 10 24 QXEA0201544 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 10 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X312.00. REPLACED NR 10 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400176 20021024 00176 NM 2002 10 24 QXEA0201545 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 10 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X298.00. REPLACED NR 10 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400177 20021024 00177 NM 2002 10 24 QXEA0201546 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 10 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X280.00. REPLACED SEAT TRACK . 2 H 7 2 4T RT A13NM 2002102400178 20021024 00178 NM 2002 10 24 QXEA0201547 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 6 CORROSION AROUND INBOARD NUT PLATE AT X565.00. REPLACED NR 6 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400179 20021024 00179 NM 2002 10 24 QXEA0201548 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 6 CORROSION AROUND INBOARD NUT PLATE AT X548.00. REPLACED NR 6 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400180 20021024 00180 NM 2002 10 24 QXEA0201549 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 1 TOP CORROSION IN SEAT ATTACH AREA AT X393.00. REPLACED NR 1 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400181 20021024 00181 NM 2002 10 24 QXEA0201550 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 1 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X407.00. REPLACED NR 1 SEAT TR ACK. 2 H 7 2 4T RT A13NM 2002102400182 20021024 00182 NM 2002 10 24 QXEA0201551 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 1 TOP CORROSION IN SEAT ATTACH AREA AT 424.00. REPLACED NR 1 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400183 20021024 00183 NM 2002 10 24 QXEA0201552 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 6 CORROSION AROUND INBOARD NUT PLATE AT X580.00. REPLACED NR 6 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400184 20021024 00184 NM 2002 10 24 QXEA0201553 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 6 CORROSION AROUND INBOARD NUT PLATE AT X580.00. REPLACED NR 6 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400185 20021024 00185 NM 2002 10 24 QXEA0201554 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 6 CORROSION AROUND OUTBOARD NUT PLATE AT X591.00. REPLACED NR 6 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102400186 20021024 00186 NM 2002 10 24 QXEA0201555 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD SEAT TRACK NR 6 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X541.00. REPLACED NR 6 SEAT TRA CK. 2 H 7 2 4T RT A13NM 2002102400187 20021024 00187 WP 2002 10 24 UPS02839427 1 20020827 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C-1 STA 8.0, LONG 33R DOUBLER, CLASSIFIED CATEGORY D. REMOVED DOUBLER, CUT OUT DAMAGED AREA NDT HFEC IN SPECTED NO CRACKS NOTED. FABRICTAED FILLER AND DOUBLER IAW SAA SK 708-080. INSTALLED FILLER AND DOUBLER IAW EO DC8-533 0-12800-C, AND SAA SK 708-080. 2 L 7 4 4F RT 4A25 2002102400188 20021024 00188 WP 2002 10 24 UPS02839433 1 20020827 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 8.000, LONG 33L DOUBLER INSTALLED, CLASSIFIED CATEGORY D. REMOVED DOUBLER, STOP DRILLED CRACK ND T HFEC INSPECTED, CRACK TERMINATES AT STOP DRILL. CUT OUT DAMAGED AREA, FABRICATED FILLER AND REPAIR DOUBLER IAW SK 708 -078, INSTALLED FILLER AND REPAIR DOUBLER IAW SAA SK708-078, AND EO DC8-53-20245. 2 L 7 4 4F RT 4A25 2002102400189 20021024 00189 WP 2002 10 24 UPS02839434 1 20020827 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C-1 LONG 17L AND END FITTING CRACKED AT STA 1772. REMOVED LONG AND END FITTING, FABRICATED LONGERON SLI CE AND DRILLED UP NEW END FITTING IAW DRAWING 5649327 AND SRM 51-1-24, INSTALLED REPAIR PARTS IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102400190 20021024 00190 WP 2002 10 24 UPS02839435 1 20020904 A 5230 PAN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C-1 A-PIT DOOR LWR PAN UNDER AFT STOP FITTING IS CRACKED STA 360.000 LONG 26R. REMOVED CRACKED LWR PAN IAW 52-4-1, NDT HFEC INSPECTED, NO CRACKS NOTED AROUND CUT OUT. FABRICATED PAN SEGMENT AND REPAIR ANGLES IAW SRM 52-4-1 , INSTALLED PAN SEGMENT AND REPAIR ANGLES. 2 L 7 4 4F RT 4A25 2002102400191 20021024 00191 WP 2002 10 24 UPS02839436 1 20020913 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CARGO BAY MALFUNCTIONED A IPXA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 894UP 46094 INSPECTION TYPE:N/A LOWER CARGO COMPARTMENT FIRE LIGHT CAME ON FOR ONE MINUTE THEN WENT OUT FWD B ON DISPLAY PANEL. PER FORM OPS CK TO LOWER CARGO SMOKE DETECTOR IAW DC-8 MM 26-18-01 ADJ &TEST OK TO CONTINUE NO FAULTS FOUND. 2 L 7 4 4F RT 4A25 2002102400192 20021024 00192 WP 2002 10 24 UPS02839438 1 20020826 A 5320 37558401 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C2 STA 1228 BATHTUB FITTING IS CRACKED BETWEEN LONG 32R-33R INSIDE TORQUE BOX. REMOVED AND REPLACED FIT TING IAW DWG 3755840, AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002102400193 20021024 00193 WP 2002 10 24 UPS02839439 1 20020822 A 5320 47533601 ATTACH FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 822 LONG 22L INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4753360, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102400195 20021024 00195 WP 2002 10 24 UPS02839441 1 20020829 A 5320 975494955 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1240 INTERCOSTAL ABOVE LONG 33R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED INTE RCOSTAL IAW DWG 9754949, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102400196 20021024 00196 WP 2002 10 24 UPS02839443 1 20020827 A 5230 ANGLE DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 A-PIT CARGO DOOR FWD AND AFT ANGLES UNDER SEAL AREA AT STA 280 AND 340 ARE CRACKED ON DOOR. REMOVED, FABRICATED AND REPLACED ANGLES IAW DWG 5754260, AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2002102400197 20021024 00197 NM 2002 10 24 SPAA0200056 1 20021022 A 3350 1000679 BATTERY PACK BOEING 737 7372T4 1384492 NM UNSECURE A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 L-2 DOOR EMERGENCY BATTERY PACK FALLS OFF. REPLACED EMERGENCY DOOR BATTERY PACK PER AMM 33-51-0, OPS CHECK GOOD PER AMM 31-51-101. 2 L 7 2 4F A16WE 2002102400198 20021024 00198 NM 2002 10 24 SPAA0200057 1 20021022 A 3350 100067 BATTERY PACK BOEING 737 7372T4 1384492 NM DISCHARGED A SPAA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 WP 28 703S 22529 L-1 DOOR EMERGENCY LIGHT PACK DIM. REPLACED LIGHT PACK PER AMM 33-51-101, OPS CHECK GOOD 2 L 7 2 4F A16WE 2002102400199 20021024 00199 EA 2002 10 24 COMA0260601 1 20021022 A 2120 DISPLAY CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J O WARNING INDICATION OTHER CR CRUISE 1 SO 01 916CA 7014 FLIGHT 6076 DISPLAY COOL CAUTION MESSAGE.REMOVED DUST BLOCKAGE FROM FLIGHT DISPLAY INLET SCREENS. 2 L 7 2 4F RT A21EA 2002102400200 20021024 00200 EA 2002 10 24 COMA0260602 1 20021022 A 7931 6087T04P05 PUMP CNDAIR CL600 CL6002B19 1900309 EA R/H ENGINE WEAK A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 446CA 2386 7546 FLIGHT 5917 RIGHT ENGINE OIL PRESSURE DROPPED STEADILY AND TEMP INCREASED.REPLACED THE LUBE/SCAVENGE OIL PUMP. 2 L 7 2 4F RT A21EA 2002102400201 20021024 00201 EA 2002 10 24 COMA0260603 1 20021022 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING E W VIBRATION/BUFFET INADEQUATE Q C CL CLIMB 1 SO 01 710CA 7241 FLIGHT 5670 LOUD SQUEAL AND VIBRATION IN FLIGHT.FOUND AIRCRAFT EXTERNAL SERVICE PANEL OPEN. INPSPECTED FOR DAMAGE AND S ECURED DOOR. 2 L 7 2 4F RT A21EA 2002102400202 20021024 00202 WP 2002 10 24 ABXA020256 1 20021021 A 2700 9957536U13 FLANGE DOUG DC9 DC932 3022066 WP RIGHT FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 RIGHT FLAP INBOARD FIXED VANE GOUGED ON UPPER SURFACE DUE TO CRACKED ATTACH ANGLE. REPLACED FIXED VANE AND CRACKED VANE ATTACH ANGLE IAW DC-9 SRM 51-30-05 AND DC-9 MM 27-51-03-2-0002. 2 L 7 2 4F A6WE 2002102400203 20021024 00203 WP 2002 10 24 ABXA020257 1 20021018 A 3260 7000010101 SWITCH DOUG DC9 DC931 3022065 WP DEFECTIVE A ABXA K NONE O OTHER AP APPROACH 1 GL 23 948AX 47065 NOSE LANDING GEAR DOWN SAFE LIGHT DID NOT ILLUMINATE WITH GEAR HANDLE DOWN AND NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINAT ED. RECYCLED HANDLE, SAME INDICATION. DURING ABNORMAL CHECKLIST, NORMAL GEAR DOWN INDICATION OCCURED. REPLACED THE NOSE LANDING GEAR DOWN LOCK POSITION AND WARNING SWITCH IAW DC-9 MM 32-60-00-0-0101. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002102400204 20021024 00204 CE 2002 10 24 044284 1 20021022 A 3210 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE FAILED A AMWA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 CE 07 131YV 0 0 UE131 AFTER TAKE OFF FROM ENID OKLAHOMA TO DENVER COLORADO ON FLIGHT 2501, THE CREW RETRACTED THE LANDING GEAR AFTER A POSITIV E RATE OF CLIMB WAS ESTABLISHED. WHEN THE GEAR WAS SELECTED UP, THE GEAR TRANSIT INTRANSIT LIGHT WOULD NOT EXTINGUISH. T HEREFORE THE AIRCRAFT RETURNED TO ENID OKLAHOMA WITH NO FURTHER INCIDENT. THE MAINTENANCE PERFORMED A WALK AROUND INSPEC TION. THE CORRECTIVE ACTION WAS THAT THEY REMOVED AND REPLACED THE LEFT HAND MAIN LANDING GEAR UPLOCK SWITCH. NO TEARDOW N REPORT WILL BE REQUIRED. 2 L 7 2 4T RT A24CE 2002102400205 20021024 00205 NM 2002 10 24 AWXA200201045 1 20021003 A 5753 655214129 SKIN BOEING 737 737301 1384611 NM WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 0 0 23261 MCN - MAJOR REPAIR - DURING C-17 CHECK A WORN AREA WAS FOUND ON THE L/H WING MID FLAP AT THE TOP INBOARD END, WBL 73. MA INTENANCE CUTOUT DAMAGED AREA OF L/H WING MID FLAP AT THE TOP INBOARD END WBL 73; FABRICATED A PLATE, 2 EACH DOUBLERS, A ND A FILLER; BONDED SKIN ASSEMBLY; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 57-53-01, PG. 206-207, FIG. 203. 2 L 7 2 4F RT A16WE 2002102400206 20021024 00206 NM 2002 10 24 AWXA200201046 1 20020730 A 5753 657373163 SKIN BOEING 737 737277 1384570 NM DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 0 0 22650 MCN - MAJOR REPAIR - DURING C-18 CHECK THE R/H WING INBOARD FORE FLAP WAS FOUND TO HAVE DELAMINATION ON UPPER SKIN 6" IN BOARD OF THE #3 FORE FLAP TRACK. MAINTENANCE CUTOUT DELAMINATED AREA OF SKIN ON R/H WING INBOARD FORE FLAP; BONDED AND P OTTED REPAIR CORE; FABRICATED A REPAIR DOUBLER; BONDED AND SEALED REPAIR DOUBLER ON R/H WING INBOARD FOREFLAP IAW B737-2 00 SRM 51-40-20, FIG. 18, PG. 63-67. 2 L 7 2 4F RT A16WE 2002102400207 20021024 00207 SO 2002 10 24 C2XA02IA224 1 20021010 A 3350 20131A BATTERY EMB 145 EMB145 3260210 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13958 145085 BNA- MAINTENANCE NOTED THAT THE ENTRY WAY EMERGENCY LIGHTS FAILED TO IL;UMINATE. BNA- MAINTENANCE REMOVED AND REPLACE D THE #1 EMERGENCY LIGHT BATTERY, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002102500005 20021025 00005 SW 2002 10 25 2002F00960 1 20021024 A 2550 52801700 CARGO HOOK BELL 407 407 1182206 SW CARGO HANDLING BROKEN G S64L K NONE O OTHER IN INSP/MAINT 1 SO 17 407HS 520 520 53256 DURING AN ANNUAL INSPECTION & 3 YEAR HOOK OVERHAUL THE MECHANIC PULLED DOWN ON THE CARGO HOOK, AND THE LT HARD POINT BRA CKET FAILED, LEAVING THE CARGO HOOK BEAM SUPPORT HELD ONLY BY THE RIGHT BRACKET. 1 G 7 1 3U O H2SW 2002102500010 20021025 00010 2002 10 25 CGO2002F00003 4 20021010 A 2562 CASE BEECH 90 C90A 1152911 CE PWA PT6 PT6* 52043 EA BATTERY CORRODED B CGOR K NONE O OTHER IN INSP/MAINT 1 GL 03 831E 201 LJ1650 DURING ANNUAL INSPECTION NOTED ELT BATTERY TO HAVE LEAKED CORROSIVE MATERIAL INTO ELT AND ONTO SURROUNDING AIRCRAFT STRU CTURE. REQUIRED REPLACEMENT OF ELT AND CORROSION REMOVAL AND TREATMENT OF AIRCRAFT MOUNT SHELF AREA. 1 L 7 2 3T 3 T RT 3A20 E2NE 2002102500012 20021025 00012 CE 2002 10 25 R2J2002F00011 1 20020830 A 2730 505246113 CONTROL CABLE BEECH 90 C90 1152913 CE PWA PT6 PT6A60A 52043 NE ELEVATOR MISINSTALLED B R2JR K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 21 35TV 9852 LJ572 DURING AUTO-PILOT TROUBLESHOOTING, INSPECTOR FOUND MAJOR BIND IN ELEVATOR CONTROLS. INSPECTION REVEALED ELEVATOR CABLE IN AFT FUSELAGE MISROUTED, DURING MAINTENANCE, (5 HOURS PREVIOUS) CAUSING ELEVATOR CABLE TO RUB SEVERELY ON HORIZONTAL S TABILIZER STRUCTURE, DAMAGING IT. CABLE WAS IMPROPERLY ROUTED JAMMING ELEVATOR DUE TO CABLE RUBBING STRUCTURE. EVIDENT LY NO INSPECTION COMPLETED AFTER MAINTENANCE. 1 L 7 2 3T 4 T 3A20 E4EA 2002102500013 20021025 00013 EU 2002 10 25 VJ32002F00088 1 20021011 A 8011 LW16635 RING GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA STARTER DAMAGED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 867AF 78 85007 FOLLOWING A ROUTINE FLIGHT, A ROUTINE INSPECTION FOUND THAT THE AFT ALTERNATOR BELT GROOVE HAD BROKEN AWAY FROM THE STAR TER RING ASSY. THIS HAD CAUSED THE BELT TO BE DAMAGED BEYOND USE. PIECES OF MATERIAL FROM THE STARTER RING AND RUBBER FROM THE BELT WERE FOUND THROUGHOUT THE ENGINE BAY. POSSIBLE CAUSE COULD BE A MFG FLAW OR EXCESSIVE BELT TENSION. 1 L 7 1 3O 3 O RT A49CE 1E4 2002102500014 20021025 00014 EU 2002 10 25 VJ32002F00090 1 20021014 A 2910 X030007 VALVE GROB 120 G120A 1660208 EU MANIFOLD LEAKING B VJ3R K NONE K FLUID LOSS IN INSP/MAINT 1 WP 07 867AF 73 85007 DURING ANNUAL INSPECTION OF AIRCRAFT HYDRAULIC PRESSURE WOULD NOT HOLD. TROUBLESHOOTING INDICATED THAT THE EMERGENCY MAI NIFOLD VALVE WAS BLEEDING DOWN. REPLACED MANIFOLD VALVE. 1 L 7 1 3O RT A49CE 2002102500015 20021025 00015 SO 2002 10 25 VJ32002F00092 1 20021014 A 2421 ALU853LS ALTERNATOR PIPER PA28 PA28181 7102807 SO LYC O320 O320D3G 41508 EA ENGINE FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 4166H 251 2843119 DURING GROUND RUN ALTERNATOR SHOWED NORMAL OUTPUT AFTER ENGINE WARMED UP TO OPERATING TEMPERATURES AND STARTED TO APPLY LOAD TO ALTERNATOR LOAD DROPPED OFF LINE AND WOULD NOT RESET. BELIEVE INTERNAL FAILURE. 1 L 7 1 3O 3 O 2A13 E274 2002102500016 20021025 00016 CE 2002 10 25 VJ32002F00093 1 20021014 A 3610 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO DRY AIR FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 1565A CE1331 DURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT U P AND AIR PRESSURE STILL LOW AT HIGHER RPM. PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP. 1 L 7 1 3O 3 O 3A15 E5CE 2002102500017 20021025 00017 CE 2002 10 25 AMW2002F00005 1 20020909 A 5210 12951405933 CABLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA PAX DOOR BROKEN A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 13ZV 21656 UE13 UPON ARRIVAL, A RAMPER PROCEEDED TO OPEN PASSENGER DOOR. THE RAMPER BACKED AWAY FROM THE DOOR AND THE DOOR PROCEEDED TO FREE FALL BREAKING THE SUPPORT ANCHOR BRACKETS. THE DOOR SNUBBER CABLE WAS DEFERRED. THE CORRECTIVE ACTION WAS THAT T HE CABLE ASSEMBLY WAS REPLACED. 2 L 7 2 4T 3 T RT A24CE E2NE 2002102500018 20021025 00018 CE 2002 10 25 AMW2002F00006 1 20020920 A 5270 MS250081 SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CARGO DOOR STUCK A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 233YV 14320 UE233 WHILE ENROUTE, THE CARGO DOOR ILLUMINATED 60 MILES OUTSIDE OF DESTINATION. THE AIRCRAFT CONTINUED, WITH NO FURTHER INCI DENT. MAINTENANCE FOUND THAT THE SWITCH WAS STUCK. C/A: LUBRICATED THE SWITCH. 2 L 7 2 4T 3 T RT A24CE E2NE 2002102500019 20021025 00019 CE 2002 10 25 CED2002F00000 1 20020905 A 2910 AN620612 REGULATOR LEAR 25 25 5170506 CE GE CJ610 CJ6106 30006 NE HYD PRESSURE CRACKED E CEDA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 05 273CA 039 AIRCRAFT WAS ENROUTE, LOST HYDRAULIC PRESSURE. AIRCRAFT DIVERTED, MAINTENANCE FOUND HYDRAULIC PRESSURE REGULATOR LEAKIN G. THE VALVE BODY WAS CRACKED AT ONE OF THE BORES. THE TIME ON THE VALVE WAS APPROX 3 HOURS SINCE REPAIR. 2 L 7 2 4J 4 J A10CE 1E16 2002102500020 20021025 00020 EU 2002 10 25 02170307 1 20021017 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA O OTHER O OTHER CR CRUISE 1 EA 27 307UE 41021 DURING CRUISE OF THE FLIGHT FROM ABE TO IAD, THE CREW REPORTED FLOOR TRACK LIGHTING(EMERGENCY LTS) BURNED OUT NEAR SEAT 3A. MAINTENANCE PERSONNEL REATTACHED EMERGENCY LIGHTING TRACK. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002102500021 20021025 00021 NM 2002 10 25 02FDEA00656 1 20020916 A 5347 ABA7680505 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 FWD CABIN BOTTOM OF PORTABLE FIRE EXTINGUISHER MOUNTING BRACKET, FOUND SEAT TRACK CORRODED AT BS 475-495. R&R SEAT TRAC K PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2002102500022 20021025 00022 NM 2002 10 25 02FDEA00657 1 20020917 A 5311 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 FUSELAGE TRANSVERSE FRAME LT CRACKED AT 2 PLACES STA Y= 535, LONGERON 19L-20L WAS 1.531 INCHES AND AT LONGERON 23L-24L W AS 2.781 INCHES. R&R FRAME PER DWG SRZ-53-503, SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 2002102500023 20021025 00023 NM 2002 10 25 PCAA0210125 1 20021023 A 3350 82410162 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM INOPERATIVE A PCAA K NONE O OTHER UK UNKNOWN 1 EA 13 846EX 326 SCE FLIGHT#3836. CREW REPORTED EMERGENCY LIGHTS CAME ON WHEN CYCLED OFF WITH EXTERNAL POWER APPLIED. LIGHTS WORK NORMALL Y WITH BATTERY POWER. MAINTENANCE REPLACED THE EMERGENCY LIGHTS CONTROL BOX. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2002102500024 20021025 00024 EA 2002 10 25 02180655 1 20021018 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 655BR 7457 DURING TAXI OF THE FLIGHT FROM ORD TO MSN, CREW REPORTED CABIN OVERHEAD EMERGENCY LIGHT BURNED OUT. MAINTENANCE PERSONN EL RELAMPED OVERHEAD CABIN EMERGENCY LIGHTING. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002102500025 20021025 00025 EU 2002 10 25 02238327 1 20020826 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 327UE 41080 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT FWD EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONN EL REMOVED AND REPLACED THE LAMP IN THE RT FWD EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCR AFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002102500026 20021025 00026 NM 2002 10 25 02238671 1 20020826 A 2133 OUTFLOW VALVE BOMBDR DHC8 DHC8402 NM GE CF34 CF34* NE FUSELAGE FAILED A VTZA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 27 671BR DURING CRUISE FROM ORD TO GSP, THE AIRCRAFT EXPERIENCED LOSS OF CABIN PRESSURE AT 33,000 FT. CREW DECLARED AN EMERGENCY WITH ATC AND PERFORMED AN EMERGENCY DESCEND. AIRCRAFT LANDED IN GSP WITHOUT ANY FURTHER INCIDENT. MAINTENANCE PERSONNEL INSPECTED AND FOUND FOREIGN OBJECT IN THE LT OUTFLOW VALVE, ITEM WAS REMOVED AND AN OPERATIONAL CHECK OF SYSTEM WAS SA TISFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE 2 H 7 2 4T 4 F RT A13NM E15NE 2002102500027 20021025 00027 EA 2002 10 25 02282648 1 20021009 A 3620 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA PYLON OUT OF POSITION A VTZA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 648BR 7406 DURING CRUISE OF THE FLIGHT FROM PWM TO ORD, THE CREW REPORTED A 14TH STAGE BLEED FAIL ANNUNCIATOR THAT DID NOT EXTINGUI SH AFTER THE QRH PROCEDURES WERE COMPLIED WITH. THE ENGINE WAS SHUTDOWN AND THE FLIGHT DIVERTED TO SYR AND LANDED WITHO UT INCIDENT. MAINTENANCE PERSONNEL FOUND THE PYLON OVERHEAT WARNING LOOP RESTING ON THE BLEED AIR DUCT. THEY REPOSITIO NED THE LOOP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002102500028 20021025 00028 EU 2002 10 25 02287313 1 20021014 A 3320 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA L ABORTED APPROACH O OTHER CR CRUISE 1 EA 27 313UE 41026 DURING CRUISE OF THE FLIGHT FROM BUF TO IAD, THE CREW REPORTED EMERGENCY LIGHT TRACKING LIGHTING INOPERATIVE ON LEFT SID E OF AIRCRAFT. MAINTENANCE SECURED CONNECTOR ON EMERGENCY TRACK LIGHTING. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4T RT A41NM 2002102500029 20021025 00029 EU 2002 10 25 02287324 1 20021014 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 324UE 41017 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LITES INOPERATIVE ON TRACK LIGHT. MAINTENANCE PERSONNEL READJUS TED LIGHTING TRACK TO EXPOSE BULBS. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002102500030 20021025 00030 EU 2002 10 25 02287324A 1 20021014 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 324UE 41017 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LITES INOPERATIVE ON TRACK LIGHT. MAINTENANCE PERSONNEL READJUS TED LIGHTING TRACK TO EXPOSE BULBS. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002102500031 20021025 00031 EA 2002 10 25 2115403 1 20021022 A 3350 LIGHT FRCHLD 125 125FRCHLD EA CABIN INOPERATIVE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 410FJ DURING INSPECTION FWD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REPLACED FWD EMERGENCY LIGHT BULB AND AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 1 Q 7 1 3I ATC368 2002102500032 20021025 00032 GL 2002 10 25 233151 1 20021024 A 3350 LIGHT BOMBDR BD700 BD7001A10 1390006 GL CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 644BR DURING INSPECTION FLOOR TRACK EMERGENCY LIGHTS 9 THRU 13 WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE POWER STRIP AN OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00003NY 2002102500033 20021025 00033 EU 2002 10 25 28023111 1 20021017 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 317UE 41031 DURING INSPECTION EMERGENCY FLOOR TRACK LIGHTS WERE INTERMITTENT. MAINTENANCE PERSONNEL CLEANED EMERGENCY LIGHT SELECTOR SWITCH. OPERATIONAL CHECK WAS DONE AND AIRCRAFT WAS RELEASED FOR SERVICE 2 L 7 2 4T RT A41NM 2002102500034 20021025 00034 NM 2002 10 25 29222021 1 20021019 A 2530 351000393 COFFEEMAKER BOMBDR DHC8 DHC8402 NM GALLEY FAILED A VTZA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 27 658BR DURING BOARDING OF THE FLIGHT ROC TO IAD, CREW REPORTED SMOKE COMING FROM THE COFFEEMAKER, CFR WAS DISPATCHED AND PASSEN GERS RETURNED TO GATE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE COFFEE MAKER AND AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A13NM 2002102500035 20021025 00035 NM 2002 10 25 29321051 1 20021020 A 3350 LIGHT BOMBDR DHC8 DHC8400 NM CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 648BR DURING INSPECTION LT AFT EXIT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED LT AFT EXIT EMERGENC Y LIGHTING. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002102500036 20021025 00036 NM 2002 10 25 29321242 1 20021020 A 3350 LIGHT BOMBDR DHC8 DHC8400 NM CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 702BR DURING INSPECTION LT EXIT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED LT EMERGENCY OVERWING LI GHT. OPS CHECK GOOD AND AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A13NM 2002102500037 20021025 00037 EU 2002 10 25 29323071 1 20021020 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 324UE 41017 DURING INSPECTION EMERGENCY FLOOR LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL RESECURED FWD CONNECTOR, O PERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A41NM 2002102500038 20021025 00038 EU 2002 10 25 29323131 1 20021020 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU CABIN BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 306UE 41020 DURING INSPECTION RT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL CLEANED RT AFT EMERGENC Y LIGHT BULB HOLDER. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A41NM 2002102500039 20021025 00039 EU 2002 10 25 29423071 1 20021021 A 3350 SIGN JETAIR JETSTM JETSTM4101 1500501 EU CABIN CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 326UE 41064 DURING INSPECTION FWD EMERGENCY EXIT SIGN WAS CRACKED. MAINTENANCE PERSONNEL REPLACED FWD EXIT LENS AND AIRCRAFT WAS REL EASED FOR SERVICE. 2 L 7 2 4T RT A41NM 2002102500040 20021025 00040 NM 2002 10 25 02FDEA00658 1 20020917 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 CORROSION LWR CHORD BS 1130, WL 200, LBL 55 - RBL 55. R&R CHORD PER EA 7-5310-62008. 2 L 7 3 4F RT A3WE 2002102500041 20021025 00041 NM 2002 10 25 02FDEA00660 1 20020917 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 DENTED FRAME AT BS 600 BETWEEN STR 24 LT & 25 LT. R&R FRAME PER EA 7-5310-65882. 2 L 7 3 4F RT A3WE 2002102500042 20021025 00042 NM 2002 10 25 02FDEA00661 1 20020917 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 STRINGER 7L, BS 720B+14 IS GOUGED. R&R STRINGER PER SRM 53-10-3 FIG 3. 2 L 7 3 4F RT A3WE 2002102500043 20021025 00043 NM 2002 10 25 02FDEA00665 1 20020919 A 3231 1U10851 SEQUENCE VALVE BOEING 727 727100 1384036 NM RT MLG WW MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 124FE 19360 UPON GEAR RETRACTION, GEAR DOORS LIGHT & RIGHT MAIN GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. RED TAB PROCEDURES ACCOMPL ISHED. WHEN INITIALLY MOVING, AND BEFORE REACHING THE "OFF" POSITION, IT APPEARED A HYDRAULIC SURGE OCCURRED , WITH A CORRESPONDING "BUMP" AND BOTH LIGHTS EXTINGUISHED. REMOVED AND REPLACED MAIN LANDING GEAR LOCK OPERATED SEQUENCE VALVE PER 727-100 MAINTENANCE MANUAL 32-32-031-4, OPERATIONAL CHECK GOOD PER 727-100 MAINTENANCE MANUAL 32-32-00-5. OK FOR SE RVICE. 2 L 7 3 4F RT A3WE 2002102500044 20021025 00044 NM 2002 10 25 02FDEA00667 1 20020917 A 5311 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 FUSELAGE TRANSVERSE FRAME AT STA Y-1701 RT SIDE DENTED & CRACKED APPROX 2 INCHES LONG. R&R FRAME PER SRM 53-30-00 VOL I. 2 L 7 3 4F RT A22WE 2002102500045 20021025 00045 NM 2002 10 25 F3LA200200339 1 20021008 A 5320 CLIP BOEING 737 7372L9 1384497 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C-2 CHECK, INSPECTION REPORTED SHEARED RIVETS ON SUB THRESHOLD "T" CLIP, BS 440, RBL 16. REPLACED "T" CLIP PER S RM 51-30-02. 2 L 7 2 4F RT A16WE 2002102500046 20021025 00046 NM 2002 10 25 F3LA200200351 1 20021004 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 DURING C 4 CHECK, CORROSION WAS FOUND ON THE FLOOR SUPPORT CHANNEL AT BS 897 AROUND THE NUT PLATE HOLE. REMOVED AND REP LACED SECTION OF FLOOR SUPPORT CHANNEL FROM BS 887 TO BS 947, RBL 3, IAW SRM 53-00-53 2 L 7 2 4F RT A16WE 2002102500047 20021025 00047 NM 2002 10 25 F3LA200200352 1 20021016 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 DURING C 4 CHECK, CORROSION WAS FOUND AROUND NUT PLATES ON INTERCOSTAL BETWEEN BS 847 AND BS 867, STRINGERS 25R AND 24R. REPAIR WAS PERFORMED IN ACCORDANCE WITH BOEING DRAWING NUMBER 65-47 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002102500048 20021025 00048 NM 2002 10 25 F3LA200200353 1 20021021 A 5230 STRUCTURE BOEING 737 7372L9 1384497 NM CARGO DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 3075 22734 DURING C 2 CHECK, THE FORWARD CARGO DOOR, LOWER CORNER, WAS FOUND TO HAVE A CRACK. THE CRACK WAS REPAIRED USING SB 737- 52A1100 AND COMPLIED WITH THE REQUIREMENTS OF AD 2000-07-06 UNDER ENGINEERING REQUEST 02-1333 2 L 7 2 4F RT A16WE 2002102500049 20021025 00049 NM 2002 10 25 F3LA200200354 1 20021018 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 DURING C 4 CHECK, CORROSION WAS FOUND ON THE INTERIOR FUSELAGE SKIN AT BS 500 AND STR 26L. FUSELAGE SKIN WAS ROUTED OUT AND REPAIRED IN ACCORDANCE WITH ENGINEERING AUTHORIZATION EA 53-737-185, SRM 53-00-01 AND SRM 53-30-03. 2 L 7 2 4F RT A16WE 2002102500050 20021025 00050 NM 2002 10 25 F3LA200200355 1 20021004 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 DURING C 4 CHECK, USING INSPECTION CRITERIA IN SRM 53-60-53, CORROSION WAS FOUND AROUND THE NUT PLATE ON THE FLOOR SUPPO RT CHANNEL AT RBL 3 AT BS 887. REMOVED AND REPLACED A SECTION OF THE FLOOR SUPPORT CHANNEL, FROM BS 887 TO BS 947 AT RB L 3, IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2002102500051 20021025 00051 NM 2002 10 25 F3LA200200356 1 20021008 A 5320 PANEL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 DURING C 4 CHECK, AFT CARGO COMPARTMENT TRANSITION PANEL WAS FOUND TO HAVE CORROSION. INSPECTION OF THE TRANSITION PANE L, IAW THE REQUIREMENTS OF SRM 53-60-53, REQUIRED FABRICATION OF REPAIR PARTS IAW SRM 53-60-53. 2 L 7 2 4F RT A16WE 2002102500052 20021025 00052 NM 2002 10 25 F3LA200200357 1 20021022 A 5347 CARGO TRACK BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 51512 22734 DURING A C 2 CHECK, CORROSION WAS FOUND IN THE CARGO TIE DOWN TRACK AT LBL 17, WL 157, BS 813. TIE DOWN TRACK WAS REPLA CED IAW SRM 53-10-05 AND SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002102500053 20021025 00053 NM 2002 10 25 F3LA200200359 1 20021021 A 5320 SILL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 DURING C 4 CHECK, CORROSION WAS FOUND ON THE R1 DOOR MOP SILL. INSPECTION, IAW SRM 53-10-15 FOUND THE SILL OUT OF TOLER ANCE. NEW SILL WAS INSTALLED IAW SRM 53-10-15 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002102500054 20021025 00054 NM 2002 10 25 F3LA200200360 1 20021008 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 55067 23257 DURING C 4 CHECK, CORROSION WAS FOUND ON THE INTERCOSTAL LOCATED AT BS 867 TO BS 887. INSPECTION REVEALED THE INTERCOST AL WAS OUT OF LIMITS IAW THE REQUIREMENTS OF SRM 53-60-04. REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW THE REQUIR EMENTS OF SRM 53-60-04. 2 L 7 2 4F RT A16WE 2002102500055 20021025 00055 NM 2002 10 25 F3LA200200361 1 20021008 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 55067 23257 DURING C 4 CHECK, THE UPPER FLANGE OF FLOOR INTERCOSTAL WAS FOUND CRACKED AT BS 344 TO BS 360. REMOVED INTERCOSTAL. FA BRICATED UPPER FLANGE OF THE INTERCOSTAL IAW SRM 53-10-51 AND INSTALLED ON INTERCOSTAL IAW SRM 53-30-01. INTERCOSTAL IN STALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002102500056 20021025 00056 NM 2002 10 25 F3LA20020053 1 20021018 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 DURING C 4 CHECK, CORROSION WAS FOUND ON INTERIOR SURFACE OF FUSELAGE SKIN AT BS 500, STR 26L. CORRODED AREA WAS ROUTED OUT AND REPAIRED IAW EA 53-737-185, SRM 53-00-01 AND SRM 53-30-3. 2 L 7 2 4F RT A16WE 2002102500057 20021025 00057 EU 2002 10 25 DHL2002363525 1 20020806 A 5230 WEB AIRBUS 300 A300B4203 3930306 EU CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 C-CHECK/FWD LOWER CARGO DOOR LWR SECTION OF ATTACHMENT FITTING OF DOOR ACTUATOR LONGITUDINAL WEB CRACKED FWD AND AFT OF FITTING. REMOVED DAMAGED PART. INSTALLED REPAIR PART IAW A300 SRM 51-30-30 AN 52-31-11. REMOVED AFT WEB SUPPORT IAW A30 0 SRM 51-30-30. FABBED NEW WEB IAW A300 SRM 52-31-11 AN 51-26-00. INSTALLED NEW AFT WEB SUPPORT IAW A300 SRM 51-30-30. 2 L 7 2 4F RT A35EU 2002102500058 20021025 00058 EU 2002 10 25 DHL2002366013 1 20021003 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 1 ENGINE MALFUNCTIONED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 366DH 249 ENGINE NR 1 LOOP 'A' FAILS TO TEST. ENGINE NR 1 LOOP 'A' TESTS NORMALLY AS PER MM 26-12-00. 2 L 7 2 4F RT A35EU 2002102500059 20021025 00059 EU 2002 10 25 DHL2002366014 1 20021017 A 5230 SHEAR PIN AIRBUS 300 A300B4203 3930306 EU CARGO DOOR DAMAGED A DHLA K NONE J WARNING INDICATION CL CLIMB 1 SO 01 366DH 249 MAIN CARGO NOT LOCKED AND CARGO SW FAULT LIGHTS ILLUMINATED ON DOORS PANEL AFTER TAKEOFF. DOOR ANNUNCIATOR ON MWP ALSO WAS ILLUMINATED, EMERGENCY CHECKLIST COMPLETED. REPLACED LATCH HANDLE SHEAR PIN IAW M/M 52-36-11. OPS CHECKED GOOD. 2 L 7 2 4F RT A35EU 2002102500060 20021025 00060 NM 2002 10 25 DHL2002715010 1 20021022 A 3150 WARNING SYSTEM BOEING 727 727155C 138404Z NM COCKPIT MALFUNCTIONED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 715DH 19618 RTO AT CVG MAXIMUM ATTAINED AIRSPEED 5 KIAS. UPON INITIATION OF TO THRUST, THE TO WARNING HORN SOUNDED. AFTER TAXIING C LEAR OF THE RUNWAY, NOTIFIED FLIGHT CONTROL AND ADVISED THEM OF THE PROBLEM. MX CONTROL HAD BEEN NOTIFIED PRIOR TO CALL ING FC. AFTER WE MOVED THE SPEED BRAKE HANDLE IN & OUT OF DETENT SEVERAL TIMES THE PROBLEM APPEARED TO BE SOLVED. THE REMAINDER OF THE FLIGHT WAS UNEVENTFUL. 2 L 7 3 4F A3WE 2002102500061 20021025 00061 NM 2002 10 25 DHL2002720500 1 20021005 A 5330 SKIN BOEING 727 727228 1384083 NM FUSELAGE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING "C" CHECK, FOUND GOUGE IN FUSELAGE SKIN AT BS 630, BELOW STR 24R. CUTOUT DAMAGED AREA. FABRICATED DOUBLER IAW B 727 SRM 53-30-3 FIG 1. INSTALLED REPAIR IAW B727 SRM 53-30-3 FIG 1. 2 L 7 3 4F RT A3WE 2002102800139 20021028 00139 WP 2002 10 28 MWEA020631 1 20021025 A 5753 5935066 SPAR DOUG DC9 DC981 3022081 WP T/E FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 RIGHT FORWARD LOWER FLAP SPAR HAS AREA OF EXFOLIATION CORROSION LOCATED JUST OUTBOARD OF XFLS 47. REMOVED CORROSION, FA BRICATED, FIT AND DRILLED UP REPAIR ANGLE AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2002110100142 20021101 00142 WP 2002 11 1 MWEA020633 1 20021025 A 1430 995777514 NUT PLATE DOUG DC9 DC981 3022081 WP FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 RIGHT FLAP LEADING EDGE ATTACH NUT PLATE IS BROKEN AT XFLS 265. FORMED RIB ANGLE, DRILLED UP RIB ANGLE AND DRILLED 2 HO LES THROUGH LEADING EDGE. INSTALLED NUT PLATES AND NOSE RIB GEAR. 2 L 7 2 4F A6WE 2002102800140 20021028 00140 WP 2002 10 28 MWEA020634 1 20021025 A 5753 99359334 CHANNEL DOUG DC9 DC981 3022081 WP T/E FLAP DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 RIGHT HAND FLAP STATION XIFO 53.0447 LOWER CHANNEL THAT ATTACHES TO RIB NEEDS TO BE FABRICATED. REMOVED LOWER CHANNEL, FABRICATED AND DRILLED UP AND INSTALLED NEW CHANNEL. 2 L 7 2 4F A6WE 2002102800143 20021028 00143 WP 2002 10 28 MWEA020636 1 20021025 A 5753 9935334 CHANNEL DOUG DC9 DC981 3022081 WP T/E FLAP DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 RIGHT HAND FLAP STATION XIFO 58.6344 LOWER CHANNEL THAT ATTACHES TO RIB NEEDS TO BE FABRICATED. REMOVED LOWER CHANNEL, FABRICATED, DRILLED UP AND INSTALLED NEW CHANNEL. 2 L 7 2 4F A6WE 2002102800144 20021028 00144 WP 2002 10 28 MWEA020637 1 20021025 A 5753 593590626 STIFFENER DOUG DC9 DC981 3022081 WP T/E FLAP DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 RIGHT HAND FLAP STATION XIFO 58.6344 FORWARD STIFFENER THAT ATTACHES TO FORWARD TEE CAP NEEDS TO BE FABRICATED. REMOVED STIFFENER, FABRICATED, DRILLED UP AND INSTALLED NEW STIFFENER. 2 L 7 2 4F A6WE 2002102800145 20021028 00145 WP 2002 10 28 MWEA020638 1 20021025 A 5753 993593210 STIFFENER DOUG DC9 DC981 3022081 WP T/E FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 RIGHT INBOARD FLAP HAS CORROSION ON INTERNAL STIFFENER AT STATION XCW 121. REMOVED CORRODED STIFFENER, DRILLED UP AND I NSTALLED NEW STIFFENER. 2 L 7 2 4F A6WE 2002102800147 20021028 00147 WP 2002 10 28 MWEA020640 1 20021025 A 5230 59101419 PAN DOUG DC9 DC981 3022081 WP CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 MID PIT DOOR INNER PAN HAS LIGHT CORROSION CHAFING BETWEEN THE NR 2 AND NR 3 STOP PADS ON THE FORWARD SIDE. REMOVED COR ROSION AND BLENDED CHAFED AREA, FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2002102800146 20021028 00146 WP 2002 10 28 MWEA020639 1 20021025 A 5280 5930584 DOUBLER DOUG DC9 DC981 3022081 WP LT MLG DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 CHAFED ON REPAIR DOUBLER AROUND LEFT GEAR DOOR SENSOR. REMOVED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 2002102800141 20021028 00141 WP 2002 10 28 MWEA020635 1 20021025 A 5753 593590624 STIFFENER DOUG DC9 DC981 3022081 WP T/E FLAP DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 RIGHT HAND FLAP STATION XIFO 53.0447 FORWARD STIFFENER THAT ATTACHES TO FORWARD TEE CAP NEEDS TO BE FABRICATED. REMOVED STIFFENER, FABRICATED, FIT AND DRILLED UP NEW STIFFENER. INSTALLED AFT VERTICAL FASTENERS, STIFFENER AND NOSE RIB. 2 L 7 2 4F A6WE 2002102500062 20021025 00062 WP 2002 10 25 UPS02839444 1 20020827 A 5230 PAN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 A-PIT DOOR FWD LOWER STOP ON DOOR AND DOOR PAN UNDER FITTING ARE CRACKED AT STA 320 AT LONG 32R. REM OVED AND REPLACED STOP FITTING, REMOVED, FABRICATED AND REPLACED LOWER PAN SECTION IAW SRM 52-4-2 AND 52-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002102500063 20021025 00063 WP 2002 10 25 UPS02839446 1 20020824 A 5240 BEAM DOUG DC8 DC871F 302199D WP SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 LEFT CENTER SERVICE DOOR BEAM SEGMENT ON DOOR IS CRACKED AT APPROX STA 1295 AT LONG 16L, 3RD LIGHTENI NG HOLE FROM TOP. CUT INTERCOSTAL/BEAM, FABRICATED AND INSTALLED BEAM SECTION IAW SRM 52-2-0 FIG 2, 52-40-01. 2 L 7 4 4F RT 4A25 2002102500064 20021025 00064 WP 2002 10 25 UPS02839447 1 20020827 A 5720 37048412 FITTING DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 S-51 STRINGER END FITTING CRACKED AFT SIDE AT XRS74.000 NR 3 ALT. REMOVED AND REPLACED FITTING IAW D C8 SRM 51-1-20D AND 51-1-23. 2 L 7 4 4F RT 4A25 2002102500065 20021025 00065 WP 2002 10 25 UPS02839448 1 20020831 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 FLOORBEAM STA 50 IS CRACKED ON UPPER FLANGE AT LT O/B END. REPAIRED IAW DC8 SRM 53-2-0 & TR 53-124. 2 L 7 4 4F RT 4A25 2002102500066 20021025 00066 WP 2002 10 25 UPS02839451 1 20020827 A 5720 FITTING DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 S-51 STRINGER END FITTING CRACKED FWD SIDE AT XRS 74.000 2 MAIN. REMOVED AND REPLACED END FITTING I AW DC8 SRM 51-1-20D AND 51-1-23. 2 L 7 4 4F RT 4A25 2002102500067 20021025 00067 WP 2002 10 25 UPS02839452 1 20020822 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 AFT PIT FRAME CORRODED AND CRACKED AT SCREW HOLE STA 1400 STRINGER 36. TRIMMED OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER IAW SRM STD-5310-002. INSTALLED REPAIR DOUBLER IAW SRM STD-5310-002. 2 L 7 4 4F RT 4A25 2002102500068 20021025 00068 NM 2002 10 25 F3LA200200364 1 20020929 A 5310 BAC1498141 STRINGER BOEING 737 7372L9 1384497 NM STA 520, STR 26L CORRODED A F3LA O OTHER O OTHER IN INSP/MAINT 1 NM 03 271FL 51512 2050 22734 DURING C 2 CHECK, CORROSION WAS FOUND ON THE STRINGER AT STA 520, STR 26L.THE STRINGER WAS REPAIRED BY REMOVING THE DAMA GED SECTION BETWEEN STA 510 AND 540 AT STR 26L. NEW PARTS WERE FABRICATED AND INSTALLED IN ACCORDANCE WITH THE REQUIREM ENTS OF SRM 53-10-3, SRM 53-10-2 AND SRM 53-10-1 2 L 7 2 4F RT A16WE 2002102500069 20021025 00069 WP 2002 10 25 UPS02839453 1 20020910 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 MAIN CABIN FS 1726-1746 INTERCOSTAL ABOVE L26L IS CRACKED. INSTALLED NEW INTERCOSTAL CLIPS IAW DC8 S RM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102500070 20021025 00070 WP 2002 10 25 UPS02839458 1 20020823 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 L1 DOOR LWR FWD DOOR JAMB CORNER HAS A CRACKED CUSP LONGERON FOUND BY RADIOGRAPHY. REMOVED AND REPLA CED CRACKED INTERCOSTAL IAW DAC DWG 5797646. 2 L 7 4 4F RT 4A25 2002102500071 20021025 00071 WP 2002 10 25 UPS02839459 1 20020826 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 LONGERON 17R AT STA 1770 HAS CRACKED FITTING. REMOVED OLD FITTING, LOCATED, DRILLED, DEBURRED AND IN STALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102500072 20021025 00072 NE 2002 10 25 000203 2 20020930 A 7261 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT MAKING METAL A CHQA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 GL 11 108 LT ENGINE OIL CHIP LIGHT ON 2 L 7 2 4T 4 T RT A52EU E8NE6 2002102500073 20021025 00073 WP 2002 10 25 UPS02839460 1 20020827 A 5313 564932744 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 AFT FUSELAGE ACCESS THROUGH DOOR 60 AT FS 1766-1790 LONGERON 17R IS CRACKED. REMOVED LONG & ASSOCIAT ED PARTS IAW DC8 SRM 51-1-20D & 51-1-21. INSTALLED NEW LONG AND ASSOCIATED PARTS IAW DC8 SRM 51-1-20D & 51-1-21. 2 L 7 4 4F RT 4A25 2002102500074 20021025 00074 WP 2002 10 25 UPS02839465 1 20020827 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 AFT FUSELAGE ACCESS THROUGH DOOR 60 AT FS 1766-1790 LONGERON 17L IS CRACKED. REMOVED AND REPLACED LO NG 17L FS 1766-1790 IAW DC8 SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 2002102500075 20021025 00075 WP 2002 10 25 UPS02839473 1 20020829 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 STA 1755 LONG 15L CRACKED AT I/B FLANGES. REMOVED DAMAGED SECTION OF LONGERON PER DC8 SRM 53-2-2 FIG 11. FABRICATED REPAIR PER DC8 SRM 53-2-2 FIG 11. INSTALLED PER DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002102500076 20021025 00076 WP 2002 10 25 UPS02839476 1 20020823 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 L2 LWR FWD DOOR JAMB CORNER CRACKED APPROX 1.5 INCHES LONG ABOVE TRIMOUT FOUND BY RADIOGRAPHY. REPAI RED AREA IAW DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2002102500077 20021025 00077 WP 2002 10 25 UPS02839477 1 20020820 A 5313 37735121 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 R2 DOOR UPPER AFT JAMB LONGERON 11 CRACKED. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102500078 20021025 00078 WP 2002 10 25 UPS02839482 1 20020823 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 R2 UPPER AFT DOOR JAMB CORNER HAS CRACKED INTERNAL DOUBLER APPROX 3 INCHES LONG FOUND BY RADIOGRAPHY. REPAIRED AREA IAW DC8 SRM 53-2-0 T/R 53-133. 2 L 7 4 4F RT 4A25 2002102500079 20021025 00079 WP 2002 10 25 UPS02839483 1 20020823 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 L1 UPPER FWD DOOR CORNER HAS 4 EACH CRACKS ON EXTERNAL SKIN. FABRICATED DOUBLERS AND FILLER. INSTAL LED REPAIR DOUBLERS, FILLERS, DOOR PAN, PAN SPLICES, DOOR SOPS, TORQUE BOX WEBS, SEAL DEPRESSOR AND CALIFORNIA PNL IAW D C8 SRM 51-1-21, 51-1-21A, 51-1-20D, AND 51-3-0. 2 L 7 4 4F RT 4A25 2002102500080 20021025 00080 WP 2002 10 25 UPS02839484 1 20020826 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 L17L AT STA 1770, FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2002102500081 20021025 00081 WP 2002 10 25 UPS02839486 1 20020910 A 5720 STRINGER CLIP DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 RIGHT WING STA XRS 289 LOWER STRINGER CLIP IS CRACKED AT STRINGER 61. REMOVED, FABRICATED, AND INSTA LLED CLIP IAW DWG 4614391, SAA SK 708-435, UPS ENGINEERING FILE NUMBER DC8-57-20058, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102500082 20021025 00082 WP 2002 10 25 UPS02839487 1 20020821 A 5320 3779658U502 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 850 LONG 10R FWD SIDE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779658, AND UPS ENGINEERING FILE NUMBER DC8-53-20246, SAA SK 708-514, SRM 51-1-20D, 51-3-0, 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2002102500083 20021025 00083 WP 2002 10 25 UPS02839488 1 20020825 A 5311 561386161 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 FRAME AT STA -12 IN LT NOSE TUNNEL IS GOUGED AND CRACKED AT LBL 24 AFT SIDE. REMOVED FRAME, FABRICAT ED AND INSTALLED FRAME IAW DWG 5613861, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102500084 20021025 00084 WP 2002 10 25 UPS02839500 1 20020821 A 5320 2649940 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C1 MAIN CABIN STA 147 LONG 21R ANGLE HAS SHORT FASTENER IN DOUBLER DRILLED HOLE. REMOVED ANGLE, CORROSI ON FOUND, BLENDED, OUT OF LIMITS IAW DC8 SRM 5 1-1-8, 51-1-20D AND SRM 53-2-0. FABBED ANGLE IAW DC8 SRM 51-1-24, AND DA C DWG 2649940. INSTALLED ANGLE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102500085 20021025 00085 WP 2002 10 25 UPS02839513 1 20020908 A 5320 3755841501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 1180 FWD SIDE BATHTUB FITTING IS CRACKED BETWEEN LONG 33R TO 34R. REMOVED AND REPLACED FITTING I AW DWG 3755841, AND SRM 53-2-0 FIG 2G. 2 L 7 4 4F RT 4A25 2002102500086 20021025 00086 WP 2002 10 25 UPS02839514 1 20020825 A 5311 97537518 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 STA 683 FWD SIDE LOWER BULKHEAD FRAME IS CRACKED BETWEEN LONG 28R TO 29R. REMOVED, FABRICATED AND RE PLACED FRAME SECTION IAW DWG 9753751, AND SRM 51-1-20D, 53-2-5, 51-3-0. 2 L 7 4 4F RT 4A25 2002102500087 20021025 00087 WP 2002 10 25 UPS02839515 1 20020828 A 5730 DOUBLER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C1 LEFT WING CENTER L/E INTERNAL CIRCUMFERENCE DOUBLER IS CRACKED ON LOWER SECTION AT XFS 348. CUTOUT C RACKED SECTION OF INTERNAL DOUBLER, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER SECTION AND SPLIC E IAW UPS ENGINEERING FILE NUMBER DC8-57-20055 AND SAA SK 708-162. 2 L 7 4 4F RT 4A25 2002102500088 20021025 00088 2002 10 25 000204 4 20021001 A 3410 INDICATOR EMB 145 EMB145 3260210 SO COCKPIT FAILED A CHQA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 GL 11 372 FO AIRSPEED AND ALTIMETER FAIL, E1 AND E2 SHORT DISPATCH. COMM 1 AND COMM 2 FAIL R/R ADC. 2 L 7 2 4F RT T00011AT 2002102500089 20021025 00089 EA 2002 10 25 COMA0260604 1 20021024 A 4990 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING K S FLUID LOSS AFFECT SYSTEMS CR CRUISE 1 SO 01 918CA 7018 FLIGHT 5796 APU LOW OIL PRESSURE CAUTION MESSAGE.SERVICED APU OIL - G OPERATONAL CHECKS NORMAL. 2 L 7 2 4F RT A21EA 2002102500090 20021025 00090 EA 2002 10 25 COMA0260605 1 20021022 A 2840 73664310 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 01 798CA 13599 7348 FLGIHT 5905 FUEL READINGS ARE ERRATIC.REPLACED THE FUEL COMPUTER. 2 L 7 2 4F RT A21EA 2002102500091 20021025 00091 EA 2002 10 25 COMA0260606 1 20021017 A 3220 16050101 STRUT CNDAIR CL600 CL6002B19 1900309 EA NOSE WORN A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 914CA 20971 7012 FLIGHT 5457 AFTER TAKE OFF FROM CVG RECEIVED A NOSE GEAR DOOR CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.REPLACED T HE NLG STRUT ASSEMBLY. 2 L 7 2 4F RT A21EA 2002102500092 20021025 00092 WP 2002 10 25 UPS02839533 1 20020917 A 5320 4645516501N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SP STA 944 FITTING IS CRACKED CENTER LINE BETWEEN MAIN GEAR DOORS. REMOVED AND REPLACED FITTING IAW DWG 4645516, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102500093 20021025 00093 WP 2002 10 25 UPS02839534 1 20020917 A 5320 5616306171 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SP STA 910 FITTING IS CRACKED CENTER LINE BETWEEN MAIN GEAR DOORS. REMOVED AND REPLACED FITTING IAW DWG 5616306 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102500095 20021025 00095 SO 2002 10 25 C2XA02IA226 1 20021024 A 3610 M1195175242 SENSOR EMB 145 EMB145ER 3260211 SO WING ROOT LEAKING A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14939 145030 IAH- FLIGHT 3498, THE CREW NOTED THAT #2 BLEED LEAK INFLIGHT,(FOLLOWED QRH, MX CONTROL ADVISED RETURN TO IAH), THE CREW RETURNED THE AIRCRAFT TO IAH, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE SECURED RIGHT WING ANTI ICE VALVE SENSOR LINE,PERFORMED A LEAK CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002102600001 20021026 00001 WP 2002 10 26 DHL2002803522 1 20020926 A 2550 3750257503 FITTING DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AFT CARGO COMPT.SPLICE FITTING WITH 3" CRACK IN IT AT STA 1040.000-1060.000.PREFORMED MAJOR REPAIR PER SRM 53-1-0 PG1.RE MOVED DAMAGED FITTING PER SRM51-1-20D PG 21.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51- 1-20D PG 9 AND 51-1-14 PG 1. 2 L 7 4 4F RT 4A25 2002102700001 20021027 00001 NE 2002 10 27 RAIA00210287 2 20021020 A 7200 PW124 ENGINE AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE SMOKE A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 03 721TE 8035 217 124169 5598-STL- TOWER REPORTED THAT AFTER LIFT-OFF RIGHT ENGINE WAS SMOKING. CREW REPORTED NO ABNORMAL ENGINE INSTRUMENT INDIC ATIONS. MAINTENANCE TROUBLE SHOOT TO INTERNAL ENGINE PROBLEM AND REMOVED AND REPLACED THE ENGINE IAW AMM, LEAK AND OPS C K OK. 2 H 7 2 4T 4 T RT A53EU E2ONE 2002102700002 20021027 00002 2002 10 27 RAIA00210288 4 20021020 A 3417 7000700967 ADC JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 565HK 16458 1541 41082 482-STL- BOTH VSI's DISPLAYED OFF FLAGS. MAINTENANCE REMOVED AND REPLACED THE AIR DATA COMPUTER, OPS CK OK. 2 L 7 2 4T RT A41NM 2002102700003 20021027 00003 EU 2002 10 27 RAIA00210290 1 20021020 A 2430 M300R64 RELAY JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 560HK 41076 5594-STL- RIGHT GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED 1PB16, #2 GENERATOR OPS CK OK. 2 L 7 2 4T RT A41NM 2002102700004 20021027 00004 EU 2002 10 27 RAIA00210293 1 20021023 A 3060 ANN50 FUSE JETAIR JETSTM JETSTM4101 1500501 EU BLOWN A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 568HK 41086 5523-GRR- LEFT PROP HEAT INOP. MAINTENANCE REMOVED AND REPLACED PROP FUSE ON POWER DISTRIBUTION UNIT, PROP HEAT OPS CK O K. 2 L 7 2 4T RT A41NM 2002102800001 20021028 00001 SO 2002 10 28 000209 1 20021015 A 3040 TERMINAL BLOCK EMB 145 EMB145 3260210 SO COCKPIT BURNED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 280 SMOKE IN THE COCKPIT. FOUND FOR W/S HEAT TERMINAL BLOCK MELTED-FERRIED TO IND FOR W/S CHANGE 2 L 7 2 4F RT T00011AT 2002102800002 20021028 00002 SO 2002 10 28 000210 1 20021016 A 3244 TIRE EMB 145 EMB145 3260210 SO NLG FAILED A CHQA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 11 273 PILOT REPORTS RT NOSE TIRE BLEW ON TAKEOFF ROLL. 2 L 7 2 4F RT T00011AT 2002102800003 20021028 00003 SO 2002 10 28 000213 1 20021023 A 2150 ACM EMB 145 EMB145 3260210 SO NR 1 MALFUNCTIONED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 381 PACK 1 OVERLOAD. MEL'D PACK 1 2 L 7 2 4F RT T00011AT 2002102800012 20021028 00012 NE 2002 10 28 BJNA021001 2 20021009 A 7230 CASE BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE LT ENGINE DAMAGED A BJNA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 11 344TM 23044 709415 ON TAKEOFF ROLL AT 115 KNOTS AIRCRAFT VEERED TO THE LT, CAPTAIN REPORTED HEARING A LOUD BANG. ABORTED TAKEOFF. MAINTEN ANCE REPORTED MAJOR DAMAGE TO TURBINE SECTION OF ENGINE. UPON FURTHER INSPECTION REVEALED THAT ALL DAMAGE WAS TOTALLY C ONTAINED TO THE ENGINE CASE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002102800013 20021028 00013 NM 2002 10 28 F3LA200200377 1 20021023 A 2133 7110033 OUTFLOW VALVE BOEING 737 73736E 138443A NM BROKEN A F3LA A UNSCHED LANDING O OTHER TO TAKEOFF 1 NM 03 315FL 25159 ON TAKE OFF, THE FLIGHT CREW FOUND THE CABIN PRESSURIZATION COULD NOT BE MAINTAINED. MAINTENANCE FOUND THE CHECK VALVE SEAL ON THE OUTFLOW VALVE HAD SEPARATED FROM THE VALVE ASSEMBLY DUE TO A BROKEN RIVET AND SLIPPED FLAPPER.MAINTENANCE RE MOVED AND REPLACED THE OUTFLOW VALVE IN ACCORDANCE WITH THE REQUIREMENTS OF BOEING MAINTENANCE MANUAL 21-31-00, PAGE 201 . 2 L 7 2 4F RT A16WE 2002102800014 20021028 00014 CE 2002 10 28 DXT2002F00004 1 20021008 A 3230 991446110 MANIFOLD CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL L/G CONTROL INOPERATIVE E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 931QS 4155 7500064 AFTER 1.5 HOURS AT FL430, WHILE DESCENDING THROUGH FL180 AT 240 KNOTS, THE CREW HEARD A LOUD RUSHING NOISE FROM FRONT O F THE AIRCRAFT AND THE NOSE GEAR LIGHT CAME ON FOR 2 SECONDS. THE LIGHT THEN WENT OUT, THE NOISE STOPPED AND THE GEAR L OWERED NORMALLY IN THE TRAFFIC PATTERN. MAINTENANCE CHECKED AND ADJUSTED THE NOSE GEAR UPLOCK SWITCH AND PERFORMED A SA TISFACTORY OPERATIONAL CHECK. THE AIRCRAFT THEN PERFORMED A SATISFACTORY OPERATIONAL CHECK FLIGHT WITH A DATA MONITORIN G UNIT INSTALLED IAW MM. MFG FACILITY REPLACED THE LANDING GEAR CONTROL MANIFOLD AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2002102800015 20021028 00015 CE 2002 10 28 JJB2002F00002 1 20020920 A 5540 AM17517A BOLT BEECH 1900 1900D 1154162 CE RUDDER BENT A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 855CA 3864 UE392 DURING INSPECTION OF RUDDER CONTROL SYSTEM, FOUND TORQUE TUBE MOUNT BOLTS LOOSE AND CONTROL HORN MOUNT BOLT BENT. PARTS RETURNED TO MFG FOR ANALYSIS. 2 L 7 2 4T RT A24CE 2002102800016 20021028 00016 NE 2002 10 28 MDR02011 1 20020930 A 6410 TIP CAP SKRSKY S64 S64E 8142604 NE TAIL ROTOR BLADE BROKEN B JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 173AC 19611 64015 TRAILING EDGE TIP WEIGHTS (UP TO 5 EA) AND ATTACHMENT BOLT (1 EA) DEPARTED FROM TIP RIB ASSEMBLY AND WENT THROUGH TIP CA P. DURING THE POCKET REPLACEMENT PROCESS AT SUPPLIER, A TIP RIB WAS INSTALLED IN THE NEW POCKET ASSEMBLY THAT WAS MISSI NG AN INBOARD DOUBLER , TO WHICH THE TRAILING EDGE NUT PLATE AND WEIGHT PACKAGE IS ATTACHED. WITHOUT THE REINFORCEMENT OF THIS INBOARD DOUBLER, IT APPEARS THAT THE STRESS APPLIED DURING FLIGHT CAUSED THE NUT PLATE TO PULL OUT OF THE TIP RI B AND THE WEIGHTS AND ATTACHMENT BOLT TO EXIT THROUGH THE TIP CAP. 2 G 7 2 4U H4EA 2002102800017 20021028 00017 EU 2002 10 28 UHL2002F00004 1 20020927 A 2613 M243084259 CONNECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT79B 30030 NE RT NACELLE WORN A UHLA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 NE 03 405Z 340A040 367488 TAIL PIPE, HOT LIGHT ILLUMINATED AT 6300 FEET. SHUT DOWN NR 2 ENGINE, DISCHARGED NR1 AND NR2 FIRE BOTTLE, RETURNED TO A IRPORT, LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED WIRING AT EXHAUST COWLING CONNECTORS. NO EVIDENCE OF FIRE NOTED. 2 L 7 2 4T 4 T RT A52EU E8NE 2002102800018 20021028 00018 2002 10 28 UIEA200200051 4 20021009 A 3450 751780010002 TRANSPONDER BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE NR 1 MODE FAILED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 517MC 23300 DURING INITIAL CLIMB, TRANSPONDER FAIL LIGHT ILLUMINATED WITH NR 1 SET SELECTED. SELECTED NR 2 TO NO AVAIL. CIRCUIT BR EAKER CHECKED OK. DIVERTED. C/A: REPLACED MODE S TRANSPONDER IAW MM. TEST CARRIED OUT. OPS CHECK SATISFACTORY. ALS O ATC TRANSPONDER NR 2 TRANSFERRED TO DMI. 2 L 7 4 4F 4 F A20WE E23EA 2002102800019 20021028 00019 NE 2002 10 28 UIEA200200052 2 20021010 A 7320 8062899 MEC BOEING 747 7472F6B 1384807 NM GE CF6 CF650E2 30018 NE NR 4 ENGINE INOPERATIVE A UIEA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 15 535MC 21833 517658 WHILE CLIMBING THROUGH 13,500 FEET AND ACCELERATING THROUGH 310 KTS, NR 4 ENGINE ROLLED BACK TO IDLE ACCOMPANIED BY A NO TICEABLE YAW. INSTRUMENTS CONFIRMED NR4 ENGINE HAD INDEED ROLLED BACK. AUTO THROTTLES WERE ENGAGED AT TIME. USING CLI MB POWER BUT NO THROTTLE INDUCEMENT OCCURRED ON ANY THROTTLE. SHORTLY AFTER ROLL BACK, ENGINE RESUMED ITS CLIMB POWER R EVOLUTIONS. ALL OTHER INDICATIONS WERE NORMAL. C/A: PERFORMED VISUAL INSPECTION AT LINKAGE, FOUND OK. CHECKED SPECIF IC GRAVITY READING 0.76. REPLACED MEC IAW MM. STATIC RIG CHECK ACCOMPLISHED. WET MOTORING PERFORMED OK. ACCOMPLISHED TEST NR 4 MAX POWER ASSURANCE TESTED, TEST SATISFACTORY. VSV TRACKING CHECK ON NR 4 ENGINE TO BE DONE, LATER CHECK. 2 L 7 4 4F 4 F A20WE E23EA 2002102800020 20021028 00020 SO 2002 10 28 ZLW2002F00000 1 20021011 A 3040 29651C CONTROLLER GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY5118 54523 EU WINDSHIELD HEAT FAILED E ZLWA K NONE O OTHER IN INSP/MAINT 1 SW 15 36MW 197 89 WINDSHIELD HEAT CONTROLLER, INTERNAL FAILIURE. 2 L 7 2 4F 4 F RT A12EA E2EU 2002102800021 20021028 00021 EU 2002 10 28 00045 1 20020926 A 7930 ENGINE AMD FALC20 FALCON 2720302 EU RIGHT MALFUNCTIONED E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 221TW 221 AIRCRAFT DEPARTED ELP, RT ENGINE OIL PRESSURE WENT TO ZERO DURING CLIMB, RETURN TO DEPARTURE AIRPORT, WILL UP DATE REPOR T AFTER MAINTENANCE. 2 L 7 2 4F A7EU 2002102800022 20021028 00022 NM 2002 10 28 0202962202 1 20020918 A 2410 072420900 CSD BOEING 727 727251 138408H NM NR 3 ENGINE MALFUNCTIONED A NWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 01 202US 48364 1762 22155 TAKEOFF WAS ABORTED AT 130 KNOTS AFTER THE NR 3 GENERATOR TRIPPED. RESET THE NR 3 GENERATOR AND IT TRIPPED AGAIN. RETU RNED TO THE GATE. REPLACED THE NR 3 CSD. RAN ENGINE. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 2002102800023 20021028 00023 EU 2002 10 28 00046 1 20020927 A 5230 MS272401 SWITCH AMD FALCON FALCON20 2730103 EU CARGO DOOR MALFUNCTIONED E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 314TW 314 AIRCRAFT CLIMBING FROM 310 TO 330 DOOR LIGHT CAME ON, PILOT REQUESTED DESENT, REDUCED CABIN PRESSURE LIGHT WENT OUT , DE CIDED TO DEVERT TO KLNK, MAINTENANCE REPLACED DOOR LIGHT SWITCH , OPS CK NORMAL , RETURN AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A7EU 2002102800024 20021028 00024 NE 2002 10 28 00049 2 20021001 A 7200 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE NR 1 FAILED E HAEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 232TW 32 304152B DURING CRUISE AT FL 310, NR 1 ENGINE INDICATED HIGH OIL PRESSURE. CREW SHUTDOWN NR 1 ENGINE, DECLARED AN EMERGENCY AND D IVERTED/LANDED WITHOUT INCIDENT. PRECAUTIONARY REMOVAL OF ENGINE. 2 L 7 2 4F 4 F A7EU E7EA 2002102800025 20021028 00025 CE 2002 10 28 00051 1 20021011 A 3250 CONTROLLER LEAR 24 24D 5170311 CE NLG STEERING OUT OF ADJUST E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 324TW 24D324 AIRCRAFT INROUTE FROM MFE TO FSM, NOSE GEAR LIGHT WOULD NOT EXTINGUISH DIVERT TO ADS, MAINTENANCE IN ADS ADJUSTED NOSE W HEEL STEERING AND PERFORMED GEAR RETRACTION TEST ALL NORMAL RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4J A10CE 2002102800026 20021028 00026 NE 2002 10 28 0202973221 2 20020916 A 7200 ENGINE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 2 MAKING METAL A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CR CRUISE 1 GL 01 321US 00262 731783 DURING CRUISE FLIGHT, THE NR 2 ENGINE COMPRESSOR STALLED AND FLAMED OUT. NO RELIGHT WAS ATTEMPTED. FLIGHT CREW DIVERTE D TO LAS AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND METAL IN THE TAILPIPE. REPLACED THE NR 2 ENGINE. 2 L 7 2 4F 4 F RT A28NM E29NE 2002102800027 20021028 00027 CE 2002 10 28 00052 1 20021012 A 2130 MODULE LEAR 24 24D 5170311 CE CABIN PRESSURE MALFUNCTIONED E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 888TW 292 AIRCRAFT DEPARTED ELP, CABIN PRESSURE WOULD CLIMB WITH AIRCRAFT, RETURN TO ELP FOR MAINTENANCE.MAINTENANCE REPOSTIONED T UBE ON CABIN PRESSURE MODULE AND OPS CK GOOD, RETURN AIRCRAFT TO SERVICE. 2 L 7 2 4J A10CE 2002102800028 20021028 00028 WP 2002 10 28 0202999919 1 20020922 A 3213 59105285026 CYLINDER DOUG DC9 DC932 3022066 WP RT MLG FAILED A NWAA O OTHER Z SIGNIFICANT FAILURE REPORT TX TAXI/GRND HDL 1 GL 01 941N 47450 THE RIGHT MAIN LANDING GEAR COLLAPSED DURING TAXI TO RUNWAY. PRELIMINARY INVESTIGATION REVEALED A FAILED MAIN LANDING G EAR STRUT CYLINDER BARREL. 2 L 7 2 4F A6WE 2002102800029 20021028 00029 NE 2002 10 28 00053 2 20021018 A 7200 ENGINE LEAR 24 24B 5170306 CE GE CJ610 CJ6106 30006 NE RIGHT FLAMED OUT E HAEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 233TW 24B221 251210A AIRCRAFT IN ROUTE FROM BRO TO ADS, AT FLT LVL 410 RT ENGINE FLAMED OUT, REQUEST LOWER TO PERFORM RESTART, NORMAL RESTART AND CLIMB TO 390, MAINTENANCE PERFORMED ENGINE CHECKS AT ADS PER THE GE MM SEI 186 FLAMEOUT TROUBLE SHOOTING GUIDE AND PERFORMED GROUND RUNS, ALL NORMAL AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4J 4 J A10CE 1E16 2002102800030 20021028 00030 WP 2002 10 28 0203119860 1 20020919 A 3240 LINE DOUG DC9 DC951 3022051 WP LT MLG BRAKE LEAKING A NWAA K NONE K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 01 769NC 47757 DURING DESCENT, THE RIGHT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. THE RIGHT HYDRAULIC PRESSURE DROPPED TO ZERO. COMP LIED WITH COM PROCEDURES AND FLIGHT CONTINUED WITH AN UNEVENTFUL APPROACH AND LANDING. MAINTENANCE FOUND THE LEFT OUTBO ARD BRAKE LINE DAMAGED AND LEAKING. REPLACED THE LEFT OUTBOARD BRAKE LINE, RIGHT HYDRAULIC PUMPS, AND FILTERS. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002102800031 20021028 00031 WP 2002 10 28 0203129860 1 20020922 A 2150 39271411 REGULATOR VALVE DOUG DC9 DC951 3022051 WP RT PACK MALFUNCTIONED A NWAA B EMER. DESCENT O OTHER CR CRUISE 1 GL 01 769NC 47757 AT FL330, CABIN WAS CLIMBING 800-1000 FPM. CREW WAS UNABLE TO CONTROL PRESSURE MANUALLY. PERFORMED COM PROCEDURES AND MADE AN EMERGENCY DESCENT. AUTO PRESSURE CONTROLLER BEGAN WORKING AGAIN AT 18,000 FT. CABIN ALTITUDE HAD REACHED 12,50 0 FT MAXIMUM. FLIGHT LANDED SAFELY AT MCO. MAINTENANCE REPLACED THE RIGHT PACK PRESSURE REGULATOR VALVE AND PILOT PRES SURE REGULATOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002102800032 20021028 00032 CE 2002 10 28 042514 1 20020820 A 2710 AILERON BEECH 1900 1900D 1154162 CE WING MISRIGGED A AMWA O OTHER W INADEQUATE Q C LD LANDING 1 CE 07 5YV UE5 AFTER LANDING IN PANAMA CITY, FLORIDA ON FLIGHT 5466, THE CREW REPORTED THAT THE AILERON WAS RIGGED IMPROPERLY.MAINTENAN CE IN PANAMA CITY FLORIDA, REINSTALLED THE CABLE DRUM AND THE CABLE TENSION. THE AIRCRAFT WAS THEN TEST FLOWN WITH SATIS FACTORY RESULTS. NO PARTS WERE USED. 2 L 7 2 4T RT A24CE 2003022000094 20030220 00094 CE 2003 2 20 043349 1 20020919 A 6120 1293640919 PCU BEECH 1900 1900D 1154162 CE LT AND RT PROP FAILED A AMWA O OTHER O OTHER LD LANDING 1 CE 07 15YV 2677 2521 UE15 UPON ARRIVAL INTO PANAMA CITY, FLORIDA ON FLIGHT 5466, THE LT AND RT AUTO FEATHER SYSTEM FAILED CAUSING THE CONDENSER BL OWER TO POP. THE SYSTEM WAS LOOKED AT BY THE PANAMA CITY MAINTENANCE. THE PROBLEM WAS THAT THE PRINTED CIRCUIT BOARD WAS BAD. THE CORRECTIVE ACTION WAS THAT THEY REMOVED AND REPLACED THE PRINTED CIRCUIT BOARD. THEY DID A GROUND RUN WHICH WA S NORMAL AND THEY RETURNED THE AIRCRAFT TO SERVICE. THE TEARDOWN REPORT REVEALED THAT THERE WAS NO DEFECTS FOUND. THE V ENDOR TESTED, CLEANED AND RECOATED AS NECESSARY. 2 L 7 2 4T RT A24CE 2002102800033 20021028 00033 2002 10 28 043874 4 20021008 A 3497 6226521016 CONTROL HEAD BEECH 1900 1900D 1154162 CE NR 1 NAVIGATION FAILED A AMWA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 CE 07 166YV 5436 5436 UE166 WHILE THE AIRCRAFT WAS IN CRUISE FROM RALEIGH-DURHAM, NORTH CAROLINA TO NORFOLK, VIRGINIA THE DISPLAY ON THE NAV CONTROL HEAD 1 BECAME INOPERABLE. THE CREW SMELLED AN ELECTRICAL FUME. THEY TURNED NAV CONTROL HEAD 1 OFF AND THE ELECTRICAL SM ELL WENT AWAY. THE CORRECTIVE ACTION WAS THAT THEY REMOVED AND REPLACED THE NR 1 NAV CONTROL HEAD. THE TEARDOWN REPORT H AS BEEN RECEIVED. THIS REPORT STATES THAT THE VENDOR FOUND A BAD FUSE ON THE INPUT LINE. THE VENDOR CORRECTIVE ACTION WA S THAT THEY REPLACED FUSE FO1. THE VENDOR ALSO REPAIRED, ALIGNED AND TESTED THE PART. 2 L 7 2 4T RT A24CE 2002102800034 20021028 00034 NM 2002 10 28 0203146730 1 20020921 A 5280 65B100192 DOOR BOEING 747 7472J9F 1384806 NM NLG DAMAGED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 630US 21668 DURING CLIMB, THE RED DOOR OPEN LIGHT ILLUMINATED WITH A NOSE LANDING GEAR OPEN INDICATION ON BOTH PRIMARY AND ALTERNATE . AIRCRAFT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT FORWARD NOSE LANDING GEAR DOOR AND ADJUSTED THE DOOR WARNING SENSORS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002102800035 20021028 00035 CE 2002 10 28 044109 1 20021016 A 5270 SWITCH BEECH 1900 1900D 1154162 CE CABIN DOOR DIRTY A AMWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 26YV UE26 AFTER TAKE OFF FROM ITHACA, NEW YORK TO PHILADELPHIA, PENNSYLVANIA ON FLIGHT 5460, THE CABIN DOOR ANNUNCIATOR ILLUMINATE D. THE AIRCRAFT WAS THEN RETURNED TO FIELD WITH NO FURTHER INCIDENT. THE CABIN DOOR ANNUNCIATOR WAS DEFERRED ON THE FOLL OWING MEL 52-1-C. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. THE CORRECTIVE ACTION WAS THAT THE MECHANICS CLEANED AND AD JUSTED THE ASD SAFETY SWITCHES. NO PARTS WERE USED. 2 L 7 2 4T RT A24CE 2002102800036 20021028 00036 NM 2002 10 28 02092601 1 20020925 A 3350 FUSE BOEING 757 757236 1384971 NM BATTERY CHARGER BLOWN A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 546NA 29945 EMERGENCY FLOOR LIGHTING FROM ROWS 14 TO 24 INOP. TROUBLESHOOTING REVEALED FAILED LIGHTING POWERPACK. INSPECTION REVEA LED A BLOWN FUSE IN THE POWERPACK BATTERY CHARGER. FUSE WAS REPLACED, BATTERY PACK ASSEMBLY REPLACED, OPS CHECK GOOD AS PER M/M 33-51-07. AIRCRAFT WAS RETURNED TO REVENUE SERVICE. 2 L 7 2 4F RT A2NM 2002112600037 20021126 00037 CE 2002 11 26 044288 1 20021022 A 3234 1013841377 HANDLE BEECH 1900 1900D 1154162 CE MLG SELECTOR FAILED A AMWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 142ZV UE142 AFTER THE DEPARTURE FROM ROSWELL, NEW MEXICO TO ALBUQUERQUE NEW MEXICO ON FLIGHT 415, THE LANDING GEAR FAILED TO RETRACT . THERE WAS NO ABNORMAL INDICATIONS IN THE COCKPIT.THE AIRCRAFT CONTINUED ON ITS FLIGHT TO ALBUQUERQUE AND LANDED WITH N O FURTHER INCIDENT. THE ALBUQUERQUE MAINTENANCE FOUND THE LANDING GEAR HANLDE HAD FAILED. THE CORRECTIVE ACTION WAS THAT THEY REMOVED AND REPLACED THE LANDING GEAR HANDLE. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. THE TEARDOWN REPORT HAS B EEN RECEIVED ON 11/18/02. THE REPORT STATES THAT THE UNIT REQUIRES THE REPLACEMENT OF TWO SWITCHES. 2 L 7 2 4T RT A24CE 2002102800038 20021028 00038 NM 2002 10 28 02FDEA00668 1 20020920 A 2613 SENSOR BOEING 727 727200 138407E NM AFT AIRSTAIRS OUT OF POSITION A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 282FE 22349 AT LEVEL OFF AT 28000 FT, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. COMPLIED WITH QRH PROCEDURES. LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED WITH NR 3 BLEED VALVE CLOSED AND RIGHT PACK OFF. CHECKED SENSOR IN AFT AIRSTAIR AREA, REPOSIT IONED TWO PLACES OF POSSIBLE CONCERN. RAN NR 3 ENGINE PER JRH FOR 5 PLUS MINUTES WITH NO OVERHEAT INDICATION. CHECKED SENSOR ON RT SIDE OF AIRSTAIRS AREA, FOUND SENSOR AT ONE PLACE TOUCHING, REPOSITION SENSOR. RAN A/C AT POWER FOR 10 MI NUTES ON GROUND MEM OPS CHECKED NORMAL. 2 L 7 3 4F RT A3WE 2002102800040 20021028 00040 NM 2002 10 28 SCNA020007 1 20021020 A 3350 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 EMERGENCY FLOOR PATH LIGHT OUT AT ROW 10. RELAMPED FLOOR PATH LIGHT AT ROW 10. OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2002102800041 20021028 00041 WP 2002 10 28 IXXA0200052S 1 20020510 A 5330 SKIN DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE AFT LOWER FUSELAGE STATION 1520 BETWEEN LONGERONS 30LT TO 30RT. REPAIR ACCOMPLISHED, DAMAGED AREA CUT OUT, FABRICATION AND INSTALLATION OF FILLER AND REPAIR DOUBLER IN ACCORD ANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002102800042 20021028 00042 WP 2002 10 28 IXXA0200053S 1 20020510 A 5330 SKIN DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE AFT LOWER FUSELAGE FORWARD OF ACCESS PANEL NUMBER 60, S TATION 1557 TO 1574, LONGERON 35 RT. REPAIR ACCOMPLISHED, REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A INTERNAL FILLER AND REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002102800043 20021028 00043 NM 2002 10 28 02FDEA00669 1 20020920 A 2910 B-NUT DOUG MD11 MD11 3023602 NM HYD SYSTEM LOOSE A FDEA F J B A ACTIVATE FIRE EXT. DUMP FUEL EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 621FE 48792 IN CRUISE GOT HYD 3 ELEV OFF THEN 3-2 NRMP INOPERATIVE LOSS OF NR 3 HYD FLUID, THEN HYD NR 3 FAILED. DUMPED APPROX 5000 0 LBS OF FUEL AND LANDED AT ORD, DECLARED EMERGENCY AND PULLED CVR. FOUND LOOSE B-NUT AT CHECK VALVE IN AFT ACCESSORY C OMP RT SIDE. TIGHTENED SAME. 2 L 7 3 4F RT A22WE 2002102800044 20021028 00044 WP 2002 10 28 IXXA0200054S 1 20020510 A 5310 STRUCTURE DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE AT STATION 1440 AT LONGERON 22RT. REPAIR ACCO MPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER AND INTERNAL FILLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002110800030 20021108 00030 NM 2002 11 8 02FDEA00671 1 20020923 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 AFTER CORROSION REMOVAL ON BARREL NUT HOLE NR 36 LT, BOTTOM SURFACE BLENDOUT EXCEEDED LIMIT AS PER SB MD11-55-023. R&R HORIZ STABILIZER PER EA 1-5510-66415. 2 L 7 3 4F RT A22WE 2002102800045 20021028 00045 WP 2002 10 28 IXXA0200055S 1 20020511 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AROUND THE SCREW HEADS ON THE TOP LEFT WING LEADING EDGE XFS 8 85. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF FILLER AND REPAIR DOUBLER IN ACCORDAN CE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002110800031 20021108 00031 NM 2002 11 8 02FDEA00672 1 20020923 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 AFTER CORROSION REMOVAL ON BARREL NUT HOLE NR 36 RT, BOTTOM SURFACE AND SIDEWALL BLEND OUT EXCEEDED LIMIT AS PER SB MD11 -55-023. R&R HORIZ STAB PER EA 1-5510-66415. 2 L 7 3 4F RT A22WE 2002102800046 20021028 00046 WP 2002 10 28 IXXA0200056S 1 20020511 A 5710 STRUCTURE DOUG DC8 DC862 3021970 WP LEADING EDGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED IN THE LEFT WING LEADING EDGE TOP SIDE AT STATION XFS 825. RE MOVAL ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGL AS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002102800047 20021028 00047 WP 2002 10 28 IXXA0200057S 1 20020511 A 5754 STRUCTURE DOUG DC8 DC862 3021970 WP LEADING EDGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RT WING OUTBOARD LEADING EDGE AT STATION XFS 705. REPA IR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER AND INTERNAL FILLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002102800048 20021028 00048 WP 2002 10 28 IXXA0200058S 1 20020511 A 5754 STRUCTURE DOUG DC8 DC862 3021970 WP LEADING EDGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LT WING OUTBOARD UPPER LEADING EDGE AT STATION XFS 705. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER AND FILLER IN ACCORDANC E WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002102800049 20021028 00049 NM 2002 10 28 02FDEA00683 1 20020924 A 3260 656021123 ACCESSORY UNIT BOEING 727 727200 138407E NM E/E BAY FAULTY A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 217FE 22938 UPON GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH LG LEVER IN THE UP POSITION. COMPLIED WITH RED T AB PROCEDURE. LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LANDING GEAR ELECTRONIC MODULE B727 M/ M 32-09-121-4. REMOVED AND REPLACED LT MLG UPLOCK SENSOR B727-200 M/M 32-61-081-4. OPS CKS GOOD PER 727-200 M/M 32-61- 081-4. OPS CK'D LANDING GEAR ELECTRONICS MODULE PER 727-200 M/M 32-09-122-5, OPS CKS GOOD. 2 L 7 3 4F RT A3WE 2002102800050 20021028 00050 WP 2002 10 28 IXXA0200059S 1 20020511 A 5754 SKIN DOUG DC8 DC862 3021970 WP LT WING LE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION AND A CRACK WAS DETECTED ON THE LEFT WING OUTBOARD LOWER LEADING EDGE AT ST ATION XFS 566. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTE RNAL DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002102800051 20021028 00051 WP 2002 10 28 IXXA0200060S 1 20020514 A 5754 SKIN DOUG DC8 DC862 3021970 WP RT WING LE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 84868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION AND A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE AT WING STATION XES 710, UPPER CHORD MOUNTS. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILL ER AND EXTERNAL DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002102800052 20021028 00052 WP 2002 10 28 IXXA0200061S 1 20020514 A 5754 SKIN DOUG DC8 DC862 3021970 WP RT WING LE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, A CRACKED WAS DETECTED ON THE RIGHT WING OUTBOARD LEADING EDGE PANEL AT THE INBOARD A REA AT STATION XRS 634. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A FILLER AND R EPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002102800053 20021028 00053 EU 2002 10 28 02FDEA00684 1 20020924 A 2720 RELAY AIRBUS 310 A310 EU RUDDER TRAVEL FAILED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 420FE 339 RUDDER TRAVEL SYSTEM TWO FAULTED IN FLIGHT, WOULD NOT RESET. RUDDER TRAVEL SYSTEM ONE ALREADY DEFERRED. CHECKED FAULT AT FLC NR 2 RUDDER TRAVEL POWER LOOP. PERFORMED T/S PER TSM 27-23-03 REPLACED 309 CY2 RELAY, BITE TEST FLC NR 2 PER MM 27-23-00. OK, NO FAULT NOTED. 2 L 7 2 4F RT A35EU 2002102800054 20021028 00054 WP 2002 10 28 IXXA0200062S 1 20020515 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 45918 DURING ROUTINE C-CHECK INSPECTION, LIGHT CORROSION WAS DETECTED ON THE TOP OF THE LEFT WING INTERSPAR SKIN BETWEEN STATI ON XW 408 XRS 590 TO STATION XRS 590. REPAIR ACCOMPLISHED CORROSION REMOVAL OF THE AFFECTED AREA IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND BOEINGS FAX TIN-MIA-02-0001. THE CORROSION REMOVAL WAS FOUND TO BE WITHIN LIMITATIO N. 2 L 7 4 4F 4A25 2002102800055 20021028 00055 WP 2002 10 28 IXXA0200063S 1 20020515 A 5711 SPAR DOUG DC8 DC862 3021970 WP WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE UPPER WING EXTERNAL PLATING BETWEEN WING STATION XFS 17 2 AND XFS 255. REPAIR ACCOMPLISHED, CORROSION REMOVAL OF THE DAMAGE ARE, FABRICATION AND INSTALLATION OF A REPAIR DOUBLE R IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND FAA DER APPROVED DRAWING Q38-R02. 2 L 7 4 4F 4A25 2002102800056 20021028 00056 WP 2002 10 28 IXXA0200064S 1 20020515 A 5711 SPAR DOUG DC8 DC862 3021970 WP LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON TOP OF THE LEFT WING INTERSPAR SKIN BETWEEN XRS 190 INBOARD TO WING WALK AREA TO INCLUDE THE MAIN SKIN EXTENSION OVER GEAR TRUNNION AREA. REPAIR ACCOMPLISHED CORROSION REMOVAL. F ABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL, BOEING'S FAX TI N-MIA-02-001, DRAWING 01-08-31-002 AND FAA DER APPROVED DRAWING Q38-R02. 2 L 7 4 4F 4A25 2002102800057 20021028 00057 WP 2002 10 28 IXXA0200065S 1 20020515 A 5330 SKIN DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK, A CRACK WAS DETECTED IN THE AFT PASSENGER DOOR FORWARD LOWER SKIN CORNER AT SKIN CUTOUT. REPAIR ACCOMPLISHED, REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER, DOUBLER AND TRIPLER IN ACCO RDANCE WITH THE DOUGLAS STRUCTURAL REAPIR MANUAL AND BOEINGS FAX TIN-MIA-02-00005F AND TIN-MIA-02-00014H. 2 L 7 4 4F 4A25 2002102800058 20021028 00058 WP 2002 10 28 IXXA0200066S 1 20020516 A 5330 SKIN DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT HAND SIDE FUSELAGE SKIN BELOW THE AFT PASSENGER DO OR SKIN CUT OUT AT STATION 1480 TO 1510. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED SKIN, FABRICATION AND INSTALLATION OF FILLER REPAIR DOULBER AND TRIPLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND BOEINGS FAX TIN-MIA-02-000 07H 2 L 7 4 4F 4A25 2002102800059 20021028 00059 WP 2002 10 28 IXXA0200070S 1 20020530 A 5330 SKIN DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 902, LONG ERONS 14,17 AND 18 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL AND DETERMINED TO BE WITH LIMITATION IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND BOEINGS FAX TIN-MIA-02-00012H. 2 L 7 4 4F 4A25 2002102800060 20021028 00060 WP 2002 10 28 IXXA0200072S 1 20020601 A 5330 SKIN DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATION 857 TO 902 BETWEEN LONGERONS 10L TO 21L. REPAIR ACCOMPLISHED CORROSION REMOVAL AND FOUND TO BE WITHIN LIMITATIONS. CORROSION REMOVAL AT FUSELAGE STATION 857, STRINGER 12 FOUND OUT OF LIMITATION. REPAIR ACCOMPLISHE REMOVAL OF DAMAGED AREA, FABRI CATION AND INSTALLATION A FILLER AND REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND DRAWING Q38-R03. 2 L 7 4 4F 4A25 2002102800061 20021028 00061 WP 2002 10 28 IXXA0200073S 1 20020609 A 5513 STRUCTURE DOUG DC8 DC862 3021970 WP HORIZONTAL STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 81868 2627 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE STATION XFS 178 TO XFS 285. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND REPAI R DOUBLER IN ACCOURDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING AUTHORIZATION 28260-5508-2002-99. 2 L 7 4 4F 4A25 2002102800062 20021028 00062 2002 10 28 IXXA0200074O 4 20020925 A 2297 3753439501 PANEL DOUG DC8 DC871F 302199D WP COCKPIT BURNED A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 825BX 83096 41 45978 WHILE ENROUTE FROM STL TO ELP, SMOKE STARTED TO EMIT FROM THE CENTER CONSOLE AFTER THE AUTO PILOT WAS ENGAGED. THE FLIG HT CREW NOTICED SMALL FLAMES AND EXTINGUISHED THEM WITH A HALON FIRE BOTTLE. THE FLIGHT CREW PULLED AND COLLERED THE CI RCUIT BREAKERS TO THE AUTO PILOT TRIM AND DECLARED AN EMERGENCY LANDING AT ELP. MAINTENANCE INSPECTED THE AIRCRAFT WHIC H REVEALED THE STABALIZER TRIM LIGHT PANEL BURNED AND MELTED. MAINTENANCE REPLACED THE LIGHT PANEL AND PERFORMED SUCESS FUL OPERATIONAL CHECKS IN ACCORDANCE WITH THE DOUGLAS MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002102800063 20021028 00063 WP 2002 10 28 IXXA0200089O 1 20021018 A 3210 56165545503 ROD END DOUG DC8 DC871F 302199D WP LANDING GEAR STRIPPED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 825BX 83187 137 45978 AFTER TAKE OFF FROM BFI, THE LANDING GEAR DOOR NOT LATCHED LIGHT AND THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED FOLLOWIN G LANDING GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR AND PERFORMED A SUCESSFUL UP LATCH CHECK, BUT THE LIGHTS REM AINED ILLUMINATED. THE FLIGHT CONTINUED TO TOL WITH AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH RE VEALED THE ROD END STRIPPED FROM THE BOGIE TRIM CYLINDER. MAINTENANCE REPLACED THE CYLINDER AND PERFORMED SUCESSFUL OPE RATIONAL CHECKS IN ACCORDANCE WITH THE DOUGLAS MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002102800064 20021028 00064 NM 2002 10 28 UPS02239809 1 20021011 A 5330 BUTT JOINT BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 C CHECK FUSELAGE AT SKIN BUTT JOINT BS 260 AND BETWEEN STR 12 RT & 13 RT IS BULGING CUT OUT DAMAGED SKIN AND INSTALL ED REPAIR DOUBLER AS PER BOEING DRAW ING 69-62161 AND UPS E.O. B727-5310-1371-F APPENDIX E 2 L 7 3 4F A3WE 2002102800065 20021028 00065 NM 2002 10 28 UPS02439546 1 20020929 A 3210 UKN ROD BOEING 747 747123 1384873 NM MLG SHEARED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 674UP 20100 AFTER T/O LEFT BODY GEAR DOOR AND GEAR UNSAFE LIGHT CAME ON, GEAR CYCLED GEAR AND STILL HAD SAME RESULT.ACFT RETURNED TO PHL . M246067 FOUND RETRACT CYL ROD SHEARED. REPLACED LT BODY GEAR RETRACT CYL PER MM 32-33-01. OPS CK NORMAL. M 246067 CLEARED. 2 L 7 4 4F A20WE 2002102800066 20021028 00066 NM 2002 10 28 UPS02439551 1 20020907 A 5311 FRAME BOEING 747 747121 1384871 NM RT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 C CHECK, RT WLG W/W OVERWING LONGERON I/B CHORD O/B SIDE CORROSION REVEALED AT STA 1250-1265 RBL 120. CORROSION REM OVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.080 X 1 X 5 INCHES EXCEED SRM 53-10-01 LIMITS. CHORD REPAIRED PER FIG 51-40 -04 FIG 3. 2 L 7 4 4F A20WE 2002102800067 20021028 00067 NM 2002 10 28 UPS02439577 1 20020903 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C CRACK FOUND AT AFT CARGO DOOR CUTOUT FWD UPPER CORNER MOST AFT REMOVED FASTENER HOLE, TWO CRACKS FOUND ON SKIN OUTER SURFACE WITH LENGTH 1/16" AND 3/32" APPROX AT 1 AND 7 O'CLOCK RESPECTIVELY. (BS 1810, WL 199) AFT CAR GO DOOR CUT-OUT FWD UPPER CRACKED SKIN REPAIRED AS PER SRM 53-30-03 FIG. 62 DETAIL II. REPEAT INSPECTION IS REQUIRED AS PER SRM 53-30-03 FIG 62 TABLE III CATEGORY 'B' REPAIR. 2 L 7 4 4F A20WE 2002102800068 20021028 00068 NM 2002 10 28 UPS02439578 1 20020906 A 5330 144U00312 PANEL BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 DURING C CHECK, M/D- BS 1238-1265 RBL 75-98 CLOSURE PANEL CRACKED. M/D RT BS 1241 CANTED PRESSURE DECK CLOSEOUT PAN EL REPLACED AS PER EO# B747-5310-2758-E APPENDIX 'E'. 2 L 7 4 4F A20WE 2002102800069 20021028 00069 NM 2002 10 28 UPS02439579 1 20020905 A 5310 STRAP BOEING 747 747121 1384871 NM BS 800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 DURING C CHECK, CRACK FOUND ON LT BS 800 FRAME STRAP AT STR 16 AREA AT FWD MOST LOWER FASTENER HOLE BY APPROX 3/8 LONG R UNNING AFT & FWD TO THE EDGE. LT BS 800 FRAME STRAP AT STR 16 & STR 17 MOST LWR FASTENERS HOLE CRACKED REPAIRED AS P ER RS R53-22-34894 & EO B747-5310-17628A REPAIRED DETAILS REF NRC#UW59712 CONTINUE INSPECTIONS EVERY 3000 FLT CYCLES PE R REF /A AS PER RS R53-22-34894 & EO B747-5310-17628A. 2 L 7 4 4F A20WE 2002102800070 20021028 00070 NM 2002 10 28 UPS02439580 1 20020907 A 5712 RIB BOEING 747 747121 1384871 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 DURING C CHECK, RT W 22 V/C FLAP I/B ROTARY ACTUATOR MOUNTING RIB MOUNT BOLT HOLE SURFACE CORROSION REVEALED AT ALL MOU NT HOLES AND BORES. (RHW OLES 1205) RT W 22 V/C FLAP I/B ROTARY ACTUATOR RIB REPAIRED AS PER RS R57-41-34900 & EO B 747-5740-17619-A. ROTARY ACTUATOR R + I PER MM 27-81-07 RIGGING AND OPERATION CHK C/OUT PER MM 27-81-00 EO B747-5740-176 19-A ACCOMPLISHED. 2 L 7 4 4F A20WE 2002102800071 20021028 00071 NM 2002 10 28 UPS02439581 1 20020914 A 5313 LONGERON BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 DURING C CHECK, CRACK FOUND AT RT SIDE OF BS 1350 OVERWING LONGERON, THE CRACK FOUND INITIATED FROM FWD EDGE OF VERTI CAL FLANGE RUNNING TOWARD AFT TO I/B HORI FLANGE, TOTAL LENGTH OF CRACK 2 INCH LONG APPROXIMATELY. BS 1350 RT OVERWI NG LONGERON UPPER CHORD CRACKED AND CORRODED INTERIM REPAIR CARRIED OUT AS PER HX RS R-53-41-34906 & EA 747-53-20110 REP EAT INSPECTIONS EVERY 2000 FLTS PER REF 'F' SB747-53-2291 APPLY. 2 L 7 4 4F A20WE 2002102800072 20021028 00072 NM 2002 10 28 UPS02439582 1 20020915 A 5313 LONGERON BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 DURING C CHECK, LT BLG OVERWING LONGERON BS 1413 FOUND TWO CRACKS BOTH CRACKS THROUGH THICKNESS ONE CRACK IS 5.5 INCH I NLENGTH ANOTHER ONE CRACK IS 3 INCH IN LENGTH . BS 1413 LT OVERWING LONGERON ANGLE REPAIR CARRIED OUT AS PER HX RS R-53-43-34909 AND RA 747-53-20114. 2 L 7 4 4F A20WE 2002102800073 20021028 00073 NM 2002 10 28 UPS02439583 1 20020907 A 5340 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LT BS 1480 LONGERON EXTENSION FITTING NR 9 FASTENER HOLE FOUND CRACK. (STR L33 TO L34). LH EXTENS ION FITTING 9 BOLT HOLE REWORKED AS PER RS R53-43-34907 AND EO B474-5310-17618-A 2 L 7 4 4F A20WE 2002102800074 20021028 00074 CE 2002 10 28 09272002 1 20020927 A 3010 CONTACTOR BEECH MU300 400A 1155402 CE HORIZ STAB BURNED E DJFA K NONE J WARNING INDICATION CR CRUISE 1 EA 23 442CW 4305 RK42 HORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT. 2 H 7 2 4F RT A16SW 2002102800075 20021028 00075 NM 2002 10 28 UPS02439584 1 20020907 A 5340 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LT BS 1480 BULKHEAD LONGERON EXTENSION FITTING 1 FASTENER HOLE FOUND CRACK.(STR L33 TO L34). LH EX TENSION FITTING #1 BOLT HOLE REWORKED AS PER RS R53-43-34907 AND EO B747-5310-17618-A 2 L 7 4 4F A20WE 2002102800076 20021028 00076 NM 2002 10 28 CA021010006 1 20020930 A 5340 85311176 FITTING DHAV DHC8 DHC8102 2809003 NM PWA PW121 PW121 52124 NE HAMSTD 14SF 14SF7 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 28293 (CAN) DURING A STRUCTURAL INSPECTION OF THE NOSE LANDING GEAR WHEEL WELL, THE NOSE LANDING GEAR UPLOCK ACTUATOR FITTING ON THE AIRFRAME SIDE WAS FOUND CRACKED. FORWARD SECTION CLOSE TO THE ACTUATOR ATTACHMENT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002102800077 20021028 00077 EU 2002 10 28 CA021011001 1 20021010 A 3251 D23119750 CONTROL UNIT AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE NLG STEERING FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) NOSEWHEEL STEERING STAYS DISCONNECTED.LEVER ON STEERING BOX FOUND STICKINGDEACTIVATION ELECTRONIC BOX REPLACED AS PER AMM TASK 32-51-12 AND FUNCTION CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2002102800079 20021028 00079 NM 2002 10 28 UPS02439585 1 20020909 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C CRACK FOUND AT LT OF BS 1480 UPPER BULKHEAD CHORD LOWER RADIUS AT FORWARD SIDE (BLG WHEEL WELL) CRACK LENGTH 1.25 INCHES APPROX WHICH INITIATED FROM LOWER EDGE EXTENDED UPWARD. (STR L32 TO L32) BS 1480 LT UPPER BULKHE AD CHORD LOWER RADIUS CRACK REPAIR CARRIED OUT AS PER HX RS R-53-43-34898 AND EO B747-5310-17628-A 2 L 7 4 4F A20WE 2002102800080 20021028 00080 NM 2002 10 28 2002UALA01401 1 20020830 A 5210 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DIRTY A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 556UA 26650 NOISE AND VIBRATION NEAR THE R2 AFT DOOR. INSPECTED AND CLEANED DOOR SEALS AT DOOR 2R AND 4R. SEALS FOUND SERVICEABLE AND NO DAMAGE PRESENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002102800081 20021028 00081 NM 2002 10 28 2002UALA01469 1 20020918 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 CABIN LEFT HAND CREASE BEAM WEB CORRODED STATION 970. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002102800084 20021028 00084 NM 2002 10 28 2002UALA01472 1 20020918 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 945UA 26684 STATION 188 FUSELAGE FRAME INNER CHORD HAS 2 ELONGATED HOLES. MAJOR REPAIR ACCOMPLISHED, REPAIR DOUBLER MANUFACTURED AN D INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102800085 20021028 00085 NM 2002 10 28 UPS02439586 1 20020913 A 5330 PANEL BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 1241 RBL 6 FUEL LINE CLOSURE PANEL LOWER CUTOUT FOUND CRACK AFTER ATTACH PANEL REMOVED. BS 1241 RBL 6 CANTED BULKHEAD WEB FUEL LINE CLOSURE PANEL CUTOUT REPAIR CARRIED OUT AS PER HX RS R-53-48-34908, RA 747-53-2 0113 2 L 7 4 4F A20WE 2002102800086 20021028 00086 NM 2002 10 28 2002UALA01473 1 20020918 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 945UA 26684 BODY STATION 188 LEFT HAND FUSELAGE FRAME CRACKED IN CHORD BEND RADIUS AT WL 207.5. MAJOR REPAIR ACCOMPLISHED, DOUBLER MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102800087 20021028 00087 NM 2002 10 28 2002UALA01474 1 20020920 A 5320 FLOOR SUPPORT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 945UA 26684 CABIN FLOOR, AT GALLEY DOOR, FROM STA 291 TO STA 344, RT SIDE CREASE BEAM, FLOOR SUPPORT ANGLE HAS CORROSION. MAJOR REP AIR ACCOMPLISHED, REPLACED CREASE BEAM FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102800088 20021028 00088 NM 2002 10 28 UPS02439587 1 20020906 A 5320 WEB BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C U/D- FLR SUPPORT ATT CURVE WEB FOUND HEAVY CORR AS MARKED. (BS 460, WL 307, RBL 24) CORROSION REMO VED IAW SRM 51-10-01. CORROSION BLEND OUT 0.032" X 1" X 2" EXCEED SRM 53-10-01 LIMITS, WEB REPAIRED PER SRM 51-40-03 FIG 3 2 L 7 4 4F A20WE 2002102800089 20021028 00089 NM 2002 10 28 2002UALA01475 1 20020919 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 CABIN BODY STATION 807 FRAME WEB CRACKED AT STRINGER 9R. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102800090 20021028 00090 NM 2002 10 28 UPS02439588 1 20020905 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C CRACK FOUND ON LT BS 800 FRAME CHORD AT STR 16 AT FWD LOWER FASTENER HOLE BY APPROX 1/16 INCHES LONG RUNNING FWD LT BS 800 FRAME STRAP AND CHORD AT STR 16 FWD LWR FASTENER HOLE CRACKED. REPAIRED AS PERPER RS R53-022- 34894 & EO B747-5310-17629- A 2 L 7 4 4F A20WE 2002102800091 20021028 00091 NM 2002 10 28 UPS02439600 1 20021001 A 5330 SKIN BOEING 747 747200 1384847 NM FUSELAGE PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 528UP 1 HOLE PUNCTURED IN FUSELAGE SKIN FWD OF AFT LWR CARGO DOOR. BS 1790 - 1805 STR 37R TO STR 38 RT EXTERIOR SKIN REPAIRED A S PER SRM 53-30-03 FIG 1. 2 L 7 4 4F RT A20WE 2002102800092 20021028 00092 NM 2002 10 28 UPS02439601 1 20020909 A 5210 SKIN BOEING 747 747121 1384871 NM PAX DOOR MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D- BS 460 - 480 WL 208 - 216, LT NR 1 DOOR EXTERIOR SKIN FOUND NON-STANDARD REPAIR. SKIN REPAIRE D AS PER SRM 52-00-03 FIG 3 & MPI# 16130. 2 L 7 4 4F A20WE 2002102800093 20021028 00093 NE 2002 10 28 751PA0003 2 20020924 A 7200 ENGINE BOEING 757 757200 1384950 NM RROYCE RB211 RB211535E437 54555 NE NR 2 FLAMED OUT A PIDA K NONE X ENGINE FLAMEOUT DE DESCENT 1 SO 05 751PA 23928 30663 ON DESCENT INTO POS, NR 2 ENGINE FLAMED OUT. WENT TO FLT AND GOT A RELIGHT. INSPECTED NR 2 ENGINE FOR INTAKE & EXHAUST FOD DAMAGE, CHECKED N3 ROTATION, INSPECTED LP FUEL PUMP FOR DAMAGE, INSPECTED LP & HP FUEL FILTERS, NO DEFECTS NOTED IA W 757 FIM 71-05-00 FIG 106. OK FOR CONTINUED SERVICE. ENG RUN NR 2 NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A2NM E12EU 2002102800094 20021028 00094 NM 2002 10 28 UPS02439602 1 20020906 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C FX- EXTERNAL SKIN SURFACE FOUND DENTS AT BS 700 S40L TO S41L AREA AS MARKED. SKIN REPAIRED AT FX BS700 BETWEEN S40L TO S41L AS PER SRM 53-30-03 FIG 1 & MPI 16131 2 L 7 4 4F A20WE 2002102800095 20021028 00095 CE 2002 10 28 92702 1 20020927 A 3010 CONTACTOR BEECH MU300 400A 1155402 CE HORIZ STAB BURNED E DJFA K NONE J WARNING INDICATION CR CRUISE 1 EA 23 442CW 4305 RK42 HORIZONTAL STABILIZER ANTI-ICING HEATING ELEMENT FAILED TO HEAT. 2 H 7 2 4F RT A16SW 2002102800096 20021028 00096 NM 2002 10 28 UPS02439618 1 20020921 A 5315 FLOORBEAM BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C BS 540 UPPER DECK FLOORBEAM UPPER HORIZONTAL FLANGE, 1 EA FASTENER HOLE CRACK FOUND AT RBL 42, 1/8 INC HES LONG RUNNING AFT. FLOORBEAM AT BS 540 RBL 42 REPAIRED AS PER SRM 53-10-07 FIG 21. 2 L 7 4 4F RT A20WE 2002102800097 20021028 00097 WP 2002 10 28 ABXA020212 1 20020919 A 3222 TORQUE LINK DOUG DC8 DC863F 302198F WP NLG DISCONNECTED A ABXA K NONE J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 GL 23 816AX 46093 GROUND SHIFT FAILED AFTER TAKEOFF, UNABLE TO RAISE GEAR HANDLE, AUTO PRESSURIZATION INOPERATIVE. TAKEOFF WARNING HORN S OUNDED. RAN ABNORMAL. PULLED GROUND CONTROL CIRCUIT BREAKERS. SYSTEMS RESTORED. AFTER LANDING, AND NOSE WHEEL TOUCH DOWN, A LOUD POP WAS HEARD AND THE NLG REPEATEDLY SHOOK FROM SIDE TO SIDE. FOUND NOSE GEAR TORQUE LINKS NOT CONNECTED. RECONNECTED AND OPS CHECKED GROUND SHIFT IAW DC-8 MM 32-23-01. SWUNG NOSE LANDING GEAR FOR RETRACTION CHECK IAW DC-8 MM 32-20-00-05. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2002102800098 20021028 00098 NM 2002 10 28 UPS02439623 1 20020921 A 5310 BEAM BOEING 747 747SR46 1384816 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C NOSE WHEEL WELL BODY STRUCTURE CRACK FOUND AT RT VERTICAL BEAM WEB STAND-OFF HOLE AT BS 320 BTN 2 & 3 ( COUNTED FROM LOWER) VERTICAL BEAM CLIPS & ANOTHER CRACKED STAND-OFF HOLE FOUND BTN NR 5 & 6 CLIPS PLEASE REFER FIGUR E ATTACHED. VERTICAL BEAM WEB REPLACED PER SRM 51-10-01 P8. 2 L 7 4 4F RT A20WE 2002102800099 20021028 00099 NM 2002 10 28 UPS02439625 1 20021005 A 3350 SIGN BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 RT CREW SERVICE DOOR EMERGENCY EXIT SIGN INOP & CREW SERVICE HALL EMERGENCY LIGHT EXTREMELY DIM (NOTE CREW SERVICE HALL LT ONLY DIM WHEN TESTED IN ON POSITION IF ARMED AND POWER TURNED OFF LIGHT IS BRIGHT.) RELAMPED EMERGENCY EXIT SIGN PER 33-51-02 & R&R EMERGENCY EXIT LIGHT IN CREW SERVICE HALL CEILING PER 33-15-07. R&R LAMPS IN CREW SERVICE HALL LIGHT . REPOPSITIONED CONTACTS FOR RT CREW DOOR EXIT SIGN. SYS OP CHECKS NORMAL PER MM CHAPTER 33-51-01. 2 L 7 4 4F A20WE 2002102800101 20021028 00101 NM 2002 10 28 UPS02439626 1 20021006 A 3350 BATTERY BOEING 747 747123F NM MAIN CARGO BAY INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 677UP 20391 SEVERAL EMERGENCY LIGHT BULBS INOP AT MAIN CARGO COMPARTMENT CEILING NEAR MAIN ENTRY DOOR AND ONE BULB INOP AT MAIN ENTR Y DOOR OVERHEAD REPLACED BATTERY ASSY IN EMERGENCY LIGHT ASSY M325 AT STATION 580 LT. LIGHT OPERATION CKS OK & 21 DO OR AFT SILL LIGHT. CK OK EMERGENCY LIGHT M385 AT STATION 350 RT TRANSFERRED TO NON ROUTINE 596229 2 L 7 4 4F A20WE 2002102800102 20021028 00102 NM 2002 10 28 UPS02439627 1 20021006 A 3350 LIGHT BOEING 747 747123F NM COCKPIT MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 TRANSFERRED FROM NONROUTINE 596216 MAIN DECK EMERGENCY LIGHT M385 AT STA 350 RT IS INOP FOUND NO LIGHT ASSY INSTALLE D REF WD 35-51-01 SNT 2, PG 2, NOTE 1 LIGHT ASSY AT THIS POSITION WAS DEACTIVATED BY EO 33-50-301A LABELED CEILING PANEL ACCORDINGLY. 2 L 7 4 4F A20WE 2002102800103 20021028 00103 NM 2002 10 28 UPS02439629 1 20021007 A 3350 LIGHT BOEING 747 747200 1384847 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 521UP 21944 ESCAPE SLIDE EMERGENCY LIGHT INOP. TRANSFER TO MEL 25-11-1 CAT C PLACARD INSTALLED. 2 L 7 4 4F RT A20WE 2002102800104 20021028 00104 NM 2002 10 28 UPS02439630 1 20020920 A 5320 SUPPORT BOEING 747 747SR46 1384816 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C FX BS 1620 RBL 50-56 BODY SUPPORT FRAME CORRODED. CORROSION BLEND OUT 0.039 X 1 X 2 INCHES EXCEED SRM LIMIT, REPAIRED AS PER SRM 53-50-01. 2 L 7 4 4F RT A20WE 2002102800105 20021028 00105 NM 2002 10 28 UPS02439634 1 20020916 A 5340 65B04393202 ATTACH ANGLE BOEING 747 747SR46 1384816 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C AFT BULK CARGO - BS 2231 S33R FRAME ATTACH ANGLE FOUND COR DAMAGED. COR BLEND OUT 0.63" X 1" X 1" EXCEED SRM LIMIT. ANGLE REPLACED AS PER SRM 51-10-01 P.8. 2 L 7 4 4F RT A20WE 2002102800107 20021028 00107 NM 2002 10 28 UPS02439635 1 20020915 A 5311 FAILSAFE BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C LT BS 800 FRAME S16 AREA, ONE FASTENER HOLE FOUND CRACKED AT STRAP 1/8 INCHES RUNNING FWD AND AFT, CRA CK AT ANGLE 0.040 INCH RUNNING FWD REF ATT SKETCH FOR DETAILS. BS 800 FRAME CRACKED AREA REPAIRED PER RS R53-22-3491 0. ** TO BE CONTINUEOUS PERFORMING REPEAT INSPECTION PER SB 747-53A2451 EVERY 3000 FLIGHT CYCLES. ** 2 L 7 4 4F RT A20WE 2002102800108 20021028 00108 NM 2002 10 28 UPS02439636 1 20020915 A 5311 FAILSAFE BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C RT BS 800 FRAME AREA FOUND 5 EA FASTENER HOLES CRACKED. REF ATT SKETCH FOR DETAILS. STRAP AND CHO RD REPAIRED AS PER RS R53-22-34910 & UPS EO NR B747-5310-17666-A. ** TO BE CONTINUEOUS PERFORMING REPEAT INSPECTION PER SB 747-53A2451 EVERY 3000 FLIGHT CYCLES.** 2 L 7 4 4F RT A20WE 2002102800109 20021028 00109 NM 2002 10 28 UPS02439644 1 20021009 A 3350 SIGN BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 EMERGENCY EXIT SIGN ABOVE R/H DOOR UPPER DECK INOPERATIVE. DEFERRED EMERGENCY EXIT SIGN FOR UPPER DECK RT DOOR PER M EL 33-15. DEF #246761.REMOVED AND REPLACED LIGHT ASSY. OPS CHECKS GOOD 2 L 7 4 4F A20WE 2002102800110 20021028 00110 NM 2002 10 28 UPS02439647 1 20020916 A 5330 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C DURING RAP MOD ACCOMPLISH, BS 970-975 STR 40L-41L PREVIOUS REPAIR DOUBLER IS LESS THAN EXISTING SKIN THICKNESS & SHORT EDGE MARGIN FOUND AT CUTOUT AREA. FX SKIN REPAIRED AT BS 970-975 STR 40L-41L AREA AS PER SRM 53-30 -03 FIG 1. 2 L 7 4 4F RT A20WE 2002102800111 20021028 00111 2002 10 28 375PA0005 4 20021025 A 2230 COMPUTER BOEING 737 7373Y0 1384671 NM AUTOPILOT MALFUNCTIONED A PIDA K NONE O OTHER TO TAKEOFF 1 SO 05 375PA 23812 AUTO THROTTLE DISENGAGED WHEN AUTO THROTTLE WAS INGAGED FOR TAKE-OFF. RE-RACKED AUTO THROTTLE COMPUTER. RAN BITE TEST ON FMC, SYSTEM TESTS NORMAL. 2 L 7 2 4F RT A16WE 2002102800112 20021028 00112 NM 2002 10 28 UPS02439648 1 20020918 A 5312 BULKHEAD BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C LT BS 1480 AREA FOUND HOLE NR 26 CRACKED AT BULKHEAD WEB. LT BS 1480 BULKHEAD SPLICE WEB NR 26 BOL T HOLE OVERSIZED TO 0.660 INCH & CONFIRMED CRACK FREE. REPAIR BUSHING FABRICATED & INSTALLED AS PER BOEING SB 747-53A239 0 FIG 11 & HAECO RS R-53-43-34911 & UPS EO B747-5310- 17623-A. THE REPEAT INSPECTION OF BS 1480 BULKHEAD & SPLICE COMPON ENT WILL BE REDUCED TO 4800 FLIGHT CYCLES AS PER UPS EO B747-5310-10732. 2 L 7 4 4F RT A20WE 2002102800113 20021028 00113 2002 10 28 375PA0006 4 20021026 A 2230 COMPUTER BOEING 737 7373Y0 1384671 NM AUTOPILOT MALFUNCTIONED A PIDA K NONE O OTHER TO TAKEOFF 1 SO 05 375PA 23812 AUTO THROTTLE WOULD NOT ARM ON TAKE-OFF. ON DECENT INTO SFB, IN LEVEL CHANGE, AT MOVED FWD & BACK SWITCHING FROM "N" TO "RETARD" REPEATEDLY. CHK'D AUTO THROTTLE COMPUTER & RAN BITE CHK. ON CDU PER MM22-31-00 PG.501-508, NO FAULTS FOUND. 2 L 7 2 4F RT A16WE 2002102800114 20021028 00114 NM 2002 10 28 UPS02439689 1 20020917 A 5310 STRAP BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C LT BS 2231 STR 25 1 EA FASTENER HOLE CRACK FOUND AT REVEAL RUNNING FWD APPROX 0.040 INCH AND RUNNING AFT APPROX 0.020 INCH. PLS REFER ATT FIG. BS 2231 S25L STRAP REPAIRED AS PER SRM 53-10-04 FIG 115. ** REPEAT INSPECT ION PER BSB 53A2450 AT 3000 FLT CYCLES INTERVAL.** 2 L 7 4 4F RT A20WE 2002102800115 20021028 00115 NM 2002 10 28 UPS02439690 1 20020919 A 5330 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C RT BS 1810 STR 27 AFT CARGO DOOR UPPER DOOR UPPER FWD CORNER 1 EA FASTENER HOLE CRACK FOUND AT SKIN , APPROX 1/8 INCH RUNNING DOWNWARD. PLS REFER ATT FIG. AFT CARGO DOOR CUTOUT UPPER FWD CORNER REPAIRED AS PER SRM 53- 30-03 FIG 62. REPEAT INSPECTION IN 3000 CYCLES INTERVAL. 2 L 7 4 4F RT A20WE 2002102800116 20021028 00116 NM 2002 10 28 UPS02439696 1 20021012 A 3510 280001 REGULATOR BOEING 747 747121 1384871 NM OXYGEN SYS LEAKING A IPXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 683UP 20353 ON PREFLIGHT CREW QXYGEN WAS 10 AT TOP OF CLIMB QUANTITY WAS 6.5 MONITORED FOR THE NEXT 25 MINUTES AND QUANTITY DROPPED TO 5.5 NOTIFIED DISPATCH AND RETURNED TO SDF. REMOVED AND REPLACED BOTH CREW O2 BOTTLES PER MM 12-15-08 REMOVED AND RE PLACED 2ND OBS O2 REG. AND MASK PER MM 35-11-07 AND OPS CHECKED PER 35-11-07(MASK ASSY P/N 358-1510V S/N N/S/N LOC FIRST OBS 2 L 7 4 4F A20WE 2002102800118 20021028 00118 NM 2002 10 28 AT0200078 1 20020919 A 5321 FLOORBOARD BOEING 717 717200 1383700 NM FUSELAGE PUNCTURED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 954AT 55016 FORWARD CARGO PIT, FLOORBOARD STA 465 TO 541 HAS SEVERAL PUNCTURES. INSTALLED NEW FLOOR BOARD AT FORWARD CARGO PIT IAW B-717 SRM 25-58-01, AND AS PER EA NR 17-2558-A1521 REV IR AND RES NR 02-0824. 2 L 7 2 4F TR A6WE 2002102800119 20021028 00119 NM 2002 10 28 UPS02439726 1 20020916 A 5311 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C M/D - BS 2231 S25R FRAME CHORD FOUND CRACKED. BS 2231 FRAME CHORD REPAIRED AT STR 24R-26R AS PER HX RS R53-62-34918 (UPS EO B747-5310-17697-A).TO BE CARRY OUT REPEAT INSPECTION IN THE REPAIR AREA AT 3000 CYCLE INTERV ALS PER SB 747-53A2450. 2 L 7 4 4F RT A20WE 2002102800120 20021028 00120 NM 2002 10 28 AT0200079 1 20020919 A 5321 FLOORBOARD BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 954AT 55016 TEMPORARY REPAIR OF FORWARD CARGO PIT FLOORBOARD STA 369 TO 426, FLOORBOARD REQUIRES FAB OF NEW BOARD. INSTALLED NEW FL OOR BOARD IAW EO 17-2558-A1530, REV IR AND RES 02-0824. 2 L 7 2 4F TR A6WE 2002102800121 20021028 00121 NM 2002 10 28 UPS02439729 1 20020918 A 5320 STRAP BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C LT SIDE BS 1241 SPLICE STRAP 2 EACH CRACKS REVEALED OF AFT HOLE RUNNING AFT THE THICKNESS. REF HX RS R-53-43-34916 & UPS EO B747-5310-17698A. THE CRACKED STRAPS MUST BE INSPECTED EVERY 3000 FIGHTS PER EO B747-5310-032 3 & SB 747-53-2283 UNTIL SPLICE STRAPS & SOILID FILLERS REPLACED WITHIN 2 YEARS. 2 L 7 4 4F RT A20WE 2002102800122 20021028 00122 NM 2002 10 28 AT0200080 1 20020919 A 5321 FLOORBOARD BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 954AT 55016 TEMPORARY REPAIR OF FORWARD CARGO PIT FLOORBOARD STA 218 TO 331, REQUIRES FAB OF NEW FLOORBOARD. INSTALLED NEW FLOOR BO ARD IAW 17-2558-A1529 REV IR AND RES NR 02-0824. 2 L 7 2 4F TR A6WE 2002102800123 20021028 00123 NM 2002 10 28 UPS02439730 1 20020918 A 5320 STRAP BOEING 747 747SR46 1384816 NM BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C RT SIDE BS 1241 BULKHEAD SPLICE STRAP CRACK REVEALED AT AFT HOLE RUNNING FWD & AFT. REFER HX RS R -53-43-34916 & UPS EO B747-5310-17698-A. THE CRACKED STRAPS MUST BE INSPECTED EVERY 3000 FLIGHTS PER EO B747-5310-0323 & SB 747-53-2283 UNTIL STRAPS AND SOILD FILLERS REPLACED WITHIN 2 YEARS. 2 L 7 4 4F RT A20WE 2002102800124 20021028 00124 2002 10 28 AWXA200200901 4 20020919 A 3442 6225132106 TRANSCEIVER BOEING 757 7572S7 1384962 NM WEATHER RADAR SHORTED A AWXA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 902AW 33721 13073 23322 BWI - AIR TURN BACK - FLT 0083 - EN ROUTE FROM BWI TO LAS A WEATHER RADAR FAIL MESSAGE APPEARED INTERMITTENTLY FOLLOWED BY A STRONG ELECTRICAL BURNING SMELL. DUE TO WEATHER EN ROUTE AIRCRAFT TURNED BACK TO BWI. MAINTENANCE REMOVED AND REP LACED THE WEATHER RADAR R/T UNIT IAW 34-43-01. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002102800131 20021028 00131 NM 2002 10 28 02FDEA00653 1 20020910 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 478FE 21395 DENT ON FUSELAGE EXTERIOR SKIN AT BS 194 BELOW STR 20L. R&R SKIN PER SRM 53-30-3 FIG 24. 2 L 7 3 4F RT A3WE 2002102800132 20021028 00132 NM 2002 10 28 02FDEA00654 1 20020916 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 478FE 21395 DENTS ON FUSELAGE EXTERNAL SKIN AT BS 268 BETWEEN STR 19R & 20R. R&R SKIN PER SRM 53-30-2 FIG 24. 2 L 7 3 4F RT A3WE 2002102800134 20021028 00134 NM 2002 10 28 02FDEA00659 1 20020917 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 DENTED FRAME AT BS 560, APPROX STR 24L. R&R FRAME PER EA 7-5310-65881. 2 L 7 3 4F RT A3WE 2002102800142 20021028 00142 NM 2002 10 28 UPS02439731 1 20020918 A 5320 STRAP BOEING 747 747SR46 1384816 NM BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C LT SIDE BS 1241 BULKHEAD SPLICE STRAP AREA, CRACK REVEALED AT AFT HOLE AT SKIN RUNNING FWD APPROX 1 /8" IN LENGTH. LH BS1241 B/H SKIN AFT HOLE REPAIRED AS PER HS RS R-53-43-34916 INSTRUCTION 'A' & UPS EO B747-5310-17 698-A. (NOTE : L/R FAILSAFE STRAP IS TO BE INSPECTED PER SB 747-53-2283 'CRACKED STRAP' PROCEDURE EVERY 3000 FLIGHTS. TH E SPLICE STRAPS & SOLID FILLERS REQUIRED TO REPLACE WITHIN 2 YEARS) 2 L 7 4 4F RT A20WE 2002102800148 20021028 00148 SO 2002 10 28 SWIA200211258 1 20020920 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 221SW 5043 5043 120290 4 WHITE & 1 RED LIGHTS ON FLOOR LEVEL EMERGENCY LIGHTING SYSTEM INOP. REMOVED AND REPLACED MID CABIN EMERGENCY LIGHT BA TTERY PACK. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002102800149 20021028 00149 SO 2002 10 28 SWIA200211259 1 20020830 A 5411 FRAME EMB 120 EMB120ER 3260203 SO NR 2 NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 295UX 120295 RT ENGINE FRAME NR 1 CRACKED AT OB TORSION MOUNT WEB. DISCOVERED DURING C-CHECK, C/W SB 120-54-0036 PART 11 FRAME ONE R EPLACEMENT. 2 L 7 2 4T RT A31SO 2002102800150 20021028 00150 EA 2002 10 28 SWIA200211260 1 20020924 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE T/E FLAP FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 441SW 7602 FLAPS FAIL MESSAGE DURING CLIMBOUT. RETURNED TO FIELD. RIGHT BPSU REMOVED DUE TO FLAPS FAIL MSG. INSTALLED A SERVICEA BLE BPSU IAW CRJ MM 27-51-10. 2 L 7 2 4F 4 F RT A21EA E15NE 2002102800151 20021028 00151 2002 10 28 SWIA200211261 4 20020920 A 2211 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT SYS MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 223SW 5186 5186 120291 AUTOPILOT AND TRIM FAILURE MAP LIGHTS ILLUMINATED ON TAKE OFF ROLL. ABORTED TAKE OFF. INSTALLED SERVICEABLE FO'S A/P C OMPUTER. AUTO PILOT SELF DIAGNOSTIC AND OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002102800152 20021028 00152 EA 2002 10 28 SWIA200211262 1 20020921 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB FAILED A SWIA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 NM 07 910SW 312 312 7566 STAB CH 1 INOP. WOULD NOT RESET.REMOVED AND REPLACED STAB HSTA ACTUATOR IAW CRJ MM 27-42-01. OPS CHECK GOOD. ALSO REM OVED AND REPLACED STAB MOTOR CONTROL UNIT IAW CRJ MM 27-42-05. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002102800153 20021028 00153 SO 2002 10 28 SWIA200211263 1 20020924 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 189SW 120048 ABORTED TAKEOFF IN SGU DUE TO ''HI-SPEED'' AURAL WARNING AND TRIPLE CHIME. HOOKED UP PITOT STATIC TEST BOX. RAN UP AIR SPEED SEVERAL TIMES TO 270 KNOTS. HIGH SPEED AURAL WARNING CHECK NORMAL WITH NO FURTHER DISCREPANCIES. UNABLE TO DUPLI CATE DISCREPANCY. 2 L 7 2 4T RT A31SO 2002102800154 20021028 00154 SO 2002 10 28 SWIA200211264 1 20020926 A 2740 CONNECTOR EMB 120 EMB120ER 3260203 SO PROX SWITCH CORRODED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 251YV 120251 TRIM AURAL WARNING SOUNDED ON TO WHEN TRIM WAS SET AT 20 PERCENT - 30 PERCENT. FOUND CORROSION ON ALL SIX PROX SWITCH C ONNECTIONS. INSTALLED 6 NEW ENVIRONMENTAL SPLICES IAW 20-00-00. SYSTEM OPS CHECK GOOD IAW 27-00-00. 2 L 7 2 4T RT A31SO 2002102800155 20021028 00155 EA 2002 10 28 SWIA200211265 1 20020926 A 2760 4916405 ECU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILER MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 07 432SW 2879 2879 7548 SPOILERON FAULT STATUS MESSAGE. REMOVED NR 1 & NR 2 SECU'S AND REPLACED WITH SERVICEABLE ONES IAW CL600 MM 27-61-05. R EMOVED LEFT INBOARD FLIGHT SPOILER PCU & REPLACED WITH SERVICEABLE ONE IAW CL600 MM 27-62-01. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002102800156 20021028 00156 EA 2002 10 28 SWIA200211266 1 20020928 A 5524 BUSHING CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR WORN A SWIA A UNSCHED LANDING F E FLT CONT AFFECTED VIBRATION/BUFFET CL CLIMB 1 NM 07 591SW 7079 PILOT REPORTS OSCILLATIONS ON CLIMB AND IN THE PITCH AT AIR SPEED OF 284 KTS TO 290 KTS. REMOVED & REPLACED HARDWARE & BUSHINGS ON ALL 6 ELEVATOR PCU'S ROD END SIDE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002102800157 20021028 00157 SO 2002 10 28 SWIA200211268 1 20020929 A 2913 63163 PUMP EMB 120 EMB120ER 3260203 SO LT ENGINE FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 232SW 120306 GREEN SYSTEM MAIN HYDRAULIC PUMP FAILED ON TAKEOFF. ELECTRONIC PUMP TOOK OVER. COMPLIED WITH QRH. RETURNED FOR NORMAL LANDING AT SFO. REPLACED LEFT ENGINE MAIN HYDRAULIC PUMP. RAN ENGINE. OPS & LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2002102800158 20021028 00158 2002 10 28 SWIA200211269 4 20021002 A 3454 6222506006 INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 584SW 5905 5905 120352 ABORTED TAKEOFF DUE TO A RED FLAG ON THE FIRST OFFICER'S RMI. RETURNED TO THE GATE. REMOVED AND REPLACED FO'S RMI IAW 34-26-01. OPS CHECK GOOD IAW MM 34-21-00 AND USED NAV 402 TEST SET TO VERIFY VOR STATION INDICATION. 2 L 7 2 4T RT A31SO 2002102800159 20021028 00159 WP 2002 10 28 UPS02839535 1 20020918 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SP ANGLE IS CRACKED ON COCKPIT SUBFLOOR STA -100 AT RBL 32. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5616101, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102800160 20021028 00160 NM 2002 10 28 UPS02439732 1 20020927 A 5320 FORGING BOEING 747 747SR46 1384816 NM BULKHEAD CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C CORROSION REVEALED ON RT BS 1241 BULKHEAD FORGING AT UPPER KICK FITTING ATTACH FASTENER HOLE BY APPRO X 0.030" DEEP AS PER ATTACH FIGURE. R/H BS 1241 B/H KICK FTG ATTACH FORGING UPPER HOLE REPAIRED AS PER HX RS R-53-43 -34916 & UPS EO B747-5310-17698-A. NOTE : L/R BS 1241 FAILSAFE STRAP IS TO BE INSPECTED PER SB 747-53-2283 'CRACK SAFE' PROCEDURE EVERY 3000 FLIGHTS. THE SPLICE STRAPS & SOLID FILLERS REQUIRED TO CHANGE WITHIN 2 YEARS. 2 L 7 4 4F RT A20WE 2002102800161 20021028 00161 NM 2002 10 28 UPS02439733 1 20020927 A 5320 FORGING BOEING 747 747SR46 1384816 NM BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C CRACK FOUND ON LT BS 1241 BULKHEAD FORGING AT LWR KICK FITTING FASTENER HOLE BY APPROX 0.050" LONG RU NNING AT FWD DIRECTION. LH BS 1241 BULKHEAD KICK FTG ATTACH FORGING LOWER BOLT HOLE REPAIRED AS PER HX RS R-53-43-34 916 & UPS EO B747-5310-17698-A. NOTE : L/R BS 1241 FAILSAFE STRAP TO BE INSPECTED PER SB 747-53-2283 'CRACKED STRAP' PRO CEDURE EVERY 3000 FLIGHTS. THE SPLICE STRAPS & SOLID FILLERS TO CHANGE WITHIN 2 YEARS. 2 L 7 4 4F RT A20WE 2002102800162 20021028 00162 NM 2002 10 28 UPS02439734 1 20020921 A 5310 BEAM BOEING 747 747SR46 1384816 NM NLGWW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C NOSE WHEEL WELL BODY STRUCTURE CRACK FOUND AT R/H VERTICAL BEAM STAND-OFF HOLE AT BS 300 BETWEEN #5 & #6 VERTICAL BEAM CLIP (COUNT FROM LOWER) REFER FIGURE ATTACHED. VERTICAL BEAM WEB REPLACED PER SRM 51-10-01 P.8. 2 L 7 4 4F RT A20WE 2002102800163 20021028 00163 NM 2002 10 28 UPS02439735 1 20020916 A 5710 STRUCTURE BOEING 747 747SR46 1384816 NM RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C RT WING LE CAVITY FRONT SPAR LOWER CHORD VERTICAL FLANGE THICKNESS FOUND BLENDED PREVIOUSLY AT OLES 1 322, PLS CHK LIMITATION. (20 INCHES O/B WING JACK AREA) RT WING L/E FRONT SPAR LWR CHORD VERTICAL FLANGE AT OLES 132 2 IS REPAIRED AS PER HX RS R-57-21-34917. (UPS AUTH # 747-57-20036) 2 L 7 4 4F RT A20WE 2002102800164 20021028 00164 NM 2002 10 28 UPS02439772 1 20021016 A 3350 LIGHT BOEING 747 747121 1384871 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:ASV FORWARD L1 DOOR EMERGENCY LIGHT "L1853" INOP. RELAMPED L1 DOOR FORWARD EMERGENCY LIGHT OPS CHECK S GOOD 2 L 7 4 4F A20WE 2002102800165 20021028 00165 NM 2002 10 28 UPS02439795 1 20021017 A 3350 LIGHT BOEING 747 747200 1384847 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: ASV EMERGENCY LIGHT ON UPPER DECK ABOVE STAIRS INOP. RELAMPED OPS CHECKED GOOD. 2 L 7 4 4F RT A20WE 2002102800166 20021028 00166 NM 2002 10 28 UPS02439802 1 20021017 A 3350 LIGHT BOEING 747 747200 1384847 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE:N/A MAIN CARGO DECK CEILING EMERGENCY LIGHT JUST OUTBD OF FWD ENTRY INOP ALSO FWD DOOR FRAME EMERG LIGH T INOP REMOVED AND REPLACED LT ASSY PER AMM33-51-04 AND RELAMPED LIGHT OPS CHECKS GOOD. 2 L 7 4 4F RT A20WE 2002102800167 20021028 00167 NM 2002 10 28 AWXA200200902 1 20020919 A 3411 856AE15 PROBE BOEING 737 737277 1384570 NM PITOT/STATIC SYS INOPERATIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 186AW 22653 PHX - AIR TURN BACK - FLT 0164 - DURING TAKEOFF FROM PHX EN ROUTE FOR SAT THE CAPTAINS NR 1 AUX PITOT STATIC LIGHT ILLUM INATED AND REMAINED ON. DUE TO CONDITIONS AT SAT THE AIRCRAFT TURNED BACK TO PHX. MAINTENANCE REMOVED AND REPLACED THE LOWER RT PITOT STATIC PROBE IAW 34-11-11, LEAK AND HEAT CHECK WERE ACCOMPLISHED IAW T/C A1B34027. 2 L 7 2 4F RT A16WE 2002102800168 20021028 00168 EU 2002 10 28 AWXA200200904 1 20020916 A 5210 FE240221001 DAMPER AIRBUS 320 A320232 3930326 EU R2 DOOR LEAKING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 642AW 584 MCN - EMERGENCY EVACUATION - DURING C-05 CHECK THE R2 DOOR DAMPER WAS FOUND TO LEAK INTERNALLY. MAINTENANCE REMOVED AND REPLACED THE R2 DOOR DAMPER DIAPHRAGM IAW AMM 52-10-00-020-053. DAMPER WAS SERVICED AND LEAK CHECKED GOOD. 2 L 7 2 4F RT A28NM 2002102800169 20021028 00169 NM 2002 10 28 UPS02439803 1 20021018 A 3350 SIGN BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 676UP 20101 EMERGENCY EXIT SIGN ABOVE RT UPPER DOOR INOP REMOVED AND REPLACED LIGHT ASSY 2 L 7 4 4F A20WE 2002102800170 20021028 00170 NM 2002 10 28 UPS02439805 1 20021022 A 3350 BATTERY PACK BOEING 747 747200 1384847 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: ASE UPPER DECK EMERGENCY EXIT DOOR SILL WOULD NOT ILLUMINATE DURING ASE CHECK REPLACED EMERGENCY LI GHT BATTERY PACK REF MM 33-51-04. LIGHT OPS CHECK GOOD. 2 L 7 4 4F RT A20WE 2002102800171 20021028 00171 NM 2002 10 28 AWXA200200905 1 20020922 A 3350 100865 POWER SUPPLY BOEING 757 7572S7 1384962 NM CABIN DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 PHX - EEL - DURING INSPECTION THE EMERGENCY EXIT LIGHT OVER R1 DOOR WAS FOUND TO COME ON INTERMITTENTLY. MAINTENANCE R EMOVED AND REPLACED THE BATTERY PACK, POWER SUPPLY, AND R1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY IAW BMM 33-51-07 AND BMM 3 3-51-01, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002102800172 20021028 00172 NM 2002 10 28 UPS02439806 1 20021021 A 3350 LIGHT BOEING 747 747123F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 671UP 20323 EMERGENCY EXIT LIGHTS IN UPPER DECK DOOR FRAME INOPERATIVE. RELAMPED OPS CK NORMAL 2 L 7 4 4F A20WE 2002102800173 20021028 00173 NM 2002 10 28 AWXA200200906 1 20020920 A 3350 20131A BATTERY PACK BOEING 757 7572S7 1384962 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 903AW 23323 PHX - EEL - DURING INSPECTION THE TWO EMERGENCY OVERHEAD LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. MAINTENANC E REMOVED AND REPLACED BATTERY PACK , OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002102800174 20021028 00174 NM 2002 10 28 UPS02639799 1 20021020 A 5347 SEAT TRACK BOEING 767 767300 1385204 NM CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 316UP 27744 BROKEN SEAT TRACK ***SUPPLEMENTAL MRR*** REMOVED AND REPLACED FLOORBOARDS PART NUMBER 457T4115-2 2 L 7 2 4F RT A1NM 2002102800175 20021028 00175 NM 2002 10 28 AWXA200200907 1 20020921 A 2560 P4010021 BATTERY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 189AW 22656 LAS - EMERGENCY EQUIPMENT - DURING INSPECTION THE AFT GALLEY EMERGENCY FLASHLIGHT WAS FOUND BLINKING. MAINTENANCE REPLA CED THE BATTERY IN THE AFT GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002102800176 20021028 00176 EU 2002 10 28 AWXA200200908 1 20020921 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 644AW 6562 317 PHX - EEL - DURING TEST OF EMERGENCY LIGHTING SYSTEM THE TEST FAILED. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (12WL) IAW AMM 33-51-38, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002102800177 20021028 00177 EU 2002 10 28 AWXA200200909 1 20020922 A 2560 P20700012015 FLASHLIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 098 SEA - EMERGENCY EQUIPMENT - DURING INSPECTION THE EMERGENCY FLASHLIGHT NEAR L2 DOOR FLIGHT ATTENDANTS SEAT WAS FOUND INO PERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT NEAR L2 DOOR FLIGHT ATTENDANTS SEAT, OPERATIONAL CH ECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002102800178 20021028 00178 EU 2002 10 28 AWXA200200910 1 20020922 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 663AW 5368 1419 LAS - EEL - TEST OF EMERGENCY LIGHTING SYSTEM FAILED. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNITS 10W L & 13WL, AND BATTERY PACKS IAW AMM 33-51-38-420, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002102800179 20021028 00179 NM 2002 10 28 AWXA200200911 1 20020922 A 2560 P4010021 BATTERY BOEING 737 7373S3 1384711 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 28 316AW 23713 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THAT A EMERGENCY FLASHLIGHT WAS INOPERATIVE IN THE CABIN. MAINTENANCE REPLACED THE BATTERY IN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002102800180 20021028 00180 NM 2002 10 28 AWXA200200912 1 20020923 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN MALFUNCTIONED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 814AW 7816 1281 LAS - EEL - EMERGENCY POWER SUPPLY UNIT INDICATED LOAD MESSAGE ON FORWARD FLIGHT ATTENDANT PANEL AFTER EMERGENCY LIGHT T EST. MAINTENANCE REMOVED AND REPLACED FORWARD LT EMERGENCY POWER SUPPLY UNIT (11WL) IAW AMM 33-51-38-401, OPERATIONAL C HECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002102800181 20021028 00181 EU 2002 10 28 AWXA200200913 1 20020923 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 638AW 29623 455 PHX - EEL - EMERGENCY LIGHT SYSTEM FAILED TEST. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS AND EMERGENCY POWER SUPP LY UNITS (11WL) & (13WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002102800182 20021028 00182 WP 2002 10 28 UPS02839248 1 20020831 A 5740 J06009522 FITTING DOUG DC8 DC873F 302199F WP RH WING ROOT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 CRACK IN STEEL STRAP UNDER R/T ADF PNL. MILLED STEEL STRAP UNDER RT ADF (FWD) PANEL CRACKED AT STA 82.7 WHERE WING MEETS CENTER TANK BUT T L7ORT VERIFIED WITH EDDY CURRENT (SKI FITTING). R&R'D FITTING IAW DWG J060095 SRM 51-1-20D, 51-1-2 1,51-3-0 & 53-1-0. C/W WITH D244478.REF N/R 591533. 2 L 7 4 4F RT 4A25 2002102800183 20021028 00183 EU 2002 10 28 AWXA200200914 1 20020923 A 2612 FIRE WARNING AIRBUS 320 A320231 3930325 EU COCKPIT FALSE INDICATION A AWXA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 WP 28 636AW 098 ORD - FIRE WARNING INDICATION - FLT 0728 - AFTER ARRIVING AT THE GATE IN ORD AS ENGINES WERE BEING SHUTDOWN AND THE CARG O DOORS OPENED, RECEIVED A ECAM FIRE WARNING INDICATION FOR THE FORWARD CARGO COMPARTMENT. DISCHARGED THE FORWARD CARGO FIRE BOTTLE PER ECAM INSTRUCTION. MAINTENANCE TROUBLESHOT THE CARGO FIRE WARNING SYSTEM AND FOUND NO DEFECTS. 2 L 7 2 4F RT A28NM 2002102800184 20021028 00184 WP 2002 10 28 UPS02839536 1 20020917 A 5340 4646309501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: SP STA. 934 FITTING IS CRACKED CENTERLINE BETWEEN MAIN GEAR DOORS REMOVED AND REPLACED FITTING I.A .W. DWG. 4646309,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2002102800185 20021028 00185 WP 2002 10 28 UPS02839537 1 20020917 A 5340 4645516501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: SP STA. 954 FITTING IS CRACKED CENTERLINE BETWEEN MAIN GEAR DOORS REMOVED AND REPLACED FITTING I.A. W. DWG. 4645516,AND SRM.51-1-20D 2 L 7 4 4F RT 4A25 2002102800186 20021028 00186 WP 2002 10 28 UPS02839547 1 20020917 A 5340 FITTING DOUG DC8 DC873F 302199F WP MGL WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SPV R/H WHEEL WELL TRAP FITTING CRACKED AT FWD LWR BOLT HOLES,AT STA 855 RT. REMOVED STIFFNER, HFEC I NSPECTED, VERIFIED TWO EACH CRACKS IN LWR TRAP FITTING, STOP DRILLED CRACKS I.A.W E.O. DC8-57-20059, AND SK 894-566,CRAC KS TERMINATE AT STOP DRILL I.A.W HFEC INSP.NDTSPM 06- 10-01.001, FABRICTED REPAIR ANGLE AND STIFFNER I.A.W SK894-566. IN STALLED REPAIR PARTS PER SRM 57-2-7, AND SK 894-566 AT ST 855-R 2 L 7 4 4F RT 4A25 2002102800187 20021028 00187 NM 2002 10 28 CALA0200506 1 20021025 A 3800 61482 BALLAST BOEING 737 7373T0 1384582 NM A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 09 12327 23457 SMOKE IN AFT LAVATORY. LEFT AFT LAVATORY MIRROR CIRCUIT BREAKER OUT. FOUND BREAKER FOR LIGHTS POPPED. BALLAST BURNT. R EMOVED AND REPLACED BALLAST. 2 L 7 2 4F RT A16WE 2002102800188 20021028 00188 NM 2002 10 28 CALA0200507 1 20021025 A 3200 MS250112 SWITCH BOEING 737 737924 13848A1 NM A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 71411 30128 AFTER TAKE OFF, ALL THREE GEAR WOULD NOT RETRACT. HAD THREE GREEN LIGHTS AND THREE RED LIGHTS WITH THE GEAR HANDLE UP. R EPLACED SWITCH PER MM 32-34-11, 820-801. SWUNG GEAR SEVEAL TIMES. 2 L 7 4 4F RT A16WE 2002102800189 20021028 00189 NM 2002 10 28 CALA0200509 1 20021027 A 5310 BAC1498139 STRINGER BOEING 737 7373T0 1384582 NM A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 39343 23581 CRACK IN STRINGER 16R FORWARD OF LIGHT AT APPROXIMATELY 500B. INSTALLED NEW STRINGER AND DOUBLER PER SRM 53-00-03. 2 L 7 2 4F RT A16WE 2002102800190 20021028 00190 NM 2002 10 28 CALA0200510 1 20021028 A 5310 6545834260 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 14336 23574 MAIN CABIN FLOOR SUPPORT HAS CORROSION BETWEEN 312-328 AT LBL 11. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002102800191 20021028 00191 WP 2002 10 28 UPS02839562 1 20020917 A 5340 FITTING DOUG DC8 DC871F 302199D WP FS 1170 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 AFT PIT STA 1170 BY LONG 33 RT FITTING CRACKED. REMOVED OLD FITTING. LOCATED & DRILLED IAW DC8 SRM 51-1-24. INSTALLE D (2) NEW FITTINGS IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002102800192 20021028 00192 WP 2002 10 28 UPS02839563 1 20020918 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 DOUBLER REPAIR 744-2R-03 STA 328 TO 338 LONG 32R CLASSIFIED AS REMOVED DOUBLER. FABBED DOUBLER AN D FILLERS IAW DC8 SRM 53-2-0. ALOD INED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 S RM 53-2-0 2 L 7 4 4F RT 4A25 2002102800193 20021028 00193 NM 2002 10 28 AWXA200200915 1 20020923 A 2560 P4010021 BATTERY BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 332AW 23384 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT EMERGENCY FLASHLIGHT INDICATOR LIGHT WAS NOT FLASHING. MAINTEN ANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002102800194 20021028 00194 WP 2002 10 28 UPS02839564 1 20020919 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 MAIN CABIN L8R CRACKED AT FS 280, 320, 340. REMOVED CRACKED LONG SECTION AT L8R FS 280-340, LOCATED AND DRILLED LONG AND SPLICE IAW DC8 SRM 51-1-247, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED LONG AND SPLICE IAW DC8 SR M 51-1-21 2 L 7 4 4F RT 4A25 2002102800195 20021028 00195 NM 2002 10 28 AWXA200200917 1 20020925 A 2497 6133344501 WIRE HARNESS BOEING 737 7373G7 1384595 NM GENERATOR SYS BURNED A AWXA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 WP 28 158AW 23780 PHX - AIR TURN BACK - FLT 0496 - ON CLIMB OUT OF PHX EN ROUTE FOR DEN THE FIRST OFFICERS FORWARD PANEL LIGHTS AND CENTER CONSOLE LIGHTS DIMMED, THEN HEARD TRANSFORMER RECTIFIER CIRCUIT BREAKERS POP, AT THIS TIME THE NR 2 GENERATOR DROPPED O FF LINE. APU CONNECTED TO NR 2 GENERATOR BUS OK, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE TROU BLESHOT AND FOUND THE NR 2 GENERATOR FEEDER CABLE BADLY BURNED. REMOVED AND REPLACED NR 2 GENERATOR FEEDER CABLE PER BM M 20-61-19. 2 L 7 2 4F RT A16WE 2002102800196 20021028 00196 WP 2002 10 28 UPS02839565 1 20020919 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 MAIN CABIN L9R CRACKED AT FS 340 REMOVED CRACKED LONG SECT AT L9R FS 340, LOCATED AND DRILLED LON G AN D SPLICE (PART# DC9-53B-009-3) IAW DC8 SRM 51-1-24, ALODINED AND PRI MED IAW DC8 SRM 51-1-8, INSTALLED LONG AND SPL ICE IAW DC8 SRM 51-1-2 1 2 L 7 4 4F RT 4A25 2002102800197 20021028 00197 NM 2002 10 28 AWXA200200918 1 20020907 A 5330 6545765725 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A .125 INCH CRACK WAS FOUND ON SKIN AT TEAR STRAP AFT, BS 420, STR 10 RT, CONFIRM ED HFEC INSPECTION. MAINTENANCE CUTOUT DAMAGE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED 2 EACH REPAIR DOUBLERS AND FILLERS, AND INSTALLED REPAIR PARTS IAW B737-200 SRM 53-30-3. 2 L 7 2 4F RT A16WE 2002102800198 20021028 00198 WP 2002 10 28 UPS02839566 1 20020920 A 5210 NPN DOUBLER DOUG DC8 DC871F 302199D WP R2 DOOR WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1 R2 DOOR FRAME AT FS 1650 AT L17R DOUBLER ON FRAME IS WORN AND CHAFFED AT RADIUS. REMOVED AND REP LACED DOUBLER IAW DAC DWG 5615700 2 L 7 4 4F RT 4A25 2002102800199 20021028 00199 WP 2002 10 28 UPS02839567 1 20020920 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 MAIN CABIN AT STA 704 STR 17L INTERCOSTAL CRACKED. ROUTED OUT DAMAGE AND FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 H EAT TREATED TO BE IAW TPS-1003. FABRICATED, LOCATED, AND DRILLED IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 INSTALLED FA STENERS IAW DC8 SRM 51-1-21D 2 L 7 4 4F RT 4A25 2002102800200 20021028 00200 WP 2002 10 28 UPS02839569 1 20020927 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 HOLES FOR LOCK PINS WORN OUT OF ACCEPTABLE LIMITS IAW DC8 SRM 53-2-3 HOLES FOUND TO BE ELONGATED BEYOND LIMITS OF DC8 SRM 53-2-3 REMOVED WORN SEAT TRACK IAW DC8 SRM 51-3-0 DRILLED NEW SEAT TRACK IAW DC8 SR M 51-1-24 I NSTALLED NEW SEAT TRACK IAW DC8 SRM 51-3-0 2 L 7 4 4F RT 4A25 2002102800201 20021028 00201 NM 2002 10 28 AWXA200200924 1 20020905 A 5230 6546921530 SKIN BOEING 737 737301 1384611 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK A .3125 INCH CRACK WAS FOUND ON THE INNER SKIN OF THE FORWARD CARGO COMPARTMENT D OOR AT LIGHTNING HOLE WHERE THE CABLE ENTERS THE DOOR. MAINTENANCE REMOVED DAMAGED SKIN, FABRICATED A REPAIR DOUBLER, A ND INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13. 2 L 7 2 4F RT A16WE 2002102800202 20021028 00202 EA 2002 10 28 COMA0260610 1 20021025 A 4910 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP SMOKE A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 964CA 13742 7129 FLIGHT 5426 SMOKE TOILET CAUTION MESSAGE.REPLACED THE APU. 2 L 7 2 4F RT A21EA 2002102800203 20021028 00203 NM 2002 10 28 AWXA200200928 1 20020906 A 5210 507945165 SKIN BOEING 737 737301 1384611 NM L1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK 2 EACH CRACKS WERE FOUND ON THE L1 DOOR INNER SKIN 24 INCHES FROM BOTTOM AFT EDGE OF DOOR STOP ACCESS HOLE, BS 318. MAINTENANCE CUTOUT CRACKS, PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FAB RICATED 2 EACH PLATES, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13. 2 L 7 2 4F RT A16WE 2002102800204 20021028 00204 EA 2002 10 28 COMA0260609 1 20021026 A 3241 WIRE CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J S WARNING INDICATION AFFECT SYSTEMS TO TAKEOFF 1 SO 01 932CA 7038 FLIGHT 5625 T/O ABORTED DUE TO ANTI SKID CAUTION MESSAGE.REPAIRED DEFECTIVE WIRE CONNECTION AT THE R/H OUTBD WHEEL SPEED TRANSDUCER 2 L 7 2 4F RT A21EA 2002102800205 20021028 00205 EU 2002 10 28 AWXA200200929 1 20020926 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN FAULTY A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 643AW 14281 315 LAS - EEL - DURING TEST OF EMERGENCY LIGHTS RECEIVED A "INT LOADS FWD L FAULT". MAINTENANCE REMOVED AND REPLACED THE FO RWARD LT EMERGENCY POWER SUPPLY UNIT (10WL) IAW AMM 33-51-38-401. 2 L 7 2 4F RT A28NM 2002102800206 20021028 00206 WP 2002 10 28 UPS02839570 1 20020917 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 AFT PIT STA 1180 BY LONG 28 AND 27L FITTING IS CRACKED REMOVED CRACKED FITTING, RECIEVED NEW FITT ING P/N 3755842-505N. FABB ED REPAIR ANGLES IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 5 1-1-8. INSTALLED IAW DC8 SRM 51-1-20D. SEALED IAW DC8 SRM 51-1-17 & 51-1-14 2 L 7 4 4F RT 4A25 2002102800207 20021028 00207 SO 2002 10 28 C2XA02CL182 1 20020908 A 3350 66367 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 25504 145186 CLE FLIGHT NR 3082, THE CREW REPORTED THE 2ND AND 3RD EMERGENCY FLOOR AISLE LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR LIGHT STRIPS. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002102800208 20021028 00208 WP 2002 10 28 UPS02839571 1 20020918 A 5340 FITTING DOUG DC8 DC871F 302199D WP DOOR WA7 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 LT AFT ENT DOOR FWD UPPER CORNER INNER FITTING CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D LOCATE D AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 INSTALLED FITTING IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002102800209 20021028 00209 SO 2002 10 28 C2XA02CL183 1 20020912 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 14920 145380 CLE FLIGHT NR 3027 THE CREW REPORTED THE EXIT LIGHT WAS INOPERATIVE ON THE GALLEY DOOR. MAINTENANCE INSPECTED AND RESEC URED THE LOOSE CONNECTOR ON THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002102800210 20021028 00210 EA 2002 10 28 COMA0260608 1 20021025 A 3241 T3K1209355 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA R/H MLG BROKEN A COMA C ABORTED TAKEOFF J S WARNING INDICATION AFFECT SYSTEMS TO TAKEOFF 1 SO 01 932CA 7038 FLIGHT 5537 ANTI SKID INOP MESSAGE DURING T/O.REPLACED THE WIRING CONNECTOR AT THE R/H OUTBD WHEEL SPEED TRANSDUCER. 2 L 7 2 4F RT A21EA 2002102800212 20021028 00212 WP 2002 10 28 UPS02839572 1 20020919 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 MAIN CABIN L 10 RT END FITTING CRACKED AT FS 680 REMOVED FITTING IAW DC8 SRM 51-1-20D DRILLED NEW FITTING IAW DC8 SRM 51-1-20D. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. INSTALLED PLI WASHER AND TIGHTENED PLI WASH ER IAW DC8 SRM 51-1-23 2 L 7 4 4F RT 4A25 2002102800213 20021028 00213 SO 2002 10 28 C2XA02CL189 1 20020925 A 2133 2099L011100 OUTFLOW VALVE EMB 145 EMB145LR 3260212 SO CABIN PRESSURE LEAKING A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 14923 5071 145318 CLE FLIGHT NR 3219 THE CREW REPORTED DURING CLIMBOUT THE AIRCRAFT PRESSURIZATION SURGED, CABIN RATE WENT FROM 1750 TO 18 00. RESET TO MANUAL AND LOST CABIN ALTITUDE INDICATION. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT INCIDENT . MAINTENANCE FOUND THE PNEUMATIC OUTFLOW VALVE WAS LEAKING. THE OUTFLOW VALVE WAS REPLACED AND OPERATIONAL CHECKS WER E GOOD. 2 L 7 2 4T RT T00011AT 2002102800214 20021028 00214 EA 2002 10 28 COMA0260607 1 20021026 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 804CA 20318 7352 FLIGHT 5340 ALL EMERGENCY LIGHTS ARE INOP.REPLACED EMERGENCY BATTERIES. 2 L 7 2 4F RT A21EA 2002102800217 20021028 00217 WP 2002 10 28 UPS02839573 1 20020920 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 MAIN CABIN BATHTUB FITTING CRACKED AT BS 678, L2L. REMOVED FITTING IAW DC8 SRM 51-1-20D, DRILLED NEW FITTING IAW DC8 SR M 51-1-20D. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. INSTALLED AN D TIGHTENED PLI WASHER IAW DC8 SRM 51-1-23 2 L 7 4 4F RT 4A25 2002102800218 20021028 00218 SO 2002 10 28 C2XA02SH064 1 20020910 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 SHV-DURING C CHECK CENTER ISLE CARBON FIBER BEAM WAS FOUND TO HAVE CORROSION UNDER IT LEFT OUTBOUND SIDE. MAINTENANCE R EPAIRED DAMAGED AREA IAW EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002102800219 20021028 00219 SO 2002 10 28 GLBA2002151 1 20020920 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN MISSING A GLBA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 03 96ZK 120096 EMERGENCY LIGHT MISSING ROW 9 LT SIDE, NO DEFECTS NOTED 2 L 7 2 4T RT A31SO 2002102800220 20021028 00220 EU 2002 10 28 02FDEA00773 1 20020928 A 2700 ATTACH FITTING AIRBUS 310 A310 EU SPOILER ACTUATOR BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 450FE 162 #4 RH SPOILER ACTUATOR ATTACH FITTING IS BROKEN. FWD I/B SIDE OF FITTING IS MISSING. ** S/D ** COMING 2 L 7 2 4F RT A35EU 2002102800221 20021028 00221 WP 2002 10 28 UPS02839574 1 20020920 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 MAIN CABIN BATHTUB FITTING CRACKED AT BS 851 L9R REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-2 0D 2 L 7 4 4F RT 4A25 2002102800223 20021028 00223 WP 2002 10 28 UPS02839575 1 20020920 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 MAIN CABIN BATHTUB FITTING CRACKED AT B S 851 L8R REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-2 0D 2 L 7 4 4F RT 4A25 2002102800224 20021028 00224 NE 2002 10 28 GLBA2002154 3 20020925 A 6140 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE COCKPIT MALFUNCTIONED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 96ZK 120096 AUTO FEATHER ANNUNCIATOR ILLUMINATED ON T/O ROLL, PERFORMED AUTO TEST WITH NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 6 C P11NE 2002102800225 20021028 00225 EU 2002 10 28 MALA020578 1 20020916 A 5522 SKIN BAC 146 AVRO146RJ85A 1500097 EU ELEVATOR DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING LIGHTENING STRIKE IN MSP, LT ELEVATOR DAMAGED AT UPPER SKIN SURFACE AT THE OUTBOARD TRAILING EDGE NEAR THE TIP. MAINTENANCE REPAIRED DAMAGE IAW EO A55019 AND SRM 55-20-11 201 FIG 206. 2 H 7 4 4F RT A49EU 2002102800226 20021028 00226 EU 2002 10 28 MALA020579 1 20020824 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C-CHECK IN CVG, NR 4 SEAT TRACK SHOWS CORROSION BEYOND SRM LIMITS IN SEVERAL PLACES. MAINTENANCE REPAIRED IAW EO NR A53026 AND SRM 53-00-32. 2 H 7 4 4F RT A49EU 2002102800227 20021028 00227 EU 2002 10 28 MALA020580 1 20020824 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C-CHECK IN CVG, NR 1 SEAT RAIL SHOWS CORROSION BEYOND SRM LIMITS IN SEVERAL PLACES. DAMAGE REPAIRED IAW EO A 530 26 AND SRM 53-00-32. 2 H 7 4 4F RT A49EU 2002102800228 20021028 00228 EU 2002 10 28 MALA020581 1 20020824 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C-CHECK IN CVG, NR 3 SEAT RAIL SHOWS CORROSION BEYOND SRM LIMITS IN SEVERAL PLACES. MAINTENANCE REPAIRED DAMAGE IAW EO NR A53026 AND SRM 53-00-32. 2 H 7 4 4F RT A49EU 2002102800229 20021028 00229 WP 2002 10 28 UPS02839591 1 20020921 A 5310 GUSSET DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 MAIN CABIN AT STA 759 STR 5R INTERCOSTAL GUSSET CRACKED. REMOVED AND REPLACED GUSSET IAW DC8 SRM 51-1-21 2 L 7 4 4F RT 4A25 2002102800230 20021028 00230 WP 2002 10 28 0203309852 1 20020919 A 5320 BRACKET DOUG DC9 DC951 3022051 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING MCK IN ATL, CRACKS WERE FOUND ON THE LEFT AND RIGHT BRACKETS AT STATION 83 X=+-10. REPAIRED PER EA 98-190725. 2 L 7 2 4F RT A6WE 2002102800231 20021028 00231 WP 2002 10 28 0203369609 1 20021001 A 2612 FIRE LOOP DOUG DC9 DC932 3022066 WP APU SHORTED A NWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 609NW 47234 DURING CLIMBOUT, THE APU FIRE WARNING LIGHT ILLUMINATED. CREW PERFORMED COM PROCEDURES AND DISCHARGED THE FIRE EXTINGUI SHING AGENT FROM THE NR 1 FIRE BOTTLE. FLIGHT RETURNED TO A NORMAL LANDING AT MSP. MAINTENANCE FOUND NO EVIDENCE OF FI RE OR SMOKE. THE APU FIRE DETECTION SYSTEM WAS SHORTING. REPLACED THE APU FIRE DETECTION SYSTEM AND THE NR 1 FIRE BOTT LE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002102800232 20021028 00232 WP 2002 10 28 UPS02839592 1 20020916 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 AIR COND/PRESS COMPT AT FS 56 ABOVE L24R FRAME IS CRACKED AT PNEUMAT IC DUCT STANDOFF ATTACH BRACKET. REMOVED FRAME SECTION FS 56 L24R IAW DC8 SRM 51-1-8, FAB NEW FRAME A ND SPLICES IAW DC8 SRM 53-3-1, ALODINED AND PRIME D IAW DC8 SRM 51-1- 8, INSTALLED FRAME AND SPLICES IAW DC8 SRM 51-1-21, HEAT TREAT FRAME AND SPICE TO 7075-T6 IAW TPS 1 003-REV A 2 L 7 4 4F RT 4A25 2002102800233 20021028 00233 WP 2002 10 28 MWEA020641 1 20021028 A 5310 995575043 STRAP DOUG DC9 DC981 3022081 WP #3 BEAM CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 FORWARD PASSENGER DOOR STRAP DOUBLER IS CRACKED AT #3 DOOR BEAM. -- REMOVED AND REPLACED STRAP. 2 L 7 2 4F A6WE 2002102800234 20021028 00234 WP 2002 10 28 MWEA020642 1 20021028 A 5310 995575D39 INTERCOSTAL DOUG DC9 DC981 3022081 WP #3 & #4 BEAM BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 FORWARD PASSENGER DOOR INTERCOSTAL BETWEEN #3 AND #4 BEAM IS BENT. -- REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F A6WE 2002102800235 20021028 00235 WP 2002 10 28 MWEA020630 1 20021024 A 3230 LANDING GEAR DOUG DC9 DC914 3022034 WP NOSE MALFUNCTIONED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 CREW WAS UNABLE TO RAISE LANDING GEAR. -- FOUND TENSION ON CABLE RUN 116 A & B LOW. PERFORMED STEPS 1-5 OF ADJUSTMENT TEST, SERVICED NOSE STRUT AND REMOVED AND REPLACED LEFT AND RIGHT NOSE TIRE. 2 L 7 2 4F A6WE 2002102800236 20021028 00236 WP 2002 10 28 UPS02839593 1 20020916 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 AIR COND/PRESS COMPT AT FS 56 ABOVE L24L FRAME IS CRACKED REMOVED FRAME AT FS 56 L24L, FAB FRAME AND SPLICES IAW DC8 SRM 53-3- 1, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED FRAME AND SPLIC E IAW DC8 SRM 51-1-21 , FRAME AND SPLICE HEAT TREATED TO 7075-T6 IAW TPS 1003 REV A 2 L 7 4 4F RT 4A25 2002102800237 20021028 00237 WP 2002 10 28 UPS02839594 1 20020919 A 5313 561094943 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 MAIN CABIN L8R CRACKED AT FS 120. INSTALLED SPLICE FITTING AND LONGERON IAW DC8 SRM 51-1-20D AND 51 -1- 21 AND DC8 SRM 53-2-2 REPLACE LONG SECTION IAW DAC DWG 5610949, ALOD INED AND PRIMED IAW DC8 SRM 51-1-8 2 L 7 4 4F RT 4A25 2002102800238 20021028 00238 SO 2002 10 28 C2XA02CL211 1 20021025 A 5610 163500112 WINDSHIELD EMB 135 EMB135ER 3260203 SO FORWARD FUSELAGE SHORTED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 25504 145186 CLE FLIGHT#3152 THE CREW REPORTED THE #2 WINDSHIELD WAS ARCING AND REPORTED ELECTRICAL SPARKS .THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE #2 WINDSHIELD AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002102800239 20021028 00239 NM 2002 10 28 ZW0A0210801 1 20021024 A 3350 408822101 BATTERY DOUG MD80 MD83 3023681 NM A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9412W 53187 THE EGRESS LIGHTS WERE INOPERATIVE FROM CABIN ROWS 20 TO 25. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 8-23- 02 STL. --CLOSED-- 2 L 7 2 4F RT 2002102800240 20021028 00240 WP 2002 10 28 ABXA020259 1 20021008 A 5700 3923258504 SUPPORT DOUG DC9 DC941 302207N WP AFT REAR SPAR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 RIGHT WING OUTBOARD SPOILER TORSION BAR SUPPORT FITTING CRACKED AT UPPER END. REPLACED FITTING IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 2002102800241 20021028 00241 WP 2002 10 28 ZW0A0210802 1 20021025 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 110HM 49787 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 20 TO 25. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 3-7-02 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2002102800242 20021028 00242 WP 2002 10 28 ABXA020260 1 20021008 A 5300 39203241 FITTING DOUG DC9 DC941 302207N WP LONGERON 30 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 ANGLE CRACKED AT LONGEON 30 JUST AFT OF FORWARD 'P' DOME, KEEL AREA. REPLACED ANGLE IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002102800243 20021028 00243 WP 2002 10 28 ABXA020261 1 20021008 A 5313 995791757 SPLICE DOUG DC9 DC941 302207N WP AFT CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 LEVEL II CORROSION AT F.S. 1013, LONGERON 27 LEFT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPLACED FRAME SPLICE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002102800244 20021028 00244 WP 2002 10 28 ABXA020262 1 20021009 A 5312 9910073 PANEL DOUG DC9 DC941 302207N WP STA. 89 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 NOSE WHEEL WELL UPPER PRESSURE PANEL STA. 89 LEFT, APPROXIMATELY 3 INCHES INBOARD, HAD CRACK. REPAIRED CRACK IAW REA D95 3-45373. 2 L 7 2 4F A6WE 2002102800245 20021028 00245 WP 2002 10 28 ABXA020263 1 20021009 A 5312 99100733 PANEL DOUG DC9 DC941 302207N WP STA. 110 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 NOSE WHEEL WELL UPPER PRESSURE PANEL HAD CRACK AT STA. 110 LEFT TUNNEL, APPROXIMATELY 24 INCHES INBOARD. REPAIRED PANEL IAW DC-9 SRM 53-01, 51-30-2, 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2002102800246 20021028 00246 WP 2002 10 28 ABXA020264 1 20021009 A 5312 99100733 PANEL DOUG DC9 DC941 302207N WP STA. 110 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 NOSE WHEEL WELL UPPER PRESSURE PANEL HAD CRACK AT STA. 110 RIGHT TUNNEL, APPROXIMATELY 14 INCHES INBOARD. REPAIRED PANEL IAW DC-9 SRM 51-30-2, 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2002102800247 20021028 00247 SO 2002 10 28 C2XA02CL191 1 20021001 A 2120 ODOR EMB 135 EMB135LR 3260305 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 16510 145323 CLE FLIGHT NR 3160 THE CREW REPORTED THE CABIN SMELLS OF FUMES WITH THE APU BLEED ON. MAINTENANCE INSPECTED AND RAN APU WITH BLEED ON AND OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2003030300053 20030303 00053 NM 2003 3 3 SABA020103 1 20021025 A 7920 AS320816 O-RING DHAV DHC8 DHC8102 2809003 NM PCU ADAPTER DAMAGED A SABA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 33 882CC 168 AIRCRAFT 882 ON FLIGHT 5057 FROM CLT TO TLH; AFTER REACHING THE TLH AREA THE NUMBER TWO ENGINE OIL LIGHT ILLUMINATED AND WOULD NOT GO OUT. AIRCREW SHUTDOWN THE ENGINE. AIRCRAFT MANE A SAFE LANDING WITH NO OTHER PROBLEMS. ENGINE DID NOT S TARVE FOR OIL. NO EMERGENCY WAS DECLARED, BUT TOWER DID DEPLOY THE FIRE FIGHTING EQUIPMENT. MAINTENANCE FROM CLT REMOV ED AND REPLACED AN O-RING UNDER THE PCU ADAPTER. ENGINE WAS SERVICED, RUN AND OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002102800248 20021028 00248 NM 2002 10 28 USAA020392 1 20021003 A 5311 FRAME BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 24479 FRAME CRACKED AT BS 827 S8L-S9L AT BIN SUPPORT BRACKET. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102800249 20021028 00249 NM 2002 10 28 USAA020393 1 20021004 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 22957 ANGLE/BEAM BS 616 VERTICAL FLOORBEAM SUPPORT, FORWARD OF RIGHT EMERGENCY EXIT. CUT OUT DAMAGE, INSTALLED FILLER AND DOU BLER IAW TR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102800250 20021028 00250 NM 2002 10 28 USAA020394 1 20021004 A 5330 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 24479 SKIN CRACKED, BS 867 BETWEEN S8L-S9L. INSTALLED DOUBLERS IWA TR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102800251 20021028 00251 NM 2002 10 28 USAA020395 1 20021014 A 5311 FRAME BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 24479 FRAME CRACKED AT STA 827 BETWEEN STR 8R AND 9R. INSTALLED ANGLE DOUBLERS IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102800252 20021028 00252 EU 2002 10 28 USAABA02020 1 20020927 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU PWA 4158 PW4158 NE CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 677UW 0380 EPSU AT L2 DOOR FAILED THE BATTERY TEST. MAINTENANCE REPLACED THE EPSU BATTERY. 2 L 7 2 4F 4 F RT A46NM E24NE 2002102800253 20021028 00253 NM 2002 10 28 USAABB02168 1 20020930 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM GE CF6 CF680 30025 NE CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 651US 24764 FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROW 19 AFT. MAINTENANCE REPLACED THE BATTERY AND BATTERY CHARGER. 2 L 7 2 4F 4 F RT A1NM E13NE 2002102800254 20021028 00254 NM 2002 10 28 USAABB02169 1 20020930 A 3350 20131A BATTERY BOEING 767 7672B7 1385107 NM GE CF6 CF680 30025 NE CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651US 24764 FOUND EXIT LIGHT AT R1/L1 DIM. MAINTENANCE REPLACED THE BATTERIES. 2 L 7 2 4F 4 F RT A1NM E13NE 2002102800255 20021028 00255 NM 2002 10 28 USAABB02174 1 20021011 A 3350 20121 CHARGER BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 647US 23899 FOUND RIGHT OVERWING EXIT LIGHT AND CROSS AISLE LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. 2 L 7 2 4F 4 F RT A1NM E13NE 2002102800256 20021028 00256 NM 2002 10 28 USAASB02187 1 20021014 A 3350 20121 CHARGER BOEING 737 737401 1384701 NM GE CFM56 CFM56* 13802 NE CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 405US 23885 MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEATS 18 DEF THROUGH 20 DEF INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY ABOVE SEAT ROW 20 DEF. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102900001 20021029 00001 NM 2002 10 29 0203522299 1 20021016 A 5330 LAP JOINT BOEING 727 727251 138408H NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 299US 22153 During special visit check found cracks in lap joints at BS 480-680 STR 26L. Repaired per EA 22-184425. 2 L 7 3 4F A3WE 2002102900002 20021029 00002 NM 2002 10 29 0203515528 1 20021022 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 528US 23843 DURING "L" CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 25. REPAIRED PER EA 55-192960. 2 L 7 2 4F RT A2NM 2002102900003 20021029 00003 NM 2002 10 29 UPS02439820 1 20021026 A 2120 ACM BOEING 747 747123 1384873 NM NR 2 ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 674UP 20100 PAC 2 EMITS VIBRATION & ACRID ODOR WHEN ACTIVATED IN FLIGHT. TRANS TO MEL PER 21-1-2-3 PLACARD INSTALLED. M247805 2 L 7 4 4F A20WE 2002102900004 20021029 00004 WP 2002 10 29 UPS02839595 1 20020917 A 5330 NPN DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1 REPAIRS DOUBLER 744-1L-01, 744-1L-03, 744-1L-04 AT BS 36 TO BS 56 LONG 28L TO LONG 30L CAT C & D REP AIRS DUE TO FASTENERS SPACING AND MA TERIAL THICKNESS AND STAINLESS STEEL REPAIR REMOVED (4) DOUBLERS IAW DC8 SRM 51 -3-2, MAT'L ID IAW DAC DWG# SRO B S300-20 DOUBLERS 2024-T3.071 PO# 389651, FILLER 2024-T3.063 PO# 3908 75, FABRICATED DO ULBER & (4) FILLERS IAW REO G08798, ALODINE AND PRI MED IAW DC8 SRM 51-1-8, TRIMMED OUT DAMAGED AREA IAW REO G08798, INS TALLED DOUBLER & (4) FILLERS IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002102900005 20021029 00005 WP 2002 10 29 UPS02839596 1 20020917 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1 AFT PIT STA 1340 TO 1360 LONGERON SPLICE FITTING CRACKED AND CORRODE D BY LONG 32L. REMOVED CRACKE D LONGERON FITTING IAW DC8 SRM 51-1-20D, LOCATED & DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED NEW FITTING IAW DC 8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002102900006 20021029 00006 WP 2002 10 29 UPS02839597 1 20020917 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1 AFT PIT STA 1220 BY LONG 33R FITTING HAS CORROSION INSIDE TORQUE BOX. REMOVED CORROSION IAW DC8 SR M 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC87 SRM 53-2-0 REMOVED TWO FITTINGS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002102900007 20021029 00007 WP 2002 10 29 UPS02839598 1 20020917 A 5330 NPN FITTING DOUG DC8 DC871F 302199D WP STA 1150 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1 AFT PIT FITTING AT SKIN TO FWD END OF C-3 DOOR TORQUE BOX CRACKED, STA 1150 BETWEEN LONGERONS 34 R - 35 R. REMOVED TWO FITTING IAW DC8 SRM 51-1-20D FAB REPAIR DOUBLERS IAW DC8 SRM 53-2-0 ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002102900008 20021029 00008 WP 2002 10 29 UPS02839599 1 20021001 A 3210 LINK DOUG DC8 DC871F 302199D WP RT MLG DOOR OUT OF ADJUST A IPXA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE: AS, DOOR NOT LATCHED LT REMAINED ON FOLLOWING GEAR RETRACTION. RT ALT MAIN GEAR DOOR LIGHT WAS ALSO O N. BOTH LTS EXTINGUISHED WHEN THE GEAR HA NDLE WAS MOVED TO THE UPLATCH CK POS. A/C ARRIVED ON PARKING SPOT WITH RH GEAR DR HANGING DOWN APPROX 2 INCHES. ADJUSTED RT MAIN LANDING GEAR DR ADJUSTABLE LINK PER M/M 32-31-05. GROUND & OPS CK G OOD. 2 L 7 4 4F RT 4A25 2002102900009 20021029 00009 WP 2002 10 29 UPS02839619 1 20021005 A 5230 WEB DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 PIT NR 31 CARGO DOOR WEB CRACKED. AT STA 40, APPROX. 12 INCHES BELOW MAIN DECK FLOOR. REMOVED DAMAGED SECTION OF WEB. T G 35574 10-6-02 FABRICATED & INSTALLED REPLACEMENT SECTION OF WEB PER DC-8 SRM 53-2-0 2 L 7 4 4F RT 4A25 2002102900010 20021029 00010 EA 2002 10 29 CA020917004 2 20020916 A 7250 PT6A34 CASE EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA RT ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 18890 (CAN) DURING ROUTINE MAINTENANCE THE MAINTENANCE CREW NOTICED TWO SMALL CRACKS ON THE RT ENGINE GAS GENERATOR CASE. THES E CRACKS ARE LOCATED AT THE FIRE SEAL MOUNTING ANGLES. THE ENGINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 4T 4 T A21SO E4EA 2002102900011 20021029 00011 NE 2002 10 29 CA020918008 2 20020710 A 7200 ENGINE BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE NACELLE FLAMED OUT W B A EMER. DESCENT UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 CA (CAN) DURING ROUTINE FLIGHT AFTER FUELING FROM A SUPPLIED SEALED DRUM OF PRE-MIXED JET FUEL (FSII) ADDED. THE ENGINE FLA MED OUT AND A FORCED LANDING RESULTING IN NO DAMAGE TO THE HELICOPTER. 1 G 7 1 4U 4 U H1SW E17EA 2002102900012 20021029 00012 NE 2002 10 29 CA020918012 2 20020917 A 7250 ENGINE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE NACELLE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING THE DISASSEMBLY OF THE ENGINE FOR HOT SECTION INSPECTION, AN OIL LEAK WAS DISCOVERED IN THE AREA OF THE 3.5 BEARING. 1 L 7 2 4F 4 F A22CE E1NE 2002102900013 20021029 00013 NE 2002 10 29 CA020923002 2 20020919 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT FAILED W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 CA (CAN) AIRCRAFT 7134 TAT, 15090.5HRS.FLIGHT 5895 FROM CVG TO ROA 'AT APPROX 1500-2000 FT IN CLIMB THERE WAS A LOUD BOOM & YAW FROM THE LT SIDE OF AIRCRAFT. NR 1 ENG ITT WAS 980+. THOUGHT THE ENGINE HAD BEEN DAMAGED & SHUT IT DOWN AFTER 30 S ECS. EVERYTHING ELSE APPEARED TO BE IN THE GREEN EXCEPT ITT. NO RELIGHT ATTEMPTED. DECLARED AN EMERGENCY AND LANDED.'M AINTENANCE CONFIRMED ITT WENT TO 1250. R&R'D ENGINE.(ENGINE INSTALLED ON DEC 31-2000) 2 L 7 2 4F 4 F RT A21EA E15NE 2002102900014 20021029 00014 SW 2002 10 29 CA020923006 1 20020923 A 3210 DARTD26681 SADDLE BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) SADDLE FOUND CRACKED DURING 100 HR INSPECTION. NOTE : TRAINING THE DAY BEFORE SADDEL FOUND CRACKED. 1 G 7 1 3U 3 U H2SW E4CE 2002102900015 20021029 00015 NE 2002 10 29 CA020930002 2 20020904 A 7230 MODULE33 COMPRESSOR BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE ENGINE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 CA (CAN) ON CLIMB A LOUD BANG WAS HEARD FOLLOWED BY A/C YAW. TGT PEAKED AT 1150-DEG C AND ENGINE SPOOL DOWN. A/C RETURNED S AFELY TO FIELD ON ONE ENGINE. ENGINE INSPECTION REVEALED METAL IN TAIL PIPE AND SEIZED LP SYSTEM. FAN AND BOOSTER FOUND OK. INTERROGATION OF THE MCDU RECORDED THE FOLLOWING DND FAULT CODES ON LEG 1, 732178 (P30 AIR TUBE LEAKAGE/BLOCKAGE), 772201 (TURBINE BEARING OVERHEATDETECTED), 772101 (TGT CIRCUIT FAULT CH-A) AND 772102 (TGT CIRCUIT FAULT CH-B) VERBAL RE PORT FROM B OROSCOPE INSPECTION AT AIRLINE REVEALED EXTENSIVE HPC DAMAGE FROM STAGE 2 DOWNWARDS. ENGINE BEING DISMANTLE INTO MODULES AT RRC CONFIRMED CUSTOMER REPORT. HP COMPRESSOR, HP TURBINE AND LP TURBINE MODULE WILL BE RETURNED AS COMPL 2 L 7 2 4F 4 F TR A6WE E00061EN 2002102900016 20021029 00016 NE 2002 10 29 CA020930003 2 20020926 A 7200 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE LEFT FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) PRELIMINARY FROM CUSTOMER REPORT, ENGINE NOT AT RRC YET.WHILE AT CLIMB POWER PASSING THRU FL210 A LOUD POP WAS HEA RD. LT ENGINE OIL PRESSURE WENT TO ZERO. ENGINE RPM REDUCED TO IDLE AND CONTINUE WINDMILL. LEFT ENGINE OIL PRESSURE AND QTY INDICATION WHERE X OUT, ENGINE OIL PRESSURE QTY LO-EAD. METAL FOUND IN JET PIPE, ENGINE REMOVED. DISCUSSION IN PROG RESS FOR ENGINE DELIVERY FOR INVESTIGATION TOROLLS-ROYCE CANADA OR ROLLS-ROYCE DEUTSCHLAND LTD &CO KG. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002102900018 20021029 00018 SW 2002 10 29 CA021001001 1 20020711 A 5210 222031233104 BRACKET BELL 222 222U 1182140 SW LYC LTS101 LTS101750C1 41560 NE CREW DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) RIGHT, LOWER DOOR SUPPORT HINGE FOUND CRACKED AFTER A FLIGHT. IT WAS DISCOVERED THAT A BELL 206 HAD LANDED AT THE BASE SEVERAL DAYS PRIOR, THIS SAME DOOR HAD FLOWN OPEN. CHECKED AFTER INCIDENT BY THE PILOTS BUT NO DAMAGE NOTED. MAY HA VE BEEN THE ULTIMATE CAUSE OF THE 'CRACK'. A SMALL INCIPIENT CRACK HAD BEEN DETECTED SEVERAL MONTHS AGO AND HAD BEEN UND ER OBSERVATION. 1 G 7 2 3U 3 U H9SW E5NE 2002102900019 20021029 00019 SW 2002 10 29 CA021001002 1 20020818 A 6510 205031818001 BEARING BELL 205031818001 BELL 205 205A1 1181414 SW LYC T53 T5317A 41549 NE TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOUND A CRACK (ON A DAILY CHECK) ON THE NR 1 TAILBOOM TAIL ROTOR DRIVE SHAFT BEARING SUPPORT, AS INDICATED IN THE DRAWING SENT. THE SUPPORT POSITIONS THE T/R DRIVE SHAFT BEARING HANGAR. THE T/R BEARING HANGAR IS REMOVED EVERY 6 MONTHS OR 600 HOURS. THIS IS TO INSPECT THE T/R HANGAR COUPLING SPLINES AND REGREASE THE COUPLING. THE T/R HANGAR BEARING SUPP ORT LOOK ORIGINAL. THE AIRFRAME TIME ON THE AIRCRAFT IS 23050.0 HOURS. 1 G 7 1 4U 4 U H1SW E17EA 2002102900021 20021029 00021 SW 2002 10 29 CA021001004 1 20020924 A 5500 BRACKET BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA LT ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) IN THE PROCESS OF DOING A 3000 HOUR INSPECTION ON THE TAILBOOM LEFT HAND ELEVATOR, THE ENGINEER FOUND THE ELEVATO R ATTACHMENT LUG BRACKET CRACKED. THE CRACK WAS ON THE AFT SIDE ATTACHMENT LUG BRACKET B ELOW THE ATTACHMENT LUG, BETWEE N THE 1ST AND 2ND RIVETS OF THE BRACKETS. 1 G 7 1 4U 4 U H4SW E22EA 2002102900022 20021029 00022 GL 2002 10 29 CA021001005 2 20020918 A 7250 6875491 SEAL SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL TURBINE SECTION DAMAGED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CA (CAN) UNSCHEDULED LANDING DUE TO FLUCTUATING OIL PRESSURE AND LOW OIL WARNING LIGHT ON. ENGINE WAS REMOVEDAND REPLACED, TURBINE TEAR DOWN IS IN PROGRESS. ADDITIONAL DETAILS TO FOLLOW. 1 G 7 2 3U 3 U H1NE E1GL 2002102900023 20021029 00023 SW 2002 10 29 CA021001010 1 20020920 A 6510 204040620011 DRIVE SHAFT BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE TAIL ROTOR CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AT TIME OF RE-GREASING THE T/R DRIVESHAFT COUPLINGS. T/R DRIVESHAFT WAS REMOVED FROM TUNNEL UNDER ENGINE. FOUND CO NTACT WAS MADE WITH TUNNEL AT ENTRANCE DIRECTLY AFT OF TRANSMISSION. SHAFT IS OF NEWER STYLE -011 WHICH IS OF A GREATER DIAMETER THAN THAT OF ORIGINAL. CONTACT WAS MADE APPROX 1.5 INCHES INSIDE (AFT) OF THE TUNNEL ENTRANCE MAKING THE DETE CTION VERY DIFFICULT. CONTACT WITH TUNNEL WAS VERY MINIMAL & ONLY PAINT WAS MARKED ONE THIRD AROUND THE DIAMETER OF TH E DRIVESHAFT. DAMAGE WAS NOT IN EXCESS OF LIMITS AND PAINT WAS RE-TOUCHED AND DRIVESHAFT RETURNED TO SERVICE. 1 G 7 1 4U 4 U H1SW E17EA 2002120200025 20021202 00025 NM 2002 12 2 920WA0005 1 20021026 A 3350 BATTERY BOEING 737 737236 1384476 NM EMERGENCY LIGHT DISCHARGED A PIDA O OTHER L NO TEST NR NOT REPORTED 1 SO 05 920WA 21791 EMERGENCY EXIT LIGHTS FLASHING ON & OFF IN ARMED POSITION. LET BATTERIES CHARGE FOR EMERGENCY LIGHTS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002102900025 20021029 00025 CE 2002 10 29 CA021002009 1 20021001 A 5520 115610010125 STRUCTURE BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 15024 (CAN) AFTER FINDING THE SPLINE CRACKED ON AN ELEVATOR THAT WAS DAMAGED FROM HANGAR RASH, INSPECTED THIS ELEVATOR THAT W AS IN THE PARTS DEPARTMENT, THE SPLINE WAS FOUND CRACKED AT SEVERAL LOCATIONS, MOST OF THE CRACKS EXTENDED FROM THE RIV ET HOLE TO THE TRAILING EDGE OF THE SPLINE, A FEW CRACKS EXTENDED FROM THE RIVET HOLE TO THE LEADING EDGE AND TWO HOLES EXTENDED COMPLETELY THROUGH THE SPLINE. APPROXIMATELY 2/3 OF THE HOLES WERE CRACKED. 1 L 7 2 3T 4 T A14CE E4EA 2002102900026 20021029 00026 WP 2002 10 29 CA021002010 1 20020825 A 6520 369D25400 GEARBOX HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL TAIL ROTOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A SCHEDULED 600 HOUR INSPECTION. DAMAGE WAS FOUND ON THE UNDER SIDE OF TAIL ROTOR GEARBOX CASE DUE TO A MI S-ALIGNMENT OF THE T/R PUSH PULL TUBE ADAPTER. DAMAGE WAS APPROXIMATELY .020 DEEP AND UPON INVESTIGATION IT WAS DETERMI NED THAT PIN HAD EXCESSIVE WEAR AT THE ASSEMBLY POINT IN THE T/R GEARBOX HOUSING ITSELF. 1 G 7 1 3U 3 U H3WE E4CE 2002102900027 20021029 00027 NE 2002 10 29 CA021002016 2 20020927 A 7261 453953 LINE BOEING 727 727225 1384077 NM PWA JT8 JT8D9A 52048 NE ENGINE OIL SHEARED W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) ENROUTE YHM-YVR AT FL310, NR 1 ENGINE LOW OIL PRESS LITE ILUMINATED, ZERO OIL QTY AND PRESS OBSERVED. ENGINE SHUT DOWN AND AIRCRAFT LANDED YVR. NR 4 BEARING MAIN OIL SUPPLY LINE FOUND SHEARED. ENGINE REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 2002102900028 20021029 00028 EA 2002 10 29 CA021003005 2 20020916 A 7200 ENGINE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA MCAULY 4HFR34 4HFR34C754 NE RIGHT MAKING METAL W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 12164 (CAN) DURING CRUISE FLIGHT, THE PILOT WAS ALERTED BY A RT ENGINE CHIP LIGHT. THE PILOT SHUTDOWN THE ENGINE AND ARETURNED TO THE AIRPORT. UPON INSPECTION OF THE MAGNETIC CHIP DETECTOR, METAL CONTAMINATION WAS FOUND, ENGINE REMOVED FOR REPAIR . 1 L 7 2 4T 4 T A24CE E4EA 6 C 3PNE 2002102900029 20021029 00029 SW 2002 10 29 CA021003007 1 20020913 A 2910 70012F000D320 HOSE BELL 204 204B 1181404 SW LYC T53 T5313B 41549 NE HYD SYSTEM LEAKING W H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION HO HOVERING 1 CA (CAN) HOSE ASSEMBLY FAILED RESULTING IN LOSS OF HYDRAULIC FLUID. THE LOSS OF FLUID RESULTED IN LOSS OF HYDRAULIC BOOST T O FLIGHT CONTROLS. AIRCRAFT WAS LANDED UNEVENTFULLY WITHOUT HYDRAULIC BOOST. THE HYDRAULIC LINE EXHIBITED NO SIGNS OF LE AKAGE PRIOR TO FAILURE AND TIME INSTALLED ON AIRCRAFT IS UNKNOWN. 1 G 7 1 4U 4 U H1SW E17EA 2002102900031 20021029 00031 EA 2002 10 29 CA021003008 2 20020501 A 8540 269A54023 NUT SCWZER 269 269D 8059501 EA LYC O360 HIO360D1A 41514 EA CLUTCH LOOSE W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DAILY INSPECTION REVEALED CLUTCH OIL ON BELT DRIVE ASSEMBLY, STATIC LEAK. INVESTIGATION REVEALED LT THREAD NUT/SEA L RUNNER WAS LOOSE. 1 G 7 1 3U 3 O 0 4H12 1E10 2002102900032 20021029 00032 NM 2002 10 29 DHL2002720521 1 20021022 A 5313 STRINGER BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, E/E COMPARTMENT STR 25 IS CORRODED THRU AT UPPER FLANGE BETWEEN FRAME STA. 460 AND 480. REPAIRED IAW SRM . 2 L 7 3 4F RT A3WE 2002102900033 20021029 00033 SO 2002 10 29 SWIA200211241 1 20020920 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE A/C BAY CONTAMINATED A SWIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 288SW 120316 F/A SMELLED SMOKE IN CABIN AFTER PAX DEPLANED IN MFR. CABIN HAD FILLED WITH SMOKE. LAV SMOKE DETECTOR ACTIVATED. CALL ED FIRE DEPT. INVESTIGATED CABIN FOR SMOKE. RAN APU ON BOTH PACKS AT SEPARATE TIMES. INSPECTED EXTERIOR OF PACK UNITS . OIL NOTED ON RT PACK. RAN RT ENGINE WITH RT PACK. DETERMINED POSSIBLE CAUSE TO BE OIL IN RT BLEED & RT PACK. INSPE CTED RT ENGINE BLEED DUCT AFT OF FIRE SEAL FOR OIL ON INSIDE. NONE NOTED. RAN RT PACK WITH RT ENGINE BLEED FOR 15-20 M INUTES. NO SMOKE NOTED. DID NOTICE RT PACK MODE SELECT IN MANUAL, SWITCHED TO AUTO. OPS CHECKED GOOD, NO DISCREPANCIE S NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2002102900034 20021029 00034 NE 2002 10 29 SWIA200211255 2 20020922 A 7320 5061T98P03 AMPLIFIER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING R F PARTIAL RPM/PWR LOSS FLT CONT AFFECTED CL CLIMB 1 NM 07 918SW 7645 AFTER ESTABLISHING CLIMB POWER AFTER DEPARTURE FROM FAT, RIGHT SIDE N1 FLUCTUATIONS OF +/- 10 PERCENT AND FUEL FLOW OF + /- 500 PPH CAUSED A/C TO YAW UP TO 20K FT. REDUCED POWER AND RIGHT ENGINE STABILIZED. NO FURTHER FLUCTUATIONS WERE OBS ERVED. RETURNED TO FAT. REPLACED NR 2 N1 AMPLIFIER. OPS CHECK GOOD IAW MM 73-21-03. 2 L 7 2 4F 4 F RT A21EA E15NE 2002102900035 20021029 00035 CE 2002 10 29 CA021003009 1 20021001 A 2750 UNK B-NUT BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA FLAP DRIVE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION THE B-NUT ON THE FLAP DRIVE CABLE WAS LOOSE, AN ATTEMPT TO TIGHTEN THE CAUSED THE NUT TO BRAKE I NTO TWO PIECES, THE NUT WAS CORRODED AT THE SEPARATION POINT. DO NOT KNOW IF IT WAS OVER TORQUE ON INSTALLATION OR IF TH E NUT WAS DEFECTIVE. THE CABLE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 2002102900036 20021029 00036 EA 2002 10 29 CA021004005 1 20020612 A 8011 MHB4016R BOLT LYC HIO360D1A SCWZER 269 269D 8059501 EA LYC O360 HIO360D1A 41514 EA STARTER BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA L2629951A (CAN) NOISE OF STARTER AT ATTEMPTED START. FOUND TWO MISSING AND TWO BROKEN BOLTS THAT HOLD MOTOR HOUSING TO DRIVE HOUSI NG. INDUSTRIAL GRADE HARDWARE WITH ONLY SHAKE PROOF WASHERS FOUND ON SERVICEABLE UNIT BEING INSTALLED. HARDWARE REPLACED WITH DRILLED HEAD BOLTS AND LOCKWIRED. 1 G 7 1 3U 3 O 0 4H12 1E10 2002102900037 20021029 00037 NE 2002 10 29 SWIA200211257 2 20020925 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NR 2 POWER LOSS A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 271YV 120271 LARGE SPLIT IN POWER LEVERS ON TAKEOFF ROLL AND AT 100 FT NR 2 NP DROPPED TO ABOUT 50 PERCENT, THE TQ STAYED AT 100 PERC ENT. ON DOWNWIND, TQ DROPPED TO 0 PERCENT, NP INCREASED TO 100 PERCENT. WE FEATHERED NR 2 AND RETURNED TO IPL. INSPEC TED NR 2 ENG WIRING & CANNON PLUGS. COULD NOT DUPLICATE SQUAWK. REPLACED K0161 RELAY WITH SERVICEABLE UNIT FOR TROUBLE SHOOTING. RAN AIRCRAFT. AUTO FEATHER CHECKS GOOD. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002102900038 20021029 00038 EA 2002 10 29 SWIA200211267 1 20020927 A 2740 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 498SW 7483 STAB CH 1 INOP STATUS MESSAGE CLIMBING THROUGH 15,000. RETURNED TO SLC. PERFORMED SELF TEST OF HSTCU AND STAB TRIM CHA NNEL NR 1. ALL TEST NORMAL. UNABLE TO DUPLICATE DISCREPANCY. 2 L 7 2 4F RT A21EA 2002110400177 20021104 00177 NM 2002 11 4 2002UALA01529 1 20021001 A 2781 CIRCUIT CARD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 10 FAULTY A UALA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 WP 29 652UA 25390 EICAS "LE SLAT ASSY" AND ASSOCIATED LIGHT ILLUMINATED WITH INDICATED 1 DEGREE FOR BOTH LEFT AND RIGHT. TROUBLESHOT SYST EM PER FAULT ISOLATION MANUAL. FOUND A5 DRIVER CARD IN THE NR 10 POSITION IN THE PROXIMITY SWITCH ELECTRONIC UNIT FAULT ED. REPLACED CARD SYSTEM OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2002102900039 20021029 00039 NM 2002 10 29 2002UALA01561 1 20021010 A 3231 114087005 VALVE AIRBUS A319 A319131 3930317 NM IAE V2527 V2527A5 NE LEAKING A UALA D H RETURN TO BLOCK DEACTIVATE SYST/CIRCUITS J K WARNING INDICATION FLUID LOSS TX TAXI/GRND HDL 1 WP 29 802UA 690 LOST GREEN HYDRAULIC PRESSURE AND QUANTITY ON TAXI OUT. RETURNED TO GATE UNDER TOW. SUPPLEM ENTAL DATA UPDATE #2 MAIN LANDING GEAR DOOR GROUND OPENING BYPASS VALVE LEAKING. REPLACED VALVE ASSEMBLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112600127 20021126 00127 NM 2002 11 26 2002UALA01578 1 20021013 A 5610 SEAL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE WINDSHIELD DEBONDED A UALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 805UA 16254 783 LANDED UNDER AMBER ALERT DUE TO CRACKED RIGHT WINDSHIELD. THE DISBONDING OF THE WHITE SILICONE PRESSURE SEAL ALLOWED WA TER TO ENTER THE BUS BAR AREA WHICH RESULTED IN ARCING AND SHATTERED THE WINDOW OUTER PLY. THE WINDOW WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002102900040 20021029 00040 EU 2002 10 29 2002UALA01607 1 20021018 A 3230 848401 SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE 29GA DAMAGED A UALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 WP 29 405UA 452 RETURNED TO FIELD DUE TO LEFT MAIN GEAR DOOR NOT UPLOCKED AFTER GEAR RETRACTION. SUPPLEMENTAL DATA UPDATE FOUND LH MAIN GEAR DOOR PROXIMITY SENSOR (29GA) AND CONNECTOR DAMAGED. REPLACED SENSOR AND CONNECTOR. ALSO DETERMINED LH MAIN LANDI NG GEAR UPLOCK ASSEMBLY NOT WORKING CORRECTLY. REPLACED UPLOCK ASSEMBLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2002102900041 20021029 00041 NM 2002 10 29 2002UALA01608 1 20021016 A 5330 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 FUSELAGE DENTED AT STATION 2108 RH SIDE, WL 192. MAJOR REPAIR ACCOMPLISHED. DOUBLER APPLIED TO DENTED AREA ON FUSELAG E, STATION 2108 RH SIDE, WL 192. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002102900042 20021029 00042 NM 2002 10 29 2002UALA01609 1 20021022 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 FRAME CORRODED. STA 1680, WL208-211, RBL 65. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER AND TRIPLER ANGLES. 2 L 7 2 4F 4 F RT A2NM E17NE 2002102900043 20021029 00043 NM 2002 10 29 2002UALA01610 1 20021022 A 5713 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 RH UPPER WING SURFACE CORRODED. WS 159, WBL 77.5 TO 79.5 BS 996 TO 1005, MAJOR REPAIR ACCOMPLISHED.INSTALLED REPAIR ANG LES ON STRINGERS AND ROTOPEEN SKIN. 2 L 7 2 4F 4 F RT A2NM E17NE 2002102900044 20021029 00044 NM 2002 10 29 2002UALA01611 1 20021022 A 5315 BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 CABIN FLOOR BEAM T-CAP CORRODED. STA 324 RBL 38-61. MAJOR REPAIR ACCOMPLISHED.INSTALLED REPAIR ANGLE ON FLOOR BEAM SUPP ORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112600057 20021126 00057 NM 2002 11 26 2002UALA01615 1 20021022 A 5511 RIB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 950UA 26695 RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE MOST INBD RIB FLANGE IS CRACKED AT LOWER END. MAJOR REPAIR ACCOMPLISHED. REPLACED RIB CHORD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002102900045 20021029 00045 NM 2002 10 29 2002UALA01618 1 20021022 A 5300 WEB BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE MISLOCATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 RIGHT HAND WHEEL WELL UPPER PRESSURE WEB HAS A MISLOCATED DRAIN HOLE FROM PREVIOUS INSTALLATION. SUPPLEMENTAL DATA UPDA TE MAJOR REPAIR ACCOMPLISHED.REPAIRED WEB 2 L 7 2 4F 4 F RT A1NM E3NE 2002102900046 20021029 00046 SO 2002 10 29 SWIA200211271 1 20020929 A 2424 51549001A GCU EMB 120 EMB120ER 3260203 SO NR 1 MALFUNCTIONED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 214SW 6934 6934 120280 CAPTAIN'S EHSI WENT BLANK ON TAXI OUT. REPLACED GCU NR 1 (AUX GEN NR 1) IAW MM 24-30-02. CHECKED OPERATION OF POWER TR ANSFER AT NP 70 PERCENT WITHOUT OBSERVING ANY ANOMALIES ON EHSI NR 1. CHECKS GOOD. PARALLELED AUX GEN'S IAW MM 24-30-0 2 ALL OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002102900047 20021029 00047 2002 10 29 SWIA200211272 4 20020929 A 3425 6226198103 COMPUTER EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 214SW 6915 6915 120280 FO'S EHSI FAILED DURING TAXI AND IN FLIGHT. EHSI SHOWS YELLOW FAIL FLAG AND HEADING FLAG. SUCCESSFULLY RESET BOTH TIME S. REPLACED FO'S HDG74. OPERATIONAL CHECK OF EHSI GOOD. 2 L 7 2 4T RT A31SO 2002102900048 20021029 00048 EA 2002 10 29 SWIA200211273 1 20020929 A 5220 SEAL CNDAIR CL600 CL6002B19 1900309 EA OVERWING EXIT DIRTY A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 595SW 7292 HIGH PITCHED WHINING NOISE REPORTED BY PASSENGERS AT ROW 7A&B. CLEANED DOOR SEAL AT LEFT OVER WING EXIT. 2 L 7 2 4F RT A21EA 2002102900049 20021029 00049 EA 2002 10 29 SWIA200211275 1 20020929 A 4950 1098046 CONTROL VALVE CNDAIR CL600 CL6002B19 1900309 EA APU MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 905SW 438 432 7437 APU LOAD CONTROL VALVE WOULD NOT CLOSE AFTER TAKEOFF. RETURNED TO FAT. REMOVED AND REPLACED APU LCV IAW CRJ MM 49-51-0 1. OPERATIONAL CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2002102900050 20021029 00050 EA 2002 10 29 SWIA200211277 1 20020930 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING DENTED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 RIGHT WING LEADING EDGE BETWEEN WS 85.5 AND WS 96.13 IS DENTED AND OIL CANNING ON LOWER SIDE OF LEADING EDGE. REPLACED INBOARD RIGHT LEADING EDGE IAW MM 57-41-01. 2 L 7 2 4F RT A21EA 2002102900051 20021029 00051 SO 2002 10 29 SWIA200211278 1 20020930 A 5280 LATCH EMB 120 EMB120ER 3260203 SO LG DOOR FAILED A SWIA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 NM 07 284YV 120284 LEFT SIDE FORWARD OUTBOARD GEAR DOOR CAME UNLATCHED IN FLIGHT. LATCHED OK, BUT HAPPENED 2X. REPLACED LANDING GEAR DOOR LATCH PIN AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002102900052 20021029 00052 SO 2002 10 29 SWIA200211279 1 20020910 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 289YV 120289 LEFT FLOOR SEAT TRACK HAS CORROSION BELOW TRACK IN BUTT STRAP. REPLACED LEFT FLOOR SEAT TRACK FULL LENGTH IAW EMB120 MM 53-10-05. 2 L 7 2 4T RT A31SO 2002102900053 20021029 00053 SO 2002 10 29 SWIA200211280 1 20020910 A 5280 CONTROL ROD EMB 120 EMB120ER 3260203 SO NLG DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 289YV 120289 NOSE LANDING GEAR RIGHT AFT DOOR CONTROL ROD HAS CORROSION. REMOVED AND REPLACED RIGHT AFT NOSE GEAR DOOR CONTROL ROD W ITH SERVICEABLE UNIT. 2 L 7 2 4T RT A31SO 2002102900054 20021029 00054 SO 2002 10 29 SWIA200211281 1 20020910 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 289YV 120289 FORE/AFT BUTT STRAP THICKNESS WORN TO LIMITS UNDER SEATS 7A AND 10B. REPLACED BUTT STRAPS IAW SRM120 51-10-02 AND SECUR ED IAW 51-40-02. 2 L 7 2 4T RT A31SO 2002102900055 20021029 00055 EA 2002 10 29 SWIA200211282 1 20021003 A 7797 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NR 2 ENGINE FAULTY A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 918SW 7645 DURING FLIGHT TO SFO AT 16,000 FT, NR 2 ENGINE N1 FLUCTUATIONS OF 8 TO 10 PERCENT WITH ASSOCIATED N2 FUEL FLOW & ITT FLU CTUATIONS. WITH THRUST BACK AT 68 PERCENT, FLUCTUATIONS STOPPED. REMOVED AND REPLACED RIGHT ENGINE BLUE AND YELLOW HAR NESS. ENGINE RUN OF SYSTEM OPS CHECKS GOOD ON THE GROUND. 2 L 7 2 4F RT A21EA 2002102900056 20021029 00056 NE 2002 10 29 SWIA200211283 2 20020930 A 7320 78639010 HMU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIA O OTHER M OVER TEMP TX TAXI/GRND HDL 1 NM 07 579SW 120347 EXPERIENCED THREE HOT STARTS ON THE LEFT ENGINE. FOLLOWED STARTER/GEN DUTY CYCLE LIMITS. FUEL FLOW PEAKED AT 150 PPH. REPLACED LEFT ENGINE HMU FUEL CONTROL AND FUEL PUMP IAW 73-22-00 & 73-14-00 . LEFT ENGINE OPS & LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002102900057 20021029 00057 EA 2002 10 29 SWIA200211284 1 20020920 A 3411 PITOT TUBE CNDAIR CL600 CL6002B19 1900309 EA RIGHT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 RIGHT SIDE PITOT/STATIC TUBE CORRODED. REMOVED AND REPLACED RIGHT PITOT/STATIC TUBE IAW 34-11-01. PERFORMED PITOT/STA TIC SYSTEM LEAK CHECK IAW MM 30-31-00. ALSO HEAT CHECKS GOOD IAW MM 34-11-00. 2 L 7 2 4F RT A21EA 2002102900058 20021029 00058 EA 2002 10 29 SWIA200211285 1 20021006 A 2421 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 IDG LOW A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 917SW 7641 RECEIVED AN IDG MESSAGE ON TAKEOFF AND ABORTED. RESET CB 1NS, 2N8, 4A2, 4A3, MESSAGE CLEARED. GOT THE IDG MESSAGE AGAI N AND ABORTED TAKEOFF. FOUND THE NR 1 IDG HAD NO OIL. SERVICED OIL TO PROPER LEVEL AND RECONNECTED IDG. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002102900059 20021029 00059 SO 2002 10 29 SWIA200211287 1 20020916 A 5420 STIFFENER EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 RIGHT NACELLE AFT SIDE OF HYDRAULIC BULKHEAD HAS A CRACKED HORIZONTAL STIFFENER. FOUND ON C-CHECK INSPECTION. FABRICAT ED AND INSTALLED A DOUBLER IAW SRM 51-00-00 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002102900060 20021029 00060 SO 2002 10 29 SWIA200211288 1 20020916 A 5420 STIFFENER EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 LEFT NACELLE AFT SIDE OF HYDRAULIC BULKHEAD APPEARS TO HAVE A CRACKED VERTICAL STIFFENER. FOUND ON C-CHECK INSPECTION. FABRICATED AND INSTALLED DOUBLER IAW SRM 51-70-05 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002102900061 20021029 00061 SO 2002 10 29 SWIA200211289 1 20020916 A 5720 BRACKET EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 SMALL LOWER BRACKET AT RIB 15 IN RIGHT FUEL CELL IS CRACKED. CRACK IS ON INBOARD SIDE OF FRAME. FOUND ON C-CHECK INSPE CTION. REMOVED AND REPLACED CRACKED SKIN CLIP IAW EMB SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002102900062 20021029 00062 SO 2002 10 29 SWIA200211290 1 20020916 A 5720 BRACKET EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 LOWER BRACKET AT RIB 16 APPEARS TO BE CRACKED ALONG OUTBOARD, AFT AREA OF BRACKET. RIGHT FUEL CELL. FOUND ON C-CHECK I NSPECTION. REMOVED CRACKED CLIP AND FABRICATED NEW CLIP AND INSTALLED NEW SKIN CLIP IAW EMB SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002102900063 20021029 00063 SO 2002 10 29 SWIA200211291 1 20020916 A 5420 CLIP EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 LEFT NACELLE OUTBOARD SIDE FRAME 17 CLIP CRACKED. FOUND ON C-CHECK INSPECTION. FABRICATED AND INSTALLED DOUBLER IAW EM B120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002102900064 20021029 00064 SO 2002 10 29 SWIA200211292 1 20021001 A 3230 UPLOCK EMB 120 EMB120ER 3260203 SO RT MLG OUT OF RIG A SWIA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 NM 07 582SW 120350 RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO DRO. RUNNING GEAR UP AND DOWN, FOUND THE UPLOCK H OOK TO BE OUT OF RIG. ADJUSTED UPLOCK HOOK ACTUATOR ROD PER MM CHAPTER 32-32-09. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002102900065 20021029 00065 SO 2002 10 29 SWIA200211293 1 20020916 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT & RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 LEFT AND RIGHT NACELLE INBOARD AND OUTBOARD EXHAUST MOUNTS HAVE INTERNAL FRAME CRACKS AT NUTPLATES. FOUND ON C-CHECK IN SPECTION. STOP-DRILLED CRACKS AND INSTALLED A REPAIR DOUBLERS ON FRAMES IAW EMB SRM 51-70-05. 2 L 7 2 4T RT A31SO 2002102900066 20021029 00066 SO 2002 10 29 SWIA200211294 1 20020916 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 FRAME 13 LEFT AND RIGHT SIDES OF STEP INTO COCKPIT CRACKED INSIDE AND OUTSIDE OF VERTICAL BRACE. FOUND ON C-CHECK INSPE CTION. REMOVED ANGLES, FABRICATED AND INSTALLED A NEW ANGLES AND A DOUBLERS IAW SRM 51-00-00 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002102900067 20021029 00067 EA 2002 10 29 SWIA200211295 1 20021001 A 5210 SPRING CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR OBSTRUCTED A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 433SW 7550 MAIN CABIN DOOR IS EXTREMELY DIFFICULT TO OPEN. INSPECTED DOOR MECHANISM AND FOUND INSIDE LATCH STOW SPRING DIFFICULT T O COMPRESS. CLEARED DEBRIS FROM SPRING. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002102900068 20021029 00068 SO 2002 10 29 SWIA200211296 1 20020916 A 5320 ANGLE EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 FRAME 13, LOWER RIGHT HAND ANGLE AND CHANNEL CRACKED. FOUND DURING C CHECK INSPECTION. REMOVED CRACKED ANGLE AND CHANN EL. FABRICATED NEW ANGLE AND SPLICED IN A SECTION OF THE CHANNEL. INSTALLED BOTH IAW EMB SRM 51-70-05 AND 51-40-02. 2 L 7 2 4T RT A31SO 2002102900069 20021029 00069 SO 2002 10 29 SWIA200211297 1 20020916 A 5420 CLIP EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 RIGHT NACELLE INBOARD AND OUTBOARD FRAME 17 CLIPS CRACKED AT BOTTOM RIVET HOLES. FOUND DURING C CHECK INSPECTION. STOP -DRILLED CRACKS AND INSTALLED REPAIR DOUBLERS ON THE FRAMES IAW EMB SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002102900070 20021029 00070 SO 2002 10 29 SWIA200211298 1 20020916 A 5320 SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 COCKPIT LEFT SIDE, JUST AFT OF DIRECT VISION WINDOW, FOUND CRACK IN INTERCOSTAL. FOUND DURING C CHECK INSPECTION. FABR ICATED AND INSTALLED DOUBLER IAW EMB SRM 51-00-00 & 51-40-02. 2 L 7 2 4T RT A31SO 2002102900071 20021029 00071 SO 2002 10 29 SWIA200211299 1 20020918 A 5320 SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 301YV 120301 SUPPORT AFT OF CAPTAIN'S DV WINDOW CRACKED. FOUND DURING C CHECK INSPECTION. REPLACED SUPPORT AFT OF CAPTAIN'S DV WIND OW WITH SERVICEABLE UNIT PER EMB SRM 51-40-02, 51-22-00, AND 51-40-01. 2 L 7 2 4T RT A31SO 2002102900072 20021029 00072 SO 2002 10 29 SWIA200211300 1 20020918 A 7110 SUPPORT EMB 120 EMB120ER 3260203 SO RT COWLING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 301YV 120301 RIGHT ENGINE FRAME 1 COWLING SUPPORT CRACKED, TOP INBOARD SIDE. FOUND DURING C CHECK INSPECTION. REMOVED AND REPLACED RIGHT ENGINE FRAME 1 COWLING SUPPORT BRACKET ON TOP INBOARD SIDE. 2 L 7 2 4T RT A31SO 2002102900073 20021029 00073 EA 2002 10 29 SWIA200211302 1 20021007 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 413SW 7102 2ND SECTION OF EMERGENCY FLOOR LIGHTS INOP. INSTALLED NEW TERMINALS FOR 2ND SECTION FLOOR TRACK LIGHTING. OPS CHECK GO OD. 2 L 7 2 4F RT A21EA 2002102900074 20021029 00074 EA 2002 10 29 SWIA200211303 1 20021006 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 07 429SW 7518 LOSS OF ALL NR 3 SYSTEM HYDRAULIC FLUID. REMOVED AND REPLACED ELECTRIC HYDRAULIC PUMP 3A WITH SERVICEABLE UNIT IAW MM 2 9-12-03. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2002102900075 20021029 00075 EA 2002 10 29 SWIA200211304 1 20021008 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 429SW 7518 CEILING EMERGENCY LIGHT INOP AT ROW 2. REMOVED THE INOP BULB AND INSTALLED A NEW BULB. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2002102900076 20021029 00076 EA 2002 10 29 SWIA200211305 1 20021004 A 2710 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT INOPERATIVE A SWIA A UNSCHED LANDING J E F WARNING INDICATION VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 NM 07 431SW 7536 AILERON SWITCH INOP. REMOVED AND REPLACED AILERON TRIM SWITCH. OPERATED AILERON TRIM. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002102900077 20021029 00077 SO 2002 10 29 SWIA200211306 1 20021007 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO CARGO DOOR OUT OF ADJUST A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 566SW 120341 CARGO DOOR ILLUMINATED WITH SUBSEQUENT DOOR AURAL WARNING DURING TAKEOFF. ABORTED TAKEOFF. ADJUSTED FORWARD MICROSWITC H AND TARGET. OPS CHECK GOOD IAW MM 52-72-03. 2 L 7 2 4T RT A31SO 2002102900078 20021029 00078 EA 2002 10 29 SWIA200211307 1 20021010 A 2740 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 498SW 7483 STAB CH 1 INOP STATUS MESSAGE ILLUMINATED ON CLIMB OUT. REENGAGED CH 1 AND MESSAGE WENT OUT. REILLUMINATED ON LANDING , WOULD NOT REENGAGE. PERFORMED OPS CHECK ON HORIZONTAL STABILIZERS CONTROL SYSTEM IAW A/C MM 27-41-00. NO FAULTS FOUN D. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002102900079 20021029 00079 SO 2002 10 29 SWIA200211308 1 20021006 A 2722 3081401003 ACTUATOR EMB 120 EMB120ER 3260203 SO RUDDER FAILED A SWIA A UNSCHED LANDING P F NO WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 209SW 120269 RUDDER PEDALS FROZE JUST AFTER TAKEOFF, NO WARNINGS OR AURAL INDICATIONS. RIGHT SIDE COULD ONLY MOVE AN 1 INCH OR SO, L EFT PEDAL HAD SLIGHTLY MORE TRAVEL. RUDDER PEDAL TRAVEL WAS NORMAL ON THE GROUND. REMOVED AND REPLACED GREEN AND BLUE SYSTEM RUDDER ACTUATORS IAW EMB MM 27-22-02. OPS AND LEAK CHECK GOOD IAW 27-20-00 & 27-22-00. 2 L 7 2 4T RT A31SO 2002102900080 20021029 00080 SO 2002 10 29 SWIA200211309 1 20021006 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP LEAKING A SWIA O OTHER K F FLUID LOSS FLT CONT AFFECTED CR CRUISE 1 NM 07 290SW 120317 RIGHT HYDRAULIC RESERVOIR EMPTIED EN ROUTE. FOUND LEFT NACELLE FLAP ACTUATOR TO BE LEAKING FROM A POSITION TRANSDUCER. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-08. OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2002102900081 20021029 00081 EA 2002 10 29 SWIA200211310 1 20021004 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 907SW 7511 STAB AND MACH TRIM DISENGAGED AT THE GATE WITH A CAUTION MESSAGE. REENGAGED SYSTEM AND STAB CHANNEL 2 WOULD NOT REENGAG E. REPLACED HORIZONTAL STAB ACTUATOR AND MOTOR CONTROL UNIT IAW 27-42-01. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2002102900082 20021029 00082 NM 2002 10 29 02FDEA00670 1 20020923 A 5320 SUPPORT BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 CORROSION ON BS 1176.9 REINFORCEMENT CHORD, RBL 50-70.5, WL 208. R&R CHORD PER SRM 51-30-2, 51-30-8, 51-30-5, 51-10-2 & MM 51-20-151-7. 2 L 7 3 4F RT A3WE 2002102900083 20021029 00083 NM 2002 10 29 02FDEA00673 1 20020921 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 478FE 21395 LT FUSELAGE EXTERIOR SKIN HAS A GOUGE AT BS 365.5 BETWEEN STR 16L - 17L. R&R SKIN PER SRM 53-30-3 FIG 3 & EA 7-5330-543 19. 2 L 7 3 4F RT A3WE 2002102900084 20021029 00084 NM 2002 10 29 02FDEA00678 1 20020919 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 CORROSION LWR CHORD BS 720 FLOORBEAM, WL 208, LBL 55 - RBL 55. R&R CHORD PER SR 27-53-034. 2 L 7 3 4F RT A3WE 2002102900085 20021029 00085 NM 2002 10 29 02FDEA00679 1 20020920 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 478FE 21395 CORROSION C53-111-01 ON STRINGER 328R, BS 480+5 FWD CARGO BAY. R&R STRINGER PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 2002102900086 20021029 00086 NM 2002 10 29 02FDEA00680 1 20020920 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 478FE 21395 FOUND CORROSION ON SKIN AT BS 483-495, 528R. R&R SKIN PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 2002102900087 20021029 00087 NM 2002 10 29 02FDEA00681 1 20020921 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 CRACK IN FRAME FAILSAFE CHORD AT BS 804, STR 14R. R&R FRAME PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2002102900088 20021029 00088 NM 2002 10 29 02FDEA00682 1 20020921 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 CRACK IN FRAME FAILSAFE CHORD BS 804, STR 14R. R&R FRAME PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2002102900089 20021029 00089 NM 2002 10 29 02FDEA00685 1 20020830 A 5320 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 STR 7R CLIP AT BS 720F HAS ELONGATED HOLE IN CLIP AND FRAME. R&R STRINGER CLIP PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002102900090 20021029 00090 NM 2002 10 29 02FDEA00688 1 20020926 A 2782 269002913L ACTUATOR BOEING 727 727200 138407E NM L/E SLAT FAILED A FDEA A UNSCHED LANDING K J F FLUID LOSS WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SO 25 263FE 21625 AFTER FLAP RETRACTION, WITH FLAPS UP AND LED LIGHT GREEN, "A" SYSTEM QUANTITY DECREASED TO ZERO. WITH LOSS OF "A" SYSTE M PRESSURE RAN APPROPRIATE EMERGENCY CHECKLISTS. FOUND NR 4 SLAT ACTUATOR BODY FAILED AT ENDCAP WHERE ROD EXITS THE HOU SING. REMOVED AND REPLACED L/E SLAT ACTUATOR IN REF TO 727-200 MM, 27-81-032-4. OPS CHECKED NORMAL. 2 L 7 3 4F RT A3WE 2002102900091 20021029 00091 NM 2002 10 29 02FDEA00689 1 20020920 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 478FE 21395 CORROSION IN FASTENER HOLES ON FLOORBEAM LOWER FLANGE AT BS 1070, LBL 45 TO RBL 45. R&R FLOORBEAM PER DWG SR27-53-034, SRM 53-10-8. 2 L 7 3 4F RT A3WE 2002102900092 20021029 00092 NM 2002 10 29 02FDEA00690 1 20020915 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 478FE 21395 LT FUSELAGE EXTERIOR SKIN HAS A GOUGE AT BS 294.5 JUST ABOVE STR 17L. R&R SKIN PER EA 7-5330-67012. 2 L 7 3 4F RT A3WE 2002102900093 20021029 00093 NM 2002 10 29 02FDEA00691 1 20020915 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 478FE 21395 CORROSION ON FLOORBEAM UPPER CHORD AT BS 344, LBL 60 - RBL 4, WL 208. R&R FLOORBEAM PER SRM 53-10-8 FIG 9. 2 L 7 3 4F RT A3WE 2002102900094 20021029 00094 NM 2002 10 29 02FDEA00692 1 20020927 A 3610 CLAMP BOEING 727 727200 138407E NM BLEED AIR OUT OF POSITION A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 268FE 21674 FL290 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, COMPLETED QRH PROCEDURES LIGHT WENT OUT. REMAINDER OF FLIGHT CONDUCTED WITH NR 3 BLEED OFF, NR 2 PACK OFF NORMAL POWER ON NR 3 ENGINE. CHECKED AFT AIRSTAIR AND FOUND RT PURGE VALVE V BAND C LAMP OPENING LESS THAN .5 INCH FROM SENSOR. REPOSITIONED V BAND CLAMP AND RAN BOTH NR 1 AND NR 3 ENGINES AND PACKS AT P OWER. LOWER BODY HEAT OPS CK GOOD IAW MM 26-14-000-5 . 2 L 7 3 4F RT A3WE 2002102900095 20021029 00095 EU 2002 10 29 02FDEA00694 1 20021001 A 5730 SKIN PANEL AIRBUS 310 A310 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 LEFT WING LWR SKIN PANEL NR 2 FOUND WITH EDGE CRACK JUST OUTBOARD OF RIB 11, CRACKED 1 INCH. R&R WING LWR SKIN PANEL NR 2 PER EA 6-5710-65099. 2 L 7 2 4F RT A35EU 2002102900099 20021029 00099 SO 2002 10 29 C2XA02CL190 1 20020930 A 2612 3601133500 FIRE LOOP EMB 145 EMB145LR 3260212 SO NR 2 ENGINE CHAFED A C2XA K NONE N FALSE WARNING UK UNKNOWN 1 SW 27 12552 145583 CLE FLIGHT NR 3242, CREW REPORTED ENGINE NR 2 FIRE DETECT FAIL MESSAGE. MAINTENANCE INSPECTED AND FOUND THE FIRE LOOP W AS CHAFED. THE NR 2 ENGINE FIRE LOOP WAS REPLACED. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002102900100 20021029 00100 SO 2002 10 29 C2XA02CL192 1 20021002 A 3320 7287503507 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 12922 145338 CLE FLIGHT NR 3282 THE CREW REPORTED SPARKS AND FIRE CAME FROM FLUORESCENT CABIN LIGHT AT SEAT 12C. MAINTENANCE INSPECT ED AND REPLACED THE PASSENGER CABIN LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVIC E. 2 L 7 2 4T RT T00011AT 2002102900101 20021029 00101 SO 2002 10 29 C2XA02CL194 1 20021002 A 2611 WARNING SYSTEM EMB 135 EMB135LR 3260305 SO COCKPIT MALFUNCTIONED A C2XA K NONE N FALSE WARNING CL CLIMB 1 SW 27 27523 145389 CLE FLIGHT NR 3001, THE CREW REPORTED A LAV SMOKE WARNING AFTER T/O, NO SMOKE WAS REPORTED. MAINTENANCE INSPECTED AND P ERFORMED LAV SMOKE WARNING. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002102900102 20021029 00102 SO 2002 10 29 C2XA02CL195 1 20021004 A 3350 66368 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 25504 145186 CLE FLIGHT NR 2093 THE CREW REPORTED THE FORWARD CABIN EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REPLA CED THE EMERGENCY AISLE PATH LIGHTING STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002102900103 20021029 00103 SO 2002 10 29 C2XA02CL198 1 20021010 A 3234 7455501 CONTROL HANDLE EMB 135 EMB135LR 3260305 SO COCKPIT FAULTY A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 17521 145378 CLE FLIGHT NR 3099 THE CREW REPORTED DURING LANDING APPROACH THEY RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE. THE C REW PERFORMED QRH MANUAL EXTENSION AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002102900104 20021029 00104 EA 2002 10 29 QXEA0201473 1 20020917 A 2820 79888211 CONTROL PANEL CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 603QX 1966 1966 10011 EUG- DURING PRESSURE REFUELING, REFUEL PANEL HAD SOME NUMBERS GO BLANK. ELECTRICAL SMELL WAS DETECTED AT FUELING PANEL. REMOVED AND REPLACED FUSELAGE REFUEL/DEFUEL CONTROL PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002102900105 20021029 00105 EA 2002 10 29 QXEA0201475 1 20020918 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 613QX 10045 FIRE DETECTION CHIMNEY IN FORWARD CARGO COMPARTMENT IS DAMAGED. REMOVED AND REPLACED FIRE DETECTION CHIMNEY. OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002102900106 20021029 00106 NM 2002 10 29 QXEA0201478 1 20020925 A 2730 WARNING SYSTEM BOMBDR DHC8 DHC8401 1390041 NM COCKPIT ACTIVATED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 410QX 4053 SUN - DURING DESCENT AT APPROXIMATELY 230 KTS, THE CREW RECEIVED A PITCH TRIM CAUTION LIGHT AND AUTO TRIM FAIL MESSAGE O N THE PFD. ELEVATOR TRIM FAIL MESSAGE WAS ALSO RECEIVED. MAINTENANCE INSPECTED THE AIRCRAFT AND RETRIEVED THE FAULT CO DES 67,63,E7, AND E3. THE SERVICE LETTER DH8-400-SL-27-003 WAS COMPLIED WITH AND THE FAULTS WERE CLEARED. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002102900107 20021029 00107 EA 2002 10 29 QXEA0201494 1 20020928 A 2820 79888211 CONTROL PANEL CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 608QX 2119 2119 10026 SEA- AIRCRAFT FUELER REPORTED SMOKE FROM SPR CONTROL PANEL WHEN POWER SWITCH SELECTED ON. PANEL SMELLED OF BURNT ELECTR ONIC COMPONENTS. REMOVED AND REPLACED REFUEL/DEFUEL PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002102900108 20021029 00108 NM 2002 10 29 QXEA0201556 1 20020926 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND INBOARD WING FRONT SPAR BOTTOM FLANGE CHAFED AT INBOARD END FROM CONTACT WITH LEADING EDGE AT YW50.0. RE PAIRED IAW RD 8-57-2054. 2 H 7 2 4T RT A13NM 2002102900109 20021029 00109 NM 2002 10 29 QXEA0201557 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 10 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X266.00 TO FORWARD END. REPL ACED NR 10 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102900110 20021029 00110 NM 2002 10 29 QXEA0201558 1 20020926 A 3220 ARM DHAV DHC8 DHC8202 2809007 NM NLG EXCESS PLAY A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - NOSE GEAR TRAILING ARM HAS RADIAL PLAY AT ATTACH POINT. REPAIRED IAW DOWTY CMM CHAPTER 32-20-01. 2 H 7 2 4T RT A13NM 2002102900111 20021029 00111 NM 2002 10 29 QXEA0201559 1 20020924 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND LEADING EDGE 511AL MOUNTING BRACKETS CRACKED, TOP AND BOTTOM. REPAIRED IAW DHC-8 MM 51-11-00. 2 H 7 2 4T RT A13NM 2002102900112 20021029 00112 NM 2002 10 29 QXEA0201560 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 1 TOP CORROSION IN SEAT ATTACH AREA AT X266.00. REPLACED NR 1 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102900113 20021029 00113 NM 2002 10 29 QXEA0201561 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 1 TOP CORROSION IN SEAT ATTACH AREA AT X280.00. REPLACED NR 1 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102900114 20021029 00114 NM 2002 10 29 QXEA0201562 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 1 TOP CORROSION IN SEAT ATTACH AREA AT X298.00. REPLACED NR 1 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102900115 20021029 00115 NM 2002 10 29 QXEA0201563 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 1 TOP CORROSION IN SEAT ATTACH AREA AT X312.00. REPLACED NR 1 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102900116 20021029 00116 NM 2002 10 29 QXEA0201564 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 1 TOP CORROSION IN SEAT ATTACH AREA AT X328.00. REPLACED NR 1 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102900117 20021029 00117 NM 2002 10 29 QXEA0201565 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 1 TOP CORROSION IN SEAT ATTACH AREA AT X343.00. REPLACED NR 1 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102900118 20021029 00118 NM 2002 10 29 QXEA0201566 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 1 TOP CORROSION IN SEAT ATTACH AREA FROM X363.00 TO X377.00. REPLACED NR 1 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102900119 20021029 00119 NM 2002 10 29 QXEA0201567 1 20020926 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 1 AT TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X377.00. REPLACED NR 1 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002102900120 20021029 00120 NM 2002 10 29 QXEA0201568 1 20020924 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND LEADING EDGE 611AR MOUNTING BRACKETS CRACKED AT TOP AND BOTTOM. REPAIRED IAW D8 MM 51-11-00. 2 H 7 2 4T RT A13NM 2002102900121 20021029 00121 NM 2002 10 29 QXEA0201570 1 20020929 A 5260 DOOR BOMBDR DHC8 DHC8401 1390041 NM AIRSTAIRS JAMMED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 412QX 4059 AIRSTAIR DOOR WILL NOT OPEN. UNJAMMED DOOR. CYCLED DOOR SEVERAL TIMES FROM INSIDE AND OUTSIDE. DOOR FUNCTIONED SMOOTH LY. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002102900122 20021029 00122 NM 2002 10 29 QXEA0201571 1 20021001 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX- NICK IN FUSELAGE ON RIGHT HAND SIDE 1.25 INCHES BELOW STRINGER 17S AND 3 INCHES FORWARD OF STATION X341.000. REPAI RED IAW DHC-8 Q400 SRM TASK 53-10-31-350-802. 2 H 7 2 4T RT A13NM 2002102900123 20021029 00123 WP 2002 10 29 MWE020665 1 20021029 A 5330 59114063 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 FUSELAGE EXTERNAL SKIN IS GOUGED AT FORWARD BOTTOM DOOR STOP SCREW. -- INSTALLED EXTERNAL SCAB DOUBLER OVER #7 STOP. 2 L 7 2 4F A6WE 2002102900124 20021029 00124 WP 2002 10 29 MWEA020666 1 20021029 A 5330 591140215 DOUBLER DOUG DC9 DC981 3022081 WP PAX DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 FUSELAGE EXTERNAL SKIN HAS LIGHT GOUGES AROUND PAX DOOR HOLD OPEN HOOK RECEPTACLE. -- INSTALLED EXTERNAL DOUBLER. 2 L 7 2 4F A6WE 2002102900125 20021029 00125 NM 2002 10 29 QXEA0201572 1 20020911 A 1430 RIVET BOMBDR DHC8 DHC8401 1390041 NM LT WING LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 CKB- RIVETS LOOSE ON LEFT HAND CENTER WING BOTTOM SKIN, AFT EDGE NEAR JACKING POINT. REPAIRED IAW Q400 SRM 51-42-00. 2 H 7 2 4T RT A13NM 2002102900127 20021029 00127 NM 2002 10 29 QXEA0201573 1 20020917 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 CKB-SCRATCH AT AFT OF FUSELAGE BELOW VERTICAL STABILIZER. REPAIRED IAW HORIZON AIR EA 6-53-120 AND WVAC EO DH8S-53-0586 . 2 H 7 2 4T RT A13NM 2002102900128 20021029 00128 NE 2002 10 29 CA021007002 1 20020919 A 3040 90009213 WINDSHIELD WIPER SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL WINDSHIELD SHEARED W O OTHER O OTHER CR CRUISE 1 CA (CAN) PILOT SIDE WIPER BLADE ATTACH PIN SHEARED AT 110 KTS AIRSPEED. SECONDARY PIN REMAINED ATTACHED BUT ALLOWED WIPER B LADE TO FLAIL AGAINST WINDSHIELD. WIPERS TURNED OFF AND AIRSPEED REDUCED TO 60 KTS. AIRCRAFT LANDED AT NEXT SCHEDULED ST OP AND WIPER ARM WAS REMOVED. WINDSHIELD WAS INSPECTED AND NO FAULT FOUND. AIRCRRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2002102900129 20021029 00129 NM 2002 10 29 QXEA0201574 1 20020912 A 5420 STIFFENER BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 CKB-LEFT HAND COWL PANEL 414AL AFT CORNER STIFFENER IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-54-1251 AND WVAC DH8S-54- 0561. 2 H 7 2 4T RT A13NM 2002102900130 20021029 00130 EA 2002 10 29 CA021007006 2 20020830 A 7322 3243621 BEARING BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA FUEL CONTROL SEIZED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING FLIGHT, WHILE ADJUSTING ENGINE POWER SETTINGS, NOTED RT TORQUE INDICATOR FLUCTUATIONS, THEN RAPID UNCONTROL LED TORQUE INCREASED. ENGINE SHUTDOWN IMMEDIATELY AND UNSCHEDULED LANDING CARRIED OUT. MAINTENANCE FOUND FUEL CONTROL UN IT HAS FAILED INTERNALLY AND SHEARED DRIVE COUPLING.OVERHAUL SHOP TEARDOWN FOUND BEARINGS SEIZED IN FCU. 1 L 7 2 3T 4 T RT 3A20 E4EA 2002102900131 20021029 00131 SW 2002 10 29 CA021007007 1 20020918 A 6510 20503181810 HANGER ASSY BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) HANGER CRACKED AT BOTH ATTACH POINTS FOR THE FLEX COUPLING ATTACH. 1 G 7 1 4U 4 U H1SW E17EA 2002102900132 20021029 00132 NM 2002 10 29 QXEA0201575 1 20020912 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 CKB-RIGHT HAND CENTER WING LEADING EDGE END RIBS HAS CRACKS ON AFT ENDS. REPAIRED IAW HORIZON AIR EA 6-57-57 AND WVAC E O DH8S-57-0568. 2 H 7 2 4T RT A13NM 2002102900133 20021029 00133 NE 2002 10 29 CA021007008 3 20020923 A 6111 8173881 SEAL DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE PROPELLER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING ENGINE RUN FOLLOWING MAINTENANCE THE LEFT PROP STARTED LEAKING OIL. LT PROP NR 1 BLADE SEAL WAS REPLACED AN D ENGINE RE RUN WITH NO FURTHER EVIDENCE OF LEAKAGE. THE INNER SPRING OF THE FAILED BLADE SEAL HAD BROKEN AT THE WELD. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002102900134 20021029 00134 NM 2002 10 29 QXEA0201576 1 20020912 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 CKB-LEFT HAND CENTER WING LEADING EDGE RIB ENDS ARE CRACKED. REPAIRED IAW HORIZON AIR EA 6-57-57 AND WVAC DH8S 57-0568. 2 H 7 2 4T RT A13NM 2002102900135 20021029 00135 NM 2002 10 29 QXEA0201577 1 20020921 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 CKB-LEFT HAND OUTBOARD FLAP HAS 2 CHAFED LINES ON TOP SKIN. REPAIRED IAW HORIZON AIR EA 6-57-62 AND WVAC EO DH8S-57-057 0A. 2 H 7 2 4T RT A13NM 2002102900136 20021029 00136 NM 2002 10 29 CA021007009 1 20020926 A 8012 1G309 START VALVE BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE ENGINE FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CA (CAN) DURING CLIMB, NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED. ENGINE SHUTDOWN CARRIED OUT, EMERGENCY DECLARED IAW CHECKLIST. AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. NR 3 ENGINE PRESSURE SWITCHREPLACED AND CHECKED SERVICEABLE IAW MM 80-11-11. 3. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2 L 7 3 4F 4 F A3WE E2EA 2002102900137 20021029 00137 NM 2002 10 29 QXEA0201578 1 20020916 A 5420 ANGLE BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 CKB-ANGLE THAT ATTACHES TO FRAME 15 SEVERELY CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-57, DHC-8 SRM 54-10-16 AND WVAC E O. DH8S-71-0532. 2 H 7 2 4T RT A13NM 2002102900138 20021029 00138 NM 2002 10 29 QXEA0201579 1 20020916 A 5411 FRAME BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 CKB-FRAME ASSEMBLY IS SEVERELY CRACKED. REPAIRED IAW DHC-8 SRM 54-10-16, HORIZON AIR EA 6-71-57 AND WVAC EO DH8S-71-056 2. 2 H 7 2 4T RT A13NM 2002102900139 20021029 00139 EU 2002 10 29 CA021007010 1 20021006 A 6220 10513143 ROD END BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE MAIN ROTOR WORN W A UNSCHED LANDING F FLT CONT AFFECTED HO HOVERING 1 CA (CAN) PILOT NOTICED UNUSUAL VERTICAL VIBRATION IN HOVER AND LANDED IMMEDIATELY. MAINTENANCE DICOVERED BLUEMAIN ROTOR RO TATING CONTROL ROD LOWER ROD END BEARING HAD EXCESSIVE PLAY. THIS WASDUE TO 1/3TH OF THE SPHERICAL BEARING OUTER RACE W ORN AWAY. SPHERICAL BALL BEARING HAD BEEN NEARLY CONTACTING THE ROD END. ROD END REPLACED, A/C TRACKED AND RETURNED TO SERVICE. 1 G 7 2 3U 3 U NC H13EU E5NE10 2002102900140 20021029 00140 EA 2002 10 29 CA021007013 1 20020911 A 7810 NOZZLE CNDAIR CL600 CL600* EA LYC ALF502 ALF502L 41580 NE EXHAUST DEPARTED W E A ENGINE SHUTDOWN UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 CA (CAN) WHILE CLIMBING THROUGH 12,000 FT, CREW REPORTED HEARING A LOUD NOISE. AUTOPILOT IMMEDIATELY DISENGAGED AND BOTH E NGINES THROTTLED BACK. WITH THE ENGINES STILL INDICATING ROTATION AND NORMAL OF PRESSURE, POWER WAS INCREASED AT WHICH T IME THE RT ENGINE SPEED BEGAN TO DECAY. THE CREW SHUTDOWN THE RT ENGINE AND RETURNED TO THEIR POINT OF DEPARTURE PERFORM ING AN UNEVENTFUL SINGLE ENGINE LANDING. INITIAL INSPECTION REVEALED THAT THE EXHAUST NOZZLE HAD DEPARTED IN-FLIGHT AND THAT THERE WAS DAMAGE TO THE FOURTH STAGE TURBINE. THE EXHAUST NOZZLE WAS LATER RECOVERED ABOUT FIVE MILES FROMTHE AIRFI ELD AND RETURNED BY THE LOCAL AUTHORITIES. THE ENGINE HAS BEEN REMOVED AND WILL BE RETURNE D TO HONEYWELL FOR REPAIR AND 2 L 7 2 4F 4 F RT A21EA E6NE 2002102900141 20021029 00141 EU 2002 10 29 CA021008005 1 20021004 A 3097 3E23604 WIRE HARNESS PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL PROP DEICE SHORTED W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) PROPELLER DE-ICE WAS REPORTED AS FAILED BY FLIGHT CREW. DEFECT WAS DISCOVERED AS AN INTERMITTENT OPEN CIRCUIT ON T WO OF THE DEICE HARNESS LEADS BETWEEN THE SPINNER BACKPLATE AND THE DEICE BOOT. ALTHOUGH THE SYSTEM TESTED OK WITH THE B LADES IN FEATHER, IT WAS DETERMINED THAT AS THE BLADES TRAVELLED TOWARDS FINE PITCH, THE HARNESS WOULD MOVE TO EXHIBIT T HE INTERMITTENT OPEN CIRCUIT.THE DEICE WARNINGLIGHT WOULD SUBSEQUENTLY ILLUMINATE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002120400111 20021204 00111 EU 2002 12 4 02FDEA00776 1 20021029 A 5230 A5237204320000 SKIN AIRBUS 310 A310 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 FOUND CORROSION AT FWD CARGO DOOR INNER SKIN LWR SECTION AT FR 20. R&R SKIN PER EA 6-5230-66467. 2 L 7 2 4F RT A35EU 2002102900145 20021029 00145 SO 2002 10 29 CA021009028 1 20021009 A 8120 TURBOCHARGER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE LEAKING W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA (CAN) TURBOCHARGER LEAKING OIL AT BOTTOM OF THE UNIT. 1 L 7 2 3O 3 O A20SO E14EA 2002102900146 20021029 00146 NM 2002 10 29 AWXA200201055 1 20021005 A 5320 65479573 WEB BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 0 0 25400 MCN - MAJOR REPAIR - DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND AROUND NUTPLATES OF SILL WEB ON AFT CARGO DOOR C UTOUT FRAME STRUCTURE BS 794 - BS 840, STR 24 R/H. MAINTENANCE REMOVED DAMAGED WEB, FABRICATED A NEW REPLACEMENT WEB, AN D INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05, PG. 1-4, FIG. 2, AND PG. 5 & 40, FIG. 9. 2 L 7 2 4F RT A16WE 2002102900147 20021029 00147 NM 2002 10 29 AWXA200201057 1 20021003 A 5330 654549611 SKIN BOEING 737 737277 1384570 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 0 0 22651 YVR - MAJOR REPAIR - DURING C-20 CHECK PITTING CORROSION WAS FOUND ON THE L/H WING LOWER SKIN AT THE #2 TRAILING EDGE FL AP TRACK ATTACH POINT WS 254 L/H. MAINTENANCE PREPARED AREA AT L/H WING LOWER SKIN FLAP TRACK ATTACH POINT WS 254 L/H; R EMOVED CORROSION; TREATED AREA; FABRICATED A TAPERED SHIM; AND INSTALLED REPAIR PART IAW AWA E.R. 15-5724-02294-TB2. 2 L 7 2 4F RT A16WE 2002103000001 20021030 00001 SO 2002 10 30 C2XA02SH116 1 20021030 A 5300 14522459003 SUPPORT EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14933 145018 SHV-DURING C CHECK THE SUPPORT RAMP ON CENTER OMEGA BEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO HAVE CORROSION. MAINTENA NCE REMOVED DAMAGE AND REPLACE SUPPORT RAMP IAW EMB SRM51-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002103000002 20021030 00002 SO 2002 10 30 C2XA02SH117 1 20021030 A 5300 14521725401 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14933 145018 SHV- DURING C CHECK NUTPLATES WITH CORROSION WERE FOUND JUST FOWARD OF SERVICE DOOR THRESHOLD. MAINTENANCE REMOVED DAMA GE AND REPLACED AFFECTED SILL IAW EMB SRM 51-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002103000003 20021030 00003 SO 2002 10 30 C2XA02SH118 1 20021030 A 5300 14520609001 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14933 145018 SHV-DURING C CHECK LEFT HAND SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 23 AND 24. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002103000004 20021030 00004 SO 2002 10 30 C2XA02SH119 1 20021030 A 5300 14000492401 BEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14933 145018 SHV-DURING C CHECK CROSS BEAM BETWEEN FRAMES 23 AND 24 FROM CENTER OMEGA BEAM T O RIGHT HAND OMEGA BEAM WAS FOUND TO HAV E CORROSION. MAITENANCE REMOVED DAMAGE AND REPLACED AFFECTED CROSS BEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVE D TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002103000006 20021030 00006 NM 2002 10 30 CA021010005 1 20020927 A 3246 50078902 WHEEL DOUG MD80 MD83 3023681 NM MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING THE OVERHAUL OF THE MAIN WHEEL ASSEMBLY THE NDT INSPECTION WAS DETECTED A CRACK ON THE UPPER SPOKE AREA. TH E CRACK WAS UNDETECTABLE WITH THE DYE PENETRANT, BUT DETECTABLE WITH EDDY CURRENT.- NOREPAIR POSSIBLE. 2 L 7 2 4F RT 2002103000009 20021030 00009 NM 2002 10 30 CA021011003 1 20021010 A 2910 82950010193 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) HYDRAULIC FLUID LEAKING FROM DRAIN HOLE IN BELLY RT SIDE AT CENTER FUSELAGE. LEAK TRACED TO PIN HOLE ON FIRST ELBO W ON INBOARD END OF R/H WING FLIGHT SPOILER UNLOADING TUBE ASSY. LINE REPLACEDIPC 29-00-00 FIG 60 ITEM 150. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002103000010 20021030 00010 NM 2002 10 30 CA021015001 1 20021011 A 2160 CONTROL VALVE BOEING 767 767333 1385301 NM PWA 4060 PW4060 52119 NE CABIN TEMP MALFUNCTIONED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA (CAN) ON DESCENT INTO YYZ (15000) A STRONG ODOR WAS NOTED AND REPORTED THROUGHOUT THE AIRCRAFT. ODOR WAS NAUSEOUS AND D ISSIPATED AFTER RECIRCULATION FAN TURNED ON. DURING INSPECTION OF AIRCRAFT FOUND THE LT PACK TEMP CONTROL VALVE MOTOR RU NNING CONSTANTLY TO THE CLOSED POSITION AND WOULD NOT SHUT OFF. TEMP CONTROL VALVE REPLACED PER AMM. AND OTHER AREAS OF AIRCRAFT INSPECTED NO FURTHER DEFECTS FOUND. 2 L 7 2 4F 4 F RT A1NM E24NE 2002103000011 20021030 00011 EA 2002 10 30 CA021015003 1 20021013 A 5312 MM67036182 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE NR 2 HYDRAULIC EDP PRESSURE LINE WAS LOOSE FROM THE BACK OF THE PRESSURE BULKHEAD, DECIDED TO OPEN THE CARGO A REA TO SEE IF IT COULD BE RETORQUED. HOLE ON THE PRESSURE BULKHEAD WAS ELONGATED AND THREAD OF THE HYDRAULIC FITTING WE RE WORN NDT INSPECTOR CONFIRMED THE PRESSURE BULKHEAD WAS CRACKED 1.556 INCH FROM THE PRESSURE LINE TO THE CASE DRAINLI NE. THE CRACK STOPPED 0.350 INCH BEFORE THE HOLE OF CASE DRAIN LINE. REPAIR WAS ISSUED TO REINFORCED THE BULKHEAD. THE B ULKHEAD FITTING AND LINE REPLACED. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002103000012 20021030 00012 EA 2002 10 30 CA021015005 1 20021012 A 7500 6019801455 LINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE UNAPPROVED PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 13997 (CAN) AIRCRAFT HAS BEEN EXPERIENCING HIGH ITT INDICATION ON THE LT ENGINE SINCE ITS ACCEPTANCE CHECK.4 LEAKS AT DIFFEREN T LOCATION FROM THE 10 STAGE WERE FOUND. ONE WAS AT THE RT 10TH STAGE MANIFOLD PRESSURE SENSING LINE. THE LINE WAS NOT S ITTING PROPERLY AND SEEMED TO BE INSTALLED UNDER TENSION. THE MECHANICS COULD NOT TIGHTEN THE LINE ANY FURTHER. IT WAS THEN DECIDED TO REMOVE THE LINE AND FOUND OUT THAT THIS PART WAS A BOGUS PART MADE OF ALUMINUM WITHOUT ANY PART NUMBER S TAMPED ON IT. A NEW LINE WAS INSTALLED AS PER THE AIRCRAFT MAINTENANCE MANUAL AND NO FURTHER LEAKS WERE FOUNDS AFTER RE PLACEMENT. 2 L 7 2 4F 4 F RT A21EA E15NE 2002103000013 20021030 00013 GL 2002 10 30 CA021015008 1 20021010 A 2797 GT41559009 WIRE GT41559009 BOMBDR BD700 BD7001A10 1390006 GL RROYCE BR700 BR700710A220 09500 NE SFCU PINCHED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION NR NOT REPORTED 1 CA 0109 (CAN) DURING RETURN TO SERVICE TESTING AFTER A MAINTENANCE DOWNTIME, THE FLAPS WERE OPERATED AND WHEN THEY REACHED APPRO XIMATELY 30 DEGREES, AN AVIONICS SMOKE MESSAGE WAS OBSERVED. PRIOR TO POWER BEING REMOVED FROM THE A/C, A SLAT/FLAP HAL F SPEED MESSAGE WAS ALSO POSTED. SUBSEQUENTLY IT WAS DISCOVERED THAT THE CIRCUIT BREAKER G9 (SFCU) HAD TRIPPED. TROUBL ESHOOTING THE MESSAGES LED THE TECHNICIAN TO INSPECT THE SFCU IN THE AVIONICS BAY. THE INSULATION BLANKET AROUND THE SFC U WAS FOUND TO BE HEAT DAMAGED AND SOME SOOT WAS FOUND AT THE SFCU COOLING VENTS AS WELL ON THE SURROUNDING STRUCTURE & DUCTING. PRELIMINARY REPORTS INDICATE AN INTERNAL PINCHING OF A WIRE IN THE CURRENT SENSOR CIRCUIT. 2 L 7 2 4F 4 F RT T00003NY E00061EN 2002103000015 20021030 00015 NM 2002 10 30 CA021016001 1 20021011 A 5414 311T306558 PANEL BOEING 767 7673Y0 NM PWA 4060 PW4060 52119 NE RT NACELLE MISSING W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING WALK AROUND FOUND PYLON PANEL MISSING RT ENGINE OUTBOARD SIDE. NEW PANEL INSTALLED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002103000016 20021030 00016 SW 2002 10 30 CA021016003 1 20020930 A 6320 B4429SP CHIP DETECTOR BELL 212040001149 BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE TRANSMISSION FLAKING W K NONE O OTHER IN INSP/MAINT 1 CA ABW01727 (CAN) TIN PLATING OF CHIP DETECTOR POLES FOUND TO BE FLAKING OFF, POTENTIAL FOR ERRONEOUS INDICATION. PART REPLACED WITH SERVICEABLE UNIT AND SENT TO MANUFACTURER FOR ANALYSIS. 1 G 7 1 4U 4 U H4SW E22EA 2002103000017 20021030 00017 NE 2002 10 30 CA021016004 2 20020702 A 7532 8550158260 BLEED VALVE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) BLEED VALVE LIGHT STAYS ON, VALVE STAYS OPEN IN FLIGHT. BLEED VALVE REPLACED WITH AIRWORTHY PART, DEFECT CORRECTED . 1 G 7 1 3U 3 U NC H9EU E19EU 2002103000018 20021030 00018 EU 2002 10 30 CA021016005 1 20020418 A 2822 P94B12209 PUMP SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE FUEL BOOST FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) NR 2 FUEL BOOST PUMP LIGHT ILLUMINATED. FAULTY (NO PRESSURE) BOOST PUMP REPLACED WITH AIRWORTHY PART. 1 G 7 1 3U 3 U H9EU E19EU 2002103000019 20021030 00019 SW 2002 10 30 CA021016006 1 20020424 A 2822 1C2710 PUMP BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FUEL BOOST FAILED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION DE DESCENT 1 CA (CAN) A FUEL PUMP FAILURE LIGHT ILLUMINATED ON CAUTION PANEL DURING FLIGHT. IT WAS DETERMINED THAT THE AFT FUEL PUMP HAD FAILED. FAULTY CARTRIDGE WAS REPLACED WITH AIRWORTHY UNIT, PUMP PRESSURES CORRECTED. 1 G 7 1 3U 3 U H2SW E4CE 2002103000020 20021030 00020 SW 2002 10 30 CA021016008 1 20020720 A 6320 2060315093 PIN BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL TRANSMISSION UNSTAKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) POST FLIGHT INSPECTION REVEALED THE SPHERICAL BEARING ON THE DRAG PIN ASSEMBLY HAD BECOME PARTIALLY UNSTAKED. REPL ACEMENT PART INSTALLED. 1 G 7 1 3U 3 U H2SW E4CE 2002103000021 20021030 00021 EU 2002 10 30 CA021016011 1 20020716 A 7714 0177555170 TACH GENERATOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED W O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA (CAN) BLEED VALVE OPEN IN FLIGHT ABOVE 97 PERCENT NG AND ON LANDING. FAULTY TACH BOX REPLACED WITH AIRWORTHY PART. NO F URTHER PROBLEMS. 1 G 7 1 3U 3 U NC H9EU E19EU 2002103000022 20021030 00022 EU 2002 10 30 CA021016012 1 20020723 A 7714 0177555170 TACH GENERATOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED W O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA (CAN) BLEED VALVE OPEN IN FLIGHT ABOVE 97 PERCENT NG AND ON LANDING. FAULTY TACH BOX REPLACED WITH AIRWORTHY PART. NO F URTHER PROBLEMS. 1 G 7 1 3U 3 U NC H9EU E19EU 2002103000023 20021030 00023 EU 2002 10 30 CA021016013 1 20020726 A 7714 0177555170 TACH GENERATOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED W O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA (CAN) BLEED VALVE DOES NOT CLOSE WHEN REQUIRED. FAULTY TACH BOX REPLACED WITH AIRWORTHY PART. NO FURTHER PROBLEMS. 1 G 7 1 3U 3 U NC H9EU E19EU 2002103000025 20021030 00025 NE 2002 10 30 CA021016015 2 20020629 A 7412 ABG6766000 EXCITER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE INTERMITTENT W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) IGNITION INTERMITTENT FROM ONE IGNITION CHANNEL. FAULTY HIGH ENERGY GENERATOR REPLACED WITH NEW PART, STARTS CORRE CTED. 1 G 7 1 3U 3 U NC H9EU E19EU 2002103000026 20021030 00026 NE 2002 10 30 CA021016016 2 20020627 A 7412 ABG6766000 EXCITER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE INTERMITTENT W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) POOR IGNITION ON ENGINE STARTS. FAULTY HIGH ENERGY GENERATOR REPLACED WITH NEW PART, STARTS CORRECTED. 1 G 7 1 3U 3 U NC H9EU E19EU 2002103000027 20021030 00027 EU 2002 10 30 CA021016017 1 20020622 A 2822 P94B12203C PUMP SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL BOOST FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) LOW FUEL PRESSURE INDICATED. FUEL BOOST PUMP GROWLING, LOW OUTPUT, PRESSURE AND VOLUME CONFIRMED. PUMP REPLACED WI TH AIRWORTHY UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002103000028 20021030 00028 EU 2002 10 30 CA021016018 1 20020726 A 2822 P94B12203 PUMP SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL BOOST FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) LOW FUEL PRESSURE INDICATED. FUEL BOOST PUMP LOW OUTPUT PRESSURE AND VOLUME CONFIRMED. PUMP REPLACED WITH AIRWORTH Y UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002103000031 20021030 00031 EU 2002 10 30 CA021016021 1 20020613 A 7714 0177555170 TACH GENERATOR SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED W O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA (CAN) BLEED VALVE NOT CLOSING AT 97 PERCENT. BLEED VALVE OPERATION INTERMITTENT. TACH BOX REPLACED, OPERATIONS NOW CORRE CTED. 1 G 7 1 3U 3 U H9EU E19EU 2002103000032 20021030 00032 2002 10 30 CA021016022 4 20021009 A 2565 D36179107 LOCK AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE SLIDE ASSY FAILED W K NONE O OTHER IN INSP/MAINT 1 CA A5635 (CAN) DURING DEPLOY TEST OF WING SLIDE ENCLOSURE LT DOOR FAILED TO RELEASE CENTER LOCK. DOOR PARTIALLY OPENED AND TORE CENTER LOCK OFF DOOR AND THEN FULLY DEPLOYED. SLIDE AND ENCLOSURE REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2002103000033 20021030 00033 EU 2002 10 30 CA021016023 1 20020714 A 7714 0177555170 TACH GENERATOR SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) BLEED VALVE WILL NOT CLOSE. TROUBLESHOOTING REVEALED FAULTY TACH BOX. TACH BOX REPLACED, OPERATIONS NOW CORRECT. 1 G 7 1 3U 3 U H9EU E19EU 2002103000034 20021030 00034 EU 2002 10 30 CA021016024 1 20020808 A 7714 0177555170 TACH GENERATOR SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED W O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA (CAN) BLEED VALVE WILL NOT CLOSE. TROUBLESHOOTING REVEALED FAULTY TACH BOX. TACH BOX REPLACED, OPERATIONS NOW CORRECT. 1 G 7 1 3U 3 U H9EU E19EU 2002103000035 20021030 00035 EA 2002 10 30 CA021016025 2 20021007 A 7200 3020807 CASE PWC DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A20 52043 EA GAS GENERATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION, CRACK FOUND ALONG WELDED SEAM. 1 H 7 2 3T 3 T RT A9EA E4EA 2002103000036 20021030 00036 SO 2002 10 30 CA021016026 2 20020911 A 8520 646778 CONNECTING ROD CESSNA 185 A185F 2072821 CE CONT O520 IO520D 17032 SO ENGINE BROKEN W A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CA (CAN) PILOT EXPERIENCED STRANGE NOISE AND VIBRATION FROM ENGINE WHILE IN CRUISE. AIRCRAFT WAS LANDED AND TOWED TO SAFE S TORAGE. ENGINE REPLACED. 1 H 7 1 3O 3 O 3A24 E5CE 2002103000037 20021030 00037 EA 2002 10 30 CA021016027 1 20021013 A 6120 2345789 SWITCH DHAV DHC6 DHC6100 2802610 EA PWA PT6 PT6A20 52043 EA HARTZL HCB3T HCB3TN3 GL NR 2 PROP FAILED W E D ENGINE SHUTDOWN RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA (CAN) AIRCRAFT WAS TAXIING AWAY FROM DOCK WHEN FLIGHT CREW DEMANDED REVERSE POWER FROM NR 2 ENGINE. IT FAILED TO RESPON D AND AIRCRAFT HIT THE DOCK WITH FRONT OF RT FLOAT. FAILURE OF PROP TO RESPOND TO POWER LEVER INPUT IS ATTRIBUTED TO TH E PROP OVERSPEED TEST SWITCH FAILING IN THE ON POSITION. 1 H 7 2 3T 3 T RT A9EA E4EA 6 C P15EA 2002103000038 20021030 00038 EU 2002 10 30 CA021016028 1 20020925 A 5310 DOOR FRAME SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) 32.5 INCH CRACK FOUND ALONG ENTIRE LT DOOR POST. 1 G 7 1 3U 3 U H9EU E19EU 2002103000039 20021030 00039 EA 2002 10 30 CA021016029 2 20021003 A 8500 LTIO540J3BD ENGINE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2A GL RIGHT MAKING METAL W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) FIRST FLIGHT OF THE DAY 2.2 HOURS DURATION WAS WITHOUT INCIDENT, ENGINE TRENDS PERFORMED & NOTHING NOTED UNUSUAL. SECOND FLIGHT, SHORTLY AFTER CRUISE POWER WAS SET AT 6500 FT, OIL PSI DROPPED TO 50 PSI, OIL TEMP APPROX 245 DEGREES & M /P DROPPED APPROX 10 INCHES. THEN OIL PSI DROPPED RAPIDLY TO 40 PSI. A STANDARD PRECAUTIONARY SHUTDOWN PERFORMED. AIRCRA FT LANDED WITHOUT INCIDENT. MAINTENANCE VISUAL & GROUND FUNCTION TEST PERFORMED. RT ENGINE OIL PSI OBSERVED APPROX 20 PS I LOW COMPRESSION LEAK DOWN C/O NO DEFECTS NOTED. OIL FILTER INSPECTION REVEALED METAL CONTAMINATION. SUCTION SCREEN INS PECTION REVEALED 0.3 OZ OF SOFT, SHINY BEARING LIKE FLAKES. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2002103000040 20021030 00040 SO 2002 10 30 CA021016031 1 20021002 A 2730 710563 SPRING PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON DAILY INSPECTION NOTICED ABNORMAL FLIGHT CONTROL 'FEEL' ON ELEVATOR. INSPECTION REVEALED BROKEN ELEVATOR SPRIN G. SPRING REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 2002103000041 20021030 00041 CE 2002 10 30 CA021016032 1 20020917 A 7120 265102215 MOUNT CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE MCAULY 3AF34C 3GFR34C703 GL ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACK FOUND IN LOWER CORNERS OF ENGINE MOUNT RING. 1 H 7 1 3T 3 T A37CE E4EA 5 C P60GL 2002103000042 20021030 00042 EA 2002 10 30 CA021016033 1 20021009 A 5711 2151002468 SPAR CNDAIR CL215 CL2151A10 1900320 EA WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON COMPLETION OF S/B 215-A463R3 (FRONT SPAR) A REJECTABLE INDICATION AT 4-7 IN THE DEFECT WINDOW 85 PERCENT SCRE EN HEIGHT WAS DISCOVERED IN THE LT FWD LOWER SPAR CAP. EDDY CURRENT & LPI CONFIRMED THE INDICATION. 1165 LOADS SINCE LAS T INSPECTION 2 H 7 2 4R RT A14EA 2002103000043 20021030 00043 CE 2002 10 30 CA021016034 1 20021001 A 7931 311360601 SLEEVE PWC 3102028 BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA COMPRESSOR FRACTURED W E A ENGINE SHUTDOWN UNSCHED LANDING K R J FLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA PCE32570 (CAN) PILOT REPORTED OIL PRESSURE FLUCTUATING.REDUCED POWER, OIL PRESSURE CONTINUED TO DECREASED. SHUT DOWN AND SECURED ENGINE. LANDED WITHOUT INCIDENT. OPENED AGB WITH STANDARD AERO REPRESENTATIVE. 2 L 7 2 4T 4 T RT A24CE E4EA 2002103000044 20021030 00044 CE 2002 10 30 CA021016035 1 20021009 A 5532 SKIN CESSNA 500 S550 2076607 CE PWA JT15 JT15D4 52112 NE VERTICAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 14151 14151 (CAN) PHASE 49 SKIN JOINT EDDY CURRENT INSPECTION INDICATED AN ANAMOLY AT FS 287.78 WL 146.6. FURTHER INVESTIGATION USIN G A 5000X MICROSCOPE REVEALED A 1 INCH LONG GOUGE AND CRACK IN SKIN DOUBLER BETWEEN SKIN EDGES. AIRCRAFT FERRIED UNPRESS URISED TO WICHITA CITATION SERVICE CENTER FOR REPAIR. 1 L 7 2 4F 4 F RT A22CE E1NE 2002103000045 20021030 00045 SO 2002 10 30 CA021016036 2 20020828 A 8530 EXHAUST VALVE CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO RT ENGINE STUCK W E A ENGINE SHUTDOWN UNSCHED LANDING A E J FLAME/FIRE VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CA (CAN) VIBRATION ON RT ENGINE WITH FIRE, ENGINE FEATHERED. - FUEL LINE MANIFOLD VALVE TO NOZZLE BROKEN DUE TO STICKING EX HAUST VALVE ON CYLINDER NR 6. THE EXHAUST VALVE WAS DISMANTLED FOR CLEANING. A REEMER (PULL THROUGH) WAS PASSED THROUG H THE VALVE GUIDE AND THE VALVE WAS FOUND TO MEET THE MANUFACTURER'S STANDARDS. 1 L 7 2 3O 3 O 3A10 E5CE 2002103000046 20021030 00046 SO 2002 10 30 CA021016037 1 20021003 A 3320 5500455 SWITCH EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA LIGHT FAILED W H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CR CRUISE 1 CA (CAN) GAP SHORT CAUSED BY POSSIBLE LOOSE AIR COLLECTOR WHEN OPEN/SHUT BY PASSENGER, COMING IN CONTACT WITH LIGHT ASSEM BLY. A SMALL PLASTIC TONGUE PROTRUDING FROM SWITCH TO ISOLATE N & P PROBES / LUGS ON SWITCH MAY HAVE BEEN BROKEN. PO SSIBLE SIMPLY INSIDE OF SWITCH, WORN MECHANISM. NO RECORD ON THIS PARTICULAR SWITCH FOR INSTALLATION. 1 L 7 2 4T 4 T A21SO E4EA 2002103000047 20021030 00047 EA 2002 10 30 CA021017001 1 20021011 A 5312 MM67036182 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INCORPORATION OF THE SB 670BA3-003 FOUND FOUR (4) CRACKS IN THE AFT PRESURE BULKHEAD WEB FS=1098.2, STR 8-9 LT AND RT. THE CRACKS ARE CONCENTRATED AROUND THE HOLES IN THE WEB FOR THE HYDRAULIC LINES (SEE ATTACHED DIGITAL PHOTO S). LHS-TWO CRACKS, ONE IS 34 MM LONG AND THE SECOND 4 MM LONG RHS-TWO CRACKS, ONE IS 65 MM LONG AND THE SECOND 33MM LON G 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002103000048 20021030 00048 EA 2002 10 30 CA021017002 1 20021016 A 2710 AILERON CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE WINGS FROZEN W O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 CA (CAN) AILERONS BECAME VERY STIFF AND WOULD MOVE ONLY UNDER HIGH LOADING, SUSPECT FROZEN CONTROLS DESCENDING OUT OF 6000 FEET CONTROLS BECAME NORMAL. LT AND RT AILERON REAR QUADRANTS CLEANED AND SPRAY WITH WATER REPELLANT. OPERATIONAL TEST CARRIED OUT AS. UNABLE TO FAULT CONSIDERED SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002103000049 20021030 00049 NM 2002 10 30 CA021017003 1 20020922 A 2197 WIRE DHAV DHC8 DHC8301 1386003 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE CARGO BAY ARCED W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) JUST BEFORE START, SMOKE WARNING OF APPROXIMATELY 3-4 SECONDS DURATION. REPORTED NO SMOKE IN THE REAR HOLD BUT F AINT 'RUBBERY' BURNING ODOR. WARNING RECURED SEVERAL TIMES. UNLOADED HOLD AND SCANNED BAGGAGE AND A/C WITH THERMAL IMAG ING CAMERA. 'HOT SPOT' OF APPROX 40C INCREASING FOUND UNDER FLOOR OF CABIN UNDER ROW 14. FLOOR LIFTED AND FAULT TRACED T O LOOSE CONNECTION OF GROUND CABLES FOR RECIRCULATION FAN. MAINTENANCE ENGINEERS FOUND THE GROUND BOLT SECURING THE GRO UND CABLES TO THE STRUCTURE WAS NOT SECURE DUE TO GROUND BOLT TOO LONG. EVIDENCE OF ARCING WAS ALSO FOUND ON THE WASHE RS. GROUND BOLT REMOVED, CLEANED AND INSPECTED. NO VISIBLE DAMAGE. TWO EXTRA THREADS CUT ONTO THE BOLT AND CABLES SECURE 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002103000050 20021030 00050 CE 2002 10 30 NSVA200200002 1 20021030 A 5100 NA STRINGER BEECH 1900D BEECH 1900 1900D 1154162 CE CRACKED A NSVA K NONE O OTHER UK UNKNOWN 1 EA 27 UE221 14073 UE221 UE221 Nom-routine work card inspection- frame at FS 456 has a crack that runs through a rivit hole to the "cutout" where strin ger #10 intersects. 2 L 7 2 4T RT A24CE 2002103000051 20021030 00051 NM 2002 10 30 SWAA022478 1 20021018 A 5330 6545785 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUT CRACKED AT RT WINDOW NR 11. REPAIRED FRAME PER BFG ER. 2 L 7 2 4F RT A16WE 2002103000052 20021030 00052 NM 2002 10 30 SWAA022479 1 20021019 A 5311 65479602 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 081SW 22730 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR CUTOUT FRAME CRACKED AT INBD FLANGE. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F A16WE 2002103000053 20021030 00053 NM 2002 10 30 SWAA022480 1 20021019 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 081SW 22730 DURING SCHEDULED C4 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED (2 EA) AT THE 12 AND 6 O'CLOCK POSITIONS RADIATING FROM RIVETS AT THE PERIPHERY OF THE DOME. REPAIRED BULKHEAD PER SWA EA. 2 L 7 2 4F A16WE 2002103000054 20021030 00054 NM 2002 10 30 SWAA022481 1 20021018 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 102SW 23108 DURING SCHEDULED C1 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED (5 EA) ON WEBS THAT CONVERGE AT THE CENTER OF THE PRESS DOME. REPAIRED BULKHEAD PER SWA EA. 2 L 7 2 4F A16WE 2002103000055 20021030 00055 NM 2002 10 30 SWAA022484 1 20021022 A 5315 BAC1509 FLOORBEAM BOEING 737 7373TO 138447G NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 773, RBL 10 TO LBL 12. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002103000056 20021030 00056 NM 2002 10 30 SWAA022485 1 20021018 A 5520 183A300 HINGE BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED PM CHECK, SWA SI 11075-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE PER S RM. 2 L 7 2 4F RT A16WE 2002103000057 20021030 00057 NM 2002 10 30 SWAA022486 1 20021019 A 5330 654577677 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE BULGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN BULGED AT BS 727 + 15,STR 27R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2002103000058 20021030 00058 NM 2002 10 30 SWAA022489 1 20021018 A 3320 026405 RHEOSTAT BOEING 737 7372H4 138448C NM CABIN OVERTEMP A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 091SW 22963 SPARKS AND SMOKE AT FWD GALLEY WORK LIGHT SW. REMOVED AND REPLACED WORK LIGHT REHOSTAT AND REPAIRED WIRES PER MM. 2 L 7 2 4F A16WE 2002103000059 20021030 00059 NM 2002 10 30 SWAA022491 1 20021021 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 758SW 27873 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS NR 1, NR 2, NR 4, NR 5, NR 6, NR 8, NR 9 AND NR 22. REMOV ED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002103000060 20021030 00060 2002 10 30 SWAA022492 4 20021021 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002103000061 20021030 00061 2002 10 30 SWAA022495 4 20021021 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 FWD ENTRY DOOR EMERGENCY EVAC SLIDE VIEWING WINDOW LOOSE. SECURED VIEWING WINDOW PER MM. 2 L 7 2 4F RT A16WE 2002103000062 20021030 00062 NM 2002 10 30 SWAA022498 1 20021022 A 5520 65C25798 HINGE BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED C4 CHECK, FOUND PLAY AT RT ELEVATOR OTBD HINGE. SECURED RT ELEVATOR OTBD HINGE FITTING PER MM. 2 L 7 2 4F RT A16WE 2002103000063 20021030 00063 NE 2002 10 30 SWAA022499 2 20021021 A 7230 JT8D9A ENGINE BOEING 737 7372H4 138448C NM JT8 JT8D9A 52048 NE RT WING STALLED A SWAA K NONE R PARTIAL RPM/PWR LOSS AP APPROACH 1 SW 29 091SW 22963 707323 DURING APPROACH NR 2 ENGINE COMPRESSOR STALLED TWO TIMES IN SHORT SUCCESSION. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2002103000064 20021030 00064 NM 2002 10 30 SWAA022501 1 20021019 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002103000065 20021030 00065 NM 2002 10 30 SWAA022502 1 20021019 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4R, BS 597 AND BS 706. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002103000066 20021030 00066 NM 2002 10 30 SWAA022503 1 20021018 A 5720 115A8161 CASTING BOEING 737 7377H4 1384404 NM LT/RT WINGS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 712SW 27846 DURING SCHEDULED C4 CHECK, FOUND BOTH LT/RT WING FLAP CASTING CRACKED (BETWEEN FLAP AND AILERON) OTBD OF OTBD FLAP. REP AIRED CASTINGS PER SWA EA. 2 L 7 2 4F RT A16WE 2002103000067 20021030 00067 NM 2002 10 30 SWAA022505 1 20021020 A 5520 65C25798 HINGE BOEING 737 7377H4 1384404 NM LT/RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 784SW 29810 DURING SCHEDULED A1 CHECK, SWA SI 11038-55, BOTH LT/RT ELEVATOR NR 4 HINGES WORN. REMOVED AND REPLACED NR 4 LT/RT ELEVA TOR TAB HINGES PER MM. 2 L 7 2 4F RT A16WE 2002103000068 20021030 00068 NM 2002 10 30 SWAA022506 1 20021017 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C PLUS 15, STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002103000069 20021030 00069 NM 2002 10 30 SWAA022507 1 20021017 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 439, STR 14R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002103000070 20021030 00070 NM 2002 10 30 SWAA022508 1 20021017 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 489, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002103000071 20021030 00071 NM 2002 10 30 SWAA022525 1 20021025 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 402WN 29814 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002103000072 20021030 00072 2002 10 30 SWAA022526 4 20021025 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002103000073 20021030 00073 2002 10 30 SWAA022530 4 20021024 A 2565 65C19901 CABLE BOEING 737 7373K2 13844BA NM AFT SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002110100189 20021101 00189 NM 2002 11 1 SWAA022535 1 20021027 A 5753 6546434 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED C4 CHECK, FOUND RT INBD AFT T/E FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED RT INBD AFT T/ E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002103000074 20021030 00074 NM 2002 10 30 SWAA022536 1 20021026 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4R, BS 727E AND BS 727D + 10. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 2002103000075 20021030 00075 NM 2002 10 30 SWAA022537 1 20021026 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 14L, BS 370 AND BS 380. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 2002103000076 20021030 00076 NM 2002 10 30 SWAA022538 1 20021027 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 12, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002103000077 20021030 00077 NM 2002 10 30 SWAA022539 1 20021027 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM SKIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 11, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002103000078 20021030 00078 NM 2002 10 30 SWAA022540 1 20021027 A 5330 6545785 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUTS CRACKED AT LT WINDOWS NR 1, NR 2, NR 32, NR 3 AND NR 6. REPAIR ED FRAMES PER BFG ER AND SRM. 2 L 7 2 4F RT A16WE 2002103000079 20021030 00079 NM 2002 10 30 SWAA022541 1 20021027 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 11, STR 14L. REPAIRED SKIN PER BFG ER. 2 L 7 2 4F RT A16WE 2002103000080 20021030 00080 NM 2002 10 30 SWAA022542 1 20021027 A 5311 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CORRODED AT BS 827, WL 156 AND RBL 3. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002103000081 20021030 00081 NM 2002 10 30 SWAA022544 1 20021025 A 5312 6546568 BULKHEAD BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED C1 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED FROM A RIVET AROUND THE PERIPHERY OF THE PRESS DOME PLUG AT THE 5 O' CLOCK POSITION. REPAIRED BULKHEAD PER SWA EA. 2 L 7 2 4F A16WE 2002103000082 20021030 00082 NM 2002 10 30 SWAA022545 1 20021026 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 19L, BS 500B + 4 AND BS 500B + 7. REPAIRED SK IN PER SRM. 2 L 7 2 4F A16WE 2002103000083 20021030 00083 NM 2002 10 30 SWAA022546 1 20021025 A 5740 6582770 FITTING BOEING 737 7373H4 1384600 NM LT AND RT MLG W/ CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG WALKING BEAM FITTINGS CORRODED. REMOVED AND REPLACED BOTH LT A ND RT MLG WALKING BEAM FITTINGS PER MM. 2 L 7 2 4F RT A16WE 2002103000084 20021030 00084 NM 2002 10 30 SWAA022547 1 20021027 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT FWD AND AFT LOWER CORNERS OF THE AFT SVC DOOR CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002103000085 20021030 00085 NM 2002 10 30 SWAA022548 1 20021027 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER FWD CORNER OF AFT ENTRY DOOR. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2002103000086 20021030 00086 NM 2002 10 30 PCAA0210128 1 20021028 A 7931 PW12A ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT LEAKING A PCAA E ENGINE SHUTDOWN K FLUID LOSS DE DESCENT 1 EA 13 981HA 31547 2490 378 120709 LGA-BWI FLIGHT#3920. CREW REPORTED THAT WHILE ON DECENT THEY NOTICED LOW OIL PRESSURE ON #1 ENGINE, OIL PRESSURE LIGHT I LLUMINATED. OIL PRESSURE DID NOT GO TO ZERO. WHEN LIGHT ILLUMINATED ENGINE WAS SECURED. MAINTENANCE REPLACED PROPELLER S HAFT SEAL AND ADDED SPACERS TO THE SEAL RETAINER. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002103000087 20021030 00087 2002 10 30 SWAA022520 4 20021023 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002103000088 20021030 00088 NM 2002 10 30 SWAA022524 1 20021023 A 5520 65C25798 HINGE BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED A2 CHECK, FOUND RT ELEVATOR TAB NR 2 AND NR 3 HINGE ATTACH POINTS WORN. REMOVED AND REPLACED NR 2 AND NR 3 HINGES PER MM. 2 L 7 2 4F RT A16WE 2002103000089 20021030 00089 NM 2002 10 30 SWAA022513 1 20021023 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 917, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002103000090 20021030 00090 NM 2002 10 30 SWAA022514 1 20021021 A 5311 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L AND STR 4L. REMOVED AND REPLACED SHE AR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002103000091 20021030 00091 NM 2002 10 30 SWAA022517 1 20021022 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 24L, BS 727E AND BS 737. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002103000092 20021030 00092 NM 2002 10 30 ASAA0210082 1 20020417 A 5310 6546534 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 520, STRINGER 28R CORRODED. REPAIRED DENT PER SRM. (M) 2 L 7 2 4F A16WE 2002103000093 20021030 00093 NM 2002 10 30 ASAA0210083 1 20020417 A 5330 6573746 SKIN BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 PAE - DURING SCHEDULED C-CHECK, FOUND AFT ENTRY DOOR (L2) SKIN PANEL CRACKED AT BS 986, STRINGER 7L-8L CRACKED. REPAIRE D DENT PER SRM. (M) 2 L 7 2 4F A16WE 2002103000094 20021030 00094 NM 2002 10 30 ASAA0210157 1 20020627 A 5330 6545800 SKIN BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 22577 SEA - FUSELAGE SKIN CRACKED AT THE R2 DOOR LOWER FORWARD CORNER. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2002103000095 20021030 00095 NM 2002 10 30 ASAA0210158 1 20020709 A 5311 65C33722 FRAME BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING INSPECTION, FOUND CHORD AT BS 727, RBL 45 - RBL 47 CRACKED. REMOVED AND REPLACED CHORD PER EA. (M) 2 L 7 2 4F RT A16WE 2002103000096 20021030 00096 NM 2002 10 30 ASAA0210159 1 20020709 A 5311 65C33722 FRAME BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING INSPECTION, FOUND CHORD AT BS 727, LBL 24 CRACKED. REMOVED AND REPLACED CHORD PER EA. (M) 2 L 7 2 4F RT A16WE 2002103000097 20021030 00097 NM 2002 10 30 ASAA0210160 1 20020709 A 5314 KEELBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING INSPECTION, FOUND KEEL BEAM AT BS 727 PLUS 3, LBL 6.3 CORRODED. REMOVED AND REPLACED DAMAGED SECTION PER E A. (M) 2 L 7 2 4F RT A16WE 2002103000098 20021030 00098 NM 2002 10 30 ASAA0210161 1 20020709 A 5312 6546547 PRESSURE PANEL BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING INSPECTION, FOUND BULKHEAD WEB AT BS 727, LBL 67 CRACKED. REPAIRED BULKHEAD WEB PER EA. (M) 2 L 7 2 4F RT A16WE 2002103000099 20021030 00099 NM 2002 10 30 ASAA0210162 1 20020709 A 5313 BAC1498117 STRINGER BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING INSPECTION, FOUND STRINGER 21L AT BS 727 PLUS 4, CORRODED. REMOVED AND REPLACED STRINGER PER SRM. (M) 2 L 7 2 4F RT A16WE 2002103000100 20021030 00100 2002 10 30 CA021018002 4 20021002 A 8300 5001T90G06 BEARING SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE ACC GEARBOX MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 295291 (CAN) ENGINE RECEIVED FOR METAL CONTAMINATION. INVESTIGATION REVEALED A FUZZ LIKE MATERIAL PRESENT ON AGB CHIP DETECT OR. MATERIAL SIMILAR TO THAT FOUND WHEN GEARS IN THE AGB IS WEARING ABNORMALLY. NR 2 BEARING SUMP MAGNETIC PLUG WAS FOU ND FREE OF CONTAMINATION. NR 3 BEARING AND POWER TURBINE MAGNETIC PLUGS BOTH HAD TRACES OF THE SAME TYPE MATERIAL. OIL FILTER WAS DISMANTLED AND FOUND TO HAVE MINOR NON-FERROUS CONTAMINATION. ENGINE LUBE PUMP WAS INSPECTED AND NO FAULT FO UND. FRONT FRAME ADU WAS REMOVED AND BEVEL GEAR BEARINGS WERE BOTH FOUND WORN. ACCESSORY GEARBOX WAS REMOVED FOR FUR THER INVESTIGATION. BOTH PINION GEAR BEARINGS WERE WORN AND HAD BLUE DISCOLORATION SIMILAR TO THE COLOR SUBJECTED TO O 2 G 7 2 4U 4 U 1H15 1E3 2002103000101 20021030 00101 NM 2002 10 30 ASAA0210163 1 20020709 A 5330 6545776536 SKIN BOEING 737 737298C 1384490 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING INSPECTION, FOUND SKIN PANEL AT BS 727 PLUS 6, STRINGER 27L GOUGED. REMOVED AND REPLACED DAMAGED SECTION O F SKIN PANEL PER EA. (M) 2 L 7 2 4F RT A16WE 2002103000102 20021030 00102 EU 2002 10 30 CA021021002 1 20020918 A 6320 463802024 BEARING BOLKMS 105 BO105CBS 5626008 EU TRANSMISSION PEELING W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) BEARING OUTER RACE PEELING/SPALLING. METAL PARTICLES FROM BEARING DAMAGED INPUT PINION . 1 G 7 2 3U NC H3EU 2002103000103 20021030 00103 NM 2002 10 30 ASAA0210164 1 20020709 A 5320 BAC1518393 STIFFENER BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING INSPECTION, FOUND VERTICAL STIFFENER AT BODY STATION 727, LBL 40 CORRODED. REMOVED AND REPLACED STIFFENER PER SRM. (M) 2 L 7 2 4F RT A16WE 2002103000104 20021030 00104 NM 2002 10 30 ASAA0210165 1 20020709 A 5314 6562125 KEELBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING INSPECTION, FOUND KEEL BEAM AT BS 727 PLUS 17, STRINGER 27L CORRODED. REMOVED AND REPLACED SECTION OF KEEL BEAM PER EA. (M) 2 L 7 2 4F RT A16WE 2002103000105 20021030 00105 EU 2002 10 30 CA021021003 1 20020828 A 6320 4619312050 BEARING 4638001004 BOLKMS 105 BO105CBS 5626008 EU ACCESSORY DRIVE PEELING W K NONE O OTHER IN INSP/MAINT 1 CA 622 (CAN) BEARING PITTED AND PEELING 1 G 7 2 3U NC H3EU 2002103000106 20021030 00106 NM 2002 10 30 ASAA0210166 1 20020709 A 5314 6562125 KEELBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - DURING INSPECTION, FOUND KEEL BEAM AT BS 727 PLUS 10, STRINGER 27L CORRODED. REMOVED AND REPLACED SECTION OF KEEL BEAM PER EA. (M) 2 L 7 2 4F RT A16WE 2002103000107 20021030 00107 NM 2002 10 30 ASAA0210168 1 20020717 A 5210 6529994 GUIDE BOEING 737 737290C 138448V NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 ANC - L1 DOOR DIFFICULT TO CLOSE. ADJUSTED UPPER GUIDE ARM AND LUBED HINGES, THEN OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 2002103000108 20021030 00108 EU 2002 10 30 CA021021004 1 20020828 A 6320 4638302023 BEARING 4638001001 BOLKMS 105 BO105CBS 5626008 EU INPUT PINION MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 1249 (CAN) RECEIVED WITH REPORT OF METAL CONTAMINATION. TEARDOWN REVEALED SUBJECT BEARING HAD PEELING ON ONE BALL ONLY. ARE A OF MATERIAL LOSS WAS 30 PERCENT. 1 G 7 2 3U NC H3EU 2002103000109 20021030 00109 EU 2002 10 30 CA021021005 1 20021020 A 3340 LENS BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE STROBE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AFTER A/C SHUTDOWN, PILOT NOTICED ANTI-COLLISION BEACON LENS BROKEN, WITH TOP PORTION MISSING BUT BASE STILL INTAC T. MAINTENANCE NOTIFIED AND INSPECTION OF TAIL ROTOR SYSTEM AND BLADES CARRIED OUT, NO DAMAGE FOUND. LENS DAMAGE APPAREN TLY CAUSED BY OVERTIGHTENED MOUNTING CLAMP AFTER RECENT REPLACEMEN T 8.8 HOURS PRIOR TO INCIDENT. 1 G 7 2 3U 3 U NC H13EU E5NE10 2002103000110 20021030 00110 NE 2002 10 30 ASAA0210170 2 20020710 A 7260 717000 GEARBOX BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE DAMAGED A ASAA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 NM 01 743AS 21821 P688228B BRW - APPROXIMATELY TWENTY SECONDS AFTER TAKEOFF, NR 2 ENGINE EXPERIENCED AN INFLIGHT SHUTDOWN. ENGINE READINGS, N1=7 P ERCENT, N2=0 PERCENT, OIL PRESSURE = 0. ENGINE SENT TO SEATTLE EBU FOR EVALUATION, FOUND SIGNIFICANT INTERNAL DAMAGE TO THE GEARBOX. GEARBOX TO BE SHIPPED TO OUTSIDE REPAIR STATION FOR DAMAGE CAUSE AND EVALUATION. (M) 2 L 7 2 4F 4 F A16WE E2EA 2002103000111 20021030 00111 EU 2002 10 30 CA021021006 1 20021001 A 6320 4638302024 BEARING 4638001001 BOLKMS 105 BO105CBS 5626008 EU INPUT PINION MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 1116 (CAN) RT INPUT BEARING OUTER RACE PEELING/SPALLING.METAL PARTICLES FROM DAMAGED INPUT PINION. 1 G 7 2 3U NC H3EU 2002103000112 20021030 00112 NM 2002 10 30 ASAA0210175 1 20020803 A 5210 6529994 GUIDE BOEING 737 7372X6C 1384552 NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 ANC - L1 DOOR WILL NOT CLOSE. ADJUSTED GUIDE ARM PER MM, THEN DOOR OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002103000113 20021030 00113 NM 2002 10 30 ASAA0240087 1 20020803 A 2612 65C380023 FIRE WARNING BOEING 737 7374Q8 138447Q NM COCKPIT FALSE ACTIVATION A ASAA K NONE N FALSE WARNING CL CLIMB 1 NM 01 791AS 28886 YUR - ON DEPARTURE FROM YUR, GEAR WAS IN TRANSIT UP AND THE FIRE WARNING BELL AND FIRE WARNING LIGHTS ILLUMINATED. BOTH CARGO SMOKE FAULT LIGHTS ILLUMINATED. PRESSED FIRE WARNING AND ALL LIGHTS WENT OFF, AND BELL SILENCED. PERFORMED FIRE TEST ON ENGINES, APU AND CARGO SMOKE SYSTEM ALL OPS NORMAL. REFORMED FORWARD AND AFT CARGO FIRE SYSTEM TEST, VISUALLY INSPECTED SMOKE DETECTORS IN CARGO PITS, NO DEFECTS NOTED. AT NO TIME WAS THERE ANY EVIDENCE OF FIRE OR SMOKE. NO DEFE CTS NOTED ON INSPECTION. ALL OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 2002103000114 20021030 00114 NM 2002 10 30 ASAA0240110 1 20020918 A 5755 2013477 HINGE BOEING 737 7374Q8 138447Q NM SPOILER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PAE - DURING C-CHECK, FOUND DAMAGE ON UPPER SURFACE OF SPOILER HINGE WEB AT INBOARD CORNER OF NR 2 SPOILER. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002103000115 20021030 00115 NM 2002 10 30 S02252036 1 20021026 A 5270 WARNING SYSTEM BOEING 747 747200 1384847 NM PWA JT9 JT9D7R4G2 52054 NE CARGO DOOR FALSE ACTIVATION W SAJF O OTHER N FALSE WARNING CL CLIMB 1 WP 03 24308 B18771 SIDE CARGO DOOR DOOR WARNING LIGHT ILLUM. ON BOTH FORWARD AND F/E PANEL DURING TAKE-OFF PHASE. CHECKED OPEN/CLOS E MOVEMENT AND CLOSING/LOCKING DEVICES FOUND ALL OK. CLOSED AND LOCKED DOOR. 2 L 7 4 4F 4 F RT A20WE E3NE 2002103000116 20021030 00116 NM 2002 10 30 ASAA0240111 1 20020918 A 5311 654654984 FAILSAFE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PAE - DURING C-CHECK, FOUND CORROSION ON FAIL/SAFE AT BL 0 BS 767 AND WL 149. REMOVED AND FABRICATED NEW SECTION IAW SR M. (M) 2 L 7 2 4F RT A16WE 2002103000117 20021030 00117 NM 2002 10 30 ASAA0240112 1 20020918 A 5320 BAC1496377 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PAE - DURING C-CHECK, FOUND AFT CARGO BAY RIGHT FLOOR TO SIDEWALL SUPPORT PLATE IS CORRODED AT BS 727 TO 767 AND RBL 17. REMOVED CORRODED PLATE, FABRICATED NEW FLOOR TO SIDEWALL SUPPORT AND INSTALLED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002103000118 20021030 00118 NM 2002 10 30 ASAA0240113 1 20020918 A 5754 65C26601382 SKIN BOEING 737 7374Q8 138447Q NM L/E SLAT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PAE - DURING C-CHECK, FOUND NR 6 SLAT EXTERNAL SKIN IS CRACKED ON LOWER L/E AT FASTENERS AT OUTBOARD END. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002103000119 20021030 00119 NM 2002 10 30 ASAA0240114 1 20020918 A 5320 6547690 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PAE - DURING C-CHECK, FOUND AFT CARGO BAY LEFT FLOOR TO SIDEWALL SUPPORT PLATE AT BS 727 TO 727E IS CORRODED. REMOVED A ND FABRICATED NEW AND INSTALLED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002103000120 20021030 00120 NM 2002 10 30 ASAA0240115 1 20020918 A 5320 465415 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PAE - DURING C-CHECK, FOUND INTERCOSTAL BETWEEN BS 747 TO 767 CRACKED. REMOVED, FABRICATED AND INSTALLED NEW PART IAW S RM. (M) 2 L 7 2 4F RT A16WE 2002103000121 20021030 00121 NM 2002 10 30 ASAA0240116 1 20020918 A 5320 654646047 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PAE - DURING C-CHECK, FOUND WIPER WEB LEFT ANGLE IS CRACKED. REMOVED, FABRICATED NEW AND INSTALLED PART IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002103000122 20021030 00122 NM 2002 10 30 ASAA0240117 1 20020919 A 5754 65C26602381 SKIN BOEING 737 7374Q8 138447Q NM L/E SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PAE - DURING C-CHECK, FOUND LEFT NR 2 SLAT UPPER AND LOWER TRAILING EDGE WEDGE SKIN IS DELAMINATED AT OUTBOARD END. REP AIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002103000123 20021030 00123 EU 2002 10 30 BAQA081081 1 20021001 A 6700 071124201 SWITCH UROCOP EC135 EC135T1 5620026 EU SLAVE CONTROL INOPERATIVE H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 118WS 1424 0089 EXCHANGE UNIT. SLAVING ACCESSORY INOPERATIVE IN SLAVE MOD. CORE RETURN REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2002103000124 20021030 00124 NM 2002 10 30 ASAA0240118 1 20020919 A 5720 65C2630923 ANGLE BOEING 737 7374Q8 138447Q NM WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PAE - DURING C-CHECK, FOUND NR 3 IFOT FAIRING HAS A CRACKED ANGLE OUTBOARD OF SIDE UPPER EDGED JUST INBOARD OF NR 3 SPOI LER. REMOVED AND REPLACED ANGLE IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002103000125 20021030 00125 WP 2002 10 30 GTIA020979 1 20020917 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 131NK ACY - FOUND EMERGENCY FLOOR PATH LIGHTING ROW 8DEF INOPERATIVE. RESECURED FLOOR PATH LIGHTING WIRE. (M) 2 L 7 2 4F A6WE 2002103000126 20021030 00126 NE 2002 10 30 BAQA081124 2 20021010 A 7323 430121204 GOVERNOR BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101750B1 41560 NE ENGINE MALFUNCTIONED H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 911WS 529 7068 INTERMEDIATE TORQUE SPLITS EXCEEDING LIMITATIONS. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U 3 U H13EU E5NE10 2002103000127 20021030 00127 NE 2002 10 30 BAQA081130 2 20021011 A 7321 430121106 FUEL CONTROL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101750B1 41560 NE ENGINE FAILED H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 911WS 923 7068 ENGINE WOULD NOT TOP. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U 3 U H13EU E5NE10 2002103000128 20021030 00128 EU 2002 10 30 BAQA081176 1 20021022 A 5210 11724274101 GUIDE BOLKMS 117 BK117B1 5626012 EU PAX DOOR WORN H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 945ME 813 7235 GUIDES WORN. INSTALLED SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002103000129 20021030 00129 WP 2002 10 30 GTIA020980 1 20020918 A 2120 ODOR DOUG DC9 DC983 3022083 WP CABIN DETECTED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 814NK 49619 AT FL310, FLIGHT ATTENDANTS REPORTED FUMES IN CABIN. AFTER THIRD CALL, PEOPLE WERE HAVING A HARD TIME BREATHING. NO SM OKE OR FUMES WERE EVIDENT IN THE COCKPIT. PERFORMED OPS CHECK OF BOTH LEFT AND RIGHT PACKS. NO DEFECTS NOTED AT THIS T IME. (M) 2 L 7 2 4F RT A6WE 2002103000130 20021030 00130 EU 2002 10 30 BAQA081182 1 20021024 A 2435 23032022 COMMUTATOR BOLKMS 117 BK117A3 5626015 EU STARTER GEN CORRODED H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 117LG 292 7032 COMMUTATOR PITTED. MAKES LOUD RAPPING NOISE WHEN OPERATED. INSTALLED WITH SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002103000131 20021030 00131 WP 2002 10 30 GTIA020981 1 20020921 A 2560 MEGAPHONE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A GTIA O OTHER L NO TEST CR CRUISE 1 GL 23 802NK 53168 DEN - FLT 313 - MID MEGAPHONE INOPERATIVE. (M) 2 L 7 2 4F RT A6WE 2002103000132 20021030 00132 WP 2002 10 30 GTIA020982 1 20020912 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - SKIN PUNCTURED CANTED STATION 1474 BETWEEN LONGERONS 7L AND 8L. REMOVED DAMAGED. FABRICATED REPAIR. INSTALLED R EPAIR. (M) 2 L 7 2 4F RT A6WE 2002103000133 20021030 00133 EU 2002 10 30 BAQA081184 1 20021024 A 6710 BEARING BOLKMS 117 BK117A1 5626010 EU DRIVING LINK ASS ROUGH H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 955ME 946 2229 7243 DRIVING LINK ASSY BEARINGS ROUGH/WORN. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002103000134 20021030 00134 WP 2002 10 30 GTIA020983 1 20020912 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND CREASE AT FS 246 BETWEEN LONGERON 17L AND 18L REQUIRES REPAIR IAW DC9 SRM 53-04, CUT OUT DAMAGED SECTION OF SKIN. FABRICATED FILLER, FINGER DOUBLER AND DOUBLER. INSTALLED REPAIR. (M) 2 L 7 2 4F RT A6WE 2002103000135 20021030 00135 EU 2002 10 30 BAQA081185 1 20021024 A 6420 BEARING BOLKMS 117 BK117A1 5626010 EU FORK LINK ASSY WORN H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 955ME 946 3494 7243 FORK LINK ASSY BEARINGS AND BUSHINGS WORN. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002103000136 20021030 00136 WP 2002 10 30 GTIA020984 1 20020913 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND SKIN NOTCHED AT PRODUCTION SPLICE AT FS 1108 BETWEEN LONGERONS 17L AND 18L. CUT OUT DAMAGE AREA AT PRODUCTI ON SPLICE. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2 L 7 2 4F RT A6WE 2002103000137 20021030 00137 WP 2002 10 30 GTIA020985 1 20020914 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - PASSENGER CABIN, LEFT SEAT TRACK BL 22, STATION 1216-1220 AND 1265-1271 CORROSION, SCRATCHES AND GOUGES. REMOVED DAMAGED SECTION OF SEAT TRACK. FABRICATED NEW SEAT TRACK. INSTALLED SPLICE AT STATION 1220 AND SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2002103000138 20021030 00138 EU 2002 10 30 BAQA081186 1 20021024 A 6240 AWEURO4 AMPLIFIER UROCOP EC135 EC135T1 5620026 EU MAST MOMENT FAILED H K NONE O OTHER IN INSP/MAINT 1 FS 01 522ME 1457 0144 MAST MOMENT INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2002103000139 20021030 00139 2002 10 30 BAQA081190 4 20021024 A 2210 9910991 HEAD UROCOP EC135 EC135T1 5620026 EU REMOTE CONTROL BROKEN H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 575ME 197 0157 REMOTE CONTROL HEAD VHF/PRIORITY SWITCH BROKEN. 1 G 7 2 3U H88EU 2002103000140 20021030 00140 WP 2002 10 30 GTIA020986 1 20020916 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND CORROSION ON FLOORBEAM SUPPORT FS 1309 LBL 22 - RBL 22. REMOVED FLOOR SUPPORT. FABRICATED SUPPORT. INSTAL LED SUPPORT. (M) 2 L 7 2 4F RT A6WE 2002103000141 20021030 00141 WP 2002 10 30 GTIA020987 1 20020914 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN, STATION 218 BL 0 SUPPORT FLOOR HAS CORROSION. REMOVED FLOOR SUPPORT. FABRICATED NEW SUPPO RT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2002103000142 20021030 00142 WP 2002 10 30 GTIA020988 1 20020914 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 200 RBL 8 INCHES TO RBL 44 INCHES FLOOR SUPPORT HAS CORROSION. REMOVED FLOOR SUPPOR T. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2002103000143 20021030 00143 WP 2002 10 30 GTIA020989 1 20020914 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 200 LBL 0 HAS CORROSION FLOOR SUPPORT. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2002103000144 20021030 00144 WP 2002 10 30 GTIA020990 1 20020914 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 200 LBL 11 INCHES HAS CORROSION AT THE FLOOR SUPPORT. REMOVED FLOOR SUPPORT. FABRI CATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2002103000145 20021030 00145 WP 2002 10 30 GTIA020991 1 20020914 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 200 TO STATION 256 LBL 15 INCHES HAS CORROSION AT FLOOR SUPPORT. REMOVED FORWARD SE CTION. FABRICATED FORWARD SECTION. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2002103000146 20021030 00146 WP 2002 10 30 GTIA020992 1 20020914 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 200 LBL 32 INCHES HAS CORROSION AT FLOOR SUPPORT. REMOVED FLOOR SUPPORT. FABRICATE D NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2002103000147 20021030 00147 NE 2002 10 30 BAQA081194 2 20021025 A 7314 9A2045 PUMP UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL2B NE FUEL SYSTEM INOPERATIVE H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 554ME 1297 0154 FUEL PUMP INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U 3 U H88EU E00054EN 2002103000148 20021030 00148 WP 2002 10 30 GTIA020993 1 20020914 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 180 TO 168 LBL 41 INCHES IS CRACKED, DAMAGED AT SURFACE WEB. CUT OUT DAMAGED SECTIO N OF WEB. FABRICATED FILLER AND DOUBLER. INSTALLED FILLER AND DOUBLER. (M) 2 L 7 2 4F RT A6WE 2002103000149 20021030 00149 WP 2002 10 30 GTIA020994 1 20020914 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 180 LBL 25 INCHES TO LBL 38 INCHES FLOOR SUPPORT IS CORRODED. FLOOR SUPPORT REMOVED . FABRICATED FLOOR SUPPORT. FLOOR SUPPORT INSTALLED. (M) 2 L 7 2 4F RT A6WE 2002103000150 20021030 00150 WP 2002 10 30 GTIA020995 1 20020914 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 160 TO STATION 200 LBL 44 INCHES FLOOR SUPPORT IS CORRODED. FLOOR SUPPORT REMOVED. FABRICATED NEW FLOOR SUPPORT. FLOOR SUPPORT INSTALLED. (M) 2 L 7 2 4F RT A6WE 2002103000151 20021030 00151 2002 10 30 BAQA081196 4 20021025 A 3450 066303402 INDICATOR BOLKMS 117 BK117A1 5626010 EU COCKPIT FAILED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 912TG 241 7174 GLIDESCOPE NEEDLE DOES NOT CENTER. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002103000152 20021030 00152 WP 2002 10 30 GTIA020996 1 20020914 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 160 TO 200 RBL 45 INCHES HAS CORROSION AT SUPPORT FLOOR. REMOVED FLOOR SUPPORT. FA BRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2002103000153 20021030 00153 2002 10 30 BAQA081197 4 20021025 A 3422 066306000 INDICATOR BOLKMS 117 BK117A1 5626010 EU COCKPIT INOPERATIVE H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 912TG 124 7174 HDG FLAG DOES NOT PULL. NAV POINTER INOPERATIVE . REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002103000154 20021030 00154 NM 2002 10 30 USAA020309 1 20020730 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 23315 PIT - FOUND STRINGER CORRODED ON ENDS OF STRINGER STATION 323.7 AND BL 0 TO S28R. (M) 2 L 7 2 4F RT A16WE 2002103000155 20021030 00155 EU 2002 10 30 USAABA02018 1 20020902 A 3350 32146210 POWER SUPPLY AIRBUS 330 A330323 3930335 EU CABIN FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 678US 0388 PHL - L3 EPSU AND BATTERY HAD FAULTS. MAINTENANCE REPLACED THE EPSU AND BATTERY. (M) 2 L 7 2 4F RT A46NM 2002103000156 20021030 00156 SW 2002 10 30 FCPA081175 1 20021021 A 3220 1018200741 FORK CLARK 1000 1000CLARK 2230102 SW NLG DAMAGED H FCPA K NONE O OTHER IN INSP/MAINT 1 FS 01 PARTO FOUND RADIAL SCORING IN STRUT BARREL OF NLG FORK APPROX. .003 INCH DEEP. 1 Q 7 1 3R 2A6 2002103000157 20021030 00157 NM 2002 10 30 USAASB02162 1 20020827 A 3350 606171 SOCKET BOEING 737 7373B7 1384580 NM CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 373US 22952 GSO - MAINTENANCE FOUND THE BULLNOSE EMERGENCY LIGHTS AT SEAT ROWS 12, 16 AND 20 INOPERATIVE. MAINTENANCE FOUND THE LIG HT SOCKET AT SEAT ROW 16 SHORTED. REPAIRED LIGHT SOCKET AND REPLACED ONE BATTERY PACK AND TWO POWER SUPPLIES . OPERATI ONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2002103000158 20021030 00158 EU 2002 10 30 IO5R081178 1 20021022 A 3340 4361646 LANDING LIGHT UROCOP EC135 EC135P1 8680990 EU EXTERIOR DEFECTIVE H IO5R K NONE L NO TEST IN INSP/MAINT 1 FS 01 552BA 453 190 LANDING LIGHT UNIT ROTATES NORMAL BUT LIGHT BULB WILL NOT ILLUMINATE, POWER IS AVAILABLE TO CONTACT REMOVED AND REPLACED 1 G 7 2 3U O H88EU 2002103000159 20021030 00159 EU 2002 10 30 IO5R081179 1 20021022 A 6730 L673M40A1001 ACTUATOR UROCOP EC135 EC135P1 8680990 EU TAIL ROTOR LEAKING H IO5R K NONE K FLUID LOSS IN INSP/MAINT 1 FS 01 551BA 436 188 LEAKING AT WEEP HOLE AND OUTPUT CONTROL ROD REMOVED AND REPLACED 1 G 7 2 3U O H88EU 2002103000160 20021030 00160 EU 2002 10 30 IO5R081180 1 20021022 A 5210 L521M00X1012 HANDLE UROCOP EC135 EC135P1 8680990 EU PAX DOOR BENT H IO5R K NONE O OTHER IN INSP/MAINT 1 FS 01 135BP 32 0197 CREW / PAX DOOR HANDLE BENT WILL NOT CLOSE REMOVED AND REPLACED 1 G 7 2 3U O H88EU 2002103000161 20021030 00161 NM 2002 10 30 0202986744 1 20020918 A 3232 1U11937 ACTUATOR BOEING 747 747212F NM BLG DOOR MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 644NW 24177 DURING CLIMB, THE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED WITH THE LANDING GEAR HANDLE IN THE OFF POSITION. RECYCLED L ANDING GEAR AND LIGHT WENT OUT BUT FLICKED ON/OFF FOR THE REMAINDER OF THE FLIGHT. AIRCRAFT CONTINUED TO DESTINATION AN D LANDED WITHOUT INCIDENT. REPLACED THE BODY LANDING GEAR DOOR ACTUATOR. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002103000162 20021030 00162 WP 2002 10 30 CALA0200511 1 20021029 A 5300 59121417075T6 ANGLE DOUG DC9 DC982 3022082 WP A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 LT ATTACH ANGLE FOR VERTICLE TO FUSELAGE IS CRACKED AT STA 1474. INSTALLED REPAIR ON ATTACH ANGLE PER SRM 53-05 FIG 23 AND SRM 53-05 FIG 23A. 2 L 7 2 4F A6WE 2002103000163 20021030 00163 NM 2002 10 30 CALA0200512 1 20021029 A 5310 6545783502 CHANNEL BOEING 737 7373T0 1384582 NM A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 39343 23581 CORROSION ON ANTENNA DOUBLER BETWEEN STA 500-500A, BL0. REMOVED AND REPLACED DOUBLER PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002103000164 20021030 00164 NM 2002 10 30 CALA0200513 1 20021029 A 2540 654681211 WEB BOEING 737 7373T0 1384582 NM A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 39343 23581 VERTICAL WEB CRACKED AT STA 1016 LBL 4. INSTALLED WEB AT STA 1016, LBL4 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002103000165 20021030 00165 2002 10 30 0203375527 4 20020930 A 2565 552160900 SLIDE BOEING 757 757251 1384970 NM CABIN FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 527US 49587 16345 23842 WHILE PERFORMING SAMPLING DEPLOYMENT INSPECTION OF DOOR 4R EVACUATION SLIDE, THE LOWER LEFT SUPPORT RIB SEAM RIPPED OPEN . REPLACED THE SLIDE. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 2002103000166 20021030 00166 NM 2002 10 30 0203386642 1 20020926 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 642NW 21942 DURING LINE CHECK, FOUND A-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002103000167 20021030 00167 EU 2002 10 30 2002FA0001228 1 20021021 A 2810 768378 FUEL CELL AGUSTA A109 A109K2 0260502 EU TMECA ARRIEL ARRIEL1 60030 NE MAIN CONTAMINATED D QKZA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 129AL 10029 16067 PILOT REPORTS FILLING MAIN TANK THINKING IT IS FULL. AFTER A TIME GAUGES INDICATE LESS THAN FULL. INSPECTION OF INSIDE TANK THROUGH FILLER HOLE REVEALED DATA PLATE FROM FUEL PROBE COVERING THE FLANGE ASSY WHICH ALLOWS FUEL TO CROSSFEED TO OTHER TANK. REMOVED PLACARD, OPS NORMAL. RELAYED INFORMATION TO TECHNICIAN. 1 G 7 2 3U 3 U RT H7EU E19EU 2002103000168 20021030 00168 WP 2002 10 30 02034191382 1 20021008 A 2550 INSULATION DOUG DC9 DC915 3022036 WP CARGO BAY OUT OF POSITION A NWAA B EMER. DESCENT S AFFECT SYSTEMS CR CRUISE 1 GL 01 9348 45787 AT FL330, CABIN PRESSURE WAS LOST. FLIGHT DESCENDED TO 10,000 FT AND CONTINUED TO DTW. MASKS DID DEPLOY IN THE CABIN. CREW WAS NOT ABLE TO COMPLETELY CLOSE THE OUTFLOW VALVE. MAINTENANCE FOUND INSULATION MATERIAL BLOCKING THE VALVE AND RESECURED IT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002103000169 20021030 00169 NE 2002 10 30 0203426638 2 20021008 A 7200 ENGINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 4 FLAMED OUT A NWAA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 01 638US 23549 715188 DURING CRUISE AT FL380, THE NR 4 ENGINE FLAMED OUT. THE CREW ATTEMPTED A RESTART BUT WAS NOT SUCCESSFUL. THE FLIGHT CO NTINUED TO NRT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE. OPERATIONAL CHECK OK. 2 L 7 4 4F 4 F A20WE E3NE 2002103000170 20021030 00170 SW 2002 10 30 B1HR631359 1 20020823 A 6300 206040320103 SHAFT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MAIN ROTOR FAILED D B1HR K NONE O OTHER IN INSP/MAINT 1 SW 19 3192G 37 809 BEARING RACES ON SHAFT ARE BELOW MIN REQUIREMENT. BEARINGS WERE SPINNING ON SHAFT. 1 G 7 1 3U 3 U H2SW E4CE 2002103000171 20021030 00171 CE 2002 10 30 NSVA200200003 1 20021030 A 5100 NA STRINGER BEECH 1900 1900D 1154162 CE A NSVA K NONE O OTHER NR NOT REPORTED 1 EA 27 UE221 UE221 Discovered during "A", "B" check. Stringer R 10 is cracked at FS 451 2 L 7 2 4T RT A24CE 2002103000172 20021030 00172 NM 2002 10 30 0203436717 1 20021017 A 2612 CIRCUIT CARD BOEING 747 747251F 1384898 NM FIRE WARNING NOT SEATED A NWAA K NONE N FALSE WARNING AP APPROACH 1 GL 01 617US 21121 DURING APPROACH, BOTH MASTER FIRE WARNING LIGHTS ILLUMINATED AND BELL SOUNDED. AIRCRAFT CONTINUED APPROACH AND LANDED W ITHOUT INCIDENT. RESEATED FIRE WARNING CARDS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002103000173 20021030 00173 NM 2002 10 30 0203446301 1 20021015 A 3350 FUSE BOEING 747 747451 1384940 NM POWER SUPPLY BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21ABC - 31ABC, AT JUMPSEAT 3L, AND LAV DR2L. REPLACED FUSE IN POWER SUPPLY. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002103000174 20021030 00174 NM 2002 10 30 0203456305 1 20021015 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK (PEK), FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 22C - 31C AND FROM 21A - 31A. RECONNEC TED WIRE AND SECURED ADAPTER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002103000175 20021030 00175 NM 2002 10 30 SWAA022482 1 20021018 A 5523 183A81003 BUSHING BOEING 737 7377H4 1384404 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 761RR 27875 DURING SCHEDULED PM CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB BUSHINGS WORN AT HINGE ATTACH POINTS NR 2, NR 3 AND NR 4. REMOVED AND REPLACED LT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002103000176 20021030 00176 NM 2002 10 30 SWAA022483 1 20021018 A 5523 183A81004 BUSHING BOEING 737 7377H4 1384404 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 761RR 27875 DURING SCHEDULED PM CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB BUSHINGS WORN AT HINGE ATTACH POINTS NR 2, NR 3 AND NR 4. REMOVED AND REPLACED RT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002103000177 20021030 00177 NM 2002 10 30 SWAA022487 1 20021019 A 5314 6562125 KEELBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED 1/4D CHECK, FOUND RT KEEL BEAM LEG CRACKED AND CORRODED AT STR 27R, BS 727 PLUS 9 AND BS 727 PLUS 15. REPAIRED KEEL BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2002103000178 20021030 00178 2002 10 30 SWAA022488 4 20021019 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002103000179 20021030 00179 NM 2002 10 30 QXEA0201816 1 20020228 A 2130 92146A010401 CONTROLLER BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 410QX 2195 2195 4053 BZN - CREW RETURNED TO FIELD WHEN AFTER TAKE-OFF THE AIRCRAFT WOULD NOT PRESSURIZE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE CABIN PRESSURE CONTROLLER. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 2002103000180 20021030 00180 SW 2002 10 30 B1HR631360 1 20020830 A 7712 407375003107 INDICATOR BELL 407 407 1182206 SW ALLSN 250C 250C20 03013 GL ENG TORQUE FAILED D B1HR K NONE O OTHER IN INSP/MAINT 1 SW 19 407KA 592 53121 REPLACED GAUGE WITH RECONDITIONED UNIT, INDICATOR HAS FALSE EXCEEDANCES THAT CAN NOT BE CLEARED. WHEN LAPTOP IS CONNECT ED GET AN ERROR SAYING THAT IP ADDRESS IS NOT CORRECT. 1 G 7 1 3U 3 U O H2SW E4CE 2002103000181 20021030 00181 SW 2002 10 30 B1HR631362 1 20020919 A 7933 407375004101 INDICATOR BELL 407 407 1182206 SW ALLSN 250C 250C* GL OIL TEMP STICKS D B1HR K NONE L NO TEST IN INSP/MAINT 1 SW 19 407KA 592 53121 OIL TEMP GAUGE STICKS AT 20 PSI WHEN HOT. 1 G 7 1 3U 3 U O H2SW E4CE 2002103000182 20021030 00182 EU 2002 10 30 HXSA0000403 1 20021014 A 5310 AS350 STRUCTURE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE FUSELAGE BUCKLED E HXSA K NONE O OTHER IN INSP/MAINT 1 AL 05 405AE 596 3286 FUSELAGE BOX STRUCTURE CROSS BRACES BUCKLED. SENT FOR JIG SET AND REPAIR. 1 G 7 1 3U 3 U H9EU E19EU 2002103000183 20021030 00183 NM 2002 10 30 SWAA022490 1 20021019 A 5312 6545409 PRESSURE PANEL BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 34. REPAIRED BEADED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002103000184 20021030 00184 2002 10 30 SWAA022493 4 20021021 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002103000185 20021030 00185 2002 10 30 SWAA022494 4 20021022 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002103000186 20021030 00186 NM 2002 10 30 SWAA022496 1 20021022 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 EEPLS LOOSE IN CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F A16WE 2002103000187 20021030 00187 NM 2002 10 30 SWAA022497 1 20021022 A 5523 6545166 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS FOR AFT R OD END ON RT TAB PER MM. 2 L 7 2 4F RT A16WE 2002103000188 20021030 00188 NM 2002 10 30 SWAA022500 1 20021019 A 5320 BAC1503 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED PM CHECK, FOUND LT VERTICAL CHORD CRACKED AT BS 663, RBL 6.5. REPAIRED CHORD PER SWA EA. 2 L 7 2 4F RT A16WE 2002103000189 20021030 00189 NM 2002 10 30 SWAA022504 1 20021020 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 784SW 29810 DURING SCHEDULED A1 CHECK, SWA SI 11038-55, BOTH LT/RT ELEVATOR TAB HINGE BUSHINGS WORN AT NR 2, NR 3 AND NR 4 HINGE ATT ACH POINTS. REMOVED AND REPLACED HINGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2002103000190 20021030 00190 2002 10 30 SWAA022509 4 20021023 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002103000191 20021030 00191 2002 10 30 SWAA022510 4 20021023 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002103000192 20021030 00192 NM 2002 10 30 SWAA022511 1 20021022 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE AT ROW NR 11. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F A16WE 2002103000193 20021030 00193 2002 10 30 SWAA022512 4 20021022 A 2565 65C16820 CABLE BOEING 737 7372T4 1384492 NM EVAC SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY AND FWD SVC DOOR EMERGENCY EVAC SLIDE CABLES MISROUTED. REROUTED CABLES PER MM. 2 L 7 2 4F A16WE 2002103000194 20021030 00194 NM 2002 10 30 SWAA022515 1 20021021 A 5323 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2002103000195 20021030 00195 NM 2002 10 30 SWAA022516 1 20021022 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER SPLICE P ER SRM. 2 L 7 2 4F RT A16WE 2002103000196 20021030 00196 NM 2002 10 30 SWAA022518 1 20021023 A 5312 6545409 PRESSURE PANEL BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 665, RBL 32. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002103000197 20021030 00197 NM 2002 10 30 SWAA022519 1 20021023 A 5312 6545409 PRESSURE PANEL BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED BETWEEN BS 664 AND BS 665, LBL 31 TO LBL 32. REPAIRED BEADE D PRESS WEB PER SWA T1. 2 L 7 2 4F RT A16WE 2002103000198 20021030 00198 NM 2002 10 30 SWAA022521 1 20021024 A 2560 PH22300L TRACK BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 PHOTOLUMINESCENT EEPLS STRIP LOOSE AT ROWS NR 8 AND NR 9 LT SIDE. SECURED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2002103000199 20021030 00199 NM 2002 10 30 SWAA022522 1 20021024 A 2910 6544625 HYDRAULIC LINE BOEING 737 7373L9 1384470 NM NLG LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 29 657SW 23331 AIR TURNBACK, NOSE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. REMOVED AND REPLACED HYDRAULIC HOSE TO NLG LOCK ACTUAT OR PER MM. 2 L 7 2 4F RT A16WE 2002103000200 20021030 00200 NE 2002 10 30 SWAA022523 2 20021024 A 7261 CFM537B22614 ENGINE BOEING 737 7377H4 1384404 NM GE CFM56 CFM56* 13802 NE RIGHT LEAKING A SWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 29 726SW 27858 888962 IN-FLT SHUTDOWN, DECLARED EMERGENCY, NR 2 ENGINE OIL PRESS WENT TO 0, OIL QUANTITY DROPPED TO 0, SHUTDOWN ENGINE. REMOV ED AND REPLACED NR 2 ENGINE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002103000201 20021030 00201 NM 2002 10 30 SWAA022527 1 20021026 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002103000202 20021030 00202 NM 2002 10 30 SWAA022528 1 20021024 A 2560 PH22300L TRACK BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP CRACKED BETWEEN ROWS NR 6 DEF AND NR 8 DEF. REMOVED AND R EPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2002103000203 20021030 00203 NM 2002 10 30 SWAA022529 1 20021025 A 3350 604222 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED RON, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002103000204 20021030 00204 2002 10 30 SWAA022531 4 20021024 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002103000205 20021030 00205 EU 2002 10 30 VY1R110892 1 20020906 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED B VY1R K NONE O OTHER IN INSP/MAINT 1 SW 19 67TV 963 2859 TAIL ROTOR LAMINATED, PART REMOVED DUE TO CRACKING. 1 G 7 1 3U 3 U NC H9EU E19EU 2002103000206 20021030 00206 2002 10 30 SWAA022532 4 20021025 A 2565 61621469 SLIDE BOEING 737 737317 138447P NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002103000207 20021030 00207 NM 2002 10 30 SWAA022533 1 20021026 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002103000208 20021030 00208 2002 10 30 VY1R110893 4 20020923 A 3120 B1894522282A CLOCK SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE COCKPIT INOPERATIVE B VY1R K NONE O OTHER IN INSP/MAINT 1 SW 19 314HP 897 3379 CLOCK, INOPERATIVE. 1 G 7 1 3U 3 U H9EU E00054EN 2002103000209 20021030 00209 2002 10 30 SWAA022534 4 20021025 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002103000210 20021030 00210 2002 10 30 VY1R110894 4 20020829 A 3421 5400111920 GYRO SNIAS 350 AS350B3 8680954 EU CONT O520 IO520* 17032 SO COCKPIT INOPERATIVE B VY1R K NONE L NO TEST IN INSP/MAINT 1 SW 19 414HP 3378 GYRO TUMBLES IN FLIGHT. 1 G 7 1 3U 3 O H9EU E5CE 2002103000211 20021030 00211 NM 2002 10 30 SWAA022543 1 20021027 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 4R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002103000212 20021030 00212 NM 2002 10 30 VNAA0210024 1 20021023 A 2731 RELAY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ELEVATOR TRIM FAILED A VNAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 07 424JS 3033 DURING THE CLIMB, THE CREW REPORTED A MAIN ELEVATOR TRIM FAIL. THE CREW ENGAGED THE STANDBY TRIM AND HAD NO FURTHER PRO BLEMS. AFTER ARRIVAL IN PIT, MAINTENANCE INSPECTED AND REPLACED THE 59CC RELAY IN ACCORDANCE WITH DORNIER MAINTENANCE M ANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002103000213 20021030 00213 NM 2002 10 30 VNAA0210025 1 20021023 A 5270 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DOOR OUT OF ADJUST A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 426JS 3038 EN ROUTE AT 27,000 FEET, THE CREW RECEIVED A DOORS LIGHT ON THE RED WARNING PANEL. THERE WAS NO CHANGE IN THE PRESSURIZ ATION. THE CREW DESCENDED TO 15,000 FEET AND THE LIGHT EXTINGUISHED. UPON ARRIVAL AT PIT, MAINTENANCE INSPECTED AND AD JUSTED THE OVER THE CENTER SWITCH SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WER E PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002103000221 20021030 00221 WP 2002 10 30 IXXA0200092O 1 20021029 A 3411 PITOT TUBE DOUG DC8 DC871F 302199D WP FUSELAGE CLOGGED A IXXA O OTHER O OTHER CL CLIMB 1 SW 11 825BX 83222 172 45978 AFTER TAKE OFF FROM BRO, THE FLIGHT CREW NOTED A DIFFERENCE BETWEEN THE NUMBER ONE AND NUMBER TWO AIRSPEED INDICATORS TH AT INCREASED AS THE AIRCRAFTS ALTITUDE INCREASED. THE FLIGHT CREW ADVISED AND COORDINATED WITH ATC TO DETERMINE THE NUM BER TWO AIRSPEED INDICATOR WAS CORRECT. THE FLIGHT CREW, WHILE COORDINATING WITH ATC, RETURNED TO BRO FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND DISCOVERED FOREIGN MATERIAL IN THE NUMBER ONE PITOT TUBE. MAINTENANCE REMOVED THE FOREIGN MATERIAL AND PERFORMED A SUCESSFUL PITOT STATIC CHECK IN ACCORDANCE WITH THE DOUGLAS REPAIR MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002103000225 20021030 00225 WP 2002 10 30 02FDEA00693 1 20020924 A 3260 PROXIMITY SWITCH DOUG DC10 DC1030 3023501 WP LANDING GEAR FAULTY A FDEA K NONE N FALSE WARNING AP APPROACH 1 SO 25 316FE 48314 ON APPROACH, WHEN LANDING GEAR HANDLE MOVED TO EXTEND, RECEIVED ALL UNSAFE GEAR INDICATIONS ON BOTH LANDING GEAR INDICAT ORS AND CONFIG PAGE. RECYCLED GEAR AND ALL INDICATIONS WERE NORMAL. REPLACED PROXIMITY SWITCH ELECTRONICS UNIT AND TES TED GOOD IAW MD 10-30 AMM 31-71-01-2. 2 L 7 3 4F A22WE 2002103000226 20021030 00226 EU 2002 10 30 02FDEA00695 1 20021001 A 5420 11802000 FITTING AIRBUS 310 A310 EU LT PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 LT ENGINE PYLON SPIGOT FITTING ASSEMBLY FOUND CORRODED. R&R FITTING PER SB A310-54-2020. 2 L 7 2 4F RT A35EU 2002103000227 20021030 00227 EU 2002 10 30 02FDEA00696 1 20021001 A 5415 A54611754500 FITTING AIRBUS 310 A310 EU RT PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 CORROSION ON RIGHT WING ENGINE PYLON THRUST AND SIDE LOAD FITTING. R&R FITTING PER EA 6-5450-65103. 2 L 7 2 4F RT A35EU 2002103000228 20021030 00228 EU 2002 10 30 02FDEA00697 1 20021001 A 5730 SKIN AIRBUS 310 A310 EU RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 AFT PYLON HYD TUBES FITTING HOLES ON RIGHT WING UNDER SURFACE SKIN FOUND ELONGATED AFT OF PYLON RIB 21. R&R WING LWR SK IN PER EA 6-5710-65098. 2 L 7 2 4F RT A35EU 2002103000231 20021030 00231 EU 2002 10 30 02FDEA00698 1 20021001 A 5415 A5461175400300 BEARING AIRBUS 310 A310 EU RT PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 RIGHT WING ENGINE PYLON AFT MOUNT FITTING BEARING CORRODED. R&R FITTING PER EA 6-5450-65104. 2 L 7 2 4F RT A35EU 2002103000233 20021030 00233 NM 2002 10 30 02FDEA00703 1 20021002 A 2782 651781823 ACTUATOR BOEING 727 727100 1384036 NM L/E SLAT FAILED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 107FE 19202 DURING FLAP RETRACTION NR 2 SLAT ON RIGHT WING REMAINED EXTENDED WITH FLAP LEVER IN UP POSITION. QRH PROCEDURES WERE FO LLOWED AND FLAPS WERE CYCLED BACK TO 5 ON SCHEDULE FLAPS RETRACTED AGAIN AND PROBLEM CONTINUED. REMOVED AND REPLACED NR 2 SLAT ACTUATOR AS PER B727 M/M 27-81-032-4, OPS AND LEAK CHECKED GOOD. A/C RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 2002103000234 20021030 00234 CE 2002 10 30 CMX2002F00000 1 20021010 A 3233 98820152 ACTUATOR CESSNA 172 172RG 2072438 CE LYC O360 O360* 41514 EA MLG BROKEN B CMXR K NONE O OTHER IN INSP/MAINT 1 CE 05 4971V 3423 172RG0436 ACTUATOR BROKEN. THIS BRAKE MAY BE THE RESULT OF A HARD LANDING. 1 H 7 1 3O 3 O 3A17 E286 2002110800035 20021108 00035 NM 2002 11 8 02FDEA00704 1 20021002 A 5514 ALC811 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 HORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 19R BOTTOM SURFACE EXCEEDED LIMIT AS PER SB. R&R HORIZ STAB PER EA 1-5510 -66415. 2 L 7 3 4F RT A22WE 2002103000235 20021030 00235 SO 2002 10 30 ESM2002F00000 1 20020905 A 3244 0213571 TIRE PIPER PA42 PA42 7104202 SO PWA PT6 PT6A11 52043 NE MLG SPLIT B ESMR K NONE O OTHER IN INSP/MAINT 1 SO 11 112BC 19 428001027 PILOT NOTED AFTER LAST LANDING, SPLITS/TEARS APPROXIMATELY 1 INCH IN LENGTH, BETWEEN OUTBOARD TREAD IN GROOVE OF TIRE. 1 L 7 2 4T 3 T A23SO E4EA 2002103000236 20021030 00236 CE 2002 10 30 FPI2002F00012 1 20021021 A 3233 98820152 ACTUATOR CESSNA 172 172RG 2072438 CE MLG CRACKED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 4752R 4057 172RG0023 RIGHT MAIN GEAR ACTUATOR FOUND CRACKED IAW AD. 1 H 7 1 3O 3A17 2002103000237 20021030 00237 CE 2002 10 30 FPI2002F00013 1 20021021 A 3233 98820152 ACTUATOR CESSNA 172 172RG 2072438 CE MLG CRACKED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 4752R 4057 172RG0023 LEFT MAIN GEAR ACTUATOR FOUND CRACKED IAW AD. 1 H 7 1 3O 3A17 2002103000239 20021030 00239 SO 2002 10 30 OG52002F00001 1 20020926 A 7160 8732802 AIR BOX PIPER PA28 PA28161 7102803 SO LYC O320 O320* 41508 EA CARB SEPARATED A OG5R K NONE O OTHER IN INSP/MAINT 1 GL 21 248ND 719 2842058 DURING SCHEDULED INSPECTION MECHANIC FOUND AIR BOX TUBE LIP SEPARATING FROM TUBE. WELDS SECURING TUBE TO AIRBOX ASSEMBL Y, WERE INTACT AND NO EXTERNAL SIGNS WERE VISIBLE. 1 L 7 1 3O 3 O 2A13 E274 2002103000240 20021030 00240 NM 2002 10 30 SROM200200019 1 20021030 A 3350 M1137BPS73 BATTERY PACK BOEING 737 737205 1384456 NM CABIN INOPERATIVE C SROM K NONE L NO TEST IN INSP/MAINT 1 AL 03 733PA 9 23466 ROW 16 RT AISLE EMERGENCY LIGHT INOP. REPLACED BATTERY PACK M1137. CKECKED GOOD. REF. 33-51-151. 2 L 7 2 4F RT A16WE 2002110800036 20021108 00036 NM 2002 11 8 02FDEA00705 1 20021002 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 HORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 9R BOTTOM SURFACE EXCEEDED LIMIT AS PER SB. R&R HORIZ STAB PER EA 1-5510- 66415. 2 L 7 3 4F RT A22WE 2002110800037 20021108 00037 NM 2002 11 8 02FDEA00706 1 20021002 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 HORIZ STAB EXTERIOR, FOUND BARREL NUT HOLE NR 14R ELONGATED. R&R STAB HORIZ PER EA 1-5510-66415. 2 L 7 3 4F RT A22WE 2002110800038 20021108 00038 NM 2002 11 8 02FDEA00707 1 20021002 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 HORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 14L OUT OF SB LIMIT. R&R HORIZ STAB PER EA 1-5510-66415. 2 L 7 3 4F RT A22WE 2002110800039 20021108 00039 NM 2002 11 8 02FDEA00708 1 20021002 A 5514 ALC810 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 HORIZ STAB INTERIOR FOUND BARREL NUT HOLE NR 21 L BOTTOM SURFACE LOCAL BLENDOUT CORROSION EXCEEDED LIMIT AS PER SB. R&R HORIZ STAB PER EA 1-5510-66415. 2 L 7 3 4F RT A22WE 2002103000241 20021030 00241 WP 2002 10 30 02FDEA00709 1 20021008 A 2722 63035 MOTOR DOUG DC10 DC1010 3022110 WP RUDDER RUPTURED A FDEA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 25 68054 47808 RUDDER MOTOR PUMP RUPTURED AND LEAKING EXCESSIVELY. R&R LWR RUDDER NON REVERSIBLE MOTOR PUMP PER MM 27-26-01-2. 2 L 7 3 4F A22WE 2002110800040 20021108 00040 NM 2002 11 8 02FDEA00710 1 20021008 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 HORIZ STAB INT, BARREL NUT HOLE 32R AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STAB PER EA 1-5510-66415. 2 L 7 3 4F RT A22WE 2002103000242 20021030 00242 NM 2002 10 30 QXEA0201580 1 20020916 A 5410 FRAME BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 CKB-103 AND 104 Z FRAMES ARE SEVERELY CRACKED. REPAIRED IAW DHC-8 SRM 54-10-16, HORIZON AIR EA. 6-71-57 AND WVAC EO. DH8 S-71-0562. 2 H 7 2 4T RT A13NM 2002103000243 20021030 00243 NM 2002 10 30 QXEA0201581 1 20020916 A 5410 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 CKB-102 AND 104 CHANNELS ARE SEVERELY CRACKED. REPAIRED IAW DHC-8 SRM 54-10-16, HORIZON AIR EA. 6-71-57 AND WVAC EO. DH8 S-71-0562. 2 H 7 2 4T RT A13NM 2002103000244 20021030 00244 NM 2002 10 30 QXEA0201582 1 20020916 A 5410 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 CKB-101 AND 103 CHANNELS ARE SEVERELY CRACKED. REPAIRED IAW DHC-8 SRM 54-10-16, HORIZON AIR EA. 6-71-57 AND WVAC EO. DH8 S-71-0562. 2 H 7 2 4T RT A13NM 2002103000245 20021030 00245 NM 2002 10 30 QXEA0201583 1 20020916 A 5410 FRAME BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 CKB-103 FRAME IS SEVERELY CRACKED. REPAIRED IAW DHC-8 SRM 54-10-16, HORIZON AIR EA. 6-71-57 AND WVAC EO. DH8S-71-0562. 2 H 7 2 4T RT A13NM 2002103000246 20021030 00246 NM 2002 10 30 QXEA0201584 1 20020917 A 5414 HINGE BOMBDR DHC8 DHC8401 1390041 NM NACELLE DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 CKB-RT LOWER NACELLE FOD DOOR HINGE POINTS ARE WORN. REPAIRED IAW HORIZON AIR EA. 6-71-58A AND WVAC EO. DH8S-71-0579A. 2 H 7 2 4T RT A13NM 2002103000247 20021030 00247 EU 2002 10 30 QXEA0201821 1 20021029 A 3260 200497005A ACTUATOR FOKKER F28 F28MK4000 4990810 EU ZONE 700 FAILED A QXEA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 NM 09 493US 44012 2998 11161 BIL - ON APPROACH, THE GEAR WAS SELECTED DOWN. THE LEFT MAIN RED LIGHT REMAINED ILLUMINATED WITH NO GREEN ILLUMINATION. A GO-AROUND WAS INITIATED AND THE ABNORMAL CHECKLIST WAS PERFORMED. RESULTS WERE THE SAME. AFTER 3 MINUTES THE GEAR INDI CATED GREEN AND AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT DOWNLOCK A CTUATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002103000248 20021030 00248 NM 2002 10 30 0203566624 1 20021025 A 2750 LITTON 98010903 BOEING 747 747251B 1384892 NM A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 624US SDS5119 21706 DURING APPROACH, THE OUTBOARD TRAILING EDGE FLAPS WOULD NOT EXTEND WITH EITHER PRIMARY OR ALTERNATE SYSTEMS. DECLARED A YELLOW EMERGENCY AND FOLLOWED THE COM PROCEDURE FOR A SPLIT FLAP LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE OUTBOARD TRAILING EDGE FLAP INDICATOR. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002103000249 20021030 00249 SO 2002 10 30 C2XA02BT065 1 20021029 A 2610 3601133500230 DETECTOR EMB 145 EMB145LR 3260212 SO FAULTY A C2XA O OTHER J WARNING INDICATION UK UNKNOWN 1 SW 27 16541 145542 EWR---CO3264, CREW REPORTED ENGINE NUMBER ONE FIRE DETECTOR FAILED ON EICAS.....MAINTENANCE REMOVED AND REPLACED ENGINE NUMBER ONE FIRE DETECTOR IAW EMB145 AMM #26-11-01. OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002103000250 20021030 00250 SO 2002 10 30 C2XA02BT066 1 20021027 A 5200 SWITCH EMB 145 EMB145LR 3260212 SO DIRTY A C2XA O OTHER J WARNING INDICATION UK UNKNOWN 1 SW 27 12563 145612 EWR---CO3353, CREW REPORTED CCAS AND DOOR PAGE SHOW EMERGENCY EXIT OPEN....MAINTENANCE CLEANED CLEANED LEFTHAND OVERWING EMERGENCY EXIT SWITCH IAW EMB145 AMM#52-21-00. OPS.CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2002103000251 20021030 00251 NM 2002 10 30 371PA0011 1 20021029 A 3350 58782 CABLE BOEING 737 737306 13844BG NM A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 371PA 23543 Emergency floor path lighting from row 20 to rear cabin Inop. R&R cable assy and accomplished test per MM33-51-21. OK 2 L 7 2 4F RT A16NE 2002103000252 20021030 00252 EU 2002 10 30 WRNA200200008 1 20021029 A 3211 C23005302 DAMPENER AIRBUS 300 A300B4203 3930306 EU UNSERVICEABLE A WRNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 506TA 207 After Take off unable to retract landing gear with system 1 or 2. Followed abnormal procedures and returned to airport. Landing normal.Corrective Action: Found L/H MLG pitch dampner at fault. R&R'd dampner I/A/W 32-11-15 Op's check satisfac tory. Aircraft returned to service. 2 L 7 2 4F RT A35EU 2002103000253 20021030 00253 NM 2002 10 30 QXEA0201604 1 20021001 A 5210 GUIDE DHAV DHC8 DHC8202 2809007 NM CABIN DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - MAIN CABIN DOOR FORWARD TOP STOP GUIDE IS WORN. INSTALLED NEW MAIN CABIN DOOR GUIDE. 2 H 7 2 4T RT A13NM 2002103000254 20021030 00254 NM 2002 10 30 QXEA0201605 1 20021001 A 5210 GUIDE DHAV DHC8 DHC8202 2809007 NM CABIN DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - MAIN CABIN DOOR AFT TOP STOP GUIDE WORN. INSTALLED NEW MAIN CABIN DOOR STOP GUIDE. 2 H 7 2 4T RT A13NM 2002103000255 20021030 00255 NM 2002 10 30 DL757021222 1 20021022 A 5330 146N35317 SKIN BOEING 757 757232 1384965 NM FS 1510, S28R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 601DL 22808 FUSELAGE / SKIN / FS 1510 / STRG. 28R-29R / AIRFONE ANTENNA CUTOUT : CORROSION REPAIR THE FUSELAGE SKIN AROUND THE AIRFONE ANTENNA CUTOUT AT FS 1510 BETWEEN STRINGERS 28R & 29R WAS FOUND CORRODED. THE CUTOUT WAS ENLARGED TO REMOVE THE CORROSION. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 383850-14, REV A. 2 L 7 2 4F RT A2NM 2002103000256 20021030 00256 NM 2002 10 30 DLM88021226 1 20021023 A 3350 0201975003 HARNESS DOUG MD88 MD88 3023688 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 904DE 53409 ROW 24ED PAX EMERGENCY ESCAPE PATH ISLE INSEAT LIGHT (RED) INOP CA FND BROKEN HARNESS, REPAIRED SAME. 2 L 7 2 4F RT A6WE 2002103000257 20021030 00257 NM 2002 10 30 DL757021233 1 20021023 A 5330 146N35112 SKIN BOEING 757 757232 1384965 NM FS 1420, S-29R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 601DL 22808 FUSELAGE / SKIN / FS 1420 / STRG. 28R-29L : DENT REPAIR THE FUSELAGE SKIN WAS FOUND WITH 2 DENTS NEAR FS 1420 BETWEEN STRINGERS 28R & 29L. THE DENTS WERE REMOVED WITH 2 CUTOUTS IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 383884-14, REV A. 2 L 7 2 4F RT A2NM 2002103000258 20021030 00258 NM 2002 10 30 DLM88021236 1 20021025 A 2160 71145730016 HOSE DOUG MD88 MD88 3023688 NM RT PACK TORN A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 946DL 49819 TAIL COMPARTMENT TEMP HIGH LITE ILLUMINATED WHILE PASSING FL250 ON CLIMBOUT. POM PROCEDURES C/W. LEFT THROTTLE AT IDLE I N LITE EXTINGUISHING FOR APPROX. 5 MINUTES, THEN REILLUMINTED. LITE WENT OUT AT 12000 MSL FOR DURATION. RIGHT PACK UNABL E TO MAINTAIN PRESSURIZATION. ENGINE AND AIRFOIL ANTIICE NOT USED ANY TIME. FOUND BOT BLOWN ON RT TEMP CONROL SYSTEM. REPLACED BOOT AND SECURED DUCT. PRESSURIZED A/C. NO LEAKS. RAN ENG AT IDLE AND T/O.NO LEAKS. OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2002103000259 20021030 00259 NM 2002 10 30 DL733021238 1 20021025 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FS 178, WL 207 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947WP 23376 FUSELAGE / BULKHEAD / FS 178 / SIDE CHORDS, FLOOR WEBS, & VERTICAL BEAM CHORDS : CRACK REPAIRS INSPECTION OF THE FS 178 BULKHEAD REVEALED CRACKS IN THE LBL & RBL VERTICAL BEAM CHORDS AT WL 184 AND CRACKS IN THE LH & RH SIDE CHORDS AND ADJACENT FLOOR WEBS AT WL 207. THE CRACKS ARE TYPICAL OF BAC S/B 737-53A1173 AND AD 2000-05-29. THE CRACKED STRUCTURE WAS REPAIRED IN ACCORDANCE WITH THE S/B AND DOCUMENTED PER ER/A 384045-14AD. 2 L 7 2 4F RT A16WE 2002103000260 20021030 00260 NM 2002 10 30 DL72W021240 1 20021025 A 3230 NAS753013 BUSHING BOEING 727 727247 138408F NM LT MLG WORN A DALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 27 296WA 22533 ATB TO TPA - LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF FOUND AIR TO GROUND SENSOR ACTUATING ARM PIVOT BUSHING - EXC ESSIVE PLAY - REPLACED SAME - OPS CHECKED GOOD PER M/M 2 L 7 3 4F A3WE 2002103000261 20021030 00261 NM 2002 10 30 DL72S021252 1 20021027 A 3350 UNK LIGHT BOEING 727 727232 1384082 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 518DA 21469 SEAT 20DEF EMERGENCY LIGHT BROKEN, (FWD,RED) CA RPLD LIGHT. 2 L 7 3 4F A3WE 2002103000262 20021030 00262 NM 2002 10 30 QXEA0201606 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 2 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X438.00. REPAIRED IAW DHC-8 SR M 51-20-16, AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000263 20021030 00263 NM 2002 10 30 QXEA0201607 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 2 TOP CORROSION IN SEAT ATTACH AREA AT X455.00. REPAIRED IAW DHC-8 SRM 51-20-16, AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000264 20021030 00264 NM 2002 10 30 QXEA0201608 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 2 GOUGES TOP AND BOTTOM IN SEAT ATTACH AREA AT X469.00. REPAIRED IAW DHC-8 SRM 5 1-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000265 20021030 00265 NM 2002 10 30 QXEA0201609 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 2 TOP CORROSION IN THE SEAT ATTACH AREA AT X487.00. REPAIRED IAW DHC-8 SRM 51-20 -16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000266 20021030 00266 NM 2002 10 30 QXEA0201610 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 2 TOP CORROSION IN SEAT ATTACH AREA AT X500.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000267 20021030 00267 NM 2002 10 30 QXEA0201611 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 3 TOP CORROSION IN SEAT ATTACH AREA AT X518.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000268 20021030 00268 NM 2002 10 30 QXEA0201612 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 3 TOP CORROSION IN SEAT ATTACH AREA AT X531.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000269 20021030 00269 NM 2002 10 30 QXEA0201613 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 3 BOTTOM CHAFED IN SEAT ATTACH AREA AT X541.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000270 20021030 00270 NM 2002 10 30 QXEA0201614 1 20021005 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - CORROSION AFT FLOOR SUPPORT, LEFT HAND CLOSING ANGLE AROUND N/P AND RIVET BETWEEN SEAT TRACK RAILS AT APPROXIMATEL Y X597.00. REPAIRED IAW DHC-8 SRM 51-20-11, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000271 20021030 00271 NM 2002 10 30 QXEA0201615 1 20021002 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LAV ANGLE AT X237 TO X239, Z104, Y42R HAS CORROSION SPOTS. REPAIRED IAW DHC-8 SRM 51-20-46, SRM 51-20-51, AND SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002103000272 20021030 00272 NM 2002 10 30 QXEA0201616 1 20021004 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - BACK UP ANGLE AFT OF LOWER TCAS APERTURE IS BENT. REPLACED BENT ANGLE IAW DHC-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103000273 20021030 00273 NM 2002 10 30 QXEA0201617 1 20021005 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - X212, Y17L, Z100 ANGLE HAS CORROSION. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103000274 20021030 00274 NM 2002 10 30 QXEA0201618 1 20021004 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LEFT HAND NR 4 FLAP TRACK INBOARD SURFACE IS PITTED, CONCENTRATED ON FORWARD 4 INCHES OF TRAVEL. REPAIRED IAW HOR IZON AIR EA 2-57-199. 2 H 7 2 4T RT A13NM 2002103000275 20021030 00275 NM 2002 10 30 QXEA0201619 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 11 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X438.00. REPAIRED IAW DHC-8 RD 8-53-1342, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000276 20021030 00276 NM 2002 10 30 QXEA0201620 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 11 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X455.00. REPAIRED IAW DHC-8 RD 8-53-1342, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000277 20021030 00277 NM 2002 10 30 QXEA0201621 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 11 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X469.00. REPAIRED IAW DHC-8 RD 8-53-1352, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000278 20021030 00278 NM 2002 10 30 QXEA0201622 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 11 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X487.00. REPAIRED IAW DHC-8 RD 8-53-1342, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000279 20021030 00279 NM 2002 10 30 QXEA0201623 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 11 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT X500.00. REPAIRED IAW DHC-8 RD 8-53-1342, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000280 20021030 00280 NM 2002 10 30 QXEA0201624 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 12 TOP AND BOTTOM GOUGES IN SEAT ATTACH AREA AT X518.00. REPAIRED IAW DHC-8 RD 8-53-3644, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103000281 20021030 00281 EA 2002 10 30 QXEA0201673 1 20021011 A 5210 LATCH CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 604QX 10019 PDX-MAIN CABIN DOOR DIFFICULT TO OPEN & CLOSE. LOCK AND UNLOCK. CLEANED AND LUBED DOOR LATCHES. OPERATIONAL CHECK GOO D. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002103000282 20021030 00282 EU 2002 10 30 QXEA0201675 1 20020920 A 3350 5515900004 CIRCUIT CARD FOKKER F28 F28MK4000 4990810 EU CABIN DEFECTIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 497US 11173 PDX-EMERGENCY EXIT SIGN OVER COCKPIT ENTRY WAY HAS BULBS BURNT OUT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT CARD. OP ERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002103000283 20021030 00283 NM 2002 10 30 AWXA200200930 1 20020906 A 5720 65C2630934 STIFFENER BOEING 737 737301 1384611 NM RT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.75 INCH CRACK WAS FOUND ON THE RT WING INTERNAL STRAP AT THE INBOARD SIDE AFT END OF NR 6 FLAP TRACK FAIRING, WS 259 RT. MAINTENANCE REMOVED DOUBLER AND DAMAGED STIFFENER, FABRICATED A NEW DOUBLER AND STIFFENER, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002103000284 20021030 00284 NM 2002 10 30 AWXA200200931 1 20020902 A 5320 654797316 ANGLE BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A .5 INCH CRACK WAS FOUND ON CREASE BEAM SHEAR WEB ANGLE AT BS 616, RBL 64, WL 20 8. MAINTENANCE REMOVED DAMAGED CREASE BEAM SHEAR WEB ANGLE, FABRICATED A NEW SECTION OF CREASE BEAM SHEAR WEB ANGLE, AND INSTALLED REPAIR PART IAW AWA ER 15-5310-02260-KB1. 2 L 7 2 4F RT A16WE 2002103000285 20021030 00285 NM 2002 10 30 AWXA200200932 1 20020923 A 5340 654868719 ATTACH ANGLE BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK A .5 INCH CRACK WAS FOUND ON THE FORWARD OUTBOARD ATTACH ANGLE AT THE LT WHEEL WE LL OPENING, CRACK RUNS FROM TOP FASTENER HOLE TO THE UPPER EDGE OF THE ANGLE, BS 679, LBL 70, WL 172. MAINTENANCE REMOV ED THE DAMAGED ATTACH ANGLE, FABRICATED AND INSTALLED REPAIR IAW B737-200 SRM 51-30-2, PG. 8, 9, & 32, FIG. 7. 2 L 7 2 4F RT A16WE 2002103000286 20021030 00286 EU 2002 10 30 AWXA200200934 1 20020927 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 604AW 1196 PHX - EEL - EMERGENCY LIGHT TEST ON FLIGHT ATTENDANT PANEL FAILED. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS A T EMERGENCY POWER SUPPLY UNITS 10WL, 11WL, AND 13WL. FUNCTIONAL TEST OF EMERGENCY LIGHTING SYSTEM WAS GOOD. 2 L 7 2 4F RT A28NM 2002103000287 20021030 00287 NM 2002 10 30 AWXA200200937 1 20020928 A 3350 20131A BATTERY BOEING 757 7572S7 1384962 NM CABIN DISCHARGED A AWXA K NONE O OTHER CL CLIMB 1 WP 28 903AW 23323 LAS - EEL - AFTER TAKEOFF OUT OF BWI THE FLIGHT ATTENDANT INFORMED THE FLIGHT DECK THAT EMERGENCY LIGHTS ILLUMINATED AND LATER WENT OUT. MAINTENANCE TROUBLESHOT AND FOUND ALL EMERGENCY LIGHT BATTERIES WEAK, REPLACED ALL EMERGENCY LIGHT BAT TERY PACKS PER BMM 33-51-07, FUNCTIONAL TEST WAS GOOD IAW T/C A1C33607. 2 L 7 2 4F RT A2NM 2002103000288 20021030 00288 EU 2002 10 30 AWXA200200938 1 20020929 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 628AW 67 LAS - EEL - EMERGENCY LIGHT BATTERY FAILED TEST AT FLIGHT ATTENDANT PANEL AND EMERGENCY POWER SUPPLY UNIT 11WL. MAINTEN ANCE REPLACED EMERGENCY LIGHT BATTERY AT EMERGENCY POWER SUPPLY UNIT 11WL. OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2002103000289 20021030 00289 NM 2002 10 30 AWXA200200939 1 20020918 A 5330 654580215 DOUBLER BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 MCN - MAJOR REPAIR - DURING C-13 CHECK EXFOLIATION CORROSION WAS FOUND ON THE FORWARD LAV PAN RING AT BS 275. MAINTENAN CE REMOVED EXTERNAL DOUBLER AND LAV PAN RING; FABRICATED A NEW EXTERNAL DOUBLER; INSTALLED REPAIR PART AND LAV PAN RING IAW B737-200 SRM 51-30-2, SRM 51-30-5, AND SRM 51-30-8. 2 L 7 2 4F RT A16WE 2002103000290 20021030 00290 NM 2002 10 30 AWXA200200950 1 20020913 A 5320 6623250 CHANNEL BOEING 737 737375 13844BN NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 23707 YVR - MAJOR REPAIR - DURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON FLOORBEAM LINK ATTACH U CHANNEL AT BS 520, BL 0. M AINTENANCE REMOVED DAMAGED LINK ATTACH CHANNEL. FABRICATED A NEW REPLACEMENT LINK ATTACH CHANNEL, INSTALLED REPAIR PART IAW DWG 66-23250, B737-300 SRM 51-10-02, AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002103000291 20021030 00291 NM 2002 10 30 AWXA200200951 1 20020902 A 5315 6546803 FLOORBEAM BOEING 737 737375 13844BN NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 23707 YVR - MAJOR REPAIR - DURING C-03 CHECK A 1 INCH CRACK WAS FOUND ON FLOORBEAM UPPER TEE CAP AT FWD SIDE OF BS 520, RBL 2 5. MAINTENANCE REMOVED DAMAGED FLOORBEAM UPPER TEE CAP. FABRICATED A NEW REPLACEMENT FLOORBEAM UPPER TEE CAP AND INSTAL LED REPAIR PART IAW B737-300 SRM 53-00-51. 2 L 7 2 4F RT A16WE 2002103000292 20021030 00292 NM 2002 10 30 AWXA200200952 1 20020904 A 5320 69353662 WEB BOEING 737 737375 13844BN NM FUSELAGE BUCKLED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 23707 YVR - MAJOR REPAIR - DURING C-03 CHECK A SHEAR WEB WAS FOUND BUCKLED AND TORN AT BS 520, LBL 25. MAINTENANCE REMOVED D AMAGED SHEAR WEB. FABRICATED A NEW REPLACEMENT SHEAR WEB AND INSTALLED REPAIR PART IAW DWG 69-35365, AND B737-300 SRM 5 1-40-02. 2 L 7 2 4F RT A16WE 2002103000293 20021030 00293 SO 2002 10 30 C2XA02SH120 1 20021030 A 5300 14522460011 STRAP EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14933 145018 SHV- DURING C CHECK CENTER FLOOR BEAM STRAP AT DOUBLER WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 15 AND16. MAINTENANCE REMOVED DAMAGE AND PEFPORMED A DOUBLER REPAIR IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002103100001 20021031 00001 NM 2002 10 31 QXEA0201586 1 20021003 A 3150 10174N07W04 INDICATOR DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 355PH 9987 9987 500 SEA- ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDED. REMOVED AND REPLACED BOTH TORQUE INDICATORS. OPERATIONAL CHECK S GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002103100002 20021031 00002 NM 2002 10 31 QXEA0201587 1 20020929 A 5753 85750900001 SKIN BOMBDR DHC8 DHC8401 1390041 NM TE FLAPS CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 2312 2312 4051 PDX - THE LEFT TOP OUTBOARD FLAP HAS A 16 INCH CHAFF THROUGH THE PAINT. MAINTENANCE BLENDED AND REPAIRED THE FLAP IAW E. A. 6-57-65, AND RD8/4-57-016. 2 H 7 2 4T RT A13NM 2002103100003 20021031 00003 NM 2002 10 31 QXEA0201588 1 20020929 A 2750 85750900002 SKIN BOMBDR DHC8 DHC8401 1390041 NM TE FLAPS CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 2312 2312 4051 PDX - RIGHT HAND TOP OUTBOARD FLAP HAS A 16 INCH LONG CHAFE THROUGH THE PAINT 67 1/2 INCHES FROM THE NACELLE AND A 2 INC H CHAFE 34 1/2 INCHES FROM NACELLE. MAINTENANCE BLENDED AND REPAIRED THE DAMAGED AREAS IAW E.A. 6-57-65 AND RD8/4-57-016 . 2 H 7 2 4T RT A13NM 2002103100004 20021031 00004 NM 2002 10 31 QXEA0201591 1 20021006 A 2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8202 2809007 NM NR 1 AND 2 LOW A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 375PH 529 SEA - AIRCRAFT RETURNED TO FIELD WHEN HYDRAULIC PRESSURE INDICATED 0 AND QUANTITY INDICATED LOW. MAINTENANCE INSPECTED T HE AIRCRAFT AND SERVICED THE NR 1 AND 2 HYDRAULIC SYSTEMS. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETUR NED TO SERVICE. 2 H 7 2 4T RT A13NM 2002103100005 20021031 00005 NM 2002 10 31 QXEA0201592 1 20021002 A 5414 SKIN BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX- RT COWL DEBRIS DOOR SURROUND STRUCTURE INBOARD AND OUTBOARD ARE CRACKED. REPAIRED IAW DHC-8 400 RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2002103100006 20021031 00006 NM 2002 10 31 QXEA0201593 1 20021002 A 5414 SKIN BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX- LT COWL DEBRIS DOOR SURROUND STRUCTURE INBOARD AND OUTBOARD CHANNEL ARE CRACKED. REPAIRED IAW DHC-8 400 RD 8/4-71-0 16. 2 H 7 2 4T RT A13NM 2002103100007 20021031 00007 EU 2002 10 31 QXEA0201594 1 20021003 A 3397 WIRE FOKKER F28 F28MK4000 4990810 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 PDX- AISLE EMERGENCY LIGHT ON SEAT 11B WILL NOT COME ON. REPAIRED BROKEN WIRE IAW FOKKER SRM 33-52-01. 2 L 7 2 4F RT A20EU 2002103100008 20021031 00008 EA 2002 10 31 QXEA0201595 1 20021005 A 5711 SPAR CNDAIR CL600 CL6002C10 1390015 EA RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX- CHAFFE DAMAGE ON WING FRONT SPAR STIFFNER RIB NEXT TO RT EJECTOR IN CENTER FUEL TANK. REPAIRED IAW HORIZON AIR EA R-57-16 2 L 7 2 4F RT A21EA 2002103100009 20021031 00009 EA 2002 10 31 QXEA0201596 1 20021005 A 5711 SPAR CNDAIR CL600 CL6002C10 1390015 EA LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX- CHAFE DAMAGE ON WING FRONT SPAR STIFFNER RIB NEXT TO LT EJECTOR IN CENTER FUEL TANK. REPAIRED IAW HORIZON AIR EA R- 57-16. 2 L 7 2 4F RT A21EA 2002103100010 20021031 00010 EU 2002 10 31 QXEA0201597 1 20021005 A 5530 ATTACH ANGLE FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX- CRACK AT FASTENER ON RT SIDE OF VERTICAL STABILIZER ATTACH ANGLE. SECOND FROM THE AFT FASTENER ON THE UPPER FLANGE OF THE ATTACH ANGLE. REPAIRED IAW FOKKER SRM 51-10-4 AND 55-31-00 2 L 7 2 4F RT A20EU 2002103100011 20021031 00011 EU 2002 10 31 QXEA0201598 1 20021005 A 5530 ATTACH ANGLE FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX- CRACK IN RADIUS OF VERTICAL STABILIZER ATTACH ANGLE AT 32 PERCENT OF VERTICAL STABILIZER SPAR ON THE LT SIDE. REPAI RED IAW FOKKER SRM 55-31-00. 2 L 7 2 4F RT A20EU 2002103100012 20021031 00012 EU 2002 10 31 QXEA0201599 1 20021005 A 1430 RIVET FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX- ON THE LT SIDE VERTICAL STABILIZER ATTACH ANGLE THE MOST AFT RIVET ON THE LOWER FLANGE OF THE ATTACH ANGLE IS LOOSE . REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2002103100013 20021031 00013 EA 2002 10 31 QXEA0201600 1 20021007 A 2910 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA NR 1 HYD SYS ACTIVATED A QXEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 600QX 10005 LGB - EMERGENCY CHECKLIST WAS PERFORMED WHEN THE CREW RECEIVED A MESSAGE THAT THE NR 1 HYDRAULIC SYSTEM FAILED DUE TO F LUID LOSS. THE ELECTRIC HYDRAULIC PUMP WAS ACTIVATED AND REMAINED IN OPERATION FOR ABOUT .5 HOUR, AT WHICH TIME IT FAILE D DUE TO FLUID LOSS. THE NR 1 HYDRAULIC SYSTEM WAS SECURED AND THE AICRAFT LANDED WITHOUT INCIDENT. AIRCRAFT DOWN FOR MA INTENANCE. 2 L 7 2 4F RT A21EA 2002103100014 20021031 00014 NM 2002 10 31 QXEA0201625 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT OUTBOARD SEAT TRACK NR 12, TOP, GOUGES IN SEAT ATTACH AREA AT APPROXIMATELY X531.00. REPAIRED IAW DHC-8 SRM 51 -00-06 AND SRM 51-20-36 PAGES 1-10. 2 H 7 2 4T RT A13NM 2002103100015 20021031 00015 NM 2002 10 31 QXEA0201626 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT OUTBOARD SEAT TRACK NR 12, TOP AND BOTTOM HAS CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X541.00. REPAIRED IAW RD 8-53-3644 AND SRM 51-20-36, PAGES 1-10. 2 H 7 2 4T RT A13NM 2002103100016 20021031 00016 NM 2002 10 31 QXEA0201627 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - CORROSION AROUND TWO RIVETS BETWEEN SEAT RAILS AFT RT FLOOR SUPPORT CLOSING ANGLE AT APPROXIMATELY X597.00. REPAIR ED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, PAGES 1-10. 2 H 7 2 4T RT A13NM 2002103100017 20021031 00017 NM 2002 10 31 QXEA0201628 1 20021001 A 5320 STOP DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - FRAME CHAFED AT UPPER CARGO DOOR STOPS STATION X520.5 AND X564.5 OF Z161.0. REPAIRED IAW RD 8-53-5461. 2 H 7 2 4T RT A13NM 2002103100018 20021031 00018 NM 2002 10 31 QXEA0201630 1 20021002 A 5320 CLIP DHAV DHC8 DHC8202 2809007 NM FUSELAGE BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LT OUTBOARD NR 1 SEAT TRACK SUPPORT CLIPS ARE BROKEN AT X333.3 AND 312.3. REPLACED IAW HORIZON AIR EA 2-53-431 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103100019 20021031 00019 NM 2002 10 31 QXEA0201631 1 20020929 A 5320 RIVET DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIVET HEADS AROUND UPPER TCAS ANTENNA MOUNT BASE HAVE BLENDING DAMAGE DURING CORROSION REMOVAL. REPLACED IAW DHC-8 -200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103100020 20021031 00020 NM 2002 10 31 QXEA0201632 1 20021004 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM WING WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LT NR 5 FLAP TRACK OUTBOARD SURFACE "E" HAS SMALL PITS ALONG BEARING RUN WEAR MARKS. REPAIRED IAW HORIZON AIR EA 2 -57-200. 2 H 7 2 4T RT A13NM 2002103100021 20021031 00021 NM 2002 10 31 QXEA0201633 1 20021001 A 5410 STRUCTURE DHAV DHC8 DHC8202 2809007 NM NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - NACELLE STRUCTURE HAS BEEN CHAFED BY DOOR HINGE ARM AND BONDING BOLT IN NR 2 WHEEL WELL FORWARD COOR AREA. REPAIRE D IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103100022 20021031 00022 NM 2002 10 31 QXEA0201634 1 20020930 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT INBOARD LOWER WING SPAR IS CHAFED APPROXIMATELY YW56.000. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-51-811. 2 H 7 2 4T RT A13NM 2002103100023 20021031 00023 NM 2002 10 31 QXEA0201635 1 20021002 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - FRETTING CORROSION AT CHAFED FRAME X651.0, Y28.0L, Z113.5. REPAIRED IAW DHC-8200 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002103100024 20021031 00024 NM 2002 10 31 QXEA0201636 1 20021001 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - SEAT TRACK NR 6 CORRODED. REPLACED SEAT TRACK IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103100025 20021031 00025 NM 2002 10 31 QXEA0201637 1 20021001 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - SEAT TRACK NR 10 CORRODED. REPLACED NR 10 SEAT TRACK IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103100026 20021031 00026 NM 2002 10 31 QXEA0201638 1 20021002 A 5220 RIVET DHAV DHC8 DHC8202 2809007 NM ESCAPE HATCH MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - TWO RIVETS ARE MISSING FROM INSIDE CORNER BRACKET FOR COCKPIT ESCAPE HATCH STRUCTURE. REPLACED RIVETS IAW DHC-8 SR M 51-40-11. 2 H 7 2 4T RT A13NM 2002103100027 20021031 00027 NM 2002 10 31 QXEA0201639 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT INBOARD SEAT TRACK NR 8 TOP AND BOTTOM HAS CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X469.00. REPAIRED IAW DHC-8 SRM 51-20-36, PAGES 1-10. 2 H 7 2 4T RT A13NM 2002103100028 20021031 00028 NM 2002 10 31 QXEA0201640 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT INBOARD SEAT TRACK NR 8 CHAFED 12 INCHES BY TRACK COVER AT APPROXIMATELY X475.00. REPAIRED IAW DHC-8 SRM 51-20- 36. PAGES 1-10. 2 H 7 2 4T RT A13NM 2002103100029 20021031 00029 NM 2002 10 31 QXEA0201641 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT INBOARD SEAT TRACK NR 8 TOP CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X487.00.. REPAIRED IAW DHC-8 SRM 51- 20-36, PAGES 1-10. 2 H 7 2 4T RT A13NM 2002103100030 20021031 00030 NM 2002 10 31 QXEA0201642 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT INBOARD SEAT TRACK NR 8 BOTTOM CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X500.00. REPAIRED IAW DHC-8 SRM 5 1-20-36, PAGES 1-10. 2 H 7 2 4T RT A13NM 2002103100031 20021031 00031 NM 2002 10 31 QXEA0201643 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND INBOARD SEAT TRACK NR 8 BOTTOM CHAFED BY TRACK COVER AT APPROXIMATELY X510.00. REPAIRED IAW DHC-8 SRM 5 1-20-36, PAGES 1-10. 2 H 7 2 4T RT A13NM 2002103100032 20021031 00032 NM 2002 10 31 QXEA0201644 1 20021004 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LT NR 4 FLAP TRACK OUTBOARD SURFACE "E" HAS SMALL PITS ALONG BEARING RUN WEAR MARK. REPAIRED IAW HORIZON AIR EA 2- 57-199. 2 H 7 2 4T RT A13NM 2002103100033 20021031 00033 2002 10 31 QXEA0201645 4 20020929 A 3445 ANTENNA DHAV DHC8 DHC8202 2809007 NM TCAS SYS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LIGHT CORROSION ON FUSELAGE UNDER UPPER TCAS ANTENNA. REPAIRED IAW CORROSION PREVENTION MANUAL, CHAPTER 4, PARAGRA PH 8A AND B. 2 H 7 2 4T RT A13NM 2002103100034 20021031 00034 NM 2002 10 31 QXEA0201646 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT INBOARD SEAT TRACK NR 8 BOTTOM GOUGES IN SEAT ATTACH AREA AT APPROXIMATELY X438.00. REPAIRED IAW DHC-8 SRM 51-2 0-36, PAGES 1-10. 2 H 7 2 4T RT A13NM 2002103100035 20021031 00035 NM 2002 10 31 QXEA0201647 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT INBOARD SEAT TRACK NR 8 BOTTOM CHAFING BY FLOOR TRIM AT APPROXIMATELY X445.00. REPAIRED IAW DHC-8 SRM 51-20-36, PAGES 1-10. 2 H 7 2 4T RT A13NM 2002103100036 20021031 00036 NM 2002 10 31 QXEA0201648 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT INBOARD SEAT TRACK NR 8 INBOARD FLANGE CHAFED AT APPROXIMATELY X462.00. REPAIRED IAW DHC-8 SRM 51-20-36, PAGES 1-10. 2 H 7 2 4T RT A13NM 2002103100037 20021031 00037 NM 2002 10 31 QXEA0201649 1 20021008 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM NR 2 NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - NR 2 ENGINE LOWER NACELLE OUTBOARD SIDE IS CHAFED ON PREVIOUS REPAIR. REMOVED AND REPLACED CHAFED REPAIR PATCH AS PER D8 RD 8-54-602. 2 H 7 2 4T RT A13NM 2002103100038 20021031 00038 NM 2002 10 31 QXEA0201650 1 20021004 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT NR 4 FLAP TRACK HAS PITTED CORROSION ON INBOARD SURFACE. REPAIRED IAW HORIZON AIR EA 2-57-198. 2 H 7 2 4T RT A13NM 2002103100039 20021031 00039 NM 2002 10 31 QXEA0201651 1 20021004 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT NR 4 FLAP TRACK HAS PITTED CORROSION ON OUTBOARD SURFACE. REPAIRED IAW HORIZON AIR EA 2-57-198. 2 H 7 2 4T RT A13NM 2002103100040 20021031 00040 NM 2002 10 31 QXEA0201652 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT INBOARD SEAT TRACK HAS NUMEROUS DISCREPANCIES. REPLACED NR 9 SEAT TRACK IAW DHC-8 SRM 51-40-11 AND RD 8-53-4472 . 2 H 7 2 4T RT A13NM 2002103100041 20021031 00041 NM 2002 10 31 QXEA0201653 1 20021003 A 5321 FLOOR PANEL DHAV DHC8 DHC8202 2809007 NM CARGO FLOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - CORROSION AT NUTPLATE, X546 BELOW CARGO FLOOR DECK. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103100042 20021031 00042 NM 2002 10 31 QXEA0201655 1 20021003 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT FRAME CHAFED AT X636.0 ABOVE FLOOR LEVEL. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103100043 20021031 00043 2002 10 31 QXEA0201656 4 20021004 A 3452 ANTENNA DHAV DHC8 DHC8202 2809007 NM ATC SYSTEM CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LIGHT SURFACE CORROSION ON FUSELAGE BELOW ATC ANTENNA. REPAIRED IAW DHC-8 SRM 51-20-16. AND SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002103100044 20021031 00044 NM 2002 10 31 QXEA0201657 1 20021005 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM NR 9 SEAT TRACK FRACTURED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - NEW RIVET IN NR 9 SEAT TRACK HAS FRACTURED BUCKTAIL AT APPROXIMATELY X598.0. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1. 2 H 7 2 4T RT A13NM 2002103100045 20021031 00045 NM 2002 10 31 QXEA0201658 1 20021005 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - GOUGE IN NEW NR 9 SEAT TRACK AT APPROXIMATELY STATION X598.0. REPAIRED IAW DHC-8 SRM 51-20-80, PAGES 1-2 AND PSM 1 , CHAPTER 5. 2 H 7 2 4T RT A13NM 2002103100046 20021031 00046 NM 2002 10 31 QXEA0201659 1 20020929 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LOWER TCAS APERTURE SKIN HAS CORROSION. REPAIRED IAW DHC-8 200 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002103100047 20021031 00047 NM 2002 10 31 QXEA0201660 1 20021006 A 5410 DRAG STRUT DHAV DHC8 DHC8202 2809007 NM NACELLE MLGWW CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - THERE ARE TWO CHAFE MARKS ON HEAVY STRUCTURE IN NR 2 WHEEL WELL FORWARD SECTION ABOVE INBOARD V LOBE OF DRAG STRUT . REPAIRED IAW DHC-8 SRM 51-20-51 AND HORIZON AIR EA 2-54-156. 2 H 7 2 4T RT A13NM 2002103100048 20021031 00048 NM 2002 10 31 QXEA0201661 1 20020929 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LIGHT CORROSION AROUND ANTENNA MOUNTING HOLES AT LOWER TCAS ANTENNA ON FUSELAGE. REPAIRED IAW DHC-8 200 SRM 51-20- 16. 2 H 7 2 4T RT A13NM 2002103100049 20021031 00049 NM 2002 10 31 QXEA0201662 1 20021003 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RT FRAME IS CHAFED AT STATION X636.0 AT FLOOR LEVEL. REPAIRED IAW DHC-8 SRM 51-40-11 AND HORIZON AIR EA 2-53-435. 2 H 7 2 4T RT A13NM 2002103100050 20021031 00050 NM 2002 10 31 QXEA0201663 1 20021006 A 5310 THRESHOLD DHAV DHC8 DHC8202 2809007 NM CARGO BAY GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - GOUGE AT CARGO DOOR THRESHOLD FLOOR SUPPORT ANGLE, X5540., Y38L, Z98.5. REPARIED IAW DHC-8 200 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2002103100051 20021031 00051 NM 2002 10 31 QXEA0201664 1 20021002 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - SEAT TRACK NR 7 HAS NUMEROUS DISCREPANCIES. REPLACED NR 7 SEAT TRACK IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103100052 20021031 00052 NM 2002 10 31 QXEA0201665 1 20021004 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - SEAT TRACK NR 4 HAS NUMEROUS DISCREPANCIES. REPLACED NR 4 SEAT TRACK IAW DHC-8 SRM 51-40-11 AND RD 8-53-1102. 2 H 7 2 4T RT A13NM 2002103100053 20021031 00053 NM 2002 10 31 QXEA0201666 1 20021004 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - SEAT TRACK NR 1 HAS NUMEROUS DISCREPANCIES. REPLACED NR 1 SEAT TRACK IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002103100054 20021031 00054 NM 2002 10 31 QXEA0201667 1 20020930 A 5720 STIFFENER DHAV DHC8 DHC8202 2809007 NM WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - GOUGE AND POSSIBLE CRACK ON RT CONTROL CABLE PULLEY BRACKET STIFFNER AFT OF RT BLEED AIR LINE SHROUD COUPLING UNDE R PANEL 261JT, STATION X381. REPAIRED IAW DHC-8 SRM 51-20-11 AND MM 20-32-02, TASKJ 20-32-02-390-801 AND MM TASK 20-34-0 8-400-801. 2 H 7 2 4T RT A13NM 2002103100055 20021031 00055 NM 2002 10 31 QXEA0201669 1 20021006 A 5410 STRUCTURE DHAV DHC8 DHC8202 2809007 NM LT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - TWO CHAFED AREAS IN THE LEFT FORWARD CORNER OF THE NR 1 NACELLE. REPAIRED IAW HORIZON AIR EA 2-54-156. 2 H 7 2 4T RT A13NM 2002103100056 20021031 00056 NM 2002 10 31 QXEA0201670 1 20021008 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LT WING UPPER SKIN HAS 1/2 X 1/4 INCH SCUFF DAMAGE NEXT TO FORWARD EDGE OF APERTURE FOR PANEL 522AT. REPAIRED IAW DHC-8 SRM 57-10-11 AMD SR, 51-20-11. 2 H 7 2 4T RT A13NM 2002103100057 20021031 00057 EA 2002 10 31 QXEA0201676 1 20021014 A 3234 533405 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG FAILED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 602QX 2372 2372 10010 SMF - CREW COMPLIED WITH ABNORMAL CHECKLIST AND ALTERNATE GEAR EXTENSION WHEN AFTER GEAR WAS SELECTED DOWN, THE GEAR DID NOT EXTEND. GEAR LOWERED NORMALLY WITH THE ALTERNATE EXTENSION AND THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED TH E AIRCRAFT AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE. LEAK CHECKS, OPERATIONAL CHECKS INCLUDING EXTENSION AND RE TRACTION CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002103100058 20021031 00058 NE 2002 10 31 QXEA0201678 2 20021014 A 7314 PUMP CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE MAIN FUEL SYS OBSTRUCTED A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 612QX 10042 BOI - ABORTED TAKEOFF. TAKEOFF RPM (N1) ON NR 1 ENGINE APPROXIMATELY 10 PERCENT BELOW REQUIRED INDICATION, FADEC CALLED FOR 88.2 PERCENT, N1 INDICATOR SHOWED APPROXIMATELY 76.3 PERCENT. REMOVED OBSTRUCTION FROM MAIN FUEL PUMP INLET AND REIN STALLED. GROUND RAN, ALL INDICATIONS NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002103100059 20021031 00059 NM 2002 10 31 QXEA0201679 1 20021008 A 5410 SUPPORT BOMBDR DHC8 DHC8401 1390041 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - NR 1 ENGINE LOWER NACELLE AFT CONE SUPPORT LOWER ANGLE CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2002103100060 20021031 00060 NM 2002 10 31 QXEA0201680 1 20021008 A 5410 ANGLE BOMBDR DHC8 DHC8401 1390041 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - NR 1 ENGINE LOWER NACELLE AFT CONE SUPPORT UPPER ANGLE CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2002103100061 20021031 00061 NM 2002 10 31 QXEA0201681 1 20021013 A 3350 6138001 BATTERY BOMBDR DHC8 DHC8401 1390041 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 407QX 663 663 4049 PDX-THREE EMERGENCY EXIT LIGHTS INOPERATIVE IN REAR OF CABIN, CENTER OF BULKHEAD, RT REAR CABIN BULKHEAD AND BESIDE LT R EAR DOOR. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2002103100062 20021031 00062 EA 2002 10 31 QXEA0201682 1 20021012 A 7160 INTAKE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 2 ENGINE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 613QX 10045 PDX - TWO GOUGES IN FORWARD AIR FLOW PATH AROUND 713C LOOKING AFT OF NR 2 ENGINE. REPAIRED IAW TASK 70-42-00-350-002, SE CTION 2, CHAPTER 70-42-00, PAGE 2 OF GE STANDARD PRACTICES. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002103100063 20021031 00063 NM 2002 10 31 QXEA0201683 1 20021017 A 7930 INDICATOR DHAV DHC8 DHC8202 2809007 NM NR 2 ENG OIL MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 09 362PH 518 EUG- DIVERSION TO EUG DUE TO NR 2 ENGINE OIL PRESSURE INDICATOR INTERMITTENTLY IN YELLOW RANGE. DROPPED MOMENTARILY TO 47 PSI THEN BACK TO GREEN. DURING DESCENT TO EUG OIL PRESSURE WAS STEADY. AIRCRAFT LANDED WITHOUT INCIDENT. VERIFIED COR RECT OIL QUANTITY. CLEANED AND RESEATED OIL PRESSURE TRANSMITTER, NO OTHER DEFECTS NOTED.OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002103100064 20021031 00064 EA 2002 10 31 QXEA0201684 1 20021017 A 2612 9847101505 SCREEN CNDAIR CL600 CL6002C10 1390015 EA FIRE SUPPRESSION DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 612QX 10042 PDX- FORWARD CARGO COMPARTMENT FIRE SUPPRESSION CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY ABOVE FORWARD CAR GO DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002103100065 20021031 00065 NM 2002 10 31 QXEA0201685 1 20021013 A 5310 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - DURING INSPECTION, MAINTENANCE INSPECTORS LOCATED SEVERAL SMALL DENTS BETWEEN FUSELAGE STATIONS X281.00 AND X321.0 . DENTS AND DAMAGE WERE REPAIRED IAW EA 6-53-48, AND EA 6-53-48-B. AN HFEC INSPECTION WAS ALSO PERFORMED WITH NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2002103100066 20021031 00066 NM 2002 10 31 QXEA0201686 1 20021017 A 5230 HANDLE BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR UNSECURE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 411QX 4055 CREW RETURNED TO FIELD WHEN AFTER TAKE-OFF THEY RECEIVED A CARGO DOOR WARNING LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE CARGO DOOR HANDLE NOT FULLY SEATED. THE DOOR HANDLE WAS RESEATED, AN OPERATIONAL CHECK WAS PERFORMED,AND THE AIRCRAFT WAS PRESSURIZED. ALL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2002103100067 20021031 00067 NM 2002 10 31 QXEA0201687 1 20021015 A 5410 ATTACH ANGLE BOMBDR DHC8 DHC8401 1390041 NM NR 2 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX- NR 2 LOWER COWL AFT COWL SUPPORT WEB HAS CRACKED UPPER AND LOWER ATTACH ANGLE. REPAIRED IAW RD8-4-71-016. 2 H 7 2 4T RT A13NM 2002103100068 20021031 00068 NM 2002 10 31 QXEA0201688 1 20021015 A 5410 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM NR 2 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX- NR 2 LOWER COWL CHANNELS INBOARD AND OUTBOARD OF DEBRIS DOOR CRACKED. REPAIRED IAW RD8-4-71-016. 2 H 7 2 4T RT A13NM 2002103100069 20021031 00069 NM 2002 10 31 QXEA0201689 1 20021015 A 5410 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM NR 2 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX- NR 2 LOWER COWL DEBRIS DOOR PIVOT POINT CHANNELS, INBOARD AND OUTBOARD CRACKED. REPAIRED IAW RD8-4-71-016. 2 H 7 2 4T RT A13NM 2002103100070 20021031 00070 NM 2002 10 31 QXEA0201690 1 20021019 A 3040 ELEMENT DHAV DHC8 DHC8202 2809007 NM WINDSHIELD HEAT SMOKE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX- SMOKE OBSERVED COMING FROM CAPTAIN'S WINDSHIELD HEATER ELEMENT WITH WARM-UP POSITION SELECTED. STOPS WHEN WINDSHIE LD IS SELECTED OFF. PERFORMED OPERATIONAL CHECK OF WINDSHIELD WIPER IAW DHC-8 MM 30-42-00 PG 501. OPERATIONAL CHECK GOO D. APPLIED WINDSHIELD SURFACE SEAL TO PILOTS WINDSHIELD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002111900116 20021119 00116 EA 2002 11 19 QXEA0201693 1 20021019 A 2697 WIRE HARNESS CNDAIR CL600 CL6002C10 1390015 EA RT ENGINE DAMAGED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 605QX 10022 PDX- FIRE SYSTEM FAULT STATUS MESSAGE ON THE RIGHT HAND ENGINE FIRE LOOP A. REPAIRED WIRE HARNESS IAW AMM TASK 26-11-07 -000-802-A01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002103100071 20021031 00071 NM 2002 10 31 QXEA0201694 1 20021020 A 5260 AIRSTAIR BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 LACK OF LUBE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 404QX 4046 PDX- AIRSTAIR DOOR IS HARD TO OPEN. CLEANED AND LUBED SLIDE RAILS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE . NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2002103100072 20021031 00072 NM 2002 10 31 QXEA0201695 1 20021010 A 3260 WIRE DHAV DHC8 DHC8202 2809007 NM NR 2 WOW SWITCH CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 DPX - NR 2 WOW HARD LINE HAS CHAFED STRUT. REPAIRED IAW HORIZON AIR EA 2-32-57. 2 H 7 2 4T RT A13NM 2002103100073 20021031 00073 NM 2002 10 31 QXEA0201696 1 20021008 A 7921 LINE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE OIL COOLER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - BRAIDED DRAIN LINE HAS A DIME SIZED CHAFE THROUGH BRAID WHERE IT HAS CONTACTED OIL COOLER LINE. REPLACED IAW MM 20 -06-03. 2 H 7 2 4T 4 T RT A13NM E20NE 2002103100074 20021031 00074 NM 2002 10 31 QXEA0201697 1 20021005 A 2621 CLAMP DHAV DHC8 DHC8202 2809007 NM FIRE BOTTLE DISC BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - FIRE BOTTLE YELLOW BLOW OUT DISC INDICATOR LINE HAS A BROKEN CLAMP STAND OFF, LOCATED BLEOW FORWARD FIRE BOTTLE. R EPLACED IAW HORIZON AIR EA 2-52-436 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103100075 20021031 00075 NM 2002 10 31 QXEA0201698 1 20021005 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - BROKEN STANDOFF ANGLE HAS WORN A GROOVE INTO AIRCRAFT SKIN AT X453.0, Z166.0 BELOW FORWARD FIRE BOTTLE AFT SQUIB. REPAIRED IAW HORIZON AEA 2-53-436, PSM 1-82-3, CHAPTER 51-20-46, PAGES 1-5. 2 H 7 2 4T RT A13NM 2002103100076 20021031 00076 NM 2002 10 31 QXEA0201699 1 20021009 A 5310 STOP DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - CARGO DOOR LOWER AFT STOP FITTING IS CHAFED. REPAIRED IAW DHC-8 200 AMM 52-30-00, PAGES 507-508, PARAGRAPH 3C. 2 H 7 2 4T RT A13NM 2002103100077 20021031 00077 NM 2002 10 31 QXEA0201700 1 20020929 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM LT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - LT WING TOP PANEL 532AT APERTURE FLANGE GOUGED. REPAIRED IAW DHC-8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103100078 20021031 00078 NM 2002 10 31 QXEA0201701 1 20021010 A 5230 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - CARGO DOOR CHAFED 1 1/2 INCH LONG, 14 INCHES FROM AFT EDGE 6 INCHES FROM TOP EDGE. REPAIRED IAW DHC-8 SRM 52-00-16 AND SRM 51-20-26, PAGE 7. 2 H 7 2 4T RT A13NM 2002103100079 20021031 00079 NM 2002 10 31 QXEA0201702 1 20021010 A 5230 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - CARGO DOOR CHAFED 1.2 INCHES DIAMETER, 3 1/2 INCHES FROM LOWER EDGE AND 12 INCHES AFT OF FORWARD EDGE. REPAIRED IA W DHC-8 SRM 51-20-16 AND SRM 51-20-26, PAGE 7. 2 H 7 2 4T RT A13NM 2002103100080 20021031 00080 NM 2002 10 31 QXEA0201703 1 20020929 A 5754 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM RT WING L/E CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 CKB - RT CENTER WING LEADING EDGE HAS ALL FOUR AFT CORNERS CRACKED. REPAIRED IAW HORIZON AIR EA 6-57-63 AND EO DH8 6-57- 0591. 2 H 7 2 4T RT A13NM 2002103100081 20021031 00081 NM 2002 10 31 QXEA0201704 1 20021006 A 5410 ANGLE BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 CKB - RT ENGINE NACELLE STRUCTURE LOWER ANGLE IS CRACKED. REPAIRED IAW WVAC EO DHC85-71-0590 AND HORIZON AIR EA 6-71-59. 2 H 7 2 4T RT A13NM 2002103100082 20021031 00082 NM 2002 10 31 QXEA0201705 1 20021006 A 5410 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 CKB - RT ENGINE NACELLE LOWER CHANNEL IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-59 AND WVAC EO DH8S-71-0590. 2 H 7 2 4T RT A13NM 2002103100083 20021031 00083 NM 2002 10 31 QXEA0201706 1 20021006 A 5410 ANGLE BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 CKB - LT ENGINE NACELLE LOWER ANGLE IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-59 AND WVAC DH8S-71-0590 2 H 7 2 4T RT A13NM 2002103100084 20021031 00084 NM 2002 10 31 QXEA0201707 1 20021006 A 5410 FRAME BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 CKB - LT ENGINE NACELLE LOWER FRAME IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-59 AND WVAC EO DH8S-71-0590. 2 H 7 2 4T RT A13NM 2002103100085 20021031 00085 NM 2002 10 31 QXEA0201708 1 20021006 A 5410 FRAME BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 CKB - RT ENGINE NACELLE LOWER FRAME IN CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-59 AND WVAC EO DH8S-71-0590. 2 H 7 2 4T RT A13NM 2002103100086 20021031 00086 NM 2002 10 31 QXEA0201709 1 20021009 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM RT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 CKB - RT FLAP IS CHAFED 1.8 INCHES FROM INBOARD EDGE AND 15.25 INCHES FROM TRAILING EDGE. REPAIRED IAW WVAC EO DH8S-57-0 594. 2 H 7 2 4T RT A13NM 2002103100087 20021031 00087 NM 2002 10 31 QXEA0201710 1 20021009 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM LT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 CKB - LT OUTBOARD FLAP CHAFED AT TWO PLACES. REPAIRED IAW WVAC EO DH8S-57-0594 AHD HORIZON AIR EA 6-57-64. 2 H 7 2 4T RT A13NM 2002103100088 20021031 00088 NM 2002 10 31 QXEA0201711 1 20021004 A 5410 FRAME BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 CKB - RT NACELLE FRAME INBOARD AND OUTBOARD CHANNELS HAVE ONE HOLE EACH WITH NO RIVET PITCH FROM ANOTHER EXISTING HOLE. REPAIRED IAW HORIZON AIR EA 6-54-132 AND WVAC EO DH8S-54-0598. 2 H 7 2 4T RT A13NM 2002103100089 20021031 00089 NM 2002 10 31 QXEA0201712 1 20021003 A 1430 RIVET BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 407QX 4049 CKB - LT NACELLE AT FIREWALL BOTTOM SEVEN RIVETS WITH INSUFFIEIENT GRIP LENGTH. REPAIRED IAW Q400 SRM 51-42-02. 2 H 7 2 4T RT A13NM 2002103100090 20021031 00090 NM 2002 10 31 QXEA0201713 1 20021004 A 5410 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 CKB - LT NACELLE INBOARD CHANNEL HAS ONE HOLE WITH NO RIVET PITCH. REPAIRED IAW HORIZON AIR EA 6-54-132 AND WVAC EO DH8S -54-0598, STEPS 1-4. 2 H 7 2 4T RT A13NM 2002103100091 20021031 00091 NM 2002 10 31 QXEA0201720 1 20021015 A 5510 SUPPORT DHAV DHC8 DHC8202 2809007 NM HORIZONTAL STAB GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - HORIZONTAL STAB, LT FORWARD SPAR, LT FORWARD SUPPORT HAS MULITPLE GOUGES ACROSS FACE OF LEG. REPAIRED IAW DHC-8200 SRM 51-20-26, PAGE 7. 2 H 7 2 4T RT A13NM 2002103100092 20021031 00092 NM 2002 10 31 QXEA0201721 1 20021015 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT WING LEADING EDGE FORWARD SPAR LOWER FLANGE CHAFED AT STATION YW138.0. REPAIRED IAW RD 8-57-20-54 2 H 7 2 4T RT A13NM 2002103100093 20021031 00093 NM 2002 10 31 QXEA0201722 1 20021015 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT WING LEADING EDGE FORWARD SPAR LOWER FLANGE CHAFED AT STATION 58.00. REPAIRED IAW RD 8-57-811. 2 H 7 2 4T RT A13NM 2002103100094 20021031 00094 NM 2002 10 31 QXEA0201723 1 20021016 A 5310 BRACKET DHAV DHC8 DHC8202 2809007 NM CARGO DOORWAY GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - ANGLE BRACKET AT THE LOWER AFT CORNER OF BAGGAGE DOOR APERTURE GOUGED. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 4, TA BLE 4 AND SRM 51-40-11, PAGE 1, PARAGRAPH 1A. 2 H 7 2 4T RT A13NM 2002103100095 20021031 00095 NM 2002 10 31 QXEA0201724 1 20021014 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT INBOARD SEAT TRACK NR 7 TOP CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X266.00. REPAIRED IAW RD 8-53-4473, RD 8-53-1102 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103100096 20021031 00096 NM 2002 10 31 QXEA0201725 1 20021014 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT INBOARD NR 7 SEAT TRACK BOTTOM CHAFED X282.00 TO X296.00. REPLACED NR 7 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002103100097 20021031 00097 NM 2002 10 31 QXEA0201726 1 20021014 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT INBOARD NR 7 SEAT TRACK BOTTOM CHAFED X380.00 TO X391.00. REPLACED NR 7 RT INBOARD SEAT TRACK. 2 H 7 2 4T RT A13NM 2002103100098 20021031 00098 NM 2002 10 31 QXEA0201727 1 20021013 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT INBOARD NR 7 SEAT TRACK BOTTOM CHAFED X410.00 TO X422.00. REPLACED NR 7 RT INBOARD SEAT TRACK. 2 H 7 2 4T RT A13NM 2002103100099 20021031 00099 NM 2002 10 31 QXEA0201728 1 20021013 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CARGO FLOOR BOARD SUPPORT ANGLE, AFT END OF LT INBOARD NR 6 SEAT TRACK CORROSION AT X598.00, Y6.00 AND Y11.00. RE PAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103100100 20021031 00100 NM 2002 10 31 QXEA0201729 1 20021013 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CARGO FLOOR BOARD SUPPORT ANGLE AFT END OF RT INBOARD NR 9 SEAT TRACK CORROSION AT APPROXIMATELY X598 AND RIGHT Y3 .00 AND Y7.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM. 2 H 7 2 4T RT A13NM 2002103100101 20021031 00101 NM 2002 10 31 QXEA0201730 1 20021013 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CORROSION AROUND CARGO FLOOR NUT PLATES, OUTBOARD OF LT PULLEY QUADRANT, X595.00 TO X599.00 AND LEFT Y20.00. REPAI RED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103100102 20021031 00102 NM 2002 10 31 QXEA0201731 1 20021013 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CORROSION AROUND CARGO FLOOR NUT PLATE OVER LT PULLEY QUADRANT X595.00 AND LEFT Y14.00. REPAIRED IAW DHC-8200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103100103 20021031 00103 NM 2002 10 31 QXEA0201732 1 20021013 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - AFT RT CARGO FLOOR SUPPORT ANGLE CORROSION X599.00 AND RIGHT Y16.00 TO Y27.00. REPAIRED IAW DHC-8200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103100104 20021031 00104 NM 2002 10 31 QXEA0201733 1 20021014 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CARGO FLOOR CORROSION AROUND NUT PLATE X653.00 AND LEFT SIDE Y22.00. REPAIRED IAW DHC8-200 SRM 51-20-51. 2 H 7 2 4T RT A13NM 2002103100105 20021031 00105 NM 2002 10 31 QXEA0201734 1 20021014 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LIGHT CORROSION ON OUTER AIRCRAFT SKIN AT LOWER ATC ANTENNA MOUNTING AREA. REPAIRED IAW DHC8-200 SRM 51-20-11 AND SRM 53-00-16. 2 H 7 2 4T RT A13NM 2002103100106 20021031 00106 NM 2002 10 31 QXEA0201735 1 20021015 A 5230 RETAINER DHAV DHC8 DHC8202 2809007 NM CARGO DOOR SEAL CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - BAGGAGE DOOR SEAL RETAINER CHAFED FROM TOP FORWARD CORNER ALONG FORWARD EDGE. REPAIRED IAW DHC8 SRM 51-40-11 AMD D HC8 MM CHAPTER 20. 2 H 7 2 4T RT A13NM 2002103100107 20021031 00107 NM 2002 10 31 QXEA0201736 1 20021015 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT WING FORWARD SPAR FLANGE CHAFED AT UPPER SURFACE YW58.00. REPAIRED IAW RD 8-57-2054. 2 H 7 2 4T RT A13NM 2002103100108 20021031 00108 NM 2002 10 31 QXEA0201737 1 20021015 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT WING FRONT SPAR LOWER CAP IS CHAFED APPROXIMATELY YW57.0. REPAIRED IAW RD 8-57-811. 2 H 7 2 4T RT A13NM 2002103100109 20021031 00109 NM 2002 10 31 QXEA0201739 1 20021018 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT UNDER WING EMERGENCY EXIT EXTERIOR HAS NICK OR GOUGE AT FORWARD EDGE OF WINDOW. REPAIRED IAW DHC-8 SRM 51-20-16 , SRM 51-20-16 AND MM 56-20-11-400-801. 2 H 7 2 4T RT A13NM 2002103100110 20021031 00110 NM 2002 10 31 QXEA0201740 1 20021017 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT OUTBOARD SEAT TRACK NR 1 TOP CORROSION IN SEAT ATTACH AREA APPROXIMATELY X280.00. REPAIRED IAW DHC-8 SRM 51-40- 00. 2 H 7 2 4T RT A13NM 2002103100111 20021031 00111 NM 2002 10 31 QXEA0201741 1 20021017 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT OUTBOARD SEAT TRACK NR 1 TOP CORROSION IN SEAT ATTACH AREA APPROXIMATELY X298.00. REPAIRED IAW DHC-8 SRM 51-40- 00. 2 H 7 2 4T RT A13NM 2002103100112 20021031 00112 NM 2002 10 31 QXEA0201742 1 20021017 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT OUTBOARD SEAT TRACK NR 1 TOP CORROSION IN SEAT ATTACH AREA APPROXIMATELY X328.00. REPAIRED IAW DHC-8 SRM 51-40- 00. 2 H 7 2 4T RT A13NM 2002103100113 20021031 00113 NM 2002 10 31 QXEA0201743 1 20021017 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CORROSION ON LT OUTBOARD SEAT TRACK NR 1 TOP SEAT ATTACH AREA APPROXIMATELY X343.00. REPAIRED IAW DHC-8 SRM 51-40- 00. 2 H 7 2 4T RT A13NM 2002103100114 20021031 00114 NM 2002 10 31 QXEA0201744 1 20021017 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CORROSION ON LT OUTBOARD SEAT TRACK NR 1 IN SEAT ATTACH AREA APPROXIMATELY X360.00 AND X368.00. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002103100115 20021031 00115 NM 2002 10 31 QXEA0201745 1 20021017 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CORROSION ON LT OUTBOARD SEAT TRACK NR 1 TOP AND BOTTOM IN SEAT ATTACH AREA APPROXIMATELY X377.00. REPAIRED IAW DH C-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002103100116 20021031 00116 NM 2002 10 31 QXEA0201746 1 20021017 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CORROSION ON TOP OF LT OUTBOARD SEAT TRACK NR 1 IN SEAT ATTACH AREA APPROXIMATELY X393.00. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002103100117 20021031 00117 NM 2002 10 31 QXEA0201747 1 20021017 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CORROSION ON TOP OF LT OUTBOARD SEAT TRACK NR 1 IN SEAT ATTACH AREA APPROXIMATELY X407.00. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002103100118 20021031 00118 NM 2002 10 31 QXEA0201748 1 20021017 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CORROSION ON TOP OF LT OUTBOARD SEAT TRACK NR 1 IN SEAT ATTACH AREA APPROXIMATELY X424.00. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002103100119 20021031 00119 NM 2002 10 31 QXEA0201749 1 20021014 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CORROSION IN TOP OF RT INBOARD SEAT TRACK NR 7 APPROXIMATELY X212.00 TO X230.00. REPLACED NR 7 RT INBOARD SEAT TRA CK. 2 H 7 2 4T RT A13NM 2002103100120 20021031 00120 NM 2002 10 31 QXEA0201750 1 20021014 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT INBOARD SEAT TRACK NR 7 HAS BARE METAL AT SEAT ATTACH POINTS. REPLACED NR 7 RT INBOARD SEAT TRACK. 2 H 7 2 4T RT A13NM 2002103100121 20021031 00121 NM 2002 10 31 QXEA0201751 1 20021016 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CORROSION ON LT INBOARD SEAT TRACK NR 4 IN FLANGE APPROXIMATELY X220.00 TO X237.00. REPLACED NR 4 LT INBOARD SEAT TRACK. 2 H 7 2 4T RT A13NM 2002103100122 20021031 00122 NM 2002 10 31 QXEA0201752 1 20021016 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - GOUGING IN SEAT ATTACH AREA OF LT INBOARD SEAT TRACK NR 4 APPROXIMATELY X280.00. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002103100123 20021031 00123 NM 2002 10 31 QXEA0201753 1 20021016 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - CORROSION ON LT INBOARD SEAT TRACK NR 4 IN SEAT ATTACH AREA AT APPROXIMATELY X377.00. REPAIRED IAW DHC-8 SRM 51-40 -00. 2 H 7 2 4T RT A13NM 2002103100124 20021031 00124 NM 2002 10 31 QXEA0201755 1 20021016 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT INBOARD NR 4 SEAT TRACK BOTTOM CHAFED X282.00 TO X296.00. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002103100125 20021031 00125 NM 2002 10 31 QXEA0201756 1 20021016 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT INBOARD NR 4 SEAT TRACK BOTTOM CHAFED X316.00 TO X327.00. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002103100126 20021031 00126 NM 2002 10 31 QXEA0201757 1 20021014 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT INBOARD NR 7 SEAT TRACK BOTTOM CHAFED X316.00 TO X327.00. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002103100127 20021031 00127 NM 2002 10 31 QXEA0201758 1 20021016 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT INBOARD NR 4 SEAT TRACK BOTTOM CHAFED X349.00 TO X359.00. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002103100128 20021031 00128 NM 2002 10 31 QXEA0201759 1 20021014 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT INBOARD NR 7 SEAT TRACK BOTTOM CHAFED X349.00 TO S359.00. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002103100129 20021031 00129 NM 2002 10 31 QXEA0201760 1 20021016 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT INBOARD NR 4 SEAT TRACK BOTTOM CHAFED X380.00 TO X391.00. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2002103100130 20021031 00130 NM 2002 10 31 QXEA0201761 1 20021016 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT INBOARD NR 4 SEAT TRACK OUTBOARD FLANGE HAS BARE METAL AND LIGHT CHAFING VARIOS AREAS ALONG FULL LENGTH. REPLAC ED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2002103100131 20021031 00131 NM 2002 10 31 QXEA0201762 1 20021016 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT INBOARD NR 4 SEAT TRACK INBOARD FLANGE AND DRIP HAVE BARE METAL AND LIGHT CHAFING IN VARIOUS AREAS ALONG FULL L ENGTH. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103100132 20021031 00132 NM 2002 10 31 QXEA0201763 1 20021014 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT INBOARD NR 7 SEAT TRACK OUTBOARD FLANGE HAS BARE METAL AND LIGHT CHAFING VARIOUS AREAS ALONG FULL LENGTH. REPLA CED SEAT TRACK. 2 H 7 2 4T RT A13NM 2002103100133 20021031 00133 NM 2002 10 31 QXEA0201764 1 20021013 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT INBOARD NR 7 SEAT TRACK INBOARD FLANGE AND DRIP HAVE BARE METAL AND LIGHT CHAFING VARIOUS AREAS ALONG FULL LENG TH. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 2002103100134 20021031 00134 NM 2002 10 31 QXEA0201765 1 20021019 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT INBOARD NR 5 SEAT TRACK FORWARD OUTBOARD FLANGE CHAFED X424.00 TO X427.00. REPAIRED IAW RD 8-53-1339 AND RD 8-5 3-4473/4472. 2 H 7 2 4T RT A13NM 2002103100135 20021031 00135 NM 2002 10 31 QXEA0201766 1 20021018 A 2760 FAIRLEAD DHAV DHC8 DHC8202 2809007 NM RT WING SPOILER MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT WING LOWER SPOILER CABLE FAIRLEAD MISSING. REPLACED FAIRLEAD. 2 H 7 2 4T RT A13NM 2002103100136 20021031 00136 NM 2002 10 31 QXEA0201767 1 20021016 A 5414 DOUBLER DHAV DHC8 DHC8202 2809007 NM NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - PREVIOUS REPAIR PATCH IN FORWARD RT CORNER OF TOP DECK OF LOWER COWL CHAFED. REPAIRED IAW RD 8-54-602. 2 H 7 2 4T RT A13NM 2002103100137 20021031 00137 NM 2002 10 31 QXEA0201768 1 20021016 A 5410 BRACKET DHAV DHC8 DHC8202 2809007 NM NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - BRACKET ON TOP RT SIDE, 15 INCES FROM AFT END OF LOWER COWL CHAFED. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-40- 00. 2 H 7 2 4T RT A13NM 2002103100138 20021031 00138 NM 2002 10 31 QXEA0201769 1 20021019 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT WING NR 4 FLAP TRACK, INBOARD SIDE LOAD BEARING SURFACE PITTED. REPAIRED IAW HORIZON AIR EA 2-57-202. 2 H 7 2 4T RT A13NM 2002103100139 20021031 00139 NM 2002 10 31 QXEA0201770 1 20021019 A 5753 CARRIAGE DHAV DHC8 DHC8202 2809007 NM RT WING TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT WING NR 4 FLAP CARRIAGE, INBOARD LOWER MAIN ROLLER TRACK BEARING SURFACE PITTED. REPAIRED IAW HORIZON AIR EA 2- 57-202. 2 H 7 2 4T RT A13NM 2002103100140 20021031 00140 NM 2002 10 31 QXEA0201771 1 20021019 A 5753 CARRIAGE DHAV DHC8 DHC8202 2809007 NM RT WING TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RT WING NR 4 FLAP CARRIAGE, OUTBOARD SIDE LOAD ROLLER TRACK, BEARING SURFACE PITTED. REPAIRED IAW HORIZON AIR EA 2 -57-202. 2 H 7 2 4T RT A13NM 2002103100141 20021031 00141 NM 2002 10 31 QXEA0201772 1 20021017 A 5320 CLIP DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - FRAME CLIP AT FRAME 4 AND 35 IS CRACKED. REPAIRED IAW RD 8-55-199. 2 H 7 2 4T RT A13NM 2002103100142 20021031 00142 NM 2002 10 31 QXEA0201773 1 20021017 A 5320 CLIP DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - FRAME CLIP AT FRAME 4 AND 4P IS CRACKED. REPAIRED IAW RD 8-55-199. 2 H 7 2 4T RT A13NM 2002103100143 20021031 00143 NM 2002 10 31 QXEA0201774 1 20021018 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT WING NR 4 FLAP TRACK, OUTBOARD SIDE, TRACK "E" HAS PITTING CORROSION LENGTH OF TRACK. REPAIRED IAW HORIZON AIR EA 2-57-204. 2 H 7 2 4T RT A13NM 2002103100144 20021031 00144 NM 2002 10 31 QXEA0201775 1 20021018 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT WING NR 4 FLAP TRACK, INBOARD SIDE, TRACK "E" HAS PITTING LENGTH OF TRACK. REPAIRED IAW HORIZON AIR EA 2-57-204 . 2 H 7 2 4T RT A13NM 2002103100145 20021031 00145 NM 2002 10 31 QXEA0201776 1 20021019 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT WING, NR 5 FLAP TRACK, OUTBOARD LWOER SURFACE, TRACK "D", HAS 3 LOCATIONS OF PITTING CORROSION. REPAIRED IAW HO RIZON AIR EA 2-57-203. 2 H 7 2 4T RT A13NM 2002103100146 20021031 00146 NM 2002 10 31 QXEA0201777 1 20021018 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT WING, NR 5 FLAP TRACK, OUTBOARD SIDE, TRACK "E", HAS TWO LOCATION OF PITTING CORROSION. REPAIRED IAW HORIZON AI R EA 2-57-203. 2 H 7 2 4T RT A13NM 2002103100147 20021031 00147 NM 2002 10 31 QXEA0201778 1 20021019 A 5754 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT WING, NR 5 FLAP TRACK, UPPER TRACK "A", HAS TWO LOCATIONS OF PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 2-5 7-203. 2 H 7 2 4T RT A13NM 2002103100148 20021031 00148 NM 2002 10 31 QXEA0201779 1 20021016 A 3213 STRUT DHAV DHC8 DHC8202 2809007 NM LT MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT MLG LOWER STRUT INBOARD SIDE HAS CHAFE MARKS. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26, PAGE 7. 2 H 7 2 4T RT A13NM 2002103100149 20021031 00149 NM 2002 10 31 QXEA0201780 1 20021016 A 2820 LINE DHAV DHC8 DHC8202 2809007 NM LT WING FUEL CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT WING, AFT SPAR FUEL LINE IS BEING CHAFED AT FEED THROUGH SKIRT. REPAIRED IAW HORIZON AIR EA 2-28-13A. 2 H 7 2 4T RT A13NM 2002103100150 20021031 00150 NM 2002 10 31 QXEA0201781 1 20021017 A 3220 ARM DHAV DHC8 DHC8202 2809007 NM NLG SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - NLG TRAILING ARM UNDERSIDE IS SCRATCHED AT .015 INCHES. REPAIRED IAW RD 8-23-289. 2 H 7 2 4T RT A13NM 2002103100151 20021031 00151 NM 2002 10 31 QXEA0201782 1 20021018 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - NR 1 SEAT TRACK HAS NUMEROUS TOOLING MARKS FROM RIVET RUN ALONG VERTICAL BEAR APPROXIMATELY 0..6 INCH DEEP AT APPR OXIMATELY STATION 264 WHERE PAINT STRIPPED. REPAIRED IAW HORIZON AIR EA 2-53-437. 2 H 7 2 4T RT A13NM 2002103100152 20021031 00152 NM 2002 10 31 QXEA0201783 1 20021017 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM FUSELAGE INADEQUATE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - ONE RIVET BUCKED TAIL DOES NOT FILL HOLE COMPLETELY, AFT RIVET NR 1 SEAT TRACK X333.30, OUTBOARD FLANGE. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2002103100153 20021031 00153 NM 2002 10 31 QXEA0201785 1 20021017 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT OUTBOARD SEAT TRACK NR 1 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X312.00. REPAIRED IAW DH C-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103100154 20021031 00154 NM 2002 10 31 QXEA0201786 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT OUTBOARD SEAT TRACK NR 2 TOP GOUGED IN SEAT ATTACH AREA AT APPROXIMATELY X438.00. REPAIRED IAW DHC-8200 SRM 51- 20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103100155 20021031 00155 NM 2002 10 31 QXEA0201787 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT OUTBOARD SEAT TRACK NR 2 TOP CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X454.00. REPAIRED IAW DHC-8 200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103100156 20021031 00156 NM 2002 10 31 QXEA0201788 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT OUTBOARD SEAT TRACK NR 2 TOP CORROSION AND BOTTOM GOUGED IN SEAT ATTACH AREA AT APPROXIMATELY X469.00. REPAIRED IAW DHC-8 200 SRM 51-20-16, PAGE 4, PARAGRAPH C, STEPS 1-8 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103100157 20021031 00157 NM 2002 10 31 QXEA0201789 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LT OUTBOARD SEAT TRACK NR 2 TOP CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X485.00 TO X491.00. REPAIRED IAW DH C-8 200 SRM 51-20-16, PAGE 4, PARAGRAPH C, STEPS 1-8 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002103100158 20021031 00158 NM 2002 10 31 QXEA0201811 1 20021024 A 5410 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - LT NACELLE OUTBOARD CHANNEL PART NUMBER 87144114 CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2002103100159 20021031 00159 NM 2002 10 31 QXEA0201812 1 20021024 A 5410 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - LT NACELLE INBOARD ZEE CHANNEL CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2002103100160 20021031 00160 NM 2002 10 31 QXEA0201813 1 20021024 A 5410 FRAME BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - RT NACELLE FRAME CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2002103100161 20021031 00161 NM 2002 10 31 QXEA0201814 1 20021025 A 5410 FRAME BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - LT NACELLE FRAME CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2002103100162 20021031 00162 EA 2002 10 31 QXEA0201815 1 20021027 A 5270 895001 SENSOR CNDAIR CL600 CL6002C10 1390015 EA CARGO DOOR OUT OF ADJUST A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 612QX 1297 1297 10042 PDX - CREW RETURNED TO FIELD WHEN AFTER TAKE-OFF, THE AFT CARGO DOOR CAUTION ILLUMINATED WITH A STATUS MESSAGE THAT REA D PROX SYSTEM FAULT 2. PSI DIFFERENTIAL WAS SEVEN. MAINTENANCE INSPECTED THE AIRCRAFT AND ADJUSTED THE PROX SENSOR AND L UBED THE AFT CARGO DOOR HANDLE. AN OPERATIONAL CHECK AND GROUND PRESSURIZATION WAS PERFORMED. NO DISCREPANCIES WERE NOTE D. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002103100163 20021031 00163 NM 2002 10 31 QXEA0201818 1 20021024 A 5280 PIN BOMBDR DHC8 DHC8401 1390041 NM NLG DOOR BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 413QX 4060 PDX- NOSE LANDING GEAR DOOR PIN BRACKET IS BENT. REPAIRED IAW MTX TASK CARD 32-31-56-400-081. 2 H 7 2 4T RT A13NM 2002103100164 20021031 00164 NM 2002 10 31 QXEA0201819 1 20021023 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX- FUSELAGE SKIN HAS DENTS AT STATION X281-X301 AND STRINGERS 8 THROUGH 12. REPAIRED IAW HORIZON AIR EA 6-53-106 2 H 7 2 4T RT A13NM 2002103100165 20021031 00165 NM 2002 10 31 QXEA0201820 1 20021026 A 1430 NUT PLATE BOMBDR DHC8 DHC8401 1390041 NM ACCESS PANEL FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 412QX 4059 PDX- INBOARD NUTPLATE FOR FUEL TANK ACCESS PANEL 522AT SPIN WHEN TRYING TO TIGHTEN OR LOOSEN THE BOLT. REPAIRED IAW Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 2002103100166 20021031 00166 NM 2002 10 31 QXEA021482 1 20020911 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX- LT WING FRONT SPAR "Z" BRACKET IS CRACKED AT TOP END AT STATION YW58.20. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002103100167 20021031 00167 SO 2002 10 31 03282002 1 20021017 A 3020 ANTI-ICE VALVE LKHEED 1329 132923A 5263106 SO GARRTT TFE731 TFE731* 01518 WP ENGINE INOPERATIVE B QQGR K NONE O OTHER IN INSP/MAINT 1 SW 09 511TS 34 5101 ANTI-ICE VALVE FAILED AFTER 43.2 HOURS AFTER OVERHAUL. VALVE STUCK IN THE OPEN POSITION. SINCE THER WAS NO REPLACEMENT VALVES AVAILABLE A SERVICEABLE AS REMOVED VALVE WAS INSTALLED AND OPERATION BECAME NORMAL. 2 L 7 4 4J 4 F 2A15 E6WE 2002103100168 20021031 00168 EU 2002 10 31 BMAC020019 1 20020928 A 7700 CONNECTOR BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE331* 01514 WP NR 2 ENGINE INOPERATIVE A B16A K NONE O OTHER IN INSP/MAINT 1 NE 05 538PA 751 NR 2 ENGINE WOULD ONLY PRODUCE APPROXIMATELY 85 PERCENT TORQUE ON TAKEOFF. TAKEOFF WAS ABORTED. NR 2 EGT WAS ERRATIC W HILE TAXING BACK. REMOVED, INSPECTED AND CLEANED THE FOLLOWING CONNECTOR PLUGS; TTL, TORQUE RIGHT, J1 AND J3 ON SIGNAL CONDITIONER, LEFT AND RIGHT AFT FIREWALL BULKHEAD. ALL CONNECTOR PLUGS ARE IN GOOD CONDITION, NO DEFECTS WERE NOTED. O PS CHECK ENGINE, SRL ON AND OFF, ALL PARAMETERS WERE NORMAL AT THIS TIME IAW MM. MOISTURE IN CONNECTOR PLUGS. WEATHER AT TIME OF OCCURRENCE WAS RAIN. 2 L 7 2 4T 3 T RT A21EU E2WE 2002103100169 20021031 00169 CE 2002 10 31 EA11200202951 1 20021022 A 7830 INDICATOR LEAR 25 25 5170506 CE GE CJ610 CJ6101 30006 NE THRUST REVERSER MALFUNCTIONED A AOQA K NONE O OTHER IN INSP/MAINT 1 EA 11 25EC 25026 RT THRUST REVERSER ILLUMINTED IN FLIGHT, SYSTEM OPERATED CORRECTLY IWA MFG MM. VISUAL INSPECTION REVEALED STICKY LATCHE S AND DEFECTIVE T/R ACCUMULATOR. AWAITING FINAL FIX AND RETURN TO SERVICE. REMOVED AND REPLACED ACCUMUALTOR AND INDICA TOR GAUGE. LATCHES WERE CLEANED AND LUBRICATED. AS PRECAUTION, T/R SELECTOR VALVES WERE REPLACED ALONG WITH THE SYSTEM RELIEF VALVE AND THE RT SIDE T/R ACTUATOR. ALL CHECKS, NORMAL. 2 L 7 2 4J 4 J A10CE 1E16 2002103100170 20021031 00170 CE 2002 10 31 ECA2002F00002 1 20021001 A 7830 2505707 ACCUMULATOR LEAR 25 25 5170506 CE GE CJ610 CJ6101 30006 NE THRUST REVERSER LEAKING E ECAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 11 25EC 25026 RT THRUST REVERSER ARM LIGHT ILLUMINATED IN FLIGHT ON LEG NR 2. A/C RETURNED TO BASE. GROUND OPS CHECK WAS PERFORMED , SYSTEM WAS OPERATING CORRECTLY IAW MM. VISUAL INSP REVEALED FOLLOWING: LATCHES WERE STICKY AND REQUIRED CLEANING AND LUBRICATION. T/R SYSTEM ACCUMULATOR HAD LOST ITS CHANGE. ACCUMULATOR WAS RESERVICED BUT LEAKED DOWN AGAIN IN A SHORT T IME. GAUGE USED TO CHECK ACCUMULATOR WAS ALSO STICKING AND PROVIDING A FALSE INDICATION OF CHARGE. ACCUMULATOR WAS REP LACED ALONG WITH THE INDICATOR GAUGE. LATCHES WERE CLEANED AND LUBRICATED. AS A FURTHER PRECAUTION THE T/R SELECTOR VAL VES WERE REPLACED ALONG WITH SYSTEM RELIEF VALVE AND RIGHT SIDE T/R ACTUATOR. SYSTEM WAS RESERVICED AND OPS CHECKED. 2 L 7 2 4J 4 J A10CE 1E16 2002103100171 20021031 00171 CE 2002 10 31 ESUA116360 1 20020913 A 2910 2419151317 LINE LEAR 25 25D 5170514 CE GE CJ610 CJ6108 30006 NE HYD SYSTEM LOOSE E ESUA O OTHER J WARNING INDICATION AP APPROACH 1 CE 03 81AX 6387 279 PILOT DECLARED AN EMERGENCY ON APPROACH, IT WAS DISCOVERED THAT THE HYDRAULIC PRESSURE INDICATED (0). THE GEAR WAS ABLE TO BE PLACED IN THE DOWN AND LOCKED POSITION WITH NO EMERGENCY PROCEDURES. AIRCRAFT LANDED ON 13L. THE AIRCRAFT WAS S TOPPED ON THE RUNWAY BY THE USE OF EMERGENCY BRAKE SYSTEM. AIRCRAFT WAS TOWED FROM RUNWAY FOR THE DETERMINATION OF THE LOSS OF HYDRAULIC FLUID. (091302) 2 L 7 2 4J 4 J A10CE 1E16 2002103100172 20021031 00172 CE 2002 10 31 ESUA116380 1 20020914 A 5240 ACCESS PANEL LEAR 24 24 5170302 CE GE CJ610 CJ6101 30006 NE OXYGEN SERVICE DEPARTED E ESUA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 CE 03 105GA 116 AFTER DEPARTURE , PASSING THROUGH 13000 FEET, PILOT HEARD A LOUD BANG FOLLOWED BY A NOTICEABLE VIBRATION. PILOT DECLARE D AN EMERGENCY, RETURNED TO AIRPORT. MAINTENANCE WAS CALL TO INVESTIGATE THE PROBLEM. IT WAS DISCOVERED THAT THE OXYGE N SERVICE DOOR ON THE RIGHT FORWARD SIDE OF THE AIRCRAFT, OPENED DURING FLIGHT. NO DAMAGE TO DOOR OCCURRED. AIRCRAFT W AS RETURNED TO SERVICE. (090214) 2 L 7 2 4J 4 J A10CE 1E16 2002103100173 20021031 00173 CE 2002 10 31 ESUA119026 1 20021013 A 3260 25EN96 SQUAT SWITCH LEAR 35 35A 5170602 CE MLG INTERMITTENT E ESUA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 72LL 275 AFTER LANDING, DURING TAXI, SECOND TURN DURING TAXI OPERATION, THE AIRCRAFT DID NOT RESPOND TO BRAKING OR STEERING. AFT ER REALIZING THAT THE AIRCRAFT WAS NOT RESPONDING DURING TAXI OPERATIONS, THE CREW ENGAGED THE EMERGENCY BRAKES TO STOP THE AIRCRAFT. AT THIS TIME THE AIRCRAFT WHEELS WERE GOING OFF THE EDGE OF THE TAXIWAY. AIRCRAFT CAME TO A COMPLETE STO P 2 TO 3 FEET OFF THE TAXING WAY. MAINTENANCE HAS DETERMINED THAT THE LEFT SQUAK SWITCH WAS INTERMITTENT. (101502) 2 L 7 2 4F A10CE 2002103100174 20021031 00174 EU 2002 10 31 2002F00968 1 20020811 A 3246 DAS2062213 BEARING BRAERO DH125 HS125700A 4230170 EU RT MLG FAILED A UG8A O OTHER O OTHER TO TAKEOFF 1 GL 23 48FB 257129 THE RIGHT OUTBOARD WHEEL NR 4 DEPARTED THE AIRCRAFT DURING TAKEOFF FROM KDIK. THE OUTER WHEEL BEARING FAILED, ALLOWING THE WHEEL TO SLIDE FROM THE AXLE. AFTER EXAMINATION OF THE WHEEL, IT APPEARS THAT THE INNER BEARING HAD ALSO FAILED. T HE AXLE ASSEMBLY WHICH WAS DAMAGED FROM THE BEARING FAILURE WAS REPLACED. THE NR 4 WHEEL WAS REPLACED. THE NR 3 WHEEL WAS REPLACED AS A PRECAUTIONARY MEASURE. THE STRUT WAS SERVICED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A3EU 2002103100175 20021031 00175 2002 10 31 2002F00969 4 20020823 A 2210 DAMPER CESSNA 750 750 2076810 CE AUTOPILOT SYS MALFUNCTIONED A UG8A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 23 5113 7500013 AMBER YAW DAMP NOT CENTERED MESSAGE ILLUMINATED DURING TAKEOFF. TAKEOFF WAS ABORTED. YAW DAMP NOT CENTERED. CREW REFE RENCED AND FOLLOWED APPROVED FLIGHT MANUAL PROCEDURES ON PAGES 3-151/3-152 OF THE AFM. SYSTEM RESET WAS NORMAL. CREW C ONTINUED TRIP. (M) 2 L 7 2 4J RT T00007WI 2002103100176 20021031 00176 NM 2002 10 31 2002F00970 1 20020819 A 5730 65B1448618 SKIN BOEING 747 747243B 1384830 NM RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 66399 10702 23300 DURING CURRENT C-CHECK AT SIAEC, FOUND RT WING L/E STATIONS NR ILES 378, 400, 446, 467, AND 546 NOSE CAP POSITIONS CRACK ED AND CORRODED AT TOP ROW OF RIVETS. SIX CRACKED/ CORRODED AREAS TRIMMED OUT. ALL AREAS HFEC INSPECTED FOR ADDITIONAL CRACKS. NONE FOUND. FABRICATED FILLER, INTERNAL REPAIR DOUBLER AND TAPERED SHIMS FOR EACH AREA. OVERSIZED EXISTING H OLES. INSTALLED REPAIR SECTIONS IAW SRM 57-30-04 FIG 2 AT ILES 378, 400, 446, 467, 515 AND 546. (M) 2 L 7 4 4F A20WE 2002103100177 20021031 00177 NE 2002 10 31 2002F00971 2 20020626 A 7230 BLADE BEECH 99 C99 1154006 CE PWA PT6 PT6A36 52043 NE RT ENGINE MISSING A TIMA E ENGINE SHUTDOWN O OTHER NR NOT REPORTED 1 NM 01 238AL U238 PCE38035 AIRCRAFT EN ROUTE TO GEG FROM SLC, HEARD LOUD NOISE IN RIGHT ENGINE. ENGINE WAS SHUT DOWN. PRELIMINARY INVESTIGATION S HOWS PT DISC WITH SEVERAL BLADES MISSING. (M) 1 L 7 2 3T 4 T A14CE E4EA 2002103100178 20021031 00178 EA 2002 10 31 2002F00972 1 20020628 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47202 7202 FLT 5805 - MKE-PHL - DURING MAINTENANCE CHECKS AFTER LANDING IN PHL MAINTENANCE NOTICED THE CENTER AISLE EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE T-SHOT THE PROBLEM TO THE INVERTER. MAINTENANCE REMOVED AND REPLACED THE INVERTER. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2002103100179 20021031 00179 CE 2002 10 31 2002F00973 1 20020724 A 2913 WARNING SYSTEM CESSNA 750 750 2076810 CE COCKPIT ACTIVATED A UG8A O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 5113 7500013 YNG - 118 - AMBER RIGHT HYDRAULIC PUMP FAIL MESSAGE ILLUMINATED WHEN THRUST REVERSERS WERE DEPLOYED WHILE LANDING AT YNG . TROUBLE SHOOTING IN PROGRESS. (M) 2 L 7 2 4J RT T00007WI 2002103100180 20021031 00180 NM 2002 10 31 AALA20020796 1 20020602 A 3244 TIRE BOEING 757 757223 1384957 NM RT MLG SEPARATED A AALA A UNSCHED LANDING S K J AFFECT SYSTEMS FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 689AA 25731 ORD - FLT 1369 - EN ROUTE ORD-MIA - AFTER TAKEOFF, AMBER LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACT ION. LOWERED LANDING GEAR AND RECEIVED NORMAL SAFE INDICATIONS. CHECKED HYDRAULIC QUANTITIES AND FOUND LEFT SIDE DECRE ASING NOTICEABLY. RETURNED AND LANDED ORD WITHOUT INCIDENT. ON LANDING, LEFT SYSTEM QUANTITY HAD DECREASED TO .52. IN SPECTION ON THE RIGHT GEAR FOUND THE NR 7 TIRE HAD THROWN THE TREAD RUBBER FROM THE CORE AND HAD IMPACTED THE INBOARD FO RWARD AND INBOARD AFT BRAKE LINES. ON IMPACT, BOTH LINES WERE SEVERED. ALSO, FOUND RIGHT GEAR TILT ACTUATOR HYDRAULIC LINE LEAKING. REPLACED ALL EFFECTED HYDRAULIC LINES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002103100181 20021031 00181 WP 2002 10 31 GTIA0201024 1 20020912 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND RIGHT INBOARD SEAT TRACK FROM FS 200 TO FS 826 LIGHT CORROSION, BARE METAL, CHAFING. REMOVED SEAT TRACK FRO M STATION 200 TO STATION 826. LOCATED, DRILLED AND DEBURRED SEAT TRACKS AND SPLICES. INSTALLED SEAT TRACKS AND SPLICES . (M) 2 L 7 2 4F RT A6WE 2002103100182 20021031 00182 WP 2002 10 31 GTIA020997 1 20020915 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 200, LBL 56 INCHES HAS CORROSION AT FLOOR SUPPORT. FLOOR SUPPORT PREVIOUSLY REMOVED . FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2002103100183 20021031 00183 WP 2002 10 31 GTIA020998 1 20020917 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND LEFT FUSELAGE WEB AT FUSELAGE CUSP LINE STATION 1023 AND 1041 HAS PITTING CORROSION. REMOVED CORROSION. FA BRICATED DOUBLER AND INSTALLED. (M) 2 L 7 2 4F RT A6WE 2002103100184 20021031 00184 WP 2002 10 31 GTIA020999 1 20020927 A 2120 ODOR DOUG DC9 DC983 3022083 WP CABIN DETECTED A GTIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 23 827NK 49793 MCO - FLT 1865 - STRONG OIL/BURN SMELL AFTER ROTATION AT LGA-HEAVY RAIN, APU ON, RIGHT CABIN TEMP HOT. STOPPED AFTER AP U SHUTDOWN AND RIGHT TEMP TO AUTO. NO FURTHER PROBLEM OR SMELL DURING FLIGHT. INSPECT APU AND ACM'S OIL LEVELS NORMAL AND CLEAN. RAN BOTH PACKS SYSTEMS OFF APU AIR EXTENSIVELY THROUGHOUT TEMP RANGES AND NO OIL SMELL DETECTED. (M) 2 L 7 2 4F RT A6WE 2002103100185 20021031 00185 WP 2002 10 31 GTIA021000 1 20020917 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND FORWARD LAVATORY ASSEMBLY, FLOORBOARD ASSEMBLY LAV HAS CRACKED/DAMAGED. REMOVED FLOORBOARD. FABRICATED NEW FLOORBOARD. INSTALLED FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2002103100186 20021031 00186 WP 2002 10 31 GTIA021001 1 20020918 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND FLO'S FLOOR PANEL IS CRACKED UPPER AND LOWER SIDES. STOPPED DRILLED CRACK. FABRICATED REPAIR DOUBLER. INS TALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2002103100187 20021031 00187 WP 2002 10 31 GTIA021002 1 20020920 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND FORWARD CABIN, STATION 200 LBL 8 INCHES HAS CORROSION ON THE WEB/SUPPORT TRACK. REMOVED DAMAGED AREA. FABR ICATED DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER. (M) 2 L 7 2 4F RT A6WE 2002103100188 20021031 00188 WP 2002 10 31 GTIA021003 1 20020920 A 5320 CHANNEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND WEB PANEL, STATION 256 TO STATION 316 LEFT OUTBOARD HAS CRACKED AT HAT SECTION AND CORROSION AT SPACER/STRIP . REMOVED CRACKED AREA OF HAT SECTION. FABRICATED SPLICE AND HAT SECTION AND INSTALLED SPLICE AND HAT SECTION. (M) 2 L 7 2 4F RT A6WE 2002103100189 20021031 00189 WP 2002 10 31 GTIA021004 1 20020920 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND WEB PANEL STATION 316 TO STATION 396 LEFT OUTBOARD HAS GOUGED AT HATS SECTION/CORROSION AT AROUND FASTENERS HOLES. WEB PANEL SKIN AREA FOUND TO BE OUT OF LIMITS. REMOVED CORROSION AROUND FASTENER HOLES AND WEB PANEL SKIN. FAB RICATED NEW WEB PANEL SKIN. INSTALLED WEB PANEL SKIN. (M) 2 L 7 2 4F RT A6WE 2002103100190 20021031 00190 WP 2002 10 31 GTIA021005 1 20020921 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND AFT PIT STATION 1117 L28 L26R HAS CORROSION. REMOVED DAMAGED AREA. FABRICATED T- FOR REPAIR. DRILLED AND LOCATED HOLES. (M) 2 L 7 2 4F RT A6WE 2002103100191 20021031 00191 WP 2002 10 31 GTIA021006 1 20020920 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FLOORBOARD STATION 313 TO STATION 339 RBL 22 TO RBL 44 INCHES HAS CRACKED/DAMAGED AND GOUGED ALONG THE PANEL. FABRICATED NEW FLOORBOARD. INSTALLED FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2002103100192 20021031 00192 WP 2002 10 31 GTIA021007 1 20020920 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND FLOORBOARD STATION 256 TO STATION 313 RBL 22 TO RBL 44 INCHES HAS CRACKED/CORRODED A BOTTOM FLOOR BOARD. FA BRICATED NEW FLOOR PANEL. INSTALLED FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2002103100193 20021031 00193 WP 2002 10 31 GTIA021008 1 20020920 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND FLOORBOARD RIGHT STATION 905, 21 INCH BY 41 INCH, HAS CRACKED/DAMAGED AT FORWARD BOTTOM PANEL. FABRICATED N EW FLOORBOARD. INSTALLED FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2002103100194 20021031 00194 WP 2002 10 31 GTIA021009 1 20020920 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND FLOORBOARD STATION 160, 9 INCH BY 12 INCHES, HAS MUSHEY/CORROSION. FABRICATED NEW FLOORBOARD. INSTALLED FL OORBOARD. (M) 2 L 7 2 4F RT A6WE 2002103100195 20021031 00195 WP 2002 10 31 GTIA021010 1 20020920 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND FLOORBOARD, STATION 541 TO STATION 579 LBL 22 TO RBL 22 INCHES HAS SOFT/MUSHY AND GOUGED ALONG PANEL. FABRI CATED NEW FLOOR BOARD. INSTALLED FLOOR BOARD. (M) 2 L 7 2 4F RT A6WE 2002103100196 20021031 00196 WP 2002 10 31 GTIA021012 1 20020919 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND FORWARD FLOOR BOARD STATION 200-237 HAS DAMAGED AND CORRODED AT INSERTS, PANEL GOUGED ENTIRE LENGTH OF SURFA CE. FABRICATED NEW FLOOR BOARD. INSTALLED FLOOR BOARD. (M) 2 L 7 2 4F RT A6WE 2002103100197 20021031 00197 WP 2002 10 31 GTIA021013 1 20020919 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND STATION 862-912 FLOOR BOARD HAS DAMAGED/SOFT AND CORROSION AT INSERTS. FABRICATED NEW FLOOR BOARD. INSTALL ED FLOOR BOARD. (M) 2 L 7 2 4F RT A6WE 2002103100198 20021031 00198 WP 2002 10 31 GTIA021014 1 20020918 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND CENTER FLIGHT COMPARTMENT FLOOR PANEL BROKEN AROUND EDGES. FABRICATED CENTER FLIGHT COMPARTMENT FLOOR PANEL . INSTALLED FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2002103100199 20021031 00199 WP 2002 10 31 GTIA021015 1 20020918 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FLIGHT COMPARTMENT FLOOR PANEL BROKEN AROUND EDGES. FABRICATED FLOOR BOARD. INSTALLED FLOOR BOARD. (M) 2 L 7 2 4F RT A6WE 2002103100200 20021031 00200 WP 2002 10 31 GTIA021016 1 20020917 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND FLOOR BOARD, RIGHT OVER FUEL TANK ACCESS PANEL, 21 INCH BY 22 INCH, IS CRACKED/DAMAGED AT CORNERS. FABRICAT ED NEW FLOOR BOARD. INSTALLED FLOOR BOARD. (M) 2 L 7 2 4F RT A6WE 2002103100201 20021031 00201 WP 2002 10 31 GTIA021017 1 20020917 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 826 TO 988 HAS CRACKED/DAMAGED. FABRICATED NEW FLOOR BOARD. INSTALLED FLOOR BOARD. (M) 2 L 7 2 4F RT A6WE 2002103100202 20021031 00202 WP 2002 10 31 GTIA021018 1 20020917 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 160 TO 180 FLOOR BOARD HAS CRACK/DAMAGED. FABRICATED NEW FLOOR BOARD. INSTALLED FL OOR BOARD. (M) 2 L 7 2 4F RT A6WE 2002103100203 20021031 00203 WP 2002 10 31 GTIA021019 1 20020917 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN, STATION 769 CENTER, 38 INCH BY 42 INCHES HAS SOFT/MUSHY. FABRICATED FLOOR PANEL. INSTALLE D FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2002103100204 20021031 00204 WP 2002 10 31 GTIA021020 1 20020917 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND FLOOR PANEL CENTER BETWEEN AFT LAVATORY HAS SOFT/DAMAGED. FABRICATED A NEW FLOOR PANEL. INSTALLED FLOOR PA NEL. (M) 2 L 7 2 4F RT A6WE 2002103100205 20021031 00205 WP 2002 10 31 GTIA021021 1 20020918 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND CABIN FLOOR BOARD, STATION 256 TO 313, RBL 22 TORN, ELONGATED HOLE AND MISSING INSERTS. FABRICATED NEW PANE L. INSTALLED PANEL. (M) 2 L 7 2 4F RT A6WE 2002103100206 20021031 00206 WP 2002 10 31 GTIA021022 1 20020912 A 5346 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND CRACK ON NR 1 ENGINE PYLON UPPER ATTACH ANGLE 19 INCHES FROM TRAILING EDGE. REMOVED DAMAGED ANGLE. FABRICA TED NEW ANGLE. INSTALLED ATTACH ANGLE. (M) 2 L 7 2 4F RT A6WE 2002103100207 20021031 00207 WP 2002 10 31 GTIA021023 1 20020912 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND RIGHT OUTBOARD SEAT TRACK FROM FS 200 TO FS 826 LIGHT CORROSION, BARE METAL, CHAFING. CUT OUT DAMAGED SECTI ON. REMOVED DAMAGED SEAT TRACK. LOCATED AND DRILLED SPLICE. FABRICATED NEW SEAT TRACK AND SPLICES. INSTALLED NEW SEA T TRACK SECTION AND SPLICES. (M) 2 L 7 2 4F RT A6WE 2002103100208 20021031 00208 WP 2002 10 31 GTIA021025 1 20020913 A 5320 SUPPORT FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FORWARD PIT STATION 364-370 L29R-L28R, FLOOR SUPPORT FITTING ATTACHED TO INTERCOSTAL, IS CRACKED ACROSS THE TOP AN D DOWN BOTH SIDES. REMOVED DAMAGED FITTING. INSTALLED NEW FITTING. (M) 2 L 7 2 4F RT A6WE 2002103100209 20021031 00209 WP 2002 10 31 GTIA021026 1 20020914 A 5320 TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN, STATION 200 TO 180 LBL 7 INCHES HAS CORROSION AT THE TRACK. REMOVED TRACK. FABRICATED NEW TRACK. INSTALLED TRACK. (M) 2 L 7 2 4F RT A6WE 2002103100210 20021031 00210 WP 2002 10 31 GTIA021027 1 20020914 A 5320 TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 200-160 RBL 7 INCHES HAS CORROSION AT THE TRACK. REMOVED TRACK. FABRICATED NEW TRA CK. INSTALLED TRACK. (M) 2 L 7 2 4F RT A6WE 2002103100211 20021031 00211 WP 2002 10 31 GTIA021028 1 20020914 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 160 TO 200 LBL 55 INCHES IS CORRODED AT SUPPORT FLOOR. REMOVED FLOOR SUPPORT. FABR ICATED NEW FLOOR SUPPORT. INSTALLED SUPPORT. (M) 2 L 7 2 4F RT A6WE 2002103100212 20021031 00212 2002 10 31 MEX2002271 4 20020819 A 3420 INDICATOR DOUG MD88 MD88 3023688 NM COCKPIT MALFUNCTIONED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 158PL 49761 MID - FLT 494 - AIRCRAFT RETURNED TO GATE DUE TO MISALIGNMENT OF IRS 2 AND LIGHT OF ALIGN TURNED ON DURING TAXI, MESSAGE S IN FMS IRS 1 AND IRS 2 FAIL SHOWING FLAGS ON NAV 1 AND 2 IN BOTH RDMI. AT REVISION WAS ALIGNED THE IRS, IT WORKED OK. IRS OPERATION WAS VERIFIED IAW MM 34-43-01, TESTS OK. (M) 2 L 7 2 4F RT A6WE 2002103100213 20021031 00213 NE 2002 10 31 MEX2002273 2 20020822 A 7200 BLADE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D NE NR 2 ENGINE DAMAGED A ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 160PL 49763 FLT 239 - GDL-MEX - DURING OVERNIGHT PERFORMED BORESCOPE INSPECTION ON NR 2 ENGINE. DURING INSPECTION DAMAGE ON BLADES WAS DETECTED TO BE OUT OF LIMITS AND WAS NECESSARY TO CHANGE THE ENGINE NR 2. (M) 2 L 7 2 4F 4 F RT A6WE E2EA 2002103100214 20021031 00214 NE 2002 10 31 MEX2002274 2 20020823 A 7321 76960612 FCU DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A ASMF D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SW 23 491SH 49150 FLT 252 - MEX-GDL - AIRCRAFT RETURNED TO GATE DUE TO ACCELERATION FAILURE OF LEFT ENGINE. THE ACCELERATION CHAMBER WAS REVISED AND IT WAS PERFORMED A TRIM IAW MM 73-20-03 AND 73-11-00, TESTS OK. THE FCU OF LEFT ENGINE WAS REPLACED, TRIM W AS PERFORMED, TESTS OK, IAW MM 73-12-02, 71-00-01, 72-00-00. (M) 2 L 7 2 4F 4 F A6WE E9NE 2002103100215 20021031 00215 NE 2002 10 31 SIMA200228201 2 20021005 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT MALFUNCTIONED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 901AE 340B401 DURING CLIMB CREW REPORTED LEFT ENGINE OIL PRESSURE FLUCTUATION WITH MASTER WARNING. CREW FOLLOWED NORMAL SHUTDOWN PROC EDURES AND DECLARED AN EMERGENCY. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW AE WORK CARD. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2002103100216 20021031 00216 2002 10 31 SIMA200228202 4 20021007 A 3425 H341ADM2 INDICATOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE COCKPIT MALFUNCTIONED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 280AE 340B280 CREW REPORTED TO OPERATIONS THAT THEY SMELLED A STRONG ELECTRICAL SMOKE SMELL WITH THE AVIONICS FAN ON. MAINTENANCE REM OVED AND REPLACED THE STANDBY ADI IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2002103100217 20021031 00217 NM 2002 10 31 CALA0200516 1 20021030 A 5300 6546812186 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 39343 23581 CABIN FLOOR R/H DIAGONAL SUPPORT HAS CORROSION ON TOP SHIM AT STA 987-1006. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002103100218 20021031 00218 EU 2002 10 31 SIMA200228203 1 20021009 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LAVATORY DIRTY A SIMA O OTHER N FALSE WARNING DE DESCENT 1 SW 21 261AE 340B261 CREW REPORTED THE LAVATORY SMOKE DETECTOR LIGHT CAME ON DURING DESCENT. CREW REPORTED NO SMOKE. MAINTENANCE CLEANED TH E LAVATORY SMOKE DETECTOR OF DUST. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2002103100219 20021031 00219 SO 2002 10 31 SIMA200228204 1 20021006 A 5330 SKIN EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL FUSELAGE PUNCTURED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 DURING A PS2 INSPECTION A 1.5 INCH PUNCTURE WAS DISCOVERED BETWEEN FRAMES 65-66 AND STRINGERS 20L AND 21L. PERFORMED A CUT OUT OF THE DAMAGED AREA. PERFORMED A EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A FILLER A ND REPAIR DOUBLER. REPAIR DONE IAW STATEMENT GST300602. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002103100220 20021031 00220 EU 2002 10 31 SIMA200228702 1 20021012 A 2750 HP1716005 CONTROL VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE T/E FLAP MALFUNCTIONED A SIMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 21 350CF 340B350 CREW REPORTED UNCOMMANDED PITCH CHANGES IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL VALVE AND FLAP CON TROL VALVE AND FLAP CONTROL BOX IAW MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2002103100221 20021031 00221 2002 10 31 02FDEA00647 4 20020912 A 3140 COMPUTER DOUG MD11 MD11 3023602 NM E/E BAY MALFUNCTIONED A FDEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 25 615FE 48767 EN ROUTE FL370 GOT CABIN SMOKE ALERT, CAME ON THEN WENT OUT THEN CAME BACK ON. FOLLOWED RED TABS AND DIVERTED TO PDX. TEST OF SMOKE DETECTOR PER MM26-14-01-5. MSC FAULTED ITSELF ON LEG 10, 20, & 30. INSPECTED SMOKE DETECTORS & WIRING & CEILING AREA FROM SMOKE CURTAIN TO AFT PRESSURE BULKHEAD. INSPECTED HF COUPLERS FOR DAMAGE. ALL CHECKS NORMAL. R&R MSC PER M-M 31-42-01-4. OPS CHECK NORMAL. 2 L 7 3 4F RT A22WE 2002103100222 20021031 00222 NM 2002 10 31 AWXA200200953 1 20020902 A 5320 6935365 WEB BOEING 737 737375 13844BN NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 23707 YVR - MAJOR REPAIR - DURING C-03 CHECK A 1.5 INCH CRACK WAS FOUND ON SHEAR WEB ALONG UPPER ANGLE AT BS 500 - BS 520, BL 0. MAINTENANCE REMOVED DAMAGED SHEAR WEB. FABRICATED A NEW REPLACEMENT SHEAR WEB, INSTALLED REPAIR PART IAW DWG 69-35 365, AND B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002103100223 20021031 00223 NM 2002 10 31 C1HA200293007 1 20020926 A 3260 WARNING SYSTEM BOEING 727 727212 138407G NM COCKPIT ACTIVATED A C1HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 293AS 21348 AFTER T/O LG FAILED TO RETRACT NORMALLY, LEFT GEAR RED AND GREEN LIGHT ILLUMINATED IN THE OFF POSITION. RETURNED TO STL . RESET LT MLG UPLOCK IAW 32-32-51. NOT ABLE TO JACK A/C, NEED INFLIGHT FUNCTIONAL CHECK OF LT MLG UPLOCK. 2 L 7 3 4F A3WE 2002103100224 20021031 00224 GL 2002 10 31 C2XA02IA200 2 20020919 A 7520 8166101 BYPASS VALVE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 PYLON INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 16919 145393 IAH- FLIGHT 2908 NR 1 BLEED OVERTEMP WHILE CLIMBING THROUGH FL200 WHEN ENTERING ICING CONDITIONS QRH COMPLETED. MAINTE NANCE REMOVED AND REPLACED NR 1 FAN AIR BYPASS VALVE, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002103100225 20021031 00225 SO 2002 10 31 C2XA02IA201 1 20020920 A 3260 WARNING SYSTEM EMB 135 EMB135LR 3260305 SO COCKPIT MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 28529 145512 CREW REPORTED THAT WHEN THE LANDING WAS RETRACTED A MASTER WARNING INDICATION WAS ILLUMINATED. THE CREW FOUND THE GEAR TO BE INDICATING UP AND LOCKED AND TRIED CYCLING THE GEAR TO CLEAR THE WARNING. THE WARNING DID NOT EXTINGUISH AND THE AIRCRAFT RETURNED TO IAH WHERE MAINTENANCE PERFORMED EXTENSION AND RETRACTION TESTS TO THE GEAR SYSTEM. NO DEFECTS WERE FOUND AND THE GEAR SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE WITHOUT ANY FURTHER REPORTS OF THE SAME DISCREPANCY. 2 L 7 2 4F RT T00011AT 2002103100226 20021031 00226 SO 2002 10 31 C2XA02SH066 1 20020928 A 5330 14520571001 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 SHV- DURING C CHECK INSPECTION THREE GOUGES WERE FOUND ON SKIN FRAME 20 AT STRINGER 11L. MAINTENANCE REMOVED AND REPAIR ED DAMAGE IN IAW EC 5320-01075. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002103100227 20021031 00227 SO 2002 10 31 C2XA02SH070 1 20020927 A 5410 14576094004 STRINGER EMB 145 EMB145LR 3260212 SO LT NACELLE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 SHV DURING C CHECK INDENTATION WAS FOUND ON LT ENGINE LOWER NACELLE SKIN OUTBOARD STRINGER 8 INCHES FROM AFT END. MAINT ENANCE REMOVED DAMAGED AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE 2 L 7 2 4T RT T00011AT 2002103100228 20021031 00228 SO 2002 10 31 C2XA02TY145 1 20020920 A 3210 23093032003 PIN EMB 145 EMB145 3260210 SO RT & LT MLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS DURING A SCHEDULED 2C INSPECTION, MAINTENANCE FOUND THE RT AND LT MLG BRACE PINS SHOWING EVIDENCE OF WEAR AND CORRO SION. MAINT R&R BOTH LEFT AND RIGHT MLG BRACE PINS IAW EMB 145 AMM-32-10-03. ALL WORK WAS ACCOMPLISHED AND WILL BE REL EASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002103100229 20021031 00229 SO 2002 10 31 C2XA02TY148 1 20020923 A 5320 14500492401 ANGLE EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE PROFILE Z AFT OF FRAME 23. MAINTENANCE REMOVED AND REPLAC ED THE PROFILE Z. IAW EMB 135/145 SRM-51-40-02, CPM-51-21-04,05. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2002103100230 20021031 00230 SO 2002 10 31 C2XA02TY149 1 20020926 A 5320 14521725025 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 TYS DURING A SCHEDULED 2C INSPECTION THE AFT SERVICE DOOR SILL WAS FOUND CORRODED. MAINTENANCE REPAIRED CORRODED AREAS OF THE SEVICE DOOR SILL IAW EMB GST 1927/02A, EMB 135/145 CPM 51-21-04. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2002103100231 20021031 00231 NM 2002 10 31 C8GA20020012 1 20020926 A 7603 THROTTLE ARM BOEING 727 727225 1384077 NM PWA JT8 JT8D9A 52048 NE NR 3 ENGINE OUT OF ADJUST A C8GA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 SO 15 808EA 22439 666361 FLT 712 FROM TOL TO BNA. ON CLIMBOUT, NR 3 ENGINE WENT TO AN OVERSPEED CONDITION WITH NO THROTTLE RESPONSE. THE NR 3 EN GINE WAS SHUTDOWN AN APPROPRIATE CHECKLIST ACCOMPLISHED. DECLARED AN EMERGENCY AND NOTIFIED ATC, AIR TURNBACK TO TOL AN D AIRCRAFT LANDED WITHOUT INCIDENT. READJUSTED AND RESECURED THE NR 3 THROTTLE ROD END BETWEEN CROSSOVER SHAFT AND FUEL CONTROL. PERFORMED ENGINE RUN AND SYSTEMS CHECK GOOD IAW MM 72-00, 76-10 & 73-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002103100232 20021031 00232 NM 2002 10 31 DHL2002743013 1 20020927 A 3040 CONNECTOR BOEING 727 727225 1384077 NM WIPER MOTOR LOOSE A DHLA K NONE O OTHER NR NOT REPORTED 1 SO 01 743DH 22438 CAPTAIN'S WIPER INOPERATIVE. SECURED LOOSE CONNECTOR ON CAPTAIN'S WIPER MOTOR. 2 L 7 3 4F A3WE 2002103100235 20021031 00235 WP 2002 10 31 DHL2002873501 1 20020913 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 83065 46091 FUSELAGE EXTERNAL SKIN CORROSION, STA 280 L21L. PERFORMED MAJOR REPAIR IAW EO DHL 020903, ED-3125, EO SEMAN 2002738. R EMOVED CORROSION IAW SRM 51-1-8 PG 17-18 OUT OF LIMITS. FABRICATED A REPAIR DOUBLER, TWO FILLERS AND TWO INTERNAL FINGE R DOUBLERS IAW EO DHL 020903 , EO-3125 , EO SEMAN 2002738. INSTALLED REPAIR IAW EO DHL 020903, ED-3215, EO SEMAN 200273 8 & SRM 51-1-21, SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002103100236 20021031 00236 EU 2002 10 31 MALA020628 1 20021030 A 7600 CONTROL QUADRANT SAAB SF340 340B 7860101 EU GE CT7TP CT75A 30030 NE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 445XJ 340B445 AFTER TAKEOFF OF FLIGHT #2914, CREW REPORTED THE F1 STOP OPEN LIGHT ILLUMINATED ONCE GEAR WAS UP AND LOCKED. AIR RETURN TO MEM. LIGHT STAYED ON ALL THE WAY TO GATE ON LANDING NORMAL BLUE FI STOP LIGHT ILLUMINATED. MAINTENANCEREMOVED AND RE PLACE QUADRANT IAW #761002. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4T 4 T RT A52EU E8NE 2002103100237 20021031 00237 WP 2002 10 31 DHL2002873502 1 20020913 A 5730 5769545507 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 83065 46091 LT WING L/E LOWER OUTER SKIN CRACKED .500, STA XW761. PERFORMED MAJOR REPAIR IAW EO DHL 020904, ED-3124, EO SEMAN 20027 37. TRIMMED OUT DAMAGED OUTER SKIN IAW EO DHL020904, ED-3214, EO SEMAN 2002737. FABRICATED A REPAIR DOUBLER AND FILLER IAW ED DHL 020904, ED-3214 EO SEMAN 2002737. INSTALLED FILLER, AND DOUBLER IAW EO DHL020904, ED-3214, EO SEMAN 2002737 AND SRM 51-1-21, SRM 51-1-21A, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002103100238 20021031 00238 NE 2002 10 31 GLBA2002150 2 20020920 A 7230 PT6A67DPS GAS GENERATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE SEIZED A GLBA C ABORTED TAKEOFF Y ENGINE STOPPAGE TO TAKEOFF 1 NM 03 195GL 15458 3520 UE195 114179 LEFT ENGINE FAILED ON TAKE OFF, R&R GAS GENERATOR AND POWER SECTION. 2 L 7 2 4T 4 T RT A24CE E26NE 2002103100239 20021031 00239 EU 2002 10 31 MALA020572 1 20020924 A 2420 SELECTOR VALVE BAC 146 AVRO146RJ85A 1500097 EU STANDBY GEN FAULTY A MALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 515XJ E2333 DURING TAXI OUT ON FLIGHT NR 3439, STANDBY GENERATOR STARTED TO RUN. A/C RETURNED TO GATE IN INVESTIGATE, STANDBY GEN I NDICATED ON LINE, HOWEVER NO LOSS OF GREEN SYSTEM HYDRAULICS OCCURRED. STANDBY GEN CONTINUED TO RUN REGARDLESS OF SWITC H POSITION. MAINTENANCE REPLACED STANDBY GEN SELECTOR VALVE. 2 H 7 4 4F RT A49EU 2002103100240 20021031 00240 2002 10 31 MALA020573 4 20020923 A 3425 6226190113 COMPUTER SAAB SF340 340B 7860101 EU NR 2 MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 448XJ 340B448 DURING FLIGHT NR 2977, RIGHT SIDE RED HEADING. PERFORMED QRH SELECTED X-SIDE DATA. AIR RETURN TO MSP. MAINTENANCE REP LACED NR 2 AHRS COMPUTER. NR 2 AHRS COMPUTER CHECKS GOOD. IAW SF340, MM CHAP 34. 2 L 7 2 4T RT A52EU 2002120600100 20021206 00100 WP 2002 12 6 GTIA021092 1 20020929 A 5320 FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND PASSENGER CABIN, RIGHT STATION 120 TO 200 HAS TWO FITTINGS CORRODED. LOCATED AND DRILLED NEW FITTINGS. INS TALLED NEW FITTINGS. (M) 2 L 7 2 4F RT A6WE 2002120900139 20021209 00139 WP 2002 12 9 GTIA021112 1 20020927 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND MID CARGO PIT FS 520-693 SKIN CORRODED BETWEEN LONGERONS 27L-27R. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A6WE 2002120900140 20021209 00140 WP 2002 12 9 GTIA021113 1 20020928 A 5310 DOUBLER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND VENTRAL STAIRWAY JAMB CORRODED AT LT SIDE STATION 1418-1485. AFTER CLEANING FOUND EXFOLIATED DOUBLER. REMO VED EXFOLIATED DOUBLER. FABRICATED ANGLE. INSTALLED ANGLE. (M) 2 L 7 2 4F RT A6WE 2002103100241 20021031 00241 WP 2002 10 31 GTIA021115 1 20021014 A 5754 RUB STRIP DOUG DC9 DC983 3022083 WP L/E SLAT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 LEFT NR 0 LEADING EDGE SLAT, OUTBOARD END RUB STRIP PANEL HAS 3 INCH CRACK ON LOWER BOTTOM CORNER THROUGH 2 EA SCREW HOL ES. REMOVED PANEL AND REPAIRED AND REINSTALLED, SEALED AND SECURED. 2 L 7 2 4F RT A6WE 2002103100242 20021031 00242 WP 2002 10 31 GTIA021117 1 20021016 A 3260 PROXIMITY SWITCH DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE LT MLG DIRTY A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 824NK 53015 INTERMITTENT GEAR DOOR OPEN ANNUNCIATOR ON IN FLIGHT. FOUND LEFT MAIN GEAR DOOR OPEN PROX SWITCH GUMMED UP. CLEANED SW ITCH. 2 L 7 2 4F 4 F RT A6WE E2EA 2002103100243 20021031 00243 WP 2002 10 31 GTIA021119 1 20021016 A 5280 DOOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE NLG UNSECURE A GTIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 23 823NK 48020 DIVERTED, VIBRATION NOISE IN NOSE AREA AFTER GEAR RETRACTION AT LGA RECYCLED GEAR, NO HELP, PUT GEAR DOWN. RIGHT NOSE L ANDING GEAR DOOR UNSECURE. INSPECTED NOSE LANDING GEAR DOORS/WHEEL WELL SECURED NOSE LANDING GEAR DOORS. 2 L 7 2 4F 4 F A6WE E2EA 2002103100244 20021031 00244 EU 2002 10 31 SIMA200229501 1 20021021 A 3230 HP848430621 CONTROL VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LANDING GEAR MALFUNCTIONED A SIMA O OTHER O OTHER AP APPROACH 1 SW 21 391AE 340B391 DURING APPROACH, LANDING GEAR FAILED TO EXTEND WHEN SELECTED DOWN. RECYCLED GEAR HANDLE WITHOUT SUCCESS. ATTEMPTED MAN UAL EXTENSION WITHOUT SUCCESS. ACTUATED EMERGENCY EXTENSION/GEAR FREEFALL, NOSE AND LT MAIN GEAR EXTENDED AND LOCKED, RIGHT MAIN GEAR EXTENDED BUT DID NOT LOCK UNTIL CREW EXECUTED PULL UP MANEUVER. A/C LANDED WITHOUT FURTHER INCIDENTS. AFTER LANDING, MAINT FOUND RIGHT MAIN GEAR EXPLOSIVE BOLT DID NOT FIRE. MAINT REMOVED AND REPLACED LANDING GEAR CONTROL VALVE FOR GEAR NOT EXTENDING AND THE RT EXPLOSIVE BOLT CONNECTOR PLUG FOR THE RT MAIN NOT LOCKING INTO PLACE. ALL WORK DONE IAW MM. OPERATIONAL CHECKS WERE SATISFACTORY AND A/C WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2002103100245 20021031 00245 NM 2002 10 31 UIEA200200041 1 20020920 A 5712 65B149153 RIB BOEING 747 747230B 1384889 NM LT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC * 21221 DURING CURRENT C CHECK, FOUND LT WING LEADING EDGE RIB CRACKED, WING STATION ILES1024 AT THE VERTICAL STIFFENER COMMON T O THE UP STOP INTERCOSTAL. DAMAGED AREA TRIMMED OUT. HFEC INSPECTED TRIMMED AREA. NO ADDITIONAL CRACKING FOUND. FABR ICATED REPAIR DOUBLER, FILLER AND SHIM. 2 L 7 4 4F A20WE 2002103100246 20021031 00246 NM 2002 10 31 UIEA200200042 1 20020920 A 5414 SKIN BOEING 747 747230B 1384889 NM NR 3 PYLON DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 21644 DURING CURRENT C CHECK AT SIAEC FOUND NR 3 PYLON OUTBOARD SIDE LOWER AFT ACCESS PLATE CUTOUT DAMAGED ON RETAINING LIP, N AC 286 ABOVE WL 136. SKIN AND DOUBLER WERE TRIMMED TO REMOVE DAMAGE. HFEC INSPECTED AREA OF REMOVED DAMAGE. NO ADDITI ONAL CRACKING FOUND. FABRICATED FILLER AND REPAIR DOUBLERS. REPAIR DOUBLERS AND FILLER WERE INSTALLED IAW SRM. 2 L 7 4 4F A20WE 2002103100247 20021031 00247 NM 2002 10 31 UIEA200200043 1 20020920 A 5314 65B15069372 KEELBEAM BOEING 747 7472D3B 1384805 NM GE CF6 CF650* 30018 NE FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 DURING CURRENT C CHECK AT KLM FOUND KEEL BEAM BOX WEB UPPER SURFACE ON BOTH LEFT/RIGHT SIDES OF BL 0 CORRODED. CUT AND REMOVED WEB FROM BS 1265 TO 1273. PERFORMED OPEN HOLE HFEC INSPECTION OF REMOVED FASTENER HOLES IN REPAIR AREA. NO ADD ITIONAL CRACKS/CORROSION FOUND. FABRICATED REPLACEMENT WEB AND TWO SPLICE DOUBLERS. INSTALLED PARTS IAW SRM STANDARD P RACTICES. 2 L 7 4 4F 4 F RT A20WE E23EA 2002103100248 20021031 00248 NM 2002 10 31 UIEA200200044 1 20020920 A 5320 WEB BOEING 747 7472D3B 1384805 NM GE CF6 CF650* 30018 NE FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 81187 21251 DURING CURRENT C CHECK AT KLM FOUND SHEAR WEB FLANGE AT BS 340 TO 360 STR 26L WITH CRACKS ALONG THE SKIN FASTENER ROW. CUT AND REMOVED THE CRACKED FLANGE AT THE WEB RADIUS. HFEC INSPECTION PERFORMED ON EXTERNAL SKIN AND WEB CUT LINE. NO ADDITIONAL CRACKS FOUND. FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM, SB. 2 L 7 4 4F 4 F RT A20WE E23EA 2002103100249 20021031 00249 NM 2002 10 31 UIEA200200045 1 20020920 A 5320 WEB BOEING 747 7472D3B 1384805 NM GE CF6 CF650* 30018 NE FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 81187 21251 DURING CURRENT C CHECK, FOUND SHEAR WEB FLANGE AT BS 340 TO 360 STR 26R WITH CRACKS ALONG THE SKIN FASTENER ROW. CUT AN D REMOVED THE CRACKED FLANGE AT THE WEB RADIUS. HFEC INSPECTION PERFORMED ON EXTERNAL SKIN AND WEB CUT LINE. NO ADDITI ONAL CRACKS FOUND. FABRICATED REPAIR ANGLE, RADIUS FILLER STRIP AND TAPERED SHIM. INSTALLED PARTS AND FASTENERS WET WI TH BMS 5-95 SEALANT IAW SRM, SB. 2 L 7 4 4F 4 F RT A20WE E23EA 2002103100250 20021031 00250 NM 2002 10 31 UIEA200200046 1 20020920 A 5711 65B1028110 SPAR BOEING 747 7472D3B 1384805 NM GE CF6 CF650* 30018 NE WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 81187 21251 DURING CURRENT C CHECK, FOUND CENTER WING LOWER REAR SPAR WEB CORRODED AT LBBL66 TO 75. BLENDED CORROSION. PERFORMED H FEC OPEN HOLE INSPECTION AND SURFACE INSPECTION OF BLENDED AREAS. NO DEFECTS FOUND. MEASURED CORROSION DEPTH, MEASUREM ENTS EXCEEDED SRM LIMITS. FABRICATED REPAIR DOUBLER AND FILLERS. INSTALLED DOUBLERS AND FILLERS . 2 L 7 4 4F 4 F RT A20WE E23EA 2002103100251 20021031 00251 NM 2002 10 31 UIEA200200047 1 20020920 A 5414 65B941284 SKIN BOEING 747 7472D3B 1384805 NM GE CF6 CF650* 30018 NE NR 4 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 81187 21251 DURING CURRENT C CHECK, FOUND NR4 PYLON RIGHT HAND FORWARD ACCESS PLATE CUTOUT, BETWEEN NAC 211 AND 220, CRACKED. CRACK S INITIATED FROM THE CLIP NUT HOLES OF THE INNER LIP DOUBLER (4 PLACES). TRIMMED AWAY INNER DOUBLER AROUND THE ENTIRE C UTOUT. FABRICATED DOUBLER AND TRIPLER. INSTALLED DOUBLER AND TRIPLER IAW SRM. 2 L 7 4 4F 4 F RT A20WE E23EA 2002103100253 20021031 00253 GL 2002 10 31 SIMA200221601 2 20020804 A 7313 23073453A FUEL NOZZLE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LT ENGINE MALFUNCTIONED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 631AE 145139 ORD - FLT 4015 - DURING CLIMB, FLIGHT CREW REPORTED A SMOKE SMELL IN COCKPIT. AIRCRAFT WAS RETURNED TO ORD WITH NO FURT HER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED ALL 16 FUEL NOZZLES ON LEFT ENGINE IAW EMB MM. OPERATIONAL AN D LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002103100254 20021031 00254 GL 2002 10 31 SIMA200221701 2 20020805 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LEFT MALFUNCTIONED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 631AE 145139 CAE311127 ORD - FLT 4218 - DURING FLIGHT CREW REPORTED SMOKE IN COCKPIT. DUE TO REPEAT DISCREPANCY, ENGINEERING DIRECTED MAINTENA NCE TO REPLACE THE LEFT ENGINE. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKS WERE GOO D AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002103100255 20021031 00255 EA 2002 10 31 SIMA200222803 1 20020815 A 2820 CC670621021 TUBE CNDAIR CL600 CL6002C10 1390015 EA CENTER TANK CRACKED A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SW 21 504AE 10044 STL - FLT 3400 - IN CRUISE FLIGHT, FUEL QTY STARTED TO INCREASE IN THE CENTER TANK, WHILE LEFT WING TANK STARTED TO DECR EASE. CREATING A 600 LB IMBALANCE IN THE WING TANKS. REMOVED AND INSTALLED TUBE ASSEMBLY IN LEFT CENTER FUEL TANK. OP S CHECK GOOD IAW CRJ 700 AMM 28-21-15. (M) 2 L 7 2 4F RT A21EA 2002103100256 20021031 00256 SO 2002 10 31 SIMA200225501 1 20020911 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - FOUND GALLEY CENTER HAT BEAM CORRODED BEYOND LIMITS. INSTALLED NEW CENTER HAT BEAM IAW EMB145 SRM 145/1142 CHAPTE R 51, REV 19, 51-40-02, 51-40-04, 51-20-01, 51-20-03 AND EMB GST-2758/02. (M) 2 L 7 2 4T RT T00011AT 2002103100257 20021031 00257 NM 2002 10 31 0203466301 1 20021009 A 2720 MODULE BOEING 747 747451 1384940 NM RUDDER MALFUNCTIONED A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 01 661US 23719 DURING CRUISE WITH AUTOPILOT ENGAGED, LOST LOWER RUDDER CONTROL WITH 17 DEGREE DEFLECTION ACCOMPANIED WITH A LEFT YAW DA MPER EICAS MESSAGE. AIRCRAFT DECLARED A RED EMERGENCY, DIVERTED TO ANC AND DURING LANDING, EXPERIENCED HOT BRAKES ON TH E LEFT WING LANDING GEAR AND LEFT BODY LANDING GEAR. AIRCRAFT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. REPLACED TH E RUDDER POWER CONTROL MODULE, UPPER AND LOWER ACTUATORS FOR THE LOWER RUDDER, UPPER YAW DAMPER MODULE, NR 4 BRAKE, NR 4 TIRE, NR 8 BRAKE, AND THE LEFT BRAKE METERING VALVE. ACCOMPLISHED A DVI OF THE VERTICAL STABILIZER AND RUDDER. OPERAT IONAL AND VISUAL CHECKS GOOD. 2 L 7 4 4F RT A20WE 2002103100258 20021031 00258 EA 2002 10 31 SWIA200211368 1 20020912 A 5411 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NA LEFT PYLON CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 RIB AT AFT LOWER ATTACH SCREW OF LEFT PYLON LEADING EDGE PANEL IS CRACKED. FOUND DURING C CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-42-06 & 51-23-11. P/N: 601-37004-85. 2 L 7 2 4F 4 F RT A21EA E15NE 2002103100259 20021031 00259 WP 2002 10 31 0203479938 1 20021020 A 2782 39200485511 ACTUATOR DOUG DC9 DC931 3022065 WP L/E SLAT LEAKING A NWAA O OTHER F K J FLT CONT AFFECTED FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 1798U 47369 DURING APPROACH FOR LANDING WHEN CREW SELECTED SLAT DEPLOYMENT, THE AIRCRAFT HAD AN UNCOMMANDED ROLL TO THE LEFT ACCOMPA NIED BY SLAT DISAGREEMENT LIGHT. COMPLIED WITH COM PROCEDURES, THE SLATS WERE RETRACTED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE RIGHT T-DUCT MOUNTING BOLT HOLES WERE IMPROPERLY DRILLED CAUSING THE T-DUCT TO BIND DURING SLAT OPERATIO N. RIGGED BOTH T-DUCTS AND REPLACED THE LOWER LEFT SLAT ACTUATOR DUE TO LEAKING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002103100260 20021031 00260 WP 2002 10 31 0203489138 1 20021018 A 2131 53895811 SENSOR DOUG DC9 DC915 3022036 WP CABIN PRESSURE FAILED A NWAA B EMER. DESCENT O OTHER CR CRUISE 1 GL 01 9348 45787 AT FL310, THE CABIN PRESSURE BECAME UNSTABLE AND THEN COMPLETELY FAILED. CREW FOLLOWED COM PROCEDURES AND DESCENDED TO 8000 FT. MASKS DID DEPLOY IN THE CABIN. FLIGHT RETURNED TO MSP AND LANDED UNEVENTFULLY. MAINTENANCE FOUND THE OUTFLOW VALVE OUT OF RIG AND REPLACED THE DIFFERENTIAL PRESSURE SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT GOOD FOR SERVICE. 2 L 7 2 4F A6WE 2002103100261 20021031 00261 NE 2002 10 31 0203496739 2 20021021 A 7200 ENGINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7R4G2 52054 NE NR 2 BIRD INGESTION A NWAA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING C F.O.D. TO TAKEOFF 1 GL 01 639US 23887 715004 DURING TAKEOFF ROLL AT 120 KTS, THE NR 2 ENGINE SUFFERED A BIRD STRIKE AND THEN COMPRESSOR STALLED. THE TAKEOFF WAS NOT ABORTED. THE CREW REPORTED THE ENGINE STILL PROVIDED THRUST BUT HAD RISING EGT. THE ENGINE WAS SHUT DOWN, FUEL WAS DU MPED, AND THE AIRCRAFT RETURNED TO SFO. THE LANDING WAS WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE INCLUDING A BORESCOPE INSPECTION WITH NO DEFECTS NOTED. AN ENGINE RUN TO HIGH POWER WAS ALSO PERFORMED WITH NORMAL INDICATIONS. 2 L 7 4 4F 4 F A20WE E3NE 2002103100262 20021031 00262 NM 2002 10 31 0203505525 1 20021021 A 3397 WIRE BOEING 757 757251 1384970 NM CABIN BROKEN A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 525US 23619 FIRST CLASS EMERGENCY FLOOR LIGHTS WILL NOT ILLUMINATE. FOUND BROKEN WIRE IN TRACK LIGHTING AT ROW NR 1. REPAIRED WIRE . OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002103100263 20021031 00263 WP 2002 10 31 0203539602 1 20021022 A 2910 O-RING DOUG DC9 DC932 3022066 WP HYD SYSTEM WORN A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 602NW 47046 AT 200 FEET DURING APPROACH FOR LANDING, THE RIGHT HYDRAULIC SYSTEM PRESSURE WAS AT 500 PSI WITH THE RIGHT HYDRAULIC PRE SSURE LOW LIGHT ILLUMINATED. RIGHT HYDRAULIC QUANTITY WAS INDICATING ZERO. LANDING WAS UNEVENTFUL AT MSP. MAINTENANCE FOUND AND REPLACED A WORN O-RING ON THE MODULE CHECK VALVE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2002103100264 20021031 00264 WP 2002 10 31 0203549867 1 20021028 A 2120 DUCT DOUG DC9 DC951 3022051 WP A/C BAY SEPARATED A NWAA B EMER. DESCENT O OTHER CR CRUISE 1 GL 01 776NC 47786 AIRCRAFT LOST AUTO PRESSURIZATION AT FL240 AND CRUISE POWER. CREW ATTEMPTED MANUAL CONTROL BUT WAS UNABLE TO KEEP THE C ABIN FROM CLIMBING. COMPLIED WITH COM PROCEDURES. FLIGHT ACCOMPLISHED AN EMERGENCY DESCENT TO 10,000 FEET. MASK DID N OT DEPLOY AND AIRCRAFT CONTINUED TO AN UNEVENTFUL LANDING AT MSY. MAINTENANCE FOUND THE ACM EXHAUST DUCT SEPARATED. DU CT WAS REINSTALLED. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2002103100265 20021031 00265 EU 2002 10 31 0203553245 1 20021024 A 2120 DUCT AIRBUS 320 A320212 3930322 EU A/C BAY DAMAGED A NWAA B EMER. DESCENT O OTHER CL CLIMB 1 GL 01 345NW 00399 ON CLIMBOUT, CABIN PRESSURE CLIMBED AT 1000 FT/MIN AT 26,000 FT: CABIN AT 8000 FT AND CLIMBING AT 600 FT/MIN. ACCOMPLIS HED EMERGENCY DESCENT TO 10,000 FT. MAXIMUM CABIN PRESSURE REACHED WAS 12,000 FT. THERE WAS A LOUD AIR LEAK SOUND IN C ABIN. OXYGEN MASKS DID NOT DEPLOY. FOUND OUTBOARD BELLOWS DUCT FOR RIGHT PACK TORN AND CLAMP MISSING. REPLACED DAMAGE D DUCT AND PRESSURIZED AIRCRAFT TO 7.9 PSI DIFFERENTIAL WITH EACH PACK INDIVIDUALLY. SYSTEM TESTED NORMAL. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002103100266 20021031 00266 WP 2002 10 31 ABXA020213 1 20020919 A 7931 CONNECTOR DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3 52039 NE NR 1 ENGINE CORRODED A ABXA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 23 852AX 46016 670958 DURING CLIMBOUT THROUGH 12,000 FT, THE NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE . LIGHT REMAINED ON. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AFTER LIGHT BECAME BRIGHTER. INSPECTED THE NR 1 ENGINE M AIN OIL SCREEN, NO DEFECTS FOUND. FOUND LOOSE CANNON PLUG ON OIL PRESSURE DIFFERENTIAL SWITCH. CLEANED AND TIGHTENED A S NECESSARY. FOUND OIL PRESSURE SWITCH CANNON PLUG HEAVILY CORRODED. AIRCRAFT 852AX HAS BEEN PARKED BY AIRBORNE EXPRES S TO BE SCRAPPED, AND THE NR 1 ENGINE WAS FOUND TO BE UNSERVICEABLE. 2 L 7 4 4F 4 F 4A25 1E8 2002103100267 20021031 00267 WP 2002 10 31 ABXA020219 1 20020929 A 5320 99105035 WEB DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 FOUND NUMEROUS CRACKS IN AFT CUSP WEB, LEFT HAND SIDE APPROXIMATELY AT FS 1002. REPAIRED CUSP WEB IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002103100269 20021031 00269 WP 2002 10 31 ABXA020221 1 20020712 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP FUSELAGE BENT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 AFT CARGO, STATION 1320, RIGHT BUTT LINE 33, FLOORBEAM WAS BENT. REPAIRED AREA IAW ABX REA D853-43921MR AND DC-8 SRM 51 -1-8. 2 L 7 4 4F 4A25 2002103100270 20021031 00270 WP 2002 10 31 ABXA020225 1 20021001 A 7931 1G1741A PRESSURE SWITCH DOUG DC8 DC863F 302198F WP PWA JT3D JT3D3B 52039 NE NR 3 & 4 ENGINE FAULTY A ABXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 814AX 42 46041 645339 NR 4 LOW OIL PRESSURE LIGHT CAME ON. THROTTLED BACK BUT LIGHT STAYED ON. SECURED THE NR 4 ENGINE. ALSO THE NR 3 LOW O IL PRESSURE LIGHT CAME ON. THROTTLED BACK AND LIGHT WENT OUT, BUT ILLUMINATED INTERMITTENTLY. AIRCRAFT DIVERTED TO LOU ISVILLE. REPLACED THE NR 4 AND NR 3 ENGINE OIL LOW PRESSURE SWITCHES IAW DC-8 MM 79-32-02-2. OPS CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 2002103100271 20021031 00271 SO 2002 10 31 C2XA02BT067 1 20021028 A 2610 PANEL EMB 145 EMB145LR 3260212 SO FAULTY A C2XA O OTHER J WARNING INDICATION IN INSP/MAINT 1 SW 27 16546 145562 EWR---CO4080, LAV FIRE TEST WILL NOT TEST....MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR PANEL IAW EMB145 AMM #26-14 -02. OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002103100272 20021031 00272 SO 2002 10 31 C2XA02BT062 1 20021020 A 3230 LEVER EMB 145 EMB145 3260210 SO COCKPIT AREA FAULTY A C2XA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 27 16963 145116 EWR---CO3543, CREW REPORTED "AIR RETURN TO EWR: LANDING GEAR WOULD NOT RETRACT QRH UNSUCCESSFUL." MAINTENANCE REMOVED A ND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 AMM #32-32-02. REMOVED AND REPLACED LGEU IAW EMB145 AMM #32-32-01. LAN DING GEAR SWING OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002103100273 20021031 00273 GL 2002 10 31 C2XA02BT063 2 20021019 A 7200 AE3007A ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14905 145476 CAE311897 BTV---CO4361, CREW REPORTED, ON TAKEOFF AT 300 FT, NR 1 ENGINE FIRE WARNING ON EICAS CAME ON, DISAPPEARED AT 30 SECONDS LATER BEFORE ENGINE POWER WAS REDUCED AND SHUTDOWN. NORMAL LANDING WAS MADE. MAINTENANCE REMOVED AND REPLACED NR 1 ENG INE IAW TASK CARD. OPS. CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002103100274 20021031 00274 SO 2002 10 31 C2XA02BT068 1 20021028 A 3260 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO INTERMITTENT A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 22909 145459 CHS//CLT---CO4006, CREW REPORTED LANDING GEAR AIR/GROUND INDICATION FAILURE AFTER TAKEOFF FROM CHS. AIRCRAFT AIR RETURNE D TO CHARLESTON (CHS). AIRCRAFT MAINTENANCE FERRIED TO CHARLOTTE (CLT). MAINTENANCE PERFORMED LANDING GEAR EXTENSION AN D RETRACTION IAW EMB145 AMM 32-30-00, TESTED LANDING GEAR PROXIMITY SWITCHES IAW EMB145 AMM#32-63-05. NO DEFECTS FOUND L ANDING GEAR OPERATION NORMAL. (AIRCRAFT RETURNED TO SERVICE) 2 L 7 2 4T RT T00011AT 2002103100275 20021031 00275 WP 2002 10 31 ABXA020228 1 20021006 A 5310 59174631 DOOR FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 CRACK IN UPPER LEFT CORNER OF THE VENTRAL DOOR JAMB. REPAIRED AREA IAW REA D953-45345-MR. 2 L 7 2 4F A6WE 2002103100276 20021031 00276 WP 2002 10 31 ABXA020229 1 20021007 A 3350 5708458503 RELAY DOUG DC8 DC863 302198A WP CABIN FAILED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 817AX 17 45928 EMERGENCY BATTERY WAS GOING DEAD. REPLACED EMERGENCY LIGHTS BATTERY AND RELAY UNIT IAW DC-8 MM 33-50-01-2. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2002103100277 20021031 00277 WP 2002 10 31 ABXA020231 1 20021007 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 EMERGENCY LIGHTING WAS DIM. REPLACED EMERGENCY POWER SUPPLY BATTERIES IAW DC-9 MM 33-53-02-4. 2 L 7 2 4F A6WE 2002103100278 20021031 00278 WP 2002 10 31 ABXA020232 1 20021008 A 2611 100064901 SMOKE DETECTOR DOUG DC9 DC932 3022066 WP CARGO BAY MALFUNCTIONED A ABXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 983AX 2004 47257 LOWER CARGO FIRE LIGHT ILLUMINATED IN FLIGHT. REPLACED SMOKE DETECTORS IAW DC-9 MM 26-15-00-4-9. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002103100279 20021031 00279 WP 2002 10 31 ABXA020233 1 20021009 A 3230 LANDING GEAR DOUG DC9 DC932 3022066 WP NLG & MLG MALFUNCTIONED A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 988AX 47084 AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. HYDRAULICS WERE NORMAL, NO OTHER ABNORMAL INDICATIONS. RECYCLED GEA R, OPS CHECKED GOOD. NO FURTHER DIFFICULTIES. INSPECTED ALL THREE LANDING GEAR AND DOORS. NO DEFECTS NOTED. CYCLED L ANDING GEAR FOUR TIMES IAW DC-9 MM 32-30-00-2-0001. OPS CHECKED GOOD EACH TIME. 2 L 7 2 4F A6WE 2002103100280 20021031 00280 WP 2002 10 31 ABXA020235 1 20020924 A 2780 UTA09600 EYEBOLT DOUG DC9 DC941 302207N WP L/E SLAT BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 SLAT DRIVE MECHANISM WAS BROKEN AT THE INBOARD ACTUATOR ON THE LEFT WING. REPLACED EYEBOLT IAW DC-9 MM 27-80-05-2-0101. 2 L 7 2 4F A6WE 2002103100281 20021031 00281 WP 2002 10 31 ABXA020239 1 20020925 A 5320 99105034 WEB DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 NUMEROUS CRACKS IN CUSP WEB BETWEEN FS 1021 AND 1041 AT LEFT BUTT LINE 54. REPAIRED AREA IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002103100282 20021031 00282 WP 2002 10 31 ABXA020242 1 20020925 A 5320 591015899 ANGLE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DOOR PAN ANGLE WAS CRACKED. REMOVED, WELDED AND REINSTALLED DOOR PAN IAW DC-9 SRM 51-30-1 AND 51-30-2, DRAWING K05818. 2 L 7 2 4F A6WE 2002103100283 20021031 00283 WP 2002 10 31 MWEA020644 1 20021029 A 5311 9936534199 DOUBLER DOUG DC9 DC981 3022081 WP STA 200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 SUBFLOOR AT FRAME STATION 200 DOT 20 INBOARD OF PAX DOOR CUTOUT CORRODED UNDER FLOOR SUPPORT. -- FABRICATED DOUBLER AN D SUBFLOOR SKIN AND INSTALLED DOUBLER AND SUBFLOOR SKIN. 2 L 7 2 4F A6WE 2002103100284 20021031 00284 WP 2002 10 31 MWEA020648 1 20021029 A 5311 593607111 INTERCOSTAL DOUG DC9 DC981 3022081 WP STA 1150-1155 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 AFT CARGO COMPARTMENT HAS MODERATE CORROSION ON INTERCOSTAL AT STATION 1150 - 1155 BETWEEN LONGERON 30-29 RIGHT. -- RE MOVED CORROSION, DRILLED HOLES AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2002103100285 20021031 00285 WP 2002 10 31 MWEA020649 1 20021029 A 5230 5912995503 PAN DOUG DC9 DC981 3022081 WP LEFT FWD SCRATCHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 LEFT FORWARD EMERGENCY EXIT DOOR INNER PAN HAS SEVERAL AREAS OF SCRATCHES AND BARE METAL. -- BLENDED OUT SCRATCHES AND INSTALLED FASTENERS. 2 L 7 2 4F A6WE 2002103100286 20021031 00286 WP 2002 10 31 MWEA020650 1 20021029 A 5313 5911401107 LONGERON DOUG DC9 DC981 3022081 WP STA 200 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 ELECTRICAL COMPARTMENT LONGERON 24 LEFT CRACKED AT FRAME STATION 200 DOT 10. -- REMOVED LONGERON 24 LEFT AND FACTORY S PLICE, FABRICATED, FIT AND DRILLED UP NEW LONGERON AND NEW SPLICE SECTION. INSTALLED REPAIR AND REINSTALLED FACTORY SPLI CE. 2 L 7 2 4F A6WE 2002103100287 20021031 00287 WP 2002 10 31 MWEA020651 1 20021029 A 5311 59366712 STIFFENER DOUG DC9 DC981 3022081 WP STA 1155 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 AFT CARGO COMPARTMENT HAS MODERATE CORROSION ON FORWARD DOOR JAMB STIFFENER AT STATION 1155 LONGERON 29 RIGHT AND 27 RIG HT DOT 256. -- BLENDED OUT CORROSION PER MWX-MKE 02-00161H. 2 L 7 2 4F A6WE 2002103100288 20021031 00288 WP 2002 10 31 MWEA020652 1 20021029 A 5220 3913616501 SEAL DOUG DC9 DC981 3022081 WP FWD EXIT CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 RIGHT FORWARD EMERGENCY EXIT DOOR SEAL DEPRESSOR HAS SEVERAL AREAS OF CHAFING. -- BLENDED CHAFE MARKS, REMOVED UPPER D EAL DERESSOR, DRILLED NEW SEAL AND INSTALLED NEW SEAL DEPRESSOR. 2 L 7 2 4F A6WE 2002103100289 20021031 00289 WP 2002 10 31 MWEA020653 1 20021029 A 5330 591141023 FINGER DOUBLER DOUG DC9 DC981 3022081 WP STA 231-237 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FORWARD CARGO BAY SKIN LAP JOINT INCLUDING FINGER DOUBLER IS CORRODED AT STATION 231-237 LONGERON 26 LEFT DOT 1. -- RE MOVED FASTENERS ON LAP JOINT AND REMOVED LONGERON SPLICE AT STATION 229, FABRICATED TWO NEW SECTIONS OF FINGER DOUBLER. INSTALLED SHIMS AND 2 EACH FINGER DOUBLERS AND LONGERON SPLICE AND REMOVED AND REPLACE SEVERAL FASTENERS. 2 L 7 2 4F A6WE 2002103100290 20021031 00290 WP 2002 10 31 MWEA020654 1 20021029 A 5313 593601010 SUPPORT BRACKET DOUG DC9 DC981 3022081 WP STA 1361 LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 HYDRAULIC LINE SUPPORT BRACKET JUST FORWARD OF FRAME STATION 1361 LONGERON 17 RIGHT LOOSE. -- REMOVED SUPPORT BRACKER AT STATION 1361 LONGERON 17 RIGHT, LOCATED AND DRILLED LONGERON SPLICE. INSTALLED SUPPORT BRACKET AND LONGERON SPLICE. 2 L 7 2 4F A6WE 2002103100291 20021031 00291 WP 2002 10 31 MWEA020656 1 20021029 A 5311 49113832 FITTING DOUG DC9 DC981 3022081 WP STA 207 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FUSELAGE FRAME FLOOR ATTACH FITTINGS AT THE CUSP LINE LEFT SIDE IS CORRODED AT STATION 207. -- REMOVED FITTING FOUND OU T OF LIMITS, LOCATED AND DRILLED NEW FITTING AND INSTALLED FITTING. 2 L 7 2 4F A6WE 2002103100292 20021031 00292 WP 2002 10 31 MWEA020658 1 20021029 A 5313 39364451 FRAME DOUG DC9 DC981 3022081 WP STA 1117 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 AFT CARGO COMPARTMENT HAS LIGHT CORROSION ON AFT SIDE OF FRAME STATION 1117 LONGERON 30-29 LEFT DOT 264. -- REMOVED CO RROSION AND FRAME, LOCATED AND DRILLED NEW FRAME AND INSTALLED NEW FRAME. 2 L 7 2 4F A6WE 2002103100293 20021031 00293 WP 2002 10 31 MWEA020662 1 20021029 A 5311 5920323187 LONGERON DOUG DC9 DC981 3022081 WP STA 275 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FUSELAGE SKIN HAS DENT AT STATION 275 LONGERON 21 RIGHT DOT 86. -- INSPECTED DENT FOR CRACKES, NO CRACK FOUND, COLD FO RMED SKIN, FABRICATED REPAIR DOUBLER AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002103100294 20021031 00294 WP 2002 10 31 MWEA020663 1 20021029 A 5313 59360033 LONGERON DOUG DC9 DC981 3022081 WP STA 705 L24 RH DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FUSELAGE SKIN HAS DENT AT STATION 705 LONGERON 24 RIGHT DOT 52. -- INSPECTED DENT FOR CRACKS NO CRACKS FOUND, COLD WOR KED DAMAGE AREA , REQUESTED NDT FOR CRACKS. NONE FOUND, FABRICATED AND INSTALLED DOUBLER REPAIR 2 L 7 2 4F A6WE 2002103100295 20021031 00295 WP 2002 10 31 MWEA020661 1 20021029 A 5313 5920323187 SKIN DC9 DC981 3022081 WP STA 278 27 RH UNSERVICEABLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 NO RECORD OF PREVIOUS REPAIR, BLENDOUT ON FUSELAGE SKIN EXTERIOR AT STATION 278 LONGERON 27 RIGHT DOT 228. -- FABRICAT ED REPAIR DOUBLER AND INSTALLED DOUBLER COMPLETE PER SRM 51-30. 2 L 7 2 4F A6WE 2002103100296 20021031 00296 NM 2002 10 31 AWXA200201063 1 20021026 A 5511 65C25146 RIB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 0 0 23218 MCN - MAJOR REPAIR - DURING C-18 CHECK A .050" CRACK WAS FOUND ON THE L/H HORIZONTAL STABILIZER LEADING EDGE 5TH RIB FRO M OUTBOARD END STAB STA. 263.30. MAINTENANCE REMOVED CRACK ON 5TH RIB FROM OUTBOARD END OF L/H HORIZONTAL STABILIZER LEA DING EDGE AT STAB STA. 263.30, MATERIAL REMOVED .098" WITHIN LIMITS IAW B737-300 SRM 55-10-09, FIG. 101, PG. 101-106. TR EATED AND PRIMED IAW SRM 51-20--01, PG. 10 & 47, FIG. 2. 2 L 7 2 4F RT A16WE 2002103100297 20021031 00297 WP 2002 10 31 ABXA020246 1 20021011 A 3397 GROUND WIRE DOUG DC8 DC863F 302198F WP COCKPIT LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 WHEN HOT CUP WAS TURNED ON, EMERGENCY EXIT LIGHTS IN COCKPIT INTERMITTENTLY FLICKERED ON AND OFF RANDOMLY. FOUND LOOSE WIRING AT GROUND STUD FOR EMERGENCY POWER SUPPLY. TIGHTENED LOOSE CONNECTION AT GROUND STUD. NO DEFECTS NOTED WITH HOT CUP. SYSTEM OPS CHECKED GOOD IAW AMM 33-50-00-0. 2 L 7 4 4F 4A25 2002103100298 20021031 00298 SO 2002 10 31 SIMA200225502 1 20020910 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20. FABRICATED AND INSTALLED A DOUBLER ANGLE FILLER PLATE AND TWO SHI MS IAW EMB-145 SRM 145/1142, CHAPTER 53, REV 19 53-21-10, FIG 201 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002103100299 20021031 00299 SO 2002 10 31 SIMA200225601 1 20020913 A 3350 37541 SIGN EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 725AE 145312 RDU - FLT 4879 - CABIN AFT OVERHEAD EMERGENCY EXIT LOCATOR SIGN IS INOPERATIVE. RAI EMERGENCY EXIT LOCATION SIGN. (M) 2 L 7 2 4F RT T00011AT 2002103100300 20021031 00300 SO 2002 10 31 SIMA200225702 1 20020904 A 5320 145425369003 CLIP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 ABI - FOUND FRAME 68 SHEAR CLIP CORRODED. INSTALLED NEW SECTION OF SHEAR CLIP IAW EMB GST 2686/02 PARA 2, AND EMB GST-2 271/02A AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002103100301 20021031 00301 SO 2002 10 31 SIMA200225703 1 20020822 A 5320 14529150001 CROSSBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 ABI - THIS IS A LEVEL 2 FINDING, RIGHT BEAM HAS CORROSION AT FRAME 23. INSTALLED REPAIR DOUBLER IAW EMB GST-2615/02. ( M) 2 L 7 2 4T RT T00011AT 2002103100302 20021031 00302 SO 2002 10 31 SIMA200225704 1 20020824 A 5320 14529150001 CROSSBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 ABI - THIS IS A LEVEL 2 FINDING, CROSSBEAM AND PROFILE AT FRAME 23 CORRODED. INSTALLED SERVICEABLE CROSSBEAM AND PROFIL E IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002103100303 20021031 00303 SO 2002 10 31 SIMA200225705 1 20020826 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 ABI - THIS IS A LEVEL 2 FINDING, CARGO ENTRY WAY LOWER SILL CORRODED. REPLACED LOWER SILL BEAM IAW EMB 145 SRM 51-40-02 . (M) 2 L 7 2 4T RT T00011AT 2002103100304 20021031 00304 SO 2002 10 31 SIMA200225706 1 20020824 A 5320 14525831003 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 THIS IS A LEVEL 2 FINDING. AFT CARGO ENTRY GUSSET CORRODED. INSTALLED SERVICEABLE AFT CARGO ENTRY GUSSET IAW EMB 145 S RM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002103100305 20021031 00305 SO 2002 10 31 SIMA200225707 1 20020830 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 ABI - FOUND CORROSION WAS FOUND ON THE SERVICE DOOR CENTER SILL. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW AEAI ETN NR EM-53-036, AND STANDARD EMB 145 SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002103100306 20021031 00306 SO 2002 10 31 SIMA200225708 1 20020904 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AE 145105 ABI - FOUND CARGO DOOR CUT OUT LOWER SILL CORRODED. REPLACED SILL BEAM IAW EMB 145, SRM 145/1142, CHAPTER 51, REV 19, 5 1-40-02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002103100307 20021031 00307 SO 2002 10 31 SIMA200226101 1 20020915 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 642AE 145193 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON STRINGER 21R BETWEEN FRAMES 12 AND 13. CUT OUT 2 DAMAGED AREAS OF S TRINGER LOWER FLANGE BETWEEN FRAMES 12 AND 13. FABRICATED 2 FILLERS, 1 REINFORCEMENT, REPAIR DONE IAW EMB GST-2763/02 P ARA 2B, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002103100308 20021031 00308 SO 2002 10 31 SIMA200226102 1 20020913 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - DURING IMBV INSPECTION, THE FORWARD DIGITAL IN THE GALLEY WAS FOUND TO BE CORRODED. CUT OUT DAMAGED PORTION ON TH E DIGITAL, 16.5 BY 21, AND FABRICATED TWO DOUBLERS, ONE SHIM. REPAIR DONE IAW EMB 145, SRM 145/1142, REV 18 SRM 53-21-1 0, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002103100309 20021031 00309 SO 2002 10 31 SIMA200226103 1 20020912 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON GALLEY RIGHT FLOOR BEAM. REMOVED CORRODED GALLEY RIGHT BEAM. INSTA LLED NEW BEAM IAW EMB-145, SRM 145/1142, CHAPTER 51, RV 19, 51-40-02, AMERICAN EAGLE AIRLINES INC ETN NR EM-53-028 AND S TANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002103100310 20021031 00310 SO 2002 10 31 SIMA200226104 1 20020907 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - DURING AN IMBV INSPECTION, FOUND SERVICE DOOR CENTER SILL CORRODED. BLENDED CORRODED AREAS AND FILLED WITH EPOXY RESIN. FABRICATED TWO L PROFILE DIFFERENT SIZES AND REINFORCEMENT DOUBLER. REPAIR DONE IAW EMB GST-2721/02 PARA 3 AND AMERICAN EAGLE ENGINEERING TECH. (M) 2 L 7 2 4T RT T00011AT 2002103100311 20021031 00311 SO 2002 10 31 SIMA200226105 1 20020914 A 2611 337000271 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 616AE 145092 ORD - DURING FLIGHT CREW REPORTED THE BAGGAGE SMOKE LIGHT FLICKERED ON. CREW DISCHARGED FIRE BOTTLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCR AFT WAS RETURNED TO SERVICE. FIRE BOTTLE WAS ALSO REPLACED. (M) 2 L 7 2 4T RT T00011AT 2002103100312 20021031 00312 SO 2002 10 31 SIMA200226106 1 20020916 A 3040 163500112 WINDSHIELD EMB 135 EMB135LR 3260305 SO COCKPIT MALFUNCTIONED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 720AE 145279 JFK - FLT 4548 - CREW REPORTED A NOTICEABLE BURNING SMELL IN THE COCKPIT STARTING DURING CLIMB-OUT. AT APPROXIMATELY 14 ,000 FEET THE SMELL VARIED FROM VERY STRONG TO BARELY NOTICEABLE WITH NO VISIBLE SMOKE SEEN. THE CREW DIVERTED TO JFK A ND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW EMB MM. OPERAT IONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2002103100313 20021031 00313 SO 2002 10 31 SIMA200226108 1 20020917 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 640AE 145183 DLH - FLT 4168 - CREW REPORTED TWO AFT EMERGENCY LIGHTS TO BE INOPERATIVE. AIRCRAFT WAS FERRIED TO ORD FOR REPAIR. MAI NTENANCE REMOVED AND REPLACED A POWER SUPPLY BATTERY PACK IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002103100314 20021031 00314 SO 2002 10 31 SIMA200226110 1 20020917 A 2760 3605501003 VALVE EMB 135 EMB135KL 3260302 SO SPOILER MALFUNCTIONED A SIMA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 SW 21 815AE 145545 YOW - FLT 4097 - DURING APPROACH SPEED BRAKES DEPLOYED BUT WOULD NOT RETRACT ALONG WITH UNCOMMANDED NOSE DOWN PITCH TRIM RUN AWAY. CREW DECLARED AN EMERGENCY AND LANDED WITH NO FURTHER INCIDENT REPORTED. SPOILERS DID RETRACT UPON LANDING. MAINTENANCE REMOVED AND REPLACED THE SPOILER BRAKE VALVE IAW EMB MM. OP'S CHECK WAS GOOD. MAINTENANCE COULD NOT DUPL ICATE DISCREPANCY FOR PITCH TRIM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2002103100315 20021031 00315 SO 2002 10 31 SIMA200226111 1 20020901 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 THIS IS A LEVEL 2 ITEM, LEFT CABIN FLOOR SILL CORRODED BETWEEN FRAME 19-23. MAINTENANCE REPLACED FLOOR SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002103100316 20021031 00316 SO 2002 10 31 SIMA200226112 1 20020901 A 5315 7272233 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - THIS IS A LEVEL 2 FINDING, PREVIOUS REPAIR ON LEFT OMEGA BEAM FRAME 20 WAS FOUND CORRODED. MAINTENANCE REMOVED AN D REPLACED OMEGA BEAM IAW EMB 145 SRM 53-21-10 AND 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002103100317 20021031 00317 SO 2002 10 31 SIMA200226113 1 20020901 A 5315 7272233 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - THIS IS A LEVEL 2 FINDING, CENTER OMEGA BEAM RAMP REQUIRES REPLACEMENT. MAINTENANCE REMOVED AND REPLACED NEW CENT ER OMEGA BEAM IAW EMB 145 SRM 51-20-01, 51-20-05, 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002103100318 20021031 00318 SO 2002 10 31 SIMA200226114 1 20020901 A 5347 14530658001 SEAT TRACK EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - THIS IS A LEVEL 2 FINDING, RIGHT INBOARD NR 1 SEAT TRACK CORRODED. MAINTENANCE REMOVED AND INSTALLED RIGHT INBOAR D NR 1 SEAT TRACK IAW EMB 145 AMM 53-01-00. (M) 2 L 7 2 4T RT T00011AT 2002103100319 20021031 00319 SO 2002 10 31 SIMA200226115 1 20020901 A 5347 14530659001 SEAT TRACK EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - THIS IS A LEVEL 2 FINDING, LEFT NR 2 SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED LEFT N R 2 SEAT TRACK IAW EMB 145 AMM 53-60-00. (M) 2 L 7 2 4T RT T00011AT 2002103100320 20021031 00320 SO 2002 10 31 SIMA200226116 1 20020901 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - THIS IS A LEVEL 2 FINDING, SERVICE DOOR FORWARD SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002103100321 20021031 00321 SO 2002 10 31 SIMA200226117 1 20020908 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 ABI - THIS IS A LEVEL 2 FINDING, GALLEY CENTER HAT BEAM IS CORRODED ADJACENT TO PREVIOUS REPAIR. MAINTENANCE REMOVED AN D INSTALLED NEW GALLEY HAT BEAM IAW EMB 145 SRM 51-20-01, 51-40-02 AND GST 2758/02. (M) 2 L 7 2 4T RT T00011AT 2002103100322 20021031 00322 SO 2002 10 31 SIMA200226201 1 20020918 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 640AE 145183 RIC - FLT 4100 - EMERGENCY LIGHTS AT RIGHT FLOOR AND WING EXIT INOPERATIVE. RAI EMERGENCY BATTERY PACK AND RIGHT FLOOR LIGHT STRIPS IAW EMB AMM 33-50, OPS CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2002103100323 20021031 00323 SO 2002 10 31 SIMA200226802 1 20020919 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 ABI - DURING AN IMBV INSPECTION MAINTENANCE FOUND STRINGER 19R CHAFED BETWEEN FRAMES 52 AND 53. BLENDED CHAFED AREA. P ERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REP AIR DONE IAW EMB-145 SRM 145/1142, CHAPTER 53, REV 19, 53-24-02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002103100324 20021031 00324 SO 2002 10 31 SIMA200226803 1 20020921 A 2611 47359713 SMOKE DETECTOR EMB 135 EMB135LR 3260305 SO CARGO BAY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 704PG 145174 RDU - FLT 4634 - DURING CLIMB-OUT, CREW REPORTED THE BAGGAGE SMOKE ANNUNCIATION OCCURRED CREW RETURNED TO RDU AND LANDED WITH NO FURTHER INCIDENTS. CREW ADVISED CFT THAT A PRECAUTIONARY LANDING WAS TAKING PLACE. MAINTENANCE REMOVED AND RE PLACED FORWARD BAGGAGE SMOKE DETECTOR IAW EMB 135 26-15-00. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 L 7 2 4F RT T00011AT 2002103100325 20021031 00325 EU 2002 10 31 SIMA200226804 1 20020923 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU RT MLG DISCONNECTED A SIMA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SW 21 400BR 340B400 TUL - FLT 3651 - CREW REPORTED NO DOWN AND LOCKED GREEN LIGHT WHEN GEAR WAS SELECTED DOWN ON THE RIGHT MAIN LANDING GEAR . CREW ELECTED TO DECLARE EMERGENCY AS A PRECAUTION AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE FOU ND THE DOWNLOCK SWITCH CANNON PLUG ON THE RIGHT MAIN LANDING GEAR TO BE DISCONNECTED. CANNON PLUG WAS RECONNECTED AND A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002103100326 20021031 00326 EU 2002 10 31 SIMA200226805 1 20020924 A 5347 7253799383 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 380AE 340B380 ABI - DURING AN MBV INSPECTION, MAINTENANCE FOUND AN EXISTING REPAIR ON SEAT TRACK BL 18.3L STATION 297 TO BE CORRODED B EYOND SRM LIMITS. REMOVED THE PREVIOUS REPAIR. PREPARED SEAT TRACK. REPAIR DONE IAW SAAB 340 SRM 53-70-60 AND STANDAR D SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2002103100327 20021031 00327 SO 2002 10 31 SIMA200226806 1 20020924 A 3350 CONNECTOR EMB 135 EMB135LR 3260305 SO CABIN DISCONNECTED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 717AE 145272 DCA - FLT 4562 - CREW REPORTED THE EMERGENCY LIGHT BY FLIGHT ATTENDANT STATION TO BE INOPERATIVE. MAINTENANCE RECONNECT ED LOOSE CANNON PLUG ON THE BATTERY PACK ABOVE CEILING PANEL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 L 7 2 4F RT T00011AT 2002103100328 20021031 00328 EU 2002 10 31 SIMA200226807 1 20020922 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 269AT 269 MIA - MAINTENANCE REPORTED THE FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS REMAIN ILLUMINATED WHEN SWITCH SELECTED TO THE DISARM POSITION. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN POWER SUPPLY UNIT 29WL IAW ATR MM. OPERATIO NAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002103100329 20021031 00329 SO 2002 10 31 SIMA200226808 1 20020923 A 3350 744412 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 616AE 145092 DFW - DURING PHASE INSPECTION MAINTENANCE REPORTED THE EMERGENCY EXIT SIGN AT ROW 3BC TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE EMERGENCY EXIT SIGN AT ROW 3BC IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002103100330 20021031 00330 EU 2002 10 31 SIMA200227001 1 20020924 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 380AE 340B380 RIGHT FUSELAGE FRAME AT STATION 677 WAS FOUND DENTED. RECONTOURED DENT AND FABRICATED AND INSTALLED A DOUBLER IAW SAAB REPAIR STATEMENT 340SDS004430 PARA 5. (M) 2 L 7 2 4T RT A52EU 2002103100331 20021031 00331 EU 2002 10 31 SIMA200227002 1 20020924 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 380AE 340B380 MBV - FUSELAGE FRAME AT STATION 658.5 WAS FOUND DENTED. RECONTOURED DENT AND FABRICATED AND INSTALLED A DOUBLER IAW SAA B 340 STATEMENT 340SDS004430 PARA 5. (M) 2 L 7 2 4T RT A52EU 2002110100005 20021101 00005 NM 2002 11 1 AW32002F00000 1 20021004 A 3350 MS1557081 BULB BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE LT OVERWING BURNED OUT A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 802MA 22433 DURING POST FLIGHT, FOUND LT WING CENTER EMERGENCY LIGHT INOPERATIVE. RELAMPED LT OVERWING EMERGENCY LIGHT. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002110100006 20021101 00006 SO 2002 11 1 CZU2002F00000 1 20021029 A 2910 AN9181D CROSSTUBE PIPER PA32 PA32RT300T 7103216 SO LYC O540 TIO540* 41532 EA HYD POWERPACK CRACKED A CZUA K NONE O OTHER IN INSP/MAINT 1 EA 25 31888 3045 32R7887013 NOSE LANDING GEAR WOULD NOT EXTEND COMPLETELY WHEN COMMANDED. DECISION WAS MADE TO LAND AS IS. ON FINAL, GEAR WENT DOW N AND LOCKED AND AIRPLANE LANDED WITHOUT INCIDENT. IN THE SHOP, ON JACKS, GEAR FAILED TO RETRACT AND POWERPACK FAILED TO RUN. MOTOR WAS HOT TO TOUCH. RESERVOIR WAS NOTED TO BE EMPTY. ALL WIRING AND RELAY OPERATION WAS CORRECT. INSTALL ATION OF OVERHAULED POWERPACK RECTIFIED PROBLEM. DURING OPERATIONAL CHECKS, SLOW SEEP OF HYDRAULIC FLUID WAS NOTED FROM THE FEMALE CROSS FITTING BENEATH THE POWERPACK. INSPECTION OF THE FITTING SHOWED 3 OF THE FOUR BOSSES TO HAVE HAIRLINE CRACKS IN THEM, ONE OF WHICH WAS LEAKING. REPLACED FITTING WITH NEW. NO LEAKS NOTED AFTER OPERATIONAL TEST. 1 L 7 1 3O 3 O A3SO E14EA 2002110100007 20021101 00007 2002 11 1 EGR2002F00011 4 20021010 A 3454 6220876 VOR SYSTEM SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C* GL COCKPIT CONTAMINATED E EGRA O OTHER O OTHER AP APPROACH 1 EA 17 886AH 760153 APPROACH, VOR/ ILS SYSTEM. NOSE OF AIRCRAFT, WATER INFILTRATION FROM RAIN. SYSTEM RAMP CHECK AND FOUND WITH TOLERANCE AND SERVICEABLE. 1 G 7 2 3U 3 U H1NE E4CE 2002110100008 20021101 00008 CE 2002 11 1 F2P2002F00000 1 20021024 A 3520 51001073942 LINE CESSNA 414 414 2075908 CE CONT O520 TSIO520* 17040 SO OXYGEN SUPPLY CORRODED E F2PA K NONE O OTHER IN INSP/MAINT 1 SO 17 414AW 5241 4140520 WHILE PERFORMING AN OXYGEN SYSTEM FUNCTION CHECK A OXYGEN LEAK WAS DETECTED BETWEEN THE TWO LEFT SIDE PASSENGER OVERHEAD (O2) OUTLETS. A SMALL HOLE WAS FOUND IN (O2) LINE. THIS HOLE WAS A RESULT OF DISSIMILAR METAL CORROSION BETWEEN THE A LUMINUM (O2) LINE AND THE STEEL SUPPORT SPRINGS OF THE PASSENGER VENTILATION DUCT. UPON FURTHER INSPECTION CORROSION HA D DEVELOPED ON OTHER (O2) SUPPLY LINES WERE THESE LINES ARE IN CONTACT WITH THE VENTILATION DUCTS. 1 L 7 2 3O 3 O RT A7CE E8CE 2002110100009 20021101 00009 NM 2002 11 1 HALA0200609 1 20021019 A 2741 RELAY BOEING 717 717200 1383700 NM RROYCE BR700 BR700710A110 NE STAB TRIM INOPERATIVE A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 483HA 55128 PRIMARY TRIM INOPERATIVE. REPLACED PRIMARY TRIM DOWN BRAKE RELAY IAW MM. GROUND CHECK, OK. 2 L 7 2 4F 4 F TR A6WE E00057EN 2002110100010 20021101 00010 SO 2002 11 1 J7H2002F00000 2 20020901 A 8520 CRANKCASE CESSNA 404 404 2075901 CE CONT O520 GTSIO520* 17032 SO ENGINE CRACKED E J7HA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 19 C6RAM 1034 4040223 THREE FACTORY NEW ENGINE CRANK CASE CRACKED JUST OVER ONE THOUSAND HOURS OF OPERATIONS, DURING NORMAL OPERATIONS. THE L AST ENGINE CRANK CASE CRACKED AT 1034 AND PRIOR 1038 AND 1032 HOURS, WHICH APPEARS TO BE A TREND. 1 L 7 2 3O 3 O RT A25CE E7CE 2002110100011 20021101 00011 EU 2002 11 1 KBMA116004 1 20020913 A 2821 KD651511 FILTER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE FUEL SYSTEM FAILED E KBMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 19 230SH 2337 DURING PREFLIGHT WITH BATTERY AND FUEL PUMP ON THE AUXILLARY AIRFRAME FUEL FILTER BYPASS LIGHT IS ILLUMINATED. REPLACED WITH NEW FILTER. 1 G 7 1 3U 3 U NC H9EU E19EU 2002110100012 20021101 00012 EU 2002 11 1 KBMA116008A 1 20020917 A 2435 150SG122Q STARTER GEN SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE FAILED E KBMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 2273A 804 2273 DURING FLIGHT, EXPERIENCED PARTIAL GENERATOR/BATTERY FAILURE. REPLACED STARTER/GENERATOR WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2002110100013 20021101 00013 CE 2002 11 1 KC82002F00005 1 20021023 A 2821 WF334761 GASKET LEAR 25 25 5170506 CE GE CJ610 CJ6105 30006 NE FUEL FILTER MISINSTALLED E KC8A K NONE W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 GL 23 39CK 005 THE LEFT AIRCRAFT LOW PRESSURE FUEL LIGHT CAME ON AS THE ENGINES WERE POWERED UP. TROUBLE SHOT LEFT FUEL SYSTEM AND FOU ND THAT THE LOW PRESSURE FUEL FILTER GASKETS THAT ARE ATTACHED TO THE FILTER WERE NOT GLUED EVENLY ON THE ENTIRE SURFACE . THIS IN TURN MADE THE GASKET ACT AS A RESTRICTOR FOR THE OUTLET FUEL, AS THE ENGINE DEMANDED FOR FUEL INCREASED WITH RPM, THE RESTRICTION WAS GREAT ENOUGH TO DROP THE FUEL PRESSURE TO BELOW THE PRESSURE SWITCH LIMIT. INSPECTED THE REMAI NING RIGHT FUEL FILTER AND FOUND THE SAME PROBLEM WITH THE GASKET. INSPECTED FUEL FILTERS IN COMPANY STOCK AND FOUND AL L FILTERS WITH THE SAME PROBLEM. REMOVED THESE FILTERS FROM STOCK AND NOTIFIED THE VENDER. 2 L 7 2 4J 4 J A10CE 1E16 2002110100014 20021101 00014 EU 2002 11 1 M7K2002F00001 1 20021015 A 6220 350A31190703 STARFLEX SNIAS 350 AS350BA 8680817 EU MAIN ROTOR DEBONDED E M7KA A UNSCHED LANDING F FLT CONT AFFECTED HO HOVERING 1 WP 19 57717 2063 1334 PILOT REPORTED ODD SHUFFLING MOTION OF THE HELICOPTER IN HOVER AND ABORTED THE PLANNED FLIGHT. INVESTIGATION BY MAINTEN ANCE STAFF REVEALED THAT THE BLUE BLADES STARFLEX STAR ARM END BUSHING HAD AN ADHESIVE BOND FAILURE. THIS STARFLEX HAD A 30 HOUR INSPECTION IAW MFG MM. 13.9 HOURS PREVIOUSLY FOR THIS SPECIFIC DEFECT. THIS EXACT DEFECT IS ADDRESSED FOR ST ARFLEX. 1 G 7 1 3U NC H9EU 2002110100015 20021101 00015 WP 2002 11 1 MEX2002330 1 20021016 A 2913 AS66411LS5666 PUMP DOUG DC9 DC987 3022087 WP HYD SYSTEM FAILED B ASMF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 23 204AM 20865 49404 AIRCRAFT RETURN TO PLATFORM DUE TO LT ENGINE DRIVEN HYD PUMP FAILURE. LOST PRSSURE SUDDENLY. HYD PUMP WAS CHANGED AND RT HYD PUMP WAS DEFERRED IAW MEL. DURING OVERNIGHT SERVICE, RIGHT PUMP WAS REPLACED IAW MM, TESTS OK. 2 L 7 2 4F RT A6WE 2002110100016 20021101 00016 WP 2002 11 1 MEX2002332 1 20021020 A 2751 WARNING SYSTEM DOUG DC9 DC987 3022087 WP PWA JT8 JT8D NE SLAT DISAGREE MALFUNCTIONED W ASMF A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 23 803ML 49726 AIRCRAFT RETURN TO PLATFORM DUE TO TAKEOFF ALARM ACTIVATED. STP TEST WAS PERFORMED DETECTING A SLATS DISAGREE LIGHT. TECHNICAL PERSONNEL OPERATED THE FLAPS SEVERAL TIMES AND FAIL WAS NOT REPRODUCED. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110100017 20021101 00017 NM 2002 11 1 MYW2002F00004 1 20021014 A 3350 90052 CHARGER BOEING 727 727243 138408D NM PWA JT8 JT8D9 52048 NE CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 521DB VA4474 21266 DURING PREFLIGHT, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT COMES ON WHEN AIRCRAFT SHUTDOWN. C/A: REMOVED AND REPLACED BATTERY CHARGER FOR RIGHT OVERWING EXIT LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2002110100018 20021101 00018 CE 2002 11 1 P742002F00000 1 20021023 A 2140 5100110217 LINE CESSNA 414 414A 2075907 CE CONT O520 TSIO520* 17040 SO FUEL SYSTEM LEAKING E P74A K NONE K FLUID LOSS IN INSP/MAINT 1 GL 27 36989 414A0503 FUEL LINE AT HEATER LOCATION WHERE THE FUEL IS ROUTED INTO THE HEATER. FIRE CAUSED BY A PIN HOLE IN LINE TO HEATER. 1 L 7 2 3O 3 O A7CE E8CE 2002110100019 20021101 00019 SW 2002 11 1 PG92002F00004 1 20020927 A 7920 23008586 SCAVENGE PUMP BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL OIL SYSTEM FAILED B PG9R A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 19 3895D 13366 45590 CAE890285 DURING OPERATIONS, AIRCRAFT HAD FLUCTUATING OIL PRESSURE AND TORQUE. PILOT LANDED AIRCRAFT AND CALLED MAINTENANCE. MEC HANIC INSPECTED AIRCRAFT AND PERFORMED GROUND RUN. MECHANIC DETERMINED THAT ENGINE OIL SCAVENGE PUMP WAS NOT SENDING AD EQUATE AMOUNT OF OIL TO SYSTEM. 1 G 7 1 3U 3 U H2SW E1GL 2002110100020 20021101 00020 SW 2002 11 1 S642002F00000 1 20021018 A 2550 BRACKET BELL 407 407 1182206 SW ALLSN 250C 250C47B GL CARGO HOOK CRACKED E S64L K NONE O OTHER IN INSP/MAINT 1 SO 17 407HS 520 53256 DURING AN ANNUAL INSPECTION THE MECHANIC PULLED DOWN ON THE CARGO HOOK AND THE LT HAND HARD POINT BRACKET FAILED. LEAVI NG THE CARGO HOOK BEAM SUPPORTED ONLY BY THE RIGHT BRACKET. SHOULD THIS BRACKET FAIL, DURING SLING WORK THE RT BRACKET WOULD NOT BE ABLE TO SUPPORT THE LOAD. THIS CONDITION IS A HAZARD TO THE PILOT AS WELL AS ANYONE ON THE GROUND. 1 G 7 1 3U 3 U O H2SW E1GL 2002110100021 20021101 00021 EU 2002 11 1 S9H2002F00001 1 20021015 A 6410 TAB SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1 60030 NE T/R BLADE DEBONDED E S9HA K NONE O OTHER IN INSP/MAINT 1 WP 19 358NT 372 1016 TAIL ROTOR TRIM TAB DEBONDED APPROXIMATELY 90 MM ON BOTH SIDES, STARTING ON THE INBOARD END. TAIL ROTOR INSTALLED. FOU ND ON PREFLIGHT, POSSIBLE IMPROPER BONDING DURING MANUFACTURE. PART RETURNED TO MFG FOR EVALUATION. 1 G 7 1 3U 3 U H9EU E19EU 2002110100022 20021101 00022 EU 2002 11 1 SIMA200228703 1 20021013 A 2612 FIRE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CARGO BAY MALFUNCTIONED A SIMA F C ACTIVATE FIRE EXT. ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 247AE 340B247 DURING TAKE OFF CREW REPORTED THE CARGO SMOKE WARNING CAME ON. CREW ELECTED TO ABORT TAKE OFF AND BLOW THE NUMBER ONE F IRE BOTTLE. MAINTENANCE FOUND NO EVIDENCE OF FIRE OR SMOKE. MEL WAS ISSUED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2002110100023 20021101 00023 2002 11 1 TSAA0134180 4 20021014 A 3457 8184401003B GPS BOEING 737 7372T4 1384492 NM PWA JT8 JT8D NE NR 1 AND 2 FAILED A TSAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 13 808AL 23445 ENROUTE, THE NR 1 AND NR 2 GPS WERE UNABLE TO LOCK ON TO THE SATELLITE SIGNAL. THE AIRCRAFT RETURNED FOR MAINTENANCE WI TH NO FURTHER INCIDENT. REMOVED AND REPLACED THE NR 1 AND NR 2 GPS NPU. GROUND OPS CHECKS GOOD AND THE AIRCRAFT WAS RE TURNED TO SERVICE. FLIGHT VERIFICATION CHECKED GOOD ON BOTH UNITS ENROUTE. 2 L 7 2 4F 4 F A16WE E2EA 2002120400034 20021204 00034 NM 2002 12 4 TSAA0226197 1 20020922 A 3411 PITOT TUBE BOEING 737 7372M6C 1384708 NM PITOT/STATIC SYS OBSTRUCTED A TSAA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 805AL 21809 FLT 930 - HNL-OGG - DURING THE CLIMB-OUT OF HNL, THE FIRST OFFICERS AIR SPEED INDICATOR WAS INDICATING 40 KNOTS SLOWER T HAN THE CAPTAIN'S INDICATOR. THE AIRCRAFT RETURNED TO AND LANDED AT HNL WITH NO FURTHER INCIDENT. MAINTENANCE PERSONNE L REMOVED FOD FROM THE FIRST OFFICERS PITOT TUBE. THE PITOT/STATIC SYSTEM TEST AND CHECKED GOOD AND THE AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002110100024 20021101 00024 NM 2002 11 1 TSAA0229193 1 20021014 A 2130 7207375 RELIEF VALVE BOEING 737 7372X6C 1384552 NM CABIN DIRTY A TSAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 13 816AL 23122 AT THE TOP OF CLIMB WHEN THE THRUST LEVERS WERE BROUGHT BACK TO IDLE THE NR 2 ENGINE MADE A LOUD BANG LIKE A COMPRESSOR STALL. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED UNEVENTFULLY. REPLACED THE SAFETY RELIEF VALVE. GROUND OPS CHE CKED WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002110100025 20021101 00025 NM 2002 11 1 TSAA0233205 1 20021008 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM PWA JT8 JT8D9 52048 NE CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 2 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2002110100026 20021101 00026 NM 2002 11 1 TSAA0233207 1 20021011 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM PWA JT8 JT8D9 52048 NE CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECKED, OK. AIRCRAFT RETURNED TO SERVICE. ( TSAA80003325) 2 L 7 2 4F 4 F A16WE E2EA 2002110100027 20021101 00027 NM 2002 11 1 TSAA0233208 1 20021011 A 3350 900835A BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED CENTER EMERGENCY CONTROL MODULE BATTERY PACK DUE TO LOW VOLTAGE. OP CHECK, OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002110100028 20021101 00028 NM 2002 11 1 TSAA0233209 1 20021009 A 3350 8610066 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED NR 1 THRU 6 FLOOR EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2002110100029 20021101 00029 NM 2002 11 1 TSAA0233210 1 20021011 A 3350 9221009 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED LEFT OVERWING EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2002110100030 20021101 00030 NM 2002 11 1 TSAA0233211 1 20021011 A 3350 9221009 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED AFT ENTRY EMERGENCY IDENT LIGHT, INOPERATIVE. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2002110100031 20021101 00031 NM 2002 11 1 TSAA0249213 1 20021017 A 4920 655280131 APU BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D NE APU BAY FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 817AL 23292 JUST AFTER TAKEOFF THE APU OVERSPEED LIGHT CAME ON AND THE APU SHUTDOWN. THE AIRCRAFT RETURNED AND LANDED, WITH NO FURT HER INCIDENT. REPLACED THE APU ACCESSORY UNIT AND THE THREE SPEED SWITCH. GROUND OPS CHECK GOOD AND AN OVERWEIGHT LAND ING CHECK WAS COMPLETED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110100032 20021101 00032 NM 2002 11 1 TSAA0253206 1 20020926 A 5330 6545871517 SKIN BOEING 737 7372S2C 138448G NM PWA JT8 JT8D9 52048 NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 FUSELAGE SKIN CRACKED 1.7500 IN LONG AT BS 767 BETWEEN STRINGER 15L AND 16L. TRIMMED OUT DAMAGE AREA TO MAINTAIN 0.5 IN MINIMUM RADIUS ON CUTOUT. PERFORMED A DETAILED VISUAL INSP ABOVE AND BELOW STRINGER 15L AND HFEC INSP AROUND CUTOUT A REA, NO DEFECTS NOTED. MADE A 0.04 IN INSURANCE CUT WITH 63 MICRO-INCHES RA FINISH ON ALL CUTOUT EDGES. FABRICATED A 0 .032 INCH DOUBLER AND 0.50 INCH TRIPLER AND STRINGER AND FRAME FILLERS, MAINTAINING 0.5 INCH SHARP EDGES FROM SKIN AND A LL REPAIR PARTS. CLEANED, TREATED ALL EXPOSED AREAS WITH ALODINE AND BMS 10-11 TYPE 1 PRIMER. INSTALLED REPAIR PARTS A ND FASTENERS WET WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW ECO, A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2002110100033 20021101 00033 EA 2002 11 1 COMA0260612 1 20021027 A 2613 24403615 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA R/H FALSE INDICATION A COMA A UNSCHED LANDING J N WARNING INDICATION FALSE WARNING CR CRUISE 1 SO 01 967CA 7134 FLIGHT 5102 MLG BAY OVERHEAT WARNING.REPLACED THE R/H MLG BAY OVERHEAT SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2002110100034 20021101 00034 NM 2002 11 1 TSAA0277212 1 20021017 A 7711 LINE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D* NE EPR SYSTEM CONTAMINATED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 816AL 23122 ON TAKEOFF, THE NR 2 ENGINE WAS AT W.01 EPR, N1-80 PERCENT, EGT-400 DEGREES C, N2-82 PERCENT WITH FUEL FLOW AT 4000 LBS. THE AIRCRAFT RETURNED AND LANDED, WITH NOT FURTHER INCIDENT. MAINTENANCE REMOVED DEBRIS (BUGS) FROM THE NOSE DOME AND CLEARED THE LINES FOR THE EPR SYSTEM. GROUND OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110100035 20021101 00035 EA 2002 11 1 COMA0260613 1 20021026 A 5320 6003603031 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 L/H 718 DOUBLER AT STRINGER 10 TO 12 IS CRACKED 3 INCHES.REMOVED AND REPLACED DOUBLER I/A/W REO 601R-53-61-193 REV A 2 L 7 2 4F RT A21EA 2002110100036 20021101 00036 EA 2002 11 1 COMA0260614 1 20021026 A 5320 6003603032 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 R/H FS 718 DOUBLER AT STRINGER 10 TO 12 IS CRACKED 3 INCHES.REMOVED AND REPLACED DOUBLER I/A/W REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2002110100037 20021101 00037 EA 2002 11 1 COMA0260615 1 20021027 A 2150 7464513 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA ACM DIRTY A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 918CA 7018 FLIGHT 5906 BURNING SMELL FILLED COCKPIT.REPLACED THE COALESCER SOCKS ON THE L/H AND R/H ACM WATER SEPERATORS. 2 L 7 2 4F RT A21EA 2002110100038 20021101 00038 EA 2002 11 1 COMA0260616 1 20021029 A 3620 601R593201 SWITCH CNDAIR CL600 CL6002B19 1900309 EA L/H WING UNRELIABLE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 938CA 7046 FLIGHT 5571 L/H WING ANTI-ICE DUCT WARNING MESSAGE.REPLACED ALL 21 LEFT WING THERMAL SWITCHES. 2 L 7 2 4F RT A21EA 2002110100039 20021101 00039 EA 2002 11 1 COMA0260617 1 20021028 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA L/H BROKEN A COMA O OTHER O OTHER DE DESCENT 1 SO 01 957CA 16609 7109 FLIGHT 5479 PILOTS WINDSHIELD SHATTERED.REPLACED WINDSHIELD 2 L 7 2 4F RT A21EA 2002110100040 20021101 00040 EA 2002 11 1 COMA0260618 1 20021029 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER AP APPROACH 1 SO 01 967CA 7134 FLIGHT 5589 FLAP POSITION INDICATED 43 DEGREES WHEN SELECTED TO 45 DEGREES.FLAP INDICATION IS WITHIN LIMITS PER AMM. 2 L 7 2 4F RT A21EA 2002110100041 20021101 00041 NE 2002 11 1 COMA0260619 2 20021018 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE R/H SMOKE A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 931CA 14905 7037 807324 FLIGHT 5847 SMOKE IN CABIN.REPLACED THE R/H ENGINE, (EVIDENCE OF OIL AROUND VG ACTUATOR SPINDLE, SUSPECT #3 CARBON SEAL FAILURE.) 2 L 7 2 4F 4 F RT A21EA E15NE 2002110100042 20021101 00042 SO 2002 11 1 UG82002F00010 1 20021011 A 2612 51653154 CONTROL UNIT GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE LT FIRE CONTROL MALFUNCTIONED E UG8A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 23 5102 551 TAKEOFF WAS ABORTED, DUE TO A RED LT LOOP "B" OVERHEAD LEGEND AND ASSOCIATED CAS MESSAGE. PERFORMED ENGINE FIRE WARNING SYSTEM MALFUNCTION CHECKLIST. SYSTEM CHECKED PROPERLY. LT FIRE CONTROL BOX MALFUNCTIONED, REPLACED LT FIRE CONTROL BO X. OPERATION NORMAL. 2 L 7 2 4F 4 F RT A12EA E00057EN 2002110100043 20021101 00043 WP 2002 11 1 MWEA020667 1 20021030 A 5754 99193115 SLAT DOUG DC9 DC932 3022066 WP #4 DRIVE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LEFT SLAT #4 DRIVE ARM ATTACH BOLT CHAFING INBOARD RIB. -- REMOVED SLAT TRACK DOOR, BLENDED OUT DAMAGE AREA AND INSTAL LED SLAT DRIVE DOOR. 2 L 7 2 4F A6WE 2002110100044 20021101 00044 NM 2002 11 1 219PA0004 1 20021030 A 3242 26010425 BRAKE ASSY BOEING 737 737222 1384473 NM A PIDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 05 219PA 19956 #3 Brake dragging. Log page entry, (found heat shield from #3 main wheel lodged in rotor of brake assy. R&R brake IAW MM32-41-41 and R&R #3 wheel IAW MM32-45-11). Upon further investigation, found brake pad separated from brake resulting in damage to wheel and dislocation of heat shield. 2 L 7 2 4F A16WE 2002110100045 20021101 00045 WP 2002 11 1 CALA0200518 1 20021031 A 5240 59100817 SKIN DOUG DC9 DC982 3022082 WP A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 AFT SERVICE DOOR OUTER SKIN CRACKED IN TWO PLACES AFT END OF HOLD OPEN HOOK WELL. REPAIRED DOOR SKIN PER ECRA 5205-01008 AND SRM 52-05, FIG 20A. 2 L 7 2 4F A6WE 2002110100046 20021101 00046 WP 2002 11 1 CALA0200519 1 20021031 A 5200 4937644U503 FITTING DOUG DC9 DC982 3022082 WP A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 AFT SERVICE DOOR HOLD OPEN HOOK PAN ON DOOR CRACKED. REMOVED AND REPLACED HOOK PAN IAW SRM 51-40-02. 2 L 7 2 4F A6WE 2002110100047 20021101 00047 2002 11 1 UG82002F00011 4 20021012 A 3160 7014300901 DISPLAY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT MALFUNCTIONED E UG8A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 5112 3162 7500010 AFTER TAXIING FROM RAMP, RETURNED TO PARKING RAMP WITH EICAS YELLOW CAUTION MESSAGE FOR THE NR 5 COCKPIT DISPLAY UNIT. MESSAGE CREATED IN WRAP AROUND CIRCUIT BETWEEN THE NR 1 AND NR 5 DISPLAY UNITS. CYCLED AVIONICS MASTER SWITCH OFF THEN BACK ON. SYSTEM OPERATION WAS NORMAL. SYSTEM SERVICEABLE. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2002110100048 20021101 00048 EU 2002 11 1 UHLA66511 1 20020915 A 7722 CONNECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT79B 30030 NE ECU LOOSE A UHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 03 1495Z 340A149 AFTER DEPARTURE, RT ITT GAUGE FLUCTUATED 25 DEGREES, POWER REDUCED, FLUCTUATION WAS AT 5-10 DEGREE SWING. RETURNED TO F IELD. FOUND LOOSE CONNECTION AT ECU RESECURED, RAN ENGINE AT VARIOUS SETTINGS, OPS NORMAL. 2 L 7 2 4T 4 T RT A52EU E8NE 2002110100049 20021101 00049 NM 2002 11 1 USAA020396 1 20021013 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 22199 INTERCOSTAL HAS 10 INCH CRACK BL 0 BETWEEN STA 540 AND 560. INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM A12EU 2002120300129 20021203 00129 NM 2002 12 3 USAABB02171 1 20021006 A 1430 NAS6706D26 BOLT BOEING 767 7672B7 1385107 NM RT MLG DOOR FRACTURED A USAA K NONE D INFLIGHT SEPARATION AP APPROACH 1 EA 19 655US 25257 SJU - FLT 1677 - ON GEAR EXTENSION FOR LANDING AT SJU, AIRCRAFT LOST THE RIGHT MAIN LANDING GEAR SHOCK STRUT DOOR. MAIN TENANCE EXAMINED THE AIRCRAFT FOR FURTHER DAMAGE AND NONE WAS FOUND. AIRCRAFT WAS FLOWN ON CDL. THE MOST LIKELY CAUSE OF THE STRUT DOOR SEPARATION WAS BOLT FATIGUE FRACTURE. THE UPPER ATTACH BOLT WAS FOUND WITH THE WASHER MISSING. THE L OWER ATTACH BOLT WAS MISSING. IT WAS ASSUMED THAT THE WASHER WAS MISSING HERE ALSO, RESULTING IN THE BOLT BEING TIGHTEN ED BEYOND THE END OF THE THREADS INTO THE BOLT SHANK, CAUSING THE FRACTURE. THE DOOR THE DEPARTED THE AIRCRAFT DUE TO W IND LOADING. THE 767 FLEET WAS INSPECTED TO ENSURE THAT THE PROPER HARDWARE WAS INSTALLED AND TORQUED CORRECTLY. (M) 2 L 7 2 4F RT A1NM 2002110100050 20021101 00050 EA 2002 11 1 HNAA0200071 1 20021026 A 2900 82950010161 HYDRAULIC LINE DHAV DHC8 DHC8311 1386006 EA LEAKING A HNAA K NONE K FLUID LOSS AP APPROACH 1 EA 07 329EN 20563 290 ON APPROACH TO EWN CREW REPORTED LOSS OF #1 HYDRAULIC SYSTEM CONTENTS. RESULTING IN #1 RUDDER ISOLATION. PRESSURE DID NO T GO BELOW 3000 PSI AND QUANTITY DID NOT GO BELOW .6 QUARTS. INSTALLED TEMPORARY FLEX LINE AT LEFT INBOARD ROLL SPLIOLER ACTUATOR UNLOADING HYDRAULIC LINE. 2 H 7 2 4T RT A13NM 2002110100051 20021101 00051 NM 2002 11 1 USAASB02188 1 20021014 A 2131 7638101 CONTROLLER BOEING 737 737401 1384701 NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE INOPERATIVE A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 409US 23746 23879 ENROUTE, AT FL250, THE CABIN ALTITUDE WARNING HORN SOUNDED AS CABIN WAS NOTED TO BE CLIMBING AT 1,200 FEET PER MINUTE. FLIGHT DESCENDED TO FL 080. CREW REGAINED CONTROL OF CABIN PRESSURE USING MANUAL MODE. FLIGHT CONTINUED AND LANDED WIT HOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECK OF AUTO AND STANDBY PRESSURIZATION MODES. OPERATIONAL C HECK GOOD. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER AND SELECTOR PANEL AS PRECAUTIONARY. CONTROLLED PRESSURIZATI ON OF CABIN IN AUTO AND STANDBY MODES. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100052 20021101 00052 EU 2002 11 1 UVV2002F00001 1 20021018 A 5754 MY20142165 RIB AMD FALC20 FALCON20C5 2730107 EU GARRTT TFE731 TFE731* 01518 WP WING LE CRACKED B UVVR K NONE O OTHER IN INSP/MAINT 1 CE 03 405JW 54 RIB HAS CRACK RADIATING THROUGH FASTENERS ATTACHING RIB TO SPAR AND A PIECE IS MISSING APPROX 6 INCHES LONG AND .2500 IN CHES WIDE, CORROSION EVIDENT, POSSIBLY DUE TO INSULATION BEING WET. THIS DEFECT CAN ONLY BE SEEN IF LEADING EDGE IS DIS ASSEMBLED. 2 L 7 2 4F 4 F RT A7EU E6WE 2002110100053 20021101 00053 GL 2002 11 1 V9M2002F00000 1 20021006 A 3260 GW312200H5 BRACE BOMBDR BD700 BD7001A10 1390006 GL RROYCE BR700 BR700710A110 NE PROX SENSOR FAILED B V9MR K NONE O OTHER IN INSP/MAINT 1 SO 09 22BH 9040 UPON EXTENSION OF LANDING GEAR, AN UNSAFE GEAR ECAS MESSAGE AND LT MAIN GEAR SHOWED UNSAFE INDICATION. FAILED PROX SENS OR TARGET WITH IN BRACE. MODIFICATION TO BRACE UNDER REVIEW AT MFG. 2 L 7 2 4F 4 F RT T00003NY E00057EN 2002110100054 20021101 00054 NE 2002 11 1 WRLA200224 2 20021006 A 7230 CF650C2 BLADE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENG COMP FAILED A WRLA E C ENGINE SHUTDOWN ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 11 526MD 46998 NR 3 ENGINE SUSPECTED COMPRESSOR STALL ON TAKE OFF, CLIMB OUT. EGT OFF SCALE, NR 1 DROPPED, VIBRATION NOTED, SHUT DOWN ENGINE IAW INFLIGHT SHUTDOWN PROCEDURES. COMPLIED WITH DC10 MM CHECK LIST TWO ENGINE FERRY FLIGHT. ACCOMPLISH BORESCOP E NR 1 AND NR 2 ENGINE BORESCOPED NO DEFECTS FOUND AT THIS TIME. NR 3 ENGINE CHANGE REQUIRED. ENGINE HAD AN INTERNAL F AILURE OF COMPRESSOR BLADES DUE TO INTERNAL OR EXTERNAL OBJECT DAMAGE. 2 L 7 3 4F 4 F A22WE E23EA 2002110100055 20021101 00055 CE 2002 11 1 X5C2002F00000 1 20021017 A 3233 O-RING LEAR 24 24 5170302 CE GE CJ610 CJ6101 30006 NE LT MLG ACTUATOR NICKED E X5CA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 17 995TD 149 LOW HYDRAULIC PRESSURE ON APPROACH, AIRCRAFT RETURNED, MAINTENANCE BASE. FOUND HYDRAULIC LEAK AT LT MAIN GEAR ACTUATOR FITTING, HYDRAULIC FLUID LEVEL LOW. LEAK CAUSED BY NICKED O-RING. REPLACED O-RING, SERVICED HYDRAULIC SYSTEM, OPERATIO NAL CHECKED SPOILER, FLAP, AND LANDING GEAR SYSTEMS, ALL NORMAL. OPERATIONAL CHECKED BOTH ENGINE DRIVEN HYDRAULIC PUMPS , BOTH NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4J 4 J A10CE 1E16 2002110100056 20021101 00056 WP 2002 11 1 XEI2002F00000 2 20021013 A 7261 31082822 SCAVENGE PUMP SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE331* 01514 WP RT ENGINE INOPERATIVE E XEIA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 27 340AE 6084 AC510 P44421C RT ENGINE STARTED LOSING OIL PRESSURE GRADUALLY. PILOT LANDED AND THEN SHUTDOWN ENGINE ON TAXIWAY. TROUBLESHOOTING LEA D TO FINDING THE REAR TURBINE SCAVENGE PUMP, INOPERATIVE. 2 L 7 2 4T 3 T RT A8SW E2WE 2002110100057 20021101 00057 WP 2002 11 1 XEI2002F00001 2 20021013 A 7261 31082822 SCAVENGE PUMP SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE331* 01514 WP ENGINE SEIZED E XEIA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 27 340AE 6084 AC510 P44421C REAR TURBINE SCAVANGE PUMP SEIZED, CAUSING DROPPED OIL PRESSURE. 2 L 7 2 4T 3 T RT A8SW E2WE 2002110100058 20021101 00058 NM 2002 11 1 AASA0240146 1 20021012 A 5311 65C22909 SHEAR TIE BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING C CHECK, FOUND CORROSION ON FRAME SHEAR TIE AT BS 500C BETWEEN STR 28L AND 28R. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100059 20021101 00059 NM 2002 11 1 ASAA0240145 1 20021012 A 5311 65C22908 SHEAR TIE BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING C CHECK, FOUND CORROSION ON FRAME SHEAR TIE AT BS 500B BETWEEN STR 28L AND 28R REPAIRED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100060 20021101 00060 NM 2002 11 1 ASAA0240147 1 20021012 A 5320 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING "C" CHECK FOUND CORROSION ON FLOOR TO BULKHEAD SUPPORT AT BS 947 RBL 21 AND WL 156. REMOVED AND REPLACED IAW SRM . 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100061 20021101 00061 NM 2002 11 1 ASAA0240149 1 20021012 A 5310 65C32396 SHEAR TIE BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING C-CHECK FOUND CORROSION ON SHEAR TIE AT BS 727G BETWEEN STR 27 LT AND 26 LT. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100062 20021101 00062 WP 2002 11 1 ABXA020227 1 20021004 A 2760 3644322509 DRIVE UNIT DOUG DC8 DC863 302198A WP RT WING BROKEN A ABXA C ABORTED TAKEOFF F FLT CONT AFFECTED LD LANDING 1 GL 23 818AX 46075 ON LANDING ROLL, SPOILER HANDLE CAME BACK, SPOILERS DEPLOYED. BLUE SPOILER EXTEND LIGHT CAME ON, THEN WENT OUT. SPOILE R EXTEND LIGHT TESTED, BUT LIGHT WOULD NOT COME ON WITH MANUAL SPOILER EXTENSION. FOUND GROUND SPOILER PULLEY BRACKET I N RIGHT WHEEL WELL AND CRANK ASSEMBLY BROKEN IN THE RIGHT WING OF AFT AREA OF GROUND SPOILER. REPLACED PULLEY BRACKET I N RIGHT WHEEL WELL AND CRANK ASSEMBLY NR 1 IN AFT WING AREA IAW DC-8 AMM 27-60-00 AND RE-RIGGED GROUND SPOILERS IAW DC-8 AMM 27-60-00-5-0101. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2002110100063 20021101 00063 WP 2002 11 1 ABXA020247 1 20020930 A 5320 SB095201389 PAN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 47065 FORWARD ENTRANCE DOOR PAN CRACKED AT LOWER SIDE OF LOWER HINGE CUT OUT. REPLACED PAN SECTION IAW DC-9 SRM 51-30-1, 51-3 0-2, 51-30-5, 51-10-3, 51-20-0 AND 51-10-4. 2 L 7 2 4F A6WE 2002110100064 20021101 00064 WP 2002 11 1 ABXA020251 1 20021002 A 5313 49122621AX LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 47065 LONGERON 14 LEFT CRACKED AT STA 980. REPAIRED AREA IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2002110100065 20021101 00065 WP 2002 11 1 ABXA020252 1 20021002 A 5313 27779224 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 47065 LONGERON 17 LEFT CRACKED AT STA 966. REPAIRED AREA IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2002110100066 20021101 00066 WP 2002 11 1 ABXA020253 1 20021002 A 5313 27779223 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 47065 LONGERON 6 LEFT WAS CRACKED AT FS 718. REPLACED LONGERON SECTION IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2002110100067 20021101 00067 WP 2002 11 1 ABXA020254 1 20021002 A 5313 27779224 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 47065 LONGERON 7 RIGHT WAS CRACKED AT FS 597. REPLACED LONGERON SECTION IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2002110100068 20021101 00068 WP 2002 11 1 ABXA020258 1 20021023 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 929AX 45874 EMERGENCY LIGHTS NOT ARMED WAS NOT ILLUMINATED ON OVERHEAD PANEL. REPLACED 2 EACH, 1.2 VDC BATTERIES IAW DC-9 MM 33-53- 00-8. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2002110100069 20021101 00069 WP 2002 11 1 ABXA020265 1 20021009 A 5310 59101309 DOOR FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 CRACKED IN BEND RADIUS AT LEFT UPPER VENTRAL DOOR CORNER. CRACK LENGTH APPROXIMATELY 1.25 INCH IN LENGTH. REPAIRED CRA CK IAW DC-9 SRM 51-10-02. 2 L 7 2 4F A6WE 2002110100070 20021101 00070 WP 2002 11 1 ABXA020266 1 20021001 A 5330 SKIN DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 FUSELAGE LEFT AFT DOOR X-RAY SHOWED CRACK AT THE LOWER FORWARD CORNER OF DOOR CUTOUT. CUTOUT CRACKED 3.8125 INCHES SECT ION AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0, 51-1-21 AND 51-1-20. 2 L 7 4 4F 4A25 2002110100071 20021101 00071 NM 2002 11 1 ASAA0240151 1 20021012 A 5311 6546559 SHEAR TIE BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING C-CHECK FOUND CORROSION ON SHEAR TIE AT BS 927 BETWEEN STR 26RT AND 27RT. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100072 20021101 00072 WP 2002 11 1 ABXA020267 1 20021019 A 5330 SKIN DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 FUSELAGE RIGHT AFT DOOR X-RAY SHOWED CRACK AT AFT UPPER CORNER OF DOOR CUTOUT. INSTALLED REPAIR DOUBLER AT RIGHT AFT DO OR UPPER CORNER IAW DC-8 DRAWING SRO 8530024 AND DC-8 SRM 53-2-0. 2 L 7 4 4F 4A25 2002110100073 20021101 00073 NM 2002 11 1 ASAA0240152 1 20021012 A 5311 65C25228 SHEAR TIE BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING C CHECK FOUND CORROSION ON SHEAR TIE AT BS 727C BETWEEN STRINGER 25R AND 26R. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100074 20021101 00074 WP 2002 11 1 ABXA020268 1 20021001 A 5313 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 FUSELAGE LONGERON 11 RIGHT HAD A 1 INCH CRACK AT FS 1660. REPAIRED LONGERON 11 IAW REA D853-41973MR. 2 L 7 4 4F 4A25 2002110100075 20021101 00075 NM 2002 11 1 ASAA0240153 1 20021012 A 5311 65C323251 SHEAR TIE BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING C CHECK FOUND CORROSION ON SHEAR TIE AT STA 500E BETWEEN STR 27R AND 28R. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100076 20021101 00076 WP 2002 11 1 ABXA020269 1 20021001 A 5310 DOOR FRAME DOUG DC8 DC863 302198A WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 EXISTING REPAIR AT PASSENGER DOOR FORWARD UPPER CORNER DID NOT CONFORM TO DRAWING ES00863. REMOVED AND REPLACED REPAIR IAW DC-8 SRM 53-2-0. 2 L 7 4 4F 4A25 2002110100077 20021101 00077 NM 2002 11 1 ASAA0240154 1 20021012 A 5311 65C25299 SHEAR TIE BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING-C- CHECK FOUND CORROSION ON SHEAR TIE AT BS 727D BETWEEN STR 25R AND 26R. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100078 20021101 00078 WP 2002 11 1 ABXA020270 1 20021002 A 5310 DOOR FRAME DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 CRACK AT FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW DC-8 S RM 53-2-0. 2 L 7 4 4F 4A25 2002110100079 20021101 00079 NM 2002 11 1 ASAA0240155 1 20021012 A 5311 6546549 SHEAR TIE BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING C CHECK FOUND CORROSION ON SHEAR TIE AT BS 768 BETWEEN STR 26L AND 27L. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100080 20021101 00080 WP 2002 11 1 ABXA020271 1 20021019 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 MAIN CABIN FRAME AT STA 220 RIGHT SIDE WAS CRACKED AT FLOOR LEVEL. INSTALLED DOUBLER REPAIR AT STA 220 RIGHT AT FLOOR L EVEL IAW DRAWING K04888 AND DC-8 SRM. 2 L 7 4 4F 4A25 2002110100081 20021101 00081 WP 2002 11 1 ABXA020272 1 20021019 A 5311 FRAME DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 MAIN CABIN FRAME AT STA 240 RIGHT SIDE WAS CRACKED AT FLOOR LEVEL. INSTALLED DOUBLER REPAIR AT STA 240 MAIN CABIN RIGHT SIDE IAW DRAWING K04888 AND DC-8 SRM. 2 L 7 4 4F 4A25 2002110100082 20021101 00082 NM 2002 11 1 ASAA0240156 1 20021012 A 5311 65C32395 FRAME BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING C-CHECK FOUND CORROSION ON FRAME AT BS 727F BETWEEN STR 26LF AND 25LF. REPAIRED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100083 20021101 00083 WP 2002 11 1 ABXA020273 1 20021007 A 5330 SKIN DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 A/C EXHAUST DUCT SKIN WAS CRACKED AT THE FORWARD UPPER CORNER AT FS 50, STRINGER 28 LEFT. CUT OUT DAMAGE AND INSTALLED REPAIR IAW DRAWING SR08530020 AND DC-8 SRM. 2 L 7 4 4F 4A25 2002110100084 20021101 00084 NM 2002 11 1 ASAA0240158 1 20021012 A 5311 65C32396 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING -C- CHECK FOUND CORROSION ON FRAME AT BS 727G BETWEEN STR 26L AND 25L. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F RT A16WE 2002110100085 20021101 00085 NM 2002 11 1 ASAA0240159 1 20021012 A 5311 6546551 SHEAR TIE BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING -C- CHECK FOUND CORROSION ON SHEAR TIE AT BS 807 LBL 12 BETWEEN STR 26 LT AND 27 LT. REMOVED AND REPLACED IAW SR M. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100086 20021101 00086 NM 2002 11 1 ASAA0240160 1 20021012 A 5320 654578315 CHANNEL BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE VHF ANTENNA CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING -C- CHECK, FOUND CORROSION ON LOWER VHF ANTENNA SUPPORT CHANNEL. REMOVED AND REPLACED IAW SRM 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100087 20021101 00087 NM 2002 11 1 ASAA0240161 1 20021012 A 5314 65C329535 KEELBEAM BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING -C- CHECK FOUND CORROSION ON LT KEELBEAM AT BS 500G+4. REPAIRED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100088 20021101 00088 NE 2002 11 1 AT0200081 2 20020926 A 7200 BR715A130 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 1 FAILED A ZZDA O OTHER R Y J PARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 15 944AT 55007 NR 1 ENGINE AUTO SHUTDOWN. WHILE IN CLIMB POWER PASSING THROUGH FL 210 A LOUD POP WAS HEARD. NR 1 LEFT ENGINE OIL PRES SURE WENT TO ZERO. ENGINE RPM REDUCED TO IDLE AND CONTINUED WINDMILL, LEFT ENGINE OIL PRESSURE AND QUANTITY INDICATIONS WHERE X-OUT. ENGINE OIL PRESSURE QUANTITY LOW, EAD. REMOVED AND REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002110100089 20021101 00089 WP 2002 11 1 AT0200082 1 20021003 A 3350 CONTACTOR DOUG DC9 DC932 3022066 WP BATTERY LOOSE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 834AT 47488 DURING SERVICE CHECK FOUND LAST ROW EMERGENCY LIGHTS INOPERATIVE. TIGHTENED CONTACTS TO BATTERY FOR LAST ROW EMERGENCY LIGHTS, OPS CHECK GOOD IAW DC-9 MM 33-00. 2 L 7 2 4F A6WE 2002110100090 20021101 00090 WP 2002 11 1 AT0200083 1 20021003 A 3397 WIRE DOUG DC9 DC932 3022066 WP VENTRAL STAIRS DISCONNECTED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 847AT 47555 EMERGENCY LIGHT OVER TAIL CONE HANDLE ON SIDE OF VERTICAL STAIR WELL WILL NOT ILLUMINATE. CORRECTED WIRING TO EMERGENCY LIGHTS, OP CHECK GOOD IAW DC-9 MM 33-00. 2 L 7 2 4F A6WE 2002110100091 20021101 00091 NE 2002 11 1 AT0200084 2 20021021 A 7200 BR715A130 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE LEFT MAKING METAL A ZZDA E ENGINE SHUTDOWN R M PARTIAL RPM/PWR LOSS OVER TEMP DE DESCENT 1 SO 15 965AT 55026 AT FLIGHT LEVEL 28,000 AND DESCENDING WHEN THE AUTO THROTTLES RETARDED, A LOUD POP OCCURRED, THE AUTO THROTTLES WENT TO GROUND IDLE, THE EXHAUST GAS TEMPERATURE STARTED TO CLIMB, AT EGT 928 DEGREES CELSIUS. CREW SHUTDOWN THE LEFT ENGINE M ANUALLY. UPON ARRIVAL METAL WAS DISCOVERED IN THE TAIL SECTION. REMOVED AND REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002110100092 20021101 00092 NM 2002 11 1 AT0200086 1 20021028 A 2450 RELAY BOEING 717 717200 1383700 NM ELECTRICAL SYS FAILED A ZZDA K NONE O OTHER CL CLIMB 1 SO 15 949AT 55003 EMERGENCY POWER RELAY STUCK CLOSED. CYCLING SWITCH HAD NO EFFECT. A/C WAS DRAINING BATTERIES. MAINTENANCE REMOVED AND REPLACED A/C BATTERIES AS A PRECAUTIONARY. REMOVED AND REPLACED LEFT DCDU, LBTR, LEPR. 2 L 7 2 4F TR A6WE 2002110100095 20021101 00095 NM 2002 11 1 0203586627 1 20021015 A 5311 WEB BOEING 747 747251B 1384892 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 627US 21709 During "H" check found crack in frame web at BS 360 RBL 4. Repaired per EA 66-191664. 2 L 7 4 4F A20WE 2002110100096 20021101 00096 NM 2002 11 1 ASAA0240162 1 20021012 A 5320 654769012 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING C-CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 767 TO 727B+5, RBL20 AND WL156. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100099 20021101 00099 EA 2002 11 1 COMA0260568 1 20021005 A 3350 363782 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 927CA 7031 EMERGENCY LIGHTS INOPERABLE ROWS 2 THROUGH 5. REPLACED FLOOR TRACK LIGHT. 2 L 7 2 4F RT A21EA 2002110100110 20021101 00110 EU 2002 11 1 MALA020571 1 20020923 A 2150 4676C000002 A/C PACK BAC 146 AVRO146RJ85A 1500097 EU A/C BAY MALFUNCTIONED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 504XJ E2311 DURING POST FLIGHT 3474, SMOKE IN CABIN WHEN NR 2 PACK IS SELECTED ON. SMOKE ENTERED CABIN THROUGH AIR VENTS WITH PACK NR 2 SELECTED ON. MAINTENANCE DEFERRED PACK NR 2, IAW MEL 21-50-1 (B) PACK NR 1 OPERATES NORMALLY WITH APU. MAINTENANC E REMOVED AND REPLACED NR 2 PACK PER JC 0312 OPS/LEAK CHECKS GOOD. 2 H 7 4 4F RT A49EU 2002110100113 20021101 00113 2002 11 1 2002F00975 4 20021026 A 2565 D31393109 SLIDE BOEING 757 75733N 1384931 NM OVER WING DEPLOYED G O OTHER O OTHER TX TAXI/GRND HDL 1 GL 11 556TZ 600 600 32590 LEFT WING OFF WING ESCAPE SLIDE DEPLOYED. MAINTENANCE REMOVED AND REPLACED ESCAPE SLIDE IAW 757 AMM 25-65-01. 2 L 7 2 4F RT A2NM 2002110100114 20021101 00114 NM 2002 11 1 2002F00976 1 20021028 A 2150 A/C PACK BOEING 757 75728A 1384976 NM LEFT MALFUNCTIONED G O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 521AT 24368 FLIGHT NUMBER 73. DURING CRUISE LT PACK TEMP EICAS MESSAGE AND PACK INOPERATIVE LIGHT ILLUMINATED IN AUTO. MANUAL MODE O PERATES NORMAL. 2 L 7 2 4F RT A2NM 2002110100115 20021101 00115 EU 2002 11 1 MALA020574 1 20020925 A 3020 447301 MODULE SAAB SF340 SF340A 7850100 EU DE-ICE SYS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 89XJ 340A089 DURING FLIGHT 2789, RT ENGINE INTAKE HEAT LIGHT ILLUMINATED IN ICING CONDITIONS. AIR RETURN TO MSP. AIRCRAFT PASSED DE -ICE/ANTI-ICE CHECKS ON THE GROUND PRIOR TO FLIGHT. AFTER TAKEOFF, ENTERED MODERATE RAIN AND TURNED ON THE INTAKE ANTI- ICE RT INTAKE CAUTION LIGHT CAME ON INTERMITTENTLY, COMPLETED QRH, LIGHT WOULD ILLUMINATE IMMEDIATELY. MAINTENANCE FOUN D EXHAUST NOZZLE HAD BROKEN LEAD, REPLACED SHOE BOX. OPS CHECK GOOD IAW SAAB AMM 30-20-900-5. 2 L 7 2 4T RT A52EU 2002110100116 20021101 00116 EU 2002 11 1 MALA020576 1 20020924 A 3260 PIN SAAB SF340 340B 7860101 EU CONNECTOR BACKED OUT A MALA A UNSCHED LANDING O OTHER AP APPROACH 1 GL 15 417XJ 340B417 ON FLIGHT 3271, RT MLG WOULD NOT INDICATE DOWN AND LOCKED (GREEN) WHEN CREW SELECTED GEAR DOWN ON APPROACH IN LSE. AIR RETURN TO MSP. MAINTENANCE FOUND PUSHED BACK PIN IN CONNECTOR 6GA, RESECURED AND CLEANED FUNCTIONAL TEST GOOD AMM 32-30 -00. 2 L 7 2 4T RT A52EU 2002110100117 20021101 00117 NM 2002 11 1 2002F00935 1 20021009 A 3150 WARNING SYSTEM BOEING 757 75723N 1384973 NM RT ENGINE ACTIVATED G AMTA O OTHER N FALSE WARNING CL CLIMB 1 GL 11 519AT 27975 FLIGHT NUMBER 337. ON CLIMBOUT RT ENG OVERHEAT EICAS AND WARNING CAME ON. RIGHT BLEED SWITCHED OFF, POWER REDUCED AND LI GHT WENT OUT, CONTINUED WITH BLEED OFF. MAINTENANCE PERFORMED RT ENGINE HIGH POWER RUN APPROX 5 MINUTES AT TAKE-OFF POWE R, NO DISCREPANCY NOTED WITH OR WITH OUT ENGINE BLEED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2002110100118 20021101 00118 EU 2002 11 1 MALA020577 1 20020926 A 3230 CONTROL BOX SAAB SF340 340B 7860101 EU LANDING GEAR MALFUNCTIONED A MALA L ABORTED APPROACH O OTHER AP APPROACH 1 GL 15 456XJ 340B456 DURING APPROACH OF FLIGHT 3141 TO DTW, GEAR DID NOT COME DOWN AFTER CYCLING C/B AND GEAR STILL WOULD NOT COME DOWN. BRO KE OFF APPROACH, CYCLED GEAR. ALL INDICATIONS NORMAL. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL BOX IAW SA AB AMM 32-00-00. INSPECTED SWINGS ALL WOW HARNESS AND CONNECTIONS IN WHEEL WELLS, PERFORMED 15 GEAR SWINGS ALL CHECKS A ND GEAR INDICATIONS NORMAL. 2 L 7 2 4T RT A52EU 2002110100119 20021101 00119 NM 2002 11 1 2002F00936 1 20021011 A 3020 7646B000 VALVE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE INOPERATIVE G AMTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 554TZ 3163 3163 32588 031817 FLIGHT NUMBER 438. DURING DESCENT RIGHT ENGINE ANTI-ICE SWITCH VALVE LIGHT REMAINED ON, WITH SWITCH IN SELECTED ON POSIT ION. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE ANTI-ICE VALVE PER AMM 30-21-03-4. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002110100120 20021101 00120 EU 2002 11 1 MALA020583 1 20020925 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 DURING 4K INSPECTION IN CWA, FWD LT AISLE SEAT TRACK HAS CORROSION. MAINTENANCE COMPLETED REPAIRS IAW EO S53060. 2 L 7 2 4T RT A52EU 2002110100121 20021101 00121 NM 2002 11 1 2002F00937 1 20021012 A 3150 WARNING SYSTEM BOEING 757 75723N 1384973 NM EICAS ACTIVATED G AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 514AT 27971 FLIGHT NUMBER 273. DURING CRUISE EICAS STATUS MESSAGE LT ENG OH LP 2 DISPLAYED. MAINTENANCE PERFORMED TROUBLESHOOTING AS PER FIM 26-11-00, MESSAGE CLEARED, SYSTEM OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2002110100122 20021101 00122 EU 2002 11 1 MALA020585 1 20020924 A 5260 7253710871 TRACK SAAB SF340 340B 7860101 EU AIRSTAIRS CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 DURING 4K-INSPECTION IN CWA, MAINTENANCE FOUND AIRSTAIR SLIDE TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED AIRSTAIR SLIDE TRACK IAW SAAB SRM 51. 2 L 7 2 4T RT A52EU 2002110100123 20021101 00123 NM 2002 11 1 2002F00938 1 20021014 A 2612 WARNING SYSTEM BOEING 757 75733N 1384931 NM RT ENG FIRE DET FALSE ACTIVATION G AMTA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 554TZ 32588 FLIGHT NUMBER 438. R TURBINE OH DET 1 STATUS MESSAGE FOUND ON PREFLIGHT, OVERHEAT SYSTEM TEST OK. MAINTENANCE PERFORMED FIM 26-13-00. MSG "RT TURBINE OVERHEAT DET 1" NO LONGER SHOWS. SYSTEM OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002110100124 20021101 00124 EU 2002 11 1 MALA020586 1 20020927 A 2913 521449 PUMP BAC 146 AVRO146RJ85A 1500097 EU ENGINE FAILED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 506XJ E2314 DURING FLIGHT GREEN SYSTEM HI TEMP LIGHT ILLUMINATED APPROXIMATELY 1 HOUR INTO FLIGHT. MAINTENANCE REPLACED NR 3 ENGINE EDP. OPS AND CHECK LEAK GOOD. 2 H 7 4 4F RT A49EU 2002110100125 20021101 00125 NM 2002 11 1 2002F00940 1 20020929 A 2163 SENSOR BOEING 757 75728A 1384976 NM EQUIP COOLING MALFUNCTIONED G AMTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 521AT 24368 FLIGHT NUMBER 208. REJECTED TAKEOFF APPROX 100 KTS DUE TO EICAS MESSAGE EQUIPMENT OVHT ILLUMINATED. AFTER SELECTING ALT EQUIP COOLING, OVHT LIGHT EXTINGUISHED BRIEFLY, THEN REILLUMINATED. RETURNED TO GATE TO INVESTIGATE OVHT. MAINTENANCE RE MOVED AIR FILTER AND FLOW SENSOR TO CLEAN THEM IN ACCORDANCE WITH AMM 21-58-21, TASK 21-58-21-002-001 AND 21-58-21-142-1 42, NO FAULTS PRESENT AT THIS TIME. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2002110100126 20021101 00126 EU 2002 11 1 MALA020587 1 20020927 A 7931 83465 SWITCH SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 370PX 340B300 DURING FLIGHT 2768, RT OIL PRESSURE LIGHT ILLUMINATED ON CWP. ENGINE PRESSURE AT 75 PSI PROP OIL AT 80 PSI, BOTH CONSIS TENTLY AT THOSE PRESSURES. AIR RETURN TO MSP. MAINTENANCE REPLACED RT ENGINE CWP PSI SWITCH P/N 8346-5 IAW SAAB AMM 79 -30-5-4. OPS CHECKS AND LEAK CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002110100127 20021101 00127 NM 2002 11 1 2002F00941 1 20020925 A 3610 312N53217 DUCT BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE LEAKING G AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 521AT 3735 3735 24368 31748 FLIGHT NUMBER 504. EICAS STATUS MESSAGE R STRUT OH DET 1 DISPLAYED DURING TAXI. MAINTENANCE REMOVED AND REPLACED ENGINE SUPPLY DUCT INACCORDANCE WITH M.M. 36-11-01. RAN ENGINE AND PERFORMED HIGH POWER TEST AND LEAK CHECK. AIRCRAFT RETURNED TO SERIVE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002110100128 20021101 00128 EU 2002 11 1 MALA020588 1 20020929 A 2913 PUMP SAAB SF340 SF340A 7850100 EU HYD SYSTEM FAILED A MALA C ABORTED TAKEOFF S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 15 106XJ 340A106 DURING TAXI OF FLIGHT 3329, A/C LOST ALL HYDRAULIC PRESSURE WITH ASSOCIATED LOSS OF NOSE WHEEL STEERING AND BRAKING, PIC UTILIZED DIFFERENTIAL POWER TO EXIT TAXIWAY INTO TURF DUE PROXIMITY TO END OF TAXIWAY. PROP STRIKE TO PROP. MAINTENAN CE REPLACED HYDRAULIC PUMP. 2 L 7 2 4T RT A52EU 2002110100129 20021101 00129 EU 2002 11 1 MALA020589 1 20020929 A 2910 CONNECTOR SAAB SF340 SF340A 7850100 EU HYD SYSTEM LOOSE A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 106XJ 340A106 DURING FLIGHT 2991 FLIGHT CREW BLEW LANDING GEAR DOWN AFTER HYDRAULIC CAUTION LIGHT ILLUMINATED. EMERGENCY AND MAIN ACC INDICATED LOW. LOWERED GEAR HANDLE AND PULLED EMERGENCY EXTENSION HANDLE PER MEMORY ITEM. GEAR LOCKED IN DOWN POSITIO N OK. MAINTENANCE ADVISED TO PUT HYDRAULIC SWITCH IN OVRD POSITION, AND ALL ACC INDICATED IN GREEN. MAINTENANCE RESECU RED CANNON PLUG ON PRESSURE SWITCH 9ML. REPLACED LT AND RT SEPARATION BOLTS. FUNCTIONAL TEST OF EXTENSION AND RETRACTI ON SYSTEM TEST GOOD. 2 L 7 2 4T RT A52EU 2002110100130 20021101 00130 WP 2002 11 1 MWEA020608 1 20021008 A 5521 9918450504 SPAR CAP DOUG DC9 DC932 3022066 WP ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 RIGHT ELEVATOR SPAR CAP HAS A CRACK INDICATION APPROXIMATELY .75 LONGERON PROTRUDING FROM A FASTENER HOLE BETWEEN STATIO N XE 144.4 AND 156.4. FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2002110100131 20021101 00131 2002 11 1 MWEA020609 4 20021008 A 3454 INDICATOR DOUG DC9 DC932 3022066 WP COCKPIT OUT OF ADJUST A MWEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 207ME 47794 BOTH CAPTAINS AND FIRST OFFICERS HORIZONTAL DIRECTION GYRO INDICATORS 30 DEGREES OFF CORRECT HEADING. RESLAVED BOTH RAD IO MAGNETIC INDICATORS IAW MM 34-21-00. OPERATIONS CHECK GOOD. 2 L 7 2 4F A6WE 2002110100132 20021101 00132 WP 2002 11 1 MWEA020620 1 20021022 A 5230 49286651 STOP FITTING DOUG DC9 DC981 3022081 WP CARGO DOOR WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 FORWARD PIT DOOR, FORWARD AND AFT UPPER AND LOWER STOP PADS ARE WORN. FABRICATED NEW SHIMS INSTALLED DOOR STOPS & SHIMS , REMOVED FORWARD STOP, BLENDED OUT DAMAGE, FABRICATED 3 SHIMS AND REPAIR DOUBLER INSTALLED REPAIR PARTS AND INSTALLED L OWER DOOR STOP. 2 L 7 2 4F A6WE 2002110100133 20021101 00133 WP 2002 11 1 MWEA020626 1 20021022 A 5230 59101A1125 PAN DOUG DC9 DC981 3022081 WP CARGO DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 AFT CARGO DOOR FORWARD LOWER DOOR STOP HAS GOUGE AROUND STOP PAD IN PAN. REMOVED DOOR STOP, FABRICATED REPAIR DOUBLER, FABRICATED AND DRILLED SHIMS AND INSTALLED REPAIR DOUBLER AND SHIMS AND INSTALLED DOOR STOP. 2 L 7 2 4F A6WE 2002110100134 20021101 00134 NM 2002 11 1 2002F00942 1 20020930 A 5210 HANDLE BOEING 737 73783N 13844HI NM PAX DOOR OUT OF ADJUST G AMTA O OTHER J WARNING INDICATION LD LANDING 1 GL 11 321TZ 28249 ON TOUCH DOWN CAUTION LIGHT FOR FORWARD ENTRY DOOR ILLUMINATED. FLIGHT ATTENDANT MOVED HANDLE BACK TO THE CLOSED POSITIO N. PERFORMED FORWARD ENTRY DOOR ADJUSTMENT AND TEST PROCEDURES PER BOEING MAINTENANCE MANUAL 52-11-00-5. TURNED HORIZO NTAL CONTROL ROD END OUT 11/2 TURNS. CHECKED GOOD. 2 L 7 2 4F RT A16WE 2002110100135 20021101 00135 NM 2002 11 1 2002F00943 1 20021003 A 3350 20121 BATTERY BOEING 757 75723N 1384973 NM CABIN DISCHARGED G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 DURING SCHEDULED MAINTENANCE L2 EMERGENCY SLIDE LIGHT WAS INOPERATIVE WHEN CONDUCTING A FUNCTIONAL CHECK. MAINTENANCE RE MOVED AND REPLACED BATTERY CHARGER IN ACCORDANCE WITH M.M. 33-51-07. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2002110100136 20021101 00136 WP 2002 11 1 MWEA020629 1 20021025 A 5753 9958000163 ANGLE DOUG DC9 DC981 3022081 WP T/E FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 RIGHT OUTBOARD FLAP ATTACH RIB UPPER MILLED ANGLE HAS EXFOLIATION CORROSION AT XFLS 151 VIEWED THROUGH LIGHTENING HOLE. REMOVED MILLED ANGLE, FABRICATED AND DRILLED UP FLAP ANGLE AND INSTALLED FLAP ANGLE. 2 L 7 2 4F A6WE 2002110100137 20021101 00137 2002 11 1 2002F00944 4 20021002 A 3460 DISPLAY BOEING 757 75723N 1384973 NM COCKPIT FAILED G AMTA O OTHER O OTHER CR CRUISE 1 GL 11 517AT 27973 FLIGHT NUMBER 273. FIRST OFFICER'S FLIGHT DIRECTOR DOES NOT DISPLAY WHEN ENGAGED, C/B E35 POPPED. 2 L 7 2 4F RT A2NM 2002110100138 20021101 00138 WP 2002 11 1 MWEA020632 1 20021025 A 5753 59359157 BAR DOUG DC9 DC981 3022081 WP T/E FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 LEFT FLAP JOINT LOWER BAR HAS CORROSION ON COUNTERSINKS. REMOVED CORROSION, FABRICATED COUNTERSINK AND INSTALLED CONICA L WASHER. 2 L 7 2 4F A6WE 2002110100139 20021101 00139 NM 2002 11 1 2002F00945 1 20020914 A 5315 FLOORBEAM BOEING 757 75723N 1384973 NM FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 518AT 27974 DURING SCHEDULED INSPECTION CABIN FLOOR SUPPORT, E&E BAY FLOORBEAM AT STATION 358 ABOVE NOSE WHEEL WELL DOGHOUSE FOUND W ITH CORROSION AT FUSELAGE STATION 365 TO 365, WATERLINE 208 TO 208, BUTTLINE 48 RIGHT TO 48 RIGHT. MAINTENANCE REPAIRED AREA PER 757 S.R.M. 53-00-51-2. CORROSION WAS LEVEL 2. 2 L 7 2 4F RT A2NM 2002110100140 20021101 00140 NM 2002 11 1 2002F00946 1 20020925 A 5315 FLOORBEAM BOEING 757 75723N 1384973 NM FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 518AT 27974 DURING SCHEDULED INSPECTION CABIN FLOOR SUPPORT WAS DISCOVERED CORRODED ON FLOORBEAM FUSELAGE STATION 345, BUTTLINE 9 LE FT TO BUTTLINE 20 LEFT. CORROSION WAS LEVEL 2. MAINTENANCE REPAIRED CORROSION ON FLOOR BEAM IN ACCORDANCE WITH 757 S.R.M . 53-00-51-2. 2 L 7 2 4F RT A2NM 2002110100141 20021101 00141 NM 2002 11 1 2002F00961 1 20021020 A 3020 WARNING SYSTEM BOEING 757 75733N 1384931 NM RT ENG ANTI ICE ACTIVATED G AMTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 554TZ 32588 FLIGHT NUMBER 455. RIGHT ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED WITH SWITCH IN ON POSITION DURING DESCENT. 2 L 7 2 4F RT A2NM 2002110100143 20021101 00143 WP 2002 11 1 MWEA020643 1 20021025 A 3230 CONTROL CABLE DOUG DC9 DC932 3022066 WP LANDING GEAR OUT OF ADJUST A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 502ME 48132 CREW UNABLE TO RAISE LANDING GEAR. FOUND CABLE TENSION LOW AND ADJUSTED CABLE AND CONFIRMED PROPER RIG. 2 L 7 2 4F A6WE 2002110100144 20021101 00144 2002 11 1 2002F00962 4 20021019 A 3460 1074944 COMPUTER BOEING 757 75723N 1384973 NM RT PYLON INOPERATIVE G AMTA K NONE J WARNING INDICATION DE DESCENT 1 GL 11 519AT 27975 FLIGHT NUMBER 862. DURING DESCENT RIGHT ENGINE BLEED VALVE OFF IECAS & OVERHEAD LIGHTS ILLUMINATED. OCCURRED DURING IDLE DESCENT APPROX. 12,000 FEET. MAINTENANCE REMOVED AND REPLACED RFCC PER MM 36-11-18-4 REFERENCE FIM 36-10-00-1, FIG 113. 2 L 7 2 4F RT A2NM 2002110100145 20021101 00145 NM 2002 11 1 2002F00963 1 20021020 A 3020 7646B000 VALVE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE INOPERATIVE G AMTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 554TZ 405 405 32588 031817 FLIGHT NUMBER 455. RIGHT ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED WITH SWITCH IN ON POSITION DURING DESCENT. MAINTENANCE REMOVED AND REPLACED ENGINE INLET THERMAL ANTI-ICE VALVE IN ACCORDANCE WITH MM 30-21-03-4. OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E12EU 2002110100146 20021101 00146 NM 2002 11 1 2002F00964 1 20021014 A 2611 WARNING SYSTEM BOEING 757 75733N 1384931 NM RT ENG FIRE LOOP FALSE ACTIVATION G AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 550TZ 32584 FLIGHT NUMBER 717. DURING CRUISE STATUS MESSAGE R ENG FIRE LP 1 DISPLAYED. MAINTENANCE RERACKED AFOLTS CARDS PER FIM 26- 11-00, FIG 103, SHEET 4, BLOCK 111. NO FURTHER DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2002110100147 20021101 00147 NM 2002 11 1 2002F00965 1 20021014 A 2611 644501 CIRCUIT CARD BOEING 757 75733N 1384931 NM E&E BAY MALFUNCTIONED G AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 550TZ 32584 FLIGHT NUMBER 593. DURING CRUISE RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE INTERMITTANT ON/OFF THROUGHOUT FLIGHT. MAINTENA NCE REMOVED AND REPLACED RIGHT ENGINE LOOP NR 1 FIRE DET. CIRCUIT CARD PER MM 26-10-01. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002110100148 20021101 00148 NM 2002 11 1 2002F00966 1 20021017 A 2611 W5008000818 FIRE LOOP BOEING 757 75733N 1384931 NM RT ENGINE CHAFED G AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 550TZ 32584 DURING CRUISE RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE INTERMITTENT ON/OFF THROUGHOUT FLIGHT. MAINTENANCE TROUBLESHOT PER FIM 26-11-00, AND WDM'S 26-11-21 & 71-51-11, FOUND NR 3 FIRE DETECTOR WIRE W5008-0008-18 WITH SMALL CHAFE TO GROUND, RE PAIRED WIRE PER STD PRACTICES. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002110100149 20021101 00149 NM 2002 11 1 AMTA200201083 1 20020821 A 5312 BULKHEAD LKHEED 1011 1011 N/A-SDR NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 195AT 193C1041 FWD FUSELAGE SECTION, STA 328 PRESSURE BULKHEAD RBL 24 IN FESC 8 INCHES ABOVE SKIN FLOOR HAS EXFOLATION CORROSION ON BUL KHEAD AND PROTUDING ALONG AND UNDER STRAP. REPAIRED DAMAGE AREA PER ERA L10-53R-4922 REV IR. 2 L 7 3 4F RT A23WE 2002110100150 20021101 00150 NM 2002 11 1 AMTA200201228 1 20020926 A 5320 FLOOR SUPPORT LKHEED 1011 1011 N/A-SDR NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 195AT 193C1041 CABIN FLOOR SUPPORT, AT F.S. 1212 FOUND CANTED BULKHEAD SUPPORT WEB CRACKED 2 INCHES AT CORNER OF WEB, WEB LOCATED APPRO XIMATELY 2 FEET INBD. FROM RT SIDEWALL. REPAIRED DAMAGE AREA PER ERA L10-53R-4972, REV IR. 2 L 7 3 4F RT A23WE 2002110100151 20021101 00151 CE 2002 11 1 NSVA200200001 1 20021017 A 2810 91210E CHECK VALVE BEECH 1900 1900C 1154161 CE FUEL SYSTEM FAILED A NSVA H DEACTIVATE SYST/CIRCUITS O OTHER TX TAXI/GRND HDL 1 EA 27 207CJ UC107 BOS- AFTER TAXIING TO GATE THE LT ENGINE WOULD NOT SHUT DOWN. FIRE T-HANDLE WAS PULLED, NO EFFECT. THE ENGINE CONTINUE D TO RUN. MAINTENANCE VERIFIED THE FIREWALL SHUTOFF VALVE WAS CLOSED. THE MANUAL SHUTOFF VALVE WAS CLOSED AS WELL WITH NO ENGINE SHUT DOWN. TRANSFERRED FUEL OUT OF THE LT TANK AND THE ENGINE FLAMED OUT. MAINTENANCE FOUND THE MOTIVE FLOW CHECK VALVE WAS STUCK OPEN ALLOWING FUEL TO BE DRAWN FROM THE COLLECTOR TANK BYPASSING THE SHUTOFF VALVES. THE MOTIVE FLOW CHECK VALVE WAS REPLACED AND OPS CHECK WAS PERFORMED. DURING THE OPERATIONAL CHECK THE ENGINE WAS STARTED AND THE FIRE T-HANDLE WAS PULLED AND THE ENGINE SHUT DOWN WITHIN 10 SECONDS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2002110100152 20021101 00152 NM 2002 11 1 AMTA200201241 1 20020902 A 5320 LONGERON LKHEED 1011 1011 N/A-SDR NM AIR SCOOP CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 195AT 193C1041 FUSELAGE FORWARD SECTION, LT RAM AIR SCOOP UPPER LONGERON CRACKED AT RADIUS F.S 267 TO F.S 281 W.L 150, 4 INCHES IN LEN GTH. 2 L 7 3 4F RT A23WE 2002110100153 20021101 00153 NM 2002 11 1 AMTA200201286 1 20021010 A 5713 STRINGER LKHEED 1011 1011 N/A-SDR NM LT WING CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 195AT 193C1041 LT WING, LWR SKIN AT IWS 425.70 AND STR NR 3 HAS A CRACK EXTENDING FWD AND AFT OUT OF THE OUTBD FASTNER OF THE STRINGER, VERIFIED BY EDDY CURRENT. COMPLIED WITH ERA L10-57R-4909. CRACK LENGTH 2.0 INCHES 2 L 7 3 4F RT A23WE 2002110100154 20021101 00154 NM 2002 11 1 AASA0210240 1 20021014 A 5313 655966414 STRINGER BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED -C- CHECK FOUND STRINGER 26 RT AT BODY STATION 360-380 CORRODED. REMOVED, FABRICATED AND INSTALLED REP AIR IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110100155 20021101 00155 NM 2002 11 1 ASAA0210231 1 20021014 A 5754 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE NR 3 SLAT WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND SKIN ON NR3 SLAT ACTUATOR CUTOUT AT WING STATION 272-313 WORN. REPAIRED SLAT SKIN IAW S RM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110100156 20021101 00156 NM 2002 11 1 ASAA0210232 1 20021014 A 5320 69372542 BRACKET BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE RAM AIR PLENUM CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND RAM AIR PLENUM BRACKET AT BODY STATION 565, RIGHT BUTTOCK LINE 50 CRACKED. REMOVED AND REPLACED BRACKET IWA SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110100157 20021101 00157 NM 2002 11 1 ASAA0210234 1 20021014 A 5314 65621252 KEELBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND KEELBEAM AT BODY STATION 720-727, RIGHT BUTTOCK LINE 7 CHAFFED. REPAIRED KEEL BEAM IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110100158 20021101 00158 NM 2002 11 1 ASAA0210235 1 20021014 A 5311 6546532515 FRAME BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND FRAME AT STA 480, BUTTOCK LINE 0, CRACKED. FABRICATED REPAIR PARTS AND INSTALLED IAW EA . 2 L 7 2 4F 4 F RT A16WE E2EA 2002110100159 20021101 00159 NM 2002 11 1 ASAA0210236 1 20021014 A 5320 6935302501 ANGLE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND SPLICE ANGLE AT BODY STATION 540, STR 22L-23L CRACKED. REMOVED AND REPLACED SPLICE ANGL E IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110100160 20021101 00160 EA 2002 11 1 COMA0260620 1 20021031 A 5311 6003603031 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FS718 CRACKED A COMA K NONE C F.O.D. IN INSP/MAINT 1 SO 01 786CA 7750 7333 DOUBLER AT LEFT HAND FRAME STATION FS 718 BETWEEN STR 10 AND STR 12 IS CRACKED.PERFORMED MAJOR REPAIR BY RECOVERING DAMA GED DOUBLER AND INSTALLING NEW DOUBLE I/A/W REO 601R-53-61-193 REV 4. 2 L 7 2 4F RT A21EA 2002110100161 20021101 00161 NM 2002 11 1 ASAA0210237 1 20021014 A 5320 65621524 FITTING BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE INTERCOSTAL DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK FOUND INTERCOSTAL CHORD FITTING AT BODY STA 360-385, LEFT BUTTOCK LINE 9. LEFT BUTTOCK LINE 16 WITH AN ELONGATED HOLE. REMOVED AND REPLACED INTERCOSTAL CHORD FITTING IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110100162 20021101 00162 EU 2002 11 1 MALA020629 1 20021030 A 7600 7239060503 CTOT PANEL SAAB SF340 340B 7860101 EU A MALA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 15 443XJ 340B443 DURING DESCENT AND APPROACH OF FLIGHT #3154 INTO MSP, LEFT ENGINE WOULD SURGEWHEN THE POWER LEVER WAS MOVED IN THE RANG E OF 50% TO 35% TORQUE. OK ABOVE OR BELOW THIS RANGE-CTOT WAS SELECTED OFF. ALSO THE POWER LEVER IS ON THE 64 DEGREE M ARK WHEN THIS HAPPENED. MAINTENANCE CND PROBLEM, FOR TROUBLESHOOTING PURPOSES REMOVED CTOT PANEL PN 7239060-503, SN/OFF 229055, INSTALLED SERVICEABLE PANEL PN 7239060-503 SN/ON 845759, CTOT PANEL OPS CHECKS GOOD PER SAAB MM 71-00-00 TEST. NO TORQUE SURGES NOTED. 2 L 7 2 4T RT A52EU 2002110100163 20021101 00163 EA 2002 11 1 COMA0260621 1 20021031 A 5311 6003603024 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 786CA 7750 7333 THE R/H SIDE UPPER AND LOWER FUSELAGE FRAME FLANGES AND DOUBLER AT FS 718 ARE CRACKED BETWEEN STR 10 AND 12.PERFORMED A MAJOR REPAIR BY REMOVING DAMAGED FRAME FLANGES AND DOUBLER BETWEEN STR 10 AND 12 AND INSTALLING NEW FRAME FLANGES AND DO UBLER I/A/W REO 601R-53-61-193 REV 4. 2 L 7 2 4F RT A21EA 2002110100164 20021101 00164 EA 2002 11 1 COMA0260622 1 20021101 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 786CA 7333 THE L/H WING LOWER SKIN HAD MINOR CORROSION AT WS58 (FUEL PANEL ACCESS HOLE 540CB).THE MINOR CORROSION WAS REMOVED AND E DDY CURRENT WAS PERFORMED AND THE AREA WAS RESTORED TO FINISH I/A/W REO 601R-57-21-030 REV A. 2 L 7 2 4F RT A21EA 2002110100165 20021101 00165 EA 2002 11 1 COMA0260611 1 20021030 A 3010 ANTI-ICE SYSTEM CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J O WARNING INDICATION OTHER CR CRUISE 1 SO 01 933CA 7040 FLIGHT 5883 LEFT WING ANTI-ICE DUCT WARNING MESSAGE.COULD NOT DUPLICATE. INSPECTED ANTI-ICE SYSTEM - NO FAULTS FOUND. 2 L 7 2 4F RT A21EA 2002110100166 20021101 00166 NM 2002 11 1 PCAA0209109 1 20020922 A 1420 SPLICE DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A PCAA K NONE L NO TEST NR NOT REPORTED 1 EA 13 849EX 337 CREW REPORTED TWO FLOOR LEVEL EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPAIRED SPLICE AT ROW 4. OPERATIONAL CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002110100167 20021101 00167 NM 2002 11 1 PCAA0209110 1 20020921 A 5312 85310055 PRESSURE PANEL DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A PCAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 13 838EX 220 MHT-LGA FLIGHT 3535, CREW REPORTED THAT DURING FINAL APPROACH FOR LANDING, GEAR SELECTED DOWN BUT FAILED TO GET DOWN IND ICATION FOR NOSE GEAR. GO-AROUND INITIATED, AND CREW STARTED MANUAL GEAR EXTENSION WHEN LIGHT CAME ON INDICATING GEAR W AS DOWN. EMERGENCY DECLARED, FLIGHT LANDED WITH OUT INCIDENT. MAINTENANCE FOUND A CRACK IN NOSE DECK AREA / FLOOR WEB. CRACKED AREA WAS REPAIRED. GEAR RETRACTION/EXTENSION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002110100168 20021101 00168 NM 2002 11 1 PCAA0209112 1 20020925 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 DURING ROUTINE MAINTENANCE VISIT RIGHT FUSELAGE EMERGENCY EXIT LIGHTS FOUND INOPERATIVE. LIGHTS WERE RELAMPED AND FUSES REPLACED IN BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002110100169 20021101 00169 NM 2002 11 1 PCAA0209113 1 20020926 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 980HA 376 DURING ROUTINE MAINTENANCE VISIT FLOOR EMERGENCY LIGHT SEAT 1DF FOUND INOPERATIVE DUE TO A BROKEN WIRE. BROKEN WIRE WAS REPAIRED, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002110100170 20021101 00170 NM 2002 11 1 PCAA0209114 1 20020928 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST NR NOT REPORTED 1 EA 13 820EX 019 ABE-FLIGHT 3515, CREW REPORTED EMERGENCY LIGHTS INOPERATIVE FROM ROW 3 THROUGH 7 ON NR 1 SIDE. MAINTENANCE REPAIRED BRO KEN WIRE IN FLOOR EMERGENCY LIGHT SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002110100171 20021101 00171 NM 2002 11 1 PCAA0210119 1 20021006 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 806EX 263 DURING ROUTINE MAINTENANCE VISIT FORWARD EMERGENCY FLOOR LIGHTS HAD 4TH RED LIGHT INOPERATIVE. BROKEN WIRE WAS RESPLICE D. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002110100172 20021101 00172 NM 2002 11 1 PCAA0210120 1 20021005 A 3350 CONTROLLER DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A PCAA K NONE O OTHER AP APPROACH 1 EA 13 804EX 227 BTV-FLIGHT 3603, CREW REPORTED EMERGENCY LIGHTS FLICKERED ON AND OFF SEVERAL TIMES JUST BEFORE LANDING AND THEY WERE UNA BLE TO TURN EMERGENCY LIGHTS OFF. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES AND CONTROLLER. OPERATIONAL CHECK GOO D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002110100173 20021101 00173 NM 2002 11 1 PCAA0210122 1 20021015 A 5710 STRUCTURE DHAV DHC8 DHC8102 2809003 NM RT WING BIRD STRIKE A PCAA K NONE K FLUID LOSS DE DESCENT 1 EA 13 847EX 333 DCA-ALB FLIGHT 3927, CREW REPORTED THAT DURING DESCENT AIRCRAFT FLEW INTO A FLOCK OF BIRDS AND TOOK SEVERAL BIRD STRIKES ON ENTIRE AIRCRAFT RESULTING IN DAMAGE TO RIGHT WING WITH FUEL LEAKING OUT, AND HOLE IN TAIL SECTION AT BASE OF VERTICA L STABILIZER. MAINTENANCE IS CURRENTLY EVALUATING TOTAL DAMAGE INCURRED. 2 H 7 2 4T RT A13NM 2002110100174 20021101 00174 NM 2002 11 1 PCAA0210124 1 20021024 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 812EX 312 DURING ROUTINE MAINTENANCE VISIT 2 FORWARD EMERGENCY FLOOR PATH LIGHTS FOUND INOPERATIVE. BROKEN WIRE WAS REPAIRED BETW EEN 2ND AND 3RD FLOOR LIGHT ASSEMBLIES ON FLOOR TRACK. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002110100175 20021101 00175 NM 2002 11 1 PCAA0210126 1 20021024 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 846EX 326 DURING ROUTINE MAINTENANCE VISIT 5 LAMPS FOR EMERGENCY PATH FLOOR LIGHTS FOUND INOPERATIVE. WIRING WAS RESECURED. OPER ATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002110100176 20021101 00176 NM 2002 11 1 PCAA0210127 1 20021026 A 3350 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 831EX 160 DURING ROUTINE MAINTENANCE VISIT LEFT SIDE OF FUSELAGE AFT EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. EMERGENCY LIGHT POWER SUPPLY AND BATTERY WERE REPLACED. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002110100177 20021101 00177 NM 2002 11 1 PCAA0210129 1 20021029 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 826EX 389 DURING ROUTINE MAINTENANCE VISIT TWO EMERGENCY FLOOR LIGHTS FOUND TO BE INOPERATIVE. SOCKETS FOR LIGHTS WERE REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002110100178 20021101 00178 NM 2002 11 1 PCAA0210130 1 20021029 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN SHORTED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 805EX 228 DURING ROUTINE MAINTENANCE VISIT SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. ALL LIGHTS FOR POWER SUPPLY 335 1-P2 WERE FOUND INOPERATIVE. AFTER TROUBLESHOOTING IT WAS DISCOVERED THAT THE LIGHT ASSEMBLY FOR LAV OCCUPIED & FORWARD EMERGENCY EXIT SIGNS WERE SHORTED OUT INTERNALLY. SHORTED CIRCUIT WAS REPAIRED AND BULBS REPLACED. OPERATIONAL CHECK G OOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002110100179 20021101 00179 NM 2002 11 1 A6WA200230020 1 20020907 A 5712 RIB DORNER DO32 DO328100 2996000 NM RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 RIGHT LEADING EDGE 612CR HAS CRACKED RIB DAMAGE ON 1ST RIB FROM INBOARD AT UPPER SURFACE. MAINTENANCE REMOVED DAMAGED A REA FROM RIGHT WING LEADING EDGE 612CR RIB. FABRICATED REPAIR PARTS REF D0328 DRM 51-27-0 AND INSTALLED REF DO328 SRM 5 7-41-23 AND DER REPORT NR HHC-02-325. (M) 2 H 7 2 4T RT A45NM 2002110100180 20021101 00180 NM 2002 11 1 A6WA200230021 1 20020907 A 5320 CHANNEL DORNER DO32 DO328100 2996000 NM FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 FLOOR CHANNEL UNDER LAVATORY AT FRAME 35 CORRODED BEYOND LIMITS. MAINTENANCE REMOVED DAMAGED FLOOR CHANNEL AT FRAME 35. FABRICATED REPLACEMENT PARTS AND INSTALLED RED DO328 SRM 51-27-0 AND REPAIR PROCEDURE NR HHC-02-327. (M) 2 H 7 2 4T RT A45NM 2002110100181 20021101 00181 NM 2002 11 1 A6WA200230022 1 20020908 A 5320 FLOOR SUPPORT DORNER DO32 DO328100 2996000 NM FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 CENTER AISLE FLOOR SUPPORT BEAM AT FRAME 14 CRACKED .28 INCH AT CENTER SCREW HOLE. MAINTENANCE REMOVED DAMAGED AREA AT FRAME 14. FABRICATED REPAIR PARTS AND INSTALLED RED DO328 SRW 53-00-50 CHANNEL REPAIR. (M) 2 H 7 2 4T RT A45NM 2002110100182 20021101 00182 NM 2002 11 1 A6WA200230026 1 20020908 A 5320 FLOOR SUPPORT DORNER DO32 DO328100 2996000 NM FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 CENTER AISLE FLOR SUPPORT BEAM AT FRAME 20 CRACKED AT CENTER SCREW HOLE. MAINTENANCE REMOVED DAMAGED AREA AT FRAME 20. FABRICATED REPAIR PART AND INSTALLED REF DO328 SRM 53-00-50 CHANNEL REPAIR. (M) 2 H 7 2 4T RT A45NM 2002110100183 20021101 00183 NM 2002 11 1 ASAA0210238 1 20021014 A 5320 7075T6 SUPPORT BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK FOUND SIDEWALL SUPPORT PLATE AT BODY STR 787-787+10, STRINGER 26R CORRODED. REMOVED AND REPLAC ED SIDEWALL SUPPORT PLATE IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110100184 20021101 00184 NM 2002 11 1 ASAA0210239 1 20021014 A 5312 6546568524 BULKHEAD BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK FOUND AFT PRESSURE BULKHEAD WEB AT BODY STA 1042, RIGHT BUTTOCK LINE 2 CRACKED. REPAIRED AFT P RESSURE BULKHEAD WEB IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110100185 20021101 00185 NM 2002 11 1 ASAA0210241 1 20021014 A 5754 69392514 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE SLATS DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND NR 4 SLAT MAIN TRACK COVER AT SLAT STA 28, SLAT STA 31 DENTED. REPAIRED DENT TO ORIGINA L CONTOUR IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110100186 20021101 00186 NM 2002 11 1 ASAA0210242 1 20021014 A 5410 6552263353 ATTACH ANGLE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE NACELLE BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK FOUND NR 2 ENGINE OUTBOARD FIXED FAIRING ATTACH ANGLE AT NACELLE STATION 139 BROKEN. REMOVED, FABRICATED AND INSTALLED NEW ATTACH ANGLE PER SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110100187 20021101 00187 NM 2002 11 1 ASAA0240143 1 20021012 A 5311 6546560 SHEAR TIE BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING C CHECK, FOUND CORROSION ON SHEAR TIE AT BS 927 BETWEEN STR 26 RT AND 25 RT. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110100188 20021101 00188 NM 2002 11 1 ASAA0240144 1 20021012 A 5311 65C22910 SHEAR TIE BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 DURING C CHECK FOUND CORROSION ON FRAME SHEAR TIE AT BS 500D BETWEEN STR 27L AND 28L. REPAIRED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110200001 20021102 00001 SO 2002 11 2 C2XA02TY160 1 20021102 A 5100 14000492401 CHANNEL EMB 145 EMB145LR 3260212 SO GALLEY FLOOR STR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 TYS During a scheduled inspection the aft galley floor step-up channel was found to be corroded at frame 23. Maintena nce removed and replaced the channel IAW EMB-145 SRM 51-40-02, the repair was satisfactory. The aircraft will be releas ed upon completion of inspection. 2 L 7 2 4T RT T00011AT 2002110300001 20021103 00001 EU 2002 11 3 RAIA00211298 1 20021027 A 2434 51539019E GCU JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 560HK 7590 41076 5458-STL- RIGHT GENERATOR FELL OF LINE. MAINTENANCE REMOVED AND REPLACED RIGHT GENERATOR CONTROL UNIT, OPS CK OK. 2 L 7 2 4T RT A41NM 2002110300002 20021103 00002 SO 2002 11 3 RAIA00211299 1 20021030 A 3240 15622101 PRESSURE SWITCH EMB 145 EMB145 3260210 SO LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 802HK 145066 5284-RIC- SYSTEM #2 HYDRAULIC FAILURE. MAINTENANCE REMOVED AND REPLACED BRAKE PRESSURE SWITCH, OPS AND LK CK OK. 2 L 7 2 4F RT T00011AT 2002110300003 20021103 00003 EU 2002 11 3 RAIA00211300 1 20021031 A 2434 51539019E GCU JETAIR JETSTM JETSTM4101 1500501 EU INTERMITTENT A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 559HK 7591 41075 5497-STL- LEFT GENERATOR INTERMITTENT FAILURE. MAINTENANCE REMOVED AND REPLACED LEFT GENERATOR CONTROL UNIT, OPS CK OK. 2 L 7 2 4T RT A41NM 2003012900184 20030129 00184 NM 2003 1 29 ASAA0210187 1 20020923 A 5311 65465264 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT FUSELAGE BS 400, STRINGER 19R CORRODED. REMOVED CORROSION AND REPAIRED P ER SRM BY DRILLING OUT DAMAGE AND INSTALLING RIVET. (M 2 L 7 2 4F RT A16WE 2003012900185 20030129 00185 NM 2003 1 29 ASAA0210188 1 20020925 A 5311 6546534 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT FUSELAGE BS 520, RIGHT BUTTOCK LINE 6, RIGHT BUTTOCK LINE 14 CORRODED. REMOVED CORROSION AND REPAIRED PER SRM BY FABRICATING AND INSTALLING REPAIR PARTS. (M) 2 L 7 2 4F RT A16WE 2002110400001 20021104 00001 NM 2002 11 4 ASAA0210222 1 20021014 A 5320 6578983544 SUPPORT FITTING BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND FAIRING SUPPORT ANGLE BODY STATION 676, RIGHT BUTTOCK LINE 17, RIGHT BUTTOCK LINE 44, CO RRODED. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110400002 20021104 00002 NM 2002 11 4 ASAA0210223 1 20021014 A 5330 6545800594 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND SKIN PANEL AT BODY STATION 312-328, STRINGER 17L-18L GOUGED. INSTALLED DOUBLER AND TRIP LER IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110400003 20021104 00003 NM 2002 11 4 ASAA0210224 1 20021014 A 5754 6546422300A STRUCTURE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE NR 5 SLAT DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND NR5 SLAT AT WING STATION 227-329 DAMAGED. REMOVED AND REPLACED NR5 SLAT. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110400004 20021104 00004 NM 2002 11 4 ASAA0210225 1 20021014 A 5754 2024T3 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE NR 2 SLAT WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND LEADING EDGE SKIN AT NR 2 SLAT ACTUATOR CUTOUT AT WING STATION 409-447 WORN. REMOVED AN D REPLACED SKIN IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110400005 20021104 00005 NM 2002 11 4 ASAA0210226 1 20021014 A 5754 2024T3 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE NR 5 SLAT WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND LEADING EDGE SKIN AT NR 5 SLAT ACTUATOR AT WING STATION 399-462.5, WORN. REPAIRED SKIN IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110400006 20021104 00006 NM 2002 11 4 ASAA0210227 1 20021014 A 5320 657893546 ANGLE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FAIRING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND FAIRING ANGLES AT BODY STATION 688, RIGHT BUTTOCK LINE 6, RIGHT BUTTOCK LINE 8 DAMAGED. REMOVED AND REPLACED ANGLES IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110400007 20021104 00007 NM 2002 11 4 ASAA0210228 1 20021014 A 5241 6545871 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE GALLEY DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND R1 GALLEY DOOR SKIN CRACKED AT UPPER HINGE CUTOUT. REPAIRED CRACKS TO R1 DOOR IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110400008 20021104 00008 NM 2002 11 4 ASAA0210229 1 20021014 A 5712 69392809 RIB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND INBOARD RIB AT WING STATION 453, CORRODED. REMOVED AND REPLACED RIB IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110400009 20021104 00009 NM 2002 11 4 ASAA0210230 1 20021014 A 5712 693928109 RIB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND OUTBOARD RIB AT WING STATION 453, CORRODED. REMOVED AND REPLACED OUTBOARD RIB IWA SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110400010 20021104 00010 NM 2002 11 4 ASAA0210233 1 20021014 A 5220 50797897 LATCH BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE EMER EXIT HATCH OUT OF ADJUST A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 747AS 23124 DURING SCHEDULED C CHECK, FOUND LT OVERWING EMERGENCY EXIT HATCH HARD TO OPEN. ADJUSTED LT OVERWING EXIT DOOR IAW MM, T HEN DOOR OPERATED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110400011 20021104 00011 SO 2002 11 4 C2XA02CL200 1 20021007 A 2530 COFFEEMAKER EMB 135 EMB135LR 3260305 SO GALLEY ODOR A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 17513 145292 CLE FLIGHT NR 3180 THE CREW REPORTED THE LT COFFEE POT WAS SMOKING AND HAD A ELECTRICAL SMELL.MAINTENANCE INSPECTED AND PLACED ON MEL 25-60-02/3.SUPPLEMENT TO FOLLOW. 2 L 7 2 4F RT T00011AT 2002110400012 20021104 00012 SO 2002 11 4 C2XA02CL201 1 20021008 A 3397 CONNECTOR EMB 135 EMB135ER 3260203 SO CABIN LOOSE A C2XA O OTHER L NO TEST NR NOT REPORTED 1 SW 27 25504 145186 CLE FLIGHT NR 3337 THE CREW REPORTED PART OF EMERGENCY AISLE LIGHTING OPERATES INTERMITTENTLY. MAINTENANCE INSPECTED AN D RESECURED THE CONNECTOR PLUG ON THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002110400013 20021104 00013 SO 2002 11 4 C2XA02CL202 1 20021015 A 2120 ODOR EMB 145 EMB145 3260210 SO CABIN DETECTED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 22971 145149 ATL FLIGHT 3268 THE CREW REPORTED A BURNING ELECTRICAL SMELL IN THE COCKPIT AND GALLEY DURING TAXI. THE AIRCRAFT WAS RE LEASED IAW 21-26-00. MAINTENANCE INSPECTED AND PERFORMED ENGINE RUNS WITH BLEEDS AND PACKS ON. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002110400014 20021104 00014 SO 2002 11 4 C2XA02CL205 1 20021017 A 3222 STRUT EMB 145 EMB145LR 3260212 SO NLG DISCHARGED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 13538 145527 CLE FLIGHT 3105 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ALONG WITH ENGINE 1 AND 2 THRUST REVERSER DISAG REE MESSAGE. THE CREW DECLEARED A EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND SERVICED TH E NOSE STRUT SHOCK ABSORBER. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002110400015 20021104 00015 SO 2002 11 4 C2XA02CL206 1 20021017 A 2750 3631001007 FCU EMB 135 EMB135LR 3260305 SO TE FLAPS FAILED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 17524 145399 CLE FLIGHT 3228 THE CREW REPORTED A FLAP FAIL MESSAGE WHEN FLAPS SELECTED. THE CREW DECLEARED A EMERGENCY AND LANDED IN CLE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FLAP ELECTRONIC CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002110400016 20021104 00016 SO 2002 11 4 C2XA02CL207 1 20021018 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145ER 3260211 SO RT MLG INTERMITTENT A C2XA O OTHER P NO WARNING INDICATION LD LANDING 1 SW 27 15932 145015 CLE FLIGHT 3292 THE CREW REPORTED A BANGING NOISE IN THE LANDING GEAR WHEELWELL ON GEAR EXTENSION.THE AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RT MLG DOWNLOCK PROXIMITY SWITCHES. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002110400017 20021104 00017 SO 2002 11 4 C2XA02CL208 1 20021018 A 2751 WARNING SYSTEM EMB 145 EMB145 3260210 SO TE FLAPS MALFUNCTIONED A C2XA O OTHER N FALSE WARNING LD LANDING 1 SW 27 14972 145151 YYZ FLIGHT 4015 THE CREW REPORTED A LANDING GEAR AURAL WARNING MESSAGE ON LANDING. MAINTENANCE INSPECTED AND REPLACED T HE AURAL WARNING UNIT AND THE FLAP SLECTOR LEVER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002110400018 20021104 00018 SO 2002 11 4 C2XA02CL209 1 20021018 A 3320 7287502507 LIGHT EMB 145 EMB145 3260210 SO CABIN BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 27962 145110 EWR FLIGHT 3324 THE CREW REPORTED A BURNING ODOR COMING FROM THE CABIN LIGHTS AT ROW 4 AND 5. MAINTENANCE INSPECTED AND REPLACED THE CABIN SIDEWALL LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002110400019 20021104 00019 SO 2002 11 4 C2XA02CL210 1 20021027 A 3620 14542872401 SENSE LINE EMB 145 EMB145LR 3260212 SO NR 1 ENGINE BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13553 145585 CLE FLIGHT 3421 THE CREW REPORTED A NR 1 ENGINE BLEED LEAK WARNING MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED AND LAN DED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE BLEED DUCT PRESSURE SENSE LINE. OPERAT IONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002110400020 20021104 00020 SO 2002 11 4 C2XA02CL213 1 20021027 A 3350 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 25504 145186 CLE FLIGHT 3208 THE CREW REPORTED THE FORWARD EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND OPERATIO NAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE 2 L 7 2 4F RT T00011AT 2002110400021 20021104 00021 SO 2002 11 4 C2XA02CL214 1 20021029 A 2560 P2070005120 CHARGER EMB 135 EMB135ER 3260203 SO CABIN BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 27512 145274 CMH FLIGHT 3961 THE CREW REPORTED A BURNED PLASTIC ODOR COMING FROM THE REAR OF THE CABIN. THEY REPORTED THE ODOR SEEME D TO BE ASSOCIATED WITH THE APU AND THE NR 2 PACK.THE AIRCRAFT WAS RELEASED IAW MEL 21-51-00/1. MAINTENANCE INSPECTED A ND PERFORMED OPERATIONAL CHECKS OF THE APU AND NR 2 PACK. NO DEFECTS WERE FOUND. MAINTENANCE FOUND THE AFT EMERGENCY FLASHLIGHT CHARGER ASSEMBLY BURNED. THE CHARGER ASSEMBLY WAS REPLACED. 2 L 7 2 4F RT T00011AT 2002110400022 20021104 00022 SO 2002 11 4 C2XA02CL215 1 20021030 A 3350 66361 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12922 145338 CLE FLIGHT 2977 THE CREW REPORTED THE GALLEY EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED T HE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002110400023 20021104 00023 SO 2002 11 4 C2XA02IA207 1 20021002 A 7830 THRUST REVERSER EMB 145 EMB145 3260210 SO NR 1 ENGINE MALFUNCTIONED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 13970 145146 DAL- ENGINE NR 1 THRUST REVERSER DISAGREE ON TAKE-OFF ROLL. DAL- MAINTENANCE PLACED THE THRUST REVERSER ON MEL. MAIN TENANCE PERFORMED A OPERATIONAL CHECK OF THE THRUST REVERSER, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400024 20021104 00024 SO 2002 11 4 C2XA02IA208 1 20021002 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 13994 145291 IAH- APU FAIL IN FLIGHT. FUEL ODOR IN CABIN WITH APU RUNNING. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE APU, N O DEFECTS NOTED. PERFORMED A VISUAL INSPECTION OF THE FUEL LINES AT THE APU, NO LEAKS NOTED, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002110400025 20021104 00025 SO 2002 11 4 C2XA02IA209 1 20021002 A 3350 7287580501 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13956 145078 IAH- DURING PERFLIGHT THE CREW NOTED THAT THE LAST THREE FLOOR EMERGENCY PROX LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLOOR LIGHT STRIP, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400026 20021104 00026 SO 2002 11 4 C2XA02IA210 1 20021001 A 3230 355022022 CONTROL UNIT EMB 145 EMB145LR 3260212 SO MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13538 145527 THE CREW NOTED THAT THE LANDING GEAR WOULD NOT RETRACT,AND RETURNED TO IAH, AND LANDED WITHOUT INCIDENT. MAINTENANCE RE MOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFEC TS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002110400027 20021104 00027 SO 2002 11 4 C2XA02IA211 1 20021003 A 3350 7287577503 SIGN EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT SIGN ON THE CEILING ADJACENT TO THE GALLEY FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEF ECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400028 20021104 00028 EU 2002 11 4 C2XA02IA212 1 20021003 A 3234 F96GA0102 SELECTOR AEROSP ATR42 ATR42320 8680930 EU MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 14819 156 FLIGHT 3752, THE CREW NOTED THAT ALL THREE GEAR DID NOT RETRACT. LT & RT MLG BANGING AGAINST UPLOCKS. MAINTENANCE INSP ECTED THE LANDING GEAR, INSTALLED THE LANDING GEAR PINS, AND RELEASED THE AIRCRAFT IAW MEL. THE AIRCRAFT FLEW FROM EFD T O IAH ON 10/04/2002. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR, PERFORMED A OPERATIONAL CHECK OF THE L ANDING GEAR SYSTEM, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002110400029 20021104 00029 SO 2002 11 4 C2XA02IA213 1 20021004 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO RT MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16951 145063 FLIGHT 3850, THE CREW NOTED DURING CLIMB THAT THE LANDING GEAR WOULDN'T RETRACT,RETURNED TO IAH, AND LANDED WITHOUT INCI DENT. MAINTENANCE REMOVED AND REPLACED THE RT SHOCK ABSORBER PROXIMITY SWITCH, PERFORMED A OPERATIONAL CHECK, NO DEFECT S NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002110400030 20021104 00030 SO 2002 11 4 C2XA02IA214 1 20021004 A 4930 TANK EMB 145 EMB145LR 3260212 SO EPA OVERFLOW ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13994 145291 IAH- THE CREW NOTED A STRONG ODOR OF FUEL AFTER TAKEOFF. THE ODOR OF FUEL WENT AWAY AFTER APU SHUT DOWN. MAINTENANCE DRAINED FUEL FROM THE EPA TANK, GROUND RAN APU, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002110400031 20021104 00031 SO 2002 11 4 C2XA02IA216 1 20021008 A 3350 375901 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 DURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY OVERHEAD LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPL ACED THE EMERGENCY EXIT LIGHT ASSEMBLY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTE D, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400032 20021104 00032 SO 2002 11 4 C2XA02IA217 1 20021008 A 3350 823010 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 DURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY OVERHEAD LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPL ACED THE EMERGENCY LIGHT ASSEMBLY, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400033 20021104 00033 SO 2002 11 4 C2XA02IA219 1 20021009 A 3260 23092900001 UPLOCK EMB 145 EMB145ER 3260211 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14940 145033 THE CREW NOTED THAT THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK BOX, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400034 20021104 00034 SO 2002 11 4 C2XA02IA221 1 20021011 A 3230 355022002 ECU EMB 145 EMB145 3260210 SO MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14974 145161 THE CREW NOTED THAT THE LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO AGU, AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED FROM AGU TO IAH FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE LGEU, PERFORMED A OPERATION AL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400035 20021104 00035 SO 2002 11 4 C2XA02IA223 1 20021010 A 5520 14523410001 BEARING EMB 145 EMB145LR 3260212 SO ELEVATOR LOOSE A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 27 13997 145298 THE CREW NOTED THAT THERE WAS A VIBRATION IN THE CONTROL YOKE. VIBRATION BEGAN IN THE LOW 30,000'S AND CONTINUED IN C LIMB TO 35,000. VIBRATION SEEMED MORE PRONOUNCED AS AIRCRAFT ACCELERATED, VIBRATION DECREASED MARKABLY BELOW 30,000 FT, COULD ALSO FEEL VIBRATION ON FLOOR. A/C RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ELEVAT OR HINGE POINTS AND FOUND THAT LT ELEVATOR BEARING TIP TORQUE TUBE HOUSING LOOSE. MAINTENANCE REMOVED AND REPLACED LT ELEVATOR TORQUE TUBE TIP BEARING HOUSING, PERFORMED ELEVATOR DEFLECTION CHECKS, NO DEFECTS NOTED AND AIRCRAFT WAS RELEA SED FOR TEST FLIGHT PURPOSES ONLY. TEST FLIGHT WAS SATISFACTORY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002110400036 20021104 00036 GL 2002 11 4 C2XA02IA225 2 20021022 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 FAILED A C2XA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 SW 27 15910 3135 145455 CAE311839 FLIGHT 3789, CREW NOTED THAT NR 1 ENGINE HAD UNCOMMANDED SHUTDOWN AT FL 280. ENGINE NR 1 AIR RESTART FAILED. THE CREW DECLAIRED EMERGENCY AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE, PERFORMED A O PERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110400037 20021104 00037 EU 2002 11 4 C2XA02IA227 1 20021026 A 3260 842503A PSEU AEROSP ATR42 ATR42320 8680930 EU MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 99838 259 CREW NOTED WITH MLG UP AND LOCKED, RT GEAR SYSTEM NR 2 GREEN LIGHT STAYS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE PSEU, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002110400038 20021104 00038 SO 2002 11 4 C2XA02IA228 1 20021026 A 2751 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO TE FLAPS ACTIVATED A C2XA B EMER. DESCENT N FALSE WARNING AP APPROACH 1 SW 27 18557 145596 FLIGHT 3277, ON APPROACH CREW NOTED THAT THE FLAP FAIL MESSAGE APPEARED ON THE EICAS. THE CREW DECLAIRED EMERGENCY, PER FORMED EMERGENCY DESCENT, AND, LANDED WITH NO FLAPS WITHOUT INCIDENT. MAINTENANCE RESET THE FLAP SYSTEM, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002110400039 20021104 00039 EU 2002 11 4 C2XA02IA229 1 20021026 A 3150 350A23008314 COMPUTER AEROSP ATR42 ATR42320 8680930 EU COCKPIT MALFUNCTIONED A C2XA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 27 16824 166 FLIGHT 3752, ON TAKEOFF THE CREW NOTED A/S OVERSPEED WARNING AND ABORTED TAKEOFF WITHOUT INCIEDNT. MAINTENANCE REMOVED AND REPLACED THE CREW ALERTING COMPUTER, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002110400040 20021104 00040 2002 11 4 C2XA02IA230 4 20021026 A 3417 7000700959 ADC AEROSP ATR42 ATR42320 8680930 EU COCKPIT MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16824 166 FLIGHT 3752, AFTER TAKEOFF THE CREW NOTED A/S OVERSPEED WARNING ON DEPARTURE, AIR RETURN TO IAH AND LANDED WITHOUT INCI DENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR DATA COMPUTER, PERFORMED A OPERATIONAL CHECK, AND, A LEAK RATE CHEC K, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 2002110400041 20021104 00041 SO 2002 11 4 C2XA02IA231 1 20021025 A 3350 66368 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15983 145239 DURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHT STRIP ON FLOOR PANELS 251FF & 261BF FAILED TO ILLUMINATE. MAI NTENANCE REMOVED AND REPLACED THE LIGHT STRIPS ON PANELS 251FF & 261BF, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY L IGHTING SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002110400042 20021104 00042 SO 2002 11 4 C2XA02IA232 1 20021029 A 3260 23092900001 UPLOCK EMB 145 EMB145ER 3260211 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 12946 145052 FLIGHT 3075, THE CREW NOTED THAT THE NOSE WHEEL WOULD NOT RETRACT, AIR RETURN TO IAH AND LANDED WITHOUT INCIDENT. MAINT ENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK BOX, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400043 20021104 00043 SO 2002 11 4 C2XA02SH072 1 20021004 A 5315 14521713005 FLOORBEAM EMB 145 EMB145ER 3260211 SO GALLEY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 SHV- DURING C CHECK THE CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION AT GALLEY MOUNT HOLES BETWEEN FRAMES 18 AND 23. MA INTENANCE REMOVED AND REPLACED CENTER FLOORBEAM BETWEEN FRAMES 18 AND 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APP ROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400044 20021104 00044 SO 2002 11 4 C2XA02SH076 1 20021004 A 5315 14521713005 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 DURING C CHECK INSPECTION NUTPLATE WAS FOUND CORRODED ON CENTER FLOORBEAM AT FRAME 18. MAINTENANCE REMOVED AND REPLACED FLOORBEAM BETWEEN FRAMES 16 AND 24 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN SERVICE. 2 L 7 2 4F RT T00011AT 2002110400045 20021104 00045 SO 2002 11 4 C2XA02SH078 1 20021004 A 5315 14521713005 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 SHV-DURING C CHECK INSPECTION NUTPLATE WAS FOUND WITH CORROSION ON CENTER FLOORBEAM AT FRAME 22. MAINTENANCE REMOVED DA MAGE AND REPLACED FLOORBEAM BETWEEN FRAMES 16 AND 24 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVI CE. 2 L 7 2 4F RT T00011AT 2002110400046 20021104 00046 SO 2002 11 4 C2XA02SH083 1 20021004 A 5510 12060867009 BUSHING EMB 145 EMB145ER 3260211 SO RUDDER DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 DURING C CHECK, ALL HAT BUSHINGS ON THE RUDDER ATTACHING BRACKETS WERE FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED ALL HAT BUSHINGS ON RUDDEDR ATTACHING BRACKETS IAW EMB AMM 20-10-08. THE AURCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400047 20021104 00047 SO 2002 11 4 C2XA02SH091 1 20021006 A 5315 14522226003 FLOORBEAM EMB 145 EMB145ER 3260211 SO CARGO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 SHV- DURING C CHECK INSPECTION CENTER FLOORBEAM BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO HAVE CORROSION ON NUTPL ATES AND NUTPLATES HOLES. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400048 20021104 00048 SO 2002 11 4 C2XA02SH092 1 20021011 A 5753 14566219401 FLAP TRACK EMB 145 EMB145ER 3260211 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 DURING C CHECK INSPECTION, RT HAND OUTBOARD FLAP CENTER TRACK WAS FOUND TO HAVE A CRACK DUE TO LIGHTING STRIKE. MAINTE NANCE REPAIRED DAMAGE IAW CONTINENTAL EXPRESS EC 5750-01185. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400049 20021104 00049 SO 2002 11 4 C2XA02SH093 1 20021009 A 5315 14522459003 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 DURING C CHECK INSPECTION, CORROSION WAS FOUND AT CENTER FLOORBEAM SUPPORT RAMP BETWEEN FRAMES 18 AND 20. MAINTENANCE R EMOVED DAMAGED SECTION, PERFORMED AN ANGLE REPAIR, AND REPLACED AFFECTED SUPPORT RAMP IAW EMB 145 SRM 51-40-02. THE A IRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400050 20021104 00050 SO 2002 11 4 C2XA02SH097 1 20021012 A 5410 14576512011 RIB EMB 145 EMB145ER 3260211 SO NR2 ENG NACELLE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 DURING C CHECK, NR 2 ENGINE NACELLE WAS FOUND TO HAVE A GOUGE ON THIRD RIB PLATE FROM THE END. MAINTENANCE REMOVED DAM AGE AND REPAIRED RIB PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400051 20021104 00051 SO 2002 11 4 C2XA02SH098 1 20021013 A 5315 14521713005 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 SHV- DURING C CHECK THE CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAITENANCE REMOVED AND REPLACED AFFEC TED FLOORBEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400052 20021104 00052 SO 2002 11 4 C2XA02SH100 1 20021017 A 5310 14522460011 BUTT STRAP EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 DURING C CHECK, BUTT STRAP RT OF CENTER FLOORBEAM AT FRAME 18 WAS FOUND TO HAVE CORROSION ANROUND NUTPLATE HOLES. MAIN TENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-0179. THE AIRCRAFT WAS APPROVED T O RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400053 20021104 00053 SO 2002 11 4 C2XA02SH101 1 20021017 A 5315 14522461003 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 SHV- DURING C CHECK, LT FLOORBEAM AT FRAME 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED A D OUBLER REPAIR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400054 20021104 00054 NM 2002 11 4 A6WA200230030 1 20020919 A 5230 DOOR FRAME DORNER DO32 DO328100 2996000 NM CARGO DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 328MX 3071 BOTTOM OF CARGO DOOR FRAME UNDER THRESHOLD PLATE HAS CORROSION. MAINTENANCE REMOVED AND BLENDED CORROSION ON UPPER SURF ACE OF CARGO DOOR FRAME THRESHOLD (DOORSILL). FABRICATED AND INSTALLED REPAIR DOUBLER REF REPAIR PROCEDURE HHC-02-358. (M) 2 H 7 2 4T RT A45NM 2002110400055 20021104 00055 NM 2002 11 4 A6WA200230031 1 20020920 A 5320 FLOOR SUPPORT DORNER DO32 DO328100 2996000 NM FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 328MX 3071 WHILE CLEANING CORROSION FROM TWO CLIP NUT ATTACHED HOLES ON FRAME 38 FOUND TWO HOLES IN FLOOR SUPPORT ANGLE TO BE CRACK ED. MAINTENANCE STOP DRILLED CRACKS AT FRAME 38. FABRICATED AND INSTALLED REPAIR DOUBLER REF HHC-02-349. REPAIR PROCE DURE AND SRM DO328 SRM 51-00-01. (M) 2 H 7 2 4T RT A45NM 2002110400056 20021104 00056 NM 2002 11 4 A6WA200230032 1 20020920 A 5315 FLOORBEAM DORNER DO32 DO328100 2996000 NM FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 328MX 3071 LAVATORY AREA FRAME 35 CORRODED BEYOND LIMITS. MAINTENANCE REMOVED FLOOR FRAME 35 AT LAVATORY AREA. FABRICATED REPLACE MENT FRAME AND INSTALLED REF HHC-02-348 REPAIR PROCEDURE AND DO328 SRM 51-10-01. (M) 2 H 7 2 4T RT A45NM 2002110400057 20021104 00057 NM 2002 11 4 A6WA200230033 1 20020920 A 5320 CHANNEL DORNER DO32 DO328100 2996000 NM FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 328MX 3071 CENTER AISLE FLOOR CHANNEL CRACKED .25 INCH AT CENTER SCREW LOCATION ON FRAME 18. MAINTENANCE REMOVED DAMAGED AREA FABR ICATED REPAIR PARTS AND INSTALLED REF DO328 SRM 53-00-50 AT FRAME 18. (M) 2 H 7 2 4T RT A45NM 2002110400058 20021104 00058 NM 2002 11 4 A6WA200230035 1 20020920 A 5315 FLOORBEAM DORNER DO32 DO328100 2996000 NM FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 328MX 3071 FLOOR BOARD SCREW HOLE ON FRAME 14 CRACKED AT CENTER AISLE 4H SIDE. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED REPAI R PARTS AND INSTALLED RED DO328 SRM 53-00-50 AT FRAME 14. (M) 2 H 7 2 4T RT A45NM 2002110400059 20021104 00059 EU 2002 11 4 AALA20020850 1 20020611 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A K NONE O OTHER IN INSP/MAINT 1 SW 21 7055A 462 FOUND EMERGENCY LIGHT ASSEMBLY IN SEAT 2G IS BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL O PERATION. (M) 2 L 7 2 4F RT A35EU 2002110400060 20021104 00060 EU 2002 11 4 AALA20020851 1 20020613 A 3350 CHARGER AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70079 619 MIA - FOUND L2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND CHARGER. SYSTEM GROUND CHECKED NORMAL OPERA TION. (M) 2 L 7 2 4F RT A35EU 2002110400061 20021104 00061 EU 2002 11 4 AALA20020873 1 20020610 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70074 517 JFK - FOUND SEAT 19C EMERGENCY LIGHT INOPERATIVE. SECURED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002110400062 20021104 00062 EU 2002 11 4 AALA20020917 1 20020618 A 3350 SWITCH AIRBUS 300 A300B4605R 3930308 EU CABIN INTERMITTENT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 MIA - TOILET EMERGENCY LIGHT CIRCUIT BREAKER POPPED. TROUBLESHOT FAULT TO AN EMERGENCY LIGHT SWITCH INTERMITTENT FAULT. REPLACED SWITCH ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002110400063 20021104 00063 EU 2002 11 4 AALA20020930 1 20020625 A 3350 321441 CHARGER AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33069 512 JFK - L2 DOOR EXIT SIGN FAILS TEST. REPLACED BATTERY AND CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002110400064 20021104 00064 EU 2002 11 4 AALA20021111 1 20020729 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1404D 11355 ORD - DURING OVERNIGHT MAINTENANCE, FLOOR BOARD EMERGENCY EXIT LIGHT AT SEAT 11D INOPERATIVE. REPAIRED FLOOR BOARD EMER GENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002110400065 20021104 00065 EU 2002 11 4 AALA20021125 1 20020801 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 JFK - FOUND EMERGENCY LIGHT AT 15G INOPERATIVE. SECURED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002110400066 20021104 00066 EU 2002 11 4 AALA20021132 1 20020807 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7062A 474 MIA - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SEAT 35G INOPERATIVE. REPOSITIONED AND SECURED CONNECTOR FOR EMERGENCY PATH LIGHTING AT SEAT 35C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002110400067 20021104 00067 NM 2002 11 4 AALA20021198 1 20020820 A 2750 285N001140 ECU BOEING 757 757223 1384957 NM E/E BAY FAILED A AALA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 21 675AN 29425 MIA - FLT 1736 - EN ROUTE SJU-MIA - INBOUND TO MIA, TRAILING EDGE FLAPS STUCK AT 20 DEGREES. LANDED AT MIA WITHOUT INCI DENT. REPLACED NR 1 FLAT/SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002110400068 20021104 00068 EU 2002 11 4 AALA20021210 1 20020822 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14056 463 MIA - FOUND EMERGENCY LIGHT AT 35G INOPERATIVE. RESECURED ATTACHING CONNECTOR AT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002110400069 20021104 00069 EU 2002 11 4 AALA20021256 1 20020901 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14061 471 MIA - FOUND EMERGENCY LIGHT AT SEAT 28G INOPERATIVE. SECURED CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002110400070 20021104 00070 EU 2002 11 4 AALA20021258 1 20020902 A 2910 HYDRAULIC LINE FOKKER F28 F28MK0100 4990807 EU RT MLG LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 1453D 11465 ORD - FLT 1451 - RIGHT MAIN LANDING UNSAFE MESSAGE ON MFDU. USED ALTERNATE GEAR EXTENSION. LANDED ORD WITHOUT INCIDENT . REPLACED RIGHT UPLOCK ACTUATOR LINE. JACKED AND CYCLED GEAR, NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATIO N. (M) 2 L 7 2 4F RT 2002110400071 20021104 00071 NM 2002 11 4 AALA20021289 1 20020824 A 5320 FITTING BOEING 757 757223 1384957 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AM 24605 TUL - FOUND AFT INBOARD FITTING CRACKED AT STATION 205.65 BEYOND LIMITS. FABRICATED AND INSTALLED BUSHING PER ESO 90309 . (M) 2 L 7 2 4F RT A2NM 2002110400072 20021104 00072 NM 2002 11 4 AALA20021296 1 20020904 A 2421 GEN3014 IDG BOEING 777 777223 1385213 NM RT ENGINE FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 797AN 30012 GRU - ON TAKEOFF AFTER FLAP RETRACTION, GOT ELEC GEN OFF R EICAS MESSAGE. RIGHT ENGINE GENERATOR PLACARDED INOPERATIVE AS PER MEL, MPM 24-3 ACCOMPLISHED, SERVICED BOTH IDG/S OIL LEVEL AS WELL APU, PLACARDED AND MIC ENTERED. ENGINES FAN CO WLS CLOSED LATCHED OK FOR SERVICE. REMOVED AND REPLACED RIGHT IDG PER MM OPS AND LEAK CHECKS NORMAL. PERFORMED TEST PE R MM ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4F RT T00001SE 2002120200026 20021202 00026 NM 2002 12 2 920WA0006 1 20021101 A 2750 654648186 SPINDLE BOEING 737 737236 1384476 NM RT TE FLAP BROKEN A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 920WA 21791 RT FLAP ASSEMBLY BROKEN. FOUND NR 8 FLAP CARRIAGE SPINDLE BROKEN. REPLACED NR 8 CARRIAGE ASSY. PER MM275181 & RIGGED P ER MM27-51-72. 2 L 7 2 4F RT A16WE 2002110400073 20021104 00073 EU 2002 11 4 AALA20021297 1 20020910 A 3210 DAM5686 DAMPER AIRBUS 300 A300B4605R 3930308 EU LT MLG FAILED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 70079 619 MIA - FLT 776 - EN ROUT MIA-EWR - LEFT MAIN LANDING GEAR WOULD NOT RETRACT. RETURNED TO MIA LANDED WITHOUT INCIDENT. R EPLACED PITCH DAMPER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002110400074 20021104 00074 NM 2002 11 4 AALA20021301 1 20020915 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 756AM 30264 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT ASSEMBLY AT 1L ENTRY COAT CLOSET BROKEN. REPLACED EMERGENCY LIGHT A SSEMBLY AT 1L ENTRY COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002110400075 20021104 00075 NM 2002 11 4 AALA20021308 1 20020918 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 351AA 24032 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 2H CUBICLE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 2H CUBICLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002110400076 20021104 00076 NM 2002 11 4 AALA20021332 1 20020922 A 2530 OVE9027 OVEN BOEING 757 757223 1384957 NM GALLEY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 692AA 26972 LAX - ON CLIMB-OUT FROM LAX FLIGHT ATTENDANTS REPORTED A BURNING SMELL IN THE FORWARD GALLEY SMOKE WAS THEN REPORTED RET URNED TO LAX. FOUND BAKED ON DEBRIS IN FORWARD OVEN. DEBRIS REMOVED AND OVEN CLEANED BY CABIN SERVICE. (M) 2 L 7 2 4F RT A2NM 2002110400077 20021104 00077 NM 2002 11 4 AALA20021334 1 20020921 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 388AA 27448 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22B INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002110400078 20021104 00078 NM 2002 11 4 AALA20021355 1 20020925 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 352AA 24033 ORD - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS AT SEAT 29 A/B INOPERATIVE. REPLACED WALL CONNECTOR AT SEAT 29 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002110400079 20021104 00079 EU 2002 11 4 AALA2021297 1 20020910 A 3210 DAM5686 DAMPER AIRBUS 300 A300B4605R 3930308 EU LT MLG FAILED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 70079 619 MIA - FLT 776 - EN ROUTE MIA-EWR LEFT MAIN LANDING GEAR WOULD NOT RETRACT. RETURNED TO MIA LANDED WITHOUT INCIDENT. RE PLACED PITCH DAMPER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002110400080 20021104 00080 WP 2002 11 4 MWEA020668 1 20021031 A 3230 RING DOUG DC9 DC914 3022034 WP LANDING GEAR BROKEN A MWEA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 31 700ME 45696 LANDING GEAR HANDLE WOULD NOT RETRACT. -- FOUND NOSE LANDING GEAR PISTON INNER RING BROKEN AND DAMAGED SEVERAL PARTS. REPLACED #74 RING, #75 SPACER, #77 VALVE, #80 RETAINER AND #82 STOP. 2 L 7 2 4F A6WE 2002110400081 20021104 00081 SO 2002 11 4 C2XA02SH102 1 20021017 A 5350 12015565502 FAIRING EMB 145 EMB145ER 3260211 SO APU INLET CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 SHV- DURING C CHECK, RT FAIRING ON APU FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED RT FAIRING IAW CONTINENTAL EXPR ESS EC 5350-01032. THE AIRCRAFT WAS APROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400082 20021104 00082 SO 2002 11 4 C2XA02SH103 1 20021017 A 5315 14522459003 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 SHV-DURING C CHECK SUPPORT RAMP ON CENTER FLOORBEAM BETWEEN FRAME 18 AND FRAME 20 WAS FOUND WITH CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED SUPPORT RAMP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400083 20021104 00083 SO 2002 11 4 C2XA02SH104 1 20021017 A 5315 14521718003 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 SHV- DURING C CHECK LT FLOORBEAM FOWARD OF FRAME 20 WAS FOUND WITH CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110400084 20021104 00084 SO 2002 11 4 SIMA200216003 1 20020609 A 5200 STRUCTURE EMB 145 EMB145LR 3260212 SO PAX DOOR GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 ABI - PASSENGER DOOR FORWARD LOWER EDGE IS GOUGED. PERFORMED EDDY CURRENT INSPECTION, NO DEFECTS. GOUGE ACCEPTED AS IS IAW EMB GST-1895/02. (M) 2 L 7 2 4T RT T00011AT 2002110400085 20021104 00085 NM 2002 11 4 USAA020364 1 20020919 A 5542 55C2584151 SKIN BOEING 737 737301 1384611 NM RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 23228 PIT - FOUND RUDDER DELAMINATED, LEFT SIDE, BOTTOM EDGE 19 INCHES AFT OF LEADING EDGE. RESIN AND OVERLAYED WITH TWO PLIE S OF GRAPHITE FABRIC PER EA 74841, SRM 55-40-01, 51-70-17. (M) 2 L 7 2 4F RT A16WE 2002110400086 20021104 00086 NM 2002 11 4 USAA020365 1 20020920 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND FRAME CRACKED 1 INCH, STATION 616 RIGHT SIDE, FRAME LOWER INBOARD END CABIN FLOOR. INSTALLED DOUBLER ANGLE PER TYPICAL REPAIR 53-61-01 AND EA 74256. (M) 2 L 7 2 4F RT A16WE 2002110400087 20021104 00087 NM 2002 11 4 USAA020370 1 20020926 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 46535 23930 PIT - FOUND SKIN WITH TWO CRACKED .25 INCH LONG, STATION 380 BODYLINE 0 AT RIVET FASTENER. INSTALLED DOUBLER, ROUTED OU T CRACK PER TYPICAL REPAIR 53-30-07 AND EA 74918. (M) 2 L 7 2 4F RT A16WE 2002110400088 20021104 00088 NM 2002 11 4 USAA020371 1 20020925 A 7120 310A10221 MOUNT BOEING 737 737301 1384611 NM ENGINE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 11060 23228 PIT - FOUND ENGINE MOUNT CROSSBEAM WORN LUG, LUG BORE ON ENGINE MOUNT. MACHINE INSIDE DIAMETER OF LUG BORE TO OVERSIZE BEARING PER TYPICAL REPAIR 550-19 REV B. (M) 2 L 7 2 4F RT A16WE 2002110400089 20021104 00089 NM 2002 11 4 USAA020372 1 20020928 A 5414 SKIN BOEING 737 737301 1384611 NM LT PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 350US 43450 23553 PIT - FOUND PYLON BONDED SKIN CRACKED 1.687, LEFT ENGINE PYLON STATION 196, PANEL NR 572 LEFT OPENING. REPAIRED PER TYP ICAL REPAIR 54-30-07. (M) 2 L 7 2 4F RT A16WE 2002110400090 20021104 00090 NM 2002 11 4 USAA020373 1 20020929 A 5512 SKIN BOEING 737 737401 1384701 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 39339 23986 PIT - FOUND HORIZ SKIN CRACKED 1.5 INCH, BETWEEN RIB STATION 120 AND 129, LEFT HORIZ SKIN. CUT OUT DAMAGE, INSTALLED EX TERNAL DOUBLER PER TYPICAL REPAIR 55-10-07 REV B. (M) 2 L 7 2 4F RT A16WE 2002110400091 20021104 00091 NM 2002 11 4 CALA0200521 1 20021102 A 5300 6551639237 RING BOEING 737 737524 1384721 NM A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 14660 28921 LH WHEEL WELL FAIRING SUPPORT RING HAS 16" CRACK. REMOVED AND REPLACED FAIRING RING IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002110400092 20021104 00092 NM 2002 11 4 CALA0200522 1 20021102 A 5200 SEAL BOEING 757 757224 1384958 NM A CALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 13113 27555 NOISE FROM L1 DOOR. INSTALLED SEAL IN TRACK TOP FORWARD DOOR 2 L 7 2 4F RT A2NM 2002110400093 20021104 00093 NM 2002 11 4 CALA0200523 1 20021103 A 5300 65528945 SUPPORT BOEING 737 7373T0 1384582 NM A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 14336 23574 FLOOR SUPPORT IB FWD CRACKED AT STA 540 LH ID TRACK. REPLACED FLOOR SUPPORT IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002110400094 20021104 00094 NM 2002 11 4 CALA0200524 1 20021104 A 2612 25261690001 FIRE WARNING BOEING 777 777224 1385225 NM CARGO BAY MALFUNCTIONED A CALA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 09 78005 27581 AFT CARGO FIRE LIGHT CAME ON. FOUND NO EVIDENCE OF FIRE. FOUND DOOR NR 4 CHILLER CIRCUIT BREAKERS POPPED 2 L 7 2 4F RT T00001SE 2002110400095 20021104 00095 NM 2002 11 4 CALA0200526 1 20021103 A 2800 2820095101 VALVE BOEING 737 7373T0 1384582 NM A CALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 14324 23375 FUEL TRANSFER AND LOSS FOM AFT AUX AND CENTER FUEL TANK TO LEFT WING TANK. REPLACED FUEL TANK SCAVENGE SHUTOFF VALVE IA W AMM 28-15-21. 2 L 7 2 4F RT A16WE 2002110400096 20021104 00096 NM 2002 11 4 USAABB02170 1 20021002 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 27144 PVD - FOUND THE EXIT IDENTIFIER BATTERY AT THE L3 DOOR WEAK. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002110400097 20021104 00097 NM 2002 11 4 USAASB02183 1 20021001 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 446US 24873 CLT - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN THE LAST SEVEN ROWS OF SEATS INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE CHARGER ASSEMBLY AND BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002110400101 20021104 00101 NM 2002 11 4 2002UALA01436 1 20020906 A 3350 58674 INVERTER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 937UA 26668 EMERGENCY FLOOR LIGHTING BETWEEN ROWS 14 AND 19 INOPERATIVE. SUPPLEMENTAL DATA UPDATE REPLACED EEL POWER INVERTER AT ROW 14-19 AND EEL LIGHT SEGMENT. EEL LIGHT SYSTEM OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400102 20021104 00102 NM 2002 11 4 2002UALA01437 1 20020909 A 2780 WARNING SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT MALFUNCTIONED A UALA L A ABORTED APPROACH UNSCHED LANDING N FALSE WARNING AP APPROACH 1 WP 29 397UA 24672 AIRCRAFT DIVERTED TO AN ALTERNATE STATION WHEN THE SLAT IN TRANSIT LIGHT ILLUMINATED DURING THE INITIAL APPROACH. CHECK ED FLAP-SLAT POSITION INDICATION SYSTEM SEVERAL TIMES AND ALL OPS AND INDICATIONS NORMAL. REPLACED FLAP-SLAT INDICATION MODULE PRECAUTIONARY. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400103 20021104 00103 2002 11 4 2002UALA01446 4 20020822 A 3417 4061100901 ADC BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E/E BAY CONTAMINATED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 336UA 24240 RETURNED TO FIELD WHEN CAPTAIN'S AIRSPEED INDICATOR AND ALTIMETER FAILED. LINE MAINTENANCE FOUND WATER IN E&E BAY. THE NR 1 ADC AND FMC WAS REPLACED FOR WATER DAMAGE AND WATER WAS CLEANED FROM SHELF FWD OF ADC. OPERATIONAL CHECKS PASSED AS NORMAL. REMOVED DADC WAS CONFIRMED TO BE CONTAMINATED / WATER DAMAGED, UNIT WAS REPAIRED IN SHOP AND RETURNED TO SER VICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400105 20021104 00105 NM 2002 11 4 2002UALA01476 1 20020920 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 CABIN BODY FRAME WEB IS CRACKED BODY STATION 767 STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. SPLICED BODY FRAME WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400106 20021104 00106 NM 2002 11 4 2002UALA01478 1 20020922 A 3397 58791 WIRE HARNESS BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 935UA 26663 CREW REPORTS DURING SETUP THAT THE EMERGENCY ELECTRICAL LIGHTING (EEL) LIGHTS BETWEEN ROWS 10-20 WERE INOPERATIVE. FEED ER CABLE AT ROW 14 WAS DISCONNECTED. FEEDER CABLE WAS RECONNECTED AND SECURED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400107 20021104 00107 NM 2002 11 4 2002UALA01479 1 20020921 A 2751 1817389 TRANSMITTER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE T/E FLAP FAILED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 317UA 23949 AIRCRAFT LANDED UNDER AMBER ALERT DUE TO SPLIT FLAP INDICATION. NR 2 FLAP TRANSMITTER INOP. REPLACED TRANSMITTER WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400109 20021104 00109 NM 2002 11 4 2002UALA01481 1 20020923 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 945UA 26684 RIGHT HAND STATION 188 FUSELAGE FRAME CRACKED IN BEND OF OUTBOARD FRAME AT WL 207.5. MAJOR REPAIR ACCOMPLISHED. INSTAL LED SKIN & FRAME DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400110 20021104 00110 SO 2002 11 4 LR7A02078 1 20021026 A 5330 SKIN LKHEED 382 382G 526414U SO FS497-537 BUCKLED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HC5303 FOUND BELLY SKIN BUCKLED OUT OF LIMITS. FS497-FS53, LBL61-RBL61, WL130.REPLAC ED BELLY SKIN IAW SRM SMP 583-53-10 PG 2-5, 51-60, AND 51-70. NR0051. 2 H 7 4 4T A1SO 2002110400111 20021104 00111 SO 2002 11 4 LR7A02079 1 20021026 A 5311 3851872 FITTING LKHEED 382 382G 526414U SO FS817E CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HSP5338 FOUND RH SUPPORT ANGLE CRACKED. FS817E, RBL73, WL204.REPLACED ANGLE IAW SRM SMP 583-51-60, AND 51-70. NR0064. 2 H 7 4 4T A1SO 2002110400112 20021104 00112 SO 2002 11 4 LR7A02080 1 20021026 A 5342 ANGLE LKHEED 382 382G 526414U SO FS1041 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5505 FOUND HORIZONTAL STABILIZER UPPER FWD SPAR CAP TO INTERNAL BULKHEAD ATTACHMEN T ANGLE CRACKED. FS1041, LBL20, WL285.REPLACED ANGLE IAW SRM SMP 583-51-60, AND 51-70. NR0070. 2 H 7 4 4T A1SO 2002110400113 20021104 00113 SO 2002 11 4 LR7A02082 1 20021026 A 5230 WEB LKHEED 382 382G 526414U SO FS889 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HC05297 FOUND SPLIT IN CARGO DOOR WEB AT LBL36. FS889, LBL36, WL220.REPAIRED WEB IAW SRM SMP 583-51-140-12, 51-60, AND 51-70. NR0078. 2 H 7 4 4T A1SO 2002110400114 20021104 00114 SO 2002 11 4 LR7A02083 1 20021026 A 5230 WEB LKHEED 382 382G 526414U SO FS865 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HC05297 FOUND CARGO DOOR WEB CRACKED. FS865, RBL6, WL210.REPAIRED WEB IAW SRM SMP 58 3-51-140-17, 51-60, AND 51-70. NR0097. 2 H 7 4 4T A1SO 2002110400115 20021104 00115 SO 2002 11 4 LR7A02084 1 20021026 A 5230 STIFFENER LKHEED 382 382G 526414U SO FS865 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HC05297 FOUND CARGO DOOR WEB STIFFENER CRACKED. FS865, LBL15, WL210.REPAIRED STIFFEN ER IAW SRM SMP 583-51-140-23, 51-60, AND 51-70. NR0098. 2 H 7 4 4T A1SO 2002110400116 20021104 00116 SO 2002 11 4 LR7A02085 1 20021026 A 5511 RIB LKHEED 382 382G 526414U SO FS1039 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5505 FOUND LH HORIZONTAL STABILIZER LEADING EDGE UPPER FORMER CRACKED. FS1039, LH SS96, WL283.REPAIRED RIB IAW SRM SMP 583-51-140-20, 51-60, AND 51-70. NR0112. 2 H 7 4 4T A1SO 2002110400117 20021104 00117 SO 2002 11 4 LR7A02086 1 20021026 A 5511 RIB LKHEED 382 382G 526414U SO FS1010 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5505 FOUND LH HORIZONTAL STABILIZER LEADING EDGE LOWER FORMERS CRACKED AT FORWARD END. FS1010, LHSS101 AND 112, WL275.REPAIRED RIB IAW SRM SMP 583-51-140-20, 51-60, AND 51-70. NR0113. 2 H 7 4 4T A1SO 2002110400118 20021104 00118 SO 2002 11 4 LR7A02087 1 20021026 A 5511 RIB LKHEED 382 382G 526414U SO FS1031 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5505 FOUND LH HORIZONTAL STABILIZER LEADING EDGE LOWER FORMERS CRACKED. FS1031, LHSS138 AND 150, WL270.REPAIRED RIB IAW SRM SMP 583-51-140-20, 51-60, AND 51-70. NR0114. 2 H 7 4 4T A1SO 2002110400119 20021104 00119 SO 2002 11 4 LR7A02088 1 20021026 A 5511 RIB LKHEED 382 382G 526414U SO FS1039 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5505 FOUND RH HORIZONTAL STABILIZER LEADING EDGE LOWER FORMERS DISTORTED AND CRAC KED. FS1039, RHSS96, WL275.REPAIRED RIB IAW SRM SMP 583-51-140-20, 51-60, AND 51-70. NR0116. 2 H 7 4 4T A1SO 2002110400120 20021104 00120 SO 2002 11 4 LR7A02089 1 20021026 A 5511 RIB LKHEED 382 382G 526414U SO FS1036 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5505 FOUND RH HORIZONTAL STABILIZER LEADING EDGE UPPER FORMER CRACKED. FS1036, RH SS116, WL283.REPAIRED RIB IAW SRM SMP 583-51-140-20, 51-60, AND 51-70. NR0117. 2 H 7 4 4T A1SO 2002110400121 20021104 00121 SO 2002 11 4 LR7A02090 1 20021026 A 5511 RIB LKHEED 382 382G 526414U SO FS1044 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5505 FOUND RH HORIZONTAL STABILIZER LEADING EDGE LOWER FORMER CRACKED. FS1044, R HSS145, WL270.REPAIRED RIB IAW SRM SMP 583-51-140-20, 51-60, AND 51-70. NR0118. 2 H 7 4 4T A1SO 2002110400122 20021104 00122 SO 2002 11 4 LR7A02091 1 20021026 A 5511 RIB LKHEED 382 382G 526414U SO FS1054 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5505 FOUND RH HORIZONTAL STABILIZER LEADING EDGE LOWER FORMERS CRACKED. FS1054, R HSS191, 208, 215, AND 221, WL271.REPAIRED RIB IAW SRM SMP 583-51-140-20, 51-60, AND 51-70. NR0120. 2 H 7 4 4T A1SO 2002110400123 20021104 00123 SO 2002 11 4 LR7A02092 1 20021026 A 5312 341973L FITTING LKHEED 382 382G 526414U SO FS497 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5315 FOUND LH MLG BAY BOW BEAM UPPER FITTING TO SKIN CRACKED. FS497, LBL61, WL23 0.REPLACED FITTING IAW SRM SMP 583-51-60, AND 51-70. NR0149. 2 H 7 4 4T A1SO 2002110400124 20021104 00124 SO 2002 11 4 LR7A02098 1 20021026 A 5320 33874289 STRUT LKHEED 382 382G 526414U SO FS491 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HC5303 FOUND RH MLG BAY LOWER FWD SPLASH PANEL SUPPORT STRUT CRACKED. FS491, RBL61, WL165.REPLACED STRUT IAW SRM SMP 583-51-60, AND 51-70. NR0225. 2 H 7 4 4T A1SO 2002110400125 20021104 00125 SO 2002 11 4 LR7A02099 1 20021026 A 5330 3725253 DOUBLER LKHEED 382 382G 526414U SO FS597 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HC5303 FOUND BELLY SKIN DOUBLER CRACKED. FS597, LBL61, WL140.REPLACED DOUBLER IAW SR M SMP 583-51-60, AND 51-70. NR0243. 2 H 7 4 4T A1SO 2002110400126 20021104 00126 SO 2002 11 4 LR7A02101 1 20021026 A 5321 INTERCOSTAL LKHEED 382 382G 526414U SO FS148-160 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5325 FOUND FLIGHT DECK LH FWD CIRCUIT BREAKER PANEL FLOOR ANGLE CORRODED. FS148-1 60, LBL50, WL200.REPLACED ANGLE IAW SRM SMP 583-51-70. NR0265. 2 H 7 4 4T A1SO 2002110400127 20021104 00127 SO 2002 11 4 LR7A02102 1 20021026 A 5321 INTERCOSTAL LKHEED 382 382G 526414U SO FS188-196 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5325 FOUND FLIGHT DECK FLOOR ANGLE CORRODED. FS188-196, BL0, WL200.REPLACED INTER COSTAL ANGLE IAW SRM SMP 583-51-70. NR0266. 2 H 7 4 4T A1SO 2002110400128 20021104 00128 SO 2002 11 4 LR7A02103 1 20021026 A 5311 FRAME LKHEED 382 382G 526414U SO FS413 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HC5303 FOUND FUSELAGE SIDE EMERGENCY EXIT DOOR UPPER FRAME CRACKED AT FWD LOCATING PI N AREA. FSFS413, RBL77, WL226.REPAIRED FRAME IAW SRM SMP 583-51-140-10, 51-60, AND 51-70. NR0274. 2 H 7 4 4T A1SO 2002110400129 20021104 00129 SO 2002 11 4 LR7A02105 1 20021026 A 5321 33808612 STRAP LKHEED 382 382G 526414U SO FS228 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5325 FOUND CREW ENTRANCE FLOOR STRAP CORRODED. FS228, LBL59, WL146.REPLACED STRAP IAW SRM SMP 583-51-70. NR0287. 2 H 7 4 4T A1SO 2002110400130 20021104 00130 SO 2002 11 4 LR7A02106 1 20021026 A 5330 SKIN LKHEED 382 382G 526414U SO FS475-607 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HC5303 FOUND LH AND RH MLG INNER FAIRING LOWER SKINS CRACKED. FS475-607, LBL51-RBL51 , WL136.REPAIRED SKINS IAW LAC MEA 382-53-02-066. NR0331. 2 H 7 4 4T A1SO 2002110400131 20021104 00131 SO 2002 11 4 LR7A02107 1 20021026 A 5312 BEAM LKHEED 382 382G 526414U SO FS577 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5315 FOUND RH UPPER MLG BAY BEAM CRACKED. FS577, RBL65, WL230.REPAIRED BEAM IAW L AC MEA 382-53-02-072. NR0333. 2 H 7 4 4T A1SO 2002110400132 20021104 00132 SO 2002 11 4 LR7A02110 1 20021026 A 5312 BEAM LKHEED 382 382G 526414U SO FS597 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5319 FOUND RH MLG BEAM CORRODED. FS597, RBL66, WL196.REPAIRED BEAM IAW LAC MEA 38 2-53-02-067. NR0345. 2 H 7 4 4T A1SO 2002110400133 20021104 00133 SO 2002 11 4 LR7A02111 1 20021026 A 5312 BEAM LKHEED 382 382G 526414U SO FS577 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5315 FOUND LH UPPER MLG BEAM CRACKED. FS577, LBL62, WL248.REPAIRED BEAM IAW LAC M EA 382-53-02-071. NR0365. 2 H 7 4 4T A1SO 2002110400134 20021104 00134 NM 2002 11 4 2002UALA01482 1 20020924 A 3397 WIRE HARNESS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 EEL LIGHTING DAMAGED AT RIGHT HAND BUSINESS CLASS GALLEY. REPLACED TWO DAMAGED EEL LIGHTING STRIPS. REPAIRED DAMAGED P OWER LEAD AND INSTALLED NEW LIGHTING COVER STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002110400135 20021104 00135 NM 2002 11 4 2002UALA01483 1 20020923 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 STATION 365 RBL10-RBL62 WL208 TOP OF FLOORBEAM HAS PAINT WORN OFF AND LT CORROSION IN SEVERAL SPOTS. MAJOR REPAIR ACCOM PLISHED. REPLACED UPPER T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002110400136 20021104 00136 NM 2002 11 4 2002UALA01484 1 20020924 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 FRAME STATION 277 SHEAR TIE CRACKED BETWEEN STRINGER 16L AND 17L AFT SIDE OF FRAME. MAJOR REPAIR ACCOMPLISHED. INSTALL ED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400137 20021104 00137 NM 2002 11 4 2002UALA01485 1 20020924 A 2910 S43500711 MANIFOLD AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE HYD SYSTEM DAMAGED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 831UA 1291 RETURNED TO FIELD DUE TO A YELLOW HYDRAULIC LOW LEVEL INDICATION. FOUND TOP CENTER PLUG OF YELLOW SYSTEM LEAKAGE MEASUR EMENT VALVE BLOWN OUT. REPLACED GROUND LEAKAGE-MEASUREMENT MANIFOLD OF THE YELLOW SYSTEM, SERVICE YELLOW SYSTEM TO FULL . 2 L 7 2 4F 4 F RT A28NM E40NE 2002110400138 20021104 00138 SO 2002 11 4 C2XA02CL216 1 20021031 A 5320 14526850601 FIREWALL EMB 145 EMB145ER 3260211 SO AFT FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14943 145040 DURING A ROUTINE INSPECTION THE APU FIREWALL WAS FOUND CRACKED AT THE UPPER RIGHT ATTACH POINT.MAINTENANCE REPAIRED THE APU FIREWALL I/A/W GST 3249/02.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002112500116 20021125 00116 NE 2002 11 25 2002UALA01489 2 20020920 A 7230 797908 BLADE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE FAILED A UALA K NONE E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 602UA 15361 15361 21863 709613 LEFT ENGINE COMPRESSOR STALL. SINGLE STG 8 HPC BLADE FAILED .75 INCH FROM BLADE TIP. FATIGUE FAILURE ORIGINATING FROM SMALL FOD/DOD NICK AT LE. MINOR TIP DMG TO REMAINDER OF STG 8. NO OTHER DMG STG 7,8 & 9 HPC BLADES ARE INSTALLED NEW AT EACH HPC DEBLADE. 2 L 7 2 4F 4 F RT A1NM E3NE 2002110400139 20021104 00139 NM 2002 11 4 2002UALA01490 1 20020925 A 5720 STIFFENER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE LT WING GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 945UA 26684 LEFT HAND WING S12 Z STIFFENER GOUGED ON EDGE OF LOWER FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400140 20021104 00140 NM 2002 11 4 2002UALA01491 1 20020926 A 5512 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 945UA 26684 LEFT HAND HORIZONTAL STABILIZER LOWER LEADING EDGE HAS 3 EA LARGE DENTS. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW SKI N TO CONTOUR & FABRICATED SPLICES. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400141 20021104 00141 NM 2002 11 4 2002UALA01492 1 20020925 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 AFT LEFT ENTRY DOOR FRAME IS CRACKED AT APPROXIMATELY STATION 967 STRINGER 12 LEFT TO 13 LEFT. MAJOR REPAIR ACCOMPLISHE D. MANUFACTURED AND INSTALLED REPAIR DOUBLER STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400142 20021104 00142 NM 2002 11 4 2002UALA01494 1 20020927 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 CABIN STUB FRAME STATION 294 RIGHT HAND SIDE CRACKED AT TOP DOOR STOP FITTING AS VIEWED FROM FORWARD SIDE. MAJOR REPAIR ACCOMPLISHED. STUB FRAME REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400143 20021104 00143 NM 2002 11 4 2002UALA01495 1 20020926 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN FRAME WEB CRACKED BODY STATION 807 STRINGER 9L WL 258. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR ON FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400144 20021104 00144 NM 2002 11 4 2002UALA01496 1 20020926 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 CABIN OVERWING FRAME AT STATION 616 LEFT HAND IS CRACKED INBOARD LOWER FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. INSTA LLED STIFFENING ANGLE, TAPERED SHIM & FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400145 20021104 00145 NM 2002 11 4 2002UALA01497 1 20020926 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 LT WW PRESSURE DECK IS CRACKED AT STA 663.75 AT LBL 31. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400146 20021104 00146 SO 2002 11 4 C2XA02CL217 1 20021031 A 3350 1317 LAMP EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17507 145215 DURING ROUTINE MAINTENANCE THE EMERGENCY AISLE LIGHT AT ROW 9 WAS INOPERATIVE.MAINTENANCE REPLACED THE LAMP IN EMERGENCY AISLE LIGHT AT ROW 9.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002112600055 20021126 00055 NE 2002 11 26 2002UALA01498 2 20020927 A 7230 50B927 BEARING BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 791UA 20719 26933 222006 LEFT ENGINE OIL FILTER DIFFERENTIAL WARNING EICAS ILLUMINATED. REPLACED ENGINE. SUBSEQUENT SHOP TEARDOWN REVEALED FAIL URE OF THE NR 1 BEARING. BOTH OF THE BEARING'S INNER RACEWAY HALVES HAD MACHINED THE CAGE INNER DIAMETER 360 DEGREES. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002110400147 20021104 00147 NM 2002 11 4 2002UALA01499 1 20020926 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 CABIN FLOOR BEAM AT STA 947 LBL 15 CORROSION REMOVAL EXCEEDED BLEND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400148 20021104 00148 NM 2002 11 4 2002UALA01500 1 20020926 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 CABIN FLOOR BEAM EXCESSIVE MATERIAL LOSS DUE TO CORROSION STATION 1640 RBL36-38.5 UPPER CAP. MAJOR REPAIR ACCOMPLISHED. REMOVED 2 STRAPS AND ANGLE INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002110400149 20021104 00149 NM 2002 11 4 2002UALA01501 1 20020927 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 CABIN DOOR 1R CUTOUT FWD FRAME CRACKED AT LOWER INBD CORNER AT FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400150 20021104 00150 NM 2002 11 4 2002UALA01502 1 20020928 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN STATION 827 FRAME WEB ABOVE STRINGER 9R SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE INSTALLED ON FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400151 20021104 00151 NM 2002 11 4 2002UALA01503 1 20020928 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN STATION 887 FRAME WEB ABOVE STRINGER 9L SHEAR TIE, IS CRACKED. REPAIR ANGLE INSTALLED ON FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400152 20021104 00152 NM 2002 11 4 2002UALA01504 1 20020928 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 STATION BODY STATION 616 STRINGER CLIP CRACKED 4L STRINGER. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400153 20021104 00153 NM 2002 11 4 2002UALA01505 1 20020928 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 STATION 727A STRINGER CLIP CRACKED STRINGER 6R. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400154 20021104 00154 NM 2002 11 4 2002UALA01506 1 20020929 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 EXTERIOR FUSELAGE STATION 1000 LEFT HAND STRINGER 15L HAS SEVERAL DENTS AFT FUSELAGE SKIN HAS DENT AT SKIN LAP STR 14L S TA 990 MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400155 20021104 00155 NM 2002 11 4 2002UALA01507 1 20020928 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN STATION 480 FRAME IS CRACKED AT STRINGER 9R AT PASSENGER SERVICE UNIT-VENT SUPPORT INBOARD FASTENER. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400156 20021104 00156 NM 2002 11 4 2002UALA01508 1 20020928 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN FLOOR BEAM INTERCOSTAL UPPER FLANGE IS CRACKED BODY STATION 500D-520, BL0, WL208. MAJOR REPAIR ACCOMPLISHED. REP LACED INTERCOSTAL UPPER FLANGE . 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400157 20021104 00157 NM 2002 11 4 2002UALA01509 1 20020928 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN STATION 887 FRAME WEB ABOVE STRINGER 9R SHEAR TIE IS CRACKED. REPAIR ANGLE INSTALLED ON FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400158 20021104 00158 NM 2002 11 4 2002UALA01510 1 20020929 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN STATION 440 FRAME IS CRACKED AT STRINGER 10L IN RADIUS JUST INBOARD OF STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED. FUSELAGE FRAME REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400159 20021104 00159 NM 2002 11 4 2002UALA01511 1 20020929 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 STRINGER 14L CRACKED AT MOST FORWARD HOLE, AFT OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400160 20021104 00160 NM 2002 11 4 2002UALA01512 1 20020929 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 STRINGER 14L CRACKED AT MOST FORWARD HOLE, AFT OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED STRINGER REPAIR & F ILLERS. FABRICATED RADIUS FILLER AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400161 20021104 00161 NM 2002 11 4 2002UALA01515 1 20020920 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 CABIN BODY FRAME WEB IS CRACKED BODY STATION 767 STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. SPLICED BODY FRAME WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400162 20021104 00162 NM 2002 11 4 2002UALA01516 1 20020930 A 5512 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN WAS CRACKED AT AFT SPAR JUST FWD OF PANEL 9207. MAJOR REPAIR ACCOMPLISHED. REMOVED INTERIM REPAIR. CUTOUT DAMAGED AREA. INSTALLED PERMANENT REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400163 20021104 00163 NM 2002 11 4 2002UALA01517 1 20020930 A 5320 SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN STATION 907 STRINGER 4R STRINGER SPLICE IS CRACKED AT 2 FASTENERS. MAJOR REPAIR ACCOMPLISHED. REPLACE STRINGER S PLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400164 20021104 00164 NM 2002 11 4 2002UALA01518 1 20020928 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 LT FUSE STA 1701 DENTED IN 2 PLACES, JUST ABOVE STRINGER 19 AND JUST BELOW STRINGER 20. 2 L 7 2 4F 4 F RT A2NM E17NE 2002110400165 20021104 00165 NM 2002 11 4 2002UALA01519 1 20020930 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 673UA 29241 EMERGENCY FLOOR PROXIMITY LIGHTS ON SEATS 26 AND 27HJ INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2002110400166 20021104 00166 2002 11 4 2002UALA01520 4 20020930 A 3414 2083111 INDICATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 354UA 24360 AIRCRAFT ABORTED TAKEOFF DUE TO LOSS OF FIRST OFFICERS AIRSPEED INDICATION. FLIGHT CREW ABORTED TAKE OFF AT 90 KNOTS DU E TO A FLAG IN VIEW ON THE FIRST OFFICERS MACH AIRSPEED INDICATOR. LINE MAINTENANCE REPLACED THE FIRST OFFICERS MACH AI RSPEED INDICATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400167 20021104 00167 NM 2002 11 4 2002UALA01521 1 20021001 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 AFT CABIN RIGHT HAND SIDE FLOOR CREASE BEAM CORRODED BETWEEN STA 947-990 JUST INBOARD OF DOOR 2 RIGHT HAND BELOW DRAIN G UTTER. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400168 20021104 00168 NM 2002 11 4 2002UALA01522 1 20021001 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN STATION 827 FRAME WEB ABOVE STRINGER 9L SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAI R. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400169 20021104 00169 NM 2002 11 4 2002UALA01523 1 20021001 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN STATION 480 FRAME IS CRACKED AT STRINGER 9L PASSENGER SERVICE UNIT VENT SUPPORT INBOARD FASTENER. MAJOR REPAIR AC COMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400170 20021104 00170 NM 2002 11 4 A6WA200230016 1 20020907 A 3830 SINK DORNER DO32 DO328100 2996000 NM LAVATORY CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 THE LAVATORY SINK HAS CORROSION AT THE SINK STOPPER. MAINTENANCE REMOVED CORROSION ON LAVATORY SINK STOP IAW DO 328 SRM 51-21-00 AND FIXED REPAIR OF PAINT COATING IAW DO 328 51-93-21. (M) 2 H 7 2 4T RT A45NM 2002110400171 20021104 00171 NM 2002 11 4 A6WA200230017 1 20020907 A 5320 FLOOR SUPPORT DORNER DO32 DO328100 2996000 NM FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 FLOOR SUPPORT AT FRAME 39 HAS MINOR SURFACE CORROSION ON TOP SURFACE AROUND CLIP NUT HOLES. REMOVED LIGHT SURFACE CORRO SION FROM FLOOR SUPPORT. REINSTALLED CLIPS. (M) 2 H 7 2 4T RT A45NM 2002110400172 20021104 00172 NM 2002 11 4 2002UALA01524 1 20021001 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN STATION 807 FRAME WEB ABOVE STRINGER 9R SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAI R. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400173 20021104 00173 NM 2002 11 4 2002UALA01525 1 20021001 A 5320 SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN 907 STRINGER 4L STRINGER SPLICE IS CRACKED AT TWO FASTENERS. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400174 20021104 00174 NM 2002 11 4 2002UALA01526 1 20021001 A 3397 58791 WIRE HARNESS BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 357UA 24378 AIRCRAFT EEL LIGHTING FOUND INOPERATIVE DURING PRE FLIGHT SETUP. REPAIRED POWER FEEDER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400175 20021104 00175 NM 2002 11 4 2002UALA01527 1 20021002 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 CABIN WHEEL WELL PRESSURE DECK STATION 664 WEB IS CRACKED FWD OF AILERON CONTROL QUADRANT. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400176 20021104 00176 NM 2002 11 4 2002UALA01528 1 20021002 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN STATION 400 FRAME IS CRACKED AT STATION 9L PASSENGER SERVICE UNIT - VENT SUPPORT INBOARD FASTENER. MAJOR REPAIR A CCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400178 20021104 00178 NM 2002 11 4 2002UALA01531 1 20021003 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN STATION 787 FRAME WEB JUST ABOVE STRINGER 9R SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE INSTA LLED ON FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400179 20021104 00179 NM 2002 11 4 2002UALA01532 1 20021003 A 3260 WARNING SYSTEM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 912UA 25290 RETURN TO FIELD DUE TO GEAR UNSAFE INDICATION. LT GEAR UNSAFE LIGHT IS ILLUMINATED WITH GEAR HANDLE IN THE OFF POSITION . OHMED LT MAIN UP SENSOR, CHECKED OK, JACKED AIRCRAFT AND SWUNG GEAR NUMEROUS TIMES, ACP MANUAL GEAR EXTENSION. CHECKS OK. UNABLE TO DUPLICATE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400180 20021104 00180 NM 2002 11 4 2002UALA01534 1 20021003 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 CREASE BEAM WEB AT STA 741-743, RBL 68, STRINGER 17 RT AT WATERLINE 208 NEEDS REPLACING. MAJOR REPAIR ACCOMPLISHED. MI D CABIN RT CREASE BEAM WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002110400181 20021104 00181 NM 2002 11 4 2002UALA01535 1 20021004 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 FORWARD CABIN STATION 360 RBL 12 FLOORBEAM HAS SURFACE CORROSION. MAJOR REPAIR ACCOMPLISHED, INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400182 20021104 00182 NM 2002 11 4 2002UALA01538 1 20021006 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 RIGHT HAND CREASE BEAM WEB CORRODED BETWEEN BODY STATION 578 AND 597. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400183 20021104 00183 NM 2002 11 4 2002UALA01539 1 20021006 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 RIGHT HAND CREASE BEAM WEB CORRODED BETWEEN BODY STATION 616 AND 639. MAJOR REPAIR ACCOMPLISHED. NEW WEB INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400184 20021104 00184 NM 2002 11 4 2002UALA01540 1 20021006 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN INTERCOSTAL, OUTBOARD ANGLE CRACKED FORWARD OF BODY STATION 291.5 FRAME AND BELOW STRINGER 11 RIGHT HAND. MAJOR R EPAIR ACCOMPLISHED. REPLACED ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400185 20021104 00185 NM 2002 11 4 2002UALA01541 1 20021006 A 2840 WARNING SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 315UA 23947 RETURN TO FIELD UNDER AMBER ALERT DUE TO FUEL QUANTITY INDICATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110400186 20021104 00186 NM 2002 11 4 2002UALA01542 1 20021004 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 CABIN FLOOR BEAM UPPER CAP HAD EXCESS MATERIAL REMOVED DURING CORROSION CLEAN UP AT STATION 680 RBL 5 TO RBL 12, TWO SPO TS STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002110400187 20021104 00187 WP 2002 11 4 AT0200087 1 20021101 A 2150 20495054 ACM DOUG DC9 DC932 3022066 WP RIGHT A ZZDA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 15 837AT 45774 TAKE OFF FRO 28L-CLIMBING THROUGH 3,000' LEAD FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, DECLARED EMERGENCY, RETURNED TO PIT, COMPLETED EMERGENCY CHECK LIST. CORRECTIVE ACTION: INSPECTED, BOTH A/C PACKS DURING FUL L POWER TAKE OFF RUN. ENGINE RUN PERFORMED TWICE. MAINTENANCE INSPECTED LAVATORIES, AFT FLIGHT ATTENDANT OVERHEAD PANE LS AND ALL CABINS BALLASTS. REMOVED AND REPLACED RIGHT AIR CYCLE MACHINE. NO FURTHER DEFECTS OR SMELLS NOTED. 2 L 7 2 4F A6WE 2002110400188 20021104 00188 SO 2002 11 4 C2XA02CL218 1 20021102 A 5270 14528237001 PIN EMB 145 EMB145LR 3260212 SO CABIN STICKING A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16954 145072 DURING ROUTINE MAINTENANCE THE RIGHT HAND EMERGENCY EXIT DOOR DID NOT INDICATE OPEN ON THE EICAS WHEN OPENED.MAINTENANCE CLEANED AND LUBRICATED THE RIGHT EMERGENCY EXIT DOOR SWITCH ACTUATION PIN.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002110400189 20021104 00189 SO 2002 11 4 C2XA02CL219 1 20021102 A 5270 14528237001 PIN EMB 145 EMB145LR 3260212 SO CABIN STICKING A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16954 145072 DURING ROUTINE MAINTENANCE THE LEFT HAND EMERGENCY EXIT DOOR DID NOT INDICATE OPEN ON THE EICAS WHEN OPENED.MAINTENANCE CLEANED AND LUBRICATED THE LEFT EMERGENCY EXIT DOOR SWITCH ACTUATION PIN.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002110400190 20021104 00190 EA 2002 11 4 COMA0260623 1 20021031 A 2420 GENERATOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 478CA 7671 FLIGHT 5660 ADG DEPLOYED DURING FLIGHT.RESTOWED ADG - CONTROL PANEL TEST WAS NORMAL. 2 L 7 2 4F RT A21EA 2002110400191 20021104 00191 EU 2002 11 4 YENA200227 1 20021101 A 3221 D23592020 SHOCK ABSORBER AIRBUS 320 A320232 3930326 EU NOSE GEAR MISALIGNED A YENA O OTHER J WARNING INDICATION CL CLIMB 1 EA 15 503JB 10723 1123 FLT #3, BUF to JFK, Landing gear shock absorber fault Wheel Nose wheel Steer fault ECAM after take off. Gear would not g o up. Nose gear 90 degree on landing with failure.Inspected nose gear, Removed and replaced shockstrut assy per AMM 32-2 1-13-401 and AMM 32-21-13-000-001, Ops and leak check ok, performed normal and alt gear operation, all normal and OK for service as per ref AMM 32-21-16-000-002. Note: Crew reported that after take off from BUF gear would not retract. resea rch of PFR data showed L/G shock absorber fault with associated NLG prox sensor faults identified by both LGCIU 1 and 2. Also a NW Steering fault was identified by BSCU 1 and 2.Aircraft landed at JFK iaw FCOM procedures 3.02.32 P1. N 2 L 7 2 4F RT A28NM 2002110400192 20021104 00192 NM 2002 11 4 AALA20021333 1 20020920 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 377AN 25446 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROW 31 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 31. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002110400193 20021104 00193 NM 2002 11 4 AWXA200201067 1 20021028 A 5313 6545767512 STRINGER BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 0 0 23218 MCN - MAJOR REPAIR - DURING C-18 CHECK A .050" CRACK WAS FOUND ON STRINGER 16 L/H AT BS 500C+4. MAINTENANCE TRIMMED OFF CRACKED END OF STRINGER 16 L/H AT BS 500C+4; FABRICATED A FILLER AND REPAIR CHANNEL; AND INSTALLED REPAIR PARTS IAW AWA E.R. 03-5312-01094-DD1, AND B737-300 SRM 51-40-02, PG. 10-11, 44-49, FIG. 12. 2 L 7 2 4F RT A16WE 2002110400194 20021104 00194 NM 2002 11 4 AWXA200201069 1 20021028 A 5342 6554842U19 ANGLE BOEING 737 7373G7 1384595 NM CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 0 0 23218 MCN - MAJOR REPAIR - DURING C-18 CHECK THE L/H VERTICAL STABILIZER TO FUSELAGE "L" ANGLE WAS FOUND CHAFED AND WORN BS 10 16 - BS 1126. MAINTENANCE REMOVED THE L/H VERTICAL STABILIZER TO FUSELAGE "L" ANGLE BS 1016 - BS 1126; FABRICATED A NEW REPLACEMENT ANGLE; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG. 3-4, & 38. 2 L 7 2 4F RT A16WE 2002110400195 20021104 00195 NM 2002 11 4 AWXA200201070 1 20021025 A 5320 654585546 FLOOR SUPPORT BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND AROUND NUTPLATES ON LOWER SURFACE OF FLOOR SUPPOR T BS 977 - BS 989, WL 208, LBL 50. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED FLOO R SUPPORT FROM BS 967 TO BS 989; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05, PG. 4, FIG. 2, AND SRM 51-40-02, PG. 5, 10-11. 2 L 7 2 4F RT A16WE 2002110500001 20021105 00001 SO 2002 11 5 C2XA02CL220 1 20021103 A 3234 7455501 LEVER EMB 145 EMB145LR 3260212 SO COCKPIT INTERMITTENT A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13550 145575 CLE FLIGHT 3024 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER.OPERATIONAL CHECKS WERE GOOD.T HE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002110500002 20021105 00002 SO 2002 11 5 C2XA02SH106 1 20021017 A 5410 14576143001 STRUCTURE EMB 145 EMB145ER 3260211 SO NR 2 ENG NACELLE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 DURING C CHECK NR 2 ENGINE LOWER NACELLE DISH AROUND INTERIOR OF ENGINE DRAIN WAS FOUND TO HAVE A GOUGE. MAINTENANCE RE MOVED AND REPLACED DISH IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2002110500003 20021105 00003 SO 2002 11 5 C2XA02SH108 1 20021017 A 5410 14576599004 STIFFENER EMB 145 EMB145ER 3260211 SO NR 2 ENG NACELLE WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 DURING C CHECK NR 2 LOWER ENGINE NACELLE HAD WEAR MARKS 12 INCHES INBOARD OF CENTER. MAITENANCE REMOVED DAMAGE AREA AND PEFORMED AN ANGLE REPAIR IAW EMB SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110500004 20021105 00004 SO 2002 11 5 C2XA02SH110 1 20021018 A 5410 14576518001 STRUCTURE EMB 145 EMB145ER 3260211 SO NR 1 ENG NACELLE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 DURING C CHECK NR 1 ENG LOWER NACELLE WAS FOUND TO HAVE A GOUGE AT FORWARD OUTBOARD ATTACHEMENT. MAITENANCE REMOVED DAMA GE AREA AND REPAIRED AFFECTED EDGE MEMBER IAW EMB 145 SRM54-10-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110500005 20021105 00005 SO 2002 11 5 C2XA02SH111 1 20021019 A 5311 14523050401 FRAME EMB 145 EMB145ER 3260211 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 DURING C CHECK, A GOUGE WAS FOUND ON FRAME 64 BETWEEM STRINGERS 6R AND 8R. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFF ECTED SECTION IAW CONTINENTAL EXPRESS EC 5330-1200. THE AIRCRAFT WAS APPROVED TO RETURN SERVICE. 2 L 7 2 4F RT T00011AT 2002110500006 20021105 00006 SO 2002 11 5 C2XA02SH112 1 20021020 A 5311 14523049401 FRAME EMB 145 EMB145ER 3260211 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 DURING C CHECK, A GOUGE WAS FOUND ON FRAME 63 BETWEEM STRINGERS 6 AND 8. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFEC TED AREA IAW CONTINENTAL EXPRESS EC 5330-1200. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110500007 20021105 00007 SO 2002 11 5 C2XA02SH113 1 20021023 A 5315 14521713003 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14933 145018 DURING C CHECK, THE CENTER FLOORBEAM AT FRAME 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110500008 20021105 00008 SO 2002 11 5 C2XA02SH121 1 20021031 A 5320 14590141001 ANGLE EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14933 145018 DURING C CHECK, LT FLOORBEAM RAMP ANGLE INBOARD AT FRAME 20 HAS CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110500009 20021105 00009 SO 2002 11 5 C2XA02TY150 1 20021013 A 5210 1202106500 SKIN EMB 145 EMB145LR 3260212 SO PAX DOOR DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 DURING A SCHEDULED INSPECTION, THE PASSENGER DOOR WAS FOUND DENTED AT LOWER FORWARD CORNER. MAINTENANCE RECONTOURED THE DENTED AREA, PERFORMED DYE PENETRANT INSPECTION, NO DEFECTS NOTED. IAW EMB-GST-2984/02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLECTION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002110500010 20021105 00010 SO 2002 11 5 C2XA02TY154 1 20021021 A 5751 14569009402 STRUCTURE EMB 145 EMB145LR 3260212 SO RT AILERON GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 DURING A SCHEDULED 2-C INSPECTION, THE RT AILERON PCA ATTACH POINT WAS FOUND WITH TOOLING MARKS. MAINT MEASURED THE DAM AGE AND BLENDED TOOLING MARKS, PRIMED AND PAINTED IAW GST-3000/02,CPM-51-21-05,06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2 L 7 2 4T RT T00011AT 2002110500011 20021105 00011 SO 2002 11 5 C2XA02TY155 1 20021025 A 5310 14521725013 SILL EMB 145 EMB145LR 3260212 SO SERVICE DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 DURING A SCHEDULED INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE A CCOMPLISHED A BLEND-OUT REPAIR IAW EMBRAER GST 1927/02A, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPO N COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002110500012 20021105 00012 SO 2002 11 5 C2XA02TY156 1 20021025 A 5514 14521904411 FITTING EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 DURING A SCHEDULED INSPECTION THE HORIZONTAL STAB LEFT INBOARD LUG FOR THE MOUNT PIN WAS FOUND TO BE GOUGED. MAINTENANC E POLISHED OUT THE DAMAGED AREA IAW EMBRAER GST 3175/02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPO N COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002110500013 20021105 00013 SO 2002 11 5 C2XA02TY157 1 20021025 A 5320 14522460005 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 DURING A SCHEDULED INSPECTION THE AFT GUSSET UNDERNEATH THE GALLEY AREA WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLIS HED A BLEND-OUT REPAIR IAW EMB145 SRM 53-21-10 AND CPM 51-21-04,05. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INS PECTION. 2 L 7 2 4T RT T00011AT 2002110500014 20021105 00014 SO 2002 11 5 C2XA02TY158 1 20021025 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM TOP CAP WAS FOUND CORRODED UNDERNEATH THE GALLEY AREA. MAINTENANCE A CCOMPLISHED A BLEND-OUT REPAIR IAW EMB-145 SRM 53-21-10, 51-21-04,05. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002110500015 20021105 00015 SO 2002 11 5 C2XA02TY159 1 20021025 A 5315 14522460005 FLOORBEAM EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 DURING A SCHEDULED INSPECTION THE AFT FLOORBEAM TOP CAP WAS FOUND CORRODED UNDERNEATH THE GALLEY AREA. MAINTENANCE ACCO MPLISHED A BLEND-OUT REPAIR IAW EMB-145 SRM 53-21-10 AND CPM 51-21-04,05. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002110500016 20021105 00016 SO 2002 11 5 C2XA02TY161 1 20021102 A 5514 14521904411 FITTING EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 DURING A SCHEDULED INSPECTION THE LEFT HAND HORIZONTAL STAB FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. MAINTENANCE A CCOMPLISHED A BLEND-OUT REPAIR IAW EMB GST 3201/02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COM PLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002110500017 20021105 00017 SO 2002 11 5 C2XA02TY162 1 20021102 A 5514 14521904412 FITTING EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 DURING A SCHEDULED INSPECTION THE RIGHT HAND HORIZONTAL STAB FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB GST 3201/02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON CO MPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002110500018 20021105 00018 SO 2002 11 5 C2XA02TY163 1 20021102 A 5315 14521713003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 DURING A SCHEDULED INSPECTION THE RT FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IA W EMB GST 1927/02A, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002110500019 20021105 00019 SO 2002 11 5 C2XA02TY164 1 20021102 A 5315 14521721009 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 DURING A SCHEDULED INSPECTION THE GALLEY FLOOR FORWARD FLOORBEAM CAP WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB-145 SRM 53-21-10, 51-40-02 AND CPM 51-21-04,05,06. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002110500020 20021105 00020 SO 2002 11 5 C2XAO2CL199 1 20021011 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14960 145100 CREW REPORTED OVERHEAD EMERGENCY SIGN WOULD NOT ILLUMINATE WHEN TESTED MAINTENANCE RESECURED CONNECTOR PLUG AND VERIFIED NORMAL OPERATION 2 L 7 2 4F RT T00011AT 2002110500021 20021105 00021 SO 2002 11 5 C2XAO2SH114 1 20021023 A 5310 THRESHOLD EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14933 145018 DURING C CHECK AFT SUPPORT UNDER MAIN DOOR THRESHOLD WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACE D AFFECTED SUPPORT IAW 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002110500022 20021105 00022 SO 2002 11 5 C2XXA02IA207 1 20021002 A 7830 WARNING SYSTEM EMB 145 EMB145 3260210 SO THRUST REVERSER ACTIVATED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 13970 145146 ENGINE NR 1 THRUST REVERSER DISAGREE ON TAKE-OFF ROLL. DAL- MAINTENANCE PLACED THE THRUST REVERSER ON MEL. 2 L 7 2 4F RT T00011AT 2002110500023 20021105 00023 SO 2002 11 5 CX2A02CL212 1 20021026 A 3397 WIRE EMB 145 EMB145ER 3260211 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13929 145009 DURING ROUTINE MAINTENANCE THE NR 3 EMERGENCY FLOOR LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND FOUND THE L IGHT STRIP HAD BROKEN WIRES. THE LIGHT STRIP WAS REPLACED.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002110500024 20021105 00024 GL 2002 11 5 CX2A02RI006 2 20021027 A 7261 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 LEAKING A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 11551 145411 CREW REPORTED SMOKE IN CABIN WITH EITHER ENGINE BLEED SELECTED AND LAV SMOKE INDICATION. MAINTENANCE DETERMINED SMOKE CO MING FROM AN OIL LEAK INTERNAL TO THE NR 1 ENGINE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE PERFORMED OPERATIONAL AN D LEAK TESTS. THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500025 20021105 00025 NM 2002 11 5 F3LA200200358 1 20021021 A 5710 65C26506506 HOUSING BOEING 737 737301 1384611 NM SLAT TRACK WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 55067 23257 DURING C 4 CHECK, TRACK HOUSING WAS FOUND TO HAVE A HOLE WORN THROUGH IT CAUSING FUEL LEAK. HOUSING IS LOCATED INSIDE THE WING TANK FOR NR 5 OUT BOARD SLAT TRACK, RT WING STA 497. REMOVED DAMAGED NR 5 OUT BOARD SLAT TRACK HOUSING IN ACCO RDANCE WITH THE REQUIREMENTS OF SRM 51-40-02. LOCATED AND DRILLED NEW HOUSING IAW THE REQUIREMENTS OF SRM 51-40-05 AND INSTALLED NEW HOUSING IAW THE REQUIREMENTS OF SRM 51-40-02 AND SEALED IAW THE REQUIREMENTS OF MM 28-11-00. 2 L 7 2 4F RT A16WE 2002110500026 20021105 00026 NM 2002 11 5 F3LA200200363 1 20021024 A 5320 FLOOR SUPPORT BOEING 737 737300 1384610 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 313FL 27617 3122 26442 DURING C 2 CHECK, THE AFT CARGO COMPARTMENT FLOOR TRACK WAS FOUND CORRODED AT STA 727D AT RBL 13.8 THE CORRODED SECTIO N OF TRACK WAS REPLACED BETWEEN STA 727 AND STA 767 IAW SRM 51-40-02 2 L 7 2 4F RT A16WE 2002110500027 20021105 00027 NM 2002 11 5 F3LA200200365 1 20021018 A 5350 TAIL CONE BOEING 737 737300 1384610 NM FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 313FL 26442 DURING C 2 CHECK, A DENT WAS FOUND ON THE LT SIDE OF THE TAIL CONE, NEAR THE ELEVATOR ATTACH POINTS. DENT WAS REPAIRED AND PAINTED IAW MAINTENANCE MANUAL 737-300 MM 51-21-99 AND SRM 51-70-06. 2 L 7 2 4F RT A16WE 2002110500028 20021105 00028 NM 2002 11 5 F3LA200200366 1 20021022 A 5320 FLOOR SUPPORT BOEING 737 737300 1384610 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 313FL 27617 3122 26442 DURING C 2 CHECK, AFT CARGO FLOOR TRACK WAS FOUND CORRODED AT STA 860, LBL 3.0 FLOOR TRACK REPLACED BETWEEN STA 791 TO STA 860. LBL 3.0, IAW SRM 51-40-02 2 L 7 2 4F RT A16WE 2002110500029 20021105 00029 NM 2002 11 5 F3LA200200367 1 20021017 A 5512 SKIN BOEING 737 737300 1384610 NM STABILIZER BIRD STRIKE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 313FL 27617 3122 26442 DURING C 2 CHECK, A BIRD STRIKE WAS FOUND ON THE RT LEADING EDGE OF THE STABILIZER BETWEEN STA 184.7 AND STA 189.2. FAB RICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55-10-01. 2 L 7 2 4F RT A16WE 2002110500030 20021105 00030 NM 2002 11 5 F3LA200200368 1 20021023 A 5754 SKIN BOEING 737 737300 1384610 NM LE FLAP PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 313FL 27617 3122 26442 DURING C 2 CHECK, IT WAS NOTED RT, IN BOARD FORE FLAP HAD A HOLE IN THE LOWER SURFACE. FLAP WAS REMOVED AND REPAIRED IA W SRM 51-70-10 AND REINSTALLED IAW BOEING 737 MM 27-51-07. 2 L 7 2 4F RT A16WE 2002110500031 20021105 00031 NM 2002 11 5 F3LA200200369 1 20021023 A 5320 FLOOR SUPPORT BOEING 737 737300 1384610 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 313FL 27617 3122 26442 DURING C 2 CHECK, AFT CARGO FLOOR TRACK WAS FOUND CORRODED AT STA 860, RBL 2. FLOOR TRACK WAS REPLACED BETWEEN STA 727 AND STA 947, RBL 2.5 IAW SRM 51-40-05 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002110500032 20021105 00032 NM 2002 11 5 F3LA200200370 1 20021024 A 5320 INTERCOSTAL BOEING 737 737300 1384610 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 313FL 27617 3122 26442 DURING C 2 CHECK, CORROSION WAS FOUND ON THE AFT CARGO PIT INTERCOSTAL SURFACE AND AROUND NUT PLATES BETWEEN STA 767 TO STA 794 AND RBL 21. NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-02, SRM 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002110500033 20021105 00033 NM 2002 11 5 F3LA200200371 1 20021020 A 5321 FLOOR PANEL BOEING 737 737300 1384610 NM CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 313FL 27617 3122 26442 DURING C 2 CHECK, THE AFT CARGO COMPARTMENT FLOOR TRANSITION PANEL WAS FOUND CORRODED BETWEEN STA 787 AND STA 807. AFT CARGO COMPARTMENT FLOOR TRANSITION PANEL WAS REMOVED AND REPLACED BETWEEN STA 727 AND 947, LBL 20 IAW SRM 53-60-53 AND S RM 51-40-02. 2 L 7 2 4F RT A16WE 2002110500034 20021105 00034 NM 2002 11 5 F3LA200200372 1 20021023 A 5320 FLOOR SUPPORT BOEING 737 737300 1384610 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 313FL 27617 3122 26442 DURING C 2 CHECK, CORROSION WAS FOUND OF THE AFT CARGO COMPARTMENT FLOOR TRACK AT STA 791, LBL 11.5. REMOVED AND REPLAC ED THE FLOOR TRACK IAW SRM 51-10-02 AND SRM 51-40-02, BETWEEN STA 727 AND STA 947 AT LBL 11.5. 2 L 7 2 4F RT A16WE 2002110500035 20021105 00035 NM 2002 11 5 F3LA200200373 1 20021008 A 5320 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 29024 3229 26301 DURING C 4 CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT LOCATED AT LBL 29, BETWEEN STA 986.5 AND STA 1006. NEW FLOOR SU PPORT WAS FABRICATED AND INSTALLED IAW SRM 53-60-51, SOPM 26-41-02 AND SRM 51-40 02. 2 L 7 2 4F RT A16WE 2002110500036 20021105 00036 NM 2002 11 5 F3LA200200374 1 20021008 A 5310 DOOR FRAME BOEING 737 7373Q8 1384670 NM PAX DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 29024 3229 26301 DURING C 4 CHECK, CORROSION WAS FOUND AT THE AFT ENTRY DOOR FRAME AND CUT OUT AREA. CORROSION WAS WITHIN LIMITS AND THE AREAS WERE TREATED, PRIMED AND PAINTED FOLLOWING BLENDING IAW SRM 53-60-15, DETAIL VIII, AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002110500037 20021105 00037 NM 2002 11 5 F3LA200200375 1 20021008 A 5310 SILL BOEING 737 7373Q8 1384670 NM PAX DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 29024 3229 26301 DURING C 4 CHECK, REAR GALLEY L 2 MOP SILL WAS FOUND TO HAVE CORROSION. NEW MOP SILL WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002110500038 20021105 00038 NM 2002 11 5 F3LA200200376 1 20021002 A 5310 SILL BOEING 737 7373Q8 1384670 NM PAX DOORWAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 319FL 29024 3229 26301 DURING C 4 CHECK, THE R1 MOP SILL WAS FOUND TO HAVE CORROSION. REMOVED AND REPLACED TNE MOP SILL AT THE R 1 DOOR IAW SR M 51-40-08, SRM 51-40-05 AND BOEING DRAWING 65-45875. 2 L 7 2 4F RT A16WE 2002110500039 20021105 00039 NM 2002 11 5 F3LA200200378 1 20021030 A 3510 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 304FL 18961 3174 27633 DURING C 6 CHECK, INSPECTION FOUND CORROSION IN THE AFT CARGO PIT FLOOR SUPPORT ANGLE AT STATION 750 TO 754. REPAIR WA S PERFOMED BETWEEN STA 767 AND 787 AND FOUND TO BE WITHIN THE LIMITS ESTABLISHED IN SRM 53-60-15, FIGURE 101, DETAIL V. THE PART WAS TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH SOPM 20-41-02 2 L 7 2 4F RT A16WE 2002110500040 20021105 00040 NM 2002 11 5 F3LA200200379 1 20021030 A 5330 PANEL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 304FL 18962 3174 27633 DURING C 6 CHECK, INSPECTION FOUND CORROSION ON THE TRANSITION PANEL FROM STA 495 TO STA 500 AT STR 26R. CORROSION WAS REMOVED, IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-30-53, FIGURE 101, DETAIL V, BETWEEN STA 495 AND STA 500. AREA W AS TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH THE REQUIREMENTS OF SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002110500041 20021105 00041 NM 2002 11 5 CALA0200481 1 20021001 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 990 FROM LBL 14 TO LBL 45. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2002110500042 20021105 00042 WP 2002 11 5 CALA0200485 1 20021003 A 2612 FIRE DETECTOR DOUG DC9 DC982 3022082 WP CARGO BAY MALFUNCTIONED A CALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 72825 49485 THE MID CARGO DET "B" CARGO DETECTION AND SUPRESSION LIGHT ILLUMINATED WHILE AT CRUISE ENROUTE FROM IAH TO ORD. SHORTLY AFTERWARDS THE MASTER WARNING AND CARGO FIRE INDICATION AND FIRE HORN ACTIVATED. BOTH FIRE BOTTLES WERE DISCHARGED AND T HE AIRCRAFT WAS DIVERTED TO STL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ALL CARGO AREAS AND FOUND NO EVI DENCE OF FIRE OR ABNORMAL CONDITIONS. THE OVERHEAD FIRE SUPPRESSION PANEL WAS REMOVED AND REPLACED. OPERATIONAL CHECKS W ERE GOOD. BOTH FIRE BOTTLES WERE REPLACED. 2 L 7 2 4F A6WE 2002110500043 20021105 00043 NM 2002 11 5 CALA0200496 1 20021012 A 5320 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33608 27321 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT WEB UPPER FLANGE BETWEEN STA 344 AND 360, BL 0. THE FLOOR SUPPORT WEB W AS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2002110500044 20021105 00044 NM 2002 11 5 CALA0200499 1 20021017 A 2612 FIRE LOOP BOEING 737 737524 1384721 NM MLG WW MALFUNCTIONED A CALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 16617 27330 THE WHEEL WELL FIRE LIGHT ILLUMINATED AND THE FIRE WARNING BELL SOUNDED SHORTLY AFTER THE LANDING GEAR WAS RETRACTED ON TAKEOFF FROM IAH. THE WARNING WAS INTERMITTENT AT FIRST AND EVENTUALLY BECAME STEADY. THE AIRCRAFT WAS RETURNED TO IAH W HERE IT LANED WITHOUT INCIDENT. THERE WAS NO EVIDENCE OF FIRE. A CHECK OF THE WHEEL WELL FIRE LOOP FOUND IT FAULTY. THE NR 3 BRAKE WAS ALSO FOUND TO BE VERY HOT. THE WHEEL WELL FIRELOOP WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE G OOD. THE NR 3 BRAKE WAS ALSO REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 2002110500045 20021105 00045 2002 11 5 CALA0200501 4 20021017 A 2564 63800103 LIFE RAFT BOEING 737 737824 13844BZ NM AFT CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 73259 4336 30803 INSPECTION FOUND AFT MOST RAFT IN CEILING STOWAGE BOX HAD LOW PRESSURE. THE RAFT WAS REPLACED IAW MM 25-64-00. 2 L 7 2 4F RT A16WE 2002110500046 20021105 00046 NM 2002 11 5 CALA0200503 1 20021023 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39343 23581 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 328-344, LBL 11. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10 -02. 2 L 7 2 4F RT A16WE 2002110500047 20021105 00047 NM 2002 11 5 CALA0200505 1 20021024 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39343 23581 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 294-312, LBL 10. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10 -02. 2 L 7 2 4F RT A16WE 2002110500048 20021105 00048 NM 2002 11 5 CALA0200508 1 20021026 A 5310 BULKHEAD BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39343 23581 AFT PRESSURE BULKHEAD SKIN AT STA. 1016 UNDER RT STIFFENER CORRODED AT BL0. INSTALLED DOUBLER PER EA 5310-04045. 2 L 7 2 4F RT A16WE 2002110500049 20021105 00049 NM 2002 11 5 CALA0200514 1 20021029 A 5720 65C2630933 STIFFENER BOEING 737 7373T0 1384582 NM NR 3 FLAP TRACK WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39343 23581 HOCKEY STICK WORN IB EDGE OF NR 3 FLAP TRACK FAIRING. REPLACED HOCKEY STICK IB EDGE OF NR 3 FLAP TRACK FAIRING PER SRM 5 1-40-02. 2 L 7 2 4F RT A16WE 2002110500050 20021105 00050 NM 2002 11 5 CALA0200515 1 20021029 A 5720 69737595 ANGLE BOEING 737 7373T0 1384582 NM NR 3 FLAP TRACK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39343 23581 SUPPORT ANGLE CRACKED TWO PLACES FORWARD OF NR 3 FLAP TRACK FAIRING. REPLACED SUPPORT COLLAR ANGLE PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002110500051 20021105 00051 NM 2002 11 5 CALA0200517 1 20021031 A 5311 654653949 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39343 23581 BS FRAME 616 CRACKED LBL 65 WL 200 I/B CHORD BELOW CABIN FLOOR LINE. INSTALLED REPAIR FILLER AND ANGLE PER ECRA 5311-01 141. 2 L 7 2 4F RT A16WE 2002110500052 20021105 00052 NM 2002 11 5 CALA0200520 1 20021101 A 5310 STRUCTURE BOEING 737 737824 13844BZ NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12216 28776 FUSELAGE AND VHF ANTENNA DAMAGE ADJACENT TO FWD CARGO DOOR. REPAIRED PER ECRA 5330-03175. 2 L 7 2 4F RT A16WE 2002110500053 20021105 00053 NM 2002 11 5 CALA0200525 1 20021104 A 2612 FIRE WARNING BOEING 777 777224 1385225 NM CARGO BAY FALSE ACTIVATION A CALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 78005 27581 AFT CARGO FIRE LIGHT AND WARNING CAME ON 1:15 INTO FLIGHT. CHECKED DETECTORS AND HEATERS AND NO TROUBLE FOUND 2 L 7 2 4F RT T00001SE 2002110500054 20021105 00054 EU 2002 11 5 DHL2002365011 1 20021030 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 A/C DAMAGED AFT OF REAR LOWER CARGO DOOR. BETWEEN FR 64 & 65, STR 32 & STR 33. CUT OUT DAMAGED SECTION OF FUSELAGE SK IN REMOVED STR 32 AND 33 FABRICATED REPAIR FILLER AND DOUBLER LOCATED AND DRILLED REPLACEMENT STRINGERS INSTALLED STRING ERS AND REPAIR PARTS AS PER SRM 53-17-00. PERFORMED HFEC OF STR HOLES AND EDGE OF DAMAGE CUTOUT. PERFORMED HFEC OF OP EN HOLES STR 32433 AND EDGE OF CUT OUT IAW WTM 51-30-00. NO INDICATION. A/C DAMAGED AFT OF REAR LOWER CARGO DOOR BETW EEN FR64 AND 65 STG 32 AND 33. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR PER GMM 2.19. 2 L 7 2 4F RT A35EU 2002110500055 20021105 00055 NM 2002 11 5 DHL2002720501 1 20021007 A 5311 FRAME BOEING 727 727228 1384083 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING "C" CHECK, DISCREPANCY AS FOLLOWS, IN FWD. CARGO FRAME AT BS 640 AT STR 24 R HAS A DENT INTO THE RADIUS. REMOV ED PREVIOUS REPAIR IAW B-727 SRM 51-30-2. CUT-OUT DAMAGED AREA PIN 2 X 1 INCH AND FABBED DOUBLER. IAW B-727 SRM 53-10 -4 FIG.1 3) PART ALODINED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED REPAIR IAW B-727 SRM 53-10-4 FIG.1. 2 L 7 3 4F RT A3WE 2002110500056 20021105 00056 NM 2002 11 5 DHL2002720502 1 20021007 A 5311 FRAME BOEING 727 727228 1384083 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING "C" CHECK, AFT. CARGO FRAME BS 970 AT STR. 24 LT HAS A DENT INTO THE RADIUS. REMOVED PREVIOUS REPAIR AND CUT-OU T DAMAGED AREA DIM 2 1/2 X 1 INCH IAW SRM FAB. REPAIR DIM 18 X 2 1/2 INCH IAW SRM. PART ALODINED AND PRIMED IAW. IN STALL DOUBLER AFT. CARGO FRAME BS 970 AT STR. 24 LT IAW SRM. 2 L 7 3 4F RT A3WE 2002110500057 20021105 00057 NM 2002 11 5 DHL2002720503 1 20021012 A 5330 SKIN BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING "C" CHECK, FUSELAGE SKIN STATION 420, BUTTSPLICE BULGING SKIN AROUND FASTENERS. REMOVED FASTENERS IAW B-727 SRM 51-30-2 AND REPAIRED AREA DAMAGED SKIN, IAW SRM. 2 L 7 3 4F RT A3WE 2002110500058 20021105 00058 NM 2002 11 5 DHL2002720504 1 20021007 A 5313 STRINGER BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING "C" CHECK, AFT. CARGO STR. 18 LT HAS CORROSION FROM BS 1166 TO BS 1183. REMOVED DAMAGE STRINGER IAW B-727 SRM 51 -30-2 DIM. 12 INCH LONG. FABRICATED NEW STRINGER. 2 L 7 3 4F RT A3WE 2002110500059 20021105 00059 NM 2002 11 5 DHL2002720505 1 20021007 A 5311 FRAME BOEING 727 727228 1384083 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING "C" CHECK, AFT. CARGO FRAME BS 950 F AT STR 24 LT HAS DENTS INTO THE RADIUS. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500060 20021105 00060 NM 2002 11 5 DHL2002720506 1 20021013 A 5712 RIB BOEING 727 727228 1384083 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING "C" CHECK, RT WING INTERIOR RIB WS 686.5 BS 8 LOWER CHORD PREVIOUS REPAIR CRACK BEYOND STOP HOLE. REPAIRED IAW SR M. 2 L 7 3 4F RT A3WE 2002110500061 20021105 00061 NM 2002 11 5 DHL2002720507 1 20021013 A 5713 STRINGER BOEING 727 727228 1384083 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING "C" CHECK, RT WING INTERIOR WS 656.5 LWR. CHORD. PREVIOUS REPAIR ST-6 CRACKED. PASSING STOP HOLE. ALSO CRACK AT S T-8 LOCATION. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500062 20021105 00062 NM 2002 11 5 DHL2002720508 1 20021013 A 5712 RIB BOEING 727 727228 1384083 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING "C" CHECK, RT WING INTERIOR RIB W.S. 601 LWR. CHORD ST-6 CRACK. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500063 20021105 00063 NM 2002 11 5 DHL2002720509 1 20021013 A 5712 RIB BOEING 727 727228 1384083 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, RT WING INTERNAL RIB W.S. 629.0 LWR. CHORD BY ST-8 RIB CRACKED. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500064 20021105 00064 NM 2002 11 5 DHL2002720510 1 20021005 A 5330 SKIN BOEING 727 727228 1384083 NM FUSELAGE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK DISCREPANCY AS FOLLOWS, GOUGE IN FUSELAGE SKIN AT B.S. 670, ABOVE STR 26R. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500065 20021105 00065 NM 2002 11 5 DHL2002720511 1 20021010 A 5330 LAP JOINT BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, FUSELAGE LONGITUDINAL LAP JOINT STR 4 RIGHT , BS 1070 CRACK INDICATION AROUND FASTENERS. REPAIRED IAW SR M. 2 L 7 3 4F RT A3WE 2002110500066 20021105 00066 NM 2002 11 5 DHL2002720512 1 20021007 A 5311 FRAME BOEING 727 727228 1384083 NM FUSELAGE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING "C" CHECK, CABIN AREA, FRAME AT STA. 760 IS CHAFED THRU ABOVE ABOVE STR 4 RT. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500067 20021105 00067 NM 2002 11 5 DHL2002720513 1 20021005 A 5330 SKIN BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING "C" CHECK, CORROSION ON FUSELAGE SKIN AT B.S. 357-360 STR 22L. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500068 20021105 00068 NM 2002 11 5 DHL2002720514 1 20021007 A 5311 FRAME BOEING 727 727228 1384083 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING "C CHECK", AFT. CARGO FRAME BS 950E AT STR 25 LT HAS A DENT INTO THE RADIUS. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500069 20021105 00069 NM 2002 11 5 DHL2002720515 1 20021017 A 5347 SEAT TRACK BOEING 727 727228 1384083 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING "C" CHECK, MAIN CABIN SEAT TRACK DAMAGED BS 480 TO 560 LBL 45.5. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500070 20021105 00070 NM 2002 11 5 DHL2002720516 1 20021022 A 5347 SEAT TRACK BOEING 727 727228 1384083 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, MAIN CABIN SEAT TRACK DAMAGED LBL 62.5 BS 620. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500071 20021105 00071 NM 2002 11 5 DHL2002720517 1 20021005 A 5753 SKIN BOEING 727 727228 1384083 NM TE FLAPS DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, RT WING OUT FLAP. AFT SECTION SHOWS DELAMINATION AREA TOP SIDE WBL 440 APPROX. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500072 20021105 00072 NM 2002 11 5 DHL2002720518 1 20021012 A 5320 FASTENER BOEING 727 727228 1384083 NM FUSELAGE DAMAGED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, DISHED FASTENERS AT BS 360 BUTT SPLICE STR 19L. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500073 20021105 00073 NM 2002 11 5 DHL2002720519 1 20021014 A 5312 STIFFENER BOEING 727 727228 1384083 NM BULKHEAD CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, FUSELAGE. AFT. PRESSURE BULKHEAD BS 1183 VERTICAL BEAM RBBL 24.6 CRACKED FROM LIGHTNING HOLE WL 260 APPR OX. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500074 20021105 00074 NM 2002 11 5 DHL2002720520 1 20021011 A 5720 STRUCTURE BOEING 727 727228 1384083 NM RT MLG WW CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, T/E FALSE SPAR UPPER BEAM IS CORRODED AFT. OF RT MLG AFT. TRUNNION. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500075 20021105 00075 NM 2002 11 5 DHL2002720522 1 20021014 A 5312 STIFFENER BOEING 727 727228 1384083 NM BULKHEAD CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, FUSELAGE. AFT. PRESSURE BULKHEAD, BS 1183 VERTICAL BEAM LBBL 36.2 CRACK INDICATION. WL 249. REPAIRED IA W SRM. 2 L 7 3 4F RT A3WE 2002110500076 20021105 00076 NM 2002 11 5 DHL2002720523 1 20021009 A 5340 FITTING BOEING 727 727228 1384083 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, UT INSPECTION CRACK INDICATION B.S. 870 RT FITTING JUST ABOVE STR. 10 RT. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500077 20021105 00077 NM 2002 11 5 DHL2002720524 1 20021014 A 5312 STIFFENER BOEING 727 727228 1384083 NM BULKHEAD CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, FUSELAGE AFT. PRESSURE BULKHEAD BS 1183 VERTICAL BEAM LBBL 24.6 CRACKED FROM LIGHTNING HOLE IN 2 PLACES WL 260. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500078 20021105 00078 NM 2002 11 5 DHL2002720525 1 20021012 A 5330 SKIN BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, LOWER FUSELAGE SKIN AT BS 350 TO 360 LBL 13 TO RBL 13 BULGING AROUND FASTENER HEADS. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500079 20021105 00079 NM 2002 11 5 DHL2002720526 1 20021007 A 5312 PRESSURE PANEL BOEING 727 727228 1384083 NM RT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, RT MLG WW BULKHEAD BS 870 HAS A CRACK APU LOAD CONTROL VALVE. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500080 20021105 00080 NM 2002 11 5 DHL2002720527 1 20021014 A 5330 SKIN BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, BULGED SKIN/DISHED FASTENER HEADS ALONG STR 8 L, BS 1330. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500081 20021105 00081 NM 2002 11 5 DHL2002720528 1 20021014 A 5711 SPAR BOEING 727 727228 1384083 NM LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, LT WING FWD. SPAR UPPER CHORD IS CORRODED AT WS 130 UPPER SURFACE AT BULGED SEALANT. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500082 20021105 00082 NM 2002 11 5 DHL2002720529 1 20021006 A 5720 STIFFENER BOEING 727 727228 1384083 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, VERTICAL STIFFENER IS CRACKED ON LEFT WING FRONT SPAR, LOWER END. LWS 130. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500083 20021105 00083 NM 2002 11 5 DHL2002720530 1 20021014 A 5730 SKIN BOEING 727 727228 1384083 NM LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, LT WING UPPER SURFACE STRAP BULGED ABOVE FRONT SPAR AFT. OF NR 3 SLAT. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500084 20021105 00084 NM 2002 11 5 DHL2002720531 1 20021011 A 5330 SKIN BOEING 727 727228 1384083 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 DURING C CHECK, RT LWR NOSE HAS AREAS OF BULGING SKIN AND DISHED FASTENERS STA. 294 TO 360. REPAIRED IAW SRM. 2 L 7 3 4F RT A3WE 2002110500085 20021105 00085 NM 2002 11 5 DHL2002726004 1 20021001 A 3010 32146451 VALVE BOEING 727 727228 1384083 NM WING ANTI ICE FAILED A DHLA C D O ABORTED TAKEOFF RETURN TO BLOCK OTHER J WARNING INDICATION TO TAKEOFF 1 SO 01 726DH 20409 ANTI-ICE DUCT OVERHEAT LIGHT ILLUMINATED AT TAKE-OFF. APPEARS TO BE NR 3 ENGINE. REMOVED & REPLACED NR 3 WING ANTI-ICE VALVE. OPS CHECKED IAW B727 M/M 30-11-31. OPS CHECKED GOOD. REJECTED TAKE-OFF! TAKE-OFF WEIGHT - 144,000 LBS, AIRSPEE D - 40 KNOTS, TEMPERATURE - 27 DEGREES C, PRESSURE ALTITUDE - 500 FT. ANTI-ICE DUCT OVERHEAT LIGHT ILLUMINATED UPON TAKE -OFF. REVERSE THRUST USED. ACCOMPLISHED REJECTED TAKE-OFF INSPECTION IAW B727 M/M 05-51-121. NO DEFECTS NOTED. 2 L 7 3 4F RT A3WE 2002110500086 20021105 00086 NM 2002 11 5 DHL2002726005 1 20021016 A 2612 FIRE WARNING BOEING 727 727228 1384083 NM APU BAY MALFUNCTIONED A DHLA F D ACTIVATE FIRE EXT. RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 726DH 20409 AFTER APU SHUT DOWN FIRE WARNING ILLUMINATED WITH NO BELL. BELL WOULD NOT TEST. DISCHARGED BOTTLE EMERGENCY PROCEDURE. DEFERRED PER MEL 49-1 CAT. "C" PLACARD 10665 INSTALLED. MAINTENANCE WAS NOTIFIED. REF. DMI #10665 - AFTER APU SHUTDOWN FIRE WARNING LIGHT ILLUMINATED NO BELLS. BELL WOULD NOT TEST. BLEW BOTTLE PER EMERGENCY PROCEDURES. REPLACED MUSHROOM ED INDICATOR LAMP AND CLEANED DETECTOR CONNECTION. OPS NORMAL 3 TIMES SUSPECT MOISTURE. DMI CONTINUES DUE TO FIRE BOTTLE . DISCHARGED BOTTLE DURING EMERGENCY PROCEDURES. BOTTLE WAS DEFERRED AND APU ALSO WAS DEFERRED ON 10-16-02. INSTALLED NEW APU FIRE BOTTLE IAW B-MM 26-23-01. THIS CLEARS DMI 49-1 CONTROL 10665. PLACARDS REMOVED. 2 L 7 3 4F RT A3WE 2002110500087 20021105 00087 NM 2002 11 5 DHL2002741014 1 20020928 A 3260 CONNECTOR BOEING 727 7272Q9 138448M NM MLG MODULE RACK DIRTY A DHLA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 741DH 21931 GEAR GREEN LIGHTS AND RED LIGHTS ILLUMINATED, RAN ABNORMAL PROCEDURES RED LIGHTS EVENTUALLY WENT OUT ON FINAL. STATES EM ERGENCY WAS DECLARED. CLEANED AND RESECURED LANDING GEAR ELECTRONIC MODULE RACK CONNECTOR. REINSTALLED LANDING GEAR EL ECTRONIC MODULE AND TESTED IAW M/M 32-09-121. NO DEFECTS NOTED. 2 L 7 3 4F RT A3WE 2002110500088 20021105 00088 NM 2002 11 5 DHL2002742009 1 20021011 A 3040 WINDSHIELD WIPER BOEING 727 727225 1384077 NM WINDSCREEN FAILED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 742DH 21290 F/O WINDSCREEN WIPER STUCK IN MIDDLE OF WINDSCREEN. WHEN WIPER ACTIVATED IT DOES NOT MOVE. ADJUSTED WIPER PER M/M 30-43 OPS NORMAL. 2 L 7 3 4F A3WE 2002110500089 20021105 00089 NM 2002 11 5 DHL2002745010 1 20021005 A 2697 CONNECTOR BOEING 727 727224 1384076 NM NR 1 FIRE WARN DIRTY A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 745DH 20665 NR 1 ENGINE FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. REPOSITIONED & CLEANED CONNECTOR PLUG. OPS CHECK ED GOOD IAW M/M 26-11-00. 2 L 7 3 4F A3WE 2002110500090 20021105 00090 NM 2002 11 5 DHL2002745011 1 20021015 A 2610 DETECTOR BOEING 727 727224 1384076 NM NR 1 ENGINE SHORTED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 745DH 20665 NR 1 ENGINE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. EXTINGUISHES AT 10,000 FT AND DIMMER WITH THRUST AT IDL E. DEFERRED NR 1 GROUND DETECTOR PER MEL REF. 26-9-1, PLACARD INSTALLED CONTROL 10655. WORKING DMI 10655 - NR 1 ENG INE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. EXTINGUISHES AT 10,000 FT AND DIMMER WITH THRUST AT IDLE. FOU ND DETECTOR TOUCHING GROUND IN 2 PLACES. REPOSITIONED DETECTOR. CHECKS OKAY PER M/M 26-11-01. THIS CLEARS DMI 10655. 2 L 7 3 4F A3WE 2002110500091 20021105 00091 NM 2002 11 5 CALA0200527 1 20021104 A 5300 6545769 SKIN BOEING 737 7373T0 1384582 NM A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 39343 23581 FUSELAGE SKIN CRACKED AT AFT SCREW HOLE LOWER FUSELAGE CENTER LINE STA 380 AT EXHAUST OUTLET. INSTALLED DOUBLER IAW ECR A 5330-02894 2 L 7 2 4F RT A16WE 2002110500092 20021105 00092 NM 2002 11 5 A6WA200230018 1 20020907 A 5320 SILL DORNER DO32 DO328100 2996000 NM FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 SURFACE CORROSION FOUND ON CARGO DOOR SILL AT ATTACH HOLES FOR SCUFF PLATE. MAINTENANCE REMOVED SURFACE CORROSION ON CA RGO DOOR SILL, CORROSION WAS FOUND TO BE OUT OF LIMITS IAW DO 328 SRM 53-51-65. FABRICATED REPAIR DOUBLERS AND INSTALLE D AT CARGO DOOR SILL ATTACH HOLES IAW DER NR HHC-02-326. (M) 2 H 7 2 4T RT A45NM 2002110500093 20021105 00093 NM 2002 11 5 A6WA200230019 1 20020907 A 5712 RIB DORNER DO32 DO328100 2996000 NM LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 LEFT WING LEADING EDGE 512AL HAS A .25 INCH RIB CRACKED ON FLANGE AT TWO PLACES. DAMAGE LOCATED ON 2ND RIB INBOARD. MA INTENANCE REMOVED DAMAGED AREA FROM LEFT LEADING EDGE 512AL RIB. FABRICATED REPAIR PARTS AND INSTALLED REF DO 328 SRM 5 1-27-0 AND REPAIR PROCEDURE HHC-02-325. (M) 2 H 7 2 4T RT A45NM 2002110500094 20021105 00094 NM 2002 11 5 A6WA200230023 1 20020908 A 5320 FLOOR SUPPORT DORNER DO32 DO328100 2996000 NM FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 CENTER AISLE FLOOR SUPPORT BEAM AT FRAME 16 CRACKED AT CENTER SCREW HOLE. MAINTENANCE REMOVED DAMAGED AREA AT FRAME 16. FABRICATED REPAIR PARTS AND INSTALLED REF DO328 SRM 53-00-50 CHANNEL REPAIR. (M) 2 H 7 2 4T RT A45NM 2002110500095 20021105 00095 NM 2002 11 5 A6WA200230024 1 20020908 A 5320 FLOOR SUPPORT DORNER DO32 DO328100 2996000 NM FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 CENTER AISLE FLOOR SUPPORT ROOM AT FRAME 17 CRACKED AT CENTER SCREW HOLE. MAINTENANCE REMOVED DAMAGED AREA AT FRAME 17. FABRICATED REPAIR PARTS AND INSTALLED REF DO328 SRM 53-00-50 CHANNERL REPAIR. (M) 2 H 7 2 4T RT A45NM 2002110500096 20021105 00096 NM 2002 11 5 A6WA200230025 1 20020908 A 5320 FLOOR SUPPORT DORNER DO32 DO328100 2996000 NM FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 CENTER AISLE FLOOR SUPPORT BEAM AT FRAME 18 CRACKED AT CENTER HOLE. MAINTENANCE REMOVED DAMAGED AREA AT FRAME 18. FABR ICATED REPAIR PARTS AND INSTALLED REF DO328 SRM 53-00-50 CHANNEL REPAIR. (M) 2 H 7 2 4T RT A45NM 2002110500097 20021105 00097 NM 2002 11 5 A6WA200230027 1 20020910 A 5320 CAP DORNER DO32 DO328100 2996000 NM FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 ROW 1DF SEAT BOTH HAVE CRACKED INBOARD ATTACH CAPS. MAINTENANCE REMOVED AND REPLACED ROW 1 DF INBOARD ATTACH CAPS RED D O328 SRM 51-43-20. (M 2 H 7 2 4T RT A45NM 2002110500098 20021105 00098 NM 2002 11 5 A6WA200230028 1 20020910 A 5320 FLOOR SUPPORT DORNER DO32 DO328100 2996000 NM FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 341PH 3065 FLOOR SUPPORT BEAM AT FRAME 36 RIGHT SIDE OUTBOARD FLANGE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED CORROSION DAMAGE AT FRAME 36. FABRICATED REPAIR PARTS AND INSTALLED RED DO328 SRM 53-00-50 FLANGE REPAIR. (M) 2 H 7 2 4T RT A45NM 2002110500099 20021105 00099 NM 2002 11 5 A6WA200230034 1 20020920 A 5320 CHANNEL DORNER DO32 DO328100 2996000 NM FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 328MX 3071 CENTER AISLE FLOOR CHANNEL .28 INCH CRACK AT CENTER SCREW LOCATION ON FRAME 17. MAINTENANCE REMOVED DAMAGED AREA. FABR ICATED REPAIR PARTS AND INSTALLED REF DO328 SRM 53-00-50 AT FRAME 17. (M) 2 H 7 2 4T RT A45NM 2002110500100 20021105 00100 EA 2002 11 5 A6WA200240027 1 20020929 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A A6WA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 31 412AW 7582 FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN, SMELLED LIKE ELECTRICAL OR MECHANICAL SOURCE. SMOKE CLEARED AFTER FOLLOWI NG QRH PROCEDURES. MAINTENANCE GROUND RAN BOTH ENGINES, OPERATED PACKS AND INSPECTED GALLEY HEATER AND FAN FOR CORRECT OPERATION. NO DEFECTS NOTED AT THIS TIME. A/C OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4F RT A21EA 2002110500101 20021105 00101 NM 2002 11 5 ASAA0210181 1 20020824 A 3350 8731002142 SIGN BOEING 737 737298C 1384490 NM CABIN MALFUNCTIONED A ASAA K NONE O OTHER DE DESCENT 1 NM 01 745AS 20794 KTN - FOUND EMERGENCY IDENTIFIER ON SMOKE BARRIER ILLUMINATED DURING DESCENT. RESET EXIT IDENTIFIER, THEN SIGN TESTED N ORMAL. (M) 2 L 7 2 4F RT A16WE 2002110500102 20021105 00102 WP 2002 11 5 ASAA0280275 1 20020821 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTING INOPERATIVE IN 1ST CLASS CABIN. REPLACED A LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002110500103 20021105 00103 WP 2002 11 5 ASAA0280278 1 20020825 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 16727 1708 53063 PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT ON AND WILL NOT TURN OFF. REPLACED PORTABLE LIGHT ASSEMBLY. LI GHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002110500104 20021105 00104 NM 2002 11 5 ASAA0280279 1 20020826 A 3350 1001191 LIGHT DOUG MD80 MD83 3023681 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 981AS 42953 7539 53472 SEA - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED PORTABLE LIGHT ASSEMBLY. LIGHT THEN OPER ATED NORMALLY. (M) 2 L 7 2 4F RT 2002110500105 20021105 00105 WP 2002 11 5 ASAA0280280 1 20020826 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 7. RECONNECTED DISCONNEC TED LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002110500106 20021105 00106 WP 2002 11 5 ASAA0280324 1 20020923 A 5313 5920319 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - C-CHECK, FOUND MID ACCESSORY COMPARTMENT LONGERON SECTION CORRODED. REPLACED LONGERON SECTION FROM STATION 550 TO 585. INSTALLED NEW SPLICE AT EACH END PER SRM 53-02, PAGE 37. (M) 2 L 7 2 4F A6WE 2002110500107 20021105 00107 WP 2002 11 5 ASAA0280325 1 20020923 A 5311 991960373 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME AND SPLICE CORRODED AT STATION 1309 FROM LONGERON 29L TO 29R. INSTALLE D NEW SECTION PER SRM 53-03, PAGE 4A. (M) 2 L 7 2 4F A6WE 2002110500108 20021105 00108 WP 2002 11 5 ASAA0280326 1 20020923 A 5753 5930479502 SKIN DOUG DC9 DC982 3022082 WP T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - C-CHECK, FOUND RIGHT WING INBOARD FLAP LOWER SURFACE HAS TWO DENTS. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PE R SRM 57-01, PAGE 15 AND 51-30-2, PAGE 4. (M) 2 L 7 2 4F A6WE 2002110500109 20021105 00109 WP 2002 11 5 ASAA0280328 1 20020924 A 5310 5936038501 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - C-CHECK, FOUND AFT CARGO COMPARTMENT LOWER DOOR BEAM VERTICAL FACE IS CORRODED. INSTALLED BEAM DOUBLER AND SPACER EPR SRM 53-05, PAGE 173-179F. (M) 2 L 7 2 4F A6WE 2002110500110 20021105 00110 WP 2002 11 5 ASAA0280329 1 20020925 A 5320 5912494501N PAN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - C-CHECK, FOUND FORWARD CARGO COMPARTMENT DOOR CUTOUT PAN VERTICAL AND HORIZONTAL LEGS ARE CORRODED FROM STATION 37 0 TO 427 IN LINE WITH LONGERON 28R. REMOVED CORROSION AND REPAIRED BY SRM 53-05 FIG 44 AND 51-30-2, PAGE 1-4. (M) 2 L 7 2 4F A6WE 2002110500111 20021105 00111 WP 2002 11 5 ASAA0280332 1 20020927 A 5310 993657813 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - C-CHECK, FOUND AFT CARGO BAY SHEAR TIE WAS FOUND DAMAGED ON FORWARD LOWER LEG STATION 1136 BETWEEN LONGERON 29R AN D 30. REPLACED SHEAR TIE WITH NEWLY FABRICATED ONE PER SRM 53-03, PAGE 4M. (M) 2 L 7 2 4F A6WE 2002110500112 20021105 00112 WP 2002 11 5 ASAA0280334 1 20020928 A 5311 993607331 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - 30K CHECK, AFT CARGO FRAME CORRODED BEYOND LIMITS AT STATION 1174. REPLACED FRAME AT STATION 1174 LONGERON 28R-27 L PER SRM 51-30-5 AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002110500113 20021105 00113 SO 2002 11 5 ASOA02249 1 20020427 A 1420 MS22759 SPLICE EMB 120 EMB120RT 3260202 SO CABIN DAMAGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 232AS 120036 FLT 4382 - DURING A GROUND INSPECTION IN ATL, THE FIRST FOUR FLOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINT ENANCE FOUND AND REPAIRED A BAD SPLICE ON THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2002110500115 20021105 00115 SO 2002 11 5 SIMA200227906 1 20020910 A 5320 14521725001 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 THIS IS A LEVEL 2 FINDING. GALLEY AREA LEFT SILL HAS CORROSION. PERFORMED NDT INSPECTION WITH NO DEFECTS NOTED. INSTA LLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002110500116 20021105 00116 SO 2002 11 5 SIMA200227907 1 20020910 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 THIS IS A LEVEL 2 FINDING, GALLEY AREA FORWARD DIAMOND GUSSET HAS CORROSION. INSTALLED SERVICEABLE GUSSET IAW EMB 145 S RM 51-40-02, 51-40-06, 51-20-03. (M) 2 L 7 2 4T RT T00011AT 2002110500117 20021105 00117 SO 2002 11 5 SIMA200227908 1 20020910 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA RIGHT AFT SILL HAS CORROSION. INSTALLED SERVICEABLE RIGHT SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002110500118 20021105 00118 SO 2002 11 5 SIMA200227909 1 20020910 A 5320 14529603003 CROSSBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA AFT CROSSBEAM AND PROFILER HAS CORROSION. INSTALLED SERVICEABLE AFT CROSSB EAM AND PROFILE IAW EMB145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002110500119 20021105 00119 SO 2002 11 5 SIMA200227910 1 20020910 A 5320 14522459003 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA RAMP SUPPORT HAS CORROSION. INSTALLED SERVICEABLE RAMP SUPPORT IN GALLEY I AW EMB SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002110500120 20021105 00120 SO 2002 11 5 SIMA200227911 1 20020911 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA CENTER BEAM HAS CORROSION. INSTALLED REPAIR DOUBLER AND FILLER IAW EMB GST -1736/02C AND ETN EM 53-034R1. (M) 2 L 7 2 4T RT T00011AT 2002110500121 20021105 00121 SO 2002 11 5 SIMA200227912 1 20020910 A 5320 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 ABI - THIS IS A LEVEL 2 FINDING, GALLEY ARE AFT DIAMOND GUSSET HAS CORROSION. INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002110500122 20021105 00122 SO 2002 11 5 SIMA200227913 1 20020910 A 5320 145217252013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA RIGHT FORWARD SILL HAS CORROSION. INSTALLED SERVICEABLE SILL IAW EMB 145 S RM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002110500123 20021105 00123 SO 2002 11 5 SIMA200227914 1 20020920 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 ABI - DURNG AN IMBV INSPECTION, THE GALLEY AREA FORWARD DIGITAL WAS FOUND TO BE CORRODED. FABRICATED A SHIM AND TWO DOU BLERS. REPAIRED IAW EMB-145 SRM 145/1142, 53-21-10, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002110500124 20021105 00124 SO 2002 11 5 SIMA200227915 1 20020919 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 ABI - DURING IMBV INSPECTION, MAINTENANCE FOUND CORROSION ON GALLEY CENTER FLOOR BEAM. CUT OUT SECTION GALLEY CENTER BE AM. FABRICATED A U-BEAM DOUBLER, FILLER. REPAIR DONE IAE EMB-145 SRM 145/1142, CHAPTER 51, REV 19, 51-40-02, ENB GST-1 736/02-C ETN EM-53-034 R1, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002110500125 20021105 00125 SO 2002 11 5 LR7A02113 1 20021104 A 5330 RISER LKHEED 382 382G 526414U SO FS600 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 596 4606 DURING SCHEDULED B1 INSPECTION PER HB0506 FOUND LH MLG BAY SKINS CRACKED. FS600, LBL61, WL170.REPLACED PANEL IAW SRM SM P 583-53-40-02, DWG. 342403, AND 51-70. NR0050. 2 H 7 4 4T A1SO 2002110500126 20021105 00126 SO 2002 11 5 LR7A02114 1 20021104 A 5330 PANEL LKHEED 382 382G 526414U SO FS617 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 596 4606 DURING SCHEDULED B1 INSPECTION PER HB0506 FOUND LH MLG BAY AFT LOWER WALL CORRODED. FS617, LBL68, WL160.REPLACED PANEL IAW SRM SMP 583-53-40-02, DWG. 339149, AND 51-70. NR0069. 2 H 7 4 4T A1SO 2002110500127 20021105 00127 SO 2002 11 5 LR7A02115 1 20021104 A 5312 RISER LKHEED 382 382G 526414U SO FS477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 596 4606 DURING SCHEDULED B1 INSPECTION PER HB0506 FOUND LH MLG BAY FWD BULKHEAD PANEL RISERS CRACKED. FS477, LBL61, WL187 AND W L192. REPAIRED PANEL RISERS IAW SRM SMP 583-53-40-10, AND 51-70. NR0075. 2 H 7 4 4T A1SO 2002110500128 20021105 00128 SO 2002 11 5 LR7A02116 1 20021104 A 5312 RISER LKHEED 382 382G 526414U SO FS477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 596 4606 DURING SCHEDULED B1 INSPECTION PER HB0506 FOUND RH MLG BAY FWD BULKHEAD PANEL RISER CRACKED. FS477, RBL61, WL180.REPAIR ED PANEL RISER IAW SRM SMP 583-53-40-10, AND 51-70. NR0080. 2 H 7 4 4T A1SO 2002110500129 20021105 00129 SO 2002 11 5 SIMA200227916 1 20020911 A 5510 14524977003 PIN EMB 145 EMB145LR 3260212 SO HORIZ STAB CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 THIS A LEVEL 2 FINDING, HORIZONTAL STABILIZER PINS ARE CORRODED. REMOVED AND REPLACED PINS IAW EMB 145 AMM 55-10-00. ( M) 2 L 7 2 4T RT T00011AT 2002110500130 20021105 00130 SO 2002 11 5 SIMA200227919 1 20020913 A 5347 14530659001 SEAT TRACK EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 ABI - THIS IS A LEVEL 2 FINDING, INBOARD SEAT TRACK FOR SEAT 1A-4A WERE FOUND TO BE CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB 145 AMM 53-01-06. (M) 2 L 7 2 4T RT T00011AT 2002110500131 20021105 00131 NM 2002 11 5 USAA020369 1 20020927 A 5750 STRUCTURE BOEING 737 737301 1384611 NM WING CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND TRAILING EDGE HAS CHAFE, 59 INCHES INBOARD FROM INBOARD END. BURNISHED/BLENDED AND INSTALLED WEAR PAD PER T YPICAL REPAIR 57-50-17. (M) 2 L 7 2 4F RT A16WE 2003022800056 20030228 00056 EA 2003 2 28 HNAA0200072 1 20021102 A 6123 82410401001 POTENTIOMETER DHAV DHC8 DHC8311 1386006 EA COCKPIT DEFECTIVE A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 284BC 23327 23327 336 AUTO FEATHER WOULD NOT ARM, ABORTED TAKEOFF. REMOVED AND REPLACED NUMBER TWO POWER LEVER POTENTIOMETER, OPERATIONAL CHE CK GOOD. 2 H 7 2 4T RT A13NM 2002110500133 20021105 00133 NM 2002 11 5 HNAA0200073 1 20021103 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8201 2809001 NM BAG BAY DIRTY A HNAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 07 988HA 26430 6452 426 SMOKE WARNING LIGHT ILLUMINATED TWICE IN FLIGHT. CHECKED FOR SIGNS OF SMOKE, NONE NOTICED. REMOVED DETECTOR CONNECTORS , CLEANED AND REINSTALLED. TESTED OK. 2 H 7 2 4T RT A13NM 2002110500134 20021105 00134 EU 2002 11 5 MALA020592 1 20020919 A 5523 TRIM TAB BAC 146 AVRO146RJ85A 1500097 EU ELEVATOR DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 501XJ E2208 DURING C-CHECK IN CVG, A/C 501 SUSTAINED DAMAGE TO THE RT ELEVATOR TRIM TAB TRAILING EDGE. MAINTENANCE REPAIRED DAMAGE IAW MAL EO NR A55020. 2 H 7 4 4F RT A49EU 2002110500135 20021105 00135 EU 2002 11 5 MALA020594 1 20021002 A 2897 50017000001 WIRE HARNESS SAAB SF340 SF340A 7850100 EU FUEL PROBE PEELING A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 27XJ 340A027 SEVERAL WIRES IN THE LEFT WING FUEL CELL HAVE THE OUTER LAYER PEELING AT STA WJ183.21, BETWEEN FUEL PANELS 523BT AND 523 CT. MAINTENANCE REPLACED LEFT OUTBOARD FUEL PROBE HARNESS. LEFT FUEL INDICATING SYSTEM OPS TESTS AND CAPACITANCE TEST GOOD IAW SAAB 340 AMM. 2 L 7 2 4T RT A52EU 2002110500136 20021105 00136 NE 2002 11 5 MALA020595 3 20021003 A 6140 M83536224L RELAY SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A1 30030 NE ROTOL R389 R3894123F26 NE WARNING SYS FAILED A MALA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 15 48XJ DURING FLIGHT NR 2937, ON TAKEOFF, AUTO COARSEN WOULD NOT ARM. RETURNED TO GATE. MAINTENANCE FERRIED AIRCRAFT TO MSP F OR REPAIR DUE TO AUTO COARSEN LIGHT NOT ARMING DURING TAKEOFF. MAINTENANCE REPLACED RELAY 44KA IAW SAAB AMM 72-00-00. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P30NE 2002110500137 20021105 00137 EU 2002 11 5 MALA020596 1 20021004 A 3610 7063250 PERISEAL BAC 146 AVRO146RJ85A 1500097 EU NR 4 PYLON WORN A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 518XJ E2337 DURING FLIGHT NR 3522 RT ZONE HIGH TEMP LIGHT ILLUMINATED DURING FLIGHT. WING AND TAIL ANTI-ICE WAS ON. AIR RETURN TO MSP. MAINTENANCE FOUND WORN OUT NR 4 PYLON AFT OF HEAT EXCHANGER PERISEALS. REPLACED SEALS. LEAK CHECK GOOD REFER AMM 36-11-00. 2 H 7 4 4F RT A49EU 2002110500138 20021105 00138 EU 2002 11 5 02305320 1 20021101 A 3350 1317 LAMP JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 320UE 41043 During preflight inspection, the crew reported that the fwd. cabin emergency exit light was inoperative. Maintenance pe rsonnelremoved and replaced the lamp in the forward cabin emergency exit light. An operational check was satisfactory a nd the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002122000030 20021220 00030 NM 2002 12 20 QXEA0201824 1 20021102 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8401 1390041 NM NR 2 FAULTY A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 404QX 8 8 4046 RDD - CREW RETURNED TO FIELD WHEN AFTER TAKEOFF THE GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPL ACED THE NUMBER 2 WEIGHT ON WHEELS HARNESS. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETUR NED TO SERVICE. 2 H 7 2 4T RT A13NM 2002110500139 20021105 00139 EA 2002 11 5 COMA0260624 1 20021101 A 3240 50105201 BRAKE ASSY CNDAIR CL600 CL6002B19 1900309 EA L/H MLG WORN A COMA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 708CA 7604 7235 FLIGHT 6047 DURING T/O FULL RT RUDDER COULD NOT COMPENSATE FOR AIRCRAFT PULLING LEFT.REPLACED THE L/H OUTBD BRAKE ASSY. 2 L 7 2 4F RT A21EA 2002110500140 20021105 00140 NE 2002 11 5 COMA0260625 2 20021030 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT FAILED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 940CA 14315 7048 807421 FLIGHT 5546 LEFT ENGINE OIL PRESSURE WARNING MESSAGE.REPLACED THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002110500141 20021105 00141 EA 2002 11 5 COMA0260627 1 20021101 A 2750 1267587 PDU CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 940CA 14225 7048 FLIGHT 9493 FLAPS FAILED WHEN SELECTED TO 8 DEGREES.REPLACED THE PDU. 2 L 7 2 4F RT A21EA 2002110500142 20021105 00142 EA 2002 11 5 COMA0260626 1 20021101 A 3020 300013000003 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA R/H INOPERATIVE A COMA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 01 821CA 23238 7420 FLIGHT 5294 R/H COWL ANTI ICE INOP.REPLACED THE COWL ANTI-ICE VALVE. 2 L 7 2 4F RT A21EA 2002110500143 20021105 00143 SO 2002 11 5 C2XA02BT069 1 20021101 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 11547 145563 EWR---CO3495, "ON THE OUTSIDE OF AIRCRAFT AFT EMERGENCY EXIT LIGHTS #1 AND #2 WERE INOPERATIVE. AIRCRAFT PREVIOUSLY RELE ASED IAW MEL #33-50-00 CATEGORY "C" CONTROL NUMBER 032880.....MAINTENANCE REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER IN THE #4 POSITION. AND REPAIRED WIRING. OPS. CHECKED GOOD. IAW EMB145 AMM CHAPTER #20 AND 33-50-04. MEL ITEM CL EARED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002110500144 20021105 00144 NM 2002 11 5 AWXA200201073 1 20021017 A 5320 141N517048 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR SUPPORT HAT CHANNEL BS 375, LBL 55 . MAINTENANCE BLENDED CORROSION AND FOUND MATERIAL LOSS BEYOND LIMITS; REMOVED DAMAGED FLOOR SUPPORT AT BS 375, LBL 55; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; AND INSTALLED REPAIR PART IAW DWG 141N5170, AND B757-200 SRM 51-40-01, PG. 3 . 2 L 7 2 4F RT A2NM 2002110500145 20021105 00145 NM 2002 11 5 AWXA200201074 1 20021016 A 5320 141N518624 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON CABIN GALLEY FLOOR SUPPORT BS 400, RBL 53. MAINTENANCE REM OVED DAMAGED FLOOR SUPPORT AT BS 400, RBL 53; FABRICATED A NEW REPLACEMENT GALLEY FLOOR SUPPORT; AND INSTALLED REPAIR PA RT IAW DWG 141N5186, AND B757-200 SRM 51-40-02, PG. 4. 2 L 7 2 4F RT A2NM 2002110500146 20021105 00146 NM 2002 11 5 AWXA200201077 1 20021016 A 5320 146N832213 WEB BOEING 757 7572S7 1384962 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 0 0 23568 LCQ - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON WEB IN MAIN CABIN BS 1375, RBL 69. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED WEB AT BS 1375, RBL 69; FABRICATED A NEW REPLACEMENT WEB; AND INSTALLED REPAIR PART IAW DWG 146N8322, AND B757-200 SRM 51-40-02, PG. 3-5. 2 L 7 2 4F RT A2NM 2002110500147 20021105 00147 NM 2002 11 5 AWXA200201079 1 20021017 A 5320 141N518617 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-08 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE AND BASE OF FLOOR SUPPORT ANGL E AT BS 365.5, RBL 50. MAINTENANCE REMOVED NUTPLATES AND BLENDED CORROSION; REMOVED GALLEY SUPPORT ANGLE, AND HAT CHANNE L SUPPORT ANGLE BENEATH GALLEY SUPPORT ANGLE AT BS 365.5, RBL 5, FOR FURTHER INSPECTION; MATERIAL LOSS WITHIN LIMITS ON GALLEY SUPPORT ANGLE; MATERIAL LOSS OUT OF LIMITS ON HAT CHANNEL SUPPORT ANGLE; FABRICATED A NEW REPLACEMENT HAT CHANNEL SUPPORT ANGLE PER DWG 141N5186; AND INSTALLED REPAIR PART AND GALLEY SUPPORT ANGLE IAW B757-200 SRM 51-40-02, PG. 16-17 . 2 L 7 2 4F RT A2NM 2002110500148 20021105 00148 NM 2002 11 5 AWXA200201080 1 20021024 A 5320 284N1038117 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-08 CHECK 1 1/2" CRACK WAS FOUND ON FLOOR SUPPORT OF MAIN EQUIPMENT CENTER COMPARTMENT AT B S 460, BETWEEN STR 24 & 26R. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT AT BS 460 BETWEEN STR 24 & 26R; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; AND INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG. 3-4. 2 L 7 2 4F RT A2NM 2002110500149 20021105 00149 NM 2002 11 5 AWXA200201081 1 20021016 A 5320 141N516081 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON CABIN FLOOR SUPPORT AT BS 330, RBL 11 TO RBL 39. MAINTENAN CE REMOVED DAMAGED FLOOR SUPPORT AT BS 330 FROM BL O TO RBL 24; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 141N5 160; AND INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG. 4, 16-17, 39-40. 2 L 7 2 4F RT A2NM 2002110500150 20021105 00150 SO 2002 11 5 SIMA200228 1 20020921 A 5313 12010732001 FRAME EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 STRINGER 19L HAS CORROSION BETWEEN FRAMES 23 AND 24 UNDER FLOOR. PERFORMED EDDY CURRENT AND THICKNESS, NO DEFECTS. REP AIR DONE IAW GST. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500151 20021105 00151 SO 2002 11 5 SIMA200228205 1 20020921 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 RIGHT HAND SILL IS CORRODED BETWEEN FRAME 29 AND 35. PERFORMED NDT INSPECTION WITH NO DEFECTS NOTED. REPAIRED RIGHT HA ND SILL BETWEEN FR 29-35 IAW GST. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500152 20021105 00152 SO 2002 11 5 SIMA200228206 1 20020920 A 5315 14568505006 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 LEFT HAND FLOOR BEAM GUSSET IS CORRODED BETWEEN FRAME 65-68. INSTALLED SERVICEABLE GUSSET IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500153 20021105 00153 SO 2002 11 5 SIMA200228207 1 20021001 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 DURING AN IMBV INSPECTION, CORROSION WAS FOUND ON THE GALLEY CENTER FLOORBEAM. REMOVED CORRODED GALLEY CENTER FLOORBEAM INSTALLED NEW BEAM IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500154 20021105 00154 SO 2002 11 5 SIMA200228208 1 20020928 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 DURING AN IMBV INSPECTION FOUND STRINGER 19L CHAFED. BLENDED CHAFE. PERFORMED AND NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500155 20021105 00155 SO 2002 11 5 SIMA200228209 1 20020919 A 5320 14524131009 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 PASSENGER DOOR FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500156 20021105 00156 SO 2002 11 5 SIMA200228210 1 20020919 A 5320 14529150001 CROSSBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 CROSSMEMBER AT FRAME 23 IS CORRODED. REMOVED CROSSMEMBER AND REPAIRED IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500157 20021105 00157 SO 2002 11 5 SIMA200228211 1 20020919 A 5347 14530659011 SEAT TRACK EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 SEAT TRACK CORRODED BETWEEN FRAMES 18 AND 23 ON LEFT FLOORBEAM. REMOVED AND REPLACED SEAT TRACK IAW AMM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500158 20021105 00158 SO 2002 11 5 SIMA200228212 1 20020919 A 5320 14529150003 ANGLE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 PROFILE AT FRAME 23 IS CORRODED. REMOVED AND REPAIRED PROFILE AND DOUBLER. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500159 20021105 00159 SO 2002 11 5 SIMA200228213 1 20020919 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 RIGHT FLOORBEAM CORRODED AT FRAME 23. REPAIRED IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500160 20021105 00160 SO 2002 11 5 SIMA200228214 1 20020920 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 CARGO DOOR SILL IS CORRODED. REMOVED AND INSTALLED NEW CARGO DOOR SILL IAW CPM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500161 20021105 00161 SO 2002 11 5 SIMA200228215 1 20020919 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 PREVIOUS REPAIR AT FRAME 20 ON LEFT FLOORBEAM IS CORRODED. REPAIRED IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500162 20021105 00162 SO 2002 11 5 SIMA200228216 1 20020927 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 DURING AN IMBV INSPECTION THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 23. BLENDED THE DAMAG ED AREA TO COMPLETELY REMOVED THE CORROSION. FABRICATED A U SHAPED DOUBLER. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500163 20021105 00163 SO 2002 11 5 SIMA200228217 1 20021002 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 DURING A IMBV INSPECTION LEFT HAND BEAM AT FRAME 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT SECTION OF DAMAG ED BEAM. FABRICATED A FILLER, TWO SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500164 20021105 00164 SO 2002 11 5 SIMA200228218 1 20020924 A 5311 12010732001 FRAME EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 DURING A IMBV INSPECTION FOUND LOWER FRAME 81 CHAFED BEYOND SRM LIMITS. REMOVED EXISTING LOWER FRAME 81. INSTALLED NEW FRAME IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500165 20021105 00165 SO 2002 11 5 SIMA200228220 1 20020930 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 DURING AN IMBV INSPECTION, THE DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED SECTION OF THE FORWA RD DIGITAL BY CUT OUT. FABRICATED A REPLACEMENT STRAP AND TWO DOUBLERS, SHIMS. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500166 20021105 00166 SO 2002 11 5 SIMA200228221 1 20020919 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 CENTER BEAM RAMP IS CORRODED. REMOVED AND INSTALLED NEW CENTER BEAM GUSSET IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500167 20021105 00167 SO 2002 11 5 SIMA200228222 1 20020929 A 5320 DOUBLER EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 DURING AN IMBV INSPECTION CORROSION WAS FOUND ON A PREVIOUS REPAIR TO THE LEFT HAND OMEGA BEAM AT FRAME 20. REMOVED PRE VIOUS REPAIR AND INSPECTION THE UNDERLYING BEAM. NO ADDITIONAL DAMAGE NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS, PLATE. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500168 20021105 00168 SO 2002 11 5 SIMA200228223 1 20020928 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 DURING AN IMBV INSPECTION OF AIRCRAFT, CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM AT FRAME 29. REMOVED CORROSION B Y CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500169 20021105 00169 SO 2002 11 5 SIMA200228224 1 20021002 A 5320 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 DURING AN MBV INSPECTION, CORROSION WAS FOUND ON SERVICE DOOR CENTER SILL THAT WAS BEYOND SRM LIMITS. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE BLENDED AREAS. NO DEFECTS NOTED. FABRICATED THREE REPAIR DOUBLERS. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500170 20021105 00170 SO 2002 11 5 SIMA200228225 1 20020921 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 RIGHT SILL CORRODED BETWEEN FRAME 24 AND 29. PERFORMED EDDY CURRENT AND THICKNESS INSPECTION WITH NO DEFECTS FOUND. RE PLACED SILL IAW GST. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500171 20021105 00171 SO 2002 11 5 SIMA200228226 1 20020925 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 145130 DURING AN IMBV INSPECTION OF AIRCRAFT, THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CO RRODED SILL. INSTALLED SERVICEABLE SILL IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500172 20021105 00172 SO 2002 11 5 SIMA200229401 1 20021017 A 4990 DRAIN LINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL APU LOOSE A SIMA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 652RS 145432 AFTER TAKE OFF CREW REPORTED THE LAVATORY SMOKE WARNING CAME ON FOR 5 MINUTES. FLIGHT ATTENDANT ALSO REPORTED AN MIST I N THE AIR WITH A BURNING SMELL. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO FIELD WITH NO FURTHER INCIDENTS REPO RTED. CONTRACT MAINTENANCE ISOLATED SMELL TO APU. MAINTENANCE FOUND A LOOSE OIL DRAIN LINE WAS TIGHTENED AND AN OPERAT IONAL CHECK WAS COMPLIED WITH. AIRCRAFT WAS THEN RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002110500173 20021105 00173 SO 2002 11 5 SIMA200229402 1 20021016 A 5610 163500109 WINDSHIELD EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 715AE 145262 CREW REPORTED THE CAPTAINS WINDSHIELD SHATTERED IN FLIGHT. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE REM OVED AND REPLACED THE CAPTAINS WINDSHIELD IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002110600001 20021106 00001 SO 2002 11 6 C2XA02SH122 1 20021105 A 5400 14576560011 RIB EMB 145 EMB145LR 3260212 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29917 145414 SHV- DURING C CHECK LEFT HAND LOWER COWLING WAS FOUND TO HAVE A GOUGE INSIDE INBOARD OF ACCESS TO AIR STARTER VALVE. MA INTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002110600002 20021106 00002 WP 2002 11 6 ABXA020281 1 20021022 A 5300 991555047 INTERCOSTAL DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 CORRODED AND CRACKED INTERCOSTAL BETWEEN STA. 1056 - 1072, BELOW THE LEFT GILLINER FLOOR SUPPORT. REPLACED INTERCOSTAL I AW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002110600003 20021106 00003 NM 2002 11 6 DHL2002745012 1 20021029 A 3260 SWITCH BOEING 727 727224 1384076 NM RT NLG DOOR OUT OF ADJUST A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 745DH 20665 NOSE GEAR DOORS LIGHT ILLUMINATED IN FLIGHT. ADJUSTED RT NOSE GEAR DOOR SWITCH IAW DHL B727 M/M 32-62-11. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2002110600004 20021106 00004 NE 2002 11 6 DHL2002746008 2 20021031 A 7530 658385001 BLEED VALVE BOEING 727 727224 1384076 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE MALFUNCTIONED A DHLA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 01 746DH 22252 700152 NR 3 ENGINE COMPRESSOR. REJECTED TAKEOFF. WOULD NOT MAKE T/O THRUST AND WAS COMPRESSOR STALLING. REPLACED NR 3 ENGINE PRBC VALVE PER M/M 75 -30-1. GROUND RAN PER DHL JRH SATISFACTORY. WT. 127.7, IAS 60 KTS, 15 DEGREES OAT, 1150 PRESS AL T. 2 L 7 3 4F 4 F A3WE E2EA 2002110600005 20021106 00005 NM 2002 11 6 DHL2002750005 1 20021003 A 3040 WINDSHIELD WIPER BOEING 727 7272M7 138407S NM RIGHT FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750DH 21951 RT WINDSHIELD WIPER INOPERATIVE EXCEPT PARK. ADJUSTED RT WINDSHIELD WIPER TENSION IAW B-M/M 30-42-01. OPS CHECKED NORM AL. 2 L 7 3 4F A3WE 2002110600006 20021106 00006 NM 2002 11 6 DHL2002755007 1 20021011 A 3040 WINDSHIELD WIPER BOEING 727 727225 1384077 NM FIRST OFFICER'S STUCK A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 755DH 21857 F/O'S WIPER STUCK MID WINDOW. ADJUSTED TENSION ON F/O'S WIPER. OPS CHECKED NORMAL PER M/M 30-42-01. 2 L 7 3 4F A3WE 2002110600007 20021106 00007 NM 2002 11 6 DHL2002755008 1 20021031 A 2612 FIRE WARNING BOEING 727 727225 1384077 NM ENGINE WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 755DH 21857 WHEN TESTING FIRE WARNING SYSTEM, SWITCH TO RIGHT NR 2 & 3 ENGINE FIRE WARNING CAPSULES DO NOT LIGHT. PERFORMED OPS CH ECK OF ENGINE FIRE WARNING SYSTEM IAW B727 M/M 26-11-01. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2002110600008 20021106 00008 WP 2002 11 6 DHL2002802011 1 20021024 A 2611 SMOKE DETECTOR DOUG DC8 DC873 302199C WP NR 5 WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802DH 46076 NR 5 MAIN CABIN SMOKE DETECTOR FAILED TO TEST. RELAMPED NR 5 MAIN CABIN SMOKE DETECTOR OPS CHECKED OK IAW M/M 26-10-0 . 2 L 7 4 4F RT 4A25 2002110600009 20021106 00009 WP 2002 11 6 DHL2002803500 1 20020926 A 5753 SUPPORT BRACKET DOUG DC8 DC873 302199C WP RT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT INBOARD FLAP CANOE FITTING LWR SUPPORT ANGLE AT STA. 97.000 WITH CRACK IN IT.R&R SUPPORT ANGLE PER M/M 27-51-12 PG 20 1-204, SRM51-3-1 PG A. 2 L 7 4 4F RT 4A25 2002110600010 20021106 00010 WP 2002 11 6 DHL2002803501 1 20020926 A 5751 STRUCTURE DOUG DC8 DC873 302199C WP LT WING AILERON DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING OUTBOARD AILERON TRAILING EDGE, SHOWS 3 DENTS (1/2 IN) BETWEEN XRS 624.000 AND XRS 693.000. REMOVED DAMAGED O /B AILERON T/E PER SRM 51-1-21 PG 1.FABRICATED NEW T/E (2024T3AL 0.030) PER SRM 57-8-1 PG 8.CLEANED TERATED AND PRIMED P ER SRM 51-1-8B.INSTALLED NEW T/E PER SRM 51-1-21 PG 1-3. 2 L 7 4 4F RT 4A25 2002110600011 20021106 00011 WP 2002 11 6 DHL2002803502 1 20020924 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING OUTBOARD L/E FRAME AT STA XRS 585.000 WITH 1/2 IN CRACK IN IT. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABR ICATED REINFOCING ANGLE (2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLE D ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002110600012 20021106 00012 WP 2002 11 6 DHL2002803503 1 20020927 A 5754 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT WING L/E FRAME UPPER PART AT STA 620.000, WITH 1/2 IN CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRIL LED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLES IAW SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW ANGLEA AND FASTNERS PERSRM 57-2-0 PG 9-10,51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002110600013 20021106 00013 WP 2002 11 6 DHL2002803504 1 20020927 A 5754 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT WING L/E FRAME UPPER PART AT STA 661.000 WITH 1/2 IN CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLE D CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLES PER IAW SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B .INSTALLED ANGLES WITH NEW FASTNERS PER SRM57-2-0 PG 9-10, 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002110600014 20021106 00014 WP 2002 11 6 DHL2002803505 1 20020929 A 5754 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT WING L/E UPPER PART FRAME CRACKED 1/2 IN AT STA 649.000. REMOVED FASTNERS PER SRM 51-121 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL 0.32) PER SRM 57-2-0 PG 9-10,51-1-21 PG 1. CLEANED TREATED AND PRIMED PER SRM 51-18B.INSTALLED ANGLE WITH NEW FASTNERS PER SRM 57-2-0 PG 9-10,51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002110600015 20021106 00015 WP 2002 11 6 DHL2002803507 1 20020926 A 5312 STIFFENER DOUG DC8 DC873 302199C WP BULKHEAD CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AFT CARGO COMPARTMENT LT PRESSURE WALL VERTICAL STIFFENER CRACKED 1 IN AT STA 1540.00. STOP DRILLED CRACK PER SRM 53-2- 0 FIG 1F. FABRICATED DOUBLER (2024.T3AL 0.050)PER SRM 53-2-0 FIG 1B.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLE D DOUBLER PER SRM 51-1-21 PG 1 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002110600016 20021106 00016 WP 2002 11 6 DHL2002803508 1 20020926 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING O/B L/E FRAME AT STA XRS 641.250 WITH 1/2 IN CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CR ACK PER SRM 57-2-0 PG9-10. FABRICATED SUPPORT ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED ,TREATED AND PRIM ED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10, AND 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002110600017 20021106 00017 WP 2002 11 6 DHL2002803509 1 20020925 A 5280 CLIP DOUG DC8 DC873 302199C WP RT MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT MLG DOOR REINFORCING CLIP LOWER PORTION CRACKED 1/2 INCH STA 902.000. REMOVED CRACKED CLIP PER SRM 51-1-21 PG 1. F ABRICATED NEW CLIP (STEEL 301 1/4 H 0.032)PER SRM53-2-0 FIG 1F. INSTALLED NEW CLIP PER SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002110600018 20021106 00018 WP 2002 11 6 DHL2002803510 1 20020926 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING CENTER L/E INTERNAL PART SHOWS FRAME CRACKED 1 INCH AT XFS 447.350. REMOVED FASTNERS PER SRM 51-1-20 D PG 21.ST OP DRILLED CRACKED FRAME XFS 447.750 PER SRM 57-2-0 PG 9-10.FABRICATED DOUBLER ANGLE (2024 T3 ALO 032")PER SRM 57-20 PG 9-10.CLEANED,TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED DOUBLER ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-20 PG 9. 2 L 7 4 4F RT 4A25 2002110600019 20021106 00019 WP 2002 11 6 DHL2002803511 1 20020926 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING CENTER L/E INTERNAL PART SHOWS FRAME WITH 2 EA CRACKS 3/4 INCH AT XFS 454.000. STOP DRILLED CRACK PER SRM57-2- 0 PG 9-10. FABRICATED DOUBLER ANGLE (2024 T3 AL0.040) PER SRM 57-2-0 PG 9-10.CLEANED TERATED AND PRIMED PER SRM 51-1-8B . INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10. 2 L 7 4 4F RT 4A25 2002110600020 20021106 00020 WP 2002 11 6 DHL2002803512 1 20020926 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING CENTER L/E INTERNAL PART SHOWS FRAME CRACKED 1 INCH AT XFS 385.250. REMOVED FASTNERS PER SRM 51-1-20D PG 21. S TOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED NEW DOUBLER ANGLE (2024T3AL0.032)PER SRM 57-2-0 PG 9-10.CLEANED TR EATED NAD PRIMED IAW SRM. INSTALLED DOUBLER ANGLE PER SRM. 2 L 7 4 4F RT 4A25 2002110600021 20021106 00021 WP 2002 11 6 DHL2002803513 1 20020926 A 5753 SKIN DOUG DC8 DC873 302199C WP RT WING TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT WING O/B FLAP UPPER SKIN CRACKED 1/2 INCH AT XW 212. PREFORMED MAJOR REPAIR PER SRM 57-1-0 PG 1. REMOVED DAMAGED SK IN PER SRM 51-1-21 PG 7. FABRICATED NEW SKIN (2024.T3.AL 0.40) PER SRM57-7-1 PG 2. CLEANED TREATED AND PRIMED PER SRM 5 1-1-8B.INSTALLED NEW SKIN PER SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002110600022 20021106 00022 WP 2002 11 6 DHL2002803514 1 20020926 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING O/B L/E FRAME AT STA XRS 622.500 WITH 1/2 INCH CRACK. STOP DRILLED CRACK PER SRM 57-1-0 PG 9-10. FABRICATED R EINFOCING ANGLE (2024 T3 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFOCI NG ANGLE PER SRM 57-2-0 PG 9-10. 2 L 7 4 4F RT 4A25 2002110600023 20021106 00023 WP 2002 11 6 DHL2002803515 1 20020926 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING O/B L/E FRAME AT STA XRS 672.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS PER SRM 57-2-0 PG 9-10. FABRICATE D SUPPORT ANGLE (2024 T3 AL0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE WITH NEW FASTNERS PER SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002110600024 20021106 00024 WP 2002 11 6 DHL2002803516 1 20020927 A 5720 DOUBLER DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING CENTER L/E INNER DOUBLER AT STA XFS 435.000 WITH 2 INCH CRACK IN IT. REMOVED DAMAGED DOUBLER PER SRM 51-1-21 PG 1. FABRICATED NEW DOUBLER (7075.T6 AL0.080) PER SRM57-2-0 FIG 2. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALL ED DOUBLER PER SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002110600025 20021106 00025 WP 2002 11 6 DHL2002803517 1 20020926 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING O/B L/E FRAME AT STA XRS 610.000 WITH 1/2 INCH. REMOVED FASTNERS PER SRM 51-1-21 PG 9-10. FABRICATED SUPPORT A NGLE (21024 T3 AL0.032) PER SRM 57-2-0 PG 9-10. CLEANED TERATED AND PRIMED PER SRM 51-1-8B. INSTALLED SUPPORT ANGLE W ITH NEW FASTNERS PER SRM 57-2-0 PG9-10 AND 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002110600026 20021106 00026 WP 2002 11 6 DHL2002803518 1 20020924 A 5720 PAN DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT WING L/E PAN UPPER PART CRACKED 2 INCH, XFS 327.000. REMOVED ZEE PAN PER SRM 51 1 20D.CLEANED TREATED AND PRIMED AR EA PER SRM 51-1-8B.INSTALLED NEW ZEE PAN FITTING PER SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002110600027 20021106 00027 WP 2002 11 6 DHL2002803519 1 20020925 A 5320 CLIP DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AFT ACCESSORY BAY, FRAME JOINT CLIP ATTACHED TO FUSELAGE CRACKED 2 INCH, STA 640.000 L-26 AND L-27R. REMOVED FASTENER S PER SRM 51-1-20D PG 21. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1B. FABRICATED REINFORCING ANGLE (2024T3AL0.050) PER S RM 53-2-0 FIG 1B. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 53-2-0 FIG 1B AND 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002110600028 20021106 00028 WP 2002 11 6 DHL2002803520 1 20020924 A 5240 SKIN DOUG DC8 DC873 302199C WP SERVICE DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FUSELAGE EXTERIOR RT FWD SERVICE DOOR FWD UPPER CORNER CRACKED 1/4 INCH AT STA 160.000. PERFORMED MAJOR REPAIR PER SRM 53-2-0 PG 87-88 FIG 14. CUT OUT DAMAGED AREA PER SRM 53-2-0 PG 87-88 FIG 14. FABRICATED FILLER (7075T60.063) PER SRM 5 3-2-0 PG 87-88 FIG 14. CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED FILLER AND DOUBLER PER SRM 53-2-0 PG 87-88 FIG 14. 2 L 7 4 4F RT 4A25 2002110600029 20021106 00029 WP 2002 11 6 DHL2002803521 1 20020926 A 5320 SUPPORT DOUG DC8 DC873 302199C WP CARGO BAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AFT CARGO BAY PRESSURE WALL VERTICAL LINING SUPPORT CRACKED 1/2 INCH AT STA 980.000 L-27H. STOP DRILLED CRACK PER SRM 5 3-2-0 FIG 7B. FABRICATED DOUBLER (2024 T3 AL0.040) PER SRM 53-2-0 FIG 7B. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 53-2-0 FIG1B AND 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002110600030 20021106 00030 WP 2002 11 6 DHL2002803523 1 20020927 A 5754 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT WING L/E FRAME PART AT STA 607.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CR ACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AN D PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002110600031 20021106 00031 WP 2002 11 6 DHL2002803524 1 20020927 A 5754 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT WING L/E FRAME UPPER PART AT STA 649.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNESS PER SRM 51-1-21 PG 1. STOP DRI LLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATE D AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM57-2-0 PG 9-10 AND SRM 51-1-21-PG 1. 2 L 7 4 4F RT 4A25 2002110600032 20021106 00032 WP 2002 11 6 DHL2002803525 1 20020929 A 5754 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT WING L/E FRAME UPPER PART AT STA 680.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DR ILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREA TED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM57-2-0 PG 9-10 AND SRM 51-1-21-PG 1. 2 L 7 4 4F RT 4A25 2002110600033 20021106 00033 WP 2002 11 6 DHL2002803526 1 20020927 A 5754 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT WING L/E FRAME LOWER PART AT STA 643.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRI LLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREAT ED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM57-2-0 PG 9-10 AND SRM 51-1-21-PG 1. 2 L 7 4 4F RT 4A25 2002110600034 20021106 00034 WP 2002 11 6 DHL2002803527 1 20020926 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING O/B L/E FRAME UPPER PART AT STA 635.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TR EATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM57-2-0 PG 9-10 AND SRM 51-1-21-PG 1. 2 L 7 4 4F RT 4A25 2002110600035 20021106 00035 WP 2002 11 6 DHL2002803528 1 20020926 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING O/B L/E FRAME UPPER PART AT STA XRS 591.250 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1.ST OP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10.CLEANED TR EATED AND PRIMED PER SRM 51-1-8B.INSTALLED REINFOCING ANGLE PER SRM57-2-0 PG 9-10 AND SRM 51-1-21-PG 1. 2 L 7 4 4F RT 4A25 2002110600036 20021106 00036 WP 2002 11 6 DHL2002803529 1 20020926 A 5720 DOUBLER DOUG DC8 DC873 302199C WP LT WING BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING CENTER L/E INTERNAL PART SHOWS DOUBLER BROKEN (2IN) AT XFS 521.250. REMOVED DAMAGED DOUBLER PER SRM 57-2-0 FIG 2. FABRICATED NEW DOUBLER (7075T6AL0.050) PER SRM 57-2-0. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLE R PER SRM 57-2-0 AND 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2002110600037 20021106 00037 WP 2002 11 6 DHL2002803530 1 20020927 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING CENTRAL L/E FRAME CRACKED AT STA XFS 471.000. REMOVED FASTNERS PER SRM 51-1-20 PG 21. STOP DRILLED CRACK PER SR M 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024 T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10 AND 51-1-20 PG 9. 2 L 7 4 4F RT 4A25 2002110600038 20021106 00038 EA 2002 11 6 02305705 1 20021101 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 705BR 7470 During preflight inspection, the crew reported that the l/h aft overwing emergency exit light was inoperative. Maintena nce personnel removed and replaced the lamp in the l/h aft overwing emergency exit light. An operational check was sati sfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002110600039 20021106 00039 EU 2002 11 6 02306327 1 20021102 A 3350 3022471 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 327UE 41080 During overnight maintenance, it was discovered that the r/h fwd. exterior emergency exit light was inoperative. Mainte nance personnel removed and replaced the r/h fwd. exterior emergency exit light assembly. An operational check was sati sfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002110600040 20021106 00040 EA 2002 11 6 02309621 1 20021105 A 3350 110049 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 621BR 7186 During overnight maintenance, it was discovered that the emergency exit lights would not extinguish. Maintenance person nel removed and replaced the #2 emergency exit light power supply. An operational check was satisfactory and the aircra ft was returned to service. 2 L 7 2 4F RT A21EA 2002110600041 20021106 00041 WP 2002 11 6 DHL2002803531 1 20020927 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING CENTRAL L/E FRAME CRACKED 1 INCH AT STA XFS 422.000. REMOVED FASTNERS PER SRM 51-1-20D PG 21. STOP DRILLED 1 I NCH CRACK PER SRM 57-20 PG 9-10.FABRICATED A DOUBLER ANGLE (2024T3AL0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10 AND 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002110600042 20021106 00042 NM 2002 11 6 02308422 1 20021104 A 2612 335000121 FIRE BOTTLE DORNER DO32 DO328300 NM A VTZA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 EA 27 422FJ 3180 During climb, the crew reported a fire warning in the r/h engine. both r/h engine fire bottles were deployed, and the a ircraft returned to CLT and landed without further incident. Maintenance personnel removed and replaced the r/h engine fire wire jumper and both fire extinguisher bottles. Operational checks were satisfactory and the aircraft was returned to service. 2 H 7 2 4T RT A55NM 2002110600043 20021106 00043 NM 2002 11 6 0203576613 1 20021023 A 2420 MODULE BOEING 747 747251B 1384892 NM GENERATOR SYS MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 613US 20358 DURING FLIGHT, AN ELECTRICAL ODOR EMITTED AND THE NR 1 FIELD OFF AND GEN OPEN LIGHT ILLUMINATED. DISCONNECTED THE NR 1 CSD AND THE BURNING SMELL DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE CSD OIL TEMPERATURE INDICATOR AND GENERATOR ASSEMBLY MODULE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002110600044 20021106 00044 EU 2002 11 6 MALA020590 1 20021001 A 2140 13051002 HEATER SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 435XJ 340B435 AFTER GETTING AIRBORNE ON FLIGHT NR 3321, GEAR WAS IN TRANSIT. FA REPORTED SMELLING AND SEEING SMOKE UNDER SEAT 2D COM ING OUT FLOOR VENT. SUPPLEMENTAL AIR WAS NOT ON AT TIME. DECLARED EMERGENCY, COMPLETED QRH LANDED NORMALLY. AIR RETUR N TO DTW. MAINTENANCE FOUND SMELL COMING FROM UNDER CENTER AISLE FLOOR BOARDS. INSPECTED WIRING AND COMPONENTS UNDER F LOOR BOARD FOUND STRONG ELECTRICAL SMELL FROM AUX AIR COMP MOTOR AND MOTOR INOP GRAND RAN A/C AND OPERATED ALL SYSTEMS, NO EFFECTS NOTED EXCEPT AUX AIR COND. MAINTENANCE REMOVED AND REPLACED FWD AUX HEATER. REPLACED AFT AUX HEATER. REPLA CED MID AUX HEATER PN 1305100-2 IAW AUXILIARY ELECTRICAL HEATING SYSTEM. 2 L 7 2 4T RT A52EU 2002110600045 20021106 00045 WP 2002 11 6 MWEA020669 1 20021106 A 5313 29207531 LONGERON DOUG DC9 DC932 3022066 WP STA 598 TOOL DAMAGE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 STATION 598 T ANGLE AT LONGERON 17 LEFT HAS TWO DRILL STARTS JX6. -- REMOVED T ANGLE, BLENDED OUT TOOLING DAMAGE, FABR ICATED AND INSTALLED NEW T ANGLE. 2 L 7 2 4F A6WE 2002110600046 20021106 00046 NM 2002 11 6 UPS02239825 1 20021025 A 3350 LIGHT BOEING 727 727180C 138406G NM CABIN NOT SEATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS ABOVE CABIN ENTRY DOOR ARE VERY DIM. CHARGED BATTERY FOR 3 HRS, RESEATED LIG HT ASSY, GROUND CHECK GOOD. 2 L 7 3 4F A3WE 2002110600047 20021106 00047 NM 2002 11 6 UPS02439846 1 20021031 A 3397 WIRE BOEING 747 747200 1384847 NM COCKPIT BROKEN A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:PFLT FOUND F/O EMERGENCY LIGHT INOP ON GLARESHIELD. R/R BULB NO HELP. FOUND WIRE W2032-WHT/BLU BROKEN. REPAIRED IAW WDM 33-13-11. OPS CHECK OKAY. 2 L 7 4 4F RT A20WE 2002110600048 20021106 00048 NM 2002 11 6 UPS02439851 1 20021102 A 3350 BATTERY PACK BOEING 747 747123 1384873 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A EMERGENCY LIGHT INOP, UPPER DECK ABOVE SUPERNUMERARY SEATS LT SIDE. REPLACED BATTERY PACK OPS CK OK . 2 L 7 4 4F A20WE 2002110600049 20021106 00049 NM 2002 11 6 UPS02439852 1 20021103 A 3350 LENS BOEING 747 747123 1384873 NM CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A EMERGENCY LIGHT LENS CRACKED ON FWD LIGHT AT UPPER DECK CREW SERVICE DOOR. REPLACED LENS ASSY LIGHT OPS CK OK. 2 L 7 4 4F A20WE 2002110600050 20021106 00050 WP 2002 11 6 DHL2002803532 1 20020926 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING O/B L/E FRAME AT STA XRS 616.250 WITH A 1/2 INCH CRACK IN IT. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRIC ATED REINFORCING ANGLE (2024-T3 AL 0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002110600051 20021106 00051 WP 2002 11 6 DHL2002803533 1 20020926 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING O/B L/E FRAME AT STA XRS 660.000 WITH A 1 IN CRACK IN IT. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024T3 AL0.032) PER SRM 57-2-0 PG 9-10. CLEAND TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG9-10 AND 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002110600052 20021106 00052 WP 2002 11 6 DHL2002803534 1 20020926 A 5754 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LT WING O/B L/E FRAME AT STA XRS 603.750 WITH A 1/2 IN CRACK IN IT. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICA TED REINFORCING ANGLE (2024T3 AL0.032) PER SRM 57-2-0 PG 9-10. CLEAND TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED A NGLE PER SRM 57-2-0 PG9-10 AND 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2002110600053 20021106 00053 NE 2002 11 6 MALA020600 2 20021008 A 7321 ECU SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE MALFUNCTIONED A MALA K NONE J WARNING INDICATION CR CRUISE 1 GL 15 423XJ 340B423 DURING FLIGHT NR 3158, LEFT ENGINE TORQUE SURGE INFLIGHT FOR 2-3 SECONDS. AN UNCOMMANDED POWER INCREASE ON LEFT ENGINE WITH ENGINE ICE OFF DESCENT CHECK COMPLETE POWER SET AT 80-85 PERCENT. INCREASED TO 120 PERCENT FOR 2-3 SECONDS, THEN RE TURNED TO SET PWR TEMP ON ENGINE 900 PLUS NO ENGINE OVERTEMP LIGHT. ON ROLLOUT RETURN AT 60 KIAS POWER LEVERS ABOVE GRO UND IDLE PROP RPM WENT TO 1350 FOR 2-3 SECONDS. TEMP WENT UP AND DOWN 830 DEGREES TO 910 DEGREES. LANDED WITHOUT INCID ENT. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE DECU ALL CHECKS GOOD FDR DOWNLOAD SHOWED LEFT ENGINE DID NOT EXCEED L IMITS IAW GE MAINTENANCE MANUAL 72-00-00. 2 L 7 2 4T 4 T RT A52EU E8NE 2002110600054 20021106 00054 WP 2002 11 6 DHL2002804011 1 20021024 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 1 ENGINE MALFUNCTIONED A DHLA E D ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 804DH 46124 NR 1 FIRE HANDLE AND BELL ILLUMINATED AND SOUNDED APPROXIMATELY 3 MINUTES. AFTER ENGINE SHUTDOWN COMPLIED WITH ENGINE FIRE CHECKLIST. NO INDICATION OF FIRE. BOTTLE NOT FIRED. ENGINE VISUALLY INSPECTED BY MAINTENANCE DURING OCCURRENCE. FOUND PYLON FIRE DETECTOR "B" LOOP AT FAULT. ITEM TRANSFERS TO DMI 10753 PER MEL 26-2-3 CAT. "C". ENGINE VISUALLY INS PECTED BY MAINTENANCE DURING OCCURRENCE. CLEANED AND INSPECTED ALL NR 1 ENGINE FIRE LOOPS. SYSTEM CHECKED GOOD IAW M/M 26-10-1. THIS CLEARS DMI 10753. PLACARD REMOVED. 2 L 7 4 4F RT 4A25 2002110600055 20021106 00055 NM 2002 11 6 DHL2002727011 1 20021104 A 2611 302313 SMOKE DETECTOR BOEING 727 727228 1384083 NM A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 727DH 20204 1) #2 L/H MAIN CABIN SMOKE DETECTOR IS INOP. 2) REMOVED AND REPLACED #1, L/H MAIN CARGO SMOKE DETECTOR IAW. B-727 M/M 26-17-0. 2 L 7 3 4F RT A3WE 2002110600056 20021106 00056 EU 2002 11 6 MALA020601 1 20021010 A 2910 HYDRAULIC LINE SAAB SF340 SF340A 7850100 EU HYD SYSTEM RUPTURED A MALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 15 46XJ 340A046 DURING FLIGHT NR 2782, MAIN HYDRAULIC QUANTITY AND PRESSURE INDICATED ZERO INFLIGHT. MAINTENANCE FOUND A RUPTURED HYDRA ULIC LINE ON POST FLIGHT INSPECTION. REPLACED LEFT GEAR DOWN HYDRAULIC FLEX LINE AND SEPARATION BOLTS. 2 L 7 2 4T RT A52EU 2002110600057 20021106 00057 WP 2002 11 6 DHL2002805053 1 20021024 A 2150 CURRENT LIMITER DOUG DC8 DC873F 302199F WP LT A/C PACK FAILED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 805DH 46125 AFTER LANDING WITH LEFT PACK ON, LEFT TEMPERATURE ROSE RAPIDLY AND BURNING ODOR FILLED COCKPIT. FOUND PHASE 1 (F1-1) C URRENT LIMITER BLOWN. REMOVED AND REPLACED. OPERATED PACK FOR MORE THAN 10 MINUTES, NO FAULT FOUND. SYSTEM OPS CHECKED NORMAL IAW M/M 21-55-00. 2 L 7 4 4F RT 4A25 2002110600058 20021106 00058 WP 2002 11 6 DHL2002873001 1 20021101 A 3350 5708458503 BATTERY DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 873SJ 46091 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY RACK ASSEMBLY. OPS CHECKS OK IAW M/M 33-50 -2. 2 L 7 4 4F RT 4A25 2002110600059 20021106 00059 EU 2002 11 6 MALA020602 1 20021006 A 5260 AIRSTAIR SAAB SF340 340B 7860101 EU PAX DOOR MALFUNCTIONED A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 370PX 340B300 ON FLIGHT NR 3260, AIR STAIR WOULD NOT COME DOWN, LOCKED IN THE UP POSITION. MAINTENANCE CHECKED DOOR OPERATION SEVERAL TIMES, COULD NOT DUPLICATE. RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2002110600060 20021106 00060 EU 2002 11 6 MALA020603 1 20021006 A 5753 SPAR SAAB SF340 SF340A 7850100 EU T/E FLAP CRACKED A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 27XJ 340A027 RT FLAP REAR SPAR IS CRACKED AT STA 142, FLAP. 2 L 7 2 4T RT A52EU 2002110600061 20021106 00061 WP 2002 11 6 DHL2002873505 1 20020908 A 5340 57500921 FITTING DOUG DC8 DC873F 302199F WP LT MLG WW DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 83065 46091 LT MLG WW TRAPEZOIDAL PANEL SHOWS (04) 3/16 INCH DIA HOLES AT BS 902.000. 2 L 7 4 4F RT 4A25 2002110600064 20021106 00064 EU 2002 11 6 MALA020604 1 20021014 A 3246 5006227 WHEEL SAAB SF340 340B 7860101 EU NLG VIBRATES A MALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 15 446XJ 340B446 DURING FLIGHT NR 3292, VIBRATION AFTER DEPARTING DTW. PILOT CONTINUED ON TO CMI. PILOT ASKED CMI TRUCK TO COME OUT IN CASE WHEEL FELL OFF. DID NOT DECLARE AN EMERGENCY. VIBRATION WAS PRESENT WHEN NOSE GEAR WAS SET ON GROUND. VIBRATION WAS FROM 110KTS, TO 80KTS LANDING WAS INCIDENT FREE. MAINTENANCE REPLACED LEFT NOSE WHEEL ASSEMBLY. SERVICED SHIMMY DA MPER IAW SAAB AMM CHAPTER 32. LUBED NOSE GEAR IAW SAAB AMM CHAP 12, ALSO FOUND UNKNOWN DEBRIS INSIDE. 2 L 7 2 4T RT A52EU 2002110600065 20021106 00065 EU 2002 11 6 MALA020605 1 20021015 A 2760 PRESSURE SWITCH BAC 146 AVRO146RJ85A 1500097 EU SPOILER FAILED A MALA O OTHER O OTHER LD LANDING 1 GL 15 532XJ E2366 UPON LANDING OF FLIGHT NR 3651 IN DTW, MANUAL SPOILERS WOULD NOT DEPLOY. MAINTENANCE REPLACED PRESSURE SWITCH IAW AMM 2 7-61-21. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2002110600066 20021106 00066 NM 2002 11 6 A4J2002F00002 1 20020908 A 7711 LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE NR 1&2 ENG PT2 BLOCKED A A4JA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SO 35 12FQ 49766 UPON ENGAGING THROTTLE THE LT ENGINE WOULD NOT SPEED TO TAKEOFF POWER. BOTH PT2 LINES ON NR 1 AND NR 2 ENGINE BLOCKED. CLEARED BLOCKAGE AND CHECKED BNUT CONNECTIONS, OCK, OK ON ENGINE RUN IAW MM. ALSO TRIMMED NR 1 AND NR 2 ENGINE., AND OCK, IAW MM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600067 20021106 00067 EU 2002 11 6 MALA020606 1 20021015 A 2720 WARNING SYSTEM SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 367PX 340B271 DURING TAXI OUT OF FLIGHT NR 3154, RUDDER LIMITER LIGHT ILLUMINATED. RETURNED A/C TO GATE. MAINTENANCE ADVISED OF PROB LEM AFTER GATE RETURN. MAINTENANCE T/S SYSTEM IAW SAAB AMM 27-21-45. ALL CHECKS GOOD, COULD NOT DUPLICATE. 2 L 7 2 4T RT A52EU 2002110600068 20021106 00068 WP 2002 11 6 NACA20020054 1 20021101 A 3260 5333660500 DOWNLOCK SWITCH DOUG DC6 DC6 3021702 WP INTERMITTENT A NACA O OTHER N FALSE WARNING LD LANDING 1 AL 03 2907F 533265 DISCREPANCY: RIGHT MAIN GEAR SHOWED GEAR UNSAFE CONDITION (UP INDICATION PLUS RED LIGHT). RECYCLED GEAR AND THE UNSAFE C ONDITION WENT AWAY.CORRECETIVE ACTION: REPLACED DOWN LOCK SWITCH, OP CHECK GOOD. 2 L 7 4 4R A781 2002110600069 20021106 00069 NE 2002 11 6 MALA020608 2 20021017 A 7510 6068T56P01 ANTI-ICE VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 451XJ 340B451 DURING CLIMB-OUT ON FLIGHT NR 3251, RT AIR VALVE LIGHT ILLUMINATED SEVERAL TIMES. AIR RETURN TO MSP. MAINTENANCE REMOV ED AND REPLACED RT ANTI-ICE VALVE PER GE MM 75-00-00, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2002110600070 20021106 00070 NM 2002 11 6 A4J2002F00003 1 20020916 A 3610 39271012 VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE AGUMENTATION INOPERATIVE A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 35 12FQ 49766 AFTER DEPARTURE, 20 MINUTES INTO FLIGHT, THE CREW GOT A TAILCONE OVERHEAT LIGHT AND DID A RETURN TO FIELD. REMOVED AND INSTALLED AUGMENTATION VALVE IAW MM. OCK GOOD IAW MM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600071 20021106 00071 WP 2002 11 6 UPS02839620 1 20021005 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:N/A PIT 31 DOOR AFT TOP CORNER OUTER SKIN HAS 4 INCH CRACK THROUGH 3 RIVETS. REMOVED DAMAGED REPAIRED I AW 52-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2002110600072 20021106 00072 WP 2002 11 6 A4J2002F00004 1 20020906 A 2722 5914387521 LIMITER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE RUDDER ACTUATOR MISALIGNED A A4JA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 35 418GE 49418 RUDDER TRAVEL LIGHT ON AFTER TAKE OFF. RETURNED TO AIRPORT. ADJUSTED RUDDER THROW LIMITER AND LINKAGE IAW MM. 2 L 7 2 4F 4 F A6WE E2EA 2002110600073 20021106 00073 NM 2002 11 6 A4J2002F00005 1 20020905 A 2120 7136821 SLEEVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D NE DUCT TORN A A4JA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 35 12FQ 49766 TAIL COMPARTMENT, HOT LIGHT CAME ON JUST AFTER TAKEOFF. FOUND TORN SLEEVE ON DUCT. REMOVED AND REPLACED DUCT SLEEVE IA W MM. OPS AND LEAK CHECK GOOD, IAW MM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600074 20021106 00074 EU 2002 11 6 MALA020609 1 20021017 A 3620 LIGHT SAAB SF340 340B 7860101 EU COCKPIT INTERMITTENT A MALA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 15 449XJ 340B449 DURING FLIGHT NR 3318, LEFT LP BLEED FAILS TO INDICATE CLOSED WHEN SELECTED. MAPS CHECK OK. MAINTENANCE INSPECTED LT B LEED VALVE OPENS AND CLOSES NORMALLY. LAMP CHECK INTERMITTENT. RELAMPED LEFT BLEED CLOSED ANNUNCIATOR AND TESTED WHILE RUNNING. CHECKS OK. 2 L 7 2 4T RT A52EU 2002110600075 20021106 00075 NM 2002 11 6 A4J2002F00006 1 20020902 A 3110 403424192 IRU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D NE INSTRUMENTS CONTAMINATED A A4JA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 SO 35 11FQ 49759 FLIGHT DIVERTED, LOST ALL INSTRUMENTS, BOTH FMS, BOTH DFG C, IRU MAINLY WENT OUT. PROBLEM ON GROUND, MAINTENANCE FOUN D WATER FROM HEAVY RAINS. DRIED MOISTURE ON DFGC, IAW. ALL SYSTEMS OPS CHECKED OK. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600076 20021106 00076 CE 2002 11 6 ACE0603021 1 20020604 A 2913 MS24171D1 RELAY BEECH 1900 1900C 1154161 CE HYD PUMP BURNED A YADA O OTHER J WARNING INDICATION AP APPROACH 1 AL 03 45GL 2223 UC45 ON APPROACH, THE LANDING GEAR WAS SELECTED DOWN AND THE GEAR EXTENDED NORMALLY, GIVING THREE GREEN SAFE INDICATIONS. MO MENTS AFTER GETTING THE GEAR DOWN AND SAFE INDICATION, THE LANDING GEAR PUMP CIRCUIT BREAKER POPPED. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE DETERMINED THAT THE LANDING GEAR HYDRAULIC PUMP MOTOR RELAY WAS STUCK IN THE CLOSED POSITION AND REPLACED SAVE. 2 L 7 2 4T RT A24CE 2002110600077 20021106 00077 EU 2002 11 6 MALA020610 1 20021018 A 3234 D49412001 CONTROL HANDLE SAAB SF340 340B 7860101 EU COCKPIT DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 451XJ 340B451 DURING FLIGHT NR 2953, INTRANSIT LIGHT WON'T GO OUT, WITH LANDING GEAR HANDLE DOWN INTRANSIT LIGHT REMAINS ON. MAINTENA NCE REPLACED GEAR HANDLE, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002110600078 20021106 00078 EA 2002 11 6 ACE0806021 2 20020807 A 7250 3040361 RING ASSEMBLY BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ENGINE LOOSE A YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 1566C UC36 DURING HSI INSPECTION, THE CT VANE RING SEGMENTS WERE NOTED BEING LOOSE. THE HOT SECTION WAS REPLACED DUE TO THIS CONDI TION. AS THE ASSY WAS SET ON A WORK BENCH, MULTIPLE SHROUD SEGMENTS WERE OBSERVED TO FALL OUT OF PLACE, HAD THIS OCCURR ED DURING ENG OPERATION, ENGINE WOULD HAVE EXPERIENCED A CATASTROPHIC INTERNAL FAILURE DUE TO CONTACT OF THE COMPRESSOR TURBINE BLADES WITH THE SEGMENTS. A REVIEW OF THE VANE RING ASSY INDIVIDUAL PN INDICATES THAT THE REASON THE SEGMENTS WERE NOT RETAINED WAS DUE TO IMPROPER MATCH. BETWEEN THE COMPRESSOR TURBINE STATOR ASSY AND SHROUD HOUSING. THE REMOVE D ASSY DID NOT HAVE PROVISIONS FOR RETAINING THE AXIAL MOVEMENT OF THE SHROUD SEGMENTS. 2 L 7 2 4T 4 T RT A24CE E4EA 2002110600079 20021106 00079 EU 2002 11 6 MALA020612 1 20021020 A 3230 CONNECTOR SAAB SF340 SF340A 7850100 EU LT MLG BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 106XJ 340A106 DURING LC1 INSPECTION, LEFT EXPLOSIVE BOLT CANNON PLUG BROKE. MAINTENANCE REPLACED LEFT EXPLOSIVE BOLT CANNON PLUG IAW SAAB 340 WM 20/30-15. 2 L 7 2 4T RT A52EU 2002110600080 20021106 00080 CE 2002 11 6 ACE0820021 1 20020820 A 3397 2065521 CONNECTOR BEECH 1900 1900C 1154161 CE STROBE SHORTED A YADA K NONE L NO TEST IN INSP/MAINT 1 AL 03 45GL 37312 UC45 DURING SCHEDULED MAINTENANCE, FOUND THAT THE WING STROBE LIGHTS WERE INOPERATIVE WITH THE NAVIGATION LIGHTS TURNED ON, T ROUBLE SHOOTING REVEALED INTERNAL SHORTING OF THE AFT PRESSURE BULKHEAD CONNECTOR. DISCOVERED THAT THE ELEVATOR ELECTRI C TRIM SERVO WIRES THAT RUN THROUGH THE SAME CONNECTOR WERE SHORTED AND GETTING POWER FROM THE STROBE/NAV LIGHT CIRCUIT BREAKERS THERE BY MAKING THE TRIM SERVO ALWAYS POWERED AND UNABLE TO BE DEENERGIZED BY SECURING THE PROPER TRIM CIRCUIT BREAKER. SAFETY OF FLIGHT ISSUE. IN THE PREVIOUS 30 DAYS, THIS AC HAD AT LEAST 4 DIFFERENT ELECTRIC ELEVATOR TRIM DISC REPANCIES THAT APPEARED TO BE INTERMITTENT AND MIGHT HAVE BEEN CAUSED BY THIS ELECTRICAL FAULT. 2 L 7 2 4T RT A24CE 2002110600081 20021106 00081 EU 2002 11 6 MALA020613 1 20021020 A 3230 85106RC84SNB CONNECTOR SAAB SF340 SF340A 7850100 EU RT MLG BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 106XJ 340A106 DURING LC1 INSPECTION, RT EXPLOSIVE BOLT CANNON PLUG BROKE IN HALF. MAINTENANCE REMOVED AND REPLACED RT EXPLOSIVE BOLT CANNON PLUG IAW SAAB WM 20-30-15. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002110600082 20021106 00082 CE 2002 11 6 ACE0822021 1 20020826 A 2913 MS24171 RELAY BEECH 1900 1900C 1154161 CE HYD PUMP CONTAMINATED A YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 45GL 37339 UC45 ON APPROACH TO LANDING, THE LANDING GEAR WOULD NOT NORMALLY EXTEND. THE FLIGHT CREW USED THE ALTERNATE HAND PUMP FOR EX TENSION AND PERFORMED AND UNEVENTFUL LANDING. MAINTENANCE CONFIRMED THAT THE LANDING GEAR HYDRAULIC MOTOR RELAY WOULD F REEZE AND NOT OPERATE THE HYDRAULIC POWER PACK. THE RELAY WAS REPLACED AND ALL SYSTEMS OPERATED NORMAL. POST REMOVAL I NSPECTION OF THE OLD RELAY CONFIRMED THAT THE PLUNGER CAVITY WAS CONTAMINATED WITH WATER. 2 L 7 2 4T RT A24CE 2002110600083 20021106 00083 2002 11 6 MALA020614 4 20021017 A 2562 ELT SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A MALA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 417XJ 340B417 ELT WENT OFF DURING TAXI. 2 L 7 2 4T RT A52EU 2002110600086 20021106 00086 EU 2002 11 6 MALA020615 1 20021018 A 2421 31342001 GENERATOR SAAB SF340 340B 7860101 EU LT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 429XJ 340B429 LEFT AC GEN INOPERATIVE SPARKS ARE VISIBLE FROM VENT AREA. AIR RETURN TO BRD. MAINTENANCE REPLACED LEFT AC GENERATOR A ND QAD ADAPTER. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2002110600088 20021106 00088 EU 2002 11 6 MALA020617 1 20021023 A 3320 SWITCH SAAB SF340 SF340A 7850100 EU CABIN MALFUNCTIONED A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 27XJ 340A027 ON PUSHBACK OF FLIGHT NR 2751, PUFF OF SMOKE OUT OF FA'S CONTROL PANEL AND SMELL OF ELECTRICAL BURNING. AC RETURNED TO GATE. MAINTENANCE REPLACED FA'S PANEL DIMMER SWITCH. ALL CHECKS GOOD IAW SF340-MM CHAP 33. 2 L 7 2 4T RT A52EU 2002110600089 20021106 00089 EU 2002 11 6 MALA020618 1 20021022 A 3060 660714263 LEAD SAAB SF340 340B 7860101 EU LT PROPELLER DEFECTIVE A MALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 442XJ 340B442 BEFORE FLIGHT NR 3264, LEFT PROP HEAT FAILS TEST ON GROUND AFTER 1:20. A/C RETURNED TO GATE. MAINTENANCE DURING TROUBL ESHOOTING NOTED BAD DE-ICE LEAD ON BLADE NR 1. REMOVED AND REPLACED IAW DOWTY CMM 61-10-39. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002110600090 20021106 00090 CE 2002 11 6 2002F00977 1 20020820 A 2711 CONTROL CABLE BEECH 1900 1900D 1154162 CE AILERON TAB IMPROPER A AMWA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CE 07 5YV UE5 FLT 5466 - AFTER LANDING IN PFN, CREW REPORTED AILERON TRIM WAS IMPROPERLY RIGGED. MAINTENANCE INSPECTED AND FOUND AILE RON TRIM CABLE IMPROPERLY INSTALLED. CABLE WAS CORRECTLY INSTALLED AND RIGGED. OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER INCIDENT. (M) 2 L 7 2 4T RT A24CE 2002110600091 20021106 00091 NE 2002 11 6 2002F00978 2 20020825 A 7230 GAS GENERATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE MALFUNCTIONED A AMWA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 07 5YV UE5 LEFT ENGINE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED IN FLIGHT. OIL PRESSURE WAS BELOW 60 PSI, LEFT ENGINE SHUTDOWN. L EFT GAS GENERATOR AND POWER SECTION WERE REPLACED. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 2002110600139 20021106 00139 2002 11 6 ASAA0280310 4 20020916 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 SEA - DURING PREFLIGHT CHECK, THE FORWARD SERVICE DOOR EMERGENCY SLIDE 'CLIP FELL OUT' LANYARD DISCONNECTED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2002110600162 20021106 00162 WP 2002 11 6 ASAA0280314 1 20020919 A 5310 5930583111 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - DURING C-CHECK, FOUND LEFT MLG DOOR JAMB WAS CRACKED AT UPLOCK SENSOR CUT OUT DOUBLER. REPLACED DOOR JAMB CUTOUT DOUBLER PER SRM 51-10-2,-3, AND -4. (M) 2 L 7 2 4F A6WE 2002110600163 20021106 00163 WP 2002 11 6 ASAA0280315 1 20020919 A 5310 5930584112 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - DURING C-CHECK, FOUND RIGHT MLG DOOR FORWARD JAMB CRACKED AROUND RIVET HEAD. REPLACED DOOR JAMB PER SRM 51-10-3, -4, 51-30-2 AND -5. (M) 2 L 7 2 4F A6WE 2002110600164 20021106 00164 WP 2002 11 6 ASAA0280316 1 20020920 A 5230 592600317 BRACKET DOUG DC9 DC982 3022082 WP BARRIER DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - FOUND C-CHECK, MID CARGO BAY BARRIER DOOR AFT GUIDE RAIL BRACKET WAS CRACKED. REPLACED BRACKET PER SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002110600165 20021106 00165 SO 2002 11 6 GMC2002F00000 1 20021021 A 3240 1159SCL5043 BRAKE ASSY GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE MLG DAMAGED B GMCR O OTHER O OTHER TX TAXI/GRND HDL 1 GL 23 5101 550 LOUD CHATTER WAS NOTICED AS AIRCRAFT WAS BEING TOWED. LT INBOARD AND OUTBOARD BRAKE ASSEMBLY WERE FOUND TO HAVE DAMAGED ROTATING DISC DRIVE KEY SLOTS DAMAGE WAS ALSO FOUND ON WHEEL ASSEMBLY. BRAKES AND WHEELS WERE REPLACED. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F 4 F RT A12EA E00057EN 2002110600166 20021106 00166 WP 2002 11 6 ASAA0280318 1 20020920 A 5320 991195338 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - FOUND C-CHECK, AFT ACCESSORY COMPARTMENT VENTRAL STAIRS RIGHT AFT SIDEWALL PANEL SUPPORT BRACKET CRACKED. INSTALL ED SIDEWALL DOUBLER PER SRM 51-10-4 AND 51-30-2. (M) 2 L 7 2 4F A6WE 2002110600167 20021106 00167 NE 2002 11 6 GTIA021118 2 20021014 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE NR 1 FAILED A GTIA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 GL 23 803NK 48087 ACCOMPLISHED EMERGENCY LANDING, NO INCIDENT. AT 1900 VERY LOUD BANG THROUGHOUT AIRCRAFT, NR 1 ENGINE LOST POWER, N1 AND N2 STILL ROTATING, TRIED RELIGHT, NO RELIGHT. REMOVED AND REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 2002110600168 20021106 00168 WP 2002 11 6 GTIA021120 1 20020929 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE LAVATORY DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 LT AFT LAV ASSY, SEVERAL AREA OF DELAMINATED AND DAMAGED FLOORBOARD SUPPORT LAV ASSY. FABBED NEW LAV FLOOR BOARD, INSTA LLED NEW LAV FLOORBOARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600169 20021106 00169 WP 2002 11 6 ASAA0280319 1 20020920 A 5350 595126615 RUB STRIP DOUG DC9 DC982 3022082 WP FAIRING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - FOUND DURING C-CHECK, LEFT WING TO BODY FAIRING AFT FILLET 2108 CHAFE STRIP WAS CRACKED AT TOP SIDE. TRIMMED CRAC K AREA AND BLENDED AREA FILLET PANEL PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002110600170 20021106 00170 WP 2002 11 6 GTIA021121 1 20020930 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE COCKPIT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FLIGHT COMPT, STA 120 TO STA 140.8 FLOOR PANEL HAS CRACK/ CORROSION. FABRICATED NEW FLOOR PANELS. INSTALLED NEW FLOOR PANELS. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600171 20021106 00171 WP 2002 11 6 ASAA0280320 1 20020920 A 5320 ACA7413 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - FOUND DURING C-CHECK, AFT CARGO COMPARTMENT LEFT INBOARD SEAT TRACK SPLICE WEB WAS CRACKED. TRIMMED AND SMOOTHED DAMAGE PER SRM 53-01.(M) 2 L 7 2 4F A6WE 2002110600172 20021106 00172 WP 2002 11 6 GTIA021122 1 20020919 A 5230 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 AFT CARGO DOOR SKIN GOUGED AND CRACKED BELOW HANDLE. ROUTED OUT GOUGE AND CRACK FABBED REPAIR DOUBLER, INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600173 20021106 00173 WP 2002 11 6 GTIA021123 1 20020920 A 5754 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE NR 1 SLAT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 RIGHT NR 1 SLAT OUTBOARD LEADING EDGE METAL STRIP UPPER SIDE IS CRACKED. FORMED NEW MATERIAL STRIP, INSTALLED NEW SLAT METAL STRIP. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600174 20021106 00174 WP 2002 11 6 GTIA021124 1 20020923 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 AFT PIT STA 1287-1309 BLO, INTERCOSTAL UPPER FLANGE IS CRACKED AT FASTENER HOLES, AREAS OF CORROSION AT AFT END. REMOVE D INTERCOSTAL. FABRICATED INTERCOSTAL. INSTALLED INTERCOSTAL. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600175 20021106 00175 NM 2002 11 6 GTIA021125 1 20020924 A 5313 LONGERON DOUG MD80 MD83 3023681 NM PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 AFT PIT, CORROSION FS 1250-1271 LONG 28R, LWR SIDE CORRODED AT SPLICE. REMOVED DAMAGED SECTION, DRILLED NEW LONGERON, F ABRICATED LONGERON SPLICE, INSTALLED SPLICE AND LONGERON SECTION. 2 L 7 2 4F 4 F RT E2EA 2002110600176 20021106 00176 WP 2002 11 6 ASAA0280321 1 20020920 A 5320 5910141103 BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - 30K-CHECK, FOUND MID CARGO BAY DOOR FORWARD HOLD-OPEN LATCH SIDE BRACKET (ANGLE) WAS CRACKED. FABRICATED AND INST ALLED REPLACEMENT ANGLE FROM 063 INCH 7075-T6 STOCK PER SRM 51-10-2. (M) 2 L 7 2 4F RT A6WE 2002110600177 20021106 00177 WP 2002 11 6 GTIA021126 1 20020924 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 AFT CABIN STA 1322 CORROSION ON FLOORBEAM. FABRICATED REPAIR ANGLE AND FILLER INSTALLED REPAIR PARTS. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600178 20021106 00178 WP 2002 11 6 ASAA0280322 1 20020921 A 5210 5914730533 MECHANISM DOUG DC9 DC983 3022083 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 969AS 53063 SEA - FOUND L1 DOOR DIFFICULT TO OPEN. ADJUSTED DOOR MECHANISM. DOOR THEN OPENED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2002110600179 20021106 00179 WP 2002 11 6 GTIA021127 1 20020928 A 5340 ATTACH ANGLE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 AFT FUSELAGE STA 1437 TO STA 1418 CORRODED AT AFT ANGLE ATTACH TO FLANGE APU GROUND CONTROL AND FIRE DOOR. REMOVED CORR ODED ANGLE, FORMED NEW ANGLE, INSTALLED NEW ANGLE. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600180 20021106 00180 WP 2002 11 6 ASAA0280333 1 20020927 A 5320 6547960916 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - C-CHECK, FOUND CORROSION IN AFT CARGO BAY AT NR 5 WEB LIGHTING HOLE FROM STATION 1193 TO 1212, LONGERON 28R TO 29R . REPLACED INTERCOSTAL AT STATION 1193 PER SRM 51-30-5, PAGE 12, PARA 7, AND 51-30-2, PAGE 3, FIG 2. (M) 2 L 7 2 4F A6WE 2002110600181 20021106 00181 NM 2002 11 6 KPVA200230 1 20021007 A 3350 10005511 BATTERY DHAV DHC8 DHC8103 1386005 NM CABIN DISCHARGED A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 807WP 023 HNL - FOUND EMERGENCY PORTABLE LIGHT VERY DIM, WEAK BATTERY. REMOVED AND REPLACED EMERGENCY PORTABLE LIGHT. OPERATION CHECK GOOD IAW DHC-8 MM 33-51-00, PAGES 201-202, 2A. NO DEFECTS NOTED. (M) 2 H 7 2 4T RT A13NM 2002110600182 20021106 00182 WP 2002 11 6 GTIA021128 1 20020929 A 5320 SUPPORT BRACKET DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 AFT FUSELAGE STA 1380 LOWER ANGLE CAP SUPPORT AFT CANTED BULKHEAD. REMOVED LOWER (T) ANGLE, LOCATED AND DRILLED NEW LOW ER (T) ANGLE. INSTALLED NEW (T) ANGLE. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600183 20021106 00183 NM 2002 11 6 USAA020374 1 20020925 A 5541 65C258873 FRAME BOEING 737 737301 1384611 NM RUDDER CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 49067 23512 PIT - FOUND FRAME CORRODED, BALANCE ASSEMBLY END FRAME ON RUDDER. CORRODED LEVEL 2. REPLACED DEFECTIVE PART WITH IDENT ICAL PART PER OM-26 AND JPC J3-65-27500-005. (M) 2 L 7 2 4F RT A16WE 2002110600184 20021106 00184 WP 2002 11 6 GTIA021129 1 20020929 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 AFT FUSELAGE, LEFT STA 1380 TO STA 1401, CORRODED AT INTERCOSTAL. REMOVED INTERCOSTAL, FABRICATED NEW INTERCOSTAL, INST ALLED NEW INTERCOSTAL. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600185 20021106 00185 EU 2002 11 6 USAA020375 1 20020929 A 5315 FLOORBEAM AIRBUS 320 A320214 3930316 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 108UW 9651 1061 TPA - FOUND FLOORBEAM CORRODED 25 SQUARE INCHES, FLOORBOARD INTERCOSTAL AT FRAME 16, 20 INCHES LEFT OF CENTER. CORROSIO N LEVEL 2. (M) 2 L 7 2 4F RT A28NM 2002110600186 20021106 00186 WP 2002 11 6 GTIA021130 1 20021004 A 5313 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 AFT CARGO PIT: LONGERON 30L FS 1212, CORRODED. REMOVED L30 SECTION. FABRICATED LONGERON 30 SECTION AND SPLICE REPAIR. INSTALLED L30 AND SPLICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110600187 20021106 00187 EU 2002 11 6 USAA020376 1 20020929 A 5315 FLOORBEAM AIRBUS 320 A320214 3930316 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 108UW 9651 1061 FOUND FLOORBEAM CORRODED 2 INCH AREA, FLOORBOARD INTERCOSTAL FRAME 16, 30 INCHES LEFT OF CENTER. CORROSION LEVEL 2. SP LICED IN NEW SECTION OF FLOORBEAM FROM FRAME 16 FORWARD PER SRM 53-11-14 FIG 202. (M) 2 L 7 2 4F RT A28NM 2002110600188 20021106 00188 EU 2002 11 6 USAA020377 1 20020929 A 5315 FLOORBEAM AIRBUS 320 A320214 3930316 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 108UW 9651 1061 TPA - FOUND FLOOR BEAM CORRODED 1 SQUARE INCH, OUTBOARD FLOORBEAM AT FLOORBOARD HOLE FORWARD OF GIRT BAR PAD. CLEANED A REA AND INSTALLED REPAIR ANGLE PER SRM 53-41-14 FIG 201, REPAIR PRINCIPAL 2. (M) 2 L 7 2 4F RT A28NM 2002110600190 20021106 00190 NM 2002 11 6 CA021028007 1 20021024 A 2597 214424185 WIRE BOEING 747 747433 NM PWA 4056 PW4056 NE VIDEO SYSTEM CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 43351 (CAN) AIRCRAFT REPORTED HAVING A CIRCUIT BREAKER POP FOR THE VIDEO SYSTEM IN ZONE ``D`` FOUND OPEN CIRCUIT WIRING AND BU RNED SHIELDED WIRES BETWEEN VDU 6 AND VDU 7 IN THE AFT ACFT CABIN. CAUSE OF THE DAMAGED WIRING WAS A FAILURE OF THE AIR CONDITIONING DUCT SUPPORTING BRACKET. THE BROKEN BRACKET HAD MIGRATED OUTBOARD AND CHAFED THE WIRING AND THE 115VAC SUP PLY WIRE CONDUCTOR WAS ALSO CONTACTED. THE BROKEN BRACKET ALSO CONTACTED THE ADJACENT GASPER DUCT AND CHAFED A 1.5 INCH CUT INTO THE 3.0 INCH GASPER DUCT.THE LOCATION OF THE BRACKET AND AREA OF DAMAGE TO THE WIRING AND GASPER DUCT IS STA 12 20 , WL 300, LBL 15. 2 L 7 4 4F 4 F RT A20WE E24NE 2002110600191 20021106 00191 EA 2002 11 6 CA021029011 1 20021021 A 5260 85210240007 HAND RAIL DHAV DHC8311 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE AIRSTAIR SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 262 (CAN) AFT AIRSTAIR DOOR SUPPORT STRUT SHEARED. FWD SUPPORT STRUT CRACKED. BOTH SUPPORT STRUTS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002110600192 20021106 00192 EU 2002 11 6 USAA020378 1 20020929 A 5315 D5347209001000 FLOORBEAM AIRBUS 320 A320214 3930316 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 108UW 9651 1061 TPA - FOUND FLOORBEAM CORRODED, LEFT AFT LAVATORY, AFT OUTBOARD LAVATORY MOUNT HOLE. CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M) 2 L 7 2 4F RT A28NM 2002110600193 20021106 00193 EA 2002 11 6 CA021031010 2 20020923 A 8520 CAMSHAFT LYC HC360H1A HUGHES 269 269C1 8059504 SW LYC O360 HO360C1A 41514 EA ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA L3490836A (CAN) ENGINE RUNS UNEVEN. FOUND METAL DEPOSITS IN OIL FILTER. ENGINE REMOVED AND SENT FOR INSPECTION/REPAIR. 1 G 7 1 3O 3 O O 4H12 E286 2002110600194 20021106 00194 SW 2002 11 6 CA021031013 1 20020805 A 2421 ALU8421 ALTERNATOR PRECISION ALU8421 HUGHES 269 269C1 8059504 SW LYC O360 HO360C1A 41514 EA ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 99074081 (CAN) ALTERNATOR LOW VOLTAGE. REPLACED ALTERNATOR. 1 G 7 1 3O 3 O O 4H12 E286 2002110600195 20021106 00195 EU 2002 11 6 USAA020379 1 20020929 A 5315 D534720900200 FLOORBEAM AIRBUS 320 A320214 3930316 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 108UW 9651 1061 TPA - FOUND FLOORBEAM CORRODED, LEFT AFT LAVATORY, AFT INBOARD LAVATORY MOUNT HOLE. DEFECTIVE PART REPLACED WITH IDENTI CAL PART NR. (M) 2 L 7 2 4F RT A28NM 2002110600196 20021106 00196 NM 2002 11 6 USAASB02185 1 20021003 A 3397 WIRE BOEING 737 737301 1384611 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 585US 23930 EWR - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT 1C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER SEATS 2A AND C. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002110600197 20021106 00197 NM 2002 11 6 2002UALA01545 1 20021007 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 AFT PIT STATION 793 BETWEEN STRINGER 24 & STRINGER 25 HAS EXCESSIVE MATERIAL LOSS IN WEB. MAJOR REPAIR ACCOMPLISHED. F RAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600198 20021106 00198 NM 2002 11 6 2002UALA01546 1 20021007 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 LEFT HAND CREASE BEAM WEB CORRODED BETWEEN BODY STATION 639 AND BODY STATION 663. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600199 20021106 00199 NM 2002 11 6 2002UALA01547 1 20021007 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 AFT CARGO DOOR FORWARD LOWER SKIN EDGE GOUGED AND DENTED STATION 797 BETWEEN STRINGER 22 & 23R. MAJOR REPAIR ACCOMPLISH ED. DOUBLER & TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600200 20021106 00200 NM 2002 11 6 2002UALA01550 1 20021009 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 CABIN FLOORBEAM STATION 324 RBL 57 TO 61 MATERIAL REMOVED EXCEEDS LIMITS. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED M ATERIAL AND INSTALLED T-CAP SPLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002110600201 20021106 00201 NM 2002 11 6 2002UALA01551 1 20021008 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 CABIN FLOOR STRUCTURE AT STATION 333 LBL 45-55, WL 208 FLOOR SUPPORT T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTAL LED T-CAP STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002110600202 20021106 00202 NM 2002 11 6 2002UALA01552 1 20021008 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 CABIN FLOOR SUPPORT T-CAP AT STATION 365, RBL 12-42, WL 208 CORRODED. MAJOR REPAIR ACCOMPLISHED. STRAP REPAIR INSTALLE D. 2 L 7 2 4F 4 F RT A2NM E17NE 2002110600203 20021106 00203 NM 2002 11 6 2002UALA01553 1 20021009 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 STATION 1681 LBL 12 CABIN PRESSURE FLOOR WEB CORRODED AROUND FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002110600204 20021106 00204 NM 2002 11 6 2002UALA01554 1 20021007 A 5330 DOUBLER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 606UA 21867 EXTERNAL FUSELAGE, LEFT HAND SIDE SKIN DOUBLER HAS POPPED RIVET AND BULGED SKIN AT BODY STATION 742-744, STRINGER 38L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A1NM E3NE 2002110600205 20021106 00205 NM 2002 11 6 2002UALA01556 1 20021003 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN STATION 787 FRAME WEB JUST ABOVE STRINGER 9R SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600206 20021106 00206 NM 2002 11 6 2002UALA01558 1 20020921 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 AFT CABIN STATION 1016 FLOORBEAM UPPER CHORD LBL 7 TO 11 HAS EXCESSIVE MATERIAL LOSS DUE TO BLEND REMOVAL OF CORROSION. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAP AND ANGLES INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600207 20021106 00207 2002 11 6 2002UALA01559 4 20021010 A 2210 SC47003 DAMPER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AUTOPILOT SYS LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 29 448UA 842 LANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. NR 1 YAW DAMPER WAS FOUND LEAKING HYDRAULIC FLUID. NEW YAW DAMPER ACTUATOR WAS INSTALLED AND OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2003031300084 20030313 00084 NE 2003 3 13 2002UALA01560 2 20021011 A 7250 1B6322002 TURBINE BLADES BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 529UA 29887 13087 25019 726640 WHILE CLIMBING THROUGH 14000 FT LEFT ENGINE EXPERIENCED A COMPRESSOR STALL. ENGINE SELF RECOVERED AND CLIMB CONTINUED T O FL260. EGT REDLINED, THROTTLE RETARDED TO IDLE. ENGINE WAS REMOVED FOR METAL IN THE TAILPIPE, IT HAD A NORMAL ECM TR END PLOT. AT ENGINE TEARDOWN, A STAGE 2 TURBINE BLADE FAILURE WAS FOUND TO BE THE CAUSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002110600208 20021106 00208 NM 2002 11 6 2002UALA01562 1 20021011 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 LEFT HAND CREASE BEAM WEB AT STATION 970-976 EXCESSIVE MATERIAL REMOVED TO ELIMINATE CORROSION. MAJOR REPAIR ACCOMPLISH ED. REPLACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002110600209 20021106 00209 NM 2002 11 6 2002UALA01564 1 20021011 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 947UA 26688 FORWARD PIT LEFT HAND FRAME STATION 440 DENTED ABOVE S25L. INTERNAL AND EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600210 20021106 00210 NM 2002 11 6 2002UALA01565 1 20021007 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 AFT CARGO DOOR FORWARD LOWER SKIN EDGE GOUGED AND DENTED STATION 797 BETWEEN STRINGER 22 & 23R. MAJOR REPAIR ACCOMPLISH ED. DOUBLER / TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600211 20021106 00211 NM 2002 11 6 2002UALA01566 1 20021007 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 AFT PIT STATION 793 BETWEEN STRINGER 24 & STRINGER 25 HAS EXCESSIVE MATERIAL LOSS IN WEB. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED PERMANENT DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600212 20021106 00212 NM 2002 11 6 2002UALA01567 1 20021012 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 947UA 26688 STATION 178 LEFT HAND SIDE CHORD CRACKED IN RADIUS AT WL 207. MAJOR REPAIR ACCOMPLISHED. DOUBLER SPLICE STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600213 20021106 00213 NM 2002 11 6 2002UALA01568 1 20021012 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 947UA 26688 STATION 178 BULKHEAD WEB CRACKED AT RIGHT HAND UPPER RADAR MOUNT OUTBOARD SIDE. MAJOR REPAIR ACCOMPLISHED. DOUBLER REP AIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600214 20021106 00214 EA 2002 11 6 COMA0260628 1 20021102 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 810CA 16631 7370 FLIGHT 6000 EMERGENCY LIGHTS ARE INOP.REPLACED EMERGENCY LIGHTS BATTERIES. 2 L 7 2 4F RT A21EA 2002110600215 20021106 00215 NM 2002 11 6 2002UALA01569 1 20021012 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 947UA 26688 STATION 178 BULKHEAD WEB CRACKED AT LEFT HAND UPPER RADAR MOUNT UPPER OUTBOARD SIDE. MAJOR REPAIR ACCOMPLISHED. DOUBLE R REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600216 20021106 00216 NM 2002 11 6 2002UALA01570 1 20021013 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 947UA 26688 EXTERNAL FUSELAGE SKIN LAP IS GOUGED AT BODY STATION 385 STRINGER 14L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600217 20021106 00217 NM 2002 11 6 2002UALA01571 1 20021012 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 RIGHT HAND BODY STATION 178 FUSELAGE CHORD CRACKED AT WL207. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB SECTION REPA IR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600218 20021106 00218 NM 2002 11 6 2002UALA01572 1 20021012 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 RIGHT HAND BODY STATION 188 FRAME CRACKED AT STRINGER 17 RIGHT HAND. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPA IR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600219 20021106 00219 EA 2002 11 6 COMA0260629 1 20021102 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA L/H BROKEN A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 912CA 7677 7011 FLIGHT 5907 PILOTS WINDSHIELD SHATTERED.REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2002110600220 20021106 00220 NM 2002 11 6 2002UALA01573 1 20021012 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 LEFT HAND BODY STATION 178 FUSELAGE CHORD CRACKED AT WL207. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600221 20021106 00221 NM 2002 11 6 2002UALA01574 1 20021012 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 LEFT HAND BODY STATION 188 FRAME CRACKED AT STRINGER 17 LEFT HAND. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR . 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600222 20021106 00222 NM 2002 11 6 2002UALA01575 1 20021012 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 AFT EDGE OF AFT CARGO DOOR CUTOUT SKIN BLENDED WORN. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600223 20021106 00223 EA 2002 11 6 COMA0260630 1 20021103 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 409CA 7441 FLIGHT 5979 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.COULD NOT DUPLICATE. DEFERRED MAINT. PER MEL. 2 L 7 2 4F RT A21EA 2002110600224 20021106 00224 NM 2002 11 6 2002UALA01576 1 20021013 A 5320 INTERCOSTAL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 950UA 26695 CABIN FLOOR INTERCOSTAL AT BODY STATION 506 BL 0 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CRACKED UPPER ANGLE O F INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600225 20021106 00225 NM 2002 11 6 2002UALA01577 1 20021013 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 FORWARD GALLEY DOOR CUTOUT FORWARD FRAME AT STOP PAD FITTING IS CRACKED (UPPER FITTING). MAJOR REPAIR ACCOMPLISHED. IN STALLED REPAIR ANGLE. INSTALLED FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110600226 20021106 00226 EA 2002 11 6 COMA0260631 1 20021102 A 7732 6233M30A ACCELEROMETER CNDAIR CL600 CL6002B19 1900309 EA LT ENG MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 984CA 15520 7171 FLIGHT 5058 N2 VIB INDICATION, LEFT ENGINE DURING T/O.REPLACED THE LT ENGINE EVM TRANSDUCER. 2 L 7 2 4F RT A21EA 2002110600227 20021106 00227 NM 2002 11 6 UPS02239863 1 20021027 A 5310 PANEL BOEING 727 72725C 138400H NM BS 249.3 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C&SI CRACK SUSPECT ON NLG BAY R/H SIDE PANEL @ BS 249.3 BETWEEN FASTENERS AFT OF R/H FWD PRESSURE PANEL CUTOUT REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1 2 L 7 3 4F A3WE 2002110600228 20021106 00228 NM 2002 11 6 UPS02239865 1 20021023 A 5310 FRAME BOEING 727 72725C 138400H NM BS 990 S29L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C&SI SUSPECT CRACK AT FUSELAGE FRAME ATTACH POINT AT BS 990 STR. 29L IN A FT CARGO BAY REPAIRED FRAM E AS PER SRM 53-10-4 FIG 11 2 L 7 3 4F A3WE 2002110600229 20021106 00229 NM 2002 11 6 UPS02239866 1 20021023 A 5340 SEAT TRACK BOEING 727 72725C 138400H NM BS 1027 & 1008RH CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C&SI AFT CARGO BAY, SEAT TRACK HAS LIGHT SURFACE CORROSION AT 2 AREAS AT BS 1027 LH & BS 1008 R/H CO RROSION REMOVED AND FOUND OUTSIDE LIMITS IAW SRM 51-10-06 SEAT TRACK REPAIRED IAW SRM 53-10-5 FIG 8 2 L 7 3 4F A3WE 2002122300025 20021223 00025 SO 2002 12 23 C2XA02TY165 1 20021105 A 5542 12020808515 SKIN EMB 145 EMB145LR 3260212 SO RUDDER DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 DURING A SCHEDULED 2-C INSPECTION, MAINTENANCE FOUND A DENT IN NR 1 RUDDER, RT SIDE BETWEEN RIB 2890.0 AND 2601.0. THE AREA WAS CUT OUT AND A EXTERNAL DOUBLER WAS FABRICATED. DRILLED,ALODINED,PRIMED AND PAINTED AND INSTALL THE DOUBLER. ALL WORK WAS ACCOMPLISHED IAW GST 3254/02;EMB 145 SRM 51-40-02'03 CPM 5121-04-05-06. A/C WILL BE REL. UPON COMPLETION OF AL L WORK. 2 L 7 2 4T RT T00011AT 2002110700001 20021107 00001 NM 2002 11 7 ABXA020285 1 20021008 A 5700 114T22027 STRUT BOEING 767 767200 1385120 NM LEFT WING L/E CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 LEFT WING FIXED LEADING EDGE RIB, W.S. 456.98, HAD CORROSION IN ANTI-ICE TAIL DUCT TO LEADING EDGE SLAT AT WING FIXED LE ADING EDGE RIB. REMOVED CORRODED RIB AND INSTALLED NEW STRUT IAW BOEING SRM 51-40-02, 57-41-09, AND BAC DWG 114T2202. 2 L 7 2 4F RT A1NM 2002110700002 20021107 00002 NM 2002 11 7 ABXA020288 1 20020826 A 5700 113T150643 HINGE FITTING BOEING 767 767200 1385120 NM LEFT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 CORROSION UNDER JUMPER BONDING BOLT, LEFT OUTBOARD AILERON, OUTBOARD HINGE FITTING, W.S. 1127.45. REPLACED FITTING IAW B OEING SRM 57-51-02, IPC 57-51-51-A01, AND DWG 113T1521. 2 L 7 2 4F RT A1NM 2002110700003 20021107 00003 NM 2002 11 7 ABXA020289 1 20021006 A 5753 113T17862 FRAME BOEING 767 767200 1385120 NM LT WING TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 LEFT WING NR 6 INBOARD TRAILING EDGE FLAP AFT FAIRING FORWARD FRAME, FOUND CRACK. NO, THIS PART HAS BEEN PREVIOUSLY ACCO MPLISHED ON A/C SB 767-57-0014. THE COMPONENT THE PART IS INSTALLED ON, IS FLAP LINKAGE FAIRING NR 3. REPAIRED AREA IAW REA B657-44390. 2 L 7 2 4F RT A1NM 2002110700004 20021107 00004 EU 2002 11 7 MALA020619 1 20021024 A 3010 DEICE SYSTEM SAAB SF340 340B 7860101 EU HORIZ STAB FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 456XJ 340B456 BEFORE FLIGHT NR 3161 STAB FAILS DEICE TEST IN MANUAL MODE OPERATION. RETURNED TO GATE. MAINTENANCE REMOVED AND REPLAC ED RIGHT HORIZONTAL STABILIZER LEADING EDGE IAW SF340 AMM AND OPS CHECK SF340 AMM 30-10-00. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002110700005 20021107 00005 NE 2002 11 7 MALA020620 2 20021024 A 7530 BLEED BAND BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 3 ENGINE BROKEN A MALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 15 532XJ E2366 ON TAKEOFF OF FLIGHT NR 3545, THE NR 3 ENGINE POWER BEGAN TO FLUCTUATE. OBSERVED EGT REACHED 685 N1 BEGAN TO FLUCTUATE THEN DROP. PULLED THRUST LEVER TO IDLE. ENGINE STABILIZED AT FLIGHT IDLE. RETURNED FOR LANDING WITH ENGINE OPERATING AT FLIGHT IDLE. PED SHOWS MAX EGT 652 FOR 10 SECONDS. AIR RETURN TO DTW. MAINTENANCE TROUBLESHOT FOUND BROKEN BLEED B AND, REMOVED AND REPLACED BLEED BAND IAW ALLIED SIGNAL MANUAL. CHECKED GAP, ALL CHECKS GOOD. RAN ENGINE ALL PARAMETERS NORMAL. DOWNLOADED FDAM TEMPS WERE WITHIN LIMITS. NO ACTION REQUIRED IAW 72-00-00, TABLE 801. 2 H 7 4 4F 4 F RT A49EU E6NE 2002110700006 20021107 00006 NE 2002 11 7 MALA020621 2 20021024 A 7210 GEARBOX SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE DAMAGED A MALA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 GL 15 444XJ 340B444 ON FLIGHT NR 2972, HAD AN INFLIGHT SHUTDOWN EVENT. CREW SHUTDOWN RT ENGINE, DECLARED AN EMERGENCY, DID AN AIR TURNBACK AND LANDED IN MSP WITHOUT INCIDENT. MAINTENANCE REMOVED COWLS, FOUND HOLE IN REAR PGB CASE AT APPROXIMATELY THE 4:30 PO SITION, AFT LOOKING FORWARD. SUSPECT THE FOLLOWING, RT IDLER GEAR WEB CRACKED CAUSING TAB WASHER FAILURE DUE TO INCREAS ED VIBRATION. THE NUT THEN BACKED OFF, ALLOWING RT IDLER GEAR TO MOVE BACK AGAINST CASE, CREATING HOLE AND CAUSING LOSS OF OIL. HISTORY SHOWS NO BYPASS PIN EVENTS OR CHIP DETECTOR FINDINGS IN PAST 12 MONTHS AND NONE PRIOR TO EVENT. 2 L 7 2 4T 4 T RT A52EU E8NE 2002110700007 20021107 00007 EU 2002 11 7 MALA020622 1 20021022 A 2435 STARTER GEN SAAB SF340 340B 7860101 EU ROTOL R390 R3904123F27 NE RT ENGINE FAILED A MALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 442XJ 340B442 BEFORE FLIGHT NR 3191, DURING P3 TEST, NOTED AUTOCOARSEN LOW LIGHT DOES NOT ILLUMINATE WITH AUTOCOARSEN SWITCH SELECTED ON, CONDITION LEVERS IN FEATHER AND TORQUE 10 PERCENT-15 PERCENT. CYCLED A/C POWER STILL NO GOOD. A/C RETURNED TO GATE . MAINTENANCE TROUBLESHOT AND FOUND RT STARTER GEN BAD. REPLACED STARTER GEN IAW TASKCARD NR 243103. GROUND RAN CHECK OF AUTOCOARSEN AND STARTER GEN GOOD. 2 L 7 2 4T RT A52EU 6 C P31NE 2002110700008 20021107 00008 EU 2002 11 7 MALA020623 1 20021025 A 7711 HTE690041 PRESSURE SWITCH BAC 146 AVRO146RJ85A 1500097 EU NR 4 ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 508XJ E2318 DURING FLIGHT NR 3460, NR 1 AND NR 4 INTAKE LOW PRESS LIGHT ON. AIR TURNBACK TO MSP. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE LOW PRESSURE SWITCH IAW ARJ AMM 30-21-14. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2002110700009 20021107 00009 EU 2002 11 7 MALA020624 1 20021026 A 3020 THERMISTER SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 456XJ 340B456 DURING FLIGHT NR 2797, LEFT INTAKE ANNUNCIATOR ILLUMINATED INTERMITTENTLY W/ ANTI-ICE SYSTEM. AIR RETURN TO MEM. MAINT ENANCE FOUND NR 3 AND NR 4 THERMISTOR BAD, SWAPPED TO NR 5. PERFORMED OPS CHECK GOOD IAW ACT SPRAYMAT REPAIR MANUAL 30- 21-03. A/C OK FOR SERVICE. 2 L 7 2 4T RT A52EU 2002110700010 20021107 00010 EU 2002 11 7 MALA020625 1 20021020 A 5753 SPAR SAAB SF340 340B 7860101 EU T/E FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369PX 340B295 DURING 6Y/4Y INSPECTION IN CWA, MAINTENANCE FOUND LEFT FLAP REAR SPAR CRACKED AT STA 142. MAINTENANCE COMPLETED REPAIR IAW EO NR S57007. 2 L 7 2 4T RT A52EU 2002110700011 20021107 00011 EU 2002 11 7 MALA020626 1 20021021 A 5347 CARGO TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369PX 340B295 DURING 6Y/4Y INSPECTION IN CWA, MAINTENANCE FOUND CARGO SEAT TRACK HAS CORROSION. MAINTENANCE COMPLETED REPAIR IAW EO N R S53060, AT BLO FROM STA 618-686.888. 2 L 7 2 4T RT A52EU 2002110700012 20021107 00012 NE 2002 11 7 MALA020627 3 20021027 A 6112 BOOT SAAB SF340 SF340A 7850100 EU ROTOL R390 R3904123F27 NE LT PROPELLER FAILED A MALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 142XJ DURING TAXI OF FLIGHT NR 3294, LEFT PROP DEICE LIGHT ILLUMINATED DURING TAXI. DEICE BOOT ON ONE OF THE PROP'S WAS BAD. MAINTENANCE REMOVED AND REPLACED LEFT PROP ASSEMBLY IAW 340 JOB CARD 6110-303, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 6 C P31NE 2002110700013 20021107 00013 EU 2002 11 7 MALA020631 1 20021103 A 3243 HP14081004 VALVE SAAB SF340 340B 7860101 EU BRAKE SYSTEM FAILED A MALA D RETURN TO BLOCK O OTHER LD LANDING 1 GL 15 421XJ 340B421 UPON LANDING, CAPT SIDE LEFT BRAKE PEDAL INOP. PEDAL STIFF AND ALMOST NO BRAKING ON LEFT SIDE. A/C PULLS RIGHT WITH EV EN TWO FOOT BRAKE APPLICATION, TESTED BRAKES ON FO'S SIDE OPERATED NORMALLY. MAINTENANCE REPLACED POWER BRAKE VALVE IA W SF340 AMM 32-42-10-4. OPS AND LEAK CHECK GOOD. A/C OK FOR CONTINUED SERVICE. 2 L 7 2 4T RT A52EU 2002110700014 20021107 00014 EU 2002 11 7 MALA020632 1 20021103 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY MALFUNCTIONED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 369PX 340B295 DURING FLIGHT NR 3229, LAV SMOKE DETECTION SYSTEM ALARMED INTERMITTENT INFLIGHT. MAINTENANCE FOUND SYSTEM NEVER SHOWED A WARNING OG. CLEANED CANNON PLUG OF LAVATORY SMOKE DETECTOR. PERFORMED OPS CHECK OF SMOKE DETECTOR, IAW SF340 AMM 26- 13-00-5. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4T RT A52EU 2002110700015 20021107 00015 EU 2002 11 7 MALA020633 1 20021104 A 3260 UPLOCK SWITCH SAAB SF340 340B 7860101 EU NLG OUT OF ADJUST A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 427XJ 340B427 AFTER TAKEOFF OF FLIGHT NR 3387 LANDING GEAR WOULD NOT COMPLETE ITS RETRACTION CYCLE. INTRANSIT LIGHT STAYED ON WITH HY DRAULIC PUMP RUNNING CONTINUOUSLY. GEAR EXTENDED NORMALLY. AIR RETURN TO CWA. MAINTENANCE FOUND NOSE UPLOCK SWITCH TO BE ADJUSTED RIGHT AT ACTUATION POINT. ADJUSTED UPLOCK SWITCH IAW SAAB MM 32-61-15. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002110700016 20021107 00016 EU 2002 11 7 MALA020634 1 20021030 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 DURING 4K INSPECTION IN CWA, MAINTENANCE FOUND FORWARD AREA OF CABIN SEAT TRACK BL 0 HAS SEVERAL SPOTS OF CORROSION. MA INTENANCE REMOVED AND REPLACED CORRODED SEAT TRACK. 2 L 7 2 4T RT A52EU 2002110700017 20021107 00017 EU 2002 11 7 MALA020635 1 20021030 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 DURING 4K INSPECTION IN CWA, MAINTENANCE FOUND LEFT SEAT TRACK WRAP AROUND HAS CORROSION. MAINTENANCE REMOVED AND REPLA CED SEAT TRACK CORROSION. 2 L 7 2 4T RT A52EU 2002110700019 20021107 00019 NE 2002 11 7 SWIA200211274 2 20020929 A 7261 6047T63P04 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NR 1 LEAKING A SWIA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 07 595SW 7292 SMOKE IN COCKPIT IMMEDIATELTY AFTER TAKEOFF. MOSTLY COMING FROM CAPTAINS'S VENT. DONNED O2 MASKS. SMOKE LAV MESSAGE FOLLOWED. PERFORMED EMERGENCY PROCEDURE. FA NOTICED SMOKE IN CABIN AS WELL. NO FIRE IN LAVATORY. PERFORMED EVAC AT G ATE. LOGGED OVERWEIGHT (50,000). REMOVED AND REPLACED NR 1 CARBON SEAL IAW GE MM. RAN PACKS WITH ENGINES. NO SMOKE I N COCKPIT OR CABIN. ALL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002110700020 20021107 00020 SO 2002 11 7 SWIA200211311 1 20021010 A 3080 D55201001 MONITOR EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 564SW 120339 DEICE MONITOR INOP. RESET CB'S A5/A6 PER MX CONTROL, WITH NO CHANGE. SMELL OF BURNED WIRING, WAITED 20 MINUTES FOR SME LL TO CLEAR, NO CHANGE. BOTH CB'S POPPED ON THEIR OWN AFTER 5 MINUTES, WILL NOT RESET. REMOVED AND REPLACED DEICE MONI TOR WITH SERVICEABLE UNIT. MONITOR CHECKS GOOD. ALL PANELS SECURED. 2 L 7 2 4T RT A31SO 2002110700021 20021107 00021 EA 2002 11 7 SWIA200211312 1 20021007 A 5210 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 594SW 7285 PASSENGER DOOR HARD TO OPEN. REMOVED AND REPLACED INBOARD SUPPORT BRACKET WITH NEW BRACKET. CLEANED, INSPECTED AND LUB ED BEARINGS IAW MM 52-11-02. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002110700022 20021107 00022 EA 2002 11 7 SWIA200211313 1 20021011 A 5210 SPRING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 429SW 7518 CABIN DOOR DIFFICULT TO OPEN. ADJUSTED SPRING ROD ASSEMBLY IAW CRJ MM 52-11-02. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002110700023 20021107 00023 SO 2002 11 7 SWIA200211314 1 20021010 A 3233 LOCKWASHER EMB 120 EMB120RT 3260202 SO LT MLG ACTUATOR BROKEN A SWIA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 NM 07 593SW 120191 AFTER DEPARTURE, LEFT MAIN GEAR WOULD NOT RETRACT. RETURNED TO RDM. FOUND TANG BROKEN ON LOCKING WASHER FOR LEFT MAIN LANDING GEAR ACTUATOR. REPLACED TANG WASHER AND RIGGED LEFT MAIN GEAR IAW MM 32-32-11. PERFORMED SEVERAL GEAR SWINGS W ITH NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2002110700024 20021107 00024 SO 2002 11 7 SWIA200211315 1 20021007 A 3397 WIRE EMB 120 EMB120RT 3260202 SO CABIN MISSING A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 236SW 120312 FORWARD EMERGENCY LIGHT EXIT SIGN DOES NOT ILLUMINATE. FOUND WIRE MISSING FROM REAR TERMINAL BLOCK. REINSTALLED WIRE F OR FORWARD EMERGENCY LIGHT WITH NEW HARDWARE. COMPLIED WITH OPS CHECK OF LIGHT AND FOUND OK. 2 L 7 2 4T RT A31SO 2002110700025 20021107 00025 SO 2002 11 7 SWIA200211316 1 20021006 A 2722 3081401003 ACTUATOR EMB 120 EMB120ER 3260203 SO RUDDER FAILED A SWIA A UNSCHED LANDING F P FLT CONT AFFECTED NO WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 RIGHT RUDDER PEDAL JAMMED AFTER TAKEOFF. RETURNED TO RAP. PERFORMED RUDDER SYSTEM HEALTH CHECK PER MM 27-22-00. FOUND BLUE SYSTEM RUDDER ACTUATOR BAD. REMOVED AND REPLACED BLUE SYSTEM ACTUATOR IAW MM 27-22-02. OPS CHECK AND LEAK CHECK GOOD. CLOSED AND SECURED ALL PANELS. 2 L 7 2 4T RT A31SO 2002110700026 20021107 00026 EA 2002 11 7 SWIA200211318 1 20020821 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 595SW 7292 RIGHT AND LEFT FLOOR SUPPORT ANGLES AT FS 621.00 ARE CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED ANGLES IAW CRJ REO 601R-53-61-117 REV A. 2 L 7 2 4F RT A21EA 2002110700027 20021107 00027 EA 2002 11 7 SWIA200211319 1 20020821 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 595SW 7292 FOUND ANGLES CRACKED AT FS 280.0 LBL AND RBL 90 INBOARD AND OUTBOARD. NEW ANGLES FIT AND INSTALLED IAW CRJ SRM 51-40-11 , 51-42-06, 51-42-13, 51-42-21. 2 L 7 2 4F RT A21EA 2002110700028 20021107 00028 EA 2002 11 7 SWIA200211321 1 20021012 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT OUT OF ADJUST A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 591SW 7079 LEFT SIDE CABIN EMERGENCY EXIT DOOR IS STUCK. FA UNABLE TO OPEN. ADJUSTED THE EMERGENCY DOOR AND LUBED THE LATCH. DOO R CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002110700029 20021107 00029 NM 2002 11 7 02FDEA00711 1 20021008 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 HORIZ STAB INT, BARREL NUT HOLE NR 26R AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510 -66415. 2 L 7 3 4F RT A22WE 2002110700030 20021107 00030 NM 2002 11 7 02FDEA00712 1 20021004 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 HORIZ STAB INT, BARREL NUT HOLE NR 20R EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER 1-5510-66415. 2 L 7 3 4F RT A22WE 2002110700031 20021107 00031 NM 2002 11 7 02FDEA00713 1 20021008 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 HORIZ STAB INT, BARREL NUT HOLE NR 23L AFTER CORROSION BLEND OUT, OUT OF SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-6 6415. 2 L 7 3 4F RT A22WE 2002110700032 20021107 00032 NM 2002 11 7 02FDEA00714 1 20021008 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 HORIZ STAB INT BARREL NUT HOLE NR 24R AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510- 66415. 2 L 7 3 4F RT A22WE 2002110700033 20021107 00033 EU 2002 11 7 MALA020599 1 20021006 A 2160 7769022 CONTROL VALVE SAAB SF340 340B 7860101 EU CABIN TEMP MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 434XJ 340B434 DURING FLIGHT NR 3196, LEFT DUCT OVER TEMP LIGHT ON AND BLEED CLOSES. WHENEVER BLEED IS RESET THE DUCT TEMP GOES UP ALL THE WAY. HAPPENS IN AUTO AND MANUAL MODES. AIR RETURN TO MSP. MAINTENANCE REPLACED LEFT DUAL TEMP CONTROL VALVE IAW SAAB AMM 21-61-05. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002110700034 20021107 00034 NM 2002 11 7 UPS02239857 1 20021104 A 3350 COVER BOEING 727 72727C 138400J NM CABIN LOOSE A IPXA K NONE O OTHER TO TAKEOFF 1 SO 01 908UP 19114 INSPECTION TYPE:N/A MAIN ENTRY DOOR EMERGENCY LIGHT FELL OUT OF BRACKET DURING T/O. R&R MAIN ENTRY DOOR EMERGENCY LIGHT COVER OK FOR CONTINUED SERVICE. 2 L 7 3 4F A3WE 2002110700035 20021107 00035 NM 2002 11 7 UPS02439858 1 20021103 A 3350 BATTERY BOEING 747 747123 1384873 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A EMERGENCY LIGHT INOP MAIN DECK CEILING AT STA 580 LT SIDE. REPLACED BATTERY ASSY, OP CHECK OK. 2 L 7 4 4F A20WE 2002110700036 20021107 00036 NM 2002 11 7 UPS02439859 1 20021104 A 3350 BATTERY BOEING 747 747123 1384873 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP MAIN DECK CEILING AT STA 640 LT SIDE. R&R BATTERY ASSY, OP CHECK OK. 2 L 7 4 4F A20WE 2002110700037 20021107 00037 NM 2002 11 7 UPS02439860 1 20021105 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A MAIN ENTRY DOOR R1 FWD EMERG LIGHT INOP. RELAMPED, OPS CHECK GOOD. 2 L 7 4 4F A20WE 2002110700038 20021107 00038 NM 2002 11 7 UPS02439861 1 20021105 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST UK UNKNOWN 1 SO 01 675UP 20390 INSPECTION TYPE:N/A I/BOUND TO SDF MX FOUND UPPER DECK, AFT EMER LIGHT FWD LIGHT BULB IN OP. R/R LIGHT. 2 L 7 4 4F A20WE 2002110700039 20021107 00039 NM 2002 11 7 UPS02439870 1 20021103 A 5720 STIFFENER BOEING 747 747123 1384873 NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 A STIFFENER CORRODED CENTER SECTION REAR SPAR. LBS. 85.6 HAS CORROSION. APPROX. 11 INCHES LONG. NEXT TO FUEL PUMP APERAT URE. REMOVED VERTICAL STIFFNER PER SRM 51 30 02 39550/ INSTALLED NEW STIFFNER PER SRM 51 10 01 REPLACEMENT OF PART. REF LOG 914476 ITEM 1 &2 FOR FINAL INSTALLATION OF REMAINING FASTNER 2 L 7 4 4F A20WE 2002110700040 20021107 00040 WP 2002 11 7 UPS02839649 1 20021009 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:ASV EMERGENCY LIGHT SYSTEM INOP. R&R EMERGENCY LIGHT BATTERY PACK OPS CK OK PER DC8 MM 33-50-00. 2 L 7 4 4F RT 4A25 2002110700041 20021107 00041 EA 2002 11 7 SWIA200211322 1 20021012 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 589SW 7072 FRONT RED FLOOR EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT CONNECTOR. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002110700042 20021107 00042 NM 2002 11 7 CALA0200528 1 20021106 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 380-420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND CABIN L/H I/B SEAT TRACK CORRODED FROM STA 380-420. THE SEAT TRACK WAS REPLACED IAW SRM 53-30-52. 2 L 7 2 4F RT A16WE 2002110700043 20021107 00043 NM 2002 11 7 CALA0200529 1 20021106 A 5320 ANGLE BOEING 737 7373T0 1384582 NM STA 1106 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND A 3" CRACK IN L-ANGLE AT L/H SIDE OF FUSELAGE STA 1106 TO RUDDER JUST BELOW VERTICAL STABILIZER. THE AN GLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW ECRA 5380-01013. 2 L 7 2 4F RT A16WE 2002110700044 20021107 00044 NM 2002 11 7 CALA0200530 1 20021106 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM STA 907-927 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND R/H O/B SEAT TRACK CORRODED FROM STA 907-927. REPLACED SEAT TRACK IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2002110700045 20021107 00045 NM 2002 11 7 CALA0200531 1 20021106 A 5230 SKIN BOEING 737 7373T0 1384582 NM AFT CARGO DR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39343 23581 INSPECTION FOUND AFT CARGO DOOR SKIN DENTED AT 35" FROM TOP AND 10" FROM FORWARD EDGE. A REPAIR DOUBLER WAS INSTALLED IA W SRM 52-00-01, FIGURE 203. 2 L 7 2 4F RT A16WE 2002110700046 20021107 00046 NM 2002 11 7 CALA0200532 1 20021106 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 1007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND STRINGER S29R CORRODED AT STA 1007. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002110700047 20021107 00047 NM 2002 11 7 CALA0200533 1 20021107 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 907 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND A 1" CRACK IN STRINGER SPLICE 4R AT STA 907. A NEW STRINGER SPLICE WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2002110700048 20021107 00048 WP 2002 11 7 CALA0200534 1 20021107 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 1193-1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 98876 49444 INSPECTION FOUND L/H I/B SEAT TRACK CORRODED AROUND HOLES AT STA 1193-1309. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2002110700049 20021107 00049 EA 2002 11 7 SWIA200211323 1 20021013 A 2741 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA E/E BAY MALFUNCTIONED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 589SW 7072 STAB TRIM CHANNEL 2 INOP. PERFORMED HSTCU BITE TEST, LIGHT WOULD NOT GO OUT ON TEST. POWERED DOWN AIRCRAFT AND RERACKE D HSTCU IAW 27-41-01. FAULTS CLEARED AND CHANNEL 2 CHECKED OK. 2 L 7 2 4F RT A21EA 2002110700050 20021107 00050 SO 2002 11 7 SWIA200211324 1 20021010 A 3260 CONNECTOR EMB 120 EMB120ER 3260203 SO LANDING GEAR LOOSE A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 213SW 6456 6456 120277 RIGHT MAIN GEAR GREEN A LIGHT DID NOT EXTINGUISH WHEN GEAR RETRACTED. GEAR DID NOT EXTEND WHEN LEVER PUT IN DOWN POSITI ON. GEAR EXTENDED WITH ELECTRICAL OVERRIDE. CYCLED GEAR 10 TIMES, COULD NOT DUPLICATE. REPLACED LANDING GEAR CONTROL BOX. CYCLED GEAR 10 TIMES, COULD NOT DUPLICATE. SWAPPED LANDING GEAR HARNESSES. RIGHT MAIN GEAR GREEN B-LIGHT REMAINE D ILLUMINATED IN FLIGHT. SWAPPED HARNESSES BACK TO ORIGINAL CONFIGURATION. FOUND LOOSE CANNON PLUG FOR UPLOCK A HARNES S AND RESECURED. CYCLED GEAR NUMEROUS TIMES. ALL GEAR LIGHTS OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4T RT A31SO 2002110700051 20021107 00051 2002 11 7 SWIA200211325 4 20021012 A 2211 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT SYS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 221SW 120290 DURING LEVEL FLIGHT AT FL230 AND -12 DEGREES CELSIUS WITH THE A/P SELECTED ON, THE CAPTAIN'S FLIGHT DIRECTOR COMMANDED A N ABRUPT ROLL TO THE LEFT, FOLLOWED BY A PITCH DOWN TO 5 DEGREES. PREVIOUS CREW REPORTED SIMILAR OCCURRENCE AT FL240. REPLACED CAPTAIN'S AUTOPILOT COMPUTER APC-65B IAW MM 22-10-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002110700052 20021107 00052 EA 2002 11 7 SWIA200211326 1 20021014 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 431SW 7536 STAB TRIM CHANNEL NR 2 WILL NOT ENGAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW M M 27-42-01 AND 27-42-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002110700053 20021107 00053 NE 2002 11 7 SWIA200211327 2 20021014 A 7261 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RT ENGINE LEAKING A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING K M J FLUID LOSS OVER TEMP WARNING INDICATION CR CRUISE 1 NM 07 430SW 7523 RIGHT ENGINE OIL PRESSURE WENT TO 25-27 PSI AND ENGINE TEMPERATURE WAS GOING UP. FOLLOWED QRH AND SHUT DOWN THE RIGHT E NGINE. DIVERTED TO DEN. INSTALLED NEW CARBON SEALS IN HYD PUMP, AIR STARTER AND IDG POSITIONS, AND NEW 3 EA SEAL RINGS IN EACH POSITION. SEALS AND SEAL RINGS CHANGED IAW GE MM SEI-756 SPECIAL PROCEDURE 63. COMPONENTS INSTALLED IAW CANAD AIR MM 72-00-00. ALL LEAK CHECKS OK. 2 L 7 2 4F 4 F RT A21EA E15NE 2002110700054 20021107 00054 NM 2002 11 7 F3LA200200385 1 20021106 A 2900 HYDRAULIC LINE BOEING 737 7372Y5 1384554 NM RIGHT WHEEL WELL DAMAGED A F3LA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 NM 03 118RW 60938 1954 23040 DURING FLIGHT, A SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO FOLLOWED BY THE FAILURE OF THE NUMBER 2 ENGINE, ENGINE DRIVEN HYDRAULIC PUMP. A SYSTEM PRESSURE REMIAINED NORMAL. ON FINAL APPROACH TO DIVERSION SITY AIRPORT, A SYSTEM PRESSURE DR OPPED TO ZERO. STANDBY SYSTEM CARRIED THE LOAD THROUGH THE LANDING.VISUAL INSPECTION OF THE WHEEL WELLS AND LANDING GEA R AREAS REVEALED A FRACTURED HYDRAULIC LINE IN THE RIGHT WHEEL WELL, FORWARD AREA OF THE WELL. INSTALLED A TEMPORARY HY DRAULIC LINE IN ACCORDANCE WITH THE REQUIREMENTS OF MM 20-10-51. REMOVED, INSPECTED AND REPLACED RETURN FILTERS IN THE A SYSTEM. TRACE AMOUNTS OF METAL WERE FOUND IN THE NUMBER 2 ENGINE CASE DRAIN FILTER. MAINTENANCE REMOVED AND REPL 2 L 7 2 4U RT A16WE 2002110700055 20021107 00055 2002 11 7 SWIA200211328 4 20021010 A 2213 8220044001 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 920SW 7660 AIRCRAFT HAD SEVERAL OCCASIONS WHERE WE RECEIVED `AP TRIM` MESSAGES BOTH PITCH TRIM AND TRIM LEFTWARD. AIRCRAFT ALSO WE NT INTO AN UNCOMMANDED LEFT ROLL. REMOVED AND REPLACED FLIGHT CONTROL PANEL AS REQUIRED. SYSTEM OPS CHECKS GOOD IAW 22 -11-00. 2 L 7 2 4F RT A21EA 2002110700056 20021107 00056 SO 2002 11 7 SWIA200211329 1 20021010 A 2121 AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203 SO CABIN FAULTY A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 288SW 120316 RIGHT GROUND COOLING FAN STOPS INTERMITTENTLY AND CAUSES SMOKE IN CABIN. REPLACED RIGHT GROUND COOLING FAN. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002110700057 20021107 00057 EA 2002 11 7 SWIA200211330 1 20020831 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 FS 280.00 RBL 9.0 FLOOR BEAM INBOARD AND OUTBOARD ANGLES FOUND CRACKED DURING C-CHECK INSPECTION. FIT AND INSTALLED NEW ANGLES IAW CRJ SRM 51-40-11, 51-42-13 AND 51-42-21. 2 L 7 2 4F RT A21EA 2002110700058 20021107 00058 EA 2002 11 7 SWIA200211331 1 20020831 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 FOUND FS 280.0 RBL 9.0 FLOOR SUPPORT ANGLE CRACKED DURING C CHECK INSPECTION. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53 -11-137. HFEC INSPECTION COMPLIED WITH ON BEAM SUPPORT CUTOUT REPAIR AS REQUIRED IAW RJ NDTM 51-20-01. NO CRACKS FOUND . 2 L 7 2 4F RT A21EA 2002110700059 20021107 00059 EA 2002 11 7 SWIA200211332 1 20020831 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 FOUND FS 280.0 RBL 9.0 PILOT BULKHEAD LOWER FLANGE CRACKED DURING C-CHECK INSPECTION. HFEC INSPECTION COMPLIED WITH ON CUTOUT REPAIR AS REQUIRED IAW RJ NDTM 51-20-01. NO CRACKS FOUND. PILOT BULKHEAD REPAIRED IAW CRJ REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2002110700060 20021107 00060 EA 2002 11 7 SWIA200211334 1 20020831 A 5346 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 FOUND FORWARD INBOARD CORNER OF LOWER ENGINE SUPPORT BEAM WEB CRACKED DURING C-CHECK INSPECTION. NDT-HFEC CARRIED OUT I AW REO 601R-53-61-366. NO CRACKS NOTED. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-366 REV `D`. 2 L 7 2 4F RT A21EA 2002110700061 20021107 00061 EA 2002 11 7 SWIA200211335 1 20020831 A 5346 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 FOUND UPPER ENGINE SUPPORT BEAM WEB CRACKED AT APPROX RBL 8 STARTING FROM AFT SIDE UNDER FIRE LOOP BRACKET. FOUND DURIN G C-CHECK INSPECTION. HFEC INSPECTION C/O ON BEAM CUTOUT REPAIR AND AREA AS REQUIRED IAW REO 601R-53-61-345 REV C. NO CRACKS FOUND. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-345 REV `C` AND CRJ REO 601R-53-61-586. 2 L 7 2 4F RT A21EA 2002110700062 20021107 00062 EA 2002 11 7 SWIA200211336 1 20020831 A 5346 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 FOUND FORWARD INBOARD CORNER OF LOWER ENGINE SUPPORT BEAM WEB CRACKED ON RIGHT SIDE. FOUND DURING C-CHECK INSPECTION, H FEC INSPECTION COMPLIED WITH ON REMOVED ANGLES (2) AND INNER ANGLES AT REPAIR AREA AS REQUIRED IAW REO 601R-53-61-366. NO CRACKS FOUND. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-366 REV D. 2 L 7 2 4F RT A21EA 2002110700063 20021107 00063 EA 2002 11 7 SWIA200211337 1 20020831 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 FOUND FS 718.00 RIGHT FRAME SECTION WEB CRACKED AT STR 12R. FOUND DURING C CHECK INSPECTION. NEW FRAME FIT AND INSTALL ED IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06. 2 L 7 2 4F RT A21EA 2002110700064 20021107 00064 EA 2002 11 7 SWIA200211338 1 20020913 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FOUND FS 280.0 LBL 9.0 FLOORBEAM INBOARD AND OUTBOARD ANGLES CRACKED. FOUND DURING C CHECK INSPECTION. FIT AND INSTALL ED NEW ANGLES IAW CRJ SRM 51-40-11, 51-42-13, 51-42-21 & FABRICATED ANGLES IAW REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2002110700065 20021107 00065 EA 2002 11 7 SWIA200211339 1 20020913 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FOUND FS 280.0 RBL 9.0 FLOORBEAM INBOARD ANGLE CRACKED. FOUND DURING C CHECK INSPECTION. FIT AND INSTALLED NEW ANGLE I AW CRJ SRM 51-40-11, 51-42-13, 51-42-21. 2 L 7 2 4F RT A21EA 2002110700074 20021107 00074 WP 2002 11 7 GTIA021131 1 20021008 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 AFT FUSELAGE STA 1380-1401 L28L, INTERCOSTAL IS CORRODED. REMOVED INTERCOSTAL, FABRICATED NEW INTERCOSTAL, INSTALLED NE W INTERCOSTAL. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110700075 20021107 00075 WP 2002 11 7 GTIA021132 1 20021018 A 5330 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 EXT FUSELAGE STA 1474 (AT RAIN GUTTER) LEFT SIDE CORROSION ON SKIN. CUT OUT DAMAGED AREA OF SKIN, FABRICATED FILLER AND DOUBLER. INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110700076 20021107 00076 WP 2002 11 7 GTIA021133 1 20020923 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 MID CARGO STA 28R JAMB BEAM CORRODED FS 535 OUTBOARD SIDE AND INBOARD SIDE. REMOVED MID CARGO JAMB BEAM. HOLES LOCATED AND DRILLED ON NEW JAMB BEAM, INSTALLED NEW JAMB BEAM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110700077 20021107 00077 WP 2002 11 7 GTIA021135 1 20020924 A 5313 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 AFT CARGO PIT FRAME AT STA 1200 BETWEEN LONGERONS 28L AND 30 HAS CORROSION AT SPLICE. LONGERON 28L AT STA 1203 IS CORRO DED OUT OF LIMITS. FABRICATED LONGERON 28L SECTION AND SPLICE. INSTALLED LONGERON AND SPLICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110700078 20021107 00078 WP 2002 11 7 GTIA021136 1 20021014 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 CABIN FLOOR PANEL HAS EXPOSED INTERNAL HONEYCOMB STRUCTURE. FS 1249, LBL 35. REPAIRED DAMAGED AREA IN CABIN FLOOR PANE L. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110700079 20021107 00079 WP 2002 11 7 GTIA021137 1 20021018 A 3260 DOWNLOCK SENSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE NLG MALFUNCTIONED A GTIA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 823NK 48020 UPON INT. DESCENT NOSE WHEEL UNSAFE LIGHT CAME ON STAYED ON AT ALL POWER SETTING. FOLLOWED QRH PROCEDURES. HAD THREE G REEN FOR LANDING. REMOVED AND REPLACED NOSE GEAR DOWN LOCK PROX SENSOR AND OPS CHECK GOOD IAW MM. 2 L 7 2 4F 4 F A6WE E2EA 2002110700080 20021107 00080 WP 2002 11 7 GTIA021138 1 20020813 A 5320 SPLICE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D9 52048 NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FORWARD CARGO STR 25L SPLICE CORRODED AND CRACKED FS 228. FABRICATED NEW SPLICE, INSTALLED NEW SPLICE. 2 L 7 2 4F 4 F A6WE E2EA 2002110700081 20021107 00081 WP 2002 11 7 GTIA021139 1 20021011 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP PWA JT8 JT8D9 52048 NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FLOOR PANEL STA 256-294 LBL 44-54 HAS CORROSION UNDER RUB STRIP. FABRICATED FLOOR PANEL. 2 L 7 2 4F 4 F A6WE E2EA 2002110700082 20021107 00082 WP 2002 11 7 GTIA0211634 1 20020924 A 5313 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 MID CARGO PIT STA 28R CORRODED. REMOVED LONGERON, DRILLED AND LOCATED NEW LONGERON SECTION, INSTALLED NEW SECTION OF LO NGERON. 2 L 7 2 4F 4 F RT A6WE E2EA 2002110700083 20021107 00083 CE 2002 11 7 O2G2002F00001 1 20021016 A 2741 99141973B PITCH CONTROL CESSNA 650 650 2076802 CE HORIZ STAB CONTAMINATED E O2GA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 NE 03 3184Z 6500032 PRIMARY PITCH TRIM FAILURE CAUSED AIRCRAFT TO DIVERT FROM ORIGINAL DESTINATION AND LAND. REPLACE PITCH TRIM CONTROL BOX AND TESTED SYSTEM OK. REMOVED COMPONENT HAS EVIDENCE OF HYDRAULIC FLUID CONTAMINATION FROM AN EARLIER LEAK THAT HAD BE EN REPAIRED. 2 L 7 2 4F A9NM 2002110700084 20021107 00084 EU 2002 11 7 QH52002F00002 1 20021023 A 7120 258ES2471 BOLT BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE731* 01518 WP ENGINE MOUNT CRACKED B QH5R K NONE O OTHER IN INSP/MAINT 1 NM 07 626CG 258041 CRACK IN THE HEAD OF THE BOLT. 2 L 7 2 4F 4 F RT A3EU E6WE 2002110700085 20021107 00085 EU 2002 11 7 REX2002F00011 1 20021017 A 3230 AIR131330 SPRING SAAB SF340 SF340A 7850100 EU RT MLG BROKEN A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 401BH 33170 340A057 UPON GEAR EXTENSION RIGHT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED. EMERGENCY DECLARED, GEAR WAS CYCLED SEVERAL T IMES AND DOWN AND LOCK INDICATION WAS CONFIRMED. LANDING WAS UNEVENTFUL. UPON INVESTIGATION, FOUND DOWN LOCK ASSIST SP RING BROKEN AND INTERFERING WITH DOWN LOCK ASSEMBLY. SPRING WAS REMOVED AND REPLACED, GEAR SWINGS PERFORMED, SYSTEM OPE RATIONALLY CHECKED GOOD. 2 L 7 2 4T RT A52EU 2002110700086 20021107 00086 NM 2002 11 7 TSAA0233215 1 20021015 A 3350 8610062 BATTERY PACK BOEING 737 73725A 1384481 NM PWA JT8 JT8D17 52049 NE CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED NR 1,2,4, AND 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK, OK. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110700087 20021107 00087 NM 2002 11 7 TSAA0253214 1 20021016 A 5711 654549816 SPAR BOEING 737 7372S5C 1384499 NM PWA JT8 JT8D17 52049 NE RT WING CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 40031 22148 REMOVED A CRACK AND CORROSION LOCKED AT RIGHT WING FRONT SPAR WEB AT FSS 124.79 AND FSS 134.80. HFEC INSPECTED TO ENSUR E THE DAMAGE COMPLETELY REMOVED. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW ECO. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110700088 20021107 00088 NM 2002 11 7 TSAA0253216 1 20021013 A 5320 65C3760716 STIFFENER BOEING 737 737230 1384401 NM PWA JT8 JT8D* NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 REPAIRED CRACK AT BS 178, WI 184 LBL 5.7 VERTICAL CHORD. CUTOUT AND REMOVED DAMAGED PORTION OF SKIN AREA. VERIFIED CRA CK REMOVED USING HFEC METHOD. FABRICATED AND INSTALLED A REPAIR ANGLE IAW SRM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110700089 20021107 00089 NM 2002 11 7 TSAA0253217 1 20021015 A 5310 655496011 SHEAR TIE BOEING 737 737282C 13844AU NM PWA JT8 JT8D NE FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 826AL 23051 FUSELAGE SHEAR TIE CRACK AT BS 460, S-17L. PERFORMED TRIMOUT TO DAMAGED AREA. HFEC INSPECTION COMPLETED NO DEFECTS NOT ED, FABRICATED AND INSTALLED NEW T-CHORD IAW ECO. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2002110700090 20021107 00090 SO 2002 11 7 UC22002F00004 1 20021028 A 1430 COTTER PIN PIPER PA28 PA28181 7102807 SO LYC O360 O360* 41514 EA COCKPIT FAILED B UC2R O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 19 4144K 2843145 DURING TRAINING FLIGHT, THE PILOTS RIGHT RUDDER PEDAL WAS REPORTED TO BE UNRESPONSIVE DURING FLIGHT. THE PILOT LANDED T HE AIRPLANE WITHOUT AN INCIDENT. UPON INSPECTION OF THE PILOTS RIGHT RUDDER PEDAL AND THE TOE BRAKE ASSEMBLY THE CLEVIS ASSY WAS FOUND DISCONNECTED FROM THE IDLER ARM AND BRAKE CYLINDER. THE CLEVIS PIN WAS FOUND ALONG SIDE OF THE COTTER P IN ON THE CABIN FLOOR. REPLACED ALL OF THE COTTER PINS. 1 L 7 1 3O 3 O 2A13 E286 2002111800132 20021118 00132 EU 2002 11 18 USAASA02084 1 20021011 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 113UW 1141 DCA - THE EMERGENCY LIGHT SYSTEM FAILED TEST. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECK S OK. (M) 2 L 7 2 4F RT A28NM 2002110700091 20021107 00091 EU 2002 11 7 USAASA02086 1 20021014 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 716UW 1055 FOUND EMERGENCY LIGHTS AT SEATS 17ABC, 19ABC, AND 21ABC INOPERATIVE. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPL Y UNIT. OPERATIONALLY CHECKED, OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2002110700092 20021107 00092 NM 2002 11 7 USAASB02189 1 20021017 A 3260 BR20AXH5V3 RELAY BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE E/E BAY FAULTY A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 449US 24893 IN PREPARATION FOR LANDING, CREW RECEIVED BOTH THE RED AND GREEN NOSE LANDING GEAR LIGHTS AFTER GEAR EXTENSION. AFTER R ECYCLING GEAR SEVERAL TIMES, CREW RECEIVED NORMAL GEAR INDICATION. FLIGHT LANDED NORMALLY, WITHOUT FURTHER INCIDENT. M AINTENANCE REMOVED AND REPLACED THE R374 NOSE GEAR LATCHING RELAY IAW MM. OPERATIONAL CHECK AND INDICATION CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700007 20021127 00007 NM 2002 11 27 2002UALA01599 1 20021016 A 7931 41820044 TRANSMITTER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 334UA 39181 24229 AIRCRAFT DIVERTED EN ROUTE WHEN ENGINE NR 2 OIL PRESSURE INDICATOR SHOWED 0 PSI. OIL PRESSURE LIGHT WAS NOT ILLUMINATED . THE PROBLEM WAS ISOLATED TO THE OIL PRESSURE TRANSMITTER. IT WAS REPLACED AND SENT TO THE SHOP FOR TESTING. THE TRA NSMITTER FAILED SHOP TEST AND WAS SCRAPPED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002110700093 20021107 00093 WP 2002 11 7 ZW0A0209801 1 20020921 A 2450 SOCKET DOUG DC9 DC982 3022082 WP CABIN SHORTED A ZW0A K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 13 958U 49703 ELECTRICAL ODOR WAS COMING FROM THE PANEL BEHIND THE FWD FLIGHT ATTENDANT SEAT. FOUND A SHORTED SOCKET AT TERMINAL STRI P S3-23 THAT HAD SHORTED OUT THE WIRING TO R2-41. THE AIRCRAFT MAINTENANCE FERRIED TO MCI WHERE WIRING CORRECTIONS WERE MADE. 2 L 7 2 4F A6WE 2002110700094 20021107 00094 NM 2002 11 7 2002UALA01625 1 20021008 A 5754 114W472012 WEDGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE #13 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 DELAMINATED T/E WEDGE, #13 SLAT MAJOR REPAIR ACCOMPLISHED. AD 2002-11-02 ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002110700095 20021107 00095 NM 2002 11 7 2002UALA01626 1 20021008 A 5754 114W472012 WEDGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE #12 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 TRAILING EDGE WEDGE DELAMINATED, #12 SLAT MAJOR REPAIR ACCOMPLISHED. AD 2002-11-02 ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002110700096 20021107 00096 NM 2002 11 7 2002UALA01627 1 20021008 A 5754 114W422011 WEDGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE #2 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 T/E WEDGE DELAMINATED, #2 SLAT. MAJOR REPAIR ACCOMPLISHED. AD 2002-11-02 ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002110700097 20021107 00097 NM 2002 11 7 2002UALA01630 1 20021026 A 5753 FLAP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 LEFT WING INBOARD TRAILING EDGE FLAP, MID SUPPORT CRACKEDAT OUTBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. REPAIRED AFT FL AP TO MID FLAP SUPPORT HINGE. 2 L 7 2 4F 4 F RT A1NM E3NE 2002110700098 20021107 00098 NM 2002 11 7 2002UALA01633 1 20021030 A 5315 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STA 968 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 RH MID CABIN STA 968.5 TO 969.5 RH CREASE BEAM WEB UPPER SURFACE CORRODED. MAJOR REPAIR ACCOMPLISHED.REPLACED CREASE BE AM WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002110700099 20021107 00099 WP 2002 11 7 ZW0A0209901 1 20020923 A 5553 ATTACH ANGLE DOUG DC9 DC983 3022083 WP VERTICAL STAB CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 931TW 49527 THE RT DORSAL ATTACH ANGLE HAD A .5 INCH CRACK IN VERTICAL LEG THAT EXTENDED INTO THE RADIUS OF THE HORIZONTAL LEG. REP LACED RT DORSAL FIN ATTACH ANGLE PER M072R22. 2 L 7 2 4F RT A6WE 2002110700100 20021107 00100 WP 2002 11 7 ZW0A0209902 1 20020923 A 5553 ATTACH ANGLE DOUG DC9 DC983 3022083 WP VERTICAL STAB CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 931TW 49527 THE LT DORSAL ATTACH ANGLE HAD A .25 INCH CRACK IN VERTICAL LEG. REPLACED LT DORSAL FIN ANGLE PER MO72R22. 2 L 7 2 4F RT A6WE 2002110700101 20021107 00101 WP 2002 11 7 ZW0A0210202 1 20020929 A 2120 ODOR DOUG DC9 DC983 3022083 WP CABIN DETECTED A ZW0A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 13 9403W 53139 A VERY STRONG FUEL ODOR WAS REPORTED IN COCKPIT AND SLIGHTLY IN C ABIN. FLIGHT RETURNED TO STL. UNABLE TO FIND ANY FUEL LEAK. CHANGED THE WATER SEPERATORS AND ACCOMPLISHED A PACK BURN OUT TO ELIMINATE THE ODOR. 2 L 7 2 4F RT A6WE 2002110700102 20021107 00102 WP 2002 11 7 ZW0A0210203 1 20020929 A 2780 CONTROL CABLE DOUG DC9 DC982 3022082 WP L/E SLAT OUT OF RIG A ZW0A O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CE 13 951U 49245 WHEN FLAPS EXTENDED TO 15 DEGREES THE SLAT DISAGREE LIGHT ILLUMINATED. DURING APPROACH SLAT DISAGREE LIGHT CONTINUED TO INTERMITTENTLY CHANGE BETWEEN OFF AND DISAGREE. NO ASYMMETRY IN FLIGHT CONTROLS WAS NOTICED. RIGGED SLAT FOLLOW UP CA BLES PER MM 27-81-02. 2 L 7 2 4F A6WE 2002110700103 20021107 00103 WP 2002 11 7 ZW0A0210302 1 20021006 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN NOT SEATED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9402W 53138 THE EGRESS LIGHT STRIP IN THE FWD SECTION OF COACH WAS INOPERATIVE. OPERATED MEL ONE LEG AND THEN THE BATTERIES IN THE POWER SUPPLY WERE PROPERLY SEATED. 2 L 7 2 4F RT A6WE 2002110700104 20021107 00104 WP 2002 11 7 ZW0A0210401 1 20021008 A 3350 58222 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 9305N 49395 THE EGRESS LIGHTING BETWEEN ROWS 15 TO 21 WERE FLASHING ON AND OFF DURING FLIGHT. REPLACED THE POWER SUPPLY. 2 L 7 2 4F RT A6WE 2002110700105 20021107 00105 NM 2002 11 7 ZW0A0210501 1 20021013 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN CONTAMINATED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 720TW 30319 THE EGRESS LIGHTS WERE INOPERATIVE FROM CABIN ROWS 26 TO 33. REMOVED MOISTURE FROM EGRESS LIGHT STRIP. 2 L 7 2 4F RT A2NM 2002110700106 20021107 00106 WP 2002 11 7 ZW0A0210502 1 20021014 A 2530 8201514000D OVEN DOUG DC9 DC983 3022083 WP GALLEY MALFUNCTIONED A ZW0A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 13 967TW 53617 STRONG ELECTRICAL SMELL WAS NOTICED IN COCKPIT AND FORWARD GALLEY. SHUT OFF GALLEY POWER AND SMELL DISSIPATED. REPLACE D THE NUMBER 2 GALLEY OVEN. 2 L 7 2 4F RT A6WE 2002110700107 20021107 00107 WP 2002 11 7 ZW0A0210602 1 20021015 A 2780 CONTROL CABLE DOUG DC9 DC982 3022082 WP L/E SLAT BROKEN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 952U 49266 DURING OVERNIGHT MAINTENANCE CHECKS THE NUMBER 5 L/E SLAT RETRACT CABLE WAS FOUND BROKEN. REPLACED THE CABLE. 2 L 7 2 4F A6WE 2002110700108 20021107 00108 NM 2002 11 7 ZW0A0210603 1 20021017 A 3350 BATTERY PACK DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9420D 49824 FOUND OVERWING EMERGENCY LIGHTS AND TWO EGRESS LIGHTS INOPERATIVE. REPLACED THE OVERWING LIGHT BATTERY PACK AND TWO EGR ESS LAMPS. 2 L 7 2 4F RT 2002110700109 20021107 00109 WP 2002 11 7 ZW0A0210604 1 20021018 A 3350 58222 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9625W 53595 CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE R5-205 AND R5-209 BATTERY PACKS. 2 L 7 2 4F RT A6WE 2002110700110 20021107 00110 WP 2002 11 7 ZW0A0210605 1 20021016 A 5712 RIB DOUG DC9 DC983 3022083 WP RT WING CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9307R 49663 DURING CHECK-C MAINT ON THE RT WING LEADING EDGE, STA 410, FOUND A RIB CRACKED IN 2 PLACES AT CABLE ACCESS. CRACKS WERE STOP DRILLED AND REPAIRED WITH DOUBLER PER SRM 57-10-F3. 2 L 7 2 4F RT A6WE 2002110700111 20021107 00111 2002 11 7 ZW0A0210701 4 20021021 A 3418 TRANSMITTER DOUG DC9 DC982 3022082 WP STALL WARNING MALFUNCTIONED A ZW0A L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CE 13 905TW 49157 ON APPROACH WHEN FLAPS SELECTED TO 40 GOT SLAT DISAGREE LIGHT. SLOWED DESCEND RATE AND GOT STICK SHAKER. ACCOMPLISHED GO AROUND. SECOND APPROACH WAS NORMAL. REPLACED LEFT AOA TRANSMITTER AND PLUNGER ASSEMBLY FOR THE LEFT NUMBER 1 SLAT P ROX SENSOR TARGET ASSY. 2 L 7 2 4F A6WE 2002110700112 20021107 00112 WP 2002 11 7 ZW0A0210803 1 20021027 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 950U 49230 THE EMERGENCY LIGHTS IN THE CEILING AT ROWS 23 TO 26, AND THE AFT OVER WING EXIT SIGN WAS INOPERATIVE. REPLACED THE BAT TERIES IN THE BATTERY PACK FOR THE CEILING LIGHTS AND REPLACED THE BATTERIES FOR THE OVERWING EXIT. 2 L 7 2 4F A6WE 2002110700113 20021107 00113 WP 2002 11 7 ZW0A0210804 1 20021023 A 5730 SKIN DOUG DC9 DC983 3022083 WP LT WING DENTED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 980TW 53630 DURING CHECK-C MAINT THE LT WING FIXED LE 15 INCHES AND 19 INCHES OTBD FROM 0 SLAT OTBD TRACK, FOUND DENT IN LE. INSTAL LED REPAIR PER SRM 57-06B, FIG 14. 2 L 7 2 4F RT A6WE 2002110700114 20021107 00114 NM 2002 11 7 ZW0A0210901 1 20021028 A 3350 1056005 MODULE DOUG MD80 MD83 3023681 NM CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9630A 53561 THE EGRESS LIGHTS WERE INOPERATIVE FROM SEAT ROW 26 TO 28. REPLACED LAMP MODULE ASSEMBLY. 2 L 7 2 4F RT 2002110700115 20021107 00115 WP 2002 11 7 ZW0A0211001 1 20021011 A 2120 DUCT DOUG DC9 DC983 3022083 WP HEAT EXCHANGER WORN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 980TW 53630 DURING CHECK-C MAINT THE FUSELAGE RT SIDE OVERBOARD DUCT FOR THE HEAT EXCHANGER WAS WORN THIN. REPAIRED PER SSRM 53-30- 101. REPLACED DUCT PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2002110700116 20021107 00116 WP 2002 11 7 ZW0A0211002 1 20021011 A 2120 DUCT DOUG DC9 DC983 3022083 WP HEAT EXCHANGER WORN A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 980TW 53630 DURING CHECK-C MAINT THE FUSELAGE LT SIDE OVERBOARD DUCT FOR THE HEAT EXCHANGER WAS WORN THIN. REPAIRED DAMAGE PER SSRM 53-30-101 PAGE 202. REPAIRED AND REPLACED DUCT PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 2002110700117 20021107 00117 WP 2002 11 7 ZW0A0211003 1 20021010 A 5320 CHANNEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9307R 49663 DURING CHECK-C MAINT THE NOSE LANDING GEAR WHEEL WELL STA 46, RBL 18 INCHES, HAD CHANNEL CRACKED ON OTBD SIDE AT FASTENE R. STOP DRILLED AND OK PER EDDY CURRENT PART 6-51-00-03. STOP DRILLED AND REPAIRED PER SRM 53-01, PAGE 10. 2 L 7 2 4F RT A6WE 2002110700118 20021107 00118 WP 2002 11 7 ZW0A0211004 1 20021010 A 5320 CHANNEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9307R 49663 DURING CHECK-C MAINT THE NOSE LANDING GEAR WHEEL WELL STA 46, LBL 18 INCHES, HAD CHANNEL CRACKED ON OTBD SIDE AT FASTENE R. EDDY CURRENT INSPECTED AND CRACKS CONTAINED. INSTALLED DOUBLER PER SRM 53-01. 2 L 7 2 4F RT A6WE 2002110700119 20021107 00119 NM 2002 11 7 ZW0A0211101 1 20021104 A 3350 BATTERY PACK BOEING 757 7572Q8 1384972 NM CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 712TW 27624 THE LEFT SIDE NUMBER 4 CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. THE POWER SUPPLY AND BATTERY PACK WERE REPLACED. 2 L 7 2 4F RT A2NM 2002110700120 20021107 00120 NM 2002 11 7 UPS02M39351 1 20020807 A 5330 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP INSPECTION TYPE:C CABIN - UPPER AUX UPPER EXTERNAL SKIN HAS SURFACE CORROSION IN NINE PLACES FROM STA 1341 TO 1375 X=65 TO X=90.00. UPPER EXT SKIN SURFACE CORRODED CLEANED AND FOUND 2EA DOUBLERS EXCEEDED LIMIT IAW SRM 57-00-01 FIG 1A VOL I . DOUBLER FABRICATED IAW DWG APB7241 & INSTALLED IAW SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2002110700121 20021107 00121 NM 2002 11 7 UPS02M39421 1 20020812 A 5347 AFA7789542 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP INSPECTION TYPE:C CORROSION FOUND ON SEAT TRACK CROWN AT STA 1964 X=-107. SEAT TRACK CORROSION EXCEEDS LIMIT IAW SRM 53 -70-00 FIG 3 VOL 1. SEAT TRACK REMOVED PER SRM 51-31-01. SPLICE HAT AND PLATE FABRICATE IAW SRM 53-70-00 FIG 1. INSTA LLED PER SRM 53-70-00 FIG 1 & 51-31-01. 2 L 7 3 4F RT A22WE 2002110700122 20021107 00122 NM 2002 11 7 UPS02M39422 1 20020807 A 5315 FLOORBEAM DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP INSPECTION TYPE:C CABIN FLOORBEAM HAS SURFACE CORROSION AND FASTENERS CORRODED AT STA 1361 X=115.00 TO X=107.25. FLOORB EAM AREA CORROSION BLENDED OUT AND FOUND EXCEEDS LIMIT PER SRM 53-00-01 VOL I. 2 L 7 3 4F RT A22WE 2002110700123 20021107 00123 NM 2002 11 7 751PA0007 1 20021101 A 3350 WIRE BOEING 757 757200 1384950 NM A PIDA K NONE O OTHER UK UNKNOWN 1 SO 05 751PA 23928 F/A report - several emergency path lights inop - mid cabin. Insp lights found broken wire - repaired & ops check good per MM 33-51-00 2 L 7 2 4F RT A2NM 2002110700124 20021107 00124 NM 2002 11 7 UPS02M39529 1 20020826 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP INSPECTION TYPE:C CRACK FOUND ON OUTBOARD FLANGE OF FRAME AT SPLICE AREA STA 495 BETWEEN L13L TO L14L. CABIN STA 495 BE TWEEN L13L-L14L O/B FRAME FLANGE CRACK AREA TRIMMED OUT AS PER EN NR 1110-02. FILLER FABRICATE AND INSTALLED AS PER EN NR 1110-02. 2 L 7 3 4F RT A22WE 2002110700125 20021107 00125 EU 2002 11 7 XNOA01071 1 20020925 A 2780 BRAKE AIRBUS 300 A300B4203 3930306 EU L/E SLAT MALFUNCTIONED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 370PC 134 ON TAXI SLATS FAIL TO EXTEND TO TAKEOFF POSITION. R&R RT SLAT FRICTION BRAKE IAW A300 MM CHAPT 27-81-47. OPS CHECK GOO D IAW A300 MM 27-81-00. 2 L 7 2 4F RT A35EU 2002110700126 20021107 00126 EU 2002 11 7 XNOA01074 1 20020927 A 2613 MODULE AIRBUS 300 A300B4203 3930306 EU OVERHEAT WARNING MALFUNCTIONED A XN0A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 370PC 134 MAIN DECK LOOP LIGHTS WARNING. CLEANED AND RERACKED MAIN DECK OVERHEAT DETECTION MODULE. OPS CHECKS GOOD IAW A300 MM 2 6-16-00. 2 L 7 2 4F RT A35EU 2002110700127 20021107 00127 EA 2002 11 7 COMA0260632 1 20021105 A 2613 35962255 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 811CA 7380 FLIGHT 5393 ANTI-ICE DUCT MESSAGE.REPLACED DEFECTIVE SECTION OF BLEED AIR DUCT LEAK SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2002110700128 20021107 00128 EA 2002 11 7 COMA0260633 1 20021105 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 951CA 7091 FLIGHT 5574 FLAPS FAIL CAUTION MESSAGE DURING LANDING.RESET THE FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002110700129 20021107 00129 EU 2002 11 7 MALA020638 1 20021105 A 3230 AIR130902 DOWNLOCK SWITCH SAAB SF340 340B 7860101 EU A MALA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 GL 15 370PX 340B300 DURING APPROACH OF FLIGHT #3189 TO BRD, THE RIGHT MAIN GEAR DIDN'T ILLUMINATED. WE PUSHED THE TEST SWITCH AND THE LIGHT S ALL TESTED OKAY ON GO-AROUND THE RIGHT GEAR LIGHT ILLUMINATED BY ITSELF. CREW LEFT THE GEAR DOWN THROUGH THE WHOLE TIM E. MAINTENANCE REMOVED AND REPLACED MLG DOWN LOCK SWITCH IAW 32-61-05-2 PN AIR130902. OPS CHECK OK. 2 L 7 2 4T RT A52EU 2002110700130 20021107 00130 NM 2002 11 7 ANCF200200024 1 20021014 A 5600 S141T4871 SEAL BOEING 767 767259 1385136 NM Zone 200 DAMAGED W ANCF D RETURN TO BLOCK O OTHER CR CRUISE 1 SO 23 986AN 24835 DURING CRUISE WITH A DIFFERENTIAL PRESSURE OVER 4.5, THERE IS A LOUDLY NOISE COMING OUT OF 2L WINDOW. MASKING CREW AND A TC COMMUNICATIONS IMPOSSIBLE, CREW DECIDED TO RETURN TO EDR.CORRECTIVE ACTION:WAS FOUND 2L WINDOW SEAL DAMAGED, CAUSING A PRESSURIZATION LEAK, REMOVED AND REPLACED 2L WINDOW SEAL IAW AMM 56-11-11 PAG 401, PERFORMED PRESSURIZATION LEAK TEST IAW AMM 05-51-24 PAG 201 TO 209, WITH SATISFACTORY RESULTS. 2 L 7 2 4F RT A1NM 2002110700131 20021107 00131 NM 2002 11 7 ASAA0210200 1 20020930 A 5320 BAC1496364 SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT AT FUSELAGE BODY STATION 500-500A, STRINGER 26R CORRODED . REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT PER SRM. (M) 2 L 7 2 4F RT A16WE 2002110700132 20021107 00132 EA 2002 11 7 SWIA200211410 1 20021027 A 2751 BPSU CNDAIR CL600 CL6002B19 1900309 EA RIGHT OUT OF RIG A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 442SW 7609 ''FLAPS FAIL'' DURING DESCENT AT ZERO DEGREES. LANDED WITH FLAPS ZERO DEGREES.COMPLIED WITH AD 98-20-01/03 MAINTENANCE ACTION. FOUND ASYMMETRY AND BPSU PROBLEMS. RIGGED RIGHT BPSU IAW MM 27-51-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002110700133 20021107 00133 EA 2002 11 7 SWIA200211413 1 20021104 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA CAPTAIN'S CRACKED A SWIA O OTHER P NO WARNING INDICATION DE DESCENT 1 NM 07 591SW 7079 CAPTAIN'S SIDE WINDSHIELD CRACKED DESCENDING INTO BNA. APPEARED TO BE AN ELECTRICAL SHORT LOW IN THE WINDSHIELD AT THE CENTER PRIOR TO THE CRACK. REMOVED AND REPLACED LEFT WINDSHIELD WITH SERVICEABLE UNIT IAW MM 56-11-01 OPS CHECK & LEAK CHECK GOOD. PN OFF/ON NP-139321-9 SN OFF 85 114H6827. 2 L 7 2 4F RT A21EA 2002110800001 20021108 00001 NM 2002 11 8 ANCF200200023 1 20021105 A 5270 WARNING SYSTEM BOEING 767 767259 1385136 NM E/E DOOR FALSE ACTIVATION W ANCF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 23 985AN 24618 E/E ACCESS DOOR EICAS MESSAGE DISPLAYED DURING TAKE OFF AT MAD, TAKE OFF WAS REJECTED AND RETURNED BACK TO APRON. CHECK ED FOR MATERIAL OR BLOCKAGES FROM ALL OF THE ELECTRONIC ACCESS DOOR LATCH PINS AND LATCH FITTINGS, PERFORMED FIM 52-71-0 0/101 FIG 106 BLOCK 1 TO 3 AND FIM 32-09-03/101 FIG 103 BLOCK 1 TEST ON GROUND NORMAL. 2 L 7 2 4F RT A1NM 2002110800002 20021108 00002 NE 2002 11 8 AUS20021078 2 20020926 A 7200 PT6A42 ENGINE BEECH 200 B200C 1152924 CE PWA PT6 PT6A42 52043 NE HARTZL HCB3T HCB3TN3 GL RIGHT SEIZED W O OTHER E Y J VIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 AU S 2944 (AUS) RT ENGINE SUFFERED AN IN FLIGHT FAILURE WITH THE ENGINE SEIZING. INSPECTION FOUND A CRACK IN THE COMPRESSOR SECTIO N INTAKE HOUSING WITH OIL POOLING IN THE EXHAUST SECTION. CRACK LENGTH 50.8MM TO 63.5MM (2IN TO 2.5IN). 1 L 7 2 4T 4 T A24CE E4EA 6 C P15EA 2002110800003 20021108 00003 NE 2002 11 8 AUS20021080 2 20020927 A 8530 STUD DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE ENGINE CYLINDER FAILED W O OTHER E VIBRATION/BUFFET DE DESCENT 1 AU S 881 (AUS) NR 5 CYLINDER BASE STUDS FAILED ALLOWING CYLINDER TO SEPARATE FROM THE CRANKCASE. THE CYLINDER REMAINED ATTACHED T O THE ENGINE BY INTAKE AND EXHAUST PIPES. THE PISTON OIL SCRAPERRING CAME OUT OF THE CYLINDER BARREL AT THE BOTTOM OF TH E PISTON STROKE AND BROKE. 1 H 7 1 3R 3 R A806 5E1 2002110800004 20021108 00004 EU 2002 11 8 AUS20021083 1 20020929 A 3244 TIRE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A67R 52043 NE HARTZL HCA6A HCA6A3 NE RT MLG FAILED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AU S LJ110 (AUS) RH MAIN LANDING GEAR TIRE BLEW. NO STRUCTUAL DAMAGE FOUND. 2 H 7 2 4T 4 T A41EU E26NE 6 C P14NE 2002110800005 20021108 00005 NM 2002 11 8 AUS20021084 1 20020927 A 3244 TIRE BOEING 747 747400 NM GE CF6 CF680C2* GL NR 5 FAILED W O OTHER O OTHER TO TAKEOFF 1 AU S (AUS) MAIN LANDING GEAR NR 5 REAR TIRE TREAD SEPARATED. SIGNIFICANT IMPACT DAMAGE OCCURRED TO THE ADJACENT COMPOSITE FAI RINGS. 2 L 7 4 4F 4 F RT A20WE E23EA 2002110800006 20021108 00006 SW 2002 11 8 AUS20021085 1 20020905 A 2750 246003 SOLENOID VALVE SWRNGN SA227 SA227AT 8780610 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED CL CLIMB 1 AU S (AUS) FLAP SOLENOID VALVE FAULTY. VALVE COIL HAD SHORT CIRCUITED. VALVE IS LOCATED IN HYDRAULIC POWER PACK. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C P61GL 2002110800007 20021108 00007 NM 2002 11 8 AUS20021086 1 20020220 A 7500 PNEUMATIC SYSTEM BOEING 767 767330 NM RROYCE RB211 RB211524* NE ENGINE BLEED AIR FAULTY W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 AU S (AUS) PNEUMATIC SYSTEM FAULTY. LIMITED INFORMATION PROVIDED. 2 L 7 2 4F 4 F RT A1NM E12EU 2002110800008 20021108 00008 NM 2002 11 8 AUS20021088 1 20021001 A 2421 711358 RELIEF VALVE BOEING 737 737800* NM GE CFM56 CFM567B24 NE IDG SEPARATED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) INTEGRATED DRIVE GENERATOR (IDG) CHARGE RELIEF VALVE SEPARATED FROM IDG. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002110800009 20021108 00009 NM 2002 11 8 AUS20021089 1 20021003 A 2597 WIRE BOEING 747 747438 NM RROYCE RB211 RB211524* NE GALLEY CHAFED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) GALLEY CHILLER WIRING CHAFED AND BURNED IN AREA ADJACENT TO THECURRENT DETECTOR Y7JR001. 2 L 7 4 4F 4 F RT A20WE E12EU 2002110800010 20021108 00010 SW 2002 11 8 AUS20021090 1 20021002 A 2910 27810322682 PIPE SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UHR WP MCAULY 4HFR34 4HFR34C652 NE HYD SYSTEM CHAFED W O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AU S 10475 (AUS) LT ENGINE DRIVEN HYDRAULIC PUMP ALUMINIUM SUPPLY LINE CHAFING ON A STAINLESS STEEL FUEL LINE. THE HYDRAULIC LINE C HAFED THROUGH RESULTING IN LOSS OF HYDRAULIC FLUID. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002110800011 20021108 00011 SW 2002 11 8 AUS20021091 1 20021002 A 2910 27810322755 PIPE SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UHR WP MCAULY 4HFR34 4HFR34C652 NE HYD SYSTEM LOOSE W O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 AU S 10476 (AUS) HYDRAULIC SYSTEM PIPE FROM FIREWALL DISCONNECTED. LOSS OF HYDRAULIC FLUID. PERSONNEL/MAINTENANCE ERROR. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002110800012 20021108 00012 SW 2002 11 8 AUS20021092 1 20021002 A 2424 51539005B GCU SWRNGN SA227DC SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UHR WP MCAULY 4HFR34 4HFR34C652 NE AC REGULATOR FAILED W O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 AU S 601 DC873B (AUS) LT GENERATOR CONTROL UNIT (GCU) FAILED. SUSPECT GCU FAILED DUE TO WATER INGRESS FOLLOWING ENGINE WASH. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002110800013 20021108 00013 SW 2002 11 8 AUS20021093 1 20021002 A 3234 27190935 SELECTOR VALVE SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UHR WP MCAULY 4HFR34 4HFR34C652 NE MLG FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S 10476 (AUS) EMERGENCY LANDING GEAR SELECTOR VALVE LEAKING. SUSPECT CAUSED BYINTERNAL SEAL FAILURE. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002110800016 20021108 00016 SW 2002 11 8 AUS20021097 1 20021002 A 2932 HOUSING SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UA 01514 WP MCAULY 4HFR34 4HFR34C652 NE HYD TRANSDUCER UNSERVICEABLE W O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 AU S (AUS) HYDRAULIC PRESSURE TRANSDUCER HOUSING SPLIT. TRANSDUCER ISLOCATED IN LT NACELLE 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002110800019 20021108 00019 NM 2002 11 8 AUS20021100 1 20021007 A 7740 WARNING SYSTEM BOEING 767 767330 NM RROYCE RB211 RB211524* NE COCKPIT EICAS FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 AU S (AUS) LOSS OF EICAS SCREEN INFORMATION. A 18 CIRCUIT BREAKER ON PANEL P6 OUT. 2 L 7 2 4F 4 F RT A1NM E12EU 2002110800020 20021108 00020 EA 2002 11 8 SWIA200211340 1 20020913 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FOUND CRACK ON RIGHT AND LEFT SIDES OF FLOOR IN THE FORWARD EQUIPMENT COMPARTMENT AT FS 193.00, WL 79.50. FOUND DURING C CHECK INSPECTION. HDT-HFEC CARRIED OUT IAW CLIENT REQUEST AND NDTM PART 1, 51-20-01. NO CRACKS NOTED. DAMAGE REPAIR ED IAW REO 601R-53-11-334. 2 L 7 2 4F RT A21EA 2002110800021 20021108 00021 NM 2002 11 8 02310414 1 20021106 A 7540 30B303303 TRANSDUCER DORNER DO32 DO328300 NM A VTZA E A ENGINE SHUTDOWN UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 EA 27 414FJ 3169 During climb of the flight, at 2500' AGL, the crew heard a loud "pop" and noticed that the r/h engine instruments were r olling back. The crew secured the engine, returned to PHL, and landed without further incident. Maintenance personnel performed a borescope inspection of the r/h engine with no adverse findings. The p3 pressure transducer was removed and replaced, engine run operational checks and a maintenance acceptance flight (MAF) were satisfactory. The aircraft was returned to service. 2 H 7 2 4T RT A55NM 2002110800022 20021108 00022 EA 2002 11 8 02311621 1 20021107 A 3350 3071BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 621BR 7186 During overnight maintenance, it was discovered that the forward cabin overhead emergency exit light was inoperative. M aintenance personnel removed and replaced the lamp in the forward cabin overhead emergency exit light. An operational c heck was satisfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002110800023 20021108 00023 EA 2002 11 8 SWIA200211421 1 20021101 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 07 403SW 7028 UPON ROTATION WE RECEIVED A SERVICE DOOR CAUTION MESSAGE. RETURNED TO SLC. ON THE DOWNWIND, THE LIGHT DID EXTINGUISH W HEN THE POWER WAS RETARDED. FOUND INNER DOOR WITH PROX SENSOR LOOSE. SECURED HANDLE. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2002110800024 20021108 00024 EA 2002 11 8 02311621A 1 20021107 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 621BR 7186 During overnight maintenance, it was discovered that the mid-cabin emergency exit light was inoperative. Maintenance pe rsonnel removed and replaced the lamp in the emergency exit light. An operational check was satisfactory and the aircra ft was returned to service. 2 L 7 2 4F RT A21EA 2002110800025 20021108 00025 EA 2002 11 8 SWIA200211341 1 20020913 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FOUND FS 484 RIGHT INTERCOSTAL RBL 27 ANGLE CRACKED. FOUND DURING C CHECK INSPECTION. NEW ANGLES FIT AND INSTALLED IAW CRJ REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2002110800026 20021108 00026 SO 2002 11 8 SWIA200211343 1 20021013 A 5310 DOOR FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 FRAME 13A DAMAGED AT DOOR ACTUATOR MOUNT. EXTENSIVE DAMAGE TO SHEAR CLIP 120-29047-001 AND SEVERAL OTHER TIPPED AND DAM AGED RIVETS OUTBOARD OF SHEAR CLIP. AT FRAME 13A, REMOVED AND REPLACED THE DAMAGED SHEAR CLIPS AND DAMAGED RIVETS IAW E MB SRM 51-00-00, 51-40-02, 53-00-03 AND 53-00-04, RII 53-301. 2 L 7 2 4T RT A31SO 2002110800027 20021108 00027 EA 2002 11 8 SWIA200211344 1 20020913 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FOUND RIGHT FRAME FS 640.0 STR 9R CRACK AT STR CUTOUT DURING C CHECK INSPECTION. REPAIRED DAMAGE AREA OF FRAME IAW CRJ REO 601R-53-61-532. NDT-HFEC CARRIED OUT IAW REO 601R-53-61-532. NO CRACKS NOTED. 2 L 7 2 4F RT A21EA 2002110800028 20021108 00028 EA 2002 11 8 SWIA200211345 1 20021018 A 2760 4916405 ECU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA C ABORTED TAKEOFF F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 437SW 7564 DURING TAXI INTO POSITION FOR TAKEOFF ALL GROUND SPOILERS DEPLOYED. REPLACED NR 1 SECU DUE TO SYSTEM TEST UNCOMMANDED. REMOVED & REPLACED IAW 27-60-01. 2 L 7 2 4F RT A21EA 2002110800029 20021108 00029 SO 2002 11 8 C2XA02BT070 1 20021107 A 3200 355022002MOD3 CONTROL UNIT EMB 145 EMB145LR 3260212 SO COCKPIT AREA INTERMITTENT A C2XA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 27 13550 145575 EWR---CO4349, CREW REPORTED "AIR RETURN--LANDING GEAR WOULD NOT RETRACT" MAINTENANCE TROUBLESHOT LANDING GEAR CONTROL S YSTEM AND FOUND INTERMITTENT LGEU FAILURE INDICATIONS IN CMC. CHECKED LANDING GEAR EXTENSION CIRCUIT AND PROXIMITY SWITC HES. NO DEFECTS NOTED. REMOVED AND REPLACED LGEU. SWUNG GEAR SEVERAL TIMES WITH NO DEFECTS NOTED. IAW EMB145 AMM. OPS. C HECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002110800032 20021108 00032 WP 2002 11 8 MWEA020670 1 20021108 A 5311 59101413 DOUBLER DOUG DC9 DC914 3022034 WP AFT CARGO DR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 AFT CARGO DOOR DOUBLER AT HANDLE IS CRACKED. -- FABRICATED NEW REPAIR DOUBLER, INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 2002110800033 20021108 00033 EU 2002 11 8 02FDEA00699 1 20020925 A 2722 ACTUATOR AIRBUS 310 A310 EU RUDDER MALFUNCTIONED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 420FE 339 RUDDER TRAVEL SYSTEM TWO FAULTED IN FLIGHT, FAULTED PASSING 170KIAS. REPLACED NR 2 ADC PER A310 MM34-11-34. OPERATIONA L CHECK AND PITOT/STATIC LEAK TEST GOOD. R&R RUDDER VARIABLE STOP ACTUATOR AS PER A-310, MM 27-23-23-4. R&R NR 1 FEEL LIMITATION COMPUTER IAW A310 MM 27-23-26. ACCOMPLISHED TESTS PER A310 MM 27-23-00-5. NO FAULT ON BOTH SYSTEM OF PITCH FEEL AND RUDDER TRAVEL. 2 L 7 2 4F RT A35EU 2002110800034 20021108 00034 NM 2002 11 8 02FDEA00702 1 20021003 A 2613 WARNING SYSTEM BOEING 727 727200 138407E NM OVERHEAT SYS MALFUNCTIONED A FDEA K NONE N FALSE WARNING CR CRUISE 1 SO 25 268FE 21674 LOWER AFT BODY OVERHEAT LIGHT BRIEFLY ILLUMINATED DURING FLIGHT. LIGHT FLICKERED ON AND THEN EXTINGUISHED APPROX 45 SEC ONDS ON THEN OFF FOR REMAINDER OF FLIGHT. INSPECTED RIGHT AND LEFT SECTION 48 OVERHEAT DETECTOR AND KEEL BEAM OVERHEAT DETECTOR, LIGHTLY PULLED DETECTORS WHILE OTHER MECHANIC MONITORED OVERHEAT LIGHT IN COCKPIT AT F/E PANEL LIGHT NEVER C AME ON, ALSO INSPECTED AFT CARGO COMPARTMENT FOR EVIDENCE OF HEAT DAMAGE AND PNEUMATIC AIR LEAK, NONE FOUND, PERFORMED A FUNCTIONAL CHECK PER M/M 26-14-001-2 A/C OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2002110800041 20021108 00041 EU 2002 11 8 02FDEA00717 1 20020923 A 5511 A55177561 SPAR AIRBUS 310 A310 EU HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 BOTH L&R HORIZ STAB UPR & LWR CHORDS OF SPAR CORRODED ENTIRE LENGTH. R&R CHORD PER SRM 55-11-21. 2 L 7 2 4F RT A35EU 2002110800042 20021108 00042 EU 2002 11 8 02FDEA00718 1 20021005 A 3340 LIGHT AIRBUS 300 A300F4605R 3930327 EU RIGHT MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 660FE 759 DURING WALK AROUND FOUND RT SIDE LANDING LIGHT MISSING BULB. RELAMPED THE BULB IAW A300-600 AMM 33-42-21-4. OPS CHECKS NORMAL AT THIS TIME. A/C IS OKAY FOR SERVICE AT THIS TIME. 2 L 7 2 4F RT A35EU 2002110800043 20021108 00043 WP 2002 11 8 02FDEA00719 1 20021009 A 5610 SEAL DOUG DC10 DC1010 3022110 WP COCKPIT LEAKING A FDEA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 68050 47804 F/O WINDOW LOCKING BOLT WAS OUT OF POSITION DURING INITIAL CLIMB-OUT. LOUD NOISE FROM AIR LEAK. RETURNED TO LAND AT MS P, DUMPED 10,000 LBS FOR LANDING WEIGHT. REINSTALLED RT SLIDING WINDOW SEAL PER STD PRAC & DC10-10 AMM 56-12-00-4. OPE RATIONAL CHECK OF RT SLIDING WINDOW NORMAL PER DC10-10 AMM 56-12-00-4 & 56-12-00-5. A/C OK FOR SERVICE. 2 L 7 3 4F A22WE 2002110800044 20021108 00044 2002 11 8 SWAA022615 4 20021103 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 781WN 30601 AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002110800045 20021108 00045 2002 11 8 SWAA022617 4 20021104 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002110800046 20021108 00046 2002 11 8 SWAA022618 4 20021104 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM CABIN DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED C3 CHECK, FOUND BOTH FWD ENTRY AND AFT SVC CABIN DOOR EMERGENCY EVAC SLIDES GIRT ASSY OUT OF ADJUST. A DJUSTED SLIDES PER MM. 2 L 7 2 4F RT A16WE 2002110800047 20021108 00047 NM 2002 11 8 SWAA022620 1 20021104 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, BELOW STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002110800048 20021108 00048 NM 2002 11 8 SWAA022623 1 20021105 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 14R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002110800049 20021108 00049 NM 2002 11 8 SWAA022625 1 20021105 A 7930 42D107A1 SWITCH BOEING 737 7372H4 138448C NM JT8 JT8D9 52048 NE NR 2 ENGINE FAULTY A SWAA E B ENGINE SHUTDOWN EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 29 081SW 22730 707374 INFLIGHT SHUTDOWN, DECLARED EMERGENCY, DURING DESCENT NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPL ACED OIL PRESS SWITCH PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2002110800050 20021108 00050 2002 11 8 SWAA022586 4 20021101 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002110800051 20021108 00051 NM 2002 11 8 SWAA022587 1 20021031 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW 4. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2002110800052 20021108 00052 2002 11 8 SWAA022590 4 20021101 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 FWD SVC DOOR EMERGENCY EVAC SLIDE DEPLOYED WHILE OPENING DOOR. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002110800053 20021108 00053 NM 2002 11 8 SWAA022592 1 20021102 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 713SW 27847 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROW NR 1 AND NR 17. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002110800054 20021108 00054 NM 2002 11 8 SWAA022594 1 20021102 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 5, STR 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002110800055 20021108 00055 NM 2002 11 8 SWAA022595 1 20021029 A 5311 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 27L AND 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002110800056 20021108 00056 NM 2002 11 8 SWAA022596 1 20021031 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 103SW 23109 FUSELAGE SKIN CRACKED AT BS 787, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002110800057 20021108 00057 NM 2002 11 8 SWAA022597 1 20021031 A 5311 6545774 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002110800058 20021108 00058 NM 2002 11 8 SWAA022598 1 20021101 A 5330 589357 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT CAPTAINS L-1 WINDOW POST. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002110800059 20021108 00059 NM 2002 11 8 SWAA022600 1 20021101 A 5520 6573783 SKIN BOEING 737 7373H4 1384600 NM RT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED 1/4D CHECK, FOUND RT HORIZ STAB L/E SKIN CRACKED 90 OTBD OF ATTACH LUG. REPAIRED RT HORIZ STAB PER SRM . 2 L 7 2 4F RT A16WE 2002110800060 20021108 00060 NM 2002 11 8 SWAA022575 1 20021031 A 3233 106202 LINE BOEING 737 7375H4 138449D NM RT MLG LEAKING A SWAA O OTHER K S FLUID LOSS AFFECT SYSTEMS LD LANDING 1 SW 29 522SW 26564 DECLARED EMERGENCY, DURING LANDING,HYD A-SYS QTY INDICATION WENT TO ZERO AND HYD LOW PRESS LIGHTS ILLUMINATED. FOUND RT MLG ACTUATOR DOWN LINE LEAKING. REMOVED AND REPLACED BOTH ACTUATOR LINES PER MM. 2 L 7 2 4F RT A16WE 2002110800061 20021108 00061 NM 2002 11 8 SWAA022576 1 20021029 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT 5 O'CLOCK POSITION AT THE FIRST ROW OF RIVETS AROUND THE PE RISPHERY OF THE PRESS DOME. REPAIRED BLKHD PER SWA EA. 2 L 7 2 4F A16WE 2002110800062 20021108 00062 NM 2002 11 8 SWAA022577 1 20021030 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEV WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 724SW 27856 DURING SCHEDULED PM CHECK, SI-11038-55, RT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED RT ELEV TAB NR 1 HI NGE BOLT AND BUSHING PER MM. 2 L 7 2 4F RT A16WE 2002110800063 20021108 00063 2002 11 8 SWAA022578 4 20021030 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE IND DATA PLATE OUT OF POSITION. REPOSTIONED DATA PLATE PER MM. 2 L 7 2 4F RT A16WE 2002110800064 20021108 00064 2002 11 8 SWAA022579 4 20021030 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE RELEASE CABLE FITTING TO COVER GAP OUT OF LIMITS. REPO STIONED FITTING PER MM. 2 L 7 2 4F RT A16WE 2002110800065 20021108 00065 NM 2002 11 8 SWAA022581 1 20021031 A 5330 6545761 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED, BS 440.5, STRINGER 14R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002110800066 20021108 00066 NM 2002 11 8 SWAA022582 1 20021031 A 5753 6546435 FLAP BOEING 737 7372H4 138448C NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBD T/E AFT FLAP DELAMINATED AT INBD SIDE. REMOVED AND REPLACED FLAP PER M M. 2 L 7 2 4F A16WE 2002110800067 20021108 00067 NM 2002 11 8 SWAA022584 1 20021031 A 2731 REP4M6 BEARING BOEING 737 7373L9 1384470 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED C4 CHECK, RT ELEVATOR FAILED FREEPLAY CHECK. REMOVED AND REPLACED RT ELEV TAB CONTROL ROD END BEARING AND BUSHING PER MM. 2 L 7 2 4F RT A16WE 2002110800068 20021108 00068 NM 2002 11 8 SWAA022585 1 20021031 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 103SW 23109 DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED APPROX 2.25 LONG, BS 787+6, STRINGER 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002110800069 20021108 00069 NM 2002 11 8 DL72E021035 1 20020904 A 2150 2040751 ACM BOEING 727 727247 138408F NM A/C BAY SMOKE A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 830WA 21482 RTB IN SAT DUE TO SMOKE IN CABIN. FOUND RT PACK ACM OUT OF OIL CAUSING SMOKE. REPLACED RT ACM PER MM CKS OK MCO ALSO R EPLACED FLOW MULT PER MM. 2 L 7 3 4F A3WE 2002110800070 20021108 00070 NM 2002 11 8 SWAA022568 1 20021029 A 2761 65C268642 ACTUATOR BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE K F FLUID LOSS FLT CONT AFFECTED TX TAXI/GRND HDL 1 SW 29 314SW 23336 AFTER LANDING, DURING TAXIING, HYD A-SYS PRESS AND QTY IND WENT TO ZERO. REMOVED AND REPLACED NR 8 SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2002110800071 20021108 00071 NM 2002 11 8 SWAA022569 1 20021029 A 2761 65C268642 ACTUATOR BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE K F FLUID LOSS FLT CONT AFFECTED TX TAXI/GRND HDL 1 SW 29 519SW 25318 AFTER LANDING DURING, TAXIING, HYD A-SYS PRESS AND QTY IND WENT TO ZERO. REMOVED AND REPLACED NR 2 SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2002110800072 20021108 00072 2002 11 8 SWAA022570 4 20021030 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM R2 DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE RELEASE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002110800073 20021108 00073 NM 2002 11 8 SWAA022571 1 20021030 A 5753 654643517 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2002110800074 20021108 00074 NM 2002 11 8 SWAA022572 1 20021030 A 5753 6546430100 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C4 CHECK, FOUND RT WING INBD T/E FORE FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2002110800075 20021108 00075 NM 2002 11 8 SWAA022573 1 20021030 A 5520 6959227 BUSHING BOEING 737 7373H4 1384600 NM RT ELEV WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED SERVICE CHECK, SI-11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELVEVATOR TAB NR 1 HINGE FITTING BUSHINGS PER MM 2 L 7 2 4F RT A16WE 2002110800076 20021108 00076 NM 2002 11 8 SWAA022574 1 20021029 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED 2 LONG, BS 360, STRINGER 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002110800077 20021108 00077 NM 2002 11 8 DL72E021115 1 20020921 A 2782 1U1110 ACTUATOR BOEING 727 727247 138408F NM KRUEGER FLAP LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 830WA 21482 SHORTLY AFTER T/O A SYS HYD QUANTITY WENT TO ZERO AND LOST PRESSURE. ATB BACK TO BWI. FOUND NBR 5 KRUEGER FLAP ACTUATO R HAD FAILED AND WAS LOSING FLUID, REPLACED SAME. 2 L 7 3 4F A3WE 2002110800078 20021108 00078 2002 11 8 SWAA022558 4 20021029 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM FWD SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM 2 L 7 2 4F RT A16WE 2002110800079 20021108 00079 NM 2002 11 8 SWAA022559 1 20021029 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 717SA 27851 EEPLS LENSES MISSING (4 EA) IN CABIN. INSTALLED LENSES PER MM. 2 L 7 2 4F RT A16WE 2002110800080 20021108 00080 NM 2002 11 8 SWAA022560 1 20021029 A 5520 BACB28AK04 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS AT NR 1 ELEV TAB HINGE PER MM. 2 L 7 2 4F RT A16WE 2002110800081 20021108 00081 NM 2002 11 8 SWAA022561 1 20021026 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2002110800082 20021108 00082 NM 2002 11 8 SWAA022562 1 20021027 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED C2 CHECK, FOUND FUSELSGE SKIN CRACKED 2.5 IN LONG, BS 747+7, STR 19R. REPAIRED SKIN PER SWA SAM FORM 3 26. 2 L 7 2 4F RT A16WE 2002110800083 20021108 00083 NM 2002 11 8 SWAA022563 1 20021028 A 5513 65C26384 TAB BOEING 737 7373H4 1384600 NM RT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED A1 CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 1 HINGE CUT OUT. REMOVED AND REPLACEDR TAB ASSY PER MM. 2 L 7 2 4F RT A16WE 2002110800084 20021108 00084 NM 2002 11 8 SWAA022564 1 20021026 A 5230 6545871 FRAME BOEING 737 7375H4 138449D NM FWD CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR LOWER FRAME AND T-CHORD CRACKED. REPAIRED DOOR PER SRM AND CCO. 2 L 7 2 4F RT A16WE 2002110800085 20021108 00085 NM 2002 11 8 SWAA022565 1 20021027 A 5314 65C26493501 WEB BOEING 737 737317 138447P NM FUSELAGE GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED C2 CHECK, FOUND KEEL BEAM WEB GOUGED ADJACENT TO LT A/C PACK VALVE. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2002110800086 20021108 00086 NM 2002 11 8 SWAA022552 1 20021028 A 5311 6546529 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 345, STR 20L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 2002110800087 20021108 00087 2002 11 8 SWAA022553 4 20021028 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002110800088 20021108 00088 NM 2002 11 8 SWAA022556 1 20021025 A 2612 33007505 FIRE LOOP BOEING 737 7373G7 1384595 NM APU FAULTY A SWAA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 SW 29 691WN 23781 AIR TURNBACK, APU FIRE WARNING LIGHT AND BELL SOUNDED WHILE AIRBORNE, DISCHARGED ONE BOTTLE. INSPECTED, FOUND NO EVIDEN CE OF FIRE. REMOVED AND REPLACED FIRE BOTTLE AND FIRE LOOP PER MM. 2 L 7 2 4F RT A16WE 2002110800089 20021108 00089 NM 2002 11 8 SWAA022557 1 20021027 A 5610 893543130 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 29 615SW 27698 R-1 COCKPIT WINDOW ARCING AND DELAMINATING, OUTER PANE CRACKED. REMOVED AND REPLACED R-1 WINDOW PER MM. 2 L 7 2 4F RT A16WE 2002110800090 20021108 00090 NM 2002 11 8 DL72E021126 1 20020923 A 2782 704082 ACTUATOR BOEING 727 727247 138408F NM KRUEGER FLAP LEAKING A DALA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 830WA 21482 TOTAL LOSS OF A SYSTEM HYDRAULICS. FOUND NR 5 LDG EDGE FLAP ACTUATOR LEAKING AT SHUTTLE VLV, REMOVED NR 5 LDG EDGE FLAP ACUATOR. REPLACED NR 5 L/E FLAP ACTUATOR AND SHUTTLE VALVE PER JIC. A SYS HYD READS 1.5 GALLON. SERVICED SAME TO FUL L RAN ALL PUMPS AND ENGS CKS GOOD. 2 L 7 3 4F A3WE 2002110800091 20021108 00091 NM 2002 11 8 DL72E021155 1 20020930 A 3350 900542 BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 21481 AFT EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY RACK AND PACK. 2 L 7 3 4F A3WE 2002110800092 20021108 00092 NM 2002 11 8 DL72E021234 1 20021025 A 2560 253876500 SEAL BOEING 727 727247 138408F NM FIRST AID KIT MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 AFT CABIN FIRST AID KIT SEAL MISSING. REPLACED FIRST AID KIT IN AFT CABIN. 2 L 7 3 4F A3WE 2002110800093 20021108 00093 NM 2002 11 8 DL72S021051 1 20020909 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 526DA 21586 DURING L/O CHECK FOUND RIGHT OVERWING EMERGENCY LIGHT INOP RELAMPED. OPS CKS GOOD. 2 L 7 3 4F A3WE 2002110800094 20021108 00094 NM 2002 11 8 DL72S021072 1 20020912 A 3350 900853A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 519DA 21470 AFT EMERGENCY EXIT IDENTIFIER INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 2002110800095 20021108 00095 NM 2002 11 8 DL72S021079 1 20020913 A 3350 10617839 CHARGER BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 523DA 21583 OVERWING EMERGENCY EXIT LIGHTS INOP IN EMERGENCY MODE. REMOVED AND REPLACED CHARGER ON RIGHT SIDE, BATTERY ON LEFT SIDE AND EMERGENCY LIGHT ASSEMBLY ON RIGHT OVERWING EXIT. 2 L 7 3 4F A3WE 2002110800096 20021108 00096 NM 2002 11 8 DL72S021111 1 20020920 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 526DA 21586 RT OVERWING EMERGENCY LIGHTS INOP. REPLACED 5 BATTERY PACKS AND 1 POWER RACK. 2 L 7 3 4F A3WE 2002110800097 20021108 00097 NM 2002 11 8 DL72S021133 1 20020924 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 523DA 21583 AFT OVERHEAD ISLE EMERGENCY LIGHT INOP. REPLACED BATTERY OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002110800098 20021108 00098 NM 2002 11 8 DL72S021136 1 20020925 A 3350 S106 BATTERY BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 805EA 22436 FWD GALLEY DOOR EMERGENCY EXIT LIGHT INOP. WILL NOT TEST, REPLACED BATTERIES AND BULBS OPERATIONAL CHECKS NORMAL. 2 L 7 3 4F RT A3WE 2002110800099 20021108 00099 NM 2002 11 8 DL72S021139 1 20020926 A 2920 HYDRAULIC LINE BOEING 727 727232 1384082 NM HYD SYSTEM CHAFED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 545DA 22494 THE HYD SYSTEM B HAD ZERO PRESSURE AND ZERO QUANTITY. FOUND THE B HYD SYSTEM QUANTITY AT .9 ON ARRIVAL, AND FOUND THE N R 2 B HYD PUMP PRESSURE LINE CHAFED, REPLACED THE LINE AND ALSO CHECKED THE CASE DRAIN FILTER WITH NO DEFECTS, LEAK CH ECK AND OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002110800100 20021108 00100 NM 2002 11 8 DL72S021144 1 20020926 A 5311 65175061 FRAME BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 THE INNER CHORD OF THE FS 1303 FRAME WAS FOUND CRACKED AT A HYDRAULIC LINE CLAMP ATTACHMENT LOCATION JUST ABOVE RT VENTR AL STAIRWAY TORQUE BOX STRUCTURE. THE CHORD WAS CUT ABOVE THE DAMAGE AND THE LOWER SECTION OF CHORD REMOVED. A NEW SEC TION OF CHORD WAS INSTALLED AND SPLICED WITH A REPAIR ANGLE PER ER/A 383919-14, REV A. 2 L 7 3 4F A3WE 2002110800101 20021108 00101 NM 2002 11 8 DL72S021164 1 20021003 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 526DA 21586 SEAT 10DEF EMERGENCY EGRESS LIGHT INOP, RELAMPED. 2 L 7 3 4F A3WE 2002110800102 20021108 00102 NM 2002 11 8 DL72S021172 1 20021006 A 3233 65404676 ACTUATOR BOEING 727 727232 1384082 NM NLG LEAKING A DALA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 515DA 21431 AFTER NORMAL LANDING WHILE TAXIING OFF THE RUNWAY, THE CAPT LOST NOSE STEERING. CHECKED A SYSTEM HYD, NO PRESSURE NO FL UID REMOVED AND REPLACED NOSE LOCK ACTUATOR REF MM 32-33-011-4 AND OPS AND LEAK CHECK GOOD. 2 L 7 3 4F A3WE 2002110800103 20021108 00103 NM 2002 11 8 DL72S021175 1 20021008 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 523DA 21583 LT SIDE OVERWING EMERGENCY LIGHTS DID NOT ILLUMINATE DURING LAYOVER TEST. REPLACED BATTERY PACK PER M/M. CKS OK. 2 L 7 3 4F A3WE 2002110800104 20021108 00104 NM 2002 11 8 DL72S021180 1 20021009 A 2611 SMOKE DETECTOR BOEING 727 727232 1384082 NM CARGO BAY FALSE ACTIVATION A DALA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 27 545DA 22494 FWD CARGO- FWD SMOKE DETECTOR RED LED LIGHT ON. REPLACED DETECTOR. 2 L 7 3 4F A3WE 2002110800105 20021108 00105 NM 2002 11 8 DL72S021190 1 20021012 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 546DA 22677 ON LAYOVER CHECK FOUND LEFT OVERWING EMERGENCY LIGHT DIM WHILE PERFORMING EMERGENCY LIGHTS CHECK. REPLACED BATTERY PAC K. 2 L 7 3 4F A3WE 2002110800106 20021108 00106 NM 2002 11 8 DL72S021251 1 20021027 A 3350 LP7265001 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 519DA 21470 EMERGENCY EXIT LIGHT AT ROW 16 INOP AND LENS MISSING. RELAMPED AND REPLACED LENS-OPS NORMAL. 2 L 7 3 4F A3WE 2002110800107 20021108 00107 NM 2002 11 8 DL72W021073 1 20020913 A 3350 334701744 BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 296WA 22533 EMERGENCY EXIT LIGHTS IN OVERHEAD PANEL AT OVERWING EXIT LOCATION AND AT AFT SERVICE DOOR LOCATION INOP. REPLACED BATTE RY M1094 AND BOTH BATTERY AND PACK A7 M1095, ALL CKS OK. 2 L 7 3 4F A3WE 2002110800108 20021108 00108 NM 2002 11 8 DL72W021212 1 20021019 A 3350 MS2452323BAC SWITCH BOEING 727 727247 138408F NM CABIN MALFUNCTIONED A DALA K NONE O OTHER CR CRUISE 1 SO 27 296WA 22533 EMERGENCY EXIT LIGHTS CAME ON AT CRUISE 1:10 MINS INTO FLIGHT. REPLACED AFT SWITCH AT FLT ATTD PANEL AND R600 EMERG EX IT RELAY. EMERGENCY EXIT LIGHTS OPS CKS NORM. 2 L 7 3 4F A3WE 2002110800109 20021108 00109 NM 2002 11 8 DL72W021219 1 20021022 A 3350 952466508 RELAY BOEING 727 727247 138408F NM COCKPIT INTERMITTENT A DALA K NONE O OTHER CR CRUISE 1 SO 27 296WA 22533 EMERGENCY LIGHTS FLICKER IN A NORMAL FLIGHT OPERATION. EFFECTED LIGHTS ARE ROW 30 AND FORWARD IN CABIN. REPLACED RELAY , OP CKS GOOD. 2 L 7 3 4F A3WE 2002110800110 20021108 00110 NM 2002 11 8 DL733021056 1 20020911 A 5755 63C2524216A SKIN BOEING 737 737347 1384647 NM SPOILER DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 WING SPOILERS WAS FOUND WITH EXCESSIVE DELAMINATION. REPAIR PER ER/A 417560-14 AND NORDAM EWO E0038848. 2 L 7 2 4F RT A16WE 2002110800111 20021108 00111 NM 2002 11 8 DL733021057 1 20020904 A 5753 6546486155 WEDGE BOEING 737 737347 1384647 NM T/E FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 DAMAGE TO LT WING INBOARD MID FLAP WEDGE. REPAIR PER ER/A 417684-14. 2 L 7 2 4F RT A16WE 2002110800112 20021108 00112 NM 2002 11 8 DL733021059 1 20020906 A 5753 6546486156 SKIN BOEING 737 737347 1384647 NM T/E FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 RT WING INBOARD MID FLAP WEDGE IS DISBONDED. REPAIR PER ER/A 417696-14. 2 L 7 2 4F RT A16WE 2002110800113 20021108 00113 NM 2002 11 8 DL733021132 1 20020923 A 3350 LIGHT BOEING 737 737347 1384647 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3301 23181 EMERGENCY EXIT LIGHT AT SEAT 10 DEF INOP. RELAMPED SAME OPS CK GOOD 2 L 7 2 4F RT A16WE 2002110800114 20021108 00114 NM 2002 11 8 DL733021152 1 20020930 A 2530 OVEN BOEING 737 737301 1384611 NM GALLEY MALFUNCTIONED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 948WP 23259 FLT ATTENDANT REPORTED SMOKE/ELECTRICAL SMELL COMING FROM F/C GALLEY OVEN AND CONTROL PANEL. FIRE EXTINGUISHER USED. N O FIRE NOTICED. GALLEY POWER SECURED. ELECTED TO DIVERT TO LBB. REMOVED AND REPLACED OVEN, OP CKS NORMAL. 2 L 7 2 4F RT A16WE 2002110800115 20021108 00115 NM 2002 11 8 DL733021199 1 20021014 A 5711 6545321513 SPAR BOEING 737 7373B7 1384580 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951WP 22951 INSPECTION OF THE MLG BEAM ATTACH FITTINGS AND REAR SPAR ON THE LT WING REVEALED 6 HOLES COMMON TO THE FITTINGS AND SPAR WITH CRACK INDICATIONS. ADDITIONAL HOLES WERE DAMAGED OR ELONGATED DURING REWORK OF AREA. THE HOLES WERE OVERSIZED TO REMOVE ALL CRACKS AND DAMAGES AND BUSHED TO NOMINAL SIZE OR OVERSIZE FASTENERS INSTALLED PER ER/A 383961-14. 2 L 7 2 4F RT A16WE 2002110800116 20021108 00116 NM 2002 11 8 DL733021237 1 20021023 A 5315 654681138 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947WP 23376 THE FS 967 & 986.5 PASSENGER FLOORBEAMS WERE FOUND WITH SEVERAL AREAS OF CORROSION ON THE UPPER CAPS OF THE BEAMS. THE UPPER CAPS WERE TRIMMED OFF TO REMOVE THE CORROSION. NEW EXTRUDED CAP SECTIONS WERE INSTALLED TO REPAIR THE AREAS PER E R/A 383998-14, REV A. 2 L 7 2 4F RT A16WE 2002110800117 20021108 00117 NM 2002 11 8 DL733021260 1 20021029 A 5753 65C263203A SPAR BOEING 737 737347 1384647 NM T/E FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304WA 23345 DURING OVERHAUL THE NR 1 MID-FLAP WAS FOUND WITH CORROSION IN THE REAR SPAR LOWER CHORD. REPAIR PER ER/A 417872-14. 2 L 7 2 4F RT A16WE 2002110800118 20021108 00118 NM 2002 11 8 DL738021131 1 20020923 A 5312 148A2280 BULKHEAD BOEING 737 737832 13844CF NM FUSELAGE CANNING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DA 29624 THE WEB OF THE AFT PRESSURE BULKHEAD WAS FOUND WITH A DEEP OIL CAN BETWEEN BL0 AND THE LEFT ADJACENT RADIAL STIFFENER. THE OIL CAN WAS REPAIRED WITH A STIFFENER PER BAC 737-800 SRM 53-80-08, REPAIR 4 AND ER/A 383897-14. 2 L 7 2 4F RT A16WE 2002110800119 20021108 00119 NM 2002 11 8 DL738021137 1 20020925 A 2751 10619265 INDICATOR BOEING 737 737832 13844CF NM COCKPIT FAULTY A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 390DA 30536 FLAPS COMMANDED TO 5 DEG, STOPPED SHORT OD FLAPS 1. NEEDLES SPLIT PRIOR TO LANDING, NEEDLES MATCHED AT/SHORT OF FLAPS 1 DEG. REPLACED INDICATOR, OPERATED FLAPS SEVERAL TIMES. OPS OK. BITE OF FSEU, NO FAULTS FOUND, NO CURRENT FAULTS. 2 L 7 2 4F RT A16WE 2002110800120 20021108 00120 NM 2002 11 8 DL738021171 1 20021006 A 5270 WARNING SYSTEM BOEING 737 737832 13844CF NM COCKPIT ACTIVATED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 3754A 29626 IR - ON TAKEOFF ROLL, MASTER CAUTION WITH LEFT AFT SERVICE DOOR LIGHT CAME ON. MADE VISUAL CHECK OF SERVICE DOOR WIRIN G SW AND ROLLER. OPS NORMAL. DOOR SECURED AND LIGHT OUT. 2 L 7 2 4F RT A16WE 2002110800121 20021108 00121 NE 2002 11 8 DL738021204 2 20021017 A 7200 CFM567 ENGINE BOEING 737 737832 13844CF NM GE CFM56 CFM56* 13802 NE NR 1 BIRD INGESTION A DALA K NONE C F.O.D. AP APPROACH 1 SO 27 3764D 2336 30818 888787 ON SHORT FINAL BIRD HIT FWD PORTION OF A/C . PERFORMED BIRD STRIKE INSPECTION AND BORESCOPE OF NR 1 ENGINE - ALL OK 2 L 7 2 4F 4 F RT A16WE E2GL 2002110800122 20021108 00122 NM 2002 11 8 DL738021231 1 20021024 A 3350 767 LIGHT BOEING 737 737832 13844CF NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3766 30820 LT AFT AND RT AFT OVERWING EMERGENCY LIGHTS INOP. RELAMPED, CKS GOOD 2 L 7 2 4F RT A16WE 2002110800123 20021108 00123 NM 2002 11 8 DL73K021062 1 20020908 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305DL 23077 THE FUSELAGE SKIN AT FS 525 AND STRINGER 16R WAS FOUND TO BE CRACKED ALONG THE UPPER CHEM-MIL EDGE OF THE INTERNAL BONDE D DOUBLER. THE CRACK FOUND WAS APPROXIMATELY 3 INCHES IN LENGTH. THE CRACK WAS NOT FOUND BY DOING INSPECTIONS PER BOEI NG SB 737-53A1210. THE CRACK WAS REPAIRED PER 737-200 SRM 53-30-3, FIGURE 1. 2 L 7 2 4F RT A16WE 2002110800124 20021108 00124 NM 2002 11 8 DL73K021109 1 20020821 A 3350 RPS1 POWER SUPPLY BOEING 737 737247 138448D NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 375DL 23602 EMERGENCY EXIT LIGHTS POWER SUPPLY FAILED ON L/O INSP. REPLACED POWER SUPPLY. 2 L 7 2 4F A16WE 2002110800125 20021108 00125 NM 2002 11 8 DL73K021134 1 20020924 A 3350 P0131A POWER SUPPLY BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 320DL 23092 DURING LAYOVER INSPECTION, FOUND FWD CABIN EMERGENCY LIGHT PATH LIGHTS INOP. R&R AFT EMERGENCY LIGHT POWER PACK LOCATED UNDER CEILING LIGHT BY THE L1 DOOR ENTRANCE. 2 L 7 2 4F RT A16WE 2002110800126 20021108 00126 NM 2002 11 8 DL73K021150 1 20020929 A 3244 TIRE BOEING 737 737247 138448D NM RT MLG SEPARATED A DALA K NONE D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 242WA 23516 NR 4 TIRE TREAD SEPARATION ON T/O FROM FLL. OUTBOARD GEAR DOOR MISSING WITH DAMAGE TO NR 2 ENGINE NACELLE AND RIGHT FL AP ASSEMBLY ONLY MINOR BUMP FELT ON T/O ROLL PRIOR TO ROTATION. REPLACED BOTH RIGHT MAIN WHEEL ASSY, REPLACED DOOR, RP D NACELLE. 2 L 7 2 4F A16WE 2002110800127 20021108 00127 NM 2002 11 8 DL73K021165 1 20021001 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE SKIN AT THE UPPER HINGE CUTOUT OF THE AFT GALLEY DOOR (R2) CUTOUT WAS FOUND WITH A .375 INCH TYPICAL CRACK. THE CRA CK WAS CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL DOUBLER PER ER/A 383941-14, REV A. 2 L 7 2 4F A16WE 2002110800128 20021108 00128 NM 2002 11 8 DL73K021167 1 20021003 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 THE FUSELAGE SKIN WAS FOUND WITH A 1.375 CRACK ALONG THE MILL LINE JUST ABOVE STRINGER 16L AT FS 525, AFT OF THE WING SC ANNING LIGHT CUTOUT. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL DOUBLER PER B737 SRM AND ER/A 383970-14. 2 L 7 2 4F A16WE 2002110800129 20021108 00129 NM 2002 11 8 2002F00979 1 20020202 A 3350 900542 POWER SUPPLY BOEING 727 727214 138407R NM CABIN DISCHARGED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 288SC 20765 FLT 182 - IAD - RIGHT EXTERNAL AFT BODY FAIRING EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT SYSTEM AND FOUND FAULTY POWER SUPPLY. REMOVED FAULTY POWER SUPPLY AND REPLACED WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD PER B727 AMM 33-0-0. ( M) 2 L 7 3 4F A3WE 2002110800130 20021108 00130 CE 2002 11 8 2002F00980 1 20020129 A 7110 63526022 NOSE COWL CESSNA 525 525A 2076615 CE RT ENGINE CRACKED A T0DA K NONE O OTHER IN INSP/MAINT 1 CE 03 323LM 182 525A0020 AFTER FINDING THE SAME CRACK ON SERIAL NR 17 PERFORMED AN INSPECTION AND FOUND A CRACK ON THE INNER SIDE APPROXIMATELY 3 O'CLOCK POSITION OF THE RIGHT ENGINE INLET NOSE CAP. THE CRACK WAS APPROXIMATELY .75 OF AN INCH IN LENGTH RUNNING FROM THE EDGE OF THE METAL TO THE ATTACHING FASTENER. (M) 1 L 7 1 4F RT A1WI 2002110800131 20021108 00131 EU 2002 11 8 2002F00981 1 20020904 A 5244 25PT75AC DOOR BRAERO DH125 HS125700A 4230170 EU ACCESSORY BAY OPEN A UG8A A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 23 48FB 257129 FLIGHT CREW NOTED A VIBRATION AFTER TAKEOFF AND RETURNED TO DEPARTURE AIRPORT. THE CREW NOTED THAT THE AFT EQUIPMENT BA Y DOOR WAS OPEN AFTER LANDING. INITIAL INSPECTION OF THE DOOR LATCHES REVEALED NO DAMAGE OR EVIDENCE OF MALFUNCTION. I T IS UNKNOWN AT THIS TIME WHAT CAUSED THE DOOR TO OPEN. THERE IS NO WARNING LIGHT SYSTEM FOR THIS DOOR. THE DOOR WAS I NSPECTED AND IT WAS NOTED THAT THE ACM EXHAUST DUCT WAS MISSING. THE DOOR HAD MINOR EDGE DAMAGE, WHICH WAS TEMPORARILY REPAIRED FOR A FERRY FLIGHT. (M) 2 L 7 2 4F A3EU 2002110800132 20021108 00132 EU 2002 11 8 2002F00982 1 20020812 A 3246 AH52786 BEARING BRAERO DH125 HS125700A 4230170 EU RT MLG FAILED A UG8A O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 GL 23 48FB 257129 THE RIGHT OUTBOARD WHEEL NR 4 DEPARTED THE AIRCRAFT DURING TAKEOFF FROM KDIK. THE OUTER WHEEL BEARING FAILED ALLOWING T HE WHEEL TO SLIDE FROM THE AXLE. (M) 2 L 7 2 4F A3EU 2002110800134 20021108 00134 CE 2002 11 8 2002F00984 1 20020123 A 5270 922AB1YA4NL PROXIMITY SWITCH CESSNA 750 750 2076810 CE PAX DOOR FAULTY A UG8A O OTHER N FALSE WARNING IN INSP/MAINT 1 GL 23 5116 7500019 PSP - MAIN CABIN DOOR WARNING LIGHT WOULD NOT EXTINGUISHED WHEN CLOSED. FAULTY DOOR HANDLE PROXIMITY SWITCH. PROBLEM W AS CORRECTED BY REPLACEMENT OF THE SWITCH. OPERATIONAL CHECK OF SYSTEM WAS GOOD IAW 750 MM CHAPTER 52-70-00. (M) 2 L 7 2 4J RT T00007WI 2002110800135 20021108 00135 EU 2002 11 8 2002F00986 1 20020923 A 7722 8972605 CONTROL UNIT BAG JETSTM JETSTM3101 1500215 EU LT ENGINE FAILED A B16A O OTHER O OTHER NR NOT REPORTED 1 NE 05 539PA 741 FOUND LEFT EGT BECAME ERRATIC, INITIALLY PLUS OR MINUS 50 TO 60 DEGREES, THEN PLUS 100 DEGREES DROPPED TO 150 DEGREES SR L OFF, ALL OTHER ENGINE INDICATIONS NORMAL. REMOVED AND REPLACED DELTA P CONTROL UNIT. OPERATIONALLY CHECKED NORMAL. (M) 2 L 7 2 4T RT A21EU 2002110800136 20021108 00136 NE 2002 11 8 2002F00987 2 20020831 A 7200 ENGINE GULSTM G73 G73 3951802 SW PWA PT6 PT6A34AG 52053 NE LEFT FAILED A FVYA C ABORTED TAKEOFF Y ENGINE STOPPAGE TO TAKEOFF 1 SO 17 130FB J30 PH0044 LEFT ENGINE FAILED ON TAKEOFF FROM PDI. AIRCRAFT TAXIED BACK TO RAMP AND PASSENGERS DEPLANED. MAINTENANCE WAS DISPATCH ED TO PDI TO INVESTIGATE. PROPELLER AND ENGINE REMOVED FROM AIRCRAFT ENGINE SENT BACK TO FLL FOR SUBSEQUENT INVESTIGATI ON BY MANUFACTURER. 1 H 7 2 3R 4 T A783 E4EA 2002110800137 20021108 00137 CE 2002 11 8 2002F00988 1 20020726 A 2913 66166 PUMP CESSNA 750 750 2076810 CE RT ENGINE FAILED A UG8A O OTHER J WARNING INDICATION LD LANDING 1 GL 23 5113 2302 7500013 YNG - AMBER RIGHT HYDRAULIC PUMP FAIL MESSAGE ILLUMINATED WHEN THRUST REVERSERS WERE DEPLOYED WHILE LANDING AT YNG. RIG HT ENGINE DRIVEN HYDRAULIC PUMP FAILED. REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP. OPERATIONAL CHECK OF THE NEW PUMP WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4J RT T00007WI 2002110800139 20021108 00139 NM 2002 11 8 ASAA0210189 1 20020925 A 5314 6573746 KEELBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM WEB AT FUSELAGE BS 642, LBL 2 CORRODED. REMOVED CORROSION AND REPAIRED PER SRM BY FABRICATING AND INSTALLING REPAIR PARTS. (M) 2 L 7 2 4F RT A16WE 2002110800140 20021108 00140 NM 2002 11 8 ASAA0210190 1 20020925 A 5320 65486531 SUPPORT ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND SUPPORT ANGLE AT FUSELAGE BODY STATION 664-675, RBL 27 CORRODED. REMOVED CORRODED AND REPAIRED PER SRM BY FABRICATING AND INSTALLING REPAIR PARTS. (M) 2 L 7 2 4F RT A16WE 2002110800141 20021108 00141 NM 2002 11 8 ASAA0210191 1 20020925 A 5260 65581707 RIB BOEING 737 7372X6C 1384552 NM AFT AIRSTAIRS DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND AFT AIRSTAIR RIB AT FUSELAGE BS 947-987 DAMAGED. REMOVED DAMAGED AREA AND REPAIRE D PER SRM BY FABRICATING AND INSTALLING REPAIR PARTS. (M) 2 L 7 2 4F RT A16WE 2002110800142 20021108 00142 NM 2002 11 8 ASAA0210192 1 20020926 A 5320 6573743 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND INTERCOSTAL AT FUSELAGE BS 500-500A, STRINGER 26R CRACKED. REMOVED DAMAGED INTERC OSTAL AND REPAIRED PER SRM BY FABRICATING AND INSTALLING NEW INTERCOSTAL. (M) 2 L 7 2 4F RT A16WE 2002110800143 20021108 00143 NM 2002 11 8 ASAA0210193 1 20020926 A 5320 6546534 SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND BULKHEAD SUPPORT AT FUSELAGE BS 520, LBL 24, RBL 30 CORRODED. REMOVED CORROSION A ND REPAIRED PER SRM BY FABRICATING AND INSTALLING NEW SUPPORT. (M) 2 L 7 2 4F RT A16WE 2002110800144 20021108 00144 NM 2002 11 8 ASAA0210194 1 20020926 A 5320 654652817 SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT AT FUSELAGE BODY STATION 500-500A, STRINGER 26R CORRODED . REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT PER SRM. (M) 2 L 7 2 4F RT A16WE 2002110800145 20021108 00145 NM 2002 11 8 ASAA0210195 1 20020928 A 5320 6546528 SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT AT FUSELAGE BODY STATION 490-520, LEFT BUTTOCK LINE 25 C ORRODED. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT PER SRM. (M) 2 L 7 2 4F RT A16WE 2002110800146 20021108 00146 NM 2002 11 8 ASAA0210196 1 20020928 A 7110 654797249 SUPPORT BOEING 737 7372X6C 1384552 NM NR 2 COWLING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE INBOARD COWL BLOWOUT DOOR SUPPORT DAMAGED AT ENGINE STATION 230. REMO VED, FABRICATED AND REPLACED ENGINE COWL BLOWOUT DOOR SUPPORT PER SRM. (M) 2 L 7 2 4F RT A16WE 2002110800147 20021108 00147 NM 2002 11 8 ASAA0210197 1 20020928 A 5320 65554846 SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND TIE DOWN SUPPORT AT FUSELAGE BODY STATION 410-520, RBL 21 WORN. REMOVED AND FABRI CATED REPAIRS TO TIE DOWN SUPPORT PER SRM. (M) 2 L 7 2 4F RT A16WE 2002110800148 20021108 00148 NM 2002 11 8 ASAA0210198 1 20020928 A 5753 65464431277 SKIN BOEING 737 7372X6C 1384552 NM T/E FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND LEADING EDGE OF OUTBOARD FORE FLAP AT LEFT WING STATION 495-499 CHAFED. FABRICATE D REPAIRS TO FLAP PER SRM. (M) 2 L 7 2 4F RT A16WE 2002110800149 20021108 00149 NM 2002 11 8 ASAA0210199 1 20020930 A 5320 FITTING BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND INTERCOSTAL CHORD FITTING AT BS 360-385, LBL 9, LBL 16 WITH AN ELONGATED HOLE. RE MOVED AND REPLACED INTERCOSTAL CHORD FITTING PER SRM. (M) 2 L 7 2 4F RT A16WE 2002110800150 20021108 00150 NM 2002 11 8 ASAA0210201 1 20020930 A 5310 6547959 DOOR FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND AFT CARGO DOOR CUTOUT FORWARD FRAME STABILIZING WEB AT FUSELAGE BS 787, STRINGER 2 4R DENTED AND GOUGED. REMOVED AND REPLACED WEB PER SRM. (M) 2 L 7 2 4F RT A16WE 2002110800151 20021108 00151 WP 2002 11 8 ASAA0280317 1 20020920 A 5320 99100643 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - FOUND DURING C-CHECK, AFT ACCESSORY COMPARTMENT RIGHT MAINTENANCE PLATFORM WAS CRACKED ON AFT SIDE. INSTALLED PLA TFORM DOUBLER PER SRM 53-01, FIG 2, PAGE 10. (M) 2 L 7 2 4F A6WE 2002110800152 20021108 00152 EU 2002 11 8 BMAC020018 1 20020923 A 7722 8972605 CONTROL UNIT BAG JETSTM JETSTM3101 1500215 EU LT ENGINE MALFUNCTIONED A B16A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 539PA 741 PSM - FLT 3580 - LEFT EGT ERRATIC INITIALLY PLUS OR MINUS 50 TO 60 DEGREES, THEN PLUS 100 DEGREES. DROPPED TO 150 DEGRE ES (SRL OFF) ALL OTHER ENGINE INDICATIONS NORMAL. REMOVED AND REPLACED MONOPOLE, DID NOT CORRECT THE PROBLEM. REPLACED DELTA P CONTROL UNIT. OPERATIONALLY CHECKED NORMAL. (M) 2 L 7 2 4T RT A21EU 2002110800153 20021108 00153 NE 2002 11 8 EIA2002088 2 20020723 A 7321 7590002 FUEL CONTROL BOEING 747 747132 1384882 NM PWA JT9 JT9D7J 52054 NE NR 1 ENGINE MALFUNCTIONED A EIAA E ENGINE SHUTDOWN R M PARTIAL RPM/PWR LOSS OVER TEMP CR CRUISE 1 NM 09 481EV 19896 689487 WHILE CRUISING AT FL 35.0, NR 1 ENGINE COMPRESSOR STALLED, N1 RPM DECREASED AND EGT INCREASED RETARDED THROTTLE. NO RES PONSE, SHUTDOWN NR 1 ENGINE. DURING WINDMILLING ATTEMPTED RESTART. EGT OUT OF LIMITS, RETURN TO ANC. REMOVED AND REPL ACED NR 1 ENGINE MAIN FUEL CONTROL AND EVC, PERFORMED ENGINE TRIM, OPS CHECKED GOOD. (M) 2 L 7 4 4F 4 F A20WE E20EA 2002110800154 20021108 00154 EU 2002 11 8 SIMA200101402 1 20020114 A 3350 CONTACTOR AEROSP ATR72 ATR72212A 8680902 EU CABIN DIRTY A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 533AT 533 MIA - FLT 5078 - CREW REPORTED THE EMERGENCY LIGHT IN THE PASSENGER DOOR IS INOPERATIVE. MAINTENANCE CLEANED CONTACTS ON LIGHT ASSEMBLY WIRES. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2002110800155 20021108 00155 EU 2002 11 8 SIMA200201401 1 20020114 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 135MQ 135 MIA - FOUND MAINTENANCE REPORTED SEVERAL FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED EMERGENCY LIGHT POWER SUPPLY 10WL IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M0 2 H 7 2 4T RT A53EU 2002110800156 20021108 00156 EU 2002 11 8 SIMA200201501 1 20020115 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 177AE 340B177 SJT - FLT 3542 - DURING PREFLIGHT, ATTENDANT REPORTED THE LEFT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. AIRCRAFT WAS FERRIED TO DFW FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT 23LN IAW SAAB MM. O PERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002110800157 20021108 00157 SO 2002 11 8 SIMA200227901 1 20020927 A 2770 SWITCH EMB 135 EMB135KL 3260302 SO COCKPIT OUT OF ADJUST A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 825AE 145589 BHM - FLT 3765 - CREW REPORTED A GUSTLOCK LIGHT INDICATION DURING FLIGHT. CREW DECLARED AN EMERGENCY AND DIVERTED TO BH M. AIRCRAFT WAS LANDED WITH NO FURTHER PROBLEMS. MAINTENANCE ADJUSTED MICROSWITCH S0658 IN PEDESTAL IAW EMB MM. OPERA TIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2002110800158 20021108 00158 SO 2002 11 8 SIMA200227903 1 20020911 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 ABI - THIS IS A LEVEL 2 FINDING, LOWER CARGO DOOR SILL CORRODED. REMOVED AND REPLACED LOWER SILL IAW EMB 145 SRM 51-41- 02. (M) 2 L 7 2 4T RT T00011AT 2002110800159 20021108 00159 SO 2002 11 8 SIMA200227904 1 20020910 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 THIS IS A LEVEL 2 FINDING, GALLEY CENTER BEAM GUSSET HAS CORROSION. INSTALLED SERVICEABLE GALLEY CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002110800160 20021108 00160 NM 2002 11 8 TSAA0251056 1 20020221 A 5511 654752817 SPAR BOEING 737 737209 13844AE NM HORIZ STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 827AL 23913 DURING HEAVY CHECK, FOUND CORROSION ON HORIZONTAL STABILIZER REAR SPAR UPPER CHORD. THE CORROSION WAS TRIMMED OUT PER S RM AND VERIFIED REMOVED USING HFEC METHOD. FABRICATED A EXTERNAL DOUBLER AND REPAIR FILLER TO FIT SKIN CUTOUT. FABRICA TED REPAIR ANGLE AND REPAIR FILLER IAW FIGURE 4A-4G. INSTALLED ALL REPAIR PARTS. VERIFIED 8110-3 APPROVAL RECEIVED AND COMPLETED REPAIR IAW ECO 2513. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002110800161 20021108 00161 NM 2002 11 8 USAA020380 1 20020924 A 5330 DOUBLER BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 775AU 24933 PIT - DOOR RECESS DOUBLER HAS CRACKS AND DISTORTION, GROUND POWER DOOR CUTOUT, FS 227.7 AND 235.8 STRINGER 20 AND 22 RIG HT. DAMAGE TRIMMED AND LATCH DOUBLER INSTALLED. (M) 2 L 7 2 4F RT A16WE 2002110800162 20021108 00162 NM 2002 11 8 USAA020381 1 20021004 A 5542 65C2584151 SKIN BOEING 737 737301 1384611 NM RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 23933 PIT - RUDDER SKIN DELAMINATED, BOTTOM L/E CORNERS RT AND LT SIDE. REMOVED DAMAGE, REPAIRED AND RESTORED PER EA 75009, A ND SRM 51-70-03. (M) 2 L 7 2 4F RT A16WE 2002110800163 20021108 00163 SO 2002 11 8 C2XA02TY167 1 20021108 A 5751 14569009407 FITTING EMB 145 EMB145LR 3260212 SO BENT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 TYS. During a scheduled inspection, the left aileron PCA fitting attach lug was found bent. Maintenance removed and repl aced the fitting. I/A/W-EC5750-01177. The repair was satisfactory and the aircraft will be released upon complection of the check. 2 L 7 2 4T RT T00011AT 2002110800164 20021108 00164 NM 2002 11 8 AWXA200201086 1 20021029 A 5313 69353502 CLIP BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 0 0 23218 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/2" CRACK WAS FOUND ON THE LOWER AFT OUTBOARD CORNER OF STRINGER CLIP AT BS 80 7, STR 16 L/H. MAINTENANCE REMOVED THE DAMAGED STRINGER CLIP AT BS 807, STR 16 L/H; FABRICATED A NEW REPLACEMENT STRINGE R CLIP; AND INSTALLED REPAIR PART IAW DWG 69-35350-2, AND B737-300 SRM 51-40-02, PG. 10-11, 38, FIG. 8 & 13. 2 L 7 2 4F RT A16WE 2002110800165 20021108 00165 NM 2002 11 8 AWXA200201087 1 20021028 A 5313 6545767512 STRINGER BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 0 0 23218 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/2" CRACK WAS FOUND ON STRINGER 16 L/H AT BS 500C+14, AFT OF EXTERIOR LIGHT CO VER. MAINTENANCE TRIMMED OFF CRACKED END OF STRINGER 16 L/H AT BS 500C+14; FABRICATED A FILLER AND REPAIR CHANNEL; AND I NSTALLED REPAIR PARTS IAW AWA E.R. 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2002110800166 20021108 00166 EA 2002 11 8 COMA0260634 1 20021106 A 2760 SPOILER CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 809CA 7366 FLIGHT 5755 SPOILERS CAUTION MESSAGE DURING FLIGHT.COULD NOT DUPLICATE. NO FAULTS CODES IN COMPUTER. 2 L 7 2 4F RT A21EA 2002110800167 20021108 00167 EA 2002 11 8 COMA0260635 1 20021107 A 3230 16215103 BRACKET CNDAIR CL600 CL6002B19 1900309 EA NLG DEFECTIVE A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 924CA 7026 FLIGHT 5227 GEAR DISAGREE MESSAGE AFTER T/OREPLACE NLG PROX SENSOR BRACKET. 2 L 7 2 4F RT A21EA 2002110800168 20021108 00168 NM 2002 11 8 P5CA0200708 1 20021107 A 7920 NONE COUPLING BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE SCAVENGE LINE LOOSE A P5CA E A ENGINE SHUTDOWN UNSCHED LANDING K F FLUID LOSS FLT CONT AFFECTED CR CRUISE 1 WP 23 505MC 21251 517529 DURING CRUISE AT FL 310, #4 ENG OIL QTY WENT FROM 3.5 TO ZERO IN APPROX. 15 MIN. OIL PRESS STARTED FLUCTUATING; OIL TEM P IN GREEN BAND (PERFORMED PRECAUTIONARY SHUTDOWN) WINDMILL RPNM 26%, N2 23%, OIL TEMP BELOW GREEN, OIL PRESS 10 PSI. E MERGENCY DECLARED & FLT DIVERTED TO ANC. AT ANC INSPECTED #4 ENG INLET & EXHAUST. NO FAULTS FOUND. INSPECTED ENG CORE - FOUND LOOSE COUPLING ON AFT ENG BEARING SCAVENGE LINE. INSPECTED LINE & COUPLING - NO ABNORMALITIES. RESECURED COUPLING . PERFORMED LEAK CHK & ENG RUN. NO LEAKS EVIDENT. 2 L 7 4 4F 4 F RT A20WE E23EA 2002110800169 20021108 00169 WP 2002 11 8 DHL2002803535 1 20021028 A 5730 5611017410 PANEL DOUG DC8 DC873 302199C WP DELAMINATED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 803DH 77211 46123 IITEM REF N/R: 0108 : RH WING LOWER SURFACE T/E LOWER PANEL EXTERNAL SLIN DELAMINATED XRS 162.000 TO XF 219.000 CORR: re moved and replaced panel iaw srm 51-1-3 2 L 7 4 4F RT 4A25 2002110800170 20021108 00170 WP 2002 11 8 DHL2002803536 1 20021020 A 5310 575054920 FITTING DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 803DH 77211 46123 ITEM REF N/R: 0470 MAIN CARGO COMPT. - SPLICE FITTING CRACKED .500 @ STA. 759.000 RBL 23 ( MAJOR REPAIR)CORR:PERFORMED M AJOR REPAIR IAW ATM# po111892 , drawing 5750549.REMOVED SPLICE FITTING CRACKED IAW SRM 51-1-20D PG. 21. CLEANED , TREATE D , AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SPLICE FITTING ( 7075T651) IAW PO111892 , DRAWING 5750549. CLEANED , TREATED , AND PRIMED IAW SRM51-1-8B. INSTALLED NEW SPLICE FITTING @ STA. 759.000 , RBL23 ON MAIN CARGO COMPARTMENT , IA W SRM51-1-20D PG. 9 2 L 7 4 4F RT 4A25 2002110800171 20021108 00171 WP 2002 11 8 DHL2002803537 1 20021010 A 5300 SKIN DOUG DC8 DC873 302199C WP DENTED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 803DH 77211 46123 ITEM REF. N/R: 0179: FUS. EXT. EXTERNAL SKIN DENTED 30.0000 " LONG NEAR L14R STA. 35.000 - STA. -12.000 ( MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW FAX BOEING DHL-CVG-02-00057H; ED-3135 & ED-3142. REMOVED FASTNERSIAW SRM 51-1-21 PG. 1 , CLEANED , TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED AN EXTERNAL DOUBLER ( 7075T6AL .063); TWO INTERNAL FINGE R DOUBLERS (7075T6AL.032) IAW BOEING FAX DHL-CVG-00056H & DHL-CVG-02-00057H: ED-3135, & ED-3142. CLEANED , TREATED AND P RIMED IAW SRM51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM51-1-15 PG. 1 INSTALEED EXTERNAL DOUBLER AND TWO INT ERNAL FINGER DOUBLERS WITH NEW FASTNERS ( STA. 35.000 - -12.000) IAW FAX BOEING DHL-CVG-02-00056H AND DHL-CVG-02-00057H 2 L 7 4 4F RT 4A25 2002110900001 20021109 00001 EU 2002 11 9 DHL2002362500 1 20021104 A 5730 SKIN AIRBUS 300 A300B4203 3930306 EU A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 362DH 84 CORROSION IN BOTTOM SKIN, BETWEEN RIBS 5-6, STRG 18&19, RH WING. BLENDED OUT TO A MAXIMUM DEPTH OF 0.9MM, AS DETAILED IN DAMAGE REPORT. CORROSION BLENDED OUT WITHOUT FASTENER REMOVAL, AREAS NDT INSPECTED, PEENED, REPROTECTED AND PAINTED AS PER TD/B/2002/0354 2 L 7 2 4F RT A35EU 2002111100001 20021111 00001 2002 11 11 RAIA00211309 4 20021105 A 2312 7510700806 RECEIVER JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 550HK 13530 165 41039 5476-STL- CAPTAIN AND FO'S #1 WILL NOT TRANSMIT. MAINTENANCE REMOVED AND REPLACED THE #1 COMM RECEIVER TRANSMITTER, OPS CK OK. 2 L 7 2 4T RT A41NM 2002111100002 20021111 00002 EU 2002 11 11 RAIA00211302 1 20021004 A 3310 LT55 POWER SUPPLY JETAIR JETSTM JETSTM4101 1500501 EU SHORTED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 550HK 14125 165 41039 5450-STL- COCKPIT OVERHEAD LIGHTING PANEL CIRCUIT BREAKER POPPED. MAINTENANCE DEFERRED PER MEL: SUBSEQUENTLY REMOVED AND REPLACED POWER SUPPLY DIMMER. 2 L 7 2 4T RT A41NM 2002111100003 20021111 00003 EU 2002 11 11 RAIA00211303 1 20021006 A 3260 350A52005009 COMPUTER AEROSP ATR72 ATR72202 8680940 EU INOPERATIVE A RAIA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 03 721TE 12975 135 217 5536-STL- NOSE LANDING GEAR INDICATION INOP FWD PANEL. MAINTENANCE DEFERRED PER MEL, SUBSEQUENTLY REMOVED AND REPLACED M ULTIFUNCTION COMPUTER, OPS CK OK. 2 H 7 2 4T RT A53EU 2002111100004 20021111 00004 SO 2002 11 11 RAIA00211305 1 20021010 A 2750 3631001005 FCU EMB 145 EMB145 3260210 SO FALSE INDICATION A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 803HK 4202 145077 5305-PIT- FLAP LOW SPEED WARNING INDICATION. MAINTENANCE DEFERRED PER MEL; SUBSEQUENTLY REMOVED AND REPLACED FLAP CONTRO L UNIT, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002111100005 20021111 00005 NM 2002 11 11 SQ7A 1 20020109 A 3350 S106 BATTERY BOEING 727 727251 138408H NM COCKPIT A SQ7A K NONE L NO TEST IN INSP/MAINT 1 SO 01 282US 21161 CVG- During preflight check, Emergency light in cockpit failed (inop)Replaced Battery, checks normalFlight delay :08 min s 2 L 7 3 4F A3WE 2002111100006 20021111 00006 NM 2002 11 11 SQ7A192002 1 20020109 A 3350 S106 BATTERY BOEING 727 727251 138408H NM COCKPIT A SQ7A K NONE L NO TEST IN INSP/MAINT 1 SO 01 282US 21161 CVG- During preflight check, Emergency light in cockpit failed (inop)Replaced Battery, checks normalFlight delay :08 min s 2 L 7 3 4F A3WE 2002111100007 20021111 00007 NM 2002 11 11 ZW0A0211201 1 20021108 A 3350 58222 POWER SUPPLY BOEING 757 7572Q8 1384972 NM CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 710TW 28169 THE EMERGENCY LIGHTS AT THE RH SIDE NUMBER 3 CABIN DOOR, AND AT THE MID LAVATORY AREA, WERE INOPERATIVE. REPLACED THE E MERGENCY LIGHT POWER SUPPLY AT THE R3 DOOR. CHECK-C 11-14-01 MCI. --CLOSED-- 2 L 7 2 4F RT A2NM 2002111100008 20021111 00008 WP 2002 11 11 ARWA20021007 1 20021028 A 7932 AN9294C CAP DOUG DC8 DC863F 302198F WP NR 4 ENGINE LOOSE A ARWA E J ENGINE SHUTDOWN DUMP FUEL K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 441J 45988 NR 4 ENGINE OIL QUANTITY DROPPED TO ZERO. PRECAUTIONARY SHUT DOWN: N1 26 PERCENT, N2 35 PERCENT, OIL TEMP 90C. INSPEC TED NR 4 ENGINE AND FOUND CSD SPLINE STAND PIPE CAP LOOSE, RE-TIGHTENED CAP IAW MM 79-20-6. SERVICED ENGINE OIL IAW 12- 20-1 RAN ENGINE PER 71-00, NO LINES NOTICED. INSPECTED MAIN OIL FILTER FOR CONTAMINATION IAW MM 79-20-7, NO CONTAMINAT ION FOUND. LEAKS CHECK PER 71-00 FOUND NORMAL. 2 L 7 4 4F 4A25 2002111100009 20021111 00009 NE 2002 11 11 ARWA20021004 2 20021012 A 7200 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 3 MALFUNCTIONED A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 802BN 51105 4988 45909 671098 DURING CRUISE NR 3 ENGINE IDLE PRESS. LIGHT ILLUMINATED. OIL PRESS. 25 PSI, QTY, 1 GALLON. TEMP 135 DEGREES. ENGINE S HUT DOWN AT 1421Z. WINDMILLING OIL PRESSURE ZERO. REMOVED ENGINE, AND REPLACE WITH SERVICEABLE ENGINE. FUNCTIONAL TEST AND GROUND RUN-UP CHECKS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2003011700125 20030117 00125 NM 2003 1 17 PCAA0211132 1 20021109 A 3350 6104781 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 805EX 228 DURING ROUTINE MAINTENANCE VISIT SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. POSITION NR 5 EMERGENCY LIGHT BATTERY FOUND DRAINED. BATTERY WAS REPLACED IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 33-51-00. OPERATIONAL CH ECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002121800041 20021218 00041 GL 2002 12 18 C2XA02BT072 2 20021111 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 LEAKING A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 21537 3857 3857 145523 CAE311494 YUL/BTV---CO3213, ENROUTE CLIMB FROM YUL CREW REPORTED, LAV SMOKE WARNING THROUGH 12000 FEET, DECLARED EMERGENCY AND DIV ERTED TO BTV, LAV SMOKE QRH COMPLETED. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE IAW T ASK CARD 6271001 REFERENCE M-602 538434 OPS. AND LEAK CHECKS GOOD. NO LAV SMOKE OR WARNINGS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002111100010 20021111 00010 SO 2002 11 11 C2XA02BT071 1 20021110 A 8010 M832481210 O-RING EMB 145 EMB145LR 3260212 SO Zone 400 LEAKING A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 21537 145523 BTV---CO3055, AFTER TAKEOFF CREW REPORTED "LAV SMOKE (WARNING) AND VISIBLE CABIN SMOKE CLIMBING THROUGH 11000 FEET", DEC LARED EMERGENCY AND AIR RETURNED BACK TO BTV, LANDED UNEVENTFULLY....MAINTENANCE REMOVED AIR TURBINE STARTER, REPLACED O -RINGS, AND REINSTALLED AIR TURBINE STARTER IAW RR AE3007 MM #80-10-01. OPS.CHECK AND LEAK CHECKED GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002111100011 20021111 00011 NM 2002 11 11 DHL2002726006 1 20021109 A 2611 100064901 SMOKE DETECTOR BOEING 727 727228 1384083 NM A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 1) FORWARD LOWER CARGO COMPARTMENT FIRE DETECTOR S/N 1698 INOP AMBER & GREEN LIGHTS ILLUMINATED ON DETECTION SYS DISPLA Y.2) DEFERRED LOWER CARGO COMPARTMENT FIRE DETECTOR S/N 1698 PER DHL MEL 26-19-1 CAT B DMI#10927. PLACARD INSTALLED.3) REF. DMI #10927 "FORWARD LOWER CARGO COMPARTMENT FIRE DETECTOR S/N1698INOP AMBER+GREEN LIGHTS ILLUMINATED ON DETECTION SYSTEM DISPLAY."4) REMOVED SMOKED DETECTOR SN#1698 INSTALLED SER NO.#15934 IN FWD PIT PERB727 M/M SUPP 26-16-01 TESTED PER B727 M/M SUPP 26-16-00 OPS CHECKS GOOD THIS ACTION CLEARS DMI # 10927 .PLACARD REMOVED 2 L 7 3 4F RT A3WE 2002111100012 20021111 00012 SO 2002 11 11 C2XA02CL224 1 20021109 A 5610 163500109 WINDSHIELD EMB 145 EMB145LR 3260212 SO FUSELAGE ARCED A C2XA O OTHER O OTHER UK UNKNOWN 1 SW 27 14905 145476 CLE FLIGHT#3432 THE CREW REPORTED THE CAPTAINS WINDSHIELD ARCHING AND THEY HAD A BURNING SMELL.MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002111100013 20021111 00013 SO 2002 11 11 C2XA02CL225 1 20021107 A 2133 2097K011100 OUTFLOW VALVE EMB 135 EMB135LR 3260305 SO AFT FUSELAGE FAULTY A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 17513 145292 CRW FLIGHT#3064 THE CREW REPORTED RAPID DECOMPRESSION IN FLIGHT.THE PRESSURIZATION WAS INOPERATIVE IN AUTO AND MANUAL MO DES.MAINTENANCE REPLACED THE ELECTROPNEUMATIC OUTFLOW VALVE.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002111100014 20021111 00014 NE 2002 11 11 ARWA20021002 2 20021007 A 7200 ENGINE DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 1 FAILED A ARWA A UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 19 30UA 55184 246 45888 669186 DURING CRUISE AT 280, NR 1 ENGINE ANTI-ICE LIGHT ON. NR 2 ERATIC FOLLOWED BY COMPRESSOR STALL. COULD NOT GET POWER OUT OF ENGINE. AT FL 280 UNABLE TO CLOSE 2N ANTI-ICE VALVE NO NR 1 ENGINE STARTED BACKFIRING AND REDUCED POWER TO PREVENT I T UNTIL POWER COMPLETELY AT IDLE THEN UNABLE TO REGAIN POWER IN ENGINE NR 1. ALSO N2 ERRATIC AND ENGINE VIBRATION & STR ANGE SOUND HEARD ON TAXI IN. NORMAL SHUTDOWN. DECISION WAS MADE WITH THE CREW TO LAND AT THE ALTERNATE BECAUSE MARGINA L WEATHER AT GUATEMALA IN CASE OF HAVING TO GO MISSED APPROACH AND ALSO POSSIBLE WET RUNWAY AND HIGH ELEVATION AIRPORT I N MOUNTAINOUS TERRAIN. PREPARED NR 1 ENGINE FOR 3 ENGINE FERRY FLIGHT FROM GUATE. 2 L 7 4 4F 4 F 4A25 1E8 2002111100015 20021111 00015 WP 2002 11 11 IXXA0200109O 1 20021106 A 3210 57155835510 CYLINDER DOUG DC8 DC873F 302199F WP GEAR DOOR DEFECTIVE A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 606AL 88897 2910 46044 ENROUTE FROM LAX TO TOL, THE LANDING GEAR DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED FOLLOWING LANDING GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR AND THE LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MA INTENANCE INSPECTED THE AIRCRAFT AND FOUND THE GEAR DOOR ACTUATOR CYLINDER DEFECTIVE. MAINTENANCE REPLACED THE CYLINDER AND PERFORMED A SUCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE 2 L 7 4 4F RT 4A25 2002111100016 20021111 00016 WP 2002 11 11 MWEA020687 1 20021108 A 5280 GEAR DOUG DC9 DC914 3022034 WP GEAR DOOR DEFECTIVE A MWEA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 31 500ME 45711 CREW REPORTED GEAR DOOR OPEN LIGHT STAYED ON WITH GEAR HANDLE UP. -- REMOVED AND REPLACED STIFFENER. 2 L 7 2 4F A6WE 2002111100017 20021111 00017 NM 2002 11 11 MWEA020688 1 20021110 A 3260 LIGHT DOUG MD88 MD88 3023688 NM GEAR DEFECTIVE A MWEA O OTHER O OTHER TO TAKEOFF 1 GL 31 701ME 49760 FOLLOWING GEAR RETRACTION THE LEFT MAIN LANDING GEAR LIGHT REMAINS ON. -- PERFORMED AUTOMATIC TEST OF PSEU, TEST PASSE D. CHECKED LATCH SENSOR WITH GO GAUGE AND WIGGLED WIRE BUNDLE WITH GO GAUGE ON SENSOR. SENSOR TESTED GOOD, SWUNG GEAR 15 TIMES WITH ALL INDICATIONS NORMAL. 2 L 7 2 4F RT A6WE 2002111100018 20021111 00018 WP 2002 11 11 CALA0200537 1 20021108 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 218-265 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 98876 49444 INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 218-265. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05-4F AN D 53-05-4B1. 2 L 7 2 4F A6WE 2002111100019 20021111 00019 NM 2002 11 11 CALA0200542 1 20021110 A 5320 WEB BOEING 737 7373T0 1384582 NM STA 578 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND A 3" CRACK IN MAIN CABIN FLOOR SUPPORT WEB FORWARD OF STA 578 AT STRINGER 17R. THE FLOOR SUPPORT WEB WA S REPLACED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2002111100020 20021111 00020 SO 2002 11 11 CX2A02IA234 1 20021108 A 2150 8152403 ACM EMB 145 EMB145 3260210 SO #1 AIE COND. BAY INOPERATIVE A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 27 27962 145110 IAH- FLIGHT 3906, THE CREW NOTED A STRONG SMOKE SMELL WHEN CLEARED INTO POSITION AND HOLD.SMELLED ELECTRICAL IN NATURE, AND, OCCURED AFTER ALL LIGHTS WERE TURNED ON. IAH- MAINTENANCE FOUND PACK #1 OVERHEAT MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE #1 ACM, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002111100021 20021111 00021 SO 2002 11 11 C2XA02BT073 1 20021108 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO INACTIVE A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 12922 145338 EWR---CO3342, CREW REPORTED, "FIRST STRIP OF EMERGENCY AISLE LIGHTS ARE INOPERATIVE....MAINTENANCE RESET AIRCRAFT ELECTR ICAL SYSTEM. OPS.CHECKED AILSE PATH EMERGENCY LIGHTS GOOD IAW EMB145 MM #33-50-00 AND #24-36-00. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4T RT T00011AT 2002111100022 20021111 00022 EU 2002 11 11 AWXA200201089 1 20021108 A 3350 E0053R8B3ASNF CONNECTOR AIRBUS 320 A320231 3930325 EU SEAT ROW 26 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 0 0 076 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 L/H WAS FOUND INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR AND BACKSHELL AT SEAT ROW 26 L/H, FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002111100023 20021111 00023 EU 2002 11 11 AWXA200201090 1 20021109 A 2931 NAS161210 PACKING AIRBUS 320 A320232 3930326 EU ZONE 190 DAMAGED A AWXA O OTHER J K WARNING INDICATION FLUID LOSS DE DESCENT 1 WP 28 667AW 0 0 1710 DTW - EMERGENCY LANDING - FLT 0231 - ON DESCENT INTO DTW EN ROUTE FROM PHX ECAM DISPLAYED YELLOW HYDRAULIC RESERVOIR LOW LEVEL, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE DISCOVERED A HYDRAULIC LEAK WHERE HYDRAULIC LIN E CONNECTS TO AUTO-BRAKE SELECTOR VALVE. REMOVED AND REPLACED O-RING PACKING, SERVICED RESERVOIR AND PERFORMED LEAK CHEC K, NO LEAKS NOTED. 2 L 7 2 4F RT A28NM 2002111100024 20021111 00024 NM 2002 11 11 AWXA200201091 1 20021029 A 5510 6547532565 ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 0 0 23218 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4" CRACK WAS FOUND ON THE FORWARD UPPER SIDE OF THE L/H HORIZONTAL STABILIZER ATTACH BRACKET, BS 1156. MAINTENANCE REMOVED THE DAMAGED L/H HORIZONTAL STABILIZER ATTACH BRACKET AT BS 1156; FABRICATE D A NEW REPLACEMENT ATTACH BRACKET; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 10-11, 42, FIG. 12. 2 L 7 2 4F RT A16WE 2002111100025 20021111 00025 EU 2002 11 11 AWXA200201092 1 20021030 A 5311 D53370241201 FRAME AIRBUS 320 A320231 3930325 EU CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 0 0 66 MCN - MAJOR REPAIR - DURING C-02 CHECK A 1/8" CRACK WAS FOUND AT FASTENER HOLE ON FRAME BS 1810, BELOW STR 14 L/H. MAINT ENANCE CUTOUT CRACK ON FRAME AT BS 1810; FABRICATED A FILLER AND REPAIR ANGLE; AND INSTALLED REPAIR PARTS IAW AWA E.O. 5 3-14-20. 2 L 7 2 4F RT A28NM 2002111100026 20021111 00026 EU 2002 11 11 AWXA200201093 1 20021030 A 5311 D53370238201 FRAME AIRBUS 320 A320231 3930325 EU CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 0 0 66 MCN - MAJOR REPAIR - DURING C-02 CHECK A 1/8" CRACK WAS FOUND AT FASTENER HOLE ON FRAME 38 AT BS 1669, BELOW STR 14 L/H. MAINTENANCE CUTOUT CRACK ON FRAME 38 AT BS 1669; FABRICATED A FILLER AND REPAIR ANGLE; AND INSTALLED REPAIR PARTS IAW A WA E.O. 53-14-20. 2 L 7 2 4F RT A28NM 2002111100027 20021111 00027 EU 2002 11 11 AWXA200201094 1 20021030 A 5311 D53370241200 FRAME AIRBUS 320 A320231 3930325 EU CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 0 0 66 MCN - MAJOR REPAIR - DURING C-02 CHECK A 1/8" CRACK WAS FOUND AT FASTENER HOLE ON FRAME 41 AT BS 1810, BELOW STR 14 R/H. MAINTENANCE CUTOUT CRACK ON FRAME 41 AT BS 1810; FABRICATED A FILLER AND REPAIR ANGLE; AND INSTALLED REPAIR PARTS IAW A WA E.O. 53-14-20. 2 L 7 2 4F RT A28NM 2002111100028 20021111 00028 EU 2002 11 11 AWXA200201095 1 20021030 A 5311 D53370239200 FRAME AIRBUS 320 A320231 3930325 EU CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 0 0 66 MCN - MAJOR REPAIR - DURING C-02 CHECK A 1/8" CRACK WAS FOUND AT FASTENER HOLE ON FRAME 39 AT BS 1725, BELOW STR 14 R/H. MAINTENANCE CUTOUT CRACK ON FRAME 39 AT BS 1725; FABRICATED A FILLER AND REPAIR ANGLE; AND INSTALLED REPAIR PARTS IAW A WA E.O. 53-14-20. 2 L 7 2 4F RT A28NM 2002111100029 20021111 00029 EU 2002 11 11 AWXA200201096 1 20021030 A 5311 D53370238200 FRAME AIRBUS 320 A320231 3930325 EU CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 0 0 66 MCN - MAJOR REPAIR - DURING C-02 CHECK A 1/8" CRACK WAS FOUND AT FASTENER HOLE ON FRAME 38 AT BS 1669, BELOW STR 14 R/H. MAINTENANCE CUTOUT CRACK ON FRAME 38 AT BS 1669; FABRICATED A FILLER AND REPAIR ANGLE; AND INSTALLED REPAIR PARTS IAW A WA E.O. 53-14-20. 2 L 7 2 4F RT A28NM 2002111100030 20021111 00030 EU 2002 11 11 AWXA200201097 1 20021105 A 3350 3402202 SPLICE AIRBUS 320 A320231 3930325 EU SEAT ROW 11 L/H LOOSE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 0 0 66 MCN - EEL - DURING C-02 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMO VED AND REPLACED A BAD SPLICE ON ESCAPE PATH LIGHT AT SEAT ROW 11 L/H PER ESPM 20-53-29, PG.4, FUNCTIONAL CHECK WAS GOOD IAW AWA T/C F1C33301. 2 L 7 2 4F RT A28NM 2002111100031 20021111 00031 EU 2002 11 11 AWXA200201098 1 20021105 A 3350 3402202 SPLICE AIRBUS 320 A320231 3930325 EU SEAT ROW 5 L/H LOOSE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 0 0 66 MCN - EEL - DURING C-02 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED A BAD SPLICE ON ESCAPE PATH LIGHT AT SEAT ROW 5 L/H PER ESPM 20-53-29, PG.4, FUNCTIONAL CHECK WAS GOOD I AW AWA T/C F1C33301. 2 L 7 2 4F RT A28NM 2002111100032 20021111 00032 NM 2002 11 11 AWXA200201099 1 20021029 A 5320 65C105924 FLOOR SUPPORT BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOOR PANEL SUPPORT DOUBL ER PLATE AT BS 958 TO BS 967, RBL 47. MAINTENANCE REMOVED DAMAGED FLOOR PANEL SUPPORT DOUBLER PLATE FROM BS 947.5 TO BS 967, AND FLOOR SUPPORT FROM BS 958 TO BS 967; FABRICATED NEW REPLACEMENT FLOOR SUPPORT; AND INSTALLED REPAIR PART IAW B7 37-300 SRM 51-40-02, PG.16-19, AND SRM 51-40-04, PG. 4. 2 L 7 2 4F RT A16WE 2002111100033 20021111 00033 NM 2002 11 11 AWXA200201100 1 20021024 A 5320 65566551 REVEAL BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 0 0 23218 MCN - MAJOR REPAIR - DURING C-18 CHECK A 3/4" CRACK WAS FOUND FORWARD TORQUE BOX REVEAL AT AFT CARGO COMPARTMENT OPENING , BS 794.3. MAINTENANCE REMOVED THE CRACKED FORWARD TORQUE BOX REVEAL AT AFT CARGO COMPARTMENT OPENING, BS 794.3; FABRIC ATED A NEW REPLACEMENT REVEAL; AND INSTALLED REPAIR PART IAW DWG 65-56655, AND B737-300 SRM 51-40-02, PG.16-19, AND SRM 51-40-04, PG. 3, FIG. 1. 2 L 7 2 4F RT A16WE 2002111100034 20021111 00034 NM 2002 11 11 AWXA200201101 1 20021104 A 5315 694122615 ANGLE BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 0 0 23218 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON THE UPPER SURFACE OF SPLICE ANGLE (AFT R/H CREASE BEAM) BS 1006 TO BS 1016, RBL 52. MAINTENANCE REMOVED THE DAMAGED SPLICE ANGLE; FABRICATED A NEW REPLACEMENT SPLICE ANGLE; AND I NSTALLED REPAIR PART IAW B737-300 SRM 51-40-05, PG. 4, FIG. 2. 2 L 7 2 4F RT A16WE 2002111200001 20021112 00001 CE 2002 11 12 AUS20021101 1 20020919 A 3230 BEARING CESSNA 441 441 2076020 CE HARTZL HCB3T HCB3TN5 GL UPLOCK HOOK WORN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT MAIN LANDING GEAR UPLOCK HOOK WORN ON PIVOT SHAFT AND BEARING. 1 L 7 2 3T RT A28CE 6 C P15EA 2002111200002 20021112 00002 EU 2002 11 12 AUS20021106 1 20021007 A 2121 034944 COOLING FAN BAG BAE146 BAE146300A 1500267 EU AIR DISTRIBUTION FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 AU S (AUS) LT ELECTRONIC FLIGHT INDICATION SYSTEM (EFIS) FAN FAILED. INVESTIGATION FOUND FAN BLADE CRACKED AND RUBBING ON GR ILL. 2 H 7 4 4F RT A49EU 2002111200003 20021112 00003 NE 2002 11 12 AUS20021107 2 20021006 A 7200 PW118A ENGINE EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14RF 14RF9 NE NACELLE VIBRATES W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S 5849 (AUS) SEVERE ENGINE VIBRATION DURING START. LIMITED INFORMATION PROVIDED. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2002111200005 20021112 00005 SW 2002 11 12 AUS20021110 1 20020925 A 2910 2781006029 LINE SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UHR WP HYD SYSTEM CRACKED W O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AU S (AUS) FLAP "UP" HYDRAULIC LINE FLARED END CRACKED. LINE IS LOCATED INBOARD OF THE REAR LT NACELLE. 2 L 7 2 4T 4 T RT A5SW E4WE 2002111200006 20021112 00006 NE 2002 11 12 AUS20021111 2 20020912 A 7532 GASKET GARRTT ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE73140 29001 NE RT ENGINE FAULTY W O OTHER J WARNING INDICATION CR CRUISE 1 AU S (AUS) RT BLEED AIR LINE THERMOSTAT GASKET FAILED. FURTHER INVESTIGATION FOUND THAT THE RT BLEED SWITCHING VALVE OUTLET T EMPERATURE WAS HIGH. 2 L 7 2 4F 4 F RT A16NM E1NM 2002111200007 20021112 00007 2002 11 12 AUS20021117 4 20021008 A 3418 9754421421 TRANSMITTER PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL STALL WARNING FAILED W O OTHER N FALSE WARNING DE DESCENT 1 AU S (AUS) LT ANGLE OF ATTACK (AOA) TRANSMITTER VANE SPRING DEFECTIVE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002111200008 20021112 00008 SW 2002 11 12 AUS20021118 1 20020828 A 2910 2781032273 LINE SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UA 01514 WP MCAULY 4HFR34 4HFR34C652 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) LT MAIN LANDING GEAR DOWN' HYDRAULIC LINE LEAKING. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002111200009 20021112 00009 EU 2002 11 12 AUS20021120 1 20020927 A 2820 AN8324J FITTING AGUSTA A109 A109C 0260118 EU ALLSN 25OC 250C20R GL FUEL SYSTEM FAULTY W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) FUEL SYSTEM UNIONS FAULTY AND LEAKING. AIRCRAFT IS REGISTERED IN USA. 1 G 7 2 3U 3 U H7EU E4CE 2002111200010 20021112 00010 SO 2002 11 12 AUS20021124 2 20020901 A 8530 CYLINDER BEECH 55 95C55 1152708 CE CONT O520 IO520C 17032 SO MCAULY 3AF32C 3AF32C75 GL RT ENGINE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT ENGINE CYLINDERS CORRODED ON CYLINDER WALLS. CORROSION PITS WERE IN EXCESS OF 0.381MM (0.015IN) DEEP. THREE CYL INDERS WERE ALSO FOUND TO BE CRACKED FROM EXHAUST SEATS TO THE EXHAUST PORTS. AIRCRAFT OPERATES FOR APPROXIMATELY 100 HO URS PER YEAR. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P22EA 2002111200011 20021112 00011 CE 2002 11 12 AUS20021128 1 20020901 A 5751 BRACKET BEECH 55 95C55 1152708 CE CONT O520 IO520C 17032 SO MCAULY 3AF32C 3AF32C75 GL AILERON HINGE MISREPAIRED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) LT AILERON INCORRECTLY SECURED TO THE HINGE BRACKET ASSEMBLY. ATTACHMENT HOLE DRILLED OVERSIZE AND A RIVNUT FITTED . UNAPPROVED PART / REPAIR. PERSONNEL / MAINTENANCE ERROR. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P22EA 2002111200012 20021112 00012 CE 2002 11 12 AUS20021134 1 20020901 A 5712 95110113 RIB BEECH 55 95C55 1152708 CE CONT O520 IO520C 17032 SO MCAULY 3AF32C 3AF32C75 GL LT & RT WING CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT AND RT WING OUTER RIBS LOCATED AT STA 191 CORRODED BEYOND LIMITS. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P22EA 2002111200013 20021112 00013 CE 2002 11 12 AUS20021136 1 20020901 A 5280 PIVOT BEECH 55 95C55 1152708 CE CONT O520 IO520C 17032 SO MCAULY 3AF32C 3AF32C75 GL MLG DOOR SEIZED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT MAIN LANDING GEAR OUTER DOOR PIVOTS SEIZED. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P22EA 2002111200014 20021112 00014 GL 2002 11 12 AUS20021137 3 20021009 A 6140 503890571 TACH GENERATOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4MP3 GL PROPELLER FAULTY W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 AU S 204 (AUS) RT PROPELLER TACH-GENERATOR FAULTY. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 2002111200015 20021112 00015 NM 2002 11 12 AUS20021138 1 20021008 A 5730 113T161329 PANEL BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL LT WING SEPARATED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT MAIN LANDING GEAR SUPPORT AFT LOWER ACCESS PANEL MISSING. 2 L 7 2 4F 4 F RT A1NM E23EA 2002111200016 20021112 00016 NM 2002 11 12 AUS20021142 1 20021009 A 2560 4108705 VALVE DHAV DHC8 DHC8315 2809010 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE INFLATION BOTTLE FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT EXIT DITCHING SYSTEM NITROGEN BOTTLE VALVE HEAD FAULTY. DURING SERVICING THE BOTTLE INADVERTENTLY DISCHARGED B UT THE DITCHING DAM FAILED TO INFLATE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002111200017 20021112 00017 NE 2002 11 12 AUS20021143 2 20021012 A 7310 P39401 VALVE BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE ENGINE FUEL LEAKING W O OTHER E K VIBRATION/BUFFET FLUID LOSS NR NOT REPORTED 1 AU S (AUS) NR 1 ENGINE DRAIN TANK EJECTOR VALVE FAULTY. 2 L 7 4 4F 4 F RT A20WE E30NE 2002111200019 20021112 00019 EU 2002 11 12 AUS20021147 1 20021007 A 2751 72A1601 PROXIMITY SWITCH PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL TE FLAP FAILED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) FLAP PROXIMITY SWITCH FAULTY. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002111200020 20021112 00020 NM 2002 11 12 AUS20021148 1 20021010 A 2497 20021N WIRE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE AC GENERATION SHORTED W O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 AU S (AUS) LT AC CONTACTOR BOX WIRE 20021N LOCATED NEAR CB9 SHORT CIRCUITED DUE TO CHAFING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002111200021 20021112 00021 NE 2002 11 12 AUS20021149 2 20021012 A 7314 PAC102MK4 PUMP BOEING 747 747338 NM RROYCE RB211 RB211524D419 54555 NE ENGINE FUEL FAILED W O OTHER F FLT CONT AFFECTED CL CLIMB 1 AU S (AUS) NR 2 ENGINE DRIVEN FUEL PUMP FAILED. 2 L 7 2 4F 4 F RT A20WE E12EU 2002111200023 20021112 00023 NE 2002 11 12 AUS20021152 2 20021012 A 7230 3400010260 BLADE BOEING 737 737800* NM GE CFM56 CFM567B24 NE NR 2 ENG COMP BIRD INGESTION W O OTHER C J F.O.D. WARNING INDICATION CR CRUISE 1 AU S (AUS) NR 2 ENGINE BIRD STRIKE. INVESTIGATION COULD FIND NO AIRFRAME DAMAGE OR EVIDENCE OF ENGINE CORE INGESTION. BIRD DE BRIS EXITED VIA BYPASS DUCT. NR 12 FAN BLADE DAMAGED BEYOND LIMITS. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002111200024 20021112 00024 WP 2002 11 12 ABXA020299 1 20021110 A 5210 59103675 DOOR FRAME DOUG DC9 DC931 3022065 WP FS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 WHILE COMPLYING WITH AD 80-02-16, FOUND CRACK IN OUTER PLUG DOOR FRAME. REPAIRED AREA IAW REA D952-45160-MR. 2 L 7 2 4F A6WE 2002111200025 20021112 00025 WP 2002 11 12 ABXA020300 1 20021018 A 5300 59343753N DOUBLER DOUG DC9 DC932 3022066 WP RT. WHEEL WELL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 RIGHT MAIN FRAME IN WHEEL WELL WAS CRACKED, INBOARD FLANGE. REPAIRED FRAME IAW REA D953-45633-MR AND S.B. 53-100. 2 L 7 2 4F A6WE 2002111200026 20021112 00026 CE 2002 11 12 AUS20021156 1 20020712 A 5712 052301141 RIB CESSNA 172 172N 2072434 CE LYC O320 O320H2AD 41508 EA MCAULY 1C160 1C160DTM GL LT & RT WING CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT AND RT WING LEADING EDGE RIBS SEVERELY CORRODED. SIXTEEN RIBS AND BOTH BOTTOM OUTBOARD WING SKINS REQUIRED REPL ACEMENT. FOUND WHEN RIBS DISMANTLED AFTER FINDING BULGING ALONG THE SPAR INSEVERAL AREAS OUTBOARD OF THE WING STRUTS DUR ING PERIODIC INSPECTION. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 2002111200027 20021112 00027 NM 2002 11 12 AUS20021157 1 20021014 A 2722 3860060101 ACTUATOR BOEING 747 747438 NM RROYCE RB211 RB211524* NE RUDDER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S 0302 (AUS) LOWER RUDDER UPPER ACTUATOR LEAKING. LOSS OF FLUID FROM NR 4 HYDRAULIC SYSTEM. 2 L 7 4 4F 4 F RT A20WE E12EU 2002111200028 20021112 00028 NM 2002 11 12 AUS20021158 1 20021006 A 3242 QF56028 BOLT BOEING 767 767300 1385204 NM RROYCE RB211 RB211524* NE BRAKE LOOSE W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 4 BRAKE RETENTION BOLTS LOOSE. 2 L 7 2 4F 4 F RT A1NM E12EU 2002111200030 20021112 00030 SO 2002 11 12 AUS20021160 1 20021014 A 2140 3716737 LINE PIPER PA34 PA34220T 7103420 SO CONT O360 TSIO360RB 17025 CE HEATER FUEL LEAKING W O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) HEATER FUEL LINE LEAKING. INVESTIGATION FOUND THE ALUMINIUM FUEL LINE HAD BEEN CHAFED BY ELECTRICAL WIRING RUNNING ADJACENT TO THE FUEL LINE. THE WIRE WAS WORN TO THE EXTENT OF ARCING AND BURNING THROUGH THE FUEL LINE. ELECTRICAL WIRI NG WAS POORLY FITTED WITH WIRE TOO TIGHT ACROSS THE FUEL CANISTER AND THE FUEL LINE WAS INADEQUATELY SUPPORTED. 1 L 7 2 3O 3 O A7SO E9CE 2002111200031 20021112 00031 CE 2002 11 12 AUS20021161 1 20020909 A 5341 ME370 GUSSET BEECH 76 76 1153005 CE FUSELAGE BROKEN W K NONE O OTHER IN INSP/MAINT 1 AU S ME370 (AUS) FORWARD FRONT WING SPAR PICKOFF STRUCTURE CRACKED AND LOOSE. FLANGED GUSSET LOCATED AT BS 94.00 BROKE FREE FROM F USELAGE STRUCTURE. 1 L 7 2 3O A29CE 2002111200033 20021112 00033 NM 2002 11 12 AUS20021163 1 20021011 A 5210 CLIP BOEING 737 737376 NM CFMINT CFM56 CFM563C 13802 EU PAX DOOR MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ENTRY DOOR L1 UPPER GUIDE ARM PIN MOVING. INVESTIGATION FOUND THE RETAINING CIRCLIP MISSING. 2 L 7 2 4F 4 F RT A16WE E21EU 2002111200034 20021112 00034 NM 2002 11 12 AUS20021164 1 20021015 A 2597 HARNESS BOEING 737 737330 13844BJ NM RROYCE RB211 RB211524* NE LAVATORY DAMAGED W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AU S (AUS) LAVATORY SHAVER LOOM DAMAGED AND ARCING. CIRCUIT BREAKER C734 POPPED. INVESTIGATION FOUND THAT THE WIRING WAS INCO RRECTLY SECURED/PROTECTED ALLOWING THE WIRING TO CONTACT THE AIRCRAFT STRUCTURE. PERSONNEL / MAINTENANCE ERROR. 2 L 7 2 4F 4 F RT A16WE E12EU 2002111200035 20021112 00035 GL 2002 11 12 AUS20021167 2 20020730 A 7230 6890502 BLADE GOVT N22 N22B 3880102 WP ALLSN 250B 250B17B 03010 GL HARTZL HCA3V HCA3VF7 GL ENGINE SEPARATED W A UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 AU S 2545 (AUS) LT ENGINE SECOND STAGE COMPRESSOR BLADE SEPARATED FROM WHEEL. INSPECTION FOUND A SMALL STAIN AT THE BLADE STUMP I NDICATING THAT A SMALL CRACK HAD BEEN PRESENT FOR SOME TIME. THE CRACKING HAD BEEN INITIATED BY CORROSION PITTING. THE ADJACENT BLADE HAD A SIMILAR CRACK PRESENT. DAMAGE TO COMPRESSOR AND TURBINE. AIRCRAFT OPERATES IN A SALT LADEN ENVIRON MENT BUT HAS REGULAR COMPRESSOR WASHES. 1 H 7 2 3T 3 T A7PC E10CE 5 C P6EA 2002111200036 20021112 00036 NM 2002 11 12 AUS20021168 1 20021016 A 3220 LANDING GEAR DHAV DHC8 DHC8315 2809010 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NOSE MALFUNCTIONED W O OTHER J WARNING INDICATION LD LANDING 1 AU S (AUS) NOSE LANDING GEAR FAILED TO EXTEND. INVESTIGATION COULD FIND NO FAULT. SUSPECT A SMALL QUANTITY OF AIR IN THE HYDR AULIC SYSTEM. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002111200037 20021112 00037 2002 11 12 AUS20021169 4 20020918 A 2210 285T0013123 DAMPER BOEING 767 767330 NM RROYCE RB211 RB211524* NE AUTOPILOT SYSTEM FAILED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 AU S DO1052 (AUS) RT YAW DAMPER FAULTY. 2 L 7 2 4F 4 F RT A1NM E12EU 2002111200038 20021112 00038 CE 2002 11 12 AUS20021170 1 20021007 A 3233 00153840021 SHAFT BEECH 76 76 1153005 CE MLG ACTUATOR FRACTURED W O OTHER O OTHER NR NOT REPORTED 1 AU S (AUS) LT MAIN LANDING GEAR ACTUATOR RAM SHAFT SNAPPED AT THREADED PORTION NEAR RODEND. RAM THEN PUNCHED THROUGH MAIN LAN DING GEAR BAY RIB AND BENT THE RAM SHAFT. 1 L 7 2 3O A29CE 2002111200039 20021112 00039 SO 2002 11 12 AUS20021172 1 20021009 A 6120 7871300 PLATE PIPER PA34 PA34220T 7103420 SO CONT O360 TSIO360RB 17025 CE MCAULY 3AF32C 3AF32C512 GL PROPELLER CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) PROPELLER CONTROL FEATHER GATE STOP PLATE ASSEMBLY LOCATED IN COCKPIT CONTROL QUADRANT CRACKED. 1 L 7 2 3O 3 O A7SO E9CE 5 C P22EA 2002111200040 20021112 00040 2002 11 12 AUS20021174 4 20020910 A 3445 WARNING SYSTEM BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU TCAS FAULTY W O OTHER J WARNING INDICATION CR CRUISE 1 AU S (AUS) TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS) SYSTEM FAULTY. 2 L 7 2 4F 4 F RT A16WE E21EU 2002111200041 20021112 00041 SO 2002 11 12 AUS20021177 1 20021016 A 3230 9515339 LINE PIPER PA34 PA34220T 7103420 SO CONT O360 TSIO360RB 17025 CE MLG HYD SYSTEM CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LANDING GEAR DOWN HYDRAULIC TUBE LOCATED IN NLG WHEEL WELL CORRODED BEYOND LIMITS. 1 L 7 2 3O 3 O A7SO E9CE 2002111200042 20021112 00042 SO 2002 11 12 AUS20021178 1 20021016 A 3230 9515340 LINE PIPER PA34 PA34220T 7103420 SO CONT O360 TSIO360RB 17025 CE MLG HYD SYSTEM CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LANDING GEAR UP HYDRAULIC TUBE LOCATED IN NLG WHEEL WELL CORRODED BEYOND LIMITS. 1 L 7 2 3O 3 O A7SO E9CE 2002111200043 20021112 00043 CE 2002 11 12 AUS20021179 1 20020914 A 3260 602EN556B UPLOCK SWITCH CESSNA 404 404CESSNA 2075901 CE CONT O520 GTSIO520M 17032 SO MCAULY 3FF32 3FF32C501 GL MLG POSITION FAILED W O OTHER N FALSE WARNING CL CLIMB 1 AU S (AUS) RT MAIN LANDING GEAR UPLOCK SWITCH FAILED. 1 L 7 2 3O 3 O A25CE E7CE 5 C P45GL 2002111200044 20021112 00044 NM 2002 11 12 AUS20021182 1 20020921 A 6520 A0211 GEARBOX ROBSIN R22 R22BETA 7640110 NM LYC O320 O320B2C 41508 EA TAIL ROTOR MAKING METAL W K NONE J WARNING INDICATION IN INSP/MAINT 1 AU S 3340 (AUS) TAIL ROTOR GEARBOX METAL CONTAMINATION. 1 G 7 1 3O 3 O H10WE E274 2002111200045 20021112 00045 NE 2002 11 12 AUS20021183 2 20021006 A 7310 216362037 MANIFOLD BAC 146 146100A 1500260 EU LYC ALF502 ALF502R3A 41580 NE ENGINE FUEL FAULTY W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) ENGINE RT FUEL MANIFOLD LEAKING. NDT INVESTIGATION FOUND A WELD DEFECT AND CORROSION PITTING. DURING TROUBLESHOOTI NG, ONE OF THE BOLTS SECURING THE AFT COMBUSTOR FUEL DRAIN BROKE OFF REQUIRING THE ENGINE TO BE CHANGED. 2 H 7 4 4F 4 F RT A49EU E6NE 2002111200046 20021112 00046 NE 2002 11 12 AUS20021184 2 20021018 A 7310 216362038 MANIFOLD BAG BAE146 BAE146300A 1500267 EU LYC ALF520 ALF520* 41580 NE ENGINE FUEL LEAKING W O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 AU S (AUS) NR 3 ENGINE RT FUEL MANIFOLD LEAKING AT MANIFOLD TO COMBUSTOR CASE JOIN. EVIDENCE OF FIRE AROUND LEAK. 2 H 7 4 4F 4 F RT A49EU E6NE 2002111200047 20021112 00047 NM 2002 11 12 AUS20021185 1 20021019 A 2497 CABLE BOEING 747 747400 NM GE CF6 CF680C2* GL NR 1,2,3,4 IDG DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 1,2,3, AND 4 IDG FEEDER CABLES CHAFED IN NUMEROUS AREAS. OVERHEATING AND POOR CABLE TERMINATION ALSO NOTED. 2 L 7 4 4F 4 F RT A20WE E23EA 2002111200048 20021112 00048 NM 2002 11 12 AUS20021186 1 20021017 A 3230 AS11706K0280 HOSE BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL MLG HYD SYSTEM FAILED W O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 AU S (AUS) RT MAIN LANDING GEAR RETRACTION ACTUATOR HOSE SPLIT. LOSS OF HYDRAULIC FLUID. 2 L 7 2 4F 4 F RT A1NM E23EA 2002111200049 20021112 00049 CE 2002 11 12 AUS20021188 1 20021007 A 8011 646275 MOTOR CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO MCAULY D3A34 D3A34C404 GL ENGINE STARTER SHORTED W O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 AU S 412 (AUS) STARTER MOTOR WINDINGS SHORT CIRCUITED TO GROUND. 1 H 7 1 3O 3 O A4CE E5CE 5 C P47GL 2002111200050 20021112 00050 EU 2002 11 12 AUS20021189 1 20021016 A 2497 LEAD REIMS 406 F406 7535723 EU PWA PT6 PT6A112 52043 NE MCAULY 3G34C7 3GFR34C701 GL STARTER GEN BROKEN W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S (AUS) STARTER-GENERATOR FAULTY. INSPECTION FOUND SEVERAL BRUSH LEADS BROKEN AND COMMUTATOR DAMAGED. 1 L 7 2 3T 3 T RT A54EU E4EA 5 C P60GL 2002111200051 20021112 00051 NM 2002 11 12 AUS20021191 1 20021004 A 3242 214665 BRAKE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE LT MLG FAULTY W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AU S (AUS) LT MAIN LANDING GEAR BRAKES FAULTY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002111200052 20021112 00052 NM 2002 11 12 AUS20021194 1 20021019 A 5320 DRAIN VALVE BOEING 747 747400 NM GE CF6 CF680C2* GL FUSELAGE CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) CENTER SECTION AFT DRAINS BLOCKED BY DUST AND DEBRIS. FOUND DURING INSPECTION IAW AD/B747/71. 2 L 7 4 4F 4 F RT A20WE E23EA 2002111200053 20021112 00053 EU 2002 11 12 AUS20021196 1 20021016 A 2797 S1800051N CONNECTOR BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FLIGHT CONTROLS CONTAMINATED W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 AU S (AUS) CONNECTOR "H" LOCATED AT 162-00-00 IN THE RT MAIN LANDING GEAR BAY MOISTURE CONTAMINATION. 2 H 7 4 4F 4 F A49EU E6NE 2002111200054 20021112 00054 NE 2002 11 12 AUS20021199 2 20021020 A 7200 13138 ENGINE BOEING 747 747438 NM RROYCE RB211 RB211524* NE NR 4 SURGES W A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 AU S (AUS) NR 4 ENGINE SURGE. EPR RAN DOWN AND EGT INCREASED. 2 L 7 4 4F 4 F RT A20WE E12EU 2002111200055 20021112 00055 SO 2002 11 12 AUS20021202 1 20021021 A 2913 38998007 PUMP PIPER PA34 PA34220T 7103420 SO HYD SYSTEM MAKING METAL W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) LANDING GEAR HYDRAULIC PUMP CONTAMINATED WITH SWARF. PUMP IS ANEW ITEM. SUSPECT POOR QUALITY CONTROL BY MANUFACTUR ER. 1 L 7 2 3O A7SO 2002111200056 20021112 00056 NM 2002 11 12 AUS20021203 1 20021013 A 2823 60B9240616 SHUTOFF VALVE BOEING 747 747400 NM GE CF6 CF680C2* GL FUEL SELECTOR UNAPPROVED PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S N52932 (AUS) NR 1 FUEL SHUTOFF VALVE INCORRECT PART. FOUND DURING INSPECTION IAW AD/B747/193. PERSONNEL/MAINTENANCE ERROR. UNAP PROVED PART. 2 L 7 4 4F 4 F RT A20WE E23EA 2002111200057 20021112 00057 NM 2002 11 12 VNAA0211002 1 20021101 A 7900 SHIM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 441JS 3059 JUST PRIOR TO DESCENDING, THE CREW RECEIVED A HIGH OIL PRESSURE INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDB OOK AND FEATHERED THE PROP WHILE PASSING THROUGH 24,000 FEET. FLIGHT 4055 LANDED AT YUL WITH NO FURTHER INCIDENTS. OUT STATION MAINTENANCE INSPECTED AND REMOVED A SHIM FROM THE OIL PRESSURE REGULATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 79-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002111200058 20021112 00058 NM 2002 11 12 VNAA0211004 1 20021105 A 3000 SPSDO328242 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LH FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 442JS 162 3060 ENROUTE, THE CREW RECEIVED A WINDSHIELD HEAT FAIL CAS MESSAGE. FLIGHT 4039 WAS IN ICING CONDITIONS AND AFTER REVIEWING THE WEATHER FOR THE REST OF THE ROUTE, MAINTENANCE HAD FLIGHT 4039 RETURN TO PHL. PIT MAINTENANCE WAS SENT TO PHL AND REPLACED THE FWD WINDSHIELD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 56-00-00. OPERATIONAL CHECKS WERE PERFORMED A ND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002111200059 20021112 00059 NM 2002 11 12 AUS20021204 1 20021021 A 2421 AM73951515B IDG BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL RT IDG FAILED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) RT INTEGRATED DRIVE GENERATOR (IDG) FAILED. METAL FOUND IN OIL FILTER. 2 L 7 2 4F 4 F RT A1NM E23EA 2002111200060 20021112 00060 NM 2002 11 12 AUS20021205 1 20021019 A 2121 732591B FAN BOEING 767 767330 NM RROYCE RB211 RB211524* NE EQUIPMENT BAY FAULTY W O OTHER E F B VIBRATION/BUFFET FLT CONT AFFECTED SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 AU S (AUS) FORWARD EQUIPMENT EXHAUST FAN FAULTY. 2 L 7 2 4F 4 F RT A1NM E12EU 2002111200061 20021112 00061 CE 2002 11 12 AUS20021206 1 20021021 A 2435 TERMINAL LUCAS LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP STARTER GEN BURNED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 AU S 104 Y0357 (AUS) APU STARTER-GENERATOR FAILED. INVESTIGATION FOUND THE BATTERY TERMINAL ON THE STARTER-GENERATOR SEVERELY BURNED AN D THE STARTER CRIMP BURNED. INTERNAL SHORT. 2 L 7 2 4F 4 F RT T00008WI E6WE 2002111200062 20021112 00062 NM 2002 11 12 AUS20021207 1 20020930 A 5315 BAC1505100617 FLOORBEAM BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FLOORBEAM UPPER T CHORD LOCATED AT STA 460 CORRODED. FOUND DURING CPCP INSPECTION. 2 L 7 3 4F 4 F RT A3WE E2EA 2002111200063 20021112 00063 CE 2002 11 12 AUS20021208 1 20021017 A 3520 510010739 LINE CESSNA 421 421C 2076016 CE CONT O520 GTSIO520M 17032 SO MCAULY 3FF32 3FF32C501 GL PAX OXYGEN CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S 3955 (AUS) OXYGEN INTERCONNECT LINES CORRODED FROM THE INSIDE OUT. 1 L 7 2 3O 3 O A7CE E7CE 5 C P45GL 2002111200064 20021112 00064 SO 2002 11 12 AUS20021210 1 20021021 A 2913 A9839TOPOFHOUSI CONTROL VALVE PIPER PA34 PA34220T 7103420 SO CONT O360 TSIO360RB 17025 CE HYDRAULIC PUMP LOOSE W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LANDING GEAR HYDRAULIC PUMP PRESSURE CONTROL VALVE LOOSE IN HOUSING. 1 L 7 2 3O 3 O A7SO E9CE 2002111200065 20021112 00065 CE 2002 11 12 AUS20021211 1 20021016 A 2720 50524326 ARM BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A42 52043 NE MCAULY 3G34C7 3GFR34C701 GL RUDDER PEDAL WORN W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RUDDER PEDAL PIVOT ARM WORN AND FINALLY FAILED IN AREA OF PIVOT BUSHES. 1 L 7 2 4T 4 T A24CE E4EA 5 C P60GL 2002111200066 20021112 00066 EU 2002 11 12 AUS20021212 1 20021015 A 3320 126039MS BALLAST BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE GALLEY LIGHT BURNED OUT W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) REAR GALLEY WORK LIGHT BALLAST BURNED OUT. 2 H 7 4 4F 4 F A49EU E6NE 2002111200067 20021112 00067 NM 2002 11 12 AUS20021213 1 20021021 A 7500 UL37991 LINE BOEING 747 747438 NM RROYCE RB211 RB211524* NE ENGINE BLEED AIR FRACTURED W C ABORTED TAKEOFF E J B VIBRATION/BUFFET WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 AU S (AUS) NR 4 ENGINE P4 PNEUMATIC LINE FRACTURED. SOME MINOR HEAT DAMAGE. 2 L 7 4 4F 4 F RT A20WE E12EU 2002111200068 20021112 00068 NM 2002 11 12 AUS20021214 1 20021022 A 2721 658D1005 ACTUATOR BOEING 767 767330 NM RROYCE RB211 RB211524* NE RUDDER TAB JAMMED W O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 AU S 1095A (AUS) RUDDER TRIM ACTUATOR JAMMED. 2 L 7 2 4F 4 F RT A1NM E12EU 2002111200070 20021112 00070 NM 2002 11 12 AUS20021233 1 20021024 A 2421 AM747194B IDG BOEING 767 767330 NM RROYCE RB211 RB211524* NE LEFT FAILED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 AU S (AUS) LT INTEGRATED DRIVE GENERATOR (IDG) FAILED. 2 L 7 2 4F 4 F RT A1NM E12EU 2002111200071 20021112 00071 WP 2002 11 12 AUS20021236 2 20021022 A 7510 8962988 SHIELD SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UA 01514 WP MCAULY 4HFR34 4HFR34C652 NE ENGINE ANTI-ICE LEAKING W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AU S 29 (AUS) RT ENGINE FIRE WARNING LIGHTS ILLUMINATED IN FLIGHT. BOTTLES DISCHARGED. COULD FIND NO FIRE OR DAMAGE. ALL RT ENGI NE FIRE DETECTORS AND FIRE BOTTLES REPLACED. DURING NEXT FLT, RT ENG FIRE WARNING AGAIN ILLUMINATED. FIRE BOTTLES AGAIN DISCHARGED. FURTHER INVESTIGATION COULD FIND NO FAULTS. TEST FLT WAS CARRIED OUT & FIRE WARNING AGAIN ILLUMINATED APPRO X 75 SEC AFTER SELECTION OF INTAKE HEAT. WARNING EXTINGUISHED WHEN INTAKE HEAT SELECTED OFF. INSPECTION COULD STILL NOT FIND ANY FAULT & COULD NOT BE DUPLICATED ON GROUND. AFTER FURTHER TROUBLESHOOTING, SMALL AIR LEAK FROM THE ENGINE ANTI-I CING SHIELD LOCATED ADJACENT TO IGNITOR BOX ATTACHMENT POSTS. AREA SEALED & A/C TEST FLOWN WITH NO FURTHER OCCURRENCES. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002111200072 20021112 00072 EU 2002 11 12 AUS20021239 1 20021026 A 3210 200877961 PAD BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT MAIN LANDING GEAR DIRECTION STOP PAD SEPARATED AND MISSING. AREA CHAFED. 2 H 7 4 4F 4 F A49EU E6NE 2002111200073 20021112 00073 SW 2002 11 12 AUS20021241 1 20021010 A 2497 WIRE HARNESS SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL COCKPIT DAMAGED W C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 AU S (AUS) AIRCRAFT WIRING LOOM LOCATED UNDER THE FLOOR PLATE TO THE REAR OF THE LT COCKPIT BULKHEAD DAMAGED. INVESTIGATION F OUND TWELVE WIRES IN THE LOOM WERE BURNT. SUSPECT CAUSED BY DRILL DAMAGE. PERSONNEL/MAINTENANCE ERROR. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2002111200074 20021112 00074 NM 2002 11 12 AUS20021242 1 20021019 A 2742 6355B000103 ACTUATOR BOEING 737 737823 13844BZ NM GE CFM56 CFM567B24 NE STABILIZER FAULTY W O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 AU S (AUS) STABILIZER TRIM FAILED TO OPERATE DUE TO A FAULTY ACTUATOR. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002111200075 20021112 00075 EU 2002 11 12 2002F00985 1 20020125 A 7603 C468CP1065 CONTROL CABLE BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE7315R 01518 WP LT ENGINE CONTAMINATED A B8MA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 NM 07 626CG 10143 258041 P91186 PRECAUTIONARY SHUTDOWN OF LEFT ENGINE BECAUSE OF INABILITY TO REDUCE POWER FROM CRUISE. SUSPECT MOISTURE IN POWER CONTR OL TELEFLEX CABLE ASSEMBLY FREEZING AT HIGH ALTITUDE. (M) 2 L 7 2 4F 4 F RT A3EU E6WE 2002111200076 20021112 00076 NM 2002 11 12 AUS20021243 1 20021029 A 2722 386006102 ACTUATOR BOEING 747 747438 NM RUDDER LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AU S 0301 (AUS) UPPER RUDDER ACTUATOR LEAKING. LOSS OF NR 1 HYDRAULIC SYSTEM FLUID. 2 L 7 4 4F RT A20WE 2002111200078 20021112 00078 NM 2002 11 12 AUS20021245 1 20021026 A 2432 279202 CHARGER BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU BATTERY FAULTY W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 AU S 1436 (AUS) BATTERY CHARGER HOT AND EMITTING ELECTRICAL ODOURS. 2 L 7 2 4F 4 F RT A16WE E21EU 2002111200079 20021112 00079 NE 2002 11 12 AUS20021246 2 20021029 A 7200 PW118A ENGINE EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14SF 14SF9 NE LEFT BIRD INGESTION W O OTHER C E J F.O.D. VIBRATION/BUFFET WARNING INDICATION LD LANDING 1 AU S 3015 (AUS) LT ENGINE CONTAINED EVIDENCE OF BIRD STRIKE. INSPECTION COULD FIND NO DAMAGE. FOLLOWING INSPECTION AND WATER WASH A GROUND RUNWAS CARRIED OUT WITH ALL INDICATIONS NORMAL. ENGINE WILL BE MONITORED FOR ANY DETERIORATION. 2 L 7 2 4T 4 T RT A31SO E20NE 6 N P11NE 2002111200081 20021112 00081 WP 2002 11 12 ASAA02803344 1 20021002 A 5320 993653433 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING 30K CHECK, FOUND MAIN CABIN FLOOR SUPPORT CORRODED BEYOND LIMITS AT STATION 180, RBL 9-43. FABRICATED AND INSTALLED REPLACEMENT SUPPORT PER SRM 51-30-2, 51-10-4 AND 51-10-2. (M) 2 L 7 2 4F RT A6WE 2002111200082 20021112 00082 WP 2002 11 12 ASAA02803345 1 20021002 A 5230 4920233U503 BRACKET DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FORWARD CARGO BAY DOOR AFT SIDE STOP, 2ND FROM TOP, BRACKET CRACKED. REPLACED BRACKET PER SRM 51-10-4, 51-30-1, AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002111200083 20021112 00083 WP 2002 11 12 ASAA02803346 1 20021002 A 5230 4920233U503 BRACKET DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING 30K-CHECK, FOUND AFT CARGO BAY DOOR FORWARD SIDE UPPER STOP BRACKET CRACKED. REPLACED BRACKET PER SRM 51-1 0-4, 51-30-1, AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002111200084 20021112 00084 WP 2002 11 12 ASAA0280336 1 20021001 A 5320 991006475 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - FOUND DURING C-CHECK, CRACK IN AFT SIDE OF RIGHT MAINTENANCE PLATFORM IN AFT ACCESSORY COMPARTMENT. INSTALLED DOU BLER ON PLATFORM PER SRM 53-01, PAG 10, FIG 2. (M) 2 L 7 2 4F A6WE 2002111200085 20021112 00085 WP 2002 11 12 ASAA0280337 1 20021002 A 5310 5936038501 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - FOUND DURING C-CHECK, VERTICAL FACE OF AFT CARGO BAY LOWER BEAM TO BE CORRODED. INSTALLED BEAM DOUBLER AND SPLICE PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002111200086 20021112 00086 WP 2002 11 12 ASAA0280338 1 20021002 A 5347 59366634521 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - FOUND DURING C-CHECK, LEFT FORWARD TIEDOWN TRACK IN AFT CARGO BAY CORRODED ON OUTBOARD SIDE. REPLACED SECTION OF TRACK FROM STATION 1007-1193 PER SRM 51-30-5, PAGE 1-14 AND 51-30-2. (M) 2 L 7 2 4F A6WE 2002111200087 20021112 00087 WP 2002 11 12 ASAA0280339 1 20021002 A 5230 592600317 BRACKET DOUG DC9 DC982 3022082 WP BARRIER DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - FOUND DURING C-CHECK, AFT CARGO BAY BARRIER DOOR OUTER SKIN FORWARD ATTACH BRACKET CRACKED. REPLACED BRACKET PER SRM 51-30-1. (M) 2 L 7 2 4F A6WE 2002111200088 20021112 00088 WP 2002 11 12 ASAA0280373 1 20021016 A 7830 3938192501 GUIDE DOUG DC9 DC983 3022083 WP THRUST REVERSER WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING 30K CHECK, LEFT ENGINE AFT THRUST REVERSER PANEL AFT MOUNT BOLT GUIDES WORN. REPLACED MOUNT BOLT GUIDE BRA CKET PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002111200089 20021112 00089 WP 2002 11 12 ASAA0280374 1 20021016 A 5347 593096125 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING 30K-CHECK, FOUND FALSE SEAT TRACK CORRODED AT FS 1155, BL 0. REPLACED TRACK PER SRM 51-30-1. (M) 2 L 7 2 4F RT A6WE 2002111200090 20021112 00090 WP 2002 11 12 ASAA0280375 1 20021016 A 5514 991840183 BRACKET DOUG DC9 DC983 3022083 WP HORIZ STAB CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K-CHECK, LEFT HORIZONTAL STABILIZER REAR SPAR CAP COVER INTERNAL BRACKET IS CRACKED. REPLACED BRAC KET PER SRM 51-10-2, AND DOUGLAS DWG 9917401. (M) 2 L 7 2 4F RT A6WE 2002111200091 20021112 00091 WP 2002 11 12 ASAA0280379 1 20021017 A 5310 5936064503 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, RIGHT FRAME TO SKIN BRACKET CORRODED AT FS 1212, LONGERON 29R. REPLACED BRACKET PER SRM 5 1-10-2 AND -4, AND DAC DWG 5936064. (M) 2 L 7 2 4F RT A6WE 2002111200092 20021112 00092 WP 2002 11 12 ASAA0280380 1 20021017 A 5310 5936064501 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING 30K-CHECK, RIGHT FRAME TO SKIN OUTBOARD BRACKET CORRODED AT FS 1220, LONGERON 29R. REPLACED BRACKET PER SR M 51-10-2 AND -4, AND DAC DWG 5936064. (M) 2 L 7 2 4F RT A6WE 2002111200093 20021112 00093 WP 2002 11 12 ASAA0280381 1 20021017 A 5310 5936064503 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K-CHECK, RIGHT FRAME TO SKIN INBOARD BRACKET CORRODED AT FS 1220, LONGERON 29R. REPLACED BRACKET P ER SRM 51-10-2 ND -4, AND DAC DWG 5936064. (M) 2 L 7 2 4F RT A6WE 2002111200094 20021112 00094 WP 2002 11 12 ASAA0280382 1 20021017 A 5320 5936071 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K-CHECK, FLOOR SUPPORT ANGLE CORRODED AT FS 1214, LONGERON 29R. REPLACED SUPPORT ANGLE PER SRM 51- 10-2 AND -4, AND DAC DWG 5936071-507. (M) 2 L 7 2 4F RT A6WE 2002111200095 20021112 00095 WP 2002 11 12 ASAA0280383 1 20021017 A 5320 5936071 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, 'J' ANGLE CORRODED AT FS 1212-1219 BETWEEN LONGERON 30-29R. REPLACED 'J' ANGLE PER SRM 51 -10-4 AND DAC DWG 5936071-507. (M) 2 L 7 2 4F RT A6WE 2002111200096 20021112 00096 WP 2002 11 12 ASAA0280384 1 20021017 A 5313 5936037501 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K-CHECK, LONGERON 29R CORRODED IN AFT PIT FROM STATION 1212-1231. REPLACED SECTION OF LONGERON 29R FROM FS 1117-1250 PER SRM 51-30-5 AND 51-10-4. (M) 2 L 7 2 4F RT A6WE 2002111200097 20021112 00097 WP 2002 11 12 ASAA0280385 1 20021017 A 5320 5936071505 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K-CHECK, INTERCOSTAL CORRODED BETWEEN LONGERON 30-29R AT FS 1153. REPLACED INTERCOSTAL PER SRM 51- 10-4 AND -30-2, AND DAC DWG 5936071. (M) 2 L 7 2 4F RT A6WE 2002111200098 20021112 00098 WP 2002 11 12 ASAA0280386 1 20021017 A 5320 5936437502 PLATE DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K-CHECK, AFT CARGO BAY SCUFF PLATE HAS DEEP GOUGES. REPLACED FORWARD HALF OF SCUFF PLATE PER SRM 5 1-10-4. (M) 2 L 7 2 4F RT A6WE 2002111200099 20021112 00099 WP 2002 11 12 ASAA0280387 1 20021017 A 5320 59364371 PLATE DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K-CHECK, AFT CARGO BAY SCUFF PLATE HAS DEEP GOUGES. REPLACED AFT HALF OF SCUFF PLATE PER SRM 51-10 -4. (M) 2 L 7 2 4F RT A6WE 2002111200100 20021112 00100 WP 2002 11 12 ASAA0280388 1 20021017 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN INOPERATIVE. REATTACHED LOOSE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2002111200101 20021112 00101 WP 2002 11 12 ASAA0280389 1 20021017 A 5310 5936038501 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 OAK - FOUND C-CHECK, AFT CARGO BAY DOOR JAMB BEAM IS CORRODED IN SEVERAL PLACES. REMOVED CORRODED AREA, ADDED FILLER, A ND INSTALLED DOUBLER PER EA 5310-02122. (M) 2 L 7 2 4F RT A6WE 2002111200102 20021112 00102 NE 2002 11 12 NSVA0208 2 20020308 A 7530 LINKAGE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE DISCONNECTED A NSVA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 277MJ 340B277 401 ORF - DURING TAKEOFF ROLL, LEFT PROP DROPPED TO 400 RPM AND TORQUE DROPPED 200. TAKEOFF WAS ABORTED AFTER ROLL BACK OF ENGINE POWER WAS EVIDENT. FOUND VG ACTUATOR/START BLEED VALVE LINKAGE DISCONNECTED. GE REP WAS CONTACTED AND A BORESCO PE OF THE ENGINE WAS CONDUCTED WITH NO SIGNIFICANT FINDINGS. DECU WAS REMOVED AND REPLACED. GPA PRODUCED AN ITT MARGIN OF 47.8 DEGREES CELSIUS. DECU SENT TO GE FOR DOWNLOAD. GROUND RUN OF ENGINE SHOWED THAT ALL PARAMETERS WERE IN LIMITS , HOWEVER DECU DATA CAME BACK SHOWING NR 1 ENGINE GAS GENERATOR HAD EXCEEDED MAX SPEED AS PER GE ITEM TRANSFERRED TO COL GAN AIR WORKORDER. PRIOR TO THIS KNOWLEDGE THE AIRCRAFT WAS RELEASED FOR FLIGHT. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2002112600042 20021126 00042 CE 2002 11 26 2002F00990 1 20021010 A 7120 12991004717 TRUSS BEECH 1900 1900D 1154162 CE RT NACELLE CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 123YV 7982 UE123 AIRCRAFT 123 WAS IN FARMINGTON NEW MEXICO FOR A STRUCTURAL INSPECTION. WHILE IN MAINTENANCE, THE RIGHT TRUSS WAS FOUND T O BE CRACKED ON THE INBOARD AND OUTBOARD COWLING SUPPORT BRACKETS. THE CORRECTIVE ACTION WAS THAT THEY REMOVED AND REPLA CED THE RIGHT TRUSS. THE TEARDOWN REPORT WAS RECIEVED ON 11/14/02. THIS REPORT STATES THAT AN 8000 HOUR MAG. PARTICLE IN SPECTION WAS PERFORMED IN ACCORDANCE TO BEECH 1900D MAINTENANCE MANUAL. THEY REPAIRED THE TRUSS SUPPORT MOUNTS 2 EACH BY GRINDING THE CRACK OUT OF WELD AND REWELDING. 2 L 7 2 4T RT A24CE 2002111200103 20021112 00103 CE 2002 11 12 044697 1 20021102 A 3260 1143610441 SQUAT SWITCH BEECH 1900 1900D 1154162 CE RT MLG MALFUNCTIONED A AMWA O OTHER N FALSE WARNING CL CLIMB 1 CE 07 140ZV UE140 AFTER TAKEOFF, FLIGHT 5431, THE LANDING GEAR HANDLE WAS PLACED IN THE UP POSITION. THE LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT AND WAS RETURNED TO THE GATE. THE ENTIRE TIME THE CREW HAD THE GEAR DOWN AND LOCKED INDICATIONS. REMOVED AND REPLACED THE RIGHT SQUAT SWITCH. NO TEARDOWN REPORT WILL BE REQUIRED. 2 L 7 2 4T RT A24CE 2003022000116 20030220 00116 CE 2003 2 20 2002F00989 1 20021016 A 7120 1299100471 TRUSS BEECH 1900 1900D 1154162 CE RT ENGINE CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 166YV 2906 UE166 AIRCRAFT 166 WAS IN FOR A STRUCTURAL INSPECTION. WHILE IN MAINTENANCE, THE RT TRUSS WAS DISCOVERED TO HAVE A CRACK AT TH E INBOARD AND OUTBOARD UPPER COWLING SUPPORT BRACKETS. REMOVED AND REPLACED THE RT TRUSS. REPORT STATES THAT VENDOR FOUN D THE TRUSS CRACKED AT BOTH UPPER COWLING BRACKETS. VENDOR PROCEEDED TO REPAIR TRUSS SUPPORT BRACKET MOUNTS BY FABRICATI NG AND INSTALLING REPAIR DOUBLERS AND FILLERS ON UPPER COWLING BRACKETS IAW REPAIR DRAWING SR-CO-00012 REV B. DATED 12-1 0-02. COMPLIED WITH "H" CHECK INSPECTION IAW REPS SRM. VISUALLY VERIFIED THE COMPLETION OS SB 71-3024 AND SB 71-3144 REV "I" HAS BEEN PREVIOUSLY COMPLIED WITH IN ACCORDANCE WITH AD 2001-22-16. P 2 L 7 2 4T RT A24CE 2002112600097 20021126 00097 NM 2002 11 26 2002UALA01650 1 20021102 A 5320 CLIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 FRAME CLIP AT STA 1300 STR 21L CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW CLIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112600101 20021126 00101 NM 2002 11 26 2002UALA01651 1 20021102 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 CREASE BEAM INBOARD CHORD STA 733-755, LBL 63 STR 17L CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED INNER CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112600105 20021126 00105 NM 2002 11 26 2002UALA01652 1 20021102 A 5320 ANGLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT SIDE OF FRAME OB CREASE BEAM TEE ANGLE CRACKED IN RADIUS, STA 902-903, STR 17R. MAJOR REPAIR ACCOMPLISHED. INSTALL ED REPAIR ANGLES. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112600111 20021126 00111 NM 2002 11 26 2002UALA01654 1 20021104 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 DOOR 2R CUT OUT CREASE BEAM IB CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED IB CHORD OF CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112600119 20021126 00119 NM 2002 11 26 2002UALA01664 1 20021104 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 CABIN FLOORBEAM UPPER CAP CORRODED, STA 310, RBL 38, STR 17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR AND L- ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700012 20021127 00012 NM 2002 11 27 2002UALA01665 1 20021104 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 CABIN FLOOR BEAM CORRODED, STA 1520, STR 27L. MAJOR REPAIR ACCOMPLISHED. INSTALLED INTERNAL ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700013 20021127 00013 NM 2002 11 27 2002UALA01666 1 20021104 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FUSELAGE FRAME CORRODED, STA 1520, STR 27L. MAJOR REPAIR ACCOMPLISHED. INSTALLED INTERNAL ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700019 20021127 00019 NM 2002 11 27 2002UALA01670 1 20021105 A 3350 AD321430 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 804UA 759 "EPSU BATTERY L" MESSAGE DISPLAYED AFTER EMERGENCY LIGHTS TEST. REPLACED BATTERY ASSEMBLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112700020 20021127 00020 NM 2002 11 27 2002UALA01671 1 20021105 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 FUSELAGE RT SIDE CREASE BEAM HAS CORRODED FASTENERS. STA 1420 - 1440. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700021 20021127 00021 NM 2002 11 27 2002UALA01672 1 20021105 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 FUSELAGE RT CREASE BEAM CORRODED, STA 1420. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700023 20021127 00023 NM 2002 11 27 2002UALA01674 1 20021106 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FRAME GOUGED, STA 1500, RBL 13. MAJOR REPAIR ACCOMPLISHED. INSTALLED INTERNAL DOUBLER STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700031 20021127 00031 NM 2002 11 27 2002UALA01685 1 20021107 A 7120 ISOLATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 NR 1 ENGINE FWD MOUNT ISOLATOR JOURNAL ON MOUNT BEAM IS WORN AND DISCOLORED. MAJOR REPAIR ACCOMPLISHED. REPLACED ENGIN E MOUNT BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700032 20021127 00032 NM 2002 11 27 2002UALA01686 1 20021107 A 5320 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 CABIN FLOOR BEAM SHEAR WEB CORRODED, STA 1680, RBL 52. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR STA 1680 TO 1686, RBL 46 TO RBL 55. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700034 20021127 00034 NM 2002 11 27 2002UALA01687 1 20021107 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 LT CABIN FLOOR CREASE BEAM INBOARD ANGLE CORRODED STA 680 TO 740, DOOR 2L. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM ANGLE, STA 663 TO 754. 2 L 7 2 4F 4 F RT A2NM E17NE 2002111200104 20021112 00104 CE 2002 11 12 AMWA044554 1 20021029 A 2910 MS287774 O-RING BEECH 1900 1900D 1154162 CE HYD SYSTEM FAILED A AMWA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CE 07 3YV UE3 ON TAXI OUT, FLIGHT 6841, THE RIGHT BRAKE BECAME MUSHY. THE AIRCRAFT THEN RETURNED TO THE GATE WITH NO FURTHER INCIDENT . THE REASON FOR THE PROBLEM WAS THAT THERE WAS LOW FLUID IN THE RESERVOIR. REMOVED AND REPLACED AN O-RING, SECURED TH E FITTING, AND SERVICED WITH FLUID. 2 L 7 2 4T RT A24CE 2002111200105 20021112 00105 CE 2002 11 12 AMWA044606 1 20021030 A 3246 1143880251 WHEEL BEECH 1900 1900D 1154162 CE RT MLG FAILED A AMWA K NONE O OTHER LD LANDING 1 CE 07 140ZV 685 685 UE140 UPON LANDING, FLIGHT 2624, THE CREW REPORTED A BAD BRAKE ACTION FROM THE RIGHT BRAKE. THE RIGHT BRAKE PEDAL FELT MUSHY. AFTER THE AIRCRAFT WAS TAXIED, THE CREW INSPECTED THE AIRCRAFT'S RIGHT WHEEL AND FOUND METAL SHAVINGS IN THE WHEEL ASSE MBLY . CHANGED THE LANDING GEAR, RIGGED AND DID TRACTION CHECKS. ALSO CHANGED THE MAIN WHEEL ASSEMBLY. 2 L 7 2 4T RT A24CE 2002111200106 20021112 00106 CE 2002 11 12 AMWA044616 1 20021030 A 3233 11238002223 ACTUATOR BEECH 1900 1900D 1154162 CE NLG FAILED A AMWA O OTHER O OTHER LD LANDING 1 CE 07 231YV 4559 4559 UE231 UPON LANDING, FLIGHT 5533, THE CREW REPORTED THAT THE NOSE GEAR ANNUNCIATOR DID NOT ILLUMINATE IN GEAR DOWN POSITION. T HE BULB WAS THEN CHECKED WHICH WAS FOUND TO BE OKAY. THE CREW MANUALLY LOWERED THE GEAR PER THE CHECKLIST. THEN DECLAR ED AN EMERGENCY LANDING IN PITTSBURGH, PENNSYLVANIA WITHOUT INCIDENT. REMOVED AND REPLACED THE NOSE GEAR ACTUATOR/SWUNG GEAR. 2 L 7 2 4T RT A24CE 2003022000121 20030220 00121 NE 2003 2 20 AMWA044664 2 20021101 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT FAILED A AMWA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 CE 07 143YV 8604 8604 UE143 114269 THE CREW OF FLIGHT 2500, ABORTED A TAKEOFF AT THE BEGINNING OF THE ROLL WHEN A LOUD BANG WAS HEARD. THE NOISE HAD CAME FROM THE LEFT ENGINE. THE CREW NEVER REACHED TAKEOFF POWER. THE LEFT ENGINE KEPT RUNNING FOR APPROXIMATELY 2-3 MINUTES AFTER THE OCCURRENCE. THE TAKEOFF WAS ABORTED WITHIN 100 FT OF START WITH APPROXIMATELY 1500 LBS OF TORQUE. THE AIRCR AFT TAXIED OFF THE RUNWAY TO THE GATE WITH IDLE POWER. THERE WAS A TIRE-LIKE ODOR THAT WAS SMELLED. THE CREW THOUGHT I T WAS A BLOWN TIRE. REMOVED AND REPLACED THE ENGINE/POWER SECTION ASSEMBLY. VENDOR REPLACED THE PT STATOR DISKS 1ST AN D 2ND STAGE. THERE FORE THE UNIT HAS BEEN PROCESSED IN ACCORDANCE WITH THE PWA SPECIFICATION F67D021, PT6A67D OVERHAUL M 2 L 7 2 4T 4 T RT A24CE E26NE 2002111200107 20021112 00107 NM 2002 11 12 SWAA022549 1 20021024 A 3211 6561740 TRUNNION BOEING 737 7373H4 1384600 NM LT & RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED SERVICE CHECK, SWA SI 11251-32, BOTH RT AND LT MLG FAILED TRUNNION PIN INSPECTION. REMOVED AND REPLACE D BOTH MLG PER MM. 2 L 7 2 4F RT A16WE 2002111200108 20021112 00108 2002 11 12 SWAA022550 4 20021026 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED RON, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PE R MM. 2 L 7 2 4F RT A16WE 2002111200109 20021112 00109 2002 11 12 SWAA022551 4 20021028 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002111200110 20021112 00110 NM 2002 11 12 SWAA022554 1 20021028 A 5230 AND10141 TEE FITTING BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR LOWER LONGITUDINAL T-CHORD CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 2002111200111 20021112 00111 EA 2002 11 12 02313670 1 20021109 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 670BR 7561 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE NR 3 CEILING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL INITIALLY DEFERRED REPAIR OF THIS DISCREPANCY IAW THE MEL. LATER THE LAMP WAS REMOVED AND REPLACED IN THE NR 3 CEILING EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002111200112 20021112 00112 NM 2002 11 12 SWAA022555 1 20021025 A 5712 6545445 RIB BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED D CHECK, FOUND RT WING LOWER RIB CHORD CRACKED AT WS 135.5, BETWEEN STRS 2 AND 3. REPAIRED RIB CHORD P ER BFG ER. 2 L 7 2 4F RT A16WE 2002111200113 20021112 00113 NM 2002 11 12 SWAA022566 1 20021027 A 3350 PH22300L COVER BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 EEPLS TRACK COVER PEELED OFF AT ROWS 21 AND 22. 2 L 7 2 4F RT A16WE 2002111200114 20021112 00114 2002 11 12 SWAA022567 4 20021029 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM CABIN DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDES PRESS IND OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2 L 7 2 4F RT A16WE 2002111200115 20021112 00115 NM 2002 11 12 SWAA022580 1 20021029 A 5230 AND10141 TEE FITTING BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED SPECIAL VISIT, FOUND AFT CARGO DOOR T-CHORD CRACKED AT AFT LOWER CORNER. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2002111200116 20021112 00116 EA 2002 11 12 02313650 1 20021109 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 650BR 7418 During overnight maintenance it was discovered that the aft aisle emergency exit light was inoperative. Maintenance per sonnel removed and replaced the lamp in the aft aisle emergency exit light. An operational check was satisfactory and t he aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002111200117 20021112 00117 NM 2002 11 12 SWAA022583 1 20021031 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 617SW 27700 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002111200118 20021112 00118 2002 11 12 SWAA022588 4 20021031 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002111200119 20021112 00119 2002 11 12 SWAA022589 4 20021031 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002111200120 20021112 00120 2002 11 12 SWAA022591 4 20021101 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002111200121 20021112 00121 NM 2002 11 12 SWAA022593 1 20021101 A 5523 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 713SW 27847 DURING SCHEDULED C4 CHECK, FOUND BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT AND RT TA B HARDWARE AND BUSHINGS ON NR 1 HINGE ATTACH POINTS. 2 L 7 2 4F RT A16WE 2002111200122 20021112 00122 NM 2002 11 12 SWAA022599 1 20021102 A 2120 3964401 VALVE BOEING 737 7373H4 1384600 NM A/C BAY MALFUNCTIONED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 332SW 23696 DURING FLIGHT SMELLED ELECTRICAL SMELL IN COCKPIT AND CABIN. FOUND ODOR ASSOCIATED WITH RT PACK WHEN TEMP SELECTED IN F ULL HOT. REMOVED AND REPLACED RT PACK VALVE PER MM. 2 L 7 2 4F RT A16WE 2002111200123 20021112 00123 2002 11 12 SWAA022616 4 20021104 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 791SW 27886 AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002111200124 20021112 00124 2002 11 12 SWAA022619 4 20021104 A 2565 D31354 SLIDE BOEING 737 7372K6 1364440 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 129SW 22340 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002111200125 20021112 00125 NM 2002 11 12 SWAA022621 1 20021105 A 5320 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (3 EA) AT STR 4L, BS 727B, 727C AND 727D. REMOVED AND REPLACED STR TIE CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002111200126 20021112 00126 NM 2002 11 12 SWAA022622 1 20021105 A 5320 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER TIE CL IP PER SRM. 2 L 7 2 4F RT A16WE 2002111200127 20021112 00127 NM 2002 11 12 SWAA022624 1 20021105 A 5320 6527314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIPS CRACKED (3 EA) AT STR 4L AT BS 597 AND BS 616, STR 4R AT BS 559. R EMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002111200128 20021112 00128 NM 2002 11 12 ASAA0210202 1 20021001 A 5210 507945178 DOOR BOEING 737 737210C 1384459 NM L1 STUCK A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 743AS 64830 8263 21821 ANC - FORWARD ENTRY L1 DOOR WOULD NOT OPEN FROM THE OUTSIDE. HEATED AND LUBED THE FORWARD ENTRY DOOR, THEN DOOR OPERATE D NORMAL. (M) 2 L 7 2 4F A16WE 2002111200129 20021112 00129 NM 2002 11 12 ASAA0210203 1 20021001 A 5320 654654777 ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND RIGHT MAIN LANDING GEAR BAY FAIRING SUPPORT ANGLE AT FUSELAGE BS 727, RBL 9, RBL 1 7 WITH WORN FASTENER HOLES. REMOVED AND REPLACED ANGLE PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200130 20021112 00130 NM 2002 11 12 ASAA0210204 1 20021001 A 5414 6573769 FAIRING BOEING 737 7372X6C 1384552 NM RT NACELLE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE OUTBOARD FIXED FAIRING AT NACELLE STATION 155, WING STATION 255R CHAFE D. REPAIRED FAIRING PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200131 20021112 00131 NM 2002 11 12 ASAA0210205 1 20021002 A 5310 6547955 SHEAR TIE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND STUB FRAME SHEAR TIE AT BODY STATION 787, STRINGER 26R CORRODED. FABRICATED, REMO VED AND REPLACED SHEAR TIE PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200132 20021112 00132 NM 2002 11 12 ASAA0210206 1 20021002 A 5311 6546534 FAILSAFE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME FAIL/SAFE CHORD AT BS 520, STRINGER 27L CORRODED. REPAIRED FRAME FAIL/SAFE CHORD PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200133 20021112 00133 NM 2002 11 12 ASAA0210207 1 20021002 A 5330 6573746 SKIN PANEL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 950, STRINGER 11R CRACKED. REPAIRED SKIN PANEL PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200134 20021112 00134 NM 2002 11 12 ASAA0210208 1 20021002 A 5320 65625073 FLOOR SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND LATERAL FLOOR SUPPORT AT BS 967-980, LBL 23, LBL 40 CORRODED. REMOVED AND REPLACE D FLOOR SUPPORT PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200135 20021112 00135 NM 2002 11 12 ASAA0210209 1 20021002 A 7110 657377322 RIB BOEING 737 7372X6C 1384552 NM NR 2 COWLING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE INBOARD COWL RIB UPPER MID SPLICE AT ENGINE STATION 136 GOUGED. REMOV ED AND REPLACED INBOARD COWL. (M) 2 L 7 2 4F RT A16WE 2002111200136 20021112 00136 NM 2002 11 12 ASAA0210210 1 20021003 A 5210 507945178 MECHANISM BOEING 737 737290C 138448V NM L1 DOOR LACK OF LUBE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 740AS 39876 5177 22578 ANC - FORWARD ENTRY DOOR (L1) DOOR DIFFICULT TO OPERATE. CLEANED AND LUBED THE FORWARD ENTRY, THEN DOOR OPERATED NORMAL . (M) 2 L 7 2 4F A16WE 2002111200137 20021112 00137 NM 2002 11 12 ASAA0210211 1 20021002 A 5753 6546431278 SKIN PANEL BOEING 737 7372X6C 1384552 NM T/E FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND FORE FLAP LOWER LEADING EDGE SKIN PANEL AT WING STATION 505R GOUGED. BLENDED AND INSTALLED REPAIR PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200138 20021112 00138 NM 2002 11 12 ASAA0210212 1 20021002 A 5330 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 1039, STRINGER 10R DENTED. REPAIRED SKIN PANEL PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200139 20021112 00139 NM 2002 11 12 ASAA0210213 1 20021003 A 5320 65621576 FITTING BOEING 737 7372X6C 1384552 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND 9-G FLOOR PAN FITTING AT BS 344-360, RBL 60, RBL 65 GOUGED. REMOVED AND REPLACED FITTING PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200140 20021112 00140 NM 2002 11 12 ASAA0210214 1 20021007 A 5314 6545866502 KEELBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM WEB AT BS 663-727, LBL 5 CRACKED. REMOVED AND REPLACED KEEL BEAM WEB PE R SRM. (M) 2 L 7 2 4F RT A16WE 2002111200141 20021112 00141 NM 2002 11 12 ASAA0210215 1 20021007 A 5313 6552918 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 20L AT BODY STATION 1040 DENTED. REPAIRED STRINGER PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200142 20021112 00142 NM 2002 11 12 ASAA0210216 1 20021007 A 5313 BAC1498157 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 18L AT BODY STATION 1040 CRACKED. REPAIRED STRINGER PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200143 20021112 00143 NM 2002 11 12 ASAA0210217 1 20021007 A 5210 DOOR FRAME BOEING 737 7372X6C 1384552 NM L1 DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND L1 DOOR FRAME AT BS 320 LBL 65 GOUGED. REPAIRED DOOR FRAME PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200144 20021112 00144 NM 2002 11 12 ASAA0210218 1 20021007 A 5313 6545800204 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 26R AT BODY STATION 337-357 CORRODED. REMOVED CORRODED SECTION, FABRICAT ED AND REPAIRED STRINGER PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200145 20021112 00145 NM 2002 11 12 ASAA0210219 1 20021007 A 5312 655163976 PRESSURE PANEL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND RIGHT MAIN WHEEL WELL WEB AT BODY STATION 706-721, RBL 20, RBL 34 CRACKED. REMOVE D AND REPLACED WEB PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200146 20021112 00146 NM 2002 11 12 ASAA0210245 1 20021015 A 5310 6546595532 SHEAR TIE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 727A, STRINGER 27R CORRODED. REMOVED CORRODED, FABRICATED AND INS TALLED REPAIR PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200147 20021112 00147 NM 2002 11 12 ASAA0210246 1 20021015 A 5314 6573746 KEELBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM FLANGE AT BS 727-735, LBL 7 CRACKED. REMOVED DAMAGE, FABRICATED AND INS TALLED REPAIR PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111200148 20021112 00148 WP 2002 11 12 ASAA02803340 1 20021002 A 5230 4920233U503 STOP FITTING DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K-CHECK FORWARD SIDE BOTTOM DOOR STOP FITTING CRACKED. REPLACED FITTING PER SRM 51-10-4, 51-30-1 A ND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002111200149 20021112 00149 WP 2002 11 12 ASAA02803341 1 20021002 A 5230 4920233U503 STOP FITTING DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING C-CHECK, FORWARD CARGO BAY DOOR FORWARD SIDE BOTTOM DOOR STOP 3RD FROM TOP, FITTING CRACKED. REPLACE D FITTING PER SRM 51-10-4, 51-30-1, AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002111200150 20021112 00150 WP 2002 11 12 ASAA02803342 1 20021002 A 5230 4920233U503 STOP FITTING DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING 30K-CHECK, FOUND FORWARD CARGO BAY DOOR FORWARD SIDE TOP DOOR STOP FITTING CRACKED. REPLACED FITTING PER S RM 51-10-4, 51-30-1 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002111200151 20021112 00151 WP 2002 11 12 ASAA02803343 1 20021002 A 5320 993653443 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING 30K-CHECK, FOUND MAIN CABIN FLOOR SUPPORT CORRODED BEYOND LIMITS AT STATION 180, LBL 25-38. FABRICATED AND INSTALLED REPLACEMENT SUPPORT PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002111200152 20021112 00152 NM 2002 11 12 VNAA0210029 1 20021030 A 5270 PROXIMITY SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EMERGENCY DOOR DIRTY A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 441JS 3059 EN ROUTE TO EVV AT 18,000 FEET, THE CREW RECEIVED A DOORS INDICATION ON THE RED WARNING PANEL AND DESCENDED TO 10,000 FE ET AND THE LIGHT EXTINGUISHED. FLIGHT 4029 LANDED AT EVV WITH NO FURTHER INCIDENTS. OUTSTATION MAINTENANCE INSPECTED A ND FOUND GREASE TO BE ON THE 9A EMERGENCY DOOR PROXY SENSOR. OUTSTATION MAINTENANCE CLEANED THE PROXY SENSOR IN ACCORD ANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERV ICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002112100148 20021121 00148 NM 2002 11 21 UPS02639892 1 20021107 A 5610 SLIDING WINDOW BOEING 767 767300 1385204 NM COCKPIT CRACKED A IPXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 311UP 27741 INSPECTION TYPE:N/A O2R WINDOW HAS CRACK AND IS ARCING, PER QRH WINDOW HEAT TURNED OFF. REPLACED O2R WINDOW PER MM 56-1 1-01-4. 2 L 7 2 4F RT A1NM 2002111200153 20021112 00153 NM 2002 11 12 QXEA0201892 1 20021107 A 5270 HANDLE BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 OPEN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 410QX 4053 SEA-ON CLIMBOUT FROM SEA, FUSELAGE DOORS WARNING LIGHT ILLUMINATED, AFT BAGGAGE DOOR SHOWED UNSAFE. FOUND AFT BAGGAGE DO OR HANDLE POPPED OUT. INSPECTED DOOR HANDLE, NO DEFECTS NOTED. RESECURED DOOR HANDLE. DOOR WARNING CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002111200154 20021112 00154 NM 2002 11 12 02FDEA00724 1 20021012 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 272FE 22037 CORROSION ON SKIN LAP AT SHEAR TIE AT BS 720B, STR 26R. R&R SKIN PER SRM 53-10-5, 51-30-2, 51-30-5. 2 L 7 3 4F RT A3WE 2002111200155 20021112 00155 NM 2002 11 12 02FDEA00725 1 20021012 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 272FE 22037 DENT IN STR FLANGE AT BS 492, STR 23L. R&R STR FLANGE PER SRM 53-10-1, 53-10-3. 2 L 7 3 4F RT A3WE 2002111200156 20021112 00156 EA 2002 11 12 COMA0260636 1 20021110 A 4990 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 806CA 7359 FLIGHT 5664 APU LOW OIL PRESSURE WARNING.APU OVER SERVICED - REMOVED 1 QUART OF OIL. 2 L 7 2 4F RT A21EA 2002111200157 20021112 00157 NM 2002 11 12 02FDEA00726 1 20021008 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 272FE 22037 CORROSION ON SEAT TRACK I/B FLANGE UPR SURFACE AROUND NUTPLATE HOLES AT BS 760-848, LBL 24, WL 208. R&R SEAT TRACK PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002111200158 20021112 00158 NM 2002 11 12 HNAA0200076 1 20021107 A 2611 PU90461S SMOKE DETECTOR DHAV DHC8 DHC8201 2809001 NM LAVATORY DEFECTIVE A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 983HA 8877 8877 478 LAV SMOKE DETECTOR GOES OFF CONTINUOULSY IN FLIGHT. REPLACED LAVE SMOKE DETECTOR, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2002111200159 20021112 00159 EA 2002 11 12 COMA0260638 1 20021108 A 5240 SERVICE DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING O W OTHER INADEQUATE Q C CL CLIMB 1 SO 01 472CA 7667 FLIGHT #5983 LOUD WIND NOISE FROM R/H SIDE OF AIRCRAFT.FOUND EXT POWER SERVICE DOOR LEFT OPEN. SECURED DOOR. 2 L 7 2 4F RT A21EA 2002111200160 20021112 00160 EA 2002 11 12 COMA0260639 1 20021109 A 2750 8575D100401 SHAFT CNDAIR CL600 CL6002B19 1900309 EA R/H #4 BROKEN A COMA O OTHER S AFFECT SYSTEMS DE DESCENT 1 SO 01 976CA 7151 FLIGHT 6011 FLAPS FAILED AT 0 DEGREES.REPLACED THE R/H #4 FLAP FLEX DRIVE. 2 L 7 2 4F RT A21EA 2002111200161 20021112 00161 EA 2002 11 12 COMA0260640 1 20021110 A 3350 59465 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR BROKEN A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 937CA 7044 FLIGHT 5751 SEVERAL EMERGENCY LIGHTS ARE INOP.REPLACED THE FLOOR LIGHTS CONNECTOR AT ROW 5. 2 L 7 2 4F RT A21EA 2002111200162 20021112 00162 EA 2002 11 12 COMA0260641 1 20021110 A 4990 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 806CA 7359 FLIGHT 5663 APU LOW OIL PRESSURE WARNING.SERVICED APU WITH 2 QTS OF OIL. 2 L 7 2 4F RT A21EA 2002111200163 20021112 00163 EA 2002 11 12 COMA0260642 1 20021111 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 989CA 7215 FLIGHT 5784 FLAPS FAILED AT 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002111200164 20021112 00164 NM 2002 11 12 AWXA200201105 1 20021111 A 3350 BMS13311122 WIRE BOEING 757 7572S7 1384962 NM SEAT ROW 6 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 0 0 23321 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH ISLE LIGHT AT SEAT ROW 6 L/H WAS FOUND INOPERATIVE. MAINTENANCE DISCOVERED A BROKEN WIRE ON THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 6 L/H, SPLICED WIRE, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002111200165 20021112 00165 EU 2002 11 12 MALA020646 1 20021106 A 5320 7383720210 SEAT TRACK SAAB SF340 340B 7860101 EU A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 414XJ 340B414 DURING A-11 INSPECTION IN CWA, MAINTENANCE FOUND FWD PORTION OF AISLE SEAT TRACK LBL 18.3 HAS CORROSION. MAINTENANCE RE MOVED AND REPLACED FWD SECTION OF AILSE SEAT TRACK LBL18.3 IAW EO #53060, REMOVED AND INSTALLED NEW FWD CLIP FWD SECTION LH SEAT TRACK LBL 18.3 IAW SRM 51 PN 7383720-210, SEE 409 #177931 FOR ALODINE, PRIME AND PAINTING 2 L 7 2 4T RT A52EU 2002111300001 20021113 00001 SO 2002 11 13 C2XA02SH125 1 20021112 A 5300 14520554003 SKIN EMB 145 EMB145LR 3260212 SO DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13914 145430 SHV-DURING C CHECK TWO DENTS WHERE FOUND AFT OF PAX DOOR BETWEEN FRAMES 20 AND 21 AT STRINGERS 13L AND 14L. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB SRM 53-21-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002111300002 20021113 00002 CE 2002 11 13 CA020927002 1 20020924 A 3020 9091009913 TUBE BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA HARTZL HCB3T HCB3TN3 GL INTAKE ANTI ICE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ENGINE ANTI-ICE INTAKE TUBES REPLACED AS PER BEECH SB 71-3142, WERE FOUND CRACKED AT FIRST INSPECTION AFTER SB COM PLIANCE. 1 L 7 2 3T 4 T RT 3A20 E4EA 6 C P15EA 2002111300003 20021113 00003 EA 2002 11 13 CA021011002 2 20020926 A 7200 ENGINE DHAV DHC6 DHC6200 2802620 EA PWA PT6 PT6A20 52043 EA NACELLE OVERTORQUED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) AIRCRAFT HIT LARGE WAVE SWELL AND CREW INADVERTENTLY ALLOWED POWER LEVER TO ADVANCE FORWARD TO OVER TORQUE ENGINE . POWER SECTION WAS REPLACED. 1 H 7 2 3T 3 T RT A9EA E4EA 2002111300004 20021113 00004 NM 2002 11 13 CA021015006 1 20021011 A 5330 SKIN BOEING 737 7372Q9 138448M NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 56484 54099 (CAN) CRACK FOUND ON OUTER FUSELAGE SKIN BETWEEN STA 747 & STA 767 AT STRINGER 18 LT. REPAIR CARRIED OUT PER SRM 53-30-3 FIG.6 SHEET 4. 2 L 7 2 4F 4 F A16WE E2EA 2002111300005 20021113 00005 NM 2002 11 13 CA021015007 1 20021011 A 5330 SKIN BOEING 737 7372Q9 138448M NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 56484 54099 (CAN) CRACK FOUND ON OUTER FUSELAGE SKIN BETWEEN STATION 727A & 727B AT STRINGER 18 LT. REPAIR CARRIED OUT PER SRM 53-30 -3 FIG 48. 2 L 7 2 4F 4 F A16WE E2EA 2002111300006 20021113 00006 CE 2002 11 13 CA021018001 1 20021015 A 1430 AN470B RIVET BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A42 52043 NE HARTZL HCD4N3 HCD4N3A GL FUSELAGE CORRODED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 12094 (CAN) DURING UNSCHEDULED MAINTENANCE, RIVET HEADS WERE FOUND SITTING ON THE FRAME BELOW THE WINDOW, AFTER FURTHER INVES TIGATION FOUND THAT THE RIVET HEADS CAME FROM THE SPLICE IN THE CHANNEL AT STA 193.00. RIVET HEADS WERE CORRODED AND SE PARATED WITH HALF OF THE HEAD STILL WITH THE REST OF THE RIVET, FOUND RIVETS IN THE SAME CONDITION IN THE SPLICE ON THE OTHER SIDE OF THE AIRCRAFT. THE SEPARATED RIVETS ARE AB RIVETS 5056T AND THE OTHER RIVETS IN THE SPLICE ARE AD RIVETS 2 117T. HAVE COMMUNICATED WITH MANUFACTURE TO FIND OUT IF THERE IS A REASON FOR THE B RIVET TO BE MIXED IN WITH THE AD RIV ETS AND WHICH RIVETS SHOULD BE IN THAT SPLICE. 1 L 7 2 4T 4 T A24CE E4EA 5 C STC 2002111300007 20021113 00007 CE 2002 11 13 CA021018003 1 20021015 A 5610 5042006933 WINDSHIELD BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL COCKPIT CRACKED W B A EMER. DESCENT UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) AIRCRAFT WAS APPROACHING CRUISING ALTITUDE OF 190 WHEN THE FLIGHT CREW HEARD A CRACK SIMILAR TO ICE SHEDDING FORM THE PROPS. THEY NOTED AT THIS TIME THAT THE CAPTAINS WINDSCREEN HAD SEVERAL CRACKS RUNNING ACROSS IT. THERE WAS NEVER AN Y LOSS OF PRESSURIZATION. AT THIS TIME THEY DECLARED AN EMERGENCY, AND INITIATED AN EMERGENCY DECENT AT A REDUCED SPEED. AIRCRAFT RETURNED TO BASE AND SUBSEQUENT LANDING WERE UNEVENTFUL. ONCE SAFELY ON THE GROUND IT WAS NOTED THAT THE CAPTA INS OUTER PLY OF THE WINDSCREEN HAD FRACTURED. MAINTENANCE REPLACED THE WINDOW. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 2002111300008 20021113 00008 NM 2002 11 13 CA021018004 1 20021017 A 5330 SKIN BOEING 737 737296 1384486 NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 54205 (CAN) TWO INCH CRACK FOUND ON FUSELAGE SKIN ABOVE STRINGER 16 LT, AT BODY STATION 787. CRACK REPAIR CARRIED OUT IAW SRM 53-30-3. 2 L 7 2 4F 4 F RT A16WE E2EA 2002111300009 20021113 00009 NM 2002 11 13 CA021021001 1 20021021 A 3897 RIBBON HEATER BOEING 767 7673Y0 NM PWA 4060 PW4060 52119 NE WATER FILL LINE FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) MAINTENANCE NOTICED A BURNING ODOR IN AFT CARGO BAY WHILE PREFORMING A WINTERIZATION PROGRAM AND 'A' CHECK AFT CAR GO WATER FILL LINE RIBBON HEATER FOUND DAMAGED BURNED NO FLAMES OR SMOKE REPORTED AND DAMAGE CONTAINED BY INSULATION COV ERING HEATER RIBBON. NO LITTER WAS FOUND IN VICINITY OF THE DAMAGE. NOTE: THIS IS SAME AIRCRAFT INVOLVED IN SIMILAR IN CIDENT THIS YEAR, AIRCRAFT IS PRESENTLY BEING FLOWN TO MONTREAL MAINTENANCE BASE FOR INVESTIGATION AND REPAIRS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002111300010 20021113 00010 EU 2002 11 13 CA021021007 1 20021018 A 3040 COMPUTER AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE WINDOW HEAT ARCED W K NONE H B ELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) WINDOW CRACKED, HEAT CIRCUIT BREAKER PULLED, WINDOW CHANGED, SUSPECT HEAT CONTROL COMPUTER WINDOW CHANGED AND COMP UTER. ARCING OCCURED FIRST THEN CIRCUIT BREAKER PULLED, THAT'S WHEN THE WINDOW CRACKED 2 L 7 2 4F 4 F RT A28NM E29NE 2002111300011 20021113 00011 CE 2002 11 13 CA021022003 1 20021011 A 3020 9091009913 TUBE BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA INTAKE ANTI-ICE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ENGINE INLET ANTI-ICE TUBES REPLACED AS PER BEECH SB 71-3142. NEW TUBES FOUND CRACKED AT FIRST INSPECTION AFTER SB COMPLIANCE. 1 L 7 2 3T 4 T RT 3A20 E4EA 2002111300012 20021113 00012 NE 2002 11 13 CA021022006 2 20021018 A 8530 70472 TUBE DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE CYLINDER INTAKE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FIVE INTAKE TUBES WERE FOUND TO BE CRACKED AROUND THE FLANGE BASE. THIS CAUSED NO OBVIOUS PROBLEMS TO THE AIRCRAFT . HOWEVER, AT SCHEDULED INSPECTION THE AMO NOTICED FUEL STAINING AT THE AFFECTED AREA AND UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT 5 OF THE 9 INTAKE TUBES WERE CRACKED. THE ENGINE HAD ONLY 364.2 HOURS SINCE OVERHAUL AND HAS ONLY BE EN IN SERVICE SINCE JUNE 2002 1 H 7 1 3R 3 R A806 5E1 2002111300013 20021113 00013 NM 2002 11 13 CA021023001 1 20021019 A 2612 894093 FIRE LOOP BOEING 737 737268 138448Q NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE FAILED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) FLIGHT CREW REPORTED ON CLIMB OUT, FIRE WARNING BELL ACTIVATED AND NR 2 ENGINE FIRE HANDLE ILLUMINATED. EMERGENCY WAS DECLEARED - ENGINE FIRE BOTTLES BLOWN AND RETURN TO YYC REQUESTED. VISUAL INSPECTION OF ENGINE FOR SMOKE/FIRE BY FLI GHT ATTENENT RESULTED IN NO FAULTS FOUND. AIRCRAFT RETURNED FOR ABNORMAL LANDING WITH EMERGENCY VEHICLES ON STANDBY. NO ABNORMALITIES TO REPORT - AIRCRAFT TAXIED TO THE GATE. MAINTENANCE INSPECTION REVEALED NR 2 ENGINE LOWER FIRE LOOP - HAR D FAULTED CORE TO SHELL SHORTED. FIRELOOP REPLACED PER MM 26-11-11, BOTH AFT/FWD ENGINE FIRE BOTTLES/SQUIBS REP LACED - SYSTEM TESTED SERVICEABLE PER MM 26-21-11.AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO REPORT. 2 L 7 2 4F 4 F A16WE E2EA 2002111300014 20021113 00014 NM 2002 11 13 CA021023004 1 20021016 A 5753 85731170 SKIN BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA TE FLAP DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE AIRCREW WAS DOING PRE-FLIGHT WALK AROUND PRIOR TO THE FIRST FLIGHT OF THE DAY. NOTICED DAMAGE TO THE LT OUTBO ARD LOWER WING SHROUD. A PORTION HAD FOLDED BACK AND METAL WAS TORN. RD 8/4-57-98 ISSUED, REPAIR CARRIED OUT. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002111300015 20021113 00015 EA 2002 11 13 CA021023006 1 20021018 A 2910 82920010177 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) CREW ADVISED THAT NR 2 HYD QUANITY AT MIN DISPATCH AND PARK BRAKE PRESSURE AT 1500 PSI. TUBE ASSY-STANDBY BRAKE PR ESSURE NR 2 SYSTEM IN RT ARMPIT FOUND LEAKING. TUBE ASSY REPLACED. IPC REF 32-44-00 FIG.5 ITEM 20 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002111300016 20021113 00016 SO 2002 11 13 CA021024001 1 20021021 A 3260 472740 SOCKET PIPER PA31T PA31T2 7103127 SO PWA PT6 PT6A135 52043 NE INDICATOR LIGHT LOOSE W L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CA (CAN) ON FINAL APPROACH, THE CREW NOTICED AN UNSAFE LANDING GEAR INDICATION. THE CREW IMMEDIATELY INITIATED A MISSED AP PROACH. THE APPROPRIATE EMERGENCY CHECKLISTS WERE PERFORMED AND WHILE LOOKING FOR THE PROBLEM, THE CREW NOTICED THAT TH E EMERGENCY GEAR SOCKET WAS LOOSE. THE SOCKET WAS TIGHTENED AND A SAFE LANDING GEAR INDICATION WAS RECEIVED. THE AIRCRA FT LANDED WITH NO FURTHER INCIDENT. 1 L 7 2 3T 4 T RT A8EA E4EA 2002111300017 20021113 00017 NE 2002 11 13 CA021024002 2 20021002 A 7421 9550175400 IGNITER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) ROUTINE INSPECTION OF ENGINE REVEALED A LOOSE CENTER ELECTRODE (ABLE TO MOVE WITH FINGERNAIL). ALSO, INSULATOR RO TATED AROUND INSIDE IGNITER TIP HOUSING. IGNITER DID FUNCTION, HOWEVER POSSIBILITY OF CATASTROPHIC ENGINE DAMAGE EXISTE D. PART HAS BEEN REPLACED UPON THE DISCOVERY. 1 G 7 1 3U 3 U H9EU E19EU 2002111300018 20021113 00018 NM 2002 11 13 CA021024003 1 20021010 A 2497 82450016 WIRE DHAV DHC8 DHC8201 2809001 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE NR 2 AC GEN SHORTED W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA (CAN) AN AIR-RETURN TO BASE DUE TO NR 2 AC GENERATOR DROPPING OFF LINE WITH RELATED CAUTION LIGHTS ILLUMINATING. INVESTI GATED THIS DEFECT AND REPORT THAT THE FAULT WAS TRACED TO A SHORTED WIRE IN THE VICINITY OF CB9 LOCATED INSIDE THE LT AC CONTACTOR BOX. THE WIRING WAS REPAIRED, AND AC GENERATION SYSTEM TESTED IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MA NUAL. OPERATOR ADVISED OF THE RELEASE OF DASH 8 SB 8-24-76 WITH A RECOMMENDATION FOR INCORPORATION. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002111300019 20021113 00019 NE 2002 11 13 CA021024004 1 20021023 A 7603 7630101910117 THROTTLE CABLE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 1 ENGINE BROKEN W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) AFTER SEVERAL UNSUCCESSFUL ATTEMPTS BY THE PILOT TO START NR 1 ENGINE, MAINTENANCE PERSONNEL DISCOVERED THAT THE THROTTLE CABLE WAS BROKEN APPROX. 12 INCHES FROM THE FUEL CONTROL UNIT ATTACHMENT. CABLE HAS BEEN REPLACED AND A/C RETU RNED TO SERVICE. A/C TOTAL TIME = 9427.5 HRS.CABLE TSN UNKNOWN. 1 G 7 2 3U 3 U H1NE E1GL 2002111300020 20021113 00020 NM 2002 11 13 CA021024005 1 20020901 A 3097 697070212 BUSS TIE BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA ROTOL R408 CR4086123F17 EU PROP DE-ICE SHORTED W E ENGINE SHUTDOWN E VIBRATION/BUFFET DE DESCENT 1 CA (CAN) AIRCRAFT EXPERIENCED PROP OVERSPEED 1060 RPM, NR 1 PEC CAUTION LIGHT AND POWERPLANT MESSAGE. POWER LEVER RETARDED TOWARDS FLIGHT IDLE, NO EFFECT. ACC. QRH ENGINE FAIL / FIRE / SHUTDOWN COMPLETED ON LT (NR 1) ENGINE. MTCE CHECKED FAU LT CODES IN CDS, FC 160-LOCAL NP MPU EXTRA PULSES, FC 999-NO DISPATCH -FC IN PEC. FSR OPENED LT HORSE COLLAR TO INSPEC T DE-ICING BUSS TIES, FOUND ONE BUSS TIE SHEARED OFF BY CONTACT WITH MPU HOUSING AND EVIDENCE OF HEAT DAMAGE TO BUSS TIE AND PROPELLER BULKHEAD ( 30 MM), SHORTING WITH PROP DE-ICE ON. OPERATOR IS AWARE OF DH8-400-SL-61-002 AND DOWTY SL FOR FC 160. REPAIR TO PROPELLER BACKPLATE / BULKHEAD PERFORMED AS PER DOWTY CONCESSION LETTER. 2 H 7 2 4T 4 T RT A13NM E00062EN 6 C P17BO 2002111300021 20021113 00021 WP 2002 11 13 CA021025001 1 20020828 A 5610 369H202472 WINDOW HUGHES 369 369E 4470707 WP ALLSN 250C 250C20B 03013 GL CREW DOOR SEPARATED W A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 CA (CAN) DURING CRUISE FLIGHT PILOT HEARD A POPPING SOUND WHICH HE THOUGHT WAS THE RT FORWARD DOOR OPENING. HE GLANCED OVER AND SAW FRAGMENTS OF PLASTIC ON THE SEAT BESIDE HIM. THE COMPLETE WINDOW HAD DEPARTED AND LEFT JUST THE VERY EDGE OF TH E MATERIAL WHICH IS RIVETED TO THE DOOR FRAME. THERE WAS NO INDICATION OF A PROBLEM WITH THE CONTROL OF THE HELICOPTER O R THAT THERE HAD BEEN AN IMPACT WITH PLASTIC DEBRIS. THE PILOT LANDED AS SOON AS PRACTICAL TO EXAMINE THE HELICO PTER AN D REPORT HIS PROBLEM. THE PLASTIC HAD SEVERELY DAMAGED THE VERTICAL STABILIZER WHICH REQUIRED IT TO BE REPLACED PRIOR TO FURTHER FLIGHT. NO OTHER DAMAGE WAS FOUND 1 G 7 1 3U 3 U H3WE E4CE 2002111300022 20021113 00022 CE 2002 11 13 CA021025007 1 20021022 A 5522 115610010125 SKIN BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 15703 (CAN) DURING INSPECTION, THE TRAILING EDGE SPLINE ON THE ELEVATORS WAS FOUND CRACKED AT SEVERAL LOCATIONS, THE ELEVATOR WAS REPLACED. THE REMOVED ELEVATOR WAS SENT TO OUR SHEET METAL SHOP FOR REPAIR, AFTER DISASSEMBLY THEY REPORTED THAT M OST OF THE CRACKS EXTENDED FROM THE RIVET HOLES TO THE TRAILING EDGE OF THE SPLINE, A FEW CRACKS EXTENDED FROM THE RIVET HOLES TO THE LEADING EDGE AND ONE CRACK EXTENDED THOUGH THE ENTIRE SPLINE. APPROXIMATELY 95 PERCENT OF THE HOLES WERE CRACKED. 1 L 7 2 3T 4 T A14CE E4EA 2002111300023 20021113 00023 NE 2002 11 13 CA021028003 2 20021024 A 7310 0164248850 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) FUEL LEAKING FROM OVERBOARD DRAIN WHEN BOOST PUMP TURNED ON TO DRAIN FUEL FILTERS. 1 G 7 1 3U 3 U H9EU E19EU 2002111300024 20021113 00024 NM 2002 11 13 CA021028005 1 20021017 A 7120 MOUNT AIRBUS A319 A319114 3930350 NM CFMINT CFM56 CFM565A1 NE ENGINE WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOUND BALL BEARING WORN AND MOUNT GOUGED AT C CHECK, BEARING REPLACED AND BLEND DONE. TOTAL AIRCRAFT TIME 13,073 H RS6,295CYCLES 2 L 7 2 4F 4 F RT A28NM E29NE 2002111300025 20021113 00025 NM 2002 11 13 CA021028006 1 20020917 A 7120 655790418 LINK BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE RT TRUNNION CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16424 (CAN) DURING AN INSPECTION (AD 2001-20-09), THE RT TRUNNION LINK BUSHING WAS FOUND LOOSE. UPON REMOVAL OF THE TRUNNION L INK ASSYEMBLY, IT WAS NOTED THAT THE FORWARD BEARING END (RACE) HAD AN APPROXIMATLEY 2 INCH CRACK ALONG IT'S VERTICAL A XIS. NOTE: TSN IS UNKNOWN. 2 L 7 3 4F 4 F A3WE E2EA 2002111300026 20021113 00026 SO 2002 11 13 MASA200200003 1 20020926 A 2560 FIRST AID KIT EMB 145 EMB145LR 3260212 SO A MASA O OTHER O OTHER IN INSP/MAINT 1 SW 07 851MJ 145572 FIRST AID KIT OPENED AND BANDAID USED. REPLACED FIRST AID KIT. 2 L 7 2 4T RT T00011AT 2002111300027 20021113 00027 NM 2002 11 13 MASA200200012 1 20021004 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM A MASA O OTHER O OTHER IN INSP/MAINT 1 SW 07 449YV 449 DURING LINE CHECK INSPECTION, THE #2 CABIN EMERGENCY LIGHT WOULD NOT ILLUMINATE. THE #2 EMERGENCY LIGHT POWER SUPPLY WAS REPLACED WITH NO FURTHER DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2002111300028 20021113 00028 EA 2002 11 13 MASA200200007 1 20021001 A 3210 GOODYEARAERO CNDAIR CL600 CL6002B19 1900309 EA A MASA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 07 37228 21972211 7228 ABOVE LISTED AIRCRAFT WAS DAMAGED DUE TO TIRE SEPARATION DURING TAKEOFF. UPON FURTHER REVIEW, MESA AIRLINES INC. CAS DEP ARTMENT FOUND GOODYEAR AERO TIRES P/N 5010571-1 S/N'S 2197XXX - 2211XXX TO HAVE MANUFACTURING DEFECTS. TIRE S/N'S AFFECT ED ARE 2197XXX-2211XXX. 2 L 7 2 4F RT A21EA 2002111300029 20021113 00029 GL 2002 11 13 CA021029001 2 20021017 A 7250 STATOR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE DEBONDED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 12683 (CAN) NR 2 ENGINE CHIP LIGHT CAME ON IN FLIGHT. FINE HAIR LIKE METAL FOUND ON FORWARD CHIP PLUG. TURBINE REMOVED AND SEN T TO SAL FOR TEAR DOWN AND INSPECTION. SILVER PLATING ON 3537 LAB STATOR FOUND DEBONDED CAUSING FINE SILVER SHAVING TO P EEL OFF. STATOR REPAIRED. TURBINE REINSTALLED AND RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2002111300030 20021113 00030 GL 2002 11 13 CA021029002 2 20020825 A 7261 369A8322 SEAL HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ENGINE OIL LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) ENGINE OIL WAS DETECTED COMING THROUGH THE UPPER AFT RT SIDE INTERIOR PANEL AND GRAVITY LEAKAGE DOWN TO THE AIRCRA FT FLOOR. THIS CONDITION ONLY EXSISTED UNDER STEEP RT TURNS OF THE HELICOPTER. AIRCRAFT RETURNED TO BASE AND UPON INVEST IGATION, IT WAS DETERMINED THAT THE RUBBER OIL SEAL FROM THE ENGINE OIL FILLER SUPPORT TO ENGINE OIL TANK, DEVELOPED A H OLE UNDER THE CLAMP AT THE TANK. OIL TANK IS LOCATED AT THE UPPER RT (AFT FACING FORWARD) OF THE MD 500D HELICOPTER. NEW SEAL WAS INSTALLED AND THE AIRCRAFT WAS GROUND RUN AND FLOWN WITH NO FURTHER LEAKAGE. 1 G 7 1 3U 3 U H3WE E4CE 2002111300031 20021113 00031 WP 2002 11 13 CA021029003 1 20020825 A 6520 CASE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL T/R GEARBOX DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 1958 (CAN) DURING A 600 HOUR INSPECTION OF AIRCRAFT, DAMAGE WAS FOUND ON THE UNDER SIDE OF THE T/R GEARBOX CASE. DUE TO A MIS -ALIGNMENT OF THE T/R PUSH PULL TUBE ADAPTER. DAMAGE WAS APPROX .020 DEEP & UPON INVESTIGATION IT WAS DETERMINED THAT PI N HAD EXCESSIVE WEAR AT THE ASSEMBLY POINT IN THE T/R GEARBOX HOUSING ITSELF. 1 G 7 1 3U 3 U H3WE E4CE 2002111300032 20021113 00032 NM 2002 11 13 CA021029004 1 20021024 A 3260 464505 DOWNLOCK SENSOR BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA RT MLG SHORTED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) DURING CRUISE AT FL 140 AT IAS 280 KT GREEN LT AND RED LT MAIN LANDING GEAR INDICATION ILLUMINATED WITH LIGHT IN T HE GEAR HANDLE. THE INDICATION WAS INTERMITTENT ON/OFF THREE TIMES. AFTER GEAR DOWN SELECTION AMBER LEFT DOOR AND RED L EFT MAIN LANDING GEAR INDICATION ILLUMINATED WITH LIGHT IN THE GEAR HANDLE. QRH APPLIED AND ALTERNATE GEAR DOWN INDICATI ON SHOWED THREE GREEN LIGHTS. ATC WAS REQUESTED TO PROVIDE STANDBY BACKUP UPON LANDING. PAX AND CABIN WERE UPDATED ON TH E LANDING SITUATION. INVESTIGATION / ACTION LT MLG NR 2 DOWNLOCK SENSOR HARNESS PINS FOUND CORRODED AT FIREWALL CONNECTO R P 24. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002111300033 20021113 00033 SW 2002 11 13 CA021029006 1 20021024 A 5532 410008513 SKIN GULSTM 690TP 690 0141720 SW GARRTT TPE331 TPE3315251K NM VERTICAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A 30 DAY INSPECTION IT WAS NOTED THAT THE VERTICAL STAB SKIN WAS CRACKED ON THE STARBOARD SIDE OF THE VERTI CAL STABILIZER. THE CRACK IS LOCATED AT APPROXIMATELY VS STA 9.1 AND IS 1 INCH IN LENGTH. THE CRACK IS RUNING FORE AND A FT. THE AIRCRAFT WILL BE RETURNED TO SERVICE UPON COMPLETION OF THE REPAIR. 1 H 7 2 3T 4 T 2A4 E2WE 2002111300034 20021113 00034 SW 2002 11 13 CA021029008 1 20020925 A 2720 CABLE BBAVIA 7 7ECA 21101NN SW LYC O235 O235C1 41505 EA RUDDER CONTROL MISINSTALLED W D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 CA (CAN) RT FORWARD RUDDER CABLE ATTACH MICO-SLEEVE FAILED DURING TAXI. ON AME INSPECTION MICO-SLEEVE FOUND TO NOT BE CRIMP ED DOWN TO PROPER DIMENSION. MICO-SLEEVE REPLACED AND CRIMPED PROPERLY. ALL MICO-SLEEVES ON AIRCRAFT CHECKED FOR PROPER CRIMP. LT FORWARD RUDDER CABLE ATTACH FOUND TO NOT BE CRIMPED TO PROPER DIMENSION. ALL OTHER MICO-SLEEVES ON AIRCRAFT PR OPER DIMENSION. FACTORY NOTIFIED AND THEY ARE SUBMITTING SDR AS WELL. 1 H 7 1 3O 3 O A759 E223 2002111300035 20021113 00035 EA 2002 11 13 CA021029009 2 20021026 A 7210 BEARING BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA REDUCTION G/B FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ROUTINE MAINTENANCE, VISUAL INSPECTION OF THE NR 1 ENGINE REDUCTION GEARBOX CHIP DETECTOR PLUG AND STRAINER WAS CARRIED OUT. FOUND NUMEROUS BALL BEARINGS APPROX.0.039 INCHES IN SIZE AND SOME PLASTIC & RUBBER DEBRIS CAUGHT IN TH E STRAINER. ENGINE MANUFACTURER AND PROPELLER OVERHAUL AGENCYS CONTACTED TO DETERMINE EFFECTED COMPONENT. PROPELLER GOVE RNOR (CSU) DETERMINED TO BE AT FAULT (POSSIBLE FLYWEIGH T PIVOT SHAFT BEARINGS). PROPELLER GOVERNOR (CSU) REPLACED AND S USPECT UNIT SENT FOR STRIP REPORT INSPECTION. ENGINE OIL SOAP ANALYSIS, OIL FILTER, OIL AND BOROSCOPE INSP. AND PERFORMA NCE INSPECTIONS CARRIED OUT. ENGINE OIL SYSTEM TO BE REINSPECTED IN NEAR FUTURE. STRIP REPORT RESULTS TO FOLLOW. 1 L 7 2 4T 4 T A24CE E4EA 2002111300036 20021113 00036 SW 2002 11 13 CA021029010 1 20021029 A 6711 1201105A14 SLEEVE BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE TAILBOOM MISMANUFACTURED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) FOUND IN MANUFACTURING, WEAR SLEEVES NOT BONDED PROPERLY TO T/R CONTROL TUBE ASSEMBLY. SUPPLIER DID NOT PERFOR MED THE SURFACE PREPARATION REQUIRED BEFORE BONDING THE WEAR SLEEVES TO THE CONTROL TUBE CAUSING LACK OF ADHESION. 1 G 7 2 3U 3 U RT H9SW E1GL 2002111300037 20021113 00037 NM 2002 11 13 CA021029013 1 20020819 A 3297 WIRE BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA DOWNLOCK SENSOR BROKEN W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) GEAR RETRACTION FAILURE WHEN SEL. GEAR UP NOSEGEAR NOT UP READ AND AMBER LIGHT ON . ACC.TO CHECKLIST SEL. GEAR DOW N, ALL GREEN LIGHTS ON.LANDING COMPLETED NORM LANDING. PASSENGER INFORMED AND BRIEFED. INVESTIGATION & ACTION DURING TROUBLESHOOTING, WIRE FOR NR 2 NOSE GEAR DOWNLOCK PROXIMITY SENSOR WAS FOUND BROKEN. PROXIMITY SENSOR HARNESS REPLACED. LANDING GEAR RETRACTION & EXTENSION TEST PERFORMED WITHOUT REMARKS 2 H 7 2 4T 4 T RT A13NM E00062EN 2002111300038 20021113 00038 NE 2002 11 13 CA021030002 2 20021021 A 7421 9550168760 IGNITER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) UPON INSPECTING THE IGNITER, IT WAS NOTED THAT THE CENTER ELECTRODE WAS MISSING. PORTION OF THE ACTUAL ELECTRODE EXPERIENCED A SEPARATION OF APPROX 6MM (1/4 INCH). THE DAMAGE CAUSED TO ENGINES HAS BEEN VARIABLE FROM ONE ENGINE TO ANO THER, BUT THERE HAS BEEN NO REPORT OF POWER LOSS OR REDUCTION IN ENGINE PERFORMANCE. IGNITERS PERIODIC INSPECTION REQUIR ES IN THE MAINTENANCE MANUAL EVERY 300 HOURS. 1 G 7 1 3U 3 U NC H9EU E19EU 2002111300039 20021113 00039 EU 2002 11 13 CA021030003 1 20021017 A 3251 100574006 ACTUATOR BRAERO 748 HS7482B 1500248 EU RROYCE DART DART5352 54509 NE ROTOL R4304 R2124304 EU NLG STEERING FAILED W D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 CA (CAN) NOSEWHEEL STEERING INTERMITTENTLY STIFF. NOSE WHEEL STEERING ACTUATOR WAS DISASSEMBLED. O-RING ON PISTON ROD WAS F OUND CUT, ALLOWING PRESSURE TO EQUALIZE ON EITHER SIDE OF THE RAM. BACKUP RINGS WHICH ARE INSTALLED ON EITHER SIDE OF TH E O-RING WERE MISSING, ALLOWING O-RING TO FLOAT, AND TWIST. ACTUATOR WAS REPLACED, REMOVED UNIT IS BEING SHIPPED BACK TO THE OVERHAUL FACILITY FOR REPAIR AND TEST. OVERHAUL SHOP HAS BEEN NOTIFIED OF THE DEFECT. 2 L 7 2 3T 4 T A24EU E297 6 C P899 2002111300040 20021113 00040 CE 2002 11 13 CA021030004 1 20021011 A 3020 9091009913 TUBE BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA INTAKE ANTI-ICE CRACKED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) ENGINE INLET ANTI-ICE TUBES REPLACED AS PER BEECH SB 71-3142. NEW TUBES FOUND CRACKED AT FIRST INSPECTION AFTER SB COMPLIANCE. 1 L 7 2 3T 4 T RT 3A20 E4EA 2002111300041 20021113 00041 NM 2002 11 13 CA021030007 1 20021025 A 2751 1812996 INDICATOR BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE TE FLAPS MALFUNCTIONED W L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CA (CAN) ON APPROACH, CREW SELECTED FLAPS AND EXTENDED NORMALLY TO FLAP 1 POSITION - FLAPS WOULD NOT EXTEND OR RETRACT FROM THAT POSITION. AIRCRAFT EXECUTED A MISSED APPROACH AND CONDUCTED THE 'TRAILING EDGE FLAP ASSEMETRY CHECKLIST'. CREW REQ UESTED FIRE TRUCKS BE ON STANDBY DUE TO HIGH SPEED LANDING - AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FLA P POSITION INDICATOR IN ACCORDANCE WITH MM 27-58-41. SYSTEM GROUND CHECKED SERVICEABLE WITH NO FAULTS FOUND. AIRCRAFT R ETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO REPORT. 2 L 7 2 4F 4 F A16WE E2EA 2002111300042 20021113 00042 GL 2002 11 13 CA021031003 2 20020924 A 7230 BEARING AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20F 03013 GL COMPRESSOR WORN W E A ENGINE SHUTDOWN UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 CA (CAN) AIRCRAFT IN CRUISE FLIGHT. PILOT NOTICED NG FLUCTUATION BETWEEN ENGINES, FOLLOWED BY ENGINE AT NR 2 CHIP LIGHT AND AN UNUSUAL NOISE & HOWL. PILOT SHUTDOWN NR 2 ENGINE AND MADE UNSCHEDULED LANDING AT NEARBY AIRPORT. NR 2 ENGINE COMPRES SOR SAGS FOUND WORN 2 1/2 BEARING IN GEARBOX. ALSO ENGINE COMPRESSOR SAGS FOUND WORN. NO PREVIOUS CHIP LITES REPORTED AN D SYSTEM CHECKED OK. AT PREVIOUS 100 HOUR INSPECTION (TIME SINCE INSPECTION 55 HOURS APPROXIMATELY). 1 G 7 2 3U 3 U H11EU E4CE 2002111300043 20021113 00043 NM 2002 11 13 CA021031008 1 20021028 A 2910 61146 LIMITER BOEING BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE HYD SYSTEM FAILED W O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA UK (CAN) AIRCRAFT EXPERIENCED A TOTAL LOSS OF SYSTEM 'A' HYDRAULICS AFTER SELECTING GEAR DOWN ON APPROACH. SYSTEM 'A' HYDRA ULIC QUANTITY INDICATED ZERO AND FLAPS STUCK AT POSITION '5'. CREW COMPLETED NON NORMAL CHECKLIST AND REQUESTED EMERGENC Y VEHICLES - AIRCRAFT LANDED WITHOUT INCIDENT AND TOWED TO THE GATE. MAINTENANCE INSPECTION REVEALED THE LEADING EDGE R ESTRICTOR FUSE (FLOW LIMITING VALVE) IN THE RT WHEEL WELL HAD ITS RESTRICTOR HOUSING CRACKED. MAINTENANCE REPLACED THE V ALVE, NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS AND ALL 'A' SYSTEM FILTERS. AIRCRAFT GROUND TESTED SERVICEABLE - NO FA ULTS OR LEAKS FOUND. AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO REPORT. 2 L 7 2 4F 4 F A16WE E2EA 2002111300044 20021113 00044 WP 2002 11 13 CA021031009 1 20021010 A 8097 CONNECTOR CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL STARTER FAILED W E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) CLIMBING OUT OF YUL LT ENGINE STARTER OVERSPEED LIGHT CAME ON. ENGINE SHUT DOWN AND RETURN TO YUL. AFTER INVESTIGA TION FOUND WIRE BROKEN IN CONNECTOR. CONNECTOR REPAIRED AND AIRCRAFT RETURNTO TO SERVICE. 2 L 7 2 4R 4 T 6A6 E282 2002111300045 20021113 00045 2002 11 13 CA021031011 4 20020730 A 3413 821020 INDICATOR HUGHES 269 269C1 8059504 SW LYC O360 HO360C1A 41514 EA VERTICAL SPEED FAILED W O OTHER N FALSE WARNING NR NOT REPORTED 1 CA (CAN) VERTICAL SPEED GIVING UNCLEAR READINGS. REPLACED VERTICAL SPEED INDICATOR. 1 G 7 1 3O 3 O O 4H12 E286 2002111300046 20021113 00046 EA 2002 11 13 CA021031012 2 20020906 A 7320 252434710 FUEL CONTROL SCWZER 269 269D 8059501 EA LYC O360 HIO360D1A 41514 EA ENGINE FAILED W O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA (CAN) FUEL INJECTOR WOULD NOT CUT OFF. ENGINE WOULD CONTINUE RUNNING. REPLACED FUEL CONTROL. 1 G 7 1 3U 3 O 0 4H12 1E10 2002111300047 20021113 00047 SW 2002 11 13 CA021031014 1 20020924 A 7603 M4414M BEARING PRECISION HA61060301 HUGHES 269 269C1 8059504 SW LYC O360 HO360C1A 41514 EA CARBUETOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 750048904 (CAN) BEARING ON CARBURETOR LOOSE IN THROTTLE. REPLACED BEARING. 1 G 7 1 3O 3 O O 4H12 E286 2002111300048 20021113 00048 EA 2002 11 13 CA021031015 2 20020911 A 7310 O-RING ROBSIN R44 R44 7640120 WP LYC O540 O540F1B5 41532 EA FUEL DRAIN LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) FUEL DRAIN VALVE LEAKING AT O-RING. REPLACED VALVE. 1 G 7 1 3O 3 O H11NM E295 2002111300049 20021113 00049 SW 2002 11 13 CA021031016 1 20020926 A 2434 LW10382 BRACKET HUGHES 269 269C1 8059504 SW LYC O360 HO360C1A 41514 EA ALTERNATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ALTERNATOR BRACKET BROKEN. REPLACED BRACKET. 1 G 7 1 3O 3 O O 4H12 E286 2002111300050 20021113 00050 CE 2002 11 13 CA021031019 1 20021031 A 5410 50980002160 SPLICE PLATE BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA RT NACELLE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 14574 14574 (CAN) THE RT NACELLE I/B SPLICE PLATE CRACKED DUE TO HOLE'S ON UPPER SPAR BEING ELONGATED, THUS CAUSING PLATE TO WORK IN THAT AREA. PARENT STRUCTURE FAILED DUE TO SPLICE PLATE BEING CRACKED AND NACELLE LOADING TRANSFURED TO THAT AREA. 1 L 7 2 3T 4 T A14CE E4EA 2002111300051 20021113 00051 CE 2002 11 13 CA021031020 1 20021030 A 3020 9091010017 TUBE BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA ANTI ICE SYSTEM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ANTI ICE FLEX TUBE FOUND CRACKED. 1 L 7 2 3T 4 T RT 3A20 E4EA 2002111300052 20021113 00052 NM 2002 11 13 CA021031021 1 20021013 A 2913 570717 SHAFT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 HYD PUMP SHEARED W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA 11872 11872 (CAN) NR 2 ENGINE DRIVEN HYDRAULIC PUMP FAILED AFTER START. SHAFT ASSY FOUND SHEARED. PUMP REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002111300053 20021113 00053 NE 2002 11 13 CA021101004 3 20021025 A 6114 57E03932 HUB BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE PROPELLER CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON NDT INSPECTION BEARING RETENTION AREAS UNSERVICEABLE DUE TO CORROSION. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002111300054 20021113 00054 SW 2002 11 13 CA021101008 1 20021022 A 6230 ASI6010454109 SLEEVE BELL 206010450113 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL SWASHPLATE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA JIJG0553 (CAN) CRACKS FOUND DURING OVERHAUL. THE CRACKS STARTED AT CORNER OF GLOVES. IT LOOKS LIKE THE PLATING (TUNGSTEN CARBIDE) STARTED TO LIFT UP. 1 G 7 1 3U 3 U H2SW E4CE 2002111300055 20021113 00055 SW 2002 11 13 CA021104001 1 20021030 A 6230 406310407101 SEAL BELL 407 407 1182206 SW ALLSN 250C 250C47B GL SWASHPLATE MISINSTALLED W K NONE K W FLUID LOSS INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) SWASHPLATE BEARING SEAL SHALL BE INSTALLED WITH SEALANT APPLIED ON MATING SURFACES. SEALANT WAS NOT APPLIED ON ALL MATING SURFACES CAUSING THE SEAL SPIN IN THE CAP ASSEMBLY TO LEAK GREASE. 1 G 7 1 3U 3 U O H2SW E1GL 2002111300057 20021113 00057 GL 2002 11 13 CA021104006 2 20020726 A 7297 WIRE CVAC 440 440 2422902 WP ALLSN 501D 501D13D 03004 GL ENGINE CHAFED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) PILOT REPORTED THAT BETA LIGHT WAS 'ON' DURING TAKEOFF ATTEMPT, PILOT ABORT TAKEOFF. MAINTENANCE INVESTIGATION FO UND THAT, BETA LIGHT AND THE FEATHER SOLENOID ENERGIZE. FURTHER INVESTIGATION FOUND THAT WIRING WAS CHAFING ON THE RT RA DIO RACK AFT OF THE APU AC CONTROL PANEL INTO THE COCKPIT. THOSE WIRES ARE: RT AUTO FEATHER CHECK RELAX AND RT FEATHER S OLENOID. WAS ABLE TO PROVE USING THE WIRING DIAGRAM THAT THOSE CHAFED WIRE COULD CAUSE THE ENGINE TO SHUT DOWN. 2 L 7 2 4R 4 T 6A6 E282 2002111300058 20021113 00058 SW 2002 11 13 CA021104008 1 20021023 A 6510 327211 DISC PACK BELL 206 206L 1181522 SW ALLSN 25OC 250C20R GL TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ROUTINE INSPECTION, BOLTS ON THE MOST FORWARD DISC PACK WAS FOUND TO BE LOOSE. THE BOLTS WERE TORQUE SEALE D AS PER MANUFACTURERS INSTRUCTIONS. THE LOOSE BOLTS WERE WORN, THE HOLES IN THE DISC PACK WERE ELONGATED AND ONE PLATE OF THE DISC PACK WAS CRACKED. ALL HARDWARE AND THE DISC PACK WAS REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 2002111300059 20021113 00059 NE 2002 11 13 MDAS091021 2 20021107 A 7230 BLADE BOEING 737 737800* NM CFMINT CFM56 CFM567B26US NE LT ENGINE FAILED W Q0MF A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 03 4778 30664 889137 ON NOV 7TH, AE 857 FLIGHT EXPERIENCED THAT TWO FAN BLADE PLATFORMS FAILED CAUSING THE LT ENGINE TO HAVE HIGH VIBRATION. CREW FOUND LT ENGINE VIBRATION INDICATION POINTED TO 5 AFTER TAKEOFF. CREW FOLLOWED QRH, CONFIRMED ENGINE VIBRATION TR UE. A/C AIR TURNED BACK, AND LANDED SAFELY. GROUND INSPECTION FOUND THAT THE NR 19 AND NR 20 FAN BLADE PLATFORMS WERE RUPTURED. AND THE DEBRIS CAUSED TO SOME OUTLET GUIDE VANES DENT OR CRACK. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002111300060 20021113 00060 EA 2002 11 13 SWIA200211438 1 20021102 A 5242 DOOR CNDAIR CL600 CL6002B19 1900309 EA EXT COMM OPEN A SWIA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 NM 07 589SW 7072 AFTER DEPARTURE FROM DSM, WE HEARD A LOUD SQUEAL FROM THE RIGHT NOSE OF THE AIRCRAFT. SUSPECTED GROUND CREW DID NOT SHU T EXTERNAL COMMUNICATIONS DOOR. RETURNED TO DSM. SHUT DOOR. ALL INDICATIONS NORMAL. 2 L 7 2 4F RT A21EA 2002121800042 20021218 00042 SO 2002 12 18 C2XA02BT074 1 20021113 A 2530 SOCKET EMB 145 EMB145LR 3260212 SO GALLEY BURNED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 11539 145536 CREW REPORTED, BURNING ODOR BY GALLEY AREA FOLLOWING LANDING, SMELLS LIKE BURNED POPCORN. MAINTENANCE REMOVED AND REPL ACED NR 2 COFFEEMAKER SOCKET IAW EMB145 AMM 25-31-01 AND NR 2 COFFEEMAKER IAW EMB AMM 25-31-01. OPS.CHECKED GOOD. NO ODO R NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002111300061 20021113 00061 SO 2002 11 13 C2XA02CL226 1 20021112 A 5610 163500110 WINDSHIELD EMB 145 EMB145ER 3260211 SO FUSELAGE ARCED A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 14943 145040 MHT FLIGHT#3595 THE CREW REPORTED THE FIRST OFFICER'S WINDSHIELD HEATING ELEMENT WAS ARCHING.MAINTENANCE INSPECTED AND R EPLACED THE FIRST OFFICER'S WINDSHIELD.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002111300062 20021113 00062 NM 2002 11 13 CALA0200544 1 20021111 A 5313 STRINGER BOEING 737 7373T0 1384582 NM STA 500C CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND A 1/2" CRACK IN STRINGER 16L AT STA 500C. A NEW STRINGER SPLICE WAS INSTALLED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2002111300063 20021113 00063 WP 2002 11 13 CALA0200545 1 20021111 A 5313 LONGERON DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 98876 49444 INSPECTION FOUND A 1" CRACK IN LONGERON 2L AT STA 1418. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 2002111300064 20021113 00064 NM 2002 11 13 CALA0200546 1 20021112 A 5230 SKIN BOEING 737 7373T0 1384582 NM AFT CARGO DR PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND A SMALL HOLE AT UPPER AFT CORNER IN OUTER SKIN OF AFT CARGO DOOR. A REPAIR WAS INSTALLED IAW SRM 52-00- 01. 2 L 7 2 4F RT A16WE 2002111300065 20021113 00065 NM 2002 11 13 CALA0200548 1 20021113 A 3350 WIRE BOEING 737 7373T0 1384582 NM BATT PACK SHORTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 WHEN THE EMERGENCY EXIT LIGHT SWITCH IN OVERHEAD WAS PUT IN ARM POSITION THE LIGHTS CAME ON. MAINTENANCE FOUND A SHORTED POWER WIRE AT EMERGENCY LIGHT BATTERY PACK(M9100) STA 378, REFERENCE WDM 33-51-01. REPAIRED WIRE AND EMERGENCY LIGHT OP ERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 2002111300066 20021113 00066 GL 2002 11 13 C2XA02CL227 2 20021112 A 7240 COMBUSTION LINER EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL #1 ENGINE CRACKED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 13936 8724 3515 145025 CAE311022 CLE FLIGHT#3280 THE CREW REPORTED A STRONG FUEL ODOR IN THE COCKPIT AFTER TAKEOFF FROM CLEVELAND.THE ODOR WAS NOTED WHEN THE PACKS WERE OPERATED FROM THE ENGINE BLEED.THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MA INTENANCE INSPECTED THE #1 ENGINE AND FOUND MULTIPLE CRACKS IN THE COMBUSTION LINER.THE #1 ENGINE WAS REPLACED.THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002111300067 20021113 00067 GL 2002 11 13 AC2A081230 2 20021018 A 7323 WASHER BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENG GOVERNOR SEPARATED H AC2A K NONE O OTHER IN INSP/MAINT 1 FS 01 8776 3089 776 POTTING COMPOUND FAILED, WASHERS AND CLIP CAME OFF THE END OF SPLINE DRIVE. GOVERNOR REPLACED 1 G 7 2 3U 3 U H3EU E4CE 2002111300068 20021113 00068 EU 2002 11 13 02315327 1 20021111 A 7722 30738451 TERMINAL JETAIR JETSTM JETSTM4101 1500501 EU A VTZA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 327UE 41080 During climb at 1000' AGL, the crew experienced fluctualting R/H engine EGT indication full deflection to both limits. The engine was shut down IAW the QRH, the aircraft was returned to IAD and landed without further incident. Maintenance personnel removed and replaced the terminal ends on the R/H engine EGT rake and reprogramed EGT parameters in the IEC. Performance engine run operational checks were satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002111300069 20021113 00069 WP 2002 11 13 DHL2002803539 1 20021028 A 5300 5654170402 PANEL DOUG DC8 DC873 302199C WP DELAMINATED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 803DH 77211 46123 ITEM REF. N/R 0409 : LOWER FUS.- #715 LH LOWER ACCESS PANEL INNER SKIN FLANGE UNBONDEDCORR: R/R #715 LH LOWER ACCESS PAN EL ON LOWER FUS. , CTR. WING IAW 51-3-0 PG. 1 2 L 7 4 4F RT 4A25 2002111300070 20021113 00070 NM 2002 11 13 DHL2002754003 1 20021112 A 3260 656021132 ACCESSORY UNIT BOEING 727 727223 1384074 NM A DHLA K O NONE OTHER J WARNING INDICATION CL CLIMB 1 SO 01 754DH 22008 1) AFTER GEAR RETRACTED ON TAKE-OFF, RED GEAR UNSAFE LIGHT AND GREEN NOSE GEAR DOWN AND LOCKED LIGHT REMAINED ILLUMINAT ED. S/O PANEL CHECKED OK, VIEWPORT SHOWED NOSE GEAR WAS NOT DOWN & LOCKED, TAKING INTO CONSIDERATION A/C PERFORMANCE, NO ISE LEVELS AND INDICATIONS ELECTED TO CONTINUE TO PHX AND 270 KIAS. 2) FOUND LANDING GEAR ACCESSORY BOX BAD. REPLACED B OX PER BMM 32-09-121 AND BMM 32-61-71-401-404. BOTH OPS TEST SATISFACTORY. NO RIGGING REQUIRED. PERFORMED LANDING GEAR A CCESSORY BOX TEST 32-09-121-501-507 SATISFACTORY. 2 L 7 3 4F A3WE 2002111300071 20021113 00071 WP 2002 11 13 DHL2002803540 1 20021023 A 5300 S1616757 LONGERON DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 803DH 77211 46123 ITEM REF. N/R: 1842: FUS. AFT OF PRESSURE DOME AREA- INTERIOR-LONGERON 17R@FUS.STA. 1766.000 WITH 1" CRACK IN IT. (MAJOR REPAIR) 2 L 7 4 4F RT 4A25 2002111300072 20021113 00072 WP 2002 11 13 DHL2002803542 1 20021010 A 5300 FORMER DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 803DH 77211 46123 ITEM REF. LH WING FORMER CENTRAL LEADING EDGE CRACKED 3" @ STA. XFS347.000 (MAJOR REPAIR).PERFORMED MAJOR REPAIR IAW SR M57-2-20 D PG. 21 STOP DRILLED CRACK IAW SRM 57-2-0 PG. 1-10 FABRICATED DOUBLERS (02EA.)(7075T6AL .071) IAW SRM 57-2-0 P G 9-10 CLEANED , TREATED , AND PRIMED IAW SRM51-1-8B INSTALLED DOUBLERS AND NEW FASTNERS IAW SRM57-2-0 PG. 9-10 SRM51-1- 20D PG. 9 2 L 7 4 4F RT 4A25 2002111300073 20021113 00073 NM 2002 11 13 ASAA0210243 1 20021015 A 5311 654654319 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 685, LBL 68 CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR PER EA. (M) 2 L 7 2 4F RT A16WE 2002111300074 20021113 00074 NM 2002 11 13 ASAA0210244 1 20021015 A 5311 654654320 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 685, RBL 68 CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR PER EA. (M) 2 L 7 2 4F RT A16WE 2002111300075 20021113 00075 NM 2002 11 13 ASAA0210248 1 20021015 A 5314 KEELBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, REQUIRED KEEL BEAM ACCESS, CUT OUT OF SKIN PANEL AT BS 727-727 PLUS 16, LEFT BUTTOCK LIN E 7. (M) 2 L 7 2 4F RT A16WE 2002111300076 20021113 00076 NM 2002 11 13 ASAA0210249 1 20021015 A 5314 656212527 KEELBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM AT BS 720-727, LBL 7 CHAFED. REMOVED AND REPLACED KEEL BEAM PER EA. (M ) 2 L 7 2 4F RT A16WE 2002111300077 20021113 00077 NM 2002 11 13 ASAA0210250 1 20021015 A 5230 6547952524 TEE FITTING BOEING 737 7372X6C 1384552 NM CARGO DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND AFT CARGO DOOR NR 5 T-ANGLE AT BS 808, RBL 65 CRACKED 1 INCH. FABRICATED REPAIR A NGLE PER EA. (M) 2 L 7 2 4F RT A16WE 2002111300078 20021113 00078 NM 2002 11 13 ASAA0210251 1 20021015 A 5311 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME INNER CHORD AT BS 808, STRINGER 25L DENTED. REMOVED AND REPLACED FRAME PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111300079 20021113 00079 NM 2002 11 13 ASAA0210252 1 20021018 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT SEAT PALLET 7-8 ILLUMINATED. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2002111300080 20021113 00080 NM 2002 11 13 ASAA0240124 1 20021004 A 5230 65479577 DOOR FRAME BOEING 737 7374Q8 138447Q NM CARGO DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 PAE - DURING C-CHECK, FOUND FORWARD CARGO DOOR FRAME AFT CLOSURE WEB LOWER FORWARD CORNER IS DAMAGED. REMOVED DAMAGED L OWER FORWARD CORNER OF FORWARD CARGO DOOR FRAME AFT CLOSURE WEB AND REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111300081 20021113 00081 NM 2002 11 13 ASAA0240126 1 20021003 A 5320 69434961 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDE WALL SUPPORT BS 847 TO 867, RBL 20 WL 156. REMOVED AND REPLACED WITH N EW SUPPORT PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111300082 20021113 00082 NM 2002 11 13 ASAA0240131 1 20021008 A 5320 65479573 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 PAE - DURING C-CHECK, FOUND CORROSION ON SUB THRESHOLD WEB AT BS 840 TO BS 794 RBL 19.5 TO 27.5 AND WL 156. REMOVED AND REPLACED THRESHOLD WEB IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111300083 20021113 00083 NM 2002 11 13 ASAA0240132 1 20021008 A 5320 69434772 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDE WALL SUPPORT AT BS 767 TO 794 RBL 20 AND WL 156. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111300084 20021113 00084 NM 2002 11 13 ASAA0240134 1 20021008 A 5320 6547690 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 727 PLUS 10 INCHES LBL 21 AND WL 156. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111300085 20021113 00085 NM 2002 11 13 ASAA0240135 1 20021008 A 5320 654769015 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 DURING C-CHECK, FOUND CORROSION ON SIDEWALL SUPPORT AT BS 727E PLUS 10 TO 835, LBL 21 AND WL 156. REMOVED AND REPLACED SUPPORT IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111300086 20021113 00086 NM 2002 11 13 ASAA0240136 1 20021008 A 5330 65C32358 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 DURING C-CHECK, FOUND GOUGE ON EXTERIOR SKIN AT BS 500 PLUS 1.5 AND 2.5 INCHES BELOW STRINGER 22R. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111300087 20021113 00087 NM 2002 11 13 ASAA0240137 1 20021008 A 5320 6547690 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 837 TO 947 AND LBL 21 AND WL 156. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111300088 20021113 00088 NM 2002 11 13 DLM88021268 1 20021030 A 5300 29525581 SKIN DOUG MD88 MD88 3023688 NM LH FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 969DL 53172 DURING HMV-2, CORROSION WAS FOUND ALONG FUSELAGE SKIN BETWEEN L-28L TO L-29L AND STA 692-718. CORROSION WAS BLENDED AND PERMANENT REPAIR MADE PER SRM 53-04 FIGURE 12B. 2 L 7 2 4F RT A6WE 2002111300089 20021113 00089 NM 2002 11 13 DL757021277 1 20021030 A 5330 143N34713 SKIN BOEING 757 757232 1384965 NM FS 558, S-26L GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 601DL 22808 FUSELAGE / SKIN / FS 558 / STRG. 26L : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND GOUGED JUST BELOW THE STRINGER 26L SKIN LAP JOINT AT FS 558. THE GOUGE WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 383880-14, REV A. 2 L 7 2 4F RT A2NM 2002111300090 20021113 00090 NM 2002 11 13 DL757021286 1 20021101 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM FS 1711, S-15L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 601DL 22808 FUSELAGE / SKIN / FS 1711 / STRG. 14L-17L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH 2 DENTS AT FS 1711 BETWEEN STRINGERS 14L & 17L. THE DENTS WERE REMOVED WITH 2 SKIN CUTOUTS. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 383877-14, REV A. 2 L 7 2 4F RT A2NM 2002111300091 20021113 00091 NM 2002 11 13 DL757021287 1 20021101 A 5330 143N35212 SKIN BOEING 757 757232 1384965 NM FS 740, S-28 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 601DL 22808 FUSELAGE / SKIN / FS 715-740 / STRG. 28L-28R : CORROSION REPAIR AT LWR VHF ANTENNAL CUTOUT THE FUSLEAGE SKIN WAS FOUND WITH AREAS OF CORROSION AROUND THE LOWER VHF ANTENNA CUTOUT BETWEEN FS 715 & 740 AND BETWEEN STRINGERS 28L & 28R. THE CUTOUT WAS ENLARGED TO REMOVE THE CORROSION AND THE AREA REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 383860-14, REV A. 2 L 7 2 4F RT A2NM 2002111300092 20021113 00092 NM 2002 11 13 DL733021289 1 20021101 A 3600 BOE20030052 SEAL BOE20030052 BOEING 737 7373B7 1384580 NM P-DOME TORN A DALA B EMER. DESCENT G MULTIPLE FAILURE CR CRUISE 1 SO 27 947WP NONE 23376 AFTER LEVELING AT FL350 MASTER CAUTION W/OVERHEAD ON THE MASTER CAUTION PANEL ILL. PASS. O2 LIGHT ON THEOVERHEAD WAS ILL. CABIN ALT. WAS AT 15,000FEET. FA CONFIRMED MASKS HAD DROPPED. AUTO FAIL LIGHT WAS ILL. BUT NO ALT. ALERT HORN HAD SOUNDED. ALT. CONT. WAS SWITCHED TO STBY BUT CABIN CONTROL WAS NOT REGAINED UNTIL DECENDING THROUGH 20,000 FEET. PRESS. CONTROLLER DID NOT SWITCH FROM AUTO TO STBY AUTOMATICALLY. CORR. ACTN. RPLD. CABIN PRESSURE SWITH.PERFORMED CABIN ALT. WARNING SW.TEST. FOUND RUBBER BOOT LEAKING ON AFT SIDE OF P-DOME ON LOWER LT. SIDE. RPLD. SAME. LEAK CK. GOOD. 2 L 7 2 4F RT A16WE 2002111300093 20021113 00093 NM 2002 11 13 DL72S021302 1 20021105 A 5310 TORQUE BOX BOEING 727 727232 1384082 NM FS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FUSELAGE / VENTRAL STAIRWAY / RH TORQUE BOX STRUCTURE / FS 1263 : CRACK REPAIR THE VENTRAL STAIRWAY ACTUATOR ON THE RH TORQUE BOX AT FS 1263 WAS FOUND PULLED THROUGH THE UPPER WEB OF THE TORQUE BOX, RESULTING IN CRACKING DAMAGE TO THE UPPER WEB, SIDE WEB, AND UNDERLYING STIFFENERS. THE DAMAGE TO THE UPPER WEB WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM DOUBLER. ALL OTHER MEMBERS REPLACED. THE REPAIR WAS ACCOMPLISHED PER ER/A 384097-14AD. 2 L 7 3 4F A3WE 2002111300094 20021113 00094 NM 2002 11 13 371PA0012 1 20021106 A 3350 362624 LIGHT BOEING 737 737306 13844BG NM A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 371PA 23543 Emergency floor lighting has 1 inop strip in aft cabin. R&R 1 light strip in aft cabin. Ops chk normal. 2 L 7 2 4F RT A16NE 2002111300095 20021113 00095 2002 11 13 0203639993 4 20021030 A 2211 25878263 COMPUTER DOUG DC9 DC931 3022065 WP A NWAA A D UNSCHED LANDING RETURN TO BLOCK F FLT CONT AFFECTED CL CLIMB 1 GL 01 8986E 47402 On takeoff at 1000 feet the flight crew experienced rapid yaw movements to both left and right. Required full yoke defle ction to maintain control of the aircraft. COM complied with and both yaw damper and rudder servo were turned off. Fligh t returned to an uneventful landing back at MEM. Maintenance replaced the stablizer augmentation computer and aircraft r eturned to service. 2 L 7 2 4F A6WE 2002111300096 20021113 00096 NM 2002 11 13 QXEA0201931 1 20021111 A 7930 APT761000100DW TRANSMITTER DHAV DHC8 DHC8202 2809007 NM ZONE 400 INOPERATIVE A QXEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 NM 09 357PH 5040 5040 504 PDX-#2 ENGINE OIL PRESSURE DROPPED DURING CLIMB OUT AS LOW AS 35 PSI. NO WARNING LIGHTS ASSOCIATED WITH LOW PRESSURE. WI TH REDUCED POWER SETTING ON DESCENT PRSSURE RETURNED TO NORMAL. OPERATED #2 ENGINE AND FOUND OIL PRESSURE TO INDICATE A CONSTANT 55 PSI. REMOVED AND REPLACED #2 ENGINE OIL PRESSURE TRANSMITTER. OPERATED #2 ENGINE AND FOUND OIL PRESSURE IND ICATING NORMAL AT 62 PSI. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002111300097 20021113 00097 WP 2002 11 13 IXXA0200112O 1 20021112 A 3210 SWITCH DOUG DC8 DC873F 302199F WP LEFT GEAR LOOSE A IXXA O OTHER J WARNING INDICATION DE DESCENT 1 SW 11 603AL 90093 1093 46003 ENROUTE FROM DFW TO TOL, THE LANDING GEAR LIGHT REMAINED ILLUMINATED FOLLOWING LANDING GEAR EXTENSION. THE FLIGHT CREW RECYCLED THE GEAR AND THE LIGHT FLICKERED THEN REMAINED ILLUMINATED. THE CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A LOOSE CONNECTION AT THE LEFT GEAR SWITCH. M AINTENANCE SECURED THE CONNECTION AND PERFORMED A SUCESSFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE DOUGLAS REPAIR MANU AL 2 L 7 4 4F RT 4A25 2002111300098 20021113 00098 NM 2002 11 13 AWXA200201115 1 20021023 A 5414 65C26301 FAIRING BOEING 737 7373U3 13844CC NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 335AW 0 0 28740 LCQ - MAJOR REPAIR - DURING C-04 CHECK A 1" CRACK WAS FOUND AT THE FORWARD UPPER CORNER RADIUS OF THE INBOARD FLAP, OUTB OARD TRACK FAIRING ASSEMBLY, INBOARD SIDE OF EXTERNAL SHELL, L/H ENG PYLON. MAINTENANCE CUTOUT CRACKED AREA AT THE FORWA RD UPPER CORNER RADIUS OF THE INBOARD FLAP, OUTBOARD TRACK FAIRING ASSEMBLY, INBOARD SIDE OF EXTERNAL SHELL, L/H ENG PYL ON; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND DOUBLER; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 54-50-70, FIG. 204. 2 L 7 2 4F RT A16WE 2002111300099 20021113 00099 NM 2002 11 13 AWXA200201116 1 20021029 A 5330 6545769 SKIN BOEING 737 7373U3 13844CC NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 335AW 0 0 28740 LCQ - MAJOR REPAIR - DURING C-04 CHECK A 1/8" CRACK WAS FOUND AT CORNER OF AIR CONDITION GROUND SERVICE DOOR CUTOUT, LOW ER FUSELAGE, BS 540. MAINTENANCE BLENDED OUT CRACK AT CORNER OF AIR CONDITION GROUND SERVICE DOOR CUTOUT, BS 540; TREATE D AND PRIMED AREA IAW B737-300 SRM 53-00-01, FIG. 101. 2 L 7 2 4F RT A16WE 2002111300100 20021113 00100 WP 2002 11 13 DHL2002803546 1 20021006 A 5313 4772397U1 FITTING DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 803DH 77211 46123 ITEM REF. N/R 0819: AFT ACCY COMPT. - FITTING 2" CRACKED, STA. 1766.000 L28L (MAJOR REPAIR)CORR: PERFORMED MAJOR REPAIR IAW SRM53-1-0 PG. 1 REMOVED DAMAGED FITTING IAW SRM51-1-20D PG. 21CLEANED , TREATED , AND AREA IAW SRM51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG. 9 , SRM51-1-14 PG 1 2 L 7 4 4F RT 4A25 2002111400001 20021114 00001 2002 11 14 AC2A081231 4 20021019 A 3425 430375002109 DISPLAY BELL 430 430 1182150 SW EFIS DEFECTIVE H AC2A O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 FS 01 430CV 1972 49072 PART IS DEFECTIVE. DURING CRUISE FLIGHT PILOT DETECTED A STRONG BURNING ODOR, ACCOMPANIED WITH A "FAIL" INDICATION ON TH E EADI. FOLLOWING EMERGENCY PROCEDURES, THE ODOR STOPPED WHEN THE EFIS WAS TURNED OFF. PART WAS REPLACED WITH SERVICEABL E UNIT. 1 G 7 2 3U RT H9SW 2002111400002 20021114 00002 SW 2002 11 14 AC2A081232 1 20021028 A 3213 206323021 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED H AC2A K NONE O OTHER IN INSP/MAINT 1 FS 01 7159H 581 51397 CORROSION WAS FOUND UNDER THE SADDLE SUPPORT CLAMP AND PART HAD ONLY 581 HOURS ON IT. REPLACED THE CROSSTUBE. 1 G 7 1 3U H2SW 2002111400003 20021114 00003 SW 2002 11 14 AC2A081233 1 20021029 A 3340 900601 LIGHT BELL 430 430 1182150 SW SEARCH LIGHT MALFUNCTIONED H AC2A K NONE L NO TEST IN INSP/MAINT 1 FS 01 430CH 492 49037 LIGHT WILL NOT RETRACT. REPLACED LIGHT. 1 G 7 2 3U RT H9SW 2002111400004 20021114 00004 GL 2002 11 14 AC2A081234 2 20021031 A 7323 23065123 SHAFT BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 2 ENG GOV DEBONDED H AC2A K NONE O OTHER IN INSP/MAINT 1 FS 01 8775 775 831789 PART IS DISBONDED. POTTING MISSING FROM END OF DRIVESHAFT. REPLACED GOVERNOR. 1 G 7 2 3U 3 U H3EU E4CE 2002111400005 20021114 00005 GL 2002 11 14 AC2A081235 2 20021101 A 7323 SHAFT BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 ENG GOV CRACKED H AC2A K NONE O OTHER IN INSP/MAINT 1 FS 01 8775 10259 775 834599 POTTING MISSING FROM END OF DRIVE SHAFT. REPLACED GOVERNOR. 1 G 7 2 3U 3 U H3EU E4CE 2002111400026 20021114 00026 WP 2002 11 14 MWEA020672 1 20021111 A 5313 591022848 LONGERON DOUG DC9 DC981 3022081 WP FRAME STA 1429 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 LONGERON 16 RIGHT AT FRAME STATION 1429 IS CRACKED. -- FABRICATED AND INSTALLED REPAIRED SECTION OF LONGERON AND INSTA LLED SPLICES. 2 L 7 2 4F A6WE 2002111400027 20021114 00027 WP 2002 11 14 MWEA020671 1 20021111 A 5313 59360043 SKIN DOUG DC9 DC981 3022081 WP STATION 655 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FUSELAGE SKIN HAS A DENT AT STATION 655 LONGERON 30-29 LEFT. -- REMOVED SHEARTIE, FABRICATED AND INSTALLED INTERNAL DOU BLER AND SPLICES. 2 L 7 2 4F A6WE 2002111400028 20021114 00028 WP 2002 11 14 MWEA020673 1 20021111 A 5313 591142275 LONGERON DOUG DC9 DC981 3022081 WP STA 1212-1193 IMPROPER A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 EXISTING HOLES IN LONGERON 5 LEFT STATION 1212-1193 CONFLICT WITH THE INSTALLATION OF THE UPPER GALLEY MOUNTS. -- REMO VED LONGERON , LOCATED AND DRILLED LONGERON . INSTALLED LONGERON AND SLPICE 2 L 7 2 4F A6WE 2002111400029 20021114 00029 WP 2002 11 14 MWEA020675 1 20021111 A 5313 991556153 WEB DOUG DC9 DC981 3022081 WP LONGERON 21-22 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 1338 BULKHEAD WEB AT LONGERON 21-22 RIGHT HAS CORROSION. -- FABRICATED AND INSTALLED WEB. 2 L 7 2 4F A6WE 2002111400030 20021114 00030 WP 2002 11 14 MWEA020676 1 20021111 A 5313 9953238109 FORMER DOUG DC9 DC981 3022081 WP STA 1322 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FORMER AT STATION 1322 BETWEEN LONGERON 17 LEFT AND CUSP HAS DEEP CHAF ON INBOARD SIDE. -- REMOVED AND REPLACED FORMER . 2 L 7 2 4F A6WE 2002111400031 20021114 00031 WP 2002 11 14 MWEA020678 1 20021111 A 5313 591142267 DOUBLER DOUG DC9 DC981 3022081 WP STA 1212-1220 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FUSELAGE SKIN AT STATION 1212-1220 LONGERON 5 LEFT IS DENTED. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002111400032 20021114 00032 WP 2002 11 14 MWEA020681 1 20021111 A 5313 59360043 SKIN DOUG DC9 DC981 3022081 WP STA 696 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FUSELAGE SKIN HAS A DENT AT STATION 696 3" ABOVE LONGERON 27 RIGHT. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002111400033 20021114 00033 WP 2002 11 14 MWEA020683 1 20021111 A 5313 59114013 SKIN DOUG DC9 DC981 3022081 WP STA 218 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FUSELAGE SKIN HAS A DENT AT STATION 218 BETWEEN LONGERON 18 LEFT AND 19 LEFT. -- COLD FORMED SKIN, CHECKED AREA FOR CR ACKS, NO DEFECTS FOUND, FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002111400034 20021114 00034 WP 2002 11 14 MWEA020684 1 20021111 A 5313 5936434127 SKIN DOUG DC9 DC981 3022081 WP STA 270 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FUSELAGE SKIN REQUIRES REPAIR AT STATION 270 BETWEEN LONGERON 29 LEFT AND 30 DUE TO THE REMOVAL OF AN ANTENNA. -- FABR ICATED AND INSTALLED EXTERNAL DOUBLER AND FINGER DOUBLERS. 2 L 7 2 4F A6WE 2002111400035 20021114 00035 WP 2002 11 14 MWEA020685 1 20021111 A 5230 59360381 BEAM DOUG DC9 DC981 3022081 WP MID CARGO CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 MID CARGO PIT DOOR JAMB LOWER TEE HAS CORROSION. -- REMOVED AND REPLACED BEAM. 2 L 7 2 4F A6WE 2002111400036 20021114 00036 WP 2002 11 14 MWEA020689 1 20021112 A 5320 995823911 SHEAR TIE DOUG DC9 DC914 3022034 WP STATION 840 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 SHEAR TIE AND DOUBLER AT STATION 840 LONGERON LEFT 14 CRACKED. -- FABRICATED AND INSTALLED FORMER. 2 L 7 2 4F A6WE 2002111400037 20021114 00037 WP 2002 11 14 MWEA020690 1 20021112 A 5313 59101462 LONGERON DOUG DC9 DC914 3022034 WP STATION 525 A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 POSSIBLE CRACK AT STATION 525 LONGERON 7 RIGHT REQUIRES INTERNAL OPEN UP FOR VISUAL INSPECTION. -- FABRICATED AND INSTA LL LONGERON SECTION AND REPAIR SPLICES. 2 L 7 2 4F A6WE 2002111400045 20021114 00045 NM 2002 11 14 2002F00991 1 20021015 A 3350 1000677 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 288SC 20765 PSM - FOUND EMERGENCY LIGHTS AT L1 AND R1 FAILED TO TEST. REMOVED AND REPLACED LIGHT ASSEMBLIES AT L1 AND R1. (M) 2 L 7 3 4F RT A3WE 2002111400046 20021114 00046 NM 2002 11 14 ASAA0240128 1 20021008 A 5320 6947957 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111400047 20021114 00047 NM 2002 11 14 ASAA0240129 1 20021008 A 5230 69479577 DOOR FRAME BOEING 737 7374Q8 138447Q NM CARGO DOOR CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 DURING C-CHECK, FOUND FORWARD CARGO DOOR FRAME AFT CLOSURE WEB LOWER FORWARD CORNER DAMAGED. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111400048 20021114 00048 NM 2002 11 14 ASAA0240130 1 20021008 A 5247 6550904625 DOUBLER BOEING 737 7374Q8 138447Q NM APU DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 PAE - DURING C-CHECK, FOUND APU COMPARTMENT DOOR REPAIR IS GOUGED 16 INCHES FROM AFT END AND 7 INCHES FROM LEFT EDGE. R EMOVED AND REPLACED DOUBLER IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111400049 20021114 00049 NM 2002 11 14 ASAA0240133 1 20021008 A 5320 694769020 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111400050 20021114 00050 NM 2002 11 14 ASAA0240138 1 20021008 A 5320 652072615 STIFFENER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 DURING C-CHECK, FOUND CORROSION ON UPPER SURFACE OF FORWARD CARGO DOOR THRESHOLD WEB STIFFENER AT BS 460, RBL 29, WL 156 . REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111400051 20021114 00051 NM 2002 11 14 ASAA0240139 1 20021008 A 5320 6520726 THRESHOLD BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 DURING C-CHECK, FOUND CORROSION ON LOWER SURFACE OF FORWARD CARGO DOOR THRESHOLD WEB AT NUT PLATED AT BS 445-490, RBL 29 AND WL 156. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111400052 20021114 00052 NM 2002 11 14 ASAA0240140 1 20021008 A 5310 6546550 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 787 RBL 17 BETWEEN STRINGER 25 RT AND 26 RT. REMOVED AND REPLA CED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111400053 20021114 00053 NM 2002 11 14 ASAA0240141 1 20021008 A 5310 6546550 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 768 BETWEEN STRINGER 26 RT AND 27 RT. REMOVED AND REPLACED SHE AR TIE PER SRM. (M) 2 L 7 2 4F RT A16WE 2002111400054 20021114 00054 NM 2002 11 14 ASAA0240142 1 20021008 A 5310 6546548 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 747 BETWEEN STRINGER 26 LEFT AND 27 LEFT. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002111400056 20021114 00056 WP 2002 11 14 ASAA0280376 1 20021016 A 5345 993653437 SUPPORT FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING 30K-CHECK, FOUND GALLEY SUPPORT FLOOR STRUCTURE CORRODED AT FS 175, RBL 26. REPLACED GALLEY SUPPORT FITTIN G PER SRM 51-10-4 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002111400057 20021114 00057 WP 2002 11 14 ASAA0280377 1 20021016 A 5320 5956028147 BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K-CHECK, CENTER CARGO DOOR FORWARD HOLD OPEN LATCH SIDE BRACKET CRACKED .50 INCH. REPLACED BRACKET PER SRM 51-10-2, AND DAC DWG 5956028. (M) 2 L 7 2 4F RT A6WE 2002111400058 20021114 00058 WP 2002 11 14 ASAA0280378 1 20021016 A 5320 5956028147 BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, CENTER CARGO DOOR AFT HOLD-OPEN LATCH SIDE BRACKET CRACKED. REPLACED BRACKET PER SRM 51-1 0-2, AND DAC DWG 5956028. (M) 2 L 7 2 4F RT A6WE 2002111400059 20021114 00059 WP 2002 11 14 ASAA0280391 1 20021019 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 165, LBL 53. REPLACED SUPPORT PER SRM 53-14-1, FIG 11 AND 53 -30-2. (M) 2 L 7 2 4F RT A6WE 2002111400060 20021114 00060 WP 2002 11 14 ASAA0280392 1 20021019 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 200, RBL 46-52. REPLACED SUPPORT PER SRM 53-14-1, FIG 11 AND 53-30-2. (M) 2 L 7 2 4F RT A6WE 2002111400061 20021114 00061 WP 2002 11 14 ASAA0280393 1 20021019 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT IS CORRODED AT FS 204, LBL 9-13. REPLACED SUPPORT PER SRM 53-14-1, FIG 11 A ND 53-30-2. (M) 2 L 7 2 4F RT A6WE 2002111400062 20021114 00062 WP 2002 11 14 ASAA0280394 1 20021019 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT IS CORRODED AT FS 160, LBL 5 - RBL 5. REPLACED SUPPORT PER SRM 53-14-1, FIG 11 AND 53-30-2. (M) 2 L 7 2 4F RT A6WE 2002111400063 20021114 00063 WP 2002 11 14 ASAA0280395 1 20021019 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT IS CORRODED AT FS 204, LBL 5 - RBL 5. REPLACED SUPPORT PER SRM 53-14-1, FIG 11 AND 53-30-2. (M) 2 L 7 2 4F RT A6WE 2002111400064 20021114 00064 WP 2002 11 14 ASAA0280396 1 20021019 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT IS CORRODED AT FS 200, LBL 15-43. REPLACED SUPPORT PER SRM 53-14-1, FIG 11 AND 53-30-2. (M) 2 L 7 2 4F RT A6WE 2002111400065 20021114 00065 WP 2002 11 14 ASAA0280397 1 20021021 A 5330 5921375 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K CHECK, FUSELAGE SKIN DENTED AT FS 208, L16R TO L17R. REPAIRED SKIN PER SRM 53-04, FIG 38. (M) 2 L 7 2 4F RT A6WE 2002111400066 20021114 00066 WP 2002 11 14 ASAA0280398 1 20021021 A 5330 29525063 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K CHECK, FUSELAGE SKIN DENTED 50 INCHES AFT OF LEFT FORWARD PASSENGER DOOR, 2 INCHES ABOVE FLOOR LI NE BEHIND LOWER SIDEWALL GRILLE. REPAIRED SKIN PER SRM 53-04, FIG 12B, SHEET 4, PG 36. (M) 2 L 7 2 4F RT A6WE 2002111400067 20021114 00067 WP 2002 11 14 ASAA0280399 1 20021021 A 5310 99360737 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY SHEAR TIE CORRODED TWO PLACES AT FS 1212. REPAIRED SHEAR TIE PER SRM 53-03, FIG 6. (M) 2 L 7 2 4F RT A6WE 2002111400068 20021114 00068 WP 2002 11 14 ASAA0280400 1 20021021 A 5310 99360737 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, AFT CARGO BAY SHEAR TIE FASTENER HOLES (8 EACH) CORRODED AT FS 1212. REPLACED SHEAR TIE PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2002111400069 20021114 00069 WP 2002 11 14 ASAA0280401 1 20021021 A 5320 593607111 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY INTERCOSTAL BETWEEN LONGERON 29R AND 30 AT FS 1155 IS CORRODED. REPLACED IN TERCOSTAL PER SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002111400070 20021114 00070 WP 2002 11 14 ASAA0280402 1 20021021 A 5310 593607117 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 957AS 53451 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY UPPER SHEAR TIE CORRODED AT FS 1155, LONGERON 30 TO 29R. REPLACED UPPER SHE AR TIE PER SRM 51-30-2 AND 51-10-2. (M) 2 L 7 2 4F RT A6WE 2002111400071 20021114 00071 WP 2002 11 14 ASAA0280403 1 20021021 A 5730 993746310 SKIN DOUG DC9 DC983 3022083 WP RT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K CHECK, RIGHT WING LEADING EDGE CRACKED .5 INCH ON RIB AT FASTENER HOLES AT WING STATION XRS 69. STOP DRILLED, REMOVED DAMAGE, AND INSTALLED DOUBLER AND SHIM PER SRM 51-10-3. (M) 2 L 7 2 4F RT A6WE 2002111400077 20021114 00077 NM 2002 11 14 AHE02064 1 20021016 A 6230 900F1401010103 SUPPORT DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE MAST CRACKED B E5ZR K NONE O OTHER IN INSP/MAINT 1 GL 05 92001 1197 90000040 DURING MAINTENANCE OPERATION TO REPLACE LIFE LIMITED NON-ROTATING SWASHPLATE ON AIRCRAFT, A SUSPECTED CRACK WAS FOUND ON THE INNER SURFACE OF THE STATIC MAST. THE CRACK APPEARS IN APPROXIMATELY .5000 THE CIRCUMFERENCE OF THE SHAFT. THE S TATIC MAST ASSEMBLY OF THE MAIN TRANSMISSION IS TO BE REPLACED WITH A NEW ITEM. PROBABLE CAUSE, UNKNOWN AT THIS TIME. 1 G 7 2 3U 3 U NC H19NM E42NE 2002111400078 20021114 00078 NM 2002 11 14 EIA2002104 1 20021028 A 5414 SKIN BOEING 747 747121 1384871 NM NR 4 NACELLE CHAFED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - AFT EDGE INNER SKIN WORN/CHAFED IN NUMEROUS AREAS ESPECIALLY BOTH LOWER CORNERS ON NR 4 ENGINE NOSE COWL TO FORWAR D FAIRING. REPAIRED AFT AND UPPER SKINS AND INNER SKIN PER B747 SRM 51-40-02 FIG 1. (M) 2 L 7 4 4F A20WE 2002111400080 20021114 00080 SO 2002 11 14 CYZ2002F00000 1 20021104 A 3260 9564306L BRACKET PIPER PA28 PA28R200 7102811 SO LYC O360 IO360A1A 41514 EA LT MLG LACK OF LUBE E CYZA K NONE O OTHER IN INSP/MAINT 1 CE 01 55131 28R7335184 UPON GEAR EXTENSION, LT MLG DOWN LIGHT WOULD NOT ILLUMINATE. GEAR WAS RECYCLED SEVERAL TIMES WITHOUT SUCCESS. ON LANDI NG THE GEAR COLLAPSED. FOUND LEFT SIDEBRACE STUD STICKING IN SIDE BRACE BRACKET AND WOULD NOT ALLOW THE GEAR TO OPERATE FREELY ENOUGH TO ENGAGE DOWN LOCK. FOUND THAT THE BRACKET DID NOT APPEAR TO HAVE BEEN LUBRICATED AFTER INSTALLATION TO COMPLY WITH AD. RT SIDE WAS ALSO INSPECTED AND WAS FOUND TO HAVE BEEN LUBRICATED. 1 L 7 1 3O 3 O 2A13 1E10 2002111400081 20021114 00081 NM 2002 11 14 EIA2002105 1 20021028 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND FRAME CRACKED AT STATION 1760 IN AFT LOWER CARGO LEFT SIDE AT APPROX S36L. REMOVED DAMAGE, FABRICATED REPAI R PARTS AND INSTALLED REPAIR PER B747 SRM 51-40-03 FIG 1. (M) 2 L 7 4 4F A20WE 2002111400082 20021114 00082 EU 2002 11 14 DCG2002F00000 1 20021011 A 6410 355A12004008 BLADE SNIAS 350 AS350* EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED A DCGA K NONE O OTHER IN INSP/MAINT 1 WP 13 798JH 2001 612 1548 DURING 500 HR INSPECTION ON TAIL ROTOR BLADES, FOUND SMALL CRACKS ORIGINATING FROM S/S LEADING EDGE ON OUTBOARD SKIN, ON POLYURETHANE STRIP. 1 G 7 1 3U 3 U H9EU E19EU 2002111400083 20021114 00083 SO 2002 11 14 EEJ2002F00004 1 20021016 A 6120 ROD PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2A GL PITCH CHANGE STRIPPED A EEJA K NONE O OTHER IN INSP/MAINT 1 NM 07 114SA 318052053 L707561A DJ12017A LT ENGINE WOULD NOT PRODUCE FULL RPM AND PROPELLER WENT TO FEATHER ON NORMAL SHUTDOWN. PROPELLER REMOVED AND TAKEN FOR INSPECTION. FOUND PITCH CHANGE ROD ADJUSTING SCREW AND HOUSING THREADS STRIPPED. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2002111400084 20021114 00084 NM 2002 11 14 GAIA02136ST 1 20021024 A 5720 STIFFENER BOEING 727 727225 1384077 NM LT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING FRONT SPAR AT FSS 106.8 VERTICAL STIFFENER IS CRACKED AT THE FORWARD END. REPAIR ACCOMPLISHED IAW BOEING 727 SRM 57-30-4, FIGURE 7. THE AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 L 7 3 4F A3WE 2002111400085 20021114 00085 SO 2002 11 14 FTU2002F00000 1 20021022 A 3211 42042002 BRACKET PIPER PA42 PA42 7104202 SO PWA PT6 PT6A41 52043 EA MLG PIVOT MISMANUFACTURED B FTUR K NONE O OTHER IN INSP/MAINT 1 NE 05 444SC 428001034 RECEIVED TWO NEW MAIN LANDING GEAR DOWN LOCK PIVOT BRACKETS, FOUND THE SLOT SUED TO CREATE THE PIVOT CAPABILITY WAS IMPR OPERLY MACHINED. WHEN INSTALLED ON THE AIRCRAFT, THE PART WOULD NOT PIVOT DUE TO CLEARANCE PROBLEM REPLACEMENT ITEM ON THIS AIRCRAFT, ALONG WITH THE APPLICABLE BOLTS. 1 L 7 2 4T 4 T A23SO E4EA 2002111400088 20021114 00088 2002 11 14 JEM2002F00007 4 20020716 A 2340 SPA400 PANEL PIPER PA31 PA31325 7103105 SO LYC O540 TIO540* 41532 EA INTERCOM FAILED A JEMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 01 174BH 317612038 DURING CRUISE FLIGHT, PILOT SMELLED A BURNING ELECTRICAL ODOR THAT WAS FOLLOWED BY A LOSS OF INTERCOM FUNCTION AND THE I NTERCOM CIRCUIT BREAKER TRIPPED. ODOR DISSIPATED. MAINTENANCE PERSONNEL FOUND A FAULTY INTERCOM PANEL AND NO DAMAGE TO WIRING OR OTHER EQUIPMENT. SPA400 INTERCOM WAS REPLACED WITH A LIKE ITEM. 1 L 7 2 3O 3 O A20SO E14EA 2002111400091 20021114 00091 EA 2002 11 14 LER2002F00000 2 20021022 A 8520 78072 BOLT PIPER PA38 PA38112 7103812 SO LYC O235 O235* 41505 EA CONNECT ROD FAILED E LERA A UNSCHED LANDING R E Y PARTIAL RPM/PWR LOSS VIBRATION/BUFFET ENGINE STOPPAGE CR CRUISE 1 NM 11 9296T 1885 3878A0335 1577215 IN CRUISE FLIGHT. 6 HOURS AFTER ENGINE START WHEN PILOT NOTICED SLIGHT ROUGHNESS FOLLOWED BY LOSS OF OIL PRESSURE. FOL LOWED IMMEDIATELY BY EXTREME VIBRATION, SMOKE AND OIL FROM ENGINE COMPARTMENT AND ENGINE STOPPAGE. PILOT COMPLETED A SU CCESSFUL EMERGENCY LANDING. UPON ENGINE INSPECTION AND TEARDOWN, IT WAS DETERMINED THAT ONE OF NR 4 CYLINDER CONNECTING ROD BOLTS HAD FAILED AND ALLOWED THE ROD CAP TO SEPARATE CAUSING LOSS OF INDICATED OIL PRESSURE AND CATASTROPHIC ENGINE FAILURE. INSPECTION OF FAILED CONNECTING ROD BOLT, INDICATES THERE WAS POSSIBLE CRACK OR DEFECT PRIOR TO FINAL SEPARA TION. INSPECTION OF CRANKSHAFT JOURNALS AND BEARING INSERT SHOWS NORMAL WEAR CONSISTENT WITH ENGINE TSO. 1 L 7 1 3O 3 O A18SO E223 2002111400092 20021114 00092 CE 2002 11 14 NZZ2002F00000 1 20021003 A 3260 1068100111 UPLOCK CABLE BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO MLG BROKEN E NZZA K NONE O OTHER IN INSP/MAINT 1 GL 03 81FD 3890 TH963 FOUND RT LANDING GEAR UP/DOWN LOCK CABLE BROKEN AT GEAR MOTOR IN FUSELAGE, RELEASING DOWN LOCK. CABLE HAD BROKEN AT SWA G. TUGGED ON LT CABLE, CABLE SEPARATED AT LOWER SWAGE. 1 L 7 2 3O 3 O 3A16 E5CE 2002111400093 20021114 00093 CE 2002 11 14 QFY2002F00002 1 20021101 A 3230 5KE51CA TRANSORB BEECH 200 B200 1152922 CE PWA PT6 PT6A11 52043 NE MLG FAILED B QFYR K NONE O OTHER IN INSP/MAINT 1 NE 03 875DM BB1354 TRANSORB FAILED TO SHORTED CONDITION. RESULTED IN LANDING GEAR CIRCUIT BREAKER TO POP CAUSING NEED FOR MANUAL EXTENSION OF LANDING GEAR. 1 L 7 2 4T 3 T A24CE E4EA 2002111400094 20021114 00094 EU 2002 11 14 R7MR35270 1 20020505 A 6240 AWEURO4 SIGNAL COND UNIT UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE MAST MOMENT INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 102HN 0159 SIGNAL PROCESSING UNIT, INOPERATIVE. NOT MAST MOMENT INDICATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002111400095 20021114 00095 EU 2002 11 14 R7MR35273 1 20020530 A 6240 AWEURO4 SIGNAL COND UNIT UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE MAST MOMENT INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 102HN 45 0159 UNIT INOPERATIVE, NO MAST MOMENT INDICATION. ADVISED BY AEC TECHNICAL SERVICE TO REPLACE UNIT. REPLACED WITH NEW UNIT FROM KIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002111400096 20021114 00096 NM 2002 11 14 GAIA02137ST 1 20021024 A 5720 WEB BOEING 727 727225 1384077 NM LT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING LEADING EDGE WEB AT WING STATION 130.7 UPPER CHORD IS CRACKED ABOUT 10 INCHES LONG. REPAIRED ACCOMPLISHED IAW BOEING 727 SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002111400097 20021114 00097 2002 11 14 920WA0007 4 20021110 A 2230 COMPUTER BOEING 737 737236 1384476 NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 920WA 21791 Airspeed bug sticks after t/o. Swapped DADC's for troubleshooting purposes. A/C ops normal per MM 34 bite. 2 L 7 2 4F RT A16WE 2002111400098 20021114 00098 NM 2002 11 14 GAIA02139ST 1 20021024 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT IN THE FORWARD CARGO LOWER BILGE BS 600, IN BETWEEN STRINGER S28L AN D S29L, THE FRAME WAS DENTED. REPAIR ACCOMPLISHED IAW BOEING 727 SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 L 7 3 4F A3WE 2002111400099 20021114 00099 NM 2002 11 14 GAIA02140ST 1 20021024 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE SKIN WAS CRACKED AT THE FORWARD ENTRY DOOR LOWER HINGE CUT OUT. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SERVICE BULLETIN 727-53-198. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002111400100 20021114 00100 NM 2002 11 14 GAIA02141ST 1 20021024 A 5755 SKIN BOEING 727 727225 1384077 NM SPOILER DELAMINATED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING NR 7 GROUND SPOILER PANEL WAS DELAMINATED AND HAD HOLE S ON THE BOTTOM SIDE OF THE PANEL. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 57-50-6, FIGURE 5. THE AIRCRAFT WAS RETU RNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002111400101 20021114 00101 NM 2002 11 14 GAIA02142ST 1 20021024 A 5730 SKIN BOEING 727 727225 1384077 NM LT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING LEADING EDGE UPPER SKIN AT THE NR 3 SLAT GUIDE FITTING CUT OUT WAS CRACKED AND HAD LOOSE FASTENERS. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 57-30-4, FIGURE 9. THE AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002111400102 20021114 00102 NM 2002 11 14 GAIA02143ST 1 20021024 A 5754 RIB BOEING 727 727225 1384077 NM L/E SLAT CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING NR 4 SLAT INTERIOR RIB WAS CRACKED AT WS 410, OUTBOARD OF THE ACTUATOR ATTACH POINT. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 57-50-3, FIGURE 9. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002111400103 20021114 00103 NM 2002 11 14 GAIA02144ST 1 20021024 A 5754 SKIN BOEING 727 727225 1384077 NM L/E SLAT DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING NR 2 SLAT NOSE UPPER SURFACE SHOWS A LARGE DENTED AREA ON THE SKIN. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 57-50-3, FIGURE 4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002111400104 20021114 00104 NM 2002 11 14 GAIA02145ST 1 20021024 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE VENTRAL STAIR CUTOUT, FORWARD RIGHT SIDE HAD A CRACK IN THE RADI US. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 53-30-3, FIGURE 13. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002111400105 20021114 00105 NM 2002 11 14 GAIA02146ST 1 20021024 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION AT FLIGHTSTAR IN JAX, IT WAS DISCOVERED THAT THE C-1 DOOR CUT OUT INNER SKIN WAS CRACKED AT BS 620, STRINGER S25R. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 51-40-2, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 L 7 3 4F A3WE 2002111400106 20021114 00106 NM 2002 11 14 GAIA02147ST 1 20021024 A 5741 BUSHING BOEING 727 727225 1384077 NM LT WING DETERIORATED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT AFT BOTTLE PIN BUSHINGS WERE DETERIORATED. THE BUSHINGS WE RE REPLACED IAW THE BOEING 727 MM 57-41-11 AND 57-41-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002111400107 20021114 00107 NM 2002 11 14 GAIA02148ST 1 20021024 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 580, AND IN BETWEEN STRINGER S24L AND S25L WAS DENTE D. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002111400108 20021114 00108 NM 2002 11 14 GAIA02149ST 1 20021024 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 560, STRINGER S25L WAS DENTED. REPAIR WAS ACCOMPLIS HED IAW BOEING 727 SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002111400109 20021114 00109 NM 2002 11 14 GAIA02150ST 1 20021024 A 5310 DOOR FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE C-1 DOOR CUTOUT AFT RIGHT FRAME HAD A CRACK IN THE SKIN IN TWO P LACES AT STRINGER S26R. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 51-40-2, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 L 7 3 4F A3WE 2002111400110 20021114 00110 NM 2002 11 14 GAIA02151ST 1 20021024 A 5754 SKIN BOEING 727 727225 1384077 NM L/E SLAT CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE RIGHT WING UPPER OUTBOARD LEADING EDGE AT WS 430 HAD A ROW OF FA STENERS WITH CRACKS RUNNING FROM HEAD HOLES AT THE NR 5 SLAT LEADING EDGE. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 5 7-30-3, FIGURE 4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002111400111 20021114 00111 NM 2002 11 14 GAIA02152ST 1 20021024 A 5313 STRINGER BOEING 727 727225 1384077 NM FUSELAGE CHAFED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 936PG 22441 DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE STRINGER AT BS 720E, S19R HAD CHAFE DAMAGE FROM FAIRING AT THE L AP JOINT. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 53-30-3, FIGURE 6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002111400112 20021114 00112 NM 2002 11 14 Q2SA742007 1 20021029 A 3244 2603561 TIRE BOEING 747 747230B 1384889 NM LT MLG BLOWN A Q2SA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 GL 23 742SA 22669 ON TAKEOFF, NR 7 AND 8 TIRES BLEW DAMAGING SURROUNDING SYSTEMS/STRUCTURES AND RESULTING IN REDUCED BRAKING FORCE. PERFO RMED PRELIMINARY INSPECTION AND FOUND EIGHT TOTAL TIRES BLOWN/DEFLATED, LEFT INBOARD FLAP DAMAGED, LEFT OUTBOARD FLAP TO RQUE TUBE BROKE, AT LEAST TWO ELECTRICAL CONDUITS BROKEN/DAMAGED, AND TWO HYDRAULIC LINES RUPTURED. (M) 2 L 7 4 4F A20WE 2003031400023 20030314 00023 WP 2003 3 14 0203739921 1 20021106 A 2720 SWITCH DOUG DC9 DC932 3022066 WP RUDDER OUT OF RIG A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 943N 47647 AT APPROXIMENTLY 118 KNOTS THE FLAP/RUDDER STOP LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND THE LIGHT EXTINGUISHED. ALL OWED BRAKES TO COOL AND RETURNED AIRCRAFT TO GATE AT YYZ. MAINTENANCE REPLACED THE FLAP/RUDDER POSITION SWITCH AND RE-R IGGED THE AUXILIARY RUDDER THROW LIMITER CONTROL VALVE. PERFORMED SYSTEM CHECK AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F A6WE 2002111400113 20021114 00113 NM 2002 11 14 0203786635 1 20021108 A 2610 BATTERY BOEING 747 747227B 1384888 NM DEFECTIVE A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 635US 21682 During cruise an electrical odor emitted from in area of the P6 panel. After a short time the odor dissipated. Aircraft continued to destination and landed without incident. Visually inspected are with no defects found.Probable source of od or was the main battery. The battery and battery charger were replaced. 2 L 7 4 4F A20WE 2002111400114 20021114 00114 SO 2002 11 14 SIMA200229601 1 20021023 A 2750 363100107 ECU EMB 135 EMB135KL 3260302 SO T/E FLAP FAILED A SIMA B EMER. DESCENT F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 803AE 145483 BOS - FLT 4757 - DURING APPROACH WHEN FLAPS WERE SELECTED CREW RECEIVED A FLAP FAIL, FLAP LOW SPEED, AND LOST FLAP INDIC ATION ON EICAS. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENTS. MAINTENANCE REMOVED AND R EPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2002111400115 20021114 00115 EU 2002 11 14 SIMA200230302 1 20021010 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 330AE 340B330 ABI - DURING A MBV INSPECTION, THE LEFT SIDE UPPER FLANGE OF THE LOWER FRAME AT STATION 258 WAS FOUND TO BE CORRODED BEY OND LIMITS. COMPLETELY REMOVED CORROSION BY CUTOUT. FABRICATED AN ANGLE AND SHIMS. REPAIR DONE IAW SAAB 340 SRM (72LK S 3079 REV 40) 53-70-30 PARA 4 FIG 206/207. (M) 2 L 7 2 4T RT A52EU 2002111400116 20021114 00116 WP 2002 11 14 MWEA020680 1 20021111 A 5347 993053839 WEB DOUG DC9 DC981 3022081 WP STA 218-237 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 CUSP WEB STATION 218-237 OF SEAT TRACK NUMBER 4 REQUIRED REPLACEMENT. -- REMOVED AND REPLACED WEB. 2 L 7 2 4F A6WE 2002111400117 20021114 00117 NM 2002 11 14 0203792299 1 20021102 A 3350 BATTERY PACK BOEING 727 727251 138408H NM INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 299US 22153 Emergency escape path lighting inoperative at rows 1-7 as well as main cabin and galley door vertical signs. Maintenance replaced battery pack. Operational tests were satisfactory. 2 L 7 3 4F A3WE 2002111400118 20021114 00118 WP 2002 11 14 0203809852 1 20021110 A 2150 SENSE LINE DOUG DC9 DC951 3022051 WP LOOSE A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 761NC 47709 Cabin continued to climb at approximate rate of 200-300 FPM after level at 35,000 feet. Crew initiated a rapid descent a nd performed COM procedures. Cabin pressure was controllable in manual mode at the lower altitudes. Flight diverted to M EM and landed without incident. Maintenance found a sense line for the right pack heat exchanger airflow disconnected an d resecured it. Pack operation is normal and the aircraft has returned to service. 2 L 7 2 4F RT A6WE 2002111400119 20021114 00119 WP 2002 11 14 0203819875 1 20021111 A 2913 314195 PUMP DOUG DC9 DC951 3022051 WP FAILED A NWAA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 GL 01 784NC 48109 During climb out from MSP the left engine driven hydraulic pump failed. Crew performed COM procedures for pump failure a nd overweight landing. Flight returned and landed uneventfully back at MSP. Maintenance replaced the engine driven pump and filters. Aircraft has been returned to service. 2 L 7 2 4F RT A6WE 2002111400120 20021114 00120 SO 2002 11 14 C2XA02BT075 1 20021113 A 4910 APU EMB 145 EMB145LR 3260212 SO EMPENNAGE ODOR A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 13994 145291 EWR---CO2912, CREW REPORTED, "STRONG FUEL SMELL IN CABIN AFTER APU START." MAINTENANCE STARTED APU IAW EMB145 AMM REFERE NCE 49-10-00. OPS.CHECKED GOOD NOTED NO FUEL SMELL. (AIRCRAFT RETURNED TO SERVICE.) 2 L 7 2 4T RT T00011AT 2002111400121 20021114 00121 EA 2002 11 14 COMA0260643 1 20021112 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 458CA 2178 7613 FLIGHT 5034 FLAPS FAIL CAUTION MESSAGE.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2002111400122 20021114 00122 WP 2002 11 14 MWEA020691 1 20021114 A 5313 59203191 LONGERON DOUG DC9 DC932 3022066 WP STA 520-524 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FORWARD CARGO BAY CORRODED AROUND FASTENERS IN LONGERON 30 STATION 520-524. -- REMOVED AND REPLACED LONGERON SECTION A ND INSTALLED FORWARD AND AFT LONGERON SPLICE. 2 L 7 2 4F A6WE 2002111400123 20021114 00123 WP 2002 11 14 MWEA020692 1 20021114 A 5313 99236893 INTERCOSTAL DOUG DC9 DC932 3022066 WP STA 484-503 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 INTERCOSTAL IN FORWARD BAG PIT HAS CORROSION ON FLANGE AT STATION 484-503 LONGERON 27-28 LEFT. -- FORMED AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2002111400124 20021114 00124 WP 2002 11 14 MWEA020693 1 20021114 A 5310 99101405 DOUBLER DOUG DC9 DC932 3022066 WP CARGO BAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FORWARD CARGO BAY SUBFLOOR CRACKED NEXT TO CARGO DOOR FORWARD HINGE ATTACH POINT. -- FABRICATED AND INSTALLED REPAIR D OUBLER. 2 L 7 2 4F A6WE 2002111400125 20021114 00125 EA 2002 11 14 COMA0260644 1 20021113 A 5210 6003804113 CAM CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 966CA 7132 FLIGHT 5893 CABIN DOOR WARNING MESSAGE.REPLACED THE DOOR INNER HANDLE CAM PLATE. 2 L 7 2 4F RT A21EA 2002111400126 20021114 00126 EA 2002 11 14 COMA0260645 1 20021112 A 3040 WINDOW CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 01 924CA 7026 FLIGHT 5949 LEFT WINDOW HEAT INOP.SWITCHED WIRING TO ALTERNATE HEAT SENSORS. OPERATONAL CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2002111400127 20021114 00127 2002 11 14 AWXA200201118 4 20021113 A 2565 2LA00546901 CONNECTOR AIRBUS 320 A320231 3930325 EU R/H OVERWING IMPROPER PART A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 0 0 66 PHX - EMERGENCY EVACUATION - DURING INSPECTION THE SLIDE DISARM LIGHTS WOULD NOT EXTINGUISH WHEN DISARMING THE L/H AND R /H OVERWING SLIDES. MAINTENANCE DISCOVERED PIN "B" ON THE L/H OVERWING SLIDE CONNECTOR 5WN1 WAS RECESSED, RESEATED PIN " B" ON L/H OVERWING SLIDE CONNECTOR 5WN1. ON THE R/H OVERWING SLIDE MAINTENANCE FOUND PIN "F" RECESSED, AND PIN "U" WAS THE TYPE ON CONNECTOR 2WN2. REMOVED AND REPLACED R/H OVERWING SLIDE CONNECTOR 2WN2, OPERATIONAL CHECK OF SLIDE DISARM LI GHTS WAS GOOD. 2 L 7 2 4F RT A28NM 2002111400128 20021114 00128 NM 2002 11 14 AWXA200201121 1 20021027 A 5315 69434772 CHANNEL BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 0 0 23218 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF AFT CARGO R/H S IDEWALL TO FLOOR SUPPORT STRAP ASSEMBLY BS 767 - 792. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMIT S; REMOVED DAMAGED SUPPORT STRAP BS 767 - 792; FABRICATED A NEW REPLACEMENT SUPPORT STRAP; INSTALLED REPAIR PART IAW B73 7-300 SRM 51-40-02, PG. 11, AND SRM 51-40-05 PG. 1-2, & 4. 2 L 7 2 4F RT A16WE 2002111400129 20021114 00129 SO 2002 11 14 C2XA02IA235 1 20021108 A 3350 20131A BATTERY EMB 145 EMB145ER 3260211 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14939 145030 BNA- WHILE PERFORMING MAINTENANCE THE MECHANIC NOTED THAT THE AISLE PATH EMERGENCY LIGHTS WERE JNOPERATIVE. BNA- MAINT ENANCE REMOVED AND REPLACED THE #2 EMERGENCY LIGHT BATTERY. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002111400130 20021114 00130 SO 2002 11 14 C2XA02IA236 1 20021108 A 3350 20131A BATTERY EMB 145 EMB145ER 3260211 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14939 145030 BNA- WHILE PERFORMING MAINTENANCE THE MECHANIC NOTED THAT THE AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. BNA- MAIN TENANCE REMOVED AND REPLACED THE #3 EMERGENCY BATTERY,PERFORMED A OPERAIO9NAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002111400131 20021114 00131 SO 2002 11 14 C2XA02IA238 1 20021110 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145ER 3260211 SO TAIL INOPERATIVE A C2XA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 27 14933 145018 IAH- FLIGHT 3558, THE CREW NOTED THAT THE RUDDER SYSTEMS #1 & #2 INOPERATIVE, ON DEPARTURE FOR (TYS), THE CREW DECLAIRE D EMERGENCY, AND, PERFORMED AN EMERGENCY DESCENT. THE AIRCRAFT RETURNED TO (IAH), AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE #1 RUDDER SYSTEM PRESSURE SWITCH, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002111500002 20021115 00002 EU 2002 11 15 R7MR35340 1 20020603 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE TORQUE INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 528SF 620 7104 PRESSURE TRANSDUCER, UNIT INOPERATIVE. INCORRECT READINGS, 40 PERCENT TOO HIGH (FLUCTUATING). REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002111500003 20021115 00003 EU 2002 11 15 R7MR35346 1 20020104 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE TORQUE INOPERATIVE B R7MR O OTHER L NO TEST NR NOT REPORTED 1 NM 07 527RM 7111 PRESSURE TRANSDUCER, UNIT INOPERATIVE. INDICATOR SPINS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002111500004 20021115 00004 EU 2002 11 15 R7MR35348 1 20020215 A 7712 G554574 TRANSDUCER BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101600A 41560 NE ENGINE TORQUE INOPERATIVE B R7MR O OTHER L NO TEST NR NOT REPORTED 1 NM 07 527RM 7111 PRESSURE TRANSDUCER, UNIT INOPERATIVE. CAUSES GAUGE TO SPIN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002111500005 20021115 00005 EU 2002 11 15 R7MR35356 1 20020316 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117A4 5626017 EU ENGINE TORQUE INOPERATIVE B R7MR O OTHER L NO TEST NR NOT REPORTED 1 NM 07 586BH 7129 PRESSURE TRANSDUCER, UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2002111500006 20021115 00006 EU 2002 11 15 R7MR35358 1 20020328 A 7712 G554574 TRANSDUCER BOLKMS 117 BK117A4 5626017 EU ENGINE TORQUE INTERMITTENT B R7MR O OTHER L NO TEST NR NOT REPORTED 1 NM 07 586BH 18 7129 PRESSURE TRANSDUCER, UNIT OPERATES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2002111500007 20021115 00007 EU 2002 11 15 R7MR35360 1 20020531 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117A4 5626017 EU ENGINE TORQUE INOPERATIVE B R7MR O OTHER L NO TEST NR NOT REPORTED 1 NM 07 586BH 119 7129 PRESSURE TRANSDUCER, INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2002111500008 20021115 00008 EU 2002 11 15 R7MR35727 1 20020815 A 6210 355A11003000 BLADE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE MAIN ROTOR DELAMINATED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 396LG 415 3336 MAIN ROTOR BLADE HAS DELAMINATION ON TOP TRAILING EDGE APPROXIMATELY 320 MM FROM TIP. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002111500009 20021115 00009 NM 2002 11 15 SROM200200020 1 20021111 A 2121 215201 MOTOR BOEING 737 737205 1384456 NM GASPER FAN INOPERATIVE I SROM O OTHER O OTHER CR CRUISE 1 AL 03 736BP 22031 13386 23465 FLIGHT CREW NOTICED A ELECTRICAL ODOR IN THE CABIN AFTER FLIGHT ATTENDENT ADJUSTED SIDE WALL LIGHTING INTENSITY. CABIN LIGHTING AND GALLEY POWER WERE SWITCHED OFF AND ODOR DIMINISHED. UPON LANDING TECHNICIANS FUNCTIONED CHECKED ALL LIGHTS , GALLEY EQUIPMENT AND PACS, WITH NO ABNORMAL INDICATIONS. GASPER FAN C/B WAS FOUND POPPED. BREAKER WOULD NOT RESET. REPLACED GASPER FAN AND OPS CHECKED NORMAL. 2 L 7 2 4F RT A16WE 2002111500010 20021115 00010 SW 2002 11 15 VH32002F00000 1 20021106 A 3210 E012402 LANDING GEAR GULSTM 690TP 690A 0141722 SW GARRTT TPE331 TPE331* 01514 WP HARTZL HCB3T HCB3T* GL LEFT DAMAGED E VH3A O OTHER E VIBRATION/BUFFET LD LANDING 1 WP 07 722EJ 11175 P06754 BV2525 UPON LANDING TOUCHDOWN, SEVERE SHIMMY. TAXIED CLEAR OF RUNWAY, SHUT DOWN AIRCRAFT. INSPECTED LEFT MAIN GEAR, FOUND DA MAGE. 1 H 7 2 3T 3 T 2A4 E2WE 6 C P15EA 2002111500011 20021115 00011 EA 2002 11 15 W6T2002F00000 2 20021030 A 8530 76220 STUD PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA NR 4 CYLINDER BROKEN E W6TA K NONE O OTHER IN INSP/MAINT 1 NM 03 495SC 318052062 RL82468A NEW STUDS AND THRU BOLTS OF OFF ON FINAL APPROACH, THE RT ENGINE STARTED RUNNING ROUGH FURTHER INVESTIGATION REVEALED TH AT THE NR 4 CYLINDER EXHAUST WAS CRACKED. THIS WAS CRACKED BECAUSE THE NR 4 CYLINDER THRU-BOLTS BROKE WHICH ALLOWED OTH ER HOLD-DOWN STUDS TO BREAK WHICH ALLOWED THE CYLINDER TO PARTIALLY SEPARATE FROM THE CRANKCASE. 1 L 7 2 3O 3 O A20SO E14EA 2002111500012 20021115 00012 SW 2002 11 15 YT2R631366 1 20021015 A 6520 206340103101 SEAL BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL T/R GEARBOX LEAKING B YT2R K NONE K FLUID LOSS IN INSP/MAINT 1 WP 01 2019F 51032 TAILROTOR GEARBOX SEAL, LEAKING UPON INSTALL. 1 G 7 1 3U 3 U H2SW E1GL 2002111500015 20021115 00015 NM 2002 11 15 A6WA200230036 1 20021015 A 6123 311694201 PROBE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE TORQUE FAILED A A6WA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 GL 31 350AD 3050 RT ENGINE TORQUE INDICATION LOST ENROUTE, FOLLOWED BY AUTOFEATHER APPROX 15 MINUTES AFTER TORQUE LOSS. CRUISE POWER TOR QUE APPROX 86 PERCENT NP WHEN FAILURE OCCURRED. ENGINE REMAINED IN FEATHER WITHOUT SHUTTING DOWN ENGINE MAINTENANCE REM OVED AND REPLACE TORQUE PROBE. 2 H 7 2 4T 4 T RT A45NM E20NE 2002111500016 20021115 00016 NM 2002 11 15 A6WA200230037 1 20021020 A 7603 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE POWER LEVER CONTAMINATED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 335LS 3035 PCE116076 UPON ARRIVAL, WHEN CONDITION LEVERS ADVANCE TO MAXIMINUM, LT PROP SPEED WAS APPROXIMATELY 68 PERCENT, LT TORQUE WOULD NO T DECREASE BELOW 60 PERCENT. MAINTENANCE RAN ENGINE TO FULL POWER TO ENSURE PROPER OPERATION. OPS CHECK GOOD. INSPECT ED CONTROL CABLES FOR FULL MOVEMENT AND SECURITY. NO DEFECTS NOTED. FERRIED, MECHANICS FOUND PCU, CSU AND FEA SOLENOID CONNECTOR PLUG COATED IN OIL. CLEANED. 2 H 7 2 4T 4 T RT A45NM E20NE 2002111500017 20021115 00017 EU 2002 11 15 A6WA200260035 1 20021004 A 5751 TAB BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA AILERON DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 DENTS LEFT AILERON TABS X 9 RECEIVED CONCESSION. 2 H 7 4 4F 4 F RT A49EU E6NE 2002111500018 20021115 00018 EU 2002 11 15 A6WA200260036 1 20021004 A 5751 TAB BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA AILERON DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 DENTS RIGHT AILERON INBOARD AND OUTBOARD TABS X 32 RECEIVED CONCESSION. 2 H 7 4 4F 4 F RT A49EU E6NE 2002111500019 20021115 00019 EU 2002 11 15 A6WA200260037 1 20021004 A 5754 TAB BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA LT LE FLAP DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 DENT LEFT FLAP INBOARD TAB X RECEIVED CONCESSION. 2 H 7 4 4F 4 F RT A49EU E6NE 2002111500020 20021115 00020 EU 2002 11 15 A6WA200260038 1 20021004 A 5280 DOOR BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA MLG DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 DENTS LEFT MAIN LANDING GEAR DOOR X 18 RECEIVED CONCESSION. 2 H 7 4 4F 4 F RT A49EU E6NE 2002111500021 20021115 00021 EU 2002 11 15 A6WA200260039 1 20021004 A 5280 DOOR BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA RT MLG DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 DENTS RT MAIN LANDING GEAR X 26 RECEIVED CONCESSION. 2 H 7 4 4F 4 F RT A49EU E6NE 2002111500022 20021115 00022 EU 2002 11 15 A6WA200260040 1 20021004 A 5330 SKIN BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA FUSELAGE DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 DENTS RIGHT FUSELAGE X 4 RECEIVED CONCESSION. 2 H 7 4 4F 4 F RT A49EU E6NE 2002111500023 20021115 00023 EU 2002 11 15 A6WA200260041 1 20021008 A 5753 STRUCTURE BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA TE FLAP DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 RIGHT FLAP INBOARD AND OUTBOARD TABS DENTED, RECEIVED CONCESSION. 2 H 7 4 4F 4 F RT A49EU E6NE 2002111500024 20021115 00024 EU 2002 11 15 A6WA200260042 1 20021008 A 5523 TAB BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA LT ELEVATOR DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 DENTS TO LEFT ELEVATOR AND TABS X 8 RECEIVED CONCESSION. 2 H 7 4 4F 4 F RT A49EU E6NE 2002111500025 20021115 00025 EU 2002 11 15 A6WA200260043 1 20021008 A 5523 TAB BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA ELEVATOR DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 DENTS TO RT ELEVATOR AND TABS X 34 RECEIVED CONCESSION. 2 H 7 4 4F 4 F RT A49EU E6NE 2002111500026 20021115 00026 EU 2002 11 15 A6WA200260044 1 20021010 A 5320 FLOOR SUPPORT BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502* 41580 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 A6WA E3122 CORROSION FOUND ON FLOOR SUPPORT STRUCTURE FRAME 15 - 2.5 INCH PORT OF AIRCRAFT CENTERLINE RIL. 2 H 7 4 4F 4 F RT A49EU E6NE 2002111500027 20021115 00027 EU 2002 11 15 A6WA200260045 1 20021016 A 2750 FLAP BAC 146 146200A 1500266 EU LYC ALF502 ALF502* 41580 EA LEFT BLOCKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 ZERO FLAP LANDING. REF FLAP FAULT WARNING. TOUCHDOWN SPEED, 157. BRAKES APPLIED, 100, BRAKE TEMPS , 470, BRAKE FANS OPE RATING, NORMAL BRAKES WERE APPLIED, 70,000 LBS LANDING WEIGHT. MAINTENANCE FOUND LT SIDE BLOCKED, CLEARED BLOCKED CON DITION WITH BUMP BOX, OP CHECK GOOD. 2 H 7 4 4F 4 F A49EU E6NE 2002111500028 20021115 00028 WP 2002 11 15 0203649852 1 20021004 A 5330 DOUBLER DOUG DC9 DC951 3022051 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9852 47709 During M-ck at ATL base, the aft cargo door internal jamb doubler was found with corrosion. The existing doubler was tri mmed betweeen L25R and L26R on both sides of the Cargo Door. Repaired per EA 98-190717. 2 L 7 2 4F RT A6WE 2002111500029 20021115 00029 WP 2002 11 15 0203659981 1 20021022 A 5510 STABILIZER DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 676MC 47652 Duting Hck in ATL, a .25" crack was found in the upper plate of the horizontal stabilizer center section. Repaired per E A 98-190787. 2 L 7 2 4F RT A6WE 2002111500030 20021115 00030 WP 2002 11 15 0203669869 1 20021102 A 5310 BRACKET DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 778NC 48100 During an Mck in ATL P/N 9957860-6 bracket was found with a .25" long crack. Rpaired per EA 98-190823. 2 L 7 2 4F RT A6WE 2002111500031 20021115 00031 WP 2002 11 15 0203699981 1 20021028 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 994Z 47097 DURING HCK IN ATL, CORROSION WAS FOUND IN THE VERTICLE FLANGE OF THE STATION 200 FLOORBEAM LOWER CAP. THE CORROSION EXTE NDED TO THE LEFT OF STATION X=0 ALL THE WAY TO THE END OF THE PART. REPAIRED PER EA 99-190813. 2 L 7 2 4F A6WE 2002111500032 20021115 00032 WP 2002 11 15 0203719986 1 20021101 A 5240 DOOR DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 986US 47480 During Hck in DHN, a .6" crack was found in the fwd galley service door pan at the #2 door stop. The crack extended from the upper corner of the upper hinge cutout. Repaired per EA 99-191372. 2 L 7 2 4F A6WE 2002111500033 20021115 00033 WP 2002 11 15 0203729984 1 20021025 A 5740 SLAT DOUG DC9 DC932 3022066 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 984US During Shop Visit in ATL, a crack and elongated hole were found on the lower skin of the subject slat at the aft otbd co rner. Repaired per EA 99-190789. 2 L 7 2 4F A6WE 2002111500036 20021115 00036 EU 2002 11 15 N9W2002F00002 1 20020505 A 3320 AL1235490 LIGHT ISRAEL 1121 1121A 0142006 EU GARRTT TFE731 TFE731* 01518 WP CABIN MELTED E N9WA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 11 9WA 407 CREW NOTICED SMOKE AND FUMES IN THE CABIN AND COCKPIT. PILOT ELECTED TO DIVERT FLIGHT TO SUITABLE AIRPORT FOR LANDING. A/C LANDED WITHOUT INCIDENT. REMOVED CABINET AND PANELS AND FOUND LIGHT TUBE AT THE NR 2 RT WINDOW SHORTED AND MELTED. IN ADDITION ASSY WIRES, RECEPTACLES AND ADJACENT WALL PANEL WERE MELTED. END CAP CONNECTOR OF LAMP ASSY HAD COME LOOS E. THIS CAUSED AN EXCESSIVE HEAT CONDITION. NR 2 CABIN LAMP WAS REPLACED WITH NEW LAMP. AIRCRAFT HAS BEEN RETURNED TO SERVICE. 2 M 7 2 4J 4 F A2SW E6WE 2002111500037 20021115 00037 2002 11 15 SIMA200229403 4 20021018 A 2300 7510700766 DISPLAY EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL COCKPIT LIGHTNING STRIKE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 CREW REPORTED A BRIGHT FLASH AT CAPTAINS WINDOW FOLLOWED BY AN ELECTRICAL SMOKE SMELL, LOSS OF NUMBER 4 GENERATOR. NUMB ER 2 COMM, AND FMS SCREEN. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENTS. MAINTENANCE CO MPLIED WITH A LIGHTENING STRIKE INSPECTION. GENERATOR WAS REPLACED. NUMBER 2 ICU WAS REPLACED, WHICH FIXED THE SMOKE S MELL. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002111500038 20021115 00038 NM 2002 11 15 CALA0200549 1 20021113 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39343 23581 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 967, RBL 46. OLD TOP CHORD REPAIR EXISTS FROM LBL 43 TO RBL 43. FLOORBEA M REPAIRED IAW ECRA 5311-01142. TOP CHORD REPLACED FROM LBL 43 TO R/H EXTREMITY AT FRAME. 2 L 7 2 4F RT A16WE 2002111500039 20021115 00039 NM 2002 11 15 CALA0200550 1 20021113 A 5210 SKIN BOEING 777 777224 1385225 NM R-4 DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78001 27577 INSPECTION FOUND AFT LOWER CORNER OF R-4 DOOR SKIN DENTED. THE SKIN WAS REPAIRED IAW SRM 52-10-01, REPAIR 8, FIGURE 202. 2 L 7 2 4F RT T00001SE 2002111500040 20021115 00040 NM 2002 11 15 CALA0200552 1 20021114 A 5330 SKIN BOEING 777 777224 1385225 NM FS 673-679 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78001 27577 INSPECTION FOUND FUSELAGE SKIN DENTED FORWARD OF L-2 DOOR AT FS 673-679 BETWEEN S27L AND S28L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, FIGURE 202, REPAIR 7. A DIP WAS INITIATED TO REINSPECT THE AREA AT 30,000 CYCLES AND REPEAT AT 16,000 CYC LES. 2 L 7 2 4F RT T00001SE 2002111500041 20021115 00041 NM 2002 11 15 CALA0200553 1 20021114 A 5210 SKIN BOEING 777 777224 1385225 NM L-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78001 27577 INSPECTION FOUND A 3/4" CRACK IN SKIN AT FORWARD MID AREA EDGE OF L-2 DOOR. REPAIRED IAW SRM 52-10-01, REPAIR 5. A DIP W AS INITIATED TO REINSPECT THE AREA AT 30,000 CYCLES AND AT 4,000 CYCLE INTERVALS. 2 L 7 2 4F RT T00001SE 2002111500042 20021115 00042 NM 2002 11 15 CALA0200554 1 20021115 A 5320 WEB BOEING 737 737524 1384721 NM STA 344-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14609 27322 INSPECTION FOUND A 2" CRACK IN MAIN DECK WEB AT STA 344-360, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002111500043 20021115 00043 EU 2002 11 15 YENA200228 1 20021114 A 7100 IAE V2527A5 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE A YENA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 15 520JB 10946 1446 10946 Flight #88, ONT to JFK, had fairly strong smell of burnt oil during inter stages of take off and climb out, Smell persis ted and aircraft returned to ONT. Landing weight was aprx 155.500. Touchdown was smooth with minimun vertical speed. Pre liminary report indicate #2 engine has possible #3 bearing problem. Aircraft maintenance Ferry to LGB for #2 Engine chan ge. This SDR is open pending further information. 2 L 7 2 4F 4 F RT A28NM E40NE 2002111500044 20021115 00044 NM 2002 11 15 SWA2002F00000 1 20021016 A 5753 654792327 SPAR BOEING 737 737300 1384610 NM GE CFM56 CFM56* 13802 NE TE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 NM 01 366SW 26577 CRACK WAS FOUND DURING D CHECK VISUAL INSPECTION IN THE BACK SHOP. DISCOVERED THE MAIN SPAR CRACKED IN THE LOWER CHORD/ WEB RADIUS COMMON TO THE OUTBOARD AFT FLAP TRACK ATTACH POINT. THE CIRCUMSTANCES UNDER WHICH IT OCCURED IS UNKNOWN. CO ULD BE FATIGUE OR AN EXCESSIVE FORCE AT THE OUTBOARD AFT FLAP TRACK. 2 L 7 2 4F 4 F RT A16WE E2GL 2002111500045 20021115 00045 CE 2002 11 15 UJ82002F00000 1 20020406 A 3244 178K431 TIRE LEAR 60 60LEAR 5170707 CE MLG FAILED E UJ8A K NONE O OTHER IN INSP/MAINT 1 SO 17 60UJ 007 TIRE, TREAD SEPARATION ON TIRE IS OCCURRING WITH ALARMING FREQUENCY. 102 LANDINGS APPEAR TO BE SLIGHTLY MORE THAN .5000 OF ITS EXPECTED LIFE. 2 L 7 2 4F RT A10CE 2002111500046 20021115 00046 WP 2002 11 15 ABXA020274 1 20021030 A 2170 COALESCER BAG DOUG DC9 DC932 3022066 WP AIR DISTRIBUTION CONTAMINATED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 901AX 47381 VERY STRONG ODOR (MUSTY) WAS PRESENT FROM TAKE-OFF THROUGH FIRST 20 TO 30 MINUTES OF FLIGHT. CLOSING A/C VENTS WOULD DEC REASE THE INTENSITY OF THE ODOR BUT WOULDN'T ELIMINATE IT. REPLACED BOTH WATER SEPARATOR COALESER BAGS IAW DC-9 MM 21-20 -02-2-0001. 2 L 7 2 4F A6WE 2002111500047 20021115 00047 WP 2002 11 15 ABXA020275 1 20021031 A 5250 LATCH DOUG DC9 DC941 302207N WP COCKPIT DOOR OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 COCKPIT DOOR MECHANISM JAMMED. WOULD NOT ALLOW DOOR TO CLOSE OR OPEN. ADJUSTED COCKPIT DOOR LATCH MECHANISM IAW DC-9 AMM 25-32-0. 2 L 7 2 4F A6WE 2002111500048 20021115 00048 WP 2002 11 15 ABXA020276 1 20021029 A 2721 59140665557 ACTUATOR DOUG DC9 DC933F 302207A WP RUDDER CONTROL FAILED A ABXA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 934AX 6754 47462 RUDDER PEDALS WERE STIFF DURING CONTROL CHECK, ON CLIMB OUT OF ICT. CLIMBING TO FL 350, AIRCRAFT STARTED TO YAW AND DUT CH ROLL. DISCONNECTED AUTO PILOT. TURNING OFF YAW DAMPER AND GOING TO MANUAL RUDDER DID NOT STOP YAW/DUTCH ROLL. AIRCRAF T SLOWED AND DESCENDED TO 280 FOR REMAINDER OF FLIGHT. FOUND RUDDER POWER CONTROL ACTUATOR ASSEMBLY BY-PASSING HYDRAULIC FLUID. REPLACED THE CONTROL ACTUATOR ASSEMBLY IAW DC-9 AMM 27-20-06-4-0002. 2 L 7 2 4F A6WE 2002111500049 20021115 00049 NM 2002 11 15 ABXA020277 1 20021102 A 5753 BACB30LE BOLT BOEING 767 767200 1385120 NM LT FLAP BEAM MISINSTALLED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 773AX 22788 WHILE INSPECTING THE OUTBOARD SUPPORT BEAM FOR THE LEFT FLAP, FOR AD2002-16-05, FOUND GAP AT FORWARD ATTACH BOLT. INSTAL LED BOLT IAW EA27510002-002. 2 L 7 2 4F RT A1NM 2002111500050 20021115 00050 WP 2002 11 15 ABXA020278 1 20021030 A 2913 623337 PUMP DOUG DC8 DC863F 302198F WP HYD SYSTEM DEFECTIVE A ABXA O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 811AX 5960 46113 MANUAL REVERSION LIGHTS CAME ON DURING FINAL APPROACH. RAN LOSS OF HYDRAULIC PROCEDURES. REPLACED BOTH LT AND RT ENGINE DRIVEN HYDRAULIC PUMPS IAW DC-8 MM 29-10-12-02 AND 29-10-12. SERVICED SYSTEM IAW DC-8 AMM 12-00. LEAK AND OPS CHECKED GO OD. 2 L 7 4 4F 4A25 2002111500051 20021115 00051 WP 2002 11 15 ABXA020279 1 20021031 A 3350 5708458503 BATTERY DOUG DC8 DC861 3021952 WP CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 611 46032 EMERGENCY EXIT LIGHTS WERE VERY DIM. REPLACED EMERGENCY LIGHT BATTERY RACK ASSEMBLY AND TESTED GOOD IAW DC-8 AMM 33-50-0 1-2. 2 L 7 4 4F 4A25 2002111500052 20021115 00052 WP 2002 11 15 ABXA020280 1 20021102 A 7830 5958782503 LINK DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE THRUST REVERSER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 4191 47494 676198 WHILE COMPLYING WITH AD 96-10-11, FOUND CRACK INDICATION ON UPPER LEFT THRUST REVERSER DRIVER LINK. INSTALLED SERVICEABL E DRIVER LINK IAW DC-9 MM 78-31-05-2-0001. 2 L 7 2 4F 4 F A6WE E2EA 2002111500053 20021115 00053 WP 2002 11 15 ABXA020282 1 20021023 A 5320 99105035 WEB DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 CRACK IN LT CUSP WEB AT FS 1039 AND LONGERON 18. REPAIRED CUSP IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002111500054 20021115 00054 WP 2002 11 15 ABXA020283 1 20021024 A 5310 995773925 SHEAR TIE DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 SHEAR TIES CRACKED ABOVE AND BELOW LONGERON 15 LEFT AT FS 1024. REPLACED CRACKED SECTION IAW DC-9 SRM 51-30-2 AND 51-30- 5. 2 L 7 2 4F A6WE 2002111500055 20021115 00055 NM 2002 11 15 ABXA020284 1 20021002 A 5753 113T2342 FITTING BOEING 767 767200 1385120 NM TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 LT WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE FITTING ASSEMBLY BEARING BORE, HAD SURFACE CORROSION. THE CORROSION WA S FOUND ON THE SURFACE OF THE BORE, WHERE BEARING INSTALLS. REPAIRED AREA IAW REA B657-44910MR. 2 L 7 2 4F RT A1NM 2002111500056 20021115 00056 NM 2002 11 15 ABXA020286 1 20020927 A 5711 113T222310 SPAR BOEING 767 767200 1385120 NM RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 RT WING INBOARD TRAILING EDGE MAIN FLAP MID SPAR UPPER FORWARD CHORD HAD CORROSION, WS 177 - 186 AND BETWEEN WS 252 - 26 1. REPAIRED AREA IAW REA B756-44900MR. 2 L 7 2 4F RT A1NM 2002111500057 20021115 00057 NM 2002 11 15 ABXA020287 1 20020930 A 5711 113T22217 SPAR BOEING 767 767200 1385120 NM LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 LT WING INBOARD TRAILING EDGE MAIN FLAP FRONT SPAR LOWER CHORD VERTICAL FLANGE BETWEEN FS 286 - 290, FOUND CORROSION. RE PAIRED AREA IAW REA B657-44906MR. 2 L 7 2 4F RT A1NM 2002111500058 20021115 00058 WP 2002 11 15 ABXA020290 1 20021002 A 5315 FLOORBEAM DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 CORROSION FOUND ON NOSE LANDING GEAR WELL HORIZONTAL PRESSURE PANEL, BETWEEN FS 12 TO FS 27. ALSO FOUND CORROSION ON FLO ORBEAM LOWER FLANGE AT FS 12, BUTT LINE '0'. REPAIRED AREA IAW REA 853-41975MR. 2 L 7 4 4F 4A25 2002111500059 20021115 00059 WP 2002 11 15 ABXA020301 1 20021020 A 5315 991224355 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 FLOORBEAM WAS SEVERLY EXFOLIATED AT LEFT PYLON BULKHEAD, BUTT LINE 40 LEFT. INSTALLED 'J' CHANNEL AND AIR GRILL AT STA. 870 - 965. INSTALLED SEAT TRACK, STA. 908 - 965, BUTT LINE 44, IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 2002111500060 20021115 00060 WP 2002 11 15 ABXA020302 1 20021022 A 5300 9911531 WINDOW FRAME DOUG DC9 DC932 3022066 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 HFEC CRACK INDICATION AT WINDOW CUTOUT 14 RIGHT, 1/2 INCHES FROM UPPER FORWARD CORNER EDGE 1/4" LONG. REPAIRED AREA IAW REA D953-45678-MR. 2 L 7 2 4F A6WE 2002111500061 20021115 00061 WP 2002 11 15 ABXA020303 1 20021022 A 5310 99155872 WINDOW FRAME DOUG DC9 DC932 3022066 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 HFEC CRACK INDICATION AT WINDOW 21 RIGHT, 1/8 INCH FROM UPPER AFT EDGE, 3/16 INCH LONG. REPAIRED AREA IAW REA D953-45696 -MR. 2 L 7 2 4F A6WE 2002111500062 20021115 00062 WP 2002 11 15 ABXA020304 1 20021030 A 5710 9919474500 STRUCTURE DOUG DC9 DC932 3022066 WP RT TE WING WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 TRAILING EDGE, WING STA. 161, UPPER SURFACE HAD EXCESSIVE WEAR. REPLACED RIB IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002111500063 20021115 00063 WP 2002 11 15 ABXA020305 1 20021112 A 2752 37741721 ACTUATOR DOUG DC8 DC863F 302198F WP RT WING BROKEN A ABXA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 GL 23 811AX 46113 HYD QTY LOSS ON LANDING. MAINTENACE FOUND THE RT INBOARD FLAP ACTUATOR CRANK ASSEMBLY BROKEN ALONG WITH A BROKEN HYD LIN E TO THE ACTUATOR AND ASSOCIATED ATTACHING HARDWARE BROKEN. OPEN: CORRECTIVE ACTION IS NOT COMPLETE. 2 L 7 4 4F 4A25 2002111500064 20021115 00064 WP 2002 11 15 ABXA020306 1 20021110 A 3260 WARNING SYSTEM DOUG DC8 DC863F 302198F WP MLG MALFUNCTIONED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 811AX 46113 DURING CLIMB, AFTER GEAR UPLATCH CHECK, AIRCRAFT HAD LIGHT TURBULANCE. THE RED GEAR UNSAFE LIGHT CAME ON CAUSED BY THE RT MAIN GEAR DOOR UPLATCH LIGHT ILLUMINATED. RECYCLED GEAR TWICE BEFORE LIGHT WENT OUT. PERFORMED ADJUSTMENT ON UPLATCH. OPS CHECKED UPLATCH AND LIGHTS OPS CHECKED GOOD IAW DC-8 MM 32-31-05. 2 L 7 4 4F 4A25 2002111500065 20021115 00065 2002 11 15 ABXA020307 4 20021108 A 2210 2586689211ABX1 CONTROLLER DOUG DC9 DC941 302207N WP AUTOPILOT MALFUNCTIONED A ABXA O OTHER O OTHER CR CRUISE 1 GL 23 952AX 703 47615 ELEVATOR OSCILLATES VIOLENTLY WHEN AUTO PILOT WAS ENGAGED. COULD NOT DUPLICATE. REPLACED THE AUTO PILOT CONTROLLER IAW DC9 M.M. 22-10-00-5. AUTO PILOT SYSTEM OPS CHECK GOOD. 2 L 7 2 4F A6WE 2002111500066 20021115 00066 WP 2002 11 15 ABXA020308 1 20021112 A 2510 5641031537ABX1 SEAT DOUG DC8 DC863F 302198F WP COCKPIT DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 584 45927 FIRST OFFICER'S SEAT SLIPPED BACKWARDS TWICE. FORE AND AFT POSITION. PIN DID NOT DROP IN PLACE. MUST ENSURE SEAT IS LOCK ED. REPLACED FIRST OFFICER'S SEAT IAW DC-8 AMM 25-11-01-2. 2 L 7 4 4F 4A25 2002111500068 20021115 00068 WP 2002 11 15 ARWA20020916 1 20020930 A 7920 LINE DOUG DC8 DC863F 302198F WP COMPRESSOR BRG LEAKING A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 441J 45988 CLIMB FL 270 NR 2 ENGINE OIL PRESSURE FLUCTUATED BELOW 35 PSI, OIL PRESS LIGHT CAME ON, OIL TEMPERATURE WENT UP. FOLLOWE D ENGINE SHUT DOWN PROCEDURES. 15 PSI OIL PRESS FOR 30 MINUTES. AIRCRAFT LANDED OVERWEIGHT WITHOUT INCIDENT. INSPECTED N R 2 ENGINE FOR EVIDENCE OF OIL LEAK, FOUND BOTH SEALS DAMAGED BETWEEN MAIN OIL FILTER TO COMPRESSOR INTERMEDIATE BEARING TUBE. REMOVED AND REPLACED TUBE ASSY AND SEALS AS REQUIRED IAW MM 79-20-6, OPS CK NORMAL IAW 71-00 NO LEAKS FOUND. ALSO INSPECTED MAIN OIL FILTER, NO METAL PARTICLES FOUND, REMOVED AND REPLACED MAIN OIL FILTER IAW DC8 MM 79-20-7, NO DEFECT S NOTED. SERVICE OIL TANK IAW DC8 MM 12-20-1. PERFORMED OVERWEIGHT LANDING INSPECTION IAW ARROW AIR DC8 MM VOL1 PAGES 5- 2 L 7 4 4F 4A25 2002111500069 20021115 00069 WP 2002 11 15 ARWA20021001 1 20021006 A 2612 D5030 FIRE DETECTOR DOUG DC8 DC863F 302198F WP NR 4 ENGINE MALFUNCTIONED A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 19 441J 45988 NR 4 ENGINE FIRE WARNING ILLUMINATED IN FLIGHT. OVERWEIGHT LANDING AT 277.0 LBS PERFORMED. REMOVED AND REPLACED NR 4 FIRE SENSOR ON BURNED SECTION OF THE ENGINE IAW MM 26-10-1. ALSO REWIRED FROM PL-1341 CONNECTOR TO PL- 1368, PL-1367 C ONNECTOR AND REPLACED CONNECTORS PL-1368 AND PL-1367. NEEDS OPS CHECK. ACCOMPLISHED SPECIAL STRUCTURAL "A" INSPECTION IA W ARROW AIR DC-8 MM, VOLUME I, 60 SERIES PAGES 5-4-8 TO 5-4-16 NO VISUAL DEFECTS NOTED. REMOVED AND REPLACED NR 4 FIRE D ETECTOR SENSOR UPPER FORWARD IAW 26-10-1. OPS CHECKED NORMAL ON GROUND. SYSTEM ENGINE TEST NORMAL IAW MM 2-6-10. 2 L 7 4 4F 4A25 2002111500070 20021115 00070 2002 11 15 ARWA20021003 4 20021008 A 3414 A4144110024 INDICATOR DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE STICKING A ARWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 906R 46087 ON TAKEOFF ROLL OUT OF MIAMI, FIRST OFFICERS AIRSPEED INDICATOR STUCK AT 70 KNOTS. CAPTAINS INDICATOR 95 KNOTS. ABORTE D TAKEOFF, RETURNED TO RAMP FOR CORRECTIVE ACTION. REMOVED & REPLACE WITH NEW PART, FIRST OFFICERS AIRSPEED INDICATOR. ALL WORK ACCOMPLISHED IAW MFG. RECOMMENDED MAINTENANCE PROCEDURES 34-12-0. PITOT STATIC CHECK OF SYSTEM AND SYSTEM TES T CHECKED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2002111500071 20021115 00071 WP 2002 11 15 ARWA20021005 1 20021010 A 3260 CONNECTOR DOUG DC8 DC863 302198A WP MLG UPLOCK FAILED A ARWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 345JW 46042 OUT OF MIA DURING CLIMB OUT, GEAR NOT LATCHED LIGHT ILLUMINATED AFTER UPLATCH CHECK. PERFORMED CHECKLIST, LIGHT STAYED ON. RETURNED TO MIA. TROUBLESHOOT RETRACT SYSTEM AND FOUND CONNECTOR TO UPLATCH SWITCH BAD. REMOVED AND REPLACED CON NECTOR, RECONNECT UPLATCH SWITCH, PERFORMED LANDING RETRACTION AND TEST IAW MM 32-22-1, ALL SYSTEMS AND INDICAITON CHECK ED NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002111500072 20021115 00072 EA 2002 11 15 COMA0260646 1 20021111 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 915CA 13546 7013 FLIGHT 5503 GEAR DISAGREE - NLG TOOK 60 SECOND TO DOWN LOCK.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002111500073 20021115 00073 EU 2002 11 15 0203823220 1 20021107 A 5330 SKIN AIRBUS 320 A320211 3930320 EU CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 320US 213 During "M" check found corrosion on fuselage skin at frame 65 between Stringers 30R and 31R. Repaired per EA 32-191301. 2 L 7 2 4F RT A28NM 2002111500074 20021115 00074 WP 2002 11 15 0203831230 1 20021028 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 230NW 46552 DURING "H" CHECK FOUND CRACK IN FLOORBEAM AT BS 575 RBL 101. REPAIRED PER EA 12-162234. 2 L 7 3 4F A22WE 2002111500075 20021115 00075 EU 2002 11 15 0203843220 1 20021107 A 5347 SEAT TRACK AIRBUS 320 A320211 3930320 EU CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 320US 213 During "M"check found corrosion on seat track at BS 1292 on frame 54 plus 20" and frame 52 plus 14". Repaired per EA32-1 92349. 2 L 7 2 4F RT A28NM 2002111500076 20021115 00076 NM 2002 11 15 0203856627 1 20021019 A 5311 FRAME BOEING 747 747251B 1384892 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 627US 21709 During "H" check found cracks in frame at BS 2231 STR 26L. Repaired per EA 66-193010. 2 L 7 4 4F A20WE 2002111500078 20021115 00078 NM 2002 11 15 UPS02239906 1 20021017 A 5300 65C232314 FITTING BOEING 727 72725C 138400H NM BS 870 R/H CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C&SI WHILE CARRYING OUT NDT ON R/H 870 FITTING CRACKS WERE FOUND IN 3 FAS TENER HOLES IN ROW 3, 1ST HOLE FROM BOTTOM AND 3RD & 4TH HOLES FROM BOTTOM R/H 870 FITTING REPLACED IAW EO B727-5310-3057 & DRAWING 65C13724 2 L 7 3 4F A3WE 2002111500079 20021115 00079 NM 2002 11 15 UPS02239907 1 20021018 A 5753 65192086 FLAP TRACK BOEING 727 72725C 138400H NM FWD ATTACH LUG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C+SI #7 FLAP TRACK HAS SURFACE CORROSION ON THE I/B FWD ATTACH LUG. SURFA CE CORROSION ALSO FOUND ON THE FWD ATTACH PAD AND ON THE ON THE I/B FACE OF THE WING ATTACH FITTING. REPAIR CARRIED OUT IAW SMRO EO 20025507. REF. UPS ENGINEERING FILE N O. 727-57-20078. NOTE THAT POST HEAT TREATMENT, A CRACK WAS FOUND AN D THE FLAP TRACK WAS REPLAC ED. REF. NRC 605735. 2 L 7 3 4F A3WE 2002111500080 20021115 00080 NM 2002 11 15 UPS02239909 1 20021021 A 2760 BRACKET BOEING 727 72725C 138400H NM NO.2 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C&SI NO. 2 SPOILER SUPPORT CASTING, I/B REAR SPAR ATTACH BRACKET IS CRACK ED AT LWR ATTACH HOLE BRAC KET REPLACED IAW SB 57-84 & DRAWING 65-17351 2 L 7 3 4F A3WE 2002111500081 20021115 00081 NM 2002 11 15 UPS02239911 1 20021022 A 2760 BRACKET BOEING 727 72725C 138400H NM NO. 13 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C&SI NO. 13 SPOILER SUPPORT CASTING, I/B SUPPORT BRACKET IS CRACKED AT LW R ATTACH HOLE BRACKET REPL ACED IAW SB 57-84 & DRAWING 65-17351 2 L 7 3 4F A3WE 2002111500082 20021115 00082 EU 2002 11 15 02318333 1 20021114 A 3350 1317 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU EXTERIOR INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 333UE 41101 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT FWD. EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE LAMP IN THE L/H FWD EXTERIOR EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY A ND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002111500083 20021115 00083 EU 2002 11 15 RAIA00211314 1 20021108 A 3610 MJ337187 GASKET JETAIR JETSTM JETSTM4101 1500501 EU LEAKING A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 570HK 41089 5538-STL- RIGHT ENGINE DID NOT MAKE TORQUE, MAINTENANCE REMOVED AND REPLACED A GASKET IN THE HP BLEED LINE, OPS CK OK. 2 L 7 2 4T RT A41NM 2002111500084 20021115 00084 GL 2002 11 15 RAIA00211315 2 20021111 A 7421 CH318981 IGNITER EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 807HK 145119 310131 5251-PIT- DURING #1 ENGINE START ATTEMPT ENGINE WOULD ROTATE BUT WOULD NOT LIGHT-OFF. MAINTENANCE REMOVED AND REPLACED T HE "A" IGNITER AND DEFERRED "B" IGNITER, OPS CK OK. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002111500085 20021115 00085 EU 2002 11 15 RAIA00211317 1 20021113 A 2910 AS11706V143 HYDRAULIC LINE AEROSP ATR72 ATR72202 8680940 EU LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 722TE 220 5585-STL- GREEN HYDRAULIC SYSTEM FAILURE. MAINTENANCE REMOVED AND REPLACED GREEN HYDRAULIC SYSTEM PRESSURE LINE, LEAK AN D OPS CK OK. 2 H 7 2 4T RT A53EU 2002111600001 20021116 00001 EU 2002 11 16 C2XA02IA240 1 20021114 A 3230 1005383Y00 CONTROL VALVE AEROSP ATR42 ATR42320 8680930 EU LT.MLG W/W INOPERATIVE A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 93840 271 IAH- FLIGHT 3677, THE CREW NOTED THAT THE GEAR WOULD NOT RETRACT. IAH- MAINTENANCE REMOVED AND REPLACED THE LANDING G EAR CONTROL VALVE, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 H 7 2 4T RT A53EU 2002111700001 20021117 00001 SO 2002 11 17 C2XA02SH127 1 20021116 A 5300 14528737001 STRINGER EMB 145 EMB145LR 3260212 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13914 145430 SHV-DURING C CHECK 19L STRINGER'S T REINFORCEMENT WAS FOUND TO HAVE A GOUGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOV ED DAMAGE AND REPAIRED AFFECTED T REINFORCEMENT IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVIC E. 2 L 7 2 4T RT T00011AT 2002111700002 20021117 00002 SO 2002 11 17 C2XA02SH128 1 20021117 A 5300 14547494003 FIREWALL EMB 145 EMB145LR 3260212 SO APU FIREWALL CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13914 145430 SHV- DURING C CHECK APU FIREWALL WAS FOUND TO HAVE A CRACK AT TOP 2 RIVETS OF R/H VERTICAL REINFORCEMENT. MAINTENANCE S TOP DRILLED CRACK AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RE TURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002111800001 20021118 00001 NM 2002 11 18 ABXA020295 1 20021001 A 5300 1435106025 CAP BOEING 767 767200 1385120 NM FWD CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 FORWARD CARGO LOWER LOBE, STATION 522, RIGHT BUTT LINE 25, DEEP CORROSION ON UPPER CAP. REPLACED CAP IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 2002111800002 20021118 00002 NM 2002 11 18 ABXA020296 1 20021008 A 5300 143T10601 CAP BOEING 767 767200 1385120 NM FWD CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 FORWARD CARGO LOWER LOBE, STATION 676, DEEP CORROSION ON UPPER CAP AT LEFT BUTT LINE 20. REPLACED CAP IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 2002111800003 20021118 00003 NM 2002 11 18 ABXA020298 1 20020923 A 5300 451T250440 FLOOR PANEL BOEING 767 767200 1385120 NM FWD CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 FORWARD CARGO LOWER LOBE, STATIONS BETWEEN 544 - 610, FROM RIGHT BUTT LINE 10, LEFT BUTT LINE 10, CORRODED SHEAR FLOOR P ANEL. REPLACED PANEL IAW N.R.C. LT 135 AND SRM. 2 L 7 2 4F RT A1NM 2002111800004 20021118 00004 NM 2002 11 18 ABXA020309 1 20021107 A 5400 313T13809 WEB BOEING 767 767200 1385120 NM #1 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 #1 ENGINE STRUT AFT FAIRING SPAR WEB, FOUND ONE CRACK ON STIFFENER (P/N 313T1380-15), AND FOUR CRACKS ON WEB (P/N 313T13 80-9). REPAIRED STRUT AFT FAIRING IAW REA B654-44936-MR. 2 L 7 2 4F RT A1NM 2002111800005 20021118 00005 WP 2002 11 18 ARWA20021008 1 20021023 A 3240 FUSE DOUG DC8 DC863F 302198F WP BRAKE ASSY MELTED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 906R 46087 DURING POST FLIGHT INSPECTION THE FOLLOWING WAS FOUND: NR 3, 4 & 8 MWA THERMAL FUSE MELTED; NR 7 MWA DUE CHANGE FROM S TRESS BEYOND LIMITS. FOUND CRACK AT NR 3 & 4 BRAKE ASSY. DURING MWA; FOUND NR 8 BRAKE ASSY. SEVERLY OVERHEATED AT MWA. FOUND NR 7 & 6 BRAKE NOT OPERATING. REMOVED AND REPLACED NR 3, 4 AND 8 MWA IAW DC8 MM 32-40-1. REMOVED AND REPLACED NR 7 MWA IAW DC8 MM 32-40-1. REMOVED AND REPLACED NR 3, 4 AND 8 BRAKE ASSY. IAW DC8 MM 32-42-1. REMOVED AND REPLACED R H OUTBD ANTISKID VALUE IAW MM 32-43-3 LEAK CHECK OK OPS CHECK OK IAW DC8 MM 32-43-0. REMOVED AND REPLACED ANTISKID CONT ROL BOX IAW MM 32-43-0. ACCOMPLISHED COMPLETE ANTISKID TEST OK IAW 32-43-0 2 L 7 4 4F 4A25 2002111800006 20021118 00006 WP 2002 11 18 ARWA20021101 1 20021101 A 5320 ANGLE DOUG DC8 DC861 3021952 WP RT MLG WW CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 30UA 46159 DURING "B" CHECK THE FOLLOWING WAS FOUND; CORROSION IN ANGLE IN RT WHEEL WELL UPPER FORWARD AREA AT STA 857 AND CW STA. 46. CUT OUT CORRODED AREA, TREATED AND PRIMED AREA. FABRICATED ANGLE AND INSTALLED FASTENERS AND FABRICATED SPLICE A NGLE AND INSTALLED AS PER REF A&S 11464C DRAWING OK TO CLOSE CENTER FUEL TANK; CLOSED TANK PLATES AS PER MM 28-10-1 AND RESEALED; INSTALLED FLOOR PANELS AND PRESSURE PANEL. PRESSURIZED A/C IAW STC ST 466CH. NO LEAKS NOTED. 2 L 7 4 4F 4A25 2002111800007 20021118 00007 WP 2002 11 18 ARWA20021102 1 20021107 A 7933 WA5296051 HEAT EXCHANGER DOUG DC8 DC862 3021970 WP FUEL/OIL FAILED A ARWA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 19 802BN 45909 NR 1 ENGINE OIL TEMPERATURE INDICATED 140 DEGREES FOR 15 MINUTES; THEN WENT TO 150 DEGREES THROTTLE IDLE, ALL OTHER PARA METERS NORMAL, PERFORMED IN FLIGHT ENGINE SHUTDOWN CHECKLIST. WITH NR 1 ENGINE SHUTDOWN, OIL PRESSURE AT 20 PSI AND TEM PERATURE 60 DEGREES WHILE WINDMILLING 0700. REMOVED AND REPLACED FOWARD OIL HEAT EXCHANGER NR 1 ENGINE IAW MM 73-11-0. ACCOMPLISHED ENGINE RUN IAW DC-8 MM 71-00. OPS AND LEAK CHECKED OK. 2 L 7 4 4F 4A25 2002111800008 20021118 00008 2002 11 18 ARWA20021103 4 20021107 A 3422 25883025 GYRO DOUG DC8 DC863 302198A WP COCKPIT FAILED A ARWA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 441J 46042 FIRST OFFICER'S COMPASS FLAG IN VIEW; FIRST OFFICER'S HORIZONTAL INDICATOR (HSI) CAPTAIN'S RADIO MAGNETIC INDICATOR (RMI ). REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO IAW MM 34-21-1. ALSO REMOVED AND REPLACED CIRCUIT BREAKER 2 AMP IAW MM 2 0-50-1. PERFORMED OPS CHECKED IIASW MM 34-21-0 FOUND NORMAL. 2 L 7 4 4F 4A25 2002111800009 20021118 00009 WP 2002 11 18 ARWA20021104 1 20021108 A 3230 4771392501 PIN DOUG DC8 DC862 3021970 WP RT MLG BROKEN A ARWA O OTHER O OTHER AP APPROACH 1 SO 19 8969U 8954 8954 46070 ON GEAR EXTENSION RIGHT HAND MAIN LANDING GEAR DROPPED DOWN WITH A LOUD BANG. FOUND RT MAIN LANDING GEAR CYLINDER RETR ACT PIN BROKEN. REMOVED RT MAIN LANDING GEAR. ROUTED TO AAR LANDING GEAR SERVICES FOR REPAIRS. REPAIRED PER DC8 OHM T APE REVISION 46, DATE 12/01/73; REFER TO AAR LGS WORK STATEMENT TRACKING NUMBER 413552 FOR WORKSCOPE.SB 32-102 ACCOMPLIS HED. REINSTALLED RT MAIN LANDING GEAR IAW ARROW AIR DC8 MM VOL.I, JOB CARD 32-05, PAGES 5-50-113 THRU 5-50-118. OPS CHE CK FOUND NORMAL IAW DC8 MM 32-30-00. 2 L 7 4 4F 4A25 2002111800010 20021118 00010 2002 11 18 ARWA20021105 4 20021113 A 3431 5222450115 RECEIVER DOUG DC8 DC862 3021970 WP VOR SYSTEM INOPERATIVE A ARWA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 19 802BN 45909 NR 2 VHF FIRST OFFICER SIDE COURSE DEVIATION INDICATOR INOPERATIVE, RETURNED TO MIAMI. REMOVED & REPLACED NR 2 VOR INST RUMENT LANDING SYSTEM RECEIVER. SYSTEM OPERATIONS NORMAL IAW MM 34-52-0. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002111800011 20021118 00011 NM 2002 11 18 AWXA200200582 1 20020705 A 2433 3111364601 TRU BOEING 737 7373Q8 1384670 NM NR 1 ARCED A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 28 327AW 23507 SNA - BURNING ODOR - FLT 0137 - EN ROUTE FROM LAS TO SNA AN ELECTRICAL AND RUBBER BURNING ODOR WAS OBSERVED IN THE COCKP IT AND CABIN. MAINTENANCE TROUBLESHOT AND FOUND THE NR 1 TRU CIRCUIT BREAKER POPPED ON THE P-6 PANEL, AND A BURNED ELECT RICAL ODOR COMING FROM THE NR 1 TRU ASSY IN THE E/E BAY. MAINTENANCE REMOVED AND REPLACED THE NR 1 TRU AND PERFORMED AN OPS CHECK IAW BMM 24-21-31, THE CHECK WAS GOOD. VENDOR BENCH TEST OF TRU AND CONFIRMED FAILURE OF UNIT, ELECTRICAL AR CING OCCURRED DURING POWER UP ON BENCH STAND. ARCING OCCURRED AS INPUT POWER WAS SLOWLY INCREASING AND DUE TO TRANSFORME R T1 BREAKING DOWN. WHEN UNIT WAS DISASSEMBLED CAPACITOR C1 WAS ALSO FOUND WITH THE END CHARED. REPLACED THE T1 TRANSFO 2 L 7 2 4F RT A16WE 2002111800015 20021118 00015 2002 11 18 AWXA200200782 4 20020819 A 3417 4062677101 CIRCUIT BOARD HONEYWELL BOEING 737 737277 1384570 NM ADC BURNED OUT A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 188AW G1172 22655 PHX - AIR TURN BACK - FLT 0620 - ON TAKEOFF FROM PHX EN ROUTE TO OAK FIRST OFFICERS AIRSPEED INDICATOR FROZE AT 60 KTS, REMAINED AT 60 KTS AFTER TAKEOFF, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE TROUBLESHOT AND REPLA CED THE NR 2 AIR DATA COMPUTER, OPERATIONAL CHECK WAS GOOD IAW BMM 34-12-11. VENDOR BENCH TEST OF AIR DATA COMPUTER CO NFIRMED FAILURE OF UNIT. UNIT WAS DISASSEMBLED AND INSPECTION FOUND THE A-4 CIRCUIT BOARD HAD BURNED COMPONENTS AND INTE RIOR OF UNIT HIGHLY CONTAMINATED BY DUST, DIRT, AND LIQUID. THE REASON THIS UNIT FAILED WAS DUE TO COMPONENTS ON THE A-4 CIRCUIT BOARD SHORTED CAUSING A CURRENT DRAW THROUGH RESISTOR R1. CAPACITORS IN THE UNITS POWER SUPPLY ALSO SHOWED EVID 2 L 7 2 4F RT A16WE 2002111800016 20021118 00016 2002 11 18 AWXA200200869 4 20020907 A 3416 4043165 ALTIMETER BOEING 757 757225 1384959 NM COCKPIT BROKEN A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 913AW 22207 PHX - ABORTED TAKEOFF - FLT 0085 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR BWI THE CAPTAINS ALTIMETER OFF FLAG WAS IN VIEW, NO FLAG IN STANDBY ALTIMETER, FLAG APPEARED AT 90 KTS AND DISAPPEARED AT 80 KTS. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE COULD NOT DUPLICATE PROBLEM, REPLACED CAPTAINS ALTIMETER IAW BMM 34-13-01, OPERATIONAL AND BITE CHECK WAS GO OD. VENDOR TEARDOWN OF ALTIMETER CONFIRMED FAILURE OF UNIT FINDING "OFF FLAG IN VIEW" WAS DUE TO A BROKEN COUNTER, REP LACED COUNTER (PART INFORMATION PROVIDED IN SECTION 5.). DURING TEARDOWN OF UNIT THE DC MOTOR AND 9 EACH SCREWS WERE AL SO FOUND WORN, REPLACED DEFECTIVE PARTS. UNIT WAS CALIBRATED, FUNCTIONAL TESTED, AND RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2002111800018 20021118 00018 NE 2002 11 18 AWXA200200900 2 20020917 A 7530 AC044798 SEAL DUNLOP BOEING 757 7572S7 1384962 NM RROYCE RB211 RB211535E4 54555 NE BLEED SOLENOID CONTAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW HS061 23568 EXHAUST DAMAGE - DURING WALK AROUND INSPECTION A LARGE SECTION OF HONEYCOMB FOUND MISSING AT RT ENGINE LT COWLING HEAT D AMAGE TO NR 2 ENGINE C-DUCT WAS DUE TO DEFECTIVE HIGH PRESSURE SOLENOID BLEED VALVE. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE LT HIGH PRESSURE BLEED VALVE ON BOTH THE LT AND RT BLEED SOLENOIDS. NR 2 ENGINE INBOARD C-DUCT WAS REPLACED. I P & HP COMPRESSOR AIRFLOW CONTROL TEST CHECKED GOOD. VENDOR BENCH TEST OF BLEED SOLENOID RELIEF HP3 VALVE FAILED FUCNTIO NAL TEST AND INLET / EXHAUST VALVE LEAKAGE TEST AT 15 LBS. UNIT WAS DISASSEMBLED AND FOUND TO BE CONTAMINATED WITH A CAR BON MATERIAL. TRIPLE SEALS ALSO CONTAMINATED WITH AN ABRADABLE MATERIAL, AND THE RELIEF VALVE SEALING SURFACE WAS DAMAGE 2 L 7 2 4F 4 F RT A2NM E12EU 2002111800019 20021118 00019 WP 2002 11 18 MWEA020697 1 20021115 A 5542 59570933 RUDDER DOUG DC9 DC981 3022081 WP ZR10 - ZR36 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 RUDDER LOWER LEADING EDGE PANEL DENTED FROM ZR10-ZR36. -- REPAIRED IAW BOEING TELEX MWX-MKE-02-00190H DATED 9/19/02. 2 L 7 2 4F A6WE 2002111800020 20021118 00020 WP 2002 11 18 MWEA020694 1 20021115 A 5753 HINGE DOUG DC9 DC981 3022081 WP FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 LEFT OUTBOARD FLAP INBOARD FORWARD HINGE HAS CORROSION IN STUD HOLE. -- REMOVED CORROSION. 2 L 7 2 4F A6WE 2002111800021 20021118 00021 WP 2002 11 18 MWEA020695 1 20021115 A 5753 BRACKET DOUG DC9 DC981 3022081 WP RH WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 RIGHT HAND WING, THE FLAP BRACKET ATTACHED TO REAR SPAR AT STATION XRS 164 HAS CORROSION IN THE POCKET AREA NEXT TO LOWE R OUTBOARD ATTACH STUD. -- REMOVED CORROSION. 2 L 7 2 4F A6WE 2002111800022 20021118 00022 NM 2002 11 18 AWXA200200916 1 20020924 A 2612 BATTERY BOEING 737 73733A 1384673 NM SMOKE DETECTOR DISCHARGED A AWXA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 28 174AW 23633 DURING TAXI OUT THE AFT FIRE LIGHT AND BELL CAME ON INDICATING FIRE IN AFT CARGO COMPARTMENT, DISCHARGED AFT CARGO COMPA RTMENT FIRE BOTTLE AFTER THREE ATTEMPTS. RETURNED TO GATE. MAINTENANCE FOUND AFT CARGO COMPARTMENT SMOKE DETECTOR (S/N 9395) FAILED, SMOKE DETECTOR (A8079) WAS PREVIOUSLY ON MEL 26-19, CONDITION 4 (SMOKE DETECTOR BATTERY). WHEN THE SECOND DETECTOR FAILED ALARM AND BELL WERE ACTIVATED. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR, THE BATTERIES WERE REPL ACED IN SMOKE DETECTOR (A8079) IAW T/C R2M26001. FUNCTIONAL TEST WAS GOOD. 2 L 7 2 4F RT A16WE 2002111800023 20021118 00023 EU 2002 11 18 AWXA200200955 1 20020926 A 5210 FE240002 DAMPENER AIRBUS 320 A320232 3930326 EU PAX DOOR BYPASSING A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 642AW 25239 584 MCN - EMERGENCY EVACUATION - DURING C-05 CHECK THE R-1 DOOR FAILED FUNCTIONAL CHECK FOR DAMPING SYSTEM. MAINTENANCE REMO VED AND REPLACED THE DOOR DAMPER AND EMERGENCY OPERATION CYCLINDER IAW AMM 52-11-14-04, PG. 20, SUB TASK 52-11-14-220-05 6. 2 L 7 2 4F RT A28NM 2002111800024 20021118 00024 EU 2002 11 18 AWXA200200956 1 20020926 A 5210 FE174001 DAMPENER AIRBUS 320 A320232 3930326 EU PAX DOOR BYPASSING A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 642AW 40362 584 MCN - EMERGENCY EVACUATION - DURING C-05 CHECK THE L-1 DOOR FAILED FUNCTIONAL CHECK FOR DAMPING SYSTEM. MAINTENANCE REMO VED AND REPLACED THE DOOR DAMPER AND EMERGENCY OPERATION CYCLINDER IAW AMM 52-11-14-04, PG. 20, SUB TASK 52-11-14-220-05 6. 2 L 7 2 4F RT A28NM 2002111800025 20021118 00025 2002 11 18 AWXA200200958 4 20020930 A 3441 COMPUTER AIRBUS A319 A319132 3930340 NM INERT GUIDANCE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 814AW 1281 FLT 0843 DURING CRUISE RECEIVED ECAM WARNING AP AUTOTHRUST YAW DAMPER 2 FAULT A/C "ALT LAW", DIVERTED TO ABQ. MAINTENAN CE DOWNLOADED PREFLIGHT REPORT AND FOUND BOTH THE NR 2 AND 3 AIR DATA INERTIAL REFERENCE UNITS (ADIRU) FAILED. REMOVED A ND REPLACED THE NR 3 ADIRU AND PLACED THE NR 2 ADIRU, COND. 4, NR 2 IR INOP. BITE TEST OF NR 3 ADIRU GOOD. MAINTENANCE REPLACED THE NR 2 ADIRU, SYSTEM OPS TEST WAS GOOD. VENDOR BENCH TEST OF ADIRU CONFIRMED FAILURE OF UNIT; IDENTIFIED RE ASON FOR FAILURE AS SLOW IGNITION GYRO. REPLACED SENSOR ASSEMBLY AND PERFORMED THERMAL CALIBRATION; FUNCTIONAL TEST WAS GOOD. VENDOR BENCH TEST OF ADIRU WAS NO FAULT FOUND; UNIT WAS THERMAL CALIBRATED, TESTED, AND RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002111800026 20021118 00026 NM 2002 11 18 AWXA200200962 1 20020924 A 5310 654656923 SHEAR TIE BOEING 737 737375 13844BN NM FUSELAGE BUCKLED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 23707 DURING C-03 CHECK TWO SHEARS TIES WERE FOUND BUCKLED AT BS 1040, BETWEEN STR 12 - 14 LT. MAINTENANCE REMOVED THE DAMAGE D SHEAR TIES AT BS 1040, BETWEEN STR 12 - 14 LT. FABRICATED 2 EACH REPLACEMENT SHEAR TIES, AND INSTALLED REPAIR PARTS. 2 L 7 2 4F RT A16WE 2002111800027 20021118 00027 NM 2002 11 18 AWXA200200963 1 20020904 A 5340 655485218 ANGLE BOEING 737 737375 13844BN NM FUSELAGE WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 23707 DURING C-03 CHECK THE RT VERTICAL STABILIZER LOWER AFT PANEL SKATE ANGLE WAS FOUND WORN THROUGH, BS 1070 - 1100. MAINTEN ANCE REMOVED THE DAMAGED AREA OF SKATE ANGLE. FABRICATED A NEW SECTION OF REPLACEMENT SKATE ANGLE, 2 EACH STRAPS, AND A SHIM, AND INSTALLED REPAIR PARTS IAW AWA E.R. 03-5381-02270-ES4. 2 L 7 2 4F RT A16WE 2002111800028 20021118 00028 NM 2002 11 18 AWXA200200964 1 20020814 A 5315 6545808 FLOORBEAM BOEING 737 737375 13844BN NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 23707 DURING C-03 CHECK A 1 INCH CRACK WAS FOUND ON FLOORBEAM AT BS 294, LBL 28. MAINTENANCE TRIMMED OUT CRACK AND PERFORMED H FEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER, 4 EACH REPAIR ANGLES, AND 2 EACH SHIMS, AND INSTALLED RE PAIR PARTS IAW AWA E.R. 03-5315-02269-ES1. 2 L 7 2 4F RT A16WE 2002111800029 20021118 00029 NM 2002 11 18 AWXA200200965 1 20020905 A 5340 655249011 ANGLE BOEING 737 737375 13844BN NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 23707 DURING C-03 CHECK A 2.5 INCHES CRACK WAS FOUND ON LT & RT SUPPORT ANGLES OF THE VERTICAL STABILIZER TRAILING EDGE 20 INC H ABOVE TAIL CONE AT BS 1110. MAINTENANCE CUTOUT SUPPORT ANGLES, FABRICATED 2 EACH SPLICE ANGLES AND A BEAM EXTRUSION, A ND INSTALLED REPAIR PARTS IAW AWA E.R. 03-5535-02267-ES4. 2 L 7 2 4F RT A16WE 2002111800030 20021118 00030 NM 2002 11 18 AWXA200200966 1 20020903 A 5314 65621258 KEELBEAM BOEING 737 737375 13844BN NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 23707 DURING C-03 CHECK A 3 3/8 INCH CRACK WAS FOUND ON RT KEEL BEAM AT BS 540. MAINTENANCE CUTOUT DAMAGED SECTION OF KEEL BEA M AT BS 540, FABRICATED A REPAIR DOUBLER, SPLICE ANGLE, ATTACH ANGLE, RADIUS BLOCK, AND TIE CLIP, AND INSTALLED REPAIR P ARTS IAW AWA E.R. 03-5369-02270-TB1. 2 L 7 2 4F RT A16WE 2002111800031 20021118 00031 NM 2002 11 18 AWXA200200968 1 20020830 A 5314 65621258 KEELBEAM BOEING 737 737375 13844BN NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 23707 DURING C-03 CHECK EXFOLIATION CORROSION WAS FOUND ON THE RT KEEL BEAM AT BS 633. MAINTENANCE REMOVED CORROSION AND FOUN D MATERIAL LOSS WITHIN LIMITS BUT ALSO DISCOVERED A 2 INCH CRACK. TRIMMED OUT CRACK AND PERFORMED HFEC INSPECTION TO VER IFY CRACKS NO LONGER EXIST. FABRICATED AN EXTRUSION BEAM AND 2 EACH ANGLES, AND INSTALLED REPAIR PARTS IAW AWA E.R. 03-5 369-02272-SS2. 2 L 7 2 4F RT A16WE 2002111800032 20021118 00032 NM 2002 11 18 AWXA200200972 1 20021003 A 2420 GCU BOEING 737 7373S3 1384711 NM NR 1 GENERATOR FAILED A AWXA A UNSCHED LANDING J H B WARNING INDICATION ELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 28 314AW 23733 FLT 0769 - ON FINAL APPROACH AT PHX EN ROUTE FROM PVR THE NR 1 GENERATOR TRIPPED OFF AND THE FLIGHT CREW NOTICED AN ELEC TRICAL BURNING SMELL. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE NR 1 GENREATOR CONTROL UNIT (GCU) INOPERATIVE. REPLACED THE NR 1 GCU IAW BMM 24-21-81-401, OPERATIONAL CHECK OF UNIT WAS GOOD PER BMM 24-21-81- 501. 2 L 7 2 4F RT A16WE 2002111800033 20021118 00033 EU 2002 11 18 AWXA200200973 1 20021003 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU ZONE 263 WILL NOT TEST A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 38515 26807 098 EMERGENCY LIGHT SYSTEM TEST FAILED (AFT LT) WHEN TESTED FROM CIDS PANEL AT FORWARD FLIGHT ATTENDANT STATION. MAINTENANCE REMOVED AND REPLACED AFT LT EMERGENCY POWER SUPPLY UNIT (13WL) AND BATTERY PACK; EMERGENCY LIGHT SYSTEM TEST CHECKED GO OD. 2 L 7 2 4F RT A28NM 2002111800034 20021118 00034 NM 2002 11 18 AWXA200200974 1 20021003 A 2560 P4010021 BATTERY BOEING 737 73733A 1384673 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 174AW 23633 FLIGHT CREW REPORTED THAT ONE OF THE FORWARD EMERGENCY FLASHLIGHTS LED WAS NOT BLINKING. MAINTENANCE REMOVED AND REPLACE D THE BATTERIES IN THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002111800035 20021118 00035 NE 2002 11 18 02320667 2 20021116 A 7260 5018T48P01 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE A VTZA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 667BR 7535 During cruise, R/H engine oil pressure and temperature dropped off. The crew shut down the R/H engine and landed at SWF without further incident. Maintenance personnel removed and replaced the seals at the accessory drive gearbox for the IDG and starter. Engine run operational checks were satisfactory and the aircraft was returned to service. 2 L 7 2 4F 4 F RT A21EA E15NE 2002111800036 20021118 00036 NM 2002 11 18 AWXA200200975 1 20021003 A 2822 P99C38605 PUMP AIRBUS A319 A319132 3930340 NM FUEL BOOST MALFUNCTIONED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 825AW 4406 1527 ON TAKEOFF FROM LGB EN ROUTE FOR PHX SHORTLY AFTER SETTING TAKEOFF POWER, THE ECAM INDICATED LT FUEL TANK NR 1 BOOST PUM P LOW PRESSURE, REJECTED TAKEOFF AND PUMP RETURNED TO NORMAL OPERATION. MAINTENANCE PLACED LT FUEL TANK PUMP ON MEL 28-2 1-01, CONDITION NR 3, " LT WING TANK PUMP INOPERATIVE". MAINTENANCE REPLACED THE LT FUEL TANK NR 1 PUMP IAW AMM 28-21- 51-401, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002111800037 20021118 00037 NM 2002 11 18 AWXA200200976 1 20020912 A 5320 140N250532 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 DURING C-06 CHECK A 3/4 INCH CRACK WAS FOUND ON CABIN UPPER INTERCOASTAL ANGLE BS 445. MAINTENANCE REMOVED THE DAMAGED I NTERCOASTAL ANGLE AT BS 445. FABRICATED A NEW INTERCOASTAL ANGLE, AND INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, F IG. 8, PG. 39-40. 2 L 7 2 4F RT A2NM 2002111800038 20021118 00038 NM 2002 11 18 AWXA200200978 1 20020915 A 5414 313N505223 PANEL BOEING 757 757225 1384959 NM NR 2 PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 DURING C-06 CHECK A 1 INCH CRACK WAS FOUND ON NR 2 ENGINE PYLON LOWER TRAILING EDGE PANEL, AT THE INBOARD FORWARD END. M AINTENANCE REMOVED THE LOWER TRAILING EDGE PANEL. FABRICATED A NEW LOWER TRAILING EDGE PANEL, AND INSTALLED REPAIR PART IAW B757-200 SRM 51-40-01, PG. 3. 2 L 7 2 4F RT A2NM 2002111800039 20021118 00039 NM 2002 11 18 AWXA200200979 1 20020912 A 5753 13N280061 STRUCTURE BOEING 757 757225 1384959 NM LT WING TE FLAP CONTAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 DURING C-06 CHECK X-RAY INDICATED MOISTURE WAS TRAPPED IN THE LT WING INBOARD AFT FLAP. MAINTENANCE REMOVED DAMAGED SKIN PLIES TO ACCESS HONEYCOMB; REMOVED DAMAGED AREA AND MOISTURE; REINSTALLED SKIN PER B757-200 SRM 51-70-04, PG. 4-31. 2 L 7 2 4F RT A2NM 2002111800040 20021118 00040 NM 2002 11 18 AWXA200200980 1 20021005 A 3350 100865 POWER SUPPLY BOEING 757 7572S7 1384962 NM FUSELAGE DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 903AW 23323 FLIGHT CREW REPORTED THAT THE EMERGENCY EXIT BULLNOSE LIGHT AT SEAT ROW 7 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE EMERGENCY EXIT LIGHT POWER SUPPLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002111800041 20021118 00041 NM 2002 11 18 AWXA200200983 1 20020918 A 2721 251N30725 STRUCTURE BOEING 757 757225 1384959 NM RUDDER WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 DURING C-06 CHECK THE RUDDER FEEL CENTERING AND TRIM QUADRANT RIG HOLE EXCEEDS SPECIFIED HOLE DIAMETER (SPECIFIED SIZE . 312, ACTUAL SIZE .380). MAINTENANCE OVERSIZED THE HOLE TO .395, FABRICATED A BUSHING AND REAMED HOLE TO .312, INSTALLED REPAIR IAW AWA E.R. 19-2721-02277-ES2. 2 L 7 2 4F RT A2NM 2002111800042 20021118 00042 NM 2002 11 18 AWXA200200984 1 20020929 A 5320 65528841 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 DURING C-12 CHECK A 1/4 INCH CRACK WAS FOUND ON MAIN CABIN FLOOR SUPPORT AT RADIUS AND FASTENER HOLE, BS 540, LBL 1, WL 208. MAINTENANCE REMOVED THE CRACKED FLOOR SUPPORT AT BS 540, LBL 1, WL 208. FABRICATED A NEW REPLACEMENT FLOOR SUPPORT, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 16-19, AND SRM 51-40-04, PG. 3 FIG. 1. 2 L 7 2 4F RT A16WE 2002111800043 20021118 00043 EU 2002 11 18 AWXA200200986 1 20021007 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 661AW 1284 DURING INSPECTION THE FORWARD LT FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT BATTERY WAS FOUND TO HAVE A LOW CHARGE. MAINTENA NCE REMOVED AND REPLACED THE LT FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002111800044 20021118 00044 NM 2002 11 18 AWXA200200987 1 20020930 A 5320 65458078 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 DURING C-12 CHECK A 1/2 INCH CRACK WAS FOUND ON THE INBOARD FORWARD END OF INTERCOASTAL AT BS 277 TO BS 291.5, WL 230, S TR 14 RT. MAINTENANCE REMOVED THE DAMAGED INTERCOASTAL WEB AT BS 277 TO BS 291.5, FABRICATED A NEW INTERCOASTAL, AND INS TALLED REPAIR IAW DWG 65-45807-8, AND B737-300 SRM 51-40-02, PG. 3-4, 10, 12, 38, 45, FIG. 8 & 12. 2 L 7 2 4F RT A16WE 2002111800045 20021118 00045 NM 2002 11 18 AWXA200200989 1 20021008 A 3150 WARNING SYSTEM BOEING 737 7373G7 1384595 NM COCKPIT MALFUNCTIONED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 309AW 24711 FLT 0864 - DURING TAKEOFF ROLL AT LAS EN ROUTE FOR SFO WITH ENGINES AT 70 PERCENT THE TOGGLE SWITCH WAS PRESSED AND THE CONFIGURATION WARNING HORN SOUNDED. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE PERFORMED A TAKEOFF WARNING SYSTEM TEST PER T/C A1B31009, TAKEOFF WARNING TEST CHECKED GOOD, COULD NOT DUPLICATE THE MALFUNCTION. 2 L 7 2 4F RT A16WE 2002111800046 20021118 00046 EU 2002 11 18 AWXA200200992 1 20021007 A 2700 3945128102 COMPUTER AIRBUS 320 A320231 3930325 EU NR 2 MALFUNCTIONED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 643AW 5081 1610 315 FLT 0462 - ON TAKEOFF AT YVR EN ROUTE FOR PHX ELEVATOR AILERON COMPUTER (ELAC) NR 2 FAULTED ON UPPER ECAM AS THRUST WAS BEING ADVANCED TOWARD "FLEX". REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED ELAC 2 IAW AMM 27- 93-34-400-001, OPERATIONAL TEST WAS GOOD IAW AMM 27-93-00-710. 2 L 7 2 4F RT A28NM 2002111800047 20021118 00047 EU 2002 11 18 AWXA200200993 1 20021008 A 5610 NP1653115 WINDSHIELD AIRBUS 320 A320232 3930326 EU COCKPIT FAILED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 659AW 10157 1166 FLT 0722 - EN ROUTE FROM LAS TO ORD THE LT WINDSHIELD OUTER PANE SHATTERED, DIVERTED TO DEN AND LANDED WITHOUT FURTHER E VENT. AIRCRAFT WAS MAINTENANCE FERRIED TO PHX FOR WINDSHIELD REPLACEMENT. MAINTENANCE IN PHX REMOVED AND REPLACED THE L T WINDSHIELD IAW AMM 56-11-11. VENDOR FUNCTIONAL CHECK OF WINDOW HEAT COMPUTER WAS NO FAULT FOUND, UNIT WAS RETURNED TO SERVICE WITH NO MAINTENANCE ACCOMPLISHED. VENDOR TEARDOWN OF LT WINDSHIELD IDENTIFIED REASON FOR OUTER PANE FAILURE WAS DUE TO MOISTURE INGRESSION ALONG THE BOTTOM EDGE OF WINDOW, MOISTURE CONTACTED ELECTRICAL WINDOW HEAT WIRES CAUSING THE WINDOW TO CRACK. REPLACED OUTER GLASS. 2 L 7 2 4F RT A28NM 2002111800048 20021118 00048 EU 2002 11 18 AWXA200200994 1 20021010 A 2121 BEARING AIRBUS 320 A320232 3930326 EU AVIONICS FAN FAILED A AWXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 28 619AW 497 527 DURING INSPECTION MAINTENANCE OBSERVED A BURNING ODOR COMING FROM THE AVIONICS FAN. REMOVED AND REPLACED AVIONICS FAN (2 0HQ) IAW AMM 21-26-51-401, OPERATIONAL TEST PERFORMED IAW AWA T/C F1B21302. VENDOR BENCH TEST OF AVIONICS FAN WAS NO F AULT FOUND. RAN FAN FOR 30 MINUTES, COULD NOT DUPLICATE A BURNING ODOR. DURING TEST A SLIGHT NOISE WAS HEARD FROM BEARIN GS, REPLACED BOTH BEARING FOR BEING LOOSE, FUNCTIONAL TEST ACCOMPLISHED IAW 21-26-42. 2 L 7 2 4F RT A28NM 2002111800049 20021118 00049 NM 2002 11 18 AWXA200200995 1 20021011 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM ROW 19 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED T HE DAMAGED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT, FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002111800050 20021118 00050 EU 2002 11 18 AWXA200200996 1 20021011 A 5250 AR47061 BOLT AIRBUS 320 A320232 3930326 EU COCKPIT DOOR SHORTED A AWXA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 28 654AW 1050 FLT 0193 - EN ROUTE FROM CMH TO LAS FAULT LIGHT CAME ON FOR COCKPIT DOOR LOCK, AREA OF CENTER LOCK WAS HOT TO THE TOUCH, ALSO OBSERVED AN ELECTRICAL BURNING ODOR, TURNED BACK TO CMH AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE COCKPIT DOOR CENTER BOLTING SYSTEM IAW AMM 52-51-12, PG. 1-23; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002111800051 20021118 00051 NM 2002 11 18 AWXA200200997 1 20021013 A 2121 6454051 FAN BOEING 737 7373S3 1384711 NM COCKPIT BURNED OUT A AWXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 312AW 16368 24060 FLT 0625 - ON TAXI OUT AT PHX THE COCKPIT FILLED WITH A STRONG ELECTRICAL BURNING ODOR, TURNED OFF AIR CONDITIONING PACK S, RECIRCULATION FAN, ENGINE GENERATORS, AND BURNING ODOR DISSIPATED. AIRCRAFT RETURNED TO GATE. MAINTENANCE DISCOVERED THE RECIRCULATION FAN CIRCUIT BREAKER EXTENDED, REMOVED AND REPLACED THE RECIRCULATION FAN IAW BMM 21-21-22-401; OPERATI ONAL TEST OF FAN WAS GOOD. 2 L 7 2 4F RT A16WE 2002111800052 20021118 00052 NM 2002 11 18 AWXA200200998 1 20021005 A 5313 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 DURING C-12 CHECK A 1/16 INCH CRACK WAS FOUND ON STRINGER TIE CLIP IN THE AFT CARGO COMPARTMENT BS 867, STR 20 RT. MAINT ENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 867, STR 20 RT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTA LLED REPAIR PART IAW DWG 65-46555, AND B737-300 SRM 51-40-02, PG. 10-11. 2 L 7 2 4F RT A16WE 2002111800053 20021118 00053 EU 2002 11 18 AWXA200201003 1 20021014 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 654AW 1050 FLIGHT CREW REPORTED THE AFT RT FLIGHT ATTENDANT JUMP SEAT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT RT FLIGHT ATTENDANT JUMP SEAT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002111800054 20021118 00054 NM 2002 11 18 AWXA200201008 1 20021015 A 2560 BATTERY BOEING 737 737301 1384611 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 326AW 23258 FLIGHT CREW REPORTED THE FORWARD HORIZONTAL EMERGENCY FLASHLIGHT BATTERY WAS DEAD. MAINTENANCE REMOVED AND REPLACED THE FORWARD HORIZONTAL EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002111800055 20021118 00055 EU 2002 11 18 AWXA200201014 1 20021014 A 5210 FE174001 CYLINDER AIRBUS 320 A320231 3930325 EU PAX DOOR LEAKING A AWXA K NONE K L FLUID LOSS NO TEST IN INSP/MAINT 1 WP 28 645AW 40153 9074 238 DURING C-01 CHECK THE R-2 DOOR WAS FOUND TO HAVE NO DAMPING ACTION WHEN CLOSING DUE TO INTERNAL LEAKAGE. MAINTENANCE REM OVED AND REPLACED THE R-2 DOOR DAMPING AND EMERGENCY CYLINDER IAW AMM TASK 52-13-14-000-001 AND TASK 52-13-14-400-001, F UNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002111800056 20021118 00056 NM 2002 11 18 AWXA200201015 1 20021016 A 3350 321454 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 832AW 2811 1643 DURING INSPECTION IT WAS DISCOVERED THAT THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE AFT L T EMERGENCY POWER SUPPLY UNIT (13WL) AND BATTERY IAW AMM 33-52-00, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002111800057 20021118 00057 EU 2002 11 18 AWXA200201016 1 20021019 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 649AW 803 DURING INSPECTION EMERGENCY EXIT LIGHTS FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT TH E RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL); OPERATIONAL CHECK WAS GOOD IAW AWA T/C 18M05319, STEP 5. 2 L 7 2 4F RT A28NM 2002111800058 20021118 00058 NM 2002 11 18 AWXA200201017 1 20021020 A 2560 P4010021 BATTERY BOEING 737 73733A 1384673 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 175AW 23634 FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT IN THE FORWARD GALLEY WAS NOT FULLY CHARGED. MAINTENANCE REMOVED AND REPL ACED THE BATTERIES ON THE FORWARD GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002111800059 20021118 00059 NM 2002 11 18 AWXA200201018 1 20021020 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 809AW 1111 FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EME RGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002111800060 20021118 00060 WP 2002 11 18 AALA20021271 1 20020828 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7548A 53030 TUL - FOUND CORROSION ON UPPER BEAM OF AFT CARGO DOOR CUTOUT AT STATION 1184. REPAIRED UPPER DOOR CUTOUT BEAM PER ESO 8 0559. (M) 2 L 7 2 4F A6WE 2002111800061 20021118 00061 WP 2002 11 18 AALA20021272 1 20020826 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7548A 53030 TUL - FOUND AFT CARGO DOOR BEAM CORRODED STATION 1174. REMOVED AND REPLACED AFT CARGO DOOR BEAM PER SRM 51-03. (M) 2 L 7 2 4F A6WE 2002111800062 20021118 00062 WP 2002 11 18 AALA20021273 1 20020826 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7548A 53030 TUL - FOUND LEFT CUSP HAS CORROSION AT STATION 1261. INSTALLED REPAIR DOUBLER PER SRM 53-0 FIG 4. (M) 2 L 7 2 4F A6WE 2002111800063 20021118 00063 WP 2002 11 18 AALA20021274 1 20020821 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7548A 53030 TUL - FOUND SEAT TRACK 1 STATION 1208 HAS CORROSION IN BOTTOM OF TRACK. REPAIRED PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2002111800064 20021118 00064 WP 2002 11 18 AALA20021275 1 20020822 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7548A 53030 TUL - FOUND CORROSION AT RIGHT CUSP AREA AROUND LIGHTING HOLE BETWEEN STA 731-739. INSTALLED CUSP REPAIR AS PER AARD 53 -00-00-02. (M) 2 L 7 2 4F A6WE 2002111800065 20021118 00065 WP 2002 11 18 AALA20021276 1 20020821 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7548A 53030 TUL - FOUND SEAT TRACK NR 1 STATION 1234 HAS CORROSION IN BOTTOM OF TRACK. REPAIRED PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2002111800066 20021118 00066 WP 2002 11 18 AALA20021277 1 20020823 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7548A 53030 TUL - FOUND CRACK AROUND FASTENER HOLE UNDER FLOORBOARD SUPPORT STATION 170-200. REMOVED CRACK DAMAGE. INSTALLED REPAI R PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2002111800067 20021118 00067 WP 2002 11 18 AALA20021278 1 20020823 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7548A 53030 TUL - FOUND 1452 FRAME CRACKED INBOARD SIDE OF STRINGER 3R, SMALL STRAIGHT FRAME BETWEEN 1437 AND 1388. STOP DRILLED CR ACK. INSTALLED DOUBLER PER AARD 53-10-00-1. (M) 2 L 7 2 4F A6WE 2002111800068 20021118 00068 WP 2002 11 18 AALA20021279 1 20020822 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7548A 53030 TUL - FOUND UPPER AFT WINDOW FLANGE SHOWS EVIDENCE OF CRACK INBOARD OF FASTENER AT RADIUS STATION 1060. STOP DRILLED CR ACK AND INSTALLED DOUBLER PER AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2002111800069 20021118 00069 WP 2002 11 18 AALA20021280 1 20020821 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7548A 53030 TUL - FOUND RIGHT SIDE OF A/C STATION 1060 UPPER AFT OF WINDOW FRAME CRACKED. TRIMMED OUT CRACK. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2002111800070 20021118 00070 NM 2002 11 18 BJNA021002 1 20021019 A 5320 BAC15061500 FLOOR SUPPORT BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 46627 23043 DURING A SCHEDULED C-CHECK INSPECTION, DISCOVERED AFT FUSELAGE FLOOR SUPPORT FRAME AT STATION 951 FROM LBL 20 TO LBL 36 HAS LEVEL 2 CORROSION. REMOVED FLOOR SUPPORT FRAME, FABRICATED AND INSTALLED FRAME REPAIR IAW BOEING SRM 53-10-2 AND 51 -30-2. (M) 2 L 7 2 4F RT A16WE 2002111800071 20021118 00071 NM 2002 11 18 BJNA021003 1 20021019 A 5313 BAC1498117 STRINGER BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 46627 23043 DURING A SCHEDULED C-CHECK INSPECTION OF THE FORWARD CARGO COMPARTMENT, DISCOVERED A TWO INCH SPOT OF LEVEL 2 CORROSION ON STRINGER 27L AT STATION 389. FABRICATED AND INSTALLED STRINGER REPAIR IAW BOEING 737 SRM 51-10-2, 51-10-6, 51-30-2, 53-10-01 FIGURE 1 AND 53-10-3 FIGURE 1. (M) 2 L 7 2 4F RT A16WE 2002111800072 20021118 00072 NM 2002 11 18 AWXA200201020 1 20021004 A 5410 313A135556 CLIP BOEING 737 737301 1384611 NM LT NACELLE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 DURING C-17 CHECK 2 EACH 3/4 INCH CRACKS WERE FOUND ON RIB BRACKETS (SPRING CLIPS) AT THE INBOARD SIDE OF THE LT PYLON N AC STA 282.67, NAC WL 117. MAINTENANCE REMOVED 2 EACH DAMAGED SPRING CLIPS AT INBOARD SIDE OF THE LT PYLON NAC STA 282.6 7, NAC WL 117; FABRICATED 2 EACH REPLACEMENT SPRING CLIPS; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5454-02289-TB1. 2 L 7 2 4F RT A16WE 2002111800073 20021118 00073 NM 2002 11 18 BJNA021004 1 20021019 A 5313 STRINGER BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 46627 23043 DURING A SCHEDULED C-CHECK INSPECTION OF THE AFT CARGO COMPARTMENT BILGE AREA, DISCOVERED LEVEL 2 CORROSION. ON THE FOR WARD END OF STRINGERS 25L AT STATION 967. CUT OUT DAMAGED SECTION, IAW BOEING SRM 53-10-3 FIGURE 1. FABRICATED AND INS TALLED STRINGER REPAIR IAW BOEING SRM 53-10-3. (M) 2 L 7 2 4F RT A16WE 2002111800074 20021118 00074 NM 2002 11 18 AWXA200201021 1 20021004 A 5410 313A135556 CLIP BOEING 737 737301 1384611 NM RT NACELLE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 DURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND ON RIB BRACKET (SPRING CLIP) AT THE OUTBOARD SIDE OF THE RT PYLON NAC STA 2 82.67, NAC WL 117. MAINTENANCE REMOVED THE DAMAGED SPRING CLIP AT THE OUTBOARD SIDE OF RT PYLON NAC STA 282.67, NAC WL 1 17; FABRICATED A NEW REPLACEMENT SPRING CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 3-4, 16-17, 26-27, FI G. 3, AND SRM 51-40-04, PG. 2, FIG. 1. 2 L 7 2 4F RT A16WE 2002111800075 20021118 00075 NM 2002 11 18 AWXA200201024 1 20021004 A 5753 654642835 FLAP TRACK BOEING 737 737277 1384570 NM NR 7 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 DURING C-20 CHECK A 1/4 INCH CRACK WAS FOUND ON THE NR 7 FLAP TRACK AT THE INBOARD ROLLER OF UPPER TRACK, AFT END. MAINT ENANCE REMOVED AND REPLACED THE DAMAGED NR 7 FLAP TRACK AT THE INBOARD ROLLER OF UPPER TRACK, AFT END IAW AWA T/C R3R270 04. 2 L 7 2 4F RT A16WE 2002111800076 20021118 00076 NM 2002 11 18 AWXA200201027 1 20021004 A 5330 6545800 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 DURING C-20 CHECK A 1 1/2 INCH CRACK WAS FOUND ON FUSELAGE SKIN L-1 DOOR CUTOUT BELOW LOWER SCUFF PLATE, APPROXIMATELY 1 0 INCH FORWARD OF AFT LOWER CORNER BS 334 - 336, STR 17 LT. MAINTENANCE REMOVED EXISTING REPAIR DOUBLER, STRAP, WEB, AND COVER PLATE AT BS 334 - 336, STR 17 LT TO ACCESS DAMAGED AREA; REMOVED CRACK AND PERFORMED HFEC INSPECTION TO VERIFY CR ACK NO LONGER EXISTS; REINSTALLED REPAIR DOUBLER, STRAP, WEB, AND COVER PLATE PER E.O. 53-44-01. 2 L 7 2 4F RT A16WE 2002111800077 20021118 00077 NM 2002 11 18 BJNA021005 1 20021023 A 5315 FLOORBEAM BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 46628 23043 DURING A SCHEDULED C-CHECK INSPECTION DISCOVERED LEVEL 2 CORROSION ADJACENT TO WATER DRAIN LINE FORWARD UNDER SIDE OF R2 DOOR SCUFF PLATE AREA BS 958 RBL 53. REMOVED CORROSION FROM LOWER OUTBOARD FLOORBEAM SUPPORT, CORROSION WENT OUT OF LI MITS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW B737 SRM 51-40-3, 51-10-2, 51-20-1 AND 51-30-2. (M) 2 L 7 2 4F RT A16WE 2002111800078 20021118 00078 NM 2002 11 18 BJNA021006 1 20021009 A 5313 STRINGER BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 23043 DURING SCHEDULED C-CHECK INSPECTION DISCOVERED AFT LOWER BILGE STATION 1006, STRINGER 23L, CLIP CORRODED. REMOVED CLIP AND S23L IN THE AFT LOWER BILGE BS 1006. FORMED REPAIR STRINGER AND CLIP AND INSTALLED IAW B737 SRM 53-10-3 AND 51-10-2 . (M) 2 L 7 2 4F RT A16WE 2002111800079 20021118 00079 NM 2002 11 18 BJNA021016 1 20021030 A 3350 6013211 POWER SUPPLY BOEING 737 737282 13844AT NM CARGO BAY DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 RIGHT OVER WING EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE ON TEST. REPLACED POWER SUPPLY PER BMM 33-51-31. (M) 2 L 7 2 4F RT A16WE 2002111800087 20021118 00087 NM 2002 11 18 AWXA200201029 1 20021021 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM FUSELAGE DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 DURING INSPECTION THE L-2 DOOR INTERIOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE L-2 DOOR EMERGENCY EXIT LIGHT BATTERY PACK IAW 33-51-01, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002111800088 20021118 00088 WP 2002 11 18 MWEA020698 1 20021118 A 5311 591015891 WEB DOUG DC9 DC932 3022066 WP AFT CARGO CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 AFT DOOR JAMB PAM WEB HAS AREAS OF CORROSION. -- REMOVED AND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2002111800089 20021118 00089 NM 2002 11 18 C7WA200200011 1 20020713 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 29R FROM BS 480 TO BS 540. REPLACED STRINGER 29R SECTION BETWEEN BS 480 AND BS 545 IAW SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2002111800090 20021118 00090 NM 2002 11 18 AWXA200201031 1 20021015 A 5310 6517688U165 DOOR FRAME BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 DURING C-20 CHECK CORROSION WAS FOUND AT THE L-1 DOOR SILL INNER CHORD UNDER DRAIN TROUGH BS 333, LBL 50. MAINTENANCE RE MOVED 2 EACH ANGLES AT BS 312 AND 344, A WEB AT BS 277 - 306, A FRAME BS 300, AND AN ANGLE BS 277 - 284 FOR ACCESS, REMO VED DAMAGED DOOR SILL INNER CHORD AT BS 333, LBL 50; FABRICATED A NEW REPLACEMENT DOOR SILL INNER CHORD; INSTALLED REPAI R PART AND REINSTALLED 2 EACH ANGLES, WEB, FRAME, AND ANGLE, IAW DWG 65-17688, B737-200 SRM 51-10-1, PG. 8, AND SRM 51-3 0-2, PG. 2-5. 2 L 7 2 4F RT A16WE 2002111800093 20021118 00093 NM 2002 11 18 AWXA200201032 1 20021005 A 5320 6935352507 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 DURING C-12 CHECK A 1/4 INCH CRACK WAS FOUND ON A STRINGER TIE CLIP IN AFT CARGO COMPARTMENT, BS 907, STR 23 LT. MAINTEN ANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 907, STR 23 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; AND INS TALLED REPAIR PART IAW DWG 69-35352, SHT 1, AND B737-300 SRM 51-40-02, PG. 38, FIG. 8. 2 L 7 2 4F RT A16WE 2002111800095 20021118 00095 NM 2002 11 18 AWXA200201033 1 20021005 A 5320 6935352507 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 DURING C-12 CHECK A 1/4 INCH CRACK WAS FOUND ON A STRINGER TIE CLIP IN AFT CARGO COMPARTMENT, BS 907, STR 21 LT. MAINTEN ANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 907, STR 21 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; AND INS TALLED REPAIR PART IAW DWG 69-35352, SHT 1, AND B737-300 SRM 51-40-02, PG. 38, FIG. 8. 2 L 7 2 4F RT A16WE 2002111800103 20021118 00103 NM 2002 11 18 AWXA200201034 1 20021005 A 5320 6935352507 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 DURING C-12 CHECK A 1/4 INCH CRACK WAS FOUND ON A STRINGER TIE CLIP IN AFT CARGO COMPARTMENT, BS 907, STR 22 LT. MAINTEN ANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 907, STR 22 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; AND INS TALLED REPAIR PART IAW DWG 69-35352, SHT 1, AND B737-300 SRM 51-40-02, PG. 38, FIG. 8. 2 L 7 2 4F RT A16WE 2002111800109 20021118 00109 SO 2002 11 18 LR7A02117 1 20021112 A 5347 371094151 TRACK LKHEED 382 382G 526414U SO FS159 WORN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 605 4763 DURING SCHEDULED B1 INSPECTION PER HB0509 FOUND FLIGHT ENGINEERS SEAT TRACKS WORN. FS159, BL0, WL200.REPLACED TRACKS IA W SRM SMP 583-51-60-00, DWGS 371094, AND 371095. NR0047. 2 H 7 4 4T A1SO 2002111800110 20021118 00110 SO 2002 11 18 LR7A02118 1 20021112 A 5330 RISER LKHEED 382 382G 526414U SO FS517 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 605 4763 DURING SCHEDULED B1 INSPECTION PER HB0506 FOUND LH MLG BAY SKIN RISER CRACKED ADJACENT TO EXISTING REPAIR. FS517-497, L BL60, WL150-175.REPAIRED SKIN RISER IAW SRM SMP 583 FIG 53-40-02, AND 51-70. NR0059. 2 H 7 4 4T A1SO 2002111800111 20021118 00111 SO 2002 11 18 LR7A02119 1 20021112 A 5312 3884824 BEAM LKHEED 382 382G 526414U SO FS577 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 605 4763 DURING SCHEDULED B1 INSPECTION PER HB0506 FOUND RH MLG BAY TRACK SUPPORT BEAM CORRODED. FS577, RBL60, WL160.REPLACED BE AM AND CAP IAW SRM SMP 583 51-70 AND DWG 388482. NR0065. 2 H 7 4 4T A1SO 2002111800112 20021118 00112 SO 2002 11 18 LR7A02120 1 20021112 A 5312 ANGLE LKHEED 382 382G 526414U SO FS617 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 605 4763 DURING SCHEDULED B1 INSPECTION PER HB0506 FOUND RH MLG BAY AFT PRESSURE BULKHEAD PANEL SLICE ANGLE CRACKED. FS617, RBL6 0, WL170.REPLACED ANGLE IAW SRM SMP 583 51-70 AND DWG 339149. NR0067. 2 H 7 4 4T A1SO 2002111800113 20021118 00113 SO 2002 11 18 LR7A02121 1 20021112 A 5343 388997112 TRACK LKHEED 382 382G 526414U SO FS577 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 605 4763 DURING SCHEDULED B1 INSPECTION PER HB0506 FOUND ON REMOVAL OF RH FS577 MLG BEAM, RH AFT FWD MLG TRACK CRACKED AT LOWER N UT HOLE. FS577, RBL60, WL160.REPLACED RH AFT MLG TRACKS IAW SRM SMP 51-70 AND DWG 388997. NR0098. 2 H 7 4 4T A1SO 2002111800114 20021118 00114 WP 2002 11 18 ZW0A0211402 1 20021116 A 2911 33115861 ACCUMULATOR DOUG DC9 DC982 3022082 WP A ZW0A K NONE O OTHER CR CRUISE 1 CE 13 950U 49230 CREW REPORTED SMELL OF KEROSENE IN COCKPIT AND CABIN. REPLACED THE RH THRUST REVERSER ACCUMULATOR ACCOUNT LEAKING HYDRA ULIC FLUID. CHECK-C 10-29-02 STL. --CLOSED-- 2 L 7 2 4F A6WE 2002111800115 20021118 00115 EA 2002 11 18 COMA0260654 1 20021111 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 915CA 13546 7013 FLIGHT 5503 GEAR DISAGREE - NLG TOOK 60 SECOND TO DOWN LOCK.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002111800116 20021118 00116 EA 2002 11 18 COMA0260647 1 20021114 A 2750 7805013 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA INST PANEL MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 01 783CA 10259 7315 FLIGHT 5706 FLAPS FAILED WHEN SELECTED UP AFTER LANDING.REPLACED THE FLAP CONTROL LEVER. 2 L 7 2 4F RT A21EA 2002111800117 20021118 00117 NM 2002 11 18 UPS02539919 1 20021111 A 2750 FLAP BOEING 757 75724APF 1384969 NM R/H I/B DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 461UP 28265 INSPECTION TYPE:ASV ON POST FLIGHT FOUND RIGHT I/B FLAP FAIRING WITH A HOLE IN IT. TRAI LING EDGE FLAP WITH DAMAGE. REPAIRED FLAP FAIRING DAMAGE PER 57-53-01. REPAIRED DAMAGE TO TRAIL ING I/B AFT FLAP PER SRM 57-53-01. OPS CHECK NORM AL PER 27-51-02. 2 L 7 2 4F RT A2NM 2002111800118 20021118 00118 EU 2002 11 18 AWXA200201126 1 20021117 A 3350 ABS0374A24 CABLE AIRBUS 320 A320232 3930326 EU SEAT ROW 26 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 605AW 0 0 543 CMH - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 26 L/H. MAINTENANCE FOUN D BROKEN WIRES AT PLUG, RECONNECTED EMERGENCY ESCAPE PATH LIGHT WIRES AT CONNECTOR SEAT ROW 26 L/H, OPERATIONAL CHECK WA S GOOD. 2 L 7 2 4F RT A28NM 2002111800119 20021118 00119 NM 2002 11 18 AWXA200201128 1 20021104 A 5313 65353523 TIE CLIP BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 0 0 23632 YVR - MAJOR REPAIR - DURING C-19 CHECK A 1/4 CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 947.5, STR 26 L/H. MAINTENANCE R EMOVED DAMAGED STRINGER TIE CLIP AT BS 947.5, STR 26 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 65-4656 01; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2 L 7 2 4F RT A16WE 2002111800120 20021118 00120 NM 2002 11 18 AWXA200201129 1 20021028 A 5313 69451561 TIE CLIP BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 0 0 23632 YVR - MAJOR REPAIR - DURING C-19 CHECK A 1/4 CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 787, STR 11 L/H. MAINTENANCE REM OVED DAMAGED STRINGER TIE CLIP AT BS 787, STR 11 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-45156; A ND INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2 L 7 2 4F RT A16WE 2002111800121 20021118 00121 NM 2002 11 18 AWXA200201130 1 20021031 A 5315 6546592 CHANNEL BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 0 0 23632 YVR - MAJOR REPAIR - DURING C-19 CHECK EXFOLIATION CORROSION WAS FOUND UNDER AFT CARGO FLOOR SUPPORT CHANNEL AT SEVERAL ANCHOR NUTS BETWEEN BS 847 - BS 867; MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT D AMAGED SECTION OF FLOOR SUPPORT CHANNEL BS 847 - BS 867, LBL 3 TO RBL 3; FABRICATED REPAIR ANGLES AND TRANSVERSE FLOOR S TRAP PER DWG 65-45296-24; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-53, FIG. 201, AND SRM 51-10-02, PG. 10. 2 L 7 2 4F RT A16WE 2002111800122 20021118 00122 NM 2002 11 18 AWXA200201131 1 20021029 A 5320 651630084 WEB BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 0 0 23632 YVR - MAJOR REPAIR - DURING C-19 CHECK A 1/2" CRACK WAS FOUND ON WEB, 5 1/2" ABOVE WL 207 AT BS 178, LBL 5.7, UPPER L/H RADAR ANTENNA MOUNT BRACKET LOCATION. MAINTENANCE CUTOUT DAMAGE AT WL 207 - 212, BS 178, LBL 5.7; FABRICATED A FILLER AN D DOUBLER; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-10-08, FIG. 210, PG. 275. 2 L 7 2 4F RT A16WE 2002111800123 20021118 00123 NM 2002 11 18 AWXA200201132 1 20021030 A 5311 6546560506 FRAME BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 0 0 23632 YVR - MAJOR REPAIR - DURING C-19 CHECK A 1/2" CRACK WAS FOUND ON FUSELAGE FRAME AT BS 947.5, STR 18 L/H. MAINTENANCE CUT OUT CRACK AT BS 947.5, STR 18 L/H AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A SHEAR TIE AND 2 EACH BELT FRAME DOUBLERS; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11, FIG. 1, PG. 1-6, DETAIL II. 2 L 7 2 4F RT A16WE 2002111800124 20021118 00124 NM 2002 11 18 AWXA200201135 1 20021030 A 5313 69353521 TIE CLIP BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 0 0 23632 YVR - MAJOR REPAIR - DURING C-19 CHECK A 1/4 CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 947.5, STR 25 R/H. MAINTENANCE R EMOVED DAMAGED STRINGER TIE CLIP AT BS 947.5, STR 25 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 65-4656 01; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2 L 7 2 4F RT A16WE 2002111800125 20021118 00125 NM 2002 11 18 AWXA200201139 1 20021029 A 5512 65C274941 SKIN BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 0 0 23632 YVR - MAJOR REPAIR - DURING C-19 CHECK LOOSE FASTENERS AND A 1 1/4" CRACK WAS FOUND ON SKIN OF THE L/H HORIZONTAL STABIL IZER LOWER SURFACE BETWEEN STAB STATIONS 138.70 AND 147.90. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON THE L/H HORIZONT AL STABILIZER LOWER SURFACE BETWEEN STAB STATIONS 138.70 AND 147.90 AND INSTALLED INTERNAL REPAIR IAW AWA E.R. 03-5516-0 2312-ES3. 2 L 7 2 4F RT A16WE 2002111800127 20021118 00127 NM 2002 11 18 KPVA200231 1 20021019 A 3350 824101655032 CONTROL BOX DHAV DHC8 DHC8103 1386005 NM CABIN FAILED A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807WP 023 REAR EXTERIOR EMERGENCY LIGHTS NR 1 AND NR 2 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL BOX. OPS CHECK GOOD IAW DHC8 MM 33-51-00. (M) 2 H 7 2 4T RT A13NM 2002111800128 20021118 00128 EU 2002 11 18 USAABA02021 1 20021020 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 673UW 337 PHL - EPSU FAULT DURING SYSTEM TEST. REPLACED BATTERY FOR EPSU 3R. (M) 2 L 7 2 4F RT A46NM 2002111800129 20021118 00129 NM 2002 11 18 QXEA0201932 1 20021113 A 3230 401020101 SENSOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 700 FAILED A QXEA O OTHER J O WARNING INDICATION OTHER AP APPROACH 1 NM 09 401QX 4031 BOI - ON APPROACH, THE CREW REPORTED THE GEAR DOORS CYCLED. LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT A ND REPLACED THE RIGHT UPLOCK PROXIMITY SENSOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002111800130 20021118 00130 NM 2002 11 18 USAABB02183 1 20021021 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 653US 24894 PHL - FOUND FLOOR TRACK LIGHTING INOPERATIVE ON RIGHT SIDE, ROWS 5 THROUGH 9. MAINTENANCE REPLACED THE BATTERY CHARGER. (M) 2 L 7 2 4F RT A1NM 2002111800131 20021118 00131 NM 2002 11 18 USAABB02185 1 20021023 A 3350 202175003 LIGHT BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 652US 24765 PHL - FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROW 9 AFT. MAINTENANCE REPLACED TWO LIGHT ASSEMBLIES. (M) 2 L 7 2 4F RT A1NM 2002111800133 20021118 00133 EU 2002 11 18 USAASA02090 1 20021026 A 3350 321430 BATTERY AIRBUS 320 A320214 3930316 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 108UW 1061 BDL - THE EMERGENCY LIGHT SYSTEM FAILED THE TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT BATTERIES. OPERATIO NALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2002111800134 20021118 00134 EU 2002 11 18 USAASA02092 1 20021026 A 3397 WIRE AIRBUS A319 A319112 3930323 EU CABIN OUT OF POSITION A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 712US 1038 PHL - FOUND THE LEFT, ROW 1, SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE, WITH A WIRE PULLED FROM THE CONNECTOR. (M) 2 L 7 2 4F RT A28NM 2002111800135 20021118 00135 EU 2002 11 18 USAASA02093 1 20021029 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 110UW 5248 1112 DCA- THE EMERGENCY LIGHT SYSTEM FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002111800136 20021118 00136 EA 2002 11 18 SWIA200211464 1 20021104 A 3234 HANDLE CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR SEL MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 440SW 7589 LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR HANDLE IAW CRJ MM 32-31-01. OPS CHECK GOOD. PN OFF/ ON 601R50967-9 SN OFF 0712. 2 L 7 2 4F RT A21EA 2002111800137 20021118 00137 EA 2002 11 18 SWIA200211468 1 20021113 A 2740 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA CAPTAIN'S MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 903SW 7425 MACH TIRM/STAB TRIM DISCONNECTED IN FLIGHT. REPLACED CAPTAIN'S TRIM SWITCH. DISCONNECT SWITCH OPS CHECKS GOOD IAW CRJ 27-41-30. PN OFF 996-0013. 2 L 7 2 4F RT A21EA 2002111900001 20021119 00001 NM 2002 11 19 AWXA200201036 1 20020930 A 5230 65C36215 SKIN BOEING 737 7373G7 1384595 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 DURING C-12 CHECK THE FORWARD CARGO DOOR FORWARD LOWER SKIN WAS FOUND CHAFED ON INSIDE OF DOOR BS 445, STR 19 RT. MAINTE NANCE BLENDED OUT CHAFED AREA AND FOUND SKIN TO BE CRACKED OUT OF LIMITS; REMOVED DAMAGED AREA OF FORWARD CARGO DOOR INN ER SKIN BS 445, STR 19 RT; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13, PG. 1-3, FIG. 1. 2 L 7 2 4F RT A16WE 2002111900002 20021119 00002 NM 2002 11 19 AWXA200201037 1 20021004 A 5230 65C25180 BEAM BOEING 737 737301 1384611 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 DURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND ON AFT CARGO DOOR LOWER CROSS BEAM AT FASTENER HOLE AFT END OF DOOR BS 801. 5, STR 23 RT. MAINTENANCE CUTOUT DAMAGED AREA OF CROSS BEAM AT BS 801.5, STR 23 RT; FABRICATED A REPLACEMENT SECTION OF TEE CHORD, 2 EACH REPAIR ANGLES, AND 2 EACH RADIUS FILLERS; INSTALLED REPAIR PARTS IAW E.O. 52-33-02, FIG. 5, PG. 29-34. 2 L 7 2 4F RT A16WE 2002111900003 20021119 00003 EU 2002 11 19 AWXA200201038 1 20021022 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 637AW 30356 10172 099 DURING INSPECTION EMERGENCY LIGHT TEST FAILED FROM FLIGHT ATTENDANTS PANEL "ESPU R COM". MAINTENANCE REMOVED AND REPLACE D THE RT EMERGENCY POWER SUPPLY UNIT (12WL) AND BATTERY PACK IAW AMM 33-51-38, SYSTEM OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT A28NM 2002111900004 20021119 00004 NM 2002 11 19 AWXA200201039 1 20021022 A 2560 P4010021 BATTERY BOEING 757 7572S7 1384962 NM LAV FLASHLIGHT DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 FLIGHT CREW REPORTED EMERGENCY FLASHLIGHT BATTERIES DEPLETED AT FLIGHT ATTENDANT STATION 2 LT. MAINTENANCE REMOVED AND R EPLACED EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002111900005 20021119 00005 NM 2002 11 19 AWXA200201040 1 20021017 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM LAV FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 322AW 25400 DURING C-12 CHECK THE FORWARD FLIGHT ATTENDANT INBOARD EMERGENCY FLASHLIGHT BATTERY WAS FOUND TO HAVE A LOW CHARGE. MAIN TENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT INBOARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL TEST WAS GOO D. 2 L 7 2 4F RT A16WE 2002111900006 20021119 00006 NM 2002 11 19 AWXA200201041 1 20021018 A 3350 1012621 SIGN BOEING 737 737277 1384570 NM BS 382 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 184AW 22651 DURING C-20 CHECK THE FORWARD SERVICE DOOR EMERGENCY EXIT SIGN WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE F ORWARD SERVICE DOOR EMERGENCY EXIT SIGN, OPERATIONAL CHECK WAS GOOD IAW AWA T/C A1C33006. 2 L 7 2 4F RT A16WE 2002111900007 20021119 00007 NM 2002 11 19 AWXA200201047 1 20021023 A 3150 WARNING SYSTEM BOEING 737 737375 13844BN NM COCKPIT MALFUNCTIONED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 336AW 23707 FLT 2220 - DURING TAKEOFF FROM SJD EN ROUTE FOR PHX TAKEOFF WARNING HORN SOUNDED, ABORTED TAKEOFF. RECONFIGURED AIRCRAFT , RETURNED TO RUNWAY, TOOK OFF WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A16WE 2002111900008 20021119 00008 NE 2002 11 19 AWXA200201048 2 20021024 A 7320 EEC AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 1 ENGINE FAILED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 825AW 1527 FLT 0186 - DURING TAKEOFF ROLL AT PHX EN ROUTE FOR SAN, AT 80 KTS NR 1 ENGINE DID NOT REACH TAKEOFF EPR; TARGET WAS 1.39 9; AT 1.25 WITH STRONG DIRECTIONAL PULL WHEN ABORTED TAKEOFF. MAINTENANCE PERFORMED A FULL AUTHORITY DIGITAL ENGINE CONT ROL AND ELECTRONIC ENGINE CONTROL TEST USING AWA T/C F571304, AND ALSO PERFORMED A POWER ASSURANCE TEST IAW AWA T/C F5M7 1312. NO FAULTS WERE FOUND, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2002111900009 20021119 00009 NM 2002 11 19 AWXA200201049 1 20021023 A 3350 BR964411 LIGHT BOEING 737 73733A 1384673 NM ZONE 900 - LAV INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 168AW 23629 DURING INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHT ON AFT LT GALLEY WALL INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE EMERGENCY ESCAPE PATH LIGHT ON AFT LT GALLEY WALL, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002111900010 20021119 00010 NM 2002 11 19 AWXA200201050 1 20021001 A 5754 65C2668722 SKIN BOEING 737 7373G7 1384595 NM NR 6 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 MCN - MAJOR REPAIR - DURING C-12 CHECK A 1/4 INCH CRACK WAS FOUND AT 4 EACH RIVETS AT THE LOWER TRAILING EDGE OF THE RT WING NR 6 SLAT, JUST BELOW THE INBOARD AUXILIARY TRACK WS 580. MAINTENANCE REMOVED DAMAGED AREA OF NR 6 SLAT AT LOWER TR AILING EDGE; FABRICATED A DOUBLER AND FILLER; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01, PG. 216. 2 L 7 2 4F RT A16WE 2002111900011 20021119 00011 NE 2002 11 19 AWXA200201051 2 20021024 A 7323 GOVERNOR BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE NR 2 ENGINE FLUCTUATES A AWXA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 28 913AW 22207 FLT 0488 - ON TAKEOFF ROLL, AUTO THROTTLES AND EPR MISMATCHED, ADJUSTED NR 2 ENGINE TO 1.58. AFTER LIFT OFF RT EPR JUMPE D TO 1.70, AFTER REDUCING RT ENGINE EPR DROPPED TO 1.24 FLUX FROM 1.65 TO 1.25. CONTINUED TO FLUX AFTER DISCON AUTO THRO T. RETURNED TO PHX LANDED W/O EVENT. MAINT R&R NR 2 ENGINE FUEL FLOW GOV. TESTED NR 2 ENG P1 SYS AIR TUBES, TEST WITHIN LIMITS. VENDOR TEST OF FUEL FLOW GOV COULDN`T CONFIRM REASON FOR REMOVAL. DISASSEMBLY OF UNIT REVEALED GOV SERVO SEAL WORN, TACH SERVO SPRING & GOV PRELOAD SPRING DISBONDED. VENDOR STATED DISCREPANCIES WERE NOT SIGNIFICANT ENOUGH TO CAUS E ENG FLUX. PARTS REPLACED AS NEEDED, FUNCTION TEST ACCOMPLISHED, UNIT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002111900012 20021119 00012 EU 2002 11 19 AWXA200201052 1 20021027 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU ZONE 263 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 638AW 2962 334 455 DURING INSPECTION EMERGENCY LIGHT SYSTEM FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE LT AFT EMERGENCY POWER SUPPLY UNIT (13WL) IAW AMM 33-51-38, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002111900013 20021119 00013 NM 2002 11 19 AWXA200201053 1 20021027 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM ROW 11 LT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 DURING A CHECK EMERGENCY ESCAPE PATH LIGHTS FAILED OPERATIONAL TEST ON TASKCARD I1M05002. MAINTENANCE REMOVED AND REPLAC ED THE EMERGENCY POWER SUPPLY BATTERY PACK AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002111900014 20021119 00014 NM 2002 11 19 AWXA200201054 1 20021026 A 5270 AN32101 SWITCH BOEING 737 737375 13844BN NM PAX DOOR MALFUNCTIONED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 336AW 23707 FLT 0836 - DURING POWER UP ON PHX RUNWAY EN ROUTE FOR LGB, THE FORWARD ENTRY DOOR WARNING LIGHT ILLUMINATED, REJECTED TA KEOFF AT 64KTS. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR WARNING SWITCH, OPERATIONAL TEST WAS GOOD IAW BM M 52-71-11-201. 2 L 7 2 4F RT A16WE 2002111900015 20021119 00015 NM 2002 11 19 AWXA200201056 1 20021007 A 5310 651960337 CREASE BEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 DURING C-20 CHECK A 1/2 INCH CRACK WAS FOUND ON CREASE BEAM STRINGER 17 LT, BS 360 - BS 380. MAINTENANCE REMOVED WEBS BE TWEEN BS 360 TO BS 400 AND BS 400 TO BS 420; CUT STRINGER 17 AT BS 396; FABRICATED A REPAIR ANGLE; INSTALLED STRINGER RE PAIR AND WEBS IAW B737-200 SRM 51-40-4, FIG. 1, PG. 1, AND SRM 51-30-2, PG. 2. 2 L 7 2 4F RT A16WE 2002111900016 20021119 00016 NM 2002 11 19 AWXA200201058 1 20021029 A 2170 1808494 COALESCER BAG BOEING 737 737277 1384570 NM CABIN CONTAMINATED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 178AW 22645 FLT 0221 - EN ROUTE FROM PHX TO AUS PASSENGER AT SEAT ROW 18 COMPLAINED OF NOXIOUS ODOR THAT CAUSED EYES TO IRRITATE. FL IGHT ATTENDANT ALSO SMELLED NOXIOUS ODOR FROM REAR OF CABIN TO SEAT ROW 6, ODOR EVEN CIRCULATED INTO THE FLIGHT DECK ARE A, DIVERTED TO SAT AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE TRIED TO DUPLICATE ODOR BY RUNNING BOTH PACKS WITH APU, AND THEN WITH BOTH ENGINES, NO ODORS WERE NOTED. INSPECTED BOTH PACK BAYS, THE OVERHEAD DUCTS, THE ENGINE AND APU, AND THE CARGO COMPARTMENT AREA, NO DISCREPANCIES WERE NOTED. FOUND COALESCER BAGS EXTREMELY CONTAMINATED, REPLACED BOTH COAL ESCER BAGS. 2 L 7 2 4F RT A16WE 2002111900017 20021119 00017 NM 2002 11 19 AWXA200201059 1 20021029 A 3350 LIGHT BOEING 737 7373G7 1384595 NM ROW 15 LT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 309AW 24711 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A LOOSE WIR E AT CONNECTOR PIN, REPINNED CONNECTOR, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002111900018 20021119 00018 NM 2002 11 19 AWXA200201060 1 20021028 A 2120 87292325V04 COMPUTER AIRBUS A319 A319132 3930340 NM ZONE 120 MALFUNCTIONED A AWXA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 WP 28 802AW 5140 23 924 FLT 0472 - ON TAXI OUT AT PHX RECEIVED ECAM MESSAGE FOR AVIONICS VENT FAULT, A BURNING ODOR WAS ALSO NOTICED IN THE CABI N AREA. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER IAW AMM 21-26-34, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002111900019 20021119 00019 EU 2002 11 19 AWXA200201061 1 20021026 A 2920 C203740001 SERVO AIRBUS 320 A320232 3930326 EU ZONE 741 DEFECTIVE A AWXA O OTHER J G WARNING INDICATION MULTIPLE FAILURE DE DESCENT 1 WP 28 642AW 584 FLT 0823 - AT DECENT INTO PHX RECEIVED A BSCU CHANNEL NR 1 FAULT, & HYD BLUE RESERVOIR LOW AIR PRESSURE MESSAGE. DECLAR ED AN EMER, A/C LANDED W/O EVENT. MAINT CHECKED BLUE HYD SYS RESERVOIR QTY WHEN A/C ARRIVED AT GATE; RESERVOIR QTY GOOD. RESERVOIR AIR PRESSURE WAS AT 75 PSI. AS PRECAUTION R & R BLUE HYD RESERVOIR PRESS SWITCH, OPS AND LEAK CHECK GOOD. BR AKE SERVO VALVE FAULTED ON DISPLAY SYSTEM. REMOVED AND REPLACED BRAKE SERVO VALVE, OPERATIONAL & LEAK CHECK GOOD. BRAKE SERVO VALVE WAS NOT TESTED, UNIT WAS OVERHAULED AND RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002111900020 20021119 00020 NM 2002 11 19 AWXA200201062 1 20021030 A 2121 FAN BOEING 737 737277 1384570 NM CABIN AIR MALFUNCTIONED A AWXA H DEACTIVATE SYST/CIRCUITS B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION DE DESCENT 1 WP 28 186AW 22653 ON DESCENT, AT APPROX 17,000 FT, AN ACRID BURNING ODOR BEGAN IN CABIN AT SEAT ROWS 5 AND 6, ODOR SPREAD THRU CABIN AND INTO COCKPIT. TURNED GASPER FAN OFF AND BOTH PACKS TO FULL COLD, ODOR DIMINISHED BUT STILL LINGERED. FLT ATTENDANT PULLE D ALL CIRCUIT BREAKERS IN BOTH GALLEYS AS PRECAUTION. MAINT TROUBLESHOT & ISOLATED PROBLEM TO PASSENGER CABIN A/C FAN, R EMOVED AND REPLACED CABIN AIR FAN IAW BMM 21-24-21. RESET GALLEY CIRCUIT BREAKERS, OPERATIONAL CHECK OF GALLEY AND CABIN AIR FAN WAS GOOD. VENDOR FUNCTIONAL TEST OF CABIN AIR (GASPER FAN) S/N AA-39653 CONFIRMED FAILURE OF UNIT. FAN WAS FOUN D TO BE VERY NOISY AND HAD ONE PHASE OUT. 2 L 7 2 4F RT A16WE 2002111900021 20021119 00021 EU 2002 11 19 AWXA200201064 1 20021101 A 3350 1013101 SIGN AIRBUS 320 A320232 3930326 EU ROW 10 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 605AW 543 FLIGHT CREW REPORTED THE EMERGENCY FLOOR LIGHT AT SEAT ROW 10 LT WAS BROKEN OFF OF THE LIGHT FIXTURE. MAINTENANCE REMOVE D AND REPLACED EMERGENCY FLOOR LIGHT EXIT SIGN AT SEAT ROW 10 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002111900022 20021119 00022 2002 11 19 AWXA200201065 4 20021101 A 3414 2083111 INDICATOR BOEING 737 737300 1384610 NM AIRSPEED MALFUNCTIONED A AWXA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 WP 28 323AW 23684 FLT 0491 - ON TAKEOFF AT PHX EN ROUTE FOR DEN AT 80 KTS THE FIRST OFFICERS AIRSPEED INDICATOR WAS INDICATING ZERO, ABORT ED TAKEOFF AT 90 KTS. AFTER TURNING OFF RUNWAY FIRST OFFICERS AIRSPEED FLAG CAME INTO VIEW. MAINTENANCE PERFORMED POWER UP TEST OF AIR SPEED INDICATOR, POWER UP WAS GOOD, NO FLAGS INDICATED. PERFORMED PITOT STATIC TEST FIRST OFFICERS PITOT STATIC INDICATED UP TO 180 KTS , OPERATION WAS NORMAL IAW BMM 34-12-00-501. 2 L 7 2 4F RT A16WE 2002111900023 20021119 00023 NM 2002 11 19 SWAA022684 1 20021114 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002111900024 20021119 00024 2002 11 19 SWAA022685 4 20021113 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002111900025 20021119 00025 NM 2002 11 19 SWAA022686 1 20021113 A 3350 07912 COVER BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER MISSING IN AFT CABIN. INSTALLED COVER PER MM. 2 L 7 2 4F A16WE 2002111900026 20021119 00026 NM 2002 11 19 SWAA022687 1 20021112 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002111900027 20021119 00027 NM 2002 11 19 SWAA022688 1 20021112 A 5311 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002111900028 20021119 00028 NM 2002 11 19 SWAA022689 1 20021112 A 5754 65C26686 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND NR 1 L/E SLAT CRACKED AT LOWER SKIN. REPAIRED NR 1 L/E SLAT PER SRM. 2 L 7 2 4F RT A16WE 2002111900029 20021119 00029 NM 2002 11 19 SWAA022691 1 20021112 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002111900030 20021119 00030 NM 2002 11 19 SWAA022692 1 20021112 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 460, STR 10L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2002111900031 20021119 00031 NM 2002 11 19 SWAA022693 1 20021114 A 5241 6969854 FRAME BOEING 737 7373H4 1384600 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT AFT LOWER CORNER. REPAIRED DOOR FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002111900032 20021119 00032 NM 2002 11 19 SWAA022694 1 20021112 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 7237E, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002111900033 20021119 00033 NM 2002 11 19 SWAA022695 1 20021114 A 5754 65C26686 SLAT BOEING 737 7373Q8 1384670 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT CRACKED AT AFT ROW OF FASTENERS. REPAIRED NR 2 L/E SLAT PER SRM. 2 L 7 2 4F RT A16WE 2002111900034 20021119 00034 NM 2002 11 19 AWXA200201066 1 20021102 A 2910 SELECTOR VALVE BOEING 757 7572G7 1384963 NM HYD SYSTEM FAILED A AWXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 28 909AW 24522 FLT 0035 - AFTER TAXI TO RUNWAY & SETTING THE PARKING BRAKES, BRAKE PRESSURE DROPPED TO 1150, RETURNED TO GATE. MAINTENA NCE REMOVED AND REPLACED THE PARKING BRAKE ACCUMULATOR IAW BMM 32-44-05, AND HYDRAULIC ALTERNATE BRAKE SELECT VALVE IAW 32-41-04. OPERATIONAL AND LEAK CHECKS WERE GOOD. TEARDOWN OF HYD BRAKE SELECT VALVE, CONFIRMED FAILURE OF UNIT, PROBLEM WAS IDENTIFIED AS WORN O-RINGS AND SEALS. UNIT WAS OVERHAULED, TESTED, AND RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2002111900035 20021119 00035 2002 11 19 SWAA022667 4 20021111 A 2565 65C19901 CABLE BOEING 737 7372T4 1384492 NM FWD SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002111900036 20021119 00036 NM 2002 11 19 SWAA022671 1 20021111 A 7700 20805 CABLE BOEING 737 7372H4 138448C NM NR 2 ENGINE FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 NR 2 ENGINE THROTTLE WILL NOT ADVANCE. REMOVED AND REPLACED NR 2 ENGINE AFT TELEFLEX CABLE PER MM. 2 L 7 2 4F A16WE 2002111900037 20021119 00037 NM 2002 11 19 AWXA200201068 1 20021028 A 5320 655966425 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON INBOARD UPPER RADIUS OF TRANSITION STRINGER CLIP AT BS 360, STR 4 LT. MAIN TENANCE REMOVED THE DAMAGED STRINGER AT BS 360, STR 4 LT; FABRICATED A NEW REPLACEMENT STRINGER CLIP; INSTALLED REPAIR P ART IAW B737-300 SRM 51-40-02, PG. 10 & 45, FIG. 12 & 14. 2 L 7 2 4F RT A16WE 2002111900038 20021119 00038 2002 11 19 SWAA022653 4 20021111 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002111900039 20021119 00039 NM 2002 11 19 SWAA022656 1 20021110 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 2, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002111900040 20021119 00040 NM 2002 11 19 SWAA022657 1 20021110 A 5330 6545866 SKIN BOEING 737 7373H4 1384600 NM KEEL BEAM CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED C3 CHECK, FOUND LEFT FUSELAGE KEEL BEAM SKIN CRACKED AT BS 695. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002111900041 20021119 00041 NM 2002 11 19 SWAA022658 1 20021111 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 773, LBL 13. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002111900042 20021119 00042 NM 2002 11 19 SWAA022661 1 20021111 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME BROKEN AT BS 767, STR 13R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002111900043 20021119 00043 NM 2002 11 19 SWAA022663 1 20021111 A 5311 6940367 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L AND STR 15L. REMOVED AND REPLACED SH EAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002111900044 20021119 00044 NM 2002 11 19 SWAA022664 1 20021111 A 2731 183A8401 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEV ATOR TAB MAST FITTING OTBD BUSHING. 2 L 7 2 4F RT A16WE 2002111900045 20021119 00045 NM 2002 11 19 AWXA200201071 1 20021015 A 5315 BAC1518338 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 DURING C-08 CHECK A 2 INCH CRACK WAS FOUND ON UPPER FLOORBEAM "T" CAP AT SEAT TRACK ATTACH POINT BS 700, RBL 25. MAINTEN ANCE CUTOUT DAMAGED SECTION OF FLOORBEAM AT BS 700, RBL 25, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; F ABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM, 2 EACH SUPPORT ANGLES, 2 EACH REINFORCEMENT STRAPS, A RADIUS FILLER, A ND A CLIP; AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, PG. 201-205, FIG. 201. 2 L 7 2 4F RT A2NM 2002111900046 20021119 00046 2002 11 19 SWAA022641 4 20021108 A 2565 61621469 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FLAP TORN. REMOVED AND REPLACED SLIDE PER M M. 2 L 7 2 4F RT A16WE 2002111900047 20021119 00047 2002 11 19 SWAA022643 4 20021109 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 416WN 32453 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002111900048 20021119 00048 NM 2002 11 19 SWAA022644 1 20021108 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, ABOVE STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002111900049 20021119 00049 NM 2002 11 19 SWAA022645 1 20021110 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002111900050 20021119 00050 NM 2002 11 19 SWAA022646 1 20021110 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND FWD ENTRY DOOR BOTTOM HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002111900051 20021119 00051 NM 2002 11 19 AWXA200201072 1 20021015 A 5315 BAC1518338 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 DURING C-08 CHECK A 3/4 INCH CRACK WAS FOUND ON UPPER FLOORBEAM "T" CAP AT SEAT TRACK ATTACH POINT BS 700, RBL 46. MAINT ENANCE CUTOUT DAMAGED SECTION OF FLOORBEAM AT BS 700, RBL 46, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM, 2 EACH SUPPORT ANGLES, 2 EACH REINFORCEMENT STRAPS, A RADIUS FILLER, AND A CLIP; AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, PG. 201-205, FIG. 201. 2 L 7 2 4F RT A2NM 2002111900052 20021119 00052 NM 2002 11 19 SWAA022647 1 20021110 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED 1/2D CHECK, FOUND LEFT WING OTBD AFT FLAP DELAMINATED ON LOWER SURFACE. REPAIRED LEFT OTBD AFT FLAP PE R SRM. 2 L 7 2 4F RT A16WE 2002111900053 20021119 00053 2002 11 19 SWAA022648 4 20021110 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM AFT SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE, FWD AND AFT ATTACHMENT BRACKETS CRACKED. REMOVED AND REPLACED FWD AND AFT ATTACHMENT BRACKETS PER MM. 2 L 7 2 4F RT A16WE 2002111900054 20021119 00054 NM 2002 11 19 SWAA022649 1 20021109 A 3210 6582770 FITTING BOEING 737 7373Q8 1384670 NM LT/RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG FWD WALKING BEAM FITTINGS CORRODED. REMOVED AND REPLACED BOTH LEFT AND RIGHT MLG FWD WALKING BEAM FITTINGS PER MM. 2 L 7 2 4F RT A16WE 2002111900055 20021119 00055 NE 2002 11 19 SWAA022651 2 20021107 A 7320 CFM56 ENGINE BOEING 737 7373H4 1384600 NM CFM56 CFM56* 13802 NE RT WING FLAMED OUT A SWAA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 29 645SW 28330 725920 NR 2 ENGINE FLAMEOUT, DECLARED EMERGENCY, AIR TURNBACK, NR 2 ENGINE FLAMED OUT DURING CLIMB. REMOVED AND REPLACED MEC A ND FUEL PUMP, PROBLEMS STILL EXIST. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002111900056 20021119 00056 NM 2002 11 19 AWXA200201075 1 20021017 A 5315 BAC1518338 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER CAP OF CABIN FLOORBEAM BS 377.5, LBL 55. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOORBEAM AT BS 377.5, LBL 55; FABRICAT ED 2 EACH ANGLES, A STRAP, A FILLER, AND A SHIM; AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, PG. 216-218, FIG. 205. 2 L 7 2 4F RT A2NM 2002111900057 20021119 00057 2002 11 19 SWAA022632 4 20021107 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002111900058 20021119 00058 NM 2002 11 19 SWAA022633 1 20021106 A 5311 6935365 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L AND STR 14L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002111900059 20021119 00059 2002 11 19 SWAA022637 4 20021107 A 2565 6567380 WINDOW BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 706SW 27840 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND VIEWING WINDOW MISSING. INSTALLED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2002111900060 20021119 00060 NM 2002 11 19 SWAA022638 1 20021106 A 5312 6546568 BULKHEAD BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED C3 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT 6 O'CLOCK POSITION RADIATING FROM RIVET AT THE PERIPHERY OF THE PRESS PLUG. REPAIRED BULKHEAD PER SRM AND SWA EA. 2 L 7 2 4F A16WE 2002111900061 20021119 00061 NM 2002 11 19 SWAA022626 1 20021106 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 796SW 27889 DURING SCHEDULED PM CHECK, FOUND EEPLS WIRES EXPOSED AT ROW 11. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002111900062 20021119 00062 NM 2002 11 19 SWAA022627 1 20021106 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 500C + 16, STR 16L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2002111900063 20021119 00063 NM 2002 11 19 SWAA022629 1 20021106 A 5520 0550009 TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED C4 CHECK, FOUND LEFT ELEVATOR TAB CRACKED AT NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS. REMOVED AND REPL ACED LT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002111900064 20021119 00064 2002 11 19 SWAA022630 4 20021105 A 2565 65C19901 CABLE BOEING 737 7375H4 138449D NM AFT SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002111900065 20021119 00065 2002 11 19 SWAA022631 4 20021105 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002111900066 20021119 00066 NM 2002 11 19 AWXA200201076 1 20021010 A 5730 114N160322 SKIN BOEING 757 7572S7 1384962 NM LT WING LE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 DURING C-08 CHECK REPAIR OF DELAMINATED AREA OF LT WING LEADING EDGE REQUIRED TO TERMINATE MONITOR. WS 106 TO WS 169 LT. MAINTENANCE REMOVED PREVIOUS REPAIR AND CUTOUT A 11 X 6.5 INCH DELAMINATED AREA OF LT INBOARD FIXED WING LEADING EDGE A T WS 106 TO WS 169; APPLIED FIBERGLASS REPAIR AND CONDUCTIVE COATING PER B757-200 SRM 51-70-08, FIG. 5, PARA 4.A. 2 L 7 2 4F RT A2NM 2002111900067 20021119 00067 NM 2002 11 19 AWXA200201078 1 20021018 A 5320 453N170411 SUPPORT ANGLE BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 DURING C-08 CHECK A 1 3/4 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT SIDEWALL SUPPORT ANGLE AT BS 1630, STR 21 RT. MA INTENANCE REMOVED DAMAGED AFT CARGO COMPARTMENT SIDEWALL SUPPORT ANGLE AT BS 1630, STR 21 RT; FABRICATED A NEW REPLACEME NT SUPPORT ANGLE; AND INSTALLED REPAIR PART IAW B757-200 SRM 51-70-13, FIG. 1, PG. 1. 2 L 7 2 4F RT A2NM 2002111900068 20021119 00068 NM 2002 11 19 VNAA0211013 1 20021111 A 3300 321473 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 425JS 18589 7469 3037 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT WORKING AT ROWS 6 TO 9. MAINTENANCE INSPECTED AND REPLACED THE EM ERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002111900069 20021119 00069 NM 2002 11 19 VNAA0211015 1 20021113 A 3200 BRAKE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 472PS 3008 THE CREW REPORTED THAT THE BRAKES WERE NOT WORKING PROPERLY. MAINTENANCE INSPECTED AND BLED THE HYDRAULIC SYSTEM IN AC CORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003062500120 20030625 00120 NM 2003 6 25 AWXA200201082 1 20021104 A 2121 6454052 FAN BOEING 737 73733A 1384673 NM CABIN SEIZED A AWXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 164AW 13774 23625 EN ROUTE FROM DFW TO LAS AT CRUISE THE FLIGHT ATTENDANT REPORTED A BURNING ODOR, TURNED OFF RECIRULATION FAN AND BURNING ODOR DISSIPATED. RECIRCULATION FAN REMAINED OFF FOR REST OF THE FLIGHT WITH NO FURTHER EVENTS REPORTED. MAINTENANCE R EMOVED AND REPLACED THE RECIRCULATION FAN IAW BMM 21-21-31, OPERATIONAL CHECK WAS GOOD. VENDOR TEARDOWN OF CABIN AIR RE CIRCULATION FAN (S/N 3412) CONFIRMED FAILURE OF UNIT. IMPELLER WAS FOUND FROZEN DUE TO MOTOR BEARINGS COMING APART. UN IT WAS REPAIRED IAW OHM 21-25-12. NO REPLACEMENT PART NUMBERS LISTED BY VENDOR. 2 L 7 2 4F RT A16WE 2002111900070 20021119 00070 NM 2002 11 19 AWXA200201083 1 20021030 A 3260 848401 PROXIMITY SENSOR AIRBUS A319 A319132 3930340 NM ZONE 700 MALFUNCTIONED A AWXA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 28 810AW 1116 FLT 0241 - ON APPROACH INTO PHX EN ROUTE FROM YYC A MLG CONTROL INTERFACE UNIT (LGCIU) NR 1 FAULT APPEARED ON ECAM. AMBE R XXX INDICATED ABOVE WHEELS ON THE WHEEL PAGE. A GO-AROUND WAS ACCOMPLISHED AND THE MLG WAS RECYCLED, AMBER XXX STILL I NDICATED ABOVE THE WHEELS (WHEELS INDICATED GREEN). A NORMAL FULL FLAP LANDING WAS ACCOMPLISHED WITH MINIMAL REVERSE USE D ON ROLL OUT, NO FURTHER PROBLEMS NOTED. MAINTENANCE REVIEWED FAULT DISPLAY SYS THAT INDICATED A PROBLEM WITH LT MLG DO OR CLOSED PROXIMITY SENSOR. FOUND RESISTANCE READING HIGH AT 15 TO 16.5 OHMS, SHOULD READ 13 OHMS. REMOVED AND REPLACED PROXIMITY SENSOR BITE TEST OF LGCIU NR 1 WAS GOOD. CYCLED MLG DOOR SEVERAL TIMES, NO FAULTS NOTED. 2 L 7 2 4F RT A28NM 2002111900071 20021119 00071 EU 2002 11 19 AWXA200201084 1 20021105 A 3150 WARNING SYSTEM AIRBUS 320 A320231 3930325 EU COCKPIT FALSE ACTIVATION A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 621AW 053 FLT 0447 - ON TAKEOFF ROLL AT SMF EN ROUTE FOR PHX AFTER FLEX THRUST SET RECEIVED AUDIO ANNUNCIATION OF "RETARD" "RETARD ", REJECTED TAKEOFF (LOW SPEED). EXITED RUNWAY, RECONFIGURED SETTINGS, AND TOOK OFF WITHOUT FURTHER EVENT. 2 L 7 2 4F RT A28NM 2002111900072 20021119 00072 NM 2002 11 19 AWXA200201085 1 20021106 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM LAV FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 157AW 23779 FLIGHT CREW REPORTED A CABIN EMERGENCY FLASHLIGHT WAS DISCHARGED. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002111900073 20021119 00073 EU 2002 11 19 AWXA200201088 1 20021108 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU ZONE 263 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 40993 55 DURING INSPECTION THE EMERGENCY LIGHT SYSTEM FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY POWER SUPPL Y UNIT (13WL), OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2002111900074 20021119 00074 NM 2002 11 19 AWXA200201102 1 20021110 A 2560 P4010021 BATTERY BOEING 757 7572G7 1384963 NM LAV FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 908AW 24233 FLIGHT CREW REPORTED THAT THE EMERGENCY FLASHLIGHT AT THE L-4 DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L-4 DOOR EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002111900075 20021119 00075 NM 2002 11 19 AWXA200201103 1 20021111 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM ZONE 263 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 817AW 5200 1373 DURING INSPECTION THE EMERGENCY LIGHTS SYSTEM FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE AFT LT EMERGENCY POWER S UPPLY UNIT (13WL), FUNCTIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2002111900076 20021119 00076 NM 2002 11 19 AWXA200201104 1 20021111 A 5210 FE174001 DAMPER AIRBUS A319 A319132 3930340 NM PAX DOOR DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 DURING INSPECTION THE R-1 EMERGENCY DOOR ASSIST CYCLINDER WAS FOUND LOW. MAINTENANCE SERVICED THE R-1 EMERGENCY DOOR ASS IST CYCLINDER TO THE PROPER LEVEL. 2 L 7 2 4F RT A28NM 2002111900077 20021119 00077 NM 2002 11 19 AWXA200201106 1 20021104 A 3397 E0053R8B3ASNF CONNECTOR AIRBUS A319 A319132 3930340 NM ROW 20 LT DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 813AW 1350 DURING B-02 CHECK THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 20 LT. MAINTENANCE REMO VED AND REPLACED A BAD PIN ON CONNECTOR 7260VC9 AT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT SEAT ROW 20 LT IAW ESPM 20-4 8-24, PG. 13. OPERATIONAL CHECK WAS GOOD IAW AMM 33-51-00, PG. 502, SUBTASK 33-51-00-710-050. 2 L 7 2 4F RT A28NM 2002111900078 20021119 00078 NM 2002 11 19 AWXA200201107 1 20021111 A 2560 P4010021 BATTERY BOEING 757 7572S7 1384962 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 906AW 23568 DURING C-08 CHECK THE EMERGENCY FLASHLIGHT AT THE L-2 DOOR FLIGHT ATTENDANT SEAT WAS FOUND INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE EMERGENCY FLASHLIGHT BATTERY AT THE L-2 DOOR FLIGHT ATTENDANT SEAT IAW BMM 25-60-00, PG. 1, AND AW2 560010. 2 L 7 2 4F RT A2NM 2002111900079 20021119 00079 NM 2002 11 19 AWXA200201108 1 20021112 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM ZONE 200 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 DURING INSPECTION THE LT EXIT ROW WALL MOUNTED EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE LT EXIT ROW WALL MOUNTED EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002111900080 20021119 00080 NM 2002 11 19 AWXA200201109 1 20021112 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM BS 975 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 DURING INSPECTION THE L-2 DOOR WALL MOUNTED EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR WALL MOUNTED EMERGENCY EXIT SIGN BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002111900081 20021119 00081 NM 2002 11 19 AWXA200201110 1 20021112 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM BS 975 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 DURING INSPECTION THE R-2 DOOR WALL MOUNTED EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR WALL MOUNTED EMERGENCY EXIT SIGN BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002111900082 20021119 00082 2002 11 19 AWXA200201111 4 20021112 A 3460 FMC AIRBUS A319 A319132 3930340 NM COCKPIT MALFUNCTIONED A AWXA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CR CRUISE 1 WP 28 805AW 1049 FLT 0822 - EN ROUTE FROM PHX TO BOS FT MANAGEMENT GUIDANCE COMPUTER (FMGC) NR 2 FAILED, DIVERTED TO CMH AND LANDED WITHO UT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FMGC NR 2 IAW AWA; NAV DATA UPLOADED IAW T/C A1B34321. FUNCTIONAL TEST GOOD. UNIT CHECKED AND NO PROBLEMS FOUND. RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002111900083 20021119 00083 NM 2002 11 19 AWXA200201112 1 20021029 A 5315 AND101362404 FLOORBEAM BOEING 737 7373U3 13844CC NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 335AW 28740 DURING C-04 CHECK 1 INCH SCATTERED SPOTS OF CORROSION WERE FOUND ON UPPER SURFACE OF FLOORBEAM BS 294, FROM RBL 28 TO RB L 54. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOORBEAM AT BS 294, RBL 28 TO RBL 54; FABRICATED 6 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-12, FIG. 1, PG. 5. 2 L 7 2 4F RT A16WE 2002111900084 20021119 00084 NM 2002 11 19 AWXA200201113 1 20021029 A 5315 654587574 FLOORBEAM BOEING 737 7373U3 13844CC NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 335AW 28740 DURING C-04 CHECK 1 INCH SCATTERED SPOTS OF CORROSION WERE FOUND ON FLOORBEAM ADJACENT TO THE R-1 DOOR, BS 311 TO BS 327 . MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOORBEAM BS 311 TO BS 327; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG 65-45875-74; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-15, PG. 14-15. 2 L 7 2 4F RT A16WE 2002111900085 20021119 00085 NM 2002 11 19 AWXA200201114 1 20021023 A 5414 65C26301 FAIRING BOEING 737 7373U3 13844CC NM RT PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 335AW 28740 DURING C-04 CHECK A 1 INCH CRACK WAS FOUND AT THE INBOARD FORWARD UPPER CORNER OF THE AFT CANOE FAIRING, RT ENGINE PYLON . MAINTENANCE CUTOUT CRACKED AREA OF AFT CANOE FAIRING, RT ENGINE PYLON; FABRICATED A FILLER AND DOUBLER; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 54-50-70, FIG. 204. 2 L 7 2 4F RT A16WE 2002111900086 20021119 00086 NM 2002 11 19 AWXA200201117 1 20021027 A 5753 6002632169 SKIN BOEING 737 7373U3 13844CC NM LT WING TE FLAP CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 335AW 28740 DURING C-04 CHECK THE LT WING OUTBOARD FLAP INBOARD LOWER MID FLAP LEADING EDGE SKIN WAS FOUND CHAFED. MAINTENANCE CUTOU T CHAFED AREA OF INBOARD LOWER MID FLAP LEADING EDGE SKIN; FABRICATED A REPAIR DOUBLER; AND INSTALLED REPAIR PART IAW B7 37-300 SRM 57-30-01, FIG. 208. 2 L 7 2 4F RT A16WE 2002111900087 20021119 00087 NM 2002 11 19 AWXA200201119 1 20021113 A 3350 CHARGER BOEING 737 73733A 1384673 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 DURING C-19 CHECK THE LT AFT OVERHEAD EMERGENCY BATTERY POWER SUPPLY / CHARGER UNIT FAILED FUNCTION TEST. MAINTENANCE RE MOVED AND REPLACED THE L./H AFT OVERHEAD EMERGENCY POWER SUPPLY UNIT IAW BMM 33-51-51, PG. 206-207. 2 L 7 2 4F RT A16WE 2002111900088 20021119 00088 NM 2002 11 19 AWXA200201120 1 20021029 A 5310 65C807351 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF CREASE BEAM (INNER CHORD) AT BS 967 - 1006, RB L 52. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED DRAIN TROUGH, 2 EACH SUPPORT ANGLES, AND DAMAGED CREASE BEAM, WEB PAN, CREASE BEAM SPLICE ANGLE BS 946 - 1016; FABRICATED A NEW REPLACEMENT CREASE BEAM, WEB PAN, AND CREASE BEAM SPLICE ANGLE; INSTALLED REPAIR PARTS AND REINSTALLED 2 EACH SUPPORT ANGLES AND DRAIN TROUGH IAW B73 7-300 SRM 51-40-02, PG. 3, 10. 2 L 7 2 4F RT A16WE 2002111900089 20021119 00089 EU 2002 11 19 AWXA200201122 1 20021114 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 657AW 1003 LAS - EEL - DURING INSPECTION THE CABIN EMERGENCY LIGHT SYSTEM FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED BATTERIES AT EMERGENCY POWER SUPPLY UNITS 10WL, 11WL, AND 13WL, OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2002111900090 20021119 00090 2002 11 19 AWXA200201123 4 20021115 A 3460 FMC AIRBUS 320 A320232 3930326 EU NR 1 MALFUNCTIONED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 655AW 1075 FLT 0179 - ON TAKEOFF ROLL AT LAS EN ROUTE FOR MEX AFTER 80 KTS RECEIVED AUTO CALLOUT "RETARD" ABORTED TAKEOFF. NO MESS AGES WERE NOTED; AUTOMATIC FLIGHT SYSTEM (AFS) INDICATED FMGC NR1 FAIL, RESET FMGC NR 1 AND PERFORMED AFS TEST, TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2002111900091 20021119 00091 EU 2002 11 19 AWXA200201124 1 20021115 A 3150 350E0177271616 WARNING SYSTEM AIRBUS 320 A320232 3930326 EU ZONE 120 MALFUNCTIONED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 655AW 11719 1075 FLT 0179 - ON TAKEOFF ROLL AT LAS EN ROUTE FOR MEX AFTER 80 KTS RECEIVED AUTO CALLOUT "RETARD THROTTLE" MESSAGE HEARD 3 -TIMES, ABORTED TAKEOFF (2ND TIME), RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED BOTH NR 1 AND 2 FLT WARNING COMPU TERS IAW AWA, OPERATIONAL TEST WAS GOOD. VENDOR TEST OF FLT WARNING COMPUTER CONFIRMED FAILURE OF UNIT, UNIT FAILED DI SCRETE INPUT TEST FOR INPUT CARDS NR 1 & 2, FAILURE WAS DUE TO A DEFECTIVE INPUT NR 2 BOARD. REPLACED DEFECTIVE INPUT NR 2 BOARD. ALSO CONFIRMED FAILURE OF FLT WARNING COMPUTER FOR UNIT FAILING OUTPUT TEST, FAILURE WAS DUE TO DEFECTIVE OUTP UT SRU, REPLACED OUTPUT SRU. PARTS REPAIRED IAW CMM. 2 L 7 2 4F RT A28NM 2002111900092 20021119 00092 NM 2002 11 19 AWXA200201125 1 20021115 A 3350 321430 BATTERY AIRBUS A319 A319132 3930340 NM ZONE 221 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 816AW 1350 DURING INSPECTION THE L-1 AND R-1 DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE DURING 8-DAY TEST. MAINTENANCE REMOVED AN D REPLACED BATTERY AT EMERGENCY POWER SUPPLY UNIT 11WL ABOVE L-1 DOOR IAW AMM 33-51-38, OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2002111900093 20021119 00093 NM 2002 11 19 AWXA200201127 1 20021025 A 5315 654681138 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF REPAIR "T" CAP AT BS 986, RBL 24 - 57. MAINTENANCE BLENDED CORROSION ON FLOORBEAM "T" CAP UPPER SURFACE AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED 2 EACH FLOOR SUPPORTS AND FLOORBEAM TEE CHORD; FABRICATED 2 EACH SPLICE ANGLES, A SHEAR TIE, FILLER, REPAIR STRAP, AND NEW REPLACEMEN T "T' CAP; INSTALLED REPAIR PARTS AND REINSTALLED 2 EACH FLOOR SUPPORTS IAW AWA E.R. 03-5300-02319-TB2. 2 L 7 2 4F RT A16WE 2002111900094 20021119 00094 NM 2002 11 19 AWXA200201133 1 20021028 A 5320 697816307 WEB BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 DURING C-19 CHECK A 1/2 INCH CRACK WAS FOUND ON SHEAR WEB IN LT MAIN LANDING GEAR WHEEL WELL AT AFT BULKHEAD BS 725, STR 18A LT. MAINTENANCE REMOVED CRACKED WEB AT BS 725, STR 18A LT; FABRICATED A NEW REPLACEMENT WEB, A TAPERED SHIM, AND RE PAIR DOUBLER; AND INSTALLED REPAIR PARTS IAW DWG 65-46877, AND B737-300 SRM 51-10-02, PG. 12. 2 L 7 2 4F RT A16WE 2002111900095 20021119 00095 NM 2002 11 19 AWXA200201134 1 20021028 A 5320 6978163U8 WEB BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 DURING C-19 CHECK A 1 INCH CRACK WAS FOUND ON SHEAR WEB IN RT MAIN LANDING GEAR WHEEL WELL AT AFT END, JUST FORWARD OF B ULKHEAD AT BS 727, STR 18 RT. MAINTENANCE REMOVED CRACKED WEB AT BS 727, STR 18 RT; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-46877; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2 L 7 2 4F RT A16WE 2002111900096 20021119 00096 NM 2002 11 19 AWXA200201136 1 20021029 A 5754 65C2660399 SKIN BOEING 737 73733A 1384673 NM L/E SLAT DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 DURING C-19 CHECK THE NR 3 LEADING EDGE SLAT AT THE OUTBOARD END OF THE TRAILING EDGE WEDGE WAS FOUND TO BE DELAMINATING . MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON THE NR 3 LEADING EDGE SLAT AT THE OUTBOARD END OF THE TRAILING EDGE WEDGE. APPLIED ADHESIVE, REPLACEMENT SKIN, AND DOUBLERS IAW B737-300 SRM 51-70-10, REPAIR NR 22, FIG 31. 2 L 7 2 4F RT A16WE 2002111900097 20021119 00097 NM 2002 11 19 AWXA200201137 1 20021028 A 5754 65C26601180 SKIN BOEING 737 73733A 1384673 NM L/E SLAT DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 DURING C-19 CHECK THE NR 6 LEADING EDGE SLAT INBOARD WEDGE WAS FOUND TO BE DELAMINATING. MAINTENANCE REMOVED DAMAGED ARE A OF SKIN ON THE NR 6 LEADING EDGE SLAT INBOARD WEDGE. APPLIED ADHESIVE, REPLACEMENT SKIN, AND DOUBLERS IAW B737-300 SRM 51-70-10, REPAIR 22, FIG 31. 2 L 7 2 4F RT A16WE 2002111900098 20021119 00098 NM 2002 11 19 AWXA200201138 1 20021028 A 5753 6546435277 SKIN BOEING 737 73733A 1384673 NM TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 DURING C-19 CHECK THE LT OUTBOARD FLAP WAS FOUND DELAMINATED AT THE AFT INBOARD CORNER OF THE TRAILING EDGE WEDGE, LT OU TBOARD FLAP. MAINTENANCE REMOVED DAMAGED AREA OF SKIN AT THE AFT INBOARD CORNER OF THE TRAILING EDGE WEDGE, FABRICATED A REPAIR CORE AND EXTERNAL DOUBLER, INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, REPAIR 11, FIG 20. 2 L 7 2 4F RT A16WE 2002111900100 20021119 00100 EU 2002 11 19 R7MR35306 1 20020604 A 7931 DK040 TRANSMITTER BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL ENG OIL PRESSURE LEAKING B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 485EC 1 S754 PRESSURE TRANSMITTER, LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H3EU E4CE 2002111900101 20021119 00101 EU 2002 11 19 R7MR35308 1 20020129 A 7931 DK040 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU ALLSN 250C 250C20 03013 GL ENG OIL INOPERATIVE B R7MR K NONE P NO WARNING INDICATION IN INSP/MAINT 1 NM 07 105LC 84 S789 PRESSURE TRANSMITTER, UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H3EU E4CE 2002111900102 20021119 00102 SW 2002 11 19 R7MR35455 1 20020314 A 6510 407340339103 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/R HANGAR ROUGH B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 490 53422 TAIL ROTOR HANGER BALL BEARING, ROUGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002111900103 20021119 00103 SW 2002 11 19 R7MR35456 1 20020314 A 6510 407340339103 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/R HANGAR ROUGH B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 178 53422 HANGER TAIL ROTOR BALL BEARING, ROUGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002111900104 20021119 00104 SW 2002 11 19 R7MR35457 1 20020314 A 6510 407340339103 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/R HANGAR ROUGH B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 178 53422 A002726 HANGAR TAIL ROTOR BALL BEARING, ROUGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002111900105 20021119 00105 SW 2002 11 19 R7MR35458 1 20020314 A 6510 407340339103 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/R HANGER ROUGH B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 407SJ 178 53422 HANGAR TAIL ROTOR BALL BEARING, ROUGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U O H2SW E1GL 2002111900106 20021119 00106 NE 2002 11 19 R7MR35467 2 20020531 A 7321 0292928610 SWITCH SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE FUEL METERING INOPERATIVE A R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 396LG 178 3336 NEUTRAL SWITCH INOPERATIVE WHEN HOT( DURING ENGINE OPERATION AND UP TO APPROX 20 MIN AFTER SHUTDOWN). REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2002111900107 20021119 00107 EU 2002 11 19 R7MR35473 1 20020618 A 6720 41800876800 ACTUATOR UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE AUTOPILOT SYS INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 101HN 0162 SMART ELECTRIC MECHANICAL ACTUATOR, UNIT INOPERATIVE. WILL NOT TEST IN AUTOPILOT MODE. SUSPECT INTERNAL SHORT. REPLAC ED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2003011700127 20030117 00127 NM 2003 1 17 PCAA0211133 1 20021118 A 2910 G831810A VALVE DHAV DHC8 DHC8102 2809003 NM LT MLG WW CRACKED A PCAA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 13 849EX 24437 24437 337 WHILE INVESTIGATING HISTORY OF HYDRAULIC FLUID LEAKING IN LEFT GEARWELL, LEFT FORWARD HYDRAULIC QUANTITY LIMITING VALVE WAS FOUND CRACKED. VALVE WAS REPLACED IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2002111900108 20021119 00108 NM 2002 11 19 0203863125 1 20021115 A 2121 TECHNOFAN AIRBUS A319 A319114 3930350 NM A NWAA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 325NB 4677 1483 Received VENT EXTRACT FAULT shortly after takeoff. Crew experienced grinding noise, mild vibration and strong smoke smel l. Returned to IAH and landed uneventfully. Found avionics cooling extract fan 18Q failed. Applied MEL 21-26-02 provisio ns and returned A/C to service. 2 L 7 2 4F RT A28NM 2002111900109 20021119 00109 SO 2002 11 19 C2XA02CL228 1 20021111 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DIRTY A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 15985 145248 EWR FLIGHT#3272 THE CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE.MAINTENANCE INSPECTED AND CLEANED THE EMERGENCY AISLE PATH LIGHT STRIP CONNECTOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002111900110 20021119 00110 WP 2002 11 19 MWEA020702 1 20021118 A 5542 9957485511 RUDDER DOUG DC9 DC981 3022081 WP SKIN SCRATCHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 LOWER LEFT RUDDER SKIN IS SCRATCHED. -- REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER AND RE-BALANCED RUDDER. 2 L 7 2 4F A6WE 2002111900111 20021119 00111 WP 2002 11 19 CALA0200555 1 20021116 A 5311 LONGERON DOUG DC9 DC982 3022082 WP STA 1287 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 98876 49444 INSPECTION FOUND AFT CARGO BELT FRAME CORRODED AT STA 1287, LONGERON 30. THE BELTFRAME WAS REMOVED AND REPLACED IAW SRM 51-30-02. 2 L 7 2 4F A6WE 2002111900112 20021119 00112 WP 2002 11 19 MWEA020700 1 20021118 A 5754 59374231 SLAT DOUG DC9 DC981 3022081 WP LEFT WING ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 LEFT SLAT NUMBER 0 INBOARD IDLER MOUNT BRACKET CLOSE OUT PANEL MOUNT HOLES ARE ENLONGATED. -- FABRICATED AND INSTALLED REPAIR BUSHINGS. 2 L 7 2 4F A6WE 2002111900113 20021119 00113 WP 2002 11 19 MWEA020704 1 20021119 A 5753 5912125502 SPAR CAP DOUG DC9 DC981 3022081 WP FRAME CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 RIGHT OUTBOARD FLAP HAS MODERATE CORROSION ON THE INTERNAL FRAME (LOWER SPAR) AS SEEN THROUGH ACCESS PANEL 1622A. -- R EMOVED AND REPLACED LOWER SPAR CAP. 2 L 7 2 4F A6WE 2002111900114 20021119 00114 WP 2002 11 19 MWEA020705 1 20021119 A 5330 59360023 DOUBLER DOUG DC9 DC981 3022081 WP DOT 213 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FUSELAGE SKIN HAS A DENT STATION 598 BELOW LONGERON 25 LEFT. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002111900115 20021119 00115 WP 2002 11 19 MWEA020706 1 20021119 A 5330 59360023 DOUBLER DOUG DC9 DC981 3022081 WP DOT 212 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FUSELAGE SKIN HAS A DENT AT STATION 598 ABOVE LONGERON 25 LEFT. -- FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002111900117 20021119 00117 NM 2002 11 19 QXEA0201790 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 12 TOP GOUGED IN SEAT ATTACH AREA AT APPROXIMATELY X531.00. REPAIRED IAW DHC-8 200 SRM 51-20-16, PAGE 4, PARAGRAPH C AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002111900118 20021119 00118 NM 2002 11 19 QXEA0201792 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RIGHT HAND INBOARD SEAT TRACK NR 8 TOP CORROSION AND GOUGING IN SEAT ATTACH AREA AT APPROXIMATELY X516.00. REPAIR ED SEAT TRACK IAW RD 8-53-1339, DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002111900119 20021119 00119 NM 2002 11 19 QXEA0201793 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RIGHT HAND INBOARD SEAT TRACK NR 9 BOTTOM CHAFED IN SEAT ATTACH AREA AT APPROXIMATELY X526.00. REPAIRED IAW RD 8- 53-4936, DHC-8 200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002111900120 20021119 00120 NM 2002 11 19 QXEA0201794 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RIGHT HAND INBOARD SEAT TRACK NR 9 BOTTOM CHAFED IN AFT BULKHEAD ATTACH AREA AT APPROXIMATELY X541.00. REPAIRED I AW RD 8-53-4936, DHC8200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002111900121 20021119 00121 NM 2002 11 19 QXEA0201795 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RIGHT HAND INBOARD NR 8 SEAT TRACK FORWARD OUTBOARD FLANGE CORROSION FROM X424.00 TO X427. REPAIRED IAW RD 8-53-1 339, DHC8200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002111900122 20021119 00122 NM 2002 11 19 QXEA0201796 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RIGHT HAND INBOARD NR 8 SEAT TRACK FORWARD INBOARD FLANGE CHAFED FROM X425.00 TO X431.00. REPAIRED IAW RD 8-53-133 9, DHC8200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002111900123 20021119 00123 NM 2002 11 19 HNAA0200078 1 20021114 A 3350 40005130003 SWITCH DHAV DHC8 DHC8102 2809003 NM CABIN INTERMITTENT A HNAA O OTHER O OTHER UK UNKNOWN 1 EA 07 931HA 37486 37486 132 FORWARD RIGHT EMERGENCY EXIT DOOR SIGN INTERMITANT. REPLACED FLIGHT ATTENDANT PANEL NORMAL ON SWITCH, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2002111900124 20021119 00124 NM 2002 11 19 QXEA0201797 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RIGHT HAND INBOARD NR 8 SEAT TRACK INBOARD FLANGE CHAFED FROM X468.00 TO X472.00. REPAIRED IAW RD 8-53-1339, DHC8 200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002111900125 20021119 00125 NM 2002 11 19 QXEA0201798 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RIGHT HAND INBOARD NR 8 SEAT TRACK BOTTOM CHAFED FROM X504.00 TO X515.00. REPAIRED IAW RD 8-53-1339, DHC8200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002111900126 20021119 00126 NM 2002 11 19 QXEA0201799 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RIGHT HAND INBOARD NR 8 SEAT TRACK OUTBOARD FLANGE CHAFED FROM X507.00 TO X517.00. REPAIRED IAW RD 8-53-1339, DHC 8200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002111900127 20021119 00127 NM 2002 11 19 QXEA0201800 1 20021020 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RIGHT HAND INBOARD NR 8 SEAT TRACK BOTTOM GOUGED AT X523.00. REPAIRED IAW RD 8-53-1339, DHC8200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002111900128 20021119 00128 NM 2002 11 19 QXEA0201801 1 20021023 A 5320 FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - FORWARD LEFT BATH TUB FITTING FOR WING TO FUSELAGE JOINT AT FRONT SPAR GOUGED AT FORWARD END. REPAIRED IAW DHC-82 00 SRM 51-20-11 AND HORIZON AIR EA 2-53-439. 2 H 7 2 4T RT A13NM 2002111900129 20021119 00129 NM 2002 11 19 QXEA0201802 1 20021023 A 5320 FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - AFT LEFT BATH TUB FITTING FOR WING TO FUSELAGE JOINT AT FRONT SPAR GOUGED AT AFT END. REPAIRED IAW DHC-8200 SRM 5 1-20-11 AND HORIZON AIR EA 2-53-439. 2 H 7 2 4T RT A13NM 2002111900130 20021119 00130 NM 2002 11 19 QXEA0201803 1 20021023 A 5320 FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - AFT RIGHT BATH TUB FITTING FOR WING TO FUSELAGE JOINT AT FRONT SPAR GOUGED AT AFT END. REPAIRED IAW DHC-8200 SRM 51-20-11 AND HORIZON AIR EA 2-53-439. 2 H 7 2 4T RT A13NM 2002111900131 20021119 00131 NM 2002 11 19 QXEA0201804 1 20021019 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LEFT HAND WING OUTBOARD FLAP UPPER SURFACE HAS CHAFE DAMAGE AT WING STATION YW172.0. REPAIRED IAW RD 8-57-1734 AN D DHC8 200 SRM 51-20-26, PAGE 7. 2 H 7 2 4T RT A13NM 2002111900132 20021119 00132 NM 2002 11 19 QXEA0201805 1 20021019 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LEFT HAND WING, NR 4 FLAP TRACK LOWER OUTBOARD TRACK D HAS PITTING CORROSION IN THREE LOCATION. REPAIRED IAW HORI ZON AIR EA 2-57-205. 2 H 7 2 4T RT A13NM 2002111900133 20021119 00133 NM 2002 11 19 QXEA0201806 1 20021018 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LEFT HAND WING, NR 4 FLAP TRACK UPPER SURFACE TRACK A HAS TWO LOCATIONS OF PITTING CORROSION. REPAIRED IAW HORIZO N AIR EA 2-57-205. 2 H 7 2 4T RT A13NM 2002111900134 20021119 00134 NM 2002 11 19 QXEA0201807 1 20021019 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LEFT HAND WING, NR 4 FLAP TRACK, INBOARD LOWER TRACK D HAS PITTING CORROSION IN TWO LOCATIONS. REPAIRED IAW HORIZ ON AIR EA 2-57-205. 2 H 7 2 4T RT A13NM 2002111900135 20021119 00135 NM 2002 11 19 QXEA0201808 1 20021020 A 7120 TRUSS DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RIGHT HAND SIDE TRUSS MOUNT, LOWER TUBE IS CHAFED NEXT TO IGNITION EXCITERS AND TRANSMITTER. REPAIRED IAW RD 8-54 -036. 2 H 7 2 4T RT A13NM 2002111900136 20021119 00136 NM 2002 11 19 QXEA0201809 1 20021019 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - AIRCRAFT SKIN IS CORRODED UNDER LOWER TCAS ANTENNA MOUNT. REPAIRED IAW DHC-8200 SRM 51-20-11 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002111900137 20021119 00137 EU 2002 11 19 SIMA200230316 1 20021021 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 330AE 340B330 ABI - DURING AN MBV INSPECTION, CARGO RIGHT FRAME AT STATION 658.8 WAS FOUND TO HAVE ONE DENT. RECONTOURED DENT AND PER FORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STAT EMENT 340SDS004554 PARA 1. (M) 2 L 7 2 4T RT A52EU 2002111900138 20021119 00138 EU 2002 11 19 SIMA200230317 1 20021017 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 330AE 340B330 ABI - DURING AN MBV INSPECTION, CARGO RIGHT FRAME AT STATION 677 WAS FOUND TO HAVE TWO DENTS. RECONTOURED DENTS AND PER FORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STAT EMENT 340SDS004527 PARA 2. (M) 2 L 7 2 4T RT A52EU 2002111900139 20021119 00139 EU 2002 11 19 SIMA200230318 1 20021017 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 330AE 340B330 ABI - DURING AN MBV INSPECTION, THE CARGO RIGHT FRAME AT STATION 686.888 WAS FOUND TO HAVE FOUR DENTS. RECONTOURED DENT S AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB RE PAIR STATEMENT 340SDS004527 PARA 1. (M) 2 L 7 2 4T RT A52EU 2002111900140 20021119 00140 EU 2002 11 19 SIMA200230331 1 20021017 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 330AE 340B330 ABI - DURING AN MBV INSPECTION, THE CARGO RIGHT FRAME AT STATION 668 WAS FOUND TO HAVE ONE DENT. RECONTOURED DENT AND P ERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 REPAI R STATEMENT 340SDS004527 PARA 3. (M) 2 L 7 2 4T RT A52EU 2002111900141 20021119 00141 EU 2002 11 19 USAASA02085 1 20021012 A 2560 LATCH AIRBUS 320 A320214 3930316 EU EMERGENCY EXIT BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 110UW 1112 DCA - THE FORWARD, LEFT EMERGENCY EXIT SLIDE ACTUATING LATCH WAS FOUND BROKEN. MAINTENANCE REPLACED THE LATCH ASSEMBLY. ALSO REPLACED THE PIN GUIDE FITTING ASSEMBLY. OPS CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002111900142 20021119 00142 EU 2002 11 19 USAASA02087 1 20021018 A 2120 ODOR AIRBUS A319 A319112 3930323 EU COCKPIT DETECTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 733UW 1205 MSY - FLT 289 - EN ROUTE DCA-MSY, DURING DESCENT INTO MSY, AN ODOR BECAME PRESENT IN BOTH THE COCKPIT AND CABIN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE ELECTRONICS BAYS AND CABIN FOR ODORS. NONE WERE FOUND. TH E ENGINES AND PACK WERE OPERATED. NO ODORS WERE NOTED. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2002111900143 20021119 00143 EU 2002 11 19 USAASA02088 1 20021021 A 3350 321430 BATTERY PACK AIRBUS 320 A320214 3930316 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 105UW 0868 DCA - DURING EMERGENCY LIGHTS TEST, RECEIVED 'EPSU LOAD EMERGENCY R' MESSAGE. MAINTENANCE REPLACED THE RIGHT EMERGENCY LIGHT BATTERY PACK. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2002111900144 20021119 00144 EU 2002 11 19 USAASA02089 1 20021021 A 3230 C247300016 UPLOCK AIRBUS 320 A320214 3930316 EU NLG MALFUNCTIONED A USAA K NONE J WARNING INDICATION CR CRUISE 1 EA 19 121UW 1294 CLT - FLT 926 - EN ROUTE LGA-CLT - WHILE IN CRUISE FLIGHT, A NOSE GEAR 'UNLOCK' LIGHT BECAME ILLUMINATED ON THE LANDING GEAR PANEL, AND AN ECAM MESSAGE 'GEAR NOT UPLOCKED' WAS RECEIVED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR UPLOCK ASSEMBLY. OPERATIONALLY AND LEAK CHECKED GOOD. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2002111900145 20021119 00145 EU 2002 11 19 USAASA02091 1 20021026 A 2810 L83A13610 DRAIN VALVE AIRBUS 320 A320214 3930316 EU RT WING LEAKING A USAA H DEACTIVATE SYST/CIRCUITS K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 116US 1210 PHL - FLT 596 - EN ROUTE SJU-PHL, A FUEL ODOR WAS REPORTED AT THE EMERGENCY EXIT ROW DURING THE FLIGHT. ADDITIONALLY, T HE RIGHT HAND INNER FUEL TANK QUANTITY DECREASED ABOVE NORMAL UNITS. ALL TANK PUMPS WERE TURNED OFF AT GRAVITY FEED ALT ITUDE. FLIGHT LANDED AT PHL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT WING, INNER CELL, WATER DRAIN OUT ER VALVE ASSEMBLY. LEAK CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2002111900146 20021119 00146 NE 2002 11 19 AMWA042655 2 20020825 A 7200 PT6A67DGG ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67 52043 NE LEFT LACK OF LUBE A AMWA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 07 5YV * 9559 UE5 WHILE INFLIGHT FROM PANAMA CITY, FLORIDA THE LEFT ENGINE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED. THE OIL PRESSURE WAS BELOW 60 PSI. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO FIELD WITH NO FURTHER INCIDENT. THE CORRECTIV E ACTION WAS THE THE LEFT GAS GENERATOR AND THE POWER SECTION WAS REPLACED. THE TEARDOWN REPORT REVEALED THAT THE PROPE LLER SHAFT HAS SEIZED AND THERE WAS NO OIL INDICATION ON THE DIPSTICK. THE CAUSE OF THE OVERHEATING DISTRESS TO THE PLA NET GEAR `Y` OCCURRED FROM LACK OF LUBRICATION. 2 L 7 2 4T 4 T RT A24CE E26NE 2002111900147 20021119 00147 NE 2002 11 19 AMWA044723 2 20021103 A 7321 FUEL CONTROL BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67 52043 NE LT ENGINE MALFUNCTIONED A AMWA E ENGINE SHUTDOWN O OTHER LD LANDING 1 CE 07 15YV UE15 AFTER LANDING IN NEW ORLEANS, LOUISIANA ON FLIGHT 5518, THE LEFT ENGINE WENT INTO REVERSE. THEN N-1 INDICATOR REACHED 1 04 PERCENT THE ITT INDICATOR WENT TO 830 DEGREES AND THE TORQUE WENT TO 3800 LBS FOR 5 SECONDS THE LEFT ENGINE WAS THEN SHUTDOWN AND THE AIRCRAFT TAXIED TO GATE WITH NO FURTHER INCIDENT. UPON INSPECTION BY THE MECHANIC, IT WAS FOUND THAT T HE FUEL CONTROL UNIT HAD JUMPED TEETH AND MOVED. THE LEFT ENGINE FUEL CONTROL UNIT WAS RIGGED AS REQUIRED. THE ENGINE WAS DETERMINED TO BE IN BETA AND LIMITS WERE NOT EXCEEDED PER PRATT & WHITNEY MANUAL. THEREFORE NO PARTS WERE USED. 2 L 7 2 4T 4 T RT A24CE E26NE 2002111900148 20021119 00148 NE 2002 11 19 NSVA110302294 2 20021103 A 7261 J221P035 PACKING SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 2 ENGINE CUT A NSVA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 27 294CJ 340B294 WHILE AT CRUISE ALTITUDE PIC NOTICED NR 2 ENGINE OIL PRESSURE AT APPROX 40 PSI AND FLUCTUATING. PRESSURE STEADILY DECRE ASING OVER PERIOD OF APPROX 2 MIN AT WHICH POINT THE RT ENG OIL PRESS LOW INDICATOR ILLUMINATED. CREW RAN CHECKLIST AND SHUT DOWN NR 2 ENGINE. AIRCRAFT LANDED IN LGA WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND FOUND THE ENGINE AND SURROUNDING NACELLE COWLING WAS COATED IN OIL. FAULT ISOLATION REVEALED A PACKING ON THE BB AXIS SEAL WA S CUT ALLOWING THE OIL LEAKAGE. THE BB AXIS SEAL WAS REPLACED AND A GROUND RUN WAS PERFORMED WITHOUT LEAKAGE. THE AIRC RAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2002111900149 20021119 00149 2002 11 19 PNSA021101 4 20021031 A 6122 GOVERNOR FRCHLD SA227 SA227DC 3377521 SW RT ENGINE OUT OF ADJUST A PNSA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 03 892DC DC892B ABORTED TAKEOFF DUE TO LOW TORQUE ON RIGHT ENGINE. MAINTENANCE ADJUSTED PROP GOVERNOR HIGH RPM AND GROUND RAN ENGINE TO TAKEOFF TORQUE. 2 L 7 2 4T RT A18SW 2002111900150 20021119 00150 NM 2002 11 19 SWAA022628 1 20021105 A 3350 6104781 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED SPECIAL VISIT, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS M1197 AND M1137 PEP MM. 2 L 7 2 4F RT A16WE 2002111900151 20021119 00151 EA 2002 11 19 COMA0260648 1 20021115 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 914CA 7012 FLIGHT 6037 EXTERNAL POWER DOOR LEFT OPEN BY GROUND CREW.INSPECTED DORO AND SURROUND; SECURED DOOR. 2 L 7 2 4F RT A21EA 2002111900152 20021119 00152 NM 2002 11 19 SWAA022634 1 20021107 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (3 EA) AT BS 639 AT STR 5R, BS 639 AT STR 1R AND BS 616 AT STR 1R. REMOVED AND REPLACED TIE CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002111900153 20021119 00153 NM 2002 11 19 SWAA022635 1 20021107 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED 1/2D CHECK, FOUND KEEL BEAM CORRODED AT BS 541, STR 28R. REMOVED AND REPLACED SECTION OF KEEL BEAM PER SRM AND SWA EA. 2 L 7 2 4F RT A16WE 2002111900154 20021119 00154 NM 2002 11 19 SWAA022636 1 20021107 A 5524 6545166 BEARING BOEING 737 7373G7 1384595 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED C4 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR CONTROL PUSH ROD AFT BEARING PER MM. 2 L 7 2 4F RT A16WE 2002111900155 20021119 00155 NM 2002 11 19 SWAA022639 1 20021107 A 2560 PH22300L TRACK BOEING 737 7375H4 138449D NM CABIN DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED C1 CHECK, FOUND SEVERAL PHOTO LUMINESCENT FLOOR STRIPS DEBONDED. REMOVED AND REPLACED STRIPS PER MM. 2 L 7 2 4F RT A16WE 2002111900156 20021119 00156 NM 2002 11 19 SWAA022640 1 20021109 A 2560 P2070001 FLASHLIGHT BOEING 737 737317 138447P NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 698SW 23176 AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED AFT LOWER FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2002111900157 20021119 00157 2002 11 19 SWAA022642 4 20021107 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002111900158 20021119 00158 2002 11 19 SWAA022652 4 20021111 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002111900159 20021119 00159 NM 2002 11 19 SWAA022654 1 20021111 A 5610 5717623122 SLIDING WINDOW BOEING 737 7373H4 1384600 NM COCKPIT STUCK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 F/O'S SLIDING WINDOW DOES NOT RELEASE FROM EXTERIOR HANDLE. REMOVED AND REPLACED SLIDING WINDOW ASSY PER MM. 2 L 7 2 4F RT A16WE 2002111900160 20021119 00160 NM 2002 11 19 SWAA022655 1 20021110 A 3350 604222 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED C3 CHECK, FOUND BOTH FWD AND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002111900161 20021119 00161 NM 2002 11 19 SWAA022659 1 20021111 A 3350 61047811 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED PM CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002111900162 20021119 00162 NM 2002 11 19 SWAA022660 1 20021111 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE P ER SRM. 2 L 7 2 4F RT A16WE 2002111900163 20021119 00163 NM 2002 11 19 SWAA022662 1 20021111 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 767, STR 13R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002111900164 20021119 00164 NM 2002 11 19 SWAA022665 1 20021111 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED SERVICE CHECK, FOUND CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW NR 18. RELAMPED EMERGENCY EXIT LI GHT PER MM. 2 L 7 2 4F RT A16WE 2002111900165 20021119 00165 NM 2002 11 19 SWAA022666 1 20021111 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS INOP IN CABIN. RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2002111900166 20021119 00166 2002 11 19 SWAA022668 4 20021112 A 2565 D31355117 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED S LIDE PER MM. 2 L 7 2 4F A16WE 2002111900167 20021119 00167 2002 11 19 SWAA022669 4 20021111 A 2565 D31591478 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002111900168 20021119 00168 NM 2002 11 19 SWAA022670 1 20021111 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE P ER SRM. 2 L 7 2 4F RT A16WE 2002111900169 20021119 00169 NM 2002 11 19 SWAA022672 1 20021112 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE P ER SRM. 2 L 7 2 4F RT A16WE 2002111900170 20021119 00170 NM 2002 11 19 SWAA022673 1 20021112 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 380, STR 14L. REMOVED AND REPLACED STRINGER TIE C LIP PER MM. 2 L 7 2 4F RT A16WE 2002111900171 20021119 00171 NM 2002 11 19 SWAA022683 1 20021114 A 3350 BR2013 TRACK BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 EEPLS PULLED UP AT CABIN FLOOR. REINSTALLED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002111900172 20021119 00172 NM 2002 11 19 SWAA022690 1 20021112 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE P ER SRM. 2 L 7 2 4F RT A16WE 2002111900173 20021119 00173 NM 2002 11 19 SWAA022696 1 20021113 A 5522 65C2574684A SKIN BOEING 737 7373Q8 1384670 NM ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED ELEVATOR PER MM. 2 L 7 2 4F RT A16WE 2002111900174 20021119 00174 NM 2002 11 19 SWAA022697 1 20021112 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPECIAL VISIT, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW NR 2. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2002111900175 20021119 00175 NM 2002 11 19 SWAA022698 1 20021112 A 3350 M01132 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY EXIT LIGHT BATTERY PACK POWER CHARGER INOP. REMOVED AND REPLACED POWER CHARGER PER MM. 2 L 7 2 4F RT A16WE 2002111900176 20021119 00176 EA 2002 11 19 SWIA200211346 1 20021019 A 2740 SWITCH CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB DIRTY A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 417SW 7400 STAN CHANNEL NR 1 INOP MESSAGE CAME ON AND WOULD NOT RESET. CLEANED STAB TRIM ENGAGE SWITCHES. PERFORMED OPERATIONAL C HECK OF HSTCU IAW MM 27-10-00-710-801 AND SELF DIAGONOSTICS OF HSTCU IAW MM 27-41-00-790-801. OPERATIONAL CHECKS SATISF ACTORY. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2002111900177 20021119 00177 EA 2002 11 19 COMA0260649 1 20021116 A 3210 601R386493 ROD CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR BROKEN A COMA O OTHER S AFFECT SYSTEMS CL CLIMB 1 SO 01 952CA 7092 FLIGHT 5459 CABIN ALTITUDE CAUTION MESSAGE - CABIN WOULD NOT PRESSURIZE.REPLACED BROKEN ROD ON CABIN DOOR VENT VALVE. 2 L 7 2 4F RT A21EA 2002111900178 20021119 00178 SO 2002 11 19 SWIA200211347 1 20021017 A 2497 WIRE EMB 120 EMB120ER 3260203 SO RT STARTER/GEN DAMAGED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 271YV 120271 RIGHT MAIN GENERATOR FAILED TO RESET ITSELF ON TAKEOFF ROLL. ABORTED TAKEOFF. REPAIRED WIRE TO RIGHT STARTER/GENERATOR . CLEANED ALL TERMINALS AND CANNON PLUGS. TAXIED ACFT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002111900179 20021119 00179 2002 11 19 SWIA200211348 4 20021015 A 3425 6226190204 COMPARATOR EMB 120 EMB120ER 3260203 SO NR 1 MALFUNCTIONED A SWIA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 217SW 120286 CAPTAIN'S AUTOPILOT WENT INTO UNCOMMANDED CLIMB. REPLACED NR 1 AHC IAW MM 34-21-01. AHRS OPS CHECK GOOD IAW MM 34-21-0 0. AUTOPILOT OPS CHECK GOOD IAW MM 22-10-00. 2 L 7 2 4T RT A31SO 2002111900180 20021119 00180 SO 2002 11 19 SWIA200211349 1 20021020 A 3234 12038594001 CONTROL HANDLE EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 217SW 120286 LANDING GEAR WOULD NOT EXTEND WHEN SELECTING GEAR DOWN. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. CYCLED GEAR 6 TIMES W/ONE EMERGENCY FREE FALL. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2002111900181 20021119 00181 EA 2002 11 19 SWIA200211350 1 20021018 A 2760 4916405 ECU CNDAIR CL600 CL6002B19 1900309 EA NR 1 MALFUNCTIONED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 597SW 7293 SPOILERONS FAULT MESSAGE REAPPEARED ON EICAS. LEFT OUTBOARD SPOILERON IS WHITE BOXED AND FLUTTERING. UNABLE TO CLEAR M ESSAGE. REMOVED AND REPLACED LEFT INBOARD SPOILERON PCU AND NR 1 SECU IAW MM 27-61-05 AND 27-62-01. OPS CHECK GOOD. L EAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2002111900182 20021119 00182 SO 2002 11 19 SWIA200211351 1 20021015 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 218SW 120287 FOUR LIGHTS ON FLOOR LEVEL EMERGENCY LIGHTING STRIPS FAIL TO ILLUMINATE. INSTALLED SERVICEABLE EMERGENCY LIGHT BATTERY FOR CENTER SECTION. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002111900183 20021119 00183 EA 2002 11 19 COMA0260650 1 20021116 A 3030 7858062 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 810CA 19596 7370 FLIGHT 5577 TAT, R/H AOA HEAT, R/H STATIC HEAT, R/H PITOT HEAT CAUTION MESSAGE.REPLACED THE #2 ADSHC 2 L 7 2 4F RT A21EA 2002111900184 20021119 00184 NE 2002 11 19 SWIA200211352 2 20021021 A 7320 RELAY EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 221SW 120290 ON TAKEOFF ROLL WE RECEIVED A RIGHT ENGINE EEC, ENGINE CONTROL WARNING. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED RIGHT ENGINE REVERSION RELAY. RAN ENGINE. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002111900185 20021119 00185 EA 2002 11 19 SWIA200211353 1 20021021 A 2742 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 429SW 7518 STAB TRIM CHANNEL 1 STATUS MESSAGE. COULD NOT ENGAGE STAB TRIM CHANNEL 1. MOTOR 1 FAILURE ON HSTCU ON GROUND TEST. RE PLACED HSTA ACTUATOR IAW 27-40-00 AND REPLACED MOTOR CONTROL UNIT IAW 27-42-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002111900186 20021119 00186 EA 2002 11 19 COMA0260651 1 20021116 A 7830 1267587 PDU CNDAIR CL600 CL6002B19 1900309 EA LEFT ENG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 971CA 5810 7145 FLIGHT 5777 LEFT ENGINE REV UNLOCKED WARNING.REPLACED THE LEFT T/R PDU. 2 L 7 2 4F RT A21EA 2002111900187 20021119 00187 EA 2002 11 19 SWIA200211354 1 20021018 A 7830 1267587 PDU CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MALFUNCTIONED A SWIA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NM 07 442SW 2887 2887 7609 `L REV UNLOCKED` CAUTION MESSAGE APPEARED IN FLIGHT AFTER THE ARMING SWITCH WAS BROUGHT TO THE ARMED POSITION. QRH PROC EDURES WERE COMPLETED, RESULTING IN LEFT ENGINE SHUTDOWN. REPLACED PDU PER MM 78-30-03 AND R-1K1KE IN JB-10. OPS CHEC K GOOD PER MM 79-32-05. 2 L 7 2 4F RT A21EA 2002111900188 20021119 00188 EA 2002 11 19 COMA0260652 1 20021117 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS CR CRUISE 1 SO 01 981CA 7163 FLIGHT 6076 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002111900189 20021119 00189 EA 2002 11 19 SWIA200211355 1 20021021 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 438SW 7574 ON FINAL, AFTER SELECTING FLAPS 45, RECEIVED FLAPS FAIL MSG. FLAPS STOPPED - LEFT 41 DEGREES, RIGHT 40 DEGREES. REPLAC ED LT BPSU IAW 27-51-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002111900190 20021119 00190 EA 2002 11 19 COMA0260653 1 20021117 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 807CA 7364 FLIGHT 5527 FLAPS FAILED AT 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002111900191 20021119 00191 EA 2002 11 19 SWIA200211356 1 20021023 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 927SW 7693 FIRST OFFICER'S SIDE WINDOW IS CRACKED. REMOVED AND REPLACED FIRST OFFICER'S RIGHT SIDE WINDOW. OPS CHECK GOOD OF WIND OW HEAT AND PRESSURIZATION IAW CRJ MM 56-00-00. 2 L 7 2 4F RT A21EA 2002111900192 20021119 00192 EA 2002 11 19 SWIA200211357 1 20021022 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 07 427SW 7497 ON DESCENT INTO DES MOINES, GOT THE FLAPS FAIL MSG. PERFORMED QRH PROCEDURE. LANDED FLAPS 0 DEGREES. REMOVED AND REPL ACED RIGHT BPSU WITH SERVICEABLE IAW MM 27-51-10. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002111900193 20021119 00193 SO 2002 11 19 SWIA200211358 1 20021023 A 3233 ACTUATOR EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJUST A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 295UX 120295 ON TAKEOFF, THE LEFT MAIN GEAR WOULD NOT RETRACT ALL THE WAY. CYCLED GEAR BUT DID NOT CLEAR PROBLEM. RETURNED TO FIELD . ADJUSTED ACTUATOR LENGTH PER MM 32-32-10 AND ADJUSTED PROX SENSORS TARGET PER MM 32-61-01. GEAR RETRACTIONS AND INDI CATIONS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002111900194 20021119 00194 EA 2002 11 19 SWIA200211359 1 20021021 A 2742 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 417SW 7400 STAB TRIM CH1 STATUS MESSAGE INTERMITTENTLY ON. ABLE TO RESET 1ST 2 TIMES, 3RD TIME TOOK SEVERAL TRIES TO RESET. REMOV ED AND REPLACED MCU, HSTA AND HSTCU IAW 27-42-01 AND 27-42-05. SYSTEMS OPS CHECK GOOD IAW 27-41-00. 2 L 7 2 4F RT A21EA 2002111900195 20021119 00195 EA 2002 11 19 SWIA200211474 1 20021118 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FORWARD PRESSURE CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 5 CRACKS FOUND TO BE RADIATING FROM PARK BRAKE CABLE CUTOUT ON LEFT SIDE OF THE FORWARD PRESSURE BULKHEAD. REPAIRS IN P ROGRESS. SUPPLEMENTAL REPORT FORTHCOMING. 2 L 7 2 4F RT A21EA 2002111900196 20021119 00196 NM 2002 11 19 DHL2002749002 1 20021114 A 2500 LEVER BOEING 727 727200 138407E NM A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 1) THE S/O SEATS MSWIVEL LEVER HAS TO BE MANUALY PLACED IN THE LOCK POSITION.2) LUBED SWIVEL LEVER ON F/E SEAT IAW B 7 27 M/M 25-10-71.OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2002111900197 20021119 00197 EU 2002 11 19 DHL2002362504 1 20021111 A 5755 A5776203120000 SPOILER PANEL AIRBUS 300 A300B4203 3930306 EU CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 L/H #2 SPOILER LOWER SIDE COVERPLATE CORRODED, REMOVED CORROSION FOUND TO BE OUT OF LIMITS. INSTALLED NEW COVERPLATE IAW A300 SRM 51-30-30 2 L 7 2 4F RT A35EU 2002111900198 20021119 00198 EU 2002 11 19 DHL2002362505 1 20021107 A 5755 A5776200118051 SPOILER AIRBUS 300 A300B4203 3930306 EU CORRODED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 362DH 84 UPPER SURFACE R/H #1 SPOILER HAS CORROSION, REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH SERVI CEABLE #1 SPOILER IAW A300 SRM 27-61-51 2 L 7 2 4F RT A35EU 2002111900199 20021119 00199 NM 2002 11 19 DHL2002721009 1 20021115 A 2500 SCREW BOEING 727 727228 1384083 NM A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 1) CAPTAINS SEAT BACK ADJ. DOES NOT COMPLETLY RELEASE MAKING IT DIFF. TO MOVE IN EITHER DIRECTION2) DEFFERED RECLINE P ORTION OF SEAT IAW MEL 25-20-3 DMI 10980 ASSIGNED PER MAINT CONTROL-SEAT REPLACEMENT SCHEDULED3) REFER TO DMI #10980 CA PT SEAT BACK ADJUSTMENT DOSE NOT COMPLETELY RELEASE4) REPLACE MISSING RIGHT ACT ADJUSTMENT SCREW NUT ADJUSTED ACTU IAW MM 25-10-41 OPS CHECK OK PLACARD REMOVED MX CONTROL WAS NOTIFIED THIS CLEARD DMI #10980 2 L 7 3 4F RT A3WE 2002111900200 20021119 00200 NM 2002 11 19 DHL2002721010 1 20021116 A 2500 808737630 SEAT BOEING 727 727228 1384083 NM A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 1) CAPTS SEAT BACK WILL NOT STAY UPRIGHT WHEN SOME PRESSURE IS APPLIED2) INSTALLED CAPT SEAT IAW B-MM 25-10-42 OPS CHE CK GOOD 2 L 7 3 4F RT A3WE 2002111900201 20021119 00201 EU 2002 11 19 DHL2002362506 1 20021010 A 5311 FRAME AIRBUS 300 A300B4203 3930306 EU CRACKED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 362DH 84 FWD CARGO DOOR CUT-OUT FWD DOOR FRAME #20, STR 45R FRAME IS CRACKED AT TOP FLANGE. FABRICATED AND INSTALLED REPAIR ANGLE IAW A300 SRM 51-41-40/FIG 701 AND RAS/DABRE/7002315/2002 2 L 7 2 4F RT A35EU 2002111900202 20021119 00202 NM 2002 11 19 DHL2002721011 1 20021116 A 2500 808737630 SEAT BOEING 727 727228 1384083 NM A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 1) CANNOT ADJUST CAPTS SEAT.2) ADJUSTED SEAT FORWARD AND BACK MOVEMENT IAW B-MM 25-10-42 OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2002111900203 20021119 00203 EU 2002 11 19 DHL2002362507 1 20021024 A 5347 A5361164021202 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU CORRODED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 362DH 84 20" AFT OF FRAME 15 ONL1 FLOOR BEAM, SEAT TRACK IS CRACKED. UPON FURTHER INVESTIGATION FOUND SEAT TRACK CORRODED INSTEAD OF CRACKED.REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK SECTION IAW A300 SRM 51-10-40 2 L 7 2 4F RT A35EU 2002111900204 20021119 00204 NM 2002 11 19 DHL2002752004 1 20021119 A 2611 SMOKE DETECTOR BOEING 727 727223 1384074 NM A DHLA O OTHER L J NO TEST WARNING INDICATION IN INSP/MAINT 1 SO 01 752DH 22466 1) LOWER CARGO SMOKEDETECTOR GREEN "OK " LIGHT IS OUT2) REMOVED POWER FROM AIRCRAFT, RESTORED POWER , SMOKE DETECTOR(L OWER CARGO)OPS CHECK GOOD IAW SECURA PLANE ST300 M/M. 2 L 7 3 4F A3WE 2002111900205 20021119 00205 NM 2002 11 19 DHL2002726007 1 20021119 A 2600 1014A POWER UNIT BOEING 727 727228 1384083 NM A DHLA O OTHER L J NO TEST WARNING INDICATION IN INSP/MAINT 1 SO 01 726DH 20409 1) AFTER HOLDING THE APU FIRE TEST S/W TO THE TEST POS. FOR 60 SEC. THE TEST DOES NOT ACTIVATE2) TRANSFER'D TO DMI #1 1007 MEL 26-11 PLACARD INSTALL'D COMPLIED WITH SP 26-113) REF DMI# 11007, APU FIRE TEST DON'T TEST.4) R&R FIRE TEST PO WER UNIT, OPS. CK. GOOD I.A.W. B.M.M. CH.26-15-0. 2 L 7 3 4F RT A3WE 2002111900206 20021119 00206 EU 2002 11 19 DHL2002362508 1 20021017 A 5311 FRAME AIRBUS 300 A300B4203 3930306 EU CORRODED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 362DH 84 AFT CARGO DOOR FR63 BETWEEN STR28R AND 29R AFT SIDE OF FRAME HAS 10SQ" INCHES OF CORROSION. REMOVED CORROSION, MATERIAL REMAINING FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER IAW REFERENCE 942-020492/007/2002, INSTALLED REPAIR PART IAW A30 0 SRM 51-30-30 2 L 7 2 4F RT A35EU 2002111900207 20021119 00207 NM 2002 11 19 AWXA200201142 1 20021029 A 5315 654585546 ANGLE BOEING 737 73733A 1384673 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 0 0 23632 YVR - MAJOR REPAIR - DURING C-19 CHECK INTERGRANULAR CORROSION WAS FOUND AT SCREW HOLES ON THE UNDERSIDE OF INTERCOSTAL BEAMS BS 927 TO BS 1016. MAINTENANCE REMOVED ANGLE UNDER DOOR SILL CHORD AT R/H SIDE BS 967 TO BS 987; BLENDED CORROSION ON INTERCOSTALS BS 947, BS 993, AND BS 1007, MATERIAL LOSS WITHIN LIMITS; FABRICATED NEW REPLACEMENT ANGLE PER DWG 65-4 5855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 3. 2 L 7 2 4F RT A16WE 2002111900208 20021119 00208 NM 2002 11 19 AWXA200201143 1 20021027 A 5330 69719478 SKIN BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 0 0 23632 YVR - MAJOR REPAIR - DURING C-19 CHECK A 1/4" CRACK WAS FOUND ON FIRST OFFICERS WINDSHIELD CUTOUT AT THE OUTBOARD UPPER CORNER. MAINTENANCE CUTOUT CRACKED AREA OF SKIN; DURING HFEC INSPECTION A 1/2" CRACK WAS FOUND ON GUSSET PLATE; CUTOUT C RACK AT GUSSET PLATE AND PERFORMED HFEC INSPECTION OF BOTH CUTOUTS TO VERIFY CRACKS CONTAINED. FABRICATED A DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PG. 3. 2 L 7 2 4F RT A16WE 2002111900209 20021119 00209 EU 2002 11 19 DHL2002362509 1 20021018 A 5730 SKIN AIRBUS 300 A300B4203 3930306 EU CORRODED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 362DH 84 R/H WING BOTTOM SKIN BETWEEN RIB 7 AND 8 AND, FRONT AND CENTER SPAR, SEVERAL AREAS WITH CORROSION.REMOVED CORROSION JUST OUT BOARD OF CENTER SPAR FOUND NTO BE OUT OF LIMITS. REPAIRED BY BLENDING OUT CORROSION, ENSURING AREA WAS CRACK AND CO RROSION FREE BY HFEC INSPECTION FOLLOWED BY FLAP PEENING AND REPROTECTING AREA, ALL IAW A300 SRM AND RAS/BAE/1355/2002 2 L 7 2 4F RT A35EU 2002112600067 20021126 00067 NM 2002 11 26 2002UALA01623 1 20021025 A 2613 355574255 OVERHEAT LOOP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING SHORTED A UALA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 WP 29 394UA 24669 WING BODY OVERHEAT LIGHT ILLUMINATED EN ROUTE, AND RETURNED TO FIELD. PERFORMED INSPECTION OF THE LEFT WING BODY OVERHE AT DETECTION SYSTEM AND FOUND A SHORT TO GROUND ON PIN 9 OF CONNECTOR D742. ISOLATED THE FAULT TO A SHORTED AFT KEEL BE AM DETECTOR M273. REPLACED DETECTOR AND AIRCRAFT WAS RETURNED TO REVENUE SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600076 20021126 00076 NM 2002 11 26 2002UALA01636 1 20021007 A 5754 114W4140 WEDGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L/E SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 TRAILING EDGE SLAT DELAMINATED SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002111900210 20021119 00210 NM 2002 11 19 2002UALA01701 1 20021111 A 5315 BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 CABIN FLOOR BEAM UPPER CAP CORRODED. STA 365 RBL 10 - RBL 40. MAJOR REPAIR ACCOMPLISHED.INSTALLED SPLICE AND ANGLE REPA IR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002111900211 20021119 00211 NM 2002 11 19 2002UALA01703 1 20021111 A 5320 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 AFT PIT FRAME TO SKIN SHEAR TIE CRACKED. STA 1300 BETWEEN STR 20L - 21L. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002111900212 20021119 00212 NM 2002 11 19 2002UALA01708 1 20021110 A 7120 MOUNT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 #1 ENGINE FORWARD MOUNT CHAFED. AFT SIDE OF FWD ISOLATOR BEARING JOURNAL. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW FWD M OUNT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002111900213 20021119 00213 NM 2002 11 19 2002UALA01720 1 20021112 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 FWD PIT FRAME CAP DENTED. STA 540 STR 24L. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002111900214 20021119 00214 NM 2002 11 19 2002UALA01721 1 20021112 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 FRAME INNER FLANGE DAMAGED. STA 1640 AT FLOOR BEAM. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002111900215 20021119 00215 NM 2002 11 19 2002UALA01722 1 20021112 A 5347 TRACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 RH IB SEAT TRACK FLANGE DOME NUT MISSING AND HOLE ELONGATED. STA 1050, RBL 24. MAJOR REPAIR ACCOMPLISHED.INSTALLED REPA IR ANGLE ON SEAT TRACK FLANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112000001 20021120 00001 EU 2002 11 20 R7MR35474 1 20020712 A 6720 418008768000 ACTUATOR UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE T/R CONTROL INOPERATIVE B R7MR O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 101HN 65 0162 ELECTRO-MECHANICAL ACTUATOR INOPERATIVE. AMBER ON PRIMARY FLIGHT DISPLAY. WOULD NOT PASS PREFLIGHT CHECK. REPLACED W ITH NEW UNIT CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002112000002 20021120 00002 EU 2002 11 20 R7MR35482 1 20020107 A 7332 9550162490 PRESSURE SWITCH BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1E 60030 NE FUEL SYSTEM INOPERATIVE B R7MR O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 117SU 7527 PRESSURE SWITCH INOPERATIVE. FUEL PRESSURE WARNING LIGHT WILL NOT GO OUT. REPLACED WITH NEW, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H13EU E19EU 2002112000003 20021120 00003 EU 2002 11 20 R7MR35483 1 20020107 A 7332 9550162490 PRESSURE SWITCH BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1E 60030 NE FUEL SYSTEM INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 117SU 7527 PRESSURE SWITCH, UNIT INOPERATIVE UPON INSTALLATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H13EU E19EU 2002112000004 20021120 00004 EU 2002 11 20 R7MR35484 1 20020504 A 7332 9550162490 PRESSURE SWITCH BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1E 60030 NE FUEL SYSTEM INOPERATIVE B R7MR O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 117SU 7527 PRESSURE SWITCH INOPERATIVE. FUEL PRESSURE LIGHT CAME ON. FOUND SWITCH TO BE PROBLEM. REPLACED WITH NEW UNIT, CORRECT ED PROBLEM. 1 G 7 2 3U 3 U NC H13EU E19EU 2002112000006 20021120 00006 EU 2002 11 20 R7MR35511 1 20020528 A 7714 430106202 PICKUP BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE ENGINE SPEED INTERMITTENT B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 7059N 215 7154 LE45549EFA ELECTROMAGNETIC SPEED PICKUP OPERATES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H13EU E5NE10 2002112000007 20021120 00007 EU 2002 11 20 R7MR35512 1 20020627 A 7714 430106202 PICKUP UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ROTOR INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 102HN 0159 ELECTROMAGNETIC NG SPEED PICKUP INOPERATIVE. ROTOR NEEDLE ERATIC. AIRFRAME PART FOR EC135 CONFIGURATION. NO ENGINE TO REFERENCE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002112000008 20021120 00008 EU 2002 11 20 R7MR35515 1 20020701 A 6240 42960 TACHOMETER SNIAS 350 AS350B 8680801 EU COCKPIT INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 5771C 156 1369 TACHOMETER INDICATOR INOPERATIVE. READS 360-370 RPM GROUND. READS 380-390 RMP IN-FLIGHT. ADJUSTED INDICATOR TWICE WIT HOUT SUCCESS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2002112000009 20021120 00009 EU 2002 11 20 R7MR35517 1 20020716 A 2842 647511011 TRANSMITTER SNIAS 350 AS350* EU ALLSN 250C 250C20 03013 GL FUEL LEVEL INOPERATIVE B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 30LG 5065 FUEL LEVEL TRANMITTER INOPERATIVE UPON INSTALL. PEGS HIGH AT ANY LEVEL ABOVE 5 PERCENT. REPLACED WITH NEW UNIT, CORREC TED PROBLEM. 1 G 7 1 3U 3 U H9EU E4CE 2002112000010 20021120 00010 EU 2002 11 20 R7MR35526 1 20020705 A 6240 42960 TACHOMETER SNIAS 350 AS350B 8680801 EU MAIN ROTOR INOPERATIVE B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 5771C 3 1369 TACHOMETER INDICATOR INOPERATIVE. NR READS LOW 370 IN-FLIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2002112000011 20021120 00011 EU 2002 11 20 R7MR35529 1 20020726 A 2432 RG390E BATTERY BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101600A 41560 NE DC SYSTEM LEAKING B R7MR K NONE K L FLUID LOSS NO TEST IN INSP/MAINT 1 NM 07 71703 7227 REJECTED NEW OUT OF BOX. DRAWS EXCESSIVE CURRENT ON TOPPING CHARGE. OOZED. SOME LIQUID FROM VENT TUBES. BATTERY BECA ME EXTREMELY HOT! REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (DISCREPANT UNIT DROP SHIPPED TO NC2) 1 G 7 2 3U 3 U H13EU E5NE 2002112000012 20021120 00012 2002 11 20 R7MR35530 4 20020708 A 2211 7004206901 COMPUTER BOLKMS 117 BK117A4 5626017 EU CSAS INOPERATIVE B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 586BH 7129 CSAS COMPUTER INOPERATIVE. ROLL CHANNEL OPERATIVES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2002112000013 20021120 00013 EU 2002 11 20 R7MR35534 1 20020801 A 6320 510286B CLUTCH UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE GEARBOX FAILED B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 135N 0086 CLUTCH IS NOT ENGAGING (NOT HEARD OR FELT). REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2002112000014 20021120 00014 2002 11 20 R7MR35536 4 20020718 A 3457 0110028010 GPS SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT INOPERATIVE B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 220CF 3411 POOR GPS COVERAGE ON SCREEN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002112000015 20021120 00015 NE 2002 11 20 R7MR35541 2 20020114 A 7240 410106701 SEAL RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SHROUD WORN B R7MR K NONE L NO TEST IN INSP/MAINT 1 NM 07 117MV 353 7089 LE45038EA SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002112000016 20021120 00016 NE 2002 11 20 R7MR35543 2 20020114 A 7240 411101009 NOZZLE BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER BURNED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 117MV 353 7089 NOZZLE HAS EXCESSIVE BURNS IN SOME AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002112000017 20021120 00017 EU 2002 11 20 R7MR35563 1 20020218 A 7720 430150102 THERMOCOUPLE BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE SHORTED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 127HH 915 7060 002548000053 THERMOCOUPLE, INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002112000018 20021120 00018 NE 2002 11 20 R7MR35576 2 20020613 A 7240 413101034 LINER BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE COMBUSTION CHAMB CRACKED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 527RM 874 7111 001972660892 COMBUSTION CHAMBER LINER, CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2002112000019 20021120 00019 EU 2002 11 20 R7MR35584 1 20020717 A 6220 BUSHING SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1 60030 NE STARFLEX DEBONDED B R7MR K NONE O OTHER IN INSP/MAINT 1 NM 07 103LN 865 M2017 3128 STARFLEX, BUSHINGS DEBONDED. REMOVED IAW AD. REPLACED WITH NEW CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 2002112000031 20021120 00031 CE 2002 11 20 DFJ2002F00000 1 20021025 A 2710 1N2070 DIODE CESSNA 210 T210L 2073449 CE CONT O520 TSIO520* 17040 SO POWER PACK DEFECTIVE A DFJS O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 03 6864C 2100 21061317 LANDING GEAR WOULD NOT EXTEND UNTIL STARTING SYSTEM WITH HAND PUMP. FOUND DEFECTIVE DIODE IN DOWN SIDE OF GEAR SELECTOR SWITCH TO CONTACTOR. DIODE LOOKED NORMAL AND HAD NO EXTERNAL DAMAGE. 1 H 7 1 3O 3 O 3A21 E8CE 2002112000032 20021120 00032 EA 2002 11 20 FMAA2002001 2 20020830 A 8520 LW019340 CAMSHAFT PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA ENGINE WORN E FMAA K NONE O OTHER IN INSP/MAINT 1 AL 01 87TS 4400 890 317300969 L442761A ALARMING AMOUNT OF METAL WAS FOUND IN THE FULL FLOW OIL FILTER, FURTHER INSPECTION REVEALED THAT ONE CAMSHAFT LOBE BEGAN WEAR EXCESSIVELY. 1 L 7 2 3O 3 O A20SO E14EA 2002112000033 20021120 00033 CE 2002 11 20 FMAA2002003 1 20020907 A 3246 C1630030302 WHEEL CESSNA 206 U206F 2073333 CE CONT O520 IO520F 17032 SO NLG CRACKED B FMAA K NONE O OTHER IN INSP/MAINT 1 AL 01 8515Q U20603372 16428772E THE NOSE WHEEL IS MADE UP OF 3 MAJOR COMPONENTS, THE 2 WHEEL FLANGES AND THE HUB. THE SCREWS HAVE NO LOCKING DEVICE, AN D AFTER MANY HOURS OF USE THE SCREWS BACK OUT OF THE HUB AND OR THE SCREW HOLES IN THE HUB CRACK AND ALLOW THE THREADED HOLE TO GET LARGER ALLOWING THE SCREW TO BACK OUT WHICH CAUSED THE TIRE TUBE TO GO FLAT AND ALSO CAUSED THE WHEEL FLANGE TO DIG INTO THE RUNWAY WHICH CAUSED THE PLANE TO FLIP OVER. 1 H 7 1 3O 3 O A4CE E5CE 2002112000034 20021120 00034 EU 2002 11 20 K5S2002F00000 1 20021107 A 3097 WIRE PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A60A 52043 NE WINDSHIELD DAMAGED B K5SR H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE NR NOT REPORTED 1 NM 07 956PC 671 323 PILOT REPORTED FIRE ON UPPER RT SIDE OF COPILOTS WINDOW. RT WINDSHIELD DEICING CIRCUIT BREAKER WAS PULLED. AFTER INVES TIGATION FOUND TWO WIRES (WIRE L AND K). WIRE L SPLICE AN AWG 10-12 SPLICE WAS SEVERELY BURNED. THE AIRCRAFT IS POST S ERVICE BULLETIN FOR HEAVY-DUTY WIRES AT THE WINDOW. SUSPECT THE POWER WIRE WAS PREVIOUSLY DAMAGED AT THE SPLICE. CAUSI NG THE SPLICE TO GET HOT AND MELT INTO THE GROUND WIRE. EVENTUALLY THE POWER WIRE SEPARATED AND WENT TO GROUND. 1 L 7 1 3T 4 T RT A78EU E4EA 2002112000035 20021120 00035 EU 2002 11 20 02323324 1 20021119 A 3350 1317 LAMP JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 324UE 41017 During preflight inspection, the crew reported that the L/H aft exterior emergency exit light was inoperative. Maintena nce personnel removed and replaced the lamp in the L/H aft exterior emergency exit light. An operational check was sati sfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002112000036 20021120 00036 EA 2002 11 20 SWIA200211360 1 20021019 A 2742 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 910SW 7566 STAB CH 1 INOP. STATUS MESSAGE WILL NOT ENGAGE AFTER NUMEROUS ATTEMPTS. REPLACED CH 1 WIRING HARNESS FROM THE MOTOR CO NTROL UNIT TO THE AFT PRESSURE BULKHEAD. REPLACED THE HSTA 1 3-PHASE C/B, REPLACED THE HSTCU, MOTOR CONTROL UNIT AND TH E STAB TRIM ACTUATORS. REPLACED THE DC BUS 2 TRU AND TESTED THE HSTA SYSTEM AND FOUND THE SYSTEM TO BE FUNCTIONING NORM ALLY. 2 L 7 2 4F RT A21EA 2002112000037 20021120 00037 EA 2002 11 20 SWIA200211361 1 20021024 A 2752 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 441SW 7602 FLAPS FAILED MESSAGE IN FLIGHT. REMOVED AND REPLACED PDU FOR FLAPS. OPS CHECKS GOOD IAW 27-52-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2002112000038 20021120 00038 SO 2002 11 20 SWIA200211362 1 20021007 A 5711 SPAR CAP EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 199SW 120237 LEFT WING FORWARD LOWER SPAR CAP HAS A CRACK BETWEEN 4533.5 AND 4945. RIVET ROW ON LOWER SKINS MARKED WHERE SKIN SEAMS MEET, OUTBD OF RIB NR17. DISCOVERED DURING LINE INSPECTION OF FUEL LEAK. REPAIRED IAW EMB 120 SRM 57-20-05 AND RII CAR D RII 57-301 AND RII28-301. 2 L 7 2 4T RT A31SO 2002112000039 20021120 00039 EA 2002 11 20 SWIA200211363 1 20021021 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 409SW 7056 `L REV UNLOCKED` INFLIGHT CLIMBING THROUGH 18,000 FEET. A/C WAS STABLE AND CONTROLLED. A/C DID NOT BUFFET OR YAW. DIV ERTED TO BZN. FOUND LEFT REVERSER STOW MICROSWITCH OUT OF ADJUSTMENT, ADJUSTED STOW SWITCH IAW MM 78-37-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002112000040 20021120 00040 EA 2002 11 20 SWIA200211364 1 20020912 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FUSE FRAME AT FS 640.0 IS CRACKED AT STR 9 CUTOUT. FOUND DURING C CHECK INSPECTION, HFEC INSPECTION CARRIED OUT ON CUTO UT EDGE AND AREA AS REQUIRED IAW REO 601R-53-61-532. NO CRACKS FOUND. REPAIRED FRAME IAW CRJ REO 601R-53-61-532 REV NC . 2 L 7 2 4F 4 F RT A21EA E15NE 2002112000041 20021120 00041 EA 2002 11 20 SWIA200211365 1 20020912 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FUSE FRAME AT FS 718 CRACKED ON RIGHT SIDE AT STR 11. FOUND DURING C-CHECK INSPECTION, HFEC INSPECTION CARRIED OUT ON CUTOUT REPAIR EDGE AND AREA AS REQUESTED IAW RJ NDTM 51-20-01. NO CRACKS FOUND. REPAIRED FRAME IAW CRJ REO 601R-53-61- 193 REV A ANGLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002112000042 20021120 00042 EA 2002 11 20 SWIA200211366 1 20020912 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS 280.0 RBL AND LBL 9.0 FLOORBEAM INBOARD ANGLES CRACKED. FOUND DURING C CHECK INSPECTION, NEW ANGLES FITTED AND INST ALLED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-42-20. 2 L 7 2 4F 4 F RT A21EA E15NE 2002112000043 20021120 00043 EA 2002 11 20 SWIA200211367 1 20020912 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 INTERCOSTAL AT FS 404.0 AND RBL 1.5 IN AVIONICS CRAWL WAY AFT OF MAIN AVIONICS DOOR HAS SURFACE CORROSION ON SIDE OF INT ERCOSTAL, BEYOND LIMITS. FOUND DURING C-CHECK INSPECTION, NDT-ET CONDUCTIVITY CARRIED OUT AND FOUND MATERIAL TO BE 30.2 0 PERCENT IACS. INTERCOSTAL REMOVED AND REPLACED IAW CRJ SRM 51-23-00 AND 51-42-06 AND 51-40-11. 2 L 7 2 4F 4 F RT A21EA E15NE 2002112000044 20021120 00044 EA 2002 11 20 SWIA200211369 1 20021020 A 4920 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY MALFUNCTIONED A SWIA O OTHER M OVER TEMP TX TAXI/GRND HDL 1 NM 07 925SW 7682 AT THE GATE, THE APU AUTO SHUTDOWN, TWICE, WITH AN EGT SPIKE OF 990 DEGREES THE SECOND TIME. REMOVED AND REPLACED APU A SSEMBLY IAW RII 49-401 AND MM 49-10-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002112000045 20021120 00045 SO 2002 11 20 SWIA200211370 1 20021018 A 3310 1021P22513 LIGHT EMB 120 EMB120ER 3260203 SO COCKPIT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 236SW 120312 CAPTAIN'S FLOODLIGHT SMOKES WHEN THE LIGHT IS ON. REPLACED CAPTAIN'S FLOODLIGHT FIXTURE WITH SERVICEABLE UNIT. 2 L 7 2 4T RT A31SO 2002112000046 20021120 00046 NM 2002 11 20 VNAA0210030 1 20021031 A 7920 REGULATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE OUT OF ADJUST A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 439JS 3057 EN ROUTE TO DCA, THE CREW RECEIVED A LEFT HAND ENGINE PRESSURE INDICATION MOVING INTO THE AMBER RANGE. THE CREW DECLARE D AN EMERGENCY AND FEATHERED THE LEFT HAND ENGINE. THE CREW THEN DIVERTED TO LGA. OUTSTATION MAINTENANCE INSPECTED AND RESHIMMED THE OIL PRESSURE REGULATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 79-00-00. OPERATIONAL CHECKS WERE P ERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002112000047 20021120 00047 NM 2002 11 20 AALA20021002 1 20020927 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 752AN 30260 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PROXIMITY LIGHT AT L1 CLOSET FLOOR BROKEN. REPLACED EMERGENCY EXIT P ROXIMITY LIGHT ASSEMBLY AT L1 CLOSET FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002112000048 20021120 00048 NM 2002 11 20 AALA20021021 1 20020927 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 312AA 22315 LAX - DURING OVERNIGHT MAINTENANCE, LEFT AFT GALLEY UNDER FLIGHT ATTENDANT SET B1 DIRECTIONAL EMERGENCY EXIT LIGHT DAMAG ED. REPLACED LEFT AFT GALLEY B1 DIRECTIONAL EMERGENCY EXIT LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A1NM 2002112000049 20021120 00049 WP 2002 11 20 AALA20021298 1 20020911 A 2130 39271411 REGULATOR VALVE DOUG DC9 DC982 3022082 WP A/C BAY DEFECTIVE A AALA G B O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 21 579AA 53156 DFW - FLT 341 - EN ROUTE GDL-DFW, AT 37,000 FEET, PRESSURE FLOW LIGHT ILLUMINATED. CABIN CLIMBED AT 300 FEET PER MINUTE . PERFORMED ABNORMAL PROCEDURE AND CABIN RATE WENT TO ZERO, THEN BOTH PACKS FLOWS WENT TO ZERO AND CABIN BEGAN CLIMBING RAPIDLY. MAXIMUM CABIN ALTITUDE REACHED WAS 1,200 FEET. CABIN MASKS DEPLOYED AS PART OF EMERGENCY DESCENT PROCEDURE. LANDED DFW WITHOUT INCIDENT. REPLACED PRESSURE REGULATOR VALVE ON LEFT SIDE, OFF 13TH STAGE BLEED AIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112000051 20021120 00051 WP 2002 11 20 AAL2002F00025 1 20020226 A 5311 FRAME DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 STA 1418 WEAR MARK FROM STANDOFF CLAMP RIGHT LOWER SIDE ON TOP OF BELL FRAME. INSTALLED DOUBLER IAW AARD. 2 L 7 2 4F 4 F A6WE E2EA 2002112000052 20021120 00052 WP 2002 11 20 AAL2002F00026 1 20020420 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 442AA 49468 HEAVY CORROSION IN NR 3 SEAT TRACK, STA 1294. CUT OUT CORRODED AREA, INSTALLED REPAIR PLUG IAW SRM. 2 L 7 2 4F 4 F A6WE E2EA 2002112000053 20021120 00053 WP 2002 11 20 AALA20021313 1 20020917 A 2613 1173T0640 OVERHEAT LOOP DOUG DC9 DC982 3022082 WP A/C BAY DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 276AA 49273 AUS - FLT 2056 - EN ROUTE SAT-ORD, DURING CLIMB-OUT, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. DURING CLIMB FOLLOWED CHECKLIST LIGHT WOULD NOT EXTINGUISH. RETURNED AUS AND ON DESCENT LIGHT EXTINGUISHED. LANDED AUS WITHOUT INCI DENT. REPLACED LEFT AND RIGHT TAIL COMPARTMENT OVERHEAT SENSORS. RAN ENGINE TO HIGH POWER, OVERTEMP LIGHT DID NOT ILLU MINATE. AIRCRAFT RELEASED FOR FUNCTIONAL CHECK FLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112000054 20021120 00054 WP 2002 11 20 AALA20021314 1 20020918 A 2120 5953625521 DUCT DOUG DC9 DC982 3022082 WP A/C BAY LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 276AA 49273 AUS - FLT 9686 - DURING CHECK FLIGHT WHILE PASSING 15,000 AT 6 MINUTES INTO FLIGHT. TAIL COMPARTMENT HIGH TEMPERATURE L IGHT ILLUMINATED. ACCOMPLISHED EMERGENCY PROCEDURES, AND LIGHT EXTINGUISHED AFTER APPROXIMATELY 1 MINUTES. RETURNED AU S AND LANDED WITHOUT INCIDENT. REPLACED AIR DUCT, RAN PACKS, AND ACCOMPLISHED LEAK CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112000055 20021120 00055 WP 2002 11 20 ASAA028027A 1 20020822 A 3397 WIRE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE EMERGENCY LIGHTS INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 DURING PREFLIGHT CHECK, MANY EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FIRST CLASS CABIN. RELAMPED AND REP AIRED BROKEN WIRING. LIGHTS THEN OPERATED PROPERLY. 2 L 7 2 4F 4 F RT A6WE E2EA 2002112000056 20021120 00056 SO 2002 11 20 ASOA02220A 1 20020415 A 3350 1317 BULB EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 244AS 120073 DURING GROUND INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURN T OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2002112000057 20021120 00057 WP 2002 11 20 AALA20021315 1 20020916 A 2120 CLAMP DOUG DC9 DC982 3022082 WP A/C BAY LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 276AA 49273 ORD - FLT 1170 - EN ROUTE FLL-ORD, DURING CLIMB-OUT THROUGH 26,000 FEET, APPROXIMATELY 20 MINUTES INTO THE FLIGHT, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. LANDED ORD WITHOUT INCIDENT. TIGHTENED PRESSURE REGULATING VALVE CLAMP S. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112000058 20021120 00058 WP 2002 11 20 AALA20021319 1 20020909 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FOUND DENT IN SKIN STATION 534 LONGERON 20R. CONDITION 1-B PER 53-04 FIG 38. INSTALLED DOUBLER PER SRM 5304. (M ) 2 L 7 2 4F RT A6WE 2002112000059 20021120 00059 EA 2002 11 20 ASOA02221A 1 20020416 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 887AS 7463 DURING A SCHEDULED INSPECTION, THE LEFT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE BURNT OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002112000060 20021120 00060 WP 2002 11 20 IXXA0200115O 1 20021119 A 3230 221037010100 BUSHING DOUG DC8 DC862 3021970 WP NOSE GEAR DEFECTIVE A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 21CX 71385 1750 45955 AFTER TAKEOFF FROM WRI ENROUTE TO BWI LANDING GEAR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. CREW PERFORMED L ANDING GEAR UPLATCH CHECK, LIGHT REMAINED ILLUMINATED WITH RUMBILING NOISE NOTED FROM NOSE LANDING GEAR AREA. AIRCRAFT R ETURNED TO WRI FOR AN UNEVENTFUL LANDING. MX INSPECTED AIRCRAFT FINDING A DEFECTIVE BUSHING ON NOSE LANDING GEAR RETRACT ACTUATOR. MX PERFORMED GOOD OPERATIONAL CHECK IAW DMM AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2002112000061 20021120 00061 WP 2002 11 20 AALA20021320 1 20020906 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FOUND GOUGE ON SKIN FS 1305 BELOW 18R, FROM COWLING DRAIN MAST CONTACT BELOW PYLON. FOUND DAMAGE AREA TO BE CONDI TION 3 PER SRM 53-04 FIG 38 SHEET 3. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 20. (M) 2 L 7 2 4F RT A6WE 2002120500085 20021205 00085 EU 2002 12 5 DHL2002362503 1 20021024 A 5230 A5237008120600 SKIN AIRBUS 300 A300B4203 3930306 EU CARGO DOOR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 FWD LOWER CARGO DOOR, INSIDE THE MOST FWD OUTER TORQUE BOX I/B AND O/B SKIN HAS CORROSION. AREA OUT OF LIMITS. REPLACE D PART IAW A300 SRM 51-10-40 & 51-30-30 2 L 7 2 4F RT A35EU 2002112000062 20021120 00062 WP 2002 11 20 AALA20021321 1 20020906 A 5320 CLIP DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FOUND RIGHT UPPER FORWARD WINDOW CLIP CRACKED STATION 947. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25 PAGE 1/2 . (M) 2 L 7 2 4F RT A6WE 2002112000063 20021120 00063 WP 2002 11 20 AALA20021322 1 20020905 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FOUND DENT AND SCRATCH APPROX STATION 235 BETWEEN L17 AND L18 LEFT. BUMPED OUT DENT, DYE CHECKED, NO CRACK FOUND. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F RT A6WE 2002112000064 20021120 00064 WP 2002 11 20 AALA20021323 1 20020909 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FOUND CORROSION IN CUSP WEB 1212-1231. CUT OUT, CORRODED AREA 1212-1219 AND INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3. 2 L 7 2 4F RT A6WE 2002112000065 20021120 00065 WP 2002 11 20 AALA20021324 1 20020909 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FOUND DENT IN SKIN FORWARD OF RIGHT FLOOD LIGHT. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 12 B, INCORPORATED REPAIR E58 NR 4207681 AND 4207640 ONE DOUBLER. (M) 2 L 7 2 4F RT A6WE 2002112000066 20021120 00066 WP 2002 11 20 AALA20021325 1 20020917 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FORWARD ENTRY DOOR TORQUE BOX INNER SKIN EXTENSION CRACKED STATION 207 AT LONGERON 15L. INSTALLED DOUBLER PER AAR D 53-10-00-11. (M) 2 L 7 2 4F RT A6WE 2002112000067 20021120 00067 WP 2002 11 20 AALA20021326 1 20020916 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FOUND CORROSION ON SEAT TRACK NR 3. INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F RT A6WE 2002112000068 20021120 00068 WP 2002 11 20 AALA20021327 1 20020910 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FOUND SEAT TRACK NR 2 CORRODED INBOARD SIDE STATION 1201. ACCOMPLISHED REPAIR IAW SRM 53-05-00. (M) 2 L 7 2 4F RT A6WE 2002112000069 20021120 00069 WP 2002 11 20 AALA20021328 1 20020917 A 5510 PLATE DOUG DC9 DC983 3022083 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FOUND RIGHT OUTBOARD HORIZONTAL STAB PIVOT BEARING LUG PLATES ARE CORRODED. REPLACED RIGHT OUTBOARD LUG PLATE AND MACHINED PIVOT BORE PER FCO KF0488A, 9, D/E. (M) 2 L 7 2 4F RT A6WE 2002112000070 20021120 00070 WP 2002 11 20 AALA20021329 1 20020917 A 5510 PLATE DOUG DC9 DC983 3022083 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FOUND LEFT OUTBOARD HORIZONTAL STAB PIVOT BEARING LUG PLATES ARE CORRODED. REPLACED LEFT OUTBOARD LUG PLATES AND MACHINED PIVOT BORE PER FCD0488A, 9, D/E. (M) 2 L 7 2 4F RT A6WE 2002112000071 20021120 00071 WP 2002 11 20 AALA20021330 1 20020917 A 5510 PLATE DOUG DC9 DC983 3022083 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FOUND RIGHT INBOARD HORIZONTAL STAB PIVOT BEARING LUG PLATES ARE CORRODED. REPLACED RIGHT INBOARD HORIZ STAB LUG PLATES AND MACHINED PIVOT BORE PER FCDKF0488A, 9, D/E. (M) 2 L 7 2 4F RT A6WE 2002112000072 20021120 00072 WP 2002 11 20 AALA20021354 1 20020913 A 2410 CSD DOUG DC9 DC982 3022082 WP RT ENGINE LACK OF LUBE A AALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 485AA 49678 DFW - FLT 1479 - ABORTED TAKEOFF AT 80 KNOTS DUE TO THE RIGHT ENGINE CSD LOW OIL PRESSURE LIGHT FLICKERING ON AND OFF AT TAKEOFF POWER. FOUND RIGHT ENGINE CSD OIL LEVEL LOW. SERVICED AND LEAK CHECKED. SYSTEM GROUND CHECKED NORMAL OPERATI ON. (M) 2 L 7 2 4F A6WE 2002112000073 20021120 00073 WP 2002 11 20 AALA20021358 1 20020924 A 2150 COALESCER BAG DOUG DC9 DC982 3022082 WP A/C BAY DIRTY A AALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 456AA 49561 SAN - FLT 418 - EN ROUTE SAN-DFW, HEAVY SMOKE IN THE CABIN. DECLARED EMERGENCY AND RETURNED TO SAN WITHOUT INCIDENT. A CCOMPLISHED MAINTENANCE CHECK MANUAL CARD 21-96-01 AND FOUND NO DISCREPANCIES. ACCOMPLISHED PACK BURN OUT PER MM 21-20- 02-2 AND REPLACED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112000074 20021120 00074 NM 2002 11 20 AALA20021382 1 20020928 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS WIRES AT SEATS 36 C/D DISCONNECTED. RECONNECTED WIRES AT CONNECTOR . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002112000075 20021120 00075 WP 2002 11 20 ARWA20021107 1 20021118 A 2911 10112301 ACCUMULATOR DOUG DC8 DC863F 302198F WP A ARWA A J UNSCHED LANDING DUMP FUEL F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 19 906R 46087 LOG PAGE # 502922. DISCREPANCY: ON CLIMB OUT OF MIA AT 8.0, OBSERVED QUANTITY DROPPED TO STAND PIPE WITH RESERVE LOW A ND AILERON AND RUDDER REVERSION LITES ON; EMERGENCY CHECK LIST ACCOMPLISHED, FUEL DUMPED TO MAX LANDING WEIGHT PER ABN C HECK LIST. CORRECTIVE ACTION: FOUND HORIZONTAL STABILIZER AND RUDDER HYDRAULIC PRESSURE ACCUMULATOR LEAKING. REMOVED AND REPLACED HYDRAULIC PRESSURE ACCUMULATOR IAW MM 27-41-11. OPS NORMAL, NO LEAKAGE NOTED. ALSO BLEEDED BOTH ENGINE D RIVEN HYDRAULIC PUMPS IAW MM 29-10-12. OPS CHECK NORMAL IAW MM 12-30-1. 2 L 7 4 4F 4A25 2002112000076 20021120 00076 WP 2002 11 20 IXXA0200113O 1 20021112 A 3260 45973405505 ACTUATOR DOUG DC8 DC873F 302199F WP MLG DOOR UPLOCK DEFECTIVE A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 606AL 88900 653 46044 EN ROUTE FROM DFW TO IAH, THE DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED DURING THE GEAR UP LATCH CHECK. THE FLIGHT CR EW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO IAH FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND DISCOVERED THE RT UPLOCK ACTUATOR DEFECTIVE. MAINTENANCE REPLACED THE U PLOCK ASSEMBLY AND PERFORMED SUCCESSFUL OPERATIONAL CHECKS IN ACCORDANCE WITH THE DOUGLAS REPAIR MANUAL. THE AIRCRAFT W AS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002112000077 20021120 00077 EU 2002 11 20 GXPA0205 1 20021106 A 7931 TRANSMITTER AMD FALC20 FALCOND 2720304 EU GE CF700 CF7002D2 30010 NE OIL PRESSURE FAILED E GXPA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 23 618GA 211 AIRCRAFT LANDED, DUE TO LT ENGINE OIL PRESSURE LIGHT CAME ON. LT ENGINE OIL PRESSURE TRANSMITTER REPLACED. GROUND RUN PERFORMED, OPS CHECKED GOOD. 2 L 7 2 4F 4 F A7EU E7EA 2002112000078 20021120 00078 CE 2002 11 20 JGV2002F00014 1 20021028 A 2720 4555400001V3800 RUDDER LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE73160 NE VERTICAL STAB OUT OF RIG B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 882CA 155 UPON REINSTALLATION OF RUDDER AFTER INSTALLATION OF SB, FOUND THAT THE RUDDER TRAVEL WAS APPROXIMATELY 25 DEGREES IN LIE U OF 30+/-DEGREES IAW MM. WHEN TRAVEL WAS CORRECTED, DISCOVERED THAT THE BOTTOM SKIN OF RUDDER WAS CONTACTING THE SKIN PRIOR TO ACHIEVING FULL TRAVEL. FIELD SERVICE AND FIELD REPAIR WERE CONTACTED. THE RUDDER WAS REPLACED WITH SAME PN AN D SN 0155. NO OTHER ACTION WAS REQUIRED AT THAT TIME. 2 L 7 2 4F 4 F RT T00008WI E1NM 2002112000079 20021120 00079 EA 2002 11 20 M02021 1 20020207 A 3340 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EXTERIOR BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17231 7231 DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT THE EXTERIOR NR 4 EMERGENCY EXIT LIGHT WAS INOPERATIVE. MECHANIC R EPLACED THE BULB, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002112000080 20021120 00080 NM 2002 11 20 M02022 1 20020209 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 449YV 449 DURING ROUTINE MAINTENANCE, SEVERAL EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE. MECHANIC REPLACED THE NR2 EMERGENCY POW ER SUPPLY. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2002112000081 20021120 00081 EA 2002 11 20 M02023 1 20020211 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF341A NE EMERGENCY LIGHT BURNED OUT A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 87353 7353 DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT THE RIGHT FORWARD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MECHANIC REMOVED AND REPLACED THE LIGHTS. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (SW072002B1585) 2 L 7 2 4F 4 F RT A21EA E15NE 2002112000082 20021120 00082 SO 2002 11 20 M02095 1 20020622 A 2120 SMOKE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN DETECTED A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 07 833MJ 145327 SMOKE AND FUMES IN CABIN WITH SMOKE DETECTOR ALARM. NO SMOKE & FUMES SOURCE DETERMINED. AFTER MECHANIC RAN UP ENGINES AND APU. FUMES AND SMELL DISSIPATED. NO FURTHER ACTION REQUIRED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002112000083 20021120 00083 NE 2002 11 20 M02121 2 20020812 A 7297 CONNECTOR DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE NR 2 ENGINE LOOSE A MASA D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 449YV 449 RETURNED TO THE GATE. NR 2 ENGINE HAD SIGNIFICANT RPM DROP WHEN POWER LEVERS MOVED FROM DISK TO FLIGHT IDLE. MECHANIC SECURED LOOSE CONNECTOR PLUG. OPS CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2002112000084 20021120 00084 WP 2002 11 20 MEX2002270 1 20020819 A 3260 0080004003 PROXIMITY SWITCH DOUG DC9 DC932 3022066 WP PWA JT8 JT8D* NE NLG FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 23 1003P 20032 20032 48150 AIRCRAFT RETURNED, DUE TO NOSE LANDING GEAR RED LIGHT AND LANDING GEAR DOORS WERE OPEN. O-RINGS FOR THE NOSE LANDING GE AR WERE REPLACED. IAW MM SENSOR T2-61 WAS REPLACED IAW WD AND THE PROXIMITY SWITCH WAS REPLACED IAW MM. AFTER THAT, DU RING THE TOWING TURNED ON AGAIN THE RED LIGHT OF THE NOSE LANDING GEAR. PROXIMITY SENSOR WERE VERIFIED. TESTS OK. 2 L 7 2 4F 4 F A6WE E2EA 2002112000085 20021120 00085 2002 11 20 S2YA02014 4 20020417 A 3418 84321 STICK SHAKER DORNER DO32 DO328300 NM PWA 306 PW306B NE STALL WARNING INOPERATIVE A S2YA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 357SK 2700 3164 JUST AFTER TAKEOFF OF FLIGHT, THERE WAS A CAS MESSAGE FOR STICK PUSHER FAIL. THE CREW DID AN AIR TURN BACK. MECHANIC R EPLACED THE STICK PUSHER AND OPERATIONAL CHECK THE SYSTEM. 2 H 7 2 4T 4 F RT A55NM E35NE 2002112000086 20021120 00086 EU 2002 11 20 USAA020361 1 20020910 A 5330 SKIN AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 723UW 1109 FUSELAGE SKIN HAS A 2 INCH CRACK. 2 L 7 2 4F 4 F RT A28NM E2GL 2002112000090 20021120 00090 CE 2002 11 20 FMAA2002002 1 20020915 A 2750 S19061 SWITCH CESSNA 207 T207 2073612 CE CONT O520 IO520F 17032 SO TE FLAPS INOPERATIVE E FMAA K NONE O OTHER IN INSP/MAINT 1 AL 01 207DG 564 20700070 280244R FLAP SWITCH IS HELD TO THE ARM ASSEMBLY WITH SMALL NR 40 MACHINE SCREWS. IF SCREWS ARE OVER TIGHTENED, THE PLASTIC SWIT CH CRACKS, IF IT IS NOT TIGHTENED ENOUGH, IT LOOSENS WHICH CHANGES THE ADJUSTMENT OF THE FLAPS. THE SWITCH WIRES OBVIOU SLY LOOSENED ENOUGH TO ALLOW THE FLAPS TO NOT COME DOWN TO THE 10 DEGREE POSITION, WHICH RESULTED IN AN ABORTED TAKEOFF AT FULL GROSS WEIGHT, WHICH RESULTED IN THE NOSE GEAR BEING TORN FROM THE AIRCRAFT. 1 H 7 1 3O 3 O A16CE E5CE 2002112000091 20021120 00091 NE 2002 11 20 HXS2002F00000 2 20020729 A 7250 LABYRINTH SEAL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE REAR BEARING DAMAGED B HXSD A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AL 05 301TH 709 9022 IT WAS NOTICED THAT AIRCRAFT WAS TRAILING OIL & SMOKE FROM THE EXHAUST IN FLIGHT AND DID A LANDING AND INVESTIGATED. F OUND OIL ON TAIL BOOM AND EXHAUST TURBINE. GROUNDED AIRCRAFT. PREFORMED ENGINE CHANGE UP, AT LANDING SITE. SENT ENGIN E FOR INVESTIGATION. IT IS DETERMINED THAT THE REAR BEARING WAS COKED AND CAUSED THE LABYRINTH SEAL TO LEAK. ENGINE WA S CLEANED TESTED AND SENT BACK AS SERVICEABLE. 1 G 7 1 3U 3 U H9EU E19EU 2002112000092 20021120 00092 NM 2002 11 20 AALA20021383 1 20020928 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AN 29606 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS AT SEATS 9H/10H INOPERATIVE. TIGHTENED EMERGENCY LIGHT CONNECTOR A T SEAT 9H/10H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002112000093 20021120 00093 NM 2002 11 20 AALA20021384 1 20020929 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7375A 25202 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 20G BULKHEAD DAMAGED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002112000094 20021120 00094 NM 2002 11 20 AALA20021417 1 20021002 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY CLOSET EMERGENCY EXIT LIGHT DAMAGED. REPLACED FORWARD GALLEY CLOSET EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002112000095 20021120 00095 NM 2002 11 20 AALA20021418 1 20021002 A 2422 INVERTER BOEING 767 767323 1385205 NM CABIN FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 363AA 24044 PIK - FLT 37 - EN ROUTE ZRH-DFW, SMOKE IN COCKPIT DURING CRUISE WITH ASSOCIATED EICAS MESSAGE. STANDBY INVERTER FAILED. DIVERTED TO PIK LANDED WITHOUT INCIDENT. REPLACED STANDBY INVERTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002112000096 20021120 00096 NM 2002 11 20 AALA20021422 1 20021004 A 3350 PIN BOEING 767 767223 1385123 NM CONNECTOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 336AA 22334 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT AT SEAT 31B INOPERATIVE. REPLACED BROKEN PIN AT CONNECT OR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002112000097 20021120 00097 NM 2002 11 20 BJNA021007 1 20021018 A 5315 FLOORBEAM BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 23043 DURING SCHEDULED C-CHECK INSPECTION DISCOVERED FORWARD LAVATORY FLOOR STATION 294.5 WL 208 LBL 12 FLOORBEAM HAS 12 INCHE S OF CORROSION. FLOORBEAM CORRODED MORE THAN 50 PERCENT, OUT OF LIMITS. REMOVED CORRODED FLOORBEAM UPPER T-CAP AND SPL ICE. FABRICATED REPAIR T-CAP AND SPLICE. INSTALLED IAW B737 53-10-9 AND 51-30-2 FIG 5. (M) 2 L 7 2 4F RT A16WE 2002120500088 20021205 00088 EU 2002 12 5 DHL2002362511 1 20021025 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 ELONGATED HOLE UNDER R1 DOOR SCUFF PLATE, 3RD HOLE FROM AFT, CENTER ROW. REAMED HOLE AND INSTALLED BUSHING. WORK DONE IAW OE-084-09-02-007, TD582.0632/2002, RAS AS/0334/2002 2 L 7 2 4F RT A35EU 2002050700187 20020507 00187 NM 2002 5 7 QXEA0200735 1 20020505 A 3350 6138001 BATTERY PACK BOMBDR DHC8 DHC8401 1390041 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 404QX 1952 4046 GEG-EMERGENCY LIGHTS IN AFT GALLEY INOPERATIVE. REPLACED BOTH BATTERY PACKS IN AFT POWER SUPPLY. LIGHTS OPERATE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002112000098 20021120 00098 NM 2002 11 20 BJNA021008 1 20021015 A 5514 ANGLE BOEING 737 737282 13844AT NM HORIZ STAB CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 46628 23043 LEFT CENTER HORIZONTAL STABILIZER REAR STABILIZER FITTING HAS CRACKED ANGLE STATION 1170, BELOW LEFT HORIZONTAL STABILIZ ER PIN/AFT. REMOVED CRACKED ANGLE IAW B737 SRM 51-30-2. TRIMMED TO FIT NEW SUPPORT ANGLE IAW B737 SRM 51-30-5, 51-10-1 , 51-20-1 FIG 1/2. INSTALLED IAW B737 SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 2003020700141 20030207 00141 EU 2003 2 7 DHL2002362512 1 20021022 A 5230 FITTING AIRBUS 300 A300B4203 3930306 EU TORQUE BOX CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 AFT CARGO DOOR, AFT LOWER CORNER NR 3 EXTERNAL TORQUE BOX AFT FITTING CRACKED, REMOVED LATCH ASSY IAW A3OO SRM 51-30-30, CUT OUT DAMAGE, NDT INSPECTED AREA IAW NTM 51-31-05, NO CRACKS FOUND. FABRICATED DOUBLER AND FILLER AND TAPPERED SHIM. TREATED AND PRIMED PARTS IAW A300 SRM 51-41-12. INSTALLED REPAIRED PARTS IAW A300 SRM 51-30-30, INSTALLED LATCH ASSY IA W A300 SRM 51-30-30. ALL WORK WAS DONE IAW APPROVAL BY DGAC ON RAS/DABRE/7002272/2002 2 L 7 2 4F RT A35EU 2003021000021 20030210 00021 NM 2003 2 10 DHL2002743500 1 20021112 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, AFT CARGO BAY HAS A CORROSION SPOT ON FRAME TO FUSELAGE BS 1070 STR 29R FWD SIDE. REMOVED SURFACE COR ROSION WITH A MATERIAL LOSS 0.28 AND IS OUT OF LIMITS IAW B-727 SRM 53-10-1. FABRICATED ANGLE REPAIR DIMENSIONS 3 X 2 X 1 INCHES. ALODINED AND PRIMED ANGLE. INSTALLED REPAIR ANGLE R 35070 IAW B-727 SRM 53-10-4. 2 L 7 3 4F A3WE 2003020700142 20030207 00142 EU 2003 2 7 DHL2002362513 1 20021114 A 5755 STRUCTURE AIRBUS 300 A300B4203 3930306 EU SPEED BRAKE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 LT NR 1 SPEED BRAKE HAS CORROSION AROUND 17 FASTENERS. DAMAGED AREA WAS REPAIRED BY CUTTING OUT AREAS OUT OF LIMITS AND FABRICATING AND INSTALLING 2 FILLERS, 1X4 INCHES, 2 L 7 2 4F RT A35EU 2002112000099 20021120 00099 NM 2002 11 20 BJNA021009 1 20021019 A 5320 FLOOR SUPPORT BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 46628 23043 DURING SCHEDULED C-CHECK INSPECTION DISCOVERED FLOOR SUPPORT BETWEEN FRAME 947-967 RIGHT APPROX BL40R HAS FLAKING CORROS ION. FLOOR SUPPORT CORRODED OUT OF LIMITS. FABRICATED REPLACEMENT SUPPORT AND INSTALLED IAW B737 SRM 53-10-1, 51-10-2 AND 51-30-2. (M) 2 L 7 2 4F RT A16WE 2002112000100 20021120 00100 NM 2002 11 20 BJNA021010 1 20021023 A 5315 FLOORBEAM BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 46628 23043 CORROSION ADJACENT TO WATER DRAIN LINE FORWARD UNDER SIDE OF R2 DOOR SCUFF PLATE AREA BS 958 RBL 53. REMOVED CORROSION FROM LOWER OUTBOARD FLOORBEAM SUPPORT, CORROSION WENT OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW B737 S RM 51-40-3, 51-10-2, 51-20-1 AND 51-30-2. (M) 2 L 7 2 4F RT A16WE 2002112000101 20021120 00101 NM 2002 11 20 BJNA021011 1 20021010 A 5320 INTERCOSTAL BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 23043 NOSE WHEEL WELL LEFT SIDE AT AFT ACCESS PANEL SUPPORT BEAMS, THREE EACH HAS EXFOLIATED CORROSION FS 280. REMOVED AND RE PLACED TWO EXFOLIATED INTERCOSTALS IAW B737 SRM 51-30-2, 51-20-1, B737 MM 51-21-0. REMOVED CORROSION FROM THIRD VERICAL BEAM FOUND TO BE WITHIN LIMITS. (M) 2 L 7 2 4F RT A16WE 2002112000102 20021120 00102 NM 2002 11 20 BJNA021012 1 20021009 A 5315 FLOORBEAM BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 23043 FLOORBEAM BS 976, LBL 53 HAS EXFOLIATED CORROSION. REMOVED FLOORBEAM, FABRICATED AND INSTALLED FLOORBEAM REPAIR 55 INCH ES BY 1.5 INCHES BAC1505-100617, IAW TIMCO REO-L00597 REV A. (M) 2 L 7 2 4F RT A16WE 2002112000103 20021120 00103 WP 2002 11 20 ZW0A021161 1 20021119 A 3350 BATTERY DOUG DC9 DC982 3022082 WP DISCHARGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 957U 49702 EMERGENCY EGRESS EXIT SIGN INOP IN TAIL SECTION. REPLACED BATTERY IN EMERGENCY EXIT SIGN. LAST CHECK C PERFORMED IN STL 11/27/2001. --CLOSED-- 2 L 7 2 4F A6WE 2002112000104 20021120 00104 WP 2002 11 20 ZW0A021162 1 20021119 A 3350 0105606003 LAMP DOUG DC9 DC983 3022083 WP BURNED OUT A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 EGRESS LIGHTING AT ROWS 27-30 INOP. REPLACED EGRESS LAMP MODULE ASSEMBLY. LAST CHECK C PERFORMED IN STL 10/19/2002. --CL OSED-- 2 L 7 2 4F RT A6WE 2002112000105 20021120 00105 NM 2002 11 20 BJNA021013 1 20021010 A 5320 STRINGER CLIP BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 23043 AFT FUSELAGE FLOORBEAM STATION 967 LEFT SIDE WHERE MEETS CIRCUMFERENTIAL FRAME HAS CORRODED STRINGER TIE. REMOVED STRIN GER TIE CLIP, FABRICATED AND INSTALLED REPAIR CLIP IAW B737 SRM 51-10-2, 51-30-2 AND 51-20-1. (M) 2 L 7 2 4F RT A16WE 2002112000106 20021120 00106 NM 2002 11 20 BJNA021014 1 20021010 A 5753 SKIN BOEING 737 737282 13844AT NM T/E FLAP GOUGED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 46628 23043 RIGHT WING OUTBOARD FLAP, LOWER FORE FLAP LEADING EDGE SKIN GOUGED, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 57-50-4 FIG 2, 51-10-2 AND 51-30-8. (M) 2 L 7 2 4F RT A16WE 2002112000107 20021120 00107 NM 2002 11 20 BJNA021015 1 20021009 A 5754 SKIN BOEING 737 737282 13844AT NM L/E SLAT CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 46628 23043 LEFT WING NR 2 SLAT TRAILING EDGE CHAFED AND CRACKED AT OUTBOARD AUX SLAT TRACK. REPAIRED CRACKED AND CHAFED LEFT WING NR 2 SLAT TRAILING EDGE AT OUTBOARD AUX SLAT TRACK BY CUTTING OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR FILLE R AND DOUBLER IAW B737 SRM 51-30-2 AND 51-40-2. (M) 2 L 7 2 4F RT A16WE 2002112000108 20021120 00108 NM 2002 11 20 USAA020384 1 20021005 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 573US 47579 23560 PIT - FOUND SKIN WITH THREE CRACKS, ONE AT .075 INCH, TWO AT .250 INCH, STATION 380 BL 0. CUT OUT DAMAGE, INSTALLED FIL LER AND DOUBLER PER TYPICAL REPAIR 53-30-07. (M) 2 L 7 2 4F RT A16WE 2002112000109 20021120 00109 NM 2002 11 20 USAA020385 1 20021006 A 5320 STIFFENER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 43582 24412 PIT - FOUND VERTICAL STIFFENER CRACKED, .5 INCH LONG, STATION BS 663.75 BULKHEAD LBBL 6.15. INSTALLED V CHANNEL AND REP AIR STRAPS PER EA 75030. (M) 2 L 7 2 4F RT A16WE 2002112000110 20021120 00110 NM 2002 11 20 USAA020386 1 20021007 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 38820 23988 PIT - FOUND SKIN CRACKED 1.25 INCH, STATION 727D STRINGER 24 LEFT. INSTALLED DOUBLER AFTER REMOVING DAMAGE PER SRM 53-0 0-01. (M) 2 L 7 2 4F RT A16WE 2002112000111 20021120 00111 NM 2002 11 20 USAA020387 1 20021004 A 5320 69620146 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 522AU 44138 23857 PIT - FOUND VERTICAL Z-ANGLE CRACKED IN HALF, CENTER OF ANGLE FORWARD BULKHEAD LEFT OF W/W STATION 663 LBBL 6.15. INSTA LLED TEMP SUPPORT ANGLE AND STRAPS EPR EA 75002. (M) 2 L 7 2 4F RT A16WE 2002112000112 20021120 00112 NM 2002 11 20 USAA020388 1 20021004 A 5320 69620146 ANGLE BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 46150 23935 PIT - FOUND VERT Z-ANGLE CRACKED IN HALF, FORWARD BULKHEAD LEFT SIDE W/W STATION 663 LBBL 6.15. INSTALLED TEMP SUPPORT ANGLE AND STRAPS PER EA 74968A. (M) 2 L 7 2 4F RT A16WE 2002112000113 20021120 00113 NM 2002 11 20 USAA020389 1 20021003 A 5320 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 48447 22957 PIT - FOUND ANGLE CRACKED 1.5 INCHES LONG, STATION 927-947.5 AT BL 0. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SR M 53-60-51 PAGE 108. (M) 2 L 7 2 4F RT A16WE 2002112000114 20021120 00114 NM 2002 11 20 USAA020390 1 20021004 A 5320 6962146 STIFFENER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 355US 42407 23558 IT - FOUND STIFFENER ANGLE CRACKED 1 INCH LONG, VERTICAL STIFFENER MLG W/W FORWARD BULKHEAD CENTER LINE STATION 663. FA BRICATED AND INSTALLED 2 REPAIR STRAPS AND ATTACH ANGLE IAW EA 75025. (M) 2 L 7 2 4F RT A16WE 2002112000115 20021120 00115 NM 2002 11 20 USAA020391 1 20021006 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 43478 24479 PIT - FOUND FASTENERS CORRODED .5 INCH CIRCLES, FS 1016 PRESS WEB RBBL 4 AFT OF LEVELING COMPAD. BLENDED CORROSION PER SRM 53-80-08 AND SRM 51-20-01. (M) 2 L 7 2 4F RT A16WE 2003021000022 20030210 00022 NM 2003 2 10 DHL2002743501 1 20021112 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, FWD. CARGO FRAME BS 600 HAS A DENT INTO THE RADIUS AT STR 25 LT. PART ALODINED AND PRIMED IAW B-727 SR M 51-10-2. INSTALLED PART IAW B-727 SRM 51-30-2. REMOVED AND REPLACED FRAME SPLICE IA/W B-727 SRM 53-10-2 FIG. 3. 2 L 7 3 4F A3WE 2002112000116 20021120 00116 WP 2002 11 20 MWEA020647 1 20021029 A 5320 99365345 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 SUBFLOOR AT FRAME STATION 194 INBOARD OF PAX DOOR CUTOUT CORRODED. SUBFLOOR CUT OUT AND REMOVED, FABRICATED AND INSTALL ED REPAIR. 2 L 7 2 4F A6WE 2002112000117 20021120 00117 WP 2002 11 20 MWEA020655 1 20021029 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 STATION 218 LONGERON 18 LEFT. REMOVED SEVERAL FASTENERS THAT ATTACH CLIP TO FRAME, REMOVED ATTACH CLIP, DRILLED NEW FI TTING AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 2002112000118 20021120 00118 WP 2002 11 20 MWEA020657 1 20021029 A 5320 59568791 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 LEFT HAND SIDE OF FUSELAGE AT STATION 200-207 HAS A WEB AT FLOOR LEVEL HAS HEAVY CORROSION. REMOVED WEB, LOCATED AND DR ILLED NEW WEB AND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2002112000119 20021120 00119 WP 2002 11 20 MWEA020659 1 20021029 A 5310 5936038501 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 AFT CARGO COMPARTMENT HAS MODERATE CORROSION ALONG LOWER DOOR JAMB STATION 1155-1193. REMOVED LOWER DOOR JAMB, LOCATED AND DRILLED DEBURRED DOOR JAMB. 2 L 7 2 4F A6WE 2002112000120 20021120 00120 WP 2002 11 20 MWEA020660 1 20021029 A 5311 39364451 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 AFT CARGO COMPARTMENT HAS LIGHT CORROSION ON AFT SIDE OF FRAME STATION 1098 LONGERON 29R TO 29L. REMOVED CORROSION AND FRAME, LOCATED AND DRILLED NEW FRAME. 2 L 7 2 4F A6WE 2002112000121 20021120 00121 WP 2002 11 20 MWEA020664 1 20021029 A 5320 59124921 PAN DOUG DC9 DC981 3022081 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FORWARD GALLEY DOOR CUTOUT LOWER PAN GOUGED IN SEVERAL PLACES. BLENDED GOUGES, BLENDED OUT AREAS ACCEPTABLE FOR STRENGT H IAW MWX-MKE 02-00164H. 2 L 7 2 4F A6WE 2002112000122 20021120 00122 WP 2002 11 20 MWEA020674 1 20021111 A 5320 99365345 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 SUBFLOOR AT FRAME STATION 200 AND 210 INBOARD OF FUSELAGE CORRODED. FABRICATED AND INSTALLED SUBFLOOR REPAIR. 2 L 7 2 4F A6WE 2002112000123 20021120 00123 WP 2002 11 20 MWEA020679 1 20021111 A 5320 9910078291 WEB DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 REMOVED FOR MAINTENANCE SECTION OF SUBFLOOR BETWEEN FRAME STATION 200-218 AND X-9.0-15.0. FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR SECTION. 2 L 7 2 4F A6WE 2002112000124 20021120 00124 WP 2002 11 20 MWEA020682 1 20021111 A 5320 993053866 WEB DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 PREVIOUS REPAIR AT SUBFLOOR BETWEEN FRAME STATIONS 237 & 256 INBOARD OF NR 4 SEAT TRACK. FABRICATED AND INSTALLED REPAI R PLATE AND SPLICE. 2 L 7 2 4F A6WE 2002112000125 20021120 00125 WP 2002 11 20 MWEA020686 1 20021111 A 5315 991556175 FLOORBEAM DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FLOORBEAM AT STATION 1338 RIGHT OUTBOARD SIDE HAS CORROSION. FABRICATED AND INSTALLED FILLER, DOUBLER, AND STAR FITTING S. 2 L 7 2 4F A6WE 2002112000126 20021120 00126 WP 2002 11 20 MWEA020696 1 20021115 A 5315 9912243209 FLOORBEAM DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 CENTER FLOOR BEAM ANGLE FLANGE AT STATION 1309 BLENDED BEYOND LIMITS. AREA IS ACCEPTABLE FOR STRENGTH AW MWX-MKE-02-001 28H. 2 L 7 2 4F A6WE 2002112000127 20021120 00127 WP 2002 11 20 MWEA020699 1 20021115 A 2410 696233B CSD DOUG DC9 DC932 3022066 WP RT ENGINE MALFUNCTIONED A MWEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 212ME 47701 CREW NOTICED RIGHT CSD LOW OIL PRESSURE LIGHT CAME ON. REMOVED AND REPLACED RIGHT CONSTANT SPEED DRIVE UNIT. 2 L 7 2 4F A6WE 2002112000128 20021120 00128 EA 2002 11 20 COMA0260655 1 20021117 A 2750 857SD100101 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA L/H #1 SHEARED A COMA O OTHER S AFFECT SYSTEMS DE DESCENT 1 SO 01 988CA 7204 FLIGHT 5443 FLAPS FAIL CAUTION MESSAGE.REPLACED THE L/H #1 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2003020700143 20030207 00143 EU 2003 2 7 DHL2002362514 1 20021115 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 ELONGATED HOLE ON SCUFF PLATE AREA BELOW R1 DOOR, 4TH HOLE DOWN ON AFT EDGE, HOLE MEASURES .284 X .305 INCH . REAMED HO LES TO .3125 INCH IAW AIRBUS TECHNICAL DEPOSITION. ROTOTEST PERFORMED PER NTM 51-30-10, NO CRACKS FOUND. INSTALLED BUSHI NG IAW A300 SRM 51-10-50. 2 L 7 2 4F RT A35EU 2002112000129 20021120 00129 WP 2002 11 20 MWE020703 1 20021119 A 2752 5912150510 BUSHING DOUG DC9 DC981 3022081 WP FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 LEFT OUTBOARD FLAP, INBOARD AFT HINGE BRACKET HINGE POINT AND ACUTATOR MOUNT HAT BUSHINGS ARE WORN. -- REMOVED CORROSI ON AND INSTALLED NEW HINGE. 2 L 7 2 4F A6WE 2002112000130 20021120 00130 WP 2002 11 20 MWEA020707 1 20021119 A 2752 4913767503 BUSHING DOUG DC9 DC981 3022081 WP FLAP WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 RIGHT OUTBOARD FLAP HINGE BRACKET HAS WORN HINGE POINT BUSHINGS. -- FABRICATED AND INSTALLED REPAIR BUSHINGS. 2 L 7 2 4F A6WE 2002112000131 20021120 00131 WP 2002 11 20 MWEA020712 1 20021119 A 5311 5912528501 PAN DOUG DC9 DC932 3022066 WP AFT PIT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 AFT PIT DOOR JAMB PAN HAS AREAS OF CORROSION. -- REMOVED AND REPLACED PAN AND SPLICE PLATE. 2 L 7 2 4F A6WE 2002112000132 20021120 00132 WP 2002 11 20 MWEA020713 1 20021119 A 5313 3912253529 SPLICE DOUG DC9 DC932 3022066 WP STA 503 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FORWARD CARGO BAY AFT SIDE AND BOTTOM SIDE OF FRAME HEAVILY CORRODED STATION 503 LONGERON 28 RIGHT TO 28 LEFT. -- CUT AND REMOVED CORRODED SECTION OF FRAME AND INSTALLED Z FRAME REPAIR SPLICE. 2 L 7 2 4F A6WE 2002112000133 20021120 00133 WP 2002 11 20 MWEA020714 1 20021120 A 5310 5956039509 TRACK DC9 DC932 3022066 WP AFT LWR PIT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 AFT PIT, AFT LEFT CARGO TIE-DOWN TRACK IS CORRODED OUT OF LIMITS. -- FABRICATED AND INSTALLED REPLACEMENT TRACK. 2 L 7 2 4F A6WE 2002112000134 20021120 00134 WP 2002 11 20 MWEA020715 1 20021120 A 5311 995791739 ANGLE DOUG DC9 DC932 3022066 WP BAGGAGE PIT DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 AFT BAGGAGE PIT FRAME HAS A DENT IN IT BETWEEN THE DOOR JAMB AND THE DOOR BEAM. -- FABRICATED AND INSTALLED REPAIR ANG LE. 2 L 7 2 4F A6WE 2002112100001 20021121 00001 EU 2002 11 21 HXS2002F00001 1 20020918 A 7712 70BM012000 MODULE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE TORQUE FAILED B HXSD O OTHER O OTHER NR NOT REPORTED 1 AL 05 405AE 465 3286 TORQUE INDICATION STARTED TO FLUCTUATE, AIRCRAFT GROUNDED. 1 G 7 1 3U 3 U H9EU E00054EN 2002112100002 20021121 00002 EU 2002 11 21 HXS2002F00002 1 20020605 A 7712 70BM012000 MODULE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE TORQUE INDICATOR FAILED A HXSD O OTHER L NO TEST NR NOT REPORTED 1 AL 05 405AE 401 56 3286 TORQUE INDICATION STARTED TO FLUCTUATE. REMOVED NR 1 MODULE WHICH HOUSES THE TORQUE TUBE AND INSTALLED A RENTAL. SENT NR 1 OUT FOR REPAIR. IT WAS DETERMINED THAT THE ROLL PINS IN TORQUE TUBE HAD SHEARED OFF. 1 G 7 1 3U 3 U H9EU E00054EN 2002112100003 20021121 00003 EU 2002 11 21 HXS2002F00003 1 20020710 A 7712 70BM012000 MODULE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE TORQUE INDICATOR FAILED A HXSD O OTHER L NO TEST NR NOT REPORTED 1 AL 01 405AE 1069 70 3286 TORQUE INDICATION STARTED TO FLUCTUATE. REMOVED MO1 MODULE WHICH HOURS THE TORQUE TUBE AND INSTALLED RENTAL MODUAL, SEN T MO1 TO MFG. THIS WAS THEIR RENTAL. THEY DID NOTIFICATION THAT THIS WAS THE SAME TYPE OF FAILURE BEFORE IN THE FACT T HAT THE ROLL PINS ON THE TORQUE TUBE HAD SHEARED. 1 G 7 1 3U 3 U H9EU E00054EN 2002112100004 20021121 00004 EU 2002 11 21 HXSA0000375 1 20020618 A 7712 70BM012000 MODULE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE TORQUE INDICATOR FAILED B HXSA O OTHER L NO TEST NR NOT REPORTED 1 AL 01 405AE 1069 70 3286 REMOVED ENGINE MODULE 1 DUE TO TORQUE SYSTEM REFERENCE SHAFT PHONIC WHEEL ROLL PINS SHEARING CAUSING LOSS OF TORQUE INDI CATION VEMD. REMOVED LOANER MODULE 1 FOR REPAIR. INSTALLED LOANER MODULE. SENDING UNIT TO MFG FOR REPAIR. 1 G 7 1 3U 3 U H9EU E00054EN 2002112100006 20021121 00006 NM 2002 11 21 2002F00995 1 20021028 A 2160 62594610 CONTROLLER BOEING 757 75728A 1384976 NM A/C BAY INOPERATIVE G K NONE J WARNING INDICATION CR CRUISE 1 GL 11 521AT 24368 (SUPP-CLOSED) FLIGHT NUMBER 73. DURING CRUISE LEFT PACK TEMP EICAS MESSAGE AND PACK INOP LIGHT ILLUMINATED IN AUTO MODE/ MANUAL MODE OPERATES NORMAL. MAINTENANCE REMOVED AND REPLACED LEFT PACK TEMP CONTROLLER PER MM 21-51-14-4. OPERATIONAL C HECKS NORMAL. 2 L 7 2 4F RT A2NM 2002112100007 20021121 00007 NM 2002 11 21 2002F00996 1 20021029 A 2840 WARNING LIGHT BOEING 757 75733N 1384931 NM FUEL BOOST ILLUMINATED G O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 551TZ 32585 (ORIG-OPEN) FLIGHT NUMBER 593. DURING CRUISE RIGHT CENTER BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED. EICAS MESSAGE "CTR R FUEL PUMP" DISPLAYED. AT THE TIME THERE WAS 4100 LBS OF FUEL. 2 L 7 2 4F RT A2NM 2002112100008 20021121 00008 2002 11 21 2002F00997 4 20021023 A 2330 7002205006 CONNECTOR BOEING 737 73783N 13844HI NM CABIN FAILED G H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 311TZ 32578 (ORIGINAL CLOSED) - FLIGHT ATTENDANT REPORTED A SMELL OF BURNINIG RUBBER AROUND ROW 21DEF,IT SEEMED TO BE COMING FROM TH E PAX HEAD SET CORDS. THE CORDS WERE UNPLUGGED AND THE POWER WAS REMOVED FROM THE INFLIGHT ENTERTAINMENT SYSTEM. REMOVE D AND REPLACED SEAT ROW 21 DEF AUDIO JACKS PER 44-04-18 OF THE ROCKWELL COLLINS A.M.M. OPERATION CHECK GOOD AT TIME PER ROCKWELL COLLINS A.M.M. 44-04-18. 2 L 7 2 4F RT A16WE 2002112100009 20021121 00009 NE 2002 11 21 2002F00998 2 20021103 A 7320 47385 CONTROLLER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE INOPERATIVE G H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 GL 11 516AT 11693 11693 27972 31449 (ORIG-CLOSED) FLIGHT NUMBER 108. DURING CRUISE RT ENGINE LIMITER & RT ENGINE EEC ILLUMINATED. MAINTENANCE TROUBLESHOT PE R FIM 73-21-00, PAGE 1, BLOCK 53 "CHANGE "A" CHANNEL DGCU. MAINTENANCE REMOVED AND REPLACED "A" CHANNEL DGCU PER AMM 73- 21-10-4. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002112100010 20021121 00010 NM 2002 11 21 2002F00999 1 20021101 A 3350 CONNECTOR BOEING 757 75723N 1384973 NM CABIN DISCONNECTED G K NONE L NO TEST IN INSP/MAINT 1 GL 11 519AT 27975 (ORIG-CLOSED) DURING SCHEDULED MAINTENANCE EGRESS FLOOR LIGHT INOPERATIVE BY AFT LAVS. MAINTENANCE RECONNECTED CONNECTOR , OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002112100011 20021121 00011 NM 2002 11 21 2002F01000 1 20021101 A 2560 G603104 CONTROL PANEL BOEING 757 75733N 1384931 NM COCKPIT INOPERATIVE G O OTHER N FALSE WARNING CL CLIMB 1 GL 11 552TZ 32586 (ORIG-CLOSED) FLIGHT NUMBER 593. DURING CLIMB EVAC SIGNAL AND LIGHTS OPERATED WITHOUT COMMAND ON GEAR RETRACT AT RSW, SI LENCED HORN, CYCLED COMMAND SWITCH TO OFF TO STOP OPERATION. MAINTENANCE REMOVED AND REPLACED EVACUATION SIGNAL PANEL ON PILOTS OVERHEAD PANEL PER AMM 25-63-01. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002112100012 20021121 00012 NM 2002 11 21 2002F01002 1 20020823 A 5754 STRUCTURE LKHEED 1011 1011 N/A-SDR NM NR 7 SLAT DAMAGED G K NONE O OTHER IN INSP/MAINT 1 GL 11 195AT 193C1041 HOLE IN 7 RT SLAT OUTBD END LOWER SIDE. REPAIRED AREA IAW SRM 57-51-00. WING STATION, FROM OWS 464.5 TO OWS 464.5 2 L 7 3 4F RT A23WE 2002112100013 20021121 00013 NM 2002 11 21 2002F01003 1 20020819 A 5751 STRUCTURE LKHEED 1011 1011 N/A-SDR NM RT AILERON LIGHTNING STRIKE G K NONE O OTHER IN INSP/MAINT 1 GL 11 195AT 193C1041 LIGHTNING STRIKE DISCHARGE AT RT OUTBD AILERON TOP SURFACE. REPAIRED AILERON IAW SRM 51-50-01. WING STATION OWS 502 TO OWS 502. 2 L 7 3 4F RT A23WE 2002112100014 20021121 00014 NM 2002 11 21 2002F01004 1 20020920 A 5311 FRAME LKHEED 1011 1011 N/A-SDR NM FUSELAGE CRACKED G K NONE O OTHER IN INSP/MAINT 1 GL 11 195AT 193C1041 FRAME HAS CRACKS AROUND FWD BOLT HOLE OF FS 1263 FRAME AND PORK CHOP FITTING. REPAIRED PER ERA L10-53R-4927 , CRACK LEN GTH 0.125, 2 CRACKS. BUTTLINE FROM 113 TO 113. 2 L 7 3 4F RT A23WE 2002112100015 20021121 00015 WP 2002 11 21 2002F01006 1 20021106 A 5210 1281T10029 ACTUATOR LKHEED 1011 10113851 5265010 WP PAX DOOR MALFUNCTIONED G K NONE L NO TEST IN INSP/MAINT 1 GL 11 186AT 193C1074 L1 DOOR STOPS MOVING IN THE CLOSE DIRECTION WHEN DOOR BEGINS TO MOVE OUTBOARD, ACTUATOR CONTINUES TO RUN, IF THE SWITCH IS RELEASED LONG ENOUGH FOR ACTUATOR TO STOP, THEN REENGAGED, THE DOOR CONTINUES TO CLOSE. REMOVED AND REPLACED ACTUATO R, REF MM 52-12-01, OPS CK GOOD. 2 L 7 3 4F A23WE 2002112100016 20021121 00016 WP 2002 11 21 2002F01007 1 20021018 A 2120 7405999 COALESCER BAG LKHEED 1011 10113851 5265010 WP CABIN CONTAMINATED G A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 186AT 193C1074 CHEMICAL SMELL DETECTED IN FWD CABIN DURING CRUISE. EMERGENCY LANDING AT MEM. OPERATED ENGINES, APU, AND PACKS, NO FLU ID LEAKS NOTED, COULD NOT DUPLICATE SMELL IN CABIN. R&R PACK WATER SEPERATOR COALECER BAGS. 2 L 7 3 4F A23WE 2002112100017 20021121 00017 WP 2002 11 21 2002F01008 1 20021021 A 5210 SKIN LKHEED 1011 1011385115 5265015 WP PAX DOOR DAMAGED G K NONE O OTHER IN INSP/MAINT 1 GL 11 194AT 193B1230 L1 ENTRY DOOR EXTERIIOR SKIN DAMAGED AT FWD UPPER CORNER. C/W ERA L10-52R-4986 2 L 7 3 4F A23WE 2002112100018 20021121 00018 NM 2002 11 21 2002F01009 1 20021007 A 3340 SWITCH BOEING 737 73783N 13844HI NM COCKPIT LIGHT FAILED G O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 326TZ 32612 IN CRUISE FLIGHT AT FL390 ENROUTE FROM SJU TO MIA CREW NOTICED A STRONG ACRID ODOR IN THE COCKPIT. THIS WAS FOLLOWED ALM OST IMMEDIATELY BY THE SIGHT OF SMOKE COMING FROM THE OVERHEAD LIGHT SWITCH PANEL. CREW DONNED O2 SMOKE MASK, ESTABLISHE D COMMUNICATION,AND FOLLOWED QRH PROCEDURE FOR ELECTRICAL SMOKE IN COCKPIT. SMOKE SUBSIDED JUST BEFORE ALL SWITCHES WERE PLACED IN THE OFF POSITION, THESE REMAINED IN THE OFF POSITION. FLIGHT CONTINUED TO MIA WITHOUT FURTHER INCIDENT. REMO VED AND REPLACED WING LOGO LIGHT SWITCH AT OVERHEAD LIGHT PANEL 2 L 7 2 4F RT A16WE 2002112100019 20021121 00019 NM 2002 11 21 2002F01010 1 20021007 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM CARGO BAY CRACKED G K NONE O OTHER IN INSP/MAINT 1 GL 11 305TZ 30706 (ORIGINAL CLOSED) AFT CARGO BAY FLOOR PANEL 140CF DENTED / CRACKED. REPAIRED DENT/CRACK IAW SRM 51-70-13-2-1 2 L 7 2 4F RT A16WE 2002112100020 20021121 00020 NM 2002 11 21 2002F01011 1 20021104 A 2820 609891002 MOTOR BOEING 757 75733N 1384931 NM CENTER TANK INOPERATIVE G D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 551TZ 32585 (ORIG-CLOSED) RT CENTER BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED. EICAS MESSAGE CTR R FUEL PUMP DISPLAYED. AT THE TIME THERE WAS 4100 LBS OF FUEL IN CENTER TANK. MAINTENANCE REMOVED AND REPLACED RIGHT CENTER MOTOR IMPELLER PER AMM 28-22-03 -4. OPERATIONAL CHECKS NORMAL. LEAK CHECKED, NO LEAKS NOTED. 2 L 7 2 4F RT A2NM 2002112100021 20021121 00021 NM 2002 11 21 2002F01012 1 20021112 A 2822 7G1105 SWITCH BOEING 757 75733N 1384931 NM FUEL BOOST INOPERATIVE G O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 551TZ 32585 (ORIG-CLOSED) FLIGHT NUMBER 597. DURING CRUISE RIGHT CENTER BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED. EICAS MESSAGE CTR R FUEL PUMP DISPLAYED. MAINTENANCE REMOVED AND REPLACED RIGHT CENTER BOOST PUMP PRESSURE SWITCH PER MM 28-42-01, OPERAT IONAL CHECK OK, NO LEAKS NOTED. 2 L 7 2 4F RT A2NM 2002112100022 20021121 00022 NM 2002 11 21 2002F01013 1 20021111 A 3350 CHARGER BOEING 757 75723N 1384973 NM CABIN FAILED G K NONE L NO TEST IN INSP/MAINT 1 GL 11 518AT 27974 (ORIG-CLOSED) DURING SCHEDULED MAINTENANCE ROWS 20 THROUGH 28 EGRESS LIGHTING STAYS ON WHEN POWER REMOVED FROM THE AIRCR AFT. FOUND DURING DAILY SERVICE CHECK. MAINTENANCE REMOVED AND REPLACED BATTERY CHARGER ASSY IAW MM 33-51-07. OPERATIONA L CHECKS GOOD. 2 L 7 2 4F RT A2NM 2002112100023 20021121 00023 NM 2002 11 21 2002F01014 1 20021111 A 2611 2156604 SMOKE DETECTOR BOEING 757 75723N 1384973 NM AFT CARGO INOPERATIVE G K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 11 514AT 27971 (ORIG-CLOSED) DURING SCHEDULED MAINTENANCE STATUS MESSAGE SHOWS AFT CARGO DET 1. MAINTENANCE REMOVED AND REPLACED AFT CA RGO SMOKE DETECTOR 1 IAW MM 26-16-01. SYSTEM OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 2002112100024 20021121 00024 2002 11 21 2002F01015 4 20021110 A 2565 GIRT BAR BOEING 757 75733N 1384931 NM ESCAPE SLIDE DIRTY G K NONE L NO TEST IN INSP/MAINT 1 GL 11 556TZ 32590 (ORIG-CLOSED) DURING SCHEDULED MAINTENANCE 1R SLIDE LIGHT INOP. MAINTENANCE TROUBLESHOT PER FIM 25-66-00, CHECKED GIRT B AR HORIZONTAL AND VERTICAL CLEARANCE DIMENSION PER MM 25-66-11, CHECKS OK. CLEANED AND LUBED GIRT BAR MECHANISM PER MM 1 2-21-18-3. ENGAGED AND DETACHED GIRT BAR NUMEROUS TIMES, 1R SLIDE LIGHT OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2002112100025 20021121 00025 NM 2002 11 21 2002F01016 1 20021112 A 2120 P199753 AIR FILTER BOEING 737 73783N 13844HI NM FWD CARGO BAY CONTAMINATED G O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 326TZ 32612 ORIGINAL CLOSED - STRONG FUMES (NO SMOKE) FIRST IN COCKPIT THEN AFT CABIN. STOPPPED SHORTLY AFTER BOTH RECIRC FANS TURNE D OFF. TS IAW FIM 21-00-00-810-804 FROM 804 (A) 2 THRU (D) 2. NO FUMES NOTED. R&R LT RECIRC FAN FILTER I/A/W AMM 21-25- 01-4 2 L 7 2 4F RT A16WE 2002112100026 20021121 00026 NM 2002 11 21 2002F01017 1 20021110 A 7500 312N53217 DUCT BOEING 757 75728A 1384976 NM RT ENGINE FAILED G O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 521AT 234 234 24368 (ORIG-CLOSED) FLIGHT NUMBER 790. DURING CRUISE EICAS STATUS MESSAGE "R STRUT OH DET 1" DISPLAYED. MAINTENANCE REMOVED AN D REPLACED HIGH PRESSURE DUCT, MESAGE ERASED AND REMAINED OFF ON ENGINE RUN. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2002112100027 20021121 00027 NE 2002 11 21 2002F01018 2 20021106 A 7200 ENGINE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE RIGHT VIBRATION G D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 GL 11 513AT 32449 31796 (ORIG-CLOSED) FLIGHT NUMBER 159. AFTER STARTING RIGHT ENGINE-VIBRATION HEARD AND FELT THROUGHOUT AIRCRAFT AT IDLE POWER. VIBERATION GOES AWAY WHEN POWER ADVANCED. MAINTENANCE PERFORMED TEST NR 10 HIGH/LOW IDLE CHECK PER MM 71-00-00, NO FAUL TS FOUND. PERFORMED TEST NR 6, ENGINE VIBRATION SURVEY PER MM 71-00-00/501, CHECK OK. PER MM 71-00-00-2 ENGINE WITH PHAS E 5 COMBUSTERS RUMBLE AT IDLE IN COLD WEATHER. OPERATION NORMAL PER MM 71-00-00-2. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002112100028 20021121 00028 NM 2002 11 21 2002F01019 1 20021105 A 2840 WARNING LIGHT BOEING 757 75723N 1384973 NM FUEL BOOST ILLUMINATED G O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 520AT 27976 (ORIG-OPEN) FLIGHT NUMBER 433. DURING CRUISE RIGHT CENTER BOOST PUMP LIGHT ILLUMINATED. EICAS MESSAGE CTR RT FUEL PUMP DISPLAYED. 2 L 7 2 4F RT A2NM 2002112100029 20021121 00029 2002 11 21 2002F01020 4 20021101 A 3413 4039893902 INDICATOR BOEING 757 75723N 1384973 NM VSI FLUCTUATES G O OTHER O OTHER CL CLIMB 1 GL 11 527AT 30886 (SUPP-CLOSED) FLIGHT NUMBER 279. DURING CLIMB AND CRUISE CAPTAINS VSI FLUCTUATES +- 500 FEET TO 1000 FEET. SWITCHED TO A LTN IRS AND FLUCTUATIONS STOPPED. MAINTENANCE REMOVED AND REPLACED VSI PER MM 34-22-06-4. OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2002112100030 20021121 00030 NM 2002 11 21 2002F00992 1 20021012 A 5330 PANEL LKHEED 1011 1011 N/A-SDR NM RAM AIR INLET GOUGED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 195AT 193C1041 NR 2 RAM AIR INLET UPPER AND LOWER WEB PANELS GOUGED. 2 L 7 3 4F RT A23WE 2002112100031 20021121 00031 NM 2002 11 21 2002F00993 1 20021029 A 2840 WARNING LIGHT BOEING 757 75733N 1384931 NM FUEL BOOST FALSE INDICATION G AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 551TZ 32585 (SUPP-CLOSED) FLIGHT NUMBER 593. DURING CRUISE RIGHT CENTER BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED. EICAS MESSAGE CTR R FUEL PUMP DISPLAYED. AT THE TIME THERE WAS 4100 LBS OF FUEL IN CENTER TANK. MAINTENANCE PERFORMED OPERATIONAL CHECK O F RIGHT CENTER FUEL PUMP IAW MM 28-22-03-4. OPERATIONAL CHECKS GOOD. NO DEFECTS NOTED. TROUBLESHOT PER FIM 28-22-00, FIG 105. 2 L 7 2 4F RT A2NM 2002112100032 20021121 00032 NM 2002 11 21 2002F00994 1 20020908 A 5310 SHEAR TIE LKHEED 1011 1011 N/A-SDR NM FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 195AT 193C1041 FESC SHEAR TIE CORRODED. REPAIRED SHEAR TIE IAW SRM 53-12-00, FIG. 805 BS 297, STRINGER 39 TO 40 LT. FROM LBL 46 TO LBL 53, LEVEL 2 CORROSION. 2 L 7 3 4F RT A23WE 2002112100033 20021121 00033 NE 2002 11 21 XNOA01072 2 20020924 A 7420 LEAD AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 2 ENG IGNITER FAILED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 371PC 157 UNABLE TO START NR 2 ENGINE WITH 'B' IGNITION. SWAPPED IGNITER LEADS IN ACCORDANCE WITH A300MM 74-11-00. OPS CHECK GO OD ON GROUND. 2 L 7 2 4F 4 F RT A35EU E23EA 2002112100034 20021121 00034 EU 2002 11 21 XNOA01073 1 20020926 A 4970 CONNECTOR AIRBUS 300 A300B4203 3930306 EU COCKPIT LOOSE A XN0A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 307FV 235 NR 1 ENGINE AND APU FAULT LITES CAME ON PRIOR TO T/O. (MANIFOLD FAULT LITES) RESET CONNECTOR ON 12 & 13 HF CONTROL BOX. "A" LOOP SYS OPS CHECK GOOD ON GROUND IAW A300MM 26-16-00. 2 L 7 2 4F RT A35EU 2002112100035 20021121 00035 NE 2002 11 21 XNOA01075 2 20020926 A 7420 CONNECTOR AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 2 ENGINE LOOSE A XN0A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 371PC 157 UNABLE TO START NR 2 ENGINE WITH "B" IGNITION. RESEATED CONNECTOR PLUG ON "B" IGNITION EXCITER BOX. OPS CHECK NORMAL I AW MM 74-11-01. 2 L 7 2 4F 4 F RT A35EU E23EA 2002112100036 20021121 00036 NE 2002 11 21 XNOA01076 2 20020929 A 7420 IGNITION LEAD AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 2 ENGINE LOOSE A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 371PC 157 NR 2 ENGINE B IGNITION INOPERATIVE. CLEANED & RESECURED B IGNITION LEAD. OPS CHECK GOOD ON GROUND RUN. 2 L 7 2 4F 4 F RT A35EU E23EA 2002112100037 20021121 00037 EA 2002 11 21 02324632 1 20021120 A 7110 2880500802 COWLING CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER LD LANDING 1 EA 27 632BR 7268 After landing, the crew reported that the R/H engine upper fan cowl had departed the aircraft during landing. Maintenan ce personnel inspected the R/H engine and surrounding area and found no further defects. The R/H engine upper fan cowl was replaced and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002112100038 20021121 00038 NM 2002 11 21 XNOA01077 1 20020928 A 2434 GENERATOR BOEING 727 727227 1384078 NM NR 2 ENGINE FAILED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 793A 20774 TAXI OUT IN BOS NR 2 GENERATOR 3 LIGHT TRIP WOULD NOT RESET. ON FAULT PANEL WENT FROM UNDER EXCITED TO UNDER VOLTAGE. ALL THREE GENERATORS ON LINE NR 2 GENERATOR HAD 0 KWS. NR 3 GENERATOR HAD 42 KWS. REMOVED & REPLACED GENERATOR ON NR 2 ENGINE IAW B727 MM 24-20-01. OPS CHECK GOOD AT THIS TIME IAW B727 MM 24-20-00. 2 L 7 3 4F A3WE 2002112100039 20021121 00039 EU 2002 11 21 XNOA01078 1 20021010 A 2710 CONTROLLER AIRBUS 300 A300B4203 3930306 EU AILERON CONTROL MALFUNCTIONED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 373PC 218 DURING FLIGHT CONTROL CHECK RT L/S AILERON WOULD NOT DEFLECT FULL RANGE. MANUALLY DISCONNECTED, THEN RECONNECTED LSA SY STEM. OPS CHECK NORMAL. NO DEFECT NOTED IAW A300 MM 27-10-00. 2 L 7 2 4F RT A35EU 2002112100040 20021121 00040 EU 2002 11 21 XNOA01079 1 20021010 A 3251 RELAY AIRBUS 300 A300B4203 3930306 EU NLG STEERING FAILED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 224KW 073 LOST STEERING DURING TAXI ACTION TAKEN: R & R NOSE STEERING GEAR RELAY AT POS NR 14GB PER A300 MM 20-46-50. SYS OPS CHE CK GOOD PER A300 MM 32-51-00. 2 L 7 2 4F RT A35EU 2002112100041 20021121 00041 EU 2002 11 21 XNOA01080 1 20021012 A 5610 TRACK AIRBUS 300 A300B4203 3930306 EU COCKPIT WINDOW DIRTY A XN0A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 13974 126 CAPT WINDOW WILL NOT LOCK. CLEANED DEBRIS FROM TRACK, WINDOW. OPS CHECKS GOOD IAW A300 MM CH 56-00-00. 2 L 7 2 4F RT A35EU 2002112100042 20021121 00042 2002 11 21 XNOA01081 4 20021015 A 3414 LINE AIRBUS 300 A300B4203 3930306 EU ADC CLOGGED A XN0A C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 23 473AS 203 NO AIRSPEED ON FO'S AIRSPEED INDICATOR ON TAKEOFF. ABORTED AT 90 KTS. ACTION TAKEN: FLUSHED NR 2 AIR DATA COMP. LINE. OP S CHECK GOOD IAW A300 MM 34-11-10. 2 L 7 2 4F RT A35EU 2002112100043 20021121 00043 NM 2002 11 21 XNOA01083 1 20021029 A 8012 WARNING LIGHT BOEING 727 727100 1384036 NM STARTER VALVE ILLUMINATED A XN0A O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 792AS CLIMBING OUT OF FL 140 NR 3 START VALVE LIGHT ILLUMINATED. PERFORMED QRH STARTER VALVE OPEN LIGHT ILLUMINATED CHECKLIST. TRANSFERRED TO DMI 2699 IAW ENA B727 MEL 80-1-1. CAT "C" PLACARDS INSTALLED. 2 L 7 3 4F RT A3WE 2002112100044 20021121 00044 EU 2002 11 21 XNOA01084 1 20021029 A 2710 AILERON AIRBUS 300 A300B4203 3930306 EU RT WING STUCK A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 372PC 196 AILERONS BECAME LOCKED OUT TO THE RT DURING FLT CONTROL CHECK. PERFORMED AUTO PILOT ROLL SERVO CHECK, AUTO PILOT ROLL ENGAGMENT & DISENGAGMENT TEST, "AILERON CONTROL WHEEL OPERATION STIFF", ALL SPEED AILERON SERVO CONTROL OPS CHECK, AIL ERON CABLE VISUAL & TENSION CHECK, AILERON MECH CONTROL SYS TEST WITH & WITHOUT DROOP INPUT, CABLE TENSION REGULATOR I NSPECTION CHECK, AILERON FUNCTION TEST OF EACH SERVO CONTROL USING SINGLE HYD. SYS, CYCLED ALL FLIGHT CONTROLS & BLEED GREEN SYSTEM OF AIR & REPLENISHED, ALL SPEED AILERON INSPECTION CHECK, LOW SPEED AILERON INSPECTION CHECK, LOW SPEED AILERON SERVO CONTROL INSPECTION CHECK, AND INTERCONNECTING SPRING ROD INSPECTION CHECK. ALL CHECKS WERE OK, NO DEFECTS 2 L 7 2 4F RT A35EU 2002112100045 20021121 00045 NM 2002 11 21 XNOA01085 1 20021030 A 3260 SWITCH BOEING 727 727227 1384078 NM RT MLG DOOR DIRTY A XN0A O OTHER N FALSE WARNING CL CLIMB 1 GL 23 793AS AFTER GEAR RETRACTION-GEAR DOOR LIGHT ILLUMINATED. RECYCLED GEAR ONCE. GEAR DOOR LT. EXTINGUISHED. CLEANED RT MAIN GEA R DOOR SWITCH. OPS CHECK GOOD IAW 727 MM CH 32-61-01. 2 L 7 3 4F A3WE 2002112100046 20021121 00046 EU 2002 11 21 XNOA01086 1 20021108 A 3260 PROXIMITY SENSOR AIRBUS 300 A300B4203 3930306 EU RT MLG MALFUNCTIONED A XN0A O OTHER N FALSE WARNING CL CLIMB 1 GL 23 473AS 203 UNABLE TO RETRACT LANDING GEAR WITH EITHER SYSTEM. REMOVED & REPLACED RT MLG BOAGIE TRIM PROXIMITY SENSORS 8GA IAW A300 MM 32-00-00. REMOVED & REPLACED LANDING GEAR EXTEND & RETRACT SWITCH IAW A300 MM 32-31-11. PERFORMED LANDING GEAR EXTEN SION & RETRACTION FOR SYS 1 & SYS 2. OPS CHECK GOOD IAW A300 MM 32-30-00. 2 L 7 2 4F RT A35EU 2002112100047 20021121 00047 NE 2002 11 21 XNOA01087 2 20021112 A 7261 CARBON SEAL BOEING 727 727173C 1384059 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE LEAKING A XN0A O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 704A 19504 NR 2 ENGINE OIL QUANTITY DECREASED IN FLT. REPLACED WORN CARBON SEAL IN ACCESSORY GEARBOX AT FUEL PUMP DRIVE. LEAK & OP S CHECKS GOOD IAW MM 73-11-1. 2 L 7 3 4F 4 F A3WE E2EA 2002112100048 20021121 00048 WP 2002 11 21 ZW0A0211301 1 20021113 A 2170 COALESCER BAG DOUG DC9 DC982 3022082 WP AIR DISTRIBUTION CONTAMINATED A ZW0A O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 13 903TW 49154 IRRITATING FUMES WERE OBSERVED IN THE CABIN. REPLACED BOTH WATER SEPARATOR ASSEMBLIES AND PERFORMED PACK BURN OUT. SUS PECT A PREVIOUS APU FUEL LEAK WHICH WAS CORRECTED BY REPLACEMENT OF A CRACKED BURNER CAN. CHECK-C 10-19-2002 MCI. --CLO SED-- 2 L 7 2 4F A6WE 2002112100049 20021121 00049 WP 2002 11 21 ZW0A0211401 1 20021115 A 3010 PRESSURE SWITCH DOUG DC9 DC982 3022082 WP AIRFOIL DEICE SY FAILED A ZW0A O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 13 953U 49267 STRONG BURNING ODOR IN COCKPIT WITH AIR FOIL ANTI ICE ON. ODOR CEASED WHEN AIRFOIL ANTI ICE TURNED OFF. ACCOMPLISHED H ANDBOOK PROCEDURE. MAINTENANCE REPLACED ANTICIPATOR, THERMOSTAT AND LOW PRESSURE SWITCH. CHECK-C 2-8-02 STL. --CLOSED- - 2 L 7 2 4F A6WE 2002112100050 20021121 00050 WP 2002 11 21 ZW0A021151 1 20021118 A 2910 B-NUT DOUG DC9 DC982 3022082 WP HYD SYSTEM LEAKING A ZW0A O OTHER K FLUID LOSS CR CRUISE 1 CE 13 954U 49426 HYDRAULIC FLUID LEAK FROM B-NUT ON LT ANTI-SKID CONTROL VALVE. TIGHTENED B-NUT AND RESERVICED HYDRAULIC SYSTEM. LAST CHE CK C PERFORMED 07/31/2002 IN STL -- CLOSED-- 2 L 7 2 4F A6WE 2002121800011 20021218 00011 EU 2002 12 18 UPS02139922 1 20021119 A 3610 6270985 SENSOR AIRBUS A300 A300F4622R 3930360 EU HP AIR INOPERATIVE A IPXA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 131UP 0816 LT HYD PUMP FAILED. NR 1 HIGH PRESS BLEED VALVE LIGHT ILLUMINATED. EMERGENCY DECLARED. *SUPPLEMENTAL* REACTIVATED SYSTEM PER DMP 36-11-03. REPLACED HP SENSOR 47HA PER AMM 36-11-23. BITE TESTED PER AMM 36-11-00, CHECKS GOOD. 2 L 7 2 4F RT A35EU 2002112100051 20021121 00051 NM 2002 11 21 UPS02239896 1 20021022 A 5741 69139017 PIN BOEING 727 72725C 138400H NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C & SI, RT WING REAR SPAR TO BODY FITTING TERMINAL BOTTLE PIN AT BS 870 HAS EVIDENCE OF PITTING CORROS ION. CORROSION OUT OF LIMITS, BOTTLE PIN REPLACED IAW MM 57-41-01. 2 L 7 3 4F A3WE 2002112100052 20021121 00052 NM 2002 11 21 UPS02239897 1 20021016 A 3211 FITTING BOEING 727 72725C 138400H NM RT MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C & SI, RT MAIN GEAR DOOR ACTUATOR SUPPORT FITTING LUG CRACKED. LUG REPLACED IAW EO B727-3210-2583 2 L 7 3 4F A3WE 2002112100053 20021121 00053 NM 2002 11 21 UPS02239898 1 20021021 A 5260 SKIN BOEING 727 72725C 138400H NM AFT AIRSTAIRS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C & SI, CORROSION ON OUTER SURFACE OF NR 6 RISER SKIN OF AFT AIR STAIRS CORROSION REMOVED IAW SRM 51-10-06, FOUND TO BE OUT OF LIMITS IAW SR M 52-00-2. REPAIRED IAW EO B727-5260-7551-A 2 L 7 3 4F A3WE 2002112100054 20021121 00054 NM 2002 11 21 UPS02239900 1 20021026 A 5310 BEAM BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C & SI, WHILE REMOVING RT BS 870 FITTING CRACK FOUND IN SIDE LOAD BEAM AT R BBL 54.50 REPAIRED IAW SMRO EO 2002-055-009. UPS ENGINEERING FILE NO. 727-53-2 0084 2 L 7 3 4F A3WE 2002112100055 20021121 00055 NM 2002 11 21 UPS02239904 1 20021023 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM AFT CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C & SI, AFT CARGO BAY, SEAT TRACK HAS LIGHT SURFACE CORROSION AT BS 1110 R/H SIDE CORROSION REMOV ED IAW SRM 51-10-06 AND FOUND TO BE OUTSIDE LIMITS IA W SRM 53-10-01 FIG 3. SEAT TRACK REPAIRED IAW SRM 53-10-01. 2 L 7 3 4F A3WE 2002112100056 20021121 00056 NM 2002 11 21 UPS02239908 1 20021024 A 5711 65319976 FRAME BOEING 727 72725C 138400H NM AFT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C &SI, APU EXHAUST, SUSPECT CORROSION ON AFT WING FRAME UNDER TADPOLE SEAL OF UPPER EXHAUST. FRAME CORRODED BEYOND LIMITS. NEW FRAME FABRICATED AND INSTALLED IAW DRAWING 65-31997. 2 L 7 3 4F A3WE 2002112100057 20021121 00057 NM 2002 11 21 UPS02239910 1 20021002 A 2760 BRACKET BOEING 727 72725C 138400H NM NR 12 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C & SI, NR 12 SPOILER SUPPORT CASTING I/B & O/B BRACKETS ARE CRACKED AT LWR ATTACH HOLES. BRACKET S REPLACED IAW DRAWING 65-17351 & SB 57-84 2 L 7 3 4F A3WE 2002112100058 20021121 00058 NM 2002 11 21 UPS02239912 1 20021017 A 5340 FITTING BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C & SI, CRACKS FOUND ON FWD OUTBOARD FLANGE OF LT BS 950 FITTING. REPAIRED CRACKS IAW SMRO EO'S 200 2-055-002 AND 2002-055-012. REF. UP S EO B727-5310-17901 AND UPS FILE NO. 727-53-20088. 2 L 7 3 4F A3WE 2002112100059 20021121 00059 NM 2002 11 21 UPS02439771 1 20021004 A 2897 WIRE HARNESS BOEING 747 747200 1384847 NM BOOST PUMP BURNED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 528UP 1 INSPECTION TYPE: C, FWD BOOST PUMP PRESS LIGHT ON , C/B CYCLES AND POPS PUMP C/B ON P14 PANEL; NR 1 & 3 BOOST PUMP PRE SS LIGHT ON. FWD CGO CEILING AT STA 920 RBL 5 WIRING BUNDLES W220 & W842 ADJACENT T O NR 4 FWD BOOST PUMP FOUND BURN ED WIRE AND POOR CONDITION. FABRICATED & REPLACED DAMAGED WIRES. 2 L 7 4 4F RT A20WE 2002112100060 20021121 00060 WP 2002 11 21 MWEA020718 1 20021121 A 5313 593607112 INTERCOSTAL DOUG DC9 DC981 3022081 WP STA 693 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 INTERCOSTAL BETWEEN LONGERON 30 AND 29 RIGHT AT STATION 693 TO 700 HAS CORROSION ON THE UPPER SURFACE. -- FABRICATED A ND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2002112100061 20021121 00061 NM 2002 11 21 C1HA200292031 1 20021119 A 3350 900835A BATTERY BOEING 727 727212 138407G NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 L-2 DOOR O/H INTERIOR EMERGENC LIGHT IS INOPREMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD 2 L 7 3 4F A3WE 2002112100062 20021121 00062 NM 2002 11 21 UPS02439891 1 20021107 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE: ASV AFT MOST CEILING EMERGENCY LIGHT INOP. REF LP915141. RELAMPED AFT MOST CEILING EMERGENCY LIGHT O PS CHECK GOOD THIS CLEARS M 248535. 2 L 7 4 4F A20WE 2002112100063 20021121 00063 NM 2002 11 21 UPS02439893 1 20021110 A 3350 LIGHT BOEING 747 747123F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE: ASV OVERHEAD EMERGENCY LIGHT OUT AT MAIN DECK STA 600 RT SIDE. RELAMPED, OPS CHECK GOOD. 2 L 7 4 4F A20WE 2002112100064 20021121 00064 NM 2002 11 21 UPS02439894 1 20021110 A 3350 LIGHT BOEING 747 747123F NM COCKPIT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:ASV OVERHEAD EMERGENCY LITE, OUTSIDE THE COCKPIT ARE DIM REMOVED AND REPLACED LITE ASY OPS CHKD GOOD . 2 L 7 4 4F A20WE 2002112100065 20021121 00065 NM 2002 11 21 UPS02439902 1 20021110 A 5414 SKIN BOEING 747 747200 1384847 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: ASV NR 3 PYLON INBD SIDE AFT AND BELOW "TEXAS" DOUBLER PREVIUOS REPAIR SHO WS EVIDENCE OF CRACK EXTENDI NG UPWARD FROM REPAIR.(MARKED). VERIFIED END OF CRACK WITH HFEC G. BUCHERT QC 10445. REMOVED DOUBLER . HS 86801 11 10 0 2. STOPDRILLED CRACK, H.S. 86801 11-10-02. VERIFIE D STOP DRILL G. BUCHERT QC 10445. INSTALLED A REPAIR DOUBLER AS PER S RM 54-34-03. 2 L 7 4 4F RT A20WE 2002112100066 20021121 00066 NM 2002 11 21 UPS02439914 1 20021116 A 3397 WIRE BOEING 747 747200 1384847 NM EMERGENCY LIGHT DAMAGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: PFLT, UPPER DECK PASSENGER AREA 3 EA CEILING EMERGENCY LIGHTS INOP. REF L/P 914473, M249145. REPAIRE D GROUND WIRE W894-L4734-20 PULLED FROM SOCKET CONTACT AT D5127P. TEST OK. THIS CLEARS M249145 2 L 7 4 4F RT A20WE 2002112100067 20021121 00067 NM 2002 11 21 2002F01021 1 20021017 A 3350 900835A BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 889MA 21854 DURING PREFLIGHT, FOUND CENTER EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY FOR EXT ERIOR OVERWING EXIT LIGHT. OPERATIONAL CHECKED OK IAW 33-50-22. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002112100068 20021121 00068 NM 2002 11 21 2002F01022 1 20021025 A 2923 AS19570C PUMP BOEING 727 727225 1384077 NM HYD SYSTEM MALFUNCTIONED A MYWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 803MA 22434 DURING ASCENT FROM MIA 30 MINUTES INTO FLIGHT NR 2 'B' SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. PERFORMED ABNOR MAL CHECKLIST, NO BREAKERS POPPED. AIRCRAFT RETURNED TO MIAMI. TROUBLESHOT HYDRAULIC SYSTEM. FOUND CURRENT DRAWS FROM RELAY ON PUMP NR 1 TO BE 16 AMPS NO LOAD, AND NR 2 PUMP 23 AMPS NO LOAD. WITH LOAD PUMP NR 1, 24 AMPS, PUMP NR 2, 34 A MPS. REMOVED AND REPLACED SYSTEM 'B' PUMP, NR 2 PUMP CIRCUIT BREAKER AND NR 2 PUMP RELAY. REMOVED AND REPLACED CASE DR AIN FILTERS TWO EACH. WORK PERFORMED IAW MM 29-00, 29-10-01, 29-12-11 AND 29-12-21. OPS CHECK AND LEAK NORMAL. AIRCRA FT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002112100069 20021121 00069 EU 2002 11 21 A6WA200260046 1 20021021 A 2160 4679C000 CONTROL VALVE BAC 146 146200A 1500266 EU A/C BAY MALFUNCTIONED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 179US 12608 E2041 DURING CLIMB, EXPERIENCED SLIGHT HAZE IN COCKPIT FOLLOWING SHUTDOWN OF NR 1 AND NR 2 PACKS, HAZE DISSIPATED. MAINTENANC E RAN BOTH PACKS, VERIFIED NR 1 PACK INOPERATIVE. REMOVED AND REPLACED PACK TEMP CONTROL VALVE. (M) 2 H 7 4 4F A49EU 2002112100070 20021121 00070 NM 2002 11 21 UPS02439915 1 20021116 A 3350 M335 BATTERY PACK BOEING 747 747200 1384847 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: PFLT, UPPER DECK CEILING EMERGENCY LIGHTS AT STA 590 AND STR 710 INOPERATIVE. R & R EMERGENCY LIG HT BATTERY PACK M335. OPS TEST NORMAL. 2 L 7 4 4F RT A20WE 2002112100071 20021121 00071 NM 2002 11 21 BJNA021017 1 20021020 A 5320 FLOOR SUPPORT BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 46628 23043 DURING SCHEDULED C-CHECK INSPECTION DISCOVERED, L1 DOOR AFT GIRTH BAR ATTACH FITTING AND OUTBOARD FLOORBOARD SUPPORT AT BS 346 LBL 60 CORRODED. FOUND GIRTH BAR FITTING AND FLOORBOARD SUPPORT CORRODED OUT OF LIMITS FORMED REPAIR FLOORBOARD SUPPORT AND GIRTH BAR FITTING. INSTALLED IAW B737 SRM 51-40-3, FIG 1, 51-30-2, 51-10-2, 51-10-7, 51-30-8 AND 51-10-1. (M) 2 L 7 2 4F RT A16WE 2002112100072 20021121 00072 NM 2002 11 21 BJNA021101 1 20021010 A 5753 SKIN BOEING 737 737282 13844AT NM T/E FLAP DELAMINATED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 23043 DURING SCHEDULED C-CHECK INSPECTION DISCOVERED RIGHT WING INBOARD AFT FLAP LOWER SKIN DELAMINATED AT T/E SECTION. CUT O UT DELAMINATED AREA .5 INCH BY 1 INCH. FABRICATED AND INSTALLED SKIN SECTION AND DOUBLER. BONDED AND APPLIED FIBERGLAS S REPAIR IAW B737 SRM 51-40-2 AND TIMCO REO-L00602 REV A. (M) 2 L 7 2 4F RT A16WE 2002112100073 20021121 00073 EA 2002 11 21 REXA02022 1 20021104 A 2613 356024310 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MALFUNCTIONED A REXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 25 8423C 7423 CRWE RECEIVED A LEFT 14TH STAGE BLEED DUCT EICAS MESSAGE IN FLIGHT. CREW FOLLOWED QRH, SHUTDOWN THE LEFT ENGINE, DECLAR ED EMERGENCY AND LANDED UNEVENTFULLY AT ALTERNATE AIRPORT. REMOVED AND REPLACED 14TH STAGE BLEED DETECTOR LOOP. (M) 2 L 7 2 4F RT A21EA 2002112100074 20021121 00074 SO 2002 11 21 SIMA20020325 1 20021020 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 145132 ABI - DURING AN IMBV INSPECTION, FOUND THE LEFT OMEGA BEAM AT FRAME 20 CORRODED BELOW SRM LIMITS. CUT OUT SECTION OF LE FT OMEGA BEAM. FABRICATED A FILLER, SHIMS, BACK PLATE AND EXTERNAL ANGLE. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 19 ) CHAPTER 53-21-10 FIG 201. (M) 2 L 7 2 4T RT T00011AT 2002112100075 20021121 00075 SO 2002 11 21 SIMA200230303 1 20021007 A 5315 14521721009 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL IN THE GALLEY AREA WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMO VED SECTION OF EXISTING DIGITAL. FABRICATED TWO REPAIR DOUBLERS AND SHIMS. REPAIR DONE IAW EMB145 SRM, SRM 145/1142 RE V 19, CHAPTER 53-21-10 PARA 4 FIG 203. (M) 2 L 7 2 4T RT T00011AT 2002112100076 20021121 00076 SO 2002 11 21 SIMA200230304 1 20021012 A 5320 CHANNEL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - DURING AN IMBV, THE GALLEY AREA RIGHT HAT BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. COMPLETELY REMOVED COR ROSION BY CUTOUT. FABRICATED A 'U' SHAPED DOUBLER. REPAIR DONE IAW EMB 145 GST-2990/02 AND STANDARD EMB SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002112100077 20021121 00077 SO 2002 11 21 SIMA200230305 1 20021014 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 145132 ABI - DURING IMBV INSPECTION, STRINGER 19L WAS FOUND TO BE CHAFED AT SKIN JUNCTION 05. BLENDED CHAFED AREA. PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145 /1142, CHAPTER 53, REV 19, 53-24-02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002112100078 20021121 00078 SO 2002 11 21 SIMA200230306 1 20021009 A 5313 STRINGER EMB 135 EMB135LR 3260305 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 736DT 145388 ABI - DURING AN MBV INSPECTION STRINGER 19R WAS FOUND TO BE CHAFED AFT OF FRAME 52. BLENDED CHAFED AREA AND PERFORMED E DDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED TWO DOUBLER ANGLES, FOUR SHIMS. REPAIR DONE IAW EMB GST-2966/ 02, AEAI ETN 53-020, EMB-145 SRM (145/1142, CHAPTER 53, REV 19, 53-24-02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002112100079 20021121 00079 SO 2002 11 21 SIMA200230308 1 20021009 A 5313 STRINGER EMB 135 EMB135LR 3260305 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 736DT 145388 ABI - DURING AN MBV INSPECTION, STRINGER 19L WAS FOUND TO BE CHAFED AFT OF FRAME 52. BLENDED CHAFED AREA. PERFORMED AN D EDDY CURRENT OF THE AREA WITH NO DEFECTS NOTED. FABRICATED TWO DOUBLERS AND FOUR SHIMS. REPAIR DONE IAW EMB 145 GST- 2966/02, AEAI ETN 53-020, EMB 145 SRM (145/1142, CHAPTER 53, REV 19, 53-24-02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002112100080 20021121 00080 SO 2002 11 21 SIMA200230310 1 20021007 A 5315 14521721009 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL IN THE GALLEY AREA WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMO VED SECTION OF EXISTING DIGITAL. FABRICATED TWO REPAIR DOUBLERS AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 R EV 19, CHAPTER 53-21-10 PARA 4 FIG 203. (M) 2 L 7 2 4T RT T00011AT 2002112100081 20021121 00081 SO 2002 11 21 SIMA200230311 1 20021012 A 5320 CHANNEL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - DURING AN IMBV INSPECTION, THE GALLEY AREA RIGHT HAT BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. COMPLETELY REMOVED CORROSION BY CUTOUT. FABRICATED A U-SHAPED DOUBLER. REPAIR DONE IAW EMB 145 GST-2990/02 AND STANDARD EMB SRM P RACTICES. (M) 2 L 7 2 4T RT T00011AT 2002112100082 20021121 00082 SO 2002 11 21 SIMA200230312 1 20021014 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 145132 ABI - DURING AN IMBV INSPECTION, STRINGER 19L WAS FOUND TO BE CHAFED AT SKIN JUNCTION 05. BLENDED CHAFED AREA. PERFORM ED AN EDDY CURRENT INSPECTION AND FOUND NO DEFECTS. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142, CHAPTER 53, REV 19) 53-24-02 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002112100083 20021121 00083 SO 2002 11 21 SIMA200230313 1 20021009 A 5313 STRINGER EMB 135 EMB135LR 3260305 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 736DT 145388 ABI - DURING AN MBV INSPECTION, STRINGER 19R WAS FOUND TO BE CHAFED AFT OF FRAME 52. BLENDED CHAFED AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA WITH NO DEFECTS NOTED. FABRICATED TWO DOUBLER ANGLES, FOUR SHIMS. REPAIR DONE IAW EMB GST-2966/02, AEAI ETN 53-020, EMB-145 SRM (145/1142, CHAPTER 53, REV 19) 53-24-02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002112100084 20021121 00084 SO 2002 11 21 SIMA200230315 1 20021017 A 5330 SKIN EMB 135 EMB135LR 3260305 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 145402 ABI - AIRCRAFT ARRIVED FOR A MAIN BASE VISIT AND PERMENANT REPAIR OF TDMI NR 7395300A4 TWO DENTS BETWEEN FRAME 67 AND 68 IN AFT SECTION UNDER CARGO AREA. PERFORMED A CUT OUT OF THE DAMAGE AREA. FABRICATED A FILLER AND REPAIR DOUBLER. REP AIR DONE IAW EMB SRM (EMB-145/1142 REV 19) CHAPTER 53-31-01. (M) 2 L 7 2 4F RT T00011AT 2002112100085 20021121 00085 SO 2002 11 21 SIMA200230319 1 20021017 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 145132 ABI - DURING A IMBV INSPECTION, THE GALLEY CENTER BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENT ER BEAM. INSTALLED NEW BEAM IAW AE ETN EM-53-028R1 AND EMB145 SRM (145/1142 REV 19) CHAPTER 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002112100086 20021121 00086 SO 2002 11 21 SIMA200230320 1 20021021 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 145132 ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FRAME 24 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT A SECTION OF THE CENTER OMEGA BEAM. FABRICATED A FILLER, SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW EMB 145 SRM (EMB SRM 145.1142 REV 19) CHAPTER 53-22-10 AND EMB 145 GST 3087/02. (M) 2 L 7 2 4T RT T00011AT 2002112100087 20021121 00087 SO 2002 11 21 SIMA200230321 1 20021022 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 7047 145132 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 24 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. CUT OUT A SECTION OF THE CENTER OMEGA BEAM. FABRICATED A FILLER, SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 19) CHAPTER 53-21-10 AND EMB 145 GST-3087/02. (M) 2 L 7 2 4T RT T00011AT 2002112100088 20021121 00088 SO 2002 11 21 SIMA200230322 1 20021017 A 5311 12010732001 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 145132 ABI - DURING AN IMBV INSPECTION FRAME 81, LOWER HALF WAS FOUND CHAFED BELOW SRM LIMITS. REMOVED DAMAGED FRAME SECTION. INSTALLED NEW FRAME IAW EMB 145 SRM (EMB SRM 145/1142 REV 19) CHAPTER 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002112100089 20021121 00089 SO 2002 11 21 SIMA200230323 1 20021015 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 145132 ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED 16.5 I NCHES BY 19.625 INCH SECTION OF THE FORWARD DIGITAL BY CUT OUT. FABRICATED A REPLACEMENT STRAP AND TWO DOUBLERS. REPAI R DONE IAW EMB-145, SRM 145/1142, CHAPTER 53 REV 19, 53-21-10 PARA 4, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002112100090 20021121 00090 SO 2002 11 21 SIMA200230324 1 20021018 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 145132 ABI - DURING AN IMBV INSPECTION, GALLEY RIGHT BEAM, WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED DAMAGED BEAM AND INSTA LLED NEW BEAM IAW EMB 145 SRM (EMB 145/1142 REV 19) CHAPTER 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002112100091 20021121 00091 SO 2002 11 21 SIMA200230326 1 20021020 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 145132 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS IN THREE AREAS. BLENDED THE THREE DAMAGED AREAS, CLEANED AND TREATED. FABRICATED THREE REINFORCEMENT DOUBLERS. REPAIR DONE IAW AE ETN EM-53-036, FIG 5. (M) 2 L 7 2 4T RT T00011AT 2002112100092 20021121 00092 SO 2002 11 21 SIMA200230327 1 20021016 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 145132 ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR OPENING LOWER CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING SILL. INSTALLED NEW SILL IAW EMB 145 SRM 9145/1142 REV 19) CHAPTER 51-20-01 AND STANDARD SRM PROCEDURE. (M) 2 L 7 2 4T RT T00011AT 2002112100093 20021121 00093 EU 2002 11 21 SIMA200230343 1 20021029 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 247AE 340B247 CREW REPORTED ALL EMERGENCY FLOOR AND EXIT LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLIES AT 20LN AND 21LN. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002112100094 20021121 00094 NM 2002 11 21 UIEA200200053 1 20021012 A 4930 360387921 METERING VALVE BOEING 747 747243B 1384830 NM APU LEAKING A UIEA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 517MC 23300 STRONG SMELL OF FUEL AFTER SUPPLYING A/C PACK WITH AIR FROM THE APU. SUSPECT FUEL LEAK. FOUND FUEL DROP FROM THE FORWA RD FUSELAGE DRAIN. APU RENDERED INOPERATIVE. REMOVED AND REPLACED FUEL METERING VALVE PER MM 49-31-07. OPS AND LEAK C HECK OK. (M) 2 L 7 4 4F A20WE 2002112100095 20021121 00095 GL 2002 11 21 UIEA200200054 2 20021013 A 7200 ENGINE BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL NR 4 FAILED A UIEA F E J A ACTIVATE FIRE EXT. ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING K J S FLUID LOSS WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 EA 15 497MC 29258 TPE/ANC - AIR TURN BACK, ENGINE NR 4 CATASTROPHIC FAILURE. ENGINE FAILED TO 1625Z. BOTH FIRE BOTTLES FIRE ON ENGINE NR 4. ENGINE DECLARED UNSERVICEABLE DUE TO DAMAGE OF LPT BLADES. PYLON WIRE BUNDLE W5312 ALSO FOUND WITH DAMAGED INSULAT ION. FOUND BOTH T/R HALVES WITH HEAT DAMAGE TO INSULATION MATERIAL. REMOVED AND REPLACED NR 4 ENGINE. NR 4 ENGINE LEF T AND RIGHT THRUST REVERSERS REPLACED IAW MM 78-31-01. WIRE BUNDLE W5312 REPLACED IAW WDM 36-21-21. REPLACED BOTH FIRE BOTTLES IAW MM 26-21-00. (M) 2 L 7 4 4F 4 F RT 1384945 E23EA 2002112100096 20021121 00096 NM 2002 11 21 UIEA200200055 1 20021020 A 7110 65B942507 HINGE FITTING BOEING 747 7472D7B 1384803 NM LT COWLING WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 DURING CURRENT C-CHECK AT SIAEC, FOUND NR 3 ENGINE LEFT AFT FAN COWL HINGE SUPPORT FITTING WITH WEAR DAMAGE IN THE LUG B ORE HOLE. REAMED LUG BORE HOLE OVERSIZED TO .610 INCH. PERFORMED MAGNETIC PARTICLE INSPECTION FOR CRACKING. NO CRACKS FOUND. FABRICATED INTERFERENCES BUSHING. INSTALLED BUSHING PER STANDARD SHRINK FIT METHOD IAW BOEING STANDARD OVERHAU L PRACTICES 71-11-21 REV 2. (M) 2 L 7 4 4F RT A20WE 2002112100097 20021121 00097 NM 2002 11 21 UIEA200200056 1 20021024 A 5313 BAC1498145 STRINGER BOEING 747 7472F6B 1384807 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 535MC 81995 21833 DURING CURRENT C-CHECK FOUND BS 2179 STRINGER 45L CORRODED ON OUTBOARD FLANGE. CUT AWAY CORRODED AREA. MANUFACTURED RE PAIR FILLER, SHIMS AND REPAIR DOUBLERS SIMILAR TO SRM 53-10-03 FIG 1. (M) 2 L 7 4 4F A20WE 2002112100098 20021121 00098 NM 2002 11 21 UIEA200200058 1 20021024 A 5311 5B0433941 FRAME BOEING 747 7472F6B 1384807 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 535MC 21833 DURING CURRENT C-CHECK, FOUND CRACKS EMANATING FROM THE LOWER OUTBOARD CORNER OF THE FRAME ACCESS HOLE CUTOUT AT BS 2040 , 2080, 2100, 2120, 2160 AT LBL 16 WL 137. EACH FRAME CRACKED AT THE SAME LOCATION. CRACKS STOP DRILLED OR CUT AWAY AS REQUIRED. REPAIR DOUBLERS, FILLERS AND OR TAPERED SHIMS FABRICATED IAW SRM 53-10-04 FIG 43. REPAIR DOUBLERS LENGTHENE D AS NECESSARY. INSTALLED RELATED REPAIR PARTS PER STANDARD SRM PRACTICES. (M) 2 L 7 4 4F A20WE 2002112100099 20021121 00099 NM 2002 11 21 UIEA200200060 1 20021025 A 5320 PANEL BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 808MC 85585 21048 DURING CURRENT C-CHECK, AT HKG FOUND REVEAL PANEL CRACKED AT NR 2 MED STATION 800 BETWEEN STRINGER 17L AND 18L. CRACK L ENGTH IS APPROX .5 INCH LONG TERMINATING IN A COMMON FASTENER HOLE. PERFORMED E/C INSPECTION TO ENSURE NO CRACK PROPAGA TION FROM HOLE. OVERSIZED HOLE .0625 INCH AND INSTALLED FASTENER COMMON TO THE CRACK END PER STANDARD SRM PROCEDURES. (M) 2 L 7 4 4F A20WE 2002112100100 20021121 00100 NM 2002 11 21 USAA020398 1 20021010 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 57344 22199 CLT - FOUND CHORD WITH MULTIPLE CRACKS, MAXIMUM WIDTH .125 INCH, UPPER CHORD OF INTERCOSTAL AT BL 0, BS 1420-1440. FABR ICATED AND INSTALLED NEW ANGLE AND SHIM PER SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 2002112100101 20021121 00101 NM 2002 11 21 USAA020399 1 20021015 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 57344 22199 CLT - FOUND INTERCOSTAL WITH 2 INCH CRACK, STATION 440 BL 0 BELOW FLOOR LEVEL. FABRICATED AND INSTALLED NEW WEB SECTION PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2002112100102 20021121 00102 NM 2002 11 21 USAA020400 1 20021015 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 57344 22199 CLT - FOUND INTERCOSTAL CRACKED 10 INCHES, BL 0 BETWEEN STATION 440 AND 460 FLOOR LEVEL. FABRICATED AND INSTALLED NEW I NTERCOSTAL PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2002112100103 20021121 00103 NM 2002 11 21 USAA020401 1 20021017 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 57344 22199 CLT - FOUND INTERCOSTAL CRACKED 1 INCH, STATION 480 LBL 40 6 INCHES BELOW FLOOR LEVEL. REPAIR ANGLE INSTALLED PER SRM 5 1-70-11. (M) 2 L 7 2 4F RT A2NM 2002112100104 20021121 00104 NM 2002 11 21 UPS02439917 1 20021118 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE:PFLT EMERGENCY LIGHTS OVER RT UPPER DECK DOOR INOP ON PREFLIGHT. SECURED BULBS & TEST OK. 2 L 7 4 4F A20WE 2002112100105 20021121 00105 NM 2002 11 21 USAABB02123 1 20020725 A 3230 161N50211 SPRING BOEING 757 757225 1384959 NM RT MLG BROKEN A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 618AU 22210 PHL - FLT 25 - ON APPROACH TO PHL, WHEN THE GEAR WAS EXTENDED, THE CREW RECEIVED THE EICAS MESSAGE 'GEAR DISAGREE' AND T HE GEAR AMBER LIGHT ILLUMINATED. CREW RECYCLED THE GEAR. ALL INDICATIONS WERE NORMAL AND THE FLIGHT LANDED WITHOUT FUR THER INCIDENT. MAINTENANCE REPLACED A BROKEN UPLOCK ACTUATOR SPRING. (M) 2 L 7 2 4F RT A2NM 2002112100106 20021121 00106 NM 2002 11 21 USAABB02178 1 20021021 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 MCO - FOUND THE EMERGENCY LIGHT AT ROW 14 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AT ROW 14. OPERATIONAL CHECK G OOD. (M) 2 L 7 2 4F RT A2NM 2002112100107 20021121 00107 NM 2002 11 21 USAABB02187 1 20021101 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 621AU 27200 LAX - FOUND LOW LEVEL EMERGENCY LIGHT AT ROW 10 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002112100108 20021121 00108 WP 2002 11 21 WXOA02008 1 20021102 A 3244 95502676 TIRE DOUG DC9 DC987 3022087 WP NLG VIBRATES A WXOA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 WP 17 948MA 49778 LGB - NOSE GEAR VIBRATION REPORTED ON TAKEOFF ROLL AT APPROXIMATELY 30 KNOTS. CREW ABORTED TAKEOFF WITHOUT INCIDENT. M AINTENANCE INSPECTED NOSE GEAR ASSEMBLY AND REPLACED LEFT NOSE TIRE AND WHEEL ASSEMBLY. ACCOMPLISHED HIGH SPEED TAXI CH ECK. NO EVIDENCE OF NOSE GEAR VIBRATION NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 2002112100109 20021121 00109 WP 2002 11 21 WXOA02009 1 20021102 A 3610 5910244363 DUCT DOUG DC9 DC921 302205A WP A/C BAY RUPTURED A WXOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 17 127NK 47361 LAS - TAIL COMPARTMENT HIGH TEMP ANNUNCIATOR INDICATION ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INC IDENT. MAINTENANCE INSPECTED TAIL COMPARTMENT AND ASSOCIATED PRESSURIZATION DISTRIBUTION SYSTEM FOR CAUSE OF HIGH TEMP INDICATION. MAINTENANCE DISCOVERED BLEED AIR LEAK FROM AN UNKNOWN SOURCE IN THE RIGHT AIR CONDITIONING SYSTEM. MAINTEN ANCE DEFERRED THE RIGHT AIR CONDITIONING SYSTEM. TAIL COMPARTMENT HIGH TEMP ANNUNCIATOR DOES NOT ILLUMINATE FOLLOWING D EFERRAL OF RIGHT AIR CONDITIONING SYSTEM. AIRCRAFT RETURNED TO SERVICE. DURING SUBSEQUENT TROUBLESHOOTING OF DEFERRAL, MAINTENANCE FOUND RUPTURED BLEED AIR SUPPLY DUCT, IN THE RIGHT AIR CONDITIONING SYSTEM. (M) 2 L 7 2 4F A6WE 2002112100110 20021121 00110 NM 2002 11 21 02FDEA00728 1 20021011 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 272FE 22037 DENT ON SKIN AT BS 465 BELOW STR 16R. R&R SKIN PER SRM 53-30-1, 53-30-3. 2 L 7 3 4F RT A3WE 2002112100111 20021121 00111 NM 2002 11 21 02FDEA00729 1 20021012 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 272FE 22037 FRAME DENTED AT BS 500, STR 23R - 24R. R&R FRAME PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2002112100112 20021121 00112 NM 2002 11 21 02FDEA00730 1 20021007 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 272FE 22037 BULGING ON BELLY SKIN BETWEEN BS 1050 TO 1060, LBL 20. R&R SKIN PER SRM 53-30-1, 53-10-1, 53-30-3. 2 L 7 3 4F RT A3WE 2002112100113 20021121 00113 NM 2002 11 21 02FDEA00731 1 20021007 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 CORROSION ON UPR CHORD FLOORBEAM AT BS 344, LBL 3, WL 208. 2 L 7 3 4F RT A3WE 2002112100114 20021121 00114 NM 2002 11 21 02FDEA00732 1 20021007 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 CORROSION ON BS 720E FRAME FWD SIDE STR 7L. R&R FRAME PER SRM 53-10-01 & EA 7-5310-67028 & SRM 53-10-14 FIG 1. 2 L 7 3 4F RT A3WE 2002112100115 20021121 00115 NM 2002 11 21 02FDEA00733 1 20021007 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 SKIN CHAFED AT BS 720D+12 AT STR 19L. R&R SKIN PER SRM 53-30-3 FIG 14. 2 L 7 3 4F RT A3WE 2002112100116 20021121 00116 NM 2002 11 21 02FDEA00734 1 20021007 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 SKIN CHAFED AT BS 720D+12 AT STR 19R. R&R SKIN PER SRM 53-30-03. 2 L 7 3 4F RT A3WE 2002112100117 20021121 00117 NM 2002 11 21 02FDEA00737 1 20021014 A 2410 CSD BOEING 727 727200 138407E NM NR 2 FAULTY A FDEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 25 201FE 22924 LEVEL AT FL 310 IN SMOOTH CONDITIONS, EXPERIENCED A THREE LIGHT TRIP. RAN QRH PROCEDURES, UNABLE TO RECOVER BTB, G/B OR FIELD. FREQS/VOLTS ON NR 2 GEN WERE ZERO (OFF SCALE LEFT). NO LIGHTS ON ELEC FAULT PANEL ILLUMINATED. NR 2 CSD WAS D ISCONNECTED. AIR TURNBACK. UNABLE TO POWER NR 2 AC BUS. REMOVED AND REPLACED NR 2 CSD IAW 727-200 M/M 24-10-011-4 AND REMOVED AND REPLACED NR 2 GEN IAW 24-20-001-4 OP AND LEAK CHECKED GOOD. 2 L 7 3 4F RT A3WE 2002112100118 20021121 00118 EU 2002 11 21 02FDEA00738 1 20021015 A 5415 A57050000200161 FITTING AIRBUS 310 A310 EU PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 R/SING PYLON FWD THRUST AND SIDE LOAD FITTING AREA, FOUND BEARING AREAS WITH BROWNISH STAINS AT TOP & BOTTOM OF FITTING. R&R FITTING PER EA 6-5450-66461. 2 L 7 2 4F RT A35EU 2002112100119 20021121 00119 EU 2002 11 21 02FDEA00739 1 20021015 A 5415 A5714126620000 FITTING AIRBUS 310 A310 EU LT PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 SIGNS OF CORROSION AT L/PYLON THRUST & SIDE LOAD FITTING SLEEVE. R&R FITTING PER EA 6-5450-66458. 2 L 7 2 4F RT A35EU 2002112100120 20021121 00120 EU 2002 11 21 02FDEA00740 1 20021014 A 5415 A5461175400300 FITTING AIRBUS 310 A310 EU RT PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 RT WING PYLON AFT MOUNT FITTING ATTACHMENTS CORRODED. R&R FITTING PER EA 6-5450-66459. 2 L 7 2 4F RT A35EU 2002112100121 20021121 00121 EU 2002 11 21 02FDEA00741 1 20021015 A 5415 A5461178700060Z FITTING AIRBUS 310 A310 EU LT PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 LT PYLON AFT THRUST AND SIDE LOAD FITTING CORRODED AT BEARING FACE. R&R FITTING PER EA 6-5450-66460. 2 L 7 2 4F RT A35EU 2002112100122 20021121 00122 EU 2002 11 21 02FDEA00742 1 20021015 A 5730 SKIN AIRBUS 310 A310 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 LT WING T/E SKIN CRACKED AT 581AB ACCESS CUTOUT AT RIB 11. R&R SKIN PER EA 6-5710-65463. 2 L 7 2 4F RT A35EU 2002112100123 20021121 00123 NM 2002 11 21 02FDEA00743 1 20021012 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 HORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 35 AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415. 2 L 7 3 4F RT A22WE 2002112100124 20021121 00124 NM 2002 11 21 02FDEA00744 1 20021016 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 478FE 21395 CORROSION ON STR 28L, BS 640-660. R&R STRINGER PER SRM 53-10-1, 53-10-3, 53-30-3. 2 L 7 3 4F RT A3WE 2002112100125 20021121 00125 NM 2002 11 21 02FDEA00745 1 20021016 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 478FE 21395 CORROSION ON FLOORBEAM AT BS 620, RBL 10, WL 208. R&R FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 2002112100126 20021121 00126 NM 2002 11 21 02FDEA00746 1 20021018 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 HORIZ STAB INTERIOR , FOUND BARREL 27TH NUT HOLE AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415. 2 L 7 3 4F RT A22WE 2002112100127 20021121 00127 NM 2002 11 21 02FDEA00747 1 20021008 A 5315 BAC150529222 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 272FE 22037 CORROSION ON TOP OF FLOORBEAM AT BS 344, LBL 45-55, WL 208. R&R UPPER CHORD PER ER 02-1505. 2 L 7 3 4F RT A3WE 2002112100128 20021121 00128 NM 2002 11 21 02FDEA00748 1 20021018 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 HORIZ STAB INTERIOR, NR 16 RT BARREL NUT HOLE CORRODED. R&R HORIZ STABILIZER PER EA 1-5510-66415. 2 L 7 3 4F RT A22WE 2002112100129 20021121 00129 NM 2002 11 21 02FDEA00749 1 20021019 A 2613 WARNING SYSTEM BOEING 727 727200 138407E NM COCKPIT MALFUNCTIONED A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 285FE 22622 AT FL 310 LOWER AFT BODY OVERHEAT LIGHT STARTED TO BLINK THEN STAYED ON UNTIL RED TAB WAS COMPLIED WITH, UPON CLOSING NR 3 BLEED, LIGHT WENT OUT. CONTINUED FLT. USING NR 2 BLEED SUPPLYING RIGHT PACK WITH NO FURTHER OVERHEAT INDICATION. I NSPECTED AFT AIRSTAIR AREA DUCTS FOR SECURITY TOOK A/C OUT TO RUN-UP AREA RAN TO 1.80 EPR PERFORMED LEAK CHECK OF BLEED DUCTS NO LEAKS NOTED RAN AT POWER. NO FAULTS OCCURRED CHECKED HISTORY AND NO HISTORY IN LAST 90 DAYS FOUND SYSTEM TO BE OPERATING NORMAL OK FOR FLIGHT. 2 L 7 3 4F RT A3WE 2002112100130 20021121 00130 NM 2002 11 21 02FDEA00750 1 20021018 A 5712 ARB2850506 RIB DOUG MD11 MD11 3023602 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING FIXED L/E STRUCTURAL RIB CRACKED AT I/B OF SLAT TRACK NR 16. 2 L 7 3 4F RT A22WE 2002112100131 20021121 00131 NM 2002 11 21 02FDEA00751 1 20021018 A 5753 ARB0029509N SUPPORT FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING O/B FLAP I/B HINGE SUPPORT FITTING CRACKED. R&R SUPPORT FITTING PER MM 57-53-01-4. 2 L 7 3 4F RT A22WE 2002112100132 20021121 00132 NM 2002 11 21 02FDEA00752 1 20021015 A 3234 CONTROL VALVE DOUG MD11 MD11 3023602 NM MLG FAULTY A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 586FE 48487 LEFT MAIN LANDING GEAR UNSAFE ON DEPARTURE. ATTEMPTED PROCEDURES IAW QRH FOR "GEAR PRIMARY OR SECONDARY LIGHTS ILLUMINA TED WITH GEAR HANDLE UP" BOTH LIGHTS REMAINED ON . DUMPED 96K FUEL ON RTB LANDING AND ROLLOUT UNEVENTFUL. R&R MLG CONT ROL VALVE PER MM 32-31-20-4 OPS LEAK/CHKS GOOD. ADJUSTED MLG GEARWELL DOOR PUSHRODS PER MM 32-31-00-5. DOORS OPS CHECK S GOOD. PERFORMED LANDING GEAR SWING. ALL INDICATIONS /FUNCTIONS NORMAL. A/C OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2002112100133 20021121 00133 NM 2002 11 21 02FDEA00753 1 20021018 A 3241 CONDUIT DOUG MD11 MD11 3023602 NM LT MLG OUT OF POSITION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 586FE 48487 ON CLIMBOUT FROM ANC "RED UNSAFE" INDICATION ON PRIMARY INDICATING SYSTEM AND "CONFIGURATION PAGE" AS WELL FOR LEFT MAIN GEAR UNSAFE ON RETRACTION. FOUND FWD ANTI SKID CONDUIT LOOSELY ROUTED THROUGH THE FWD HOSE AND CONDUIT GUIDE ASSY SUSP ECT UNDER AIR LOAD ANTI SKID CONDUIT WAS STRIKING THE UPLOCK TARGET BRINGING IT OUT OF SENSOR RANGE, REROUTED ANTI SKID CONDUIT AND BRAKE LINES SO THERE WAS CORRECT ROUTING REF MM 32-11-40-4. CHECKED ALL PROXIMITY SENSORS FOR OPERATION AND RIG REF MM 32-61-15-4. ALSO CHANGED WORN PARTS IN MAIN LANDING GEAR LATCH REF IPC 32-34-05-01 ITEMS 80,85,90,95, AND 1 00. 2 L 7 3 4F RT A22WE 2002112100134 20021121 00134 WP 2002 11 21 02FDEA00754 1 20021022 A 2781 WARNING SYSTEM DOUG DC10 DC1030 3023501 WP COCKPIT MALFUNCTIONED A FDEA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 309FE 9885 5766 48298 AFTER T/O ON FLAP & SLAT RETRACTION HAD SLAT DISAGREE LIGHT ILLUMINATE. FOLLOWED RED TAB TO SLAT EXTEND LIGHT EXT. RET URN TO AIRPORT. DUMPED FUEL. INSPECTED ALL 6 SENSORS & TARGETS. PERFORMED BITE TEST ON SENSOR AT PROX BOX. ALL TESTS GOOD. DID SHAKE TEST ON ALL SLATS AT SENSORS, NO DISAGREE LIGHT SHOWING. CYCLED SLATS MANY TIMES & COULD NOT REPRODUC E MALFUNCTION. R&R PROX SWITCH CONTROL BOX FOR PRECAUTION & REPEATED ALL ABOVE TESTS. ALL CHECK NORMAL. NO HISTORY SHO WN. ALL MX DONE IAW MM 27-80-01-6 2 AND 27-84-01-2. 2 L 7 3 4F A22WE 2002112100135 20021121 00135 NM 2002 11 21 PCAA0211135 1 20021119 A 3230 NAS302370870 CABLE DHAV DHC8 DHC8102 2809003 NM NOSE GEARWELL KINKED A PCAA O OTHER O OTHER NR NOT REPORTED 1 EA 13 817EX 191 SCE FLIGHT#3816. CREW REPORTED NOSE GEAR WOULD NOT EXTEND DOWN, ALTERNATE EXTENSION PERFORMED AND NOSE GEAR WOULD STILL NOT EXTEND. GEAR PUMPED DOWN, 3 GREEN LIGHTS ILLUMINATED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED DRAG BRACE PROXIMITY SWITCH AND ALTERNATE EXTENSION CABLE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002112100136 20021121 00136 NM 2002 11 21 02FDEA00760 1 20021021 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 EXTERNAL SKIN DENTED WITH TWO GOUGES AT BS 365, ABOVE STR 17L. 2 L 7 3 4F RT A3WE 2002112100137 20021121 00137 NM 2002 11 21 02FDEA00761 1 20021021 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 FRAME DENTED AT STR 950F, LBL 30, STR 26L. REPAIRED FRAME IAW SRM 51-40-3 FIG 1 SHEET 3 & EA 7-5310-67056. 2 L 7 3 4F RT A3WE 2002112100138 20021121 00138 NM 2002 11 21 02FDEA00762 1 20021021 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 FRAME IS DENTED AT BS 990, LBL 30, WL 146. R&R FRAME PER SRM 53-10-1. 2 L 7 3 4F RT A3WE 2002112100139 20021121 00139 NM 2002 11 21 02FDEA00763 1 20021021 A 5320 WEB BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 CORROSION ON WEB AT BS 1166, LBL 10, WL 140. R&R WEB PER SRM 53-10-1, 51-30-2, 51-20-1. 2 L 7 3 4F RT A3WE 2002112100140 20021121 00140 NM 2002 11 21 02FDEA00764 1 20021021 A 5320 WEB BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 CORROSION ON WEB AT BS 1166, RBL 10, WL 140. R&R WEB PER SRM 53-10-1, 51-30-2, 51-20-1. 2 L 7 3 4F RT A3WE 2002112100141 20021121 00141 NM 2002 11 21 02FDEA00766 1 20021025 A 5345 WSP0668501 ATTACH FITTING DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 INBD AFT TOILET MOUNTING ATTACHMENT CORRODED AT BS 421. R&R SUPPORT PER SRM 51-33-01, VOL II. 2 L 7 3 4F RT A22WE 2002112100142 20021121 00142 NM 2002 11 21 02FDEA00767 1 20021025 A 5347 ABA7680505 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 FWD CABIN LT SEAT TRACK AT BS 470 FOUND CORRODED. R&R SEAT TRACK PER SRM 53-70-00. 2 L 7 3 4F RT A22WE 2002112100143 20021121 00143 NM 2002 11 21 02FDEA00769 1 20020906 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 CORROSION ON HORIZONTAL STABILIZER. R&R HORIZONTAL STABILIZER PER ME 11-55-023. 2 L 7 3 4F RT A22WE 2002112100144 20021121 00144 EU 2002 11 21 MALA020660 1 20021119 A 3350 6122751 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 517XJ E2335 DURING WALK AROUND INSPECTION, RT FWD VESTIBULE EMERGENCY LIGHTS DO NOT TEST ALONG WITH TWO FLOOR LIGHTS. MAINTENANCE I NSTALLED NEW EMERGENCY BATTERY PACK IN LF22 POSITION PN 61-2275-1 SN/ON 9805516, SN/OFF 9911203 PER JC 0494 OPS CHECK GO OD. 2 H 7 4 4F RT A49EU 2002112100145 20021121 00145 NM 2002 11 21 UPS02439916 1 20021116 A 3350 LIGHT BOEING 747 747259B 1384804 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:PFLT 1 EMERGENCY LT INOP UPPER DECK JUST FWD OF JUMPSEATS ON CEILING. RELAMPED. OPS CK OK. 2 L 7 4 4F RT A20WE 2002112100146 20021121 00146 NM 2002 11 21 UPS02439918 1 20021115 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE:PFLT UPPER DECK EMERGENCY EXIT DOOR HAS 1 LIGHT INOP. REMOVED PANEL, RELAMPED UPPER DECK CREW SERVICE D OOR AFT EMERGENCY LIGHT & INSTALLED & SECURED PANEL. 2 L 7 4 4F A20WE 2002112100147 20021121 00147 NM 2002 11 21 UPS02539920 1 20021114 A 5753 FLAP BOEING 757 75724APF 1384969 NM LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:ASV FOUND LEFT INBOARD TRAILING EDGE FLAP DAMAGED AND LEFT INBOARD FLAP BEAM ASS BELLCRANK BROKEN. R&R LEFT INBOARD TRAILING EDGE AFT FLAP PER MM 27-51-12. R&R LT MAIN INBD BELLCRANK BEAM. 2 L 7 2 4F RT A2NM 2002112100149 20021121 00149 WP 2002 11 21 UPS02839641 1 20021008 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:N/A RIVETS POPPED DUE TO CORROSION BETWEEN STA 120 & 130 LONGERON 31R 2 LAP SEAM. REMOVED CORRODED SECT ION OF FINGER DOUBLER & SKIN. VERIFIED CORROSION REMOVED ACCOMPLISHED REPAIR PER SRM 53-2-1 2 L 7 4 4F RT 4A25 2002112100150 20021121 00150 WP 2002 11 21 UPS02839651 1 20020919 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 LEFT MID GALLEY SERVICE DOOR LOWER FWD CORNER OF JAMB HAS A CRACK FOUND WITH HFEC. REPAIRED DOOR COR NER IAW DC8 SRM T/R 53-2-0 FIG 15A. 2 L 7 4 4F RT 4A25 2002112100151 20021121 00151 WP 2002 11 21 UPS02839652 1 20020919 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 REPAIR DOUBLER 744-3L-03 STA 1715 TO 1720 AND LONG 17L IS CAT B DUE TO PROXIMITY 18 IN TO REPAIR 744- 3L-04 AND NO CUTOUT STOP DRILLED ONLY UPPER CRITICAL ROW HIDDEN SKIN. REPAIRED AREA IAW DC8 SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2002112100152 20021121 00152 WP 2002 11 21 UPS02839840 1 20021021 A 5320 3755822505N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 STA 320 BETWEEN LONG 33L TO 34L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITT ING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002112200001 20021122 00001 SO 2002 11 22 C2XA02SH130 1 20021122 A 5300 14522460005 STRAP EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16919 145393 SHV- DURING C CHECK BUTT STRAP BETWEEN FRAMES 15 AND 16 CENTERLINE WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAM AGE AND PEFORMED A SPLICE REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002112200002 20021122 00002 NM 2002 11 22 UPS02539824 1 20021030 A 7100 ENGINE BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE RIGHT OVERTEMP A IPXA F A ACTIVATE FIRE EXT. UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 25324 RT ENGINE TEMP CLIMBED TO 944 +. ENGINE WAS SHUT DOWN AND ONE FIRE BOTTLE WAS BLOWN. T/S PER FIM 71-05-00 FIG 110- R EPLACED W-31 EGT HARNESS - PERFORMED EGT CABLE & THERMOCOUPLE TEST, CHECKED OK PER MM77-21-03-5.SEI 6 LOW COMPARED TO EI CAS. W31 HARNESS. ENGINE RUN CHECKED OK. NR 1 FIRE BOTTLE REPLACED, ITEM 3 THIS L/P. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112200003 20021122 00003 WP 2002 11 22 UPS02839621 1 20021007 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 LT WING DOUBLER SKIN CRACKED, FERRIED TO VENDOR AQUAMISED, NR 2 MAIN TANK 5788, INSTALLED DOUBLER & TRIPLER PER EO DC8 -2810-6720I. H FEC INSPECTION PER NDT SPM 06-10-01.00 OF THE LT WING REAR SPAR LOWER ROOT DID NOT DETECT ANY CRACKS. VISUALLY INSPECTED ALL STRIPPED AREAS TO VERIFY NO STRUCTURAL DISCREPANCIES EXIST PER SAME EO. NO DESCREPANCIE S FOUND. APPLIED SEALANT TO AQUAMISED AREA. PERFORMED 12 HR FUEL SOA K CHECK PER DC8 MM 28-10-01. NO LEAKS NOTED. 2 L 7 4 4F RT 4A25 2002112200004 20021122 00004 WP 2002 11 22 UPS02839650 1 20020920 A 5330 NPN SKIN DOUG DC8 DC871F 302199D WP FS 1714 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, REPAIR DOUBLER 744-3R-02, STA 1714 - 1723 AND LONG 17 RT TO 18 RT IS CAT D ONLY 2 ROWS BEYOND DAM AGED. NO CUT-OUT (STOP-DRILLED) AND UPPER CRIT ICAL ROW HIDDEN SKIN REMOVED EXISTING REPAIR DOUBLER AND DAMAGED AREA IAW DC8 SRM 51-1-21 AND 53-2-1 FIG 7. REMOVED LONGERON 17 RT CAP INTERCOSTAL AND SHEAR TIE. FABRICATE REPAIR DOUBLER IAW D C8 SRM 53-2-1 FIG 7, ALODINED & PR9 IMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 53-2-1 FIG 7. REINSTALLED LONG 17 RT CAP INTERCOSTAL AND SHEAR TIE IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002112200005 20021122 00005 WP 2002 11 22 UPS02839653 1 20020919 A 5330 NPN SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, REPAIR DOUBLER 744-3L-02 STA 1710 TO 1737 AND LONG 26 LT TO 28 LT IS CAT D, DUE TO NO FASTNER RO WS BELOW CUT-OUT AND SKIN CRITICAL ROWS HIDDEN. REMOVED EXISTING DOUBELR, FABRICATED NEW DOUBLER, SKIN DILLER, AND FIN GER DOUBLERS AND INSTALLED IAW DC8 SRM 53-2-1 FIG 7. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 2 L 7 4 4F RT 4A25 2002112200006 20021122 00006 WP 2002 11 22 UPS02839654 1 20021003 A 5210 DOUBLER DOUG DC8 DC871F 302199D WP PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, L1 DOOR CORNER UPPER AFT DOUBLER IS STEEL. REMOVED DOUBLER IAW DC8 SRM 51-1-21. ROUTED OUT CRACKS , REPERFORMED HFEC AND NO CRACKS WERE NOTED. FABRICATED FILLERS AND DOUBLERS IAW DC8 SRM 53-2-0 FIG 15. ALODINED AND PRI MED IAW DC8 SRM 51-1-8. INSTALLED DBLR/TRIPLER AND FILLERS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002112200007 20021122 00007 WP 2002 11 22 UPS02839655 1 20020925 A 5330 57799117 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, FS 450 BETWEEN LONGERON 36 AND 35 RT HAS FOUND TO HAVE DAMAGE IN SKIN SPLICE DOUBLER. FABRICATED DOUBLER PN 5779911-7 IAW DAC DWG 5779911-7. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND FABRICATED FINGER DOUBLER IAW DA C DWG 5779911-9 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FINGER DOUBLER AND STRAP IAW DC8 SRM 51-1-21 AND 51-1- 20D 2 L 7 4 4F RT 4A25 2002112200008 20021122 00008 WP 2002 11 22 UPS02839656 1 20020921 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, FUSELAGE AT STA 1745 ABOVE LONGERON 15 RT, SKIN CRACKED. PERFORMED HFEC IAW DAC SPM NDT MANUA L PT 6 51-00-01.003 TO VERIFY CRACK REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER, FINGER DOUBLERS AND FILLER IAW DC8 SRM 53-2-1 FIG 7 ALODINED AND PRIMED REPAIR PART S IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-1 FIG 7, 51-1-21, AND 51-1-20D 2 L 7 4 4F RT 4A25 2002112200009 20021122 00009 WP 2002 11 22 UPS02839657 1 20020920 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, BELLY SKIN AT STA 150 UNDER LOWER VHF ANTENNA IS EXFOLIATED, REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 AND 5 1-1-8 PROCURED MATERIAL IAW DC8 SRM 53-2-1 FIG 7. CUT OUT DAMAGED AR EA IAW DC8 SRM 53- 2-1 FIG 7. FABBED DOUBLER, FILLER AND 4 EA FINGER DOUBLERS IAW DC8 SRM 53-2-1 FIG 7 ALODINED AND PRIMED IAW DC8 SRM 51 - 1-8. INSTALLED IAW DC8 SRM 53-2-1 FIG 7 2 L 7 4 4F RT 4A25 2002112200010 20021122 00010 WP 2002 11 22 UPS02839658 1 20020921 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE MISINSTALLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, REPAIR DOUBLER 744-2R-04 DETERMINED TO BE CAT D, DUE TO LESS THAN 3 ROWS OF FASTNERS PAST DAMAGE FS 450-455 LONGERON 35 RT FABRICATED FILLER, DOUBELR, DINGERS IAW DC8 SRM 53-2-1 ALODINED AND PRIMED IAW DC8 SRM 51- 1-8 AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-1 -20D 2 L 7 4 4F RT 4A25 2002112200011 20021122 00011 WP 2002 11 22 UPS02839659 1 20020921 A 5315 575352211 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, FLOORBEAM ATTACH ANGLE STA 1766, LBL 20 HAS CORROSION UNDER NUTPLATE ON VERTICAL LEG. REMOVED AND REPLACED ANGLE IAW DC8 SRM 51-1-21 2 L 7 4 4F RT 4A25 2002112200012 20021122 00012 WP 2002 11 22 UPS02839660 1 20020921 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, REPAIR 744-3L-05 STA 1748 TO 1754 AND LONGERON 14 LT TO LONGERON 15 LT, IS CAT B REPAIR, 9 INCHE S TO REPAIR 744-3L-04 ONLY 2 ROWS BEYOND DAMAGE LOWER CRITICAL ROW SKIN HIDDEN, REPAIRED AREA IAW DC8 SRM 53-2-0, FIG 7, CLASS II 2 L 7 4 4F RT 4A25 2002112200013 20021122 00013 WP 2002 11 22 UPS02839661 1 20020922 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, R1 DOOR JAMB LWR AFT CORNER HAS 2 CRACKS FOUND WITH NDT, REPAIRED AREA IAW DC8 SRM 53-2-0 FIG 14 2 L 7 4 4F RT 4A25 2002112200014 20021122 00014 WP 2002 11 22 UPS02839662 1 20020920 A 5340 3779762501 FITTING DOUG DC8 DC871F 302199D WP STA 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, BATHTUB FITTING CRACKED AT BS 681, LONGERON 3 RT. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-2 0D 2 L 7 4 4F RT 4A25 2002112200015 20021122 00015 NM 2002 11 22 VNAA0211019 1 20021118 A 3200 TIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NOSE WHEEL FAILED A VNAA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 461PS 3075 DURING TAKE OFF, THE CREW EXPERIENCED A NOSE WHEEL VIBRATION AND ABORTED TAKE OFF. MAINTENANCE AND TIRES WERE THEN SENT TO DCA. MAINTENANCE INSPEECTED AND REPLACED THE NOSE WHEEL TIRES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-0 0. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002112200016 20021122 00016 WP 2002 11 22 UPS02839663 1 20020920 A 5330 SKIN DOUG DC8 DC871F 302199D WP FS 1436 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, REPAIR DOUBLER 744-3R-04, STA 1436 TO 1445 AND LONGERON 26 RT TO 27 RT IS CAT C STEEL WITH REPLAC ABLE BLIND FASTENERS AND ALL CRITICAL ROWS FASTENERS SKIN HIDDEN. REMOVED OLD DOUBLER & FILLER FOM. PREFORMED HFEC O N CUTOUT SKIN. NO CRACKS FOUND IAW NDT SPM 06-10-01-001. FABBED -15 & -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 21 ALODINED AN D PRIMED IAW DC8 SRM 51-1-8. IN STALLED -15 & -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 21 2 L 7 4 4F RT 4A25 2002112200017 20021122 00017 2002 11 22 SWAA022700 4 20021114 A 2565 65C19901 CABLE BOEING 737 7375H4 138449D NM AFT SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED C2 CHECK, FOUND AFT SVD DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002112200018 20021122 00018 2002 11 22 SWAA022701 4 20021114 A 2565 6551463 HOOK BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 732SW 27864 FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2002112200019 20021122 00019 NM 2002 11 22 SWAA022704 1 20021114 A 2751 6546434 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 602SW 27953 DURING SCHEDULED C2 CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT INBD AFT T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002112200020 20021122 00020 2002 11 22 SWAA022707 4 20021116 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002112200021 20021122 00021 2002 11 22 SWAA022708 4 20021116 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002112200022 20021122 00022 2002 11 22 SWAA022709 4 20021116 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED GIRT BA R BRACKET PER MM. 2 L 7 2 4F RT A16WE 2002112200023 20021122 00023 2002 11 22 SWAA022712 4 20021115 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002112200024 20021122 00024 WP 2002 11 22 UPS02839664 1 20020920 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, FLOORBEAM AT FS 1723 BL16L HAS CORROSION UNDERNEATH LOWER FLANGE. REMOVED CORROSION IAW DC8 SR M 51-1-8 FOUND TO BE OUT OF LIMITS IAW D C8 SRM 53-2-0 REMOVED FLOORBEAM IAW DC8 SRM 51-1-20D FABBED FLOORBEAM IAW DC8 D AC DWG 5755032 ALODINED AND PRIMED FLOORBEAM IAW DC8 SRM 51-1-8 INSTALLED IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002112200025 20021122 00025 NM 2002 11 22 SWAA022739 1 20021119 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002112200026 20021122 00026 NM 2002 11 22 SWAA022740 1 20021118 A 5330 6545785 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUT CRACKED AT RT WINDOW NR 28. REPAIRED CUTOUT PER SRM. 2 L 7 2 4F RT A16WE 2002112200027 20021122 00027 NM 2002 11 22 SWAA022741 1 20021119 A 5313 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED STRINGER TIE C LIP PER SRM. 2 L 7 2 4F RT A16WE 2002112200028 20021122 00028 NM 2002 11 22 SWAA022742 1 20021119 A 5330 6545775 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 14R, BS 867 AND BS 897. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 2002112200029 20021122 00029 NM 2002 11 22 SWAA022743 1 20021118 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002112200030 20021122 00030 NM 2002 11 22 SWAA022744 1 20021118 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, ABOVE STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002112200031 20021122 00031 NM 2002 11 22 SWAA022745 1 20021118 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C3, FOUND FUSELAGE SKIN CRACKED AT BS 767, ABOVE STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002112200032 20021122 00032 WP 2002 11 22 UPS02839665 1 20020920 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, REPAIR DOUBLER 744-3R-01 STA 1690-1697 AND LONGERON 26 - 28 RT IS CAT D, DUE TO DEFORMED FASTENER LESS THAN 3 ROWS OF FASTENERS BEYOND DAMAGED AND IS A STEEL REPAIR LESS THAN BASE SKIN. FABRICATED NEW REPAIR DOUBL ER, FINGER DOUBLER, TEAR STRIP AND FILLER IAW DC8 SRM 53-2-1 FIG 7 SHEET 5 ALODINED & PRIMED IAW DC8 SRM 51-1- 8. INSTAL LED REPAIR DOUBLER, FINGER DOUBLER, TEAR STRIP, FILLER, FIT TINGS AND PROCUCTION BOLTS IAW DC8 SRM 51-1-20D, 51-1-21, AN D 51-3-0 . 2 L 7 4 4F RT 4A25 2002112200033 20021122 00033 WP 2002 11 22 UPS02839666 1 20020920 A 5320 CHANNEL DOUG DC8 DC871F 302199D WP FLOOR SUPPORT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, FLOOR SUPPORT CHANNEL CORRODED AT APPROX BL10L FS 1717 REMVOED CORROSION IAW DC8 SRM 51-1-8 AND FOUND TO BE OUT OF LIMITS I AW DC8S SRM 53-2-0 HEAT TREATED NEW CHANNEL FROM 0 TO T6 IAW TPS -10 03 FABBED CHANNEL IAW DC8 DAC DWG 5755032 ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED CHANNEL IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2003020700146 20030207 00146 EU 2003 2 7 DHL2002362515 1 20021121 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 CORROSION BETWEEN SKIN AND DOUBLER AT AFT LAVATORY SERVICE PANEL (DEACTIVATED). AREA WAS REPAIRED BY CUTTING OUT DAMAGE AND INSTALLING A FILLER AND AN EXTERNAL DOUBLER. 2 L 7 2 4F RT A35EU 2003020700147 20030207 00147 EU 2003 2 7 DHL2002362516 1 20021119 A 5531 ANGLE AIRBUS 300 A300B4203 3930306 EU VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 VERTICAL STAB AT RIB 28, THE VERY TOP OF STAB, THE VERY AFT ANGLE IS CRACKED. REMOVED ANGLE, FABBED ANGLE AND INSTALLED 2 L 7 2 4F RT A35EU 2002112200034 20021122 00034 WP 2002 11 22 UPS02839667 1 20020920 A 5320 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, FLOOR SUPPORT ANGLE CORRODED AT FS 1766 LBL13. CORROSION OUT OF LIMITS, FABBED NEW ANGLE IAW DAC DWG 5755032 INSTAL LED NEW ANGLE IAW DC8 SRM 51-1-21D 2 L 7 4 4F RT 4A25 2002112200035 20021122 00035 WP 2002 11 22 UPS02839826 1 20021013 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 75 AT STRINGER 9. CUTOUT CRACKED SKIN, NDT VERIFIED NO CRACK S AT CUTOUT, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 2002112200036 20021122 00036 WP 2002 11 22 UPS02839827 1 20021014 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 LEFT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 11. CUTOUT CRACKED SKIN, NDT VERIFIED NO CRACK S AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 2002112200037 20021122 00037 WP 2002 11 22 UPS02839828 1 20021016 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 AFT ACCY COMPARTMENT LONG 33L CORRODED BEYOND LIMITS BETWEEN STATION 1540 TO 1545. REMOVED LONGERON SECTION FROM STA 1515 TO 1550 AT LONG 33L, FABRICATED AND INSTALLED LONGERON SECTION AND SPLICES IAW SRM 53-2-2, FIG 10, 53-4-1 FIG 43. 2 L 7 4 4F RT 4A25 2002112200038 20021122 00038 WP 2002 11 22 UPS02839668 1 20020920 A 5320 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, FLOOR SUPPORT ANGLE CORRODED AT FS 1766 24 LBL. CORROSION OUT OF LIMITS, FABBED NEW ANGLE IAW DAC DWG 5755032 INSTAL LED NEW ANGLE IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002112200039 20021122 00039 WP 2002 11 22 UPS02839829 1 20021015 A 5514 37014272N FITTING DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 RIGHT HORIZONTAL STAB LOWER PLANK FITTING IS CRACKED AT XFS 46. REMOVED AND REPLACED FITTING IAW DWG 3701427, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002112200040 20021122 00040 WP 2002 11 22 UPS02839830 1 20021013 A 5320 4772397U1 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 LONG 17L AND END FITTING IS CRACKED AT STA 1766 AFT SIDE OF BULKHEAD. REMOVED AND REPLACED LONGERON AND END FITTING IAW DWG 5649327, 4772397 AND SRM 51-1-20D, 51-1-21, LONGERON FABRICATED IAW DWG 5649327. 2 L 7 4 4F RT 4A25 2002112200041 20021122 00041 WP 2002 11 22 UPS02839831 1 20021014 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 RIGHT WING CENTER L/E LOWER SKIN IS CRACKED AT FASTENER HOLE AT XFS 347.75. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATES AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B. 2 L 7 4 4F RT 4A25 2002112200042 20021122 00042 WP 2002 11 22 UPS02839832 1 20021022 A 5320 3750257U503 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 STATION 1040-1050 LONGERON 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 37502 57, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002112200043 20021122 00043 WP 2002 11 22 UPS02839836 1 20021013 A 5313 4772397U1 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 STA 1766 LONG 17R AND END FITTING ARE CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON AND END FIT TING IAW DWG 5649327, 4772397, SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2002112200044 20021122 00044 WP 2002 11 22 UPS02839837 1 20021011 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM THE R1 DOOR UPPER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 14. REMOVE STEE L DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER,TRIPLER AND FILLER IAW SRM 53-2-0 FIG 14. 2 L 7 4 4F RT 4A25 2002112200045 20021122 00045 WP 2002 11 22 UPS02839838 1 20021025 A 5320 3755822505 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 STA 300 BETWEEN LONG 35L TO 36 BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTI NG IAW DWG 3755822, AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002112200046 20021122 00046 WP 2002 11 22 UPS02839839 1 20021021 A 5320 3755822505N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 STA 300 BETWEEN LONG 33L TO 34L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITT ING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2002112200047 20021122 00047 WP 2002 11 22 UPS02839843 1 20021022 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 STA 300-305 LONGERON 35R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON SECTIO N BETWEEN STA 290 TO 330 AT LONG 35R IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2002112200048 20021122 00048 WP 2002 11 22 UPS02839844 1 20021022 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 STA 300-305 LONG 35L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON 35L SECTIO N BETWEEN STA 290 TO 330 IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2002112200049 20021122 00049 WP 2002 11 22 UPS02839845 1 20021014 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 RADIOGRAPHIC (X-RAY) INSPECTION DETECTED 2 CRACKS ON THE L1 DOOR LOWER AFT CORNER APPROX 5.25 INCHES AND .419 INCH AT STA 60 LONG 20L. REMOVED EXISTING DOUBLER, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABR ICATED AND INSTALLED DOUBLERS, TRIPLERS, AND FILLERS AT L1 DOOR FWD AND AFT CORNERS IAW SRM 53-2-0 FIG 14, PREVIOUS DOUB LER COVERED BOTH CORNERS. 2 L 7 4 4F RT 4A25 2002112200050 20021122 00050 WP 2002 11 22 UPS02839847 1 20021021 A 5320 4611159501N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 STA 70 LONG 22L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4611159, AND SRM 51-1-2 0D. 2 L 7 4 4F RT 4A25 2002112200051 20021122 00051 WP 2002 11 22 UPS02839848 1 20021011 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM THE R2 DOOR UPPER AFT CORNER AND REPAIR PER SRM 53-2-0 FIG 16, STA 1660 LON G 11R AND SKIN AND INTERNAL DOUBLER ARE CRACKED. REMOVED STEEL DOUBLER, CUTOUT DAMAGED AREA ON SKIN AND INTERNAL DOUBLE R, NDT VERIFIED NO CRACKS AT CUTOUT, AND CRACK ON LONGERON TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED DOUBLER , TRIPLER FILLER AND STRAP IAW SRM 53-2-0 FIG 16, SAA SK 779-225 AND UPS EO DC8-5330-17754-A. 2 L 7 4 4F RT 4A25 2003020700149 20030207 00149 EU 2003 2 7 DHL2002362517 1 20021119 A 5311 SHEAR TIE AIRBUS 300 A300B4203 3930306 EU FUSELAGE FRAME CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 CORRODED SHEAR TIE AT FRAME 46, STRINGER 54 TO 56. FOUND TO BE OUT OF LIMITS. FABRICATED 1 REPAIR ANGLE, 1 REPAIR ANGLE , 2 REPAIR FILLERS IAW A300 SRM, AND INSTALLED. 2 L 7 2 4F RT A35EU 2002112200052 20021122 00052 CE 2002 11 22 2002F01023 1 20021018 A 3231 66003611 CONTROL VALVE LEAR 35 31A 5170531 CE MLG INTERMITTENT A AOQA O OTHER J WARNING INDICATION CL CLIMB 1 EA 11 583LJ 1533 151 DURING CLIMB, LANDING GEAR DID NOT RETRACT WHEN SELECT UP ON FIRST RETRACTION ATTEMPT. SELECTOR HANDLE CYCLED GEAR OPER ATED NORMALLY ON ALL SUBSEQUENT SELECTIONS. ACCOMPLISHED OPERATION CHECKS COULD NOT DUPLICATE, TROUBLESHOT SYSTEM AND R EPLACED SUSPECTED INTERMITTENT MAIN LANDING GEAR DOOR CONTROL VALVE. ACCOMPLISHED NUMEROUS GEAR SWINGS TO INSURE PROPER OPERATION AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A10CE 2002112200053 20021122 00053 NM 2002 11 22 MEX2002333 1 20021024 A 2410 696233B CSD DOUG MD88 MD88 3023688 NM PWA JT8 JT8D217 52053 NE LT ENGINE LEAKING A ASMF E A ENGINE SHUTDOWN UNSCHED LANDING K M FLUID LOSS OVER TEMP CL CLIMB 1 SW 23 168PL 53174 FLT 189 - LAP-MEX - DURING TRANSIT, LOW OIL LEVEL IN BOTH LEFT AND RIGHT CSD'S WAS FOUND. AFTER 20 MINUTES DEPARTURE FR OM LAP, THE FLIGHT CREW OF AIRPLANE NOTICED HIGH TEMPERATURE INDICATIONS IN LEFT ENGINE. SUBJECT ENGINE WAS SHUTDOWN AS PER APPLICABLE PROCEDURES AND AIRPLANE RETURNED TO DEPARTING AIRPORT. THE GEAR BOX CHIP DETECTOR, PRESSURE LINES AND M AIN FILTER OIL WERE VERIFIED. THE ENGINE 1 TANK OIL LEVEL WAS FOUND EXCEEDED AND CSD OIL LEVEL WAS FOUND IN RED RANGE. THE EXCEEDED OIL WAS DRAINED. DURING OVERNIGHT SERVICE THE CSD, CSD HEAT EXCHANGER AND SEALS WERE REPLACED IAW MM 24-1 0-01, 24-20-01 AND 24-10-03, RESPECTIVELY. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002112200054 20021122 00054 SO 2002 11 22 SIMA200230202 1 20021028 A 2741 PITCH CONTROL EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A SIMA A UNSCHED LANDING F P FLT CONT AFFECTED NO WARNING INDICATION CL CLIMB 1 SW 21 637AE 145170 FLT 3789 - DFW - DURING CLIMB, CAPTAINS PITCH TRIM FAILED WITH NO INDICATION ON EICAS. FIRST OFFICER AND STANDBY PITCH TRIM WORKED NORMAL. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY. MAINTENANCE COULD NOT DUPLICATE DISCREPA NCY. OPERATIONAL CHECK WAS COMPLIED WITH IAW EMB MM WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002112200055 20021122 00055 WP 2002 11 22 UPS02839669 1 20020920 A 5320 S2652479 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, FLOOR SUPPORT CORRODED AT BL0 FS 1723-1730 LT LOWER FLANGE. BLENDED CORROSION IAW DC8 SRM 51-1- 8 OUT OF LIMITS IAW DC8 SRM 53-2- 0 MAD ID FLOOR SUPPORT PN S2652479, ALODINED & PRIMED IAW DC8 SRM 51 -1-8, INSTALLED I AW DC8 SRM 51-1-21D 2 L 7 4 4F RT 4A25 2002112200056 20021122 00056 WP 2002 11 22 UPS02839670 1 20020920 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, REPAIR 744-3R-05, STA 1376-1384 AND LONGERON 24 - 26 RT IS CATEGORY D, DUE TO ONLY 2 ROWS OF FAS TENER BEYOND CUTOUT AND AFT CRITICAL ROW FASTENER SKIN HIDDEN REMOVED OLD DOUBLER IAW DC8 SRM 51-1-21, REMOVED DAMAG ED AREA, FABBED NEW DOUBLER, FINGER DOUBLERS AND FILLER IAW DC8S RM 53-2-1 FIG 7 S H 4 AND REO G08806 ALODINED AND PRIME D IAW DC8 SRM 51-1-8 INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21 AND 51-1-20D 2 L 7 4 4F RT 4A25 2002112200057 20021122 00057 2002 11 22 SIMA200230203 4 20021024 A 2297 4PB717T2 WIRE EMB 145 EMB145LR 3260212 SO AUTOPILOT SYS CHAFED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 21 634AE 145150 ROC - FLT 4145 - DURING LANDING ON SHORT FINAL SMOKE CAME FROM THE FIRST OFFICERS CONTROL YOKE PITCH TRIM SWITCH FOLLOWE D BY THE PITCH TRIM CIRCUIT BREAKER TRIPPING. CONTRACT MAINTENANCE FOUND NO PROBLEMS WITH THE PITCH TRIM SWITCH, BUT TH EY FOUND SIGNS OF ELECTRICAL ARCING AT A CHAFED WIRE ON THE AUTO PILOT DISCONNECT PUSHBUTTON SWITCH. MAINTENANCE REMOVE D AND REPLACED THE AUTO PILOT DISCONNECT SWITCH AND REPAIRED THE CHAFED WIRE IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002112200058 20021122 00058 WP 2002 11 22 UPS02839671 1 20020916 A 5210 SKIN DOUG DC8 DC871F 302199D WP PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1` L1 DOOR CORNER UPPER FWD DOUBLER IS STEEL, CUT OUT CRACKS IN SKIN IAW DC8 SRM 53-2-0 FIG 15 TR 53-1 29 AND REO G 08797 PERFORMED HFEC IAW DC8 SPM NDT MAN 06-10-01.001 FABBED -15 & - 17 DOUBLERS AND -19 FILLER IAW DC8 SRM 53-2-0 FIG 15 TR 53-129 AND REO G08797. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLERS & FILLERS IAW DC8 SRM 51-1-20D,53-2-0 FIG 15 TR 53-129 & REO G08797 2 L 7 4 4F RT 4A25 2003020700150 20030207 00150 EU 2003 2 7 DHL2002362518 1 20021119 A 5754 RIB AIRBUS 300 A300B4203 3930306 EU SLAT DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 LT WING LEADING EDGE NR 1 SLAT HAD TOOL MARKS ON ANGLE INSIDE OF SLAT STRUCTURE, VIEWED WITH A BOROSCOPE THRU OUTBOARD D RAIN HOLE NEAR JACKSCREW. AREA WAS REPAIRED BY CUTTING OUT DAMAGE AND INSTALLING A FILLER. 2 L 7 2 4F RT A35EU 2002112200059 20021122 00059 WP 2002 11 22 UPS02839672 1 20020924 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, AFT LOWER CARGO AT STA 1420 FRAME AT LONGERON 22 RT HAS ELONGATED HOLES. REMOVED OLD FRAME, LOCA TED DRILLED, AND DEBURRED NEW FRAME IAW DC8 SR M 51-1-21 ALODINED & PRIMED IAW DC8 SRM 51-1-8 INSTALLED NEW FRAME IAW D C8 SRM 51-1-24 2 L 7 4 4F RT 4A25 2002112200060 20021122 00060 SO 2002 11 22 SIMA200230204 1 20021027 A 3244 TIRE EMB 135 EMB135KL 3260302 SO RT MLG BLOWN A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 821AE 145577 PHX - FLT 3420 - DURING TAKEOFF ROLL, CREW FELT A SHUDDERING FROM RIGHT SIDE OF AIRCRAFT DUE TO A TIRE BLOW OUT. CREW T AXIED AIRCRAFT OFF THE RUNWAY AND DEPLANED THE PASSENGERS WITH NO FURTHER INCIDENTS REPORTED. AFTER POST FLIGHT INSPECT ION MAINTENANCE NOTED DAMAGE TO RIGHT MLG DOOR, BOTH NR 3 AND 4 TIRES WERE OFF THEIR RIMS, RUBBER MARKS ON RIGHT SIDE OF FUSELAGE, AND POSSIBLE INGESTION INTO NR 2 ENGINE. (M) 2 L 7 2 4F RT T00011AT 2002112200061 20021122 00061 WP 2002 11 22 UPS02839673 1 20020920 A 5340 3779658502 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C 1, MAIN CABIN BATHTUB FITTING CRACKED AT BS 857 LONGERON 10 RT. REMOVED AND REPLACED FITTING AIW DC 8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002112200062 20021122 00062 SO 2002 11 22 SIMA20023028 1 20021026 A 5320 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON A PREVIOUS REPAIR TO THE LEFT OMEGA BEAM AT FRAME 20. REMOVED PREVIO US REPAIR AND INSPECTION. THE UNDERLYING BEAM. NO ADDITIONAL DAMAGE NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142, CHAPTER 53, REV 19) 53-21-10 PARA 2 FIG 201 SHEET 1, AND STANDARD SRM PRA CTICES. (M) 2 L 7 2 4T RT T00011AT 2002112200063 20021122 00063 WP 2002 11 22 UPS02839674 1 20020920 A 5340 3779658502 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, MAIN CABIN BATHTUB FITTING CRACKED AT BS 587 L10L REMOVED AND REPLACED FITTING IAW DC8 SRM 51- 1-20D 2 L 7 4 4F RT 4A25 2002112200064 20021122 00064 SO 2002 11 22 SIMA200230329 1 20021026 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND TO BE CHAFED BEYOND SRM LIMITS AT SKIN JUNCTION 05. BLEND ED CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE, TWO SHIMS. R EPAIR DONE IAW EMB 145 SRM (145/1142, CHAPTER 53, REV 19) 53-24-02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002112200065 20021122 00065 WP 2002 11 22 UPS02839675 1 20021005 A 5340 45715111 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, MAIN CABIN INTERIOR RT SIDE OVERWING HATCH UPPER AFT FITTING CRACKED. REMOVED AND REPLACED CRAC KED FITTING IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002112200066 20021122 00066 SO 2002 11 22 SIMA200230330 1 20021026 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 737MW 145396 ABI - DURING MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. COMPLETELY REMOVED CORROSION BY CUTOUT . PERFORMED AN EDDY CURRENT INSPECTION OF THE CUT OUT AREA WITH NO DEFECTS NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER , TWO SHIMS. REPAIR DONE IAW EMB-145 (SRM 145/1142, CHAPTER 53, REV 19) 53-21-10 PARA 2, FIG 201 SHEET 2, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002112200067 20021122 00067 WP 2002 11 22 UPS02839676 1 20020920 A 5340 37797621 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, BATHTUB FITTING CRACKED AT BS 681, LONGERON 7 RT. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1- 20D 2 L 7 4 4F RT 4A25 2002112200068 20021122 00068 WP 2002 11 22 UPS02839677 1 20020920 A 5340 37797621 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, BATHTUB FITTING CRACKED AT BS 681, LONGERON 10 LT. REMOVED AND REPLACED FITTING IAW DC8 SRM 51 -1-20D 2 L 7 4 4F RT 4A25 2002112200069 20021122 00069 SO 2002 11 22 SIMA200230332 1 20021017 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 145402 ABI - DURING AN MBV INSPECTION THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS AT FRAME 20. CUT OUT SECTI ON OF DAMAGED OMEGA BEAM AND APPLIED SURFACE TREATMENT. FABRICATED A FILLER, TWO SHIMS, BACK PLATE AND DOUBLER. REPAIR DONE IAW EMB SRM (EMB 145/1142 REV 19) 53-21-10 FIG 201 AND STANDARD SRM PROCEDURES. (M) 2 L 7 2 4F RT T00011AT 2002112200070 20021122 00070 SO 2002 11 22 SIMA200230333 1 20021002 A 5347 14530659001 SEAT TRACK EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - THIS IS A LEVEL 2 FINDING, LEFT FORWARD INBOARD SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SEAT TRACK IAW EMB 145 AMM 53-01-06. (M) 2 L 7 2 4T RT T00011AT 2002112200071 20021122 00071 SO 2002 11 22 SIMA200230334 1 20021002 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA CENTER BEAM GUSSET HAS CORROSION. INSTALLED SERVICEABLE CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002112200072 20021122 00072 SO 2002 11 22 SIMA200230335 1 20021002 A 5320 1452245903 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - THIS IS A LEVEL 2 FINDING, GALLEY RAMP SUPPORT HAS CORROSION. INSTALLED SERVICEABLE GALLEY RAMP SUPPORT IAW EMB 1 45 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002112200073 20021122 00073 SO 2002 11 22 SIMA200230336 1 20021002 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - THIS IS A LEVEL 2 FINDING, GALLEY ARE AFT DIAMOND GUSSET HAS CORROSION. INSTALLED SERVICEABLE AFT DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002112200074 20021122 00074 SO 2002 11 22 SIMA200230337 1 20021002 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA FORWARD GUSSET (DIAMOND) HAS CORROSION. INSTALLED SERVICEABLE GUSSET IAW E MB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002112200075 20021122 00075 SO 2002 11 22 SIMA200230338 1 20021002 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - THIS IS A LEVEL 2 FINDING, RIGHT FORWARD SILL HAS CORROSION. INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002112200076 20021122 00076 SO 2002 11 22 SIMA200230339 1 20021002 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - THIS IS A LEVEL 2 FINDING, SERVICE DOOR CENTER SILL HAS CORROSION. REMOVED AND REPLACED SILL IAW EMB GST-2969/02. (M) 2 L 7 2 4T RT T00011AT 2002112200077 20021122 00077 SO 2002 11 22 SIMA20023034 1 20021002 A 5315 14521718003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - THIS IS A LEVEL 2 FINDING, LEFT OMEGA BEAM FLOOR SUPPORT ANGLE HAS CORROSION. REMOVED AND REPLACED FLOOR ANGLE IA W EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002112200078 20021122 00078 SO 2002 11 22 SIMA200230341 1 20021004 A 5320 14521725001 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA LEFT SILL HAS CORROSION. INSTALLED SERVICEABLE LEFT SILL IAW EMB 145 SRM 5 1-40-02. (M) 2 L 7 2 4T RT T00011AT 2002112200079 20021122 00079 SO 2002 11 22 SIMA200230342 1 20021002 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 ABI - THIS IS A LEVEL 2 FINDING, RIGHT AFT SILL HAS CORROSION. INSTALLED SERVICEABLE SILL IAW EMB SRM 51-40-02, 51-40-0 6 AND 51-20-03. (M) 2 L 7 2 4T RT T00011AT 2002112200080 20021122 00080 SO 2002 11 22 SIMA200230344 1 20021029 A 5330 14520622003 SKIN EMB 135 EMB135KL 3260302 SO FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 145529 SAW - AIRCRAFT FERRIED TO SAW FOR REPAIR OF DENT ON RIGHT SIDE OF AIRCRAFT AFT OF SERVICE DOOR, AT FRAME 25. DAMAGED ST RINGERS, FRAME, AND SKIN WERE REPAIRED IAW ENGINEERING ORDER EB-53MR-124. (M) 2 L 7 2 4F RT T00011AT 2002112200081 20021122 00081 EU 2002 11 22 SIMA200230801 1 20021101 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 180AE 340B180 DFW - FLT 3533 - CREW REPORTED SEVERAL FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE EMERGENCY POWER SUPPLY UNIT AT 24LN. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002112200082 20021122 00082 EU 2002 11 22 SIMA200231007 1 20021104 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU LT MLG DISCONNECTED A SIMA K NONE N FALSE WARNING AP APPROACH 1 SW 21 380AE 340B380 ABI - ON APPROACH, THE LEFT MAIN GEAR (GREEN LIGHT) WOULD NOT ILLUMINATE. PUMP AND THE TRANSIT LIGHT FUNCTIONED NORMALL Y. MADE NORMAL LANDING AFTER FOLLOWING AOM CHECKLIST. MAINTENANCE FOUND THE LEFT DOWNLOCK SWITCH CANNON PLUG NOT CONNE CTED. MAINTENANCE FOUND THE LEFT DOWNLOCK SWITCH CANNON PLUG NOT CONNECTED. MAINTENANCE RECONNECTED THE CANNON PLUG, A RETRACTION CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002112200083 20021122 00083 NM 2002 11 22 VNAA0211001 1 20021101 A 3250 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING DIRTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 328JS 3030 DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE AND ABORTED TAKEOFF. UPON RETURNING TO THE GAT E, MAINTENANCE INSPECTED AND CLEANED THE CANNON PLUGS ON THE NOSE WHEEL STEERING ELECTRONIC CONTROL, HYDRAULIC MANIFOLD, NOSE WHEEL TILLER, AND THE NOSE LANDING GEAR BULKHEAD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIO NAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002112200084 20021122 00084 2002 11 22 VNAA0211003 4 20021105 A 3454 7510100813 VOR SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NR 2 MALFUNCTIONED A VNAA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 472PS 18041 3008 ON APPROACH TO CAK, THE CREW WAS RECEIVED ERRATIC INDICATIONS FROM THE LOCALIZER ON TWO ATTEMPTS. THE CREW ALSO RECEIVE D A FLAP OVER SPEED INDICATION OF 6 KNOTS. THE CREW THEN DIVERTED TO CLE. MAINTENANCE WAS SENT FROM CAK TO PERFORM A F LAP OVERSPEED INSPECTION AND REPLACE THE NR 2 NAV UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-00-00. OPERATIO NAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002112200085 20021122 00085 WP 2002 11 22 UPS02839821 1 20021013 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 STA 1600 L21L FLOORBEAM FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, DRILLED NEW FITTING AND INSTALLED IAW DC8 SRM 51-1-20D AND DAC DWG 3751062. 2 L 7 4 4F RT 4A25 2002112200086 20021122 00086 WP 2002 11 22 UPS02839822 1 20021013 A 5320 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 AFT LWR PIT BETWEEN STA 1440 TO 1460 AT LONG 27R IN TORQUE BOX WEB IS CORRODED. REMOVED WEB, INTERC OSTAL AND (2) ATTACH CLIPS IAW DC8 SRM 51-1-21A & 51-1-21. FAB NEW INTERCOSTAL, WEB, & REPAIR IAW DC8 SRM 53-2-0 & DAC DWG 5616674. REC'D LOCATED (2) NEW ATTACH CLIPS IAW DC8 SRM 51-1-2 4. INSTALLED IAW DC8 SRM 51-1- 20D & 51-1-21 2 L 7 4 4F RT 4A25 2002112200087 20021122 00087 WP 2002 11 22 UPS02839823 1 20021022 A 5310 56402431 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 SHEAR TIE AT FS 1680 CRACKED AT LONG 18L. REMOVED AND REPLACED SHEAR TIE IAW DAC DWG 5640243-1. 2 L 7 4 4F RT 4A25 2002112200088 20021122 00088 WP 2002 11 22 UPS02839849 1 20021011 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM THE L2 DOOR UPPER AFT CORNER AND REPAIR PER SRM 53-2-0 FIG 18, STA 1660 AT LONG 10L. REMOVED STEEL DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT FABRICATED AND INSTALLED DOUBLER IAW S RM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2002112200089 20021122 00089 WP 2002 11 22 UPS02839850 1 20021015 A 5230 DOOR FRAME DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 A-PIT DOOR FRAME IS CRACKED AFT SIDE OF 3RD UPPER HOOK FROM FWD END ON DOOR AT APPROX STA 300 AT LONG 23R ON DOOR. REMOVED FRAME SECTIONS, FABRICATED AND INSTALLED 2EA FRAME SECTIONS AND DOUBLERS IAW SRM 52-2-0 FIG 2 AND DWG 9754100. 2 L 7 4 4F RT 4A25 2002112200090 20021122 00090 WP 2002 11 22 UPS02839853 1 20021101 A 3230 CONTROL CABLE DOUG DC8 DC871F 302199D WP LT MLG OUT OF RIG A IPXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 705UP 45949 INSPECTION TYPE:N/A AFTER GEAR RETRACTION WITH GEAR HANDLE IN THE "UP" POSITION THE DOORS NOT LATCHED LIGHT IS ILLUMINAT ED. THE LT MLG DOOR ALTERNATE AMBER LIGHT IS ILLUMINATED. GEAR HAD TO BE CYCLED SEVERAL TIMES TO GET THE DOORS NOT LAT CHED LIGHT. RIGGED LT MLG FOLLOWUP GEAR DOOR CABLES PER MM 32-31-05 RIG & OPS CHECKED GOOD, CHECKED UPLOCK ROLLER CLEAR ANCE & PULL CHECK OPS CHECKED NORMAL. CYCLED GEAR, FREE FULL & LIGHT INDICATIONS CHECKED NORMAL PER MM 32-31-05, 32-31- 04. 2 L 7 4 4F RT 4A25 2002112200091 20021122 00091 WP 2002 11 22 UPS02839869 1 20021105 A 3350 BATTERY DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP WHEN SWITCH PLACED IN ARM POS AND BAT/EXT POWER SWITCH IN BAT FAILS TEST REF P S CHK. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT, OPS CHK GOOD REF 33-50-02. 2 L 7 4 4F RT 4A25 2002112200092 20021122 00092 WP 2002 11 22 UPS02839871 1 20021011 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM THE L2 DOOR LOWER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 18, APPROX STA 1 620 LONG 10L. REMOVED STEEL DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 2002112200093 20021122 00093 WP 2002 11 22 UPS02839872 1 20021014 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C2 STA 300-320 LONG 34L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED LONGERON REPAIR SE CTION AND SPLICES IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2002112200094 20021122 00094 WP 2002 11 22 UPS02839873 1 20021014 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 AFT CARGO PIT AT FS 1160 BETWEEN L35R-36 Z FITTING IS CORRODED. REMOVED CORRODED ZEE FITTING, LOCAT E NEW FITTING, DRILLED EXISTING FASTENER HOLES AND DEBURRED IAW DC8 SRM 51-3-2. FABRICATE REPAIR SPLICES IAW DC8 SRM 53 -2-0. INSTALLED ZEE FITTING AND REPAIR SPLICES IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002112200095 20021122 00095 WP 2002 11 22 UPS02839874 1 20021014 A 5330 47517341 STRAP DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 L2 AFT PAX DOOR, UPPER FWD CORNER HAS CRACK INDICATION AT FRAME ATTACHMENT FOUND BY RADIOGRAPHIC INS PECTION. REMOVED AND REPLACED STRAP IAW DAC DWG 5750985 AND DC8 SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 2002112200096 20021122 00096 NM 2002 11 22 HNAA0200080 1 20021120 A 5610 NP1579014 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM CRACKED A HNAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 07 968 8392 465 At 22000 feet the F/O's windshield cracked and shattered. Aircraft diverted to SAV where windshield was replaced. 2 H 7 2 4T RT A13NM 2002112200097 20021122 00097 WP 2002 11 22 UPS02839678 1 20020920 A 5340 37797621 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, BATHTUB FITTING CRACKED AT BS 681, L9R REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002112200098 20021122 00098 WP 2002 11 22 UPS02839679 1 20020920 A 5340 37797621 FITTING DOUG DC8 DC871F 302199D WP STA CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1 BATHTUB FITTING CRACKED AT BS 681, L8R REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002112200099 20021122 00099 WP 2002 11 22 UPS02839680 1 20020920 A 5340 37797621 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 BATHTUB FITTING CRACKED AT BS 681, L6R REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002112200100 20021122 00100 WP 2002 11 22 UPS02839681 1 20020920 A 5340 37797621 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 IN MAIN CABIN L2L END FITTING ON AFT SIDE OF BS 680 IS CRACKED REMOVED AND REPLACED FITTING IAW D C8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002112200101 20021122 00101 WP 2002 11 22 UPS02839682 1 20020920 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 IN MAIN CABIN L4L END FITTING ON AFT SIDE OF BS 680 IS CRACKED REMOVED AND REPLACED FITTING IAW D C8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002112200102 20021122 00102 WP 2002 11 22 UPS02839683 1 20020916 A 5340 FITTING DOUG DC8 DC871F 302199D WP FWD ACCESS BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 FWD ACCESS COMP'T AT FS 660 ABOVE L35L-L35R COMP DOOR UPPER TRACK FI TTING IS CRACKED REMVOED & R EPLACED FITTING IAW DC8 SRM 51-3-0 2 L 7 4 4F RT 4A25 2002112200103 20021122 00103 WP 2002 11 22 UPS02839684 1 20020920 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 LONGERON FITTING CRACK AT STA 1767 AT L17R ACCESS THRU DOOR 60 REMOVED AND REPLACE LONGERON END F ITTING IAW DC8 SRM 51-1-20D & 51-1 -21 2 L 7 4 4F RT 4A25 2002112200104 20021122 00104 WP 2002 11 22 UPS02839685 1 20020920 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 REPAIR DOUBLER 744-1R-02 DETERMINED TO BE CATEGORY B DUE TO PROXIMITY TO 744-1R-01 REMOVED EXISTI NG DOUBLERS AND REPAIRED AREA IAW DC8 SRM 53-2-1 FIG 7 2 L 7 4 4F RT 4A25 2002112200105 20021122 00105 WP 2002 11 22 UPS02839686 1 20020920 A 5320 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 FLOOR SUPPORT ANGLE CORRODED AT FS 1766 BL 18L REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC 8 SRM 53-2-0, REMOVED ANGLE IAW DC8 SRM 51-1-21 FAB, LOCATED AND DRILLED IAW DAC DWG 5 755032, ALODINE AND PRIMED IAW DC 8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-21D 2 L 7 4 4F RT 4A25 2002112200106 20021122 00106 WP 2002 11 22 UPS02839687 1 20020921 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 REPAIR DOUBLER 744-2R-07 STA 718 & 727 AND LONG 13R IS CAT D STAINLESS STEEL REPAIR WITH 2 ROWS OF FA STENERS BEYOND CUTOUT AND ALL CRITICAL ROW HIDDEN. REPAIRED AREA IAW REO G08803 2 L 7 4 4F RT 4A25 2002112200107 20021122 00107 NM 2002 11 22 HNAA0200081 1 20021119 A 5610 NP1579014 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM CRACKED A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 927HA 10847 117 After Take-off F/O's windshield cracked. A/C returned to DCA where windshield was replaced. 2 H 7 2 4T RT A13NM 2002112200108 20021122 00108 WP 2002 11 22 UPS02839688 1 20020921 A 5320 STIFFENER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C1 VERTICAL STIFFENER, LBL 20, ON FWD FACE OF AFT PRESSURE BULKHEAD HAS CORROSION ON LOWER END AT FLOOR LEVEL REPAIRED IAW REO G08808 2 L 7 4 4F RT 4A25 2002112200109 20021122 00109 WP 2002 11 22 UPS02839691 1 20020929 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 RT WING LE UPPER RIB IS CRACKED AT XFS 797.5. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINA TED AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER I.A.W. SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2002112200110 20021122 00110 WP 2002 11 22 UPS02839692 1 20020928 A 5310 4646547 ATTACH FITTING DOUG DC8 DC871F 302199D WP MAIN CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 STA. 822 FLOORBEAM ATTACH FITTING IS CRACKED AT RBL. 24 REMOVED AND REPLACED FITTING I.A.W. DWG.4 646547,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2002112200111 20021122 00111 WP 2002 11 22 UPS02839693 1 20021001 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 STA. 1746 LONG. 16L IS CRACKED. CUTOUT DAMAGED AREA FABRICATED AND INSTALLED LONGERON SECTION AND SP LICE I.A.W. SRM. 53-2-2 FIG. 10 2 L 7 4 4F RT 4A25 2002112200112 20021122 00112 WP 2002 11 22 UPS02839694 1 20020929 A 5340 DC853B00939 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, STA. 1600-1620 LONGERON 36 AND END FITTING ARE CORRODED BEYOND LIMITS. REMOVED, FABRICATED,AND REPLACED LONGERON SECTION AND END FITTING I.A.W. DWG. DC8-53B-009-39,AND SRM. 53-2-2 FIG. 10 2 L 7 4 4F RT 4A25 2002112200113 20021122 00113 WP 2002 11 22 UPS02839695 1 20020926 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, REMOVE STEEL DOUBLER FROM R-2 DOOR UPPER AFT CORNER AND REPAIR PER SRM. AT STA. 1660 LONG. 11RT. REMOVED EXISTING REPAIR, CUTOUT DAMAGED AREA,NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRI PLER AND FILLER I.A.W. SAA SK 729-895 AND EO DC8-5330-17661-A. 2 L 7 4 4F RT 4A25 2002112200114 20021122 00114 WP 2002 11 22 UPS02839697 1 20020924 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, AFT LOWER CARGO STA 1420 LONGERON 22 RT CORRODED AND CRACKED. CUTOUT DAMAGED AREA OF LONGERON, LOCATED DRILLED, & DEBURRED NEW SECT OF LONGERON & 2 EA SPLICE FITTING IAW DC8 SRM 53-2-2 FIG 4. ALODINED AND PR IMED I AW DC8 SRM 51-1-8. INSTALLED NEW SECT OF LONG & 2 EA SPLICES I AW DC8 SRM 53-2-2 FIG 4 2 L 7 4 4F RT 4A25 2002112200115 20021122 00115 WP 2002 11 22 UPS02839698 1 20020924 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, CABIN INTERCOSTAL CRACKED AT FWD END FS 960 S-5 BLENDED AREA AND FOUND TO BE IN LIMITS IAW DC8 SRM 53-2-0 ALODINED A ND PRIMED IAW DC8 SRM 51-10-8 INSTALLED FASTNERS IAW DC8 SRM 51-1-21 D 2 L 7 4 4F RT 4A25 2002112200116 20021122 00116 WP 2002 11 22 UPS02839699 1 20020920 A 5313 563932743 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, LONGERON CRACK AT STA 1767 AT L17L ACCESS THRU DOOR 60. REMOVED & REPLACED LONGERON PN 5639327- 43 IAW DC8 SRM 51-1-20D AND 5 1-1-21 2 L 7 4 4F RT 4A25 2002112200117 20021122 00117 WP 2002 11 22 UPS02839700 1 20020920 A 5313 564932744 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, LONGERON CRACK AT STA 1767 L17R ACCESS THRU DOOR 60. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-20D AND 51-1-21 2 L 7 4 4F RT 4A25 2002112200118 20021122 00118 WP 2002 11 22 UPS02839701 1 20021003 A 5315 9754022504A FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, FWD PIT FS 340 RT FLOORBEAM END FITTING CRACKED. REMOVED AND REPLACED CRACK FITTING P/N 67540 22-504A IAW DC8 SRM 51-1 -20D AND 51-3-0 2 L 7 4 4F RT 4A25 2002112200119 20021122 00119 WP 2002 11 22 UPS02839702 1 20020916 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, R-1 DOOR CORNER DOUBLER IS STEEL UPPER FWD. REMOVED STEEL DOUBLER IAW DC8 SRM 53-2-0 AND TRIMM ED CRACK AREAS IAW DC8 SRM 53-2-0 FABBED FILLER AND 2 EA DOUBLERS IAW DC8 SRM 53-2-0 A LODINED & PRIMED IAW DC8 SRM 51- 1-8 INSTALLED IAW DC8 SRM 51-1-20D A ND 51-1-21 PREFORMED HF-TEST TO LOCATE CRACKS 2 L 7 4 4F RT 4A25 2002112200120 20021122 00120 WP 2002 11 22 UPS02839703 1 20020929 A 5210 DOUBLER DOUG DC8 DC871F 302199D WP PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, L2 DOOR UPPER FWD CORNER HAS CRACK IN EXISTING DOULBER REPAIR. REMOVED CRACKED DOUBLER AND INST ALLED NEW DOUBLER IAW DC8 SRM 52-2-0 2 L 7 4 4F RT 4A25 2002112200121 20021122 00121 NM 2002 11 22 HNAA0200082 1 20021120 A 5310 85311176 ATTACH FITTING DHAV DHC8 DHC8102 2809003 NM A HNAA O OTHER O OTHER IN INSP/MAINT 1 EA 07 938HA 36536 152 During A-check inspection a crack was found in the NLG drag strut actuator fitting. The fitting was changed. 2 H 7 2 4T RT A13NM 2002112200122 20021122 00122 WP 2002 11 22 UPS02839704 1 20021002 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, AFT PIT FS 1160 RAMP PANEL SUPPORT FITTING CORRODED AT LONGERON 36 REMOVED SUPPORT LOCATED A ND DRILLED NEW SUPPORT IAW DC8 SRM 51-1-24 INSTALLED SUPPORT IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002112200123 20021122 00123 WP 2002 11 22 UPS02839705 1 20020920 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C1, REPAIR DOUBLER 744-2L-01 DETERMINED TO BE CATEGORY B WITH HIDDEN ROWS (ALSO DOUBLER IS STEEL) FS 415-423 LONG 20L-21L REMOVED EXISTING DOUBLER, CUTOUT DAMAGED SECTION OF SKIN IAW REO G08 800 FABRICATED REPAIR DOU BLER, TRIPLER, FILLER IAW REO G08800 ALODIN ED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED NEW DOUBLER, TRIPLER, FILL ER IAW REO G08800 2 L 7 4 4F RT 4A25 2002112200124 20021122 00124 WP 2002 11 22 UPS02839777 1 20020927 A 5240 INTERCOSTAL DOUG DC8 DC871F 302199D WP RT AFT SERVICE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, R-2 AFT RT SERVICE DOOR INTERCOSTAL IS CRACKED AT STA. 1630 AT LONG. 14R APPROX. REMOVED CRACK ED INTERCOSTAL SECTION,FABRICATED REPLACEMENT SECTION, DOUBLERS AND INSTALLED I.A.W. SRM. 52-2-0 FIG.2 2 L 7 4 4F RT 4A25 2002112200125 20021122 00125 WP 2002 11 22 UPS02839778 1 20020926 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, DOUBLER & TRIPLER REPAIR DOES NOT CONFORM TO SRM. ON L-2 DOOR UPPER AFT CORNER STA. 1660 LONG. 11L APPROX. REMOVED EXISTING REPAIR,NDT EXISTING CUTOUT AND VERIFIED NO CRACKS, FABRICATED AND INSTALLED DOUBLER,TRIPLE R AND FILLER I.A.W SRM.53-2-0 FIG. 18 2 L 7 4 4F RT 4A25 2002112200126 20021122 00126 WP 2002 11 22 UPS02839779 1 20020929 A 5230 INTERCOSTAL DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, C-PIT DOOR HAS A CRACKED INTERCOSTAL ABOVE LOWER DOOR HOOK AT STA. 1176 AT LONG. 32R AREA ON DOOR. CUTOUT CRACKED INTERCOSTAL, FABRICATED INTERCOSTAL SECTION, AND DOUBLER I.A.W. SRM. 52-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2002112200127 20021122 00127 WP 2002 11 22 UPS02839780 1 20021008 A 5210 INTERCOSTAL DOUG DC8 DC871F 302199D WP PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, R-1 FWD. SERVICE DOOR HAS INTERCOSTAL CRACKED UPPER AFT CORNER AFT SIDE OF INNER WEB STA. 200-220 LONG. 13R REMOVED INTERCOSTAL,FABRICATED DOUBLER AND FILLER AND INSTALLED I.A.W. SRM. 53-2-0 FIG. 23 2 L 7 4 4F RT 4A25 2002112200128 20021122 00128 WP 2002 11 22 UPS02839781 1 20020926 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, REMOVED STEEL DOUBLER FROM R-1 DOOR UPPER AFT CORNER AND REPAIR PER SRM. 53-2-0 FIG. 14. REMOVED EXISTING DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLE R I.A.W SRM 53-2-0 FIG. 14 2 L 7 4 4F RT 4A25 2002112200129 20021122 00129 WP 2002 11 22 UPS02839782 1 20020930 A 5320 FINGER DOUBLER DOUG DC8 DC871F 302199D WP COCKPIT SUBFLOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, STA. 8 TO -25 AT LBL 60 FINGER DOUBLER IS CORRODED BEYOND LIMITS REMOVED,FABRICATED AND INSTAL LED DOUBLER I.A.W. DWG.5612298,AND SRM. 51-1-21,51-1-20D 2 L 7 4 4F RT 4A25 2002112200130 20021122 00130 WP 2002 11 22 UPS02839783 1 20021003 A 5230 FRAME DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, A-PIT DOOR FRAME IS CRACKED ABOVE BOX WEB STA. 300 AT LONG. 31R REMOVED,FABRICATED AND INSTA LLED FRAME SECTION,DOUBLER AND INSTALLED I.A.W. SRM. 52-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2002112200131 20021122 00131 WP 2002 11 22 UPS02839784 1 20021007 A 5330 FILLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, SEVERAL STRESS FASTENERS AT STA. 1660 LONG. 31 RT. OPENED SKIN FOUND FILLER CORRODED BEYOND LIMI TS, FABRICATED AND REPLACED FILLER IAW DWG. 5773311,AND CLOSED SKIN I.A.W. SRM. 51-1-21,51-1-20D 2 L 7 4 4F RT 4A25 2002112200132 20021122 00132 WP 2002 11 22 UPS02839785 1 20020926 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, REMOVE STEEL DOUBLER FROM L-2 DOOR LOWER FWD. CORNER STA. 1620 LONGERON 20L-21L. REMOVED EXISTI NG REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SAA SK729-250,AND SRM 53-2-0 FIG. 18 2 L 7 4 4F RT 4A25 2002112200133 20021122 00133 WP 2002 11 22 UPS02839786 1 20020928 A 5511 RIB DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, LT HORIZONTAL STAB L/E LOWER RIB IS CRACKED AT XFS 116.25. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM. 55-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2002112200134 20021122 00134 WP 2002 11 22 UPS02839787 1 20020926 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, FUSELAGE SKIN IS CRACKED AT STA 1746 BELOW DOUBLER ABOVE LONGERON 16LT. REMOVED DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLERS, AND FINGER DOUBLER I.A.W. SAA SK729 -255 2 L 7 4 4F RT 4A25 2002112200135 20021122 00135 WP 2002 11 22 UPS02839788 1 20020930 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, STA. -12 TO -32 INTERCOSTAL BEAM IS CRACKED AT LBL 12 CUTOUT DAMAGE,FABRICATED AND INSTALLED R EPAIR DOUBLER I.A.W. SRM. 53-2-0 FIG. 1B 2 L 7 4 4F RT 4A25 2002112200136 20021122 00136 WP 2002 11 22 UPS02839789 1 20020926 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, REMOVE STEEL DOUBLER FROM L-1 DOOR UPER AFT CORNER AND REPAIR PER SRM. 53-2-0 FIG. 15. REMOVED EX ISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER I AW SRM. 53-2-0 FIG. 15 2 L 7 4 4F RT 4A25 2002112200137 20021122 00137 WP 2002 11 22 UPS02839790 1 20021012 A 5320 ATTACH ANGLE DOUG DC8 DC871F 302199D WP BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, INTERCOSTAL TO AFT PRESSURE BULKHEAD ATTACH ANGLE IS CRACKED AT LONGERON 5L AT STA. 1766. RE MOVED, FABRICATED AND REPLACED ANGLE IAW DWG.5773844,AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2002112200138 20021122 00138 NM 2002 11 22 HNAA0200083 1 20021121 A 5610 NP5790111 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM CRACKED A HNAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 07 927HA 18836 117 L/H Forward Sindshield shattered in flight at 16,000 FT. A/C diverted to GSP the windshield fram was inspected and the windscreen replaced. 2 H 7 2 4T RT A13NM 2002112200139 20021122 00139 NM 2002 11 22 FL3A200200389 1 20021116 A 3600 M9131 CHECK VALVE BOEING 737 7372Y5 1384554 NM FUSELAGE INOPERATIVE A F3LA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 118RW 61015 23040 DURING CLIMB OUT, THE FLIGHT CREW NOTED AN ILLUMINATED WING/BODY OVERHEAT LIGHT WHICH WOULD NOT EXTINGUISH WHEN QUICK RE FERENCE HANDBOOK ITEMS WERE ACCOMPLISHED. THE AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT.MAINTENANCE REMOVED AND REPLAC ED THE START MANIFOLD CONNECTION CHECK VALVE IN ACCORDANCE WITH THE REQUIREMENTS OF MM 21-21-15. 2 L 7 2 4U RT A16WE 2003012900160 20030129 00160 NM 2003 1 29 QXEA0201970 1 20021120 A 2910 DSC252B40124 HYDRAULIC LINE DHAV DHC8 DHC8202 2809007 NM HYD SYSTEM BROKEN A QXEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 360PH 10779 10779 515 PDX- RETURNED TO FIELD DUE TO NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT IS ILLUMINATED. NR 2 HYDRAULIC QUANTITY INDICATO R IS ZERO. AIRCRAFT WAS FLOWN WITH ZERO FLUID FOR 50 MINUTES. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE DRIVEN PUMP, CASE DRAIN FILTER AND BROKEN RIGHT HAND NOSE LANDING GEAR DRAG STRUT ACTUATOR HYDRAULIC LINE. OPERA TIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002112200140 20021122 00140 NM 2002 11 22 QXEA0201971 1 20021120 A 6120 697073002 PITCH CONTROL BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 INOPERATIVE A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 402QX 3505 3505 4032 MFR-#2 PROP RPM INCRREASED TO 1020 (UNCOMMANDED) FROM 900 CONTROL LEVER SETTING. INCREASED BOTH PROPS TO 1020 THEN RESET TO 900 THEN 850, #2 PROP INCREASED AGAIN TO 1020. FEATHERED #2 PROP. REMOVED AND REPLACED #2 PITCH CONTROL UNIT. OPERAT IONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002112200141 20021122 00141 WP 2002 11 22 UPS02839875 1 20021013 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 AFT ACCESSORY COMPT AT STA 1620 LONG 25R FRAME HAS CORROSION. REMOVED CORRODED FRAME SPLICE IAW DC8 SRM 51-1-20D. LOCATED AND DRIL LED NEW SPLICE IAW DC8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002112200142 20021122 00142 WP 2002 11 22 UPS02839876 1 20021012 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 AIR COND/PRESS COMPT AT FS 56 ABOVE L24L FRAME IS CRACKED AT A/C DUCT STANDOFF ATTACH BRACKET. REMO VED FRAME SECTION, FAB NEW FRAME SECTION AND SPLICE IAW DC8 SRM 53-2-0, INSTALLED FRAME SECTION AND SPLICES IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002112200143 20021122 00143 WP 2002 11 22 UPS02839877 1 20021012 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 A/C PRESS COMPT AT FS 56 AT L24R FRAME IS CRACKED AT AC DUCT STANDOFF ATTACH BRACKET. FABRICATED NE W FRAME SEGMENT AND SPLICES IAW DC8 SRM 53-2-0. INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002112200150 20021122 00150 EA 2002 11 22 COMA0260657 1 20021120 A 2613 355924400 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA R/H PYLON MALFUNCTIONED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 739CA 7273 FLIGHT 9494 R/H 14TH STAGE BLEED AIR DUCT WARNING.REPLACED THE R/H PYLON SECTION OF BLEED AIR LEAK SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2002112200151 20021122 00151 EA 2002 11 22 COMA0260658 1 20021121 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA D O RETURN TO BLOCK OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 807CA 7364 FLIGHT 5394 FLAPS FAIL MESSAGE DURING TAXI.RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002112200152 20021122 00152 EU 2002 11 22 02325324 1 20021121 A 3350 1317 LAMP JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 324UE 41017 During overnight maintenance, it was discovered that the L/H aft emergency exit light was inoperative. Maintenance pers onnel removed and replaced the lamp in the L/H aft emergency exit light. An operational check was satisfactory and the aircraft was returned to serivice. 2 L 7 2 4T RT A41NM 2002112200153 20021122 00153 NM 2002 11 22 249TR0008 1 20021111 A 3350 1000679 LIGHT BOEING 737 7372K5 138448X NM A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 L2 emergency exit overhead light inop. Removed and replaced L2 overhead emergency exit light. Ops chk OK. 2 L 7 2 4F RT A16WE 2002112200154 20021122 00154 EA 2002 11 22 COMA0260659 1 20021119 A 3040 2315M1082 WINDSHIELD WIPER CNDAIR CL600 CL6002B19 1900309 EA R/H BROKEN A COMA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 SO 01 713CA 7245 FLIGHT 5080 COPILOTS WINDSHIELD WIPER CAME APART DURING T/O.REPALCED WIPER BLADE ASSY. 2 L 7 2 4F RT A21EA 2002112200155 20021122 00155 WP 2002 11 22 UPS02839808 1 20021022 A 2510 56410351 SEAT DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:N/A FE SEAT WILL NOT LOCK IN POSITION. R&R SEAT OPS CK GOOD W/REF TO MM 25-11-02. 2 L 7 4 4F RT 4A25 2002112200156 20021122 00156 WP 2002 11 22 UPS02839810 1 20021014 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 AFT CARGO PIT AT FS 1160 BETWEEN L33R-L34R Z FITTING IS CRACKED. REMOVED CRACKED Z FITTING TO FOM. RECEIVED NEW Z FITTING. FABBED FILLER IAW DC8 SRM 53-2-0 FIG 20. LOCATED DRILLED DEBURRED NEW FITTING IAW DC8 SRM 53- 2-0 FIG 20. 2 L 7 4 4F RT 4A25 2002112200157 20021122 00157 WP 2002 11 22 UPS02839814 1 20021013 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 AFT ACCESSORY COMP AT STA 1660 FLOORBEAM ABOUT BL20 HAS CORROSION AND MISSING 4 EA ATTACHING BOLTS. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. REMOVED DAMAGED AREA & FABBED 1 EA FILL ER & 2 EA REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 1B. INSTALLED FILLER AND REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2002112200158 20021122 00158 WP 2002 11 22 UPS02839815 1 20021014 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 AFT CARGO PIT AT FS 1150-1160 BETWEEN L35L-35R SKIN IS CORRODED. REMOVED EXISTING FITTING, LOCATE, DRILL & DEBURRED NEW FITTING AND FABRICATED DRILLED REPAIR SPLICES, AND INSTALLED FITTING AND REPAIR SPLICES IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002112200159 20021122 00159 WP 2002 11 22 UPS02839816 1 20021022 A 5347 3657503501 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 2ND OBSERVER'S FWD SEAT TRACK LOCK PIN HOLES WORN. REMOVED OLD SEAT TRACK IAW DC8 SRM 51-3-0. DRIL LED NEW SEAT TRACK IAW DC8 SRM 51-1-24. INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2002112200160 20021122 00160 WP 2002 11 22 UPS02839817 1 20021015 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 LT WING LOWER WING SKIN, O/B OF FUEL VENT PANEL, FWD OF REAR SPAR, IS CORRODED ON EXTERIOR SURFACE. CUT OUT DAMAGE, FABRICATED DOUBLER AND FILLER IAW REO G08852 AND DC8 SRM 57-2-0 FIG 2A, AND INSTALLED DOUBLER REPAIR IA W REO G08852 AND DC8 SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 2002112200161 20021122 00161 WP 2002 11 22 UPS02839878 1 20021013 A 5312 PRESSURE PANEL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 LT MLG W/W INBD WEB CRACKED ABOUT KEELBEAM AS STA 906.00 TO 910.00, JUST AFT OF MLG DOOR ACTUATOR MO UNT FITTING. CUT-OUT DAMAGED SECTION OF WEB IAW DAC DWG 5754125, FABBED AND LOCATED AND DRILLED REPAIR PARTS IAW DAC DW G 5614943 & 5754125, INSTALLED REPAIR IAW DAC DWG 5614943 & DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2002112200162 20021122 00162 WP 2002 11 22 UPS02839880 1 20021016 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 AFT ACCY COMPARTMENT FS 1680 AT LBL 48 LOWER SURFACE OF UPPER FLOORBEAM FLANGE IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, BEYOND LIMITS IAW DC8 SRM 53-2-0 FIG 1F. FABRICATED REPAIR ANGLES AND FILLER IAW DC8 SRM 53-2-0 FIG 1B SHEET 3. INSTALLED IAW DC8 SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 2002112200163 20021122 00163 WP 2002 11 22 UPS02839881 1 20021018 A 5720 3704841502 FITTING DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 LT WING STR 51 I/B END, STR END FITTING CRACKED. RECEIVED NEW FITTING LOCATED AND DRILLED IAW DC8 S RM 51-1-24. INSTALLED IAW DC8 SRM 51-3-0 & 51-1-20D. 2 L 7 4 4F RT 4A25 2002112200164 20021122 00164 WP 2002 11 22 UPS02839882 1 20021021 A 5720 3704841502 FITTING DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 LT WING STR 51, O/B FWD STRINGER END FITTING IS CRACKED. RECEIVED NEW FITTING LOCATED & DRILLED FIT TING IAW DC 8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2002112200165 20021122 00165 WP 2002 11 22 UPS02839883 1 20021010 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 L2 DOOR JAMB LOWER FWD AND AFT CORNERS HAVE A REPAIR THAT DIFFERS FROM SRM. REMOVED AND REPLACED SK IN FROM STA 1642 TO 1690 IAW DAC DWG 5615775 AND 5750985. REPAIRED FWD LOWER CORNER IAW REO G08850. 2 L 7 4 4F RT 4A25 2002112200166 20021122 00166 WP 2002 11 22 UPS02839884 1 20021010 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 R2 DOOR JAMB LOWER FWD AND AFT CORNERS HAVE A REPAIR THAT DIFFERS FROM SRM. REMOVED AND REPLACED SK IN STA 1642 TO 1690 IAW DAC DWGS 5772776 AND 5772656. REPAIRED LOWER FWD CORNER IAW REO G08849. 2 L 7 4 4F RT 4A25 2002112200167 20021122 00167 WP 2002 11 22 UPS02839886 1 20021014 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 R2 AFT SERVICE DOOR, UPPER AFT CORNER HAS CRACK INDICATION BETWEEN FASTENERS FOUND BY RADIOGRAPHIC I NSPECTION. TRIMMED OUT CRACKED AREA. FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW DC8 SRM 53-2-0 FIG 16. 2 L 7 4 4F RT 4A25 2002112200168 20021122 00168 WP 2002 11 22 UPS02839887 1 20021012 A 5320 47723591 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 FWD CARGO PIT ATTACH FITTING FOR MAIN CABIN FLOORBOARD CRACKED ON FWD SIDE OF FLOORBEAM STA 160 BL 0 . FABRICATED ONE FITTING IAW DC8 DWG 4772359, LOCATED HOLES AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2002112200169 20021122 00169 WP 2002 11 22 UPS02839888 1 20021016 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C-2 MAIN CABIN AT FS 1655 LONGERON 11R IS CRACKED. REMOVED AND REPLACED LONGERON PER DC8 SRM 51-1-21 AN D 51-1-20D. 2 L 7 4 4F RT 4A25 2002112200170 20021122 00170 WP 2002 11 22 UPS02839899 1 20021111 A 3350 6012233 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:ASV EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, CKS OK. 2 L 7 4 4F RT 4A25 2002112200171 20021122 00171 WP 2002 11 22 UPS02839921 1 20021118 A 3350 5708458503 BATTERY DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:N/A DURING BITE CHECK, EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. RECYCLED BREAKER AND CHECK AGAIN. E MERGENCY LIGHTS DID NOT ILLUMINATE SECOND TIME. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER MM 33-50-01 OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2002112200172 20021122 00172 WP 2002 11 22 UPS02839923 1 20021119 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:PFLT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS CK OK. 2 L 7 4 4F RT 4A25 2002112200173 20021122 00173 NM 2002 11 22 UPS02M39589 1 20020809 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP INSPECTION TYPE:C CABIN SEAT TRACK HAS CORROSION AT STA 1351-1361 X=-75.25. SEAT TRACK AT STA 1351-1361 CORROSION EXCEE D LIMITS PER SRM 53-70-00 FIG3 VOL1 REV31. SEAT TRACK FABRICATED & REPLACED FROM STA 1260 TO 1391 AS PER SRM53- 70-00 F IG1 VOL1 REV31. 2 L 7 3 4F RT A22WE 2002112200174 20021122 00174 NM 2002 11 22 UPS02M39590 1 20020807 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP INSPECTION TYPE:C CABIN SEAT TRACK CORRODED FROM STA1321 TO 1361X=75.25 & TRACK JOINER AT STA1351X=75.25. SEAT TRACK AT STA 1321 TO STA1361,X=75.25 & STA1351,X=75.25 EXCEEDED LIMIT AS PER SRM 53-70-00 FIG3 VOL1 REV31. SEAT TRACK FABRICATE D & REPLACED FROM STA 1260 TO STA1391,X=75.25 AS PER SRM53-70-00 FIG1 VOL1 REV31. 2 L 7 3 4F RT A22WE 2002112200175 20021122 00175 NM 2002 11 22 UPS02M39791 1 20021017 A 3350 LIGHT DOUG MD11 MD11F 3023600 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 251UP INSPECTION TYPE:ASV EMERGENCY LIGHT OVER LT ENTRY DOOR INOP. RELAMPED, OPS OK. 2 L 7 3 4F RT A22WE 2002112200176 20021122 00176 NM 2002 11 22 UPS02M39835 1 20020822 A 5347 S49291487075T SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP INSPECTION TYPE:C CABIN - SEAT TRACK CROWN HAS CORROSION AT STA 1361 X=107.25. SEAT TRACK BADLY CORRODED, EXCEEDED LIMI TS IAW SRM 53-70-00 FIG 3 VOL 1 REV 31. NEW SEAT TRACK, SPLICE HAT REWORKED, SPLICE PLATE FABRICATED AND INSTALLED PER SRM 53-70-00 FIG.1 VOL 1 REV 31. 2 L 7 3 4F RT A22WE 2003020700151 20030207 00151 EU 2003 2 7 DHL2002362519 1 20021122 A 5754 SKIN AIRBUS 300 A300B4203 3930306 EU LE SLAT GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 RT OUTBOARD SLAT ABOVE NR 2 PYLON T/E HAS ONE GOUGE. EDDY CURRENT INSPECTED AREA AFTER CUTOUT DUE TO GOUGE OUT OF LIMIT S. NO CRACKS FOUND. FABRICATED EDGE FILLER, INNER DOUBLERS AND FILLER IAW A300 SRM 57-58-12. 2 L 7 2 4F RT A35EU 2003020700155 20030207 00155 EU 2003 2 7 DHL2002362520 1 20021112 A 5730 SKIN AIRBUS 300 A300B4203 3930306 EU RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 RT UPPER WING HAS ONE FASTNER WITH CORROSION AROUND IT AT RIB 4 AND APPOX 1 INCH AFT OF THE REAR SPAR AREA. REMOVED COR ROSION, FOUND TO BE OUT OF LIMITS. EDDY CURRENT INSPECTED PER NTM 51-31-05, NO CRACKS FOUND. FLAP PEENED AREA IAW A300 S RM 51-40-19. ALODINED AND PRIMED AREA IAW A300 SRM 51-40-18 AND 51-40-12. FILLED BLEND DEPRESSION WITH SEALENT IAW A300 SRM 51-40-20. ALL WORK PERFORMED IAW A300 SRM AND RAS/BAE/1338/2002, REPAIR IS GOOD UNTIL NEXT C-CHECK. 2 L 7 2 4F RT A35EU 2003021000026 20030210 00026 NM 2003 2 10 DHL2002743505 1 20021013 A 5313 STRINGER BOEING 727 727225 1384077 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, IN MAIN CARGO BETWEEN BS 720B AND 720C, STR 15L IS CRACKED AFT OF WING LIGHT HOUSING. CUT-OUT CRACKED SECTION OF STR 15L IAW B-727 SRM 53-10-3. FABRICATED ONE CHANNEL REPAIR. FABRICATED ONE FILLER. FABRICATED ONE FILLER IAW B-727 SRM 53-10-3. TREATED AND PRIMED AND INSTALLED IAW B-727 SRM CHAPTER 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2003021000027 20030210 00027 NM 2003 2 10 DHL2002743506 1 20021112 A 5311 FRAME BOEING 727 727225 1384077 NM AFT CARGO BAY BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, STA. 950F FRAME IS BENT AND BUCKLED AT STR. 26 LT IN AFT CARGO BAY. CUT-OUT DAMAGE FRAME IAW B-727 SRM 53-10-4. FABRICATED REPAIR ANGLE IAW B-727 SRM 53-10-2. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED REPAIR ANGLE IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2003021000028 20030210 00028 NM 2003 2 10 DHL2002743507 1 20021108 A 5313 STRINGER BOEING 727 727225 1384077 NM LIGHTNING STRIKE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, LIGHTNING STRIKE AT STA. 227 STR. 19 LT. CHEMICALLY REMOVED PAINT FOR ACCESS MM 51-20-1, BLENDOUT IAW B-727 SRM 53-30-1. MATERIAL LOSS FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1. CUT-OUT DAMAGE AREA, FABRICATED DOUBLER IAW B-727 SRM 53-30-3. PART ALODINED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED DOUBLER IAW B-727 SRM 53-30-3. 2 L 7 3 4F A3WE 2002121800028 20021218 00028 NE 2002 12 18 UPS02639924 2 20021121 A 7200 ENGINE BOEING 767 767300 1385204 NM GE CF6 CF680C2B7 NE NR 2 FAILED A IPXA C ABORTED TAKEOFF Y ENGINE STOPPAGE TO TAKEOFF 1 SO 01 312UP 27763 RT ENGINE FAILURE ON TAKE OFF. REPLACED NR 2 ENGINE, TESTED AND OPERATED NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2002112500001 20021125 00001 WP 2002 11 25 UPS02839793 1 20020927 A 5730 SKIN DOUG DC8 DC871F 302199D WP LEFT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, LT WING UPPER SKIN IS CRACKED AT XRS AT STRINGER 9 CUTOUT CRACKED AREA,NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM. 57-2-1 FIG. 10 2 L 7 4 4F RT 4A25 2002112500002 20021125 00002 WP 2002 11 25 UPS02839794 1 20020926 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, FUSELAGE SKIN HAS 2 CRACKS AT CANTED FRAME 1702 AT LONGERON 17L AT STATION 1740. CUTOUT CRACKED AR EA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SAA SK 729-255 2 L 7 4 4F RT 4A25 2002112500003 20021125 00003 WP 2002 11 25 UPS02839796 1 20020926 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, REMOVE STEEL DOUBLER FROM L-1 DOOR UPPER FWD CORNER CUTOUT AND REPAIR PER SRM. 53-2-0 FIG. 15. RE MOVED EXISTING REPAIR, NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM.53-2-0 FI G. 15 2 L 7 4 4F RT 4A25 2002112500004 20021125 00004 2002 11 25 UPS02839800 4 20021021 A 2565 SLIDE DOUG DC8 DC873F 302199F WP MAIN CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 852UP 46052 MAIN CABIN EXIT SLIDE INOP M247198. REPLACED SLIDE CONTAINER AND SLIDE PER MM-25-60-01 2 L 7 4 4F RT 4A25 2002112500005 20021125 00005 WP 2002 11 25 UPS02839801 1 20021018 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 818UP 46108 EMERGENCY LIGHTS FAILED OP CHECK. REMOVED AND REPLACED BATTERY PACK. 2 L 7 4 4F RT 4A25 2002112500006 20021125 00006 WP 2002 11 25 UPS02839804 1 20020929 A 5230 5754260U7 ANGLE DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C2, CARGO DOOR HAS FWD ANGLE UNDER SEAL AREA, CRACKED AT STA 280 BETWEEN LONG 28 TO 31 RT. REMOVED AND REPLACED ANGLE IAW DWG 5754260,AND SRM. 51-1-21 2 L 7 4 4F RT 4A25 2002112500007 20021125 00007 WP 2002 11 25 UPS02839807 1 20021019 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 818UP 46108 OPS CK OF EMERGENCY LIGHTS FAILED TO LIGHT UP GLARESHIELD COCKPIT DOME, LAV / COURIER DOME, FWD ENTRANCE. REPLACED EMER GENCY LIGHT BATTERY PACK OPS CK GOOD. 2 L 7 4 4F RT 4A25 2002112500008 20021125 00008 WP 2002 11 25 UPS02839879 1 20021015 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE: C-2, R-1 FORWARD SERVICE DOOR CUTOUT, UPPER FORWARD CORNER HAS CRACK INDICATION ON EXTERNAL SKIN. FA BRICATED -23 FILLER, -15 AND -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 1 4. ALODINED AND PRIMED FILLER AND DOUBLERS IAW DC8 SR M 51-1-8. INSTALLED -15, -17 DOUBLER AND -23 FILLER IAW DC8 SRM 53-2-0 FIG 14. INSTALLED UPPER FWD AND CENTER WEBS IAW D C8 SRM 51-1-20D, 51-1-21 2 L 7 4 4F RT 4A25 2002112500009 20021125 00009 WP 2002 11 25 UPS02839890 1 20021025 A 5710 36440462 STRAP DOUG DC8 DC871F 302199D WP NR 4 ALT TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE: C2, RT WING HAS A CRACKED LONGERON 64 END FITTING-STRAP, AND LOWER SPAR IS CRACKED 1/2 INCH FROM EDGE OF SPAR TO FASTENER HOLE AT XRS 450. NDT VERIFIED 1/2 INCH CRACK AT XRS 450 FROM EDGE OF SPAR TO FASTENER HOLE, REMOVED , FABRICATED AND INSTALLED REPLACEMENT STRAP IAW DWG. 3644046 AND OVERSIZED HOLE AT CRACK LOCATION AND INSTALLED FASTENE R AND STRAP IAW SAA SK 779-634 AND UPS EO DC8-5710-17626-A. 2 L 7 4 4F RT 4A25 2002112500010 20021125 00010 WP 2002 11 25 UPS02839925 1 20021118 A 5310 FINGER DOUBLER DOUG DC8 DC871F 302199D WP FWD A/C DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE: LNSV, RIVET POPPED ON RT FWD SECTION OF FUSELAGE NEXT TO D10 CONDITIONED AIR DOOR. REMOVED POPPED RIV ET AT STA 8 AND FOUND FINGER DOUBLER SEVERLY CORRO DED. FABBED NEW FINGER DOUBLER IAW DAC DWG 5613862 MATERIAL ID 02570 75T6 PO 0349922 IAW DAC DWG 5613862 ALODINED & PRIMED IAW DC8 SRM 51 -1-8 AND INSTALLED FINGER DOUBLER IAW DC8 SRM 51-1- 21 & 51-1-20D 2 L 7 4 4F RT 4A25 2002112500011 20021125 00011 NM 2002 11 25 UPS02M39420 1 20020811 A 5320 DOUBLER DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP INSPECTION TYPE: C, STA 1905 STR 27 RT, SHEAR WEB LOWER SURFACE, CORRODED APPROXIMATELY 4 SQ INCHES WHERE INDICATED. RT WEB LOWER DOUBLER STA 1905, STR 27 RT, BADLY CORRODED & EXCEEDS LIMITS IAW SRM 53-00-01. REMOVED PER SRM 51-31-0 1. NEW DOUBLER FABRICATE IAW AGA3807. NEW DOUBLER PAINTED PER SRM51-21-01. NEW DOUBLER AND SURROUNDING FASTENERS I NSTALLED IAW SRM 51-31-01 VOL II REV 31. 2 L 7 3 4F RT A22WE 2002112500026 20021125 00026 CE 2002 11 25 A592002F00000 1 20021028 A 3211 08411132 BRACE CESSNA 310 310R 2074245 CE CONT O520 IO520* 17032 SO RT MLG BROKEN E A59A K NONE O OTHER IN INSP/MAINT 1 GL 17 22DM 15426 310R0069 RIGHT MAIN LANDING GEAR LOWER SIDE BRACE LOCK ASSEMBLY WORN EXCESSIVELY, CAUSING ADJUSTING SCREW PIN TO CARRY WEIGHT OF AIRCRAFT, ADJUSTING SCREW THEN BEANT AND BROKE. RECOMMEND INSPECTING LOWER SIDE BRACE LOCK ASSEMBLY FOR WEAR. 1 L 7 2 3O 3 O 3A10 E5CE 2002112500028 20021125 00028 2002 11 25 F2P2002F00001 4 20021106 A 2330 FRC1200 SPEAKER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA ENTERTAINMT SYS BURNED E F2PA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 17 888JJ 1826 99070143 317852078 PILOT NOTICED SMOKE AND FIRE IN CABIN DURING CLIMBOUT. PILOT DECLARED EMERGENCY, SHUT OFF ALL ELECTRIC POWER AND LANDED AIRCRAFT, WITHOUT FURTHER INCIDENT, NO PASSENGERS ON BOARD. FOUND PASSENGER ENTERTAINMENT SPEAKER LOCATED RIGHT SIDE PAX CABIN AT STATION 209, BURNED OUT. FIRE DAMAGE TO SURROUNDING INTERIOR PANEL FABRIC APPROX 12 SQ INCHES AND ADJACENT PAX SEAT CUSHION. FOUND NO CIRCUIT PROTECTION DEVICES TRIPPED. FOUND 24 VOLTS TO ONE SIDE OF DAMAGED SPEAKER. INSPEC TED ENTIRE CIRCUIT WIRING , NO DEFECTS FOUND. ALL OTHER AIRCRAFT ELECTRIC SYSTEMS FUNCTION CHECK, OK. FAILURE OF THE S PEAKER AMP TO ALLOW 24 VOLTS TO SPEAKERS ALL EQUIPMENT HAS BEEN REMOVED AND WILL BE SENT TO MANUFACTURER FOR EVALUATION. 1 L 7 2 3O 3 O A20SO E14EA 2002112500029 20021125 00029 NM 2002 11 25 DL73K021318 1 20021113 A 5330 SKIN BOEING 737 737232 1384475 NM FS 986.5, S-27R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 FUSELAGE / SKIN / AFT LAV SERVICE CUTOUT / FS 986.5 / STRG. 27R : CORROSION CUTOUT REPAIR AN AREA OF CORROSION WAS FOUND IN THE SKIN AT THE FWD INBD CORNER OF THE AFT LAVATORY SERVICE DOOR CUTOUT. THE CORROSION WAS REMOVED WITH A 4" X 4" CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 384164-14, REV B. 2 L 7 2 4F RT A16WE 2002112500030 20021125 00030 NM 2002 11 25 DLM88021319 1 20021113 A 5340 591214186 ATTACH ANGLE DOUG MD88 MD88 3023688 NM STA 1474, RH CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 990DL 53342 FUSELAGE / VERT STAB TO FUSELAGE ATTACH ANGLE / RH : CRACK REPAIR THE RH VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE WAS FOUND WITH A CRACK NEAR CANTED FRAME STA. 1474. THE CRACK WAS .75" LONG IN THE HORIZONTAL FLANGE OF THE ANGLE AND WAS REMOVED WITH A TRIMOUT TO THE FLANGE. THE AREA WAS REPAIRED WITH A STEEL REPAIR ANGLE PER ER/A 384165-14, REV A. 2 L 7 2 4F RT A6WE 2002112500031 20021125 00031 NM 2002 11 25 DLM11021325 1 20021114 A 5510 ALC8132502 SPAR CAP DOUG MD11 MD11 3023602 NM XE 50 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 813DE 48600 HORIZ STABILIZER / RH / REAR SPAR / LOWER CAP : GROUND DAMAGE REPAIR THE RH HORIZONTAL STABILIZER REAR SPAR LOWER CAP STRUCK A WORK PLATFORM DURING A TOWING OPERATION. THE AFT FLANGE OF THE LOWER CAP WAS CRACKED BETWEEN XE 49 & 61. THE CRACK WAS REMOVED BY TRIMMING OFF THE AFT FLANGE OVER A 12" LENGTH. THE TRIMMED ARE WAS REPAIRED WITH AN ALUMINUM REPAIR ANGLE AND REPAIR STRAP PER ER/A 384119-14, REV A. 2 L 7 3 4F RT A22WE 2002112500032 20021125 00032 NM 2002 11 25 DL757021326 1 20021114 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FS 620, S-16L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 FUSELAGE / SKIN / FS 590-661 / STRG. 14L-19L : GROUND DAMAGE REPAIR THE FUSELAGE SKIN WAS FOUND WITH SEVERAL DENTS, GOUGES, AND SCRATCHES BETWEEN FS 590 & 661 AND BETWEEN STRINGERS 14L & 19L. THE SKIN WAS CUT AT FS 590 BETWEEN STRINGERS 14L & 19L AND THE AFT SECTION OF SKIN PANEL REMOVED. A NEW SECTION OF SKIN WAS SPLICED IN WITH AN INTERNAL AND EXTERNAL ALUMINUM DOUBLER PER ER/A 384081-14, REV A. 2 L 7 2 4F RT A2NM 2002112500033 20021125 00033 NM 2002 11 25 DL76L021332 1 20021116 A 5200 312540011 SQUIB BOEING 767 767332 1382001 NM RT INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 186DN 27962 IR - WHILE REACTIVATING OVERWING SLIDE SYSTEM DOING SQUIB TEST SHOWS RT SLIDE DOOR SQUIB INOP. ON INSPECTION FOUND SLIDE DOOR OPEN AND SQUIB BLOWN. CA - REPLACED R/H OVWG DOOR LATCH OPENING ACTUATOR PER AMM/6 _____ C/P STILL NEEDS TO BE CONNECTED./605396. CONNECTED OV_____ LATCH OPENING ACTUATOR ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2 L 7 2 4F RT A1NM 2002112500034 20021125 00034 NM 2002 11 25 DLM88021334 1 20021117 A 3350 41B004AD073 BATTERY DOUG MD88 MD88 3023688 NM ENTRY DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 945DL 49818 COCKPIT AND ENTRY OVERHEAD EMERGENCY LIGHTS INOP REPLD BATTERY PACK IN CEILING PWR SUPPLY ABOVE NEON AISLE LIGHT 2 L 7 2 4F RT A6WE 2002112500035 20021125 00035 NM 2002 11 25 DL73K021337 1 20021117 A 5330 6545775594 SKIN BOEING 737 737232 1384475 NM FS 727, S-19R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312DL 23084 FUSELAGE / SKIN / FS 727 / STRG. 19R : CRACK REPAIR THE FUSELAGE SKIN WAS FOUND WITH A 2.5" CRACK ALONG THE BONDED DOUBLER LINE AT STRINGER 19R. THE CRACK IS TYPICAL OF THOSE NOTED IN BAC S/B 737-53A1210. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER THE B737 SRM AND PER ER/A 384189-14. 2 L 7 2 4F RT A16WE 2002112500036 20021125 00036 NM 2002 11 25 DLM88021338 1 20021118 A 2130 39271411 VALVE DOUG MD88 MD88 3023688 NM AFT UNRELIABLE A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 910DE 53419 LOSS OF PRESSURIZATION, DECOMPRESSION GRADUAL. DESCENT BELOW 10,000 DIVERT TO BDL - REPLACED LEFT PRSOV 2 L 7 2 4F RT A6WE 2002112500037 20021125 00037 NM 2002 11 25 DL72S021343 1 20021119 A 5700 UNK ANGLE BOEING 727 727225A 1384077 NM NO.4 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 1/4IN CRACK AT NO.4 L/E SLAT LWR COVE SKIN ANGLE AT O/B STOP PAD REPAIRED PER MM 57-54-000-8 2 L 7 3 4F RT A3WE 2002112500038 20021125 00038 NM 2002 11 25 DL72S021344 1 20021119 A 5700 574203482 STIFFENER BOEING 727 727225A 1384077 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 NBR #3 SLATI/B ACT CASTING CRACKED AT FASTNER HOLE REMOVE AND REPLACE STIFFENER 2 L 7 3 4F RT A3WE 2002112500039 20021125 00039 NM 2002 11 25 DL733021347 1 20021120 A 5410 311A11112 BEAM BOEING 737 737347 1384647 NM PYLON WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 WORN AREAS WERE FOUND ON THE CROWN BEAM LUG BORES OF THE #1 AND #2 PYLONS. THE BORES WERE OVERSIZED TO 3.100" AND 3.102 RESPECTIVELY. REPAIR BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2002112500040 20021125 00040 NM 2002 11 25 DLM88021360 1 20021122 A 5200 591479261 DOOR DOUG MD88 MD88 3023688 NM AFT LAV SERVICE MISSING A DALA K NONE D INFLIGHT SEPARATION CR CRUISE 1 SO 27 908DL 49539 AFT LAV SERVICE DOOR NOT ON A/C UPON ARRIVAL DFW. INSPECTED A/C. NO DAMAGE NOTED OTHER THAN DOOR. REPLACE AFT LAV SERVICE DOOR. 2 L 7 2 4F RT A6WE 2002112500041 20021125 00041 SO 2002 11 25 FFS2002F00007 1 20021102 A 2140 A23D0475 VALVE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA FWD HEATER LEAKING A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 820FS 502 317952185 FOUND WHILE COMPLYING WITH AD. ON THIS ASSEMBLY, IT CAN BE SEEN THAT THE RED RUBBER VALVE DIAPHRAGM IS VISIBLE ON 3 SID ES ONLY. THE (IN) SIDE OF THE VALVE SHOWS THE DIAPHRAGM TO BE RECESSED PAST THE SEAL AREA OF THE CASTING. EITHER THE D IAPHRAGM WAS ASSEMBLED INCORRECTLY OR THE FASTENERS THROUGH THE VALVE BODY WERE OVER-TORQUED, MISSHAPING THE ADJUSTMENT CAP. CAP APPEARS TO BE WARPED, WHICH DOES NOT ALLOW DIAPHRAGM RUBBER TO SEAL. 1 L 7 2 3O 3 O A20SO E14EA 2002112500042 20021125 00042 EA 2002 11 25 JEM2002F00008 2 20021025 A 7200 THRU BOLT BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA ENG CASE LOOSE E JEMA K NONE O OTHER IN INSP/MAINT 1 CE 01 366EA BB841 PILOT REPORTED UNUSUAL NOISE COMING FROM LT ENGINE. TECH INVESTIGATED AND COULD NOT DETERMINE SOURCE OF NOISE. DECISIO N WAS MADE TO REMOVE ENGINE AND SEND TO ENGINE SHOP FOR FURTHER TEAR DOWN AND EVALUATION. ENGINE SHOP FOUND ENGINE THRU BOLT LOOSE. 1 L 7 2 4T 4 T A24CE E4EA 2002112500043 20021125 00043 CE 2002 11 25 JEM2002F00009 1 20021016 A 5610 1013840252410 WINDSHIELD BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA COCKPIT CRACKED E JEMA K NONE O OTHER IN INSP/MAINT 1 CE 01 366EA 1909 BB841 PCE58090 FLIGHT ELEVATION OF 28,000 FT. AIRCRAFT HAD DEPARTED, PILOTS REPORTED THAT THE WINDSHIELD HEAT WAS ON, WHEN THE RT WIND SHIELD SUDDENLY CRACKED. AIRCRAFT PRESSURE WAS NOT AFFECTED. FLIGHT CREW DECIDED TO RETURN AND AN UNEVENTFUL LANDING W AS MADE. 1 L 7 2 4T 4 T A24CE E4EA 2002112500044 20021125 00044 SO 2002 11 25 N6P2002F00001 1 20021011 A 2820 80048004 HOSE PIPER PA31 PA31350 7103110 SO FUEL PRESSURE CRACKED E N6PA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 27682 7970 317852105 DURING GROUND RUN, PILOT REPORTED FUEL ODOR IN COCKPIT. UPON LOOKING UNDER INSTRUMENT PANEL, FUEL WAS SEEN RUNNING DOWN COPILOTS LT RUDDER PEDAL. WHEN RADAR DISPLAY UNIT WAS REMOVED AND FUEL PRESSURE APPLIED WITH BOOST PUMPS, A FINE STREA M OF FUEL WAS SPRAYING IN DIRECTION OF REAR OF AVIONICS STACK THAT ORIGINATED FROM ONE OF TWO FUEL PRESSURE LINES THAT C ONNECT TO BACK OF FUEL PRESSURE GAUGE. CAUSE WAS A CRACK IN HOSE, NEAR PHENOLIC BLOCK THAT HOLDS FUEL PRESSURE LINES. HOSE IS NOT RATED FOR FUEL OR OIL, OTHER HOSE WAS IN BETTER CONDITION EVEN THROUGH IT WAS OF SAME AGE. BOTH HOSES WERE REPLACED WITH SAME MATERIAL PENDING AVAILABILITY OF A MORE SUITABLE HOSE. 1 L 7 2 3O A20SO 2002112500045 20021125 00045 NM 2002 11 25 A4J2002F00007 1 20021101 A 5270 833703 SWITCH DOUG MD88 MD88 3023688 NM PWA JT8 JT8D NE R1 DOOR INTERMITTENT A A4JA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 35 11FQ 49759 AT 6000 FT REAR 1 DOOR OPEN ANNUNCIATOR LIGHT ILLUMINATED. NO PRESSURIZATION LEAKS. NO AIR LEAKS. RETURNED TO AIRPORT FOR EVALUATION. AIRCRAFT CONTINUED FLIGHT WHERE MAINTENANCE CLEANED SWITCH, OPERATIONAL CHECK GOOD IAW MM, MEL CLEARED . 2 L 7 2 4F 4 F RT A6WE E2EA 2002112500046 20021125 00046 EA 2002 11 25 ASOA02578S 1 20021031 A 7700 4033T65P03 SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ENGINE INOPERATIVE A ASOA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 11 877AS 2246 7579 DURING TAKEOFF, BOTH ENGINES WERE SET AT APPROXIMATELY 90 PERCENT. DURING CLIMB OUT THE LT ENGINE N1 WENT TO THE LOW 70 PERCENT AND FLUXED BETWEEN THE LOW TO HIGH 70. THERE WAS ALSO A FUEL FLOW FLUX AND THE OIL PRESSURE REMAINED CONSTANT. AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED AND LANDED SAFETLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2002112500047 20021125 00047 SO 2002 11 25 ASOA02581S 1 20021103 A 7110 12025600669 COWL DOOR EMB 120 EMB120 3260201 SO PWA 118 PW118 NE LT ENGINE DAMAGED A ASOA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SO 11 504AS 120278 DURING FLIGHT, THE LT ENGINE INBOARD COWLING DOOR CAME OPEN. AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED AND LAND ED SAFELY. C/A: MAINTENANCE REMOVED AND REPLACED THE COWLING DOOR AND UPPER COWLING. NO ADDITIONAL PARTS OR REPAIRS W ERE NECESSARY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2003011000019 20030110 00019 EA 2003 1 10 ASOA02584 1 20021106 A 2822 21SN41112 SWITCH CNDAIR CL600 CL6002B19 1900309 EA FUEL SYSTEM FAILED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 821AS 7194 FLT 4513 - DURING CLIMB-OUT FROM ATL, A LOW FUEL PRESSURE CAUTION MESSAGE ON THE RIGHT ENGINE WAS RECEIVED. THE CAPTAIN SHUT DOWN THE ENGINE AND DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED A ND REPLACED THE FUEL BOOST PUMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003011000020 20030110 00020 EA 2003 1 10 ASOA02585 1 20021108 A 2170 8188182 DUCT CNDAIR CL600 CL6002B19 1900309 EA A/C BAY LEAKING A ASOA A UNSCHED LANDING O OTHER DE DESCENT 1 SO 11 820AS 7188 FLT 4541 - DURING DESCENT INTO MCO, A RAPID LOSS OF CABIN PRESSURE WAS EXPERIENCED. AS A PRECAUTIONARY MEASURE THE CREW USED THE OXYGEN MASKS. AN EMERGENCY WAS DECLARED AND THE LANDED SAFELY IN MCO. MAINTENANCE REMOVED AND REPLACED THE L EFT WATER SEPARATOR OUTLET DUCT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002112500048 20021125 00048 EA 2002 11 25 ASOA02587 1 20021110 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EXTERIOR BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 883AS 3039 7504 DURING GROUND INSPECTION, THE RT EXTERIOR EMERGENCY LIGHT OVER THE WING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE RIGHT EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002112500049 20021125 00049 SO 2002 11 25 ASOA02588 1 20021110 A 6120 CONTROLLER EMB 120 EMB120RT 3260202 SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE LT PROPELLER MALFUNCTIONED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 240AS 120060 DURING CLIMB OUT, THE LT PROPELLER SPEED REACHED 101.2 PERCENT IN A STEADY STATE. THE CREW SET THE PROPELLER SPEED TO 8 5 PERCENT FOR CRUISE AND THE PROPELLER SPEED BECAME NORMAL. FLIGHT IDLE WAS SELECTED AND THE PROPELLER WAS FEATHERED. THE AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE RAN THE LEFT ENGINE FOR 45 MINUTES AND THE PROPELLER SPEED NEVER EXCEEDED 100.8 PERCENT ON EITHER ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2002112500050 20021125 00050 CE 2002 11 25 DBCA1222D1 1 20021106 A 2130 2T4687 RELAY LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP CONTROL BOX FAILED E DBCA K NONE O OTHER IN INSP/MAINT 1 GL 13 505EE 4445 505 DURING PRE-TAKEOFF CHECKS, LT HAND PRESSURIZATION WENT INTO EMERGENCY PRESSURIZATION MODE AND WOULD NOT RESET TO NORMAL . PILOT RETURNED TO DEPARTURE AREA AND ABORTED TRIP. TROUBLESHOT TO FAILED RELAY IN MODULATING VALVE CONTROL BOX. FAI LED RELAY INTERRUPTED GROUND PATH FOR EMERGENCY PRESSSURIZATION VALVE CONTROL BOX. FAILED RELAY INTERRUPTED GROUND PATH FOR EMERGENCY PRESSURIZATION VALVE CAUSING IT TO OPEN. REPLACED MOD. VALVE CONTROL BOX WITH SERVICEABLE UNIT. OPERAT IONS CHECKED GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2002112500051 20021125 00051 CE 2002 11 25 DBCA122D 1 20021004 A 5210 62113681 SPRING CESSNA 650 650 2076802 CE CABIN DOOR FAILED E DBCA K NONE O OTHER IN INSP/MAINT 1 GL 13 403CB 7982 6500099 WHEN CABIN ENTRANCE DOOR WAS OPENED AFTER FLIGHT, CREW NOTICED DOOR OPENED VERY RAPIDLY. INSPECTED DOOR AND FOUND FORWA RD COUNTER BALANCE SPRING HAD FAILED. AFTER SPRING WAS INTACT. FORWARD COUNTER BALANCE SPRING WAS REPLACED WITH NEW. DOOR OPERATIONS CHECK GOOD. 2 L 7 2 4F A9NM 2002112500052 20021125 00052 CE 2002 11 25 FFS2002F00008 1 20021102 A 5260 11451403013 LATCH BEECH 1900 1900C 1154161 CE PWA PT6 PT6A11 52043 NE AIRSTAIR DOOR BROKEN E FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 575Q UC160 LOWER AFT AIRSTAIR DOOR LATCH CABLE BROKE, PREVENTING DOOR BEING OPENED. PASSENGERS HAD TO EXIT THRU CARGO DOOR. WHEN THE AIRSTAIR DOOR IS CLOSED, ANY DIRT OR MOISTURE ON THE TREADS IS FUNNELLED TOT HE LOWER PULLEY FOR THIS CABLE. THIS C ABLE IS BLENDED AND BROKEN IN TWO LOCATIONS THAT CORRESPOND TO THE LOWER AFT PULLEY TRAVEL AND LOWER AFT LATCH CAM PULLE Y. OPERATOR RECOMMENDS MORE FREQUENT DETAILED INSPECTION OF CABIN DOOR. 2 L 7 2 4T 3 T RT A24CE E4EA 2002112500053 20021125 00053 EU 2002 11 25 G1FR100YA 1 20021114 A 2710 10604320 CONTROL UNIT AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP AILERON SYS LEAKING B G1FR K NONE K FLUID LOSS IN INSP/MAINT 1 GL 13 634H 8808 178 AILERON ARTHUR FAILS RESISTANCE CHECKS. STATIC LEAKS BEYOND LIMITS. TIME SINCE OVERHAUL UNKNOWN. UNIT REPACED WITH OV ERHAULED UNIT. 2 L 7 3 4F 4 F A46EU E6WE 2002112500054 20021125 00054 EU 2002 11 25 G1FR100Y1 1 20021114 A 2710 10604319 CONTROL UNIT AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP AILERON SYS LEAKING A G1FR K NONE K FLUID LOSS IN INSP/MAINT 1 GL 13 634H 8808 178 ELEVATOR ARTHUR FAILS RESISTANCE CHECKS. UNIT HAS STATIC LEAD MORE THAT 70 FEET/MINUTE. TSO UNKNOWN. UNIT REPLACED WI TH OVERHAULED UNIT. 2 L 7 3 4F 4 F A46EU E6WE 2002112500055 20021125 00055 NM 2002 11 25 P9R2002F00009 1 20021028 A 3350 SG9422 LIGHT BOEING 727 727200 138407E NM PWA JT8 JT8D17 52049 NE GALLEY 2 FLOOR LOOSE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 910PG 22606 PHOTOLUMINISCENT STRIP AT G2 MISSING, RESECURED PHOTOLUMINISCENT STRIP AT G2. THE CAUSE OF THE MALFUNCTION WAS THE PHO TOLUMINESCENT STRIP COMING UNGLUED FROM FLOOR. THERE WERE NO EMERGENCY MEASURES EXECUTED. 2 L 7 3 4F 4 F RT A3WE E2EA 2002112500056 20021125 00056 NM 2002 11 25 UIEA200200057 1 20021024 A 5753 65B170636 FLAP TRACK BOEING 747 7472F6B 1384807 NM GE CF6 CF650* 30018 NE NR 6 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 535MC 81995 21833 DURING CURRENT "C" CHECK, FOUND NR 6 FLAP OUTBOARD BUSHING OF PIVOT FITTING LOOSE. DISASSEMBLY REVEALED CORROSION ON TH E LEFT SIDE TO SIDE LOAD FITTING ON CONTACT AREAS, (NO CORROSION LEVEL DECLARED). REMOVED TRACK, ROUTED TO SHOP. MACHI NED FLAP TRACK FLANGES TO REMOVE CORROSION. NDI INSPECTED TO ENSURE CORROSION REMOVAL. NO FINDINGS. SHOT PEENED AND R EFINISHED REWORK AREA. FABRICATED REPLACEMENT BEARING PLATES TO COMPENSATE FOR REMOVED MATERIAL IAW STANDARD OVERHAUL P RACTICE. TRACK OVERHAULED AND RESTORED TO ORIGINAL STANDARDS IAW MM. REINSTALLED FLAP TRACK. 2 L 7 4 4F 4 F A20WE E23EA 2002112500057 20021125 00057 NM 2002 11 25 UIEA200200059 1 20021025 A 5330 65B070021 SKIN BOEING 747 747212B 1384886 NM PWA JT9 JT9D* NE FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 808MC 85585 21340 21048 DURING CURRENT "C" CHECK, FOUND CORROSION BETWEEN OUTER SKIN, DOUBLER AND TRIPLER AT BS 1960 STR 42 RT, LOCATED AT THE A FT LOWER CORNER CUTOUT OF THE AFT LOWER LOBE COMPARTMENT DOOR. NO LEVEL DECLARED BUT CORROSION CONSIDERED LOCAL. OUTER SKIN, DOUBLER AND TRIPLER TRIMMED AWAY. PERFORMED E/C OPEN HOLE INSPECTION AND SURFACE INSPECTION OF CUTOUTS TO ENSURE A CRACK FREE CONDITION. NO DEFECTS FOUND. FABRICATED FILLERS, DOUBLER AND TRIPLER. TREATED AND PRIME PAINTED IAW SRM . INSTALLED FASTENERS IAW SRM WET WITH BMS 5-95 SEALANT. REPAIR IS TIME LIMITED FOR 12 MONTHS PENDING DETERMINATION OF ALTERNATE INSPECTION PROCEDURES IAW SSI. 2 L 7 4 4F 4 F A20WE E20EA 2002112500058 20021125 00058 NM 2002 11 25 UIEA200200061 1 20021106 A 2910 65B015122678 LINE BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE HYD SYSTEM CRACKED A UIEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 15 526MC 22337 AIR TURN BACK, NR 1 HYDRAULIC SYSTEM LEAKING. QUANTITY STOPPED AT 2 GALLONS AFTER PLACING EDP SWITCH TO DEPRESS. ADP W ORKED NORMAL AFTER 20 MINUTES IN CONTINUOUS ADP PRESSURE DROPPED TO ZERO. FOUND LINE CRACKED AT CLAMP IN SAILBOAT AREA. REMOVED AND REPLACED HYDRAULIC LINE IAW MM. CASE DRAIN FILTERS CHANGED AND SYSTEM OPERATED AND LEAK CHECKED IAW MM. 2 L 7 4 4F 4 F RT A20WE E23EA 2003020600111 20030206 00111 NM 2003 2 6 WRLA200227 1 20021112 A 3230 AYG70505507 CONTROL VALVE DOUG MD11 MD11 3023602 NM MLG WW MALFUNCTIONED A WRLA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 271WA 48518 AFTER TAKEOFF, LEFT MAIN GEAR WOULD NOT RETRACT. VOLUME 1 PROCEDURE ACCOMPLISHED UNSUCCESSFUL. RETURNED TO DEPARTING S TATION. AIRCRAFT RELEASED FOR FERRY. DOWN GEAR PER RELEASE NR GMM STANDARD PRACTICE 3122, 9/15/02. AIRCRAFT FERRIED T O EVERGREEN AIRCRAFT SERVICES TPI. AIRCRAFT WAS JACKED THE LANDING GEAR WAS CYCLED 4 TIME OPERATED NORMAL NO DEFECTS NO TED. PRECAUTIONARY CHANGE OF THE LANDING GEAR SELECTOR VALVE WAS ACCOMPLISHED IAW FIM 32-30-01-01 PERFORMED BITE TEST O F PSEU AND ALL LDG SENSORS INDICATED SATISFACTORY INSPECTED ALL LDG AND TASK 32-31-20 CONDITION NORMAL/LEAK CHECK NO LEA K FOUND. ALL GEAR RETRACT TIME TEST AND ALTERNATE GEAR EXTENSION TEST PER MM TASK 32-31-00 SATISFACTORY. 2 L 7 3 4F RT A22WE 2002112500059 20021125 00059 WP 2002 11 25 WXOA02009A 1 20021102 A 2120 5910244367 DUCT DOUG DC9 DC921 302205A WP PWA JT8 JT8D NE RIGHT PACK CRACKED E WXOA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 07 127NK 47361 TAIL COMP HIGH TEMP ANNUNCIATOR INDIC ILLUMINATED INFLIGHT. AC RETURNED TO STATION W/O INCIDENT. MAINT INSP TAIL COMP AND ASSOC PRESS DIST SYS FOR CAUSE OF HIGH TEMP INDICATION. MAINT DISCOVERED BLEED AIR LEAK FROM AN UNKNOWN SOURCE IN T HE RT AIR COND SYS. MAINT DEFERRED RT AIR COND SYS IAW MEL. TAIL COMP HIGH TEMP ANNUNCIATOR DOES NOT ILLUMINATE FOLLOW ING DEFERRAL OF RT AIR COND SYS. AC RETURNED TO SERVICE. MAINT FOUND RUPTURED BLEED AIR SUPPLY DUCT IN THE RT AIR COND SYS. SYS REMAINS DEFERRED AWAITING ARRIVAL OF REPLACEMENT DUCT ASSY. MAINT CLEARED THE DEFERRAL WITH THE REPLACEMENT OF RIGHT PACK DUCT ASSEMBLY. RT HAND AIR COND SYS LEAK AND OPERATIONAL CHECK NORMAL. AC RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2002112500060 20021125 00060 NM 2002 11 25 ANCF200200025 1 20021113 A 2760 SWITCH DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE DRAG CONTROL MALFUNCTIONED W ANCF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 190AN 53190 WITH AUTO SPOILERS DISARM, AUTO BRAKES SELECTOR IN OFF AND AUTO BRAKES SWITCH IN DISARM, WHEN THROTTLES WERE ADVANCED F OR TAKE OFF, "AUTO BRAKES TAKE OFF WARNING" CONFIGURATION CAME ON. TAKE OFF WAS ABORTED. REJECTED TAKE OFF SWITCHES WERE ADJUSTED PROPERLY IAW AMM 27-62-08 PAGE 201. RESULTS SATISFACTORY. 2 L 7 2 4F 4 F RT E9NE 2002112500061 20021125 00061 NE 2002 11 25 EVAS091022 2 20021120 A 7200 ENGINE DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE NR 2 FLAMED OUT W QOCF D RETURN TO BLOCK X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 WP 03 16101 NR 2 ENGINE FLAMED OUT AFTER START. NR 2 ENGINE WET MOTORING AND DRY MOTORING. NR 2 ENGINE IDLE RUN TEST NML IAW AMM 71-00-00 2 L 7 3 4F 4 F RT A22WE E31N3 2002112500062 20021125 00062 NM 2002 11 25 FE5F200200005 1 20021113 A 5320 9911246115 ANGLE DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED W FE5F K NONE O OTHER IN INSP/MAINT 1 WP 03 9423 53602 DURING THE C4 CHECK, PERFORMING THE TASK NO.0828 AND CPCP CARD NO.59-53301,AN LOCAL CORROSION WAS FOUND AT STA1380 ,X=-1 8.6~-21.1 (L=2.5", W=0.8",D=0.04"). REQUEST BOEING ASSISTANCE AND IAW BOEING'S RESPONSE REPAIR THE CORROSION TEE ANGLE. MANUFACTURER ISSUED FAA FORM 8110-3. AND APPROVED REPAIR PROCESS. 2 L 7 2 4F RT 2002112500063 20021125 00063 2002 11 25 S02234040 4 20021117 A 3452 TRANSPONDER BOEING 747 747200 1384847 NM PWA JT9 JT9D7R4G2 52054 NE ATC FAILED W SAJF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 03 24308 BOTH ATC TRANSPONDER FAILED LIGHT ILLUM. BEFORE T/O. ATC CONTROL PANEL REPLACED NR 2 ATC NML IAW 34-53-00 T/S BUT NR 1 ATC STILL NO GOOD IAW MEL 34-26 SAFE FOR FLIGHT,ITEM C/F TO D/D PAGE D0045481 CAT "C". THE ATC FRONT PANEL TEST SWITCH LOST THE BITE TEST FUNCTION, REPLACED THE ATC TRANSPONDER. THE ATC CONTROL PANEL J1,J2 SOME TIME POOR CONTACT, REPLACE D THE DB9011A J1, DB9011B J2 ATC CONTROL PANEL CONNECTOR & THE WIRE W037-SX1024-22 ALSO POOR CONTACT . 2 L 7 4 4F 4 F RT A20WE E3NE 2002112500064 20021125 00064 NE 2002 11 25 S02271039 2 20021110 A 7261 OIL SYSTEM BOEING 747 747200 1384847 NM PWA JT9 JT9D7R4G2 52054 NE NR 1 ENGINE LOW W SAJF E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 03 24308 NR 1 ENGINE OIL QUANTITY SHOW ZERO AND LOW OIL PRESS LIGHT ILLUMINATED DURING CLIMB. FLIGHT CREW DECIDED TO SHUT DOWN EN GINE IN FLIGHT. THEN DIVERT TO SINGAPORE. ENGINE REPLACED, WAITING SHOP INVESTIGATION. 2 L 7 4 4F 4 F RT A20WE E3NE 2002112500065 20021125 00065 EU 2002 11 25 YENA200225 1 20021016 A 2120 ODOR AIRBUS 320 A320232 3930326 EU CABIN DETECTED A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 537JB 1785 ON CLIMB OUT, SMELLED ACRID ODOR, SEEMED TO BE STRONGER IN AFT CABIN. ODOR OCCURRED 3 TIMES IN RAPID SUCCESSION. RETURNE D TO JFK. PERFORMED INSPECTION OF LTV SYSTEM COMPONENTS, ALL SEATS SEB'S & WIRING HARNESS SEB'S & MRM RACK. AVIONIC INL ET/EXHAUST MOTORS INSPECTION OF WIRING HARNESS, BOTH INLETS FOR PACKS. NO DEBRIS OR DAMAGE FOUND. CHECKED RECIRC FAN AND ALL COFFEEMAKERS, CHECKED FOR ODOR AND DAMAGE. ALL AREAS NORMAL, NO DEFECTS NOTED. THE ONLY DEFECT WAS EVIDENCE OF MID AFT COFFEEMAKER GROUND BAG BROKEN AND GRINDS ALL OVER. NO OTHER DEFECT. TEST FLIGHT ACCOMPLISHED COMPLETED, COULD NOT DU PLICATE REPORTED SYMPTOMS. NO UNFAMILIAR ODORS NOTICED. LTV FUNCTIONS NORMALLY AS WELL AS ALL OTHER A/C SYSTEMS. 2 L 7 2 4F RT A28NM 2002112500077 20021125 00077 NM 2002 11 25 AALA20020037 1 20020111 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 619AA 24577 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 33D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBL Y. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500078 20021125 00078 NM 2002 11 25 AALA20020576 1 20020501 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 652AA 24610 JFK - EMERGENCY EXIT LIGHT BELOW OVERHEAD BIN 12 ABC IS OUT. REMOVED AND REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKE D NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500079 20021125 00079 NM 2002 11 25 AALA20020647 1 20020513 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 DFW - AISLE BULLNOSE EMERGENCY LIGHT AT 12C AND LEFT OVERWING EXIT EMERGENCY SIGN INOPERATIVE. REMOVED AND REPLACED BAT TERY PACK ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500080 20021125 00080 NM 2002 11 25 AALA20021221 1 20020824 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 JFK - EMERGENCY LIGHTS FROM 5E TO 6F ARE INOPERATIVE. RECONNECTED LOOSE CONNECTION AT STRIP LIGHT ASSEMBLY. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500081 20021125 00081 NM 2002 11 25 AALA20021234 1 20020828 A 3350 SWITCH BOEING 757 757223 1384957 NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 634AA 24592 DFW - COCKPIT EMERGENCY LIGHT UNARMED LIGHT INDICATION INOPERATIVE. REPLACED COCKPIT OVERHEAD EMERGENCY LIGHT UNARMED S WITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500082 20021125 00082 NM 2002 11 25 AALA20021255 1 20020829 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 182AN 29592 ORD - FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FIRST CLASS AND HALF OF COACH SECTIONS. REPAIRED WIRING AT FORW ARD SEAT AND R2 GALLEY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500083 20021125 00083 NM 2002 11 25 AALA20021259 1 20020905 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 194AA 32388 MIA - FOUND WIRE BROKEN AT SIDEWALL CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 16DEF. REPLACED PINS AND CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500084 20021125 00084 EU 2002 11 25 YENA200226 1 20021020 A 3411 O851HL PITOT HEAD AIRBUS 320 A320232 3930326 EU NR 2 FALSE INDICATION A YENA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 15 529JB 3886 1610 FLT 62, RSW TO JFK, F/O AIRSPEED INDICATED 0 ON TAKE OFF ROLL, ABORTED T.O AT 80-KTS. PLACED ADR NR 2 ON MEL REF 34-10- 01. REMOVED AND REPLACED NR 2 PITOT PROBE AS PER M.M REF 34-11-15-000-001. OPS CHECK OK. 2 L 7 2 4F RT A28NM 2002112500085 20021125 00085 NM 2002 11 25 AALA20021269 1 20020908 A 3350 CONTACTOR BOEING 757 757223 1384957 NM EXTERIOR DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 619AA 24577 JFK - RIGHT SIDE EXTERIOR EMERGENCY LIGHTS, SECOND FROM FRONT, INOPERATIVE. CLEANED CONTACTS AND RELAMPED. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500086 20021125 00086 EU 2002 11 25 YENA200229 1 20021118 A 2530 COFFEEMAKER AIRBUS 320 A320232 3930326 EU GALLEY ODOR A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 547JB 1968 FLT 187, JFK TO MCO, SMELLED SMOKE, NONE VISIBLE, FLIGHT ATTENDANT REPORTED 2 FWD COFFEEMAKERS BREAKERS POPPED. RETURNED TO JFK, REMOVED AND REPLACED COFFEEMAKER, PERFORMED GENERAL VISUAL INSPECTION OF AREA BEHIND COFFEEMAKERS AND REMOVED F WD GALLEY ELECTRICAL CONTROL PANEL, ACCOMPLISHED GENERAL INSPECTION, NO PROBLEM NOTED. 2 L 7 2 4F RT A28NM 2002112500087 20021125 00087 SO 2002 11 25 LR7A02081 1 20021026 A 5230 WEB LKHEED 382 382G 526414U SO CARGO DOOR DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HC05297 FOUND HOLE IN CARGO DOOR WEB BELOW LOADING RAMP STOWAGE INSTRUCTION PLATE FS 889, LBL 3, WL 220. REPAIRED HOLE IAW SRM SMP 583-51-140-12. 2 H 7 4 4T A1SO 2002112500088 20021125 00088 SO 2002 11 25 LR7A02093 1 20021026 A 5315 FLOORBEAM LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5302 FOUND FLOORBEAM WITH CORROSION ON TOP FS 257E, LBL 61-RBL 61, WL 146. REPLAC ED BEAM CAP IAW SRM SMP 583-53-40-06, 51-60, 51-70, AND DWG 364242. 2 H 7 4 4T A1SO 2002112500089 20021125 00089 WP 2002 11 25 2002F00939 1 20021008 A 2520 78652A FRAME DOUG DC9 DC982 3022082 WP MID CABIN SEAT CRACKED D K NONE O OTHER IN INSP/MAINT 1 GL 13 DURING GENERAL VISUAL INSPECTION OF MID FLIGHT ATTENDANT SEAT FOUND SEAT FRAME HAD A CRACK IN THE LOWER HORIZONTAL MEMBE R ADJACENT TO THE LOWER MOUNT/PIVOT POINT. CRACK LENGTH APPROX 1/2 CIRCUMFERENCE OF FRAME TUBE. 2 L 7 2 4F A6WE 2002112500090 20021125 00090 SO 2002 11 25 000219 1 20021029 A 3230 LANDING GEAR EMB 145 EMB145 3260210 SO MAIN MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 290 LANDING DISAGREE MESSAGE AND LANDING GEAR WOULD NOT RETRACT. 2 L 7 2 4F RT T00011AT 2002112500091 20021125 00091 SO 2002 11 25 000220 1 20021104 A 3610 WARNING SYSTEM EMB 145 EMB145 3260210 SO BLEED SYS FALSE INDICATION A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 260 BLEED 2 LEAK. PERFORMED GROUND RUN FOR BLEED LEAKS NO LOCK NOTED AND NO EICAS MSG FOR BLEED LEAK NOTED 2 L 7 2 4F RT T00011AT 2002112500092 20021125 00092 SO 2002 11 25 000221 1 20021104 A 3610 WARNING SYSTEM EMB 145 EMB145 3260210 SO BLEED INDICATION FALSE INDICATION A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 260 BLEED 2 LEAK. PERFORMED GROUND RUN FOR BLEED LEAKS NO LOCK NOTED AND NO EICAS MSG FOR BLEED LEAK NOTED, 2 L 7 2 4F RT T00011AT 2002112500093 20021125 00093 SO 2002 11 25 000222 1 20021105 A 3610 CLAMP EMB 145 EMB145 3260210 SO BLEED SYSTEM LOOSE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 260 BLEED 2 LEAK TIGHTENED BOTH U CLAMPS AT THE LINE AND REPLACED BOTH UPPER AND LOWER BLEED O'RINGS IN CARGO COMPT 2 L 7 2 4F RT T00011AT 2002112500094 20021125 00094 SO 2002 11 25 LR7A02094 1 20021026 A 5315 395220 FLOORBEAM LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5302 FOUND CORROSION ON FLOORBEAM FS 537, LBL 61-RBL 61, WL 146. REPLACED BEAM CA P IAW SRM SMP 583-51-70-00, 51-60, AND DWG 395220. 2 H 7 4 4T A1SO 2002112500095 20021125 00095 SO 2002 11 25 LR7A02095 1 20021026 A 5315 364242 FLOORBEAM LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5302 FOUND CORROSION ON FLOORBEAM FS 357, LBL 61-RBL 61, WL 146. REPLACED BEAM CA P IAW SRM SMP 583-51-70-00, 51-60, AND DWG 364242. 2 H 7 4 4T A1SO 2002112500096 20021125 00096 SO 2002 11 25 LR7A02096 1 20021026 A 5315 3642421 FLOORBEAM LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5302 FOUND CORROSION ON FLOORBEAM FS 297E, LBL 61-RBL 61, WL 146. REPLACED BEAM C AP IAW SRM SMP 583-51-70, 51-60, AND DWG 364242. 2 H 7 4 4T A1SO 2002112500097 20021125 00097 SO 2002 11 25 LR7A02097 1 20021026 A 5315 356120 FLOORBEAM LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5302 FOUND CORROSION ON FLOORBEAM FS 457, LBL 61-RBL 61, WL 146. REPLACED BEAM CA P IAW SRM SMP 583-51-70-00, 51-60, AND DWG 356120. 2 H 7 4 4T A1SO 2002112500098 20021125 00098 SO 2002 11 25 LR7A02100 1 20021026 A 5320 3723951L ANGLE LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5325 FOUND FLIGHT DECK NAV STATION ANGLE CORRODED. FS 196-212, RBL 50, WL 200. R EPLACED ANGLE IAW SRM SMP 583-51-60, AND 51-70. 2 H 7 4 4T A1SO 2002112500099 20021125 00099 SO 2002 11 25 LR7A02104 1 20021026 A 5315 3317069 FLOORBEAM LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2205 4698 DURING SCHEDULED C4 INSPECTION PER HST5302 FOUND FLOORBEAM TOP CAP CORRODED FS 737E, LBL 61-RBL 61, WL 146. REPLACED BE AM CAP IAW SRM SMP 583-51-60, 51-70 AND DWG 3317069. 2 H 7 4 4T A1SO 2002112500100 20021125 00100 NM 2002 11 25 VNAA0211005 1 20021106 A 2731 RELAY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ELEVATOR SYS FAILED A VNAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 424JS 3033 DURING CLIMB, THE CREW ADVISED DISPATCH THAT THE NORMAL ELEVATOR TRIM WOULD NOT WORK IN THE NOSE DOWN DIRECTION. THE CR EW FOLLOWED THE QUICK REFERENCE HANDBOOK AND INDICATED THAT THE STANDBY TRIM WAS WORKING NORMALLY. FLIGHT 4100 WAS THEN INSTRUCTED TO DIVERT TO PIT DUE TO GUSTY WINDS IN DCA. MAINTENANCE INSPECTED AND REPLACED THE 49CC AND 59CC RELAYS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FO R SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002112500101 20021125 00101 NM 2002 11 25 VNAA0211008 1 20021108 A 2910 HYDRAULIC SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE CONTAMINATED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 472PS 3008 EN ROUTE, THE CREW RECEIVED AN EMERGENCY PARK ACCUMULATOR FAIL CAS MESSAGE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO BWI. MAINTENANCE INSPECTED AND BLED THE HYDRAULIC SYSTEM IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-00-00. O PERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002112500102 20021125 00102 NM 2002 11 25 VNAA0211010 1 20021110 A 2913 4206801 PUMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE HYD SYSTEM FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 461PS 3658 1012 3075 DURING CLIMB, THE CREW RECEIVED A MAIN HYDRAULIC INOP BLUE CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK PROCEDURE AND THE MESSAGE DID NOT CLEAR. MAINTENANCE CONTROL WAS CALLED AND FLIGHT 4064 RETURNED TO DCA. MAINTENANCE I NSPECTED AND REPLACED THE MAIN HYDRAULIC PUMP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-00-00. OPERATIONAL CHECK S WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002112500103 20021125 00103 NM 2002 11 25 VNAA0211012 1 20021110 A 3350 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DIRTY A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 457PS 3048 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT 9A WAS NOT WORKING. MAINTENANCE INSPECTED AND CLEANED THE LIGHTING CON NECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS R ELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002112500104 20021125 00104 2002 11 25 VNAA0211016 4 20021114 A 3418 STALL WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 426JS 3038 DURING TAKEOFF, THE CREW RECEIVED AN AOA SENSOR FAIL CAWS MESSAGE AND ABORTED TAKEOFF. AFTER CLEARING THE RUNWAY THE ME SSAGE CLEARED AND FLIGHT 4165 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4165 THEN DEPARTED WITH NO FURTHER INCIDE NTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002112500105 20021125 00105 NM 2002 11 25 VNAA0211017 1 20021114 A 3240 BRAKE ASSY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LANDING GEAR CONTAMINATED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 470PS 3006 THE CREW REPORTED THAT THE FIRST OFFICER'S BRAKE PEDALS HAD NO BRAKING RESPONSE WHEN APPLIED. MAINTENANCE INSPECTED AND BLED THE BRAKES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRC RAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002112500106 20021125 00106 2002 11 25 VNAA0211018 4 20021115 A 3460 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 461PS 3075 DURING TAKEOFF AT 45 KNOTS, THE CREW RECEIVED A FLIGHT GUIDANCE CONTROL UNIT MESSAGE AND ABORTED TAKEOFF. AFTER CLEARIN G THE RUNWAY THE MESSAGE CLEARED BY ITSELF. FLIGHT 4099 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FU RTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002112500108 20021125 00108 NE 2002 11 25 2002UALA01364 2 20020828 A 7261 1A5839 CARBON SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE FAILED A UALA B A EMER. DESCENT UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 29 578UA 9028 26694 726688 AFT LAV SMOKE DETECTOR ALARM ON AND A BLUISH SMOKE IN CABIN WITH SMELL OF OIL. CABIN WAS CLEARED BUT SMOKE RETURNED. F OLLOWING LINE TROUBLE SHOOTING TO ELIMINATE THE APU AS THE OIL SOURCE THE SUBJECT ENGINE WAS REPLACED AND SENT TO THE EN GINE SHOP FOR REPAIR. INSPECTION SHOWED THAT OIL FROM THE NR 3 AFT CARBON SEAL HAD ENTERED THE GAS PATH THROUGH THE 10T H OR 14TH STAGE BLEED DUCT. THE ROOT CAUSE IS A FAILED 2/3 CARBON SEAL CAUSING HIGH GEARBOX BREATHER PRESSURE AND THE LEAKAGE PAST THE NR 3 AFT CARBON SEAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112500109 20021125 00109 NE 2002 11 25 2002UALA01398 2 20020901 A 7261 1A5839 CARBON SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE FAILED A UALA A B UNSCHED LANDING EMER. DESCENT K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 578UA 9028 26694 726688 HAZE AND NON-ELECTRICAL SMELL IN CABIN AT FLT 360 AFTER FA'S TURNED ON MOVIE SYSTEM. ATTENDANTS HAS TURNED OFF GALLEY P OWER, VIDEO SYSTEM AND LIGHTS IN CABIN AND DID NOT SEEM TO HELP. SMELL AND HAZE WAS ONLY SLIGHT IN FLIGHT DECK. LINE T ROUBLE SHOOTING TO ELIMINATE THE APU AS THE OIL SOURCE THE SUBJECT ENGINE WAS REPLACED AND SENT TO THE ENGINE SHOP FOR R EPAIR. INSPECTION SHOWED THAT OIL FROM THE NR 3 AFT CARBON SEAL HAD ENTERED THE GAS PATH THROUGH THE 10TH OR 14TH STAGE BLEED DUCT. THE ROOT CAUSE IS A FAILED 2/3 CARBON SEAL CAUSING HIGH GEARBOX BREATHER PRESSURE AND THE LEAKAGE PAST THE NR 3 AFT CARBON SEAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112500110 20021125 00110 SO 2002 11 25 C2XA02CL230 1 20021122 A 4900 APU EMB 135 EMB135LR 3260305 SO OVERSERVICED A C2XA O OTHER J WARNING INDICATION UK UNKNOWN 1 SW 27 27523 145389 YUL FLIGHT#4092 THE CREW REPORTED A LAV SMOKE WARNING ON THE EICAS AND A STRONG OIL SMELL IN THE CABIN.MAINTENANCE INSPE CTED AIRCRAFT FOR SMOKE OR FIRE DAMAGE AND NONE WAS FOUND.THE APU WAS DETERMINED TO BE GIVING OFF THE OIL SMELL AND WAS PLACED ON MEL.MAINTENANCE INSPECTED THE APU ON 11/23/02 AND FOUND THE APU WAS OVERSERVICED WITH OIL.MAINTENANCE SERVICED THE APU TO THE PROPER LEVEL AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002112500111 20021125 00111 NM 2002 11 25 HNAA0200084 1 20021123 A 3320 11200705 CONTROL PANEL DHAV DHC8 DHC8201 2809001 NM GALLEY MALFUNCTIONED A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 07 989HA 427 F/A REPORTED OF SMOKE IN GALLEY AREA. F/A PULLED GALLEY C/B AND CREW PULLED C/B 1C BUFFET POWER ON SECONDARY C/B PANEL AFTER THAT NO SMOKE NOTED. MAINTENANCE INSPECTION FOUND GALLEY LIGHT FIXTURE BURNT. ENGINEERING WAS CALLED FOR AN E/O TO PULL AND COLLAR GALLEY LIGHT C/B AT F/A STATION AND MEL THE GALLEY LIGHTS. A/C OVERNIGHTED IN JAX WHERE THE F/A CONT ROL PANEL WAS REPLACED. 2 H 7 2 4T RT A13NM 2002112500112 20021125 00112 NM 2002 11 25 2002UALA01421 1 20020907 A 2120 SMOKE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT DETECTED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 672UA 30027 STRONG SMOKE OR BURNT RUBBER SMELL IN COCKPIT ON FIRST OFFICER'S SIDE. SMELL WAS FROM POSSIBLE BURNT BALLAST. ALL LIGH TS WERE TURNED ON IN COCKPIT FOR 90 MINUTES. PANELS P11, P5, P61, P64, P1-3, AND TOP OF P8 WERE ALL OPENED. CHECKED IN E&E COMPARTMENT UNDER FLOOR FOR DAMAGED WIRES, NOTHING WAS NOTED. ACCOMPLISHED ENGINE RUNS, RAN PACKS WITH APU AND WIT H ENGINES, NO ABNORMAL SMELLS WERE DETECTED. UNABLE TO DUPLICATE SMELL OR FIND ANY DISCREPANCIES THAT MIGHT HAVE CAUSED THE SMELL. 2 L 7 2 4F 4 F RT A1NM E24NE 2002112500115 20021125 00115 NM 2002 11 25 PCAA0211136 1 20021122 A 3230 574205A SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM ONLY INOPERATIVE A PCAA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 EA 13 845EX 16560 3755 344 ROC-LGA FLIGHT#3862. CREW REPORTED DURING FINAL APPROACH GEAR HANDLE SELECTED DOWN, GEAR DID NOT COME DOWN AND 3 RED UNS AFE LIGHTS ILLUMINATED. ALTERNATE EXTENSION PERFORMED, AND FLEW BY TOWER TO VISUALLY VERIFY GEAR DOWN. AIRCRAFT LANDED W ITH OUT INCIDENT. MAINTENANCE PERFORMED PSEU SELF TEST, TARGET TEST, AND CLEANED ALL PROXIMITY SENSORS. LANDING GEAR SEL ECTOR VALVE WAS REPLACED. OPERATIONAL CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002112500117 20021125 00117 NM 2002 11 25 AALA20021270 1 20020908 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 619AA 24577 JFK - FOUND LEFT SIDE EXTERIOR EMERGENCY LIGHTS, THIRD FROM FRONT, INOPERATIVE. CLEANED CONTACTS AND RELAMPED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500118 20021125 00118 NM 2002 11 25 AALA20021284 1 20020909 A 3350 SOCKET BOEING 757 757223 1384957 NM EXTERIOR DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 608AA 27446 SFO - EXTERNAL EMERGENCY LIGHT AT R2 DOOR INOPERATIVE. CLEANED SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500119 20021125 00119 NM 2002 11 25 AALA20021302 1 20020915 A 3350 SOCKET BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 619AA 24577 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH LIGHTING AT ROW 31 INOPERATIVE. REPLACED EMERGENCY PATH LIGHT SOCKET AT ROW 31. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500120 20021125 00120 NM 2002 11 25 AALA20021335 1 20020920 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 184AN 29594 DFW - FLOOR TRACK LIGHTS FROM R2 DOOR BACK TO SEAT FORWARD OF OVERWING EXIT DOOR INOPERATIVE. REPLACED DAMAGED SECTION OF FLOOR TRACK WIRES FORWARD OF ROW 15. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002112500121 20021125 00121 WP 2002 11 25 AALA20021337 1 20020920 A 3350 BAT5014 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 579AA 53156 LAX - DURING OVERNIGHT MAINTENANCE EMERGENCY CEILING LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED FIRST CLASS CABI N EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112500122 20021125 00122 WP 2002 11 25 AALA20021338 1 20020923 A 3350 BAT5014 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7549A 53031 DFW - DURING OVERNIGHT MAINTENANCE, AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS BETWEEN AFT LAVS INOPERATIVE. REPLACED AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT BATTERY PACK IN AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112500123 20021125 00123 WP 2002 11 25 AALA20021339 1 20020920 A 3350 EMBS1392 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 216AA 49167 LAX - DURING OVERNIGHT MAINTENANCE, FIRST CLASS CEILING EMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTING BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112500124 20021125 00124 WP 2002 11 25 AALA20021340 1 20020923 A 3350 BAT5014 BATTERY PACK DOUG DC9 DC982 3022082 WP TAILCONE DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED TAIL CONE EMERGENCY EXIT LIGH T BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112500125 20021125 00125 WP 2002 11 25 AALA20021341 1 20020922 A 3350 EMBS1392 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 216AA 49167 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING ROW 8 THROUGH 12 INOPERATIVE. REPLACED EMERGENCY ESC APE PATH LIGHTING BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112500126 20021125 00126 WP 2002 11 25 AALA20021342 1 20020922 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7528A 49920 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT ON SEAT 19D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112500127 20021125 00127 WP 2002 11 25 AALA20021343 1 20020920 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7528A 49920 DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN FORWARD LAVATORY INOPERATIVE. RESECURED LOOSE WIRE TO EMERG ENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112500128 20021125 00128 EU 2002 11 25 02327333 1 20021123 A 3350 1317 LAMP JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 333UE 41101 During preflight inspection, the crew reported that the L/H fwd emergency exit light was inoperative. Maintenance perso nnel removed and replaced the lamp in the L/H fwd emergency exit light. An operational check was satisfactory and the a ircraft was returned to service. 2 L 7 2 4T RT A41NM 2002112500129 20021125 00129 WP 2002 11 25 AALA20021344 1 20020923 A 3350 BAT5014 BATTERY PACK DOUG DC9 DC982 3022082 WP LAVATORY DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 466AA 49596 RDU - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT IN AFT LAVATORY INOPERATIVE. REPLACED EMERGENCY EXIT BATTERY PACK IN AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112500130 20021125 00130 WP 2002 11 25 AALA20021345 1 20020919 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP BATTERY PACK LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS DIM BETWEEN ROWS 13 THROUGH 16 AND IN FRONT OF CABIN S ERVICE DOOR INOPERATIVE. RESECURED LOOSE CONTACTS TO EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL O PERATION. (M) 2 L 7 2 4F A6WE 2002112500131 20021125 00131 WP 2002 11 25 AALA20021346 1 20020919 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7528A 49920 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS ROW 18B/D INOPERATIVE. RESECURED BATTERIES IN BATTERY PACK TO EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002112500132 20021125 00132 NM 2002 11 25 USAABB02180 1 20021021 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 631AU 27809 SFO - ALL FLOOR LEVEL EMERGENCY LIGHTS FAILED THE LIGHT TEST. MAINTENANCE REPLACED ALL TEN BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002112500133 20021125 00133 NM 2002 11 25 USAABB02181 1 20021022 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 631AU 27809 PVD - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002112500134 20021125 00134 NM 2002 11 25 USAABB02184 1 20021023 A 3350 8731002511REV15 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 618AU 22210 CLT - FOUND L3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002112500135 20021125 00135 NM 2002 11 25 CALA0200558 1 20021122 A 5720 STIFFENER BOEING 737 7373T0 1384582 NM WS 453 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND A 7" CRACK IN STIFFENER AT I/B SIDE OF WEB, L/H WING STA 453. REPAIRED IAW ECRA 5713-01000. 2 L 7 2 4F RT A16WE 2002112500136 20021125 00136 WP 2002 11 25 CALA0200559 1 20021122 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 98876 49444 INSPECTION FOUND A 1" CRACK IN BELTFRAME AT STA 1418, LONGERON 2R. A REPAIR WAS INSTALLED IAW ECRA 5310-04296. 2 L 7 2 4F A6WE 2002112500137 20021125 00137 NM 2002 11 25 CALA0200560 1 20021123 A 5330 SKIN BOEING 737 737524 1384721 NM STA 360 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27610 27323 A DENT WAS DISCOVERED IN FUSELAGE SKIN AT STA 360 ABOUT 3" ABOVE CUSP LINE AND 22" AFT OF L-1 DOOR. INSTALLED DOUBLER IA W SRM 53-00-01. 2 L 7 2 4F RT A16WE 2002112500138 20021125 00138 NM 2002 11 25 CALA0200561 1 20021124 A 5320 ANGLE BOEING 737 737524 1384721 NM STA 344-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27610 27323 INSPECTION FOUND A 1" CRACK IN ANGLE AT STA 344-360, LBL 12. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002112500139 20021125 00139 NM 2002 11 25 CALA0200562 1 20021124 A 5320 ANGLE BOEING 737 737524 1384721 NM STA 500-520 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27610 27323 INSPECTION FOUND A 1" CRACK IN ANGLE AT STA 500-520, BL O. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002121800045 20021218 00045 SO 2002 12 18 C2XA02BT078 1 20021122 A 4990 APU EMB 135 EMB135LR 3260305 SO APU BAY OVERSERVICED A C2XA A UNSCHED LANDING W B J INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 27523 145389 LAV SMOKE WARNING INDICATION ON EICAS, JUST SHUTDOWN APU, AIRCRAFT RETURNED TO YUL. MAINTENANCE FOUND APU GIVING OFF ST RONG OIL ODOR, APU WAS PLACED ON MEL. MAINTENANCE FOUND APU TO BE OVERSERVICED WITH OIL BY 400 CC. REMOVED EXCESS OIL, REVERIFIED PROPER OIL SERVICE LEVEL. OPS. CHECKED APU, CHECKED GOOD. NO OIL SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. SDR CLOSED. 2 L 7 2 4F RT T00011AT 2002112500140 20021125 00140 EU 2002 11 25 RAIA00211318 1 20021103 A 3260 EO24428A0 RELAY AEROSP ATR72 ATR72202 8680940 EU DEFECTIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 721TE 217 5595-STL- NLG DOWN LOCK LIGHTS ON FORWARD PANEL FLASHING. MAINTENANCE DEFERRED PER MEL 32-61-1(B), SUBSEQUENTLY REMOVING AND REPLACING RELAY 96B, OPS CK OK. 2 H 7 2 4T RT A53EU 2002112500141 20021125 00141 EU 2002 11 25 RAIA00211319 1 20021107 A 6120 4122006002 PUMP AEROSP ATR72 ATR72202 8680940 EU MALFUNCTIONED A RAIA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 03 721TE * 14842 217 5465-BMI- LEFT ENGINE AUTO TAKE- OFF POWER CONTROL WILL NOT TEST. MAINTENANCE DEFERRED PER MEL 73-21-1C SUBSEQUENTLY REM OVED AND REPLACED #1 PROP FEATHER PUMP, OPS AND LK CK OK. 2 H 7 2 4T RT A53EU 2002112500142 20021125 00142 EU 2002 11 25 RAIA00211321 1 20021109 A 3320 BCI0072002 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU DEFECTIVE A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 555HK 41072 5588-SGF- SMOKE COMING FROM CEILING LIGHT AT SEAT 3B. MAINTENANCE DEFERRED PER MEL 33-7 (c) SUBSEQUENTLY REMOVING AND RE PLACING THE CEILING LIGHT FIXTURE. 2 L 7 2 4T RT A41NM 2002112500143 20021125 00143 EU 2002 11 25 RAIA00211322 1 20021115 A 7931 3038450 PACKING AEROSP ATR42 ATR42300 8680920 EU DETERIORATED A RAIA O OTHER J WARNING INDICATION LD LANDING 1 CE 03 423TE 119 5555-SBN- LOST #2 ENGINE OIL PRESSURE. MAINTENANCE REMOVED AND REPLACED PCU PUMP PACKING, LK AND OPS CK OK. 2 H 7 2 4T RT A53EU 2002112500144 20021125 00144 NM 2002 11 25 AWXA200201153 1 20021119 A 5330 6545775594 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 0 0 23218 MCN - MAJOR REPAIR - DURING 8-DAY CHECK A 3" LONG CRACK WAS FOUND ON THE FUSELAGE SKIN FORWARD OF THE AFT CARGO DOOR AT BS 767, STR 21 R/H. MAINTENANCE CUTOUT DAMAGED SKIN AT BS 762.5 TO BS 766.2, STR 21 R/H; PREFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR FILLER AND DOUBLER; AND INSTALLED REPAIR PARTS IAW AWA E.R. 03-536 1-02326-TB2. 2 L 7 2 4F RT A16WE 2002112500145 20021125 00145 NM 2002 11 25 AWXA200201154 1 20021119 A 5330 6545775594 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 0 0 23218 MCN - MAJOR REPAIR - DURING 8-DAY CHECK A 1 1/2" CRACK WAS FOUND ON THE FUSELAGE SKIN AFT LOWER SIDE OF THE R/H WING TO BODY FAIRING AT BS 727E, STR 23 R/H. MAINTENANCE CUTOUT DAMAGED SKIN AT BS 727E, STR 23 R/H; PREFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED 3 EACH STRUCTURAL FILLERS, 1 EACH INTERNAL FILLER, 2 EACH DOUBLES, AND A TRIPLER; AND INSTALLED REPAIR PARTS IAW AWA E.R. 03-5361-02326-TB2. 2 L 7 2 4F RT A16WE 2002112500146 20021125 00146 2002 11 25 COMA0260660 4 20021123 A 3430 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 403CA 7428 FLIGHT 5199 EFIS COMP ERROR CAUTION MESSAGERESET THE AHRS - OPERATION NORMAL. 2 L 7 2 4F RT A21EA 2002112500147 20021125 00147 EA 2002 11 25 COMA0260637 1 20021108 A 3350 6464 CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR INOPERATIVE A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 786CA 7333 FLIGHT 5460 EMERGENCY FLOOR LIGHTING, ROW 5 FORWARD, ARE INOP.REPLACED THE FWD SECTION POWER STRIP. 2 L 7 2 4F RT A21EA 2002112500148 20021125 00148 EA 2002 11 25 COMA02606661 1 20021123 A 3220 TARGET CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 932CA 7038 FLIGHT 6153 GEAR DISAGREE WARNING - NLG DID NOT RETRACT.REALIGNED NLG CENTERED, PROXIMITY TARGET. 2 L 7 2 4F RT A21EA 2002112500149 20021125 00149 SO 2002 11 25 RAIA00211326 1 20021119 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145 3260210 SO INOPERATIVE A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 805HK 2187 41 145096 5301-SBN- SEVERAL EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002112500150 20021125 00150 EU 2002 11 25 RAIA00211327 1 20021119 A 2750 AIR87390 SELECTOR VALVE JETAIR JETSTM JETSTM4101 1500501 EU INTERMITTENT A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 562HK 14139 2258 41078 5350-RIC- FLAPS WOULD NOT RETRACT AFTER TAKE OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY SELECTOR VALVE, OPS AND LK CK OK. 2 L 7 2 4T RT A41NM 2002112500151 20021125 00151 SO 2002 11 25 RAIA00211328 1 20021019 A 8011 35059105 STARTER EMB 145 EMB145 3260210 SO INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 806HK 7822 145112 5322-PIT- RIGHT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED THE #2 AIR TURBINE STARTER, OPS CK OK 2 L 7 2 4F RT T00011AT 2002112500152 20021125 00152 2002 11 25 RAIA00211329 4 20021119 A 3414 7002860909 INDICATOR AEROSP ATR42 ATR42300 8680920 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 424TE 28440 1700 124 5499-MSM- FO's AIR SPEED INDICATOR DISPLAYED OFF FLAG. MAINTENANCE REMOVED AND REPLACED AIR SPEED INDICATOR, OPS CK OK. 2 H 7 2 4T RT A53EU 2002112500153 20021125 00153 EU 2002 11 25 RAIA00211330 1 20021120 A 2750 TY175603C CONTROL VALVE JETAIR JETSTM JETSTM4101 1500501 EU INTERMITTENT A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 562HK 14255 41078 5360-GSO- FLAPS STUCK AT 9 DEGREES. MAINTENANCE REMOVED AND REPLACED THE FLAP HYDRAULIC CONTROL UNIT, LK AND OPS CK OK. 2 L 7 2 4T RT A41NM 2002112500154 20021125 00154 EU 2002 11 25 PNSA021102 1 20021122 A 2611 4730791 SMOKE DETECTOR SAAB SF340 340B 7860101 EU DIRTY A PNSA K NONE J WARNING INDICATION CR CRUISE 1 AL 03 675PA 141 340B206 False cargo warning in flight. Nightshift Maintenance replaced aft detector pn 473079-1 sn 1055 with non approved post S B 26-023 PN CGAB1201-01 sn 1146 to clear discrepancy. Chief Inspector found wrong PN installed while doing daily record audit and informed Maintenance supervisor of problem who had original part sn 1055 cleaned and function checked and rein stalled. Original part had 141.7 hours on it after bench check from MFG. suspect moisture contamination caused original problem. 2 L 7 2 4T RT A52EU 2002112600001 20021126 00001 2002 11 26 000223 4 20021109 A 3414 INDICATOR EMB 145 EMB145 3260210 SO COCKPIT INACCURATE A CHQA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 11 269 AIR SPEED READS 40 KNOTS LOWER THAN CAPTAINS AND STANDBY ON TAKEOFF ROLL. FOUND NR 2 ADC BAD. RR'D. 2 L 7 2 4F RT T00011AT 2002112600002 20021126 00002 2002 11 26 000224 4 20021111 A 3140 WARNING SYSTEM EMB 145 EMB145 3260210 SO NR 2 T/R ACTIVATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 291 E2 REV DISAGREE MESSAGE CAME ON DURING TAKEOFF. DEFERRED NR 2 THRUST REVERSER. 2 L 7 2 4F RT T00011AT 2002112600003 20021126 00003 SO 2002 11 26 000225 1 20021112 A 3620 AIR FILTER EMB 145 EMB145 3260210 SO ENGINE CONTAMINATED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 265 BLEED 1&2 OVERTEMP WHEN IN ICING. REMOVED AND REPLACED THE FAN AIR FILTER ON BOTH ENGINES. 2 L 7 2 4F RT T00011AT 2002112600004 20021126 00004 SO 2002 11 26 000226 1 20021116 A 3150 WARNING SYSTEM EMB 145 EMB145 3260210 SO NR 2 T/R ACTIVATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 291 NR 2 ENGINE THRUST REVERSER DISAGREE ON TAKEOFF ROLL. RE-ENTERED NR 2 ENGINE THRUST REVERSER DISAGREE MESSAGE. 2 L 7 2 4F RT T00011AT 2002112600005 20021126 00005 SO 2002 11 26 000227 1 20021117 A 2120 DUCT EMB 145 EMB145 3260210 SO CABIN MELTED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 260 SMOKE IN CABIN. AIR CONDITIONING DUCT MELTED DUE TO DUCT BLOWOFF. RR'D THE AIR CONDITIONING DUCTS 2 L 7 2 4F RT T00011AT 2002112600006 20021126 00006 SO 2002 11 26 000228 1 20021124 A 4920 APU EMB 145 EMB145 3260210 SO APU BAY FAILED A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 11 279 APU SHUTDOWN, SMOKE AND BURNING ODOR FILLED AFT CABIN. DEFERRED. 2 L 7 2 4F RT T00011AT 2002112600007 20021126 00007 EU 2002 11 26 00055 1 20021024 A 2133 OUTFLOW VALVE AMD FALC20 FALCON 2720302 EU CABIN PRESSURE MALFUNCTIONED E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 165TW 65 AIRCRAFT DEPARTED AND CABIN WOULD NOT PRESSURIZE, RETURN FOR MAINTENANCE, RESET DUMP SWITCH TO NORMAL AND SAFETIED WITH BREAKAWAY WIRE. GROUND CHECK PERFORMED GOOD, RETURN AIRCRAFT TO SERVICE. 2 L 7 2 4F A7EU 2002112600008 20021126 00008 2002 11 26 00056 4 20021028 A 3422 25883023 GYRO AMD FALC20 FALCONE 2720305 EU COCKPIT FAILED E HAEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SW 05 285TW 285 AIRCRAFT DEPARTED AND PILOT DIRECTIONAL GYRO STOPPED MOVING, AIRCRAFT DIVERTED FOR MAINTENANCE, REMOVED AND REPLACED L EFT DIRECTIONAL GYRO, AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F A7EU 2002112600009 20021126 00009 CE 2002 11 26 00057 1 20021030 A 7931 B-NUT LEAR 24 24B 5170306 CE OIL PRESS XMITER LOOSE E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 233TW 24B221 DURING TAKEOFF RUN, CREW RECEIVED A LOW OIL PRESSURE LIGHT ON THE LT ENGINE AND ABORTED TAKEOFF. AFTER CLEARING THE RUN WAY, INDICATION WAS NORMAL. SHORTLY AFTER DEPARTING WITH INDICATIONS NORMAL, THE LOW OIL PRESSURE LIGHT AGAIN ILLUMIN ATED. THE CREW RETURNED TO DEPARTURE AIRPORT FOR MAINTENANCE. MAINTENANCE TIGHTENED B-NUT ON THE HIGH PRESSURE LINE AT THE OIL PRESSURE TRANSMITTER, SERVICED AND RAN ENGINE FOR LEAKS, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4J A10CE 2002112600010 20021126 00010 EU 2002 11 26 00058 1 20021031 A 3510 OXYGEN BOTTLE AMD FALC20 FALCON 2720302 EU CREW SYSTEM DISCHARGED E HAEA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 05 240TW 40 AIRCRAFT DEPARTED AND CREW DISCOVERED OXYGEN SUPPLY WAS AT ZERO, DIVERTED, HAD OXYGEN BOTTLE SERVICED. 2 L 7 2 4F A7EU 2002112600011 20021126 00011 CE 2002 11 26 00059 1 20021101 A 2742 66084444 CONTROL BOX LEAR 24 24D 5170311 CE TRIM CONTROL INOPERATIVE E HAEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 05 888TW 292 AIRCRAFT DEPARTED AND AFTER INTERMIDIATE LEVEL OFF, NORMAL PITCH TRIM WAS FOUND TO BE NOT WORKING. AIRCRAFT RETURNED TO DEPARTURE AIRPORT FOR MAINTENANCE USING EMERGENCY TRIM. REMOVED AND REPLACED TRIM SPEED CONTROL BOX, OPS CHECK GOOD. RETURN AIRCRAFT TO SERVICE. 2 L 7 2 4J A10CE 2002112600012 20021126 00012 NE 2002 11 26 00060 2 20021106 A 7261 5045T99P03 SEAL LEAR 24 24E 5170316 CE GE CJ610 CJ610* 30006 NE ENGINE OIL FAILED E HAEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 330TW 330 AIRCRAFT DEPARTED, ON THIRD LEG OF THE DAY, OIL PRESSURE DROPPED AND LOW OIL PRESSURE LIGHT ILLUMINATED. AIRCRAFT DIV ERTED, NO EMERGENCY DECLARED. MAINTENANCE WAS SENT, REMOVED AND REPLACED AXIS GEAR SEAL. AIRCRAFT SERVICED AND OPS CHEC K GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4J 4 J A10CE 1E16 2002112600013 20021126 00013 EU 2002 11 26 00061 1 20021104 A 2820 PUMP AMD FALC20 FALCON 2720302 EU FUEL TRANSFER MALFUNCTIONED E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 165TW 65 PILOT REPORTED, AIRCRAFT ENROUTE, LEFT FUEL TRANSFER PUMP FAILED AND UNABLE TO TRANSFER FUEL FROM WING TO WING. UNSHED ULED LANDING MADE. FERRY PERMIT ISSUED, AIRCRAFT MOVED FOR MAINTENANCE. MAINTENANCE CLEANED THE WING JET PUMPS IAW M/M. OPS CHECK NORMAL, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A7EU 2002112600014 20021126 00014 EU 2002 11 26 00062 1 20021111 A 3010 DEICE SYSTEM AMD FALC20 FALCON 2720302 EU LT WING LE DAMAGED E HAEA A UNSCHED LANDING E F VIBRATION/BUFFET FLT CONT AFFECTED CR CRUISE 1 SW 05 165TW 65 AIRCRAFT DEPARTED, AFTER REACHING ALTITUDE AND PILOTS DISCUSSED HOW THE AIRCRAFT WAS FLYING THEY NOTICED DAMAGE TO THE LEFT DLE. AIRCRAFT DIVERTED AND LANDING AT UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED LEFT WING CENTER SECTION OF DLE AND GAP SEAL, ALL OPS CHECK GOOD. AIRCAFT RETURN TO SERVICE. 2 L 7 2 4F A7EU 2002112600015 20021126 00015 CE 2002 11 26 00063 1 20021118 A 3260 INDICATOR LEAR 24 24 5170302 CE MLG MALFUNCTIONED E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 157TW 24157 AIRCRAFT DEPARTED, GEAR UNSAFE LIGHTS DID NOT GO OUT, AIRCRAFT RETURNED FOR UNEVENTFUL LANDING. AIRCRAFT FERRIED, D IRECT GEAR DOWN AND LOCKED FOR MAINTENANCE. WILL UPDATE AFTER MAINTENANCE. 2 L 7 2 4J A10CE 2002112600016 20021126 00016 NM 2002 11 26 0203596302 1 20021031 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. AFT OF ROW 52R, INSTALLED CONNECTOR ON LIGHT AT 52R. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002112600017 20021126 00017 NM 2002 11 26 0203606303 1 20021102 A 3397 WIRE BOEING 747 747451 1384940 NM EMERGENCY LIGHT DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 52ABC-61ABC. RESECURED WIRE CONNECTOR. OPERA TIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002112600018 20021126 00018 NM 2002 11 26 0203616313 1 20021102 A 3397 WIRE BOEING 747 747451 1384940 NM EMERGENCY LIGHT DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 673US 30268 DURING LINE CHECK FOUND ZONE D LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REINSTALLED WIRE, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002112600019 20021126 00019 NE 2002 11 26 0203623209 2 20021030 A 7200 ENGINE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 1 FAILED A NWAA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 01 309US 118 731305 DURING CRUISE FLIGHT, ENGINE NR 1 FLAMED OUT. FLIGHT CREW DIVERTED AIRCRAFT AND PERFORMED AN UNEVENTFUL LANDING. MAINT ENANCE FOUND THE ALTERNATOR/STATOR (PMA) DAMAGED AND METAL ON THE GEARBOX CHIP DETECTOR. ENGINE NR 1 REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2002112600020 20021126 00020 WP 2002 11 26 0203679947 1 20021009 A 5310 DOOR FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8938E 47161 WHILE IN FOR A L CHECK. A CRACK WAS FOUND IN THE LOWER FORWARD CORNER OF THE R1 SERVICE DOOR JAMB. REPAIRED PER EA. 2 L 7 2 4F A6WE 2002112600021 20021126 00021 WP 2002 11 26 0203689947 1 20021004 A 5310 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8938E 47161 DURING L CHECK, A CRACK WAS FOUND IN THE UPPER AFT CORNER OF THE R1 SERVICE DOOR JAMB. REPAIRED PER EA. 2 L 7 2 4F A6WE 2002112600022 20021126 00022 WP 2002 11 26 0203709981 1 20021031 A 5320 STIFFENER DOUG DC9 DC931 3022065 WP BULKHEAD CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 994Z 47097 DURING H CHECK, CORROSION WAS FOUND ON THE UPPER SURFACE OF STATION 756 BULKHEAD TEE BETWEEN LONGERONS 29R AND 30. REPA IRED PER EA. 2 L 7 2 4F A6WE 2002112600023 20021126 00023 EU 2002 11 26 YENA200230 1 20021123 A 2133 TECHNOFAN AIRBUS 320 A320232 3930326 EU A YENA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 15 543JB 2887 1823 Durning Takeoff Roll had vent avionics extract valve fault. Continued takeoff then returned aircraft to TPA. Corrective Action: Mel 21-26-04 applied. Subsequent removal and replacement of Outlet Valve IAW AMM 21-26-53. 2 L 7 2 4F RT A28NM 2002112600024 20021126 00024 NE 2002 11 26 0203743141 2 20021107 A 7200 BLADE AIRBUS A319 A319114 3930350 NM CFMINT CFM56 CFM565B5 NE NR 1 ENGINE BIRD STRIKE A NWAA A UNSCHED LANDING C E K F.O.D. VIBRATION/BUFFET FLUID LOSS CL CLIMB 1 GL 01 341NB 1738 AFTER TAKEOFF AT 500 FEET ENGINE NR 1 EXPERIENCED SEVERE VIBRATION. THRUST WAS REDUCED AND VIBRATION DECREASED. ENGINE NR 1 OIL LOSS WAS THEN NOTICED AND ENGINE NR 1 WAS SHUTDOWN. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT AND PER FORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND FOUR DAMAGED FAN BLADES DUE TO A BIRD STRIKE AND THE OIL OUT LINE OF THE FUEL/OIL HEAT EXCHANGER LOOSE. ENGINE BORESCOPE INSPECTION CHECKED GOOD. REPLACED 8 FAN BLADES, TIGHTENED OIL COOLER LINE AND PERFORMED ENGINE NR 1 RUNUP, VIBRATION LEVELS IN LIMIT. 2 L 7 2 4F 4 F RT A28NM E37NE 2002112600025 20021126 00025 NM 2002 11 26 0203756301 1 20021106 A 3350 LIGHT BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK FOUND ZONE 4 RIGHT SIDE FLOOR EMERGENCY PATH LIGHTS INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2002112600026 20021126 00026 NM 2002 11 26 0203876743 1 20021116 A 7711 SENSOR BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 3 ENGINE MALFUNCTIONED A NWAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 643NW 22245 702057 DURING TAKE-OFF ROLL, THE NR 3 ENGINE WOULD NOT REACH THE TARGET EPR OF 1.58. MAXIMUM EPR INDICATED ON THE NR 3 ENGINE WAS 1.47 WITH THE POWER LEVER AT THE FORWARD STOP. THE TAKE-OFF WAS ABORTED AT 100 KNOTS. MAINTENANCE INSPECTED THE PT7 LINE FOR LEAKS WITH NO DEFECTS FOUND. THE EPR TRANSMITTER AND THE TT2 SENSOR WERE BOTH REPLACED. AN ENGINE RUN WAS P ERFORMED AND TAKE-OFF EPR WAS REACHED. 2 L 7 4 4F 4 F A20WE E3NE 2002112600027 20021126 00027 EU 2002 11 26 0203883241 1 20021116 A 7932 TRANSMITTER AIRBUS 320 A320212 3930322 EU CFMINT CFM56 CFM565A3 NE ENG OIL QTY MALFUNCTIONED A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 341NW 380 731730 FLIGHT CREW ABORTED TAKE-OFF AT 110 KNOTS DUE TO ENGINE NR 1 OIL QUANTITY INDICATION RAPID DECREASE. AIRCRAFT RETURNED TO GATE. MAINTENANCE FOUND ENGINE NR 1 TANK FULL AND NO ENGINE OIL LEAKS. REPLACED OIL QUANTITY TRANSMITTER. 2 L 7 2 4F 4 F RT A28NM E29NE 2002112600028 20021126 00028 NM 2002 11 26 02102802 1 20021027 A 2760 COMPUTER BOEING 757 75728A 1384976 NM SPOILER CONFIG MALFUNCTIONED A N8TA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 19 551NA 25621 SPOILER CONFIGURATION LIGHT AND HORN ON TAKEOFF. ABORTED TAKEOFF, RETURNED TO GATE TO RESET COMPUTER AND CHECK. PERF ORMED SPOILER SYSTEM OPS CHECK AS PER M/M. OPS CHECK NORMAL, NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT A2NM 2002112600029 20021126 00029 CE 2002 11 26 02341 1 20021022 A 2435 BEARING RKWELL NA265 NA26565 7630107 CE GARRTT TFE731 TFE7313R1D 01518 WP STARTER GEN FAILED E DGCA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CE 03 265M 577 1590 46531 P83151 PILOT BEGAN FEELING VIBRATION FROM LEFT ENGINE, LEFT GENERATOR HOT LIGHT CAME ON, FOLLOWED BY GENERATOR FAILURE. 2 L 7 2 4J 4 F A2WE E6WE 2002112600030 20021126 00030 NE 2002 11 26 02FDEA00700 2 20020927 A 7320 HMU AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 2 ENGINE FAULTY A FDEA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 25 661FE 760 NR 2 ENGINE FF 2500-5000 LB FLUCTUATION- ON CLIMB OUT, NOTICED FLUCTUATING FUEL FLOW EFFECTING A SPIKE IN N1 (5-10 PERC ENT) EGT TEMP VARY 3-5 DEGREES ALONG WITH A SLIGHT N2 SPIKE (2 PERCENT) NOTIFIED MECHANIC, RETURNED TO LANDING RWY 36 R. TAXI IN, INSTRUMENTS APPEARED NORMAL. REMOVED AND REPLACED NR 2 HMU IAW MM. IAW MOCC REQUEST REMOVED AND REPLACED N R 2 MAIN FUEL FILTER IAW A300 MM. ALL CHECKS COMPLIED WITH NORMALLY. 2 L 7 2 4F 4 F RT A35EU E13NE 2003031400024 20030314 00024 WP 2003 3 14 02FDEA00720 1 20021008 A 5753 FLAP TRACK DOUG MD10 MD1010F WP TE FLAP VANE DAMAGED A FDEA O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED LD LANDING 1 SO 25 566FE 46989 EXCESSIVE LT WING DOWN INPUT REQUIRED TO HOLD LEVEL FLIGHT ON APPROACH AFTER FLAPS 50 SELECTED. AIRCRAFT WOULD ROLL AGG RESSIVELY TO RT IF PILOT RELEASE PRESSURE ON YOKE. WINDS 110 AT 4KTS LANDING 16L AT AFW. DIRECTIONAL CONTROL WAS POSSI BLE BUT CREW ALSO NOTED LEVEL 3 STAB TRIM ALERT AFTER LANDING AND 11.1 ANU UNITS BOXED AMBER. STAB RAN W/O CREW INPUT A T TOUCHDOWN. *S/D* REMOVED AND REPLACED ALL THREE FLAP VANE TRACK ASSY AND REINSTALLED INBOARD FLAP VANE TO INBOARD FL AP, REMOVED AND REPLACED INBOARD FLAP SPRING CARTRIDGE AND ADJUSTED VANE PER MM 27-50-03-2. 2 L 7 3 4F RT A22WE 2002112600031 20021126 00031 NE 2002 11 26 2002F01027 2 20021113 A 7310 37D401672P106 LINE LEAR 24 24E 5170316 CE GE CJ610 CJ610* 30006 NE RT ENGINE CRACKED B O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 21 207RG 339 211070A PILOT REPORTED AN UNSATISFACTORY INDICATION OF RT ENGINE ANTI-ICE SYSTEM. AFTER REMOVING ENGINE COWLING, ANTI-ICE VALVE BLEED AIR SUPPLY LINE CONNECTOR HOSE WAS FOUND TO BE RUPTURED AND COMPLETELY TORN FREE. ANTI-ICE VALVE BLEED AIR SUPPLY LINE HAD ALSO CRACKED AT WELD AROUND THE MOUNTING FLANGE AND COMPLETELY PULLED AWAY FROM THE ANTI-ICE VALVE. HOT BLEED AIR WAS BLOWING DIRECTLY ON ANTI-ICE VALVE CANON PLUG WHICH MELTED PIN SOLDER, ALLOWED ELECTRICAL WIRE TO PULL OUT OF CA NON PLUG INTO ENG COMPARTMENT. NOTE: REPLACEMENT BLEED AIR LINE WAS ORDERED AND DURING AN INSPECTION FOUND TO BE CRACKED AT THE SAME LOCATION (AROUND THE WELD AT THE MOUNTING FLANGE). 2 L 7 2 4J 4 J A10CE 1E16 2002112600032 20021126 00032 CE 2002 11 26 2002F01024 1 20021120 A 3320 6900042 POWER SUPPLY BEECH 200 200BEECH 1152920 CE CABIN FAILED E DDNA E D ENGINE SHUTDOWN RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 27 911MN 9000 BB229 MECHANICS REPORT-PILOTS REPORTED SPARKING AND ELECTRICAL BURNING SMELL UPON AIRCRAFT START UP. AIRCRAFT WAS SHUT DOWN. UPON INSPECTION BOTTOM OF POWER SUPPLY MELTED AND INTERNAL COMPONENTS MELTED AND DESTROYED. IT CAUSED TWO SQUARE IN CHES OF INSULATION TO BE SINGED AND ASH DEPOSITS TO BE LEFT IN AREA OF PROBLEM. EXACT LOCATION IS ABOVE RIGHT SIDE WIN DOW 2 AFT IN CABIN AREA. INSPECTED ALL POWER SUPPLIES IN CABIN AND NO SIGNS OF DEFECTS FOUND. 1 L 7 2 4T A24CE 2002112600035 20021126 00035 SO 2002 11 26 BGS2002F00000 1 20021106 A 8120 LW15456 CHECK VALVE PIPER PA32 PA32R301T 7103220 SO LYC O540 TIO540* 41532 EA TURBO CHARGER FAILED B BGSR O OTHER O OTHER NR NOT REPORTED 1 EA 21 521AS 32R8229051 L677361A TURBO CHARGER FAILED AT 450 HOURS. INVESTIGATION POINTS TO THE POSSIBILITY OF A RESTRICTED CHECK VALVE AT TURBO OIL POR T INLET, PREVENTING PROPER OIL FLOW TO THE TURBINE. VALVE HAS NOT BEEN DISTURBED, AWAITING FURTHER INVESTIGATION BY OUT SIDE AGENCY IF DESIRED. 1 L 7 1 3O 3 O A3SO E14EA 2002112600036 20021126 00036 CE 2002 11 26 CGO2002F00004 1 20021030 A 2810 10138901153 RELIEF VALVE BEECH 36 B36TC 1151609 CE CONT O520 TSIO520* 17040 SO FUEL SYSTEM INOPERATIVE A CGOR K NONE O OTHER IN INSP/MAINT 1 GL 03 400WT 184 EA690 VERIFIED COMPLAINT OF FUEL TANKS UNDER PRESSURE WHEN FILLED IN COLDER WEATHER THEN AIRCRAFT HANGARED IN WARMER TEMPERATU RE AREA. FUEL SPRAYING OUT UNDER PRESSURE WHEN FILLER CAPS REMOVED. FOUND FUEL VENT SYSTEM LEFT, RIGHT PRESSURE RELIE F VALVES TO BE OPERATING AT APPROX 8 PSI, VERIFIED W/RAC TECH SUPPORT SHOULD BE OPENING AT 1.5 PSI TO .18 PSI. REPLACED PRESSURE RELIEF VALVE ASSEMBLIES. REMOVED VALVE ASSEMBLIES MANUFACTURED BY COMMERCIAL AIRCRAFT PRODUCTS. MFG CODE 440 600 NOTED TO BOTH VALVE ASSEMBLIES. 1 L 7 1 3O 3 O 3A15 E8CE 2002112600038 20021126 00038 CE 2002 11 26 044616 1 20021030 A 3297 WIRE BEECH 1900 1900D 1154162 CE MLG ACTUATOR FAILED A AMWA A UNSCHED LANDING P NO WARNING INDICATION LD LANDING 1 CE 07 231YV 10643 10643 UE231 UPON LANDING IN PITTSBURGH, THE CREW REPORTED THAT THE NOSE GEAR ANNUNCIATOR DID NOT ILLUMINATE IN GEAR DOWN POSITION. T HE BULB WAS THEN CHECKED WHICH WAS FOUND TO BE OKAY. THE CREW MANUALLY LOWERED THE GEAR PER THE CHECKLIST. THEN THEY DEC LARED AN EMERGENCY LANDING IN PITTSBURGH WITHOUT INCIDENT. REMOVED AND REPLACED THE NOSE GEAR ACTUATOR / SWUNG GEAR. THE TEARDOWN REPORT REVEALED THAT THEY FOUND SWITCH WIRES BROKEN OFF AT SWITCH. CORROSION ON BARREL IS EXCESSIVE AND MUST B E REPLACED. 2 L 7 2 4T RT A24CE 2003022000101 20030220 00101 CE 2003 2 20 044935 1 20021111 A 2822 SHAFT BEECH 1900 1900D 1154162 CE FUEL PUMP BROKEN A AMWA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CE 07 233YV 12 12 B835 UE233 A REPORT OF THE RT ENGINE LEAKING FUEL FROM THE GANG DRAIN. IN THE REPORT THEY FOUND THE RT ENGINE DRIVEN LOW PRESSURE F UEL PUMP LEAKING DUE TO INTERNAL FAILURE. REMOVED AND REPLACED THE LT HAND PRESSURE FUEL PUMP. UPON RECEIPT OF THE TEARD OWN REPORT FROM THE VENDOR, THEY DISASSEMBLED THE PART FOR INSPECTION. THEY FOUND THAT THE RELEIF VALVE WAS PITTED AND SEAL WAS DAMAGED. ALL THE OTHER MAJOR COMPONENTS WERE WITHIN MANUFACTURING TOLERANCES. THE VENDOR PROCEEDED TO FIX THE P ART. THEY LAPPED RELIEF VALVE AND HOUSING, REASSEMBLED WITH OVERHAUL KIT AND OVERHAULED AND TESTED AS PER MANUFACTURING SPECIFICATIONS. THEN IT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2002112600039 20021126 00039 CE 2002 11 26 044989 1 20021112 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE LT ENGINE BROKEN A AMWA K NONE L NO TEST IN INSP/MAINT 1 CE 07 126YV UE126 DURING CREW CHANGEOVER IN ALBUQUERQUE, THE PILOTS DISCOVERED THAT THE LT FIRE HANDLE ILLUMINATED DURING PREFLIGHT CHECKS . THE LIGHT WOULD NOT EXTINGUISH. THE CORRECTIVE ACTION WAS THAT MAINTENANCE FOUND THE FORWARD LOOP BROKE. THEY INSTALLE D A NEW LOOP. NO TEARDOWN WILL BE REQUIRED. 2 L 7 2 4T RT A24CE 2002112600040 20021126 00040 CE 2002 11 26 045127 1 20021116 A 3260 ANNUNCIATOR BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER P NO WARNING INDICATION LD LANDING 1 CE 07 159YV UE159 UPON LANDING IN PHOENIX, THERE WAS UNSAFE GEAR INDICATION ON MLG (PER BOTTOM ANNUNCIATOR) UPON NORMAL GEAR EXTENSION. TH E BOTTOM MAIN GEAR ANNUNCIATOR WOULD NOT ILLUMINATE. PERFORMED TOWER FLY BY AND TOWER SAID IT LOOKED OKAY. FINALY GOT A DOWN AND LOCKED INDICATION (ALL ANNUNCIATORS) AFT THE 3RD ATTEMPT WAS MADE TO PUMP GEAR DOWN. RESISTANCE WAS FELT, BUT S TILL NO GREEN AFTER FIRST TWO ATTEMPTS. PERFORMED NORMAL LANDING AND THE GROUND EQUIPMENT TOWED THE AIRPLANE FROM THE RU NWAY. THE CORRECTIVE ACTION WAS THAT THEY INSPECTED THE GEAR INDICATION CHECKED THE ANNUNCIATOR. THEY CYCLED GEAR 5 TIME S AND COULD NOT DUPLICATE. PERFORMED CHECK FLIGHT OF AIRCRAFT AND WAS RETURNED TO SERVICE. NO PARTS WERE USED. 2 L 7 2 4T RT A24CE 2002112600041 20021126 00041 CE 2002 11 26 045208 1 20021119 A 2130 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE CABIN PRESSURE OUT OF ADJUST A AMWA G O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 CE 07 3199Q UE213 DURING THE CLIMB PHASE ON FLIGHT 106 FROM COLORADO SPRINGS TO ALBUQUERQUE, THE HIGH ALTITUDE ANNUNCIATOR ILLUMINATED. TH E OXYGEN MASK WAS DEPLOYED. THE APPROPRIATE MEMORY ITEMS AND THE CABIN ALTITUDE HIGH EMERGENCY CHECKLIST WAS COMPLETED. DURING THE DESCENT, THE CABIN ALTITUDE HIGH ANNUNCIATOR EXTINGUISHED. FURTHER DESCENTS WERE APPROVED AS THE TERRAIN PERM ITTED. THE MASKS REMAINED DOWNED AS A PRECAUTION UNTIL AIRCRAFT DESCENDED THROUGH 10,000FEET. THE AIRCRAFT LANDED WITHOU T INCIDENT. THE CORRECTIVE ACTION WAS THAT THEY REMOVED AND RE-ADJUSTED THE CABIN ALT PRESSURE SWITCH. NO PARTS WERE USE D. 2 L 7 2 4T RT A24CE 2002112600043 20021126 00043 CE 2002 11 26 2002F01026 1 20021113 A 7500 37D401672P106 LINE LEAR 24 24E 5170316 CE GE CJ610 CJ610* 30006 NE RT ENGINE CRACKED B A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 21 207RG 339 211070A DURING IN-FLIGHT OPERATIONS THE PILOT REPORTED AN UNSAT INDICATION OF THE RT ENGINE ANTI-ICE SYS. AFTER REMOVING THE COW LING, THE ANTI-ICE VALVE BLEED AIR SUPPLY LINE CONNECTOR HOSE WAS FOUND TO BE RUPTURED AND COMPLETELY TORN FREE. THE ANT I-ICE VALVE BLEED AIR SUPPLY LINE HAD ALSO CRACKED AROUND THE MOUNTING FLANGE AND COMPLETELY PULLED AWAY FROM THE ANTI-I CE VALVE. HOT BLEED AIR WAS NOW BLOWING DIRECTLY ONTO THE ANTI-ICE VALVE CONNECTOR PLUG WHICH MELTED THE PIN SOLDER AND ALLOWED THE ELECTRICAL WIRE TO PULL OUT OF THE PLUG INTO THE ENGINE BAY. IT SHOULD ALSO BE NOTED THAT AN AS REMOVED REPL ACEMENT BLEED AIR LINE WAS ORDERED AND DURING AN INCOMING INSPECTION FOUND TO BE CRACKED AT THE SAME LOCATION. 2 L 7 2 4J 4 J A10CE 1E16 2002112600044 20021126 00044 CE 2002 11 26 8393298 1 20021114 A 2430 1293800161 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT GENERATOR INOPERATIVE G JJBA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 01 839CA 3093 RT GENERATOR FELL OFF LINE IN FLIGHT AND FLIGHT CREW WAS UNABLE TO TIE RIGHT GENERATOR BUS BACK TO ELECTRICAL SYSTEM. MA INTENANCE REPLACED RIGHT DC POWER A257 BUS TIE CONTROL PCB ASSEMBLY. 2 L 7 2 4T 3 T RT A24CE E2NE 2002112600045 20021126 00045 WP 2002 11 26 CALA0200564 1 20021125 A 5350 CABLE DOUG DC9 DC982 3022082 WP TAILCONE FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 98876 49444 THE TAILCONE DROP TEST FAILED AT EACH OF THREE LOCATIONS. MAINTENANCE FOUND THE LEFT UPPER TAILCONE JETTISON CABLE FRAYE D IN TWO PLACES. THE CABLE WAS REMOVED AND REPLACED. PERFORMED ADJUSTMENT OF TAILCONE RELEASE SYSTEM IAW MM 53-53-00. 2 L 7 2 4F A6WE 2002112600046 20021126 00046 NM 2002 11 26 CALA0200565 1 20021125 A 5320 WEB BOEING 737 737524 1384721 NM STA 344-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27610 27323 INSPECTION FOUND A 2" CRACK IN WEB AT STA 344-360, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002112600047 20021126 00047 2002 11 26 AMTA200201440 4 20021124 A 2565 D30170557 SLIDE LKHEED 1011 1011385115 5265015 WP PAX DOOR DEPLOYED G AMTT O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 GL 11 198AT 193B1111 L1 DOOR SLIDE INADVERTENTLY DEPLOYED FROM SLIDE COVER. 2 L 7 3 4F A23WE 2002112600048 20021126 00048 NM 2002 11 26 ANZF2002 1 20020901 A 5753 65B3902529 FITTING BOEING 747 747400 NM TE FLAP BROKEN G ANZF O OTHER P D F NO WARNING INDICATION INFLIGHT SEPARATION FLT CONT AFFECTED CL CLIMB 1 WP 23 ZKNBS 61156 24386 AFTER DEPARTURE, THE RT INBOARD FORE FLAP ATTACH POINT FAILED. THE BROKEN (HALF ROUND) ATTACH PIECE WAS RECOVERED FROM T HE CANOE BY MAINTENANCE. SUBSEQUENT VIBRATION AND FLUTTER CAUSED THE FLAP TO BREAK INTO THREE PIECES OF WHICH THE TWO T HIRDS ON THE INBOARD SIDE DEPARTED THE AIRCRAFT. FLIGHT CREW WAS UNAWARE OF THE INCIDENT AND CONTINUED THE FLIGHT. LATER , TRANSPORTATION AUTHORITIES RECOVERED THE TWO PIECES OF THE FLAP FROM THE BAY UNDER THE DEPARTURE END OF THE AIRPORT. A IRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT TWO THIRDS OF THE FORE FLAP WAS MISSING. SECONDARY DAMAGE WAS SUSTAINED TO THE MID FLAP, THE FUSELAGE, AND THE OUTER FLAP WELL WING RIB ALONG WITH OTHER RELATED SYSTEMS. 2 L 7 4 4F RT A20WE 2002112600049 20021126 00049 EU 2002 11 26 MALA020665 1 20021125 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 423XJ 340B423 CARGO SMOKE DETECTION SYSTEM WOULD NOT TEST. AIRCRAFT FERRIED FROM MLI TO MSP FOR FURTHER REPAIR AND TROUBLESHOOTING OF CARGO SMOKE DETECTION. MAINTENANCE REMOVED AND REPLACED CARGO SMOKE DETECTOR PER AMM 26-13-15-4 OPS CHECKS GOOD. PN CGA B1201-01 SN/OFF 750, SN/ON 088. 2 L 7 2 4T RT A52EU 2002112600050 20021126 00050 WP 2002 11 26 MWEA020719 1 20021122 A 3010 SYLZ9885 SWITCH DOUG DC9 DC932 3022066 WP LH ENGINE DEFECTIVE A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 501ME 47132 AFTER LEFT ENGINE START LEFT AIRFOIL ICE PROTECTION TEMPERATURE LIGHT CAME ON. -- REMOVED AND REPLACED ELECTRONIC THER MAL SWITCH CONTROL. 2 L 7 2 4F A6WE 2002112600051 20021126 00051 SO 2002 11 26 C2XA02CL231 1 20021125 A 3260 BJE61 DIODE EMB 135 EMB135LR 3260305 SO COCKPIT INTERMITTENT A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 28529 145512 CLE FLIGHT#3001 THE CREW REPORTED A LANDING GEAR INTERMITTENT AURAL WARNING DURING FLIGHT.MAINTENANCE INSPECTED AND REPL ACED THE AURAL WARNING DIODE CR105.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002112600052 20021126 00052 WP 2002 11 26 ZW0A021171 1 20021125 A 3350 7742 LAMP DOUG DC9 DC983 3022083 WP BURNED OUT A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9619V 53566 EGRESS LIGHTING INOP BETWEEN ROWS 21 AND 28. RELAMPED SECTION OF LIGHTS. LAST CHECK C PERFORMED IN STL 10/30/2002 --CLOS ED-- 2 L 7 2 4F RT A6WE 2002112600053 20021126 00053 NE 2002 11 26 L10666 3 20021030 A 6111 E7016 CLAMP BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3A NE PROPELLER CRACKED B O OTHER O OTHER IN INSP/MAINT 1 EA 13 855CA UE392 HJ1428 PROPELLER WAS RECEIVED FOR OVERHAUL AND DURING DYE PENETRANT INSPECTION TWO CRACK INDICATIONS WERE NOTED IN THE BOLT HOL E AREA. THEN AN EDDY CURRENT INSPECTION WAS PERFORMED WHICH CONFIRMED PRIOR INDICATIONS. CLAMP WAS RED TAGGED AND REMOVE D FROM SERVICE. PART RETURNED TO HARTZELL PROPELLER FOR FURTHER EVALUATION. 2 L 7 2 4T RT A24CE 5 C P10NE 2003011700032 20030117 00032 WP 2003 1 17 ARWA20021109 1 20021120 A 2910 240000060166 HYDRAULIC LINE DOUG DC8 DC863 302198A WP THRUST REVERSER LEAKING A ARWA O OTHER K FLUID LOSS LD LANDING 1 SO 19 345JW 46042 LOSS OF HYDRAULIC FLUID ON LANDING. REMOVED AND REPLACED PRESSURE HYDRAULIC LINE ON REVERSER PUMP. LEAK CHECK NORMAL I AW MM 29-10-0. 2 L 7 4 4F 4A25 2002112600056 20021126 00056 NM 2002 11 26 2002UALA01614 1 20021022 A 2450 91252ZC7C4001 RELAY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ELECTRICAL SYS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 344UA 24248 AIRCRAFT RETURNED TO FIELD WHEN NUMBER 2 GENERATOR CIRCUIT BREAKER TRIPPED, UNABLE TO RESET. REPLACED TRANSFER RELAYS R 3 AND R4. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600058 20021126 00058 NM 2002 11 26 2002UALA01616 1 20021022 A 2131 11511007 CONTROLLER BOEING 777 777222 1385219 NM CABIN PRESSURE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 223UA 30224 BOTH LEFT AND RIGHT AUTO CABIN PRESSURE CONTROLLERS INOP. EICAS CABIN ALT AUTO MESSAGE RECEIVED. BOTH LT & RT ASCPC (A IR SUPPLY & CABIN PRESSURE CONTROLLER) FAILED DUE TO INTERNAL FAULT. BOTH ASCPC'S LOST PRIMARY CONTROL RESULTING IN CAB IN PRESSURE CONTROL SYSTEM ON MANUAL CONTROL. BOTH ASCPC WERE REPLACED, AND A/C RETURNED TO REVENUE SERVICE WITHOUT FUR THER INCIDENT. HONEYWELL IS RELEASING A NEW ASCPC SOFTWARE UPGRADE TO FIX THIS PROBLEM SB 1151100-36-39, BOEING SB 777- 36-0013. 2 L 7 2 4F RT T0001SE 2002112600059 20021126 00059 NE 2002 11 26 2002UALA01617 2 20021019 A 7230 ENGINE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RIGHT BIRD STRIKE A UALA E A ENGINE SHUTDOWN UNSCHED LANDING C E M F.O.D. VIBRATION/BUFFET OVER TEMP CL CLIMB 1 WP 29 607UA 21868 709621 BIRD STRIKE TO RIGHT ENGINE. RETURNED TO FIELD. THE BIRD STRIKE CAUSED THE FAILURE OF A FAN BLADE. THE TIP OF THE FAN BLADE LIBERATED INBOARD OF THE MIDSPAN SHROUD, WHICH CAUSED ABNORMAL VIBRATION AND OVERTEMP. THE ENGINE WAS SHUT DOWN AND RETURNED TO FIELD. THE ENGINE WAS REPLACED DUE TO HEAVY DAMAGE AND OVERTEMP. 2 L 7 2 4F 4 F RT A1NM E3NE 2002112600060 20021126 00060 NM 2002 11 26 2002UALA01620 1 20021027 A 5312 PRESSURE PANEL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 950UA 26695 RIGHT WHEEL WELL CEILING ABOVE THE SPOILER MIXER HAS EXCESSIVE MATERIAL REMOVED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600061 20021126 00061 NM 2002 11 26 2002UALA01621 1 20021024 A 3350 58783 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 359UA 24452 EMERGENCY EXIT LIGHTS BETWEEN ROWS 3 AND 10 AND 17 TO THE AFT CABIN INOPERATIVE. REPLACED POWER STRIP 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600062 20021126 00062 NM 2002 11 26 2002UALA01622 1 20021025 A 5512 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 950UA 26695 RT HORIZONTAL STABILIZER LEADING EDGE APPROXIMATELY MIDWAY HAS A SERIES OF DENTS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER AND REINSTALLED LEADING EDGE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600063 20021126 00063 SO 2002 11 26 LR7A02122 1 20021120 A 5312 RISER LKHEED 382 382G 526414U SO FS477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 553 4590 DURING SCHEDULED B3 INSPECTION PER HB0506 FOUND RH MLG BAY FWD PRESSURE BULKHEAD PANEL RISER CRACKED. FS477, RBL60, WL1 90.REPAIRED PANEL IAW SRM SMP 583 FIG 53-40-10. NR0024. 2 H 7 4 4T A1SO 2002112600064 20021126 00064 SO 2002 11 26 LR7A02123 1 20021120 A 5330 FRAME LKHEED 382 382G 526414U SO FS94 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 553 4590 DURING SCHEDULED B3 INSPECTION PER HB0502 FOUND PILOT DV WINDOW FRAME CRACKED. 0.25 INCHES LONG STARTING AT RADIUS OF LO WER FWD CORNER OF WINDOW FRAME AND RUNNING FWD AND DOWN. FS94, LBL10, WL231.REPAIRED PILOTS DV WINDOW FRAME IAW SRM SMP 583 FIG 53-30-27. NR0050. 2 H 7 4 4T A1SO 2002112600065 20021126 00065 SO 2002 11 26 LR7A02124 1 20021120 A 5311 CAP LKHEED 382 382G 526414U SO FS858 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 553 4590 DURING SCHEDULED B3 INSPECTION PER HB0505 FOUND TEE CAP CRACKED. FS858, BL66, WL186.REPAIRED TEE CAP IAW SRM SMP 583 FI G 51-140-22. NR0075. 2 H 7 4 4T A1SO 2002112600066 20021126 00066 SO 2002 11 26 LR7A02125 1 20021120 A 5330 CAP LKHEED 382 382G 526414U SO FS317 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 553 4590 DURING SCHEDULED B3 INSPECTION PER HB0502 FOUND LOWER BELLY FRAME CAP CORRODED. FS317, BL0, WL126.REPAIRED FRAME CAP IA W SRM SMP 583 FIG 53-40-29. NR0085. 2 H 7 4 4T A1SO 2002112600068 20021126 00068 NM 2002 11 26 2002UALA01624 1 20021025 A 2121 732591F BEARING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RECIRC FAN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 199UA 21608 28717 SMOKE IN CABIN BY ROW 6. STATUS MESSAGE RECIRC FAN LOWER R. THE LOWER RIGHT HAND RECIRCULATION FAN BEARING FAILED. TH E FAN WAS REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 2002121700202 20021217 00202 NM 2002 12 17 2002UALA01628 1 20021024 A 2120 VALVE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GROUND COOLING MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 619UA 21879 UNABLE TO CONTROL CABIN ALTITUDE. CABIN AT 9400 FT, AIRCRAFT AT 11000 FT. THE SAME IN AUTO 1 AND AUTO 2. IN MANUAL, C ABIN ALTITUDE INCREASED BY 200 FPM. RETURNED TO FIELD. THE LEFT AND RIGHT OUTFLOW VALVES ACTUATORS AND THE CABIN PRES SURIZATION ALTIMETER WERE REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. THE AIRCRAFT RETURNED TO THE FIELD AGAIN FOR A SIMILAR PROBLEM ON 30 OCT, 2002. THE GROUND EQUIPMENT COOLING VALVE WAS FOUND TO BE THE ROOT CAUSE OF THE PROBLEM. 2 L 7 2 4F 4 F RT A1NM E3NE 2002112600069 20021126 00069 NE 2002 11 26 2002UALA01629 2 20021024 A 7313 PUMP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 1 ENG FUEL FLUCTUATES A UALA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 615UA 21876 FROM TAKE OFF TO ABOUT 6000 FT AT REDUCED CLIMB THRUST, NR 1 ENGINE FLUCTUATED ABOUT 4 PERCENT (N1). STABILIZED AFTER T HAT. SUPPLEMENTAL DATA UPDATE FUEL CONTROL AND FUEL PUMP REPLACED PER MM. ENGINE RUN, CHECKED OK. FP AND FCU ROUTED T O OSV. 2 L 7 2 4F 4 F RT A1NM E3NE 2002112600070 20021126 00070 2002 11 26 2002UALA01631 4 20021029 A 3460 B546CCM0104 FMC AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 452UA 955 FLIGHT DIVERTED DUE TO A FLIGHT CONTROL UNIT FAULT. UPPER ECAM MESSAGE AUTO FLIGHT "FCU 1 FAULT". REPLACED FLIGHT MAN AGEMENT & GUIDANCE COMPUTER FMGC NR 1. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112600071 20021126 00071 EU 2002 11 26 2002UALA01632 1 20021025 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 465UA 1341 DENT TO FUSELAGE APPROXIMATELY 1 FOOT BELOW FORWARD CUTOUT OF DOOR 2L. DAMAGE CONSISTS OF AN APPROXIMATE 2 INCH DIAMETE R DENT. DENT IS DEEP BORDERING ON PUNCTURE. UNDERLYING RIB IS ALSO DENTED. MAJOR REPAIR ACCOMPLISHED, MANUFACTURED DO UBLER & INSTALLED FASTENERS. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112600072 20021126 00072 NM 2002 11 26 2002UALA01634 1 20021030 A 5512 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HORIZ STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 946UA 26687 LT HORIZONTAL STABILIZER LEADING EDGE SKIN HAS EXCESSIVE MATERIAL LOSS 50 INCHES FROM INBOARD END. MAJOR REPAIR ACCOMPL ISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600073 20021126 00073 NE 2002 11 26 2002UALA01635 2 20021030 A 7200 ENGINE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 2 FAILED A UALA A UNSCHED LANDING R Y PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CL CLIMB 1 WP 29 607UA 21868 COMPRESSOR STALL NR 2 ENGINE AT 2,500 FEET. ENGINE SHUTDOWN, RETURNED TO FIELD. SUPPLEMENTAL DATA UPDATE POST FLIGHT EX AM SHOWED N2 SYSTEM FROZEN. CHIP DETECTORS FULL . ENGINE WAS LEASED FROM AIR CANADA, 97 HRS OUT OF A FULL OVERHAUL. ENGINE RETURNED TO LESSOR FOR FAILURE INVESTIGATION. 2 L 7 2 4F 4 F RT A1NM E3NE 2002112600075 20021126 00075 CE 2002 11 26 ROSA200200001 1 20021008 A 2910 AN8376D ELBOW LEAR 35 35A 5170602 CE HYD LINE LOOSE E ROSA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 01 135DE 830 830 667 LOST ALL HYDRUALIC PRESSURE IN FLIGHT, AUX PRESSURE WORKED OK. FOUND HYDRUALIC LEAK IN LEFT MAIN GEAR WELL AIRFRAME FITT ING TO RETRACT SIDE OF MAIN GEAR ACTUATOR. TIGHTENED FITTING TO RETRACT ACTUATOR PER LEARJET MAINTENANCE MANUAL 20-30-0 0, SERVICED RESERVIOR PERFORMED RETRACTION AND EXTENSION FUNCTION CHECK OF LANDING GEAR PER LEARJET MAINTENANCE MANUAL 3 2-33-00 APGE 201, SERVICED EMERGENCY AIR BOTTLE AND PERFORMED OPERATIONAL CHECK OF ENGINE DRIVEN HYDRUALIC PUMPS, ALL SY STEMS FUNCTION CHECK SATISFACTORY AIRCRAFT RETURNED TO SERVICE.AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A10CE 2002112600077 20021126 00077 NM 2002 11 26 2002UALA01637 1 20021030 A 7930 OIL FILTER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 607UA 21868 NR 2 ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED. ALL OTHER ENGINE PARAMETERS NORMAL. SUPPLEMENTAL DATA UPDATE ENGINE LEASED FROM AIR CANADA. OIL FILTERS AND CHIP DETECTORS CHECKED OK.OIL FILTER DIFFERENTI AL SWITCH CHECKED OK IN COMPONENT SHOP. ENGINE FAILED NEXT DEPARTURE . 2 L 7 2 4F 4 F RT A1NM E3NE 2002121900026 20021219 00026 NM 2002 12 19 2002UALA01638 1 20021030 A 3610 33990047U1 CONTROLLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE MALFUNCTIONED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 548UA 25396 727249 LT ENGINE HIGH STAGE CAUTION ON EICAS AND HIGH STAGE LIGHT ILLUMINATED AT APPROX 40 KTS. REPLACED LT ENGINE HIGH STAGE CONTROLLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121700204 20021217 00204 NM 2002 12 17 2002UALA01639 1 20021030 A 2120 3209953 VALVE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GROUND COOLING FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 619UA 69179 1395 21879 UNABLE TO PRESSURIZE THE CABIN. FLIGHT RETURNED TO FIELD. THIS AIRCRAFT HAD A SIMILAR PROBLEM ON 10/24/02. THE GROUND EQUIPMENT COOLING EXHAUST VALVE FAILED OPEN. THE VALVE WAS FOUND TO HAVE WORN BEARINGS AND INTERNAL PARTS CAUSING INTE RMITTENT OPERATION. 2 L 7 2 4F 4 F RT A1NM E3NE 2002112700010 20021127 00010 NM 2002 11 27 2002UALA01640 1 20021030 A 3350 58674 INVERTER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 356UA 24362 EMERGENCY ELECTRICAL LIGHTING STRIP INOPERATIVE THE LAST FOUR ROWS OF COACH. INOPERATIVE INVERTER AND POOR LIGHT STRIP CONNECTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600078 20021126 00078 NM 2002 11 26 CALA0200535 1 20021108 A 3350 FUSE BOEING 767 767424ER 1385270 NM POWER SUPPLY BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 66057 29452 THE EMERGENCY LIGHTS ON PASSENGER SEATS ROW 23-28 LT AND RT SIDE WERE FOUND INOPERATIVE. INSPECTION FOUND LOOSE CONNECTO R AT SEAT 22D AND BLOWN FUSE IN POWER SUPPLY FOR EMERGENCY LIGHTS AT STA 785 RT SIDE. SECURED LOOSE CONNECTOR AND REPLAC ED POWER SUPPLY. 2 L 7 2 4F RT A1NM 2002112600079 20021126 00079 WP 2002 11 26 CALA0200536 1 20021108 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 98876 49444 INSPECTION FOUND FLOOR SUPPORT BETWEEN PANEL H AND G CORRODED AT STA 148.5 TO 200. REMOVED AND REPLACED FLOOR SUPPORT IA W SRM 51-30-0. 2 L 7 2 4F A6WE 2002112600080 20021126 00080 NM 2002 11 26 2002UALA01641 1 20021031 A 5320 INTERCOSTAL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 946UA 26687 INTERCOSTAL CRACKED BETWEEN BS188 AND BS196 FUSELAGE FRAMES AT STRINGER 17 RIGHT HAND. MAJOR REPAIR ACCOMPLISHED. REPL ACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600081 20021126 00081 WP 2002 11 26 CALA0200538 1 20021109 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 98876 49444 INSPECTION FOUND FORWARD ENTRY I/B FLOOR SUPPORT FOR PANEL K AND O/B SUPPORT FOR PANEL I AND J CORRODED THE FLOOR SUPPOR TS WERE REMOVED AND REPLACED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 2002112600082 20021126 00082 NM 2002 11 26 CALA0200539 1 20021109 A 3350 BR9664411 SOCKET BOEING 757 757224 1384958 NM SEAT 28 DAMAGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12114 27556 INSPECTION FOUND EMERGENCY LIGHT CONNECTOR IN SEAT 28ABC DAMAGED. THE EMERGENCY LIGHT WAS REPLACED IAW IFM 25-20-10 AND FUNCTIONAL CHECKS WERE PERFORMED IAW MM 33-51-00. 2 L 7 2 4F RT A2NM 2002112600083 20021126 00083 NM 2002 11 26 CALA0200540 1 20021109 A 3397 WIRE BOEING 757 757224 1384958 NM EXIT LIGHT DEFECTIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12114 27556 INSPECTION FOUND SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 14ABC INOPERATIVE DUE TO A DEFECTIVE SPLICE. THE WIRING WAS R EPAIRED IAW WIRING MANUAL 20-10-13. FUNCTIONAL CHECKS WERE GOOD IAW MM 33-51-00. 2 L 7 2 4F RT A2NM 2002112600084 20021126 00084 2002 11 26 2002UALA01642 4 20021031 A 3441 HG2030AD09 IRU AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 837UA 1474 LOST CAPTAIN'S AIRSPEED TAPE INDICATION ON ROTATION. REPLACED AIR DATA INERTIAL REFERENCE UNIT NR 1. BUILT IN TEST EQU IPMENT CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112600085 20021126 00085 NM 2002 11 26 CALA0200541 1 20021109 A 3397 CONNECTOR BOEING 757 757224 1384958 NM EXIT SIGN FAULTY A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12114 27556 INSPECTION FOUND R-2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. THE WIRE BETWEEN R-2 DOOR AND EMERGENCY EXIT SIGN AND REMOVAB LE SPLICE CONNECTOR WERE FOUND AT FAULT. PIN CONTACT AND SPLICE CONNECTOR WERE REPLACED IAW WIRING MANUAL 20-30-12. THE CONNECTOR WAS REFITTED IAW WDM 33-51-13. FUNCTIONAL CHECKS WERE GOOD IAW MM 33-51-00. 2 L 7 2 4F RT A2NM 2002112600086 20021126 00086 WP 2002 11 26 CALA0200543 1 20021111 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 98876 49444 INSPECTION FOUND CENTER FLOOR SUPPORT ANGLE CORRODED AT STA 1174 BETWEEN LEFT AND RIGHT I/B SEAT TRACKS. THE FLOOR SUPPO RT WAS REMOVED AND REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2002112600087 20021126 00087 NM 2002 11 26 CALA0200547 1 20021112 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND LT MLG WHEEL WELL KEEL BEAM LOWER CHORD CORRODED AT STA 707-727. A REPAIR WAS INSTALLED IAW ECRA 5310-0 3740. 2 L 7 2 4F RT A16WE 2002112600088 20021126 00088 NM 2002 11 26 2002UALA01643 1 20021030 A 5610 141W74002 WINDOW BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT CRACKED A UALA B EMER. DESCENT O OTHER CR CRUISE 1 WP 29 772UA 15047 1950 26930 1ST OFFICER'S FWD OUTER WINDSHIELD FAILED. PRESSURIZATION MAINTAINED AT ALL TIMES. THE OUTER LAYER OF GLASS SHATTERED DUE TO ARCING AT THE UPPER BUS BAR FOR THE WINDOW HEAT SYSTEM. THE CAUSE OF THE ARCING WAS DUE TO MOISTURE INGRESS INTO THE ELECTRICAL HEAT SYSTEM BUS BAR AT THE AREA WHERE THE HEAT FILM ATTACHES TO THE BUS BAR. CONTRIBUTING FACTORS OF PO OR ADHESION OF THE MOISTURE SEAL AND DELAMINATION IN AND AROUND THE UPPER BUS BAR AREA ALLOWED THE WATER TO PENETRATE IN TO THE AREA. REMOVED AND REPLACED THE WINDOW ASSY PER AMM 56-11-01-401. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002112600089 20021126 00089 WP 2002 11 26 CALA0200551 1 20021114 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 98876 49444 INSPECTION FOUND CUSP WEB CORRODED IN CABIN AT RT SIDE, STA 513-579. THE CUSP WEB SECTION WAS REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2002112600090 20021126 00090 NM 2002 11 26 2002UALA01644 1 20021101 A 5512 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HORIZ STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 946UA 26687 RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE HAS EXCESSIVE MATERIAL LOSS AT BLEND 67 INCHES OB OF IB END. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLUSH DOUBLER & FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600091 20021126 00091 NM 2002 11 26 CALA0200556 1 20021121 A 5314 KEELBEAM BOEING 737 737524 1384721 NM FUSELAGE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14609 27322 INSPECTION FOUND DEEP WEAR ON KEEL BEAM AT BS 710-727, RBL 8 (LOWER FILLET PANEL ATTACH FLANGE). A FILLER AND STRAP REPA IR WAS INSTALLED IAW ECRA 5311-01143. 2 L 7 2 4F RT A16WE 2002112600092 20021126 00092 NM 2002 11 26 CALA0200557 1 20021115 A 5312 PRESSURE PANEL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND A 1 INCH CRACK IN PRESSURE DECK AT BS 664, RBL 40. REPAIRED IAW SRM 53-60-51. 2 L 7 2 4F RT A16WE 2002112600093 20021126 00093 NM 2002 11 26 2002UALA01646 1 20021103 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 946UA 26687 FUSELAGE SKIN HAS SEVERAL HOLES DAMAGED AT NR 2 AIRPHONE ANTENNA BASE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER RE PAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600094 20021126 00094 NM 2002 11 26 CALA0200563 1 20021124 A 3234 DIODE BOEING 737 7373T0 1384582 NM MLG LEVER DISCONNECTED A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 70353 23591 THE LANDING GEAR WOULD NOT RAISE AFTER TAKEOFF FROM RDU. THE GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION. THE AIRCR AFT WAS RETURNED TO RDU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT JUMPER, DIODE M416, ON BACK OF THE GEAR LEVER ASSEMBLY WAS POPPING LEVER LATCH CIRCUIT BREAKER WHEN HOOKED INTO SYSTEM. THE DIODE WAS FOUND MIS-CONNECTED. THER E WAS NO HISTORY OF WORK IN THIS AREA AND NO PREVIOUS WRITEUPS FOR THIS PROBLEM. THE DIODE WAS RECONNECTED IAW WIRING DI AGRAM 31-31-01 AND ALL GROUND OPERATION WAS NORMAL. 2 L 7 2 4F RT A16WE 2002112600095 20021126 00095 NM 2002 11 26 2002UALA01647 1 20021104 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 CABIN BODY FRAME WEB IS CRACKED BODY STATION 827 STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. SPLICED BODY FRAME WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600096 20021126 00096 NM 2002 11 26 2002UALA01648 1 20021104 A 5311 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 CABIN BODY FRAME INTERCOSTAL ASSEMBLY IS CRACKED BODY STATION 291 JUST BELOW STRINGER 10R. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL ASSY. 2 L 7 2 4F 4 F RT A16WE E2GL 2003031300118 20030313 00118 NM 2003 3 13 2002UALA01649 1 20021102 A 3244 TIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG BLOWN A UALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 127UA 28813 REPORT FROM TOWER OF SMOKE FROM AFT MAIN GEAR. SUBSEQUENT INSPECTION SHOWED INNER AFT BODY GEAR TIRE BLOWN. REMOVED AN D REPLACED BLOWN 4R TIRE AND MATING NR 3 TIRE PER BLOWN TIRE PROCEDURES. REASON FOR TIRE FAILURE UNKNOWN. TIRE WAS A R ECAP 3 LEVEL. 2 L 7 4 4F 4 F RT A20WE E24NE 2002112600098 20021126 00098 CE 2002 11 26 101502 1 20021013 A 3240 25EN96 SQUAT SWITCH LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP MLG INTERMITTENT E ESUA O OTHER G MULTIPLE FAILURE TX TAXI/GRND HDL 1 CE 03 72LL 275 AFTER LANDING, DURING TAXI, SECOND TURN DURING TAXI OPERATION, THE AIRCRAFT DID NOT RESPOND TO BRAKING OR STEERING. AFTE R RELIZING THAT THE AIRCRAFT WAS NOT RESPONING DURING TAXI OPERATIONS, THE CREW ENGAGED THE EMERGANCY BRAKES TO STOP THE AIRCRAFT. AT THIS TIME THE AIRCRAFT WHEELS WERE GOING OFF THE EDGE OF THE TAXIWAY. AIRCRAFT CAME TO A COMPLETE STOP 2 T O 3 FT OFF THE TAXING WAY. MAINTENANCE HAS DETERMINED THAT THE LT SQUAK SWITCH WAS INTERMITTENT. AT THE TIME OF THE INCI DENT THE AIRCRAFT THOUGHT IT WAS IN THE AIR, NOT ON THE GROUND, WHICH CAUSED NO STEERING OR BRAKING. 2 L 7 2 4F 4 F A10CE E6WE 2002112600099 20021126 00099 CE 2002 11 26 102302 1 20021022 A 2915 238003015 REGULATOR VALVE LEAR 25 25B 5170511 CE HYD SYSTEM MALFUNCTIONED E ESUA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 425JL 127 AT FLIGHT LEVEL 430 HYRDRALIC PRESSURE INDICATED 0, AIRCRAFT WAS DIVERTED TO LIT. DURING DESENT THE LT ENGINE OIL LIGHT CAME ILLUMINATED. THIS ENGINE WAS SHUT DOWN. AIRCRAFT WAS PREPARE FOR EMERGANCY LANDING PROCEDURES. CAUSE OF THE HYD FAI LURE WAS PRESSURE RELIEF VALVE AND THE CAUSE FOR THE OIL LIGHT WAS A OIL PRESSURE LINE COMING LOOSE. 2 L 7 2 4J A10CE 2002112600100 20021126 00100 NE 2002 11 26 102402 2 20021021 A 7261 OIL SYSTEM LEAR 25 25B 5170511 CE GE CJ610 CJ610* 30006 NE LT ENGINE LEAKING E ESUA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 03 425JL 127 240209A DURING DESENT INTO LIT, THE LT ENGINE OIL LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN. THE CAUSE WAS A LOOSE OIL LINE, P RESSURE LINE 2 L 7 2 4J 4 J A10CE 1E16 2002112600102 20021126 00102 2002 11 26 102502 4 20021022 A 2297 WIRE HAWKER BAE125 BAE125700B 7450007 EU AUTOPILOT SYS BROKEN E ESUA O OTHER P NO WARNING INDICATION CL CLIMB 1 CE 03 810GS 9725 257061 PILOTS WERE ASSIGN A ALTITUDE AFTER DEPARTURE, AND FLOW THROUGH THE ASSIGNED ALTITUDE BY 1700 FT. THE PILOTS SELECTED TH E ALTITUDE INTO THE ALTITUDE ALERT SYSTEM. THE SYSTEM FAILED TO CAPTURE THE ASSIGNED ALTITUDE. CAUSE WAS A BROKEN WIRE T O THE ALTITUDE ALERT SYSTEM 2 L 7 2 4F RT A3EU 2002112600103 20021126 00103 CE 2002 11 26 103102 1 20021031 A 3210 23411195605 TORQUE LINK LEAR 35 35A 5170602 CE LT MLG CRACKED E ESUA K NONE O OTHER IN INSP/MAINT 1 CE 03 72LL 13028 275 DURING EDDY CURRENT OF LOWER TORQUE LINK ON THE LT MLG, A CRACK WAS DISCOVERED. THE PART WAS REPLACED. 2 L 7 2 4F A10CE 2002112600104 20021126 00104 NE 2002 11 26 110702 2 20021106 A 7200 ENGINE LEAR 25 25B 5170511 CE GE CJ610 CJ610* 30006 NE NACELLE FLAMED OUT E ESUA B EMER. DESCENT X ENGINE FLAMEOUT CL CLIMB 1 CE 03 254SC 5920 3895 102 249057A ENGINE FLAMED OUT AT FL 390, 20 MIN. INTO THE FLIGHT. PILOT DECLARED AN EMERGANCY. THE PILOT RELITE THE ENGINE. THE AIRC RAFT RETURNED TO THE GROUND AT FXE. THE PROBLEM COULD NOT BE DUPLITCATE ON THE GROUND. A/C WAS RETURNED TO SERVICE. AFTE R A TEST FLIGHT WAS PERFORMED, IT WAS DETERMINED THAT THE ENGINE STILL WAS NOT OPERATING CORRECTLY. IT WAS DETERMINED TH AT THE CAUSE WAS THE COMPRESSOR SECTION. ANOTHER ENGINE IS BEING INSTALLED. 2 L 7 2 4J 4 J A10CE 1E16 2002112600106 20021126 00106 SO 2002 11 26 111202 1 20021112 A 5412 BULKHEAD GULSTM G1159 G1159 3953505 SO NACLELLE CRACKED E ESUA K NONE O OTHER IN INSP/MAINT 1 CE 03 629TD 12988 92 RT ENGINE NOSE COWLING BULKHEAD HAS 3 CRACKS, 2 CRACKS WERE WITHIN LIMITS, THE 3RD WAS OVER 3 INCHES WHICH IS OUT OF LIM ITS. 2 L 7 2 4F RT A12EA 2002112600107 20021126 00107 EU 2002 11 26 1115 1 20021115 A 7120 30710702 MOUNT HAWKER BAE125 BAE125700B 7450007 EU LT ENGINE CRACKED E ESUA K NONE O OTHER IN INSP/MAINT 1 CE 03 619TD 6298 257118 UPPER, FORWARD LEFT HAND ENGINE MOUNT FOUND CRACKED DURING MAG PARTICAL INSPECTION. 2 L 7 2 4F RT A3EU 2002112600108 20021126 00108 NM 2002 11 26 2002UALA01653 1 20021103 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 CABIN FLOOR BEAM CORRODED ON UPPER SURFACE OF CAP, STA 324, RBL 8 STR 17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED TWO NE STED ANGLES BELOW UPPER CAP WITH FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112600109 20021126 00109 EU 2002 11 26 111502 2 20021111 A 7320 301RAAZ ACTUATOR GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY511* 54523 EU RT ENGINE FAILED E ESUA E ENGINE SHUTDOWN P NO WARNING INDICATION CL CLIMB 1 CE 03 227GA 3176 3176 76 11001 AFTER DEPARTURE FROM HNL, PILOT SHUT DOWN RT ENGINE BECAUSE THE TGT WAS CLIMBING. THE ENGINE WAS SHUTDOWN AT 540TGT. THE PILOT DECLARED AN EMERGANCY AND RETURN TO HNL. AFTER MAINTENANCE LOOKED AT THE A/C, THE PROBLEM WAS THE TOP TEMP ACTUAT OR. 2 L 7 2 4F 4 F RT A12EA E2EU 2002112600110 20021126 00110 SO 2002 11 26 111512 1 20021111 A 7720 8DJ100WAS2 GAUGE GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY511* 54523 EU TGT STUCK E ESUA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 227GA 485 485 76 11001 TGT WAS RAISING TO 540 WHEN THE ENGINE WAS SHUT DOWN. THE TGT GAUGE BECAME INOP. THE GAUGE STUCK. 2 L 7 2 4F 4 F RT A12EA E2EU 2002112600112 20021126 00112 SO 2002 11 26 112502 1 20021121 A 5330 ACCESS PANEL GULSTM G1159 G1159 3953505 SO FUSLEAGE CRACKED E ESUA K NONE O OTHER IN INSP/MAINT 1 CE 03 629TD 92 CRACK WAS FOUND DURING INSPECTION, ACCESS PANEL 107-22-FIL-7. APPROX. BL 15R. CRACK WAS REPAIRED IAW SRM 51-20-03. 2 L 7 2 4F RT A12EA 2002112600113 20021126 00113 NM 2002 11 26 2002UALA01655 1 20021104 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 CABIN FLOOR CREASE BEAM WEB CORRODED, STA 742, RBL 62. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002120400131 20021204 00131 NM 2002 12 4 2002UALA01656 1 20021103 A 2751 INDICATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 375UA 24640 AIRCRAFT LANDED UNDER AMBER ALERT WHEN THE FLIGHT CREW WAS UNABLE TO EXTEND THE FLAPS BEYOND 10 DEGREES. FLAP POSITION INDICATOR INOPERATIVE. REPLACED FLAP POSITION INDICATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600114 20021126 00114 NM 2002 11 26 2002UALA01657 1 20021104 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 BODY STATION 616, LT FUSELAGE FRAME INBOARD CHORD ANGLE HAS 2 INCH CRACK 6 INCHES BELOW CREASE BEAM WEB WL 201. MAJOR R EPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600115 20021126 00115 NM 2002 11 26 2002UALA01658 1 20021104 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 BODY STATION 847, STRINGER 9L CABIN BODY FRAME IS CRACKED. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED DOUBLER . 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600116 20021126 00116 NM 2002 11 26 2002UALA01659 1 20021104 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 BODY STATION 847, STRINGER 9R CABIN BODY FRAME WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED REP AIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600117 20021126 00117 NM 2002 11 26 2002UALA01660 1 20021104 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 CABIN PRESSURE WEB CRACKED, STA 675,LBL 30. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700011 20021127 00011 NM 2002 11 27 2002UALA01661 1 20021101 A 2612 47348708 CIRCUIT CARD BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FIRE WARNING DEFECTIVE A UALA F E J A ACTIVATE FIRE EXT. ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 773UA 1039 26929 777002 RIGHT ENGINE FIRE WARNING CAME ON IN FLIGHT. BOTH BOTTLES DISCHARGED. OPENED COWLS AND CHECKED FOR INDICATION OF FIRE OR OVERHEAT. NONE FOUND. FIRE WARNING WAS A FALSE ALARM. BOTH FIRE LOOP ELEMENTS AND WIRING CHECKED GOOD. REPLACED N R 2 ENGINE FIRE DETECTION CARD. OEM KIDDE TESTED AND CONFIRMED CARD FAILURE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002121900027 20021219 00027 NM 2002 12 19 2002UALA01662 1 20021031 A 2150 CONTROL VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT A/C PACK FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 790UA 26943 RT A/C PACK PROBLEM AND ASSOC. ETOPS RESTRICTION. FCVS FAILED IN THE CLOSED POSITION. THE RT PACK UPPER FLOW CONTROL V ALVE (FCV) WAS DEFERRED OUT OF DEN EARLIER THAT DAY. THE RT PACK LOWER FCV FAILED DURING CLIMB OUT OF IAD. BOTH FCV WE RE REPLACED IN JFK. BOTH VALVES HAD FAILED TORQUE MOTOR & DAMAGED BUTTERFLY DISK SEAL RING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002112600118 20021126 00118 NM 2002 11 26 2002UALA01663 1 20021104 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 562UA 26664 DENT AND GOUGE 34 INCHES AFT OF DOOR 2L, STA 760, STR 16L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700022 20021127 00022 NM 2002 11 27 2002UALA01673 1 20021106 A 2121 732591F FAN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAILED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 198UA 22526 28716 SMOKE SMELL IN CABIN. LWR REC FAN STATUS MESSAGE. FOUND LOWER RIGHT HAND FAN MOTOR BEARINGS FAILED. REPLACED FAN MOTO R. 2 L 7 4 4F 4 F RT A20WE E24NE 2002112600120 20021126 00120 NM 2002 11 26 2002UALA01676 1 20021106 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 NOSE FLIGHT DECK FLOOR STATION 196 RIGHT HAND CREASE BEAM WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900029 20021219 00029 NE 2002 12 19 2002UALA01683 2 20021106 A 7261 70R555 DRIVE GEAR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OIL PUMP SHEARED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K M FLUID LOSS OVER TEMP CR CRUISE 1 WP 29 658UA 27113 717682 NR 1 ENGINE SHUTDOWN DUE TO LOSS OF OIL PRESSURE AND HIGH TEMP. OIL PUMP DRIVE GEAR FAILURE. OIL PUMP DRIVE BEARING AN D GEAR ASSY WERE FOUND LOOSE AND COCKED IN THE GEARBOX BEARING BORE. BEARING RETAINING SCREWS (ITEM 10 ) WERE BACKED OUT OF THE GEARBOX HOUSING AND LAYING IN THE BOTTOM OF THE GEARBOX. THIS RESULTED IN FRACTURE OF THE OIL PUMP DRIVE MODULE GEAR SHAFT IN THE WEB OF THE GEAR. THE FINAL ROOT CAUSE IS STILL BE INVESTIGATED. ENGINE WILL REQUIRE OVERHAUL OF ALL BE ARINGS DUE TO LOSS OF OIL PRESSURE. MAIN GEARBOX WILL BE OVERHAULED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002112600121 20021126 00121 EA 2002 11 26 02304631 1 20021031 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 631BR 7261 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTS BETWEEN SEAT ROWS 2 AND 6 WERE INOP ERATIVE. MAINTENANCE PERSONNEL SECURED THE CONNECTOR FOR THE EMERGENCY FLOOR TRACK LIGHT STRIP. AN OPERATIONAL CHECK W AS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002112600122 20021126 00122 EA 2002 11 26 02305637 1 20021101 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 637BR 7308 DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT THE NR 1 OVERHEAD CABIN EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAIN TENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE NR 1 OVERHEAD CABIN EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002112600123 20021126 00123 EA 2002 11 26 02307621 1 20021103 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 621BR 7186 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WOULD NOT EXTINGUISH WITH ALL POWER SOURCE S OFF AND THE LIGHTS SWITCH IN THE OFF POSITION. MAINTENANCE PERSONNEL SECURED THE EMERGENCY POWER PACK CANNON PLUG. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002112600124 20021126 00124 NM 2002 11 26 02312408 1 20021108 A 3350 LIGHT DORNER DO32 DO328300 NM CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 408FJ 3160 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT TWO FORWARD CABIN EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENA NCE PERSONNEL REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND T HE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002112600125 20021126 00125 EA 2002 11 26 02312629 1 20021108 A 3350 CONTACTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN CONTAMINATED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 629BR 7251 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTING NEAR THE PASSENGER ENTRY DOOR WAS INOPERATIVE. MAINTENANCE PERSONNEL FOUND THAT THE AREA WAS WET FROM RAIN. DRIED THE AREA, CLEANED THE CONTACTS AND RE CONNECTED. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002112600126 20021126 00126 EU 2002 11 26 02324309 1 20021120 A 3397 WIRE JETAIR JETSTM JETSTM4101 1500501 EU CABIN DAMAGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 309UE 41022 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF THE EMERGENCY FLOOR TRACK LIGHTING WAS INOPER ATIVE. MAINTENANCE PERSONNEL REPAIRED A BROKEN WIRE AT THE FORWARD EMERGENCY FLOOR TRACK LIGHT. AN OPERATIONAL CHECK W AS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002112600128 20021126 00128 NM 2002 11 26 2002UALA01580 1 20021013 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 CABIN FLOORBEAM UPPER CAP EXCESSIVE MATERIAL REMOVED STATION 680 LBL 1 TO RBL 16. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112600129 20021126 00129 NM 2002 11 26 2002UALA01581 1 20021011 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 CABIN FLOOR SUPPORT UNDER DRAIN GUTTER AT STATION 1640 RBL 65 STRINGER 17R HAD EXCESSIVE MATERIAL REMOVED DURING CORROSI ON CLEANUP. MAJOR REPAIR ACCOMPLISHED. REMOVED AND INSTALLED NEW BOEING FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112600130 20021126 00130 NM 2002 11 26 2002UALA01583 1 20021002 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 578UA 26694 SKIN CREASED LEFT SIDE OF FUSELAGE STA 1725, STR 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112600131 20021126 00131 NM 2002 11 26 2002UALA01585 1 20021015 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 947UA 26688 EXTERNAL FUSELAGE SKIN HAS EXCESSIVE MATERIAL LOSS AFTER BLEND. 30 PERCENT LOSS AT LOWER AFT CORNER OF AFT ENTRY DOOR C UTOUT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600132 20021126 00132 NM 2002 11 26 2002UALA01586 1 20021015 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 947UA 26688 EXTERNAL FUSELAGE SKIN, INTERNAL DOUBLER & STRAP WERE REPAIRED. MAJOR REPAIR ACCOMPLISHED. DOUBLER & TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600133 20021126 00133 NM 2002 11 26 2002UALA01587 1 20021014 A 5310 TEE FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 AFT PIT DOOR OPENING FORWARD FRAME TEE FITTING FOR BOTTOM STOP PAD FITTING IS CORRODED BEYOND LIMITS. MAJOR REPAIR ACCO MPLISHED. REPLACED SUPPORT TEE FITTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600134 20021126 00134 NM 2002 11 26 2002UALA01588 1 20021014 A 3610 VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE BLEED AIR SYS FAILED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 827UA 1022 NR 2 RIGHT HAND THRUST REVERSER TRANSLATING SLEEVE COWL DELAMINATED ON FORWARD ACOUSTIC SKIN. CAUSED BY HEAT OF FAILED VALVE IN THE OPEN POSITION FOR 10TH STAGE BLEED VALVE. ENGINE VIBRATION SURVEY ACCOMPLISHED ON GROUND, WITH FAILED VALV E, LEADING TO UNUSUALLY LONG EXPOSURE TO 10TH STAGE BLEED AIR. REPLACED FORWARD ACOUSTICAL SKIN. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112600135 20021126 00135 NM 2002 11 26 2002UALA01589 1 20021015 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 CABIN STATION 640 FLOOR BEAM CAP CORRODED FROM LBL 43 TO RBL 23. MAJOR REPAIR ACCOMPLISHED. STRAP REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112600136 20021126 00136 NM 2002 11 26 2002UALA01591 1 20021014 A 2740 6042H110 RELAY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE STABILIZER TRIM DEFECTIVE A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 343UA 24247 HORIZONTAL STABILIZER TRIM CIRCUIT BREAKER, AND THEN THE FLAP CIRCUIT BREAKER POPPED. TROUBLESHOOTING REVEALED FAULTY C IRCUIT BREAKER C210 AND RELAY R64. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600137 20021126 00137 NM 2002 11 26 2002UALA01592 1 20021015 A 5320 ANGLE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 950UA 26695 AFT GALLEY DOOR FUSELAGE CUTOUT LOWER SILL ZEE ANGLE INNER CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW ZE E ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600138 20021126 00138 EU 2002 11 26 2002UALA01593 1 20021015 A 3350 321454 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 427UA 512 EMERGENCY LIGHTS FAIL SYSTEM TEST AT 3 SVC. REPLACED BATTERY PACK AT RT OVERWING EXIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112600139 20021126 00139 NM 2002 11 26 2002UALA01594 1 20021015 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 CABIN FLOOR BEAM STATION 310 RBL 39 TO 42 MATERIAL REMOVED EXCEEDS LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED SUPPOR T ANGLE-REINFORCEMENT STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112600140 20021126 00140 NM 2002 11 26 2002UALA01595 1 20021015 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 FORWARD GALLEY FLOOR BEAM UPPER CAP REPAIR PLATE IS CORRODED AT BODY STATION 365 FROM RBL 13 TO RBL 54. MAJOR REPAIR AC COMPLISHED. INSTALLED SUPPORT ANGLE-REINFORCEMENT STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112600141 20021126 00141 NM 2002 11 26 2002UALA01596 1 20021016 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CABIN FLOOR INTERCOSTAL UPPER FLANGE CRACKED AT BODY STATION 933 BL 0. MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER FLANGE . 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600142 20021126 00142 EU 2002 11 26 2002UALA01597 1 20021012 A 2612 73040102 FIRE LOOP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE MALFUNCTIONED A UALA O OTHER N FALSE WARNING DE DESCENT 1 WP 29 407UA 456 NUMBER 2 ENGINE FIRE WARNING LIGHT ILLUMINATED DURING DESCENT WITH NO SECONDARY INDICATIONS. THE FIRE DETECTION UNIT WA S CHANGED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112600143 20021126 00143 NM 2002 11 26 2002UALA01598 1 20021016 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 356UA 24362 EMERGENCY ELECTRICAL LIGHTING INOPERATIVE IN THE AFT CABIN. DEFECTIVE LAMP ASSEMBLY. RELAMPED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600144 20021126 00144 NM 2002 11 26 2002UALA01602 1 20021018 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 CRACK IN FUSELAGE SKIN DOUBLER AT FORWARD EDGE OF FORWARD PIT DOOR CUTOUT 13 INCHES ABOVE LOWER EDGE. MAJOR REPAIR ACCO MPLISHED. TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600145 20021126 00145 NM 2002 11 26 2002UALA01603 1 20021018 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 352UA 24320 AFT CARGO COMPARTMENT DOOR CUTOUT FRAME AT BODY STATION 794 S23R TO S24R AFT SIDE HAS EXCESSIVE MATERIAL REMOVED TO CLEA N CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600146 20021126 00146 NM 2002 11 26 2002UALA01604 1 20021020 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 950UA 26695 FUSELAGE SKIN AT STATION 807 STRINGER 17R HAS BLENDED AREA WITH EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. SK IN REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600147 20021126 00147 NM 2002 11 26 2002UALA01605 1 20021020 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 950UA 26695 AFT PIT FRAME STATION 787 RBL 20 UPPER SURFACE GOUGED FROM SUPPORT STRAP. MAJOR REPAIR ACCOMPLISHED. FRAME CAP HOLE ST RAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600148 20021126 00148 NM 2002 11 26 2002UALA01606 1 20021021 A 5511 RIB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 950UA 26695 LEFT HAND HORIZONTAL STABILIZER APPROXIMATELY MID POINT HAS SERIES OF DENTS ACROSS RIB. MAJOR REPAIR ACCOMPLISHED. INS TALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112600149 20021126 00149 NE 2002 11 26 2002UALA01612 2 20021018 A 7230 COMPRESSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE STALLED A UALA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 534UA 25129 726604 NUMBER 1 ENGINE COMPRESSOR STALL CLIMBING THROUGH 10000 FT AND PASSING THROUGH 767 WAKE TURBULENCE. ENGINE SELF RECOVER ED AND CONTINUED NORMAL OPERATION. SURGE INSPECTION/CHECK WAS PERFORMED, WITH NO DISCREPANCIES FOUND. ENGINE TSI WAS 1 4,000 FLIGHT HOURS WITH NORMAL ECM TREND PLOT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700009 20021127 00009 2002 11 27 2002UALA01613 4 20021018 A 3197 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EICAS SYS CHAFED A UALA O OTHER N FALSE WARNING DE DESCENT 1 WP 29 590UA 28708 717965 RIGHT ENGINE OIL FILTER BYPASS INDICATION ILLUMINATED MOMENTARILY. WIRING CHECKS WERE PERFORMED, AND THE WIRE THAT GOES TO THE EICAS COMPUTERS WAS FOUND CHAFFED. WIRE WAS REPAIRED. WIRE NUMBER W3494-1027-18 EIGHT INCHES FROM CONNECTOR D4 0116J. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700074 20021127 00074 EU 2002 11 27 2002UALA01718 1 20021112 A 3610 D3617003000200 DUCT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE BLEED AIR SYS LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 435UA 613 FLIGHT DIVERTED DUE TO A LEFT WING BLEED MESSAGE. FOUND SOURCE OF LEAK AT HIGH PRESSURE GROUND AIR CONNECTION DUCT/CLAM P. REPLACED DUCT AND CLAMPS. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112600150 20021126 00150 NM 2002 11 26 2002UALA01745 1 20021119 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 804UA 759 FUSELAGE SKIN DENTED BETWEEN STRINGER 28L AND 29L, 2" AFT OF FRAME 18 STA 760 DAMAGE IS AT THE SKIN LAP. MAJOR REPAIR ACCOMPLISHED. SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112600151 20021126 00151 NM 2002 11 26 2002UALA01749 1 20021119 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 LEFT HAND FUSELAGE STATION 613 AND 617 BELOW STRINGER 16 SKIN DENTED BELOW PREVIOUS INSTALLED REPAIR DOUBLER. MAJOR RE PAIR ACCOMPLISHED.SKIN DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112600152 20021126 00152 EA 2002 11 26 COMA0260662 1 20021121 A 2910 601R7528651 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA #2 HYD SYSTEM CHAFED A COMA A UNSCHED LANDING S K AFFECT SYSTEMS FLUID LOSS CL CLIMB 1 SO 01 971CA 7145 FLIGHT #5404 #2 HYDRAULIC SYSTEM LOW PRESSURE CAUTION MESSAGE.REPLACED THE #2 SYSTEM CASE DRAIN LINE ASSY. 2 L 7 2 4F RT A21EA 2002112600153 20021126 00153 EA 2002 11 26 COMA0260663 1 20021123 A 7830 2100140007 THROTTLE CONTROL CNDAIR CL600 CL6002B19 1900309 EA R/H ENG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 964CA 9681 7129 FLIGHT 5273 R/H THRUST REVERSER UNLOCKED MESSAGE.REPLACED THE THROTTLE GEAR BOX. 2 L 7 2 4F RT A21EA 2002112600154 20021126 00154 EA 2002 11 26 COMA0260664 1 20021123 A 2410 755469B IDG CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA C ABORTED TAKEOFF J F WARNING INDICATION FLT CONT AFFECTED TO TAKEOFF 1 SO 01 914CA 17980 127 7012 FLIGHT 5081 CON FIG SPOILERS MESSAGE DURING T/O.REPLACED THE R/H ENGINE IDG. 2 L 7 2 4F RT A21EA 2002112600155 20021126 00155 EA 2002 11 26 COMA0260665 1 20021124 A 3030 PITOT HEAD CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 983CA 7169 FLIGHT 5369 LT PITOT AND AOA HEAT CAUTION MESSAGE.COULD NOT DUPLICATE RESET SYSTEM AND OPS NORMAL. 2 L 7 2 4F RT A21EA 2002112600156 20021126 00156 EA 2002 11 26 COMA0260666 1 20021125 A 5210 600380389 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR CORRODED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 966CA 7132 FLIGHT 5407 CABIN DOOR LATCH CAUTION AND DOOR WARNING.REPLACED THE DOOR INNER HANDLE SPRING LATCH MECHANISM. 2 L 7 2 4F RT A21EA 2002112600157 20021126 00157 EA 2002 11 26 COMA0260667 1 20021124 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 914CA 1366 7012 FLIGHT 5473 FLAPS FAIL MESSAGE.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2002112600158 20021126 00158 NM 2002 11 26 C1HA200284005 1 20021122 A 3350 BULB BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 684CA 22491 Emergency track lighting bulb at row 20 INOP.Relamped emergency track light at row 20. 2 L 7 3 4F A3WE 2002112600159 20021126 00159 SO 2002 11 26 C2XA02CL232 1 20021125 A 3350 1317 BULB EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 16525 145403 CLE FLIGHT#2996 THE CREW REPORTED THE EMERGENCY EXIT SIGN AT SERVICE DOOR WAS INOPERATIVE.MAINTENANCE INSPECTED AND REPL ACED THE LIGHT BULBS.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002112700001 20021127 00001 SO 2002 11 27 C2XA02SH132 1 20021127 A 5400 14576036015 RIB EMB 135 EMB135LR 3260305 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16520 145372 SHV- DURING C CHECK LEFT HAND UPPER COWLING MOST AFT REINFORCEMENT RIB WAS FOUND GOUGED ON OUTBOARD SIDE. MAINTENANCE R EMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 135 SRM 54-10-07.THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002112700002 20021127 00002 SO 2002 11 27 C2XA02SH133 1 20021127 A 5400 14576036015 RIB EMB 135 EMB135LR 3260305 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16520 145372 SHV- DURING C CHECK THE RIGHT HAND UPPER COWLING MOST AFT REINFORCEMENT RIB WAS FOUND GOUGED OUTBOARD SIDE. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 135 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002112700003 20021127 00003 NM 2002 11 27 801DM0008 1 20021126 A 2560 FLASHLIGHT BOEING 757 757200 1384950 NM A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 801DM 26240 Flight deck right bulkhead emergency flashlight inop. R&R emergency flashlight IAW MM 25-00 Ops Chk normal. 2 L 7 2 4F RT A2NM 2002112700004 20021127 00004 NM 2002 11 27 730PA0001 1 20021118 A 5321 65C2645947 SKIN PANEL BOEING 737 7373L9 1384470 NM A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 730PA 27924 Floor panels damaged for aft cargo bin. Removed aft cargo floor panels and fabricated new per EA 53-319 authorizing the use of 2024-T3 .071 alclad sheet per the -60 installation. 2 L 7 2 4F RT A16WE 2002112700005 20021127 00005 NM 2002 11 27 249TR0009 1 20021105 A 3350 1000679 LIGHT BOEING 737 7372K5 138448X NM A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 L2 door emergency exit overhead light inop. Installed new emergency exit light assy. 2 L 7 2 4F RT A16WE 2002120200021 20021202 00021 NM 2002 12 2 249TR0010 1 20021105 A 3350 1000629 LIGHT BOEING 737 7372K5 138448X NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 L2 OUTSIDE EMERGENCY LIGHT INOP. INSTALLED NEW EMERGENCY EXIT LIGHT ASSY. 2 L 7 2 4F RT A16WE 2002112700006 20021127 00006 NM 2002 11 27 2002UALA01444 1 20020911 A 1430 SCREW BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE BACKED OUT A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 652UA 25390 717553 NO OIL PRESSURE IN LEFT ENGINE, ENGINE SHUTDOWN. FLIGHT LANDED WITHOUT INCIDENT. OIL PUMP DRIVE GEAR FAILURE. REF IPC 72-61-00-019: OIL PUMP DRIVE BEARING AND GEAR ASSY WERE FOUND LOOSE AND COCKED IN THE GEARBOX BEARING BORE. BEARING RET AINING SCREWS WERE BACKED OUT OF THE GEARBOX HOUSING AND LAYING IN THE BOTTOM OF THE GEARBOX. THIS RESULTED IN FRACTURE OF THE OIL PUMP DRIVE MODULE GEAR SHAFT IN THE WEB OF THE GEAR. ENGINE WILL REQUIRE OVERHAUL OF ALL BEARINGS DUE TO LOS S OF OIL PRESSURE.MAIN GEARBOX WILL BE OVERHAULED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002112700008 20021127 00008 2002 11 27 MALA020671 4 20021123 A 3410 6223975001 ALTIMETER SAAB SF340 340B 7860101 EU A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 452XJ 340B452 DURING FLIGHT #3073, CAPT'S ALTIMETER WENT TO 7000' AND NOT BEYOND. ALTIMETER RED FLAGGED SO A/C WAS TURNED BACK TO MSP. AIR RETURN TO MSP. MAINTENANCE REPLACED #1 ALTIMETER PN 622-3975-001, SN/OFF 7937, SN/ON 7662. #1 ALTIMETER OPS CHECK GOOD IAW SF340 AMM CHAP 34. 2 L 7 2 4T RT A52EU 2002112700014 20021127 00014 NM 2002 11 27 2002UALA01667 1 20021105 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 BODY STATION 867, STRINGER 9L, CABIN BODY FRAME WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700016 20021127 00016 NM 2002 11 27 2002UALA01668 1 20021105 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 CABIN FUSELAGE FRAME WEB STA 867 IS CRACKED AT STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME DOUBLER REPAIR 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700017 20021127 00017 NM 2002 11 27 2002UALA01669 1 20021106 A 5512 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZ STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE HAD EXCESS MATERIAL REMOVED, 24 INCHES FROM FUSELAGE. MAJOR REPAIR ACCOMP LISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700024 20021127 00024 NM 2002 11 27 2002UALA01675 1 20021106 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 334UA 24229 EMERGENCY LIGHT AFT OF AFT ENTRY DOOR INOPERATIVE. RELAMP. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700025 20021127 00025 NM 2002 11 27 2002UALA01677 1 20021106 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 NOSE STATION 196 LEFT HAND CREASE BEAM WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700026 20021127 00026 NM 2002 11 27 2002UALA01678 1 20021106 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 BODY STATION 887, STRINGER 9R CABIN BODY FRAME CRACKED. MAJOR REPAIR ACCOMPLISHED. DOUBLER MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700027 20021127 00027 NM 2002 11 27 2002UALA01679 1 20021106 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 BODY STATION 827, STRINGER 9L CABIN BODY FRAME WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. DOUBLER MANUFACTURED AND I NSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700028 20021127 00028 NM 2002 11 27 2002UALA01681 1 20021106 A 5743 BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 LEFT HAND MLG BEAM OUTBOARD END GOUGED FROM SPAR REPAIR FASTENER. MAJOR REPAIR ACCOMPLISHED. BLEND REPAIR ACCOMPLISHED . 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700029 20021127 00029 NM 2002 11 27 2002UALA01682 1 20021107 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 CABIN BODY FRAME WEB IS CRACKED BODY STATION 400 STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. SPLICED BODY FRAME WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700030 20021127 00030 2002 11 27 2002UALA01684 4 20021107 A 3197 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EICAS SYS CHAFED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 590UA 28708 717965 RIGHT ENGINE OIL FILTER BYPASS EICAS MESSAGE ILLUMINATED. WIRING CHECKS WERE PERFORMED, AND THE GROUND WIRE THAT GOES T O THE EICAS COMPUTERS FOR THE OIL BYPASS MESSAGE WAS FOUND CHAFED. WIRE WAS REPAIRED. WIRE NUMBER W3494-1027-18 EIGHT INCHES FROM CONNECTOR D40116J. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700036 20021127 00036 NM 2002 11 27 2002UALA01688 1 20021107 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 FUSELAGE SKIN DENTED, STA 583 STR 26R TO 27R. MAJOR REPAIR ACCOMPLISHED. TRIPLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700037 20021127 00037 EU 2002 11 27 2002UALA01689 1 20021108 A 5310 SHEAR TIE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 467UA 1359 AFT PIT FRAME 58 AT STRINGER 41L HAS BENT SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED NEW SHEAR TIE. REPLACED BENT SHEAR TIE. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112700038 20021127 00038 EU 2002 11 27 2002UALA01690 1 20021108 A 5310 SHEAR TIE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 467UA 1359 AFT PIT FRAME 59 AT STRINGER 42L HAS BENT SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. NEW SHEAR TIE MANUFACTURED. REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112700039 20021127 00039 EU 2002 11 27 2002UALA01691 1 20021108 A 5310 SHEAR TIE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 467UA 1359 AFT PIT FRAME 59 AT STRINGER 43L HAS BENT SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. NEW SHEAR TIE MANUFACTURED. SHEAR TIE REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112700040 20021127 00040 EU 2002 11 27 2002UALA01692 1 20021108 A 5310 SHEAR TIE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 467UA 1359 AFT PIT FRAME 59 AT STRINGER 41L HAS BENT SHEAR TIE. MAJOR REPAIR ACCOMPLISHED. NEW SHEAR TIE MANUFACTURED. SHEAR TIE REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112700041 20021127 00041 NM 2002 11 27 2002UALA01693 1 20021107 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 CABIN CIRC FRAME, STATION 927 STRINGER 9L, WEB IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REINFORCEMENT J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700042 20021127 00042 NM 2002 11 27 2002UALA01694 1 20021107 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 CABIN FLOOR INTERCOSTAL STATION 340 CL CRACKED AT UPPER FLANGE ATTACH FWD AND AFT SIDE STA 340 AND 360. MAJOR REPAIR AC COMPLISHED. INSTALLED REINFORCEMENT ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700043 20021127 00043 NM 2002 11 27 2002UALA01695 1 20021107 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 BODY STATION 887, STRINGER 9L, CABIN BODY FRAME WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. DOUBLER MANUFACTURED AND INSTA LLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700049 20021127 00049 NM 2002 11 27 2002UALA01696 1 20021107 A 5280 DOOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NLG OUT OF ADJUST A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 313UA 23674 AIRCRAFT RETURNED TO FIELD DUE TO VIBRATION FELT IN THE CONTROL CABIN. FOUND RIGHT NOSE DOOR IN AIRSTREAM WHEN GEAR UP. ADJUSTED DOOR. TROUBLESHOT AND FOUND NO OBVIOUS DISCREPANCIES. INSPECTED AS REQUIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700050 20021127 00050 NM 2002 11 27 2002UALA01697 1 20021108 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 948UA 26691 FLIGHT DECK WINDOW POST SKIN CRACKED AT UPPER LT CORNER OF NR 1 WINDOW. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700052 20021127 00052 NM 2002 11 27 2002UALA01698 1 20021111 A 5310 DOOR FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 912UA 25290 FORWARD CARGO DOOR FORWARD FUSELAGE FRAME CRACK AT LWR STOP FITTING OUTBOARD LOWER CORNER. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900030 20021219 00030 NM 2002 12 19 2002UALA01699 1 20021110 A 2121 4100941A COOLING FAN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FWD CARGO BAY FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 785UA 25103 26954 EQUIPMENT COOLING EICAS MESSAGE "EQP CLNG OVRID". EQUIPMENT COOLING MESSAGES HIT ON PREVIOUS FLIGHTS. PROBLEM WAS FIX ED BY REPLACING THE RT EQUIPMENT COOLING SUPPLY FAN. SHOP REPORTS THAT THE FAN FAILED DUE TO DEFECTIVE BEARINGS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002112700054 20021127 00054 NM 2002 11 27 2002UALA01700 1 20020828 A 5754 114W41101 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L/E SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 26947 DELAMINATED TRAILING EDGE WEDGE SKIN. SLAT 1A. SKIN REPAIRED/REPLACED PER AUTOCLAVE REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002112700055 20021127 00055 NM 2002 11 27 2002UALA01702 1 20020829 A 5754 114W41607 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L/E SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 776UA 26937 LOWER SURFACE DELAMINATED ON WEDGE T/E INBOARD END. SKIN REPAIRED/REPLACED PER AUTOCLAVE REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002112700056 20021127 00056 NM 2002 11 27 2002UALA01704 1 20021109 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 UPPERDECK LEFT EMERGENCY DOOR BATTERY PACK INOP. REPLACED BATTERY - CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2002112700057 20021127 00057 NM 2002 11 27 2002UALA01705 1 20021110 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 CABIN FLOOR BEAM UPPER T-CAP CORRODED, STA 324, RBL 45. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700059 20021127 00059 NM 2002 11 27 2002UALA01706 1 20021106 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 SKIN PUNCTURED FWD OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. NEW ONE PIECE DOUBLER REPAIR AT STA 720 ON STR 27. CAT B SK IN REPAIR. REPAIR INSTALLED WITH ALL SOLID FASTENERS. 2 L 7 4 4F 4 F RT A20WE E24NE 2002112700060 20021127 00060 NM 2002 11 27 2002UALA01707 1 20021110 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 CABIN FLOORBEAM CORRODED, STA 310, RBL 40 TO 44. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2003031300129 20030313 00129 NE 2003 3 13 2002UALA01709 2 20021109 A 7250 1B6322002 TURBINE BLADES BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 516UA 29887 13087 24860 726640 NR 1 ENGINE COMPRESSOR STALL AT FL200, ENGINE SELF RECOVERED. ENGINE WAS REMOVED FOR METAL IN THE TAILPIPE, IT HAD A NO RMAL ECM TREND PLOT. AT ENGINE TEARDOWN, A STAGE 2 TURBINE BLADE FAILURE WAS FOUND TO BE THE CAUSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121900035 20021219 00035 NE 2002 12 19 2002UALA01710 2 20021110 A 7310 MS8005E111CFBA LINE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUEL PRESSURE KINKED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 365UA 24534 724415 AIRCRAFT RETURNED TO FIELD WHEN FUEL FILTER BYPASS LIGHT ILLUMINATED DURING CLIMB. INTERMITTENT ILLUMINATION OF THE FUEL BYPASS WARNING LIGHT INDICATING EXCESSIVE PRESSURE DIFFERENTIAL ACROSS THE FUEL FILTER WAS ATTRIBUTED TO A KINK IN THE FLEXIBLE PRESSURE LINES WHICH ARE LOCATED BETWEEN THE FUEL FILTER AND THE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH. BOT H LINES HAVE BEEN REPLACED, ALONG WITH THE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH AS PRECAUTIONARY. THE FUEL FILTER WA S ALSO CHECKED FOR CONTAMINATION AND REPLACED. THE NEW FILTER WAS SUBSEQUENTLY RECHECKED AFTER 24 HOURS AND NO CONTAMIN ATION FOUND. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700206 20021217 00206 NM 2002 12 17 2002UALA01711 1 20021110 A 2751 INDICATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 WP 29 359UA 24452 AIRCRAFT DIVERTED TO A MAINTENANCE STATION WHEN CREW WAS UNABLE TO EXTEND THE FLAPS WHEN MAKING AN APPROACH TO THE SCHED ULED DESTINATION. FLAP POSITION INDICATOR. REPLACED FLAP POSITION INDICATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900038 20021219 00038 NM 2002 12 19 2002UALA01712 1 20021108 A 3350 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 935UA 26663 AFT CABIN EMERGENCY EXIT LIGHTING IS INOPERATIVE. REPLACED POWER STRIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700061 20021127 00061 NM 2002 11 27 2002UALA01713 1 20021111 A 5320 ANGLE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 948UA 26691 AFT CARGO COMPARTMENT DOOR CUTOUT DOOR THRESHOLD BULLNOSE ANGLE UNDER SILL WEB IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700062 20021127 00062 NM 2002 11 27 2002UALA01714 1 20021111 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 STATION 1002 STRINGER 14L FUSELAGE SKIN DENTED AT FRAME ON SKIN LAP. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALL ED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700063 20021127 00063 EU 2002 11 27 2002UALA01715 1 20021111 A 3320 325080 BALLAST AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN OVERHEATED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 478UA 1533 FLIGHT DIVERTED DUE TO BURNING ODOR. REPLACED BALLAST AT SEAT ROWS 9 & 10ABC, BALLAST HAD ELECTRICAL ODOR . 2 L 7 2 4F 4 F RT A28NM E40NE 2002112700067 20021127 00067 NM 2002 11 27 2002UALA01716 1 20021112 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 948UA 26691 FUSELAGE STATION 178 BULKHEAD WEB CRACKED AT RT UPPER RADAR MOUNT, LT LOWER RADAR MOUNT, RT LOWER RADAR MOUNT. MAJOR RE PAIR ACCOMPLISHED. ONE PIECE DOUBLER INSTALLED FOR ALL DAMAGE LOCATIONS. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700070 20021127 00070 SO 2002 11 27 H122002F00000 2 20020930 A 8500 ENGINE CESSNA 414 414A 2075907 CE CONT O520 TSIO520* 17040 SO RIGHT MALFUNCTIONED E H12A E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 GL 17 855H 414A0855 RT ENGINE INDICATED IMMINENT FAILURE. DECREASED MANIFOLD PRESSURE WAS FOLLOWED BY DROPPING OIL PRESSURE AND RISING OIL TEMPERATURE. RT ENGINE WAS SHUT DOWN (FEATHERED). RT ENGINE WILL BE REPLACED WITH OVERHAULED ENGINE. 1 L 7 2 3O 3 O A7CE E8CE 2002112700071 20021127 00071 NM 2002 11 27 2002UALA01717 1 20021112 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 CABIN FLOOR BEAM T CAP UPPER SURFACE STATION 291 RBL 10-50 HAS AREAS OF EXCESSIVE MATERIAL LOSS DUE TO CORROSION. MAJOR REPAIR ACCOMPLISHED. T CAP REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700072 20021127 00072 CE 2002 11 27 HSY2002F0000A 1 20020910 A 5312 26120605 BULKHEAD CESSNA 208 208B 2073701 CE PWA PT6 PT6A11 52043 NE FUSELAGE CRACKED E HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 924FE 6971 208B0024 STRUCTURAL DEFECT DISCOVERED DURING SCHEDULED INSPECTION (PHASE 5). METAL FATIGUE, CANTED BULKHEAD, STRUCTURAL REPAIR I NITIATED, AND WORK IS IN PROCESS. 1 H 7 1 3T 3 T A37CE E4EA 2002112700073 20021127 00073 2002 11 27 MV5R055M 4 20021024 A 2210 334C9A SERVO GULSTM 690TP 695A 7630519 SW GARRTT TPE331 TPE331* 01514 WP AUTO PILOT SEIZED B MV5R O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 11 695GG 449 96036 AILERON PRIMARY AUTO PILOT SERVO SEIZED. FLIGHT CREW APPLIED SUFFICIENT FORCE IN AN ATTEMPT TO FREE AILERON MOVEMENT. CAUSING AILERON CONTROL CABLE TO BECOME DISLODGED FROM FORWARD AILERON CONTROL DRUM. INVESTIGATION OF THE SERVO REVEALE D A BEARING FAILURE WITHIN THE SERVO ALLOWING BEARING MATERIAL TO RESTRICT SERVO MOVEMENT. 1 H 7 2 4T 3 T 2A4 E2WE 2002112700075 20021127 00075 SO 2002 11 27 C2XA02CL234 1 20021126 A 3350 20131A BATTERY PACK EMB 145 EMB145ER 3260211 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14940 6459 15 145033 DURING ROUTINE MAINTENANCE THE LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS AND THE AFT AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE.MAINTENANCE REPLACED THE #4 EMERGENCY BATTERY PACK.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED F OR SERVICE. 2 L 7 2 4F RT T00011AT 2002112700076 20021127 00076 SO 2002 11 27 SWIA200211371 1 20021026 A 2497 TERMINAL BLOCK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AHAR LOOSE A SWIA O OTHER G J MULTIPLE FAILURE WARNING INDICATION NR NOT REPORTED 1 NM 07 190SW 120050 MULTIPLE FAILURES ASSOCIATED WITH THE AHAR: HSI ROTATES 60 DEGREES-BOTH SIDES THEN CENTERS ADI-COMPUTER FAILURE LT SID E ASSOCIATED WITH A GYRO FLAG RIGHT SIDE COMPUTER FAILURE-NO GYRO FLAG.FOUND SEVERAL NUTS ON TB0033 LOOSE AND RUBBER N IPPLE ON W138-0001-2 MISSING. INSTALLED WASHERS AND TIGHTENED NUTS ON TB0033. INSTALLED RUBBER NIPPLE ON WIRE W138-0001 -2. INSTALLED RUBBER NIPPLE ON W158-0001-2 AND REPLACED ALL TERMINAL ENDS ON WIRES THAT ATTACH TO STUD NR 2 AND TIGHTEN ED ALL NUTS ON TB0034 IAW EMB WM 20-00-00. OPERATIONAL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2002112700077 20021127 00077 NM 2002 11 27 2002UALA01719 1 20021112 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 CABIN FLOORBEAM CORRODED, STA 365, RBL 6. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED SPLICE, ANGLE AND STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700078 20021127 00078 EU 2002 11 27 2002UALA01723 1 20021113 A 5340 FITTING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 467UA 1359 AFT CARGO DOOR CUT OUT LOWER SILL 3RD FROM FRONT LUG HAS GOUGE AFT LOWER END. MAJOR REPAIR ACCOMPLISHED. 3RD FROM FRON T LOWER LUG BLENDED & ROTO PEENED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112700079 20021127 00079 SO 2002 11 27 SWIA200211372 1 20021017 A 6120 78249046 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PROPELLER MALFUNCTIONED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 07 190SW DURING CLIMB, RIGHT NP DROPPED TO 96 PERCENT. TURNED OFF EEC WITH POWER LEVER AT FLIGHT IDLE AND CL MAX T6 780, TORQUE 97 PERCENT AND NP 56 PERCENT. WE FEATHERED THE ENGINE PER QRH PRECAUTIONARY ENGINE SHUT DOWN AND DIVERTED TO CYS. REPL ACED RT ENGINE PCU IAW MM 61-21-00. OPS CHECK GOOD. TRANSFER TUBE REMOVAL AND REINSTALLATION DONE PER 61-10-00. NO LE AKS NOTED.SN OFF 1213. 2 L 7 2 4T RT A31SO 2002112700080 20021127 00080 NM 2002 11 27 2002UALA01724 1 20021113 A 5512 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 948UA 26691 RT HORIZONTAL STABILIZER LEADING EDGE HAS 2 EA DENTS OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. FLUSH REPAIR DOUBLER IN STALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700081 20021127 00081 EA 2002 11 27 SWIA200211373 1 20021017 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 448SW 26 26 7677 STATUS MESSAGES JUST AFTER TAKEOFF ''FLT SPOILERS FAULT'' AND ''OB GRND SPOILERS FAULT''. RETURNED TO SLC. REMOVED AND REPLACED NR 1 SECU. RAN SYSTEM BITE AND SECU TEST. OPS CHECK GOOD. P/N OFF: 2 L 7 2 4F RT A21EA 2002112700082 20021127 00082 NM 2002 11 27 2002UALA01725 1 20021113 A 5320 CHANNEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 CABIN FLOOR STRUCTURE CHANNEL BETWEEN STATION 365.25 AND 377.7 RBL 12 STR 17R CORRODED. MAJOR REPAIR ACCOMPLISHED. REM OVED CHANNEL AND INSTALLED NEW PART. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700083 20021127 00083 SO 2002 11 27 SWIA200211374 1 20021003 A 5310 BEAM EMB 120 EMB120ER 3260203 SO CENTER CARGO BAY DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 585SW 120353 CENTER CARGO BAY OMEGA BEAM AFT IS DAMAGED. REMOVED AND REPLACED OMEGA BEAM IAW SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002112700084 20021127 00084 NM 2002 11 27 2002UALA01726 1 20021114 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PRESSURE DECK STA 1692 RBL 5.5 & STA 1694 RBL 7.25 CORRODED. MAJOR REPAIR ACCOMPLISHED. BLENDED CORROSION AND INST ALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700085 20021127 00085 NM 2002 11 27 2002UALA01727 1 20021113 A 5242 SEAL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE E/E BAY DOOR OUT OF POSITION A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 941UA 26676 NA AIRCRAFT RETURNED TO FIELD WHEN IT FAILED TO PRESSURIZE. FOUND E/E DOOR SEAL OUT OF ALIGNMENT. ADJUSTED SEAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700086 20021127 00086 SO 2002 11 27 SWIA200211375 1 20021003 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RIGHT TAILPIPE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 585SW 120353 RT OUTBOARD INTERNAL FRAME UNDER TAIL PIPE ATTACHMENT CRACKED. FOUND DURING C CHECK INSPECTION. FABRICATED AND INSTALL ED .050 ALUMINUM DOUBLER TO FRAME DAMAGE IAW EMB120 SRM 51-00-00 & 51-40-02. 2 L 7 2 4T RT A31SO 2002121700207 20021217 00207 NM 2002 12 17 2002UALA01728 1 20021113 A 3397 58781 CABLE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 940UA 26675 EMERGENCY EXIT LIGHTING FROM ROW 15 TO THE END OF CABIN IS INOPERATIVE. EEL POWER STRIP CABLE ASSY INOPERATIVE. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700087 20021127 00087 SO 2002 11 27 SWIA200211376 1 20021003 A 5411 BRACKET EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 585SW 120353 FRAME 17 ON THE RT NACELLE OUTBOARD HAS A CRACKED ATTACH BRACKET. FOUND DURING C CHECK INSPECTION. STOP-DRILLED CRACK AND INSTALLED REPAIR DOUBLER ON THE FRAME IAW EMB SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002112700088 20021127 00088 EU 2002 11 27 2002UALA01729 1 20021114 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 467UA 1359 AIRCRAFT SUSTAINED DAMAGE TO AFT LWR BELLY SKIN BETWEEN FRAME 58 AND 64 BETWEEN STRINGER 41R AND 40L. MAJOR REPAIR ACCO MPLISHED. INSTALLED SKINS AND DOUBLER. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112700089 20021127 00089 SO 2002 11 27 SWIA200211377 1 20021003 A 5320 CLIP EMB 120 EMB120ER 3260203 SO CENTER CARGO BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 585SW 120353 CENTER CARGO BAY FLOORBEAM HAS 2 CRACKED CLIPS. FOUND DURING C CHECK INSPECTION. REMOVED OLD CLIPS, FABRICATED AND INS TALLED NEW CLIPS IAW SRM 51-40-02 AND 51-00-00. 2 L 7 2 4T RT A31SO 2002112700090 20021127 00090 SO 2002 11 27 SWIA200211378 1 20021003 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 585SW 120353 FRAME 13 LT AND RT SIDES OF COCKPIT OPENING CRACKED ON BOTH SIDES OF VERTICAL BRACE. FOUND DURING C CHECK INSPECTION. FABRICATED AND INSTALLED .040 ALUM. DOUBLER FOR THE CRACKED FRAME 13'S IAW EMB SRM 51-00-00 & 51-40-02. 2 L 7 2 4T RT A31SO 2002121700208 20021217 00208 EU 2002 12 17 2002UALA01730 1 20021114 A 2611 RAI2800M0504 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SMOKE DETECTION MALFUNCTIONED A UALA F B A ACTIVATE FIRE EXT. EMER. DESCENT UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 417UA 483 FLIGHT MADE AN EMERGENCY LANDING DUE TO A FIRE WARNING IN THE AFT CARGO PIT. SMOKE DETECTOR CONTROL UNIT WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112700091 20021127 00091 SO 2002 11 27 SWIA200211379 1 20021003 A 5720 CLIP EMB 120 EMB120ER 3260203 SO RT FUEL CELL RIB CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 585SW 120353 RIGHT FUEL CELL RIB NR 15, 3RD CLIP FROM FORWARD (LONGER CENTER CLIP) CRACKED AT FORWARD END. FOUND DURING C CHECK INSP ECTION. REMOVED AND REPLACED CLIP IAW SRM 51-40-02. 2 L 7 2 4T RT A31SO 2002112700092 20021127 00092 EU 2002 11 27 2002UALA01731 1 20021115 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 467UA 1359 SKIN IS DAMAGED FROM STRINGER 41R TO 40L, FRAMES 58 THROUGH 61. MAJOR REPAIR ACCOMPLISHED. REPLACED DAMAGED SKIN SECTI ON. 2 L 7 2 4F 4 F RT A28NM E40NE 2002121900042 20021219 00042 NM 2002 12 19 2002UALA01732 1 20021114 A 2410 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT GENERATOR FAILED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 507UA 24743 RT GENERATOR FAILED. RT AC INTEGRATED DRIVE GENERATOR (IDG) FAILURE. REPLACED THE RT IDG AND REPLACED IDG CONNECTOR D5 134. THE IDG PASSED ALL PRELIMINARY TESTS. NO FAULTS FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700093 20021127 00093 NM 2002 11 27 2002UALA01733 1 20021114 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 MAIN CABIN FLOOR BEAM T-CAP CORRODED STATION 850-854, RBL 48-RBL 52. MAJOR REPAIR ACCOMPLISHED. REPAIRED ANGLE-DOUBLER AND SHIMS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002112700094 20021127 00094 EA 2002 11 27 SWIA200211380 1 20021024 A 2752 853D10017 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 438SW 7574 FLAPS FAIL CAUTION MESSAGE RECEIVED ON APPROACH. FLAPS FAILED AT 4 DEGREES. NR 3 FLAP ACTUATOR ON LT SIDE CHATTERS ON EXTENSION. REMOVED FLAP PDU AND REPLACED IT WITH A SERVICEABLE UNIT IAW CL600 27-52-05. INFLIGHT FUNCTION TEST REQUIR ED - FAILED. REMOVED AND REPLACED LT NR 3 FLAP ACTUATOR. OPS CHECK GOOD IAW RII 27-412. PCU PN OFF 865D100-7 SN OFF 0870. 2 L 7 2 4F RT A21EA 2002112700095 20021127 00095 NM 2002 11 27 2002UALA01734 1 20021114 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 MAIN CABIN FLOOR BEAM T-CAP CORRODED STATION 850-854, LBL 48 TO LBL 52. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE SPLICE S AND SHIMS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002112700096 20021127 00096 EA 2002 11 27 SWIA200211381 1 20021027 A 2742 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA H/S ACTUATOR MALFUNCTIONED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 406SW 118 118 7030 STAB CH 1 WILL NOT ENGAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-42-01. R EMOVED AND REPLACED HORIZONTAL STAB TRIM MOTOR CONTROL UNIT IAW 27-42-05. OPS CHECK GOOD IAW MM 27-40-00 & 27-41-00. PN OFF 8369-3 SN OFF 748. 2 L 7 2 4F RT A21EA 2002112700097 20021127 00097 EU 2002 11 27 2002UALA01735 1 20021116 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 467UA 1359 CABIN FLOOR STRUCTURE FRAME 12+2, LBL 9 TRANSVERSE FLOORBEAM CRACKED FWD FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. SPL ICED IN NEW SECTION OF TRANSVERSE FLOORBEAM WITH 4EA NESTED ANGLES. 2 L 7 2 4F 4 F RT A28NM E40NE 2002112700098 20021127 00098 NM 2002 11 27 2002UALA01736 1 20021116 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 AFT CARGO DOOR FORWARD CUTOUT AT STRINGER 22 SKIN EDGE CLEAN UP OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700099 20021127 00099 SO 2002 11 27 SWIA200211382 1 20021021 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 189SW 53 120048 ROW 3 OVERHEAD LIGHT INOP. REPLACED FORWARD EMERGENCY LIGHTING POWER SUPPLY. ROW 3 OVERHEAD LIGHT OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112700100 20021127 00100 SO 2002 11 27 SWIA200211383 1 20021026 A 7712 TORQUE SENSOR EMB 120 EMB120ER 3260203 SO RIGHT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING R F PARTIAL RPM/PWR LOSS FLT CONT AFFECTED CL CLIMB 1 NM 07 569SW 120342 ABOVE V1, AFTER FLAP & GEAR RETRACTION, THE RT ENGINE FEATHERED. TQ READ ZERO, ALL OTHER PARAMETERS NORMAL. POWER LEVE R WAS BROUGHT TO FLIGHT IDLE, CONDITION LEVER FEATHER, ENGINE WAS LEFT RUNNING AND A SINGLE ENGINE LANDING WAS PERFORMED . REPLACED RT PROP ASSEMBLY IAW EMB120 MM 61-10-03. COMPLIED WITH RIGHT ENGINE BOROSCOPE INSPECTION PER P&W MM. COMP LIED WITH OVERTORQUE FORM ST72-334. ALL INSPECTIONS FOUND TO BE FREE OF DISCREPANCIES. REPLACED RT ENGINE TORQUE SENSO R WITH SERVICEABLE UNIT. PERFORMED ENGINE RUN-UP, TORQUE CHECKS GOOD, ALL OTHER PARAMETERS NORMAL. PN OFF 3116942-01 SN OFF 7537. 2 L 7 2 4T RT A31SO 2002112700101 20021127 00101 SO 2002 11 27 SWIA200211384 1 20021012 A 5310 BUTT STRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 560SW 120334 FORWARD CENTER BUTT STRAP IS CORRODED IN CABIN (IN FRONT OF GALLEY). FOUND DURING C CHECK INSPECTION. REPLACED BUTT ST RAP IAW 120 SRM 51-10-02. 2 L 7 2 4T RT A31SO 2002112700102 20021127 00102 SO 2002 11 27 SWIA200211385 1 20021012 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 560SW 120334 FORWARD LEFT FLOOR SEAT TRACK FOUND CORRODED. FOUND DURING C CHECK INSPECTION. REMOVED AND REPLACED LEFT FORWARD SEAT TRACK. 2 L 7 2 4T RT A31SO 2002112700103 20021127 00103 SO 2002 11 27 SWIA200211386 1 20021012 A 5347 GALLEY TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 560SW 120334 GALLEY, FORWARD INBOARD LOWER ATTACH POINT TRACK ON FLOOR, HAS CORROSION. FOUND DURING C CHECK INSPECTION. REPLACED FL OOR TRACK THAT SERVES AS FORWARD LOWER INBOARD ATTACHMENT POINT FOR GALLEY. 2 L 7 2 4T RT A31SO 2002112700104 20021127 00104 2002 11 27 SWIA200211387 4 20021026 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO ELEVATOR MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 196SW 120151 LOUD SOUND OF CABLE RUBBING AS THE YOKE IS PULLED BACK. REPLACED ELEVATOR AUTOPILOT SERVO (SVO-65). OPS CHECK GOOD. SN OFF 7088. 2 L 7 2 4T RT A31SO 2002112700105 20021127 00105 SO 2002 11 27 SWIA200211388 1 20021024 A 2701 YOKE EMB 120 EMB120ER 3260203 SO CONTROL COLUMN CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 229SW 120305 CAPTAINS YOKE IS CRACKED. REMOVED AND REPLACED CAPTAIN'S YOKE IAW 07-11-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112700106 20021127 00106 EA 2002 11 27 SWIA200211389 1 20021022 A 3297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA ANTI- SKID SYS DAMAGED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 432SW 7548 ON TAKEOFF ROLL PRIOR TO V1, BOTH INBOARD AND OUTBOARD ANTI-SKID CAUTION LIGHTS ILLUMINATED. ABORTED TAKEOFF AND RETUR NED TO GATE. INSPECTED ALL WHEEL SPEED TRANSDUCERS AND ANTI-SKID SUBHARNESSES. FOUND NR 1 OB SUBHARNESS BACKSHELL AND WIRING DAMAGED. REMOVED AND REPLACED NR 1 OB ANTISKID SUBHARNESS IAW TEMPCO CMM 32-61-20-00. CONDUCTED HIGH SPEED TAXI CHECK. ALL OPERATIONS NORMAL. NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A21EA 2002112700107 20021127 00107 SO 2002 11 27 SWIA200211390 1 20021021 A 3260 CONNECTOR EMB 120 EMB120ER 3260203 SO MLG PROX SENSOR CONTAMINATED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 198SW 120227 LANDING GEAR WOULD NOT COME UP. USED DOWNLOCK RELEASE TO RAISE GEAR. CLEANED CONTANIMATION FROM LEFT MLG PROXIMITY SEN SOR CONNECTOR. LANDING GEAR OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112700108 20021127 00108 SO 2002 11 27 SWIA200211391 1 20021023 A 2751 3471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 214SW 120280 FLAP DISAGREEMENT ON TAKEOFF. RECYCLED 3 TIMES - UNSUCCESSFULLY. FLAP DISAGREEMENT ON OUTBOARD PAIR DURING RETRACTION. RETURNED TO DEN. CLEANED AND INSPECTED FLAP TRACKS AND RERACKED FCU. INSTALLED SERVICEABLE FLAP ANNUNCIATOR. OPERAT ED FLAPS SEVERAL TIMES. NO DEFECTS NOTED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112700109 20021127 00109 EA 2002 11 27 SWIA200211392 1 20021028 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 442SW 7609 RECEIVED ''FLAPS FAIL'' MESSAGE DURING DESCENT. MESSAGE DID NOT CLEAR. REMOVED FECU AND REPLACED IT WITH A SERVICEABLE UNIT IAW CL600 MM 27-51-05. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002112700110 20021127 00110 NM 2002 11 27 2002UALA01738 1 20021117 A 5310 STOP FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 FORWARD GALLEY DOOR CUTOUT, UPPER FORWARD STOP CASTING CRACKED ON TOP SIDE. MAJOR REPAIR ACCOMPLISHED. REPLACED STOP P LATE CASTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700111 20021127 00111 EA 2002 11 27 SWIA200211394 1 20020924 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 597SW 7293 FS 280.0 RBL 9.0 FLOORBEAM ANGLES INBOARD AND OUTBOARD FOUND CRACKED. FOUND DURING C CHECK INSPECTION. NEW ANGLES FIT AND INSTALLED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13 & 51-42-21. P/N: 601R31113-58 2 L 7 2 4F RT A21EA 2002112700112 20021127 00112 NM 2002 11 27 2002UALA01739 1 20021117 A 5320 STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 FORWARD GALLEY DOOR CUTOUT TOP CENTER SUPPORT STRAP CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SUPPORT STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700113 20021127 00113 EA 2002 11 27 SWIA200211395 1 20020924 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 597SW 7293 FS 484 RBL 27 INTERCOSTAL ATTACH ANGLE FOUND CRACKED. FOUND DURING C CHECK INSPECTION. NEW ANGLE (CLIP) FITTED AND INS TALLED IAW CRJ REO 601R-53-41-059 REV ''A''. 2 L 7 2 4F RT A21EA 2002112700114 20021127 00114 NM 2002 11 27 2002UALA01740 1 20021117 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 CABIN FRAME AT STATION 827 CRACKED AT STRINGER 9R AT FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTING DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700115 20021127 00115 EA 2002 11 27 SWIA200211396 1 20020924 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 597SW 7293 FS 484 LBL 27.0 INTERCOSTAL ANGLE FOUND CRACKED. FOUND DURING C CHECK INSPECTION. NEW ANGLE FIT AND INSTALLED IAW CRJ REO 601R-53-41-059 REV. ''A''.P/N: 601R31171-17 2 L 7 2 4F RT A21EA 2002112700116 20021127 00116 EA 2002 11 27 SWIA200211397 1 20020924 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT PYLON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 597SW 7293 FS 718.0 RT PYLON FITTING ANGLE CRACKED. FOUND DURING C CHECK INSPECTION. NEW TIE ANGLE FIT AND INSTALLED IAW SRM 51-4 0-11, 51-42-06 AND 51-42-21. 2 L 7 2 4F RT A21EA 2002112700117 20021127 00117 NM 2002 11 27 2002UALA01741 1 20021117 A 5330 SKIN BOEING 777 777222 1385219 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 204UA 28713 AFT FUSELAGE RT SIDE SKIN CRACKED STA 2668 12 INCHES FWD OF LWR HORIZONTAL STABILIZER FAIRING. MAJOR REPAIR ACCOMPLISHE D. DOUBLER AND FILLER REPAIR INSTALLED. 2 L 7 2 4F RT T0001SE 2002112700118 20021127 00118 SO 2002 11 27 SWIA200211398 1 20021002 A 7921 1602825 OIL COOLER EMB 120 EMB120ER 3260203 SO LEFT ENGINE CHAFED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 251YV 120251 LEFT ENGINE OIL COOLER OUTBOARD FORWARD FRAME CHAFED THROUGH. FOUND DURING C CHECK INSPECTION. REPLACED LEFT OIL COOLE R WITH SERVICEABLE PART. 2 L 7 2 4T RT A31SO 2002112700119 20021127 00119 NM 2002 11 27 2002UALA01742 1 20021117 A 5330 SKIN BOEING 777 777222 1385219 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 204UA 28713 LEFT HAND FUSELAGE STATION 2268 EXTERNAL SKIN CRACKED 12 INCHES FWD OF HORIZONTAL STABILIZER LOWER FAIRING. MAJOR REPAI R ACCOMPLISHED. DOUBLER AND FILLER REPAIR INSTALLED. 2 L 7 2 4F RT T0001SE 2002112700120 20021127 00120 SO 2002 11 27 SWIA200211399 1 20021002 A 5411 FRAME EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT & LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 251YV 120251 LT AND RT NACELLE FRAME NR 1 FOUND CRACKED AT TORSION MOUNT AREA. FOUND DURING C CHECK INSPECTION.COMPLIED WITH PART II OF SB 120-54-0036. REPLACED RIGHT AND LEFT FRAME NR 1 WITH SERVICABLE UNITS. 2 L 7 2 4T 4 T RT A31SO E20NE 2002112700121 20021127 00121 SO 2002 11 27 SWIA200211400 1 20021002 A 5320 BEAM EMB 120 EMB120ER 3260203 SO LEFT WINDOW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 251YV 120251 DIRECT VISION WINDOW LOWER BEAM CRACKED FORWARD OF LT WINDOW POST. FOUND DURING C CHECK INSPECTION. REPAIRED CRACK ON DV WINDOW LOWER BEAM PER EMBRAER GST-3029/02 DATED 10-9-02. 2 L 7 2 4T RT A31SO 2002112700122 20021127 00122 SO 2002 11 27 SWIA200211401 1 20021002 A 5320 BRACKET EMB 120 EMB120ER 3260203 SO RT WINDOW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 251YV 120251 RIGHT AND LEFT FRAME 9 BRACKETS FORWARD AND BELOW DV WINDOW CRACKED. FOUND DURING C CHECK INSPECTION. RE-WORKED RIGHT FRAME 9 IAW SB 120-53-0073. 2 L 7 2 4T RT A31SO 2002112700123 20021127 00123 SO 2002 11 27 SWIA200211402 1 20021002 A 5320 SUPPORT EMB 120 EMB120ER 3260203 SO LT WINDOW CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 251YV 120251 SUPPORT AFT OF CAPTAIN'S DIRECT VISION WINDOW CRACKED. FOUND DURING C CHECK INSPECTION. REPLACED SUPPORT AFT OF CAPTAI N'S DV WINDOW WITH A SERVICEABLE UNIT IAW MM 53-00-00. 2 L 7 2 4T RT A31SO 2002112700124 20021127 00124 SO 2002 11 27 SWIA200211403 1 20021031 A 2133 2091G010800 OUTFLOW VALVE EMB 120 EMB120ER 3260203 SO CABIN PRESSURE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 198SW 6010 1400 120227 AUTO PRESSURIZATION WOULD NOT HOLD - CLIMB 2000 FPM - SWITCH TO MANUAL PRESSURIZATION AND MANUAL CONTROLLER COULD NOT MA INTAIN PRESSURIZATION EITHER. RETURNED TO SLC. REPLACED ELECTROPNEUMATIC OUTFLOW VALVE WITH A SERVICEABLE UNIT IAW 21- 30-03. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112700125 20021127 00125 NM 2002 11 27 2002UALA01743 1 20021115 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT CABIN PRESSURE DECK CORRODED STATION 1680 TO STA 1683, RBL 42 TO RBL 53. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUB LER AND TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700126 20021127 00126 NM 2002 11 27 2002UALA01744 1 20021118 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 CABIN STATION 827 FRAME CRACKED AT STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700127 20021127 00127 NM 2002 11 27 2002UALA01746 1 20021119 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 BODY STATION 277 FRAME STRINGER CLIP CRACKED AT STRINGER 15R. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700128 20021127 00128 NM 2002 11 27 2002UALA01747 1 20021119 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 CRACK IN BODY STATION 867 FRAME AT STRINGER 9 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700129 20021127 00129 SO 2002 11 27 SWIA200211404 1 20021030 A 3260 TARGET EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 213SW 120277 ON TAKEOFF WE PUT THE GEAR HANDLE UP, ALL LIGHTS WENT OUT EXCEPT LEFT RED ''A''. A VERY LOUD NOISE ALSO REMAINED. WE R ECYCLED THE GEAR 4 TIMES AND HAD THE SAME RESULTS. RETURNED TO JAC. ADJUSTED LEFT MAIN GEAR TARGET AND RE-RACKED CANNO N PLUG FOR LANDING GEAR DOOR SOLENOID VALVE. SWUNG GEAR 12 TIMES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112700130 20021127 00130 NM 2002 11 27 2002UALA01748 1 20021119 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 FUSELAGE FRAME STATION 500A CRACKED AT STRINGER 9L AT OVERHEAD BIN ATTACH CLIP FASTENER. MAJOR REPAIR ACCOMPLISHED. IN STALLED FRAME REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700131 20021127 00131 SO 2002 11 27 SWIA200211405 1 20021030 A 3010 BOOT EMB 120 EMB120ER 3260203 SO LT H/S DEICE SYS TORN A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 207SW 120266 RIGHT AND LEFT OUTBOARD STAB AND VERT FIN BOOTS INOP AFTER 28 SECONDS ON TIMERS 1 & 2. RETURNED TO DEN. REPLACED LEFT HORIZONTAL STAB DEICE BOOT IAW MM CHAPTER 30-10-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112700132 20021127 00132 NM 2002 11 27 2002UALA01750 1 20021120 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 FLOORBEAM SEAT TRACK SPLICE CRACKED AT STATION 786, LBL 10. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM WITH REPAIR SPLICES AND FILLERS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002112700133 20021127 00133 SO 2002 11 27 SWIA200211406 1 20021029 A 2460 RELAY EMB 120 EMB120ER 3260203 SO COCKPIT ARCED A SWIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 308SW 120326 RELAYS FO SIDE PANEL HOT. SMOKE ODOR IN COCKPIT. REPLACED APU FEEDER PROTECTION RELAY K0152 AND BUS BARS W1264, W163 D UE TO ARCING. OPERATED AIRCRAFT ELECTRICAL UNDER HEAVY LOADS ON APU GENERATOR WITHOUT CONTACTOR OR BUS BAR AREA SHOWING ANY SIGNS OF ABNORMAL HEATING. 2 L 7 2 4T RT A31SO 2003031300131 20030313 00131 NM 2003 3 13 2002UALA01751 1 20021120 A 3230 A42006028305 SOLENOID BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 347UA 24251 AIRCRAFT RETURNED TO FIELD WHEN THE LANDING GEAR FAILED TO RETRACT. THE LANDING GEAR FAILED TO RETRACT DUE TO A FAULTY AUTO FLOW REGULATOR. THE UNIT WAS REMOVED AND REPLACED WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700134 20021127 00134 SO 2002 11 27 SWIA200211407 1 20021026 A 7931 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 1 ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 393SW 120330 NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED INFLIGHT FOR 2 MINUTES, WITH NORMAL OIL PRESSURE OF 63 PSID. ALL OTHER INDIC ATIONS ALSO NORMAL.REMOVED AND REPLACED NR 1 ENGINE LOW OIL PRESSURE SWITCH. CONDUCTED ENGINE RUN. NO LEAKS NOTED. CH ECKS GOOD. NO LIGHTS OR WARNINGS. IAW EMB120 MM 73-30-00. PROP HEAT CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002112700135 20021127 00135 SO 2002 11 27 SWIA200211408 1 20021030 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO MLG CONTAMINATED A SWIA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 07 198SW 120227 RT MAIN LANDING GEAR WOULD NOT RETRACT AFTER DEPARTURE. RECYCLED GEAR PER QRH. SUSPECT ICE. RETURNED TO SLC. REPLACE D RIGHT MLG PROXIMITY SENSOR AND HARNESS WITH NEW UNIT IAW AMM 32-01-01. OPS CHECK GOOD. P/N: ZS-00417-02, T0Q-120-20 505-1 2 L 7 2 4T RT A31SO 2002112700136 20021127 00136 SO 2002 11 27 SWIA200211409 1 20021030 A 6123 PUMP EMB 120 EMB120ER 3260203 SO RT ENGINE FLUCTUATES A SWIA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 07 190SW 120050 AUX FEATHER PUMP BROKEN, RT ENGINE TORQUE FLUCTUATES 3 PERCENT TO 4 PERCENT AT CRUISE. REMOVED AND REPLACED AUX FEAT HER PUMP. 2 L 7 2 4T RT A31SO 2002120400132 20021204 00132 NM 2002 12 4 2002UALA01752 1 20021121 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 RT FUSELAGE FRAME 480 CRACKED AT STRINGER 9R OVERHEAD BIN ATTACH CLIP FASTENER. MAJOR REPAIR ACCOMPLISHED. DOUBLER INS TALLED ON FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2002120400133 20021204 00133 NM 2002 12 4 2002UALA01753 1 20021121 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 CABIN FRAME AT STATION 887 STRINGER 9R CRACKED AT FASTENER. MAJOR REPAIR ACCOMPLISHED. EXTERNAL NESTING DOUBLER INSTALL ED. 2 L 7 2 4F 4 F RT A16WE E2GL 2003011500134 20030115 00134 NM 2003 1 15 2002UALA01754 1 20021121 A 3222 STRUT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG INCORRECT A UALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 WP 29 804UA 759 UNABLE TO RETRACT LANDING GEAR. THE NLG LOWER STRUT ASSEMBLY WAS FOUND TO BE ASSEMBLED INCORRECTLY. THE UPPER CAM WAS MISALIGNED PREVENTING THE SHOCK ABSORBER LUGS FROM ENGAGING INTO THE SHOCK STRUT BACKPLATE. THE NLG LOWER STRUT ASSEMBL Y, WHEELS, TIRES AND APPLICABLE SENSORS WERE REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2002121900046 20021219 00046 NM 2002 12 19 2002UALA01755 1 20021121 A 2910 271N63111132 LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT PYLON CRACKED A UALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 520UA 24890 ON LANDING, LOST RT HYDRAULICS. THE NR 2 ENGINE REVERSER HYDRAULIC PRESSURE TUBE WORE THRU AND LEAKED. CAUSE OF THE TUB ING WEAR WAS FROM A DEGRADED CLAMP RUBBER SLEEVE CAUSED BY ENGINE VIBRATION. TUBE WAS REPLACED AND A NEW CLAMP WAS INST ALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002112700137 20021127 00137 NM 2002 11 27 2002UALA01756 1 20021120 A 5753 65C263102 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE T/E FLAP BIRD STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 31126 24301 RT INBOARD FLAP SKIN DAMAGED FROM A BIRD STRIKE. MAJOR REPAIR ACCOMPLISHED. REPLACED 54 INCH SECTION OF THE UPPER CHOR D. 2 L 7 2 4F 4 F RT A16WE E2GL 2002112700138 20021127 00138 EA 2002 11 27 SWIA200211498 1 20021118 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA LEFT SIDE, COCKP CRACKED A SWIA O OTHER P NO WARNING INDICATION AP APPROACH 1 NM 07 917SW 7641 LEFT SIDE WINDOW CRACKED ON BASE TO FINAL @ 5500'. REMOVED & REPLACED LT SIDE WINDOW WITH SERVICEABLE UNIT IAW MM 56-12 -01 & RII56-402. OPS CHECK GOOD. PN OFF NP-139322-5 SN OFF 01354H5562. 2 L 7 2 4F RT A21EA 2002112700139 20021127 00139 WP 2002 11 27 ZW0A021191 1 20021126 A 2500 8921460G5 WATER HEATER DOUG DC9 DC982 3022082 WP A ZW0A K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 13 958U 49703 FIRST CLASS LAV WATER HEATER CAUSED CIRCUIT BREAKER TO OPEN. REMOVED AND REPLACED WATER HEATER. LAST CHECK C PERFORMED I N STL 06/17/2002 --CLOSED-- 2 L 7 2 4F A6WE 2002112900001 20021129 00001 SO 2002 11 29 SWIA200211411 1 20021029 A 2752 3203001005 ACTUATOR EMB 120 EMB120RT 3260202 SO LT TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED LD LANDING 1 NM 07 269UE 9 9 120194 AFTER FLAP RETRACTION ON LANDING, THE INBOARD PAIR OF FLAPS REMAINED AT 25 DEGREES. THERE WERE NO CONTROL FAULTS OR DIS AGREEMENT WARNINGS. AFTER RESETTING THE SYSTEM, THE FLAPS RETRACTED. REPLACED LEFT INBOARD FLAP ACTUATOR WITH SERVICEA BLE UNIT IAW MM 27-50-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112900002 20021129 00002 SO 2002 11 29 SWIA200211412 1 20021030 A 3230 LANDING GEAR EMB 120 EMB120ER 3260203 SO LT & RT MALFUNCTIONED A SWIA A UNSCHED LANDING J E F WARNING INDICATION VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 NM 07 218SW 120287 UPON GEAR RETRACTION, WE GOT A GEAR DISAGREEMENT ON BOTH MAIN GEAR WITH LOUD VIBRATION. CYCLED GEAR 3 TIMES. DID NOT C ORRECT IT. RETURNED TO RDM. PERFORMED GEAR SWING. SYSTEM OPS CHECK GOOD. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4T RT A31SO 2002112900003 20021129 00003 SO 2002 11 29 SWIA200211414 1 20021031 A 2751 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FLAP ACTUATOR CONTAMINATED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 214SW 120280 FLAP DISAGREEMENT THAT WOULD NOT CLEAR AFTER TAKEOFF. RETURNED TO SLC. DEICE FLUID FOUND IN OUTBOARD FLAP ACTUATOR CON NECTOR PLUGS. CLEANED CONNECTOR PLUGS. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 2002112900004 20021129 00004 EA 2002 11 29 SWIA200211415 1 20021030 A 3040 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA PITOT HEAT ILLUMINATED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 448SW 7678 ''STBY PITOT HEAT'' CAUTION MESSAGE WILL NOT CLEAR PER QRH PROCEDURE. RETURNED TO SLC. CYCLED POWER, PULLED & RESET CB P3-B6 AND CB4A13. MESSAGE CLEARED. 2 L 7 2 4F RT A21EA 2002112900005 20021129 00005 EA 2002 11 29 SWIA200211416 1 20021029 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ACTIVATED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 493SW 7450 WHEN SELECTING FLAPS FROM 20 DEGREES TO 30 DEGREES, WE RECEIVED A ''FLAPS FAIL'' MESSAGE. PERFORMED QRH PROCEDURE AND L ANDED WITH FLAPS AT 20 DEGREES. COMPLIED WITH AD 98-20-01. NO DISCREPANCIES NOTED. FLAPS FAIL MESSAGE CLEARED. 2 L 7 2 4F RT A21EA 2002112900006 20021129 00006 EA 2002 11 29 SWIA200211417 1 20021030 A 2421 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA NR 2 GEN ILLUMINATED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 426SW 7468 AT START OF TAKEOFF WE RECIEVED IDG NR 2 AND GEN NR 2 CAUTION MESSAGES. CLEARED RUNWAY, RESET PER QRH AND CLEARED FAULT S. NR 2 GENERATOR CHECKS NORMAL ON GROUND RUN UP. 2 L 7 2 4F RT A21EA 2002112900007 20021129 00007 SO 2002 11 29 SWIA200211418 1 20021104 A 5752 TAB EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT AILERON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 568SW 120343 LT AILERON TRIM TAB CRACKED ON LOWER INBOARD SIDE.REMOVED AND REPLACED LEFT AILERON TRIM TAB ASSEMBLY WITH SERVICEABLE U NIT IAW MM 27-12-02. 2 L 7 2 4T 4 T RT A31SO E20NE 2002112900008 20021129 00008 SO 2002 11 29 SWIA200211419 1 20021101 A 4920 APU EMB 120 EMB120ER 3260203 SO APU BAY SMOKE A SWIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 223SW 120291 RT PACK BLOWS HOT AIR AND SETS OFF LAV SMOKE DETECTOR WITH PROMINENT PACK BURNING ODOR. RAN BOTH ENGINES WITH RT PACK O N. FOUND LAV SMOKE DETECTOR NOT GOING OFF. RAN APU WITH THE RT PACK ON. FOUND THAT THE APU BLEEDS SMOKE INTO THE CABI N. SUPPLEMENTAL REPORT FORTHCOMING. 2 L 7 2 4T RT A31SO 2002112900009 20021129 00009 2002 11 29 SWIA200211420 4 20021101 A 2210 6229968001 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NR 2 YAW DAMPER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 916SW 7634 YAW DAMPER NR 2 FAILED IN FLIGHT. MESSAGE ON EICAS. REMOVED AND REPLACED NR 2 YAW DAMP LINEAR ACTUATOR IAW CRJ MM 22-2 2-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002112900010 20021129 00010 SO 2002 11 29 SWIA200211422 1 20021104 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO NR 2 ENGINE ACTIVATED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 567SW 120342 TRIPLE CHIME ''OIL'' WARNING ON ROTATION. FLUCTUATION 45 TO 55 PSID ON NR 2 ENGINE. RETURNED TO SBA. ADDED 1-1/2 QUART S OF OIL TO NR 2 ENGINE. RAN NR 2 ENGINE EXTENSIVELY. COULD NOT DUPLICATE LOW OIL PRESS OR FLUCTUATION. COMPLIED WITH ST72-344. 2 L 7 2 4T RT A31SO 2002112900011 20021129 00011 SO 2002 11 29 SWIA200211423 1 20021102 A 3230 LANDING GEAR EMB 120 EMB120ER 3260203 SO LEFT MALFUNCTIONED A SWIA A UNSCHED LANDING J E F WARNING INDICATION VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 NM 07 218SW 120287 LT MAIN GEAR WOULD NOT RETRACT UNTIL 5TH LANDING GEAR CYCLE. RETURNED TO PDX. SWING GEAR COULD NOT GET TO DUPLICATE. CHECKED GAP ON HOOK IAW 32-32-10 CHECK GOOD. ADJUSTED TARGET IAW MM 32-61-01 AND ADJUSTED GEAR DOOR SEQUENCE VALVE (I NBOARD AND OUTBOARD) IAW MM 32-32-04. SWUNG GEAR SEVERAL TIMES. SYSTEM CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002112900012 20021129 00012 EA 2002 11 29 SWIA200211424 1 20021005 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 FS 625.0 STR 14 INTERCOSTAL ANGLES (L&R) CRACKED. FOUND DURING C CHECK INSPECTION.FIT AND INSTALLED NEW ANGLES IAW CRJ SRM 51-40-11, 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2002112900013 20021129 00013 EA 2002 11 29 SWIA200211425 1 20021005 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 FS 621 (LT AND RT) FLOOR SUPPORT ANGLES CRACKED. FOUND DURING C CHECK INSPECTION. REPAIRED DAMAGED AREA IAW CRJ REO 601 R-53-117 REV ''A''.ANGLE P/N: 601453-61-117-3 FLOOR ANGLE P/N: 601R53-61-117-1 2 L 7 2 4F RT A21EA 2002112900014 20021129 00014 EA 2002 11 29 SWIA200211426 1 20021005 A 5415 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT & RT PYLON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 FS 718 LT AND RT PYLON FITTING TIE ANGLES CRACKED. FOUND DURING C CHECK INSPECTION. NEW TIE ANGLE FIT AND INSTALLED IA W CRJ SRM 51-40-11, 51-42-06, 51-42-21.P/N: 600-36030-31 2 L 7 2 4F RT A21EA 2002112900015 20021129 00015 EA 2002 11 29 SWIA200211427 1 20021005 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 FS 280 LBL 9.0 FLOORBEAM IB ANGLE CRACKED. FOUND DURING C CHECK INSPECTION. FIT AND INSTALLED NEW ANGLE IAW CRJ SRM 51 -40-11, 51-42-06, 51-42-21. 2 L 7 2 4F RT A21EA 2002112900016 20021129 00016 EA 2002 11 29 SWIA200211428 1 20021005 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 FS 280 RBL 9.0 FLOORBEAM ANGLES IB & OB CRACKED. FOUND DURING C CHECK INSPECTION. FIT AND INSTALL NEW ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21. P/N: 601R31113-58 2 L 7 2 4F RT A21EA 2002112900017 20021129 00017 EA 2002 11 29 SWIA200211429 1 20021005 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA E/E BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 ELECTRICAL BAY FLOOR FS 193.00 RT CRACKED. FOUND DURING C CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-11-24 5 REV. ''NC''. HFEC INSPECTION C/O ON CUTOUT AS REQUIRED IAW REO 601R-53-11-245. NO CRACKS FOUND. 2 L 7 2 4F RT A21EA 2002112900018 20021129 00018 EA 2002 11 29 SWIA200211430 1 20021005 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA INTERCOSTAL CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 FS 484.0 LBL 27.0 INTERCOSTAL CLIP CRACKED. FOUND DURING C CHECK INSPECTION. FIT AND INSTALLED NEW CLIP IAW CRJ REO 601R-53-41-059 REV. ''A''.P/N: 601R-31171-17 2 L 7 2 4F RT A21EA 2002112900019 20021129 00019 EA 2002 11 29 SWIA200211431 1 20021005 A 5412 FIREWALL CNDAIR CL600 CL6002B19 1900309 EA LT PYLON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 LT PYLON LOWER FIRE BOX PANEL (412 DB) HAS A CRACK IN ITS FORWARD DIVIDER. FOUND DURING C CHECK INSPECTION. REPLACED DIVIDER IAW CRJ SRM 51-42-06. 2 L 7 2 4F RT A21EA 2002112900020 20021129 00020 SO 2002 11 29 SWIA200211432 1 20021030 A 2133 2091G010800 OUTFLOW VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CABIN PRESSURE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 197SW 6010 1849 120186 AUTO PRESSURIZATION UNABLE TO CONTROL PRESSURE. CONTRACT MAINTENANCE PERFORMED MX PROCEDURE FOR DEFERRAL. NEXT FLIGHT RETURNED TO GJT WITH MANUAL PRESSURIZATION INOPERATIVE REMOVED AND REPLACED ELECTRO OUTFLOW VALVE IAW MM 21-30-03. OP S CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002112900021 20021129 00021 SO 2002 11 29 SWIA200211433 1 20021031 A 6120 78249046 PCU EMB 120 EMB120ER 3260203 SO LT PROPELLER MALFUNCTIONED A SWIA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 NM 07 293SW 120322 ABORTED TO - POSITIONED POWER LEVER, JUST BEYOND FLT. IDLE, LT TORQUE RAPIDLY INCREAASING (TO APPROX. 60 PERCENT TQ). N P DECREASED TO APPROXIMATELY 25 PERCENT THEN RAPIDLY INCREASED TO APPROXIMATELY 70 PERCENT WHILE STILL IN BETA ON THE LT ONLY. REPLACED LT PCU IAW MM 61-21-00. OPS AND LEAK CHECKED GOOD. 2 L 7 2 4T RT A31SO 2002112900022 20021129 00022 EA 2002 11 29 SWIA200211434 1 20021030 A 2120 SMOKE CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 903SW 7425 ON CLIMB OUT OF FAT, THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. RETURNED TO FAT. CHECKED ENGINE OIL SERVICE, FO UND SATISFACTORY. RAN ENGINES AT CRUISE FOR 5 MIN AT RUN-UP AREA AND COULD NOT FURTHER DUPLICATE, FOUND SATISFACTORY. 2 L 7 2 4F RT A21EA 2002112900023 20021129 00023 SO 2002 11 29 SWIA200211435 1 20021107 A 3260 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO LT MLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 566SW 120341 AFTER TAKEOFF, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION WHEN SELECTED. HAD TO SELECT DOWNLOCK RELEASE TO SELECT GEAR HANDLE TO THE UP POSITION. REPLACED LT LANDING GEAR PROXIMITY SWITCH PER EMB 120 32-41-01. OPS CHECK GO OD. 2 L 7 2 4T RT A31SO 2002112900024 20021129 00024 2002 11 29 SWIA200211436 4 20021104 A 2210 6229815704 CIRCUIT BOARD CNDAIR CL600 CL6002B19 1900309 EA NR 1 FLT COMP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 720SW 61 61 7297 STAB TRIM CHANNELS 1 AND 2 WILL NOT ENGAGE.REMOVED AND REPLACED NR 1 FCC CARD IAW 22-10-14. OPS CHECK GOOD.PN OFF/ON 62 2-9815-704 SN OFF 4X1A SN ON337. 2 L 7 2 4F RT A21EA 2002112900025 20021129 00025 EA 2002 11 29 SWIA200211437 1 20021106 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 440SW 7589 RT WINDSHIELD FAILED (OUTER PANEL SHATTERED) DURING CLIMBOUT. REMOVED AND REPLACED RT SIDE WINDSHIELD IAW RJ MM 56-11-0 1. 2 L 7 2 4F 4 F RT A21EA E15NE 2002112900026 20021129 00026 EA 2002 11 29 SWIA200211439 1 20021106 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 442SW 2159 2159 7609 ON TAXI TO THE GATE, RECEIVED A STAB CHANNEL 1 MESSAGE. THE HSTCU FLAGS THE MCU. REMOVED AND REPLACED THE MCU & HSTA PER MM 27-42-01 AND 27-42-05. OPS CHECKS GOOD. HSTA PN OFF 8396-3 SN OFF 843. 2 L 7 2 4F RT A21EA 2002112900027 20021129 00027 SO 2002 11 29 SWIA200211440 1 20021105 A 3350 BATTERY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 224SW 120294 EMERGENCY FLOOR LIGHTING AT ROW 5 AND 6 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112900028 20021129 00028 SO 2002 11 29 SWIA200211441 1 20021105 A 5280 BRACKET EMB 120 EMB120ER 3260203 SO LT MLG DOOR DAMAGED A SWIA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 NM 07 284YV 120284 LEFT OUTBOARD MAIN GEAR DOOR OPENED IN FLIGHT ON LEFT MAIN GEAR. REPLACED AFT HINGE BRACKETS ON LEFT NACELLE OUTBOARD F ORWARD DOOR WITH SERVICEABLE UNITS. STRAIGHTENED DOOR SKIN. INSPECTED LATCH MECHANISM AND FOUND TO BE SERVICEABLE. OP S CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112900029 20021129 00029 2002 11 29 SWIA200211442 4 20021103 A 2210 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA NR 1 YAW DAMPER MALFUNCTIONED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 448SW 2384 2384 7678 YAW DAMPER 1 INOP STATUS MESSAGE RECEIVED ON TAXI OUT. COULD NOT CLEAR THE MESSAGE. REMOVED AND REPLACED FCC CARD 1 IA W 22-12-14. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002112900030 20021129 00030 SO 2002 11 29 SWIA200211443 1 20021104 A 2435 23080013 CABLE EMB 120 EMB120ER 3260203 SO APU START GEN SHORTED A SWIA O OTHER M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 251YV 5486 2256 120251 APU WILL NOT START. STARTER APPEARS TO WORK BUT NO EGT OR RPM RISE. FOUND APU START/GEN GROUND CABLE MELTED DUE TO ARC ING BETWEEN GENERATOR TERMINALS. ALSO FOUND TERMINAL ON START/GEN TO BE MELTED. REMOVED START/GEN AND GROUND CABLE AND REPLACED WITH SERVICEABLE UNITS. REMOVED AND REPLACED APU GCU WITH A SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112900031 20021129 00031 EA 2002 11 29 SWIA200211444 1 20021107 A 2761 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERONS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 417SW 6891 6891 7400 SPOILERON FAULT MESSAGE (STATUS) APPEARED AFTER ENGINE START. REMOVED AND REPLACED SPOILERON PCU ASSEMBLY IAW 27-62-01. OPS AND LEAK CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002112900032 20021129 00032 2002 11 29 SWIA200211445 4 20021107 A 3414 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA AIRSPEED MALFUNCTIONED A SWIA O OTHER S AFFECT SYSTEMS DE DESCENT 1 NM 07 432SW 7548 OUT OF 32,000 FT, OBSERVED STANDBY AIRSPEED INDICATOR SHOWING 450 KTS (CAPT & FO A/S = 260 KTS). AS WE DESCENDED BACK TO SLC, STANDBY AIRSPEED INDICATOR CAME DOWN WITH ALTITUDE (ACTED LIKE ALTIMETER). REMOVED AND REPLACED STANDBY DRAIN A SSY IAW 34-11-00. OPS & LEAK CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002112900033 20021129 00033 EA 2002 11 29 SWIA200211446 1 20021107 A 3411 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 432SW 6757 2629 7548 STALL FAIL CAUTION MESSAGE ILLUMINATED CLIMBING OUT OF 500 FT. RAN QRH AND MESSAGE WOULD NOT CLEAR. RETURNED TO SLC. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW CRJ MM 27-35-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002112900034 20021129 00034 EA 2002 11 29 SWIA200211447 1 20021110 A 4950 1098047 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA APU MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 440SW 2521 2521 7589 BLEED AIR WILL NOT SWITCH FROM APU TO ENGINE BLEED AIR IN FLIGHT, THEN VERY HARD TO GET BACK ON APU BLEED. RETURNED TO SLC. REMOVED AND REPLACED APU LOAD CONTROL VALVE IAW MM 49-51-01. RAN APU AND LT AND RT ENGINES. ALL OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2002112900035 20021129 00035 EA 2002 11 29 SWIA200211448 1 20021108 A 2740 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 720SW 7297 ON CLIMB OUT OF SLC, RECEIVED STAB TRIM & MACH TRIM CAUTION MESSAGES . RAN QRH, COULD NOT GET TRIM ENGAGED. AFTER REPE ATED ATTEMPTS, GOT CH 2 ENGAGED. RETURNED TO SLC. REMOVED FO'S DISCONNECT SWITCH, CLEANED AND REINSTALLED PER MM 27-41 -30. OPS CHECK SYSTEM SEVERAL TIMES. GROUND CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002112900036 20021129 00036 SO 2002 11 29 SWIA200211449 1 20021108 A 3297 WIRE HARNESS EMB 120 EMB120ER 3260203 SO RT MLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 268UE 120207 LANDING GEAR WOULD NOT EXTEND, USED ELECTRICAL OVERRIDE. RH MLG GREEN ''A'' LIGHT REMAINS ON. REMOVED AND REPLACED RI GHT MAIN DOWNLOCK ''A'' PROXIMITY SENSOR HARNESS IAW MM 32-61-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112900037 20021129 00037 2002 11 29 SWIA200211450 4 20021108 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 268UE 120207 DISTINCT BUMP OR GRAB FELT IN LT RUDDER WHEN LEFT RUDDER IS PRESSED. REMOVED AND REPLACED RUDDER AUTOPILOT SERVO IAW MM 22-10-05. SYSTEM TESTS GOOD. 2 L 7 2 4T RT A31SO 2002112900038 20021129 00038 SO 2002 11 29 SWIA200211451 1 20021108 A 2120 ODOR EMB 120 EMB120ER 3260203 SO COCKPIT DETECTED A SWIA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 07 223SW 120291 ON TAKEOFF ROLL, WITH POWER SET AT APPROXIMATELY 90 PERCENT TORQUE, THE FLIGHT DECK STARTING TO FILL WITH UNIDENIFIED VA POR. CABIN ALSO BEGAN TO FILL WITH VAPOR. ABORTED TAKEOFF. PERFORMED ENGINE RUNS. FOUND TO BE WATER VAPOR IN THE AIR CONDITIONING SYSTEM. RAN PACKS FOR 15 MINUTES TO CLEAR. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112900039 20021129 00039 SO 2002 11 29 SWIA200211461 1 20021110 A 3010 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO LT STAB ANTI ICE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 196SW 120151 ON CLIMB OUT, WITH LIGHT ICING CONDITIONS PRESENT, THE OUTBOARD LT STAB FAILED. APPLIED QRH AND CHANGED TIMERS. REMAIN ED FAILED FOR 20 MINUTES, THEN WORKED AGAIN. RETURNED TO SLC. REPLACED LEFT OUTBOARD STAB TRIM PRESSURE SWITCH. OPS C HECK GOOD IAW 30-00-00. PN OFF 211C117-183 SN OFF V0830A. 2 L 7 2 4T RT A31SO 2002112900040 20021129 00040 EA 2002 11 29 SWIA200211462 1 20021109 A 3411 SENSOR CNDAIR CL600 CL6002B19 1900309 EA LT AOA MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 591SW 7079 ''STALL FAIL'' CAUTION MESSAGE DURING CLIMB. RETURNED TO SLC. INBOARD GROUND SPOILERS CAUTION MESSAGE AFTER LANDING. REMOVED AND REPLACED LEFT AOA. OPS CHECKS GOOD. PN OFF 4515034 SN OFF 404. 2 L 7 2 4F RT A21EA 2002112900041 20021129 00041 SO 2002 11 29 SWIA200211463 1 20021112 A 5210 SEAL EMB 120 EMB120ER 3260203 SO PAX DOOR DIRTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 393SW 120330 MAIN CABIN DOOR DOES NOT CLOSE. THE RED HANDLES DO NOT MOVE, BUT THE DOOR GOES UP AND DOWN. CLEANED AND LUBRICATED CAB IN DOOR SEAL AND LOCKING MECHANISM. OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2002112900042 20021129 00042 NE 2002 11 29 SWIA200211465 2 20021112 A 7314 311709501 PUMP EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NM 07 189SW 5934 5934 120048 DURING TAKEOFF THE RT ENGINE WOULD ONLY PRODUCE 91 PERCENT TORQUE AT FULL POWER. LT ENGINE NORMAL 100 PERCENT TORQUE. FUEL FLOW ON THE RT ENGINE 100 LBS LESS THAT OF THE LEFT ENGINE. ABORTED TAKEOFF. INSTALLED SERVICEABLE HMU AND FUEL P UMP. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002112900043 20021129 00043 EA 2002 11 29 SWIA200211466 1 20021109 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 413SW 5455 4111 7102 FLOOR EMERGENCY LIGHTING ROW 1 - 5 INOP. LOWER EMERGENCY DOOR EXIT SIGN INOP. REPLACED EMERGENCY BATTERY PACK. OPS CH ECK LIGHTS GOOD. ALL EMERGENCY LIGHTS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002112900044 20021129 00044 EA 2002 11 29 SWIA200211467 1 20021114 A 5210 ROD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 449SW 7699 MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE AFTER TAXI IN. ADJUSTED SPRING ROD IAW 52-11-15. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002112900045 20021129 00045 EA 2002 11 29 SWIA200211469 1 20021111 A 5350 FAIRING CNDAIR CL600 CL6002B19 1900309 EA FLAPS TO FUSE DAMAGED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 916SW 7634 FLAPS FAIL AT ''0'' DURING APPROACH TO LANDING. REMOVED AND REPLACED LT INBOARD FLAP TO FUSELAGE FAIRING IAW SRM 51-71 -00. 2 L 7 2 4F RT A21EA 2002112900046 20021129 00046 SO 2002 11 29 SWIA200211470 1 20021022 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 226SW 120296 RIGHT NACELLE FRAME 10 CRACKED INSIDE WHEEL WELL ON FORWARD INBOARD SIDE. INSTALLED DOUBLER TO FRAME 10 INSIDE WHEEL WE LL FORWARD INBOARD SIDE OF RIGHT NACELLE PER SRM STD. PRACTICES 51-00-00. 2 L 7 2 4T RT A31SO 2002112900047 20021129 00047 SO 2002 11 29 SWIA200211471 1 20021024 A 5320 ANGLE EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292SW 120319 FOUND CRACKED ANGLE INSIDE COCKPIT BELOW FLOOR AT FRAME 11, RT SIDE.APPLIED DOUBLER IAW SRM120 51-10-02. 2 L 7 2 4T RT A31SO 2002112900048 20021129 00048 SO 2002 11 29 SWIA200211472 1 20021024 A 5320 BRACKET EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292SW 120319 RIVET HEAD SHEARED OFF BRACKET BETWEEN CAPTAIN'S DV WINDOW AND PASSENGER DOOR, COCKPIT INTERIOR. FOUND BRACKET TO BE CR ACKED. NEW BRACKET INSTALLED IAW SRM120 51-10-02. 2 L 7 2 4T RT A31SO 2002112900049 20021129 00049 SO 2002 11 29 SWIA200211473 1 20021024 A 5712 RIB EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292SW 120319 RT INBOARD LEADING EDGE RIB IS CRACKED. CRACKED AREA STOP-DRILLED AND DOUBLER ADDED TO DAMAGED AREA IAW EMB120 SRM 51-1 0-02. 2 L 7 2 4T RT A31SO 2002112900050 20021129 00050 SO 2002 11 29 SWIA200211475 1 20021107 A 3010 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO STAB ANTI ICE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 578SW 120346 LT INBOARD STABILIZER BOOT FAILED WITH BLEED IN AUTO AND LOW. RETURNED TO SFO DUE TO WEATHER AT DESTINATION. REPLACED LEFT INBOARD STAB DEICE PRESSURE SWITCH. RAN SYSTEM FOR EIGHT MINUTES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112900051 20021129 00051 EA 2002 11 29 SWIA200211476 1 20021116 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 589SW 7072 CAPTAIN'S WINDSHIELD SHATTERED IN FLIGHT AT FL410. DIVERTED TO DFW. REMOVED CAPTAIN'S WINDSHIELD AND REPLACED IT WITH A SERVICEABLE ONE IAW CL600 MM 56-11-01. OPS CHECK GOOD. PN OFF NP-139321-9 SN OFF 94259H4058. 2 L 7 2 4F RT A21EA 2002112900052 20021129 00052 EA 2002 11 29 SWIA200211477 1 20021112 A 3260 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING ILLUMINATED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 590SW 7077 UPON DEPARTURE WHEN RETRACTING GEAR, WE RECEIVED NOSE STEERING INOP, GEAR DISAGREE, AND NOSE DOOR MESSAGES. FOLLOWED QR H, RETURNED TO SLC. INSPECTED AND SERVICED NOSE GEAR IAW CRJ MM 12-12-32. PERFORMED GEAR SWING IAW CRJ MM 32-30-00. O PS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002112900053 20021129 00053 EA 2002 11 29 SWIA200211478 1 20021116 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA SPOILERS ACTIVATED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 591SW 7079 RECEIVED INBOARD AND OUTBOARD GROUND SPOILERS FAULT MESSAGES AIRBORNE. RAN QRH AND RETURNED TO SLC. RESET CBP1 N8, 2-N 8 & 4 A2 & 3 PER FAULT ISOLATION MANUAL. SYSTEM CHECKS OK. 2 L 7 2 4F RT A21EA 2002112900054 20021129 00054 2002 11 29 SWIA200211479 4 20021108 A 2210 6229968001 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NR 1 YAW DAMPER MALFUNCTIONED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 448SW 7678 YD 1 STATUS MESSAGE COMES ON DURING TAXI. RETURNED TO GATE. REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR WITH A SERVICEABL E UNIT IAW 22-22-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002112900055 20021129 00055 SO 2002 11 29 SWIA200211480 1 20021114 A 2750 3075001007 CONTROL UNIT EMB 120 EMB120RT 3260202 SO TE FLAPS MALFUNCTIONED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 269UE 4059 2934 120194 CONTROL FAULT ON INBOARD FLAPS AFTER TRYING TO RAISE FLAPS. REMOVED AND REPLACED FLAP CONTROL UNIT. FLAPS FUNCTIONAL C HECK GOOD. 2 L 7 2 4T RT A31SO 2002112900056 20021129 00056 SO 2002 11 29 SWIA200211481 1 20021112 A 3260 WARNING LIGHT EMB 120 EMB120ER 3260203 SO MLG ILLUMINATED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 250YV 120250 A/B NOSE GEAR LIGHTS DISAGREE, COULD NOT PUT LANDING GEAR DOWN. HAD TO EXTEND LANDING GEAR USING MANUAL OVERRIDE. FOUN D NOSE GEAR A SYSTEM DOWN SENSOR HARNESS FAILS. INSPECTED NLG A & B SYSTEM HARNESS. CHECKED PROXIMITY SENSOR CLEARANCE S. FOUND NO DEFECTS. CYCLED GEAR SEVERAL TIMES. COULD NOT DUPLICATE PROBLEM ON THE GROUND. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112900057 20021129 00057 SO 2002 11 29 SWIA200211482 1 20021116 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 220SW 120288 AFT SECTION OF CABIN EMERGENCY LIGHTS ARE INOP. INSTALLED SERVICEABLE BATTERY PACK. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112900058 20021129 00058 SO 2002 11 29 SWIA200211483 1 20021116 A 2120 SMOKE EMB 120 EMB120ER 3260203 SO CABIN DETECTED A SWIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 235SW 120310 PACK BURNING ODOR AND VISIBLE SIGNS OF SMOKE IN CABIN. APPEARS TO BE COMING FROM RIGHT PACK. RAN PACKS FOR 20 MINUTES ON GROUND. ALL CHECKS NORMAL. BOTH PACKS OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112900059 20021129 00059 SO 2002 11 29 SWIA200211484 1 20021119 A 2797 WIRE EMB 120 EMB120ER 3260203 SO NR 1 TRIM SWITCH BROKEN A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 301YV 120301 WITH AUTO PILOT SELECTED TO CAPTAIN'S SIDE, RECEIVED RED ''TRIM FAIL'' ON MAP, WITH TRIPLE CHIME AND AURAL WARNING AFTER ROTATION AND DURING LANDING ROLLOUT. REPAIRED WIRING TO NR 1 TRIM SWITCH AS REQUIRED. SYSTEM OPS CHECKS GOOD IAW 22-1 0-00. 2 L 7 2 4T RT A31SO 2002112900060 20021129 00060 SO 2002 11 29 SWIA200211485 1 20021112 A 7712 SEDLOC2R INDICATOR EMB 120 EMB120ER 3260203 SO RT TORQUE MALFUNCTIONED A SWIA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 NM 07 301YV 6582 6582 120301 RIGHT TORQUE GAUGE, DIGITAL PORTION ONLY, FAILED ON TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED RIGHT TORQUE GAUGE. OPS C HECK GOOD ON ENGINE RUN. 2 L 7 2 4T RT A31SO 2002112900061 20021129 00061 SO 2002 11 29 SWIA200211486 1 20021111 A 5210 HANDLE EMB 120 EMB120ER 3260203 SO COCKPIT WINDOW OUT OF ADJUST A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 199SW 120237 CAPTAIN'S DIRECT VISION WINDOW VERY HARD TO OPEN AND THEN IMPOSSIBLE TO CLOSE. ADJUSTED CAPTAIN'S DV WINDOW HANDLE OPEN ING ROD AND DEBURRED CATCH. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112900062 20021129 00062 SO 2002 11 29 SWIA200211487 1 20021114 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO NLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 199SW 120237 AFTER ROTATION, WHEN SELECTING THE LANDING ''UP'', THE NOSE A & B SYSTEM RED AND GREEN LIGHTS REMAINED ILLUMINATED. CYCL ED THE GEAR PER THE QRH AND NO GEAR MOVEMENT NOTED. RETURNED TO LAX AND WHILE ENROUTE LIGHTS EXTINGUISHED. NORMAL LAND ING GEAR EXTENSION WAS ACCOMPLISHED.REPLACED NOSE GEAR A SYSTEM DOWN POSITION PROXIMITY SENSOR. CYCLED LANDING GEAR MUL TIPLE TIMES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002112900063 20021129 00063 2002 11 29 SWIA200211488 4 20021117 A 3417 7858062 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA RT ADC MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 410SW 7140 5117 7066 AFTER TAKEOFF WE RECEIVED RIGHT AOA HEAT, R STATIC HEAT, R PITOT HEAT AND TAT PROBE HEAT CAUTION MESSAGES. RETURNED TO SLC. REMOVED AND REPLACED THE RIGHT SIDE AIR DATA SENSOR CONTROLLER. SYSTEM OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002112900064 20021129 00064 EA 2002 11 29 SWIA200211489 1 20021118 A 2750 855D10011 SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT BPSU MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 442SW 2243 2243 7609 ''FLAP FAIL'' CAUTION MESSAGE CAME ON IN FLIGHT IN LIGHT TURBULANCE, ALONG WITH ''BTMS ICONS'' ON FLIGHT CONTROL PAGE. FLAPS INDICATED ''0'' WITH AMBER ICONS. PERFORMED QRH PROCEDURES. LANDED WITH FLAPS ''0''.REMOVED AND REPLACED LEFT AN D RIGHT BPSU IAW 27-51-10. RIGGED BPSU'S IAW MM 27-51-10. FLAP SYSTEM OPS CHECK GOOD AT THIS TIME IAW 27-54-00. (LT BP SU) PN OFF 855D100-11 SN OFF 1709. 2 L 7 2 4F RT A21EA 2002112900065 20021129 00065 SO 2002 11 29 SWIA200211490 1 20021002 A 3060 RCCB EMB 120 EMB120ER 3260203 SO RT PROPELLER MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 188SW 120039 INFLIGHT ''RIGHT INOP'' PROP DEICE LIGHT ILLUMINATED, TIMER 1 AND TIMER 2, COLD AND NORM. FAILS 1:30 IN NORM AND ;35 IN COLD. RETURNED TO THE FIELD. REMOVED AND REPLACED RCCB CB0226 IAW EMB 120 MM 24-52-05. OPS CHECK OF LEFT AND RIGHT PROPELLER DEICE GOOD. 2 L 7 2 4T RT A31SO 2002112900066 20021129 00066 SO 2002 11 29 SWIA200211491 1 20021111 A 2751 3471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 295SW 6799 6799 120322 UPON SELECTING FLAPS 15 DEGREES ON TAXI OUT, WE HAD A ''CONTROL FAULT'' AFFECTING THE OUTBOARD PAIR OF FLAPS. REPLACED FLAP ANNUNCIATOR UNIT. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002112900067 20021129 00067 SO 2002 11 29 RAIA00211334 1 20021127 A 2797 0020BN4 COMPUTER EMB 145 EMB145 3260210 SO INOPERATIVE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 809HK 3398 1336 145187 5256-PIT- STALL PROTECTION SYSTEM WARNING INDICATION.MAINTENANCE REMOVED AND REPLACED THE STALL PROTECTION COMPUTER, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002120200001 20021202 00001 EA 2002 12 2 SWIA200211492 1 20021115 A 5230 HANDLE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR UNSECURE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 594SW 7285 ON ROTATION AT TAKE OFF THE CARGO DOOR LIGHT CAME ON. WE RETURNED TO SLC. COMPLIED WITH THE HARD/OVERWEIGHT LANDING IN SPECTION IAW ST 12-407. INSPECTED CARGO DOOR HANDLE, NO DEFECTS NOTED. CARGO DOOR HANDLE WAS FOUND POPPED WHEN AIRCRAFT ARRIVED. CARGO HANDLE OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002120200002 20021202 00002 SO 2002 12 2 SWIA200211493 1 20021119 A 3260 BULB EMB 120 EMB120ER 3260203 SO MLG INDICATOR BURNED OUT A SWIA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 NM 07 295SW 120322 ON APPROACH INTO SFO, THE RT MLG SHOWED ALL LIGHTS OUT WITH GEAR DOWN. INSTALLED NEW BULBS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002120200003 20021202 00003 EA 2002 12 2 SWIA200211494 1 20021116 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA OXYGEN SERVICE UNSECURE A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 928SW 7701 UPON ROTATION, HEARD A LOUD SQUEAL FROM THE NOSE OF THE AIRCRAFT. RETURNED TO THE FIELD. FOUND THE OXYGEN SERVICE DOOR UNLATCHED. INSPECTED DOOR. NO DAMAGE NOTED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002120200004 20021202 00004 EA 2002 12 2 SWIA200211495 1 20021124 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA NR 2 TRIM MOTOR MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 427SW 4554 4554 7497 STAB TRIM CHANNEL NR 2 WHEN ENGAGED AND TRIM IS TRIED, IT DISCONNECTS. STAB TRIM CHANNEL NR 1 OK. REMOVED AND REPLACED TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-40-00, 27-42-01 & 27-42-05. OPS CHECKS GOOD. ACTUATOR PN OFF 8396-3 S N OFF 715. 2 L 7 2 4F RT A21EA 2002120200005 20021202 00005 SO 2002 12 2 SWIA200211496 1 20021121 A 2497 TERMINAL EMB 120 EMB120RT 3260202 SO NR 1 GEN WIRE BROKEN A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 269UE 120194 DURING THE TAKEOFF RUN THE NR 1 GEN OFF BUS LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED. ATTEMPTED RESET PER QRH WITH N O SUCCESS. FOUND BROKEN WIRE ON NR 1 GENERATOR. REPLACED WIRE EYELET WITH SERVICEABLE UNIT AND CONNECTED TO NR 1 GENER ATOR. RAN RT ENGINE, APPLIED LOAD TO NR 1 GENERATOR AND PARALLELED GCU TO 28.50 VDC. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002120200006 20021202 00006 SO 2002 12 2 SWIA200211497 1 20021122 A 2750 CONTROL UNIT EMB 120 EMB120RT 3260202 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 269UE 120194 FLAPS HAD RT INBOARD FLAP ASYMMETRY WHEN SET FOR LANDING AND FAILED TO RETRACT AFTER LANDING (RT AND LT INBOARD). RE-RA CKED FLAP CONTROL UNIT. PERFORMED FUNCTIONAL CHECK OF FLAP SYSTEM. CYCLED FLAPS SEVERAL TIMES. NO DISCREPANCIES NOTED . 2 L 7 2 4T RT A31SO 2002120200007 20021202 00007 SO 2002 12 2 SWIA200211499 1 20021118 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 186SW 4890 4890 120034 EMERGENCY LIGHTS INOPERATIVE, INSTALLED SERVICEABLE EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002120200008 20021202 00008 SO 2002 12 2 SWIA200211500 1 20021124 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAPS MALFUNCTIONED A SWIA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 07 199SW 6948 6948 120237 FLAP DISAGREEMENT ON NACELLE FLAPS ON RETRACTION FROM 45 DEGREES. REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-00. LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2002120200009 20021202 00009 SO 2002 12 2 SWIA200211501 1 20021118 A 2752 CONNECTOR EMB 120 EMB120ER 3260203 SO LT TE FLAP ACT CONTAMINATED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 214SW 120280 AFTER TAKEOFF, RECEIVED A FLAP DISAGREEMENT WITH 2 BARS ON OUTBOARD FLAPS, AND ALL LIGHTS ON THE 10 DEGREE LINE FLASHING . RESET AS PER QRH. RESET NOT SUCCESSFUL. RETURNED TO LAX. FOUND LT OUTBOARD FLAP ACTUATOR CONNECTOR PLUG CONTAMINAT ED WITH MOISTURE. CLEANED AND DRIED AS NEEDED. OPERATED FLAPS AND GROUND CHECKS GOOD. 2 L 7 2 4T RT A31SO 2002120200010 20021202 00010 SO 2002 12 2 SWIA200211502 1 20021122 A 7712 30005000057 SIGNAL COND UNIT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF F R J FLT CONT AFFECTED PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NM 07 214SW 120280 NR 2 PROPELLER FEATHERED WHEN TAKEOFF POWER APPLIED. TORQUE REACHED 125 PERCENT INSTANTANEOUSLY. NP 18.9 PERCENT WHEN POWER BROUGHT BACK TO IDLE. REPLACED RIGHT ENGINE TORQUE SIGNAL CONDITIONER IAW EMB MM 77-11-01. OPERATIONAL CHECKS GO OD. REPLACED NR 2 ENGINE PROP ASSEMBLY IAW EMB 120 MM 61-10-03. 2 L 7 2 4T 4 T RT A31SO E20NE 2002120200011 20021202 00011 SO 2002 12 2 SWIA200211503 1 20021120 A 5270 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PAX DOOR ILLUMINATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 563SW 120338 CLIMBING THROUGH 11,000 FT, THE FORWARD DOOR LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURE. LIGHT WOULD NOT EXTINGUISH. RETURNED TO LAX. CHECKED CABIN DOOR WARNING SYSTEM. PRESSURIZED AIRCRAFT TO 7.0 PSID. NO WARNINGS NOTED. OK FOR CONT INUED SERVICE. 2 L 7 2 4T RT A31SO 2002120200012 20021202 00012 SO 2002 12 2 SWIA200211504 1 20021124 A 3230 LANDING GEAR EMB 120 EMB120ER 3260203 SO MAINS CONTAMINATED A SWIA A UNSCHED LANDING E F J VIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 584SW 120352 ON DEPARTURE OUT OF CPR, LANDING GEAR WOULD NOT RETRACT AND HAD RT MLG DISAGREEMENT. PERFORMED QRH AND GEAR EXTENDED. RETURNED TO CPR. INSPECTED LANDING GEAR DUE TO ICE ACCUMULATION. PERFORMED GEAR SWINGS IAW MM 32-30-00. OPS CHECK GO OD. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4T RT A31SO 2002120200013 20021202 00013 EA 2002 12 2 SWIA200211505 1 20021123 A 2710 10231007 DAMPER CNDAIR CL600 CL6002B19 1900309 EA LT AILERON MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 426SW 5204 5204 7468 LT AILERON FLUTTER DAMPER MESSAGE INTERMITTENT. REPLACED LT AILERON FLUTTER DAMPER IAW 27-15-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002120200014 20021202 00014 EA 2002 12 2 SWIA200211506 1 20021124 A 3020 32144424 VALVE CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM MALFUNCTIONED A SWIA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 NM 07 426SW 5210 5210 7468 ON END OF RUNWAY, APPLIED 80 PERCENT N1 WITH A LT WING A/I CAUTION MSG THAT WOULD NOT EXTINGUISH. 10 SECONDS LATER REC EIVED A WING OVERHEAT MESSAGE FOR THE RT WING, ALSO POPPED B-4 CB ON CBP-4. REDUCED THRUST, EXITED RUNWAY, RAN QRH AND RETURNED TO GATE. REPLACED LT 14TH STAGE ANTI-ICE MODULATING VALVE PER MM 30-12-04. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002120200015 20021202 00015 SO 2002 12 2 SWIA200211507 1 20021115 A 2841 INDICATOR EMB 120 EMB120ER 3260203 SO FUEL QTY MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 196SW 120151 ENROUTE THE FIRST OFFICER NOTICED ''SOMETHING WET'' ON THE RT WING. RT FUEL GAUGE SHOWED AN IMBALANCE AND INCREASING. RETURNED TO DEN. ON SHORT FINAL THE FUEL GAUGE BECAME ERRATIC. CHECKED FUEL GAUGE WITH FUEL TANK STICKS. NO DEFECTS NOTED. OPS CHECK GOOD. NO LEAKS FOUND. 2 L 7 2 4T RT A31SO 2002120200016 20021202 00016 SO 2002 12 2 SWIA200211508 1 20021120 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 226SW 120296 EMERGENCY LIGHTS AT OVERHEAD BIN 9C INOPERATIVE. REPAIRED BROKEN WIRE BY FORWARD HINGE OF OVERHEAD BIN ASSY AT 9BC. OP S CHECK GOOD. 2 L 7 2 4T RT A31SO 2002120200017 20021202 00017 SO 2002 12 2 SWIA200211509 1 20021122 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 226SW 120296 EMERGENCY LIGHTS AT MAIN DOOR INOPERATIVE. REPAIRED WIRE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002120200018 20021202 00018 NM 2002 12 2 159PL0001A 1 20021021 A 3350 LENS BOEING 737 737242 1384477 NM EMERGENCY LIGHT LOOSE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 159PL 21186 ONE EMEERGENCY FLOOR LIGHT BULB LENS KICKED OFF AT ROW 5D. R&R BULB AND INSTALLED LENS AS REQUIRED. OPS. CHECK GOOD. 2 L 7 2 4F A16WE 2002120200019 20021202 00019 NM 2002 12 2 159PL0002A 1 20021024 A 3350 100865 POWER SUPPLY BOEING 737 737242 1384477 NM EMERGENCY LIGHT MALFUNCTIONED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 159PL 21186 FWD SECTION OF EMERGENCY FLOOR LIGHTING COMES ON INTERMITTENTLY, UNCOMMANDED. R&R FWD FLOOR LIGHTING POWER UNIT PER MM3 3-51-0, OPS GOOD. 2 L 7 2 4F A16WE 2002120200020 20021202 00020 NM 2002 12 2 219PA0001A 1 20021030 A 3242 26010425 BRAKE ASSY BOEING 737 737222 1384473 NM NR 3 DAMAGED A PIDA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 05 219PA 19956 NR 3 BRAKE DRAGGING. LOG PAGE ENTRY, (FOUND HEAT SHIELD FROM NR 3 MAIN WHEEL LODGED IN ROTOR OF BRAKE ASSY. R&R BRAKE IAW MM32-41-41 AND R&R NR 3 WHEEL IAW MM32-45-11). UPON FURTHER INVESTIGATION, FOUND BRAKE PAD SEPARATED FROM BRAKE RESU LTING IN DAMAGE TO WHEEL AND DISLOCATION OF HEAT SHIELD. 2 L 7 2 4F A16WE 2002120200022 20021202 00022 NM 2002 12 2 374PA0001A 1 20021004 A 2780 189929 SENSOR BOEING 737 73736M 138443B NM LE FLAP FAILED A PIDA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 374PA 28333 TAKEOFF WARNING HORN ACTIVATED DURING T/O ROLL, OBSERVED LE FLAPS TRANSIT LIGHT ILLUMINATED, PERFORMED RTO. FOUND NR 1 KRUGER FLAP POSITION SENSOR BAD. R&R PROXIMITY SENSOR PER MM 27-88-11, OPS CHECKED. GOOD. 2 L 7 2 4F RT A16WE 2002120200023 20021202 00023 2002 12 2 375PA0007 4 20021120 A 2230 CONTROL UNIT BOEING 737 7373Y0 1384671 NM AUTO THROTTLES MALFUNCTIONED A PIDA O OTHER O OTHER TO TAKEOFF 1 SO 05 375PA 23812 DURING TAKE-OFF, AUTO THROTTLES DISENGAGE WHEN TOGA BUTTONS ARE ENGAGED. AUTO THROTTLES CAN BE RE-ENGAGED MANUALLY. UN ABLE TO DUPLICATE. PERFORMED AUTO THROTTLE BITE TEST. NO FAULTS PER MM 22-31-00 2 L 7 2 4F RT A16WE 2002120200024 20021202 00024 2002 12 2 377PA0008 4 20021005 A 2210 CONTROL UNIT BOEING 737 7373L9 1384470 NM AUTOPILOT MALFUNCTIONED A PIDA O OTHER J WARNING INDICATION CR CRUISE 1 SO 05 377PA 23718 CHANNEL B ON AUTO PILOT INOPERATIVE. AUTO THROTTLES RETARD TO IDLE, WOULD NOT DISPLAY MACH SPEED ON MCP. PERFORMED A/P LAND VERIFY BITE CHECK THROUGH FMC. NO FAULTS INDICATED. 2 L 7 2 4F RT A16WE 2002120200027 20021202 00027 EU 2002 12 2 RAIA00210284 1 20021017 A 3350 SOCKET AEROSP ATR72 ATR72202 8680940 EU EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 721TE 217 PAX DOOR EMERGENCY LIGHT INOPERATIVE. ADJUSTED LIGHT BULB IN SOCKET. 2 H 7 2 4T RT A53EU 2002120200028 20021202 00028 EU 2002 12 2 RAIA00210285 1 20021017 A 3350 SOCKET AEROSP ATR42 ATR42300 8680920 EU EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 423TE 119 PAX DOOR EMERGENCY LIGHT INOPERATIVE. ADJUSTED LIGHT BULB IN SOCKET. 2 H 7 2 4T RT A53EU 2002120200029 20021202 00029 SO 2002 12 2 RAIA00210289 1 20021020 A 2731 CIRCUIT BREAKER EMB 145 EMB145 3260210 SO NR 1 PITCH TRIM TRIPPED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 803HK 145077 NR 1 PITCH TRIM FAILED. MAINTENANCE RESET BOTH PITCH TRIM CIRCUIT BREAKERS, OPS CHECK OK. 2 L 7 2 4F RT T00011AT 2002120200030 20021202 00030 2002 12 2 RAIA00210291 4 20021021 A 3160 WARNING LIGHT AEROSP ATR72 ATR72202 8680940 EU COCKPIT FALSE INDICATION A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 723TE 283 CREW REPORTED ELECTRICAL SMOKE INDICATION ON CAPTION PANEL. MAINTENANCE TROUBLESHOT AND COULD NOT DUPLICATE PROBLEM, ENG INE, ELECTRICAL, AND AIR CONDITION SYSTEMS ALL CHECKED GOOD. 2 H 7 2 4T RT A53EU 2002120200031 20021202 00031 EU 2002 12 2 RAIA00210292 1 20021022 A 3260 DOWNLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU NLG OUT OF ADJUST A RAIA O OTHER N FALSE WARNING LD LANDING 1 CE 03 556HK 41073 ON APPROACH FOR LANDING NLG DOWN LOCK INDICATION WAS INOPERATIVE WITH GEAR WARNING HORN SOUNDING. MAINTENANCE ADJUSTED N LG DOWN LOCK SWITCH, OPS CHECKED OK. 2 L 7 2 4T RT A41NM 2002120200032 20021202 00032 EU 2002 12 2 RAIA00210294 1 20021024 A 5270 WARNING SYSTEM JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR FALSE ACTIVATION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 554HK 41067 BAGGAGE DOOR INDICATED UNLOCKED. MAINTENANCE TROUBLESHOT AND COULD NOT DUPLICATE PROBLEM WITH DOOR CLOSED AND LOCKED IND ICATING SYSTEM OPS CK OK. 2 L 7 2 4T RT A41NM 2002120200033 20021202 00033 2002 12 2 RAIA00211295 4 20021025 A 3160 WARNING SYSTEM AEROSP ATR72 ATR72202 8680940 EU COCKPIT FALSE ACTIVATION A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 723TE 283 ELECTRIC SMOKE WARNING INDICATION DURING CLIMB. PERFORMED GROUND RUN, UNABLE TO DUPLICATE MALFUNCTION. 2 H 7 2 4T RT A53EU 2002120200034 20021202 00034 EU 2002 12 2 RAIA00211296 1 20021026 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 569HK 41088 EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. RE-SECURED EMERGENCY PATH LIGHT STRIP CONNECTOR, OPS CK OK 2 L 7 2 4T RT A41NM 2002120200035 20021202 00035 EU 2002 12 2 RAIA00211297 1 20021026 A 5230 DOOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY UNSECURE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 574HK 41093 BAGGAGE DOOR WARNING ILLUMINATED ON TAKE-OFF. MAINTENANCE RE SECURED DOOR LOCKING HANDLE. 2 L 7 2 4T RT A41NM 2002120200036 20021202 00036 EU 2002 12 2 RAIA00211301 1 20021031 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 557HK 41074 EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AFT CABIN. RE-SECURED CONNECTOR AT EMERGENCY ESCAPE PATH LIGHTING STRIP, OPS CK OK. 2 L 7 2 4T RT A41NM 2002120200037 20021202 00037 EU 2002 12 2 RAIA00211304 1 20021010 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR DIRTY A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 556HK 41073 BAGGAGE DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE DEFERRED PER MEL; SUBSEQUENTLY CLEANED DOOR SWITCHES AND OPS CK OK. 2 L 7 2 4T RT A41NM 2002120200038 20021202 00038 EU 2002 12 2 RAIA00211306 1 20021025 A 2760 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU RT SPOILER DIRTY A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 569HK 41088 RT SPOILER WARNING INDICATION. MAINTENANCE DEFERRED PER MEL; SUBSEQUENTLY CLEANED SPOILER ACTUATOR CONNECTOR PLUG, OPS C K OK. 2 L 7 2 4T RT A41NM 2002120200039 20021202 00039 WP 2002 12 2 RAIA00211307 2 20021103 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE331* 01514 WP RIGHT MALFUNCTIONED A RAIA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CE 03 554HK 41067 RT ENGINE TORQUE DROP 12 PERCENT. MAINTENANCE INSPECTED ENGINE AND PERFORMED SEVERAL GROUND RUNS AND COULD NOT DUPLICATE THE MALFUNCTION. 2 L 7 2 4T 3 T RT A41NM E2WE 2002120200040 20021202 00040 EU 2002 12 2 RAIA00211308 1 20021104 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR FALSE ACTIVATION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 574HK 41093 MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATED DURING TAKE OFF. MAINTENANCE INSPECTED THE DOOR AND OPERATED IT SEVERAL TIME S AND EACH TIME THE WARNING SYSTEM OPS CK OK. 2 L 7 2 4T RT A41NM 2002120200041 20021202 00041 EU 2002 12 2 RAIA00211310 1 20021106 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR FALSE ACTIVATION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 567HK 41085 BAGGAGE DOOR OPEN WARNING LIGHT CAME ON. MAINTENANCE CYCLED CARGO DOOR HANDLE, OPS CHECKED OK. 2 L 7 2 4T RT A41NM 2002120200042 20021202 00042 EU 2002 12 2 RAIA00211311 1 20021107 A 2750 RELIEF VALVE JETAIR JETSTM JETSTM4101 1500501 EU TE FLAPS BYPASSING A RAIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CE 03 562HK 41078 AFTER TAKEOFF FLAPS REMAINED AT 9 DEGREES WHEN FLAPS ZERO SELECTED. MAINTENANCE RESET THE PRESSURE RELIEF BYPASS PIN, OP S CK OK. 2 L 7 2 4T RT A41NM 2002120200043 20021202 00043 EU 2002 12 2 RAIA00211312 1 20021107 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR FALSE ACTIVATION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 554HK 41067 BAGGAGE DOOR WARNING CAME ON DURING TAKEOFF. MAINTENANCE OPERATIONAL INSPECTED AND CHECKED DOOR WARNING SYSTEM, NO DEFEC TS NOTED. 2 L 7 2 4T RT A41NM 2002120200044 20021202 00044 EU 2002 12 2 RAIA00211313 1 20021108 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 571HK 41090 EMERGENCY PATH LIGHTS INOPERATIVE ROWS 1 TO 3. RE-SECURED CONNECTOR TO LIGHT STRIP, OPS CK OK. 2 L 7 2 4T RT A41NM 2002120200045 20021202 00045 SO 2002 12 2 RAIA00211316 1 20021112 A 3397 CONNECTOR EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 808HK 145157 FWD ESCAPE PATH LIGHTS INOPERATIVE. RE-SECURED FORWARD FLOOR EMERGENCY LIGHTING STRIP CONNECTOR, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002120200046 20021202 00046 EU 2002 12 2 RAIA00211320 1 20021107 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR FALSE ACTIVATION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 574HK 41093 BAGGAGE DOOR WARNING LIGHT ILLUMINATED DURING TAKE-OFF. MAINTENANCE DEFERRED PER MEL 52-3C SUBSEQUENTLY INSPECTING THE D OOR LATCH AND INDICATING SYSTEMS WITH NO DEFECTS NOTED. 2 L 7 2 4T RT A41NM 2002120200047 20021202 00047 EU 2002 12 2 RAIA00211323 1 20021116 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR FALSE ACTIVATION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 551HK 41040 BAGGAGE DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE INSPECTED LATCHING AND INDICATING SYSTEMS WITH NO DEFECTS NOTED, AND SECURED DOOR. 2 L 7 2 4T RT A41NM 2002120200048 20021202 00048 EU 2002 12 2 RAIA00211324 1 20021117 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR FALSE ACTIVATION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 574HK 41093 BAGGAGE DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE INSPECTED LATCHING AND INDICATING SYSTEMS WITH NO DEFECTS NOTED, LUB RICATED MECHANISM AND SECURED DOOR. 2 L 7 2 4T RT A41NM 2002120200049 20021202 00049 EU 2002 12 2 RAIA00211325 1 20021117 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR FALSE ACTIVATION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 551HK 41040 BAGGAGE DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE INSPECTED LATCHING AND INDICATING SYSTEMS WITH NO DEFECTS NOTED, LUB RICATED MECHANISM AND SECURED DOOR. 2 L 7 2 4T RT A41NM 2002120200050 20021202 00050 SO 2002 12 2 MASA200200001 1 20020904 A 2560 SEAL EMB 145 EMB145LR 3260212 SO MEDICAL KIT BROKEN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 830MJ 145259 WRAPPER TORN OFF EMERGENCY MEDICAL KIT. KIT NOT SEALED. INVENTORIED KIT AND RESEALED PER GPM. CONTINUED OPS. 2 L 7 2 4T RT T00011AT 2002120200051 20021202 00051 NM 2002 12 2 MASA200200004 1 20020928 A 3350 6519020 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 448YV 448 DURING A LINE CHECK INSPECTION, THE FWD EMERGENCY ESCAPE PATH LIGHT WOULD NOT ILLUMINATE. THE FWD ESCAPE PATH LIGHT STRI P WAS REPLACED WITH NO FURTHER DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2002120200052 20021202 00052 EA 2002 12 2 MASA200200005 1 20020930 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 17231 7231 AIR SHUTTLE 6132 FROM MRY TO PHX HAD THE 3RD INTERIOR CEILING EMERGENCY EXIT LIGHT INOPERATIVE. THE LIGHT WAS PLACED ON MEL AND THE A/C DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2002120200053 20021202 00053 EA 2002 12 2 MASA200200006 1 20020930 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 17231 7231 AIR SHUTTLE 6131 FROM MRY TO PHX HAD THE EXTERIOR RT MIDDLE EMERGENCY EXIT LIGHT INOPERATIVE. THE LIGHT WAS PLACED ON ME L AND THE A/C DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2002120200054 20021202 00054 SO 2002 12 2 MASA200200008 1 20021002 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 830MJ 145259 AIRSHUTTLE 5731 FROM PHL TO DTW PILOT REPORTED THE CABIN CEILING EMERGENCY EXIT LIGHT INOPERATIVE. MAINT REPLACED THE LI GHT. 2 L 7 2 4T RT T00011AT 2002120200055 20021202 00055 EA 2002 12 2 MASA200200009 1 20021002 A 2710 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA AILERON TRIM FALSE ACTIVATION A MASA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 37208 7208 ABORTED TAKEOFF FOR AILERON MISS TRIM MSG. (TAKEOFF NO CONFIG) MX PERFORMED OPS CHECK OF AILERON SYSTEM. NO DEFECTS NOTE D A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002120200056 20021202 00056 EA 2002 12 2 MASA200200010 1 20021003 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7305V 7305 CAPTAINS EMERGENCY FLASHLIGHT WILL NOT CHARGE. MX R/R. FLASHLIGHT ASSY OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002120200057 20021202 00057 SO 2002 12 2 MASA200200011 1 20021003 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 837MJ 145367 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MX T/S AND FOUND CONNECTOR LOOSE. RESECURED, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2002120200058 20021202 00058 SO 2002 12 2 MASA200200013 1 20021004 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 838MJ 145384 AIR SHUTTLE 5834 FROM PHL TO CLE HAD THE NR 4 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. WHEN MX REMOVED THE COVER TO RE PLACE THE LAMP, THE LIGHT STARTED WORKING NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4T RT T00011AT 2002120200059 20021202 00059 SO 2002 12 2 MASA200200014 1 20021004 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 836MJ 145359 AIR SHUTTLE 5860, CLT TO BTR HAD A SEGMENT OF EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. MX T/S AND REPLACED THE SEGMENT BATTERY. 2 L 7 2 4T RT T00011AT 2002120200060 20021202 00060 EA 2002 12 2 MASA200200015 1 20021004 A 3260 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR FAILED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 37342 7342 AIR SHUTTLE 9342 FROM SAT TO DEN RETURNED TO FIELD DUE TO THE NLG WOULD NOT RETRACT WITH AN ASSOCIATED DISAGREE & DOOR M ESSAGES. MX ADJUSTED THE NLG PROXIMITY SWITCH AND THE SYSTEM OPERATED NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2002120200061 20021202 00061 EA 2002 12 2 MASA200200016 1 20021005 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 77286 7286 ONE CABIN CEILING EMERGENCY LIGHT INOPERATIVE. MEL'D PER 33-51-01 AND CONTINUED OPS. 2 L 7 2 4F RT A21EA 2002120200062 20021202 00062 EA 2002 12 2 MASA200200017 1 20021005 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA NR 2 OUT OF RIG A MASA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 07 77260 7260 AIR SHUTTLE 6999 PHX TO CMH RETURNED TO FIELD WHEN THE CREW RECEIVED THE NR 2 T/R UNLOCK MESSAGE. THE CREW DECLARED AN E MERGENCY. MX FOUND THE T/R OUT OF RIG AND RERIGGED. THE FLIGHT WAS SWAPPED WITH ANOTHER A/C. N77260 WAS RETURNED TO SERV ICE LATER THE SAME DAY. 2 L 7 2 4F RT A21EA 2002120200063 20021202 00063 EA 2002 12 2 MASA200200018 1 20021008 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77260 7260 FWD EMERGENCY LIGHT GO OUT FWD OF THE PASSENGER DOOR. ART WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A21EA 2002120200064 20021202 00064 EA 2002 12 2 MASA200200019 1 20021009 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77181 7181 AT ACCEPTANCE INSPECTION, THE CREW FOUND THE AFT CEILING EMERGENCY EXIT LIGHT INOPERATIVE. ITEM WAS PLACED ON MEL AND CO NTINUED OPS. PHX MX REPLACED THE BULB. OPS NORMAL. 2 L 7 2 4F RT A21EA 2002120200065 20021202 00065 EA 2002 12 2 MASA200200020 1 20021009 A 2434 GENERATOR CNDAIR CL600 CL6002B19 1900309 EA NR 2 MALFUNCTIONED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 77260 7260 ABORTED TAKEOFF AT THE START OF THE ROLL DUE TO IDG NR 2 FAULT CAUTION MSG. AIRCRAFT RETURNED TO GATE AND MX PLACED THE GEN 2 ON MEL. 2 L 7 2 4F RT A21EA 2002120200066 20021202 00066 EA 2002 12 2 MASA200200021 1 20021009 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27314 7314 DURING PREFLIGHT, AFT 3 SECTIONS OF EMERGENCY FLOOR LIGHTING FROM ROW 9 AFT WERE INOPERATIVE. MX FOUND LOOSE CONNECTOR A ND RESECURED IT IN THE HARNESS. OPS NORMAL. 2 L 7 2 4F RT A21EA 2002120200067 20021202 00067 EA 2002 12 2 MASA200200022 1 20021014 A 2752 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A MASA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 SW 07 47239 7239 AIRSHUTTLE 6412 FROM PHX TO COS DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO THE FLAPS SYSTEM FAILING AT DEGRE ES. MAINTENANCE HAD REPLACED THE LT IB FLAP ACTUATOR THE NIGHT BEFORE FOR A PREVIOUS FAILURE. MAINTENANCE IS STILL TROUB LESHOOTING. 2 L 7 2 4F RT A21EA 2002120200068 20021202 00068 SO 2002 12 2 MASA200200023 1 20021015 A 7500 DUCT EMB 145 EMB145LR 3260212 SO BLEED AIR RUPTURED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 855MJ 145614 AIRSHUTTLE 5776 FROM CLT TO LIT WHILE ON APPROACH INTO LIT CREW REPORTED WHAT THEY THOUGHT WAS SMOKE IN THE COCKPIT AND DECLARED AN EMERGENCY. AFTER AN UNEVENTFUL LANDING, MX WAS ABLE TO DETERMINE THAT A BLEED AIR DUCT HAD RUPTURED SHREDDIN G AN INSULATION BLANKET. THE CAUSE OF THE BLOWN DUCT IS STILL UNDER INVESTIGATION BUT THE "SMOKE" HAS BEEN DETERMINED TO BE INSULATION PARTICLES BLOWN ALL OVER THE A/C THROUGH THE VENTILATION SYSTEM. 2 L 7 2 4T RT T00011AT 2002120200069 20021202 00069 NM 2002 12 2 MASA200200024 1 20021016 A 3350 COVER DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT OPEN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 446YV 446 EMERGENCY LIGHT COVER AT SEAT 1C IS OPEN. SECURED COVER. OPS NORMAL. 2 H 7 2 4T RT A13NM 2002120200070 20021202 00070 EA 2002 12 2 MASA200200025 1 20021017 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 27172 7172 AIRSHUTTLE 6497 FROM PHX TO EUG DECLARED AN EMERGENCY DUE TO FLAP FAIL AT 8 DEGREES AND RETURNED TO PHX. MX COMPLIED WIT H PART A OF MTC 27-50-0001 AND RETURNED A/C TO SERVICE. 2 L 7 2 4F RT A21EA 2002120200071 20021202 00071 EA 2002 12 2 MASA200200026 1 20021017 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 77286 7286 AIRSHUTTLE 6023 HAD THE CABIN EMERGENCY FLOOD LIGHT INOPERATIVE. MX REPLACED THE BULB AND OPS CHECK THE SYSTEM OK. 2 L 7 2 4F RT A21EA 2002120200072 20021202 00072 SO 2002 12 2 MASA200200027 1 20020924 A 4920 APU EMB 145 EMB145LR 3260212 SO APU BAY FIRE A MASA O OTHER A J FLAME/FIRE WARNING INDICATION DE DESCENT 1 SW 07 851MJ 145572 UPON DESCENT INTO BTR, CAPTAIN ATTEMPTED TO START APU. EXPERIENCED 3 HUNG STARTS OF APU. AFTER THIRD START ATTEMPT, CAPT AIN EXPERIENCED AN APU FIRE WARNING MSG ON THE EICAS. A/C LANDED AT BTR WITHOUT INCIDENT. UPON INSPECTION AFTER LANDING, THERE WAS EVIDENCE OF SLIGHT CHARRING ON THE A/C SKIN AFT OF THE APU ACCESS PANEL. 2 L 7 2 4T RT T00011AT 2002120200073 20021202 00073 EA 2002 12 2 MASA200200028 1 20021021 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 27191 7191 FLT 6132 PHX TO MRY. DURING PREFLIGHT, THE CREW DISCOVERED THAT THE AFT EMERGENCY CABIN FLOOD LIGHT WAS INOPERATIVE. MX REPLACED THE BULB AND THE SYSTEM OPERATIONALLY CHECKED NORMAL. A/C CONTINUED WITHOUT INCIDENT. 2 L 7 2 4F RT A21EA 2002120200074 20021202 00074 SO 2002 12 2 MASA200200029 1 20021022 A 3350 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BROKEN A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 826MJ 145214 AFT EMERGENCY TRACK LIGHTING BROKEN. WIRES SEPARATING FROM TRACK LIGHTING. 2 L 7 2 4T RT T00011AT 2002120200075 20021202 00075 EA 2002 12 2 MASA200200030 1 20021017 A 7931 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT FAILED A MASA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 07 87353 7353 AIRSHUTTLE 6017 FROM PHX TO FAT DECLARED AN EMERGENCY WHEN CREW RECEIVED RT ENGINE OIL PRESSURE WARNING IN FLIGHT. A/C R ETURNED BACK TO PHX. MX WILL BE REPLACING THE ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200076 20021202 00076 NM 2002 12 2 2002F01029 1 20020926 A 3320 3662M641 BALLAST BOEING 727 727224 1384076 NM CABIN MALFUNCTIONED A FX7A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 19 79750 22452 DURING CLIMB, SMOKE ALARMS IN BOTH AFT LAVATORIES WENT ON, SMOKE WAS NOTICED. AFTER 20 OR 3 MINUTES IT WAS CLEAR, AFT G ALLEY POWER WAS SWITCHED OFF AS PRECAUTIONARY A/C CONTINUED TO MIAMI. ON THE GROUND, FOUND AFT CABIN CEILING LIGHTS DUA L FILTER BALLAST BURNED OUT AND ONE TERMINAL LOOSE ON BALLAST. REMOVED AND REPLACED FILTER BALLAST AND CHECKED WIRES PE R MM 33-20-32 AND 33-20-61, OPS CHECKED SYSTEM, OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002120200078 20021202 00078 EU 2002 12 2 AALA20021099 1 20020726 A 3234 A2519903E SELECTOR VALVE AIRBUS 300 A300B4605R 3930308 EU LANDING GEAR MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7055A 462 JFK - FLT 1751 - EN ROUTE JFK-SJU - AFTER TAKEOFF, PLACED LANDING GEAR HANDLE IN UP POSITION INDICATOR SHOWED 3 GREEN AN D RED UNSAFE LIGHTS. RETURNED JFK AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR SELECTOR VALVE AND LANDING GEAR H ANDLE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002120200079 20021202 00079 EU 2002 12 2 AALA20021172 1 20020815 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80058 466 TUL - FOUND CORROSION ON SEAT TRACK 'C' RIGHT BETWEEN FRAMES 31 AND 33. INSTALLED NEW SEAT TRACK ON 'C' RIGHT BETWEEN F RAMES 25 AND 34 PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2002120200080 20021202 00080 WP 2002 12 2 AALA20021303 1 20020911 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 451AA 49477 LAX - DURING OVERNIGHT MAINTENANCE, LEFT AND RIGHT AFT AUXILIARY EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED AFT AUXILIA RY EMERGENCY EXIT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002120200081 20021202 00081 WP 2002 12 2 AALA20021304 1 20020912 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAILCONE CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 573AA 53092 DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY EXIT LIGHTS ON HANDLE INOPERATIVE. REPLACED WIRE FOR EME RGENCY EXIT LIGHTS ON HANDLE IN TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002120200082 20021202 00082 WP 2002 12 2 AALA20021305 1 20020912 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 447AA 49473 DFW - DURING OVERNIGHT MAINTENANCE, LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS ABOVE EXIT DOOR AT ROW 21 INOPERATIVE. TIGHTENED WIRE FOR OVERWING EMERGENCY EXIT LIGHTS AT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002120200083 20021202 00083 WP 2002 12 2 AALA20021306 1 20020912 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAILCONE LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90511 49805 DFW - DURING OVERNIGHT MAINTENANCE, TAILCONE EMERGENCY EXIT LIGHT INOPERATIVE. TIGHTENED WIRE FOR TAILCONE EMERGENCY EX IT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002120200084 20021202 00084 WP 2002 12 2 AALA20021307 1 20020912 A 3350 P2070003001 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33502 49739 DFW - DURING OVERNIGHT MAINTENANCE, PORTABLE EMERGENCY EXIT LIGHT AT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED PORTABL E EMERGENCY EXIT LIGHT AT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002120200085 20021202 00085 WP 2002 12 2 AALA20021309 1 20020914 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 472AA 49647 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTING AT SEAT 7D INOPERATIVE. REPLACED SEAT 7D EMERGENC Y EXIT SEAT PATH LIGHTING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002120200086 20021202 00086 WP 2002 12 2 AALA20021310 1 20020913 A 3350 LIGHT DOUG DC9 DC983 3022083 WP TAILCONE INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 562AA 49344 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD TAIL CONE WALKWAY EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD TAIL C ONE WALKWAY EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2002120200087 20021202 00087 WP 2002 12 2 AALA20021311 1 20020917 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 464AA 49594 IAH - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT FORWARD GALLEY AISLE SIDEWALL INOPERATIVE. REPLA CED EMERGENCY EXIT FLOOR PATH LIGHT AT FORWARD GALLEY AISLE SIDEWALL WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002120200088 20021202 00088 EU 2002 12 2 AALA20021316 1 20020912 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 11060 470 TUL - FOUND LEFT SEAT TRACK C IS CORRODED. INSTALLED SERVICEABLE TRACK PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2002120200089 20021202 00089 WP 2002 12 2 AALA20021347 1 20020920 A 3350 BPS73 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 579AA 53156 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS AT L2 615-672 INOPERATIVE. REPLACED EMERGENCY EXIT CE ILING BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002120200090 20021202 00090 WP 2002 12 2 AALA20021348 1 20020920 A 3350 BPS73 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7506 49800 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN CEILING AT ROWS 3-7 INOPERATIVE. REPLACED EMERGENCY EXIT L IGHT BATTERY PACK IN CEILING AT ROWS 3-7. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002120200091 20021202 00091 WP 2002 12 2 AALA20021349 1 20020920 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 557AN 53087 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS AT ROW 18-21 ARE DIM. SECURED BATTERY PACK AT ROW 18- 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002120200092 20021202 00092 NM 2002 12 2 AALA20021350 1 20020924 A 2910 HYDRAULIC LINE BOEING 757 757223 1384957 NM HYD SYSTEM LOOSE A AALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 21 607AM 27058 MIA - FLT 1193 - EN ROUTE JFK-MBJ, PASSENGER REPORTED WHITE STREAK COMING OFF LEFT WING DURING CRUISE. CREW INVESTIGATE D SHUTDOWN LEFT ENGINE PER FUEL LEAK CHECK LIST. LANDED AT MIA WITHOUT INCIDENT. INSPECTED AND FOUND HYDRAULIC LINE LE AKING. TIGHTENED LEAKING LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120200093 20021202 00093 EU 2002 12 2 AALA20021352 1 20020924 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 MIA - EMERGENCY LIGHT INOPERATIVE AT SEAT 13G. RESECURED LOOSE CONNECTOR AND WIRES. SYSTEM GROUND CHECKED NORMAL OPERA TION. (M) 2 L 7 2 4F RT A35EU 2002120200094 20021202 00094 EU 2002 12 2 AALA20021385 1 20020929 A 3350 PIN AIRBUS 300 A300B4605R 3930308 EU CONNECTOR BACKED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 91050 423 MIA - EMERGENCY SEAT MOUNTED LIGHT AT 32G INOPERATIVE. RESECURED PIN THAT WAS FOUND OUT OF CONNECTOR. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002120200095 20021202 00095 NM 2002 12 2 AALA20021386 1 20020930 A 3260 WARNING LIGHT BOEING 757 757223 1384957 NM COCKPIT INOPERATIVE A AALA K NONE N FALSE WARNING AP APPROACH 1 SW 21 194AA 32388 DFW - FLT 452 - EN ROUTE SNA-DFW, ON APPROACH, AFTER LOWERING GEAR, NO GREEN LIGHT FOR LEFT MAIN GEAR. DECLARED EMERGEN CY AND LANDED AT DFW WITHOUT INCIDENT. RELAMPED AND REPLACED LIGHT ASSEMBLY FOR THE LEFT MAIN GEAR DOWN INDICATOR. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120200096 20021202 00096 NM 2002 12 2 AALA20021433 1 20021008 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 363AA 24044 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHT AT SEAT 34B INOPERATIVE. REPAIRED WIRE ON EMERGENCY ESCAPE L IGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002120200097 20021202 00097 NM 2002 12 2 AALA20021434 1 20021007 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHT ASSEMBLY AT SEAT 39C INOPERATIVE. REPLACED EMERGENCY ESCAPE LIGHT ASSEMBLY AT SEAT 39C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002120200098 20021202 00098 NE 2002 12 2 AALA20021439 2 20021008 A 7597 WIRE BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE BLEED AIR SYS BROKEN A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 354AA 24035 BOS - FLT 146 - EN ROUTE BOS-CDG, RIGHT ENGINE BLEED LIGHT CAME ON ONE HOUR AFTER TAKEOFF. WIRE AT AFT TERMINAL ON AIR SUPPLY MODULE BROKEN. RETURNED BACK TO BOS. LANDED WITHOUT INCIDENT. REPLACED WIRE, INSTALLED NEW TERMINAL. BITE ON AIR SUPPLY MODULE SHOWS NO FAULTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 2002120200099 20021202 00099 EU 2002 12 2 AALA20021441 1 20021013 A 3350 PIN AIRBUS 300 A300B4605R 3930308 EU CONNECTOR NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 JFK - EMERGENCY LIGHT AT SEAT 33B INOPERATIVE. RESEATED PIN TO SEAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002120200100 20021202 00100 EU 2002 12 2 MALA020673 1 20021126 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY MALFUNCTIONED A MALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 423XJ 340B423 CREW REPORTED LAV SMOKE LIGHT ILLUMINATED AFTER TAKEOFF ROLL OF FLIGHT 2782. ABORTED TAKEOFF. MAINTENANCE REMOVED AND R EPLACED LAV SMOKE DETECTOR PN 72-111211-000 SN/ON A5172, SN/OFF A5534. IAW SF340 MM 26-13-10-4. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002120200101 20021202 00101 NM 2002 12 2 AALA20021442 1 20021010 A 3244 TIRE BOEING 757 757223 1384957 NM LANDING GEAR SEPARATED A AALA A UNSCHED LANDING S AFFECT SYSTEMS TO TAKEOFF 1 SW 21 675AN 29425 MIA - FLT 2111 - EN ROUTE MIA-LIM, DURING TAKEOFF, NR 7 TIRE CAP SEPARATED. RETURNED TO MIA WITHOUT INCIDENT. FOUND DA MAGE TO THE RIGHT WING, TRAILING EDGE FLAP AND NR 2 ENGINE COWL. COMPLETED REPAIRS TO TRAILING EDGE FLAP, A WING PANEL, AND ENGINE COWLING. REPLACED THE NR 7 TIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120200102 20021202 00102 EA 2002 12 2 MDR02021 1 20021009 A 5320 6013501252 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 432AW 7257 DURING BRIDGING INSPECTION DISCOVERED RIGHT UPPER OBLIQUE ANGLE CRACKED IN RADIUS 1.0 INCH AT FS 621-625.3. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200103 20021202 00103 EA 2002 12 2 MDR02022 1 20021009 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 432AW 7237 7257 DURING BRIDGING INSPECTION DISCOVERED LEFT FS 718 FRAME CRACKED AT STRINGER 11L, .5 INCHES LONG. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200104 20021202 00104 EA 2002 12 2 MDR02023 1 20021009 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 432AW 7257 DURING BRIDGING INSPECTION DISCOVERED FLOOR SUPPORT ANGLE AT FS 484, LBL27, WL73.1 CRACKED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200105 20021202 00105 EA 2002 12 2 MDR02024 1 20021009 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 432AW 7237 7257 DURING BRIDGING INSPECTION DISCOVERED FLOOR SUPPORT ANGLE AT FS484, LBL34, WL73.1 CRACKED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200106 20021202 00106 EA 2002 12 2 MDR02025 1 20021009 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE NICKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 432AW 7237 7257 DURING BRIDGING INSPECTION, FOUND NICK IN SKIN BELOW CARGO DOOR, FS 605.00 WL 89.00. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200107 20021202 00107 EA 2002 12 2 MDR02026 1 20021009 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE DENTED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 432AW 7237 7257 DURING BRIDGING INSPECTION, FOUND DENT IN FUSELAGE AT FS 605.00, WL 86, .010 DEEP BY 1 INCH LONG. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200108 20021202 00108 EA 2002 12 2 MDR02027 1 20021009 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 432AW 7237 7257 DURING BRIDGING INSPECTION FOUND LEFT HAND SIDE CARGO FLOOR SUPPORT ANGLE IS CRACKED AT FS621.00. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200109 20021202 00109 EA 2002 12 2 MDR02028 1 20021009 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 432AW 7257 DURING BRIDGING INSPECTION, FOUND RIGHT HAND SIDE CARGO FLOOR SUPPORT ANGLE IS CRACKED AT FS 621.00. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200110 20021202 00110 NM 2002 12 2 QXEA0202022 1 20021129 A 2420 DH103024600CSIIB INVERTER DHAV DHC8 DHC8202 2809007 NM ZONE 100 FAILED A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 368PH 8272 342 512 PDX- ON FLIGHT 2044 MFR-SEA AIRCRAFT DIVERTED TO PDX DUE TO ALL THREE INVERTER CIRCUIT BREAKERS WITH ASSOCIATED CAUTION LIGHTS AND SMELL IN COCKPIT AND CABIN WITHOUT ANY SMOKE. RAN PRIMARY INVERTER CHECKLIST. AIRCRAFT LANDED WITHOUT INCIDEN T. REMOVED AND REPLACED PRIMARY INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002120200111 20021202 00111 EA 2002 12 2 MDR02029 1 20021009 A 5310 STRIKER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE DOOR FRAME DENTED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 434AW 5331 7322 DURING BRIDGING INSPECTION FOUND PAX DOOR SEAL STRIKER AT FS 349, WL 86 IS DENTED APPROXIMATELY .025 INCH DEEP BY .5 INC H LONG. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200112 20021202 00112 EA 2002 12 2 MDR02030 1 20021009 A 5311 6003603023 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 432AW 7237 7257 LEFT FS 718.0 FRAME IS CRACKED AT STRINGER 11L, CRACK IS .5 INCH LONG. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200113 20021202 00113 EA 2002 12 2 MDR02033 1 20021020 A 7830 22850860105 TORQUE BOX CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE THRUST REVERSER CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 576ML 7257 DURING BRIDGING INSPECTION FOUND LEFT TORQUE BOX CASCADE AT 12 O'CLOCK POSITION CRACKED ON FORWARD RIGHT SIDE .25 INCH. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200114 20021202 00114 EA 2002 12 2 MDR02034 1 20021023 A 5320 6003501252 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 580ML 6202 7289 DURING BRIDGING INSPECTION, FOUND OBLIQUE ANGLE CRACKED 1.25 INCHES BETWEEN FS621 TO 630 RBL 36.20 + 8.5 WL 97.50. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200115 20021202 00115 EA 2002 12 2 MDR02039 1 20021108 A 5320 6013501251 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 575ML 7059 7256 DURING BRIDGING INSPECTION DISCOVERED LEFT OBLIQUE ANGLE CRACKED IN RADIUS 1.2500 INCHES AT FS 621-630. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200116 20021202 00116 EA 2002 12 2 MDR02040 1 20021108 A 5320 6013501252 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 575ML 7059 7256 DURING BRIDGING INSPECTION DISCOVERED RIGHT OBLIQUE ANGLE CRACKED IN RADIUS 1.2500 AT FS 621-630. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200117 20021202 00117 EA 2002 12 2 MDR02041 1 20021108 A 5320 6003603031 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 575ML 7059 7256 DURING BRIDGING INSPECTION DISCOVERED LEFT DOUBLER CRACKED IN RADIUS 3 INCHES AT FS 718 BETWEEN STRINGERS 10 AND 12. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200118 20021202 00118 EA 2002 12 2 SWIA200211512 1 20021105 A 5315 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NA FS 621, LEFT CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 427SW 7497 FS 621 LEFT FLOOR SUPPORT ANGLE CRACKED. FOUND DURING C CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 R EV. ''A''. ANGLE P/N: 601R53-61-117-1. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200119 20021202 00119 EA 2002 12 2 SWIA200211515 1 20021014 A 5345 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 411SW 7067 #2 PRESSURE AND RETURN MANIFOLD CHANNEL CRACKED THROUGH BOLT HOLE. FOUND DURING C CHECK INSPECTION. FITTED AND INSTAL LED NEW CHANNEL IAW SRM 51-40-11, 51-42-06. RE-INSTALLED HYDRAULIC COMPONENTS IAW CRJ MM CH. 49-11-05. P/N: 600-75221- 130 2 L 7 2 4F RT A21EA 2002120200120 20021202 00120 EA 2002 12 2 SWIA200211516 1 20021014 A 5315 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 640, STR 9S CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 411SW 7067 FRAME AT FS 640 IS CRACKED AT STR 9S. FOUND DURING C CHECK INSPECTION. FRAMED REPAIRED IAW CRJ REO 601R-53-61-532. HF EC INSPECTION CARRIED OUT ON CUTOUT REPAIR EDGE AS REQUIRED IAW REO 601R-53-61-532/RJ NDTM 51-20-06. NO CRACKS FOUND. 2 L 7 2 4F RT A21EA 2002120200121 20021202 00121 EA 2002 12 2 MDR02042 1 20021109 A 7830 22850809801 TRACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT ENGINE CHAFED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 575ML 7059 7256 DURING BRIDGING INSPECTION DISCOVERED LEFT ENGINE TORQUE BOX MAIN TRACK AT 4 O'CLOCK POSITION AFT END FITTING CHAFED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200122 20021202 00122 EA 2002 12 2 MDR02043 1 20021109 A 7830 22850809801 TRACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT ENGINE CHAFED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 575ML 7059 7256 DURING BRIDGING INSPECTION DISCOVERED LEFT ENGINE TORQUE BOX MAIN BOX MAIN TRACK AT 6 O'CLOCK POSITION AFT END FITTING C HAFED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200123 20021202 00123 EA 2002 12 2 MDR02044 1 20021109 A 7110 22850080S PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT COWLING CHAFED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 575ML 7256 DURING BRIDGING INSPECTION DISCOVERED LEFT ENGINE COWL PANEL 432 AT TRAILING EDGE CHAFED 1 INCH BY .5 INCH BY .003 INCH DEEP. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200124 20021202 00124 EA 2002 12 2 MDR02045 1 20021111 A 5320 60035031563 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 575ML 7059 7256 DURING BRIDIGING INSPECTION FOUND FS 621 FLOOR SUPPORT ANGLE LEFT SIDE CRACKED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200125 20021202 00125 EA 2002 12 2 MDR02046 1 20021111 A 5320 60035031563 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 575ML 7059 7256 DURING BRIDGING INSPECTION FOUND FS 621 FLOOR SUPPORT ANGLE RIGHT SIDE CRACKED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200126 20021202 00126 EA 2002 12 2 WVE2002F00019 1 20021025 A 5320 60035031563 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 580ML 6202 7289 FS 621, LEFT SIDE THE FLOOR SUPPORT ANGLE IS CRACKING. MFG REO HAS BEEN ISSUED FOR REPAIRS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200127 20021202 00127 EA 2002 12 2 WVE2002F00020 1 20021026 A 5311 6003603023 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 580ML 7289 FS 718 FRAME LOCATED ON THE LEFT SIDE OF THE FUSELAGE IS CRACKING IN THE FRAME FLANGE RADIUS. CRACKS ARE BETWEEN STRING ER 10-12. MANUFACTURE HAS ISSUED REO. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200128 20021202 00128 EA 2002 12 2 WVE2002F00021 1 20021025 A 5320 60035031563 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 580ML 6202 7289 FS 621 RIGHT SIDE THE FLOOR SUPPORT ANGLE IS CRACKING. MANUFACTURER TO REVIEW THIS PROBLEM AND DEVELOP A PERMANENT FIX. REO HAS BEEN ISSUED FOR REPAIRS. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200129 20021202 00129 CE 2002 12 2 WVE2002F00022 1 20021015 A 3213 6041105003 BEARING LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE RT & LT MLG CORRODED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 225FX 127 DURING 3000 LANDING INSPECTION THE LOWER BEARING OF THE LEFT AND RIGHT MAIN LANDING GEAR STRUT ASSEMBLIES WERE FOUND COR RODED. 2 L 7 2 4F 4 F RT A10CE E35NE 2002120200130 20021202 00130 EA 2002 12 2 WVE2002F00023 1 20021101 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT & RT WING CORRODED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 580ML 6202 7289 MINOR SURFACE CORROSION ON THE LEFT AND RIGHT HAND WINGS FOUND ON THE FUEL TANK ACCESS CUTOUTS. WING SKINS AFFECTED ARE : WING FORWARD LOWER SKIN, WING CENTER LOWER SKIN. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120200179 20021202 00179 NM 2002 12 2 2002F01031 1 20020913 A 5512 SKIN BOEING 727 727222 1384073 NM HORIZ STAB DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7644U 20038 AT C-CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN HAD 1 DENT WITH CREASE AND 1 DENT WITH CHERRY MAX RIVET IN CENTE R OF DENT AT STABILIZER STATION 4 AND APPROXIMATELY 10 INCHES FORWARD AT STATION 14 IS 2 CREASES WITH A DENT AT DRAIN HO LE. (M) 2 L 7 3 4F A3WE 2002120200180 20021202 00180 NM 2002 12 2 2002F01032 1 20020913 A 5343 651628912 ATTACH FITTING BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7644U 20038 AT C-CHECK, FOUND RIGHT LANDING GEAR SUPPORT BEAM OUTBOARD ATTACH FITTING CRACKED. (M) 2 L 7 3 4F A3WE 2002120200183 20021202 00183 EU 2002 12 2 CA021108019 1 20021018 A 5270 848401 SENSOR AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211TRENT77 NE AFT CARGO DOOR FAILED W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA (CAN) ECAM MESSAGE; CARGO AFT DOOR AMBER ON DOOR/OXY PAGE WITH NO V/S CHANGE DURING FLIGHT. MAINTENANCE INSPECTION OF A FT CARGO DOOR WAS CARRIED OUT. BITE TEST WAS CARRIED OUT ON PSCU. PSCU PROX SENSORS 26MJ OR28MJ AT FAULT. MEL 52-71-01BR AISED. ADPM 527100040810 WAS RAISED OUT ON SENSOR 26MJ. FINAL OPERATIONAL CHECK FAILED. ADPM WAS CARRIED ON SENSOR 28MJ. FINAL OPERATIONAL CHECK WAS SATISFACTORY. SENSOR 28MJ FAULTY. MAINTENANCE CHOOSE SENSOR 26MJ FIRST DUE TO RECURRENT DEF ECT 22792 AND FINDING ON PFR (POST FLIGHT REPORT) 2 L 7 2 4F 4 F RT A46NM E39NE 2002120200187 20021202 00187 NM 2002 12 2 2002F01033 1 20020911 A 5320 FITTING BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7644U 20038 AT C-CHECK, FOUND CRACK IN TIE FITTING, INTERIOR STRUCTURE OF FUSELAGE, UPPER LOBE, FS 950 STRINGER 4R. (M) 2 L 7 3 4F A3WE 2002120200188 20021202 00188 NM 2002 12 2 2002F01034 1 20020911 A 5320 FITTING BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7644U 20038 AT C-CHECK, FOUND CRACKS IN TIE FITTING, INTERIOR STRUCTURE OF FUSELAGE, UPPER LOBE, FS 950E STRINGER 4R. (M) 2 L 7 3 4F A3WE 2002120200189 20021202 00189 NM 2002 12 2 2002F01035 1 20020911 A 5320 FITTING BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7644U 20038 AT C-CHECK, FOUND CRACK IN TIE FITTING, INTERIOR STRUCTURE OF FUSELAGE, UPPER LOBE, FS 950E, STRINGER 4L. (M) 2 L 7 3 4F A3WE 2002120200190 20021202 00190 NM 2002 12 2 2002F01036 1 20020911 A 5320 FITTING BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7644U 20038 AT C-CHECK, FOUND CRACK IN TIE FITTING, INTERIOR STRUCTURE OF FUSELAGE, UPPER LOBE, FS 950F STRINGER 4R. (M) 2 L 7 3 4F A3WE 2002120200191 20021202 00191 NM 2002 12 2 2002F01037 1 20020911 A 5320 FITTING BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7644U 20038 AT C-CHECK, FOUND CRACK IN TIE FITTING, INTERIOR STRUCTURE OF FUSELAGE, UPPER LOBE, FS 1070 STRINGER 4L. (M) 2 L 7 3 4F A3WE 2002120200192 20021202 00192 NM 2002 12 2 2002F01038 1 20020911 A 5320 FITTING BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7644U 20038 AT C-CHECK, FOUND CRACKS IN TIE FITTING, INTERIOR STRUCTURE OF FUSELAGE, UPPER LOBE, FS 1050 STRINGER 4L. (M) 2 L 7 3 4F A3WE 2002120200193 20021202 00193 NM 2002 12 2 2002F01039 1 20020911 A 5320 FITTING BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7644U 20038 AT C-CHECK, FOUND CRACK IN TIE FITTING, INTERIOR STRUCTURE OF FUSELAGE, UPPER LOBE, FS 950F STRINGER 4L. (M) 2 L 7 3 4F A3WE 2002120200194 20021202 00194 NM 2002 12 2 2002F01040 1 20020914 A 5320 DOUBLER BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7644U 20038 AT C-CHECK, FOUND PREVIOUS REPAIR WITH SEVERAL CRACKS AT MAIN CARGO, STATION 400-420 BL 0.0. (M) 2 L 7 3 4F A3WE 2002120200195 20021202 00195 NM 2002 12 2 2002F01041 1 20020914 A 5310 65453132 SHEAR TIE BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7644U 20038 AT C-CHECK, FOUND CABIN SHEAR TIE CLIP CRACKED AT BS 970 STRINGER 4R. (M) 2 L 7 3 4F A3WE 2002120200196 20021202 00196 NM 2002 12 2 2002F01042 1 20020914 A 5320 654531313 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7644U 20038 AT C-CHECK, FOUND FUSELAGE UPPER LOBE STRINGER SHEAR CLIP, BS 950B STRINGER 9L, CRACKED. (M) 2 L 7 3 4F A3WE 2002120200197 20021202 00197 NM 2002 12 2 DHL2002727014 1 20021127 A 2611 BULB BOEING 727 727228 1384083 NM A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 727DH 20204 1) MAIN CARGO COMPARTMENT LH SIDE #5 SMOKE DETECTOR TEST LIGHT FAILED TO ILLUMINATE DURING TEST. 2) REPLACED SMOKE DET ECTOR BULB AT #5 LH IN MAIN CARGO COMPARTMENT. OPS CHECK WAS GOOD. 2 L 7 3 4F RT A3WE 2002120200198 20021202 00198 NM 2002 12 2 AALA20021443 1 20021011 A 2120 SMOKE BOEING 757 757223 1384957 NM COCKPIT DETECTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 670AA 25335 DFW - FLT 1870 - EN ROUTE DFW-ATL, AT TAKEOFF, ELECTRICAL SMOKE IN THE COCKPIT AND MID CABIN LIGHT SMELL. RETURNED AND LANDED AT DFW WITHOUT INCIDENT. PERFORMED CHECK OF EQUIPMENT IN FLIGHT DECK, E/E COMPARTMENT, MAIN CABIN AND RECIRCULAT ION FANS. SYSTEMS GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120200199 20021202 00199 NE 2002 12 2 AALA20021444 2 20021012 A 7261 O-RING BOEING 757 757223 1384957 NM RROYCE RB211 RB211535* NE RT ENGINE CUT A AALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 21 635AA 24593 JFK - FLT 837 - EN ROUTE LGA-MCO, AFTER TAKEOFF, CLIMBING THROUGH 8,000 FEET, RIGHT ENGINE OIL PRESSURE DROPPED INTO YEL LOW BAND. OIL PRESSURE FLUCTUATED AND THEN STEADILY DECREASED. DECLARED EMERGENCY AND LANDED AT JFK WITHOUT INCIDENT. INSPECTED AND FOUND RIGHT ENGINE PRESSURE OIL FILTER LEAKING. REMOVED PRESSURE OIL FILTER HOUSING AND FOUND OIL RING C UT. REPLACED O-RING AND INSPECTED PRESSURE OIL FILTER ELEMENT. SERVICED ENGINE. SYSTEMS GROUND CHECKED NORMAL OPERATI ON. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2002120200200 20021202 00200 NM 2002 12 2 DHL2002752005 1 20021129 A 3350 BATTERY BOEING 727 727223 1384074 NM A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 752DH 22466 1) EXIT LIGHT OVER FORWARD ENTRY DOOR INOPERATIVE.2) REMOVED AND REPLACED BATTERIES PER 727 M/M 33-50-101. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2002120200201 20021202 00201 NM 2002 12 2 AALA20021472 1 20021013 A 3350 TERMINAL BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 358AA 24039 DFW - DURING OVERNIGHT MAINTENANCE, LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT AT L389 INOPERATIVE. REPLACED TERMINAL E ND AT EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002120200202 20021202 00202 EU 2002 12 2 AALA20021478 1 20021018 A 8011 35056482 STARTER FOKKER F28 F28MK0100 4990807 EU NR 2 ENGINE MALFUNCTIONED A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 1402K 11353 ORD - FLT 1641 - EN ROUTE ORD-SAT, SMELLED SMOKE THROUGHOUT AIRPLANE ON TAKEOFF ROLL, CREW THOUGHT IT WAS FROM AIRPLANE CLOSE TO THEM THAT WAS IN FRONT. FUMES GOT STRONGER AND RMDFU ALERTED 'SMOKE AFT RIGHT TOILET'. RETURNED ORD AND LANDE D WITHOUT INCIDENT. REPLACED NR 2 ENGINE STARTER PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. NO ODOR OR SMOKE IN CABIN. (M) 2 L 7 2 4F RT 2002120200203 20021202 00203 EU 2002 12 2 AALA20021479 1 20021004 A 3350 PIN FOKKER F28 F28MK0100 4990807 EU CONNECTOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1425A 11408 DFW - DURING OVERNIGHT MAINTENANCE, SERVICE DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPINNED NR 3 WIRE ON SERVICE DOOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002120200204 20021202 00204 EU 2002 12 2 AALA20021486 1 20021015 A 2910 O-RING FOKKER F28 F28MK0100 4990807 EU HYD SYSTEM TORN A AALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 21 1436A 11426 CVG - FLT 1712 - EN ROUTE DFW-CVG, LEFT HYDRAULIC SYSTEM QUANTITY ALERT. MANUALLY LOWERED GEARS AND FLAPS. LANDED CVG WITHOUT INCIDENT. REPLACED NR 1 HYDRAULIC SYSTEM O-RING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002120200205 20021202 00205 EU 2002 12 2 AALA20021487 1 20021010 A 5280 D13312404 DOOR FOKKER F28 F28MK0100 4990807 EU RT MLG DEFECTIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 1433B 11418 JAX - FLT 2097 - EN ROUTE JAX-DFW - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. RETURNED JAX AND LANDED WITHOUT INCID ENT. REPLACED RIGHT MAIN GEAR DOOR ASSEMBLY AND CHECKED FIT. ADJUSTED HYDRAULIC ACTUATORS AND INSTALLED AND ADJUSTED U PLOCK BRACKET. REPLACED AND ADJUSTED SEQUENCE VALVE LINKAGE ACCOMPLISHED GEAR SWING PER MM. SYSTEM GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 2 4F RT 2002120200206 20021202 00206 NM 2002 12 2 AALA20021488 1 20021018 A 3234 PIN BOEING 757 757223 1384957 NM CONTROL MODULE BACKED OUT A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 669AA 25334 TUL - FLT 1215 - EN ROUTE TUL-DFW, AFTER TAKEOFF, GEAR HANDLE WOULD NOT RAISE ABOVE CENTER OFF POSITION. ON APPROACH TO TUL, WITH GEAR HANDLE DOWN AND GEAR ALL INDICATING DOWN, RECEIVED GEAR PROXIMITY WARNING. RETURNED TUL AND LANDED WITH OUT INCIDENT. TROUBLESHOT AND FOUND PIN PUSHED BACK AT CONNECTOR OF LANDING GEAR LEVER MODULE. SYSTEM GROUND CHECKED N ORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120200207 20021202 00207 NM 2002 12 2 AALA20021500 1 20021020 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 359AA 24040 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 2H BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT S EAT 2H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002120200208 20021202 00208 NM 2002 12 2 AALA20021501 1 20021020 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 384AA 26996 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35H INOPERATIVE. RESEATED CONNECTOR AT SEAT 35H. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002120200209 20021202 00209 NM 2002 12 2 AALA20021502 1 20021019 A 3350 SIGN BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 332AA 22331 LAX - DURING OVERNIGHT MAINTENANCE, FLOOR PROXIMITY BIDIRECTIONAL EMERGENCY EXIT SIGN ON FORWARD GALLEY INOPERATIVE. RE PLACED BIDIRECTIONAL EMERGENCY EXIT FORWARD GALLEY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002120200210 20021202 00210 NM 2002 12 2 AALA20021503 1 20021018 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 LHR - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHTING IN FIRST CLASS GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PROXIMITY LIGHTING ASSEMBLY AT CORNER OF FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002120200211 20021202 00211 NM 2002 12 2 AALA20021504 1 20021020 A 3350 FUSE BOEING 777 777223 1385213 NM BATTERY PACK BLOWN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - LEFT FORWARD AISLE CEILING EMERGENCY EXIT SIGN AND ALL G3 GALLEY FLOOR PROXIMITY WALL MOUNTED EMERGENCY EXIT LIGHT S INOPERATIVE. REPLACED THE FORWARD FUSE ON BATTERY PACK AT L1 DOOR CEILING PANEL. SYSTEM GROUND CHECKED NORMAL OPERAT ION. (M) 2 L 7 2 4F RT T00001SE 2002120200212 20021202 00212 NM 2002 12 2 UPS02239937 1 20021118 A 5310 FITTING BOEING 727 72751C 1384015 NM BS 910 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:C SUSPECT CRACK ON RH BS 910 FITTING REPAIR CARRIED OUT IAW EO B727-5310-1896-B APPENDIX B 2 L 7 3 4F A3WE 2002120200213 20021202 00213 NM 2002 12 2 UPS02239940 1 20021118 A 5310 65C2719423 FITTING BOEING 727 72751C 1384015 NM BS910 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:C SUSPECT CRACK ON L/H BS 910 FITTING REPAIR CARRIED OUT IAW EO B727-5310-1896-B APPENDIX B 2 L 7 3 4F A3WE 2002120200214 20021202 00214 NM 2002 12 2 UPS02239942 1 20021115 A 5310 INTERCOSTAL BOEING 727 72751C 1384015 NM VERT BEAM 17.8 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:C HORIZONTAL INTERCOSTAL CRACKED ON VERTICAL BEAM 17.8 L/H AT WL 283 1 183 BULKHEAD NEW INTERCOSTAL FABRICATED & INSTALLED PER BOEING DRAWING 65-16350 S HEET 6 & 65C15764 SH. 5 & SRM 51-30-2 2 L 7 3 4F A3WE 2002120200215 20021202 00215 NM 2002 12 2 UPS02239943 1 20021125 A 5310 NPN PRESSURE PANEL BOEING 727 72751C 1384015 NM NOSE WHEEL WELL CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:C SEVERAL CRACKS ON NLG WHEEL WELL PRESSURE WEB RHS FROM BS 260 DOWN 1 1" FROM CEILING AND 1" FWD OF THE AFT PRESSURE PANEL TP BS 279 6" BE LOW AFT PRESSURE PANEL DAMAGED AREAS REPAIRED IAW SRM51-40-2 FIG 1 2 L 7 3 4F A3WE 2002120200216 20021202 00216 NM 2002 12 2 UPS02239944 1 20021119 A 5310 NPN PRESSURE PANEL BOEING 727 72751C 1384015 NM NOSE WHEEL WELL. CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:C CRACK ON NLG WHEEL WELL PRESSURE WEB @ BS 243.6 LHS 4" AFT FROM FWD PRESSURE PANEL. DAMAGED AREA C UT OUT IAW SRM 51-40-02 FIG1, HFEC AROUND CUTOUT NDF, REPAIR CARRIED OUT IAW SRM 51-40-02 FIG 1 2 L 7 3 4F A3WE 2002120200217 20021202 00217 2002 12 2 375PA0008 4 20021125 A 2230 106201730 COMPUTER BOEING 737 737317 138447P NM A PIDA K NONE O OTHER TO TAKEOFF 1 SO 05 375PA 23812 Auto throttles disengage during take-off when TOGA is engaged. All other TOGA indications are normal. This is an inter mittent condition. R&R #2 N1 speed sensor per MM 77-12-01. R&R A/T computer & performed BITE test per MM 22-04-10. Op s checked good. 2 L 7 2 4F RT A16WE 2002120200218 20021202 00218 SO 2002 12 2 C2XA02CL235 1 20021130 A 3260 14521586403 WIRE HARNESS EMB 135 EMB135LR 3260305 SO LEFT FAULTY A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 15527 145413 CLE FLIGHT#3141 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE DURING FLIGHT ASSOCIATED WITH "THUMP" NOISE UND ER NOSE.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR WOW PROXIMITY SWITC H WIRE HARNESS W510.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002120200219 20021202 00219 EA 2002 12 2 02331647 1 20021127 A 3350 BM10006002 LIGHT CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 647BR 7399 During preflight inspection, the crew reported that the r/h aft exterior emergency exit light was inoperative. Maintena nce personnel removed and replaced the r/h aft exterior emergency exit light assy. An operational check was satisfactor y and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002120200220 20021202 00220 SO 2002 12 2 C2XA02CL236 1 20021129 A 3231 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NOSE GEAR FAULTY A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 11536 145520 CLE FLIGHT#3915 THE CREW REPORTED A LOUD ROARING NOISE FROM AREA BELOW COCKPIT FLOOR IN FLIGHT.MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS WOULD NOT RETRACT.THE NOSE GEAR DOOR SEQUENCE PROXIMITY SWITCH WAS REPLACED.OPERATIONAL CHECK S WERE GOOD. 2 L 7 2 4T RT T00011AT 2002120200221 20021202 00221 WP 2002 12 2 ZW0A0212002 1 20021127 A 3350 7732 LAMP DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9405T 53141 THE FLOOR EGRESS LIGHT AT ROW 3, AND THE EMERGENCY CEILING LIGHTS AT ROW 11 RH SIDE, WERE INOPERATIVE. RESEATED THE EGR ESS LAMP AT ROW 3, AND REPLACED THE CEILING LAMP AT ROW 11. CHECK-C 10-19-02 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2002120200222 20021202 00222 2002 12 2 920WA0008 4 20021124 A 2210 4038890948 PANEL BOEING 737 737236 1384476 NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 920WA 21791 At 12000 feet, autopilot on, in heading select mode, displayed heading changed on its own several times. R&R mode contr ol panel IAW MM 22-11-341. Ops checked normal. 2 L 7 2 4F RT A16WE 2002120200223 20021202 00223 WP 2002 12 2 MWEA020722 1 20021126 A 5330 SKIN DOUG DC9 DC932 3022066 WP STATION 1121 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 SKIN AT STATION 1121 LONGERON LEFT 18 HAS A APPROXIMATE 1.5" HOLE. -- REMOVED AND REPLACED SKIN. 2 L 7 2 4F A6WE 2002120200224 20021202 00224 EA 2002 12 2 COMA0260668 1 20021122 A 2760 SPOILER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 01 973CA 7146 FLIGHT 5754 CONFIG SPOILERS CAUTION DURING T/O.COULD NOT DUPLICATE. RESET SYS, NO FAUTLS NOTED. 2 L 7 2 4F RT A21EA 2002120200225 20021202 00225 EA 2002 12 2 COMA0260669 1 20021127 A 2130 1037708 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA A UNSCHED LANDING O S OTHER AFFECT SYSTEMS CL CLIMB 1 SO 01 810CA 6455 7370 FLIGHT 5364 CABIN ALTITUDE CAUTION MESSAGE - PRESSURIZATON SYSTEM IS INOP.REPLACED THE PRIMARY OUTFLOW VALVE. 2 L 7 2 4F RT A21EA 2002120200226 20021202 00226 EA 2002 12 2 COMA0260670 1 20021126 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 710CA 7241 FLIGHT 5371 FLAPS FAILED AT 0 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002120200227 20021202 00227 EA 2002 12 2 COMA0260671 1 20021128 A 2760 SPOILER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J F WARNING INDICATION FLT CONT AFFECTED TO TAKEOFF 1 SO 01 716CA 7250 FLIGHT 5867 CONFIG SPOILERS CAUTION DURING T/O.COULD NOT DUPLICATE - NO FAULT CODES IN COMPUTER. 2 L 7 2 4F RT A21EA 2002120200228 20021202 00228 EA 2002 12 2 COMA0260672 1 20021126 A 5270 864202 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR MALFUNCTIONED A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 952CA 7092 FLIGHT 5863 CABIN DOOR WARNING.REPLACED PROXIMITY SWITCH 546. 2 L 7 2 4F RT A21EA 2002120200229 20021202 00229 EA 2002 12 2 COMA0260673 1 20021127 A 2750 7805013 SELECTOR SWITCH CNDAIR CL600 CL6002B19 1900309 EA INST PANEL MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 978CA 9936 7158 FLIGHT 5895 FLAPS FAILED AT 20 DEGREES.REPLACED FLAP CONTROL LEVER. 2 L 7 2 4F RT A21EA 2002120200230 20021202 00230 EA 2002 12 2 COMA0260674 1 20021127 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 959CA 7116 FLIGHT 6034 FLAPS FAIL CAUTION MESSAGE.RESET SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002120200231 20021202 00231 EA 2002 12 2 COMA0260675 1 20021126 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 962CA 7123 FLIGHT 5513 R/H THRUST REVERSER CAUTION MESSAGE.DEFERRED MAINTENANCE PER MEL. 2 L 7 2 4F RT A21EA 2002120200232 20021202 00232 EA 2002 12 2 COMA0260676 1 20021127 A 3030 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 977CA 7157 FLIGHT 5234 WING OVERHEAT WARNING MESSAGE DURING T/O.COULD NOT DUPLICATE OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A21EA 2002121800044 20021218 00044 SO 2002 12 18 C2XA02BT077 1 20021120 A 3220 LANDING GEAR EMB 145 EMB145LR 3260212 SO NOSE COLLAPSED A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 27 14573 145638 NLG COLLAPSED AFTER PUSH BACK. R & R OLEO STRUT, MAIN DRAG LEG AND LOCKING STRUT, 2NDARY DRAG LEG & LOCKING STRUT, DWN TENSION SPRINGS, DWN-UNLCK ACTUATOR, ACTUATING CYLINDER. R & R MLG CONTROL LEVER , LGEU, MLG SOLENOID VALVE & CHECK VAL VE. DFDR & CMC DWNLOADED, REMOVED TOW BAR & INSPECTED, NLG BAY & OLD NLG ASSY INSPECTED. NO DEFECTS NOTED BEFORE REMOVA L. INSPECT NLG DOORS & ATTACH FITT, NO DEFECTS NOTED. DREW SAMPLES FROM NR 1 HYD SYS. MANUFACTURE REQUEST A SIM PUSHBACK & TAXI, OPS CHECKED OK, & MANUFACTURE REQUESTED CHECK OF WIRING OF MLG EXTEND/RETRACT SYS IAW WIRING MANUAL. A/C FERRIE D TO IAH TO COMPLY WITH REQUEST. IAH MAINT REPORTED NO DEFECTS OR FAULTS. AIRCRAFT RETURNED TO SERVICE. SDR OPEN. 2 L 7 2 4T RT T00011AT 2002120200233 20021202 00233 NM 2002 12 2 ASAA0210253 1 20021020 A 3350 86210144 BATTERY PACK BOEING 737 737290C 138448V NM PWA JT8 JT8D17 52049 NE CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 730AS 22577 DURING PREFLIGHT CHECK FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE ON PALLET 8-9. REMOVED AND REPLACED THE BATTERY P ACK. THE TRACK LIGHTS THEN OPERATED NORMALLY. 2 L 7 2 4F 4 F A16WE E2EA 2002120200234 20021202 00234 NM 2002 12 2 ASAA0210254 1 20021022 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 746AS 23123 DURING PREFLIGHT CHECK, FOUND FOUR EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 18. REMOVED AND REPLACED REMOTE RECE IVER BATTERY. LIGHTS THEN OPERATED PROPERLY. 2 L 7 2 4F 4 F RT A16WE E2EA 2002120200235 20021202 00235 NM 2002 12 2 ASAA024164 1 20021019 A 3350 8100022607 LIGHT BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 774AS 25107 EMERGENCY FLOOR LIGHTS ARE INOPERATIVE AT ROWS 17-19. RECONNECTED TRACK LIGHTS. TRACK LIGHTS THEN OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2002120200236 20021202 00236 NM 2002 12 2 ASAA024165 1 20021022 A 3350 8100022607 LIGHT BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 754AS 25095 EMERGENCY FLOOR LIGHTS ARE INOPERATIVE NEAR AFT LAVATORY AREA. RECONNECTED TRACK LIGHTS. TRACK LIGHTS THEN OPERATED NO RMALLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2002120200237 20021202 00237 2002 12 2 ASAA0280404 4 20021023 A 2565 D29982107 HARNESS DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE SERVICE DOOR FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 969AS 37212 1536 53063 DURING C CHECK, FORWARD SERVICE DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLIDE. SYSTEM CHE CKED, OK. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120200238 20021202 00238 WP 2002 12 2 ASAA0280461 1 20021026 A 5320 9957906503 WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 WEB CORRODED IN AFT CARGO BAY AT FUSELAGE STATION 1183-1212. REPLACED WEB SECTION IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120200239 20021202 00239 WP 2002 12 2 ASAA0280519 1 20021104 A 3320 0398010 BALLAST DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE CABIN FAILED A ASAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 02 944AS 53019 ELECTRICAL SMELL NOTED AT ROW 17. DIVERTED, FOUND ALL FOUR BALLAST SUPPORT GROMMETS FRIED. FERRIED TO SEA. REPLACED D EFECTIVE BALLAST. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120200240 20021202 00240 WP 2002 12 2 ASAA0280522 1 20021105 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 948AS 39705 53021 DURING PREFLIGHT CHECK FOUND FIRST TWO EMERGENCY TRACK LIGHTS INOPERATIVE. RECONNECTED MODULE. LIGHTS THEN OPERATED PR OPERLY. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120200241 20021202 00241 WP 2002 12 2 ASAA0280523 1 20021107 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 931AS 37505 2932 49232 DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY (INCLUDING BATTERY PACK). LIGHT THEN OPERATED NORMALLY. 2 L 7 2 4F 4 F A6WE E2EA 2002120200242 20021202 00242 WP 2002 12 2 ASAA0280530 1 20021108 A 3350 803900 BATTERY PACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 976AS 53452 THREE TAILCONE PASSAGEWAY EMERGENCY LIGHTS WERE FOUND INOPERATIVE. RESEATED ASSOCIATED POWER SUPPLY. LIGHT THEN OPERAT ED PROPERLY. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120200243 20021202 00243 EU 2002 12 2 AWXA200201159 1 20021119 A 5315 D53910714200 WEB AIRBUS 320 A320231 3930325 EU CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 0 0 091 MCN - MAJOR REPAIR - DURING C-02 CHECK A 1" CRACK WAS FOUND ON FORWARD END OF WEB FLOOR SUPPORT BRACKET JUST INSIDE AVIO NICS DOOR 824 AT FS 6393 TO FS 6425. MAINTENANCE REMOVED DAMAGED WEB FLOOR SUPPORT BRACKET AT FS 6393 TO FR 6425; FABRIC ATED A NEW REPLACEMENT WEB FLOOR SUPPORT BRACKET; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 6-22, 28-30, & 39-41, FIG. 8, 12, & 18, AND DWG D53910714. 2 L 7 2 4F RT A28NM 2002120200244 20021202 00244 SO 2002 12 2 C2XA02IA243 1 20021120 A 3350 20131A BATTERY PACK EMB 145 EMB145ER 3260211 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14940 145033 BNA- DURING MAINTENANCE THE MECHANIC NOTED THAT THE AFT OVERWING, AND, AFT THREE AISLE EMERGENCY LIGHT STRIPS INOP. BN A- MAINTENANCE REMOVED AND REPLACED THE #4 EMERGENCY LIGHT BATTERY PACK, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTE D, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002120200245 20021202 00245 SO 2002 12 2 C2XA02IA245 1 20021128 A 3350 487190 RECEPTACLE EMB 145 EMB145 3260210 SO CABIN DIRTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 IAH- DURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY AISLE PATH LIGHTS FORWARD STRIP WAS INTERMITTENT. IAH- MAIN TENANCE CLEANED AND RESECURED THE LIGHT STRIP CONNECTOR, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002120300001 20021203 00001 GL 2002 12 3 S02472043 2 20021129 A 7200 CF680C2* ENGINE GE BOEING 747 747400 NM GE CF6 CF680C2* GL # 4 W SAJF D RETURN TO BLOCK O OTHER CL CLIMB 1 WP 03 1263 B-18705 NO.4 ENG OCCURRED N2 VIB AND SURGE DURING CLIMBING.C/A:1.BORESCOPE INSP. GAS PATH PER AMM 72-00-00 P206 FOUND DA MAGE STARTING AT STAGE 4. FOUND A VARIABLE VANE BROKEN AND TURNED INTO THE AIR STREAM, HALH OF THE VANE STARTING AT THE TIP MISSING. ALL STAGE 5 BLADES BENT AND TORN AT THE LEADING EDGE.2.REPLACE NO.4 ENGINE AND ENG RUN UP TEST NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 2002120300002 20021203 00002 WP 2002 12 3 15HA0258007 1 20021102 A 3233 523500 ACTUATOR CVAC 340 34031 2422704 WP ALLSN 501D 501D13 03004 GL NLG SEPARATED A I5HA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 23 581P 7129 29 AFTER TAKEOFF, ENROUTE, THE PILOT HEAR A POP OR SNAP AFTER RAISING THE LANDING GEAR. THERE WERE NO OTHER ABNORMAL INDIC ATIONS IN THE COCKPIT AND THE FLIGHT WAS CONTINUED AND TERMINATED. THE LANDING WAS LOWERED UNEVENTFULLY. DURING THE PO STFLIGHT INSPECTION, THE PILOT FOUND THAT THE NOSE LANDING GEAR ACTUATOR HAD BROKEN OFF THE NOSE LANDING GEAR WHERE IT A TTACHES TO THE GEAR. THE AIRCRAFT WAS FERRIED TO MAINTENANCE BASE WITH LANDING GEAR DOWN. WHERE THE NOSE LANDING GEAR WAS REMOVED AND REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4R 4 T 6A6 E282 2002120300003 20021203 00003 NM 2002 12 3 171944 1 20021015 A 2913 65466A7 HOUSING BOEING 737 737* NM HYD MODULE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 81178 HOUSING IS CRACKED AT PORT INTERSECTIONS. PROBABLE CAUSE MATERIAL IS TOO THIN AT INTERSECTION. REMOVE THIN WALL AT INT ERSECTION AND MAKE HOUSING STRONGER. 2 L 7 2 4F RT A16WE 2002120300004 20021203 00004 NM 2002 12 3 VNAA0211025 1 20021124 A 2611 SD9422A0A0 SMOKE DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LAVATORY MALFUNCTIONED A VNAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 440JS 18415 9890 3058 THE CREW RECEIVED A LAV SMOKE CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120300005 20021203 00005 NM 2002 12 3 VNAA0211029 1 20021126 A 3600 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 459PS 3070 DURING TAKE OFF, THE CREW RECEIVED A BLEED SHUT OFF VALVE CAS MESSAGE AND ABORTED TAKE OFF. AFTER THE AIRCRAFT CLEARED THE RUNWAY, THE CREW CYCLED THE BLEED VALVE AND THE MESSAGE CLEARED. FLIGHT 9424 WAS THEN CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND FLIGHT 9424 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120300006 20021203 00006 NM 2002 12 3 VNAA0211030 1 20021126 A 3600 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 433JS 3047 DURING TAKE OFF, THE CREW RECEIVED A BLEED SHUT OFF VALVE CAS MESSAGE AND ABORTED TAKE OFF. WHILE THE AIRCRAFT WAS CLEA RING THE RUNWAY THE MESSAGE CLEARED. THE CREW WAS THEN NOTIFIED THAT THERE WAS TWO PASSENGERS THAT WERE ON THE WRONG FL IGHT AND WANTED TO GET OFF THE PLANE. ONCE THE PLANE WAS BACK AT THE GATE THE CREW FOUND OUT THEY JUST WANTED TO GET OF F THE PLANE BECAUSE OF THE ABORTED TAKE OFF. FLIGHT 4043 WAS THEN CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND DEPARTED WI TH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120300007 20021203 00007 NM 2002 12 3 SWAA022749 1 20021120 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROWS NR 6 AND NR 9. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002120300008 20021203 00008 NM 2002 12 3 SWAA022751 1 20021121 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 411, STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002120300009 20021203 00009 NM 2002 12 3 SWAA022753 1 20021121 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500A + 11, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002120300010 20021203 00010 NM 2002 12 3 SWAA022754 1 20021120 A 3242 26010425 BRAKE BOEING 737 7372H4 138448C NM LT MLG WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 ON LANDING AND TAXI, LEFT BRAKE CYCLES AND GRABS. REMOVED AND REPLACED NR 1 BRAKE AND LT METERING VALVE PER MM. 2 L 7 2 4F A16WE 2002120300011 20021203 00011 2002 12 3 SWAA022756 4 20021120 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED BC1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002120300012 20021203 00012 NM 2002 12 3 SWAA022757 1 20021121 A 5753 6546435277 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED C2 CHECK, FOUND LT T/E OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED LEFT T/E OTBD AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2002120300013 20021203 00013 NE 2002 12 3 SWAA022758 2 20021121 A 7260 3353109040 SEAL BOEING 737 7373H4 1384600 NM CFM56 CFM56* 13802 NE NR 1 ENGINE LEAKING A SWAA B EMER. DESCENT J K WARNING INDICATION FLUID LOSS DE DESCENT 1 SW 29 652SW 27722 857197 IN-FLIGHT SHUTDOWN, DECLARED EMERGENCY, NR 1 ENGINE LOW OIL PRESS LIGHT ILLUMINATED, OIL QUANITY ZERO. PERFORMED PRECAU TIONARY ENGINE SHUTDOWN. REMOVED AND REPLACED SEAL ON OIL SCAVENGE LINE ON TRANSFER GEAR BOX PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002120300014 20021203 00014 NM 2002 12 3 SWAA022760 1 20021121 A 2782 654485113 ACTUATOR BOEING 737 7373G7 1384595 NM LT WING LEAKING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 LEFT INBD GROUND SPOILER ACTUATOR LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED LEFT INBD GROUND SPOILER ACTUATOR PER M M. 2 L 7 2 4F RT A16WE 2002120300015 20021203 00015 NM 2002 12 3 SWAA022761 1 20021121 A 2782 654456115 ACTUATOR BOEING 737 7373H4 1384600 NM RT WING LEAKING A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 29 311SW 23333 ON TAXI OUT, LOSS OF HYDRAULIC 'A' SYSTEM, ZERO QUANITY AND ZERO PRESS. REMOVED AND REPLACED NR 6 SPOILER ACTUATOR AND CASE DRAIN FILTER PER MM. 2 L 7 2 4F RT A16WE 2002120300016 20021203 00016 2002 12 3 SWAA022762 4 20021122 A 3417 HG480B13 ADC BOEING 737 7372H4 138448C NM E/E COMP FAULTY A SWAA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 29 103SW 23109 AIR TURNBACK, CAPTAINS ALTIMETER FAILED, ALTITUDE ALERT FAILED AND MACH TRIM FAIL LIGHT ILLUMINATED. REMOVED AND REPLAC ED AIR DATA COMPUTER PER MM. 2 L 7 2 4F A16WE 2002120300017 20021203 00017 NM 2002 12 3 SWAA022763 1 20021121 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500B + 13, STR 4R. REPAIRED SKIN PER BFG ER. 2 L 7 2 4F RT A16WE 2002120300018 20021203 00018 NM 2002 12 3 SWAA022764 1 20021124 A 5313 65C27314 TIE CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 312, STR 18R. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2002120300019 20021203 00019 2002 12 3 SWAA022765 4 20021123 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 772SW 27880 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002120300020 20021203 00020 NM 2002 12 3 SWAA022767 1 20021121 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 440 AND BS 459, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002120300021 20021203 00021 2002 12 3 SWAA022768 4 20021122 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002120300022 20021203 00022 NM 2002 12 3 SWAA022769 1 20021123 A 5330 589357 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT UPPER OTBD CORNER ON L-1 COCKPIT WINDOW. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002120300023 20021203 00023 NM 2002 12 3 SWAA022770 1 20021121 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 DURING SCHEDULED C2 CHECK, FOUND BS 1016 BULKHEAD CRACKED (2 EA) AT 11: 00 O'CLOCK POSITION RADIATING FROM RIVETS AT THE PERIPHERY OF THE PRESS PLUG. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F A16WE 2002120300024 20021203 00024 NM 2002 12 3 SWAA022771 1 20021123 A 5753 6546434302 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED C2 CHECK, FOUND RT INBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT INBD AFT T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002120300025 20021203 00025 NM 2002 12 3 SWAA022772 1 20021124 A 5753 6546435282 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED C2 CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OTBD AFT T/E FLAP. 2 L 7 2 4F RT A16WE 2002120300026 20021203 00026 NM 2002 12 3 SWAA022779 1 20021121 A 3350 M1132 BATTERY BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPECIAL VISIT, FOUND CABIN EMERGENCY EXIT LIGHTS M1132 BATTERY DISCHARGED. RECHARGED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002120300027 20021203 00027 NM 2002 12 3 SWAA022780 1 20021123 A 3210 654610918 CLEVIS BOEING 737 7373H4 1384600 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED C2 CHECK, FOUND RT MLG ACTUATOR WALKING BEAM ARM CLEVIS CORRODED. REMOVED AND REPLACED WALKING BEAM AR M CLEVIS PER MM. 2 L 7 2 4F RT A16WE 2002120300028 20021203 00028 NM 2002 12 3 SWAA022782 1 20021123 A 3210 6582770 FITTING BOEING 737 737317 138447P NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND RT MLG FWD WALKING BEAM HANGER ATTACH LUG CORRODED. REMOVED AND REPLACED HANGER F ITTING PER MM. 2 L 7 2 4F RT A16WE 2002120300033 20021203 00033 NM 2002 12 3 ASAA0210320 1 20021114 A 3350 86210144 BATTERY PACK BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE EXIT LIGHTS DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 743AS 21821 DURING RECON INSPECTION, FOUND OVERWING EXIT IDENTIFIERS FLASHING. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES. THE N LIGHTS OPERATED NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 2002120300034 20021203 00034 WP 2002 12 3 ASAA0280514 1 20021101 A 5311 97079776 FRAME DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 CIRCUMFERENTIAL FRAME IS CORRODED AT FUS STA 588 BETWEEN LONGERON 28R AND 28L IN MID CARGO BAY. REPAIRED WITH DOUBLER I AW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120300035 20021203 00035 2002 12 3 ASAA0280517 4 20021103 A 2565 3961899501 LANYARD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 935AS 49236 DURING PREFLIGHT CHECK, L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. 2 L 7 2 4F 4 F A6WE E2EA 2002120300036 20021203 00036 WP 2002 12 3 ASAA0280529 1 20021108 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 976AS 53452 EMERGENCY LIGHT WAS FOUND INOPERATIVE AT ROW 31. RESEATED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120300037 20021203 00037 WP 2002 12 3 ASAA0280532 1 20021107 A 3350 0105606 LIGHT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE CABIN MISSING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 953AS 49386 DURING PREFLIGHT CHECK DISCOVERED TRACK LIGHTING-3EA LITE FROM FRONT TOP COVER MISSING. (BASED ON THE CORRECTIVE ACTION , THIS WRITE-UP WAS TAKEN TO MEAN 3 EA EMERGENCY TRACK (AISLE) LIGHTS WERE MISSING.) AT EACH LOCATION, REPLACED LENS AN D LAMP, BOTH SUB-ASSEMBLIES TO THE LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. 2 L 7 2 4F 4 F A6WE E2EA 2002120300038 20021203 00038 WP 2002 12 3 ASAA0280533 1 20021107 A 3350 0105606 LENS DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE EMERGENCY LIGHT BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 953AS 49386 DURING PREFLIGHT, CHECK FOUND EMERGENCY TRACK LIGHT WHITE LENS BROKEN. REPLACED LENS, A SUB-ASSEMBLY OF THE LIGHT MODUL E. LIGHTS WHEN OPERATED PROPERLY. 2 L 7 2 4F 4 F A6WE E2EA 2002120300039 20021203 00039 WP 2002 12 3 ASAA0280534 1 20021110 A 3350 0105606 LIGHT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 948AS 53021 DURING LINE CHECK FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 21-23. REPLACED TWO LIGHTS MODULES. LIGHTS THEN OPER ATED PROPERLY. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120300040 20021203 00040 NM 2002 12 3 AALA20021516 1 20021024 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 383AN 26995 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 24B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECT OR AT SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002120300041 20021203 00041 2002 12 3 AALA20021533 4 20021024 A 2330 PROJECTOR BOEING 767 767323 1385205 NM CABIN MALFUNCTIONED A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 360AA 24041 ZRH - FLT 37 - EN ROUTE ZRH-DFW, PASSENGER VIDEO SYSTEM SMOKED AT POWER SUPPLY AND BLEW MAIN CIRCUIT BREAKER WHEN SWITCH ED ON. CREW SMELLED SMOKE IN FLIGHT DECK. REPLACED ZONES ABC PROJECTORS AND ALSO REPLACED CONTROL DISTRIBUTION BOX. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002120300042 20021203 00042 NM 2002 12 3 AALA20021538 1 20021027 A 2782 755299D ACTUATOR BOEING 757 757223 1384957 NM L/E SLAT FAILED A AALA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 663AM 25297 MIA - FLT 971 - EN ROUTE DFW-MIA, ON APPROACH TO MIA, RECEIVED LEADING SLAT ASYMMETRY EICAS MESSAGE WHEN EXTENDING FLAPS FROM 1 DEGREE. DECLARED EMERGENCY AND LANDED AT MIA WITHOUT INCIDENT. TROUBLESHOT AND REPLACED NR 7 SLAT OUTBOARD ROT ARY SLAT ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120300043 20021203 00043 NM 2002 12 3 AALA20021540 1 20021027 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 352AA 24033 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 26 A/B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 26 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002120300044 20021203 00044 NM 2002 12 3 AALA20021550 1 20021028 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 775AN 29584 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD LOWER RIGHT FORWARD FACING EMERGENCY ESCAPE PATH LIGHT ASSEMBLY IN G3 GALLEY WALL MISSING. REPLACED FORWARD LOWER RIGHT FORWARD FACING EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT G3 GALLEY WALL. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002120300045 20021203 00045 2002 12 3 SWAA022784 4 20021125 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM L2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 AFT ENTRY DOOR EMERGENCY EVACUATION SLIDE COMING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2002120300046 20021203 00046 2002 12 3 SWAA022785 4 20021121 A 2565 65C16820 RETAINER BOEING 737 7377H4 1384404 NM L1 DOOR. LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 701GS 27836 FWD ENTRY DOOR EMERGENCY EVACUATION SLIDE GIRT BAR FWD RETAINER CLIP FASTENER SHEARED. INSTALLED RETAINER CLIP FASTENER PER MM AND SRM. 2 L 7 2 4F RT A16WE 2002120300047 20021203 00047 2002 12 3 SWAA022786 4 20021121 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 FWD ENTRY DOOR EMERGENCY EVACUATION SLIDE COMING OUT OF CONTAINER. REINSTALLED SLIDE ASY PER MM. 2 L 7 2 4F RT A16WE 2002120300048 20021203 00048 NM 2002 12 3 SWAA022787 1 20021124 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM CABIN FLOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 1/2D CHECK, FOUND BS 328 FLOORBEAM CORRODED BETWEEN LBL 30 AND RBL 60. REPAIRED PER SWA EA. 2 L 7 2 4F RT A16WE 2002120300049 20021203 00049 NM 2002 12 3 SWAA022788 1 20021125 A 5330 6552988 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED, BS 940, STRINGER 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002120300050 20021203 00050 NM 2002 12 3 SWAA022789 1 20021125 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA CRACKS AT FUSELGE SKIN, BS 942, STRINGER 23L AND STRINGER 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002120300051 20021203 00051 NM 2002 12 3 SWAA022790 1 20021125 A 3350 6104789 BATTERY BOEING 737 7372H4 138448C NM CABIN WEAK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED SPECIAL VISIT, FOUND FWD CABIN AND RT OVERWING EMERGENCY EXIT LIGHT BATTERIES OUTPUT LOW. REMOVED AND REPLACED BATTERIES PER MM. 2 L 7 2 4F A16WE 2002120300052 20021203 00052 NM 2002 12 3 SWAA022791 1 20021126 A 5313 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA STRINGER SPLICES CRACKED, BS 908, STRINGER 4L, AND STRINGER 4R. REMOVED AND REPLACED BOTH STRINGER SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2002120300053 20021203 00053 NM 2002 12 3 SWAA022792 1 20021125 A 3350 65C34691 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING AT ROW 19 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002120300054 20021203 00054 NM 2002 12 3 SWAA022793 1 20021126 A 5315 BAC1509 BEAM BOEING 737 7373H4 1384600 NM AFT CARGO COMPT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED, BS 845 TO BS 860, RBL 8. REPAIRED BEAM PER SRM AND SWA RA. 2 L 7 2 4F RT A16WE 2002120300055 20021203 00055 NM 2002 12 3 SWAA022794 1 20021126 A 5311 6545812 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELTFRAME CRACKED 3 LONG, BS 328, BETWEEN STRINGERS 20R-21. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002120300056 20021203 00056 NM 2002 12 3 SWAA022796 1 20021126 A 5330 6545819 WEB BOEING 737 7373A4 1384585 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED C1 CHECK, FOUND 3 EA CRACKS AT NLG W/W FWD CENTER BULKHEAD WEB. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002120300057 20021203 00057 NM 2002 12 3 AALA20021551 1 20021028 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE R1 CLOSET DOOR EMERGENCY LIGHT ASSEMBLY BROKEN. REPLACED R1 CLOSET DOOR EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002120300058 20021203 00058 NM 2002 12 3 AALA20021553 1 20021028 A 5320 FLOOR SUPPORT BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AA 24526 TUL - FOUND CORROSION ON FLOOR SUPPORT AT BL0 AND FS 1650. INSTALLED NEW FLOOR SUPPORT AT STATION 1650 PER AARD 51-20-0 0-1. (M) 2 L 7 2 4F RT A2NM 2002120300059 20021203 00059 NM 2002 12 3 AALA20021554 1 20021028 A 5315 FLOORBEAM BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AA 24526 TUL - FOUND 14 SCREW HOLES CORRODED ON FLOOR FRAME AT FS 1640. INSTALLED 'T' ANGLE REPAIR PER SRM 53-00-51-2. (M) 2 L 7 2 4F RT A2NM 2002120300060 20021203 00060 EU 2002 12 3 AALA20021563 1 20021030 A 5320 ANGLE FOKKER F28 F28MK0100 4990807 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1400H 11340 TUL - FOUND OBLIQUE FRAME 50-2 ANGLE CRACKED. REMOVED AND REPLACED PER AARD 53-70-00-2. (M) 2 L 7 2 4F RT 2002120300061 20021203 00061 2002 12 3 372PA0014 4 20021126 A 2210 4051600913 COMPUTER BOEING 737 737306 13844BG NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 372PA 23546 Occasional FCC in-flight faults on FMC Bite. Swapped FCC's for further evaluation. Both FCC's Ops normal per LRU inter face Bite checks 2 L 7 2 4F RT A16NE 2002120300062 20021203 00062 NM 2002 12 3 CALA0200566 1 20021126 A 5330 SKIN BOEING 737 737524 1384721 NM W/S POST CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27610 27323 INSPECTION FOUND A 1/8" CRACK IN SKIN OF CO-PILOT'S WINDSHIELD POST AT UPPER R/H CORNER. A DOUBLER WAS INSTALLED IAW SRM 53-10-01. 2 L 7 2 4F RT A16WE 2002120300063 20021203 00063 NM 2002 12 3 CALA0200568 1 20021201 A 3350 20131A BATTERY PACK BOEING 737 737524 1384721 NM L2 EXIT LT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14662 28923 INSPECTION FOUND EMERGENCY EXIT LIGHT OVER L-2 DOOR INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATION OF THE LIGH T WAS RESTORED. 2 L 7 2 4F RT A16WE 2002120300064 20021203 00064 NM 2002 12 3 CALA0200569 1 20021202 A 5330 SKIN BOEING 777 777224 1385225 NM STA 671-676 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78002 27578 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 671-676, S27L-28L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 7, FIGURE 202. A DIP WAS ISSUED TO INSPECT THE REPAIR WITHIN 16,000 FLIGHT CYCLES AND REPAIR WITHIN 30,000 FLIGHT CYCLES IAW SRM 53-00-01, REPAIR 7, TABLE 304. 2 L 7 2 4F RT T00001SE 2002120300065 20021203 00065 NM 2002 12 3 CALA0200570 1 20021202 A 5330 SKIN BOEING 777 777224 1385225 NM STA 2112-2116 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78002 27578 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 2112-2116 BETWEEN S25L AND S26L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, RE PAIR 7, FIGURE 202. A DIP WAS ISSUED TO REINSPECT THE AREA WITHIN 16,000 FLIGHT CYCLES AND TO PERFORM A PERMANENT REPAIR WITHIN 30,000 FLIGHT CYCLES IAW SRM 53-00-01, REPAIR 7, TABLE 204. 2 L 7 2 4F RT T00001SE 2002120300066 20021203 00066 EU 2002 12 3 AALA20021582 1 20021101 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MECHANIC FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED DEFECTIVE BATTERY PACK. (M) 2 L 7 2 4F RT A35EU 2002120300067 20021203 00067 NM 2002 12 3 AALA20021583 1 20021101 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY AT R-1 DOOR IS BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT R-1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002120300068 20021203 00068 2002 12 3 AALA20021584 4 20021101 A 3140 COMPUTER BOEING 767 767323 1385205 NM EICAS SYSTEM MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 381AN 25450 JFK - FLT 38 - EN ROUTE DFW-ZRH, TWO AND ONE-HALF HOURS INTO FLIGHT, BLUE CARGO DOOR EICAS MESSAGE CAME ON THEN BEGAN FL ICKERING ON AND OFF FOR 30 MINUTES. WHILE CALLING TECH GOT THE BULK CARGO DOOR EICAS STEADY AGAIN AND A QUICK BELL AND TWO QUICK RED EICAS MESSAGES WHICH WENT OUT BEFORE IT WAS READ. THIS WAS ALSO FOLLOWED BY EICAS DISAGREE AND LEFT EICAS COMPUTER WHITE MESSAGES. LANDED JFK WITHOUT INCIDENT. REPLACED LEFT EICAS COMPUTER AND ACCOMPLISHED CHECK. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002120300069 20021203 00069 NM 2002 12 3 AALA20021601 1 20021105 A 5414 FAIRING BOEING 767 767223 1385123 NM LT PYLON DEPARTED A AALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SW 21 320AA 22321 SFO - FLT 1994 - EN ROUTE SFO-DFW - ON TAKEOFF, LEFT PYLON DOGHOUSE FAIRING DEPARTED THE AIRCRAFT. RETURNED TO SFO WITH OUT INCIDENT. INSPECTED AIRCRAFT AND LEFT PYLON FOR OTHER DAMAGES. NO OTHER DAMAGED NOTED, PER SRM 54-5170-01 INTERIM REPAIR WAS PERFORMED. REINSPECT AT EACH B-CHECK FOR PROGRESSION AND PERFORM PERMANENT REPAIR AT NEXT MBV. GROUND CHECK ED OPERATION NORMAL. (M) 2 L 7 2 4F RT A1NM 2002120300071 20021203 00071 2002 12 3 159PL0023 4 20021201 A 2210 2588812902 COMPUTER BOEING 737 737242 1384477 NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 159PL 21186 Roll channel will not engage. R&R roll channel computer per MM 22-11-161. Ops check good. 2 L 7 2 4F A16WE 2002120300072 20021203 00072 EA 2002 12 3 ASOA02506 1 20020918 A 5270 601R3877211 STRIKER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT DEFECTIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 900EV 760B DURING GROUND INSPECTION AT BHM, THE LEFT OVERWING EMERGENCY EXIT INDICATED AN AMBER CAUTION MESSAGE WITH THE DOOR INSTA LLED. DEFERRED IAW MEL 52-70-03. MAINTENANCE DETERMINED THE MICROSWITCH STRIKER PLATE IS NEEDED TO CLEAR THIS DEFERRAL . THE DEFERRAL WAS CLEARED BY MAINTENANCE REMOVING AND REPLACING THE MICROSWITCH STRIKER PLATE. OPERATIONAL CHECKS GOO D. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2002120300073 20021203 00073 EA 2002 12 3 ASOA02513 1 20020922 A 3397 64643 CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 855AS 73955 FLT 4427 - DURING GROUND INSPECTION IN XNA, THE FLOOR EMERGENCY LIGHTS AT ROWS 1-5 WERE FOUND TO BE INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE FLOOR EMERGENCY LIGHT TRACK CABLE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SE RVICE. (M) 2 L 7 2 4F RT A21EA 2002120300074 20021203 00074 EU 2002 12 3 ASOA02514 1 20020923 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 634AS 370 DURING HANGAR INSPECTION AT MCN, THE PASSENGER DOOR EMERGENCY DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MA INTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY AT THE 61W POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2002120300075 20021203 00075 NM 2002 12 3 GAIA02154OP 1 20021107 A 5344 HINGE BOEING 727 727251 138408H NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 DURING ROUTINE INSPECTION OF THE MAIN CARGO DOOR HINGE, A CRACK WAS INDICATED ON THE FORWARD END OF BOTH HALVES, FUSELAG E/DOOR. ALSO, AT THE AFT END OF FUSELAGE HALF. NON DESTRUCTIVE INSPECTION CONFIRMED FINDING. REMOVED AND REPLACED HIN GE IAW SB AEIO1-01 REV B. ACCOMPLISHED ON KITTY HAWK EA B7-51-003. NDI HOLES WITH NO CRACKS NOTED. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 2002120300076 20021203 00076 NM 2002 12 3 GAIA02155OP 1 20021112 A 2782 1U1110 ACTUATOR BOEING 727 727225 1384077 NM L/E FLAP CRACKED A GAIA J DUMP FUEL K FLUID LOSS CL CLIMB 1 SW 07 936PG 22441 DURING CLIMB-OUT OF SCHEDULE FLIGHT NR 705 FROM IAH-FWA, THE CREW NOTICED THE LOSS OF SYSTEM 'A' HYDRAULIC QUANTITY, AND PRESSURE WENT TO ZERO. THE CREW DECLARED AND EMERGENCY AND RETURNED IAH. THE AIRCRAFT LANDED WITHOUT ANY INCIDENT. M AINTENANCE FOUND THE NR 3 LEADING EDGE ACTUATOR BROKEN AND LEAKING. REPLACED THE ACTUATOR AND SERVICED THE 'A' SYSTEM H YDRAULIC RESERVOIR. LEAK CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002120300077 20021203 00077 WP 2002 12 3 MEX2002335 1 20020511 A 3240 284703 CONTROL VALVE DOUG DC9 DC982 3022082 WP MLG FAULTY A ASMF O OTHER O OTHER LD LANDING 1 SW 23 501AM 49188 FLT 127 - GDL-MEX - DURING LANDING, WITH AUTO BRAKES ENGAGE, BREAKING WAS MINIMUM, AND CONTROL BRAKE OPERATED IN A STRON G WAY. BRAKING WITH LEFT SIDE DROPPED TO 0 IN LESS IN ITS RESPECTIVE DIAL INDICATOR. TECHNICAL PERSONNEL FOUND A BRAKE CONTROL VALVE FAULT. SUCH VALVE WAS REPLACED IAW MM 32-42-2, TEST OK. (M) 2 L 7 2 4F A6WE 2002120300078 20021203 00078 2002 12 3 MEX2002340 4 20021011 A 3425 92743642 RELAY DOUG DC9 DC987 3022087 WP FLIGHT DIRECTOR FAILED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 753RA 49587 FLT 579 - MEX-CUN - AIRCRAFT RETURN TO PLATFORM DUE TO SIF LIGHT TURN ON AND BOTH FLIGHT DIRECTORS DISAPPEAR ON TAKEOFF MODE. DURING CHECK IT WAS DETECTED THAT THE RELAY R2-6 MAINTAINS IN FLIGHT MODE ALL THE TIME. RELAY WAS REPLACED AND T ESTS WERE PERFORMED IAW MM 34-19-00. (M) 2 L 7 2 4F RT A6WE 2002120300079 20021203 00079 NM 2002 12 3 371PA0013 1 20021126 A 3350 LIGHT BOEING 737 737306 13844BG NM A PIDA K NONE O OTHER UK UNKNOWN 1 SO 05 371PA 23543 Floor emergency path inop from row 20 to back. R&R floor emergency path strip per MM 33-50-00Test OK. 2 L 7 2 4F RT A16NE 2002120300080 20021203 00080 NM 2002 12 3 TSAA0228198 1 20021001 A 2820 O-RING BOEING 737 73776N 13844CH NM FUEL SYSTEM DAMAGED A TSAA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 741AL 28641 FLT 462 - HNL-BUR, FUEL BURNING OUT OF THE NR 2 MAIN TANK WITH THE CENTER PUMPS 'ON' CAUSING FUEL IMBALANCE BETWEEN THE WING TANKS. THE BURN RATE IS 600 LBS PER HOUR. TURNED NR 2 PUMPS OFF AND REDUCED THE BURN RATE TO APPROXIMATELY 300 LB S PER HOUR. TURNING THE AFT FUEL PUMP OFF ONLY REDUCED THE BURN RATE TO 100 LBS. RETURNED TO HNL FOR UNEVENTFUL LANDIN G. MAINTENANCE VERIFIED WHEN NR 2 AFT FUEL PUMP IS ON, THE NR 2 MAIN FUEL TANK QUANTITY MIGRATES TO THE CENTER FUEL TAN K. REMOVED AND REPLACED NR 2 AFT FUEL PUMP DISCHARGE CHECK VALVE O-RINGS. VERIFIED NO FUEL MIGRATION WITH NR 2 AFT FUE L PUMP ON. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2002120300081 20021203 00081 NM 2002 12 3 USAA020411 1 20021030 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 51238 22956 CLT - FOUND SKIN WITH TWO CRACKS 2 INCHES AND .125 INCH, STATION 727E S24R. INSTALLED DOUBLER AND TRIPLER PER EA 86717. (M) 2 L 7 2 4F RT A16WE 2002120300082 20021203 00082 NM 2002 12 3 USAA020412 1 20021030 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 51238 22956 CLT - FOUND SKIN CRACKED 1.5 INCHES, STATION 767 S19R. INSTALLED DOUBLER AND TRIPLER PER EA 86718. (M) 2 L 7 2 4F RT A16WE 2002120300083 20021203 00083 NM 2002 12 3 USAA020413 1 20021031 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 48406 23594 PIT - FOUND SKIN CRACKED 1.25 INCH LONG, STATION 380 B/L 0. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07 AND EA 75219C . (M) 2 L 7 2 4F RT A16WE 2002120300084 20021203 00084 NM 2002 12 3 USAA020414 1 20020920 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND FRAME CRACKED .5 INCH LONG, STATION 616 RIGHT SIDE FRAME LOWER INBOARD END. INSTALLED DOUBLER ANGLE PER TYP ICAL REPAIR 53-61-01 AND EA 74856. (M) 2 L 7 2 4F RT A16WE 2002120300085 20021203 00085 NM 2002 12 3 PCAA0211139 1 20021129 A 3397 1013079 SOCKET DHAV DHC8 DHC8102 2809003 NM 5F DISCONNECTED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 836EX 297 DURING ROUTINE MAINTENANCE VISIT TWO FLOOR PATHWAY EMERGENCY LIGHTS FOUND TO BE INOPERATIVE AT SEATS 5F AND 7F. WIRE WAS FOUND PULLED OUT AT SEAT 5F. SOCKET PART #10-1307-9 WAS REPLACED. PIN FOUND BROKEN OFF AT SEAT 7F UNDER FLOOR, WIRE #33 52P9. REMOVED AND REPLACED PIN PART#640545-1. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002120300086 20021203 00086 NM 2002 12 3 USAA020415 1 20021104 A 5512 SKIN BOEING 737 737301 1384611 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND LEADING EDGE REMOVABLE SKIN WITH CRACKS, 1 INCH BY 1 INCH AREA BEYOND 25 PERCENT MAXIMUM LIMITS, 14 EACH BLE NDED AREAS, LEFT HORIZ STABILIZER LEADING EDGE STATION 86.66-151.75. BLENDED AND POLISHED PER SRM 55-10-01. (M) 2 L 7 2 4F RT A16WE 2002120300087 20021203 00087 NM 2002 12 3 USAA020416 1 20021002 A 5320 SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND SUPPORT CORRODED SEVERAL AREAS, BS 960 Z-ANGLE SUPPORT, AFT ENTRY THRESHOLD DOOR JAM. CORROSION, LEVEL 2, T ASK NR C53-107-01. REPLACED Z-ANGLE PER BOEING DWG 65-52878. (M) 2 L 7 2 4F RT A16WE 2002120300088 20021203 00088 NM 2002 12 3 USAA020417 1 20021107 A 5522 ELEVATOR BOEING 737 737301 1384611 NM ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 23228 PIT - FOUND LEFT ELEVATOR SPLINTERING AND DELAMINATED, STATION 95, 81, 100 INBOARD SIDE. ACCOMPLISHED SKIN AND CORE REP AIRS PER SRM 55-20-01, 51-70-17 AND EA 75277. (M) 2 L 7 2 4F RT A16WE 2002120300089 20021203 00089 NM 2002 12 3 USAA020418 1 20021104 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND SHELF CRACKED 1 INCH LONG, AFT END OF RIGHT 18A SHELF, FED OF STATION 727. REMOVED AND REPLACED SHELF PER S RM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002120300090 20021203 00090 NM 2002 12 3 USAA020419 1 20021104 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND FRAME CRACKED .5 INCH DIAMETER, S27L AND STATION 336 IN FRAME OF EYE OPENING. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2002120300091 20021203 00091 NM 2002 12 3 USAA020420 1 20021104 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND INTERCOSTAL CRACKED .5 INCH BY 7 INCH AREA, STATION 303 AND 310 AT STRINGER 4L. FABRICATED WEB, STRAP AND T -FITTING PER SRM 53-02-04. (M) 2 L 7 2 4F RT A16WE 2002120300092 20021203 00092 NM 2002 12 3 USAA020421 1 20021104 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND INTERCOSTAL CRACKED .75 INCH LONG, STATION 357 AND STRINGER 16L. DEFECTIVE PART REPLACED WITH IDENT PART NR . (M) 2 L 7 2 4F RT A16WE 2002120300093 20021203 00093 NM 2002 12 3 USAA020422 1 20021104 A 5313 1126919 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND STRINGER CRACKED .375 INCH LONG, STRINGER 17R BETWEEN STATION 616-639. DEFECTIVE PART REPLACED WITH IDENT P ART NR. (M) 2 L 7 2 4F RT A16WE 2002120300094 20021203 00094 NM 2002 12 3 USAA020423 1 20021104 A 5310 112337 SHEAR TIE BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND SHEAR TIE CRACKED .5 INCH LONG, SHEAR TIE S2L AT STATION 639. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2002120300095 20021203 00095 NM 2002 12 3 USAA020424 1 20021104 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND FRAME CRACKED .375 INCH, STATION 663 AND STRINGER 2L. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE AND STRINGER SPLICES PER EA 74814. (M) 2 L 7 2 4F RT A16WE 2002120300096 20021203 00096 NM 2002 12 3 USAA020425 1 20021104 A 5320 CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND CLIP CRACKED .5 INCH LONG, STATION 663 STRINGER 10L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2002120300097 20021203 00097 NM 2002 12 3 USAA020426 1 20021104 A 5320 BRACKET BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND BRACKET CRACKED .5 INCH LONG, STATION 663 STRINGER 8L AND 9L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2002120300098 20021203 00098 NM 2002 12 3 USAA020427 1 20021104 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND STRINGER CRACKED .5 INCH LONG, FS 663 STRINGER 4L. REMOVED TIE CLIP, HFEC INSPECTION OF STRINGER AND CLIP P ER SRM 51-40-02 AND NDT 0-4-53-10. (M) 2 L 7 2 4F RT A16WE 2002120300099 20021203 00099 NM 2002 12 3 USAA020428 1 20021104 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND FRAME CRACKED .5 INCH LONG, FS 480 STRINGER 8L AND 9L. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES PER EA 74 802-A. (M) 2 L 7 2 4F RT A16WE 2002120300100 20021203 00100 NM 2002 12 3 USAA020429 1 20021104 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND FRAME CRACKED .125 INCH, STATION 480 STRINGER 8R AND 9R. REMOVED DAMAGED AND INSTALLED REPAIR ANGLES PER EA 74802-A. (M) 2 L 7 2 4F RT A16WE 2002120300101 20021203 00101 NM 2002 12 3 USAA020430 1 20021004 A 5320 ATTACH ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 43748 24479 PIT - FOUND ATTACH ANGLE CRACKED .5 INCH, BS 290 BETWEEN S11R AND S12R. INSTALLED NEW ATTACH ANGLE PER SRM 51-10-02 AND 51-40-05. (M) 2 L 7 2 4F RT A16WE 2002120300102 20021203 00102 NM 2002 12 3 USAA020431 1 20021004 A 5330 69719477 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 23512 PIT - FOUND SKIN CRACKED .25 INCH LONG, BETWEEN AT 1 AND NR 2 CAPTAINS WINDOW. INSTALLED BOEING DOUBLER PER SRM 53-10-0 1. (M) 2 L 7 2 4F RT A16WE 2002120300103 20021203 00103 NM 2002 12 3 USAA020432 1 20021104 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 48746 23228 PIT - FOUND SHELF WITH 1 INCH LONG CRACK, AFT END OF LEFT 18A SHELF, FORWARD OF STATION 727. REMOVED AND REPLACED 18A S HELF PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2002120300104 20021203 00104 NM 2002 12 3 USAA020433 1 20021028 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 48447 22957 PIT - FOUND KEEL BEAM CRACKED 2 INCHES LONG AND PROGRESSIVE FORWARD, LEFT KEEL BEAM, AFT STRINGER 540. REPAIRED PER TYP ICAL REPAIR 53-60-09. (M) 2 L 7 2 4F RT A16WE 2002120300105 20021203 00105 NM 2002 12 3 USAA020434 1 20021004 A 5320 1131253 STIFFENER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 43748 24479 PIT - FOUND ANGLE STIFFENER CRACKED .5 INCH, BS 290 BETWEEN S12R-S13R. INSTALLED NEW ATTACH ANGLE PER SRM 51-10-02 AND 51-40-05. (M) 2 L 7 2 4F RT A16WE 2002120300106 20021203 00106 NM 2002 12 3 USAA020435 1 20021004 A 5320 1131966 ATTACH ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 43748 24479 PIT - FOUND ATTACH ANGLE CRACKED .5 INCH, BS 290 BETWEEN S13R-S14R. INSTALLED NEW ATTACH ANGLE PER SRM 51-10-02 AND 51- 40-05. (M) 2 L 7 2 4F RT A16WE 2002120300107 20021203 00107 NM 2002 12 3 USAA020436 1 20021004 A 5320 1135256 ATTACH ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 43748 24479 PIT - FOUND ATTACH ANGLE CRACKED .5 INCH, BS 290 BETWEEN S9R-S10R. INSTALLED NEW ATTACH ANGLE PER SRM 51-10-02 AND 51-4 0-05. (M) 2 L 7 2 4F RT A16WE 2002120300108 20021203 00108 WP 2002 12 3 ABXA020314 1 20021104 A 5700 99193318 FORMER DOUG DC9 DC933F 302207A WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 THIRD LEADING EDGE RIB OUTBOARD OF #11 SLAT TRACK CRACKED AT AFT UPPER END. REPLACED RIB IAW DC-9 SRM 51-30-2, 51-30-5, AND 51-10-3B. 2 L 7 2 4F A6WE 2002120300109 20021203 00109 WP 2002 12 3 ABXA020315 1 20021105 A 5700 3923255504N SUPPORT DOUG DC9 DC933F 302207A WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 INBOARD SPOILER ACTUATOR OUTBOARD SUPPORT FITTING WAS CRACKED AT UPPER FLANGE. REPLACED SUPPORT IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002120300110 20021203 00110 WP 2002 12 3 ABXA020317 1 20021105 A 5300 49162701 CLIP DOUG DC9 DC933F 302207A WP CENTER WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 CLIP CRACKED FRONT SIDE OF FRAME AT F.S. 637 AT LONGERON 29 LEFT. REPLACED CLIP IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002120300111 20021203 00111 WP 2002 12 3 ABXA020319 1 20021105 A 5300 99577417 FORMER DOUG DC9 DC933F 302207A WP CENTER WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 CRACK AT OUTBOARD END OF FRAME F.S. 658 AND LONGERON 27 RIGHT CANTED KEEL AREA. REPAIRED FRAME IAW DC-9 SSRM DWG. #K0515 9. 2 L 7 2 4F A6WE 2002120300112 20021203 00112 WP 2002 12 3 ABXA020322 1 20021106 A 5300 54956034513 SUPPORT DOUG DC9 DC933F 302207A WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 FLOOR SUPPORT FITTING AT F.S. 980 LONGERON 28 LEFT CRACKED UNDER STRAP. REPLACED SUPPORT FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002120300113 20021203 00113 WP 2002 12 3 ABXA020324 1 20021107 A 5300 591359511 CLIP DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 CRACKED SHEAR TIE AT STA. 1076 (AFT SIDE) BETWEEN LONGERONS 15 - 16 LEFT. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 2002120300114 20021203 00114 WP 2002 12 3 ABXA020326 1 20021130 A 5300 57552713 SKIN DOUG DC8 DC863F 302198F WP F.S. 216 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 46097 LOWER BELLY SKIN AFT OF ANTENNA F.S. 216 BETWEEN LONGERON 33 RIGHT AND 34 RIGHT WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 2002120300115 20021203 00115 NM 2002 12 3 USAA020437 1 20021103 A 5313 6546877144 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 23512 PIT - FOUND ANGLE CRACKED .5 INCH, SHELF 18A RIGHT SIDE JUST FORWARD OF 727. ATTACHED PARTS PER BOEING DWG 65-46877. ( M) 2 L 7 2 4F RT A16WE 2002120300116 20021203 00116 NM 2002 12 3 USAA020438 1 20021105 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 49067 23512 PIT - FOUND ANGLE CRACKED .5 INCH, LT SHELF 18A FORWARD OF STATION 727. FABRICATED NEW PART PER BOEING DWG 65-46877. ( M) 2 L 7 2 4F RT A16WE 2002120300117 20021203 00117 NM 2002 12 3 USAA020439 1 20021103 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 49067 23512 PIT - FOUND SKIN CRACKED 1.5 INCH, LOWER AFT RADIUS OF FORWARD SERVICE DOOR SKIN CUT OUT FS 32. REPAIRED IAW WITH SRM 5 3-10-01 AND PER EA 74911 AND 75007. (M) 2 L 7 2 4F RT A16WE 2002120300118 20021203 00118 NM 2002 12 3 USAA020443 1 20021102 A 5320 STRINGER CLIP BOEING 737 7373B7 1384580 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 43748 24479 PIT - FOUND STRINGER WITH MANGLED CLIP, BS 360 S-11R. INSTALLED REMANUFACTURED BELT FRAME CLIP PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002120300119 20021203 00119 NM 2002 12 3 USAA020444 1 20021105 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 44072 23860 PIT - FOUND SKIN CRACKED 1.5 INCH CRACK, STATION 727D, STRINGER S23L. CRACKED REMOVED AND SKIN DOUBLER INSTALLED PER TY PICAL REPAIR 53-60-03. (M) 2 L 7 2 4F RT A16WE 2002120300120 20021203 00120 NM 2002 12 3 USAA020445 1 20021105 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 44072 23860 PIT - FOUND SKIN CRACKED 1.5 INCH, STATION 727D, STRINGER S23R. CRACK REMOVED AND SKIN DOUBLER INSTALLED PER TYPICAL RE PAIR 53-60-03. (M) 2 L 7 2 4F RT A16WE 2002120300121 20021203 00121 NM 2002 12 3 USAA020446 1 20021110 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 48447 22957 PIT - FOUND FRAME CRACKED .250 INCH, STATION 663 AND STRINGER 2L. REMOVED DAMAGED FRAME SECTION, FABRICATED AND INSTALL ED REPAIR ANGLE AND FILLERS PER SRM 53-00-07, EA 75. (M) 2 L 7 2 4F RT A16WE 2002120300122 20021203 00122 NM 2002 12 3 USAA020447 1 20021110 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 48447 22957 PIT - FOUND FRAME CRACKED .100 INCH LONG, STATION 663 STRINGER 3L. FABRICATED AND INSTALLED REPAIR ANGLES AND FILLERS P ER SRM 53-00-07, EA 75015. (M) 2 L 7 2 4F RT A16WE 2002120300123 20021203 00123 NM 2002 12 3 USAA020448 1 20021110 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 48447 22957 PIT - FOUND FRAME CRACKED .500 INCH LONG, STATION 639 STRINGER 9L. MANUFACTURED AND INSTALLED NEW SECTION PER EA 75051. (M) 2 L 7 2 4F RT A16WE 2002120300124 20021203 00124 NM 2002 12 3 USAA020449 1 20021110 A 5320 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 48447 22957 PIT - FOUND ANGLE CRACKED .250 INCH LONG, FRAME TO SKIN ANGLE, STATION 616 BETWEEN STRINGER 8L AND 7L. FABRICATED NEW A NGLE PER BOEING DWG, HEAT TREATED AND INSTALLED PER DWG NR 66-24124. (M) 2 L 7 2 4F RT A16WE 2002120300125 20021203 00125 NM 2002 12 3 USAA020450 1 20021110 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 48477 22957 PIT - FOUND FRAME CRACKED .100 INCH, STATION 639 STRINGER 9R. REMOVED DAMAGED SECTION OF FRAME PER SRM 53-00-01 FIG 101 . (M) 2 L 7 2 4F RT A16WE 2002120300126 20021203 00126 NM 2002 12 3 USAA020451 1 20021110 A 5320 1131403 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 48447 22957 PIT - FOUND ANGLE CRACKED 26 INCHES, RBBL 57 STATION 580-608 LOWER FUSELAGE SKIN. REMOVED AND REPLACED DAMAGED ANGLE PE R SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002120300127 20021203 00127 NM 2002 12 3 USAA020452 1 20021102 A 5320 65C1059210 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 48477 22957 PIT - FOUND BEAM WITH ELONGATED HOLES, STATION 980 LBBL 18-30. REMOVED DAMAGED FLOOR SUPPORT AND REPLACED WITH LIKE P/N PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2002120300128 20021203 00128 EU 2002 12 3 USAABA02022 1 20021103 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 678US 0388 PHL - FOUND THE EPSU BATTERY AT THE L4 DOOR IN NEED OF REPLACEMENT. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A46NM 2002120300130 20021203 00130 2002 12 3 USAABB02179 4 20021018 A 2230 948E308G2 COMPUTER BOEING 767 7672B7 1385107 NM AUTOTHRUST SYS MALFUNCTIONED A USAA K NONE J WARNING INDICATION CR CRUISE 1 EA 19 656US 26847 PHL - FLT 15, AT CRUISE, THE THROTTLES MOVED TOWARD IDLE. THE F/S POINTER INDICATED FAST AND FLAP LIMIT WAS DISPLAYED. THESE INDICATIONS LASTED FROM 3-5 SECONDS, AND THEN DID NOT REOCCUR. MAINTENANCE REPLACED THE THRUST MANAGEMENT COMPUT ER. (M) 2 L 7 2 4F RT A1NM 2002120300131 20021203 00131 2002 12 3 USAABB02182 4 20021020 A 2565 101651303 SLIDE BOEING 767 7672B7 1385107 NM L1 DOOR MALFUNCTIONED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651US 24764 PHL - DURING THE ANNUAL SLIDE OPERATIONAL CHECK OF THE L1 DOOR, THE SLIDE INFLATED BUT DEPLOYED IN A CROOKED MANNER. MA INTENANCE PERSONNEL STATED THE THE VELCRO ON THE LEFT SIDE OF THE SLIDE DID NOT RELEASE PROPERLY, FORCING THE SLIDE TO C ANT TO THE RIGHT SIDE. MAINTENANCE REPLACED THE SLIDE. TWO MORE SLIDES WILL BE PROGRAMMED FOR OPERATIONAL CHECKS TO DE TERMINE IF A FLEET-WIDE PROBLEM EXISTS. (M) 2 L 7 2 4F RT A1NM 2002120300132 20021203 00132 NM 2002 12 3 USAABB02186 1 20021028 A 2121 6066223 FAN BOEING 767 767201 1385125 NM CABIN MALFUNCTIONED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 649US 23901 LGW - FLT 15 EN ROUTE FROM MUC TO PHL, CREW REPORTED A SMELL OF SMOKE IN THE COCKPIT AND CABIN AS WELL AS A FLICKERING I N THE OVERHEAD LIGHTING. FLIGHT DIVERTED TO LGW AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINT ENANCE REPLACED THE RIGHT RECIRCULATION FAN. 2 L 7 2 4F RT A1NM 2002120300133 20021203 00133 NM 2002 12 3 USAABB02188 1 20021103 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 611AU 27123 LAX - FOUND THE FLOOR LEVEL EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002120300134 20021203 00134 NM 2002 12 3 USAABB02189 1 20021105 A 1420 8021703 TERMINAL BOEING 767 767201 1385125 NM RT ENGINE BROKEN A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 645US 23897 PHL - FLT 740 - EN ROUTE PIT-LGW, CREW RECEIVED THE EICAS MESSAGE 'R ENG HPSOV'. FLIGHT DIVERTED TO PHL AND LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 TERMINAL ON THE HPSOV BROKEN. THE WIRING WAS REPAIRED. (M) 2 L 7 2 4F RT A1NM 2002120300135 20021203 00135 NM 2002 12 3 USAABB02190 1 20021110 A 5414 FAIRING BOEING 767 7672B7 1385107 NM LT ENGINE DETACHED A USAA K NONE D INFLIGHT SEPARATION LD LANDING 1 EA 19 655US 25257 PHL - FLT 43 - UPON LANDING, THE FORWARD PORTION OF THE LEFT ENGINE STRUT FAIRING PARTIALLY DETACHED. THE NR 5 SPOILER AND THE A30 MAIN LANDING GEAR TIRE WERE DAMAGED. MAINTENANCE REPLACED THE STRUT FAIRING AND THE WHEEL ASSEMBLY, AND PRO GRAMMED THE SPOILER FOR REPAIR. (M) 2 L 7 2 4F RT A1NM 2002120300136 20021203 00136 2002 12 3 USAASA02094 4 20021102 A 2565 SLIDE AIRBUS A321 A321211 3930370 EU CABIN DEFECTIVE A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 186US 1701 BDL - DURING THE EMERGENCY LIGHT TEST, 'EPSU EXIT LOAD FWD L' MESSAGE DISPLAYED. MAINTENANCE REPLACED THE FORWARD ENTRY DOOR EMERGENCY EXIT SLIDE. OPS CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002120300137 20021203 00137 NM 2002 12 3 USAASB02166 1 20020902 A 3350 30043229 LIGHT BOEING 737 7373B7 1384580 NM EXTERIOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 523AU 23858 ORD - MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT BY THE AFT RIGHT SERVICE DOOR INOPERATIVE. MAINTENANCE ADJUSTED TH E BULB POWER CONTACT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002120300138 20021203 00138 NM 2002 12 3 USAASB02168 1 20020907 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 563AU 23551 GSO - MAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT THE LEFT ESCAPE HATCH FLOOR LEVEL, SEAT ROW 10 LEFT SIDE AN D THE BULLNOSE LIGHT AT SEAT ROW 15 RIGHT SIDE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK G OOD. (M) 2 L 7 2 4F RT A16WE 2002120300139 20021203 00139 NM 2002 12 3 USAASB02170 1 20020911 A 3350 3114981 SOCKET BOEING 737 737301 1384611 NM CABIN DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 356US 23559 IND - MAINTENANCE FOUND THE EMERGENCY LIGHT AT THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E REFLECTOR SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002120300140 20021203 00140 NM 2002 12 3 USAASB02174 1 20020918 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 776AU 24934 EWR - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 24ABC AND 25ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY IN CEILING OF AFT GALLEY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002120300141 20021203 00141 NM 2002 12 3 USAASB02178 1 20020922 A 3350 1012721 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 443US 24842 IND - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 6 ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SOCKET/ LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002120300142 20021203 00142 NM 2002 12 3 USAASB02179 1 20020923 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 446US 24873 EWR - MAINTENANCE FOUND THE EMERGENCY LIGHTS FROM SEAT ROWS 7 TO 23 AND THE RIGHT AFT EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT THE AFT LEFT POSITION. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002120300143 20021203 00143 NM 2002 12 3 USAASB02180 1 20020924 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 523AU 23858 DCA - MAINTENANCE FOUND THE AFT RIGHT CABIN EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY P ACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002120300144 20021203 00144 NM 2002 12 3 USAASB02181 1 20020924 A 3350 110049 CHARGER BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 531AU 24478 IND - MAINTENANCE FOUND THE MAIN ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHAR GER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002120300145 20021203 00145 NM 2002 12 3 USAASB02190 1 20021019 A 3230 LANDING GEAR BOEING 737 737301 1384611 NM NLG & MLG MALFUNCTIONED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 574US 23739 DTW - FLT 1904 - IN PREPARATION FOR LANDING AT DTW FROM PHL, AT APPROXIMATELY 1,500 FEET, CREW RECEIVED AN UNSAFE GEAR I NDICATION WITH THREE RED AND THREE GREEN GEAR LIGHTS ILLUMINATING. CREW INITIATED A GO-AROUND AND RESET THE GEAR SELECT OR HANDLE DOWN. A NORMAL GEAR INDICATION OF THREE GREEN GEAR LIGHTS WAS RECEIVED. FLIGHT LANDED WITHOUT FURTHER INCIDE NT. NO EMERGENCY WAS DECLARED. (M) 2 L 7 2 4F RT A16WE 2002120300146 20021203 00146 NM 2002 12 3 USAASB0219010 1 20021019 A 3230 LANDING GEAR BOEING 737 737301 1384611 NM NLG & MLG MALFUNCTIONED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 574US 23739 DTW - FLT 1904 - IN PREPARATION FOR LANDING AT DTW FROM PHL, AT APPROXIMATELY 1,500 FEET, CREW RECEIVED AN UNSAFE GEAR I NDICATION WITH THREE RED AND THREE GREEN GEAR LIGHTS ILLUMINATING. CREW INITIATED A GO-AROUND AND RESET THE GEAR SELECT OR HANDLE DOWN. A NORMAL GEAR INDICATION OF THREE GREEN GEAR LIGHTS WAS RECEIVED. FLIGHT LANDED WITHOUT FURTHER INCIDE NT. NO EMERGENCY WAS DECLARED. MAINTENANCE PINNED THE GEAR AND CHECKED OPERATION OF THE LANDING GEAR LEVER MECHANISM. OPERATION OF LANDING GEAR LEER MECHANISM CHECKS GOOD. MAINTENANCE COULD NOT DUPLICATE PROBLEM. REMOVED GEAR PINS. AI RCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002120300147 20021203 00147 NM 2002 12 3 USAASB02197 1 20021101 A 2120 ODOR BOEING 737 7373B7 1384580 NM CABIN DETECTED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 517AU 23703 LGA - FLT 370 - ON TAKEOFF FROM PIT, EN ROUTE TO LGA, CREW REPORTED A STRONG BURNED OIL SMELL AT THE FORWARD LEFT ENTRY DOOR AND AT THE AFT LEFT ENTRY DOOR. SMELL DISSIPATED DURING FLIGHT. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCID ENT AT LGA. MAINTENANCE INSPECTED AIR CONDITIONING PACKS, ENGINE INLETS AND RAN APU. INSPECTED GALLEYS AND OVERHEADS. COULD NOT DUPLICATE SMELL. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002120300148 20021203 00148 NM 2002 12 3 USAASB02198 1 20021102 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 391US 23313 PIT - DURING WEEKLY CHECK, WHILE ACCOMPLISHING OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE AFT GAL LEY OVERHEAD EMERGENCY EXIT SIGN/AFT SERVICE DOOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002120300149 20021203 00149 NM 2002 12 3 USAASB02199 1 20021103 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 446US 24873 PIT - MAINTENANCE FOUND THE CENTER AISLE EMERGENCY EXIT LIGHT FOR THE OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002120300150 20021203 00150 NM 2002 12 3 SWAA022699 1 20021117 A 3211 6546100 TRUNNION BOEING 737 7373H4 1384600 NM RT MLG SHEARED A SWAA K NONE E VIBRATION/BUFFET DE DESCENT 1 SW 29 652SW 27722 DECLARED EMERGENCY, UPON GEAR EXTENSION HEARD LOUD BANG AND ASSOCIATED VIBRATION. FOUND RT MLG RETRACT TRUNNION SHEARED . REMOVED AND REPLACED RT MLG PER MM. 2 L 7 2 4F RT A16WE 2002120300151 20021203 00151 2002 12 3 SWAA022702 4 20021115 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT CABIN DOORS OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BC1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDES PRESS IND OUT OF VIEW. REPOSITIONED SLIDES PER MM. 2 L 7 2 4F RT A16WE 2002120300152 20021203 00152 NM 2002 12 3 SWAA022703 1 20021115 A 3211 6546113 PIN BOEING 737 7373H4 1384600 NM MLG TRUNNION CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED SERVICE CHECK, SWA SI 11251-32, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRUNNION PINS PER MM. 2 L 7 2 4F RT A16WE 2002120300153 20021203 00153 2002 12 3 SWAA022705 4 20021116 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002120300154 20021203 00154 2002 12 3 SWAA022706 4 20021116 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002120300155 20021203 00155 NM 2002 12 3 SWAA022710 1 20021116 A 3350 6556633 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002120300156 20021203 00156 NM 2002 12 3 SWAA022711 1 20021115 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE IN AFT CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2002120300157 20021203 00157 NM 2002 12 3 SWAA022737 1 20021118 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 739GB 29275 EEPLS INOP AT FWD CABIN. REMOVED AND REPLACED EEPLS SECTION PER MM. 2 L 7 2 4F RT A16WE 2002120300158 20021203 00158 NM 2002 12 3 SWAA022738 1 20021114 A 2560 P2070001 BATTERY BOEING 737 7372T4 1384492 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 702ML 22054 EMERGENCY FLASHLIGHT INOP AT FWD CABIN INBD. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002120300159 20021203 00159 2002 12 3 SWAA022746 4 20021120 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002120300160 20021203 00160 NM 2002 12 3 SWAA022747 1 20021119 A 5753 6571909117 SPAR BOEING 737 7372H4 138448C NM T/E FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 086SW 22827 DURING SCHEDULED C2 CHECK, FOUND LT OTBD T/E MIDFLAP AFT SPAR CRACKED. REMOVED AND REPLACED LT OTBD T/E MIDFLAP PER MM. 2 L 7 2 4F A16WE 2002120300161 20021203 00161 NM 2002 12 3 SWAA022748 1 20021119 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 086SW 22827 DURING SCHEDULED C2 CHECK, FOUND EEPLS END CAP MISSING AT AFT CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2002120300162 20021203 00162 NM 2002 12 3 2002UALA01769 1 20021124 A 5315 FASTENER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ELONGATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 CABIN FLOOR SEAT TRACK FLANGE FASTENER HOLE FOR FLOOR BOARD ON INBD SIDE OF FLANGE ELONGATED LOCATED AT STA.572 LBL 44. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. L-ANGLE AND STRAP INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002120300163 20021203 00163 NM 2002 12 3 2002UALA01770 1 20021124 A 5313 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 CABIN, L.H. CREASE BEAM WEB AT STATION 996 TO 1020 HAD EXCESSIVE CORROSION ON UPPER SURFACE AT STRINGER 17R. SUPPLEMENTA L DATA UPDATE MAJOR REPAIR ACCOMPLISHED.MANUFACTURED AND INSTALLED WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002120300164 20021203 00164 NM 2002 12 3 2002UALA01771 1 20021124 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 FUSELAGE FRAME IN AFT PIT STATION 1500 UNDER FLOOR STRUCTURE BETWEEN RBL 3" AND 16" RBL HAD EXCESS MATERIAL REMOVED FROM UPPER FLANGE DURING CORROSION CLEAN-UP. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002120300165 20021203 00165 NM 2002 12 3 2002UALA01772 1 20021124 A 5315 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 CABIN FLOOR SUPPORT INTERCOSTAL WEB CRACKED IN RADIUS ON FORWARD END STATION 661 LBL 44" STRINGER 17L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REMOVED AND INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002120300166 20021203 00166 NM 2002 12 3 2002UALA01773 1 20021126 A 5313 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 CABIN RIGHT HAND CREASE BEAM WEB CORRODED AT OUTER CHORD AT BODY STATION 966 RBL 68". SUPPLEMENTAL DATA UPDATE MAJOR REP AIR ACCOMPLISHED. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002120300167 20021203 00167 NM 2002 12 3 2002UALA01774 1 20021126 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 LEFT FUSELAGE SKIN STATION 544, STRINGER 25L DAMAGED AT FASTENER HOLE COMMON TO TEAR STRAP DUE TO LIGHTNING STRIKE. MAJ OR REPAIR ACCOMPLISHED. DOUBLER AND FILLERS INSTALLED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002120300168 20021203 00168 WP 2002 12 3 IXXA0200081S 1 20020703 A 5210 DOOR DOUG DC8 DC871F 302199D WP FWD ENTRY CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 825BX 83050 2948 45978 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED AT FUSELAGE STATION 60 LONGERON 21L.REPAIR ACCOMPLISHED, REMOVED DAMAGED AREA AND INTERNAL DOUBLER AND TRIPLER, FABRICATION AND INSTALLATION OF FILLER AND REPAIR DOUBLER AND TRIPLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL 2 L 7 4 4F RT 4A25 2002120300169 20021203 00169 WP 2002 12 3 IXXA0200085S 1 20020709 A 5210 DOOR DOUG DC8 DC871F 302199D WP AFT PASSENGER CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 825BX 83050 2948 45978 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LEFT HAND SIDE OF THE AFT PASSENGER DOOR SKIN IN THE FORW ARD LOWER CORNER BELOW AN EXISTING REPAIR AT FUSELAGE STATION 1640 LONGERON 22L. REPAIR ACCOMPLISHED, REMOVAL OF EXISTI NG DOUBLER, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR FILLERS DOUBLERS AND TRIPLERS IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING AUTHORITY 28276-5248-02-110. 2 L 7 4 4F RT 4A25 2002120300170 20021203 00170 NM 2002 12 3 AWXA200201160 1 20021123 A 5330 65458001215 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 0 0 23777 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1/8" CRACK WAS FOUND ON FUSELAGE SKIN COMING FROM FASTENER HOLE ABOVE THE L-1 D OOR LOWER HINGE BS 312. MAINTENANCE REMOVED CRACKED FUSELAGE SKIN ABOVE THE L-1 DOOR LOWER HINGE BS 312; FABRICATED A NE W SECTION OF REPLACEMENT FUSELAGE SKIN PER BOEING DWG 65-45800; AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02, PG. 37, FIG. 7, PG. 25, FIG. 2, AND PG. 48, FIG. 12. 2 L 7 2 4F RT A16WE 2002120400001 20021204 00001 SO 2002 12 4 145499 1 20020917 A 3397 WIRE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL LIGHT DIMMER FAILED E CWQA K NONE L NO TEST IN INSP/MAINT 1 GL 05 325JF 145499 WIRE NR W101-0072-20 WAS FOUND BURNED IN HALF DURING INSPECTION AND TROUBLE SHOOTING TO CORRECT AN MEL ON THE BACK LIGHT ING ON THE PILOTS SIDE ELECTRONIC CLOCK. DURING INVESTIGATION IT WAS FOUND THAT THE SYSTEM DESIGN USED 20 GAUGE WIRE AT THE OUTPUT OF THE DC LAMP DIMMER THAT HAS AN INTERNAL CIRCUIT PROTECTION THAT TRIPS AT 16.75 AMPS WHICH EXCEEDS THE RAT ING FOR 20 GAUGE WIRE. RECOMMEND REEVALUATION OF SYSTEM DESIGN AND PROTECTION OF WIRING ON OUTPUT SIDE OF DC LAMP DIMME R. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002120400005 20021204 00005 2002 12 4 ASAA0280424 4 20021020 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D1 52044 NE ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 DURING PREFLIGHT CHECK, LANYARD BETWEEN GIRT BAR AND SLIDE COVER, BECAME DISCONNECTED. REATTACHED LANYARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120400006 20021204 00006 2002 12 4 ASAA0280425 4 20021021 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 DURING PREFLIGHT CHECK, LANYARD BETWEEN GIRT BAR AND SLIDE COVER, BECAME DISCONNECTED. REATTACHED LANYARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120400007 20021204 00007 2002 12 4 ASAA0280448 4 20021026 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D1 52044 NE ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 DURING PREFLIGHT CHECK LANYARD BETWEEN GIRT BAR AND SLIDE COVER WAS FOUND DISCONNECTED. REATTACHED LANYARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120400008 20021204 00008 WP 2002 12 4 ASAA0280451 1 20021026 A 5347 593054763 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 LEFT INBOARD SEAT TRACK IS GOUGED AT STA 693, LBL 22. REPLACED DAMAGED SECTION OF TRACK IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120400009 20021204 00009 WP 2002 12 4 ASAA0280452 1 20021026 A 5320 9936534165 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 FLOOR SUPPORT CORRODED AT STA 160-200, RBL 60. REPLACED FLOOR SUPPORT IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120400010 20021204 00010 WP 2002 12 4 ASAA0280453 1 20021026 A 5320 993653433 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 FLOOR SUPPORT CORRODED AT STA 200, BL 0- RBL 60. REPLACED FLOOR SUPPORT IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120400011 20021204 00011 WP 2002 12 4 ASAA0280454 1 20021026 A 5320 993653423 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 FLOOR SUPPORT CORRODED AT STA 195, LBL 44. REPLACED FLOOR SUPPORT IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120400012 20021204 00012 2002 12 4 ASAA0280479 4 20021029 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP PWA JT3D JT3D* 52039 NE ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 974AS 53450 DURING PREFLIGHT CHECK LANYARD BETWEEN GIRT BAR AND SLIDE COVER WAS FOUND DISCONNECTED. REATTACHED LANYARD. 2 L 7 2 4F 4 F RT A6WE 1E8 2002120400013 20021204 00013 NE 2002 12 4 BJNA021102 2 20021110 A 7220 812039 COVER BOEING 737 737200 1384453 NM PWA JT8 JT8D17A 52049 NE NR 1 ENG BEARING BROKEN A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 688356 HARD COMPRESSOR STALL ON NR 1 ENGINE AT 2.20 EPR - 96 PERCENT N1 - 20 KNOTS SPEED, POWER WAS PULLED TO IDLE WITHIN 300 F T OF TAKE OFF ROLL, TAKE OFF ABORTED. ENGINE INSPECTION: NOSE CONE OFF AND DAMAGED BASEBALL SIZE DAMAGE TO INNER LINER AND HONEYCOMB STRUCTURE OF THE NOSE COWL AT APPROXIMATELY 9:30 POSITION, DOME ATTACHING STUD HELICOILS PULLED FROM FRON T ACCESSORY COVER, ONE STRIPPED STUD HOLE ALSO BROKEN OUT WITH PIECE MISSING, CONNECTOR PLUG ATTACHING MOUNT BROKEN ON N R 1 TACH. JT8D BORESCOPE INSPECTION , FIRST STAGE FAN BLADES, ONE DENT OUT OF LIMITS IAW INSPECTION. PROBABLE CAUSE: FAILURE OF DOME ATTACHING STUD HELICOILS IN THE FRONT ACCESSORY COVER. REPLACED DAMAGED PARTS. 2 L 7 2 4F 4 F A16WE E2EA 2002120400014 20021204 00014 CE 2002 12 4 CGO2002F00005 1 20021115 A 2840 10138901827 PRESSURE SWITCH BEECH 2000 2000 1152000 CE PWA PT6 PT6A11 52043 NE FUEL SYSTEM MALFUNCTIONED B CGOR O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 03 8283S 8 NC41 REPLACED PRESSURE SWITCH ASSEMBLY. PILOT COMPLAINT OF LOW FUEL PRESSURE WARNING LIGHT COMING ON ALTITUDE. HAVE NOTED T HIS TO BE A REOCCURRING PROBLEM WITH NEW -27 SWITCH ASSEMBLY. OLDER DASH NUMBER SWITCH ASSEMBLY USUALLY HAD A MUCH LONG ER TBF RATE. PRESSURE SWITCH ASSEMBLY, FAILURE MODE SEEMS TO ALWAYS BE ALTITUDE RELATED, WARNING LIGHTS USUALLY ILLUMIN ATE AT OR ABOVE 12,000 FT MSL. 1 L 7 2 4T 3 T RT A38ACE E4EA 2002120400015 20021204 00015 NM 2002 12 4 F9B2002F00000 1 20021120 A 7160 ASM001 DUCT DOUG DC10 DC10 N/A-SDR NM INLET DAMAGED E F9BR K NONE O OTHER IN INSP/MAINT 1 SW 05 INLET DUCT ASSEMBLY DAMAGED. 2 L 7 3 4F RT A22WE 2002120400016 20021204 00016 NM 2002 12 4 F9B2002F00001 1 20021120 A 5753 113W1340 FITTING BOEING 777 777 UTILUSE NM TE FLAPS DAMAGED E F9BR K NONE O OTHER IN INSP/MAINT 1 SW 05 TRAILING EDGE FLAP FITTING, DAMAGED. 2 L 7 2 4F RT T00001SE 2002120400017 20021204 00017 SO 2002 12 4 FL178168 1 20021118 A 8120 NUT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA TURBOCHARGER LOOSE E FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 4112K FEL00016 318353006 THE MECHANIC WAS SPINNING THE TURBOCHARGER COMPRESSOR-TURBINE SHAFT BEFORE HE PUT THE INTAKE ELBOW ON THE TURBOCHARGER. WHEN HE DISCOVERED THAT THE LOCK NUT ON THE INTAKE END OF THE SHAFT COULD BE SPUN OFF BY HAND. NO EVIDENCE OF THE INSP ECTORS LOCK SEAL, ETC. NUT TO THREAD FIT IS LOOSE. TURBOCHARGER TSO IS -0- HOURS. ENGINE OVERHAULED AT MFG. 1 L 7 2 3O 3 O A20SO E14EA 2002120400018 20021204 00018 SO 2002 12 4 FMAA2002004 2 20021106 A 8530 SAC520011B CYLINDER CESSNA 206 U206G 2073356 CE CONT O520 IO520L 17032 SO NR 4 CRACKED E FMAA K NONE O OTHER IN INSP/MAINT 1 AL 01 734GW 1148 U20604832 567534 PROBLEMS ENCOUNTERED WITH SUPERIOR CYLINDERS, B OR B SERIES. NR 4 CYLINDER HAD STUCK EXHAUST VALVE AND BENT PUSH ROD. NR 1 AND NR 2 CYLINDERS HAD CRACKS EXTENDING FROM THE SPARK PLUG HOLE TO THE FIN AREA LEFT OF THE SPARK PLUG HOLE TO THE FIN AREA LEFT OF THE SPARK PLUG HOLE (WHEN FACING THE CYLINDER). FIELD INFORMATION INDICATES THIS IS A PROBLEM WITH B S ERIES CYLINDERS AND NOT THE D SERIES. 1 H 7 1 3O 3 O A4CE E5CE 2002120400019 20021204 00019 NM 2002 12 4 IU62002F00033 1 20021021 A 2760 654494713 HOUSING BOEING 737 737* NM ACTUATOR CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 4872 HOUSING IS CRACKED AT THE BASE, NEX TO BEARING ON THE RETRACT SIDE. METAL FATIGUE IS PROBABLE CAUSE OF FAILURE. 2 L 7 2 4F RT A16WE 2002120400020 20021204 00020 NM 2002 12 4 IU62002F00034 1 20020930 A 2910 654458211 HOUSING BOEING 737 737* NM HYD VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 THE HOUSING IS CRACKED THROUGH INTERNALLY FROM ONE VALVE TO ANOTHER. PROBABLE CAUSE COULD BE WEAK MATERIAL OR OVER PRES SURIZATION. 2 L 7 2 4F RT A16WE 2002120400021 20021204 00021 CE 2002 12 4 M2G2002F00000 1 20021126 A 7120 SUPPORT CESSNA 320 320C 2074510 CE CONT O470 TSIO470B 17026 SO ENGINE CORRODED E M2GA K NONE O OTHER IN INSP/MAINT 1 WP 01 3029T 3962 320C0029 FOUND LEFT AND RIGHT ENGINE SUPPORT STRUCTURE TO BE EXCESSIVELY CORRODED WHERE ENGINE BEAMS INTERSECT CANTED BULKHEAD. RIVET TAILS WHERE FLAKING OFF WITHIN BULKHEAD (THIS NORMALLY CAN NOT BE SEEN BY VISUAL INSPECTION THIS CONDITION WAS DIS COVERED DURING DISASSEMBLY. SB LED TO THIS DISCOVERY. LT AND RT ENGINE SUPPORT STRUCTURES HAD TO BE REPLACED. 1 L 7 2 3O 3 O 3A25 3E3 2002120400022 20021204 00022 EU 2002 12 4 UHL2002F00005 1 20021024 A 3243 HP14081004 CONTROL VALVE SAAB SF340 SF340A 7850100 EU BRAKE CONTROL WORN A UHLA K NONE O OTHER IN INSP/MAINT 1 NE 03 360SZ 38258 340A006 UPON LANDING, PILOT REPORTED BRAKES FELT WEAK ON STARBOARD SIDE. FELT OK, AIRCRAFT INSPECTED AIRCRAFT AND FERRIED FOR F URTHER INVESTIGATION. REMOVED AND REPLACED BRAKE CONTROL VALVE AND FURTHER PROBLEMS NOTED. 2 L 7 2 4T RT A52EU 2002120400023 20021204 00023 EU 2002 12 4 UHL2002F00006 1 20021112 A 7712 INDICATOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE TORQUE ERRATIC A UHLA K NONE O OTHER IN INSP/MAINT 1 NE 03 138SD 138 179 NR 2 TORQUE GAUGE ERRATIC ON TAKEOFF ROLL WHEN SET GAUGE WENT 100 PERCENT TO 120 PERCENT TORQUE AT 50-60 KNOTS. NO ENGI NE POWER PROBLEMS NOTED. ABORTED TAKEOFF. 2 L 7 2 4T 4 T RT A52EU E8NE 2002120400024 20021204 00024 CE 2002 12 4 WUX2002F00000 1 20021115 A 7830 545353711 BRACKET RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP THRUST REVERSER MISLOCATED E WUXA K NONE O OTHER IN INSP/MAINT 1 NM 11 327LJ 258490 LEFT THRUST REVERSER STOW HOSE PULLED OUT OF SWAGGED FITTING AT PYLON ATTACH POINT, CAUSING IT TO LEAK. DETERMINED THAT LOWER SUPPORT BRACKET ATTACHED AT THE LOWER 5:30 CLOCK POSITION ON THE T/R IS RIVETED .250 CLOSER TO LIGHTING HOLE (WHE RE HOSE PASSES THROUGH) WHEN COMPARING BRACKET ALIGNMENT TO OTHER SIMILAR AIRCRAFT, CAUSING HOSE TO BE STRETCHED TO THE POINT OF SEPARATION. CONTACTED MFG FOR APPROVAL TO MOVE BRACKET TO RELEAVE TENSION ON HOSE. MOVED BRACKET IAW MFG INST RUCTION AND REPLACED HOSE WITH NEW AND PERFORMED LEAK CHECK WITH NO DEFECTS NOTED.(A1/1102) 2 L 7 2 4F 4 F RT A3EU E6WE 2002120400025 20021204 00025 CE 2002 12 4 X5C2002F00001 1 20021017 A 3233 O-RING LEAR 24 24 5170302 CE GE CJ610 CJ6101 30006 NE LT MLG ACTUATOR FAILED E X5CA K NONE O OTHER IN INSP/MAINT 1 GL 17 995TD 149 LOW HYDRAULIC PRESSURE DURING LANDING APPROACH. REPLACED O-RING AT LEFT MAIN LANDING GEAR ACTUATOR FITTING, OPS CHECK G OOD. 2 L 7 2 4J 4 J A10CE 1E16 2002120400032 20021204 00032 SO 2002 12 4 C2XA02CL237 1 20021202 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 12922 145338 CLE FLIGHT#2347 THE CREW REPORTED THE 1ST ROW OF EMERGENCY LIGHTS WERE INOPERATIVE.MAINTENANCE INSPECTED AND RESECURED T HE CONNECTOR ON THE EMERGENCY LIGHT STRIP.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002120400033 20021204 00033 2002 12 4 AALA20021555 4 20021028 A 2210 K157ABM6 CONTROL PANEL AIRBUS 300 A300B4605R 3930308 EU COCKPIT MALFUNCTIONED A AALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 21 41063 506 MIA - FLT 934 - EN ROUTE GYE-MIA, AT FL310, .78 MACH, RIGHT AUTOPILOT KICKED OFF RESULTING IN TAIL SWING AND RIGHT BANK. CHECKED SYSTEMS AND REENGAGED AUTOPILOT. LANDED AT MIA WITHOUT FURTHER INCIDENT. MAINTENANCE DOWN LOADED DFDR. VERI FIED THAT RIGHT BANK WAS 21 DEGREES AND .27 LATERAL ACCELERATION. ACCOMPLISHED SECTION 12 TURBULENCE CARD 05-92-13. RE PLACED FLIGHT CONTROL PANEL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2002120400035 20021204 00035 NM 2002 12 4 USAASB02175 1 20020918 A 2410 735511A CSD BOEING 737 737301 1384611 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC DE DESCENT 1 EA 19 587US 23932 TPA - FLT 1883 - FLIGHT DEPARTED CLT, EN ROUTE TO SRQ, WITH MEL 49-1 APPLIED TO APU FOR NOT STARTING. DURING DESCENT IN TO SRQ, AT 8,000 FEET, THE NR 2 ENGINE GENERATOR TRIPPED AND THE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNEC TED THE NR 2 CSD AND DIVERTED TO TPA WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAIN TENANCE FOUND THE NR 2 ENGINE CSD HAD FAILED. REMOVED AND REPLACED NR 2 ENGINE CSD PER MM 24-11-11. ALSO, FLUSHED LINE S AND REPLACED CSD AIR/OIL COOLER AND CSD LINE FILTER. REPLACED NR 2 ENGINE GENERATOR AS PRECAUTIONARY. OPERATIONAL CH ECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002120400036 20021204 00036 NM 2002 12 4 QXEA0202052 1 20021201 A 3260 465507 ACTUATOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 700 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 410QX 2378 4053 PDX - AFTER TAKE-OFF AND THE GEAR WAS SELECTED UP, THE RIGHT MAIN GEAR SHOWED UNSAFE WITH AN AMBER DOOR LIGHT FOR ABOUT 20 SECONDS. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT MAIN LANDING GEAR ACTUATOR. THE # 2 HYDRAULIC SYST EM WAS BLED AND OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002120400037 20021204 00037 NM 2002 12 4 USAASB02192 1 20021023 A 3260 189929 SAFETY SWITCH BOEING 737 737301 1384611 NM LANDING GEAR FAILED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 19 339US 23236 PIT - FLT 1591 - EN ROUTE, SEVERAL DISCREPANCIES THAT INDICATE THE A/C LOGIC WAS IN GROUND MODE. CB`S WERE NORMAL. AIR CRAFT STARTED TO DEPRESSURIZE AT FL280. NO OFF TIME ON ACARS. NO TCAS. TRANSPONDER WAS REPORTED INOP BY ATC. ENGINE LOW IDLE WAS IN THE GROUND OPERATING RANGE IN FLIGHT. AUTOTHROTTLE INOP. AUTO SPOILERS INOP. FLIGHT DIVERTED AND LAND ED WITHOUT INCIDENT. NO EMERGENCY DECLARED. MAINTENANCE R&R THE S105 AND S106 AIR/GROUND SAFETY SENSORS AND M990 LANDI NG GEAR LOGIC SHELF PRINTED CIRCUIT CARD. ACCOMPLISHED ADJUSTMENT AND TEST OF AIR/GROUND SAFETY SENSORS PER MM 32-09-01 AND ACCOMPLISHED LANDING GEAR LOGIC SHELF TEST FOR PRINTED CIRCUIT CARD M990 PER MM 32-09-20. ALL CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2002120400038 20021204 00038 NM 2002 12 4 USAASB02200 1 20021103 A 2910 BACH8A06EE0260T HYDRAULIC LINE BOEING 737 7373B7 1384580 NM HYD SYSTEM LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 389US 23311 CLT - FLT 794 - AFTER TAKEOFF AND GEAR RETRACTION FROM CLT, EN ROUTE TO SYR, CREW REPORTED THE LOSS OF SYSTEM 'A' HYDRAU LICS DURING FLAP RETRACTION FROM 5 UNITS TO 1 UNIT. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT CLT. FLIGHT LA NDED WITHOUT FURTHER INCIDENT AND WAS TOWED TO THE GATE. MAINTENANCE FOUND THE RIGHT MLG RETRACT ACTUATOR FLEX LINE LEA KING FROM A HOLE WORN IN THE LINE. REMOVED AND REPLACED THE FLEX LINE. PERFORMED GEAR SWING PER MM 32-32-11. OPERATIO NAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002120400039 20021204 00039 NM 2002 12 4 USAASB02201 1 20021104 A 3260 3186301001035 WARNING LIGHT BOEING 737 7374B7 1384702 NM COCKPIT BURNED OUT A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 778AU 24980 LGA - FLT 1836 - IN PREPARATION FOR LANDING AT LGA, FROM PIT, CREW DID NOT RECEIVE A LEFT MAIN LANDING GEAR GREEN LIGHT AFTER GEAR EXTENSION. CHECKED THE BULB AND IT WAS JAMMED. CREW ACCOMPLISHED AN EMERGENCY GEAR EXTENSION AND A VISUAL T HROUGH THE PERISCOPE WHICH INDICATED THE GEAR WAS DOWN. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT MAIN LANDING GEAR GREEN LIGHT BURNED OUT. RELAMPED LIGHT. OPERATIONAL TEST GOOD . (M) 2 L 7 2 4F RT A16WE 2002120400040 20021204 00040 NM 2002 12 4 USAASB02202 1 20021105 A 3350 CONNECTOR BOEING 737 737401 1384701 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 424US 23991 ORD - MAINTENANCE FOUND THE EMERGENCY EXIT IDENTIFIER AND THE SEAT AISLE LIGHT AT ROW 11C INOPERATIVE. MAINTENANCE RECO NNECTED PLUG AT SEAT ROW 11 JUNCTION BOX, LEFT SIDE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2002120400041 20021204 00041 NM 2002 12 4 USAASB02204 1 20021109 A 2131 7612608 CONTROLLER BOEING 737 7373B7 1384580 NM CABIN PRESSURE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 395US 23317 CLT - FLT 1279 - ON CLIMB-OUT FROM CLT, EN ROUTE TO MKE, CREW REPORTED THE CABIN ALTITUDE WARNING HORN SOUNDED PASSING T HROUGH FL030. FLIGHT RETURNED TO FIELD AT CLT. SHORTLY AFTER BEGINNING DESCENT, CABIN ALTITUDE RETURNED TO NORMAL. NO OXYGEN MASKS WERE DEPLOYED AND TO EXPEDITE ARRIVAL, AN EMERGENCY WAS DECLARED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. OPERATIONAL CHECK SATISFACTORY PER MM. AIRCRAFT OK F OR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002120400042 20021204 00042 WP 2002 12 4 WRLA200225 1 20021011 A 2720 CONTROL CABLE DOUG DC10 DC1030 3023501 WP RUDDER BROKEN A WRLA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 27 14075 46922 LEFT RUDDER CABLE BROKE AT APPROXIMATE STATION 1920. REPLACED RUDDER LEFT CONTROL CABLE SEGMENT 1D AND PERFORMED RIGHT CHECK IAW DC-10 MM 27-20-00. RIG CHECKED ACCOMPLISHED. FOUND CHAFED WIRE HARNESS FOR L4 FLIGHT ATTENDANT CONTROL PANEL BELOW FLOOR AT APPROXIMATE STATION 1820. ACCOMPLISHED WIRING REPAIR IAW SWP 20-10-01. REPLACED RUDDER CABLE AND REPAI RED CHAFED WIRES. (M) 2 L 7 3 4F A22WE 2002120400043 20021204 00043 WP 2002 12 4 WRLA200226 1 20021107 A 5270 SWITCH DOUG DC10 DC1030F 3023504 WP A/C BAY DOOR FAILED A WRLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 304WL 47928 AIR CONDITIONING DOOR LIGHT CAME ON IN FLIGHT. AIRCRAFT WAS DEPARTING OZARK AIRCRAFT SYSTEMS AT THE COMPLETION OF SCHED ULED 'A' CHECK AIRCRAFT RETURNED TO REPAIR STATION. TROUBLESHOT FOUND NR 2 AIR CONDITIONING BAY DOOR SWITCH INOPERATIVE . (M) 2 L 7 3 4F RT A22WE 2002120400044 20021204 00044 NM 2002 12 4 PCAA0211140 1 20021201 A 3397 BV0330211150 SOCKET DHAV DHC8 DHC8102 2809003 NM SEAT 2 D/F BURNED A PCAA K NONE M OVER TEMP NR NOT REPORTED 1 EA 13 832EX 280 LGA-FLIGHT#3747. CREW REPORTED A HOT ELECTRICAL SMELL IN THE FORWARD CABIN. MAINTENANCE FOUND A LIGHT SOCKET SHORTED OUT , REMOVED THE BULB AND ISOLATED THE SOCKET. MEL 33-02 WAS ISSUED AND AIRCRAFT RETURNED TO SERVICE. DURING MAINTENANCE RO N 03DEC02 BOTH OVERHEAD LIGHT SOCKETS AT SEAT 2D/F WERE REPLACED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVI CE. 2 H 7 2 4T RT A13NM 2002120400045 20021204 00045 EU 2002 12 4 QXEA0202026 1 20021127 A 4990 38075412 APU FOKKER F28 F28MK4000 4990810 EU ZONE 200 FAILED A QXEA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 09 492US 32592 1950 11159 PDX- SMOKE DETECTOR IN LAVATORY SOUNDING, WITH SLIGHT OIL SMELL IN AFT CABIN. APU STARTED APPROXIMITLY 15-20 MINUTES WI TH CABIN HEATING SELECTED ON. ALARM STOPPED ABOUT ONE MINUTE AFTER SELECTING THE APU AIR OFF.REMOVED AND REPLACED APU. O PERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002120400046 20021204 00046 NM 2002 12 4 SWAA022750 1 20021120 A 3350 604222 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 704SW 27838 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER M M. 2 L 7 2 4F RT A16WE 2002120400047 20021204 00047 NM 2002 12 4 SWAA022752 1 20021121 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER SPLICE P ER SRM. 2 L 7 2 4F RT A16WE 2002120400048 20021204 00048 NM 2002 12 4 SWAA022755 1 20021120 A 3350 7003661 BALLAST BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM. 2 L 7 2 4F RT A16WE 2002120400049 20021204 00049 NM 2002 12 4 SWAA022759 1 20021121 A 2920 65C268391134 HYDRAULIC LINE BOEING 737 7373H4 1384600 NM HYD SYSTEM LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 29 399WN 27693 AIR TURNBACK, DURING CRUISE, NR 2 ENGINE HYDRAULIC PUMP LOW PRESS LIGHT ILLUMINATED, QUANTITY DECREASED TO 1/4. REMOVED AND REPLACED B-SYSTEM HYDRAULIC LINE AT ACOUSTIC FILTER TO PRESS MODULE PER MM. 2 L 7 2 4F RT A16WE 2002120400050 20021204 00050 NM 2002 12 4 SWAA022766 1 20021121 A 5752 654645522C SKIN BOEING 737 7373H4 1384600 NM AILERON TAB DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND RT AILERON TAB DELAMINATED AT INBD UPPER SURFACE. REMOVED AND REPLACED RT AILERON TAB PER MM. 2 L 7 2 4F RT A16WE 2002120400051 20021204 00051 NM 2002 12 4 SWAA022773 1 20021122 A 3211 654611321 PIN BOEING 737 7373H4 1384600 NM LT MLG TRUNNION CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED C2 CHECK, SWA SI 11251-32, FOUND LT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED LEFT MLG TRUNNION PIN PER MM. 2 L 7 2 4F RT A16WE 2002120400052 20021204 00052 NM 2002 12 4 SWAA022774 1 20021123 A 3211 654611321 PIN BOEING 737 7373H4 1384600 NM RT MLG TRUNNION CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED C2 CHECK, SWA SI 11251-32, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNNION PI N PER MM. 2 L 7 2 4F RT A16WE 2002120400053 20021204 00053 NM 2002 12 4 SWAA022775 1 20021124 A 2731 6545166 ROD END BOEING 737 7373H4 1384600 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEV ATOR TAB AFT OTBD CONTROL ROD END PER MM. 2 L 7 2 4F RT A16WE 2002120400054 20021204 00054 NM 2002 12 4 SWAA022776 1 20021124 A 3350 6104789 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 071SW 22358 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH FWD AND AFT EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTER IES PER MM. 2 L 7 2 4F A16WE 2002120400055 20021204 00055 NM 2002 12 4 SWAA022777 1 20021124 A 3350 100885 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 071SW 22358 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002120400056 20021204 00056 NM 2002 12 4 SWAA022778 1 20021124 A 3350 100885 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 071SW 22358 DURING SCHEDULED SPECIAL VISIT, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY P ER MM. 2 L 7 2 4F A16WE 2002120400057 20021204 00057 NM 2002 12 4 QXEA0202035 1 20021126 A 6120 8Z8990051 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 FAILED A QXEA K NONE E VIBRATION/BUFFET DE DESCENT 1 NM 09 414QX 4061 SEA- ON LANDING APPROACH 1 1/2 NOUTICAL MILES OUT, PROP RPM DESTABILIZED BETWEEN 1020 AND 950 IN TWO SECOND CYCLES ON BO TH ENGINES. AIRSPEED ABOUT 130, TORQUE 13-15%, REDUCED NP NOT SELECTED. ADJUSTING TORQUE DID NOT STOP CYCLES. MOVING CON DITION LEVERS TO 950 DID NOT STABILIZE PROPS AND THEY REMAINED STABILIZED AT 1020 WHEN MAX THEN SELECTED. AIRCRAFT LANDE D WITHOUT INCIDENT. REMOVED AND REPLACED FUEL/ENGINE/PROPELLER CONTROL PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002120400058 20021204 00058 NM 2002 12 4 SWAA022781 1 20021124 A 3222 6561740 CYLINDER BOEING 737 7373H4 1384600 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED C2 CHECK, FOUND RT MLG TRUNNION PIN CORRODED AND FROZEN INSIDE OUTER CYLINDER. REMOVED AND REPLACED RT MLG OUTER CYLINDER PER MM. 2 L 7 2 4F RT A16WE 2002120400059 20021204 00059 NM 2002 12 4 SWAA022783 1 20021125 A 5523 183A8300 HINGE BOEING 737 7377H4 1384404 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 DURING SCHEDULED SERVICE CHECK, SI 11075-55, FOUND BOTH LT AND RT ELEVATOR TAB NR 4 HINGES HARDWARE WORN. REMOVED AND R EPLACED BOTH NR 4 ELEVATOR TAB HINGES HARDWARE PER MM. 2 L 7 2 4F RT A16WE 2002120400060 20021204 00060 2002 12 4 SWAA022795 4 20021126 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM . 2 L 7 2 4F RT A16WE 2002120400061 20021204 00061 NM 2002 12 4 VNAA0211020 1 20021120 A 3240 AC69965 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PARKING BRAKE FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 472PS 15438 4249 3008 EN ROUTE, THE CREW RECEIVED AN EMERGENCY BRAKE ACCUMULATOR CAS MESSAGE AND RESET IT TWO TIMES. ON THE THIRD OCCURRENCE THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CONTACTED MAINTENANCE CONTROL AND THE DECISION WAS MADE TO DIVERT TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120400062 20021204 00062 NM 2002 12 4 VNAA0211021 1 20021122 A 2612 51653151 FIRE LOOP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE CONTAMINATED A VNAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 463PS 9677 3087 EN ROUTE, THE CREW RECEIVED A RIGHT HAND ENGINE FIRE CAS MESSAGE. THE CREW FIRED THE FIRE BOTTLES AND DECLARED AN EMERG ENCY IN ACCORDANCE WITH PROCEDURES. FLIGHT 4178 THEN DIVERTED TO BOS. OUTSTATION MAINTENANCE INSPECTED AND FOUND THE FIRE DETECTOR CONTROL SUBMERGED IN RAIN WATER UNDER THE FLOORBOARDS. OUTSTATION MAINTENANCE THEN REPLACED THE FIRE DETE CTOR CONTROL AND THE EXTINGUISHED FIRE BOTTLES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHEC KS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120400063 20021204 00063 NM 2002 12 4 VNAA0211022 1 20021122 A 2612 440TS08Y01 CONTROL PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 463PS 9677 3087 DURING CLIMB, THE CREW RECEIVED A RIGHT HAND ENGINE FIRE WARNING ON THE RED WARNING PANEL AND THE CHIMES AND FIRE BELL W ENT OFF. THE CREW WENT THROUGH THE CHECKLIST AND FIRED THE FIRE BOTTLES THEN SHUT OFF THE RIGHT HAND ENGINE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO BOS. THE MAINTENANCE CONTROL MANAGER AND MECHANICS FROM DAY WERE DISPATCHED TO BO S. MAINTENANCE THEN INSPECTED AND REPLACED THE OVERHEAD FIRE PANEL AND THE FIRE BOTTLES IN ACCORDANCE WITH DORNIER MAIN TENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120400064 20021204 00064 2002 12 4 VNAA0211023 4 20021123 A 3418 STICK SHAKER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 472PS 3008 DURING TAKEOFF, THE CREW RECEIVED A PUSHER SHAKER FAIL MESSAGE AND ABORTED TAKEOFF. WHEN FLIGHT 4134 CLEARED THE RUNWAY THE MESSAGE CLEARED ITSELF. FLIGHT 4134 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4134 THEN DEPARTED WITH NO FU RTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120400065 20021204 00065 NM 2002 12 4 VNAA0211024 1 20021123 A 3350 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DAMAGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 439JS 3057 THE CREW REPORTED THAT THE FORWARD CABIN EMERGENCY LIGHTS WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPAIRED THE LIGHT CONNECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIR CRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120400066 20021204 00066 2002 12 4 VNAA0211026 4 20021124 A 3425 7015327905 FLIGHT DIR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 439JS 1567 289 3057 THE CREW REPORTED A BURNT ELECTRICAL SMELL IN THE COCKPIT WITHOUT THE PACKS ON. PIT MAINTENANCE WAS DISPATCHED, INSPECT ED, AND REPLACED THE GP-300 IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 22-00-00. OPERATIONAL CHECKS WERE PERFORMED A ND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120400067 20021204 00067 NM 2002 12 4 VNAA0211027 1 20021125 A 2720 LIMITER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RUDDER FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 459PS 3070 DURING CLIMB OUT, THE CREW RECEIVED A RUDDER NOT LIMITED ABOVE 165 KNOTS MESSAGE AND RETURNED TO RIC. THE TOWER DECLARE D AN EMERGENCY AND FLIGHT 4084 LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE DEFERRED THE RUDDER LIMITER, 27-4 C. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120400068 20021204 00068 NM 2002 12 4 VNAA0211028 1 20021125 A 3350 501122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 470PS 2238 3006 THE CREW REPORTED THAT THE BACK UP AND EMERGENCY BATTERIES FAIL TO TEST. MAINTENANCE INSPECTED AND CHANGED THE EMERGENC Y POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRA FT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120400069 20021204 00069 WP 2002 12 4 ABXA020329 1 20021111 A 5313 5920319513 LONGERON DOUG DC9 DC931 3022065 WP FWD. CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 LONGERON 29 LEFT CRACKED BETWEEN F.S. 579 AND 596. CRACKED ON BOTH VERTICAL FLANGES. REPAIRED LONGERON IAW REA D553-4578 0MR. 2 L 7 2 4F A6WE 2002120400070 20021204 00070 WP 2002 12 4 ABXA020330 1 20021111 A 5313 59203311 SPLICE DOUG DC9 DC931 3022065 WP FWD. CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 LONGERON 30 END FITTING BETWEEN F.S. 579 AND 596 CRACKED ON BOTH VERTICAL FLANGES. REPLACED END FITTINGS IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002120400071 20021204 00071 WP 2002 12 4 ABXA020331 1 20021111 A 5300 59114481 FRAME DOUG DC9 DC931 3022065 WP FWD. CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 LEVEL II CORROSION ON FRAME AT STA. 446, AFT SIDE, BETWEEN LONGERON 28 LEFT AND 28 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53 -03. 2 L 7 2 4F A6WE 2002120400072 20021204 00072 WP 2002 12 4 ABXA020332 1 20021111 A 5200 59101577 PANEL DOUG DC9 DC931 3022065 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 AFT LOWER CARGO DOOR, OUTER PAN CRACKED AT BLIND NUT AND BULGED OUT AT SAME LOCATION LOWER AFT CORNER. REPLACED AFT LOWE R CORNER DOOR IAW DC-9 MM AND NON ROUTINE #0345. 2 L 7 2 4F A6WE 2002120400073 20021204 00073 WP 2002 12 4 ABXA020333 1 20021111 A 5200 3913249503 CLIP DOUG DC9 DC931 3022065 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 AFT LOWER CARGO DOOR, #5 BEAM FORWARD END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345. 2 L 7 2 4F A6WE 2002120400074 20021204 00074 WP 2002 12 4 ABXA020334 1 20021111 A 5200 39132491 FITTING DOUG DC9 DC931 3022065 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 AFT LOWER CARGO DOOR, #2 BEAM FORWARD END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345. 2 L 7 2 4F A6WE 2002120400075 20021204 00075 WP 2002 12 4 ABXA020335 1 20021111 A 5200 391324902 FITTING DOUG DC9 DC931 3022065 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 AFT LOWER CARGO DOOR, #4 BEAM AFT END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #03 45. 2 L 7 2 4F A6WE 2002120400076 20021204 00076 WP 2002 12 4 ABXA020336 1 20021111 A 5200 3913249501 CLIP DOUG DC9 DC931 3022065 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 AFT LOWER CARGO DOOR, INNER ANGLE AT #2 BEAM FITTING AREA WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345. 2 L 7 2 4F A6WE 2002120400077 20021204 00077 WP 2002 12 4 ABXA020337 1 20021111 A 5200 39132492 FITTING DOUG DC9 DC931 3022065 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 AFT LOWER CARGO DOOR, #3 BEAM AFT END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #03 45. 2 L 7 2 4F A6WE 2002120400078 20021204 00078 WP 2002 12 4 ABXA020339 1 20021112 A 5312 3917624511 FITTING DOUG DC9 DC931 3022065 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 FORWARD SIDE OF AFT PRESSURE BULKHEAD RIGHT VENTRAL DOOR WEB SUPPORT ANGLE WAS CRACKED. REPLACED SUPPORT ANGLE IAW DC-9 SRM 51-10-4, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2002120400079 20021204 00079 WP 2002 12 4 ABXA020340 1 20021112 A 5300 59356507 DOUBLER DOUG DC9 DC931 3022065 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 LEFT MAIN FRAME AT F.S. 699 WAS CRACKED IN FORWARD POCKET AT/BETWEEN "Z" CLIP ATTACH BOLTS. REPAIRED MAIN FRAME ON E.A. 53400110-001-1 AND DC-9 SRM. 2 L 7 2 4F A6WE 2002120400080 20021204 00080 EA 2002 12 4 COMA0260677 1 20021127 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 710CA 7241 FLIGHT 6009 FLAPS FAILED AT ZERO DEGREES.COULD NOT DUPLICATE. C/W EO 27-045 AND 27-046. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2002120400081 20021204 00081 EA 2002 12 4 COMA0260678 1 20021127 A 5210 600381095 ROLLER CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 952CA 7092 FLIGHT 5465 CABIN DOOR LATCH CAUTION MESSAGE.REPLACED THE INNER HANDLE LATCH ROLLER. 2 L 7 2 4F RT A21EA 2002120400082 20021204 00082 EA 2002 12 4 COMA0260679 1 20021129 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 917CA 7017 FLIGHT 6033 CABIN DOOR WARNING MESSAGE.COULD NOT DUPLICATE. OPERATIONAL CHECK OF DOOR FOUND NO FAULTS. 2 L 7 2 4F RT A21EA 2002120400083 20021204 00083 EA 2002 12 4 COMA0260680 1 20021129 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 SO 01 952CA 7092 FLIGHT 5478 CABIN DOOR WARNING MESSAGE.RIGGED/ADJUSTED THE CABIN DORO LATCHING MECHANISM TO M/M SPECIFICATIONS. 2 L 7 2 4F RT A21EA 2002120400084 20021204 00084 EA 2002 12 4 COMA0260681 1 20021130 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS DE DESCENT 1 SO 01 710CA 18571 7241 FLIGHT 5238 FLAPS FAILED AT 8 DEGREES.REPLACED THE PDU. 2 L 7 2 4F RT A21EA 2003020600190 20030206 00190 WP 2003 2 6 02FDEA00721 1 20021010 A 2425 WARNING LIGHT DOUG DC10 DC1010 3022110 WP COCKPIT ILLUMINATED A FDEA H J A DEACTIVATE SYST/CIRCUITS DUMP FUEL UNSCHED LANDING H J G ELECT. POWER LOSS-50 PC WARNING INDICATION MULTIPLE FAILURE CL CLIMB 1 SO 25 383FE 46616 DURING CLIMBOUT AFTER T/O PASS 16,000 NR 3 GEN FAIL LIGHT ILLUMINATED. ACCOMPLISHED RED TABS THAT REQUIRE NR 3 GEN CSD TO BE DISCONNECTED. STARTED APU & IT RAN NORMAL FOR 10 MINS THEN APU LOW OIL PRESSURE LIGHT ILLUMINATED & APU SHUT DOWN . DUMPED FUEL & RTN DUE TO WX EN ROUTE TO MEMPHIS. 2 L 7 3 4F A22WE 2002120400085 20021204 00085 NM 2002 12 4 02FDEA00722 1 20021010 A 2751 18129942F1 INDICATOR BOEING 727 727200 138407E NM COCKPIT STICKING A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 208FE 22930 ON INITIAL FLAP RETRACTION, THE OUTBOARD TRAILING EDGE FLAP STOPPED MOVING AT ABOUT 1 DEG AND THE LEFT AND RIGHT NEEDLES ON THE GAUGE SHOWED ONE NEEDLE WIDTH SPLIT. RED TAG PROCEDURES ACCOMPLISHED AND AIR ABORT ACCOMPLISHED. UPON INSP FOU ND O/B FLAP IND STICKING. R&R O/B FLAP IND IAW MM CH 27-52-021-2. CYCLED FLAPS SEVERAL TIMES. NO FLAP SPLIT NOTED AND ALL INDICATIONS AND LIGHTS, OPS NORMAL. 2 L 7 3 4F RT A3WE 2002120400086 20021204 00086 WP 2002 12 4 ASAA0280455 1 20021026 A 5347 593054768 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 SEAT TRACK CORRODED AT FUSELAGE STATION 237-240, RBL 22. REPLACED SEAT TRACK IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120400087 20021204 00087 WP 2002 12 4 ASAA0280456 1 20021026 A 5310 995773997 SHEAR TIE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 SHEAR TIE CORRODED IN AFT CARGO BAY AT FUSELAGE STATION 1287, L29L-L29R. REMOVED CORROSION AND INSTALLED DOUBLER IAW SR M. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120400088 20021204 00088 WP 2002 12 4 ASAA0280457 1 20021026 A 5320 993053813 WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELGAE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 LEFT CUSP WEB CORRODED AT FUSELAGE STATION 465-484. REMOVED CORROSION AND REPAIRED IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120400089 20021204 00089 WP 2002 12 4 ASAA0280458 1 20021026 A 5320 5930536 ANGLE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 ANGLE CORRODED AT FUSELAGE STATION 134, CUSP LINE RBL 54. REPLACED ANGLE IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120400090 20021204 00090 NM 2002 12 4 ABXA020293 1 20021006 A 5311 143T106015 FRAME BOEING 767 767200 1385120 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 FORWARD CARGO LOWER LOBE, STATION 720, LEFT BUTT LINE 45, CORRODED UPPER CHORD. REPLACED CHORD IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 2002120400091 20021204 00091 NM 2002 12 4 ABXA020294 1 20021008 A 5310 140T2102331 SHEAR TIE BOEING 767 767200 1385120 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 FORWARD CARGO LOWER LOBE, STATION 742, BETWEEN STRINGERS 37 - 39 RIGHT, AND STRINGER 38 LEFT, CORRODED SHEAR TIES. REPL ACED SHEAR TIES IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 2002120400092 20021204 00092 NM 2002 12 4 ABXA020297 1 20020905 A 5420 313T3310U207 ANGLE BOEING 767 767200 1385120 NM NR 1 PYLON CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 LEFT WING, NR 1 PYLON SKIRT, LOWER CHORD MID SECTION, HAD INTERGRANULAR CORROSION. ALSO FROM MID TO AFT END FOUND SPOTS OF CORROSION. REPLACED CHORD (ANGLE) IAW SRM 54-51-71. 2 L 7 2 4F RT A1NM 2002120400094 20021204 00094 WP 2002 12 4 ABXA020310 1 20021125 A 2740 59109625 JACKSCREW DOUG DC9 DC932 3022066 WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 2928 47522 DURING HORIZONTAL STABILIZER JACKSCREW INSPECTION PER AD 2000-15-15, DC-9 SB DC-9-27A362, FOUND BRONZE METAL SHAVINGS IN SIDE THE LUBRICATION GREASE AND THE JACKSCREW THREADS WERE PITTED AND CORRODED. REPLACED JACKSCREW ASSEMBLY IAW DC-9 MM 27-40-01-4-0001. 2 L 7 2 4F A6WE 2002120400095 20021204 00095 2002 12 4 ABXA020311 4 20021126 A 2565 COVER BOEING 767 767200 1385120 NM EVAC SLIDE BINDING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 EMERGENCY SLIDE WOULD NOT ARM WHEN MAIN ENTRY DOOR CLOSED. FOUND COVER FOR SLIDE BINDING. ADJUSTED DOOR COVER, SLIDE A RMS NORMAL. 2 L 7 2 4F RT A1NM 2002120400096 20021204 00096 WP 2002 12 4 ABXA020313 1 20021103 A 5320 99236685 WEB DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 LEVEL I CORROSION ON SUB-FLOOR SEVERAL PLACES, BUTT LINE '0', OUTBOARD TO LONGERON 18 RIGHT, FS 133.4 TO FS 148. REPAIR ED AREA IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2002120400097 20021204 00097 WP 2002 12 4 ABXA020316 1 20021105 A 5730 39190932 SKIN DOUG DC9 DC933F 302207A WP CENTER WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 EXFOLIATION ON LOWER CENTER WING SKIN - XCW 20, AT STRINGER 19 RIGHT. REPAIRED AREA IAW DC-9 SRM 52-03. 2 L 7 2 4F A6WE 2002120400098 20021204 00098 WP 2002 12 4 ABXA020318 1 20021105 A 5313 39161741 LONGERON DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 LONGERON END CRACKED JUST AFT OF FORWARD "P" DOME ON LONGERON 29 LEFT. REPAIRED AREA IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002120400099 20021204 00099 WP 2002 12 4 ABXA020320 1 20021106 A 5330 5912350501 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 CRACK IN BELLY SKIN STA 465 BETWEEN LONGERON 29 LEFT TO 30. REPAIRED CRACK IN BELLY SKIN IAW REA D953-45748MR. 2 L 7 2 4F A6WE 2002120400100 20021204 00100 WP 2002 12 4 ABXA020321 1 20021106 A 5320 991556161 FLOOR SUPPORT DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 FLOOR SUPPORT AT FS 996 LONGERON 30, HEAVILY EXFOLIATED AND BROKEN OFF. REPLACED FLOOR SUPPORT IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2002120400101 20021204 00101 WP 2002 12 4 ABXA020323 1 20021107 A 5311 995823812 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 STA 980 FRAME REPAIR BELOW LONGERON 14 RIGHT WAS CRACKED. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2002120400102 20021204 00102 NM 2002 12 4 ABXA020325 1 20021202 A 3350 20131A BATTERY PACK BOEING 767 767200 1385120 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 773AX 22788 DURING PREDEPARTURE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE, WOULD NOT TEST. INSTALLED NEW EMERGENCY LIGHT BATTERY PA CK IN THE LOWER POSITION. OPS CHECKED GOOD IAW B767 MM. 2 L 7 2 4F RT A1NM 2002120400103 20021204 00103 WP 2002 12 4 ABXA020327 1 20021202 A 3350 5708458503 BATTERY PACK DOUG DC8 DC863F 302198F WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 815AX 1054 46097 EMERGENCY LIGHTS BATTERY PACK WOULD NOT CHARGE. REPLACED EMERGENCY LIGHT BATTERY AND RELAY PACK IAW DC-8 MM 33-50-01. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2002120400104 20021204 00104 WP 2002 12 4 ABXA020328 1 20021108 A 5542 SB5523AX2 SKIN DOUG DC9 DC931 3022065 WP RUDDER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 RUDDER TOP RIGHT SIDE HAD LARGE CRACK. REPLACED RUDDER IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002120400105 20021204 00105 WP 2002 12 4 ABXA020338 1 20021112 A 5315 991224359 FLOORBEAM DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 FLOORBEAM AT STA 995 WAS CORRODED ON THE TOP FLANGE AT LEFT BUTT LINE 46. REPAIRED FLOOR BEAM IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002120400106 20021204 00106 WP 2002 12 4 ABXA020341 1 20021114 A 5320 991224355 ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 RIGHT L ANGLE AT STA 965, LBL 30 - 52, HAD HEAVY CORROSION. REPLACED L ANGLE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002120400107 20021204 00107 NM 2002 12 4 02FDEA00759 1 20021021 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 BULGE IN COCKPIT FLOOR. R&R BEAM PER SRM 51-30-2, 51-30-5, 51-30-8. 2 L 7 3 4F RT A3WE 2002120400108 20021204 00108 NM 2002 12 4 02FDEA00770 1 20021026 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 BS 1352 T-CHORD AFT FLANGE IS WORN IN SEVERAL LOCATIONS FROM 3-9 O'CLOCK AND KNIFE EDGED AT 5 O'CLOCK. R&R BS 1352 T-CH ORD PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2002120400109 20021204 00109 EU 2002 12 4 02FDEA00774 1 20021029 A 5511 SPAR AIRBUS 310 A310 EU HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 RIGHT HORIZ STAB REAR SPAR TOP T-CHORD CORRODED BETWEEN RIB 5 TO 9. R&R T CHORD PER EA 6-5100-66468. 2 L 7 2 4F RT A35EU 2002120400110 20021204 00110 EU 2002 12 4 02FDEA00775 1 20021029 A 5511 SPAR AIRBUS 310 A310 EU HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 LEFT HORIZ STAB REAR SPAR TOP T-CHORD CORRODED APPROX 280 MM FROM RIB 3 TO 5. R&R T CHORD PER EA 6-5100-66468. 2 L 7 2 4F RT A35EU 2002120400112 20021204 00112 EU 2002 12 4 02FDEA00777 1 20021029 A 5511 SPAR AIRBUS 310 A310 EU HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 RIGHT HORIZ STAB REAR SPAR TOP T-CHORD CORRODED BETWEEN RIB 3 TO 5. R&R T CHORD PER EA 6-5100-66468. 2 L 7 2 4F RT A35EU 2003021000048 20030210 00048 NM 2003 2 10 DHL2002743513 1 20021116 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, AFT SIDE OF BS 1166 FRAME, STR 27 LT TO 28 LT IS CORRODED. REMOVED LOWER ANGLE AND STIFFNER FOR ACCESS AND FOUND CORRODED OUT OF LIMITS IAW B-727 SRM 53-10-1 CUT-OUT DAMAGE ON WEB AND FABRICATED FILLER AND NEW STIFFNER REPA IR DOUBLER IAW B-727 SRM 51-40-2. REMOVED 3 DAMAGED ANGLES AND REPLACED IAW B-727 SRM 53-10-2. AND 51-20-1. PARTS ALODI NED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2002120400113 20021204 00113 EU 2002 12 4 02FDEA00778 1 20021029 A 5312 BULKHEAD AIRBUS 310 A310 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 CORROSION ON NOSE LAND GEAR WHEEL WELL BULKHEAD AT LEFT TOP CORNER NEAR FRAME 16. R&R SKIN PER EA 6-5340-66864. 2 L 7 2 4F RT A35EU 2002120400114 20021204 00114 NM 2002 12 4 02FDEA00779 1 20021029 A 5314 KEELBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 CORROSION AT BS 950C=12, STR 29R. REPAIRED KEELBEAM BS 950C+12 STR 29R IAW FEDEX DWG SR 27-53-023. 2 L 7 3 4F RT A3WE 2002120400115 20021204 00115 NM 2002 12 4 02FDEA00780 1 20021025 A 5314 KEELBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 CORROSION ON KEELBEAM AT BS 950D TO 950E, STR 29 LT. REPAIRED KEEL BEAM STA 950D TO 950I STR 29L IAW FEDEX DWG SR 27-53 -023. 2 L 7 3 4F RT A3WE 2002120400116 20021204 00116 NM 2002 12 4 02FDEA00785 1 20021027 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 CORROSION ON SHEAR TIE AT BS 950B, STR 29R. 2 L 7 3 4F RT A3WE 2002120400117 20021204 00117 NM 2002 12 4 02FDEA00787 1 20021029 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 FRAME IS BENT AT BS 1010, LBL 30, WL 146. REPAIRED FRAME BS 1010 LBL 30 WL 146 IAW EA 7-5310-67044 AND SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2002120400118 20021204 00118 NM 2002 12 4 02FDEA00790 1 20021027 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 CORROSION ON SHEAR TIE AT BS 950B, STR 29R. R&R SHEAR TIE PER SRM 53-10-4 & EA 7-5310-67049. 2 L 7 3 4F RT A3WE 2002120400119 20021204 00119 NM 2002 12 4 02FDEA00791 1 20021104 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 GOUGE IN 1176 CHORD AT RBL 28, WL 208. R&R CHORD PER EA 7-5310-67046. 2 L 7 3 4F RT A3WE 2002120400120 20021204 00120 NM 2002 12 4 02FDEA00792 1 20021021 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 FRAME DENTED AT 970, LBL 30, STR 26L. R&R FRAME PER SRM 51-40-3 FIG & EA 7-5310-67055. 2 L 7 3 4F RT A3WE 2002120400121 20021204 00121 NM 2002 12 4 02FDEA00793 1 20021030 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 480FE 21462 BS 950C FRAME IS DENTED AT STR 25R UPPER FLANGE. R&R FRAME PER SRM 51-40-3 FIG 3 & EA 7-5310-67053. 2 L 7 3 4F RT A3WE 2002120400122 20021204 00122 NM 2002 12 4 02FDEA00799 1 20021105 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 DENT IN STR AT BS 392. REPAIRED STR 23R BS 392 IAW SRM 53-10-3, 51-10-2. 2 L 7 3 4F RT A3WE 2002120400123 20021204 00123 2002 12 4 UPS02139927 4 20021118 A 2565 D310230101 SLIDE AIRBUS A300 A300F4622R 3930360 EU CABIN FAILED A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 135UP 0819 INSPECTION TYPE:PS-7 ESCAPE SLIDE FAILED TEST DURING PS-7 CHECK. REMOVED AND REPLACED ESCAPE SLIDE PER A300 AMM 25-61-2 0. 2 L 7 2 4F RT A35EU 2002120400124 20021204 00124 NM 2002 12 4 UPS02239930 1 20021121 A 5753 SKIN BOEING 727 72725C 138400H NM T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:N/A RIGHT INBD AFT FLAP HAS DAMAGE (DENT WITH CRACKED SKIN) JUST OUTBOARD OF INBD CANOE FAIRING. REMOVE D DAMAGED SKIN AND CORE, REMOVED INBD AFT FLAP SECTION, REPAIRED FLAP IAW SRM 51-40-20. 2 L 7 3 4F A3WE 2002120400125 20021204 00125 NM 2002 12 4 UPS02239931 1 20021112 A 5321 524239000CA2 FLOOR PANEL BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C MAIN ENTRY DOOR FLOOR PANEL CORRODED BETWEEN FS 312 AND 344. REMOVED AND REPLACED FLOOR PANEL. 2 L 7 3 4F A3WE 2002120400126 20021204 00126 NM 2002 12 4 UPS02239932 1 20021112 A 5315 BAC150529222 FLOORBEAM BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C MAIN ENTRY DOOR FLOORBEAM T ANGLE SUPPORT SHOWS EVIDENCE OF CORROSION BETWEEN FS 312 AND FS 344. REMO VED AND REPLACED T ANGLE SUPPORT. 2 L 7 3 4F A3WE 2002120400127 20021204 00127 NM 2002 12 4 UPS02239933 1 20021125 A 3350 1000679 BATTERY PACK BOEING 727 72762C 138402C NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 913UP 19245 INSPECTION TYPE:IN BOTH EMERGENCY EXITS WILL NOT ARM. R&R BOTH BATTERY PACKS & INSTALLED NEW BATTERIES OPS CHECK GOOD. 2 L 7 3 4F A3WE 2002120400128 20021204 00128 NM 2002 12 4 UPS02239938 1 20021116 A 5514 PIN BOEING 727 72751C 1384015 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:C PITTING FOUND ON RT STAB INNER PINS. RT STAB INNER PIN REPLACED IAW MM 55-10-01. 2 L 7 3 4F A3WE 2002120400129 20021204 00129 NM 2002 12 4 UPS02239941 1 20021114 A 5315 FLOORBEAM BOEING 727 72751C 1384015 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:C BEAM TIE CRACKED ON FLOORBEAM LWR FLANGE BS 328 RBL 40. REPAIR PLATE FABRICATED AND FITTED AS PER ARM 53-10-8. 2 L 7 3 4F A3WE 2002120400130 20021204 00130 NM 2002 12 4 UPS02239945 1 20021119 A 5312 PRESSURE PANEL BOEING 727 72751C 1384015 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:C SUSPECT CRACK ON NLG CEILING AT BS 273 LBL14. HFEC CONFIRMS CRACK, DAMAGED ARE CUTOUT IAW SRM 51-40-0 2 FIG, HFEC CONFIRMS NDF. REPAIR CARRIED OUT SRM 51-40-02 FIG 1. 2 L 7 3 4F A3WE 2002120400134 20021204 00134 NM 2002 12 4 2002UALA01757 1 20021122 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 CABIN INTERCOSTAL CRACKED STATION 291.5 BELOW STRINGER 11R. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002120400135 20021204 00135 NM 2002 12 4 2002UALA01758 1 20021123 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 CABIN BODY STATION 807 FRAME CRACKED AT STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002120400136 20021204 00136 NM 2002 12 4 2002UALA01759 1 20021123 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 BODY STATION 727A FUSELAGE FRAME, STRINGER 8L STRINGER CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP . 2 L 7 2 4F 4 F RT A16WE E2GL 2002120400137 20021204 00137 NM 2002 12 4 2002UALA01760 1 20021123 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 BODY STATION 727B FUSELAGE FRAME, STRINGER 4R STRINGER CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP . 2 L 7 2 4F 4 F RT A16WE E2GL 2002120400138 20021204 00138 NM 2002 12 4 2002UALA01761 1 20021123 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 BODY STATION 727C FUSELAGE FRAME, STRINGER 7R STRINGER CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP . 2 L 7 2 4F 4 F RT A16WE E2GL 2002120400139 20021204 00139 NM 2002 12 4 2002UALA01762 1 20021124 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 BODY STATION 727A FUSELAGE FRAME, STRINGER 2R STRINGER CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP . 2 L 7 2 4F 4 F RT A16WE E2GL 2002120400140 20021204 00140 NM 2002 12 4 2002UALA01763 1 20021124 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 BODY STATION 727A FUSELAGE FRAME, STRINGER 3R STRINGER CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP . 2 L 7 2 4F 4 F RT A16WE E2GL 2002120400141 20021204 00141 NM 2002 12 4 2002UALA01764 1 20021124 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 BODY STATION 727B FUSELAGE FRAME, STRINGER 3R STRINGER CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP . 2 L 7 2 4F 4 F RT A16WE E2GL 2002120400142 20021204 00142 NM 2002 12 4 2002UALA01765 1 20021124 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 BODY STATION 727B FUSELAGE FRAME, STRINGER 7R STRINGER CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP . 2 L 7 2 4F 4 F RT A16WE E2GL 2002120400143 20021204 00143 NM 2002 12 4 2002UALA01766 1 20021124 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 BODY STATION 727D FUSELAGE FRAME, STRINGER 7R STRINGER CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP . 2 L 7 2 4F 4 F RT A16WE E2GL 2002120400144 20021204 00144 NM 2002 12 4 2002UALA01767 1 20021121 A 5330 SKIN BOEING 777 777222 1385219 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 792UA 26934 FOUND DENT AT STATION 676 STRINGER 27L MEASURING 5.5 INCHES LONG BY 1.5 INCHES WIDE AND .093 INCHES DEEP. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F RT T0001SE 2002120400145 20021204 00145 NM 2002 12 4 2002UALA01768 1 20021121 A 5330 SKIN BOEING 777 777222 1385219 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 792UA 26934 FOUND DENT AT STATION 697 STRINGER 27L MEASURING 4 INCHES IN LENGTH AND 2 INCHES IN WIDTH AND .078 INCHES IN DEPTH. DEN T EXTENDS INTO CIRCUMFERENTIAL FRAME MEMBER. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2 L 7 2 4F RT T0001SE 2002121700209 20021217 00209 NM 2002 12 17 2002UALA01775 1 20021126 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 STATION 887, STRINGER 9L FUSELAGE FRAME IS CRACKED AT RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. DOUBLER MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700210 20021217 00210 NM 2002 12 17 2002UALA01776 1 20021126 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 STATION 827, STRINGER 9R, FUSELAGE FRAME CRACKED AT RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. FRAME DOUBLER MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700211 20021217 00211 NM 2002 12 17 2002UALA01777 1 20021126 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 STRINGER CLIP CRACKED AT STATION 685 STRINGER 10L AT FASTENERS. MAJOR REPAIR ACCOMPLISHED. STRINGER CLIP REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700212 20021217 00212 NM 2002 12 17 2002UALA01778 1 20021126 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 STRINGER CLIP CRACKED AT STATION 706 STRINGER 8L AT FASTENERS. MAJOR REPAIR ACCOMPLISHED. STRINGER CLIP REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700213 20021217 00213 NM 2002 12 17 2002UALA01779 1 20021126 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 CABIN FRAME AT STATION 847 ON STRINGER 9R IS CRACKED AT RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. FRAME DOUBLER INSTALLED . 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700245 20021217 00245 NM 2002 12 17 2002UALA01780 1 20021126 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 LEFT HAND FUSELAGE FRAME STATION 400 CRACKED AT STOW BIN ATTACH CLIP. MAJOR REPAIR ACCOMPLISHED. NESTED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700260 20021217 00260 NM 2002 12 17 2002UALA01781 1 20021127 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 RT AFT CABIN STATION 950 INBOARD CHORD HAS EXCESSIVE MATERIAL LOSS JUST ABOVE CABIN FLOOR. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700261 20021217 00261 NM 2002 12 17 2002UALA01782 1 20021127 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 CABIN STATION 727B STRINGER 5L CLIP CRACKED AT FASTENER. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900051 20021219 00051 2002 12 19 2002UALA01783 4 20021124 A 2213 SERVO BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RUDDER FAILED A UALA O OTHER F FLT CONT AFFECTED LD LANDING 1 WP 29 661UA 27158 DURING CAT2 AUTOLAND, AT APPROX 20-30 FT, AIRCRAFT PITCHED UP AUTOMATICALLY, THEN AT 15 FT AUTOPILOT DISCONNECTED ITSELF . CAPTAIN TOOK OVER AND MANUALLY LANDED. THERE WAS A FAILURE OF THE RT AUTOPILOT RUDDER SERVO ON THIS AIRPLANE DURING A PREVIOUS FLT. AS A RESULT, THE RT RUDDER SERVO CIRCUIT BREAKER WAS PULLED AND COLLARED AND THE AC WAS IN A CAT2 STATUS WHEN THIS EVENT OCCURRED. THE MCDP REPORTED THE AUTOPILOT DISCONNECT WAS CAUSED BY A PITCH AXIS MODE ERROR. THIS EITHE R CAN BE CAUSED BY THE PILOT OVERRIDING THE PITCH SERVO, OR THE ELEVATOR SURFACE POSITION DIFFERING FROM THE ELEVATOR SE RVO POSITION BY MORE THAN FOUR DEGREES. THE RT RUDDER SERVO AND RT FCC WERE REPLACED AND THE AC WAS RESTORED TO CAT3. 2 L 7 2 4F 4 F RT A1NM E24NE 2003022700067 20030227 00067 NM 2003 2 27 2002UALA01784 1 20021126 A 3620 WARNING SYSTEM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT MALFUNCTIONED A UALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 29 617UA 21877 RIGHT ENGINE BLEED LIGHT ILLUMINATED AND EICAS MSG. ABORTED TAKEOFF AT 110 KNOTS. ACCOMPLISHED BITE OF RIGHT PNEU SYST EM, NO FAULTS FOUND. NO MAINTENANCE ACTION TAKEN, AND NO SUBSEQUENT PROBLEMS IN RIGHT PNEUMATIC SYSTEM HAVE BEEN REPORT ED. 2 L 7 2 4F 4 F RT A1NM E3NE 2003021000058 20030210 00058 NM 2003 2 10 DHL2002743514 1 20021111 A 5754 FITTING BOEING 727 727225 1384077 NM NR 4 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, LT WING NR 4 SLAT ACTUATOR PISTON END ATTACH FITTING LOOSE FASTENERS ALSO INTERNAL ANGLES 2 EACH PLUS RI B ARE CRACKED. REMOVED NR 4 SLAT IAW B-727 M.M. 27-81-11. CUT-OUT AREA IN AFT LOWER. SKIN IAW B-727 SRM 57-50-3 AND RE MOVED 2 DAMAGED REPAIR ANGLES AND 2 RIBS IAW B-727 SRM 51-30-2. FABRICATED 2 RIBS IAW B-727 SRM 57-50-2. PARTS ALODINED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2003022800050 20030228 00050 NM 2003 2 28 DHL7432002515 1 20021124 A 5313 STRINGER BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C-CHECK, STRINGER 27 LEFT STATION 1010-1030 IS CORRODED AT FASTENER HOLES. CUT-OUT DAMAGED STRINGER BS 1010-1030 APPROXIMATELY 20 INCHES IAW B-727 SRM 53-10-3 FIG 1. FABBED NEW STRINGER AND SPLICES 2 EACH IAW B-727 SRM 53-10-3 FIG 1. INSTALLED REPAIR PARTS IAW B-727 SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2002120400147 20021204 00147 WP 2002 12 4 ARWA20021201 1 20021201 A 5610 5887276501 WINDSHIELD DOUG DC8 DC862 3021970 WP A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 1804 45896 LOG PAGE # 109140. DISCREPANCY: APPROACHING FL350, CAPTAIN'S WINDSHIELD DEVELOPED MULTIPLE CRACKS. CORRECTIVE ACTION : REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-10-2; ALSO CAPTAIN'S WINDSHIELD CONTROLLER IAW MM 30-41-1. FOUND N ORMAL OPS CHECK. 2 L 7 4 4F 4A25 2002120400148 20021204 00148 EA 2002 12 4 SWIA200211521 1 20021014 A 5315 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 364 CORRODED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 411SW 7067 FRAME AT FS 364 BETWEEN STR 25P AND 25S CORRODED BEYOND LIMITS. FOUND DURING C CHECK INSPECTION. REPLACED FRAME SECT ION IAW CRJ SRM 51-40-06, 51-40-11, 51-42-06, 51-42-21, 51-23-00. 2 L 7 2 4F RT A21EA 2002120500001 20021205 00001 NM 2002 12 5 AUS20021265 1 20021029 A 7830 001199 COWLING BOEING BOEING 737 737724 13844BY NM GE CFM56 CFM567B24 NE THRUST REVERSER LIGHTNING STRIKE W K NONE O OTHER IN INSP/MAINT 1 AU S 001199 (AUS) LT ENGINE THRUST REVERSER OUTER COWL TRAILING EDGE EXHIBITED SIGNS OF LIGHTNING STRIKE. DAMAGE EXCEEDED LIMITS. AR EAS OF DAMAGE 81MM BY 30MM BY 2MM DEEP (0.318IN BY 0.118IN BY 0.078INDEEP) AND 60MM BY 15MM BY 2MM DEEP. (0.236IN BY 0.5 9IN BY 0.078IN DEEP) 2 L 7 2 4F 4 F RT A16WE E00055EN 2002120500002 20021205 00002 NM 2002 12 5 AUS20021270 1 20021102 A 5410 TIE ROD BOEING 747 747238B 1384828 NM RROYCE RB211 RB211524D419 54555 NE NR 3 ENG COWL BROKEN W O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 AU S (AUS) NR 3 ENGINE EXPERIENCED HIGH VIBRATION LEVELS. INSPECTION FOUND A NACELLE TIE ROD BROKEN AND FOULING ON A PIPE LOC ATED ADJACENT TO THE AVM PICKUP. FAN BLADES CLEANED AND LUBRICATED AND AN ENGINE RUN CARRIED OUT. 2 L 7 4 4F 4 F A20WE E12EU 2002120500003 20021205 00003 2002 12 5 AUS20021271 4 20021102 A 2397 WIRE HARNESS BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE ENTERTAIN SYS BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) IN FLIGHT ENTERTAINMENT (IFE) SCREEN WIRING HARNESS LOCATED AT SEAT 48HJK BURNED. 2 L 7 4 4F 4 F RT A20WE E30NE 2002120500004 20021205 00004 CE 2002 12 5 AUS20021272 1 20021030 A 3213 BOLT BEECH 200 B200C 1152924 CE PWA PT6 PT6A41 52043 EA STRUT SEPARATED W O OTHER O OTHER NR NOT REPORTED 1 AU S 4265 (AUS) LT MAIN LANDING GEAR OLEO STRUT PISTON SEPARATING FROM AXLE. SHEAR BOLT HAD SHEARED AND THE PISTON HAD MIGRATED OU T BY APPROXIMATELY 25MM (0.98IN). 1 L 7 2 4T 4 T A24CE E4EA 2002120500005 20021205 00005 NE 2002 12 5 AUS20021273 2 20021101 A 7200 ENGINE BAC 146 146100A 1500260 EU LYC ALF502 ALF502R5 41580 NE NR 3 ODOR W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) FUMES ENTERING AIR CONDITIONING SYSTEM FROM NR 3 ENGINE. 2 H 7 4 4F 4 F RT A49EU E6NE 2002120500006 20021205 00006 CE 2002 12 5 AUS20021276 1 20021024 A 3221 10581002367 FRAME BEECH 76 76 1153005 CE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT MAIN LANDING GEAR ``A`` FRAME CRACKED. FOUND DURING INSPECTION IAW AD/BEECH76/18 AMDT1. 1 L 7 2 3O A29CE 2002120500007 20021205 00007 SW 2002 12 5 AUS20021278 1 20021030 A 3411 STATIC LINE SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UA 01514 WP MCAULY 4HFR34 4HFR34C652 NE PITOT/STATIC SYS CONTAMINATED W O OTHER N FALSE WARNING DE DESCENT 1 AU S (AUS) AIRCRAFT STATIC SYSTEM CONTAMINATED WITH WATER. FALSE GPWSWARNINGS DURING DESCENT. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002120500013 20021205 00013 NM 2002 12 5 AUS20021287 1 20021105 A 3242 STATOR BOEING 747 747238B 1384828 NM RROYCE RB211 RB211524D419 54555 NE BRAKE ASSY DISINTEGRATED W O OTHER F FLT CONT AFFECTED LD LANDING 1 AU S B7265 (AUS) NR 4F BRAKE STATOR DISINTEGRATED CAUSING DAMAGE TO WHEEL. 2 L 7 4 4F 4 F A20WE E12EU 2002120500014 20021205 00014 NE 2002 12 5 AUS20021289 2 20021104 A 7200 ENGINE DHAV DHC8 DHC8315 2809010 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE ENGINE (TURBINE/ OVERTORQUED W O OTHER E VIBRATION/BUFFET CR CRUISE 1 AU S (AUS) LT AND RT ENGINES AND PROPELLERS SUFFERED OVERTORQUE. ENGINE GAS GENERATOR MODULES SUFFERED OVERSPEED. CAUSED BY O PERATING INEXTREME TURBULENCE. BOTH ENGINES AND PROPELLERS REMOVED AND RETURNED TO RESPECTIVE MANUFACTURERS FOR INSPECTI ON. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002120500015 20021205 00015 EU 2002 12 5 AUS20021292 1 20021031 A 6220 365A31181004 STARFLEX 365A31001202 AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1A 60030 NE MAIN ROTOR HEAD DEBONDED W K NONE O OTHER IN INSP/MAINT 1 AU S 919 M1260 (AUS) MAIN ROTOR HEAD STARFLEX BUSHING DEBONDED. 1 G 7 2 3U 3 U RT H10EU E19EU 2002120500017 20021205 00017 NM 2002 12 5 AUS20021295 1 20021107 A 2913 5718603 PUMP BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE HYD SYSTEM OVERHEATED W C ABORTED TAKEOFF K M J FLUID LOSS OVER TEMP WARNING INDICATION TO TAKEOFF 1 AU S 186 (AUS) NR 1 HYDRAULIC PUMP OVERHEATED. 2 L 7 3 4F 4 F RT A3WE E2EA 2002120500018 20021205 00018 NM 2002 12 5 AUS20021296 1 20021107 A 2913 5718603 PUMP BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE HYD SYSTEM OVERHEATED W C ABORTED TAKEOFF K M J FLUID LOSS OVER TEMP WARNING INDICATION TO TAKEOFF 1 AU S 1 (AUS) NR 1 HYDRAULIC PUMP OVERHEATED. 2 L 7 3 4F 4 F RT A3WE E2EA 2002120500019 20021205 00019 EU 2002 12 5 AUS20021297 1 20021107 A 7797 S2401 CONNECTOR BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE ENG INDICATOR CORRODED W D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 AU S (AUS) NR 1 ENGINE N1 WIRING CONNECTOR 221-02-00 AA PIN B7 CORRODED.CONNECTOR IS LOCATED AT FORWARD PRODUCTION BREAK. 2 H 7 4 4F 4 F A49EU E6NE 2002120500020 20021205 00020 2002 12 5 AUS20021301 4 20021112 A 3442 6225130114 CONTROL PANEL BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE WX RADAR SYS FAILED W O OTHER O OTHER NR NOT REPORTED 1 AU S (AUS) WEATHER RADAR CONTROL PANEL FAULTY. 2 L 7 4 4F 4 F RT A20WE E30NE 2002120500021 20021205 00021 NM 2002 12 5 AUS20021302 1 20021112 A 2781 834503 SENSOR BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL LE SLAT FAULTY W O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 AU S (AUS) LEADING EDGE SLAT SENSOR S282 FAULTY. 2 L 7 2 4F 4 F RT A1NM E23EA 2002120500022 20021205 00022 WP 2002 12 5 AUS20021305 2 20020828 A 7310 692545XX SOLENOID CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP HARTZL HCB3T HCB3TN5 GL ENG FUEL DIST LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) LT ENGINE PRIMARY-ONLY SOLENOID LEAKING FROM VALVE BODY. 1 L 7 2 3T 4 T RT A28CE E4WE 6 C P15EA 2002120500023 20021205 00023 CE 2002 12 5 AUS20021309 1 20021031 A 5551 551006 FITTING CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO MCAULY 3AF32C 3AF32C505 GL HORIZONTAL STAB DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) HORIZONTAL STABILISER ATTACHMENT FITTING HOLES OVERSIZE. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2002120500024 20021205 00024 CE 2002 12 5 AUS20021310 1 20021031 A 5343 52130409 WEB CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO MCAULY 3AF32C 3AF32C505 GL NLG TRUNNION CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NLG TRUNNION MOUNTING WEBS CRACKED. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2002120500027 20021205 00027 EU 2002 12 5 AUS20021317 1 20021108 A 2410 5243212161 DRIVE SHAFT PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL NR 2 GENERATOR SHEARED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 AU S (AUS) NR 2 GENERATOR DRIVE SHAFT FRACTURED AT SHEAR POINT. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002120500028 20021205 00028 NM 2002 12 5 AUS20021318 1 20021107 A 2520 SEAT BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU CABIN MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) SEATS LOCATED AT ROW 10A AND 10F PARTIALLY BLOCKING EMERGENCY EXITS. PERSONNEL/MAINTENANCE ERROR. 2 L 7 2 4F 4 F RT A16WE E21EU 2002120500033 20021205 00033 NM 2002 12 5 AUS20021324 1 20021114 A 2721 233T620121 CONTROL PANEL BOEING 767 767338 1385151 NM GE CF6 CF680C2* GL RUDDER TAB FAULTY W O OTHER F FLT CONT AFFECTED DE DESCENT 1 AU S D00416 (AUS) RUDDER TRIM CONTROL PANEL SUSPECT FAULTY. 2 L 7 2 4F 4 F RT A1NM E23EA 2002120500039 20021205 00039 CE 2002 12 5 AUS20021332 1 20021118 A 3297 P270D8 WIRE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA MLG C/B LOOSE W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LANDING GEAR CONTROL CIRCUIT BREAKER WIRE P270D8 LOOSE. 2 L 7 2 4T 4 T RT A24CE E4EA 2002120500040 20021205 00040 2002 12 5 AUS20021334 4 20021120 A 3416 A79000182 HOSE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE ALTIMETER FRACTURED W K NONE O OTHER IN INSP/MAINT 1 AU S 2880 (AUS) STANDBY ALTIMETER STATIC PRESSURE HOSE KINKED AND FRACTURED. PERSONNEL/MAINTENANCE ERROR. 2 L 7 2 4F 4 F RT A28NM E29NE 2002120500041 20021205 00041 NM 2002 12 5 AUS20021336 1 20021119 A 3810 COOLER BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE R5 TOILET BLOCKED W O OTHER M J OVER TEMP WARNING INDICATION DE DESCENT 1 AU S (AUS) R5 TOILET WATER COOLER OVERHEATED DUE TO AIRFLOW BLOCKAGE. 2 L 7 4 4F 4 F RT A20WE E30NE 2002120500043 20021205 00043 EU 2002 12 5 AUS20021338 1 20021115 A 7603 CABLE BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502* 41580 EA POWER LEVER CHAFED W D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 AU S (AUS) NR 4 THROTTLE LEVER CABLE FOULING ON CENTER ROOF PANEL. PREVIOUS MAINTENANCE HAD BEEN CARRIED OUT FOR BATTERY PACK REPLACEMENT. PERSONNEL/MAINTENANCE ERROR. 2 H 7 4 4F 4 F RT A49EU E6NE 2002120500044 20021205 00044 EU 2002 12 5 AUS20021339 1 20021114 A 6220 365A31188901 STOP UROCOP AS350BASSY SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR HEAD CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) MAIN ROTOR HEAD SPHERICAL STOP CORRODED. FOLLOWING STRIPPING OF THE PAINT, FURTHER INSPECTION FOUND A CRACK ORIGIN ATING FROM THERADIUS LOCATED ON THE REAR SIDE WHICH EXTENDED AROUND HALF OF THE OUTER SIDE. 1 G 7 1 3U 3 U H9EU E19EU 2002120500045 20021205 00045 EU 2002 12 5 AUS20021340 1 20021111 A 6510 365A33621300 COUPLING AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1A 60030 NE TAIL ROTOR DRIVE CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) TAIL ROTOR DRIVESHAFT REAR FLEXIBLE COUPLING CRACKED. 1 G 7 2 3U 3 U RT H10EU E19EU 2002120500050 20021205 00050 NM 2002 12 5 AUS20021346 1 20021120 A 2612 WARNING LIGHT BOEING 737 737476 NM CFMINT CFM56 CFM563C 13802 EU APU FALSE ACTIVATION W F D ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 AU S (AUS) APU FIRE WARNING. FIRE BOTTLE DISCHARGED. INSPECTION FOUND NO EVIDENCE OF FIRE. 2 L 7 2 4F 4 F RT A16WE E21EU 2002120500052 20021205 00052 EU 2002 12 5 AUS20021350 1 20021122 A 3520 117019020304 GENERATOR AIRBUS 320 A320* EU CFMINT CFM56 CFM565A1 NE PAX OXYGEN FAULTY W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S 2880 (AUS) CABIN OXYGEN GENERATORS (48 OUT OF 56) HAD THE LANYARD PIN INCORRECTLY FITTED INTO THE TRANSPORT HOLE OF THE OXYGE N GENERATOR FIRING PINS INSTEAD OF THE CORRECT LANYARD PIN HOLE.PERSONNEL/MAINTENANCE ERROR. 2 L 7 2 4F 4 F RT A46NM E29NE 2002120500054 20021205 00054 NM 2002 12 5 AUS20021354 1 20021119 A 2121 6054577 FAN BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE AIR DISTRIBUTION FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AU S (AUS) GASPER FAN FAILED. 2 L 7 2 4F 4 F RT A1NM E3NE 2002120500057 20021205 00057 SW 2002 12 5 AUS20021359 1 20021123 A 3411 STATIC LINE SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UHR WP MCAULY 4HFR34 4HFR34C652 NE PITOT/STATIC SYS CONTAMINATED W O OTHER J WARNING INDICATION DE DESCENT 1 AU S (AUS) STATIC LINE TO AIR DATA COMPUTER CONTAMINATED WITH WATER. EGPWS GAVE FALSE READINGS. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2002120500058 20021205 00058 NE 2002 12 5 AUS20021360 2 20021125 A 7250 BEARING BOEING 737 737724 13844BY NM GE CFM56 CFM567B24 NE NR 2 ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 2 ENGINE CHIP DETECTOR CONTAMINATED. CONTAMINATION IDENTIFIED AS M50 MATERIAL. SUSPECT NR 3 BEARING FAILURE. 2 L 7 2 4F 4 F RT A16WE E00055EN 2002120500059 20021205 00059 NE 2002 12 5 CA021022002 2 20021018 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT LEAKING W A UNSCHED LANDING N B FALSE WARNING SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) 'FLIGHT RETURN DUE TO SMOKE IN CABIN' PASSENGERS DISEMBARKED ON THE RUNWAY AND PARAMEDICS CALLED. FOUND RT DUCTS A ND WATER SEPARATOR HOUSING STILL REQUIRED SOME CLEANING. REPLACED RIGHT WATER SEPARATOR SOCK AND CLEANED DUCTS BETWEEN ACM & SEPARATOR. INSPECTED DISTRIBUTION BOX FOR CONTAMINATION. NONE FOUND. DURING GROUND RUNS VERY STRONG OIL SMELL IN THE CABIN (LIKE VOMIT) AND SMOKE. DETERMINED TO BE COMING FROM THE RT ENGINE. APU AND LT ENGINE WAS FINE.OIL FOUND EM INATING FROM THE IGVS. REPLACED RIGHT ENGINE. RAN RT PACK FROM APU TO EXPEL ODOR. COMPLIED WITH OVERWEIGHT LANDING CHE CK. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120500064 20021205 00064 EU 2002 12 5 CA021023005 1 20021021 A 2121 C209690D FAN SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE COCKPIT FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) THE AIRCRAFT LANDED AND WAS IN THE PROCESS OF UNLOADING WHEN THE FLIGHT ATTENDANT NOTED AN ELECTRICAL ODOR IN THE CABIN. THE REMAINING PASSENGERS EXITED THE AIRCRAFT AS INSTRUCTED AND THE PILOTS ALERTED TO A POSSIBLE PROBLEM. AT ABOU T THE SAME TIME AFTER ENGINE SHUTDOWN, THE FLIGHT CREW NOTED THAT THE FLIGHT DECK RECIRCULATION FAN CIRCUIT BREAKER HAD POPPED. THE FLIGHT CREW INVESTIGATED AND OBSERVED A STRONG ELECTRICAL ODOR IN THE FLOOR AREA ADJACENT TO THE FAN LOCATIO N. MAINTENANCE INSPECTION OF THE AIRCRAFT CONFIRMED THAT THE RECIRC FAN HAD INDEED FAILED. THE FAN ASSY WAS REPLACED. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002120500065 20021205 00065 EA 2002 12 5 CA021023007 1 20021018 A 2730 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE HORIZONTAL STAB FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA (CAN) SHORTLY AFTER AIRBORNE, STAB & MACH TRIM DISCONNECTED. RE-ENGAGED SUCCESSFULLY, BUT WOULD DICONNECT AGAIN SHORTLY AFTER.(30SEC) HORIZ STAB TRIM CONTROL UNIT DISPLAYED 'MOTOR 1''CHANNEL 1' FAILED MESSAGE. UNIT REPLACED 2 L 7 2 4F 4 F RT A21EA E15NE 2002120500066 20021205 00066 EA 2002 12 5 CA021023008 1 20021019 A 5210 601R3807413 FITTING CNDAIR CL6002B19 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE PAX DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 7376 (CAN) DURING OVERNIGHT CHECK, MAINTENANCE FOUND AFT ANCHOR FITTING OF PASSENGER DOOR COUNTER BALANCE MECHANISM CRACKED I N MIDDLE OF BRACKET. BRACKET REPLACED. IPC REF 52-11-17 FIG.2 ITEM 395. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120500067 20021205 00067 SW 2002 12 5 CA021024006 1 20021022 A 2730 27K44062003 CONTROL CABLE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP ELEVATOR BROKEN W O OTHER F FLT CONT AFFECTED LD LANDING 1 CA (CAN) ON SHORT FINAL A NOTICABLE CHANGE IN THE ELEVATOR CONTROL WAS REPORTED BY THE CREW. THE AIRCRAFT LANDED WITHOUT IN CIDENT. A SUBSEQUENT INSPECTION REVEALED THAT THE ELEVATOR DOWN SPRING CABLE HAD BROKEN AT THE PULLEY LOCATEDAT WL 138.7 6. THE PULLEYS AND FAIRLEADS WERE INSPECTED WITH NO DEFECTS FOUND. 2 L 7 2 4T 4 T RT A8SW E4WE 2002120500068 20021205 00068 EA 2002 12 5 CA021025003 1 20021024 A 5610 601R3303312 WINDOW CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COCKPIT CRACKED W O OTHER O OTHER AP APPROACH 1 CA (CAN) FIRST OFFICER'S SIDE WINDOW CRACKED (INNER PANE) DURING CRUISE ENROUTE . WINDOW WAS REMOVED AND REPLACED WITH SERV ICABLE COMPONENT. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002120500069 20021205 00069 EA 2002 12 5 CA021025004 1 20021017 A 5610 601R3303312 WINDOW CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COCKPIT CRACKED W O OTHER O OTHER DE DESCENT 1 CA (CAN) FIRST OFFICER'S SIDE WINDOW CRACKED (INNER PANE) DURING DESCENT . WINDOW WAS REMOVED AND REPLACED WITH SERVICABLE COMPONENT. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002120500070 20021205 00070 EA 2002 12 5 CA021025005 1 20021016 A 5610 601R3303311 WINDOW CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COCKPIT CRACKED W O OTHER O OTHER AP APPROACH 1 CA (CAN) CAPTAIN SIDE WINDOW CRACKED DURING DESCENT . WINDOW WAS REMOVED AND REPLACED WITH SERVICABLE COMPONENT. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002120500071 20021205 00071 EA 2002 12 5 CA021025006 1 20021021 A 5610 NP1393212 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT FAILED W D RETURN TO BLOCK D INFLIGHT SEPARATION TX TAXI/GRND HDL 1 CA 14898 (CAN) AIRCRAFT 7046 TAT = 18805.9 HOURS.FLIGHT 5539 FROM CVG TO MKE.R. WINDSHIELD SHATTERED ON TAXI OUT. INSTALLED REPLA CEMENT WINDSHIELD 2 L 7 2 4F 4 F RT A21EA E15NE 2002120500072 20021205 00072 NE 2002 12 5 CA021028001 2 20021023 A 7230 MODULE33 COMPRESSOR BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 1 FAILED W A UNSCHED LANDING D R J INFLIGHT SEPARATION PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) AIR RETURN AFTER THE NR 1 ENG ON AC 712 SURGED AS THE AC WAS CLIMBING THROUGH FL130, ENG SUFFERED 4 LOUD BANGS WIT H ALL ENG PARAMETERS DROPPING. PILOT RETARDED NR 1 THROTTLE TO THE IDLE. PILOT RETURNED TO ATLANTA WITH ENGINE AT IDLE THROUGHOUT REMAINDER OF FLT. MCD INSPECTED WITH NO DEBRIS NOTED. LOWER LT CORE FAIRING REMOVED AND INSPECTION OF VIGV A ND VSV SYSTEM REVEALED ONE OFF STAGE 1 VSV LEVER ARM FAILED AT UNISON RING. BORESCOPE INSPEC WAS PERFORMED WITH NO DAMA GE NOTED UNTIL REACHING HPC STAGE 5 AND 6 ACCESS. WITH BORESCOPE LOOKING AFT, DAMAGE WAS SEEN AT STAGE 6 STATOR VANE T/E AND STAGE 6 BLADE L /E. NO FURTHER DAMAGE WAS NOTED IN HPC OR THE HPT. ENG REMOVED AND ROUTED TO RRC. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002120500073 20021205 00073 NM 2002 12 5 02FDEA00723 1 20021010 A 2781 SWITCH BOEING 727 727200 138407E NM L/E SLAT FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 266FE 21672 DURING FLAP RETRACTION FROM 2 DEG TO UP (NR 6 LE FLAP) NR 6 LED REMAINED AMBER, NO ADVERSE ROLL NOTED. REMOVED AND REPL ACED NR 6 LEADING EDGE FLAP POSITION INDICATOR SWITCH PER MAINTENANCE MANUAL 27-82-001-4. OPERATIONAL CHECKS GOOD. 2 L 7 3 4F RT A3WE 2002120500074 20021205 00074 NM 2002 12 5 02FDEA00755 1 20021023 A 5280 DOOR SEAL BOEING 727 727200 138407E NM NLG DEFECTIVE A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 279FE 22346 ON APPROACH TO CID-EXTENDED LAND GEAR, NOSE DOOR AMBER LT ON S/O PANEL & RED DOORS LIGHT ON. ELECTED TO DO MISS APPROAC H & RECYCLE GEAR. LT WENT OUT. ON RE-EXTENSION RED GEAR DOOR LT WENT OUT. BELOW 200 KTS ON RECYCLE. CHECKED QRH. NO OTHER PROBLEM. FOUND NOSE GEAR DOORS BINDING ON FRONT DOOR SEAL REPLACED SEAL PER M/M 32-22-001-5. CHECKS OK. 2 L 7 3 4F RT A3WE 2002120500075 20021205 00075 WP 2002 12 5 02FDEA00756 1 20021022 A 3234 CONTROL HANDLE DOUG DC10 DC1030 3023501 WP COCKPIT DIRTY A FDEA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 25 303FE 46802 ON GEAR EXTENSION DURING FINAL APPROACH ALL FOUR L/G INDICATORS STAYED RED, SYSTEM DISPLAY SHOWED ALL RED ALSO. RECYCLE D GEAR HANDLE - NORMAL EXTENSION. FOUND THAT WHEN LANDING GEAR HANDLE IS PULLED OUT THAT THE HANDLE WILL NOT FULLY RETU RN TO THE STOWED POSITION REMAINING IN THE TEST POSITION. A SLIGHT TAP ON THE GEAR HANDLE EXTINGUISHES ALL OF THE GEAR INDICATION LIGHTS. CLEANED DUST AND LINT FROM GEAR HANDLE SLIDE AND GEAR HANDLE SWITCH S1-431 PER SMP. GEAR HANDLE NO W OPERATES SMOOTHLY AND STOWS FULLY EACH TIME. TESTS NORMAL IAW M/M 32-60-00-5. 2 L 7 3 4F A22WE 2002120500076 20021205 00076 NM 2002 12 5 02FDEA00757 1 20021023 A 3244 ACG74531 TIRE DOUG MD11 MD11 3023602 NM NLG DAMAGED A FDEA K NONE D E INFLIGHT SEPARATION VIBRATION/BUFFET CL CLIMB 1 SO 25 613FE 48749 AFTER T/O GEAR RETRACTED- NLG MADE LOUD ROTATIONAL NOISE WITH STRONG VIBRATION. PRESSURE 196/199. UP INDICATION OK. F OUND RT NOSE TIRE DAMAGE, (MISSING CORD). R&R RT NOSE TIRE AS REQUIRED. 2 L 7 3 4F RT A22WE 2002120500077 20021205 00077 EU 2002 12 5 02FDEA00758 1 20021022 A 7830 CONNECTOR AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER INSTALLED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TO TAKEOFF 1 SO 25 678FE 6072 792 NR 1 ENG THRUST REV PRESSURIZED ON T/O. BROUGHT NR 1 TO IDLE PER ECAM & QRH AND RETURNED TO MEM. FOUND CANNON PLUGS CO NNECTED TO DPV PRESSURE SWITCH AND SOLENOID TO BE CONNECTED. DISCONECTED CANNON PLUGS AND CONNECTED TO STORAGE BRACKETS . OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2002120500078 20021205 00078 EU 2002 12 5 02FDEA00771 1 20021027 A 2612 FIRE LOOP AIRBUS 300 A300F4605R 3930327 EU NR 1 ENGINE OUT OF POSITION A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 668FE 772 ON CLIMB OUT NR 1 FIRE WARN/BELL WARN LT RET'D THROTTLE AND WARN STOPPED. COMPLETED FIRE S/D CKLIST AND RTO TO MEM FOR LD. LT & BELL EXT WHEN THROTTLE RTO, BUT ACTIVATED WHEN THROTTLE ADVANCED. INSP FIRE LOOPS NR 1 ENG FOUND LOOP MAKING PHYSICAL CONTACT WITH PNEUMATIC DUCT. FOUND HYD RESERVOIR HOSE CHAFED, CONTACT WITH LOOP SECT DH4. REPOSITIONED DH4 LO OP, REPLACED HYD RESERVOIR PRESS LINE IAW A300 MM 20-23-12-0. NO ENG RUN, CLOSED COWLS PER IAW A300 MM 71-13-00-3F. RA N ENG PER IAW JRH6-10 POWER ASSURANCE RUN FOR 5 MINS & 73 PERCENT WITH HP OPEN FOR 5 MINS & TAXI TO HIGH POWER RUN PAD, CND, OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2002120500079 20021205 00079 2002 12 5 DL72S021264 4 20021030 A 3442 20671570153 TRANSCEIVER BOEING 727 727232 1384082 NM WEATHER RADAR MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 516DA 21432 ATB, WX RADAR C/B POPPED TWICE. REPLACED WX RADAR R/T TEST PATTERN NORMAL - OPERATED IN WX MOD OBTAINED TARGETS, ALL OP S NORMAL. 2 L 7 3 4F A3WE 2002120500080 20021205 00080 NM 2002 12 5 DL72S021297 1 20021106 A 3350 900835A BATTERY PACK BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 8890Z 21859 2 EMERGENCY EXIT LIGHTS MID CABIN OVERHEAD EXIT SIGNS INOP. REPLACED POWER SUPPLY AND BATTERY PACK, CKS OK. 2 L 7 3 4F RT A3WE 2002120500081 20021205 00081 NM 2002 12 5 DL72S021342 1 20021119 A 5320 WEB BOEING 727 727225A 1384077 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 FOUND ON C-1 LETTER CK, CRACK ON LT VERTICAL WEB STA 1233 AND 1218. REPAIRED PER SRM 51-40-2. 2 L 7 3 4F RT A3WE 2002120500082 20021205 00082 NM 2002 12 5 QXEA0202083 1 20021202 A 3260 SENSOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 OUT OF RIG A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 403QX 4037 BOI - DURING CLIMBOUT, THE GEAR CYCLED MOMENTARILY. THE CREW SAW THE LAEFT AND RIGHT MAIN GEAR DOOR LIGHTS FLASH AND HEA RD THE GEAR LOCK BACK INTO THE UP POSITION. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-RIGGED THE MAIN LANDING GEAR DOOR PROX SENSOR. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REP LACED. 2 H 7 2 4T RT A13NM 2002120500083 20021205 00083 NM 2002 12 5 DL72W021270 1 20021031 A 3350 KD4A017 RELAY BOEING 727 727247 138408F NM CABIN FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 EMERGENCY LIGHT REMAINS ON IN THE ARM POSITION. REPLACED R600, CKS OK. 2 L 7 3 4F A3WE 2002120500084 20021205 00084 EU 2002 12 5 DHL2002362501 1 20021009 A 5730 SKIN AIRBUS 300 A300B4203 3930306 EU RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 RT WING BOTTOM SKIN BETWEEN RIB 1 & 2, CENTER AND AFT SPAR, CORROSION FOUND. REMOVED CORROSION IAW A300 SRM 51-40-11, N DT AREA IAW NTM 51-31-05, NO CRACKS FOUND, THICKNESS CHECKED AREA PER NTM 51-20-00, 5 PERCENT LOSS OF MATERIAL, AREA FOU ND TO BE IN LIMITS IAW A300 SRM 57-33-11. 2 L 7 2 4F RT A35EU 2002120500086 20021205 00086 NM 2002 12 5 CALA0200572 1 20021203 A 5230 SKIN BOEING 777 777224 1385225 NM FWD CARGO DR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78002 27578 INSPECTION FOUND FORWARD CARGO DOOR EXTERNAL SKIN DENTED AT FORWARD LOWER CORNER BELOW PANEL 821CR. THE DOOR SKIN WAS RE PAIRED IAW ECRA 5230-01702. A DIP WAS ISSUED TO REINSPECT THE REPAIR AT INTERVALS NOT TO EXCEED 30000 FLIGHT CYCLES. 2 L 7 2 4F RT T00001SE 2002120500087 20021205 00087 EU 2002 12 5 DHL2002362510 1 20021025 A 5230 A5237407820200 DOOR FRAME AIRBUS 300 A300B4203 3930306 EU CARGO DOOR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 AFT LOWER CARGO DOOR EXTERNAL LOWER CORNER HAS CORROSION INSIDE FRAME. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. RE MOVED, DRILLED LOWER AFT CORNER SKIN IAW A300 SRM 51-30-30. INSTALLED IAW A300 SRM 51-30-30. 2 L 7 2 4F RT A35EU 2002120500089 20021205 00089 NM 2002 12 5 02FDEA00800 1 20021105 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 DENT ON FRAME AT STR 23R ASSOCIATED WITH E&E CATWALK. REPAIRED FRAME IAW SRM 51-40-3. 2 L 7 3 4F RT A3WE 2002120500090 20021205 00090 NM 2002 12 5 02FDEA00802 1 20021106 A 2782 ACTUATOR BOEING 727 727200 138407E NM L/E SLAT LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 208FE 22930 AFTER T/O, LOST A SYSTEM HYDRAULICS. PERFORMED CHECKLISTS AND RED TAB PROCEDURES. DECLARED EMERGENCY, CALLED MOCC. AF TER SLAT ACTUATOR CHANGE PER 27-80-6282 SERVICED HYD SYS PER MM 12-12-000-3. OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2002120500091 20021205 00091 EU 2002 12 5 02FDEA00804 1 20021105 A 5753 A5796351 SKIN AIRBUS 300 A300F4605R 3930327 EU T/E FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 667FE 771 RT I/B UPPER FLAP HAS 2 CHAFE MARKS 0.009 & 0.011 DEEP, 1.5 INCHES APART 77 INCHES FROM I/B SIDE. R/R FLAP. 2 L 7 2 4F RT A35EU 2002120500092 20021205 00092 NM 2002 12 5 02FDEA00805 1 20021107 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 CORROSION ON STR 29L, BS 1000 TO 1018. R&R STRINGER PER EO 7-5310-7-2356. 2 L 7 3 4F RT A3WE 2002120500093 20021205 00093 NM 2002 12 5 02FDEA00806 1 20021107 A 5314 KEELBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 CORROSION ON KEELBEAM BS 1000, STR 29L. R&R KEELBEAM PER EO 7-5310-7-2356. 2 L 7 3 4F RT A3WE 2002120500094 20021205 00094 NM 2002 12 5 02FDEA00807 1 20021106 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 DENT IN ETERNAL FUSELAGE SKIN AT BS 1045 JUST BELOW STR 20L. R&R SKIN PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 2002120500095 20021205 00095 WP 2002 12 5 02FDEA00808 1 20021108 A 5210 L30825601 MOTOR DOUG DC10 DC1010 3022110 WP R1 DOOR FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 R-1 DOOR PNEU DRIVE MOTOR FAILED EMERGENCY ACTUATION TEST (SPLINE SHAFT SEPARATED FROM MOTOR). 2 L 7 3 4F A22WE 2002120500096 20021205 00096 NM 2002 12 5 02FDEA00814 1 20021029 A 5753 ARC2512504 BUSHING DOUG MD11 MD11 3023602 NM T/E FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING BUSHINGS ON INBD FLAP OUTBD HINGE FITTING WERE FOUND WORN AFTER FLAP REMOVAL. R&R HINGE BRACKET PER EA 1-5750-6 5921. 2 L 7 3 4F RT A22WE 2002120500097 20021205 00097 NM 2002 12 5 02FDEA00815 1 20021101 A 5753 ARC2512503 BUSHING DOUG MD11 MD11 3023602 NM T/E FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING INBD FLAP OUTBD FAIRING HINGE BUSHINGS WORN. R&R HINGE BRACKET PER EA 1-5750-65924. 2 L 7 3 4F RT A22WE 2002120500098 20021205 00098 NM 2002 12 5 02FDEA00816 1 20021111 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 CORROSION ON FRAME BS 420, STR 23R. R&R FRAME PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2002120500099 20021205 00099 NM 2002 12 5 02FDEA00817 1 20021101 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 CORROSION ON SHEAR TIE AT BS 720C+1 BETWEEN STR 18L - 28R. R&R SHEAR TIE PER SRM 51-30-2, 51-20-1. 2 L 7 3 4F RT A3WE 2002120500100 20021205 00100 NM 2002 12 5 02FDEA00818 1 20021107 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 CORROSION ON FLOORBEAM LOWER CHORD BS 1070, RBL 46, WL 200. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 8. 2 L 7 3 4F RT A3WE 2002120500101 20021205 00101 NM 2002 12 5 02FDEA00819 1 20021110 A 5320 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 STRINGER CLIP CRACKED AT BS 660, STR 1. REMOVED CRACKED STR CLIP, INSTALLED NEW STR CLIP AT BS 660 STR 1 IAW SRM 51-30- 2. 2 L 7 3 4F RT A3WE 2002120500102 20021205 00102 NM 2002 12 5 02FDEA00820 1 20021110 A 5320 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 STRINGER CLIP CRACKED BS 680, STR 10R. R&R STR CLIP BS 680, STR 10R IAW SRM 51-30-2, 51-30-5 FEDEX MM 51-20-151-7. 2 L 7 3 4F RT A3WE 2002120500103 20021205 00103 NM 2002 12 5 02FDEA00821 1 20021108 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 CORROSION ON FRAME BS 720E, STR 27R TO 28R. R&R FRAME PER SRM 53-10-4 FIG 11. 2 L 7 3 4F RT A3WE 2002120500104 20021205 00104 NE 2002 12 5 2002F01043 2 20020809 A 7230 BLADE BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE ERODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7645U 20039 649495 AT C-CHECK, FOUND NR 3 ENGINE C-1 DISK BLADES DAMAGED AT LEADING EDGES. (M) 2 L 7 3 4F 4 F A3WE E2EA 2002120500105 20021205 00105 WP 2002 12 5 2002F01044 1 20020525 A 5320 2929348 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSLEAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND MAIN CABIN FLOOR SUPPORT CORRODED AT STATION 840, RBL 31. (M) 2 L 7 3 4F A22WE 2002120500106 20021205 00106 WP 2002 12 5 2002F01045 1 20020513 A 5347 604498 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND FORWARD CARGO COMPARTMENT, MAIN SEAT TRACK HAS CORROSION AS VIEWED FROM FORWARD CARGO COMPARTMENT, AT STATION 791 TO 833, RBL 9. (M) 2 L 7 3 4F A22WE 2002120500107 20021205 00107 WP 2002 12 5 2002F01046 1 20020508 A 5230 AFA3953 HINGE DOUG DC10 DC1010 3022110 WP CARGO DOOR CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION ON AFT CARGO DOOR FUSELAGE HINGE. (M) 2 L 7 3 4F A22WE 2002120500108 20021205 00108 WP 2002 12 5 2002F01047 1 20020513 A 5320 ADA7603 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND TWO FLOOR SUPPORT AND GUSSETS CORRODED, AT STATION 824-833 BL 0. (M) 2 L 7 3 4F A22WE 2002120500109 20021205 00109 WP 2002 12 5 2002F01048 1 20020525 A 5345 AGA32851 MOUNT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND GALLEY SERVICE TIE DOWN RETRACTABLE POST SUPPORT MOUNT CORRODED, AT STATION 815, RBL 95. (M) 2 L 7 3 4F A22WE 2002120500110 20021205 00110 WP 2002 12 5 2002F01049 1 20020509 A 5320 INTERCOSTAL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND CORROSION IN AFT CARGO BAY ON LOWER SURFACE OF INTERCOSTAL AT STATION 1787, APPROXIMATELY SIX INCHES B ELOW FLOOR LEVEL, BETWEEN STRINGER 45L AND 48L. (M) 2 L 7 3 4F A22WE 2002120500111 20021205 00111 WP 2002 12 5 2002F01050 1 20020523 A 5320 WEB DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND AFT LAVATORY GALLEY AREA WEB WITH EXFOLIATED CORROSION, AT STATION 1964, LBL 19 TO 31. (M) 2 L 7 3 4F A22WE 2002120500112 20021205 00112 WP 2002 12 5 2002F01051 1 20020522 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572RY 46977 AT C-CHECK, FOUND MAIN CABIN FLOOR SUPPORT CORRODED, AT STATION 840, LBL 48. (M) 2 L 7 3 4F A22WE 2002120500113 20021205 00113 NM 2002 12 5 2002F01052 1 20020703 A 5320 65453132 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 950C, RIGHT SIDE AT STRINGER 8R. (M) 2 L 7 3 4F A3WE 2002120500114 20021205 00114 NM 2002 12 5 2002F01053 1 20020703 A 5320 65453132 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 950C, RIGHT SIDE AT STRINGER 5R. (M) 2 L 7 3 4F A3WE 2002120500115 20021205 00115 NM 2002 12 5 2002F01054 1 20020703 A 5320 65453132 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 950C, RIGHT SIDE AT STRINGER 4R. (M) 2 L 7 3 4F A3WE 2002120500116 20021205 00116 NM 2002 12 5 2002F01055 1 20020703 A 5320 65453132 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 950C, RIGHT SIDE AT STRINGER 2R. (M) 2 L 7 3 4F A3WE 2002120500117 20021205 00117 NM 2002 12 5 2002F01056 1 20020702 A 5320 STRUCTURE BOEING 727 727222 1384073 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND CORROSION AT STATION 876, STRINGER 10R, BETWEEN STRINGER AND SKIN. (M) 2 L 7 3 4F A3WE 2002120500118 20021205 00118 NM 2002 12 5 2002F01057 1 20020703 A 5320 65453136 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 950A, RIGHT SIDE AT STATION 7R. (M) 2 L 7 3 4F A3WE 2002120500119 20021205 00119 2002 12 5 A6WA200230015 4 20020811 A 3140 DAU DORNER DO32 DO328100 2996000 NM E/E BAY MALFUNCTIONED A A6WA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 330MX 3067 ENGINE MISCOMPARE MESSAGE ON TAKEOFF WITH NO OBVIOUS ENGINE PROBLEMS. ABORTED TAKEOFF. MAINTENANCE RERACKED DAU NR 1 A ND NR 2, CREW PERFORMED ENGINE RUN UP. OPS CHECK GOOD, NO MESSAGE NOTED. (M) 2 H 7 2 4T RT A45NM 2002120500120 20021205 00120 EA 2002 12 5 A6WA200240026 1 20020813 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 ENGINE LACK OF LUBE A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 417AW 7610 ABORTED TAKEOFF IDG NR 2 CAUTION MESSAGE. MAINTENANCE SERVICED NR 2 IDG. (M) 2 L 7 2 4F RT A21EA 2002120500121 20021205 00121 NM 2002 12 5 AALA20020133 1 20020131 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 645AA 24603 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 34 DEF INOPERATIVE. SECURED EMERGENCY EXIT LIGHT HOLDER AT SEAT 34 DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500122 20021205 00122 NM 2002 12 5 AALA20020147 1 20020214 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 605AA 27056 MIA - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY SEAT PATH LIGHTING AT SEAT 26D INOPERATIVE. RE-PINNED PLUG ON SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500123 20021205 00123 NM 2002 12 5 AALA20020296 1 20020312 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 605AA 27056 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT ROW 25 THROUGH 34 INOPERATIVE. REPAIRED WIRE ON EME RGENCY EXIT PATH LIGHTING AT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500124 20021205 00124 NM 2002 12 5 AALA20020320 1 20020316 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 607AM 27058 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 34 INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500125 20021205 00125 NM 2002 12 5 AALA20020509 1 20020420 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 183AN 29593 DFW - FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT LEFT AND RIGHT SERVICE DOORS. REPLACED BATTERY PACK AND MODULE AT R2 D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500126 20021205 00126 NM 2002 12 5 AALA20020514 1 20020420 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 183AN 29593 DFW - LEFT AND RIGHT EMERGENCY LIGHTS AND EMERGENCY EXITS ARE INOPERATIVE. REPLACED BATTERY PACK AND MODULE AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500127 20021205 00127 NM 2002 12 5 AALA20020546 1 20020425 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 676AN 29426 MIA - FOUND EMERGENCY ESCAPE PATH LIGHTING STRIP ALONG RIGHT SIDE FROM SEAT 4E TO 6E INOPERATIVE. SECURED LOOSE CONNECT OR ON EMERGENCY PATH LIGHTING STRIP UNDER SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500128 20021205 00128 NM 2002 12 5 AALA20020553 1 20020429 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY LIGHT ON SEAT 6E INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500129 20021205 00129 NM 2002 12 5 AALA20020554 1 20020428 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 183AN 29593 DFW - AFT LAVATORY EMERGENCY PATH FLOOR TRACK EXIT MARKER LIGHT OUT. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NO RMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500130 20021205 00130 NM 2002 12 5 AALA20020585 1 20020502 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 639AA 24597 DFW - FOUND SEAT MOUNTED EMERGENCY LIGHT AT 32D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT 32D. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500131 20021205 00131 NM 2002 12 5 AALA20020642 1 20020511 A 2450 TERMINAL BLOCK BOEING 757 757223 1384957 NM E/E BAY DEFECTIVE A AALA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 172AJ 32400 BOS - FLT 1044 - ON TAXI-IN, SEVERAL COMPONENTS ON LEFT BUS ARE INOPERATIVE. REPLACED TERMINAL BLOCK AND TERMINAL ENDS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500132 20021205 00132 2002 12 5 AALA20020643 4 20020512 A 3442 RECEIVER BOEING 757 757223 1384957 NM WEATHER RADAR INOPERATIVE A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 7667A 25301 MIA - FLT 860 - EN ROUTE MIA-LGA, AIRCRAFT INTERRUPTED BACK TO MIA DUE TO WEATHER RADAR INOPERATIVE. REPLACED WEATHER R ECEIVER PER MM. ACCOMPLISHED ADJUSTMENT AND TEST PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500133 20021205 00133 NM 2002 12 5 AALA20020897 1 20020615 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 638AA 24596 DFW - FOUND EMERGENCY LIGHTS ON SEAT SIDE PANELS IN FIRST CLASS ARE DIM. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENC Y LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500134 20021205 00134 NM 2002 12 5 AALA20020931 1 20020624 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 618AA 24526 DFW - FOUND EMERGENCY LIGHTING INOPERATIVE AT ROW 32. RECONNECTED LOOSE ELECTRICAL PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500135 20021205 00135 NM 2002 12 5 AALA20021126 1 20020806 A 3350 LEAD BOEING 757 757223 1384957 NM CABIN CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 609AA 27447 SFO - RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CORROSION OFF OF GROUND LEAD OF LAMP HOUSING. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002120500136 20021205 00136 NM 2002 12 5 GAIA02099OP 1 20020828 A 3350 1000679 LIGHT BOEING 727 727251 138408H NM CABIN INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 252US 19971 DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE CABIN EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND R EPLACED THE CABIN EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002120500137 20021205 00137 WP 2002 12 5 GTIA020744 1 20020626 A 2910 HYDRAULIC LINE DOUG DC9 DC981 3022081 WP HYD SYSTEM LEAKING A GTIA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 810NK 48015 DTW - FOUND RUDDER POWER CONTROL VALVE LINE, TO T-FITTING JUST FORWARD OF HYDRAULIC FILTERS IN TAIL SECTION RIGHT SIDE I S LEAKING. INSTALLED TEMP FLEX LINE, DEFECTIVE LINE IS REMOVED. PLACED TEMP FLEX LINE ON C/O 38818-2. REMOVED TEMPORA RY FLEX LINE AND REPLACED WITH RIGID LINE. (M) 2 L 7 2 4F A6WE 2002120500138 20021205 00138 WP 2002 12 5 GTIA020911 1 20020724 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND DENT FS 236 BETWEEN LONGERONS 6L AND 7L REQUIRES REPAIR. REWORKED DENT. FABRICATED REPAIR DOUBLER. INSTAL LED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2002120500139 20021205 00139 WP 2002 12 5 GTIA020912 1 20020724 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND E/E BAY LONGERON 24L AT STATION 200 HAS EXFOLIATION/CRACK WHERE CAP IS FASTENED TO LONGERON. REMOVED DAMAGE D SECTION OF LONGERON. LOCATED AND DRILLED NEW LONGERON AND LONGERON SPLICE. INSTALLED LONGERON AND SPLICES. (M) 2 L 7 2 4F A6WE 2002120500140 20021205 00140 WP 2002 12 5 GTIA020913 1 20020724 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND DENT AT FS 223 BETWEEN LONGERON 15L AND 16L REQUIRES REPAIR. REWORKED DENT. FABRICATED INTERNAL REPAIR DOU BLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2002120500141 20021205 00141 WP 2002 12 5 GTIA020914 1 20020724 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND DENT AT FS 655 BETWEEN LONGERONS 14R AND 15R REQUIRES REPAIR. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR PLUG AND REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2002120500142 20021205 00142 WP 2002 12 5 GTIA020947 1 20020706 A 5522 SKIN DOUG DC9 DC982 3022082 WP ELEVATOR SCRATCHED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND LEFT ELEVATOR SURFACE HAS A DEEP SCRATCH AT STATION XH5-170. REMOVED DAMAGED SECTION OF SKIN. FABRICATED N EW SKIN SECTION, FINGER DOUBLER, STRAP, OUTBOARD INTERNAL DOUBLER, SPLICE. INSTALLED DOUBLER SPLICE, REPAIR SKIN, STRAP , DOUBLER. (M) 2 L 7 2 4F A6WE 2002120500143 20021205 00143 WP 2002 12 5 GTIA020948 1 20020619 A 7830 ACOUSTIC PANEL DOUG DC9 DC981 3022081 WP THRUST REVERSER CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 810NK 48015 FTW - FOUND NR 1 ENGINE T/R HAS DENT AND CRACK AT ACOUSTIC PANEL. T/R REPLACED ON BOO03611-R-2. (M) 2 L 7 2 4F A6WE 2002120500144 20021205 00144 WP 2002 12 5 GTIA020949 1 20020628 A 7110 5930645509 NOSE COWL DOUG DC9 DC982 3022082 WP NR 3 ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - NR 3 ENGINE NOSE COWL DAMAGED SEVERAL DIFFERENT AREAS. REPLACED DAMAGED NOSE COWL. (M) 2 L 7 2 4F A6WE 2002120500145 20021205 00145 NM 2002 12 5 HNAA0200085 1 20021203 A 2700 82710108005 COVER DHAV DHAV DHC8 DHC8102 2809003 NM BROKEN A HNAA K NONE O OTHER NR NOT REPORTED 1 EA 07 936HA 36788 145 CREW REPORTED FIRST OFFICERS CONTROL YOKE WAS BINDING. FOUND PIECES OF THE FO'S CONTROL COLUMN UPPER PLASTIC COVERS BROK EN OFF AND LODGED IN THE CONTROL CHAIN UPPER SPROCKET. REMOVED PLASTIC PIECES AND TRIMED COVERS PER EO. 2 H 7 2 4T RT A13NM 2002120500146 20021205 00146 NM 2002 12 5 MEX2002311 1 20020927 A 2720 37723745503 O-RING DOUG MD80 MD83 3023681 NM RUDDER DAMAGED A ASMF A B UNSCHED LANDING EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 23 861LF 49826 FLT 509 - MEX-VSA - AIRCRAFT PERFORMED AN EMERGENCY DESCENT AND UNSCHEDULED LANDING AT MEX DUE TO LOSS OF HYDRAULIC FLUI D INTO THE RIGHT SYSTEM. TECHNICAL PERSONNEL VERIFIED THE SYSTEMS, RIGHT SYSTEM WAS EMPTY. HYDRAULIC LIQUID WAS RECHAR GED TO VERIFIED SYSTEM BY LEAKAGES. LEAKAGE WAS FOUND IN A CAP OF THE SHUTOFF RUDDER VALVE. THE O-RING CAP WAS REPLACE D IAW MM 27-20-09, TESTS OK. AT RON MEX 27/28, THE SHUTOFF RUDDER VALVE WAS REPLACED IAW MM 27-20-09, TESTS OK. (M) 2 L 7 2 4F RT 2002120500147 20021205 00147 WP 2002 12 5 MEX2002312 1 20020927 A 2913 AS66411LS666 PUMP DOUG DC9 DC982 3022082 WP LT ENGINE FAILED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 501AM 49188 FLT 579 - MEX-CUN - AIRCRAFT RETURNED TO BLOCKS DUE TO THE ABSENCE OF HYDRAULIC PRESSURE FROM THE LEFT ENGINE DURING TAX IING. TECHNICAL PERSONNEL REVIEWED THE HYDRAULIC PUMP AND IT WAS REPLACED IAW MM 29-10-05, TEST OK. (M) 2 L 7 2 4F A6WE 2002120500148 20021205 00148 NM 2002 12 5 USAABB02137 1 20020823 A 2560 140N27661 LOCK BOEING 757 757225 1384959 NM GIRT FITTING MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 22203 PHL - FOUND R4 DOOR GIRT BAR FORWARD LOCK END MISSING. MAINTENANCE REPLACED THE FORWARD BARLOCK. (M) 2 L 7 2 4F RT A2NM 2002120500149 20021205 00149 NM 2002 12 5 USAABB02142 1 20020828 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AU 27199 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 13, 22, 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002120500150 20021205 00150 NM 2002 12 5 USAABB02143 1 20020829 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 602AU 22196 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002120500151 20021205 00151 NM 2002 12 5 USAABB02144 1 20020830 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2002120500152 20021205 00152 NM 2002 12 5 P9R2002F00010 1 20021019 A 2560 SG9422 STRIP BOEING 727 727200 138407E NM PWA JT8 JT8D17 52049 NE CABIN MISSING A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 910PG 22606 PHOTO LUMINESCENT STRIP IS MISSING FROM FORWARD GALLEY. RESECURED PHOTO LUMINESCENT IN FORWARD GALLEY. THE CAUSE OF TH E MALFUNCTION WAS THE PHOTO LUMINESCENT STRIP COMING UNGLUED FROM FLOOR. 2 L 7 3 4F 4 F RT A3WE E2EA 2002120500153 20021205 00153 WP 2002 12 5 DHL2002803011 1 20021204 A 2611 LAMP DOUG DC8 DC873 302199C WP A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 803DH 46123 1) #13 SMOKE DETECTOR WILL NOT TEST.2) DEFERRED PER MEL 26-6-1 DMI #11131.3) RE: DMI #11131 - #13 SMOKE DETECTOR WILL NOT TEST.4) REMOVED AND REPLACED BOTH LAMPS IN #13 SMOKE DETECTOR. SYSTEM CHECKED GOOD PER 26-10-0. CLEARED DMI #11131 . PLACARD REMOVED. 2 L 7 4 4F RT 4A25 2002120500154 20021205 00154 WP 2002 12 5 0203939995 1 20021201 A 2780 GUIDE DOUG DC9 DC931 3022065 WP WINGS A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 8978E 47327 When configuring for landing at JAX the "slat disagreement" light illuminated and the aircraft rolled to the right. COM procedures were followed and crew landed aircraft with "flaps only" without incident. Maintenace found the "T-Ducts" out board spacer guides on both sides worn and a stripped bolt. All were replaced, aircraft was returned to service. 2 L 7 2 4F A6WE 2002120500155 20021205 00155 SO 2002 12 5 C2XA02BT079 1 20021129 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO DISCONNECTED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 12922 145338 EWR---CO3491, CREW REPORTED, "ON POST FLIGHT INSPECTION, EMERGENCY LIGHT AT MAIN CABIN DOOR IS INOPERATIVE....MAINTENANC E RESECURED LOOSE WIRES ON EMERGENCY LIGHT STRIP IAW EMB145 AMM #33-50-08. (OPS.CHECKED GOOD) 2 L 7 2 4T RT T00011AT 2002120500156 20021205 00156 SO 2002 12 5 C2XA02BT080 1 20021127 A 3350 BATTERY PACK EMB 145 EMB145LR 3260212 SO DISCHARGED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14952 145067 YYZ---CO3350, CREW REPORTED, "AFT OF ROW SIX EMERGENCY LIGHTS COME ON THEN GO OUT (DURING TEST)"....MAINTENANCE REMOVED AND REPLACED #3 AND #4 EMERGENCY BATTERY PACKS IAW EMB145 MM #33-50-04. OPS.CHECKED SERVICEABLE. AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4T RT T00011AT 2002120500157 20021205 00157 NM 2002 12 5 ASAA0210221 1 20021010 A 3350 BATTERY BOEING 737 737290C 138448V NM PWA JT8 JT8D17 52049 NE CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 740AS 22578 DURING INSPECTION FOUND EMERGENCY FLOOR TRACK LIGHTS IN THE AFT PASSENGER CABIN WILL NOT EXTINGUISH. REMOVED AND REPLAC ED REMOTE ASSEMBLY BATTERY, THEN LIGHTS TESTED NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 2002120500158 20021205 00158 NM 2002 12 5 ASAA0210280 1 20021104 A 7110 654796636 COWLING BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 743AS 21821 DURING SCHEDULED C CHECK, FOUND NR 2 ENGINE COWL AT NACELLE STATION 165, CHAFFED. REMOVED AND REPLACED NR 2 ENGINE OUTB OARD COWL 12TH RIB IAW SRM. 2 L 7 2 4F 4 F A16WE E2EA 2002120500159 20021205 00159 NM 2002 12 5 ASAA0210281 1 20021104 A 7110 657377391 COWLING BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 743AS 21821 DURING SCHEDULED C CHECK, FOUND NR 2 ENGINE COWL AT NACELLE STATION 169.5 GOUGED. REPAIRED NR 2 ENGINE COWL IAW SRM. 2 L 7 2 4F 4 F A16WE E2EA 2002120500160 20021205 00160 NM 2002 12 5 ASAA0210282 1 20021104 A 7110 65479674 LONGERON BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE NR 2 COWLING CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 743AS 21821 DURING SCHEDULED C CHECK FOUND NR 2 ENGINE COWL LONGERON AT NACELLE STATION 99.25-200 CHAFED AND GOUGED. REMOVED AND RE PLACED NR 2 ENGINE COWL LONGERON IAW SRM. 2 L 7 2 4F 4 F A16WE E2EA 2002120500161 20021205 00161 NM 2002 12 5 ASAA0210283 1 20021106 A 7110 6573773 SKIN BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE NR 2 COWLING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 743AS 21821 DURING SCHEDULED C CHECK FOUND NR 2 ENGINE COWL SKIN AT NACELLE STATION 180 GOUGED. REMOVED DAMAGE AND INSTALLED DOUBLE R ON NR 2 ENGINE COWL IAW SRM. 2 L 7 2 4F 4 F A16WE E2EA 2002120500162 20021205 00162 NM 2002 12 5 ASAA0210284 1 20021106 A 5320 6546534 SUPPORT BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 743AS 21821 DURING SCHEDULED C CHECK, FOUND CEILING SHROUD PANEL SUPPORT AT BODY STATION 520, RBL 30 - RBL 61 CORRODED. REMOVED AND REPLACED CEILING SHROUD PANEL SUPPORTS IAW SRM. 2 L 7 2 4F 4 F A16WE E2EA 2002120500163 20021205 00163 NM 2002 12 5 ASAA0210285 1 20021106 A 5754 6546419183 SKIN BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE L/E SLAT GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 743AS 21821 DURING SCHEDULED C CHECK, FOUND NR 2 SLAT LEADING EDGE AT WING STATION 479L GOUGED. REMOVED DAMAGE AND REPAIRED IAW SR M. 2 L 7 2 4F 4 F A16WE E2EA 2002120500164 20021205 00164 NM 2002 12 5 ASAA0210286 1 20021106 A 7710 6573773 SKIN BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE NR 2 COWLING DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 743AS 21821 DURING SCHEDULED C CHECK FOUND NR 2 ENGINE COWL AT NACELLE STATION 170, DENTED. REMOVED DAMAGE AND FABRICATED REPAIRS I AW SRM. 2 L 7 2 4F 4 F A16WE E2EA 2002120500165 20021205 00165 NM 2002 12 5 ASAA0210287 1 20021106 A 5754 6546422293A SKIN BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 743AS 21821 DURING SCHEDULED C CHECK FOUND NR 2 SLAT LEADING EDGE SKIN AT SLAT STATION 177, CHAFED. REPAIRED NR 2 SLAT IAW EA. 2 L 7 2 4F 4 F A16WE E2EA 2002120500166 20021205 00166 NM 2002 12 5 ASAA0210288 1 20021107 A 5242 654583065 SKIN BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE E/E BAY DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 743AS 21821 DURING SCHEDULED C CHECK FOUND E-BAY DOOR SKIN AT BODY STATION 328-344, LBL 12 - RBL 12 DENTED. REMOVED AND REPLACED DO OR SKIN IAW SRM. 2 L 7 2 4F 4 F A16WE E2EA 2002120600001 20021206 00001 SO 2002 12 6 C2XA02SH137 1 20021206 A 5300 14522459001 SUPPORT EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14916 145415 SHV DURING C CHECK THE RAMP ANGLE SUPPORT ON CENTER OMEGA BEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO HAVE CORROSION. MA INTENANCE REMOVED AND REPLACED AFFECTED RAMP ANGLE SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002120600002 20021206 00002 SO 2002 12 6 CA021028004 1 20021023 A 3230 14470 TORQUE LINK EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13000 13000 (CAN) DURING A LANDING GEAR INSPECTION THE TECHNICAIAN FOUND THE CENTER POINT OF TORQUE LINK PART NUMBER 14470 CRACKED. 1 L 7 2 4T 4 T A21SO E4EA 2002120600003 20021206 00003 EU 2002 12 6 CA021029005 1 20021015 A 2560 503270411 CABLE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE SHOULDER HARNESS WORN W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) THE PRIMARY FUNCTION OF THIS IS TO ADD FRICTION TO THE INERTIA REEL PORTION OF THE SHOULDER HARNESSES. THE RUBBER SHEATH THAT COVERS THE CABLE HAD SEPARATED AT BOTH ENDS OF THE CABLE ASSEMBLY DUE TO THE LACK OF SUPPORT. THE PREVIOUS A SSEMBLIES THAT WERE MANUFACTURED BY EUROCOPTER HAD ADDITIONAL SUPPORT AT THE CABLE ENDS. HOWEVER, DUE TO A CHANGE IN VEN DORS THE CABLE NO LONGER IS MANUFACTURED WITH THE ADDED SWAGED ENDS FOR ADDITIONAL SUPPORT. 1 G 7 1 3U 3 U H9EU E19EU 2002120600004 20021206 00004 EA 2002 12 6 CA021029007 1 20021029 A 2910 215751588 LINE CNDAIR CL215 CL2151A10 1900320 EA PWA R2800 R2800* 52026 NE HAMSTD 43E 43E60 NE HYD SYSTEM CRACKED W O OTHER K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING A 'B' CHECK INSPECTION, A HYDRAULIC SYSTEM FUNCTION CHECK WAS BEING COMPLETED. A LEAK WAS DETECTED AT THE A UX HYDRAULIC RETURN LINE LOCATED IN THE FORWARD SKI SLOPE OF THE AIRCRAFT. UPON INVESTIGATION A CRACK WAS FOUND WITH A P IECE OF THE LINE MISSING FROM THE CRACKED AREA. THE DIMENSION OF THE MISSING PIECE IS APPROXIMATELY 1/4 X 1/16 INCH. THE HYDRAULIC TANK WAS REMOVED FROM THE AIRCRAFT AND INSPECTED INSIDE FOR SIGNS OF CONTAMINATION. THE TANK WAS FLUSHED AND REINSTALLED IN THE AIRCRAFT.THE LINE WAS REPLACED WITH A SERVICEABLE UNIT AND A LEAK CHECK OF THE SYSTEM WAS COMPLETED. 2 H 7 2 4R 4 R RT A14EA 5E8 6 C P871 2002120600005 20021206 00005 EA 2002 12 6 CA021029014 1 20021029 A 3233 215340141 FITTING CNDAIR CL215 CL2151A10 1900320 EA PWA R1340 CWASP 52016 NE MLG ACTUATOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON INSPECTION PRIOR TO INSTALLING AN UPGRADE KIT(K215-0399) TO STRENGTHEN THE MAIN LANDING GEAR ACTUATOR BOX STR UCTURE, IT WAS DISCOVERED THAT THE FITTINGS THAT ATTACH TO BOX STRUCTURE HAD FAILED. THIS WAS THE SECOND AIRCRAFT TO HAV E THIS OCCURRENCE OF FAILURE IN THIS AREA. THE UPGRADE KITS HAD BEEN ORDERED PREVIOUSLY AND ARE BEING INSTALLED IN ALL O F THE OPERATOR'S CL-215 AIRCRAFT. 2 H 7 2 4R 3 R RT A14EA ATC14 2002120600006 20021206 00006 EA 2002 12 6 CA021029015 1 20021029 A 3233 215340141 FITTING CNDAIR CL215 CL2151A10 1900320 EA PWA R1340 CWASP 52016 NE MLG ACTUATOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON INSPECTION PRIOR TO INSTALLING AN UPGRADE KIT(K215-0399) TO STRENGTHEN THE MAIN LANDING GEAR ACTUATOR BOX STR UCTURE, IT WAS DISCOVERED THAT THE FITTINGS THAT ATTACH TO BOX STRUCTURE HAD FAILED. THIS WAS THE SECOND AIRCRAFT TO HAV E THIS OCCURRENC OF FAILURE IN THIS AREA. THE UPGRADE KITS HAD BEEN ORDERED PREVIOUSLY AND ARE BEING INSTALLED IN ALL OF THE OPERATOR'S CL-215 AIRCRAFT. 2 H 7 2 4R 3 R RT A14EA ATC14 2002120600007 20021206 00007 EA 2002 12 6 CA021029016 1 20021029 A 3233 215340141 FITTING CNDAIR CL215 CL2151A10 1900320 EA PWA R1340 CWASP 52016 NE MLG ACTUATOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON INSPECTION PRIOR TO INSTALLING AN UPGRADE KIT(K215-0399) TO STRENGTHEN THE MAIN LANDING GEAR ACTUATOR BOX STR UCTURE, IT WAS DISCOVERED THAT THE FITTINGS THAT ATTACH TO BOX STRUCTURE HAD FAILED. THIS WAS THE SECOND AIRCRAFT TO HAV E THIS OCCURRENCE OF FAILURE IN THIS AREA. THE UPGRADE KITS HAD BEEN ORDERED PREVIOUSLY AND ARE BEING INSTALLED IN ALL O F THE OPERATOR'S CL-215 AIRCRAFT. 2 H 7 2 4R 3 R RT A14EA ATC14 2002120600009 20021206 00009 SO 2002 12 6 CA021030005 1 20021015 A 5415 ATTACH ANGLE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA NACELLE SKIN CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10611 (CAN) DURING ROUTINE 100 HOUR INSPECTION FOUND CRACKED LT AND RT PLATES LOCATED ON INBOARD SIDE OF NACELLE JUST AFT OF F IREWALL. PLATES ATTACH SKIN OF NACELLE TO FRAME. AIRCRAFT IS OPERATED FOR LOW LEVEL TERRAIN FOLLOWING SURVEY. PREVIOUSLY FOUND SAME PLATES CRACKED ON TWO OTHER AIRCRAFT. THIS AIRCRAFT ORIGINALLY HAS BEEN INSPECTED FOR THE SAME DEFECT AT 102 28.3 HR TTSEN. AND ON ALL OTHER REPETITIVE INSPECTIONS AND CRACK WAS FOUND DURING THIS INSPECTION. 1 L 7 2 3O 3 O A20SO E14EA 2002120600010 20021206 00010 SO 2002 12 6 CA021030006 1 20021028 A 3246 300608 WHEEL EMB 110 EMB110* SO PWA PT6 PT6A34 52043 EA MLG FRACTURED W O OTHER D INFLIGHT SEPARATION LD LANDING 1 CA (CAN) INNER WHEEL HALF BEAD SEAT FAILED AROUND APPROXIMATELY HALF THE CIRCUMFRENCE OF THE WHEEL DURING LANDING PHASE. WH EEL WAS REPLACED AND NO OTHER DAMAGE REPORTED OR FOUND. 1 L 7 2 4T 4 T RT A21SO E4EA 2002120600011 20021206 00011 EU 2002 12 6 CA021030008 1 20021029 A 3242 STATOR PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL MLG BRAKE WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ROUTINE WHEEL BEARING SERVICING, THE RT MAIN WHEEL WAS FOUND WITH EXCESSIVE BRAKE DRAG. THE STATOR WEAR PAD S WERE OBSERVED TO BE WARPED AND EXCESSIVELY WORN. THE ROTOR HAS WORN INTO THE WEAR PADS TO THE POINT WHERE THE TOP OF T HE STATOR PAD IS TOUCHING THE ROTOR DISC ,METAL TO METAL. THIS IS THE SECOND INSTANCE ON FILE AT THIS BASE. THE COMPLETE BRAKE ASSY WAS REPLACED WITH NEW. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2002120600012 20021206 00012 EA 2002 12 6 CA021031001 1 20021027 A 5210 051940 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE PAX DOOR BROKEN W B EMER. DESCENT D INFLIGHT SEPARATION CL CLIMB 1 CA 14456 (CAN) IN CLIMB TO FL 240, A LOUD NOISE COMING FROM THE PAX DOOR WAS HEARD ALONG WITH A DEPRESSURIZATION OF THE AIRCRAFT OF APPROXIMATELY -4000 FT/MIN (ON EICAS). THE FLIGHT CREW DID AN EMERGENCY DESCENT PER THE QRH AND LANDED AT THE DESTINA TION AIRPORT. ONCE AT AIRPORT, IT WAS OBSERVED THAT THE PAX DOOR SEAL WAS DE BONDED ON A LENGTH OF APPROXIMATLY 1.5 METE R AND THAT A PIECE OF 30 CM WAS MISSING.THE AIRCRAFT WAS FERRIED, UNPRESSURIZED, WHERE THE SEAL WAS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120600018 20021206 00018 EA 2002 12 6 CA021101001 1 20021003 A 2742 212071440 PIN CNDAIR CL601 CL6013A 8070802 EA GE CF34 CF343A 30015 NE HORIZONTAL STAB SHEARED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) UPON INSPECTION OF THE HORIZONTAL STAB TRIM ACTUATOR, P/N 600-92301-963, PER THE TIME LIMITS/MAINTENANCE CHECKS, 6 00 HOUR INSPECTION, IT WAS FOUND THAT PIN 21207-1440 WAS FOUND SHEARED. THE SHEAR OCCURRED ON THE THREADED PORTION OF TH E PIN. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120600026 20021206 00026 EA 2002 12 6 CA021104003 1 20021028 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT FAILED W O OTHER D INFLIGHT SEPARATION DE DESCENT 1 CA 16609 (CAN) CAPTAIN'S WINDSHIELD SHATTERED AT 28,000FT ON DESCENT.CABIN AT 8 PSID. NO EMERGENCY DECLARED.SENT ROAD CREW TO R& R WINDSHIELD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120600029 20021206 00029 NM 2002 12 6 CA021105001 1 20021021 A 7160 4100S02802 ADAPTER BOMBDR DHC8 DHC8402 NM PWC 150 PW150A EA HEATER ELEMENT BURNED OUT W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) ENGINE INLET ADAPTER HEATER BURNED OUT BOTH ELEMENTS WHEN SELECTED ON JUST PRIOR TO TAKE OFF. ENGINE BLEEDS WERE O N AND THE RESULTING SMOKE DRAWN THROUGH AIR CONDITIONING SYSTEM CAUSED A SEVERE BURNING SMELL IN AIRCRAFT. INTAKE HEATER NR 1 C/B TRIPPED, AIRCRAFT RETURNED TO HANGAR FOR INLET ADAPTER RE PLACEMENT. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002120600030 20021206 00030 NM 2002 12 6 CA021105002 1 20021021 A 3230 471901 GUIDE BOMBDR DHC8 DHC8402 NM PWC 150 PW150A EA NLG CABLE BENT W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) NLG UPPER CABLE GUIDE FOUND BENT. THIS HAS OCCURRED DURING LANDING GEAR RETRACTION. THE GUIDE ASSY CAN BE PULLED F ORWARD TO AN OVER CENTER CONDITION WHEN GEAR IS DOWN, THIS WILL PREVENT PROPER FOLDING OF THE GUIDE DURING GEAR RETRACTI ON. THE GUIDE AND WIRING CONDUIT WILL BE DAMAGED DURING NEXT GEAR RETRACTION. SUGGEST ALL DHC-8 MAINTAINERS BE AWARE OF THIS AND BE DILIGENT TO PREVENT THIS CONDITION. 2 H 7 2 4T 4 T RT A13NM E00062EN 2002120600031 20021206 00031 SW 2002 12 6 CA021105003 1 20021101 A 3260 2782186057 INDICATOR FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL MLG FAILED W O OTHER N FALSE WARNING AP APPROACH 1 CA (CAN) UPON SELECTION OF THE LANDING GEAR ON APPROACH , THE NOSE DID NOT INDICATE DOWN AND LOCK. THE UNSAFE ANNUNCIATOR W AS NOT ILLUMINATED SUGGESTING THAT THE NOSE WAS EXTENDED. LAMP TEST OF THE NOSE LIGHT DID NOT WORK EITHER. THE NOSE GEAR COULD BE SEEN AS EXTENDED BY VIEWING IN THE PROP SPINNER. A FLYBY CONFIRMED THAT THE GEAR WAS EXTENDED AND VISUALLY APP EARED TO BE OVER CENTER. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED THE FAULT TO BE IN THE LANDING GEA R INDICATOR ITSELF. A POOR CONNECTION OF THE NOSE LAMP SOCKET/HOLDER RESULTED IN AN INTERMITTENT INDICATION. THE SPRING TAB ON THE SOCKET WAS REPOSITIONED AND THE GEAR INDICATING SYSTEM TESTED THROUGH SEVERAL CYCLES, FAULT FREE. 2 L 7 2 4T 4 T RT A18SW E4WE 6 C P61GL 2002120600032 20021206 00032 SW 2002 12 6 CA021105004 1 20021104 A 5270 WARNING LIGHT FRCHLD SA227 SA227CC 3377522 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL CARGO DOOR FALSE ACTIVATION W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) AFTER TAKE-OFF AND AS THE AIRCRAFT BEGAN TO PRESSURIZE THE CARGO DOOR WARNING LIGHT ILLUMINATED. THECREW REQUESTED A RETURN TO BASE AND LANDED UNEVENTFULLY. MAINTENANCE INSPECTION OF THE AIRCRAFT DET ERMINED THAT A FALSE WARNING INDIC ATION OF THE CARGO DOOR WARNING SYSTEM WAS CAUSED BY THE PRESENCE OF MOISTURE IN THE AREA OF THE CARGO DOOR WARNING SWIT CHESAND CLICK-CLACK LATCHES. THE SWITCHES AND LATCHES WERE DRIED, CLEANED AND LUBRICATED AND THE DOOR CLOSURE AND INDICA TING SYSTEM FUNCTION CHECKED SERVICEABLE. 2 L 7 2 4T 4 T RT A18SW E4WE 6 C P61GL 2002120600033 20021206 00033 SW 2002 12 6 CA021105005 1 20021028 A 2822 IC2710 PUMP BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FUEL BOOST FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) PUMP STOPPED PUMPING FOLLOWED BY A BOOST PUMP AFT CAUTION LIGHT. 1 G 7 1 3U 3 U H2SW E4CE 2002120600034 20021206 00034 NE 2002 12 6 CA021105006 3 20021031 A 6114 E3932 HUB BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3A NE PROPELLER FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON DISASSEMBLY OF PROPELLER A C792 BEARING WAS FOUND TO BE CRACKED AND BROKEN. ON FURTHER INVESTIGATION IT WAS F OUND THAT THE BEARING HAD CAUSED DAMAGE TO THE HUB RENDERING IT UNSERVICEABLE. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2002120600040 20021206 00040 SW 2002 12 6 CA021105012 1 20021104 A 6710 BELLCRANK BELL 204 204B 1181404 SW LYC T53 T5311B 41549 NE MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AT 1000 HR INSPECTION BELLCRANK FOR THE CYCLIC WAS REMOVED FOT GREASING OF THE BEARINGS. BELLCRANK WAS FOUND TO BE CRACKED AT ONE BEARING. CRACK WAS COMPLETELY THROUGH TO THE OUTER RACE OF THE BEARING. BELLCRANK WAS REPLACED WITH A SE RVICEABLE ONE.ALL OTHER CONTROLS INSPECTED NO FURTHER PROBLEM FOUND. CRACKED BELL CRANK HAS BEEN QUARANTINED. 1 G 7 1 4U 4 U H1SW E1EA 2002120600041 20021206 00041 NE 2002 12 6 CA021105013 2 20021025 A 7200 ENGINE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 FAILED W E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) CREW REPORTED A VIBRATION ON NR 2 ENG DURING SHUTDOWN. VIBRATION WAS FELT THRU PEDESTAL ON CUTOFF LEVER. CREW AD VISED MAINT ALL ENGINE PARAMETERS WERE NORM DURING FLT AND ON APPROACH. MAINT INSPECTED ENG AND FOUND 'BLADE TIP RUBBIN G SOUNDS' DURING ROTATION OF THE C1. ENG-DRIVEN COMPONENTS AND TAIL PIPE INSPECTED FOR DAMAGE/SECURITY. NO OTHER IRREG ULARITIES WERE FOUND. MAINT CONDUCTED IDLE RUNS WITH CSD DISCONNECTED. DURING RUN, PEDESTAL STARTED TO VIBRATE AND ENG RPM BEGAN TO DROP AND SUDDENLY FELL OFF (EGT REMAINED STABLE). RADIOED TO SHUTDOWN ENG AS METAL EXITED THE TAIL PIPE. MA INT REPLACED ENG, GROUND RUNS COMPLETED AND CHECKED SERVICEABLE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2002120600042 20021206 00042 NE 2002 12 6 CA021105014 2 20021101 A 7250 ENGINE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 FAILED W B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) FLIGHT CREW REQUESTED IMMEDIATE RETURN TO YOW SHORTLY AFTER TAKEOFF DUE TO NR 1 ENGINE FAILURE (PILOT SHUTDOWN). E MERGENCY SERVICES CALLED OUT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTION REVEALED 'TURBINE FAILURE'. AIR CRAFT STILL ON GROUND IN YOW - SPARE ENGINE ENROUTE. FAULTY ENGINE BEING SENT TO OVERHAUL FACILITY FOR POSSIBLE CAUSE OF ENGINE FAILURE. AWAITING 'TEARDOWN REPORT'. 2 L 7 2 4F 4 F A16WE E2EA 2002120600043 20021206 00043 EA 2002 12 6 CA021106002 2 20020927 A 7322 BEARING BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA FUEL CONTROL WORN W O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA (CAN) DURING CRUISE PILOT NOTICED LT ENGINE NG SLOWLY INCREASING. PILOT INCREASED THROTTLE TO COMPENSATE.STABILIZED AT ONE THROTTLE KNOB FORWARD OF RT THROTTLE. LANDED WITH NO FURTHER INCIDENT. FCU REMOVED FOR REPLACEMENT (NO OTHER DISCREP ANCIES FOUND). FOUND DRIVE END BEARING COMING APART. REPLACED FCU. RUNUP NORMAL. AFTER NEXT FLT REINSPECTED. FOUND SLIGH T FUEL LEAK AT PUMP DRAIN. PUMP REPLACED. 1 L 7 2 4T 4 T A24CE E4EA 2002120600044 20021206 00044 NM 2002 12 6 CA021107002 1 20021103 A 2910 AN938D8 FITTING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING ENGINE RUNS FOR REPAIR OF ANOTHER DEFECT, NR 1 ENGINE/NACELLE AREA DEVELOPED A HYDRAULIC LEAK. TRACED TO FI TTING IN NR 1 NACELLE AT APPROX STN Y143.12. FITTING REPLACED.IPC REF 29-00-00 FIG. 30ITEM 190 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002120600045 20021206 00045 NM 2002 12 6 CA021107003 1 20021104 A 2435 STARTER GEN DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 FAILED W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 CA 25377 (CAN) AIR TURNBACK DUE TO FAILURE OF NR 1 DC GENERATOR DURING CLIMB OUT. STARTER/GENERATOR REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002120600046 20021206 00046 EA 2002 12 6 CA021108001 1 20021102 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT FAILED W A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 CA (CAN) CAPTAIN'S WINDSHIELD SHATTERED AT FL290. DIVERTED. WINDSHIELD REPLACED AND AIRCRAFT RETURNED IN SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120600048 20021206 00048 EU 2002 12 6 CA021108004 1 20021107 A 2916 4178881 CAP ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE73140 29001 NE HYD SYSTEM LEAKING W J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) DEPARTED ENROUTE 30 MIN AFT. DEPARTURE CLIMBING THROUGH FL310 POP/BANG HEARD FOLLOWED BY HYD LIGHT THEN LT HYD PUM P LIGHT THEN DECREASE IN HYD PRESSURE TO 1500 PSI. RT PUMP LIGHT ON PRESSURE DROP TO 1500 PSI. A/C TURNED AROUND FOR Y YZ, FUEL DUMPED, AS THEY DESCENDED BELOW FL250 HYD SYSTEM RETURNED TO NORMAL NO LIGHTS. LANDED GROUND CHECKED FOUND H YD CAP OFF NR 1 SYSTEM WITH NO FLUID LOSS. CAP CHECKED FOR DAMAGE NONE FOUND CAP REINSTALLED A/C GROUND RUN SYSTEM CHEC KED OK AND RELEASED TO SERVICE. 2 L 7 2 4F 4 F RT A16NM E1NM 2002120600049 20021206 00049 EU 2002 12 6 CA021108005 1 20021106 A 5342 F53574150004 BOLT AIRBUS 330 A330342 EU RROYCE RB211 RB211TRENT77 NE HORIZONTAL STAB LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AT C02 CHECK FOUND THIS MAIN HINGE FITTING Y-BOLT O/B BEARING MIGRATED BY .0130 INCH AT REAR SPAR ATTACHMENT BOLT REPLACED BY NEW BOLT AT AC 11,599 HRS, 2,322 CYCL 1 L 7 2 4F 4 F RT A46NM E39NE 2002120600050 20021206 00050 EU 2002 12 6 CA021108006 1 20021101 A 5744 D5725260120000 WASHER AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE ANTI-ROTATION MISMANUFACTURED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) ANTI-ROTATION WASHER SHOWN IN IPC 57-26-13 FIG 01B ITEM 60 IS NOT MANUFACTURED INACCORDANCE WITH DRAWING. SHARP E DGE CUTOUT ON WASHER INTERFERES WITH RADIUS LUG ON FITTING-PREVENTS WASHER FROM LAYING FLAT ON THE ACTUATOR FITTING-PREV ENTS BEARING FROM BEING PROPERLY TORQUED. 2 L 7 2 4F 4 F RT A28NM E29NE 2002120600052 20021206 00052 NM 2002 12 6 CALA0200574 1 20021206 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM STA 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND FLOORBEAM CORRODED AT FASTENER HOLE, STA 312, RBL 37. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2002120600053 20021206 00053 EA 2002 12 6 02335659 1 20021201 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA AC BAY FAULTY A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 27 659BR 7509 AFTER LANDING, THE CREW RECEIVED A "TOILET SMOKE" EICAS MESSAGE FOLLOWED BY CONFIRMED SMOKE IN THE CABIN. THE AIRCRAFT WAS STOPPED AND PASSENGERS WERE EVACUATED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE RT AIR CONDI TIONING PACK AIR CYCLE MACHINE (ACM). THE PACK COALESCER SOCKS WERE REPLACED DUE TO THE SMOKE AND THE OVERWING EMERGENC Y EXIT DOORS WERE INSPECTED AND REINSTALLED. OPERATIONAL AND PRESSURIZATION CHECKS WERE SATISFACTORY AND THE AIRCRAFT W AS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002120600054 20021206 00054 EU 2002 12 6 02338309 1 20021204 A 2750 TY175603C CONTROL UNIT JETAIR JETSTM JETSTM4101 1500501 EU A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 309UE 41022 After take-off at flap retraction, the crew reported that the flaps would not retract beyond nine degrees. The flight r eturned to IAD and landed without further incident. Maintenance personnel removed and replaced the flap control unit. Operational checks were satisfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002120600057 20021206 00057 NM 2002 12 6 2002F01066 1 20020703 A 5320 65453136 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 950B, RIGHT SIDE AT STRINGER 7R. (M) 2 L 7 3 4F A3WE 2002120600059 20021206 00059 NM 2002 12 6 2002F01067 1 20020703 A 5320 65453132 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 950B, RIGHT SIDE AT STRINGER 6R. (M) 2 L 7 3 4F A3WE 2002120600060 20021206 00060 NM 2002 12 6 2002F01068 1 20020707 A 5320 65453132 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 950B, RIGHT SIDE AT STRINGER 3R. (M) 2 L 7 3 4F A3WE 2002120600061 20021206 00061 NM 2002 12 6 2002F01069 1 20020703 A 5320 654531314 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 950A, RIGHT SIDE AT STRINGER 9R. (M) 2 L 7 3 4F A3WE 2002120600062 20021206 00062 NM 2002 12 6 2002F01070 1 20020703 A 5753 6521630173 SKIN BOEING 727 727222 1384073 NM T/E FLAP CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND LEFT WING INBOARD FORE FLAP LEADING EDGE SKIN CRACKED, AT WBL 94. (M) 2 L 7 3 4F A3WE 2002120600063 20021206 00063 NM 2002 12 6 2002F01071 1 20020703 A 5320 65453136 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 950E, RIGHT SIDE AT STRINGER 7R. (M) 2 L 7 3 4F A3WE 2002120600064 20021206 00064 NM 2002 12 6 2002F01072 1 20020703 A 5320 65453132 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 950E, RIGHT SIDE AT STRINGER 5R. (M) 2 L 7 3 4F A3WE 2002120600065 20021206 00065 NM 2002 12 6 2002F01073 1 20020703 A 5320 65453132 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 950D, RIGHT SIDE AT STRINGER 8R. (M) 2 L 7 3 4F A3WE 2002120600066 20021206 00066 NM 2002 12 6 2002F01074 1 20020702 A 7120 MOUNT BRACKET BOEING 727 727222 1384073 NM NR 2 ENGINE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND NR 2 ENGINE, AFT VIBRATION ISOLATOR ASSEMBLY MOUNT BRACKET RUSTED AND CORRODED ON FRONT AND BACK SIDE. (M) 2 L 7 3 4F A3WE 2002120600067 20021206 00067 NM 2002 12 6 2002F01075 1 20020703 A 5320 65453136 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED, AT STATION 950F, RIGHT SIDE AT STRINGER 7R. (M) 2 L 7 3 4F A3WE 2002120600068 20021206 00068 NM 2002 12 6 2002F01076 1 20020703 A 5320 65453132 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 990, RIGHT SIDE AT STRINGER 5R. (M) 2 L 7 3 4F A3WE 2002120600069 20021206 00069 NM 2002 12 6 2002F01065 1 20020703 A 5320 65453132 STRINGER CLIP BOEING 727 727222 1384073 NM FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7642U 19915 AT C-CHECK, FOUND STRINGER TIE CLIP CRACKED AT STATION 950B, RIGHT SIDE AT STRINGER 8R. (M) 2 L 7 3 4F A3WE 2002120600071 20021206 00071 EU 2002 12 6 A6WA200260034 1 20020820 A 3233 CLAMP BAC 146 146200A 1500266 EU MLG ACTUATOR OUT OF POSITION A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 DAMAGE TO THE MAIN LANDING GEAR BAY SKIN AT FRAME 29 LEFT SIDE AS CAUSED BY DOWN LOCK ACTUATOR CLAMP. MAINTENANCE DAMAG E BLENDED OUT IAW SRM 51-10-2. (M) 2 H 7 4 4F A49EU 2002120600072 20021206 00072 NM 2002 12 6 AALA20020836 1 20020605 A 2421 GEN5103 IDG BOEING 767 767323 1385205 NM RT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 21 379AA 25448 FRA - FL 84 - ONE HOUR AFTER TAKEOFF RIGHT GEN DRIVE LIGHT CAME ON GEN DISCONNECTED. REPLACED RIGHT IDG. OPS AND LEAK C HECK NORMAL PER AMM 24-11-01-04. (M) 2 L 7 2 4F RT A1NM 2002120600074 20021206 00074 NM 2002 12 6 AALA20020877 1 20020603 A 2432 BAT5040 BATTERY BOEING 777 777223 1385213 NM E/E BAY FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 758AN 32637 BOS - FLT 108 - MAIN BATTERY CHARGER NO LAND 3 STATUS MESSAGE. REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER ALL STATU S MESSAGES ERASED. OPS CHECKED ALL SATISFACTORY. (M) 2 L 7 2 4F RT T00001SE 2002120600076 20021206 00076 2002 12 6 AALA20020926 4 20020617 A 3441 IRU BOEING 767 767323 1385205 NM E/E BAY FAILED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 368AA 25195 MIA - FOS ATTITUDE HEADING AND VSI FAILED DURING CLIMB-OUT, SELECTING IRS TO ALT FIXED PROBLEM. CHECKED AND FOUND RIGHT IRU AT FAULT REPLACED RESET IRU PERFORMED ALL REQUIRED TEST PER M/M ALL CHECKS GOOD OK FOR SERVICE. (M) 2 L 7 2 4F RT A1NM 2002120600077 20021206 00077 EU 2002 12 6 CA021108014 1 20021105 A 6220 704A3363320861 THRUST BEARING SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR HEAD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION A DEEP CRACK IN THE LAMINATED RUBBER WAS FOUND. CRACK WAS TO THE MAXIMUM LIMIT OF 10MM. THE PART S WERE REMOVED AND NEW SPHERICAL THRUST BEARINGS INSTALLED. 1 G 7 1 3U 3 U H9EU E19EU 2002120600078 20021206 00078 WP 2002 12 6 GTIA021045 1 20021006 A 7120 K221478A1 ISOLATOR DOUG DC9 DC932 3022066 WP NR 2 ENGINE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DTW - NR 2 ENGINE FORWARD LOWER VIBRATION ISOLATOR IS CORRODED AND PLATING IS FLAKING OFF ON INNER CONICAL AREA. REMOVE D AND REPLACED NR 2 ENGINE FORWARD LOWER VIBRATION ISOLATOR (CLOSED 10/15/02). (M) 2 L 7 2 4F A6WE 2002120600079 20021206 00079 EU 2002 12 6 CA021108015 1 20021023 A 6220 RL12R BEARING SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE VIBRATION ABSORB CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON INSPECTION THE BEARING WAS FOUND TO BE PITTED WITH CORROSION. ALTHOUGH THERE WAS ONLY 529 HOURS SINCE NEW ON THE BEARING,, WE FOUND THAT THE AIRCRAFT HAD SAT FOR LONG PERIODS OF TIME IN WET WEATHER CONDITIONS. 1 G 7 1 3U 3 U H9EU E19EU 2002120600080 20021206 00080 2002 12 6 GTIA021077 4 20021013 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 ORD - FLT 842 - FOUND ON PREFLIGHT, SLIDE PACK MAIN DOOR (L1) OFF. REINSTALLED SLIDE PACK. (M) 2 L 7 2 4F A6WE 2002120600082 20021206 00082 WP 2002 12 6 GTIA021078 1 20020813 A 5522 DOUBLER DOUG DC9 DC981 3022081 WP ELEVATOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND LEFT ELEVATOR OUTBOARD TRAILING EDGE DOUBLER BENT AND CRACKED. REMOVED LEFT ELEVATOR OUTBOARD TRAILING EDGE DOUBLER. FABRICATED LEFT ELEVATOR OUTBOARD TRAILING EDGE DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2002120600083 20021206 00083 WP 2002 12 6 GTIA021079 1 20020919 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND FLOORBOARD SUPPORT CORRODED AT STATION 200. FABRICATED SUPPORT. INSTALLED FLOOR BOARD SUPPORT. (M) 2 L 7 2 4F A6WE 2002120600084 20021206 00084 WP 2002 12 6 GTIA021080 1 20020919 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND THRESHOLD MOUNT BRACKETS AT R1 DOOR ENTRY BROKEN (2EA) CRACKS IN WEB. REMOVED CRACKED WEB. FABRICATED NEW WEB. INSTALLED WEB. (M) 2 L 7 2 4F A6WE 2002120600085 20021206 00085 WP 2002 12 6 GTIA021081 1 20020919 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND FLOORBOARD SUPPORT BEAM CORRODED FROM STATION 160-200. REMOVED DAMAGED FLOOR SUPPORT. FABRICATED A NEW FLO OR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002120600086 20021206 00086 WP 2002 12 6 GTIA021082 1 20020919 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND FLOORBOARD SUPPORT BEAM CORRODED (C) AT STATION 200. REMOVED DAMAGED FLOORBOARD SUPPORT. FABRICATED A NEW PART. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2002120600087 20021206 00087 WP 2002 12 6 GTIA021083 1 20020813 A 5210 STRAP DOUG DC9 DC981 3022081 WP L1 DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 L1 DOOR SUPPORT STRAP IS CRACKED UNDER DOOR HINGE AREA. REMOVED PART. FORMED NEW STRAP. INSTALLED NEW STRAP. (M) 2 L 7 2 4F A6WE 2002120600088 20021206 00088 SW 2002 12 6 CA021108017 1 20020528 A 2497 12GAUGE WIRE BELL 214 214B 1182100 SW LYC T55 T5508D 41555 NE CIRCUIT BREAKER CHAFED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS HO HOVERING 1 CA (CAN) WHILE HOVERING DURING HELI-LOGGING OPERATIONS, PILOT NOTICED SMOKE AND SPARKS ORIGINATING FROM THE LT OVERHEAD CCT BREAKER PANEL. THE PILOT INITIATED AN UNSCHEDULED LANDING AND SHUT DOWN THE A/C WITHOUT FUTHER INCIDENT. IT WAS LATER DETERMINED THAT A WIRE BUNDLE CLAMP IN THE LT O/H CCT BREAKER PANEL HAD FAILED, ALLOWING THE LANDING LIGHT POWER WIRE TO CHAFE THROUGH ITS INSULATION AND SHORT TO GROUND. SUBSEQUENT HEAT GENERATED BY THE SHORTED WIRE MELTED THE INSULATION A ND CAUSED THEM TO SHORT TO GROUND AS WELL. IT APPEARED THE CASCADING EFFECT HAPPENED FASTER THAN THE CCT BREAKERS COULD TRIP OPEN. THE AFFECTED WIRES WERE REPLACED AND NEW CLAMPS WERE INSTALLED PAYING PARTICULAR ATTENTION TO BUNDLE ROUTING. 2 G 7 1 4U 4 U H6SW E4NE 2002120600089 20021206 00089 WP 2002 12 6 GTIA021084 1 20020926 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - PASSENGER CABIN FLOOR PANEL STATION 160 TO STATION 190 GOUGES, SOFT DAMAGE. FABRICATED FLOORBOARD. INSTALLED FLO ORBOARD. (M) 2 L 7 2 4F RT A6WE 2002120600090 20021206 00090 WP 2002 12 6 GTIA021085 1 20020926 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND PASSENGER CABIN, FLOOR PANEL STATION 200-256, SOFT/MUSHY DAMAGED. FABRICATED PASSENGER CABIN FLOOR PANEL. INSTALLED FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2003010900031 20030109 00031 NE 2003 1 9 CA021108020 2 20021014 A 7310 AS62404 CLIP AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211TRENT77 NE FUEL TUBE CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) RUBBER ON CLAMP DETERIORATED AND FUEL LINE WAS FOUND BADLY CHAFED (CLAMP WORE THROUGH THE LINE APPROX 0.035 TO 0.0 40), ON NR 1 ENGINE. CLIPS WERE REPLACED IAW AMM 73-11-40 AND A NEW FUEL TUBE ASSY REPLACED IAW AMM 73-11-00. 2 L 7 2 4F 4 F RT A46NM E39NE 2002120600091 20021206 00091 WP 2002 12 6 GTIA021086 1 20020929 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FLIGHT COMPARTMENT, COPILOT SIDE STATION 148, FLOOR PANEL IS CRACKED/DAMAGED AT CORNERS, 2 EACH PLATE ATTACH PANEL IS CORRODED. FABRICATED NEW PANEL. INSTALLED NEW PANEL. (M) 2 L 7 2 4F RT A6WE 2002120600092 20021206 00092 EU 2002 12 6 CA021108021 1 20021012 A 3246 C20211170 BOLT AIRBUS 310 A310304 3930339 EU WHEEL SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING AIRCRAFT WALK AROUND, FOUND NR 4 MLG WHEEL ASSY BOLT SHEARED AND MISSING. 2 L 7 2 4F RT A35EU 2002120600093 20021206 00093 WP 2002 12 6 GTIA021087 1 20020929 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FLOORBOARD RT INBOARD STATION 180-200 CRACKED/DAMAGED/CORRODED. FABRICATED FLOOR BOARD. INSTALLED FLOORBOAR D. (M) 2 L 7 2 4F RT A6WE 2002120600094 20021206 00094 WP 2002 12 6 GTIA021088 1 20020929 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FLOORBOARD RIGHT INBOARD STATION 160 TO STATION 180 SOFT/DAMAGED. FABRICATED FLOORBOARD PANEL. INSTALLED F LOORBOARD PANEL. (M) 2 L 7 2 4F RT A6WE 2002120600095 20021206 00095 NM 2002 12 6 CA021108022 1 20021107 A 4920 APU BOEING 737 7372M8 1384483 NM PWA JT8 JT8D15 52051 NE APU BAY FAILED W B F EMER. DESCENT ACTIVATE FIRE EXT. J E WARNING INDICATION VIBRATION/BUFFET AP APPROACH 1 CA (CAN) ON APPROACH, APU WAS STARTED AS NORMAL. SHORTLY AFTER START UP A VIBRATION WAS FELT THROUGHOUT THE AIRFRAME. AUTO SHUTDOWN OF THE APU OCCURRED,AS WELL AS A FIRE WARNING IN THE COCKPIT. APU FIRE QRC WAS ACCOMPLISHED WITH ASSOCIATED FIR E HANDLE PULLED AND BOTTLES DISCHARGED - FIRE LIGHT WENT OUT. FLIGHT CREW DECLARED AN EMERGENCY AND CFR WAS CALLED OUT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTION OF THE APU AND RELATED SYSTEMS REVEALED NO SIGNS OF FIRE OR DA MAGE TO MOUNTS,AS RESULT OF VIBRATION. AIRCRAFT GROUND CHECKED SERVICEABLE, APU WAS MEL'D (49-1) AND RETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO REPORT. APU SCHEDULED FOR REMOVAL & REPLACEMENT ON 09 NOV.02 2 L 7 2 4F 4 F A16WE E2EA 2002120600096 20021206 00096 WP 2002 12 6 GTIA021089 1 20020929 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FLOORBOARD LEFT INBOARD STATION 160 TO STATION 196 SOFT/MUSHY CORRODED. FABRICATED FLOOR PANEL. INSTALLED FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2002120600097 20021206 00097 WP 2002 12 6 GTIA021090 1 20020929 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FLOORBOARD LEFT INBOARD STATION 160 TO 196 CRACKED/DAMAGED AND CORRODED. FABRICATED NEW FLOORBOARD. INSTAL LED FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2002120600098 20021206 00098 WP 2002 12 6 GTIA021091 1 20020929 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FLOORBOARD RIGHT OUTBOARD STATION 196 TO 256 SOFT/MUSHY CORROSION. FABRICATED FLOORBOARD. INSTALLED FLOORB OARD. (M) 2 L 7 2 4F RT A6WE 2002120600099 20021206 00099 EU 2002 12 6 CA021110001 1 20021009 A 3320 F15T12WW LIGHT AIRBUS 310 A310300 3930305 EU CABIN BURNED OUT W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) IN CRUISE AT39 000 FT. COCKPIT CREW NOTICED A BURNING ODOR COMING FROM THE OVERHEAD PANEL. NOTHING CAME OUT OF TH E SNIFFER FAN (THE ODOR WAS NOTICED INTERMITTENTLY FOR 30 MINS. AND THEN STOPPED.). THE ODOR WAS NOTICED EQUALLY AT ROW 2 AND 15. TROUBLE SHOOTING WAS CARRIED OUT. ALL SYSTEMS POWERED THROUGHOUT CABIN. THE ONLY FAULT FOUND WAS AT DOOR L-1 ON THE OVER HEAD LIGHTING. ONE FLUORESCENT TUBE WAS BURNED OUT. TUBE REPLACED IAW MM 33-21-21 AND FOUND SERVICEABLE.(REF TO IPC 33-21-04 PAGE 625G ITEM 20) 2 L 7 2 4F RT A35EU 2002120600101 20021206 00101 WP 2002 12 6 GTIA021093 1 20020929 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FLIGHT COMPARTMENT, FLOOR PANEL STATION 120 TO STATION 160 CENTER SOFT/MUSHY CORROSION. FABRICATED NEW FLOORBOARD . INSTALLED NEW FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2002120600102 20021206 00102 WP 2002 12 6 GTIA021094 1 20020923 A 7110 5930645505 NOSE COWL DOUG DC9 DC983 3022083 WP RT ENGINE OVERHEATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND RIGHT ENGINE NOSE COWL INLET LIP HAS EVIDENCE OF OVERHEATING FROM 9 TO 8 O'CLOCK POSITION. REMOVED NR 2 ENG INE NOSE COWL. INSTALLED SERVICEABLE NOSE COWL. (M) 2 L 7 2 4F RT A6WE 2002120600103 20021206 00103 WP 2002 12 6 GTIA021095 1 20021001 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - E/E COMPARTMENT LONGERON 30 STATION 120 TO 133 HAS CORROSION FOUND ON REMOVAL OF BATTERY TRAY TO FOM. DRILLED NEW STRINGER 30, INSTALLED L30. (M) 2 L 7 2 4F RT A6WE 2002120600104 20021206 00104 WP 2002 12 6 GTIA021096 1 20020921 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND PASSENGER CABIN LEFT INBOARD SEAT TRACK WORN AND CORRODED FS 1012-1088. REMOVED LEFT INBOARD SEAT TRACK. L OCATED AND DRILLED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2002120600105 20021206 00105 WP 2002 12 6 GTIA021097 1 20020921 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND PASSENGER CABIN CENTER FLOOR PANEL FS 200 IS CAVED IN AND DELAMINATED. REMOVED FLOORBOARD. FABRICATED NEW FLOORBOARD. INSTALLED FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2002120600106 20021206 00106 WP 2002 12 6 GTIA021098 1 20020923 A 5320 SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - AFT PIT STATION 1322-1338 L23R, LONGERON SPLICE IS CORRODED. REMOVED LONGERON SPLICE. DRILLED AND LOCATED NEW LO NGERON SPLICE. INSTALLED NEW LONGERON SPLICE. (M) 2 L 7 2 4F RT A6WE 2002120600107 20021206 00107 WP 2002 12 6 GTIA021099 1 20020923 A 5312 BULKHEAD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - AFT PIT STATION 1338 L29R-L29L EXISTING T-CHORD REPAIR ON AFT SIDE OF FRAME HAS EXFOLIATION CORROSION. FOUND OUT OF LIMITS. REMOVED CORROSION ON BULKHEAD WEB AND LONGERON SUPPORT. FABRICATED WEB DOUBLER, REPAIR SPLICE, ANGLES AND S PLICERS. FABRICATED WEB DOUBLER, REPAIR SPLICE, ANGLES AND SPLICERS. LOCATED AND DRILLED NEW LONGERON SUPPORT FRAME, F ITTINGS AND ANGLES. INSTALLED ANGLE SUPPORTS, REINFORCING ANGLES, BULKHEAD SPLICE REPAIR WEB AND NEW FITTINGS. (M) 2 L 7 2 4F RT A6WE 2003010900032 20030109 00032 NM 2003 1 9 CA021110002 1 20021006 A 3246 431276E BOLT BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE MLG WHEEL SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING WALK AROUND INSPECTION, A MAIN WHEEL WAS FOUND WITH ONE TIE BOLT MISSING AND TWO OTHERS NOT SAFE (TORQUE WI SE). THEY COULD BE ROTATED USING HAND FORCE. ALL THE BOLTS AFFECTED WERE SIDE BY SIDE. UPON FURTHER INVESTIGATION THE FI NAL FINDINGS WERE: 1 BOLT WAS BROKEN OFF AND MISSING AND 2 BOLT WERE SHEARED BUT REMAINED IN PLACE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002120600108 20021206 00108 WP 2002 12 6 GTIA021100 1 20020923 A 5320 STRAP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND MID CARGO ST 628 SUB FRAME UPPER STRAP CORRODED UNDER SUPPORT. FABRICATED NEW STRAP. INSTALLED NEW STRAP. (M) 2 L 7 2 4F RT A6WE 2002120600109 20021206 00109 WP 2002 12 6 CA021110003 1 20021010 A 2497 71751006 CONTROL BOX LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE ELECTRICAL FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) CENTER CARGO LT SIDE CIRCUIT BREAKER ON CONTROL RELAY BOX ASSEMBLY POPPED WHEN RESELECTED (PUSHED IN), SPARKS OCCU RRED INSIDE OF THE CONTROL RELAY BOX NEAR LOWER CONNECTOR PLUG. THE CONTROL RELAY BOX ASSEMBLY WAS FOUND AT FAULT. PART WAS REPLACED AND THE AIRCRAFT WAS SENT BACK TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 2002120600110 20021206 00110 2002 12 6 CA021112002 4 20021008 A 2215 6224404101 SERVO CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT AILERON ACT FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 18561 (CAN) AILERON STIFFNESS DURING LAST 3000 FT OF APPROACH IN RAIN AILERON STIFFNESS DURING LAST 3000 FT OF APPROACH IN RAI N. PERFORMED GROUND INSPECTION DE-ICING FLUID ON BOTH AILERON PCU PANEL AND ON LT LOWER AILERON SERVO MOUNT ADJUSTMENT T EST FOUND SLIP-CLUTCH BREAKAWWAY TORQUE TO HIGH 70 POUND INCHES IAW AMM 22-11-11 AND AILERON SERVO WORN. PLS REPLACE MOU NT AND AILERON SERVO. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120600111 20021206 00111 NM 2002 12 6 C1HA200296016 1 20021109 A 3350 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 696CA 22574 EMERGENCY EXIT SIGN RT OF AFT AIRSTAIR EXIT 1 BULB OUT. RELAMPED 1 BULB EMERGENCY EXIT SIGN RIGHT OF AFT AIRSTAIR EXIT. 2 L 7 3 4F RT A3WE 2002120600112 20021206 00112 EA 2002 12 6 COMA0260682 1 20021204 A 3010 601R593201 SENSOR CNDAIR CL600 CL6002B19 1900309 EA L/H WING UNRELIABLE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 796CA 7338 FLIGHT 5403 ANTI-ICE DUCT WARNING.COULD NOT DUPLICATE - REPLACED ALL 21 L/H WING DUCT LEAK SENSORS. 2 L 7 2 4F RT A21EA 2002120600113 20021206 00113 EA 2002 12 6 COMA0260683 1 20021201 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S O AFFECT SYSTEMS OTHER CL CLIMB 1 SO 01 957CA 7109 FLIGHT 5150 DURING CLIMB, LOUD WIND NOISE AT CABIN DOOR. CABIN ALTITUDE CLIMBING RAPIDLY.COULD NOT DUPLICATE. INSPECTION OF DOOR FOUND NO DEFECTS. PRESSURIZATION CHECK WAS NORMAL. 2 L 7 2 4F RT A21EA 2002120600114 20021206 00114 EA 2002 12 6 COMA0260684 1 20021203 A 2150 32156221 VALVE CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 983CA 10021 7169 FLIGHT 5207 L/H AC HIGH PRESSURE WARNING DURING T/O.REPLACED THE L/H PRSOV. 2 L 7 2 4F RT A21EA 2002120600115 20021206 00115 EA 2002 12 6 COMA0260685 1 20021202 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 739CA 6844 7273 FLIGHT 5722 GEAR DISAGREE WARNINGREPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002120600116 20021206 00116 EA 2002 12 6 COMA0260686 1 20021130 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 739CA 4756 7273 FLIGHT 5018 GEAR DISAGREE WARNING WHEN GEAR SELECTED UP.REPLACED THE MLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2002120600117 20021206 00117 EA 2002 12 6 COMA0260687 1 20021203 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 920CA 7022 FLIGHT 5471 FLAPS FAILED AT 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01 2 L 7 2 4F RT A21EA 2002120600118 20021206 00118 EA 2002 12 6 COMA0260688 1 20021204 A 3297 WIRE CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 779CA 7306 FLIGHT 5201 ANTI-ICE DUCT WARNING - SYSTEM SELECTED OFF.REPAIRED CHAFED WIRING, R/H WING LEADING EDGE. 2 L 7 2 4F RT A21EA 2002120600119 20021206 00119 NM 2002 12 6 C1HA200283020 1 20021130 A 3350 900835A BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 683CA 22490 Ceiling emergency sign adjacent to the aft galley intermittent.Inspected and found low battery. Removed and replaced ba ttery in ceiling emergency exit sign adjacent to aft galley. 2 L 7 3 4F A3WE 2002120600120 20021206 00120 NM 2002 12 6 C1HA200283021 1 20021117 A 3350 6104789 BATTERY BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER UK UNKNOWN 1 GL 15 683CA 22490 Fwd emergency exit light flashing.Removed ant replaced battery in Fwd emergency exit light. 2 L 7 3 4F A3WE 2002120600121 20021206 00121 WP 2002 12 6 MEWA020723 1 20021206 A 5315 993653437 SUPPORT DOUG DC9 DC981 3022081 WP STA 160-200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 STATION 160 TO 200 FLOORBOARD SUPPORT 18" INBOARD FROM THE GALLEY DOOR HAS CORROSION. -- REMOVED AND REPLACED NEW SUPP ORT. 2 L 7 2 4F A6WE 2002120600122 20021206 00122 WP 2002 12 6 MWEA020724 1 20021206 A 5315 993653435 SUPPORT DOUG DC9 DC981 3022081 WP STA 180 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 STATION 180 FLOORBOARD SUPPORT FROM THE AIRCRAFT CENTERLINE OUTBOARD TO THE #4 SEAT TRACK HAS HEAVY CORROSION. -- REMO VED AND FABRICATED AND INSTALLED NEW PART. 2 L 7 2 4F A6WE 2002120600123 20021206 00123 WP 2002 12 6 GTIA021101 1 20020923 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND AFT CARGO PIT FS 1287-1309 RIGHT SIDE OUTBOARD SEAT TRACK SUB FLOOR WEB CRACKED AT LIGHTENING HOLE OR STIFFE NER HOLE, SEVERAL AREAS OF CORROSION AND MISSING OR PULLED FASTENERS. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2002120600124 20021206 00124 WP 2002 12 6 GTIA021102 1 20020924 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FORWARD CARGO FS 220 CEILING AREA WEB CRACKED RBL 46 INCHES. CUT OUT DAMAGED SECTION OF WEB. FABRICATED FILLER A ND DOUBLER. INSTALLED DOUBLER AND FILLER. (M) 2 L 7 2 4F RT A6WE 2002120600125 20021206 00125 2002 12 6 HALA0200569 4 20020927 A 2210 AUTOPILOT SYS DOUG DC10 DC1010 3022110 WP COCKPIT MALFUNCTIONED A HALA A UNSCHED LANDING F N FLT CONT AFFECTED FALSE WARNING CL CLIMB 1 WP 13 128AA 46984 FLT 11 - SFO - CLIMBING-OUT OF 9000 FEET FMA BRIEFLY SHOWED ALPHA SPEED AT 250 KTS LEVEL OFF FL360, NR 2 AUTOTHROTTLES D ROPPED OFF, NR 1 STILL FUNCTIONED. AT 1 MINUTE LATER, STICK SHAKER OCCURRED, FOLLOWED BY AUTO SLAT EXTENSION AT MACH .8 1.5. DESCENDED TO FL340. LEVEL AT 340 AND MACH .83 ANOTHER STICK SHAKER OCCURRED FOLLOWED BY AUTO SLAT EXTENSION. SLA T HAS BEEN RESET ON DESCENT TO FL340. ACCOMPLISHED ABNORMAL CHECKLIST AUTO SLAT EXTENSION, AIRPLANE CONFIRMED NOT IN ST ALL, ACCOMPANIED BY STICK SHAKER RETURNED TO SFO. (M) 2 L 7 3 4F A22WE 2002120600126 20021206 00126 NM 2002 12 6 USAA020382 1 20021003 A 5320 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 517AU 46662 23703 RON - FOUND Z-ANGLE CRACKED 2 INCHES, MLG W/W STIFFENER VERTICAL Z-ANGLE 663.75 BULKHEAD LBL 6.15. REPLACED Z-ANGLE IAW EA 75004. (M) 2 L 7 2 4F RT A16WE 2002120600127 20021206 00127 NM 2002 12 6 USAA020383 1 20021003 A 5320 ANGLE BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 46662 23234 PIT - FOUND Z-ANGLE CRACKED 2 INCHES, W/W FORWARD BULKHEAD LEFT CENTER VERTICAL Z-ANGLE. MANUFACTURED IAW EA 75003. (M) 2 L 7 2 4F RT A16WE 2002120600128 20021206 00128 NM 2002 12 6 USAABB02175 1 20021012 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AU 27807 MCO - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 18, 26, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M ) 2 L 7 2 4F RT A2NM 2002120600129 20021206 00129 NM 2002 12 6 USAABB02176 1 20021012 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AU 27807 MCO - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002120600130 20021206 00130 NM 2002 12 6 USAABB02177 1 20021015 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 605AU 22201 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 6 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2002120600131 20021206 00131 NM 2002 12 6 ASAA0210289 1 20021107 A 5330 6455866642 SKIN PANEL BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 743AS 21821 DURING SCHEDULED C CHECK FOUND SKIN PANEL AT BODY STATION 580, BUTTOCK LINE 0 CORRODED. REMOVED CORROSION AND REPAIRED SKIN PANEL IAW SRM. 2 L 7 2 4F 4 F A16WE E2EA 2002120600132 20021206 00132 NM 2002 12 6 ASAA0210290 1 20021107 A 5210 507945 SKIN BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE L1 DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 743AS 21821 DURING SCHEDULED C CHECK FOUND L1 DOOR SKIN AT BODY STATION 318, LBL 65 CRACKED. REMOVED CRACK AND REPAIRED L1 DOOR SKI N IAW SRM. 2 L 7 2 4F 4 F A16WE E2EA 2002120600133 20021206 00133 NM 2002 12 6 ASAA0210291 1 20021108 A 5320 6546579 STIFFENER BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 SW 23 743AS 21821 DURING SCHEDULED C CHECK FOUND APU INLET HORIZONTAL CHORDS AT BODY STATION 1088-1135, RIGHT REPAIRED CHORDS PER SRM. 2 L 7 2 4F 4 F A16WE E2EA 2002120600134 20021206 00134 WP 2002 12 6 ASAA0280370 1 20021014 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D15 52051 NE CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 977AS 53453 DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN, INOPERATIVE. REATTACHED LOOSE CONNECTORS. LIG HTS THEN OPERATED PROPERLY. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120600135 20021206 00135 WP 2002 12 6 ASAA0280459 1 20021026 A 5320 993061221 WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 CUSP WEB CORRODED FROM FUSELAGE STATION 1074 TO 1149. REPAIRED CORRODED SECTION IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120600136 20021206 00136 WP 2002 12 6 ASAA0282369 1 20021014 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D1 52044 NE CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 958AS 53024 DURING PREFLIGHT CHECK SOME EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN WERE FOUND TO BE INOPERATIVE. REATTACHED LOOSE CO NNECTORS. LIGHTS THEN OPERATED PROPERLY. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120600137 20021206 00137 WP 2002 12 6 ASAA0282460 1 20021026 A 5310 99364545 SHEAR TIE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 SHEAR TIE CORRODED IN AFT CARGO BAY AT FUSELAGE STATION 1098, L30-L29R. REPLACED SHEAR TIE IAW SRM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002120600138 20021206 00138 SO 2002 12 6 000229 1 20021126 A 3150 WARNING SYSTEM EMB 145 EMB145 3260210 SO COCKPIT ACTIVATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 288 NO TAKEOFF, CONFIG EICAS MESSAGE. RESET AC. 2 L 7 2 4F RT T00011AT 2002120600139 20021206 00139 NM 2002 12 6 2002F01062 1 20021202 A 3350 LIGHT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE CABIN INOPERATIVE G K NONE L NO TEST IN INSP/MAINT 1 GL 11 518AT 27974 DURING SCHEDULED MAINTENANCE EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 20 WOULD NOT TEST. 2 L 7 2 4F 4 F RT A2NM A12EU 2002120600140 20021206 00140 WP 2002 12 6 IXAA0200084S 1 20020729 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 83050 2948 45978 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AT FUSELAGE STATION 45 LONGERON 29L LOWER AREA. REPAIR ACCOMP LISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IAW THE DOUGLAS SRM. 2 L 7 4 4F RT 4A25 2002120600141 20021206 00141 WP 2002 12 6 DHL2002801021 1 20021206 A 2611 BULB DOUG DC8 DC873F 302199F WP A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 1) #14 SMOKE DETECTOR DOES NOT TEST.2) REMOVED AND REPLACED #14 SMOKE DETECTOR TEST LIGHT BULB. OPS CHECKED GOOD PER D C-8 M/M 26-10-6. 2 L 7 4 4F RT 4A25 2002120600142 20021206 00142 EA 2002 12 6 HNAA0200086 1 20021204 A 3234 574205A SELECTOR VALVE DHAV DHC8 DHC8311 1386006 EA INOPERATIVE A HNAA O OTHER O OTHER AP APPROACH 1 EA 07 342EN 17742 4634 395 LANDING GEAR WOULD NOT EXTEND NORMALLY. CREW USED ALTERNATE EXTENSION TO EXTEND GEAR. REPLACED LANDING GEAR SELECTOR VAL VE. 2 H 7 2 4T RT A13NM 2002120600143 20021206 00143 NM 2002 12 6 HNAA0200087 1 20021203 A 5542 85540001003 RUDDER DHAV DHC8 DHC8201 2809001 NM CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 969HA 8435 468 R/H SKIN OF FORE RUDDER HAS LARGE CRACK AT FIRST AND SECOND RIB BELOW TOP CLOSING RIB. REPLACED RUDDER. 2 H 7 2 4T RT A13NM 2002120600144 20021206 00144 WP 2002 12 6 IXXA0200077S 1 20020702 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 83050 2948 45978 DURING ROUTINE C-CHECK INSPECTION, GOUGES WERE DETECTED ON THE FUSELAGE SKIN ABOVE THE FORWARD UPPER CORNER OF THE AFT P IT DOOR CUT OUT, FUSELAGE STATION 1400, LONGERON 24 RT. REPAIR ACCOMPLISHED, BLENDING OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR EXTERNAL DOUBLER AND TRIPLER IAW DOUGLAS SRM. 2 L 7 4 4F RT 4A25 2002120600145 20021206 00145 WP 2002 12 6 IXXA0200078S 1 20020702 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 83050 2948 45978 DURING ROUTINE C-CHECK INSPECTION, A DENT WAS DISCOVERED ON THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 1560 LONGE RON 25R. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER AND FILLER IAW THE DOUGLAS SRM. 2 L 7 4 4F RT 4A25 2002120600146 20021206 00146 WP 2002 12 6 IXXA0200079S 1 20020702 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 83050 2948 45978 DURING ROUTINE C-CHECK INSPECTION, CRACKS AND CORROSION WERE DETECTED ON THE FUSELAGE AFT RIGHT DOOR UPPER AFT CUT OUT F USELAGE STATION 1660 LONGERON 11R. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA AND INTERNAL DOUBLERS. FABRICATION AND I NSTALLATION OF REPAIR FILLERS, DOUBLERS AND TRIPLERS IAW THE DOUGLAS SRM. 2 L 7 4 4F RT 4A25 2002120600147 20021206 00147 WP 2002 12 6 IXXA0200080S 1 20020702 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 83050 2948 45978 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE SEAM LONGERON 11L F/S 1620. REMOVED CORROSION, SEALED AREA, IAW THE DOUGLAS SRM. 2 L 7 4 4F RT 4A25 2002120600148 20021206 00148 WP 2002 12 6 IXXA0200082S 1 20020704 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 83050 2948 45978 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DISCOVERED ON THE FUSELAGE SKIN AT FUSELAGE STATION 35 LONGERON 33R. R EPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR FILLER AND DOUBLER IAW THE DOUGLAS S RM AND EA 28276-5384-02-111. 2 L 7 4 4F RT 4A25 2002120600149 20021206 00149 WP 2002 12 6 IXXA0200083S 1 20020707 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 83050 2948 45978 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FORWARD CARGO COMPARTMENT AFT DOOR SKIN TOP REAR AREA A T FUSELAGE STATION 557.5 AND LONGERON 27R. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR FILLER AND DOUBLER IAW THE DOUGLAS SRM. 2 L 7 4 4F RT 4A25 2002120600150 20021206 00150 EU 2002 12 6 U30A200200030 1 20021201 A 2530 72073750 OVEN AIRBUS 320 A320214 3930316 EU AFT CENTER OVEN SPARKS A U30A O OTHER O OTHER CR CRUISE 1 EA 17 261AV * * 1615 During Cruise on Flt 256 EWR - PUJ, the Flight Attendant reported a spark coming out of aft center oven. Flt crew turned oven of and pulled circuit breaker immediatley. On ground at PUJ, Maintenance performed an operational check I/A/W AMM 25-35-00-501 with no defects noted. The oven was not used and circuit breaker remained open for the return trip back to EWR (Flt 257). Upon return to EWR the aft center oven was deactivated and deferred per MEL 25-22-03 for precautionary me asures. The electrical connections displayed no evidence of arcing or burning.The oven will be removed and sent out for operational checks and repair. 2 L 7 2 4F RT A28NM 2002120600151 20021206 00151 WP 2002 12 6 AALA20021362 1 20020925 A 5200 BEAM DOUG DC9 DC982 3022082 WP DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND FORWARD END OF TOP HORIZONTAL BEAM IS CRACKED. INSTALLED BEAM MODIFICATION PER SRM 52-05. (M) 2 L 7 2 4F A6WE 2002120600152 20021206 00152 SO 2002 12 6 RAIA00211332 1 20021124 A 2436 51545001B GCU EMB 145 EMB145 3260210 SO MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 807HK 2665 145119 5282-PIT- LEFT GENERATOR OFF LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE GENERATOR CONTROL UNIT, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002120600153 20021206 00153 2002 12 6 RAIA00211333 4 20021126 A 3140 350A52005099 COMPUTER AEROSP ATR72 ATR72202 8680940 EU A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 723TE 10875 87 283 5585-STL- RECEIVED EMERGENCY BATTERY CHARGING FAULT INDICATION. MAINTENANCE REMOVED AND REPLACED THE MULTI FUNCTION COMP UTER, OPS CK OK, 2 H 7 2 4T RT A53EU 2002120600154 20021206 00154 SO 2002 12 6 RAIA00211337 1 20021128 A 8012 32153582 CONTROL VALVE EMB 145 EMB145 3260210 SO INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 806HK 3737 285 145112 5321-PIT- RIGHT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE STARTER CONTROL VALVE, OPS CK O K. 2 L 7 2 4F RT T00011AT 2003011600225 20030116 00225 2003 1 16 RAIA00212340 4 20021204 A 3425 7003360948 COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAULTY A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 564HK 13416 3789 41081 5610-STL- PITCH AND ROLL COMPARATOR ERROR INDICATION. MAINTENANCE REMOVED AND REPLACED THE NR 1 AHRS COMPUTER, OPS CHEC K OK. 2 L 7 2 4T RT A41NM 2002120600155 20021206 00155 EU 2002 12 6 RAIA00211338 1 20021127 A 7931 8210181 OVRSPEED LIMITER AEROSP ATR42 ATR42300 8680920 EU NICKED A RAIA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CE 03 423TE 17632 6656 119 5533-PIA- RIGHT ENGINE OIL PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED OVER SPEED GOVERNOR AND GASKET DO TO DAMAGED M OUNTING FLANGE. 2 H 7 2 4T RT A53EU 2002120600156 20021206 00156 EU 2002 12 6 RAIA00211339 1 20021130 A 2750 2659A4TT CHECK VALVE JETAIR JETSTM JETSTM4101 1500501 EU LEAKING A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 562HK 41078 5350-RIC- FLAPS STUCK AT 9 DEGREES. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY SELECTOR CHECK VALVE, OPS AND LK CK O K. 2 L 7 2 4T RT A41NM 2002120600157 20021206 00157 EU 2002 12 6 RAIA00212342 1 20021204 A 3060 B5JFR36C1103DE PROPELLER JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 554HK 12767 2933 41067 5574-STL- LEFT PROP HEAT FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED LEFT PROPELLER, LK AND OPS CK OK. 2 L 7 2 4T RT A41NM 2002120600158 20021206 00158 EU 2002 12 6 RAIA00212343 1 20021204 A 3010 8485020A CONTROL BOX AEROSP ATR42 ATR42300 8680920 EU INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 423TE 19703 11857 119 5620-STL- AIRFRAME DE-ICE FAULT INDICATION. MAINTENANCE REMOVED AND REPLACED THE DE-ICE CONTROLLER, OPS CK OK. 2 H 7 2 4T RT A53EU 2002120600159 20021206 00159 NE 2002 12 6 RAIA00211331 2 20021123 A 7421 CH34687 IGNITER AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 424TE 124 121372 5465-BMI- LEFT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED BOTH IGNITERS. 2 H 7 2 4T 4 T RT A53EU E20NE 2002120900001 20021209 00001 NE 2002 12 9 CA021112003 2 20021110 A 7200 ENGINE BOEING 757 757* NM RROYCE RB211 RB211535E4 54555 NE RIGHT FOD W E C ENGINE SHUTDOWN ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 CA (CAN) ABORTED TAKEOFF FROM THE NEW YORK AREA. FLIGHT CREW HEARD THE RIGHT ENGINE SURGE AND PASSENGERS REPORTED FLAMES C OMING OUT THETAIL PIPE. THE TAKE-OFF WAS ABORTED UNEVENTFULLY AT APPROXIMATELLY 100KTS, ENGINE WAS SUSEQUENTLY S HUT DOW N AND AIRCRAFT RETURNED TO GATE. CUSTOMER REPORTED FOD OF IPC AND/OR POSSIBLY THE HPC FORWARDSTAGES AFTER BOROSCOPE INSP ECTION. CAUSE OF FOD UNKNOWN AND ENGINE REMOVED. ENGINE HOURS AND CYCLES NOT KNOWN AT THIS TIME. 2 L 7 2 4F 4 F RT A2NM E12EU 2002120900003 20021209 00003 EA 2002 12 9 CA021112006 1 20021108 A 5610 601R3303312 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COCKPIT FAILED W A UNSCHED LANDING D INFLIGHT SEPARATION AP APPROACH 1 CA (CAN) COPILOT SIDE WINDOW MIDDLE LAYER SHATTERED (CRACKED) WHILE AIRCRAFT WAS ON APPROACH . UNEVENTFUL LANDING COMPLETED AFTER USUAL QRH PROCEDURES FOLLOWED. NO GAP FOUND AROUND CONTOUR AT REMOVAL OF WINDSHIELD. PART REPLACED BY NEW ONE. CO NDITIONS: 1700Z, VMC, 020/03, 29.67HG, +4C, 10K VIS.A/S 200 KIAS, 1500 FT, MLG UP, FLAPS/SLATS 0 DEG. SPOILERS STOWED, A UTOPILOT OFF.END. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2002120900005 20021209 00005 NE 2002 12 9 CA021113001 2 20021020 A 7310 3035987 LINE DHAV DHC8 DHC8301 1386003 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE ENGINE FUEL WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AFTER SCHEDULED ENGINE REMOVAL , DURING ENGINE SHOP INSPECTION , TUBE FOUND WORN, WHERE TUBE PASSES THROUGHT FIREW ALL GROMMET/FIRESEAL RING . 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002120900006 20021209 00006 NM 2002 12 9 CA021113002 1 20021020 A 2820 30347156 VENT DHAV DHC8 DHC8301 1386003 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE FIREWALL WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AFTER SCHEDULED ENGINE REMOVAL , DURING ENGINE SHOP INSPECTION , TUBE FOUND WORN, WHERE TUBE PASSES THROUGH FIREWA LL GROMMET/FIRESEAL RING . 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002120900008 20021209 00008 EA 2002 12 9 CA021114001 1 20021109 A 2750 1104SD100401 SHAFT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RT TE FLAPS SHEARED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 CA 14942 (CAN) ON APPROACH, FLAP FAIL MSG AT 0 DEG. LOCAL MECHANIC TRIED TO MECHANICALLY REPOSITION FLAPS TO 8 DEG FOR FERRY FL T RT OUTBOARD FLAP SURFACE INCURRED SOME TWISTING (SKIN RIPPLING). FOUND NR 4 FLEX DRIVE UNRAVELLED WITH OUTBOARD DRIVE END BROKEN OFF (AT NR 4 SCREWJACK). 2 L 7 2 4F 4 F RT A21EA E15NE 2002120900009 20021209 00009 EA 2002 12 9 CA021114002 1 20021104 A 5610 NP1393219 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W O OTHER O OTHER DE DESCENT 1 CA 16410 (CAN) CAPTAIN'S WINDSHIELD CRACKED DESCENDING.APPEARED TO BE AN ELECTRICAL SHORT LOW IN THE WINDSHIELD AT THE CENTER PRI OR TO THE CRACK.REMOVED AND REPLACED LEFT WINDSHIELD WITH SERVICEABLE UNIT IAW MM 56-11-01. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120900010 20021209 00010 EA 2002 12 9 CA021114003 1 20021112 A 5610 NP13932110 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) RT WINDSHIELD CRACKED DURING CRUISE. A/C DIVERTED WHERE THE WINDSHIELD WAS REPLACED REPLACEMENT WINDSHIELD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120900011 20021209 00011 SW 2002 12 9 CA021114004 1 20021114 A 2750 19023 CONTROL CABLE BBAVIA 8 8GCBC 1220803 SW LYC O360 O360C2E 41514 EA TE FLAP CONTROL FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CABLE FRAYED AT WING ROOT PULLEY- STAINLESS STEEL CABLE 1 H 7 1 3O 3 O A21CE E286 2002120900013 20021209 00013 NM 2002 12 9 CA021114006 1 20021112 A 3221 69634801 BOLT BOEING 727 727260 NM PWA JT8 JT8D17 52049 NE RT MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AT C-CHECK. WHILE PERFORMING FWD MLG TRUNION FITTING REPLACEMENT ON THE RT MLG. TECH NOTICED NO SHIMS WERE INSTAL LED BETWEEN FWD TRUNNION BEARING AND TRUNNION LINK TO OBTAIN REQUIRED 0.00 TO 0.003 INCH CLEARANCE. NO MEARSURMENT WAS T AKEN DUE TO FWD TRUNNION REPLACEMENT REQUIRES SHIM CLEARANCE BE RESET. AFTER TRUNNION LINK REMOVAL, SHOCK STRUT SHIFTE D FORWARD AT THE AFT BEARING. WHILE TRYING TO REPOSITION THE SHOCK STRUT, SHOCK STRUT DISENGAGED FROM THE AFT BEARING AL LOWING THE SHOCK STRUT TO FALL FORWARD AND FREE FALL FROM AIRCRAFT. UPON EXAMINATION, AFT TRUNNION FUSE BOLT SHANK WAS F OUND CRACKED THRU AT BOLT HEAD AREA, TRUNNION BEARING UNI-BALL FOUND CRACKED, AND SHOCK STRUT AFT TRUNNION CRACKED. 2 L 7 3 4F 4 F RT A3WE E2EA 2002120900016 20021209 00016 CE 2002 12 9 CA021114010 1 20021112 A 5520 115610010125 STRUCTURE BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 18097 (CAN) DURING INSPECTION, THE TRAILING EDGE SPLINE ON THE ELEVATORS WERE FOUND CRACKED AT SEVERAL LOCATIONS, THIS IS THE 4TH SDR REGARDING THIS SPLINE. THE ELEVATORS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE 1 L 7 2 3T 4 T A14CE E4EA 2002120900018 20021209 00018 EA 2002 12 9 02340621 1 20021206 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 621BR 7186 During preflight inspection at RDU, the crew reported that the R/H forward emergency exit light was inoperative. Repair was initially deferred iaw the MEL. Later at ORD, maintenance personnel removed and replaced the lamp in the R/H forwa rd emergency exit light. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002120900020 20021209 00020 WP 2002 12 9 CA021115003 1 20020927 A 2910 HOSE DOUG DC4 C54GDC 3021534 WP PWA R2000 D3 52023 NE HYD SYSTEM LEAKING W O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CA (CAN) HYDRAULIC PRESSURE HOSE WAS LEAKING. 2 L 7 4 4R 4 R A762 E230 2002120900021 20021209 00021 NM 2002 12 9 VNAA0212010 1 20021205 A 3000 851003 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 429JS 18786 5969 3043 THE CREW RECEIVED A RIGHT HAND AIRFOIL DE-ICE FAIL AND REPORTED IT TO MAINTENANCE CONTROL. FLIGHT 4055 WAS THEN ADVISED TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EJECTOR FLOW CONTROL VALVE IN ACCORDANCE WITH DORNIER MAINTEN ANCE MANUAL 30-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120900022 20021209 00022 NM 2002 12 9 VNAA0212009 1 20021122 A 2100 22260A030201 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 437JS 2630 2498 3055 THE CREW REPORTED THAT THE PRESSURIZATION FAILED AND RECEIVED AN AUTO MODE CABIN ALTITUDE CAS MESSAGE. MAINTENANCE INS PECTED AND REPLACED THE CPCS CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WE RE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120900023 20021209 00023 NM 2002 12 9 VNAA0212006 1 20021204 A 3000 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 441JS 3059 DURING THE CLIMB OUT, THE CREW RECEIVED A CAPTAIN'S WINDSHIELD HEAT FAIL AND RETURNED TO PIT. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE WILL REPLACE THE WINDSHIELD AND COMPLY WITH SERVICE BULLETIN 328-30-206. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120900024 20021209 00024 NM 2002 12 9 VNAA0212005 1 20021204 A 3000 SCREW DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 441JS 3059 WHILE ENROUTE TO EVV, THE CREW RECEIVED A CAPTAIN'S WINDSHIELD HEAT FAIL CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE I NSPECTED AND CLEANED THE WINDSHIELD SCREWS AND RESEALED THE WINDSHIELD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30- 00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120900025 20021209 00025 NM 2002 12 9 VNAA0211033 1 20021128 A 2400 1030200 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 439JS 18505 3057 DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND DC GENERATOR FAIL CAS MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECT ED AND REPLACED THE RIGHT HAND HALL EFFECT SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL C HECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120900026 20021209 00026 NE 2002 12 9 VNAA0212001 2 20021201 A 7300 8110994L27 HMU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RH FAILED A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 430JS 15797 3794 3044 ENROUTE FROM PIT TO TYS, THE CREW EXPERIENCED A TORQUE JUMP DURING FUEL CROSS FEED AND MAINTENANCE CONTROL ADVISED THE C REW TO RETURN TO PIT. MAINTENANCE ISNPECTED AND REPLACED THE HYDROMECHANICAL UNIT IN ACCORDANCE WITH DORNIER MAINTENANC E MANAUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002120900027 20021209 00027 NM 2002 12 9 SWAA022797 1 20021127 A 5330 6545768 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 308, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002120900028 20021209 00028 NM 2002 12 9 SWAA022802 1 20021126 A 5523 65C2638415M TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, LEFT ELEVATOR NR 3 AND NR 4 HINGE ATTACH POINTS WORN. REMOVED AND REPL ACED LEFT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002120900029 20021209 00029 2002 12 9 SWAA022803 4 20021126 A 2565 6557463 RETAINER BOEING 737 7373H4 1384600 NM AFT SVC DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. SECURED RETAINER PER MM. 2 L 7 2 4F RT A16WE 2002120900030 20021209 00030 NM 2002 12 9 SWAA022807 1 20021201 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002120900031 20021209 00031 NM 2002 12 9 SWAA022808 1 20021127 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 DURING SCHEDULED C4 CHECK, FOUND SEVERAL COVERS CRACKED BETWEEN ROW NR 1 AND ROW NR 22. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002120900032 20021209 00032 NM 2002 12 9 SWAA022811 1 20021129 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CRACKED AT BS 598, STRINGER 15R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2002120900033 20021209 00033 2002 12 9 SWAA022813 4 20021129 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM BOTH ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED C1 CHECK, FOUND BOTH CABIN ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2 L 7 2 4F RT A16WE 2002120900034 20021209 00034 2002 12 9 SWAA022814 4 20021129 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002120900035 20021209 00035 2002 12 9 SWAA022817 4 20021130 A 2565 6557463 BRACKET BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 720WN 27854 DURING SCHEDULED C3 CHECK, FOUND LOOSE FASTENER AT FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKET. REMOVED AND REPLACED FASTENER PER SRM. 2 L 7 2 4F RT A16WE 2002120900036 20021209 00036 NM 2002 12 9 SWAA022822 1 20021129 A 5330 6545785 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 086SW 22827 DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUTS CRACKED AT LT WINDOWS NR 2, NR 6, NR 8 AND NR 26. REPAIRED SKI N PER BFG ER AND SRM. 2 L 7 2 4F A16WE 2002120900037 20021209 00037 NM 2002 12 9 SWAA022823 1 20021201 A 5230 6545871 FRAME BOEING 737 7373A4 1384585 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR CRACKED ON UPPER FRAME BEHIND PULLEY BRACKET. REMOVED AND REPLACED F RAME PER SRM. 2 L 7 2 4F RT A16WE 2002120900038 20021209 00038 NM 2002 12 9 SWAA022824 1 20021130 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, LT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED LT E LEVATOR TAB NR 2, NR 3 AND NR 4 HINGE HARDWARE AND BUSHINGS PER MM AND SWA SI. 2 L 7 2 4F RT A16WE 2002120900039 20021209 00039 NM 2002 12 9 SWAA022825 1 20021130 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, RT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACE RT EL EVATOR TAB NR 2 AND NR 4 HINGE HARDWARE AND BUSHINGS PER MM AND SWA SI. 2 L 7 2 4F RT A16WE 2002120900040 20021209 00040 NM 2002 12 9 SWAA022826 1 20021130 A 7930 1032698 TRANSMITTER BOEING 737 7372H4 138448C NM JT8 JT8D9 52048 NE NR 2 ENGINE FAULTY A SWAA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION UK UNKNOWN 1 SW 29 081SW 22730 707374 IN-FLIGHT SHUTDOWN, AIR TURNBACK, SHUT DOWN NR 2 ENGINE DUE TO OIL FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACE D OIL FILTER AND FILTER BYPASS TRANSMITTER PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2002120900041 20021209 00041 NM 2002 12 9 SWAA022829 1 20021201 A 5311 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, RBL 10. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002120900042 20021209 00042 NM 2002 12 9 SWAA022830 1 20021201 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002120900043 20021209 00043 NM 2002 12 9 SWAA022833 1 20021202 A 5230 6547952 SKIN BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED PM CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2002120900044 20021209 00044 NM 2002 12 9 SWAA022834 1 20021201 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD CRACKED (5 EA) RADIATING FROM RIVETS AT THE PERIPHERY OF THE PRESS P LUG. REPAIRED BULKHEAD PER SWA EA 2 L 7 2 4F A16WE 2002120900045 20021209 00045 2002 12 9 SWAA022835 4 20021202 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM CABIN DOORS MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED C2 CHECK, FOUND BOTH FWD ENTRY AND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLES MISROUTED. REROUTED CABLES PER MM. 2 L 7 2 4F RT A16WE 2002120900046 20021209 00046 2002 12 9 SWAA022836 4 20021203 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002120900047 20021209 00047 NM 2002 12 9 SWAA022839 1 20021202 A 7603 208055 CABLE BOEING 737 7372H4 138448C NM NR 1 ENGINE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 071SW 22358 DURING SCHEDULED RON, FOUND NR 1 ENGINE THRUST CONTROL TELEFLEX CABLE WORN. REMOVED AND REPLACED NR 1 ENGINE THRUST CON TROL TELEFLEX CABLE PER MM. 2 L 7 2 4F A16WE 2002120900048 20021209 00048 NM 2002 12 9 SWAA022841 1 20021203 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 17R. REPAIRED SKIN PER BFG ER. 2 L 7 2 4F RT A16WE 2002120900049 20021209 00049 NM 2002 12 9 SWAA022842 1 20021203 A 5753 6546434302 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED C4 CHECK, FOUND RT INBD AFT T/E FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED RT INBD AFT T/ E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002120900050 20021209 00050 2002 12 9 SWAA022844 4 20021203 A 2565 65C19901 CABLE BOEING 737 7375H4 138449D NM AFT SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002120900051 20021209 00051 NM 2002 12 9 SWAA022846 1 20021204 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 SEVERAL EEPLS COVERS BROKEN IN CABIN. REMOVED AND REPLACED LIGHT ASSY'S AND REPAIRED WIRES PER MM. 2 L 7 2 4F RT A16WE 2002120900052 20021209 00052 NM 2002 12 9 SWAA022847 1 20021203 A 2750 6550324 TRANSMISSION BOEING 737 7373K2 13844BA NM RT/LT WING FAULTY A SWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 29 340LV 23738 FLAPS WOULD NOT DEPLOY WHEN THE FLAP LEVER WAS POSITIONED OUT OF THE UP POSITION. ALTERNATE FLAP SWITCH WAS USED TO SEL ECT FLAPS 15 DEGREES FOR LANDING. REMOVED AND REPLACED NR 4 AND NR 5 FLAP TRANSMISSIONS PER MM. 2 L 7 2 4F RT A16WE 2002120900053 20021209 00053 NM 2002 12 9 DL733021065 1 20020912 A 5415 311A11111 BEAM BOEING 737 737347 1384647 NM NR1 & NR2 PYLON WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305WA 23346 WORN AREAS WERE FOUND IN THE CROWN BEAM LUG BORES ON THE NR 1 AND NR 2 PYLONS. THE WORN AREAS WERE REMOVED BY OVERSIZIN G THE LUG BORES ON THE NR 1 AND NR 2 PYLON. OVERSIZED BUSHINGS WERE INSTALLED IN THE BORES. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2002120900054 20021209 00054 NM 2002 12 9 DL733021087 1 20020916 A 5551 6549925507 FITTING BOEING 737 737347 1384647 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305WA 23346 CORROSION WAS FOUND ON THE RT INBOARD LUG BORE ON THE HORIZONTAL STABILIZER CENTER SECTION UPPER FITTING. THE BORE WAS OVERSIZED AND A REPAIR BUSHING INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2002120900055 20021209 00055 NM 2002 12 9 DL733021102 1 20020918 A 5553 65468725 FITTING BOEING 737 737347 1384647 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305WA 23346 CORROSION WAS FOUND ON THE AFT FACE OF THE NR 3 LUG AND THE FORWARD FACE OF THE NR 6 LUG OF THE VERTICAL STABILIZER FIN ATTACH LUG. THE BUSHINGS WERE REPLACED WITH THICKER FLANGES 2 L 7 2 4F RT A16WE 2002120900056 20021209 00056 NM 2002 12 9 DL733021125 1 20020923 A 5553 FITTING BOEING 737 737347 1384647 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305WA 23346 CORROSION WAS FOUND ON THE LUG BORES AND FACES OF THE VERTICAL STABILIZER ATTACH LUGS. THE BORE DIAMETERS WERE INCREASE D AND THE FACES BLENDED. OVERSIZED BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND HMV. 2 L 7 2 4F RT A16WE 2002120900057 20021209 00057 NM 2002 12 9 DL733021191 1 20021013 A 3040 5893543130RPR WINDOW BOEING 737 737347 1384647 NM COCKPIT DEFECTIVE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 305WA 23346 HAD ARCING AT POWER WIRE FOR FO WINDSHIELD WINDOW HEAT. REPLACED WINDOW. 2 L 7 2 4F RT A16WE 2002120900058 20021209 00058 NM 2002 12 9 DL733021266 1 20021030 A 3350 20131A BATTERY PACK BOEING 737 737347 1384647 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 305WA 23346 FIRST 5 ROWS OF EMERGENCY EXIT LIGHTS NOT WORKING. REPLACED BATTERY PACK, OP CKS NORMAL. 2 L 7 2 4F RT A16WE 2002120900059 20021209 00059 NM 2002 12 9 DL733021304 1 20021108 A 3350 RPS1 POWER SUPPLY BOEING 737 737347 1384647 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 305WA 23346 EMERGENCY SEAT LIGHTS NOT WORKING FROM ROWS 1-12. REPLACED POWER SUPPLY UNIT. LIGHTS OPS NORMAL. 2 L 7 2 4F RT A16WE 2002120900060 20021209 00060 NM 2002 12 9 DL733021340 1 20021119 A 5753 6546486150 FLAP BOEING 737 737347 1384647 NM WING DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305WA 23346 INBOARD MID FLAP WAS FOUND DAMAGED BEYOND ALLOWABLE LIMITS. REPAIR PER ER/A 417941-14. 2 L 7 2 4F RT A16WE 2002120900062 20021209 00062 NM 2002 12 9 DL733021346 1 20021120 A 5711 654532422 SPAR BOEING 737 737347 1384647 NM WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 WHILE REPLACING THE MLG BEAM SUPPORT FITTING A FASTENER HOLE WAS DAMAGED IN THE REAR SPAR CHORD AND REAR SPAR WEB. THE HOLE WAS OVERSIZED AND A REPAIR BUSHING INSTALLED. 2 L 7 2 4F RT A16WE 2002120900063 20021209 00063 2002 12 9 CA021115005 4 20021013 A 8300 1176625001 SHIELD BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ACCESSORY G/B CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACKS AT LT ENGINE AFT FIRE SHIELD ASSEMBLY AT AREA AROUND ACCESSORY GEARBOX VENT BULKHEAD FITTING. 1 G 7 2 3U 3 U H13EU E5NE10 2002120900065 20021209 00065 EA 2002 12 9 CA021115007 1 20021113 A 2910 AE4096G0060000 HOSE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE HYD SYSTEM DETERIORATED W O OTHER K FLUID LOSS CR CRUISE 1 CA (CAN) NR 3 HYDRAULIC SYSTEM LEAK AND QUANTITY DEPLETED TO ZEROAIRCRAFT WAS DIVERTED TO YUL FOR REPAIRS AND GEAR WAS VERY SLOW TO EXTEND. HYDRAULIC HOSE ASSY ON ACMP 3B FOUND LEAKING. HOSE ASSY, 3B HYD PUMP AND CASE DRAIN FILTERS REPLACED. LANDING GEAR RETRACTION TEST AND LEAK CHECK TEST COMPLETED CHECKING SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002120900067 20021209 00067 NE 2002 12 9 DL733021354 2 20021121 A 7200 CFM563 ENGINE BOEING 737 737347 1384647 NM GE CFM56 CFM563B1 13802 NE NR 1 MAKING METAL A DALA O OTHER Y ENGINE STOPPAGE CL CLIMB 1 SO 27 303WA 7923 23183 860155 CLIMBING THROUGH FL240, NR 1 ROLLED BACK TO 0 INDICATIONS AFTER LOUD BANG. ENG FAIL CK LIST WAS COMPLETED. METAL IN TA IL PIPE, ENG CHANGED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002120900068 20021209 00068 NM 2002 12 9 DL73K021082 1 20020912 A 3830 16007045 DIAPHRAGM BOEING 737 737232 1384475 NM FWD LAV TANK MISSING A DALA A UNSCHED LANDING C S E F.O.D. AFFECT SYSTEMS VIBRATION/BUFFET CR CRUISE 1 SO 27 318DL 23090 IRR/ NR 2 ENG HIGH VIBES AT FL 350. FLT DIVERTED TO RDU. VISUAL INSP FOUND EXTENSIVE FAN DAMAGE AND BLUE ICE COMING FR OM FWD LAV SVC PANEL AND BLUE STAINS AT NR 2 ENG INLET. NR 2 ENG REPLACED RDU PER TRANS 3T214AD. FOUND FWD LAV TANK FI LL VALVE LINE CHECK VALVE MISSING ITS DIAPHRAGM. REPLACED SAME. PRESSURIZED AIRCRAFT AND LEAK CHECKED. NO LEAKS FOUND . 2 L 7 2 4F RT A16WE 2002120900070 20021209 00070 NE 2002 12 9 CA021115011 2 20021111 A 7230 ENGINE BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE NR 2 FAILED W C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 CA (CAN) DURING TAKEOFF AT HIGH SPEED, CREW EXPERIENCED TWO BANGS. TAKEOFF REJECTED AT 140 KNOTS. NR 2 ENGINE REPLACED AND HIGH ENERGY STOP INSPECTION CARRIED OUT AS PER MM 05-51-11 PARA D. 2 L 7 2 4F 4 F A16WE E2EA 2002120900071 20021209 00071 NM 2002 12 9 DL73K021178 1 20021008 A 2121 214991949 GASPER FAN BOEING 737 737247 138448D NM CARGO BAY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 244WA 23518 ON ARRIVAL PBI CREW OFF FLT 2309 REPORTED UNIDENTIFIABLE ODOR THROUGHOUT THE AIRCRAFT. AIRCRAFT WAS CARRYING HUMAN REMA INS, AND CREW SUSPECTED THIS TO BE THE SOURCE OF THE ODOR. BOTH MTC AND GROUND CREW INSPECTED CARGO COMPARTMENTS AND FO UND CLEAN. GRD CREW REPORTED REMAINS WERE LOADED PER DELTA STANDARDS, AND NO LEAKS WERE NOTED. CREW REFUSED FLIGHT. M TC REPLACED GASPER FAN AND AIRED CABIN. REMOVED FAN BEARINGS WERE FOUND TO BE WORN AND FAN SMELLED OF BURNING INSULATIO N. 2 L 7 2 4F A16WE 2002120900072 20021209 00072 NM 2002 12 9 DL73K021188 1 20021011 A 2131 7638101 CONTROLLER BOEING 737 737232 1384475 NM CABIN PRESSURE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 321DL 23093 DURING CLIMB CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE ABOVE 10000 FT CABIN VSI +500/MIN IN AUTO MODE WITH NO WARNING LIGHTS OR FAILURE OF AUTO MODE SHOWING. CABIN ALTITUDE CONTROLLED WITH MANUAL CONTROL. REPLACED CABIN PRESS C ONTROLLER AND CONTROL PANEL PER M/M AND PERFORMED OPERATIONAL TEST AND CABIN LEAK DOWN CHECK NTF. 2 L 7 2 4F RT A16WE 2002120900073 20021209 00073 EU 2002 12 9 CA021115012 1 20021114 A 2782 830A000002 ACTUATOR AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE TE FLAPS FAILED W K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 CA (CAN) ON APPROACH YVR WHEN FLAP SELECTED 'F/CTL SLAT FAULT' MASSAGE APPEARING AND SLATS FAILED TO OPERATE.LT NR 2 SLAT A CTUATOR TORQUE LIMITER INDICATOR FOUND POPPED. R/H OUTBD. SLAT ACTUATOR 6029 CM REPLACED AS PER AMM 27-84-49 AND SLAT FU NCTION CHECKED SERVICEABLE.NOTE: SHOP REPORT REQUESTED. 2 L 7 2 4F 4 F RT A28NM E29NE 2002120900074 20021209 00074 EA 2002 12 9 COMA0260689 1 20021202 A 5210 DOOR LATCH CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 952CA 7092 FLIGHT 5103 CABIN DOOR WARNING DURING FLIGHT.ADJUSTED CABIN DOOR LATCH MECHANISM. 2 L 7 2 4F RT A21EA 2002120900075 20021209 00075 EA 2002 12 9 COMA0260690 1 20021205 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 484CA 7702 FLIGHT 5661 FLAPS FAILED DURING TAXI.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002120900076 20021209 00076 EA 2002 12 9 COMA0260691 1 20021205 A 5210 DOOR LATCH CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 967CA 7134 FLIGHT 5287 CABIN DOOR LATCH CAUTION MESSAGE.ADJUSTED DOOR LATCH MECHANISM. 2 L 7 2 4F RT A21EA 2002120900077 20021209 00077 EA 2002 12 9 COMA0260692 1 20021205 A 3080 DETECTOR CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 914CA 7012 FLIGHT 6029 ICE-CAUTION MESSAGE DURING T/O.DEFERRED MAINT. ON #1 ICE DETECTOR PER MEL. 2 L 7 2 4F RT A21EA 2002120900078 20021209 00078 EA 2002 12 9 COMA0260693 1 20021205 A 2750 852D100911 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA L/H UNRELIABLE A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 936CA 8369 7043 FLIGHT 5489 FLAPS FAIL MESSAGE.REPLACED THE L/H INBD FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 2002120900081 20021209 00081 EU 2002 12 9 CA021115015 1 20021106 A 5210 1371113C401 HINGE BAG JETSTM JETSTM3212 1500217 EU GARRTT TPE331 TPE33110U 01514 WP ROTOL R333 R333482F12 GL PAX DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 20771 (CAN) WHEN DOOR HINGE WAS REMOVED FOR MAINTENANCE CRACKS WERE FOUND RUNNING TO THE OUTSIDE OF HINGE FROM THE 2 HOLES CLO SEST TO THE BEARING END. 3 AIRCRAFT WERE CHECKED AND 2 WERE FOUND WITH CRACKS SB 52-JM5319 ADDRESSES THIS PROBLEM BUT I T IS NOT A MANDITORY INSP. 2 L 7 2 4T 4 T RT BA15CAA E4WE 6 C P61GL 2002120900082 20021209 00082 EA 2002 12 9 CA021115016 1 20021107 A 5530 C6FSM181829 PLATE DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION OF AFT FUSELAGE TO FIN ATTACH ADAPTER PLATES AS PER CF-99-11. THE AFT PLATE WAS FOUND CRACKED AT STA 535. ALL ADAPTER PLATES ARE THE POST MODIFICATON TYPE OF A MORE CORROSION RESISTANT MATERIAL. SB 6/516 CALLS UP ON LY A SIMPLE VISUAL INSPECTION. THIS CRACK WOULD NOT HAVE BEEN DETECTED IF THE RIB WAS NOT REMOVED FROM THE AIRCRAFT. 1 H 7 2 3T 4 T RT A9EA E4EA 2002120900083 20021209 00083 NM 2002 12 9 CA021115017 1 20021030 A 7170 82970410115 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 ENG DRAIN CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) ON NR 1 ENG SHUTDOWN FOUND RETURN CASE DRAIN TUBE ASSY AT XN 124.00 TO STN XN 146.40 LEAKING. IPC REF 29-10-00 FIG 15 ITEM 190. LINE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002120900084 20021209 00084 NM 2002 12 9 CA021115019 1 20021031 A 2910 82970009407 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE SPOILER DAMAGED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING MAINTENACE LT WING LIFT DUMP SPOILER LINE FOUND LEAKING. PIN HOLE AT TOP ELBOW ON O/B SIDE OF LINE. IPC REF 27-14-00 FIG. 40 ITEM 250. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002120900085 20021209 00085 EA 2002 12 9 CA021115020 1 20021103 A 2421 31708001A GENERATOR DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 2 FAILED W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 CA 20025 (CAN) AIR TURN BACK DUE TO FAILURE OF NR 2 AC GEN ON TAKEOFF. NR 2 AC GEN CAUTION LIGHT ILLUMINATED AND WOULD NOT RESET. AC GEN REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002120900086 20021209 00086 NM 2002 12 9 DHL2002741019 1 20021207 A 5210 90100722 SNUBBER BOEING 727 7272Q9 138448M NM A DHLA K O NONE OTHER O OTHER NR NOT REPORTED 1 SO 01 741DH 21931 1) FWD ENTRY DOOR LEVER GRINDS AND IS DIFFICULT TO OPERATE.2) INSTALLED SERVICEABLE SNUBBER IAW CHAPTER 52-11-33. 2 L 7 3 4F RT A3WE 2002120900087 20021209 00087 CE 2002 12 9 CA021115021 1 20021023 A 3020 50389028 BOOT BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA ENGINE INLET BURNED W O OTHER L NO TEST CR CRUISE 1 CA (CAN) AIRCRAFT WAS ENROUTE AND WAS ENTERING ICING CONDITIONS. CREW TURNED ON ALL DEICING EQUIPMENT INCLUDING ENGINE INL ET DEICE BOOTS. AFTER APPROX 5 MIN, AN ODOR WAS DETECTED IN THE COCKPIT AND ENGINE INLET DEICERS WERE TURNED OFF. ODOR D ISAPPEARED AND PILOTS CONTINUED WITH NO PROBLEMS. UPON INSPECT OF INLET DEICERS, RT INLET BOOT WAS BURNED AND ELEMENTS E XPOSED. ENGINE COWL WAS REMOVED AND BOOT REMOVED, EXPOSING FIBERGLASS LEADING EDGE OF THE INLET. INSPECT REVEALED THE D UCT WAS EXPOSED TO HEAT ALONG HALF OF LEADING EDGE OF COWL. A NEW INLET DEICE BOOT INSTALLED. SYSTEM CIRCUIT BREAKERS W ERE TESTED AND FOUND TO BE IN GOOD WORKING ORDER. 1 L 7 2 3T 4 T A14CE E4EA 2002120900088 20021209 00088 CE 2002 12 9 CA021115022 1 20021111 A 7120 575100615 MOUNT CESSNA 441 441 2076020 CE GARRTT TPE331 TPE33110 01514 WP ENGINE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON ENGINE COWLING REMOVAL DURING A SCHEDULED MAINTENANCE EVENT THE O/B UPPER ENGINE MOUNT TRUSS TUBE WAS FOUND B ROKEN. 1 L 7 2 3T 4 T RT A28CE E4WE 2002120900089 20021209 00089 NM 2002 12 9 PCAA0212143 1 20021207 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM POSITION 400 INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 804EX 30850 30850 227 DURING ROUTINE MAINTENANCE VISIT RIGHT AFT FUSELAGE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. POWER SUPPLY AND B ATTERY WERE REPLACED AT POSITION 400. OPERATIONAL CHECK WAS GOOD AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002120900091 20021209 00091 SO 2002 12 9 CA021115024 1 20021115 A 5751 1710018 SPAR PIPER PA23 PA23250 7102308 SO LYC O540 TIO540C1A 41532 EA RT AILERON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOUND RT AILERON INBOARD TRAILING EDGE RIB CRACKED AROUND BOTTOM MOUNTING HOLE.UPON REMOVAL OF RIB, FOUND SPAR IS ALSO HAS A 1/2 INCH CRACKED BESIDE BOTTOM MOUNTING HOLE. 1 L 7 2 3O 3 O 1A10 E14EA 2002120900092 20021209 00092 NM 2002 12 9 DL73K021206 1 20021017 A 5514 WEB BOEING 737 737247 138448D NM HORIZ STAB CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 FOUND ON Q1 LETTER CK RT AND LT INBD BALANCE BOARD PANELS CHAFING THROUGH THE INBD WEBS. REPAIRED PER SRM 51-40-20 AND OPERATION 1000 2 L 7 2 4F A16WE 2002120900093 20021209 00093 NM 2002 12 9 DL73K021211 1 20021018 A 3350 20131A BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 320DL 23092 CABIN EMERGENCY ESCAPE PATH LIGHTING BATTERY PACK WEAK, R/R BATTERY PACK PER M/M. 2 L 7 2 4F RT A16WE 2002120900094 20021209 00094 NM 2002 12 9 DL73K021215 1 20021020 A 5511 65499271 SPAR BOEING 737 737232 1384475 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 THE CENTER SECTION OF THE HORIZONTAL STAB WAS PREVIOUSLY REWORKED FOR CORROSION IN SEVERAL LUGS. THE REWORK WAS APP ROVED FOR A 24 MONTH LIMIT WHICH HAS BEEN REACHED. THE HORIZONTAL STAB WAS REMOVED FROM THE AIRCRAFT AND THE REAR SPAR LOWER CHORD REPLACED TO RESTORE THE AIRCRAFT. THE WORK WAS ACCOMPLISHED PER BAC S/B 737-55-1056 & -1055 AND PER ER/A 3 83918-14. 2 L 7 2 4F RT A16WE 2002120900095 20021209 00095 WP 2002 12 9 CA021117001 1 20021116 A 3600 1560580109 DUCT LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE WING PYLON CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) IN HANGAR, AT ENGINE INSTALLATION DURING RE CONNECTION OF THE INTERMEDIATE PRESSURE, (IP) DUCT INSIDE THE PYLON NR 3 AREA IT WAS NOTICED THAT THE FLEXIBLE SECTION OF THE PIPE SECTION FOR THE ANTI-ICE TAP-OFF OF THE IP DUCT WAS CHAFED THROUGH. DAMAGE OCCURRED WITH A CLOSE BY BRACKET HOLDING HYDRAULIC PIPES. ONLY THE DUCT ASSEMBLY SUFFERED DAMAGE. ALL C OMPONENTS IN THE AREA WERE INSPECTED AND FOUND SECURE AND IN GOOD CONDITION. DUCT SECTION WAS REPLACED, WITH A OVERHAUL ED DUCT ASSEMBLE. AN INSPECTION WAS CARRIED OUT AFTER INSTALLATION TO CHECK FOR CLEARANCES WITH SURROUNDING COMPONENTS A ND ALL WAS CLEAR. A LEAK CHECK WAS CARRIED OUT AND NO LEAKS WERE FOUND. 2 L 7 3 4F 4 F A23WE E12EU 2002120900096 20021209 00096 NM 2002 12 9 DL73K021229 1 20021024 A 3397 WIRE BOEING 737 737247 138448D NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 382DL 23609 RED TRACK LIGHTING INOP AT FWD COAT CLOSET, REPAIRED WIRE. 2 L 7 2 4F A16WE 2002120900097 20021209 00097 NM 2002 12 9 DL73K021241 1 20021025 A 3350 BPS73 POWER SUPPLY BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 320DL 23092 FWD EMERGENCY ESCAPE PATH LIGHTS INOP ROWS 1-4. R/R BATTERY PACK POWER SUPPLY PER M/M CKS GOOD. 2 L 7 2 4F RT A16WE 2002120900098 20021209 00098 EU 2002 12 9 CA021117002 1 20021110 A 7500 13842515 DUCT AIRBUS 310 A310300 3930305 EU GE CF6 CF680C2A5 NE ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) BLEED DUCT ON AIRFRAME SIDE OF ENGINE BLEED VALVE ON TAKE TO REVERSER AIR MOTOR OF NR 1 ENGINE WAS FOUND CRACKED A ND SEVERELY LEAKING. DUCT WAS REPLACED AND A LEAK CHECK WAS CARRIED OUT AND NONE WERE FOUND. 2 L 7 2 4F 4 F RT A35EU E13NE 2002120900099 20021209 00099 CE 2002 12 9 CA021118001 1 20021115 A 2435 03600918 BEARING LUCAS 23085001 BEECH B300 B300B350C CE PWA PT6 PT6A60A 52043 NE STARTER GEN MAKING METAL W D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 CA 99093 (CAN) SHORTLY AFTER LANDING BEECH KING AIR MODEL B300 WHILE TAXING HAD THE LEFT HAND STARTER GENERATOR GO OFF LINE. GENE RATOR WAS RESET ONCE AND WENT OFF LINE AGAIN. AIRCRAFT RETURNED TO HANGER.UPON INSPECTION OF THE STARTER GENERATOR IT WA S APPARENT THE AFT BEARING HAD FAILED. ARMATURE SHAFT COULD BE MOVE UP AND DOWN IN THE SUPPORT HOUSING. PIECES OF THE BE ARING FELL OUT WHEN THE COMPONENT WAS REMOVED FROM THE A/C. AS A RESULT OF BEARING FAILURE COOLING FAN CAME INTO CONTACT WITH THE AIR INLET HOUSING CAUSING DAMAGE TO BOTH. 2 L 7 2 4T 4 T RT A24CE E4EA 2002120900100 20021209 00100 WP 2002 12 9 CA021118002 1 20021105 A 5630 36935071 WINDOW HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL PILOT DOOR BROKEN W A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 CA (CAN) FLYING ALONG STRAIGHT AND LEVEL ALONG BRAGG CREEK WHEN THE DOOR POPPED OPEN. I SHUT THE DOOR AND CONTINUED FLYING. APPROXIMATELY 2 MINUTES LATER THE WINDOW BROKE LOSE AND FLEW AWAY FROM THE HELICOPTER. LANDED IMMEDIATELY AND SHUT DOWN TO INSPECT THE HELICOPTER. AFTER FINDING NO DAMAGE STARTED BACKUP AND SEARCHED FOR THE WINDOW. HAVING NO LUCK WE ABANDE NED THE SEARCH AND FLEW BACK TO SPRING BANK. 1 G 7 1 3U 3 U H3WE E4CE 2002120900102 20021209 00102 NE 2002 12 9 CA021118005 2 20021104 A 7261 311145101 CARBON SEAL BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE RT ENGINE FAILED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) PILOT NOTICED SLIGHT OIL PRESSURE FLUCTUATION OF THE RT ENGINE DURING A TRAINING FLIGHT AND RETURNED TO BASE. OIL LOSS CONFIRMED AND DETERMINED THAT THE OIL (4 LITERS) HAD EXITED THROUGH THE ENGINE BREATHER SYSTEM. REMOVED ACCESSORY G EARBOX AND REPLACED THE BREATHER CARBON SEAL . ENGINE REASSEMBLED, GROUND RUN AND TEST FLOWN. SATISFACTORY ENGINE FILTER S/SCREENS AND CHIP DETECTOR EXAMINED. FOUND CLEAN, AS PER MM, QUANTITY LOST AND POWER SETTINGS NO FURTHER ACTION REQUIRE D. 1 L 7 2 4T 4 T A24CE E4EA 2002120900103 20021209 00103 NE 2002 12 9 CA021118006 2 20021105 A 7310 A13311 HOUSING AIRBORNE 1093890001 BEECH B300 B300B350C CE PWA PT6 PT6A60A 52043 NE ENGINE FILTER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING PRE-RUN WALK-A-ROUND, DISCOVERED FUEL LEAK ORIGINATING FROM AROUND THE BYPASS INDICATOR OF THE LT ENGINE PR IMARY FUEL FILTER ASSEMBLY. AS NO FIELD REPAIRS ARE ALLOWED, THE ENTIRE FILTER HOUSING ASSEMBLY WAS REPLACED WITH NEW. G ROUND TESTS PERFORMED SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E4EA 2002120900105 20021209 00105 EU 2002 12 9 02FDEA00768 1 20021022 A 3230 PIVOT ASSY AIRBUS 310 A310 EU LT MLG SEIZED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 445FE 297 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. IN SYS 1 OR 2 TROUBLESHOT INTERLOCK SYSTEM. FOR NR 1 AND NR 2 SYSTEMS, F OUND ALL ELECTRICAL FUNCTIONS CHECK GOOD. CHECKS GOOD WITH GROUND ON RECEPTACLE OF PROX BOX AT PINS 44 AND 55. JACKED AIRCRAFT IAW M/M AND FOUND LEFT MAIN LANDING GEAR BOGIE BEAM WILL NOT PIVOT. REMOVED PITCH DAMPER IAW M/M AND BOGIE STI LL LOCKED UP. REMOVED ALL 4 BRAKE TORQUE ARMS AND BOGIE STILL LOCKED UP AT CENTER PIVOT POINT. WILL NEED FURTHER DISAS SEMBLY TO DETERMINE DAMAGE. 2 L 7 2 4F RT A35EU 2002120900106 20021209 00106 NM 2002 12 9 02FDEA00782 1 20021028 A 2570 ABH75465 PANEL DOUG MD11 MD11 3023602 NM E/E BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 AVIONICS COMPARTMENT ABOVE MAIN AVIONICS RACK STATION 401 FOUND A SHIELD PANEL, FITTING CRACKED AND METAL SKIN TORN AT 2 EACH PLACES, CRACK LENGTH APPROX 2.0 INCHES. REMOVED AND REPLACED PANEL AND METAL SKIN IAW SRM. 2 L 7 3 4F RT A22WE 2002120900107 20021209 00107 NM 2002 12 9 02FDEA00783 1 20021028 A 5321 ABA83031N FLOOR PANEL DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 AVIONICS COMPARTMENT, ABOVE MAIN AVIONICS RACK STATION 401 FOUND A MACHINED FLOOR PANEL LOWER FITTING CRACKED APPROXIMA TELY 3.0 INCHES. REMOVED AND REPLACED PANEL IAW SRM. 2 L 7 3 4F 4 F RT A22WE E13NE 2002120900108 20021209 00108 NM 2002 12 9 02FDEA00784 1 20021030 A 7931 ST104Z INDICATOR BOEING 727 727200 138407E NM GE CF6 CF680 30025 NE COCKPIT FAULTY A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 467FE 21449 NR 2 OIL PRESSURE AT 28 PSI IN FLIGHT, SHUT DOWN NR 2 ENGINE, WINDMILLED IN FLIGHT FOR 25 MINUTES WITH 28 PSI OIL PRESS INDICATOR. REMOVED AND REPLACED OIL PRESSURE INDICATOR IAW MM. LEAK AND OPS CHECK, OK FOR SERVICE. 2 L 7 3 4F 4 F RT A3WE E13NE 2002120900109 20021209 00109 NM 2002 12 9 02FDEA00786 1 20021031 A 5753 BUSHING BOEING 727 72722 1384002 NM PWA JT8 JT8D1 52044 NE T/E FLAP OUT OF ADJUST A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 25 148FE 19086 MODERATE AIRFRAME FLUTTER ABOVE 280 KNOTS, GOES AWAY WITH SPEED BRAKE HANDLE PULLED TO ABOVE 5 DEGREES WHEN SLOWED DOWN, FLUTTER RETURNS DURING LEFT TURNS. FOUND RIGHT OUTBOARD TRAILING EDGE FLAP, ECCENTRICS REQUIRED ADJUSTMENT. ADJUSTED AFT FLAP ECCENTRIC BUSHINGS IAW MM. AIRCRAFT OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2002120900110 20021209 00110 WP 2002 12 9 AALA20021361 1 20020925 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND CUSP CRACKED AT LIGHTENING HOLE, FS 247. FABRICATED AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 2002120900111 20021209 00111 WP 2002 12 9 AALA20021364 1 20020925 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND INTERCOSTAL UNDER FLOORBOARD IS CRACKED, FS 560. INSTALLED NEW INTERCOSTAL PER 51-03. (M) 2 L 7 2 4F A6WE 2002120900112 20021209 00112 WP 2002 12 9 AALA20021365 1 20020925 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND WINDOW FRAME CRACKED, FS 1060. INSTALLED DOUBLER PER AARD 53-10-002J. (M) 2 L 7 2 4F A6WE 2002120900113 20021209 00113 WP 2002 12 9 AALA20021366 1 20020925 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND WINDOW FRAME CRACKED UPPER AFT CORNER STATION 1022 RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2002120900114 20021209 00114 WP 2002 12 9 AALA20021367 1 20020925 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND WINDOW FRAME CRACKED, UPPER AFT CORNER, FS 1041. REPAIRED CRACK PER AARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2002120900115 20021209 00115 WP 2002 12 9 AALA20021368 1 20020925 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND LEFT CUSP CRACKED AT LIGHTENING HOLE, FS 1245. INSTALLED REPAIR DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002120900116 20021209 00116 WP 2002 12 9 AALA20021369 1 20020925 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND CRACK IN CUSP UNDER NR 5 SEAT TRACK, FS 218. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002120900117 20021209 00117 WP 2002 12 9 AALA20021370 1 20020925 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND FUSELAGE SKIN CRACKED, FS 1380 LONGERON 14L. REPAIRED PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002120900118 20021209 00118 WP 2002 12 9 AALA20021371 1 20020925 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND FUSELAGE SKIN CRACKED, FS 1380 LONGERON 14R. INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3. (M) 2 L 7 2 4F A6WE 2002120900119 20021209 00119 WP 2002 12 9 AALA20021374 1 20020925 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND CORROSION ON LEFT CUSP STATION 1140 AND 1142 AROUND FASTENER HOLES. INSTALLED DOUBLER REPAIR PER AARD 53-00 -00-02 AND SRM 53-01 FIG 1. (M) 2 L 7 2 4F A6WE 2002120900120 20021209 00120 WP 2002 12 9 AALA20021375 1 20020925 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND FLOORBEAM CRACKED, FS 1022. FABRICATED NEW FLOORBOARD SUPPORT AND REPLACED AT STATION 1022 PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002120900121 20021209 00121 WP 2002 12 9 AALA20021376 1 20020925 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND CORROSION ON SUBFLOOR STATION 183 TO STATION 200. INSTALLED DOUBLER WET PER SRM 53-01 FIG 4. () 2 L 7 2 4F A6WE 2002120900122 20021209 00122 WP 2002 12 9 AALA20021378 1 20020911 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 443AA 49469 TUL - FOUND STATION LONGERON 11 LEFT INNER SKIN CRACKED. CUT OFF TAB AND INSTALLED REPAIR STRAP PER AARD 53-10-00-11. (M) 2 L 7 2 4F A6WE 2002120900123 20021209 00123 WP 2002 12 9 AALA20021381 1 20020923 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 443AA 49469 TUL - FOUND CRACK ON FUSELAGE AT STATION 1380 1 INCH ABOVE L14L SKIN IS CRACKED AROUND FASTENER. INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002120900124 20021209 00124 WP 2002 12 9 AALA20021420 1 20021002 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 296AA 49308 TUL - FOUND EXTERNAL LONGERON 20R IS CRACKED IN RADIUS AT STATION 995 CRACK IS APPROX .75 INCH IN LENGTH. INSTALLED DOU BLER REPAIR PER AARD 53-10-00-18. (M) 2 L 7 2 4F A6WE 2002120900125 20021209 00125 WP 2002 12 9 AALA20021421 1 20021002 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 296AA 49308 TUL - FOUND EXTERNAL LONGERON 20L IS CRACKED IN RADIUS AT STATION 995 CRACK IS APPROX .875 INCH IN LENGTH. INSTALLED DO UBLER PER AARD 53-10-00-18. (M) 2 L 7 2 4F A6WE 2002120900126 20021209 00126 WP 2002 12 9 GTIA021036 1 20021001 A 7120 K221975A1 ISOLATOR DOUG DC9 DC941 302207N WP NR 1 ENGINE DEFECTIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 DTW - FOUND UPPER NR 1 ENGINE ISOLATOR DOES NOT HAVE ANTI-ROTATION MARK. REMOVED AND REPLACED NR 1 ENGINE UPPER ISOLATO R, CLOSED 10/10/02. (M) 2 L 7 2 4F A6WE 2002120900127 20021209 00127 WP 2002 12 9 GTIA021037 1 20021001 A 7120 K22197SA1 ISOLATOR DOUG DC9 DC941 302207N WP NR 1 ENGINE DEFECTIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 DTW - FOUND LOWER NR 1 ENGINE ISOLATOR DOES NOT HAVE ANTI-ROTATION MARK. REMOVED AND REPLACED NR 1 ENGINE LOWER ISOLATO R, CLOSED 10/10/02. (M) 2 L 7 2 4F A6WE 2002120900128 20021209 00128 WP 2002 12 9 GTIA021040 1 20021001 A 3350 TRACK DOUG DC9 DC932 3022066 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 133NK 48111 DTW - FOUND EMERGENCY TRACK LIGHTING NEEDS TO BE REPAIRED FROM O/W EXIT TO AFT OF CABIN. REMOVED AND REPLACED EMERGENCY TRACK LIGHTING FROM FORWARD AND O/W EXIT TO AFT CABIN. (M) 2 L 7 2 4F A6WE 2002120900129 20021209 00129 WP 2002 12 9 GTIA021044 1 20021004 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 133NK 48111 DTW - FOUND AFT STAIRWAY EXIT SIGN STAYS ON WITH NO POWER TO AIRCRAFT. EMERGENCY LIGHTS SWITCHES CYCLED, LIGHT REMOVED, ILLUMINATED. SECURED LOOSE WIRE ON POWER SYSTEM. (M) 2 L 7 2 4F A6WE 2002120900130 20021209 00130 WP 2002 12 9 GTIA021103 1 20020924 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND AFT PIT FS 1174-1193 SUBFLOOR WEB OUTBOARD OF OUTBOARD SEAT TRACK CORRODED. REMOVED DAMAGED WEB. FABRICATE D NEW WEB AND DOUBLER. INSTALLED NEW WEB AND DOUBLER. (M) 2 L 7 2 4F RT A6WE 2002120900131 20021209 00131 WP 2002 12 9 GTIA021104 1 20020924 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - AFT PIT FS 1287 LONGERON 29R CORROSION OUTBOARD FLANGE UNDERSIDE, HI-LOCK. INSTALLED LONGERON. (M) 2 L 7 2 4F RT A6WE 2002120900132 20021209 00132 WP 2002 12 9 GTIA021105 1 20020924 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND AFT CABIN STATION 1338 FLOORBEAM CORRODED RBL 20 INCHES. REMOVED DAMAGED AREA. FABRICATED ANGLE AND FILLER . INSTALLED ANGLE AND FILLER. (M) 2 L 7 2 4F RT A6WE 2002120900133 20021209 00133 WP 2002 12 9 GTIA021106 1 20020924 A 5320 STIFFENER DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND AFT CABIN STATION 1338 CRACK AT STIFFENER SUPPORT AFT LEFT LOWER DOOR JAMB. REMOVED CRACKED STIFFENER. FAB RICATED REPLACEMENT SUPPORT. INSTALLED REPLACEMENT SUPPORT. (M) 2 L 7 2 4F RT A6WE 2002120900134 20021209 00134 WP 2002 12 9 GTIA021107 1 20020925 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FLOORBOARD SUPPORT LBL 8 STATION 200-256 CORRODED. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTA LLED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2002120900135 20021209 00135 WP 2002 12 9 GTIA021108 1 20020925 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND WEBBING AT FORWARD LAVATORY LBL 41 STATION 233 CORRODED. CUT OUT THE DAMAGED AREA. FABRICATED DOUBLERS REP AIR AND FILLER. INSTALLED DOUBLERS REPAIR AND FILLER. (M) 2 L 7 2 4F RT A6WE 2002120900136 20021209 00136 WP 2002 12 9 GTIA021109 1 20020925 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FLOORBOARD SUPPORT CORRODED LBL 60 STATION 195. FORMED NEW ANGLE FLOOR SUPPORT. INSTALLED FLOOR SUPPORT AN GLE. (M) 2 L 7 2 4F RT A6WE 2002120900137 20021209 00137 WP 2002 12 9 GTIA021110 1 20020925 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FLOORBOARD SUPPORT CORRODED LBL 51 STATION 160-185. REMOVED SUPPORT ANGLE. FABRICATED SUPPORT ANGLE. INST ALLED FLOOR SUPPORT ANGLE. (M) 2 L 7 2 4F RT A6WE 2002120900138 20021209 00138 WP 2002 12 9 GTIA021111 1 20020925 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FLOORBOARD SUPPORT CORRODED RBL 1 STATION 180. FORMED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2002120900141 20021209 00141 WP 2002 12 9 GTIA021114 1 20021002 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FLOOR SUPPORT CORRODED STATION 190 JUST INBOARD OF MAIN ENTRY DOOR. REMOVED FLOOR SUPPORT ANGLE. FABRICATE D NEW FLOOR SUPPORT ANGLE. INSTALLED FLOOR SUPPORT ANGLE. (M) 2 L 7 2 4F RT A6WE 2002120900142 20021209 00142 NM 2002 12 9 02FDEA00822 1 20021112 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 CORROSION ON SHEAR TIE BS 580 JUST O/B OF STR 28R. R&R SHEAR TIE PER SRM 51-30-2, 51-10-6, 51-20-1, 51-30-5. 2 L 7 3 4F RT A3WE 2002120900143 20021209 00143 NM 2002 12 9 02FDEA00823 1 20021113 A 2781 40173 SWITCH BOEING 727 727200 138407E NM KRUEGER FLAP FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 204FE 22926 DURING FLAP RETRACTION, NR 3 KRUEGER FLAP REMAINED IN TRANSIT. NO GREEN LIGHT ON FRONT PNL. AMBER LIGHT ILLUMINATED ON S/O PNL. PERFORMED QRH FOR LED FAILURE DURING FLAP RETRACTION LED'S WERE POSITIONED NORMALLY AT FLAPS 5. RETURNED TO DLH FOR A NORMAL LANDING. REMOVED AND REPLACED LEADING EDGE FLAP POSITION SWITCH IAW MM 27-82-001. SYSTEM OPS CHECKED NORM. 2 L 7 3 4F RT A3WE 2002120900144 20021209 00144 NM 2002 12 9 02FDEA00824 1 20021112 A 2121 215201 GASPER FAN BOEING 727 727200 138407E NM CABIN MALFUNCTIONED A FDEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 206FE 22928 GASPER FAN CB POPPED. MILD ELECTRICAL SMOKE IN FLT STATION. REPLACED GASPER FAN PER M/M 21-23-011-4. SYSTEM OPS CHECK OK. 2 L 7 3 4F RT A3WE 2002120900145 20021209 00145 NM 2002 12 9 02FDEA00826 1 20021112 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON FLOORBEAM UPPER CHORD AT BS 1110, RBL 16, WL 200 AT NUTPLATE HOLES. FOUND CORROSION ON FLOORBEAM UPPER CHO RD TO BE OUT OF LIMITS IAW SRM 53-10-1. CUT OUT DAMAGE AREA & REPAIRED IAW SRM 53-10-8 FIG 8. 2 L 7 3 4F RT A3WE 2002120900146 20021209 00146 SO 2002 12 9 C2A02SH136 1 20021206 A 5320 14521721009 BUTT STRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14916 145415 SHV- DURING C CHECK THE CENTER OMEGA BEAM BUTTSTRAP BETWEEN FRAMES 16 AND 17 WAS FOUND TO HAVE CORROSION. MAINTENANCE R EMOVED DAMAGE AREA AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SER VICE. 2 L 7 2 4T RT T00011AT 2002120900147 20021209 00147 WP 2002 12 9 IXXA0200086S 1 20020710 A 5230 DOOR FRAME DOUG DC8 DC871F 302199D WP CARGO DOOR CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 83050 2948 45978 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FORWARD CARGO COMPARTMENT C1 DOOR JUST BELOW THE AFT LO CK BRACKET. REPAIR ACCOMPLISHED, REMOVAL OF EXISTING REPAIR AND CORROSION, FABRICATION AND INSTALLATION OF NEW EXTENDED FRAME IAW THE DOUGLAS SRM. 2 L 7 4 4F RT 4A25 2002120900148 20021209 00148 NE 2002 12 9 MALA020678 2 20021206 A 7220 CT79B ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 411XJ 340B411 AFTER TAKEOFF ON FLIGHT #3142, AT APPROXIMATELY 400' DURING THE AFTER TAKEOFF FLOW THE LH ENGINE TORQUE WENT TO 20%, AND A MASTER WARNING LIGHT ILLUMINATED. ALMOST SIMULTANIOUSLY THE LH ENGINE OVERTEMP LIGHT WENT ON TEMP WAS AT 1000-1007 D EGREES C. CLEAR, NO ICE. AIR RETURN TO PIR. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE AND PGB ASSEMBLY PN CT7-9B SN /OFF GE-E-785692, SN/ON GE-E-785370 PER JC 7100-301. LH AND WORK PACKAGE FROM PLANNING ISSUED 12/6/02. REFERENCE WO # 33 7791. ALL LEAK AND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2002120900149 20021209 00149 EU 2002 12 9 CA021118010 1 20021028 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R390 R3904123F27 NE CARGO BAY FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) CARGO BAY SMOKE DETECTOR FALSE WARNING. MAINTENANCE.DETECTOR REMOVED S/.N 337. INSTALLED 19/06/01. TIS 2531.5 HOUR S.THE INSTALLATION OF THESE SMOKE DETECTORS WAS MANDATED BY SWEDISH AD 1-151 TO IMPROVE RELIABILITY.CONSULTATION WITH SA AB REVEALED 12 CONFIRMED FAILURES ON FAA REG AIRCRAFT IN THE PAST 12 MONTHS. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P31NE 2002120900150 20021209 00150 NE 2002 12 9 DHL2002803012 2 20021207 A 7314 FUEL FILTER DOUG DC8 DC873 302199C WP GE CFM56 CFM562C1 13802 NE A DHLA K O NONE OTHER O OTHER NR NOT REPORTED 1 SO 01 803DH 46123 693482 1) #3 FUEL BYPASS LIGHT ILLUMINATED IN FLIGHT. PERFORMED ABNORMAL PROCEEDURE AND LIGHT EXTINGUISHED. BYPASS LIGHT ILLUM INATED A SECOND TIME AND WOULD NOT EXTINGUISH. FUEL FILTER BYPASS RESET LIGHT INOPERATIVE.2) FOUND #3 ENGINE FUEL FILTE R CONTAMINATED. REMOVED AND REPLACED FILTER IAW M/M 73-10-2. OPS CHECKED GOOD DURING GROUND RUN. RELAMPED FUEL FILTER BY PASS RESET LIGHT SWITCH. OPS CHECKED OK IAW TR 73-24, 73-34-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2002120900151 20021209 00151 EU 2002 12 9 CA021118011 1 20021030 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R390 R3904123F27 NE CARGO BAY FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 608 (CAN) CARGO BAY SMOKE DETECTOR WILL NOT TEST. MAINTENANCE.DETECTOR REMOVED S/N 608. INSTALLED 20/07/02. TIS 553.6 HOURS. THE INSTALLATION OF THESE SMOKE DETECTORS WAS MANDATED BY SWEDISH AD 1-151 TO IMPROVE RELIABILITY.CONSULTATION WITH SAAB REVEALED 12 CONFIRMED FAILURES ON FAA REG AIRCRAFT IN THE PAST 12 MONTHS. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P31NE 2002120900152 20021209 00152 EU 2002 12 9 CA021118012 1 20021030 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R390 R3904123F27 NE CARGO BAY FAILED W K NONE N FALSE WARNING TO TAKEOFF 1 CA 663 (CAN) CARGO BAY FIRE WARNING ON TAKEOFF. TAKEOFF ABORTED. FALSE WARNING.DETECTOR REMOVED S/N 663. INSTALLED 19/06/01. TI S 3339.4 HOURS. THE INSTALLATION OF THESE SMOKE DETECTORS WAS MANDATED BY SWEDISH AD 1-151 TO IMPROVE RELIABILITY.CONSUL TATION WITH SAAB REVEALED 12 CONFIRMED FAILURES ON FAA REG AIRCRAFT IN THE PAST 12 MONTHS. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P31NE 2002120900153 20021209 00153 EU 2002 12 9 CA021118013 1 20021030 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R390 R3904123F27 NE CARGO BAY FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 662 (CAN) CARGO BAY SMOKE DETECTOR FAILED TO TEST AFTER RECTIFICATION OF ABOVE INCIDENT. MAINTENANCE. DETECTOR REMOVED S/N 6 62. INSTALLED 19/06/01. TIS 3339.4 HOURS. THE INSTALLATION OF THESE SMOKE DETECTORS WAS MANDATED BY SWEDISH AD 1-151 TO IMPROVE RELIABILITY.CONSULTATION WITH SAAB REVEALED 12 CONFIRMED FAILURES ON FAA REG AIRCRAFT IN THE PAST 12 MONTHS. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P31NE 2002120900154 20021209 00154 EU 2002 12 9 CA021118014 1 20021103 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R390 R3904123F27 NE CARGO BAY FAILED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 338 (CAN) CARGO BAY FIRE WARNING LIGHT ON DURING C/PIT CHECKS.DETECTOR REMOVED S/N 338. INSTALLED 20/06/01. TIS 5214.1 HOURS . THE INSTALLATION OF THESE SMOKE DETECTORS WAS MANDATED BY SWEDISH AD 1-151 TO IMPROVE RELIABILITY.CONSULTATION WITH SA AB REVEALED 12 CONFIRMED FAILURES ON FAA REG AIRCRAFT IN THE PAST 12 MONTHS. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P31NE 2002120900155 20021209 00155 2002 12 9 MWEA020725 4 20021207 A 3416 88113129 ALTIMETER DOUG DC9 DC981 3022081 WP COCKPIT DEFECTIVE A MWEA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 803ME 48029 FIRST OFFICER'S ALTIMETER INOP. -- REMOVED AND REPLACED ALTIMETER. 2 L 7 2 4F A6WE 2002120900156 20021209 00156 EU 2002 12 9 CA021118015 1 20021103 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R390 R3904123F27 NE CARGO BAY FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 676 (CAN) AFT CARGO BAY SMOKE DETECTOR WILL NOT TEST. MAINTENANCE.SUNSEQUENT TO THE ABOVE A SYSTEM CHECK WAS CARRIED OUT. N O DEFECTS FOUND. DETECTOR REMOVED S/N 676. INSTALLED 30/10/02. TIS 31.2 HOURS. THE INSTALLATION OF THESE SMOKE DETECTOR S WAS MANDATED BY SWEDISH AD 1-151 TO IMPROVE RELIABILITY. CONSULTATION WITH SAAB REVEALED 12 CONFIRMED FAILURES ON FA A REG AIRCRAFT IN THE PAST 12 MONTHS. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P31NE 2002120900157 20021209 00157 EU 2002 12 9 CA021119001 1 20021118 A 2530 145201 CABLE BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL CARGO HOOK BROKEN W O OTHER O OTHER CR CRUISE 1 CA (CAN) THE AIRCRAFT EXPERIENCED AN IN FLIGHT LOSS OF IT'S SLING LOAD. INVESTIGATION REVEALED THAT THE SWAGED END OF THE EMERGENCY RELEASE CABLE HAD COMPLETELY SEPARATED FROM THE CABLE CONDUIT. THIS PLACED THE CABLE CONSTANTLY UNDER PRELOAD .THE RESULT BEING THAT AS THE CARGO LOAD SWUNG IN FLIGHT, IT INADVERTENTLY OPENED THE EMERGENCY RELEASE MECHANISM. 1 G 7 2 3U 3 U H3EU E4CE 2002120900158 20021209 00158 SW 2002 12 9 CA021119002 1 20021101 A 6510 204040620011 DRIVE SHAFT BELL 205 205A1 1181414 SW LYC T53 T5317A 41549 NE TAIL ROTOR SCORED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE DOING A 100 HOUR INSPECTION ON THE BELL 205A-1, THE TAIL ROTOR DRIVE SHAFT ASSEMBLY WAS FOUND SCORED BEYOND LIMITS. THE INSPECTION IS A CLEARANCE CHECK BETWEEN THE T/R DRIVE SHAFT COVER AND THE T/R DRIVE SHAFT. THIS CLEARANCE C HECK IS DUE TO POSSIBLE DAMAGE TO THE T/R DRIVE SHAFT COVER (GETTING DENTED DUE TO THE WEIGHT OF THE T/R DRIVE SHAFT) BY THE INSTALLATION OR REMOVAL OF THE STARTER GENERATOR. THE STARTER GEN IS POSITIONED JUST ABOVE THE T/R DRIVE SHAFT COVE R. THE STARTER GEN WAS REMOVED AND REINSTALLED 25 HOURS PREVIOUSLY TO THIS 100 HOUR INSPECTION. AD 92-27-21 REGARDING TH IS SUBJECT WAS CARRIED OUT AT THE REMOVAL AND INSTALLATION OF THE STARTER GEN. 1 G 7 1 4U 4 U H1SW E17EA 2002120900159 20021209 00159 EU 2002 12 9 CA021119003 1 20021008 A 6410 355A12004008 HUB AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20F 03013 GL TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) IT WAS NOTED THAT ON THE LAST SHUTDOWN A NOISE WAS BEING GENERATED FROM THE T/R BLADE ASSY REGION. IT WAS MENTION ED TO AN ENGINEER AND THEY CARRIED OUT A EQUIVALENT TO A 30 HOUR INSPECTION AS PER AD 84-064-037(B)R3. (NO DISASSEMBLY) A VERY SLIGHT NOISE WAS HEARD. THE ENGINEER DECIDED THAT THE 500 HOUR INSPECTION AS PER AD WAS TO BE CARRIED OUT (DISASS EMBLY). A LONGITUDINAL CRACK WAS FOUND ON THE TAIL ROTOR SPAR. TAIL ROTOR WAS REMOVED FROM SERVICE. 1 G 7 2 3U 3 U H11EU E4CE 2002120900160 20021209 00160 WP 2002 12 9 ABXA020351 1 20021125 A 5300 99582305 INTERCOSTAL DOUG DC9 DC941 302207N WP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 INTERCOSTAL CRACKED AT STA. 973, LONGERON 28 RIGHT. REPLACED INTERCOSTAL IAW DC-9 SRM. 2 L 7 2 4F A6WE 2002120900161 20021209 00161 WP 2002 12 9 ABXA020352 1 20021204 A 5330 SKIN DOUG DC8 DC863F 302198F WP F.S. 1700 - 1746 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 TEMPORARY REPAIR FUSELAGE SKIN STA. 1700 AND 1746 IAW ABX REA D853-43878. REMOVED TEMPORARY REPAIRS AND REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-1. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-1. ALODINED AND PRIMED AREA AND REPAIR PARTS IAW DC- 8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC-8 SRM 53-2-1. 2 L 7 4 4F 4A25 2002120900162 20021209 00162 GL 2002 12 9 CA021119005 3 20021106 A 6111 BLADE CESSNA 150 150M 2071830 CE CONT O200 O200A 17020 SO MCAULY 1A102 1A102OCM GL PROPELLER IMPROPER PART W A K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) PROPELLER HAD BEEN WELDED TO COVER UP DEFECTS. PROPELLER IS SCRAP. THIS IS A REOCCURRING PROBLEM. 1 H 7 1 3O 3 O 3A19 E252 5 N P918 2002120900163 20021209 00163 WP 2002 12 9 AALA20021286 1 20020828 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 558AA 53088 TUL - FOUND CORROSION ON SEAT TRACK FROM STATION 218-351 SEVERAL PLACES THAT ARE OVER MM LIMIT TO BLENDOUT. CORRODED SE AT TRACK WAS REMOVED FROM STATION 218-351 AND REPLACED PER SRM 53-05 FIG 4. (M) 2 L 7 2 4F A6WE 2002120900164 20021209 00164 GL 2002 12 9 CA021119006 3 20021106 A 6114 C5270 BEARING CESSNA 180 180K 2072624 CE CONT O470 O470U 17026 SO MCAULY 2A34C C2A34C204 GL PROPELLER CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PROPELLER WOULD NOT CHANGE PITCH. PROPELLER WAS SO BADLY CORRODED INTERNALLY THAT THE BEARING SEIZED. ENTIRE PROPE LLER SCRAP DUE TO CORROSION. NO HISTORY OF PROPELLER HAVING BEEN SUBMERGED. 1 H 7 1 3O 3 O 5A6 E273 5 C P3EA 2002120900165 20021209 00165 GL 2002 12 9 CA021119007 3 20021030 A 6110 8332 COUNTERWEIGHT CESSNA 310 310D 2074212 CE CONT O470 IO470D 17026 SO HARTZL HC82V HC82V* GL PROPELLER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PROPELLER RECEIVED FOR AD 97-18-02 REPETITIVE INSPECTION. CRACK DISCOVERED DURING M.P.I. INSPECTION OF THE CLAMPS. AT ONE TIME DURING THE HISTORY OF THE PROP THE COUNTERWEIGHT SHOWS DAMAGE FROM CONTACT AGAINST THE PROP PISTON. PUSHING OUT THE THIN WALL AND LEAVING A CRACK 1/2 INCH LONG. 1 L 7 2 3O 3 O 3A10 3E1 5 C P23EA 2002120900166 20021209 00166 WP 2002 12 9 AALA20021290 1 20020822 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 560AA 53090 TUL - FOUND SHALLOW DENT ON FUSELAGE, STATION 316 BETWEEN L22L AND 23L. INSTALLED DOUBLER PER SRM 53-04, FIG 38. (M) 2 L 7 2 4F A6WE 2002120900167 20021209 00167 WP 2002 12 9 AALA20021317 1 20020910 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FOUND L2R CRACKED AT END FITTING. REMOVED DAMAGED SECTION OF 2R. INSTALLED SPLICE AND DOUBLER PER AARD 53-30-00- 2. (M) 2 L 7 2 4F RT A6WE 2002120900168 20021209 00168 WP 2002 12 9 AALA20021318 1 20020916 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 596AA 53286 TUL - FOUND CORROSION ON SEAT TRACK NR 3, FS 1174. INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F RT A6WE 2002120900169 20021209 00169 WP 2002 12 9 0203959914 1 20021113 A 5220 DOOR DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 964N 47416 During Hck in DHN, two cracks were found, on in the pan and one in the support of the aft ventral door. Repaired per EA 99-191379. 2 L 7 2 4F A6WE 2002120900170 20021209 00170 WP 2002 12 9 0203969914 1 20021113 A 5330 DOOR FRAME DOUG DC9 DC931 3022065 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 964N 47416 During HCK in DHN, corrosion was found just forward and below the aft cargo door forward lower corner. The existing repa ir was removed and a new repair was installed per EA 99-191383. 2 L 7 2 4F A6WE 2002120900171 20021209 00171 WP 2002 12 9 0203979914 1 20021115 A 5230 DOOR DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 964N 47416 While in DHN for HCK a crack was found in the inner pan of the aft cargo door. The crack emanated from the edge of the l ightening hole at the aft cut out for the aft hinge. Repaired per EA 99-191382. 2 L 7 2 4F A6WE 2002120900172 20021209 00172 WP 2002 12 9 0203999961 1 20021124 A 5410 INTERCOSTAL DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 924RW 47185 During overnight in ATL a pylon intercostal support angle was found cracked. Repaired per EA 99-190867. 2 L 7 2 4F A6WE 2002120900173 20021209 00173 WP 2002 12 9 0204009915 1 20021125 A 5710 CAP DOUG DC9 DC931 3022065 WP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 965N 47417 During HCK in ATL, corrosion was found in the upper flange of the center wing skin cap. Corrosion was out of limits. Rep aired per EA 99-190861. 2 L 7 2 4F A6WE 2002120900174 20021209 00174 WP 2002 12 9 MWEA020727 1 20021206 A 8010 19073 STARTER DOUG DC9 DC932 3022066 WP LEFT ENGINE INOPERATIVE A MWEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 31 209ME 47730 LEFT ENGINE STARTER INOPERATIVE -- REMOVED AND REPLACED ENGINE STARTER. 2 L 7 2 4F A6WE 2002120900175 20021209 00175 WP 2002 12 9 AALA20021336 1 20020912 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 452AA 49553 TUL - FOUND NR 1 SEAT TRACK CORRODED IN NUMEROUS LOCATIONS, STATION 200-798. REPLACED NR 1 SEAT TRACK FROM STATION 200- 798. (M) 2 L 7 2 4F A6WE 2002120900176 20021209 00176 WP 2002 12 9 AALA20021360 1 20020925 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33414 49325 TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET ABOVE PYLON ANGLE STATION 1380. STOP DRILLED CRACK. FABRICATED AND INSTALLE D DOUBLER PER AARD 53-30-00-2. (M) 2 L 7 2 4F A6WE 2002120900177 20021209 00177 WP 2002 12 9 AALA20021372 1 20020925 A 5532 SKIN DOUG DC9 DC982 3022082 WP VERTICAL STAB DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND 19 FASTENERS LOOSE/PULLING THROUGH SKIN JUST ABOVE INTAKE AT BASE OF VERITCAL STABILIZER, ZFS 11.562. INSTA LLED DOUBLER STRAPS PER ESO 80559. (M) 2 L 7 2 4F A6WE 2002120900178 20021209 00178 WP 2002 12 9 AALA20021373 1 20020925 A 5320 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND SEAT TRACK NR 2, CORROSION ON SPLICE. INSTALLED SEAT TRACK PLUG PER ESO 80559. (M) 2 L 7 2 4F A6WE 2002120900184 20021209 00184 NM 2002 12 9 DL757021037 1 20020904 A 3397 WIRE BOEING 757 757232 1384965 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 618DL 22908 ON INSPECTION FOUND RED EMERGENCY PATH LIGHT ON, AFT LAV INOP. FOUND WIRING BROKEN FOR LIGHT ASSY. REPLACED LIGHT ASSY AND REPAIRED WIRING. OPS NORMAL. 2 L 7 2 4F RT A2NM 2002120900185 20021209 00185 SO 2002 12 9 C2XA02CL240 1 20021206 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145ER 3260211 SO LEFT GEAR FAULTY A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 16944 145045 CLE FLIGHT#3085 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT.THE AIRCRAFT LANDED WITHOUT FURTHER I NCIDENT.MAINTENANCE INSPECTED AND REPLACED THE RIGHT AND LEFT WOW PROXIMITY SWITCHES ON THE LEFT MAIN GEAR.OPERATIONAL C HECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002120900186 20021209 00186 2002 12 9 ZW0A0212101 4 20021207 A 2330 6176265001 MONITOR BOEING 757 7572Q8 1384972 NM A ZW0A A UNSCHED LANDING O OTHER CR CRUISE 1 CE 13 713TW 28173 THE PASSENGER ENTERTAINMENT MONITOR AT CABIN ROW 27, LEFT SIDE, OVERHEATED AND CAUSED AN ELECTRICAL ODOR. FLIGHT MADE A N UNSCHEDULED LANDING AT JAX. THE ELECTRICAL CONNECTOR WAS REMOVED FROM THE MONITOR AND THE AIRCRAFT OPERATED MINIMUM E QUIPMENT. THE MONITOR WAS LATER REPLACED. CHECK-C 12-20-01 MCI. ---CLOSED-- 2 L 7 2 4F RT A2NM 2002120900187 20021209 00187 2002 12 9 CA021119014 4 20020929 A 3418 COMPUTER LEAR 45 45LEAR 5170805 CE STALL WARNING MALFUNCTIONED W D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA (CAN) DURING TAXI DOWN WIND THE RT STICK SHAKER INTERMITTENTLY ACTIVATED WHEN THE AOA VANE WAS BLOWN OUT OF TRAIL. TROUB LESHOOTING TRACED THIS TO THE STALL WARNING COMPUTER.WE RECEIVED FROM THE MANUFACTURER AND USED 2 OTHER COMPUTERS AND DI SCOVERED DIFFERENT INTERMITTENT FAULTS. INVESTIGATION OF BREAKDOWN REPORTS FOUND MANUFACTURER HAD TESTED UNITS SERVICEAB LE AND NOT DONE ANY REPAIRS. THE THIRD UNITRECEIVED WAS CHECKED PRIOR TO INSTALLATION AND FOUND TO BE REPAIRED AND PERFO RMED SATISFACTORILY 2 L 7 2 4F RT T00008WI 2002120900188 20021209 00188 NM 2002 12 9 DL757021069 1 20020912 A 3260 CIRCUIT BOARD BOEING 757 757232 1384965 NM COCKPIT BURNED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 650DL 24390 BURNING SMELL IN COCKPIT. SMOKE COMING FROM HOLE AROUND GEAR HANDLE. FOUND LEFT GEAR GREEN INDICATOR LIGHT ASSEMBLY CI RCUIT BOARD BURNED. REPLACED SAME. 2 L 7 2 4F RT A2NM 2003022700078 20030227 00078 2003 2 27 751PA0008 4 20021207 A 3431 285T05534 CONTROL HEAD BOEING 757 757200 1384950 NM ILS SYSTEM MALFUNCTIONED A PIDA K NONE O OTHER AP APPROACH 1 SO 05 751PA 23928 FD DID NOT CAPTURE LOC, LOC ARMED SHOWN ON FMA BUT NO CAPTURE. REPLACED ILS CONTROL HEAD IAW MM 34-31-01. OPS CHECK & INDICATIONS NORMAL. 2 L 7 2 4F RT A2NM 2002120900189 20021209 00189 SO 2002 12 9 C2XA02CL243 1 20021208 A 3350 110049 CHARGER EMB 145 EMB145 3260210 SO CABIN FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14974 145161 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT ABOVE ROW 17 WOULD NOT ILLUMINATE.MAINTENANCE INSPECTED AND REPLACED THE #4 EMERGENCY BATTERY CHARGER ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002120900190 20021209 00190 NM 2002 12 9 UPS02239953 1 20021124 A 5310 FITTING BOEING 727 72730C 1384009 NM R/H TENSION TIE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C TAILSKID BAY RH LWR TENSION TIE AFT FITTING HAS EVIDENCE OF CRACK INSTALLED NEW R/H LWR TENSION TI E FITTING IAW SRM 51-30-02 & DRAWING 65-25992 2 L 7 3 4F A3WE 2002120900191 20021209 00191 NM 2002 12 9 UPS02239954 1 20021124 A 5310 FITTING BOEING 727 72730C 1384009 NM L/H TENSION TIE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C TAILSKID BAY L/H UPPER TENSION TIE AFT FITTING CRACKED L/H UPPER TENSION TIE REPLACED IAW SRM 51-3 0-02 & DRAWING 65-25992 2 L 7 3 4F A3WE 2002120900192 20021209 00192 NM 2002 12 9 UPS02239955 1 20021126 A 5310 FITTING BOEING 727 72730C 1384009 NM TENSION TIE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C L/H LWR TENSION TIE FITTING CRACKED AT O/B LUG IN TAILSKID COMPARTME NT INSTALLED NEW L/H LWR TENS ION TIE FITTING IAW SRM 51-30-02 & DRAWING 65-25992 2 L 7 3 4F A3WE 2002120900193 20021209 00193 NM 2002 12 9 UPS02239961 1 20021202 A 7111 LONGERON BOEING 727 72730C 1384009 NM #2 R/H CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C ENG. #2 R/H FWD COWL CRACK ON UPPER LONGERON AT BS 1387 APPROX UNDER BLOCK(DOOR SHEAR) LONGERON R EMOVED IAW SRM 51-30-02. NEW LONGERON FABRICATED IAW SRM 5 1-30-1 NEW LONGERON INSTALLED IAW SRM 51-30-02 & REPORTECTED IAW MM 51-20-01 2 L 7 3 4F A3WE 2002120900194 20021209 00194 NM 2002 12 9 UPS02239962 1 20021124 A 5310 FITTING BOEING 727 72730C 1384009 NM TAILSKID BAY RH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C TAILSKID BAY R/H UPPER TENSION TIE AFT FITTING CRACKED NEW R/H UPPER TENSION TIE AFT FITTING INSTA LLED IAW SRM 51-30-02 AND DRAWING 65-25992 2 L 7 3 4F A3WE 2002120900195 20021209 00195 NM 2002 12 9 UPS02239963 1 20021122 A 2730 ELEVATOR BOEING 727 72730C 1384009 NM ELEV. STA 47 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C X-RAY INSP. SHOWS A CRACK INDICATION ON THE RIGHT ELEVATOR JUST I/B OF THE TAB AT ELEV. STA. 47, APPRO X. REPAIR CARRIED OUT IAW SRM 51-30-2,51-10-1, 55-20-3, 51-40-5, 51-10- 2 & DRAWING 65-25638 2 L 7 3 4F A3WE 2002120900196 20021209 00196 NM 2002 12 9 AWXA200201166 1 20021208 A 3350 BMS13311122 WIRE BOEING 737 737301 1384611 NM SEAT ROW 12 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 0 0 23261 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPA IRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 12 L/H, FUNCTIONAL TEST WAS GOOD. 2 L 7 2 4F RT A16WE 2002120900197 20021209 00197 NM 2002 12 9 AWXA200201171 1 20021119 A 5230 6547952166 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 0 0 23782 YVR - MAJOR REPAIR - DURING C-14 CHECK A 3/4" CRACK WAS FOUND ON THE AFT CARGO DOOR LOWER BEAM WEB, MID POINT NEAR BALAN CE CABLE PULLEY BRACKET. MAINTENANCE TRIMMED OUT DAMAGE ON LOWER BEAM WEB; FABRICATED A FILLER AND REPAIR SPLICE; AND IN STALLED REPAIR PARTS IAW AWA E.R. 03-5235-02340-ES2. 2 L 7 2 4F RT A16WE 2002120900198 20021209 00198 NM 2002 12 9 AWXA200201172 1 20021127 A 5320 6545834525 INTERCOSTAL BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 0 0 23777 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1/2" CRACK WAS FOUND ON VERTICAL WEB (INTERCOSTALS) AT BS 347, BL 0, WL 208.5. MAINTENANCE REMOVED ATTACH ANGLE, SHIM, STIFFENER, AND CRACKED INTERCOSTALS; FABRICATED A NEW REPLACEMENT INTERCOSTALS I AW B737-300 SRM 51-40-05, PG. 4, FIG. 2; AND INSTALLED REPAIR PART AND REINSTALLED REMOVED ATTACH ANGLE, SHIM, STIFFENER IAW B737-300 SRM 51-40-02, PG. 9-11, & 32, FIG. 8. 2 L 7 2 4F RT A16WE 2002120900199 20021209 00199 NM 2002 12 9 AWXA200201173 1 20021127 A 5311 654868719 ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 0 0 23777 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1" CRACK WAS FOUND ON THE LOWER FLANGE (ANGLE) OF THE L/H WHEEL WELL FRAME AT B S 680, LBL 66. MAINTENANCE REMOVED CRACKED ANGLE AT L/H WHEEL WELL FRAME BS 680, LBL 66; FABRICATED A NEW REPLACEMENT AN GLE; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 1-4, 6, & 38. 2 L 7 2 4F RT A16WE 2002121000001 20021210 00001 SO 2002 12 10 C2XA02CL244 1 20021205 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145ER 3260211 SO LEFT GEAR FAULTY A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 27 14925 145004 CLE FLIGHT#3031 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE WHEN THE GEAR WAS LOWERED.THE AIRCRAFT LANDED W ITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN GEAR AFT PROXIMITY SWITCH.OPERATIONAL CHECKS WE RE GOOD. 2 L 7 2 4F RT T00011AT 2002121000002 20021210 00002 SO 2002 12 10 C2XA02TY170 1 20021209 A 5710 INCC018880050A SPAR EMB 145 EMB145LR 3260212 SO CRACKED A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 16951 10631 145063 During mtx taxi of the aircraft, the R/H wing outbd. leading edge struck a storage shed causing damage to the R/H leadin g edge, wing tip, and fwd. spar. Maintenance spliced in a new section of spar 1, replaced rib 25, and replaced the outbd . leading edge and wing tip IAW EA5710-01036, EMB AMM, and EMB SRM. Aircraft perfomed satisfactory test flight following the repair and was returned to service. 2 L 7 2 4T RT T00011AT 2002121000003 20021210 00003 WP 2002 12 10 AALA20021396 1 20020926 A 3230 LINKAGE DOUG DC9 DC982 3022082 WP LT MLG DOOR DISCONNECTED A AALA K NONE J WARNING INDICATION DE DESCENT 1 SW 21 452AA 49553 TUL - FOUND DURING DESCENT TO LANDING WHEN GEAR WAS EXTENDED, GEAR DOOR LIGHT WOULD NOT EXTINGUISH. RAN ABNORMAL PROCED URE AND LANDED WITH GEAR DOORS EXTENDED, MINIMIZED LANDING ROLL. CHECKED AND FOUND LEFT DOOR SEQUENCE LINKAGE DISCONNEC TED, RECONNECTED LINKAGE. CHECKED AND FOUND RIGHT DOOR STRUCTURALLY SOUND. INSTALLED SERVICEABLE LEFT GEAR DOOR. DOOR RIGGED AND FIT CHECKED PER AA MM 32-31-04-02. (M) 2 L 7 2 4F A6WE 2002121000004 20021210 00004 WP 2002 12 10 AALA20021397 1 20020925 A 5342 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 278AA 49294 TUL - FOUND RIGHT VERTICAL STAB ATTACH ANGLE CRACKED AT CANT STATION 1463. INSTALLED DOUBLER PER AARD 53-10-00-2 PAGE 1 REPAIR 2. (M) 2 L 7 2 4F A6WE 2002121000005 20021210 00005 WP 2002 12 10 DHL2002807013 1 20021210 A 3297 WIRE DOUG DC8 DC873F 302199F WP A DHLA L O ABORTED APPROACH OTHER J WARNING INDICATION AP APPROACH 1 SO 01 807DH 45990 1) AFTER GEAR EXTENSION, NOSE GEAR LIGHT DID NOT COME ON. GEAR WAS CYCLED. NOSE GEAR LIGHT DID NOT COME ON. APPROACH WA S ABORTED AND DURING GO AROUND GEAR LIGHT CAME ON.2) CLEANED CONNECTOR OPS CHECKED GOOD IAW M/M 32-30-0. FOUND AND REPA IRED BROKEN WIRE IAW DC-8 WIRE DIAGRAM 32-1-0. 2 L 7 4 4F RT 4A25 2002121000006 20021210 00006 NM 2002 12 10 DL72S021146 1 20020928 A 7830 WARNING SYSTEM BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE COCKPIT MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 526DA 21586 700044 ON T/O ROLL, SPEED LESS THAN 60KTS, T/O POWER ESTABLISHED 1.94 EPR. THE NR 3 THRUST REV OPERATING LIGHT ILLUMINATED. T /O DISCONTINUED. AFTER CLEARING RUNWAY WITH ENGINE AT IDLE POWER THRUST REV OPERATING LIGHT WENT OUT. T/S THRUST REV O PERATING LIGHT SWITCH, CHECKED SW ADJ. SHOOK DOWN WIRING. INSP THRUST LINKAGE CLEANED SWITCH AND STRIKE PLATE. RAN TH RUST REV, ALL CK OK 2 L 7 3 4F 4 F A3WE E2EA 2002121000007 20021210 00007 EU 2002 12 10 DHL2002362010 1 20021209 A 2610 RELAY AIRBUS 300 A300B4203 3930306 EU A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 362DH 84 1) #2 ENGINE "B" LOOP WILL NOT TEST.2) TROUBLESHOT PER SCHEMATIC 26-12-00, JUMPERED 30WD PINS B AND 4, SYSTEM OPS CHEC KED NORMAL, REMOVED AND REPLACED RELAY 30WD, SYSTEM OPS CHECKED NORMAL AND OK FOR SERVICE PER M/M 26-12-00. 2 L 7 2 4F RT A35EU 2002121000008 20021210 00008 NM 2002 12 10 DL73K021187 1 20021011 A 5320 DRAIN BOEING 737 737247 138448D NM FUSELAGE FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 242WA 23516 ON CLIMBOUT NOTICED EXCESSIVE CABIN CLIMB RATE. LEVELED OFF AT 10000 FT. CABIN CONTINUED TO CLIMB TO 10000 FT. OUTFLO W VALVE SHOWED FULL CLOSED. FORWARD OUTFLOW VALVE SHOWS FULL CLOSED. COULD NOT CONTROL CABIN ALTITUDE AT ALL IN DESCEN T. REPLACED SEVERAL FUSELAGE DRAINS. 2 L 7 2 4F A16WE 2002121000009 20021210 00009 NM 2002 12 10 02FDEA00827 1 20021110 A 5315 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON UPPER SURFACE OF FLOORBEAM AROUND FLOOR BOARD HOLES AT BS 360, LBL 6 - RBL 6, WL 208. INSTALLED REPAIR AT LBL 7 BS 360 IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000010 20021210 00010 NM 2002 12 10 02FDEA00828 1 20021110 A 5315 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON TRANSVERSE FLOORBEAM AT BS 900, LBL 65, WL 205. REMOVED AND REPLACED FLOORBEAM IAW EA AND SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000011 20021210 00011 NM 2002 12 10 02FDEA00829 1 20021110 A 5320 STRINGER CLIP BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 STRINGER CLIP CRACKED AT BS 680, STR 10R. REMOVED AND REPLACED STRINGER CLIP IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000012 20021210 00012 NM 2002 12 10 02FDEA00830 1 20021108 A 5315 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 FLOORBEAM SURFACE CORROSION OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000013 20021210 00013 NM 2002 12 10 02FDEA00831 1 20021113 A 3260 WARNING SYSTEM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE COCKPIT MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 490FE 21493 ON TAKEOFF, GEAR RETRACTED NORMALLY, ALL LIGHTS OUT. WHEN GEAR HANDLE MOVED TO OFF, RED DOORS LIGHT ILLUMINATED, NO IND ICATION ON S/O PANEL. LIGHT WENT OUT WHEN HANDLE MOVED TO UP. REPEAT, GAVE SAME INDICATIONS. THIRD ATTEMPT, GEAR HAND LE OFF, ALL LIGHTS OUT. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000014 20021210 00014 NM 2002 12 10 02FDEA00832 1 20021110 A 5320 STRINGER CLIP BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 STRINGER CLIP CRACKED AT BS 660, STR 1. REMOVED AND REPLACED STRINGER CLIP IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000015 20021210 00015 NM 2002 12 10 02FDEA00833 1 20021111 A 5315 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON LOWER CHORD OF BS 950D AT NUTPLATE HOLE RBL 14-40, WL 200. REPAIRED LOWER CHORD OF FLOORBEAM AT BS 950 RBL 14-40. ALL WORK DONE IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000016 20021210 00016 NM 2002 12 10 02FDEA00834 1 20021113 A 2420 RCCB DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE ELECTRICAL SYS FAULTY A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 619FE 48770 JUST PRIOR TO TOP OF CLIMB, RIGHT EMERGENCY AC BUS OFF. CONSULTED WITH MOCC, RETURNED TO AIRPORT. EPCU FAULT LOGGED AN D FOUND B1-138 RCCB IN CAC SHOWED OPEN INDICATOR BUT B1-139 CONT CB WAS CLOSED. REMOVED AND REPLACED B1-138 RCCB IAW AM M, ALSO PRECAUTION REMOVED AND REPLACED B1-139 CB. EPCU RTS TEST PASSED IAW AMM. 2 L 7 3 4F 4 F RT A22WE E13NE 2002121000017 20021210 00017 NM 2002 12 10 02FDEA00838 1 20021114 A 2781 WARNING LIGHT BOEING 727 727200 138407E NM PWA JT8 JT8D* NE COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 273FE 22038 DURING FLAP RETRACTION FROM FLAPS 2 TO FLAPS UP. LED AMBER LIGHT REMAINED ILLUMINATED. POSITION TEST SELECTOR INDICATE D NR 2 LED WAS STILL EXTENDED, NR 2 SLAT. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000018 20021210 00018 NM 2002 12 10 02FDEA00839 1 20021113 A 5315 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION AT BS 344, WL 208, LBL 65 UNDERSIDE OF FLOORBEAM UPPER CHORD, AROUND THE NUTCLIP. REMOVED CORROSION ON FLOORB EAM UPPER CHORD. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED CHORD AND SPLICE IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000019 20021210 00019 NM 2002 12 10 02FDEA00840 1 20021113 A 5315 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON FLOORBEAM NUT PLATE HOLES BS 950F, LBL 10, WL 208. REMOVED CORROSION ON FLOORBEAM. FOUND TO BE OUT OF LIM ITS, REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PARTS IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000020 20021210 00020 NM 2002 12 10 02FDEA00841 1 20021113 A 5315 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON UPPER CHORD OF FLOORBEAM AROUND FLOORBOARD HOLES AT BS 680, RBL 4 TO RBL 21, WL 208. REMOVED AND REPLACED FLOORBEAM IAW EA AND ER. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000021 20021210 00021 NM 2002 12 10 02FDEA00842 1 20021113 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 BS 680, LBL 28 TO LBL 41, WL 208 FASTENER HOLES HAS CORROSION AT LWR SIDE. BLENDED CORROSION ON FLOORBEAM. FOUND FLOOR BEAM TO BE OUT OF LIMITS IAW SRM. 2 L 7 3 4F RT A3WE 2002121000022 20021210 00022 NM 2002 12 10 02FDEA00843 1 20021113 A 5315 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION BS 680, LBL 2 TO LBL 24, WL 208 FLOOR SUPPORT TOP AND BOTTOM. BLENDED CORROSION ON FLOORBEAM. FOUND FLOORBEA M TO BE OUT OF LIMITS IAW. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000023 20021210 00023 NM 2002 12 10 02FDEA00844 1 20021113 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON LWR CHORD OF BS 1070 FLOORBEAM AROUND NUTPLATE HOLES, BL0 - RBL 31, WL 200. REMOVED AND REPLACED FLOORBEAM IAW EA AND SRM. 2 L 7 3 4F RT A3WE 2002121000024 20021210 00024 NM 2002 12 10 02FDEA00845 1 20021112 A 5330 SKIN BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON SKIN AT BS 686, WL 147, STR 28R. SKIN WAS FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED SKIN. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000025 20021210 00025 NM 2002 12 10 02FDEA00846 1 20021112 A 5320 STRINGER CLIP BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON STR CLIP AT BS 680, STR 26R. STR CLIP WAS FOUND TO BE OUT LIMITS IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000026 20021210 00026 WP 2002 12 10 AALA20021287 1 20020829 A 2820 FUEL LINE DOUG DC9 DC982 3022082 WP FUEL SYSTEM CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 560AA 53090 TUL - FOUND FUEL LINE CRACKS WHERE THE FUEL LINE CONTACTS THE UPPER WING STRUCTURE PANEL NUMBER 1409C, OUTBOARD OF STATI ON XCW 121.688. FUEL LINE WAS REPAIRED BY INSTALLING A DOUBLER AND ADJUSTING THE CLAMPS THAT HOLD THE LINE SO THAT IT H AS CLEARANCE AFTER INSTALLATION SHOP ESO FOR FUEL LINE REPAIR. (M) 2 L 7 2 4F A6WE 2002121000027 20021210 00027 WP 2002 12 10 AALA20021379 1 20020911 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 443AA 49469 TUL - FOUND STATION 209 LONGERON 15 LEFT INNER SKIN CRACKED. CUT OFF TAB AND INSTALLED REPAIR STRAP PER AARD 53-10-00-1 1. (M) 2 L 7 2 4F A6WE 2002121000028 20021210 00028 WP 2002 12 10 AALA20021380 1 20020923 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 443AA 49469 TUL - FOUND SHEAR TIE DOUBLER CLIP CRACKED 1452 FRAME LEFT SIDE BETWEEN STRINGER 1 AND 3L. REMOVED CRACKED CLIP INSTALL ED NEW SHEAR TIE DOUBLER CLIP FRAME 1452. (M) 2 L 7 2 4F A6WE 2002121000029 20021210 00029 WP 2002 12 10 AALA20021390 1 20020917 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - AFT CARGO DOOR BEAM HAS CORROSION ON HORIZONTAL AND VERTICAL LEGS FROM STATION 1155-1212. BLENDED OUT CORROSION P ER SRM 51-10-03. INSTALLED FULL LENGTH DOUBLER PER AARD 53-10-00-16. (M) 2 L 7 2 4F A6WE 2002121000030 20021210 00030 WP 2002 12 10 AALA20021391 1 20020919 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - FOUND GROOVE WORN INTO BELTFRAME, STATION 1418 AT L18R. BLENDED OUT DAMAGE PER SRM 53-01. FABRICATED AND INSTALL ED DOUBLER PER AARD 53-10-00-14. (M) 2 L 7 2 4F A6WE 2002121000031 20021210 00031 WP 2002 12 10 AALA20021392 1 20020914 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 TUL - FOUND NR 1 SEAT TRACK AFT STATION 1250 CORRODED TOP SIDE OUTBOARD FLANGE. INSTALLED STRAP ON NR 1 SEAT TRACK AFT STATION 1250 PER AARD 53-20-00-13. (M) 2 L 7 2 4F A6WE 2002121000032 20021210 00032 WP 2002 12 10 AALA20021393 1 20020923 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 559AA 53089 TUL - FOUND CORROSION ON AFT CARGO HORIZONTAL AND VERTICAL LEG OF DOOR BEAM. INSTALLED DOUBLER REPAIR AT STATION 1172.1 TO STATION 1195.1. (M) 2 L 7 2 4F A6WE 2002121000033 20021210 00033 WP 2002 12 10 AALA20021394 1 20020923 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 559AA 53089 TUL - FOUND CORROSION ON NR 2 SEAT TRACK, FS 1295-1309. REPLACED SEAT TRACK PER 53-05-00. (M) 2 L 7 2 4F A6WE 2002121000034 20021210 00034 WP 2002 12 10 AALA20021395 1 20020925 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33414 49325 TUL - FOUND SHEAR TIE CRACKED ON AFT SIDE OF STATION 1437. INSTALLED NEW SHEAR TIE PER SRM. (M) 2 L 7 2 4F A6WE 2002121000035 20021210 00035 WP 2002 12 10 AALA20021398 1 20020925 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33414 49325 TUL - FOUND SHEAR TIE DOUBLER CRACKED UNDER LEFT SIDE VERTICAL STABILIZER ATTACH ANGLE. INSTALLED NEW SHEAR TIE PER SRM 51. (M) 2 L 7 2 4F A6WE 2002121000036 20021210 00036 WP 2002 12 10 AALA20021400 1 20020925 A 5730 SKIN DOUG DC9 DC982 3022082 WP WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33414 49325 TUL - FOUND NR 8 SLAT TRACK AREA, TOP OF LEADING EDGE HAS CRACK TO SKIN, XRS 256. STOP DRILLED CRACK AND INSTALLED DOUB LER PER AARD 57-30-00-8. (M) 2 L 7 2 4F A6WE 2002121000037 20021210 00037 WP 2002 12 10 AALA20021404 1 20020912 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 561AA 53091 TUL - FOUND CORROSION INSIDE SEAT TRACK NR 5 AT STATION 235. REMOVED DAMAGED AREA OF TRACK AND INSTALLED PLUG REPAIR PE R SRM 53-05-00 FIG 4A. (M) 2 L 7 2 4F A6WE 2002121000038 20021210 00038 WP 2002 12 10 AALA20021405 1 20020913 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 561AA 53091 TUL - FOUND CRACK IN SUB-FLOOR DIAPHRAGM AT STATION 210 OUTBOARD OF NR 4 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-00-0 0-02 PAGE NR 1. (M) 2 L 7 2 4F A6WE 2002121000039 20021210 00039 WP 2002 12 10 AALA20021406 1 20020912 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 561AA 53091 TUL - FOUND CORROSION ON NR 1 SEAT TRACK STATION 1250. REMOVED CORROSION. INSTALLED STRAP REPAIR PER AARD 53-20-00-13. (M) 2 L 7 2 4F A6WE 2002121000040 20021210 00040 WP 2002 12 10 AALA20021407 1 20020912 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 561AA 53091 TUL - FOUND CORROSION ON NR 1 SEAT TRACK STATION 1278. REMOVED CORROSION. INSTALLED STRAP REPAIR PER AARD 53-20-00-13. (M) 2 L 7 2 4F A6WE 2002121000041 20021210 00041 WP 2002 12 10 AALA20021408 1 20020917 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 561AA 53091 TUL - FOUND DENT AT STATION 237 BETWEEN STRINGER 18L AND 19L. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER PER SRM 53-04 F IG 2B. (M) 2 L 7 2 4F A6WE 2002121000042 20021210 00042 WP 2002 12 10 AALA20021409 1 20020912 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 561AA 53091 TUL - FOUND CORROSION ON RIGHT CUSP STATION 490 AROUND LIGHTENING HOLE. REMOVED DAMAGE, INSTALLED DOUBLER REPAIR PER SR M 53-01. (M) 2 L 7 2 4F A6WE 2002121000043 20021210 00043 WP 2002 12 10 AALA20021410 1 20020918 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 561AA 53091 TUL - FOUND RIGHT CUSP MEMBRANE CORRODED STATION 987-991. CUT OUT DAMAGE FABRICATED AND INSTALLED DOUBLER PER AARD 53-0 0-00-02. (M) 2 L 7 2 4F A6WE 2002121000044 20021210 00044 WP 2002 12 10 AALA20021411 1 20020917 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 561AA 53091 TUL - FOUND CORROSION ON NR 6 SEAT TRACK STATION 218. INSTALLED SEAT TRACK SPLICE REPAIR PER SRM 53-05 PK10K FIG 4F SHE ET 5. (M) 2 L 7 2 4F A6WE 2002121000045 20021210 00045 WP 2002 12 10 AALA20021412 1 20020912 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 561AA 53091 TUL - FOUND CORROSION ON NR 3 SEAT TRACK STATION 1204. INSTALLED REPAIR PER SRM 53-05 FIG 4. (M) 2 L 7 2 4F A6WE 2002121000046 20021210 00046 WP 2002 12 10 AALA20021419 1 20021004 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 477AA 49652 TUL - FOUND TORSION BRACKET CRACKED BELOW AFT STAIR LEFT UPLOCK ACTUATOR. REMOVED CRACK ANGLE BRACKET AND INSTALLED FAB RICATED ANGLE BRACKET. (M) 2 L 7 2 4F A6WE 2002121000047 20021210 00047 WP 2002 12 10 AALA20021435 1 20021008 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 291AA 49303 TUL - FOUND FUSELAGE SKIN CRACKED JUST ABOVE SKIN LAP AT STATION 1380 AT L11L LONGERON APPROX .25 INCH LONG CRACK. INST ALLED DOUBLER AFTER STOP DRILL OF CRACK PER SRM 53-01-00 AND AARD 53-30-00-02. (M) 2 L 7 2 4F A6WE 2002121000048 20021210 00048 WP 2002 12 10 AALA20021436 1 20021008 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 291AA 49303 TUL - FOUND FUSELAGE SKIN CRACKED AT FASTENER STATION 1380 LONGERON 14L RT. STOP DRILLED CRACK AND INSTALLED DOUBLER PE R SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2002121000049 20021210 00049 WP 2002 12 10 AALA20021437 1 20021008 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 291AA 49303 TUL - FOUND SHEAR TIE CRACKED AFT SIDE OF FS 1451 FRAME AFT OF LONGERON 2R. REMOVED AND REPLACED CRACKED SHEAR TIE AT 2 R AND 1451 PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002121000050 20021210 00050 WP 2002 12 10 AALA20021463 1 20020927 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 556AA 53086 TUL - FOUND CORROSION IN LIGHTENING HOLE CUT OUT, LOWER SIDE OF CUSP. MADE DOUBLER REPAIR PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002121000051 20021210 00051 WP 2002 12 10 AALA20021464 1 20021003 A 5320 STRAP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 556AA 53086 TUL - FOUND FORWARD GALLEY DOOR CUTOUT LOWER SILL STRAP AND SUBPLATE CORRODED. REMOVED AND REPLACED CORRODED SILL STRAP AND SUBPLATE. (M) 2 L 7 2 4F A6WE 2002121000052 20021210 00052 WP 2002 12 10 AALA20021465 1 20020930 A 5320 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 556AA 53086 TUL - FOUND ATTACH ANGLE ON AFT SIDE OF FS 1429 FRAME CRACKED, 10 INCHES TO THE LEFT OF LONGERON 1. INSTALLED NEW ATTAC H ANGLE ON AFT SIDE OF FS 1429. (M) 2 L 7 2 4F A6WE 2002121000053 20021210 00053 EU 2002 12 10 02344330 1 20021210 A 3350 6147051 BATTERY PACK JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 330UE 41098 During a maintenance check, it was discovered that the #1 emergency lighting power pack and battery was inoperative. Ma intenance personnel removed and replaced the #1 emergency lighting power pack and battery. An operational check was sat isfactory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002121000054 20021210 00054 WP 2002 12 10 AALA20021466 1 20021007 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 556AA 53086 TUL - FOUND SHEAR TIE DOUBLER CRACKED ABOVE Y-DUCT FRAME 1445 AFT SIDE BETWEEN STRINGER 1 AND 3L. REMOVED AND REPLACED DOUBLER PER SRM 51-10-01. (M) 2 L 7 2 4F A6WE 2002121000055 20021210 00055 WP 2002 12 10 AALA20021467 1 20020926 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 556AA 53086 TUL - FOUND LEFT CABIN WINDOW FRAME CRACKED LOWER FORWARD CORNER STATION 1022. INSTALLED DOUBLER ON WINDOW FRAME LOWER FORWARD CORNER STATION 1022, PER 53-10-00-25 PAGE 1/2. (M) 2 L 7 2 4F A6WE 2002121000056 20021210 00056 WP 2002 12 10 AALA20021468 1 20020926 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 556AA 53086 TUL - FOUND LEFT CABIN WINDOW FRAME CRACKED LOWER FORWARD CORNER STATION 984. INSTALLED DOUBLER ON WINDOW FRAME LOWER F ORWARD CORNER STATION 984 IAW 53-10-00-25 PAGE 1/2. (M) 2 L 7 2 4F A6WE 2002121000057 20021210 00057 WP 2002 12 10 AALA20021469 1 20021009 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 556AA 53086 TUL - FOUND AFT CARGO DOOR BEAM HAS CORROSION FROM STATION 1160-1207. INSTALLED BEAM PER AARD 53-10-00. (M) 2 L 7 2 4F A6WE 2002121000058 20021210 00058 SO 2002 12 10 000231 1 20021130 A 2120 SMOKE EMB 145 EMB145 3260210 SO COCKPIT DETECTED A CHQA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 11 265 SMOKE IN COCKPIT ON LANDING, AIRCRAFT TAXIED TO GATE UNDER OWN POWER. 2 L 7 2 4F RT T00011AT 2002121000059 20021210 00059 EU 2002 12 10 00065 1 20021127 A 7931 11346AA INDICATOR AMD FALC20 FALCON 2720302 EU COCKPIT FAILED E HAEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 05 240TW 40 PILOT REPORTED LEFT ENGINE OIL PRESSURE INDICATION DROP TO (0) IN FLIGHT, DIVERTED FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED OIL PRESSURE INDICATOR. OP'S CK GOOD, RETURN AIRCRAFT TO SERVICE. 2 L 7 2 4F A7EU 2002121000060 20021210 00060 NM 2002 12 10 0203906306 1 20021128 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 666US 23821 DURING LINE CHECK, FOUND RIGHT (D) ZONE FLOOR EMERGENCY PATH LIGHTS INOPERATIVE. REPAIRED WIRING AND OPERATIONALLY CHEC K GOOD. 2 L 7 4 4F RT A20WE 2002121000061 20021210 00061 NM 2002 12 10 0203916739 1 20021201 A 3260 CIRCUIT CARD BOEING 747 747251F 1384898 NM WARNING SYSTEM FAULTY A NWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 01 639US 23887 DURING APPROACH, THE RED LANDING GEAR LIGHT ILLUMINATED WITH LANDING GEAR DOWN. RECEIVED A GPWS WARNING AT 500 FEET. A IRCRAFT EXECUTED A GO-AROUND. RECYCLED THE LANDING GEAR AND ALL INDICATIONS WERE NORMAL. REPLACED AURAL WARNING SYSTEM CIRCUIT CARDS A3, A6 & A11. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2002121000062 20021210 00062 WP 2002 12 10 0203949940 1 20021113 A 5310 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3322L 47031 DURING AN OVERNIGHT CHECK, A CRACK WAS FOUND IN THE AFT PRESSURE BULKHEAD DOORJAMB. THE AIRCRAFT WAS FERRIED TO ACCOMPL ISH REPAIRS. THE CRACK WAS 2 INCHES LONG AT STATION X=59.8. REPAIRED IAW EA. 2 L 7 2 4F A6WE 2002121000063 20021210 00063 WP 2002 12 10 0203989955 1 20021122 A 5330 SKIN DOUG DC9 DC931 3022065 WP PWA JT8 JT8D1 52044 NE FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 922RW 47182 IN MSP A 2.1 INCH CRACK WAS FOUND ON THE RIGHT SIDE OF FUSELAGE SKIN AT STA 1143 ABOVE L14. REPAIRED IAW EA. 2 L 7 2 4F 4 F A6WE E2EA 2002121000064 20021210 00064 CE 2002 12 10 0226 1 20021114 A 2612 FIRE LOOP CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP NR 1 ENGINE OUT OF POSITION E DJFA E ENGINE SHUTDOWN N FALSE WARNING TO TAKEOFF 1 EA 23 311CW 6500011 P87138C NR 1 ENGINE FIRE LIGHT CAME ON DURING TAKEOFF. FOUND SENSOR LOOP TOUCHING OIL COOLER. REPOSITIONED, OPS CHECKED OK. 2 L 7 2 4F 4 F A9NM E6WE 2002121000065 20021210 00065 NM 2002 12 10 02333413 1 20021129 A 3350 LIGHT DORNER DO32 DO328300 NM CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 413FJ 3168 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AFT EMERGENCY FLOOR LIGHTING WAS INOPERATIVE. MAINTENANCE PERSO NNEL SECURED THE AFT CABIN EMERGENCY FLOOR LIGHT STRIP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETU RNED TO SERVICE. 2 H 7 2 4T RT A55NM 2002121000066 20021210 00066 EU 2002 12 10 02334320 1 20021130 A 3397 GROUND WIRE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE331* 01514 WP CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 320UE 41043 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE PER SONNEL SECURED GROUND WIRES EP37 AND EP38. AN OPERATIONAL CHECK OF THE EMERGENCY EXIT LIGHTS WAS SATISFACTORY AND THE A IRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A41NM E2WE 2002121000067 20021210 00067 EA 2002 12 10 02337652A 1 20021203 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 652BR 7429 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIV E. THE AIRCRAFT WAS FERRIED TO IAD FOR MAINTENANCE. MAINTENANCE PERSONNEL SECURED THE CONNECTOR FOR THE FORWARD SECTIO N OF EMERGENCY FLOOR TRACK LIGHTING. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2002121000068 20021210 00068 NM 2002 12 10 02FDEA00847 1 20021112 A 5330 DOUBLER BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON SKIN DOUBLER BS 680, STR 27R, WL 147. CORROSION WAS FOUND TO BE OUT OF LIMITS AT BS 680, STR 27R, WL 147. REPAIRED AREA IAW EA AND SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000069 20021210 00069 NM 2002 12 10 02FDEA00848 1 20021113 A 5315 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON FLOORBEAM UPPER FLANGE AROUND NUTPLATE HOLES AT BS 950C, RBL45-55, WL 208. REMOVED AND REPLACED FLOORBEAM IAW EA AND SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000070 20021210 00070 NM 2002 12 10 02FDEA00849 1 20021113 A 5315 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON BS 1090 FLOORBEAM LOWER CHORD AT NUTPLATE HOLES, RBL 21, WL 200. REMOVED AND REPLACED FLOORBEAM IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000071 20021210 00071 NM 2002 12 10 02FDEA00850 1 20021101 A 5330 SKIN BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 CORROSION ON SKIN BS 720C+1 BETWEEN STR 28L-28R. REPAIRED SKIN BS 720C+1, STR 28L-28R IAW EA. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000072 20021210 00072 NM 2002 12 10 02FDEA00851 1 20021110 A 5314 KEELBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 COMPLY WITH EO REV C1 PT5 KEELBEAM CHORD REPAIR BS 980-1007, STR 29L. REPAIRED KEELBEAM BS 980-1007, STR 29L IAW EO. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121000073 20021210 00073 NM 2002 12 10 02FDEA00853 1 20021112 A 5310 SHEAR TIE BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON SHEAR TIE BS 950C AFT SIDE OF FRAME JUST OUTBOARD OF STR 29L. CORROSION ON SHEAR TIE AT BS 950C O/B OF STR 29L WAS FOUND OUT OF LIMITS REPAIRED SHEAR TIE IAW FEDEX EA AND SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2003012200110 20030122 00110 EU 2003 1 22 AWXA200201174 2 20021208 A 7321 8063207 MEC BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 ENGINE FAULTY A AWXA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 WP 28 150AW 37606 1423 23218 721138 ON DESCENT CAUTION PANEL INDICATED RT ENG FAILED. COMPLETED ENG SHUTDOWN. RESTARTED NR 2 ENG. MX REMOVED NR 2 ENG FUE L FILTER & INSPECTED FILTER & HIGH PRESSURE FUEL PUMP. ENG PERF & DETERIORATION TEST, POWER TRIM CHECK, CHECKS GOOD. F UEL FILTER REPLACED. NR 2 ENG MAIN FUEL PUMP & MAIN ENG CONTROL REPLACED. VENDOR BENCH TEST OF ENG MAIN FUEL PUMP, NO FAULT FOUND, REPLACED FUEL FILTER ELEMENT. COULD NOT CONFIRM FAILURE. TWO POINTS ON POWER LEVER, TRANSDUCER, AND ON ACC EL & VSV FOUND SLIGHTLY OUT OF LIMITS, ONE POINT ON TORQUE MOTOR, CDP & DECEL. UNIT SATISFACTORY. VENDOR STATES TEST F IGURES OBTAINED WOULD NOT INDICATE A CONDITION THAT WOULD RESULT IN AN ENG SPOOL DOWN. 2 L 7 2 4F 4 F RT A16WE E21EU 2002121000074 20021210 00074 NM 2002 12 10 AWXA200201175 1 20021119 A 5330 2024T3056 SKIN BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 0 0 22656 LCQ - MAJOR REPAIR - DURING C-14 CHECK A 1/2" CRACK WAS FOUND ON THE FUSELAGE SKIN AT BS 1071, STR 22 R/H, NEAR FIRE EXT INGUISHER INDICATOR. MAINTENANCE CUTOUT CRACK AT BS 1071, STR 22 R/H; FABRICATED A REPAIR DOUBLER AND INSTALLED REPAIR P ART IAW B737-200 SRM 53-30-3, FIG. 1, PG. 2B-2E. 2 L 7 2 4F RT A16WE 2002121000075 20021210 00075 NM 2002 12 10 AWXA200201176 1 20021120 A 5313 693535213 TIE CLIP BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 0 0 22656 LCQ - MAJOR REPAIR - DURING C-14 CHECK A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 6 L/H. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 616, STR 6 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-35352; AND INS TALLED REPAIR PART IAW AWA E.O. 53-12-01. 2 L 7 2 4F RT A16WE 2002121000076 20021210 00076 NM 2002 12 10 AWXA200201177 1 20021120 A 5313 693535214 TIE CLIP BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 0 0 22656 LCQ - MAJOR REPAIR - DURING C-14 CHECK A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 685, STR 4 R/H. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 685, STR 4 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-35352; AND INS TALLED REPAIR PART IAW AWA E.O. 53-12-01. 2 L 7 2 4F RT A16WE 2002121000077 20021210 00077 NM 2002 12 10 AWXA200201178 1 20021120 A 5313 6935353214 TIE CLIP BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 0 0 22656 LCQ - MAJOR REPAIR - DURING C-14 CHECK CRACKS WERE FOUND ON STRINGER TIE CLIPS BS 727A, STR 7 & 9 L/H, AND STR 3 R/H. MA INTENANCE REMOVED CRACKED STRINGER TIE CLIPS BS 727A, STR 7 & 9 L/H, AND STR 3 R/H; FABRICATED 3 NEW REPLACEMENT STRINGE R TIE CLIPS PER DWG 69-35352; AND INSTALLED REPAIR PARTS IAW AWA E.O. 53-12-01, PG.7. 2 L 7 2 4F RT A16WE 2002121000078 20021210 00078 NM 2002 12 10 AWXA200201179 1 20021120 A 5313 693535214 TIE CLIP BOEING 737 737277 1384570 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 0 0 22656 LCQ - MAJOR REPAIR - DURING C-14 CHECK A CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 787, STR 8 L/H. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 787, STR 8 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-35352; AND INS TALLED REPAIR PART IAW AWA E.O. 53-12-01. 2 L 7 2 4F RT A16WE 2002121000079 20021210 00079 WP 2002 12 10 CALA0200575 1 20021208 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP STA 1287-1309 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72830 49490 INSPECTION FOUND A 3" CRACK IN INTERCOSTAL IN AFT BAGGAGE BIN AT CEILING BETWEEN STA 1287 AND 1309, JUST RIGHT OF CENTER . A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-05. 2 L 7 2 4F A6WE 2002121000080 20021210 00080 WP 2002 12 10 CALA0200576 1 20021209 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP STA 1271-1287 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72830 49490 NSPECTION FOUND A 3" CRACK IN INTERCOSTAL IN AFT BAGGAGE BIN BETWEEN STA 1271 AND 1287 AT CEILING RIGHT OF CENTERLINE. I NSTALLED REPAIR IAW SRM 51-30. 2 L 7 2 4F A6WE 2002121000081 20021210 00081 WP 2002 12 10 CALA0200577 1 20021209 A 5313 LONGERON DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72830 49490 INSPECTION FOUND A 2" CRACK IN LONGERON 2R AT STA 1418. A REPAIR WAS PERFORMED IAW ECRA 5311-01132. 2 L 7 2 4F A6WE 2002121000082 20021210 00082 NM 2002 12 10 CALA0200578 1 20021209 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 380 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND A 0.15" CRACK IN SKIN AT A/C ACCESSORY COOLING EXHAUST OUTLET ON AFT SIDE, STA 380, S27L. A REPAIR DOUB LER WAS INSTALLED IAW ECRA 5330-02894. 2 L 7 2 4F RT A16WE 2002121100003 20021211 00003 CE 2002 12 11 CA021120004 1 20021116 A 3233 58130441 BRACKET CESSNA 441 441 2076020 CE GARRTT TPE331 TPE33110 01514 WP NLG ACTUATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A SCHEDULED INSPECTION, THE NOSE LANDING GEAR ACTUATOR ATTACH BRACKETS WERE FOUND TO BE CRACKED. 1 L 7 2 3T 4 T RT A28CE E4WE 2002121100006 20021211 00006 EA 2002 12 11 CA021120007 2 20021120 A 7314 GEAR DHAV DHC6 DHC6200 2802620 EA PWA PT6 PT6A20 52043 EA ROTARY PUMP WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FUEL PUMP WAS REMOVED FROM ENGINE DURING ENGINE CONVERSION FROM PT6A-20 TO PT6A-27. THE PUMP WAS SENT TO PWC FOR B ENCH TEST AND INHIBITING. CONTRACTOR ASSERTS THAT THE PUMP WAS TESTED AND THAT THE SEALS WERE LEAKING. DISMANTLED THE PU MP AND FOUND THAT THERE IS EXCESSIVE WEAR IN THE INTERNAL SPLINES IN THE DRIVING GEAR AND COUPLING, RENDERING BOTH PARTS UNSERVICEABLE. THE PUMP HAS IN EXCESSIVE OF 0.006 INCH WEAR AND A BROWN SUBSTANCE ON THE SPLINES. THE PUMP HAS 340.3 HO URS SINCE OVERHAUL 1 H 7 2 3T 3 T RT A9EA E4EA 2002121100007 20021211 00007 SW 2002 12 11 CA021120008 1 20021104 A 6310 CLUTCH KAMAN K1200 K1200 05625F6 SW LYC T53 T5317A 41549 NE ENG/XMSN FAILED W A UNSCHED LANDING D INFLIGHT SEPARATION AP APPROACH 1 CA (CAN) PILOT HEARD A LOUD BANG AS HE WAS LOWERING A LOG ONTO LANDING WITH A SLIGHT DROP IN ALTITUDE. THE AIRCRAFT WAS LAN DED AND THE MAIN DRIVE SHAFT BETWEEN ENGINE AND TRANSMISSION WAS ROTATED. THE ROTATIONHAD A ROUGH SOUND WHICH WAS REPORT ED TO THE AIRCRAFT MANUFACTURER. THE CLUTCH ASSY WAS REMOVED ANDHAD SIGNS OF SPRAG DAMAGE. THE MANUFACTURE RECOMMENDED C HANGING CLUTCH AND INPUT. A MANUFACTURES REPRESENTITIVE IS GOING TO LOOK AT CLUTCH AND INSTALL NEW INPUT. INVESTIGATION BY MANUFACTURER IS CONTINUING. A/F TIME 6504.3 DATE OF OCCURANCE NOV.4/02 1 G 7 1 4F 4 U NT TR7BO E17EA 2002121100011 20021211 00011 EA 2002 12 11 CA021121006 1 20021114 A 3397 SPLICE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE PSU OVERHEATED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) BURNING ODOR IN CABIN AROUND ROW 11 & 12 OVERHEAD BIN AREA. ODOR DISSIPATED WHEN CABIN LIGHTING WAS TURNED OFF. M AINTENANCE DISCOVERED BURNED PIDC SPLICES OVER PASSENGER SERVICE UNIT NR 4 (RT FWD). SEVERAL SPLICES WERE REPLACED ON B IN HARNESS USING SPLICE, SUPPLIMENTARY INFORMATION AND INSPECTION PROCEDURES: A SIMILAR SITUATION ON ANOTHER AIRCRAFT T HE PREVIOUS MONTH REQUIRED RECTIFICATION OF SEVERAL SPLICES AND SOME WIRE CONNECTIONS. THIS PROMPTED A FLEET CAMPAIGN DI RECTIVE FOR ALL DH8 AIRCRAFT IN OUR FLEET. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2002121100019 20021211 00019 EA 2002 12 11 CA021125002 1 20021111 A 2710 BEARING CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A NE AILERONS BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 12368 (CAN) DURING 300-600 HOURS INSPECTION AILERON PCU OPERATION TEST, FOUND AILERON QUADRANT IN RT WHEEL WELL IS NOISY (SNAP PING).AFTER REMOVING RT/ AILERON QUADRANT ASSEMBLY FOR INVESTIGATION, FOUND RT/ QUADRANT, BEARING IS DAMAGED (RACES HAL F WAY ROUND). CHANGED BOTH RT AND LT QUADRANT ASSEMBLIES, NOISE DISAPPEARED. 2 L 7 2 4F 4 F RT A21AE E15NE 2002121100022 20021211 00022 NM 2002 12 11 MEX2002347 1 20021122 A 7500 233N32516 PANEL BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE BLEED AIR FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 806AM 26273 CAPTAIN REPORTED THAT THE RT ENGINE BLEED VALVE SWITCH WAS OUT OF SERVICE PANEL WAS REMOVED AND SWITCH WAS UNCLOGGED AND PNEUMATIC SYSTEM WAS LET OUT OF SERVICE IAW MM. DURING TRANSIT PANEL ASSEMBLY BLEED AIR WAS REPLACED IAW MM. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121100023 20021211 00023 NM 2002 12 11 MEX2002348 1 20021123 A 2613 371215280 THERMOSWITCH DOUG MD88 MD88 3023688 NM PWA JT8 JT8D9 52048 NE TAIL FAILED W ASMF A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 23 158PL 49761 CAPTAIN REPORTED THAT DURING CLIMB TAIL COMPT TEMP HIGH LIGHT TURNED ON. FOLLOWING THE PROCEDURE WAS DETERMINED LEAKAGE ON RIGHT ENGINE DESCENDING. FLIGHT TEMPERATURE SENSOR WAS INTERCHANGED WITH THE LEFT, TURNING LIGHT OFF. DURING PASSE NGERS BOARDING LIGHT TURN ON AGAIN. RIGHT SENSOR WAS DISCONNECTED TURNING OF THE LIGHT. SENSOR WAS REPLACED IAW MM AND TEST WERE PERFORMED IAW MM. 2 L 7 2 4F 4 F RT A6WE E2EA 2002121100037 20021211 00037 GL 2002 12 11 AC2A081568 2 20021203 A 7200 6898642 GEARSHAFT SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL ENGINE BROKEN H AC2A K NONE O OTHER IN INSP/MAINT 1 FS 01 7266K 760283 N-1 WENT TO ZERO, ENGINE OUT AUDIO CAME ON, ENGINE CHIP LIGHT ON 1 G 7 2 3U 3 U H1NE E1GL 2002121100038 20021211 00038 GL 2002 12 11 AC2A081579 2 20021125 A 7321 23065104 FUEL CONTROL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL ENGINE LEAKING H AC2A K NONE K FLUID LOSS IN INSP/MAINT 1 FS 01 8776 8535 776 FUEL CONTROL LEAKING FUEL FROM WHERE THE MAX FLOW STOP SHAFT ENTERS THE FUEL CONTROL BODY. THIS WAS FOUND DURING GROUND RUN, PRIOR TO TAKE-OFF. REPLACED FUEL CONTROL. 1 G 7 2 3U 3 U H3EU E4CE 2002121100040 20021211 00040 SW 2002 12 11 AC2A081581 1 20021130 A 3210 222036037111 SUPPORT BELL 430 430 1182150 SW MLG CRACKED H AC2A K NONE O OTHER IN INSP/MAINT 1 FS 01 430CV 2109 49072 PART IS CRACKED. REPLACED WITH SERVICEABLE FITTING ASSEMBLY. 1 G 7 2 3U RT H9SW 2002121100041 20021211 00041 SW 2002 12 11 AC2A081582 1 20021130 A 3213 430036140105 CROSSTUBE BELL 430 430 1182150 SW MLG CORRODED H AC2A K NONE O OTHER IN INSP/MAINT 1 FS 01 430CV 49072 CORROSION ON AFT CROSSTUBE, RIGHT HAND SIDE JUST OUTBOARD OF CLAMP. REPLACED WITH SERVICEABLE CROSSTUBE. 1 G 7 2 3U RT H9SW 2002121100042 20021211 00042 SW 2002 12 11 AC2A081583 1 20021130 A 5302 222035231105 FITTING BELL 430 430 1182150 SW TAILBOOM BROKEN H AC2A K NONE O OTHER IN INSP/MAINT 1 FS 01 430CV 2109 49072 ONE OF THE EARS BROKE OFF THE FITTING. REPLACED WITH SERVICEABLE FITTING ASSEMBLY. 1 G 7 2 3U RT H9SW 2002121100043 20021211 00043 SW 2002 12 11 AC2A081584 1 20021130 A 6210 430015001123 BLADE BELL 430 430 1182150 SW BLADE CRACKED H AC2A K NONE O OTHER IN INSP/MAINT 1 FS 01 430CV 2109 49072 LEADING EDGE ABRASION STRIP IS CRACKED CHORDWISE, ABOUT MIDWAY DOWN BLADE. REPLACED WITH NEW SERVICEABLE MAIN ROTOR BLAD E. 1 G 7 2 3U RT H9SW 2002121100044 20021211 00044 SW 2002 12 11 AC2A081585 1 20021203 A 7810 230063301101 DUCT BELL 430 430 1182150 SW EXHAUST CRACKED H AC2A K NONE O OTHER IN INSP/MAINT 1 FS 01 430CH 49037 EXHAUST DUCT ASSY IS CRACKED. REPLACED EXHAUST DUCT ASSY. 1 G 7 2 3U RT H9SW 2002121100045 20021211 00045 SO 2002 12 11 ALGA081570 2 20021203 A 8550 23030999 HOUSING CLARK 1000 1000CLARK 2230102 SW CONT R670 W6706N 17016 SO OIL PUMP CORRODED H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 PARTO OIL PUMP HOUSING HAS CORROSION IN FWD AND AFT GEAR BORES, AND OIL PORT. 1 Q 7 1 3R 3 R 2A6 E162 2002121100046 20021211 00046 EU 2002 12 11 ALGA081576 1 20021204 A 6730 SC50911 SERVO UROCOP EC120 EC120B 8680987 EU CYCLIC BROKEN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 515AL 519 1165 ON NR 2 HYDRAULIC, GROUND CYCLIC MOVES HARD LT. 1 G 7 2 3U NC R0001RD 2002121100047 20021211 00047 EU 2002 12 11 ALGA081577 1 20021204 A 6730 SC50911 SERVO UROCOP EC120 EC120B 8680987 EU CYCLIC BROKEN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 515AL 519 1165 ON NR 2 HYDRAULIC SYS. GROUND CYCLIC MOVES HARD LT. 1 G 7 2 3U NC R0001RD 2002121100048 20021211 00048 SW 2002 12 11 ALGA081586 1 20021206 A 6510 206061432121 HOUSING BELL 407 407 1182206 SW BLOWER CRACKED H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 403AL 1442 53478 HOUSING CRACKED. REMOVED AND REPLACED. RETURNING FAILED UNIT. 1 G 7 1 3U O H2SW 2002121100049 20021211 00049 EU 2002 12 11 B3OR20020021 1 20021108 A 2110 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE AC COMPRESSOR FAILED B B3OR K NONE O OTHER IN INSP/MAINT 1 SW 03 5204X 3099 9570 DURING POST FLIGHT INSPECTION TECHNICAN ROTATED MAIN ROTOR TO INSPECT. WHILE TURNING HE NOTED THAT IT WAS VERY HARD TO TURN. FURTHER TROUBLESHOOTING REVEALED THE AIR CONDITIONER COMPRESSOR BELT SLIPPING ON THE COMPRESSOR DRIVE PULLEY. THE AIR CONDITIONER COMPRESSOR CLUTCH BEARING HAD FAILED MAKING IT VERY HARD TO TURN. 1 G 7 1 3U 3 U H9EU E19EU 2002121100050 20021211 00050 EU 2002 12 11 BAQA081165 1 20021017 A 3610 97914211 VALVE BOLKMS 117 BK117B1 5626012 EU AIR SYSTEM LEAKING H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 213AE 230 7219 AIR VALVE LEAKS. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002121100051 20021211 00051 2002 12 11 BAQA081534 4 20021126 A 3421 4021541671 INDICATOR BOLKMS 117 BK117A3 5626015 EU COCKPIT FAILED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 911BK 6440 7099 GYRO TAKES TOO LONG TO COME ON LINE. 4-5 MINUTES. SPEX FILE WITH NO NUMBER REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002121100052 20021211 00052 NM 2002 12 11 02FDEA00866 1 20021119 A 2781 CONNECTOR BOEING 727 727200 138407E NM L/E SLAT DIRTY A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 287FE 21849 LEADING EDGE FLAPS WOULD NOT RETRACT AFTER T/O. AMBER L/E FLAPS LIGHT DID NOT EXTINGUISH AT 2 DEG. AMBER IN TRANSIT LI GHT ON NR 2 SLAT LEFT WING WAS ILLUMINATED ON S/O PANEL. ENG ANTI-ICE WAS ON, WING ANTI-ICE WAS CLOSED. NR 2 L/E SLAT HAS JUMPER INSTALLED PER B-727-200 MM27-82-000. CYCLED FLAPS INITIALLY WITH ALL INDICATIONS NORMAL. CLEANED CONNECTERS AND INSTALLED JUMPER PRE- CAUTIONARY FOR POSSIBLE INTERMITTENT INDICATION. 2 L 7 3 4F RT A3WE 2002121100053 20021211 00053 2002 12 11 BAQA081535 4 20021126 A 3422 40205773 GYRO BOLKMS 117 BK117A3 5626015 EU COCKPIT MALFUNCTIONED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 911BK 7099 DISPLAY STICKS PERIODICALLY AND LIGHT COMES ON AND OFF DURING FLIGHT. SPEX FILE. NO NUMBER GIVEN. REPLACED WITH SERVIC EABLE UNIT. 1 G 7 2 3U H13EU 2002121100054 20021211 00054 2002 12 11 BAQA081536 4 20021126 A 2210 7000299908 SWITCH BOLKMS 117 BK117A1 5626010 EU AUTOPILOT FAILED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 955ME 5887 7243 FDSEL SWITCH STICKS. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002121100055 20021211 00055 2002 12 11 BAQA081545 4 20021127 A 3120 B1894522284DN CLOCK UROCOP EC135 EC135T1 5620026 EU COCKPIT FAILED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 575ME 766 0157 CLOCK STOPPED. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2002121100056 20021211 00056 NM 2002 12 11 02FDEA00867 1 20021119 A 5230 HANDLE BOEING 727 727100 1384036 NM CARGO DOOR OUT OF POSITION A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 136FE 19855 ON DEPARTURE, FWD CARGO DOOR LT ILLUM FOLLOWED RED TABS AND ELECTED TO RETURN TO PIT FOR MX ACTION. PRESSURIZATION NOT NORMAL/NOTED PRESS BUMP DURING CLIMBOUT. UPON INSPECTION OF FORWARD LOWER CARGO DOOR. FOUND HANDLE INSIDE DOOR SLIGHTL Y OPPOSITE OF OUTSIDE HANDLE. REPOSITIONED INSIDE HANDLE AND CYCLED DOOR A DOZEN TIMES. DOOR CLOSED AND LATCHED NORMALL Y AND LIGHT EXTINGUISHED. 2 L 7 3 4F RT A3WE 2002121100057 20021211 00057 2002 12 11 BAQA081546 4 20021127 A 3422 501184501 GYRO UROCOP EC135 EC135T1 5620026 EU COCKPIT MALFUNCTIONED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 575ME 485 0157 LIGHTING INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2002121100058 20021211 00058 EU 2002 12 11 BAQA081559 1 20021202 A 2560 3100 FIRST AID KIT UROCOP EC135 EC135P1 8680990 EU COCKPIT DETERIORATED H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 911TS 344 0167 DETERIORATION TO THE POINT OF UNSERVICEABILITY. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U O H88EU 2002121100059 20021211 00059 NM 2002 12 11 02FDEA00868 1 20021121 A 5243 6556235159 DOOR BOEING 727 727200 138407E NM HYD SERVICE MISSING A FDEA O OTHER D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 25 276FE 22041 DURING POST FLIGHT WALK AROUND FOUND HYD SERVICE DOOR MISSING. INSPECTED AREA FOR DAMAGE FROM DOOR COMING OFF. NO DAMA GE FOUND. INSTALLED SERVICEABLE DOOR IAW STANDARD MAINT PRACTICES, OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2002121100060 20021211 00060 NM 2002 12 11 02FDEA00869 1 20021110 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264 21626 CORROSION ON LWR CHORD OF BS 950F AT NUT PLATEHOLE, RBL 24, WL 200. 2 L 7 3 4F A3WE 2002121100061 20021211 00061 NM 2002 12 11 02FDEA00871 1 20021122 A 5320 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON STR CLIP AT STA 660 STR 26R. 2 L 7 3 4F RT A3WE 2002121100062 20021211 00062 EU 2002 12 11 BAQA081575 1 20021204 A 2822 1176415103 PUMP BOLKMS BK117 BK117C1 5626025 EU FUEL BOOST INTERMITTENT H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 911TG 1177 7506 FUEL BOOST PUMP INTERMITTENT OPERATION. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U NC H13EU 2002121100063 20021211 00063 NM 2002 12 11 02FDEA00872 1 20021122 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON LONGITUDINAL FLOORBEAM BS 790 - 850, RBL 25, WL 208. 2 L 7 3 4F RT A3WE 2002121100064 20021211 00064 2002 12 11 BAQA081589 4 20021206 A 3422 5222644011 AMPLIFIER BEECH 100 100BEECH 1152916 CE SLAVING UNIT MALFUNCTIONED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 777GS 9926 B241 LOOSES SLAVE. SLOW TO ROTATE. REPLACED WITH SERVICEABLE UNIT. 1 L 7 2 3T A14CE 2002121100065 20021211 00065 EU 2002 12 11 IO5R081567 1 20021203 A 7120 L633M201101 MOUNT UROCOP EC135 EC135P1 8680990 EU ENGINE DEFECTIVE H IO5R A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 FS 01 552BA 554 190 Z-ARIS MOUNT WAS HITTING STOP IN-FLIGHT CAUSING VIBRATION IN CABIN IN EXCESS ON 1.4 IPS REMOVED AND REPLACED. 1 G 7 2 3U O H88EU 2002121100066 20021211 00066 GL 2002 12 11 LU42002F00000 3 20021119 A 6114 2AF34C55NO HUB BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO MCAULY 2AF34C 2AF34C55 GL PROP HUB CRACKED B LU4R K NONE L NO TEST IN INSP/MAINT 1 SO 17 555BG TC1269 711618 HUB WITH RELEVENT CRACK INDICATION. 1 L 7 2 3O 3 O RT 3A16 3E1 5 C P5EA 2002121100067 20021211 00067 GL 2002 12 11 LU42002F00001 3 20021119 A 6114 HUB BEECH 95 95B55 1152729 CE MCAULY 2AF34C 2AF34C55 GL PROPELLER CLOSED B LU4R K NONE L NO TEST IN INSP/MAINT 1 SO 17 555BG 711766 HUB HAS A RELEVENT CRACK INDICATION. 1 L 7 2 3O RT 3A16 5 C P5EA 2002121100068 20021211 00068 GL 2002 12 11 LU42002F00002 3 20021119 A 6114 C3112 NUT BEECH 95 95B55 1152729 CE MCAULY 2AF34C 2AF34C55 GL HUB CRACKED B LU4R K NONE L NO TEST IN INSP/MAINT 1 SO 17 555BG TC1269 711618 LOCK NUT CRACKED, REMOVED FROM CRACKED HUB. 1 L 7 2 3O RT 3A16 5 C P5EA 2002121100069 20021211 00069 GL 2002 12 11 LU42002F00003 3 20021119 A 6114 D3A32C90MN HUB CESSNA 188 A188B 2073005 CE CONT O520 IO520* 17032 SO MCAULY 3A32C D3A32C90 GL PROPELLER CRACKED B LU4R K NONE O OTHER IN INSP/MAINT 1 SO 17 4904R 18802422T 771300 HUB HAS A RELEVENT CRACK INDICATION. 1 L 7 1 3O 3 O A9CE E5CE 5 C P21EA 2002121100070 20021211 00070 SW 2002 12 11 MV52002F00005 1 20021008 A 5720 26002633 BRACKET GULSTM 690TP 695B 3970610 SW GARRTT TPE331 TPE331* 01514 WP LT WING CRACKED B MV5R K NONE O OTHER IN INSP/MAINT 1 GL 11 2VA 4332 96062 LT WING OUTBOARD FLAP INBOARD ATTACHMENT TO THE WING HAD A CRACK IN THE BRACKET ON THE WING LOWER AFT BOLT. CRACK WAS O NE INCH LONG IN A FORWARD AND AFT DIRECTION. 1 H 7 2 4T 3 T RT 2A4 E2WE 2002121100071 20021211 00071 WP 2002 12 11 MV52002F00006 2 20020919 A 7210 8961735K MOUNT GULSTM 690TP 695A 7630519 SW GARRTT TPE331 TPE33110 01514 WP G/B OIL JET CRACKED A MV5R K NONE O OTHER IN INSP/MAINT 1 GL 11 707TS 3153 96038 P38254 OIL JET UTILIZED TO LUBRICATE THE BULL GEAR LOCATED WITHIN THE GEARBOX WAS CRACKED AT THE MOUNTING BASE. THIS CONDITION COULD CAUSE A REDUCED AMOUNT OF OIL FOR LUBRICATION TO THE BULL GEAR. 1 H 7 2 4T 4 T 2A4 E4WE 2002121100072 20021211 00072 CE 2002 12 11 QC42002F00000 1 20021104 A 5280 BRACKET BEECH 58 58 1152740 CE CONT O550 IO550* SO MLG DOOR HINGE CRACKED B QC4R K NONE O OTHER IN INSP/MAINT 1 SO 01 220SA 309 TH2003 FOUND CRACKED BRACKETS IN THE AFT HINGE OF THE INBOARD MAIN GEAR DOOR. RIGHT SIDE, AFT HINGE, FORWARD BRACKET: CRACKED. LEFT SIDE, AFT HINGE, AFT BRACKET: CRACKED. BOTH BRACKETS CRACKED IN THE TRANSITION FROM THE .5 INCH FLANGE TO THE WI DE FLANGE THAT ATTACHES TO THE GEAR DOOR HINGE BRACKET. TRANSITION CORNER IS TOO SHARP, METAL GAUGE IS THIN. 1 L 7 2 3O 3 O 3A16 E3SO 2002121100073 20021211 00073 SW 2002 12 11 QC42002F00001 1 20021126 A 8010 HOUSING GULSTM 112 114 7630314 SW LYC O540 IO540T4B5 41532 EA STARTER CRACKED B QC4R K NONE O OTHER IN INSP/MAINT 1 SO 01 526AW 101 14226 L1595648A THE BENDIX DRIVE HOUSING CRACKED COMPLETELY THROUGH AND THE FORWARD BEARING SECTION FELL OFF THE AIRCRAFT. IAW LOG BOOK S, THIS STARTER HAS BEEN OVERHAULED TWICE WITHIN 240 HOURS OF OPERATION. THE LOGS DO NOT STATE THE REASON FOR THE OVERH AULS. 1 L 7 1 3O 3 O A12SO 1E4 2002121100074 20021211 00074 CE 2002 12 11 TIM2002F00015 1 20020924 A 5740 5012009743 ATTACH FITTING BEECH 99 99A 1154003 CE PWA PT6 PT6* 52043 EA RT WING CRACKED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 326CA U135 CRACK FOUND IN RT WING ATTACH FITTING. (BATH TUB FITTINGS) LOCATION CENTER SECTION UPPER FORWARD ATTACH FITTING. RECU RRING INSPECTION INTERVAL (SUPER SPAR) 1000 HOURS OR 3 YEARS WHICHEVER OCCURS FIRST. (CONTROL NUMBER 004) 1 L 7 2 3T 3 T A14CE E2NE 2002121100075 20021211 00075 CE 2002 12 11 TIM2002F00016 1 20020924 A 5740 9041104 ATTACH FITTING BEECH 99 B99 1154004 CE PWA PT6 PT6A11 52043 NE RT WNG CRACKED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 950AA 32480 U159 CRACK FOUND IN RIGHT WING ATTACH FITTING. (BATH TUB FITTING) LOCATION CENTER SECTION UPPER FORWARD ATTACH FITTING. RE CURRING INSPECTION INTERVAL (STANDARD SPAR WITH STAP) 500 HOURS OR 1 YEARS WHICHEVER OCCURS FIRST. (CONTROL NUMBER 005) 1 L 7 2 3T 3 T A14CE E4EA 2002121100076 20021211 00076 EU 2002 12 11 VJ32002F00094 1 20021121 A 8011 ARMATURE GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA STARTER BURNED OUT B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 865AF 394 85005 L2826448A DURING GROUND START OF AIRCRAFT ENGINE WOULD NOT START. MAINTENANCE PERSONNEL INSPECTED AND FOUND STARTER HAD BECOME IN OPERATIVE. THE STARTER HAS AN ORDER OF BURNED OUT ARMATURE. NO RECOMMENDATION, PART SENT BACK FOR WARRANTY. 1 L 7 1 3O 3 O RT A49CE 1E4 2002121100077 20021211 00077 NM 2002 12 11 DL73K021245 1 20021026 A 2120 CLAMP BOEING 737 737247 138448D NM LT AIR CLEANER LOOSE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 376DL 23603 ON T/O ROLL RECEIVED A PACK TRIP OFF INDICATION. CONTINUED TAKEOFF. ONCE AIRBORNE PERFORMED PROCEDURE PER POM. WHEN T HE PACK WAS RESET THE PRESSURE PEGGED TO TOP OF SCALE. WING BODY OVERHEAT ILLUMINATED FOLLOWED BY A BLEED TRIP OFF INDI CATION. ALL INDICATIONS OCCURRED ON THE LEFT SIDE OF SYSTEM. OPENED NR 1 ENG COWLS AND LT PACK BAY DOOR. INSPECTED AI R DUCTS FROM ENG TO PACK BAY AND DUCTS IN PACK BAY. NO DEFECTS. FOUND AIR LEAKING FROM INBOARD CLAMP OF LT AIR CLEANER HOT AIR BLOWING DIRECTLY ON OVERHEAT LOOP. SECURED CLAMP NO LEAKS. PERFORMED T/O POWER CHECK FOR 3 MIN DUCT PRESS AND PACK OPERATION NORMAL. 2 L 7 2 4F A16WE 2002121100078 20021211 00078 EA 2002 12 11 COMA0260694 1 20021208 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA WING INSTALLED A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 936CA 4210 7043 FLIGHT 5675 FLAPS FAIL WARNING DURING APPROACH.COULD NOT DUPLICATE. REPLACED THE PDU FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 2002121100079 20021211 00079 EA 2002 12 11 COMA0260695 1 20021208 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 977CA 7157 FLIGHT 5963 EMERGENCY LIGHTS ARE INOP ROWS 1 THRU 5.SECURED LOOSE WIRING CONNECTOR. 2 L 7 2 4F RT A21EA 2002121100080 20021211 00080 EA 2002 12 11 COMA0260696 1 20021206 A 4910 APU CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 956CA 7105 FLIGHT 5169 FUEL FUMES IN FWD SECTION OF AIRCRAFT AFTER APU START.COULD NOT DUPLICATE, OPERATIONAL CHECK OF APU WAS NORM AL. 2 L 7 2 4F RT A21EA 2002121100081 20021211 00081 EA 2002 12 11 COMA0260697 1 20021209 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 01 936CA 7043 FLIGHT 5827 FLAPS FAILED DURING APPROACH.COULD NOT DUPLICATE. C/W SERVICE BULLETINS 27-114A & 27-120A WHICH INSTALLS NE W AND IMPROVED FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 2002121100082 20021211 00082 EA 2002 12 11 COMA0260698 1 20021207 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA D O RETURN TO BLOCK OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 983CA 7169 FLIGHT 5072 FLAPS FAILED AT 26 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002121100083 20021211 00083 EA 2002 12 11 COMA0260699 1 20021207 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CR CRUISE 1 SO 01 962CA 7123 FLIGHT 5349 R/H THRUST REVERSER UNLOCK CAUTION MESSAGE.SECURED THE T/R AND DEFERRED MAINTENANCE PER MEL. 2 L 7 2 4F RT A21EA 2002121100084 20021211 00084 EA 2002 12 11 COMA0260700 1 20021207 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SO 01 938CA 7046 FLIGHT 5227 FLAPS FAILED AT 30 DEGREES DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002121100085 20021211 00085 EA 2002 12 11 COMA0260701 1 20021206 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA L/H MALFUNCTIONED A COMA O OTHER S AFFECT SYSTEMS DE DESCENT 1 SO 01 936CA 5778 7043 FLIGHT 5862 FLAPS FAILED AT 34 DEGREES DURING APPROACH.REPLACED THE FLAP BPSU'S. 2 L 7 2 4F RT A21EA 2002121100086 20021211 00086 EU 2002 12 11 02FDEA00873 1 20021125 A 5753 A57960300003 SKIN AIRBUS 300 A300F4605R 3930327 EU T/E FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 678FE 792 RT WING CENTER FLAP LWR SKIN AREA AT TRACK 4 HAS 2 EA DENTS BETWEEN T/E RIBS 23 & 21A. REPAIRED LWR R/CENTER FLAP SKIN IAW FEDEX EA 6-5750-66761. CUT DAMAGED SKIN AT DENT NR 2 PER SRM. EDDY CURRENT INSP'D DENTS. FOUND NO CRACKS EXISTED. FLAP PEENED REWORKED AREA PER SRM. FILLED DENT NR 1. FABRICATED REPAIR DOUBLER IAW A300 SRM 57-50-00 FIG 205 & EXTEND ED DOUBLER TO ACCOM BOTH DENTS. INSTALLED REPAIR DOUBLER PER SRM 57-50-00 FIG 205. 2 L 7 2 4F RT A35EU 2002121100087 20021211 00087 NM 2002 12 11 02FDEA00875 1 20021126 A 5720 SUPPORT DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LT WING L/E WING SUPPORT FOUND CRACKED AT NR 16 SLAT TRACK. 2 L 7 3 4F RT A22WE 2002121100088 20021211 00088 NM 2002 12 11 02FDEA00876 1 20021126 A 5311 6515929 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FRAME DENTED IN TWO PLACES AT BS 520 BETWEEN STR 25L & 22L 2 L 7 3 4F RT A3WE 2002121100089 20021211 00089 NM 2002 12 11 02FDEA00877 1 20021126 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION BS 1050 RBL 35 WL 208 UNDERSIDE OF FLOORBEAM UPPER CHORD AROUND FASTENER HOLE. 2 L 7 3 4F RT A3WE 2002121900004 20021219 00004 NM 2002 12 19 02FDEA00878 1 20021126 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION BS 1030, RBL 35, WL 208 UNDERSIDE OF FLOORBEAM UPPER CHORD AROUND FASTENER HOLE, REPAIRED FLOORBEAM BS 1030 , RBL 35, WL 208 IAW SRM 53-10-8 FIG 8 2 L 7 3 4F RT A3WE 2002121900005 20021219 00005 NM 2002 12 19 02FDEA00879 1 20021126 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION AT BS 1070, BL 0, RBL 45, WL 200 ON THE UNDERSIDE OF THE FLOORBEAM. REPAIRED FLOORBEAM BS 1070, BL 0, RBL 45 , WL 200 IAW FEDEX EA. 7-5310-68121 2 L 7 3 4F RT A3WE 2002121900006 20021219 00006 NM 2002 12 19 02FDEA00880 1 20021126 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION AT BS 1070, BL 0, LBL 65, WL 200 ON THE BOTTOM OF THE FLOORBEAM. REPAIRED FLOORBEAM IAW EA 7-5310-68121 2 L 7 3 4F RT A3WE 2002121100090 20021211 00090 NM 2002 12 11 02FDEA00881 1 20021126 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON LWR CHORD OF BS 1130 FLOORBEAM LBL 65 - RBL 65 WL 200 AROUND NUT PLATE HOLES. 2 L 7 3 4F RT A3WE 2003021000148 20030210 00148 NE 2003 2 10 DHL2002803013 2 20021210 A 7310 WARNING LIGHT DOUG DC8 DC873 302199C WP GE CFM56 CFM562C1 13802 NE FUEL BYPASS FALSE INDICATION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 803DH 46123 693482 NR 3 FUEL BYPASS LIGHT KEEPS ILLUMINATING IN FLIGHT. RESETS OK, BUT RE-ILLUMINATES WITHIN ONE MINUTE. DEFERRED NR 3 FU EL BYPASS LIGHT PER MEL 73-2-2. REMOVED AND REPLACED NR 3 FUEL FILTER. NO CONTAMINATION PRESENT. DMI 11188 ASSIGNED. SPE CIAL PROCEDURE COMPLIED WITH LIGHT DEACTIVATED. 2 L 7 4 4F 4 F RT 4A25 E2GL 2002121100091 20021211 00091 EU 2002 12 11 02FDEA00882 1 20021127 A 7830 THRUST REVERSER AIRBUS 300 A300F4605R 3930327 EU NR 2 ENGINE MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 685FE 803 NR 2 REVERSER PRESSURIZED AT 60KTS ON TAKEOFF MSP. ACN RELEASED FOR SERVICE PER MEL/CDL. ENGINE NR 2 THRUST REVERSER I NOP. THRUST (1 OR 2) REVERSER DEACTIVATED IN FORWARD THRUST POSITION. 2 L 7 2 4F RT A35EU 2002121100092 20021211 00092 NM 2002 12 11 DHL2002747008 1 20021210 A 2697 TERMINAL BOEING 727 727224 1384076 NM A DHLA K O NONE OTHER O OTHER NR NOT REPORTED 1 SO 01 747DH 22253 1) ENGINE NO.1 DETECTOR CIRCUIT GROUND LIGHT ON CIRCUIT BREAKER PANEL P6-3 ILLUMINATED INTERMITTENTLY. FIRE DETECTION T ESTED OK.2) FOUND WIRE 458-20 PULLED OUT OF TERMINAL CONNECTOR. INSTALLED NEW TERMINAL CONNECTOR. OPS CHECKED SERVICEAB LE. 2 L 7 3 4F A3WE 2002121100093 20021211 00093 EU 2002 12 11 AWXA200201180 1 20021210 A 3350 ABS0374A24 CABLE AIRBUS 320 A320231 3930325 EU SEAT ROW 22 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 0 0 66 LAS - EEL - DURING INSPECTION BROKEN WIRES WERE FOUND ON THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 L/H. MAINTENANCE REPAIRED EMERGENCY ESCAPE PATH LIGHT WIRES AT SEAT ROW 22 L/H, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 2002121100094 20021211 00094 NM 2002 12 11 02FDEA00883 1 20021126 A 5311 6515931 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FWD CARGO BAY FRAME IS DENTED IN TWO PLACES AT BS 560 ABOVE STR 24L & 25L+3. 2 L 7 3 4F RT A3WE 2002121100095 20021211 00095 NM 2002 12 11 02FDEA00884 1 20021126 A 5311 6515932 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FWD CARGO BAY FRAME IS DENTED IN TWO PLACES AT BS 580 ABOVE STR 24L & 25L+3. 2 L 7 3 4F RT A3WE 2002121100096 20021211 00096 NM 2002 12 11 02FDEA00885 1 20021126 A 5311 6515933 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FWD CARGO BAY FRAME IS DENTED IN TWO PLACES AT BS 600 ABOVE STR 24L & 25L. 2 L 7 3 4F RT A3WE 2002121100097 20021211 00097 NM 2002 12 11 02FDEA00886 1 20021126 A 5311 6515936 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FWD CARGO BAY FRAME IS DENTED BS 660 STR 24L. 2 L 7 3 4F RT A3WE 2002121100098 20021211 00098 NM 2002 12 11 02FDEA00887 1 20021126 A 5311 6515957 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FWD CARGO BAY FRAME IS DENTED BS 680 BETWEEN STR 24L - 25L. 2 L 7 3 4F RT A3WE 2002121100099 20021211 00099 NM 2002 12 11 02FDEA00888 1 20021126 A 5311 6515938 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FWD CARGO BAY FRAME IS DENTED BS 700 BETWEEN STR 24L & 25L. 2 L 7 3 4F RT A3WE 2002121100100 20021211 00100 NM 2002 12 11 02FDEA00889 1 20021126 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION ON SHEAR TIE B/S 720 BETWEEN STR 25L & 24L. 2 L 7 3 4F RT A3WE 2002121900007 20021219 00007 NM 2002 12 19 02FDEA00890 1 20021126 A 5311 6515939 FRAME BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION IN FWD CARGO BAY ON FRAME BS 720 RBL 19. REPAIRED FRAME BS 720, RBL 19 IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2002121900009 20021219 00009 NM 2002 12 19 02FDEA00891 1 20021126 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION FWD CARGO BAY ON SHEAR TIE BS 720E BETWEEN STR 28 LT & 28 RT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 15 AND E A 7-5310-68106. 2 L 7 3 4F RT A3WE 2002121100101 20021211 00101 NM 2002 12 11 02FDEA00892 1 20021126 A 5311 6515939 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FRAME DAMAGED IN AFT BAY BS 1110 UNDER FLOOR TO SIDEWALL SUPPORT LBL 21. REPAIR PER 727 SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2002121100102 20021211 00102 NM 2002 12 11 02FDEA00893 1 20021126 A 5311 6515939 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FRAME DAMAGED IN AFT BAY BS 1130 UNDER FLOOR TO SIDEWALL SUPPORT LBL 21. REPAIRED IAW SRM 51-40-3 FIG 1 2 L 7 3 4F RT A3WE 2002121100103 20021211 00103 NM 2002 12 11 02FDEA00894 1 20021126 A 5311 6515939 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FRAME DAMAGED IN AFT BAY BS 1070 UNDER FLOOR TO SIDEWALL SUPPORT. 2 L 7 3 4F RT A3WE 2002121100104 20021211 00104 NM 2002 12 11 02FDEA00895 1 20021126 A 5311 6515939 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FRAME DAMAGED IN AFT BAY BS 1050 UNDER FLOOR TO SIDEWALL SUPPORT LBL 21. REPAIRED PER 727 SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2002121100105 20021211 00105 NM 2002 12 11 02FDEA00896 1 20021126 A 5311 6515939 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FRAME DAMAGED IN AFT BAY BS 1050 UNDER FLOOR TO SIDEWALL SUPPORT RBL 21. 2 L 7 3 4F RT A3WE 2002121100106 20021211 00106 NM 2002 12 11 02FDEA00897 1 20021126 A 5311 6515939 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FRAME DAMAGED IN AFT BAY BS 1070 UNDER FLOOR TO SIDEWALL SUPPORT RBL 21. 2 L 7 3 4F RT A3WE 2002121900010 20021219 00010 NM 2002 12 19 02FDEA00898 1 20021126 A 5315 FLOORBEAM BOEING 727 727200 138407E NM N/A CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION ON FLOORBEAM AT BS 1070, RBL 53, WL 208. REPAIRED FLOORBEAM IAW SRM. 2 L 7 3 4F RT A3WE 2002121100107 20021211 00107 NM 2002 12 11 02FDEA00899 1 20021126 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION ON TOP OF FLOORBEAM BS 560 BL 0 TO RBL 25, WL 208, LWR SURFACE OF UPPER FLANGE AT FASTENER HOLES. 2 L 7 3 4F RT A3WE 2002121100108 20021211 00108 NM 2002 12 11 02FDEA00900 1 20021126 A 5311 6515928 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FRAME DENTED IN NUMEROUS PLACES AT BS 500 BETWEEN STR 25L & 22L. 2 L 7 3 4F RT A3WE 2002121100109 20021211 00109 NM 2002 12 11 02FDEA00901 1 20021127 A 5230 SKIN BOEING 727 727200 138407E NM CARGO DOOR CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 NR 3 CARGO DOOR SKIN IS CHAFED AT DOOR HANDLE CUT OUT. 2 L 7 3 4F RT A3WE 2002121100110 20021211 00110 NM 2002 12 11 02FDEA00902 1 20021127 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION ON FLOORBEAM AT BS 1110, RBL 45 TO LBL 45, WL 208. REPAIRED B.S. 1110 FLOOR BEAM LBL 45 - RBL 45 IAW FED EX E .A. 7-5310-68117. 2 L 7 3 4F RT A3WE 2002121100111 20021211 00111 NM 2002 12 11 02FDEA00903 1 20021127 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION ON TOP OF FLOORBEAM AT FASTENER HOLES BS 312, LBL 2 TO LBL 50, WL 208. REMOVED AND REPLACED SEAT TRACK AND T- CHORD OF LONGITUDINAL BEAM B.S. 760-850, LBL 25, WL 208 IAW SRM 51-10-5, 51-30-2, 51-30-5, 51-30-8. 2 L 7 3 4F RT A3WE 2002121900011 20021219 00011 NM 2002 12 19 02FDEA00904 1 20021127 A 5754 2850506 SUPPORT DOUG MD11 MD11 3023602 NM SLAT TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RT WING LE SUPPORT LOCATED ON NR 16 SLAT TRACK AT XOS 1005.124. FOUND WITH CRACK APPROX. 1 INCH IN LENGTH. CRACKED SUP PORT RIB ON RT WING LE LOCATED ON NR 16 SLAT TRACK AT XOS 1005.124 REMOVED AND REPLACED AS PER SRM 51-31-01, VOL. II. 2 L 7 3 4F RT A22WE 2002121100112 20021211 00112 NM 2002 12 11 02FDEA00905 1 20021120 A 5534 FITTING BOEING 727 727200 138407E NM VERTICAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 FRETTING CORROSION UPPER SURFACE OF LUG FOR AFT VERT BOLTS OF TENSION TIE COMMON TO VERT STAB. 2 L 7 3 4F RT A3WE 2002121100113 20021211 00113 NM 2002 12 11 02FDEA00906 1 20021126 A 5534 STRUCTURE BOEING 727 727200 138407E NM VERTICAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION IN FWD TWO VERTICAL BOLT HOLES FOR TENSION TIE COMMON TO VERT STAB. R&R VERTICAL BOLT HOLES PER ER 02-1753. 2 L 7 3 4F RT A3WE 2002121100114 20021211 00114 NM 2002 12 11 02FDEA00854 1 20021112 A 5310 SHEAR TIE BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION AT BS 950E+4 BETWEEN STR 28 & 29R. REPAIRED SHEAR TIE IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121100115 20021211 00115 NM 2002 12 11 02FDEA00855 1 20021107 A 5311 FRAME BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON LOWER FRAME BS 700, STR 28-27R. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED SHEAR TIE, FABRICATED REPA IR PARTS AND INSTALLED IAW SRM AND EA. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121100116 20021211 00116 NM 2002 12 11 02FDEA00856 1 20021112 A 5311 FRAME BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON FRAME AFT SIDE OF SHEAR TIE AT BS 1030, WL 148, RBL 5. REPAIRED IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121100117 20021211 00117 NM 2002 12 11 02FDEA00857 1 20021110 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 328, LBL 3, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS CUT OUT DAMAGE AREA. FABRICATED REPAIR ANGLES, AND FILLERS, & INSTALLED IAW SRM 51-30-2, 51-30-5, 51-30-8. 2 L 7 3 4F RT A3WE 2002121100118 20021211 00118 NM 2002 12 11 02FDEA00858 1 20021114 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON LWR CHORD OF BS 970 FLOORBEAM AROUND NUTPLATE HOLE, RBL 22, WL 200. R&R FLOORBEAM PER SRM 53-10-1 & 53-10- 8 FIG 8. 2 L 7 3 4F RT A3WE 2002121100119 20021211 00119 NM 2002 12 11 02FDEA00859 1 20021114 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON LOWER CHORD OF BS 970 FLOORBEAM AROUND NUTPLATE HOLE, RBL 11, WL 200. R&R FLOORBEAM PER SRM 53-10-1 & 53-1 0-8 FIG 8. 2 L 7 3 4F RT A3WE 2002121100120 20021211 00120 NM 2002 12 11 02FDEA00860 1 20021112 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON SKIN AT BS 706, STR 26R FWD CARGO BAY. CORROSION WAS FOUND OUT OF LIMITS, FABRICATED REPAIR PARTS, REMOVED DAMAGE AREA INSTALLED REPAIR PARTS PER SRM 53-30-3 FIG 5. 2 L 7 3 4F RT A3WE 2002121100121 20021211 00121 NM 2002 12 11 02FDEA00863 1 20021112 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 CORROSION ON STRINGERS AT BS 685, STR 26-28R. REPAIRED STA 26R AT BS 686 PER SRM 53-10-3, 51-10-2 CORROSION WAS FOUND O UT OF LIMITS PER SRM 53-10-2, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 2002121100122 20021211 00122 NM 2002 12 11 02FDEA00864 1 20021118 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 EXTERNAL SKIN GOUGED AT BS 1035 BETWEEN STR 22L & 21L. BLENDED GOUGE ON SKIN, FOUND TO BE OUT OF LIMITS PER SRM 53-30-4 FIG 2. CUT OUT DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS AND APPLIED FINISH PER SRM 53-30-3 FIG 1. 2 L 7 3 4F RT A3WE 2002121100123 20021211 00123 NM 2002 12 11 2002F01079 1 20021203 A 3350 CONNECTOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE CABIN LOOSE G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 519AT 27975 DURING SCHEDULED MAINTENANCE ROW 27 THROUGH 28 FLOOR LIGHTING INOPERATIVE. MAINTENANCE RECONNECTED LOOSE CONNECTION IAW MM. 2 L 7 2 4F 4 F RT A2NM A12EU 2002121100124 20021211 00124 NM 2002 12 11 2002F01081 1 20021002 A 5315 FLOORBEAM BOEING 757 75723N 1384973 NM FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 518AT 27974 DURING SCHEDULED INSPECTION, LEVEL 2 CORROSION DISCOVERED ON MAIN CABIN FLOORBEAM UPPER CHORD NEAR R1 DOOR. FUSELAGE ST ATION 365, WL 208, RBL 48. MAINTENANCE REPAIRED FLOORBEAM UPPER CHORD IAW SRM. 2 L 7 2 4F RT A2NM 2002121100125 20021211 00125 WP 2002 12 11 AALA20021426 1 20021004 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 477AA 49652 TUL - FOUND FUSELAGE SKIN CRACKED AROUND RIVET ABOVE LEFT ENGINE PYLON, STATION 1380, LONGERON 12L. STOP DRILLED CRACK. INSTALLED DOUBLER REPAIR PER SRM 53-01-00 PAGE 9, FIG 2 SHEET 3. (M) 2 L 7 2 4F A6WE 2002121100126 20021211 00126 NM 2002 12 11 DHL2002750007 1 20021210 A 7100 CONTROL ROD BOEING 727 7272M7 138407S NM A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 1) AT FL 330 ENGINE #3 THRUST LEVER WILL NOT ADVANCE PAST 81% N1.2) FOUND #3 ENGINE THROTTLE CONTROL ROD END BOLT TOO LONG AND CHAFING AGAINST FUEL ROD BOLT. REMOVED AND REPLACED CONTROL ROD BOLT. RAN #3 ENGINE, CHECKED TRIM. CHECKED GOOD IAW JRH 5.2 & 71-00. (NOTE: SDR #DHL2002750007 WAS ORIGINALLY FILED ON 12-10-2002 AS AN UPDATE TO SDR #DHL2002750001. O N 12-11-2002 SDR# DHL2002750001 WAS UPDATED TO CONTAIN ITS CORRECT DATA, AND SDR #DHL2002750007 WAS FILED AS IT WAS SUPP OSED TO BE ON 12-10-2002.) 2 L 7 3 4F A3WE 2002121100127 20021211 00127 WP 2002 12 11 AALA20021427 1 20021004 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 477AA 49652 TUL - FOUND SHEAR TIE STIFFENER CRACKED, AFT SIDE OF 1451 FRAME, AT LONGERON 2R. REMOVED CRACKED SHEAR TIE STIFFENER. INSTALLED NEW STIFFENER PER SRM 51-00-00. (M) 2 L 7 2 4F A6WE 2002121100128 20021211 00128 WP 2002 12 11 AALA20021438 1 20021008 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 219AA 49171 TUL - FOUND FUSELAGE SKIN CRACKED STATION 1380 ABOVE LONGERON 14R. INSTALLED DOUBLER PER SRM 53-01 AND AARD 53-30-00-02 REVISION 8/30/02. (M) 2 L 7 2 4F A6WE 2002121100129 20021211 00129 WP 2002 12 11 AALA20021511 1 20021021 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 295AA 49307 TUL - FOUND FUSELAGE SKIN IS CRACKED, 3 PLACES, AT STATION 1380, L12R. INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3. (M) 2 L 7 2 4F A6WE 2002121100130 20021211 00130 WP 2002 12 11 AALA20021512 1 20021016 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 493AA 49731 TUL - FOUND FUSELAGE SKIN CRACKED AT STATION 1380 BELOW L12R JUST ABOVE SKIN LAP, CRACKED .25 INCH IN 3 PLACES. STOP DR ILLED CRACKS AND STOP DRILLED. INSTALLED DOUBLER PER SRM 53-01 FIG 2, SHEET 3. (M) 2 L 7 2 4F A6WE 2002121100131 20021211 00131 WP 2002 12 11 AALA20021518 1 20021008 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 445AA 49471 TUL - FOUND DEN AND GOUGES ON LEFT OF AIRCRAFT APPROXIMATELY 12 INCHES BELOW CABIN NEG PRESS PORTS AND STATIC PORTS. DA MAGED AREA CUT OUT, REPAIR DOUBLER INSTALLED PER SRM 53-04. (M) 2 L 7 2 4F A6WE 2002121100132 20021211 00132 WP 2002 12 11 AALA20021519 1 20021008 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 445AA 49471 TUL - FOUND LONGERON 2R CRACKED AFT SIDE AT FRAME 1418. REMOVED DAMAGED SECTION OF STRINGER SPLICED REPAIR SECTION PER AARD 53-30-00-2. (M) 2 L 7 2 4F A6WE 2002121100133 20021211 00133 WP 2002 12 11 AALA20021548 1 20021124 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AA 49293 TUL - FOUND FUSELAGE SKIN CRACKED AT FASTENER HOLE. REPAIR DOUBLER INSTALLED PER SRM 53-01-00 AND AARD 53-30-00-02. (M ) 2 L 7 2 4F A6WE 2002121100134 20021211 00134 WP 2002 12 11 AALA20021549 1 20021024 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AA 49293 TUL - FOUND SHEAR TIE CRACKED, FS 1380. INSTALLED DOUBLER PER AARD 53-10-00-20. (M) 2 L 7 2 4F A6WE 2002121100135 20021211 00135 WP 2002 12 11 AALA20021558 1 20021025 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 TUL - FOUND CANTED FRAME WEB CRACKED. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-32. (M) 2 L 7 2 4F RT A6WE 2002121100136 20021211 00136 WP 2002 12 11 AALA20021559 1 20021029 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 293AA 49305 TUL - FOUND FUSELAGE SKIN HAS .75 INCH CRACK AT STATION 1380, L13R. EXTERNAL DOUBLER APPLIED AFTER CRACK HAD BEEN STOP DRILLED PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002121100137 20021211 00137 WP 2002 12 11 AALA20021561 1 20021028 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 487AA 49680 TUL - FOUND FRAME WITH .25 INCH CRACK ON LEFT, CANT FRAME 1474 6 INCHES FORWARD OF LOUVER BOX DRAIN TUBE FITTING ON FUSE LAGE. STOP DRILLED CRACK, MFG AND INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG NR 2. (M) 2 L 7 2 4F A6WE 2002121100138 20021211 00138 WP 2002 12 11 AALA20021562 1 20021028 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 487AA 49680 TUL - FOUND SKIN CRACK AT COUNTERSINK RIVET 6 INCHES ABOVE LEFT PYLON. REPAIRED PER SRM 53-01-00 AND AARD 53-30-00-02. (M) 2 L 7 2 4F A6WE 2002121100139 20021211 00139 WP 2002 12 11 AALA20021585 1 20021024 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 597AA 53287 TUL - FOUND LIGHT CORROSION IN SPOTS ALONG AFT CARGO DOOR BEAM. INSTALLED DOUBLER ON AFT CARGO LOWER DOOR JAMB PER AARD 53-10-3. (M) 2 L 7 2 4F RT A6WE 2002121100140 20021211 00140 WP 2002 12 11 AALA20021586 1 20021023 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 597AA 53287 TUL - NR 1 SEAT TRACK CORRODED AT STATION 1208, 1235, AND 1259, STATION 1235 CORROSION FOUND TO BE OUT OF LIMITS. REMOV ED AND REPLACED ENTIRE SECTION OF NR 1 SEAT TRACK WITH NEW TRACK FROM STATION 1168 TO STATION 1309 PER SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2002121100141 20021211 00141 WP 2002 12 11 AALA20021587 1 20021021 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 597AA 53287 TUL - FOUND DEEP CORROSION PITTING STATION 1312-1320 SEAT TRACK NR 3. INSTALLED NEW SEAT TRACK PER SRM 53-05-00. (M) 2 L 7 2 4F RT A6WE 2002121100142 20021211 00142 WP 2002 12 11 AALA20021588 1 20021022 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 597AA 53287 TUL - FOUND LEFT CUSP STATION 1229 HAS A HOLE NEXT TO SEAT TRACK. INSTALLED DOUBLER ON LEFT CUSP STATION 1229 PER SRM 5 3-01. (M) 2 L 7 2 4F RT A6WE 2002121100143 20021211 00143 WP 2002 12 11 AALA20021596 1 20021104 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 408AA 49319 TUL - FOUND LONGERON 20R CRACKED AT STATION 1000, APPROX, AT RIGHT FLAP ACTUATOR. INSTALLED DOUBLER REPAIR PER AARD 53- 10-00-18. (M) 2 L 7 2 4F A6WE 2002121100144 20021211 00144 WP 2002 12 11 AALA20021597 1 20021101 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 486AA 49679 TUL - FOUND FUSELAGE SKIN CRACKED. STOP DRILLED CRACK AT ENDS. INSTALLED DOUBLER PER SRM 53-01-00 AND 51-01-01. (M) 2 L 7 2 4F A6WE 2002121100145 20021211 00145 WP 2002 12 11 AALA20021598 1 20021101 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 486AA 49679 TUL - FOUND CORROSION ON CUSP LOWER SURFACE, LEFT SIDE STATION 622. FABRICATED AND INSTALLED DOUBLER REPAIR TO CUSP PER SRM 53-01-06. (M) 2 L 7 2 4F A6WE 2002121100146 20021211 00146 WP 2002 12 11 AALA20021607 1 20020821 A 5730 SKIN DOUG DC9 DC982 3022082 WP LT WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 420AA 49332 TUL - FOUND 5 INCH CRACK IN LEFT WING LOWER FIXED LEADING EDGE AT WING STATION 214. STOP DRILLED CRACK, INSTALLED REPAI R DOUBLER/ AND STRAP AARD 80559, CHECK OK. (M) 2 L 7 2 4F A6WE 2002121100147 20021211 00147 NM 2002 12 11 UPS02239964 1 20021203 A 7830 SKIN BOEING 727 72730C 1384009 NM UPPER DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C ENGINE #1 THRUST REVERSER UPPER DOOR INNER SKIN CRACKED AT UPPER I/B CORNER OF LWR SKIN REPAIRED DAMAGED AREA IAW SRM 78-30-01 FIG 201 2 L 7 3 4F A3WE 2002121100148 20021211 00148 NM 2002 12 11 UPS02239965 1 20021129 A 7830 SKIN BOEING 727 72730C 1384009 NM UPPER DOOR I/B CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C ENG. #1 THRUST REVERSER, UPPER DOOR, INNER SKIN CRACKED AT I/B OF CE NTER OF LWR SKIN REPAIRED DAM AGED AREA IAW SRM 78-30-01 FIG 201 2 L 7 3 4F A3WE 2002121100149 20021211 00149 NM 2002 12 11 UPS02239970 1 20021206 A 5720 ANGLE BOEING 727 72730C 1384009 NM WS 383 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C SMALL AREA OF CORROSION NOTED IN R/H WING T/E STRUCTURE WS 383, ANGL E BETWEEN SUPPORT WEB & UPPER T/E SKIN REMOVED FASTNERS FROM CORRODED AREA AS PER SRM 51-30-02 & CUT AND TR IMMED ANGLE AS PER SRM 51-20-00. FABRICAT ED REPAIR PARTS IAW SRM 51- 40-04. FABRICATED PARTS INSTALLED IAW SRM 51-30-02 2 L 7 3 4F A3WE 2002121100150 20021211 00150 NM 2002 12 11 UPS02239972 1 20021122 A 2730 ELEVATOR BOEING 727 72730C 1384009 NM ELEV. STA 204 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C X-RAY INSPECTION SHOWS A CRACK INDICATION ON THE LEFT ELEVATOR AT EL EV STA. 204, APPROX 5" FWD OF THE TRAILING EDGE REPAIR CARRIED OUT IAW SRM 51-30-02, 55-20-3, 51-40-5 2 L 7 3 4F A3WE 2002121100151 20021211 00151 NM 2002 12 11 UPS02239973 1 20021202 A 5310 WEB BOEING 727 72730C 1384009 NM NOSE W/W R/H CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:C SUSPECT CRACKS IN NOSE WHEEL WELL R/H WEB, JUST BELOW FWD END OF AFT PRESSURE PANEL REPAIR CARRIE D OUT IAW SRM 51-40-2 & 51-30-2. REPAIR PARTS LEAK CEHC KED OK IAW MM 5-51-25 2 L 7 3 4F A3WE 2002121100152 20021211 00152 EA 2002 12 11 COMA0260702 1 20021206 A 2150 7536893 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA ACM DIRTY A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 708CA 7235 FLIGHT 5270 SMOKE TOILET WARNING - SMOKE SMELL IN CABIN AND COCKPIT.REPLACED THE ACM WATER COALESCER BAGS. 2 L 7 2 4F RT A21EA 2002121100153 20021211 00153 EA 2002 12 11 COMA0260703 1 20021209 A 3230 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA #3 MALFUNCTIONED A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 914CA 19384 7012 FLIGHT #6030 GEAR DISAGREE WARNING - MANUAL EXTENSION USED TO LOWER LANDING GEAR.REPLACED THE #3 HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A21EA 2002121100154 20021211 00154 EA 2002 12 11 COMA0260705 1 20021210 A 2760 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA D RETURN TO BLOCK J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 938CA 7046 FLGIHT 5085 SPOILERS FAULT MESSAGE DURING TAXI.RESET THE SECU CIRCUIT BREAKERS - SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 2003062500068 20030625 00068 NE 2003 6 25 YENA200232 2 20021210 A 7530 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE VSV ACTUATOR DIRTY A YENA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 507JB 1240 V10739 RTO AT CLOSE TO 80KTS -ECAM MESSAGE OF ENG 1 COMPRESSOR VANE. CFDS MESSAGE BOTH CHANNELS CH A/B VSV/HC/EEC1. T/S PER C AATS TASK 75-30-00-810-852. EXAMINED AND CLEANED CONNECTORS ON VSV ACTUATOR PER STEP 1 OF TASK & LUBED VSV UNISON RING PER AMM TASK. POWER ASSURANCE RUN WAS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2003022000117 20030220 00117 CE 2003 2 20 AMW3 1 20021127 A 5320 1295140411 INTERCOSTAL BEECH 1900 1900D 1154162 CE FUSELAGE FAILED A AMWA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 07 146ZV UE146 AFTER TAKE OFF THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR NR 2 ENGI NE START. TAKE OFF ROLL WAS NORMAL. JUST AFTER ROTATION, A STRONG VIBRATION BEGAN. THE LANDING GEAR RETRACTED AND THE EN GINE INSTRUMENTS WERE NORMAL. THE AIRCRAFT WAS THEN RETURNED TO FIELD AND THE CARGO DOOR WAS FOUND OPEN. HOWEVER THE CAR GO DOOR ANNUNCIATOR FAILED TO ILLUMINATE. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPLACED 3 CRACKED INTE RCOSTALS, DORSAL FIN AND 2 SHOCKS. THEY ALSO RIG CHECKED THE DOOR. NO TEARDOWN REPORT WILL BE REQUIRED. 2 L 7 2 4T RT A24CE 2002121100155 20021211 00155 CE 2002 12 11 AMW4 1 20021127 A 5230 12944004475 INTERCOSTAL BEECH 1900 1900D 1154162 CE CRACKED A AMWA D RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 CE 07 146ZV UE146 AFTER TAKE OFF FROM HOT SPRINGS ARKANSAS, THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS E XTINGUISHED PRIOR TO #2 ENGINE START. TAKE OFF ROLL WAS NORMAL. JUST AFTER ROTATION, A STRONG VIBRATION BEGAN. THE LANDI NG GEAR RETRACTED AND THE ENGINE INSTRUMENTS WERE NORMAL. THE AIRCRAFT WAS THEN RETURNED TO FIELD AND THE CARGO DOOR WAS FOUND OPEN. HOWEVER THE CARGO DOOR ANNUNCIATOR LIGHT FAILED TO ILLUMINATE. THE CORRECTIVE ACTION WAS THAT MAINTENANCE R EMOVED AND REPLACED 3 CRACKED INTERCOSTALS, DORSEL FIN AND 2 SHOCKS. THEY ALSO RIG CHECKED THE DOOR. NO TEARDOWN REPORT WILL BE REQUIRED. REFER TO CONTROL #045447. 2 L 7 2 4T RT A24CE 2002121200007 20021212 00007 NM 2002 12 12 DY12002F00000 1 20021106 A 3233 980044503 ROD END PIPER PA60 PA60601P 7106012 NM LYC O540 IO540* 41532 EA MLG ACTUATOR BROKEN B DY1R O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 13 86AT 61P0364114 AFTER AIRCRAFT MADE AN UNEVENTFUL LANDING PILOT NOTICED THAT LEFT GEAR DOWN LIGHT WAS BLINKING ON AND OFF WITH SUBSEQUEN T ACTIVATION OF GEAR WARNING HORN WHEN LIGHT WAS OFF. AC TAXIED TO HANGER WITHOUT INCIDENT. EXAMINATION OF LEFT GEAR R EVEALED THAT THE GEAR ACTUATOR ROD END HAD BROKEN, ALLOWING ENOUGH PLAY IN GEAR OVER CENTER BRACES TO CAUSE INTERMITTENT GEAR DOWN LIGHT. REPLACED ROD END AND CHECKED GEAR RIGGING WITH NO PROBLEMS FOUND. BROKEN ROD END HAD NO SIGNS OF COR ROSIONS OR PREVIOUS CRACKING. EVALUATION OF ROD ENDS TO DETERMINE IF THEY ARE STRONG ENOUGH FOR THIS APPLICATION. 1 M 7 2 3O 3 O RT A17WE 1E4 2002121200008 20021212 00008 CE 2002 12 12 FPI2002F00014 1 20021113 A 8011 643109 CLUTCH SPRING CESSNA 210 210L 2073448 CE CONT O520 IO520L 17032 SO STARTER FRACTURED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 14 59130 6 21060110 STARTER ADAPTER CLUTCH SPRING FAILED AT 6.7 HOURS IN SERVICE. SPRING FAILURE WILL NOT ALLOW FOR AN ENGINE START. SUGGE ST THAT SPRING WAS FATIGUED AND BROKEN UNDER STRESS OF TURNING ENGINE. 1 H 7 1 3O 3 O 3A21 E5CE 2002121200009 20021212 00009 CE 2002 12 12 H3A2002F00000 1 20020826 A 7500 9691911 DUCT BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO THROTTLE BODY SEPARATED E H3AA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SO 11 58CK TH567 UNSCHEDULED LANDING WAS MADE DUE TO RIGHT ENGINE SURGING. EXAMINATION OF ENGINE REVEALED A 1 X 2 INCH SECTION OF DUCT W AS MISSING BETWEEN THE AIR BOX AND THROTTLE BODY. PART OF DUCT SEPARATED AND WENT THROUGH INDUCTION SYSTEM AND CYLINDER CAUSING TEMPORARY SURGING. REPLACED DUCT ON BOTH ENGINES. ENGINE RUN UP WAS NORMAL. 1 L 7 2 3O 3 O 3A16 E5CE 2002121200010 20021212 00010 CE 2002 12 12 QC42002F00003 1 20021106 A 2110 585550111 BRACKET BEECH 58 58 1152740 CE CONT O550 IO550* SO AC COMPRESSOR BROKEN B QC4R K NONE O OTHER IN INSP/MAINT 1 SO 01 220SA TH2003 DURING INSPECTION, FOUND A MOUNTING LOBE COMPLETELY BROKEN OFF THE BRACKET THAT HOLDS THE AIR CONDITIONER COMPRESSOR ON THE FRONT OF THE LEFT ENGINE. THIS BRACKET IS ATTACHED TO THE ENGINE CASE WITH 4 BOLTS. WHILE INSTALLING THE NEW BRACK ET, IT REQUIRED INSTALLING SHIMS UNDER SOME OF THE MOUNTING LOBES TO AVOID A PRELOAD CONDITION AFTER THE BOLTS ARE TORQU ED. BRACKET WAS NOT SHIMMED CORRECTLY AT THE FACTORY AND THE BRACKET HAD A LARGE PRELOAD STRESS ON THE LOBES. 1 L 7 2 3O 3 O 3A16 E3SO 2002121200011 20021212 00011 EA 2002 12 12 UWW2002F00000 2 20021125 A 8530 LW11167 EXHAUST VALVE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540A2C 41532 EA NR 1 CYLINDER FAILED E UWWA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 19 63705 117 317712033 L446061A DURING NORMAL CRUISE FLIGHT, EXHAUST VALVE STEM BROKE ON NR 1 CYLINDER CAUSING PARTIAL LOSS AND METAL CONTAMINATION THRO UGH OUT THE ENGINE. 1 L 7 2 3O 3 O A20SO E14EA 2002121200012 20021212 00012 EA 2002 12 12 UWW2002F00001 2 20021125 A 8530 LW13622 INTAKE VALVE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540A2C 41532 EA NR 3 CYLINDER BROKEN E UWWA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 19 63705 317712033 L446061A DURING NORMAL CRUISE FLIGHT, INTAKE VALVE STEM BROKE ON NR 3 CYLINDER CAUSING PARTIAL POWER LOSS AND METAL CONTAMINATION THROUGHOUT ENGINE. 1 L 7 2 3O 3 O A20SO E14EA 2002121200013 20021212 00013 NM 2002 12 12 ZW0A0211821 1 20021120 A 3350 BATTERY BOEING 757 7572Q8 1384972 NM CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 703TW 27620 SECTION OF EGRESS LIGHTING INOPERATIVE, REPLACED BATTERY AND POWER SUPPLY UNIT. LAST CHECK C PERFORMED MCI 10/12/2002 2 L 7 2 4F RT A2NM 2002121200014 20021212 00014 WP 2002 12 12 ZW0A021192 1 20021119 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 939AS 49657 FLOOR TIE BETWEEN STRINGERS 28 AND 27 RT AND FROM STA 1003 TO 1079 IN AFT AUX FUEL TANK CAVITY HAS CORROSION. INSTALLED NEW TRACK FROM STA 1022 TO STA 1079. LAST CHECK C PERFORMED IN STL 01/07/02 --CLOSED-- 2 L 7 2 4F RT A6WE 2002121200015 20021212 00015 WP 2002 12 12 ZW0A021193 1 20021121 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 939AS 49657 FLOOR TIE DOWN TRACK BETWEEN STRINGERS 27 AND 28 LT AND STA 1003 AND 1079 IN AFT AUX FUEL TANK HAS CORROSION. REPLACED T RACK SPLICE AND TRACK I.A.W. SRM 53-05-10R. LAST CHECK C PERFORMED IN STL 01/07/02 --CLOSED-- 2 L 7 2 4F RT A6WE 2002121200016 20021212 00016 WP 2002 12 12 ZW0A021194 1 20021122 A 5510 BRACKET DOUG DC9 DC983 3022083 WP HORIZONTAL STAB CRACKED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 939AS 49657 BRACKET CRACKED INSIDE HORIZONTAL STABILIZER AT STA 1429 AND RBL 6. REPLACED ANGLE PER SPM 6-70-01 AND DOUGLAS DRAWING 5 912188. LAST CHECK C PERFORMED IN STL 01/07/02 --CLOSED-- 2 L 7 2 4F RT A6WE 2002121200017 20021212 00017 WP 2002 12 12 ZW0A021195 1 20021120 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 939AS 49657 FLOOR SUPPORTS BETWEEN STA 160 AND STA 200 FOUND WITH SURFACE CORROSION. FABRICATED NEW SUPPORTS AND INSTALLED PER SRM 5 1-03-02. LAST CHECK C PERFORMED IN STL 01/07/02 --CLOSED-- 2 L 7 2 4F RT A6WE 2002121200018 20021212 00018 WP 2002 12 12 ZW0A021196 1 20021126 A 4990 OIL SYSTEM DOUG DC9 DC982 3022082 WP APU LEAKING A ZW0A D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 13 950U 49230 OIL LEAKING IN APU CAUSING SMOKE TO ENTER CABIN. REMOVED AND REPLACED LEFT AUTO TEMP CONTROL ANTICIPATOR. LAST CHECK C P ERFORMED IN STL 10/29/02 --CLOSED-- 2 L 7 2 4F A6WE 2002121200019 20021212 00019 NM 2002 12 12 ZW0A0212001 1 20021201 A 3397 58541 WIRE BOEING 747 747230B 1384889 NM EMERGENCY LIGHTS CUT A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 719TW 28487 THE CABIN EGRESS LIGHTS FLASHED ON AND OFF IN "C" ZONE. REPLACED THE FEEDER CABLE, WHICH WAS CUT IN SEVERAL PLACES. CHE CK-C 7-7-02 MCI. --CLOSED-- 2 L 7 4 4F A20WE 2002121200020 20021212 00020 WP 2002 12 12 ZW0A0212003 1 20021127 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9405T 53141 THE EMERGENCY CEILING LIGHTS IN FIRST CLASS, ROW 17 THRU 31, AND AT THE OVERWING EXITS, AND THE INTERIOR EMERGENCY OVERW ING EXIT LIGHTS FWD AND AFT, WERE ALL INOPERATIVE. REPLACED THE POWER SUPPLY BATTERIES AT EACH OF THE LOCATIONS. CHECK- C 10-19-02 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2002121200021 20021212 00021 NE 2002 12 12 AT0200088 2 20021130 A 7320 8061965 FMU BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE RT ENGINE INOPERATIVE A ZZDA E C ENGINE SHUTDOWN ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 15 947AT 55010 RT ENGINE SYSTEM FAIL, LOW RPM, SHUT DOWN. REMOVED AND REPLACED RT FMC AND RT EEC IN ACCORDANCE WITH AIRCRAFT MAINTE NANCE MANUAL 73-23 AND 73-21. PERFORMED HIGH POWER RUN, OPS CHECK GOOD. 2 L 7 2 4F 4 F TR A6WE E00061EN 2002121200022 20021212 00022 SW 2002 12 12 N1078C111702 1 20021117 A 7930 WARNING LIGHT BELL 206 206L1 1182107 SW ALLSN 250C 250C28 03013 GL ENGINE ILLUMINATED E YTRA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 1078C 45392 CAE860112 ENGINE CHIP LIGHT CAME-ON IN CRUISE FLIGHT. 1 G 7 1 3U 3 U H2SW E1GL 2002121200023 20021212 00023 SW 2002 12 12 N37AJ102302 1 20021023 A 2910 70010H000A15A LINE BELL 206 206B 1181511 SW HYD SYSTEM DETERIORATED I YTRA O OTHER K F FLUID LOSS FLT CONT AFFECTED CR CRUISE 1 SW 03 37AJ 1877 IN CRUISE FLIGHT NOTICED STIFFNESS IN FLIGHT CONTROLS. 1 G 7 1 3U H2SW 2002121200024 20021212 00024 NM 2002 12 12 XNOA01088 1 20021121 A 2751 TOGGLE BOEING 727 727227 1384078 NM LE FLAPS DAMAGED A XN0A O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 23 793A 20774 AFTER T/O, ON FLAP RETRACTION, OUTBOARD FLAPS JAMMED BETWEEN 2 DEGREES AND 5 DEGREES.ACTION TAKEN: INSPECTED OUTBOARD FL APS SYSTEM IAW B727 MM 27-51-00. FOUND LT OUTBOARD FLAP AT FAULT. FURTHER INSPECTION FOUND LT INBOARD FLAP, INBOARD & OU TBOARD, FORE FLAP SEQUENCING CARRIAGES TOGGLES DAMAGED. REMOVED & REPLACED INBOARD & OUTBOARD TOGGLES IAW B727 MM 27-57- 14. PERFORMED OPERATIONAL TEST OF INBOARD & OUTBOARD FLAP SYSTEMS IAW B727 MM 27-51-00. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2002121200025 20021212 00025 NM 2002 12 12 XNOA01089 1 20021123 A 5610 WINDOW BOEING 727 727227 1384078 NM COCKPIT CRACKED A XN0A A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 76753 21249 AFTER T/O R-1 WINDOW PANE CRACKED. REMOVED & REPLACED R-1 WINDSHIELD AS REQ IAW B727 ENA MM REF 56-11-11. NO OTHER DEFEC TS NOTED AT THIS TIME. 2 L 7 3 4F A3WE 2002121200026 20021212 00026 EU 2002 12 12 XNOA01090 1 20021126 A 2780 SLAT AIRBUS 300 A300B4203 3930306 EU WINGS FAILED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 224KW 073 SLATS WOULD NOT EXTEND ON TAXI OUT. 2 L 7 2 4F RT A35EU 2002121200027 20021212 00027 NM 2002 12 12 XNOA01091 1 20021127 A 2913 PUMP BOEING 727 727227 1384078 NM HYD SYSTEM FAILED A XN0A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 793A 20774 AFTER T/O COMPLETE LOSS OF SYS "A" HYDRAULICS. MEMORY ITEM & EMERGENCY ABNORMAL CHECKLISTS PERFORMED. FOUND NR 2 ENGINE DRIVEN PUMP LEAKING FROM FLANGE BOLTS. REMOVED & REPLACED PUMP AS PER MM 29-11-31. 2 L 7 3 4F A3WE 2002121200028 20021212 00028 EU 2002 12 12 XNOA01092 1 20021203 A 2710 REGULATOR AIRBUS 300 A300B4203 3930306 EU CABLE TENSION FAILED A XN0A D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 472AS 125 DURING FLIGHT CONTROL CHECK AILERONS CONTROL VERY HEAVY. WILL NOT RETURN TO NEUTRAL. REMOVED & REPLACED LT CONTROL CABL E TENSION REGULATOR ASSY IAW A300 MM 27-11-17. PERFORMED OPERATIONAL AND FUNCTIONAL INSPECTION. 2 L 7 2 4F RT A35EU 2002121200029 20021212 00029 EU 2002 12 12 XNOA01093 1 20021205 A 3251 VALVE AIRBUS 300 A300B4203 3930306 EU NLG STEERING FAILED A XN0A D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 224KW 073 NOSE WHEEL STEERING BINDING WITH VERY LITTLE CONTROL. RUDDER STEERING SEEMED INEFFECTIVE. RETURNED TO BLOCKS. BLEED GRE EN & YELLOW STEERING VALVES IAW A300 MM CHAPT 32-51-00. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2002121200030 20021212 00030 EU 2002 12 12 VYGA20020002 1 20020708 A 2197 MS3106A16SL3S CONNECTOR BAG JETSTM JETSTM3201 1500217 EU AIR DISTRIBUTION DAMAGED E VYGA H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 15 3108 824 AIR DUCT OFF CIRCUIT BREAKER POPPED. TROUBLE SHOOTING REVEALED THAT CONNECTOR WITH WIRING REMOVED MEASURED 20 OHMS RESIS TANCE BETWEEN PINS. CLOSER EXAMINATION REVEALED THAT INSULATOR HAS BEEN SLOWLY BAKED BY HEAT FROM NEARBY EXHAUST DUCT. T HIS IS THE SECOND CONNECTOR AT THIS LOCATION ON OUR FLEET OF JETSTREAMS TO FAIL IN THIS MANNER IN LAST 90 DAYS.RECOMEND WRAPPING CONNECTOR PLUG TO SHEILD FROM LONG TERM HEATING. 2 L 7 2 4T RT A56EU 2002121200031 20021212 00031 EU 2002 12 12 VYGA20020003 1 20020516 A 3397 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU STROBE LIGHT SHORTED E VYGA K NONE L NO TEST IN INSP/MAINT 1 SO 15 431AM 881 WING TIP STROBE LIGHT ASSEMBLY, CONNECTOR PINS ARCH BETWEEN PINS DUE TO INSULATOR BREAK DOWN. THE RESULT WAS SEVERAL POW ER SUPPLIES SLOWLY BROKE DOWN BY STRAY VOLTAGE SHORTING IN THE CONNECTOR. 2 L 7 2 4T RT A56EU 2002121200032 20021212 00032 EU 2002 12 12 VYGA20020004 1 20020516 A 3397 MS3106A10SL3S CONNECTOR BAG JETSTM JETSTM3201 1500217 EU STROBE LIGHT SHORTED E VYGA K NONE L NO TEST IN INSP/MAINT 1 SO 15 431AM 881 BELLY STROBE LIGHT ASSEMBLY CONNECTOR PINS ARCH BETWEEN PINS DUE TO INSULATOR BREAK DOWN. THE RESULT WAS SEVERAL POWERSU PPLIES SLOWLY BROKE DOWN BY STRAY VOLTAGE SHORTING IN THE CONNECTOR. 2 L 7 2 4T RT A56EU 2002121200033 20021212 00033 EU 2002 12 12 02344321 1 20021210 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU TRACK LIGHTS INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 321UE 41045 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF THE EMERGENCY FLOOR TRACK LIGHTING WAS INOPER ATIVE. MAINTENANCE PERSONNEL REPAIRED THE EMERGENCY FLOOR TRACK LIGHTING PIGTAIL CONNECTOR AT SEAT ROW FOUR. AN OPERAT IONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2002121200034 20021212 00034 GL 2002 12 12 2002304623 1 20021027 A 3350 BULB BOMBDR BD700 BD7001A10 1390006 GL EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 623BR LEFT HAND FORWARD MOST EMERGENCY LIGHTS OUT. REPLACED BULBS OPS CHECKED GOOD. 2 L 7 2 4F RT T00003NY 2003022700077 20030227 00077 EA 2003 2 27 21143 1 20021018 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 671BR DURING INSPECTION NR 2 CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED NR 2 CEILING EMERGENCY LIGHT. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 2002121200035 20021212 00035 EA 2002 12 12 21685 1 20021019 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 621BR 7186 DURING INSPECTION THREE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED EMERGENCY LIGHTS. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 2002121200036 20021212 00036 NM 2002 12 12 VNAA0211031 1 20021126 A 6120 A5656 PUMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PROP CONTROL FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 423JS 15875 2366 3032 DURING TAKE OFF, THE CREW RECEIVED A TAKE OFF CONFIGURATION WARNING ON THE RED WARNING PANEL AND ABORTED TAKE OFF. MAIN TENANCE INSPECTED AND THE HIGH PRESSURE PUMP WAS ALLOWING FLUCTUATIONS OF THE PROP BLADE ANGLES. MAINTENANCE THEN REPLA CED THE HIGH PRESSURE PUMP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-00-00. OPERATIONAL CHECKS WERE PERFORMED AN D THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002121200037 20021212 00037 WP 2002 12 12 02FDEA00772 1 20021026 A 2910 O-RING DOUG DC10 DC1010 3022110 WP HYD SYSTEM DAMAGED A FDEA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 386FE 46620 NR 3 HYDRAULIC QUANTITY DROPPED TO 4.9 GAL. WITH HYDRAULIC 3 ELEVATOR OFF LEVEL 2 ALERT, DECLARED EMERGENCY. APPROACH, LANDING AND TAXI NORMAL. ON BLOCK IN NR 3 HYDRAULIC QUANTITY WAS DOWN TO 3.4 GAL. FOUND PRESSURE TRANSDUCER LEAKING AT SEALS (O-RINGS). MANIFOLD NR 3 LOCATED RIGHT WHEEL WELL. REMOVED AND REPLACED 2 EACH O-RINGS ON HYDRAULIC SYSTEM 3 MA NIFOLD PRESSURE TRANSDUCER IAW MD, MM SERVICED NR 3 HYDRAULIC RESERVOIR IAW MD. OPERATIONAL AND LEAK CHECK GOOD, AIRCRA FT CONTINUED SERVICE. 2 L 7 3 4F A22WE 2002121200038 20021212 00038 NM 2002 12 12 VNAA0211034 1 20021129 A 3251 CIRCUIT BREAKER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 470PS 3006 AFTER LANDING, THE CREW RECEIVED A NOSE WHEEL STEERING CAS MESSAGE. THE AIRCRAFT WAS TAKEN TO A RUN UP PAD AND THE PASS ENGERS WERE PICKED UP BY A BUS AND TAKEN TO THE GATE. MAINTENANCE INSPECTED AND CYCLED THE CIRCUIT BREAKERS IN ACCORDAN CE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS TAXIED TO THE GATE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002121200039 20021212 00039 WP 2002 12 12 02FDEA00781 1 20021028 A 2910 O-RING DOUG DC10 DC1030 3023501 WP HYD SYSTEM DAMAGED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 318FE 46837 LOST HYDRAULIC NR 2 FLUID, RUDDER STANDBY POWER OFF, LIGHT ILLUMINATED, LANDED WITHOUT INCIDENT. PERFORMED HYDRAULIC SY STEM NR 2 FAULT ISOLATION AND TRACED PROBLEM TO NONREVERSIBLE S/O VALVE. REPLACED DEFECTIVE O-RING, SERVICED HYDRAULICS TO PROPER LEVEL. CREW NR 2 SYSTEM EDP DID NOT WORK LONG WITHOUT FLUID, AS PRECAUTIONARY ACTION REMOVED AND REPLACED N R 2 HYD MANIFOLD FILTERS IAW MM. CHECKED EDP CASE DRAIN FILTERS ALL OK. PERFORMED LEAK CHECK, MOTORIZED NR 2 ENG CHECK ED FLT SURFACES AND NO LEAKS NOTED. OK FOR SERVICE. 2 L 7 3 4F A22WE 2002121200040 20021212 00040 NM 2002 12 12 VNAA0212002 1 20021201 A 5297 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EMERGENCY DOOR OUT OF ADJUST A VNAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 439JS 3057 ENROUTE FROM PIT TO CAE, THE CREW EXPERIENCED A DOOR LIGHT CAS MESSAGE AND CHIMES. THE CREW FOLLOWED THE QUICK REFERENC E HANDBOOK AND DESCENDED AND THE LIGHT EXTINGUISHED. FLIGHT 4017 THEN DIVERTED TO CAE. MAINTENANCE INSPECTED AND ADJUS TED THE WIRING AT THE 9A EMERGENCY DOOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002121200041 20021212 00041 NM 2002 12 12 VNAA0212003 1 20021203 A 3240 AC69965 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE BRAKE ASSY FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 442JS 959 3060 WHILE ENROUTE TO DCA, THE CREW RECEIVED A EMERGENCY PARKING BRAKE ACCUMULATOR CAS MESSAGE AND DIVERTED TO PHL. MAINTENA NCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OP ERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002121200042 20021212 00042 NM 2002 12 12 VNAA0212004 1 20021203 A 3350 501122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 07 462PS 18438 1150 3084 THE CREW REPORTED THAT THE BACK UP BATTERY DOES NOT ILLUMINATE DURING TEST. MAINTENANCE INSPECTED AND REPLACED THE EMER GENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AI RCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002121200043 20021212 00043 WP 2002 12 12 02FDEA00788 1 20021031 A 2910 O-RING DOUG DC10 DC1030 3023501 WP GE CF6 CF650* 30018 NE HYD SYSTEM DAMAGED A FDEA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 25 318FE 46837 LOST ALL FLUID ON HYDRAULIC NR 2 SYS, RUDDER STANDBY POWER OFF LIGHT ILLUMINATED. DUMPED FUEL AND LANDED AT AIRPORT. P ERFORMED HYDRAULIC SYSTEM NR 2 LEAKAGE FAULT ISOLATION AND TRACED PROBLEM AT NON-REV SHUTOFF VALVE. REMOVED AND REPLACE D DEFECTIVE O-RING, FILL UP HYDRAULIC SYSTEM TO PROPER LEVEL AND RETURN TO NORMAL. NR 2 SYSTEM EDP HYDRAULIC DID NOT WO RK LONGER W/O FLUID, REMOVED AND REPLACED SYSTEM NR 2 HYDRAULIC MANIFOLD FILTERS IAW MM. VISUALLY CHECKED EDP CDASE FIL TER, FOUND OK TO SERVICE. PERFORMED DEEP LEAK CHECKS. RUN HYDRAULIC ELECT PUMP AND MOTORIZED NR 2 ENG MOVE FLT SURFACE S AND NO LEAKS NOTED. ACFT OK TO SERVICE. 2 L 7 3 4F 4 F A22WE E23EA 2002121200044 20021212 00044 NM 2002 12 12 VNAA0212007 1 20021204 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 07 463PS 9575 3087 THE CREW REPORTED THAT THE FIRST TRACK OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPL ACED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORME D AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002121200045 20021212 00045 NM 2002 12 12 VNAA0212008 1 20021204 A 3242 MASTER CYLINDER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE BRAKE SYSTEM FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 472PS 3008 THE CREW REPORTED THAT THE FIRST OFFICER'S BRAKES WERE NOT WORKING. MAINTENANCE INSPECTED AND BLED THE FIRST OFFICER'S MASTER CYLINDER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002121200046 20021212 00046 EU 2002 12 12 V9C2002F00000 1 20021014 A 2741 ACTUATOR ISRAEL 1124 1124 4500102 EU H/S TRIM FAILED A V9CR K NONE L NO TEST IN INSP/MAINT 1 NM 01 430BJ 430 DURING PILOT PREFLIGHT TEST OF THE HORIZONTAL TRIM ACTUATOR, THE MANUAL FUNCTION DID NOT OPERATE. MAINTENANCE WAS CALLE D TO TROUBLESHOOT DEFECT. AFTER CHECKING COCKPIT SWITCH AND WIRING BACK TO THE ACTUATOR, IT WAS DETERMINED THAT THE MAN UAL MOTOR ATTACHED TO THE ACTUATOR HAD FAILED. THE PRIMARY MOTOR DID CHECK PROPERLY IAW MM. DUE TO RESTRAINTS OF PERFO RMING MAINTENANCE ON THIS ASSEMBLY IAW MM, THE HORIZONTAL TRIM ACTUATOR WAS REMOVED AND A LOANER WAS INSTALLED AND CHECK ED IAW MM, NO FURTHER DEFECTS WERE NOTED AFTER INSTALLATION. 2 M 7 2 4F A2SW 2002121200047 20021212 00047 NM 2002 12 12 02FDEA00789 1 20021028 A 3620 MFC DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE NR 1 MALFUNCTIONED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 603FE 48459 AFTER TAKEOFF, RECEIVED A LEVEL 2 AIR MANF 1 FAIL ALERT. DUMPED 62000 LBS FUEL AND MFC FAULT REVIEW LAST LEG SHOWS IN F LIGHT FAULTED MFC PNEU 1 OUT AND ON GROUND FAULTED ALARM (PNEU 1 Z4 OVHT). INSPECT Z4 FOR AIR LEAK NOT FOUND. TROUBLES HOT FIM 36-23-06 R AND I MFC PER MM AND RTS ALL TEST PASSED. A/C OK FOR SERVICE. 2 L 7 3 4F 4 F RT A22WE E13NE 2002121200048 20021212 00048 NM 2002 12 12 2002UALA01513 1 20020927 A 2824 AS1734D32 NUT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RELIEF VALVE DAMAGED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 WP 29 771UA 26932 CREW REPORTED UNCOMMANDED FUEL TRANSFER FROM RT TO LT WING AT A RATE THAT REQUIRED CONSTANT FUEL BALANCING. NO EVIDENCE OF TOTAL FUEL QTY LOSS. A LEAKING WIGGINS COUPLING ON THE JETTISON / REFUEL MANIFOLD, IN THE LT MAIN TANK. ADJACENT T O THE LT OUTBOARD REFUEL VALVE. THE RT MAIN JETTISION FUEL PUMP WAS RUNNING UNCOMMANDED DUE TO ITS ELCU, M28212, FAILIN G IN THE CLOSED POSITION (THUS POWERING THE PUMP.THE COUPLING NUT & SEAL, AND THE ELCU WERE REPLACED 2 L 7 2 4F 4 F RT T0001SE E46NE 2002121200049 20021212 00049 EU 2002 12 12 02FDEA00794 1 20021102 A 3230 MODULE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF66D 30020 GL LANDING GEAR MALFUNCTIONED A FDEA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 657FE 748 ON TAKEOFF, LDG GEAR WOULD NOT RETRACT ON NR 2 SYSTEM. SWITCHED TO NR 1 SYSTEM AND GEAR WOULD STILL NOT RETRACT. REMOV ED LANDING GEAR CONTROL HANDLE 2GA IAW TSM, CONTINUITY CHECKS GOOD BUT MODULE HAS A VERY SUSPICIOUS RATTLE. REMOVED AND REPLACED 2GA MODULE IAW A300 AMM AS PRECAUTIONARY. RECEIVED LANDING GEAR SAFETY RELAY CONTROL MODULE FROM MEM AND PERF ORMED ADJUSTMENT/TEST OF RELAY EM SAFETY SYSTEM IAW A300 AMM. ALL SYSTEMS OPERATE NORMAL, ALL IND CHECK NORMAL. DISCONN ECTED TEST SET AND RETURNED AIRCRAFT TO NORMAL. INSTALLED NEW PROXIMITY DETECTION UNIT 54GB AND PERFORMED DETECTOR CONT INUITY TEST. 2 L 7 2 4F 4 F RT A35EU E23EA 2002121200050 20021212 00050 NM 2002 12 12 02FDEA00803 1 20021106 A 3230 PIVOT BOEING 727 727200 138407E NM GE CF6 CF66D 30020 GL NLG CONTAMINATED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 203FE 22925 DURING NORMAL GEAR EXTENSION, NOSE GEAR DID NOT COME DOWN, HAD NO GREEN LIGHT, HAD RED DOORS AND UNSAFE LIGHT. MAINS CA ME DOWN NORMALLY. FOLLOWED RED TABS TO MANUALLY EXTEND NOSE, CAME DOWN OK. FOUND WATER COMING FROM NOSE LANDING GEAR P IVOT KNUCKLE. REMOVED BOTH PLUGS AND LUBED KNUCKLE IAW M/M. PURGED KNUCKLE OF EXCESSIVE WATER. JACKED AIRCRAFT NOSE A ND TESTED NOSE LANDING GEAR EXTENSION AND RETRACTION IAW M/M, CYCLED GEAR NUMEROUS TIMES OPS CHECK GOOD. OK FOR SERVICE . 2 L 7 3 4F 4 F RT A3WE E23EA 2002121200051 20021212 00051 WP 2002 12 12 0204019929 1 20021210 A 2780 5919526508 DUCT DOUG DC9 DC931 3022065 WP LACK OF LUBE A NWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 01 8923E 45838 When the slats were extended the aircraft rolled and the "Slat Disagreement" light illuminated. After about 2 minutes th e light extinguished and the aircraft flew normally. Landing at YYG was without incident. No mention of COM procedures. Maintenance found no discrepencies with either wing slat system. The right T-Duct was lubricated and will be replaced wi thin 5 cycles. The aircraft has been returned to service. 2 L 7 2 4F A6WE 2002121200052 20021212 00052 WP 2002 12 12 0204029929 1 20021208 A 2780 5919526508 DUCT DOUG DC9 DC931 3022065 WP A NWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 01 8923E 45838 During approach the aircraft rolled left on slat extension. "Slat Disagreement" light was illuminated. COM procedures we re performed and the aircraft landed uneventfully. Maintenance replaced a T-Duct in the left wing. The aircraft was retu rned to service. 2 L 7 2 4F A6WE 2002121200053 20021212 00053 NE 2002 12 12 02FDEA00811 2 20021107 A 7260 CHIP DETECTOR DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 2 ENGINE CONTAMINATED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 303FE 46802 ENGINE NR 2 OIL FILTER LEVEL 2 ALERT, CAME ON AT TOP OF CLIMB. THROTTLE WAS RETARDED TO IDLE BUT ALERT STAYED ON. ENGI NE NR 2 WAS SHUT DOWN IAW THE CHECKLIST. ENGINE FAN COWLS WERE OPENED AND THE MASTER CHIP DETECTOR WAS PULLED, FERROUS METAL STRANDS WERE COVERING THE END. THE LUBE SUPPLY FILTER AND SCAVENGE OIL FILTER WAS REMOVED AND SAMPLES WERE PLACED IN SAMPLE BAGS & TAGGED. MEM PP ENGINE WAS NOTIFIED THAT A FINE FERROUS CONTAMINANT GOLD IN COLOR, WAS PRESENT. PULLE D SCAVENGE PUMP FILTER SCREENS AND FOUND METAL IN THE B SCAVENGE IN FILTER. 2 L 7 3 4F 4 F RT A22WE E23EA 2002121200054 20021212 00054 GL 2002 12 12 02FDEA00812 2 20021107 A 7200 CF66D ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1 FAILED A FDEA E C ENGINE SHUTDOWN ABORTED TAKEOFF A FLAME/FIRE TO TAKEOFF 1 SO 25 384FE 46617 SETTING STANDARD POWER ON EWR 4L, WIND 3309, AIRCRAFT BEGAN TO ROLL, AND IMMEDIATELY AND EXPLOSION OCCURRED, PULLING THE AIRCRAFT HARD LEFT. AIRCRAFT EXITED THE RUNWAY WITH TORCHING FROM LEFT ENGINE REPORTED BY TRAILING AIRCRAFT. NR 1 ENG INE SHUTDOWN ACCOMPLISHED AFTER FIRE REPORTED. TOWER ASKED IF EMERGENCY TRUCKS REQUIRED. WE ACCEPTED BECAUSE THERE WAS NO FIRE INDICATION IN COCKPIT. IDLE POWER ON NR 1 NORMAL DURING ABORT. INSPECTED ENGINE, FOUND DAMAGE TO NR 7 COMPONE NT TRAILING EDGE NR 8 AND NR 9 COMPONENT SECTION BLADES WERE MISSING. S/D COMING. 2 L 7 3 4F 4 F A22WE E23EA 2002121200055 20021212 00055 NM 2002 12 12 2002UALA01557 1 20021009 A 2430 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 343UA 24247 AIRCRAFT LANDED UNDER AMBER ALERT WHEN BOTH LT AND RT DC FAIL LIGHTS ILLUMINATED IN FLIGHT. SUPPLEMENTAL DATA UPDATE RES ET C-B GEN POWER CONT ON P6-5. OPS CHECKED NORMAL 2 L 7 2 4F 4 F RT A16WE E2GL 2002121200056 20021212 00056 NM 2002 12 12 2002UALA01579 1 20021011 A 2611 SMOKE DETECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE E/E BAY MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 660UA 27115 AFTER GEAR RETRACTION FORWARD EQUIPMENT SMOKE EICAS MESSAGE AND OVERHEAD SMOKE LIGHT ON. SUPPLEMENTAL DATA UPDATE CAUSE: NO SIGNS OF SMOKE OR HEAT WERE REPORTED TO SUGGEST A SMOKE OR HEAT CONDITION EXISTED. NO PREVIOUS HISTORY IN AMIS PR IOR TO RETURN TO FIELD OR AFTER DETECTOR (TS164) REPLACEMENT IN IADMM 12 OCT 02. CORRECTIVE ACTION: IADMM MECHANIC REP LACED EE COOLING SMOKE DETECTOR AND GROUND CHECK WAS NORMAL. NO FURTHER CHRONICS IN AMIS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002121200057 20021212 00057 EU 2002 12 12 U30A200200022 1 20020918 A 2700 3945128102 COMPUTER AIRBUS 320 A320214 3930316 EU ELAC SYSTEM INTERMITTENT A U30A O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 17 261AV 2462 2462 1615 AFTER FLIGHT 256, EWR - PUJ, WHILE ON THE GATE AT PUJ, NR 2 ELAC (ELEVATOR AILERON COMPUTER) FAULTED ON ECAM. SWAPPED NR 1 & 2 ELAC'S PER AMM 27-93-34. PERFORMED OPS CHECK FOR BOTH ELAC'S PER AMM 27-93-00-710-001 AND TESTED OK. DEFERRED NR 1 ELAC PER MEL 27-93-01-2. UPON RETURN TO EWR (THE NEXT FLIGHT), REPLACED NR 1 ELAC AND OPS CHECKED PER AMM 27-93-00-70 1-001 OK. 2 L 7 2 4F RT A28NM 2002121200058 20021212 00058 NE 2002 12 12 02FDEA00813 2 20021108 A 7230 CF650C2 COMPRESSOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE DAMAGED A FDEA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 318FE 46837 517465 ON TAKEOFF AND JUST 5 AFTER ROTATION HEARD LOUD NOISE AND ENGINE NR 3 ROLLED BACK TO APPROXIMATELY 35 PERCENT N1. ENGIN E OVER TEMP LIGHT CAME ON MOMENTARILY. ENGINE CONTINUED TO WINDMILL. DUE TO NOISE AND VIBRATION PULLED ENGINE FIRE HAN DLE AND BLEW NR 1 BOTTLE. FOUND SOME SMALL METAL PIECES IN THE TAILPIPE JUST AFT OF BLADES IN THE SHROUD AREA. EGT IND ICATOR RECORDED MAX EGT AT 999 FOR 1 SECOND. REMOVED BORESCOPE PLUGS B1-3, B1-11, B3-1 AND B3-2. ENGINE HAS MASSIVE BL ADE DAMAGE, WELL BEYOND MM LIMITS FROM ABOUT 12TH STAGE ON BACK, ENGINE REQUIRES REMOVAL. 2 L 7 3 4F 4 F A22WE E23EA 2002121200059 20021212 00059 NE 2002 12 12 02FDEA00825 2 20021113 A 7311 9250M97P04 OIL COOLER DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE NR 1 ENGINE LEAKING A FDEA E ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 SO 25 590FE 48505 AFTER TAKEOFF NR 1 OIL QUANTITY DROPPED TO 2 QTS. TEMPERATURE ROSE 30 DEGREES ABOVE NR 2 AND NR 3. PRESSURE DROPPED 25 PSI BELOW NR 2 AND NR 3. ENGINE SHUT DOWN. REMOVED AND REPLACED O-RING IAW MM. REMOVED AND REPLACED FUEL OIL HEAT EX CHANGER IAW MM. ENGINE FLUSH CARRIED OUT IAW MM. ENGINE RUN CARRIED OUT IAW MM. 2 L 7 3 4F 4 F RT A22WE E13NE 2002121200060 20021212 00060 EU 2002 12 12 02FDEA00836 1 20021114 A 3260 SWITCH AIRBUS 310 A310 EU GE CF6 CF680 30025 NE NLG FAILED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 426FE 245 GO-AROUND DUE TO ONLY 2 GREEN LANDING GEAR LIGHT ON FORWARD LANDING GEAR PANEL, OVERHEAD LANDING PANEL 3 GREEN AS NORMAL . DURING GO-AROUND FORWARD GREEN NOSE GEAR LIGHT CAME ON. NORMAL LANDING ON SECOND PASS. LANDING GEAR INDICATING PANEL S SYSTEM NR 1 NOSE GEAR DOWN LOCK INDICATOR INOPERATIVE. REMOVED AND REPLACED MICRO SWITCH 40GB IAW AMM. OPS CHECK NOR MAL. 2 L 7 2 4F 4 F RT A35EU E13NE 2002121200061 20021212 00061 EU 2002 12 12 02FDEA00837 1 20021114 A 7797 WIRE AIRBUS 310 A310 EU EGT INDICATOR CHAFED A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 419FE 345 ON TAKEOFF ROLL GREATER 80 KNOTS TO POWER NOT ACHIEVED. NR 2 EGT FLUCTUATION +- 200C FOLLOWED BY ROLLBACK TO ZERO. DAS HED LINES RTD ON TAXI OUT/IN OK. REPAIRED CHAFED WIRING TO NR 2 EGT INDICATOR IAW EA. COMPLIED WITH PART 2 EA. OPS CH ECK NORMAL. 2 L 7 2 4F RT A35EU 2002121200062 20021212 00062 EU 2002 12 12 02FDEA00874 1 20021125 A 5753 SKIN AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE T/E FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 678FE 792 RT WING CENTER FLAP LOWER SKIN TRAILING EDGE AREA AT TRACK 3, 5 EA DENTS BET TRAILING EDGE RIBS 12A AND 13A. REPAIRED L OWER RIGHT CENTER FLAP SKIN IAW EA. CUT DAMAGED SKIN AT DENTS. EDDY CURRENT INSPECTED DENTS, NO CRACKS EXISTED. FLAP PEENED REWORKED AREA IAW SRM. FILLED DENTS 1, 2, AND 3 AND FABRICATED REPAIR DOUBLER IAW A300 SRM AND EXTENDED DOUBLE R TO ACCOMMODATE DENTS 1, 2 & 3. INSTALLED REPAIR DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A35EU E13NE 2002121200063 20021212 00063 NM 2002 12 12 02FDEA00908 1 20021203 A 5270 WARNING SYSTEM BOEING 727 727200 138407E NM COCKPIT MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 209FE 22931 AFT AIRSTAIR LIGHT CAME ON AFTER TAKE OFF AND REMAINED ILLUMINATED THROUGH BLOCK IN. CYCLED AIR STAIRS SEVERAL TIMES. STAIRS WORKED & LIGHT WENT OUT EACH OUT. 2 L 7 3 4F RT A3WE 2002121200064 20021212 00064 NM 2002 12 12 02FDEA00909 1 20021204 A 5320 STRAP BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION ON FLOOR STRAP AT BS 1174, LBL 24 TO RBL 24, WL 208. SEVERAL AREA'S OUT OF LIMITS IAW SRM 53-10-01. REMOVED CHORD AND INSTALLED NEW CHORD IAW 51-30-2. 2 L 7 3 4F RT A3WE 2002121900012 20021219 00012 NM 2002 12 19 02FDEA00910 1 20021204 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION IN FWD CARGO BAY ON STRINGER 27 LT, BS 660. REPAIRED STR 27 LT, BS 660 IAW SRM 53-10-3. 2 L 7 3 4F RT A3WE 2002121900013 20021219 00013 NM 2002 12 19 02FDEA00911 1 20021204 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION ON UPPER FLANGES OF THE TRANSVERSE FLOORBEAM. BS 760 - 840, RBL 25, WL 208. REPAIRED TRANSVERSE FLOORBEAM BY REPLACEMENT IAW SRM 51-30-2, 53-10-1, DWG 65-16279. 2 L 7 3 4F RT A3WE 2002121900014 20021219 00014 NM 2002 12 19 02FDEA00912 1 20021204 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION IN FWD CARGO BAY ON STRINGER 28 RT, BS 659. REPAIRED STRINGER 28 RT, BS 659. IAW SRM 53-10-3 2 L 7 3 4F RT A3WE 2002121900015 20021219 00015 NM 2002 12 19 02FDEA00913 1 20021204 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 SEAT TRACK FROM BS 760 TO 850 IS CORRODED. LBL 25, WL 208. REPLACED SEAT TRACK AND T-CHORD OF LONGITUDINAL BEAM IAW SRM 53-10-5, 51-30-2 51-30-8. 2 L 7 3 4F RT A3WE 2002121200065 20021212 00065 NM 2002 12 12 02FDEA00914 1 20021204 A 5315 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D9 52048 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION ON TOP OF FLOORBEAM BS 344, RBL 17 TO LBL 64, WL 208. REMOVED AND REPLACED UPPER CHORD B.S. 344, LBL 65 - R BL 64, WL 208 IAW SRM 51-30-2, DWG SR 27-53-007. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121900016 20021219 00016 NM 2002 12 19 02FDEA00915 1 20021204 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 CORROSION AT STA 617-624, WL 151, RBL 15, ON STRINGER 27 RT. INSPECTION OF STRINGER 27 RT, WL 151, BS 617 - 624 FOUND I T TO BE OUT OF LIMITS PER BOEING SRM REMOVED DAMAGED AREA AND REPLACED PER BOEING SRM 53-10-3. 2 L 7 3 4F RT A3WE 2002121900017 20021219 00017 NM 2002 12 19 02FDEA00916 1 20021204 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 DENT IN EXTERIOR SKIN AT BS 48, 1 INCH BELOW STRINGER 21 RT. REPAIRED SKIN BS 480, 1 INCH BELOW STRINGER 21 RT IAW SR M 53-30-3. 2 L 7 3 4F RT A3WE 2002121200066 20021212 00066 NM 2002 12 12 02FDEA00917 1 20021124 A 5531 STRINGER BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 NR 8R STRINGER CRACKED AT RIB IN VERTICAL STABILIZER TUNNEL. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121900018 20021219 00018 WP 2002 12 19 02FDEA00918 1 20021204 A 2120 DUCT DOUG DC10 DC1010 3022110 WP E/E BAY OVERHEATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 RADIO RACK FAN EXHAUST DUCT EXHIBITS SIGNS OF FIRE AND OVERHEATING, INSULATION BLANKETS AND FOAM MATERIAL FROM INSIDE OF DUCT BELOW MAIN CABIN FLOORING AT BS 475 THRU BS 495. R&R DUCT ASSY, BLACK FOAM DETERIORATED. INSPECTION FOUND NO EVI DENCE OF FIRE. 2 L 7 3 4F A22WE 2002121200067 20021212 00067 EU 2002 12 12 02FDEA00919 1 20021204 A 7830 THRUST REVERSER AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE NR 1 ENGINE MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 681FE 799 DURING TAKEOFF POWER APPLICATION AS POWER STABILIZED AT TOGA SETTING, ECAM ANNUNCIATED A NR 1 REVERSER PRESSURIZED WARNI NG. TAKEOFF WAS ABORTED AT ABOUT 60 KTS. ENGINE NR 1 THRUST REVERSER , INOPERATIVE. THRUST NR 1 (1 OR 2) REVERSER DEA CTIVATED IN FORWARD THRUST POSITION. 2 L 7 2 4F 4 F RT A35EU E13NE 2002121200068 20021212 00068 EU 2002 12 12 02FDEA00920 1 20021204 A 7830 CONNECTOR AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE THRUST REVERSER LOOSE A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 684FE 802 GOT ECAM WARNING, NR 2 ENGINE THRUST REVERSER PRESSURIZED ON TAKEOFF ROLL, BELOW 80 KNOTS. SECURED CONNECTOR PLUGS AND RAN ENGINES, NO ECAM MESSAGE REPEAT. 2 L 7 2 4F 4 F RT A35EU E13NE 2002121200069 20021212 00069 WP 2002 12 12 02FDEA00921 1 20021204 A 5210 MOTOR DOUG DC10 DC1010F 3022111 WP GE CF6 CF6* 30020 GL R1 DOOR FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 DOOR HARD TO OPEN. MOTOR SOUNDS LIKE SPINS, CLUTCH SLIPS. R/R R1 DOOR ELECTRIC MOTOR, SHAFT, BEARINGS AND PNEU MOTOR REF MM 52-11-01-02. 2 L 7 3 4F 4 F A22WE E23EA 2002121200070 20021212 00070 WP 2002 12 12 02FDEA00925 1 20021205 A 5230 5211702 BEAM DOUG DC10 DC1030F 3023504 WP GE CF6 CF650* 30018 NE CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 319FE 47820 CENTER CARGO DOOR COUNTER BALANCE BEAM CRACKED AT FORWARD BRACKET. REMOVED AND REPLACED COUNTER BALANCE BEAM ASSEMBLY I AW MM. 2 L 7 3 4F 4 F RT A22WE E23EA 2002121200071 20021212 00071 WP 2002 12 12 AALA20021532 1 20021010 A 5720 CASTING DOUG DC9 DC982 3022082 WP RT WING GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 TUL - FOUND LEADING EDGE SLAT CABLE PULLEY CUT GROOVE IN NR 1 SLAT CASTING INBOARD SIDE FORWARD SIDE OF CASTING RT WING. BLENDED GOUGE AND INSTALLED DOUBLER PER ESO 80559. (M) 2 L 7 2 4F A6WE 2002121200072 20021212 00072 2002 12 12 U30A200200023 4 20021017 A 3460 B546CAM0103 COMPUTER AIRBUS 320 A320214 3930316 EU FLT MANAGEMENT FAULTY A U30A K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 17 261AV 2713 2713 1615 ON PRE-FLIGHT AT EWR FOR FLT 266 EWR-CUN, NR 2 FLIGHT MANAGEMENT GUIDANCE COMPUTER (FMGC) FAULTED ON ECAM. DEFERRED PER MEL 22-83-01(2). REMOVED AND REPLACED NR 2 FMGC I/A/W AMM 22-83-34-401, TWO FLIGHTS LATER THAT DAY. 2 L 7 2 4F RT A28NM 2002121200073 20021212 00073 WP 2002 12 12 AALA20021556 1 20021011 A 5310 STRAP DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 573AA 53092 TUL - FOUND FORWARD PASSENGER AFT FRAME STRAP CRACKED STATION 207 LONGERON 15 LEFT. INSTALLED DOUBLER TO REPAIR CRACKED FRAME. STRAP ON FORWARD PASS DOOR CUT OUT STATION 207, LONGERON 15 PER AARD REF 53-10-00-11. (M) 2 L 7 2 4F A6WE 2002121200074 20021212 00074 EU 2002 12 12 U30A200200024 1 20021025 A 2612 WARNING LIGHT AIRBUS 320 A320214 3930316 EU COCKPIT FALSE INDICATION A U30A O OTHER N FALSE WARNING CR CRUISE 1 EA 17 261AV 1615 UPON COCKPIT SCAN FOUND NR 1 ENGINE FIRE BOTTLE DISCHARGE LIGHT ON. NO ECAM NOTED AND NO PRESENT LEG FAULTS FOUND. PERFO RMED TEST NR 1 AGENT ENG NR 1 FIRE EXTINGUISH LIGHT. ACCORDING TO AMM 26-11-00-01 AGENT NR 1 ENGINE FIRE LIGHT OF FOR SE RVICE. 2 L 7 2 4F RT A28NM 2002121200075 20021212 00075 2002 12 12 SWAA022798 4 20021126 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002121200076 20021212 00076 NM 2002 12 12 SWAA022799 1 20021124 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 4L, BS 400 AND BS 420. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002121200077 20021212 00077 NM 2002 12 12 SWAA022800 1 20021127 A 3350 604222 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED RON, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002121200078 20021212 00078 NM 2002 12 12 SWAA022801 1 20021127 A 3350 6104781 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED SPECIAL VISIT, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002121200079 20021212 00079 2002 12 12 U30A200200025 4 20021028 A 2211 COMPUTER AIRBUS 320 A320214 3930316 EU GUIDANCE SYS MALFUNCTIONED A U30A O OTHER J WARNING INDICATION CR CRUISE 1 EA 17 260AV 1564 DURING CRUISE OF FLT 135 MYNN (NASSAU) TO KBWI (BALTIMORE) NR 2 FLIGHT MANAGEMENT GUIDANCE COMPUTER (FMGC) FAULTED ON EC AM. PERFORMED RESET OF SYSTEM AT BWI IN ACCORDANCE WITH TSM TASK 24-00-00-810-818. NO DEFECTS NOTED, MESSAGE CLEARED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2002121200080 20021212 00080 NM 2002 12 12 SWAA022804 1 20021127 A 3350 BR9442 HOUSING BOEING 737 7373A4 1384585 NM LAVATORY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 1/2D CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT HOUSING DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT A SSY PER MM. 2 L 7 2 4F RT A16WE 2002121200081 20021212 00081 NM 2002 12 12 SWAA022805 1 20021126 A 3350 300432 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 708SW 27842 DURING SCHEDULED SERVICE CHECK, FOUND FWD RT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED RT EXTERIOR EMERGENCY EXIT LI GHT PER MM. 2 L 7 2 4F RT A16WE 2002121200082 20021212 00082 EU 2002 12 12 U30A200200026 1 20021111 A 3350 321430 BATTERY PACK AIRBUS 320 A320214 3930316 EU ZONE 242 DISCHARGED A U30A K NONE L NO TEST IN INSP/MAINT 1 EA 17 260AV 839 839 1564 DURING DAILY INSPECTION AT ORD, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED BATTERY PACK I/A W AM M 33-51-38-401 AND OPERATIONALLY CHECKED THE SYSTEM WITH NO FURTHER DEFECTS. 2 L 7 2 4F RT A28NM 2002121200083 20021212 00083 2002 12 12 SWAA022806 4 20021127 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002121200084 20021212 00084 EU 2002 12 12 U30A200200027 1 20021112 A 3350 PL22412LH055 LIGHT AIRBUS 320 A320214 3930316 EU CABIN CRACKED A U30A K NONE O OTHER IN INSP/MAINT 1 EA 17 262AV 1760 1760 1725 AFTER FLT 9262, DURING DAILY INSPECTION, A SECTION OF PHOTOILLUMINESCENT STRIP ON FLOOR AT SEAT 1R IS CRACKED (ALTHOUGH STILL OPERATIONAL). REPLACED PHOTOILLUMINSCENT STRIP SECTION AT SEAT 1R PER AMM 33-51-21-000-001. OPS CK'D OK. 2 L 7 2 4F RT A28NM 2002121200085 20021212 00085 NM 2002 12 12 SWAA022809 1 20021129 A 3397 BR2013 WIRE BOEING 737 7372H4 138448C NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 071SW 22358 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW NR 1. RESPLICED EEPLS PER MM. 2 L 7 2 4F A16WE 2002121200086 20021212 00086 EU 2002 12 12 U30A200200028 1 20021115 A 2700 3945128102 COMPUTER AIRBUS 320 A320214 3930316 EU ZONE 127 MALFUNCTIONED A U30A O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 17 263AV 92 92 1860 PRIOR TO DEPARTURE OF FLT 9263 ORD-ELP, THE NR 1 ELEVATOR AND AILERON COMPUTER (ELAC) [PITCH] FAULTED ON ECAM. DEFERRED ELAC NR 1 PER MEL 27-93-01-2. ALL MAINTENANCE AND OPERATIONS REQUIRED ITEMS ACCOMPLISHED. REPLACED NR 1 ELAC PER AMM 27- 93-34 AND OPS CHECKED OK IAW AMM 27-93-00-710-001 ON RETURN TO ORD ON NOV.16, 2002. 2 L 7 2 4F RT A28NM 2002121200087 20021212 00087 NM 2002 12 12 SWAA022810 1 20021129 A 5523 65C2638428A TRIM TAB BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVAT OR TAB PER MM. 2 L 7 2 4F RT A16WE 2002121200088 20021212 00088 2002 12 12 SWAA022812 4 20021130 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002121200089 20021212 00089 2002 12 12 SWAA022815 4 20021130 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002121200090 20021212 00090 EU 2002 12 12 U30A200200029 1 20021122 A 5210 CYLINDER AIRBUS 320 A320214 3930316 EU PAX DOOR DISCHARGED A U30A K NONE O OTHER IN INSP/MAINT 1 EA 17 262AV 1725 DURING "DAILY" INSPECTION AFTER FLT 155 IN PHL, THE L1 CREW / PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS L OW. SERVICED THE EMERGENCY OPERATION CYLINDER WITH NITROGEN IAW AMM 52-10-00-614-050. FOR PRECAUTIONARY MEASURES; REPLAC ED SEALS AND PACKINGS IN THE PERCUSION MECHANISM OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ON 11/23/02. NO FUR THER PRESSURE DROP HAS BEEN OBSERVED. 2 L 7 2 4F RT A28NM 2002121200091 20021212 00091 2002 12 12 SWAA022816 4 20021130 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002121200092 20021212 00092 NM 2002 12 12 SWAA022818 1 20021201 A 5523 65C2638428A TRIM TAB BOEING 737 7373H4 1384600 NM RT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED A1 CHECK, SWA SI 11139-55, RT ELEVATOR TAB CRACKED AT NR 3 HINGE CUTOUT. REMOVED AND REPLACED RT ELEVA TOR TAB PER MM. 2 L 7 2 4F RT A16WE 2002121200093 20021212 00093 NM 2002 12 12 SWAA022819 1 20021130 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STRINGER 14L. REMOVED AND REPLACED STRINGER SP LICE PER SRM. 2 L 7 2 4F RT A16WE 2002121200094 20021212 00094 2002 12 12 U30A200200031 4 20021203 A 2565 D30665109 SLIDE RAFT AIRBUS 320 A320214 3930316 EU PAX DOOR FAILED A U30A K NONE L NO TEST IN INSP/MAINT 1 EA 17 261AV 3124 3124 1615 DURING A PLANNED INTENTIONAL DEPLOYMENT OF THE LEFT AFT (L2) SLIDE / RAFT ASSY, THE SLIDE / RAFT ASSY FAILED TO DEPLOY P ROPERLY. FULL INFLATION AND DEPLOYMENT WAS NOT ACHIEVED. NOTE: THE DOOR ASSIST BOTTLE PRESSURE AND THE SLIDE / RAFT BOTT LE PRESSURE WERE VERIFIED AS CORRECT PRIOR TO THE EXERCISE. THE FAILED UNIT HAS BEEN SENT TO THE REPAIR STATION FOR INVE STIGATION AND REPAIR.THIS SLIDE / RAFT ASSY HAS BEEN INSTALLED ON THE AIRCRAFT SINCE NEW AS DELIVERED FROM AIRCRAFT MANU FACTURER. 2 L 7 2 4F RT A28NM 2002121200095 20021212 00095 EU 2002 12 12 U30A200200032 1 20021203 A 3350 32145410 LIGHT AIRBUS 320 A320214 3930316 EU ZONE 241 INOPERATIVE A U30A K NONE L NO TEST IN INSP/MAINT 1 EA 17 260AV 2766 2766 1564 DURING SCHEDULED INSPECTION AT YWG, EMERGENCY EXIT (11WL), THE EMERGENCY PATHWAY SYSTEM UNIT (EPSU) FAILED TO OPERATE. R EPLACED EPSU AND TESTED SYSTEM IAW AMM 33-51-38-401. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F RT A28NM 2002121200096 20021212 00096 NM 2002 12 12 SWAA022820 1 20021201 A 3350 6104789 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED PM CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002121200097 20021212 00097 2002 12 12 U30A200200033 4 20021208 A 2211 C13042AA01 COMPUTER AIRBUS 320 A320214 3930316 EU ZONE 128 MALFUNCTIONED A U30A O OTHER J WARNING INDICATION CR CRUISE 1 EA 17 264AV 76 76 1867 DURING CRUISE ON FLT 9518, ORD-CUN, AUTO PILOT NR 2 (AP2) FAULTED. UPON ARRIVAL IN CUN, DEFERRED PER MEL 22-83-01. REPLA CED FMGC NR 2 IN ORD ON DEC. 9, 2002 IAW AMM 22-83-34-400-001. AFS TEST OK PER AMM 22-96-00-710-001. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F RT A28NM 2002121200098 20021212 00098 NM 2002 12 12 SWAA022821 1 20021201 A 2560 BR9442 SIGN BOEING 737 7373K2 13844BA NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 EMERGENCY EXIT SIGN AT FWD ENTRY DOOR BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2002121200099 20021212 00099 NM 2002 12 12 SWAA022827 1 20021201 A 3350 6556633 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT BULB INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F A16WE 2002121200100 20021212 00100 NM 2002 12 12 PCAA0212146 1 20021212 A 2160 BYLF51514 SENSOR DHAV DHC8 DHC8102 2809003 NM COCKPIT OVERHEATED A PCAA K NONE M OVER TEMP NR NOT REPORTED 1 EA 13 826EX 17273 3610 389 PHL - FLIGHT#3740. CREW REPORTED A BURNING SMELL IN COCKPIT. MAINTENANCE INSPECTED ALL ELECTRICAL EQUIPMENT IN COCKPIT AND COULD NOT FIND ANY DEFECTS. AFTER INSPECTING THE COCKPIT ZONE SENSOR IT WAS FOUND TO BE OVERHEATED. ZONE SENSOR REPL ACED, NO FURTHER ODORS DETECTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002121200101 20021212 00101 NM 2002 12 12 SWAA022828 1 20021201 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASS Y PER MM. 2 L 7 2 4F A16WE 2002121200102 20021212 00102 NE 2002 12 12 SWIA200211510 2 20021118 A 7324 3033960 FLOW DIVIDER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF R Y J PARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 NM 07 223SW 6146 3621 120291 ON TAKEOFF ROLL BELOW 80 KTS, THE LT ENGINE SHUT DOWN. ABORTED THE TAKEOFF. REMOVED AND REPLACED LT ENGINE FLOW DIVIDER . RAN ENGINE. SYSTEM OPS CHECK AND LEAK CHECK GOOD IAW EMB120 MM 73-14-00 & P&W MM. 2 L 7 2 4T 4 T RT A31SO E20NE 2002121200103 20021212 00103 SO 2002 12 12 SWIA200211511 1 20021124 A 2910 FITTING EMB 120 EMB120ER 3260203 SO HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 308SW 120326 WHILE INFLIGHT RECEIVED A LOW RESERVOIR PRESSURE LIGHT. WHEN EXTENDING GEAR THE MAIN PUMP LOW PRESSURE LIGHT ILLUMINATE D. TURNED ELECTRIC PUMP TO ON. IMMEDIATELY LOW LEVEL LIGHT ILLUMINATED AND GAUGE WENT TO 0. PRESSURE FLUCTUATED BUT F LAPS CAME DOWN. PRESS DROPPED WHEN ELECTRIC PUMP OFF. TIGHTENED LOOSE HYDRAULIC LINE FITTING AT RIGHT ENGINE FIREWALL AND REPLACED ENGINE DRIVEN HYDRAULIC PUMP. RAN RIGHT ENGINE 30 MINUTES. NO LEAKS. 2 L 7 2 4T RT A31SO 2002121200104 20021212 00104 EA 2002 12 12 SWIA200211513 1 20021105 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW 7497 ANGLE BRACKETS AT LBL AND RBL 9 AND FS 280 FOUND CRACKED DURING C CHECK INSPECTION. REPLACED BRACKETS IAW CRJ SRM 51- 40-11, 51-42-21, 51-42-06. 2 L 7 2 4F RT A21EA 2002121200105 20021212 00105 EA 2002 12 12 SWIA200211514 1 20021105 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW 7497 FS 484 LEFT INTERCOSTAL OUTBOARD FLANGE FOUND CRACKED AT LBL 36.00. FOUND DURING C CHECK INSPECTION. DAMAGED AREA REP AIRED IAW CRJ REO 601R-53-41-059. NDT-HFEC CARRIED OUT IAW REO 601R-53-41-0059. NO OTHER CRACKS NOTED. 2 L 7 2 4F RT A21EA 2002121200106 20021212 00106 EA 2002 12 12 SWIA200211517 1 20021014 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 411SW 7067 FS 280.0 RBL 9.0 INBOARD FLOOR SUPPORT ANGLE CRACKED. FOUND DURING C CHECK INSPECTION. FIT AND INSTALLED NEW ANGLE IAW CRJ SRM 51-40-11, 51-42-06, AND 51-42-21. 2 L 7 2 4F RT A21EA 2002121200107 20021212 00107 WP 2002 12 12 IXXA0200118S 1 20020823 A 5700 WING DOUG DC8 DC871F 302199D WP LOWER L/E CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LEFT WING LOWER LEADING EDGE SCREW HOLE. REPAIR ACCOMPLI SHED, REMOVAL OF PREVIOUS REPAIR, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF FILLER AND DOUBLER IN ACCORDANCE WI TH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING AUTHORIZATION R12-R01 2 L 7 4 4F RT 4A25 2002121200108 20021212 00108 WP 2002 12 12 IXXA0200132S 1 20020828 A 5240 DOOR DOUG DC8 DC871F 302199D WP FWD CARGO DAMAGED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A TEMPORARY REPAIR WAS DISCOVERED ON THE LOWER FORWARD CARGO COMPARTMENT FORWARD DOOR CUT OUT ON THE RIGHT HAND SIDE FORWARD AND AFT CORNERS @ FUSELAGE STATION 280 LONGERON 30R. REPAIR ACCOMPLISHED, REMOVA L OF TEMPORARY REPAIR, FABRICATION AND INSTALLATION OF REPAIR DOUBLERS AND TRIPLERS IN ACCORDANCE WITH THE DOUGLAS STRUC TURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2002121200109 20021212 00109 WP 2002 12 12 IXXA0200135S 1 20020911 A 5313 LONGERON DOUG DC8 DC871F 302199D WP LONGERON 33R CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LONGERON 33R AT STATION 350 AFT OF THE C-1 DOOR CUT OUT. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED LONGERON FROM STATION 340 TO 450, FABRICATION AND INSTALLATION OF NEW LONGERON IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2002121200110 20021212 00110 WP 2002 12 12 IXXA0200137S 1 20020912 A 5313 LONGERON DOUG DC8 DC871F 302199D WP STATION 36 CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON LONGERON 36 AT STATION 380. REPAIR ACCOMPLISHED, REMOVAL O F DAMAGED LONGERON FROM STATION 360 TO 450, FABRICATION AND INSTALLATION OF NEW LONGERON IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2002121200111 20021212 00111 WP 2002 12 12 IXXA0200138S 1 20020925 A 5700 WING DOUG DC8 DC871F 302199D WP R/H UPPER CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE UPPER RIGHT WING, INBOARD OF FUEL PANEL 505F AT THE UPPER AFT PLANK. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLERS AND DOUBLERS IN ACCOR DANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2002121200112 20021212 00112 EA 2002 12 12 SWIA200211518 1 20021014 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 411SW 7067 FS 280 PILOT'S BULKHEAD FLOORBEAM CRACKED AT RBL 9.0 & LBL 9.0. FOUND DURING C CHECK INSPECTION. HFEC INSPECTION CAR RIED OUT ON CUTOUT REPAIRS AS REQUIRED IAW RJ NDTM 51-20-06. NO CRACKS FOUND. REPAIRED DAMAGED AREA IAW CRJ REO 601R-5 3-11-171, REV. ''NC''. 2 L 7 2 4F RT A21EA 2002121200113 20021212 00113 EA 2002 12 12 SWIA200211519 1 20021014 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA E/E BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 411SW 7067 ELECTRICAL BAY FLOOR FS 193.0 RIGHT AND LEFT SIDES CRACKED. FOUND DURING C CHECK INSPECTION. HFEC INSPECTION CARRIED OUT ON CUTOUT REPAIR EDGE AND AREA AS REQUIRED IAW REO 601R-53-11-245. NO CRACKS FOUND. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-11-245 REV. ''NC''. REINSTALLED ADG PUMP IAW CRJ AMM 24-23-19-401-801. 2 L 7 2 4F RT A21EA 2002121200114 20021212 00114 EA 2002 12 12 SWIA200211520 1 20021014 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 411SW 7067 FS 280 PILOT'S BULKHEAD RBL AND LBL 9.0 AFT UPPER FLOORBEAM CRACKED. FOUND DURING C CHECK INSPECTION.HFEC INSPECTION CARRIED OUT ON CUTOUT REPAIR AS REQUESTED IAW RJ NDTM 51-20-06. NO CRACKS FOUND. REPAIRED DAMAGED AREA IAW CRJ REO 601 R-53-11-137 REV. ''NC''. 2 L 7 2 4F RT A21EA 2002121200115 20021212 00115 EA 2002 12 12 SWIA200211522 1 20021124 A 3620 OVERHEAT SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT WING MALFUNCTIONED A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 916SW 7634 ABORTED THE TAKEOFF DUE TO AN ''ANTI-ICE DUCT'' WARNING MESSAGE. THE SYNOPTIC PAGE WARNING WAS FOR THE RT WING LEADING EDGE. REPLACED ALL 21 RT WING OVERHEAT SENSORS IAW CRJ MM 30-12-12. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002121200116 20021212 00116 SO 2002 12 12 SWIA200211523 1 20021113 A 7722 SELOC19EG INDICATOR EMB 120 EMB120ER 3260203 SO LT ENGINE ERRATIC A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 188SW 5855 5855 120039 ERRATIC T6 INDICATIONS, FLUCTUATING AS MUCH AS 100 PERCENT, ON THE LT ENGINE. ALL OTHER GAUGES REMAINED NORMAL. NO SUR GING OF ENGINE HEARD OF FELT. REPLACED NR 1 T6 INDICATOR. RAN ENGINE. ALL INDICATIONS NORMAL. 2 L 7 2 4T RT A31SO 2002121200117 20021212 00117 EA 2002 12 12 SWIA200211524 1 20021125 A 2740 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 591SW 7079 ON DEPARTURE FROM DFW THE CAPTAIN'S STAB TRIM WOULD NOT TRIM NOSE UP. NO ASSOCIATED STAB TRIM MESSAGES NOTED. REMOVED AND REPLACED CAPTAIN'S PITCH TRIM SWITCH WITH SERVICEABLE UNIT IAW MM 27-41-05. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2002121200118 20021212 00118 EA 2002 12 12 SWIA200211525 1 20021127 A 5245 DOOR CNDAIR CL600 CL6002B19 1900309 EA EXTERNAL COMM OPEN A SWIA A UNSCHED LANDING W E INADEQUATE Q C VIBRATION/BUFFET CL CLIMB 1 NM 07 427SW 7497 NOSE ELECTRICAL/COMMUNICATIONS EXTERNAL DOOR WAS NOT SHUT PROPERLY. RETURNED TO PHX. SECURED DOOR AND INSPECTED FOR DA MAGE. NO DAMAGE FOUND. 2 L 7 2 4F RT A21EA 2002121200119 20021212 00119 NM 2002 12 12 PCAA0212147 1 20021211 A 5610 07802 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM CAPTAINS CRACKED A PCAA K NONE Z SIGNIFICANT FAILURE REPORT NR NOT REPORTED 1 EA 13 844EX 10579 339 LGA- FLIGHT#3877. CREW REPORTED CAPTAINS WINDSHIELD WAS CRACKED AT THE LOWER LEFT CORNER. MAINTENANCE REPLACED CAPTAINS WINDSHIELD IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 56-10-11 AND ALLEGHENY AIRLINES JOBCARD#330. AIRCRAF T WAS GROUND RAN TO TEST WINDSHIELD HEAT SYSTEM. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002121200120 20021212 00120 EA 2002 12 12 SWIA200211526 1 20021127 A 2760 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA NR GND SPOILER MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 408SW 5007 5007 7055 AFTER PUSHBACK RECEIVED AN INBOARD & OUTBOARD GROUND SPOILER FAULT MESSAGE. REMOVED AND REPLACED NR 2 SECU IAW MM 27-6 1-04. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002121200121 20021212 00121 2002 12 12 SWAA022831 4 20021127 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING DOOR. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002121200122 20021212 00122 NM 2002 12 12 SWAA022832 1 20021130 A 3211 654611324 PIN BOEING 737 7373H4 1384600 NM LT MLG TRUNNION CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG STRUT AND TRUNNION PIN CORRODED. REMOVED AND REPLACED LT MLG STRUT AND TRU NNION PIN PER MM. 2 L 7 2 4F RT A16WE 2002121200123 20021212 00123 NM 2002 12 12 SWAA022837 1 20021202 A 3350 57771 CAP BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 103SW 23109 DURING SCHEDULED C2 CHECK, FOUND EEPLS END CAP MISSING AT AFT CABIN. INSTALLED EEPLS END CAP PER MM. 2 L 7 2 4F A16WE 2002121200124 20021212 00124 NM 2002 12 12 SWAA022838 1 20021201 A 2560 PH22300L STRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROWS NR 7 AND NR 8 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2002121200125 20021212 00125 NM 2002 12 12 SWAA022840 1 20021204 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 EEPLS LENS MISSING AT ROW NR 2. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2002121200126 20021212 00126 NM 2002 12 12 SWAA022843 1 20021203 A 3350 6104781 CHARGER BOEING 737 7373T5 1384608 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED C1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY CHAR GER AND BATTERY PER MM. 2 L 7 2 4F RT A16WE 2002121200127 20021212 00127 NM 2002 12 12 SWAA022845 1 20021203 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED C2 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED IN CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2002121200128 20021212 00128 NM 2002 12 12 DHL2002754004 1 20021212 A 3240 26045611 TIRE BOEING 727 727223 1384074 NM A DHLA K O NONE OTHER E O VIBRATION/BUFFET OTHER TO TAKEOFF 1 SO 01 754DH 22008 1) NOTED EXCESSIVE VIBRATION ON TAKE-OFF AND LANDING. STRONG RUBBER SMELL NOTED AFTER GEAR RETRACTION.2) FOUND LARGE F LAT SPOT ON #2 TIRE. REMOVED AND REPLACED #2 MLG TIRE IAW DHL M/M 32-45-01. RETORQUED #3 AND #4 MLG TIRES IAW DHL M/M 32 -45-01. 2 L 7 3 4F A3WE 2002121200129 20021212 00129 WP 2002 12 12 AALA20021557 1 20021022 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 573AA 53092 TUL - FOUND CORROSION ON NR 6 SEAT TRACK, STATION 216-218. REPLACED SEAT TRACK NR 6 SECTION FROM STATION 216-305 PER SR M 53-05-00. (M) 2 L 7 2 4F A6WE 2002121200130 20021212 00130 WP 2002 12 12 AALA20021617 1 20021106 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 483AA 49676 TUL - FOUND .25 INCH CRACK IN OUTBOARD END OF RIGHT WHEEL WELL AFT LANDING. ROUTED OUT DAMAGE AND INSTALLED REPAIR ANGL ES PER SRM 53-01-00 FIG 2. AREA DYE-CHECKED, NO INDICATION OF CRACK FOUND. (M) 2 L 7 2 4F A6WE 2002121200131 20021212 00131 WP 2002 12 12 AALA20021618 1 20021107 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 483AA 49676 TUL - FOUND LEFT AFT FUSELAGE SKIN CRACKED AT FASTENER HOLE, STATION 1380, LONGERON 12L. DAMAGE REMOVED, DOUBLER INSTAL LED PER AARD 53-30-00-02. (M) 2 L 7 2 4F A6WE 2002121200132 20021212 00132 WP 2002 12 12 AALA20021619 1 20021107 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 483AA 49676 TUL - FOUND FORWARD CARGO LOWER FRAME HORIZONTAL FLANGE CORRODED AT MAIN DOOR CUTOUT. REMOVED CORROSION. CUT OUT DAMAG ED AREA. INSTALLED FILLER AND INTERIM REPAIR DOUBLER PER ESO 80559, DATED 11-07-02. (M) 2 L 7 2 4F A6WE 2002121200133 20021212 00133 WP 2002 12 12 AALA20021630 1 20021101 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 451AA 49477 TUL - FOUND FRAME WORN STATION 1418 AT LONGERON 20R. REMOVED DAMAGE. INSTALLED DOUBLER PER AARD 53-10-00-14. (M) 2 L 7 2 4F A6WE 2002121200134 20021212 00134 NM 2002 12 12 QXEA0202037 1 20021128 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM NACELLE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - SMOKING RIVET APPROXIMATELY 2 INCHES FORWARD OF INBOARD CORNER OF FORWARD GEAR DOOR. REPAIRED IAW DHC-8 SRM 51-20- 51. 2 H 7 2 4T RT A13NM 2002121200135 20021212 00135 NM 2002 12 12 QXEA0202038 1 20021128 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM NACELLE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - NUMEROUS SMOKING RIVETS BELOW RIGHT HAND OIL COOLER. INBOARD AND OUTBOARD SIDES. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2002121200136 20021212 00136 NM 2002 12 12 QXEA0202039 1 20021129 A 5720 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT WING FRONT SPAR LEADING EDGE SUPPORT BRACKET CRACKED. LONG BRACKET FOR 611AR NEAR NACELLE. REPLACED IAW RD 8-57-078. 2 H 7 2 4T RT A13NM 2002121200137 20021212 00137 NM 2002 12 12 QXEA0202040 1 20021129 A 5720 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT WING UPPER FRONT SPAR LEADING EDGE 611AR SUPPORT BRACKET NEAR NACELLE CRACKED. REPAIRED IAW RD 8-57-078. 2 H 7 2 4T RT A13NM 2002121200138 20021212 00138 NM 2002 12 12 QXEA0202041 1 20021130 A 7110 PLATE DHAV DHC8 DHC8202 2809007 NM RT COWLING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT HAND ENGINE LOWER COWL, LEFT HAND FORWARD BUTT PLATE CHAFED AROUND THE CIRCUMFERENCE OF OPENING IN PLATE. R EPAIRED IAW RD 8-71-170 AND RD 8-71-030. 2 H 7 2 4T RT A13NM 2002121200139 20021212 00139 NM 2002 12 12 QXEA0202042 1 20021130 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - MAIN CABIN DOOR THRESHOLD ANGLE IS CORRODED AT FIVE EACH NUT PLATES. REPAIRED IAW DHC-8 200 SRM 51-40-11, PAGES 1 THROUGH 4. 2 H 7 2 4T RT A13NM 2002121200140 20021212 00140 NM 2002 12 12 QXEA0202043 1 20021130 A 5320 FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - MAIN CABIN DOOR THRESHOLD AFT CORNER FITTING HAS CORROSION AT ONE NUTPLATE. REPAIRED IAW DHC-8 200 SRM 51-40-11, PAGES 1 THROUGH 4. 2 H 7 2 4T RT A13NM 2002121200141 20021212 00141 NM 2002 12 12 QXEA0202088 1 20021202 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - CORROSION VISIBLE AT MAIN CABIN DOOR THRESHOLD ON UPPER SURFACE OF LOWER SILL. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002121200142 20021212 00142 NM 2002 12 12 QXEA0202089 1 20021203 A 5753 BEAM DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT HAND NR 4 FLAP BEAM, INBOARD TRACK E HAS A .075 INCH DIAMETER PIT AT O POSITION. REPAIRED IAW HORIZON AIR E A 2-57-210. 2 H 7 2 4T RT A13NM 2002121200143 20021212 00143 NM 2002 12 12 QXEA0202090 1 20021203 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - FRAME CHAFED, CARGO BAY RIGHT HAND WHERE CONTACTS WITH 251EZ, LOWER OUTBOARD CORNER. REPAIRED IAW DHC-8 SRM 51-20 -26, PAGE 7, PARAGRAPH 5A(4). 2 H 7 2 4T RT A13NM 2002121200144 20021212 00144 NM 2002 12 12 QXEA0202091 1 20021203 A 5320 STRAP DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT HAND AT CARGO FLOOR BOARD LEVEL, FRAME REINFORCING STRAP IS CHAFED. REPAIRED IAW DHC-8 SRM 51-20-26, PAGE 7 , PARAGRAPH 5A(4). 2 H 7 2 4T RT A13NM 2002121200145 20021212 00145 NM 2002 12 12 QXEA0202092 1 20021202 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - NR 1 NACELLE FIREWALL HAS A CRACK IN CLOSING ANGLE ON INBOARD SIDE OF FIREWALL APPROXIMATELY VERTICAL STATION 171. 90. REPAIRED IAW DHC-8 200 RD 8-54-109. 2 H 7 2 4T RT A13NM 2002121200146 20021212 00146 NM 2002 12 12 QXEA0202093 1 20021204 A 5320 DEFLECTOR DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT HAND INBOARD SEAT TRACK AT STATION X352.5 DRIP DEFLECTOR IS DAMAGED. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, PARAGRAPH B(2). 2 H 7 2 4T RT A13NM 2002121200147 20021212 00147 NM 2002 12 12 CALA0200580 1 20021210 A 5320 WEB BOEING 737 7373T0 1384582 NM AFT BAG BIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND UPPER SURFACE OF AFT BAGGAGE BIN LOWER THRESHOLD WEB CORRODED. THE THRESHOLD WEB WAS REMOVED AND REPLAC ED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2002121200148 20021212 00148 WP 2002 12 12 CALA0200581 1 20021211 A 3350 60030451 BATTERY PACK GRIMES DOUG DC9 DC982 3022082 WP STA 1338R INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 49635 THE TAILCONE SLIDE EMERGENCY LIGHTS WOULD NOT TEST. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00. 2 L 7 2 4F A6WE 2002121200149 20021212 00149 NM 2002 12 12 CALA0200582 1 20021211 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 727A CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77303 23354 INSPECTION FOUND A 1.5" CRACK IN R/H FUSELAGE SKIN AT STA 727A JUST FORWARD AND BELOW EMERGENCY LIGHT AND AFT OF WHEEL W ELL. A DOUBLER WAS INSTALLED IAW ECRA 5330-03090. 2 L 7 2 4F RT A16WE 2002121200150 20021212 00150 WP 2002 12 12 CALA0200583 1 20021211 A 5350 CABLE DOUG DC9 DC982 3022082 WP TAILCONE FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72830 49490 THE TAILCONE RELEASE AT EXTERIOR AND INTERIOR HANDLES PULLED HIGH. THE UPPER L/H TAILCONE JETTISON CABLE WAS FOUND WORN AND FRAYED AT UPPER FORWARD PULLEY. REMOVED AND REPLACED CABLE ASSEMBLY. RIGGED AND ADJUSTED TAILCONE RELEASE SYSTEM IAW MM 53-53-00. 2 L 7 2 4F A6WE 2002121200151 20021212 00151 NM 2002 12 12 AWXA200201188 1 20021127 A 5320 69353656 ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 0 0 23777 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1/2" CRACK WAS FOUND ON VERTICAL WEB ANGLE PROTRUDING FROM SCREW HOLE, BS 390, BL 0, WL 208.5. MAINTENANCE REMOVED CRACKED VERTICAL WEB ANGLE AT BS 390, BL 0, WL 208.5; FABRICATED A NEW REPLACEMENT V ERTICAL WEB ANGLE; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 2-4. 2 L 7 2 4F RT A16WE 2002121200152 20021212 00152 NM 2002 12 12 AWXA200201191 1 20021207 A 5313 69353521 TIE CLIP BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 0 0 23777 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1/4" CRACK WAS FOUND ON STRINGER TIE CLIP ON FORWARD SIDE OF BS 847, STR 25 L/H . MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT BS 847, STR 25 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; I NSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 38, FIG. 8, AND PG. 6-8, & 45, FIG 12 SHT 2. 2 L 7 2 4F RT A16WE 2002121200153 20021212 00153 NM 2002 12 12 AWXA200201192 1 20021126 A 5330 659187911 SKIN PANEL BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 0 0 23777 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1/2" CRACK WAS FOUND ON LOWER KEEL BEAM EXTERNAL SKIN AT OUTBOARD EDGE IN THE M IDDLE OF WHEEL WELL BS 690, RBL 6. MAINTENANCE REMOVED DAMAGED LOWER KEEL BEAM EXTERNAL SKIN AT OUTBOARD EDGE IN THE MID DLE OF WHEEL WELL BS 690, RBL 6; FABRICATED A NEW REPLACEMENT KEEL BEAM SKIN AND 2 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5310-02085-JS1. 2 L 7 2 4F RT A16WE 2003011700035 20030117 00035 WP 2003 1 17 ARWA20021204 1 20021211 A 3260 7000010101 LIMIT SWITCH DOUG DC8 DC862 3021970 WP NLG FAULTY A ARWA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 19 8968U 46069 ON UPLATCH CHECK RED DOORS LIGHT ILLUMINATED. FOUND NOSE LANDING GEAR DOWN LIMIT SWITCH FAULTY. REMOVED AND REPLACED L IMIT SWITCH IAW MM 32-60-0. ALL CONDITIONS ARE MET UNDER PARAGRAPH 1, ITEM B ON PAGE 201; SYSTEM OPERATIONS CHECK NORMA L ON GROUND IAW MM 32-60-0. ALSO LUBRICATED MAIN LANDING GEAR DOOR AND UP-LATCH MECHANISM AND NOSE LANDING GEAR DOOR & UP-LATCH MECHANISM IAW MM 12-81-1. 2 L 7 4 4F 4A25 2002121200154 20021212 00154 NE 2002 12 12 RAIA00212344 2 20021205 A 7200 PW124 ENGINE AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE LEAKING A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 723TE 20909 283 12441 5532-STL- ELECTRICAL SMOKE IN COCKPIT. MAINTENANCE REMOVED AND REPLACED #1 ENGINE, LK AND OPS CK OK. 2 H 7 2 4T 4 T RT A53EU E2ONE 2002121200155 20021212 00155 EU 2002 12 12 RAIA00212345 1 20021206 A 2910 14129015133 LINE JETAIR JETSTM JETSTM4101 1500501 EU LEAKING A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 551HK 41040 5514 STL HYDRAULIC PRESSURE WENT TO ZERO. MAINTENANCE REMOVED AND REPLACED HYDRAULIC PUMP PRESSURE LINE. 2 L 7 2 4T RT A41NM 2002121200156 20021212 00156 EU 2002 12 12 RAIA00212346 1 20021209 A 2700 C850176 VANE JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 566HK 11684 4185 41084 5578-STL- RIGHT STALL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED R/H AOA VANE, OPS CK OK. 2 L 7 2 4T RT A41NM 2002121300001 20021213 00001 EA 2002 12 13 SWIA200211527 1 20021128 A 5210 GATE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 408SW 7055 CABIN CLIMBED UNCONTROLLABLY IN AUTO AND MANUAL MODES. RETURNED TO BIL. REPAIRED AND RIGGED THE PASSENGER DOOR GATE I AW CRJ MM TASK 52-11-15-820-801. OPERATIONAL CHECK OF PRESSURE SYSTEM IAW 21-32-00 GOOD. OPS CHECK OF PRESSURE CONTROL SYSTEM IAW CRJ MM TASK 21-31-00-710-801 GOOD. 2 L 7 2 4F RT A21EA 2002121300002 20021213 00002 SO 2002 12 13 SWIA200211528 1 20021126 A 2841 944101 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUEL QTY INACCURATE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 234SW 5945 313 120308 FUEL TOTALIZER INACCURATELY INDICATES FUEL REMAINING AS TWICE THE AMOUNT OF FUEL IN TANKS. REPLACED FUEL TOTALIZER IAW EMB120 MM 28-41-00. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2002121300003 20021213 00003 EA 2002 12 13 SWIA200211529 1 20021130 A 7830 1267587 PDU CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE T/R MALFUNCTIONED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 592SW 2992 2992 7279 DURING FLIGHT AT FL 350 WE RECEIVED AN ''R REV UNLOCK'' MESSAGE. FOLLOWED MEMORY ITEMS AND THEN QRH. ENGINE WAS SHUT D OWN PER QRH. NORMAL SINGLE ENGINE LANDING WAS MADE. REMOVED AND REPLACED PDU IAW MM 78-32-03 AND RIGGED LOWER INBOARD BALLSCREW ACTUATORS IAW MM 78-32-03. OPS GOOD. 2 L 7 2 4F RT A21EA 2002121300004 20021213 00004 SO 2002 12 13 SWIA200211530 1 20021105 A 5347 SCREW EMB 120 EMB120ER 3260203 SO SEAT TRACKS CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 FLOOR SEAT TRACKS HAVE CORROSION ON 90 PERCENT OF SCREW HEADS. FOUND DURING C CHECK INSPECTION. REPLACED RT AND LT FLO OR SEAT TRACKS AND ATTACHING HARDWARE IAW EMB MM 53-01-05. 2 L 7 2 4T RT A31SO 2002121300005 20021213 00005 SO 2002 12 13 SWIA200211531 1 20021105 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 FLOOR SUPPORT AT STATION 40 AND 41 UNDER CARGO FLOOR CUT ON RT SIDE OF AIRCRAFT IN FRONT AND BEHIND CABLE PULLEYS. REPL ACED RIBS 40 AND 41 IAW 120 SRM 51-10-02. 2 L 7 2 4T RT A31SO 2002121300006 20021213 00006 SO 2002 12 13 SWIA200211532 1 20021105 A 5410 BRACKET EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 RT NACELLE HYDRAULIC RESERVOIR AREA, CRACKED BRACKET JUST AFT OF HYDRAULIC RETURN FILLER PORT. FOUND DURING "C" CHECK I NSPECTION. REPLACED BRACKET IAW 120 SRM 51-10-02. 2 L 7 2 4T RT A31SO 2002121300007 20021213 00007 SO 2002 12 13 SWIA200211533 1 20021105 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 LT ENGINE NACELLE FRAME NR 1 CRACKED. FOUND DURING "C" CHECK INSPECTION. INSTALLED NEW FRAME NR 1 IAW SB 120-54-0036. 2 L 7 2 4T RT A31SO 2002121300008 20021213 00008 SO 2002 12 13 SWIA200211534 1 20021105 A 2897 WIRE HARNESS EMB 120 EMB120ER 3260203 SO LT WING CHAFED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 LT WING WIRE HARNESS CHAFED ON FUEL LINE THAT GOES TO VENT VALVE. FOUND DURING "C" CHECK INSPECTION. REMOVED AND REPLA CED LT WING WIRE HARNESS WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002121300009 20021213 00009 SO 2002 12 13 SWIA200211535 1 20021201 A 2932 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO HYD SYSTEM MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 301YV 120301 LT HYDRAULIC RESERVOIR LOW PRESSURE LIGHT ILLUMINATED DURING TAKEOFF. ABORTED THE TAKEOFF. REMOVED & REPLACED LT HYDR AULIC RESERVOIR LOW PRESSURE SWITCH. OPS CHECK GOOD. NO LEAKS NOTED. PN OFF 120-48659-001 SN OFF 0134. 2 L 7 2 4T RT A31SO 2002121300010 20021213 00010 2002 12 13 SWIA200211536 4 20021130 A 3454 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA ADI MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 437SW 7564 SHORTLY AFTER DEPARTURE WHEN SWITCHING NAV 2, RECEIVED DASHED LINES ON THE ADI. COULD NOT INPUT FREQUENCY. RETURNED T O SLC. CYCLED POWER WITH CB2H-9. FREQUENCY RETURNED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2002121300011 20021213 00011 EA 2002 12 13 SWIA200211537 1 20021203 A 3233 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 587SW 7062 UPON GEAR RETRACTION AFTER TAKEOFF, ''GEAR DISAGREEMENT'' AND ''NOSE DOOR'' WARNINGS ILLUMINATED. RETURNED TO FAT. ALS O ''WOW INPUT'' , ''NOSE WHEEL STEERING'' CAUTIONS ILLUMINATED AND ''WOW OUTPUT FAIL'' STATUS ILLUMINATED. ''NWS'' CAUT ION EXTINGUISHED UPON CYCLING. REPLACED NLG PRIORITY VALVE IAW RJ MM 32-33-15. ALL LEAK CHECKS AND GEAR SWINGS CHECK GO OD. SYSTEM 3A & 3B LEAK DOWN CHECKS GOOD IAW 29-10-00. RETRACTION TIME CHECK GOOD IAW 32-30-00. PN OFF 4622. 2 L 7 2 4F 4 F RT A21EA E15NE 2002121300012 20021213 00012 2002 12 13 SWIA200211538 4 20021202 A 3422 DETECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 405SW 7029 CAPTAIN'S HEADING 5-10 DEGREES OFF FROM COMPASS AND FIRST OFFICER'S. RECEIVED SEVERAL EFIS COMP MON CAUTION MESSAGES. PERFORMED QRH PROCEDURE AND RETURNED TO SLC. REMOVED AND REPLACED LT FLUX DETECTOR UNIT IAW MM 34-21-04. DEGAUSSED WIN GS AND LANDING GEAR. OPS CHECK OF HEADING SYSTEM GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2002121300013 20021213 00013 NE 2002 12 13 SWIA200211539 2 20021203 A 7261 OIL SYSTEM EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE NR 2 ENGINE LOW A SWIA C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 NM 07 297SW 120327 ''OIL PRESSURE NR 2'' MESSAGE ILLUMINATED ON TAKEOFF ROLL AT APPROXIMATELY 60-70 KTS. ABORTED TAKEOFF. OIL PRESSURE GA UGE INDICATION WAS WITHIN NORMAL RANGE. ADDED 2 QUARTS OF OIL TO THE RT ENGINE. RAN ENGINE AT 100 PERCENT TORQUE. NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2003021000008 20030210 00008 EU 2003 2 10 DHL2002367010 1 20021129 A 3240 C200601004 BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU MLG SEIZED A DHLA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 367DH 265 DURING NORMAL TAXI, WITHOUT TOUCHING THE BRAKES, AIRCRAFT ABRUPTLY CAME TO A HALT WHILE PULLING TO THE RT. AIRCRAFT WOUL D NOT MOVE AFTERWARDS. REMOVED AND REPLACED NR 4 BRAKE ASSEMBLY IAW A300 MM 32-42-27. REMOVED AND REPLACED NR 3 AND 4 W HEEL ASSEMBLIES IAW A300 MM 12-37-32. LEAK AND OPERATIONAL CHECK SERVICEABLE. 2 L 7 2 4F RT A35EU 2002121300015 20021213 00015 NM 2002 12 13 AWXA200201140 1 20021028 A 5754 65C26603138 WEDGE BOEING 737 73733A 1384673 NM GE CFM56 CFM56* 13802 NE LE SLAT DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MAJOR REPAIR DURING C-19 CHECK, NR 4 LEADING EDGE SLAT INBOARD WEDGE WAS FOUND TO BE DELAMINATED. MAINTENANCE REMOVED A ND REPLACED THE NR 4 LEADING EDGE SLAT IAW BMM. OPERATIONAL CHECK ACCOMPLISHED IAW BMM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121300016 20021213 00016 NM 2002 12 13 AWXA200201141 1 20021028 A 5754 65C26602218 SKIN BOEING 737 73733A 1384673 NM LE SLAT DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 DURING C-19 CHECK THE NR 5 LEADING EDGE SLAT AT THE INBOARD AND OUTBOARD ENDS OF WEDGE WAS FOUND TO BE DELAMINATED. MAIN TENANCE REMOVED DAMAGED AREA OF SKIN ON THE NR 5 LEADING EDGE SLAT AT THE INBOARD AND OUTBOARD END OF WEDGE. APPLIED ADH ESIVE, REPLACEMENT SKIN, AND DOUBLERS IAW SRM. 2 L 7 2 4F RT A16WE 2002121300017 20021213 00017 NM 2002 12 13 AWXA200201144 1 20021028 A 5753 6546435278 SKIN BOEING 737 73733A 1384673 NM RT TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 YVR - MAJOR REPAIR - DURING C-19 CHECK THE RT OUTBOARD FLAP WAS FOUND DELAMINATED AT THE INBOARD AFT CORNER. MAINTENANCE REMOVED AND REPLACED THE RT OUTBOARD FLAP IAW AWA T/C R8M27002. 2 L 7 2 4F RT A16WE 2002121300018 20021213 00018 EU 2002 12 13 AWXA200201145 1 20021121 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU ZONE 241 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 7400 55 SEA - EEL - DURING INSPECTION, THE EMERGENCY ESCAPE LIGHT SYSTEM TEST FAILED AT PROGRAMMING AND TEST PANEL. MAINTENANCE REMOVED AND REPLACED THE LT OVER WING EMERGENCY POWER SUPPLY UNIT (11WL); OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002121300019 20021213 00019 EU 2002 12 13 AWXA200201147 1 20021121 A 2121 EVT3454H FAN AIRBUS 320 A320232 3930326 EU CABIN FAILED A AWXA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 604AW 8545 1196 ABQ - DIVERSION - FLT 0612 - EN ROUTE FROM PHX TO ATL **SUPP** ADDITIONAL INFORMATION ** RECEIVED AN EXTRACT FAN FAULT F OLLOWED BY A STRONG ELECTRICAL ODOR IN THE COCKPIT. DEACTIVATED SYSTEM PER ECAM INSTRUCTIONS AND ODOR DISSIPATED; DIVERT ED TO ABQ AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE ISSUED MEL 21-26-02 COND. 1 "EXTRACT FAN INOP". WHEN AIRCRAFT AR RIVED IN PHX EXTRACT FAN WAS REPLACED IAW AMM 21-26-51; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002121300020 20021213 00020 NM 2002 12 13 AWXA200201148 1 20021124 A 2560 P4010021 BATTERY BOEING 757 7572S7 1384962 NM ZONE 900 - LAV DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 905AW 23567 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AT L-1 DOOR WAS INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE BATTERIES IN THE EMERGENCY FLASHLIGHT AT THE L-1 DOOR, FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2002121300021 20021213 00021 NM 2002 12 13 AWXA200201149 1 20021122 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM ZONE 900 - LAV DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 154AW 23776 LAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE BATTERIES IN THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002121300022 20021213 00022 EU 2002 12 13 AWXA200201150 1 20021124 A 2820 VENT AIRBUS 320 A320231 3930325 EU FUEL SYSTEM LEAKING A AWXA C ABORTED TAKEOFF K FLUID LOSS TO TAKEOFF 1 WP 28 643AW 315 PHX - ABORTED TAKEOFF - FLT 0881 - ON TAKEOFF AT PHX EN ROUTE TO FLL FUEL WAS OBSERVED COMING OUT FROM BELOW RT WING, RE JECTED TAKEOFF AT LOW SPEED. MAINTENANCE FOUND FUEL COMING FROM RT FUEL VENT, TROUBLESHOT FUEL SYSTEM AND FOUND NO DEFEC TS. CLEANED FUEL FROM LOWER OUTBOARD WING AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A28NM 2003012200103 20030122 00103 2003 1 22 AWXA200201151 4 20021124 A 3460 1714970501 FMC BOEING 737 7373G7 1384595 NM COCKPIT MALFUNCTIONED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 306AW 24633 PHX - ABORTED TAKEOFF - FLT 0341 - ON TAKEOFF FROM PHX EN ROUTE TO LAS THE FLIGHT MANAGEMENT COMPUTER FAILED AT 90 KTS, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE FLIGHT MANAGEMENT COMPUTER IAW BMM 34-62-21 -401 REV 3, NAV DATA DOWNLOAD ACCOMPLISHED IAW T/C A1B34060. VENDOR BENCH TEST RESULTS FOR FLIGHT MANAGEMENT COMPUTER F AILED INCOMING TEST DUE TO THE UNIT TIMED OUT. REPAIR ACTION STATES TESTED EXTENSIVELY WITH NO FAULT FOUND. INFORMATIO N HAS BEEN PROVIDED TO CHRONIC COMPONENT PROGRAM AND WARRANTEES. 2 L 7 2 4F RT A16WE 2003012200106 20030122 00106 EU 2003 1 22 AWXA200201152 1 20021123 A 2932 501310000 PRESSURE SWITCH AIRBUS 320 A320232 3930326 EU NR 1 ENGINE FAILED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 639AW 29987 2539 471 ON CLIMBOUT, RECEIVED ECAM WARNING FOR GREEN HYD SYS NR 1 ENGINE LOW PRESSURE AND FLUID QUANTITY. TURNED BACK TO PHX AN D LANDED, TAXIED BACK TO GATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE (GREEN HYD SYS) ENGINE DRIVEN PUMP IAW AMM 29-11-51-000-010, LEAK CHECK WAS GOOD, BUT OPERATIONAL CHECK INDICATED FAULTS TQ 0085 AND TQ 0894. REMOVED AND REPL ACED HYD PRESSURE SWITCH (1074GK), LEAK AND OPERATIONAL CHECK WERE GOOD IAW AMM 29-11-17. VENDOR BENCH TEST OF ENGINE D RIVEN HYD PUMP COULD NOT CONFIRM FAILURE. UNIT PASSED TO SPECIFICATIONS AS RECEIVED, PRESSURE SET AT 3025 PSI PER CMM 2 9-11-33. 2 L 7 2 4F RT A28NM 2002121300023 20021213 00023 NM 2002 12 13 AWXA200201155 1 20021130 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM SEAT ROW 13 LT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 309AW 24711 SNA - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002121300024 20021213 00024 NM 2002 12 13 AWXA200201156 1 20021201 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM ZONE 263 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 806AW 12599 1056 PHX - EEL - DURING EMERGENCY LIGHT TEST THE LT AFT EMERGENCY POWER SUPPLY UNIT FAILED CIDS BITE CHECK. MAINTENANCE REMOV ED AND REPLACED THE LT AFT EMERGENCY POWER SUPPLY UNIT (13WL) IAW AMM 33-51-38-401, FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002121300025 20021213 00025 NM 2002 12 13 AWXA200201157 1 20021130 A 7711 ENGINE BOEING 737 737277 1384570 NM NR 2 EPR OUT OF ADJUST A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 179AW 22646 TUS - ABORTED TAKEOFF - FLT 0448 - ON TAKEOFF FROM TUS EN ROUTE TO PHX AT APPROXIMATELY 70 KIAS WITH THE NR 1 ENGINE IND ICATED NORMAL EPR AT 1.99, NR 2 ENGINE INDICATED LOW EPR AT APPROXIMATELY 1.45. NR 1 ENGINE N1 WAS 94 PERCENT, NR 2 ENGI NE N1 APPROXIMATELY 84 PERCENT. ADVANCED NR 2 ENGINE THRUST LEVER SLIGHTLY WITH NO CHANGE IN EPR OR N1. ABORTED TAKEOFF, DID NOT OBSERVE EGT, N2, OR FUEL FLOW ON NR 2 ENGINE PRIOR TO REJECTION. MAINTENANCE ADJUSTED EPR SETTINGS IAW BMM 71-0 9-236, HG AT 29.4, TEMPERATURE AT 13C, EPR SETTINGS 2.14 ALL PARAMETERS EQUAL. PERFORMED ACCELERATION TEST IAW BMM 71-09 -200 EPR WAS REACHED IN 3 SECONDS ON BOTH ENGINES. EGT, N1, N2 , AND FUEL FLOW ALL OPERATED NORMALLY. 2 L 7 2 4F RT A16WE 2002121300026 20021213 00026 NM 2002 12 13 AWXA200201158 1 20021130 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM SEAT ROW 17 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 326AW 23258 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT WAS BROKEN. MAINTENANCE REMOVED AND R EPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2003012200107 20030122 00107 NM 2003 1 22 AWXA200201161 1 20021202 A 5270 189915 PROXIMITY SENSOR BOEING 737 73733A 1384673 NM PAX DOOR FAULTY A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 168AW 23629 DURING CLIMBOUT AT 5000 FT FORWARD ENTRY DOOR WARNING LIGHT ILLUMINATED. FORWARD ENTRY DOOR HANDLE WAS SECURE. TURNBAC K TO LAS. MX ADJUSTED L-1 DOOR SENSOR. ACFT WAS PRESSURIZED TO 4 PSI, NO FAULTS WERE NOTED. DURING PRESSURIZATION SHO OK HANDLE, LIGHT REMAINED EXTINGUISHED. PROBLEM RETURNED NEXT FLT, LIGHT REMAINED ON DURING TAXI TO GATE. THE L-1 DOOR UPPER HINGE GUIDE ARM WAS ADJUSTED AND LIGHT EXTINGUISHED AND REMAINED OFF; LIGHT ILLUMINATED ONCE MORE AS ACFT TAXIED TO GATE ON RETURN FLIGHT TO LAS. TROUBLESHOT TO INTERMITTENT WIRING PROBLEM, PLACED ON MEL 52-03-19, COND 1. MX REMOVE D & REPLACED L-1 DOOR INDICATION SENSOR S199, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2002121300027 20021213 00027 NM 2002 12 13 AWXA200201162 1 20021203 A 4930 38848641 CHECK VALVE AIRBUS A319 A319132 3930340 NM ZONE 315 BYPASSING A AWXA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 WP 28 802AW 924 SNA - APU TAIL PIPE FIRE - APU FIRE REPORTED BY GROUND PERSONNEL, APU FIRE EXTINGUISHER WAS DISCHARGED. MAINTENANCE VISU ALLY INSPECTED THE APU COMPARTMENT, TAIL PIPE, AND SURROUNDING AREA, NO DAMAGE WAS NOTED. SYSTEM WAS PLACED ON MEL 26-22 -00, COND. 1 (APU FIRE EXTINGUISHER SYSTEM INOPERATIVE). WHEN AIRCRAFT ARRIVED IN PHX THE TURBINE VENT CHECK VALVE WAS REPLACED PER TSM 49-00-00-810-851, AND FIRE EXTINGUISHER BOTTLE WAS REPLACED IAW AWA T/C R6A26301. RAN APU, OPERATIONAL CHECK WAS GOOD WITH NO FIRE OR SMOKE NOTED DURING RUN OR AFTER SHUTDOWN. **SUPP** AFTER FURTHER INVESTIGATION IT WAS FO UND THAT THE PART REPLACED WAS A TURBINE CAVITY CHECK VALVE NOT A TURBINE VENT CHECK VALVE, THE PART LISTED IN SECTION 5 2 L 7 2 4F RT A28NM 2002121300028 20021213 00028 WP 2002 12 13 AALA20021460 1 20021007 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 556AA 53086 TUL - FOUND FUSELAGE SKIN DENTED TWO PLACES AT RIGHT GROUND FLOOD LIGHT STATION 557 LONGERON 21R. REMOVED INTERNAL DAMA GED PARTS AND INSTALLED REPAIRS PER ESO 80559 DATED 10/7/2002. (M) 2 L 7 2 4F A6WE 2003020600141 20030206 00141 NM 2003 2 6 02FDEA00936 1 20021211 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 FOUND CORROSION ON INNER SURFACE OF SKIN BS 965 LBL 17 WL 139. 2 L 7 3 4F RT A3WE 2002121300029 20021213 00029 NM 2002 12 13 02FDEA00937 1 20021211 A 5313 STRINGER BOEING 727 727277 138408S NM PWA JT8 JT8D9 52048 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 FUSELAGE STRINGER 24L HAS DENT DAMAGE AT BS 565. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121300030 20021213 00030 NM 2002 12 13 02FDEA00938 1 20021211 A 5313 STRINGER BOEING 727 727277 138408S NM PWA JT8 JT8D9 52048 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 FOUND CORROSION ON STR 27L BS 965. REPAIRED DAMAGED STRINGER 27L BS 965 PER SRM 53-10-3 FIG 1 2 L 7 3 4F 4 F RT A3WE E2EA 2002121300031 20021213 00031 NM 2002 12 13 02FDEA00939 1 20021211 A 5311 FRAME BOEING 727 727277 138408S NM PWA JT8 JT8D9 52048 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 FUSELAGE FRAME BS 520 UPPER FLANGE HAS SEVERAL DENTS RBL 33-42. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121300032 20021213 00032 NM 2002 12 13 02FDEA00940 1 20021211 A 5313 STRINGER BOEING 727 727277 138408S NM PWA JT8 JT8D9 52048 NE FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 STR 15R AT BS 720B+4 CRACKED. REPAIRED PER SRM 53-10-3 FIG 5. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121300033 20021213 00033 NM 2002 12 13 02FDEA00941 1 20021211 A 5330 SKIN BOEING 727 727277 138408S NM PWA JT8 JT8D9 52048 NE FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 GOUGE IN SKIN BS 1070, STR 25R, WAS FOUND OUT OF LIMITS. REPAIRED SKIN AT BS 1070, STR 25R PER SRM 53-30-3, FIGURE 3. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121300034 20021213 00034 NM 2002 12 13 02FDEA00942 1 20021211 A 8010 65224464 DUCT BOEING 727 727222 1384073 NM PWA JT8 JT8D1 52044 NE NR 3 STARTER BLOWN A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 188FE 19081 AFTER TAKEOFF NR 3 ENGINE HAD FIRE INDICATOR, IAW FLIGHT MANUAL QRM SHUTDOWN ENGINE, FIRELIGHT EXTINGUISHED BY ITSELF A ND TESTED GOOD. NO ABNORMAL ENGINE INDICATIONS WERE NOTED. AFTER ENGINE SHUTDOWN WINDMILLED FOR APPROXIMATELY 10 MIN. NR 3 OIL PRESS APPROX 10 PSI (WINDMILLING). OPENED NR 3 ENGINE COWLING. FOUND SUPPLY DUCT (1ST ELBOW) OFF OF STARTER, BLOWN. REMOVED AND REPLACED THE NR 3 ENGINE STARTER SUPPLY DUCT IAW MM, LEAK CHECK OK. INSPECTION NR 3 ENGINE MAIN OI L STRAINER AND CHIP DETECTORS AS REQUIRED FOR ENGINE WINDMILLING CONDITION IAW MM. NO CONTAMINATION FOUND. REMOVED AND REPLACED NR 3 ENGINE MAIN OIL FILTER IAW MM. 2 L 7 3 4F 4 F A3WE E2EA 2002121300035 20021213 00035 WP 2002 12 13 AALA20021631 1 20021101 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 451AA 49477 TUL - FOUND CORROSION ON NR 2 SEAT TRACK IN SEVERAL PLACES FROM STATION 1240 TO 1309. REPLACED NR 2 SEAT TRACK FROM STA TION 1222 TO 1309 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2002121300036 20021213 00036 WP 2002 12 13 AALA20021632 1 20021030 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 578AA 53155 TUL - FOUND AFT CARGO LOWER DOOR JAMB BEAM HAS HEAVY CORROSION. REMOVED AND REPLACED AFT CARGO DOOR BEAM PER SRM 51-01- 00. (M) 2 L 7 2 4F A6WE 2002121300037 20021213 00037 EU 2002 12 13 AWXA200201163 1 20021205 A 3350 321452 POWER SUPPLY AIRBUS 320 A320231 3930325 EU ZONE 242 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 629AW 29737 076 PHX - EEL - DURING INSPECTION THE EMERGENCY LIGHTING SYSTEM FAILED TEST. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWE R SUPPLY UNITS AND BATTERY PACKS AT RT OVERWING EXIT (12WL), AND LT AFT (13WL) IAW AMM 33-51-38-401, FUNCTIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2002121300038 20021213 00038 WP 2002 12 13 AALA20021633 1 20021028 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 578AA 53155 TUL - FOUND CORROSION ON SEAT TRACK NR 1 AT STATION 1174. INSTALLED NEW SEAT TRACK STATION 1174 TO 1309 PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2002121300039 20021213 00039 WP 2002 12 13 AALA20021634 1 20021029 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 578AA 53155 TUL - FOUND SIDEWALL WEB CRACKED STATION 207 LONGERON 15L. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER AARD 53-10-0 0-11. (M) 2 L 7 2 4F A6WE 2002121300040 20021213 00040 WP 2002 12 13 AALA20021635 1 20021029 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 TUL - FOUND SEVERAL CORRODED AREAS ON LOWER DOOR BEAM. INSTALLED DOUBLER ON DOOR BEAM PER SRM 53-10-00-03. (M) 2 L 7 2 4F A6WE 2002121300041 20021213 00041 WP 2002 12 13 AALA20021636 1 20021029 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 TUL - FOUND CRACKED LONGERON AT FASTENER HOLES, TO RADIUS AND ALONG RADIUS, APPROX .5 INCH BOTH SIDES. PREVIOUS REPAIR NO RADIUS BLOCKS USED, OR SHIMS. APPROXIMATELY 2 FEET OF FORWARD END OF NR 3L LONGERON REMOVED AND NEW PIECE REPLACED W ITH SPLICE AND RADIUS BLOCKS USED AT FRAME ATTACHED POINTS, SRM 53-02-00 FIG 18, SHEET. (M) 2 L 7 2 4F A6WE 2002121300042 20021213 00042 WP 2002 12 13 AALA20021637 1 20021030 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 TUL - FOUND CUSP CRACKED AT EDGE OF 2ND LIGHTENING HOLE FORWARD OF 1309 BULKHEAD LEFT. FOUND CORROSION ALONG CUSP ATTAC H FASTENERS. FOUND CORROSION 4 INCHES FORWARD OF 1309. INSTALLED NEW CUSP LEFT STATION 1250 TO 1309 REF SRM 53-00-00 F IG 97 SHEET 1. (M) 2 L 7 2 4F A6WE 2002121300043 20021213 00043 WP 2002 12 13 AALA20021638 1 20021024 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 TUL - FOUND CORROSION NR 3 SEAT TRACK. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10 REPAIR NR 10. (M) 2 L 7 2 4F A6WE 2002121300044 20021213 00044 WP 2002 12 13 AALA20021639 1 20021024 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 TUL - FOUND NR 3 SEAT TRACK HAS PITTING AT STATION 673. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2002121300045 20021213 00045 WP 2002 12 13 AALA20021640 1 20021028 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 TUL - FOUND CRACK IN RADIUS OF LONGERON, AT AREA OF FASTENER TO FRAME. APPROX 2 FEET REMOVED FORWARD END AND NEW PIECE INSTALLED WITH SPLICE REPAIR. (M) 2 L 7 2 4F A6WE 2002121300046 20021213 00046 WP 2002 12 13 AALA20021642 1 20021105 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 TUL - FOUND FRAME LANDING IS WORN FROM CONTACT WITH APU ACCESS DOOR STATION 1380 AT LONGERON 28L. INSTALLED DOUBLER PER AARD 53-10-00-34. (M) 2 L 7 2 4F A6WE 2002121300047 20021213 00047 2002 12 13 IXXA0200140O 4 20021211 A 3422 1428302001 GYRO DOUG DC8 DC862 3021970 WP FAULTY A IXXA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 SW 11 799AL 45922 AFTER TAKEOFF FROM HIK CREW NOTED #2 "ADI" ATITUDE DIRECTIONAL INDICATOR ROLLING RANDOMLY. AS PRECAUTION CREW ELECTED TO RETURN TO HIK. AFTER AN UNEVENTFUL LANDING. MAINTENANCE TROUBLE SHOT AND REPLACED THE GYRO PER THE ATI DC-8 MAINTENANCE MANUAL AND E.O. 34-DC8-1806 UPON GROUND TEST SYSTEM CHECKED NORMAL AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 4 4F 4A25 2002121300048 20021213 00048 NM 2002 12 13 AWXA200201164 1 20021127 A 5320 651758347 STIFFENER BOEING 737 7373G7 1384595 NM BULKHEAD CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1 INCH CRACK WAS FOUND AT VERTICAL STIFFENER BS 178, LBL 5.7, WL 184. MAINTENAN CE CUTOUT DAMAGE AT VERTICAL STIFFENER BS 178, LBL 5.7, WL 184; FABRICATED 4 EACH REPAIR ANGLES, 2 EACH STRAP, AND 6 EAC H FILLERS; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, PG. 221-240, FIG 205. 2 L 7 2 4F RT A16WE 2002121300049 20021213 00049 WP 2002 12 13 AALA20021643 1 20021112 A 5310 STOP FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 579AA 53156 TUL - FOUND STOP FITTING CRACKED .250 INCH AT STOP ATTACH HOLE. REPLACED STOP FITTING WITH A NEW STOP FITTING. (M) 2 L 7 2 4F A6WE 2002121300050 20021213 00050 NM 2002 12 13 AWXA200201165 1 20021205 A 2930 HYDRAULIC SYSTEM BOEING 737 737277 1384570 NM LOW A AWXA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 WP 28 183AW 22650 AIR TURN BACK - FLT 0624 - SHORTLY AFTER TAKEOFF OBSERVED HYD QTY STARTING TO DROP, QUANTITY CONTINUED TO DROP TO 1.5 GA LLONS. QUANTITY LEVEL WAS JUST ABOVE REFILL LINE PRIOR TO DEPARTURE, TURNED BACK TO OAK AND LANDED WITHOUT FURTHER EVENT . MAINTENANCE IN OAK FOUND NO VISUAL EVIDENCE OF LEAK, SERVICED HYD SYSTEM WITH 1 GALLON OF HYDRAULIC FLUID. OPERATED AL L FLIGHT CONTROL SURFACES AND THRUST REVERSES, NO EVIDENCE OF LEAKAGE NOTED. AS PRECAUTION AIRCRAFT WAS MAINTENANCE FERR IED BACK TO PHX. WHEN AIRCRAFT ARRIVED IN PHX FLUID LEVEL WAS NORMAL, AGAIN ALL FLIGHT CONTROL SURFACES WERE OPERATED WH ILE LOOKING FOR EVIDENCE OF HYDRAULIC LEAK, NO LEAKS WERE NOTED. 2 L 7 2 4F RT A16WE 2002121300051 20021213 00051 WP 2002 12 13 AALA20021647 1 20021105 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 TUL - FOUND FRAME LANDING IS WORN FROM CONTACT WITH APU ACCESS DOOR STATION 1380 AT LONGERON 28R. INSTALLED DOUBLER PER AARD 53-10-00-34. (M) 2 L 7 2 4F A6WE 2002121300052 20021213 00052 EU 2002 12 13 AWXA200201167 1 20021122 A 5411 D5463080900000 ANGLE AIRBUS 320 A320232 3930326 EU NR 2 PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 638AW 455 MAJOR REPAIR - DURING C-06 CHECK A 3/16 INCH CRACK WAS FOUND ON THE NR 2 PYLON OUTBOARD UPPER SPAR ANGLE (WELDED ASSY) I N THE RADIUS BETWEEN RIBS 5 & 6, PYLON STA 5066 R/H. MAINTENANCE REMOVED, WELDED, AND REINSTALLED OUTBOARD UPPER SPAR AN GLE (WELDED ASSY) ON NR 2 PYLON IAW PMS 01-04-36, A320 AMM SUB TASK 54-57-22-020-051, AND SUB TASK 54-57-22-420-052. 2 L 7 2 4F RT A28NM 2002121300053 20021213 00053 NM 2002 12 13 ASA0240174 1 20021104 A 5347 SEAT TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 PAE - DURING CHECKED, FOUND SEAT TRACKS IS DAMAGED AT BS 540 LEFT AND RIGHT BL 25, LEFT AND RIGHT BL 45 AND WL 208. REP AIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002121300054 20021213 00054 NM 2002 12 13 AWXA200201168 1 20021120 A 5512 65C274941 SKIN BOEING 737 7373G7 1384595 NM HORIZONTAL STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MAJOR REPAIR - DURING C-14 CHECK, A 3 1/4 INCH CRACK WAS FOUND ON THE LOWER SURFACE SKIN OF THE LT HORIZONTAL STABILIZE R 82 INCHES OUTBOARD OF THE FUSELAGE AT REAR SPAR, HFEC CONFIRMED. MAINTENANCE STOP DRILLED THE CRACK; FABRICATED AND IN STALLED A REPAIR DOUBLER IAW AWA E.R. 03-5516-02339-ES2. 2 L 7 2 4F RT A16WE 2002121300055 20021213 00055 WP 2002 12 13 ASAA0208547 1 20021110 A 5320 591226911 SILL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 SW 21 975AS 53451 OKC - FOUND 30K CHECK, R1 DOOR SILL PAN FORWARD EDGE IS CRACKED. WELD REPAIRED PAN EDGE PER EA 53-20-01551. (M) 2 L 7 2 4F RT A6WE 2002121300056 20021213 00056 NM 2002 12 13 AWXA200201169 1 20021122 A 5312 6516300 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE NOSE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MAJOR REPAIR - DURING C-14 CHECK, 4 CRACKS WERE FOUND ON FORWARD PRESSURE BULKHEAD BS 178; 3 EACH CRACKS AT WL 212, LBL 5.7, AND 1 EACH CRACK AT WL 212, RBL 5.7. MAINTENANCE CUTOUT STRAPS AT BS 178, WL 212, LBL 5.7, WL 212, RBL 5.7, AND RE MOVED DAMAGED PARTS; FABRICATED A REPAIR DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, P G. 275-286, FIG. 210. 2 L 7 2 4F RT A16WE 2002121300057 20021213 00057 NM 2002 12 13 ASAA0240167 1 20021026 A 5320 65C2630013 ATTACH FITTING BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 756AS 25097 PAE - DURING C-CHECK, FOUND AFT SUPPORT INBOARD ATTACH BRACKET CRACKED. REMOVED AND REPLACE IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002121300058 20021213 00058 NM 2002 12 13 AWXA200201170 1 20021120 A 7110 314A101010 INLET BOEING 737 7373G7 1384595 NM NR 2 ENGINE DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MAJOR REPAIR - DURING C-14 CHECK, THE NR 2 ENGINE INLET WAS FOUND DELAMINATED AT THE 2 O'CLOCK POSITION APPROXIMATELY 2 INCH FORWARD OF THE AFT END. MAINTENANCE TRIMMED OUT DAMAGE; FILLED CORE WITH POTTING COMPOUND; FABRICATED A TAPERED REP AIR FILLER AND FIRE SHIELD; AND INSTALLED REPAIR PARTS IAW AWA ER 03-7111-02339-GF2. 2 L 7 2 4F RT A16WE 2002121300059 20021213 00059 NM 2002 12 13 ASAA0240169 1 20021025 A 5320 65C3379710 RETAINER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 756AS 25097 PAE - DURING C-CHECK, FOUND CORROSION ON RETAINER LEFT MAIN WHEEL WELL. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002121300060 20021213 00060 NM 2002 12 13 ASAA0240170 1 20021025 A 5320 654583469 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 756AS 25097 PAE - DURING C-CHECK, FOUND STRAP IN E/E BAY IS CRACKED .68 INCH. REMOVED AND REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002121300061 20021213 00061 NM 2002 12 13 ASAA0240171 1 20021103 A 5320 65C264594 SPLICE PLATE BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 793AS 28888 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR SPLICE PLATE AT STATION 727F PLUS 6 AND WL 156. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002121300062 20021213 00062 NM 2002 12 13 AWXA200201181 1 20021210 A 2782 830A000004 ACTUATOR AIRBUS A319 A319132 3930340 NM SLATS BINDING A AWXA O OTHER J WARNING INDICATION LD LANDING 1 WP 28 804AW 13066 1049 EMERGENCY LANDING - FLT 0571 - ON LANDING, RECEIVED CLASS 1 SLAT FAULT, EMERGENCY DECLARED, LANDED WITHOUT SLATS. MAINT ENANCE INSPECTED SLAT SYSTEM AND FOUND THE TORQUE LIMITER INDICATOR VISIBLE ON THE NR 2 SLAT ROTARY ACTUATOR. REMOVED AN D REPLACED THE NR 2 SLAT ROTARY ACTUATOR IAW AMM 27-84-49-04, OPERATIONAL CHECK WAS GOOD. VENDORS INSPECTION AND FUNCTI ONAL TEST OF SLAT ROTARY ACTUATOR S/N 17022 WAS NO FAULT FOUND. 2 L 7 2 4F RT A28NM 2002121300063 20021213 00063 NM 2002 12 13 AWXA200201182 1 20021210 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 150AW 23218 EMERGENCY EQUIPMENT - DURING INSPECTION THE EMERGENCY FLASHLIGHT JUST ABOVE THE FORWARD FLIGHT ATTENDANT SEAT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT BATTERY; OPERATI ONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002121300064 20021213 00064 NM 2002 12 13 ASAA0240173 1 20021103 A 5320 65C35767 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 PAE - DURING C-CHECKED, FOUND FORWARD CARGO COMPARTMENT STRINGER CLIP IS CRACKED .25 INCH AT BS 480 AND STRINGER 22L. RE PAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002121300065 20021213 00065 NM 2002 12 13 ASAA0240175 1 20021104 A 5320 BAC14902831 FLOOR SUPPORT BOEING 737 737490 1384715 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 793AS 28888 PAE - DURING C-CHECK, FOUND DAMAGED FLOOR SUPPORTS AT BS 747 TO 817 WL 156 AND LEFT/RIGHT BL 8-12. REPAIRED IAW SRM AND EA. (M) 2 L 7 2 4F RT A16WE 2002121300066 20021213 00066 NM 2002 12 13 AWXA200201183 1 20021211 A 3397 BMS13311122 WIRE BOEING 737 737300 1384610 NM SEAT ROW 21 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 323AW 23684 DURING INSPECTION A BROKEN WIRE WAS FOUND AT THE EMERGENCY ESCAPE PATH LIGHT SEAT ROW 21 LT. MAINTENANCE REPAIRED A BROK EN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 21 LT, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2002121300067 20021213 00067 NM 2002 12 13 AWXA200201184 1 20021211 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM OVERWING EXIT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 DURING INSPECTION THE EMERGENCY EXIT LIGHTS AT LT OVERWING EXIT, L-2 DOOR, AND R-2 DOOR WERE FOUND INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERY PACK (M1051), OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A16WE 2002121300068 20021213 00068 NM 2002 12 13 AWXA200201185 1 20021205 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM SEAT ROW 6 LT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 189AW 22656 DURING C-14 CHECK, THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 6, 8, 10, AND 19 LT WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULBS ON THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 6, 8, 10, AND 19 LT, AND REPLACED THE LIGHT A SSEMBLY AT SEAT ROW 6 LT, OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2002121300069 20021213 00069 NM 2002 12 13 ASAA0240177 1 20021104 A 5320 654963183 SUPPORT ANGLE BOEING 737 737490 1384715 NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 793AS 28888 DURING C-CHECK, FOUND CORROSION ON BULKHEAD SUPPORT ANGLE AT BS 500G WL 156 AND LBL 24. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002121300070 20021213 00070 NM 2002 12 13 ASAA0240178 1 20021105 A 5320 65C264594 SPLICE PLATE BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 793AS 28888 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR SPLICE PLATE STATION 727F PLUS 6 AND WL 156. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002121300071 20021213 00071 NM 2002 12 13 ASAA0240179 1 20021105 A 5320 654961612 ANGLE BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 793AS 28888 PAE - DURING C-CHECK, FOUND CORROSION ON 947 BULKHEAD L-ANGLE. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002121300072 20021213 00072 NM 2002 12 13 AWXA200201186 1 20021206 A 2560 P4010021 BATTERY BOEING 737 737277 1384570 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 189AW 22656 EMERGENCY EQUIPMENT - DURING C-14 CHECK, THE FORWARD FLIGHT ATTENDANT STATION INBOARD EMERGENCY FLASHLIGHT WAS FOUND TO HAVE A WEAK BATTERY. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE INBOARD EMERGENCY FLASHLIGHT AT THE FORWARD FL IGHT ATTENDANT STATION; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002121300073 20021213 00073 NM 2002 12 13 ASAA0240180 1 20021105 A 5320 6547690 SUPPORT BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 793AS 28888 PAE - DURING C-CHECK, FOUND CORROSION ON SIDEWALL SUPPORT AT BS 757-797 AND WL 156. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002121300074 20021213 00074 NM 2002 12 13 ASAA0240181 1 20021105 A 5320 1496377 SUPPORT BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 793AS 28888 PAE - DURING C-CHECK, FOUND CORROSION ON SIDE WALL SUPPORT AT BS 727G AND WL 156. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2002121300075 20021213 00075 EU 2002 12 13 AWXA200201187 1 20021210 A 2781 WARNING SYSTEM AIRBUS 320 A320232 3930326 EU SLAT CONTROL FALSE ACTIVATION A AWXA O OTHER J WARNING INDICATION AP APPROACH 1 WP 28 650AW 856 EMERGENCY LANDING - FLT 0273 - ON APPROACH INTO IAH EN ROUTE FROM PHX SELECTED FLAP 3 WHEN RECEIVED ECAM FLIGHT CONTROL FLAPS FAULT ALONG WITH A FLIGHT CONTROL SLAT FAULT. CONFERRED WITH MAINTENANCE CONTROL AND FOLLOWED ECAM PROCEDURES, REC YCLED FLAPS FROM 2 TO 3; FLAPS OPERATED NORMALLY. EMERGENCY WAS DECLARED; MADE FLAPS 3 LANDING. MAINTENANCE TROUBLESHOT PER TSM 27-51-00-810-851, NO DEFECTS WERE NOTED. 2 L 7 2 4F RT A28NM 2002121300076 20021213 00076 NM 2002 12 13 AWXA200201189 1 20021123 A 5311 651630087 FRAME BOEING 737 7373G7 1384595 NM 178 BULKHEAD CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MAJOR REPAIR - DURING C-14 CHECK A 1/4 INCH CRACK WAS FOUND ON BS 178 RT FRAME AT WL 207, AFT SIDE OF CENTER RADIUS. MAI NTENANCE REMOVED CRACKED RT FRAME BS 178, WL 207, RT FRAME SPLICE, AND RT WEB; FABRICATED A NEW REPLACEMENT RT FRAME. IN STALLED REPAIR PART, AND REINSTALLED RT FRAME SPLICE, AND RT WEB IAW B737-300 SRM 51-40-02, PG. 3-4, 29-30, & 32-36. 2 L 7 2 4F RT A16WE 2002121300077 20021213 00077 NM 2002 12 13 AWXA200201190 1 20021125 A 5414 311A102311 DOUBLER BOEING 737 7373G7 1384595 NM NR 1 PYLON SKIN CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MAJOR REPAIR - DURING C-14 CHECK, A 1/2 INCH CRACK WAS FOUND ON INTERNAL DOUBLER FOR PANEL 5727 LT, NR 1 PYLON. MAINTEN ANCE STOP DRILLED CRACK ON INTERNAL DOUBLER FOR PANEL 5727 LT, NR 1 PYLON; PERFORMED A HFEC INSPECTION TO VERIFY CRACK W AS CONTAINED; FABRICATED A NEW REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA E.R. 03-5433-00340-DL1. 2 L 7 2 4F RT A16WE 2002121300078 20021213 00078 NM 2002 12 13 ASAA0240182 1 20021105 A 5320 FLOOR SUPPORT BOEING 737 737490 1384715 NM FUSELAGE DENTED A K NONE O OTHER IN INSP/MAINT 1 NM 01 793AS 28888 PAE - DURING C-CHECK, FOUND DENT ON FLOOR SUPPORT AT BS 794 AND WL 156. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2003022100001 20030221 00001 2003 2 21 AWXA200201193 4 20021212 A 3417 46657602 CIRCUIT BOARD AIRBUS A319 A319132 3930340 NM ZONE 100 FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 827AW 1547 ON CLIMB FROM LAX EN ROUTE FOR CMH WITH AIR DATA SWITCH IN FIRST OFFICER 3 POSITION; FIRST OFFICERS AIR SPEED INDICATOR RED LINE DECREASED TO APPROXIMATELY 240 KTS. SWITCHED BACK TO AIR DATA NORMAL POSITION AND INDICATIONS WENT BACK TO NORM AL. DUE TO FIRST OFFICERS STATIC HEATER PORT ON MEL, DIVERTED TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE #3 AIR DATA INERTIAL REFERENCE UNIT IAW AWA T/C R2A34304, ALL INTERFACE TESTS WERE GOOD. MAINTENANCE ALSO CLEARED THE MEL FOR F/O'S STATIC PORT HEATER BY REPLACING THE HEAT PROBE COMPUTER IAW AMM 30-31-34-401. VENDOR TEARDOWN OF HEAT PROBE CO MPUTER SN B4988 CONFIRMED FAILURE OF UNIT FINDING DIODE CR09 BURNED OPEN ON THE PRINTED CIRCUIT BOARD. REPLACED PRINTED 2 L 7 2 4F RT A28NM 2002121300079 20021213 00079 WP 2002 12 13 ASAA0280548 1 20021110 A 5730 593746816 SKIN DOUG DC9 DC983 3022083 WP RT WING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - DURING 30K CHECK, FOUND RIGHT WING LOWER LEADING EDGE IS GOUGED AT STATION XFS9. REPAIRED PER BAC TLX AOC-OKC-02- 00110H AND EA 5740-01329. (M) 2 L 7 2 4F RT A6WE 2003021000145 20030210 00145 WP 2003 2 10 DHL2002801022 1 20021212 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CARGO BAY WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 NR 3 CARGO SMOKE DETECTOR WILL NOT TEST. DEFERRED PER MEL 26-6-1. DMI #11218. 2 L 7 4 4F RT 4A25 2002121300080 20021213 00080 EU 2002 12 13 MALA020636 1 20021030 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 367PX 340B271 DURING 4K INSPECTION IN CWA, CENTER AISLE SEAT TRACK BL 0 HAS CORROSION IN CARGO AREA. MAINTENANCE REMOVED CORROSION IN CARGO AREA, COMPLETED REPAIR IAW MAL EO S53060. A/C RELEASE DATE 11/6/02. 2 L 7 2 4T RT A52EU 2002121300081 20021213 00081 EU 2002 12 13 MALA020637 1 20021030 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 367PX 340B271 DURING 4K INSPECTION IN CWA, RT SEAT TRACK IN CARGO AREA HAS CORROSION. MAINTENANCE COMPLETED REPAIR IAW MAL EO S53060. A/C RELEASE DATE 11/6/02. 2 L 7 2 4T RT A52EU 2002121300082 20021213 00082 WP 2002 12 13 DHL2002801023 1 20021212 A 2611 100064901 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP A DHLA K O NONE OTHER N FALSE WARNING IN INSP/MAINT 1 SO 01 801DH 46033 1) LOWER SMOKE DETECTOR FB6863 FALSE WARNING.2) TROUBLESHOT SYSTEM FOUND FB6863 SDU BAD. REMOVED AND REPLACED UNIT REP ROGRAMMED SYSTEM IAW M/M 26-16-01 AND ST 300. 2 L 7 4 4F RT 4A25 2002121300083 20021213 00083 EU 2002 12 13 MALA020639 1 20021106 A 3020 44730501 MODULE SAAB SF340 340B 7860101 EU DEICE SYSTEM FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 449XJ 340B449 DURING FLIGHT 3158, RT INTAKE HEAT IS INOPERATIVE. RT INTAKE CAUTION LIGHT ON WILL NOT RESET. A/C DIVERTED TO DTW. M AINTENANCE REMOVED AND REPLACED RT DEICE MODULE. GROUND RAN A/C FOR 25 MINUTES NO FAULTS NOTED AT THIS TIME. 2 L 7 2 4T RT A52EU 2002121300084 20021213 00084 EU 2002 12 13 MALA020640 1 20021020 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 521XJ E2346 DURING C-CHECK INSPECTION IN CVG, NR 1 SEAT TRACK FORWARD OF FRAME 20, UPPER SURFACE HAS CORROSION. MAINTENANCE REPAIRE D NR 1 SEAT TRACK IAW EO 53026. RELEASE DATE WAS 11/11/02 2 H 7 4 4F RT A49EU 2002121300085 20021213 00085 EU 2002 12 13 MALA020641 1 20021020 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 521XJ E2346 DURING C-CHECK INSPECTION IN CVG, NR 3 SEAT TRACK FORWARD OF FRAME 20 IS CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED N R 3 SEAT TRACK IAW EO A53026. A/C RELEASE DATE: 11/11/02. 2 H 7 4 4F RT A49EU 2002121300086 20021213 00086 EU 2002 12 13 MALA020642 1 20021020 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 521XJ E2346 DURING C-CHECK IN CVG, NR 4 SEAT TRACK FORWARD OF FRAME 20 IS CORRODED. MAINTENANCE REPAIRED NR 4 SEAT TRACK IAW A53026 . A/C RELEASE DATE 11/11/02. 2 H 7 4 4F RT A49EU 2002121300087 20021213 00087 EU 2002 12 13 MALA020643 1 20021023 A 5311 FRAME BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 521XJ E2346 DURING C-CHECK IN CVG, FOUND CORROSION ON UPPER SURFACE OF FRAME 18 ADJACENT TO SEAT TRACK NR 4. BEYOND LIMITS, REPAIRE D FRAME 18 IAW EO A53101 & BAE FAX BARA/AVR/6113/02-0DC. A/C RELEASE DATE: 11/11/02 2 H 7 4 4F RT A49EU 2002121300088 20021213 00088 EU 2002 12 13 MALA020644 1 20021024 A 5311 FRAME BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 521XJ E2346 DURING C-CHECK IN CVG, FOUND CORROSION BEYOND LIMITS ON UPPER SURFACE OF FRAME 15. MAINTENANCE REPAIRED DAMAGE IAW EO A 53102. A/C RELEASE DATE 11/11/02. 2 H 7 4 4F RT A49EU 2002121300089 20021213 00089 EU 2002 12 13 MALA020645 1 20021107 A 5347 STRUCTURE SAAB SF340 340B 7860101 EU SEAT TRACK CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 414XJ 340B414 DURING A11 INSPECTION IN CWA, MAINTENANCE FOUND RT SEAT TRACK WRAP AROUND HAS CORROSION. MAINTENANCE REMOVED AND REPLAC ED RT SEAT TRACK WRAP AROUND IAW SRM CHAP 51. A/C RELEASE DATE 11/12/02 2 L 7 2 4T RT A52EU 2002121300090 20021213 00090 NM 2002 12 13 DHL2002743014 1 20021212 A 2510 808737631 SEAT BOEING 727 727225 1384077 NM A DHLA K O NONE OTHER O OTHER NR NOT REPORTED 1 SO 01 743DH 22438 1) F/O SEATBACK POPS BACKWARD WHEN PRESSURE EXERTED AGAINST IT.2) REMOVED AND REPLACED F/O'S SEAT IAW B-727 M/M 25-10- 42. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2002121300091 20021213 00091 EU 2002 12 13 MALA020648 1 20021109 A 3150 6071T02P18 CONTROL UNIT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 456XJ 340B456 DURING CLIMBOUT ON FLT 3395, RT ENGINE ITT DROPPED TO 355 INFLIGHT. THE CABIN PRESSURE WARNING LIGHT ILLUMINATED ALSO. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED DECU. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2002121300092 20021213 00092 EU 2002 12 13 MALA020649 1 20021110 A 7400 MS2740127 RELAY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE IGNITION LIGHT FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 428XJ 340B428 DURING FLIGHT 2923, THE LT IGNITION LIGHT ILLUMINATED AFTER TAKEOFF. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLAC ED RELAY 43PC IAW AMM 74-30-15-2. NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A52EU E8NE 2002121300093 20021213 00093 EU 2002 12 13 MALA020650 1 20021112 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS WILL NOT TEST A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 417XJ 340B417 DURING MAINTENANCE ON A/C, EMERGENCY BATTERY PACKS 20LN AND 21LN FAILED TEST. MAINTENANCE REPLACED BOTH BATTERIES, AND TESTS GOOD. 2 L 7 2 4T RT A52EU 2002121300094 20021213 00094 NE 2002 12 13 MALA020651 3 20021112 A 6110 PROPELLER SAAB SF340 SF340A 7850100 EU ROTOL R390 R3904123F27 NE RIGHT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 89XJ 340A089 DURING CLIMBOUT OF FLIGHT 2907, RT ENGINE SURGED DURING CLIMB. TORQUE WENT TO 120 PERCENT FOR 10 SECONDS, TEMP WENT TO 9 68 DEGREES FOR 10 SECONDS. PROP RPM REMAINED STABLE. CTOT WAS OFF, AUTO COARSEN OFF, AUTO PILOT ON. PILOT WENT TO TORQ UE MOTOR LOCK OUT PER QR HAND ENGINE PARAMETERS STABILIZED. AIR RETURN TO DTW. MAINTENANCE REPLACED RT PROP ASSEMBLY. REPLACED DEC IAW GE-MM 72-00-00. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 6 C P31NE 2002121300095 20021213 00095 EU 2002 12 13 MALA020652 1 20021112 A 5210 SEAL SAAB SF340 340B 7860101 EU PAX DOOR OBSTRUCTED A MALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 15 408XJ 340B408 IMMEDIATELY AFTER TAKE OFF, FLT 3032, MAIN DOOR MADE VERY LOUD NOISE. AIR RETURN TO MEM. MAINTENANCE FOUND STICKER ON MAIN DOOR FRAME MATING SURFACE WHICH CAUSED MAIN DOOR TO NOT SEAL PROPERLY. INSPECTED MAIN DOOR SEAL AND DOOR FRAME SU RFACE, NO FURTHER DISCREPANCIES NOTED. RAN AND PRESSURIZED A/C, NO NOISES HEARD FROM MAIN DOOR, NORMAL PRESSURIZATION O CCURED A/C RTS. 2 L 7 2 4T RT A52EU 2002121300096 20021213 00096 EU 2002 12 13 MALA020653 1 20021113 A 3020 44730501 CONTROL MODULE SAAB SF340 340B 7860101 EU RT INTAKE HEAT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 430XJ 340B430 DURING FLT 2919, RT INTAKE HEAT INTERMITTENT, CYCLES ON AND OFF. A/C RETURN TO MSP. MAINTENANCE REPLACED RT DEICE CONT ROL MODULE, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2002121300097 20021213 00097 NM 2002 12 13 DHL2002755010 1 20021212 A 2610 SWITCH BOEING 727 727225 1384077 NM A DHLA K O NONE OTHER O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 1) FIRE WARNING BELL FOR ENGINE AND WHEELWELL DETECTOR INTERMITTENT, LIGHTS OK.2) REMOVED AND REPLACED FAULTY BELL CUT -OUT SWITCH & OPS CHECKED IAW B727 M/M 26-11-0. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2002121300098 20021213 00098 EU 2002 12 13 MALA020654 1 20021115 A 3020 NH24668169 DUCT SAAB SF340 340B 7860101 EU RT INTAKE DEICE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 404XJ 340B404 DURING FLT 3181, RT INTAKE HEAT FAULTED IN FLIGHT, RT INTAKE ANNUNCIATOR LIGHT ILLUMINATED INTERMITTENTLY WITH RT ANTI-I CE SWITCH ON. A/C RETURNED TO MEMPHIS. MAINTENANCE REPLACED LOWER DUCT IAW SF3 MM CHAP 71-60-05-4. OPS CHECK OF RT EN GINE ANTI-ICE GOOD IAW SF3 MM CHAP 30-20-00-6. 2 L 7 2 4T RT A52EU 2002121300099 20021213 00099 EU 2002 12 13 MALA020655 1 20021118 A 3251 708572 ACTUATOR SAAB SF340 340B 7860101 EU NLG STEERING FAILED A MALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 407XJ 340B407 UPON TAXIING TO GATE, NOSE WHEEL STEERING NOT CONTROLLABLE. WITH NOSE WHEEL STEERING ENGAGED, MAIN HYD ACCUMULATOR PRES SURE DROPS BELOW 1850 IN 1-2 SECONDS. NOSE WHEEL STEERING DOES NOT RESPOND WITH HYD PUMP SWITCH IN AUTO OR OVERRIDE. PU MP CYCLES EVERY 2 SECONDS WITH NOSE WHEEL STEERING ENGAGED. NO VISIBLE LEAKS FLUID LEVEL IS WITHIN LIMITS. MAINTENANCE REPLACED NOSE WHEEL STEERING ACTUATOR. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2002121300100 20021213 00100 EU 2002 12 13 MALA020656 1 20021112 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 370PX 340B300 DURING 6Y/4Y INSPECTION, SEAT TRACK BL 0, STA 297-348 HAS CORROSION. MAINTENANCE COMPLETED SEAT TRACK REPAIR SPLICE IAW EO 53060. A/C RELEASE DATE 11/20/02. 2 L 7 2 4T RT A52EU 2002121300101 20021213 00101 EU 2002 12 13 MALA020657 1 20021118 A 5414 SKIN SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 370PX 340B300 DURING 6Y/4Y INSPECTION IN CWA, CHAFING DAMAGE TO LT INBOARD NACELLE SKIN CAUSED BY WING LEADING EDGE FAIRING SEAL. MAI NTENANCE COMPLETED REPAIR IAW EO S54053. A/C RELEASE DATE 11/20/02 2 L 7 2 4T RT A52EU 2002121300102 20021213 00102 EU 2002 12 13 MALA020658 1 20021120 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 370PX 340B300 DURING 6Y/4Y INSPECTION IN CWA, NOTED LT FWD SEAT TRACK LBL 18.3 HAS HEAVY CORROSION. MAINTENANCE COMPLETED REPAIR BETW EEN STA 297-329 IAW EO S53060. A/C RELEASE DATE 11/20/02 2 L 7 2 4T RT A52EU 2002121300103 20021213 00103 EU 2002 12 13 MALA020659 1 20021119 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 370PX 340B300 DURING 6Y/4Y INSPECTION IN CWA, SEAT TRACK CORROSION IN CARGO AREA. MAINTENANCE COMPLETED SEAT TRACK SPLICE REPAIR IAW EO S53060 AT BL 0 STA 619.138 - 686.888. A/C RELEASE DATE 11/20/02. 2 L 7 2 4T RT A52EU 2002121300104 20021213 00104 EU 2002 12 13 MALA020661 1 20021119 A 3030 856MU HEATER SAAB SF340 340B 7860101 EU PITOT STATIC MALFUNCTIONED A MALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 434XJ 340B434 BEFORE TAKEOFF OF FLT 2765, CREW REPORTED THE STANDBY PITOT HEAT LIGHT ILLUMINATED. A/C RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED STBY PITOT/STATIC TUBE, CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002121300105 20021213 00105 NM 2002 12 13 VNAA0212014 1 20021209 A 3200 870004MODB PSEU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 441JS 14575 5 3059 THE CREW RECEIVED A PROXY SYSTEM AMBER CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FO R SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002121300106 20021213 00106 2002 12 13 VNAA0212012 4 20021207 A 3100 501122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FORWARD FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 438JS 17642 866 3056 THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY FAILS TO TEST. MAINTENANCE INSPECTED AND REPLACED THE FORWARD EMERGEN CY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002121300107 20021213 00107 2002 12 13 SWAA022873 4 20021208 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 711HK 27845 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002121300108 20021213 00108 2002 12 13 SWAA022874 4 20021208 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 711HK 27845 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002121300109 20021213 00109 NM 2002 12 13 SWAA022876 1 20021209 A 5311 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R AND STR 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002121300110 20021213 00110 NM 2002 12 13 SWAA022877 1 20021209 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 103SW 23109 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 761, BELOW STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002121300111 20021213 00111 NM 2002 12 13 SWAA022878 1 20021208 A 5520 6525798 HINGE BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 755SA 27871 DURING SCHEDULED A2 CHECK, SWA SI 11038-55, LT ELEVATOR TAB NR 4 HINGE WORN. REMOVED AND REPLACED LT ELEVATOR TAB NR 4 HINGE PER MM. 2 L 7 2 4F RT A16WE 2002121300112 20021213 00112 NM 2002 12 13 SWAA022879 1 20021209 A 5330 6545785 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUTS CRACKED AT WINDOWS NR 12, NR 30, NR 32 AND NR 33. REPAIRED SKI N PER BFG ER & SRM. 2 L 7 2 4F RT A16WE 2002121300113 20021213 00113 NM 2002 12 13 SWAA022880 1 20021207 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 14L. REPAIRED SKIN PER BFG ER AND SRM. 2 L 7 2 4F RT A16WE 2002121300114 20021213 00114 NM 2002 12 13 SWAA022881 1 20021207 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED C2 CHECK, FOUND BS 1016 BULKHEAD CRACKED (2 EA) AT STR 11 AND STR 13 POSITIONS RADIATING FROM RIVETS AT THE PERIPHERY OF THE PRESS PLUG. REPAIRED BULKHEAD PER SWA EA. 2 L 7 2 4F A16WE 2002121300115 20021213 00115 NM 2002 12 13 SWAA022882 1 20021207 A 3220 65463382 BRACKET BOEING 737 737317 138447P NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SERVICE CHECK, FOUND NLG UPPER ACTUATOR SUPPORT BRACKET CRACKED. REMOVED AND REPLACED NLG UPPER ACTUAT OR SUPPORT BRACKET PER SRM. 2 L 7 2 4F RT A16WE 2002121300116 20021213 00116 NM 2002 12 13 SWAA022883 1 20021207 A 5513 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM ELEVATORS WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 751SW 29803 DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, BOTH LEFT AND RIGHT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH LEFT AND RT ELEVATOR TAB NR 1 HINGE BUSHINGS. 2 L 7 2 4F RT A16WE 2002121300117 20021213 00117 NM 2002 12 13 SWAA022884 1 20021208 A 5210 MS20253 HINGE PIN BOEING 737 7375H4 138449D NM FWD ENTRY DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 ON ARRIVAL UNABLE TO OPEN FWD ENTRY DOOR. FOUND, UPPER HINGE PIN PARTIALLY DISLODGED. REINSERTED PIN AND INSTALLED CIR CLIP PER MM. 2 L 7 2 4F RT A16WE 2002121300118 20021213 00118 NM 2002 12 13 SWAA022885 1 20021207 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C2 CHECK, FOUND BOTH UPPER AND LOWER HINGE CUTOUTS CRACKED ON AFT ENTRY DOOR. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002121300119 20021213 00119 NM 2002 12 13 SWAA022886 1 20021206 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT EXTERNAL AIR CONDITIONING DOOR CUTOUT AT FWD LT SIDE. REPAIRE D SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002121300120 20021213 00120 NM 2002 12 13 SWAA022888 1 20021206 A 2731 BACB10AD12 BEARING BOEING 737 7372H4 138448C NM LT ELEVATOR WORN A SWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 29 071SW 22358 IN FLIGHT, ELEVATOR VERY STIFF. ON APPROACH ELEVATOR HAS DEAD BAND AREA. REMOVED AND REPLACED LEFT ELEVATOR CONTROL ROD INPUT BEARING. 2 L 7 2 4F A16WE 2002121300121 20021213 00121 NM 2002 12 13 SWAA022890 1 20021207 A 3220 65446915 PRIORITY VALVE BOEING 737 7373Q8 1384670 NM RT MLG W/W FAULTY A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 29 687SW 23388 ON DEPARTURE, RT MLG DID NOT RAISE, INDICATED DOWN AND UNSAFE WITH GEAR HANDLE IN UP AND OFF. CYCLED GEAR HANDLE TO UP AND RT MLG CAME UP. RECYCLED GEAR DOWN AND BACK UP ALL INDICATIONS NORMAL. REMOVED AND REPLACED RT MLG POSITION PRIORI TY VALVE PER MM. 2 L 7 2 4F RT A16WE 2002121300122 20021213 00122 NM 2002 12 13 SWAA022848 1 20021205 A 3350 079123 COVER BOEING 737 7377H4 1384404 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 EEPLS WIRES EXPOSED AT ROW 17. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002121300123 20021213 00123 2002 12 13 SWAA022849 4 20021204 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT DOORS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED C2 CHECK, FOUND BOTH AFT DOOR EVACUATION SLIDE PRESSURE INDICATORS OUT OF VIEW. REPOSITIONED BOTH AFT DOOR SLIDES PER MM. 2 L 7 2 4F A16WE 2002121300124 20021213 00124 NM 2002 12 13 SWAA022850 1 20021204 A 5320 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED SPECIAL VISIT, FOUND BS 727B STRINGER CLIP CRACKED AT STR 4L. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2002121300125 20021213 00125 NM 2002 12 13 SWAA022851 1 20021204 A 5313 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED SPECIAL VISIT, FOUND BS 360 STRINGER SPLICE CRACKED AT STR 4L. REMOVED AND REPLACED STRINGER SPLICE PE R SRM. 2 L 7 2 4F RT A16WE 2002121300126 20021213 00126 2002 12 13 SWAA022852 4 20021204 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002121300127 20021213 00127 NM 2002 12 13 SWAA022854 1 20021205 A 2730 6559227 BUSHING BOEING 737 7373A4 1384585 NM LT ELEV WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C2 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR CONTROL ROD END BUSHING PER MM. 2 L 7 2 4F RT A16WE 2002121300128 20021213 00128 2002 12 13 SWAA022855 4 20021205 A 2565 65C19901 CABLE BOEING 737 7373A4 1384585 NM L2 DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE CABLE MISROUTED. REROUTED SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2002121300129 20021213 00129 NM 2002 12 13 SWAA022856 1 20021205 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C2 CHECK, FOUND A 3.5 FUSELAGE SKIN CRACK, BS 807, STRINGER 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002121300130 20021213 00130 NM 2002 12 13 SWAA022857 1 20021205 A 5230 6547952 SKIN BOEING 737 7373A4 1384585 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR EXTERNAL SKIN CRACKED AT HANDLE CUT OUT, UPPER AFT CORNER. REPAIRED SKI N PER SWA EA. 2 L 7 2 4F RT A16WE 2002121300131 20021213 00131 NM 2002 12 13 SWAA022858 1 20021205 A 3245 113786 LINE BOEING 737 7375H4 138449D NM LT MLG LEAKING A SWAA O OTHER J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 29 521SW 25320 DECLARED EMERGENCY, AFTER TAKEOFF, DURING GEAR RETRACTION, HYD WARNING SYS LIGHT ILLUMINATED, HYD PRESS INDICATED ZERO. AFTER GEAR RETRACTION PRESS INDICATION RETURNED TO NORMAL. REMOVED AND REPLACED LT MLG ACTUATOR DOWN HYD LINE. REMOVE D AND REPLACED HYD A-SYS ENG DRIVEN AND ELEC DRAIN CASE FILTERS, (NO DEBRIS FOUND). REMOVED AND REPLACED NR 1 ENG HYD PU MP, ALL IAW MM. 2 L 7 2 4F RT A16WE 2002121300132 20021213 00132 NM 2002 12 13 SWAA022860 1 20021206 A 5751 6546454 AILERON BOEING 737 7372H4 138448C NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 DURING WALK AROUND INSPECTION, FOUND LT AILERON DELAMINATED AT OUTER EDGE ON BOTH UPPER AND LOWER SURFACE. REMOVED AND REPLACED LT AILERON PER MM. 2 L 7 2 4F A16WE 2002121300133 20021213 00133 NM 2002 12 13 SWAA022862 1 20021206 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 EEPLS COVER MISSING AT ROW NR 11. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2002121300134 20021213 00134 NM 2002 12 13 SWAA022863 1 20021206 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS380, STR 14R. REPAIRED SKIN PER BFG ER. 2 L 7 2 4F RT A16WE 2002121300135 20021213 00135 2002 12 13 SWAA022864 4 20021205 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002121300136 20021213 00136 2002 12 13 SWAA022868 4 20021206 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM FWD SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002121300137 20021213 00137 2002 12 13 SWAA022870 4 20021206 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 732SW 27864 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002121300138 20021213 00138 NM 2002 12 13 AWXA200201197 1 20021125 A 5313 6517688131 ANGLE BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 0 0 23777 MCN - MAJOR REPAIR - DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON THE LOWER SURFACE OF CREASE BEAM SUPPORT ANGLE BS 331, LBL 57, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS, REMOVED DAMAGED CREASE BEA M SUPPORT ANGLE BS 331, LBL 57, WL 208; FABRICATED A NEW REPLACEMENT CREASE BEAM SUPPORT ANGLE; INSTALLED REPAIR PART IA W B737-300 SRM 51-40-02, PG. 3-4, & 10-11. 2 L 7 2 4F RT A16WE 2002121300139 20021213 00139 EU 2002 12 13 MALA020662 1 20021120 A 3230 PIN SAAB SF340 340B 7860101 EU MLG DAMAGED A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 438XJ 340B438 UPON GEAR RETRACTION FLT 2951, FOUND GEAR PIN DETACHED FROM CLIP AND PIN LANYARD AND STILL IN NOSE GEAR. AIR RETURN TO D TW. MAINTENANCE FOUND GEAR PIN DETACHED FROM CLIP AND PIN LANYARD AND STILL IN NOSE GEAR. REMOVED AND REPLACED GEAR P IN, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002121300140 20021213 00140 NE 2002 12 13 MALA020663 2 20021122 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A1 30030 NE RIGHT MALFUNCTIONED A MALA E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 991XJ 340A091 WHEN STARTING, RT ENGINE LIGHT-OFF TOOK LONGER THAN NORMAL BUT WAS WITHIN LIMITS. AFTER LIGHT-OFF ITT STABILIZED AT 775 AND NG AT 65. IT NEVER SEEMED TO FULLY START UPON SHUTDOWN, SMOKE CAME OUT INTAKE. MAINTENANCE RAN ENGINE TO CLEAR RES IDUAL FUEL OUT OF COMBUSTER CAN ENGINE. OPS CHECKS GOOD ON START IDLE SPEED AND SHUTDOWN IAW GE MM 72-00-00. 2 L 7 2 4T 4 T RT A52EU E8NE 2002121300141 20021213 00141 EU 2002 12 13 MALA020664 1 20021123 A 2497 WIRE SAAB SF340 340B 7860101 EU DC GENERATOR DISCONNECTED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 452XJ 340B452 DURING FLIGHT 2919, LT DC GEN LIGHT ILLUMINATED IN FLT. AIR RETURN TO MSP. MAINTENANCE RESECURED WIRE AT DC GEN TERMINA L. DC GEN OPS CHECK GOOD. IAW AMM 24-30-00. 2 L 7 2 4T RT A52EU 2002121300142 20021213 00142 EU 2002 12 13 MALA020666 1 20021124 A 2560 P4010021 BATTERY BAC 146 AVRO146RJ85A 1500097 EU FLASHLIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 518XJ E2337 AFT FLIGHT ATTENDENT EMERGENCY FLASHLIGHT LED NOT FLASHING. MAINTENANCE REPLACED BATTERY, OPS CHECKS GOOD. 2 H 7 4 4F RT A49EU 2002121300143 20021213 00143 EU 2002 12 13 MALA020667 1 20021122 A 3520 OXYGEN MASK BAC 146 AVRO146RJ85A 1500097 EU NR 1 C & D DEPLOYED A MALA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 15 506XJ E2314 SEATS 1C & 1D OXGYEN MASK DROPPED UNCOMMANDED DURING PUSHBACK. MAINTENANCE RESECURED 02 MASKS AND PANEL. 2 H 7 4 4F RT A49EU 2002121300144 20021213 00144 WP 2002 12 13 AALA20021461 1 20021003 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 556AA 53086 TUL - FOUND LONGERON 2L CRACKED AT FRAME 1418, JUST FORWARD OF END FITTING OUTBOARD SIDE. REPAIRED PER AARD 53-30-00-2. (M) 2 L 7 2 4F A6WE 2002121300145 20021213 00145 WP 2002 12 13 AALA20021462 1 20020926 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 556AA 53086 TUL - FOUND CRACK IN CUSP AT STATION 506. INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002121300146 20021213 00146 WP 2002 12 13 AALA20021491 1 20021011 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 455AA 49560 TUL - FOUND CRACK AROUND FASTENER IN FUSELAGE SKIN ABOVE PYLON STATION 1380 LEFT SIDE. REPAIRED PER SRM 53-01. (M) 2 L 7 2 4F A6WE 2002121300147 20021213 00147 WP 2002 12 13 AALA20021492 1 20021008 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 455AA 49560 TUL - FOUND CORROSION AROUND TIEDOWN TRACK ATTACH SCREWS AND CLIPNUT HOLES LEFT SIDE. INSTALLED SERVICEABLE LEFT TIEDOW N TRACK AFT CARGO BETWEEN STATION 1220-1309, PER SRM 51-10. (M) 2 L 7 2 4F A6WE 2002121300148 20021213 00148 WP 2002 12 13 AALA20021493 1 20021007 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 455AA 49560 TUL - FOUND CORROSION AROUND FASTENERS ON DOOR BEAM AND AROUND 2 BOTTOM DOOR STOPS ON BEAM, FS 1155-1212. REMOVED CORRO SION TREATED AND PRIMED, INSTALLED DOUBLER PER SRM 53-10-00-3. (M) 2 L 7 2 4F A6WE 2002121300149 20021213 00149 WP 2002 12 13 AALA20021494 1 20021001 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 455AA 49560 TUL - FOUND FRAME STATION 1174 IS CRACKED BELOW LONGERON 6L. INSTALLED SPACER AND DOUBLER AT STATION 1174 AND 6L PER AA RD 53-10-00-30. (M) 2 L 7 2 4F A6WE 2002121300150 20021213 00150 WP 2002 12 13 AALA20021495 1 20021003 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 455AA 49560 TUL - FOUND CORROSION ON CUSP STATION 694 TO 699. REPAIRED PER AARD 52-00-00-02. (M) 2 L 7 2 4F A6WE 2002121300151 20021213 00151 WP 2002 12 13 AALA20021496 1 20021004 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 455AA 49560 TUL - FOUND NR 6 SEAT TRACK HAS CORROSION, SEVERAL AREA'S OUT OF LIMITS STATION 275-791. NEW SEAT TRACK INSTALLED/AMM 5 3-40-01,01-02. (M) 2 L 7 2 4F A6WE 2002121300152 20021213 00152 WP 2002 12 13 AALA20021497 1 20021017 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 573AA 53092 TUL - FOUND CORROSION ON CABIN FLOORBOARD SUPPORT RIGHT OF A/C CENTERLINE STATION 150. INSTALLED NEW FLOORBOARD SUPPORT ON TOP OF CUSP RT OF CENTERLINE STATION 150. (M) 2 L 7 2 4F A6WE 2002121300153 20021213 00153 WP 2002 12 13 AALA20021498 1 20021017 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 573AA 53092 TUL - FOUND RN 1 SEAT TRACK UNDER GALLEY CORRODED AT STATION 1177, 1195, 1208, 1215, 1225-1229, 1241 AND 1281. INSTALLE D NEW SEAT TRACK NR 1 FROM STATION 1174 TO 1308 PER AMM 53-40-01. (M) 2 L 7 2 4F A6WE 2002121300154 20021213 00154 WP 2002 12 13 AALA20021510 1 20020930 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 455AA 49560 TUL - FOUND CORROSION ON SEAT TRACK NR 6 STATION 1212-1213. REMOVED CORROSION PER SRM 51-10-03 BEYOND SRM LIMITS. REMO VED DAMAGE AND INSTALLED PLUG PER SRM 53-05 FIG 4A. (M) 2 L 7 2 4F A6WE 2002121300155 20021213 00155 WP 2002 12 13 AALA20021520 1 20021009 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 445AA 49471 TUL - FOUND CUSP AND CUSP T-ANGLE BENT AT STATION 238 TO 240 LEFT SIDE. CUT OUT DAMAGED AREA OF T-ANGLE AND CUSP AND RE PAIRED PER AARD 53-00-00-02 AND ESO 80559 10-07-02. (M) 2 L 7 2 4F A6WE 2002121300156 20021213 00156 WP 2002 12 13 AALA20021521 1 20021009 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 TUL - FOUND GOUGE IN STATION 1380 FRAME FORWARD SIDE AT STATION 5L. FABRICATED DOUBLER, ALODINED AND PRIMED AND INSTALL ED DOUBLER AT STATION 1380 SRM 51-70-4. (M) 2 L 7 2 4F A6WE 2002121300157 20021213 00157 WP 2002 12 13 AALA20021522 1 20021004 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 TUL - FOUND SKIN CRACK AT FASTENER LONGERON 14L STATION 1380. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53-01 -00. (M) 2 L 7 2 4F A6WE 2002121300158 20021213 00158 WP 2002 12 13 AALA20021523 1 20021004 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 TUL - FOUND STATION 225-227 LEFT CUSP OUTBOARD OF NR 1 TRACK, CUSP HAS 2 INCH CRACK EMITTING FROM FORWARD SIDE OF LIGHTE NING HOLE. STOP DRILLED, DYE CHECKED AND NO CRACKS FOUND. FABRICATED DOUBLER ALODINED, PRIMED AND INSTALLED PER MM 53- 10-01. (M) 2 L 7 2 4F A6WE 2002121300159 20021213 00159 WP 2002 12 13 AALA20021524 1 20021003 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 TUL - FOUND NR 4 SEAT TRACK, LUG CRACKED AT STATION 270. INSTALLED REPAIR PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2002121300160 20021213 00160 WP 2002 12 13 AALA20021525 1 20021002 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 TUL - FOUND WINDOW INNER FRAME CRACKED AT STATION 845 UPPER CORNER. INSTALLED DOUBLER PER AARD 53-10-00. (M) 2 L 7 2 4F A6WE 2002121300161 20021213 00161 WP 2002 12 13 AALA20021526 1 20021004 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 TUL - FOUND CORROSION ON FLOOR WEB AROUND GALLEY TIE DOWN STATION 170 RBL 11. REMOVED DAMAGE. INSTALLED DOUBLER PER SR M 53-01-00 FIG 4 SHEET 3. (M) 2 L 7 2 4F A6WE 2002121300162 20021213 00162 WP 2002 12 13 AALA20021527 1 20021004 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 TUL - FOUND STATION 627 LEFT CUSP HAS .5 INCH CRACK EMITTING FROM INBOARD EDGE OF CENTER LIGHTENING HOLE. INSTALLED REP AIR DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2002121300163 20021213 00163 WP 2002 12 13 AALA20021528 1 20021007 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 TUL - FOUND INTERIM REPAIR ACCOMPLISHED ON AFT CARGO BEAM CORROSION, STATION 1174. REPLACED AFT CARGO DOOR CUT OUT, LOW ER BEAM PER SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2002121300164 20021213 00164 WP 2002 12 13 AALA20021529 1 20021007 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 TUL - FOUND 2 GOUGES STATION 231 LEFT BETWEEN LONGERON 17L AND 18L. DYE CHECKED DAMAGE, NO CRACKS. INSTALLED REPAIR DO UBLER PER SRM 53-04-00 FIG 38. (M) 2 L 7 2 4F A6WE 2002121300165 20021213 00165 WP 2002 12 13 AALA20021530 1 20021008 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 TUL - FOUND FRAME CRACKED IN RADIUS AFT SIDE STATION 1418, LONGERON 2R. STOP DRILLED CRACK. INSTALLED DOUBLER REPAIR P ER SRM 53-01-0 PAGE 10. (M) 2 L 7 2 4F A6WE 2002121300166 20021213 00166 WP 2002 12 13 AALA20021531 1 20021009 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 TUL - FOUND LONGERON DAMAGED 1 INCH AFT OF STATION 1338, STRINGER 17L. INSTALLED LONGERON SPLICE PER SRM 53-02-00 AND A ARD 53-00-00-05. (M) 2 L 7 2 4F A6WE 2002121300167 20021213 00167 WP 2002 12 13 AALA20021616 1 20021107 A 5342 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 483AA 49676 TUL - FOUND VERTICAL STABILIZER TO FUSELAGE RIGHT ATTACH ANGLE CRACKED, AT AFT END. CUT OUT DAMAGED SECTION OF SKATE AN GLE. INSTALLED FILLER AN DOUBLER REPAIR PER AARD 53-10-00-2. (M) 2 L 7 2 4F A6WE 2002121300168 20021213 00168 NM 2002 12 13 AALA20020866 1 20020613 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 191AN 32385 FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 19 INOPERATIVE. RECONNECTED SIDEWALL CONNECTOR ON RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121300169 20021213 00169 NM 2002 12 13 AALA20020996 1 20020711 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 183AN 29593 MIA - FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE BETWEEN SEAT 3F AND 6F. REMOVED AND REPLACED BROKEN CONNECTOR. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121300170 20021213 00170 NM 2002 12 13 AALA20021171 1 20020818 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 632AA 24590 DFW - FOUND EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. RECONNECTED CONNECTOR AT SIDEWALL LIGHTS. SYSTEM GROUND CHECKED N ORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121300171 20021213 00171 NM 2002 12 13 AALA20021423 1 20021005 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AA 24488 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING AT SEAT 16D INOPERATIVE. REPLACED EMERGENCY ESCAPE P ATH LIGHTING ASSEMBLY AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121300172 20021213 00172 NM 2002 12 13 AALA20021458 1 20021011 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 618AA 24526 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE IN FORWARD CABIN. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121300173 20021213 00173 NM 2002 12 13 AALA20021470 1 20021014 A 3350 SOCKET BOEING 757 757223 1384957 NM CABIN CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 698AN 26980 DFW - FOUND EMERGENCY LIGHT AT L4 DOOR SLIDE INOPERATIVE. CLEANED CORROSION FROM LIGHT SOCKET. SYSTEM GROUND CHECKED N ORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121300174 20021213 00174 NM 2002 12 13 AALA20021509 1 20021024 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 696AN 26976 MIA - FOUND EMERGENCY LIGHT AT 4A IS INOPERATIVE. SECURED CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121300175 20021213 00175 NM 2002 12 13 AALA20021539 1 20021026 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 673AN 29423 DFW - FOUND EMERGENCY PATH LIGHTING INOPERATIVE AT DOOR 2R. REPLACED FLOOR LIGHT SEGMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121300176 20021213 00176 NM 2002 12 13 AALA20021542 1 20021028 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 675AN 29425 JFK - FOUND FLOOR PATH LIGHT IN FIRST CLASS INOPERATIVE. SECURED CONNECTOR IN FIRST CLASS. SYSTEM GROUND CHECKED NORMA L OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121300177 20021213 00177 NM 2002 12 13 AALA20021581 1 20021029 A 3350 0201991008 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 648AA 24606 BDL - FOUND SEAT MOUNTED ESCAPE PATH LIGHT ASSEMBLY ON SEAT 14D INOPERATIVE. INSTALLED NEW LIGHT ASSEMBLY. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121300178 20021213 00178 NE 2002 12 13 AALA20021627 2 20021112 A 7200 ENGINE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E437 54555 NE RIGHT MAKING METAL A AALA A UNSCHED LANDING R M PARTIAL RPM/PWR LOSS OVER TEMP CL CLIMB 1 SW 21 618AA 24526 LAX - FLT 192 - EN ROUTE LAX-BOS, AT CLIMB POWER, RIGHT ENGINE COMPRESSOR STALLED AND OVERTEMPED. RETURNED AND LANDED A T LAX WITHOUT FURTHER INCIDENT. FOUND METAL IN TAIL PIPE. REPLACED RIGHT ENGINE. GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F 4 F RT A2NM E12EU 2002121300179 20021213 00179 NM 2002 12 13 AALA20021644 1 20021113 A 3350 BATTERY BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 176AA 32395 DFW - FOUND EXTERIOR EMERGENCY LIGHT AT RIGHT AFT ENTRY DOOR INOPERATIVE. CLEANED SOCKET AND REPLACED BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121300180 20021213 00180 NM 2002 12 13 AALA20021645 1 20021113 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 369AA 25196 DFW - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT PATH MARKER FORWARD OF SEAT 24 E/F LENS CLIP BROKEN. REPLACED EMERGE NCY PATH LIGHT ASSEMBLY FORWARD OF SEAT 24 E/F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002121300181 20021213 00181 EU 2002 12 13 AALA20021648 1 20021114 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1414D 11377 DFW - DURING EMERGENCY, EXIT FLOOR PATH LIGHT STRIP AT SEAT 8D INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT ST RIP WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2002121300182 20021213 00182 NM 2002 12 13 AALA20021649 1 20021116 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 DFW - FOUND EMERGENCY TRACK LIGHTS IN FIRST CLASS ARE INOPERATIVE. FOUND LOOSE CONNECTION. RESECURED CONNECTOR. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121300183 20021213 00183 NM 2002 12 13 AALA20021650 1 20021116 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 646AA 24604 DFW - FOUND SEAT MOUNTED EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. FOUND LIGHT ASSEMBLY DISCONNECTED. RECONNECTED. (M) 2 L 7 2 4F RT A2NM 2002121300184 20021213 00184 WP 2002 12 13 ASAA0280549 1 20021110 A 5730 593746816 SKIN DOUG DC9 DC983 3022083 WP RT WING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - DURING 30K CHECK, FOUND RIGHT WING LOWER LEADING EDGE IS GOUGED AT STATION XFS67. REPAIRED PER BAC TLX AOC-OKC-02 -00110H AND EA 5740-01329. (M) 2 L 7 2 4F RT A6WE 2002121300185 20021213 00185 SO 2002 12 13 ACT 1 20021212 A 3200 20885 ACTUATOR EMB 120 EMB120ER 3260203 SO A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 96ZK 10075 120096 LANDING GEAR FAILED TO RETRACT AFTER TAKE OFF, REPLACED L/H MLG UPLOCK ACTUATOR OPS CHECK GOOD 2 L 7 2 4T RT A31SO 2002121300186 20021213 00186 EU 2002 12 13 MALA020668 1 20021113 A 5522 SKIN SAAB SF340 340B 7860101 EU RT & LT ELEVATOR DEBONDED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 DURING 6Y/4Y INSPECTION FOUND LT AND RT ELEVATOR LEADING EDGES HAVE DEBONDS ON TOP SURFACE. MAINTENANCE REPAIRED IAW EO S55031. A/C RELEASE DATE 11/17/02. 2 L 7 2 4T RT A52EU 2002121300187 20021213 00187 EU 2002 12 13 MALA020669 1 20021120 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 370PX 340B300 DURING 6Y/4Y INSPECTION IN CWA, FOUND TOP FLANGE ON BOTTOM FRAME AT STA 294 LBL 18.3 HAS CORROSION OUT OF LIMITS. MAINT ENANCE COMPLETED REPAIR IAW EO S53108. A/C RELEASE DATE 11/24/2002. 2 L 7 2 4T RT A52EU 2002121300188 20021213 00188 EU 2002 12 13 MALA020670 1 20021113 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 370PX 340B300 DURING 6Y/4Y INSPECTION IN CWA, WEBBING AT STA 288 HAD 294 HAS CORROSION. MAINTENANCE INSTALLED WEBBING AT STA 288 AND 294 IAW SF340 AMM SRM 51-40-21 AND MAL EO S53108. A/C RELEASE DATE 11/24/2002 2 L 7 2 4T RT A52EU 2002121300189 20021213 00189 EU 2002 12 13 MALA020672 1 20021125 A 3020 MODULE SAAB SF340 340B 7860101 EU DEICE SYSTEM MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 429XJ 340B429 DURING FLT3354, WITH ENGINE ANTI-ICE SELECTED, THE RT INTAKE LIGHT ILLUMINATED FOR 15 SECONDS. OFF FOR 5 SECONDS, THEN BACK ON FOR 15 SECONDS. REPEATS CYCLES. AIR RETURN TO DTW. MAINTENANCE REPLACED DEICE CONTROL MODULE IAW MM. ALL CHEC KS GOOD. 2 L 7 2 4T RT A52EU 2002121300190 20021213 00190 EU 2002 12 13 MALA020674 1 20021125 A 5320 STRUCTURE BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR SILL CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 525XJ E2350 DURING A SPECIAL INSPECTION FOUND FWD AND AFT Z-MEMBERS AT AFT PAX DOOR LOWER SILL CORRODED GREATER THAN SRM ALLOWS. MA INTENANCE PERFORMED REPAIR TO AFT DOOR SILL Z-MEMBERS PER SRM 51-71-11. 2 H 7 4 4F RT A49EU 2002121300191 20021213 00191 EU 2002 12 13 MALA020675 1 20021115 A 5315 FLOORBEAM BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C-CHECK IN CVG, FLOORBEAM 18 BETWEEN NR 3 AND 4 SEAT TRACK AND OUTBOARD 1.0 INCH FROM NR 4 SEAT TRACK HAS CORROSI ON ON UPPER SURFACE BEYOND LIMITS. MAINTENANCE REPAIRED FLOORBEAM 18 IAW EO A53013 AND BAE FAX BARA/AVR/6171/02-DC. 2 H 7 4 4F RT A49EU 2002121300192 20021213 00192 EU 2002 12 13 MALA020676 1 20021115 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C-CHECK IN CVG, NR 4 SEAT TRACK SECTION FROM FRAME 18 TO FRAME 20 IS CORRODED BEYOND LIMITS. MAITENANCE REPAIRED SEAT TRACK IAW SRM 53-00-32-201 AND EO A53026. 2 H 7 4 4F RT A49EU 2002121300193 20021213 00193 EU 2002 12 13 MALA020677 1 20021115 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C-CHECK IN CVG, NR 3 SEAT TRACK SECTION FROM FRAME 18 TO FRAME 20 IS CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED SEAT TRACK IAW SRM 53-00-32 201 AND EO A53026. 2 H 7 4 4F RT A49EU 2002121300194 20021213 00194 EU 2002 12 13 MALA020680 1 20021208 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 340B426 DURING 4K INSPECTION IN CWA, FRAME TIP PROFILES FWD AND AFT HAVE CORROSION. MAINTENANCE REPAIRED PROFILES IAW S53102, RELEASE DATE 12/10/02. 2 L 7 2 4T RT A52EU 2002121300195 20021213 00195 EU 2002 12 13 MALA020681 1 20021208 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 340B426 DURING 4K-INSPECTION IN CWA, WEBBING AT STA 288 AND 294 HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED WEBBING. A/C RELEASE DATE 12/10/02. 2 L 7 2 4T RT A52EU 2002121300196 20021213 00196 EU 2002 12 13 MALA020682 1 20021207 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 453XJ 340B453 DURING FLIGHT 3021, AVIONICS SMOKE LIGHT ILLUMINATED ON THE CWP. AIR RETURN TO MSP. NO SMOKE IN CABIN. MAINTENANCE INS TALLED NEW SMOKE DETECTOR, 2 L 7 2 4T RT A52EU 2002121300197 20021213 00197 CE 2002 12 13 CGO2002F00006 1 20021125 A 2121 1143800287 BLOWER BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA AIR DISTRIBUTION OVERHEATED E CGOR O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 03 800CA UE383 INVESTIGATED COMPLAINT OF SMOKE ODOR IN CABIN WHEN BLOWER IS OPERATING. FOUND EVIDENCE OF AFT BLOWER ASSEMBLY OVERHEATI NG AND NOTED BURNED ODOR. REPLACED AFT BLOWER ASSEMBLY, SYSTEM OPERATIONAL CHECKS, OK. 2 L 7 2 4T 3 T RT A24CE E2NE 2002121300198 20021213 00198 2002 12 13 DAT2002F00002 4 20021003 A 6122 8210209 GOVERNOR STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA RT PROPELLER FLUCTUATES A DATA E A ENGINE SHUTDOWN UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 13 330AC 168 SH3007 DURING THE SET UP FOR A CRUISE CLIMB CONFIGURATION THE PROP RPM WAS REDUCED TO THE NORMAL 1400 RPM WHEN THE RT PROP KEPT FALLING UNTIL IT STABILIZED AT 750 RPM WITH 4300 POUNDS OF INDICATED TORQUE. AFTER INCREASING AND DECREASING THE RT PR OP AND POWER LEVELS WITH NO CHANGE, THE DECISION WAS MADE TO SHUT DOWN THE RT ENGINE TO PREVENT FURTHER DAMAGE. THE AIR CRAFT WAS LANDED UNEVENTFULLY. THE RT PROP GOVERNOR AND PROXIMITY SWITCH WAS REPLACED. THE BETA VALVE AND BETA LINKAGE WAS ADJUSTED. THE RUN AND OPS CHECK WAS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T A41EU E4EA 2002121300199 20021213 00199 WP 2002 12 13 DBCA1220 2 20021127 A 7420 30708733 IGNITION LEAD LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP NR 2 ENGINE FAILED E DBCA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 13 505EE 4385 505 NR 2 ENGINE START ATTEMPTED. ENGINE WOULD SPOOL, BUT NOT LIGHT-OFF. PILOT ABORTED START ATTEMPT AND CONTACTED MAINTENA NCE. TROUBLESHOT AND FOUND ONE IGNITION LEAD BAD. REPLACED DEFECTIVE LEAD AND BOTH IGNITORS. OPS CHECKED GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2002121300200 20021213 00200 SW 2002 12 13 GXP2002F00005 1 20021204 A 3297 WIRE SWRNGN SA226 SA226TC 8780404 SW RT MLG BROKEN E GXPA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 164GA TC281 RT MAIN LANDING GEAR INDICATION SHOWED IN TRANSIT (RED). ATTEMPTED EMERGENCY EXTENSION AND ALTERNATE PROCEDURE WITH NO CHANGE. REPAIRED BROKEN WIRE ON RT LANDING GEAR DOWN SWITCH. OPS CHECKED GOOD. 2 L 7 2 4T RT A8SW 2002121300201 20021213 00201 NM 2002 12 13 IU62002F00035 1 20021002 A 2913 HOUSING BOEING 737 737* NM HYD PUMP ERODED A IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 14108 EROSION AROUND STROKING PISTON PORT. STEEL SLEEVE OR ALTERNATE SEAL. 2 L 7 2 4F RT A16WE 2002121300202 20021213 00202 WP 2002 12 13 ZW0A0212301 1 20021212 A 3350 0105601003PA57 COVER DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER NR NOT REPORTED 1 CE 13 976TW 53626 THE EGRESS LIGHTING AT SEAT 25D WAS INOPERATIVE. REPLACED THE TRACK COVER. CHECK-C 9-17-02 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2002121300203 20021213 00203 SO 2002 12 13 C2XA02BT081 1 20021212 A 2620 336000575 FIRE BOTTLE EMB 145 EMB145ER 3260211 SO EMPENNAGE FAULTY A C2XA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 14940 145033 EWR---CO3359, CREW REPORTED, "EICAS MESSAGES E1/E2 EXTBTL A INOP"; OCCURRED SHORTLY AFTER LANDING. MAINTENANCE REMOVED AND REPLACED "A" FIRE EXTINGUISHER BOTTLE. AIRCRAFT TESTS GOOD IAW EMB145 MM 26-21-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002121500001 20021215 00001 SO 2002 12 15 C2XA02IA251 1 20021212 A 5600 163500109 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT CRACKED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 11551 145411 IAH- DURING CLIMB OUT THE CREW NOTED THAT THE CAPTAINS WINDSHIELD SHATTERED IN FLIGHT. THE CREW DID AN AIR RETURN TO I AH, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD, PERFORMED A OPERATION AL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002121600001 20021216 00001 NM 2002 12 16 DL73K021303 1 20021105 A 5312 6546568567 BULKHEAD BOEING 737 737232 1384475 NM FS1016,LBL2, CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 A .625 INCH CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE GORE/WEB OF THE AFT PRESSURE DOME AT FS 1016 AT LBL 2 & WL 244. THE CRACK TIPS WERE STOP DRILLED AND REPAIRED WITH A DOUBLER PER ER/A 384128-14, REV A. 2 L 7 2 4F RT A16WE 2002121600002 20021216 00002 NM 2002 12 16 DL73K021315 1 20021112 A 3244 TIRE BOEING 737 737247 138448D NM NR 4 SEPARATED A DALA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 SO 27 373DL 23520 ON WALK AROUND FOUND TIRE TREAD MISSING ON NR 4 MAIN TIRE. TREAD SEPARATION CAUSED DAMAGE TO THE RT INBD UNDERWING FIXE D PANEL, RT TRAILING EDGE MID FLAP AND BROKE THE INNER AND CENTER RT GEAR DOORS. REPLACED WHEEL ASSY AND REPAIRED DAMAG E. 2 L 7 2 4F A16WE 2003021000131 20030210 00131 NM 2003 2 10 DHL2002747010 1 20021211 A 2612 WARNING LIGHT BOEING 727 727224 1384076 NM NR 1 FIRE DETECT ILLUMINATED A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 747DH 22253 NR 1 ENGINE FIRE WARNING GROUND FAULT SYSTEM LIGHT ILLUMINATED. DEFERRED PER MEL 26-9, CONTROL 11203, PLACARD INSTALLE D. 2 L 7 3 4F A3WE 2003030300035 20030303 00035 NM 2003 3 3 HNAA0200089 1 20021208 A 2820 82820026001 TUBE DHAV DHC8 DHC8201 2809001 NM FUEL SYSTEM LEAKING A HNAA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 07 995HA 15319 15319 460 FUEL LEAKING AT SINGLE POINT REFUEL VALVE DRAIN. REPLACED FUEL TUBE. 2 H 7 2 4T RT A13NM 2002121600003 20021216 00003 NM 2002 12 16 HNAA0200088 1 20021209 A 2800 AS3209220 PACKING DHAV DHC8 DHC8102 2809003 NM #2 NACELLE LEAKING A HNAA O OTHER K FLUID LOSS IN INSP/MAINT 1 EA 07 917HA 41603 41603 075 9 DEC. 2002FUEL DRIPPING OUT OF GEAR WELL ABOVE CONTACTOR BOX #2 NACELLE. WIGGINS FITTING FWD OF NACELLE FIRE SEAL WAS FOUND LEAKING. REPLACED O-RINGS PN AS3209-218 LEAK CHECK GOOD.10 DEC. 2002FUEL COMING OUT OF DRAIN ON INBD SIDE OF #2 N ACELLE. FOUND LEAK AT REFUEL/DEFUEL T FITTING IN #2 NACELLE LEAKING AT BOTTOM. REPLACED O-RINGS PN AS3209-220, LEAK CH ECK GOOD. 2 H 7 2 4T RT A13NM 2002121600004 20021216 00004 WP 2002 12 16 ABXA020360 1 20021203 A 5313 59203192 LONGERON DOUG DC9 DC932 3022066 WP FWD. CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 LONGERON 30 CRACKED AT STA. 408 - 427. REPAIRED CRACKED LONGERON 30 IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2002121600005 20021216 00005 WP 2002 12 16 ABXA020361 1 20021203 A 5300 99578743 FRAME DOUG DC9 DC932 3022066 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 FRAME AT STA. 180, LONGERON 4 LEFT, CRACKED FROM INBOARD LONGERON FASTENER. REPAIRED IAW DC-9 SSRM AND DRAWING K05159. 2 L 7 2 4F A6WE 2002121600006 20021216 00006 EU 2002 12 16 DHL2002364015 1 20021213 A 3040 4098954 DRIVE SHAFT AIRBUS 300 A300B4203 3930306 EU SHEARED A DHLA K O NONE OTHER O OTHER NR NOT REPORTED 1 SO 01 364DH 141 1) CAPTAIN'S WINDSHIELD - WIPER VERY NOISY DURING OPS. AND DOES NOT CONTACT OUTER/ UPPER 40% OF SWEEP. 2) FOUND D RIVE SHAFT SHEARED. REMOVED AND REPLACED CAPTAIN'S WIPER DRIVE SHAFT. REMOVED AND REPLACED WIPER BLADE. OPS CHECKED OK IAW M/M 30-41-01. 2 L 7 2 4F RT A35EU 2002121600007 20021216 00007 EU 2002 12 16 DHL2002366016 1 20021213 A 3040 WINDSHIELD WIPER AIRBUS 300 A300B4203 3930306 EU A DHLA K O NONE OTHER O OTHER NR NOT REPORTED 1 SO 01 366DH 249 1) CAPTAIN'S WINDSHIELD WIPER ONLY CLEANS BOTTOM HALF OF WINDSHIELD.2) REMOVED AND REPLACED CAPTAIN'S WINDSHIELD WIPER BLADE IAW M/M 30-41-12. OPS CHECKED GOOD. 2 L 7 2 4F RT A35EU 2002121600008 20021216 00008 SO 2002 12 16 C2XA02BT083 1 20021215 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 16525 145403 EWR---CO3465, CREW REPORTED EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR WILL NOT LIGHT.....MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW EMB145 MM 33-50-09. OPS. CHECKED GOOD. (AIRCRAFT RETURNED TO SERVICE.) 2 L 7 2 4F RT T00011AT 2002121600009 20021216 00009 NM 2002 12 16 DL73K021333 1 20021116 A 2910 HYDRAULIC SYSTEM BOEING 737 737247 138448D NM A SYSTEM LOW A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 373DL 23520 SYSTEM A HYD QTY INDICATOR DROPPED TO 1.5 GALLONS FOLLOWED BY ILLUMINATION OF SYSTEM B LOW QTY LIGHT. ABNORMAL PROCEDUR ES FOLLOWED. A/C ARRIVED WITH A SYSTEM AT 2.5 GAL. SERVICED TO FULL EXERCISED FLAPS/SLATS AND SPOILERS OPERATED GEAR H ANDLE. PERFORMED YAW DAMP TEST OPERATED RUDDER. RAN B SYSTEM FOR SEVERAL HOURS. NO LEAKS FOUND. 2 L 7 2 4F A16WE 2002121600010 20021216 00010 NM 2002 12 16 DL73K021341 1 20021119 A 3830 CHECK VALVE BOEING 737 737247 138448D NM LAV SERVIE LEAKING A DALA K NONE S AFFECT SYSTEMS CR CRUISE 1 SO 27 245WA 23519 ON ARRIVAL FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE DENTED. SUSPECT DAMAGE FROM BLUE ICE CAUSED BY LEAKING FWD LA V SERVICE PANEL. REPLACED STAB L/E ASSY AND REPLACED LAV SERVICE LINE CHECK VALVE. 2 L 7 2 4F A16WE 2002121600011 20021216 00011 NM 2002 12 16 DL73K021351 1 20021120 A 2120 ODOR BOEING 737 737232 1384475 NM CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 312DL 23084 BURNING SMELL FILLS AIRCRAFT WHILE GASPER FAN IS ON OR OFF. A/C FILLED WITH SMOKE AT GATE. ALL ELECTR POWER REMOVED AN D SMOKE STOPPED. COCKPIT ELECTR LOAD CENTER (CB'S,RELAYS,FEEDER CABLES ETC), NO DISCREPANCIES NOTED. INSP E/E COMPT FO R FLUID LEAKS, NONE FOUND, ALSO INSP WIRING AND RACKS FOR ELECTRICAL MALF, NONE NOTED. INSP LT/RT A/C BAYS AND PLENUM A REA, ALL CKS OK. RAN A/C PACKS WITH APU AND ENG AIR, BOTH A/C PACK OPS NORMAL. PERF POWER RUN OF 01/02 ENGS PER PFHB, ALL SYS CK NORMAL UNDER VARYING ELECT/PNEU LOADS. R&R COALESCER BAGS. 2 L 7 2 4F RT A16WE 2002121600012 20021216 00012 NE 2002 12 16 DL757021025 2 20020901 A 7261 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 LEAKING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 692DL 13982 29724 727276 15 MINS OUT FROM ATL ON DESCENT THE LEFT ENGINE OIL QUANTITY WENT TO ZERO, FOLLOWED BY THE LEFT ENGINE OIL PRESSURE FALL ING TO ZERO. THE LEFT ENGINE WAS SHUTDOWN. INSPECTION OF THE LEFT ENGINE FOUND OIL DRIPPING FROM THE NUMBER 5 BEARING AND THE TAIL PIPE WAS COVERED WITH OIL, REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121600013 20021216 00013 NM 2002 12 16 DL757021032 1 20020831 A 5320 143N851212 SILL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 611DL 22818 CORROSION REPAIR, THE LOWER SILL CHORD OF THE C1 DOOR OPENING WAS FOUND CORRODED. THE LOWER SECTIONS WERE TEMPORARILY R EMOVED TO ALLOW FOR SILL REPLACEMENT AND THEN SPLICED BACK WITH REPAIR DOUBLERS AND ANGLES PER ER/A 383631-14, REV A. 2 L 7 2 4F RT A2NM 2002121600014 20021216 00014 NM 2002 12 16 DL757021081 1 20020914 A 3222 AXLE BOEING 757 757232 1384965 NM NLG SHEARED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 668DN 25141 A/C NOSE LANDING GEAR RT AXLE SHEARED ON TAXIWAY, HAD TO REPLACE NOSE LANDING GEAR PISTON. 2 L 7 2 4F RT A2NM 2002121600015 20021216 00015 NM 2002 12 16 HNAA0200090 1 20021213 A 2731 85520001003 ELEVATOR DHAV DHC8 DHC8201 2809001 NM TAIL ICED A HNAA K NONE O OTHER DE DESCENT 1 EA 07 998HA 9254 9254 509 UNABLE TO PITCH DOWN WITH ELEVATOR IN FLIGHT, CAPTAIN SUSPECTS ICING. INSPECTED ELEVATOR AND TABS FOR PHYSICAL DAMAGE A ND OPERATED ELEVATORS, NO DAMAGE NOTED OPERATED NORMAL. 2 H 7 2 4T RT A13NM 2002121600016 20021216 00016 NM 2002 12 16 DL757021093 1 20020916 A 5320 146N852247 SILL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 SILL CORROSION AND FRAME SPLICE REPAIR THE OUTER CHORD OF THE LOWER SILL OF THE C2 DOOR OPENING WAS FOUND CORRODED AND R EQUIRED REPLACEMENT. A NEW SILL CHORD WAS INSTALLED, AND THE FRAME CHORD AND WEB WERE SPLICE BACK IN WITH REPAIR DOUBLE RS AND ANGLES PER ER/A 383694-14, REV A. 2 L 7 2 4F RT A2NM 2002121600017 20021216 00017 NM 2002 12 16 DL757021100 1 20020917 A 3350 S283T0143 BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 638DL 23761 R4 EXTERNAL EMERG LIGHT INOP. REPLACED BATTERY PACK, OP CKS GOOD. 2 L 7 2 4F RT A2NM 2002121600018 20021216 00018 SO 2002 12 16 C2XA02CL223 1 20021105 A 3350 66368 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 11535 145518 THE CREW REPORTED THE EMERGENCY LIGHTS IN THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY AISLE PATH LIG HT STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002121600019 20021216 00019 SO 2002 12 16 C2XA02CL229 1 20021103 A 3350 66368 LIGHT EMB 135 EMB135ER 3260203 SO ALLSN AE3007 AE3007C GL CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27512 145274 THE CREW REPORTED A FLOOR EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FLOOR EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002121600020 20021216 00020 SO 2002 12 16 C2XA02CL233 1 20021126 A 3234 14532170401 CONTROL HANDLE EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007C GL COCKPIT INTERMITTENT A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 27962 145110 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE DURING GEAR EXTENSION. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR L EVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002121600021 20021216 00021 SO 2002 12 16 C2XA02CL239 1 20021205 A 3350 78812 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 18982 145223 THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE AT ROW 11. MAINTENANCE INSPECTED AND REPLACED THE A ISLE PATH LIGHTING STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2002121600022 20021216 00022 SO 2002 12 16 C2XA02CL241 1 20021206 A 2701 YOKE EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A C2XA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SW 27 13955 145075 THE CREW REPORTED DURING TAKEOFF ROLL, THE YOKE MOVED TO FULL PITCH UP POSITION AND FROZE THERE. THE SYSTEM RELAXED AFT ER ABORTED TAKEOFF. MAINTENANCE INSPECTED THE FLIGHT CONTROL SYSTEMS AND PERFORMED A HIGH SPEED TAXI. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS TEST FLOWN AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2002121600023 20021216 00023 SO 2002 12 16 C2XA02CL242 1 20021206 A 5210 LINKAGE EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL PAX DOOR LACK OF LUBE A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 25504 145186 THE CREW REPORTED THE PASSENGER DOOR COULD NOT BE OPENED FROM THE INSIDE. MAINTENANCE INSPECTED AND LUBED DOOR LINKAGE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002121600024 20021216 00024 SO 2002 12 16 C2XA02CL245 1 20021206 A 3234 14532170401 CONTROL HANDLE EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL COCKPIT INTERMITTENT A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 12934 145019 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE AFTER TAKEOFF. THE CREW RECYCLED THE GEAR AND AFTER 1 MINUTE TH E MESSAGE WENT AWAY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002121600025 20021216 00025 SO 2002 12 16 C2XA02CL246 1 20021211 A 2530 CBC16707 CONNECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GALLEY BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 11536 145520 THE CREW REPORTED A BURNING SMELL COMING FROM THE LEFT HOT JUG IN THE GALLEY. MAINTENANCE INSPECTED AND REPLACED THE LE FT HOT JUG CONNECTOR AND HOT JUG. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002121600026 20021216 00026 SO 2002 12 16 C2XA02IA233 1 20021028 A 3234 7455501 CONTROL HANDLE EMB 145 EMB145LR 3260212 SO RROYCE DART DART* NE COCKPIT INTERMITTENT A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 26545 145558 THE CREW NOTED ON CLIMB THAT THE LANDING GEAR INDICATION SHOWED THREE (3) DOWN IN AMBER AFTER RAISING GEAR LEVER, TOUCHE D HANDLE, THEN GEAR WENT UP. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER, PERFORMED A OPERATIONAL C HECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 T RT T00011AT 2002121600027 20021216 00027 2002 12 16 C2XA02IA237 4 20021110 A 2210 7017000 CIRCUIT CARD EMB 145 EMB145ER 3260211 SO AUTOPILOT SYS MALFUNCTIONED A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 14933 145018 THE CREW NOTED THAT THE AUTOPILOT/YAW DAMPER FAILED. MAINTENANCE REMOVED AND REPLACED THE NR 1 IC-600. PERFORMED A OPE RATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002121600028 20021216 00028 SO 2002 12 16 C2XA02IA239 1 20021110 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL RUDDER FAILED A C2XA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 27 14933 145018 THE CREW NOTED THAT THE RUDDER SYSTEMS NR 1 AND NR 2, INOPERATIVE. ON DEPARTURE, THE CREW DECLARED EMERGENCY. PERFORME D AN EMERGENCY DESCENT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 R UDDER SYSTEM PRESSURE SWITCH. PERFORMED AN OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002121600029 20021216 00029 SO 2002 12 16 C2XA02IA241 1 20021122 A 3350 7287580505 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12922 145338 DURING PREFLIGHT THE CREW NOTED THAT THE 1ST ROW OF EMERGENCY LIGHTS ON LEFT (SEATS 2A-3A) AND EMERGENCY LIGHTS BY GALLE Y DOOR, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP ON FIRST ROW. PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002121600030 20021216 00030 SO 2002 12 16 C2XA02IA242 1 20021122 A 3234 7455501 CONTROL HANDLE EMB 145 EMB145 3260210 SO COCKPIT INTERMITTENT A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 27 11109 145657 THE CREW NOTED THAT THE LANDING GEAR WOULD NOT COME UP. AFTER USING QRH, GEAR CAME UP. MAINTENANCE REMOVED AND REPLACE D THE LANDING GEAR CONTROL LEVER. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4F RT T00011AT 2002121600031 20021216 00031 SO 2002 12 16 C2XA02IA244 1 20021128 A 3350 7287580505 LIGHT EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007C GL CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY AISLE PATH LIGHTS FORWARD STRIP FAILED TO ILLUMINATE. MAINTENANCE RE MOVED AND REPLACED THE FORWARD EMERGENCY AISLE PATH LIGHT STRIP. PERFORMED AN OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002121600032 20021216 00032 NM 2002 12 16 C1HA200283019 1 20021117 A 3350 6104791 BATTERY PACK BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A C1HA K NONE L NO TEST UK UNKNOWN 1 GL 15 683CA 22490 EMERGENCY FLOOR TRACK LIGHTING MID/TRACK INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CK OK. 2 L 7 3 4F A3WE 2002121600034 20021216 00034 NM 2002 12 16 C1HA200292032 1 20021118 A 3350 SOCKET BOEING 727 727212 138407G NM PWA JT8 JT8D NE EXTERIOR CORRODED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 292AS 21458 LEFT OVERWING EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED CORROSION FROM LIGHT SOCKETS AND RELAMPED. OPS CHECK WAS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2002121600035 20021216 00035 NM 2002 12 16 C1HA200293010 1 20021004 A 5310 DOOR FRAME BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 FRAME CORRODED AT FORWARD END OF OPENING FOR E/E DOOR. REMOVED AND REPLACED THE FRAME FORWARD OF E/E BAY DOOR OPENING I AW SRMS 51-10-1, 51-30-2, AND 51-10-2. 2 L 7 3 4F A3WE 2002121600036 20021216 00036 NM 2002 12 16 C1HA200293011 1 20021004 A 5311 FRAME BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 FRAME AT STA 310 RIGHT IS EXFOLIATED AT LOWER END WHERE IT MEETS T-CHORD. TEMP REPAIR IAW AVIATION ENGINEERING MRB NR A AR 1004-02. 2 L 7 3 4F A3WE 2002121600037 20021216 00037 NM 2002 12 16 C1HA200295013 1 20021122 A 3397 WIRE BOEING 727 727290 138408W NM CABIN BROKEN A C1HA K NONE L NO TEST UK UNKNOWN 1 GL 15 295AS 22147 EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE FROM NR 1 GALLEY TO SEAT ROW 8DEF. REPAIRED BROKEN WIRE AT SEAT ROW 7DEF FLO OR TRACK LIGHT. OPS CHECK GOOD, OK FOR SERVICE. 2 L 7 3 4F A3WE 2002121600038 20021216 00038 WP 2002 12 16 IXXA00136S 1 20020911 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, FOUND A TEMPORARY REPAIR ON FUSELAGE FRAME STATION 340. REPAIR ACCOMPLISHED, REMOVAL OF TEMPORARY REPAIR, FABRICATION AND INSTALLATION OF REPAIR DOUBLERS IAW THE DOUGLAS SRM AND ENGINEERING DRAWING R12-R0 4. 2 L 7 4 4F RT 4A25 2002121600039 20021216 00039 WP 2002 12 16 IXXA0200087S 1 20020724 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 83050 2948 45978 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT OUTBOARD SLOT LEADING EDGE AREA ON THE MOUNTING SU RFACE WING STATION XFS422.750. REPAIR ACCOMPLISHED, REMOVAL OF CORROSION, FABRICATION AND INSTALLATION OF REPAIR DOUBLE RS AND SHIMS IAW THE DOUGLAS SRM. 2 L 7 4 4F RT 4A25 2002121600040 20021216 00040 WP 2002 12 16 IXXA0200091O 1 20021023 A 2910 FITTING DOUG DC8 DC873F 302199F WP RT MLG WW LOOSE A IXXA O OTHER K FLUID LOSS CR CRUISE 1 SW 11 605AL 91228 205 46106 EN ROUTE FROM TOL TO ANC, THE FLIGHT CREW NOTICED A DECLINE IN THE MAIN HYDRAULIC QUANTITY SYSTEM. THE FLIGHT CREW FOLL OWED COMPANY PROCEDURES AND CONTINUED TO ANC FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEAL ED A LOOSE FITTING AT THE SWIVEL GLAND IN THE MAIN GEAR ACTUATOR. MAINTENANCE TIGHTENED THE FITTING AND PERFORMED A SUC CESSFUL OPERATIONAL CHECK IAW THE DOUGLAS MM. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002121600041 20021216 00041 WP 2002 12 16 IXXA0200093S 1 20020714 A 5542 SKIN DOUG DC8 DC862F 3021972 WP RUDDER CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RUDDER TRAILING EDGE ABOVE THE TAB. REPAIR ACCOMPLISHE D, REMOVED SURFACE CORROSION IAW THE DOUGLAS SRM. 2 L 7 4 4F 4A25 2002121600042 20021216 00042 NM 2002 12 16 2002UALA01792 1 20021201 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 FRAME IN AT PIT AREA AT STATION 1480 HAD EXCESS MATERIAL REMOVED DURING CORROSION CLEANUP AND BETWEEN STRINGER 26R AND 2 7R AREA EFFECTED WAS UPPER INNER FLANGE OF FRAME. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP RE PAIR UNDER INNER FLANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121600043 20021216 00043 NM 2002 12 16 2002UALA01795 1 20021201 A 5344 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 STRAP AT ENTRY DOOR CUTOUT 1L EXTERIOR AT UPPER HINGE CUTOUT STATION 331. STRINGER 21L HAD GOUGE THAT EXCEEDED MATERIAL REMOVAL LIMIT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.STRAP REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121600044 20021216 00044 NM 2002 12 16 2002UALA01796 1 20021202 A 5313 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 SHEAR TIE AT FRAME STATION 1560 BETWEEN STRINGER 25L AND 26L IS CRACKED IN RADIUS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121600045 20021216 00045 NM 2002 12 16 2002UALA01797 1 20021129 A 5313 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 FUSELAGE STRINGER 25L AT STATION 544 HAS A DAMAGED FASTENER HOLE DUE TO LIGHTNING STRIKE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED STRINGER WITH SPLICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2002121600046 20021216 00046 NM 2002 12 16 2002UALA01798 1 20021129 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 FORWARD CARGO, LEFT HAND FRAME UPPER CHORD ANGLE IS BENT,STATION 500 AND STRINGER 31L. SUPPLEMENTAL DATA UPDATE MAJOR RE PAIR ACCOMPLISHED.REPLACED FRAME UPPER CHORD. 2 L 7 2 4F 4 F RT A1NM E24NE 2002121600047 20021216 00047 NM 2002 12 16 2002UALA01800 1 20021128 A 5320 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 LEFT HAND NOSE TUNNEL AT BODY STATION 246, LBL23, VERTICAL STIFFENER CRACKED FORWARD SIDE OF FLOOR BEAM. SUPPLEMENTAL DA TA UPDATE MAJOR REPAIR ACCOMPLISHED.REPLACED STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002121600048 20021216 00048 NM 2002 12 16 2002UALA01801 1 20021128 A 5400 PYLON BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 #2 PYLON STRUT UPPER TORQUE BOX WEB AT GENERATOR FEED CABLE CUT-OUT IS CRACKED IN CORNER RADIUS. SUPPLEMENTAL DATA UPDAT E MAJOR REPAIR ACCOMPLISHED.DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002121600049 20021216 00049 NM 2002 12 16 2002UALA01802 1 20021128 A 5400 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 #1 ENG PYLON AFT UPPER WEB AT PNEUMATIC DUCT FEED-THROUGH IS CRACKED IN RADIUS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR AC COMPLISHED. REPAIRED WEB WITH REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002121600050 20021216 00050 NM 2002 12 16 2002UALA01803 1 20021128 A 5400 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 #1 PYLON UPPER WEB AT ELECT. WIRE BUNDLE FEED-THROUGH HAS 2 EA. CRACKS AT NUTPLATES. SUPPLEMENTAL DATA UPDATE MAJOR REPA IR ACCOMPLISHED.REPAIRED WEB WITH REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002121600051 20021216 00051 NM 2002 12 16 2002UALA01804 1 20021128 A 5400 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 #1 PYLON UPPER WEB AT GENERATOR CABLE FEED-THROUGH HAS 2 EA CRACKS AT NUTPLATES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR A CCOMPLISHED. REPAIRED WEB WITH REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2002121900055 20021219 00055 NM 2002 12 19 2002UALA01822 1 20021206 A 5320 CHANNEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 CABIN FLOOR SUPPORT CHANNEL HAS CORROSION STATION 310 TO STATION 324 RBL 41. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121600052 20021216 00052 EA 2002 12 16 COMA0260706 1 20021210 A 4910 APU CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 01 951CA 7091 FLIGHT 5123 APU DOOR INHIBIT CLOSED STATUS MESSAGE.UNINHIBITED DOOR, OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F RT A21EA 2002121600053 20021216 00053 WP 2002 12 16 IXXA0200094S 1 20020713 A 5730 SKIN PANEL DOUG DC8 DC862F 3021972 WP RT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RIGHT WING UPPER LEADING EDGE PANEL BY THE NUMBER FOUR PYLON. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IAW THE DOUGLAS SRM AND DRAWING 57-02491. 2 L 7 4 4F 4A25 2002121600054 20021216 00054 EU 2002 12 16 SIMA200231711 1 20021107 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 381AE 340B381 ABI - DURING A MBV INSPECTION, ONE DENT ON CARGO FRAME 677 WAS FOUND. DAMAGE WAS LOCATED ON THE RIGHT SIDE NEAR THE FLO OR SUPPORTS. REMOVED DAMAGED AREA BY CUTOUT. PERFORMED AN EDDY CURRENT INSPECTION OF THE CUT OUT. NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS004631, PARA 11, AND STANDARD SRM PRACTICES. ( M) 2 L 7 2 4T RT A52EU 2002121600055 20021216 00055 EU 2002 12 16 SIMA200232402 1 20021117 A 3350 66902 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 374AE 340B374 BTR - FLT 3560 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT ROW 6, 7, AND 8 TO BE INOPERATIVE. AIRCRAFT WAS FERRIED TO DFW FOR REPAIR. MAINTENANCE REPLACED THE FLOOR LIGHT STRIP IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRC RAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002121600056 20021216 00056 EU 2002 12 16 SIMA200232404 1 20021117 A 3350 330151 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 389AE 340B389 DFW - FLT 3686 - CREW REPORTED THE CABIN EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS (S/N'S 1281, 1216, 1114 AND 1188) AW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2002121600057 20021216 00057 EU 2002 12 16 USAASA02097 1 20021115 A 3350 321430 BATTERY PACK AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 733UW 1205 PIT - THE LEFT EMERGENCY POWER SUPPLY UNIT FAULTED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED EMERGENCY POW ER SUPPLY BATTERY PACK. OPERATIONALLY CHECK OK. (M) 2 L 7 2 4F RT A28NM 2002121600058 20021216 00058 EA 2002 12 16 COMA0260707 1 20021211 A 2720 RUDDER CNDAIR CL600 CL6002B19 1900309 EA A COMA C ABORTED TAKEOFF J F WARNING INDICATION FLT CONT AFFECTED TO TAKEOFF 1 SO 01 810CA 7370 FLIGHT 5971 RUDDER CONFIG MESSAGE DURING T/O.COULD NOT DUPLICATE. OPERATIONAL CHECK OF RUDDER INDICATION WAS SATISFACTO RY. 2 L 7 2 4F RT A21EA 2002121600059 20021216 00059 EU 2002 12 16 USAASA02098 1 20021115 A 3350 321430 POWER SUPPLY AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 169UW 1455 BDL - THE EMERGENCY LIGHT SYSTEM FAILED THE OPERATIONAL CHECK, WITH 'EPSU INT LOAD EXIT R' AND 'EPSU INT LOAD EXIT L', M ESSAGES DISPLAYED. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002121600060 20021216 00060 EU 2002 12 16 USAASA02099 1 20021117 A 3350 321430 BATTERY AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 705UW 0929 PIT - AN 'EPSU BATT EMER R' MESSAGE CAME ON DURING THE EMERGENCY LIGHTS TEST. REPLACED RIGHT EMERGENCY POWER SUPPLY UNI T BATTERY. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002121600061 20021216 00061 EU 2002 12 16 USAASA02100 1 20021118 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 113UW 1141 TPA - AN EMERGENCY LIGHTS FAULT FOR THE LEFT SIDE WAS RECEIVED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED A N EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002121600062 20021216 00062 EU 2002 12 16 USAASA02101 1 20021120 A 3350 321430 BATTERY PACK AIRBUS 320 A320214 3930316 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 106US 1044 BOS - THE LEFT OVERWING BATTERY PACK EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALL Y CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002121600063 20021216 00063 2002 12 16 COMA0260708 4 20021211 A 3450 6227194201 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA L ABORTED APPROACH O OTHER AP APPROACH 1 SO 01 812CA 6529 7381 FLIGHT 5263 AIRCRAFT UNABLE TO TRACK GLIDE SLOPE.REPLACED THE #2 VIR-432 2 L 7 2 4F RT A21EA 2002121600064 20021216 00064 NE 2002 12 16 COMA0260709 2 20021211 A 7320 6078T55917 FCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT ENGINE MALFUNCTIONED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 798CA 7463 7348 FLIGHT 5639 LEFT ENGINE LAGGED SIGNIFICANTLY DURING POWER APPLICATION ON T/O ROLL.REPLACED THE LEFT ENIGNE FUEL CONTROL. 2 L 7 2 4F 4 F RT A21EA E15NE 2002121600065 20021216 00065 EA 2002 12 16 COMA0260710 1 20021211 A 5210 SEAL RING CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING C O F.O.D. OTHER CL CLIMB 1 SO 01 451CA 7562 FLIGHT 5667 LOUD SQUEAL FROM CABIN DOOR. F/A COULD SEE DAYLIGHT THROUGH DOOR SEAL.REPAIRED DOOR SEAL NIBS, PER SRM. 2 L 7 2 4F RT A21EA 2002121600066 20021216 00066 EA 2002 12 16 COMA0260711 1 20021212 A 3350 6464 POWER CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR INOPERATIVE A COMA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 949CA 7080 FLIGHT 5893 EMERGENCY FLOOR PATH LIGHTING IS INOP.REPLACED TRACK LIGHTING POWER STRIPS. 2 L 7 2 4F RT A21EA 2002121600067 20021216 00067 EA 2002 12 16 QXEA0201823 1 20021030 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 603QX 10011 PDX- THIS SDR IS BEING REPORTED AS PER THE REQUEST OF FISDO-09. FORWARD CARGO BAY CENTER CHIMNEY DAMAGED. REMOVED AND REPLACED FORWARD CARGO BAY CENTER CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002121600068 20021216 00068 WP 2002 12 16 ASAA0280551 1 20021110 A 5730 993749819 SKIN DOUG DC9 DC983 3022083 WP LT WING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, LEFT WING LEADING EDGE UPPER SKIN GOUGED AT STATION XFS 142. CUT OUT DAMAGED AREA AND REPAIRED P ER BAC TLX AOC-OKC-02-0081H AND EA 5740-01330. (M) 2 L 7 2 4F RT A6WE 2002121600069 20021216 00069 WP 2002 12 16 ASAA0280557 1 20021110 A 5230 5910141105 RETAINER DOUG DC9 DC983 3022083 WP CARGO DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, MID CARGO BAY DOOR SEAL RETAINERS ARE GOUGED NEAR RADIUS AT FORWARD AND AFT LOWER SEAL RETAINER. BLENDED PER BAC TLX AOC-OKC-02-00125H AND EA 5230-01183. (M) 2 L 7 2 4F RT A6WE 2002121600070 20021216 00070 WP 2002 12 16 GTIA021206 1 20021114 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND DENT RIGHT SIDE FS 605 BETWEEN LONGERONS 20R AND 21R. FABRICATED DOUBLER FOR STATION 602. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2002121600071 20021216 00071 WP 2002 12 16 GTIA021207 1 20021112 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND DENT LEFT SIDE FS 218 BETWEEN LONGERON 15L AND 16L. DENT LEFT SIDE FUSELAGE STATION 216 BETWEEN LONGERONS 1 5L AND 16L. FABRICATED DOUBLER. INSTALLED DOUBLER PER MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 2002121600072 20021216 00072 WP 2002 12 16 GTIA021208 1 20021112 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND PASSENGER SEAT TRACK RIGHT OUTBOARD, GOUGE AT FS 248, 291, CORROSION AT FS 256, 277, 301, 340, 400-418, 424- 447, 458-478, 492-496, 523-536, 551-566, 582-598. REMOVED SEAT TRACK STATION 256-291. LOCATED AND DRILLED NEW SEAT TRA CK. LOCATED AND DRILLED SEAT TRACK SPLICE. INSTALLED SEAT TRACK AND SPLICE. (M) 2 L 7 2 4F A6WE 2002121600073 20021216 00073 WP 2002 12 16 GTIA021209 1 20020813 A 5755 SPOILER DOUG DC9 DC981 3022081 WP LT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND LEFT WING MIDDLE SPOILER PANEL UPPER SIDE TAPS DELAMINATED INBOARD TO OUTBOARD. REMOVED LEFT INBOARD FLIGHT SPOILER. OK TO INSTALL SERVICEABLE LEFT INBOARD FLIGHT SPOILER. INSTALLED LEFT INBOARD FLIGHT SPOILER. (M) 2 L 7 2 4F A6WE 2002121600074 20021216 00074 WP 2002 12 16 GTIA021210 1 20020811 A 5310 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND AFT CARGO DOOR JAMB BEAM CORRODED FS 1155-1212. REMOVED DOOR JAMB BEAM FROM STATION 1147-1250 DRILLED AND L OCATED HOLES IN NEW BEAM. INSTALLED NEW DOOR JAMB BEAM. (M) 2 L 7 2 4F A6WE 2002121600075 20021216 00075 WP 2002 12 16 GTIA021212 1 20020814 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - DENTS LOCATED AT FS 411.5 AND 415 BETWEEN L19R AND L20R. REWORKED DENT AT FS 408, 411.5 AND 415. FORMED REPAIR, DOUBLER AND TRIPLER. INSTALLED DOUBLER AND TRIPLER. (M) 2 L 7 2 4F A6WE 2002121600076 20021216 00076 WP 2002 12 16 GTIA021213 1 20020822 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - PASSENGER CABIN FS 1135, STRINGER 2L LONGERON CRACKED. REMOVED DAMAGED SECTION OF LONGERON. LOCATED AND DRILLED NEW LONGERON AND SPLICES. INSTALLED NEW LONGERON AND 2 EACH SPLICES. (M) 2 L 7 2 4F A6WE 2002121600077 20021216 00077 WP 2002 12 16 GTIA021214 1 20021108 A 3350 LIGHT DOUG DC9 DC981 3022081 WP CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FLIGHT ATTENDANT FORWARD EMERGENCY HAND HELD LIGHT BROKEN. REMOVED FLIGHT ATTENDANT FORWARD EMERGENCY HAND HELD L IGHT. INSTALLED NEW FLIGHT ATTENDANT FORWARD EMERGENCY HAND HELD LIGHT. (M) 2 L 7 2 4F A6WE 2002121600078 20021216 00078 WP 2002 12 16 GTIA021215 1 20020811 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND FUSELAGE EXTERNAL SKIN CORRODED IN AREA FOR FORWARD CARGO DOOR SCUFF PLATE FS 370-427. FUSELAGE SKIN HAS SH ARP CREASE AT FS 390. CREASE AT FS 382 BELOW DOOR BEAM. CREASE AT FS 370 BELOW DOOR BEAM. DEEP GOUGE AT FS 388 BELOW DOOR BEAM. AREA OUT OF LIMITS FROM FS 391-406. INSTALLED REPAIR DOUBLER AND FILLERS. (M) 2 L 7 2 4F A6WE 2002121600079 20021216 00079 WP 2002 12 16 GTIA021216 1 20020813 A 5755 SPOILER DOUG DC9 DC981 3022081 WP RT WING DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - RIGHT WING MIDDLE SPOILER PANEL DELAMINATED AT LOWER INBOARD SIDE. RIGHT WING MIDDLE SPOILER UPPER SIDE DELAMINAT ED. REMOVED RIGHT WING MIDDLE SPOILER. OK TO INSTALL SERVICEABLE RIGHT WING INBOARD FLIGHT SPOILER. INSTALLED RIGHT I NBOARD FLIGHT SPOILER. (M) 2 L 7 2 4F A6WE 2002121600080 20021216 00080 WP 2002 12 16 GTIA021217 1 20021119 A 5754 5922533501 SLAT DOUG DC9 DC982 3022082 WP LT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 RSW - FLT 4978 - LEFT WING NR 3 SLAT HAS CRACK ON INBOARD SIDE APPROX 6 INCHES LONG. REMOVED AND REPLACED LEFT WING NR 3 SLAT. (M) 2 L 7 2 4F A6WE 2002121600081 20021216 00081 WP 2002 12 16 GTIA021218 1 20021120 A 3250 39346895001 CYLINDER DOUG DC9 DC983 3022083 WP NLG STEERING DEFECTIVE A GTIA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 23 802NK 53168 DTW - ON APPROACH TO DENVER, THE NOSE GEAR DID NOT INDICATE DOWN WHILE THE MAINS DID. AFTER CYCLING THE GEAR, THE SAME INDICATION RESULTED. UPON REVIEW OF PROPER CHECK LIST, WITH MANUAL GEAR EXT, LEVER PULLED, AND GEAR HANDLE DOWN. THE S AME INDICATION RESULTED. THERE WAS SEVERAL ATTEMPTS AT YAWING THE A/C. FINALLY AFTER STOWING THE MANUAL LEVER AND CYCL ING THE GEAR, THE SAME INDICATION RESULTED AGAIN. AFTER STOWING THE A/C FOR THE 3RD TIME AND JERKING THE YOKE. THE NOS E GEAR EXTENDED. HAD PROPER INDICATION AND LANDED. REMOVED AND REPLACED RIGHT AND LEFT NOSE STEERING CYL. (M) 2 L 7 2 4F RT A6WE 2002121600082 20021216 00082 SO 2002 12 16 SIMA200231001 1 20021030 A 5330 SKIN EMB 135 EMB135LR 3260305 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 737MW 145396 ABI - DURING AN IMBV INSPECTION, A DENT WAS FOUND ON LEFT FORWARD FUSELAGE SKIN. CUT OUT DAMAGED AREA. PERFORMED AN ED DY CURRENT INSPECTION OF THE AREA WITH NO DEFECTS NOTED. FABRICATED AN EXTERNAL DOUBLER. REPAIR DONE IAW EMB GST-3190/ 02 AND STANDARD EMB135 SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002121600083 20021216 00083 SO 2002 12 16 SIMA200231002 1 20021027 A 5320 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 737MW 145396 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON THE SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING. PERFO RMED EDDY CURRENT INSPECTION OF THE AREA WITH NO DEFECTS NOTED. FABRICATED TWO REPAIR DOUBLERS. REPAIR DONE IAW EMB GS T-3181/02, AMERICAN EAGLE AIRLINES INC ETN'S EM53-036, EM53-013 AND STANDARD EMB 135 SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002121600084 20021216 00084 SO 2002 12 16 SIMA200231003 1 20021031 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED DAMAGED CENTER SILL. INSTALLED NEW SILL IAW EMB SRM, EMB 145/1142 REV 19, CHAPTER 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2002121600085 20021216 00085 SO 2002 12 16 SIMA200231004 1 20021030 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - DURING IN IMBV INSPECTION, THE LEFT OMEGA BEAM AFT OF FRAME 24 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGED SECTION OF LEFT OMEGA BEAM AND TREATED BARE METAL EDGES. FABRICATED AN EXTERNAL ANGLE, TWO SHIMS AND FILLER. REPAIR DONE IAW EMB 145 SRM, EMB 145/1142 CHAPTER 53 REV 19, 53-21-10, FIG 202. (M) 2 L 7 2 4T RT T00011AT 2002121600086 20021216 00086 SO 2002 12 16 SIMA200231005 1 20021103 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 ABI - DURING A IMBV INSPECTION, THE RIGHT HAT BEAM AT FRAME 23 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXIST ING HAT BEAM. INSTALLED NEW BEAM IAW EMB 145 SRM, EMB 145/1142 REV 19, CHAPTERS 51-20-03, 51-40-02, AND 51-40-07. (M) 2 L 7 2 4T RT T00011AT 2002121600087 20021216 00087 SO 2002 12 16 SIMA200231006 1 20021030 A 5330 SKIN EMB 135 EMB135LR 3260305 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 737MW 145396 ABI - DURING AN IMBV INSPECTION, FOUND DENT IN LEFT FORWARD FUSELAGE SKIN. CUT OUT DAMAGED AREA. PERFORMED EDDY CURREN T INSPECTION OF THE AREA. NO DEFECTS NOTED. FABRICATED AN EXTERNAL DOUBLER, FILLER PLATE. REPAIR DONE IAW EMB GST-319 0/02 AND STANDARD EMB135 SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2002121600088 20021216 00088 SO 2002 12 16 SIMA200231008 1 20021105 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 ABI - DURING A IMBV INSPECTION, THE CARGO DOOR OPENING LOWER CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REM OVED EXISTING CENTER SILL. INSTALLED NEW SILL IAW EMB145 SRM, EMB SRM-145/1142 REV 19) CHAPTERS 51-20-01, 51-20-03, 51- 40-04 AND 51-40-06. (M) 2 L 7 2 4T RT T00011AT 2002121600089 20021216 00089 SO 2002 12 16 SIMA200231501 1 20021103 A 3040 163500111 ELEMENT EMB 135 EMB135LR 3260305 SO WINDSHIELD MALFUNCTIONED A SIMA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING A FLAME/FIRE CR CRUISE 1 SW 21 716AE 145264 BWI - DURING LEVEL FLIGHT AT 27,000 FEET, THE CAPTAINS WINDSHIELD HEAT ELEMENT CAUGHT FIRE AND SHORTED. CREW TURNED OFF LEFT WINDSHIELD HEAT. WINDOW HEAT ELEMENT HAD BURN MARKS IN FOUR PLACES ALONG THE LEFT HEAT STRIP. MAINTENANCE FOUND NO EVIDENCE OF FIRE, WINDSHIELD WAS REMOVED AND REPLACED IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WA S RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2002121600090 20021216 00090 SO 2002 12 16 SIMA200231502 1 20021106 A 5311 12010732001 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 ABI - DURING AN IMBV INSPECTION OF AIRCRAFT MAINTENANCE, FOUND FRAME 81 CRACKED ON LOWER EDGE. REMOVED CRACKED FRAME AN D INSTALLED NEW FRAME IAW EMB-145 SRM 145/1142 CHAPTER 51, REV 19, 51-40-02, AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2002121600091 20021216 00091 SO 2002 12 16 SIMA200231503 1 20021107 A 3610 CLAMP EMB 145 EMB145LR 3260212 SO E/E BAY LOOSE A SIMA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 620AE 145102 ORF - FLT 4025 - CREW REPORTED A BLEED LEAK MESSAGE ON EICAS DURING CRUISE FLIGHT. CAPTAIN DECLARED AN EMERGENCY AND CO NTINUED TO ORF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A LOOSE V-BAND CLAMP IN THE AFT AVIONICS COMPARTM ENT. CLAMP WAS TIGHTENED AND OPERATIONAL CHECK WAS COMPLIED WITH. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002121600092 20021216 00092 EU 2002 12 16 SIMA200231710 1 20021107 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 381AE 340B381 ABI - DURING AN MBV INSPECTION, ONE DENT ON CARGO FRAME 640 WAS FOUND. DAMAGE WAS LOCATED ON THE RIGHT SIDE 13 INCHES A BOVE THE FLOOR LINE. REMOVED DAMAGED AREA BY CUTOUT. PERFORMED AN EDDY CURRENT INSPECTION OF THE CUTOUT, NO DEFECTS NO TED. FABRICATED A DOUBLER ANGLE. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS004631, PARA 10, AND STANDARD SRM PRACTIC ES. (M) 2 L 7 2 4T RT A52EU 2002121600093 20021216 00093 EA 2002 12 16 2002F01087 1 20020916 A 2612 47259701 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA FIRE DETECTION FAULTY A REXA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SO 25 8488D 7488 ON TAXI OUT, CREW RECEIVED AN APU/ENGINE FIRE FAIL MESSAGE FOLLOWED BY AN LEFT ENGINE AND APU FIRE INDICATION. UPON INV ESTIGATION FALSE INDICATION WAS CAUSED BY FAULTY FIRE DETECTION WARNING CONTROL UNIT. UNIT WAS REMOVED AND REPLACED AND FUNCTIONALLY CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2002121600094 20021216 00094 NE 2002 12 16 2002F01089 2 20020829 A 8550 38360130 SEAL DHAV DHC2 DHC2* 2800108 EA PWA R985 R985* 52008 NE OIL PUMP DAMAGED A W0PC O OTHER O OTHER NR NOT REPORTED 1 AL 05 12UA 700 FOUND OIL RESERVOIR TO BE PRESSURIZED AFTER ENGINE RUN. FOUND BAD SEALS IN OIL PUMP. REPLACED PUMP PART NR 38360-130 P ROBLEM WENT AWAY. (M) 1 H 7 1 3R 3 R A806 5E1 2002121600096 20021216 00096 NM 2002 12 16 AALA20020511 1 20020419 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 613AA 24489 MIA - EMERGENCY LIGHTS AT SEAT 14D INOPERATIVE. REPLACED LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121600097 20021216 00097 NM 2002 12 16 CALA0200584 1 20021212 A 5330 SKIN BOEING 777 777224 1385225 NM FS 846-867 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78003 27579 INSPECTION FOUND R/H FUSELAGE SKIN DENTED 6 FEET BELOW AND 5 FEET AFT OF R-2 DOOR AT FS 846-867, STRINGER 35R-36R. REPAI RED IAW SRM 53-00-01, REPAIR 7 AND SUBSEQUENT INSPECTION OF REPAIR AREA IAW SRM 52-00-01, REPAIR 7, TABLE 204. 2 L 7 2 4F RT T00001SE 2002121600098 20021216 00098 WP 2002 12 16 CALA0200585 1 20021213 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP STA 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72830 49490 INSPECTION FOUND A 1/2" CRACK IN BELTFRAME AT STA 1418, LONGERON 2L-2R. A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 31 AND ECRA 5310-04301. 2 L 7 2 4F A6WE 2002121600099 20021216 00099 NM 2002 12 16 CALA0200586 1 20021213 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 727A CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34315 23366 INSPECTION FOUND A 3" CRACK IN R/H FUSELAGE SKIN JUST AFT OF R/H WHEEL WELL WING TO BODY FAIRING AT STA 727A, S23R. A RE PAIR DOUBLER/TRIPLER WAS INSTALLED IAW ECRA 5330-03185. 2 L 7 2 4F RT A16WE 2002121600100 20021216 00100 WP 2002 12 16 MWEA020729 1 20021216 A 5311 9910078215 DOUBLER DOUG DC9 DC915 3022036 WP STA 160 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 CORROSION THROUGH SUBFLOORING JUST AFT OF STATION 160 AT LEFT SIDE OF FUSELAGE CENTERLINE.. -- REMOVED CORROSION, FABRI CATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002121600101 20021216 00101 WP 2002 12 16 MWEA020730 1 20021216 A 5311 9910078215 DOUBLER DOUG DC9 DC915 3022036 WP STA 170 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 CORROSION IN SUBFLOOR AT APPROXIMATELY STATION 170 ABOUT 20 INCHES RIGHT OF FUSELAGE CENTERLINE. -- REMOVED CORROSION FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002121600102 20021216 00102 WP 2002 12 16 MWEA020731 1 20021216 A 5311 9910078215 DOUBLER DOUG DC9 DC915 3022036 WP SAT 165 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 EXISTING REPAIR ON SUBFLOOR AT STATION 165 APPROXIMATELY 10 INCHES RIGHT SIDE FROM CENTERLINE HAS SEVERAL FASTENERS PULL ING THROUGH FLOOR WEB. 2 L 7 2 4F A6WE 2002121600103 20021216 00103 NM 2002 12 16 AALA20020512 1 20020419 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 654A 24612 DFW - LEFT NR 2 DOOR OUTSIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121600104 20021216 00104 NM 2002 12 16 AALA20020513 1 20020420 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 183AN 29593 DFW - FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE FROM SEAT ROW 17 THROUGH 34. REPLACED BATTERY PACK AND MODULE AT R2 DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121600105 20021216 00105 NM 2002 12 16 AALA20020526 1 20020423 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 601AN 27052 DFW - EMERGENCY PATH LIGHTING INOPERATIVE AT ROW 4. RESEATED CONNECTOR FOR EMERGENCY PATH LIGHTING. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121600106 20021216 00106 NM 2002 12 16 AALA20020544 1 20020425 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 649AA 24607 DFW - AFT AISLE EMERGENCY LIGHTS ARE MORE BRIGHT FROM THE EXIT ROWS BACK THAN FROM THE EXIT ROWS FORWARD. REMOVED AND R EPLACED FORWARD BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121600107 20021216 00107 NM 2002 12 16 AALA20020551 1 20020426 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 642AA 24600 DFW - CEILING EXIT LOCATOR SIGN AT ROW 17 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121600108 20021216 00108 WP 2002 12 16 AALA20021425 1 20020930 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 TUL - FOUND RIGHT W/W DOOR LAND CRACKED AT AFT OUTBOARD CORNER. INSTALLED DOUBLER PER SRM 53-01 FIG 2, STOP DRILL CRACK . (M) 2 L 7 2 4F A6WE 2002121600109 20021216 00109 NM 2002 12 16 AALA20021440 1 20021012 A 7714 GEN3004 TACH GENERATOR BOEING 757 757223 1384957 NM RT ENGINE FAILED A AALA K NONE O OTHER CR CRUISE 1 SW 21 183AN 29593 LAX - RIGHT ENGINE N3 INDICATION. RIGHT N3 INOPERATIVE. REPLACED RIGHT ENGINE N3 TACH GENERATORS, GROUND CHECKS NORMAL . (M) 2 L 7 2 4F RT A2NM 2002121600110 20021216 00110 NM 2002 12 16 AWXA200201203 1 20021124 A 5312 65163007 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 0 0 23777 MCN - MAJOR REPAIR - DURING C-14 CHECK A 1/4" CRACK WAS FOUND ON BS 178 BULKHEAD WEB, LBL 4.7, WL 210, AT EDGE OF REINFO RCEMENT STRAP. MAINTENANCE CUTOUT DAMAGE AREA OF CRACKED WEB BS 178, LBL 4.7, WL 210; FABRICATED A REPAIR DOUBLER; INSTA LLED REPAIR IAW B737-300 SRM 53-10-08, PG. 287-288, FIG. 211. 2 L 7 2 4F RT A16WE 2002121600111 20021216 00111 NE 2002 12 16 MALA020683 2 20021215 A 7220 LF5071F ENGINE BAC 146 AVRO146RJ85A 1500097 EU LF507 LF5071F NE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 502XJ E2307 AFTER DEPARTING MSP ON FLIGHT #3625, CAPT FROM 502XJ CALLED MAINTENANCE CONTROL, WITH THE FOLLOWING INFORMATION. #2 ENG INE N1 85.5, N2 93.2, EFT 608. MAINTENANCE CONTROL HAD CREW MOVE POWER LEVER UP LOOKING FOR INCREASE IN THE TEMP WITH V ERY LITTLE CHANGE IN N1. THEORY PROVED TO BE CORRECT. AIR RETURN TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE SUSPECTS BLEED BAND. MAINTENANCE REPLACED #2 ENG P/N ON/OFF LF507-1F S/N ON PO7791 S/N OFF LF07650 IAW AML JC 7100-502. 2 H 7 4 4F 4 F RT A49EU E6NE 2002121600112 20021216 00112 NM 2002 12 16 QXEA0202164 1 20021210 A 3260 858601 PSEU DHAV DHC8 DHC8202 2809007 NM ZONE 700 FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 345PH 7075 7075 476 SEA- LANDING GEAR INOPERATIVE CAUTION LIGHT ILLUMINATED. LEFT MAIN GEAR DOOR OPENED IN FLIGHT AND REMAINED OPEN. AIRCRAF T LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PSEU. OPERATIONAL CHECLS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002121700003 20021217 00003 SO 2002 12 17 JG12002F00000 1 20021107 A 3246 WHEEL GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU MLG CRACKED B JG1R K NONE O OTHER IN INSP/MAINT 1 EA 25 577VU 1385 WHEEL HUB CRACKED AT BRAKE DRIVE BAR BOLT HOLE AT 4-5 OCLOCK POSITION. FOUND HORIZONTAL GROOVE IN SPACER. 2 L 7 2 4F 4 F RT A12EA E25NE 2002121700004 20021217 00004 2002 12 17 ON929ML112602 4 20021126 A 3421 258733513 GYRO AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE73131C 01518 NE COCKPIT FAILED E AOQA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 11 929ML 9549 92 AUTOPILOT PITCHES NOSE DOWN WHEN ENGAGED IN CRUISE FLT. REMOVED NR 1 VERTICAL GYRO AND INSTALLED OVERHAULED UNIT. OPS CHECK GOOD. 2 L 7 3 4F 4 F A46EU E6WE 2002121700005 20021217 00005 NM 2002 12 17 P9R2002F00011 1 20021027 A 2751 INDICATOR BOEING 727 7272J4 1384006 NM PWA JT8 JT8D NE TE FLAPS DEFECTIVE A P9RA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 11 288SC 20765 ON TAXI OUT, THE INBOARD FLAP INDICATOR DISPLAYED ASSYMETRIC CONDITION. FLAPS LOCKED OUT. RETURNED TO GATE. RESET FLA P INDICATION SYSTEM IAW MM. OPS CHECK GOOD. THERE WERE NO EMERGENCY MEASURES EXECUTED. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121700006 20021217 00006 NM 2002 12 17 P9R2002F00012 1 20021028 A 3350 SG9422 LIGHT BOEING 727 727200 138407E NM PWA JT8 JT8D17 52049 NE CABIN MISSING A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 910PG 22606 PHOTOLUMINISCENT STRIP AT G2 MISSING. RESECURED PHOTOLUMINISCENT STRIP AT G2. THE CAUSE OF THE MALFUNCTION WAS THE PHO TOLUMINESCENT STRIP COMING UNGLUED FROM FLOOR. THERE WERE NO EMERGENCY MEASURES EXECUTED. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121700007 20021217 00007 NM 2002 12 17 P9R2002F00013 1 20021101 A 2560 PA01002 BATTERY PACK BOEING 727 727231 1384079 NM PWA JT8 JT8D9 52048 NE FLASHLIGHT FAILED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 54344 21631 FORWARD F/A STATION RIGHT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED POWERLIGHT IAW MM, OPS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2002121700008 20021217 00008 NM 2002 12 17 P9R2002F00014 1 20021101 A 3350 900835A BATTERY PACK BOEING 727 727231 1384079 NM PWA JT8 JT8D9 52048 NE CABIN FAILED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 54344 21631 AFT AISLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD IAW MM. 2 L 7 3 4F 4 F A3WE E2EA 2002121700009 20021217 00009 NM 2002 12 17 P9R2002F00015 1 20021107 A 2781 40174 SWITCH BOEING 727 727200 138407E NM PWA JT8 JT8D17 52049 NE NR 5 KRUGER FLAP FAILED A P9RA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 11 919PG 22604 ON FLAP RETRACTION, NR 5 KRUGER FLAP WOULD NOT RETRACT. LED LIGHT INDICATED NR 5 EXTENDED. INSPECTION ON GROUND INDICA TED FLAP WAS FULLY RETRACTED. REPLACED THE NR 5 KRUGER FLAP SWITCH IAW MM. OPS CHECK GOOD. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121700010 20021217 00010 NM 2002 12 17 P9R2002F00016 1 20021112 A 3350 1102833 LIGHT BOEING 727 727231 1384079 NM PWA JT8 JT8D9 52048 NE CABIN INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 54344 21631 DURING "A" CHECK FOUND EMERGENCY LIGHT INOPERATIVE AT CENTER AISLE STATION 720. REMOVED AND REPLACED EMERGENCY LIGHT AT STATION 720. OPS TESTED NORMAL IAW MM. 2 L 7 3 4F 4 F A3WE E2EA 2002121700011 20021217 00011 NM 2002 12 17 P9R2002F00017 1 20021114 A 3230 CONTROL CABLE BOEING 727 727231 1384079 NM PWA JT8 JT8D9 52048 NE RT MLG OUT OF ADJUST A P9RA O OTHER J WARNING INDICATION DE DESCENT 1 SO 11 54344 21631 DURING DESCENT, RT MLG DOOR OPENED, GEAR HANDLE IN OFF POSITION, DOOR RED LIGHTS ON FWD PANEL ILLUMINATED AS WELL AS RT MLG LIGHT. ADUSTED RT MLG RELEASE CABLES IAW MM. OPS CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2002121700012 20021217 00012 CE 2002 12 17 QC42002F00002 1 20021022 A 5610 10138402521 WINDSHIELD BEECH B300 B300 1159232 CE PWA PT6 PT6* 52043 EA COCKPIT FAILED B QC4R A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SO 01 160AC 1472 FL215 PILOT WINDSHIELD INNER PANE SHATTERED WHILE IN FLIGHT. THE OUTERPANE HELD WITH NO PROBLEM AND THE COPILOT WAS ABLE TO L AND THE PLANE SAFELY. INSPECTION OF THE WINDSHIELD AFTER REMOVAL SHOWED NO OBVIOUS DAMAGE OR CHIPS IN THE OUTER PANE T HAT WOULD HAVE LEAD TO THE INNER PANE FAILURE. SOP IS TO TURN ON THE WINDSHIELD HEAT WHEN PASSING THROUGH 18,000 FEET. THE FAILED WINDSHIELD WAS ORIGINAL EQUIPMENT AND HAD 1472.8 HOURS AND 1713 LANDINGS. 2 L 7 2 4T 3 T RT A24CE E2NE 2002121700013 20021217 00013 EU 2002 12 17 UHL2002F00007 1 20021026 A 2450 A2043C PDU SAAB SF340 SF340A 7850100 EU RT MAIN BUSS INOPERATIVE A UHLA K NONE O OTHER IN INSP/MAINT 1 NE 03 101CN 340A101 DURING APPROACH, PILOT REPORTED LOSS OF RT EFIS BUSS, RT MAIN BUSS RESULTING IN LOSS OF FIRST OFFICERS EFIS TUBE, PILOT ABORTED LANDING AND RETURNED. MAINTENANCE REPLACED RT PDU, NO FURTHER PROBLEMS, A/C RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2002121700014 20021217 00014 EU 2002 12 17 UHL2002F00008 1 20021127 A 3250 CIRCUIT BREAKER SAAB SF340 SF340A 7850100 EU NLG STEERING TRIPPED A UHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NE 03 101CN 340A101 ON TAXI OUT, PILOT REPORTED NLG STEERING CIRCUIT BREAKER POPPED. AIRCRAFT RETURNED TO GATE. 2 L 7 2 4T RT A52EU 2002121700015 20021217 00015 EU 2002 12 17 UHL2002F00009 1 20021201 A 6120 1103P0620 PRESSURE SWITCH SAAB SF340 SF340A 7850100 EU GE CT7TP CT79B 30030 NE AUTOCOARSEN INOPERATIVE A UHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NE 03 123XS 340A123 PILOT REPORTS AUTOCOARSEN SYSTEM FAILED ON TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE. MECHANIC PERFORMED GROUND RUN ON A UTOCOARSEN SYSTEM ADJUSTMENT & TEST IAW MM. OPS CHECKED GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2002121700016 20021217 00016 EU 2002 12 17 UHLA10081 1 20021205 A 6120 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE AUTOCOURSEN ILLUMINATED A UHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NE 03 123XS 340A123 DURING TAKEOFF ROLL, PILOT REPORTED AT 60 KNOTS THE AUTOCOURSEN LIGHT ON CWP ILLUMINATED. ABORTED AND RETURNED TO GATE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002121700017 20021217 00017 EA 2002 12 17 UHLA110941 1 20021205 A 6120 CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA GE CT7TP CT75A2 30030 NE AUTOCOARSEN INOPERATIVE A UHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NE 03 340CA 10062 PILOT REPORTED THAT THE AUTOCOARSEN SYSTEM WOULD NOT ARM DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED. 2 L 7 2 4F 4 T RT A21EA E8NE6 2002121700018 20021217 00018 SO 2002 12 17 WVBA20022017 1 20021211 A 7810 LW16620 EXHAUST PIPE PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA RT ENGINE BROKEN E WVBA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 AL 01 792FC 1544 317552108 L267368A A REJECTED TAKEOFF. PILOT DETERMINED THAT THE RT ENGINE WAS NOT MAKING MANIFOLD PRESSURE OR RPM. AFTER RETURNING, IT W AS DISCOVERED THAT THE RT EXHAUST PIPE WAS BROKEN AT THE FLANGE. THE PIPE WAS REPLACED AND THE AIRCRAFT INSPECTED FOR EX HAUST DAMAGE. THE PLANE WAS RUNUP AFTER THE REPAIR AND OPERATIONS CHECK WAS NORMAL. 1 L 7 2 3O 3 O A20SO E14EA 2002121700022 20021217 00022 SW 2002 12 17 ALGA081611 1 20021210 A 6320 204040132001 BEARING RACE BELL 407 407 1182206 SW TRANSMISSION FAILED H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 5NBEP A47 53107 TRANSMISSION HAS METAL IN OIL. BEARING RACE FAILURE 1 G 7 1 3U O H2SW 2002121700023 20021217 00023 SW 2002 12 17 ALGA081615 1 20021211 A 6510 407340340103 DISC PACK BELL 407 407 1182206 SW TAIL ROTOR CRACKED H K NONE O OTHER IN INSP/MAINT 1 FS 01 58236 53069 THE DISC PACK IS CRACKED. 1 G 7 1 3U O H2SW 2002121700024 20021217 00024 EU 2002 12 17 ALGA081616 1 20021211 A 6510 C651A2001101 DISC PACK UROCOP EC120 EC120B 8680987 EU TAIL ROTOR CRACKED H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 524AL 506 1263 FOUND THE DISC PACK CRACKED. 1 G 7 2 3U NC R0001RD 2002121700025 20021217 00025 SW 2002 12 17 ALGA081620 1 20021211 A 6420 406312100101 BEARING BELL 407 407 1182206 SW T/R HUB WORN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 437AL 428 A152 53141 FOUND 4 EA. TAIL ROTOR YOKE BEARINGS WORN. AXIAL PLAY. 1 G 7 1 3U O H2SW 2002121700027 20021217 00027 SW 2002 12 17 ALGA081622 1 20021211 A 6300 406310405101 UNIVERSAL BELL 407 407 1182206 SW MAIN ROTOR WORN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 627AL 868 53284 FOUND BEARINGS WORN. BEARING HAS A 5000 HR. RETIREMENT LIFE. 1 G 7 1 3U O H2SW 2002121700028 20021217 00028 SW 2002 12 17 ALGA081623 1 20021211 A 6300 406310405101 UNIVERSAL BELL 407 407 1182206 SW MAIN ROT.RO WORN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 404AL 858 53479 FOUND BEARINGS WORN. BEARING HAS A 5000 HR. RETIREMENT LIFE. 1 G 7 1 3U O H2SW 2002121700030 20021217 00030 SW 2002 12 17 ALGA081625 1 20021211 A 6300 406310405101 UNIVERSAL BELL 407 407 1182206 SW MAIN ROTOR WORN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 547AL 199 53240 FOUND BEARINGS WORN. BEARINGS HAS A 5000 HR. RETIREMENT LIFE. 1 G 7 1 3U O H2SW 2002121700031 20021217 00031 SW 2002 12 17 ALGA081626 1 20021211 A 6300 406310405101 UNIVERSAL BELL 407 407 1182206 SW MAIN ROTOR WORN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 409AL 150 53494 FOUND BEARINGS WORN. BEARING HAS A 5000 HR. RETIREMENT LIFE. 1 G 7 1 3U O H2SW 2002121700032 20021217 00032 SW 2002 12 17 ALGA081627 1 20021211 A 6300 406310405101 UNIVERSAL BELL 407 407 1182206 SW MAIN ROTOR WORN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 527AL 1537 53211 FOUND BEARINGS WORN. BEARINGS HAS A 5000 HR RETIREMENT LIFE. 1 G 7 1 3U O H2SW 2002121700033 20021217 00033 SW 2002 12 17 ALGA081629 1 20021211 A 6300 406310405101 UNIVERSAL BELL 407 407 1182206 SW MAIN ROTOR WORN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 1116H 2650 53046 FOUND BEARINGS WORN. BEARINGS HAS A 5000 HR. RETIREMENT LIFE. 1 G 7 1 3U O H2SW 2002121700035 20021217 00035 SW 2002 12 17 ALGA081634 1 20021212 A 6320 412010182101 BEARING BELL 412 412 1182202 SW M/R GEARBOX WORN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 9YTJM 3240 33159 MAIN ROTOR GEARBOX BEARING HAS AXIAL PLAY THAT EXCEEDS ALLOWABLE LIMITS, PART DID NOT REACH ITS LIFE EXPECTANCY OF 5000H RS. 1 G 7 2 4U H4SW 2002121700036 20021217 00036 SW 2002 12 17 ALGA081635 1 20021212 A 6320 412010182101 BEARING BELL 412 412 1182202 SW M/R GEARBOX WORN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 9YTJM 3240 33159 MAIN ROTOR GEARBOX BEARING HAS AXIAL PLAY THAT EXCEEDS ALLOWABLE LIMITS, BEARINGS LIFE EXPECTANCY DID NOT REACH 5000HRS. 1 G 7 2 4U H4SW 2002121700037 20021217 00037 EA 2002 12 17 02350644 1 20021216 A 3350 364911 LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 644BR 7379 During preflight inspection, the crew reported that the forward section of emergency floor track lighting was inoperativ e. Maintenance personnel removed and replaced the forward emergency floor track lamp and harness. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002121700038 20021217 00038 SW 2002 12 17 ALGA081636 1 20021212 A 6320 412010182101 BEARING BELL 412 412 1182202 SW M/R GEARBOX WORN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 9YTJM 3240 33159 MAIN ROTOR GEARBOX BEARING HAS AXIAL PLAY THAT EXCEEDS ALLOWABLE LIMITS, BEARING DID NOT REACH ITS EXPECTED 5000HR LIFE. 1 G 7 2 4U H4SW 2002121700039 20021217 00039 NM 2002 12 17 DL733021367 1 20021125 A 5342 65495587 FITTING BOEING 737 737347 1384647 NM 48 SECTION CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 CORROSION WAS FOUND IN THE LUB BORE OF THE LHS FORWARD CLEVIS LUG. THE LUG BORE WAS OVERSIZED TO 1.4385" AND AN OVERSIZED BUSHING WAS INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2002121700040 20021217 00040 NM 2002 12 17 DL733021368 1 20021125 A 5315 SKIN PANEL BOEING 737 737347 1384647 NM KEEL BEAM CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 SEVERAL CRACKS WERE FOUND IN THE KEEL BEAM LOWER SKIN PANEL FROM FS 661 TO FS 727. THE SKIN PANEL WAS REPLACED PER S/B 737-53-1104. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2002121700041 20021217 00041 NM 2002 12 17 DL733021369 1 20021125 A 5553 56468725 ATTACH FITTING BOEING 737 737347 1384647 NM VERT. STAB. CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 CORROSION WAS FOUND ON THE AFT FACE OF THE #3 LUG AND THE FORWARD FACE OF THE #6 LUG OF THE VERTICAL STABILIZER FIN ATTACH LUGS. THE CORROSION WAS REMOVED AND NEW BUSHINGS INSTALLED. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2002121700042 20021217 00042 NM 2002 12 17 DLM11021379 1 20021125 A 5330 AJC705949 SKIN DOUG MD11 MD11 3023602 NM FS 2140, L-36R PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 813DE 48600 FUSELAGE / SKIN / FS 2122-2145 / LONG. 36R-37R : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS PUNCTURED BETWEEN FS 2122 & 2145 AND BETWEEN LONGERONS 36R & 37R WHEN THE AIRCRAFT STRUCK A MTC. WORK STAND. THE DAMAGE WAS REMOVED WITH A 24" X 6" CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 384123-14, REV A. 2 L 7 3 4F RT A22WE 2002121700043 20021217 00043 NM 2002 12 17 DL767021395 1 20021201 A 7100 CF680A2 ENGINE BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE #1 ENGINE FAILED A DALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 27 103DA 46005 4384 22215 580108 LEFT ENG SURGE IN FLIGHT AND ON LANDING. ENG SHUT ITSELF DOWN ON LANDING AT 5 THOUSAND FT. ENG CHANGE IS IN WORK 2 L 7 2 4F 4 F RT A1NM E13NE 2002121700044 20021217 00044 NM 2002 12 17 DLM11021397 1 20021129 A 5751 NRC6043501 AILERON DOUG MD11 MD11 3023602 NM LH WING PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 813DE 48600 WING / LH / INBD AILERON / INBD TRAILING EDGE : GROUND DAMAGE REPAIR THE UPPER SKIN, TRAILING EDGE WEDGE, AND INBD CLOSEOUT RIB OF THE LH WING INBD AILERON WERE DAMAGED WHEN THE AIRCRAFT STRUCK A MTC. WORK STAND. THE DAMAGED SECTION OF UPPER SKIN WAS CUT AND REMOVED AND A NEW SECTION SPLICED IN WITH AN ALUMINUM DOUBLER. NEW SECTIONS OF RIB CAP WERE SPLICED IN WITH ALUMINUM ANGLES, AND THE WEDGE SECTION REPLACED. THE REPAIR WAS ACCOMPLISHED PER ER/A 418035-14, REV A. 2 L 7 3 4F RT A22WE 2002121700045 20021217 00045 NM 2002 12 17 DLM11021398 1 20021129 A 5330 AJC7207519 SKIN DOUG MD11 MD11 3023602 NM FS 2000, L-46L PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 813DE 48600 FUSELAGE / SKIN / FS 1997-2015 / L-45L-47L : GROUND EQUIPMENT PUNCTURE REPAIR THE FUSELAGE SKIN WAS PUNCTURED BY A WORK STAND BETWEEN FS 1997 & 2015 AND BETWEEN LONGERON 45L & 47L. THE DAMAGE WAS REMOVED WITH A 19" X 6" CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER ER/A 384125-14, REV A. 2 L 7 3 4F RT A22WE 2002121700046 20021217 00046 NE 2002 12 17 DL76K021408 2 20021205 A 7200 9381M17G85 PANEL BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE #1 ENGINE DAMAGED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 178DZ 30596 706131 _ON TAKE OFF FROM LGA A/C BEHIND FLT 471 NOTICED PANEL DEPA RTING A/C. PART RETREIVED WAS FOUND TO BE ACOUSTICAL PANEL F ROM FAN EXIT CASE. A/C DIVERTED TO JFK DUE TO ENGINE VIBRATION REPLACED PANEL AND BRACKETS. 2 L 7 2 4F 4 F RT A1NM E13NE 2002121700047 20021217 00047 NM 2002 12 17 DL777021411 1 20021205 A 3610 32153024 VALVE UNK BOEING 777 777232 1385232 NM LEFT ENG INOPERATIVE A DALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 27 860DA 9142 29951 LEFT ENG BLEED INOP. R/R LEFT ENG PRSOV PER M/M AND RAN ENG CHECK GOOD PER M/M 36-10-00-5 ETOPS CATEGORY 'B': DIVERSION OR TURNBACK 2 L 7 2 4F RT T00001SE 2002121700048 20021217 00048 NM 2002 12 17 DL72S021413 1 20021205 A 5700 ANGLE BOEING 727 727225A 1384077 NM NO.12 SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 NO. 12 SPOILER ACTUATOR ATTACH BRACKET CRACKED OUT BOARD ENDREPLACED ATTACH ANGLE 2 L 7 3 4F RT A3WE 2002121700049 20021217 00049 NM 2002 12 17 DLM88021415 1 20021205 A 2560 487191 SPLICE DOUG MD88 MD88 3023688 NM 1L DOOR BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 928DL 49715 ON INSPECTION FOUND EMERGENCY EXIT LIGHT AT 1L DOOR INOP RELAMPED-NO HELP. FOUND WIRES DISCONNECTED BEHIND DOOR CLOS EOUT PANELS. REMOVED PANELS AND REPAIRED QUICK DISCONNECT CONNECTORS ON LIGHT ASSY. OPN OF LIGHT NORMAL. REPLACED REM OVED CLOSEOUT PANELS. 2 L 7 2 4F RT A6WE 2002121700050 20021217 00050 NE 2002 12 17 DLM88021417 2 20021206 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE #1 ENGINE FAILED A DALA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SO 27 989DL 36230 0 53341 718128 ON DEPARTURE FROM HOU ON FLT 0532 LT ENGINE FAILED AT 10500 FT. RETURNED TO HOU. ENGINE OIL PRESS WENT TO -0- AFTER FAILURE WINDMILLED FOR 12-18 MINS WITH -0- OIL PRESS. ENGINE CHANGE REQURIED DUE TO -0- OIL PRESS 2 L 7 2 4F 4 F RT A6WE E9NE 2002121700051 20021217 00051 NM 2002 12 17 DLM88021426 1 20021210 A 3200 AS15308K0254 LINE DOUG MD88 MD88 3023688 NM TAIL LEAKING A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 914DE 49957 DURING CRUISE AT FL370 RT HYD DECREASED TO 7 QTS. DURING RT SYSTEM HYD FAILURE CK LIST, HYD QTY DECREASED TO 4 QTS. FO UND #2 PRESSURE LINE TO CASE DRAIN FILTER LEAKING - REPLACED SAME 2 L 7 2 4F RT A6WE 2002121700052 20021217 00052 NM 2002 12 17 DL72S021436 1 20021210 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM S-4R, FS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 FUSELAGE / SKIN / FS 481-681 / STRG. 4R / SKIN LAP JOINT : CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R LAP JOINT REVEALED CRACK INDICATIONS BETWEEN FS 481 & 681. INTERNAL MFEC INSPECTION CONFIRMED A TOTAL OF 14 CRACKS ALONG THE LOWER ROW OF FASTENERS IN THE LOWER SKIN. THE ENTIRE PANEL LAP JOINT WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 384192-14AD. 2 L 7 3 4F A3WE 2002121700053 20021217 00053 NM 2002 12 17 DL73K021443 1 20021213 A 5330 6545767531 SKIN BOEING 737 737247 138448D NM FS 390, S-17L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 374DL 23521 FUSELAGE / SKIN / FS 370-400 / STRG. 17L-18L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS DENTED AT FS FS 395 BETWEEN STRINGERS 17L & 18L. THERE WAS AN ADJACENT SKIN REPAIR WITHIN 10" OF THE DENT. THE EXISITING REPAIR WAS REMOVED AND UNDERLYING CUTOUT INSPECTED. THE DENT WAS REMOVED WITH A 7" X 9" CUTOUT. BOTH CUTOUTS WERE REPAIRED WITH 2 ALUMINUM REPAIR DOUBLERS PER ER/A 384249-14, REV B. 2 L 7 2 4F A16WE 2002121700054 20021217 00054 NM 2002 12 17 DL757021445 1 20021217 A 2620 M982480 BOTTLE BOEING 757 757232 1384965 NM AFT LEFT UNSERVICEABLE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 654DL 24394 IR WATER FIRE EXTINGUISHER AT AFT LEFT JUMPSEAT HAS BROKEN SEAL CA REPLACED H2O FIRE BOTTLE 2 L 7 2 4F RT A2NM 2002121700055 20021217 00055 SW 2002 12 17 ALGA081637 1 20021212 A 6320 412010182101 BEARING BELL 412 412 1182202 SW M/R GEARBOX WORN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 9YTJM 3240 33159 MAIN ROTOR GEARBOX BEARING HAS AXIAL PLAY THAT EXCEEDS ALLOWABLE LIMITS, BEARING DID NOT REACH ITS EXPECTED LIMITS. 1 G 7 2 4U H4SW 2002121700056 20021217 00056 EA 2002 12 17 COMA0260712 1 20021213 A 3010 WING CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 SO 01 984CA 7171 FLIGHT 5229 ANTI-ICE DUCT WARNING.COULD NOT DUPLICATE. INSPECTED BLEED LEAK SENSORS AND WIRING. 2 L 7 2 4F RT A21EA 2002121700057 20021217 00057 NE 2002 12 17 BAQA081133 2 20021011 A 7314 430137703 PUMP BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101650B1 41560 NE FUEL SYSTEM FAILED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 955ME 454 7243 FUEL PUMP FAILURE, SUSPECTED BLUE GREASE WASHOUT. 453.8 HOURS SINCE LAST COMPLIANCE WITH ASB LTS101-73-0168. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U 3 U H13EU E5NE 2002121700058 20021217 00058 EU 2002 12 17 BAQA081226 1 20021107 A 6320 L632M1001966 TRANSMISSION UROCOP EC135 EC135T1 5620026 EU MAIN ROTOR MAKING METAL H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 136MH 0161 REMOVED FOR METAL CHIP EVENTS. THE MAIN TRANSMISSION WAS SENT DIRECTLY FROM WASHINGTON D.C. TO AEC. THE HARD CARD IS W ITH THE UNIT. 1 G 7 2 3U H88EU 2002121700059 20021217 00059 NM 2002 12 17 DL72S021376 1 20021123 A 5753 SHIM BOEING 727 727232 1384082 NM FLAP TRACK OUT OF POSITION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 REPAIR FOR MIGRATED SHIM, INSPECTION OF LT WING INBD FLAP INBD FLAP TRACK REVEALED A MIGRATED LAMINATED SHIM. THE CONDI TION IS TYPICAL OF THAT DOCUMENTED PER BAC S/B 727-57-0178 AND AD 90-07-05. THE SHIM WAS MIGRATED BEYOND THE ALLOWABLE LIMITS OF THE S/B AND WAS REPLACED PER THE S/B INSTRUCTIONS AND PER ER/A 384219-14AD. 2 L 7 3 4F A3WE 2002121700060 20021217 00060 EA 2002 12 17 COMA0260713 1 20021213 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA R/H MALFUNCTIONED A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 938CA 9631 7046 FLIGHT 5218 FLAPS FAILED AT 0 DEGREES.REPLACED THE R/H BPSU. 2 L 7 2 4F RT A21EA 2002121700061 20021217 00061 NM 2002 12 17 DL72S021378 1 20021125 A 5210 HANDLE BOEING 727 727232 1384082 NM L2 DOOR BROKEN A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 533DA 22046 L2 DOOR UPPER CRANK BROKE WHILE CLOSING DOOR, ROD ALSO DAMAGED SHEET METAL ON DOOR. REPLACED DOOR. 2 L 7 3 4F A3WE 2002121700062 20021217 00062 EA 2002 12 17 COMA0260714 1 20021213 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 486CA 7707 FLIGHT 5115 FLAPS FAILED AT 26 DEGREES DURING TAXI.ADJUSTED FLAP RIGGING TO C/W M/M LIMITS. 2 L 7 2 4F RT A21EA 2002121700063 20021217 00063 2002 12 17 BAQA081532 4 20021126 A 3416 3A433220F281CL ALTIMETER UROCOP EC135 EC135T1 5620026 EU COCKPIT OUT OF TOLERANCE H BAQA O OTHER O OTHER NR NOT REPORTED 1 FS 01 135MH 1686 0131 ALTIMETER OUT OF TOLERANCE +120 FT. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2002121700064 20021217 00064 EU 2002 12 17 BAQA081557 1 20021202 A 2842 L284M30C1001 PROBE UROCOP EC135 EC135P1 8680990 EU FUEL CELL FAILED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 577LF 269 0140 FUEL QUANTITY DEGRADE ON DISPLAY. TEST INDICATED BAD PROBE FROM AFT TANK. 1 G 7 2 3U O H88EU 2002121700065 20021217 00065 EU 2002 12 17 BAQA081571 1 20021203 A 2822 1176415103 PUMP BOLKMS 117 BK117A3 5626015 EU FUEL BOOST INOPERATIVE H BAQA O OTHER O OTHER NR NOT REPORTED 1 FS 01 911BK 759 7099 BOOST PUMP INOPERATIVE. SHORTED. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002121700066 20021217 00066 EU 2002 12 17 BAQA081591 1 20021206 A 2435 23081043 STARTER GEN BOLKMS BK117 BK117C1 5626025 EU ENGINE FAILED H BAQA O OTHER O OTHER NR NOT REPORTED 1 FS 01 911TG 169 7506 BELIEVE INTERNAL MALFUNCTION. BRUSHES LOOK GOOD. NO GENERATION. THIS STARTER GENERATOR WAS INSTALLED 7/1/02 AND ONLY HAS 168.5 HOURS. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U NC H13EU 2002121700067 20021217 00067 NM 2002 12 17 DL72S021389 1 20021129 A 3350 0201720001 LIGHT BOEING 727 727232 1384082 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 EMERGENCY FLOOR LIGHT DAMAGED AT SEAT ROW 22 DEF. REPLACED LIGHT ASSY, OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 2002121700068 20021217 00068 2002 12 17 BAQA081592 4 20021206 A 3455 066107204 RECEIVER BOLKMS 117 BK117B1 5626012 EU ADF SYSTEM INTERMITTENT H BAQA O OTHER O OTHER NR NOT REPORTED 1 FS 01 945ME 270 7235 ADF RECEIVER DISPLAY IS INTERMITTENT. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002121700069 20021217 00069 2002 12 17 BAQA081595 4 20021209 A 3421 4021541791 INDICATOR BOLKMS 117 BK117A1 5626010 EU COCKPIT CONTAMINATED H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 955ME 1658 7243 ARTIFICIAL HORIZON INDICATOR GLASS FOGGED. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002121700071 20021217 00071 EU 2002 12 17 BAQA081599 1 20021209 A 2822 1176415103 PUMP BOLKMS 117 BK117B2 5626013 EU FUEL BOOST INOPERATIVE H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 296GL 7222 BOOST PUMP INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U NC H13EU 2002121700072 20021217 00072 EU 2002 12 17 BAQA081600 1 20021209 A 2435 524031 STARTER GEN AEROSP AS365 AS365N2 8680815 EU ENGINE INOPERATIVE H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 915ME 365 6417 STARTER GENERATOR WILL NOT TURN. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U RT H10EU 2002121700073 20021217 00073 EU 2002 12 17 BAQA081603 1 20021209 A 3610 97924011 SHUTOFF VALVE BOLKMS 117 BK117A4 5626017 EU BLEED SYS INTERMITTENT H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 9024Z 4821 7134 SHUTOFF VALVE INTERMITTENT. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002121700074 20021217 00074 EU 2002 12 17 BAQA081604 1 20021210 A 6240 11794564 INDICATOR BOLKMS 117 BK117A4 5626017 EU MAST MOMENT INOPERATIVE H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 911WJ 874 7050 INDICATOR INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H13EU 2002121700075 20021217 00075 NM 2002 12 17 DL72S021391 1 20021130 A 2782 10605594 ACTUATOR BOEING 727 727232 1384082 NM L/E SLAT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 518DA 21469 AFTER T/O AMBER LED LIGHT REMAINED ILLUMINATED AT FLAPS 2. POSITION TEST SHOWED NR 4 L/E DEVICE NOT RETRACTED. REPLACE D NR 4 SLAT ACTUATOR. 2 L 7 3 4F A3WE 2002121700076 20021217 00076 NM 2002 12 17 DL72S021405 1 20021203 A 3350 900835A BATTERY PACK BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8875Z 21293 LT OVERWING EMERGENCY LIGHT AT FWD MOST POSITION IS INOP. REPLACED BATTERY PACK OPERATES NORMAL. 2 L 7 3 4F RT A3WE 2002121700077 20021217 00077 2002 12 17 DL72S021433 4 20021211 A 3436 3186304951008 MODULE BOEING 727 727225A 1384077 NM COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 8875Z 21293 AFTER LEVEL OFF AT 330 ALL BUT 3 OR 4 LIGHTS ON FWD INST PANEL CAME ON. COULD NOT ISOLATE PROBLEM. LIGHTS WENT OUT AFT ER 10 MIN AND COCKPIT WAS FILLED WITH STRONG BURNING ELECTRICAL SMELL. WENT TO 02. LANDED ASAP. FOUND WINDSHEAR DC C/ B OUT. DURING WINDSHEAR TEST NUMEROUS LIGHTS ON INST PANEL FLASH. FOUND CAPT RED WINDSHEAR LIGHT MODULE BURNED UP. RE PL AMBER AND RED MODULES. REPL MASTER DIM AND TEST MODULE AS PRECAUTION. WINDSHEAR AND MASTER DIM AND TEST CK GOOD PER MM. WINDSHEAR DC C/B RESET. 2 L 7 3 4F RT A3WE 2002121700078 20021217 00078 NM 2002 12 17 DL733021365 1 20021125 A 5753 6746486155 WEDGE BOEING 737 737347 1384647 NM T/E FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 TE WEDGE DISBONDED. REPAIRED PER ER/A 418046-14. 2 L 7 2 4F RT A16WE 2002121700079 20021217 00079 EU 2002 12 17 MALA020684 1 20021212 A 3350 BATTERY PACK SAAB SF340 SF340A 7850100 EU A MALA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 GL 15 31XJ 340A031 EMERGENCY LIGHT AT 41LN, 42LN, 43LN, 3LN,4LN, 49LN, 50LN WOULD NOT COME ON. MAINTENANCE FOUND POWER SUPPLY/BATTERY PACK 24LN TO BE AT FAULT. NO OTHER INFORMATION AT THIS TIME. 2 L 7 2 4T RT A52EU 2002121700080 20021217 00080 EU 2002 12 17 MALA020686 1 20021216 A 2420 51634002 GCU SAAB SF340 SF340A 7850100 EU A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 27XJ 340A027 DURING FLIGHT #3367, RH AC GEN FELL OFF LINE, CREW RESET THEN IT FELL OFF LINE SHORTLY AFTER. AIR RETURN TO MSP. MAINT ENANCE CND, SWAPPED AC GCU'S SIDE TO SIDE PN 51634-002, SN/ON RH SIDE, 97005, SN/ON LH SIDE 96036. OPS CHECK GOOD. IAW S AAB AMM 24/21/10. INSPECTION OF RH AC GEN SHAFT SHEER SECTION AND CLAMP POSITION GOOD. 2 L 7 2 4T RT A52EU 2002121700081 20021217 00081 GL 2002 12 17 BAQA081639 2 20021212 A 7200 23057142 ENGINE AEROSP AS355 AS355F2 8680812 EU ALLSN 250C 250C20F 03013 GL ENGINE BAY MALFUNCTIONED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 941MS 4917 5495 ENGINE FAILING POWER CHECK. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U 3 U H11EU E4CE 2002121700082 20021217 00082 NM 2002 12 17 DL733021366 1 20021125 A 5753 6546486156 WEDGE BOEING 737 737347 1384647 NM T/E FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 RH INBD MID FLAP T/E WEDGE DISBONDED. REPAIRED PER ER/A 418047-14. 2 L 7 2 4F RT A16WE 2002121700083 20021217 00083 NM 2002 12 17 DL738021381 1 20021126 A 3350 GE767 LIGHT BOEING 737 737832 13844CF NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3741S 30487 LEFT WING AFT EXTERIOR EMERGENCY LIGHT BULB INOP. RELAMPED. 2 L 7 2 4F RT A16WE 2002121700084 20021217 00084 GL 2002 12 17 BAQA081640 2 20021212 A 7200 ENGINE AEROSP AS355 AS355F2 8680812 EU ALLSN 250C 250C20F 03013 GL ENGINE BAY MALFUNCTIONED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 941MS 7236 5495 ENGINE FAILING POWER CHECK. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U 3 U H11EU E4CE 2002121700085 20021217 00085 NM 2002 12 17 DL73K021384 1 20021127 A 3244 B737N TIRE BOEING 737 737232 1384475 NM NLG FLAT A DALA K NONE O OTHER AP APPROACH 1 SO 27 305DL 23077 IR/ UPON EXTENSION OF GEAR AND 3 GREEN INDICATIONS. SEVERAL SECONDS LATER HEARD A THUMP NOISE. INSPECTED GEAR THROUGH NOSE GEAR PORT AND CONFIRMED GEAR DOWN. EMERGENCY DECLARED MCO. FOUND LEFT NOSE TIRE FLAT. REPLACED BOTH NOSE WHEEL A SSYS PER MM. 2 L 7 2 4F RT A16WE 2002121700086 20021217 00086 EU 2002 12 17 BAQA081641 1 20021212 A 6730 L673M40A1001 ACTUATOR UROCOP EC135 EC135T1 5620026 EU FENESTRON WORN H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 135MH 1686 0131 FENESTRON ACTUATOR ARM WORN. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2002121700087 20021217 00087 2002 12 17 BAQA081651 4 20021213 A 2312 069102525 TRANSCEIVER UROCOP EC135 EC135P1 8680990 EU COCKPIT DAMAGED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 135ME 77 0009 TRANSCEIVER LED'S BURNED OUT. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U O H88EU 2002121700088 20021217 00088 NM 2002 12 17 DL73K021387 1 20021128 A 7931 1163P181 SWITCH BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE FAILED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 322DL 23094 709114 ON CLIMBOUT 20 MIN AFTER T/O NR 2 OIL FILTER BYPASS LIGHT ILLUMINATED. RETARDED THROTTLE, LIGHT ON, SHUTDOWN ENG AND RE TURNED TO MCO. REMOVED AND INSP OIL FILTER/MCD. NO EVIDENCE OF CARBON OR DEBRIS, REPLACED FILTER AND OIL PRESS SWITCH. CLEARED OIL PRESS LINES. NO BLOCKAGE DETECTED. RAN ENG, LK CK GOOD. OPN/PARAMETERS CK GOOD. INLET AND EXHAUST CK N ORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 2002121700089 20021217 00089 GL 2002 12 17 HDNA081647 2 20021212 A 7250 23031938 NOZZLE CLARK 1000 1000CLARK 2230102 SW ALLSN 250C 250C20B 03013 GL 2ND STAGE MISINSTALLED H HDNA K NONE W INADEQUATE Q C IN INSP/MAINT 1 FS 01 PARTO NEWLY OVERHAULED 2ND STAGE NOZZLE. DIAPHRAGM IS IMPROPERLY POSITIONED AND FOWARD TO AFT FLANGE OUT OF LIMITS. RETURNED FOR REPAIR. 1 Q 7 1 3R 3 U 2A6 E4CE 2002121700090 20021217 00090 GL 2002 12 17 HDNA081648 2 20021212 A 7250 6878498 NOZZLE CLARK 1000 1000CLARK 2230102 SW ALLSN 250C 250C20B 03013 GL 2 ND STAGE MISINSTALLED H HDNA K NONE W INADEQUATE Q C IN INSP/MAINT 1 FS 01 PARTO NEWLY OVERHAULED 2ND STAGE NOZZLE. DIAPHRAGM IS IMPROPERLY POSITIONED, FORWARD TO AFT FLANGEDIM. OUT OF LIMITS AND INTE RSTAGE SEAL IMPROPERLY SPRAYED. RETURNED FOR REPAIR. 1 Q 7 1 3R 3 U 2A6 E4CE 2002121700091 20021217 00091 NM 2002 12 17 DL73K021406 1 20021203 A 3610 12924011 REGULATOR VALVE BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE LEAKING A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 244WA 23518 709225 AIR TURNBACK FROM FLL TO BDL, RETURNED TO FLL. BLEED TRIP OFF NR 1 ENG ON TAKEOFF ROLL. REPLACED PRESSURE REGULATOR BL EED LINES FOR LEAKING. 2 L 7 2 4F 4 F A16WE E2EA 2002121700092 20021217 00092 NM 2002 12 17 DL73K021437 1 20021213 A 3350 20121 POWER SUPPLY BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 307DL 23079 EMER LIGHTS INOP ROWS 17-20 AND AFT GALLEY. REPLACED POWER SUPPLY M9222. LIGHTS NOW CHECK GOOD. 2 L 7 2 4F RT A16WE 2002121700093 20021217 00093 EU 2002 12 17 HE66081587 1 20021206 A 2435 COMMUTATOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1B2 60030 NE STARTER GEN WORN H HEEA K NONE L NO TEST IN INSP/MAINT 1 FS 01 135CR 647 0164 30240 STARTER GEN INSPECTED FOR WEAR. WEAR WAS EXCESSIVE, COMMUTATOR WAS EXTREMELY WORN AND GOUGED. REPLACED 1 G 7 2 3U 3 U H88EU E19EU 2002121700094 20021217 00094 EU 2002 12 17 HE66081588 1 20021206 A 2435 23081057 STARTER GEN UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1B2 60030 NE NR 2 ENGINE WORN H HEEA O OTHER L NO TEST TX TAXI/GRND HDL 1 FS 01 135CR 647 0164 30246 NR 2 ENGINE FAILED TO START. REPLACED STARTER GENERATOR 1 G 7 2 3U 3 U H88EU E19EU 2002121700095 20021217 00095 NM 2002 12 17 DL757021098 1 20020917 A 5230 SF15614542 SEAL BOEING 757 757232 1384965 NM CARGO DOOR TORN A DALA B EMER. DESCENT O OTHER CR CRUISE 1 SO 27 613DL 22820 FLIGHT CREW DECLARED EMERGENCY DURING CRUISE FLIGHT. HAD RT BLEED TRIP RENDERING RT PACK INOP. UNABLE TO MAINTAIN CABI N PRESSURE. FOUND AFT CARGO DOOR SEAL LEAKING AND TORN. ALSO HAD ABOUT ONE FOOT OF SEAL OUT OF RETAINER. R&R RT FAN A IR MOD VLV RR 490 DEG THERMAL SENSOR SWITCH RAN ENGS PER PFHB BLEED LIGHT OPS NORMAL PREFORMED EXCESSIVE CABIN PRESSURE LEAKAGE CK PER MM 05-21-24-2. REMOVED AFT CARGO DOOR SEAL AND LWR FWD RETAINER REPLACED LWR FWD SEAL RETAINER AND DOOR SEAL INSTALLATION. 2 L 7 2 4F RT A2NM 2002121700096 20021217 00096 NM 2002 12 17 DL757021106 1 20020917 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 FUSELAGE SKIN, FS 590-660, STR 14L-19L. THE FUSELAGE SKIN WAS FOUND WITH SEVERAL DENTS NEAR FS 640 ALONG STRINGER 17L. THE DAMAGES WERE IN CLOSE PROXIMITY TO AN EXISTING REPAIR. THE SKIN WAS CUT AT FS 590 FROM STRINGER 14L TO 19L AND THE AFT SECTION OF PANEL REMOVED. A NEW SECTION WAS INSTALLED AND SPLICED IN PLACE WITH INTERNAL AND EXTERNAL DOUBLERS PE R ER/A 383714-14, REV A. 2 L 7 2 4F RT A2NM 2002121700097 20021217 00097 NM 2002 12 17 DL757021107 1 20020918 A 5330 143N35002 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 FUSELAGE SKIN & KEEL CHORD AT LOWER FWD VHF ANTENNA. FS 730 STR 28L&R. CORROSION REPAIR, THE THE SKIN AROUND THE LOWER VHF ANTENNA CUTOUT WAS FOUND CORRODED. THE HORIZONTAL FLANGES OF THE STRINGER 28L & 28R KEEL CHORDS WERE ALSO FOUND WI TH CORROSION. THE SKIN CUTOUT WAS ENLARGED TO REMOVE THE CORROSION AND THE KEEL CHORDS, BLENDED. THE SKIN WAS REPAIRED WITH 2 EXTERNAL DOUBLERS AND THE CHORDS WITH REPAIR ANGLES PER ER/A 383812-14, REV B. 2 L 7 2 4F RT A2NM 2002121700098 20021217 00098 NM 2002 12 17 DL757021120 1 20020921 A 3350 CONTACTOR BOEING 757 757232 1384965 NM EXTERIOR DIRTY A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 622DL 22912 ON LAYOVER CHECK FOUND L4 DOOR EXTERIOR EMERGENCY LIGHT INOP. CLEANED CONTACT ON LIGHT OPERATIONAL CHECKS OK. 2 L 7 2 4F RT A2NM 2002121700099 20021217 00099 2002 12 17 DL757021121 4 20020922 A 3441 HG1050AD05 IRU BOEING 757 757232 1384965 NM E/E BAY FAILED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 684DA 27104 ON T/O FMC SCRATCH PAD-IRS NOTATION WITH BOTH YAW DAMPS AND FMC FAILURE MSGS. REPLACED CENTER IRU, ALIGMENT OK. 2 L 7 2 4F RT A2NM 2002121700100 20021217 00100 NM 2002 12 17 DL757021122 1 20020922 A 3246 B757N WHEEL BOEING 757 757232 1384965 NM NLG DAMAGED A DALA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 27 668DN 25141 ON TAXI OUT BHM, NOSE GEAR STEERING GOT VERY WOBBLY, CALLED MTC, THAY FOUND THE RIGHT NOSE GEAR TIRE ASSEMBLY TO HAVE CO ME APART. SUSPECT OUTER BEARING FROZEN. REMOVED AND REPLACED NOSE WHEEL. 2 L 7 2 4F RT A2NM 2002121700101 20021217 00101 NM 2002 12 17 DL757021128 1 20020923 A 4960 491003493 ECU BOEING 757 757232 1384965 NM APU MALFUNCTIONED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 628DL 21384 22918 APU SHUT DOWN IN CRUISE, ONE RESTART ATTEMPTED, FAULT LIGHT AGAIN. NOTE NR 2 GENERATOR WAS DISCONNECTED AT TAKEOFF FROM SFO FOR RIGHT GENERATOR DRIVE LIGHT ILLUMINATING. FOUND APU AUTO-SHUTDOWN FOR OVERSPEED PER FIM REPLACED ECU, CHECK OI L QTY AND APU AREA, ALL CHECKED GOOD. NR 2 GENERATOR FOUND LOW ON OIL, SERVICED TO FULL CHECKED FOR LEAKS NONE NOTED, R AN ENGINE FOR 20 MIN WITH FULL LOAD NO PROBLEMS, REINSPECTED FOR LEAKS NONE NOTED. 2 L 7 2 4F RT A2NM 2002121700102 20021217 00102 NM 2002 12 17 DL757021140 1 20020925 A 3610 285N000611 CIRCUIT CARD BOEING 757 757232 1384965 NM E/E BAY FAULTY A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 639DL 23993 FL 310 LT ENG BLEED OFF, A/I VALVE, LT ENG WING LT VALVE ON. REINSTATED A/I THROUGH ISOL VALVE. RT BLEED OFF. NO PRES S SOURCE. CABIN CLIMBED TO 8000FT REINSTATED LT BLEED. SAME SEQ OF EVENTS OCCURRED AT FL 240 DIVERTED TO DFW. R&R LT AND RT ENG BLEED CONFIG CARDS RAN BLEED SYS TEST PER PFHB, ALL CKS OK PRESS A/C CKS OK RAN WITH A/I ON AND OFF ALL CKS O K. 2 L 7 2 4F RT A2NM 2002121700103 20021217 00103 NM 2002 12 17 DL757021142 1 20020926 A 3350 0201720001 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 652DL 24392 ON INSPECTION FOUND EMERGENCY LIGHTS INOP AT ROW 28. REPLACED LIGHT ASSY PER MM. OPN OF LIGHTS NORMAL. 2 L 7 2 4F RT A2NM 2002121700104 20021217 00104 EU 2002 12 17 HE66081642 1 20021212 A 6210 L621M1010054 BLADE UROCOP EC135 EC135T1 5620026 EU MAIN ROTOR DEFECTIVE H HEEA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 FS 01 135CR 654 0164 AIRCRAFT HAD A LATERAL VIBRATION. AFTER TRACKING WEIGHT NEEDED TO OFF SET LATERAL VIBRATION WAS BEYOND LIMITS. BLADES MU ST BE ABSORBING WATER. RETURN AND INSTALLED A TEMPORARY ROTOR BLADE. 1 G 7 2 3U H88EU 2002121700105 20021217 00105 EU 2002 12 17 IO5R081607 1 20021210 A 6320 L633M2010101A004 MOUNT UROCOP EC135 EC135P1 8680990 EU ANTI-RESONANCE FAILED H A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 FS 01 552BA 562 190 ARIS MOUNT FAILED IN FLIGHT, WATER EVERYWHERE REMOVED AND REPLACED 1 G 7 2 3U O H88EU 2002121700106 20021217 00106 NE 2002 12 17 AALA20021484 2 20021017 A 7314 384300 PUMP DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LT ENGINE FAILED A AALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 21 556AA 53086 ORD - FLT 390 - EN ROUTE ORD-LGA, UPON SWITCHING THE LEFT ENGINE HEAT OFF, THE LEFT ENGINE SHUT DOWN. ENGINE IGNITION W AS IN CONTINUOUS AT THE TIME. LEFT FUEL TEMPERATURE FLUCTUATING ON RETURN TO ORD. LANDED ORD WITHOUT INCIDENT. REPLAC ED LEFT ENGINE FUEL PUMP, FUEL CONTROL AND FUEL TEMPERATURE BULB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 2002121700107 20021217 00107 WP 2002 12 17 AALA20021485 1 20021016 A 3222 5963254501 STRUT DOUG DC9 DC982 3022082 WP NLG MALFUNCTIONED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 459AA 49564 EWR - FLT 1789 - EN ROUTE EWR-MSY, ON DEPARTURE FROM LGA, AIRCRAFT SYSTEMS REMAINED IN GROUND MODE. COULD NOT RETRACT G EAR. RETURNED AND LANDED EWR WITHOUT INCIDENT. REPLACED NOSE GEAR INNER STRUT ASSEMBLY AND SERVICED PER MM. ACCOMPLIS HED NOSE GEAR RETRACTION AND STEERING TEST. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002121700108 20021217 00108 WP 2002 12 17 AALA20021517 1 20021023 A 2120 DUCT DOUG DC9 DC983 3022083 WP A/C BAY DEFECTIVE A AALA K NONE J WARNING INDICATION CL CLIMB 1 SW 21 599AA 53289 SAN - FLT 512 - EN ROUTE SAN-ORD, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB-OUT. AFTER EMERGENCY PROCEDURES WERE COMPLETE LIGHT CAME BACK ON WITH INCREASE IN POWER. POWER WAS REDUCED AND THE LIGHT STAYED OUT FOR REM AINDER OF FLIGHT. RETURNED SAN AND LANDED WITHOUT INCIDENT. REPLACED GASKET ON THERMOSTAT LEFT SIDE IN TAIL COMPARTMEN T. REPLACED TUBE ON AIR CONDITIONING DUCT ON RIGHT SIDE IN TAIL COMPARTMENT. REPLACED SEALS ON RIGHT SIDE SLIP JOINT N EAR COOLING TURBINE IN TAIL COMPARTMENT. LEAK CHECKS GOOD. NO TAIL COMPARTMENT LIGHT. SYSTEM GROUND CHECKED NORMAL OP ERATION. (M) 2 L 7 2 4F RT A6WE 2002121700109 20021217 00109 WP 2002 12 17 AALA20021537 1 20021025 A 2120 SMOKE DOUG DC9 DC983 3022083 WP CABIN DETECTED A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 599AA 53289 SAN - FLT 460 - EN ROUTE SAN-ORD, SMOKE AND SMELL OF SMOKE IN CABIN BY SEAT 15B. SMOKE AND SMELL DISSIPATED, BUT SMELL CAME BACK. RETURNED SAN AND LANDED WITHOUT INCIDENT. PERFORMED CABIN ODOR TROUBLESHOOTING CARD AND PACK BURN OUT. SYS TEM GROUND CHECKED NORMAL OPERATION. AIRCRAFT SCHEDULED FOR FUNCTIONAL CHECK FLIGHT. FUNCTIONAL CHECK FLIGHT ACCOMPLIS HED WITH NO SMOKE OBSERVED. (M) 2 L 7 2 4F RT A6WE 2002121700110 20021217 00110 WP 2002 12 17 AALA20021590 1 20021102 A 2913 314195 PUMP DOUG DC9 DC982 3022082 WP LT ENGINE FAILED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 442AA 49468 SJC - FLT 828 - EN ROUTE SJC, LEFT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED WITH QUANTITY DECREASING TO ZERO. AIRCRAFT LANDED SJC WITHOUT INCIDENT. REPLACED ENGINE HYDRAULIC PUMP. REPLACED CASE DRAIN FILTERS. SYSTEM GROUND CHECKED NORMA L OPERATION. (M) 2 L 7 2 4F A6WE 2002121700111 20021217 00111 NE 2002 12 17 AALA20021595 2 20021105 A 7260 GEARBOX DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE DAMAGED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 591AA 53254 717307 MEM - FLT 814 - DFW-PHL, EN ROUTE AIRCRAFT LOST OIL PRESSURE IN NR 2 ENGINE. AIRCRAFT LANDED MEM WITHOUT INCIDENT. MAI NTENANCE DISCOVERED PORT LP5 GEARBOX THREADS STRIPPED. AIRCRAFT BEING FERRIED TO TUL FOR ENGINE CHANGE. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2002121700112 20021217 00112 WP 2002 12 17 AALA20021599 1 20021104 A 2910 HYDRAULIC SYSTEM DOUG DC9 DC982 3022082 WP LT ENGINE LEAKING A AALA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 232AA 49179 DFW - FLT 598 - DURING TAXI AIRCRAFT FILLED WITH SMOKE ACCOMPANIED BY A DIRTY SOCK SMELL. AIRCRAFT TAXIED TO GATE WITH NO FURTHER INCIDENT. FOUND HYDRAULIC LEAK AT LEFT ENGINE HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F A6WE 2002121700113 20021217 00113 WP 2002 12 17 AALA20021600 1 20021105 A 2613 WARNING SYSTEM DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 21 585AA 53248 DFW - FLT 1806 - DFW-JFK, ON CLIMB-OUT FROM DFW, TAIL COMP TEMP HIGH LIGHT ILLUMINATED. LIGHT EXTINGUISHED AFTER 1.5 MI NUTES. AIRCRAFT LANDED ORD WITHOUT INCIDENT. GROUND RAN A/C AT HIGH POWER SEVERAL TIMES FOR SEVERAL MINUTES. NO DEFEC TS AND NO LEAKS NOTED. REMOVED AND REPLACED LEFT AND RIGHT TAIL COMPARTMENT OVERHEAT SWITCH AS A PRECAUTION. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002121700114 20021217 00114 EU 2002 12 17 IO5R081608 1 20021210 A 6320 L633M2011101 MOUNT UROCOP EC135 EC135P1 8680990 EU ANTI-RESONANCE DEFECTIVE H IO5R A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 FS 01 135BP 41 0197 LT FWD ARIS MOUNT DEFLATED REMOVED AND REPLACED 1 G 7 2 3U O H88EU 2002121700115 20021217 00115 EU 2002 12 17 IO5R081609 1 20021210 A 6320 L633M201101 MOUNT UROCOP EC135 EC135P1 8680990 EU ANTI-RESONANCE DEFECTIVE H IO5R A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 FS 01 135BP 41 0197 LT AFT ARIS MOUNT DEFLATED IN FLIGHT REMOVED AND REPLACED 1 G 7 2 3U O H88EU 2002121700116 20021217 00116 EU 2002 12 17 IO5R081638 1 20021212 A 2400 45033501 SWITCH UROCOP EC135 EC135P1 8680990 EU ELECT CONTROL FAILED H IO5R O OTHER O OTHER NR NOT REPORTED 1 FS 01 551BA 560 188 NR 1 ENGINE CRANK WILL NOT ENGAGE BY FADEC CONTROL OR VENT SWITCH REMOVED AND REPLACED 1 G 7 2 3U O H88EU 2002121700117 20021217 00117 EU 2002 12 17 IO5R081649 1 20021212 A 6240 SVEURO4 INDICATOR UROCOP EC135 EC135P1 8680990 EU MAST MOMENT FAILED H IO5R O OTHER O OTHER CR CRUISE 1 FS 01 551BA 560 188 NO MAST MOMENT INDICATION REMOVED AND REPLACED 1 G 7 2 3U O H88EU 2002121700118 20021217 00118 2002 12 17 SROM200200021 4 20021213 A 2565 15611173 SLIDE BOEING 737 737205 1384456 NM L2 DOOR TORN C SROM K NONE O OTHER IN INSP/MAINT 1 AL 03 736BP 1356 23465 DURING C CHECK INSPECTION WHILE PERFORMING L2 ESCAPE SLIDE TEST PER TASK CARD SLIDE DEPLOYED, INFLATED THEN DEFLATED BEC AUSE OF TORN SEAM. 2 L 7 2 4F RT A16WE 2002121700119 20021217 00119 WP 2002 12 17 MWEA020733 1 20021217 A 5311 5911285509 PAN DOUG DC9 DC981 3022081 WP WINDOW #32 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 RIGHT WINDOW #32 WINDOW PAN IS CRACKED AT FASTENER ON TOP FORWARD CORNER JUST AFT OF STATION 845. -- FABRICATED REPAIR ANGLE AND SHIM AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 2002121700120 20021217 00120 WP 2002 12 17 MWEA020734 1 20021217 A 5210 995757 DOUBLER DOUG DC9 DC981 3022081 WP BEAM #6 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 PASSENGER DOOR BEAM #6 IS CRACKED BY FASTENER 18" AFT OF THE FORWARD EDGE. -- FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002121700121 20021217 00121 WP 2002 12 17 MWEA020735 1 20021217 A 5313 59568791 WEB DOUG DC9 DC981 3022081 WP STA 207 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FORWARD PASSENGER DOOR JAMB WEB HAS A CRACK AT STATION 207 AND LONGERON 15 LEFT. -- FABRICATED AND INSTALLED FILLER AN D DOUBLER. 2 L 7 2 4F A6WE 2002121700122 20021217 00122 WP 2002 12 17 MWEA020736 1 20021217 A 5313 5956879501 WEB DOUG DC9 DC981 3022081 WP STA 207 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FORWARD PASSENGER DOOR JAMB WEB HAS A CRACK AT STATION 207 AND LONGERON 11 LEFT. -- FABRICATED AND INSTALLED FILLER AN D DOUBLER. 2 L 7 2 4F A6WE 2002121700123 20021217 00123 NM 2002 12 17 AALA20021603 1 20021107 A 2742 6355B000103 ACTUATOR BOEING 737 737823 13844BZ NM HORIZ STAB FAULTY A AALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SW 21 915AN 29516 ORD - FLT 1891 - BOS-ORD, STAB TRIM FAILED WHEN AUTO PILOT WAS DISCONNECTED DURING DESCENT. TRIM BEGAN TO RUN AWAY ON S HORT FINAL. TURNED OFF BOTH TRIM MOTORS. LANDED ORD WITHOUT INCIDENT. AFTER LANDING TURNED TRIM MOTORS BACK ON AND WA S UNABLE TO TURN TRIM WITH THE ELECTRIC FROM EITHER PILOT LOCATION. REPLACED ELECTRIC TRIM ACTUATOR. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2002121700124 20021217 00124 SW 2002 12 17 YTRR081612 1 20021210 A 5302 206033426001 SUPPORT BELL 206 206L3 1182108 SW T/R GEARBOX CRACKED H YTRA K NONE O OTHER IN INSP/MAINT 1 FS 01 405RL 4290 51405 CRACK WAS FOUND ON TAILROTOR GEARBOX MOUNTING CASTING. CRACK PROPOGATED FROM AFT LEFT MOUNTING HOLE THROUGH LIGHTING HOL E. 1 G 7 1 3U H2SW 2002121700125 20021217 00125 WP 2002 12 17 AALA20021604 1 20021107 A 4990 5940405503 OIL SYSTEM DOUG DC9 DC982 3022082 WP APU LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 560AA 53090 DFW - FLT 530 - DFW-RIC, ON CLIMB-OUT ABOVE 1000 FEET HAD BURNING SMELL IN THE COCKPIT WITH MODERATE SMOKE THROUGHOUT TH E CABIN. AIRCRAFT RETURNED AND LANDED DFW WITHOUT INCIDENT. INSPECTED ACM/PACK HEAT EXCHANGER DUCTING. NO DEFECTS NOT ED. INSPECTED APU, FOUND OIL PRESENT IN THE APU PLENUM. REPLACED APU. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002121700127 20021217 00127 GL 2002 12 17 YTRR081619 2 20021211 A 7261 357950111452 SHAFT BELL 206 206L4 1182110 SW ALLSN 250C 250C30 03013 GL OIL PUMP WORN H YTRA O OTHER O OTHER NR NOT REPORTED 1 FS 01 207RT 612 52207 OIL PUMP SHAFT SPLINES WORN TO THE POINT OF ROTOR TACH FAILURE. 1 G 7 1 3U 3 U NC H2SW E1GL 2002121700128 20021217 00128 EU 2002 12 17 00064 1 20021126 A 2932 SEAL AMD FALC20 FALCON 2720302 EU HYD SYSTEM LEAKING E HAEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 05 204TW 204 PILOT REPORTED JEWEL LIGHT ILLUMINATED AFTER TAKE OFF, DIVERTED FOR MAINTENANCE. MAINTENANCE FOUND NR 1 HYDRAULIC TRANS MITTER SEAL LEAKING, CLEANED AND LUBED SEAL. OPS CHECK RESERVOIR PRESSURE SYSTEM AND INDICATION SYSTEMS, RETURN AIRCRAF T TO SERVICE. 2 L 7 2 4F A7EU 2002121700129 20021217 00129 NE 2002 12 17 00066 2 20021203 A 7200 ENGINE LEAR 24 24B 5170306 CE GE CJ610 CJ6106 30006 NE LEFT FLAMED OUT E HAEA B EMER. DESCENT X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 05 233TW 24B221 251013A PILOT REPORTED THE LT ENGINE FLAMED OUT CLIMBING FROM 41,800 TO 43,000. CENTER CLEARED THEM TO 24,000 FOR RELIGHT. AF TER RELIGHT, CLIMBED BACK TO 39,000. AFTER COMPLETION OF THIS LEG, PILOT INSPECTED ENGINE AND FOUND NO INDICATION OF DA MAGE OR LEAKAGE. ON THE NEXT FLIGHT, SECOND LEG LEFT ENGINE FLAMED OUT AT 38,800, DECENT AND RELIGHT NORMAL. AIRCRAFT R OUTED TO MAINTENANCE BASE. WILL UPDATE REPORT AS SOON AS AVAILABLE. 2 L 7 2 4J 4 J A10CE 1E16 2002121700130 20021217 00130 NE 2002 12 17 00067 2 20021216 A 7200 ENGINE LEAR 24 24D 5170311 CE GE CJ610 CJ6106 30006 NE LEFT FLAMED OUT E HAEA B EMER. DESCENT X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 05 324TW 24324 251718A PILOT REPORTED LEFT ENGINE FLAMMED OUT DURING CLIMB, PASSING 40,300FT. ATC CLEARED FOR DECENT RELIGHT AT 28K CLIMB BACK TO FL370 TO COMPLETE TRIP. PILOT INSPECTED ENGINE FOR FOD DAMAGE AND LEAKS, NONE FOUND. WILL UPDATE REPORT AFTER AIRCR AFT RETURNS TO MAINTENANCE BASE. 2 L 7 2 4J 4 J A10CE 1E16 2003022700065 20030227 00065 CE 2003 2 27 00068 1 20021206 A 3260 SWITCH LEAR 24 24 5170302 CE LANDING GEAR OUT OF ADJUST E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 157TW 24157 PILOT REPORTED 3 RED LIGHTS (DOOR LIGHTS) AFTER DEPARTURE FROM YIP AND RETURNED TO YIP. MAINTENANCE JACKED AND SWUNG GE AR OPS CK GOOD. AIRCRAFT DEPARTED YIP WITH SAME PROBLEM AND RETURNED. AIRCRAFT JACKED AND GEAR SWING PERFORMED POSITIO N OF ALL SWITCHES CK GOOD, OPS CK GOOD. AIRCRAFT DEPARTED YIP WITH SAME PROBLEM AND RETURNED. MAINTENANCE ADJUSTED LAN DING GEAR SWITCH AND PERFORMED GEAR SWING, OPS CK GOOD AIRCRAFT HAS NOT HAD PROBLEM SINCE ADJUSTMENT. 2 L 7 2 4J A10CE 2002121700131 20021217 00131 NM 2002 12 17 AALA20021611 1 20021105 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 DFW - DURING OVERNIGHT MAINTENANCE, MID GALLEY RIGHT AFT EMERGENCY EXIT LIGHT LOOSE FROM SIDE WALL. INSTALLED NEW EMERG ENCY EXIT LIGHT ASSEMBLY AT MID GALLEY RIGHT AFT. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 2 4F RT T00001SE 2002121700132 20021217 00132 WP 2002 12 17 0203899150 1 20021120 A 2170 SEPARATOR DOUG DC9 DC914 3022034 WP PWA JT8 JT8D7 52053 NE AIR DISTRIBUTION CONTAMINATED A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 8908E 48947 2797 45749 649472 DURING CLIMB, SMOKE AND FUMES ENTERED THE CABIN WITH ASSOCIATED LAVATORY SMOKE DETECTORS ACTIVATING. AIRCRAFT RETURNED TO AIRPORT. MAINTENANCE FOUND WATER SEPARATORS SATURATED WITH OIL. MAINTENANCE REPLACED THE WATER SEPARATORS AND PERFOR MED ENGINE BURN OFF PROCEDURE. NO SMOKE OR FUMES PRESENT, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2002121700133 20021217 00133 NM 2002 12 17 AALA20021612 1 20021106 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 391AA 27451 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT ROW 26H INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGH TING ASSEMBLY AT ROW 26H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002121700134 20021217 00134 NM 2002 12 17 AALA20021613 1 20021113 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - DURING OVERNIGHT MAINTENANCE, AFT SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 4D HAS ONE LAMP INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY PATH LIGHT ASSEMBLY AT SEAT 4D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2002121700135 20021217 00135 NM 2002 12 17 0203926739 1 20021201 A 3040 CONTROLLER BOEING 747 747251F 1384898 NM PWA JT9 JT9D* NE WINDOW HEAT FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 639US 23887 DURING CLIMB, AN ELECTRICAL FUME FOLLOWED BY A PUFF OF SMOKE EMITTED FROM THE FLIGHT DECK. AIRCRAFT DECLARED AN EMERGENC Y, RETURNED AND LANDED WITHOUT INCIDENT. REPLACED WINDOW HEAT CONTROLLER, TERMINAL BLOCK HARDWARE AND CLEANED UPPER WIND OW ELECTRICAL CONNECTOR. OPERATIONL CHECKS GOOD. 2 L 7 4 4F 4 F A20WE E20EA 2002121700136 20021217 00136 NM 2002 12 17 AALA20021615 1 20021110 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 312AA 22315 LAX - DURING OVERNIGHT MAINTENANCE, RIGHT EMERGENCY LIGHT BY FORWARD GALLEY INOPERATIVE. REPAIRED WIRE AT EMERGENCY EXI T LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2002121700137 20021217 00137 WP 2002 12 17 AALA20021621 1 20021104 A 3610 DUCT DOUG DC9 DC982 3022082 WP A/C BAY DAMAGED A AALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 7520A 49897 SLC - FLT 360 - EN ROUTE SLC-DFW, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED SOON AFTER TAKEOFF ROTATION. ANTI -ICE NOT ON. CLOSED CROSSFEED AND SE PACK TO HIGH PRESSURE BLEED OFF, BUT LIGHT REMAINED ILLUMINATED. FLIGHT ATTENDANT S REPORTED BURNING SMELL. RETURNED SLC, WITH POWER REDUCED TO IDLE, TEMPERATURE HIGH LIGHT EXTINGUISHED AND PRESSURIZAT ION FLOW LIGHT ILLUMINATED. LANDED WITHOUT INCIDENT. REPLACED ELBOW DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F A6WE 2002121700138 20021217 00138 NE 2002 12 17 0212111 2 20021211 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R389* NE RIGHT MALFUNCTIONED A UHLA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NE 03 121CQ 121 464 DRG955988 ON TAKEOFF ROLL, EXPERIENCED A LOSS OF TORQUE INDICATION ON THE RIGHT POWERPLANT. AIRCRAFT ABORTED TAKEOFF AND WAS TOLD TO RETURN TO THE GATE BY MOC, MECHANIC WAS NOTIFIED TO MEET AIRCRAFT AT THE GATE. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002121700139 20021217 00139 WP 2002 12 17 AALA20021622 1 20021104 A 2120 CLAMP DOUG DC9 DC982 3022082 WP A/C BAY DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SW 21 241AA 49254 TUL - FLT 9623 - DURING FUNCTIONAL CHECK, FLIGHT ACCOMPLISHED A MAXIMUM POWER TAKEOFF WITH APU RUNNING. CLIMB POWER WAS SELECTED AS NORMAL AFTER TAKEOFF. AT 9,000 FEET, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIRFOIL ANTI-ICE WAS NOT BEING USED. WHEN MOVED TO HIGH PRESSURE BLEED OFF TAIL LIGHT FLICKERED. WHEN ENGINE POWER WAS REDUCED, LIGHT EXTINGUISHED. LANDED TUL WITHOUT INCIDENT. REPLACED AUG VALVE CLAMPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002121700140 20021217 00140 WP 2002 12 17 AALA20021623 1 20021106 A 2150 39271012 REGULATOR VALVE DOUG DC9 DC982 3022082 WP A/C BAY STICKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 560AA 53090 DFW - FLT 1145 - EN ROUTE DFW-SFO, AIRCRAFT ON CLIMB-OUT, EMITTED SMOKE AND FUMES FROM AIRCRAFT GASPERS THROUGHOUT THE P LANE. SMOKE STOPPED AFTER APPROXIMATELY 5 MINUTES. RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT AIR CONDI TIONING PRESSURE REGULATOR VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002121700141 20021217 00141 WP 2002 12 17 AALA20021624 1 20021110 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 443AA 49469 DFW - DURING OVERNIGHT MAINTENANCE, CENTER TAIL CONE EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED CENTER TAIL CONE EMERGE NCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002121700142 20021217 00142 WP 2002 12 17 AALA20021625 1 20021109 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 410AA 49321 DFW - DURING OVERNIGHT MAINTENANCE, R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED R1 DOOR EMERGENCY EXIT LIGHT BAT TERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002121700143 20021217 00143 EU 2002 12 17 0212112 1 20021201 A 2613 1734362450 CONNECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R389* NE TAILPIPE SENSOR CONTAMINATED A UHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NE 03 152CQ 152 199 DRG558988 AIRCRAFT WAS ON TAKE-OFF ROLL AT 110 KNOTS WHEN THE PILOT OBSERVED THE RIGHT TAILPIPE HOT LIGHT WAS ILLUMINATED. PILOT ABORTED TAKE-OFF AND RETURNED TO GATE. MAINTENANCE FOUND MOISTURE IN THE RIGHT OUTBOARD TAILPIPE HEAT SENSOR CONNECTOR. MECHANIC DRIED CONNECTOR AND PERFORMED GROUND RUN OF RIGHT ENGINE. ENGINE RUN OPS CHECK WAS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002121700144 20021217 00144 EU 2002 12 17 0212113 1 20021211 A 2613 CONNECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R389* NE TAILPIPE SENSOR CORRODED A UHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NE 03 340SZ 340A004 401 DRG189789 RIGHT AFTER TAKEOFF, PILOT RECIEVED LEFT TAILPIPE HOT INDICATION. PILOT RETARDED POWER AND LEFT TAILPIPE HOT LIGHT EXTI NGUISHED. PILOT RETURNED TO FIELD. MECHANIC FOUND CORROSION ON OUTBOARD TAILPIPE HEAT SENSOR CONNECTOR, REMOVED CORROS ION. PERFORMED GROUND RUN OF LEFT ENGINE, OPS CHECKS GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002121700145 20021217 00145 NM 2002 12 17 AALA20021626 1 20021110 A 2750 285N001140 FSEU BOEING 757 757223 1384957 NM E/E BAY MALFUNCTIONED A AALA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 659AA 24617 CUN - FLT 1671 - EN ROUTE JFK-CUN, ON FINAL APPROACH, LEADING EDGE SLAT DISAGREE MESSAGE APPEARED UPON FLAP EXTENSION. UTILIZING ALTERNATE LEADING EDGE/TRAILING EDGE FLAP SWITCHES, EXTINGUISHED MESSAGE. LANDED AT CUN WITHOUT INCIDENT. RE PLACED ROTARY ACTUATOR BEHIND NR 5 SLAT PANEL AND REPLACED THE NR 1 FLAP SLAT ELECTRIC UNIT. SYSTEM GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 2 4F RT A2NM 2002121700146 20021217 00146 WP 2002 12 17 AALA20021628 1 20021112 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 203AA 49145 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROWS 15-16 INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002121700147 20021217 00147 EU 2002 12 17 0212131 1 20021213 A 2613 CONNECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R389* NE TAILPIPE SENSOR CONTAMINATED A UHLA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 03 123XS 123 360 DRG486887 PILOT REPORTED, OBSERVED THE LEFT TAILPIPE HOT LIGHT ILLUMINATED SHORTLY AFTER TAKE-OFF. PILOT SHUT DOWN THE LEFT ENGIN E DECLARING AN EMERGENCY, AND RETURNED TO FIELD. CLEANED MOISTURE FROM LEFT TAILPIPE SENSOR CONNECTIONS AND RESEALED. PERFORMED GROUND RUN, OPERATIONAL CHECK OF LEFT TAILPIPE OVERHEAT SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002121700148 20021217 00148 WP 2002 12 17 AALA20021629 1 20021112 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7512A 49806 DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROWS 19-21 INOPERATIVE. RESEATED EMERGENCY EXIT LI GHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2002121700149 20021217 00149 EU 2002 12 17 0212132 1 20021212 A 2613 WIRE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R389* NE TAILPIPE SENSOR SHORTED A UHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NE 03 123XS 123 360 DRG486887 DURING TAKEOFF ROLL PILOT OBSEVRED THE LEFT TAILPIPE HOT LIGHT ILLUMINATED. PILOT ABORTED TAKEOFF AND RETURNED TO GATE. SENDING MECHANIC TO TROUBLESHOOT SYSTEM. MECHANIC ARRIVED, FOUND SHORT TO GROUND, REPAIRED WIRE IAW SF340 WM 20-20-00. PERFORMED GROUND RUN TO OPS CHECK LEFT TAILPIPE HEAT SYSTEM. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002121700150 20021217 00150 EU 2002 12 17 0212141 1 20021214 A 2420 31342003 GENERATOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R389* NE RT AC SYSTEM FAILED A UHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 03 340SZ 7257 1430 340A004 401 DRG189789 RIGHT AC GENERATOR AND RIGHT INTAKE LIGHTS ILLUMINATED DURING FLIGHT. AIRCRAFT RETURNED TO FIELD. AFTER TROUBLESHOOTIN G THE AC SYSTEM, MECHANIC REMOVED AND REPLACED THE RIGHT AC GENERATOR. OPERATIONAL CHECKS GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002121700151 20021217 00151 SO 2002 12 17 SIMA200221901 1 20020807 A 2520 7277120501 PSU EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 636AE 145160 ORD - FLT 4173 - DURING TAXI, FLIGHT CREW REPORTED SMOKE COMING FROM PASSENGER READING LIGHT AT SEAT 7A. MAINTENANCE RE MOVED AND REPLACED THE PASSENGER SERVICE UNIT PCB ASSEMBLY AT ROW 7 IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002121700152 20021217 00152 NM 2002 12 17 02FDEA00923 1 20021204 A 5320 STRAP BOEING 727 727233 138408A NM PWA JT8 JT8D9 52048 NE FLOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 CORROSION ON FLOOR STRAP AT BS 1174, LBL 24 TO RBL 24, WL 208. REMOVED CHORD AND INSTALLED NEW CHORD IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2002121700153 20021217 00153 GL 2002 12 17 SIMA200223501 2 20020820 A 7200 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 2 SHUTDOWN A SIMA A UNSCHED LANDING F Y J FLT CONT AFFECTED ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 21 733KR 145368 CAE311645 RDU - FLT 4634 - NR 2 ENGINE HAD UNCOMMANDED SHUTDOWN. FLIGHT CREW REPORTS THAT DURING CLIMB TO 13,000 FEET THE NR 2 EN GINE ACCELERATED RAPIDLY ON ITS OWN, A/C YAW'D TO THE LEFT. IGNITION A-B LIGHT CAME ON, THEN ENGINE 2 OUT MESSAGE CAME ON, AND THE ENGINE RPM INDICATION WENT TO ZERO. RAI NR 2 ENGINE ASSEMBLY. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002121700154 20021217 00154 EA 2002 12 17 SIMA200228701 1 20021010 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 503AE 10021 DFW - FLT 3801 - CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS 1, 2 , AND 3 (S/N'S 67338, 67360, 73137) IAW CRJ MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE . (M) 2 L 7 2 4F RT A21EA 2002121700155 20021217 00155 SO 2002 12 17 SIMA200228704 1 20021014 A 3350 20131A BATTERY PACK EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 738NR 145401 ORF - FLT 4524 - CREW REPORTED THE OVERWING INTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. AIRCRAFT WAS INSPECTED AND FERRI ED TO BOS FOR CORRECTIVE ACTION. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY POWER SUPPLY BATTERY PACK IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2002121700156 20021217 00156 SO 2002 12 17 SIMA200228901 1 20021014 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 617AE 145093 LSE - FLT 4186 - DURING CABIN CHECK, CREW REPORTED THE MID CABIN FLOOR PROXIMITY EMERGENCY LIGHTS WERE INOPERATIVE. MAI NTENANCE REMOVED AND REPLACED THE NR 3 POWER SUPPLY UNIT IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WA S RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2002121700157 20021217 00157 SO 2002 12 17 SIMA200230201 1 20021027 A 3350 66364 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 621AE 145105 ORD - FLT 4348 - CREW REPORTED THE LAST ROW OF FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 7 FLOOR STRIP LIGHT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE (M) 2 L 7 2 4T RT T00011AT 2002121700158 20021217 00158 GL 2002 12 17 SIMA200232306 2 20021114 A 7200 FIRE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 1 ENGINE DETECTED A SIMA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SW 21 831AE 145616 BOS - FLT 4772 - CREW REPORTED A NR 1 ENGINE TAILPIPE FIRE DURING START. ALL ENGINE INDICATIONS WERE NORMAL AND NO FIRE WARNING OR EICAS MESSAGES. CREW FIRED BOTH FIRE BOTTLES AND SAFELY EVACUATED PASSENGERS FROM AIRCRAFT. MAINTENANCE CO ULD NOT DUPLICATE DISCREPANCY. FAULT ISOLATION MANUAL WAS FOLLOWED WITH NO DEFECTS NOTED DURING 5 ENGINE STARTS. AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002121700159 20021217 00159 NM 2002 12 17 02FDEA00924 1 20021205 A 2797 WIRE BOEING 727 727200 138407E NM NR 6 LE FLAP DAMAGED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 221FE 20932 ON CLIMBOUT, DURING FLAP RETRACT, MOVED HANDLE FROM FLAP 5 TO FLAP 2 AND 6. LEADING EDGE FLAP SHOWED IN TRANSIT ON S/O AUX PANEL WITH AMBER LEADING EDGE FLAP LIGHT ON FOWARD PANEL. INSTALLED JUMPER CABLE ON NR 6 LEADING EDGE FLAP IAW M M. MAINTENANCE AND OPERATIONAL CHECK GOOD. (CONTORL NUMBER 145201) AIRCRAFT OK FOR SERVICE AT THIS TIME. 2 L 7 3 4F RT A3WE 2002121700160 20021217 00160 NE 2002 12 17 SIMA200232403 2 20021118 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT POWER LOSS A SIMA O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 SW 21 386AE 340B386 785392 LBB - FLT 3493 - DURING FINAL APPROACH, CREW REPORTED THE LOSS OF RIGHT ENGINE TORQUE FOLLOWED BY ALL OTHER ENGINE PARAM ETERS FALLING OFF RAPIDLY. NO ABNORMAL NOISES OR VIBRATIONS WERE NOTED. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2002121700161 20021217 00161 NM 2002 12 17 UIEA200200062 1 20021114 A 5312 PRESSURE PANEL BOEING 747 747230B 1384889 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 507MC 21380 DURING CURRENT C-CHECK, FOUND FORWARD PRESSURE DECK SKIN CRACKED TWO PLACES STATION 140 AT RBL 34 AND RBL 43 NEAR WL 215 . CRACK LENGTH WAS .025 INCH AT EACH LOCATION FROM EXISTING FASTENER HOLES. CRACKED AREAS TRIMMED AWAY. PERFORMED EC INSPECTION OF CUT OUT AREAS TO ENSURE NO CRACKS. NO CRACKS FOUND. FABRICATED REPAIR DOUBLERS FOR FORWARD AND AFT SIDES OF PRESSURE WEB. INSTALLED DOUBLERS IAW SRM 51-30-05. (M) 2 L 7 4 4F A20WE 2002121700162 20021217 00162 NM 2002 12 17 02FDEA00943 1 20021213 A 2797 WIRE BOEING 727 727227 1384078 NM PWA JT8 JT8D9 52048 NE TE FLAPS FAILED A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 488FE 21491 ON ARRIVAL, WHEN TRAILING FLAPS EXTENDED TO 5 DEG, THE AMBER LEADING EDGE FLAPS LIGHT REMAINED ILLUMINATED ON FO PANEL AND THE NR 5 LEADING EDGE FLAP LIGHT (BOTH GREEN AND AMBER), DID NOT ILLUMINATE ON SO PANEL. RAN QRH PROCEDURE AND DIVER TED. ON ARRIVAL, FLAPS/SLATS EXTENDED NORMALLY. INSTALLED LEADING EDGE FLAP JUMPER SWITCH FOR NR 5 LEADING EDGE FLAP SWITCH. OPERATED FLAP SYSTEM SEVERAL TIMES AND SYSTEM CKS GOOD IAW MM. REQUIRES JUMPER, REMOVED AND FLAP SWITCH REPLAC ED AS TIME PERMITS. 2 L 7 3 4F 4 F A3WE E2EA 2002121700163 20021217 00163 2002 12 17 SWAA022853 4 20021205 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR GIRT BAR BRACKETS LOOSE. SECURED BRACKETS PER MM. 2 L 7 2 4F RT A16WE 2002121700164 20021217 00164 NM 2002 12 17 SWAA022859 1 20021205 A 2612 6566207 FIRE LOOP BOEING 737 7373Q8 1384670 NM APU BAY MALFUNCTIONED A SWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 662SW 23255 AIR TURNBACK, APU FIRE WARNING LIGHT AND BELL WENT OFF AT APPROX 1000 FEET. COMPLIED WITH AIRCRAFT PROCEDURES CHECK LIS T, AND DISCHARGED APU FIRE BOTTLE. APU FIRE WARNING LIGHT WOULD NOT EXTINGUISH. COMPLIED WITH APU COMPT AND APU INSP. NO EVIDENCE OF FIRE NOTED. 2 L 7 2 4F RT A16WE 2002121700165 20021217 00165 NM 2002 12 17 02FDEA00944 1 20021213 A 3260 DOWNLOCK SWITCH BOEING 727 72724C 1384005 NM PWA JT8 JT8D1 52044 NE NLG INOPERATIVE A FDEA O OTHER N FALSE WARNING LD LANDING 1 SO 25 114FE 19527 DURING LANDING GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT ILLUMINATED. NO DOWN, GREEN LIGHT. NOTE: MANUAL GEAR EXTENSION PROCEDURE COMPLETED EMERGENCY, DECLARED WITH ATC. TROUBLESHOT LANDING GEAR POSITION INDICATING SYSTEM IAW M.M. FOUND FAULTY NOSE LANDING GEAR LOCK SWITCH. REMOVED AND REPLACED NOSE LANDING GEAR LOCK SWITCH IAW MM. ADJUSTMENT/TEST, LANDI NG GEAR LOCK AND POSITION SWITCHES IAW MM, NOSE GEAR INDICATIONS NORMAL.. 2 L 7 3 4F 4 F A3WE E2EA 2002121700166 20021217 00166 NM 2002 12 17 SWAA022861 1 20021204 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 SEVERAL EEPLS COVERS BROKEN IN CABIN. REMOVED AND REPLACED EEPLS COVERS AND REPAIRED WIRES PER MM. 2 L 7 2 4F RT A16WE 2002121700167 20021217 00167 NM 2002 12 17 02FDEA00945 1 20021215 A 5754 RIB DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE RT WING SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RIGHT WING LEADING EDGE SLAT TRACK NR 16 INBOARD STRUCTURAL RIB FOUND CRACKED APPROXIMATELY (0.125). 2 L 7 3 4F 4 F RT A22WE E13NE 2002121700168 20021217 00168 NM 2002 12 17 SWAA022865 1 20021206 A 3350 57771 CAP BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING AT FWD CABIN. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2002121700169 20021217 00169 NM 2002 12 17 SWAA022866 1 20021206 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS NR 10, NR 11, NR 12, NR 13 AND NR 15. REMOVED AND REPLACE D EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2002121700170 20021217 00170 NM 2002 12 17 SWAA022867 1 20021206 A 3350 BR2013 LIGHT BOEING 737 7373Y0 1384671 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 EEPLS LOOSE BETWEEN ROW NR 6 AND NR 7. REMOVED AND REPLACED EEPLS SECTION PER MM. 2 L 7 2 4F RT A16WE 2002121700171 20021217 00171 NM 2002 12 17 SWAA022869 1 20021207 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 071SW 22358 DURING SCHEDULED PM CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2002121700172 20021217 00172 2002 12 17 SWAA022871 4 20021208 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002121700173 20021217 00173 NM 2002 12 17 SWAA022872 1 20021207 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2002121700174 20021217 00174 NM 2002 12 17 SWAA022875 1 20021208 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2002121700175 20021217 00175 NM 2002 12 17 SWAA022887 1 20021207 A 3211 654611324 PIN BOEING 737 7373H4 1384600 NM MLG TRUNNION CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED 1/4D CHECK, FOUND BOTH LEFT AND RIGHT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LEFT AND R IGHT TRUNNION PINS PER MM. 2 L 7 2 4F RT A16WE 2002121700176 20021217 00176 NE 2002 12 17 SWAA022889 2 20021207 A 7200 CFM56 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 1 MALFUNCTIONED A SWAA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SW 29 646SW 28331 858518 ABORTED TAKEOFF, DURING TAKEOFF, BANG/GRINDING NOISE, FLASH FROM NR 1 ENGINE AREA. ENGINE INDICATIONS NORMAL, SHUTDOWN BOTH ENGINES AS PRECAUTIONARY MEASURE. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700177 20021217 00177 NM 2002 12 17 2002UALA01785 1 20021127 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 BODY STATION 947 CABIN FLOOR BEAM, LBL19 UPPER FLANGE CORRODED UNDER TIEDOWN FITTING. MAJOR REPAIR ACCOMPLISHED. INSTAL LED UPPER CAP SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2003020600142 20030206 00142 NM 2003 2 6 02FDEA00946 1 20021216 A 5754 RIB DOUG MD11 MD11 3023602 NM L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LT WING L/E SLAT TRACK NR 16 I/B STRUCTURAL RIB FOUND CRACKED APPROX 0.125 INCH. 2 L 7 3 4F RT A22WE 2002121700178 20021217 00178 NM 2002 12 17 2002UALA01786 1 20021127 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 LEFT HAND CREASE BEAM WEB IS CORRODED FROM BODY STATION 787 TO BODY STATION 807. MAJOR REPAIR ACCOMPLISHED. REPLACED CR EASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700179 20021217 00179 NM 2002 12 17 2002UALA01787 1 20021130 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 CABIN FRAME AT STATION 827 ON STRINGER 9L IS CRACKED AT RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700180 20021217 00180 NM 2002 12 17 2002UALA01788 1 20021201 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 BODY STATION 887 FUSELAGE FRAME CRACKED AT STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700181 20021217 00181 CE 2002 12 17 045447 1 20021127 A 5230 12944004473 INTERCOSTAL BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CARGO DOOR FAILED A AMWA A UNSCHED LANDING E P VIBRATION/BUFFET NO WARNING INDICATION CL CLIMB 1 CE 07 146ZV UE146 AFTER TAKE OFF, THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR TO NR 2 ENGINE START. TAKE OFF ROLL WAS NORMAL. JUST AFTER ROTATION, A STRONG VIBRATION BEGAN. THE LANDING GEAR RETRACTED AND TH E ENGINE INSTRUMENTS WERE NORMAL. THE AIRCRAFT WAS THEN RETURNED TO FIELD AND THE CARGO DOOR WAS FOUND OPEN. HOWEVER, T HE CARGO DOOR ANNUNCIATOR LIGHT FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED 3 CRACKED INTERCOSTALS, DORSEL FI N AND 2 SHOCKS. THEY ALSO RIG CHECKED THE DOOR. 2 L 7 2 4T 3 T RT A24CE E2NE 2002121700182 20021217 00182 NM 2002 12 17 2002UALA01789 1 20021201 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 STRINGER 14L DAMAGED AT BODY STATION 1006. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2003011500137 20030115 00137 NM 2003 1 15 2002UALA01790 1 20021127 A 2913 MR29157 PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 647UA 3 25284 RIGHT ENGINE DRIVEN HYDRAULIC PUMP FAILED. DIVERTED TO JFK. NR 2 ENGINE PUMP FAILURE. REPLACED PUMP AND APPLICABLE FI LTERS. 2 L 7 2 4F 4 F RT A1NM E24NE 2002121700183 20021217 00183 CE 2002 12 17 045461 1 20021127 A 3297 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MLG INOPERATIVE A AMWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 15YV UE15 AFTER TAKE OFF, THE LANDING GEAR FAILED TO RETRACT. THERE WAS ONE ADDITIONAL ATTEMPT TO CYCLE THE GEAR. IT STILL WOULD NOT RETRACT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED A WIRE IN THE LEFT NACELLE GROUND POINT. NO PAR TS WERE USED. 2 L 7 2 4T 3 T RT A24CE E2NE 2003022700069 20030227 00069 NM 2003 2 27 2002UALA01791 1 20021201 A 7920 FITTING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT IDG LOOSE A UALA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 601UA 21862 RIGHT GENERATOR DRIVE LIGHT AND EICAS MSG DISPLAYED WHEN POWER SET ON TAKEOFF. ABORTED TAKEOFF AT 65 KTS. LOOSE OIL LI NE FITTING IN IDG EXTERNAL OIL CIRCUIT CAUSED LOSS OF OIL RESULTING ILLUMINATION OF IDG DRIVE LIGHT DUE TO LOW OIL PRESS . OIL LINE TIGHTENED, IDG SERVICED, LEAK CHECK OF EXTERNAL OIL CIRCUIT ACCOMPLISHED. NO FURTHER PROBLEMS REPORTED. 2 L 7 2 4F 4 F RT A1NM E3NE 2003022700070 20030227 00070 NM 2003 2 27 2002UALA01793 1 20021128 A 2751 1817389 TRANSMITTER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE T/E FLAP FAULTY A UALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 29 917UA 25384 AIRCRAFT FLEW A MISSED APPROACH BECAUSE OF A FLAP ASYMMETRY CONDITION. REPLACED FLAP TRANSMITTER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700184 20021217 00184 CE 2002 12 17 045518 1 20021130 A 3200 CIRCUIT BREAKER BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MLG TRIPPED A AMWA O OTHER J WARNING INDICATION AP APPROACH 1 CE 07 173YV UE173 UPON ARRIVAL, THE MAIN LANDING GEAR WOULD NOT EXTEND TO NORMAL OPERATION. AFTER NOTICING THAT THE CIRCUIT BREAKER HAD POPPED, THE CREW RESET IT THREE TIMES, AFTER THE THIRD RESETTING THE CIRCUIT BREAKER STAYED. IT SHOWED 3 GREENS WITH NO RED HANDLE. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. A FUNCTIONAL CHECK WAS PERFORMED AND A TEST FLIGHT WAS MADE. NO PARTS WERE USED. 2 L 7 2 4T 3 T RT A24CE E2NE 2002121700185 20021217 00185 NM 2002 12 17 2002UALA01794 1 20021201 A 5320 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 RIGHT SIDE COCKPIT FLOOR WEB CRACKED THROUGH FASTENER HOLE STATION 210 ADJACENT TO SKIN ATTACH FLANGE. MAJOR REPAIR ACC OMPLISHED. FLOOR WEB REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121700186 20021217 00186 NM 2002 12 17 2002UALA01799 1 20021128 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 657UA 27112 EMERGENCY EXTERIOR LIGHT INOPERATIVE, AFT OF RIGHT WING. RELAMPED LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2002121700187 20021217 00187 WP 2002 12 17 IXXA0200095S 1 20020716 A 5330 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DISCOVERED ON THE FUSELAGE STATION 1210 LONGERON 19L FORWARD OF THE AFT E MERGENCY EXIT DOOR. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IAW TH E DOUGLAS SRM AND DRAWING 53-02491-2. 2 L 7 4 4F 4A25 2002121700188 20021217 00188 2002 12 17 045745 4 20021209 A 2230 SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA AUTOFEATHER SYS INOPERATIVE A AMWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 5YV UE5 DURING TAKE OFF ROLL ON FLIGHT ABOUT 80 KILOMETERS OUT, THE AUTOFEATHER ON AND REPEATER LIGHTS WENT OUT. THIS INDICATED THAT THE AUTOFEATHER WAS NOT ARMED. THE FLIGHT CREW ABORTED THE TAKE OFF AND RETURNED TO THE GATE WITH NO FURTHER INCIDE NT. MAINTENANCE ADJUSTED THE AUTOFEATHER THROTTLE SWITCHES AND DID A SYSTEM CHECK. NO PARTS WERE USED. 2 L 7 2 4T 3 T RT A24CE E2NE 2002121700189 20021217 00189 WP 2002 12 17 IXXA0200096S 1 20020716 A 5730 SKIN DOUG DC8 DC862F 3021972 WP LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT WING LEADING EDGE OUTBOARD XW488. REPAIR ACCOMPLI SHED, REMOVAL OF DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW THE DOUGLAS SRM AND EA 28298-5269- 02-129 2 L 7 4 4F 4A25 2002121700190 20021217 00190 WP 2002 12 17 IXXA0200097S 1 20020716 A 5330 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION AND CRACKS WERE DETECTED UNDER AN EXISTING REPAIR ON THE FUSELAGE AT STATIO N 1530 LONGERON 21L TO LONGERON 21R. REPAIR ACCOMPLISHED, REMOVED DAMAGED AREA AND EXISTING DOUBLER, FABRICATION AND IN STALLATION OF NEW REPAIR DOUBLER, FILLER AND FINGER DOUBLER IAW THE DOUGLAS SRM AND EA 28298-5209-02-125 2 L 7 4 4F 4A25 2002121700191 20021217 00191 2002 12 17 045748 4 20021209 A 2350 129034343601 CONTROL PANEL BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA AUDIO SYSTEM FAILED A AMWA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 07 15YV UE15 WHILE ENROUTE, THE CREW NOTICED THAT BOTH COMM 1 AND 2 WERE TRANSMITTING ALTHOUGH NEITHER OF THE MIC SWITCHES HAD BEEN D EPRESSED. THE CREW TURNED THE RADIOS OFF AND THEN BACK ON. THE MALFUNCTION APPEARED TO CORRECT ITSELF. THE CREW ALSO OBS ERVED THAT WHEN THE CAPTAINS WAFER SWITCHES WAS PLACED IN COMM 2 BOTH RADIOS WERE AGAIN TRANSMITTING. ABOUT 1 MINUTE AFT ER TURNING THE RADIOS BACK ON THEY REALIZED THAT THEY WERE NO LONGER ABLE TO TRANSMIT TO AIR TRAFFIC CONTROLLER ON EITHE R RADIO. THEY SQUAWKED 7600 AND PROCEEDED BACK UNEVENTFULLY. THE CREW MAINTAINED CONTACT THE ENTIRE WAY AND THEY WERE A BLE TO LAND WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE AUDIO CONTROL PANEL AND DID A SYSTEM OPERATIONAL CHECK. 2 L 7 2 4T 3 T RT A24CE E2NE 2002121700192 20021217 00192 WP 2002 12 17 IXXA0200098S 1 20020716 A 5730 SKIN DOUG DC8 DC862F 3021972 WP LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT WING LEADING EDGE AT XW 485. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF FILLER AND EXTERNAL DOUBLER IAW THE DOUGLAS SRM. 2 L 7 4 4F 4A25 2002121700193 20021217 00193 NM 2002 12 17 2002200284 1 20021127 A 3350 20131A BATTERY PACK BOEING 737 73733A 1384673 NM EMERGENCY LIGHTS INOPERATIVE B ERKR K NONE L NO TEST IN INSP/MAINT 1 WP 07 368CE 27456 FLOOR EMERGENCY LIGHTS IN ZONE 3 LEFT SIDE ( AFT CABIN ) ARE INOPERATIVE. REMOVED AND REINSTALLED EMERGENCY LIGHT BATTE RY PACK IAW MM AND POWER SUPPLY IAW MM. 2 L 7 2 4F RT A16WE 2002121700194 20021217 00194 SW 2002 12 17 20026 1 20021028 A 3242 212033 BRAKE SWRNGN SA226 SA226TB 8780406 SW GARRTT TPE331 TPE331* 01514 WP LEFT BURNED E STZA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 AL 03 95AC 81 81 T381 LEFT BRAKES CAUGHT FIRE DURING TAXI TO COMPANY HANGAR. PILOT REPORTED THAT THE LEFT BRAKE PEDAL WENT FLAT ON ROLL OUT, C ONTROL WAS TRANSFERED TO THE NON FLYING PILOT WHO REPORTED THE SAME. ENGINE THRUST AND HYDRAULIC STEERING WAS USED TO PR OVIDE BRAKING AND STEERING CONTOL. FIRE WAS OBSERVED AND EXTINGUISHED BY GROUND PERSONNEL. AIRCRAFT MASTER CYLINDERS, S HUTTLE VALVES, AND PARKING BRAKE VALVES WERE TESTED AND FOUND TO BE OPERATING NORMALY. BRAKE RESERVOIR WAS FULL AND NO E VIDENCE OF HYDRAULIC LEAKAGE WAS FOUND. BRAKES AND WHEELS WERE REPLACED AND A BRAKE (BURN IN) PROCEDURE WAS PERFORMED WI TH SATISFACTORY RESULTSTHE BRAKES HAVE BEEN RETURNED TO THE VENDOR FOR INVESTIGATION. 2 L 7 2 4T 3 T RT A5SW E2WE 2002121700195 20021217 00195 WP 2002 12 17 IXXA0200099S 1 20020718 A 5330 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE AT FUSELAGE STATION 1030 LONGERON 21R. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IAW THE DOUGLAS SRM AND ENGINEERING DRA WING 53-02491-3. 2 L 7 4 4F 4A25 2002121700196 20021217 00196 NM 2002 12 17 2002F01058 1 20021113 A 5210 SHROUD BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE PAX DOOR OUT OF ADJUST G AMTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 11 518AT 27974 DURING GROUND HANDLING, ESCAPE SLIDE ENGAGED WARNING PLACARD L-2 INOPERATIVE. MAINTENANCE ADJUSTED L-2 DOOR SHROUD. SL IDE ENGAGED WARNING OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM A12EU 2002121700197 20021217 00197 NM 2002 12 17 2002F01059 1 20021114 A 2110 6259283 SENSOR BOEING 757 75733N 1384931 NM A/C BAY INOPERATIVE G H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 GL 11 550TZ 32584 FLIGHT NUMBER 533. DURING CRUISE, LT PACK OFF AND PACK TEMP DISPLAYED (EICAS) INOP & PACK OFF LIGHT ILLUMINATED. LIGHT R E-ILLUMINATED AFTER PACK RESET IN STANDBY. MAINTENANCE REMOVED AND REPLACED COMPRESSOR OUTLET SENSOR TS41 IN ACCORDANCE WITH M.M. 21-51-11. PERFORMED OPS CHECK, PACK CHECKS NORMAL IN STANDBY MODE. OPERATIONAL CHECK IN AUTO MODE FAILS. REF 2 150/859 LOGPAGE 519724 ITEM 4 FOR NEW DISCREPANCY. 2 L 7 2 4F RT A2NM 2002121700198 20021217 00198 NM 2002 12 17 2002F01060 1 20021113 A 3610 32896265 VALVE BOEING 757 75723N 1384973 NM RT ENG PYLON INOPERATIVE G O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 515AT 27598 DURING CRUISE, RT ENGINE BLEED OFF DISPLAYED. MAINTENANCE REMOVED AND REPLACED FAN AIR MODULATING VALVE IAW MM 36-11-16 . OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2002121700199 20021217 00199 2002 12 17 2002F01061 4 20021126 A 2565 GIRT BAR BOEING 757 75723N 1384973 NM ESCAPE SLIDE OBSTRUCTED G D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 11 516AT 27972 DURING GROUND HANDLING, 4L DOOR SLIDE LIGHT, INOPERATIVE. MAINTENANCE FOUND ATTACHMENT POINT FOR SURVIVAL KIT ROPE STU CK UNDER GIRT BAR CAUSING ARM LIGHT TO FAIL DUE TO EXCESSIVE CLEARANCE BETWEEN GIRT BAR SLIDER (AFT SIDE). REPOSITIONED ATTACHMENT POINT OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2002121700200 20021217 00200 NM 2002 12 17 2002F01063 1 20021105 A 2822 609891004 IMPELLER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE BOOST PUMP INOPERATIVE G A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 520AT 27976 DURING CRUISE, RIGHT CENTER BOOST PUMP LIGHT ILLUMINATED. EICAS MESSAGE CTR RT FUEL PUMP DISPLAYED. MAINTENANCE REMOVED AND REPLACED THE RIGHT CENTER IMPELLER IAW M.M. 28-22-03-4. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM A12EU 2002121700201 20021217 00201 NE 2002 12 17 2002F01064 2 20021203 A 7510 7646B000 VALVE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE INOPERATIVE G O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 556TZ 896 896 32590 31864 DURING DESCENT LT ENGINE ANTI-ICE VALVE STUCK CLOSED. MAINTENANCE REMOVED AND REPLACED LT ENGINE ANTI-ICE VALVE. OPERATI ONAL CHECKS GOOD IAW MM. 2 L 7 2 4F 4 F RT A2NM E12EU 2002121700203 20021217 00203 NM 2002 12 17 2002F01077 1 20021130 A 2410 727792L IDG BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE LT ENGINE FAILED G AMTA H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CR CRUISE 1 GL 11 522AT 19047 19047 29330 31604 DURING CRUISE, RECEIVED EICAS MESSAGE GEN DRIVE DISPLAYED, GENERATOR DRIVE LIGHT ILLUMINATED. CREW DISCONNECTED GEN DRIV E. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE IDG IAW MM. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM A12EU 2002121700205 20021217 00205 2002 12 17 2002F01078 4 20021126 A 3460 4077880908 CDU BOEING 757 75733N 1384931 NM COCKPIT INOPERATIVE G O OTHER O OTHER CR CRUISE 1 GL 11 554TZ 32588 DURING CRUISE, RIGHT FMC CDU LIGHT INOPERATIVE. MAINTENANCE INSTALLED SERVICABLE RIGHT FMS CDU IAW MM, OPERATIONAL CHEC KS GOOD. 2 L 7 2 4F RT A2NM 2002121700214 20021217 00214 NE 2002 12 17 2002F01080 2 20021203 A 7320 EEC BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE INOPERATIVE G O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 558TZ 32592 31859 DURING CRUISE EEC AND RIGHT ENGINE LIMITER, INOPERATIVE, LIGHT ILLUMINATED. EICAS MESSAGE RIGHT ENG EEC & RIGHT ENG LIMI TER DISPLAYED. MAINTENANCE PERFORMED BITE CHECK ON RIGHT EEC, IAW FIM, NO FAULTS NOTED. SWAPPED RIGHT AND LEFT EEC FOR T ROUBLESHOOTING PURPOSES, RAN ENGINES, NO FAULTS NOTED. RETURNED LEFT AND RIGHT EEC TO ORIGINAL POSITION, RAN ENGINES, NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2002121700215 20021217 00215 NM 2002 12 17 2002F01082 1 20021126 A 2421 4077880908 CDU BOEING 757 75733N 1384931 NM COCKPIT INOPERATIVE G O OTHER O OTHER CR CRUISE 1 GL 11 554TZ 32588 DURING CRUISE RIGHT FMC CDU LIGHT INOPERATIVE. MAINTENANCE INSTALLED SERVICEABLE RIGHT FMS CDU IAW MM. OPERATIONAL CHEC KS GOOD. 2 L 7 2 4F RT A2NM 2002121700216 20021217 00216 NM 2002 12 17 2002F01083 1 20021130 A 3246 LM52254620629 BEARING BFGOODRICH BOEING 727 727264 138408M NM MAIN WHEEL ASSY FAILED A J A DUMP FUEL UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 01 260 47518403 20780 DURING TAKE OFF THE NR 4 MAIN WHEEL ASSEMBLY SEPARATED FROM THE MAIN LANDING GEAR. PILOTS REPORTED NO ABNORMAL INDICATIO NS IN THE COCKPIT. THE FLIGHT CREW WAS NOTIFIED OF THE SITUATION. THE AIRCRAFT LANDED SAFELY. INVESTIGATION REVEALED FA ILURE OF THE OUTBOARD BEARING CAUSING THE MAIN WHEEL ASSEMBLY TO FALL OFF THE STRUT . THE PART (BEARING) IS NOT APPROVED DUE TO THE FAILURE IT SUFFERED - THE TIRE HAD BEEN INSTALLED ON THE AIRCRAFT SINCE 12 OCTOBER 2002 OPERATING FOR 260:45 HRS AND 160 CYCLES, UNDER WORK ORDER 20020121 DATED 08 AUG 2002. DURING THE TIME OF OPERATION THE MWA WAS REMOVED AND R EINSTALLED TO ACCOMPLISH A MAIN BRAKE REPLACEMENT. 2 L 7 3 4F A3WE 2002121700217 20021217 00217 NM 2002 12 17 2002F01084 1 20021205 A 3350 LIGHT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE CABIN DISCONNECTED G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 DURING SCHEDULED MAINTENANCE FLOOR EGRESS LIGHTS ROWS 29-32 AND 35-37 WOULD NOT TEST. MAINTENANCE FOUND EGRESS LIGHT SO CKETS AT SEAT 32 AND 35 DISCONNECTED, RESECURED SOCKETS. EGRESS LIGHTING OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM A12EU 2002121700218 20021217 00218 NM 2002 12 17 2002F01085 1 20021211 A 3350 RING BOEING 757 75733N 1384931 NM RROYCE RB211 RB211* 54555 NE LIGHT SWITCH MISLOCATED G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 551TZ 32585 DURING GROUND HANDLING, SILVER METAL RETAINER RING ON EMERGENCY LIGHTS (PASSENGER) DOES NOT ALLOW EMERGENCY LIGHT SWITCH TO ARM LIGHTS WHEN BLACK COVER SWITCH IS PLACED IN THE ARM POSITION. MAINTENANCE REPOSITIONED RETAINER RING. SYSTEM OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM A12EU 2002121700219 20021217 00219 NM 2002 12 17 2002F01086 1 20021206 A 5315 FLOORBEAM BOEING 757 75723N 1384973 NM FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 517AT 27973 DURING SCHEDULED INSPECTION, LEVEL 2 CORROSION DISCOVERED AT FORWARD FUSELAGE SECTION, CORROSION ON FLOORBEAM TOP CAP AT FS 345, LBL 15. MAINTENANCE REPAIRED FLOORBEAM TOP CAP AFT SECTION AT FS 345, LBL 15 IAW SRM. 2 L 7 2 4F RT A2NM 2002121700220 20021217 00220 2002 12 17 2002F01090 4 20021212 A 3160 CIRCUIT CARD BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE EICAS SYS MALFUNCTIONED G AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 514AT 27971 DURING CRUISE EICAS STATUS MESSAGE L ENG OH LP 2 DISPLAYED. MAINTENANCE RERACKED PRINTED CIRCUIT CARD NR M10276 IAW MM, PERFORMED OPERATIONAL TEST, NO FAULTS OR MESSAGES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM A12EU 2002121700221 20021217 00221 CE 2002 12 17 5600097 1 20021008 A 3297 CIRCUIT BREAKER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG TRIPPED E ERYA O OTHER O OTHER CL CLIMB 1 CE 07 898CB 5600097 LANDING GEAR CONTROL CIRCUIT BREAKER TRIPPED WHEN GEAR RETRACT SELECTED. GEAR WILL NOT RETRACT 10/15/2002 PERFORMED CON TINUITY CHECK OF LANDING GEAR WIRING. FOUND NO DISCREPANCIES. PERFORMED FUNCTIONAL CHECK OF LANDING GEAR RETRACTION SY STEM NUMEROUS TIMES WITH NO DISCREPANCIES NOTED. COULD NOT DUPLICATE SQUAWK. 2 L 7 2 4F 4 F RT A22CE E25EA 2002121700222 20021217 00222 WP 2002 12 17 ABXA020342 1 20021126 A 2730 ELEVATOR DOUG DC9 DC931 3022065 WP PWA JT8 JT8D NE TAIL JAMMED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 908AX 47008 ELEVATOR JAMMED, WOULD NOT PULL BACK WHILE PERFORMING CONTROL CHECK. INSPECTED ELEVATOR TABS, CONTROL VALVES, FOLLOW UP MECHANISMS, LOAD FEEL AND CENTERING SPRING, VISIBLE PORTIONS OF CABLE RUNS IN TAIL COMPARTMENT AND E/E COMPARTMENT. NO D EFECTS FOUND. CONTROL COLUMN FORCES AND FLIGHT CONTROL SURFACE MOVEMENT CHECK, GOOD IAW MM. 2 L 7 2 4F 4 F A6WE E2EA 2002121700223 20021217 00223 WP 2002 12 17 ABXA020343 1 20021123 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP PWA JT8 JT8D* NE COCKPIT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 989AX 47314 COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND LIGHT BULBS. OPS CHECKED GOOD IAW AMM. 2 L 7 2 4F 4 F A6WE E2EA 2002121700224 20021217 00224 WP 2002 12 17 ABXA020344 1 20021126 A 3260 CONTACTOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE NLG IND LIGHT DAMAGED A ABXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 928AX 47392 ON DESCENT, NOSE GEAR UNSAFE LIGHT WAS INTERMITTENT WITH THROTTLES AT IDLE. CREW REPORTED CYCLED GEAR, CHECKED GOOD. FOU ND NOSE GEAR LIGHT BULB POSITIVE CONTACT FLATTENED AND MUSHROOMED CAUSING INTERMITTENT INDICATION. REPAIRED CONTACT. OPS CHECKED GOOD IAW AMM. 2 L 7 2 4F 4 F A6WE E2EA 2002121700225 20021217 00225 SO 2002 12 17 C2XA02BT084 1 20021216 A 3350 LIGHT EMB 145 EMB145ER 3260211 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 15926 145005 EWR---CO3533, CREW REPORTED AISLE PATH LIGHTING BETWEEN SEAT ROW 10A AND 12A INOPERATIVE....MAINTENANCE REMOVED AND REPL ACED AISLE PATH LIGHTING AT THE EMERGENCY EXIT IAW EMB145 AMM #33-50-08. OPS. CHECKED SYSTEM GOOD. 2 L 7 2 4F RT T00011AT 2002121700226 20021217 00226 WP 2002 12 17 ABXA020345 1 20021203 A 3260 DOWNLOCK SWITCH DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE NLG FAILED A ABXA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 23 928AX 47392 NOSE LANDING GEAR SAFE LIGHT TOOK SEVERAL MINUTES TO ILLUMINATE AFTER SELECTING GEAR DOWN. RESULTING IN A MISSED APPROA CH. THE GEAR SAFE LIGHT THEN ILLUMINATED. REPLACED THE NOSE LANDING GEAR DOWN LOCK SWITCH IAW MM. OPS CHECKED GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2002121700227 20021217 00227 WP 2002 12 17 ABXA020346 1 20021204 A 3260 WARNING LIGHT DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE NLG ILLUMINATED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 818AX 46075 NOSE GEAR FAILED UPLATCH GEAR UNSAFE LIGHT ON WITH GEAR RETRACTED. FOUND NOSE GEAR PIN INSTALLED WHEN AIRCRAFT TAXIED IN . INSPECTED NOSE GEAR AND CABLES FOR SAFETY OF FLIGHT INSPECTION. NO DEFECTS FOUND. AIRCRAFT OK FOR FLIGHT. 2 L 7 4 4F 4 F 4A25 1E8 2002121700228 20021217 00228 WP 2002 12 17 ABXA020347 1 20021206 A 3260 0080004003 CONTROL ARM DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE E & E BAY DEFECTIVE A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 825AX 604 46115 WITH GEAR HANDLE DOWN, GREEN LIGHTS NOT ON, RED LIGHTS NOT ON EITHER. ACCOMPLISHED ABNORMAL PROCEDURE, STILL NO LIGHTS. OTHER CHECKLIST ITEMS INDICATED ALL GEAR WAS DOWN AND LOCKED. FOUND GEAR WARNING INTERLOCK CIRCUIT BREAKER INTERMITTENT (D-3). REPLACED CIRCUIT BREAKER AND PROXIMITY SENSOR BOX. SYSTEM OPS CHECKED GOOD IAW MM. 2 L 7 4 4F 4 F 4A25 1E8 2002121700229 20021217 00229 WP 2002 12 17 ABXA020348 1 20021204 A 3350 5708458503 BATTERY DOUG DC8 DC863 302198A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 822AX 576 46079 EMERGENCY LIGHTS DIM WHEN PERFORMED CHECK FOR (A) CHECK. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW MM. 2 L 7 4 4F 4A25 2002121700230 20021217 00230 WP 2002 12 17 ABXA020349 1 20021206 A 2121 5007025211 FAN DOUG DC9 DC932F 3022067 WP PWA JT8 JT8D1 52044 NE E & E BAY BURNED OUT A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 904AX 214 47040 STRONG ELECTRICAL BURNING ODOR IN COCKPIT. RADIO RACK COOLING FAN FOUND TO BE SOURCE OF BURNING ODOR. REPLACED RADIO R ACK COOLING FAN IAW MM. OPS CHECKED GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2002121700231 20021217 00231 WP 2002 12 17 ABXA020353 1 20021206 A 7830 5958782503 LINK DOUG DC9 DC941 302207N WP PWA JT8 JT8D1 52044 NE THRUST REVERSER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 962AX 618 47768 NR 1 ENGINE UPPER RIGHT LINK THRUST REVERSER CRACKED. REPLACED IAW MM. 2 L 7 2 4F 4 F A6WE E2EA 2002121700232 20021217 00232 NM 2002 12 17 AMTA200201456 1 20021201 A 3350 BR9279109 SIGN LKHEED 1011 1011 N/A-SDR NM RROYCE RB211 RB21122* 54555 NE CABIN INOPERATIVE G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 195AT 193C1041 R-3 DOOR EMERGENCY EXIT SIGN OUT. 2 L 7 3 4F 4 F RT A23WE A12EU 2002121700233 20021217 00233 WP 2002 12 17 AMTA200201484 1 20021206 A 3350 5165744 BATTERY PACK LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211* 54555 NE CABIN DISCHARGED G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 164AT 1238 BATTERY PACK AMBER DISCHARGER LIGHT ON AT ALL TIME AT 1R CABIN DOOR. 2 L 7 3 4F 4 F A23WE A12EU 2002121700234 20021217 00234 CE 2002 12 17 AMW1 1 20021127 A 5230 12944004471 INTERCOSTAL BEECH 1900 1900D 1154162 CE PWA PT6 PT6A11 52043 NE CARGO DOOR FAILED A AMWA A UNSCHED LANDING E P VIBRATION/BUFFET NO WARNING INDICATION CL CLIMB 1 CE 07 146ZV UE146 AFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR TO NR 2 E NGINE START. TAKE OFF ROLL WAS NORMAL. JUST AFTER ROTATION, A VIBRATION BEGAN. THE LANDING GEAR RETRACTED AND THE ENGINE INSTRUMENTS WERE NORMAL. THE AIRCRAFT WAS THEN RETURNED TO FIELD AND THE CARGO DOOR WAS FOUND OPEN. HOWEVER THE CARGO D OOR ANNUNCIATOR LIGHT FAILED TO ILLUMINATE. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPLACED 3 CRACKED I NTERCOSTALS, DORSEL FIN AND 2 SHOCKS. THEY RIG CHECKED THE DOOR. NO TEARDOWN REPORT WILL BE REQUIRED. REFER TO CONTR OL NR045447. 2 L 7 2 4T 3 T RT A24CE E4EA 2002121700235 20021217 00235 CE 2002 12 17 AMW2 1 20021127 A 5230 10151418313 INTERCOSTAL BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CARGO DOOR FAILED A AMWA A UNSCHED LANDING E P VIBRATION/BUFFET NO WARNING INDICATION CL CLIMB 1 CE 07 146ZV UE146 AFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR TO NR2 EN GINE START. TAKE OFF ROLL WAS NORMAL. JUST AFTER ROTATION, A STRONG VIBRATION BEGAN. THE LANDING GEAR RETRACTED AND THE ENGINE INSTRUMENTS WERE NORMAL. THE AIRCRAFT WAS THEN RETURNED TO FIELD AND THE CARGO DOOR WAS FOUND OPEN. HOWEVER THE C ARGO DOOR ANNUNCIATOR FAILED TO ILLUMINATE. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPLACED 3 CRACKED IN TERCOSTALS, DORSEL FIN AND 2 SHOCKS. THEY ALSO RIG CHECKED DOOR. NO TEARDOWN REPORT WILL BE REQUIRED. REFER TO CONTROL N R045447. 2 L 7 2 4T 3 T RT A24CE E2NE 2002121700236 20021217 00236 NE 2002 12 17 ARWA20021106 2 20021114 A 7200 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D* 52039 NE NR 2 FAILED A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 802BN 55658 8477 45909 645781 AT 2130Z, NR 2 OIL QUANTITY RAPIDLY DROPPED TO 1 GALLON, SUBSEQUENTLY OIL PRESSURE DROPPED TO 5 PSI AND OIL PRESSURE LOW LIGHT ILLUMINATED. PERFORMED IN FLIGHT ENGINE SHUTDOWN PROCEDURE IAW ABNORMAL CHECKLIST, WINDMILLING OIL PRESSURE. RE MAINED AT 5 PSI. INSPECTED NR 2 ENGINE, FOUND EXCESSIVE AMOUNTS OF OIL INSIDE THRUST REVERSER AND EXHAUST DUCT AREA. PE RFORMED MAINTENANCE PROCEDURES FOR ONE ENGINE INOPERATIVE FERRY FLIGHT IAW MM. FERRY FLIGHT ACCOMPLISHED WITHOUT INCIDE NT. REMOVED AND REPLACED NR2 ENGINE IAW MM MASTER TALLY SHEET ON WORK ORDER # 0016160. PERFORMED RUN UP, CHECKED OK. 2 L 7 4 4F 4 F 4A25 1E8 2002121700237 20021217 00237 WP 2002 12 17 ARWA20021108 1 20021120 A 3230 45973405501 CYLINDER DOUG DC8 DC862 3021970 WP PWA JT3D JT3D* 52039 NE MLG INOPERATIVE A ARWA O OTHER J WARNING INDICATION CR CRUISE 1 SO 19 802BN 45909 IN FLIGHT, AFTER NORMAL GEAR RETRACTION , RED GEAR LIGHT ON AFTER UP LATCH CHECK. FOLLOWED ABNORMAL CHECKLIST. REMOVED AND REPLACED LEFT GEAR UP LATCH CYLINDER IAW MM, REMOVED AND REPLACED LEFT GEAR ACTUATING CYLINDER IAW MM. PERFORMED C HECK, NO LEAK, GOOD. PERFORMED GEAR EXTENSION AND RETRACTION IAW MM AND CHECKED INDICATION IAW MM. FOUND NORMAL OPERAT ION. 2 L 7 4 4F 4 F 4A25 1E8 2002121700238 20021217 00238 WP 2002 12 17 ARWA20021110 1 20021123 A 2910 75C756011 MODULE LKHEED 1011 1011385115 5265015 WP HYD SYSTEM FAILED A ARWA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 19 307GB 193U1131 LOST (A) HYDRAULIC SYSTEM QUANTITY JUST BEFORE TOUCHDOWN. REMOVED AND REPLACED HIGH PRESSURE FILTER HOUSING IAW MM. OP ERATIONS AND LEAK CHECK NORMAL IAW MM. 2 L 7 3 4F A23WE 2002121700239 20021217 00239 EA 2002 12 17 COMA0260715 1 20021215 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 959CA 7116 FLIGHT 9457 CABIN DOOR WARNING.COULD NOT DUPLICATE. OPERATIONAL CHECK OF DOOR AND WARNING SYSTEM WAS SATISFACTORY. 2 L 7 2 4F RT A21EA 2002121700240 20021217 00240 EA 2002 12 17 COMA0260718 1 20021215 A 3260 622EN1436 SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG INOPERATIVE A COMA L ABORTED APPROACH J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 920CA 7022 FLIGHT 9460 GEAR DISAGREE WARNING - NLG DID NOT EXTEND.REPLACED NLG DOORS MICROSWITCH DI14. 2 L 7 2 4F RT A21EA 2002121700241 20021217 00241 EA 2002 12 17 COMA0260719 1 20021214 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNRELIABLE A COMA L ABORTED APPROACH J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 920CA 7796 8 7022 FLIGHT 5134 GEAR DISAGREE WARING - NLG DID NOT EXTEND.REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2003020400159 20030204 00159 WP 2003 2 4 MWEA020728 1 20021212 A 3242 BRAKE DOUG DC9 DC982 3022082 WP MLG MALFUNCTIONED A MWEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 31 808ME 48070 AUTO BRAKES WILL NOT ARM. SYSTEM SHUTS OFF AFTER A FEW SECONDS. DEFERRED PER MEL 32-09. T-FUNCTION WITH DEACTIVATION KIT INSTALLED ON T/O (LEFT) MANIFOLD. 2 L 7 2 4F A6WE 2002121700242 20021217 00242 EA 2002 12 17 COMA0260716 1 20021215 A 5610 NP1393222 WINDOW CNDAIR CL600 CL6002B19 1900309 EA R/H INOPERATIVE A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 729CA 9526 7265 FLIGHT 5271 R/H COCKPIT WINDOW HEAT CAUTION.REPLACED THE COPILOTS WINDOW. 2 L 7 2 4F RT A21EA 2002121700243 20021217 00243 EA 2002 12 17 COMA0260720 1 20021213 A 3230 555406 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNRELIABLE A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 920CA 7022 FLIGHT 6084 GEAR DISAGREE, NLG DID NOT EXTEND.REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2002121700244 20021217 00244 EU 2002 12 17 QXEA0202176 1 20021215 A 2930 LINE FOKKER F28 F28MK4000 4990810 EU ZONE 400 LEAKING A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 492US 36480 11159 SEA - FLIGHT 2409 - UTILITY SYSTEM HYDRAULIC QUANTITY DROPPED BELOW THE YELLOW ARC IN FLIGHT. UPON GEAR EXTENTION, THE G EAR DOORS DID NOT RETRACT. CREW COMPLIED WITH THE APPLICABLE CHECKLISTS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A HYDRAULIC LINE IN THE RIGHT STUB WING LEAKING. THE LINE WAS REPLACED, LEAK CHECKS AND OPERATIONAL CHECKS WERE PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2002121700246 20021217 00246 EA 2002 12 17 COMA0270001 1 20021216 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 331CA 10061 FLIGHT 5132 NLG DOORS WARNING AND PROX SYSTEM FAULT.ADJUSTED NLG PROXIMITY SENSORS. 2 L 7 2 4F RT A21EA 2002121700247 20021217 00247 CE 2002 12 17 GLBA2002203 1 20021216 A 2400 1013810087 BATTERY BEECH 1900 1900D 1154162 CE A GLBA D RETURN TO BLOCK O OTHER CR CRUISE 1 NM 03 240GL 981 UE240 BATT TIE ANNUN ILLUMS IN FLIGHT, R&R BATTERY 2 L 7 2 4T RT A24CE 2002121700248 20021217 00248 NM 2002 12 17 AWXA200201204 1 20021216 A 2912 271N63111099 TUBE BOEING 757 7572S7 1384962 NM ZONE 444 CRACKED A AWXA O OTHER J K S WARNING INDICATION FLUID LOSS AFFECT SYSTEMS DE DESCENT 1 WP 28 903AW 0 0 23323 PHX - EMERGENCY LANDING - FLT 0085 - INBOUND TO PHX EN ROUTE FROM LAS THE L/H HYDRAULIC SYSTEM FLUID LEVEL WENT TO "0". DECLARED EMERGENCY AND LANDED SAFELY; AIRCRAFT TAXIED TO GATE UNDER ITS OWN POWER. MAINTENANCE TROUBLESHOT FLUID LOSS AN D FOUND THE L/H ENGINE HYDRAULIC PUMP PRESSURE SWITCH LINE CRACKED. REMOVED AND REPLACED CRACKED HYDRAULIC LINE, AND REP LACED THE CASE DRAIN FILTER. SERVICED HYDRAULIC SYSTEM AND RAN ENGINE, LEAK CHECK WAS GOOD IAW T/C R5M29601. 2 L 7 2 4F RT A2NM 2002121700249 20021217 00249 NM 2002 12 17 2002UALA01810 1 20021203 A 5320 CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 STATION 360 FUSELAGE FRAME, AT STRINGER 14 AND 15 RIGHT, FRAME ATTACH CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700250 20021217 00250 NM 2002 12 17 2002UALA01811 1 20021203 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 STATION 747, AT STRINGER 9L, FUSELAGE FRAME CRACKED AT RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER MANUFACTU RED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700251 20021217 00251 NM 2002 12 17 2002UALA01812 1 20021203 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 STATION 767, AT STRINGER 9R, FUSELAGE FRAME CRACKED AT RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER MANUFACTU RED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700252 20021217 00252 NM 2002 12 17 2002UALA01813 1 20021203 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 STATION 807 AT STRINGER 9L, FUSELAGE FRAME CRACKED AT RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. DOUBLER MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700253 20021217 00253 NM 2002 12 17 2002UALA01814 1 20021203 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 BODY STATION 947, LBL 17 THROUGH LBL 21. FLOORBEAM UPPER FLANGE HAS MATERIAL LOSS EXCEEDING LIMITS. MAJOR REPAIR ACCOMP LISHED. FLANGE REPAIR DOUBLER STRAP INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2003022700071 20030227 00071 NE 2003 2 27 2002UALA01815 2 20021123 A 7261 515B186 CARBON SEAL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE COKED A UALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 221UA 5623 30552 222154 SMOKE IN CABIN PER CREW. STRONG ODOR AND THIN SMOKE IN COCKPIT. NUMBER 1 ENGINE PRODUCING OIL SMELL IN CABIN. FOUND O IL IN THE SPINNER. CLEANED SPINNER AND DISK. RAN ENGINE AT HIGH POWER FOR 30 MINUTES. FOUND MORE OIL IN THE SPINNER. REPLACED ENGINE. ENGINE TEARDOWN FINDINGS: NR 1 BEARING CARBON SEAL SURFACE CONTAINED DEPOSITS OF BLACK OIL/COKE THAT AFFECTED PROPER CONTACT WITH THE SEAL SEAT. THE SEAL SEAT SHOWED SIGNS OF UNEVEN CONTACT WITH THE CARBON ELEMENT. THI S ALLOWED OIL TO LEAK INTO THE GAS PATH UPSTREAM OF THE LOW PRESSURE COMPRESSOR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002121900052 20021219 00052 NM 2002 12 19 2002UALA01817 1 20021203 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 CABIN FLOORBEAM UPPER CHORD IS CORRODED BS 324, RBL 61, WL 208. MAJOR REPAIR ACCOMPLISHED. SPLICED CABIN FLOORBEAM UPPE R CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121700254 20021217 00254 NM 2002 12 17 2002UALA01818 1 20021205 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 AFT PIT WEB CLIP TORN AT BODY STATION 807 STRINGER 26R. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700255 20021217 00255 NM 2002 12 17 2002UALA01819 1 20021204 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 EXTERNAL FUSELAGE SKIN DENT AT STATION 1008 JUST BELOW STRINGER 14L IS OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRI CATED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700256 20021217 00256 NM 2002 12 17 2002UALA01820 1 20021205 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 FORWARD ENTRY DOOR CUTOUT INTERCOSTAL OUTBOARD CORD CRACKED AT STA 360 STRINGER 14L. MAJOR REPAIR ACCOMPLISHED. REPLAC ED FORWARD ENTRY DOOR CUTOUT INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700257 20021217 00257 NM 2002 12 17 2002UALA01821 1 20021205 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE LIGHTNING STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 LIGHTNING STRIKE TO FUSELAGE SKIN. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN REPAIRED PER SRM. 2 L 7 4 4F 4 F RT A20WE E24NE 2002121700258 20021217 00258 NM 2002 12 17 2002UALA01823 1 20021205 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 949UA 26692 CABIN FLOOR BEAM UPPER CORD TOP SURFACE HAS EXCESSIVE MATERIAL LOSS AT BODY STATION 986 RBL 28 RBL 32 AND RBL 40. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700259 20021217 00259 NM 2002 12 17 2002UALA01824 1 20021205 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 949UA 26692 CABIN STATION 986 RBL 40 FLOORBEAM WEB HAS ELONGATED HOLE MEASURING .437. MAJOR REPAIR ACCOMPLISHED. INSTALLED FREEZE PLUG. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700262 20021217 00262 NM 2002 12 17 2002UALA01805 1 20021202 A 5310 CREASE BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 949UA 26692 AFT GALLEY DOOR LOWER SILL CREASE BEAM INNER CHORD HAS CORROSION STATION 947-986, STRINGER 17R, WL 208. MAJOR REPAIR AC COMPLISHED. REPLACED CREASE BEAM INNER CHORD. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700263 20021217 00263 NM 2002 12 17 2002UALA01806 1 20021202 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 FUSELAGE FRAME AT STATION 887, STRINGER 9R, FRAME CRACKED AT RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR MAN UFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700264 20021217 00264 NM 2002 12 17 2002UALA01807 1 20021202 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 STATION 867, STRINGER 9R, FUSELAGE FRAME CRACKED AT RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. DOUBLER MANUFACTURED AND IN STALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121700265 20021217 00265 NM 2002 12 17 2002UALA01808 1 20021202 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 STATION 294 THROUGH 398 AT STRINGER 17R, FLOOR CREASE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. NEW CREASE BEAM INSTAL LED. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121800001 20021218 00001 SO 2002 12 18 C2XA02SH140 1 20021218 A 5300 14524188001 CAP EMB 145 EMB145ER 3260211 SO CABIN GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV-DURING C CHECK CROSSBEAM CAP WAS FOUND GOUGED BETWEEN CENTER AND RIGHT HAND OMEGA BEAMS AT FRAME 22. MAINTENACE REM OVED AND REPLACED AFFECTED CROSSBEAM CAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002121800002 20021218 00002 SO 2002 12 18 C2XA02SH141 1 20021218 A 5300 14522459001 ANGLE EMB 145 EMB145ER 3260211 SO CABIN DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV- DURING C CHECK ANGLE WAS FOUND DENTED ON CENTER OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED AFFECTED ANGLE IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002121800003 20021218 00003 SO 2002 12 18 C2XA02SH142 1 20021218 A 5300 14522460009 BUTT STRAP EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV- DURING C CHECK CENTER OMEGA BEAM BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 23. MAINTENANCE REMO VED AND REPLACED AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002121800004 20021218 00004 SO 2002 12 18 C2XA02SH145 1 20021218 A 5400 14576603014 STIFFENER EMB 145 EMB145ER 3260211 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV- DURING C CHECK NUMBER 2 LOWER COWLING STIFFENER WAS FOUND GOUGED NEAR CENTER LINE AT STAION XN=2180.0MM. MAINTENAN CE REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO S ERVICE. 2 L 7 2 4F RT T00011AT 2002121800005 20021218 00005 SO 2002 12 18 C2XA02SH146 1 20021218 A 5400 14576525015 GUSSET EMB 145 EMB145ER 3260211 SO NICKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV DURING C CHECK GUSSET WAS FOUND NICKED ON NUMBER 2 LOWER COWLING AT STAION XN=3167.5MM. MAINTENANCE REMOVED AND REP LACED AFFECTED GUSSET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002121800006 20021218 00006 SO 2002 12 18 C2XA02SH148 1 20021218 A 5300 14525480003 BEAM EMB 145 EMB145ER 3260211 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV- DURING C CHECK CARGO DOOR CUT OUT LOWER BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTE D BEAM IAW EMB 145 SRM 51-40-06. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002121800007 20021218 00007 WP 2002 12 18 ARWA20021203 1 20021211 A 2910 AE7095071 HOSE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D* 52039 NE HYD SYS DAMAGED A ARWA O OTHER K FLUID LOSS DE DESCENT 1 SO 19 802BN 45909 LOST HYDRAULIC QUANTITY TOP OF DESCEND FOLLOWED BY ABNORMAL CHECKLIST AND PROCEDURES. CORRECTIVE ACTION: FOUND HYDRAULI C HOSE FROM PUMP ENGINE NR 2 DAMAGE. REMOVED AND REPLACED HOSE IAW MM, OPERATIONS CHECK OK IAW MM. 2 L 7 4 4F 4 F 4A25 1E8 2003022100002 20030221 00002 2003 2 21 AWXA200201195 4 20021212 A 2230 MODULE BOEING 737 7373G7 1384595 NM NR 2 ENGINE FAILED A AWXA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 WP 28 160AW 23782 ABORTED T/O DUE TO 2.5 KNOB THRUST LEVER STAGGER WITH AUTOTHROTS ENGAGED, THROT HOLD IN EFFECT, NR 2 THROT IN ADVANCED P OSITION. MAINT TROUBLESHOT PROBLEM, PERFORMED AUTOTHROT STAT TEST & RANGE CHECK, BOTH OK. BOTH ENGS RAN TO T/O POWER WIT H PMCS ON, NO DISCREPANCIES, WITH PMCS OFF A .25 KNOB SPLIT, EVERYTHING ELSE OK. AUTOTHROT SYS NEEDS MORE TROUBLESHOOT ING, PLACED ON MEL, COND. NR 1. AUTOTHROT SYS INOP. MAINT CHECKED FLT FAULT RECORD, ALL BUT 1 OF FLTS INDICATED NR 1 P MC/PLA FAULTED. R & R NR 2 ENG PMC, AUTOTHROT BITE TEST GOOD. BENCH TEST PMC CONFIRMED FAILURE. UNIT FAILED TEST FOR TOR QUE MOTOR LIMITER CHECK AS FUNCTION OF PLA. R & R A9 MODULE AND RESELECTED A6 MODULE AS C/A. UNIT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2002121800008 20021218 00008 NM 2002 12 18 AWXA200201196 1 20021212 A 2721 CONTROL SWITCH BOEING 737 7373G7 1384595 NM GE CFM56 CFM56* 13802 NE RUDDER TRIM INOPERATIVE A AWXA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 WP 28 150AW 23218 AIR TURN BACK ON CLIMB OUT, EXPERIENCED RUDDER AND TRIM PROBLEMS. UNABLE TO TRIM THE RUDDER, WITH AN INDICATION OF ONLY 2 UNITS, LEFT TRIM WILL NOT MOVE. REQUIRED AILERON 20 UNITS TO THE RIGHT IN ORDER TO MAINTAIN STRAIGHT AND LEVEL FLIGH T. TURNED BACK TO AIRPORT AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE RUDDER TRIM CONTROL SWI TCH, OPERATIONAL CHECK WAS GOOD. SDR WILL BE SUBMITTED UPON RECEIPT OF VENDOR BENCH TEST REPORT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121800009 20021218 00009 SO 2002 12 18 C2XA02CL221 1 20021104 A 3350 74441 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GALLEY INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16911 145446 THE CREW REPORTED THE EMERGENCY EXIT LIGHT IN THE GALLEY WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002121800010 20021218 00010 SW 2002 12 18 HMI2002F00000 1 20021116 A 6510 476440333 UNIVERSAL JOINT BELL 47 47G 1181002 SW FRNKLN 6AV335 6V335* 27040 EA TAIL ROTOR FAILED E HMIA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SW 15 6330D 778 1044 BEARING FAILURE IN UNIVERSAL JOINT. NOTICED BY VIBRATION IN FLIGHT AND CLICKING SOUND ON SHUT DOWN. INVESTIGATION SHOW ED OFF SET IN UNIVERSAL JOINT AND EXCESSIVE RUN OUT OF AFT TAIL ROTOR SHAFT. REPLACED UNIVERSAL JOINT, CHECKED RUN OUT, AFT SHAFT AND EXTERIOR SHAFT. AIRCRAFT RETURNED FOR SERVICE. 1 G 7 1 3O 3 O H1 E244 2002121800012 20021218 00012 NM 2002 12 18 UPS02239946 1 20021121 A 5312 PRESSURE PANEL BOEING 727 72751C 1384015 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE: C, NLG WHEEL WELL PRESSURE PANEL CRACKED AT BS 268, 3 INCHES DOWN FROM W/W CEILING. DAMAGED AREA CUTO UT IAW SRM 51-40-2 FIG 1 HFEC CONFIRMS A DEFECT FREE CONDITION, AREA REPAIR IAW SRM 51-40-2 F IG 1. 2 L 7 3 4F A3WE 2002121800013 20021218 00013 NM 2002 12 18 UPS02239947 1 20021113 A 5340 FITTING BOEING 727 72751C 1384015 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE: C&SI, WHILE CARRY OUT HFEC INSPECTION ON LT BS 950 FITTING. CRACK FOUND IN ROW 1 UP PER FASTENER HOLE , COMMON TO STR 9. DISCREPANT HOLE REPAIRED IAW SMRO EO 2002-061-003 UPS ENG. FILE NO. B727-5310-17956 2 L 7 3 4F A3WE 2002121800014 20021218 00014 NM 2002 12 18 UPS02239948 1 20021115 A 5310 BEAM BOEING 727 72751C 1384015 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE: C, DURING INSPECTION OF VERTICAL BEAM 17.8 RT, A CRACK WAS FOUND ON THE BEAM FLANGE. STOP CUT-OUT AT WL 273, BS 1183 REPAIR PARTS DRILLED OFF IAW EO B727-5310-11743. REPAIR ANGLES INSTALLED WET WITH SEALANT IAW EO B7 27-5310-11743 REPAIR COMPLETED ON EO B727-5310-11743 2 L 7 3 4F A3WE 2002121800015 20021218 00015 NM 2002 12 18 UPS02239949 1 20021119 A 3211 BOLT BOEING 727 72751C 1384015 NM MLG TRUNNION CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE: C, DURING REMOVAL OF LT HAND TRUNNION LINK, THE LT MAIN GEAR AFT TRUNNION BOLT AND TRUNNION HOUSING FO UND SHEARED. ON REMOVAL OF LT MLG, AFT BEARING MOUNTING JOURNAL FOUND CRACKED & PIECE BROKEN OFF. END OF JOURNAL.BEARI NG RETAINING BOLT SHEARED & SLIGHT DAMAGED TO BEARING. REF NRC 609755 FOR AFT TRUNNION BEARING REPLACEMENT. REF TC 1249 FOR LT MLG REPLACEMENT & SMRO EO 2002-061-007U PS. UPS ENGINEERING FILE NO. 727-54-20021 2 L 7 3 4F A3WE 2002121800016 20021218 00016 NM 2002 12 18 UPS02239950 1 20021115 A 5753 SPAR BOEING 727 72751C 1384015 NM RT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE: C, DURING LFEC INSPECTION OR RT INBOARD MID FLAP REAR SPAR UPPER CHORD, A CRACK WAS FOUND AROUND A FAS TENER HOLE. REPAIRED PER EO.B727-5750-3582. 2 L 7 3 4F A3WE 2002121800017 20021218 00017 NM 2002 12 18 UPS02239956 1 20021128 A 7830 BRACKET BOEING 727 72730C 1384009 NM THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE: C, ENGINE NR 1 & 3 THRUST REVERSER OUTBOARD FAIRING MID SUPPORT BRACKETS CRACKED. REPLACED BRACKETS I AW MM 20-80-01 2 L 7 3 4F A3WE 2002121800018 20021218 00018 NM 2002 12 18 UPS02239957 1 20021124 A 5312 BULKHEAD BOEING 727 72730C 1384009 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE: C, SUSPECT CRACKS IN NOSE WHEEL WELL BULKHEAD RT SIDE, BETWEEN FASTENER JUST UNDER CENTER OF FWD RT PR ESSURE PANEL REPAIR CARRIED OUT IAW SRM 51-10-1 & SRM 51-40-2 FIG 2 2 L 7 3 4F A3WE 2002121800019 20021218 00019 NM 2002 12 18 UPS02239958 1 20021204 A 3231 DOOR BOEING 727 72731C 1384011 NM NLG OUT OF RIG A IPXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 925UP 19230 NOISE FROM NLG AREA DURING FLIGHT, WITH RED DOOR WARNING INDICATION. LEVEL AT FL260, MACH 0.82, 342 KIAS. HEARD LOUD T HUMPING FROM FRONT OF AIRCRAFT WITH ASSCOCIATED RED 'DOORS' ANNUNCIATOR, SLOWED TO MACH 0.80 AND CONDITION WENT AWAY. P ERFORMED NLG DOOR RIG PER MM 32-22-01, CK GOOD 2 L 7 3 4F A3WE 2002121800020 20021218 00020 NM 2002 12 18 UPS02239960 1 20021202 A 5413 LONGERON BOEING 727 72730C 1384009 NM LT NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE: C, ENGINE NR 2, LT NACELLE. CRACK ON UPPER LONGERON AT BS 1387 APPROX UNDER BLOCK (DOOR SHEAR). LONGER ON REMOVED IAW SRM 51-30-02. NEW LONGERON MANUFACTURED IAW SRM 51-20-1. NEW LOGERON INSTALLED IAW SRM 51-30-02 & RE-PROT ECTED 2 L 7 3 4F A3WE 2002121800021 20021218 00021 NM 2002 12 18 UPS02239969 1 20021122 A 5312 PRESSURE PANEL BOEING 727 72730C 1384009 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE: C. SUSPECT CRACKS ON RT VERTICAL WEB OF NOSE WHEEL WELL IN AREA ADJACENT TO AFT LOWER CORNER OF AFT PR ESS PANEL REPAIR PARTS FABRICATED IAW SRM 51-40-2 FIG 1. REPAIR PARTS PROTECTED AS PER SRM 51-10-02. REPAIR PARTS AS SEMBLED AND FASTNERS INSTALLED AS PER SRM 51-30-02 & SRM 51-40-2 FIG 1 REMAINING FASTNERS INSTA LLED IAW SRM 51-30-02 & 51-40-2 FIG 1 2 L 7 3 4F A3WE 2002121800022 20021218 00022 NM 2002 12 18 UPS02239971 1 20021122 A 5312 PRESSURE PANEL BOEING 727 72730C 1384009 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE: C, SUSPECT CRACKS ON RT VERTICAL WEB OF NOSE WHEEL WELL AT UPPER FWD EN D OF AFT PRESSURE PANEL. R EPAIR CARRIED OUT IAW SRM 51-40-2 2 L 7 3 4F A3WE 2002121800023 20021218 00023 NM 2002 12 18 UPS02239974 1 20021122 A 5710 STRUCTURE BOEING 727 72730C 1384009 NM LEADING EDGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE: C, RT LE, REMOVABLE SECTION, SOME SCREWS HAVE PULLED THROUGH ON UPPER SURFACE AT O/B END (INTERSECTION OF NR 6 KREUGER & NR 5 SLAT). REPAIR CARRIED OUT IAW SMRO EO 2002-057-003. 2 L 7 3 4F A3WE 2002121800024 20021218 00024 NM 2002 12 18 UPS02439966 1 20021208 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INTERMITTENT A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 525UP 21939 INSPECTION TYPE: PFLT. EMERGENCY EXIT LIGHT IN CEILING JUST INBOARD OF UPPER DECK ESCAPE LATCH, COMES ON THEN GOES OFF AFTER A FEW SECONDS. REMOVED AND REPLACED LIGHT ASSY. OPS CHECK NORMAL IAW BMM 33-51-07. 2 L 7 4 4F A20WE 2002121800025 20021218 00025 NM 2002 12 18 UPS02439975 1 20021210 A 3150 CONTROL MODULE BOEING 747 747123 1384873 NM AURAL WARNING MALFUNCTIONED A IPXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 671UP 20323 ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN. TAKEOFF WARNING HORN SOUNDS WHEN THRUST LEVERS ARE ADVANCED WITH THE FOLLO WING CONDITIONS: FLAPS 20, TRIP 4.9 UNITS. REMOVED AND REPLACED AURAL WARNING CONTROL LOGIC MODULE PER MM -31-26-03 2 L 7 4 4F A20WE 2002121800026 20021218 00026 NM 2002 12 18 UPS02439979 1 20021207 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: PFLT, (FUSELAGE SKIN REPAIR REF "D" 246890) FUSELAGE SKIN REPAIR DOUBLER AT TAIL STAND DENTED & GOUGED . DRILLED OFF DAMAGED REPAIR DOUBLER. REMOVED TAILSTAND ATTACH FITTING FROM STRINGER 46 RT STA 2598. FABRICATED NEW DOU BLER & DRILLED. BEGAN FASTNER INSTALLATION IN REPAIR DOUBLER. COMPLETED INSTALLATION OF REMOVED PARTS & DOUBLER PER 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2002121800027 20021218 00027 NM 2002 12 18 UPS02439985 1 20021213 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 AFT MAIN DECK EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AS PER MM-33-51-07 OPS CK OK 2 L 7 4 4F A20WE 2002121800029 20021218 00029 NM 2002 12 18 UPS02639934 1 20021126 A 3231 537213 STRUT BOEING 767 767300 1385204 NM NLG DOOR FAILED A IPXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 314UP 27742 AIR TURN BACK DUE TO NOSE GEAR DOOR UPLATCH BROKE DURING GEAR RETRACTION WITH VIBRATION. FOUND RT NOSE GEAR DOOR STR UT ASSY FAILED INTERNALLY. 2 L 7 2 4F RT A1NM 2003012800121 20030128 00121 NM 2003 1 28 UPS02639978 1 20021207 A 5330 SKIN BOEING 767 76734AF 1385212 NM FUSELAGE BUCKLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 323UP 27749 INSPECTION TYPE:PFLT SKIN BUCKLED AT NOSE JACK POINT STA 287. REMOVED FASTENERS THROUGH SKIN IN DENTED AREA IAW SRM 51- 40-02. INSTALLED 90 PERCENT OF FASTNERS THAT WERE REMOVED AT BX 287 NOSE JACK POINT IN DENTED AREA IAW SRM 51-40-02. RE MAINING FASTENERS FOUND TO BE COMMON TO FRAME REPAIR AT BS 287. 2 L 7 2 4F RT A1NM 2002121800030 20021218 00030 NM 2002 12 18 UPS02639981 1 20021212 A 2750 ECU BOEING 767 767300 1385204 NM FLAP/SLATS INOPERATIVE A IPXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 327UP 27753 FLAP ASSYMETRY DURING FLAP RETRACTION AND FLAP T/E LOCKED. REMOVED AND REPLACED ELECTRONIC FLAPS/SLATS ASSY UNIT. PE R 767 MM 27-51-01-4 FLAP SYSTEM GROUND OPS CHECK NORMAL 2 L 7 2 4F RT A1NM 2002121800031 20021218 00031 WP 2002 12 18 UPS02839928 1 20021124 A 5312 PRESSURE PANEL DOUG DC8 DC871F 302199D WP RT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 BULGE AND POPPED FASTENERS IN RT W/W PRESSURE PANEL POSSIBLE FERRY FOR REPAIR. FABBED REPAIR PARTS IAW REO G08940, ALOD INED & PRIMED IAW DC8 SRM 51 -1-8 FABBED STIFFENER SPLICES AND STRAPS IAW DAC DWG SR08530029, INSTALLED REPAIR SPLICES A ND STIFFENER IAW DC8 SRM 51-1-20D & 51-1-21 INSTALLED CABLE PULLEY AND BRACKET IAW DC8 SRM 51-3-0 2 L 7 4 4F RT 4A25 2002121800032 20021218 00032 WP 2002 12 18 UPS02839929 1 20021124 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 STA 990, RT SIDE OUTBOARD FLOORBEAM LOWER FLANGE CORRODED POSSIBLE FERRY FOR REPAIR. FABBED REPAIR PARTS IAW REO G0894 0, ALODINED & PRIMED IAW DC8 SRM 51 -1-8 FABBED STIFFENER SPLICES AND STRAPS IAW DAC DWG SR08530029, INSTALLED REPAIR S PLICES AND STIFFENER IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2002121800033 20021218 00033 WP 2002 12 18 UPS02839936 1 20021126 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE: ASV, BULGE LT SIDE RUDDER. RUDDER HAS SKIN BULGE AT APPROX 4 FEET BELOW TIP AND 8 INCHES FROM TRAILING EDGE (BETWEEN LOWER STATIC WICKS) ON LT SIDE OF RUDDER. REMOVED RUDDER IAW MM 27-21-01 P401-P406 INSPCTED VERTICAL STR UCTURE FOR RUDDER SUPPORT. NO DAMAGE OK TO INSTALL RUDDER INSTALLED RUDDER PER MM 27-21-01 TO STEP 14L. 2 L 7 4 4F RT 4A25 2002121800034 20021218 00034 WP 2002 12 18 UPS02839951 1 20021201 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: ASV, EMERGENCY LIGHTS INOPERATIVE. REPAIRED OPEN AT P1-1345 PIN 11 AS REQUIRED REF WDW 33-50-01. SYS TEM OPS NORMAL. 2 L 7 4 4F RT 4A25 2002121800035 20021218 00035 WP 2002 12 18 UPS02839952 1 20021203 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE: ASV, EMERGENCY BATTERY PACK LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER 33 -50-00 OPS NORMAL. 2 L 7 4 4F RT 4A25 2002121800036 20021218 00036 WP 2002 12 18 UPS02839967 1 20021209 A 5320 WEB DOUG DC8 DC871F 302199D WP PRESSURE PANEL BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE: PFLT, LT W/W AREA HAS 3 POPPED RIVETS AND BULGE IN WEB. REMOVED 2 SECTIONS OF PRESSURE PANEL WEB IN L T WW AT STA 902. REMOVED CORROSION FROM FLOORBEAM FS 902 PER EO DC83107989 A-2. VERIFIED CORROSION REMOVAL & PERFORMED U LTRASOUND THICKNESS CHECK. ECA 43924-INSTALLED REPAIR STRINGER / SPLICES AT STA 902. INSTALLED STIFFNERS & PULLEYS SEALE D ENTIRE AREA. 2 L 7 4 4F RT 4A25 2003062500065 20030625 00065 WP 2003 6 25 UPS02839968 1 20021207 A 5280 DOOR DOUG DC8 DC873F 302199F WP NLG DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: PFLT, RT FUSELAGE NOSE W/W BELOW VENT DOOR SHEET METAL REPAIR. FERRIED TO TCO. REMOVED DAMAGE IAW DC8 SRM 51-1-21,OUT OF LIMITS IAW DC8 SRM 53-2-0. HEAT TREATED SPLICE CHANNEL & REPAIR SPLICE FABBED SPLICE CHANNEL & REPA IR SPLICE IAW DC8 DWG 5613861 & DC8 SRM 53-2-0, OK TO ALODINE. ALODINED SPLICE CHANNEL & REPAIR SPLICE IAW DC8 SRM 51-1 -8. PRIMED SPLICE CHANNEL & REPAIR SPLICE IAW DC8 SRM 51-1-8, OK TO INSTALL. 2 L 7 4 4F RT 4A25 2002121800037 20021218 00037 WP 2002 12 18 UPS02839976 1 20021209 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: PFLT, EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW MM 33- 50-01. 2 L 7 4 4F RT 4A25 2002121800038 20021218 00038 WP 2002 12 18 UPS02839977 1 20021210 A 3350 CONNECTOR DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE: PFLT, EMERGENCY LIGHT DISARM CHECK INOPERATIVE. REPLACED CONNECTOR PLUG P01-1345. SYSTEM CHECKS GOOD IAW M/M 33-50-01 2 L 7 4 4F RT 4A25 2002121800039 20021218 00039 WP 2002 12 18 UPS02839982 1 20021212 A 3350 570845803 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE: PFLT, EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. CHECKS OK. 2 L 7 4 4F RT 4A25 2003062500062 20030625 00062 WP 2003 6 25 UPS02839983 1 20021213 A 2611 SMOKE DETECTOR DOUG DC8 DC871F 302199D WP CARGO BAY WILL NOT TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: PFLT, MAIN CARGO DECK SMOKE DETECTORSPAA0200058S NR 1, 5, 6, 7 WILL NOT PROPERLY SELF TEST. REMOVED A ND REPLACED SMOKE DETECTOR AMPLIFIER. 2 L 7 4 4F RT 4A25 2002121800040 20021218 00040 WP 2002 12 18 UPS02839984 1 20021216 A 2611 AMPLIFIER DOUG DC8 DC873F 302199F WP SMOKE DETECTION INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 866UP 45966 NUMEROUS MAIN DECK SMOKE DETECTORS INOPERATIVE. REMOVED AND REPLACED SMOKE DETECTOR AMPLIFIER. ALL DETECTORS TEST OK. 2 L 7 4 4F RT 4A25 2002121800043 20021218 00043 CE 2002 12 18 NSVA200200007 1 20021216 A 5210 12951409513 CABLE BEECH BEECH 1900 1900D 1154162 CE BROKEN A NSVA O OTHER O OTHER UK UNKNOWN 1 EA 27 155CJ UE55 After parking at gate crew attempted to open airstair door. Door would not open with interior handle. Maintenance was dispatched and found the internal door cable was broken which prevented the six (6) door cams from rotating off of the d oor posts and unlocking the door. Maintenance replaced the broken cable with a new cable and returned the aircraft to s ervice. 2 L 7 2 4T RT A24CE 2002121800046 20021218 00046 2002 12 18 ABXA020362 4 20021217 A 3425 M05122503 ANNUNCIATOR DOUG DC9 DC932F 3022067 WP COCKPIT DEFECTIVE A ABXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 909AX 624 47148 BEFORE TAKE-OFF, ELECTRICAL BURNING ODOR AND SMOKE IN COCKPIT APPEARED. VERIFIED PROBLEM, FOUND WATER INTRUSION IN LEFT FLIGHT DIRECTOR MODE ANNUNCIATOR ASSEMBLY. REMOVED AND REPLACED CAPTAIN'S FLIGHT DIRECTOR MODE ANNUNCIATOR. OPS CHECKED GOOD IAW DC-9 MM 34-25-00. 2 L 7 2 4F A6WE 2002121800047 20021218 00047 SO 2002 12 18 C2XA02BT082 1 20021212 A 2611 WARNING SYSTEM EMB 145 EMB145 3260210 SO LAV SMOKE ACTIVATED A C2XA O OTHER N FALSE WARNING LD LANDING 1 SW 27 18102 145643 LAV SMOKE WARNING UPON LANDING FOR APPROXIMATELY 15 SECONDS. MAINTENANCE INSPECTED THE LAV NO FAULTS FOUND. OPERATIONAL TEST OF LAV SMOKE DETECTION SYSTEM AS PER EMB145 MM 26-14-00-700, CHECKS SERVICEABLE. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2002121800048 20021218 00048 WP 2002 12 18 IXXA0200100S 1 20020720 A 5313 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE SKIN STATION 1000 LONGEORN 19L. REPAIR ACCOMP LISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLAION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAI R MANUAL AND ENGINEERING DRAWING 53-02491-1. 2 L 7 4 4F 4A25 2002121800049 20021218 00049 WP 2002 12 18 IXXA0200101S 1 20020720 A 5330 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FORWARD COMPARTMENT DOOR CUT OUT LOWER CORNER AFT SECTION . REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF BELLY SKIN FROM STATION 270 TO 390 IN ACCORDA NCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 2002121800050 20021218 00050 WP 2002 12 18 IXXA0200102S 1 20020723 A 5230 STRUCTURE DOUG DC8 DC862F 3021972 WP CARGO DOOR DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION AND DENTS WERE DISCOVERED ON THE C-3 DOOR SCUFF PLATE. REPAIR ACCOMPLISHED , REMOVAL OF SCUFF PLATE AND DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER AND TRIPLER AND NEW SCUFF PLAT E IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING AUTHORIZATION 28298-5632-02-139 2 L 7 4 4F 4A25 2002121800051 20021218 00051 WP 2002 12 18 IXXA0200103S 1 20020731 A 5310 WINDOW FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FIRST LEFT CABIN WINDOW FRAME FUSELAGE STATION 300 LONG ERON 16L. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IAW DOUGLAS SRM. 2 L 7 4 4F 4A25 2002121800052 20021218 00052 WP 2002 12 18 IXXA0200104S 1 20020731 A 5310 WINDOW FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FOURTH LEFT CABIN WINDOW FRAME FUSELAGE STATION 490 LON GERON 16L. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE W ITH THE DOUGLAS STRUCTURAL REPAIR MANUAL 2 L 7 4 4F 4A25 2002121800053 20021218 00053 WP 2002 12 18 IXXA0200105S 1 20020813 A 5330 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE FUSELAGE STATION 742.250 LONGERON 21R BELOW FO RWARD EMERGENCY DOOR. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF FINGER DOUBLER AND DOUBLE R IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL 2 L 7 4 4F 4A25 2002121800054 20021218 00054 WP 2002 12 18 IXXA0200106S 1 20020819 A 5310 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE STATION 902 STRINGER 11. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANU AL AND DRAWING Q95-R01 2 L 7 4 4F 4A25 2002121800055 20021218 00055 NM 2002 12 18 371PA0014 1 20021216 A 2930 PLUG BOEING 737 737306 13844BG NM A PIDA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 SO 05 371PA 23543 Out of 21000, Hyd. electric pump A overheat light came on. Found case drain overheat switch plug dirty, cleaned plug, r econnected, A system electric pump ops chks good per MM 29-15-22. 2 L 7 2 4F RT A16NE 2002121800056 20021218 00056 WP 2002 12 18 2002F01094 1 20020603 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 961R 46133 FOUND DURING DOUGLAS D-CHECK INSPECTION, LIGHT SURFACE CORROSION ON LOWER CENTER FUSELAGE AREA BETWEEN CENTER WING STRIN GERS 67 AND 68 5 INCHES RIGHT OF ECWO. CORROSION OUT OF LIMITS STATION 759-768, 6 INCHES RIGHT OF CENTER LINE, ITEM 4 O N FORM 84. REMOVED CORROSION. FABRICATED DOUBLER TREATED, PRIMED AND INSTALLED DOUBLER. ALL WORK ACCOMPLISHED PER EO NR 02-039 REV A WITH APPROVED 8110-3. (M) 2 L 7 4 4F RT 4A25 2002121800057 20021218 00057 NM 2002 12 18 DL757021151 1 20020929 A 2530 811150417 COFFEEMAKER BOEING 757 757232 1384965 NM FWD GALLEY SHORTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 630DL 22920 A/C 630 ON FLT 1107 HAD ATB TO SAV DUE TO F/C GALLEY COFFEE MAKER HAD AN ELECTRICAL SHORT AND CAUSED HAZE/SMELL IN FWD GALLEY/CABIN AREAS. CREW REPORTED NO SMOKE IN COCKPIT. RETURNED TO SAV WITHOUT INCIDENT. FOUND FWD COFFEE MAKER BAD R EPLACED COFFEE MAKER OPS CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2002121800058 20021218 00058 WP 2002 12 18 IXXA0200107S 1 20020819 A 5330 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AT STATION 922 AND LONGERON 20L. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL 2 L 7 4 4F 4A25 2002121800059 20021218 00059 NM 2002 12 18 DL757021153 1 20020930 A 2432 BA0601 BATTERY BOEING 757 757232 1384965 NM APU OVERHEATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 6705Y 30397 AT GATE SMELL OF BURNING ELECTRICAL WIRE FROM AFT SECTION OF CABIN. APU BATTERY OVERHEAT, REPLACED APU BATTERY AND CHAR GER PER M/M OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2002121800060 20021218 00060 WP 2002 12 18 IXXA0200108S 1 20020716 A 5730 SKIN DOUG DC8 DC862F 3021972 WP LT WING LE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON A SCREW HOLE ON THE LEFT WING OUTBOARD LEADING EDGE STA XFS 7 10. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER AND DOUBLER IN ACCORDANCE WIT H THE DOUGLAS STRUCTURAL REPAIR MANUAL 2 L 7 4 4F 4A25 2002121800061 20021218 00061 NM 2002 12 18 DL757021176 1 20021009 A 2133 60883221 OUTFLOW VALVE BOEING 757 757232 1384965 NM CABIN PRESSURE MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 647DL 24218 SMOKE REPORTED IN AFT CABIN AT GATE DURING PREFLIGHT. R&R OUTFLOW VALVE ASSY PER M/M. OP CK GOOD. 2 L 7 2 4F RT A2NM 2002121800062 20021218 00062 NM 2002 12 18 DL757021177 1 20021005 A 5220 80330033 BOTTLE BOEING 757 757232 1384965 NM L4 DOOR LOW A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 ON L/O FOUND L4 DOOR OPEN ASSIST BOTTLE LOW. REPLACED BOTTLE PER MM. 2 L 7 2 4F RT A2NM 2002121800063 20021218 00063 NE 2002 12 18 DL757021179 2 20021009 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 LEAKING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 614DL 51909 22821 716308 ON APPROACH OIL PRESSURE STARTED TO FLUX IN YELLOW BAND. OIL PRESSURE WENT RED AND FLIGHT CREW SHUT ENGINE DOWN. FOUND NUMEROUS METAL ON NR 2 AND NR 3 BEARING CHIP DET AND ALSO MAIN OIL FILTER, REPLACED NR 1 ENG. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121800064 20021218 00064 NM 2002 12 18 DL757021186 1 20021011 A 2121 731376A FAN BOEING 757 757232 1384965 NM E/E BAY SEIZED A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 625DL 22915 AFTER TWO HOURS OF FLIGHT, STRONG ELECTRICAL/SULPHUR SMELL NOTED IN CABIN AND COCKPIT. ALSO GOT EQUIP OVERHEAT EICAS AN D LIGHT. LIGHT WENT OUT AFTER SELECTING OVERRIDE. FOUND FWD EQUIPMENT SUPPLY FAN NR 1 SEIZED. REPLACED FAN AND SYST EM NOW OPERATES NORMALLY. 2 L 7 2 4F RT A2NM 2002121800065 20021218 00065 WP 2002 12 18 IXXA0200110S 1 20020716 A 5311 FRAME DOUG DC8 DC862F 3021972 WP TAIL CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE AFT TAIL COMPARTMENT RT CIRCUMFERENTIAL FRAME, AFT AND AB OVE ACCESS PANEL 62 ZONE 37. REPAIR ACCOMPLISHED, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL 2 L 7 4 4F 4A25 2002121800066 20021218 00066 NM 2002 12 18 DL757021195 1 20021014 A 3350 LIGHT BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 6711M 30483 EMERGENCY EXTERIOR EGRESS LIGHT FOR R4 DOOR INOP. RELAMPED CHECKS OK. 2 L 7 2 4F RT A2NM 2002121800067 20021218 00067 WP 2002 12 18 IXXA0200111S 1 20020718 A 5320 DRAIN MAST DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 73466 2988 46129 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE BASE OF THE DRAIN MAST AT STATION 1574 LONGERON 28R. R EPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STR UCTURAL REPAIR MANUAL 2 L 7 4 4F 4A25 2002121800068 20021218 00068 NM 2002 12 18 DL757021196 1 20021015 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 626DL 22916 ONE SECTION OF EMERGENCY LIGHTING IS INOP AFT CABIN RIGHT SIDE. REPLACED POWER SUPPLY M736. ALL EMERGENCY LIGHTS NOW O PERATE NORMALLY. 2 L 7 2 4F RT A2NM 2002121800069 20021218 00069 NM 2002 12 18 DL757021213 1 20021019 A 3350 20131A BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 678DL 25983 SEVERAL AFT EMERG LIGHTS INOP IN AFT CABIN. REPLACED MODULE 737 BATTERY PACK. CKS OK. 2 L 7 2 4F RT A2NM 2002121800070 20021218 00070 NM 2002 12 18 DL757021225 1 20021023 A 3350 OL307IBPEGPL LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 652DL 24392 DOOR 1L EMERGENCY EXIT SIGNS INOP, RELAMPED. 2 L 7 2 4F RT A2NM 2002121800071 20021218 00071 WP 2002 12 18 IXXA0200114O 1 20021119 A 3260 STRIKER DOUG DC8 DC862 3021970 WP MLG UPLOCK LOOSE A IXXA O OTHER N FALSE WARNING CR CRUISE 1 SW 11 728PL 82639 771 45918 ENROUTE KWA TO HIK, THE GEAR DOOR NOT LATCH LIGHT ILLUMINATED. THE FLIGHT CREW CYCLED THE GEAR, PERFORMED AN GEAR UPLOCK CHECK AND THE WARNING INDICATION EXTINGUISHED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPE CTED THE LANDING GEAR INDICATION SYSTEM LOCATING THE MAIN GEAR DOORS STRIKERS LOOSE. MAINTENANCE SECURED THE STRIKERS AN D PERFORMED A SUCCESSFUL OPERATIONAL TEST IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVIC E. 2 L 7 4 4F 4A25 2002121800072 20021218 00072 WP 2002 12 18 IXXA0200116O 1 20021202 A 2910 O-RING DOUG DC8 DC862 3021970 WP HYD SELECT VALVE LEAKING A IXXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 11 728PL 45918 EN ROUTE FROM NKW TO BAH. FLIGHT CREW NOTED MAIN HYDRAULIC SYSTEM FLUID QUANITY DECLINING. CREW FOLLOWED COMPANY PROCEDU RES AND CONTINUED WITHOUT INCIDENT TO BAH. MAINTENANCE DISCOVERED O-RING LEAKING AT MAIN HYDRAULIC SYSTEM SELECTOR VALVE . REPLACED O-RING AND SERVICED HYDRAULIC SYSTEM IN ACCORDANCE WITH THE DOUGLAS MAINTENANCE MANUAL. 2 L 7 4 4F 4A25 2002121800073 20021218 00073 NM 2002 12 18 SPAA0200059 1 20021215 A 5313 UNK INTERCOSTAL BOEING 737 7372T4 1384492 NM CRACKED A SPAA O OTHER O OTHER IN INSP/MAINT 1 WP 28 703S 48754 22529 Initial compliance of A.D. 2000-05-29, Service Bulletin 737-53A1173 revealed a crack in the intercostal on the L/H side behind Sta 178 pressure bulkhead at WL 195 LBL 24. Intercostal repaired per SRM 53-10-1, Figure 10. 2 L 7 2 4F A16WE 2002121800074 20021218 00074 WP 2002 12 18 IXXA0200117S 1 20020802 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A CRACK ALONG WITH CORROSION WAS DETECTED ON THE LT WING UPPER AFT SKIN ABOVE THE LT GEAR TRUNNION AREA. REAPIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACC ORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING AUTHORIZATION R12-R01. 2 L 7 4 4F RT 4A25 2002121800075 20021218 00075 NM 2002 12 18 DL757021230 1 20021024 A 2520 845414402 SHROUD BOEING 757 757232 1384965 NM SEAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 628DL 22918 ONE OF TWO RED EMERG ESCAPE PATH LIGHTS RIPPED OUT OF SEAT 26D. DUE TO SHROUD DAMAGE REPLACED SEAT ASSY. 2 L 7 2 4F RT A2NM 2002121800076 20021218 00076 WP 2002 12 18 IXXA0200119S 1 20020822 A 5310 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED UNDER A TEMPORARY REPAIR OF THE FORWARD FUSELAGE, STATION 45 AT LONGERON 9L ADJACENT TO L-1 DOOR FRAME. REPAIR ACCOMPLISHED, REMOVAL OF THE TEMPORARY REPAIR AND DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER, DOUBLER AND TRIPLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEER ING AUTHORIZATION R12-R03. 2 L 7 4 4F RT 4A25 2002121800077 20021218 00077 NM 2002 12 18 DL757021249 1 20021027 A 2120 ODOR BOEING 757 757232 1384965 NM CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 633DL 23614 ODORS DETECTED IN CABIN NEAR ROWS 26-29. NO SMOKE BUT STRONG RUBBER LIKE ODOR PRESENT. ODOR SUBSIDED AFTER LANDING. R AN ENGINES AND PRESSURIZED A/C TO 5 PSID. INSPECTED CABIN, GALLEYS AND LAVS. NO UNUSUAL ODORS PRESENT. VERIFIED CARGO COMPARTMENTS NORMAL. NO ODORS PRESENT. 2 L 7 2 4F RT A2NM 2002121800078 20021218 00078 NM 2002 12 18 DL757021250 1 20021027 A 3231 2670296M1 SEQUENCE VALVE BOEING 757 757232 1384965 NM NLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 656DL 24396 AFTER T/O CREW REPORTED GEAR DOOR LIGHT ILLUMINATED WITH ASSOCIATED EICAS MSG. CREW REQUESTED TO CYCLE GEAR, NO HELP, C REW REPORTED THAT IT SOUNDED/FELT AS IF THE NOSE GEAR DOOR DID NOT CLOSE. REPLACED NOSE GEAR DOOR SEQUENCE VALVE AND NL G OPERATED SEQUENCE VALVE. JACKED A/C AND CYCLED NOSE GEAR, NOSE GEAR/DOOR OPERATION NOW CHKS NORMAL. 2 L 7 2 4F RT A2NM 2002121800079 20021218 00079 NM 2002 12 18 DL757021253 1 20021028 A 2520 829913434 SEAT BOEING 757 757232 1384965 NM CABIN BROKEN A DALA K NONE O OTHER TO TAKEOFF 1 SO 27 604DL 22811 SEAT FRAME BROKE ON TOURIST SEAT 22DEF ON TAKEOFF IN PHL. REPLACED SEAT. 2 L 7 2 4F RT A2NM 2002121800080 20021218 00080 NM 2002 12 18 DL757021254 1 20021025 A 5330 143N31311 SKIN BOEING 757 757232 1384965 NM FUSELAGE LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 601DL 22808 LIGHTNING STRIKE DAMAGE REPAIR, THE FUSELAGE SKIN WAS FOUND WITH LIGHTNING STRIKE DAMAGE AT FS 499, JUST ABOVE THE STRIN GER 4R SKIN LAP JOINT. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL REPAIR DOUBLER PER ER/A 3839 92-14, REV A. 2 L 7 2 4F RT A2NM 2002121800081 20021218 00081 NM 2002 12 18 DL757021255 1 20021027 A 5330 143N31311 SKIN BOEING 757 757232 1384965 NM FUSELAGE LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 601DL 22808 LIGHTNING STRIKE DAMAGE REPAIR, THE FUSELAGE SKIN WAS FOUND WITH LIGHTNING STRIKE DAMAGE AT FS 478 AT THE STRINGER 4L SK IN LAP JOINT. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL REPAIR DOUBLER PER ER/A 383991-14, REV A. 2 L 7 2 4F RT A2NM 2002121800082 20021218 00082 NM 2002 12 18 DL757021256 1 20021027 A 5330 143N31212 SKIN BOEING 757 757232 1384965 NM FUSELAGE LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 601DL 22808 LIGHTNING STRIKE DAMAGE REPAIR, THE FUSELAGE SKIN AT FS 720 WAS FOUND WITH LIGHTNING DAMAGE AT STRINGER 3L. THE DAMAGE WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL REPAIR DOUBLER PER ER/A 384001-14, REV A. 2 L 7 2 4F RT A2NM 2002121800083 20021218 00083 NM 2002 12 18 DL757021272 1 20021031 A 3350 20131A BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 626DL 22916 AFT RT EMERGENCY LIGHTS WILL NOT TEST WITH FWD TEST SWITCHES. REPLACED BATTERY PACK CKS GOOD. 2 L 7 2 4F RT A2NM 2002121800084 20021218 00084 WP 2002 12 18 IXXA0200120S 1 20020826 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FUSELAGE, FS 1620 LONGERON 21L BY THE AFT ENTRY DOOR CUT OUT ON THE LOWER FORWARD CORNER. REPAIR ACCOMPLISHED, REMOVED DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER, DO UBLER AND TRIPLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2002121800085 20021218 00085 NM 2002 12 18 DL757021275 1 20021031 A 5330 146N36106 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 601DL 22808 CUTOUT REPAIR, THE FUSELAGE SKIN WAS FOUND WITH SIGNS OF CORROSION AT AN EXISTING SKIN REPAIR. THE REPAIR WAS REMOVED A ND ALL CORROSION DAMAGE REMOVED WITH A CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL REPAIR DOUBLER PER ER/A 383949- 14, REV A. 2 L 7 2 4F RT A2NM 2002121800086 20021218 00086 WP 2002 12 18 IXXA0200121S 1 20020826 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE SKIN. FUSELAGE STATION 8 LONGERON 28R. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER AND DOUBLER IN ACCORDANCE WITH THE DOUGL AS STRUCTURAL REPAIR MANUAL AND ENGINEERING AUTHORIZATION R12-R05. 2 L 7 4 4F RT 4A25 2002121800087 20021218 00087 NM 2002 12 18 DL757021276 1 20021030 A 5320 143N852210 SILL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 601DL 22808 CORROSION REPAIR, THE OUTBD CHORD OF THE LOWER SILL OF THE C1 DOOR CUTOUT WAS FOUND WITH SEVERAL AREAS OF CORROSION. TH E OUTER CHORD AND WEB OF THE FS 620 OPENING FRAME WERE CUT AT STR 25R AND THE LOWER ENDS REMOVED TO ALLOW REMOVAL OF THE SILL CHORD. A NEW SILL CHORD WAS INSTALLED AND THE DOOR FRAME AND WEB SPLICED BACK IN WITH REPAIR ANGLES AND DOUBLERS PER ER/A 383863-14, REV B. 2 L 7 2 4F RT A2NM 2002121800088 20021218 00088 NM 2002 12 18 DL757021278 1 20021030 A 5330 146N35317 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 601DL 22808 CORROSION REPAIR, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT THE LOWER AFT VHF ANTENNA CUTOUT AT FS 1473 AND RBL 3. TH E CUTOUT WAS ENLARGED TO REMOVE ALL DAMAGE AND REPAIRED WITH 2 EXTERNAL REPAIR DOUBLERS PER ER/A 383865-14, REV A. 2 L 7 2 4F RT A2NM 2002121800089 20021218 00089 NM 2002 12 18 DL757021279 1 20021030 A 5330 143N31311 SKIN BOEING 757 757232 1384965 NM FUSELAGE LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 601DL 22808 LIGHTNING STRIKE REPAIR, THE FUSELAGE CROWN SKIN WAS FOUND WITH A LIGHTNING BURN DAMAGE LOCATION AT FS 600 BETWEEN STRIN GERS 2R & 3R. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 2 EXTERNAL REPAIR DOUBLERS PER ER/A 384019-14, REV A. 2 L 7 2 4F RT A2NM 2002121800090 20021218 00090 NM 2002 12 18 DL757021291 1 20021104 A 7920 B-NUT BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE LOOSE A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 610DL 22817 727274 FLIGHT DIVERTED TO DEN EN ROUTE TO SAN BECAUSE OF OIL LOSS IN THE RIGHT ENGINE. FOUND OIL LINE LEAKING AT FUEL/OIL HEAT EXCHANGER. TIGHTENED B-NUT ON LINE ALONG WITH ALL OTHER LINES GOING TO AND COMING FROM EXCHANGER. RAN ENGINE LEAK CKS OK. ENGINE WAS NOT SHUTDOWN INFLIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121800091 20021218 00091 NM 2002 12 18 SPAA0200060 1 20021215 A 5313 UNK INTERCOSTAL BOEING 737 7372T4 1384492 NM Zone 200 CRACKED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 48754 22529 Intercostal at Fuselage Station 178 R/H side, WL 195, RBL 24 is cracked. 2 L 7 2 4F A16WE 2002121800092 20021218 00092 NM 2002 12 18 DL757021301 1 20021107 A 2560 61020 BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 640DL 23994 DURING LAYOVER FOUND AFT RIGHT F/A EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PACK. 2 L 7 2 4F RT A2NM 2002121800093 20021218 00093 NM 2002 12 18 DL757021308 1 20021110 A 3350 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 648DL 24372 EMERGENCY EXIT LIGHT OVER 2R DOOR INOP. 2 L 7 2 4F RT A2NM 2002121800094 20021218 00094 NM 2002 12 18 DL757021320 1 20021114 A 3233 161N0001147 ACTUATOR BOEING 757 757232 1384965 NM RT MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 628DL 22918 EICAS, MSGS AFTER GEAR HANDLE RAISED, RIGHT MLG SHOWED DOWN AND GREEN THROUGHOUT. REPLACED RT MLG RETRACT ACTUATOR PER MM. JACKED A/C, PERFORMED 3 GEAR RETRACTION/EXTENTIONS. GEAR OPERATION AND IND CHKS OK PER MM. RETRACT ACT LEAK CHK O K. 2 L 7 2 4F RT A2NM 2002121800095 20021218 00095 NM 2002 12 18 DL757021328 1 20021114 A 5320 143N851212 SILL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 CORROSION REPAIR, THE OUTER CAP OF THE C1 DOOR OPENING LOWER SILL BEAM WAS FOUND CORRODED. TO FACILITATE REMOVAL, THE O UTER CHORD OF THE FS 620 OPENING FRAME WAS CUT AT STR 25R AND THE LOWER SECTION REMOVED. A NEW SILL CHORD WAS INSTALLE D AND THE FRAME CHORD SPLICED BACK IN WITH REPAIR ANGLES. THE WORK WAS ACCOMPLISHED PER ER/A 384082-14, REV A. 2 L 7 2 4F RT A2NM 2002121800096 20021218 00096 NM 2002 12 18 DL757021329 1 20021115 A 2530 811150417 COFFEEMAKER BOEING 757 757232 1384965 NM GALLEY MALFUNCTIONED A DALA H B DEACTIVATE SYST/CIRCUITS EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 657DL 0544 24419 AT FLT LVL 270 FROM ATL TO BWI FLT ATTN REPORTED WHITE/GRAYISH SMOKE COMING FROM THE AFT GALLEY ABOVE THE CEILING PANEL. REMOVED GALLEY POWER, SMOKE STILL EVIDENT. DECLARED EMERGENCY INTO CLT. DISCOVERED THE AFT GALLEY LEFT COFFEE MAKER HAS BURNED HEATING ELEMENT AND WAS SOURCE OF SMOKE. REPLACED COFFEE MAKER. 2 L 7 2 4F RT A2NM 2002121800097 20021218 00097 NM 2002 12 18 DL757021330 1 20021116 A 7110 314N301016B COWLING BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE LEAKING A DALA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 27 619DL 22909 716599 PANEL UNDER LT ENG FWD COWL OPENED EN ROUTE LGA. FOUND AIR LEAK INSIDE INLET COWL. REPLACED LT ENG NOSE COWL PER MM PE RFORMED ENG ANTI-ICE CKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121800098 20021218 00098 NM 2002 12 18 DL757021356 1 20021121 A 3350 LIGHT BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 601DL 22808 DURING L/O CK FOUND R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED CKS GOOD. 2 L 7 2 4F RT A2NM 2002121800099 20021218 00099 NM 2002 12 18 DL757021358 1 20021122 A 7830 SWITCH BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE THRUST REVERSER OUT OF ADJUST A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 601DL 22808 716334 ON INITIAL POWER APPLICATION FOR T/O LEFT ENGINE REVERSER LIGHT ILLUMINATED. WITH POWER REDUCED LIGHT EXTINGUISHED. DE ACTIVATION PINS INST LOCKING T/REV IN FWD THRUST. ADJUSTED RIGHT SIDE CENTER PROX SWITCH. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121800100 20021218 00100 NM 2002 12 18 DL757021362 1 20021124 A 2120 ODOR BOEING 757 757232 1384965 NM CABIN DETECTED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 677DL 25982 SEVERAL FLT ATT AND PAX REPORTED AN ODOR LIKE BURNT RUBBER AROUND ROW 4 RETURNED TO GATE. UNABLE TO DUPLICATE. 2 L 7 2 4F RT A2NM 2002121800101 20021218 00101 NM 2002 12 18 DL757021363 1 20021123 A 2120 ODOR BOEING 757 757232 1384965 NM CABIN DETECTED A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 606DL 22813 5 MIN FROM LANDING F/A CALLED COCKPIT AND SAID THEY SMELLED SMOKE NEAR ROW 36. VECTORED FOR IMMEDIATE LANDING. LANDED W/O INCIDENT. STOPPED ON TAXIWAY, F/A REPORTED SMELL HAD CLEARED. AIRCRAFT INSPECTED BY FIRE OFFICIALS W/O RESULT. RA N ENGS AND PACKS W/ NO RESULT. DUE TO EVOLVING HISTORY OF AFT CARGO HEAT FAN, REPLACED SAME. CKS OK. 2 L 7 2 4F RT A2NM 2002121800102 20021218 00102 NM 2002 12 18 DL757021388 1 20021129 A 4990 SOLENOID BOEING 757 757232 1384965 NM APU FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 672DL 25977 APU WILL NOT START IN FLIGHT AFTER NUMBER TWO ENGINE IDG WAS DISCONNECTED FOR DRIVE LIGHT. REPLACED APU DEOILER SOLENOI D NOW CKS NORMAL. 2 L 7 2 4F RT A2NM 2002121800103 20021218 00103 WP 2002 12 18 IXXA0200122S 1 20020826 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FUSELAGE, AT FS 1620 LONGERON 11R ON THE UPPER AFT CORNE R OF THE AFT SERVICE DOOR CUT OUT. REPAIR ACCOMPLISHED, CUT OUT DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR FI LLER, DOUBLER AND TRIPLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2002121800104 20021218 00104 2002 12 18 DL757021399 4 20021202 A 2330 CIRCUIT BREAKER BOEING 757 757232 1384965 NM E/E BAY FAILED A DALA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE IN INSP/MAINT 1 SO 27 604DL 22811 C/B "VIDEO SYS AC UTILITY" IN E/E COMPARTMENT FUSED CLOSED. ALSO ALL 5 VIDEO MONITOR C/B'S POPPED AND WON'T RESET. CAU SING C/B TO CATCH ON FIRE. REPLACED C/B AND RELAY. 2 L 7 2 4F RT A2NM 2002121800105 20021218 00105 WP 2002 12 18 IXXA0200123S 1 20020826 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FUSELAGE UPPER FORWARD CORNER OF THE FORWARD SERVICE DOOR CUT OUT. REPAIR ACCOMPLISHED, REMOVED DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER, DOUBLER AND TRIPLER IN AC CORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND DRAWING R12-R03. 2 L 7 4 4F RT 4A25 2002121800106 20021218 00106 WP 2002 12 18 IXXA0200124S 1 20020826 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FUSELAGE AT FS 490 LONGERON 11R UPPER AFT CORNER OF THE F ORWARD SERVICE DOOR CUT OUT. REPAIR ACCOMPLISHED, REMOVED DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOULBER AND TRI PLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING AUTHROIZATION EAR12-01. 2 L 7 4 4F RT 4A25 2002121800107 20021218 00107 NM 2002 12 18 DL757021407 1 20021204 A 5270 140N27661 BRACKET BOEING 757 757232 1384965 NM GIRT BAR OUT OF POSITION A DALA O OTHER L NO TEST TX TAXI/GRND HDL 1 SO 27 616DL 22823 1R SLIDE INDICATOR LIGHT INOPERATIVE. FOUND 1R DOOR FORWARD GIRT BAR VISUAL INDICATOR ARMING BRACKET CAME OFF. REINSTA LLED FWD VISUAL INDICATOR ARMING BRACKET AND REATTACHED BUSTLE. DOOR NOW ARMS NORMALLY. 2 L 7 2 4F RT A2NM 2002121800108 20021218 00108 NM 2002 12 18 DL757021414 1 20021204 A 2497 MS2721233 WIRE BOEING 757 757232 1384965 NM ELECTRICAL SYS BURNED A DALA K NONE G MULTIPLE FAILURE AP APPROACH 1 SO 27 606DL 22813 IN FLT, R FWD AND L AFT FUEL PUMP C/B'S POPPED AND LOST NR 1 ATC XPONDER, GPS, L EICAS COMP, ASA, CAPT INST XFER, WX RAD AR. T/S FOUND BURNT WIRE ON TB5012 BEHIND P6-3 PANEL. REPLACED TB5012 AND RETERMINATED WIRES. CHECKED BOOST PUMPS, AT C, TCAS, L EICAS COMP AND WX RADAR ON GROUND POWER AND ON L ENG GEN ALL IND NORMAL. 2 L 7 2 4F RT A2NM 2002121800109 20021218 00109 WP 2002 12 18 IXXA0200125S 1 20020826 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, TWO CRACKS WERE DECTECTED ON THE FUSELAGE SKIN AT STATION 490 ON THE LOWER AFT CORNER OF THE FORWARD ENTRY DOOR CUT OUT. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOULB ER AND TRIPLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING AUTHORIZATION R12-R03 2 L 7 4 4F RT 4A25 2002121800110 20021218 00110 NM 2002 12 18 DL757021419 1 20021206 A 2530 831610401 OVEN BOEING 757 757232 1384965 NM GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 660DL 24422 ON LAYOVER FOUND MID GALLEY AFT RT OVEN PRODUCING SMOKE AND HEAT FROM THE CONTROLLER AREA. PULLED CIRCUIT BREAKER. REP LACED OVEN AND RT CAVITY CIRCUIT BREAKER. 2 L 7 2 4F RT A2NM 2002121800111 20021218 00111 NM 2002 12 18 DL757021423 1 20021206 A 5310 143N831215 DOOR FRAME BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 CORROSION REPAIR, THE INNER CHORD OF THE FS 729 FRAME OF THE L2 DOOR OPENING WAS FOUND WITH CORROSION ON THE INBD FLANGE AT WL 212. THE CORROSION WAS REMOVED WITH A TRIMOUT TO THE FLANGE. THE TRIMOUT WAS REPAIRED WITH A REPAIR ANGLE PER T HE B757 SRM AND ER/A 384167-14. 2 L 7 2 4F RT A2NM 2002121800112 20021218 00112 NM 2002 12 18 DL757021442 1 20021213 A 5310 143N85121 DOOR FRAME BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 CORROSION REPAIR, THE OUTER CHORD OF THE C1 DOOR CUTOUT LOWER SILL BEAM WAS FOUND CORRODED AND REQUIRED REPLACEMENT. TO FACILITATE THE REPLACEMENT, THE FS 620 FRAME WEB AND OUTER CHORD WERE CUT BETWEEN STRINGERS 25R-26R AND THE LOWER PORTI ONS REMOVED. THE SILL CHORD WAS REPLACED, AND THE FRAME WEB AND CHORD SPLICED BACK IN PLACE WITH REPAIR DOUBLERS AND AN GLES PER ER/A 384163-14, REV A. 2 L 7 2 4F RT A2NM 2003021000018 20030210 00018 NM 2003 2 10 DHL2002741022 1 20021218 A 2611 302842 SMOKE DETECTOR BOEING 727 7272Q9 138448M NM FAILED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 741DH 21931 1) NR 5 SMOKE DETECTOR DOES NOT TEST. (NO LIGHT) REPLACED NR 5 SMOKE DETECTOR IAW B-M/M 26-17-000. OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 2002121800113 20021218 00113 NM 2002 12 18 DL75A021141 1 20020926 A 2120 ODOR BOEING 757 757212 1384951 NM CABIN DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 757AT 23127 ON CRUISE F/A SMELT ODOR SIMILAR TO BURNT POPCORN NEAR ROW 33. ENG A/I WAS ON. SMELL DISSIPATED AFTER A/I AND LIGHTS W ERE TURNED OFF. OPERATED PACKS BOTH INDEPENDENTLY AND TOGETHER IN FULL HOT POSITION. ALSO RAN BOTH ENG USING INDIVIDUA L ENGS ANTI ICE NO BURNT ODOR SCENTED. 2 L 7 2 4F RT A2NM 2002121800114 20021218 00114 NE 2002 12 18 DL764021047 2 20020907 A 7310 1997M36P01 FUEL LINE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2B7 NE NR 2 ENGINE LEAKING A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 836MH 29709 706225 NR 2 ENG FUEL JUMPER LINE LEAKING REF IPC 73-11-06-11 ITEM 85. REMOVED AND REPLACED LEAKING FUEL HOSE ON RT ENG, PERFOR MED LEAK TESTS NR 2 AND 3 PER PFHB 1-0-7-7 NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A1NM E13NE 2002121800115 20021218 00115 WP 2002 12 18 IXXA0200126S 1 20020826 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FUSELAGE STATION 1660 LONGERON 11L UPPER AFT CORNER ON TH E AFT ENTRY DOOR CUTOUT. REPAIR ACCOMPLISHED, REMOVED DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER, DOUBLER AN D TRIPLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2002121800116 20021218 00116 WP 2002 12 18 IXXA0200127S 1 20020827 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE SKIN DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A DENT WAS DISCOVERED UNDER AN EXISTING REPAIR ON THE CENTER SECTION OF THE LOWER FOR WARD CARGO COMPARTMENT FUSELAGE STATION 335. REPAIR ACCOMPLISHED, REMOVAL OF PREVIOUS REPAIR, REMOVAL OF DAMAGE, FABRICA TION AND INSTALLATION OF REPAIR ANGLE IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING AUTHORIZAT ION R12-R04. 2 L 7 4 4F RT 4A25 2002121800117 20021218 00117 NM 2002 12 18 DL764021070 1 20020912 A 2752 256T63102 ACTUATOR BOEING 767 767432ER 1385134 NM T/E FLAP TRIPPED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 839MH 29712 T/E FLAP DISAGREE AFTER T/O RAISED WITH ALT SYSTEM. DUE TO SHORT RUNWAY IN OGG DIVERTED TO HNL. T/S PER FIM, FOUND NR 6 T/E FLAP ROTARY ACT TRIPPED. RESET SAME. CYCLED FLAPS NO OTHER FAULTS. 2 L 7 2 4F RT A1NM 2002121800118 20021218 00118 WP 2002 12 18 IXXA0200128S 1 20020827 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED UNDER AND EXISTING REPAIR DOUBLER AFT OF THE C-1 DOOR LONGERON 36, FS 333 TO FS 450. REPAIR ACCOMPLISHED, REMOVAL OF REPAIR DOUBLER, CORROSION AND SKIN PANEL, FABRICATION AND INSTAL LATION OF NEW SKIN PANEL IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING DRAWING 5755271. 2 L 7 4 4F RT 4A25 2002121800119 20021218 00119 WP 2002 12 18 2002F01095 1 20020603 A 5320 3546956U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 961R 84102 46133 FOUND DURING DOUGLAS D-CHECK INSPECTION, LONGERON 24L SURFACE CORROSION ON BOTH SIDES OF BATHTUB FITTING STATION 940 AT LONGERON ATTACH. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED AND REPLACED BATHTUB FITTING STATION 940 IAW DC-8 SR M 51-1-24, 51-3-0. (M) 2 L 7 4 4F RT 4A25 2002121800120 20021218 00120 SW 2002 12 18 2002F01096 1 20020709 A 2910 D357 VALVE GULSTM G73 G73 3951802 SW HYD SYSTEM LEAKING A FVYA O OTHER K FLUID LOSS TO TAKEOFF 1 SO 17 142PA J42 ON TAKEOFF FROM BIMINI, HYDRAULIC FLUID WAS SEEPING OUT OF THE INERTIAL DOOR SEPARATOR HANDLES. THE FIRST OFFICER WHO W AS IN COMMAND WAS SPRAYED WITH HYDRAULIC FLUID AND PASSED THE AIRCRAFT OVER TO THE CAPTAIN. AN ATTEMPT WAS MADE TO ISOL ATE THE HYDRAULIC SYSTEM TO NO AVAIL. FLIGHT CONTINUED INTO FLL AS THE LEAKAGE WAS MINIMAL AND HYDRAULIC PRESSURE REMAI NED AT NORMAL WITH NO INDICATION OF HYDRAULIC QUANTITY PROBLEMS. LANDING WAS UNEVENTFUL AND PASSENGER AND CREW GOT OFF THE AIRPLANE SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 2 INERTIAL SEPARATOR VALVE AND SERVICED HYDRAULIC SYSTEM. OPERATIONAL CHECK ACCOMPLISHED WITH NO LEAKS NOTED. (M) 1 H 7 2 3R A783 2002121800121 20021218 00121 WP 2002 12 18 2002F01097 1 20020607 A 3260 WARNING LIGHT DOUG DC8 DC863 302198A WP COCKPIT ILLUMINATED A T64R O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 03 950R 45903 RED 'GEAR NOT LATCHED' LIGHT ON FORWARD INSTRUMENT PANEL ILLUMINATED. ABNORMAL PROCEDURE COMPLETED. (M) 2 L 7 4 4F 4A25 2002121800122 20021218 00122 WP 2002 12 18 2002F01098 1 20020607 A 5320 3647117U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 961R 46133 FOUND DURING DOUGLAS D-CHECK INSPECTION, RIGHT LONGERON AND BATHTUB FITTING STATION 960 AFT SIDE HAS SPOT OF SURFACE COR ROSION. REMOVED CORROSION FROM LONGERON 24R AND BATHTUB FITTING IAW DC-8 SRM 51-1-8. LONGERON 24 REPAIRED. REMOVED AN D REPLACED BATHTUB FITTING IAW DC-8 SRM 53-2-0, FIG 8 51-3-0. (M) 2 L 7 4 4F RT 4A25 2002121800123 20021218 00123 WP 2002 12 18 2002F01099 1 20020610 A 3297 WIRE DOUG DC8 DC863 302198A WP UPLOCK SWITCH DAMAGED A T64R K NONE N FALSE WARNING IN INSP/MAINT 1 SO 03 950R 45903 RED ' GEAR NOT LATCHED' LIGHT ON FORWARD INSTRUMENT PANEL ILLUMINATED. ABNORMAL PROCEDURE COMPLETED. REPAIRED WIRE BY REPINNING ON LEFT UPLATCH SWITCH CONNECTOR IAW DC-8 MM 20-50-1. ACCOMPLISHED NORMAL UPLATCH CHECK AND EMERGENCY EXTENSI ON. OPS CHECKS GOOD IAW DC-8 MM 32-30-0. (M) 2 L 7 4 4F 4A25 2002121800124 20021218 00124 WP 2002 12 18 2002F01100 1 20020611 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 961R 46133 FOUND DURING DOUGLAS D-CHECK INSPECTION, REPAIR AT STATION 55 LEFT LONGERON 31 HAS NO SUPPORTING DOCUMENTATION. REMOVED DOUBLER IAW DC-8 SRM 51-1-21. CRACK HAD EXTENDED .5 BEYOND STOP DRILL. STOP DRILLED CRACK IAW DC-8 SRM 53-2-0. FABRI CATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED REPAIR PER EO NR 02-039 WITH APPROVED 8110-3, DATED 05/31/02. (M) 2 L 7 4 4F RT 4A25 2002121800125 20021218 00125 WP 2002 12 18 2002F01101 1 20020611 A 5711 SPAR CAP DOUG DC8 DC873F 302199F WP RT WING CRACKED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 961R 46133 FOUND DURING DOUGLAS D-CHECK INSPECTION, RIGHT WING LOWER FRONT SPAR CAP FORWARD TANG APPROXIMATELY STATION 520 SPAR CAP HAS CRACK. REMOVED INTERNAL REPAIR ANGLE FOR EVALUATION IAW DC-8 SRM 51-1-20D. REPAIR IS ACCEPTABLE AS TEMP REPAIR PE R BOEING LETTER TEK-02-000727H DATED 28 MAY 02. TREATED, PRIMED AND RE-INSTALLED REPAIR ANGLE IAW DC-8 SRM 51-1-20D WIT H APPROVED 8110-3 FROM DOUG COP DATED 5/28/02. (M) 2 L 7 4 4F RT 4A25 2002121800126 20021218 00126 WP 2002 12 18 2002F01102 1 20020611 A 5753 WEB DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 961R 46133 FOUND DURING DOUGLAS D-CHECK INSPECTION, RIGHT INBOARD FLAP INBOARD WEB HAS PREVIOUS REPAIR CRACK EXTENDS TO NEW STOP DR ILL AT END OF CRACK BEYOND REPAIR DOUBLER. STOP DRILLED END OF CRACK IAW DC-8 SRM 57-2-0. FABRICATED DOUBLER IAW DC-8 SRM 57-2-0, FIG 2. TREATED, PRIMED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-8, 51-1-21 AND 51-3-0. (M) 2 L 7 4 4F RT 4A25 2002121800127 20021218 00127 WP 2002 12 18 2002F01103 1 20020605 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 961R 46133 FOUND DURING DOUGLAS D-CHECK INSPECTION, REPAIR AT STATION 300 RIGHT LONGERON 33 HAS NO SUPPORT DOCUMENTATION. REMOVED DOUBLER IAW DC-8 SRM 51-1-21. IT IS ACCEPTABLE TO USE EXISTING FILLER. FABRICATED NEW DOUBLER. TREATED AND PRIMED ALL PARTS AND INSTALLED REPAIR PER EO NR 02-039, WITH APPROVED 8110-3 DATED 05/31/02. (M) 2 L 7 4 4F RT 4A25 2002121800128 20021218 00128 WP 2002 12 18 2002F01105 1 20020604 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 961R 46133 FOUND DURING DOUGLAS D-CHECK INSPECTION, STATION 460 HAS CORROSION ON FRAME BETWEEN STRINGERS 2/3 LEFT. REMOVED CORROSI ON. FOUND OUT OF LIMITS. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4, 53-2-0 AND 53-2-0, FIG 1F. (M) 2 L 7 4 4F RT 4A25 2002121800129 20021218 00129 CE 2002 12 18 2002F01106 1 20020626 A 3240 CYLINDER CESSNA 310 310R 2074245 CE MLG BRAKE FAILED A FSEA O OTHER O OTHER TX TAXI/GRND HDL 1 NE 05 87508 310R0597 CYLINDER FAILED, RESULTING IN NO BRAKING ON RIGHT SIDE OF AIRCRAFT. PILOT FAILED TO MAINTAIN CONTROL OF AIRCRAFT, AIRCR AFT WENT BEYOND PAVED AREA OFF TAXI WAY ON TO GRASS AREA. NO DAMAGE WAS DONE TO THE AIRCRAFT. WHEN PILOT REALIZED THAT BRAKES WERE NOT WORKING, BOTH ENGINES WERE SHUTDOWN AND AIRCRAFT WAS TOWED TO MAINTENANCE. (M) 1 L 7 2 3O 3A10 2002121800130 20021218 00130 NM 2002 12 18 2002F01107 1 20020601 A 5311 FRAME BOEING 747 747341 13848AM NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 DURING CURRENT D-CHECK AT SIAEC, FOUND STATION 440L FRAME CRACKED AT CUT OUT OF STRINGER 10A. CRACK LENGTH .1875. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLRS AND INSTALLED PER SRM 53-10-20 AND 53-10-04. FRAME IS SUBJECT TO RECURRENT IN SPECTIONS PER SB 747-53A2265 AT 3000 CYCLES. (M) 2 L 7 4 4F RT A20WE 2002121800131 20021218 00131 NM 2002 12 18 2002F01108 1 20020629 A 3260 8125403 CIRCUIT CARD DHAV DHC8 DHC8103 1386005 NM COCKPIT FAULTY A KPVA O OTHER N FALSE WARNING TO TAKEOFF 1 WP 13 806WP 357 WEIGHT ON WHEELS CAUTION LIGHT CAME ON 3 TIMES ON TAKEOFF. REMOVED AND REPLACED CAUTION LIGHT PANEL CIRCUIT CARD NR 2. OPS CHECK IAW DASH 8 MM 33-12-01 PAGE 201. RELEASED FOR TEST FLIGHT. POST MAINTENANCE TEST FLIGHT SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 2002121800132 20021218 00132 NM 2002 12 18 2002F01109 1 20020130 A 2920 B-NUT BOEING 727 727224 1384076 NM HYD SYSTEM LOOSE A FX7A O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 296CS DURING FLIGHT BOTH SYSTEM 'B' PUMPS LOW PRESSURE LIGHTS ILLUMINATE. NO PRESSURE AT ALL ON 'B' SYSTEM, ZERO PRESSURE ON THE SYSTEM. FOUND 'B' NUT OF HYDRAULIC PRESSURE LINE 'B' PUMP NR 2 SYSTEM LOOSE TIGHTENED B-NUT AND SERVICE IAW MM 12-1 2-0. OPS CHECK ALL FLIGHT CONTROL NORMAL. NO LEAKS FOUND IAW MM 27-00 AND MM 29-12-0. (M) 2 L 7 3 4F A3WE 2002121800133 20021218 00133 EU 2002 12 18 2002F01110 1 20020202 A 2613 1734362450 WARNING SYSTEM SAAB SF340 340B 7860101 EU COCKPIT ACTIVATED A CX7A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 03 308CE 340B210 TAIL PIPE HOT CAME ON AFTER TAKEOFF. TAIL PIPE HOT SENSOR AIR RETURN. (M) 2 L 7 2 4T RT A52EU 2002121800134 20021218 00134 EU 2002 12 18 2002F01111 1 20020131 A 2613 1734362450 WARNING SYSTEM SAAB SF340 340B 7860101 EU COCKPIT ACTIVATED A CX7A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 03 311CE 340B214 TAIL PIPE HOT CAME ON AFTER TAKEOFF, AIR RETURN. TAIL PIPE HOT SENSOR. (M) 2 L 7 2 4T RT A52EU 2002121800135 20021218 00135 NM 2002 12 18 SPAA0200062 1 20021215 A 5311 UNK FRAME BOEING 737 7372T4 1384492 NM A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 Corrosion on frame at BS1006, Stringer 25L. Beltframe at Sta 1006 repaired I.A.W. Boeing SRM 53-10-4, Fig 1-4. 2 L 7 2 4F A16WE 2002121800136 20021218 00136 NM 2002 12 18 ZW0A0212401 1 20021216 A 5220 80330034 CYLINDER BOEING 757 7572Q8 1384972 NM A ZW0A O OTHER K FLUID LOSS IN INSP/MAINT 1 CE 13 712TW 27624 THE LEFT SIDE NUMBER 2 CABIN DOOR, THE ASSIST BOTTLE PRESSURE WAS LOW. REPLACED THE CYLINDER. CHECK-C 12-10-02 MCI. - -CLOSED-- 2 L 7 2 4F RT A2NM 2002121800137 20021218 00137 NM 2002 12 18 SPAA0200063 1 20021215 A 5311 UNK FRAME BOEING 737 7372T4 1384492 NM CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 Corrosion on frame at BS1006, Stringer 20R. Repaired frame at Sta 1006 per Boeing SRM 53-10-4, Fig 1, Sheets 1 of 4. 2 L 7 2 4F A16WE 2002121800138 20021218 00138 EU 2002 12 18 2002F01112 1 20020130 A 2613 1734362450 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT ILLUMINATED A CX7A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 03 303CE 340B194 ON TAKEOFF ROLL AS TORQUE WAS PASSING 60 DEGREES AND TAIL PIPE HOT LIGHT ILLUMINATED. ABORTED TAKEOFF LIGHT EXTINGUISHE D ABOUT 1 MINUTE LATER. (M) 2 L 7 2 4T RT A52EU 2002121800139 20021218 00139 WP 2002 12 18 IXXA0200129S 1 20020827 A 5313 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE SKIN INADEQUATE A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A TEMPORARY REPAIR AT FUSELAGE STATION 45 LONGERON 29L WAS DETECTED. REPAIR ACCOMPLIS HED, REMOVAL OF TEMPORARY REPAIR, DAMAGE. FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2002121800140 20021218 00140 WP 2002 12 18 IXXA0200130S 1 20020828 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LOWER FORWARD CARGO COMPARTMENT FRAME CLOSE TO AFT DOOR CUT OUT OF FUSELAGE STATION 520 LONGERON 27R. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED FRAME SECTION, FABRICATION AND IN STALLATION OF REPAIR FILLER AND REPAIR CHANNELS IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2002121800141 20021218 00141 WP 2002 12 18 IXXA0200131S 1 20020828 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE INADEQUATE A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A TEMPORARY REPAIR WAS DISCOVERED ON THE LOWER FORWARD CARGO COMPARTMENT FORWARD DOOR CUT OUT FORWARD SIDE AT FS 280 STRINGER 36. REPAIR ACCOMPLISHED, REMOVAL OF THE TEMPORARY REPAIR, FABRICATION AND INSTA LLATION OF REPAIR FILLER AND DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2002121800142 20021218 00142 NM 2002 12 18 SPAA0200061 1 20021215 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM FUSELAGE CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 CORROSION ON FLOORBEAM TOP FLANGE AT STA. 1016, LBL 6 TO RBL 5. BEYOND SRM LIMITS. REPAIRED FLOOR BEAM TOP FLANGE PER SR M 53-10-9, FIG 1 PGAS 1-9 2 L 7 2 4F A16WE 2002121800143 20021218 00143 NM 2002 12 18 F3LA200200390 1 20021203 A 5320 INTERCOSTAL BOEING 737 73736Q 1384409 NM STA. 747-767 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 305FA 3492 28662 DURING C-6 CHECK, INSPECTION REPORTED INTERCOSTAL AT STR. 26-R BETWEEN STA.747-767 CORRODED. FABRICATED AND INSTALLED R EPLACEMENT INTERCOSTAL PER DRAWING 69-16500, ITEM 4, AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2002121800144 20021218 00144 NM 2002 12 18 SPAA0200064 1 20021215 A 5320 FLOOR SUPPORT BOEING 737 7372T4 1384492 NM FUSELAGE CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 CORROSION ON FLOORBOARD SUPPORT AT BS 986 TO BS1006, BL 0. REPLACED FLOORBOARD SUPPORT PER SRM 53-40-4, FIG 1 PGS 1-7. 2 L 7 2 4F A16WE 2002121800145 20021218 00145 WP 2002 12 18 GTIA021153A 1 20020919 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 SW 15 805NK 48058 FTW - FOUND AFT CABIN STATION 1309 CORROSION ON BEAM ATTACH FITTING RBL 60. REMOVED ATTACH FITTING. UPON REMOVAL OF AT TACH FITTING FOUND CORROSION ON WEB. REMOVED CORRODED WEB. LOCATED, DRILLED AND DEBURRED REPAIR WEB. INSTALLED REPAIR WEB. LOCATED, DRILLED AND DEBURRED ATTACH FITTING. INSTALLED ATTACH FITTING. 2 L 7 2 4F A6WE 2002121800146 20021218 00146 WP 2002 12 18 GTIA021211A 1 20021023 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED G GTIA K NONE O OTHER IN INSP/MAINT 1 SW 15 802NK 53168 FTW - FOUND AFT ACC AREA FRAME T-CAP AT AFT SHROUD OF APU HAS CORROSION AT STATION 1401, 27L-27R. INTERCOSTAL AT FS 138 0 TO 1401 LBL 13 IS FOUND TO BE OUT OF LIMITS. FABRICATED NEW INTERCOSTAL. FRAME AT 1394 IS CRACKED. FABRICATED NEW F RAME. REMOVED LOWER T-CAP. LOCATED AND DRILLED NEW LOWER T-CAP. FOUND CRACK ON RT LEG OF VERTICAL BEAM. REMOVED VERTI CAL BEAM. LOCATED AND DRILLED NEW RT VERTICAL BEAM. INSTALLED T-CAP. INSTALLED VERTICAL BEAM. INSTALLED RT INTERCOST AL. 2 L 7 2 4F RT A6WE 2002121800147 20021218 00147 WP 2002 12 18 GTIA021211B 1 20021023 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED G GTIA K NONE O OTHER IN INSP/MAINT 1 SW 15 802NK 53168 FTW - FOUND AFT ACC AREA FRAME T-CAP AT AFT SHROUD OF APU HAS CORROSION AT STATION 1401, 27L-27R. INTERCOSTAL AT FS 138 0 TO 1401 LBL 13 IS FOUND TO BE OUT OF LIMITS. FABRICATED NEW INTERCOSTAL. FRAME AT 1394 RBL 13 IS CRACKED. FABRICATE D NEW FRAME. REMOVED LOWER T-CAP. LOCATED AND DRILLED NEW LOWER T-CAP. FOUND CRACK ON RT LEG OF VERTICAL BEAM. REMOVE D VERTICAL BEAM. LOCATED AND DRILLED NEW RT VERTICAL BEAM. INSTALLED T-CAP. INSTALLED VERTICAL BEAM. INSTALLED RT IN TERCOSTAL. 2 L 7 2 4F RT A6WE 2002121800148 20021218 00148 NM 2002 12 18 C1HA2002009 1 20021101 A 5310 SHEAR TIE BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 CORROSION ON FRAME TO SKIN TIE AT STA 720A BETWEEN STR 28R - 27R FWD SIDE OF FRAME. 2 L 7 3 4F RT A3WE 2002121800149 20021218 00149 NM 2002 12 18 C1HA2002011 1 20021102 A 5320 SUPPORT BRACKET BOEING 727 727270 138408P NM FUSELAGE CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 FWD PIT SUPPORT BRACKET CRACKED FS 520 AND DEFORMED AT FS 540 S23L. 2 L 7 3 4F RT A3WE 2003062500063 20030625 00063 NM 2003 6 25 SPAA0200065 1 20021215 A 5320 65468185187 FLOOR SUPPORT BOEING 737 7372T4 1384492 NM FUSELAGE CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 CORROSION ON FLOORBOARD SUPPORT AT LAV DOOR, BS 990 TO BS 1016, LBL 6 TO LBL 19. REPLACED FLOORBOARD SUPPORTS PER SRM 5 1-10-1 AND 51-30-1, P/N 65-46812-185 AND 65-46812-187. 2 L 7 2 4F A16WE 2002121800150 20021218 00150 NM 2002 12 18 AWXA200201211 1 20021111 A 5320 146N853017 BEAR STRAP BOEING 757 757225 1384959 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 0 0 22207 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT LOWER CORNER OF THE AFT CARGO DOOR BODY SK IN CUTOUT (BEAR STRAP) BS 1440, STR 26 R/H. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; PERFORM ED HFEC INSPECTION AND DISCOVERED A 1 1/4" CRACK ON INNER SKIN BS 1440, STR 26 R/H; STOPPED DRILLED CRACK AND PERFORMED ANOTHER HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED. REMOVED NUT PLATE STRIP, INTERCOSTALS, AND LOWER SEAL RETAINE R TO GAIN ACCESS FOR REPAIR; OPENED UP SKIN SECTION BS 1380 TO BS 1460 AND TRIMMED OUT A 3" RADIUS OF CORRODED & CRACKED AREA OF BEAR STRAP; FABRICATED 2 EACH FILLERS, A DOUBLER, AND A TRIPLER; INSTALLED REPAIR PARTS AND REMOVED PARTS IAW A 2 L 7 2 4F RT A2NM 2002121800151 20021218 00151 NM 2002 12 18 AWXA200201219 1 20021119 A 5313 140N1530 STRINGER BOEING 757 757225 1384959 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 0 0 22207 LCQ - MAJOR REPAIR - DURING C-09 CHECK CORROSION WAS FOUND ON STRINGER 29 L/H, AT BS 1680. MAINTENANCE CUTOUT 4" SECTION OF CORRODED STRINGER AND FOUND CORROSION ON SKIN; CLEANED CORROSION OFF SKIN AND FOUND MATERIAL LOSS OUT OF LIMITS; CUT OUT CORRODED SECTION OF AIRCRAFT SKIN; PERFORMED HFEC INSPECTION OF SKIN AND STRINGER CUTOUTS TO VERIFY NO CRACKS EXIST; FABRICATED A NEW SECTION OF STRINGER, AND A STRINGER SPLICE IAW B757-200 SRM 53-00-03, PG. 201. FABRICATED A REPAIR DOU BLER FOR SKIN CUTOUT; INSTALLED REPAIR PARTS IAW AWA E.R. 19-5361-02345-SS2. 2 L 7 2 4F RT A2NM 2002121800152 20021218 00152 NM 2002 12 18 AWXA200201220 1 20021119 A 5320 140N1530 STRINGER BOEING 757 757225 1384959 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 0 0 22207 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT STRINGER AT BS 1290, S TR 28 L/H. MAINTENANCE CUTOUT CORROSION DAMAGE ON STRINGER 28 L/H AT BS 1290; FABRICATED A NEW SECTION OF STRINGER, AND STRINGER SPLICE ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-03, PG. 201 2 L 7 2 4F RT A2NM 2002121800153 20021218 00153 NM 2002 12 18 AWXA200201221 1 20021122 A 5311 146N1019 FRAME BOEING 757 757225 1384959 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 0 0 22207 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION AND A DENT WERE FOUND ON TOP FLANGE OF FRAME IN THE AFT CAR GO COMPARTMENT AT BS 1560, LBL 9. MAINTENANCE CUTOUT CORRODED SECTION OF FRAME AT BS 1560, LBL 9; FABRICATED 2 EACH CHAN NELS AND A FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-07, PG. 201-203. 2 L 7 2 4F RT A2NM 2002121800154 20021218 00154 NM 2002 12 18 AWXA200201222 1 20021122 A 5311 146N102 FRAME BOEING 757 757225 1384959 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 0 0 22207 LCQ - MAJOR REPAIR - DURING C-09 CHECK A 1 1/4" CRACK WAS FOUND ON AFT CARGO COMPARTMENT FRAME AT BS 1420, BETWEEN STRIN GERS 26 L/H AND 27 L/H. MAINTENANCE CUTOUT DAMAGED SECTION OF FRAME AT BS 1420, BETWEEN STRINGERS 26 L/H AND 27 L/H; FAB RICATED 2 EACH CHANNELS; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-07, PG. 202. 2 L 7 2 4F RT A2NM 2002121800155 20021218 00155 NM 2002 12 18 AWXA200201223 1 20021122 A 5311 146N1011 FRAME BOEING 757 757225 1384959 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 0 0 22207 LCQ - MAJOR REPAIR - DURING C-09 CHECK A 3/4" CRACK WAS FOUND ON AFT CARGO COMPARTMENT FRAME AT BS 1400, BETWEEN STRINGE RS 25 L/H AND 26 L/H. MAINTENANCE CUTOUT DAMAGED SECTION OF FRAME AT BS 1400, BETWEEN STRINGERS 24 L/H AND 27 L/H; FABRI CATED 2 EACH CHANNELS; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-07, PG. 202. 2 L 7 2 4F RT A2NM 2003062500064 20030625 00064 NM 2003 6 25 SPAA0200066 1 20021215 A 5320 FLOOR PANEL BOEING 737 7372T4 1384492 NM FUSELAGE CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 CORROSION ON UNDERSIDE OF FLOOR SKIN AT SINK FITTINGS FS 1000 LBL 45. REPAIRED FLOOR PER SRM 51-402 FIGURE 1. 2 L 7 2 4F A16WE 2002121800156 20021218 00156 NM 2002 12 18 C1HA2002018 1 20021105 A 5320 INTERCOSTAL BOEING 727 727270 138408P NM FUSELAGE CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 CRACKED INTERCOSTAL BS 1050 STR 26R AFT PIT. 2 L 7 3 4F RT A3WE 2003011700106 20030117 00106 NM 2003 1 17 F3LA200200391 1 20021203 A 5320 ANGLE BOEING 737 73736N 1384408 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 306FL 3392 28563 DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON L-ANGLE IN FWD CARGO COMPARTMENT, STA 500D, LBL 29 TO RBL 21. REPAIR ED ANGLE PER SRM 51-40-02, 51-40-05 AND 51-10-02. 2 L 7 2 4F RT A16WE 2002121800157 20021218 00157 NM 2002 12 18 C1HA2002019 1 20021105 A 5311 FRAME BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 CORROSION ON FRAME AFT SIDE LOWER CORD AT STA 1166 STR 20 - 21R AFT PIT. 2 L 7 3 4F RT A3WE 2002121800158 20021218 00158 NM 2002 12 18 C1HA2002020 1 20021105 A 5310 SHEAR TIE BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 CORRODED SHEAR TIE BS 950F STR 29R. 2 L 7 3 4F RT A3WE 2002121800159 20021218 00159 NM 2002 12 18 C1HA2002010 1 20021102 A 5320 FLOOR SUPPORT BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 CORROSION ON FLOOR SUPPORT AT BS 715, LBL 3 WL 160 BOTTOM SIDE. 2 L 7 3 4F RT A3WE 2002121800160 20021218 00160 NM 2002 12 18 C1HA2002012 1 20021102 A 5320 SPLICE BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 CORROSION EMANATING FROM SPLICE AT BS480 RBL3 WL 160, FLOOR TRACK TO BULKHEAD SUPPORT BRACKET. 2 L 7 3 4F RT A3WE 2002121800161 20021218 00161 NM 2002 12 18 C1HA2002013 1 20021103 A 5311 FRAME BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 STA 1050 I/B FLANGE OF FRAME BETWEEN S22L AND 21L HAS CORROSION. 2 L 7 3 4F RT A3WE 2002121800162 20021218 00162 NM 2002 12 18 C1HA2002014 1 20021102 A 5320 ANGLE BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 AFT PIT, CORROSION AT STA 970 S28R AT ANGLE. 2 L 7 3 4F RT A3WE 2002121800163 20021218 00163 NM 2002 12 18 C1HA2002015 1 20021102 A 5310 SHEAR TIE BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 CORROSION ON SHEAR TIE IN AFT PIT STA 950 BL 0. 2 L 7 3 4F RT A3WE 2002121800164 20021218 00164 NM 2002 12 18 C1HA2002016 1 20021104 A 5320 WEB BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 STRINGER 25R STA 333 UNDER RT DOGHOUSE WALKWAY WEB CORRODED. 2 L 7 3 4F RT A3WE 2002121800165 20021218 00165 NM 2002 12 18 C1HA2002021 1 20021106 A 5320 STIFFENER BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 CORROSION ON TOP DOGHOUSE STIFFENER MARKED C8 STA 315 BL 0. 2 L 7 3 4F RT A3WE 2002121800166 20021218 00166 EU 2002 12 18 QXEA0202193 1 20021215 A 2930 A71911437 LINE FOKKER F28 F28MK4000 4990810 EU ZONE 600 FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 492US 11159 SEA ON FLIGHT 2409- UTILITY SYSTEM HYDRAULIC QUANTITY DROPPED BELOW YELLOW ARC IN FLIGHT. COMPLETED APPLICABLE CHECKLIS T. UPON GEAR EXTENSION, GEAR DOOR DID NOT RETRACT AND UTILITY SYSTEM PRESSURE DROPPED TO 200 PSI AFTER GEAR AND FLAPS WE RE SELECTED. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND HYDRAULIC LINE IN NO.2 STUB WING LEAKING. REMOVED AND REPLACED HYDR AULIC LINE. OPERATIOANL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2003011700108 20030117 00108 NM 2003 1 17 F3LA200200392 1 20021205 A 5320 WEB BOEING 737 73736N 1384408 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 306FL 3392 28563 DURING C-6 CHECK, INSPECTION REPORTED WEB BETWEEN STA 794.3 AND 847, STR 25-R, CORRODED AROUND SEVERAL NUT PLATE HOLES. REPLACED AND INSTALLED WEB PER SRM 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A16WE 2002121800167 20021218 00167 NM 2002 12 18 F3LA200200393 1 20021205 A 5320 STRAP BOEING 737 73736N 1384408 NM STA. 774 - 858 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 306FL 3392 28563 DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR LOWER SILL STRAP, STA. 774 TO 858, RBL 20. REPLACED S ILL STRAP PER SRM 51-40-07 AND 51-10-02. 2 L 7 2 4F RT A16WE 2002121800168 20021218 00168 NM 2002 12 18 C1HA2002022 1 20021106 A 5320 SUPPORT BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 UPPER SUPPORT CORD FOR LT SIDE OF DOG HOUSE EXFOLIATED AT APPROX STA 312, CHORD IS MOUNTED AT THE FLOOR WEB. 2 L 7 3 4F RT A3WE 2002121800169 20021218 00169 NM 2002 12 18 C1HA2002023 1 20021107 A 5313 STRINGER BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 CORROSION ON STRINGER 27R BETWEEN STA 360 AND STA 380. 2 L 7 3 4F RT A3WE 2003011700109 20030117 00109 NM 2003 1 17 F3LA200200394 1 20021205 A 5320 STRAP BOEING 737 73736N 1384408 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 306FL 3392 28563 DURING C-6 CHECK, INSPECTION REPORTED FILLER/STRAP CORRODED BETWEEN STA 787 AND 807, RBL 20 ABOVE STR 25-R. REPLACED FI LLER/STRAP PER SRM 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A16WE 2002121800170 20021218 00170 NM 2002 12 18 C1HA2002024 1 20021108 A 5313 STRINGER BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 STR 28R IN THE E&E BAY IS CORRODED BETWEEN STA 420 AND 440 2 L 7 3 4F RT A3WE 2002121800171 20021218 00171 NM 2002 12 18 C1HA2002025 1 20021110 A 5313 STRINGER BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 RT STR 27 CHORD HAS CORROSION AT FRAME ATTACH POINTS FS 312 AND FS 305. 2 L 7 3 4F RT A3WE 2002121800172 20021218 00172 NM 2002 12 18 C1HA2002026 1 20021126 A 5330 SKIN BOEING 727 727270 138408P NM FUSELAGE DAMAGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 FUSELAGE SKIN GOUGED AND PUNCTURED AT STA 1283 RT CENTRAL AREA. 2 L 7 3 4F RT A3WE 2002121800173 20021218 00173 NM 2002 12 18 C1HA2002027 1 20021030 A 5315 FLOORBEAM BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 FS 1110 MAIN CABIN FLOORBEAM IS EXFOLIATED AT LBL 25 ON THE BOTTOM SIDE OF THE UPPER 'T'. 2 L 7 3 4F RT A3WE 2002121800174 20021218 00174 NM 2002 12 18 C1HA2002028 1 20021030 A 5347 SEAT TRACK BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 SEAT TRACK LBL 55 PITTED IN 4 PLACES AND CORRODED IN SEVERAL PLACES ON BOTH TRACK FLANGES, UPPER AND LOWER, FROM FS 1070 TO 1138. 2 L 7 3 4F RT A3WE 2002121800175 20021218 00175 NM 2002 12 18 C1HA2002029 1 20021030 A 5320 SUPPORT ANGLE BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 L-2 SILL DRAIN ATTACHING HARDWARE AND SUPPORT ANGLE 'T' IS CORRODED, TOP AND BOTTOM SIDES OF THE ANGLE. 2 L 7 3 4F RT A3WE 2002121800176 20021218 00176 NM 2002 12 18 C1HA2002030 1 20021030 A 5320 FLOOR SUPPORT BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 LT FLOOR SUPPORT JUST FWD OF FS STA 1070 BETWEEN LBL 45.5 AND LBL 6.3 IS EXFOLIATED IN SEVERAL PLACES. 2 L 7 3 4F RT A3WE 2002121800177 20021218 00177 NM 2002 12 18 C1HA200293009 1 20021004 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 T-CHORD CORRODED AT STA 328 AS VIEWED FROM FUSELAGE INTERIOR ON RT SIDE. 2 L 7 3 4F A3WE 2002121800178 20021218 00178 NM 2002 12 18 F3LA200200395 1 20021203 A 4910 COWL DOOR BOEING 737 73736N 1384408 NM CHAFED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 306FL 3392 28563 DURING C-6 CHECK, INSPECTION REPORTED PREVIOUS REPAIR ON LT. SECTION OF APU COWL DOOR CHAFFED/GROOVED. REMOVED ADDITION AL DAMAGE FOUND AT EDGE OF PREVIOUS REPAIR. FABRICATED NEW DOUBLER TO ENCOMPASS NEW CUTOUT IN SKIN PER SRM 52-40-02, 52 -40-01, MM 51-21-41 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2002121900001 20021219 00001 WP 2002 12 19 IXXA0200133S 1 20020828 A 5330 SKIN DOUG DC8 DC871F 302199D WP DOOR CUTOUT DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A HOLE WAS DISCOVERED IN THE MAIN CARGO DOOR RT AFT LOWER FORWARD CUT OUT AREA. REPA IR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCT URAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2002121900002 20021219 00002 WP 2002 12 19 IXXA0200134S 1 20020911 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, CORRODED DOUBLERS WERE DISCOVERED ON THE FUSELAGE BY STA 340 AND 360 AFT OF THE C-1 D OOR. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLERS AND REPAIR SPLICE DOUBLERS IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING AUTHROIZATION R12-R04. 2 L 7 4 4F RT 4A25 2002121900003 20021219 00003 WP 2002 12 19 IXXA0200139S 1 20020826 A 5310 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 80111 2955 45993 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DISCOVERED ON THE FUSELAGE BY THE LEFT HINGE OF THE RADOME. REPAIR ACCOM PLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER AND DOUBLER, IN ACCORDANCE WITH THE DOUGLAS ST RUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2002121900008 20021219 00008 WP 2002 12 19 MWEA020739 1 20021218 A 5311 995766412 INTERCOSTAL DOUG DC9 DC915 3022036 WP BEAM #5 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FORWARD CARGO DOOR, INTERCOSTAL IS CRACKED BETWEEN BEAM #5 AND UPPER DOOR PAN. -- LOCATED AND DRILLED AND INSTALLED NE W INTERCOSTAL. 2 L 7 2 4F A6WE 2002121900019 20021219 00019 WP 2002 12 19 02FDEA00948 1 20021216 A 3242 BRAKE ASSY DOUG MD10 MD1010F WP GE CF6 CF6* 30020 GL MLG DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 NUMBER 2 BRAKE BINDING. DURING TIRE CHANGE, FOUND FIRST THREE SETS OF ROTORS FROZEN & STUCK. REMOVED OLD DEFECTIVE NR 2 BRAKE AND INSTALLED NEW BRAKE IAW MM. 2 L 7 3 4F 4 F RT A22WE E23EA 2002121900020 20021219 00020 NM 2002 12 19 02FDEA00950 1 20021217 A 5310 SHEAR TIE BOEING 727 727227 1384078 NM PWA JT8 JT8D9 52048 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 CORROSION ON AFT BAY SHEAR TIE AT BS 1010, LBL 9, WL 138. 2 L 7 3 4F 4 F A3WE E2EA 2002121900021 20021219 00021 NM 2002 12 19 02FDEA00951 1 20021217 A 5311 FRAME BOEING 727 727227 1384078 NM PWA JT8 JT8D9 52048 NE FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 FUSELAGE FRAME AT BS 540, HAS NUMEROUS EMPTY HOLES NEAR UPPER FLANGE BETWEEN STR 22 LT AND 26 LT. 2 L 7 3 4F 4 F A3WE E2EA 2002121900022 20021219 00022 NM 2002 12 19 02FDEA00952 1 20021217 A 5310 STRINGER BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 FOUND CRACK IN STR 21 LT AT BS 540. 2 L 7 3 4F RT A3WE 2002121900023 20021219 00023 WP 2002 12 19 02FDEA00953 1 20021217 A 5210 MOTOR DOUG MD10 MD1010F WP GE CF6 CF6* 30020 GL PAX DOOR FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 R1 ENTRY DOOR HARD TO OPEN, MOTOR SOUNDS LIKE IT SPINS, CLUTCH SLIPS. REMOVED AND REPLACED R1 DOOR ELECTRIC MOTOR, SHAF T, BEARINGS, AND PNEUMATIC MOTOR REF MM. 2 L 7 3 4F 4 F RT A22WE E23EA 2002121900024 20021219 00024 WP 2002 12 19 2002F01088 2 20020520 A 7230 3101160 CARBON SEAL SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33111U 01514 WP ENGINE DAMAGED A I7WA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 05 446MA 2715 693 AUA - FLT 7120 - PILOT REPORTED SMOKE IN COCKPIT AGAIN FROM RIGHT BLEED AIR. ENGINE IS USING OIL AND PILOT CAN SEE OIL VAPORS AND SMELL OIL VAPORS, IT IS NOT SMOKE. MAINTENANCE HAS DEFERRED THE RIGHT BLEED AIR DUE TO HIGH OIL CONSUMPTION CAUSING BAD SMELL AND VAPORS. MAINTENANCE ADVISES THAT OIL CONSUMPTION IS STILL WITHIN LIMITS. THE STATUS OF THE ENGIN E IS BEING REEVALUATED. (M) 2 L 7 2 4T 4 T RT A5SW E4WE 2002121900025 20021219 00025 WP 2002 12 19 02FDEA00954 1 20021217 A 5753 CDTT44463 BEARING DOUG MD10 MD1010F WP GE CF6 CF6* 30020 GL TE FLAP CARRIAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 RT WING OUTBOARD FLAP CARRIAGE ASSY HAS 2 SMALL ROLLER BEARINGS WORN. REMOVED AND REPLACED 2 SMALL ROLLER BEARINGS. 2 L 7 3 4F 4 F RT A22WE E23EA 2002121900028 20021219 00028 NM 2002 12 19 QXEA0201810 1 20021024 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - UPPER ATC ANTENNA MOUNT POINT ON UPPER AIRCRAFT FUSELAGE HAS TWO GOUGES AT FORWARD RIGHT HAND CORNER. REPAIRED IA W HORIZON AIR EA 2-51-442. 2 H 7 2 4T RT A13NM 2002121900031 20021219 00031 NM 2002 12 19 QXEA0201825 1 20021031 A 7110 WEB BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 PDX - LEFT HAND LOWER COWL AFT CONE SUPPORT WEB IS CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2002121900032 20021219 00032 NM 2002 12 19 QXEA0201826 1 20021031 A 7110 WEB BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - RIGHT HAND LOWER COWL AFT CONE SUPPORT WEB IS CRACKED. REPAIRED IAW RD 8/4-71-16. 2 H 7 2 4T RT A13NM 2002121900033 20021219 00033 NM 2002 12 19 QXEA0201827 1 20021031 A 7110 SUPPORT BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - RIGHT HAND LOWER COWL BYPASS DOOR INBOARD VERTICAL SUPPORT CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2002121900034 20021219 00034 EU 2002 12 19 QXEA0201831 1 20021031 A 5312 PRESSURE PANEL FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX-DENT IN FORWARD WALL OF NOSE WHEEL WELL IN SECOND CHANNEL AREA 6 INCHES FROM TOP. REPAIRED IAW FSRM 51-31-01 AND 53 -02-01. 2 L 7 2 4F RT A20EU 2003011700110 20030117 00110 NM 2003 1 17 F3LA200200396 1 20021203 A 5247 SUPPORT ANGLE BOEING 737 73736N 1384408 NM APU DOOR GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 306FL 3392 28563 DURING C-6 CHECK, INSPECTION REPORTED SUPPORT ANGLE ON AFT SIDE OF AFT DOOR LATCH CUTOUT GOUGED ON APU DOOR. FABRICATED NEW SUPPORT ANGLE PER SRM 52-40-02 AND 51-70-11. ALODINED AND PRIMED PER MM 51-21-41 AND SOPM 20-41-02. INSTALLED NEW ANGLE PER SRM 52-40-02 AND 51-70-11. 2 L 7 2 4F RT A16WE 2002121900036 20021219 00036 EA 2002 12 19 02352630 1 20021218 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 630BR 7255 During preflight inspection, the crew reported that a cabin ceiling emergency light was inoperative. Repair was initial ly deferred in accordance with the MEL. Later, maintenance personnel removed and replaced the lamp in the cabin ceiling emergency light. An operational check was satisfactory and the aircraft was returned to service. 2 L 7 2 4F RT A21EA 2002121900037 20021219 00037 NM 2002 12 19 QXEA0201832 1 20021021 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - LEFT HAND NACELLE AFT FIREWALL IS CRACKED AT APPROXIMATELY XN125.50, INBOARD SIDE AT SUPPORT BRACKET. REPAIRED IA W DHC-8 RD 8-54-109. 2 H 7 2 4T RT A13NM 2002121900039 20021219 00039 NM 2002 12 19 QXEA0201833 1 20021024 A 5420 SEAL DHAV DHC8 DHC8202 2809007 NM NR 2 NACELLE TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - NR 2 ENGINE PANEL 423AL UPPER SEAL IS TORN. REPAIRED IAW DHC-8 SRM 51-40-00 AND HORIZON AIR EA 2-71-190. 2 H 7 2 4T RT A13NM 2002121900040 20021219 00040 NM 2002 12 19 QXEA0201834 1 20021025 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 11 TOP AND BOTTOM CORROSION IN SEAT ATTACH AREA AT APPROXIMATELY X431.00 TOP AND X438.00 TOP AND BOTTOM. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002121900041 20021219 00041 NM 2002 12 19 QXEA0201835 1 20021104 A 2750 RELAY BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP MALFUNCTIONED A QXEA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 09 403QX 4037 PDX - DURING FLAP EXTENSION TO 15 DEGREES, THE FLAP POWER CAUTION LIGHT ILLUMINATED. FLAPS STOPPED MOVING AT 10 DEGREES . THE CREW PERFORMED THE CHECKLIST AND THE CONDITION REMAINED. THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND RESET THE LATCH RELAY IAW THE FAULT ISOLATION MANUAL 27-50-00-810-004. AN OPERATIONAL CHECK WAS PERFORMED AND CHECKED GOOD. NO PARTS WERE REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002121900043 20021219 00043 NM 2002 12 19 QXEA0201836 1 20021106 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 3 HAS MARRED EDGES AND MISSING PAINT AT STATION X529 AND X514. REPAIRED IAW RD 8 -53-1342 AND DHC 8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002121900044 20021219 00044 NM 2002 12 19 QXEA0201837 1 20021104 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 2 HAS LIGHT PITTING CORROSION AT STATION X453. REPAIRED IAW RD 8-53-1352 AND DHC -8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002121900045 20021219 00045 NM 2002 12 19 QXEA0201838 1 20021103 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - UPPER WING SKIN GOUGED JUST AFT OF PANEL 622AT. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2002121900047 20021219 00047 NM 2002 12 19 QXEA0201839 1 20021106 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 1 HAS LIGHT PITTING CORROSION AT STATION X418. REPAIRED IAW DHC-8 SRM 51-40-00 A ND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002121900048 20021219 00048 NM 2002 12 19 QXEA0201840 1 20021104 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SEAT TRACK NR 6 MINOR CORROSION IN CHANNEL AT STATION X542.000. REPAIRED IAW RD 8-53-4936 AND DHC-8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002121900049 20021219 00049 NM 2002 12 19 SPAA0200058 1 20021215 A 5311 6516300301 FRAME BOEING 737 7372T4 1384492 NM BULKHEAD CRACKED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 48754 22529 CRACKS NOTED IN SIDE FRAME AT BS 178, WL 195 TO WL 207 BL36L. VISUAL CRACKS VERIFIED BY HFEC INSPECTION. REPLACED SIDE C HORD PER BOEING SERVCICE BULLETIN 737-53A1173. 2 L 7 2 4F A16WE 2002121900050 20021219 00050 EU 2002 12 19 02351324 1 20021217 A 3350 FU248 FUSE JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 324UE 41017 During overnight maintenance, it was discovered that a section of emergency floor track lighting was inoperative. Maint enance personnel removed and replaced a fuse in the emergency lighting power supply. An operational check was satisfact ory and the aircraft was returned to service. 2 L 7 2 4T RT A41NM 2002121900053 20021219 00053 NM 2002 12 19 QXEA0201841 1 20021104 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SEAT TRACK NR 8 HAS SURFACE CORROSION AT STATION X503. REPAIRED IAW RD 8-53-1339 AND DHC-8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002121900054 20021219 00054 NM 2002 12 19 QXEA0201842 1 20021106 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SEAT TRACK NR 9 HAS CORROSION NEAR RIVETS BETWEEN STATIONS X200 AND X220. REPAIRED IAW RD 8-53-4473, RD 8-53-1102 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002121900056 20021219 00056 NM 2002 12 19 QXEA0201843 1 20021105 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM FUSELAGE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - RIVET APPEARS TO BE SMOKING IN RIGHT HAND AFT TAIL CONE AREA AT APPROXIMATELY FRAME 7, Z176.50. REPAIRED IAW DHC- 8 SRM 51-40-11, SRM 51-20-36 AND SRM 51-20-41. 2 H 7 2 4T RT A13NM 2002121900057 20021219 00057 NM 2002 12 19 2002UALA01825 1 20021206 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 BS 188 LT SIDE, WL207 FUSELAGE FRAME IS CRACKED IN 2 AREAS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900058 20021219 00058 NM 2002 12 19 2002UALA01827 1 20021207 A 5320 STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 AFT PRESSURE BULKHEAD RT FORWARD CIRCUMFERENTIAL STRAP WAS DENTED AT FASTENERS. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAI R. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900059 20021219 00059 NM 2002 12 19 QXEA0201844 1 20021104 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - LEFT HAND WING LOWER LEADING EDGE FLANGE CHAFED AT INBOARD EDGE. REPAIRED IAW RD 8-57-811, DHC-8 SRM 51-20-36 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2002121900060 20021219 00060 NM 2002 12 19 2002UALA01828 1 20021207 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 FRAME STA 500 ABOVE STRINGER 26 RT LWR SURFACE OF FRAME CAP AT NUTPLATE HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOM PLISHED. INSTALLED EXTERNAL FRAME DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900061 20021219 00061 NM 2002 12 19 QXEA0201845 1 20021106 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - LEFT HAND WING, NR 4 FLAP TRACK HAS RUST AND PITTING ON OUTBOARD SIDE TRACK (TRACK E). REPAIRED IAW HORIZON AIR E A 2-57-208. 2 H 7 2 4T RT A13NM 2002121900062 20021219 00062 NM 2002 12 19 QXEA0201846 1 20021106 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - LEFT HAND WING, NR 4 FLAP TRACK HAS 6 INCH GROOVE WITH PITTING ON LOWER OUTBOARD TRACK (TRACK D). REPAIRED IAW HO RIZON AIR EA 2-57-207. 2 H 7 2 4T RT A13NM 2002121900063 20021219 00063 NM 2002 12 19 2002UALA01829 1 20021207 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 AFT CABIN FLOORBEAM, STA 986, RBL 40 TO 46 HAS GOUGES AND CORROSION. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND STRAP REPAI R. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900064 20021219 00064 NM 2002 12 19 2002UALA01830 1 20021207 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 STATION 664, LBL 32 UPPER PRESSURE DECK FWD OF AIL TOWER SHAFT, WEB IS CRACKED 2 PLACES AROUND PILLOWED AREA. ACCOMPLIS HED MAJOR REPAIR. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900065 20021219 00065 NM 2002 12 19 2002UALA01831 1 20021207 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 AFT CARGO BAY, STA 727C BETWEEN STRINGER 21 LT AND STR 22 LT. FRAME IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL STRAP REPAIR . 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900066 20021219 00066 NM 2002 12 19 QXEA0201847 1 20021106 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 513 PDX - LEFT HAND WING, NR 4 FLAP TRACK HAS PITTING ON INBOARD SIDE TRACK (TRACK E). REPAIRED IAW HORIZON AIR EA 2-57-217 . 2 H 7 2 4T RT A13NM 2002121900067 20021219 00067 NM 2002 12 19 2002UALA01832 1 20021207 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 DENT INBOARD OF BS 747 FRAME ABOVE STRINGER 24 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL DOUBLER REPAIR. REPLA CED STRINGER CLIP AT STRINGER 24 LT. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900068 20021219 00068 NM 2002 12 19 QXEA0201849 1 20021106 A 1430 FASTENER DHAV DHC8 DHC8202 2809007 NM THRESHOLD CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - BAGGAGE COMPARTMENT DOOR THRESHOLD SCREWS AND SCREW NUTPLATES HAVE CORROSION ON THEM AT APPROXIMATELY STATIONS X55 0.000 AND X564.500. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2002121900069 20021219 00069 WP 2002 12 19 2002F01104 1 20020605 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 961R 46133 FOUND DURING DOUGLAS D-CHECK INSPECTION, REPAIR AT STATION 275 RIGHT 31 AND 32 HAS NO SUPPORTING DOCUMENTATION. REMOVED REPAIR IAW DC-8 SRM 51-1-20D. FABRICATED FILLER, DOUBLER. TREATED AND PRIMED AND INSTALLED REPAIR PER EO NR 02-039, W ITH APPROVED 8110-3 DATED 05/31/02. (M) 2 L 7 4 4F RT 4A25 2002121900070 20021219 00070 WP 2002 12 19 GTIA021153 1 20020919 A 5320 ATTACH FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND AFT CABIN STATION 1309 CORROSION ON BEAM ATTACH FITTING RBL 60 INCHES. REMOVED ATTACH FITTING. UPON REMOVA L OF ATTACH FITTING FOUND CORROSION ON WEB. REMOVED CORRODED WEB. LOCATED, DRILLED, AND DEBURRED REPAIR WEB. INSTALLE D REPAIR WEB. LOCATED DRILLED AND DEBURRED ATTACH FITTING. INSTALLED ATTACH FITTING. (M) 2 L 7 2 4F A6WE 2002121900071 20021219 00071 WP 2002 12 19 GTIA021154 1 20020822 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND CABIN RIGHT OUTBOARD SEAT TRACK CORRODED FS 294-466. REMOVED RIGHT OUTBOARD SEAT TRACK STATION 303-341. FA BRICATED 1 NEW SEAT TRACK SECTION RIGHT OUTBOARD STATION 303-341 AND 1 NEW SEAT TRACK SECTION RIGHT OUTBOARD STATION 341 -437. LOCATED AND DRILLED 3 SEAT TRACK REPAIR SPLICES. INSTALLED TWO NEW SEAT TRACK SECTIONS AND THREE REPAIR SPLICES. (M) 2 L 7 2 4F A6WE 2002121900072 20021219 00072 WP 2002 12 19 GTIA021155 1 20020822 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND CABIN RIGHT INBOARD SEAT TRACK CORRODED FS 294-466. REMOVED DAMAGED, CORRODED SEAT TRACK STATION 264 TO 342 . FABRICATED NEW SEAT TRACK SECTION. INSTALLED RIGHT INBOARD SEAT TRACK. REMOVED RIGHT INBOARD SEAT TRACK STATION 342 -436. LOCATED SEAT TRACK AND SEAT TRACK SPLICES. INSTALLED SEAT TRACK AND SEAT TRACK SPLICE. (M) 2 L 7 2 4F A6WE 2002121900073 20021219 00073 WP 2002 12 19 GTIA021156 1 20020813 A 5313 STRINGER DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND FORWARD CARGO STRINGER CORRODED FS 218-237. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED NEW SPLICES. FABRICATED NEW LONGERON. INSTALLED NEW LONGERON. INSTALLED NEW SPLICES. (M) 2 L 7 2 4F A6WE 2002121900074 20021219 00074 WP 2002 12 19 GTIA021157 1 20021011 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND FLOOR WEBBING STATION 130-140 AFT OF CAPTAINS SEAT IS PUNCTURED CRACKED IN 2 PLACES AND CORRODED. COCKPIT F LOOR WEB TORN AND CORRODED UNDER PILOTS INBOARD AFT SEAT TRACK. CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS DOUBLER AND FILLER. INSTALLED REPAIR INBOARD WEB REPAIR DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2002121900075 20021219 00075 WP 2002 12 19 GTIA021158 1 20021013 A 5512 SKIN DOUG DC9 DC981 3022081 WP HORIZ STAB CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND LEFT HORIZONTAL INBOARD STABILIZER HAS MISSING RIVET, CRACK AND HOLE 3 INCHES FROM INBOARD EDGE. STOP DRILL ED CRACK. FORMED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2002121900076 20021219 00076 WP 2002 12 19 GTIA021159 1 20021028 A 3260 833703 PROXIMITY SENSOR DOUG DC9 DC981 3022081 WP LT MLG FAULTY A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 806NK 48051 ORD - FLT 1226 - RED LEFT MAIN GEAR INDICATOR LIGHT FLICKERED OCCASIONALLY IN CLIMB-OUT FROM FL200 TO FL280 THEN REMAINE D OUT. FOUND LEFT MAIN UPLATCH PROXIMITY SENSOR BAD. REMOVED AND REPLACED LEFT MAIN UP LATCH PROX SENSOR. SYSTEM OPS CHECKS GOOD. PERFORMED PROX BOX TEST. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2002121900077 20021219 00077 NM 2002 12 19 2002UALA01833 1 20021209 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE NOSE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 949UA 26692 CRACK DETECTED WITH NDT BS 178 PRESSURE BULKHEAD WL 201 RBL 5 BEHIND LOWER RT ANTENNA MOUNT. MAJOR REPAIR ACCOMPLISHED . INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900078 20021219 00078 WP 2002 12 19 GTIA021161 1 20020927 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FORWARD CARGO STRINGER 29R FLOOR SUPPORT CORRODED FS 351-427. REMOVED FLOOR SUPPORT. INSTALLED SUPPORT FLO OR. (M) 2 L 7 2 4F RT A6WE 2002121900079 20021219 00079 WP 2002 12 19 GTIA021163 1 20021101 A 2781 STRIKER DOUG DC9 DC982 3022082 WP L/E SLAT DEFECTIVE A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 801NK 48048 ACY - FLT 311 - UPON SLAT RETRACT, THE SLAT DISAGREEMENT LIGHT CAME ON AND SLAT OVERSPEED WARNING IN FLIGHT. FOLLOWED Q RH PROCEDURES RETURNED TO KACY THERE WAS NO ROLL ASYMMETRY, AIRCRAFT WAS STABLE IN FLIGHT. REMOVED AND REPLACED NR 4 SL AT DRIVE DISAGREE PROX STRIKER PLATE IAW MD-80 SRM CH 51-30. (M) 2 L 7 2 4F A6WE 2002121900080 20021219 00080 NM 2002 12 19 2002UALA01834 1 20021208 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 FRAME REPAIR AT STATION 727C BETWEEN STRINGER 1R AND 2R HAS 4 EA DAMAGED HOLES. MAJOR REPAIR ACCOMPLISHED. DOUBLE J A NGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900081 20021219 00081 NM 2002 12 19 2002UALA01835 1 20021209 A 5314 KEELBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 LT SIDE OF KEELBEAM STATION 712 2ND TO LAST RIB AT FWD LT PUMP LEG ATTACH RIB IS CRACKED IN RADIUS. MAJOR REPAIR ACCOMP LISHED. REPLACED RIB. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900082 20021219 00082 NM 2002 12 19 2002UALA01836 1 20021206 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 FLOORBEAM UPPER T-CAP HAD EXCESS MATERIAL REMOVED DURING CORROSION CLEAN UP AT STA 365, RBL 42 AT STRINGER 17R. MAJOR RE PAIR ACCOMPLISHED. INSTALLED REPAIR WITH TWO STRAPS UNDER FWD CAP AND TWO J-ANGLE PLATES ON AFT SIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121900083 20021219 00083 NM 2002 12 19 2002UALA01837 1 20021207 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 CABIN CREASE BEAM HAS CORROSION AT STATION 324 RBL 62. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED INB OARD CREASE BEAM CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121900084 20021219 00084 NM 2002 12 19 2002UALA01838 1 20021208 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 FWD NOSE COMPARTMENT STATION 202, AT STRINGER 18 RIGHT HORIZONTAL FLOOR SUPPORT ANGLE CRACKED IN RADIUS AND ALONG HORIZO NTAL FLOOR WEB. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT ANGLE WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121900085 20021219 00085 NM 2002 12 19 2002UALA01839 1 20021206 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 DENT 3 FEET FORWARD OF DOOR 2L AT DOOR SILL LEVEL JUST FORWARD OF PREVIOUS REPAIR DENT MEASURES 1.5 BY 1.25 INCHES WITH DEPTH OF 5/32 INCH. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & STRINGER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121900086 20021219 00086 WP 2002 12 19 MWEA020740 1 20021219 A 5311 5912492501 ANGLE DOUG DC9 DC981 3022081 WP GALLEY SERV DR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 CUSP ANGLE AT FORWARD GALLEY SERVICE DOOR FORWARD AND AFT LOWER JAMB CORNERS HAS AREA OF LIGHT CORROSION 2 L 7 2 4F A6WE 2002121900087 20021219 00087 NM 2002 12 19 2002UALA01840 1 20021209 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 CABIN FLOORBEAM HAS CORROSION UNDER GUTTER AT BS 365, RBL 59-61. MAJOR REPAIR ACCOMPLISHED. INSTALLED CABIN FLOOR BEAM UPPER CAP "I" BEAM REDUCED SPLICE LENGTH REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2003011500142 20030115 00142 NM 2003 1 15 2002UALA01841 1 20021206 A 2920 HYDRAULIC SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE B SYSTEM CONTAMINATED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 392UA 24667 AIRCRAFT RETURNED TO FIELD WHEN RIGHT HAND LEADING EDGE DEVICES FAILED TO RETRACT AFTER TAKEOFF. PRIOR TO THE ABOVE INC IDENT, AIRCRAFT HAD TOTAL B SYS HYDRAULIC LOSS, CYCLED ALL CONTROLS THROUGH SEVERAL CYCLES TO ELIMINATE ANY AIR IN SYS. NO PHYSICAL OR INDICATION PROBLEMS NOTED IN SLAT OR FLAP SYSTEM. SYSTEM OPERATES NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900088 20021219 00088 NE 2002 12 19 2002UALA01842 2 20021209 A 7321 FUEL CONTROL BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING R Y J PARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 WP 29 615UA 21876 LOSS OF POWER TO NR 2 ENGINE. ENGINE RESTARTED. ENGINE WOULD NOT GO ABOVE IDLE. FCU CHANGED. BENCH CHECK SHOWED ACCE L & DECEL SCHEDULE UNDER LOW LIMITS, PROBABLE CAUSE OF POWER LOSS AT ALT 41K. 2 L 7 2 4F 4 F RT A1NM E3NE 2002121900089 20021219 00089 NM 2002 12 19 2002UALA01843 1 20021211 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 CABIN FRAME AT STATION 867 STRINGER 9R CRACKED AT FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED "J" ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2003021000017 20030210 00017 NM 2003 2 10 DHL2002741021 1 20021214 A 2612 POWER UNIT BOEING 727 7272Q9 138448M NM APU FIRE DETECT MALFUNCTIONED A DHLA K NONE L NO TEST NR NOT REPORTED 1 SO 01 741DH 21931 APU FIRE WARNING WILL NOT TEST. TRANSFERRED TO DMI 11242 PER MEL 26-11, CAT. "C". PLACARD INSTALLED. REF. DMI 11242 - APU FIRE WARNING WILL NOT TEST. REMOVED AND REPLACED APU FIRE TEST RELAY, IAW BMM 26-15-0. NO HELP, DMI 11242 STILL IN EFFECT. REF. DMI 11242 - APU FIRE WARNING WILL NOT TEST. REMOVED AND REPLACED APU FIRE TEST POWER UNIT MM 26-15-00. DMI #11242 REMAINS OPEN. 2 L 7 3 4F RT A3WE 2003032000068 20030320 00068 NM 2003 3 20 2002UALA01844 1 20021207 A 2840 WARNING SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUEL SYSTEM FALSE ACTIVATION A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 772UA 26930 ENGINE FUEL FILTERS ON LT & RT DIFFERENTIAL PRESSURE ACROSS LT FUEL FILTER APPROACHES BYPASS CONDITION. STATUS ENGINE FUEL FILTER DISPLAYED AFTER TAKE-OFF. REMAINED ON FOR APPROXIMATELY 30 SECONDS. FUEL CONTAMINATION CHECKS WERE MADE A T FUELING STATION, NO CONTAMINATION. BOTH FUEL FILTERS WERE REPLACED, SOME DEBRIS FOUND, BUT BELIEVED INSUFFICIENT TO CAUSE BYPASS. ONE FILTER WAS FLOW CHECKED. MAX DELTA-P ACROSS THE FILTER WAS 3 PSID; INSUFFICIENT TO TRIP THE DELTA-P S WITCH. BOTH DELTA-P SWITCHES WERE CHECKED. CLOSED AND OPENED WITHIN SPEC. SWITCHES WERE DISASSEMBLED - NO ANAMOLIES FOU ND. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002121900090 20021219 00090 NM 2002 12 19 QXEA0201850 1 20021106 A 5210 ATTACH FITTING DHAV DHC8 DHC8202 2809007 NM PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - MAIN CABIN DOOR SHELL, FORWARD LOWER ATTACH POINT FOR STEP ASSEMBLY FRETTING CORROSION. REPAIRED IAW CORROSION PR EVENTION MANUAL, CHAPTER 4, PAGES 4-26, PARAGRAPH 9B (6)(A) AND CHAPTER 5, PAGE 5-1, PARAGRAPH 2B. 2 H 7 2 4T RT A13NM 2002121900091 20021219 00091 NM 2002 12 19 QXEA0201851 1 20021106 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM CARGO DOOR LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - CENTER ROW OF RIVETS ON EXTERIOR OF CARGO DOOR SMOKING AT FORWARD AND AFT ENDS. REPAIRED IAW DHC-8 SRM 51-40-11, PAGES 1-4. 2 H 7 2 4T RT A13NM 2002121900092 20021219 00092 NM 2002 12 19 QXEA0201852 1 20021024 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - RIGHT WING CENTER LEADING EDGE INBOARD AND OUTBOARD RIBS ARE CRACKED IN FOUR PLACED. REPAIRED IAW DHC-8 SRM 51-00 -02 AND HORIZON AIR EA 6-57-74A. 2 H 7 2 4T RT A13NM 2002121900093 20021219 00093 NM 2002 12 19 QXEA0201853 1 20021024 A 5712 85720220001 RIB BOMBDR DHC8 DHC8401 1390041 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - LEFT WING CENTER LEADING EDGE INBOARD AND OUTBOARD RIBS ARE CRACKED IN FOUR PLACES. REPAIRED IAW EO DH85-57-0614A AND HORIZON AIR EA 6-57-74A. 2 H 7 2 4T RT A13NM 2002121900094 20021219 00094 NM 2002 12 19 QXEA0201854 1 20021028 A 7110 FITTING BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - LEFT HAND ENGINE LOWER COWLING BOTH INBOARD AND OUTBOARD Z MEMBER 87144116 ARE CRACKED. REPAIRED IAW DHC-8 Q400 S RM 51-42-05. 2 H 7 2 4T RT A13NM 2002121900095 20021219 00095 NM 2002 12 19 QXEA0201855 1 20021028 A 7110 FRAME BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - LEFT HAND ENGINE LOWER COWLING FRAME 87144120 IS CRACKED. REPAIRED IAW DHC-8 Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 2002121900096 20021219 00096 NM 2002 12 19 QXEA0201856 1 20021028 A 7110 ANGLE BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - LEFT HAND ENGINE LOWER COWLING ANGLE 87144121-101 IS CRACKED. REPAIRED IAW DHC-8 Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 2002121900097 20021219 00097 NM 2002 12 19 QXEA0201857 1 20021028 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - RIGHT HAND ENGINE LOWER COWLING, BOTH INBOARD AND OUTBOARD 87144114 CHANNELS ARE CRACKED. REPAIRED IAW DHC-8 Q400 SRM 51-42-45. 2 H 7 2 4T RT A13NM 2002121900098 20021219 00098 NM 2002 12 19 CALA0200588 1 20021216 A 5330 SKIN BOEING 737 7373T0 1384582 NM STA 727E CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND A 2.25" CRACK IN L/H FUSELAGE SKIN ABOUT TWO FEET AFT OF EMERGENCY LIGHT, AFT OF LEFT WHEEL WELL, STA 7 27E, S24L. REPAIRED IAW ECRA 5330-03188. 2 L 7 2 4F RT A16WE 2002121900099 20021219 00099 WP 2002 12 19 CALA0200589 1 20021217 A 5330 SKIN DOUG DC9 DC982 3022082 WP @MCD CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 98876 49444 INSPECTION FOUND A 1" CRACK IN FUSELAGE SKIN AROUND HOLD OPEN HOOK AT MAIN CABIN DOOR. DOUBLERS WERE INSTALLED IAW SRM 5 3-04, FIGURE 24. 2 L 7 2 4F A6WE 2002121900100 20021219 00100 NM 2002 12 19 CALA0200590 1 20021217 A 5754 SLAT BOEING 777 777224 1385225 NM #12 POSN. DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78003 27579 INSPECTION FOUND A DENT IN R/H WING #12 L/E SLAT AT I/B PORTION OF EXTERIOR SURFACE. THE DENT WAS REPAIRED IAW SRM 57-43 -01, FIGURE 201. 2 L 7 2 4F RT T00001SE 2002121900101 20021219 00101 NM 2002 12 19 CALA0200591 1 20021218 A 7110 NOSE COWL BOEING 777 777224 1385225 NM L/H ENGINE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78003 27579 INSPECTION FOUND A DENT IN L/H ENGINE NOSE COWL L/E LIP. REPAIRED IAW SRM 54-11-01, FIGURE 202. 2 L 7 2 4F RT T00001SE 2002121900102 20021219 00102 NM 2002 12 19 CALA0200593 1 20021218 A 5330 SKIN BOEING 777 777224 1385225 NM STA 172 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78003 27579 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 172, STRINGER 34L. REPAIRED IAW ECRA 5330-03187. A DIP WAS ISSUED TO PERFOR M AN EXTERNAL VISUAL INSPECTION OF THE REPAIR AREA EVERY 2,000 FLIGHT CYCLES AND TO HAVE AIRCRAFT PLANNING NOTIFY STRUCT URES ENGINEERING 30-60 DAYS PRIOR TO DEC. 12, 2003. 2 L 7 2 4F RT T00001SE 2002121900103 20021219 00103 NM 2002 12 19 QXEA0201858 1 20021028 A 7110 ANGLE BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - RIGHT HAND ENGINE LOWER COWLING ANGLE 87144121-101 IS CRACKED. REPAIRED IAW DHC-8 Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 2002121900104 20021219 00104 NM 2002 12 19 QXEA0201859 1 20021028 A 7110 FRAME BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - RIGHT HAND ENGINE LOWER COWLING FRAME 87144120 IS CRACKED. REPAIRED IAW DHC-8 Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 2002121900105 20021219 00105 NM 2002 12 19 2002UALA01845 1 20021205 A 2710 FLAPERON BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT & RT MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 209UA 30215 AIRCRAFT EXPERIENCED FISHTAILING, LASTING 30 SECONDS. SYNOPTIC INDICATED INDEPENDENT CYCLING OF LT & RT FLAPERONS NEAR FULL UP DEFLECTION. AFTER 3-4 CYCLES OPS NORMAL. AUTOPILOT ENGAGED DURING ENCOUNTER, FL380. NO FMC DIRECTED TURNS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002121900106 20021219 00106 NM 2002 12 19 QXEA0201860 1 20021025 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - LEFT HAND OUTBOARD FLAP TOP SKIN STATION 191.5 DEEP CHAFE LINE EXISTS. REPAIRED IAW HORIZON AIR EA 6-57-77 AND EO DH8S-57-0620. 2 H 7 2 4T RT A13NM 2002121900107 20021219 00107 NM 2002 12 19 2002UALA01847 1 20021212 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 955UA 26703 FRAME BENT AT BS 336 AT APPROXIMATELY STRINGER 18 LT. MAJOR REPAIR ACCOMPLISHED. ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2002121900108 20021219 00108 NM 2002 12 19 QXEA0201861 1 20021025 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - LEFT HAND OUTBOARD FLAP, TOP SKIN DEEP CHAFE LINE EXISTS AT STATION 225.4. REPAIRED IAW HORIZON AIR EA 6-57-77 AND EO DH8S-57-0620. 2 H 7 2 4T RT A13NM 2003022700075 20030227 00075 EU 2003 2 27 2002UALA01848 1 20021212 A 2121 EVT3454G FAN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E/E BAY FAILED A UALA B A EMER. DESCENT UNSCHED LANDING B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CR CRUISE 1 WP 29 463UA 1282 BURNING ELECTRICAL SMELL IN THE COCKPIT ACCOMPANIED BY AIRCRAFT VIBRATION. REPLACED AEVC BLOWER FAN, WHICH HAD EXPERIEN CED BEARING FAILURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2002121900109 20021219 00109 NM 2002 12 19 2002UALA01849 1 20021210 A 5310 SILL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE PAX DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 LT ENTRY DOOR WAY CUT OUT UPPER SILL HAS 4 HOLES DRILLED INTO IT. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121900110 20021219 00110 NM 2002 12 19 2002UALA01850 1 20021212 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 CABIN FLOORBEAM UPPER CAP CORRODED AT STA 324, RBL 45, 50, 53, 57 AND 58 (BOTH FWD AND AFT SIDES OF UPPER CAP) MAJOR RE PAIR ACCOMPLISHED. FLOORBEAM CAP REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2002121900111 20021219 00111 NM 2002 12 19 2002UALA01851 1 20021212 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 DENT IN SKIN JUST BELOW SKIN LAP AT STA 272, STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A1NM E24NE 2002121900112 20021219 00112 2002 12 19 0212133 4 20021213 A 3460 6227718004 DISPLAY SAAB SF340 SF340A 7850100 EU COCKPIT FAULTY A UHLA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 NE 03 108CQ 2681 2681 340A108 IN HGR BOTH EFIS AND MFD BLANKS OUT ON AND OFF CAPTAINS SIDE. THE SYSTEM WAS MEL. THE SYSTEM WAS OPERATIONAL IN DRIVE T RANSFER IAW THE MEL REQUIREMENTS. AWAITING TEARDOWN REPORT FOR CLOSER. 2 L 7 2 4T RT A52EU 2002121900113 20021219 00113 EU 2002 12 19 0212151 1 20021215 A 3230 AIR123530 PIN SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R389* NE NLG DRAG BRACE BINDING A UHLA B EMER. DESCENT J WARNING INDICATION LD LANDING 1 NE 03 104CQ 47 LK8500524 340A104 UPON LANDING GEAR EXTENSION CREW NOTED THAT THE NOSE GEAR WOULD NOT INDICATE DOWN AND LOCKED, WITH A LANDING GEAR CAUTIO N LIGHT ILLUMINATED. CREW RECYCLED GEAR AND GOT THE SAME EFFECT. CREW TRIED TO HAND PUMP GEAR DOWN FOR UP TO 20 MINUTE S WITH NO EFFECT. CREW DECLARED AN EMERGENCY, PERFORMED A SAFE LANDING. UPON LANDING MECHANIC DID VERIFY THAT THE NOSE LANDING GEAR WAS NOT LOCKED DOWN. FOUND LOCK AND BEARING LEVER AND PIVOT PIN ON NOSE GEAR DRAG BRACE TO BE FROZEN. WOULD NOT TRAVEL TO THE FULL DOWN AND LOCKED POSITION. DISASSEMBLED, CLEANED, AND REASSEMBLED, PERFORMED MULTIPLE GEAR SWING S, OPS CHECKS GOOD IAW MM. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002121900114 20021219 00114 EU 2002 12 19 0212181 1 20021218 A 3260 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A1 30030 NE ROTOL R389 R3894123F25 NE MLG ACTIVATED A UHLA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NE 03 104CQ 340A104 375 DGR612287 FLT 4539 APPROACH TO PIT HAD A UNSAFE GEAR WARNING INDICATOR ON LT MAIN GEAR. PILOT PERFORMED A GO AROUND AND AFTER RETR ACT AND SECOND EXTENSION CREW REPORTED 3 GREEN DOWN AND LOCKED INDICATION AND LANDED WITHOUT INCIDENT. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P30NE 2002121900115 20021219 00115 EU 2002 12 19 UHL2002F00010 1 20021202 A 3231 55028K PUSHROD SAAB SF340 SF340A 7850100 EU GE CT7TP CT79B 30030 NE RT MLG DIRTY A UHLA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NE 03 152CQ 340A152 DURING FLIGHT, PILOT CALLED, REPORTED THAT RIGHT MAIN GEAR DOOR EXTENDED IN FLIGHT . ADVISED PILOT TO REDUC AIRSPEED T O PREVENT DAMAGE TO DOOR UPON LANDING . MAINTENANCE WAS DISPATCHED TO REPAIR AND INSPECT DOOR FOR OVERSPEED DAMAGE IAW MM. CLEANED TELESCOPIC ROD ON MAIN DOOR TEST. FLEW AIRCRAFT ABOVE GEAR SPEED, NO FURTHER PROBLEMS NOTED. 2 L 7 2 4T 4 T RT A52EU E8NE 2002121900116 20021219 00116 NM 2002 12 19 AWXA200201225 1 20021122 A 5311 1461023 FRAME BOEING 757 757225 1384959 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 0 0 22207 LCQ - MAJOR REPAIR - DURING C-09 CHECK CORROSION WAS FOUND ON TOP OF FRAME IN THE AFT CARGO COMPARTMENT AT BS 1640, LBL 15. MAINTENANCE CUTOUT CORRODED SECTION OF FRAME AT BS 1640, LBL 15; FABRICATED 2 EACH CHANNELS AND A FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-07, PG. 201-203. 2 L 7 2 4F RT A2NM 2002121900117 20021219 00117 NM 2002 12 19 AWXA200201226 1 20021122 A 5311 146N1021 FRAME BOEING 757 757225 1384959 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 0 0 22207 LCQ - MAJOR REPAIR - DURING C-09 CHECK A 3" VERTICAL CRACK WAS FOUND ON FRAME IN THE AFT CARGO COMPARTMENT AT BS 1600, L BL 20. MAINTENANCE CUTOUT CRACKED SECTION OF FRAME AT BS 1600, LBL 20; FABRICATED REPAIR DOUBLER AND FILLER; INSTALLED R EPAIR PARTS IAW B757-200 SRM 53-00-07, PG. 201. 2 L 7 2 4F RT A2NM 2002121900118 20021219 00118 NM 2002 12 19 AWXA200201228 1 20021218 A 3350 BR963190 HARNESS BOEING 757 7572S7 1384962 NM SEAT ROW 3 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 0 0 23321 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 L/H WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT ROW 3 L/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2003011600163 20030116 00163 SO 2003 1 16 C2XA02SH149 1 20021223 A 5544 12033826001 SUPPORT EMB 145 EMB145ER 3260211 SO RUDDER DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV- DURING C-CHECK RUDDER NUMBER 1 CENTER HINGE POINT UPPER LEADING EDGE SKIN SUPPORT WAS FOUND BENT. MAINTENANCE REMO VED AND REPLACED AFFECTED SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2003011600164 20030116 00164 SO 2003 1 16 C2XA02SH150 1 20021223 A 5544 12033826001 SUPPORT EMB 145 EMB145ER 3260211 SO RUDDER DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV - DURING C-CHECK RUDDER 1 CENTER HINGE POINT LOWER LEADING EDGE SKIN SUPPORT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002122000001 20021220 00001 SO 2002 12 20 C2XA02SH151 1 20021220 A 5500 12033826001 RIB EMB 145 EMB145ER 3260211 SO RUDDER 1 BENT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV DURING C CHECK RIB WAS FOUND BENT ON RUDDER NUMBER ONE AT LOWER SIDE OF UPPER CENTER HINGE BRACKET. MAINTENANCE REM OVED AND REPLACED AFFECTED RIB IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2003011600165 20030116 00165 SO 2003 1 16 C2XA02SH152 1 20021223 A 5541 12033825001 RIB EMB 145 EMB145ER 3260211 SO RUDDER CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV- DURING C-CHECK RIB FOUND CRACKED ON RUDDER NUMBER 1 AT LOWER CENTER HINGE BRACKET. MAINTENANCE REMOVED AND REPLACE D AFFECTED RIB IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002122000002 20021220 00002 SO 2002 12 20 C2XA02SH153 1 20021220 A 5300 14521725103 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV DURING C CHECK SILL FOWARD OF SERVICE DOOR WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECT ED SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002122000003 20021220 00003 SO 2002 12 20 C2XA02SH154 1 20021220 A 5300 14521725015 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV DURING C CHECK SILL ON RIGHT SIDE SERVICE DOOR WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 SECTION 7 AND GST-3627/02. 2 L 7 2 4F RT T00011AT 2002122000004 20021220 00004 EU 2002 12 20 UHLA100771 1 20021201 A 6120 1103P0620 PRESSURE SWITCH SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE AUTOCOARSEN FAILED A UHLA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 NE 03 123XS N123XS PILOT REPORTS AUTOCOARSEN SYSTEM FAILED ON TAKEOFF ROLL AIRCRAFT RETURNED TO GATE. MECHANIC PERFORMED GROUND RUN AUTOCO ARSEN SYSTEM ADJUSTMENT/TEST IAW MM. OPS CHECKED GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2002122000015 20021220 00015 CE 2002 12 20 GLBA2002140 1 20020909 A 3230 571302 MOTOR BEECH 1900 1900D 1154162 CE MLG POWER PACK FAILED A GLBA O OTHER J WARNING INDICATION LD LANDING 1 NM 03 249GL 999 999 UE249 LANDING GEAR CIRCUIT BREAKER POPPED, MLG HAD TO BE HAND PUMPED DOWN, REMOVED AND REPLACED POWER PACK MOTOR OPS CHECK GOO D. 2 L 7 2 4T RT A24CE 2002122000017 20021220 00017 CE 2002 12 20 GLBA2002148 1 20020915 A 2130 SQUAT SWITCH BEECH 1900 1900D 1154162 CE CABIN PRESSURE FAILED A GLBA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CR CRUISE 1 NM 03 253GL UE253 A/C WILL NOT PRESSURIZE IN FLIGHT, REMOVED AND REPLACED SQUAT SWITCH, OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2002122000018 20021220 00018 2002 12 20 GLBA2002152 4 20020921 A 3422 6226136002 GYRO BEECH 1900 1900D 1154162 CE FIRST OFFICER FAILED A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 NM 03 251GL 4837 4837 UE251 BOTH PILOT & CO-PILOT EHSI SCREENS FROZE WHILE TURNING, REMOVED AND REPLACED FIRST OFFICER'S DIRECTIONAL GYRO. 2 L 7 2 4T RT A24CE 2002122000019 20021220 00019 CE 2002 12 20 GLBA2002155 1 20021002 A 2430 1293800161 CONTROL PANEL BEECH 1900 1900D 1154162 CE NR 1 DC GEN FAILED A GLBA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 NM 03 257GL 8156 65 UE257 LEFT DC GENERATOR FAILED ON TAKE OFF, REPLACED DC POWER PANEL. 2 L 7 2 4T RT A24CE 2002122000020 20021220 00020 CE 2002 12 20 GLBA2002156 1 20021002 A 3230 114810000656 TORQUE KNEE BEECH 1900 1900D 1154162 CE LT MLG BROKEN A GLBA O OTHER O OTHER LD LANDING 1 NM 03 228GL 14645 6767 UE228 LEFT MAIN GEAR TORQUE KNEE BROKE ON ROLL-OUT, REPLACED MAIN GEAR 2 L 7 2 4T RT A24CE 2002122000021 20021220 00021 CE 2002 12 20 GLBA2002159 1 20021008 A 2434 GENERATOR BEECH 1900 1900D 1154162 CE LEFT FAILED A GLBA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 NM 03 UE245 UE245 AIR RETURN, LT GENERATOR TIE OPEN ANNUNCIATOR ILLUMINATED IN FLIGHT, REMOVED AND REPLACED P172 & A257 OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2002122000022 20021220 00022 SO 2002 12 20 GLBA2002160 1 20021011 A 2741 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO LT ELEVATOR FAILED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 293UX 120293 ON TAKE OFF RECEIVED AURAL WARNING AND ABORTED TAKE OFF, REMOVED & REPLACED LEFT ELEVATOR TRIM PROXIMITY SENSOR. OPS CHE CK GOOD 2 L 7 2 4T RT A31SO 2002122000023 20021220 00023 CE 2002 12 20 GLBA2002161 1 20021011 A 3110 TUBE BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL DAMAGED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 204GL UE204 RT BLEED FAIL ANNUNCIATOR ILLUMINATED AFTER TAKE OFF, THEN RT & LT ENVIRONMENTAL FAIL ANNUNCIATOR ILLUMINATED, REPAIRED RT INSTRUMENT AIR TUBE 2 L 7 2 4T RT A24CE 2002122000024 20021220 00024 CE 2002 12 20 GLBA2002162 1 20021011 A 3110 TUBE BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL FAILED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 204GL UE204 AFTER TAKE OFF LT & RT ENVIRONMENTAL FAIL ANNUNCIATORS ILLUMINATED WITH LT BLEED ON AND RT BLEED OFF, REPAIRED RIGHT INS TRUMENT AIR TUBE OPS CHECKED SATISFACTORY. 2 L 7 2 4T RT A24CE 2002122000025 20021220 00025 CE 2002 12 20 GLBA2002163 1 20021014 A 3260 BULB BEECH 1900 1900D 1154162 CE MLG INDICATOR BURNED OUT A GLBA O OTHER P NO WARNING INDICATION AP APPROACH 1 NM 03 184UX UE184 LANDING GEAR LIGHT RIGHT SIDE WILL NOT ILLUMINATE, REPLACED BULB 2 L 7 2 4T RT A24CE 2002122000026 20021220 00026 CE 2002 12 20 GLBA2002164 1 20021018 A 6120 CONTROLLER BEECH 1900 1900D 1154162 CE LT PROPELLER OUT OF ADJUST A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 179GL UE179 LEFT PROPELLER 1650 MAX RPM AT TAKE OFF/ADJUSTED LEFT PROP. MAX RPM 2 L 7 2 4T RT A24CE 2002122000027 20021220 00027 CE 2002 12 20 GLBA2002165 1 20021018 A 7712 1143800653 INDICATOR BEECH 1900 1900D 1154162 CE TORQUE FAILED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 251GL 9999 9999 UE251 DISC TORQUE INDIATOR FAILED ON TAKE OFF. REMOVED AND REPLACED INDICATOR. 2 L 7 2 4T RT A24CE 2002122000028 20021220 00028 NM 2002 12 20 CALA0200594 1 20021219 A 5754 SKIN BOEING 777 777224 1385225 NM #7 SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78003 27579 NSPECTION FOUND L/H WING #7 SLAT SKIN DENTED IN LEADING EDGE. REPAIRED IAW ECRA 5750-03106. 2 L 7 2 4F RT T00001SE 2002122000029 20021220 00029 NE 2002 12 20 GLBA2002166 2 20021021 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 FAILED A GLBA E C ENGINE SHUTDOWN ABORTED TAKEOFF B Y J SMOKE/FUMES/ODORS/SPARKS ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 NM 03 249GL 15342 2 UE249 114406 NR 2 ENGINE PRODUCED A SEVERE VIBRATION AND EXPELLED SPARKS ON TAKE OFF POWER UP, REMOVED & REPLACED RT ENGINE. OPS CHE CK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2002122000031 20021220 00031 EA 2002 12 20 SWIA200211573 1 20021214 A 2740 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA #2 MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 595SW 7292 SHORTLY AFTER TAKEOFF, STAB TRIM DISENGAGED AND WOULD NOT REENGAGE (FLAPS & GEAR WERE UP). REPLACED COPILOT TRIM DISCON NECT SWITCH IAW MM 27-41-05. OPS CHECKS GOOD IAW MM 27-40-00 AND 27-41-00. SYSTEM OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2002122000032 20021220 00032 EA 2002 12 20 SWIA200211576 1 20021214 A 3010 SENSOR CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE DUCT MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 409SW 7056 DURING CRUISE CLIMB WE RECEIVED AN ''ANTI-ICE DUCT'' WARNING MESSAGE WHICH WOULD NOT EXTINGUISH WHILE ANTI-ICE WAS ON. ANTI-ICE SYNOPTIC PAGE SHOWED LEFT WING ANTI-ICE DUCT ILLUMINATED IN RED. REMOVED AND REPLACED SENSOR.IAW AMM 30-12-00. PERFORMED ENGINE RUNS FOR OPS CHECK. OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2002122000033 20021220 00033 EA 2002 12 20 SWIA200211578 1 20021216 A 2910 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA BLUE #1 BROKEN A SWIA D RETURN TO BLOCK J K WARNING INDICATION FLUID LOSS TX TAXI/GRND HDL 1 NM 07 438SW 7574 ON THE TAXI OUT, #1 HYDRAULIC 1B CAUTION ILLUMINATED, FOLLOWED BY #1 HYDRAULIC LOW PRESSURE CAUTION MESSAGE. #1 HYDRAUL IC RESERVOIR ON SYNOPTICPAGE SHOWED NO FLUID. REPAIRED BROKEN HYDRAULIC LINE FOR BLUE #1 HYDRAULIC SYSTEM (HYDRAULIC SE RVICE LINE/SYSTEM RETURN LINE) IAW MM 20-22-00. LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2002122000034 20021220 00034 WP 2002 12 20 0204049915 1 20021209 A 5310 BULKHEAD DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 965N 47417 During an Hck in ATL and while accomplishing an inspection, a crack was found in the aft pressure bulkhead doorjamblower sill channel. The crack is in the upper flange of the channel and extends approximately .75" through a screw hole. Repa ired per EA 99-190869. 2 L 7 2 4F A6WE 2002122000035 20021220 00035 WP 2002 12 20 0204059869 1 20021113 A 5310 BULKHEAD DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 778NC 48100 During Mck at ATL, a crack was found in the 5910130-13 doubler radius of the upper LHS corner door jamb and extended und er the 59-10130-9 channel. Also, another crack was found in the LHS upper corner. Repaired per EA 98-190832. 2 L 7 2 4F RT A6WE 2002122000036 20021220 00036 WP 2002 12 20 0204069854 1 20021114 A 5310 BULKHEAD DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 763NC 47716 During M ck in ATL maintenance base, a .5" crack was found in the RH side APB channel extending down from the upper bend cut out. Repaired per EA 98-190854. 2 L 7 2 4F RT A6WE 2002122000037 20021220 00037 WP 2002 12 20 0204079869 1 20021118 A 5330 DOOR FRAME DOUG DC9 DC951 3022051 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 778NC 48100 During MCK at ATL base, the forward upper corner of the forward cargo door doorjamb was found cracked 1/16" long. The cr ack was repaired per EA 98-190835. 2 L 7 2 4F RT A6WE 2002122000038 20021220 00038 EA 2002 12 20 2002F01115 1 20020601 A 3220 16040111 PACKING CNDAIR CL600 CL6002B19 1900309 EA NLG DAMAGED A MASA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 47202 7202 FLT 5853 - CLE-PHL - GEAR DISAGREE MESSAGE. NOSE GEAR WILL NOT RETRACT ON FIRST ATTEMPT. MAINTENANCE WAS CALLED. MAIN TENANCE REPLACED PACKING, ADJUSTED TARGET. OP CHECKS GOOD IAW CRJ MM 32-21-00. (M) 2 L 7 2 4F RT A21EA 2002122000039 20021220 00039 EA 2002 12 20 2002F01116 1 20021014 A 2750 601R931059 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A MASA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 47239 7239 FLT 6412 - PHX-COS, DECLARED AN EMERGENCY AND RETURNED TO FIELD DUE TO FLAPS SYSTEM FAILING AT DEGREES. MAINTENANCE HAD REPLACED THE LT INBOARD FLAP ACTUATOR THE NIGHT BEFORE FOR A PREVIOUS FAILURE. MAINTENANCE REMOVED AND REPLACED BPSU. MAINTENANCE COMPLIED WITH PART A ON 10/13 AND PART B ON 10/14. (M) 2 L 7 2 4F RT A21EA 2002122000040 20021220 00040 EA 2002 12 20 2002F01117 1 20020513 A 3260 16050109 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF ADJUST A MASA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 47202 7202 FLT 5786 - CVG-CLT, DURING LANDING GEAR RETRACTION GOT GEAR DISAGREE MESSAGE. NOSE GEAR WAS SLOW TO RETRACT AND LOCK. AIRCRAFT LANDED WITHOUT INCIDENT IN CLT. MAINTENANCE ADJUSTED PROXIMITY SENSOR. OP CHECKS GOOD IAW CRJ AMM 32-35-05. (M) 2 L 7 2 4F RT A21EA 2002122000041 20021220 00041 EA 2002 12 20 ASOA02589 1 20021111 A 7920 4037T34P02 B-NUT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE LOOSE A ASOA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 11 839AS 7284 FLT 4476 - DURING CLIMB-OUT FROM ATL-HPN, THE LEFT ENGINE OIL PRESSURE DROPPED BELOW 25 PSI. THE CAPTAIN SHUT THE ENGIN E DOWN AND THE AIRCRAFT RETURNED TO ATL. AN EMERGENCY LANDING WAS MADE SAFELY IN ATL. MAINTENANCE FOUND THE LEFT ENGIN E 5 QUARTS LOW OF OIL AND THE B-NUT ON THE C-SUMP 4 O'CLOCK RETURN LINE LOOSE. MAINTENANCE TIGHTENED THE B-NUT ON THE R ETURN LINE AND SERVICED THE LEFT ENGINE WITH 5 QUARTS OF OIL. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVIC E. (M) 2 L 7 2 4F RT A21EA 2002122000042 20021220 00042 NM 2002 12 20 GAIA02157OP 1 20021120 A 3260 CONNECTOR BOEING 727 727251 138408H NM NLG LOOSE A GAIA K NONE N FALSE WARNING AP APPROACH 1 SW 07 278US 21157 FLT 516 - FWA-ELP, ON APPROACH WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION. THE NOSE LANDING GEAR R ED LIGHT REMAINED ILLUMINATED WITH NO NOSE GREEN LIGHT AT ALL. THE GEAR WAS RECYCLED AND THE RED LIGHT EXTINGUISHED. T HE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. INSPECTION FOUND A LOOSE CONNECTOR ON THE NLG DOWN LOCK SWITCH. OPERATION ALLY CHECKED GOOD. INSPECTION COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2002122000043 20021220 00043 WP 2002 12 20 GTIA021164 1 20021031 A 3397 WIRE DOUG DC9 DC981 3022081 WP A/C BAY DISCONNECTED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 806NK 48051 DTW - FOUND EMERGENCY LIGHTS ABOVE TAIL COMPARTMENT WALKWAY INOPERATIVE. RECONNECTED WIRES TO LIGHT. OPS CHECKS GOOD IA W 33-53-02. (M) 2 L 7 2 4F A6WE 2002122000044 20021220 00044 WP 2002 12 20 GTIA021165 1 20020924 A 5314 KEELBEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND RIGHT KEEL BEAM INTERIOR STRUCTURE HAS SEVERAL AREAS OF CORROSION STATION 826-843. REMOVED SUPPORT FITTING. REMOVED BATHTUB FITTING. REMOVED CORROSION FROM RIGHT KEEL BEAM HORIZONTAL FLANGE FOUND TO BE OUT OF LIMITS. FABRICA TED NEW FITTING AT STATION 826, LONGERON 29R. LOCATED AND DRILLED LONGERON 29R FITTING. INSTALLED LONGERON 29R FITTING . FABRICATED REPAIR DOUBLER -3. LOCATED AND DRILLED NEW FITTING AT STATION 843 RIGHT. LOCATED AND DRILLED BATHTUB FIT TING. INSTALLED -3 DOUBLER IAW SPIRIT AIRLINES EA 5310-0247. INSTALLED 3936377-2 FITTING AT STATION 843 RIGHT. INSTAL LED RIGHT BATHTUB FITTING. (M) 2 L 7 2 4F RT A6WE 2002122000045 20021220 00045 WP 2002 12 20 GTIA021167 1 20020923 A 5320 CLIP DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FS 840 KEEL BEAM LEFT BATHTUB FITTING UPPER T-CLIP CRACKED. REMOVED BATHTUB FITTING. REMOVED T-CLIP. FABR ICATED NEW TEE CLIP. LOCATED AND DRILLED TEE. INSTALLED TEE CLIP. LOCATED AND DRILLED LEFT BATHTUB FITTING. INSTALLE D LEFT BATHTUB FITTING. (M) 2 L 7 2 4F RT A6WE 2002122000046 20021220 00046 WP 2002 12 20 GTIA021168 1 20021023 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE. L1 DOOR EMERGENCY CARRY AROUND LIGHT STAYS ON WHEN NOT ARMED AFTER A RMING AND DISARMING. FOUND LOOSE TERMINAL WIRING ON EMERGENCY LIGHTING BATTERY CHARGER, REPAIRED WIRING. FOUND BROKEN WIRES ON CONNECTOR AT PORTABLE BATTERY CHARGER LIGHT AT L1 DOOR, REPAIRED WIRES. (M) 2 L 7 2 4F RT A6WE 2002122000047 20021220 00047 WP 2002 12 20 GTIA021169 1 20020926 A 5313 STRINGER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND MID CARGO PIT STRINGER 29R CORRODED AT FS 712-750, FS 788-817. MID CARGO FS 712-731 STRINGER 29R CORRODED. MID CARGO FS 731-750 STRINGER 29R CORRODED. MID CARGO STRINGER 29R CORRODED FS 807-817. MID CARGO FS 807-788 STRINGER 29R CORRODED. REMOVED DAMAGED LONGERON SECTION STATION 712-740. FABRICATED A NEW LONGERON SECTION AND SPLICE. FLOORB OARDS SUPPORT OUT OF LIMITS. LOCATED AND DRILLED AND DEBURRED REPAIR 'L' ANGLE 2. INSTALLED NEW LONGERON AND SPLICE. INSTALLED REPAIR 'L' ANGLES 2 STRAP ON FLOORBOARD SUPPORT BEAM. (M) 2 L 7 2 4F RT A6WE 2002122000048 20021220 00048 WP 2002 12 20 GTIA021170 1 20021019 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND LEFT OUTBOARD SEAT TRACK APPROXIMATELY STATION 807, 788, 768, 750, 731, 712, 693, 674, 655, 636, 617, 598, 5 60 AND 541. GOUGES AND CORROSION IN TRACK, APPROX STATION 807, 788, 768, 758 740, 731, 712, 693, 623, 674 AND 655 CORRO SION AND GOUGES AT SCALLOPS. MATERIAL LOSS IS OUT OF LIMITS LEFT OUTBOARD SEAT TRACK STATION 715 AND 790. REMOVED DAMA GED SECTION TO SPLICE AT STATION 798. FABRICATED NEW SEAT TRACK SECTION. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2002122000049 20021220 00049 WP 2002 12 20 GTIA021171 1 20020822 A 5313 STRINGER DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND PASSENGER CABIN FS 1117 STRINGER 1 CRACKED. REMOVED LONGERON 1 STATION 1110-1164. LOCATED AND DRILLED NEW LONGERON. INSTALLED NEW LONGERON. (M) 2 L 7 2 4F A6WE 2002122000050 20021220 00050 WP 2002 12 20 GTIA021172 1 20020919 A 5315 FLOORBEAM DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - AFT CABIN STATION 1322 FLOORBEAM CRACKED AT LBL 30 INCHES. REMOVED DAMAGED AREA. LOCATED AND DRILLED REPAIR ANGL E AND FILLERS. INSTALLED REPAIR ANGLE AND FILLERS. (M) 2 L 7 2 4F A6WE 2002122000051 20021220 00051 WP 2002 12 20 GTIA021173 1 20021026 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND PASSENGER CABIN FLOOR PANEL STATION 1117 TO STATION 1080 IS CRACKED/DAMAGED. FABRICATED NEW CABIN FLOOR PAN EL. (M) 2 L 7 2 4F A6WE 2002122000052 20021220 00052 WP 2002 12 20 GTIA021174 1 20021024 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - PASSENGER CABIN FLOORBOARD STATION 160 TO 200 LEFT SIDE (12X40) FRONT L1 DOOR, HAS SOFT/MUSHY AND CORRODED AT INSE RTS 22. FABRICATED PASSENGER CABIN FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002122000053 20021220 00053 WP 2002 12 20 GTIA021175 1 20021024 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND PASSENGER CABIN FLOORBOARD STATION 200 TO STATION 256 CENTER AREA SEVERAL CRACKED/DAMAGED AT INSERTS. FABRI CATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2002122000054 20021220 00054 WP 2002 12 20 GTIA021176 1 20021024 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND PASSENGER CABIN FLOORBOARD STATION 160 TO STATION 200 RIGHT SIDE FRONT R1 DOOR HAS CRACKED/DAMAGED AROUND TH E EDGE. FABRICATED FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002122000055 20021220 00055 WP 2002 12 20 GTIA021177 1 20021024 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND PASSENGER CABIN FLOOR PANEL STATION 196 TO STATION 256 HAS SOFT/MUSHY AND CORRODED AT INSERTS. FABRICATED N EW PANEL. (M) 2 L 7 2 4F A6WE 2002122000056 20021220 00056 WP 2002 12 20 GTIA021178 1 20021024 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 PASSENGER CABIN FLOOR BOARD STATION 160 TO 172 FRONT R1 DOOR, HAS CRACKED/SOFT CORRODED AT INSERTS. FABRICATED, LOCATED AND DRILLED HOLES ON PANEL. (M) 2 L 7 2 4F A6WE 2002122000057 20021220 00057 SO 2002 12 20 GLBA2002167 1 20021022 A 3260 WARNING LIGHT EMB 120 EMB120ER 3260203 SO RT MLG MALFUNCTIONED A GLBA O OTHER N FALSE WARNING CL CLIMB 1 NM 03 293UX 120293 RT GEAR A & B RED LIGHT REMAIN ILLUMINATED AFTER RETRACTION, DEICED LANDING GEAR- INSP-TEST FLIGHT SATISFACTORY. 2 L 7 2 4T RT A31SO 2002122000058 20021220 00058 WP 2002 12 20 GTIA021179 1 20020920 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND FLOOR PANEL RIGHT SIDE UNDER RUDDER PEDAL CRACKED IN RIBS. REMOVED RIGHT AND LEFT INBOARD RIBS FROM FLOOR P ANEL. FABRICATED RIBS. FOND FLOOR PANEL WEB MATERIAL CRACKED. FABRICATED DOUBLER. FABRICATED FILLER. INSTALLED DOUB LER AND FILLER. INSTALLED RIBS. (M) 2 L 7 2 4F A6WE 2002122000059 20021220 00059 WP 2002 12 20 GTIA021180 1 20021027 A 5320 ATTACH ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FLOOR SUPPORT PANEL ATTACH ANGLES AT STATION 408 AND 427 CRACKED. REMOVED TWO SUPPORT ANGLES. FABRICATED TWO SUP PORT ANGLES. INSTALLED TWO SUPPORT ANGLES. (M) 2 L 7 2 4F A6WE 2002122000060 20021220 00060 WP 2002 12 20 GTIA021182 1 20021027 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND MID B/B DOOR, LOWER JAMB CORROSION FROM 636-693. REMOVED JAMB BEAM. LOCATED AND DRILLED NEW DOOR BEAM. IN STALLED JAMB BEAM PER MD80 SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2002122000061 20021220 00061 WP 2002 12 20 GTIA021184 1 20021105 A 3320 BALLAST DOUG DC9 DC983 3022083 WP CABIN DIRTY A GTIA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 GL 23 814NK 49619 ORD - FLT 1441 - FLIGHT ATTENDANT REPORTED HOT SMELL ROW 9 A/C RIGHT. TURNED OFF SIDEWALL LIGHTS AND HOT SMELL DISAPPEA RED, NO SMOKE OR HEAT WAS OBSERVED IN AREA. INSPECTED BALLAST ABOVE ROW 9 A/C RIGHT AND LEFT SIDE. CLEANED DUST OFF BA LLAST. NO DEFECTS NOTED, IAW MD-80 MM 33-21-03. (M) 2 L 7 2 4F RT A6WE 2002122000062 20021220 00062 WP 2002 12 20 GTIA021186 1 20021107 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 DTW - FUSELAGE DAMAGED APPROXIMATELY 18 INCHES AFT OF LOWER RIGHT CORNER OF L1 DOOR. REPAIRED PER MD-80 SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2002122000063 20021220 00063 2002 12 20 GTIA021187 4 20021109 A 2565 SLIDE DOUG DC9 DC982 3022082 WP DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 MYR - FLT 1481 - FORWARD SLIDE PACK FELL OFF. REINSTALLED FORWARD SLIDE PACK IAW MM 25-62-00. (M) 2 L 7 2 4F A6WE 2002122000064 20021220 00064 WP 2002 12 20 MWEA020743 1 20021220 A 5310 9910073285 BRACKET DOUG DC9 DC981 3022081 WP STA 42 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 CORROSION ON FORWARD ACCESSORY DOOR APPROXIMATELY SWITCH SUPPORT BRACKET AT STATION 42 CEILING AREA. -- FABRICATED AND INSTALLED SUPPORT BRACKET. 2 L 7 2 4F A6WE 2002122000065 20021220 00065 WP 2002 12 20 MWEA020746 1 20021220 A 5311 595606515 STIFFENER DOUG DC9 DC915 3022036 WP SLANT PANEL CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 SIX EACH STIFFENERS CORRODED ON LEFT PRESSURE PANEL. -- FABRICATED AND INSTALLED STIFFENERS. 2 L 7 2 4F A6WE 2002122000066 20021220 00066 WP 2002 12 20 GTIA021188 1 20021110 A 5240 SEAL DOUG DC9 DC982 3022082 WP L2 DOOR OUT OF POSITION A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 823NK 48020 DTW - FLT 639 - AT 9,000 FT SOUTH OF DTW, LOST PRIMARY AND SECONDARY PRESSURE CONTROLLER, WENT TO MANUAL CONTROLLER, WEN T BACK TO AUTO, WORKED OK AT 29,000 FT IN CRUISE, CABIN STARTED TO CLIMB IN AUTO AND MANUAL FULL FORWARD. DESCENDED TO 25,000 FT. MAINTAINED CABIN AT 8,500 IN AUTO AND MANUAL PER F/A, NOISE FORWARD LEFT EMERGENCY EXIT. QRH PROCEDURES COM PLIED WITH. INTERMITTENT FLOW LIGHT IN CRUISE 1.90 EPR AND LESS. CHECKED CABIN PRESSURE CONTROL SYSTEM. NO DEFECTS NO TED. FOUND LOWER AREA OF L2 DOOR SEAL OUT OF GROOVE. REINSTALLED INTO GROOVE PER M/M 52-42-02. PRESSURIZED A/C. INSP ECTED L2 DOOR AND EMERGENCY OVERWING EXIT DOORS FOR LEAKS. NO LEAKS NOTED. OK TO CONTINUE. (M) 2 L 7 2 4F A6WE 2002122000067 20021220 00067 WP 2002 12 20 GTIA021189 1 20021017 A 7110 SKIN DOUG DC9 DC983 3022083 WP LT NOSE COWL DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND LEFT ENGINE COWL HAS DENT ON LIP AT 7 O'CLOCK POSITION. REMOVED LEFT ENGINE NOSE COWL. INSTALLED SERVICEAB LE NOSE COWL. (M) 2 L 7 2 4F RT A6WE 2002122000068 20021220 00068 WP 2002 12 20 GTIA021190 1 20021107 A 3350 CONTACTOR DOUG DC9 DC983 3022083 WP CABIN DIRTY A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND EMERGENCY OVERWING LIGHTS INOPERATIVE. T/S SYSTEM IAW MD80 MM 33-53-00 FOUND FAULTY LAMP CONTACTS, CLEANED CONTACT SYSTEM OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 2002122000069 20021220 00069 WP 2002 12 20 GTIA021191 1 20021013 A 5310 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND FORWARD ENTRANCE, AFT LOWER DOUBLER JAMB CORRODED AND MISSING 3 FASTENERS SUPPORT FORMER, STATION 207. REMO VED DOOR JAMB DOUBLER. INSTALLED FORWARD ENTRANCE AFT LOWER DOOR JAMB DOUBLER. (M) 2 L 7 2 4F A6WE 2002122000070 20021220 00070 WP 2002 12 20 GTIA021192 1 20021018 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND EXISTING DOUBLER AT FS 541 BETWEEN LONGERON 24R AND 25R REQUIRES REPLACEMENT. REMOVED EXISTING REPAIR. REM OVED ADDITIONAL MATERIAL BETWEEN LONGERON 23R AND 25R. FABRICATED NEW SKIN SECTION, DOUBLERS, LONGERON STRAPS AND FINGE R DOUBLERS. INSTALLED NEW REPAIR PARTS, 5, 7, 9 AND 31. (M) 2 L 7 2 4F A6WE 2002122000071 20021220 00071 WP 2002 12 20 GTIA021193 1 20021103 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND CORRODED INTERCOSTAL IN AFT CARGO COMP, FS 1026 LONGERON 28R. REMOVED DAMAGED INTERCOSTAL. FABRICATED INTE RCOSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2002122000072 20021220 00072 WP 2002 12 20 GTIA021194 1 20020813 A 5320 SPLICE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND AFT PIT STATION 1290-1309 L30, CORROSION IN LONGERON AROUND FASTENERS. REMOVED DAMAGED SPLICE. INSTALLED N EW SPLICE. (M) 2 L 7 2 4F A6WE 2002122000073 20021220 00073 WP 2002 12 20 GTIA021195 1 20020822 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND CABIN RIGHT INBOARD SEAT TRACK CORRODED FS 200-294. REMOVED SEAT TRACK. FABRICATED NEW SECTION OF SEAT TRA CK. INSTALLED NEW SEAT TRACK. (M) 2 L 7 2 4F A6WE 2002122000074 20021220 00074 WP 2002 12 20 GTIA021196 1 20020822 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND CABIN RIGHT OUTBOARD SEAT TRACK CORRODED FS 200-294. REMOVED DAMAGE SECTION. TRIMMED, LOCATED, AND DRILLED NEW SECTION. INSTALLED NEW SEAT TRACK SECTION. (M) 2 L 7 2 4F A6WE 2002122000075 20021220 00075 WP 2002 12 20 GTIA021197 1 20021024 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - PAX CABIN RIGHT WEB FLOOR PANEL STATION 200-256 IS CRACKED/DAMAGE AT HATS SECTION, BOTH SIDE. REPAIRED DAMAGED AR EAS. (M) 2 L 7 2 4F A6WE 2002122000076 20021220 00076 WP 2002 12 20 GTIA021198 1 20020919 A 5315 FLOORBEAM DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND AFT CABIN STATION 1338 AT RBL 48 CORROSION ON STRUCTURE. REMOVED DAMAGED AREA AT FLOORBEAM. FABRICATED TWO ANGLES. INSTALLED TWO REPAIR ANGLES. (M) 2 L 7 2 4F A6WE 2002122000077 20021220 00077 WP 2002 12 20 GTIA021199 1 20021030 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND CABIN FLOORBOARD STATION 1174-1117, BROKEN, DELAMINATED AND SOFT. FABRICATED A NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2002122000078 20021220 00078 CE 2002 12 20 GLBA2002168 1 20021023 A 3060 BRUSH BLOCK BEECH 1900 1900D 1154162 CE RT PROPELLER DAMAGED A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 228GL UE228 RIGHT PROP HEAT SLOWLY DROPS TO ZERO AMPS, DIVERTED AC TO CYS. R&R RIGHT PROP HEAT BRUSH BLOCK. 2 L 7 2 4T RT A24CE 2003021000134 20030210 00134 NM 2003 2 10 DHL2002747012 1 20021218 A 2610 WARNING LIGHT BOEING 727 727224 1384076 NM NR 1 ENGINE ILLUMINATED A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 747DH 22253 NR 1 ENGINE GROUND CIRCUIT DETECTOR LIGHT ILLUMINATED. DEFERRED PER MEL 26-9. CONTROL 11286 ASSIGNED. PLACARD INSTALL ED. 2 L 7 3 4F A3WE 2002122000079 20021220 00079 NM 2002 12 20 QXEA0202200 1 20021219 A 3350 6104789 BATTERY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 1835 194 524 PSC-EMERGENCY LIGHTS AT FORWARD AND 3RD LIGHT CEILING PANEL AND AFT EGRESS LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT PS2. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002122000080 20021220 00080 WP 2002 12 20 DHL2002873002 1 20021219 A 2611 100105201 CONTROL UNIT DOUG DC8 DC873F 302199F WP SMOKE DETECT FAILED A DHLA K O NONE OTHER O OTHER IN INSP/MAINT 1 SO 01 873SJ 46091 LOWER CARGO SMOKE DETECTOR (AD4338-B). REPORTED ON PREFLIGHT. DEFERRED FURTHER TROUBLESHOOTING AND REPAIR PER MEL 26-1 0-1 CAT. "C" SMOKE DETECTOR (AD4338-B) DMI 11310. PLACARD INSTALLED. REF. DMI #11310: LOWER CARGO SMOKE DETECTION (AD 4338-B), REPORTED ON PREFLIGHT. REMOVED AND REPLACED CCU PER SECURAPLANE M/M REF. 26-15-01-2. OPS CHECKED GOOD. OK TO CONTINUE. THIS ACTION CLEARS DMI 11310. PLACARDS REMOVED. 2 L 7 4 4F RT 4A25 2002122000081 20021220 00081 CE 2002 12 20 GLBA2002169 1 20021023 A 3060 CONNECTOR BEECH 1900 1900D 1154162 CE LT PROPELLER LOOSE A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 255GL UE255 LT PROP DE-ICE FLUCUATED 0-3 AMPS IN OFF MODE UP TO 35 AMPS. SECURED LOOSE CONNECTION ON DE-ICE AMMETER IAW M.M AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4T RT A24CE 2002122000082 20021220 00082 SO 2002 12 20 C2XA02TY175 1 20021219 A 3243 9067403 CHECK VALVE EMB 145 EMB145LR 3260212 SO INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 10848 10848 145181 TYS, During a scheduled inspection, the parking brake system failed operational check of the return line valve. Maintena nce removed and replaced the return line check valve. operational checked good. I/A/W-EMB-145-AMM-32-44-08 and 01. Aircr aft released to service. 2 L 7 2 4T RT T00011AT 2002122000083 20021220 00083 CE 2002 12 20 GLBA2002170 1 20021024 A 3020 ANTI-ICE SYSTEM BEECH 1900 1900D 1154162 CE RT ENGINE MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 153UE UE153 RT. ENGINE ICE-VANE WOULD NOT EXTEND IN FLIGHT, RIG DOOR OPS CHECK GOOD 2 L 7 2 4T RT A24CE 2002122000084 20021220 00084 WP 2002 12 20 GTIA021200 1 20020822 A 5313 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND PASSENGER CABIN FS 1174 STRINGER 3L, LONGERON CRACKED. REMOVED DAMAGED SECTION OF LONGERON. LOCATED AND DR ILLED NEW LONGERON AND TWO SPLICES. INSTALLED NEW LONGERON. (M) 2 L 7 2 4F A6WE 2002122000085 20021220 00085 SO 2002 12 20 GLBA2002171 1 20021024 A 5753 CHANNEL EMB 120 EMB120ER 3260203 SO TE FLAP DAMAGED A GLBA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 NM 03 96ZK 120096 ON TAKE OFF FLAPS WOULD NOT RETRACT TO 0 DEGREE & IND. A FLAP DISGREEMENT THE O.B. FLAP STUCK BETWEEN 0-15 PERCENT, R& R LT OUTBOARD MOVABLE CHANNEL OPS CHECK GOOD 2 L 7 2 4T RT A31SO 2002122000086 20021220 00086 WP 2002 12 20 GTIA021201 1 20021028 A 5532 SKIN DOUG DC9 DC981 3022081 WP VERTICAL STAB CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND FIN ASSEMBLY VERTICAL STABILIZER LOWER LEADING EDGE SKIN 5912188-35 ANGLE CRACK ON SKIN AT RIGHT FORWARD LOW ER HOLE AT ZFS=26.812. REMOVED DAMAGED SKIN AREA. FABRICATED REPLACEMENT SKIN AND SPLICE. INSTALLED SKIN AND SPLICE. (M) 2 L 7 2 4F A6WE 2002122000087 20021220 00087 WP 2002 12 20 GTIA021202 1 20021029 A 5342 ATTACH ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND VERTICAL STABILIZER RIGHT AND LEFT LOWER LEADING EDGE SKIN ATTACH ANGLES TO FUSELAGE, APPROX FS 1437, CRACKE D. REMOVED RIGHT AND LEFT SKIN ATTACH ANGLES. LOCATED AND DRILLED LEFT ANGLE. LOCATED AND DRILLED RIGHT ANGLE. INSTA LLED TWO NEW ANGLE. (M) 2 L 7 2 4F A6WE 2002122000088 20021220 00088 WP 2002 12 20 GTIA021203 1 20021018 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - SHARP CREASES FROM FS 520 TO FS 540 BETWEEN LONGERON 19R AND 20R REQUIRES REPAIR. CUT OUT DAMAGED SECTION OF SKIN . FABRICATED NEW SECTION OF SKIN, 5 DOUBLERS, 10 AND 9 FINGER DOUBLER. INSTALLED 1 FINGER DOUBLER. INSTALLED 10 EACH D OUBLER -5 FROM FS 520-570 BETWEEN LONGERONS 19R-20R-21R. INSTALLED 01 EACH NEW SECTION OF SKIN. (M) 2 L 7 2 4F A6WE 2002122000089 20021220 00089 WP 2002 12 20 GTIA021211 1 20021023 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND AFT ACC AREA FRAME T-CAP AT AFT SHROUD OF APU HAS CORROSION STATION 1401, 27L-27R. INTERCOSTAL AT FS 1380 T O 1401 BL13L IS FOUND TO BE OUT OF LIMITS. FABRICATED NEW INTERCOSTAL. FRAME AT FS 1394 RT BL 13R IS CRACKED. FABRICA TED NEW FRAME. REMOVED LOWER T-CAP. LOCATED AND DRILLED NEW LOWER T-CAP. FOUND CRACK ON RIGHT LEG OF VERTICAL BEAM. REMOVED VERTICAL BEAM. LOCATED AND DRILLED NEW RIGHT SIDE VERTICAL BEAM. INSTALLED T-CAP. INSTALLED VERTICAL BEAM. I NSTALLED RIGHT INTERCOSTAL. (M) 2 L 7 2 4F RT A6WE 2002122000090 20021220 00090 SO 2002 12 20 GLBA2002173 1 20021031 A 3233 ACTUATOR EMB 120 EMB120ER 3260203 SO LT MLG FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 96ZK 120096 LEFT MAIN GEAR WOULD NOT COME UP. R&R LEFT MAIN GEAR ACTUATOR 2 L 7 2 4T RT A31SO 2002122000091 20021220 00091 SO 2002 12 20 C2XA02TY179 1 20021219 A 5311 14523511401 FRAME EMB 145 EMB145LR 3260212 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 TYS, During a scheduled inspection, the first frame behind the cargo compartment (frame 68) has several gouges, Maintena nce burnished the gouges I/A/W-EMB145-SRM-51-10-02, CMP-51-21-04 and 05. Aircraft was released to service. 2 L 7 2 4T RT T00011AT 2002122000092 20021220 00092 CE 2002 12 20 GLBA2002174 1 20021102 A 5270 SWITCH BEECH 1900 1900D 1154162 CE CARGO DOOR DIRTY A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 96UX UE96 CARGO DOOR ANNUNCIATOR ILLUMINATED AT 250FL STAYED ILLUMINATED UNTIL SHORT FINAL, CLEANED AND ADJUSTED CARGO DOOR SWITCH OPS CHECK GOOD 2 L 7 2 4T RT A24CE 2002122000093 20021220 00093 CE 2002 12 20 GLBA2002175 1 20021101 A 5270 SWITCH BEECH 1900 1900D 1154162 CE PAX DOOR DIRTY A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 251GL UE251 CABIN DOOR UNSAFE ANNUNCICATOR ILLUMINATED, CLEANED UPPER SWITCH OPS CHECK GOOD 2 L 7 2 4T RT A24CE 2002122000094 20021220 00094 SO 2002 12 20 C2XA02TY180 1 20021219 A 5313 12020333047 STRINGER EMB 145 EMB145LR 3260212 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 TYS, During a scheduled inspection, External stringer 19L gouged at frame 54. Maintenance blended the gouge, fabricated a doubler, installed, primed and painted. I/A/W-EMB145-SRM-53-24-02, CMP-51-21-02, 04 and 06. The repair was satisfactor y and the Aircraft was released to service. 2 L 7 2 4T RT T00011AT 2002122000095 20021220 00095 CE 2002 12 20 GLBA2002176 1 20021101 A 6120 BETA SWITCH BEECH 1900 1900D 1154162 CE LT ENGINE MALFUNCTIONED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 94GL UE94 LEFT TORQUE, PROP, AND FUEL FLOW IND. FLUCTUATE IN FLT. R&R ENGINE BETA LEVER AND LOW PITCH SOLENOID BEARINGS 2 L 7 2 4T RT A24CE 2002122000096 20021220 00096 CE 2002 12 20 GLBA2002180 1 20021108 A 2422 INVERTER BEECH 1900 1900D 1154162 CE AC BUSS FAILED A GLBA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 NM 03 169GL UE169 LT AC BUSS INOPERATIV, R&R LT INVERTER 2 L 7 2 4T RT A24CE 2002122000097 20021220 00097 CE 2002 12 20 GLBA2002181 1 20021110 A 3030 WARNING LIGHT BEECH 1900 1900D 1154162 CE PITOT HEAT ILLUMINATED A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 184UX UE184 RT PITOT HEAT ANNUNCIATOR ILLUMINATED IN FLIGHT, OPS CHECK GOOD 2 L 7 2 4T RT A24CE 2002122000098 20021220 00098 CE 2002 12 20 GLBA2002183 1 20021119 A 3150 WARNING HORN BEECH 1900 1900D 1154162 CE AIRSPEED ACTIVATED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 219GL UE219 OVERSPEED WARNING SOUNDED ON CLIMB, SILENCED ON DECENT/SWAPPED LT & RT AIRSPEED INDICATORS FOR TROUBLE SHOOTING OPS CHEC K GOOD 2 L 7 2 4T RT A24CE 2002122000099 20021220 00099 SO 2002 12 20 GLBA2002184 1 20021121 A 3260 DOWNLOCK SENSOR EMB 120 EMB120ER 3260203 SO MLG FAILED A GLBA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 NM 03 293UX 120293 LDG SYSTEM LIGHTS WON'T COME ON, R&R DOWN LOCK PROXIMITY SENSOR OPS CHECK GOOD 2 L 7 2 4T RT A31SO 2002122000100 20021220 00100 SO 2002 12 20 GLBA2002186 1 20021126 A 3250 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO NLG STEERING FAILED A GLBA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 03 297UX 120297 ON TAXI INTO GATE, NOSE WHEEL STEERING INOPERATIVE. TUGGED AIRCRAFT TO GATE. R&R NOSE PROXIMITY SENSOR 2 L 7 2 4T RT A31SO 2002122000101 20021220 00101 CE 2002 12 20 GLBA2002187 1 20021127 A 7712 TRANSMITTER BEECH 1900 1900D 1154162 CE RT TORQUE IND MALFUNCTIONED A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 204GL UE204 RT N1 & TORQUE FLUCTUATIONS, R&R N1 TACH & TORQUE TRANSMITTER 2 L 7 2 4T RT A24CE 2003012100099 20030121 00099 NE 2003 1 21 GLBA2002188 2 20021128 A 7314 1143890425 PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 96UX 9526 UE96 LT LOW FUEL PRESS ANN ILLUM. REMOVED AND REPLACED LT LOW PRESS FUEL PUMP. 2 L 7 2 4T 4 T RT A24CE E26NE 2002122000102 20021220 00102 CE 2002 12 20 GLBA2002189 1 20021201 A 7330 WARNING LIGHT BEECH 1900 1900D 1154162 CE RT TANK COLLECTO ILLUMINATED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 226GL UE226 RT COLLECTOR TANK LOW ANNUNCIATOR ILLUMINATED ON ROLL, PENDING CORRECTIVE ACTION 2 L 7 2 4T RT A24CE 2002122000103 20021220 00103 CE 2002 12 20 GLBA2002190 1 20021206 A 2810 CAP BEECH 1900 1900D 1154162 CE RT WING LEAKING A GLBA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 NM 03 219GL UE219 FUEL LEAKING OUT OF RT OUTBOARD WING CAP, CHECKED FUEL CAP CHECK GOOD FUEL EXPANSION OVERFILL FORCED FUEL FROM CAP. 2 L 7 2 4T RT A24CE 2002122000104 20021220 00104 CE 2002 12 20 GLBA2002191 1 20021206 A 3246 WHEEL BEECH 1900 1900D 1154162 CE NLG VIBRATION A GLBA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 03 261GL UE261 A/C VIBRATING IN CLIMB, R&R NOSE WHEEL ASSY 2 L 7 2 4T RT A24CE 2003012100100 20030121 00100 SO 2003 1 21 GLBA2002192 1 20021206 A 2932 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO HYD SYSTEM FAULTY A GLBA O OTHER N FALSE WARNING CR CRUISE 1 NM 03 71GL 120071 RT LOW HYD PRESS LIGHT FLICKERS. REMOVED AND REPLACED PRESSURE SWITCH, OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2002122000105 20021220 00105 CE 2002 12 20 GLBA2002193 1 20021206 A 3610 SPLICE BEECH 1900 1900D 1154162 CE EVA TUBE DAMAGED A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 261GL UE261 LEFT BLEED AIR FAIL ANNUCIATOR ILLUMINATED, REPAIRED EVA TUBE SPLICE 2 L 7 2 4T RT A24CE 2002122000106 20021220 00106 2002 12 20 GLBA2002194 4 20021207 A 3416 CONNECTOR BEECH 1900 1900D 1154162 CE NR 1 ALTIMETER LOOSE A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 245GL UE245 NR 1 ALTIMETER FLAGGED, FOUND LOOSE CONNECTOR ON THE BACK OF NR 1 ALTIMETER RESECURED 2 L 7 2 4T RT A24CE 2002122000107 20021220 00107 CE 2002 12 20 GLBA2002195 1 20021207 A 7714 INDICATOR BEECH 1900 1900D 1154162 CE N1 READS HIGH A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 192GL UE192 RT N1 GAUGE READING TOO HIGH, R&R NR 2 N1 INDICATOR 2 L 7 2 4T RT A24CE 2002122000109 20021220 00109 CE 2002 12 20 GLBA2002197 1 20021211 A 3150 CIRCUIT BREAKER BEECH 1900 1900D 1154162 CE ANNUCIATOR PANEL FAILED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 219GL UE219 LOWER PORTION OF ANNUNCIATOR PANEL INOPERATIVE, R&R PANEL CIRCUIT BREAKER OPS CHECK GOOD 2 L 7 2 4T RT A24CE 2002122000110 20021220 00110 CE 2002 12 20 GLBA2002198 1 20021212 A 3150 WARNING LIGHT BEECH 1900 1900D 1154162 CE COCKPIT ILLUMINATED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 226GL UE226 ON TAKE OFF, RT COLLECTOR TANK LOW ANNUCIATOR ILLUMINATED, PENDING CORRECTIVE ACTION. 2 L 7 2 4T RT A24CE 2002122000111 20021220 00111 WP 2002 12 20 MEX2002341 1 20021115 A 2781 SENSOR DOUG DC9 DC987 3022087 WP L/E SLAT OUT OF ADJUST A ASMF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 23 216AM 49586 FLT 950 - MEX-MTY - AIRCRAFT SUSPENDED TAKEOFF AS A RESULT OF SLAT DISAGREE LIGHT TURN O BETWEEN 60 AND 70 KNOW. AIRCRA FT WAS SENT TO THE MAIN BASE. TECHNICAL PERSONNEL PERFORMED A BITE PROXIMITY SWITCH IAW MM 32-60-04, ALL CORRECT. LEFT SLAT ADVISOR SENSOR C WAS ADJUSTED IAW MM 27-80-06, TESTS CORRECT. ADDITIONALLY HIGH ENERGY STOP CHECK WAS PERFORMED I AW MM 05-45-00, ALL CORRECT. (M) 2 L 7 2 4F RT A6WE 2003030300096 20030303 00096 EA 2003 3 3 SWIA200211589 1 20021111 A 5411 FRAME CNDAIR CL600 CL6002B19 1900309 EA RT PYLON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 FS 718.0 RT PYLON FAIRING ATTACH POINT FRAME CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED AREA IAW CRJ R EO 601R-53-61-193 REV A. NDT-HFEC CARRIED OUT IAW CLIENT REQUEST. NO CRACKS NOTED. 2 L 7 2 4F RT A21EA 2002122000112 20021220 00112 EA 2002 12 20 COMA0260722 1 20021217 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 713CA 7245 FLIGHT 5053 GEAR DISAGREE WARNING MESSAGE.COULD NOT DUPLICATE EXTENSION AND RETRACTION CHECKS ALL NORMAL. HYDRAULIC PUM PS AND RESERVOIR REPLACED FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 2002122000113 20021220 00113 EA 2002 12 20 COMA0260723 1 20021217 A 3620 20035008067 CONTROL BOX CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 916CA 20073 7014 FLIGHT 5393 ANTI ICE DUCT WARNING.REPLACED THE BLEED AIR LEAK CONTROL UNIT. 2 L 7 2 4F RT A21EA 2002122000114 20021220 00114 SO 2002 12 20 C2XA02TY183 1 20021219 A 5320 123007729001 CHANNEL EMB 145 EMB145LR 3260212 SO DISTORTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 TYS, During a scheduled inspection a support channel between the cockpit floor beam and frame 13L was found distorted. M aintenance removed and replaced the channel. I/A/W-EMB-145-SRM-53-12-10 and 51-40-02. The repair was satisfactory and th e aircraft was released to service. 2 L 7 2 4T RT T00011AT 2003011600185 20030116 00185 EA 2003 1 16 COMA0260721 1 20021217 A 3222 16100111 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 739CA 7273 FLIGHT 5857 GEAR DISAGREE WARNING. REPLACED THE NLG OLD STRUT ASSY. 2 L 7 2 4F RT A21EA 2002122000115 20021220 00115 NM 2002 12 20 TSAA0233219 1 20021029 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 3 AND NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4F RT A16WE 2002122000116 20021220 00116 SO 2002 12 20 GLBA2002199 1 20021212 A 3233 ACTUATOR EMB 120 EMB120ER 3260203 SO MLG FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 96ZK 120096 LANDING GEAR FAILED TO RETRACT AFTER TAKE OFF, REPLACED LT MLG UPLOCK ACTUATOR OPS CHECK GOOD 2 L 7 2 4T RT A31SO 2002122000117 20021220 00117 NM 2002 12 20 TSAA0233220 1 20021028 A 3350 9221009 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED LEFT OVERWING IDENTICAL POWER PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2002122000118 20021220 00118 EU 2002 12 20 022001 1 20021220 A 2610 1734362450 FIRE DETECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE SATURATED A UHLA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 NE 03 123CQ 123 360 DRG486887 FLT 4463 AFTER TAKEOFF LEFT ENG TAIL PIPE HOT LIGHT ILLUMINATED PILOT RETURNED TO FIELD, LIGHT EXTINGUISHED ON LANDING, MAINTENANCE DISPATCHED TO INSPECT AC.AC SET ON GROUND DURING LIGHT RAIN AND PART APPEARED TO BE WET, CLEANED CANNON PLUG S AND FOUND MOISTURE, PERFORMED GROUND RUNS, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002122000119 20021220 00119 CE 2002 12 20 GLBA2002200 1 20021212 A 5270 WARNING LIGHT BEECH 1900 1900D 1154162 CE PAX DOOR ILLUMINATED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 249GL UE249 CABIN DOOR LIGHT ILLUMINATED IN FLIGHT, CLEANED & ADJUSTED OPS CHECK GOOD 2 L 7 2 4T RT A24CE 2002122000120 20021220 00120 SO 2002 12 20 C2XA02TY184 1 20021219 A 5755 14568750415 SPEED BRAKE EMB 145 EMB145LR 3260212 SO DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 TYS, During a scheduled inspection, composite damage was found to leading edge of left speed brake. Maintenance repaired the damage. I/A/W-EC5750-01190. The repair was satisfactory and the aircraft was released to service. 2 L 7 2 4T RT T00011AT 2002122000121 20021220 00121 NM 2002 12 20 UIEA02019 1 20020601 A 5753 65B1706870 FLAP TRACK BOEING 747 747341 13848AM NM T/E FLAP CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 51111 23395 DURING CURRENT D-CHECK AT SIAEC, THE NR 5 FLAP TRACK OUTBOARD LOWER FLANGE IN THE MID SECTION WAS FOUND WITH LEVEL 1 COR ROSION FOR APPROX 10 INCHES. CORROSION MACHINED OUT AND BLENDED MAINTAINING A 100 TO 1 BLEND RATION TO ENSURE A SMOOTH FLAT SURFACE. AREA MAGNETIC PARTICLE INSPECTED TO ENSURE NO CRACKING DURING PROCESS. NO DEFECTS FOUND. AREA MEASURED AND RECORDED. SURFACE TREATED AND REFINISHED. REWORK PERFORMED IAW SOPM 20-10-01/02. (M) 2 L 7 4 4F RT A20WE 2002122000122 20021220 00122 NM 2002 12 20 USAA020402 1 20021025 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 47194 23317 PIT - FOUND RUDDER WITH DELAMINATION, STATION 0.00 RT, 1.5 LEFT, 121.0 LEFT, 174.9 RT, 200.0 RT. REPAIRED WITH WET LAYU P USING SRM 51-70-17, 51-60-00 PER EA 75136. (M) 2 L 7 2 4F RT A16WE 2002122000123 20021220 00123 NM 2002 12 20 USAA020403 1 20021024 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 48412 23700 PIT - FOUND SKIN CRACKED 1 INCH LONG, STATION 380 B/L 0. INSTALLED REPAIR DOUBLER PER EA 75166 AND TYPICAL REPAIR 53-30 -07. (M) 2 L 7 2 4F RT A16WE 2002122000124 20021220 00124 NM 2002 12 20 USAA020404 1 20021024 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 46532 23743 PIT - FOUND SKIN CRACKED 2.25 INCH, STATION 967 STRINGER 21L. CUT OUT DAMAGE, INSTALLED DOUBLER PER SRM 53-00-0 PAGE 20 6. (M) 2 L 7 2 4F RT A16WE 2002122000125 20021220 00125 NM 2002 12 20 USAA020405 1 20021010 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 48477 22957 PIT - FOUND BEAM WITH CHAFFING 1 INCH AREA, TOP FLOOR BEAM, STATION 520 OUTBOARD LEFT OUTBOARD SEAT TRACK. BLENDED AND INSALLED STRAP PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 2002122000126 20021220 00126 NM 2002 12 20 USAA020406 1 20021028 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 48447 22957 CLT - FOUND STRINGER CRACKED .375 INCH, STATION 663.75 STRINGER 2 RIGHT. CUT OUT DAMAGE, INSTALLED DOUBLERS PER EA 7501 3, SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2002122000127 20021220 00127 SO 2002 12 20 C2XA02TY185 1 20021219 A 5530 14540881001 BUSHING EMB EMB 145 EMB145LR 3260212 SO LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 TYS, During a scheduled inspection, the left hand vertical stab spherical bushings where found loose. Maintenance reamed the hole for oversized bushing and alodined and installed bushings. I/A/W-EC5510-001045. The repair was satisfactory an d the aircraft was released to service. 2 L 7 2 4T RT T00011AT 2002122000128 20021220 00128 SO 2002 12 20 C2XA02TY186 1 20021219 A 5530 14540881001 BUSHING EMB EMB 145 EMB145LR 3260212 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 TYS, During a scheduled inspection, the right hand vertical stab spherical bushings where found gouged. Maintenance ream ed the hole for oversized bushing and alodined and installed bushings. I/A/W-EC5510-001045. The repair was satisfactory and the aircraft was released to service. 2 L 7 2 4T RT T00011AT 2002122000129 20021220 00129 CE 2002 12 20 GLBA2002201 1 20021214 A 2120 O-RING BEECH 1900 1900D 1154162 CE CABIN PRESSURE FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 100UX UE100 CLIMBING THROUGH 16000 FT, ALTITUDE HIGH ANNUNCIATOR ILLUMINATED, R&R O-RINGS AND RESECURED CLAMPS OPS CHECK GOOD 2 L 7 2 4T RT A24CE 2002122000130 20021220 00130 NM 2002 12 20 USAA020407 1 20021025 A 5320 CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 48447 22957 PIT - FOUND CLIPS CRACKED .375 INCH, IN TIE CLIPS 360 AND 380, 8 LEFT. SPLICED IN STRINGER AND REPLACED TIE CLIPS PER S RM 53-00-03 FIG 203. (M) 2 L 7 2 4F RT A16WE 2002122000131 20021220 00131 NM 2002 12 20 USAA020408 1 20021020 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 48447 22957 PIT - FOUND STRINGER CRACKED .5 INCH, STATION 807-S9L. DAMAGE CUT OUT AND INSTALLED DOUBLERS PER TYPICAL REPAIR 53-10-2 0. (M) 2 L 7 2 4F RT A16WE 2002122000132 20021220 00132 NM 2002 12 20 USAA020409 1 20021028 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 49066 23311 PIT - FOUND SKIN CRACKED 2.4375 INCH, RIGHT SIDE STATION 727E AT STRINGER 18 RIGHT. SKIN DOUBLER INSTALLED PER SRM 53-0 0-01, FIG 201. (M) 2 L 7 2 4F RT A16WE 2002122000133 20021220 00133 NM 2002 12 20 QXEA0201828 1 20021030 A 2720 2379003001 REGULATOR DHAV DHC8 DHC8202 2809007 NM RUDDER MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 NM 09 364PH 7870 5 524 PDX-RETURNED TO FIELD FOR NR 1 RUDDER HYDRAULIC, RUDDER FULL PRESSURE AND RUDDER PRESSURE CAUTION LIGHTS. HYDRAULIC PRE SSURE WAS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RUDDER PRESSURE REGULATOR AND ISOLATION. OPE RATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002122000134 20021220 00134 NM 2002 12 20 QXEA0201829 1 20021031 A 3260 WARNING SYSTEM BOMBDR DHC8 DHC8401 1390041 NM LANDING GEAR MALFUNCTIONED A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 406QX 4048 GEG-WEIGHT ON WHEELS CAUTION LIGHT CYCLES ON AND OFF WHILE IN FLIGHT. AFTER GEAR DOWN, STILL CYCLED ON AND OFF. REPAIR ED IAW AMM 32-61-06. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002122000135 20021220 00135 EA 2002 12 20 QXEA0201830 1 20021022 A 2810 CC670624247 BRACKET CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM MISINSTALLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 PDX- BRACKET NUMBER IS INSTALLED IN THE REVERSE POSITION. REPARIED IAW HORIZON AIR EO R-28-82 "A". 2 L 7 2 4F RT A21EA 2002122000136 20021220 00136 NM 2002 12 20 QXEA0201848 1 20021105 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 512 PDX - CARGO DOOR MID BEAM TO SKIN RIVET BUCKTAIL DAMAGED. REPAIRED IAW DHC-8 SRM 51-40-11, SRM 51-20-36 AND SRM 51-20-4 1. 2 H 7 2 4T RT A13NM 2002122000137 20021220 00137 NM 2002 12 20 QXEA0201862 1 20021025 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - LEFT HAND FLAP TOP SKIN DEEP CHAFE LINE EXISTS AT STATION 238.4. REPAIRED IAW HORIZON AIR EA 6-57-77 AND EO DH8S- 57-0620. 2 H 7 2 4T RT A13NM 2002122000138 20021220 00138 NM 2002 12 20 QXEA0201863 1 20021024 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - LEFT HAND OUTBOARD FLAP TOP SKIN DEEP CHAFE LINE EXISTS AT STATION 280.2. REPAIRED IAW DHC-8 Q400 SRM 57-52-30-94 0-001. 2 H 7 2 4T RT A13NM 2002122000139 20021220 00139 NM 2002 12 20 QXEA0201867 1 20021026 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - RIGHT HAND INBOARD FLAP HAS A CHAFE ON THE TOP SKIN INBOARD END. REPAIRED IAW DHC-8 Q400 SRM 57-51-30-740-001. 2 H 7 2 4T RT A13NM 2002122000140 20021220 00140 NM 2002 12 20 QXEA0201868 1 20021023 A 5420 FITTING BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - LEFT HAND NACELLE ONE HOLE IN BOTTOM FLANGE OF BRACE FITTING IS OVERSIZED. REPAIRED IAW HORIZON AIR EA 6-54-140 A ND WVACDH8S-54-0627. 2 H 7 2 4T RT A13NM 2002122000141 20021220 00141 NM 2002 12 20 QXEA0201869 1 20021024 A 5420 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - LEFT NACELLE FIVE HOLES SHOW INDICATION DURING EDDY CURRENT INSPECTION ARE OVERSIZED. REPAIRED IAW HORIZON AIR EA 6-54-142A AND WVAC EO DH8S-54-0627A. 2 H 7 2 4T RT A13NM 2002122000142 20021220 00142 NM 2002 12 20 QXEA0201870 1 20021028 A 5420 FITTING BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE ACTIVATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - RIGHT HAND NACELLE OUTBOARD SIDE FITTING SECOND HOLE INBOARD SHOWS POSITIVE INDICATION FOR NDT. FINAL HOLE DIAMETE R .435. REPAIRED IAW HORIZON AIR EA 6-54-140A AND WVAC EO DH8S-54-0627A. 2 H 7 2 4T RT A13NM 2002122000143 20021220 00143 NM 2002 12 20 QXEA0201872 1 20021027 A 2750 FLAP BOMBDR DHC8 DHC8401 1390041 NM LT WING FOD A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - LEFT HAND OUTBOARD FLAP FULL OF FOD. REPAIRED IAW DHC-8 Q400 SRM 51-42-45-330-80. 2 H 7 2 4T RT A13NM 2002122000144 20021220 00144 NM 2002 12 20 QXEA0201873 1 20021021 A 5230 FITTING BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - CARGO DOOR AFT TOP FITTING REQUIRE REPLACEMENT. REMOVED AND REINSTALLED IAW HORIZON AIR EO 6-52-108, ITEM 23. 2 H 7 2 4T RT A13NM 2002122000145 20021220 00145 NM 2002 12 20 QXEA0201874 1 20021021 A 5230 FITTING BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 CKB - AFT BAGGAGE BAY CARGO DOOR FORWARD TOP FITTINGS REQUIRE REPLACEMENT. REPLACED IAW HORIZON AIR EAO 6-52-108, ITEM 23. 2 H 7 2 4T RT A13NM 2002122000146 20021220 00146 NM 2002 12 20 QXEA0201875 1 20021107 A 1430 SNAP RING BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR DEFECTIVE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 405QX 4047 SEA - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKE OFF THE AIRCRAFT DEPRESSURIZED AT 7000 FEET. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE SNAP RING ON THE VENT DOOR SHAFT OF THE FORWARD CARGO DOOR. OPERATIONAL CHECKS WERE PERFORME D AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002122000147 20021220 00147 WP 2002 12 20 ZW0A0212603 1 20021219 A 3350 58541 CABLE DOUG DC9 DC982 3022082 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 911TW 49182 THE FIRST CLASS CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE CABLE AND DRIED MOISTURE FROM THE TRACK. CHECK-C 8- 15-02 STL. --CLOSED-- 2 L 7 2 4F A6WE 2002122000148 20021220 00148 EA 2002 12 20 COMA0260724 1 20021219 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 995CA 7229 FLIGHT 5226 FLAPS FAILED WHEN SELECTED TO 8 DEGREES.RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002122000149 20021220 00149 EA 2002 12 20 COMA0260725 1 20021219 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 927CA 5105 7031 FLIGHT 5159 GEAR DISAGREE WARNING AFTER T/O.REPLACED THE PSEU 2 L 7 2 4F RT A21EA 2002122000150 20021220 00150 NM 2002 12 20 USAA020410 1 20021021 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 49066 23311 PIT - FOUND SKIN CRACKED 1.24 INCH, RIGHT SIDE STATION 747 AT STRINGER 18 RIGHT. SKIN DOUBLER INSTALLED PER SRM 53-00-0 1, FIG 201. (M) 2 L 7 2 4F RT A16WE 2002122000151 20021220 00151 NM 2002 12 20 USAA020440 1 20021101 A 5240 SKIN BOEING 757 757225 1384959 NM L4 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 57344 22199 CLT - FOUND INNER SKIN CRACKED .250 INCH, ABOVE LOWER HINGE BOX, L4 DOOR INNER SKIN 1661. INSTALLED REPAIR DOUBLER ON I NNER DOOR SKIN PER EA 86643. (M) 2 L 7 2 4F RT A2NM 2002122000152 20021220 00152 NM 2002 12 20 USAA020441 1 20021101 A 5753 SKIN BOEING 757 757225 1384959 NM T/E FLAP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 22199 CLT - FOUND SKIN CRACKED .75 INCH, INBOARD TRAILING EDGE FLAP RIGHT WING ABOVE NR 6 FLAP TRACK LINKAGE. INSTALLED REPAI R STRAP AFTER DAMAGE AREA TRIMMED PER EA 86716. (M) 2 L 7 2 4F RT A2NM 2002122000153 20021220 00153 NM 2002 12 20 USAA020442 1 20021009 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 57344 22199 CLT - FOUND CHORD CRACKED .125 INCH, UPPER CHORD INTERCOSTAL AT BL 0, BS 1420-1440. FABRICATED AND INSTALLED NEW ANGLE PER SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 2002122000154 20021220 00154 EA 2002 12 20 SWIA200211592 1 20021111 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA LEFT FORWARD PRE CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 5 CRACKS FOUND RADIATING OUT FROM PARK BRAKE BULKHEAD FITTING, LEFT FORWARD PRESSURE BULKHEAD. FOUND DURING C CHECK INSPECTION. NDT-HFEC CARRIED OUT IAW CLIENT REQUEST. FIVE (5) CRACKS FOUND TO BE RADIATING FROM PARK BRAKE BULKHEAD TH ROUGH FITTING CUTOUT IN LH FWD PRESSURE BULKHEAD. NDT-HFEC CARRIED OUT IAW 601R-53-11-362. NO CRACKS NOTED. REPAIRED IAW REO 601R-53-11-362 REV NC, RII 53-401. 2 L 7 2 4F RT A21EA 2002122000155 20021220 00155 NM 2002 12 20 USAABB02191 1 20021112 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 624AU 27245 BWI - FOUND FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE AT ROWS 1 AND 13. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2002122000156 20021220 00156 NM 2002 12 20 QXEA0202205 1 20021219 A 5270 HANDLE BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 A QXEA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 NM 09 406QX 4048 SEA - FLIGHT 2312 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A MAIN BAGGAGE DOOR LIGHT. MAINTENAN CE INSPECTED AND FOUND THE AFT BAGGAGE DOOR HANDLE RELEASE LOCK NOT FULLY ENGAGED. A FUNCTIONAL CHECK OF THE AFT BAGGAGE DOOR CHECKED GOOD. THE LOCK RELEASE AND HANDLE WAS VERIFIED TO OPERATE PROPERLY. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002122000157 20021220 00157 EU 2002 12 20 USAASA02095 1 20021104 A 3350 LIGHT AIRBUS 320 A320214 3930316 EU CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 EA 19 113UW 1141 TPA - THE EMERGENCY LIGHTS FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE SECURED LOOSE CONNECTOR ON R-1 DOOR EMERGENCY E SCAPE SLIDE. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2002122000158 20021220 00158 EU 2002 12 20 USAASA02096 1 20021113 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 108UW 1061 CLT - FOUND THE EMERGENCY LIGHTS SYSTEM FAILED THE OPERATIONAL TEST. MAINTENANCE REPLACED AN EPSU. OPERATIONALLY CHECK S OK. (M) 2 L 7 2 4F RT A28NM 2002122000159 20021220 00159 WP 2002 12 20 GTIA021166 1 20020926 A 5313 STRINGER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FORWARD CARGO PIT STRINGER 29L CORRODED AT FS 376-446. FORWARD CARGO FS 427-446 STRINGER 29L CORRODED. FOR WARD CARGO FS 408-427 STRINGER 29L CORRODED. FORWARD CARGO STRINGER 29L CORRODED FS 370-389. FORWARD CARGO FS 389-408 STRINGER 29L CORRODED. INTERCOSTAL FOUND TO BE OUT OF LIMITS STRINGER 29L STATION 446 TO BE OUT OF LIMITS. FORMED NEW INTERCOSTAL. CUT OUT EXISTING AREA. FABRICATED FORWARD SPLICE. INSTALLED NEW SPLICE AT STATION 416. FABRICATED NEW S PLICE FOR STATION 446-460. INSTALLED INTERCOSTAL. INSTALLED NEW LONGERON SECTION FS 416-455. (M) 2 L 7 2 4F RT A6WE 2002122000160 20021220 00160 EA 2002 12 20 QXEA0201876 1 20021105 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 614QX 10049 PDX - THIS SDR IS BEING REPORTED PER REQUEST OF FSDO-09 ASI. FORWARD CARGO BAY CENTER CHIMNEY ASSEMBLY IS DAMAGED. MAINT ENANCE REMOVED AND REPLACED CENTER CHIMNEY IN THE FORWARD CARGO BAY. OPERATIONAL CHECK AND SECURITY IS GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002122000161 20021220 00161 NM 2002 12 20 QXEA0201877 1 20021102 A 2611 SMOKE DETECTOR BOMBDR DHC8 DHC8401 1390041 NM LAVATORY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 406QX 4048 PDX - AFTER TAKE-OFF, THE LAVATORY SMOKE DETECTOR WENT OFF. THE FLIGHT ATTENDANT VERIFIED THAT IT WAS ON, BUT NO FIRE O R SMOKE WAS NOTICED. THE DETECTOR SILENCED AFTER APPROXIMATELY 2 MINUTES. THE UNIT TESTED OK. MAINTENANCE INSPECTED T HE DETECTOR AND IT TESTED GOOD IAW-8 (400) 26-12-11, TASK 26-12-11-710-801. THE AIRCRAFT WAS RETURNED TO SERVICE. NO P ARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2002122000162 20021220 00162 NM 2002 12 20 QXEA0202206 1 20021218 A 3240 216051 BRAKE BOMBDR DHC8 DHC8401 1390041 NM ZONE 700 SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 09 411QX 983 983 4055 PDX - FLIGHT 2379 - GROUND CREW NOTICED AND REPORTED THAT THE # 1 AND # 2 WHEEL/TIRE ASSEMBLIES WERE SMOKING AND SPARKIN G DURING PARKING. MAINTENANCE INSPECTED AND REPLACED BOTH THE # 1 AND 2 WHEEL ASSEMBLIES AND ASSOCIATED BRAKES. OPERATIO NAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002122000163 20021220 00163 NM 2002 12 20 QXEA0201888 1 20021109 A 5210 MECHANISM BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 SEA - THE FORWARD CABIN DOOR HANDLE IS HARD TO OPERATE. MAINTENANCE INSPECTED THE DOOR HANDLE MECHANISM AND LUBRICATED SAME IAW AMM 51-22-00-720-801. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002122000164 20021220 00164 NM 2002 12 20 QXEA0201889 1 20021109 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 364PH 524 SEA-4TH FLOOR PATH LIGHT FROM BACK OF CABIN INOPERATIVE. REMOVED AND REPLACED 4TH EMERGENCY PATH LIGHT STRIP FROM BACK OF CABIN. EMERGENCY LIGHTS OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002122000165 20021220 00165 NM 2002 12 20 QXEA0201890 1 20021110 A 2434 11524002 GENERATOR BOMBDR DHC8 DHC8401 1390041 NM NR 2 FAILED A QXEA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 09 410QX 772 772 4053 GEG- NR 2 DC GENERATOR CAUTION LIGHT ILLUMINATED. COMPLIED WITH EMERGENCY ABNORMAL CHECKLIST. BOTH LEFT AND RIGHT TRU CAUTION LIGHTS WERE NOT ILLUMINATED. REMOVED AND REPLACED NR 2 DC GENERATOR. OPERATIONAL CHECK GOOD. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002122000166 20021220 00166 EA 2002 12 20 QXEA0201891 1 20021105 A 2530 ODOR CNDAIR CL600 CL6002C10 1390015 EA CABIN DETECTED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 601QX 10009 BOI-FOUL ODOR COMING FROM GALLEY AREA AND FORWARD CABIN. SMELL REPORTED AS SMELLY SOCKS OR VOMIT. DEODORIZED BY FLEET SERVICE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2002122000167 20021220 00167 NM 2002 12 20 QXEA0201901 1 20021110 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 12 HAS PAINT MISSING WHERE SEAT ATTACHES AND SEAT LOCKING POINTS ARE MARRED BY S EAT AT STATION 514 AND STATION 529. REPAIRED IAW RD 8-53-3644 AND RD 8-51-102. 2 H 7 2 4T RT A13NM 2002122000168 20021220 00168 NM 2002 12 20 QXEA0201902 1 20021110 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 11 AT STATION 435 HAS LIGHT PITTING CORROSION AND MARRED EDGES AT LOCKING POINTS . REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-51-102. 2 H 7 2 4T RT A13NM 2002122000169 20021220 00169 NM 2002 12 20 QXEA0201903 1 20021104 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 2 HAS MARRED EDGES, LIGHT CORROSION AND MISSING PAINT AT STATION X484. REPAIRED IAW RD 8-53-1342 AND DHC-8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002122000170 20021220 00170 NM 2002 12 20 QXEA0201904 1 20021104 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SEAT TRACK NR 6 HAS CORROSION IN CHANNEL AT STATION X544.000. REPAIRED IAW RD 8-53-4963 AND DHC-8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002122000171 20021220 00171 NM 2002 12 20 QXEA0201905 1 20021108 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SEAT TRACK NR 7 HAS CORROSION ON TOP EDGES AT LOCATIONS X187.5, X207, X213.5 AND X222. REPAIRED IAW DHC-8 SRM 51- 40-11. 2 H 7 2 4T RT A13NM 2002122000172 20021220 00172 NM 2002 12 20 QXEA0201906 1 20021104 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SEAT TRACK NR 8 HAS SURFACE CORROSION BETWEEN LOCATIONS X484 AND X488.5. REPAIRED IAW RD 8-53-1339 AND SRM 51-20-3 6. 2 H 7 2 4T RT A13NM 2002122000173 20021220 00173 NM 2002 12 20 QXEA0201907 1 20021104 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SEAT TRACK NR 5 GOUGED AT LOCATION X436.5. REPAIRED IAW SRM 53-00-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002122000174 20021220 00174 NM 2002 12 20 QXEA0201908 1 20021104 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SEAT TRACK NR 5 HAS SURFACE CORROSION BETWEEN LOCATIONS X483 AND X494. REPAIRED IAW RD 8-53-1339 AND DHC-8 SRM 51 -20-36. 2 H 7 2 4T RT A13NM 2002122000175 20021220 00175 NM 2002 12 20 QXEA0201909 1 20021104 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SEAT TRACK NR 5 HAS SURFACE CORROSION BETWEEN LOCATIONS X501 AND X505. REPAIRED IAW RD 8-53-1339 AND DHC-8 SRM 51 -20-36. 2 H 7 2 4T RT A13NM 2002122000176 20021220 00176 NM 2002 12 20 QXEA0201910 1 20021104 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SEAT TRACK NR 5 HAS SURFACE CORROSION BETWEEN STATIONS X515 AND X519. REPAIRED IAW RD 8-53-1339 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002122000177 20021220 00177 NM 2002 12 20 QXEA0201911 1 20021103 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SEAT TRACK NR 5 HAS SURFACE CORROSION AT LOCATION X86.5. REPAIRED IAW RD 8-53-1339 AND DHC-8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2002122000178 20021220 00178 NM 2002 12 20 QXEA0201912 1 20021110 A 5730 DOUBLER DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SCRATCH IN LOWER WING SKIN DOUBLER AT STATION YW174.5 JUST AFT OF FORWARD SPAR. REPAIRED IAW DHC-8 SRM 57-10-21 A ND SRM 51-20-26, PAGE 7. 2 H 7 2 4T RT A13NM 2003012100102 20030121 00102 CE 2003 1 21 GLBA2002202 1 20021215 A 5270 SWITCH BEECH 1900 1900D 1154162 CE PAX DOOR OUT OF ADJUST A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 249GL UE249 AIR RETURN, CABIN DOOR ANNUN ILLUM AFTER T/O. CLEANED AND ADJUSTED DOOR SWITCH. 2 L 7 2 4T RT A24CE 2003012100110 20030121 00110 CE 2003 1 21 GLBA2002204 1 20021216 A 2130 1143641407 PRINTED CKT BOAR BEECH 1900 1900D 1154162 CE CABIN PRESSURE FAULTY A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 179GL 7925 UE179 LT ENVIRO FAIL ILLUM ON TAKEOFF ROLL. REMOVED AND REPLACED A317 PCB, OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2003012100111 20030121 00111 CE 2003 1 21 GLBA2002205 1 20021216 A 7331 MS3116F84S CONNECTOR BEECH 1900 1900D 1154162 CE PWA R2000 2SD13G 52021 NE FUEL FLOW DEFECTIVE A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 184UX UE184 RT FUEL INDICATOR READS ZERO. REMOVED AND REPLACED RT FUEL FLOW TRANSMITTER CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4T 4 R RT A24CE E230 2003020400158 20030204 00158 CE 2003 2 4 GLBA2002206 1 20021218 A 3150 PIN BEECH 1900 1900D 1154162 CE WARNING SYSTEM DEFECTIVE A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 226GL UE226 RT COLLECTOR TANK LOW ANNUN ILLUM ON TAKEOFF ROLL. REMOVED AND REPLACED SOCKET CONTACTS ON PINS 1, 2 & 3 ON ANNUN POWER SOURCE PCB CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2002122300001 20021223 00001 CE 2002 12 23 GLBA202182 1 20021118 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 211GL UE211 IN-TRANSIT LIGHT STAYS ON WITH GEAR UP, R&R LT UP-LOCK SWITCH 2 L 7 2 4T RT A24CE 2002122300002 20021223 00002 SO 2002 12 23 C2XA02CL222 1 20021105 A 3350 78241 LIGHT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16525 145403 THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON GALLEY PARTITION WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002122300003 20021223 00003 SO 2002 12 23 C2XA02CL247 1 20021213 A 3350 66368 LIGHT EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 13956 145078 THE CREW REPORTED EMERGENCY AISLE PATH LIGHT STRIP AT ROW 17,18 AND 19 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERG ENCY AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2002122300004 20021223 00004 SO 2002 12 23 C2XA02CL248 1 20021214 A 2750 3631001005 FCU EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL TE FLAPS INTERMITTENT A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 13995 145295 FLIGHT NR 3109, THE CREW REPORTED THE FLAPS WOULD NOT EXTEND OUT OF (0) DEGREES FOR LANDING. THE CREW DECLEARED A EMERG ENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. THE AIR CRAFT WAS TEST FLOWN AND THEN RELEASED FOR SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002122300005 20021223 00005 SO 2002 12 23 C2XA02CL249 1 20021213 A 7500 14521182405 TUBE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BLEED AIR CRACKED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 18982 145223 FLIGHT NR3713 THE CREW REPORTED A NR 1 BLEED LEAK AFTER TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCID ENT.MAINTENANCE INSPECTED AND FOUND THE NR 1 ENGINE BLEED AIR TUBE ASSEMBLY CRACKED. MAINTENANCE REPLACED THE NR 1 BLEE D TUBE ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002122300006 20021223 00006 SO 2002 12 23 C2XA02CL250 1 20021218 A 3350 66903 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 IAH FLIGHT 3650, THE CREW REPORTED THE AISLE PATH LIGHTING WAS INOPERATIVE AT THE MAIN CABIN DOOR. MAINTENANCE INSPECTE D AND REPLACED THE AISLE PATH LIGHTING STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002122300007 20021223 00007 SO 2002 12 23 C2XA02IA246 1 20021129 A 2131 22250N030201 CONTROLLER EMB 135 EMB135LR 3260305 SO DIGITAL PRESSURE INOPERATIVE A C2XA G O2 MASK DEPLOYED O OTHER CR CRUISE 1 SW 27 17524 145399 DURING FLIGHT AUTO PRESSURIZATION FAILED. MANUAL WOULD NOT STOP CABIN CLIMBING TO 14,000 FEET. MASKS DROPPED. MAINTEN ANCE REMOVED AND REPLACED THE DIGITAL PRESSURE CONTROLLER, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002122300008 20021223 00008 SO 2002 12 23 C2XA02IA247 1 20021130 A 3350 66367 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17984 145246 ONE SECTION OF EMERGENCY LIGHTS NOT WORKING. MAINTENANCE RELEASED IAW MEL. MAINTENANCE REMOVED AND REPLACED THE EMERG ENCT LIGHT STRIP, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122300009 20021223 00009 SO 2002 12 23 C2XA02IA248 1 20021205 A 3020 14531128402 DUCT EMB 145 EMB145ER 3260211 SO NR 2 ENGINE DAMAGED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 14933 145018 FLIGHT 3789, THE CREW NOTED A FIRE INDICATION NR 2 ENGINE AFTER TAKEOFF. THE CREW SHUTDOWN NR 2 ENGINE, DECLARED EMERGE NCY, AND, RETURNED TO HSV, AND, LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ANTI ICE BLEE D DUCT, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, 2 L 7 2 4F RT T00011AT 2002122300010 20021223 00010 EU 2002 12 23 C2XA02IA249 1 20021208 A 3230 1005383Y00 CONTROL VALVE AEROSP ATR42 ATR42320 8680930 EU MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 93840 271 UPON GEAR RETRACTION AFTER TAKEOFF, THREE GREEN GEAR LIGHTS LIT UP SIMULTANEOUSLY WITH THREE RED UNLOCK LIGHTS ON BOTH O VERHEAD PANEL, AND, MAIN INSTRUMENT PANEL, AND, THE GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED, AND,REPLACED THE LANDI NG GEAR CONTROL VALVE, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. 2 H 7 2 4T RT A53EU 2002122300011 20021223 00011 SO 2002 12 23 C2XA02IA250 1 20021214 A 3350 1980101 LIGHT EMB 145 EMB145 3260210 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18114 145665 DURING PREFLIGHT THE CREW NOTED THAT THE SERVICE DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. MAINTENANCE CONNECTED THE E MERGENCY LIGHT TO THE CONNECTOR, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002122300012 20021223 00012 SO 2002 12 23 C2XA02IA252 1 20021214 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18557 145596 THE CREW NOTED THAT THERE WAS A STRONG SMELL OF DEICE FLUID IN THE CABIN. CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT, AND, PLACED THE RECIRCULATION FAN ON MEL, AND, SECURED THE CIRCUIT BREAKER IN THE OPEN POSITION. MAINTENANCE REMOVED AN D REPLACED THE RECIRCULATION FAN, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122300013 20021223 00013 SO 2002 12 23 C2XA02SH123 1 20021109 A 5310 14521700007 BEAM EMB 145 EMB145ER 3260211 SO CABIN CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14933 145018 DURING C CHECK LT OMEGA BEAM WAS FOUND TO HAVE A CRACK ON RIVET AT FRAME 22. MAINTENANCE REPAIRED CRACK ON RIVET IAW CO NTINENTAL EXPRESS EC 5320-01081. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002122300014 20021223 00014 SO 2002 12 23 C2XA02SH124 1 20021112 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13914 145430 DURING C CHECK CENTER STRAP BETWEEN FRAMES 18 AND 13 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFEC TED STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122300015 20021223 00015 SO 2002 12 23 C2XA02SH126 1 20021117 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13914 145430 DURING C CHECK EMERGENCY LIGHT ON PANEL 191 HL WAS FOUND INOPERATIVE. MAINTENANCE REMOVED ANT REPLACED BULB OF AFFECTED LIGHT. OPERATIONAL CHECKED GOOD IAW EMB 145 AMM 33-50-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122300016 20021223 00016 SO 2002 12 23 C2XA02SH129 1 20021121 A 5330 14527605001 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16919 145393 DURING C CHECK, A DENT WAS FOUND JUST AFT OF FRAME 12A BY STRINGER 18 LT. MAITENTANCE REPAIRED DENT IAW CONTINENTAL EXPR ESS EC 5330-01206. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122300017 20021223 00017 SO 2002 12 23 C2XA02SH131 1 20021127 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16520 145372 DURING C CHECK, THE CENTER BUTT STRAP WAS FOUND TO HAVE A GOUGE AND CORROSION BETWEEN FRAMES 20 AND 23. MAINTENANCE R EMOVED DAMAGE AND REPLACED AFFECTED BUTT STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE . 2 L 7 2 4F RT T00011AT 2002122300018 20021223 00018 SO 2002 12 23 C2XA02SH134 1 20021204 A 3350 110049 BATTERY EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16520 145372 DURING C CHECK THE OVERWING LIGHTS BECAME IN-OPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY SUPPLY NR 4 AND PERFORMED OPERATIONAL CHECK, OPERATIOANL CHECK WAS GOOD IAW EMB 135 AMM 33-50-04. THE AIRCRAFT WAS APPROVED TO RETU RN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002122300019 20021223 00019 SO 2002 12 23 C2XA02SH135 1 20021204 A 5310 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14916 145415 DURING C CHECK, THE CENTER OMEGA BEAM BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 20 AND 23. MAINTENANCE REM OVED DAMAGE AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122300020 20021223 00020 SO 2002 12 23 C2XA02SH138 1 20021206 A 5310 14521700007 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14916 145415 DURING C CHECK, THE LT HAND OMEGA BEAM AT FRAME 20 INBOARD SIDE WAS FOUND TO HAVE CORROSION. MAITENACE REMOVED DAMAGED AREA AND PERFORMED A SPLICE REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122300021 20021223 00021 SO 2002 12 23 C2XA02SH139 1 20021206 A 5410 14528168001 PLATE EMB 145 EMB145LR 3260212 SO NR 1 PYLON GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14916 145415 SHV-DURING C CHECK, NR 1 ENGINE, FOWARD PYLON YOKE GUSSET PLATE WAS FOUND TO HAVE A GOUGE BY LOWER ENGINE MOUNT. MAINT ENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5420-01038. THE AIRCRAFT WAS APPROVED TO RE TURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122300022 20021223 00022 SO 2002 12 23 C2XA02SH143 1 20021218 A 5310 14521713003 BEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 DURING C CHECK, CENTER OMEGA BEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 20 AND 22. MAINTENANCE REMOVED DAMAGE SEC TION AND REPLACED AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002122300023 20021223 00023 SO 2002 12 23 C2XA02SH144 1 20021218 A 5410 14576514604 STRUCTURE EMB 145 EMB145ER 3260211 SO NR 2 NACELLE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 DURING C CHECK, NR 2 LOWER NACELLE STRUCTURE WAS FOUND TO HAVE A GOUGED EDGE MEMBER AT STATION XN=776.8MM. MAINTENANCE REMOVED AND REPLACED AFFECTED EDGE MEMBER IAW EMB 145 SRM. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002122300024 20021223 00024 SO 2002 12 23 C2XA02SH147 1 20021218 A 5310 14521713003 BEAM EMB 145 EMB145ER 3260211 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 DURING C CHECK CENTER OMEGA BEAM WAS FOUND GOUGED AT FRAME 23. MAINTENANCE REMOVED AND REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002122300026 20021223 00026 SO 2002 12 23 C2XA02TY166 1 20021106 A 7160 14575183003 INTAKE EMB 145 EMB145LR 3260212 SO NR 1 ENGINE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 DURING A SCHEDULED 2-C INSPECTION, THE NR 1 ENGINE INLET INNER SKIN WAS FOUND PROTRUDING ON AFT SIDE OF SKIN AT 4:00 AN D 10:00 O`CLOCK POSITIONS. MAINT. MEASURED THE PROTRUDING SKINS ON THE AFT SIDE .THEY RECONTOURED THE AFFECTED AREA TO T HE ORIGINAL SHAPE AND PERFORMED NDI; NO CRACKS NOTED, APPLIED SEALANT, ALODINED, PRIMED AND PAINTED IAW GST 3274/02 AND CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED. UPON COMPLETION OF ALL WORK. 2 L 7 2 4T RT T00011AT 2002122300027 20021223 00027 WP 2002 12 23 MWEA020742 1 20021220 A 5322 99365343 FASTENER DOUG DC9 DC981 3022081 WP STA 207 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 GALLEY SUBFLOOR HAS SMALL CRACKS AROUND FASTENERS HOLES JUST AFT OF SERVICE DOOR ENTERANCE UNDER FLOOR SUPPORT ANGLE STA TION 207 RIGHT. 2 L 7 2 4F A6WE 2002122300028 20021223 00028 SO 2002 12 23 C2XA02TY168 1 20021121 A 3350 20131A BATTERY EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHTS SHORTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14940 145033 DURING A SCHEDULED SERVICE AND ROUTINE INSPECTION, THE AFT OVERWING EMERGENCY LIGHT, FLOOR STRIP LIGHTS AFT OF EMERGENC Y EXITS,AND OVERHEAD EMERGENCY LIGHT WAS ALL FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGH T BATTERY AND THE OPS CHECK WAS GOOD IAW EMB 145 AMM 2 33-50-04. A/C RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2003012800163 20030128 00163 GL 2003 1 28 C2XA02TY169 2 20021201 A 7261 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ENGINE LEAKING A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16981 10830 4102 145208 TYS AFTER TAKEOFF THE CREW WAS COMPLETING THE AIR PORTION OF THE ICE TEST WHEN A ODOR WAS SMELL IN THE CABIN AFTER A MIN UTE THE ICIAS SHOWED SMOKE IN THE LAV BUT NO CABIN INDICATION OR SMOKE WERE NOTED IN THE LAV THE CREW RETURNED TO TYS. MAINT PERFORMED ALL TEST AND COULD'NT DUPLICATE. A DECISION WAS MADE TO R/R THE ENGINE, EVIDENCE SHOWED CARBON SEAL FAI LURE. ENG WAS R/R IAW ROLLS-ROYCE MM. AND OPS CHECKS GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2002122300029 20021223 00029 SO 2002 12 23 C2XA02TY171 1 20021211 A 5310 14521725015 SILL EMB 145 EMB145LR 3260212 SO SERVICE DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 DURING A SCHEDULED INSPECTION THE RIGHT HAND SERVICE DOOR SILL PLATE WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB GST 1927/02A, EMB-145 SRM 51-40-02, CPM 51-21-04, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002122300030 20021223 00030 SO 2002 12 23 C2XA02TY172 1 20021211 A 5310 14521725013 SILL EMB 145 EMB145LR 3260212 SO SERVICE DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 DURING A SCHEDULED INSPECTION THE LT HAND SERVICE DOOR SILL PLATE WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB GST 1927/02A, EMB-145 CPM 51-21-04,05 & 06, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002122300031 20021223 00031 SO 2002 12 23 C2XA02TY173 1 20021211 A 5320 14522459003 ANGLE EMB 145 EMB145LR 3260212 SO GALLEY FLOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 DURING A SCHEDULED INSPECTION THE RT GALLEY RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RA MP ANGLE IAW EMB-145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPEC TION. 2 L 7 2 4T RT T00011AT 2002122300032 20021223 00032 WP 2002 12 23 MWEA020748 1 20021222 A 5310 991007397 BRACKET DOUG DC9 DC981 3022081 WP STATION 42 LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 UPON REMOVAL OF PROXIMITY SWITCH BRACKET, FASTENER HOLE PLUG WAS LOOSE/REMOVED. LOCATED AT STATION 42 CEILING AREA. -- INSTALLED FLANGE BUSHING. 2 L 7 2 4F A6WE 2002122300033 20021223 00033 SO 2002 12 23 C2XA02TY174 1 20021211 A 5320 14522460007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO CENTER FLOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 DURING A SCHEDULED INSPECTION THE CENTER FLOOR SUPPORT HAT BEAM TOP CAP WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLIS HED A DOUBLER REPAIR IAW EMB SRM 53-21-10, CPM 51-21-04, & 05, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEAS ED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2002122300034 20021223 00034 SO 2002 12 23 C2XA02TY176 1 20021219 A 5311 14525514001 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 DURING A SCHEDULED INSPECTION, FRAME 63, FORWARD OF THE CARGO DOOR, HAS AREAS OF CHAFE MARKS. MAINTENANCE BURNISHED THE CHAFFED AREA, ALODINED, PRIMED AND PAINTED.IAW-EMB-145-SRM-51-10-02, 51-21-04, 05 AND 06. AIRCRAFT RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122300035 20021223 00035 SO 2002 12 23 C2XA02TY177 1 20021219 A 5311 14523524001 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 7532 7532 145181 DURING A SCHEDULED INSPECTION, FRAME 64, FORWARD OF THE CARGO DOOR, HAS AREAS OF CHAFE MARKS. MAINTENANCE BURNISHED THE CHAFFED AREA, ALODINED, PRIMED AND PAINTED.I/A/W-EMB-145-SRM-51-10-02, 51-21-04, 05 AND 06. AIRCRAFT RELEASED TO SERVICE . 2 L 7 2 4T RT T00011AT 2002122300036 20021223 00036 NM 2002 12 23 DHL2002747013 1 20021220 A 2697 PIN BOEING 727 727224 1384076 NM A DHLA K O NONE OTHER O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 1) #1 ENGINE GROUND FAULT LIGHT ILLUMINATED 45 MIN. AFTER POWER ON. TROUBLESHOT SYSTEM - WITH FORWARD CONNECTOR REMOVE D LIGHT STILL REMAINS ON - REINSTALLED CONNECTOR - PROBLEM IS WITH WIRING TO CONNECTOR.2) DEFERRED PER MEL 26-9-1 CAT. "C". DMI #11339 PLACARD INSTALLED. REMOVED AND REPLACED "OPERATING POWER UNIT", NO HELP.3) REF.: DMI #11339, #1 ENGINE GROUND FAULT LIGHT ILLUMINATED 45 MIN. AFTER POWER ON. TROUBLESHOT SYSTEM WITH FORWARD CONNECTOR REMOVED. LIGHT REMAINS ON. REINSTALLED CONNECTOR. REMOVED AND REPLACED "OPERATING POWER UNIT", NO HELP. PROBLEM IS IN WIRING.4) REPINED FORWA RD FIRE LOOP CONNECTOR PER M/M 20-11-0. OPS CHECKED GOOD PER M/M 26-11-001. THIS CLEARS DMI #11339. PLACARD 2 L 7 3 4F A3WE 2002122300037 20021223 00037 SO 2002 12 23 C2XA02TY178 1 20021219 A 5311 14523051405 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 7532 7532 145181 DURING A SCHEDULED INSPECTION, FRAME 65, FORWARD OF THE CARGO DOOR, HAS AREAS OF CHAFE MARKS. MAINTENANCE BURNISHED THE CHAFED AREA, ALODINED, PRIMED AND PAINTED.I/A/W-EMB-145-SRM-51-10-02, 51-21-04, 05 AND 06. AIRCRAFT RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122300038 20021223 00038 SO 2002 12 23 C2XA02TY181 1 20021219 A 5310 14521700007 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 DURING A SCHEDULED INSPECTION THE LEFT OMEGA BEAM AT FRAME 20 HAS CORROSION AT CROSS BEAM. MAINTENANCE REPAIRED THE CORR ODED AREA, PRIMED AND PAINTED. I/A/W-EMB-145-SRM-53-21-10. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122300039 20021223 00039 SO 2002 12 23 C2XA02TY182 1 20021219 A 5320 14529150001 CHANNEL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 TYS, DURING A SCHEDULED INSPECTION THE RIGHT FUSELAGE Z CHANNEL AT FRAME 23 IS CORRODED. MAINTENANCE REMOVED AND REPLACE D THE Z CHANNEL AT FRAME 23. IAW EMB-145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED TO SERV ICE. 2 L 7 2 4T RT T00011AT 2002122300040 20021223 00040 WP 2002 12 23 ABXA020355 1 20021211 A 7603 CONTROL CABLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D NE THROTTLE CONTAMINATED A ABXA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 980AX 47176 THROTTLES EXTREMELY DIFFICULT TO MOVE DURING FLIGHT. EXPECTED ICE CONTAMINATION. CLEANED AND LUBRICATED CABLES AND FAIRL EADS ABOVE FORWARD BAG BIN. ICE REMNENTS NOTED ON GILL LINER ABOVE BAG BIN. THROTTLE MOVEMENT NORMAL. REMOVED ICE. MO PPED CARGO COMPARTMENT AS REQUIRED. 2 L 7 2 4F 4 F A6WE E2EA 2002122300041 20021223 00041 NM 2002 12 23 ABXA020356 1 20021213 A 3350 SWITCH BOEING 767 767200 1385120 NM EMERGENCY LIGHTS INOPERATIVE A ABXA O OTHER L NO TEST DE DESCENT 1 GL 23 790AX 23140 EMERGENCY LIGHTS WOULD NOT EXTINGUISH IN OFF POSITION. LIGHTS EXTINGUISHED IN ARMED POSITION AND ILLUMINATED IN ON. CLEANED AND LUBRICATED SWITCH (SW5) IN EMERGENCY CONTROL LIGHT PANEL. EMERGENCY LIGHTS OPS CHECKED GOOD IAW MM. 2 L 7 2 4F RT A1NM 2002122300042 20021223 00042 WP 2002 12 23 ABXA020358 1 20021202 A 5320 99576641 INTERCOSTAL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 FORWARD LOWER CARGO DOOR LOWER AFT STOP FITTING INTERCOSTAL CRACKED IN TWO PLACES. REPLACED FORWARD LOWER CARGO DOOR IAW SRM. 2 L 7 2 4F 4 F A6WE E2EA 2002122300043 20021223 00043 WP 2002 12 23 ABXA020359 1 20021202 A 5230 59101577 PANEL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D* NE CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 AFT LOWER CARGO DOOR OUTER PANEL CRACKED AND HAD IMPROPER EDGE DISTANCE AT THE NR 2 BEAM FORWARD SIDE. (HOLD OPEN LATCH AREA) REPLACED AFT LOWER CARGO DOOR ASSEMBLY IAW SRM. 2 L 7 2 4F 4 F A6WE E2EA 2002122300044 20021223 00044 NE 2002 12 23 HEEA082388 1 20021206 A 2435 200SGL115Q STARTER GEN SKRSKY S76 S76A 8143006 NE ENGINE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546K 760082 STARTER GENERATOR WILL NOT TURN OVER. 1 G 7 2 3U H1NE 2002122300046 20021223 00046 GL 2002 12 23 HEEA082390 2 20021211 A 7250 6886407 TURBINE WHEEL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136H 1040 S833 CAE821629F ENGINE PRODUCING LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED SULFIDATION ON 1ST STAGE WHEEL BLADES. SCRAPPED. 1 G 7 2 3U 3 U H3EU E4CE 2002122300047 20021223 00047 NE 2002 12 23 HEEA082391 1 20021211 A 2840 12281301 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT READS LOW E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22342 760096 FUEL FLOW INDICATOR READING LOW. 1 G 7 2 3U H1NE 2002122300048 20021223 00048 NE 2002 12 23 HEEA082392 1 20021211 A 7714 0177555240 TACHOMETER SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 TACHOMETER MALFUNCTIONED, OVERSPEED LIGHT STAYS ON. 1 G 7 2 3U H1NE 2002122300049 20021223 00049 2002 12 23 HEEA082393 4 20021212 A 2312 064100900 TRANSCEIVER SKRSKY S76 S76A 8143006 NE COCKPIT INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546G 760076 TRANSCEIVER INOPERATIVE. IN SHOP FOR REPAIR. 1 G 7 2 3U H1NE 2002122300050 20021223 00050 NM 2002 12 23 CALA0200595 1 20021221 A 5347 SEAT TRACK BOEING 777 777224 1385225 NM BS 1497-1567 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78003 27579 INSPECTION FOUND SEAT TRACK CORRODED AT BS 1497-1567, RBL 74. THE SEAT TRACK WAS REPAIRED IAW ECRA 5310-04307. 2 L 7 2 4F RT T00001SE 2002122300051 20021223 00051 NM 2002 12 23 CALA0200596 1 20021221 A 5330 SKIN BOEING 777 777224 1385225 NM BS 359 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78003 27579 INSPECTION FOUND L/H FUSELAGE SKIN DENTED AT BS 359, S33L. THE SKIN WAS REPAIRED IAW ECRA 5330-03189. 2 L 7 2 4F RT T00001SE 2002122300052 20021223 00052 NM 2002 12 23 CALA0200597 1 20021221 A 5330 SKIN BOEING 777 777224 1385225 NM STA 345 & 382 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78003 27579 INSPECTION FOUND L/H FUSELAGE SKIN DENTED AT STA 345 AND STA 382, S33L. REPAIRED SKIN IAW ECRA 5330-03189. 2 L 7 2 4F RT T00001SE 2002122300053 20021223 00053 WP 2002 12 23 CALA0200598 1 20021221 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 229 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND R/H INBOARD SEAT TRACK CORRODED AT STA 229. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-05, FI GURE 4F. 2 L 7 2 4F A6WE 2002122300054 20021223 00054 NM 2002 12 23 CALA0200599 1 20021221 A 5330 SKIN BOEING 777 777224 1385225 NM BS 655-675 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78003 27579 INSPECTION FOUND L/H FUSELAGE EXTERNAL SKIN DENTED AT BS 655-675, S24L-28L. REPAIRED IAW SRM 53-00-01, REPAIR 7, FIGURE 202. A DIP WAS ISSUED TO REINSPECT THE AREA AND PERFORM AN EXTERNAL LFEC OR INTERNAL HFEC INSPECTION WITH A DETAILED VIS UAL INSPECTION OF THE AREA WITHIN 30,000 FLIGHT CYCLES. 2 L 7 2 4F RT T00001SE 2002122300055 20021223 00055 WP 2002 12 23 CALA0200600 1 20021222 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP STA 229 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND R/H O/B SEAT TRACK CORRODED AT STA 229. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 51-30-02. 2 L 7 2 4F A6WE 2002122300056 20021223 00056 SO 2002 12 23 C2XA02BT085 1 20021221 A 3230 3631101007 CONTROL HANDLE EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 SW 27 16954 145072 EWR---CO3418, CREW REPORTED , "AFTER TAKEOFF, GEAR GOT STUCK INTRANSIT. RECYCLED GEAR LEVER, GEAR WOULD NOT GO UP. GEAR SELECTOR RETURNED TO GEAR DOWN AND AIR RETURNED BACK TO NEWARK". MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 MM #32-32-02. OPS.CHECKED OF LANDING GEAR SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122300058 20021223 00058 EU 2002 12 23 MALA020689 1 20021222 A 2560 P4010021 BATTERY SAAB SF340 340B 7860101 EU A MALA K NONE L NO TEST NR NOT REPORTED 1 GL 15 403XJ 340B403 DEAD EMERGENCY FLASHLIGHT BATTERIES. MAINTENANCE REPLACED BATTERY PN P4-01-0021. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2002122300060 20021223 00060 2002 12 23 HEEA082396 4 20021212 A 3451 066106602 TRANSCEIVER SKRSKY S76 S76A 8143006 NE DME SYSTEM FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 476X 760436 DOES NOT DISPLAY INFORMATION ON KDI572. INDICATOR FUNCTIONS PROPERLY. IN SHOP REPAIR. 1 G 7 2 3U H1NE 2002122300061 20021223 00061 2002 12 23 HEEA082397 4 20021212 A 3451 066106602 TRANSCEIVER SKRSKY S76 S76A 8143006 NE DME SYSTEM FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 476X 760436 DOES NOT DISPLAY INFORMATION ON KDI572. IN SHOP REPAIR. 1 G 7 2 3U H1NE 2002122300063 20021223 00063 NE 2002 12 23 HEEA082399 1 20021212 A 2560 110175601 SEAT BELT SKRSKY S76 S76A 8143006 NE COCKPIT DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546K 760082 COPILOT BELT WILL NOT ADJUST. TO BE SENT TO VENDOR FOR REPAIR. 1 G 7 2 3U H1NE 2002122300065 20021223 00065 NE 2002 12 23 HEEA082401 1 20021212 A 6321 CALIPER SKRSKY S76 S76A 8143006 NE ROTOR BRAKE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1546G 760076 CALIPERS LEAKING. SERIAL NUMBERS REMOVED ARE AUG80-00389 AND B060-00219. IN SHOP REPAIR. 1 G 7 2 3U H1NE 2002122300066 20021223 00066 2002 12 23 HEEA082402 4 20021212 A 3442 7007700614 INDICATOR SKRSKY S76 S76A 8143006 NE WX RADAR SYS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 INDICATOR SPIKING. PENDING VENDOR REPAIR. 1 G 7 2 3U H1NE 2002122300067 20021223 00067 EU 2002 12 23 AWXA200201232 1 20021207 A 5220 FE12710004 SHEAR PIN AIRBUS 320 A320231 3930325 EU R-1 DOOR SHEARED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 0 0 65 MCN - EMERGENCY EVACUATION - DURING C-03 CHECK THE R-1 DOOR DAMPER ARM SHEAR PIN WAS FOUND BROKEN. MAINTENANCE REMOVED A ND REPLACED THE R-1 DOOR DAMPER SHEAR PIN IAW AMM 52-10-00-020-053, AND 52-10-00-420-051. 2 L 7 2 4F RT A28NM 2002122300068 20021223 00068 EU 2002 12 23 AWXA200201233 1 20021207 A 5220 FE12710004 SHEAR PIN AIRBUS 320 A320231 3930325 EU R-2 DOOR BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 0 0 65 MCN - EMERGENCY EVACUATION - DURING C-03 CHECK THE R-2 DOOR DAMPER CYLINDER STRIKER ARM SHEAR PIN WAS FOUND BROKEN. MAIN TENANCE REMOVED AND REPLACED THE R-2 DOOR DAMPER SHEAR PIN IAW AMM 52-10-00-020-053, AND 52-10-00-420-051. 2 L 7 2 4F RT A28NM 2002122300069 20021223 00069 EU 2002 12 23 AWXA200201234 1 20021207 A 5220 FE12710004 SHEAR PIN AIRBUS 320 A320231 3930325 EU L-1 DOOR SHEARED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 0 0 65 MCN - EMERGENCY EVACUATION - DURING C-03 CHECK THE L-1 DOOR DAMPER CYLINDER STRIKER ARM SHEAR PIN WAS FOUND BROKEN. MAIN TENANCE REMOVED AND REPLACED THE L-1 DOOR DAMPER SHEAR PIN IAW AMM 52-10-00-020-053, AND 52-10-00-420-051. 2 L 7 2 4F RT A28NM 2002122300070 20021223 00070 NM 2002 12 23 AWXA200201236 1 20021219 A 5313 69353521 TIE CLIP BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 0 0 23776 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1/4" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 578, STR 4 R/H. MAINTENANCE REM OVED THE DAMAGED STRINGER TIE CLIP AT BS 578, STR 4 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; AND INSTALLED R EPAIR PART IAW B737-300 SRM 51-40-02, PG. 3-4, 10-11, 38, & 45, FIG. 8 & 12. 2 L 7 2 4F RT A16WE 2002122400001 20021224 00001 SO 2002 12 24 C2XA02SH155 1 20021223 A 5500 14520739403 BRACKET EMB 145 EMB145ER 3260211 SO CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV- DURING C CHECK PULLEY BRACKET INSIDE PANEL 325 LR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED BRA CKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002122400002 20021224 00002 SO 2002 12 24 C2XA02SH156 1 20021223 A 5300 12010732001 FRAME EMB 145 EMB145ER 3260211 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 SHV DURING C CHECK FRAME 81 WAS FOUND GOUGED AT BOTTOM CENTER. MAINTENANCE REMOVED DAMAGED SECTION AND REPAIRED FRAME 8 1 IAW CONTINENTAL EXPRESS EC 5310-01223. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2002122400003 20021224 00003 2002 12 24 372PA0015 4 20021222 A 3460 COMPUTER BOEING 737 737306 13844BG NM A PIDA K NONE O OTHER UK UNKNOWN 1 SO 05 372PA 23546 FMC will not accept any data on the route page. Re-racked FMC & ran Bite chk. Chks normal at this time IAW 34-62-01. 2 L 7 2 4F RT A16NE 2002122400004 20021224 00004 2002 12 24 372PA0016 4 20021222 A 3450 RECEIVER BOEING 737 737306 13844BG NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 372PA 23546 V-Nav disconnects for no obvious reason. Re-racked both Nav receivers. Ran Bite chk. Ops normal at this time IAW MM34- 22-00. 2 L 7 2 4F RT A16NE 2003032400021 20030324 00021 2003 3 24 250TR0005 4 20021219 A 2297 WIRE BOEING 737 7372K5 138448X NM AUTOFLIGHT BROKEN A PIDA O OTHER G MULTIPLE FAILURE NR NOT REPORTED 1 SO 05 250TR 22597 A/T FAILS INTERFACE TEST 6.9 & 56.9 SUB.TEST 8 & 9. ITEM DEFERRED IAW 737-200 MEL 22-4 CONTROL NR 1221003. 01/10/2003. REPAIRED BROKEN WIRES AT SUMMING POINTS ON E1-3 SHELF PER WDM CHPT. 20 A/T OPS NORMAL PER BITE & A/P INTERFACE TESTS. CLEARED MEL 22-4, CONTROL # 1221003. 2 L 7 2 4F RT A16WE 2002122400005 20021224 00005 EU 2002 12 24 02358308 1 20021223 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 308UE 41023 During preflight maintenance inspection, the crew reported the L/H Fwd External Emergency Light fixture has one inoperat ive bulb. Maintenance personnel relamped L/H Fwd Emergency Light. Ops ck'd good. Aircraft returned to service. 2 L 7 2 4T RT A41NM 2002122400006 20021224 00006 SO 2002 12 24 C2XA02CL252 1 20021223 A 3350 3071 BULB EMB 145 EMB145ER 3260211 SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14925 145004 DURING ROUTINE MAINTENANCE THE RIGHT EXTERNAL OVERWING EMERGENCY LIGHT WAS INOPERATIVE.MAINTENANCE REPLACED THE RIGHT EM ERGENCY LIGHT BULB.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2002122400007 20021224 00007 NM 2002 12 24 2002UALA01860 1 20021007 A 5754 114W424611 WEDGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE #11 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 T/E WEDGE DELAMINATED, SLAT #11 MAJOR REPAIR ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2002122400008 20021224 00008 NM 2002 12 24 S02427048 1 20021220 A 2750 FLAP BOEING BOEING 747 747400 NM PWA 4056 PW4056 NE LT INBOARD TE MALFUNCTIONED W SAJF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 03 24310 INBOARD TE FLAP ASYMETRY, A/C RETURNED TO HKG. LT INBOARD FLAP SHOW 5 DEG, RT INBOARD FLAP SHOW 10 DEG WHILE FLAP LEVER SET IN 10 UNIT. REPLACED LT INBOARD FLAP POS RVDT IAW MM 27-58-01, FLAP POS RVDT ADJ/TEST SATISFACTORY 2 L 7 4 4F 4 F RT A20WE E24NE 2002122600001 20021226 00001 2002 12 26 HEEA082404 4 20021212 A 2370 80510800001 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 792CH 760193 INDICATOR COMES ON THEN CUTS OFF COMPLETELY, DISPLAY NEVER STAYS ON. PENDING VENDOR REPAIR. 1 G 7 2 3U H1NE 2002123100003 20021231 00003 2002 12 31 HEEA082405 4 20021212 A 3130 9806020023 CVR SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 792CH 760193 COCKPIT VOICE RECORDER ALLOWS TEST LIGHT TO REMAIN ON. PENDING VENDOR REPAIR. 1 G 7 2 3U H1NE 2002123100004 20021231 00004 2002 12 31 HEEA082406 4 20021212 A 3130 9806020023 CVR SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 792CH 760193 COCKPIT VOICE RECORDER ALLOWS TEST LIGHT TO REMAIN ON. PENDING VENDOR REPAIR. 1 G 7 2 3U H1NE 2002123100005 20021231 00005 2002 12 31 HEEA082407 4 20021212 A 2312 064100900 TRANSCEIVER SKRSKY S76 S76A 8143006 NE VHF SYSTEM WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 VHF TRANSCEIVER IS WEAK AND GARBLED. VERIFIED RECEIVER WEAK AND REALIGNED PRESELECTOR AND I.F. SECTION OF RECEIVER. ADJ USTED C/N SQUELCH AND CARRIER SQUELCH. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002122600002 20021226 00002 2002 12 26 HEEA082408 4 20021212 A 3451 SENSOR SKRSKY S76 S76A 8143006 NE IND PHOTOCELL MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546G 760076 INDICATOR WILL NOT DIM. REPLACED PHOTOCELL AND LENS, APPLIED DC-4 COMPOUND TO HEADER. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002123100006 20021231 00006 2002 12 31 HEEA082409 4 20021212 A 3452 066107100 TRANSPONDER SKRSKY S76 S76A 8143006 NE ATC SYSTEM CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 TRANSPONER HAS NO POWER OUT. CLEANED EXCESSIVE CORROSION. REPLACED Q501/Q502 TRANSISTORS, 2 EACH INSULATORS AND 3 EACH WASHERS. ALIGNED RECEIVER TO SPECS. TRANSMIT POWER VERY WEAK. FOUND PROBLEM ON TRANSMITTER BOARD. SENT IN FOR INSPE CTION AND REPAIR. 1 G 7 2 3U H1NE 2002123100007 20021231 00007 2002 12 31 HEEA082410 4 20021212 A 3416 066011560101 TRANSPONDER SKRSKY S76 S76A 8143006 NE ALTIMETER INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546G 760076 ALTIMETER TRANSPONDER INOPERATIVE. FOUND UNIT DRAWING EXCESSIVE CURRENT, TROUBLESHOT UNIT, FOUND V101 CAVITY TUBE BAD, R EPLACED. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002123100008 20021231 00008 2002 12 31 HEEA082411 4 20021212 A 2312 071101218 TRANSCEIVER SKRSKY S76 S76A 8143006 NE VHF SYSTEM MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 TRANSCEIVER CAUSES STATIC IN RECEIVE MODE (MOTOR BOATING). COULD NOT DUPLICATE COMPLAINT. FOUND 5 VOLT LIGHTS INOPERATI VE, REPLACED 2 EACH BULBS, 5 VOLT DECAL AND S3 TEST SWITCH. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002122600003 20021226 00003 2002 12 26 HEEA082412 4 20021212 A 3455 KNOB SKRSKY S76 S76A 8143006 NE CONTROL BOX LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 CONTROL KNOB IS LOOSE AND CANNOT BE TIGHTENED. REPLACED 28V LIGHTS, DECAL, DISPLAY LENS AND TIGHTENED KNOB. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002122600004 20021226 00004 NE 2002 12 26 HEEA082414 1 20021212 A 5610 076204002 WINDSHIELD SKRSKY S76 S76A 8143006 NE COCKPIT CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 WINDSHIELD IS CRACKED. 1 G 7 2 3U H1NE 2002122600005 20021226 00005 2002 12 26 HEEA082415 4 20021212 A 3421 1113034 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT PRECESSES E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22342 760096 ATTITUDE INDICATOR PRECESSES IN FLIGHT. 1 G 7 2 3U H1NE 2002122600006 20021226 00006 2002 12 26 HEEA082416 4 20021212 A 3421 1113034 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT RATCHETING E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 ATTITUDE INDICATOR HAS RATCHETY MOVEMENT. 1 G 7 2 3U H1NE 2002122600007 20021226 00007 NE 2002 12 26 HEEA082417 1 20021212 A 6220 BEARING SKRSKY S76 S76A 8143006 NE POSITIONING ROD WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 760047 POSITIONING ROD HAS WORN BEARINGS. REPAIRED. 1 G 7 2 3U H1NE 2002122600008 20021226 00008 NE 2002 12 26 HEEA082418 1 20021212 A 6700 1945E81 FITTING SKRSKY S76 S76A 8143006 NE FLIGHT CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 FLIGHT CONTROL FITTING IS WORN. SCRAPPED. 1 G 7 2 3U H1NE 2002122600009 20021226 00009 NE 2002 12 26 HEEA082419 1 20021212 A 2435 200SGL115Q STARTER GEN SKRSKY S76 S76A 8143006 NE ENGINE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546K 760082 STARTER GENERATOR WILL NOT TURN OVER. 1 G 7 2 3U H1NE 2002122600010 20021226 00010 NE 2002 12 26 HEEA082420 1 20021212 A 7100 23069740 CHECK VALVE SKRSKY S76 S76A 8143006 NE ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 CHECK VALVE CRACKED AND LEAKING. SCRAPPED. 1 G 7 2 3U H1NE 2002122600011 20021226 00011 NE 2002 12 26 HEEA082421 1 20021212 A 2435 23081043 STARTER GEN SKRSKY S76 S76A 8143006 NE ENGINE MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546K 760082 STARTER GENERATOR WON'T COME ON LINE. 1 G 7 2 3U H1NE 2002122600012 20021226 00012 NE 2002 12 26 HEEA082422 1 20021212 A 2435 SHAFT SKRSKY S76 S76A 8143006 NE STARTER GEN SHEARED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 760PH 15816 477 760078 STARTER GENERATOR HAS A SHEARED SHAFT. REPLACED DRIVE SHAFT AND REPAIRED. 1 G 7 2 3U H1NE 2002122600013 20021226 00013 NE 2002 12 26 HEEA082423 1 20021212 A 2842 23356 PRESSURE SWITCH SKRSKY S76 S76A 8143006 NE FUEL LOW INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22342 760096 FUEL LOW PRESSURE SWITCH INTERMITTENT, LIGHT WOULD NOT COME ON. 1 G 7 2 3U H1NE 2002122600014 20021226 00014 NE 2002 12 26 HEEA082424 1 20021212 A 3000 2820 SWITCH SKRSKY S76 S76A 8143006 NE ANTI ICE WARNING FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546K 760082 SWITCH FAILED, ANTI ICE WARNING LIGHT WILL NOT GO OUT. 1 G 7 2 3U H1NE 2002122600015 20021226 00015 NE 2002 12 26 HEEA082425 1 20021212 A 3212 297800013 BOTTLE SKRSKY S76 S76A 8143006 NE EMERGENCY FLOAT DISCHARGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 FLOAT BOTTLE DISCHARGED. REPAIRED. 1 G 7 2 3U H1NE 2002122600016 20021226 00016 NE 2002 12 26 HEEA082426 1 20021212 A 3212 297800013 BOTTLE SKRSKY S76 S76A 8143006 NE EMERGENCY FLOAT DISCHARGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 EMERGENCY FLOAT BOTTLE DISCHARGED. REPAIRED. 1 G 7 2 3U H1NE 2002122600017 20021226 00017 NE 2002 12 26 HEEA082427 1 20021212 A 3212 297800013 BOTTLE SKRSKY S76 S76A 8143006 NE EMERGENCY FLOAT DISCHARGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 EMERGENCY FLOAT BOTTLE DISCHARGED. REPAIRED. 1 G 7 2 3U H1NE 2002122600018 20021226 00018 NE 2002 12 26 HEEA082428 1 20021212 A 3212 297800013 BOTTLE SKRSKY S76 S76A 8143006 NE EMERGENCY FLOAT DISCHARGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 EMERGENCY FLOAT BOTTLE DISCHARGD. REPAIRED. 1 G 7 2 3U H1NE 2002122600020 20021226 00020 WP 2002 12 26 DHL2002806015 1 20021218 A 2900 HOSE DOUG DC8 DC873F 302199F WP A DHLA O OTHER O OTHER CL CLIMB 1 SO 01 806DH 46002 1) DURING CRUISE, HYDRAULIC SYSTEM PRESSURE WENT TO ZERO. HYDRAULIC QUANTITY WENT TO THE "AUX" LEVEL. AILERON AND RUDDE R CONTROL MANUEL LIGHT ILLUMINATED. (NOTE: DHL EVENT REPORT DATED 12-18-2002 STATES EMERGENCY WAS DECLARED.)2) FOUND LT BOGIE TRIM HYDRAULIC HOSE LEAKING. REPLACED HOSE ASSEMBLY. OPS AND LEAK CHECKED GOOD PER DC-8 M/M 32-53-2. (NOTE: DHL A IRWAYS EVENT REPORT 12-18-2002, FLIGHT #102, FROM SFO TO CVG. THIS REPORT STATES DURING CLIMB FROM SFO OUT OF 31500 WITH THE AUTO PILOT ON NOTICED AILERON MOVING RIGHT AND HYDRAULIC LOSS AND MANUAL LIGHT CAME ON. WE RAN THE ABNORMAL CHECKLI ST AND FLEW HOME IN MANUAL REVISION. DURING APPROACH WE RAN THE PROCEDURE AND ALL WORKED NORMAL TO A NORMAL LANDING. 2 L 7 4 4F RT 4A25 2002122600021 20021226 00021 NE 2002 12 26 HEEA082430 1 20021212 A 3212 297800013 BOTTLE SKRSKY S76 S76A 8143006 NE EMERGENCY FLOAT DISCHARGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 EMERGENCY FLOAT BOTTLE DISCHARGED, REPAIRED. 1 G 7 2 3U H1NE 2002122600022 20021226 00022 NE 2002 12 26 HEEA082431 1 20021212 A 3212 297800013 BOTTLE SKRSKY S76 S76A 8143006 NE EMERGENCY FLOAT DISCHARGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 EMERGENCY FLOAT BOTTLE DISCHARGED, REPAIRED. 1 G 7 2 3U H1NE 2002122600023 20021226 00023 NE 2002 12 26 HEEA082432 1 20021212 A 3212 297800013 BOTTLE SKRSKY S76 S76A 8143006 NE EMERGENCY FLOAT DISCHARGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 EMERGENCY FLOAT BOTTLE DISCHARGED, REPAIRED. 1 G 7 2 3U H1NE 2002122600024 20021226 00024 NE 2002 12 26 HEEA082433 1 20021212 A 2612 30326E7 AMPLIFIER SKRSKY S76 S76A 8143006 NE FIRE WARNING FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 FIRE WARNING WILL NOT TEST. REPLACE THE CONTROL AMPLIFIER. 1 G 7 2 3U H1NE 2002122600025 20021226 00025 2002 12 26 HEEA082434 4 20021212 A 3442 36140788201 INDICATOR SKRSKY S76 S76A 8143006 NE WX RADAR SYSTEM MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 RADAR INDICATOR WILL NOT PAINT OR WORK UNTIL CYCLED ON AND OFF MULTIPLE TIMES. 1 G 7 2 3U H1NE 2002122600027 20021226 00027 2002 12 26 HEEA082436 4 20021212 A 3442 4000038 CONTROL HEAD SKRSKY S76 S76A 8143006 NE WX RADAR SYS INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546G 760076 VOLUME CONTROL INTERMITTENT. REPLACED VOLUME CONTROL, BAD VOLUME KNOB AND BAD TEST SWITCH AND BAD FACEPLATE. BENCH CHEC K GOOD. 1 G 7 2 3U H1NE 2002122600028 20021226 00028 2002 12 26 HEEA082437 4 20021212 A 3442 4000038001 CONTROL UNIT SKRSKY S76 S76A 8143006 NE WX RADAR SYS INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 760047 VOLUME KNOB IS INTERMITTENT. FOUND FACEPLATE, VOLUME KNOB, CHANNEL SELECTOR KNOB, TONE SWITCH S2 BAD. REPAIRED. ALSO C LEANED MINOR CORROSION ON CASE. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002122600029 20021226 00029 2002 12 26 HEEA082438 4 20021212 A 3421 LIGHT SKRSKY S76 S76A 8143006 NE ATTITUDE IND INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22342 4114 760096 ATTITUDE INDICATOR BACK LIGHT IS INOPERATIVE. REPAIRED. 1 G 7 2 3U H1NE 2002122600030 20021226 00030 NE 2002 12 26 HEEA082439 1 20021212 A 7714 54487129110 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT INACCURATE E K NONE L NO TEST IN INSP/MAINT 1 SW 03 22342 760096 INDICATOR WILL NOT COMPUTE THE PROPER N. FOR GIVEN TEMPERATURE AND PENSITY ALTITUDE. 1 G 7 2 3U H1NE 2002122600031 20021226 00031 2002 12 26 HEEA082444 4 20021212 A 3446 7000839904 INDICATOR SKRSKY S76 S76A 8143006 NE RADAR ALTIMETER MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 RADAR ALTIMETER INDICATOR HAS AN UNRELIABLE OFF FLAG AND NEEDLE PARKS DURING FLIGHT. 1 G 7 2 3U H1NE 2002122600033 20021226 00033 2002 12 26 HEEA082446 4 20021212 A 3442 7007700614 INDICATOR SKRSKY S76 S76A 8143006 NE WX RADAR SYS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 760PH 760078 WEATHER RADAR INDICATOR TILT IS INOPERATIVE. 1 G 7 2 3U H1NE 2002122600034 20021226 00034 NE 2002 12 26 HEEA082447 1 20021212 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE TAIL ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 14641 760082 TAIL ROTOR BLADE PADDLE "B" HAS A HOLE AT THE TIP. 1 G 7 2 3U H1NE 2002122600035 20021226 00035 NE 2002 12 26 HEEA082448 1 20021212 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE TAIL ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 13834 760096 TAIL ROTOR BLADE PADDLE "B" HAS AN EROSION HOLE AT THE TIP END. 1 G 7 2 3U H1NE 2002122600036 20021226 00036 NE 2002 12 26 HEEA082449 1 20021212 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE TAIL ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 761PH 9093 760224 TAIL ROTOR BLADE PADDLE "A" HAS HOLE THROUGH THE END CAP. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND R EPAIR. 1 G 7 2 3U H1NE 2002122600037 20021226 00037 NE 2002 12 26 HEEA082450 1 20021212 A 6410 7610105101042 BLADE SKRSKY S76 S76A 8143006 NE TAIL ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5435V 3001 760158 TAIL ROTOR BLADE PADDLE "A" HAS VOID IN THE AIRFOIL REGION BEYOND FIELD LIMITS. SENT TO INTERNATIONAL AVIATION COMPOSITE S FOR INSPECTION AND REPAIR. 1 G 7 2 3U H1NE 2002122600038 20021226 00038 NE 2002 12 26 HEEA082451 1 20021212 A 6730 7610408015103 PIN SKRSKY S76 S76A 8143006 NE ROTOR SERVO FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 476X 760436 EXPANDABLE PIN FAILED TORQUE CHECK ON 300 HOUR INSPECTION. SCRAPPED. 1 G 7 2 3U H1NE 2002122600039 20021226 00039 NE 2002 12 26 HEEA082452 1 20021212 A 6230 BEARING SKRSKY S76 S76A 8143006 NE ROTATING SCISSOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911UK A19200407 760275 ROTATING SCISSORS HAVE WORN BEARINGS. REPLACED BEARINGS. 1 G 7 2 3U H1NE 2002122600040 20021226 00040 NE 2002 12 26 HEEA082453 1 20021212 A 6220 7610608000049 DAMPER SKRSKY S76 S76A 8143006 NE MAIN ROTOR LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1546K 760082 MAIN ROTOR DAMPER LEAKING. 1 G 7 2 3U H1NE 2002122600041 20021226 00041 NE 2002 12 26 HEEA082454 1 20021212 A 6220 7610608000050 DAMPER SKRSKY S76 S76A 8143006 NE MAIN ROTOR LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1546K 760082 MAIN ROTOR DAMPER LEAKING. 1 G 7 2 3U H1NE 2002122600042 20021226 00042 WP 2002 12 26 MWEA020749 1 20021226 A 5311 591016315 STIFFENER DOUG DC9 DC915 3022036 WP RADIAL 20 LEFT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 STIFFENER AT AFT PRESSURE BULKHEAD AFT SIDE RADIAL 20 LEFT IS CRACKED. -- FABRICATED AND INSTALLED STIFFENER. 2 L 7 2 4F A6WE 2002122600043 20021226 00043 WP 2002 12 26 MWEA020750 1 20021226 A 5230 95200133 DOUBLER DOUG DC9 DC915 3022036 WP FWD CARGO CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FORWARD CARGO DOOR OUTER PAN RADIUS IS CRACKED INBOARD OF LOWER FORWARD DOOR STOP PAD. -- FABRICATED, DRILLED AND INST ALLED DOUBLER. 2 L 7 2 4F A6WE 2002122600044 20021226 00044 WP 2002 12 26 MWEA020751 1 20021226 A 5311 591016316 STIFFENER DOUG DC9 DC915 3022036 WP RADIAL 20 RIGHT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 STIFFENER AT AFT PRESSURE BULKHEAD AFT SIDE RADIAL 20 RIGHT. -- FABRICATED AND INSTALLED STIFFENER. 2 L 7 2 4F A6WE 2002122600045 20021226 00045 EA 2002 12 26 COMA0260727 1 20021219 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 918CA 7018 FLAPS FAILED DURING TAXI.INSPECTED FLAP SYSTEM IAW AD 98-20-01. 2 L 7 2 4F RT A21EA 2003011600212 20030116 00212 EA 2003 1 16 COMA0260729 1 20021220 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 963CA 7127 CABIN ALTITUDE CAUTION MESSAGE. COULD NOT DUPLICATE, CABIN PRESSURE CONTROL SYSTEM OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A21EA 2002122600046 20021226 00046 EA 2002 12 26 COMA0260731 1 20021221 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 957CA 7109 FLFIGHT 5720 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002122600047 20021226 00047 EA 2002 12 26 COMA0260735 1 20021223 A 3030 CONTROL BOX CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 929CA 7035 FLIGHT 5443 LEFT ANGLE OF ATTACK HEAT CAUTION MESSAGE.RESET SYSTEM - COULD NOT DUPLICATE. 2 L 7 2 4F RT A21EA 2002122600048 20021226 00048 2002 12 26 HEEA082458 4 20021212 A 2230 7611133 AMPLIFIER SKRSKY S76 S76A 8143006 NE AFCS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 AFCS ROLL SLICE (ROLL CHANNEL KICKS IN FLIGHT). 1 G 7 2 3U H1NE 2002122600049 20021226 00049 SO 2002 12 26 RAIA00212348 1 20021129 A 7830 TY203911A ACTUATOR EMB 145 EMB145LR 3260212 SO INTERMITTENT A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 817HK 8507 145058 5682-STL- THRUST REVERSER DISAGREE MESSAGE. MAINTENANCE DEFERRED PER MEL, AND SUBSEQUENTLY REMOVED AND REPLACED #1 T/R A CTUATOR SN TO86. 2 L 7 2 4T RT T00011AT 2002122600050 20021226 00050 EU 2002 12 26 RAIA00212349 1 20021201 A 3060 D45081B TIMER JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 553HK 13611 4441 41066 5504-STL- RIGHT PROP DE-ICE INOP. MAINTENANCE DEFERRED PER MEL AND SUBSEQUENTLY REMOVED AND REPLACED PROP DE-ICE TIMER. 2 L 7 2 4T RT A41NM 2002122600051 20021226 00051 SO 2002 12 26 RAIA00212351 1 20021206 A 3221 23092900401 LOCK ACTUATOR EMB 145 EMB145LR 3260212 SO INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 816HK 8996 145055 5719-STL- NOSE LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR UP-LOCK BOOK, OPS CK OK . 2 L 7 2 4T RT T00011AT 2002122600052 20021226 00052 SO 2002 12 26 RAIA00212352 1 20021209 A 3350 110049 BATTERY PACK EMB 145 EMB145LR 3260212 SO WEAK A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 815HK 7420 507 145048 MX-STL- OVER WING EMERGENCY LIGHT INOP. MAINTENANCE DEFERRED PER MEL, AND SUBSEQUENTLY REMOVED AND REPLACED EMERGENCY LI GHT BATTERY PACK, OPS CK OK. 2 L 7 2 4T RT T00011AT 2002122600053 20021226 00053 EU 2002 12 26 RAIA00212353 1 20021210 A 7810 141780015 STOP JETAIR JETSTM JETSTM4101 1500501 EU WORN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 572HK 41091 5392-SYR- LEFT ENGINE OVERHEAT INDICATION. MAINTENANCE REMOVED AND REPLACED STOP PLATES ON LEFT ENGINE TAIL EXHAUST PIPE , OPS CK OK. 2 L 7 2 4T RT A41NM 2002122600054 20021226 00054 EU 2002 12 26 RAIA00212355 1 20021215 A 2700 C850176 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 574HK 12188 10600 41093 5594-STL- LEFT AOA SENSOR WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED THE LEFT AOA SENSOR, OPS CK OK. 2 L 7 2 4T RT A41NM 2002122600055 20021226 00055 EU 2002 12 26 AWXA200201237 1 20021224 A 3350 ABS0374A24 CABLE AIRBUS 320 A320231 3930325 EU SEAT ROW 11 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 0 0 65 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 L/H WAS FOUND MOUNTED UPSIDE DOWN WITH A BR OKEN WIRE AT CONNECTOR. MAINTENANCE REPAIRED THE BROKEN WIRE AT CONNECTOR AND REMOUNTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 L/H; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2002122600056 20021226 00056 NM 2002 12 26 AWXA200201238 1 20021225 A 3350 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM SEAT ROW 15 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 0 0 24711 TUS - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPA IRED A BAD GROUND WIRE SPLICE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 15 L/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2002122600057 20021226 00057 NM 2002 12 26 AWXA200201240 1 20021218 A 5313 69353654 ANGLE BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 0 0 23776 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1/2" CRACK WAS FOUND AT FASTENER HOLE OF MAIN CABIN FLOOR SUPPORT UPPER ATTACH ANGLE BS 500D - BS 520, BL O. MAINTENANCE REMOVED DAMAGED MAIN CABIN FLOOR SUPPORT UPPER ATTACH ANGLE BS 500D - BS 520, BL O; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT UPPER ATTACH ANGLE IAW B737-300 SRM 51-40-05, PG. 1 & 4, FIG 2; AND IN STALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 1-4, 10-11, 28, & 32-35, FIG. 6, AND SRM 51-40-04, PG. 2, TABLE 1. 2 L 7 2 4F RT A16WE 2002122700001 20021227 00001 NE 2002 12 27 HEEA082442 1 20021212 A 3150 DISPLAY SKRSKY S76 S76A 8143006 NE WARNING SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 DISPLAY GOES TO ZERO DURING FLIGHT CAUSING HORN TO SOUND GEAR UP. REPAIRED. 1 G 7 2 3U H1NE 2002122700003 20021227 00003 NE 2002 12 27 HEEA082459 1 20021212 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 760PH 760078 THE FIBERGLASS ON THE END CAP IS ERODED BEYOND LIMITS. 1 G 7 2 3U H1NE 2002122700004 20021227 00004 NE 2002 12 27 HEEA082460 1 20021212 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 MAIN ROTOR BLADE HAS THE FIBERGLASS SKIN TORN, LIFTED AND ERODED AT THE TIP. 1 G 7 2 3U H1NE 2002122700005 20021227 00005 NE 2002 12 27 HEEA082461 1 20021212 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 MAIN ROTOR BLADE LEADING ABRASION STRIP UNBONDING AND LIFTING. 1 G 7 2 3U H1NE 2002122700006 20021227 00006 NE 2002 12 27 HEEA082462 1 20021212 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 MAIN ROTOR BLADE TIP CAP HAS FIBERGLASS BETWEEN INTERNAL AND EXTERNAL DOUBLER BROKEN. CRACK IN THE ABRASION STRIP ON TH E LOWER SIDE. 1 G 7 2 3U H1NE 2002122700007 20021227 00007 NE 2002 12 27 HEEA082463 1 20021212 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 MAIN ROTOR BLADE ABRASION STRIP ON THE LOWER SIDE HAS TWO SHARP DENTS. ONE HAS SOME PENETRATION THROUGH THE STRIP. 1 G 7 2 3U H1NE 2002122700008 20021227 00008 NE 2002 12 27 HEEA082464 1 20021212 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/ R BLADE DELAMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 MAIN ROTOR BLADE TIP CAP FIBERGLASS DELAMINATING FROM BOTTOM SIDE. 1 G 7 2 3U H1NE 2002122700009 20021227 00009 NE 2002 12 27 HEEA082465 1 20021212 A 6210 7615009043054 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 MAIN ROTOR TIP CAP FIBERGLASS ERODED AND TORN ON LOWER SIDE. 1 G 7 2 3U H1NE 2002122700010 20021227 00010 NE 2002 12 27 HEEA082466 1 20021212 A 6210 7615009100049A BLADE SKRSKY S76 S76A 8143006 NE MAIN ROTOR SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 14142 760231 MAIN ROTOR BLADE HAS THE SPLICE REPAIR NEAR STA 173 HAS SOME SEPARATION. 1 G 7 2 3U H1NE 2002122700011 20021227 00011 NE 2002 12 27 HEEA082467 1 20021212 A 6210 7615009100049A BLADE SKRSKY S76 S76A 8143006 NE MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5435V 13548 760158 MAIN ROTOR BLADE HAS THE TITANIUM LEADING EDGE STRIP HAS SEPERATION AT THE SPLICE AREA WITH A DEEP GASH. SENT TO INTERNA TIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR. 1 G 7 2 3U H1NE 2002122700012 20021227 00012 NE 2002 12 27 HEEA082468 1 20021212 A 6210 7615009100049A BLADE SKRSKY S76 S76A 8143006 NE MAIN ROTOR UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 760PH 11941 760078 THE TIP RIB IS UNBONDED AND THE ABRASION STRIP HAS A CHORDWISE CRACK WITH EXCESSIVE SEPARATION ON THE MAIN ROTOR BLADE. 1 G 7 2 3U H1NE 2002122700013 20021227 00013 NE 2002 12 27 HEEA082469 1 20021212 A 6210 7615009100051A BLADE SKRSKY S76 S76A 8143006 NE MAIN ROTOR SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 11973 760193 MAIN ROTOR BLADE TRIM TAB IS SEPARATED BEYOND LIMITS. 1 G 7 2 3U H1NE 2002122700014 20021227 00014 NE 2002 12 27 HEEA082470 1 20021212 A 6210 7615009100051A BLADE SKRSKY S76 S76A 8143006 NE MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 13138 760193 MAIN ROTOR BLADE SPLICE SECTION AT STA 132 HAS EXCESSIVE SEPARATION. TIP CAP HAS SEPARATION ON THE ABRASION STRIP. 1 G 7 2 3U H1NE 2002122700015 20021227 00015 NE 2002 12 27 HEEA082471 1 20021212 A 6210 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE MISMANUFACTURED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 13778 A08601344 TIP CAP DOES NOT FIT ON M/R BLADE. SENT TO HELICOPTER SUPPORT, INC. FOR WARRANTY REPAIR. 1 G 7 2 3U H1NE 2002122700016 20021227 00016 NE 2002 12 27 HEEA082472 1 20021212 A 6210 STRIP SKRSKY S76 S76A 8143006 NE M/R BLADE SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5435V 7477 A08601731 760158 MAIN ROTOR BLADE LEADING EDGE ABRASION STRIP SEPARATED NEXT TO THE SPLICE REPAIR. 1 G 7 2 3U H1NE 2002122700017 20021227 00017 NE 2002 12 27 HEEA082473 1 20021212 A 6210 SKIN SKRSKY S76 S76A 8143006 NE M/R BLADE ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 3578 A08602180 760050 MAIN ROTOR BLADE FIBERGLASS SKIN NEAR THE OUTBOARD END IS ERODED BEYOND LIMITS. 1 G 7 2 3U H1NE 2002122700018 20021227 00018 NE 2002 12 27 HEEA082474 1 20021212 A 6210 SKIN SKRSKY S76 S76A 8143006 NE M/R BLADE CRUSHED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 1004 A08602588 760035 BLADE HAS A HOLE IN THE SKIN AND THE TITANIUM STRIP ALSO HAS A HOLE. TRAILING EDGE HAS A NICK NEAR THE ROOT END. 1 G 7 2 3U H1NE 2002122700019 20021227 00019 EA 2002 12 27 HNAA0200091 1 20021218 A 3350 82410162001 CONTROL BOX DHAV DHC8 DHC8311 1386006 EA A HNAA K NONE O OTHER CR CRUISE 1 EA 07 327EN 261 Overhead and sidewall emergency lights flickered in flight. R&R of emergency light control box followed by a ground op erational check. 2 H 7 2 4T RT A13NM 2003021000146 20030210 00146 WP 2003 2 10 DHL2002801024 1 20021226 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CABIN MALFUNCTIONED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 7 MAIN DECK SMOKE DETECT WILL NOT TEST. REPORTED ON PREFLIGHT (P/N 30-231-4). RELAMPED 7 MAIN SMOKE DETECT AND RESECUR ED CONNECTOR PLUG. NO HELP. DEFERRED FURTHER TROUBLESHOOTING AND REPAIR PER MEL 26.6 CAT. "C". PLACARD INSTALLED DMI #11 389. 2 L 7 4 4F RT 4A25 2002122700020 20021227 00020 NE 2002 12 27 HEEA082475 1 20021212 A 3150 2820 SWITCH SKRSKY S76 S76A 8143006 NE CENTRAL WARNING STICKING E HEEA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 03 911MJ 760231 INTERNAL SWITCH CONTACTS STICKING CAUSING NR 2 ENGINE ANTI ICE CAUTION LIGHT TO STAY ON CONSTANTLY. PENDING VENDOR REPAI R. 1 G 7 2 3U H1NE 2002122700021 20021227 00021 NE 2002 12 27 HEEA082477 1 20021213 A 6300 7625002108041 BELLCRANK SKRSKY S76 S76A 8143006 NE MAIN ROTOR DRIVE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 MAIN ROTOR DRIVE BUSHINGS WORN AND CORROSION IN BARREL NUT AREA. REPLACED BELLCRANK DUE TO CORROSION. 1 G 7 2 3U H1NE 2002122700022 20021227 00022 NE 2002 12 27 HEEA082478 1 20021213 A 3201 7625100702043 LINK SKRSKY S76 S76A 8143006 NE MLG BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 MLG LINK IS BROKEN. SCRAPPED. 1 G 7 2 3U H1NE 2002122700023 20021227 00023 NE 2002 12 27 HEEA082479 1 20021213 A 3201 7625100702043 LINK SKRSKY S76 S76A 8143006 NE MLG BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 MLG LINK ASSY BROKEN. SCRAPPED. 1 G 7 2 3U H1NE 2002122700024 20021227 00024 NE 2002 12 27 HEEA082482 1 20021213 A 3212 7625101102110 FLOAT SKRSKY S76 S76A 8143006 NE MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 RT MAIN LANDING GEAR EMERGENCY FLOAT BAG LEAKING. 1 G 7 2 3U H1NE 2002122700025 20021227 00025 NE 2002 12 27 HEEA082483 1 20021213 A 3212 7625102702042 LINE SKRSKY S76 S76A 8143006 NE EMERGENCY FLOAT CHAFED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 RT EMERGENCY FLOAT FLOAT LINE FROM BAG TO MANIFOLD CHAFED. SCRAPPED. 1 G 7 2 3U H1NE 2002122700026 20021227 00026 NE 2002 12 27 HEEA082484 1 20021213 A 7160 7630207028060 SCREEN SKRSKY S76 S76A 8143006 NE INTAKE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 RT INTAKE SCREEN CRACKED. SCRAPPED. 1 G 7 2 3U H1NE 2002122700027 20021227 00027 NE 2002 12 27 HEEA082485 1 20021213 A 7160 7630207028060 SCREEN SKRSKY S76 S76A 8143006 NE INTAKE SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 RT INTAKE SCREEN SEPARATED. SCRAPPED. 1 G 7 2 3U H1NE 2002122700028 20021227 00028 NE 2002 12 27 HEEA082486 1 20021213 A 7160 7630207028060 SCREEN SKRSKY S76 S76A 8143006 NE INTAKE TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 INTAKE SCREEN TORN. SCRAPPED. 1 G 7 2 3U H1NE 2002122700029 20021227 00029 NE 2002 12 27 HEEA082487 1 20021213 A 2820 7630703900101 CHECK VALVE SKRSKY S76 S76A 8143006 NE FUEL SYS MALFUNCTIONED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 FUEL CHECK VALVE HARD TO START ON FIRST START. SCRAPPED. 1 G 7 2 3U H1NE 2002122700031 20021227 00031 NE 2002 12 27 HEEA082489 1 20021213 A 6700 BEARING SKRSKY S76 S76A 8143006 NE IDLER OUTPUT RATCHETING E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5435V 760158 FLIGHT CONTROL IDLER OUTPUT HAS RATCHETY BEARINGS. REPAIRED. 1 G 7 2 3U H1NE 2002122700032 20021227 00032 WP 2002 12 27 MWEA020757 1 20021226 A 5311 593643423 LONGERON DOUG DC9 DC981 3022081 WP STA 541 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 LONGERON 30 AT STATION 541 HAS MODERATE CORROSION. -- LOCATED, DRILLED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 2002122700033 20021227 00033 WP 2002 12 27 MWEA020763 1 20021227 A 5330 5911408125 SKIN DOUG DC9 DC981 3022081 WP STA 238-245 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FUSELAGE SKIN HAS SEVERAL DENTS STATION 238-245 BELOW LONGERON 6 LEFT. -- REMOVED DAMAGED SKIN, FABRICATED AND INSTALL ED NEW REPAIR SKIN. 2 L 7 2 4F A6WE 2002122700034 20021227 00034 WP 2002 12 27 MWEA020756 1 20021226 A 5311 593643423 LONGERON DOUG DC9 DC981 3022081 WP STA 541 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FORWARD PIT LONGERON 29 LEFT AT STATION 541 HAS MODERATE CORROSION. -- REMOVED CORROSION, LOCATED, DRILLED AND INSTALL ED LONGERON. 2 L 7 2 4F A6WE 2002122700035 20021227 00035 WP 2002 12 27 MWEA020760 1 20021226 A 5311 99100789 WEB DOUG DC9 DC981 3022081 WP STA 200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 THE FUSELAGE CUSP WEB AT STATION 200 ON LEFT SIDE OF FUSELAGE HAS HEAVY CORROSION. -- FABRICATED AND INSTALLED NEW CUSP WEB AND SPLICE REPAIR, DRILLED UP AND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2002122700036 20021227 00036 WP 2002 12 27 MWEA020761 1 20021226 A 3210 5930583224 DOOR DOUG DC9 DC981 3022081 WP DOT 451 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 RIGHT MAIN LANDING GEAR DOOR HAS LIGHT CORROSION AT FORWARD UPPER CORNER. -- REMOVED CORROSION, PLUGGED AND REDRILLED PILOT HOLES AND INSTALLED STRAPS AND FASTENERS. 2 L 7 2 4F A6WE 2002122700037 20021227 00037 WP 2002 12 27 MWEA020764 1 20021227 A 2780 3937425502 BUSHING DOUG DC9 DC981 3022081 WP #0 SLAT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 RIGHT SLAT OUTBOARD SHEAR PIN SUPPORT HAS PITTING CORROSION IN THE BEARING HOLE. -- FABRICATED AND INSTALLED REPAIR BU SHING. 2 L 7 2 4F A6WE 2002122700038 20021227 00038 2002 12 27 249TR0011 4 20021224 A 2210 SWITCH BOEING 737 7372K5 138448X NM A PIDA K NONE O OTHER UK UNKNOWN 1 SO 05 249TR 22598 A/P & F/D mode indicates TO/GA prior to take-off without input from crew & IAS changes to 165 knots on its own. Cleaned #2 throttle TO/GA switch, performed AP/FD bite test per MM 22-11-01.System tests normal. 2 L 7 2 4F RT A16WE 2002122700039 20021227 00039 NE 2002 12 27 HEEA082490 1 20021213 A 6700 BEARING SKRSKY S76 S76A 8143006 NE IDLER OUTPUT RATCHETING E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 911MJ 760231 FLIGHT CONTROL IDLER OUTPUT HAS RATCHETY BEARINGS. REPAIRED. 1 G 7 2 3U H1NE 2002122700040 20021227 00040 NE 2002 12 27 HEEA082495 1 20021213 A 6700 BEARING SKRSKY S76 S76A 8143006 NE BELLCRANK WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 WORN BEARINGS. REPAIRED. 1 G 7 2 3U H1NE 2002122700041 20021227 00041 NE 2002 12 27 HEEA082496 1 20021213 A 6700 7640009502046 BEARING SKRSKY S76 S76A 8143006 NE BELLCRANK WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 760PH 760078 FLIGHT CONTROL BELLCRANK HAS WORN BEARINGS. REPAIRED. 1 G 7 2 3U H1NE 2002122700042 20021227 00042 2002 12 27 HEEA082497 4 20021213 A 2213 BEARING SKRSKY S76 S76A 8143006 NE AFCS ACTUATOR WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1546K 760082 AFCS ACTUATOR HAS WORN BEARINGS. REPAIRED. 1 G 7 2 3U H1NE 2002122700043 20021227 00043 NE 2002 12 27 HEEA082498 1 20021213 A 6700 BEARING SKRSKY S76 S76A 8143006 NE BELLCRANK WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5435V 760158 FLIGHT CONTROL BELLCRANK HAS WORN BEARINGS. REPAIRED. 1 G 7 2 3U H1NE 2002122700044 20021227 00044 2002 12 27 HEEA082499 4 20021213 A 3414 7645000801101 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT READS LOW E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1546K 760082 AIRSPEED INDICATOR READING LOW. REPAIRED. 1 G 7 2 3U H1NE 2002122700045 20021227 00045 2002 12 27 HEEA082500 4 20021213 A 3450 7645001010043 CONTROLLER SKRSKY S76 S76A 8143006 NE COMPASS WILL NOT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 760158 NO METER MOVEMENT WHEN TESTED ON AIRCRAFT. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H1NE 2002122700046 20021227 00046 NM 2002 12 27 AWXA200201241 1 20021211 A 5313 69414372 TIE CLIP BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 0 0 23712 YVR - MAJOR REPAIR - DURING C-16 CHECK A 3/8" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 663, STR 10 L/H. MAINTENANCE RE MOVED THE DAMAGED STRINGER TIE CLIP AT BS 663, STR 10 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-414 37; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 12. 2 L 7 2 4F RT A16WE 2002122700047 20021227 00047 NM 2002 12 27 AWXA200201242 1 20021211 A 5313 69414372 TIE CLIP BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 0 0 23712 YVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 2 L/H. MAINTENANCE REMOV ED THE DAMAGED STRINGER TIE CLIP AT BS 616, STR 2 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 12. 2 L 7 2 4F RT A16WE 2002122700048 20021227 00048 NM 2002 12 27 AWXA200201243 1 20021211 A 5313 69414372 TIE CLIP BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 0 0 23712 YVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 1. MAINTENANCE REMOVED T HE DAMAGED STRINGER TIE CLIP AT BS 616, STR 1; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INST ALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 12. 2 L 7 2 4F RT A16WE 2002122700049 20021227 00049 NM 2002 12 27 AWXA200201244 1 20021211 A 5313 69414372 TIE CLIP BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 0 0 23712 YVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 2 R/H. MAINTENANCE REMOV ED THE DAMAGED STRINGER TIE CLIP AT BS 616, STR 2 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 12. 2 L 7 2 4F RT A16WE 2002122700050 20021227 00050 NM 2002 12 27 AWXA200201245 1 20021211 A 5313 69414372 TIE CLIP BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 0 0 23712 YVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 663, STR 10 R/H. MAINTENANCE REMO VED THE DAMAGED STRINGER TIE CLIP AT BS 663, STR 10 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437 ; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 12. 2 L 7 2 4F RT A16WE 2002122700051 20021227 00051 WP 2002 12 27 MWEA020762 1 20021227 A 5311 995823879 FRAME DOUG DC9 DC981 3022081 WP STA 1322 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 AFT CARGO COMPARTMENT HAS MODERATE CORROSION ON TOP OF FRAME AT STATION 1322 LONGERON 29 RIGHT AND 26 RIGHT. -- REMOVE D DAMAGED SECTION, LOCATED AND DRILLED AND INSTALLED NEW SECTION. 2 L 7 2 4F A6WE 2002122700052 20021227 00052 NE 2002 12 27 HEEA082502 1 20021213 A 7714 7645001076103 INDICATOR SKRSKY S76 S76A 8143006 NE TRIPLE TACH MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 TROUBLSHOT DIFFERENCE BETWEEN PILOT AND COPILOT INDICATOR. 1 G 7 2 3U H1NE 2002122700053 20021227 00053 NE 2002 12 27 HEEA082503 1 20021213 A 2930 7645001078104 INDICATOR SKRSKY S76 S76A 8143006 NE HYD PRESSURE READS LOW E HEEA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 03 22342 760096 HYDRAULIC PRESSURE INDICATOR READS LOW. 1 G 7 2 3U H1NE 2002122700054 20021227 00054 NE 2002 12 27 HEEA082504 1 20021213 A 7931 7645001078112 INDICATOR SKRSKY S76 S76A 8143006 NE OIL PRESSURE INTERFERENCE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 INTERMITTENT INDICATION OF OIL PRESSURE. 1 G 7 2 3U H1NE 2002122700056 20021227 00056 NE 2002 12 27 HEEA082506 1 20021213 A 2140 7650007904101 PRESSURE SWITCH SKRSKY S76 S76A 8143006 NE HEATER MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 HEATER SWITCH ON TRANSMISSION LIGHT WOULD NOT COME ON. SCRAPPED. 1 G 7 2 3U H1NE 2002122700057 20021227 00057 NE 2002 12 27 HEEA082507 1 20021213 A 2420 7655009005104 GCU SKRSKY S76 S76A 8143006 NE AC SYSTEM WILL NOT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 AC GENERATOR CONTROL UNIT WOULD NOT TEST IN OVERVOLTAGE CHECK. 1 G 7 2 3U H1NE 2002122700058 20021227 00058 NM 2002 12 27 QXEA0202263 1 20021226 A 2130 DOOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 DIRTY A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 410QX 4053 BOI - FLIGHT 02391 - ON CLIMB OUT, THE AIRCRAFT WOULD NOT PRESSURIZE. LOUD WHISTLING NOISE WAS HEARD BY FLIGHT ATTENDANT . MAINTENANCE INSPECTED THE AIRCRAFT AND CLEANED DEBRIS FROM THE REAR PASSENGER DOOR SEAL. MAINTENANCE ALSO VERIFIED THA T NO FAULTS WERE LOGGED ON THE CDS. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SER VICE. 2 H 7 2 4T RT A13NM 2002122700059 20021227 00059 NE 2002 12 27 HEEA082508 1 20021213 A 3297 CONNECTOR SKRSKY S76 S76A 8143006 NE WIRE HARNESS CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 476X 760436 WIRE HARNESS CONNECTOR CORRODED. SCRAPPED. 1 G 7 2 3U H1NE 2002122700060 20021227 00060 NE 2002 12 27 HEEA082509 1 20021213 A 3340 7655002005102 SEARCH LIGHT SKRSKY S76 S76A 8143006 NE EXTERIOR MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 476X 760436 SEARCH LIGHT WILL NOT TURN OFF. REPAIRED. 1 G 7 2 3U H1NE 2002122700061 20021227 00061 NE 2002 12 27 HEEA082510 1 20021213 A 2420 7655009005104 GCU SKRSKY S76 S76A 8143006 NE AC SYSTEM INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 AC GENERATOR GCU INOPERATIVE. 1 G 7 2 3U H1NE 2002122700062 20021227 00062 NE 2002 12 27 HEEA082511 1 20021213 A 2421 7655009005105 GENERATOR SKRSKY S76 S76A 8143006 NE AC SYSTEM INOPERATIVE E HEEA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 SW 03 1545X 760050 GENERATOR INOPERATIVE AFTER FLYING THROUGH HEAVY RAIN. 1 G 7 2 3U H1NE 2002122700063 20021227 00063 NE 2002 12 27 HEEA082512 1 20021213 A 2434 7655009006106 CONTROL UNIT SKRSKY S76 S76A 8143006 NE DC SYSTEM MALFUNCTIONED E HEEA O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 SW 03 1546G 760076 DIFFICULT TO RESET, APP. 30 SECOND DELAY FROM SWITCH ACTIVATION TO GENERATOR ON LINE. 1 G 7 2 3U H1NE 2002122700064 20021227 00064 2002 12 27 HEEA082513 4 20021213 A 3421 7660002113103 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT MELTED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 VERTICAL GYRO CAUSES KICK IN AFCS. 1 G 7 2 3U H1NE 2002122700065 20021227 00065 2002 12 27 HEEA082514 4 20021213 A 3421 7660002113103 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 VERTICAL GYRO SPINS IN PITCH AND ROLL, OFF FLAG WILL NOT PULL. 1 G 7 2 3U H1NE 2002122700066 20021227 00066 2002 12 27 HEEA082515 4 20021213 A 3421 7660002113103 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 913UK 760276 PILOTS REPORT NR 1 AFCS PITCH CHANNEL ACTUATOR KICKS IN CRUISE FLIGHT. 1 G 7 2 3U H1NE 2002122700067 20021227 00067 SO 2002 12 27 C2XA02BT086 1 20021224 A 3350 INVERTER EMB 145 EMB145 3260210 SO FAULTY A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 16112 145660 EWR---CO3547, CREW REPORTED, LEFTSIDE EMERGENCY LIGHT INOPERATIVE ON SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED EME RGENCY LIGHT INVERTER IAW EMB145 AMM #33-50-11. OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2002122700068 20021227 00068 WP 2002 12 27 MWEA020765 1 20021227 A 5311 59560655 NUT PLATE DOUG DC9 DC915 3022036 WP SLANT PANEL CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 PRESSURE SLANT PANEL CORRODED AROUND LOWER NUT PLATES ON LEFT SIDE FROM APPROXIMATELY 22 INCHES TO 44 INCHES FROM CENTER LINE. -- FABRICATED AND INSTALLED NEW SLANT PANEL AND INSTALLED NUT PLATES. 2 L 7 2 4F A6WE 2002122700069 20021227 00069 WP 2002 12 27 MWEA020766 1 20021227 A 5311 5910163255 DOUBLER DOUG DC9 DC915 3022036 WP 5 O'CLOCK CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FORWARD FACE OF THE AFT PRESSURE BULKHEAD AT THE FIVE O'CLOCK POSITION PLUG DOOR JAMB PIN HOLDER IS CRACKED. -- FABRIC ATED AND INSTALLED FINGER DOUBLER AND REPAIR DOUBLER. 2 L 7 2 4F A6WE 2002122700070 20021227 00070 WP 2002 12 27 MWEA020767 1 20021227 A 5311 5910163255 DOUBLER DOUG DC9 DC915 3022036 WP 7 O'CLOCK CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FORWARD FACE OF THE AFT PRESSURE BULKHEAD AT THE SEVEN O'CLOCK POSTION DOOR JAMB PIN HOLDER IS CRACKED. -- FABRICATED AND INSTALLED FINGER DOUBLER AND DOUBLER. 2 L 7 2 4F A6WE 2002122700071 20021227 00071 EU 2002 12 27 RAIA00212356 1 20021216 A 3350 0341519 FUSE AEROSP ATR72 ATR72202 8680940 EU BROKEN A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 723TE 283 MX-STL- EMERGENCY PATH LIGHTING HAS FOUR LIGHTS OUT. REMOVED AND REPLACED FUSE AT FWD POWER SUPPLY, OPS CK OK. 2 H 7 2 4T RT A53EU 2002122700072 20021227 00072 2002 12 27 RAIA00212357 4 20021216 A 3418 7001840937 ALTIMETER EMB 145 EMB145 3260210 SO INTERMITTENT A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 803HK 7775 145077 5316-PIT- STALL PROTECTION SYSTEM 2 INOP INDICATION. MAINTENANCE REMOVED AND REPLACED THE RADIO ALTIMETER, OPS CK OK. 2 L 7 2 4F RT T00011AT 2002122700073 20021227 00073 EU 2002 12 27 RAIA00212358 1 20021217 A 3230 350452005009 COMPUTER AEROSP ATR72 ATR72202 8680940 EU DAMAGED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 722TE 12848 4288 220 5590-STL- LANDING GEAR HANDLE WILL NOT GO UP. MAINTENANCE REMOVED AND REPLACED BOTH MULTI FUNCTION COMPUTER, OPS CK OK 2 H 7 2 4T RT A53EU 2002122700074 20021227 00074 EU 2002 12 27 RAIA00212359 1 20021217 A 2421 243211 GCU AEROSP ATR42 ATR42300 8680920 EU DEFECTIVE A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 422TE 27046 14775 106 5463-BMI- SMOKE SMELL IN COCKPIT AND #1 A/C WILD GENERATOR FAULT INDICATION. MAINTENANCE REMOVED AND REPLACED THE #1 A/C WILD GENERATOR CONTROL UNIT, OPS CK OK. 2 H 7 2 4T RT A53EU 2002122700075 20021227 00075 2002 12 27 RAIA00212362 4 20021222 A 3160 35133672101 DISPLAY AEROSP ATR42 ATR42300 8680920 EU MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 421TE 25757 24 102 5460-STL- THE "T/O INHI" LIGHT FAILS TO STAY ILLUMINATED BEFORE TAKE-OFF. MAINTENANCE REMOVED AND REPLACED THE CENTRAL C REW ALERT SYSTEM DISPLAY, OPS CK OK. 2 H 7 2 4T RT A53EU 2002122700076 20021227 00076 EU 2002 12 27 RAIA00212363 1 20021223 A 3350 1317 BULB JETAIR JETSTM JETSTM4101 1500501 EU BURNED OUT A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 557HK 41074 5407-RIC- EMERGENCY LIGHT AT 9A INOP. REMOVED AND REPLACED BULB, OPS CK OK. 2 L 7 2 4T RT A41NM 2002122700077 20021227 00077 EU 2002 12 27 RAIA00212364 1 20021223 A 3260 AIR135692 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 568HK 41086 5512-STL- LEFT RED BETA, ICE, AND TAT ANNUNCIATOR LIGHTS ILLUMINATED ON TAXI OUT. MAINTENANCE REMOVED AND REPLACED THE L EFT MLG AOG SWITCH, OPS CK OK. 2 L 7 2 4T RT A41NM 2002122700078 20021227 00078 EU 2002 12 27 RAIA00212365 1 20021224 A 3097 B03AA1031 VALVE AEROSP ATR42 ATR42300 8680920 EU DEFECTIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 423TE 7125 4659 119 5600-STL- AIRFRAME DE-ICE FAULT. MAINTENANCE REMOVED AND REPLACED THE LEFT WING DE-ICE DISTRIBUTOR VALVE, OPS CK OK. 2 H 7 2 4T RT A53EU 2002122700079 20021227 00079 EU 2002 12 27 RAIA00212366 1 20021224 A 7930 31056294 BETA SWITCH JETAIR JETSTM JETSTM4101 1500501 EU INTERMITTENT A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 553HK 5859 2734 41066 5623-STL- RIGHT PROPELLER GREEN BETA LIGHT INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT BETA SWITCH. 2 L 7 2 4T RT A41NM 2002122700080 20021227 00080 2002 12 27 RAIA00212367 4 20021224 A 3420 7003110901 INDICATOR JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 564HK 14329 7366 41081 5502-STL- CAPTAIN LOWER EFIS SCREEN WENT BLANK. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S ELECTRONIC FLIGHT INSTRUM ENT SYSTEM INDICATOR, OPS CK OK 2 L 7 2 4T RT A41NM 2002122700081 20021227 00081 EU 2002 12 27 RAIA00212368 1 20021226 A 2613 51228801 ELEMENT JETAIR JETSTM JETSTM4101 1500501 EU SHORTED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 573HK 41092 5597-STL-RIGHT OVER HEAT LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVER HEAT ELEMENT, OPS CK OK. 2 L 7 2 4T RT A41NM 2002122800001 20021228 00001 SO 2002 12 28 C2XA02SH157 1 20021228 A 5300 14522461011 DOUBLER EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 SHV- DURING C CHECK TWO DOUBLERS WERE FOUND TO HAVE CORROSION ON RIGHT OMEGA BEAM BETWEEN FRAMES 20 AND 22. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED DOUBLERS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE . 2 L 7 2 4T RT T00011AT 2002122800002 20021228 00002 SO 2002 12 28 C2XA02SH160 1 20021228 A 5400 14576599003 STIFFENER EMB 145 EMB145LR 3260212 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 SHV- DURING C CHECK NUMBER ONE LOWER COWLING AFT STIFFENER WAS FOUND GOUGED. MAINTENANCE REMOVED AND REPLACED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122800003 20021228 00003 SO 2002 12 28 C2XA02SH162 1 20021228 A 5400 14576631011 STIFFENER EMB 145 EMB145LR 3260212 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 SHV- DURING C CHECK NUMBER ONE COWLING STIFFENER AT STATION 2180 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2002122900001 20021229 00001 EU 2002 12 29 CX7A194J28 1 20021224 A 2731 SA614A1503 BUSHING SAAB SF340 340B 7860101 EU EXCESS PLAY A CX7A A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 03 303CE 340B194 AIR RETURN - PITCH VIBRATION FELT THROUGH CONTROL YOKE 2 L 7 2 4T RT A52EU 2002122900002 20021229 00002 SO 2002 12 29 C2XA02TY187 1 20021229 A 5320 14522459003 ANGLE EMB 135 EMB135LR 3260305 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17521 145378 TYS, During a scheduled inspection corrosion was found on the center omega beam ramp angle. Maintenance removed and repl aced the ramp angle I/A/W-EMB-135/145-SRM-51-40-02. The repair was satisfactory and the aircraft will be released upon c omplection of inspection. 2 L 7 2 4F RT T00011AT 2002122900003 20021229 00003 SO 2002 12 29 C2XA02TY190 1 20021229 A 3220 14522717001 WEB EMB 135 EMB135LR 3260305 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17521 145378 TYS, During a scheduled inspection the nose gear, right eschutcheon plate and rivet head was found gouged. Maintenance b lended out the gouged area, replaced the rivet and performed dyt-pen inspection, alodined, primed and painted I/A/W-GST- 3715/02. The repair was satisfactory and the aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2002122900004 20021229 00004 SO 2002 12 29 C2XA02TY191 1 20021229 A 5550 14525021407 BRACKET EMB 135 EMB135LR 3260305 SO GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17521 145378 TYS, During a scheduled inspection the left hand horizontal stab. actuator mounting bracket was found gouged. Maintenanc e removed and replaced the fitting I/A/W-EMB-135/145-SRM-51-40-02, CMP-51-21-04, 05 and 06. The repair was satisfactory and the aircraft will be released upon complection of inspection. 2 L 7 2 4F RT T00011AT 2003062500066 20030625 00066 EU 2003 6 25 YENA200235 1 20021229 A 2910 D2901010200800 TUBE AIRBUS 320 A320232 3930326 EU HYD SYSTEM LEAKING A YENA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 503JB 1123 APPROX 1 HOUR AFTER DEPARTURE FROM JFK, FLT. 91, CREW REPORTED GREEN HYD SYSTEM QTY LOW. APPROX 1 HOUR LATER CREW REPOR TED ECAM GRN RES LOW QTY. CREW C/W ECAM ACTION, DISCUSSED OAK ARRIVAL ACTION. GRAVITY GEAR EXTENSION, ALT BRAKES AVAIL ABLE AND HAVING A/C MAINT MEET AIRCRAFT AT END OF RUNWAY WITH TUG AND TOWBAR. CREW AS PRECAUTIONARY DECLARED EMERGENCY. FOUND EDP CASE DRAIN LINE LEAKING IN PYLON. REPLACEMENT LINE NOT AVAILABLE LOCALLY. PERMASWAGE OR RYNGLOC PERMANENT REPAIR NOT AN OPTION DUE TO SPACE CONSTRAINTS. C/W TEMP FLEX LINE REPAIR IAW AMM 20-23-11-300-004. PERMANENT REPAIR DU E AT NEXT -A- CHECK AND DAILY REINSPECT REQUIRED. 2 L 7 2 4F RT A28NM 2002123000001 20021230 00001 NE 2002 12 30 HEEA082481 1 20021213 A 3212 7625101102105 ELBOW SKRSKY S76 S76A 8143006 NE EMERGENCY FLOAT DETERIORATED E O OTHER O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 ELBOW ON EMERGENCY FLOAT IS DETERIORATED. 1 G 7 2 3U H1NE 2002123000002 20021230 00002 NE 2002 12 30 HEEA082516 1 20021213 A 3230 7665001801103 BOTTLE SKRSKY S76 S76A 8143006 NE MLG LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 BLOW DOWN LEAKING AT HEAD CONNECTION. REPAIRED. 1 G 7 2 3U H1NE 2002123000003 20021230 00003 NE 2002 12 30 HEEA082517 1 20021213 A 3230 VALVE SKRSKY S76 S76A 8143006 NE BLOWDOWN BOTTLE LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 827 760193 LANDING GEAR WILL NOT RETRACT. INSPECTED AND FOUND EMERGENCY BLOW DOWN BOTTLE VALVE LEAKING. THIS MOVED THE LANDING GE AR CONTROL VALVE TO BYPASS PREVENTING LANDING GEAR RETRACTION. REPAIRED. 1 G 7 2 3U H1NE 2002123000004 20021230 00004 NE 2002 12 30 HEEA082518 1 20021213 A 6200 7665001802102 VTA ACTUATOR SKRSKY S76 S76A 8143006 NE M/R SYSTEM LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 VTA ACTUATOR LEAKING. 1 G 7 2 3U H1NE 2002123000005 20021230 00005 NE 2002 12 30 HEEA082519 1 20021213 A 6321 7665009803103 POWERPACK SKRSKY S76 S76A 8143006 NE ROTOR BRAKE MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 761PH 760224 WILL NOT MAINTAIN PRESSURE. KEEPS CYCLING ON. 1 G 7 2 3U H1NE 2002123000006 20021230 00006 NE 2002 12 30 HEEA082520 1 20021213 A 2913 SEAL SKRSKY S76 S76A 8143006 NE HYD PUMP LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 4253S 198731 760035 HYDRAULIC PUMP SEAL IS LEAKING. 1 G 7 2 3U H1NE 2002123000007 20021230 00007 2002 12 30 HEEA082521 4 20021213 A 2215 7690001802106 ACTUATOR SKRSKY S76 S76A 8143006 NE AFCS INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 AFCS ACTUATOR NR 1 ROLL INOPERATIVE. 1 G 7 2 3U H1NE 2002123000008 20021230 00008 2002 12 30 HEEA082522 4 20021213 A 2215 7690001802106 ACTUATOR SKRSKY S76 S76A 8143006 NE AFCS INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22342 760096 AFCS ACTUATOR NR 1 YAW INOPERATIVE. 1 G 7 2 3U H1NE 2002123000009 20021230 00009 2002 12 30 HEEA082523 4 20021213 A 2215 7690001802106 ACTUATOR SKRSKY S76 S76A 8143006 NE AFCS INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 AFCS ACTUATOR INOPERATIVE. 1 G 7 2 3U H1NE 2002123000010 20021230 00010 2002 12 30 HEEA082524 4 20021213 A 2215 7690001802106 ACTUATOR SKRSKY S76 S76A 8143006 NE AFCS INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546K 760082 AFCS ACTUATOR INOPERATIVE. 1 G 7 2 3U H1NE 2002123000011 20021230 00011 2002 12 30 HEEA082525 4 20021213 A 3422 7690001808102 GYRO SKRSKY S76 S76A 8143006 NE RATE OR CLIMB MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22342 760096 RATE GYRO RT FLAG REMAINED. 1 G 7 2 3U H1NE 2002123000012 20021230 00012 NE 2002 12 30 HEEA082526 1 20021213 A 6240 7690001881103 AMPLIFIER SKRSKY S76 S76A 8143006 NE VIB ABSORBER MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 VTA WILL NOT TUNE. 1 G 7 2 3U H1NE 2002123000013 20021230 00013 2002 12 30 HEEA082527 4 20021213 A 3442 78808659008 DISPLAY SKRSKY S76 S76A 8143006 NE WX RADAR SYS INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 WEATHER RADAR DISPLAY HAS AN INOPERATIVE DISPLAY. 1 G 7 2 3U H1NE 2002123000014 20021230 00014 2002 12 30 HEEA082528 4 20021213 A 3442 78806059008 DISPLAY SKRSKY S76 S76A 8143006 NE WX RADAR SYS INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 WEATHER RADAR SYSTEM DISPLAY INOPERATIVE. 1 G 7 2 3U H1NE 2002123000015 20021230 00015 2002 12 30 HEEA082529 4 20021213 A 3442 80510800001 INDICATOR SKRSKY S76 S76A 8143006 NE WX RADAR SYS BURNED OUT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 WEATHER RADAR SYSTEM CAUSED TWO INDICATORS TO BURN OUT. REPAIRED. 1 G 7 2 3U H1NE 2002123000016 20021230 00016 2002 12 30 HEEA082530 4 20021213 A 3442 80510800001 RADAR SKRSKY S76 S76A 8143006 NE WX SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 ERROR CODE 30 AND RECONFIGURING DOES NOT HELP. REPAIRED. 1 G 7 2 3U H1NE 2002123000017 20021230 00017 2002 12 30 HEEA082531 4 20021213 A 3457 8143902240B GPS SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 760158 GPS DOES NOT POWER UP. CYCLED POWER SEVERAL TIMES. 1 G 7 2 3U H1NE 2002123000018 20021230 00018 2002 12 30 HEEA082532 4 20021213 A 3457 8143902240B DISPLAY SKRSKY S76 S76A 8143006 NE GPS SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 760158 GPS DISPLAY BLINKS THROUGHOUT ALL OPERATIONS. 1 G 7 2 3U H1NE 2002123000019 20021230 00019 2002 12 30 HEEA082533 4 20021213 A 3457 8143902240B GPS SKRSKY S76 S76A 8143006 NE COCKPIT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 760047 BROKEN KNOB. FOUND ON/OFF KNOB MISSING AND ON/OFF SWITCH SHAFT BROKEN. REPLACED KNOB AND SWITCH. CLEANED FACEPLATE AND TOUCHED UP WITH BLACK PAINT. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002123000020 20021230 00020 2002 12 30 HEEA082534 4 20021213 A 3457 8143902240B GPS SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 761PH 760224 ANTENNA FAULT, RAIM UNRELIABLE. SENT TO ASM FREEFLIGHT FOR INSPECTION AND REPAIR. 1 G 7 2 3U H1NE 2002123000021 20021230 00021 2002 12 30 HEEA082535 4 20021213 A 3416 8800T ENCODER SKRSKY S76 S76A 8143006 NE ALTIMETER MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 ENCODER CAUSES EXTERNAL ALTIMETER "ERROR" TO BE DISPLAYED ON GPS. 1 G 7 2 3U H1NE 2002123000022 20021230 00022 NE 2002 12 30 HEEA082537 1 20021213 A 7700 9550158500 THERMOCOUPLE SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1S1 60030 NE ENGINE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 761PH 760224 3505TEC THERMOCOUPLE LEAD HAS OPEN IN THERMOCOUPLE END. 1 G 7 2 3U 3 U H1NE E19EU 2002123000023 20021230 00023 NE 2002 12 30 HEEA082538 1 20021213 A 2430 A1077B RELAY SKRSKY S76 S76A 8143006 NE DC SYSTEM INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 BUS TIE RELAY CONTACTOR INOPERATIVE. 1 G 7 2 3U H1NE 2002123000024 20021230 00024 NE 2002 12 30 HEEA082539 1 20021213 A 2430 A1077D RELAY SKRSKY S76 S76A 8143006 NE DC GENERATOR FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 NR 2 GENERATOR REQUIRES RESET AFTER EACH START. 1 G 7 2 3U H1NE 2002123000025 20021230 00025 2002 12 30 HEEA082540 4 20021213 A 2340 A3016W INTERPHONE SKRSKY S76 S76A 8143006 NE CABIN DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 KNOB CRACKED. FOUND AMP BOARD AR2, SWITCH S1, SELECTOR KNOB AND VOLUME KNOB BAD. REPLACED SAME. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002123000026 20021230 00026 2002 12 30 HEEA082541 4 20021213 A 2340 SWITCH SKRSKY S76 S76A 8143006 NE INTERPHONE BOX DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546K 0205393 760082 FM BLEEDING OVER. FOUND SWITCHES S1, S2, S7, S9, S10, S11 BAD. REPLACED SAME. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002123000027 20021230 00027 2002 12 30 HEEA082542 4 20021213 A 2340 FACEPLATE SKRSKY S76 S76A 8143006 NE INTERPHONE BOX DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 7602015 760047 FACEPLATE WORN. FOUND LIGHT PANEL AND SELECTOR KNOB BAD. REPLACED. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002123000028 20021230 00028 2002 12 30 HEEA082543 4 20021213 A 2340 FACEPLATE SKRSKY S76 S76A 8143006 NE INTERPHONE BOX DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911UK 7803033 760275 FACEPLATE OF CONTROL DEFACED. INSTALLED NEW FACEPLATE AND ALSO NEW VOLUME AND SELECTOR KNOBS. REPAIRED. BENCH CHECK GO OD. 1 G 7 2 3U H1NE 2002123000029 20021230 00029 2002 12 30 HEEA082544 4 20021213 A 2397 WIRE SKRSKY S76 S76A 8143006 NE INTERPHONE BOX BROKEN E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 8001131 760035 SIDETONE WEAK. FOUND TRANSFORMER T1 BAD AND BROKEN WIRE ON PIN 1. REPLACED. RESOLDERED BROKEN WIRE. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002123000030 20021230 00030 2002 12 30 HEEA082545 4 20021213 A 2340 A3016W INTERPHONE SKRSKY S76 S76A 8143006 NE CABIN MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5426U 760167 GARBLED FM. COULD NOT DUPLICATE PROBLEM BUT FOUND LIGHT PANEL NOT LIGHTING UP. REPAIRED CONNECTIONS TO LIGHT PANEL CONN ECTOR AND REPLACED 3 BAD LAMPS INSIDE LIGHT PANEL. REPAIRED. FOUND MONITOR SWITCHES S2 - S11 BAD. REPLACED S2 - S11 M ONITOR SWITCHES. REPAIRED. ALSO REPLACED BAD SELECTOR KNOB. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002123000031 20021230 00031 2002 12 30 HEEA082546 4 20021213 A 2340 A3016W INTERPHONE SKRSKY S76 S76A 8143006 NE CABIN MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546G 760076 FM2 INTERMITTENT. COULD NOT VERIFY COMPLAINT. FOUND SELECTOR KNOB BAD. REPLACED SAME. REPAIRED. TOUCHED PAINT ON FA CEPLATE. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002123000032 20021230 00032 2002 12 30 HEEA082547 4 20021213 A 2340 A3016W INTERPHONE SKRSKY S76 S76A 8143006 NE CABIN DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 CANNOT EQUALIZE VOL BETWEEN VHF AND INT. COULD NOT VERIFY COMPLAINT. TOUCHED UP PAINT. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002123000033 20021230 00033 2002 12 30 HEEA082548 4 20021213 A 2330 FUSE SKRSKY S76 S76A 8143006 NE PA SIREN FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 1281 760158 WILL NOT POWER UP. FOUND FUSE F101 BAD. REPLACED SAME. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002123000034 20021230 00034 NE 2002 12 30 HEEA082549 1 20021213 A 3212 D24676108 FLOAT SKRSKY S76 S76A 8143006 NE MLG LEAKING E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1546K 760082 RT MAIN FLOAT BAG LEAKING. 1 G 7 2 3U H1NE 2002123000035 20021230 00035 2002 12 30 HEEA082550 4 20021213 A 3442 FUSE SKRSKY S76 S76A 8143006 NE WX RADAR SYS BURNED OUT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 RADAR SYSTEM INOPERATIVE. FOUND FUSE BURNED. REPLACED TRANSISTORS Q601, Q604, AND Q605. REPAIRED PROBLEM. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002123000036 20021230 00036 2002 12 30 HEEA082551 4 20021213 A 3442 MI5852013 INDICATOR SKRSKY S76 S76A 8143006 NE WX RADAR SYS INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 WEATHER RADAR SYSTEM INDICATOR SHUTS OFF THEN ON INTERMITTENTLY. CLEANED DIRTY "CYC" SWITCH ON ASSY. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 2002123000037 20021230 00037 2002 12 30 HEEA082553 4 20021213 A 3413 RC30VIL INDICATOR SKRSKY S76 S76A 8143006 NE RATE OF CLIMB INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22342 760096 RATE OF CLIMB INDICATOR INTERIOR LIGHTING IS INTERMITTENT. SENT TO MASCO FOR INSPECTION AND REPAIR. 1 G 7 2 3U H1NE 2002123000038 20021230 00038 2002 12 30 HEEA082554 4 20021213 A 3442 S672002 ANTENNA SKRSKY S76 S76A 8143006 NE WX RADAR SYS BROKEN E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 WEATHER RADAR OFF FLAG FLICKERS. FOUND ANTENNA TO BE BROKEN BEYOND REPAIR. SCRAPPED. 1 G 7 2 3U H1NE 2002123000039 20021230 00039 2002 12 30 HEEA082555 4 20021213 A 3442 S672002 ANTENNA SKRSKY S76 S76A 8143006 NE WX RADAR SYS DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 NO SIGNAL ON INDICATOR. ANTENNA MALFUNCTION. SCRAPPED. 1 G 7 2 3U H1NE 2002123000040 20021230 00040 NE 2002 12 30 HEEA082556 1 20021213 A 6220 SB5064102 BEARING SKRSKY S76 S76A 8143006 NE MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 MAIN ROTOR HAS A WORN BEARING. SCRAPPED. 1 G 7 2 3U H1NE 2002123000041 20021230 00041 SW 2002 12 30 HEEA082558 1 20021126 A 6510 206073913001 BLOWER BELL 206 206L3 1182108 SW TAIL ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 TAIL ROTOR COOLER BLOWER POPS NR 3 INVERTER CIRCUIT BREAKER. 1 G 7 1 3U H2SW 2002123000042 20021230 00042 2002 12 30 HEEA082559 4 20021202 A 2210 214074301105 AMPLIFIER BELL 214 214ST 1182106 SW SCAS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 SCAS AMPLIFIER ROLL TRIPS OFF. 2 G 7 2 4U H10SW 2002123000043 20021230 00043 SW 2002 12 30 HEEA082560 1 20021202 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 2002123000044 20021230 00044 2002 12 30 HEEA082563 4 20021206 A 2350 A3016W INTERPHONE BELL 212 212 1181420 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 102PH 30899 UNIT BLEEDS OVER WHEN FM IS SELECTED. PERFORMED PRELIMINARY INSPECTION. CLEANED S1 SELECTOR SWITCH. REPAIRED PROBLEM. ALSO REPLACED BAD LIGHT PANEL AND COMPLETED TESTING UNIT. UNIT BENCH CHECK GOOD. 1 G 7 1 4U H4SW 2002123000045 20021230 00045 SW 2002 12 30 HEEA082564 1 20021206 A 7714 BEARING BELL 212 212 1181420 SW TACH GENERATOR ROUGH E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 102PH D42 30899 INOPERATIVE. BALL BEARING ROUGH. REPAIRED AND REPLACED BALL BEARING. 1 G 7 1 4U H4SW 2002123000046 20021230 00046 SW 2002 12 30 HEEA082565 1 20021206 A 7100 4068T96P01 PRESSURE SWITCH BELL 214 214ST 1182106 SW ENGINE MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5748M 28102 PRESSURE SWITCH MALFUCNTIONED, BLOWER LIGHT WOULD FLICKER. PENDING VENDOR RETURN. 2 G 7 2 4U H10SW 2002123000047 20021230 00047 SW 2002 12 30 HEEA082566 1 20021206 A 6322 SHAFT BELL 214 214ST 1182106 SW BLOWER ASSY BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 SUSJ2258 28140 NR 2 ENGINE PARTICLE SEPERATOR BLOWER SHAFT BROKEN. RETURNED TO VENDOR. 2 G 7 2 4U H10SW 2002123000048 20021230 00048 2002 12 30 HEEA082567 4 20021206 A 3457 13824120234 RECEIVER CLARK 1000 1000CLARK 2230102 SW GPS MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 GPS RECEIVER SHOWS INTERNAL BATTERY FAILURE AND WILL RETAIN MEMORY. FOUND BATTERY VOLTAGE GOOD BUT NO USER WAYPOINTS. P ROGRAMMED NEW USER WAYPOINTS AND UNIT BENCH CHECK GOOD. 1 Q 7 1 3R 2A6 2002123000049 20021230 00049 SW 2002 12 30 HEEA082568 1 20021206 A 3340 GEARBOX BELL 230 230 1182149 SW SEARCH LIGHT SHORTED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 911RC 2164 23037 SEARCH LIGHT HAS AN ELECTRICAL SHORT LOCATED IN THE ROTATION AXIS GEARBOX. 1 G 7 2 3U NC H9SW 2002123000050 20021230 00050 EU 2002 12 30 02361306 1 20021227 A 2432 BATTERY PACK JETAIR JETSTM JETSTM4101 1500501 EU A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 306UE 41020 During preflight inspection, the crew reported that the aft portion of floor tracking emergency lights will not illumina te on battery. Maintenance personnel removed and replaced batery. Ops ck'd ok. Aircraft returned to service. 2 L 7 2 4T RT A41NM 2002123000051 20021230 00051 CE 2002 12 30 GLBA2002212 1 20021228 A 2400 SPC10 INVERTER BEECH 1900 1900D 1154162 CE A GLBA D RETURN TO BLOCK O OTHER CL CLIMB 1 NM 03 170GL 999 UE170 LH INVERTER FAILED, R&R INVERTER 2 L 7 2 4T RT A24CE 2002123000052 20021230 00052 2002 12 30 HEEA082569 4 20021209 A 3442 MI5852013 INDICATOR CLARK 1000 1000CLARK 2230102 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 UPON INITIAL INSTALLATION FUNCTIONAL CHECK SHOWED INDICATOR DISPLAYS A FINE ONE INCH BLUE LINE CENTER LEFT SIDE OF SCREE N AND INTERMITTENTLY FLASHES TEST PATTERN. SENT FOR REPAIR. 1 Q 7 1 3R 2A6 2002123000053 20021230 00053 2002 12 30 HEEA082570 4 20021209 A 2312 TRANSISTOR BELL 212 212 1181420 SW TRANSCIEVER VHF FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5736D 2265 31135 VHF TRANSCIEVER HAS GARBLED TRANSMIT AND RECEIVE. REMOVED CORROSION FROM CHASSIS. REPLACED BAD Q110 TRANSISTOR SOCKET. FOUND REALIGNED RECEIVER AND TRANSMITTER. UNIT BENCH CHECK GOOD. 1 G 7 1 4U H4SW 2002123000054 20021230 00054 SW 2002 12 30 HEEA082571 1 20021209 A 6210 204031920003 DAMPER BELL 212 212 1181420 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 102PH 30899 DAMPER HAS WORN INNER MEMBER AND BEARING LOOSE. REPAIRED. REPLACED HOUSING P/N J99941 DUE TO WEAR. 1 G 7 1 4U H4SW 2002123000055 20021230 00055 2002 12 30 HEEA082572 4 20021209 A 2370 9806020023 CVR BELL 212 212 1181420 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3131S 30953 COCKPIT VOICE RECORDER CAUSES TEST LIGHT TO STAY ON. 1 G 7 1 4U H4SW 2002123000056 20021230 00056 SW 2002 12 30 HEEA082573 1 20021209 A 2421 ASH5845 INVERTER BELL 212 212 1181420 SW AC SYSTEM FAILED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 102PH 30899 AC INVERTER FAILED IN FLIGHT. 1 G 7 1 4U H4SW 2002123000057 20021230 00057 SW 2002 12 30 HEEA082574 1 20021209 A 3212 D24650112 FLOAT BELL 212 212 1181420 SW MLG FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3131S 30953 DURING MANUAL INFLATION INSPECTION, BAG FAILED AT 3 EACH INLET AREAS. BAG MATERIAL SEPARATED AT SWIVEL ATTACHMENT ALLOW ING NITROGEN TO ESCAPE OUTSIDE THE BAG. 1 G 7 1 4U H4SW 2002123000058 20021230 00058 2002 12 30 HEEA082575 4 20021209 A 2312 064102300 TRANSCEIVER BELL 214 214ST 1182106 SW VHF WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 59806 28140 VHF TRANSCIEVER WEAK AND GARBLED. ALIGNED TRANSMITTER AND ADJUSTED C/N SQUELCH. COMPLETED TESTING UNIT AND ADJUSTED CAR RIER SQUELCH AND SIDETONE. UNIT BENCH CHECK GOOD. 2 G 7 2 4U H10SW 2002123000059 20021230 00059 2002 12 30 HEEA082576 4 20021209 A 2312 064102300 TRANSCEIVER BELL 214 214ST 1182106 SW VHF WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 59806 28140 VHF TRANSCEIVER WEAK RECEIVE. COULD NOT DUPLICATE PROBLEM OF WEAK RECEIVE BUT FOUND RECEIVER COMPRESSOR NOT WORKING. RE PLACED BAD I303 IC CHIP. REPAIRED. REMOVED CORROSION FROM UNIT. ADJUSTED C/N SQUELCH, MIC GAIN, TRANSMIT COMPRESSOR A ND SIDETONE. UNIT BENCH CHECK GOOD. 2 G 7 2 4U H10SW 2002123000060 20021230 00060 2002 12 30 HEEA082577 4 20021209 A 3451 066106900 INDICATOR BELL 214 214ST 1182106 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5748M 28102 DME INDICATOR DISPLAYS "800 AL". REPLACED Q803 TRANSISTOR AND I803 (IC), REPAIRED. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 2002123000061 20021230 00061 2002 12 30 HEEA082578 4 20021209 A 3452 071119208 CONTROL UNIT BELL 214 214ST 1182106 SW COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 59806 28140 ATC TRANSPONDER DISPLAY IS UNREADABLE. FOUND IC I303 BAD, REPLACED, REPAIRED. CLEANED FACEPLATE. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 2002123000062 20021230 00062 WP 2002 12 30 ZW0A0213002 1 20021227 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP A ZW0A K NONE O OTHER NR NOT REPORTED 1 CE 13 9615W 53562 THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 7-7-02 STL. --CLOSED-- 2 L 7 2 4F RT A6WE 2002123000063 20021230 00063 SW 2002 12 30 HEEA082579 1 20021209 A 6200 BEARING BELL 214 214ST 1182106 SW TUBE ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N A16 28106 MAIN ROTOR HAS A WORN ROD END BEARING. REPAIRED AND REPLACED BEARING. 2 G 7 2 4U H10SW 2002123000064 20021230 00064 SW 2002 12 30 HEEA082580 1 20021209 A 6300 BEARING BELL 214 214ST 1182106 SW MAIN ROTOR DRIVE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 MAIN ROTOR DRIVE HAS WORN BEARINGS. REPAIRED AND REPLACED BEARINGS. 2 G 7 2 4U H10SW 2002123000065 20021230 00065 SW 2002 12 30 HEEA082581 1 20021209 A 6320 214001373101 IDLER GEAR BELL 214 214ST 1182106 SW MAIN ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 MAIN ROTOR HAS WORN BEARINGS. REPAIRED AND REPLACED BEARINGS. 2 G 7 2 4U H10SW 2002123000066 20021230 00066 SW 2002 12 30 HEEA082582 1 20021209 A 6420 214011801125 ROTOR HEAD BELL 214 214ST 1182106 SW TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 4979 28102 TAIL ROTOR HEAD HAS WORN BEARINGS. REPAIRED AND REPLACED BEARINGS. 2 G 7 2 4U H10SW 2002123000067 20021230 00067 SW 2002 12 30 HEEA082583 1 20021209 A 6420 SEAL BELL 214 214ST 1182106 SW T/R HEAD LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 1810 TR082400 28101 TAIL ROTOR HEAD GREASE SEAL LOOSE. REPAIRED. 2 G 7 2 4U H10SW 2002123000068 20021230 00068 SW 2002 12 30 HEEA082584 1 20021209 A 6210 214015300107 BLADE BELL 214 214ST 1182106 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 9877 28106 OUTBOARD ABRASION STRIP HAS SEVERAL HOLES AND A TRIM TAB DEBONDED. 2 G 7 2 4U H10SW 2002123000069 20021230 00069 SW 2002 12 30 HEEA082585 1 20021209 A 6300 BEARING BELL 214 214ST 1182106 SW RESTRAINT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 LK0376 28140 MAIN ROTOR DRIVE RESTRAINT ASSY HAS WORN BEARINGS. REPAIRED. 2 G 7 2 4U H10SW 2003021000138 20030210 00138 NM 2003 2 10 DHL2002747014 1 20021224 A 2612 WARNING LIGHT BOEING 727 727224 1384076 NM NR 1 ENGINE ILLUMINATED A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 747DH 22253 NR 1 ENGINE FIRE DETECTION GROUND FAULT LIGHT ILLUMINATED. DEFERRED IAW MEL 26-9 CONTROL 11371 ASSIGNED. 2 L 7 3 4F A3WE 2002123000070 20021230 00070 SW 2002 12 30 HEEA082586 1 20021209 A 6300 BEARING BELL 214 214ST 1182106 SW RESTRAINT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 MAIN ROTOR DRIVE RESTRAINT ASSY HAS WORN BEARINGS. REPAIRED. 2 G 7 2 4U H10SW 2002123000071 20021230 00071 SW 2002 12 30 HEEA082587 1 20021209 A 6300 BEARING BELL 214 214ST 1182106 SW STOP WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 STOP ASSY ON MAIN ROTOR DRIVE HAS WORN BEARINGS. REPAIRED. 2 G 7 2 4U H10SW 2002123000072 20021230 00072 SW 2002 12 30 HEEA082588 1 20021209 A 6510 214040600103 HANGER ASSY BELL 214 214ST 1182106 SW TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 HIGH IPS READING FROM AVMS. REPAIRED. REPLACED WORN BEARING. 2 G 7 2 4U H10SW 2002123000073 20021230 00073 SW 2002 12 30 HEEA082589 1 20021209 A 6510 214040600103 HANGER ASSY BELL 214 214ST 1182106 SW TAIL ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 HANGER ASSY HAS CORROSION PITS ON MOUNTING FACE. REPAIRED. REPLACED COUPLING DUE TO CORROSION. 2 G 7 2 4U H10SW 2002123000074 20021230 00074 SW 2002 12 30 HEEA082590 1 20021209 A 6510 214040600103 HANGER ASSY BELL 214 214ST 1182106 SW TAIL ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 HANGER ASSY HAS PLATING MISSING, CORROSION ON MOUNT FACE, ROUGH BEARING. REPAIRED. REPLACED BEARING. 2 G 7 2 4U H10SW 2002123000075 20021230 00075 SW 2002 12 30 HEEA082591 1 20021209 A 6510 214040600103 HANGER ASSY BELL 214 214ST 1182106 SW TAIL ROTOR VIBRATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 HANGER ASSY HAS VIBRATION - AVMS. REPAIRED. REPLACED BEARING DUE TO WORN AND BOLT DUE TO CORROSION. 2 G 7 2 4U H10SW 2002123000076 20021230 00076 SW 2002 12 30 HEEA082592 1 20021209 A 7120 214060207102 FITTING BELL 214 214ST 1182106 SW ENGINE MOUNT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 ENGINE MOUNT FITTING HAS WORN BEARINGS. REPAIRED. REPLACED BEARINGS. 2 G 7 2 4U H10SW 2002123000077 20021230 00077 NM 2002 12 30 EIAA2002146 1 20021227 A 3230 2089487 HOSE BOEING 747 747SR46 1384816 NM PIN HOLE A EIAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 NM 09 477EV 20784 #4HYD SYSTEM FLUID LOSS RETURNED TO HIKFOUND RUPUTRED HYDRAULIC ON RT WING GEAR FOR EXTENTION AND RETRACTION CYL. R&RD L INE, CKD CASE PRESSURE AND RETURN FILTER MODULES, DIFF PRESS INDICATORS FOR POPPED CONDITION. CHD CASE DRAIN FILTER MAG PLUGS, NO METAL FOUND. SERVICED #4 HYD SYS FULL. OPERATED GEAR DOOR OPS CKD NORMAL NO LEAKS NOTED. 2 L 7 4 4F RT A20WE 2002123000078 20021230 00078 SW 2002 12 30 HEEA082593 1 20021209 A 7100 6038T59P02 BLOWER BELL 214 214ST 1182106 SW ENGINE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 BLOWER ASSY PARTICLE SEPERATOR LIGHT CAME ON. FOUND SHAFT SHEARED. TO BE SENT TO VENDOR FOR REPAIR. 2 G 7 2 4U H10SW 2002123000079 20021230 00079 2002 12 30 HEEA082594 4 20021209 A 2340 A3016W INTERPHONE BELL 214 214ST 1182106 SW COMMS INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5748M 28102 COMM 1 AND COMM 2 CUTS OUT DURING TRANSMIT. FOUND SWITCH S1, FM1 DECAL AND FM2 DECAL BAD. REPLACED. REPAIRED. BENCH C HECK GOOD. 2 G 7 2 4U H10SW 2002123000080 20021230 00080 SW 2002 12 30 HEEA082595 1 20021209 A 6720 PHI214ST103 COUNTERWEIGHT BELL 214 214ST 1182106 SW TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 TAIL ROTOR COUNTERWEIGHT WORN. REPAIRED. 2 G 7 2 4U H10SW 2002123000081 20021230 00081 SW 2002 12 30 HEEA082596 1 20021209 A 6720 PHI214ST103 COUNTERWEIGHT BELL 214 214ST 1182106 SW TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 TAIL ROTOR COUNTERWEIGHT ASSY HAS WORN BEARINGS. REPAIRED. 2 G 7 2 4U H10SW 2002123000083 20021230 00083 SW 2002 12 30 HEEA082598 1 20021209 A 2432 RG214 BATTERY BELL 214 214ST 1182106 SW MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8045T 309 28101 MAIN BATTERY WEAK. 2 G 7 2 4U H10SW 2002123000084 20021230 00084 SW 2002 12 30 HEEA082599 1 20021209 A 2432 RG214 BATTERY BELL 214 214ST 1182106 SW MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8045T 309 28101 MAIN BATTERY WEAK. 2 G 7 2 4U H10SW 2002123000085 20021230 00085 SW 2002 12 30 HEEA082600 1 20021211 A 5320 214031270122S ANGLE BELL 214 214ST 1182106 SW FUSELAGE MISMANUFACTURED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 RT LOWER CAP ANGLE FOUND TO HAVE A TAB MISSING FROM THE AFT END OF TOP FLANGE, MAKING THE CAP 15/16 INCH TOO SHORT. 2 G 7 2 4U H10SW 2002123000086 20021230 00086 SW 2002 12 30 HEEA082601 1 20021211 A 6220 214010103115 SPINDLE BELL 214 214ST 1182106 SW M/R HEAD DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 MAIN ROTOR HEAD SPINDLE HAS THE FOLLOWING DISCREPANCIES: TANGS HAVE ROUGH CUT FINISH AND BORE HAS GOUGE IN PLATING. 2 G 7 2 4U H10SW 2002123000087 20021230 00087 SW 2002 12 30 HEEA082602 1 20021211 A 6220 214010103115 SPINDLE BELL 214 214ST 1182106 SW M/R HEAD DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 MAIN ROTOR HEAD SPINDLE HAS THE FOLLOWING DISCREPANCIES: (1 EACH) OF THE (7 EACH) HOLES AT THE END OF THE SPINDLE JOUR NAL IS COUNTER SUNK; (4 EACH) TANGS ROUGH CUT FINISH; (1 EACH) BUSHING TOO HIGH; AND (1 EACH) BUSHING TOO DEEP (WILL GOU GE OUT PAD ON YOKE). 2 G 7 2 4U H10SW 2002123000088 20021230 00088 SW 2002 12 30 HEEA082603 1 20021213 A 6300 206340300105 DRIVE SHAFT BELL 407 407 1182206 SW M/R DRIVE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 473 53188 INPUT DRIVESHAFT IS CORRODED. 1 G 7 1 3U O H2SW 2002123000089 20021230 00089 SW 2002 12 30 HEEA082604 1 20021213 A 6210 407015001117 BLADE BELL 407 407 1182206 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 3473 53159 MAIN ROTOR BLADE PEELING PAINT AT TOP SURFACE TIP END AND LOWER WEIGHT POCKET COVER SCREWS NOT SEALED HEAD SIDE. 1 G 7 1 3U O H2SW 2002123000090 20021230 00090 SW 2002 12 30 HEEA082605 1 20021213 A 6210 407015001117 BLADE BELL 407 407 1182206 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 447PH 1899 53114 MAIN ROTOR BLADE HAS WEIGHT POCKET UNBONDED AND SCREWS CORRODED. 1 G 7 1 3U O H2SW 2002123000091 20021230 00091 SW 2002 12 30 HEEA082606 1 20021213 A 6210 407015001117 BLADE BELL 407 407 1182206 SW MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 447PH 1989 53114 MAIN ROTOR BLADE WEIGHT POCKET UNBONDED AND SCREWS CORRODED. 1 G 7 1 3U O H2SW 2002123000092 20021230 00092 NE 2002 12 30 HEEA082607 2 20021213 A 7323 25249995 GOVERNOR BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE NR 1 ENGINE FAILED E HEEA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 03 3911L 33023 NR 1 ENGINE DECELERATED ON TAKEOFF. REPLACED NR 1 GOVERNOR. 1 G 7 2 4U 4 U H4SW E22EA 2002123000093 20021230 00093 EU 2002 12 30 HEEA082608 1 20021204 A 6340 1171265601 TRANSMITTER BOLKMS 117 BK117A1 5626010 EU XMSN OIL PRESS MALFUNCTIONED E HEEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 03 911TL 7198 AFTER LIFT OFF, TRANSMISSION OIL PRESSURE CAUTION LIGHT ILLUMINATED IN CONJUNCTION WITH LOWER THAN NORMAL READING ON NR 2 TRANSMISSION OIL PRESSURE GAUGE. REPLACED NR 2 TRANSMISSION OIL PRESSURE TRANSMITTER. 1 G 7 2 3U H13EU 2002123000094 20021230 00094 2002 12 30 HEEA082609 4 20021211 A 2312 064105430 TRANSCEIVER BOLKMS 117 BK117A1 5626010 EU VHF SYSTEM DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 911RZ 7092 VOLUME KNOB BROKEN. REPLACED ON/OFF VOLUME POTENTIOMETER, FACEPLATE, INSTALLED TWO SHIELDS ON BOTTOM OF MAIN BOARD THAT WERE MISSING, AND REPLACED DISPLAY. FIRED UNIT UP BUT NOTICED BLEED OVER ON DISPLAY. 1 G 7 2 3U H13EU 2002123000095 20021230 00095 2002 12 30 HEEA082610 4 20021211 A 3453 066402600 RECEIVER BOLKMS 105 BO105S 5626006 EU LORAN SYS DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6607K S841 LORAN RECEIVER LARGE KNOB ON LT SIDE HARD TO TURN. IN SHOP REPAIR. 1 G 7 2 3U H3EU 2002123000096 20021230 00096 EU 2002 12 30 HEEA082611 1 20021211 A 6210 10515150 BLADE BOLKMS 105 BO105S 5626006 EU MAIN ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136H 8409 S833 MAIN ROTOR BLADE TRAILING EDGE HAS SOME DAMAGE JUST OUTBOARD OF THE TRIM TAB. 1 G 7 2 3U H3EU 2002123000097 20021230 00097 EU 2002 12 30 HEEA082612 1 20021211 A 6220 10513143 ROD END BOLKMS 105 BO105S 5626006 EU MAIN ROTOR HEAD WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U S678 ROD END BEARING WORN. SCRAPPED. 1 G 7 2 3U H3EU 2002123000098 20021230 00098 EU 2002 12 30 HEEA082613 1 20021211 A 6220 10513144 ROD END BOLKMS 105 BO105S 5626006 EU MAIN ROTOR HEAD WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U S678 MAIN ROTOR HEAD ROD END BEARING WORN. SCRAPPED. 1 G 7 2 3U H3EU 2002123000099 20021230 00099 EU 2002 12 30 HEEA082614 1 20021211 A 6510 10531541 SHAFT BOLKMS 105 BO105S 5626006 EU TAIL ROTOR DRIVE PEELING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50293 5687 S677 TAIL ROTOR DRIVE SHAFT PLATING PEELING. REPAIRED. 1 G 7 2 3U H3EU 2002123000100 20021230 00100 EU 2002 12 30 HEEA082615 1 20021211 A 6420 10531703 ROTOR HEAD BOLKMS 105 BO105S 5626006 EU TAIL ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 135AE 7187 S838 UNABLE TO BALANCE TAIL ROTOR HEAD. REPAIRED. REPLACED TWO EACH BLADES DUE TO PAINT ERODED. 1 G 7 2 3U H3EU 2002123000102 20021230 00102 EU 2002 12 30 HEEA082617 1 20021211 A 7810 10560196 EXHAUST PIPE BOLKMS 105 BO105S 5626006 EU ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6607K S841 RT INBOARD EXHAUST STACK CRACKED. REPAIRED. 1 G 7 2 3U H3EU 2002123000103 20021230 00103 EU 2002 12 30 HEEA082619 1 20021211 A 6510 112131521 SHAFT BOLKMS 105 BO105S 5626006 EU TAIL ROTOR DRIVE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 9312 S828 FWD BEARING ROUGH; AFT BEARING DETERIORATED. REPLACED BEARINGS AND REPAIRED. 1 G 7 2 3U H3EU 2002123000104 20021230 00104 EU 2002 12 30 HEEA082620 1 20021211 A 6520 112131561 SHAFT BOLKMS 105 BO105S 5626006 EU TAIL ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50293 S677 TAIL ROTOR GEARBOX SHAFT HAS PLATING PEELING. REPAIRED. 1 G 7 2 3U H3EU 2002123000105 20021230 00105 EU 2002 12 30 HEEA082621 1 20021211 A 6220 117141071 ROTOR HEAD BOLKMS 117 BK117A1 5626010 EU MAIN ROTOR LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 8134 7092 MAIN ROTOR HEAD YELLOW GRIP LEAKS. REPAIRED. 1 G 7 2 3U H13EU 2002123000106 20021230 00106 EU 2002 12 30 HEEA082622 1 20021211 A 2822 1176415103 PUMP BOLKMS 117 BK117A1 5626010 EU FUEL BOOST INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 911RZ 7092 FUEL BOOST PUMP INOPERATIVE. REPAIRED. 1 G 7 2 3U H13EU 2002123000107 20021230 00107 NM 2002 12 30 AWXA200201249 1 20021210 A 5754 65C26602218 SLAT BOEING 737 7373S3 1384711 NM DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 0 0 23712 YVR - MAJOR REPAIR - DURING C-16 CHECK THE #5 SLAT WAS FOUND DELAMINATED AT THE OUTBOARD UPPER TRAILING EDGE SURFACE. MA INTENANCE REMOVED THE #5 SLAT AND REPAIRED DAMAGE IAW B737-300 SRM 51-70-10 REPAIR 22 & 23. REINSTALLED #5 SLAT IAW BMM 27-81-21, PG. 401-419. 2 L 7 2 4F RT A16WE 2002123000108 20021230 00108 NM 2002 12 30 AWXA200201250 1 20021209 A 5754 65C26603100 SLAT BOEING 737 7373S3 1384711 NM DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 0 0 23712 YVR - MAJOR REPAIR - DURING C-16 CHECK THE #4 SLAT WAS FOUND DELAMINATED AT THE INBOARD UPPER TRAILING EDGE SURFACE. MAI NTENANCE REMOVED THE #4 SLAT AND REPAIRED DAMAGE IAW B737-300 SRM 51-70-10 REPAIR 22 & 23. REINSTALLED #4 SLAT IAW BMM 2 7-81-21, PG. 401-419. 2 L 7 2 4F RT A16WE 2002123000109 20021230 00109 NM 2002 12 30 AWXA200201251 1 20021212 A 5320 AND101401204 FLOOR SUPPORT BOEING 737 7373B7 138447F NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 LCQ - MAJOR REPAIR - DURING C-11 CHECK EXFOLIATION CORROSION WAS FOUND AROUND 3 FASTENER HOLES ON FLOOR SUPPORT AT BS 99 5 - 1006, LBL 13. MAINTENANCE REMOVED THE DAMAGED FLOOR SUPPORT AT BS 995 - 1006, LBL 13; FABRICATED A NEW REPLACEMENT F LOOR SUPPORT; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 6. 2 L 7 2 4F RT A16WE 2002123000110 20021230 00110 NM 2002 12 30 AWXA200201252 1 20021213 A 5330 6545871523 SKIN BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 0 0 23377 LCQ - MAJOR REPAIR - DURING C-11 CHECK 2 CRACKS WERE FOUND ON THE R-1 DOOR EXTERNAL SKIN AT THE LOWER HINGE CUTOUT BS 30 0. MAINTENANCE STOP DRILLED CRACKS ON R-1 DOOR EXTERNAL SKIN AT THE LOWER HINGE CUTOUT BS 300; PERFORMED HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED; FABRICATED A REPAIR DOUBLER; AND INSTALLED REPAIR PART IAW AWA E.R. 03-5241-02350-SS 2. 2 L 7 2 4F RT A16WE 2002123000111 20021230 00111 NM 2002 12 30 AWXA200201253 1 20021217 A 5311 651630087 FRAME BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 0 0 23377 LCQ - MAJOR REPAIR - DURING C-11 CHECK A 1/2" CRACK WAS FOUND IN THE RADIUS OF FRAME ON THE FORWARD PRESSURE BULKHEAD BS 178, WL 207, RBL 28. MAINTENANCE REMOVED R/H FORWARD PRESSURE BULKHEAD WEB AND THE CRACKED R/H FORWARD PRESSURE BULKHEA D FRAME AT BS 178, WL 207, RBL 28; FABRICATED A NEW REPLACEMENT FRAME; AND INSTALLED REPAIR PART AND REMOVED R/H FORWARD PRESSURE BULKHEAD WEB IAW B737-300 SRM 51-40-02, FIG. 8, PG. 38. 2 L 7 2 4F RT A16WE 2002123000112 20021230 00112 NM 2002 12 30 AWXA200201255 1 20021217 A 5330 5079454 SKIN BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 0 0 23776 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1/2" CRACK WAS FOUND ON THE L-1 DOOR INNER SKIN AT 5TH AFT STOP PAD FROM BOTTOM , BS 344. NO STOP DRILL REQUIRED, CRACK EXTENDS FROM EDGE OF WEB AND TERMINATES AT LIGHTENING HOLE. MAINTENANCE FABRICAT ED A REPAIR DOUBLER AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 9, PG. 3 & 5. 2 L 7 2 4F RT A16WE 2002123000113 20021230 00113 WP 2002 12 30 IXXA0200156O 1 20021227 A 2750 5751152503 LINK DOUG DC8 DC871F 302199D WP LEFT WING BROKEN A IXXA O OTHER F FLT CONT AFFECTED LD LANDING 1 SW 11 823BX 84660 1490 46064 !DURING LANDING AT ANC FROM SEA, THE FLIGHT CREW HEARD A LOUD NOISE FOLLOWED BY AIRCRAFT ROLL THE FLIGHT CREW CONTINUE D WITH AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED A BROKEN FLAP ACTUATOR ATTACH BRACKET O N THE LEFT WING. MAINTENANCE REPLACED THE BRACKET AND PERFORMED SUCESSFUL OPERATIONAL CHECKS IN ACCORDANCE WITH THE DOUG LAS MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2002123100001 20021231 00001 2002 12 31 0212271 4 20021227 A 6122 387 BULB SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE INOPERATIVE A UHLA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 NE 03 35SZ 35 372 DRG342189 Flight 4456 TTN-BED. Autocoarsen failed to arm on take off. R&R'd anunciator bulbs. Lamp test good. Performed Autocoarse n test IAW SF 340A AMM 61-22-00-5. Ops check good. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2002123100002 20021231 00002 NE 2002 12 31 HEEA082403 1 20021212 A 7600 7630103004042 SHAFT SKRSKY S76 S76A 8143006 NE ENGINE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 TORQUE SHAFT BUSHING HOLES WORN. IN SHOP REPAIR. 1 G 7 2 3U H1NE 2002123100009 20021231 00009 NE 2002 12 31 HEEA082413 1 20021212 A 5610 076201004 WINDOW SKRSKY S76 S76A 8143006 NE COCKPIT MISMANUFACTURED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 911MJ 760231 WINDOW HAS PRE-DRILLED MOUNTING HOLES THAT ARE 1/2 HOLE SIZE OFF. 1 G 7 2 3U H1NE 2003010600110 20030106 00110 NM 2003 1 6 SWAA023003 1 20021223 A 3211 6546113 TRUNNION PIN BOEING 737 7373H4 1384600 NM LT/RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT ML G TRUNNION PINS PER MM. 2 L 7 2 4F RT A16WE 2003010600111 20030106 00111 NM 2003 1 6 SWAA023004 1 20021221 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 401, STR 15L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2003010600113 20030106 00113 NM 2003 1 6 SWAA023005 1 20021222 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STR 2R AND RBL 10. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2002123100010 20021231 00010 NM 2002 12 31 SWAA023011 1 20021226 A 3350 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002123100011 20021231 00011 NM 2002 12 31 SWAA023014 1 20021226 A 5330 655298871 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 955, WL 209, LOWER FWD CORNER OF FWD SVC DOOR. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2002123100012 20021231 00012 NM 2002 12 31 SWAA023007 1 20021222 A 5230 6546920 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME PER SWA CCO 52-30-0012. 2 L 7 2 4F RT A16WE 2002123100013 20021231 00013 NM 2002 12 31 SWAA023009 1 20021224 A 5330 6545768 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 327, STR 4R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F A16WE 2002123100014 20021231 00014 NM 2002 12 31 SWAA023010 1 20021224 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 FUSELAGE SKIN CRACKED JUST BEHIND THE RT WING TO BODY FAIRING. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002123100015 20021231 00015 NM 2002 12 31 SWAA022973 1 20021219 A 5315 BAC1509 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 777, LBL 8.0. REPAIRED FLOORBEAM PER SWA RA. 2 L 7 2 4F RT A16WE 2002123100016 20021231 00016 NM 2002 12 31 SWAA022974 1 20021220 A 5330 6545765 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 12L. REPAIRED SKIN PER MM. 2 L 7 2 4F RT A16WE 2002123100017 20021231 00017 2002 12 31 SWAA022975 4 20021219 A 2565 65C19901 CABLE BOEING 737 7375H4 138449D NM AFT CABIN DOORS MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED C1 CHECK, FOUND BOTH AFT ENTRY AND AFT SVC DOOR EMERGENCY EVAC SLIDE RELEASE CABLES MISROUTED. REROUTE D CABLES PER MM. 2 L 7 2 4F RT A16WE 2002123100018 20021231 00018 NM 2002 12 31 SWAA022976 1 20021220 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 719SW 27853 DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVAT OR TAB HARDWARE AND BUSHING AT INBD HINGE ATTACH POINT. 2 L 7 2 4F RT A16WE 2002123100019 20021231 00019 NM 2002 12 31 SWAA022977 1 20021220 A 5520 BACB28AH04 BUSHING BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED C4 CHECK, SWA SI 11075-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TA B HARDWARE AND BUSHING AT NR 1 HINGE ATTACH POINT PER MM. 2 L 7 2 4F RT A16WE 2002123100020 20021231 00020 2002 12 31 SWAA022978 4 20021221 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002123100021 20021231 00021 NM 2002 12 31 SWAA022979 1 20021220 A 3350 101114 LENS BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2002123100022 20021231 00022 2002 12 31 SWAA022983 4 20021221 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT CABIN DOORS MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C3 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE RELEASE CABLES MISROUTED. REROUTED CABLES PER MM. 2 L 7 2 4F RT A16WE 2002123100023 20021231 00023 NM 2002 12 31 SWAA022985 1 20021220 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 DURING SCHEDULED C2 CHECK, FOUND FIRST TWO EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002123100024 20021231 00024 2002 12 31 SWAA022986 4 20021220 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM ALL CABIN DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 717SA 27851 DURING SCHEDULED C4 CHECK, FOUND ALL FOUR CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2 L 7 2 4F RT A16WE 2002123100025 20021231 00025 NM 2002 12 31 SWAA022987 1 20021221 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKS (2 EA) AT BS 727E AT STR 10R AND BS 747 AT STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002123100026 20021231 00026 2002 12 31 SWAA022988 4 20021219 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002123100027 20021231 00027 2002 12 31 SWAA022992 4 20021222 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 755SA 27871 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002123100028 20021231 00028 NM 2002 12 31 SWAA022993 1 20021222 A 5311 6547951 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER SWA T1. 2 L 7 2 4F RT A16WE 2002123100029 20021231 00029 NM 2002 12 31 SWAA022994 1 20021222 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 081SW 22730 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F A16WE 2002123100030 20021231 00030 NM 2002 12 31 SWAA022996 1 20021222 A 5311 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIES CRACKED (2 EA) AT BS 400 BETWEEN STR 15L AND 16L AND BS 787, ABOVE STR 14R. REPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2002123100031 20021231 00031 NM 2002 12 31 SWAA022997 1 20021222 A 5313 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED, FOUND STRINGER TIE CLIPS CRACKED (9 EA) BS 380 AT STR 15L, BS 500D AT STR 1L, BS 500D AT STR 4R, BS 52 0 AT STR'S 2R, 3R AND 4R, BS 767 AT STR 2L, BS 747 AT STR 4R AND BS 787 AT STR 4R. REMOVED AND REPLACED STRINGER TIE CL IPS PER SRM. 2 L 7 2 4F RT A16WE 2002123100032 20021231 00032 NM 2002 12 31 SWAA022999 1 20021220 A 2720 65C370539 PCU BOEING 737 7372H4 138448C NM TAIL FAULTY A SWAA K NONE F FLT CONT AFFECTED UK UNKNOWN 1 SW 29 081SW 22730 AIRCRAFT WOULD NOT TRIM. REMOVED AND REPLACED RUDDER PCU PER MM. 2 L 7 2 4F A16WE 2002123100033 20021231 00033 NM 2002 12 31 SWAA022939 1 20021216 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 755SA 27871 DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, FOUND RT ELEVATOR TAB HINGE ATTACH POINTS NR 2 AND NR 4 WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS AT NR 2 AND NR 4 HINGE ATTACH POINTS PER MM. 2 L 7 2 4F RT A16WE 2002123100034 20021231 00034 NM 2002 12 31 SWAA022940 1 20021215 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 464, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002123100035 20021231 00035 NM 2002 12 31 SWAA022941 1 20021215 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 743, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002123100036 20021231 00036 NM 2002 12 31 SWAA022942 1 20021216 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 753, ABOVE STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002123100037 20021231 00037 NM 2002 12 31 SWAA022943 1 20021215 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, ABOVE STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002123100038 20021231 00038 NM 2002 12 31 SWAA022946 1 20021217 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 871, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002123100039 20021231 00039 NM 2002 12 31 SWAA022949 1 20021215 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED LT/RT AT BS 188, WL 208. REMOVED AND REPLACED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2002123100040 20021231 00040 NM 2002 12 31 SWAA022953 1 20021216 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 755SA 27871 DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS AT NR 1, NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM. 2 L 7 2 4F RT A16WE 2002123100041 20021231 00041 NM 2002 12 31 SWAA022955 1 20021217 A 5754 65C26603201A SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 3 SLAT T/E WEDGE DELAMINATED AT INBD END. REMOVED AND REPLACED NR 3 SLAT PE R MM. 2 L 7 2 4F RT A16WE 2002123100042 20021231 00042 NM 2002 12 31 SWAA022956 1 20021217 A 5753 6546435304 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED C2 CHECK, FOUND RT WING INBD T/E AFT FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2002123100043 20021231 00043 2002 12 31 SWAA022957 4 20021217 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002123100044 20021231 00044 2002 12 31 SWAA022958 4 20021217 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT SVC DOOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION AND GIRT ASSY WORN. REMOVED AND REPL ACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002123100045 20021231 00045 NM 2002 12 31 SWAA022959 1 20021218 A 5315 65C34537 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED 1/4D CHECK, FOUND CENTER LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL O. REPAIRED FLOORBEAM PER SWA EA . 2 L 7 2 4F A16WE 2002123100046 20021231 00046 NM 2002 12 31 SWAA022960 1 20021216 A 5330 6545772157 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10L, BETWEEN BS 727A AND BS 727B. REPAIRED SK IN PER SWA EA. 2 L 7 2 4F A16WE 2002123100047 20021231 00047 NM 2002 12 31 SWAA022962 1 20021218 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SERVICE CHECK, FOUND A 3.5 INCH LONG CRACK AT FUSELAGE SKIN, BS 328, BELOW STRINGER 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002123100048 20021231 00048 2002 12 31 SWAA022964 4 20021218 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM L1 DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE RELEASE CABLE MISROUTED. REINSTALLED CABLE PER MM. 2 L 7 2 4F A16WE 2002123100049 20021231 00049 2002 12 31 SWAA022965 4 20021218 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2002123100050 20021231 00050 NM 2002 12 31 SWAA022967 1 20021219 A 5310 6545409 WEB BOEING 737 7373H4 1384600 NM CENTER CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED .5 INCH LONG, BS 664, LBL 31. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2002123100051 20021231 00051 NM 2002 12 31 SWAA022968 1 20021218 A 5230 6545871 FRAME BOEING 737 7373TO 138447G NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR INBD AND OUTBOARD FRAMES CRACKED. REMOVED AND REPLACED AFT CARGO DOOR P ER MM. 2 L 7 2 4F RT A16WE 2002123100052 20021231 00052 NM 2002 12 31 SWAA022893 1 20021209 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED AT R0W NR 1, NR 13, NR 18 AND NR 22. REMOVED AND REPLACED EEPLS C OVERS PER MM. 2 L 7 2 4F RT A16WE 2002123100053 20021231 00053 2002 12 31 SWAA022895 4 20021211 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002123100054 20021231 00054 NM 2002 12 31 SWAA022897 1 20021211 A 5311 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BELOW STR 14L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2002123100055 20021231 00055 NM 2002 12 31 SWAA022898 1 20021210 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 735, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002123100056 20021231 00056 NM 2002 12 31 SWAA022899 1 20021211 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002123100057 20021231 00057 NM 2002 12 31 SWAA022900 1 20021210 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002123100058 20021231 00058 2002 12 31 SWAA022901 4 20021210 A 2565 65C19901 CABLE BOEING 737 7375H4 138449D NM AFT SVC DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002123100059 20021231 00059 NM 2002 12 31 SWAA022902 1 20021210 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2002123100060 20021231 00060 NM 2002 12 31 SWAA022903 1 20021211 A 5753 6546434335 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED C2 CHECK, FOUND LT INBD T/E FLAP DELAMINATED. REMOVED AND REPLACED LEFT INBD T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2002123100061 20021231 00061 NM 2002 12 31 SWAA022904 1 20021211 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAMES CRACKED (2 EA) AT STR 14L, BS 767 AND BS 787. REPAIRED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2002123100062 20021231 00062 NM 2002 12 31 SWAA022906 1 20021209 A 5330 589358 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED C2 CHECK, FOUND F/O'S NR 1 WINDOW POST SKIN CRACKED AT LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2002123100063 20021231 00063 NM 2002 12 31 SWAA022907 1 20021211 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 769, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002123100064 20021231 00064 NM 2002 12 31 SWAA022908 1 20021211 A 5330 6545785 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUTS CRACKED AT RT WINDOWS NR 29 AND NR 35. REPAIRED SKIN PER BFG E R. 2 L 7 2 4F RT A16WE 2002123100065 20021231 00065 NM 2002 12 31 SWAA022910 1 20021212 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 EEPLS TRACK COVERS LOOSE AT ROWS 6 AND 15. REMOVED AND REPLACED EEPLS TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2002123100066 20021231 00066 2002 12 31 SWAA022911 4 20021211 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM R1 DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 2002123100067 20021231 00067 2002 12 31 SWAA022912 4 20021211 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F A16WE 2002123100068 20021231 00068 NM 2002 12 31 SWAA022913 1 20021212 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CORRODED, BS 907 STRINGER 26L. REPAIRED STRINGER SECTION PER SRM 2 L 7 2 4F A16WE 2002123100069 20021231 00069 NM 2002 12 31 SWAA022914 1 20021211 A 5313 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED, BS 360, STRINGER 14L. REMOVED AND REPLACED STRINGER SPLI CE PER SRM. 2 L 7 2 4F RT A16WE 2002123100070 20021231 00070 NM 2002 12 31 SWAA022915 1 20021210 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR FUSELAGE SKIN CUTOUT CRACKED AT LOWER AFT CORNER. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2002123100071 20021231 00071 2002 12 31 SWAA022916 4 20021211 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR. FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2002123100072 20021231 00072 NM 2002 12 31 SWAA022918 1 20021212 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 745SW 29491 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS NR 1, NR 5, NR 8, NR 13, NR 16 AND NR 18. REMOVED AND REP LACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2002123100073 20021231 00073 2002 12 31 SWAA022921 4 20021213 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002123100074 20021231 00074 2002 12 31 SWAA022922 4 20021215 A 2565 65C168209 RETAINER BOEING 737 7372H4 138448C NM AFT ENTRY DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. SECURED RETAINER PER MM. 2 L 7 2 4F A16WE 2002123100075 20021231 00075 2002 12 31 SWAA022923 4 20021213 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 FWD ENTRY DOOR EMERGENCY EVAC SLIDE DEPLOYED WHEN OPENING DOOR. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2002123100076 20021231 00076 NM 2002 12 31 SWAA022924 1 20021215 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 777, STR 11L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2002123100077 20021231 00077 NM 2002 12 31 SWAA022926 1 20021214 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4R, BS 625 AND BS 713. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002123100078 20021231 00078 NM 2002 12 31 SWAA022927 1 20021216 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 20L, BS 972 AND BS 978. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2002123100079 20021231 00079 NM 2002 12 31 SWAA022928 1 20021214 A 5320 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED AT LBL 70, BS 727A + 18 & BS 727B + 9. REMOVED AND REPLACED CR EASE BEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2002123100080 20021231 00080 NM 2002 12 31 SWAA022929 1 20021213 A 5241 6545871132 SKIN BOEING 737 7373H4 1384600 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR SKIN CRACKED AT BOTH UPPER AND LOWER HINGE ATTACH POINTS. REMOVED AND REP LACED FWD SVC DOOR PER MM. 2 L 7 2 4F RT A16WE 2002123100081 20021231 00081 NM 2002 12 31 SWAA022930 1 20021212 A 5520 BACB28AM07 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C4 CHECK, SWA SI 11139-55,FOUND LT ELEVATOR TRIM TAB WORN AT INBD HINGE POINT. REMOVED AND REPLACED BU SHING AT INBD HINGE POINT PER MM. 2 L 7 2 4F RT A16WE 2002123100082 20021231 00082 NM 2002 12 31 SWAA022932 1 20021213 A 2917 7321124001 MODULE BOEING 737 7377H4 1384404 NM RT MLG W/W LEAKING A SWAA A D UNSCHED LANDING RETURN TO BLOCK K FLUID LOSS CL CLIMB 1 SW 29 718SW 27852 AIR TURNBACK, DECLARED EMERGENCY, SLIGHT HYDRAULIC SMELL DURING TAXI, STRONG HYDRAULIC SMELL AT HIGH POWER DURING TAKEOF F. REMOVED AND REPLACED HYDRAULIC RESEVOIR AIR PRESSURE MODULE, BOTH COALESCER BAGS AND HEPA FILTER PER MM. 2 L 7 2 4F RT A16WE 2002123100083 20021231 00083 NM 2002 12 31 SWAA022935 1 20021214 A 5330 6545765 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10L, BS 500A, BS 520 AND BS 500B. REPAIRED SK IN PER SRM. 2 L 7 2 4F A16WE 2002123100084 20021231 00084 NM 2002 12 31 SWAA022936 1 20021216 A 5313 65C27314 TIE CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 874 AT STR 4L AND BS 500A AT STR 10L. REM OVED AND REPLACED STRINGER TIE CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2002123100085 20021231 00085 NM 2002 12 31 SWAA022938 1 20021214 A 2731 65C35943 BEARING BOEING 737 7372H4 138448C NM TAIL WORN A SWAA K NONE F P FLT CONT AFFECTED NO WARNING INDICATION NR NOT REPORTED 1 SW 29 071SW 22358 FLIGHT CONTROLS BINDING IN PITCH HEAVY FEEL. REMOVED AND REPLACED ELEVATOR TORQUE TUBE BEARING PER MM. 2 L 7 2 4F A16WE 2002123100086 20021231 00086 2002 12 31 VNAA0212028 4 20021222 A 3100 501122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 442JS 18969 2128 3060 THE CREW REPORTED THAT THE EMERGENCY BACK UP BATTERY FAILS TO TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PO WER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT W AS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002123100087 20021231 00087 NM 2002 12 31 VNAA0212024 1 20021219 A 3200 2342500000 HARNESS DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA O OTHER O OTHER LD LANDING 1 GL 07 440JS 18576 3600 3058 ON APPROACH, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE AS WELL AS A PROXY SYSTEM FAIL AND PROXY BYPASS FA IL ON THE SYSTEM PAGE. THE CREW EXECUTED A MISSED APPROACH AND CALLED MAINTENANCE CONTROL AND THE MESSAGES CLEARED. DU RING THE SECOND APPROACH, THE CREW AGAIN RECEIVED THE SAME MESSAGES, THE CREW COMPLIED WITH THE QUICK REFERENCE HANDBOOK AND THE MESSAGES CLEARED. THE CREW DECLARED AN EMERGENCY AND FLIGHT 4106 LANDED WITH NO FURTHER INCIDENTS. MAINTENANC E INSPECTED AND REPLACED THE NOSE WHEEL ELECTRICAL HARNESS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPER ATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002123100088 20021231 00088 NM 2002 12 31 VNAA0212022 1 20021216 A 2600 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE APU FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 458PS 3068 THE CREW REPORTED THAT THE APU FIRE TEST FAILS. MAINTENANCE INSPECTED AND FOUND A LOOSE CONNECTOR ON THE FIRE LOOP. MA INTENANCE TIGHTENED THE CONNECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFO RMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2002123100089 20021231 00089 NE 2002 12 31 HEEA082440 1 20021212 A 3350 6013211 POWER SUPPLY SKRSKY S76 S76A 8143006 NE EMERGENCY LIGHTS INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22342 760096 EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. 1 G 7 2 3U H1NE 2002123100090 20021231 00090 2002 12 31 HEEA082441 4 20021212 A 3444 7001840903 TRANSCEIVER SKRSKY S76 S76A 8143006 NE COCKPIT INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 760050 TRANSCEIVER INTERMITTENTLY INOPERATIVE. 1 G 7 2 3U H1NE 2003011600186 20030116 00186 EA 2003 1 16 COMA0260726 1 20021219 A 3620 355862255 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA BLEED AIR SYS DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 806C 7359 ANTI ICE DUCT WARNING. REPLACED BLEED LEAK SENSING LOOP A18WK. 2 L 7 2 4F RT A21EA 2003011600184 20030116 00184 EA 2003 1 16 COMA0260717 1 20021212 A 3020 300013000003 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA LT COWLING MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 470CA 1415 7650 FLIGHT 5128 LEFT COWL ANTI ICE CAUTION MESSAGE. REPLACED THE COWL ANTI ICE VALVE. 2 L 7 2 4F RT A21EA 2003011600214 20030116 00214 EA 2003 1 16 COMA0260730 1 20021221 A 3397 64645 POWER CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 798CA 7348 FLIGHT 5660 EMERGENCY FLOOR PATH LIGHTS INOPERABLE ROW 9 & AFT. REPLACED FLOOR LIGHTING POWER STRIP. 2 L 7 2 4F RT A21EA 2003011600217 20030116 00217 EA 2003 1 16 COMA0260732 1 20021221 A 3397 64645 POWER CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 818CA 7408 FLIGHT 575 EMERGENCY FLOOR PATH LIGHTING AT ROW 1 IS INOPERABLE. REPLACED THE FLOOR LIGHTING POWER STRIP. 2 L 7 2 4F RT A21EA 2003011600218 20030116 00218 EA 2003 1 16 COMA0260734 1 20021223 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 806CA 3609 7359 FLIGHT 5798 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LEFT BRAKE AND POSITION SENSOR UNIT. 2 L 7 2 4F RT A21EA 2002123100091 20021231 00091 NE 2002 12 31 COMA0260733 2 20021222 A 7260 5016T32P01 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE L/H ENG LEAKING A COMA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 924CA 7026 807532 FLIGHT 5954 LEFT ENGINE OIL PRESSURE WARNING I.F.S.D.REPLACED THE BB AXIS DRIVE SEAL ON ACCESSORY GEAR BOX. 2 L 7 2 4F 4 F RT A21EA E15NE 2002123100092 20021231 00092 WP 2002 12 31 CALA0200601 1 20021229 A 5531 SPAR DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND A 10 INCH CRACK IN VERTICAL STABILIZER L/H FRONT SPAR AT LOWER END AT CANTED BULKHEAD STA 1388. INSTALL ED DOUBLERS IAW SRM 55-02, FIGURE 26. 2 L 7 2 4F A6WE 2002123100093 20021231 00093 WP 2002 12 31 MWEA020768 1 20021231 A 5320 9910078215 DOUBLER DOUG DC9 DC915 3022036 WP STA 160 PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 THERE IS A PUNCTURE IN THE SUBFLOORING JUST AFT OF STATION 160 AT RIGHT SIDE OF CENTERLINE OF FUSELAGE. -- REMOVED DAM AGED AREA, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2002123100094 20021231 00094 EA 2002 12 31 COMA0260736 1 20021225 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 957CA 7109 FLIGHT 6034 FLAPS FAIL MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2002123100095 20021231 00095 NE 2002 12 31 COMA0260737 2 20021225 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE A COMA C ABORTED TAKEOFF J E WARNING INDICATION VIBRATION/BUFFET TO TAKEOFF 1 SO 01 984CA 7171 FLIGHT 5511 LEFT ENGINE VIB MESSAGE.COULD NOT DUPLICATE. NO VIB LOGGED IN MDC. 2 L 7 2 4F 4 F RT A21EA E15NE 2002123100096 20021231 00096 EA 2002 12 31 COMA0260738 1 20021225 A 7730 6632M16 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA LEFT ENGINE MALFUNCTIONED A COMA C ABORTED TAKEOFF J E WARNING INDICATION VIBRATION/BUFFET TO TAKEOFF 1 SO 01 984CA 4275 7171 FLIGHT 5585 LEFT ENGINE VIB MESSAGE.COULD NOT DUPLICATE REPLACED THE VIB SIGNAL CONDITIONER. 2 L 7 2 4F RT A21EA 2002123100097 20021231 00097 EA 2002 12 31 COMA0260740 1 20021224 A 2750 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 978CA 7158 FLIGHT 5893 FLAPS FAIL MESSAGE AFTER T/O.FOUND PDU CIRCUIT BREAKERS OUT - RESET BREAKERS. 2 L 7 2 4F RT A21EA 2003011600219 20030116 00219 EA 2003 1 16 COMA0260739 1 20021225 A 3010 ANTI-ICE SYSTEM CNDAIR CL600 CL6002B19 1900309 EA LT WING MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 977CA 7157 FLIGHT 5211 LEFT WING ANTI ICE CAUTION MESSAGE. COULD NOT DUPLICATE. SYSTEM OPERATION WAS NORMAL. 2 L 7 2 4F RT A21EA 2003011600220 20030116 00220 EA 2003 1 16 COMA0260741 1 20021223 A 5280 DOOR CNDAIR CL600 CL6002B19 1900309 EA NLG BINDING A COMA A UNSCHED LANDING S W AFFECT SYSTEMS INADEQUATE Q C CL CLIMB 1 SO 01 927CA 7031 FLIGHT 5344 GEAR DISAGREE WARNING, NLG DID NOT RETRACT. FOUND NLG DOORS BINDING. TRIMMED EXCESS MATERIAL FROM NLG DOOR S. 2 L 7 2 4F RT A21EA 2003011600210 20030116 00210 EA 2003 1 16 COMA0260728 1 20021220 A 7931 APTE142100013 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA LEFT ENGINE MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 721CA 6034 7259 LEFT ENGINE OIL PRESSURE INDICATED 157 PSI. REPLACED THE OIL PRESSURE TRANSDUCER. 2 L 7 2 4F RT A21EA 2002123100098 20021231 00098 EA 2002 12 31 COMA0260742 1 20021220 A 2130 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 963CA 7127 CABIN ALTITUDE CAUTION MESSAGE.COULD NOT DUPLICATE, CABIN PRESSURE CONTROL SYSTEM OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A21EA 2002123100099 20021231 00099 WP 2002 12 31 ZW0A0213101 1 20021230 A 3350 58203 LAMP DOUG DC9 DC982 3022082 WP A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 929TW 48014 THE EMERGENCY LIGHT IN THE TAIL COMPARTMENT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 2-8-02 STL. --CLOSED-- 2 L 7 2 4F A6WE 2002123100100 20021231 00100 NM 2002 12 31 P5CA0200715 1 20021227 A 2740 285U0015110 CONTROL MODULE BOEING 747 74746NF 13848BT NM LEFT STAB. TRIM FAILED A P5CA D RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 WP 23 454PA 30812 TRIM #2 & #3 FAILED AFTER T/O IN BOTH AUTO & MANUAL. A/C RETURNED TO MIA. REMOVED & REPLACED STAB. TRIM UNIT AS PER MM 2 7-41-06. OPS CHECK NORMAL. 2 L 7 4 4F RT A20WE 2002123100101 20021231 00101 NE 2002 12 31 HEEA082476 1 20021213 A 5330 7620102007041 PANEL SKRSKY S76 S76A 8143006 NE FUSELAGE MISMARKED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 PANEL IMPROPERLY IDENTIFIED PART NUMBER. HELICOMB P/N IS 76201-02021-041. THE CORRECT P/N IS 76201-02007-041. 1 G 7 2 3U H1NE 2002123100102 20021231 00102 NM 2002 12 31 PCAA0212145 1 20021231 A 5610 7803 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM FIRST OFFICERS CRACKED A PCAA A UNSCHED LANDING Z SIGNIFICANT FAILURE REPORT CR CRUISE 1 EA 13 835EX 16010 289 FLIGHT#3636 BTV-LGA. WHILE IN CRUISE FLIGHT FIRST OFFICERS WINDSHIELD BEGAN TO CRACK IN SEVERAL PLACES AND SPARK DUE TO WINDSHIELD HEAT BEING TURNED ON. WINDSHIELD HEAT SELECTED OFF AND SPARKING STOPPED. AIRCRAFT RETURNED TO BTV, AND EMERGE NCY DECLARED. MAINTENANCE REPLACED FIRST OFFICERS WINDSHIELD IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 56 -10-11. GROUND RAN AIRCRAFT TO PERFORM OPERATIONAL CHECK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2002123100103 20021231 00103 WP 2002 12 31 MWEA020769 1 20021231 A 5320 991224617 WEB DOUG DC9 DC932 3022066 WP STA 1038 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FOUND TWO CRACKS IN WEB AT FUSELAGE STATION 1038 LEFT SIDE AT APPROXIMATELY LONGERON 12. -- REMOVED AND REPLACED NEW S ECTION. 2 L 7 2 4F A6WE 2002123100104 20021231 00104 NE 2002 12 31 HEEA082480 1 20021213 A 3210 7625100702043 LINK SKRSKY S76 S76A 8143006 NE MLG BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 MLG LINK BROKEN. SCRAPPED. 1 G 7 2 3U H1NE 2002123100105 20021231 00105 NE 2002 12 31 HEEA082501 1 20021213 A 7714 7645001076101 TACH GENERATOR SKRSKY S76 S76A 8143006 NE ENGINE MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911UK 760275 ENGINE OUTLIGHT DOES NOT COME ON BRIGHT WITH BATTERY ON AND WILL NOT EXTINGUISH WHEN ENGINE RUNNING. 1 G 7 2 3U H1NE 2002123100106 20021231 00106 NM 2002 12 31 AWXA200201257 1 20021210 A 5330 6552988 SKIN BOEING 737 7373S3 1384711 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 0 0 23712 YVR - MAJOR REPAIR - DURING C-16 CHECK A 1/2" CRACK WAS FOUND ON FUSELAGE SKIN AT THE UPPER HINGE CUTOUT OF THE L-2 DOOR , BS 951, STR 10 L/H. MAINTENANCE CUTOUT CRACKED AREA OF SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; AND INSTALLED REPAIR PART IAW B737-300 SRM 53-60-01, FIG 205, PG. 211. 2 L 7 2 4F RT A16WE 2002123100107 20021231 00107 NM 2002 12 31 AWXA200201259 1 20021212 A 5315 7075T6050 ANGLE BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 0 0 23377 LCQ - MAJOR REPAIR - DURING C-11 CHECK A CRACK WAS FOUND AROUND FASTENER HOLE OF CABIN FLOOR SUPPORT ANGLE BETWEEN BS 50 0D AND BS 500E AT BL "0". MAINTENANCE REMOVED DAMAGE ON CABIN FLOOR SUPPORT ANGLE BETWEEN BS 500D AND BS 500E AT BL "0"; FABRICATED 3 EACH REPAIR ANGLES; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-30-51, PG. 103, AND SRM 51-30-01, PG. 1 2. 2 L 7 2 4F RT A16WE 2002123100108 20021231 00108 NM 2002 12 31 AWXA200201260 1 20021213 A 5330 2024T3040 SKIN BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 0 0 23377 LCQ - MAJOR REPAIR - DURING C-11 CHECK A 1/2" CRACK WAS FOUND ON LOWER AFT INNER SKIN OF L-1 DOOR ON INBOARD SIDE. MAINT ENANCE REMOVED CRACKED ANGLE AND STOP DRILLED CRACK ON INNER SKIN; HFEC INSPECTION WAS ACCOMPLISHED TO VERIFY CRACK WAS CONTAINED; FABRICATED A REPAIR ANGLE AND REPAIR DOUBLER; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PG. 16-19 , AND SRM 51-70-13, PG. 1-5. 2 L 7 2 4F RT A16WE 2002123100109 20021231 00109 NM 2002 12 31 AWXA200201261 1 20021214 A 5315 65528941 ANGLE BOEING 737 7373B7 1384580 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 0 0 23377 LCQ - MAJOR REPAIR - DURING C-11 CHECK A CRACK WAS FOUND ON THE UNDERSIDE RADIUS OF FLOOR BEAM SUPPORT ANGLE BS 540, BL "O". MAINTENANCE REMOVED CRACKED FLOOR BEAM SUPPORT ANGLE AT BS 540, BL "0"; FABRICATED A NEW REPLACEMENT FLOOR BEAM SUP PORT ANGLE; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 1-2. 2 L 7 2 4F RT A16WE 2002123100110 20021231 00110 SO 2002 12 31 C2XA02IA253 1 20021229 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14916 145415 BNA- DURING MAINTENANCE THE MECHANIC NOTED THAT THE #1 EMERGENCY LIGHT BATTERY WOULD NOT HOLD CHARGE. BNA- MAINTENANC E REMOVED AND REPLACED THE #1 EMERGENCY LIGHT BATTERY,PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM, NO DE FECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2003010200001 20030102 00001 NE 2003 1 2 HEEA082536 1 20021213 A 3040 9001643 BLADE SKRSKY S76 S76A 8143006 NE WINDSHIELD WIPER TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 WINDSHIELD WIPER BLADE IS WORN AND TORN. SCRAPPED. 1 G 7 2 3U H1NE 2003010200002 20030102 00002 2003 1 2 HEEA082552 4 20021213 A 2300 N0001553 ANTENNA SKRSKY S76 S76A 8143006 NE COMM SYS CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 COMMUNICATIONS ANTENNA CRACKED. SCRAPPED. 1 G 7 2 3U H1NE 2003010200003 20030102 00003 NE 2003 1 2 HEEA082557 1 20021213 A 2497 V110J024AB RELAY SKRSKY S76 S76A 8143006 NE WILL NOT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 NON ESSENTIAL RELAY BUS RECOVERY DOES NOT TEST. SCRAPPED. 1 G 7 2 3U H1NE 2003010200004 20030102 00004 EU 2003 1 2 HEEA082623 1 20021211 A 7100 1564T1005 ACTUATOR BOLKMS 105 BO105S 5626006 EU ENGINE INOPERATIVE E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5031U S678 NO RESPONSE FROM ACTUATOR WHEN SWITCH IN ON POSITION.. 1 G 7 2 3U H3EU 2003010200005 20030102 00005 EU 2003 1 2 HEEA082624 1 20021211 A 7100 1564T1005 ACTUATOR BOLKMS 105 BO105S 5626006 EU ENGINE INOPERATIVE E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5031U S678 ACTUATOR INOPERATIVE. 1 G 7 2 3U H3EU 2003010200007 20030102 00007 EU 2003 1 2 HEEA082626 1 20021211 A 7923 209072433101 VALVE BOLKMS 105 BO105S 5626006 EU OIL SHUTOFF MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5031U S678 OIL SHUTOFF VALVE POPS CIRCUIT BREAKER. TO BE SENT TO VENDOR FOR REPAIR. 1 G 7 2 3U H3EU 2003010200008 20030102 00008 EU 2003 1 2 HEEA082627 1 20021211 A 7923 209072433101 VALVE BOLKMS 105 BO105S 5626006 EU OIL SHUTOFF STUCK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5031U S678 NR 2 DECK OIL SHUTOFF VALVE STUCK OPEN. 1 G 7 2 3U H3EU 2003010200009 20030102 00009 GL 2003 1 2 HEEA082628 2 20021211 A 7320 23033400 FILTER BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C30 03013 GL PC AIR DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U S678 NR 1 ENGINE PC FILTER HANG STARTS ON ENGINE RINSE. REPLACED WITH SERVICEABLE FILTER. 1 G 7 2 3U 3 U H3EU E1GL 2003010200011 20030102 00011 GL 2003 1 2 HEEA082630 2 20021211 A 7320 95704 CHECK VALVE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C30 03013 GL ENGINE FAILED E HEEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 03 5031U S678 ENGINE SMOKING ON SHUTDOWN. SCRAPPED CHECK VALVE. 1 G 7 2 3U 3 U H3EU E1GL 2003010200012 20030102 00012 GL 2003 1 2 HEEA082631 2 20021211 A 7320 252464430 FUEL CONTROL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C30 03013 GL ENGINE MALFUNCTIONED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5031U S678 FUEL CONTROL DECEL TIME TOO LONG, ON/ABOUT 70 SECONDS. IN SHOP REPAIR. 1 G 7 2 3U 3 U H3EU E1GL 2003010200013 20030102 00013 GL 2003 1 2 HEEA082632 2 20021211 A 7323 252466714 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C30 03013 GL ENGINE MALFUNCTIONED E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 5031U S678 GOVERNOR TORQUE SPLITS. IN SHOP REPAIR. 1 G 7 2 3U 3 U H3EU E1GL 2003010200014 20030102 00014 EU 2003 1 2 HEEA082633 1 20021211 A 6320 CASE BOLKMS 105 BO105S 5626006 EU TRANSMISSION CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50293 6915 965 S677 LOWER TRANSMISSION CASE CORRODED AT ATTACHMENT FLANGE. REPAIRED. 1 G 7 2 3U H3EU 2003010200016 20030102 00016 2003 1 2 HEEA082635 4 20021211 A 3424 9551A INDICATOR BOLKMS 105 BO105S 5626006 EU TURN & BANK INCORRECT E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 81832 S828 TURN AND BANK INDICATOR INOPERATIVE, SLIP NEEDLE STICKS. TO BE SENT TO VENDOR FOR REPAIR. 1 G 7 2 3U H3EU 2003010200017 20030102 00017 2003 1 2 HEEA082636 4 20021211 A 2340 A3016W INTERPHONE BOLKMS 105 BO105S 5626006 EU COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5031U S678 INTERPHONE BOX PRODUCING FEEDBACK NOISE ON CHANNEL 2. IN SHOP REPAIR. 1 G 7 2 3U H3EU 2003010200018 20030102 00018 EU 2003 1 2 HEEA082637 1 20021211 A 3340 A413AHDADF28 POWER SUPPLY BOLKMS 105 BO105S 5626006 EU STROBE INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5031U S678 EXTERNAL STROBE POWER SUPPLY INOPERATIVE. 1 G 7 2 3U H3EU 2003010200019 20030102 00019 EU 2003 1 2 HEEA082638 1 20021211 A 3340 A413AHDADF28 POWER SUPPLY BOLKMS 105 BO105S 5626006 EU STROBE INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5031U S678 NO OUTPUT FROM STROBE POWER SUPPLY. 1 G 7 2 3U H3EU 2003010200021 20030102 00021 EU 2003 1 2 HEEA082640 1 20021211 A 2822 D107318D1 PUMP BOLKMS 105 BO105S 5626006 EU FUEL SYSTEM INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U S678 FUEL PUMP INTERMITTENT. 1 G 7 2 3U H3EU 2003010200022 20030102 00022 EU 2003 1 2 HEEA082641 1 20021211 A 3340 BULB BOLKMS 105 BO105S 5626006 EU LANDING LIGHT BLOWN E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 81832 S828 LANDING LIGHT HAS A BLOWN BULB. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 2003010200023 20030102 00023 EU 2003 1 2 HEEA082642 1 20021211 A 7712 DK50439 INDICATOR BOLKMS 105 BO105S 5626006 EU DUAL TORQUE STUCK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 81832 S828 DUAL TORQUE INDICATOR NR 1 NEEDLE STICKS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 2003010200025 20030102 00025 EU 2003 1 2 HEEA082644 1 20021211 A 7714 DL41239 INDICATOR BOLKMS 105 BO105S 5626006 EU ENGINE RPM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5031U S678 RPM INDICATOR NEEDLE JUMPS AS MUCH AS 15 PERCENT. 1 G 7 2 3U H3EU 2003010200026 20030102 00026 EU 2003 1 2 HEEA082645 1 20021211 A 2810 FTA017521E FUEL CELL BOLKMS 105 BO105S 5626006 EU FUSELAGE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 81832 S828 FUEL CELL LEAKING. 1 G 7 2 3U H3EU 2003010200027 20030102 00027 2003 1 2 HEEA082646 4 20021211 A 2561 PHI10090 LIFE VEST BOLKMS 105 BO105S 5626006 EU CABIN LEAKING E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5031U S678 LIFE VEST LEAKING. 1 G 7 2 3U H3EU 2003010200028 20030102 00028 EU 2003 1 2 HEEA082647 1 20021211 A 2810 PHI105752 CAP BOLKMS 105 BO105S 5626006 EU FUEL CELL DAMAGED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6607K S841 FUEL CAP HARD TO OPEN AND CLOSE. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 2003010200029 20030102 00029 EU 2003 1 2 HEEA082648 1 20021211 A 2432 CASE BOLKMS 105 BO105S 5626006 EU BATTERY CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54191 S804 BATTERY HAS EXCESSIVE CORROSION ON OUTER CASE. 1 G 7 2 3U H3EU 2003010200030 20030102 00030 WP 2003 1 2 CALA0200602 1 20021231 A 5320 ANGLE DOUG DC9 DC981 3022081 WP STA 389 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 INSPECTION FOUND A 1.25" CRACK IN FORWARD CARGO COMPARTMENT BELTFRAME SIDEWALL SUPPORT ANGLE AT STA 389, L25L. A DOUBLER WAS INSTALLED IAW 5320-01263. 2 L 7 2 4F A6WE 2003010200032 20030102 00032 EU 2003 1 2 HEEA082649 1 20021211 A 2432 COVER BOLKMS 105 BO105S 5626006 EU BATTERY DAMAGED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 CBC434488 COVER ON BATTERY PULLED UP. RIVET PULLED UP. 1 G 7 2 3U H3EU 2003010200033 20030102 00033 EU 2003 1 2 HEEA082650 1 20021211 A 2432 RG390E BATTERY BOLKMS 117 BK117A1 5626010 EU MAIN WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 911RZ 130 7092 MAIN BATTERY WEAK. 1 G 7 2 3U H13EU 2003010200034 20030102 00034 EU 2003 1 2 HEEA082651 1 20021211 A 7933 TM41039 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE OIL TEMP INTERMITTENT E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 6607K S841 TRANSMISSION OIL TEMP GOES TO ZERO INTERMITTENTLY. REPLACED INDICATOR. 1 G 7 2 3U H3EU 2003010200035 20030102 00035 NM 2003 1 2 DHL2002752007 1 20021230 A 3350 BATTERY BOEING 727 727223 1384074 NM A DHLA K O NONE OTHER L NO TEST IN INSP/MAINT 1 SO 01 752DH 22466 1) EMERGENCY EXIT LIGHT OVER MAIN CABIN DOOR BURNED OUT.2) REPLACED BATTERIES PER M/M 33-50-101 OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2003010200036 20030102 00036 2003 1 2 159PL0024 4 20021231 A 2210 SOLENOID BOEING 737 737242 1384477 NM A PIDA K NONE O OTHER CR CRUISE 1 SO 05 159PL 21186 Elev. channel auto pilot disengaged during flight. Elev. "B" PCU solenoid Inop. MEL Elev channel per MEL 22-1, Control No. 12-31-001, Class B. 2 L 7 2 4F A16WE 2003010200037 20030102 00037 WP 2003 1 2 MWEA020752 1 20021226 A 5311 991152737 SHEAR TIE DOUG DC9 DC981 3022081 WP SAT 541 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FORWARD PIT BETWEEN LONGERON 30 AND LEFT 29 AT STATION 541 SHEAR TIE HAS MODERATE CORROSION. -- REMOVED CORROSION, FAB RICATED AND INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F A6WE 2003010200038 20030102 00038 WP 2003 1 2 MWEA020758 1 20021226 A 5311 59560805 LONGERON DOUG DC9 DC981 3022081 WP STA 220 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 ELECTRICAL COMPARTMENT, FLOOR SUPPORT CORRODED AT FRAME STATION 220 BETWEEN LONGERON 29 RIGHT AND 30 ABOVE LONGERON 28 L EFT. -- LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT. 2 L 7 2 4F A6WE 2003010200039 20030102 00039 WP 2003 1 2 MWEA020759 1 20021226 A 5311 29524621 LONGERON DOUG DC9 DC981 3022081 WP STA 541 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 FORWARD PIT BETWEEN LONGERON 30 AND LEFT 29 AT STATION 541 SKIN HAS MODERATE CORROSION. -- FABRICATED AND INSTALLED SK IN AND DOUBLER. 2 L 7 2 4F A6WE 2003010200040 20030102 00040 2003 1 2 HEEA082652 4 20021211 A 2312 064105430 TRANSCEIVER BOLKMS 117 BK117A1 5626010 EU VHF SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 911TL 7198 VOLUME CONTROL INCONSISTENT. REPLACED S901 VOLUME CONTROL SWITCH, REPLACED BAD DISPLAY LENS, INTERMITTENT DS901 DISPLAY AND REPAINTED FACEPLATE. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 2003010200041 20030102 00041 EU 2003 1 2 HEEA082654 1 20021211 A 6220 BEARING BOLKMS 105 BO105S 5626006 EU ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U S678 YELLOW MAIN ROTOR PITCH CONTROL LINK LOWER ROD END BEARING WORN. SCRAPPED. 1 G 7 2 3U H3EU 2003010200042 20030102 00042 EU 2003 1 2 HEEA082655 1 20021211 A 6220 BEARING BOLKMS 105 BO105S 5626006 EU ROD END WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U S678 YELLOW MAIN ROTOR PITCH CONTROL LINK LOWER ROD END BEARING WORN. SCRAPPED. 1 G 7 2 3U H3EU 2003010200043 20030102 00043 EU 2003 1 2 HEEA082656 1 20021211 A 6410 10531980 BLADE BOLKMS 105 BO105S 5626006 EU TAIL ROTOR CHIPPED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 TAIL ROTOR BLADE HAS PAINT CHIPPED. 1 G 7 2 3U H3EU 2003010200044 20030102 00044 EU 2003 1 2 HEEA082657 1 20021211 A 6410 10531980 BLADE BOLKMS 105 BO105S 5626006 EU TAIL ROTOR CHIPPED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 TAIL ROTOR BLADE HAS PAINT CHIPPED. 1 G 7 2 3U H3EU 2003010200045 20030102 00045 EU 2003 1 2 HEEA082658 1 20021211 A 6420 1053172901 ROTOR HEAD BOLKMS 105 BO105S 5626006 EU TAIL ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6607K S841 TAIL ROTOR HEAD HAS CORROSION. 1 G 7 2 3U H3EU 2003010200046 20030102 00046 EU 2003 1 2 HEEA082659 1 20021211 A 7332 10593910 SWITCH BOLKMS 105 BO105S 5626006 EU DIFFERENTAL PRES FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5031U S678 PRESSURE SWITCHFAILED F/P 300 HOUR INSPECTION (WOULD NOT TEST). SCRAPPED. 1 G 7 2 3U H3EU 2003010200047 20030102 00047 EU 2003 1 2 HEEA082660 1 20021211 A 6420 10531738101 SLEEVE BOLKMS 117 BK117A1 5626010 EU ROTOR HEAD CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 050088 7092 TAIL ROTOR HEAD INNER SLEEVE HAS CORROSION AT SEAL RIDE. 1 G 7 2 3U H13EU 2003010200048 20030102 00048 EU 2003 1 2 HEEA082661 1 20021211 A 6410 11731743 BLADE BOLKMS 117 BK117A1 5626010 EU TAIL ROTOR ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 TAIL ROTOR BLADE HAS PAINT EROSION. 1 G 7 2 3U H13EU 2003010200049 20030102 00049 EA 2003 1 2 02361705 1 20021227 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 705BR 7470 During preflight inspection, the crew reported forward floor emergency light does not work. Maintenance personnel clean ed connector at first section off floor emergency lites. Ops ck'd good. Aircraft returned to service. 2 L 7 2 4F RT A21EA 2003010200050 20030102 00050 NM 2003 1 2 AWXA200300003 1 20021226 A 5754 D5746027700100 SLAT AIRBUS A319 A319132 3930340 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 814AW 0 0 1281 MCN - MAJOR REPAIR - DURING B-02 CHECK A 1/2" CRACK AND 1/2" X 1/2" SECTION OF #2 SLAT WAS FOUND MISSING AT THE UPPER TR AILING EDGE 8" FROM THE INBOARD END. MAINTENANCE BLENDED OUT DAMAGED AREA ON #2 SLAT AT UPPER TRAILING EDGE INBOARD END; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; AND INSTALLED REPAIR PART IAW AWA E .R. 25-5740-02365-JS1. 2 L 7 2 4F RT A28NM 2003010200052 20030102 00052 NE 2003 1 2 S02472009 2 20020408 A 7200 ENGINE PWA BOEING 747 747400 NM PWA 4056 PW4056 NE NR 1 FAILED W SAJF E ENGINE SHUTDOWN O OTHER CL CLIMB 1 WP 03 28710 DURING TAKE OFF ROLL NR 1 ENGINE SURGE ENCOUNTERED. AFTER AIRBORNE NR 1 ENGINE SHUT DOWN AND AIR TURN AROUND. AN UNEVENT FUL LANDING WAS ACCOMPLISHED. NR 1 ENGINE INLET AND EXHAUST VISUAL INSPECTION. CONDITION NORMAL. CHECKED CHIP DECTECTO R CONDITION NORMAL. NR 1 ENGINE FADEC BITE CHECK, NO FAULT MESSAGE WAS SET. PRILIMINARY ANALYSIS GROUP 3 SURGE WAS SUS PECTED. AN AOG TEAM HAD BEEN SENT AND SPARE ENGINE HAD BEEN SHIPPED ON 4/8/2002. NR 1 ENGINE HAD BEEN CHANGED. 2 L 7 4 4F 4 F RT A20WE E24NE 2003010300002 20030103 00002 EU 2003 1 3 HEEA082662 1 20021211 A 6410 11731743 BLADE BOLKMS 117 BK117A1 5626010 EU TAIL ROTOR ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 TAIL ROTOR BLADE HAS PAINT EROSION. 1 G 7 2 3U H13EU 2003010300004 20030103 00004 GL 2003 1 3 AC2A082141 2 20021212 A 7323 23065123 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL NR 2 ENGINE LOOSE H AC2A K NONE O OTHER IN INSP/MAINT 1 FS 01 50588 9904 780 890915 POTTING COMPOUND IS BROKEN LOOSE AT SHAFT REPLACED WITH SERVICEABLE GOVERNOR 1 G 7 2 3U 3 U H3EU E4CE 2003010300005 20030103 00005 GL 2003 1 3 AC2A082143 2 20021217 A 7323 23065123 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL ENGINE LOOSE H AC2A K NONE O OTHER IN INSP/MAINT 1 FS 01 50588 9301 780 POTTING COMPOUND IS BROKEN LOOSE AT SHAFT REPLACED WITH SERVICEABLE GOVERNOR. 1 G 7 2 3U 3 U H3EU E4CE 2003010300006 20030103 00006 SW 2003 1 3 AC2A082144 1 20021217 A 8097 SM20CCD200B21 CONTACTOR BELL 430 430 1182150 SW STARTER MALFUNCTIONED H AC2A K NONE O OTHER IN INSP/MAINT 1 FS 01 430CT 967 49089 AFTER BEING ENGAGED, THE START CONTACTOR WOULD ONLY DISENGAGE BY TURNING BATTERY SWITCH OFF. REPLACED PART. 1 G 7 2 3U RT H9SW 2003010300007 20030103 00007 EU 2003 1 3 BAQA081531 1 20021125 A 2140 1177258203 VALVE BOLKMS BK117 BK117C1 5626025 EU HEATER INTERFERENCE H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 117NC 1427 7517 HEATER MIXIING VALVE HAS INTERMITTENT OPERATION. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U NC H13EU 2003010300008 20030103 00008 EU 2003 1 3 BAQA081644 1 20021212 A 2140 JBS8803 VALVE UROCOP EC135 EC135T1 5620026 EU HEATER MALFUNCTIONED H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 533ME 960 132 MIXING VALVE WOULD NOT MODULATE TEMPERATURE. FULL HOT ALL THE TIME. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2003010300009 20030103 00009 WP 2003 1 3 IXXA0200158O 1 20021231 A 3260 SWITCH DOUG DC8 DC873F 302199F WP NOSE GEAR LOOSE A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 605AL 91511 429 46106 ON APPROACH TO SAN CREW NOTICED NOSE LANDING GEAR "GREEN" INDICATING LIGHTS NOT ILLUMINATED. CREW FOLLOWED COMPANY PROCE DURE AND RETURNED TO SAN FOR AN UNEVENTFUL LANDING. INSPECTION REVEALED THE NOSE GEAR PROXIMITY SWITCH CONNECTOR HAD BEC OME INSECURE. MAINTENANCE SECURED THE CONNECTOR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL PERFORMED AN OPERATIO NAL CHECKOUT OF THE SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 4 4F RT 4A25 2003010300010 20030103 00010 2003 1 3 BAQA082135 4 20021217 A 3120 B1894522281A CLOCK UROCOP EC135 EC135T1 5620026 EU COCKPIT INTERMITTENT H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 511ME 664 0143 CLOCK HAS INTERMITTENT OPERATION. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2003010300020 20030103 00020 2003 1 3 CZMA082767 4 20020329 A 3424 214075244101 GYRO BELL 412 412 1182202 SW COCKPIT FAILED E CZMA K NONE L NO TEST IN INSP/MAINT 1 SO 03 911BE 6670 36018 GYRO FAILED REPLACED WITH IN HOUSE SPARE. 1 G 7 2 4U H4SW 2003010300021 20030103 00021 SW 2003 1 3 ERAA082696 1 20021107 A 6220 412010190103 SPINDLE 412010100139 BELL 412 412 1182202 SW ROTOR HEAD CRACKED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 416EH 6552 AAD00014M 33011 SPINDLE IS CRACKED IN SPLINE AREA. AWAITING METALURGICAL TESTS. 1 G 7 2 4U H4SW 2003010300022 20030103 00022 SW 2003 1 3 ERAA082699 1 20021114 A 6220 412010190103 SPINDLE 412010100139 BELL 412 412 1182202 SW ROTOR HEAD DEBONDED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 412EH 9022 AAD00057M 33001 SPINDLE BEARING IS DEBONDED. MATCHED UP WITH PITCH HORN. BEARING TOTALLY SEPERATED FROM SPINDLE. DUE TO TT OF SPINDLE , SPINDLE WILL BE STORED, NOT ECONOMICAL TO REPAIR. INSTALLED PITCH HORN ON NEW SPINDLE, TORQUED AND SAFTIED IAW 412 C R&O. 1 G 7 2 4U H4SW 2003010300023 20030103 00023 SW 2003 1 3 ERAA082700 1 20021114 A 6220 412010190103 SPINDLE BELL 412 412 1182202 SW ROTOR HEAD SPLIT H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 419EH 6091 AAD00037M SPINDLE BEARING STARTING TO SPLIT, DELAMINATING. SPINDLE SCRAPPED. PITCH HORN, NUT, WASHER AND PINS (8EA) VISUALLY I NSPECTED AND FOUND TO BE IN SERVICEABLE CONDITION IAW BHT-412-CR&O. ALL PARTS RTS'D. 1 G 7 2 4U H4SW 2003010300024 20030103 00024 SW 2003 1 3 ERAA082702 1 20021114 A 6510 212040600005 HANGER ASSY BELL 412 412 1182202 SW TAIL ROTOR LEAKING A ERAA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 03 167EH 10773 33089 GREASE LEAKING EXCESSIVELY FROM BEARING. BEARING DENTED AT GREASE SEAL. CAP RETAINER WRONG PART NUMBER. DISASSEMBLED , CLEANED, VISUALLY INSPECTED ALL PARTS AND COMPLIED WITH NDT. REASSEMBLED INSTALLING NEW BEARING, NEW SEAL, NEW CAP RE TAINER, NEW TEMP PLATES AND HARDWARE. REPACKED COUPLING WITH GREASE DATED 9-20-01. OVERHAULED IAW BHT 412-CR&JO CHAPTE R 65 TT 10773.0. 1 G 7 2 4U H4SW 2003010300025 20030103 00025 SW 2003 1 3 ERAA082703 1 20021115 A 6310 212040005103 DRIVE SHAFT BELL 412 412 1182202 SW MAIN ROTOR CORRODED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 169EH 15355 33064 TEMPLATE TURNED BLACK. PITTING ON SPLINES OF INNER & OUTER COUPLING. C/W PRELIMINARY ISPECTION & FOUND TEMPLATE MISSING AND TEMPLATE BLACK. DISASSEMBLED, CLEANED & VISUAL INSPECTED ALL PARTS. FOUND NO OBVIOUS REASON FOR TEMPLATE TO BE BL ACK. PITTING BEYOND LIMITS ON INNER & OUTER FWD COUPLING. SCRAPPED IAW CR&O CHAP 63 INSTALLED NEW INNER & OUTER COUPLI NG. INSTALLED NEW TEMPLATES, O RINGS & REPACKED WITH GREASE DATED 9-20-01. REASSEMBLED WITH NEW WASHERS & BOLTS. TORQ UED & SAFTIED ALL REQUIRED HARDWARE & C/W PULL TEST ON TEMPLATES. 1 G 7 2 4U H4SW 2003010300026 20030103 00026 EU 2003 1 3 ERAA082704 1 20021115 A 6420 10531714 ROTOR HEAD BOLKMS 105 BO105A EU TAIL ROTOR STIFF H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 291EH 13134 S842 AC HAS STIFF PEDALS. SUSPECT TAIL ROTOR IS CAUSE. NO OBVIOUS DEFECTS TO BUSHINGS. BLADES HAVE SHIPPING DAMAGE. REMOVE D BLADES & MOUNTING FORKS. VISUALLY INSPECTED & DIMENSIONS CHECKED FRICTION SURFACES OF PITCH CHANGE BUSHINGS; NO DEFEC TS. COMPLIED WITH PULL TEST ; NO DEFECTS. BENT BLADES OUT FOR EVALUATION DUE TO SHIPPING DAMAGE. INSTALLED 2 SERVICE ABLE BLADES, REASSEMBLED & STATIC BALANCED.REPAIRED IAW BO-105 REM 301, MM CH 33,34 & 107 TT 13134.4 TSI 296.1. 1 G 7 2 3U H3EU 2003010300027 20030103 00027 EU 2003 1 3 ERAA082705 1 20021115 A 6320 4638001007 TRANSMISSION BOLKMS 105 BO105S 5626006 EU MAIN ROTOR MAKING METAL H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 152EH 12902 S701 TRANSMISSION MAKING METAL. MAST BEARING INNER RACE BREAKING DOWN, MIXING LEVER BEARINGS FROZE UP, BEARING BLOCK BEARING S ROUGH, ACCESS. DRIVE SEALS LEAKING, TOP CASE BEARING PITTED, SWASHPLATE BOOT TORN, COLLECTIVE LEVER BEARINGS ROUGH. RE MOVED TOP CASE ASSY, FOUND MAST BEARING BREAKING DOWN, INSTALLED NEW MAST BEARINGS, MAST SEAL, REASSEMBLED & REINSTALLED LT & RT INPUTS, COMPLIED WITH AD 97.26-02, ASB BO-105-10-110, ASB BO-105-40-103. REASSEMBLED IAW REM 103. COMPLIED WIT H AD97-26-02, ASB BO-105-10-110, ASB BO-105-40-103. 1 G 7 2 3U H3EU 2003010300028 20030103 00028 EU 2003 1 3 ERAA082706 1 20021115 A 6320 4638001001 TRANSMISSION BOLKMS 105 BO105C 5626005 EU MAIN ROTOR MAKING METAL H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 4046 TRANSMISSION MAKING METAL. OIL MANIFOLD, TEMP PLUG & SWASHPLATE DRIVE LINK BUSHING NOT INSTALLED ON TRANSMISSION. PLAN ETARY AXLE BREAKING DOWN. SCRAPPED 1 GEAR, 5 PLANETARY AXLES, 5 DOUBLE ROW CAGES. REMOVED TOP CASE, LT & RT INPUT PINIO NS & PLANETARY, DISASSEMBLED LT & RT PINIONS & PLANETARY. REPAIRED PLANETARY, REASSEMBLED PLANETARY & PINION ASSYS, REA SSEMBLED & REINSTALLED IAW REM 103. 1 G 7 2 3U H3EU 2003010300029 20030103 00029 EU 2003 1 3 ERAA082707 1 20021119 A 5302 10530051 STRUCTURE BOLKMS 105 BO105S 5626006 EU TAILBOOM CRACKED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 294EH S675 BULKHEAD, SKINS, LONGERON CRACKED. GEARBOX FITTING CORRODED. REPLACED SKIN, FLANGE, LONGERON, BULKHEAD. CLEAN, TREATED AND PRIMED ALL CORROSION. 1 G 7 2 3U H3EU 2003010300030 20030103 00030 EU 2003 1 3 ERAA082708 1 20021119 A 6320 SLEEVE BOLKMS 105 BO105A EU TRANSMISSION STIFF H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 290EH 14806 863 S850 SLIDING SLEEVE STIFF. SLIDING SLEEVE BUSHINGS ARE VERY TIGHT, UPON REMOVAL SLIDING SLEEVE, SCRAPPED DUE TO EXCESSIVE CO RROSION. INSTALLED NEW SLIDING SLEEVE, MAST SEAL & PACKINGS. REASSEMBLED TOP CASE ASSY & REINSTALLED IAW REM 103, COM PLIED WITH FREEWHEEL INSPECTION IAW REM 103. 1 G 7 2 3U H3EU 2003010300031 20030103 00031 EU 2003 1 3 ERAA082709 1 20021119 A 6320 SLEEVE BOLKMS 105 BO105C 5626005 EU TRANSMISSION STIFF H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 14806 863 TRANSMISSION SLIDING SLEEVE STIFF. 1 G 7 2 3U H3EU 2003010300032 20030103 00032 EU 2003 1 3 ERAA082710 1 20021119 A 3212 D24873102 FLOAT BOLKMS 105 BO105S 5626006 EU MLG LEAKING H ERAA K NONE L NO TEST IN INSP/MAINT 1 FS 01 131EH 5315 595 PERFORMED 6 MONTH INSPECTION. FLOAT HAS TORN END CAP, AND LEAK IN NR 2 CELL. PERFORMED 6 MONTH INSPECTION, REPLACED EN D CAP, & REPAIRED LEAK. 1 G 7 2 3U H3EU 2003010300033 20030103 00033 EU 2003 1 3 ERAA082711 1 20021119 A 3212 D24873102 FLOAT BOLKMS 105 BO105S 5626006 EU MLG LEAKING H ERAA K NONE L NO TEST IN INSP/MAINT 1 FS 01 296EH 9330 S849 RT FLOAT ASSY DUE 6 MONTH INSPECTION. CYLINDER LEAKING BETWEEN VALVE ASSY, AND CYLINDER HEAD. FLOAT COVER TORN. REMOVE D AND REPLACED O-RING AND GASKET FOR CYLINDER LEAK. REMOVED AND REPLACED FLOAT COVER. 1 G 7 2 3U H3EU 2003010300034 20030103 00034 EU 2003 1 3 ERAA082713 1 20021119 A 3212 D24873102 FLOAT BOLKMS 105 BO105S 5626006 EU MLG LEAKING H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 125EH 11914 S562 RT FLOAT ASSY DUE 6 MONTH INSPECTION. BAG LEAKING, COVER WORN, REPLACED CYLINDER, PERFORMED 6 MONTH INSPECTION. CHANGED BAG & COVER, & REPLACED CYLINDER, & PERFORMED 6 MONTH INSPECTION. COMPLIED WITH ERA AAIP & AIR CRUISERS. 1 G 7 2 3U H3EU 2003010300035 20030103 00035 GL 2003 1 3 ERAA082715 2 20021120 A 7320 252466715H GOVERNOR BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20 03013 GL ENGINE MALFUNCTIONED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 292EH 11001 562 CANNOT MAKE FINE ADJUSTMENTS TO ACHIEVE MAX BEEP. UNIT HAD DROOP. CHANGE BUSHING, D BEARING, L BEARINGS, W BEARINGS, TU BE DIAPHRAGM. REPAIRED AND FUNCTIONALLY TESTED. 1 G 7 2 3U 3 U H3EU E4CE 2003010300036 20030103 00036 GL 2003 1 3 ERAA082716 2 20021120 A 7320 2524667 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL ENGINE MALFUNCTIONED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 124EH 8614 S559 UNABLE TO ADJUST FOR TORQUE SPLITS. PC, PY FITTINGS LOOSE. LEVER CAM WORN, O LEVER. REPLACED WORN PARTS FOUND DURING INSPECTIN IAW CMM 73-20-25. FUNCTIONALLY TESTED 10-29-02. 1 G 7 2 3U 3 U H3EU E4CE 2003010300037 20030103 00037 NE 2003 1 3 ERAA082718 1 20021120 A 6510 7636104007041 BEARING SKRSKY S76 S76A 8143006 NE TAIL ROTOR WORN H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 579EH 760274 BEARING WORN & SOME CORROSION. MISMATCHED INNER AND OUTER HOUSINGS. 763610401103 OUTER HOUSING WITH S613764325001 INNE R HOUSING INSTALLED. MISMATCHED MAGNESIUM INNER HOUSING, REPLACED WITH INNER HOUSING PN S613764325102 TO MATCH PN 763610 4012103 ALREADY INSTALLED UNIT NDW REVERTS TO PN 7636104007042. 1 G 7 2 3U H1NE 2003010300038 20030103 00038 NE 2003 1 3 ERAA082719 1 20021120 A 6210 6117020201067 BLADE SKRSKY S61 S61N 8142104 NE MAIN ROTOR DEBONDED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 561EH 8277 61471 LEADING EDGE DEBONDED. SENT TO REPAIR STATION FOR REPAIRS. INSPECTED PER SRM SA 4045-31E CHAPTER SECTION 65-10-01 REV 5. PATCHED POCKETS NR 8, 9 & 20 ON LOWER SURFACE AND NR 6 & 17 ON UPPER SURFACE PER S61 SRM SA404531E DATED 1 NOVEMBER 1970 CHANGE 30 APRIL 1998. REPLACED ALL ABRASION STRIPS PER S61LN SRM SA4040531E CHAPTER 65-10-01 PROCEDURE 4C AND SB61B 15-25C. RECHARGED SPAR PER S-61N MM SA4045-80 REV MARCH 1, 1978. 2 G 7 2 4U 1H15 2003010300039 20030103 00039 NE 2003 1 3 ERAA082720 1 20021120 A 6210 617020201067 BLADE SKRSKY S61 S61N 8142104 NE MAIN ROTOR ERODED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 561EH 81741 61471 MAIN ROTOR BLADE HAS ERODED OR PUNCTURED LEADING EDGE. REPLACED 2 EA OUTBOARD STRIPS, REPLINED NR 18 POCKET L/S, REPLACE D METAL BUTT COVERS, STATIC BALANCED, TOUCHED UP PAINT, RECHARGED SPAR. 2 G 7 2 4U 1H15 2003010300040 20030103 00040 SW 2003 1 3 ERAA082721 1 20021120 A 6230 412040366105 MAST BELL 412 412 1182202 SW MAIN ROTOR LEAKING H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 164EH 11790 33004 MAST SEAL IS LEAKING. MAST SPLINES CORRODED, BEARING PITTED, NUT CORRODED, PLATE PITTED, RACE NUT GOUGED, LINGER SCORED & WORN. DISASSEMBLED FOR SEAL CHANGE & FOUND CORROSION. COMPLETELY DISASSEMBLED AND FOUND MAST UNECONOMICAL TO REPAIR DUE TO SO MANY UNSERVICEABLE ITEMS. PERFORMED VISUAL & NDT INSPECTIONS ON LOCK PLATE & CHECKED SLINGER AND FOUND NO DEF ECTS. SCRAPPED MAST ASSEMBLY. 1 G 7 2 4U H4SW 2003010300041 20030103 00041 GL 2003 1 3 ERAA082724 2 20021121 A 7250 6898731 SUPPORT BOLKMS 105 BO105A EU ALLSN 250C 250C20 03013 GL TURBINE SECTION CRACKED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 291EH S842 POWER TURBINE SUPPORT WAS OVERHAULED AND RETIRED WITH A CRACK ADJACENT TO A TACK WELD ON 25-28 SEAL. 1 G 7 2 3U 3 U H3EU E4CE 2003010300042 20030103 00042 EU 2003 1 3 HEEA082663 1 20021211 A 7923 209072433007 VALVE BOLKMS 105 BO105S 5626006 EU OIL SHUTOFF STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136H S833 DECK VALVE STUCK OPEN. 1 G 7 2 3U H3EU 2003010300044 20030103 00044 GL 2003 1 3 HEEA082664 2 20021211 A 7320 23033400 FILTER BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL PC AIR DAMAGED E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 5031U S678 PC FILTER HANG STARTS ON ENGINE RINSE CYCLE. SCRAPPED. 1 G 7 2 3U 3 U H3EU E4CE 2003010300045 20030103 00045 GL 2003 1 3 HEEA082665 2 20021211 A 7320 B-NUT BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL PC TUBE STRIPPED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U S678 PC TUBE FROM SCROLL TO PC FILTER B-NUT STRIPPED. SCRAPPED. 1 G 7 2 3U 3 U H3EU E4CE 2003010300047 20030103 00047 EU 2003 1 3 HEEA082667 1 20021211 A 7714 DRIVE SHAFT BOLKMS 105 BO105S 5626006 EU TACH GENERATOR BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6607K S841 DRIVE SHAFT BROKEN. REPAIRED. 1 G 7 2 3U H3EU 2003010300048 20030103 00048 EU 2003 1 3 HEEA082668 1 20021211 A 7810 4606AC CLAMP BOLKMS 105 BO105S 5626006 EU EXHAUST PIPE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 EXHAUST PIPE CLAMP CRACKED. SCRAPPED. 1 G 7 2 3U H3EU 2003010300049 20030103 00049 EU 2003 1 3 HEEA082669 1 20021211 A 6520 4619003003 ROTOR HEAD BOLKMS 105 BO105S 5626006 EU TAIL ROTOR CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 81832 18120 S828 INPUT FLANGE AND SWASHPLATE AREA RUSTED. REPAIRED. 1 G 7 2 3U H3EU 2003010300050 20030103 00050 EU 2003 1 3 HEEA082670 1 20021211 A 6320 4638001004 TRANSMISSION BOLKMS 105 BO105S 5626006 EU MAKING METAL E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 81992 18481 S827 TRANSMISSION MAKING METAL. REPAIRED. 1 G 7 2 3U H3EU 2003010300051 20030103 00051 EU 2003 1 3 HEEA082671 1 20021211 A 6320 4638001004 TRANSMISSION BOLKMS 105 BO105S 5626006 EU MAIN ROTOR MAKING METAL E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 7170D 10417 S840 TRANSMISSION MAKING METAL. REPAIRED. 1 G 7 2 3U H3EU 2003010300052 20030103 00052 2003 1 3 HEEA082672 4 20021211 A 3421 5040017901 INDICATOR BOLKMS 105 BO105S 5626006 EU COCKPIT INACCURATE E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5031U S678 ATTITUDE INDICATOR SHOWS 5 DEGREE BANK IN LEVEL FLIGHT. REPAIRED. 1 G 7 2 3U H3EU 2003010300053 20030103 00053 2003 1 3 HEEA082673 4 20021211 A 3421 504001790116 GYRO BOLKMS 105 BO105S 5626006 EU COCKPIT INOPERATIVE E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 7170D S840 HORIZON GYRO INOPERATIVE. REPAIRED. 1 G 7 2 3U H3EU 2003010300054 20030103 00054 2003 1 3 HEEA082674 4 20021211 A 2340 FACEPLATE BOLKMS 105 BO105S 5626006 EU INTERPHONE DAMAGED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 4573B 8109693 S673 FACEPLATE BAD. FOUND LIGHT PANEL, VOLUME AND SELECTOR KNOBS, SWITCHES S6, S10, AND S11 BAD. REPLACED, REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 2003010300055 20030103 00055 2003 1 3 HEEA082675 4 20021211 A 2370 ACS775SL AUDIO PANEL BOLKMS 117 BK117A1 5626010 EU COCKPIT DAMAGED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 911RZ 7092 VOLUME KNOB WILL NOT ADJUST ICS. 1 G 7 2 3U H13EU 2003010300058 20030103 00058 EU 2003 1 3 HEEA082678 1 20021213 A 7931 BSE206150G3 TRANSDUCER BOLKMS 105 BO105S 5626006 EU NR 2 ENGINE FAILED E HEEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 03 5031U S678 AFTER TAKEOFF NR 2 ENGINE OIL PRESSURE DROPPED TO ZERO. REPLACED NR 3 ENGINE OIL PRESSURE TRANSMITTER. 1 G 7 2 3U H3EU 2003010300059 20030103 00059 GL 2003 1 3 HEEA082679 2 20021213 A 7323 252466715 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL NR 2 ENGINE FAILED E HEEA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 03 7136H 11954 S833 NR 2 ENGINE DECELLED ON TAKEOFF. REPLACED NR 2 GOVERNOR. 1 G 7 2 3U 3 U H3EU E4CE 2003010300062 20030103 00062 EA 2003 1 3 SWIA200211645 1 20021126 A 5340 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR STR 1 CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 CARGO DOOR FORWARD TRACK CHANNEL STR 16L IS CRACKED. FOUND DURING C CHECK INSPECTION. REPAIRED DAMAGED CHANNEL IAW CRJ SRM 53-61-23, 51-24-16, 51-40-11, 51-25-06, 51-25-00, 51-42-06 & 51-24-11. 2 L 7 2 4F RT A21EA 2003011700113 20030117 00113 NM 2003 1 17 F3LA200200398 1 20021229 A 5730 SKIN BOEING 737 73736E 138443A NM RT WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 314FL 2419 25256 INSPECTION REPORTED APPROXIMATELY A 7 INCH CRACK IN THE RT WING L/E JUST ABOVE AND OUTBOARD OF NR 4 SLAT ACTUATOR. PERF ORMED INTERIM REPAIR PER SRM 51-70-14, PAGE 7, PARA 8. PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT C-CHECK. AREA WILL BE REINSPECTED EVERY A-CHECK PER SRM 51-70-14, PAGE 3, PARA 4, UNTIL PERMANENT REPAIR IS ACCOMPLISHED. 2 L 7 2 4F RT A16WE 2003010300064 20030103 00064 EA 2003 1 3 SWIA200211666 1 20021230 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA #2 MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 498SW 7483 ON BEGINNING OF TAKEOFF ROLL WE GOT A CONFIG. SPOILERS AURAL WARNING FOLLOWED BY GEN 2 OFF CAUTION MESSAGE. ABORTED TAK EOFF ROLL AND RETURNED TO THE GATE. PERFORMED QRH PROCEDURE WITH NO FURTHER FAULTS. SPOILERS NEVER DID DEPLOY. INSPEC TED THE SPOILERS AND COULD NOT FIND ANY FAULTS. SUSPECT THE SPOILERS FAULTED UPON POWER SWITCHING. DEFERRED THE #2 GEN ERATOR IAW 24-11-1B. REMOVED AND REPLACED #2 IDG IAW CRJ MM 24-11-01. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME. P/N OFF: 755471E S/N OFF: 1163 2 L 7 2 4F RT A21EA 2003010300065 20030103 00065 GL 2003 1 3 RAIA00212370 2 20021230 A 7421 20359139 IGNITER EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 801HK 145053 310137 5293-STL- RIGHT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED THE LOWER IGNITION IGNITER, OPS CK OK. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2003010300071 20030103 00071 SO 2003 1 3 LR7A02126 1 20021231 A 5330 SKIN LKHEED 382 382G 526414U SO FS 138 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2236 5025 DURING SCHEDULED C3 INSPECTION PER JOB CARD HC5303 FOUND FS 138 SKIN CRACKED AT LBL 36, WL 160.REPAIRED IAW SRM SMP 583 51-140-12. NR 2004. 2 H 7 4 4T A1SO 2003010300072 20030103 00072 SO 2003 1 3 LR7A02127 1 20021231 A 5312 3319685 SPLICE PLATE LKHEED 382 382G 526414U SO FS 497 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2236 5025 DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP53224 FOUND LH FS 497 BULKHEAD FITTING DOUBLER CRACKED AT LBL 50, WL 267. REPLACED SPLICE PLATE IAW SRM SMP 583 51-70. NR 2064. 2 H 7 4 4T A1SO 2003010600002 20030106 00002 GL 2003 1 6 2003FA0000006 3 20021231 A 6114 05503671 SPINNER CESSNA 172 172S 2072439 CE MCAULY 1A170 1A170E GL PROPELLER CRACKED D K NONE O OTHER IN INSP/MAINT 1 WP 07 586SP 172S8516 THIS AIRCRAFT HAS HAD NUMEROUS SPINNERS ( 5 ) AND REAR BULKHEAD FAILURES ( 3 ) EVEN AFTER COMPLIANCE WITH CESSNA SB02-61 -01. LATEST FAILURE WAS 47.8 HRS SINCE SPINNER REPLACEMENT AND SB COMPLIANCE. FAILURES OCCURRED AT THE FOLLOWING TIMES S PINNERS PN 0550367-1:828.3, 845.1, 1232.4, 1280.2, 1328.0,REAR BULKHEADS PN 055032111 : 967.0, 1232.4, 1280.2 SB 02-61-0 1 PERFORMED AT 967.0 AMD 1280.2 IT APPEARS THAT THE POLISHED SPINNERS OF THE MILLENNIUM EDITIONS DO NOT HAVE THIS PROBLE M DUE TO BEING MADE OUT OF SLIGHTLY THICKER MATERIAL. 1 H 7 1 3O NT 3A12 5 N P857 2003010600008 20030106 00008 CE 2003 1 6 11060230 1 20021113 A 7100 ENGINE BEECH 18 H18 1151012 CE GARRTT TPE331 TPE33110UA 01514 WP LT & RT FLAMED OUT E HKGA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 17 228A 32417 32417 BA629 BOTH ENGINES FLAMED OUT. INSPECTION DID NOT REVEL ANY MECHANICAL MALFUNCTION. AIRCRAFT LANDED SAFELY. DID NOT RELIGHT ON THEIR OWN. 1 L 7 2 3R 4 T A765 E4WE 2003010600009 20030106 00009 NE 2003 1 6 12262002 1 20021226 A 5600 7620601001112 WINDSHIELD SKRSKY S76 S76B 8143007 NE PWA PT6 PT6B36 52043 EA COCKPIT CRACKED E O OTHER O OTHER CR CRUISE 1 GL 09 176BA 7730 760317 PILOTS WINDSHIELD CRACKED IN FLIGHT WITH THE WINDSHIELD HEAT "ON". WHEN THE CRACK OCCURED, THERE WERE SPARKS COMING FROM THAT AREA. ALSO, THERE WERE TWO AREAS APPROXIMATELY 3 INCH IN LENGTH THAT HAD MELTED PLASTIC EXTRUDED OUT OF THE CRACK. THE INNER LAYER OF GLASS SHOWED NO SIGNS OF DAMAGE. 1 G 7 2 4U 4 U H1NE E4EA 2003010600025 20030106 00025 SO 2003 1 6 2003F00000 1 20021220 A 5210 46624003 SUPPORT PIPER PA31T PA31T 7103124 SO PAX DOOR HINGE CRACKED B K NONE O OTHER IN INSP/MAINT 1 SW 09 199ND 31T7620035 DURING PREFLIGHT INSPECTION PILOT FOND A MISSING RIVET ON THE MAIN CABIN DOOR HINGE FWD END. AFTER OPENING INTERIOR OF D OOR SUPPORT PN 46624-003 WAS FOUND TO HAVE A CRACK APPROXIMATELY 6 INCHES LONG, JUST ABOVE HINGE ATTACHMENT. ATTACHING BULKHEADS PN 46550-004 AND 46526-000 WERE ALSO CRACKED AT HINGE ATTACHMENT. DOOR WAS REPAIRED BY INSTALLING NEW SUPPORT AND BULKHEADS PER STANDARD PRACTICES. 1 L 7 2 3T A8EA 2003010600026 20030106 00026 CE 2003 1 6 2003F00007 1 20020516 A 7110 B140048 LATCH BEECH 200 200BEECH 1152920 CE RT ENGINE FAILED A HSYA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 05 4298S BB198 AFTER LEVELING OFF AT FLIGHT LEVEL 160, CREW NOTICED THAT THE AFT EDGE OF THE UPPER FORWARD RT ENGINE COWLING APPEARED T O BE DISPLACED. DECLARED AND EMERGENCY AND RETURNED. MISLATCHED UPPER FORWARD COWLING AFT LATCH. COWLING AND LATCHES WERE INSPECTED FOR DAMAGE, AND MISADJUSTMENT, RESECURED, AND THE AIRCRAFT RETURNED TO SERVICE. THERE HAVE BEEN NO FURTH ER PROBLEMS SINCE THAT TIME. 1 L 7 2 4T A24CE 2003010600033 20030106 00033 CE 2003 1 6 BX42002F00000 1 20021203 A 5531 0531006110 SPAR CESSNA 172 172N 2072434 CE LYC O320 O320* 41508 EA VERTICAL STAB CRACKED B BX4R K NONE O OTHER IN INSP/MAINT 1 NM 03 739VN 4216 17270842 FIN REINFORCEMENT ASSEMBLY (FORWARD SPAR) IS CRACKED AND BROKEN. JUST ABOVE WHERE THE LOWER RIBS ARE RIVETED TO THE REI NFORCEMENT. THE REINFORCEMENT IS BROKEN THRU ITS WEB FROM RELIEF TO RELIEF, ONLY THE FLANGES ARE INTACT. THE LOWER FOR WARD RIB IS CRACKED ON THE RIGHT SIDE WHERE IT IS RIVETED TO THE REINFORCEMENT. 1 H 7 1 3O 3 O NT 3A12 E274 2003010600034 20030106 00034 CE 2003 1 6 BYK2002F00000 1 20021119 A 8120 12583921 TURBOCHARGER CESSNA 210 T210M 2073451 CE CONT O520 TSIO520* 17040 SO ENGINE FOD D BYKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 17 761HS 3062 21062275 TOTAL FAILURE OF TURBO CHARGER DURING TAKE OFF ROLL DUE TO THE STEEL STRIP FOR INDUCTION ALTERNATE AIR DOOR MAGNET WEDGE D INTO TURBO INLET BLADES. LEADING EDGES OF ALL INTAKE TURBINE BLADES DAMAGED. DISSIMILAR METAL CORROSION OF STEEL STR IP ATTACHMENT ALUMINUM RIVETS. CORRODED RIVETS FAILED, STEEL STRIP DROPPED AND WAS DRAWN INTO TURBO INTAKE. CLEANED DO OR AND STEEL STRIP BY BEAD BLASTING, REASSEMBLED USING (2 PART) SEALING COMPOUND BETWEEN THE PARTS FOR ADDED STRENGTH AN D NEW RIVETS. TURBO ASSEMBLY WAS REPLACED. 1 H 7 1 3O 3 O 3A21 E8CE 2003010600035 20030106 00035 CE 2003 1 6 CGO2002F00007 1 20021203 A 7331 12181302 TRANSDUCER RAYTHN 390 390 CE WILINT FJ44 FJ44 66000 GL FUEL FLOW LEAKING B CGOR K NONE K FLUID LOSS IN INSP/MAINT 1 GL 03 972PF 12 RB38 INVESTIGATED PILOT COMPLAINT OF FUEL PUDDLING IN BOTTOM OF LT COWLING. FOUND FUEL FLOW INDICATING TRANSDUCER LEAKING IN TERNALLY. FIRST TRANSDUCER REPLACED AT 132.8 HRS FOR SAME FAULT. INSTALLED OVERHAULED UNIT, LEAK CHECKED OK. NOTED ON TEAR DOWN REPORT FOR INSTALLED UNIT THAT WAS OVERHAULED FOR SAME COMPLAINT OF LEAKAGE. 1 7 2 3F 4 F RT A00010WI E3GL 2003010600036 20030106 00036 EA 2003 1 6 K7B2002F00000 2 20021201 A 7322 30804 FLOAT CESSNA 172 172M 2072418 CE LYC O320 O320E2D 41508 EA CARBURETOR CRACKED A K7BA K NONE O OTHER IN INSP/MAINT 1 WP 07 21272 BL2010167 17263920 RECEIVED THIS CARBURETOR FLOAT IN CRACKED CONDITION. CAUSE UNKNOWN. FLOAT HAS SPLIT IN SEAM. 1 H 7 1 3O 3 O NT 3A12 E274 2003010600037 20030106 00037 CE 2003 1 6 MGO2002F00000 1 20021213 A 3610 3909740320005 LINE RAYTHN 390 390 CE PNEUMATIC LINE SPLIT B MGOR K NONE O OTHER IN INSP/MAINT 1 CE 09 414TE RB4 PNEUMATIC LINE PROVIDES FOR A MOISTURE DRAIN POINT FOR THE PNEUMATIC MANIFOLD WHICH PROVIDES REGULATED AIR PRESSURE TO T HE HYDRAULIC PACKAGE THE PRIMARY OUTFLOW VALVE, THE COCKPIT ALTERNATE AIR VALVE AND PASSENGER DOOR SEAL. LINE IS BULGED AND SPLIT 1.250 INCHES FROM LOWER END. PROBABLE CAUSE WAS FREEZING OF ACCUMULATED MOISTURE IN LINE. 1 7 2 3F RT A00010WI 2003010600038 20030106 00038 GL 2003 1 6 MNG2002F00000 1 20021209 A 7120 14059001 ISOLATOR CIRRUS SR SR22 2130001 GL CONT O550 IO550* SO ENGINE MOUNT FAILED B MNGR K NONE O OTHER IN INSP/MAINT 1 SW 05 730CD 300 0053 DURING TROUBLESHOOTING FOR ENGINE VIBRATION IT WAS NOTED THAT THE FRONT ENGINE MOUNTS WERE SAGGING TO THE POINT THAT THE ISOLATOR WAS TOUCHING THE ENGINE MOUNT STRUCTURE. REPLACEMENT OF THE ISOLATORS WAS NEEDED. 1 L 7 1 3O 3 O NT A00009CH E3SO 2003010600039 20030106 00039 GL 2003 1 6 MNG2002F00001 1 20021209 A 1430 RIVET CIRRUS SR SR22 2130001 GL CONT O550 IO550* SO ATTACH BRACKET FAILED A MNGR K NONE O OTHER IN INSP/MAINT 1 SW 05 730CD 300 0053 RIVETS HOLDING THE ATTACH BRACKET TO THE INTAKE ASSEMBLY, FAILED AND CAME OUT. THE RIVETS HAD NO WHERE TO GO BUT THROUG H THE INTAKE AND THROUGH THE ENGINE. THE MANUFACTURER IS AWARE OF PROBLEM, BUT HAS NOT YET CORRECTED. 1 L 7 1 3O 3 O NT A00009CH E3SO 2003010600046 20030106 00046 NM 2003 1 6 SROM200200027 1 20021217 A 5720 6552263 GUSSET BOEING 737 737205 1384456 NM WING GOUGED C SROM K NONE O OTHER IN INSP/MAINT 1 AL 03 736BP 32285 1255 23465 DURING C CHECK INSPECTION FOUND NUMBER TWO FIXED FAIRING NR 3 RIB GUSSET GOUGED. REMOVED, FABRICATED AND INSTALLED # 3 RI GUSSET PER SRM 54-30-1 & 51-30-2. MINOR REPAIR. 2 L 7 2 4F RT A16WE 2003010600048 20030106 00048 NM 2003 1 6 SROM200200029 1 20021219 A 5320 65512982 GUSSET BOEING 737 737205 1384456 NM FUSELAGE CRACKED C SROM K NONE O OTHER IN INSP/MAINT 1 AL 03 736BP 32285 1255 23465 DURING C CHECK INSPECTION FOUND FRAME GUSSET AT STA 520, STR 19L FWD SIDE CRACKED IN FRAME RADIUS. REMOVED FRAME GUSSET AND CRACKED ANGLE, FABRICATED REPLACEMENT ANGLE AND REINSTALLED ANGLE GUSSET PER 51-30-2 & 51-10-2. MAJOR REPAIR. 2 L 7 2 4F RT A16WE 2003010600049 20030106 00049 NM 2003 1 6 SROM200200030 1 20021219 A 5414 657377391 SKIN BOEING 737 737205 1384456 NM NR 1 NACELLE GOUGED C SROM K NONE O OTHER IN INSP/MAINT 1 AL 03 736BP 1255 23465 DURING C CHECK FOUND NR 1 ENGINE OUTBOARD COWL INNER SKIN GOUGED 24 INCHES FROM FWD END. REMOVED DAMAGE, FABRICATED REP AIR PARTS AND INSTALLED REPAIR PARTS PER SRM 54-30-1 & 53-30-3 MINOR REPAIR 2 L 7 2 4F RT A16WE 2003010600050 20030106 00050 NM 2003 1 6 SROM200200031 1 20021219 A 5311 6546596 FRAME BOEING 737 737205 1384456 NM ZONE 100 DENTED C SROM K NONE O OTHER IN INSP/MAINT 1 AL 03 736BP 32285 1255 23465 DURING C CHECK INSPECTION FOUND STA 727B FRAME DENTED STR 22R - 23R. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND INST ALLED PARTS PER SRM 51-40-3, PG 1, 2, 3 & 5. MAJOR REPAIR. 2 L 7 2 4F RT A16WE 2003010600051 20030106 00051 NM 2003 1 6 SROM200200032 1 20021219 A 5311 6546596 FRAME BOEING 737 737205 1384456 NM ZONE 100 DENTED C SROM K NONE O OTHER IN INSP/MAINT 1 AL 03 736BP 32285 1255 23465 DURING C CHECK INSPECTION FOUND AT STA 727A FRAME DENTED ON IB FLANGE STR 24L. REMOVED DAMAGE, FABRICATED REPAIR DOUBLE R AND REINSTALLED REPAIR PARTS PER SRM 51-40-1, FIG. 1. MAJOR REPAIR. 2 L 7 2 4F RT A16WE 2003010600052 20030106 00052 NM 2003 1 6 SROM200200033 1 20021219 A 5311 654868847 FRAME BOEING 737 737205 1384456 NM ZONE 100 MISINSTALLED C SROM K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 736BP 32285 1255 23465 DURING C CHECK INSPECTION FOUND A FRAME SEGMENT IN AFT LT MLG WHEELWELL STA 726 LBL 36 FOR CLOSEOUT PANEL THAT HAS A DOU BLE DRILLED HOLE. REMOVED AND REPLACED FRAME SEGMENT PER SRM 51-30-2 STEP 9A-D. MINOR REPAIR. 2 L 7 2 4F RT A16WE 2003010600053 20030106 00053 NM 2003 1 6 SROM200200034 1 20021219 A 5320 657893543 CHANNEL BOEING 737 737205 1384456 NM ZONE 100 CHAFED C SROM K NONE O OTHER IN INSP/MAINT 1 AL 03 736BP 32285 1255 23465 DURING C CHECK INSPECTION FOUND LT MLG WHEEL WELL CHANNEL AT 698 CHAFFED. REMOVED AND REPLACED LT WHEEL WELL CHANNEL PE R SRM 51-30-2 STEP 9A-D. MINOR REPAIR. 2 L 7 2 4F RT A16WE 2003010600054 20030106 00054 NM 2003 1 6 SROM200200035 1 20021219 A 5311 6546549 FRAME BOEING 737 737205 1384456 NM ZONE 100 DENTED C SROM K NONE O OTHER IN INSP/MAINT 1 AL 03 736BP 32285 1255 23465 DURING C CHECK INSPECTIONS FOUND AT STA 767 FRAME DENTED AT STR 22R. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND INST ALLED REPAIR PARTS PER SRM 51-40-3 FIG 1. MAJOR REPAIR 2 L 7 2 4F RT A16WE 2003010600062 20030106 00062 NE 2003 1 6 2003F00024 2 20021023 A 7310 O-RING BEECH 99 C99 1154006 CE PWA PT6 PT6A36 52043 NE LT ENGINE DAMAGED A HSYA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 05 175EE U175 BIL - DURING DESCENT INTO BIL, THE PILOT SELECTED THE LEFT BLEED TO ENVIRO, AND SMELLED FUEL VAPOR IN THE COCKPIT. FUEL LEAK AT THE LEFT ENGINE FLOW DIVIDER, AND DUMP VALVE. LEAK CHECKED ENGINE, FOUND FUEL LEAK AT THE FUEL PRESSURE SIDE O F THE DUMP VALVE, DISASSEMBLED, AND REPLACED THE O-RINGS, AND BACK UP RINGS. THE ENGINE WAS RUN AND LEAK CHECKED WITH N O LEAK NOTED. (M) 1 L 7 2 3T 4 T A14CE E4EA 2003010600063 20030106 00063 SO 2003 1 6 2003F00027 1 20021023 A 3231 12032943001 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO RT MLG DOOR OUT OF ADJUST A HSYA O OTHER J WARNING INDICATION CL CLIMB 1 NM 05 125AM 120017 CPR - FLT 8788 - RIGHT MAIN LANDING GEAR FORWARD DOORS DID NOT CLOSE WHEN GEAR UP WAS COMMANDED. THE DOOR SEQUENCE VALV E WAS OUT OF ADJUSTMENT. READJUSTED LANDING GEAR DOOR SEQUENCE VALVE IAW EMB MM AND OPERATIONALLY TESTED OPS CHECK OK. (M) 2 L 7 2 4T RT A31SO 2003010600064 20030106 00064 SO 2003 1 6 2003F00028 1 20021023 A 3231 12032943001 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO RT MLG OUT OF ADJUST A HSYA O OTHER J WARNING INDICATION CL CLIMB 1 NM 05 125AM 120017 CPR - FLT 8788 - RIGHT MAIN LANDING GEAR FORWARD DOORS DID NOT CLOSE WHEN GEAR UP WAS COMMANDED. THE DOOR SEQUENCE VALV E WAS OUT OF ADJUSTMENT. READJUSTED LANDING GEAR DOOR SEQUENCE VALVE IAW EMB MM AND OPERATIONALLY TESTED OPS CHECK OK. (M) 2 L 7 2 4T RT A31SO 2003010600065 20030106 00065 SO 2003 1 6 2003F00029 1 20021023 A 3231 12032943001 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO RT MLG OUT OF ADJUST A HSYA O OTHER J WARNING INDICATION CL CLIMB 1 NM 05 125AM 120017 CPR - FLT 8788 - RIGHT MAIN LANDING GEAR FORWARD DOORS DID NOT CLOSE WHEN GEAR UP WAS COMMANDED. THE DOOR SEQUENCE VALV E WAS OUT OF ADJUSTMENT. READJUSTED LANDING GEAR DOOR SEQUENCE VALVE IAW EMB MM AND OPERATIONALLY TESTED, OPS CHECK OK. (M) 2 L 7 2 4T RT A31SO 2003010600066 20030106 00066 SO 2003 1 6 2003F00030 1 20021015 A 3260 922AA2YA6P2722A PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO RT MLG MALFUNCTIONED A HSYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 125AM 120017 UPON DEPARTURE FROM CPR, WHEN THE GEAR HANDLE WAS COMMANDED TO THE RETRACTED POSITION THE 'A' SYSTEM LIGHT FOR THE RIGHT MLG ILLUMINATED AND THE RIGHT MLG REMAINED EXTENDED. AFTER CYCLING THE GEAR SEVERAL TIMES THE CREW RETURNED TO CPR. R IGHT MLG PROXIMITY SWITCH MALFUNCTION. THE RIGHT MLG 'A' SYSTEM PROXIMITY SENSOR WAS REPLACED, AND THE LANDING GEAR RET RACTION/EXTENSION SYSTEM WAS SUCCESSFULLY OPERATIONALLY TESTED. (M) 2 L 7 2 4T RT A31SO 2003010600067 20030106 00067 2003 1 6 SWAA022891 4 20021209 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2003010600068 20030106 00068 NM 2003 1 6 SWAA022892 1 20021210 A 3211 654611324 PIN BOEING 737 7373H4 1384600 NM LT/RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED C1 CHECK, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRU NNION PINS PER MM. 2 L 7 2 4F RT A16WE 2003010600069 20030106 00069 NM 2003 1 6 SWAA022894 1 20021210 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2003010600070 20030106 00070 NM 2003 1 6 SWAA022896 1 20021211 A 2560 P2070001 BATTERY BOEING 737 737301 1384611 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 660SW 23230 AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2003010600071 20030106 00071 NM 2003 1 6 SWAA022905 1 20021210 A 2560 P2070001 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 711HK 27845 DURING SCHEDULED PM CHECK, FOUND EMERGENCY FLASHLIGHT INOP AT FWD CABIN. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2003010600072 20030106 00072 NM 2003 1 6 SWAA022909 1 20021211 A 3350 20131ALP BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY EXIT LIGHTS AT ROW NR 7, NR 9, NR 11, NR 19 AND NR 20 LT INOP. REMOVED AND REPLACED BATTERY (M1135) PER MM. 2 L 7 2 4F RT A16WE 2003010600073 20030106 00073 2003 1 6 SWAA022917 4 20021212 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2003010600074 20030106 00074 2003 1 6 SWAA022919 4 20021214 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED SPECIAL VISIT, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER M M. 2 L 7 2 4F RT A16WE 2003010600075 20030106 00075 NM 2003 1 6 SWAA022920 1 20021214 A 2560 P2070001 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED SPECIAL VISIT, FOUND FWD LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2003010600076 20030106 00076 NM 2003 1 6 SWAA022925 1 20021213 A 5312 6516300 BULKHEAD BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 222 AND LBL 2 TO LBL 3. REPAIRED BULKHEAD WEB PER BFG ER. 2 L 7 2 4F RT A16WE 2003010600077 20030106 00077 NM 2003 1 6 SWAA022931 1 20021215 A 3211 6546113 PIN BOEING 737 7373H4 1384600 NM LT/RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED PM CHECK, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRU NNION PINS PER MM. 2 L 7 2 4F RT A16WE 2003010600078 20030106 00078 NM 2003 1 6 SWAA022933 1 20021215 A 3397 BR2013 WIRE BOEING 737 7372H4 138448C NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 090SW 22905 EEPLS INOP AT OVER WING EXIT. REPAIRED EEPLS WIRING PER MM. 2 L 7 2 4F A16WE 2003010600079 20030106 00079 2003 1 6 SWAA022934 4 20021216 A 2565 61620468 SLIDE BOEING 737 7375H4 138449D NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2003010600080 20030106 00080 NM 2003 1 6 SWAA022937 1 20021216 A 3350 D71702001 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 701GS 27836 DURING SCHEDULED 5Y CHECK, FOUND EMERGENCY LIGHT BATTERY PACK AT FWD GALLEY LT CEILING INOP. REMOVED AND REPLACED BATTE RY PER MM. 2 L 7 2 4F RT A16WE 2003012100190 20030121 00190 EU 2003 1 21 MALA020692 1 20021230 A 3246 BEARING BAC 146 AVRO146RJ85A 1500097 EU LT MLG FAILED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 504XJ E2311 DURING TAXI IN OF FLIGHT 3481, UPON TAXIING TO THE GATE THE GROUND CREW NOTICED SPARKS COMING FROM THE AREA OF THE LT I/ B BRAKE. THEY STOPPED THE A/C AND CHECKED THE BRAKES AND COULD NOT SEE ANYTHING WRONG. CREW CONTINUED TO BRING A/C UP T O THE GATE. AS THEY MOVED FORWARD THEY AGAIN SAW SPARKS COMING FROM THE SAME AREA. MAINTENANCE INSPECTED LT WHEEL ASSE MBLY INNER WHEEL BEARING FAILURE LOCKED ONTO AXLE. REPLACED AXLE IAW AMM 32-10-31. 2 H 7 4 4F RT A49EU 2003010600081 20030106 00081 NE 2003 1 6 SWAA022944 2 20021215 A 7320 8901274 SENSOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE FAULTY A SWAA K NONE P NO WARNING INDICATION LD LANDING 1 SW 29 378SW 26585 DURING LANDING ROLLOUT, NR 1 ENG EXPERIENCED TWO LOUD POPS, SHORTLY THERE AFTER TWO MORE LOUD POPS. COMPLIED WITH NR 1 ENG BORESCOPE INSP, AND REMOVED AND REPLACED NR 1 ENGINE CIT SENSOR PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010600082 20030106 00082 2003 1 6 SWAA022945 4 20021217 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2003010600083 20030106 00083 2003 1 6 SWAA022947 4 20021216 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2003010600084 20030106 00084 NM 2003 1 6 SWAA022948 1 20021217 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 092SW 22964 DURING SCHEDULED A2 CHECK, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 2003010600085 20030106 00085 NM 2003 1 6 SWAA022950 1 20021217 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2003010600086 20030106 00086 NM 2003 1 6 SWAA022951 1 20021217 A 3350 6556633 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2003010600087 20030106 00087 NM 2003 1 6 SWAA022952 1 20021217 A 3350 6104789 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED SERVICE CHECK, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2003010600088 20030106 00088 NM 2003 1 6 SWAA022954 1 20021218 A 3350 100855 CHARGER BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED A2 CHECK, FOUND AFT SECTION OF EEPLS AND BOTH AFT CABIN DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND R EPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F A16WE 2003010600090 20030106 00090 NE 2003 1 6 SWAA022961 2 20021217 A 7200 3321A1000 ENGINE BOEING 737 7373A4 1384585 NM GE CFM56 CFM56* 13802 NE LEFT MALFUNCTIONED A SWAA K NONE M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 29 679AA 23291 858519 DURING CLIMB-OUT, NR 1 ENGINE SURGED TO 107 PERCENT N1 AND NR 1 EGT RED LIGHT ILLUMINATED, NR 1 PMC INOP AND ALSO ILLUMI NATED. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010600091 20030106 00091 NM 2003 1 6 SWAA022963 1 20021218 A 2150 20405011 ACM BOEING 737 7375H4 138449D NM A/C BAY OVERHEATED A SWAA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SW 29 509SW 24186 SMOKE IN CABIN, RT A/C PACK TRIP OFF LIGHT ILLUMINATED. SHUT RT A/C PACK OFF AND SMOKE DISSIPATED. REMOVED AND REPLACE D RT AIR CYCLE MACHINE AND TURBO FAN PER MM. 2 L 7 2 4F RT A16WE 2003010600092 20030106 00092 NM 2003 1 6 SWAA022966 1 20021218 A 3350 65C27095 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2003010600093 20030106 00093 NM 2003 1 6 SWAA022969 1 20021219 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED C4 CHECK, FOUND EEPLS FWD LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2003010600094 20030106 00094 2003 1 6 SWAA022970 4 20021220 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 29 322SW 23343 AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2003010600095 20030106 00095 NM 2003 1 6 SWAA022971 1 20021222 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER TIE CL IP PER SRM. 2 L 7 2 4F RT A16WE 2003010600096 20030106 00096 2003 1 6 SWAA022972 4 20021219 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2003010600097 20030106 00097 NM 2003 1 6 SWAA022980 1 20021221 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 725SW 27857 EEPLS INOP AT ROW NR 2. REMOVED AND REPLACED EEPLS LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2003010600098 20030106 00098 2003 1 6 SWAA022981 4 20021220 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 080SW 22675 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2003010600099 20030106 00099 NM 2003 1 6 SWAA022982 1 20021220 A 3350 6556633 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 688SW 23254 RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2003010600101 20030106 00101 NM 2003 1 6 SWAA022984 1 20021221 A 3350 65C27093 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2003010600102 20030106 00102 NM 2003 1 6 SWAA022989 1 20021219 A 3350 612825 BATTERY BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED C3 CHECK, FOUND AFT CABIN OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTE RY PER MM. 2 L 7 2 4F RT A16WE 2003010600103 20030106 00103 NM 2003 1 6 SWAA022990 1 20021219 A 3350 604222 CHARGER BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED C3 CHECK, FOUND BOTH FWD ENTRY AND FWD SVC DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2003010600104 20030106 00104 NM 2003 1 6 SWAA022991 1 20021220 A 2612 7275W FIRE LOOP BOEING 737 7373H4 1384600 NM APU BAY FAULTY A SWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 356SW 25251 AIR TURNBACK, DECLARED EMERGENCY, DURING CLIMB APU FIRE WARNING LIGHT ILLUMINATED AND FIRE ALARM SOUNDED, DISCHARGED APU FIRE BOTTLE. APU WAS NOT RUNNING. REMOVED AND REPLACED APU FIRE DETECTION HARNESS AND FIRE BOTTLE PER MM. 2 L 7 2 4F RT A16WE 2003010600105 20030106 00105 NM 2003 1 6 SWAA022995 1 20021222 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPECIAL VISIT FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 360 AT STR 4R AND BS 908 AT STR 4L. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2003010600106 20030106 00106 NM 2003 1 6 SWAA022998 1 20021221 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 705SW 27839 EEPLS INOP AT FWD CABIN. REMOVED AND REPLACED (2 EA) LIGHT ASSY'S AND REPAIRED WIRING PER MM. 2 L 7 2 4F RT A16WE 2003010600107 20030106 00107 NM 2003 1 6 SWAA023000 1 20021222 A 2560 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 RT OVERWING EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2003010600108 20030106 00108 NM 2003 1 6 SWAA023001 1 20021222 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2003010600109 20030106 00109 NM 2003 1 6 SWAA023002 1 20021222 A 5210 507945 FLANGE BOEING 737 7373H4 1384600 NM ENTRY DOOR BENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 AFTER LANDING FWD ENTRY DOOR WOULD NOT OPEN. UNJAMMED FWD ENTRY DOOR, STRAIGHTEN OUT UPPER RT CORNER FLANGE AND REPAIRE D SEAL PER MM. 2 L 7 2 4F RT A16WE 2003010600112 20030106 00112 NM 2003 1 6 SROM200200036 1 20021225 A 3230 657376210 LANDING GEAR BOEING 737 737205 1384456 NM NOSE CONTAMINATED C SROM A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 733PA 4472 23466 ON AN AIRCRAFT EQUIPED WITH A NOSE GEAR GRAVEL DEFLECTOR SKI THE NOSE GEAR FAILED TO GIVE A UP AND LOCKED INDICATION 9 R ED NOSE GEAR LIGHT WOULD NOT GO OUT) UPON RETRACTION AFTER TAKE-OFF. RETURNED TO DEPARTURE AIRPORT WITHOUT INCIDENT. N OTE: THERE WAS HEAVY SNOW CONDITIONS AND THE SKI AREA WAS DE-ICED PRIOR TO TAXI. ACCOMPLISHED NOSE GEAR RETRACTION TES T AFTER REMOVING ICE FROM SKI. PS CHECKED GOOD PER WORK CARDS. NO PROBLEMS ON SUBSEQUENT FLIGHT. 2 L 7 2 4F RT A16WE 2003010600114 20030106 00114 2003 1 6 SWAA023006 4 20021223 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2003010600115 20030106 00115 NM 2003 1 6 SROM200200037 1 20021217 A 7110 6552263276 ANGLE BOEING 737 737205 1384456 NM FAIRING BROKEN C SROM K NONE O OTHER IN INSP/MAINT 1 AL 03 736BP 32285 1255 23465 DURING C CHECK INSPECTION FOUND NR 2 ENGINE INBOARD FIXED FAIRING'S 12TH RIB UPPER ANGLE BROKE. REMOVED, FABRICATED AND INSTALLED ANGLE AND GUSSET ON NR 2 I/B FIXED FAIRING PER SRM 51-30-2. MINOR REPAIR. 2 L 7 2 4F RT A16WE 2003010600116 20030106 00116 NM 2003 1 6 SWAA023008 1 20021225 A 3350 65C34691 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT AT ROW NR 1 INOP. REMOVED AND REPLACE D EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2003010600117 20030106 00117 NM 2003 1 6 SROM200200038 1 20021217 A 7110 65522631007 ANGLE BOEING 737 737205 1384456 NM NR 1 NACELLE BROKEN C SROM K NONE O OTHER IN INSP/MAINT 1 AL 03 736BP 32285 1255 23465 DURING C CHECK INSPECTION FOUND NR 1 I/B FIXED FAIRING'S NR 12 RIB ANGLE BROKE. REMOVED, FABRICATED AND INSTALLED ANGLE ON NR 12 RIB PER SRM 54-10 & 51-30-2. MINOR REPAIR. 2 L 7 2 4F RT A16WE 2003010600118 20030106 00118 NM 2003 1 6 SROM200200039 1 20021215 A 5410 6585378 BRACKET BOEING 737 737205 1384456 NM NR 1 NACELLE CRACKED C SROM K NONE O OTHER IN INSP/MAINT 1 AL 03 736BP 1255 23465 DURING C CHECK INSPECTION FOUND NR 1 ENGINE INLET COWL AFT FACE BRACKET CRACKED AT 5 O'CLOCK POSITION. REMOVED, FABRICA TED AND INSTALLED BRACKET ON #1 ENGINE INLET COWL PER SRM 51-20-01 & 51-30-2. MINOR REPAIR. 2 L 7 2 4F RT A16WE 2003010600119 20030106 00119 NM 2003 1 6 SROM200200040 1 20021215 A 5410 65NO7120223 INTERCOSTAL BOEING 737 737205 1384456 NM NR 2 NACELLE GOUGED C SROM O OTHER K FLUID LOSS IN INSP/MAINT 1 AL 03 736BP 32285 1255 23465 DURING C CHECK INSPECTION FOUND NR 2 ENGINE I/B FIXED FAIRING GOUGED ON INNER UPPER SURFACE 16 INCHES FROM FWD END. REM OVED AND REPLACED DAMAGED ANGLE PER SRM 51-30-2. MINOR REPAIR. 2 L 7 2 4F RT A16WE 2003010600120 20030106 00120 SW 2003 1 6 VE32002F00006 1 20021120 A 2913 206076022101 PUMP BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL HYDRAULIC SYS LEAKING A VE3R K NONE K FLUID LOSS IN INSP/MAINT 1 WP 23 305FD 598 4541 THE HYDRAULIC PUMP WAS LEAKING. IT WAS SENT TO A LOCAL VENDOR FOR REPAIR. THE VENDOR BORE PLUGGED FROM RESEVOIR PORT T O RELIEF BORE. THE CAUSE WAS EXCESSIVE CASTING IN THE HOLE AT MANUFACTURE. 1 G 7 1 3U 3 U H2SW E4CE 2003010600121 20030106 00121 EU 2003 1 6 VY1R103157 1 20020828 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE T/R GEARBOX FAILED B VY1R K NONE O OTHER IN INSP/MAINT 1 SW 19 6093R 373 2415 BEARING, UNITS FAILED WITH 373.9 TT, REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2003010600122 20030106 00122 NM 2003 1 6 SWAA023012 1 20021226 A 3350 50000043 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED A2 CHECK, FOUND BOTH OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2003010600123 20030106 00123 NM 2003 1 6 SWAA023013 1 20021226 A 3350 50000043 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 080SW 22675 DURING SCHEDULED PM CHECK, FOUND RT OVERWING AND RT AFT EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PE R MM. 2 L 7 2 4F A16WE 2003010600124 20030106 00124 EU 2003 1 6 VY1R103208 1 20020131 A 2913 1502780 SPLINE ADAPTER SNIAS 350 AS350B2 8680813 EU HYD PUMP WORN B VY1R K NONE O OTHER IN INSP/MAINT 1 SW 19 170PA 2637 HYDRAULIC PUMP SPLINE DRIVE WORN, WAS LUBRICATED IAW MSR PRIOR. 1 G 7 1 3U H9EU 2003010600125 20030106 00125 SW 2003 1 6 YBU2002F00000 1 20021122 A 3230 453041 BRACE GULSTM 112 114 7630314 SW LYC O540 IO540T4B5 41532 EA LT MLG CRACKED B YBUR O OTHER O OTHER LD LANDING 1 EA 03 5832N 2610 14381 L1768848A PILOT REPORTED NORMAL LANDING. THEN LOST CONTROL OF AIRCRAFT. AIRCRAFT CAME TO REST OFF THE LT SIDE OF THE RUNWAY, LT MAIN GEAR COLLAPSED. LT MAIN GEAR, UPPER DRAG BRACE SPLIT IN TWO. SUSPECTED METAL FAILURE, DUE TO IMPURTIES AND FATIGU E. 1 L 7 1 3O 3 O A12SO 1E4 2003010600126 20030106 00126 SW 2003 1 6 ALGA082680 1 20021224 A 6320 407040037101 BEVEL GEAR BELL 407 407 1182206 SW M/R GEARBOX SCORED H K NONE O OTHER IN INSP/MAINT 1 FS 01 408AL 1184 A516 53491 BEVEL GEAR CRACKED AT BOLT HOLE. THIS IS THE 1ST TIME THIS GEARBOX WAS OPENED UP FOR MAINT. SHAFT SCORED. REMOVE AND RE PLACED. 1 G 7 1 3U O H2SW 2003010600127 20030106 00127 SW 2003 1 6 ALGA082682 1 20021224 A 6420 406012108107 PITCH HORN BELL 407 407 1182206 SW TAIL ROTOR HEAD CORRODED H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 577AL 53247 STARTING TO SEE A TREND OF NUMEROUS PITCH HORNS WITH CORROSION PROBLEMS, IN BARREL NUT BORE. 1 G 7 1 3U O H2SW 2003010600128 20030106 00128 EU 2003 1 6 ALGA082690 1 20021227 A 6700 C623A2005102 BUSHING UROCOP EC120 EC120B 8680987 EU FLIGHT CONTROLS WORN H ALGA K NONE O OTHER IN INSP/MAINT 1 FS 01 514AL 698 1266 FLIGHT CONTROL TEFLON BUSHINGS WORN. MFG HAS NO REPLACMENT PROCEDURE. 1 G 7 2 3U NC R0001RD 2003010600131 20030106 00131 EU 2003 1 6 BAQA082136 1 20021217 A 6730 SC80331 SERVO AEROSP SA365 SA365N 8680669 EU FLIGHT CONTROLS LEAKING H BAQA K NONE O OTHER NR NOT REPORTED 1 FS 01 199SM 6885 6396 MAIN SERVO LEAKING FROM ACTUATING ROD. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H10EU 2003010600132 20030106 00132 EU 2003 1 6 BAQA082147 1 20021219 A 2140 JBS8803 VALVE UROCOP EC135 EC135T1 5620026 EU HEATER EJECTOR STUCK H BAQA K NONE O OTHER NR NOT REPORTED 1 FS 01 118WS 674 0089 HEATER EJECTOR VALVE STUCK CLOSED. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2003010600133 20030106 00133 2003 1 6 BAQA082148 4 20021219 A 3424 5090004910 INDICATOR BOLKMS 117 BK117B2 5626013 EU TURN AND BANK FROZEN H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 117KC 5416 7168 TURN AND BANK INDICATOR NEEDLE FROZEN. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U NC H13EU 2003010600134 20030106 00134 SO 2003 1 6 2002F01119 1 20020614 A 3230 LINKAGE EMB 120 EMB120ER 3260203 SO NLG OBSTRUCTED A HSYA O OTHER J WARNING INDICATION AP APPROACH 1 NM 05 223AS 120021 POS - FLT 8109 - ON APPROACH INTO POS, THE NOSE LANDING GEAR WOULD NOT FULLY EXTEND THROUGH NORMAL MEANS. ALTERNATE EXT ENSION PROCEDURES WERE USED. FOREIGN MATTER INTERFERED WITH THE CORRECT OPERATION OF THE SYSTEM. CLEANED AND LUBRICATE D THE NOSE LANDING GEAR LINKAGES, AND DOOR MECHANISMS, OPERATIONALLY TESTED OK AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2003010600135 20030106 00135 EU 2003 1 6 BAQA082684 1 20021226 A 2435 23081057 STARTER GEN UROCOP EC135 EC135T1 5620026 EU ENGINE FAILED H BAQA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 FS 01 136MH 1924 0161 STARTER GEN FAILED. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2003010600136 20030106 00136 NM 2003 1 6 2002F01122 1 20021113 A 3350 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 803MA 22434 DURING PREFLIGHT TRANSIT, FOUND LEFT AFT OUTSIDE EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATIO NAL CHECKED GOOD IAW MM 33-50-01. (M) 2 L 7 3 4F A3WE 2003010600137 20030106 00137 SO 2003 1 6 2003F00008 1 20020515 A 3260 922AA2YA6PZ722 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO MLG FAULTY A HSYA O OTHER J WARNING INDICATION DE DESCENT 1 NM 05 125AM 120017 JAC/CPR - FLT 8788 - LANDING GEAR WOULD NOT EXTEND THROUGH NORMAL MEANS. LIGHT GREEN 'A' PROXIMITY SWITCH FAILURE. TRO UBLESHOT THE SYSTEM, AND REPLACED FAULTY PROXIMITY SWITCH. OPERATIONALLY CHECKED SYSTEM. (M) 2 L 7 2 4T RT A31SO 2003010600138 20030106 00138 GL 2003 1 6 BAQA082689 2 20021227 A 7323 23065123 GOVERNOR AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20F 03013 GL NR 2 ENGINE MALFUNCTIONED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 5797X 1895 5182 NR 2 ENGINE SN 841010 WOULD NOT TRIM. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U 3 U H11EU E4CE 2003010600139 20030106 00139 CE 2003 1 6 2003F00009 1 20020707 A 2823 SHUTOFF VALVE BEECH 99 C99 1154006 CE LEFT FAILED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 175EE U175 OLF - FLT 5011 - LEFT ENGINE WOULD NOT START. LEFT FIREWALL SHUTOFF VALVE FAILURE. VALVE FAILED IN CLOSED POSITION. R EMOVED AND REPLACED LEFT FIREWALL FUEL SOV IAW B99 MM 28-21-0 PAGE 201. OPERATIONAL AND LEAK CHECK SATISFACTORY. (M) 1 L 7 2 3T A14CE 2003010600140 20030106 00140 EU 2003 1 6 BAQA082694 1 20021227 A 2510 3120 CUSHION UROCOP EC135 EC135T1 5620026 EU SEAT UNSERVICEABLE H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 136MH 623 0161 CUSHIONING BEYOND SERVICEABLE LIMITS. REPLACED WITH SERVICEABLE SEAT. 1 G 7 2 3U H88EU 2003010600141 20030106 00141 2003 1 6 BAQA082729 4 20021230 A 3160 L316M30C1003 CDU UROCOP EC135 EC135T1 5620026 EU COCKPIT FAILED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 118WS 87 0089 CENTRAL DISPLAY UNIT HAS DIGITAL SEGMENTS BURNED OUT, AND SELECT SWITCH KNOB BROKEN OFF. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2003010600142 20030106 00142 SO 2003 1 6 2003F00010 2 20020226 A 7414 1016301010 MAGNETO GULSTM 500 500A 0141104 SW CONT O470 IO470M 17026 SO LT ENGINE FAILED A HSYA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 NM 05 9382R 500A8998 BIL - FLT 1599 - DURING CRUISE AT 12,000 FEET, LEFT ENGINE BEGAN TO SURGE, THE ENGINE WAS SHUT DOWN. ATC WAS CONTACTED, AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO BIL AND MADE AN UNEVENTFUL LANDING. NR 1 ENGINE LEFT MAGNETO FAILURE. REPLACED WITH A SERVICEABLE MAGNETO, REPLACED 7 SPARK PLUGS, OPERATIONALLY TESTED, AND RETURNED TO SERVICE. ( M) 1 H 7 2 3O 3 O 6A1 3E1 2003010600146 20030106 00146 NE 2003 1 6 HEEA082798 2 20021216 A 7200 ENGINE AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1 60030 NE NACELLE MAKING METAL E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 975AE 2777 ENGINE HAS HIGH FERROUS COUNT IN OIL SAMPLE, OIL FLOW DECLINING STEADILY. 1 G 7 2 3U 3 U H11EU E19EU 2003010600147 20030106 00147 WP 2003 1 6 AALA20021359 1 20020924 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 411AA 49322 DFW - FOUND CEILING LIGHTS INOPERATIVE AT 8B, 9B/D, 11B, 22BD, 24B, AND 26BD. REPLACED BATTERY PACK FOR EMERGENCY LIGHT S AT ROWS 9-12 AND 22-26. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600150 20030106 00150 EU 2003 1 6 HEEA082801 1 20021216 A 8012 9550178290 START VALVE AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1D1 NE ENGINE FAILED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 975AE 2777 9728 ENGINE DOES NOT START. START VALVE SUSPECTED. 1 G 7 2 3U 3 U H11EU E19EU 2003010600151 20030106 00151 GL 2003 1 6 HEEA082802 2 20021216 A 7414 SEAL AEROSP AS355 AS355* EU ALLSN 250C 250C* GL MAGNETO LEAKING E HEEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 972AE 3234 22085 SEAL LEAKING OUT OF AFT OUTPUT SEAL ON ENGINE. SENT TO VENDOR. 1 G 7 2 3U 3 U H11EU E4CE 2003010600152 20030106 00152 EU 2003 1 6 HEEA082803 1 20021223 A 8012 9550178290 START VALVE AEROSP AS355 AS355* EU ALLSN 250C 250C* GL ENGINE LEAKING E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 975AE 12 2777 ENGINE START VALVE LEAKING FUEL. TO BE SENT TO VENDOR. 1 G 7 2 3U 3 U H11EU E4CE 2003010600170 20030106 00170 WP 2003 1 6 AALA20021387 1 20020930 A 3350 BPS73 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7518A 49895 AUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SEAT 14DEF INOPERATIVE. REPLACED EMERGENCY ESCAPE PA TH LIGHTING BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600171 20030106 00171 WP 2003 1 6 AALA20021388 1 20021001 A 3350 BPS73 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 589AA 53252 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SEATS 23, 24 AND 26 INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTING BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2003010600172 20030106 00172 WP 2003 1 6 AALA20021389 1 20020930 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 481AA 49656 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SEATS 20D AND AFT INOPERATIVE. RECONNECTED LOOSE CON NECTOR TO EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600173 20030106 00173 NM 2003 1 6 AALA20021401 1 20020930 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 653A 24611 MIA - FOUND FORWARD EMERGENCY LIGHT ON SEAT 6E INOPERATIVE. CLEANED CONNECTOR ON LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003010600174 20030106 00174 WP 2003 1 6 AALA20021414 1 20021001 A 3350 P2070003001 LIGHT DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70404 49315 DFW - DURING OVERNIGHT MAINTENANCE, L1 DOOR MOUNTED PORTABLE EMERGENCY EXIT LIGHT DAMAGED. REPLACED L1 DOOR MOUNTED POR TABLE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600175 20030106 00175 WP 2003 1 6 AALA20021416 1 20021001 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70404 49315 DFW - DURING OVERNIGHT MAINTENANCE, SEAT 7D EMERGENCY EXIT PATH LIGHT INOPERATIVE. REPLACED SEAT 7D EMERGENCY EXIT PATH LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600176 20030106 00176 WP 2003 1 6 AALA20021445 1 20021011 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 429AA 49341 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS BETWEEN ROWS 27-30 INOPERATIVE. REPLACED EMERGENCY EXIT BATTE RY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600177 20030106 00177 WP 2003 1 6 AALA20021446 1 20021012 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 470AA 49600 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ROW 18, 20, 21 AND 28 INOPERATIVE. REPLACED EMERGENCY EXIT BA TTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600178 20030106 00178 WP 2003 1 6 AALA20021447 1 20021013 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 224AA 49174 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD AISLE CEILING, FORWARD GALLEY CEILING, LEFT ENTRY CEILING AND COCKPIT CEILIN G EMERGENCY ESCAPE PATH LIGHTING DIM. REPLACED EMERGENCY EXIT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600179 20030106 00179 WP 2003 1 6 AALA20021448 1 20021013 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 224AA 49174 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT SEAT 8D INOPERATIVE. REPLACED EMERGENCY EXIT LIGH T ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600180 20030106 00180 WP 2003 1 6 AALA20021449 1 20021015 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 492AA 49730 LAX - DURING OVERNIGHT MAINTENANCE, COCKPIT AND FORWARD ENTRANCE AND GALLEY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED COCKPIT AND FORWARD ENTRANCE AND GALLEY EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600181 20030106 00181 WP 2003 1 6 AALA20021450 1 20021015 A 3350 AAP3274A CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 224AA 49174 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600182 20030106 00182 WP 2003 1 6 AALA20021451 1 20021015 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 237AA 49253 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-671 AND L2-615 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHTS B5-27 CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600183 20030106 00183 WP 2003 1 6 AALA20021452 1 20021015 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 450AA 49476 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-711 THROUGH I2-714 INOPERATIVE. REPLACED BATTERY PACK B5-1 02. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600184 20030106 00184 WP 2003 1 6 AALA20021453 1 20021015 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 450AA 49476 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-637 THROUGH L2-639 INOPERATIVE. REPLACED BATTERY PACK B5-2 8. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600185 20030106 00185 WP 2003 1 6 AALA20021454 1 20021015 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 593AA 53256 AUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS B5-27 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECK ED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2003010600186 20030106 00186 WP 2003 1 6 AALA20021455 1 20021014 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 410AA 49321 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 11D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600188 20030106 00188 WP 2003 1 6 AALA20021456 1 20021015 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 450AA 49476 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT L2-727 THROUGH L2-729 INOPERATIVE. REPLACED EMERGENCY EXIT BATTERY PACK B5-107. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600189 20030106 00189 WP 2003 1 6 AALA20021457 1 20021013 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 269AA 49292 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROWS 9 THROUGH 11 INOPERATIVE. REPLACED EMERGENCY EXIT BAT TERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600190 20030106 00190 WP 2003 1 6 AALA20021459 1 20021011 A 3350 AAP3274A CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 575AM 53152 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN TAIL INOPERATIVE. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600191 20030106 00191 WP 2003 1 6 AALA20021473 1 20021015 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 420AA 49332 TUL - FOUND EMERGENCY LIGHTS DIM DUE TO LOW BATTERY CHARGE. CHANGED BATTERY PACK DURING ROUTINE MAINTENANCE. (M) 2 L 7 2 4F A6WE 2003010600192 20030106 00192 SW 2003 1 6 HEEA082821 1 20021216 A 6710 214001347005 ACTUATOR BELL 214 214ST 1182106 SW ROTORY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INTERMITTENTLY WILL NOT HOLD. 2 G 7 2 4U H10SW 2003010600193 20030106 00193 WP 2003 1 6 AALA20021474 1 20021020 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 400AA 49311 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROW 7-12 INOPERATIVE. SECURED BATTERIES FOR EMERGENCY EXIT LIGHTS FOR ROW 7-12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600194 20030106 00194 WP 2003 1 6 AALA20021475 1 20021019 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 234AA 49181 DFW - DURING OVERNIGHT MAINTENANCE, LEFT CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIR LEFT CEILING EMERGENCY EXIT LIGHTS WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600195 20030106 00195 WP 2003 1 6 AALA20021476 1 20021019 A 3350 P4010049 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 593AA 53256 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS SYSTEM INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2003010600196 20030106 00196 WP 2003 1 6 AALA20021477 1 20021018 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77421 49333 DFW - DURING OVERNIGHT MAINTENANCE, LEFT AFT OVERWING EMERGENCY EXIT LIGHTS INTERMITTENT. REPAIR LEFT AFT OVERWING EMER GENCY EXIT LIGHTS CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600197 20030106 00197 WP 2003 1 6 AALA20021480 1 20021005 A 3350 P2070003001 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 591AA 53254 DFW - DURING OVERNIGHT MAINTENANCE, L1 DOOR MOUNTED PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED L1 DOOR MOUNTED PORTABLE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2003010600198 20030106 00198 SW 2003 1 6 HEEA082822 1 20021219 A 7712 7046M95G04 ECU BELL 214 214ST 1182106 SW ENG TORQUE FAILED E HEEA O OTHER J WARNING INDICATION DE DESCENT 1 SW 03 5748M 28102 DURING DECENT FOR LANDING, TORQUE STARTED SPLITTING, BUT WITH NO OTHER INDICATIONS OF ABNORMALITY. WHEN POWER WAS PULLE D BACK IN NR 2, TORQUE STAYED AT 50 PERCENT, NR 1 MGT INCREASED TO 780 DEGREES AND N2 TO 96 PERCENT. LANDING WAS ABORTE D AND NR 2 TORQUE CAME BACK UP TO NORMAL. 2 G 7 2 4U H10SW 2003010600199 20030106 00199 WP 2003 1 6 AALA20021481 1 20021008 A 3350 P4010049 CONTACTOR DOUG DC9 DC982 3022082 WP BATTERY PACK LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 476AA 49651 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. RESECURED TAIL CONE EMERGENCY EXIT LIG HT BATTERY PACK CONTACT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600200 20030106 00200 WP 2003 1 6 AALA20021482 1 20021016 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 554AA 53084 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS AT ROW 9-12 INOPERATIVE. SECURED BATTERY PACK CONNECT ION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600201 20030106 00201 WP 2003 1 6 AALA20021483 1 20021017 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 417AA 49328 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHTS AT SECTION 8-11 INOPERATIVE. SECURED BATTERY PACK CON NECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600202 20030106 00202 WP 2003 1 6 AALA20021489 1 20021020 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70425 49337 DFW - DURING OVERNIGHT MAINTENANCE, SEAT 22D EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT AS SEMBLY ON SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600203 20030106 00203 SW 2003 1 6 HEEA082823 1 20021219 A 6710 206062721105 ACTUATOR BELL 206 206L3 1182108 SW MAIN ROTOR INTERMITTENT E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 ACTUATOR INTERMITTENT OPERATION. 1 G 7 1 3U H2SW 2003010600204 20030106 00204 WP 2003 1 6 AALA20021490 1 20021020 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7535A 49989 DFW - DURING OVERNIGHT MAINTENANCE, SEAT 15D EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT SO CKET ON SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600205 20030106 00205 WP 2003 1 6 AALA20021513 1 20021023 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 554AA 53084 AUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 11AB, 9DEF, 9AB, AND 8AB INOPERATIVE. REPLACED EMERGE NCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600206 20030106 00206 WP 2003 1 6 AALA20021544 1 20021027 A 3350 TERMINAL DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 432AA 49350 DFW - DURING OVERNIGHT MAINTENANCE, AFT SERVICE DOOR AREA EMERGENCY LIGHTS INOPERATIVE. CLEANED TERMINALS TO B5-107 CON NECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600207 20030106 00207 SW 2003 1 6 HEEA082825 1 20021223 A 6730 C4264112 SLEEVE 206076031023 CLARK 1000 1000CLARK 2230102 SW SERVO VALVE LEAKING E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 RH2185 SLEEVE ASSY CAUSING EXCESSIVE INTERNAL LEAKAGE DURING FINAL TEST. 1 Q 7 1 3R 2A6 2003010600208 20030106 00208 WP 2003 1 6 AALA20021545 1 20021027 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP A/C BAY DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 442AA 49468 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIR STAIR FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED DEFECTIVE CONNECTOR FOR AFT FORWARD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600209 20030106 00209 WP 2003 1 6 AALA20021546 1 20021028 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 501AA 49738 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SECTION 22 THROUGH 26 DIM. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010600210 20030106 00210 SW 2003 1 6 HEEA082826 1 20021223 A 5302 STRUCTURE BELL 214 214ST 1182106 SW ELEVATOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 803 A200 28140 CORROSION UNDERSIDE OF RT ELEVATOR. REPLACED WITH SERVICEABLE ELEVATOR. 2 G 7 2 4U H10SW 2003010600211 20030106 00211 SW 2003 1 6 HEEA082828 1 20021223 A 6510 214040600103 HANGER ASSY BELL 214 214ST 1182106 SW T/R DRIVE CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 3897N 28106 CORROSION PITS ON MOUNTING RACE. REPLACED COUPLING 214-040-614-003, S/N A20-01819 DUE TO CORROSION. REPAIRED. 2 G 7 2 4U H10SW 2003010600213 20030106 00213 EU 2003 1 6 CA021127003 1 20021124 A 2932 PRESSURE SENSOR HYDRAELECT 9738114304 PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL HYD SYSTEM MALFUNCTIONED W H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 CA 0481T (CAN) PILOT RETRACTED THE LANDING GEAR, AND NOTICED THAT THE HYDRAULIC CAUTION LIGHT CAME ON SHORTLY AFTER THE GEAR HAD FINISHED MOVING. THE HYDRAULIC CIRCUIT BREAKER WAS PULLED, AND RESET ON THE DECENT FOR LANDING. THE CAUTION LIGHT REMAIN ED ON UNTIL THE AIR CRAFT'S POWER WAS TURNED OFF. WHEN THE POWER WAS TURNED ON AGAIN, THE LIGHT DID NOT RETURN. A VISUA L INSPECTION FOR LEAKS, FLUID LEVEL, AND N2 CHARGE WERE PERFORMED WITH NO DEFECTS BEING NOTED. THE SYSTEM PRESSURE SWITC H WAS REPLACED, AND A FUNCTIONAL TEST OF THE LANDING GEAR SYSTEM COMPLETED. NO PROBLEMS HAVE REOCCURRED SINCE THE SWITCH WAS REPLACED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2003010600214 20030106 00214 SW 2003 1 6 CA021129007 1 20021025 A 6320 206040948101 TUBE BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL MRGB OIL CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) AN OIL LEAK APPEARING TO BE ORIGINATED FROM BRAIDED STEEL TRANSMISSION RETURN LINE FROM THE FREEWHEELING UNIT. CL OSER INSPECTION REVEALED THAT ADJACENT ALUMINUM TUBE WAS CHAFED. VERIFIED PROPER CLAMPING OF THE AFFECTED PARTS, NO FA ULT WAS FOUND. APPARENTLY THE STEEL BRAIDED HOSE CHAFED AGAINST THE TUBE DURING MAXIMUM (100%) TORQUE OPERATION, ALTHOU GH THERE SEEMED TO BE SUFFICIENT CLEARANCE DURING FLAT PITCH OPERATION ON THE GROUND. TUBE REPLACED. A/C RETURNED TO S ERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003010600216 20030106 00216 SW 2003 1 6 CA021203011 1 20021202 A 6320 205040230003 SUN GEAR BELL 205 205A1 1181414 SW M/R GEARBOX SPALLED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA (CAN) TRANSMISSION REMOVED FOR METAL CONTAMINATION SUN GEAR FOUND DAMAGED ON INSPECTION. 1 G 7 1 4U H1SW 2003010600220 20030106 00220 NE 2003 1 6 CA021211008 2 20021209 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MALFUNCTIONED W E A ENGINE SHUTDOWN UNSCHED LANDING E J D VIBRATION/BUFFET WARNING INDICATION INFLIGHT SEPARATION CL CLIMB 1 CA (CAN) ON TAKE-OFF, CREW REPORTED AN HIGH VIBRATION AND A LOUD NOISE, FOLLOWED BY AN ITT INCREASE. ENGINE SHUT DOWN, AND RETURNED TO DEPARTURE AIRPORT. ENGINE REPLACED 2 L 7 2 4F 4 F RT A21EA E15NE 2003010600222 20030106 00222 EA 2003 1 6 CA021218003 1 20021216 A 5610 COPILOT WINDOW CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER AP APPROACH 1 CA (CAN) CO-PILOT SIDE WINDOW CRACKED IN FLIGHT. CAUSE UNKNOWN. UNEVENTFUL LANDING MADE AT CYMX. WINDSHIELD REMOVED AND NEW WINDSHIELD INSTALLED. NO MORE PROBLEM FOUND. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2003010600223 20030106 00223 CE 2003 1 6 CA021218004 1 20021212 A 3242 AE3663218G0150 LINE AEROQUIP CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE BRAKE SYSTEM RUPTURED W L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CA (CAN) AT A FLEX POINT NEAR THE UPPER FITTING OF THE LOWER BRAKE LINE RUPTERED ALLOWING THE BRAKE FLUID TO ESCAPE. UPON ARRIVAL AT CYXD ON FINAL FOR RUNWAY 16, THE GEAR WAS SELECTED DOWN. IMMEDIATELY TWO LIGHTS ILLUMINATED (POWER BRAKE LOW PRESS AND ANTISKID INOP) AND STAYED ON. TOWER WAS ADVISED, CREW CLIMBEDTO 4,000 FT WEST OF EDMONTON AND FOLLOWED THE CH ECKLIST. LANDING DISTANCE WAS RECALCULATED AND THE CITATION WAS LANDED WITHOUT FURTHER INCIDENT, USING REVERSE THRUST AN D EMERGENCY BRAKING. AIRCRAFT WA S SHUTDOWN ON THE RUNWAY AND TOWED IN. NO DAMAGE EVIDENT. 1 L 7 2 4F 4 F A22CE E1NE 2003010600224 20030106 00224 EA 2003 1 6 CA021221001 1 20021116 A 5610 NP1393219 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA 17424 (CAN) CAPTAIN'S WINDSHIELD CRACKED IN FLIGHT AT FL410. THE WINDSHIELD WAS REPLACED IAW AMM 56-11-01THE WINDSHILED INSTAL LED WAS A POST SERVICE BULLETIN WINDSHIELD. 2 L 7 2 4F 4 F RT A21EA E15NE 2003010600225 20030106 00225 EA 2003 1 6 CA021222002 1 20021218 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COCKPIT CRACKED W O OTHER O OTHER AP APPROACH 1 CA (CAN) LT WINDSHIELD CRACKED DURING APPROACH AT FL80, IAS 220 KNOTS. WINDSHIELD WAS REMOVED AND REPLACED PER AMM. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2003010600226 20030106 00226 EA 2003 1 6 CA021228003 1 20021223 A 5610 601R3303311 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER LD LANDING 1 CA (CAN) UPON LANDING IN BUDAPEST IT WAS NOTICED THE CAPT'S SIDE WINDOW WAS CRACKED.CAPT'S SIDE WINDOW REPLACED AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2003010600227 20030106 00227 NM 2003 1 6 AWXA200300009 1 20021218 A 5312 6516300511 WEB BOEING 737 7373G7 1384595 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 0 0 23776 MCN - MAJOR REPAIR - DURING C-16 CHECK HFEC INSPECTION INDICATED A 1/4" CRACK ON BS 178 BULKHEAD WEB, WL 234, RBL 9, AT BUTTON HEAD HILOC FASTENER HOLE. MAINTENANCE REMOVED FASTENER, AND CUTOUT CRACKED AREA OF BULKHEAD WEB AT BS 178, WL 234 , RBL 9; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND REPAIR DOUBLER; AND IN STALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, PG. 265-268, FIG. 209. 2 L 7 2 4F RT A16WE 2003010600228 20030106 00228 NM 2003 1 6 AWXA200300010 1 20021229 A 5311 146N1005 FRAME BOEING 757 7572G7 1384963 NM CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 0 0 24523 LCQ - MAJOR REPAIR - DURING C-10 CHECK THE CABIN FRAME WAS FOUND CHAFED AT BS 1280, STR 11 R/H, RBL 68. MAINTENANCE REMO VED CHAFED REPAIR DOUBLER AT BS 1280, STR 11 R/H, RBL 68; FABRICATED A REPAIR DOUBLER; AND INSTALLED REPAIR PART IAW B75 7-200 SRM 53-00-07, PG. 201-203, FIG. 201. 2 L 7 2 4F RT A2NM 2003010600230 20030106 00230 GL 2003 1 6 P5CA0300716 1 20021231 A 2810 NONE SEAL BOEING 747 747300 GL GE CF6 CF650E2 30018 NE #2 ENG PYLON LEAKING A P5CA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 WP 23 354MC 23394 530274 AFTER FUELING WAS COMPLETED, A STEADY DRIPPING OF FUEL ONTO #2 ENGINE FROM #2 PYLON WAS NOTICED. FOUND LEAK COMING FROM SEALANT ON FWD SPAR ON #2 ENGINE PYLON. INSTALLED FUEL LEAK SEAL IAW BMM 28-11-00 & PAC SERVICE FUELING MANUAL 4-05-02, ITEM 7. NO LEAKS NOTED. 2 L 7 4 4F 4 F RT A20WE E23EA 2003010700002 20030107 00002 NE 2003 1 7 BAQA081652 2 20021216 A 7323 430137201 LIMITER BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENG OVERSPEED MALFUNCTIONED H BAQA K NONE L NO TEST IN INSP/MAINT 1 FS 01 117LC 7027 ENGINE OVERSPEED TEST INTERMITTENTLY. ENGINE NR LE 45085 REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U 3 U H13EU E5NE 2003010700003 20030107 00003 SW 2003 1 7 HEEA082829 1 20021223 A 7120 BEARING BELL 214 214ST 1182106 SW MOUNT FITTING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 ENGINE MOUNT FITTING HAS WORN BEARINGS. REPLACED BEARING PN VTB03500 AND PN VTB03490 DUE TO WORN. REPAIRED. 2 G 7 2 4U H10SW 2003010700004 20030107 00004 SW 2003 1 7 HEEA082830 1 20021223 A 7120 BEARING BELL 214 214ST 1182106 SW MOUNT FITTING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 ENGINE MOUNT FITTING HAS WORN BEARINGS. REPLACED BEARING P/N VTB03500 AND P/N VTB03490 DUE TO WORN. REPAIRED. 2 G 7 2 4U H10SW 2003010700005 20030107 00005 SW 2003 1 7 HEEA082831 1 20021223 A 6720 PHI214ST103 COUNTERWEIGHT BELL 214 214ST 1182106 SW TAIL ROTOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 BEARINGS SPINNING. REPLACED BEARING 214010774001 DUE TO ROUGH; RETAINER MS27426-3133B (2 EACH) DUE TO CORROSION; CAP 214 -010-729-009 DUE TO CORROSION; CROSSHEAD 214010806105 DUE TO MECH DAMAGE; AND BEARING SET 214010856103 DUE TO CORROSION ON OUTER RACE. REPAIRED. 2 G 7 2 4U H10SW 2003010700006 20030107 00006 2003 1 7 HEEA082832 4 20021223 A 3442 7021450601 INDICATOR BELL 214 214ST 1182106 SW WX RADAR SYS WEAK E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 8045T 28101 WEATHER RADAR SYSTEM HAS WEAK AND SCRATCHY RECEPTION. 2 G 7 2 4U H10SW 2003010700007 20030107 00007 2003 1 7 HEEA082834 4 20021216 A 3416 066011560101 TRANSPONDER AEROSP AS355 AS355* EU ALTIMETER MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 855PH 3351 UNABLE TO ADJUST BEEP RANGE. COULD NOT DUPLICATE PROBLEM. FOUND A SEGMENT DIM AND PARTS OF IT MISSING. REPLACED DISPLA Y, REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H11EU 2003010700008 20030107 00008 2003 1 7 HEEA082835 4 20021216 A 3444 066305401 ALTIMETER AEROSP AS355 AS355* EU COCKPIT MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 40466 3004 NEEDLE STICKS AT DIFFERENT ALTITUDES. FOUND DATA PLATE MISSING AND BEZEL IS LOOSE. SCRAPPED UNIT. 1 G 7 2 3U H11EU 2003010700009 20030107 00009 EU 2003 1 7 HEEA082836 1 20021216 A 6220 117775P BALL JOINT AEROSP AS355 AS355* EU STARFLEX DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 972AE 3234 ROTOR OVERSPEED TO 500 RPM CAUSED BY ENGINE OVERSPEED. SCRAPPED. 1 G 7 2 3U H11EU 2003010700010 20030107 00010 EU 2003 1 7 HEEA082837 1 20021216 A 6220 117775P BALL JOINT AEROSP AS355 AS355* EU STARFLEX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 975AE 2777 STARFLEX HAS WORN BALL END LINING. REPLACED BALL ENDS. 1 G 7 2 3U H11EU 2003010700011 20030107 00011 EU 2003 1 7 HEEA082838 1 20021216 A 6240 350A08386100 WARNING HORN AEROSP AS355 AS355* EU ROTOR RPM INOPERATIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 856PH 3352 ROTOR RPM WARNING HORN DOES NOT WORK. LOOSE PARTS FROM INSIDE. REPLACED. 1 G 7 2 3U H11EU 2003010700012 20030107 00012 EU 2003 1 7 HEEA082839 1 20021216 A 6710 350A27195010 PITCH ROD AEROSP AS355 AS355* EU MAIN ROTOR HEAD CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 855PH 3351 MAIN ROTOR HEAD PITCH ROD IS CORRODED. PENDING VENDOR RETURN. 1 G 7 2 3U H11EU 2003010700014 20030107 00014 EU 2003 1 7 HEEA082840 1 20021216 A 6220 350A31177120 PIN AEROSP AS355 AS355* EU M/R BLADE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 972AE 3234 ROTOR OVERSPEED TO 500 RPM CAUSED BY ENGINE OVERSPEED. SCRAPPED MAIN ROTOR BLADE PIN. 1 G 7 2 3U H11EU 2003010700015 20030107 00015 NE 2003 1 7 P5CA0200700 2 20021005 A 7261 OIL SYSTEM BOEING 747 747200 1384847 NM PWA JT9 JT9D7J 52054 NE ENGINE MALFUNCTIONED A P5CA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 WP 23 524UP 21446 702000 PRECAUTIONARY ENGINE SHUTDOWN OCCURRED AT 2250 DUE TO NR 2 OIL QTY DECREASED TO 0.1 GAL. INDICATED, FOLLOWED BY SLOW DE CREASE IN OIL PRESSURE ALT PROCEDURES 6-15-9 & 6-15-11 C/W & ENGINE SECURED IAW 5-04-9. FL 390 FUEL APPROX 78.0. DISP ATCH NOTIFIED, PROCEEDED TO DESTINATION & DESCENDED TO FL 350. WINDMILLING OIL PRESSURE 18 PSI, N2 23%, N1 30% AT FL 35 0. PERFORMED STATIC LEAK CHECK AY ICN. NO LEAK FOUND PER MM 71-00-00. 2 L 7 4 4F 4 F RT A20WE E20EA 2003010700016 20030107 00016 NE 2003 1 7 P5CA0200701 2 20021006 A 7261 804275 GARLOCK SEAL BOEING 747 747200 1384847 NM PWA JT9 JT9D7J 52054 NE NR 2 ENGINE LEAKING A P5CA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 23 524UP 21446 702000 USED 2 GALLONS OF ENG OIL ON NR 2 ENG IN 3.7 HOURS OF FLT. QTY LOSS TO 0.1 GALLONS INDICATED. NR 2 ENG OIL SYSTEM STAT IC LEAK CHECKED IN HKG. TEST NR 6 CARRIED IAW AMM 71-00-00. FOUND GENERATOR DRIVE CARBON GARLOCK SEAL LEAKING. SEAL C HANGED IAW AMM 72-61-08, PG 401. SYSTEM STATIC LEAK CHECK OK, ENG GROUND IDLE RUN C/OUT SATISFACTORY. ALSO FOUND NR 1 & NR 2 BEARING CHIP DETECTOR HAD OIL LEAK. REMOVED & REPLACED CHIP DETECTOR ASSY. LEAK CHECK OK PER MM 72-61-01. 2 L 7 4 4F 4 F RT A20WE E20EA 2003010700017 20030107 00017 NE 2003 1 7 P5CA0200702 2 20021007 A 7230 A07527 CASE BOEING 747 747200 1384847 NM PWA JT9 JT9D7 52054 NE NR 2 ENGINE CRACKED A P5CA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 23 524UP 21446 702000 EN ROUTE NR 2 ENG OIL DROPPED FROM 6.7 GALLONS TO 3.9 GALLONS BY TOC. OIL QTY CONTINUED TO DROP AT A RATE OF 1.4 GALLON S IN 1ST HOUR OF CRUISE. ALL OTHER PARAMETERS NORMAL. AN EMERGENCY WAS DECLARED, DIVERTED TO NRT. FUEL DUMP WAS PERFO RMED TO LAND AT MAX LANDING WT & WAS UNEVENTFUL. ACCOMPLISHED NR 6 TEST STATIC LEAK CHECK IAW MM 71-00-00. NO OIL FOUN D IN 3.5 BLEED. CHECKED OIL FILTER MAIN CHIP DETECTOR ANGLE GEAR BEARING 3 & 4 TOWER SHAFT 1/2 BEARING DE-AERATOR. REM OVED CSD GENERATOR & INSTALLED DISPATCH EQUIPMENT. CONDUCTED NR 2 ENG HI POWER RUN EPR 1.32 FOR 15 MIN. VISUALLY INSPE CTED & FOUND NO OIL LEAKS. FURTHER INSPECTION REVEALED A CRACK IN THE INTERMEDIATE CASE. ENGINE REMOVED & REPLACED. 2 L 7 4 4F 4 F RT A20WE E20EA 2003011500144 20030115 00144 NM 2003 1 15 2002UALA01891 1 20021223 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE LIGHTNING STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 501UA 24622 LEFT HAND FUSELAGE SKIN LIGHTNING STRIKE LOCATION STATION 654 ON STRINGER 21L. MAJOR REPAIR ACCOMPLISHED. HFEC ACCOMPL ISHED AND REINSTALLED FASTENER. 2 L 7 2 4F 4 F RT A2NM E17NE 2003010700019 20030107 00019 NM 2003 1 7 2002UALA01904 1 20021230 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 356UA 24362 PUNCTURE HOLE BETWEEN WL194 AND WL207.5 AND BODY STATION 227.8 AND BODY STATION 243.7. AREA IS JUST FORWARD AND ABOVE RI GHT PITOT TUBE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010700020 20030107 00020 NM 2003 1 7 2003UALA00003 1 20021231 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 951UA 26696 AFT PIT FRAME AT STATION 727B STRINGER 22L, UPPER CAP DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLE R REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010700021 20030107 00021 NM 2003 1 7 2003UALA00004 1 20021224 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 606UA 21867 LOWER FUSELAGE SKIN HAS PILLOWING AT STRINGER 39R TWO EACH AREAS MKD STATION 588 TO 610. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A1NM E3NE 2003010700022 20030107 00022 NM 2003 1 7 2003UALA00005 1 20021224 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 606UA 21867 RIGHT HAND BELLY SKIN, 20 INCHES AFT OF SECTION 41 BUTT JOINT, 18 INCHES OUTBOARD OF E&E EXHAUST PORT CRACKED. SUPPLEMEN TAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A1NM E3NE 2003010700023 20030107 00023 EA 2003 1 7 2003F00033 1 20021004 A 3260 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF ADJUST A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 37342 7342 FLT 9342 - SAT-DEN, RETURNED TO FIELD DUE TO THE NLG WOULD NOT RETRACT WITH AN ASSOCIATED DISAGREE AND DOOR MESSAGES. M AINTENANCE ADJUSTED THE NLG PROX SWITCH AND THE SYSTEM OPERATED NORMALLY. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4F RT A21EA 2003010700024 20030107 00024 EA 2003 1 7 2003F00034 1 20021001 A 3244 299K631 TIRE CNDAIR CL600 CL6002B19 1900309 EA LT MLG SEPARATED A MASA K NONE O OTHER CL CLIMB 1 SW 07 37228 7228 FLT 6072 - COS-PHX - UPON TAKEOFF ROTATION, A LIGHT THUD WAS HEARD. ALL INDICATIONS IN THE COCKPIT WERE NORMAL. WHILE IN CRUISE, THE F/A NOTIFIED THE FLIGHT DECK WITH A REPORT FROM A PASSENGER. THE PASSENGER STATED THAT HE HAD THOUGHT WE HAD BLOWN A TIRE ON TAKEOFF. THE LANDING WAS UNEVENTFUL. THE TOWER WAS NOTIFIED AND NO DEBRIS WAS FOUND ON RUNWAY IN PHX. AFTER LANDING, THE TIRE WAS STILL INFLATED BUT THE ENTIRE TREAD SURFACE WAS MISSING. UNDERSIDE OF INBOARD FLAP WA S DAMAGED. MAINTENANCE REMOVED AND REPLACED NR 2 MWA. (M) 2 L 7 2 4F RT A21EA 2003010700025 20030107 00025 EA 2003 1 7 2003F00035 1 20020711 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG LOW A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 592ML 7410 BFL-PHX - ON CLIMB-OUT, GEAR WOULD NOT RETRACT DUE TO NOSE GEAR DISAGREE. AIRCRAFT RETURNED TO BFL. INSPECTED AIRCRAFT FOUND NO DAMAGE. AIRCRAFT WAS FERRIED TO FAT FOR MAINTENANCE. MAINTENANCE SERVICED THE STRUT. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2003010700026 20030107 00026 2003 1 7 2003F00036 4 20020902 A 3460 403424192 COMPUTER DOUG MD88 MD88 3023688 NM E/E BAY CONTAMINATED A A4JA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 35 11FQ 49759 IFE DIVERTED INTO BWI, LOST ALL INSTRUMENT, BOTH FMS, BOTH DFG C'S. IRU'S MAINLY WENT OUT. PROBLEM ON GROUND, MAINTENA NCE FOUND WATER FROM HEAVY RAINS IN E/E. DRIED MOISTURE ON DFGC'S IAW 34-33-00 AND 22-01-5. ALL SYSTEMS OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2003010700027 20030107 00027 NM 2003 1 7 2003F00037 1 20021101 A 5270 P401002 SWITCH DOUG MD88 MD88 3023688 NM R1 DOOR DIRTY A A4JA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 35 11FQ 49759 AT 6000 FEET, R-1 DOOR OPEN ANNUNCIATOR LIGHT ILLUMINATED. NO PRESSURIZATION LEAKS. NO AIR LEAKS. RETURNED TO PUJ FOR EVALUATION. MEL'D INDICATION PER MEL 52-7. PERFORMED OVERWEIGHT INSPECTION. CLEANED SWITCH, OPERATIONAL CHECK GOOD I AW MM 52-07-00. (M) 2 L 7 2 4F RT A6WE 2003010700028 20030107 00028 NM 2003 1 7 2003F00038 1 20021101 A 5270 833703 SWITCH DOUG MD88 MD88 3023688 NM R1 DOOR DIRTY A A4JA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 35 11FQ 49759 AT 6000 FEET, R-1 DOOR OPEN ANNUNCIATOR LIGHT ILLUMINATED. NO PRESSURIZATION LEAKS. NO AIR LEAKS. RETURNED TO PUJ FOR EVALUATION. MEL'D INDICATION PER MEL 52-7. AIRCRAFT CONTINUED FLIGHT TO CLE WHERE MAINTENANCE CLEANED SWITCH, OPERATI ONAL CHECK GOOD IAW MM 52-07-00 MEL 52-7 CLEARED. (M) 2 L 7 2 4F RT A6WE 2003010700029 20030107 00029 NM 2003 1 7 2003F00039 1 20021104 A 5610 5912290501 WINDSHIELD DOUG MD88 MD88 3023688 NM COCKPIT CRACKED A A4JA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 35 11FQ 49759 AFTER TAKEOFF AT 8000 FEET, THE CAPTAINS WINDSHIELD OUTER PANE CRACKED. AIR RETURN CLE FOR REPLACEMENT OF WINDSHIELD. REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW MM 56-10-02, ALSO REMOVED AND REPLACED CAPTAINS WINDSHIELD TEMPERATURE CONTROLLER DUE OT WINDSHIELD CHANGE IAW MM 30-41-01, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2003010700030 20030107 00030 NM 2003 1 7 2003F00040 1 20021128 A 3350 P4010021 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 11FQ 49759 FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT INOPERATIVE. PROBLEM WAS DETERMINED TO BE BATTERIES. REMOVED AND REPLAC ED BATTERIES IAW 25-60-00 MM. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2003010700031 20030107 00031 NM 2003 1 7 2003F00041 1 20020905 A 2120 7136821 SLEEVE DOUG MD88 MD88 3023688 NM A/C BAY TORN A A4JA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 35 12FQ 49766 TAIL COMPARTMENT, HOT LIGHT CAME ON JUST AFTER TAKEOFF. FOUND TORN SLEEVE ON DUCT. REMOVED AND REPLACED DUCT SLEEVE IA W MD80 MM CHAPTER 20-10-11. OPS AND LEAK CHECK GOOD IAW MD 80 MM CHAPTER 21-20-00. (M) 2 L 7 2 4F RT A6WE 2003010700032 20030107 00032 NE 2003 1 7 2003F00042 2 20020908 A 7320 SENSE LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LT ENGINE BLOCKED A A4JA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 35 12FQ 49766 UPON ENGAGING AUTO THROTTLE THE LEFT ENGINE WOULD NOT SPEED TO TAKEOFF POWER. FOUND TWO B-NUTS ON NR 1 ENGINE PT-2 LINE AND BOTH P2-2 LINES ON NR 1 AND NR 2 ENGINE BLOCKED. CLEARED BLOCKAGE AND TIGHTENED B-NUTS, OPS CHECK OK ON ENGINE RUN IAW MD80 MM 71-11-01. ALSO, TRIMMED NR 1 AND NR 2 ENGINE, AND OPS CHECK IAW MD80 MM 71-00-00. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2003010700033 20030107 00033 NM 2003 1 7 2003F00043 1 20020916 A 3610 VALVE DOUG MD88 MD88 3023688 NM BLEED AIR SYS MALFUNCTIONED A A4JA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 35 12FQ 49766 AFTER DEPARTURE FROM PIE-20 MINUTE INTO FLIGHT TO SFB, THE CREW GOT A TAILCONE OVERHEAT LIGHT AND DID A RETURN TO FIELD PIE. REMOVED AND INSTALLED AUGMENTATION VALVE IAW MD80 MM 36-10-01. OPS CHECK GOOD IAW MD80 MM 36-10-00. (M) 2 L 7 2 4F RT A6WE 2003010700034 20030107 00034 WP 2003 1 7 2003F00044 1 20020906 A 2720 5914387521 LIMITER DOUG DC9 DC982 3022082 WP RUDDER OUT OF ADJUST A A4JA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 35 418GE 49418 RUDDER TRAVEL 'UNRESTRICTED' LIGHT ON AFTER TAKEOFF. RETURNED TO PIE. ADJUSTED RUDDER THROW LIMITER AND LINKAGE IAW MD 80 MM 27-20-00. (M) 2 L 7 2 4F A6WE 2003010700035 20030107 00035 WP 2003 1 7 2003F00045 1 20021015 A 3350 9721055 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 920LG 47797 DURING THE B-4 CHECK, FOUND CABIN FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. THE PROBLEM WAS DETERMINED TO BE THE BATTE RIES. REMOVED AND REPLACED 5 EMERGENCY LIGHT BATTERIES IAW LEGENDS STC SA3951NM, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 2003010700036 20030107 00036 WP 2003 1 7 2003F00046 1 20021015 A 3350 41B004AD07G3 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 920LG 47797 DURING THE B-4 CHECK, ROW 8'S CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. THE PROBLEM WAS DETERMINED TO BE THE BATTERY PACK, MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IAW 33-50-00, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 2003010700037 20030107 00037 WP 2003 1 7 2003F00049 1 20021202 A 3350 7912 LENS DOUG DC9 DC931 3022065 WP CABIN BROKEN A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 35 933JK 48159 EMERGENCY FLOOR PATH LIGHTS CLEAR LENS ARE BROKEN. REPLACED THE EMERGENCY FLOOR CLEAR LENS. SYSTEM OPERATIONAL CHECK G OOD IAW 33-53-0. (M) 2 L 7 2 4F A6WE 2003010700038 20030107 00038 WP 2003 1 7 2003F00050 1 20021101 A 3350 60030431 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 935DS 48158 AFT OVERWING EMERGENCY DOOR LIGHTS INOPERATIVE. PROBLEM WAS DETERMINED TO BE THE BATTERY POWER SUPPLY. REMOVED AND REP LACED THE BATTERY POWER SUPPLY IAW DC9 MM 33-53-O, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 2003010700039 20030107 00039 EA 2003 1 7 2003F00051 1 20021030 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 17217 7217 FLT 3893 - DEN-ONT - RETURNED TO FIELD AND DECLARED AN EMERGENCY WHEN THE NLG WOULD NOT RETRACT AFTER TAKEOFF. THE CREW RECEIVED A 'GEAR DISAGREE' AND 'NLG DOOR' WARNING MESSAGES. MAINTENANCE IS CURRENTLY TROUBLESHOOTING DISCREPANCY. (M) 2 L 7 2 4F RT A21EA 2003010700040 20030107 00040 EU 2003 1 7 2003F00052 1 20020912 A 5230 7252300211 PLATE SAAB SF340 SF340A 7850100 EU CARGO DOOR CRACKED A UHLA K NONE O OTHER IN INSP/MAINT 1 NE 03 360SZ 38090 340A006 DURING RIGGING OF THE CARGO DOOR, IT WAS NOTED BY THE MECHANIC THAT THE CARGO DOOR HANDLE SLIDE PLATE WAS CRACKED AT THE TOP LOCKING PIN HOLE. SERVICE BULLETIN 340-52-022 HAD NOT BE COMPLIED WITH. AS A CORRECTIVE ACTION, THE CARGO DOOR WA S REMOVED AND SENT OUT FOR REPAIR. (M) 2 L 7 2 4T RT A52EU 2003010700041 20030107 00041 CE 2003 1 7 2003F00053 1 20020924 A 3230 ANL325 CURRENT LIMITER BEECH 200 200BEECH 1152920 CE LANDING GEAR FAILED A O2GA O OTHER O OTHER AP APPROACH 1 NE 03 4AT BB281 LANDING GEAR HAD TO BE EXTENDED USING EMERGENCY EXTENSION METHOD. AIRCRAFT LANDED SAFELY. PROBLEM WAS TRACED TO 325 AM P CURRENT LIMITER. PART WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 L 7 2 4T A24CE 2003010700042 20030107 00042 SO 2003 1 7 2003F00054 1 20020924 A 2910 11362 COUPLING GULSTM G1159 GIV 3980115 SO HYD SYSTEM LOOSE A UG8A O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 473CW 1194 THE FLIGHT CREW NOTED A COMBINED HYDRAULIC SYSTEM FAILURE MESSAGE. THE SYSTEM LOST PRESSURE DUE TO FLUID STARVATION AT THE SUPPLY LINE TO THE HYDRAULIC PUMP ON THE LEFT ENGINE. THE QUICK DISCONNECT COUPLING APPARENTLY HAD NOT BEEN LOCKED INTO PLACE. THE QUICK DISCONNECT WAS RELOCKED AND TESTED. NO DEFECTS NOTED. THE HYDRAULIC SYSTEM WAS INSPECTED AND TE STED USING G-IV MM RECOMMENDATIONS. NO DEFECTS WERE NOTED. THE SYSTEM WAS THOROUGHLY TESTED. NO DEFECTS NOTED. THE A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A12EA 2003010700043 20030107 00043 WP 2003 1 7 2003F00055 1 20020617 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 961R 46133 FOUND DURING DOUGLAS D-CHECK INSPECTION, AT STATION 1600 LBL 42 INCH FLOORBEAM UPPER FLANGE LOWER SURFACE HAS 1 INCH BY 2 INCH CORRODED BEYOND LIMITS. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER, FILLER IAW EO NR 02-0 39. TREATED, PRIMED AND INSTALLED REPAIR PER EO NR 02-039 WITH APPROVED 8110-3 DATED 06/06/02. (M) 2 L 7 4 4F RT 4A25 2003010700044 20030107 00044 NE 2003 1 7 2003F00056 2 20020326 A 7200 ENGINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 4 FLAMED OUT A KCSA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 23 709CK 20247 NR 4 ENGINE FLAMED OUT AT FL 38 ALL PARAMETERS NORMAL, RESTARTED ENGINE WITH NO FURTHER MALFUNCTIONS. INSPECTED NR 4 EN GINE IAW B747 MM CH 71-00, NO DEFECTS NOTED. RAN NR 4 ENGINE AND LEAK CHECK IAW B747 MM CH 71-00. NO LEAKS NOTED. (M) 2 L 7 4 4F 4 F A20WE E20EA 2003010700045 20030107 00045 NE 2003 1 7 2003F00057 2 20020326 A 7230 BLADE BOEING 747 747146 1384905 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 ON POST FLIGHT INSPECTION, FOUND NR 1, 2, 3 AND 4 ENGINES HAD EVIDENCE OF C-1 BLADE DAMAGE. REMOVED ALL DAMAGED C-1 (N1 ) BLADES AND INSTALLED MATCHED SET OF C-1 BLADES ON ALL 4 ENGINES IAW B747 MM 72-32-02/72-31-01 AND ACCOMPLISHED FOD DAM AGE INSPECTION AND FOUND NO DEFECTS IAW B747 MM 72-00-00. (M) 2 L 7 4 4F 4 F RT A20WE E20EA 2003010700046 20030107 00046 NM 2003 1 7 2003F00058 1 20020202 A 3350 900542 POWER SUPPLY BOEING 727 7272J4 1384006 NM CABIN FAULTY A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 288SC 20765 FLT 182 - IAD - RIGHT EXTERNAL AFT BODY FAIRING EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT SYSTEM AND FOUND FAULTY POWER SUPPLY. REMOVED FAULTY POWER SUPPLY AND REPLACED WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD PER B-727 AMM 33-0-0. (M) 2 L 7 3 4F RT A3WE 2003010700047 20030107 00047 WP 2003 1 7 AALA20021429 1 20021005 A 3350 0201720003S SOCKET DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 295AA 49307 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT SEAT 11D HAS BULB, INOPERATIVE. REPLACED EMERGENCY EXIT P ATH LIGHTING AT SEAT 11D SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2003010700048 20030107 00048 WP 2003 1 7 AALA20021505 1 20021022 A 3350 P4010049 BATTERY DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE CABIN DETACHED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 494AA 49732 DURING OVERNIGHT MAINTENANCE AFT GALLEY EMERGENCY EXIT LIGHTS IN THE CEILING INOPERATIVE. REATTACHED AFT GALLEY EMERGEN CY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2003010700049 20030107 00049 WP 2003 1 7 AALA20021506 1 20021022 A 3350 P400110049 BATTERY DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7514A 49891 DURING OVERNIGHT MAINTENANCE CEILING EMERGENCY EXIT LIGHTS AT ROWS 8, 10, AND 11, INOPERATIVE. RESEATED CEILING EMERGEN CY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2003010700050 20030107 00050 WP 2003 1 7 AALA20021508 1 20021022 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7514A 49891 DURING OVERNIGHT MAINTENANCE FIRST CLASS CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. TIGHTENED CEILING EMERGENCY EXIT LI GHTS CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2003010700051 20030107 00051 WP 2003 1 7 AALA20021535 1 20021027 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 490AA 49683 DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT SEATS 27, 28, AND 30, INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT B ATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2003010700052 20030107 00052 WP 2003 1 7 AALA20021536 1 20021025 A 3350 P2070003001 LIGHT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 405A 49316 DURING OVERNIGHT MAINTENANCE FORWARD ENTRY DOOR EMERGENCY EXIT PORTABLE LIGHT INOPERATIVE. REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT PORTABLE LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2003010700053 20030107 00053 WP 2003 1 7 AALA20021552 1 20021029 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 244AA 49256 EMERGENCY LIGHT OVERHEAD AFT OF VAULT DOOR INOPERATIVE. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2003010700054 20030107 00054 WP 2003 1 7 AALA20021564 1 20021030 A 3397 WIRE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 402A 49313 DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT ON SIDEWALL IN AFT STAIRWAY, INOPERATIVE. REPLACED WIRE AT EMERGENCY EXIT LIGHT ON SIDEWALL IN AFT STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2003010700055 20030107 00055 NM 2003 1 7 USAA020467 1 20021127 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 RUDDER SKIN DAMAGE. LEFT SIDE TRIM DAMAGE SRM IAW EA. 2 L 7 2 4F RT A16WE 2003010700056 20030107 00056 NM 2003 1 7 USAA020468 1 20021130 A 5330 SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 23231 SKIN, RIGHT SIDE STA 727E AT STR 23 RT, CRACKED. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010700057 20030107 00057 NM 2003 1 7 USAA020469 1 20021127 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 FLOORBEAM TOP FLANGE LOWER FORWARD SIDE CORRODED. 2 L 7 2 4F RT A16WE 2003010700058 20030107 00058 NM 2003 1 7 USAA020470 1 20021127 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 47519 23379 CORRODED SKIN, LEVEL 1 STA 986 BETWEEN STR S17L-S17R. FILLER AND EXTERNAL DOUBLER INSTALLED IAW SRM. 2 L 7 2 4F RT A16WE 2003010700059 20030107 00059 NM 2003 1 7 USAA020471 1 20021130 A 5330 SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 23231 SKIN, 2.8 INCH CRACK, RIGHT SIDE STA 727E AT STR 23 RIGHT. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010700060 20030107 00060 NM 2003 1 7 USAA020472 1 20021130 A 5510 FRAME BOEING 737 7373B7 1384580 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 47519 23379 HORIZONTAL STABILIZER, LOWER CHORD, 1.5 INCH CRACKED. TRIM OUT AFT SECTION LOWER CHORD AND SPLICE IN NEW SECTION. 2 L 7 2 4F RT A16WE 2003010700061 20030107 00061 NM 2003 1 7 USAA020473 1 20021201 A 5512 SKIN BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 HORIZONTAL STABILIZER SKIN, 1.125 INCH LONG CRACK. RIGHT HORIZONTAL STABILIZER UNDER SIDE SKIN, STA 125 AT SPAR CHORD. CUT OUT DAMAGE, INSTALLED EXT DOUBLER WITH BLIND FASTENERS IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010700062 20030107 00062 NM 2003 1 7 USAA020474 1 20021201 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 23317 SKIN, 2 INCH CRACK, 3 INCHES BELOW PREVIOUS PATCH AT WING EMERGENCY LIGHT. CUT OUT DAMAGE, INCORP ENTIRE AREA INTO ONE EXTERIOR DOUBLER/TRIPLER REPAIRED IAW EA. 2 L 7 2 4F RT A16WE 2003010700063 20030107 00063 NM 2003 1 7 USAA020475 1 20021210 A 5330 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU SKIN CRACKED, .500 INCH. FORWARD SERVICE DOOR, LOWER AFT CORNER STA 328 SILL PLATE. CUT OUT DAMAGE AND INSTALLED EXTER NAL DOUBLERS IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010700064 20030107 00064 EU 2003 1 7 USAABA02024 1 20021212 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 676UW 0375 FOUND EPSU AT R2 AND R3 DOORS FAILED. MAINTENANCE REPLACED BATTERIES IN BOTH EPSU. 2 L 7 2 4F RT A46NM 2003010700065 20030107 00065 2003 1 7 USAABB02206 4 20021210 A 3418 964CABM0D0001AB VANE BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE STALL WARNING FAULTY A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 649US 62234 23901 AT ROTATION, CAPTAINS STICK SHAKER ACTIVATED. CREW ALSO RECEIVED AN ALPHA SPEED INDICATION ON LOWER LEFT HAND CORNER OF CAPTAINS ADI AND BOTH FLIGHT DIRECTORS WERE INOPERATIVE. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT AIR DATA COMPUTER, THE LEFT INERTIAL REFERENCE UNIT, AND THE LEFT AOA VANE. 2 L 7 2 4F 4 F RT A1NM E13NE 2003010700066 20030107 00066 EU 2003 1 7 USAASA02104 1 20021203 A 2121 EVT3454H BLOWER AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE E/E BAY MALFUNCTIONED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 762US 6388 1358 EN ROUTE, AN ACRID ODOR WAS DETECTED IN THE COCKPIT, FOLLOWED BY AN ECAM MESSAGE OF VENT BLOWER INOPERATIVE. FLIGHT LAN DED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE AVIONICS VENT BLOWER FAN, FIN20HQ. SYSTEM BITE CHECKS, OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2003010700067 20030107 00067 2003 1 7 USAASA02105 4 20021207 A 2565 FLAP AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE L1 DOOR OUT OF POSITION A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 106US 1044 THE SLIDE FOR DOOR L1 WOULD NOT REMAIN ARMED. MAINTENANCE REPOSITIONED THE GIRT FLAP ON THE GIRT BAR TO ELIMINATE FRICT ION. THE SLIDE ARMING OF THE L1 DOOR NOW OPERATIONALLY CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2003010700068 20030107 00068 EU 2003 1 7 USAASA02107 1 20021211 A 2160 1320A000001 VALVE AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE A/C SYSTEM STUCK A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 715UW 6317 1051 EN ROUTE, WHILE CLIMBING THROUGH 10,000 FEET, FLIGHT ATTENDANT REPORTED AN ODOR OF SMOKE IN THE CABIN. THE FLIGHT RETUR NED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AFT TRIM VALVE. OPERATIONALLY CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2003010700069 20030107 00069 NE 2003 1 7 KCS2003F00000 2 20020326 A 7230 BLADE BOEING 747 747146 1384905 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 ON POST FLIGHT INSPECTION, FOUND NR 1, NR 2, NR 3, AND NR 4 ENGINES HAD EVIDENCE OF C-1 BLADE DAMAGE. REMOVED ALL DAMAG ED C-1 (N1) BLADES AND INSTALLED MATCHED SET OF C-1 BLADES ON ALL 4 ENGINES IAW MM AND ACCOMPLISHED FOD DAMAGE INSPECTIO N AND FOUND NO DEFECTS IAW MM. 2 L 7 4 4F 4 F RT A20WE E20EA 2003010700070 20030107 00070 EU 2003 1 7 USAASA02108 1 20021211 A 2160 132A000001 VALVE AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE A/C SYSTEM STUCK A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 715UW 6317 1051 EN ROUTE, A BURNING ODOR WAS PRESENT IN THE AIRCRAFT CABIN DURING THE FLIGHT. MAINTENANCE REPLACED THE AFT TRIM VALVE. OPERATIONALLY CHECKED, OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2003010700071 20030107 00071 EU 2003 1 7 USAASB02216 2 20021206 A 7320 9334M96P02 SENSOR BOEING 737 737401 1384701 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 ENGINE FAILED A USAA O OTHER O OTHER DE DESCENT 1 EA 19 404US 38785 12993 23886 725204 UPON NORMAL DESCENT, CREW REPORTED A THUMPING NOISE COMING FROM THE NR 1 ENGINE, SOUNDING LIKE COMPRESSOR STALLS. COMPR ESSOR STALLS BECAME PROGRESSIVELY WORSE AS RPM BECAME LOWER ON THE ENGINE. FLIGHT LANDED WITHOUT INCIDENT. THE ENGINE WAS NOT SHUT DOWN AND NO EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE COMPRESSOR INLET TEMPERATURE SENSOR. RAN ENGINE. NO COMPRESSOR STALLS AND NO THROTTLE SPLIT THROUGH OUT POWER RANGE WAS NOTED. NO LEAKS NOTED. AI RCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2003010700072 20030107 00072 SO 2003 1 7 SIMA200233801 1 20021121 A 5320 14522463001 BEAM EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 735TS 145386 DURING AN INSPECTION CORROSION WAS FOUND ON THE LEFT HAND BEAM AT FRAME 20. COMPLETELY REMOVED CORROSION BY CUT OUT. F ABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2003010700073 20030107 00073 NM 2003 1 7 AWXA200201194 1 20021212 A 3350 321430 BATTERY PACK AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 817AW 1373 DURING INSPECTION THE LEFT AFT DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT EMERGENCY POWER SUPPLY BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2003010700074 20030107 00074 NM 2003 1 7 AWXA200201198 1 20021213 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM GE CFM56 CFM56* 13802 NE FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 150AW 23218 EMERGENCY EQUIPMENT - DURING INSPECTION MAINTENANCE FOUND THE FORWARD GALLEY EMERGENCY FLASHLIGHT HAD A WEAK BATTERY. RE MOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010700075 20030107 00075 NM 2003 1 7 AWXA200201199 1 20021214 A 2560 P2070001214 BATTERY BOEING 737 7373G7 1384595 NM GE CFM56 CFM56* 13802 NE FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST NR NOT REPORTED 1 WP 28 150AW 23218 EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THAT THE AFT EMERGENCY FLASHLIGHT BATTERY WAS DEAD. REMOVED AND REPLACED TH E AFT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010700076 20030107 00076 EU 2003 1 7 AWXA200201200 1 20021215 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 38342 1798 098 DURING INSPECTION THE EMERGENCY LIGHT POWER SUPPLY CHECK FAILED AT THE LEFT MID CABIN. MAINTENANCE REMOVED AND REPLACE D THE LEFT MID CABIN EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2003010700077 20030107 00077 EU 2003 1 7 AWXA200201201 1 20021215 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 644AW 317 DURING INSPECTION THE LEFT FORWARD EMERGENCY LIGHT POWER PACK FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE LEFT F ORWARD EMERGENCY POWER SUPPLY UNIT BATTERY PACK, OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2003010700081 20030107 00081 WP 2003 1 7 AALA20021547 1 20021028 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 580AA 53157 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING AT SEAT 16D INOPERATIVE. REPLACED SOCKET ASSEMBLY FOR 16D EMERGENCY LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010700082 20030107 00082 WP 2003 1 7 AALA20021589 1 20021102 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 283AA 49296 DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010700083 20030107 00083 WP 2003 1 7 AALA20021591 1 20021102 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 434AA 49452 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS FROM ROWS 27-31 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2003010700084 20030107 00084 WP 2003 1 7 AALA20021592 1 20021104 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 429AA 49341 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY OVERHEAD LIGHTS AT SEATS 27-29 INOPERATIVE. REPLACED BATTERY PACK. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010700085 20030107 00085 WP 2003 1 7 AALA20021593 1 20021104 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 440AA 49459 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT OVER AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010700086 20030107 00086 WP 2003 1 7 AALA20021594 1 20021105 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 505AA 49799 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS IN CEILING OF ENTIRE AIRCRAFT INOPERATIVE. PERFORMED BATTERY TRICK LE CHARGE FOR 6 HOURS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010700087 20030107 00087 WP 2003 1 7 AALA20021602 1 20021107 A 3397 WIRE DOUG DC9 DC982 3022082 WP A/C BAY BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 405A 49316 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT IN TAIL SECTION FOR TAIL CONE RELEASE HANDLE STATION 1516 INOPERATIV E. REPAIRED BROKEN WIRE ON TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT AT STATION A482. SYSTEM GROUND CHECKED NORMAL OPE RATION. (M) 2 L 7 2 4F A6WE 2003010700088 20030107 00088 WP 2003 1 7 AALA20021605 1 20021107 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7506 49800 PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS AT SEATS 24-26 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010700089 20030107 00089 WP 2003 1 7 AALA20021606 1 20021107 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59523 49915 RDU - FOUND DURING OVERNIGHT MAINTENANCE, LEFT AND RIGHT EMERGENCY LIGHTS AT STATION 909 OVERWING EXITS INOPERATIVE. RE PLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010700090 20030107 00090 WP 2003 1 7 AALA20021654 1 20021119 A 3350 PIN DOUG DC9 DC982 3022082 WP CONNECTOR NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 455AA 49560 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 5E INOPERATIVE. RESEATED PIN IN EMERGENCY EXIT LIGHT C ONNECTOR AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010700091 20030107 00091 WP 2003 1 7 AALA20021655 1 20021119 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 489AA 49682 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHT AT ROW 7-11 INOPERATIVE. CLEANED EMERGENCY EXIT CEILIN G LIGHT BATTERY CONNECTOR AT SEAT 7-11. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010700092 20030107 00092 WP 2003 1 7 AALA20021656 1 20021115 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP FWD AIRSTAIRS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7537A 49991 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. SECURED EMERGENCY EXIT LIGHT QUI CK DISCONNECT AT FORWARD AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003010700093 20030107 00093 NM 2003 1 7 AALA20021676 1 20021122 A 3350 SOCKET BOEING 767 767323 1385205 NM EXTERIOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 379AA 25448 SFO - DURING OVERNIGHT MAINTENANCE, L2 DOOR OUTSIDE EMERGENCY LIGHT INOPERATIVE. RESEATED L2 DOOR EMERGENCY LIGHT SOCKE T. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003010700094 20030107 00094 NM 2003 1 7 AALA20021677 1 20021123 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT AT 40B INOPERATIVE. REPLACED SEAT HARNESS TO FLOOR HARNESS CONNECTO R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003010700095 20030107 00095 NM 2003 1 7 AALA20021685 1 20021123 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 690AN 29590 DFW - DURING OVERNIGHT MAINTENANCE, FLOOR MOUNT EMERGENCY PATH EXIT SIGN LIGHT AT MID GALLEY INOPERATIVE. REPLACED CONN ECTOR AT EMERGENCY PATH EXIT SIGN LIGHT AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003010700096 20030107 00096 NM 2003 1 7 AALA20021686 1 20021123 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 690AN 29590 DFW - DURING OVERNIGHT MAINTENANCE, FLOOR MOUNT EMERGENCY PATH EXIT SIGN AT SEAT 17D INOPERATIVE. REPLACED CONNECTOR AT EMERGENCY PATH EXIT SIGN AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003010700097 20030107 00097 NM 2003 1 7 AALA20021687 1 20021123 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 697AN 26977 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY LIGHT AT AFT RIGHT DOOR DAMAGED. REPLACED LIGHT ASSEMBLY AT FORWA RD AFT RIGHT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003010700098 20030107 00098 EU 2003 1 7 AALA20021688 1 20021124 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 50051 459 MIA - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY LIGHT WIRE AT SEAT 30G BROKEN. REPLACED SEAT MOUNTED EMERGEN CY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2003010700099 20030107 00099 NM 2003 1 7 AALA20021694 1 20021127 A 3350 PIN BOEING 767 767323 1385205 NM CONNECTOR UNSECURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 381AN 25450 ORD - EMERGENCY FLOOR LIGHT AT SEAT 25H WILL NOT ILLUMINATE. RESECURED PIN AT 25H SEAT CONNECTOR. SYSTEM GROUND CHECKE D NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003010700100 20030107 00100 NM 2003 1 7 AALA20021695 1 20021125 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 32B INOPERATIVE. REPAIRED FEMALE CONNECTO R AT SIDEWALL PANEL AT SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003010700101 20030107 00101 NM 2003 1 7 AALA20021697 1 20021126 A 2421 GEN3014 IDG BOEING 777 777223 1385213 NM RT ENGINE FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 787AL 30010 ORD - ELEC GENERATOR SYSTEM R MESSAGE APPEAR WITH ASSOCIATED LOSS OF RIGHT MAIN AC GENERATOR AFTER APPROXIMATELY 4.5 HOU RS OF FLIGHT. REMOVED AND REPLACED NR 2 ENGINE IDG PER MM. OPS AND LEAK CHECK NORMAL. (M) 2 L 7 2 4F RT T00001SE 2003010700102 20030107 00102 NM 2003 1 7 AALA20021698 1 20021126 A 2421 GEN5103 IDG BOEING 767 767323 1385205 NM NR 1 FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 353AA 24034 LEFT GENERATOR CAME OFF LINE DURING FLIGHT. GENERATOR CONTINUED OFF AND FIELD WERE ONLY INDICATIONS, ALL OTHER INDICATI ONS NORMAL. CYCLED LEFT ENGINE SWITCH AND RESET THE LEFT FIELD SWITCH AN AUX PANEL. RESET NORMAL. AS PRECAUTION, SWAP PED LT GCU WITH APU GCU. LEFT IDG SERVICED OK. RAN LEFT ENGINE AT IDLE POWER NO FAULTS. REMOVED AND REPLACED NR 1 IDG PER M/M. PERFORMED RUN-UP, OPS CHECK OK. LEAK CHECK GOOD. CLEARED MIC SHEET. REMOVED PLACARD 11-420DC-A. (M) 2 L 7 2 4F RT A1NM 2003010700103 20030107 00103 NM 2003 1 7 AALA20021710 1 20021128 A 3350 SOCKET BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 35B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003010700104 20030107 00104 NM 2003 1 7 AALA20021711 1 20021127 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 306AA 22312 LAX - DURING OVERNIGHT MAINTENANCE, GALLEY PARTITION EMERGENCY EXIT PATH LIGHTS BROKEN. REPAIRED BROKEN GALLEY PARTITIO N EMERGENCY EXIT PATH LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003010700105 20030107 00105 NM 2003 1 7 AALA20021712 1 20021128 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN OUT OF POSITION A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 189AA 32383 MIA - FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 33 INOPERATIVE. REPOSITION CONNECTOR UNDER SEAT. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 2 4F RT A2NM 2003010700106 20030107 00106 NM 2003 1 7 AALA20021713 1 20021128 A 2420 C9010 CIRCUIT BREAKER BOEING 757 757223 1384957 NM COCKPIT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7667A 25301 MIA - EMERGENCY ESCAPE SLIDE SQUIB TEST INOPERATIVE. FOUND LEFT GENERATOR CIRCUIT BREAKER WITH BROKEN 'A' PHASE TERMINA L. REPLACED CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 2 4F RT A2NM 2003010700107 20030107 00107 NM 2003 1 7 AALA20021714 1 20021126 A 2722 ACT6058 ACTUATOR BOEING 767 767323 1385205 NM RUDDER LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 368AA 25195 KEF - LEFT HYDRAULIC SYSTEM DECREASED TO .73 WITH THE RF SYMBOL DISPLAYED ON DESCENT QUANTITY INCREASED TO .76. REMOVED AND REPLACED CENTER RUDDER PCA LEAK COMING FROM THERE. AFTER REPLACEMENT OP AND LEAK CHECK OK. OK FOR SERVICE. (M) 2 L 7 2 4F RT A1NM 2003010700108 20030107 00108 NM 2003 1 7 AALA20021715 1 20021128 A 2933 TRANSMITTER BOEING 767 767223 1385123 NM HYD SYSTEM FAULTY A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 316AA 22318 SJC - FLT 268 - EN ROUTE SJC-BOS, IMMEDIATELY AFTER TAKEOFF RIGHT HYDRAULIC SYSTEM INDICATED ZERO. AIRCRAFT RETURNED TO SJC.; LANDED WITHOUT INCIDENT. REPLACED RIGHT HYDRAULIC TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003010700109 20030107 00109 NM 2003 1 7 AALA20021719 1 20021203 A 3350 PIN BOEING 757 757223 1384957 NM CONNECTOR BACKED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 687AA 25695 SFO - EMERGENCY LIGHT AT SEAT 4E INOPERATIVE. REPOSITIONED PUSHED PIN AT LIGHT ASSEMBLY CONNECTOR. SYSTEM GROUND CHECK ED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003010700110 20030107 00110 EU 2003 1 7 AALA20021720 1 20021231 A 3244 TIRE AIRBUS 300 A300B4605R 3930308 EU NR 1 BLOWN A AALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 21 7082A 643 MIA - FLT 989 - EN ROUTE MIA-SJO, ON TAKEOFF, NR 1 TIRE BLOWOUT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 TIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2003010700111 20030107 00111 NM 2003 1 7 AALA20021721 1 20021204 A 2120 4051399 DUCT BOEING 757 757223 1384957 NM CABIN BLOWN A AALA O OTHER O OTHER CL CLIMB 1 SW 21 688AA 25730 HNL - AFTER TAKEOFF AT KOA PASSENGERS AND F/A HEARD LOUD BANG MID MAIN CABIN CEILING PANEL IS BUCKLED NO PRESSURIZATION PROBLEM NOTED. FOUND BLOWN DUCT AT ROWS 17 A/C TO BE FERRIED TO LAX FOR CONT REPAIR LOOSE PANELS REMOVED AND PLACARD IN CGO COMPARTMENT. AIRCRAFT INSPECTED AND FOUND IN SAFE CONDITION FOR FERRY FLIGHT FROM HNL TO LAX PER SPOTTING MSG. FE RRIED TO LAX FOR DUCT REPLACEMENT. (M) 2 L 7 2 4F RT A2NM 2003010700112 20030107 00112 NM 2003 1 7 AALA20021722 1 20021201 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 332AA 22331 LAX - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE EMERGENCY EXIT LIGHT AT SEATS 1 THROUGH 9 INOPERATIVE. REPAIRED WIRING A T RIGHT SIDE EMERGENCY EXIT LIGHT CONNECTOR. (M) 2 L 7 2 4F RT A1NM 2003010700113 20030107 00113 NM 2003 1 7 ASAA0210293 1 20021109 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST DE DESCENT 1 NM 01 747AS 23124 ANC - DURING DESCENT INTO ANC, EMERGENCY FLOOR TRACK LIGHTING ILLUMINATED ON PALLETS 9-3 AND 7-12. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES AT PALLETS 9-3 AND 7-12, THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2003010700114 20030107 00114 NM 2003 1 7 ASAA0210295 1 20021110 A 5730 655076611 SKIN BOEING 737 737210C 1384459 NM LT WING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND LEFT WING LEADING EDGE AT WING STATION 453, GOUGED. REMOVED AND REPLACED DAMAGED SECTION OF LEFT WING LEADING EDGE PER SRM. (M) 2 L 7 2 4F A16WE 2003010700115 20030107 00115 NM 2003 1 7 ASAA0210296 1 20021110 A 5330 6545774 SKIN PANEL BOEING 737 737210C 1384459 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT FUSELAGE BODY STATION 780-788, LBL 70 DENTED. REPAIRED SKIN PANEL P ER SRM. (M) 2 L 7 2 4F A16WE 2003010700116 20030107 00116 NM 2003 1 7 ASAA0210297 1 20021110 A 7110 RIB BOEING 737 737210C 1384459 NM NR 2 COWLING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL RIB AT NACELLE STATION 140, GOUGED. REPAIRED ENGINE COWL RIB PER SRM. (M) 2 L 7 2 4F A16WE 2003010700117 20030107 00117 NM 2003 1 7 ASAA0210298 1 20021110 A 5730 SKIN BOEING 737 737210C 1384459 NM RT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND RIGHT WING LEADING EDGE AT WING STATION 325R-339R CRACKED 2 INCHES. REMOVED DAMAG ED SECTION AND REPAIRED LEADING EDGE PER SRM. (M) 2 L 7 2 4F A16WE 2003010700118 20030107 00118 NM 2003 1 7 ASAA0210299 1 20021110 A 5320 6552457 WEB BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND WEB AT BS 1016-1030, RBL 50, LBL 50 CORRODED. REMOVED AND REPAIRED WEB PER SRM. (M) 2 L 7 2 4F A16WE 2003010700119 20030107 00119 NM 2003 1 7 ASAA0210292 1 20021109 A 3397 07912 SPLICE BOEING 737 737298C 1384490 NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING EMERGENCY FLOOR TRACK LIGHTING IN THE FORWARD CABIN WILL NOT TEST. REPLACED BROKEN WIRE SPLICE AT ROW 9, T HEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2003010700120 20030107 00120 EA 2003 1 7 2003F00011 2 20020220 A 7200 ENGINE BEECH 99 99A 1154003 CE PWA PT6 PT6A27 52043 EA NR 2 SHUTDOWN A HSYA A UNSCHED LANDING Y ENGINE STOPPAGE DE DESCENT 1 NM 05 199CA U96 41172 GTF - FLT 5031 - UNCOMMANDED NR 2 ENGINE SHUTDOWN DURING DESCENT INTO GTF AFTER POWER LEVER WAS RETARDED. UPON ARRIVAL INTO GTF, THE ENGINE, IGNITION, AND AUTO IGNITION SYSTEMS WERE INSPECTED, AND OPERATIONALLY CHECKED. THERE WERE NO DEFE CTS NOTED THE AIRCRAFT WAS RETURNED TO SERVICE. THE FOLLOWING FLIGHT THE AIRCRAFT WAS PLACED IN THE SAME FLIGHT ATTITUD E, AND ALTITUDE IN AN ATTEMPT TO DUPLICATE THE PROBLEM. THE AIRCRAFT PERFORMED PROPERLY AND THERE HAVE BEEN NO OCCURREN CES SINCE THAT TIME. (M) 1 L 7 2 3T 4 T A14CE E4EA 2003010800005 20030108 00005 WP 2003 1 8 0204219976 1 20021226 A 5320 SHEAR TIE DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9340 47389 During "H" check found crack in shear clip below longeron L14 RH. Repaired per EA 99-193292. 2 L 7 2 4F A6WE 2003010800006 20030108 00006 WP 2003 1 8 0204229911 1 20021231 A 5330 SKIN DOUG DC9 DC931 3022065 WP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 961N 47405 During "H" check found crack in skin at upper aft corner of forward passenger door opening. Repaired per EA 99-193295. 2 L 7 2 4F A6WE 2003010800007 20030108 00007 EU 2003 1 8 2002F01118 1 20020806 A 3213 200920004 GLAND NUT STBROS SD3 SD360 8100606 EU LT MLG FAILED A HSYA O OTHER O OTHER LD LANDING 1 NM 05 617FB SH3617 HNL FLT 7670 - AFTER LANDING AT HNL, THE AIRCRAFT WAS LEANING TO THE RIGHT SIDE. THE LEFT MLG SHOCK STRUT GLAND NUT FAI LED ALLOWING THE SHOCK STRUT TO OVER EXTEND, AND BIND IN THAT POSITION. THE LEFT MLG FAIRING SUSTAINED DAMAGE DUE TO TH E OVER EXTENSION. SHOCK STRUT GLAND NUT FRACTURED, SHOCK STRUT DAMAGED, BRAKE LINES TORN, LT MLG FAIRING DAMAGED. A HI DDEN DAMAGE STRUCTURAL INSPECTION/REPAIR IS UNDERWAY, AND REPLACEMENT PARTS HAVE BEEN ORDERED AND ARE INTRANSIT TO THE A IRCRAFT AT THIS TIME. GLAND NUT INSPECTION WAS COMPLIED WITH 2801 CYCLES PREVIOUSLY ON 4-30-96, AT 26494 TAC. (M) 2 H 7 2 4T A41EU 2003010800016 20030108 00016 EA 2003 1 8 2002F01120 2 20020610 A 7200 ENGINE STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA WING MALFUNCTIONED A HSYA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NM 05 331SB SH3015 OGG - FLT 7672 - OIL PRESSURE FLUCTUATION, LOW OIL PRESSURE WHICH RESULTED IN AN EIFSD, AND A SUBSEQUENT AIR RETURN. IN TERNAL COMPONENT FAILURE. UNDETERMINED AT THIS TIME AWAITING TEARDOWN REPORTS FROM OVERHAUL FACILITY. REPLACED POWER S ECTION WITH SERVICEABLE UNIT, OPERATIONALLY TESTED, AND RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T A41EU E4EA 2003010800018 20030108 00018 WP 2003 1 8 2003F00047 1 20020802 A 3231 H50002125268 LATCH DOUG DC9 DC931 3022065 WP BYPASS DOOR WORN A A4JA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 35 932MJ 48156 AFTER T/O FROM PIE, THE LANDING GEAR LEVER WAS PLACED IN THE UP POSITION, CREW REPORTED NO RESPONSE TO GEAR HANDLE SELEC TION, GEAR REMAINED DOWN AND LOCKED AND MLG DOORS OPEN. RECYCLED THE GEAR HANDLE, NO HELP. RETURNED TO PIE. DURING TH E POST FLIGHT INSPECTION THE MAINTENANCE BYPASS DOOR WAS FOUND IN THE DOWN POSITION. WHEN THE MAINTENANCE BYPASS DOOR W AS CLOSED AND WITH HYDRAULIC PRESSURE APPLIED THE MAIN GEAR DOORS CLOSED. THE LEFT GEAR DOOR WAS REPLACED IAW MM 32-12- 1 AND A GEAR SWING WAS PERFORMED IAW MM 32-30-0 WITH ALL GEAR SYSTEMS OPERATING NORMAL. THE BYPASS DOOR LATCH WAS REPLA CED DUE TO AN UNSERVICEABLE SPRING AND WAS DETERMINED TO BE THE PRIMARY CAUSE OF THE AIR TURN BACK. (M) 2 L 7 2 4F A6WE 2003010800019 20030108 00019 WP 2003 1 8 ASAA0280544 1 20021112 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 ONT - DURING LINE CHECK, FOUND THAT 1ST CLASS EMERGENCY TRACK LIGHTING ILLUMINATED UPON POWERING AIRCRAFT. REPLACED ASS OCIATED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2003010800020 20030108 00020 WP 2003 1 8 ASAA0280556 1 20021110 A 5230 59101419 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K CHECK, MID CARGO BAY DOOR SEAL RETAINERS ARE CHAFED AND SKIN IS GOUGED. BLENDED AND REPAIRED PER BAC TLX AOC-OKC-02-00125H AND EA 5230-01183. (M) 2 L 7 2 4F RT A6WE 2003010800021 20030108 00021 WP 2003 1 8 ASAA0280558 1 20021111 A 5230 5910141105 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K-CHECK, AFT CARGO BAY DOOR SKIN AND SEAL RETAINER GOUGED AT AFT LOWER CORNER. BLENDED GOUGES PER BAC TLX AOC-OKC-02-00126H AND EA 5230-0-1182. (M) 2 L 7 2 4F RT A6WE 2003010800022 20030108 00022 WP 2003 1 8 ASAA0280562 1 20021111 A 5347 593054763 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K-CHECK, LEFT INBOARD SEAT TRACK GOUGED AT FS 693, LBL 22. REMOVED DAMAGED SECTION AND INSTALLED R EPAIR PART PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003010800023 20030108 00023 WP 2003 1 8 ASAA0280564 1 20021111 A 5330 5953050123 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K-CHECK, FUSELAGE SKIN DENTED AT FS 237 BETWEEN LONGERON 19L AND 20L. INSTALLED DOUBLER REPAIR PER SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2003010800024 20030108 00024 WP 2003 1 8 ASAA0280565 1 20021111 A 5321 99365813 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K-CHECK, FLOORBOARD HAS SOFT SPOT AT FS 1003 TO 1022 AT LBL 22 TO RBL 22. REPLACED FLOORBOARD PER SRM 53- 05. (M) 2 L 7 2 4F RT A6WE 2003010800025 20030108 00025 WP 2003 1 8 ASAA0280569 1 20021112 A 5321 993655211 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K-CHECK, FLOORBOARD HAS SOFT SPOT AT FS 218 TO 229, BL 0. REPLACED FLOORBOARD PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003010800026 20030108 00026 WP 2003 1 8 ASAA0280570 1 20021112 A 5321 99365841 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K-CHECK, FLOORBOARD IS PUNCTURED AT FS 256-275, LBL 36. REPLACED FLOORBOARD PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003010800027 20030108 00027 WP 2003 1 8 ASAA0280571 1 20021112 A 5321 99366543 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, FLOORBOARD IS PUNCTURED AT FS 1117-1174, LBL 22-LBL 44. REPLACED FLOORBOARD PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003010800028 20030108 00028 WP 2003 1 8 ASAA0280572 1 20021112 A 5321 99365855 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K-CHECK, FOUND FLOORBOARD IS DELAMINATED FORWARD OF FS 617, RBL 36. REPLACED FLOORBOARD PER SRM 53-05. ( M) 2 L 7 2 4F RT A6WE 2003020700070 20030207 00070 NE 2003 2 7 NACA20020065 2 20021231 A 8530 356993 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 6 CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 1377K 2517 2517 44596 NK510186 NR 3 ENGINE PRECAUTIONARY SHUT DOWN FOR A NR 6 CYLINDER DOUBLE SHORTED SECONDARY. REPLACED NR 3 ENGINE, NR 6 CYLINDE R. 2 L 7 4 4R 4 R A781 5E8 2003020700069 20030207 00069 NE 2003 2 7 NACA20020064 2 20021223 A 8530 404482 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 9 CRACKED A NACA E ENGINE SHUTDOWN K R FLUID LOSS PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 2907F 1001 1001 44636 55337 NR 1 ENGINE PRECAUTIONARY SHUT DOWN FOR EXCESSIVE OIL CONSUMPTION AND NR 16 CYLINDER SHORTED SECONDARY. REPLACED NR 1 E NGINE, NR 9 CYLINDER. 2 L 7 4 4R 4 R A781 5E8 2003010800038 20030108 00038 WP 2003 1 8 ASAA0280573 1 20021114 A 2170 COALESCER BAG DOUG DC9 DC982 3022082 WP A/C BAY DIRTY A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 01 953AS 49386 LAX - FOUND CABIN BEGAN TO FILL WITH FUMES/SMOKE WITH APU OPERATING ON DESCENT INTO LAX. SHUTDOWN APU, AND FUMES/SMOKE DISSIPATED. PERFORMED TASK CARD 28525011 DUCT CLEANING PROCEDURE AND REPLACED COALESCER BAGS. NO APU DEFECTS FOUND. OP CHECKED OK ON GROUND. (M) 2 L 7 2 4F A6WE 2003020700068 20030207 00068 NE 2003 2 7 NACA20020063 2 20021218 A 7421 URHB32E SPARK PLUG DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 6 CYLINDER CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 1377K 2471 2471 44596 NK510186 NR 3 ENGINE PRECATIONARY SHUT DOWN DUE TO DOUBLE SHORTED SECONDARY. REPLACED NR 3 ENGINE NR 6 CYLINDER FRONT AND REAR S PARK PLUGS. (CERAMICS BROKEN) 2 L 7 4 4R 4 R A781 5E8 2003010800039 20030108 00039 CE 2003 1 8 2002F01121 1 20020416 A 2612 302157 CONNECTOR BEECH 99 99A 1154003 CE NR 2 ENGINE CONTAMINATED A HSYA O OTHER N FALSE WARNING CR CRUISE 1 NM 05 199CA U96 NR 2 FIRE WARNING SYSTEM CAME ON IN FLIGHT, ALL ENGINE INDICATIONS WERE NORMAL. THE PILOT CONTINUED THE FLIGHT AND MONI TORED ENGINE, AND ENGINE INDICATORS. FLIGHT CONDITIONS WERE IN WET SNOW. MOISTURE CONTAMINATION OF ELECTRICAL CONNECTO R TO NR 2 ENGINE LOWER SENSOR CAUSED A FALSE FIRE WARNING. CLEANED AND DRIED CONNECTOR, REMOVED, AND REPLACED NR 2 LOWE R FIRE LOOP. (M) 1 L 7 2 3T A14CE 2003010800040 20030108 00040 CE 2003 1 8 2003F00012 1 20020124 A 3240 BRAKE ASSY CESSNA 208 208B 2073701 CE LT MLG CONTAMINATED A HSYA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 05 710FX 208B0431 BZN - FLT 8771 - LEFT BRAKE WAS SPONGY AND HAD MINIMAL EFFECTIVENESS. AIR ENTRAPMENT IN THE BRAKE SYSTEM. BLED BOTH LE FT AND RIGHT BRAKE SYSTEMS, OPERATIONALLY CHECKED OK. NO EVIDENCE OF LEAKAGE. (M) 1 H 7 1 3T A37CE 2003010800043 20030108 00043 CE 2003 1 8 2003F00025 1 20021105 A 3097 WIRE CESSNA 208 208B 2073701 CE COCKPIT FAULTY A HSYA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 05 885FE 208B0185 GFK - FLT 7563 - DURING CRUISE, THE PILOT NOTICED THE CIRCUIT BREAKER FOR THE PROP ANTI-ICE WAS OPEN. THE PITOT RESET T HE CIRCUIT BREAKER, AND A BURNED PLASTIC SMELL WAS EMANATING FROM THE INSTRUMENT PANEL NEAR THE PROP ANTI-ICE AMMETER. POWER WAS REMOVED FROM THE CIRCUIT WHILE THE COCKPIT WAS VENTILATED, AND THE FLIGHT CONTINUED UNEVENTFULLY. A SHORT CIR CUIT EVENT DUE TO A FAULTY WIRING CONNECTION THAT WAS MADE DURING A PREVIOUS MAINTENANCE VISIT. THE SYSTEM WAS TROUBLES HOT, FAULT WIRING CONNECTION WAS CORRECTED, WIRE HA32 LEADING FROM THE PROP DE-ICE AMMETER, AND CONNECTINOR P161 WAS REP LACED, THE SYSTEM WAS OPS CHECKED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 H 7 1 3T A37CE 2003020700067 20030207 00067 NE 2003 2 7 NACA20020062 2 20021218 A 8530 356994 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 5 CRACKED A NACA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 AL 03 2907F 1637 1637 44636 55337 PRECAUTIONARY SHUT DOWN ON NR 1 ENGINE DUE TO EXCESSIVE OIL CONSUMPTION. REPLACED NR 1 ENGINE NR 5 CYLINDER. 2 L 7 4 4R 4 R A781 5E8 2003010800044 20030108 00044 NE 2003 1 8 2003F00026 2 20021023 A 7320 MS905804 O-RING BEECH 99 C99 1154006 CE PWA PT6 PT6A36 52043 NE LT ENGINE DAMAGED A HSYA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 05 175EE U175 BIL - DURING DESCENT INTO BIL, THE PILOT SELECTED THE LEFT BLEED TO ENVIRO, AND SMELLED FUEL VAPOR IN THE COCKPIT. FUEL LEAK AT THE LEFT ENGINE FLOW DIVIDER, AND DUMP VALVE. LEAK CHECKED ENGINE, FOUND FUEL LEAK AT THE FUEL PRESSURE SIDE O F THE DUMP VALVE, DISASSEMBLED, AND REPLACED THE O-RINGS, AND BACK UP RINGS. THE ENGINE WAS RUN AND LEAK CHECKED WITH N O LEAKS NOTED. (M) 1 L 7 2 3T 4 T A14CE E4EA 2003020700066 20030207 00066 NE 2003 2 7 NACA20020061 2 20021123 A 8530 356994 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 1 CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 1377K 2373 2373 44596 510186 NR 3 ENGINE RUNNING ROUGH. PRECAUTIONARY SHUT DOWN. REPLACED NR 1 CYLINDER. 2 L 7 4 4R 4 R A781 5E8 2003020700065 20030207 00065 NE 2003 2 7 NACA20020060 2 20021120 A 8520 76270 CAM DOUG DC6 DC6B 3021712 WP PWA R2800 R2800CB3 52026 NE NR 2 ENGINE DAMAGED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 7919C 1449 1449 43554 P34324 NR 2 ENGINE FEATHER DUE TO NR 17 CYLINDER DOUBLE SHORTED SECONDARY. DURING INSPECTION FOUND FRONT CAM DAMAGE. 2 L 7 4 4R 4 R 6A4 5E8 2003010800045 20030108 00045 EA 2003 1 8 2003F00032 1 20021017 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A MASA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 27172 7172 FLT 6497 - PHX-EUG, DECLARED AN EMERGENCY DUE TO FLAP FAIL AT 8 DEGREES AND RETURNED TO PHX. MAINTENANCE COMPLIED WITH PART A/B OF MTS-27-50-001 AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2003020700063 20030207 00063 NE 2003 2 7 NACA20020058 2 20021106 A 8530 9265 GLAND NUT PWA DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 15 CYLINDER LOOSE A NACA E D ENGINE SHUTDOWN RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 AL 03 2907F 96 96 A593WCHO 533265 33553 NR 4 ENGINE PRECAUTIONARY SHUT DOWN DUE TO THE LOWER INBOARD SIDE OF THE ENGINE PRODUCING A STEADY STREAM OF BLUE SMOK E. TIGHTENED THE NR 4 ENGINE, NR 15 CYLINDER EXHAUST PUSH ROD TUBE GLAND NUT, LEAK CHECK GOOD. 2 L 7 4 4R 4 R A781 5E8 2003020700062 20030207 00062 NE 2003 2 7 NACA20020057 2 20021105 A 8530 356994 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 7 CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 99330 1338 1338 43576 P31669 NR 1 ENGINE PRECAUTIONARY SHUT DOWN FOR RUNNING ROUGH. FOUND NR 1 ENGINE NR 7 CYLINDER WITH A CRACKED HEAD. REPLACED CY LINDER, OP CHECK GOOD. 2 L 7 4 4R 4 R 6A3 5E8 2003010800046 20030108 00046 EA 2003 1 8 COMA0360005 1 20021226 A 5610 SEALANT CNDAIR CL600 CL6002B19 1900309 EA A COMA B EMER. DESCENT D INFLIGHT SEPARATION CR CRUISE 1 SO 01 916CA 7014 FLIGHT 5390 STREAK ON PILOTS WINDSHIELDINSPECTED WINDSHIELD FOUND SEALANT MISSING - REPLACED SEALANT. 2 L 7 2 4F RT A21EA 2003020700061 20030207 00061 NE 2003 2 7 NACA20020056 2 20021104 A 8520 CASE DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 4 ENGINE MAKING METAL A NACA E ENGINE SHUTDOWN K R FLUID LOSS PARTIAL RPM/PWR LOSS DE DESCENT 1 AL 03 43872 1720 1720 533294 36434 NR 4 ENGINE LOSS OF BMEP AND LOSS OF OIL QUANTITY. REPLACED NR 4 ENGINE DUE TO HIGH METAL CONTENT FOUND IN FRONT ACCESS ORY SECTION. 2 L 7 4 4R 4 R A781 5E8 2003010800050 20030108 00050 WP 2003 1 8 2003F00048 1 20021117 A 2842 050022002 PROBE DOUG DC9 DC931 3022065 WP LT FUEL TANK FAULTY A A4JA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 35 932MJ 48156 EN ROUTE TO EWR-RDU, LEFT FUEL GAUGE WAS NOTICED TO BE DECREASING MORE RAPIDLY THAN THE RIGHT FUEL GAUGE. AT ONE POINT, FUEL QUANTITY GAUGES SHOWED IMBALANCE OF APPROXIMATELY 1500 LBS. FLIGHT CREW ELECTED TO DECLARE AN EMERGENCY, FLIGHT D IVERTED TO ORF. AIRCRAFT WAS DEFUELED AND REFUELED WITH KNOWN A QUANTITY. THE LEFT INDICATION SYSTEM WAS DEFERRED PER MEL 28-7. FUEL SYSTEM WAS FOUND TO HAVE MICROBIAL CONTAMINATION AND FAILED COMPENSATOR PROBE. FUEL SYSTEM WAS CLEANED IAW MM 28-10-01 AND COMPENSATOR PROBE WAS REPLACED IAW MM 28-40-05. (M) 2 L 7 2 4F A6WE 2003010800051 20030108 00051 NM 2003 1 8 2003F00059 1 20020304 A 2560 STRIP BOEING 727 727200 138407E NM CABIN LOOSE A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 919PG 22604 FLT 322 - MSP - ESCAPE PATH ILLUMINATION STRIP HAS CAME LOOSE FROM FORWARD GALLEY FLOOR. REINSTALLED SAFETY GLOW ESCAPE PATH STRIP IN FORWARD GALLEY PER CHAPTER 25. (M) 2 L 7 3 4F RT A3WE 2003010800052 20030108 00052 NM 2003 1 8 2003F00060 1 20020304 A 2560 STRIP BOEING 727 727200 138407E NM CABIN LOOSE A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 919PG 22604 FLT 322 - MSP - AFT CABIN ESCAPE PATH ILLUMINATION STRIP IS NOT ATTACHED TO FLOOR BY AFT GALLEY LEFT SIDE. REINSTALLED SAFETY GLOW ESCAPE PATH STRIP AT LEFT AFT LAVATORY PER CHAPTER 25. (M) 2 L 7 3 4F RT A3WE 2003010800053 20030108 00053 NM 2003 1 8 2003F00061 1 20020410 A 2612 CONNECTOR BOEING 747 747230B 1384889 NM NR 3 ENGINE LOOSE A Q2SA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 23 744SA 22363 DURING TAKEOFF, AT 60 KNOTS, FIRE DETECTION LIGHT ON FORWARD INSTRUMENT PANEL ILLUMINATED AND NR 3 ENGINE NACELLE TEMPER ATURE INDICATOR 'B' LOOP WAS AT 8.5 ON INDICATOR. CHECKED FOR AIR LEAK IAW AMM 36-11-00, NO DISCREPANCIES NOTED. CHECK ED FIRE LOOP NR 3 ENGINE IAW AMM 71-10-00 AND FOUND LOOSE CONNECTOR AND CLAMP. TRANSFERRED TO DEFERRED ITEM NR 5849. R AN ENGINE IAW AMM 71-00-00 AND CHECKED GOOD. (M) 2 L 7 4 4F A20WE 2003010800054 20030108 00054 NM 2003 1 8 AALA20020905 1 20020616 A 2150 MAC5421 ACM BOEING 757 757223 1384957 NM A/C BAY FAILED A AALA O OTHER O OTHER CL CLIMB 1 SW 21 690AA 25696 AFTER TAKEOFF, A/C COCKPIT TEMP UNCONTROLLABLE ON COLD SIDE, AND EXTREMELY NOISY TO THE POINT CREW COULD NOT HEAR EACH O THER. REMOVED AND REPLACED LEFT PACK ACM. FOUND IT FROZEN WOULD NOT SPIN. REPLACED LEFT ACM PER MM REQUIRES OPS AND L EAK CHECK EMP 486492. LEAK CHECK AND OPS CHECK OK. (M) 2 L 7 2 4F RT A2NM 2003010800055 20030108 00055 NM 2003 1 8 AALA20021431 1 20021008 A 2433 INV7002 TRU BOEING 767 767323 1385205 NM ELECTRICAL SYS FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 363AA 24044 PIK - STANDBY INVERTER MESSAGE ON LOWER EICAS. ELECTRICAL FUMES OBSERVED THROUGHOUT CABIN AND FLIGHT DECK. PUNGENT ELE CTRICAL BURNING ODOR. FOUND STANDBY INVERTER OVERHEATED, REPLACED TRU AND ALL OPS AND INDICATIONS NORMAL RAISED MRR. ( M) 2 L 7 2 4F RT A1NM 2003010800056 20030108 00056 NM 2003 1 8 ASAA0210300 1 20021110 A 7110 COWLING BOEING 737 737210C 1384459 NM NR 1 ENGINE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL AT NACELLE STATION 142, CHAFED. REPAIRED NR 1 ENGINE COWL PER SR M. (M) 2 L 7 2 4F A16WE 2003010800057 20030108 00057 NM 2003 1 8 ASAA0210301 1 20021111 A 3350 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 11, 12 AND 15 INOPERATIVE. REMOVED AND REPLACED REM OTE ASSEMBLY BATTERIES, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2003010800058 20030108 00058 NM 2003 1 8 ASAA0210302 1 20021111 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT SEAT PALLETS 2-8 AND 4-4 FAILED RECON INSPECTION. REMOVE D AND REPLACED REMOTE ASSEMBLY BATTERIES TWO, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2003020700060 20030207 00060 NE 2003 2 7 NACA20020055 2 20021016 A 8550 232 GASKET PWA DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE RELIEF VALVE LOOSE A NACA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 2907F 1 1 533265 P31893 NR 3 ENGINE SHUT DOWN ON GROUND AFTER LANDING DUE TO OIL LOSS. RESEALED AND RETORQUED OIL PRESSURE RELIEF VALVE, LEAK CHECK GOOD. 2 L 7 4 4R 4 R A781 5E8 2003020700059 20030207 00059 NE 2003 2 7 NACA20020053 2 20021029 A 8530 356993 CYLINDER DOUG DC6 DC6B 3021712 WP PWA R2800 R2800CB3 52026 NE NR 18 BURNED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 7919C 1418 1418 43554 P34324 NR 2 ENGINE SHUT PRECAUTIONARY SHUT DOWN FOR RUNNING ROUGH. NR 18 CYLINDER BURNED THROUGH THE SIDE. REPLACED NR 18 CYL INDER, OP CHECK GOOD. 2 L 7 4 4R 4 R 6A4 5E8 2003020700058 20030207 00058 NE 2003 2 7 NACA20020052 2 20020929 A 8520 76270 CAM DOUG DC6 C118A 3021710 WP PWA R2800 R2800CB3 52026 NE NR 3 ENGINE FAILED A NACA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 AL 03 1377K 2131 2131 44596 P33192 NR 3 ENGINE SHUT DOWN DUE TO OIL LOSS. REPLACED NR 3 ENGINE DUE TO FRONT CAM FAILURE. 2 L 7 4 4R 4 R 6A3 5E8 2003010800061 20030108 00061 NE 2003 1 8 COMA0360011 2 20021231 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE A COMA E A ENGINE SHUTDOWN UNSCHED LANDING E M Y VIBRATION/BUFFET OVER TEMP ENGINE STOPPAGE CL CLIMB 1 SO 01 712CA 7244 807109 FLIGHT 5848 LEFT ENG FAN VIB WARNING, ITT IN RED. IFSDREPLACED THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2003010800062 20030108 00062 EA 2003 1 8 COMA0360012 1 20021231 A 3250 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA A COMA H DEACTIVATE SYST/CIRCUITS S AFFECT SYSTEMS CL CLIMB 1 SO 01 785CA 7326 FLIGHT 5295 NWS CAUTION MESSAGE AFTER T/O.COULD NOT DUPLICATE. SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 2003030300039 20030303 00039 NE 2003 3 3 NACA20020051 2 20020928 A 8530 33640 PUSHROD DOUG DC6 C118A 3021710 WP PWA R2800 R2800* 52026 NE NR 4 ENGINE BENT A NACA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 AL 03 1377K 1075 44596 P34403 NR 4 ENGINE SHUT DOWN AT 1802Z FOR A NR 12 CYLINDER DOUBLE SHORTED SECONDARY AND WON'T LEAN. FOUND EXHAUST AND INTAKE P USH RODS BENT. REPLACED AND SET VALVES. INSPECTED CYLINDER FOR DAMAGE, CHECKED GOOD. OP CHECK GOOD ON RUNUP. 2 L 7 4 4R 4 R 6A3 5E8 2003020700057 20030207 00057 NE 2003 2 7 NACA20020050 2 20021023 A 8530 CYLINDER HEAD DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 4 CYLINDER CRACKED A NACA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 AL 03 779TA 513 513 45529 P35317 NR 2 ENGINE PRECAUTIONARY SHUT DOWN, RUNNING ROUGH. REPLACED NR 4 CYLINDER FOR A CRACKED HEAD, OP CHECK GOOD. 2 L 7 4 4R 4 R A781 5E8 2003020700054 20030207 00054 NE 2003 2 7 NACA20020048 2 20020901 A 7421 URHB32E SPARK PLUG PWA DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 13 CYLINDER CRACKED A NACA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 2907F 262 3458514 533265 CP450668 NR 4 ENGINE, NR 2 CYLINDER SHOWS A DOUBLE SHORTED SECONDARY, ENGINE BACKFIRING WHEN LEANED. REPLACED NR 13 CYLINDER FR ONT AND REAR SPARK PLUGS ONCE ENGINE ANYLIZER TIMING CORRECTED. 2 L 7 4 4R 4 R A781 5E8 2003020700049 20030207 00049 NE 2003 2 7 NACA20020047 2 20020913 A 8530 356994 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 4 ENGINE CRACKED A NACA E D ENGINE SHUTDOWN RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 AL 03 2907F 2523 2523 533265 CP450668 LOW BMEP "95" ON NR 4 ENGINE. REPLACED NR 1 CYLINDER ON NR 4 ENGINE. 2 L 7 4 4R 4 R A781 5E8 2003020700048 20030207 00048 NE 2003 2 7 NACA20020046 2 20020912 A 7414 10884501 DISTRIBUTOR DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 3 ENG MAGNETO DAMAGED A NACA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 2907F 1154 447 533265 P34459 NR 3 ENGINE, SEVERAL OPEN PRIMARIES ON L1 CIRCUIT. REPLACED LT DISTRIBUTOR. 2 L 7 4 4R 4 R A781 5E8 2003010800063 20030108 00063 NM 2003 1 8 NACA20020036 1 20020314 A 5310 ATTACH FITTING BOEING 727 72723 1384004 NM A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 930FT 19387 DURING "C" CHECK INSPECTION FOUND 2 EA STARTED DRILL HOLES IN THE ATTACH FITTING AT B.S. 1183, WL 278, AND RBL 27. CORRE CTED BY INSTALLING 2 PIECE FREEZE PLUG, AND DOUBLER PER BOEING PROVIDED REPAIR PLAN NAC-ANC-02-00003H AND REIVISION NAC- ANC-02-00004H. 2 L 7 3 4F A3WE 2003010900002 20030109 00002 EU 2003 1 9 HEEA082841 1 20021216 A 6220 350A31182703 FREQ ADAPTER AEROSP AS355 AS355* EU MAIN ROTOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 972AE 1165 3234 ROTOR OVERSPEED TO 500 RPM CAUSED BY ENGINE OVERSPEED. SCRAPPED. 1 G 7 2 3U H11EU 2003010900003 20030109 00003 EU 2003 1 9 HEEA082842 1 20021216 A 6220 350A31185002 SLEEVE AEROSP AS355 AS355* EU M/R HEAD DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 972AE 1165 3234 ROTOR OVERSPEED TO 500 RPM CAUSED BY ENGINE OVERSPEED. 1 G 7 2 3U H11EU 2003010900004 20030109 00004 EU 2003 1 9 HEEA082843 1 20021216 A 6220 350A31185003 SLEEVE AEROSP AS355 AS355* EU M/R HEAD DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 972AE 1165 3234 ROTOR OVERSPEED TO 500 RPM CAUSED BY ENGINE OVERSPEED. 1 G 7 2 3U H11EU 2003010900005 20030109 00005 EU 2003 1 9 HEEA082844 1 20021216 A 6220 350A31185421 SCREW AEROSP AS355 AS355* EU M/R HEAD DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 972AE 1141 3234 ROTOR OVERSPEED TO 500 RPM CAUSED BY ENGINE OVERSPEED. 1 G 7 2 3U H11EU 2003010900006 20030109 00006 EU 2003 1 9 HEEA082845 1 20021216 A 6220 350A31191600 STARFLEX AEROSP AS355 AS355* EU M/R HEAD DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 972AE 337 3234 ROTOR OVERSPEED TO 500 RPM CAUSED BY ENGINE OVERSPEED. 1 G 7 2 3U H11EU 2003010900007 20030109 00007 EU 2003 1 9 HEEA082846 1 20021216 A 6520 350A33215001 BEARING AEROSP AS355 AS355* EU T/R SPIDER WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 40466 MA0957 3004 TAIL ROTOR SPIDER HAS A WORN BEARING. TO BE SENT TO VENDOR. 1 G 7 2 3U H11EU 2003010900008 20030109 00008 EU 2003 1 9 HEEA082847 1 20021216 A 6520 SEAL AEROSP AS355 AS355* EU SPIDER ASSY SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 856PH 1441 MA1154 3352 SEAL CAME OUT. REPAIRED. 1 G 7 2 3U H11EU 2003010900009 20030109 00009 EU 2003 1 9 HEEA082848 1 20021216 A 6520 350A33215300 BEARING AEROSP AS355 AS355* EU TAIL ROTOR HEAD DELAMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 856PH 3352 TAIL ROTOR HEAD BEARING DELAMINATED. TO BE SENT TO VENDOR. 1 G 7 2 3U H11EU 2003010900010 20030109 00010 EU 2003 1 9 HEEA082849 1 20021216 A 6230 350A37114820 PITCH LINK AEROSP AS355 AS355* EU MAIN ROTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 855PH 3351 MAIN ROTOR PITCH LINK CORRODED. TO BE SENT TO VENDOR. 1 G 7 2 3U H11EU 2003010900011 20030109 00011 EU 2003 1 9 HEEA082850 1 20021216 A 6230 350A37124420 SCREW AEROSP AS355 AS355* EU M/R HEAD DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 972AE 140 3234 ROTOR OVERSPEED TO 500 RPM CAUSED BY ENGINE OVERSPEED. 1 G 7 2 3U H11EU 2003010900012 20030109 00012 EU 2003 1 9 HEEA082851 1 20021216 A 6230 350A37124520 SCREW AEROSP AS355 AS355* EU M/R HEAD DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 972AE 140 3234 ROTOR OVERSPEED TO 500 RPM CAUSED BY ENGINE OVERSPEED. 1 G 7 2 3U H11EU 2003010900013 20030109 00013 EU 2003 1 9 HEEA082852 1 20021216 A 3210 350A4110161351 PAD AEROSP AS355 AS355* EU MLG BENT E HEEA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 03 972AE 1165 3234 PAD BENT AFTER AUTO ROTATION TO THE GROUND DUE TO ENGINE OVERSPEED. SCRAPPED. 1 G 7 2 3U H11EU 2003010900014 20030109 00014 EU 2003 1 9 HEEA082853 1 20021216 A 3210 350A41107620 SKID SHOE AEROSP AS355 AS355* EU MLG FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 970AE 3235 SKID SHOE FLAT; FAILED 500 HOUR INSPECTION. TO BE SENT TO VENDOR. 1 G 7 2 3U H11EU 2003010900015 20030109 00015 EU 2003 1 9 HEEA082854 1 20021216 A 7160 350A54108004 INTAKE AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1D1 NE ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 855PH 3351 ENGINE AIR INTAKE CRACKED AND CORRODED. TO BE SENT TO VENDOR. 1 G 7 2 3U 3 U H11EU E19EU 2003010900016 20030109 00016 EU 2003 1 9 HEEA082855 1 20021216 A 6210 355A11003002 BLADE AEROSP AS355 AS355* EU MAIN ROTOR OVERSPEED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 972AE 140 3234 MAIN ROTOR BLADE OVERSPEED TO 500 RPM. 1 G 7 2 3U H11EU 2003010900017 20030109 00017 EU 2003 1 9 HEEA082856 1 20021216 A 6410 355A12005004 BLADE AEROSP AS355 AS355* EU TAIL ROTOR OVERSPEED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 972AE 1165 3234 TAIL ROTOR BLADE OVERSPEED TO 500 RPM. 1 G 7 2 3U H11EU 2003010900018 20030109 00018 EU 2003 1 9 HEEA082857 1 20021216 A 6220 704A3363321151 SPHERICAL STOP AEROSP AS355 AS355* EU MAIN ROTOR OVERSPEED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 972AE 1165 3234 OVERSPEED TO 500 RPM. SCRAPPED. 1 G 7 2 3U H11EU 2003010900019 20030109 00019 EU 2003 1 9 HEEA082858 1 20021216 A 2910 704A34412034 HOSE AEROSP AS355 AS355* EU HYD SYSTEM LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 974AE 2653 HYDRAULIC HOSE LEAKING. SCRAPPED. 1 G 7 2 3U H11EU 2003010900020 20030109 00020 2003 1 9 HEEA082859 4 20021216 A 2312 9710831 RADIO AEROSP AS355 AS355* EU COCKPIT MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 970AE 3235 VHF RADIO WILL NOT TRANSMIT. 1 G 7 2 3U H11EU 2003010900021 20030109 00021 EU 2003 1 9 HEEA082860 1 20021216 A 5260 D23623 SUPPORT AEROSP AS355 AS355* EU STEP BENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 972AE 1165 3234 BENT AFTER AUTO ROTATION TO THE GROUND DUE TO ENGINE OVERSPEED. SCRAPPED. 1 G 7 2 3U H11EU 2003010900022 20030109 00022 EU 2003 1 9 HEEA082861 1 20021216 A 6730 SC5072 SERVO AEROSP AS355 AS355* EU TAIL ROTOR LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 970AE 1443 3235 SERVO PISTON SEAL OR PILOT VALVE LEAKING. TO BE SENT TO VENDOR. 1 G 7 2 3U H11EU 2003010900023 20030109 00023 EU 2003 1 9 HEEA082862 1 20021216 A 6220 BUSHING AEROSP AS355 AS355* EU STARFLEX DEBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 856PH 2181 M1310 3352 BUSHING ON END OF STARFLEX ARM DEBONDING. 1 G 7 2 3U H11EU 2003010900024 20030109 00024 EU 2003 1 9 HEEA082863 1 20021216 A 6730 SC5084 SERVO AEROSP AS355 AS355* EU CYCLIC CONTROL MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 856PH 3352 CYCLIC HARD TO CONTROL IN FLIGHT. REMOVE SERVO. 1 G 7 2 3U H11EU 2003010900025 20030109 00025 EU 2003 1 9 HEEA082864 1 20021223 A 7712 305731365 INDICATOR AEROSP AS355 AS355* EU TORQUEMETER MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 975AE 2777 TORQUE GAUGES SPINS ON POWER UP AND IS INTERMITTENT IN OPERATION. TO BE SENT TO VENDOR. 1 G 7 2 3U H11EU 2003010900026 20030109 00026 2003 1 9 HEEA082865 4 20021223 A 3454 069102505 TRANSCEIVER AEROSP AS355 AS355* EU VOR SYSTEM MALFUNCTIONED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 974AE 2653 DURING FUNCTION CHECK FOR NAV COM RADIO, DISPLAY STARTED FLASHING AND ALSO CHANGING FREQUENCY DISPLAYED WITH NO OPERATOR INPUT. COULD NOT DUPLICATE PROBLEM. RESEATED MICROPROCESSOR AND CATHODE AND ANODE DRIVERS. CLEANED ALL PLUG CONNECTOR S FOR ICS. ADJUSTED FREQUENCY AND SQUELCH FOR COMM. BENCH CHECK GOOD. 1 G 7 2 3U H11EU 2003010900027 20030109 00027 EU 2003 1 9 IO5R082685 1 20021226 A 6720 41800876800 ACTUATOR UROCOP EC135 EC135P1 8680990 EU TAIL ROTOR DEFECTIVE H IO5R O OTHER J WARNING INDICATION CR CRUISE 1 FS 01 552BA 606 190 YAW SAS ACTUATOR CAPTION ON CAD REMOVED AND REPLACED. 1 G 7 2 3U O H88EU 2003010900028 20030109 00028 EU 2003 1 9 IO5R082686 1 20021226 A 3340 4361646 LANDING LIGHT UROCOP EC135 EC135P1 8680990 EU EXTERIOR LIGHTS DEFECTIVE H IO5R O OTHER O OTHER CR CRUISE 1 FS 01 551BA 577 188 LANDING LIGHT WILL NOT TURN OFF RETRACTED REMOVED AND REPLACED 1 G 7 2 3U O H88EU 2003010900029 20030109 00029 EU 2003 1 9 IO5R082687 1 20021226 A 7120 L633M201101 MOUNT UROCOP EC135 EC135P1 8680990 EU ENGINE FAILED H IO5R A UNSCHED LANDING O OTHER CR CRUISE 1 FS 01 552BA 619 190 ARIS MOUNT FAILED IN FLIGHT REMOVED ARIS MOUNT FROM S/N 197 AND INSTALLED ON S/N 190 1 G 7 2 3U O H88EU 2003010900030 20030109 00030 EU 2003 1 9 IO5R082688 1 20021226 A 6720 41800876800 ACTUATOR UROCOP EC135 EC135P1 8680990 EU TAIL ROTOR FAILED H IO5R O OTHER J WARNING INDICATION CR CRUISE 1 FS 01 551BA 600 188 YAW SAS ACTUATOR FAILURE ON CAD. REMOVED AND REPLACED 1 G 7 2 3U O H88EU 2003010900034 20030109 00034 NM 2003 1 9 2002UALA01852 1 20021213 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2040 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 STATION 1640, RBL 57 FLOORBEAM UPPER CAP CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE IN STALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2003031300132 20030313 00132 NM 2003 3 13 2002UALA01853 1 20021214 A 2150 396480132144887 CONTROL VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A/C BAY MALFUNCTIONED A UALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 WP 29 539UA 25223 ON CLIMBOUT LEFT PACK CYCLED ON AND OFF EVERY TWO SECONDS. TURNED LEFT PACK OFF. RIGHT PACK UNABLE TO HOLD CABIN PRESS URE. REPLACED, LEFT PACK FLOW CONTROL VALVE / LEFT ENGINE PRSOV. FOUND RIGHT PACK DUCT SUPPLY TUBE SEPARATED FROM CHEC K VALVE. WHEN LEFT PACK SELECTED OFF AND RIGHT PACK AIR-FLOW DISRUPTED, AIRCRAFT UNABLE TO PRESSURIZE. 2 L 7 2 4F 4 F RT A2NM E17NE 2003010900035 20030109 00035 NE 2003 1 9 2002UALA01854 2 20021216 A 7230 COMPRESSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 2 ENGINE STALLED A UALA O OTHER Y ENGINE STOPPAGE DE DESCENT 1 WP 29 603UA 21864 NR 2 ENGINE COMPRESSOR STALL, UNSUCCESSFUL RESTART. VANES WOULD NOT TRACK. EVBC REPLACED. DISASSEMBLY OF EVBC SHOWED E VACUATED BELLOW DEFECTIVE. 2 L 7 2 4F 4 F RT A1NM E3NE 2003010900036 20030109 00036 NM 2003 1 9 2002UALA01857 1 20021210 A 2121 BEARING MR21271 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RECIRC FAN FAILED A UALA K NONE J WARNING INDICATION CR CRUISE 1 WP 29 176UA 4078 24383 ACRID ODOR IN CABIN OF ELECTRICAL OVERHEATING. CMC MESSAGE SHOWS UPPER AND LOWER LEFT RECIRCULATION FAN FAILED. SUPPLE MENTAL DATA UPDATE THE LOWER LEFT RECIRCULATION FAN MOTOR BEARINGS FAILED . THE MOTOR WAS REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 2003010900037 20030109 00037 NM 2003 1 9 2002UALA01858 1 20021217 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 DURING HMV3 THE BS794 AFT CARGO DOOR SURROUND FRAME BETWEEN STR 23R AND 24R, FOUND WITH ELONGATED HOLE. MAJOR REPAIR A CCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLE AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2003031800048 20030318 00048 NM 2003 3 18 2002UALA01859 1 20021217 A 5270 135W19201 TARGET BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CARGO DOOR BENT A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 799UA 26926 FORWARD CARGO DOOR LIGHT ON IN FLIGHT. SUPPLEMENTAL DATA UPDATE MAINTENANCE FOUND THE DOOR CLOSED SWITCH SENSOR TARGET B ENT OUT OF RANGE FOR THE SENSOR TO SENSE THE DOOR CLOSED. MAINTENANCE REPOSITIONED THE TARGET. 2 L 7 2 4F 4 F RT T0001SE E46NE 2003010900038 20030109 00038 NM 2003 1 9 2002UALA01861 1 20021216 A 3350 GUARD BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR SWITCH LOOSE A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHTS ADVISORY EICAS ALERT. SWITCH IS OFF, LIGHTS ARE ON. FOUND GUARD ON 1L DOOR SWITCH, ON PANEL, LOOSE. IT WAS SECURED. 2 L 7 4 4F 4 F RT A20WE E24NE 2003031400033 20030314 00033 NM 2003 3 14 2002UALA01862 1 20021216 A 3240 CZ9284E TRANSDUCER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE BRAKE STEERING FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 827UA 1022 BRAKE STEERING CONTROL UNIT CHANNEL 1 ECAM MESSAGE IN FLIGHT. *S/D* FAILURE OF THE NORMAL BRAKE PRESSURE TRANSDUCER (1 2GG) AS IDENTIFIED BY THE BSCU. REPLACED NORMAL BRAKE PRESSURE TRANSDUCER (12GG) AND PERFORMED OPERATIONAL CHECKS. 2 L 7 2 4F 4 F RT A28NM E40NE 2003010900039 20030109 00039 NM 2003 1 9 2002UALA01863 1 20021215 A 3397 GROUND WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 171UA 24322 DURING FLIGHT, THERE WAS A BURNING SMELL NEAR UPPER DECK ROW 12. OVERHEAD CEILING LIGHT SOCKET MELTED AND SPARKED FORWA RD AND AFT OF ROW 12. BOTH FLORESCENT LIGHT BALLASTS WERE DISCONNECTED. SUPPLEMENTAL DATA UPDATE FOUND BROKEN GROUND CO NNECTION ON LIGHT ASSEMBLY. REPAIRED GROUND CONNECTION. REPLACED SOCKET AND BALLAST. 2 L 7 4 4F 4 F RT A20WE E24NE 2003031800049 20030318 00049 NM 2003 3 18 2002UALA01864 1 20021217 A 3020 2703350 SEAL BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE ANTI ICE SYSTEM LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 WP 29 619UA 21879 LEFT BLEED DUCT LEAK EICAS MESSAGE. RETURNED TO FIELD. SUPPLEMENTAL DATA UPDATE LEFT ENGINE ANTI-ICE VALVE SEAL (S) LE AKING AT CLAMP. SEALS REPLACED, NO OTHER ACTION REQUIRED, 2 L 7 2 4F 4 F RT A1NM E3NE 2003010900040 20030109 00040 EU 2003 1 9 2002UALA01866 1 20021221 A 4920 APU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE APU BAY MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 401UA 435 RETURNED TO FIELD UNDER AMBER ALERT DUE TO APU AUTO SHUTDOWN. 2 L 7 2 4F 4 F RT A28NM E40NE 2003010900041 20030109 00041 NM 2003 1 9 2002UALA01867 1 20021220 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 RIGHT FUSELAGE SKIN, FORWARD OF POWER RECPT DOOR, HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED SKIN REPAIR . 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900042 20030109 00042 NM 2003 1 9 2002UALA01868 1 20021220 A 5320 CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 CABIN FRAME SUPPORT CLIP ON STRINGER 11R, CRACKED AT STATION 344. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLE D NEW CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900043 20030109 00043 NM 2003 1 9 2002UALA01869 1 20021220 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 EXTERNAL FUSELAGE SKIN IS DENTED AT STATION 312 BELOW STRINGER 24R. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER MANUFACTU RED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900044 20030109 00044 NM 2003 1 9 2002UALA01870 1 20021220 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 MID CABIN STATION 616 RIGHT FUSELAGE FRAME INNER CHORD CRACKED AT LOWER EDGE, JUST BELOW CABIN FLOOR. MAJOR REPAIR ACC OMPLISHED. REPAIR ANGLE MANUFACTURED AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900045 20030109 00045 NM 2003 1 9 2002UALA01871 1 20021220 A 5320 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 STRINGER CLIP CRACKED AT STATION 616, STRINGER 2L. MAJOR REPAIR ACCOMPLISHED. STRINGER CLIP REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900046 20030109 00046 NM 2003 1 9 2002UALA01872 1 20021220 A 5320 BRACKET BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 FORWARD CABIN RIGHT SIDE STATION 291.5, STR 11 AND 12 RIGHT, JUST INBOARD OF GALLEY DOOR CUTOUT, ANGLE BRACKET CRACKED. MAJOR REPAIR ACCOMPLISHED. CRACKED ANGLE REMOVED AND REPLACED WITH NEW. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900047 20030109 00047 NM 2003 1 9 2002UALA01873 1 20021220 A 5312 BULKHEAD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 AFT PRESSURE BULKHEAD, RIGHT FORWARD CIRCUMFERENTIAL STRAP BULKHEAD DENTED AT FASTENERS. MAJOR REPAIR ACCOMPLISHED. MA NUFACTURED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900048 20030109 00048 NM 2003 1 9 2002UALA01874 1 20021221 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 355UA 24361 FUSELAGE FRAME, STATION 188, LEFT OUTBOARD CHORD CRACKED AT STRINGER 17 WL 207. MAJOR REPAIR ACCOMPLISHED. CHORD AND W EB REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900049 20030109 00049 NM 2003 1 9 2002UALA01875 1 20021221 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 355UA 24361 CABIN FUSELAGE FRAME STATION 747 IS CRACKED AT STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900050 20030109 00050 NM 2003 1 9 2002UALA01876 1 20021221 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 355UA 24361 FUSELAGE FRAME, STATION 188, RIGHT SIDE IS CRACKED IN OUTBOARD CHORD AT STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900051 20030109 00051 NM 2003 1 9 2002UALA01877 1 20021221 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 355UA 24361 FUSELAGE WEB STA 188-199 AT WL 207 ON LEFT SIDE CRACKED IN CUTOUT RADIUS FOR FRAME FLANGE. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900052 20030109 00052 NM 2003 1 9 2002UALA01878 1 20021222 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 355UA 24361 CABIN STA 827 FRAME CRACKED AT FASTENER ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME REPAIR . 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900053 20030109 00053 NM 2003 1 9 2002UALA01879 1 20021222 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 355UA 24361 AFT CABIN FRAME IS CRACKED STATION 767 STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED DOUBLER REPA IR. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900054 20030109 00054 NM 2003 1 9 2002UALA01880 1 20021222 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 355UA 24361 CABIN STATION 807 FRAME CRACKED AT FASTENER JUST ABOVE STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTAL LED FRAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900055 20030109 00055 NM 2003 1 9 2002UALA01881 1 20021223 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 355UA 24361 CABIN STATION 847 FRAME IS CRACKED AT FASTENER JUST ABOVE STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED A J-ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900056 20030109 00056 NM 2003 1 9 2002UALA01882 1 20021223 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 355UA 24361 CABIN STATION 867 FRAME CRACKED JUST ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED A J-ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900057 20030109 00057 NM 2003 1 9 2002UALA01883 1 20021223 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 355UA 24361 CABIN STATION 807 FRAME CRACKED AT FASTENER JUST ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED A J-ANGLE DOU BLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900058 20030109 00058 NM 2003 1 9 2002UALA01884 1 20021220 A 2750 FLAP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE WING MALFUNCTIONED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 905UA 25005 UPON SELECTING FLAPS ONE, FLAP NEEDLES SPLIT AND FLAPS LOCKED OUT. CREW FOLLOWED FLIGHT MANUAL PROCEDURE AND DIVERTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900059 20030109 00059 NM 2003 1 9 2002UALA01885 1 20021222 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 667UA 29239 EXTERIOR EMERGENCY LIGHT AT DOOR 1L, INOPERATIVE. ORDERED NEW LIGHT ASSEMBLY. LIGHT ASSEMBLY LEFT OPEN AND DISASSEMBLE D. 2 L 7 2 4F 4 F RT A1NM E24NE 2003010900060 20030109 00060 NM 2003 1 9 2002UALA01887 1 20021223 A 3350 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 109UA 26906 TWO LEFT UPPER OVERWING ESCAPE LIGHTS ARE INOPERATIVE. POWER SUPPLY MODULE REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 2003010900061 20030109 00061 NM 2003 1 9 2002UALA01888 1 20021224 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 355UA 24361 FORWARD CABIN FRAME AT STATION 400 IS CRACKED STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED A J-ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900062 20030109 00062 EU 2003 1 9 2002UALA01889 1 20021223 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 497UA CREASE UNDER LEFT HAND SIDE WINDOW. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A28NM E40NE 2003010900063 20030109 00063 NM 2003 1 9 2002UALA01895 1 20021224 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 813UA 858 RECEIVED 'EPSU FWD L' MESSAGE ON FWD FLT ATTENDANT PANEL. REPLACED EMERGENCY POWER SUPPLY UNIT. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2003010900064 20030109 00064 NM 2003 1 9 2002UALA01898 1 20021226 A 5320 CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 355UA 24361 BODY STATION 178 LOWER CHORD RBL20, WL188, Z CLIP TO INTERCOSTAL IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED Z CLI P. 2 L 7 2 4F 4 F RT A16WE E2GL 2003031800052 20030318 00052 NM 2003 3 18 2002UALA01899 1 20021229 A 3242 M12301IND02 TIRE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 9 FAILED A UALA K NONE S AFFECT SYSTEMS LD LANDING 1 WP 29 221UA 262 30552 DURING LANDING NR 9 TIRE, BURST, CAUSING DAMAGE TO THE AFT FLAP. DAMAGE AREA APPROXIMATELY 13 X 10 INCHES. HOLE IS APP ROX 6 X 5.5 INCHES. SUPPLEMENTAL DATA UPDATE UPON LANDING NR 9 TIRE THREW TREAD WHICH CONTACTED AND DAMAGED THE LH IN BD TE FLAP ASSEMBLY. DAMAGED AND ADJACENT TIRE WAS REPLACED. PRELIMINARY INSPECTION OF THE DAMAGED TIRE SHOWS EVIDENCE OF FOREIGN OBJECT DAMAGE WHICH MAY HAVE STARTED DELAMINATION AND LOSS OF TIRE TREAD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2003031800053 20030318 00053 NE 2003 3 18 2002UALA01901 2 20021230 A 7200 1B5222 BLADE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STAGE 2 TURBINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 525UA 33621 4121 24978 727117 RT ENGINE EICAS MSG FOR FUEL FILTER. SUPPLEMENTAL DATA UPDATE AT ENGINE TEARDOWN, A STAGE 2 TURBINE BLADE FAILURE WAS F OUND TO BE THE CAUSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2003010900065 20030109 00065 NM 2003 1 9 2002UALA01903 1 20021230 A 5512 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 355UA 24361 DENT IN LEADING EDGE OF RIGHT HAND HORIZONTAL STABILIZER, 8 INCHES INBOARD OF TIP. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2003010900067 20030109 00067 NM 2003 1 9 2003UALA00006 1 20021224 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE BULGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 606UA 21867 LOWER EXTERNAL FUSELAGE SKIN BULGING STATION 720 STRINGER 38R. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A1NM E3NE 2003010900068 20030109 00068 EA 2003 1 9 02347684 1 20020213 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA FA SERVICE PANEL NOT SEATED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 684BR 7708 DURING OVERNIGHT MAINTENANCE IT WAS DISCOVERED THAT THE FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH WAS INOPERATIVE. MAINTE NANCE PERSONNEL RESEATED THE CONNECTOR PLUG AT THE FLIGHT ATTENDANT SERVICE PANEL. AN OPERATIONAL CHECK OF THE EMERGENC Y LIGHTS WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003010900079 20030109 00079 NM 2003 1 9 02FDEA00677 1 20020922 A 3230 ACTUATOR DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE MLG MALFUNCTIONED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 593FE 48551 AFTER TAKEOFF, BOTH PRIMARY (LIGHT BY HANDLE) AND SECONDARY (SYNOPTIC) SHOWED UNSAFE FOR LEFT MAIN LANDING GEAR WITH GE AR HANDLE UP. CYCLED GEAR, NO HELP. INDICATIONS OK WITH HANDLE DOWN. DUMPED FUEL, RETURNED FOR NORMAL LANDING. REMOV ED AND REPLACED LEFT GEAR BRAKE LINE BRACKET SUPPORT ASSY, BOGIE BEAM TRIM ACTUATOR OPS CHECKED IAW MM, OPS NORMAL. PERFORMED OPS EXTENSION RETRACTION TEST ON LEFT MAIN LANDING GEAR IAW MM. OPS, NORMAL. PERFORMED ANTISKID CONTROL UNIT TEST IAW MM. ALL TEST PASS. 2 L 7 3 4F 4 F RT A22WE E13NE 2003010900080 20030109 00080 NM 2003 1 9 02FDEA00922 1 20021204 A 5315 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D9 52048 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 CORROSION ON FLOORBEAM, BS 720D, LBL 5. BLENDED CORROSION ON FLOORBEAM, FOUND TO BE OUT OF LIMITS IAW SRM. CUT OUT DAM AGE FROM BS 720-720F, BL 0. FABRICATED AND INSTALLED REPAIR IAW EA. 2 L 7 3 4F 4 F RT A3WE E2EA 2003010900081 20030109 00081 NM 2003 1 9 02FDEA00930 1 20021206 A 5311 FRAME BOEING 727 727200 138407E NM PWA JT8 JT8D9 52048 NE FUSELAGE BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 FUSELAGE FRAME BS 500 UPPER FLANGE IS BENT RBL 33 WL 160. REMOVED DAMAGE AND REPAIRED IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2003010900082 20030109 00082 NM 2003 1 9 02FDEA00932 1 20021206 A 5311 FRAME BOEING 727 727200 138407E NM PWA JT8 JT8D9 52048 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 FUSELAGE FRAME BS 500 UPPER FLANGE HAS SEVERAL DENTS LBL 33-47. REMOVED EXISTING FRAME SPLICE BS 500, LBL 33. CUT OUT DAMAGED AREAS AT LBL 33 TO LBL 47. FABRICATED AND DRILLED UP NEW FRAME SPLICE. INSTALLED NEW FRAME SPLICE AND FASTENER S IAW B727 SRM AND EA. 2 L 7 3 4F 4 F RT A3WE E2EA 2003010900083 20030109 00083 NM 2003 1 9 02FDEA00956 1 20021218 A 5320 SUPPORT ANGLE BOEING 727 727200 138407E NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 212FE 22934 CORROSION FLOORBEAM SUPPORT ANGLE, UPPER FLANGE, LWR SURFACE BS 825, RBL 62, 207.5. REMOVED, FABRICATED AND REPLACED FL OORBEAM SUPPORT ANGLE IAW SRM AT BS 825, RBL 62. 2 L 7 3 4F 4 F RT A3WE E2EA 2003010900084 20030109 00084 NM 2003 1 9 02FDEA00957 1 20021218 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 212FE 22934 CORROSION, BS 720A, FWD SIDE OF FRAME AT STR 8L. 2 L 7 3 4F RT A3WE 2003010900085 20030109 00085 NM 2003 1 9 02FDEA00960 1 20021221 A 5753 6521630265 FLAP BOEING 727 727200 138407E NM PWA JT8 JT8D9 52048 NE T/E FLAP MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 FOUND APPROXIMATELY 5.5 FT INBOARD SECTION OF THE LEFT FORE FLAP MISSING ON POST FLIGHT INSPECTION. REMOVED LEFT INBOAR D FORE FLAP ASSEMBLY IAW MM. INSTALLED LEFT INBOARD FORE FLAP IAW M/M, SYSTEMS OPS, CHECK NORMAL. 2 L 7 3 4F 4 F RT A3WE E2EA 2003010900086 20030109 00086 EU 2003 1 9 02FDEA00961 1 20021222 A 7933 BULB AIRBUS 310 A310 EU PWA JT9 JT9D* NE NR 1 ENGINE FAULTY A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 450FE 162 707715 LEVELED OFF AT FL330, OIL TEMPERATURE BEGAN INCREASING. INCREASED THRUST, ATTEMPTING TO DECREASE OIL TEMPERATURE, BUT I T CONTINUED TO CLIMB, TURNING AMBER, THEN RED UNTIL IT REACHED 165 DEGREES, SHUT DOWN NR 1 ENGINE AND DIVERTED. REMOVED AND REPLACED TEMP BULB IAW MM. RAN ENGINE FOR 1 HOUR AT VARIOUS POWER SETTINGS AND OIL TEMPERATURE NEVER CLIMBED ABOVE 100 DEGREES. OPS AND LEAK CHECK GOOD, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A35EU E20EA 2003010900087 20030109 00087 NM 2003 1 9 02FDEA00962 1 20021220 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MDCC FLOOR SEAT TRACK FLANGE FOUND WITH CORROSION AT STA 1521, LBL 8. TRIMMED CORRODED FLANGE AT STA 1521, LBL 8 IAW SR M. NON DESTRUCTIVE TESTING CARRIED OUT AT TRIMMED AREA IAW DAC NDT SPM. FAB FILLER AND STRAP IAW SRM. INSTALLED IAW SRM. 2 L 7 3 4F RT A22WE 2003020600143 20030206 00143 NM 2003 2 6 02FDEA00963 1 20021220 A 5320 STRAP DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MDCC LT FUSELAGE FRAME STA Y 1199 STR 16 FOUND TIE STRAP WITH CORROSION. 2 L 7 3 4F RT A22WE 2003010900088 20030109 00088 NM 2003 1 9 02FDEA00964 1 20021223 A 5315 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D* NE FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 212FE 22934 LONGITUDINAL FLOORBEAM OUTBOARD, LOWER FLANGE, UPPER SIDE IS GOUGED, JUST BELOW FASTENER HOLES FROM BS 740-848, RBL 51, WL 208. FABRICATED AND REPLACED LONGITUDINAL BEAM UPPER CHORD IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2003010900089 20030109 00089 NM 2003 1 9 02FDEA00965 1 20021223 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MDCC FLOOR SEAT TRACK FOUND WITH CORROSION AT STA 585, 685 X -75.25. TRIMMED OUT DAMAGED AREA ON SEAT TRACK FLANGE IAW SRM, FABRICATED FILLER AND STRAP IAW SRM. INSTALLED FILLER AND STRAP IAW SRM. 2 L 7 3 4F 4 F RT A22WE E13NE 2003010900090 20030109 00090 NM 2003 1 9 02FDEA00966 1 20021223 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MDCC FLOOR SEAT TRACK FOUND WITH CORROSION AT STA 585 - 685, X=-107.25. TRIMMED DAMAGED AREA ON FLANGE AT STA 653 RBL 1 07.25 IAW SRM. FABRICATED FILLER AND STRAP IAW SRM. INSTALLED FILLER AND STRAP IAW SRM. 2 L 7 3 4F RT A22WE 2003010900091 20030109 00091 NM 2003 1 9 02FDEA00967 1 20021226 A 5313 STRINGER DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK CARGO COMPARTMENT, RIGHT FUSELAGE FRAME, BS Y 1139-1159, STRINGER 17, CRACKED. R/R MDCC RT FUSELAGE FRAME BS Y 1139-1159 STRINGER. 2 L 7 3 4F RT A22WE 2003010900092 20030109 00092 NM 2003 1 9 02FDEA00968 1 20021226 A 5313 STRINGER BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 LOWER FUSELAGE, STRINGER 21R, IS CRACKED AT STA 400. 2 L 7 3 4F RT A3WE 2003010900093 20030109 00093 NM 2003 1 9 02FDEA00969 1 20021226 A 5313 STRINGER BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 AFT CARGO COMPARTMENT, STA 1070 TO 1090, STRINGER 29R IS CORRODED. REMOVED AND REPLACED STRINGER SECTION IAW SRM. 2 L 7 3 4F RT A3WE 2003010900094 20030109 00094 NM 2003 1 9 02FDEA00970 1 20021226 A 5330 LAP JOINT BOEING 727 727100 1384036 NM FUSELAGE BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 FUSELAGE SKIN BETWEEN STA 595 AND 620 ALONG STR 14R SKIN LAP JOINT IS BULGING AT RIVETS. REPAIRED IAW EA. 2 L 7 3 4F RT A3WE 2003010900095 20030109 00095 NM 2003 1 9 02FDEA00971 1 20021226 A 5313 STRINGER BOEING 727 727100 1384036 NM PWA JT8 JT8D1 52044 NE FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 LOWER FUSELAGE, STRINGER 21R, IS CRACKED AT STA 400. REMOVED DAMAGED SECTION OF STRINGER FROM STATION 390-410 AND REPLA CED IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2003010900096 20030109 00096 NM 2003 1 9 ASAA0210303 1 20021111 A 5410 6570947252 PYLON BOEING 737 737210C 1384459 NM RT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND RIGHT PYLON AT FAIRING STATION 80, WING STATION 166.5 CRACKED. REMOVED DAMAGE AND FABRICATED REPAIRS PER SRM. (M) 2 L 7 2 4F A16WE 2003010900097 20030109 00097 NM 2003 1 9 ASAA0210304 1 20021112 A 5320 BAC150529222 SUPPORT ANGLE BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND SUPPORT ANGLE AT BS 520, RBL 48 - RBL 60 CORRODED. REMOVED, FABRICATED AND INSTAL LED SUPPORT ANGLE PER SRM. (M) 2 L 7 2 4F A16WE 2003010900098 20030109 00098 NM 2003 1 9 ASAA0210305 1 20021112 A 5320 654860828 SUPPORT BOEING 737 737210C 1384459 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND AFT FAIRING SUPPORT AT BS 540, LEFT BUTTOCK LINE 8, LEFT BUTTOCK LINE 70 CRACKED. REMOVED AND REPLACED AFT FAIRING SUPPORT PER SRM. (M) 2 L 7 2 4F A16WE 2003010900099 20030109 00099 NM 2003 1 9 ASAA0210306 1 20021112 A 7110 657377322 RIB BOEING 737 737210C 1384459 NM NR 1 COWLING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL AT NACELLE STATION 144.20 GOUGED. REMOVED AND REPLACED NR 1 ENGI NE COWL RIB PER SRM. (M) 2 L 7 2 4F A16WE 2003010900100 20030109 00100 NM 2003 1 9 ASAA0210307 1 20021112 A 5315 65548932 FLOORBEAM BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 420, LEFT BUTTOCK LINE 49, LEFT BUTTOCK LINE 59 CORRODED. REMOVED CORROSION AND FABRICATED REPAIR PER EA. (M) 2 L 7 2 4F A16WE 2003010900101 20030109 00101 NM 2003 1 9 ASAA0210308 1 20021113 A 5315 65549063 FLOORBEAM BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 500B, LEFT BUTTOCK LINE 6, LEFT BUTTOCK LINE 44 CORRODED. REMOVED CORROSION AND FABRICATED REPAIR PER EA. (M) 2 L 7 2 4F A16WE 2003010900102 20030109 00102 NM 2003 1 9 ASAA0210309 1 20021113 A 5315 6546568 FLOORBEAM BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BODY STATION 1016, LEFT BUTTOCK LINE 36, RIGHT BUTTOCK LINE 36 CORROD ED. REMOVED CORROSION AND FABRICATED REPAIR PER EA. (M) 2 L 7 2 4F A16WE 2003010900103 20030109 00103 NM 2003 1 9 ASAA021031 1 20021113 A 7110 65701935 COWLING BOEING 737 737210C 1384459 NM NR 2 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 THRUST REVERSER COWLING AT REVERSER STATION 98.2 GOUGED. REPAIRED THRUST REV ERSER COWLING PER SRM. (M) 2 L 7 2 4F A16WE 2003010900104 20030109 00104 NM 2003 1 9 ASAA0210310 1 20021113 A 5315 655490510 FLOORBEAM BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 480, LEFT BUTTOCK LINE 42 CORRODED. REMOVED CORROSION AND FABRICA TED REPAIR PER EA. (M) 2 L 7 2 4F A16WE 2003010900105 20030109 00105 NM 2003 1 9 ASAA0210311 1 20021113 A 5315 FLOORBEAM BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM FLANGE AT BS 787, LEFT BUTTOCK LINE 45, RIGHT BUTTOCK LINE 45 CORRODED. REMOVED CORROSION AND FABRICATED REPAIR PER EA. (M) 2 L 7 2 4F A16WE 2003010900106 20030109 00106 NM 2003 1 9 C1HA200292033 1 20021222 A 3350 LIGHT BOEING 727 727212 138407G NM BROKEN A C1HA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 292AS 21458 EMERGENCY LIGHT FEEL DURING TAXI OUT-RETURNED TO GATE.INSTALLED SERVICEABLE EMERG. LIGHT COVER AT DOOR 1. OK FOR SERVICE . 2 L 7 3 4F A3WE 2003010900107 20030109 00107 NM 2003 1 9 C1HA200293012 1 20021231 A 2621 APU BOEING 727 727212 138407G NM FIRE A C1HA F ACTIVATE FIRE EXT. A FLAME/FIRE IN INSP/MAINT 1 GL 15 293AS 21348 APU FIRE BOTTLE DISCHARGEDREMOVED AND REPLACED APU FIRE BOTTLE PER MM 26-23-1. 2 L 7 3 4F A3WE 2003010900108 20030109 00108 NM 2003 1 9 C1HA200294010 1 20021210 A 2612 FIRE LOOP BOEING 727 727290 138408W NM A C1HA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 294AS 22146 ENGINE FIRE DETECTION LIGHT ON CB PANEL LIGHT ONREPOSITIONED FIRE LOOP AS REQUIRED OK FOR SERVICE 2 L 7 3 4F A3WE 2003010900109 20030109 00109 NM 2003 1 9 C1HA200294013 1 20021210 A 2751 SWITCH BOEING 727 727290 138408W NM A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 294AS 22146 TAKE -OFF WARNING HORN SOUNDED ON T/OFOUND SPEED BRAKE DETENT SWITCH ARM BENT. ADJUSTED ARM SWITCH AND TAKE-OFF WARNING CHECKS GOOD.REPLACED AUTO SPEED BRAKE ARMING SWITCH AS PRECAUTIONARY IAW 727 MM 27-62-101. 2 L 7 3 4F A3WE 2003010900110 20030109 00110 NM 2003 1 9 C1HA200294014 1 20021213 A 2751 SWITCH BOEING 727 727290 138408W NM A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 294AS 22146 TO AUREL WARNING SOUNDED @ APP 1.8 EPR ON TO ROLL HELD SPEED BRAKE DOWN WITH 1 HAND SILENCED HORN WHEN RELEASED IT RESOU NDEDR&R'D SPEED BRAKE WARN TAKEOFF SWITCH AS PER STANDARD WIRING PRACTICES. PERFORMED TAKE-OFF WARNING TEST. 2 L 7 3 4F A3WE 2003010900111 20030109 00111 NM 2003 1 9 C1HA200281008 1 20021225 A 2611 SMOKE DETECTOR BOEING 727 7272S7 138407Z NM A C1HA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 15 681CA 22020 CARGO/SMOKE AFT COMPARTMENT B CHANNEL FAULT. AFT COMPARTMENT A CHANNEL TEST OK.CLEANED CARGO BAY SMOKE DETECTORS PER CHA MPION TASK CARD B727-2611-01. OPS CK GOOD. 2 L 7 3 4F A3WE 2003010900112 20030109 00112 NM 2003 1 9 C1HA200281009 1 20021218 A 3260 SWITCH BOEING 727 7272S7 138407Z NM A C1HA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 681CA 22020 NOSE GEAR DOOR LIGHT (BOTH F.E. AMBER/FRONT RED) LIGHTS INTERMITTENT ON TAXICLEANED NOSE GEAR DOOR SWITCH. CYCLED DOOR SEVERAL TIMES. OPS CHECKED GOOD. REF M/M 32-60 2 L 7 3 4F A3WE 2003010900113 20030109 00113 NM 2003 1 9 C1HA200282017 1 20021211 A 3350 BULB BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 L-2 & R-2 EMERGENCY EXIT SIGNS INOPRELAMPED L-2 & R-2 EMERG EXIT LWR DOOR SIGNS IAW MM 33-50-11. OPS CHKS GOOD. 2 L 7 3 4F A3WE 2003010900114 20030109 00114 NM 2003 1 9 C1HA200282018 1 20021211 A 3350 BATTERY PACK BOEING 727 7272S7 138407Z NM A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 LH FWD OVERWING EMERGENCY EXIT LIGHT INOPR&R L/H FWD EMERG EXIT LIGHT BATTERY PACK IAW MM 33-50-21, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2003010900115 20030109 00115 NM 2003 1 9 C1HA200285014 1 20021209 A 2613 AIR DUCT BOEING 727 7272S7 138407Z NM A C1HA E ENGINE SHUTDOWN M OVER TEMP CL CLIMB 1 GL 15 685CA 22492 INTERMITTENT FIRE LIGHT / BELL #2 PERFORMED #2 SHUTDOWN PROCEDURE EMERGENCY DECLARED. WARNING OCCURED DURING CLIMB OUT. FUEL DUMPED ENG #2 WINDMILLED 20 MINUTES, OIL PRESSURE 20 PSI, OIL PRESS AT SHUTDOWN 45 PSI.REMOVE AND REPLACE ENG. FIRE EXTINGUSHER BOTTLE IAW M/M 26-21-01. REMOVE AND REPLACE 13TH STAGE DUCT CAP IAW M/M 36-10-00. REMOVE AND REPLACED ENG O IL FILTER IAW M/M 79-23-00 RUN ENG. NO LEAK NOTED 2 L 7 3 4F A3WE 2003010900116 20030109 00116 NM 2003 1 9 C1HA200297030 1 20021205 A 3350 LIGHT BOEING 727 727270 138408P NM A C1HA O OTHER O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 EMERGENCY LIGHT AT BOTTOM OF AIRSTAIR IS INOPREMOVED AND REPLACED LIGHT ASSYMBLY IAW MM REF 33-51-01 2 L 7 3 4F RT A3WE 2003010900117 20030109 00117 NM 2003 1 9 C1HA200297031 1 20021222 A 3350 LIGHT BOEING 727 727270 138408P NM A C1HA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 15 697CA 23052 THIRD OVERHEAD EXIT SIGN - LIGHT INOP.OPS CHECKED EMER EXIT LIGHTS DURING SERVICE CHECK AND FOUND ALL TO BE OPERATING NO RMALLY. COULD NOT DUPLICATE REPORTED MALFUNCTION. 2 L 7 3 4F RT A3WE 2003010900118 20030109 00118 NM 2003 1 9 C1HA200297032 1 20021205 A 3350 LIGHT BOEING 727 727270 138408P NM A C1HA O OTHER O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 R-1 DOOR O/H EMERGENCY LIGHT INOPINSTALL PORTABLE EMERGENCY EXIT LIGHT OVER R-1 DOOR IAW MM 33-50-101 OPS CHECK GOOD 2 L 7 3 4F RT A3WE 2003010900119 20030109 00119 2003 1 9 C1HA200297033 4 20021212 A 3417 ADC BOEING 727 727270 138408P NM A C1HA B EMER. DESCENT G MULTIPLE FAILURE CL CLIMB 1 GL 15 697CA 23052 ON INITIAL CLIMB OUT OF LAS AIR DATA COMPUTER CIRCUT BREAKER POPPED. COMPLETED THE " CIRCUT BREAKER OPEN" CHECKLIST RESE T CIRCUT BREAKER ONCE. CAPT'S AIRSPEED INDICATOR FAILED, GPWS FAILED, TRANSPONDER MODE C FAILED, LAS ALTITUDE REPORTER F AILED, SUSPECT ADC BAD.REMOVED AND REPLACED AIR DATA COMPUTER #1, SYSTEM OPS CK NORMAL. IAW 727M/M 34-12-0 PAGE 7, 34-12 -11 PAGE 401. 2 L 7 3 4F RT A3WE 2003010900122 20030109 00122 EA 2003 1 9 02364621 1 20021230 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN MALFUNCTIONED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 621BR 7186 DURING INSPECTION, MAINTENANCE CREW REPORTED FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE IN AFT CABIN. MAINTENANCE PERSONN EL PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2003010900123 20030109 00123 CE 2003 1 9 GUU2003F00000 1 20021210 A 2697 GROUND WIRE BEECH 1900 1900D 1154162 CE FIRE PROTECTION LOOSE A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 17 48544 UE183 DURING FLIGHT, NUMBER TWO ENGINE FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY. CONTINUED TO FLL. LANDE D WITHOUT INCIDENT. TIGHTENED LOOSE GROUND WIRE ON NUMBER TWO ENGINE FIRE EXTINGUISHER. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2003010900125 20030109 00125 NM 2003 1 9 AWXA200300020 1 20021224 A 5315 146N5130 SEAT TRACK BOEING 757 7572G7 1384963 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 0 0 24523 LCQ - MAJOR REPAIR - DURING C-10 CHECK A 3/4" CRACK WAS FOUND ON THE UPPER RADIUS OF THE OUTBOARD R/H SEAT TRACK IN THE AFT CARGO COMPARTMENT. MAINTENANCE REMOVED THE SEAT TRACK FROM BS 1180 TO BS 1280, RBL 45.5; FABRICATED A NEW REPLACEMEN T SEAT TRACK ; INSTALLED REPAIR PART IAW B757-200 SRM 53-60-52, PG. 1-2. 2 L 7 2 4F RT A2NM 2003010900126 20030109 00126 NM 2003 1 9 AWXA200300022 1 20021219 A 5315 BAC1520792 SEAT TRACK BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 0 0 23776 MCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON SEAT TRACK BS 335 TO BS 338, RBL 45. MAINTENANCE BLENDED O UT CORROSION ON SEAT TRACK AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS PER B737-300 SRM 51-30-02, PG. 68, FIG. 1; REMOVE D DAMAGED SEAT TRACK FROM BS 335 TO BS 344, RBL 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; AND INSTALLED REPAIR PART I AW B737-300 SRM 51-40-05, PG. 4, FIG. 2. 2 L 7 2 4F RT A16WE 2003010900127 20030109 00127 WP 2003 1 9 2003F00003 1 20021222 A 3350 5165741 POWER SUPPLY LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122* 54555 NE CABIN DISCHARGED G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 198AT 193B1111 DURING SCHEDULED INSPECTION RIGHT 1 DOOR EXTERIOR EGRESS LIGHT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED RIGHT 1 DOOR POWERPACK IAW MM, OPERATIONAL CHECK GOOD. 2 L 7 3 4F 4 F A23WE A12EU 2003011000002 20030110 00002 NM 2003 1 10 2003F00062 1 20021021 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 335US 23232 MCO - DURING OVERNIGHT CHECK, WHILE ACCOMPLISHING EMERGENCY LIGHT OPERATIONAL TEST, MAINTENANCE FOUND THE LOW LEVEL EMER GENCY LIGHTS AT SEAT ROWS 11 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSE MBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003011000003 20030110 00003 NE 2003 1 10 2003F00063 2 20021116 A 7510 6058T80P03 ANTI-ICE VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE MALFUNCTIONED A UHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 03 157SD 3344 786 157 FLT 4511 - PIT-CLE - DID AN AIRTURNBACK TO PIT DUE TO RIGHT ENGINE ANTI-ICE VALVE CAUTION LIGHT CYCLES ON AND OFF IN ONE MINUTE INTERVALS. MAINTENANCE REMOVED AND REPLACED THE ANTI-ICE VALVE ON THE RIGHT ENGINE. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 2003011000004 20030110 00004 EU 2003 1 10 2003F00064 1 20021108 A 7830 FGFB583701200D3 BLOCKER DOOR AMD FALC90 FALCON900EX 2730009 EU THRUST REVERSER CRACKED A IK9A K NONE O OTHER IN INSP/MAINT 1 NE 03 93CR 96 DURING A ROUTINE INSPECTION OF THE THRUST REVERSER IAW THE MANUFACTURER'S OCIP PROGRAM, TWO CRACKS WERE FOUND ON THE INN ER SKIN, OUTBOARD EDGE, OF THE RIGHT SIDE THRUST REVERSER BLOCKER DOOR. THE DOOR WAS REPLACED WITH A NEW DOOR PROCEDURE FROM DASSAULT AND RETURNED TO SERVICE. AIRCRAFT TOTAL TIME WAS 456 HOURS. (M) 2 L 7 3 4F RT A46EU 2003011000005 20030110 00005 EU 2003 1 10 2003F00065 1 20021114 A 3150 005WS00 WEU SAAB SF340 SF340A 7850100 EU COCKPIT MALFUNCTIONED A UHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NE 03 121CQ 2757 121 FLT 4471 - TTN-BED, ABORTED TAKEOFF, DUE TO A CONFIGURATION WARNING AND WHITE BITE LIGHT. MAINTENANCE REMOVED AND REPLA CED THE WEU. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2003011000006 20030110 00006 EU 2003 1 10 2003F00066 1 20021114 A 5230 DOOR SAAB SF340 SF340A 7850100 EU CARGO DOOR OBSTRUCTED A UHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NE 03 43SZ 340A043 FLT 4480 - DURING TAXI, PIT TO TOL, THE CARGO DOOR WARNING LIGHT CAME ON THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED THE CARGO DOOR PULL DOWN ROPE FROM UNDER THE DOOR. THE CARGO DOOR WARNING SYSTEM CHECKED GOOD, THE AIRCRAFT WA S RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 2003011000007 20030110 00007 EU 2003 1 10 2003F00068 1 20021111 A 2913 4018502 PUMP SAAB SF340 SF340A 7850100 EU HYD SYSTEM FAILED A UHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 03 101CN 340A101 FLT 4504 - IN CRUISE, THE MAIN HYDRAULIC PUMP FAILED. THE PILOT DECLARED AN EMERGENCY AND RETURNED TO PIT. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC PUMP. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2003011000008 20030110 00008 NE 2003 1 10 2003F00069 2 20021106 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE NR 1 & NR 2 POWER LOSS A UHLA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 NE 03 149SZ 23105 340A149 367149 ON TAKEOFF, TORQUE LAGGED POWER LEVER ADVANCEMENT, OBTAINED ONLY 80 PERCENT TORQUE ON BOTH ENGINES. ENGINE ANTI-ICE ON. ABORTED TAKEOFF IN PIT. MAINTENANCE INSPECTED THE ENGINE AND PERFORMED A GROUND RUN UP. NO DISCREPANCIES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2003011000009 20030110 00009 NE 2003 1 10 2003F00070 2 20021106 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE NR 1 & NR 2 POWER LOSS A UHLA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 NE 03 149SZ 340A149 367470 ON TAKEOFF, TORQUE LAGGED POWER LEVER ADVANCEMENT, OBTAINED ONLY 80 PERCENT TORQUE ON BOTH ENGINES. ENGINE ANTI-ICE ON. ABORTED TAKEOFF IN PIT. MAINTENANCE INSPECTED THE ENGINE AND PERFORMED A GROUND RUN UP. NO DISCREPANCIES NOTED. THE A/C WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2003011000010 20030110 00010 NE 2003 1 10 2003F00080 2 20021105 A 7200 SMOKE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LT ENGINE DETECTED A UHLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NE 03 123XS 123 378360 ON CLIMB-OUT, AT IPT, GROUND PERSONNEL REPORTED AN ORANGE GLOW WITH PUFFS OF SMOKE COMING FROM THE LEFT ENGINE. ALL COC KPIT INDICATIONS WERE NORMAL. THE AC RETURNED TO IPT. MAINTENANCE INSPECTED THE LEFT ENGINE, PERFORMED A GROUND RUN. NO DISCREPANCIES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2003011000011 20030110 00011 EU 2003 1 10 2003F00081 1 20021031 A 3213 AIR8302212 STRUT SAAB SF340 SF340A 7850100 EU LT MLG LOW A UHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 03 118SD 7170 3771 118 ON CLIMB-OUT FROM FWA, COULD NOT RETRACT LANDING GEAR WITHOUT DEPRESSING DOWN LOCK RELEASE. UPON BRINGING CONDITION LEV ERS BACK IN CLIMB, CONFIG WARNING HORN SOUNDED. AFTER GEAR RETRACTION, OAT WARNING LIGHT ILLUMINATED. FLIGHT 4505 RETUR NED TO FWA, MAINTENANCE RESERVICED THE LEFT MAN LANDING GEAR STRUT. OPS AND FLIGHT TEST OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT A52EU 2003011000012 20030110 00012 EA 2003 1 10 2003F00082 1 20020611 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A MASA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 77181 7181 FLT 6416 - EUG-PHX - PILOT DECLARED AN EMERGENCY DUE TO FLAPS FAILING AT ZERO. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE BPSU AND THE RIGHT NR 5 FLEXSHAFT. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F RT A21EA 2003011000013 20030110 00013 NM 2003 1 10 2003F00088 1 20021108 A 5753 NRC6053509 WEDGE DOUG DC10 DC1040F 3023507 NM T/E FLAP DAMAGED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 140WE 54411 46920 DURING ROUTINE MAINTENANCE, THE LEFT WING OUTBOARD FLAP INBOARD TRAILING EDGE WEDGE WAS FOUND DAMAGED. ACCOMPLISHED REP AIR IAW AS11 DRAWING AS11467, AND 8110-3 WAS ISSUED. RETURNED AIRCRAFT TO REVENUE SERVICE. (M) 2 L 7 3 4F RT A22WE 2003011000014 20030110 00014 NM 2003 1 10 2003F00089 1 20021103 A 7830 1960006508 THRUST REVERSER DOUG DC10 DC1040F 3023507 NM NR 2 ENGINE DEBONDED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 52596 46661 DURING ROUTINE MAINTENANCE, THE NR 2 ENGINE THRUST REVERSER INNER SURFACE WAS FOUND DEBONDED. REMOVED DEBONDED AREA, FA BRICATED DOUBLER REPAIR AND REPAIRED AREA IAW AS11 DRAWING AS11465, AND AN 8110-3 WAS ISSUED. RETURNED AIRCRAFT TO REVE NUE SERVICE. (M) 2 L 7 3 4F RT A22WE 2003011000015 20030110 00015 WP 2003 1 10 ASAA0280574 1 20021119 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 PDX - FOUND OVERHEAD EMERGENCY SPOT LIGHT FOUND INOPERATIVE AT ROW 19-21. REPLACED ASSOCIATED POWER SUPPLY, BATTERY PAC K. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003011000016 20030110 00016 WP 2003 1 10 ASAA0280582 1 20021117 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 LAS - DURING PREFLIGHT CHECK, THE EMERGENCY TRACK LIGHTING IN FIRST CLASS CABIN WAS INOPERATIVE. REPAIRED BROKEN WIRE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003011000017 20030110 00017 WP 2003 1 10 ASAA0280603 1 20021120 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING LINE CHECK, THE EMERGENCY TRACK LIGHTING IN FIRST CLASS CABIN WAS INOPERATIVE. RECONNECTED LOOSE CONNECTOR . LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003011000018 20030110 00018 EA 2003 1 10 ASOA02578 1 20021031 A 7714 4033T65P03 SENSOR CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAILED A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 877AS 7579 FLT 4793 - DURING TAKEOFF FROM ATL-DHN, BOTH ENGINES WERE SET AT APPROXIMATELY 90 PERCENT. DURING CLIMB-OUT, THE LEFT E NGINE N-1 WENT TO THE LOW 70 PERCENT AND FLUXED BETWEEN THE LOW TO HIGH 70'S. THERE WAS ALSO A FUEL LOW FLUX AND THE OI L PRESSURE REMAINED CONSTANT. AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. THE LEFT AND RIGHT ENGINE SPEED CONTROL SYSTEM WAS DEFERRED. MAINTENANCE CLEARED THE DEFERRAL BY REMOVING AND REPLACING THE LEFT EN GINE T2 SENSOR, AND CLEANING ALL ASSOCIATED CANNON PLUGS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003011000021 20030110 00021 SO 2003 1 10 ASOA02590 1 20021114 A 2197 W201162820 WIRE EMB 120 EMB120ER 3260203 SO COCKPIT BROKEN A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 261AS 120141 FLT 4835 - DURING CLIMB-OUT FROM XNA-DFW, A SMOKE SMELL OCCURRED IN THE COCKPIT. AN EMERGENCY WAS DECLARED AND THE AIRC RAFT RETURNED TO XNA. THE SMELL INTENSIFIED DURING THE RETURN UNTIL THE AIRCRAFT POWERED DOWN ON THE GROUND AFTER LANDI NG SAFELY IN XNA. MAINTENANCE FOUND THE NR 1 INSTRUMENT CONSOLE COOLING FAN CONNECTOR WIRES BROKEN AND REPAIRED THE WIR ES. COOLING FAN OPERATIONAL CHECKS WERE NORMAL. MAINTENANCE RAN THE ENGINES AND SWAPPED BLEED SOURCES WITH NO EVIDENCE OF THE BURNED ODOR RETURNING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2003011000022 20030110 00022 SO 2003 1 10 ASOA02591 1 20021115 A 3350 1317 LIGHT EMB 120 EMB120ER 3260203 SO EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 504AS 120278 FLT 4998 - DURING GROUND INSPECTION AT DFW, THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAI NTENANCE REMOVED AND REPLACED THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FO R SERVICE. (M) 2 L 7 2 4T RT A31SO 2003011000023 20030110 00023 SO 2003 1 10 ASOA02592 1 20021116 A 2120 12011639001 CHECK VALVE EMB 120 EMB120ER 3260203 SO LT PACK STICKING A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 11 262AS 120146 FLT 4020 - DURING DESCENT INTO ATL, SMOKE OCCURRED IN THE CABIN AND COCKPIT. THE CREW COMPLIED WITH THE QRH AND THE SMO KE DISSIPATED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE FOUND THE LEFT PACK RAM AIR CHECK VALVE STICKING AND FRE ED THE FLAPPER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2003011000024 20030110 00024 EA 2003 1 10 ASOA02593 1 20021116 A 7830 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 844AS 7317 FLT 4403 - DURING CLIMB THROUGH 10,000 FEET FROM GRR-ATL, A RIGHT THRUST REVERSER UNLOCK MESSAGE OCCURRED AND AN EMERGEN CY WAS DECLARED. THE AIRCRAFT RETURNED TO GRR AND LANDED SAFELY. MAINTENANCE DEFERRED THE THRUST REVERSER SYSTEM IAW M EL NR 78-30-1. (M) 2 L 7 2 4F RT A21EA 2003011000025 20030110 00025 EU 2003 1 10 ASOA02594 1 20021117 A 3350 3012000 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 636AS 375 FLT 4154 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT OVER THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2003011000026 20030110 00026 NM 2003 1 10 C7WA200200032 1 20021019 A 2781 40141CMGJ POSITION SWITCH BOEING 727 727232 1384082 NM L/E SLAT FAILED A CYWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 17 511PE 20634 FLT 41 - DURING TAKEOFF AT 80 KNOTS, THE FORWARD LEADING EDGE INTRANSIT LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. REMOVE D AND REPLACED NR 8 LEADING EDGE SLAT POSITION SWITCH IAW MM 27-81-11. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 2003011000027 20030110 00027 NM 2003 1 10 C7WA200200033 1 20021022 A 2197 GROUND WIRE BOEING 727 727232 1384082 NM CABIN PRESSURE LOOSE A C7WA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 17 511PE 20634 CLIMBING THROUGH FL195 FOR FL280 CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE WAS AT 10.5. EMERGENCY DESCENT IN ITIATED AS PRESSURE COULD NOT BE MAINTAINED IN STANDBY, ONLY IN MANUAL DC. CABIN REACHED 12 BEFORE PRESSURE COULD BE CO NTROLLED MARGINALLY AT 8000 FEET. CABIN PRESSURE COULD NOT BE MAINTAINED IN ANY MODE. RESECURED LOOSE GROUND WIRE ON L EFT FLOW MODULATION CONTROL VALVE IAW MM 20-10-4. PRESSURIZED AIRCRAFT IN AUTO, STANDBY, AND MANUAL MODES. AIRCRAFT PR ESSURE NORMAL. (M) 2 L 7 3 4F A3WE 2003011000031 20030110 00031 EU 2003 1 10 02351311 1 20021217 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33112UHR WP CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 311UE 41029 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE AT SEAT ROWS 8 TO 10. MAINTENANCE PERSONNEL SECURED THE EMERGENCY FLOOR LIGHT STRIP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRC RAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A41NM E4WE 2003011000032 20030110 00032 EU 2003 1 10 02361303 1 20021227 A 3397 WIRE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE331* 01514 WP CABIN DAMAGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 303UE 41015 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CENTER SECTION OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE PER SONNEL REPAIRED WIRE ON CENTER SECTION OF FLOOR EMERGENCY LIGHTS. OPERATIONAL CHECK, GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4T 3 T RT A41NM E2WE 2003011000033 20030110 00033 NM 2003 1 10 02FDEA00972 1 20021227 A 5315 FLOORBEAM BOEING 727 7272S2F 1384O81 NM PWA JT8 JT8D17 52049 NE FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 212FE 22934 LONGITUDINAL FLOORBEAM OUTBOARD, LOWER FLANGE SIDE IS GOUGED JUST BELOW FASTENER HOLES BS 760-848, LBL 51, WL 208. LONG ITUDINAL FLOORBEAM, BS 760-848, FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED DAMAGED BEAM, FABRICATED, ALODINED, PRIMED A ND INSTALLED REPLACEMENT BEAM IAW SRM. 2 L 7 3 4F 4 F A3WE E2EA 2003011000034 20030110 00034 EU 2003 1 10 02FDEA00973 1 20021227 A 2611 SMOKE DETECTOR AIRBUS 310 A310203 3930313 EU GE CF6 CF680 30025 NE E/E BAY MALFUNCTIONED A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 404FE 233 AVIONICS SMOKE ECAM WARNING ON TAKEOFF. REJECTED AND PERFORMED ECAM AND AVIONICS SMOKE PROCEDURES, NO SNIFFER SMOKE DET ECTED, DID RTO CHECKLIST AND RETURNED TO GATE AVIONICS SMOKE WARNING CAME ON 2 MORE TIMES BEFORE BLOCKING IN. REMOVED AND REPLACED E/E SMOKE DETECTOR IAW AMM. OPS CHECK REF, ALL NORMAL. 2 L 7 2 4F 4 F RT A35EU E13NE 2003011000035 20030110 00035 NM 2003 1 10 02FDEA00974 1 20021226 A 5330 SKIN BOEING 727 727227 1384078 NM PWA JT8 JT8D1 52044 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 DENTS IN SKIN, BS 660 - 670, S22R. REPAIRED DENTS IN SKIN IAW SRM. 2 L 7 3 4F 4 F A3WE E2EA 2003011000036 20030110 00036 NM 2003 1 10 02FDEA00975 1 20021226 A 5330 SKIN BOEING 727 727200 138407E NM PWA JT8 JT8D1 52044 NE FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 FUSELAGE SKIN DAMAGED AT BS 1050, STR 19R, JUST BELOW THE LAP. REPAIRED SKIN IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2003011000046 20030110 00046 CE 2003 1 10 129JR120502 1 20021205 A 3210 LANDING GEAR LEAR 60 60LEAR 5170707 CE MAIN CONTAMINATED E AOQA I CABIN DEPRESSURIZATION O OTHER IN INSP/MAINT 1 EA 11 129JR 093 DURING GEAR RETRACTION, NOSE WHEEL UNSAFE LIGHT ILLUMINATED. INSPECTION WAS COMPLETED ON NOSE GEAR AND DOORS, NOSE GEAR UPLOCK, UPLOCK ACTUATORS AND SHUTTLE VALVE. NO DISCREPANCIES NOTED. GEAR OPERATIONAL CHECK ACCOMPLISHED, CYCLED 10 TI MES AND FOUND OPS CHECK GOOD. SUSPECT CAUSE TO BE RELATED TO AIRCRAFT BEING COLD SOAKED DUE TO WEATHER CONDITIONS. 2 L 7 2 4F RT A10CE 2003011000057 20030110 00057 EA 2003 1 10 A6WA200260078 2 20021223 A 7530 216118216 BLEED BAND BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA NR 2 ENGINE OUT OF TOLERANCE A A6WA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 31 616AW E3145 UPON APPLICATION OF TAKEOFF POWER, NR 2 ENGINE DID NOT RESPOND WHILE TGT WENT TO 950 DEGREES FOR AN ESTIMATED 5 SECONDS BEFORE SECURING. MAINTENANCE FOUND NR 2 ENGINE BLEED BAND OUT OF TOLERANCE. ADJUSTED AS REQUIRED AND PERFORMED 4 POINT RUN. ALL RUNS WITHIN PARAMETERS IAW MM. 2 H 7 4 4F 4 F RT A49EU E6NE 2003011000058 20030110 00058 NM 2003 1 10 AJN2002F00000 1 20021127 A 7500 652245320 DUCT BOEING 727 727200 138407E NM PWA JT8 JT8D17R 52049 NE NR 3 ENGINE CRACKED E AJNA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 11 906PG 20728 AIRCRAFT AIR RETURNED DUE TO NR 3 ENGINE FIRE WARNING ILLUMINATED ON TAKEOFF CLIMB. CREW COMPLETED CHECKLIST. LIGHT EX TINGUISHED AFTER NR 3 THROTTLE AT IDLE. MAINTENANCE FOUND NR 3 ENGINE 8TH STAGE DUCT CRACKED AND UPPER COWL DAMAGED. R EMOVED AND REPLACED NR 3 ENGINE 8TH STAGE DUCT IAW MM. LEAK CHECK GOOD ON ENGINE RUN. ACCOMPLISHED SRM REPAIR ON UPPER COWL IAW SRM. 2 L 7 3 4F 4 F RT A3WE E2EA 2003011000059 20030110 00059 SO 2003 1 10 BSY2003F00000 1 20021209 A 3234 487155 SOLENOID PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA GEAR HANDLE INOPERATIVE E BSYA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 4UE 318152061 AFTER TAKEOFF, GEAR HANDLE WOULD NOT GO UP. FOUND SOLENOID IN GEAR HANDLE, INOPERATIVE. REMOVE AND REPLACE SOLENOID IN GEAR HANDLE, CYCLED GEAR OPS CHECK GOOD 1 L 7 2 3O 3 O A20SO E14EA 2003011000060 20030110 00060 CE 2003 1 10 BSY2003F00001 1 20021209 A 3260 BEPBA07GBP BULB LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP COCKPIT INOPERATIVE E BSYA O OTHER N FALSE WARNING LD LANDING 1 GL 07 51LC 302 LT MAIN GEAR DOWN AND LOCK LIGHT INOPERATIVE. CHECKED WITH TOWER FOR LANDING LIGHTS BEING ON. LANDED NO PROBLEM. REMO VED AND REPLACED BULB, OPS CHECK GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2003011000062 20030110 00062 NM 2003 1 10 C7WA200200035 1 20021019 A 5340 FITTING BOEING 727 72731 1384010 NM PWA JT8 JT8D1 52044 NE FUSELAGE CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 220NE 18905 DURING CPCP INSPECTION WITH JOB CARD C5322401 FOUND 8 INCH CRACK IN MAIN DECK HORIZONTAL FITTING BETWEEN BS 930 AND BS 9 50 AT STR 14L. C/A: REMOVED AND REPLACED HORIZONTAL FITTING AT STRINGER 14L. BETWEEN BS 930 AND BS 950 IAW SRM. 2 L 7 3 4F 4 F A3WE E2EA 2003011000064 20030110 00064 CE 2003 1 10 CNQ2003F00000 1 20021206 A 2910 AE1011923H0152 HOSE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL HP HYD SYS RUPTURED B A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 05 915QS 2978 7500015 ON CLIMB OUT, HYDRAULIC SYSTEM (A) LOST ALL FLUID. UPON INSPECTION THE HOSE THT RUNS FROM SYSTEM (A) PRESSURE FILTER TO POWER TRANSFER UNIT WAS NOTED TO BE REPTURED. THE HOLE WAS SENT TO TEAM (X) AT ICT. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2003011000065 20030110 00065 CE 2003 1 10 CVM2003F00000 1 20021127 A 2620 CONNECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP EXTINGUISHING SY MISINSTALLED E CVMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 05 799S 258588 UPON COMPLETION OF INSPECTION E1 OF FLEXIBLE MAINTENANCE SCHEDULE FOR THE FUNCTIONAL TEST OF MAIN ENGINE FIRE EXTINGUISH ERS THE TECH NOTICED THAT THE WIRING INSTALLATION WAS INCORRECT. FOUND CONNECTOR PLUGS ON NR 2 (GJ) HEAD (A) AND (B) IN OPPOSITE POSITIONS. REROUTED WIRE HARNESS TO ALLOW FOR CORRECT WIRE HARNESS TO ALLOW FOR CORRECT WIRE ROUTING OF ENG 2 : SHOT 1 CIRCUIT TO REACH HEAD (B), ALSO WIRED ENG 1: SHOT 2 TO HEAD A. OPS CHECK GOOD, NOTED THAT NONE OF THE CORRE CTOR CONNECTION. 2 L 7 2 4F 4 F RT A3EU E6WE 2003011000066 20030110 00066 EU 2003 1 10 EHA2003F00000 1 20020824 A 2435 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE STARTER GEN FAILED B EHAR O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 AL 03 353EV 254 105 2444 9109 DURING RETURN FLIGHT, THE GENERATOR MASTER CAUTION LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO BASE. UPON INSPECTION IT WAS FOUND THAT THE STARTER GENERATOR FORWARD BEARINGS HAD FAILED. THE BEARINGS ON THIS STARTER/GEN ARE ADDRESSED UND ER SB. THIS SB HAD BEEN COMPLECTED IN CONJUNCTION WITH A FULL OVERHAUL, THIS UNIT HAD A TSO OF 254.9 HOURS. THE ALTERN ATE PN WAS INSTALLED, AND IS AWAITING MAINTENANCE OPERATIONAL CHECK BEFORE A RETURN TO SERVICE IS ISSUED. 1 G 7 1 3U 3 U H9EU E19EU 2003011000067 20030110 00067 NM 2003 1 10 AWXA200300025 1 20021231 A 5315 657N3311 INTERCOSTAL BOEING 757 7572G7 1384963 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 0 0 24523 LCQ - MAJOR REPAIR - DURING C-10 CHECK A 1" CRACK WAS FOUND ON MAIN CABIN INTERCOSTAL AT BS 1620, LBL 45. MAINTENANCE CU TOUT CRACKED SECTION ON MAIN CABIN INTERCOSTAL BETWEEN BS 1620 TO BS 1640, LBL 45; FABRICATED A REPAIR DOUBLER AND FILLE R; AND INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-13, PG. 1-2. 2 L 7 2 4F RT A2NM 2003011300001 20030113 00001 GL 2003 1 13 EOO2002F0000A 2 20020822 A 7240 6870992 COMBUST CHAMBER DOUG DC3 DC3DR183090C 3021470 WP ALLSN 250C 250C20B 03013 GL ENGINE CRACKED B EOOG A UNSCHED LANDING M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 AL 03 C6PHC 180257D AIRCRAFT SUDDENLY STARTED TO RUN HOT, SUBSEQUENT POWER CHECK SHOWED ENGINE RUNNING 75 DEGREE C, HOTTER THAN PREVIOUS POW ER CHECK TWO DAYS BEFORE. AIRCRAFT LANDED AND ON INSPECTION IT WAS FOUND THAT THE OUTER COMBUSTION CAN WAS CRACKED IN T HE ARMPIT AREA. 2 L 7 2 4R 3 U A669 E4CE 2003011300002 20030113 00002 CE 2003 1 13 FFS2002F00009 1 20021214 A 2497 11498003321 LEAD BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT NACELLE CHAFED A FFSA K NONE N FALSE WARNING IN INSP/MAINT 1 AL 01 575D UE24 EXTERNAL POWER ANNUNCIATOR WOULD NOT EXTINGUISH. FOUND AFT STIFFENER IN LT NACELLE AFT SKIN, HAD CHAFED THRU INSULATION ON ELECTRICAL LEADS THAT GO FROM THE EXTERNAL POWER RECEPTACLE IN THE WHEEL WELL, TO THE EXTERNAL POWER RELAY IN THE LT NACELLE. THIS CAUSED THESE LARGE (6 OR 8 GAUGE) WIRES TO BE GROUNDED TO THE AIRFRAME. REROUTING OR BETTER ANTI-CHAFE PROTECTION. POTENTIAL FOR FIRE OR SEVERE ELECTRICAL PROBLEMS. 2 L 7 2 4T 3 T RT A24CE E2NE 2003011300003 20030113 00003 CE 2003 1 13 FFS2003F00000 1 20020730 A 5260 1145140309 CABLE BEECH 1900 1900C 1154161 CE PWA PT6 PT6* 52043 EA AIRSTAIR DOOR FRAYED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 575Q UC160 AIRSTAIR DOOR LATCH CABLE FRAYED. 2 L 7 2 4T 3 T RT A24CE E2NE 2003011300004 20030113 00004 CE 2003 1 13 FFS2003F00001 1 20020726 A 5260 11451403013 CABLE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA AIRSTAIR DOOR FRAYED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 575A UC83 AIRSTAIR DOOR LATCH CABLE FOUND FRAYED DURING INSPECTION. 2 L 7 2 4T 4 T RT A24CE E4EA 2003011300005 20030113 00005 CE 2003 1 13 FFS2003F00002 1 20021003 A 5260 11451403013 CABLE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA AIRSTAIR DOOR FRAYED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 575P UC95 AIRSTAIR DOOR LATCH CABLE FRAYED. 2 L 7 2 4T 4 T RT A24CE E4EA 2003011300006 20030113 00006 CE 2003 1 13 FFS2003F00003 1 20021018 A 5260 11451403017 CABLE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA AIRSTAIR DOOR FRAYED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 575P UC95 AIRSTAIR DOOR LATCH CABLE FOUND FRAYED/DAMAGED DURING INSPECTION. 2 L 7 2 4T 4 T RT A24CE E4EA 2003011300007 20030113 00007 CE 2003 1 13 FFS2003F00004 1 20021101 A 5260 11454103013 CABLE BEECH 1900 1900C 1154161 CE PWA PT6 PT6* 52043 EA AIRSTAIR DOOR FRAYED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 575Q UC160 AIRSTAIR DOOR WOULD NOT OPEN. BROKEN CABLE PREVENTED LATCHES FROM ROTATING. 2 L 7 2 4T 3 T RT A24CE E2NE 2003011300008 20030113 00008 CE 2003 1 13 FPI2003F00000 1 20021216 A 2910 128050989 LINE CESSNA 210 210M 2073450 CE CONT O520 IO520* 17032 SO NLG HYD SYS CHAFED E FPIA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 15 7660E 7626 21062692 LANDING GEAR DOWN LINE CHAFED THRU BY AILERON RUDDER INTERCONNECT CABLE. WHEN SELECTING DOWN, ALL FLUID WAS PUMPED OUT OF SYSTEM. NOSE GEAR CAME DOWN AND LOCKED, MAIN GEAR DID NOT. 1 H 7 1 3O 3 O 3A21 E5CE 2003011300009 20030113 00009 EA 2003 1 13 FTU2003F00000 2 20021219 A 8510 LW11147 BRACKET GULSTM 500 500S 0141107 SW LYC O540 IO540* 41532 EA ALTERNATOR BROKEN B FTUR K NONE O OTHER IN INSP/MAINT 1 NE 05 1938S 3167 DURING ANNUAL INSPECTION AND REMOVAL OF ENGINE FOR OVERHAUL, ALTERNATOR BELT TENSION BRACKET WAS FOUND BROKEN AT THE END THAT IS BOLTED TO THE ENGINE NOSE CASE. ON THIS INSTALLATION A VIEW OF THAT TEND OF THE BRACKET IS VERY DIFFICULT TO S EE, WHEN THE BRACKET WAS DISCONNECTED FROM THE ALTERNATOR END, IT BECAME VERY APPARENT THE PART WAS BROKEN. 1 H 7 2 3O 3 O 6A1 1E4 2003011300010 20030113 00010 SO 2003 1 13 FTU2003F00001 1 20021219 A 3246 16106900 WHEEL PIPER PA23 PA23250 7102308 SO LYC O540 TIO540* 41532 EA RT MLG CRACKED B FTUR O OTHER O OTHER NR NOT REPORTED 1 NE 05 327DR 277654080 WHEEL HAD AN APPARENT CRACK, AT RIVET TO BRAKE DISC AREA PRIOR TO FAILURE. PILOT REPORTED A SIDE SKID DURING TAKEOFF, T HAT COULD HAVE CAUSED A SECTION OF THE WHEEL FLANGE TO BREAK OFF THE INBOARD WHEEL HALF. SECTION WAS MISSING AT THE TIR E BEAD AREA. 1 L 7 2 3O 3 O 1A10 E14EA 2003011300011 20030113 00011 SO 2003 1 13 FXGA030A 1 20021211 A 3233 AN311A BOLT PIPER PA32 PA32R300 7103213 SO LYC O540 TIO540* 41532 EA NLG ACTUATOR FAILED E FXGA O OTHER N FALSE WARNING NR NOT REPORTED 1 AL 01 108NS 32R7680288 AIRCRAFT GEAR UNSAFE LIGHT STAYED ON IN FLIGHT WITH GEAR IN THE UP POSITION. UPON INSPECTION THE AFT BOLT TO THE NOSE G EAR ACTUATOR WAS FOUND TO BE BROKEN. A NEW BOLT WAS INSTALLED AND A GEAR FUNCTION TEST WAS PERFORMED WITH NO DEFECTS. AN INSPECTION AT EACH 100 HOUR OR ANNUAL TO REMOVE THE BOLT FOR A MORE DETAILED INSPECTION FOR DEFECTS MIGHT DETECT PROB LEMS BEFORE THEY START. IT IS POSSIBLE THAT THE NOSE GEAR COULD FAIL TO COME DOWN AND INTO THE LOCKED POSITION CAUSING THE NOSE GEAR TO FAIL WHILE ON THE GROUND. 1 L 7 1 3O 3 O A3SO E14EA 2003011300012 20030113 00012 CE 2003 1 13 G4V2003F00000 1 20021211 A 3201 071333421 FAIRING CESSNA 182 T182 2072736 CE LYC O540 TIO540* 41532 EA NLG MISINSTALLED B G4VE O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 07 5253L T18208169 AFT NOSE GEAR FAIRING APPEARED TO BE INSTALLED INCORRECTLY ALLOWING IT TO BE HIGHER THAN THE FORWARD NOSE GEAR FAIRING, CAUSING IT TO ACT AS AN AIR SCOOP, AIR LOADS WERE TRYING TO PULL THE FAIRING OFF THE AIRCRAFT, CAUSING THE BELLY SKIN TO CRACK. 1 L 7 1 3O 3 O 3A13 E14EA 2003011300013 20030113 00013 CE 2003 1 13 G4V2003F00001 1 20021211 A 3201 FAIRING CESSNA 182 T182 2072736 CE LYC O540 TIO540* 41532 EA NLG MISINSTALLED B G4VE O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 07 52977 16 T18208183 AFT NOSE GEAR FAIRING APPEARED TO BE INSTALLED INCORRECTLY, ALLOWING IT TO BE HIGHER THAN THE FORWARD NOSE GEAR FAIRING AND CAUSING IT TO ACT AS AN AIR SCOOP, AIR LOADS WERE TRYING TO PULL THE FAIRING OFF THE AIRCRAFT, CAUSING THE BELLY SK IN TO CRACK. 1 L 7 1 3O 3 O 3A13 E14EA 2003011300014 20030113 00014 NM 2003 1 13 GAIA02166OP 1 20021220 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM PWA JT8 JT8D9 52048 NE COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6806 19481 DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLAC ED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2003011300015 20030113 00015 EU 2003 1 13 GJQ2002F00004 1 20021118 A 3397 WIRE AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE73140 29001 NE LANDING LIGHT SHORTED B GJQR K NONE L NO TEST IN INSP/MAINT 1 NM 01 39WP 1535 294 AIRCRAFT RETURNED WITH RT LANDING LIGHT INOPERATIVE. INVESTIGATION REVEALED OPEN CIRCUIT IN WIRING. DISCOVERED TERMINA L BURNED AND OVERHEATED AT TERMINAL JUNCTION. SUSPECT HIGH RESISTANCE AT TERMINAL JUNCTION. 2 L 7 3 4F 4 F A46EU E1NM 2003011300016 20030113 00016 EU 2003 1 13 GQU2002F00000 1 20021210 A 2435 BEARING BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE731* 01518 WP STARTER GEN FAILED E GQUA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 05 403DP 867 96050 NA0281 AIRCRAFT DEPARTED FOR FLIGHT AND NOTICED A VIBRATION COMING THROUGH THE AIRCRAFT. THE PILOT RETARDED THE RT ENGINE POWE R LEVER AND VIBRATION WENT AWAY. PILOT THEN TURNED THE AIRCRAFT BACK WHERE THE AIRCRAFT LANDED AND MAINTENANCE PERSONNE L TROUBLESHOT THE PROBLEM. THE RT STARTER GENERATOR WAS SUBSEQUENTLY REMOVED AND AN OVERHAULED GENERATOR WAS INSTALLED. 2 L 7 2 4F 4 F A3EU E6WE 2003011300017 20030113 00017 NE 2003 1 13 GTIA021242 2 20021202 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217A 52053 NE NR 1 VIBRATION A GTIA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 23 806NK 48051 708450 DURING CRUISE, A STRONG VIBRATION NOTICED AND ERRATIC EPR AND OIL QUANTITY. HIGH OIL TEMPERATURE, REDUCED LT THROTTLE A ND VIBRATION SUBSIDED BUT DID NOT GO AWAY. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AND LANDING. REPLACED NR 1 ENGINE IAW MM. OPS CHECK GOOD ON ENGINE RUN. 2 L 7 2 4F 4 F A6WE E9NE 2003011300018 20030113 00018 WP 2003 1 13 GTIA021243 1 20021208 A 5330 SKIN DOUG DC9 DC981 3022081 WP PWA JT8 JT8D NE FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 2.250 INCH CRACK ON AIRCRAFT RT SIDE, JUST AFT OF ELEVATOR ACCUMULATOR ACCESS DOOR. (UNPRESSURIZED AREA) TRANSFERRED T O COI, REPAIRED WITHIN 10 DAYS. 2 L 7 2 4F 4 F A6WE E2EA 2003011300019 20030113 00019 NM 2003 1 13 GTIA021247 1 20021129 A 5320 INTERCOSTAL DOUG MD80 MD83 3023681 NM PWA JT8 JT8D NE FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 AFT CARGO BAY HAS A CRACKED FLOORBEAM INTERCOSTAL AT FS 1287-1309 (IN OVERHEAD). REMOVED INTERCOSTAL. FABRICATED NEW I NTERCOSTAL. AND INSTALLED. 2 L 7 2 4F 4 F RT E2EA 2003011300020 20030113 00020 NM 2003 1 13 GTIA021248 1 20021210 A 5320 INTERCOSTAL DOUG MD80 MD83 3023681 NM PWA JT8 JT8D NE FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 AFT CARGO PIT CRACKED FLOORBEAM INTERCOSTAL FS 1271-1287 OBL (IN OVERHEAD). REMOVED INTERCOSTAL. FABRICATED NEW INTER COSTAL AND INSTALLED. 2 L 7 2 4F 4 F RT E2EA 2003011300021 20030113 00021 NM 2003 1 13 GTIA021249 1 20021203 A 5320 ATTACH FITTING DOUG MD80 MD83 3023681 NM PWA JT8 JT8D NE INTERCOSTAL CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 AFT FUSELAGE LT SIDE IS CRACKED AT INTERCOSTAL ATTACH TO 1510 CANT, 1497 CANT. REMOVED DAMAGED INTERCOSTAL. FABRICATED REPAIR PART AND INSTALLED. 2 L 7 2 4F 4 F RT E2EA 2003011300022 20030113 00022 NM 2003 1 13 GTIA021250 1 20021126 A 5730 PANEL DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE WING LE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 LT LEADING EDGE PANEL NR 1168C HAS BARE METAL, CORRODED. MATERIAL LOSS IS OUT OF LIMITS, FABRICATED NEW LT LEADING EDGE PANEL. 2 L 7 2 4F 4 F RT E2EA 2003011300023 20030113 00023 NM 2003 1 13 GTIA021251 1 20021210 A 7120 K22199SA31 ISOLATOR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE RT ENGINE MISINSTALLED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 822NK 49392 RT LOWER FORWARD VIBRATION ISOLATOR MARKS MISALIGNED. REMOVED RT ENGINE LOWER FORWARD VIBRATION ISOLATOR. REPLACED RT ENGINE LOWER FORWARD VIBRATION ISOLATOR. 2 L 7 2 4F 4 F RT E2EA 2003011300024 20030113 00024 NM 2003 1 13 GTIA021252 1 20021124 A 7120 K22199SA31 ISOLATOR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE ENGINE MISALIGNED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 LT LOWER FORWARD VIBRATION ISOLATOR MARKS MISALIGNED. REMOVED LT LOWER FORWARD VIBRATION ISOLATOR. INSTALLED LT LOWER FORWARD VIBRATION ISOLATOR. 2 L 7 2 4F 4 F RT E2EA 2003011300025 20030113 00025 NM 2003 1 13 GTIA0221246 1 20021127 A 5320 ANGLE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D NE CARGO BAY CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 MID CARGO BAY HAS A CRACKED VERTICAL ANGLE, LT LOWER END OF FS 522 LONGERON 23 LT. REMOVED VERTICAL ANGLE. FABRICATED NEW VERTICAL ANGLE AND INSTALLED. 2 L 7 2 4F 4 F RT E2EA 2003011300026 20030113 00026 SW 2003 1 13 GXP2002F00006 1 20021204 A 3297 WIRE SWRNGN SA226 SA226TC 8780404 SW RT MLG BROKEN E GXPA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 164GA TC281 RT MLG INDICATION SHOWED IN TRANSIT (RED). ATTEMPTED EMERGENCY EXTENSION AND ALTERNATE PROCEDURE WITH NO CHANGE. REPA IRED BROKEN WIRE ON RT MLG UP SWITCH, OPS CHECKED GOOD. 2 L 7 2 4T RT A8SW 2003011300027 20030113 00027 WP 2003 1 13 HXS2003F00000 1 20021220 A 6320 369D25100901 TRANSMISSION HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL MAIN ROTOR MAKING METAL B HXSR K NONE O OTHER IN INSP/MAINT 1 AL 05 1107P 792 210897D 833545 MAIN ROTOR TRANSMISSION, MAKING METAL. 1 G 7 1 3U 3 U H3WE E4CE 2003011300028 20030113 00028 SO 2003 1 13 HYTA2002001 1 20021216 A 5320 40987002 CHANNEL PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA NLG WW CRACKED D HYTA K NONE O OTHER IN INSP/MAINT 1 AL 01 54WA 317652067 PART SITS ON TOP OF NLG TUNNEL AND IS PART OF THE GEAR ACTUATOR ATTACH POINT. IT ALSO HAD A TWIST IN IT, PROBABLY FROM STRESS FROM THE ACTUATOR. 1 L 7 2 3O 3 O A20SO E14EA 2003011300029 20030113 00029 2003 1 13 I122003F00000 4 20021122 A 3415 DRA76C14 SWITCH LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP MACH OVERSPEED FAILED B I12R K NONE L NO TEST IN INSP/MAINT 1 EA 23 971K 373 MACH OVERSPEED SWITCH FAILED DURING FUNCTIONAL TEST. 2 L 7 2 4F 4 F A10CE E6WE 2003011300030 20030113 00030 GL 2003 1 13 IBU2003F00000 2 20021227 A 7323 252469011 GOVERNOR BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL ENGINE FAILED E IBUA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 07 203M 51365 GOVERNOR FAILED CAUSING ENGINE RPM, TORQUE, TOT. TO NOT REMAIN STABLE. FLUCTUATION OF RPM WERE SEVERE ENOUGH TO CAUSE AIRCRAFT TO YAW LT AND RT WITH INCREASE AND DECREASE OF RPM. 1 G 7 1 3U 3 U H2SW E1GL 2003011300031 20030113 00031 WP 2003 1 13 IZ22003F00000 2 20021218 A 7321 89777026 FUEL CONTROL MTSBSI MU2 MU2B26A 5780414 CE GARRTT TPE331 TPE331* 01514 WP RT ENGINE OVERTORQUED B IZ2R E A ENGINE SHUTDOWN UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 15 82WC 393SA ON CLIMBOUT AT 15,000 FT, THE RT ENGINE EXPERIENCED AN OVERTORQUE CONDITION WITH NO SUBSEQUENT RESPONSE TO POWER LEVER M OVEMENT. ENGINE WAS IMMEDIATELY SHUTDOWN AND A SINGLE ENGINE LANDING WAS MADE. FUEL CONTROL WAS REPLACED BEFORE FURTHER FLIGHTS. 1 H 7 2 3T 3 T RT A10SW E2WE 2003011300032 20030113 00032 NE 2003 1 13 KCS2003F00001 2 20020326 A 7230 BLADE BOEING 747 747146 1384905 NM PWA JT9 JT9D7A 52054 NE COMPRESSOR DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 ON POST FLIGHT INSPECTION, FOUND NR 1, 2, 3, AND 4 ENGINES HAD EVIDENCE OF C-1 BLADE DAMAGE. REMOVED ALL DAMAGED C-1 (N 1) BLADES AND INSTALLED MATCHED SET OF C-1 BLADES ON ALL 4 ENGINES IAW MM AND ACCOMPLISHED FOD DAMAGE INSPECTION AND FOU ND NO DEFECTS IAW MM. 2 L 7 4 4F 4 F RT A20WE E20EA 2003011300033 20030113 00033 SO 2003 1 13 MA2982323 1 20021217 A 5620 GASKET GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE WINDOW DAMAGED B BTVR K NONE O OTHER IN INSP/MAINT 1 GL 23 502KA 3084 502 DURING MAINTENANCE, CABIN CARPET AND PADDING WAS FOUND TO BE WATER SOAKED. AFTER REMOVAL, SEVERE CORROSION WAS FOUND ON THE SEAT TRACKS IN THE PRESSURE BOARD AREA BETWEEN FS 426-576.5 AT LBL 30.5, LBL AND RBL 18.5 AND ALSO LBL 6.0. STRUCT URAL EVALUATION DETERMINED THAT ALL FOUR SECTIONS OF SEAT TRACK REQUIRED REPLACEMENT. SOURCE OF WATER INTRUSION WAS DET ERMINED TO BE FROM ALL 12 CABIN WINDOWS LEAKING DURING AN UNPRESSURIZED CONDITION. FORM IN PLACE SEALS WERE REMOVED AND REPLACED ON ALL CABIN WINDOWS. DETAILED INSP OF CABIN INTERIOR STRUCTURE FROM BELOW CABIN WINDOWS TO BL 0.0 REVEALED N O CORROSION OR DAMAGE OTHER THAN THAT NOTED ON THE SEAT TRACKS. 2 L 7 2 4F 4 F RT A12EA E00057EN 2003011300034 20030113 00034 WP 2003 1 13 MEX2002363 1 20021215 A 2910 79182825001 CHECK VALVE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE HYD SYSTEM FAILED W ASMF O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 23 838AM 49397 AIRCRAFT RETURN TO PLATFORM DUE TO A LT HYD SYSTEM LEAK. DURING CHECK, DETECTED DAMAGE TO THE CHECK VALVE. A LINE WAS INSTALLED AT THE FLUID QUANTITY LIMITER OF BRAKE NR 1, LEAK CHECKED IAW MM. DURING OVERNIGHT SERVICE, LINE WAS REMOVED AND CHECK VALVE WAS INSTALLED IAW MM, TESTS OK. 2 L 7 2 4F 4 F RT A6WE E2EA 2003011300035 20030113 00035 2003 1 13 MEX2002367 4 20021218 A 3414 4038891903 INDICATOR BOEING 757 7572Q8 1384972 NM MACH AIRSPEED FAILED W ASMF A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 23 806AM 3678 26273 AIRCRAFT RETURNED DUE TO FIRST OFFICER AIRSPEED INDICATOR OUT OF SERVICE, CAPTAIN PERFORMED ABNORMAL PROCEDURES AND FAIL CONTINUED DURING DESCENT, AIRSPEED INDICATOR STARTED FUNCTIONING AND WARNING INDICATIONS STOPPED. FIRST OFFICER AIRSP EED INDICATOR AND CADC WERE REPLACED IAW MM, ALL CORRECT. 2 L 7 2 4F RT A2NM 2003011300036 20030113 00036 WP 2003 1 13 MEX2002368 1 20021219 A 3246 BEARING DOUG DC9 DC9* WP PWA JT8 JT8D NE NLG WHEEL DAMAGED W ASMF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 23 501AM 49188 AIRCRAFT RETURN TO PLATFORM DUE TO A NOISE IN NOSE NLG BEARINGS. WHEELS AND NOSE LANDING GEAR WERE CHECKED FOR GENERAL CONDITION, ALL CORRECT. AIRCRAFT WAS TAXED TO CONFIRM THE NOISE ON NLG WHEELS. BOTH WHEELS WERE REPLACED IAW MM. 2 L 7 2 4F 4 F A6WE E2EA 2003011300037 20030113 00037 NM 2003 1 13 MEX2002375 1 20021222 A 2420 696233B CSD DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE LEFT DAMAGED W ASMF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 23 168PL 26986 53174 AIRCRAFT RETURN FROM FLIGHT, DURING CLIMB, LT CSD OIL PRESSURE AND LT GENERATOR OFF LIGHTS ILLUMINATED WITH INDICATION S GEN 0 AND NORMAL CSD TEMPERATURE. DURING CHECK CSD WAS WITHOUT OIL AND PLUNGER ACTIVATED. DURING CSD REPLACEMENT IT WAS DETECTED THAT THE CSD AND GENERATOR WERE DAMAGED. THEY WERE REPLACED IAW MM, TESTS OK. ADDITIONALLY DURING OVERNIG HT SERVICE THE APU WAS INSTALLED IAW MM. 2 L 7 2 4F 4 F RT A6WE E2EA 2003011300038 20030113 00038 NM 2003 1 13 0204236740 1 20021216 A 5412 BULKHEAD BOEING 747 747251F 1384898 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 During "L" check found crack on number 4 pylon torque bulkhead. Repaired per EA 67-193401. 2 L 7 4 4F A20WE 2003011300041 20030113 00041 WP 2003 1 13 IXXA0200142S 1 20021014 A 5700 WING DOUG DC8 DC871F 302199D WP LEFT UPPER LE CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 2906 45811 DURING ROUTINE C CHECK INSPECTION, CRACKS WERE DETECTED JUST OUTBOARD OF THE INBOARD STUB WING AREA ON THE LEFT WING UPP ER LEADING EDGE. REPAIRED ACCOMPLISHED REMOVAL OF DAMAGED AREA FABRICATION AND INSTALLATION REPAIR OF DOULBER IN ACCORDA NCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2003011300042 20030113 00042 WP 2003 1 13 IXXA0200143S 1 20021014 A 5700 WING DOUG DC8 DC871F 302199D WP LT WING LOWER LE CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 2906 45811 DURING ROUTINE C CHECK INSPECTION A CRACK WAS DETECTED ADJACENT TO THE INBOARD FIRE BOTTLE VIEWING DOOR ON LEFT WING LOW ER LEADING EDGE. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANC E WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER R74-R02-IR 2 L 7 4 4F RT 4A25 2003011300043 20030113 00043 CE 2003 1 13 AHQA055N 1 20021227 A 3520 C3512000 OXYGEN MASK CESSNA 500 S550 2076607 CE PWA JT15 JT15D4 52112 NE CABIN TORN B AHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 598WC S5500098 AT COMPLIANCE WITH AD DISCOVERED TWO O2 MASKS CONTAINED TEARS IN THE FACE CUSHION. 1 L 7 2 4F 4 F RT A22CE E1NE 2003011300044 20030113 00044 CE 2003 1 13 N3F2003F00000 1 20021209 A 2820 LINE BBAVIA 8 8KCAB 2110612 CE FUEL SYS HEADER LEAKING A N3FA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 11 28YH 28 8982002 AIRCRAFT FORMED FUEL LEAKS WITHIN 28.8 HOURS OF SERVICE. THIS AIRCRAFT WAS BROUGHT IN FOR SERVICE WHEN THE PILOT REPORT ED FUEL LEAKING FROM THE INVERTED FUEL SYSTEM HEADER TANK ONTO HIS LEGS AND FEET. PERFORMING A VISUAL INSPECTION OF THE SYSTEM SIX FUEL LEAKS AND IMPROPER FLARING ON THE INVERTED FUEL SYSTEM .3750 ALUMINUM LINES. 1 H 7 1 3O A21CE 2003011300046 20030113 00046 NM 2003 1 13 ASAA0210255 1 20021023 A 1420 07912 SPLICE BOEING 737 7372Q8C 138448S NM CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 16 WERE INOPERATIVE. REPAIRED WIRE SPLICE AT ROW 16 LIGHT ASSEMBLY. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2003011300047 20030113 00047 NM 2003 1 13 ASAA0210256 1 20021024 A 3350 86210144 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY LIGHT PACK INOPERATIVE AT ROW 8. REMOVED AND REPLACED THE BATTERY PACK. THE EMERGENCY LIGHT PACK THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2003011300048 20030113 00048 WP 2003 1 13 ASAA0280516 1 20021102 A 3397 0105606 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 PDX - DURING PREFLIGHT CHECK, ONE EMERGENCY TRACK LIGHT AT THE OVERWING EMERGENCY EXIT WAS FOUND TO BE INOPERATIVE. REP AIRED BROKEN WIRE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2003011300049 20030113 00049 WP 2003 1 13 ASAA0280524 1 20021104 A 5311 9707976 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OAK - FOUND C-CHECK, AFT SIDE OF CIRCUMFERENTIAL FRAME IS CORRODED AT FS 588 BETWEEN LONGERON 28R AND 28L. REPAIRED WIT H DOUBLER PER SRM 53-01, 53-03, 51-10-3, AND 51-10-3B. (M) 2 L 7 2 4F RT A6WE 2003011300050 20030113 00050 WP 2003 1 13 ASAA0280525 1 20021104 A 5320 SR0953013713 SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OAK - FOUND ON C-CHECK, SPLICE CORRODED AT FS 1117-1136 ON LONGERON 30. REPLACED SPLICE PER SRM 53-01, 53-02, 51-10-3, 51-10-3B, AND 51-30-1. (M) 2 L 7 2 4F RT A6WE 2003011300051 20030113 00051 WP 2003 1 13 ASAA0280526 1 20021108 A 5320 DOUBLER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OAK - FOUND C-CHECK, HORIZONTAL FLANGE UNDER AFT CARGO BAY DOOR BEAM DOUBLER IS CORRODED. REPLACED PREVIOUS DOUBLER AND SPACER PER EA 5310-02130. (M) 2 L 7 2 4F RT A6WE 2003011300052 20030113 00052 WP 2003 1 13 ASAA0280527 1 20021106 A 5347 5936663503 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OAK - FOUND C-CHECK, AFT CARGO BAY LEFT TIEDOWN TRACK IS CORRODED FROM FS 1212 TO 1338. REPLACED TIEDOWN TRACK PER SRM 51-10-4 AND 51-30-0. (M) 2 L 7 2 4F RT A6WE 2003011300053 20030113 00053 WP 2003 1 13 ASAA0280528 1 20021106 A 5347 5936663503 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OAK - FOUND C-CHECK, AFT CARGO BAY LEFT TIEDOWN TRACK IS CORRODED FROM FS 1212 TO 1338 AT LONGERON 27L. REPLACED TIEDOW N TRACK PER SRM 51-10-4 AND 51-30-0. (M) 2 L 7 2 4F RT A6WE 2003011300054 20030113 00054 WP 2003 1 13 ASAA0280531 1 20021109 A 5320 593607111 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, INTERCOSTAL CORRODED AT FS 1155 BETWEEN LONGERON 29R AND 30. REPLACED INTERCOSTAL PER SRM 51-10- 2, 51-10-4, 51-30-5, AND DAC DWG 5936071. (M) 2 L 7 2 4F RT A6WE 2003011300055 20030113 00055 WP 2003 1 13 ASAA0280535 1 20021109 A 5311 993648723 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, FRAME WEB CORRODED AT FS 1022 BETWEEN LONGERON 29R AND 30. REPLACED SHEAR CLIP AND REPAIRED PER BAC TLX AOC-OKC-02-0012OH, EA 5310-02138 (AAR EA 13-53-EA078). (M) 2 L 7 2 4F RT A6WE 2003011300057 20030113 00057 WP 2003 1 13 ASAA0280536 1 20021109 A 5320 995782821 PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, TRANSITION PANEL INBOARD OF R-1, RIGHT FORWARD SERVICE, DOOR IS CORRODED AT FS 160-200. REPLACED TRANSITION PANEL PER SRM 51-10-5, 51-10-4 AND DAC DWG 9957828. (M) 2 L 7 2 4F RT A6WE 2003011300058 20030113 00058 WP 2003 1 13 ASAA0280537 1 20021109 A 5347 SR095301157003 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, SEAT TRACK FOUND CORRODED AT FS 562, RBL 44. REMOVED CORRODED SECTION. SPLICED IN REPLACEMENT S ECTION PER SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2003011300059 20030113 00059 WP 2003 1 13 ASAA0280538 1 20021109 A 5347 SR095301157003 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, FOUND SEAT TRACK CORRODED AT FS 235-237, RBL 44. REMOVED CORRODED SECTION. SPLICED IN REPLACEME NT PER SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2003011300060 20030113 00060 WP 2003 1 13 ASAA0280541 1 20021109 A 5311 59624501 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, FRAME CORRODED ON AFT SIDE AT FS 1079 BETWEEN LONGERON 29L AND 29R. REPAIRED WITH SPLICE PER BAC TLX AOC-OKC-02-0091H, EA 5310-01232 (AAR EA 13-53-EA072). (M) 2 L 7 2 4F RT A6WE 2003011300061 20030113 00061 WP 2003 1 13 ASAA0280542 1 20021109 A 5330 593602229 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, SKIN CORRODED ON INNER SURFACE AT FS 1060-1079, LONGERON 29L-29R. REMOVED CORROSION AND REPAIRED PER BAC TLX AOC-OKC-02-0088H AND EA 5330-01609. (M) 2 L 7 2 4F RT A6WE 2003011300062 20030113 00062 WP 2003 1 13 ASAA0280552 1 20021110 A 5310 5936064 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, UPPER SHEAR TIE CORRODED AT FS 1212, LONGERON 28R. REPLACED SHEAR TIE PER SRM 53-24-0, 51-10-2, 51-10-4, AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003011300063 20030113 00063 WP 2003 1 13 ASAA0280559 1 20021111 A 5313 5936037501 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND LONGERON 29R IS CORRODED IN RADIUS AT FS 1180.25-1183. BLENDED AREA PER BAC TLX AOC-OKC-02-0086H AND EA 531 0-02134. (M) 2 L 7 2 4F RT A6WE 2003011300064 20030113 00064 WP 2003 1 13 ASAA0280560 1 20021111 A 5347 593054767 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, LEFT INBOARD SEAT TRACK IS CORRODED AT FS 574-598, LBL 22. REMOVED DAMAGED SECTION AND INSTALLED REPAIR PARTS PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003011300065 20030113 00065 EA 2003 1 13 O2G2003F00000 1 20021211 A 2420 604908007 RAM AIR TURB CNDAIR CL604 CL604 1900301 EA AUX ELECTRICAL INOPERATIVE E O2GA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NE 03 1DG 172 5516 AUTOMATIC DEPLOYMENT OF ADG OCCURRED AT ALTITUDE WHILE ENROUTE. NO ADVANCE WARNING OR INDICATION WAS GIVEN PRIOR TO DEP LOYMENT. CREW PROCEEDED WITHOUT FURTHER INCIDENT. MAINTENANCE CREW STOWED AND PERFORMED OPERATIONAL CHECKS IAW MM. NO DEFECTS NOTED. AIRCRAFT RETURNED WITHOUT ANY REOCCURRENCE. THE FOLLOWING PARTS WERE CHANGED AS A PRECAUTIONARY MEASUR E. 2 L 7 2 4F RT A21EA 2003011300066 20030113 00066 NM 2003 1 13 P9R2002F00018 1 20021205 A 3350 LIGHT BOEING 727 727200 138407E NM PWA JT8 JT8D17 52049 NE GALLEY MISSING A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 919PG 22604 PHOTOLUMINESCENT STRIP MISSING IN FORWARD GALLEY. INSTALLED PHOTOLUMINESCENT STRIP IAW MM. 2 L 7 3 4F 4 F RT A3WE E2EA 2003011300067 20030113 00067 NM 2003 1 13 P9R2002F00019 1 20021207 A 3350 LIGHT BOEING 727 727200 138407E NM PWA JT8 JT8D17 52049 NE FWD GALLEY LOOSE A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 919PG 22604 FORWARD GALLEY EMERGENCY FLOOR DIRECTIONAL TRACK LOOSE. RESCURED EMERGENCY FLOOR DIRECTIONAL TRACK IAW MM. 2 L 7 3 4F 4 F RT A3WE E2EA 2003011300068 20030113 00068 WP 2003 1 13 ASAA0280561 1 20021111 A 5310 995773997 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K CHECK, SHEAR TIE IN AFT CARGO BAY CORRODED IN TWO AREAS AT FS 1287, L29L TO L29R. REMOVED CORROS ION AND REPAIRED WITH DOUBLER PER SRM 53-01, 53-03, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003011300069 20030113 00069 WP 2003 1 13 ASAA0280563 1 20021111 A 5320 993653423 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K-CHECK, MAIN CABIN FLOOR SUPPORT CORRODED AT FS 195, LBL 44. INSTALLED NEW SUPPORT PER SRM 51-10- 2 AND 51-10-4. (M) 2 L 7 2 4F RT A6WE 2003011300070 20030113 00070 WP 2003 1 13 ASAA0280566 1 20021112 A 5321 99365513 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, FLOORBOARD HAS NUMEROUS CORRODED INSERTS AND FASTENERS AT FS 207, LBL 22 TO RBL 22. REPLACED FLO ORBOARD PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003011300071 20030113 00071 WP 2003 1 13 ASAA0280567 1 20021112 A 5321 993654511 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, FLOORBOARD HAS NUMEROUS CORRODED INSERTS AND FASTENERS AT FS 160-207, BL 0 TO LBL 60. REPLACED F LOORBOARD PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003011300072 20030113 00072 WP 2003 1 13 ASAA0280568 1 20021112 A 5321 993655043 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND FLOORBOARD HAS NUMEROUS CORRODED INSERTS AND FASTENERS AT FS 207, LBL 22-44. REPLACED FLOORBOARD PER SRM 53 -05. (M) 2 L 7 2 4F RT A6WE 2003011300073 20030113 00073 WP 2003 1 13 GTIA021140 1 20020925 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - AFT PIT CORROSION FS 1250-1287 LONGERON 29R AND LWR SIDE CORRODED AT SPLICE. REMOVED DAMAGED SECTION. FABRICATED LONGERON SECTION. INSTALLED THE LONGERON SECTION. FABRICATED LONGERON SPLICE. INSTALLED SPLICE REPAIR. (M) 2 L 7 2 4F RT A6WE 2003011300074 20030113 00074 WP 2003 1 13 GTIA021141 1 20021018 A 3350 SOCKET DOUG DC9 DC983 3022083 WP A/C BAY DIRTY A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FLIGHT COMPARTMENT EMERGENCY FLOOD LIGHTS INOPERATIVE. TAIL COMPARTMENT RIGHT SIDE OF SLIDE LIGHT INOPERATI VE. FOUND LAMP SOCKETS NEED CLEANING, CLEANED SOCKETS. TROUBLE SHOT TAIL EMERGENCY LIGHT ON RT SIDE SLIDE AND FOUND SO CKETS NEEDED TO BE CLEANED, CLEANED SOCKET. (M) 2 L 7 2 4F RT A6WE 2003011300075 20030113 00075 WP 2003 1 13 GTIA021142 1 20021020 A 3350 TERMINAL DOUG DC9 DC983 3022083 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. FOUND TERMINAL LOOSE ON TERMINAL STRIP 53-384, SECURE TERMINAL LU G. (M) 2 L 7 2 4F RT A6WE 2003011300076 20030113 00076 WP 2003 1 13 GTIA021143 1 20021017 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND CORRODED FORMER IN UNPRESSURIZED TAIL SECTION FS 1418 LBL 18. REMOVED FORMER. LOCATED AND DRILL FITTING. INSTALLED NEW FORMER FITTING. (M) 2 L 7 2 4F RT A6WE 2003011300077 20030113 00077 WP 2003 1 13 GTIA021144 1 20020926 A 5313 STRINGER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FORWARD CARGO PIT STRINGER 30 CORRODED FROM FS 389-446, FORWARD CARGO FS 389-408 STRINGER 30 CORRODED. FOUN D FORWARD CARGO FS 427-446 STRINGER 30 CORRODED, FORWARD CARGO FS 408-427 STRINGER 30 CORRODED. (M) 2 L 7 2 4F RT A6WE 2003011300078 20030113 00078 WP 2003 1 13 GTIA021145 1 20020924 A 5313 STRINGER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND MID CARGO STRINGER 28L CORRODED FS 576-579. REMOVED DAMAGED AREA. FABRICATED SPLICE ON LONGERON SECTION. INSTALLED SPLICE AND LONGERON. (M) 2 L 7 2 4F RT A6WE 2003011300079 20030113 00079 WP 2003 1 13 GTIA021146 1 20020922 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND PASSENGER CABIN RIGHT INBOARD SEAT TRACK WORN AND CORRODED FS 1259 TO AFT END OF TRACK. REMOVED SEAT TRACK. DRILLED AND LOCATED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2003011300080 20030113 00080 WP 2003 1 13 GTIA021147 1 20020922 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND PASSENGER CABIN LEFT INBOARD SEAT TRACK WORN AND CORRODED FS 1088-1183. REMOVED LEFT OUTBOARD SEAT TRACK. LOCATED AND DRILLED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2003011300081 20030113 00081 WP 2003 1 13 GTIA021148 1 20021016 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND FORWARD CARGO DOOR HANDLE CUT OUT IS CRACKED. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2003011300082 20030113 00082 WP 2003 1 13 GTIA021150 1 20021027 A 3297 WIRE DOUG DC9 DC981 3022081 WP LT MLG BROKEN A GTIA K NONE N FALSE WARNING CL CLIMB 1 GL 23 806NK 48051 MCO - FLT 1927 - CLIMBING THROUGH 10,000 FEET LEFT RED GEAR UNSAFE LIGHT CAME ON PERFORMED QRH PROCEDURE. LIGHT REMAINED ON. FOUND BROKEN WIRE AT LEFT POSITION SWITCH. REPAIRED BROKEN WIRE. OPS CHECK NORMAL IAW MD80 MM 32-60-01. (M) 2 L 7 2 4F A6WE 2003011300083 20030113 00083 WP 2003 1 13 GTIA021151 1 20021012 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND PASSENGER CABIN SUBFLOOR WEB CRACKED AND CORRODED STATION 200 AND 218 AT RBL 48, UNDER SEAT TRACK. REMOVED PASSENGER CABIN CRACKED SUBFLOOR WEB. FABRICATED PASSENGER CABIN SUBFLOOR WEB. INSTALLED WEB. (M) 2 L 7 2 4F A6WE 2003011300084 20030113 00084 WP 2003 1 13 GTIA021152 1 20020919 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND FLOOR SUB STRUCTURE CORRODED STATION 160 LBL 42. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2003011300085 20030113 00085 NM 2003 1 13 UPS03440011 1 20021231 A 5330 SKIN BOEING 747 747259B 1384804 NM LWR FUSE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 527UP 21730 INSPECTION TYPE:C FX LOWER FUSELAGE, EXTERNAL SKIN EDGE FOUND HEAVY CORROSION AT STA 983 LH SIDE STG 41L TO STG 42L(2 LO CATIONS). SKIN REPAIRED AS PER SRM 53-30-03 FIG.1. (DEPTH 0.063", WIDTH 2", LENGTH 4") 2 L 7 4 4F RT A20WE 2003011300092 20030113 00092 WP 2003 1 13 GTIA021204 1 20021112 A 3260 833703 SENSOR DOUG DC9 DC983 3022083 WP NLG INTERMITTENT A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 826NK 49391 LGA - FLT 1865 - NOSE LANDING GEAR UNSAFE LIGHT (RED LIGHT), BLINKS ON AND OFF INTERMITTENTLY IN FLIGHT. OPS CHECKED LA NDING GEAR RETRACTION TEST PER MD80 MM 32-60-00. NO FAULTS ALL INDICATION NORMAL. REMOVED AND REPLACED NOSE GEAR UP SE NSOR, RETRACTION TEST NORMAL UP SENSOR CHANGE AS PRECAUTIONARY PER 32-60-05. (M) 2 L 7 2 4F RT A6WE 2003011300094 20030113 00094 WP 2003 1 13 GTIA021205 1 20021115 A 3260 CONTROL BOX DOUG DC9 DC982 3022082 WP LANDING GEAR LOOSE A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 821NK 49508 DTW - FLT 503 - DEPART DTW OUT OF 13,500 FEET AT 320 KTS, GEAR HANDLE UP, THERE WAS AN INTERMITTENT GEAR UNSAFE (ALL 3) INDICATION DURING LIGHT TURBULENCE. LIGHT WENT OUT IN SMOOTH AIR. AT 330, IN SMOOTH AIR, AT FL 200 GEAR UNSAFE LIGHTS CAME ON UNTIL FL330 IN SMOOTH AIR CONT UPON LIGHT TURBULENCE LIGHT WOULD COME ON AND OFF. NORMAL GEAR INDICATION UPON L ANDING. INSPECTED THROTTLE SWITCHES AND LANDING GEAR LEVER SWITCH FOR SECURITY AND OPERATION. NO DEFECTS NOTED AT THIS TIME. PERFORMED BITE TEST, AFTER RESECURING PROXIMITY CONTROL BOX PER MM 32-60-05. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 2003011300095 20030113 00095 EA 2003 1 13 EXO2003F00000 1 20021121 A 7830 2150640527 THRUST REVERSER CNDAIR CL600 CL6001A11 1900302 EA LYC ALF502 ALF502* 41580 EA RT ENGINE DAMAGED E EXOA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 17 63HJ 1021 DURING CLIMB THROUGH FL130 A LOUD BANG FOLLOWED BY RT THRUST REVERSER UNLOCK LIGHT, RETURNED TO AIRPORT. FOUND 12 O'CLO CK BALL SCREW ACTUATOR AFT ATTACH POINT FAILED CAUSING TRANSLATING STRUCTURE TO MOVE DOWN AND AFT ENOUGH TO CAUSE OTHER TWO ATTACH POINTS TO FAIL DUE TO AIR LOAD. THIS RESULTED IN ENTIRE TRANSLATING TO MOVE COMPLETELY AFT. THE FOUR BLOCKE R DOOR ARMS WERE ALL THAT HELD STRUCTURE ON THE AIRCRAFT. 1 X 3 FT SKIN MISSING AND THE FOUR DIVERTER DOORS WERE MISSI NG. 2 L 7 2 4F 4 F RT A21EA E6NE 2003011300096 20030113 00096 WP 2003 1 13 GTIA021219 1 20021120 A 2611 824P4 SMOKE DETECTOR DOUG DC9 DC983 3022083 WP LAVATORY MALFUNCTIONED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FLL - FLT 1442 - FORWARD LAVATORY SMOKE DETECTOR KEPT SOUNDING IN GATE. REPLACED SMOKE DETECTOR IN FORWARD LAVATORY IAW MD80 MM 26-14-00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2003011300097 20030113 00097 CE 2003 1 13 FFS2003F00005 1 20021214 A 5320 11498C03321 STIFFENER BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ZONE 522 CHAFED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 575D UE24 EXTERNAL POWER ANNUNCIATOR WOULD NOT EXTINGUISH. FOUND AFT STIFFENER IN LEFT NACELLE AFT SKIN HAD CHAFED THROUGH INSULA TION ON ELECTRICAL LEADS THAT GO FROM THE EXTERNAL POWER RECEPTICAL IN THE WHEEL WELL, TO THE EXTERNAL POWER RELAY IN TH E LEFT NACELLE. THIS CAUSED THESE LARGE (6 OR 8 GAUGE) WIRES TO BE GROUNDED TO THE AIRFRAME SUGGEST REROUTING OR BETTER ANTI CHAFE PROTECTION POTENTIAL FOR FIRE OR SEVERE. ELECTRICAL PROBLEMS. 2 L 7 2 4T 3 T RT A24CE E2NE 2003011300098 20030113 00098 WP 2003 1 13 GTIA021221 1 20021112 A 2611 SMOKE DETECTOR DOUG DC9 DC981 3022081 WP LAVATORY MALFUNCTIONED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND SMOKE DETECTOR IN AFT LEFT LAV COMES ON INTERMITTENTLY. REMOVED SMOKE DETECTOR. INSTALLED SMOKE DETECTOR. (M) 2 L 7 2 4F A6WE 2003011300099 20030113 00099 WP 2003 1 13 GTIA021222 1 20020814 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - TEMP REPAIR INSTALLED FS 160 LOWER RIGHT SIDE. REMOVED EXTERNAL DOUBLER. AFTER DOUBLER REMOVAL, FOUND L27R DENTE D AT SKIN CUT OUT. REMOVED SECTIONS OF L27R FROM FS 150 TO 170. REMOVED SECTION OF L27R FROM FS 150 TO 110. REMOVED D AMAGED SECTION OF SKIN. FABRICATED DOUBLERS AND FILLER. LOCATED AND DRILLED NEW LONGERON L27R. LOCATED AND DRILLED SPL ICE. INSTALLED L27R SPLICE. INSTALLED NEW LONGERON 27R FS 110-165. INSTALLED NEW DOUBLER AND NEW FILLER ON OUTER SKIN . (M) 2 L 7 2 4F A6WE 2003011300100 20030113 00100 WP 2003 1 13 GTIA021223 1 20021018 A 5753 SKIN DOUG DC9 DC981 3022081 WP T/E FLAP DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND DENT XRS 240 RIGHT OUTBOARD FLAP REQUIRES REPAIR. REMOVED DAMAGE SKIN AREA. INSTALLED FLAP SKIN REPAIR. ( M) 2 L 7 2 4F A6WE 2003011300101 20030113 00101 CE 2003 1 13 FFS2003F00006 1 20021224 A 5412 1189700367 SEAL BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA BULKHEAD MISALIGNED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 575A UC83 DURING INSPECTION OF THE RT FORWARD COWLING ASSEMBLY, IT WAS FOUND THAT THE AFT BULKHEAD HAD CRACKED AT THE LOWER MOUNT HOLES. WHEN THIS BULKHEAD IS BOLTED TO THE CORRESPONDING BULKHEAD FOR THE REAR COWLING ASSY, A SEAL INCORPORATED IN THE COWL ASSEMBLY. FLAT ACROSS THE SEAM BETWEEN BULKHEADS. IN THIS INSTANCE, HOWEVER THE SEAL HAD CURLED OVER AND BECOM E TRAPPED BETWEEN THE BULKHEADS FORMING AN EMPTY SPACE APPROXIMATELY .050 BETWEEN ADJOINING SURFACES SO WHEN THE BOLTS W ERE TORQUED IT SET UP LOCALIZED STRESS AT THE BOLT HOLES AND CAUSING THEM TO CRACK. 2 L 7 2 4T 4 T RT A24CE E4EA 2003011300102 20030113 00102 WP 2003 1 13 GTIA021224 1 20021018 A 5753 SKIN DOUG DC9 DC981 3022081 WP T/E FLAP DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND EXISTING REPAIR ON RIGHT INBOARD FLAP UPPER SURFACE 10 INCHES FROM T/E REQUIRES REPAIR. CUT DAMAGE OUT. FA BRICATED DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2003011300103 20030113 00103 WP 2003 1 13 GTIA021225 1 20021001 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - E/E COMPARTMENT LONGERON 30 STATION 120 TO 133 HAS CORROSION FOUND ON REMOVAL OF BATTERY TRAY TO FOM. DRILLED NEW STRINGER 30. INSTALLED L30. (M) 2 L 7 2 4F RT A6WE 2003011300104 20030113 00104 CE 2003 1 13 G0241 1 20021205 A 3097 AC065CG01120 WIRE CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL PITOT HEAT BROKEN E UG8A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 5113 3400 7500013 DURING TAXI, THE RT PITOT HEAT FAIL CAS MESSAGE ILLUMINATED. BROKEN GROUND WIRE AT THE RIGHT HAND PITOT TUBE. REPAIRED BROKEN GROUND WIRE. OPERATIONAL CHECK IS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2003011300105 20030113 00105 WP 2003 1 13 GTIA021226 1 20020923 A 3350 LIGHT DOUG DC9 DC983 3022083 WP AFT AIRSTAIRS BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - THREE AFT AIRSTAIRS EMERGENCY LIGHTING ASSEMBLY BROKEN. REMOVED THREE AFT AIRSTAIRS EMERGENCY LIGHTING ASSEMBLY. INSTALLED THREE AFT AIRSTAIR EMERGENCY LIGHTING ASSEMBLY. DURING INSPECTION FOUND A FOURTH LIGHT BROKEN. INSTALLED ON E AFT AIRSTAIR EMERGENCY LIGHTING. (M) 2 L 7 2 4F RT A6WE 2003011300106 20030113 00106 WP 2003 1 13 GTIA021290 1 20021224 A 5730 PANEL DOUG DC9 DC981 3022081 WP PWA JT8 JT8D9 52048 NE CENTER WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 OVERWING FUEL PANEL STA 927-1003 HAS PUNCTURES, EDGE CRACKS AND BENT UP METAL. FABBED NEW FLOORBOARD. 2 L 7 2 4F 4 F A6WE E2EA 2003011300107 20030113 00107 WP 2003 1 13 GTIA021291 1 20020812 A 5340 FITTING DOUG DC9 DC981 3022081 WP PWA JT8 JT8D9 52048 NE CARGO DOORWAY CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FORWARD CARGO DOOR JAMB FORWARD LOCK PIN FITTING CRACKED AND WORN. REMOVED FITTING. INSTALLED NEW FITTING. 2 L 7 2 4F 4 F A6WE E2EA 2003011300108 20030113 00108 WP 2003 1 13 GTIA021294 1 20020813 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP PWA JT8 JT8D9 52048 NE FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 AFT PIT STA 1290-1309 BL0 INTERCOASTAL BETWEEN MAIN CABIN FLOORBEAMS HAS CRACKS IN UPPER FLANGE AT FASTENER HOLES. REMO VED INTERCOASTAL BETWEEN FLOORBEAMS ON AFT PIT STA 1290-1309 BLO. FORMED NEW INTERCOASTAL STA 1290-1309 BLO. INSTALLED NEW INTERCOASTAL. 2 L 7 2 4F 4 F A6WE E2EA 2003011300109 20030113 00109 WP 2003 1 13 GTIA021227 1 20020927 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FORWARD LAVATORY EQUIPMENT DAMAGED AT FLOORBOARD SUPPORT. REMOVED DAMAGED FLOORBOARD FORWARD LAVATORY. FABRICATE D NEW FLOORBOARD FORWARD LAVATORY. INSTALLED NEW FLOORBOARD FORWARD LAVATORY. (M) 2 L 7 2 4F RT A6WE 2003011300110 20030113 00110 WP 2003 1 13 GTIA021295 1 20020814 A 5280 FITTING DOUG DC9 DC981 3022081 WP PWA JT8 JT8D9 52048 NE NG DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 RT FORWARD NLG DOOR STRUCTURAL SUPPORT FITTING CRACKED. FITTING REMOVED. LOCATED AND DRILLED NEW FITTING. INSTALLED N EW FITTING. 2 L 7 2 4F 4 F A6WE E2EA 2003011300111 20030113 00111 WP 2003 1 13 GTIA021296 1 20020822 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP PWA JT8 JT8D9 52048 NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 LEFT OUTBOARD SEAT TRACK CORRODED. FS 200-260. MATERIAL LOSS FROM STA 250-260 FOUND TO BE OUT OF LIMITS. CUT SEAT TRA CK AT STA 303 LEFT OUTBOARD SEAT TRACK. FABRICATE NEW SECTION OF SEAT TRACK AT STA 250. INSTALLED NEW SEAT TRACK AT ST A 250-303 AND SPLICE REPAIR AT 303 LEFT OUTBOARD. 2 L 7 2 4F 4 F A6WE E2EA 2003011300112 20030113 00112 WP 2003 1 13 GTIA021297 1 20020814 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP PWA JT8 JT8D9 52048 NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 LT INBOARD SEAT TRACK CORRODED FS 826-1003. REMOVED SEAT TRACK STA 915-1047. FABRICATED SEAT TRACK. INSTALLED SEAT T RACK LEFT OUTBOARD FS 826-1003. 2 L 7 2 4F 4 F A6WE E2EA 2003011300113 20030113 00113 WP 2003 1 13 GTIA021298 1 20021030 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP PWA JT8 JT8D9 52048 NE LAVATORY BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FORWARD LAV AREA FLOORBOARD BROKEN AND DELAMINATED. REPAIRED DAMAGED AND DELAMINATED AREAS. 2 L 7 2 4F 4 F A6WE E2EA 2003011300114 20030113 00114 NE 2003 1 13 GUU2003F00001 2 20021209 A 7200 3044800 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT FAILED A GUUA C ABORTED TAKEOFF R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SO 17 16540 14257 6710 UE172 114329 DURING TAKE OFF ROLL, HEARD A LOUD THUMP FROM LT ENGINE. ABORTED TAKE OFF. DETERMINED LT POWER SECTION SEIZED. REMOVE D AND REPLACED LT ENGINE ASSEMBLY AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. 2 L 7 2 4T 4 T RT A24CE E26NE 2003011300115 20030113 00115 EA 2003 1 13 REXA02024 1 20021204 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LAVATORY FALSE INDICATION A REXA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 25 8390A 7390 CREW RECEIVED EICAS TOILET SMOKE INDICATION ALONG WITH VISIBLE SMOKE IN AFT CABIN AND LAVATORY QRH FOLLOWED UNEVENTFUL U NSCHEDULED RETURN TO AIRPORT. PERFORMED ENGINE RUNS AND OPERATIONAL CHECKS OF BLEED AIR SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2003011300116 20030113 00116 WP 2003 1 13 GTIA021228 1 20020930 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND AFT FUSELAGE STATION 1497 RT AFT PLATFORM IS CRACKED AT RT FRAME. STOP DRILLED CRACK. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A6WE 2003011300117 20030113 00117 WP 2003 1 13 GTIA021230 1 20021128 A 5230 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 DTW - FOUND AFT CARGO PIT DOOR SKIN CRACKED AT HANDLE POCKET AREA. STOP DRILLED CRACK AND INSTALLED SCUFF PLATE IAW MD8 0 SRM 52-05. (M) 2 L 7 2 4F A6WE 2003011300118 20030113 00118 EA 2003 1 13 REXA02025 1 20021205 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LAVATORY DETECTED A REXA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SO 25 8390A 7390 CREW RECEIVED EICAS TOILET SMOKE INDICATION, THERE WAS A SLIGHT SMOKY HAZE IN THE VICINITY OF THE LAVATORY AS WELL AS A STRONG SMELL OF BURNED PLASTIC. QRH FOLLOWED UNEVENTFUL UNSCHEDULED RETURN TO AIRPORT. RAN CABIN PACK, INSPECTED AND O PERATIONALLY CHECKED LAV SMOKE DETECTOR. OPS CHECK GOOD IAW MM. NO EVIDENCE OF SMOKE. PERFORMED TEST FLIGHT, ALSO NO EVIDENCE OF SMOKE. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2003011300119 20030113 00119 WP 2003 1 13 GTIA021231 1 20021115 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND AFT PIT STATION 1287-1309 BL 0 INTERCOSTAL UPPER FLANGE CRACKED AT FASTENER HOLES. REMOVED UPPER FLANGE REP AIR ANGLE. FABRICATED ANGLE. INSTALLED ANGLE. (M) 2 L 7 2 4F A6WE 2003011300120 20030113 00120 EA 2003 1 13 REXA02026 1 20021208 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE RIGHT MALFUNCTIONED A REXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 25 8390A 5912 7390 LAVATORY EICAS SMOKE INDICATION IN FLIGHT. TROUBLESHOT PROBLEM TO THE RT AIR CYCLE MACHINE. DEFERRED RIGHT ACM IAW MEL . 2 L 7 2 4F 4 F RT A21EA E15NE 2003011300121 20030113 00121 CE 2003 1 13 RU32003F00000 1 20021113 A 5210 1313232C13 PIN BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE FWD DOOR HOOK BROKEN E RU3A A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SW 15 68 FF3 AFTER LEVELING OFF AT 18,000 FT, HEAR A LOUD THUMP FOLLOWED BY ILLUMINATION OF RED CABIN DOOR LIGHT. COMPLETED EMERGENC Y CHECKLIST. PRESSURIZATION REMAINED AT 6.0 PSID. REQUESTED DESCENT AND RETURN. REMAINDER OF FLIGHT UNEVENTFUL. FOUN D PIN BROKEN IN FORWARD UPPER DOOR HOOK. 2 L 7 2 4T 4 T A24CE E4EA 2003011300122 20030113 00122 WP 2003 1 13 GTIA021232 1 20021112 A 7120 ISOLATOR DOUG DC9 DC982 3022082 WP NR 2 ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND LOWER FORWARD ISOLATOR ALIGNMENT MARK BEYOND LIMITS NR 2 ENGINE. REMOVED FORWARD LOWER ISOLATOR. INSTALLED LOWER FORWARD ISOLATOR ON NR 2 ENGINE. (M) 2 L 7 2 4F A6WE 2003011300123 20030113 00123 NE 2003 1 13 SDR020040 2 20021224 A 7321 SHAFT BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE FUEL CONTROL SHEARED A MYWA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SO 19 802MA 22433 DURING CLIMB OUT, THROUGH 1000 FT ALT ENGINE NR 1 FLAMED OUT. (FUEL FLOW AND EPR WENT TO ZERO. DURING TAKEOFF ALL ENGI NE INDICATIONS WERE NORMAL. C/W AOM PROCEDURES AND RETURNED TO AIRPORT. REMOVED AND REPLACED FUEL CONTROL UNIT AND FUE L PUMP FUEL PUMP UNIT. PERFORMED ENGINE TRIM RUN. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2003011300124 20030113 00124 WP 2003 1 13 GTIA021233 1 20021116 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND EXISTING REPAIRS AT FS 301 AND FS 310 BETWEEN L23R AND L25R ARE TOO CLOSE TOGETHER AND REQUIRES REPAIRS TO B E COMBINED. CUT OUT DAMAGED AREA. FORMED NEW REPAIR. LOCATED AND DRILLED ALL REPAIR PARTS. INSTALLED TWO FINGER DOUB LER FOUR EACH, DOUBLER FOUR EACH, STRAP 1 EACH FILLER. (M) 2 L 7 2 4F A6WE 2003011300125 20030113 00125 WP 2003 1 13 GTIA021234 1 20021112 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - PASSENGER SEAT TRACK LEFT INBOARD, WORN AT FS 1005-1809, 1118-1129, 1222, 1241, 1274, 1280. OUT OF LIMITS AT STAT ION'S 1118 TO 1129, 1241, 1274 AND 1280. CUT AND REMOVED DAMAGED SECTION OF SEAT TRACK. DRILLED NEW SEAT TRACK SECTION OF LEFT INBOARD FS 1107 TO 1305 AND TWO PLICES. INSTALLED NEW SEAT TRACK AND SPLICES. (M) 2 L 7 2 4F A6WE 2003011300126 20030113 00126 WP 2003 1 13 GTIA021235 1 20021116 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FLOORBOARD PANEL FS 1118-1184 BL0-BL23 HAS CORRODED INSERTS AND PUNCHER WITH DELAMINATION. FABRICATED NEW FLOORBO ARD FS 1118-1184. (M) 2 L 7 2 4F A6WE 2003011300127 20030113 00127 WP 2003 1 13 GTIA021236 1 20021115 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FLOOR WEB CRACKED TWO PLACES BETWEEN STATION 1287-1309 RIGHT. FABRICATED DOUBLERS. UPON FURTHER EVALUATION 3 CRA CKS WERE FOUND. INSTALLED DOUBLERS. (M) 2 L 7 2 4F A6WE 2003011300128 20030113 00128 SO 2003 1 13 SIMA200234303 1 20021207 A 2701 CONTROL COLUMN EMB 135 EMB135KL 3260302 SO RROYCE DART DART* NE COCKPIT VIBRATION A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 816AE 145552 DURING CLIMB THROUGH 25000 FT AT 290 KNOTS CREW REPORTED A VIBRATION IN THE CONTROL YOKE AND RUDDER PEDELS. VIBRATION L ESSENED AS AIRCRAFT SPEED WAS LOWERED AND STOPPED AT 230 KNOTS. AIRCRAFT WAS RETURNED AND LANDED WITH NOT FURTHER INCID ENTS. MAINTENANCE INSPECTED AIRCRAFT WITH NO DEFECTS NOTED. A FUNCTIONAL CHECK FLIGHT WAS PERFORMED WITH NO DISCREPANC IES NOTED. AIRCRAFT WAS THEN RETURNED TO SERVICE. 2 L 7 2 4F 4 T RT T00011AT 2003011300129 20030113 00129 SO 2003 1 13 SIMA200234501 1 20021210 A 3260 WARNING LIGHT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL MLG ILLUMINATED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 822AE 145581 DURING DESCENT CREW REPORTED GEAR UNSAFE. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. UPON L ANDING CREW RECEIVED THREE GREEN INDICATION FOR THE LANDING GEAR. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2003011300130 20030113 00130 SO 2003 1 13 SIMA200234502 1 20021204 A 5310 14522178005 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 DURING AN IMBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER SIL L AND INSTALLED SERVICEABLE SILL IAW EMB GST. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2003011300131 20030113 00131 WP 2003 1 13 GTIA021237 1 20021116 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND MID PIT STATION 636 TO 693 CORROSION AT T-SUPPORT INBOARD BEAM AND ELONGATED HOLES. REMOVED THE INBOARD BEA M T-SUPPORT. LOCATED AND DRILLED NEW SUPPORT BEAM. INSTALLED NEW SUPPORT BEAM. (M) 2 L 7 2 4F A6WE 2003011300132 20030113 00132 SO 2003 1 13 SIMA200234506 1 20021204 A 5310 14525480003 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL CARGO DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 637AE 145170 DURING AN IMBV INSPECTION THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED DAMAGED CENTER SILL AND REPLACED WITH SERVICEABLE SILL. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2003011300133 20030113 00133 WP 2003 1 13 GTIA021238 1 20021117 A 5313 STRINGER DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - AFT ACCESSORY COMPARTMENT 1474 CANT LONGERON 18L, 1 INCH CRACK ON STRINGER. STOP DRILL CRACK. FABRICATED TWO FOR MER DOUBLERS. INSTALLED TWO FORMER DOUBLER REPAIR. (M) 2 L 7 2 4F A6WE 2003011300134 20030113 00134 WP 2003 1 13 GTIA021239 1 20021115 A 5320 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND FORWARD CARGO FS 227 STRINGER 28L SPLICE FITTING CORRODED. REMOVED LONGERON SPLICE. LOCATED AND DRILLED NEW SPLICE. INSTALLED SPLICE. (M) 2 L 7 2 4F A6WE 2003011300135 20030113 00135 WP 2003 1 13 GTIA021240 1 20021115 A 5320 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND FORWARD PIT FS 227 STRINGER 27L SPLICE FITTING CORRODED. REMOVED SPLICE FITTING. FORMED SPLICE. INSTALLED SPLICE. (M) 2 L 7 2 4F A6WE 2003011300136 20030113 00136 WP 2003 1 13 GTIA021241 1 20021116 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND MID PIT STATION 541 FORWARD BULKHEAD AFT FACE HAS CORROSION AT ANGLE LOWER ATTACH TO BULKHEAD RBL 16 INCH LB L 16 INCHES. REMOVED LOWER ANGLE. FORMED NEW ANGLE. INSTALLED NEW ANGLE. (M) 2 L 7 2 4F A6WE 2003011300138 20030113 00138 GL 2003 1 13 2002365673 1 20021231 A 3350 LIGHT BOMBDR BD700 BD7001A10 1390006 GL GE CF34 CF34* NE CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 673BR 673BR RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. 2 L 7 2 4F 4 F RT T00003NY E15NE 2003011300139 20030113 00139 NM 2003 1 13 ASAA0210312 1 20021113 A 7110 65701934 COWLING BOEING 737 737210C 1384459 NM NR 2 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 THRUST REVERSER COWLING AT REVERSER STATION 96.4 GOUGED. REPAIRED THRUST REV ERSER COWLING PER SRM. (M) 2 L 7 2 4F A16WE 2003011300140 20030113 00140 NM 2003 1 13 ASAA0210314 1 20021113 A 7110 657377315 COWLING BOEING 737 737210C 1384459 NM NR 1 ENGINE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWLING AT NACELLE STATION 139.5 CHAFED. REMOVED DAMAGE AND REPAIRED ENGINE COWLING PER SRM. (M) 2 L 7 2 4F A16WE 2003011300141 20030113 00141 NM 2003 1 13 ASAA0210315 1 20021113 A 7110 COWLING BOEING 737 737210C 1384459 NM NR 2 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWLING AT NACELLE STATION 148 GOUGED. REMOVED DAMAGE AND REPAIRED EN GINE COWLING PER SRM. (M) 2 L 7 2 4F A16WE 2003011300144 20030113 00144 NM 2003 1 13 ASAA0210316 1 20021113 A 5315 FLOORBEAM BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 420, LEFT BUTTOCK LINE 12, LEFT BUTTOCK LINE 48 CORRODED. REPAIRE D FLOORBEAM PER EA. (M) 2 L 7 2 4F A16WE 2003011300145 20030113 00145 NM 2003 1 13 ASAA0210317 1 20021113 A 5315 655490510 FLOORBEAM BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BODY STATION 480, LEFT BUTTOCK LINE 29, LEFT BUTTOCK LINE 43 CORRODED . REPAIRED FLOORBEAM PER EA. (M) 2 L 7 2 4F A16WE 2003011300146 20030113 00146 NM 2003 1 13 ASAA0210318 1 20021113 A 5315 65548935 FLOORBEAM BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 500, LEFT BUTTOCK LINE 44 CORRODED. REPAIRED FLOORBEAM PER EA. ( M) 2 L 7 2 4F A16WE 2003011300147 20030113 00147 NM 2003 1 13 ASAA0210319 1 20021113 A 5315 65549063 FLOORBEAM BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 500B, RIGHT BUTTOCK LINE 11, RIGHT BUTTOCK LINE 24 CORRODED. REPA IRED FLOORBEAM PER EA. (M) 2 L 7 2 4F A16WE 2003011300149 20030113 00149 NM 2003 1 13 ASAA0210321 1 20021116 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 13 WOULD NOT EXTINGUISH. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES AND RECEIVERS, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2003011300151 20030113 00151 NM 2003 1 13 AWXA200300034 1 20021224 A 5753 113N2800 FLAP BOEING 757 7572G7 1384963 NM SATURATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 0 0 24523 LCQ - MAJOR REPAIR - DURING C-10 CHECK X-RAY INSPECTION FOUND MOISTURE ENTRAPMENT IN R/H WING INBOARD AFT FLAP; X-RAY AL SO REVEALED A CRACK IN ENVIRONMENTAL END SEAL. MAINTENANCE CUTOUT AND CLEANED DAMAGED AREAS OF R/H WING INBOARD AFT FLAP ; INSTALLED BOND REPAIR IAW B757-200 SRM 51-70-04, FIG. 5, PG. 32. 2 L 7 2 4F RT A2NM 2003011300152 20030113 00152 WP 2003 1 13 ASAA0280533A 1 20021107 A 3350 0105607 LENS DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 977AS 53453 PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT WHITE LENS BROKEN. REPLACED LENS, A SUB-ASSY OF THE LIGHT MOD ULE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003011300153 20030113 00153 WP 2003 1 13 IXXA0200154S 1 20021109 A 7100 ENGINE DOUG DC8 DC871F 302199D WP I/B T/R SUP.RING CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 2906 45811 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DISCOVERED IN THE # 3 ENGINE INBOARD THRUST REVERSER HALF BLOCKER DOOR SU PPORT RING AT THE 11 O'CLOCK POSITION. REPAIR ACCOMPLISHED REMOVAL STOP DRILLED CRACK FABRICATION AND INSTALLATION OF RE PAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND DRAWING R74-R03. 2 L 7 4 4F RT 4A25 2003011400001 20030114 00001 WP 2003 1 14 GTIA021300 1 20020920 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP PWA JT8 JT8D9 52048 NE COCKPIT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FLOOR PANEL, RT SIDE, UNDER RUDDER PEDAL, CRACKED IN RIBS. REMOVED RT AND LT INBOARD RIBS, FROM FLOOR PANEL STA 84-107. FABRICATED RIBS FOR FLOOR PANEL. UPON FURTHER INVESTIGATION FOUND FLOOR PANEL WEB MATERIAL CRACKED. FABRICATED DOUBL ER. FABRICATED FILLER. DRILLED AND LOCATED DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER ON RT FLOORPANEL STA 84-1 07. 2 L 7 2 4F 4 F A6WE E2EA 2003011400002 20030114 00002 NM 2003 1 14 GTIA021301 1 20021210 A 5320 WEB DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FUSELAGE AFT CARGO BAY FS 1290 LONGERON 18R HAS CRACKED CUSP WEB DOUBLER AT NR 2 ENGINE TELFLEX CABLE FLOOR ACCESS. CU T OUT DAMAGED WEB AT CUSP LONGERON 18 RT STA 1278-1309. FABRICATED WEB FOR REPAIR AT CUSP, LONGERON 18 RT STA 1275-1309 . INSTALLED WEB REPAIR. 2 L 7 2 4F 4 F RT E2EA 2003011400003 20030114 00003 NM 2003 1 14 GTIA021302 1 20021212 A 5320 FLOOR SUPPORT DOUG MD80 MD83 3023681 NM PWA JT8 JT8D NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 PAX CABIN, STA 200 TO 160 SUPPORT FLOOR CORRODED LBL 54. REMOVED FLOOR SUPPORT, LOCATED AND DRILLED NEW FLOOR SUPPORT, INSTALLED NEW FLOOR SUPPORT COMMON TO PAX CABIN, STA 200-160. 2 L 7 2 4F 4 F RT E2EA 2003011400004 20030114 00004 NM 2003 1 14 GTIA021303 1 20021212 A 5320 WEB DOUG MD80 MD83 3023681 NM PWA JT8 JT8D NE SUB FLOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 PAX CABIN STA 1654, LBL 53, CORRODED ON SUB FLOOR WEB. REMOVED DAMAGED SECTION, FABBED FILLER AND REPAIR DOUBLER, INS TALLED REPAIR. 2 L 7 2 4F 4 F RT E2EA 2003011400005 20030114 00005 NM 2003 1 14 GTIA021304 1 20021212 A 5321 FLOORBOARD DOUG MD80 MD83 3023681 NM PWA JT8 JT8D NE PAX CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 PAX CABIN STA 200 TO 160 FLOORBOARD CORRODED AT INSERTS/ DELAMINATED. FABRICATED NEW FLOORBOARD. 2 L 7 2 4F 4 F RT E2EA 2003011400006 20030114 00006 NM 2003 1 14 GTIA021305 1 20021130 A 5320 SUPPORT DOUG MD80 MD83 3023681 NM PWA JT8 JT8D NE CARGO BAY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 STA 218 FORWARD CARGO BAY, UPPER BLOCK SHELF SUPPORT CORRODED, ENTIRE LENGTH. REMOVED UPPER SUPPORT. FABRICATED UPPER SUPPORT. INSTALLED UPPER SUPPORT. 2 L 7 2 4F 4 F RT E2EA 2003011400007 20030114 00007 NM 2003 1 14 GTIA021306 1 20021125 A 5310 BEAM DOUG MD80 MD83 3023681 NM PWA JT8 JT8D NE CARGO DOORWAY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 MID CARGO DOOR, BOTTOM FORWARD AND AFT DOOR STOPS HAVE CORRODED UNDERNEATH. MID CARGO DOOR JAM BEAM HAS CORROSION ON TH E REPAIR STRAP INSIDE OF BEAM. REMOVED JAMB BEAM. LOCATED AND DRILLED NEW JAMB BEAM. INSTALLED DOOR JAMB BEAM. 2 L 7 2 4F 4 F RT E2EA 2003011400008 20030114 00008 NM 2003 1 14 GTIA021308 1 20021124 A 5712 RIB DOUG MD80 MD83 3023681 NM PWA JT8 JT8D NE LT WING LE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 LT WING LEADING EDGE RIB, CRACKED AT XRS267. FABRICATED 2 REPAIR ANGLES. STOP DRILLED CRACK ON LT WING LEADING EDGE RI B AT XRS 267. INSTALLED REPAIR ANGLES AT XRS 267 LT WING LEADING EDGE. 2 L 7 2 4F 4 F RT E2EA 2003011400009 20030114 00009 WP 2003 1 14 GTIA021310 1 20021116 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 STA 1322-1338, LONGERON 22 LT INTERCOSTAL HAS CORROSION. REMOVED 2 INTERCOSTALS AT STA 1322-1338, 22L, 21L. FABRICATED 2 EA INTERCOSTAL. INSTALLED 2 EA INTERCOSTALS AT STA 1322 TO 1338. 2 L 7 2 4F 4 F A6WE E2EA 2003011400010 20030114 00010 SO 2003 1 14 SIMA200234508 1 20021120 A 5347 14530659011 SEAT TRACK EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 A LEVEL 2 CORROSION FOUND DURING A IMBV INSPECTION. LT HAND FORWARD LOWER SEAT TRACK CORRODED BETWEEN FRAMES 19 AND 24. REMOVED AND INSTALLED SERVICEABLE SEAT TRACK IAW MM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2003011400011 20030114 00011 SO 2003 1 14 SIMA200234509 1 20021120 A 5310 14521725615 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GALLEY DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 A LEVEL 2 CORROSION FOUND DURING AN IMBV INSPECTION. AFT SERVICE DOOR SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE DOOR SILL IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2003011400012 20030114 00012 SO 2003 1 14 SIMA200234510 1 20021120 A 5320 147524131011 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 A LEVEL 2 CORROSION FOUND DURING AN IMBV INSPECTION. PASSENGER DOOR AREA AFT FLOOR SUPPORT CORRODED. REMOVED AND INSTA LLED SERVICABLE SUPPORT IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2003011400013 20030114 00013 SO 2003 1 14 SIMA200234511 1 20021120 A 5320 14524131009 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 A LEVEL 2 CORROSION FOUND DURING AN IMBV INSPECTION REFERENCE. PASSENGER DOOR AREA FORWARD FLOOR SUPPORT CORRODED. RE MOVED AND INSTALLED A SERVICEABLE FORWARD FLOOR SUPPORT IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2003011400014 20030114 00014 SO 2003 1 14 SIMA200234512 1 20021120 A 5320 14521718003 PROFILE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GALLEY RAMP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 LEVEL 2 CORROSION FOUND DURING AN IMBV INSPECTION. GALLEY RAMP PROFILE AT FRAME 20 CORRODED. REMOVED AND INSTALLED SER VICEABLE PROFILE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2003011400015 20030114 00015 SO 2003 1 14 SIMA200234513 1 20021120 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 LEVEL 2 CORROSION FOUND DURING AN IMBV INSPECTION. RT BEAM AFT DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEA BLE GUSSET IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2003011400016 20030114 00016 GL 2003 1 14 TU3R12042 2 20021031 A 7321 206064702001 CONTROL ROD BELL 206 206L3 1182108 SW ALLSN 250B 250B17 03012 GL FUEL CONTROL CORRODED B TU3R K NONE O OTHER IN INSP/MAINT 1 WP 07 112TV 11057 51123 DURING RIGGING OF THE NR 1 FUEL SYSTEM, THE TECH STARTED TO ADJUST THE ROD END BEARING ON THE LOWER END OF THE CONTROL R OD FOR THE FUEL CONTROL UNIT AND THE CONTROL ROD FAILED APPROX 1 INCH FROM THE LOWER END. CORROSION STARTED IN THE INTE RIOR OF THE ROD AND WAS NOT VISIBLE PRIOR TO BREAKING. CORROSION APPEARS TO BE SETTING ON TOP THE STUD THAT IS RIVETED ON FOR THE ROD END BEARING AND THERE IS NO VISIBLE PATH THAT MOISTURE CAN ENTER THE ROD. THERE WAS NO RECORD OF THIS PA RT BEING CHANGE DURING THE LIFE OF THE AIRCRAFT. 1 G 7 1 3U 3 T H2SW E10CE 2003011400017 20030114 00017 SW 2003 1 14 TU3R12048 1 20021029 A 6220 222310126101 BEARING BELL 230 230 1182149 SW ALLSN 250C 250C30 03013 GL M/R HEAD DELAMINATED B TU3R K NONE O OTHER IN INSP/MAINT 1 WP 07 303PS A22 23016 DURING MAIN ROTOR TRACK AND BALANCE FLIGHTS, THE CREW WOULD HAVE THE RIDE, ACCEPTABLE BY FEEL AND BY READINGS, AND RELE ASE THE AIRCRAFT FOR SERVICE. THE NEXT FLIGHT THE RIDE WOULD BE WORSE. DURING THE INSPECTION OF THE ROTOR SYSTEM, THE HYDRAULIC CART WAS CONNECTED TO THE AIRCRAFT AND FOUND THE INNER RACE OF THE OUTBOARD FEATHERING BEARING DISCONNECTED FR OM THE REST OF THE BEARING. THIS IS THE SECOND OCCURRENCE OF DELAMINATION OF THIS BEARING. DUE TO LOADING OF THE MAI N ROTOR SYSTEM AND THE WAY THAT THE CONTROL INPUTS ARE DESIGNED, A HYDRAULIC CART IS NEEDED TO FIND LOOSE BEARINGS. 1 G 7 2 3U 3 U NC H9SW E1GL 2003011400018 20030114 00018 NM 2003 1 14 UIEA200200067 1 20021213 A 2410 766088A IDG BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL NR 3 FAILED A UIEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 409MC 30558 706104 REFJECTED TAKEOFF DUE TO ELECTRIC DRIVE NR 3 WARNING ON TAKEOFF ROLL. ABORT OCCURRED AT 70 KNOTS. TRANSFERRED TO DMI, IDG OIL SERVICED TOO FULL. THREE QUARTS ADDED. REMOVED AND REPLACED NR 3 IDG IAW MM. PERFORMED OPS TEST IAW MM. OPS TEST OK. ALL INDICATIONS NORMAL. STATUS MESSAGE CLEARED. NO LEAKS FOUND ON IDG. 2 L 7 4 4F 4 F RT 1384945 E23EA 2003011400019 20030114 00019 NM 2003 1 14 USAASB02217 1 20021207 A 2160 3981161 VALVE BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE LAVATORY STUCK A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 512AU 41665 23595 AFTER LIFTOFF, THE FORWARD LAVATORY SMOKE DETECTOR BEGAN SOUNDING. AN ELECTRICAL ODOR WAS ALSO NOTED COMING FROM THE FO RWARD LAVATORY. CREW PULLED THE CIRCUIT BREAKERS FOR THE WATER HEATER IN THE FORWARD LAVATORY AND THE SMOKE ALARM STOPP ED SOUNDING. THE ODOR WAS ALSO DETECTED IN THE AFT CABIN, BUT NO ALARMS. EMERGENCY WAS DECLARED AD THE FLIGHT RETURNED TO FIELD. FLIGHT LANDED WITHOUT FURTHER INCIDENT. UPON ARRIVAL, THE ELECTRICAL SMELL WAS NOT AS STRONG. MAINTENANCE FOUND THE LT MIXING VALVE STUCK. ALSO, REMOVED AND REPLACED THE CABIN TEMPERATURE INDICATOR, DUE TO INACCURACY. ACCOMP LISHED GROUND RUN. OPERATIONAL CHECK GOOD. NO ODOR NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2003011400020 20030114 00020 NM 2003 1 14 USAASB02219 1 20021208 A 2780 2061141 JACKSCREW BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE LE FLAPS LACK OF LUBE A USAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 19 389US 23311 AFTER TAKEOFF, THE LEADING EDGE FLAPS WOULD NOT RETRACT. CREW WENT THROUGH SEVERAL PROCEDURES BUT THE FLAPS STILL WOULD NOT RETRACT FROM THE 2 DEGREE POSITION. FLIGHT RETURNED TO THE FIELD WITH A 15 DEGREE FLAP LANDING WITHOUT FURTHER INC IDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE AFT FLAPS DRY AND IN NEED OF LUBRICATION. ACCOMPLISHED JACKSC REW LUBE AND FLAP LUBRICATION. REMOVED AND REPLACED FLAP POSITION INDICATOR AS PRECAUTIONARY. OPERATIONALLY CHECKED FL APS NUMEROUS TIMES. NO FAULTS OR DEFECTS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2003011400021 20030114 00021 SO 2003 1 14 VWA2003F00000 1 20021203 A 5610 159SCCE10011 WINDSHIELD GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY50614 54519 EU COCKPIT CRACKED D VWAV A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 41AV 5803 61 ON INITIAL CLIMB GOING THROUGH 28,000 FT THE PILOTS WINDSHIELD CRACKED. FOLLOWING PROCEDURES IN THE CHECKLIST, THE CREW DESCENDED TO THE RECOMMENDED ALTITUDE. LANDED THE AIRPLANE WITHOUT ANY PROBLEMS. THE CREW REPORTED THE PROBLEM TO THE MAINTENANCE DEPARTMENT, AT WHICH TIME THE AIRCRAFT WAS GROUNDED. AIRCRAFT WAS INSPECTED, A NEW WINDSHIELD ORDERED AND INSTALLED. FAILED WINDSHIELD WAS INSTALLED 10/21/74. 2 L 7 2 4F 4 F RT A12EA E2EU 2003011400022 20030114 00022 NE 2003 1 14 WXOA02007 2 20020918 A 7261 DRIVE GEAR DOUG DC9 DC921 302205A WP PWA JT8 JT8D11 52044 NE SCAVENGE PUMP FAILED A WXOA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 17 127NK 47361 ENROUTE, NR 1 ENGINE LOW OIL PRESSURE ANNUNCIATOR INDICATION ILLUMINATED. CREW COMPLIED WITH AOM EMERGENCY/ ABNORMAL PR OCEDURES. PRECAUTIONARY INFLIGHT ENGINE SHUTDOWN ACCOMPLISHED. AIRCRAFT CONTINUED TO STATION WITHOUT INCIDENT. THE EN GINE WAS REMOVED AND SENT FOR EVALUATION. THE NR 4, 7, AND 5 SCAVENGE PUMP DRIVE GEARS WERE FOUND TO HAVE FAILED. THE ENGINE REMAINS DISASSEMBLED AND WILL NOT BE RETURNED TO SERVICE AT THIS TIME. 2 L 7 2 4F 4 F A6WE E2EA 2003011400023 20030114 00023 EA 2003 1 14 ZKG2003F00000 2 20021126 A 7414 ES10382585 POINTS PIPER PA24 PA24250 7102404 SO LYC O540 IO540* 41532 EA RT MAGNETO DAMAGED B ZKGR O OTHER R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 NE 05 8028P 921 243274 ROUGH MAGNETO ON RUN UP, FOUND MAGNETO TIMING ON RT MAGNETO OFF. INSPECTED CONTACT POINTS AND FOUND FOLLOWER THAT RIDES ON CAM IN MAGNETO TO HAVE LOOSE RIVETS. REPLACED POINTS. REINSTALLED MAG AND RUNUP CHECKS WERE OK. 1 L 7 1 3O 3 O 1A15 1E4 2003011400024 20030114 00024 SO 2003 1 14 ZLW2002F00001 1 20021011 A 3040 CONTROLLER GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY5118 54523 EU WINDSHIELD HEAT CRACKED E ZLWA O OTHER O OTHER NR NOT REPORTED 1 SW 15 36MW 3952 91294H0188X 89 CRACKED WINDSHIELD ON COPILOT SIDE. AFTER THE NEW WINDSHIELD WAS INSTALLED A FUNCTIONAL CHECK WAS PERFORMED AND IT WAS NOTED THAT THE WINDSHIELD STAYED FULL HOT. THE WINDSHIELD HEAT CONTROLLER WERE SWAPPED AND THE WINDSHIELD HEATED NORMAL LY. 2 L 7 2 4F 4 F RT A12EA E2EU 2003011400025 20030114 00025 NE 2003 1 14 ANCF200200026 2 20021209 A 7261 7578678 OIL FILTER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LT ENGINE CLOGGED W ANCF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 593AN 53093 728104D DURING TAKEOFF ROLL, AT 90 KNOTS, LT OIL STRAINER CLOGGED LIGHT ANNUNCIATION APPEARED. LT ENGINE MAIN OIL FILTER WAS RE MOVED AND REPLACED IAW AMM 79-20-06/202. ENGINE RUN UP WAS PERFORMED IAW AMM 71-00-00/506 WITH SATISFACTORY RESULTS. 2 L 7 2 4F 4 F RT A6WE E9NE 2003011400026 20030114 00026 NM 2003 1 14 CA021112008 1 20021112 A 2910 DSC252B40124 HOSE DHAV DHC8 DHC8301 1386003 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 2 HYD SYSTEM RUPTURED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER DEPARTURE, GEAR FAILED TO RETRACT WHEN SELECTED UP & NR 2 HYD QUANTITY DROPPED . AIRCRAFT RETURNED TO DEPART URE AIRPORT FOR NORMAL LANDING . INSPECTION FOUND NLG UPLOCK/RETRACTION ACTUATOR FLEX HOSE RUPTURED CAUSING LOSS OF NR 2 HYDRAULIC QUANTITY & FAILURE OF GEAR TO RETRACT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011400028 20030114 00028 NM 2003 1 14 VNAA0212039 1 20021231 A 3200 870004MODA PSEU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FAILED A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 424JS 10018 711 3033 DURING TAKE OFF, THE AIRCRAFT STARTED PULLING TO THE LEFT AT 70 KNOTS AND THE CREW ABORTED TAKE OFF. MAINTENANCE INSPEC TED AND REPLACED THE TORQUE LINKS, PSEU, AND ADJUSTED THE FEED BACK POTS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 3 2-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400045 20030114 00045 NM 2003 1 14 SWAA023031 1 20021230 A 5210 6547952 SKIN BOEING 737 7372H4 138448C NM FWD ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 071SW 22358 DURING WALK AROUND INSPECTION, FOUND FWD ENTRY DOOR SKIN CRACKED AT UPPER AFT CORNER. REMOVED AND REPLACED FWD ENTRY DO OR PER MM. 2 L 7 2 4F A16WE 2003011400046 20030114 00046 NM 2003 1 14 SWAA023034 1 20021230 A 5520 BACB28AKO4 BUSHING BOEING 737 7373K2 13844BA NM ELEVATOR WORN A SWAA K NONE E VIBRATION/BUFFET NR NOT REPORTED 1 SW 29 345SA 23786 DURING FLIGHT VIBRATION FELT FROM AFT CABIN. REMOVED AND REPLACED RT ELEVATOR TAB ASSY PER MM. 2 L 7 2 4F RT A16WE 2003011400047 20030114 00047 2003 1 14 SWAA023035 4 20021230 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2003011400048 20030114 00048 NM 2003 1 14 SWAA023036 1 20021229 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2003011400049 20030114 00049 NM 2003 1 14 SWAA023038 1 20021230 A 5330 6545776 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 20L, BS 970 AND BS 980. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2003011400050 20030114 00050 NM 2003 1 14 SWAA023040 1 20021229 A 5520 BACB28AK04 BUSHING BOEING 737 7377H4 1384404 NM BOTH ELEVATORS WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 760SW 27874 DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT ELEVATOR TAB HINGE ATTACH POINTS NR 3 AND NR 4 WORN. REMOVED AND R EPLACED HARDWARE AND BUSHINGS AT NR 3 AND NR 4 HINGE ATTACH POINTS PER MM. 2 L 7 2 4F RT A16WE 2003011400051 20030114 00051 NM 2003 1 14 SWAA023041 1 20021231 A 2612 6578947 DUCT BOEING 737 7372H4 138448C NM A/C BAY RUPTURED A SWAA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 SW 29 091SW 22963 ( AIR TURNBACK )………………………FWD CARGO FIRE DETECTION ACTIVATED WITH SMOKE IN CABIN, DISCHARGED BOTTLE. MX FERRY TO DALLAS. FOUND RH PNEUMATIC DUCT RUPURED IN A/C MIX BAY. R&R PNEUMATIC DUCT PER MM. 2 L 7 2 4F A16WE 2003011400052 20030114 00052 NM 2003 1 14 SWAA023043 1 20021229 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 4L. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2003011400053 20030114 00053 NM 2003 1 14 SWAA023046 1 20021230 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT # 5 DOOR STOP. RE PAIRED DOOR FRAME PER SWA T1. 2 L 7 2 4F RT A16WE 2003011400054 20030114 00054 2003 1 14 SWAA023048 4 20021230 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2003011400055 20030114 00055 2003 1 14 SWAA023049 4 20021230 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 787SA 29812 DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2003011400068 20030114 00068 2003 1 14 SWAA023015 4 20021228 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM FWD ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2003011400069 20030114 00069 NM 2003 1 14 SWAA023018 1 20021226 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED (5 EA) BETWEEN BS 727D AND BS 887, BETWEEN STR 22L AND STR 25L. REP AIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2003011400070 20030114 00070 2003 1 14 SWAA023021 4 20021226 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM AFT SVC DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2003011400071 20030114 00071 NM 2003 1 14 SWAA023022 1 20021227 A 5241 6547952 SKIN BOEING 737 7373G7 1384595 NM AFT SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR OUTER SKIN CRACKED (2 EA) AT LOWER FWD CORNER ABOVE LOWER GATE. REMOVED A ND REPLACED AFT SVC DOOR PER MM. 2 L 7 2 4F RT A16WE 2003011400072 20030114 00072 NM 2003 1 14 SWAA023023 1 20021226 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2003011400073 20030114 00073 NM 2003 1 14 SWAA023024 1 20021227 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 930 AND BS 933, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2003011400074 20030114 00074 NM 2003 1 14 SWAA023025 1 20021226 A 5610 589354 WINDOW BOEING 737 7375H4 138449D NM COCKPIT CRACKED A SWAA K NONE P NO WARNING INDICATION CR CRUISE 1 SW 29 512SW 24189 DURING CRUISE FO'S R1 COCKPIT WINDOW ARCED AND CRACKED. REMOVED AND REPLACED R1 WINDOW PER MM. 2 L 7 2 4F RT A16WE 2003011400075 20030114 00075 NM 2003 1 14 SWAA023026 1 20021227 A 3350 101114 COVER BOEING 737 7373T5 1384608 NM MID CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 RT OVERWING EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2003011400076 20030114 00076 NM 2003 1 14 SWAA023029 1 20021228 A 5755 6546452 SPOILER BOEING 737 7373T5 1384608 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED C4 CHECK, FOUND NR 5 GROUND SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED NR 5 GROUND SPO ILER PER MM. 2 L 7 2 4F RT A16WE 2003011400077 20030114 00077 NM 2003 1 14 SWAA023030 1 20021227 A 5520 BACB28AKO4 BUSHING BOEING 737 7377H4 1384404 NM ELEVATOR WORN A SWAA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 29 714CB 27848 MODERATE AIRFRAME VIBRATION FROM AFT GALLEY TO OVERWING AREA. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TABS PER SWA EA. 2 L 7 2 4F RT A16WE 2003011400081 20030114 00081 NE 2003 1 14 C7WA200200034 2 20021022 A 7311 548003 OIL COOLER BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAULTY A C7WA E ENGINE SHUTDOWN M OVER TEMP CL CLIMB 1 SO 17 511PE 20634 AFTER TAEKOFF, NR 1 ENGINE OIL TEMPERATURE WENT INTO YELLOW ARC (APPROX 126) AND STAYED THERE. HIGH OIL TEMP ABNORMAL C HECKLIST ACCOMPLISHED. AFTER 15 MINUTES OF OIL TEMPERATURE IN YELLOW BAND PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED AS PER CHECKLIST. HIGHEST OIL TEMPERATURE OBSERVED 150. TEMPERATURE SLOWLY WENT TO NORMAL AFTER SHUTDOWN. REMOVED AND R EPLACED NR 1 FUEL OIL HEAT EXCHANGER IAW MM 79-20-01. OPS AND LEAK CHECKS GOOD. OIL TEMP NORMAL ON ENGINE RUN IAW MM 7 9-34-0. (M) 2 L 7 3 4F 4 F A3WE E2EA 2003011400082 20030114 00082 NM 2003 1 14 DL764021084 1 20020905 A 2752 256T62004 ACTUATOR BOEING 767 767432ER 1385134 NM T/E FLAP TRIPPED A DALA K NONE F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 833MH 29706 IRREG: TRAILING EDGE FLAP DISAGREE AFTER TO WHEN RETRACTING FROM FLAPS 5 TO 1. RAISED FLAPS ELECTRICALLY WITH THE STAND BY SYSTEM. TROUBLESHOT PER FIM 27-51-00 PERFORMED BITE ON FSEU WITH FAULT 27-51104 INSPECTED ROTARY ACTUATORS FOUND LT WING FLAP ACTUATORS NR 1 AND NR 3 AND RT WING FLAP ACTUATORS NR 6 AND NR 7 TRIPPED RESET ACTUATORS. CYCLED FLAPS AND SL ATS NO FAULTS NOTED. 2 L 7 2 4F RT A1NM 2003011400083 20030114 00083 EU 2003 1 14 MALA020630 1 20021102 A 3240 BRAKE SAAB SF340 SF340A 7850100 EU MLG MALFUNCTIONED A MALA O OTHER O OTHER LD LANDING 1 GL 15 106XJ 340A106 DURING POSTFLIGHT OF FLIGHT NR 3146, ALL FOUR MAIN TIRES FOUND FLAT ON POSTFLIGHT. MAINTENANCE REPORTED FUSE PLUGS BLOW N, BRAKES RED HOT AND GLOWING. MAINTENANCE COMPLETED INSPECTION IAW, AMM CHAP. 5-50-00. REPLACED ALL 4 WHEELS AND BRAK ES IAW JC 3240-301 AND 3240-302. 2 L 7 2 4T RT A52EU 2003011400084 20030114 00084 NM 2003 1 14 P5CA0200703 1 20021011 A 2810 FUEL CELL BOEING 747 747200 1384847 NM RT WING LEAKING A P5CA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 23 524UP 21446 DURING EXTENDED GROUND TIME, NOTICED FUEL SEEP/STAIN RT WING GEAR DOOR FWD EDGE. SEEP SEALED PER FSM 4-05-1 NR 3 MAIN K ICK FITTING AREA. STAIN WIPED CLEAN. OK FOR SERVICE. 2 L 7 4 4F RT A20WE 2003011400085 20030114 00085 2003 1 14 P5CA0200704 4 20021016 A 2565 7A1326104 SLIDE BOEING 747 747300 GL RT DOOR FAILED A P5CA K NONE O OTHER TX TAXI/GRND HDL 1 WP 23 24837 CF650E2 RIGHT UPPER DECK ESCAPE SLIDE DEPLOYED ACCIDENTLY, BUT DID NOT DEPLOY FULLY, AND DOOR BOTTLE DISCHARGED. SLIDE ASSY REM OVED & REPLACED PER 25-68-07, PG 601, DOOR AIR BOTTLE REMOVED & REPLACED PER MM 25-68-08 AND PRESSURE CARTRIDGE PER 52-2 3-15. 2 L 7 4 4F RT A20WE 2003011400086 20030114 00086 NM 2003 1 14 P5CA0200705 1 20021026 A 3244 260356116 TIRE BOEING 747 7472U3B 1384846 NM NLG OUT OF BALANCE A P5CA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 WP 23 923FT 22769 ON TAKEOFF ROLL FROM RWY 24L-ANC, A VIBRATION BEGAN & INCREASED IN INTENSITY. AT 100 KTS IT BECAME VERY SEVERE. T/O WA S REJECTED AT 110 KTS. VIBRATION SEEMED MOST SEVERE IN NOSE GEAR REGION OR MAIN GEAR. DURING DECELERATION, A/C PULLED TO THE RIGHT. PERFORMED AIRFRAME VIBRATION INSPECTION IAW BMM 05-51-38. NOSE TIRE FOUND TO BE OUT OF BALANCE. REMOVED & REPLACED RIGHT NOSE TIRE WHEEL ASSY IAW BMM 32-45-02. SPIN & AXLE CHECK GOOD. 2 L 7 4 4F RT A20WE 2003011400087 20030114 00087 NM 2003 1 14 P5CA0200706 1 20021027 A 5230 65B0732926 ROD BOEING 747 747200 1384847 NM CARGO DOOR BROKEN A P5CA K NONE O OTHER TX TAXI/GRND HDL 1 WP 23 524UP 21446 DURING OFF LOADING OPERATIONS, LWR AFT CARGO DOOR EXPERIENCED AN OUT OF SEQUENCE CONDITION. UPON INSPECTION FOUND SEVEN ROD ASSYS HAD SHEARED & THE MOST FORWARD DOOR INSPECTION PANEL WAS DAMAGED. REMOVED & REPLACED ROD ASSYS & INSPECTION DOOR PANEL AS PER 52-34-00. PERFORMED DOOR OPERATION CHECK AS PER MM 52-34-00. OPS OK. 2 L 7 4 4F RT A20WE 2003011400090 20030114 00090 NM 2003 1 14 P5CA0200707 1 20021103 A 5755 65B0225049 PANEL BOEING 747 747283B 1384867 NM SPOILER DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 ON POST-FLT INSPECTION, NR 9 SPOILER PANEL WAS FOUND TO BE DAMAGED (POSSIBLE DELAMINATION). REMOVED & REPLACED NR 9 SPO ILER PANEL IAW AMM 27-61-00. OPERATIONAL CHECK SATISFACTORY. 2 L 7 4 4F A20WE 2003011400092 20030114 00092 GL 2003 1 14 P5CA0200709 1 20021121 A 3610 65B945321 DUCT BOEING 747 747300 GL GE CF6 CF650E2 30018 NE NR 4 ENGINE SEPARATED A P5CA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 WP 23 354MC 23394 530273 NR 4 ENG - FIRE INDICATION AFTER TAKEOFF IN CLIMB. PRECAUTIONARY ENGINE SHUTDOWN & FUEL DUMP PERFORMED. FIRE BOTTLE NO T REQUIRED. FOUND 8TH STAGE BLEED CROSSOVER DUCT SEPARATED FROM DUCTING SYSTEM. REPLACED WITH CROSSOVER DUCT & PRECOOL ER DOWNSTREAM DUCT. PRSOV & PRESSURE RELIEF VLV REPLACED, ALSO AS PRECAUTION PER MM 36-11-01, PG 401. ADDT'L 16 PIECE PARTS REPLACED DUE TO DAMAGE DURING DUCT LIBERATION. HIGH STAGE VALVE LOCKED CLOSED FOR DISPATCH PER DDPG DUE NOT READI LY AVAILABLE. HIGH POWER R/U PERFORMED WITH ALL DUCTING WRAPPED WITH FOIL. AFTER R/U, LEAK CHECK WAS NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 2003011400093 20030114 00093 NM 2003 1 14 P5CA0200710 1 20021203 A 3350 S136B37 LIGHT BOEING 747 747200 1384847 NM CABIN INOPERATIVE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 524UP 21446 UPPER DECK FWD EMERGENCY LIGHT WOULD NOT STAY ILLUMINATED. REPLACED EMERGENCY LIGHT ASSY & OPERATIONS RETURNED TO NORMA L. 2 L 7 4 4F RT A20WE 2003011400094 20030114 00094 NM 2003 1 14 CA021121002 1 20021120 A 5700 FAIRING BOEING 747 747475 NM GE CF6 CF680C2D1F 30025 NE WING TE FLAP DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PANELS 462EL AND 462FL FOUND MISSING OFF NR 2 ENGINE PYLON AND NR 1 TRAILING EDGE FLAP AND CANOE FAIRING FOUND DAM AGED ON WALK AROUND. AIRCRAFT WAS ON A DELIVERY FLIGHT AFTER HAVING UNDER GONE A HEAVY MAINTENANCE VISIT IN SINGAPORE. A IRCRAFT RELEASED FROM WITH CANOE AND FLAP TEMPORARY REPAIRED AND MISSING PANELS DEFERRED UNDER MEL INTERNAL INVESTIGATIO N CALLED AS TO CAUSE OF EVENT 2 L 7 4 4F 4 F RT A20WE E31N3 2003011400095 20030114 00095 NM 2003 1 14 P5CA0200711 1 20021206 A 7330 INDICATOR BOEING 747 7472D3B 1384805 NM GE CF6 CF680C2* GL COCKPIT MALFUNCTIONED A P5CA E ENGINE SHUTDOWN N FALSE WARNING LD LANDING 1 WP 23 505MC 21251 517353 ON LANDING & AFTER T/R'S STOWED, NR 3 ENGINE FUEL FLOW SPIKED. PRECAUTIONARY ENGINE SHUTDOWN PERFORMED IMMEDIATELY. F/ F INDICATION REMAINED AT 12000 PLUS. PERFORMED BITE CHECK OF F/F SYSTEM. OPERATED NR 3 ENGINE, ALL PARAMETERS NORMAL P ER MM 71-00-00 & MM 78-31-00. 2 L 7 4 4F 4 F RT A20WE E23EA 2003011400096 20030114 00096 NM 2003 1 14 CA021122005 1 20021107 A 7830 THRUST REVERSER BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE DAMAGED W O OTHER O OTHER LD LANDING 1 CA (CAN) ON LANDING IT WAS OBSERVED THE TRAIL SKID INDICATOR ILLUMINATED INDICATING A TAIL STRIKE. THE AIRCRAFT HAD LANDE D WITHOUT INCIDENT. A DETAILED INSPECTION FOUND DAMAGE TO THE FOLLOWING: TAIL SKID ASSEMBLY, NR 3 VHF COMM. ANTENNA, N R 2 ENGINE THRUST REVERSER & TAILPIPE. NR 2 ENGINE BORESCOPE CARRIED OUT AND CHECKED SERVICEABLE. HARD LANDING CHECK C ARRIED OUT IAW MM & CHECKED SERVICEABLE. TAIL SKID ASSEMBLY REPLACED & CHECKED SERVICEABLE IAW MM. NR 3 VHF COMM ANTEN NA REPLACED & FUNCTIONED SERVICEABLE IAW MM. NR 2 ENGINE THRUST REVERSER ASSY REPLACED & CHECKED SERVICEABLE IAW MM. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2 L 7 3 4F 4 F A3WE E2EA 2003011400098 20030114 00098 NE 2003 1 14 P5CA0200712 2 20021214 A 7250 FRAME BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 355MC 23395 455793 A 2 INCH CRACK FOUND, NR 3 ENGINE, TURBINE MID FRAME HOT SECTION AT NR 7 TIME (10 O'CLOCK POSITION). CRACK WELDED IAW G E SOPM 70-41-00. REF EDA 7254E001. 2 L 7 4 4F 4 F RT A20WE E23EA 2003011400099 20030114 00099 NM 2003 1 14 P5CA0200713 1 20021214 A 5730 65B14963916 SKIN BOEING 747 747341 13848AM NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 355MC 23395 DELAMINATION FOUND ON RT WING UPPER SURFACE LEADING EDGE COVER (NU-CAP) PANEL AT WING STATION 557 & HAS 3 FEET X 6 INCHE S OF EXPOSED HONEYCOMB. REPLACEMENT PANEL INSTALLED IAW SRM 51-30-02. FILLET SEAL APPLIED TO EDGE OF PANEL IAW SRM 51- 10-06. 2 L 7 4 4F RT A20WE 2003011400100 20030114 00100 NM 2003 1 14 SWAA023016 1 20021228 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED 5Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2003011400101 20030114 00101 NM 2003 1 14 SWAA023017 1 20021227 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROW NR 10 AND ROW NR 13. RECONNECTED WIRE PER MM. 2 L 7 2 4F RT A16WE 2003011400102 20030114 00102 NM 2003 1 14 SWAA023019 1 20021228 A 3350 AD20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED A2 CHECK, FOUND AFT LT EXTERIOR EMERGENCY EXIT LIGHT AND 3 EA INTERIOR OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED MID CABIN BATTERY PACK AND BATTERY CHARGER BASE ASSY PER MM. 2 L 7 2 4F RT A16WE 2003011400103 20030114 00103 NM 2003 1 14 SWAA023020 1 20021224 A 3350 AD20131A BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 704SW 27838 DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL EMERGENCY LIGHTS INOP THROUGH OUT CABIN. REMOVED AND REPLACED MID CABIN B ATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2003011400104 20030114 00104 NM 2003 1 14 SWAA023027 1 20021227 A 2560 P2070001 FLASHLIGHT BOEING 737 7373TO 138447G NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 697SW 23838 EMERGENCY FLASHLIGHT AT AFT CABIN STATION INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2003011400105 20030114 00105 NM 2003 1 14 SWAA023028 1 20021229 A 3350 D71701400 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 783SW 29809 DURING SCHEDULED RON CHECK, FOUND FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2003011400106 20030114 00106 2003 1 14 SWAA023032 4 20021230 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 2003011400107 20030114 00107 NM 2003 1 14 SWAA023033 1 20021229 A 3350 604222 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 722WN 22698 AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM. 2 L 7 2 4F A16WE 2003011400108 20030114 00108 NM 2003 1 14 SWAA023037 1 20021229 A 3350 6556633 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT AFT BULB INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2003011400109 20030114 00109 2003 1 14 SWAA023039 4 20021230 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM AFT ENTRY DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLID E PER MM. 2 L 7 2 4F RT A16WE 2003011400110 20030114 00110 2003 1 14 SWAA023042 4 20021230 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2003011400111 20030114 00111 NM 2003 1 14 SWAA023044 1 20021231 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT CRACKED AT T/E EDGE. REMOVED AND REPLACED NR 1 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2003011400112 20030114 00112 2003 1 14 SWAA023045 4 20021230 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2003011400113 20030114 00113 NM 2003 1 14 SWAA023047 1 20021231 A 3350 900835A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED A1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT MID CABIN. REMOVED AND REPLACED EXIT LIGHT BATTE RY PER MM. 2 L 7 2 4F A16WE 2003011400120 20030114 00120 NE 2003 1 14 CA021122007 2 20021107 A 7321 7045402L2 FUEL CONTROL SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE NR 2 ENGINE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) A/C DEPARTED WITH A 13,000 LB LOAD OF LOGS, COLLECTIVE WAS LOWERED TO DECREASE ENGINE POWER. CREW HEARD A SWOOSH S OUND & NR 2 ENG N1 UNDER-SPEED WARNING SOUNDED & WARNING LIGHTS ILLUMINATED INDICATING A SOFT STALL. JETTISONED LOAD AN D EXECUTED INFLIGHT SHUTDOWN AND MOTORING OF ENG TO PREVENT OVERTEMP. NR 2 ENG SHUTDOWN COMPLETE, A/C MADE AN UNEVENTFUL SINGLE ENG LANDING. COMPLETE INSPECTION OF ENG & CONTROL LINKAGES REVEALED NOTHING ABNORMAL. ENGINE FUEL FILTER WAS IN SPECTED FOR CONTAMINATION. ENGINE FUEL CONTROL UNIT & THE FUEL PRESSURING AND DUMP VALVE WERE CHANGED. ENGINE WAS RESTAR TED AND GROUND RUN TO CHECK ALL ENG OPERATING PARAMETERS. ALL PARAMETERS WERE OK AND A/C WAS RELEASED FOR FLIGHT. 2 G 7 2 4U 4 U H4EA E15EA 2003011400128 20030114 00128 NE 2003 1 14 CA021125004 2 20021006 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT FAILED W C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 CA 10869 (CAN) WHILE ADVANCING POWER LEVERS (APPROXIMATELY 50 PERCENT N1 ONLY) TO INITIATE T/O ROLL, FLIGHT CREW NOTICED A HOT IC ON AND EXCESSIVE ITT READINGS ON THE RT ENGINE. CONTRACT MAINTENANCE LOOKED AT THE MDC EXCEEDENCE PAGE AND REPORTED THE RT ENGINE EXPERIENCED TWO EXCEEDENCES: ITT = 1187OC FOR 5 SECONDSVIB = 3.1 MILS FOR .2 SECONDS DURING INSPECTION EXCESSI VE COMPRESSOR AND VG BLADE DAMAGE AND METAL FOUND IN THE JETPIPE. ENGINE CHANGED AND SHIPPED TO GE. 2 L 7 2 4F 4 F RT A21EA E15NE 2003011400129 20030114 00129 SW 2003 1 14 CA021125005 1 20021114 A 2910 994043 SEAL BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL HYD PACK LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) N2 TACH DRIVE SIDE OFF OF THE HYDRO-PACK WAS LEAKING HYDRAULIC FLUID. 1 G 7 1 3U 3 U H2SW E4CE 2003011400131 20030114 00131 WP 2003 1 14 CA021125007 1 20021119 A 6220 369H120321 LINK HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ROTOR HEAD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE PERFORMING A 300 HOUR INSPECTION ON THE AIRCRAFT THE AME NOTICED A CRACKED LUG ON THE LEAD LUG LINK. AD 95-0 3-13 CALLS FOR A REPETITIVE 15 HOUR INSPECTION OF THIS AREA. 1 G 7 1 3U 3 U H3WE E4CE 2003011400138 20030114 00138 WP 2003 1 14 CA021126001 1 20021123 A 7810 A10601X EXHAUST PIPE DOUG DC4 C54GDC 3021534 WP PWA R2000 D3 52023 NE NR 2 ENGINE FAILED W E ENGINE SHUTDOWN A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 CA (CAN) DURING TAKE-OFF, THE FIRE WARNING WENT OFF FOR NR 2 ENGINE. THE PILOT LOOKED OUT HIS WINDOW AND NOTICED AN ORANGE GLOW. SHUT DOWN THE ENGINE AND THE FIRE WENT OUT. CONTINUED TO BASE WHERE IT WAS NOTICED THAT THE EXHAUST SEGMENT HAD CO ME APART AND HAD BURNED THROUGH THE CARB AIR SCOOP. THE CARB AIR SCOOP AND THE EXHAUST SEGMENT WERE CHANGED. 2 L 7 4 4R 4 R A762 E230 2003011400139 20030114 00139 EU 2003 1 14 CA021126002 1 20021126 A 2910 10546682 SERVO VALVE BOLKMS 117 BK117A1 5626010 EU HYD SYSTEM CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) HYDRAULIC UNIT RECEIVED FROM THE USA. UNIT SENT FOR SCHEDULED INSPECTION AND REPAIR OF LEAKAGE. DURING FINAL FUNCT ION TEST IT WAS NOTED THAT SYSTEM NR 1 LONGITUDINAL ACTUATOR SERVO VALVE CENTERING PLAY EXCEEDED THE LIMIT. ACTUATOR DI SASSEMBLED AND SERVO VALVE CONNECTING HEAD WAS CRACKED. TOTAL TIME ON HYDRAULIC UNIT 7026.4 HOURS. 1 G 7 2 3U H13EU 2003011400140 20030114 00140 EU 2003 1 14 CA021127001 1 20021120 A 3030 9651112302 HEATER PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL LT PITOT SYS FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) PILOT ADVISED P/S 2 LIGHT CAME ON. A CHECK OF THE SYSTEM SHOWED THAT THE HEATING ELEMENT IN THE LT PITOT STATIC T UBE HAD FAILED. THE PITOT STATIC TUBE WAS REPLACED WITH A NEW UNIT. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2003011400143 20030114 00143 2003 1 14 VNAA0212011 4 20021207 A 3418 STALL WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 472PS 3008 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND SHAKER ON SIDE AND PUSHER FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE SYSTE M THEN RESET ITSELF. FLIGHT 4193 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400145 20030114 00145 NM 2003 1 14 VNAA0212013 1 20021209 A 3250 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 430JS 3044 DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE MESSAGE HAD EXTINGUIS HED AND FLIGHT 4137 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4137 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400147 20030114 00147 SW 2003 1 14 CA021128001 1 20021117 A 2910 2781032755 LINE SWRNGN SA226 SA226TC 8780404 SW HYD PUMP CRACKED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) ON DEPARTURE WHEN THE LANDING GEAR WAS SELECTED UP AND BOTH HYD PRESSURE WARNING LIGHTS ILLUMINATED, LIGHTS EXTING UISHED ONCE THE GEAR WAS UP, SHORTLY AFTER, THE LIGHT ILLUMINATED AGAIN, THE GEAR WAS EXTENDED NORMALLY AND THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. AN INSPECTON REVEALED THAT THE PART NR 27-81032-755 RT ENGINE DRIVEN HYD PUMP D ISCARGE LINE WAS CRACKED IN THE RADIUS OF THE BEND. THERE WAS NO EVIDENCE OF MECHANICAL DAMAGE ON THIS LINE. THE HYD LIN E WAS REPLACED , THE SYSTEM SERVICED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A8SW 2003011400148 20030114 00148 NE 2003 1 14 CA021128002 2 20021110 A 7320 87620097021 ROD DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HMU MISINSTALLED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING 'L' CHECK IT WAS NOTICED THAT NR 2 ENGINE POWER LEVER APPEARED TO NOT MAKE FULL FORWARD TRAVEL. UPON INVEST IGATION, FOUND POWER LEVER BINDING AT FULL PWR SETTING DUE TO HMU TO PCU POWER LEVER ROD ASSEMBLY INSTALLED ON WRONG SI DE OF HMU PWR LEVER. POWER LEVER ROD ASSEMBLY REINSTALLED ON CORRECT SIDE IAW DASH 8 MM CH 76-10-00 FIG 206 PG 218. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011400149 20030114 00149 EA 2003 1 14 CA021129001 1 20021121 A 7830 THRUST REVERSER CNDAIR CL600 CL600* EA LYC ALF502 ALF502L 41580 NE RT ENGINE DAMAGED W A UNSCHED LANDING D J INFLIGHT SEPARATION WARNING INDICATION CL CLIMB 1 CA (CAN) WHILE CLIMBING THROUGH 13,000 FT THE CREW HEARD A LOUD 'BANG' FOLLOWED BY A RT T/R UNLOCK INDICATION. THE CREW RET URNED TO THE POINT OF DEPARTURE AND LANDED WITHOUT INCIDENT. EXAMINATION ON THE GROUND REVEALED THAT THE RT THRUST REVER SER ACTUATOR ATTACHMENT POINTS AT THE TRANSLATING STRUCTURE HAD FAILED. A SECTION OF THE TRANSLATING COWL OUTER SKIN STR UCTURE AT THE 6 O'CLOCK POSITION HAD TORN AWAY & DEPARTED THE AIRCRAFT. THE TRANSLATING STRUCTURE WAS HELD IN PLACE ON THE ENGINE BY THE BLOCKER AND FLIPPER DOOR LINKAGES. THE AIRCRAFT WAS FERRIED TO THE CUSTOMER'S FACILITY FOR REPAIRS. 2 L 7 2 4F 4 F RT A21EA E6NE 2003011400150 20030114 00150 NM 2003 1 14 CA021129003 1 20021121 A 2130 WL1103AMMS10 SERVO BOEING 737 7372L9 1384497 NM PWA JT8 JT8D17A 52049 NE ALTIMETER MALFUNCTIONED W B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CA (CAN) CRUISING FL310, AURAL WARNING FOR PRESSURIZATION SOUNDED, OVERHEAD MASTER CAUTION ILLUMINATED.INITIATED EMERG. DES CENT, PRESSURIZATION CONTROLLED MANUALLY BUT NOT BEFORE MASKS IN CABIN DROPPED. EMERG. DESCENT & RAPID DEPRESSURIZATION CHECKLIST COMPLETED. 2 L 7 2 4F 4 F RT A16WE E2EA 2003011400152 20030114 00152 EA 2003 1 14 CA021129005 1 20021129 A 2760 C670170855 FITTING CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE SPOILER HINGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A SCHEDULE DOWN TIME FOR EICAS 5 MOD PROGRAM FOUND CRACKED FITTING HINGE AT RT INBOARD WS 185.11, THE PART WAS REPLACED BY A NEW ONE AND THE CRACKED FITTING WAS SHIPPED FOR ANALYSIS. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2003011400153 20030114 00153 NM 2003 1 14 CA021129006 1 20021125 A 2910 82950010197 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING OVERNIGHT CHECK HYDRAULIC LEAK NOTICED FROM RT ARMPIT. LOST NR 1 SYSTEM FLUID. MLG DOWN PRESSURE TUBE ASSY IN RT WING REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011400154 20030114 00154 NM 2003 1 14 CA021129008 1 20021126 A 7120 8DK1763001 MOUNT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE LT ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING COMPLETION OF AD CF200120 SMALL CRACK FOUND ON OUTBOARD REAR ENGINE STRUT ON LT ENGINE. BOTH REAR ENGINE S TRUTS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011400155 20030114 00155 GL 2003 1 14 CA021129009 2 20021017 A 7261 23053320 SEAL BELL 206 206A 1181508 SW ALLSN 250C 250C20 03013 GL ENGINE OIL WARPED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) AME INSTALLED TURBINE ASSEMBLY FOLLOWING REPAIR. ON GROUND RUN, OIL LEAK WAS OBSERVED BETWEEN PT SUPPORT AND THE EXTERNAL OIL SUMP. SUMP WAS REMOVED AND SEALING FLANGE INSPECTED WITH A STRAIGHT EDGE. SEALING FLANGE WAS WARPED EXCESS IVELY (CRUSH SEAL FAILED TO PREVENT OIL LEAK). AME REPLACED EXTERNAL OIL SUMP AND CRUSH SEAL. A/C RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 2003011400156 20030114 00156 NE 2003 1 14 CA021129010 2 20021127 A 7210 GEARBOX DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 REDUCTION MAKING METAL W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA (CAN) DURING A LINE CHECK FOUND NR 2 REDUCTION GEARBOX CHIP DETECTOR FLAGGED. NON ALLOWABLE CATEGORY 3 DEBRIS FOUND ON DETECTOR AND IN SCAVENGE FILTER. NR 2 ENGINE AND REDUCTION GEARBOX ASSEMBLIES REPLACED 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011400157 20030114 00157 GL 2003 1 14 CA021129011 2 20021007 A 7261 6848194 CONNECTOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE OIL LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) AME INSTALLED TURBINE ASSEMBLY FOLLOWING OVERHAUL. ON GROUND RUN SEVERE OIL LEAK WAS OBSERVED FROM 6 & 7 PRESSUR E OIL CONNECTOR ('TEE FITTING) AREA. INSPECTION REVEALED THAT TWO RETAINING BOLTS HAD LESS THAN 10 IN/LBS. BREAK TORQUE . AME REPLACED CRUSH SEALS, REASSEMBLED TUBING AND AFTER SATISFACTORY GROUND RUN, RETURNED A/C TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 2003011400158 20030114 00158 NE 2003 1 14 CA021201001 2 20021125 A 7261 SHAFT GE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE SCAVENGE PUMP BROKEN W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 15429 NMAAD228 (CAN) A ' RT ENG OIL PRESS' CAUTION MESSAGE INDICATED DURING CLIMB. THE OIL PUMP DRIVE SHAFT WAS FOUND BROKEN. THE ENGIN E WAS REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2003011400159 20030114 00159 2003 1 14 CA021202001 4 20021122 A 3425 6229682004 DISPLAY CESSNA 441 441 2076020 CE COCKPIT FAILED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION DE DESCENT 1 CA (CAN) MOMENTARY INTERMITTENT FAILURE IN DESCENT. 'DPU FAILURE' MESSAGE WOULD BE SHOWN. AND IAT WOULD SHUTDOWN, THEN COME BACK ON LINE. NOTE: THIS IS THIRD TIME UNIT. HAS BEEN REMOVED AND SENT TO MANUFACTURER. MANUFACTURER HAS BEEN UNABLE TO DUPLICATE THE PROBLEM BUT NOW HAS SUPPLIED US WITH A REPLACEMENT UNIT. 1 L 7 2 3T RT A28CE 2003011400160 20030114 00160 2003 1 14 CA021202002 4 20020725 A 3457 0110055010 GPS CESSNA 441 441 2076020 CE COCKPIT INTERMITTENT W O OTHER O OTHER CR CRUISE 1 CA (CAN) GPS FUNCTION FAILS INTERMITTENTLY. 1 L 7 2 3T RT A28CE 2003011400161 20030114 00161 2003 1 14 CA021202003 4 20020917 A 3451 6221233001 TRANSPONDER CESSNA 441 441 2076020 CE COCKPIT FAILED W O OTHER O OTHER CR CRUISE 1 CA (CAN) INTERMITTENT FAILURE, DISPLAY UNITS WOULD GIVE ----- OR 8888 INSTEAD OF CORRECT SPEED OR DISTANCE DISPLAY. NOTE: 2 CAUSES WERE FOUND: (1) INTERMITTENT FAILURE OF IL IN THE DME 40 UNIT. (2) GNS 530 CHANNELING WAS INCORRECTLY PROGRAME D CAUSING THE DME NOT TO FUNCTION ON SOME CHANNELS. 1 L 7 2 3T RT A28CE 2003011400162 20030114 00162 NE 2003 1 14 CA021202004 1 20021118 A 2910 S548C2C165000 LINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL HYD SYSTEM LEAKING W E D ENGINE SHUTDOWN RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) THE AIRCRAFT LOST PRESSURE IN NR 2 HYDRAULIC DURING TAXI, AFTER SHUT DOWN NR 2 SYSTEM INDICATOR WAS AT EMPTY AND H YDRAULIC OIL WAS FOUND ON DECK UNDER MGB, PIN HOLE WAS FOUND ON ABOVE MENTIONED FLEX LINE. LINE WAS REPLACED AND NR 2 HY DRAULIC SYSTEM SERVICED. 10 MINUTES GROUND RUN AND LEAK CHECK CARRIED OUT. AIRCRAFT RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2003011400163 20030114 00163 CE 2003 1 14 CA021202005 1 20021118 A 5540 504200337 BEAM BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA RUDDER SUPPORT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 21788 (CAN) PILOTS RUDDER QUADRANT SUPPORT BEAM FOUND CRACKED AT ROUTINE INSPECTION. BEAM REPLACED 1 L 7 2 3T 4 T A14CE E4EA 2003011400164 20030114 00164 NM 2003 1 14 VNAA0212015 1 20021209 A 2612 3280170 CONTROL PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAULTY A VNAA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 07 471PS 2661 1766 3007 THE CREW REPORTED THAT THE CARGO FIRE TEST WAS INOP AND THE CREW DEFERRED THIS WITH MAINTENANCE CONTROL USING 26-6C. W HEN THE AIRCRAFT ARRIVED IN PIT, MAINTENANCE INSPECTED AND REPLACED THE FIRE DETECTION PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400165 20030114 00165 NM 2003 1 14 VNAA0212016 1 20021209 A 2612 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FIRE DETECTION MALFUNCTIONED A VNAA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 07 427JS 3039 THE CREW REPORTED THAT THE APU FIRE DETECTION SYSTEM WAS INOP. THE CREW DEFERRED THIS WITH MAINTENANCE CONTROL USING 49 -1C. UPON ARRIVAL AT CAK, MAINTENANCE INSPECTED AND TROUBLESHOT THE SYSTEM BUT WAS UNABLE TO DUPLICATE THE PROBLEM OR F IND ANY FURTHER DISCREPANCIES. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400166 20030114 00166 NE 2003 1 14 CA021203001 2 20021129 A 7261 726201 SHROUD BOEING 757 757* NM RROYCE RB211 RB211535E4 54555 NE ENGINE FRACTURED W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) FLT 1974, MBJ-CLT, DIVERTED TO MIA WHILE PASSING OVER URSUS (CUBA) IN STRAIGHT AND LEVEL CRUISE, THE FIRST OFFICE R NOTICED THE OIL PRESSURE LIGHT FLICKER. IN VERY SHORT ORDER, OIL QUANTITY WENT TO ZERO FOLLOWED BY OIL PRESSURE. ENGI NE SHUTDOWN PROCEDURE WAS CONSULTED WITH TWO MINUTES ELAPSING FROM ZERO OIL PRESSURE AND COMMANDED SHUTDOWN. ALL OTHER ENGINE PARAMETERS WERE REPORTED NORMAL UP TO THE POINT OF SHUTDOWN. AIRCRAFT LANDED UNEVENTFULLY AT MIA WITH NINETEEN M INUTES SINGLE ENGINE TIME. POST INSPECTION REVEALED THE UPPER RADIAL DRIVE SHAFT SHROUD HAD FRACTURED 360 DEGREES AROUN D UPPER TUBE. A PIECE OF BEARING CAGE WAS RECOVERED, PROBABLE SOURCE FROM STEADY BEARING ASSEMBLY ENGINE REMOVED AND E 2 L 7 2 4F 4 F RT A2NM E12EU 2003011400167 20030114 00167 NM 2003 1 14 VNAA0212017 1 20021211 A 2611 SMOKE WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FALSE ACTIVATION A VNAA O OTHER N FALSE WARNING AP APPROACH 1 GL 07 462PS 3084 THE CREW REPORTED RECEIVING A LAV SMOKE CAS MESSAGE DURING FINAL THERE WAS NO SMOKE, JUST AN ERRONEOUS MESSAGE. MAINTEN ANCE CONTROL AND THE CREW DEFERRED THE LAV SMOKE DETECTION SYSTEM WITH 26-3 CODE C. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400168 20030114 00168 NM 2003 1 14 VNAA0212019 1 20021212 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 463PS 14898 58 3087 THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 1, 2, AND 3 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPL ACED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORME D AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400169 20030114 00169 NM 2003 1 14 VNAA0212020 1 20021213 A 3040 328510 CONTROLLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 423JS 15729 1182 3032 THE CREW RECEIVED A FIRST OFFICER WINDSHIELD HEAT FAIL CAS MESSAGE. THE CREW THEN FOLLOWED THE QUICK REFERENCE HANDBOOK AND CALLED MAINTENANCE CONTROL. FLIGHT 4056 WAS THEN INSTRUCTED TO RETURN TO CAK. MAINTENANCE INSPECTED AND REPLACED THE FIRST OFFICER'S WINDSHIELD HEAT CONTROLLER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-00-00. OPERATIONAL CHEC KS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400170 20030114 00170 2003 1 14 CA021203002 4 20021128 A 6122 5008016 FLYWEIGHT WOODWARD 210718 RKWELL 700 700 7630520 SW LYC O540 TIO540R2AD 41532 EA HARTZL HCE3Y HCE3YR2A GL PROP GOVERNOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 1296026BL (CAN) GOVERNOR WAS BENCH CHECKED & FOUND TO HAVE ABOUT A 30-RPM OVER SPEED WITH FULL CONTROL OF GOVERNOR OVER ENTIRE R PM RANGE. GOVERNOR WAS DISASSEMBLED, FOUND FLYWEIGHT HAD PARTIALLY FAILED. DRIVE SPRING WAS DISCONNECTED FROM DRIVER, AL LOWING FLYWEIGHT HEAD TO ROTATE AGAINST ENDS OF 2 SCREWS. CAUSING END OF SCREWS TO SHEAR OFF. 1 L 7 2 3O 3 O A12SW E14EA 5 C P33EA 2003011400172 20030114 00172 CE 2003 1 14 CA021203004 1 20021128 A 3260 327 BULB BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA HARTZL HCB4T HCB4TN3 GL MLG INDICATOR BURNED OUT W O OTHER N FALSE WARNING DE DESCENT 1 CA (CAN) A/C HAD AN INTERMITTENT LT MLG DOWN LIGHT INDICATION. TROUBLESHOOTING REVEALED THAT THE FILAMENT IN THE 327 BULB APPEARED TO BE BROKEN AND WAS INTERMITTENTLY CONTACTING. COMPLETE ASSEMBLY WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE . 1 L 7 2 3T 4 T A14CE E4EA 6 C P40EA 2003011400173 20030114 00173 SW 2003 1 14 CA021203005 1 20021203 A 6510 206040015103 DRIVE SHAFT BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL TAIL ROTOR OVERTEMP W K NONE M OVER TEMP IN INSP/MAINT 1 CA (CAN) THE PILOT NOTICED ON HIS DAILY INSPECTION THAT THE DRIVESHAFT TEMPLATES ON THE TRANSMISSION SIDE WERE ALL BLACK, I NDICATING AN OVERTEMP ON THE COUPLING. THIS OCCURRED 4 HOURS AFTER THE 600 HOUR LUBRICATION INSPECTION OF THE DRIVESHAFT . AFTER CLOSE INSPECTION THERE WERE NO INDICATIONS OF IMPROPER GREASING. THE DRIVESHAFT WAS INSPECTED/REGREASED AND PUT INTO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 2003011400174 20030114 00174 NM 2003 1 14 CA021203006 1 20021114 A 2810 SKIN ROBSIN R22 R22BETA 7640110 NM LYC O360 O360J2A 41514 EA FUEL TANK CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) SKIN CRACKED AT LOWER OUTBOARD CORNER OF FUEL TANK, CRACK TERMINATES AT RIVET HOLE, RESULT WAS A FUEL LEAK. 1 G 7 1 3O 3 O H10WE E286 2003011400175 20030114 00175 NM 2003 1 14 VNAA0212021 1 20021214 A 2450 230GC02Y02 CONTROL PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 439JS 410 109 3057 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL CAS MESSAGE AND ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE WAS DISPATCHED TO PHL, INSPECTED, AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 2 4-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400177 20030114 00177 NM 2003 1 14 VNAA0212023 1 20021216 A 3243 MASTER CYLINDER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT CONTAMINATED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 472PS 3008 THE CREW REPORTED THAT THE FIRST OFFICER'S LEFT HAND BRAKE GOES TO THE PEDAL STOP. OUTSTATION MAINTENANCE INSPECTED AND BLED THE FIRST OFFICER'S MASTER CYLINDERS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS W ERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400178 20030114 00178 NE 2003 1 14 VNAA0212025 2 20021219 A 7532 311995704 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 471PS 7928 3007 DURING TAKEOFF, THE CREW EXPERIENCED A TORQUE JUMP AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HA ND INTERCOMP BLEED VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 75-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400179 20030114 00179 NM 2003 1 14 CA021203008 1 20021201 A 2497 669236 GUIDE BOEING 747 747433 NM PWA 4056 PW4056 NE CONNECTOR PLUG FAILED W K NONE W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) STRONG ELECTRICAL BURNING ODOR IN COCKPIT AFTER EXTERNAL POWER APPLIED. INVESTIGATION REVEALED THAT ONE PHASE OF T HE GPU PLUG WAS APPLIED TO THE NEUTRAL WIRE OF THE RECEPTACLE. THIS IS POSSIBLE TO DO IF THE PLUG IS INSERTED INCORRECTL Y AND A RESET IS SELECTED ON THE GPU. ALSO IT IS POSSIBLE TO INSTALL THE PLUG OFFSET HORIZONTALLY AND VERTICALLY. OUR FI X AND WITH OUR PREVIUOUS INCIDENT OF THE SAME NATURE A YEAR AGO, WE ARE GOING TO INSTALL A MORE RIGID GUIDE , THE SAME A S THE 767 WITH NO CUT OUT. 2 L 7 4 4F 4 F RT A20WE E24NE 2003011400180 20030114 00180 SW 2003 1 14 CA021203012 1 20021203 A 6320 205040249001 BEARING BELL BELL 412 412 1182202 SW TRANSMISSION SPALLED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA A250 (CAN) TRANSMISSION REMOVED BECAUSE OF CHIP INDICATIONS. BEARING FOUND SPALLED ON INPECTION. 1 G 7 2 4U H4SW 2003011400181 20030114 00181 EA 2003 1 14 CA021204001 2 20021123 A 7321 3028325 LINE BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA P3 AIR FILTER BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE GOVERNOR WAS LAGGING BEHIND. THE ENGINEER CARRIED OUT SOME ADJUSTMENTS BUT THE ADJUSTMENTS DID NOT HELP. A P3 AIR LEAK CHECK WAS CARRIED OUT AND THE ENGINEER DISCOVERED AIR LEAKING NEAR THE P3 AIR FILTER. FURTHER INVESTIGATION REV EALED THE LINE WAS BROKEN THAT WENT FROM THE P3 AIR FILTER TO A FI TTING AND FROM THE FITTING ENDING UP AT THE FUEL CONT ROL. 1 G 7 1 4U 4 U H4SW E22EA 2003011400182 20030114 00182 NE 2003 1 14 CA021204002 3 20021114 A 6110 A2431 BOLT SOCATA TBM TBM700 8682000 EU HARTZL HCE4N HCE4N3 NE PROPELLER ASSY FAILED W K NONE O OTHER IN INSP/MAINT 1 CA HH50 (CAN) DURING PROPELLER OVERHAUL, BOLT PN A2431 WAS MAGNAFLUXED AND FOUND A CRACK INDICATION RUNNING LENGTH WISE ON THE BOLT THREADS. NEW BOLT INSTALLED. 1 L 7 1 3T RT A60EU 5 C P10NE 2003011400183 20030114 00183 NE 2003 1 14 CA021204003 3 20021114 A 6111 A65 DOWEL PIN HARTZL SOCATA TBM TBM700 8682000 EU HARTZL HCE4N HCE4N3 NE COUNTERWEIGHT BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA H39703 (CAN) DURING OVERHAUL A BROKEN COUNTERWEIGHT DOWEL PIN WAS DISCOVERED. NEW INSTALLED. 1 L 7 1 3T RT A60EU 5 C P10NE 2003011400184 20030114 00184 EU 2003 1 14 CA021204004 1 20021114 A 6123 B476 SLEEVE SOCATA TBM TBM700 8682000 EU HARTZL HCE4N HCE4N3 NE PROPELLER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) MAG PARTICAL INSPECTION FOUND CRACK INDICATION ON THE B476 SLEEVE UNIT AT THE SLOTTED END ABOUT 1/8 INCH LONG. HAR TZELL SERVICE BULLETIN 61235 INCORPORATED. 1 L 7 1 3T RT A60EU 5 C P10NE 2003011400185 20030114 00185 NM 2003 1 14 VNAA0212027 1 20021221 A 2810 40006 PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT MALFUNCTIONED A VNAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 432JS 365 96 3045 DURING FLIGHT THE CREW RECEIVED A LEFT HAND FEEDER LOW CAS MESSAGE AND DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLA CED THE REFUEL/DEFUEL PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED A ND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400187 20030114 00187 NM 2003 1 14 VNAA0212029 1 20021224 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 463PS 15464 50 3087 THE CREW REPORTED THAT THE FIRST SECTION OF EMERGENCY LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATION CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400188 20030114 00188 CE 2003 1 14 CA021204006 1 20021128 A 3240 133893 STATOR BFGOODRICH CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE BRAKE ASSY BROKEN W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 0063 (CAN) AFTER LANDING, WHILE TAXING THE A/C MADE A SUDDEN UNCOMMANDED RT TURN DUE TO A SEIZED RT WHEEL. MAINTENANCE PERSO NAL DETERMINED THE BRAKE ASSY WAS JAMMED ON DUE TO A CRACKED STATOR PLATE. THE BRAKE ASSY WAS RETURNED FOR INVESTIGATION . 1 L 7 2 4F 4 F A22CE E1NE 2003011400189 20030114 00189 SO 2003 1 14 CA021204007 1 20021129 A 2450 454656 CIRCUIT BREAKER PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA CB PANEL CRACKED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA (CAN) MAIN VOLTAGE REGULATOR 5 AMP CIRCUIT BREAKER. AUXILIARY VOLTAGE REGULATOR 5 AMP CIRCUIT BREAKER. BOTH CB'S HAD C RACKED TERMINALS. THIS CONDITION DID NOT CAUSE THE CB'S TO 'POP', BUT DID CAUSE SYSTEM TO SHUT DOWN. 1 L 7 2 3O 3 O A20SO E14EA 2003011400191 20030114 00191 2003 1 14 VNAA0212030 4 20021225 A 3418 WARNING SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 426JS 3038 AFTER THE POWER LEVERS WERE ADVANCED, THE CREW RECEIVED A ANGLE OF ATTACK FAIL MESSAGE AND ABORTED TAKEOFF. THE MESSAGE EXTINGUISHED BY ITSELF AND FLIGHT 4172 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4172 THEN DEPARTED WITH NO FURT HER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400193 20030114 00193 NM 2003 1 14 VNAA0212031 1 20021225 A 5270 870004MODB PSEU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE WARNING SYSTEM FAILED A VNAA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 422JS 15040 3018 DURING CLIMBOUT, THE CREW RECEIVED A UNSAFE CABIN DOOR INDICATION AND RETURNED TO DAY. MAINTENANCE INSPECTED AND FOUND CODE A06 ON THE PSEU. MAINTENANCE THEN REPLACED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400194 20030114 00194 NM 2003 1 14 VNAA0212032 1 20021225 A 5270 TARGET DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE GALLEY DOOR OUT OF ADJUST A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 436JS 3052 EN ROUTE, THE CREW RECEIVED A GALLEY DOOR OPEN MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND LANDED BAC K AT PIT. MAINTENANCE INSPECTED AND FOUND THE TARGET A 1/4 LOOSE. THE AIRCRAFT WAS THEN FERRIED TO CAK. MAINTENANCE THEN ADJUSTED THE TARGET IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400195 20030114 00195 NM 2003 1 14 VNAA0212034 1 20021226 A 3243 S4340200001 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MLG FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 441JS 21284 13978 3059 EN ROUTE, THE CREW RECEIVED A PARKING BRAKE ACCUMULATOR PRESSURE LOW CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO ROC. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PARKING BR AKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WA S RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400197 20030114 00197 NM 2003 1 14 VNAA0212035 1 20021228 A 2121 FAN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY FAILED A VNAA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 441JS 3059 THE CREW REPORTED A BURNING SMELL IN THE COCKPIT AREA. THEN THE AVIONICS FAN FAILED. MAINTENANCE INSPECTED THE AVIONIC S FAN AND FOUND IT DID FAIL. MAINTENANCE CONTROL THEN DEFERRED THE AVIONICS FAN WITH THE CREW USING CODE 21-6 B. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400198 20030114 00198 NE 2003 1 14 CA021205001 2 20021129 A 7230 COMPRESSOR AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211TRENT77 NE NR 2 ENGINE DAMAGED W D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 CA 41089 (CAN) NR 2 ENGINE STALL & FLAMED OUT WHILE TAXIING, AIRCRAFT RETURNED TO GATE. AFTER BOROSCOPE INSPECTION, FOUND 6TH ST AGE OF HPC DAMAGE. 2 L 7 2 4F 4 F RT A46NM E39NE 2003011400199 20030114 00199 EU 2003 1 14 CA021205002 1 20021205 A 5260 5521012312 SHOCK MOUNT PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL PAX DOOR STEP FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) SHOCK STRUT WOULD NOT DAMPEN THE STEPS AS THE PASSENGER DOOR IS LOWERED.SHOCK STRUT REPLACED WITH NEW. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2003011400200 20030114 00200 CE 2003 1 14 CA021205005 1 20021203 A 2820 99920000115 LINE BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA FUEL SYSTEM CHAFED W K NONE W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 CA (CAN) AIRCRAFT WAS INSPECTED FOR FUEL LEAK IN LT NACELLE AREA. PROBLEM WAS CAUSED BY A 'CHAFED' FUEL LINE. THE CHAFIN G WAS CAUSED BY A FUEL BOOST PUMP POWER WIRE THAT WAS ROUTED IN THE SAME HOLE AS THE FUEL LINE.THERE WAS NO PROTECTIVE M ATERIAL BETWEEN THE WIRE AND THE TUBE. THE WIRE WAS ALSO CHAFED THROUGH TO THE BARE WIRE AND SLIGHT EVIDENCE OF ARCING WAS FOUND IN THE CHAFED AREA.TUBE REPLACED, WIRE REPAIRED AND PROTECTIVE MATERIAL INSTALLED TO PREVENT FUTURE CHAFING. 1 L 7 2 3T 4 T A14CE E4EA 2003011400201 20030114 00201 EU 2003 1 14 CA021206001 1 20021203 A 6220 134615P BUSHING BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE ROTOR HEAD WORN W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) PRIMARY BUSHING WAS NOT FULLY INSTALLED INTO THE BLADE. THE UPPER PORTION WAS PROTRUDING. THIS PROTRUSION CAUSED W EAR ON THE LOWER SURFACE OF THE UPPER GRIP OF THE MAIN ROTOR HEAD INNER SLEEVE. THE WEAR WAS BEYOND SERVICEABLE LIMITS. THE MAIN ROTOR HEAD WAS REMOVED AND A SERVICEABLE UNIT WAS INSTALLED. THIS PROBLEM WAS DISCOVERED DURING A BLADE 1200 H R. SCHEDULED INSPECTION. 1 G 7 2 3U 3 U NC H13EU E5NE10 2003011400202 20030114 00202 EA 2003 1 14 CA021206003 1 20021127 A 2722 2379003001 REGULATOR DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE RUDDER PRESSURE FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 25986 25986 (CAN) AFTER T/O AT 2000 FT AGL AND ABOVE 150 KTS RUDDER PRESSURE AND RUDDER FULL PRESSURE CAUTION LIGHTS ILLUMINATED. L IGHTS WENT OUT SLOWING THRU 130 KTS. AIR TURN BACK AND LANDED WITHOUT INCIDENT. RUDDER DUAL PRESSURE REGULATOR REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011400203 20030114 00203 CE 2003 1 14 CA021206004 1 20021206 A 3340 MS25306222 SWITCH CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE MCAULY 3AF34C 3GFR34C703 GL LANDING LIGHT SHORTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA (CAN) ON APPROACH FLIGHT CREW COULD SMELL A BURNING ODOR IN THE COCKPIT WHEN LT LANDING LIGHT WAS TURNED ON. MAINTENANC E FOUND THE LT LANDING LIGHT SWITCH TO HAVE A INTERNAL SHORT. ALTHROUGH SWITCH AND THE LANDING LIGHT ITSELF STILL WORKE D, IT WAS DISCOVERED THAT THE SWITCH HAD A HIGH RESISTANCE CAUSING A HIGH HEAT BUILD UP OF THE AFFIXED WIRING TO THE LAN DING LIGHT AFTER BEING TURNED ONFOR A SHORT PERIOD OF TIME. WIRING WAS INSPECTED AND SWITCH REPLACED. THE LANDING LIGHT CIRCUIT BREAKER DID NOT TRIP. 1 H 7 1 3T 3 T A37CE E4EA 5 C P60GL 2003011400204 20030114 00204 NM 2003 1 14 VNAA0212038 1 20021230 A 3297 2328500000 WIRE HARNESS DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 429JS 19772 3043 DURING CLIMB OUT, THE CREW RECEIVED A PROXI SYSTEM AND PROXI LOCK FAIL INDICATIONS. THE CREW CONTACTED MAINTENANCE CONT ROL AND WERE INSTRUCTED TO DIVERT TO PIT FOR MAINTENANCE. AFTER ARRIVAL IN PIT, MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR HARNESS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003011400211 20030114 00211 GL 2003 1 14 CA021209001 1 20020521 A 3897 304313T RIBBON HEATER BOMBDR BD700 BD7001A10 1390006 GL RROYCE BR700 BR700710A220 09500 NE CABIN MELTED W O OTHER M OVER TEMP NR NOT REPORTED 1 CA (CAN) RIBBON HEATERS INSTALLED ON FORWARD CABIN LINES WERE INOPERATIVE. ON INVESTIGATION IT WAS FOUND THAT THE HEATERS W ERE BURNED AND MELTED CAUSING OPEN CIRCUITS. 2 L 7 2 4F 4 F RT T00003NY E00061EN 2003011400212 20030114 00212 2003 1 14 CA021209005 4 20021206 A 2211 COMPUTER BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA AUTO PILOT INTERMITTENT W D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA (CAN) AUTO PILOT NR 2 - TRIM WHEEL MOVED IN THE WRONG DIRECTION ON TRIM LIGHT/TRIM WHEEL CHECK. LIGHT ILLUMINATION WAS I NTERMITTENT. 1 L 7 2 3T 4 T RT 3A20 E4EA 2003011400215 20030114 00215 NM 2003 1 14 CA021209007 1 20021129 A 2750 66232231 BOLT BOEING 737 737281 138448P NM PWA JT8 JT8D17 52049 NE SLAT TRACK CRACKED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) ON APPROACH FLIGHT CREW REPORTED UPON SELECTION OF FLAPS TO NR 1 POSITION THE NR 4 SLAT HUNG UP UNTIL FLAPS WERE S ELECTED TO '15' POSITION. ALL INDICATIONS WERE NORMAL AFTER FLAPS '15' SELECTION AND NO CONTROL DIFFICULTIES. MAINTENANC E INSPECTION REVEALED NR 4 SLAT OUTBOARD MAIN TRACK BOLT SHEARED. BOLT REPLACED AND SLAT MOVEMENT AND OPERATIONAL CHECK ED PERFORMED IAW MM27-81-00. AIRCRAFT FERRIED TO CALGARY (YYC). MAINTENANCE REPLACED NR 4 SLAT ASSEMBLY, OUTBOARD MAIN T RACK ROLLER ATTACH BOLTS AND TRACK GUIDES IAW 27-81-21. SYSTEM GROUND CHECKED SERVICEABLE. AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO REPORT. 2 L 7 2 4F 4 F A16WE E2EA 2003011400216 20030114 00216 EU 2003 1 14 CA021209009 1 20021206 A 6510 11788659 BELLCRANK BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE TAIL ROTOR GROOVED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) TAIL ROTOR BELLCRANK FOUND WITH 11.45MM LONG BY 2MM WIDE, DEPTH STILL UNKNOWN RADIAL GROOVE WORN 2MM ADJACENT TO S PHERICAL BEARING HOUSING. DAMAGE CAUSED BY EARS OF TAIL ROTOR BELLOWS RUBBING AGAINST BELLCRANK ASSY. 1 G 7 2 3U 3 U NC H13EU E5NE10 2003011400217 20030114 00217 EU 2003 1 14 CA021210002 2 20021028 A 8530 854116 EXHAUST VALVE DIAMON DA20 DA20A1 2990000 GL ROTAX 912 ROTAX912 55555 EU HOFMAN HOV352 HOV352F NE CYLINDER HEAD BROKEN W A UNSCHED LANDING R Y J PARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CA (CAN) EXHAUST VALVE BROKE AT SEAT CONTACT AREA CAUSING PISTON DAMAGE AND ENGINE STOPPAGE. REMAINDER OF VALVE TRAIN PARTS SHOWED MORE WEAR THAN NORMAL INDICATING HAMMERING OF VALVE TRAIN COMPONENTS. THIS CONDITION IS RELATED TO IMPROPER PURG ING OF THE OIL SYSTEM AT ENGINE INSTALLATION. 1 L 7 1 3O 3 I NT TA4CH EXPE3I 5 C TP5BO 2003011400218 20030114 00218 EA 2003 1 14 CA021210004 1 20021210 A 3240 B7200R SHOE SCWZER SG2 SGS233A 8051606 EA BRAKE ASSY BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PIVOT END OF BRAKE SHOE BROKEN. 1 K 0 0 G2EA 2003011400219 20030114 00219 EU 2003 1 14 USAA020453 1 20021105 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 11023 1033 TPA - FOUND FLOORBEAM CORRODED 1 SQUARE INCH, FRAME 66 AT STATION 71292 LEFT AFT LAVATORY AREA. REMOVED CORROSION, USED NDT PROCEDURE, SEALED AND RESTORED FINISH PER EA 94371. (M) 2 L 7 2 4F RT A28NM 2003011400220 20030114 00220 CE 2003 1 14 CA021210005 1 20021206 A 3221 58130441 BRACKET CESSNA 404 404CESSNA 2075901 CE CONT O520 GTSIO520M 17032 SO MCAULY 3FF32 3FF32C501 GL NLG ACTUATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12097 12097 (CAN) CRACKED BRACKET FOR NOSE GEAR ACTUATOR. AFT END ATTACHES AT THIS BRACKET. 1 L 7 2 3O 3 O A25CE E7CE 5 C P45GL 2003011400221 20030114 00221 EU 2003 1 14 USAA020454 1 20021105 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 11023 1033 TPA - FOUND FLOORBEAM CORRODED .25 INCH, Y503.2, 1 INCH AFT OF C-14. BLENDED DAMAGED AREA PER TYPICAL REPAIR 53-11-01. (M) 2 L 7 2 4F RT A28NM 2003011400222 20030114 00222 EU 2003 1 14 USAA020455 1 20021108 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 11023 1033 TPA - FOUND FLOORBEAM CORRODED .25 INCH, FLOORBOARD ATTACH HOLE, FORWARD OF FORWARD GIRT BAR PAD. CLEANED CORRODED AREA , DIMENSIONAL CHECK PER SRM AND INSTALLED REPAIR ANGLES PER SRM 53-41-14 FIG 201. (M) 2 L 7 2 4F RT A28NM 2003011400223 20030114 00223 CE 2003 1 14 CA021210006 1 20021206 A 3221 5213040910 STRUCTURE CESSNA CESSNA 404 404CESSNA 2075901 CE CONT O520 GTSIO520M 17032 SO MCAULY 3FF32 3FF32C501 GL TRUNNION ATTACH CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12097 12097 (CAN) NOSE GEAR STRUCTURE WAS CRACKED AT ALL MOUNTING POINTS. SUSPECT UNREPORTED HARD LANDING. 1 L 7 2 3O 3 O A25CE E7CE 5 C P45GL 2003011400224 20030114 00224 EU 2003 1 14 USAA020456 1 20021108 A 5315 D5347209000200 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 11023 1033 TPA - FOUND FLOORBEAM CORRODED 2 SQUARE INCH, AFT END OF BEAM AT LEFT AFT LAVATORY, AFT INBOARD ATT HOLE. DEFECTIVE PAR T REPLACED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A28NM 2003011400225 20030114 00225 EU 2003 1 14 USAA020457 1 20021108 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 11023 1033 TPA - FOUND FLOORBEAM CORRODED 1 SQUARE INCH, FLOOR ATT HOLE, OUTBOARD FLOORBEAM 12 INCHES INBOARD AFT GIRT BAR. REMOVE D CORROSION, AND DAMAGED AREA, INSTALLED TRIPLER OVER SPLICE DOUBLER PER EA 94369. (M) 2 L 7 2 4F RT A28NM 2003011400226 20030114 00226 EU 2003 1 14 USAA020458 1 20021116 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 12914 0922 TPA - FOUND FLOORBEAM CORRODED 1 SQUARE INCH, UPPER SURFACE FLOOR SUPPORT BEAM Y1732 FRAME 66. CLEANED CORRODED AREA, I NSTALLED REPAIR ANGLES PER SRM 53-41-14 FIG 201. (M) 2 L 7 2 4F RT A28NM 2003011400227 20030114 00227 EU 2003 1 14 USAA020459 1 20021116 A 5320 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 12914 0922 PIT - FOUND BEAM CORRODED 1 SQUARE INCH, UPPER SURFACE FLOOR SUPPORT 71292 AT FRAME 68. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR TRIPLER AT EXISTING SPLICE PER EA 94375. (M) 2 L 7 2 4F RT A28NM 2003011400228 20030114 00228 2003 1 14 CA021210007 4 20021203 A 3425 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE FLIGHT DIRECTOR MALFUNCTIONED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) INTERMITTENT UNCOMMANDED RUDDER MOVEMENT RESULTING IN CONSTANT OSCILLATION OF A/C. ON FLIGHT CONT. SYN PG RT AIL+2 UNITS/ RT ELEVATOR SHOWS CONSTANT MOTION/RUDDER SHOWS CONSTANT MOVEMENT ALSO A/C UNCOMMANDED BANK TO LT WHEN A/P DISCON NECTED. FCC CHANGED, TEST FLIGHT COMPLETED, CHECK SERVICEABLE 2 L 7 2 4F 4 F RT A21EA E15NE 2003011400229 20030114 00229 EU 2003 1 14 USAA020460 1 20021116 A 5320 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 12914 0922 FOUND BEAM CORRODED .5 INCH AREA AROUND ATTACH HOLE, UPPER SURFACE FLOOR SUPPORT BEAM Y1292 AT FRAME 66. BLENDED CORROD ED AREA AND RESTORED FINISH PER EA 94374. (M) 2 L 7 2 4F RT A28NM 2003011400231 20030114 00231 EU 2003 1 14 USAA020461 1 20021116 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 12914 0922 TPA - FOUND FLOORBEAM CORRODED 1 SQUARE INCH, UPPER SURFACE FLOORBEAM Y1292 AT FRAME 16. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-11-15. (M) 2 L 7 2 4F RT A28NM 2003011400233 20030114 00233 EU 2003 1 14 USAA020462 1 20021116 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 12914 0922 TPA - FOUND FLOORBEAM WITH 1 INCH SQUARE CORRODED AREA, UPPER SURFACE FLOOR SUPPORT BEAM Y765 AT FRAME 66. REMOVED AND REPLACED FLOORBEAM PER SRM 53-41-04. (M) 2 L 7 2 4F RT A28NM 2003011400234 20030114 00234 NM 2003 1 14 USAA020463 1 20021115 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 45063 23510 PIT - FOUND SKIN CRACKED 1.650 INCHES LONG, BETWEEN STATION 727E AND 747 STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00- 01 FIG 202. () 2 L 7 2 4F RT A16WE 2003011400235 20030114 00235 NM 2003 1 14 USAA020464 1 20021121 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 50018 22952 PIT - FOUND SKIN CRACKED 2 INCHES, RIGHT SIDE STATION 727E STRINGER 24 RT. CUTOUT DAMAGE, INSTALLED DOUBLER AND FILLER PER SRM 53-00-01 FIG 225. (M) 2 L 7 2 4F RT A16WE 2003011400236 20030114 00236 NE 2003 1 14 CA021210010 2 20021121 A 8530 153084 CYLINDER HEAD DOUG DC4 C54A 3021512 WP PWA R2000 R20007M2 52023 NE NR 3 CYLINDER CRACKED W E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA (CAN) DURING CRUISE THE PILOT NOTICED THAT NR 3 ENGINE WAS BACKFIRING EXCESSIVELY. THE ENGINE WAS SHUT DOWN AND FEATHERE D. WHEN MAINTENANCE INSPECTED THE ENGINE, THEY FOUND NR 4 CYLINDER WAS CRACKED BETWEEN BOTH SPARK PLUG HOLES. THE CYLIND ER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4R 4 R A762 5E5 2003011400237 20030114 00237 2003 1 14 USAABA02023 4 20021117 A 2565 7A1539113 SLIDE AIRBUS 330 A330323 3930335 EU L2 DOOR DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 671UW 12556 0323 PHL - DURING ANNUAL SLIDE OPERATIONAL CHECK ON THE L2 DOOR, THE SLIDE DEPLOYED NORMALLY, HOWEVER, A HOLE WAS FOUND IN TH E SLIDE. THE SLIDE HELD PRESSURE LONG ENOUGH TO EVACUATE THE AIRCRAFT. (M) 2 L 7 2 4F RT A46NM 2003011400238 20030114 00238 NM 2003 1 14 USAABB02192 1 20021120 A 3397 WIRE BOEING 767 767201 1385125 NM CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 650US 23902 FRA - FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE AT RIGHT MID LAVATORY. MAINTENANCE RECONNECTED A LOOSE WIRE. (M) 2 L 7 2 4F RT A1NM 2003011400239 20030114 00239 NM 2003 1 14 USAABB02193 1 20021124 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 626AU 27303 MIA - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2003011400240 20030114 00240 NM 2003 1 14 USAABB02194 1 20021121 A 3350 873100151REV12 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 600AU 22192 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2003011400241 20030114 00241 NM 2003 1 14 USAABB02195 1 20021124 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 630AU 27808 BDL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2003011400242 20030114 00242 GL 2003 1 14 CA021211003 3 20021206 A 6110 B3476A2 BETA RING BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA HARTZL HCD4N3 HCD4N3A GL PROPELLER MISINSTALLED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE BETA RING WAS RUBBING ON THE ENGINE NOSE CASE STUDS. PROPELLER WAS REMOVED AND THE BETA RING WAS ADJUSTED AND REINSTALLED ONTO THE ENGINE 1 L 7 2 3T 4 T A14CE E4EA 5 C STC 2003011400243 20030114 00243 NM 2003 1 14 USAABB02196 1 20021126 A 3350 8731002511REV15 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 632AU 27810 BDL - FOUND THE R2 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2003011400244 20030114 00244 NM 2003 1 14 USAABB02197 1 20021129 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 605AU 22201 TPA - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROW 1 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2003011400245 20030114 00245 EU 2003 1 14 CA021211004 1 20021203 A 5710 D5735110120000 LOCK PLATE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE WING TIP CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ACCOMPLISHMENT OF AN H02 CHECK. FOUND THAT THE LT AFT LOCKING PLATE FOR THE LT WING TIP FENCE AND THE AFT A TTACH HARDWARE(2) BOLTS WERE FOUND BADLY CORRODED. THERE WAS NO CORROSION INDICATION AT THE LT FWD ATTACHMENT AND THE A FT THAT SHOWS EXTREME CORROSION. AIRCRAFT TOTAL TIME 36,353 IPC FIGURE 57-31-05-02ITEM 090 2 L 7 2 4F 4 F RT A28NM E29NE 2003011400246 20030114 00246 SW 2003 1 14 CA021212003 1 20021212 A 5532 410008171173 SKIN GULSTM 690TP 690 0141720 SW GARRTT TPE331 TPE3315251K NM VERTICAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION PRIOR TO INSTALLATION OF SB218 KIT (REF AD95-13-02) TWO CRACKS WERE NOTED ON THE RT VERTICAL STA B SKIN AT FS 409.65 WL 5.10 AND 4.10. TH CRACK LENGTHS WERE 5/16 OF AN INCH. 1 H 7 2 3T 4 T 2A4 E2WE 2003011400247 20030114 00247 WP 2003 1 14 ASAA0280539 1 20021109 A 5347 SR095301157003 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K-CHECK, SEAT TRACK GOUGED AT FS 257-259, LBL 44. REMOVED GOUGED SECTION. SPLICED IN REPLACEMENT SECTION PER SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2003011400248 20030114 00248 WP 2003 1 14 ASAA0280540 1 20021109 A 5320 5910244143 SUPPORT ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND DURING 30K-CHECK, LONGERON 8R SUPPORT ANGLE FOUND BROKEN AT FS 1415. REPLACED SUPPORT ANGLE PER SRM 51-30-5 . (M) 2 L 7 2 4F RT A6WE 2003011400260 20030114 00260 NM 2003 1 14 CA021213002 1 20021111 A 2710 ACTUATOR BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE AILERION MALFUNCTIONED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 CA 541D (CAN) ENGINE INDICATION AND CREW ALERT SYSTEM MESSAGE APPEARED, AILERON LOCKOUT' CAPTION CAME ON DURING APPROACH. FAULT ED LEFT ACTUATOR, ACTUATOR REPLACED 2 L 7 2 4F 4 F RT A1NM E3NE 2003011500002 20030115 00002 NE 2003 1 15 CA021213003 2 20021205 A 7310 FITTING PIPER PA31T PA31T2 7103127 SO PWA PT6 PT6A135 52043 NE FUEL MANIFOLD MISALIGNED W A UNSCHED LANDING W K J INADEQUATE Q C FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) ON DEPARTURE, THE FLIGHT CREW NOTICED FLUID LEAKING FROM THE RT ENGINE NACELLE. THE CREW RETURNED TO BASE FOR MAI NTENANCE INVESTIGATION. MAINTENANCE REPLACED NR 6, 7, 8, 9 & 10 FUEL NOZZLE GASKETS AND TRANSFER TUBE O-RINGS. GROUND RUN WAS FOUND SATISFACTORY. WHEN AIRPLANE RETURNED FOR FLIGHT, CREW NOTICED FLUID LEAKING FROM RT NACELLE AGAIN. THE A IRPLANE WAS RETURNED TO BASE. MAINTENANCE REPLACED NR 9, 10, 11 & 12 FUEL NOZZLE ASSEMBLIES AND FUEL TRANSFER TUBES. T HE FITTING ON FUEL MANIFOLD WAS FOUND MISALIGNED. THE AIRPLANE WAS TEST FLOWN WITH NO FURTHER OCCURRENCE. 1 L 7 2 3T 4 T RT A8EA E4EA 2003011500005 20030115 00005 NM 2003 1 15 CA021216002 1 20021210 A 2910 82970009325 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 HYD SYSTEM CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) NR 2 HYDRAULIC SYSTEM FOUND DEPLETED. RT NACELLE TOTALLY SOAKED WITH FLUID. MAINPRESSURE LINE IN RT NACELLE FROM E DP INTO PRESSURE MANIFOLD FOUND TO HAVE A CRACKED FLARE. LINE REPLACED 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011500006 20030115 00006 EA 2003 1 15 CA021216003 1 20021202 A 3150 8006221 CONTROL UNIT DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE LIGHT PANEL FAILED W K NONE B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING IN INSP/MAINT 1 CA (CAN) WHILE AT GATE PRIOR TO START UP, CREW REPORTED ODOR OF ELECTRICAL SMOKE IN COCKPIT ONLY. A/C DEPLANED. PILOTS BOOK ED OFF FEELING NAUSEOUS. INITIALLY MAINTENANCE COULD NOT DUPLICATE ODOR. ELECTRICAL POWER CONNECTED ALL NIGHT IN SAME C ONFIGURATION ON RAMP. NO BURNED BALLEST OR WIRING COULD BE FOUND. IN MORNING ON TAXI TO GATE MANY WARNING LIGHTS ILLUMIN ATED: CABIN PRESSURE, PAX & BAGGAGE DOOR ( WITH DOORS CLOSED). WARNING LIGHT PANEL WOULD NOT DIM. WARNING LIGHT CONTROL UNIT REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011500007 20030115 00007 NE 2003 1 15 CA021217001 2 20021110 A 7250 411109008 NOZZLE SNIAS 350 AS350D 8680803 EU LYC LTS101 LTS101600A2 41560 NE ENGINE ERODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING DISASSEMBLY OF ENGINE, THE THREE RING SEALING FEATURE OF NOZZLE WAS FOUND SEPARATED FROM THE NOZZLE, AFT O F THE VANE TRAILING EDGE. SEPARATION IS ATTRIBUTED TO EXCESSIVE EROSION CAUSED BY INEFFICIENT FUEL BURN (ENGINE GENERAT ED CARBON BALL EROSION). NOTE: THE AFFECTED PART WAS INSTALLED IN GAS PRODUCER MODULE 4-101-00-5, S/N 79M003. 1 G 7 1 3U 3 U H9EU E5NE 2003011500010 20030115 00010 NM 2003 1 15 CA021217004 1 20021113 A 2910 82970009387 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) IN NR 2 ENGINE NACELLE, FLIGHT VALVE SPOILER DUMP VALVE HYDRAULIC LINE LEAKING THROUGH PIN HOLES AT BEND RADIUS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011500011 20030115 00011 NM 2003 1 15 CA021217005 1 20021201 A 7921 OIL COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE LT ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) LT ENGINE OIL COOLER FOUND LEAKING. OIL COOLER REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011500012 20030115 00012 NM 2003 1 15 CA021217007 1 20021216 A 5610 NP15790213 WINDOW DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE COCKPIT CRACKED W O OTHER O OTHER NR NOT REPORTED 1 CA (CAN) CREW REPORTED EXTENSIVE CRACKING ON CAPTAIN'S SIDE WINDOW OUTER PANE. FERRY FLIGHT COMPLETED TO MAINTENANCE BASE W HERE WINDOW WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011500013 20030115 00013 EA 2003 1 15 CA021217008 1 20021128 A 5210 601R386541 GATE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR OUT OF RIG W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 21351 (CAN) CABIN CLIMBED UNCONTROLLABLY IN AUTO AND MANUAL MODES. REPAIRED AND RIGGED THE PASSENGER DOOR GATE IAW CRJ MM TASK 52-11-15-820-801.OPERATIONAL CHECK OF PRESSURE SYSTEM IAW 21-31-00-710-801 GOOD 2 L 7 2 4F 4 F RT A21EA E15NE 2003011500014 20030115 00014 EA 2003 1 15 CA021217009 1 20021130 A 7830 1267587 PDU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE THRUST REVERSER FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA 1604 (CAN) DURING FLIGHT AT FL350 RECEIVED A RT REVERSER UNLOCK WARNING MESSAGE. FOLLOWED MEMORY ITEMS AND THEN QRH. ENGINE SHUTDOWN PER QRH. NORMAL SINGLE ENGINE LANDING WAS MADED. REMOVED AND REPLACED PDU IAW MM78-32-03 AND RIGGED LOWER INB OARD BALLSCREW ACTUATORS IAW MM 78-32-03.OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2003011500015 20030115 00015 NM 2003 1 15 CA021217010 1 20021126 A 8011 38315212 STARTER BOEING 727 727171C 1384057 NM PWA JT8 JT8D7A 52053 NE NR 2 ENGINE MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING B CHECK INSPECTION OF ENGINE A METAL FRAGMENT WAS FOUND ON THE MAGNETIC CHIP PLUG OF THE NR 2 ENGINE STARTE R. THE STARTER WAS CHANGED OUT AND THE AIRCRAFT RETURNED TO SERVICE. THE STARTER WILL BE SENT FOR EVALUATION. 2 L 7 3 4F 4 F A3WE E2EA 2003011500017 20030115 00017 NM 2003 1 15 CA021218007 1 20020814 A 3150 C12431AB MODULE BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA WARNING SYS FAILED W D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CA (CAN) TAKE OFF CONFIGURATION WARNING, WHEN ADVANCING PL. WAS NOT ABLE TO SOLVE THE PROBLEM AND RETURNED TO RAMP. IT WAS ESTABLISHED THAT IOM (INPUT/OUTPUT MODULE) NR 1 WAS FAULTY AND IT WAS CONSEQUENTLY REPLACED. IOM OUT S/N 131 AND IN S/N 227. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003011500018 20030115 00018 2003 1 15 CA021218008 4 20020817 A 3425 CAPACITOR BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA AHRU FAILED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 CA (CAN) DURING CLIMB, YAW DAMPER WAS AUTOMATIC DISENGAGED WHEREBY WE ALSO RECEIVED AN AUTOPILOT FAILURE. THIS WAS FOLLOWE D BY ATTITUDE FAIL, IVSI FAIL AND HDG FAIL ON PFD NR 2 (AHRS 2 FAILURE). CLIMB WAS STOPPED AT FL120, A/C RETURNED FOR LA NDING. DURING RETURN FLIGHT ALL THE FAILURES CAME AND WENT SERVAL TIMES INDICATING A LOT OF CAUTIONS AND AURAL ALERTS. INVESTIGATION/ACTIONAFTER THIS OCCURRENCE, THE AHRU NR 2 WAS REPLACED. THE FAULT WAS CONFIRMED AT THE SHOP, IT WAS FOUND TO BE THAT ONE CAPACITOR ON THE POWER SUPPLY BOARD HAVE DEVELOPED LEAKAGE AT HIGH TEMPERATURE AND/OR AGING. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003011500019 20030115 00019 CE 2003 1 15 CA021218009 1 20021216 A 3233 4377113 CAP PHOENIX BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA NLG ACTUATOR FRACTURED W E A ENGINE SHUTDOWN UNSCHED LANDING K R J FLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 CA 0011 (CAN) AIRCRAFT SELECTED GEAR DOWN AND NO GREEN LIGHTS. CYCLED GEAR AND MAIN GEAR LIGHTS CAME ON. COULD NOT GET NOSE GEAR TO LOCK. EMERGENCY EXTENSION DID NOT GET NOSE GEAR LIGHT TO COME ON. AIRCRAFT LANDED WITH NOSE GEAR NOT LOCKED. NOSE GEAR COLLAPSED ON LANDING. NOSE GEAR ACTUATOR END CAP HAD THE END FRACTURED THROUGH 90 PERCENT. 1 L 7 2 3T 4 T A14CE E4EA 2003011500020 20030115 00020 EA 2003 1 15 CA021219001 1 20021213 A 2910 82910010177 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING A LINE CHECK MAINTENANCE FOUND A HYDRAULIC LEAK IN NOSE GEAR WHEEL WELL. TRACED TO NOSE GEAR DOOR RETRACT L INE BEHIND DEBRIS GUARD COVER. TEMPORARY FLEX LINE INSTALLED AND WORK CARD ISSUED TO REPLACE WITH RIGID LINE 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011500021 20030115 00021 SO 2003 1 15 CA021219002 1 20021218 A 3230 4198300 UPLOCK HOOK PIPER PA31 PA31325 7103105 SO LYC O540 TIO540F2BD 41532 EA MLG LACK OF LUBE W L ABORTED APPROACH W J INADEQUATE Q C WARNING INDICATION LD LANDING 1 CA (CAN) LT MLG DOWNLOCK INDICATION FAILED TO COME ON AFTER GEAR SELECTION. MLG HANDLE DID NOT NEUTRALIZE AND RED MLG UNSA FE LIGHT WAS ON. AFTER UNEVENTFUL LANDING, THE MLG DOWNLOCK HOOK WAS FOUND TO BE NOT ENGAGED. MLG HOOK DID NOT FREELY ROTATE ON THE MOUNTING BOLT DUE TO RUST. BOLT REPLACED AND GEAR CYCLED NO FURTHER FAULT FOUND. LUBRICATION OF THE GEAR HOOK WAS CARRIED OUT PER PIPER MAINTENANCE MANUAL LESS THAN 70 HOURS BEFORE. IT IS OUR OPINION THIS AREA REQUIRED DISA SSEMBLY IN ORDER TO PROPERLY LUBRICATE THE BEARING AREA. 1 L 7 2 3O 3 O A20SO E14EA 2003011500022 20030115 00022 NM 2003 1 15 CA021219004 1 20021217 A 6123 3000500003 SIGNAL COND UNIT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 PROP TORQUE INTERMITTENT W A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA 25886 25886 (CAN) AFTER TAKEOFF, AUTOFEATHER WAS DESELECTED. ABOUT 1 MIN LATER THE 'ARM' LIGHT REILLUMINATED AND REMAINED ON FOR APP ROX 15 MINUTES. PLUGS IN RT WING ROOT CLEANED AND INSPECTED. RELAYS 6121- K1, K2, K3, AND K5 REPLACED FOR TROUBLESHOOTIN G. NR 2 ENGINE TORQUE SIGNAL CONDITIONER UNIT REPLACED DUE TO 3 SECOND TIME DELAY FUNCTION (AUTOFEATHER) INTERMITTENT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011500024 20030115 00024 2003 1 15 CA021219006 4 20021219 A 3413 457400GA1312 INDICATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE TCAS/VSI FAILED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 19508 19508 (CAN) ON CLIMB OUT F/O'S VSI WAS INDICATING 500 FT PER MINUTE. CAPTAIN'S VSI WAS INDICATING 1300 FT CLIMB PER MINUTE. CR EW IN CONSULTING WITH MAINTENACE DETERMINED F/O'S VSI NOT FUNCTIONING. AIRCRAFT COMPLETED AIR TURN BACK. DURING TROUBLE SHOOTING F/O'S VSI INDICATED RA FAIL, AND GIVING ERRATIC READINGS DURING TEST. F/O'S VSI REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003011500026 20030115 00026 2003 1 15 CA021219007 4 20020830 A 3420 42000332501 COMPUTER BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA AHRU FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK G J MULTIPLE FAILURE WARNING INDICATION TO TAKEOFF 1 CA (CAN) DURING T/O-RUN AT APPROXIMATELY 100 KNOTS 'ATT FAIL' AND 'HDG FAIL' WAS OBSERVED ON PFD1 AND MFD 1. T/O ABORTED. LEVEL TWO CHIME CAME ON DURING THE ABORTION TOGETHER WITH 'ELEVATOR FEEL' CAUTION. OTHER 'RED' INDICATIONS ON PFD WAS IV SI FAIL, CUE, AND MDA. RETURNED TO RAMP. MALFUNCTIONS RESET SUCCESSFULLY ACCORDING TECHNICAL ADVISORY FROM BASE. A/C WOR KED W.O.R. ON NEXT THREE LEGS. THE FAULT WAS RESET BY THE PROCEDURE SUPPLIED TO THE CREW. 8 DAYS LATER THE FAULT REOCCUR RED AND THE AHRU NR 1 (P/O AHRS) WAS REPLACED. AT THE SHOP THE FAULT WAS CONFORMED AND AT THE SAME TIME THE AHRU WAS MOD IFIED WITH A PERMANENT FIX TO THIS TYPE OF FAULT. SAGEM SB 420-34-008 ISSUED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003011500027 20030115 00027 CE 2003 1 15 CA021219009 1 20021216 A 3233 508202085 ACTUATOR BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA NLG DAMAGED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) DURING A LANDING GEAR SWING DONE AT INSPECTION, A SMALL CHIRPING SOUND WAS NOTICED COMING FROM THE NOSE LANDING GE AR AREA. AFTER SEVERAL SWINGS, THE NOISE WAS ISOLATED TO THE NOSE GEAR ACTUATOR. THE SOUND VARIED IN INTENSITY FROM A S MALL CHIRP TO A LARGE SCREECH. THE ACTUATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 2003011500028 20030115 00028 CE 2003 1 15 CA021220001 1 20021218 A 3233 508202085 ACTUATOR BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA MLG BINDING W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) AFTER HAVING PROBLEMS WITH A LOW TIME ACTUATOR ON ONE OTHER AIRCRAFT, WE DECIDED TO CHECK ALL ACTUATORS THAT WERE OVERHAULED BY THAT SUPPLIER. DURING SPECIAL INSPECTION OF THIS ACTUATOR, WE FOUND THAT THE LANDING GEAR MOTOR SEEMED TO BE WORKING HARDER THAN USUAL. WE REMOVED THE ACTUATOR FROM THE AIRCRAFT AND FOUND THE ACTUATOR WAS HARDER TO TURN THEN OTHERS AND IT WAS BINDING IN CERTAIN AREAS. THE ACTUATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 2003011500029 20030115 00029 NM 2003 1 15 CA021220003 1 20020905 A 6120 699018001 CONTROL UNIT BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA PROPELLER FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) DURING TAKE-OFF AUTOFEATHER DID NOT ARM AND TAKE OFF WAS ABORTED. FAULT CODE 274 OBSERVED IN CDS FOR THE LT ENGIN E PROPELLER ELECTRONIC CONTROL UNIT (PECU). FOR TROUBLESHOOTING PURPOSES THE PECU'S WERE CROSS CHANGED. THE FAULT MOVED TO THE OTHER SIDE. NEW PECU INSTALLED ACCORDING AMM 61-20-32. TEST RUN PERFORMED W/O REMARKS. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003011500030 20030115 00030 EA 2003 1 15 CA021220005 1 20021206 A 3040 16591 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE WINDSCREEN HEAT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE AIRCRAFT WAS SITTING AT GATE CREW NOTICED THAT RT WINDSCREEN OUTER PLY WAS CRACKED. WINDSCREEN REPLACED. CR EW ALSO NOTED THAT WINDOW HEAT CAME ON 2 TIMES (2 SEPERATE FLIGHTS) BUT CLEARED WHEN SWITCHED TO RESET/ON. RT WINDSHIELD TEMP CONTROLLER WAS REPLACED AS WELL. 2 L 7 2 4F 4 F RT A21EA E15NE 2003011500031 20030115 00031 CE 2003 1 15 CA021220007 1 20021220 A 5753 6521158192 RIB CESSNA CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE TE FLAPS WORN W K NONE O OTHER IN INSP/MAINT 1 CA 701702 (CAN) RIB EXTENSIONS WORN. WHEN FLAP IS FULLY RETRACTED THE RIB EXTENSIONS FRETTING ON THE FLAP TRACK AND FLAP TRACK RI VETS. 1 L 7 2 4F 4 F A22CE E1NE 2003011500032 20030115 00032 EU 2003 1 15 CA021220008 1 20021219 A 3010 WARNING SYSTEM PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL WING DE-ICE MALFUNCTIONED W O OTHER N FALSE WARNING AP APPROACH 1 CA (CAN) DE-ICE CAUTION LIGHT ILLUMINATED ALONG WITH A FLASHING 'DEICE BOOTS'. BOOT INFLATION SEQUENCE APPEARED TO BE FUNC TIONING NORMALLY. CONTINUITY & FUNCTION CHECK OF ALL 5 PRESSURE SWITCHES REVEALED NO FAULTS. FUNCTIONAL TESTS USING BOT H SHOP EQUIPMENT AND ENGINE RUNNING WERE PERFORMED WITH NO FAULTS. PROBLEM COULD NOT BE DUPLICATED. A DE-ICE TIMER WAS ORDERED, TO BE REPLACED AS SUSPECT DUE TO THE ELAPSED TIME OF SEQUENCES MAY NOT AGREE WITH THE CENTRAL ADVISORY AND WAR NING SYSTEM. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2003011500033 20030115 00033 CE 2003 1 15 CA021220009 1 20021220 A 3230 5541205678 PIN CESSNA CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE MLG TRUNNION CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CORROSION RESISTANT PINS WERE HARD TO REMOVE FROM THE BUSHINGS DUE TOO HEAVY CORROSION. 1 L 7 2 4F 4 F A22CE E1NE 2003011500034 20030115 00034 CE 2003 1 15 CA021220010 1 20021220 A 5740 FITTING CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE LT & RT WING NICKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) NICKS ON UPPER LUGS OF WING CARRY THROUGH FITTINGS ON FWD & REAR SPARS. 1 L 7 2 4F 4 F A22CE E1NE 2003011500035 20030115 00035 CE 2003 1 15 CA021220011 1 20021220 A 5740 FITTING CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE LT/RT WING SPAR NICKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) NICKS FOUND DURING INSPECTION. LOCATED ON UPPER LUGS OF WING SPAR CARRY THROUGH FITTINGS ON LT & RT SIDES OF MAIN & REAR STUB WING SPAR ASSY'S. 1 L 7 2 4F 4 F A22CE E1NE 2003011500036 20030115 00036 EA 2003 1 15 CA021222001 1 20021219 A 2820 CC670621042 TUBE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE FUEL CELL CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING MAINT. IT WAS OBSERVED THAT FUEL WAS GETTING INTO THE CENTER TANK (CTR. TANK QUANTITY INCREASE OVER TIME) W HEN EVER THE BOOST PUMPS WERE SELECTED ON. INVESTIGATION BY MAINT. IDENTIFIED A CRACK ON TUBE CC670621042 LOCATED IN TH E RT SIDE OF THE CENTER TANK. MAINTENANCE REPLACED THE DEFECTIVE TUBE SECTION. THIS CRACK WAS FOUND POST SB 670BA28008. THE SB IS CALLING FOR THE INSPECTION OF THE FWD END OF THE TUBE AND NOT THE AFT END OF THE TUBE WHERE THE CRACK WAS FOUN D. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2003011500039 20030115 00039 SO 2003 1 15 000236 1 20021221 A 3411 CAP EMB 145 EMB145 3260210 SO PITOT/STATIC SYS DEFECTIVE A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 277 IAS FLAG OVER AIRSPEED TAPE ON CAPTAIN SIDE DURING TAKEOFF. REMOVED AND REPLACED F/O PITOT DRAIN CAP. 2 L 7 2 4F RT T00011AT 2003011500040 20030115 00040 NE 2003 1 15 CA021223004 2 20021221 A 7320 978A000007 CONTROLLER AIRBUS 330 A330322 3930325 EU PWA 4168 PW4168 NE ENGINE ZONE MALFUNCTIONED W C ABORTED TAKEOFF G J MULTIPLE FAILURE WARNING INDICATION TO TAKEOFF 1 CA (CAN) REJECTED TAKE-OFF AT APPROX. 50 KTS FOR ECAM WARNING: ENG-THRUST LOSS (AMBER) ABNORMAL WING A. ICE (AMBER)THRUST L EVERS, IDLE (BLUE) AIRCRAFT RETURNED TO GATE WHERE MAINTENANCE FOLLOWED TROUBLE SHOOTING TASK 71-00-00-810-934, REPLAC ED THE ZONE CONTROLLER AND CARRIED OUT ENGINE RUNS. NO FURTHER FAULTS. 2 L 7 2 4F 4 F RT A46NM E36NE 2003011500041 20030115 00041 NE 2003 1 15 00069 2 20021207 A 7200 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE LEFT FLAMED OUT E HAEA B EMER. DESCENT X ENGINE FLAMEOUT CL CLIMB 1 SW 05 977TW 13 299061 PILOT REPORTED THAT ON THE SECOND LEG OF THE DAY THE LEFT ENGINE FLAMED OUT CLIMBING THROUGH 36,500, DECENT AND RELIGHT AT 31,000. PILOT PERFORMED INSPECTION OF ENGINE FOR FOD AND LEAKS, CK GOOD. NO FURTHER PROBLEM WITH NEXT LEGS AT ALTI TUDE. 2 L 7 2 4F 4 F A7EU E7EA 2003011500042 20030115 00042 EA 2003 1 15 CA021227001 1 20021222 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT FAILED W O OTHER O OTHER DE DESCENT 1 CA (CAN) CAPTAIN WINDSHIELD OUTER PAN SHATTERED ON DESCENT. REPLACED WINDSHIELD, HEAT CONTROLLER ALSO REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2003011500045 20030115 00045 SW 2003 1 15 CA021227004 1 20021222 A 2910 2781006019 LINE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313UW 01514 WP HARTZL HCB3T HCB3TN5 GL HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING INSPECTION A LARGE AMOUNT OF HYRAULIC FLUID WAS FOUND IN THE LT WHEEL WELL, FURTHER INVESTRICATION REVEALED A SMALL PIN HOLE IN THE LINE. THE LINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P15EA 2003011500046 20030115 00046 NM 2003 1 15 0204036717 1 20021214 A 2612 MODULE BOEING 747 747251F 1384898 NM PWA JT9 JT9D3 52050 NE FIRE WARNING MALFUNCTIONED A NWAA K NONE N FALSE WARNING UK UNKNOWN 1 GL 01 617US 21121 DURING FLIGHT THE FIRE WARNING BELL SOUNDED AND LIGHTS ILLUMINATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE AURAL WARNING MODULE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F 4 F A20WE E20EA 2003011500047 20030115 00047 EA 2003 1 15 CA021228001 1 20021219 A 3230 FITTING CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE FELXIBLE HOSE LEAKING W H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA (CAN) ON APPROACH, AFTER GEAR DOWN SELECTION AND GEAR DOWN INDICATION, MESSAGE HYD 3 LOW PRESS (C) WITH LOSS OF HYDRAULI C 3 QUANTITY. HYDRAULIC PUMP 3A AND 3B SHUT DOWN AND AIRCRAFT LANDED SAFELY. MECHANICS FOUND THAT THE LEAK WAS COMING F ROM ONE OF THE FLEXIBLE HOSE ATTACHED TO THE NLG RETRACT ACTUATOR. THE HOSE WAS REPLACED AND THE SYSTEM TESTED GOOD PRIO R AIRCRAFT RETURN TO SERVICE. AIRCRAFT HAD 3217 FH AND 3136 FC AT THE TIME OF THE EVENT. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2003011500048 20030115 00048 WP 2003 1 15 0204089872 1 20021216 A 3230 BUNGEE CYLINDER DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NLG FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 01 781NC 48121 UPON LOWERING GEAR INTO LAN NOSE GEAR WOULD NOT EXTEND. FLIGHT RETURNED TO AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR BUNGEE CYLINDER. GEAR OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A6WE E2EA 2003011500049 20030115 00049 2003 1 15 0204099882 4 20021218 A 3425 INDICATOR DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE COCKPIT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 670MC 47659 EN ROUTE CAPTAINS HSI INOPERATIVE. ALL FOUR RED BOW TIE LIGHTS ILLUMINATED. FLIGHT DIVERTED AND LANDED WITHOUT INCIDEN T. REPLACED CAPTAINS COURSE INDICATOR. REPLACED NAV/INST MONITOR UNIT AND REPLACED AMPS. SYSTEM OPERATION CHECKS GOOD. 2 L 7 2 4F 4 F RT A6WE E2EA 2003011500050 20030115 00050 WP 2003 1 15 0204109866 1 20021218 A 2120 SMOKE DOUG DC9 DC951 3022051 WP CABIN DETECTED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 775NC 47785 AFTER TAKEOFF FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL IN REAR OF AIRCRAFT. NO REPORT OF SMOKE. FLIGHT RETURNED AND LA NDED WITHOUT INCIDENT. TROUBLESHOOTING ACCORDING TO MM INDICATED NO ANOMALIES. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2003011500051 20030115 00051 WP 2003 1 15 0204119995 1 20021216 A 3222 STRUT DOUG DC9 DC931 3022065 WP PWA JT8 JT8D1 52044 NE NLG FLAT A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 8978E 47327 AFTER TAKEOFF WHEN GEAR WAS RETRACTED LOUD VIBRATION IN NOSE GEAR AREA. NO UNSAFE INDICATIONS ON GEAR. EXTENDED GEAR A ND VIBRATION STOPPED. FLIGHT RETURNED AND LANDED WITHOUT INCIDENT. UPON RETURN TO GATE FOUND RIGHT NOSE GEAR DOOR OPEN . NOSE GEAR STRUT FLAT AND MAIN GEAR STRUTS UNDERSERVICED. SERVICED ALL STRUTS AND ADJUSTED NOSE GEAR DOOR DRIVE RODS. GEAR OPERATION CHECKS GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2003011500052 20030115 00052 WP 2003 1 15 0204129986 1 20021214 A 2161 CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D NE CABIN TEMP FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 986US 47480 DURING CLIMB, FLIGHT ATTENDANT REPORTED CABIN RAPIDLY BECAME HOT AND SMELLED HOT. F/O REPORTED RIGHT PACK TEMP HIGH. P ACK TEMP REDUCE IN MANUAL OPERATION. FLIGHT RETURNED TO AND LANDED WITHOUT INCIDENT. REPLACED CABIN TEMP CONTROLLER AND RIGHT COALESCER BAG. PERFORMED PACK BURN OUT AND SYSTEM OPERATION CHECKS GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2003011500053 20030115 00053 NE 2003 1 15 0204149881 2 20021222 A 7200 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 1 MALFUNCTIONED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 676MC 47652 688833 CLIMBING THROUGH 8000 FEET, MASTER CAUTION ILLUMINATED. ENGINE NR 1 OIL QUANTITY WAS ZERO AND OIL PRESSURE LIGHT WAS IL LUMINATED. ENGINE NR 1 WAS SHUTDOWN. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT PERFORMING AN UNEVENTFUL LANDIN G. MAINTENANCE REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A6WE E2EA 2003011500054 20030115 00054 CE 2003 1 15 CA021231001 1 20021217 A 2810 1003810051 FUEL CAP BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA LT MAIN CELL DEPARTED W A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 CA (CAN) AFTER TAKE-OFF FROM YYR THE FLIGHT CREW NOTED THAT THE LEFT MAIN FUEL CAP CAME OFF AND EXITED THE AIRCRAFT. THE AI RCRAFT RETURNED TO BASE. MAINTENANCE INSPECTED THE FUEL FILLER OPENING AND WING CAP FITTING. NO DEFECTS WERE NOTED. THE MISSING FUEL CAP WAS NEVER FOUND. ALL FUEL CAPS ON THIS AIRCRAFT TYPE IN THE FLEET WERE THEN INSPECTED WITH NO DEFECTS N OTED. 1 L 7 2 4T 4 T A24CE E4EA 2003011500055 20030115 00055 NM 2003 1 15 0204156719 1 20021220 A 2720 PCU BOEING 747 747251F 1384898 NM PWA JT9 JT9D* NE RUDDER MALFUNCTIONED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 629US 22388 APPROACHING TOP OF CLIMB AT FL350, THE LOWER RUDDER WAS POSITIONED 5 DEGREES LEFT OF CENTER WITH THE UPPER RUDDER ONE DE GREE RIGHT OF CENTER. AFTER LEVEL OFF THE LOWER RUDDER SUDDENLY MOVED TO 5 DEGREES RIGHT OF CENTER. THE AUTOPILOT WAS THEN DISCONNECTED AND THE CREW USED AILERON INPUT TO MAINTAIN LATERAL AND DIRECTIONAL CONTROL. APPROXIMATELY ONE MINUTE LATER BOTH RUDDERS RETURNED TO A NORMAL ZERO DEGREE DEFLECTION. NO FURTHER RUDDER MALFUNCTIONS WERE EXPERIENCED. THE FLIGHT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH THE UPPER AND LOWER RUDDER PCU'S BOTH UPPER AND LOWER YAW DAMPER COMPUTERS AND THE NR 2 INU. 2 L 7 4 4F 4 F A20WE E20EA 2003011500056 20030115 00056 NM 2003 1 15 0204166303 1 20021229 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROW 51ABC-61ABC. REPAIRED WIRE CONNECTOR AT SEAT 51 . OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2003011500057 20030115 00057 NM 2003 1 15 0204176311 1 20021224 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 671US 26477 DURING LINE CHECK FOUND FLOOR EMERGENCY PATH LIGHTS INOPERATIVE BETWEEN DOORS 2R AND 3R. REPAIRED BROKEN WIRE. OPERATION AL CHECK GOOD. 2 L 7 4 4F RT A20WE 2003011500058 20030115 00058 CE 2003 1 15 CA030102005 1 20020511 A 5330 SKIN BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA HARTZL HCD4N3 HCD4N3A GL FUELAGE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 15478 (CAN) BEFORE INSTALLING BAGGAGE PAD, MAINTENANCE NOTICED THAT BELLY SKIN AFT OF REAR SPAR AT STA 226.5 WAS SLIGHTLY WRIN KLED, AND LOWER FLAP/FUSELAGE FAIRING SLIGHTLY WRINKLED. HARD LANDING/TURBULENT AIR INSPECTION AS PER 5-50-00 CARRIED OU T. SLIGHT WRINKLE ON RT INBOARD WING AT AUXILIARY FUEL PANEL TOP SKIN NOTED. NO OTHER DAMAGE FOUND, NO LOOSE FASTENERS N OTED. NO STRUCTURAL DAMAGE FOUND. AFTER DISCUSSING WITH RAYTHEON TECHNICAL SUPPORT, AIRCRAFT ALLOWED TO RETURN TO SERVIC E. RAYTHEON WILL BE REVIEWING DATA AND ISSUING REPAIR DATA IF REQUIRED. 1 L 7 2 4T 4 T A24CE E4EA 5 C STC 2003011500059 20030115 00059 NM 2003 1 15 0204186307 1 20021220 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK FOUND LEFT (C) ZONE FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOO D. 2 L 7 4 4F RT A20WE 2003011500060 20030115 00060 NE 2003 1 15 0204199153 2 20021229 A 7200 ENGINE DOUG DC9 DC914 3022034 WP PWA JT8 JT8D7 52053 NE NR 1 DAMAGED A NWAA A UNSCHED LANDING Y ENGINE STOPPAGE DE DESCENT 1 GL 01 8912E 45829 657274 ENGINE NR 1 FAILED AND SHUTDOWN AFTER A THRUST REDUCTION AT 17,000 FEET. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIR PORT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND ENGINE FOD DAMAGE AND REPLACED THE ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 2003011500061 20030115 00061 CE 2003 1 15 CA030102007 1 20021113 A 2780 1013800001 CONTROL CABLE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA HARTZL HCD4N3 HCD4N3A GL TE FLAPS TWISTED W O OTHER O OTHER NR NOT REPORTED 1 CA (CAN) LT INBOARD FLAP CABLE FOUND DRIVE END AT ACTUATOR TWISTED, FLAP SAFETY FUSE PULLED OUT ON LT FLAPS. NEW INBOARD LT FLAP CABLE INSTALLED. FLAP SAFETY FUSE RESET AND FUSE PULL WIRE ADJUSTED. FUNCTION TEST OF FLAP SYSTEM CARRIED OUT SERV ICEABLE. 1 L 7 2 4T 4 T A24CE E4EA 5 C STC 2003011500062 20030115 00062 WP 2003 1 15 0204209958 1 20021230 A 3231 DOOR DOUG DC9 DC931 3022065 WP RT MLG MALFUNCTIONED A NWAA O OTHER O OTHER LD LANDING 1 GL 01 917RW 47145 RIGHT GEAR DOOR OPENED ON LANDING AND CONTACTED RUNWAY SURFACE. PASSENGERS DEPLANED ON TAXIWAY AND AIRCRAFT TOWED TO RAM P. REPLACED AND RIGGED RIGHT MAIN LANDING GEAR DOOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 2003011500063 20030115 00063 CE 2003 1 15 CA030103005 1 20021212 A 1430 RIVET BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA MCAULY 4HFR34 4HFR34C754 NE FUSELAGE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 14019 (CAN) LT AND RT SIDE FRAME PN 10143002611 TO LONGERON ATTACH CLIP RIVETS (3 EACH SIDE) FAILED. SOME RIVETS COMPLETELY GO NE, SOME HEADS POPPED OFF. RAYTHEON FIELD REPAIR FR-KA-00814 CARRIED OUT. FAILED RIVETS REPLACED. 1 L 7 2 4T 4 T A24CE E4EA 6 C 3PNE 2003011500064 20030115 00064 SO 2003 1 15 02050241 1 20020904 A 5320 1159B21554179 CLIP GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY5118 54523 EU FUSELAGE CRACKED B Y3PR K NONE O OTHER IN INSP/MAINT 1 SO 35 500JW 234 SHEAR CLIP CRACKED AT FS 757.562 BETWEEN STRINGER 3R AND 4R. 2 L 7 2 4F 4 F RT A12EA E2EU 2003011500065 20030115 00065 CE 2003 1 15 CA030103006 1 20021212 A 1430 101430014 RIVET BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA MCAULY 4HFR34 4HFR34C754 NE WING SPAR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 14019 (CAN) WHILE CONDUCTING A STRUCTURAL INSPECTION A RIVET HEAD WAS FOUND MISSING AT STN 187.3 RT ATTACH CHANNEL TO SPAR CAP ATTACHMENT CLIP. RIVET REPLACED IN ACCORDANCE WITH RAYTHEON FIELD REPAIR FR-KA-00807. 1 L 7 2 4T 4 T A24CE E4EA 6 C 3PNE 2003011500066 20030115 00066 2003 1 15 0212311 4 20021231 A 3425 6226190113 COMPUTER SAAB SF340 SF340A 7850100 EU GE CT7TP CT79B 30030 NE ROTOL R389 R3894123F25 NE COCKPIT INOPERATIVE A UHLA A UNSCHED LANDING O OTHER CR CRUISE 1 NE 03 149SZ 2475 2475 340A149 FLT 4484 PILOT REPORTED THAT HIS LT AHRS SYSTEMS WENT INOPERATIVE DURING FLIGHT. AIRCRAFT RETURNED, MECHANIC REMOVED A ND REPLACED THE LT AHRS COMPUTER AND PERFORMED ALL RELATIVE OPERATIONAL CHECKS FOR THAT COMPONENT. OPERATIONAL CHECK WAS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P30NE 2003011500067 20030115 00067 CE 2003 1 15 CA030103007 1 20021212 A 5312 11543008435 BULKHEAD BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA MCAULY 4HFR34 4HFR34C754 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 14019 (CAN) WHILE CONDUCTING A STRUCTURAL INSPECTION, BULKHEAD AT STATION 236.5 WAS FOUND CRACKED WHERE IT JOINS WITH RT SIDE FRAME BETWEEN RT STRINGER NR 12 AND 13. FRAME/BULKHEAD REPAIR CARRIED OUT IN ACCORDANCE WITH RAYTHEON FIELD REPAIR FR-KA -00814. 1 L 7 2 4T 4 T A24CE E4EA 6 C 3PNE 2003011500069 20030115 00069 EU 2003 1 15 0212312 1 20021231 A 2613 1734362450 SENSOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE TAILPIPE MALFUNCTIONED A UHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 03 123CQ 123 FLIGHT 4558, AFTER TAKEOFF, TAILPIPE HOT LIGHT ILLUMINATED, PILOT RETURNED TO FIELD WITHOUT MISHAP. MECHANIC REMOVED A ND REPLACED TAILPIPE COWLING AND SENSORS, PERFORMED GROUND RUN OF ENGINE. OPERATIONAL CHECK, GOOD. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2003011500070 20030115 00070 EU 2003 1 15 0212313 1 20021231 A 6120 8542M2 COMPUTER SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE AUTOCOARSEN FAILED A UHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NE 03 360CA 1622 1622 360 FLIGHT 4467, UPON TAKEOFF, AUTOCOARSEN WARNING LIGHT ILLUMINATED. PILOT ABORTED TAKEOFF AND RETURNED TO GATE. AIRCRAF T PREPARED FOR FERRY FLIGHT. FWA MECHANIC REMOVED AND REPLACED AUTOCOARSEN COMPUTER AND PERFORMED OPERATIONAL CHECK OF AUTOCOARSEN SYSTEM. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2003011500071 20030115 00071 GL 2003 1 15 02FDEA00976 2 20021227 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1 FAILED A FDEA B A EMER. DESCENT UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SO 25 375FE 46613 IN CRUISE, FL 330, NR 1 ENGINE FAILED. OIL PRESSURE 0, OIL QUANTITY AND TEMPERATURE NORMAL. FUEL PRESSURE NORMAL. HYD RAULIC QUANTITY, PRESSURE AND TEMPERATURE NORMAL. ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 ENGINE. CL OSED COWLING IAW SMP. RAN NR 1 ENGINE IAW JRH, OPS CHECK AND LEAK CHECK NORMAL. 2 L 7 3 4F 4 F A22WE E23EA 2003011500073 20030115 00073 WP 2003 1 15 02FDEA00977 1 20021227 A 2612 WARNING LIGHT DOUG DC10 DC1030F 3023504 WP GE CF6 CF650* 30018 NE COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 309FE 48298 ENGINE NR 3 TEMP LIMITING POWER ALL REGIMES. SHORTLY AFTER TAKEOFF RECEIVED LOOP B FIRE LIGHT. ENGINE 3 FIRE LOOPS, A AND B BOTH TEST PROPERLY, REDUCED PWR, LOOP LIGHT EXTINGUISHED, PARAMETERS STABLE. DIVERTED. 2 L 7 3 4F 4 F RT A22WE E23EA 2003011500074 20030115 00074 NM 2003 1 15 EVAS091023 1 20021211 A 5415 BEARING BOEING 767 767300 1385204 NM NR 1 PYLON LOOSE W QOCF K NONE O OTHER IN INSP/MAINT 1 WP 03 16605 26064 DURING ROUTINE MAINT INSPECTION, FOUND BEARING FREELY ROTATED AND GAP BETWEEN BEARING OUTER RACE AND FITTING LUG ON NR 1 PYLON LT SIDE LOAD FITTING & NR 2 PYLON RT SIDE LOAD FITTING REPLACED SIDE LOAD FITTING BEARING. 2 L 7 2 4F RT A1NM 2003011500075 20030115 00075 NM 2003 1 15 02FDEA00979 1 20021228 A 2150 VALVE DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE A/C PACK LEAKING A FDEA B A EMER. DESCENT UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 602FE 48402 DECLARED INFLIGHT EMERGENCY, SMOKE IN COCKPIT. SOURCE OF SMOKE WAS BELIEVED TO BE AIR CONDITIONING SYSTEM. NOTICED A D IRTY SOCK ODOR DURING TAXI. IN FLIGHT, THE SMOKE KEPT INCREASING, RETURNED TO BASE. USED EMERGENCY ESCAPE SLIDE TO EGR ESS ON RUNWAY. FIRE DEPARTMENT ACCIDENTLY DEPLOYED THE OTHER ESCAPE SLIDE. FOUND NR 1 PACK ANTI ICE VALVE LEAKING INSTA LLED NR 1 PACK ANTI ICE VALVE PER MD11 M.M. 21-53-27-2 OK FOR SERVICE PERFORMED PER MD11 MM 21-53-00-7 PARA 2 CLEANING AIR CONDITIONING PACK AND DISTRIBUTION APPROX 5 TIMES NO SMOKE AND NO OIL ODOR AT THIS TIME 2 L 7 3 4F 4 F RT A22WE E13NE 2003011500076 20030115 00076 NM 2003 1 15 02FDEA00980 1 20021220 A 5313 STRINGER DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MDCC FUSELAGE FRAME STA 1139-1159, STRINGER 17R, FOUND WITH CRACK. 2 L 7 3 4F 4 F RT A22WE E13NE 2003011500077 20030115 00077 NM 2003 1 15 EVAS091024 1 20021226 A 5330 BEAR STRAP BOEING 747 74745E 1384947 NM FUSELAGE CORRODED W QOCF K NONE O OTHER IN INSP/MAINT 1 WP 03 16462 27173 CORROSION FOUND ON BEAR STRAP OF R3 DOOR CUTOUT 13191 LONG 16 RT. BLEND OUT THE CORROSION DAMAGE PORTION & PERFORM EXT ERNAL REPAIR BY USING TWO DOUBLERS ON FUSELAGE SKIN PANEL. 2 L 7 4 4F RT A20WE 2003011500078 20030115 00078 NM 2003 1 15 02FDEA00981 1 20021230 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN CABIN, SEAT TRACK DAMAGED AT FS 1350.5 X=-47.50. TRIMMED OUT DAMAGED SEAT TRACK IAW SRM. FABRICATED SEAT TRACK AN D SPLICE HAT IAW SRM. INSTALLED SEAT TRACK AND SPLICE HAT IAW SRM. 2 L 7 3 4F 4 F RT A22WE E13NE 2003011500079 20030115 00079 NM 2003 1 15 EVAS091025 1 20021226 A 5510 STRUCTURE BOEING 767 767300 1385204 NM HORIZONTAL STAB CORRODED W QOCF K NONE O OTHER IN INSP/MAINT 1 WP 03 16605 26064 TWO DEEP SITES CORROSION WERE FOUND WITH LT HORIZONTAL STAB, CUTOUT THE DAMAGE PORTION & PERFORM EXTERNAL REPAIR BY USIN G TWO DOUBLER. TWO DEEP SITES CORROSION WERE FOUND WITH INBOARD MAIN FLAP LOWER. CUTOUT THE DAMAGE PORTION & PERFORM S PLICE REPAIR BY USING TWO ANGLES ON EACH SIDE OF TEE CHORD. BEARING FREELY ROTATED & GAP BETWEEN BEARING OUTER RACE & F ITTING LUG ON NR 1 PYLON LT SIDE FITTING & PYLON RT SIDE LOADING FITTING, REPLACE THE SUBJECT BEARING. 2 L 7 2 4F RT A1NM 2003011500080 20030115 00080 EU 2003 1 15 02FDEA00982 1 20021231 A 3020 ANTI-ICE VALVE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE NR 1 ENGINE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 655FE 742 EN ROUTE, DESTINATION ICING CONDITIONS EXISTED. NR 1 ENGINE NACELLE ANTI-ICE VALVE FAILED TO OPEN WHEN SELECTED. RELEA SED FOR SERVICE IAW MEL/CDL. NR 1 ANTI-ICE INOPERATIVE ENGINE NACELLE. VALVES SECURED OPEN. REMOVED AND REPLACED NR 1 ENGINE NACELLE ANTI-ICE VALVE. OPS CHECK'S OK PER M/M REF 30-21-11-4-01. 2 L 7 2 4F 4 F RT A35EU E13NE 2003011500081 20030115 00081 EU 2003 1 15 02FDEA00983 1 20021218 A 5712 RIB AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 LEFT WING, MAIN LANDING GEAR RIB 5 HOLE NR 52, GOUGED. 2 L 7 2 4F 4 F RT A35EU E13NE 2003011500082 20030115 00082 EU 2003 1 15 02FDEA00984 1 20021218 A 5712 RIB AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE RT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 RIGHT WING MAIN LANDING GEAR RIB 5 HOLE NR 47 GOUGED. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F 4 F RT A35EU E13NE 2003011500083 20030115 00083 EU 2003 1 15 02FDEA00985 1 20021218 A 5712 RIB AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 LEFT WING MAIN LANDING GEAR, RIB 5 HOLE NR 52 IS GOUGED. REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A35EU E13NE 2003011500084 20030115 00084 SW 2003 1 15 AC2A082960 1 20021218 A 3340 A402AR LENS BELL 430 430 1182150 SW TAILBOOM STROBE CRACKED H AC2A K NONE L NO TEST IN INSP/MAINT 1 FS 01 430CM 10 49090 TAILBOOM STOBE LENS IS CRACKED. THIS LENS HAD 10 (TEN) HOURS TOTAL TIME. REPLACED LENS. 1 G 7 2 3U RT H9SW 2003011500087 20030115 00087 SW 2003 1 15 AC2A082961 1 20021222 A 3340 A402AR LENS BELL 430 430 1182150 SW TAILBOOM STROBE CRACKED H AC2A K NONE L NO TEST IN INSP/MAINT 1 FS 01 430CV 49072 TAILBOOM STROBE LENS IS CRACKED. REPLACED LENS. 1 G 7 2 3U RT H9SW 2003011500089 20030115 00089 SW 2003 1 15 AC2A082962 1 20021222 A 3340 A402AR LENS BELL 430 430 1182150 SW TAILBOOM STOBE CRACKED H AC2A K NONE L NO TEST IN INSP/MAINT 1 FS 01 430CM 49090 TAILBOOM STROBE LENS IS CRACKED. REPLACED LENS. 1 G 7 2 3U RT H9SW 2003011500104 20030115 00104 EU 2003 1 15 BAQA081542 1 20021127 A 3340 G62505 SEARCH LIGHT BOLKMS 117 BK117A4 5626017 EU EXTERIOR MALFUNCTIONED H BAQA O OTHER O OTHER NR NOT REPORTED 1 FS 01 117CJ 7051 SEARCH LIGHT WILL NOT EXTEND OR RETRACT. REPLACED WITH SERVICEABLE LIGHT. 1 G 7 2 3U H13EU 2003011500109 20030115 00109 EU 2003 1 15 BAQA082137 1 20021217 A 6730 SC7282 SERVO AEROSP SA365 SA365N 8680669 EU SERVO SYS LEAKING H BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 FS 01 199SM 732 6396 SERVO LEAKING BETWEEN VALVE BODIES. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H10EU 2003011500110 20030115 00110 EU 2003 1 15 BAQA082725 1 20021230 A 7712 430109910 SENSOR BOLKMS 117 BK117A4 5626017 EU TORQUE INDICATOR INACCURATE H BAQA O OTHER N FALSE WARNING NR NOT REPORTED 1 FS 01 117CJ 2008 7051 PILOTS REPORTED TORQUE SPLITS. REPLACED WITH SERVICEABLE TORQUE SENSOR. 1 G 7 2 3U H13EU 2003011500128 20030115 00128 NM 2003 1 15 03FDEA00020 1 20021111 A 5312 69191222 BULKHEAD BOEING 727 727227 1384078 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 483FE 21465 GENERATED DUE TO NOSE LANDING GEAR DOWNLOCK ACTUATOR FITTING CRACKED. UPON REPLACEMENT OF SUPPORT, FOUND NOSE LANDING G EAR AFT BULKHEAD WEB AND CHANNEL SUPPORT CRACKED. WEB REPAIR WAS ACCOMPLISHED IAW EA NR 7-5310-64754. 2 L 7 3 4F 4 F A3WE E2EA 2003011500130 20030115 00130 CE 2003 1 15 044606 1 20021030 A 3246 1143880251 WHEEL BEECH 1900 1900D 1154162 CE RT MLG FAILED A AMWA K NONE S AFFECT SYSTEMS LD LANDING 1 CE 07 140ZV 685 685 UE140 UPON LANDING FLIGHT 2624, THE CREW REPORTED A BAD BRAKE ACTION FROM THE RIGHT BRAKE. THE RIGHT BRAKE PEDAL FELT MUSHY. AFTER THE AIRCRAFT WAS TAXIED, THE CREW INSPECTED THE AIRCRAFT'S RIGHT WHEEL AND FOUND METAL SHAVINGS IN THE WHEEL ASSEM BLY. CHANGED THE LANDING GEAR, RIGGED AND DID TRACTION CHECKS THEY ALSO CHANGED THE MAIN WHEEL ASSEMBLY. THE TEARDOWN REPORT REVEALED THAT THE VENDOR INSTALLED SERVICEABLE TIRES AND BOLTS, THEREFORE THE MAIN WHEEL ASSEMBLY WAS OVERHAULED AND REASSEMBLED. 2 L 7 2 4T RT A24CE 2003022000098 20030220 00098 CE 2003 2 20 044910 1 20021107 A 7120 12991004717 TRUSS BEECH 1900 1900D 1154162 CE LT ENGINE CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 171ZV 1917 1917 UE171 WHILE PERFORMING AN "H" CHECK ON LT ENGINE TRUSS, MAINT FOUND A CRACK AT THE OUTBOARD COWLING ATTACH BRACKET. MAINT R & R WITH ANOTHER TRUSS. UPON RECEIPT OF OLD TRUSS, VENDOR DID A REPORT. REPORT REVEALED THAT A CRACK AT BOTH UPPER COWL ING BRACKETS AND CHAFED AT LT BRACKET. PERFORMED AN 8000 HOUR MAG PARTICLE INSPECTION IAW REPS MM. VENDOR REPAIRED TRUSS SUPPORT BRACKET MOUNTS IAW REPAIR DRAWING SR-CO-00012 REV "B". COMPLIED WITH "H" CHECK INSPECTION IAW REPS SRM. VISUAL LY VERIFIED THE COMPLETION OF SB 71-3024 AND SB 71-3144 REV "I" HAS BEEN PREVIOUSLY COMPLIED WITH IAW AD 2001-22-16. BLE NDED CHAFE AT LT UPPER BRACKET TO WITHIN LIMITS IAW SRM 71-91-03. 2 L 7 2 4T RT A24CE 2003011500131 20030115 00131 EU 2003 1 15 ERAA082917 1 20021218 A 2432 EE00050111 BATTERY SNIAS AS332 AS332C 8680808 EU EPU DEFECTIVE H ERAA O OTHER O OTHER NR NOT REPORTED 1 FS 01 170EH 129 2016 EPU BATTERY RECEIVED WITH 129.0 HRS AND CONTINUOUSLY BLOWS 10 AMP FUSE WITH 28V. 2 G 7 2 4U H4EU 2003011500132 20030115 00132 EU 2003 1 15 ERAA082919 1 20021219 A 6420 SLEEVE BOLKMS 105 BO105S 5626006 EU TAIL ROTOR HEAD CRACKED H ERAA O OTHER O OTHER NR NOT REPORTED 1 FS 01 13466 294 INNER SLEEVE BUSHING CRACKED. INNER SLEEVE BUSHINGS WORN. ONE CONTROL LEVER SCRAP, INNER SLEEVE BUSHINGS SCRAP, MOUNTI NG FORK BUSHINGS, SEALS, RINGS, & SLEEVES SCRAP, END CAPS ROTTEN. DISASSEMBLED, CLEANED & VISUALLY INSPECTED. REPAIRED ONE CONTROL LEVER, 4 INNER SLEEVE BUSHINGS, AND MOUNTING FOR TEFLON BUSHINGS, SEALS, RINGS, SLEEVES AND END CAPS. C/W 1 200 HR & 2400 HR/6 YEAR INSPECTIONS ON TAIL ROTOR. 300 HR & 2400 HR BLADE INSPECTIONS DONE. REASSEMBLED HUB, TORQUED A ND SAFETIED AS REQUIRED. INSTALLED 2 SERVICEABLE BLADES AND STATIC BALANCED. INSPECTED AND REPAIRED IAW BO105 REM 301, MM 33, 34, & 107 TT 103,446.2 TSI -0-. 1 G 7 2 3U H3EU 2003011500133 20030115 00133 EU 2003 1 15 ERAA082921 1 20021231 A 6420 10531714 ROTOR HEAD BOLKMS 105 BO105S 5626006 EU TAIL ROTOR BINDING H ERAA O OTHER J WARNING INDICATION HO HOVERING 1 FS 01 130EH 8819 558 TAIL ROTOR CONTROLS BINDING AND STIFF IN HOVER. NO OBVIOUS DEFECTS. REMOVED BLADES AND MOUNTING FORKS. VISUALLY INSPE CTED SURFACES OF TEFLON AND STEEL BUSHINGS AND FOUND NO DEFECTS. PERFORMED SLIDING FRICTION TEST AND FOUND NO DEFECTS. REASSEMBLED, TORQUED AND SAFETIED AS REQUIRED. INSTALLED 2 SERVICEABLE BLADES AND STATIC BALANCED. INSPECTED IAW BO-10 5. RE, 301, MM CH 33, 34, & 107. TT 8818.8 TSI 31.2 1 G 7 2 3U H3EU 2003011500135 20030115 00135 EU 2003 1 15 ERAA082922 1 20021231 A 6420 10531714 ROTOR HEAD BOLKMS 105 BO105S 5626006 EU TAIL ROTOR DAMAGED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 426EH 3943 552 INNER SLEEVE BUSHINGS DAMAGED. BLADE PAINT ERRODED & CRACKING, INNER SLEEVE BUSHINGS WORN & ONE PITCH HORN CONTROL BOLT DEBONDED. COMPLETELY DISASSEMBLED TAIL ROTOR, CLEANED & VISUALLY INSPECTED. REPLACED GRIP BUSHINGS (TEFLON) AND ONE RI NG, CONTROL LEVER BOLTS & BUSHINGS. REPLACED INNER SLEEVE BUSHINGS. COMPLIED WITH 2400 HR / 6 YR INSPECTIONS ON TAIL R OTOR AND 300 HR & 2400 HR BLADE INSPECTGIONS WERE DONE. ASSEMBLED WITH NEW NUTS, WASHERS, & GASKETS. INSTALLED 2 SERVIC EABLE BLADES AND STATIC BALANCED. INSPECTED, REPAIRED IAW BO-105 REM 301, MM 33, 34, & 107. 1 G 7 2 3U H3EU 2003011500136 20030115 00136 EU 2003 1 15 ERAA082923 1 20021231 A 6420 10531714 ROTOR HEAD BOLKMS 105 BO105S 5626006 EU TAIL ROTOR DAMAGED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 128EH 13724 572 IMPACT DAMAGE TO BLADE. PITCH CHANGE BUSHINGS WORN. BLADE PAINT CHIPPED OFF IN ONE AREA. PITCH CHANGE BUSHINGS WORN. DISASSEMBLED, CLEANED & VISUALLY INSPECTED. REPLACED INNER SLEEVE BUSHINGS, STRAP PACK BOLTS, GRIP TEFLON BUSHINGS, S EALS & 1 RING. COMPLIED WITH 1200 HR & 2400 HR / 6 YEAR INSPECTIONS ON TAIL ROTOR. 300 HR & 2400 HR BLADE INSPECTIONS DONE BY AMERICAN EUROCOPTER. REASSEMBLED WITH NEW HARDWARE, TORQUED & SAFETY WIRED AS REQUIRED. INSTALLED 2 SERVICEABL E BLADES & STATIC BALANCED. INSPECTED & REPAIRED. 1 G 7 2 3U H3EU 2003011500138 20030115 00138 EU 2003 1 15 ERAA082924 1 20021231 A 3212 D24762102 FLOAT BOLKMS 105 BO105S 5626006 EU EMERGENCY MLG LEAKING H ERAA K NONE L NO TEST IN INSP/MAINT 1 FS 01 298EH 920 S845 FLOAT BAG IS LEAKING THROUGH FABRIC IN SEVERAL PLACES. COMPLIED WITH ALL REPAIRS , TESTS AND INSPECTIONS IAW 25-60-95. 1 G 7 2 3U H3EU 2003011500139 20030115 00139 SW 2003 1 15 ERAA082925 1 20021231 A 3212 D24921119 FLOAT BELL 412 412 1182202 SW EMERGENCY MLG LEAKING A ERAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 421EH 593 33067 FLOAT BAG LEAKS. FLOAT COMPLIED WITH REPAIRS, ALL INSPECTIONS AND TESTS SERVICEABLE IAW SI-412-2. 1 G 7 2 4U H4SW 2003011500140 20030115 00140 SW 2003 1 15 ERAA082926 1 20021231 A 3212 D24922117 FLOAT BELL 412 412 1182202 SW EMERGENCY MLG LEAKING H ERAA K NONE L NO TEST IN INSP/MAINT 1 FS 01 1187 FLOAT BAG LEAKS. FLOAT WAS REPAIRED, COMPLIED WITH ALL TESTS & ALL INSPECTIONS. SERVICEABLE IAW SI-412-2. 1 G 7 2 4U H4SW 2003011500141 20030115 00141 2003 1 15 ERAA082927 4 20021231 A 3442 40008330208 INDICATOR BELL 412 412 1182202 SW WX RADAR SYS SMOKE H ERAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 FS 01 415EH 33009 SMOKE AND ODOR IN COCKPIT, SUSPECT SMOKE AND ODOR CAME FROM WEATHER RADAR INDICATOR. TESTED GOOD ON BENCH 1 G 7 2 4U H4SW 2003011500146 20030115 00146 WP 2003 1 15 ZW0A0212202 1 20021211 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9409F 53121 THE CABIN ROW 22 EGRESS LIGHTS WERE INOPERATIVE AND HAD A BROKEN TRACK COVER. REPLACED THE COVER AND RECONNECTED THE EG RESS LIGHT CONNECTOR. 2 L 7 2 4F RT A6WE 2003011500147 20030115 00147 NM 2003 1 15 ZW0A0212302 1 20021212 A 3350 CHARGER BOEING 757 757231 1384950 NM CABIN FAILED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 719TW 28487 THE EGRESS LIGHTS WERE INOPERATIVE AT ROW 26. REPLACED POWER SUPPLY AND POWER SUPPLY BATTERY, DUE TO FAILURE OF BATTERY CHARGER. 2 L 7 2 4F RT A2NM 2003011500148 20030115 00148 NM 2003 1 15 ZW0A0212501 1 20021218 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN MALFUNCTIONED A ZW0A K NONE O OTHER DE DESCENT 1 CE 13 719TW 28487 THE CREW REPORTED EMERGENCY LIGHTS CAME ON IN DESCENT AND STAYED ON EVEN WITH THE SWITCH TURNED OFF. MAINTENANCE WAS UN ABLE TO DUPLICATE THE PROBLEM. OPERATION CHECKED NORMAL. 2 L 7 2 4F RT A2NM 2003011500150 20030115 00150 WP 2003 1 15 ZW0A0212601 1 20021218 A 3350 408822101 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 952U 49266 THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE FROM THE GALLEYS TO THE AFT LAVS, ROW 12 THROUGH 22, AND ABOVE THE AFT FLI GHT ATTENDANT POSITION. REPLACED THE POWER SUPPLY FOR EACH OF THE LOCATIONS. 2 L 7 2 4F A6WE 2003011500151 20030115 00151 WP 2003 1 15 ZW0A0212602 1 20021218 A 3350 408822101 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 952U 49266 THE TAIL COMPARTMENT EMERGENCY WHITE LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY. 2 L 7 2 4F A6WE 2003011500152 20030115 00152 WP 2003 1 15 ZW0A0212604 1 20021219 A 3350 408822101 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 901TW 49166 THE CEILING EMERGENCY LIGHTS AT ROW 8 THROUGH 16 AND ROW 21 THROUGH 31, AND THE EGRESS LIGHTS IN THE FIRST CLASS CABIN, WERE INOPERATIVE. REPLACED THE POWER SUPPLY AT EACH OF THE LOCATIONS. 2 L 7 2 4F A6WE 2003011500154 20030115 00154 WP 2003 1 15 ZW0A0212701 1 20021222 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9409F 53121 THE L1 DOOR EMERGENCY PORTABLE LIGHT, THE AFT FLIGHT ATTENDANT SEAT CEILING LIGHT JUST FWD OF RT LAV, AND THE FLOOR EGRE SS LAMP AT SEAT ROWS 6 AND 9, WERE ALL INOPERATIVE. REPLACED THE PORTABLE LIGHT, REPLACED THE BATTERY PACK AT AFT LAV, AND REPLACED BOTH EGRESS LIGHT LAMPS. 2 L 7 2 4F RT A6WE 2003011500156 20030115 00156 WP 2003 1 15 ZW0A0212702 1 20021222 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 9304C 49530 THE EMERGENCY EXIT LIGHT ABOVE THE OVERWING EXIT DOOR ROW 21 LEFT AND RT SIDE, WERE INOPERATIVE. REPLACED THE BATTERY P ACK. 2 L 7 2 4F RT A6WE 2003011500157 20030115 00157 WP 2003 1 15 ZW0A0212801 1 20021223 A 2150 SEAL DOUG DC9 DC983 3022083 WP HEAT EXCHANGER LOOSE A ZW0A A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 CE 13 9305N 49395 BOTH HEAT EXCHANGERS LEAKING NOT ALLOWING AIRCRAFT TO PRESSURIZE. TIGHTENED SEALS ON BOTH HEAT EXCHANGERS. 2 L 7 2 4F RT A6WE 2003011500160 20030115 00160 WP 2003 1 15 ASAA02280553 1 20021110 A 5313 593666713 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, LONGERON 30 CORRODED ON BOTTOM AND HORIZONTAL LEG AT FS 1237 AND 1245. BLENDED CORROSION AND REP AIRED PER BAC TLX AOC-OKC-02-00083H, EA 5310-02126. (M) 2 L 7 2 4F RT A6WE 2003011500161 20030115 00161 NM 2003 1 15 ASAA024166 1 20021024 A 3350 8100022607 CONNECTOR BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 769AS 25103 PDX - FOUND EMERGENCY FLOOR LIGHTS ARE INOPERATIVE AT ROWS 14-16. RECONNECTED TRACK LIGHTS. TRACK LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2003011500162 20030115 00162 WP 2003 1 15 ASAA0280421 1 20021019 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE FROM ROW 2 FORWARD. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003011500163 20030115 00163 WP 2003 1 15 ASAA0280446 1 20021027 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 937AS 15449 173 49364 SEA - DURING LINE CHECK, FOUND THAT EXTERNAL EMERGENCY LIGHTS STAYED ON WITH SWITCH OFF AND EXTINGUISHED WITH SWITCH IN ARMED POSITION. REPLACED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2003011500164 20030115 00164 WP 2003 1 15 ASAA0280447 1 20021025 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 SAN - DURING PREFLIGHT CHECK, FOUND THAT EXTERNAL EMERGENCY LIGHTS INOPERATIVE FORWARD OF ROW 10. REPLACED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2003011500165 20030115 00165 NM 2003 1 15 ASAA0280513 1 20021101 A 3350 0105606 CONNECTOR DOUG MD80 MD83 3023681 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 981AS 53472 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE CONNECTION . LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT 2003011500166 20030115 00166 WP 2003 1 15 ASAA0280515 1 20021102 A 3350 MODULE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 6. REPLACED TRACK LIGHT MODULE. TRACK LIGHTS T HEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2003011500167 20030115 00167 WP 2003 1 15 ASAA0280543 1 20021113 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53078 2316 53449 LAX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY, INC LUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2003011500168 20030115 00168 WP 2003 1 15 ASAA0280545 1 20021110 A 5330 593602229 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, SKIN CORRODED ON INNER SURFACE AROUND FASTENER HOLES AND SEALANT AT FS 1079-1098, LONGERON 28L-28 R. REMOVED CORROSION AND REPAIRED PER BAC TLX AOC-OKC-02-0088H AND EA 5330-01609. (M) 2 L 7 2 4F RT A6WE 2003011500169 20030115 00169 WP 2003 1 15 ASAA0280546 1 20021110 A 5313 59360281 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, LONGERON 30 CORRODED BY FASTENER AT FS 1007-1022. REMOVED CORROSION AND FASTENER. REPAIRED PER BAC TLX AOC-OKC-02-00080H AND EA 5310-02131. (M) 2 L 7 2 4F RT A6WE 2003011500170 20030115 00170 WP 2003 1 15 ASAA0280550 1 20021110 A 5313 59360281 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, LONGERON 30 IS CORRODED AT SPLICE AT FS 1193-1212 ON LOWER SIDE. BLENDED CORROSION, THEN REPAIRE D PER BAC TLX AOC-OKC-02-0087H AND EA 5310-02133. (M) 2 L 7 2 4F RT A6WE 2003011500171 20030115 00171 WP 2003 1 15 ASAA0280554 1 20021110 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, LONGERON 29R CORRODED IN TWO AREAS AT FS 1212-1231. BLENDED CORROSION AND REPAIRED PER BAC TLX A OC-OKC-02-00090H, EA 5310-02135. (M) 2 L 7 2 4F RT A6WE 2003011500172 20030115 00172 WP 2003 1 15 ASAA0280555 1 20021110 A 5311 59624501 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 OKC - FOUND 30K CHECK, FRAME CORRODED ON AFT SIDE AT FS 1060 BETWEEN LONGERON 29L AND 30. CUT OUT DAMAGE AND REPAIRED P ER BAC TLX AOC-OKC-02-00095H, EA 5310-02137. (M) 2 L 7 2 4F RT A6WE 2003011500173 20030115 00173 WP 2003 1 15 ASAA0280605 1 20021119 A 5310 5936395501 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 960AS 53074 OAK C-CHECK, RIGHT MLG AFT DOOR JAMB HAS 1 INCH CRACK AT UPPER END. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53 -01, 51-10-2, AND 51-30-1. (M) 2 L 7 2 4F RT A6WE 2003011500174 20030115 00174 WP 2003 1 15 ASAA0280606 1 20021121 A 5320 SR0953013713 SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 960AS 53074 OAK - FOUND C-CHECK, SPLICE CORRODED AROUND FASTENERS IN AFT CARGO BAY AT FS 1250-1271, L30. REPLACED SPLICE PER SRM 53 -02, 51-10-4, 51-10-3, 51-10-3B, AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003011500175 20030115 00175 WP 2003 1 15 ASAA0280609 1 20021122 A 5230 5956273 LATCH DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND 30K CHECK, MID CARGO BAY DOOR HOLD-OPEN LATCHES AND CORNER BRACKET CRACKED AT FORWARD END. REPLACED HOLD-OP EN LATCHES AND BRACKET PER SRM 51-10-2, 51-10-4, 51-30-3 AND DAC DWG 5956273. (M) 2 L 7 2 4F RT A6WE 2003011500176 20030115 00176 WP 2003 1 15 ASAA0280610 1 20021124 A 5753 49140551 PANEL DOUG DC9 DC983 3022083 WP T/E FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND 30K CHECK, LEFT WING FLAP EXPANSION JOINT PANEL NR 1531A HAS FRETTING CORROSION. REPLACED EXPANSION JOINT P ANEL PER SRM 57-50-14, 51-10-2, 51-10-4, AND 51-10-3. (M) 2 L 7 2 4F RT A6WE 2003011500177 20030115 00177 WP 2003 1 15 ASAA0280611 1 20021125 A 5311 27779306 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 960AS 53074 OAK - DURING C-CHECK, AFT CARGO BAY FLOOR SUPPORT CIRCUMFERENTIAL FRAME CORRODED ON AFT SIDE AT FS 1271. REPLACED FRAME PER SRM 51-10-3, 51-C1, 53-C3, 51-10-4, AND 51-10-3B. (M) 2 L 7 2 4F RT A6WE 2003011500178 20030115 00178 WP 2003 1 15 ASAA0280612 1 20021126 A 5310 3938383 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 960AS 53074 OAK - FOUND C-CHECK, FORWARD ACCESSORY COMPARTMENT DOOR JAMB FOUND WORN IN SEVERAL AREAS AROUND CIRCUMFERENCE. INSTALLE D DOUBLER ON DOOR JAMB PER SRM 53-01 AND 53-10-3. (M) 2 L 7 2 4F RT A6WE 2003011500179 20030115 00179 WP 2003 1 15 ASAA0280617 1 20021202 A 5347 5936663503 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 960AS 53074 OAK - FOUND C-CHECK, FOUND CORROSION ON SCREW HOLES AND MOUNT SCREWS ON LEFT TIEDOWN TRACK IN AFT CARGO BAY AT FS 1007 T O 1307 ABOVE LONGERON 28L. REPLACED TIEDOWN TRACK PER SRM 51-10-4, 51-30-1, AND 51-10-3. (M) 2 L 7 2 4F RT A6WE 2003011500180 20030115 00180 WP 2003 1 15 ASAA0280618 1 20021202 A 5320 SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 960AS 53074 OAK - FOUND CORROSION ON C-CHECK, LONGERON 30 SPLICE SECTION AT FS 1200-1240 IN AFT CARGO BAY. REPLACED SPLICE SECTION PER BAC DWG 5936050, SRM 51-10-4, AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003011500181 20030115 00181 WP 2003 1 15 ASAA0280619 1 20021202 A 5320 5936660167 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 960AS 53074 OAK - FOUND C-CHECK CORROSION ON Z-ANGLE IN AFT CARGO BAY AT FS 1145-1155 ABOVE LONGERON 28R. REPLACED Z-ANGLE PER SRM 51-10-4, 51-10-3, 51-30-1, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003011500182 20030115 00182 WP 2003 1 15 ASAA0280620 1 20021202 A 5313 59360281 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 960AS 53074 OAK - FOUND C-CHECK, CORRODED ON LONGERON 30 AT FS 1007. REPLACED DAMAGED SECTION PER EA 5310-02147. (M) 2 L 7 2 4F RT A6WE 2003011500183 20030115 00183 WP 2003 1 15 ASAA0280621 1 20021202 A 5532 59121662801 SKIN DOUG DC9 DC983 3022083 WP VERTICAL STAB GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 960AS 53074 OAK - FOUND C-CHECK, VERTICAL STABILIZER SKIN GOUGED AT UPPER ATTACH POINT FOR ELEPHANT EAR FAIRING. REPLACED DAMAGED S KIN PER SRM 51-10-4, 51-10-3, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003011500184 20030115 00184 NM 2003 1 15 C7WA200200036 1 20021030 A 3231 DOOR BOEING 727 727225 1384077 NM RT MLG OUT OF RIG A C7WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 17 8887Z 21856 UPON GEAR RETRACTION RED RIGHT GEAR LIGHT AND RED DOORS LIGHT REMAIN ILLUMINATED. CYCLED GEAR 3 TIMES, NO HELP. AIR TU RNBACK. RE-RIGGED RIGHT GEAR DOOR PER MM 32-12-1, PAGE 501-502. GROUND TEST OK. (M) 2 L 7 3 4F A3WE 2003011500185 20030115 00185 NM 2003 1 15 C7WA200200037 1 20021030 A 3610 BACC10DU450 CLAMP BOEING 727 727225 1384077 NM NR 3 STRUT LOOSE A C7WA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 17 8887Z 21856 NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED ON TAKEOFF, EPRS 2.01/2.03 WHEN THROTTLES BACKED OFF TO 1.7 EPR LIGHT EXTIN GUISHED. TIGHTENED LOOSE CLAMP IN STRUT AREA PER MM 75-00 AND 20-80-1. (M) 2 L 7 3 4F A3WE 2003011500186 20030115 00186 NE 2003 1 15 SIMA200227902 2 20021004 A 7321 FUEL CONTROL CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ENGINE MALFUNCTIONED A SIMA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 501BG 10017 XNA - FLT 3837 - DURING CRUISE FLIGHT CREW REPORTED AN INTERMITTENT CAUTION MESSAGE ON EICAS WITH AN ENGINE ONE ITT SPIK E. CREW DECLARED AN EMERGENCY, REDUCED POWER AND CONTINUED TO XNA AND LANDED WITH NO FURTHER PROBLEMS. MAINTENANCE RES ET FADECS, OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2003011500187 20030115 00187 SO 2003 1 15 SIMA200231701 1 20021107 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 738NR 145401 ABI - DURING AN MBV INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABR ICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 (SRM 145/1142, CHAPTER 53, REV 19) 53-21-10 PAR A 2 FIG 201 SHEET 2 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2003011500189 20030115 00189 WP 2003 1 15 ZW0A0212902 1 20021226 A 3222 VALVE DOUG DC9 DC983 3022083 WP NLG DEFECTIVE A ZW0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 13 9305N 49395 NOSE GEAR STRUT FLAT NOT ALLOWING GEAR TO RETRACT. REMOVED AND REPLACED SCHRADER VALVE AND RESERVICED STRUT. 2 L 7 2 4F RT A6WE 2003011500191 20030115 00191 NE 2003 1 15 ZW0A0213001 2 20021227 A 7230 COMPRESSOR BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A ZW0A E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 13 725TW 30338 4913 AFTER TAKE OFF, DURING GEAR RETRACTION, THE NR 1 ENGINE STALLED AND ENGINE PARAMETERS STARTED FALLING OFF. FLIGHT RETUR NED TO LGA. COMPRESSOR DAMAGE WAS FOUND DURING BORESCOPE AND THE ENGINE WAS REPLACED. THE HPC 10TH - 11TH STATOR FAILE D. 2 L 7 2 4F 4 F RT A2NM E17NE 2003011500192 20030115 00192 WP 2003 1 15 ZW0A0213003 1 20021227 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ZW0A K NONE L NO TEST NR NOT REPORTED 1 CE 13 963TW 53613 THE EGRESS LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. REPAIRED WIRE AT SPLICE. 2 L 7 2 4F RT A6WE 2003011500194 20030115 00194 WP 2003 1 15 ZW0A0213102 1 20021218 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 983TW 53633 DURING CHECK-C FOUND ON THE FWD LT FUSELAGE ALL BLIND FASTENERS IN A LARGE REPAIR AT STA 218, LONGERON 18L TO 19L. REMO VED EXISTING REPAIR. CUTOUT DAMAGED SKIN AND INSTALLED FILLER AND DOUBLER PER SRM 53-04, FIG 12B, SHEET 34. 2 L 7 2 4F RT A6WE 2003011500198 20030115 00198 NM 2003 1 15 DL733021446 1 20021216 A 5330 6545775594 SKIN BOEING 737 737347 1384647 NM FS 727D, S-23R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311WA 23597 FUSELAGE / SKIN / FS 727D / STRG. 23R : CRACK REPAIR A 3" CRACK WAS FOUND IN THE FUSELAGE SKIN JUST AFT OF FS 727D. THE CRACK RAN ALONG THE EDGE OF THE INTERNAL BONDED INTERNAL DOUBLER JUST BELOW STRINGER 23R. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 384315-14. 2 L 7 2 4F RT A16WE 2003011500199 20030115 00199 NM 2003 1 15 DL73K021447 1 20021214 A 5312 BULKHEAD BOEING 737 737232 1384475 NM FS 1016, BL0 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 325DL 23097 FUSELAGE / AFT PRESSURE BULKHEAD / FS 1016 / BL 0 : CORROSION REPAIR THE AFT PRESSURE BULKHEAD WEB AND STIFFENER AT BL 0 WERE FOUND CORRODED. THE CORROSION IS TYPICAL OF BAC S/B 737-53A 1075 AND AD 2002-10-11. THE CORROSION WAS REMOVED AND REPAIRED PER THE REQUIREMENTS OF THE S/B AND DOCUMENTED PER ER/A 384295-14AD. 2 L 7 2 4F RT A16WE 2003011500200 20030115 00200 NM 2003 1 15 DL72S021449 1 20021213 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM S-4R, FS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 FUSELAGE / SKIN / FS 681-740 / STRG. 4R / SKIN LAP JOINT : CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP JOINT BETWEEN FS 681 & 740 GAVE CRACK INDICATIONS. INTERNAL MFEC INSPECTIONS CONFIRMED 8 CRACK LOCATIONS ALONG THE LOWER ROW OF FASTENERS IN THE LOWER SKIN PANEL. THE ENTIRE LAP JOINT WAS CUTOUT AN REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 384201-14AD, REV A. 2 L 7 3 4F A3WE 2003011500201 20030115 00201 NM 2003 1 15 DL757021453 1 20021217 A 5400 012N88883 SUPPORT FITTING BOEING 757 757232 1384965 NM #1 PYLON TOOL DAMAGE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 DURING ACCOMPLISHMENT OF PYLON MOD EO 6-70332-3AD, HOLE 5 IN THE LEFT WING SUPPORT FITTING HAD DAMAGE THAT REQUIRED REMO VAL PRIOR TO FASTENER INSTALLATION. REPAIRED PER ER/A 389427-14AD. REPAIR OVERSIZED HOLE, INSTAL LED FREEZE PLUG, THEN INSTALLED FASTENER PER EO. 2 L 7 2 4F RT A2NM 2003011500202 20030115 00202 NM 2003 1 15 DL72S021457 1 20021221 A 2910 10605582 ACTUATOR 95027 BOEING 727 727232 1384082 NM #4 LE INBD FLAP LEAKING A DALA O OTHER K FLUID LOSS AP APPROACH 1 SO 27 533DA 4225ADEGP 22046 ON APPROACH AFTER FLAPS 15 COMPLETE LOSS OF A SYSTEM QUANTITY AND PRESSURE. EMERGENCY PROCEDURES CHECKLIST FOLLOWED WITH MANUAL LANDING GEAR EXTENSION. A SYSTEM HYDRAULIC PUMPS WERE DEACTIVATED WITHIN 2 MINUTES CA_FOUND NBR 4 KREUGER FLAP ACTUATOR LEAKING. REPL SHUTTLE VVALVE PER MM. RMVD NBR 4 ACTUATOR FOUND ATTACH POINT O/B CRA SUPPORT BRACKET AND REPL NBR 4 KREUGER FLAP ACTUATOR PER OPN7054. 2 L 7 3 4F A3WE 2003011500203 20030115 00203 NM 2003 1 15 DL733021460 1 20021223 A 5410 311A11112 FITTING BOEING 737 737347 1384647 NM #1 PYLON CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307WA 23440 CORROSION WAS FOUND IN THE BORE OF THE #1 PYLON CROWN BEAM AFT FITTING. THE BORE WAS REAMED TO A DIAMETER OF 3.102" TO REMOVE THE CORROSION. THE DAMAGE WAS FOUND AT HMV. 2 L 7 2 4F RT A16WE 2003011500204 20030115 00204 NM 2003 1 15 DLM88021464 1 20021223 A 3200 7936937561 BRACKET 59164605509 DOUG MD88 MD88 3023688 NM W/W FAILED A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 920DE EFS21692 53423 AFTER T/O L/R MAIN GEAR WARNING LTS REMAINED ILLUM W/ AMBER GEAR DOOR CAUTION LT. NOTED THE EMERGENCY LNDG GEAR EXTENSI ON HANDLE DOOR COVER PARTIALLY RAISED AND HANDLE OUT OF DETENT. PUSHED HANDLE DOWN TO NRML POSITION RESULTING IN NORMAL INDICATION FOUND BRACKET BENT ON LEFT STRUT THAT SUPPORTS THE NUMBER 2 BRAKE HYDRAULIC LINE. OUT OF POSITION LINE CONTACTED ALT GEAR EXTEND MECH AT LEFT GEAR DOOR UPLOCK. REPLACED BRACKET, LINES, CLAMPS AND HARDWARE ON LEFT SHOCK STRUT. GEAR CYCLED NUMEROUS TIMES AND CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2003011500205 20030115 00205 NM 2003 1 15 DL76G021472 1 20021226 A 2410 734284F GCU BOEING 767 7673P6 1385105 NM RIGHT FAULTY A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 155DL 25269 R GEN OFF WITH SLIGHT ELECTRICAL SMELL INITIALLY. APU POWERING THE RIGHT BUS. NO SMELL NOW. BPCU SHOWS R GEN NO RESPONSE FROM CONTROL FAULT AND WILL NOT RESET. T/S PER FIM 24-20-00. ALL WIRING CHECKS OK PER TABLE PG 180Y. FOUND GEN MAIN WINDINGS OPEN TO NEUTRAL WINDING. REPLACED RT GCU AND RESET BPCU. REPLACED RT IDG PER MM. LEA CKS OK. FOUND PIN 5 ON D4266J SHORTED. REPLACED D4266J AND CHECK NOW OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2 L 7 2 4F RT A1NM 2003011500206 20030115 00206 NM 2003 1 15 DL72S021475 1 20021226 A 5500 RIB BOEING 727 727225A 1384077 NM VERTICLE FIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 VERT. STAB RIB L/H ATTACH ANGLE CRACKED AT FIN STA 133.800 AND STR 9LEFT REPAIR PER M/M 55-30-000-8 2 L 7 3 4F RT A3WE 2003011500207 20030115 00207 NM 2003 1 15 DL757021485 1 20021229 A 5330 143N34714 SKIN BOEING 757 757232 1384965 NM FS 600, S-26L GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 FUSELAGE / SKIN / FS 600 / STRG. 26L-27L : GOUGE REPAIR THE FUSELAGE SKIN WAS FOUND WITH 3 GOUGES AT FS 600 BETWEEN STRINGERS 26L & 27L. THE GOUGES WERE REMOVED WITH A SINGLE CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 384277-14. 2 L 7 2 4F RT A2NM 2003011600001 20030116 00001 EU 2003 1 16 BAQA081239 1 20021111 A 5312 1172463611 HINGE BOLKMS 117 BK117B1 5626012 EU BULKHEAD WORN H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 945ME 5952 7235 PRESSURE BULKHEAD. HOLES ARE WORN. REPLACED WITH SERVICEABLE HINGE. 1 G 7 2 3U H13EU 2003011600002 20030116 00002 EU 2003 1 16 BAQA081240 1 20021111 A 5312 1172463612 HINGE BOLKMS 117 BK117B1 5626012 EU BULKHEAD WORN H BAQA K NONE O OTHER IN INSP/MAINT 1 FS 01 945ME 7235 PRESSURE BULKHEAD. HOLES ARE WORN. REPLACED WITH SERVICEABLE HINGE. 1 G 7 2 3U H13EU 2003011600087 20030116 00087 NM 2003 1 16 02FDEA00978 1 20021227 A 2450 RELAY DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE AC SYSTEM FAILED A FDEA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 25 591FE 48527 MID-FLIGHT, EMERGENCY POWER ON ALERT ILLUMINATED. REVIEWED CHECK 20-30 WEST OF LIT, BATTERY LOW ALERT ILLUMINATED. SHO RTLY THEREAFTER MULTIPLE ELECT ALERTS OCCURRED. INCLUDING FCC 1B FAULT, FADEC ALT, ALL 3 ENGINES AND OTHERS. CAPTAIN, NR 1 AND NR 3 DU FAILED. NR 2 DU GAVE ATTITUDE ONLY, NO SPEED OR ALTITUDE. EMERGENCY DECLARED. CHECKLISTS COMPLETED. ON FINAL, LEFT EMERGENCY AC BUS FAIL OCCURRED. INSTALLED NEW AC BUS 1 SENSING RELAY IAW SMP A-3-15. ALL OPERATIONS /F UNCTIONS APPEAR TO BE NORMAL, AIRCRAFT ENGINE RUN COMPLETE OPS CHECK, GOOD. 2 L 7 3 4F 4 F RT A22WE E13NE 2003011600095 20030116 00095 WP 2003 1 16 12190279 2 20021219 A 7250 31081251 TURBINE BLADES SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL NR 1 ENGINE FAILED E HKGA E A ENGINE SHUTDOWN UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 17 373P 2462 AC538 P44264 768184 AFTER TAKEOFF, TOWER REPORTED THAT AIRCRAFT WAS TRAILING SMOKE. THE NR 1 ENGINE LOSS OF OIL PRESSURE FOLLOWED BY OIL WA RNING LIGHT. ELECTED TO SHUT ENGINE DOWN AND RETURN TO AIRPORT. SUBSEQUENT INSPECTION REVILED THAT A PROBABLE FAILURE O F ONE OR MORE 1ST STAGE TURBINE WHEEL BLADE(S), CAUSED A RUPTURE OF THE TURBINE BEARING OIL SUPPLY TUBE, CREATING THE RE PORTED SMOKE, OIL LOSS, AND LOSS OF OIL PRESSURE. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2003011600098 20030116 00098 EU 2003 1 16 1231001 1 20021231 A 2613 OVERHEAT SENSOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE FAILED A UHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 03 123XS 123 PILOT REPORTED THAT AFTER ROTATION FOR CLIMBOUT, LEFT TAILPIPE HOT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD, MAI NTENANCE DISPATCHED TO AIRCRAFT FOR REPAIR. 2 L 7 2 4T 4 T RT A52EU E8NE6 2003011600100 20030116 00100 NM 2003 1 16 2002F01113 1 20021206 A 5347 SEAT TRACK BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 517AT 27973 DURING SCHEDULED INSPECTION LEVEL 2 CORROSION DISCOVERED AT FORWARD FUSELAGE SECTION, FS 381, LBL 25, TM 91 IN SEAT ATTA CH TRACK. MAINTENANCE REMOVED AND REPLACED SEAT TRACK IAW SRM. 2 L 7 2 4F 4 F RT A2NM A12EU 2003011600104 20030116 00104 NM 2003 1 16 2002F01114 1 20021216 A 2420 BACC63CM2430PN CONNECTOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211* 54555 NE LT GENERATOR FAILED G AMTA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 GL 11 554TZ 3762 32588 AT TOP OF CLIMB, LEFT GENERATOR DRIVE LIGHT AND LEFT GENERATOR CONT OFF LIGHT ILLUMINATED AT THE SAME TIME. CREW DEACTI VATED SYSTEM. MAINTENANCE INSTALLED SERVICEABLE CONNECTOR PLUG, IAW WDM. OPERATIONAL CHECKS GOOD IAW MM. 2 L 7 2 4F 4 F RT A2NM A12EU 2003011600106 20030116 00106 2003 1 16 2002F01123 4 20021223 A 2565 LANYARD BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE R1 DOOR OUT OF POSITION G AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 518AT 27974 FLIGHT NR 155, PRIOR TO PUSHBACK RIGHT NR 1 DOOR SLIDE WOULD NOT ENGAGE. MAINTENANCE FOUND LANYARD IN GIRT BAR TRACK. REMOVED AND STOWED LANYARD, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM A12EU 2003011600108 20030116 00108 NM 2003 1 16 2002F01124 1 20021218 A 7720 INDICATOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211* 54555 NE COCKPIT FLUCTUATES G AMTA K NONE O OTHER CR CRUISE 1 GL 11 551TZ 32585 31811 FLIGHT NUMBER 538, DURING CRUISE, LEFT ENGINE INDICATOR FLUCTUATES, STANDBY ENGINE INDICATOR ALSO ABNORMAL. 2 L 7 2 4F 4 F RT A2NM A12EU 2003011600110 20030116 00110 NM 2003 1 16 2002F01125 1 20021208 A 5315 FLOORBEAM BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE FUSELAGE CORRODED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 517AT 27973 DURING SCHEDULED INSPECTION, MAINTENANCE FOUND LEVEL 2 CORROSION ON TOP AND BOTTOM FORWARD EDGE OF FLOORBEAM TOP CAP ARO UND FLOORBOARD ATTACH FORWARD BOLT HOLES. FS 365, RBL 0 TO RBL 52, TM 99. MAINTENANCE REPAIRED FLOORBEAM TOP CAP IAW S RM. 2 L 7 2 4F 4 F RT A2NM A12EU 2003011600136 20030116 00136 NM 2003 1 16 2002UALA01892 1 20021225 A 3150 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 305UA 23666 AFT CARGO LIGHT CAME ON JUST BEFORE V1. RETURN TO FIELD. 2 L 7 2 4F 4 F RT A16WE E2GL 2003011600150 20030116 00150 WP 2003 1 16 2003F00002 1 20021220 A 3350 59262 LIGHT LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 164AT 1238 DURING SCHEDULED INSPECTION, EMERGENCY LIGHT AT FORWARD GALLEY WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED FORWARD GALLEY LIGHT STRIP IAW MM, OPERATIONAL CHECK GOOD. 2 L 7 3 4F A23WE 2003011600152 20030116 00152 WP 2003 1 16 2003F00004 1 20021222 A 3350 516574 POWERPACK LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED G K NONE L NO TEST IN INSP/MAINT 1 GL 11 198AT 193B1111 DURING SCHEDULED INSPECTION R1 DOOR EXTERIOR EGRESS LIGHT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED R1 DOOR POWER PACK IAW MM, OPERATIONAL CHECK GOOD. 2 L 7 3 4F A23WE 2003011600154 20030116 00154 WP 2003 1 16 2003F00005 1 20021214 A 2697 7017J18 WIRE LKHEED 1011 1011385115 5265015 WP FIRE LOOP FAULTY G K NONE N FALSE WARNING CR CRUISE 1 GL 11 198AT 193B1111 FLIGHT NUMBER 7113. DURING CRUISE, NR 1 ENGINE FIRE DETECTION LOOP (B) ON INTERMITTENTLY. LOOP (A) TESTS FINE. MAINTEN ANCE REPLACED WIRE NUMBER 7017J18 AND SENSOR PLUGS IAW WDM. SYSTEM CHECKS GOOD IAW MM. 2 L 7 3 4F A23WE 2003011600160 20030116 00160 SO 2003 1 16 C2XA02CL251 1 20021220 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15555 145594 DURING ROUTINE MAINTENANCE THE LEFT AND RIGHT EXTERNAL OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2003011600161 20030116 00161 SO 2003 1 16 C2XA02IA254 1 20021230 A 3350 M8372375R1624N CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16559 145603 GSO- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS FAILED TO ILLUMINATE. GSO- MAINTENANCE INSPECTED AND T ROUBLESHOT THE AIRCRAFT. A LOOSE CONNECTOR WAS FOUND TO BE THE PROBLEM. THE CONNECTOR WAS RECONNECTED, AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS PERFORMED, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. 2 L 7 2 4T RT T00011AT 2003011600162 20030116 00162 GL 2003 1 16 C2XA02RI007 2 20021218 A 7261 OIL SYSTEM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE LEAKING A C2XA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 14907 145468 RIC-FLT 4161 CREW REPORTED OIL SMELL FROM ENGINE BLEEDS ON DESCENT. MAINTENANCE DETERMINED SMELL TO BE COMING FROM AN I NTERNAL OIL LEAK IN THE NR 1 ENGINE. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE PERFORMED OPERATIONAL AND LEAK TE STS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2003011600166 20030116 00166 SO 2003 1 16 C2XA02SH158 1 20021228 A 5320 14522460011 BUTT STRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 SHV- DURING C-CHECK BUTT STRAP AT FRAME 17 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED B UTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2003011600167 20030116 00167 SO 2003 1 16 C2XA02SH159 1 20021228 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 SHV - DURING C-CHECK LEFT HAND OMEGA BEAM WAS FOUND TO HAVE CORROSION ON DOUBLER INBOARD AT FRAME 20. MAINTENANCE REMOV ED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2003011600168 20030116 00168 SO 2003 1 16 C2XA02SH161 1 20021228 A 7110 14576517002 STRUCTURE EMB 145 EMB145LR 3260212 SO NR 1 COWLING GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 SHV - DURING C-CHECK NUMBER 1 LOWER COWLING OUTBOARD EDGE MEMBER WAS GOUGED BETWEEN STATIONS XN=2905.0 AND XN=3167.5. M AINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN T O SERVICE. 2 L 7 2 4T RT T00011AT 2003011600180 20030116 00180 SO 2003 1 16 C2XA02TY188 1 20021229 A 5315 14521721009 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17521 145378 TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD DIGITAL AT COCKPIT ENTRANCE. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED, ALODINED, PRIMED AND INSTALLED STRAPS, DOUBLERS AND SHIMS I/A/W-EMB-135/145-SRM-51-21-10, CMP- 51-21-04, 05 AND 06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2003011600181 20030116 00181 SO 2003 1 16 C2XA02TY189 1 20021229 A 5320 14510169005 STIFFENER EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17521 145378 TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND UNDER THE SERVICE DOOR THRESHOLD. MAINTENANCE REMOVED THE CORROS ION IAW-GST-1927/02A. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2003011600183 20030116 00183 EA 2003 1 16 COMA0260704 1 20021210 A 3040 THERMISTER CNDAIR CL600 CL6002B19 1900309 EA WINDOW MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 713CA 7245 FLIGHT 5859 LT WINDOW HEAT CAUTION MESSAGE. SWAPPED CONTROLLER CONNECTIONS TO THE SPARE THERMISTORS, OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F RT A21EA 2003011600224 20030116 00224 EU 2003 1 16 RAIA00211336 1 20021127 A 3350 LIGHT AEROSP ATR72 ATR72202 8680940 EU PAX STAIRS LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 721TE 217 5536-STL- EMERGENCY LIGHT AT PAX STAIRS INOP. SECURED LOOSE BULB IN AT PAX STAIR EMERGENCY LIGHT. 2 H 7 2 4T RT A53EU 2003011600227 20030116 00227 EU 2003 1 16 RAIA00212341 1 20021204 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 557HK 41074 5397-BWI- EMERGENCY PATH LIGHTS OUT ROWS 6-10. SECURED CONNECTOR AT EMERGENCY PATH LIGHTS, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2003011600229 20030116 00229 SO 2003 1 16 RAIA00212347 1 20021210 A 2931 NAS16125 O-RING EMB 145 EMB145 3260210 SO HYD SYSTEM DAMAGED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 801HK 145053 5316-PIT- NR 1 HYD SYSTEM FAIL WARNING. MAINTENANCE REMOVED AND REPLACED NR 1 PRESSURE SWITCH O-RING. NR 1 PUMP REMOVE D AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F RT T00011AT 2003011600231 20030116 00231 EU 2003 1 16 RAIA00212350 1 20021201 A 2611 SMOKE WARNING AEROSP ATR72 ATR72202 8680940 EU COCKPIT ACTIVATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 723TE 283 5598-STL- ELECTRICAL SMOKE WARNING INDICATION. MAINTENANCE GROUND RAN BOTH ENGINES AND PERFORMED SYSTEM CHECKS AND COUL D NOT DUPLICATE THE MALFUNCTION. ALL SYS OPS NORMAL AT THIS TIME. 2 H 7 2 4T RT A53EU 2003011600232 20030116 00232 SO 2003 1 16 RAIA00212354 1 20021215 A 3350 CONNECTOR EMB 145 EMB145ER 3260211 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 808HK 145157 MX-PIT- EMERGENCY PATH LIGHTING INOP. RECONNECTED EMERGENCY PATH LIGHTING ELECTRICAL CONNECTOR, OPS CHECK OK. 2 L 7 2 4F RT T00011AT 2003011600234 20030116 00234 SO 2003 1 16 RAIA00212360 1 20021217 A 3350 CONNECTOR EMB 145 EMB145ER 3260211 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 808HK 145157 5295-STL- EMERGENCY PATH LIGHTING INOP AT SEAT 1A. RESECURED EMERGENCY PATH LIGHT ELECTRICAL CONNECTOR, OPS CHECK OK. 2 L 7 2 4F RT T00011AT 2003011600235 20030116 00235 EU 2003 1 16 RAIA00212361 1 20021218 A 3350 CONNECTOR AEROSP ATR42 ATR42300 8680920 EU CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 423TE 119 5621-STL-EMERGENCY LIGHT AT PAX DOOR INOP. CLEANED LIGHT BULB CONNECTOR ON THE PAX DOOR EMERGENCY LIGHT, OPS CHECK OK. 2 H 7 2 4T RT A53EU 2003011600236 20030116 00236 EU 2003 1 16 RAIA00212369 1 20021226 A 3397 WIRE JETAIR JETSTM JETSTM4101 1500501 EU CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 574HK 41093 MX-STL- EMERGENCY PATH LIGHTS INOP ROWS 1-4. REPAIRED BROKEN WIRE AT EMERGENCY PATH STRIP, OPS CHECK OK. 2 L 7 2 4T RT A41NM 2003011600237 20030116 00237 SO 2003 1 16 RAIA00212371 1 20021231 A 4950 WARNING SYSTEM EMB 145 EMB145ER 3260211 SO COCKPIT ACTIVATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 808HK 145157 5305-PIT- APU BLEED VALVE FAULT INDICATION. MAINTENANCE DEFERRED PER MEL 49-52-02. 2 L 7 2 4F RT T00011AT 2003011600239 20030116 00239 NM 2003 1 16 ZW0A0212201 1 20021210 A 3350 20121 POWER SUPPLY BOEING 757 757231 1384950 NM CABIN DISCHARGED A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 719TW 28487 THE ROW 32 EMERGENCY AISLE LIGHTS AND THE AFT GALLEY WALL EMERGENCY LIGHTS GO OFF AND ON. REPLACED THE POWER SUPPLY IN THE LEFT SIDE AFT GALLEY CEILING. 2 L 7 2 4F RT A2NM 2003011600240 20030116 00240 NM 2003 1 16 ZW0A0213103 1 20021216 A 5320 ATTACH FITTING BOEING 757 757231 1384950 NM FUSELAGE CORRODED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 705TW 28479 DURING CHECK-C MAINT THE FWD CARGO DOOR FRAME, AFT BARRIER STRAP ATTACH FITTING, AT THRESHOLD, HAD INTERGRANULAR CORROSI ON. REMOVED FITTING, REMOVED CORROSION, AND REPLACED WITH NEW FITTING WITH HI-LOKS PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 2003011600241 20030116 00241 NM 2003 1 16 ZW0A0213104 1 20021211 A 5330 SKIN BOEING 757 757231 1384950 NM FUSELAGE BULGED A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 705TW 28479 DURING CHECK-C MAINT FOUND A BULGE IN THE FUSELAGE SKIN ABOUT STA 688, BETWEEN STRINGER 26R AND 27R. INSTALLED FLUSH RE PAIR PER SRM 53-00-01, FIGURE 208. 2 L 7 2 4F RT A2NM 2003011600249 20030116 00249 WP 2003 1 16 ABXA020366 1 20021219 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 EMERGENCY LIGHTING DIM. REMOVED AND REPLACED BATTERIES. OPS CHECKED GOOD IAW MM. 2 L 7 2 4F A6WE 2003011600250 20030116 00250 WP 2003 1 16 ABXA030008 1 20021216 A 5240 5936446503 PAN DOUG DC9 DC931 3022065 WP PWA JT8 JT8D* NE SERVICE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 SERVICE DOOR PAN CRACKED AT UPPER HINGE CUTOUT, INSIDE. REPAIRED AREA IAW SRM. REMOVED AND REINSTALLED SEAL RETAINER A ND STOPS IAW SRM. 2 L 7 2 4F 4 F A6WE E2EA 2003011600251 20030116 00251 WP 2003 1 16 ABXA030009 1 20021218 A 5523 5910413504 SKIN DOUG DC9 DC931 3022065 WP PWA JT8 JT8D1 52044 NE ELEVATOR TAB DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 RIGHT CONTROL TAB DELAMINATED IN NUMEROUS PLACES UPPER SKIN. REPLACED RIGHT ELEVATOR CONTROL TAB IAW DC-9 MM 27-30-03-2- 0000. 2 L 7 2 4F 4 F A6WE E2EA 2003011600252 20030116 00252 WP 2003 1 16 ABXA030010 1 20021218 A 5523 5910414502 SKIN DOUG DC9 DC931 3022065 WP PWA JT8 JT8D1 52044 NE ELEVATOR TAB DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 RIGHT GEAR TAB DELAMINATED IN NUMEROUS PLACES UPPER SURFACE. REPLACED RIGHT GEARED TAB IAW DC-9 MM 27-30-04-2-0001. 2 L 7 2 4F 4 F A6WE E2EA 2003011600253 20030116 00253 WP 2003 1 16 ABXA030011 1 20021218 A 5523 5910413501 SKIN DOUG DC9 DC931 3022065 WP PWA JT8 JT8D1 52044 NE ELEVATOR TAB DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 LEFT CONTROL TAB DELAMINATED UPPER SURFACE IN NUMEROUS PLACES. REPLACED LEFT ELEVATOR CONTROL TAB IAW DC-9 MM 27-30-03- 2-0001. 2 L 7 2 4F 4 F A6WE E2EA 2003011600254 20030116 00254 WP 2003 1 16 ABXA030012 1 20021219 A 5311 9919617501 FRAME DOUG DC9 DC931 3022065 WP PWA JT8 JT8D1 52044 NE FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 LEFT MAIN FRAME, STA 699, HAD CRACK IN FORWARD FLANGE FROM POINT J TO POINT G. REPAIRED LEFT MAIN FRAME IAW EA 53400100 -001-1. 2 L 7 2 4F 4 F A6WE E2EA 2003011600255 20030116 00255 NM 2003 1 16 ABXA030013 1 20021118 A 5313 143T300117 STRINGER BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 795AX 23145 STRINGER 19L, BETWEEN STA 632 AND STA 654, AFT SIDE OF EXISTING LAMP HAD CRACKS ON STRINGER. THE CRACKS LENGTH WERE APP ROXIMATELY .5 INCHES FROM THE EDGE OF STRINGER. PERFORMED STRINGER REPAIR IAW SRM 53-30-03 AND SRM 53-00-03, FIGURE 201 . PART OF STRINGER WITH CRACKS REMOVED AND THE AREA PROTECTED IAW SRM 51-10-02. THE PARTS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 2003011600256 20030116 00256 NM 2003 1 16 ABXA030014 1 20021120 A 5315 141T511194 FLOORBEAM BOEING 767 767281 1385109 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 796AX 23145 CABIN RIGHT SIDE STA 287 FLOORBEAM, RBL 73, FOUND CORROSION ON UPPER FLANGE OF FLOORBEAM, WL 199.5. PERFORMED FLOORBEAM UPPER CHORD REPAIR IAW SRM 53-00-51, FIGURE 201, REF SRM 53-10-51 AND DWG NR 141T5111. INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 2003011600257 20030116 00257 NM 2003 1 16 ABXA030015 1 20021128 A 5320 141T833073 TEE FITTING BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 795AX 23145 FORWARD FUSELAGE CABIN LEFT SIDE, WL 251.8, STA 287. FOUND CRACK ON TEE CONNECT TO FRAME. CRACKED TEE REMOVED AND INST ALLED NEW TEE, FASTENERS IAW SRM, INSTALLATION. 2 L 7 2 4F RT A1NM 2003011600270 20030116 00270 WP 2003 1 16 ABXA202365 1 20021220 A 3350 LIGHT DOUG DC8 DC863F 302198F WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 819AX 45927 OVERHEAD EMERGENCY LIGHT FOR FORWARD CREW DOOR WAS INOPERATIVE. REPLACED OVERHEAD EMERGENCY LIGHTS FOR FORWARD CABIN DOO R. OPS CHECKED GOOD IAW DC-8 MM. 2 L 7 4 4F 4A25 2003011600271 20030116 00271 NM 2003 1 16 AWXA200201206 1 20021120 A 5210 2024T3040 SKIN BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE L1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 MAJOR REPAIR, DURING C-14 CHECK A .500 INCH CRACK WAS FOUND ON AFT EDGE OF THE LEFT NR 1 DOOR INNER SKIN 12 INCHES ABOVE AFT LOWER LATCH ROLLER. NO NDT NEEDED, CRACK TERMINATES AT THE END OF SKIN. MAINTENANCE FABRICATED AND INSTALLED REPA IR DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2003011600272 20030116 00272 NM 2003 1 16 AWXA200201207 1 20021217 A 3397 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM GE CFM56 CFM56* 13802 NE CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 309AW 24711 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 20 LEFT, WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKE N WIRE ON THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 20 LEFT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2003011600274 20030116 00274 NM 2003 1 16 AWXA200201208 1 20021217 A 4930 APU AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE APU BAY MALFUNCTIONED A AWXA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE TX TAXI/GRND HDL 1 WP 28 805AW 1049 TAILPIPE FIRE, AFTER (APU) SHUT DOWN, A TAILPIPE FIRE WAS NOTICED BY GROUND CREW. MAINTENANCE INSPECTED THE APU AND FOU ND NO DAMAGE TO TAILPIPE OR SURROUNDING AREA. PLACED SYSTEM ON MEL, COND. 1. 2 L 7 2 4F 4 F RT A28NM E311NE 2003011600278 20030116 00278 WP 2003 1 16 ASAA0280613 1 20021126 A 5320 59360849 STRAP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND 30K CHECK, L-2 AFT GALLEY SERVICE DOOR SILL PLATE BACKING STRAPS ARE CORRODED. REMOVED CORROSION FROM 7 STR AP AND REPLACED 9 STRAP PER SRM 51-10-2, 51-10-4, 51-30-2 AND DAC DWG 5936084. (M) 2 L 7 2 4F RT A6WE 2003011600284 20030116 00284 WP 2003 1 16 ASAA0280614 1 20021126 A 5320 9936527 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND 30K CHECK, LONGERON 18R EXTERNAL ATTACH ANGLE IS CRACKED AT FS 788. REPLACED ATTACH ANGLE PER SRM 51-10-2, 51-30-2, 51-30-5, AND DAC DWG 9936527. (M) 2 L 7 2 4F RT A6WE 2003011600287 20030116 00287 WP 2003 1 16 ASAA0280615 1 20021126 A 5320 593666137 SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND 30K-CHECK, AFT CARGO BAY FORWARD BULKHEAD SUPPORT IS CRACKED AT FS 1007. REPLACED SUPPORT PER SRM 53-24-0, 51-10-2, 51-10-4 AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003011600288 20030116 00288 NM 2003 1 16 C7WA200200038 1 20021031 A 3231 652476431 BRACKET BOEING 727 727225 1384077 NM RT MLG DOOR MISINSTALLED A C7WA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 17 8887Z 21856 UPON GEAR RETRACTION, RED RIGHT GEAR LIGHT AND RED DOORS LIGHT REMAIN ILLUMINATED, AS WELL AS SECOND OFFICERS AMBER RIGH T GEAR DOOR LIGHT, CYCLED GEAR. UPON TROUBLESHOOTING FOUND INBOARD DOOR DRIVE ROD BRACKET INSTALLED BACKWARDS. REPOSIT IONED BRACKET AS PER MM 32-32-0. OPS CHECK NORMAL. (M) 2 L 7 3 4F A3WE 2003011600289 20030116 00289 NM 2003 1 16 C7WA200200039 1 20021031 A 3610 BACC10DU450 DUCT BOEING 727 727225 1384077 NM NR 3 STRUT LOOSE A C7WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 17 8887Z 21856 NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED ON TAKEOFF WHILE CLIMBING 200 FEET. EPRS 2.08/2.11. THROTTLES BACKED OFF TO 1.7 EPR LIGHT EXTINGUISHED. TROUBLESHOOTING FOUND DUCT CONNECTION TO NR 3 ENGINE PRECOOLER LOOSE. TIGHTENED, NO FUR THER LEAKS, MM 36-11-0. (M) 2 L 7 3 4F A3WE 2003011600290 20030116 00290 NM 2003 1 16 C7WA20020029 1 20021015 A 3411 PITOT TUBE BOEING 727 7272J7 138400E NM PITOT/STATIC SY OBSTRUCTED A C7WA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 17 128NA 20879 REJECTED TAKEOFF FROM SJC AT 90 KNOTS DUE TO LACK OF AIRSPEED INDICATION ON COPILOTS SIDE. CHECKED PITOT TUBES AND FOUN D INSPECT BLOCKAGE FROM FIRST OFFICERS PITOT TUBE. REMOVED BLOCKAGE CHECKED SYSTEM IAW MM 34-11-31. (M) 2 L 7 3 4F A3WE 2003011600291 20030116 00291 NM 2003 1 16 QXEA0202094 1 20021202 A 5320 WEB DHAV DHC8 DHC8202 2809007 NM FUSELAGE BUCKLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - AFT CARGO UNDER FLOOR, STATION X601-609, RT Y9.25 VERTICAL WEB IS BUCKLED ADJACENT TO FLOOR SUPPORT RAIL. REPAIRE D IAW RD8-53-55. 2 H 7 2 4T RT A13NM 2003011600292 20030116 00292 NM 2003 1 16 QXEA0202095 1 20021202 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - CARGO DOOR APERTURE UPPER FRAME IS CHAFED AT FORWARD AND AFT DOOR STOPS. REPAIRED IAW RD8-53-5461. 2 H 7 2 4T RT A13NM 2003011600293 20030116 00293 NM 2003 1 16 AWXA200300043 1 20021224 A 5330 148N3611 SKIN BOEING 757 7572G7 1384963 NM CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 0 0 24523 LCQ - MAJOR REPAIR - DURING C-10 CHECK FUSELAGE SKIN PANELS BELOW R/H HORIZONTAL STABILIZER BS 1862 WERE FOUND CHAFED FR OM STAB SLIDING SEAL. MAINTENANCE BLENDED CHAFED AREA AND FOUND MATERIAL LOSS OUT OF LIMITS PER B757-200 SRM 53-80-01, P G. 103; REMOVED 2 EACH CHAFED FUSELAGE SKIN PANELS AT BS 1862; FABRICATED 2 EACH NEW REPLACEMENT PANELS; INSTALLED NEW R EPAIR PARTS IAW AWA E.R. 19-5381-03002-ES1 2 L 7 2 4F RT A2NM 2003011700033 20030117 00033 NE 2003 1 17 ARWA20021202 2 20021205 A 7200 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 4 MALFUNCTIONED A ARWA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 19 8969U 54698 476 46070 671435 PRECAUTIONARY NR 4 ENGINE SHUTDOWN; OIL QUANTITY LOW. TIME: 0605Z, N1: 37 PERCENT. OIL PRESSURE 0-10 PSI. ACCOMPLISHE D INFLIGHT ENGINE SHUTDOWN CHECKLIST. REMOVED AND REPLACED NR 4 ENGINE IAW ARROW AIR TASK CARD DC8 UN-003 AND MASTER TA LLY UNDER W/O 6016275. ENGINE RUN-UP FOUND NORMAL IAW DC8 MM 71-00. 2 L 7 4 4F 4 F 4A25 1E8 2003011700036 20030117 00036 NM 2003 1 17 F3LA200200380 1 20021104 A 5321 FLOOR PANEL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 304FL 18962 3174 27633 DURING C 6 CHECK, CORROSION WAS FOUND IN THE AFT CARGO PIT FLOOR TRANSITION PANEL FROM STA 750 TO 754 AT RBL 20. REMOVE D PANEL AND FABRICATED NEW PART IN ACCORDANCE WITH BOEING DRAWING 69-43477. PAINTED AND INSTALLED IN ACCORDANCE WITH SO PM 20-4602. 2 L 7 2 4F RT A16WE 2003011700038 20030117 00038 NM 2003 1 17 F3LA200200381 1 20021106 A 5321 FLOOR PANEL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 304FL 18962 3174 27633 DURING C 6 CHECK, CORROSION WAS FOUND IN THE AFT CARGO PIT, RIGHT HAND, TRANSITION PANEL FROM STA 767 TO 727 AT RBL 21. INSPECTION FOUND THE PANEL TO BE OUT OF LIMITS IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 63-60-53. A NEW PANEL WAS FA BRICATED AND INSTALLED BETWEEN STA 727 AND STA 767 AT RBL 21 IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 57-40-02. 2 L 7 2 4F RT A16WE 2003011700039 20030117 00039 NM 2003 1 17 F3LA200200382 1 20021105 A 5321 FLOOR PANEL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 304FL 18962 3174 27633 DURING C 6 CHECK, THE AFT CARGO PIT FLOOR TRANSITION PANEL, LEFT HAND, WAS FOUND CORRODED BETWEEN STA 727 TO STA 787, LB L 28. REMOVED DAMAGED PANEL AND FABRICATED REPLACEMENT. REPLACEMENT WAS PRIMED, PAINTED AND INSTALLED IN ACCORDANCE WI TH THE REQUIREMENTS OF SRM 51-40-02, 53-60-53, 51-40-05 AND 51-21-02. 2 L 7 2 4F RT A16WE 2003011700040 20030117 00040 NM 2003 1 17 F3LA200200383 1 20021101 A 5320 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 304FL 18962 3174 27633 DURING C 6 CHECK, CORROSION WAS FOUND ON THE WEB BETWEEN STA 787 AND 794 AT STR 25R. THE WEB WAS REMOVED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-40-02. CORROSION WAS FOUND TO BE OUT OF LIMITS IN ACCORDANCE WITH THE REQUIREMENTS OF S RM 53-60-15, FIGURE 101, DETAIL V. A NEW PART WAS FABRICATED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-30-01. TRE ATED, PRIMED AND PAINTED IN ACCORDANCE WITH THE REQUIREMENTS OF SOPM 20-41-02. INSTALLED IN ACCORDANCE WITH THE REQUIRE MENTS OF SRM 51-40-02. 2 L 7 2 4F RT A16WE 2003011700041 20030117 00041 NE 2003 1 17 F3LA200200384 2 20021101 A 7261 STUD BOEING 737 7372P6 1C84609 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE LOOSE A F3LA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 03 1PC 26995 825 21613 DURING CLIMBOUT, THE FLIGHT CREW REPORTED THE NUMBER ONE ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND OIL QUANTITY WAS SHOWN AT ZERO. THE AIRCRAFT RETURNED TO ITS DEPARTURE AIRPORT. MAINTENANCE FOUND A LOOSE STUD ON THE MAIN OIL FILTER. THE STUD HOLE WAS HELI-COILED IN ACCORDANCE WITH BAC 5064. THE ENGINE WAS SERVICED IN ACCORDANCE WITH THE REQUIREMENTS OF MM 12-13-11. THE ENGINE WAS RUN AND LEAK CHECKED AND FOUND TO BE OPERATING CORRECTLY. 2 L 7 2 4F 4 F RT A16WE E2EA 2003011700042 20030117 00042 NM 2003 1 17 F3LA200200386 1 20021106 A 5320 SUPPORT ANGLE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 304FL 18961 3174 27633 DURING C 6 CHECK, THE AFT CARGO PIT BULKHEAD LOWER SUPPORT ANGLE WAS FOUND TO BE CORRODED FROM LBL 20 TO RBL 20 ON THE T OP AND BOTTOM SURFACES. MAINTENANCE REMOVED THE AFT CARGO PIT AFT BULKHEAD LOWER SUPPORT ANGLE AND CORROSION WAS FOUND TO BE WITHIN LIMITS, IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-10-2. THE AREA WAS TREATED AND PRIMED IN ACCORDANCE WITH THE REQUIREMENTS OF SOPM 20-41-02 AND INSTALLED IN ACCORDANCE WITH SRM 51-40-02. 2 L 7 2 4F RT A16WE 2003011700043 20030117 00043 NM 2003 1 17 F3LA200200387 1 20021106 A 5320 SILL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 304FL 18962 3174 27633 DURING C 6 CHECK, THE AFT CARGO COMPARTMENT LOWER DOOR SILL WAS FOUND CORRODED FROM STA 787 TO STA 800, RBL 20. MAINTEN ANCE REMOVED THE AFT CARGO COMPARTMENT LOWER DOOR SILL BETWEEN STA 787 AND STA 800 AT RBL 20. THE NEW PART WAS MATCH DR ILLED IN ACCORDANCE WITH SRM 51-40-06 AND INSTALLED IN ACCORDANCE WITH SRM 51-40-02. 2 L 7 2 4F RT A16WE 2003011700044 20030117 00044 NM 2003 1 17 F3LA200200388 1 20021106 A 5320 STRAP BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 304FL 18962 3174 27633 DURING C 6 CHECK, STRAP UNDER THE AFT CARGO PIT LOWER DOOR SILL WAS FOUND CORRODED AT STA 788 TO STA 791 AND RBL 18. MA INTENANCE REMOVED THE DAMAGED AFT CARGO COMPARTMENT DOOR SILL TAPERED STRAP BETWEEN STA 778 AND 799 AT RBL 18. A NEW PA RT WAS MATCH DRILLED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-40-06 AND INSTALLED IN ACCORDANCE WITH SRM 51-40-02. 2 L 7 2 4F RT A16WE 2003011700045 20030117 00045 WP 2003 1 17 AALA20021808 1 20021211 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 205AA 49155 TUL - FOUND SKIN CRACKED AT STATION 1380 ABOVE LONGERON 14L AT SHEAR TIE FASTENERS. INSTALLED DOUBLER, PER SRM 53-01-00 , PAGE 1 AARD 53-30-00-02 PAGE 1. (M) 2 L 7 2 4F A6WE 2003011700046 20030117 00046 WP 2003 1 17 AALA20021809 1 20021212 A 3350 P2070003001 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7514A 49891 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT L1 DOOR PORTABLE FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY EXIT PORT ABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700049 20030117 00049 NM 2003 1 17 AALA20021810 1 20021210 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN SHORTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 775AN 29584 AFW - POSSIBLY WHILE POTABLE WATER COMPRESSOR WAS BEING REPLACED THE WIRE WAS CRUSHED THEN AT SOME POINT SHORTED OUT ON A GROUND STRAP. SPLICED NEW WIRE IN. (M) 2 L 7 2 4F RT T00001SE 2003011700051 20030117 00051 NM 2003 1 17 AALA20021811 1 20021210 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 AFW - B/C AND COACH EPL AISLE LIGHTS FAILED TO ILLUMINATE FOR FULL 10 MINUTES PER PC0357. ALL OTHERS WORKED FINE. REPL ACED B/C AND COACH BATTERY PACKS. OPS CHECK OK. (M) 2 L 7 2 4F RT T00001SE 2003011700060 20030117 00060 NE 2003 1 17 AALA20021813 2 20021216 A 7230 SHAFT BOEING 777 777223 1385213 NM RROYCE RB211 RB211TRENT89 NE NR 1 ENGINE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 776AN 29582 51133 AFW - NR 1 ENGINE FAN RETENTION SHAFT HAS DAMAGE ALONG INNER BORE. CORED 90 PERCENT OF LENGTH, THROUGH THE SURFACE COAT ING INTO PARENT METAL. SCORE IS .200 WIDE AND MEASURES APPROX .010 DEEP. PER ROLLS ROYCE, TECHNICAL VARIANCE NR 211-43 261 IT IS ACCEPTABLE FOR ENGINE S/N 51133 TO CONTINUE IN SERVICE WITH THE DAMAGE DESCRIBED ABOVE PROVIDED THE PART IS RE MOVED PRIOR TO ACCUMULATING 1032 CYCLES FROM 10/21/2002, OR THE NEXT ENGINE REMOVAL, WHICHEVER IS SOONER. (M) 2 L 7 2 4F 4 F RT T00001SE E00050EN 2003011700061 20030117 00061 NM 2003 1 17 AALA20021814 1 20021206 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 378AN 25447 AFW - EPL WIRE BROKE AT CONNECTORS ON HARNESS COMING FROM SIDE WALL AT SEAT 29HJ. FOUND DURING MAINTENANCE. REPAIRED C ONNECTORS AT SEAT 29HJ FOR EP. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A1NM 2003011700062 20030117 00062 NM 2003 1 17 AALA20021815 1 20021206 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 378AN 25447 AFW - DURING MAINTENANCE, FOUND EPL LIGHT BULBS INOPERATIVE AT SEATS 27 HJ, 26HJ, 30AB, 37HJ AND 40 HJ. REMOVED AND REP LACED EPL LIGHT BULBS AT SEATS 27HJ, 26HJ, 30AB, 37HJ AND 40 HJ. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A1NM 2003011700063 20030117 00063 NM 2003 1 17 AALA20021816 1 20021206 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 AFW - EVAC SWITCH LIGHTS BURNED OUT. REMOVED AND REPLACED L1 ENTRY DOOR EVAC LIGHT ASSEMBLY, OPS CHECKS GOOD. (M) 2 L 7 2 4F RT T00001SE 2003011700065 20030117 00065 WP 2003 1 17 AALA20021817 1 20021218 A 2910 CONTROL VALVE DOUG DC9 DC982 3022082 WP HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 409AA 49320 ORD - FLT 1547 - VERY STRONG FUMES IN COCKPIT AND CABIN JUST AFTER TAKEOFF ORD. AIRCRAFT WAS SMOKEY WITH FUMES. CABIN FIRE/SMOKE CHECKLIST COMPLETED. FUMES PARTICULARLY STRONG IN FIRST CLASS CABIN. RETURNED TO ORD AND LANDED WITHOUT INC IDENT. REPAIRED HYDRAULIC LEAK TO LEFT AND RIGHT THRUST REVERSER CONTROL VALVE AND RUDDER SHUTOFF VALVE. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700067 20030117 00067 WP 2003 1 17 AALA20021818 1 20021216 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 413AA 49324 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ON SEATS 27 AND FORWARD EMERGENCY EXIT DOORS AT MID CABIN INOP ERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700068 20030117 00068 WP 2003 1 17 AALA20021819 1 20021215 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 462AA 49592 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ENTRY LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT ENTRY LIGHT. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700070 20030117 00070 WP 2003 1 17 AALA20021820 1 20021216 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 203AA 49145 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 19D INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT CONNE CTOR AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700071 20030117 00071 EU 2003 1 17 AALA20021821 1 20021216 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1426A 11411 ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEATS 4E-5E INOPERATIVE. RESECURED WIRE TO EMERGENCY EXIT L IGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2003011700072 20030117 00072 EU 2003 1 17 AALA20021822 1 20021217 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1444N 11447 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 11 INOPERATIVE. RESECURED CONNECTOR TO EMERGENCY E XIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2003011700073 20030117 00073 WP 2003 1 17 AALA20021823 1 20021217 A 2560 P2070003001 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 44503 49797 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PORTABLE FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY EXIT FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700076 20030117 00076 WP 2003 1 17 AALA20021824 1 20021216 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 233AA 49180 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AFT STAIR PASSAGE WAY FLOOR LIGHT BROKEN. REPLACED EMERGENCY EXIT AF T STAIR PASSAGE WAY FLOOR LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700079 20030117 00079 NM 2003 1 17 AALA20021825 1 20021216 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 676AN 29426 MIA - FOUND FLOOR EMERGENCY LIGHTS IN FIRST CLASS ARE INOPERATIVE. REPAIRED LOOSE CONNECTION NEAR SEAT 1E. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003011700080 20030117 00080 WP 2003 1 17 IXXA0200159O 1 20021203 A 5411 WING DOUG DC8 DC871 302199A WP #1 PYLON CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 829BX 85887 1589 45994 AFTER LANDING AT SEA THE FLIGHT CREW NOTICED A SLOW FUEL LEAK COMING FROM THE #1 PYLON INBOARD SIDE. MAINTENANCE INSPECT ED THE AIRCRAFT AND CATORGIZED IT AS A SLOW SEEP. REPAIR ACCOMPLISHED, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR I N ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND BOEINGS LETTER TIN-LIT-02-00024H. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2003011700081 20030117 00081 WP 2003 1 17 AALA20021826 1 20021216 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 TUL - FOUND CUSP CRACKED BETWEEN INSPECTION HOLES BEYOND DOUBLER RIGHT SIDE STATION 1298. INSTALLED DOUBLER PER ESO NR 80559 DATED 12/16-2002. (M) 2 L 7 2 4F RT A6WE 2003011700082 20030117 00082 WP 2003 1 17 AALA20021827 1 20021217 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76200 53290 TUL - FOUND SUB FLOOR BELOW NR 1 GALLEY DRAIN PAN RBL 49-51 CORRODED AT STAINLESS STEEL FITTING. INSTALLED DOUBLER ON S UB FLOOR BELOW NR 1 GALLEY DRAIN PAN RBL 49-RBL 51 PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2003011700083 20030117 00083 WP 2003 1 17 AALA20021828 1 20021217 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76200 53290 TUL - FOUND CORROSION ON NR 3 SEAT TRACK STATION 1280-1282. INSTALLED SEAT TRACK SPLICE PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003011700084 20030117 00084 WP 2003 1 17 AALA20021829 1 20021217 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76200 53290 TUL - FOUND CORROSION ON SEAT TRACK NR 3 STATION 1201-1205. REPLACED SEAT TRACK NR 3 FOR STATION 1186-1307 SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2003011700085 20030117 00085 WP 2003 1 17 AALA20021830 1 20021217 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76200 53290 TUL - FOUND AFT LOWER CORNER OF FORWARD GALLEY DOOR CUTOUT CUSP WEB CORRODED STATION 198-200. INSTALLED DOUBLER PER AAR D 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 2003011700086 20030117 00086 WP 2003 1 17 AALA20021831 1 20021217 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76200 53290 TUL - DEEP GOUGE IN LEFT FRAME STATION 807 BELOW SLAT DRIVE MECHANISM. CUT OUT DAMAGE INSTALLED DOUBLER REPAIR PER SRM 53-01-00 AND AARD 053-10-00-15. (M) 2 L 7 2 4F RT A6WE 2003011700112 20030117 00112 NM 2003 1 17 F3LA200200397 1 20021223 A 3221 65758279501 TRUNNION BOEING 737 7372Y5 1384554 NM NLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921WA 23039 DURING NOSE GEAR CHANGE, INSPECTED REPORTED LT NOSE GEAR TRUNNION BOSS CORRODED. REPLACED NOSE GEAR TRUNNION BOSS. 2 L 7 2 4U RT A16WE 2003011700115 20030117 00115 2003 1 17 F3LA200200399 4 20021231 A 3414 INDICATOR AIRBUS A319 A319111 3930336 NM COCKPIT MALFUNCTIONED A F3LA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 912FR 1803 ABORTED TAKEOFF. FLIGHT CREW REPORTED AIRSPEED INDICATIONS UNRELIABLE AT 90 KTS. PERFORMED TSM 22-66-00-810-872, LOSS OF SPEED LIMITS INDICATION ON BOTH PFD'S. NO FAULTS ON PFR. RAN CFD'S CHECK OF NR 1, 2 AND 3 ADR'S. NO FAULTS NOTED. INSPECTED FOR HOT BRAKES PER TASK 05-51-16-200-001. ALLOWED BRAKES TIME TO COOL. 2 L 7 2 4F RT A28NM 2003011700117 20030117 00117 EU 2003 1 17 NSVA200200004 1 20021130 A 7603 C822249 CONTROL CABLE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE POWER LEVER BROKEN A NSVA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 252 252 785332 IAD-ON TAKEOFF ROLL RIGHT ENGINE DROPPED OFF LINE TO GROUND IDLE, ABORTED TAKEOFF. POWER LEVER DID NOT RESPOND TO ANY I NPUTS. MAINTENANCE FOUND RT POWER LEVER CABLE HAD SEPARATED/BROKEN INTERNALLY (ON CONDITION). REMOVED AND REPLACED BRO KEN CABLE IAW SAAB 340 MM 76-10-46-4, PERFORMED ENGINE RUN OPERATIONAL CHECK IAW SAAB 340 MM 71-00-05, OP'S CHECK GOOD. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2003011700120 20030117 00120 EU 2003 1 17 NSVA200200005 1 20021122 A 3246 13889 BEARING SAAB SF340 340B 7860101 EU NLG FAILED A NSVA K NONE O OTHER NR NOT REPORTED 1 EA 27 299 299 AFTER LANDING/TAXI TO GATE IT WAS DISCOVERED THAT THE BEARING (MANUFACTURED BY TIMKEN) IN THE LEFT FRONT NOSE WHEEL ASSE MBLY (MANUFACTURED BY AIRCRAFT BRAKING SYSTEMS ABS) HAD FAILED. IT WAS SUSPECTED THAT BEARING ASSEMBLY WAS SUBJECTED TO CONTAMINATION FROM WATER CAUSING A BRAKE DOWN OF THE LUBRICATING PROPERTIES IN THE GREASE. DURING THE BEARING FAILURE THE NOSE WHEEL AXLE SUSTAINED SUBSEQUENT DAMAGED. MAINTENANCE REMOVED AND REPLACED NOSE WHEEL ASSEMBLIES AND AXLE. 2 L 7 2 4T RT A52EU 2003011700122 20030117 00122 EU 2003 1 17 NSVA200200006 1 20021126 A 3246 13889 BEARING SAAB SF340 340B 7860101 EU NLG WORN A NSVA K NONE O OTHER NR NOT REPORTED 1 EA 27 252 252 LEFT NOSE WHEEL BEARING LOOSE ON AXLE. WHEEL MOVED INWARD 1 INCH FROM HUB TOWARD NLG STRUT. REMOVED AND REPLACED NOSE WHEEL ASSEMBLY AND AXLE. 2 L 7 2 4T RT A52EU 2003011700129 20030117 00129 NM 2003 1 17 PCAA0211134 1 20021120 A 1420 SPLICE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 806EX 263 DURING ROUTINE MAINTENANCE VISIT TWO FORWARD EMERGENCY FLOOR PATH LIGHTS WERE FOUND INOPERATIVE. UPON INVESTIGATION TWO WIRE SPLICES WERE FOUND BROKEN AND ONE BULB FOUND INOPERATIVE. SPLICES WERE REPAIRED AND BULB REPLACED. OPERATIONAL C HECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003011700131 20030117 00131 NM 2003 1 17 PCAA0211137 1 20021125 A 3350 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST NR NOT REPORTED 1 EA 13 811AW 201 PHL- FLIGHT 3514 CREW REPORTED EMERGENCY LIGHTS WOULD NOT OPERATE FROM EITHER COCKPIT OR CABIN. ALL EMERGENCY LIGHT BAT TERIES, EMERGENCY LIGHT CONTROL BOX, AND FLIGHT ATTENDANTS LIGHT SWITCH WERE REPLACED. OPERATIONAL CHECK GOOD. AIRCRAF T RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003011700133 20030117 00133 NM 2003 1 17 PCAA0211138 1 20021127 A 3350 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 816EX 329 DURING ROUTINE MAINTENANCE VISIT FORWARD AISLE EMERGENCY LIGHT AND GALLEY OVERHEAD LIGHT WERE FOUND INOPERATIVE. EMERGE NCY LIGHT BATTERY REPLACED AT POSITION 200. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003011700136 20030117 00136 NM 2003 1 17 PCAA0211141 1 20021127 A 5710 STRUCTURE DHAV DHC8 DHC8102 2809003 NM RT WING BIRD STRIKE A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 846EX 326 MDT-FLIGHT 3800 CREW REPORTED LARGE BIRD STRIKE ON RIGHT WING. DAMAGE CURRENTLY BEING EVALUATED. MAINTENANCE REPAIRED RIGHT WING IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWINGS RD8-57-2481, RD8-57-2482, RD8-53-2483, RD8-57-2484. WORK ACCO MPLISHED BY BOMBARDIER UNDER WORK ORDER 812108-60064. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003011700137 20030117 00137 NM 2003 1 17 PCAA0212142 1 20021206 A 2120 ODOR DHAV DHC8 DHC8102 2809003 NM GALLEY DETECTED A PCAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 851EX 343 LGA-FLIGHT NR 3802. FLIGHT ATTENDANT DETECTED AN INTERMITTENT ODOR OF BURNING RUBBER COMING FROM THE OVERHEAD GALLEY VE NT. MAINTENANCE INSPECTED WIRING IN THE COAT CLOSET, HOT JUG AREA, AND OVERHEAD AREA OF THE GALLEY. NO DEFECTS WERE NO TED, COULD NOT DUPLICATE PROBLEM ON THE GROUND. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003011700138 20030117 00138 NM 2003 1 17 PCAA0212144 1 20021208 A 2120 ODOR DHAV DHC8 DHC8102 2809003 NM CABIN DETECTED A PCAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 980HA 376 ITH- FLIGHT 3729 FLIGHT ATTENDANT REPORTED THAT WITH THE BLEEDS ON A BURNING SMELL WAS PRESENT AND CABIN WAS VERY HOT WI TH TEMPERATURE GAUGE IN COCKPIT IN MIDDLE OF GREEN. MAINTENANCE INSPECTED ACM, PACK AND TRIM VALVES, INSPECTED BLEEDS F OR LEAKS, NONE NOTED. GROUND RAN WITH CREW WITH APU AND ENGINE BLEEDS ON. SYSTEM OPERATED NORMAL. SUSPECT CONDENSER M IXER FROZEN UP IN FLIGHT. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003011700141 20030117 00141 NM 2003 1 17 PCAA0212148 1 20021214 A 3350 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 812EX 312 DURING ROUTING MAINTENANCE VISIT SEVERAL EMERGENCY LIGHTS WERE FOUND TO GO OUT AFTER 10 MINUTES OF BEING ON. ALL SIX EM ERGENCY LIGHT BATTERIES WERE REPLACED IN CONJUNCTION WITH ALLEGHENY AIRLINES S-6 SERVICE CHECK. OPERATIONAL CHECK WAS G OOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003011700144 20030117 00144 WP 2003 1 17 AALA20021775 1 20021209 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 573AA 53092 DFW - DURING MAINTENANCE, OVERHEAD EMERGENCY EXIT COCKPIT LIGHTS INOPERATIVE. RESEATED FIRST CLASS OVERHEAD BATTERY. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700145 20030117 00145 WP 2003 1 17 AALA20021776 1 20021209 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33414 49325 DFW - DURING OVERNIGHT MAINTENANCE, BOTH FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED CONTACTS ON OVERWI NG BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700146 20030117 00146 WP 2003 1 17 AALA20021777 1 20021209 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7534A 49988 AUS - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTER Y. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700147 20030117 00147 WP 2003 1 17 AALA20021779 1 20021201 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP A/C BAY LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7543A 53025 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN TAIL CONE AREA INOPERATIVE. SECURED EMERGENCY EXIT BATTERY . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700148 20030117 00148 WP 2003 1 17 AALA20021780 1 20021201 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN UNSECURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7543A 53025 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN COCKPIT AND FORWARD GALLEY AREA INOPERATIVE. SECURED EMERG ENCY EXIT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700149 20030117 00149 WP 2003 1 17 AALA20021781 1 20021130 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN UNSECURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 586AA 53249 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SIGN BY SEAT 21A INOPERATIVE. SECURED EMERGENCY EXIT LIGHT SIG N BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700150 20030117 00150 WP 2003 1 17 AALA20021782 1 20021127 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP A/C BAY NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7528A 49920 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AFT STAIR AREA INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATT ERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700152 20030117 00152 WP 2003 1 17 AALA20021783 1 20021206 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DETACHED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 483A 49676 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. REATTACHED EMERGENCY EXIT LIGH T BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700153 20030117 00153 WP 2003 1 17 AALA20021784 1 20021206 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 435AA 49453 AUS - DURING OVERNIGHT MAINTENANCE, L1 DOOR PORTABLE FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY PORTABLE FLASHLIGHT AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2003011700154 20030117 00154 WP 2003 1 17 AALA20021785 1 20021206 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 440AA 49459 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHT AT ROW 29-30D INOPERATIVE. SECURED EMERGENCY EXIT CEIL ING LIGHT BATTERY CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700155 20030117 00155 WP 2003 1 17 AALA20021786 1 20021206 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 224AA 49174 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AT FORWARD MAIN ENTRY INOPERATIVE. REPLACED EMERGENCY EXIT AT FORWAR D MAIN ENTRY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700156 20030117 00156 EU 2003 1 17 AALA20021787 1 20021206 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1422J 11405 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AT FORWARD LAVATORY INOPERATIVE. REPLACED EMERGENCY EXIT LAVATORY LI GHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2003011700157 20030117 00157 WP 2003 1 17 AALA20021788 1 20021206 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 557AN 53087 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-690-691 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700158 20030117 00158 WP 2003 1 17 AALA20021789 1 20021208 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33414 49325 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AFT CABIN INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700159 20030117 00159 WP 2003 1 17 AALA20021790 1 20021208 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 221AA 49172 AUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ROWS 20 AND 27 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BAT TERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700163 20030117 00163 WP 2003 1 17 AALA20021791 1 20021208 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 221AA 49172 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AFT SECTION DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700164 20030117 00164 WP 2003 1 17 AALA20021795 1 20021204 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 241AA 49254 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT ROWS 27-29 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003011700167 20030117 00167 EA 2003 1 17 2003F00098 2 20020321 A 7320 FUEL CONTROL STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA LT ENGINE DIRTY A DATA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 GL 13 167RC SH3038 ON FLT 42310, ON THE DESCENT INTO CWA THE FIRST OFFICER PULLED THE POWER BACK AND THE LEFT ENGINE WOULD NOT GO BELOW 230 0 LBS OF TORQUE. THE CREW DECIDED TO PRECAUTIONARY SHUTDOWN THE ENGINE ON THE APPROACH INTO CWA. THE CWA ATC WAS NOTIF IED AND AN EMERGENCY WAS NOT DECLARED. THE EMERGENCY VEHICLES WERE DISPATCHED ANYWAY. THE AIRCRAFT WAS LANDED WITHOUT INCIDENT AND WAS TAXIED TO THE RAMP. THE MECHANICS WERE DISPATCHED FROM MKE TO CWA. THE LEFT ENGINE WAS INSPECTED AND FOUND THE CAMBOX TO BE DIRTY. THE CAMBOX WAS CLEANED AND LUBRICATED. OPS CHECK GOOD AND THE AIRCRAFT WAS RETURNED BACK TO SERVICE. (M) 2 H 7 2 4T 4 T A41EU E4EA 2003012000008 20030120 00008 NM 2003 1 20 0204246628 1 20021220 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 628US 22389 DURING "H" CHECK FOUND CORROSION ON AFT CARGO FLOOR BEAM UPPER CHORD AFT FLANGE AT BS 1920 RBL 33. REPAIRED PER EA 66-1 93799. 2 L 7 4 4F RT A20WE 2003012000009 20030120 00009 NM 2003 1 20 0204256628 1 20021212 A 5311 FRAME BOEING 747 747251B 1384892 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 628US 22389 During "H" check found cracks on frame at BS 480 S10A to S12AL. Repaired per EA 66-192945. 2 L 7 4 4F A20WE 2003012100071 20030121 00071 NM 2003 1 21 DL72S021476 1 20021226 A 3030 69158533 HEATER BOEING 727 727225A 1384077 NM F/O STATIC PORT INOPERATIVE A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 8891Z 21860 F/O STATIC PORT HEATER INOP, ATB RETURN TO CVG. REPLACED STATIC PORT HEATER. 2 L 7 3 4F RT A3WE 2003012100073 20030121 00073 NM 2003 1 21 ABXA030016 1 20021128 A 5320 141T833074 TEE FITTING BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 795AX 23145 FORWARD FUSELAGE CABIN RIGHT SIDE, WL 251.8, STA 287, FOUND CRACK ON TEE CONNECT TO FRAME. CRACKED TEE REMOVED AND INST ALLED NEW TEE. REF SRM 53-10-16, FIGURE 1 AND BAC DWG NR 141T8330/-6 INSTALLATION. 2 L 7 2 4F RT A1NM 2003012100086 20030121 00086 WP 2003 1 21 ABXA030037 1 20021227 A 5280 59203671 DOOR DOUG DC9 DC931 3022065 WP LT MLG CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 CRACK IN UPPER FORWARD CORNER OF INBOARD GEAR DOOR. REPLACED PAN IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-5 AND 51-30-8. 2 L 7 2 4F A6WE 2003012100114 20030121 00114 CE 2003 1 21 GLBA2002207 1 20021220 A 7333 12281301 METER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUEL FLOW FAULTY A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 219GL 6037 UE219 RIGHT FUEL FLOW INDICATOR INOP. REMOVED AND REPLACED FUEL FLOW METER, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2003012100116 20030121 00116 2003 1 21 GLBA2002208 4 20021223 A 3414 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 228GL UE228 ABORTED T/O, NO AIRSPEED IND CAPT'S SIDE. PERFORMED OPS AND LEAK CHECK, OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2003012100118 20030121 00118 CE 2003 1 21 GLBA2002209 1 20021226 A 7910 OIL SYSTEM BEECH 1900 1900D 1154162 CE NR 2 ENGINE LOW A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 219GL UE219 OIL PRESSURE ON NR 2 ENGINE FLUCTUATES 65 TO 90 ASI. SERVICED RT ENG, OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2003012100122 20030121 00122 SO 2003 1 21 GLBA2002210 1 20021227 A 3520 OXYGEN MASK EMB 120 EMB120ER 3260203 SO CABIN DEPLOYED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 108UX 120108 THE O2 MASKS FELL DOWN IN ROW 6. RESECURED O2 MASKS. 2 L 7 2 4T RT A31SO 2003012100124 20030121 00124 CE 2003 1 21 GLBA2002211 1 20021228 A 7720 3034857 THERMOCOUPLE BEECH 1900 1900D 1154162 CE LT ENGINE FAULTY A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 255GL UE255 LT ENGINE TEMP LIMITED. REMOVED AND REPLACED THERMOCOUPLE, OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2003012100132 20030121 00132 EU 2003 1 21 MALA020685 1 20021212 A 2421 31342003 GENERATOR SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 366XJ DURING FLIGHT 3155, RT AC GEN CAUTION LIGHT ON, QRH COMPLETED. AIR RETURN TO MSP. MAINTENANCE REPLACED RT AC GENERATOR IAW MM. ALL CHECKS GOOD OF AC GEN SYSTEM IAW MM. 2 L 7 2 4T RT A52EU 2003012100138 20030121 00138 WP 2003 1 21 AT0300001 1 20021228 A 3350 41B004AD0763 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 845AT 47238 OVERWING EMERGENCY EXIT DOOR LIGHTS WILL NOT ILLUMINATE (SEAT ROW 18A & F). REMOVED AND REPLACED BATTERY AND POWER SUPP LY. 2 L 7 2 4F A6WE 2003012100141 20030121 00141 WP 2003 1 21 IXXA02001158O 1 20021231 A 3260 CONNECTOR DOUG DC8 DC873F 302199F WP NLG LOOSE A IXXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 605AL 91511 429 46106 ON APPROACH TO SAN CREW NOTICED NOSE LANDING GEAR GREEN INDICATING LIGHTS NOT ILLUMINATED. CREW FOLLOWED COMPANY PROCED URE AND RETURNED TO SAN FOR AN UNEVENTFUL LANDING. INSPECTION REVEALED THE NOSE GEAR PROXIMITY SWITCH CONNECTOR HAD BEC OME INSECURE. MAINTENANCE SECURED THE CONNECTOR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. PERFORMED AN OPERA TIONAL CHECKOUT OF THE SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 4 4F RT 4A25 2003012100144 20030121 00144 WP 2003 1 21 IXXA0200141S 1 20021019 A 5744 SUPPORT DOUG DC8 DC871F 302199D WP RT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 2906 45811 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE INBOARD AND OUTBOARD LOWER AREA OF THE NR 2 FLAP HINGE UPPER SUPPORT ON THE RIGHT WING. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND BOEING'S LETTER TIN-MIA-02-00017H. 2 L 7 4 4F RT 4A25 2003012100145 20030121 00145 WP 2003 1 21 IXXA0200144S 1 20021014 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE LIGHTNING STRIKE A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 2906 45811 DURING ROUTINE C-CHECK INSPECTION EVIDENCE OF LIGHTNING STRIKES WERE DETECTED ON FUSELAGE STATION 180 LONGERONS 9R. REP AIR ACCOMPLISHED REMOVAL OF DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUC TURAL MANUAL AND DRAWING R-74-R01. 2 L 7 4 4F RT 4A25 2003012100147 20030121 00147 WP 2003 1 21 IXXA0200145S 1 20021014 A 5240 SKIN DOUG DC8 DC871F 302199D WP SERVICE DOOR DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 2906 45811 DURING A ROUTINE C-CHECK INSPECTION, A TEMPORARY REPAIR WAS DISCOVERED ON THE FORWARD SERVICE DOOR AT STATION 400. REPA IR ACCOMPLISHED REMOVAL OF TEMPORARY REPAIR AND DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANC E WITH DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2003012100148 20030121 00148 WP 2003 1 21 IXXA0200146S 1 20021014 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE LIGHTNING STRIKE A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 2906 45811 DURING ROUTINE C-CHECK INSPECTION, EVIDENCE OF LIGHTNING STRIKES WERE DETECTED ON FUSELAGE STATION 460, 480 & 520 LONGER ONS 7R-8R. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WI TH DOUGLAS STRUCTURAL MANUAL AND DRAWING R74-R01. 2 L 7 4 4F RT 4A25 2003012100150 20030121 00150 WP 2003 1 21 IXXA0200147S 1 20021014 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE LIGHTNING STRIKE A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 290 45811 DURING ROUTINE C-CHECK INSPECTION EVIDENCE OF LIGHTNING STRIKES WERE DETECTED ON FUSELAGE STATION 600 LONGERON 7R. REPA IR ACCOMPLISHED REMOVAL OF DAMAGED AREA FABRICATION AND INSTALLATION OF INTERNAL FINGER DOUBLERS IN ACCORDANCE WITH DOUG LAS STRUCTURAL MANUAL AND ENGINEERING ORDER R74-R01. 2 L 7 4 4F RT 4A25 2003012100151 20030121 00151 WP 2003 1 21 IXXA0200148S 1 20021014 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE LIGHTNING STRIKE A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 2906 45811 DURING A ROUTINE C-CHECK INSPECTION, EVIDENCE OF LIGHTNING STRIKES WERE DETECTED ON FUSELAGE STATION 120 LONGERON 9R. R EPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STR UCTURAL MANUAL AND DRAWING R74-R01. 2 L 7 4 4F RT 4A25 2003012100153 20030121 00153 WP 2003 1 21 IXXA0200149S 1 20021015 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE LIGHTNING STRIKE A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 2906 45811 DURING A ROUTINE C-CHECK INSPECTION, EVIDENCE OF LIGHTNING STRIKES WERE DETECTED ON FUSELAGE STATION 280 LONGERON 10R AN D FUSELAGE STATION 340 LONGERON 9R. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL MANUAL AND DRAWING R74-R01. 2 L 7 4 4F RT 4A25 2003012100155 20030121 00155 WP 2003 1 21 IXXA0200150S 1 20021016 A 5240 SKIN DOUG DC8 DC871F 302199D WP SERVICE DOOR CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 2906 45811 DURING A ROUTINE C-CHECK INSPECTION, A CRACK WAS DISCOVERED ON THE LOWER FORWARD CORNER OF THE AFT RIGHT SERVICE DOOR S TATION 1620. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION REPAIR OF DOUBLER AND TRIPLER I N ACCORDANCE WITH DOUGLAS STRUCTURAL MANUAL. 2 L 7 4 4F RT 4A25 2003012100156 20030121 00156 WP 2003 1 21 IXXA0200151S 1 20021016 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 2906 45811 DURING A ROUTINE C-CHECK INSPECTION, A TEMPORARY REPAIR WAS DISCOVERED OF THE RIGHT AFT CORNER OF THE CARGO DOOR. REPAI R ACCOMPLISHED REMOVAL OF TEMPORARY REPAIR AND DAMAGED AREA. FABRICATION AND INSTALLATION OF DOUBLER AND TRIPLER IN ACC ORDANCE WITH DOUGLAS STRUCTURAL MANUAL. 2 L 7 4 4F RT 4A25 2003012100159 20030121 00159 WP 2003 1 21 IXXA0200152S 1 20021022 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 2906 45811 DURING ROUTINE C-CHECK INSPECTION, A TEMPORARY REPAIR WAS DISCOVERED IN THE LOWER FORWARD L-2 DOOR JAMB STATION 1620. R EPAIR ACCOMPLISHED REMOVAL OF TEMPORARY REPAIR AND DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER AND TRIPL ER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2003012100161 20030121 00161 WP 2003 1 21 IXXA0200153S 1 20021022 A 5310 DOOR ACTUATOR DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 82897 2906 45811 DURING ROUTINE C-CHECK INSPECTION, A TEMPORARY REPAIR WAS DISCOVERED ON THE UPPER FORWARD L-1 DOOR JAMB STATION 25. REP AIR ACCOMPLISHED REMOVAL OF TEMPORARY REPAIR AND DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER AND TRIPLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2003022700076 20030227 00076 NM 2003 2 27 2003UALA00047 1 20020111 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 501UA 24622 STRINGER 16L BENT STATION 600. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE, INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2003012100166 20030121 00166 NE 2003 1 21 IXXA0200155O 2 20021220 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 1 MALFUNCTIONED A IXXA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 SW 11 606AL 88277 2595 46044 693534 AFTER TAKEOFF FROM MEM, THE FLIGHT CREW NOTICED NR 1 ENGINE INDICATIONS STARTED FLUCTUATING. AFTER ENGINE IDLE DOWN NO CHANGE IN ENGINE INDICATION, THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND SHUTDOWN THE NR 1 ENGINE. THE FLIGHT CONTI NUED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED VISUAL AND MAINTENANCE CHECKS I N ACCORDANCE WITH DOUGLAS MAINTENANCE MANUAL AND THE GENERAL ELECTRIC CFM56 MAINTENANCE MANUAL WITH NO FAULTS NOTED. TH E AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2003012100169 20030121 00169 WP 2003 1 21 IXXA0200157O 1 20021228 A 2710 57147155513 CYLINDER DOUG DC8 DC871F 302199D WP AILERON LEAKING A IXXA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 11 830BX 74206 966 45973 AFTER TAKEOFF FROM DEN, THE FLIGHT CREW NOTICED A DROP IN THE HYDRAULIC SYSTEM QUANTITY. THE FLIGHT CREW RETURNED TO DE N FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED A LEAK AROUND THE LEFT AILERON PACK. MA INTENANCE REPLACED THE LEFT HAND AILERON POWER CYLINDER PER THE AIRCRAFT MAINTENANCE MANUAL AND RETURNED AIRCRAFT TO SER VICE. 2 L 7 4 4F RT 4A25 2003012100178 20030121 00178 EU 2003 1 21 MALA020687 1 20021218 A 3620 CONTROL UNIT SAAB SF340 340B 7860101 EU BLEED AIR SYS FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 366PX 340B267 INFLIGHT 3054, HAD A LT BLD AIR LEAK LIGHT. PERFORMED QRH LIGHT WENT OUT. AIR RETURN TO DTW. MAINTENANCE REPLACED BL EED LEAK DETECTION CONTROL UNIT (3WU) IAW MM 36-23. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2003012100179 20030121 00179 EU 2003 1 21 MALA020688 1 20021219 A 2760 SPOILER BAC 146 AVRO146RJ85A 1500097 EU WINGS DEPLOYED A MALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 15 534XJ E2370 DURING FLIGHT 3657, AIR BRAKE DEPLOYED UNCOMMANDED. AIR RETURN TO MSP. MAINTENANCE PERFORMED ADJUSTMENT TEST PROCEDURE S IAW AMM 27-63-00 501. ALL OPS CHECK GOOD. CLEANED CL4 POTENTIOMETER CANNON PLUG. 2 H 7 4 4F RT A49EU 2003012100183 20030121 00183 EU 2003 1 21 MALA020690 1 20021223 A 7722 ECU SAAB SF340 340B 7860101 EU ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 418XJ 340B418 DURING FLIGHT 2981, CLIMBING THROUGH 16K LT ITT ANALOG AND DIGITAL BEGAN TO DECLINE, SETTLED AT 650 DEGREES WITH TORQUE OF 65 PERCENT RT GAUGE READ 845 WITH SAME TORQUE READING. ALL OTHER INDICATIONS NORMAL ON DESCENT AND LEVELING AT 7000. TEMP RETURNED TO NORMAL. AIR RETURN TO DTW. MAINTENANCE PERFORMED TROUBLESHOOTING PER GEMM 72-00-00 TROUBLE 11 FOR I NFLIGHT OP. PERFORMED TRIMMER AND YELLOW CABLE CHECK, PER TASK CARD 7420-301 AND ITT CAL CHECK PER TASK CARD 720001-1. REMOVED AND REPLACED DECU. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2003012100186 20030121 00186 EU 2003 1 21 MALA020691 1 20021226 A 2917 AIR916622 REGULATOR BAC 146 AVRO146RJ85A 1500097 EU HYD SYSTEM ACTIVATED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 512XJ E2326 DURING FLIGHT 3641, AIR LOW PRESSURE ON YELLOW HYDRAULIC SYSTEM ILLUMINATED. AIR RETURN TO MSP. MAINTENANCE REPLACED PSI REGULATOR VALVE. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2003012100208 20030121 00208 EU 2003 1 21 MALA030105 1 20020105 A 3230 UPLOCK SAAB SF340 SF340A 7850100 EU LANDING GEAR ICED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 112XJ AFTER TAKEOFF ON FLIGHT 2738, THE LANDING GEAR HANDLE LIGHT REMAINS ON RAN QRH, AND TALKED TO MAINTENANCE, LIGHT STILL R EMAINED ON. A/C DIVERTED TO BRD. MAINTENANCE REMOVED ICE BUILD-UP FROM NOSE GEAR UP-LOCK PAD AND LT & RT MLG UP-LOCK P ADS, PERFORMED GEAR SWINGS, OPS CHECK GOOD IAW MM 32-30-00. 2 L 7 2 4T RT A52EU 2003012100239 20030121 00239 EU 2003 1 21 MALA030110 1 20020114 A 3230 CONTROL VALVE SAAB SF340 340B 7860101 EU LANDING GEAR FAULTY A MALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 15 360PX 340B220 GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR UP SELECTION. HYDRAULIC PUMP CONTINUED TO RUN. COMPLETED QRH AND LIGHT WEN T OUT AND PUMP STOPPED. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL VALVE AS PER SF340 MM 32-31-15-4, ADJUSTE D MAIN LANDING GEAR UPLOCK SWITCH (LT) AS PER SAAB AMM 32-32-00-5, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2003012100250 20030121 00250 EU 2003 1 21 CA021230002 1 20021223 A 7933 INDICATOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE ENG OIL TEMP FALSE INDICATION W E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 CA 35903 (CAN) ON APPROACH THE LT ENGINE OIL TEMP WENT INTO THE RED ARC ON THE INDICATOR. ALL OTHER ENGINE PARAMETERS WERE NORMAL . THE ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE. THE CREW ELECTED TO PROCEED TO YYR AS THE RUNWAY CONDITIONS IN YA Y WERE NOT SUITABLE FOR A SINGLE ENGINE LANDING. THE AIRCRAFT LANDED IN YYR WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND OIL TEMP INDICATING SYSTEM AND DETERMINED THAT THE OIL TEMP INDICATOR WAS DEFECTIVE. THE INDICATOR WAS REPLAC ED. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2003012100251 20030121 00251 SW 2003 1 21 CA030103002 1 20021030 A 6310 269A9533001 CONTROL UNIT SCWZER 269A95323 HUGHES 269 269C1 8059504 SW LYC O360 HO360C1A 41514 EA MAIN ROTOR FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION HO HOVERING 1 CA (CAN) PILOT REPORTED DURING HOVER, THE TAXI LOW ROTOR WARNING ACTIVATED BUT ROTOR RPM WAS IN PROPER AREA OF GREEN ARC ON DUAL TACH. DURING SHUTDOWN, SWITCHING BELT DRIVE ENGAGEMENT SWITCH TO DISENGAGE MADE ENGINE QUIT. TROUBLESHOOTING REVE ALED CONTROL UNIT DISCONNECTION REQUIRED FOR ENGINE START AND OPERATION AND CONTROL UNIT HAD FAINT ELECTRONIC BURNED ODO R. SYSTEM DISABLED FOR AIRCRAFT RETURN TO SERVICE. 1 G 7 1 3O 3 O O 4H12 E286 2003012100254 20030121 00254 SW 2003 1 21 CA030108003 1 20021201 A 6510 407340340103 DISC PACK BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/R DRIVESHAFT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ONE TAIL ROTOR DISC CRACKED. TOTAL TEN DISC IN PACK. 1 G 7 1 3U 3 U O H2SW E1GL 2003012100255 20030121 00255 CE 2003 1 21 CA030110006 1 20021212 A 2435 3083949AT STARTER GEN LEAR 25 25B 5170511 CE GE CJ610 CJ6106 30006 NE LT ENGINE FAILED W O OTHER X M J ENGINE FLAMEOUT OVER TEMP WARNING INDICATION CR CRUISE 1 CA (CAN) DEPARTED AIRPORT AND LEVELED OFF AT FL410. VERY LIGHT TURBULENCE WAS ENCOUNTERED. APPROXIMATELY TWO MINUTES INTO CRUISE, THE RT ENGINE PRODUCED A LIGHT BANG & BEGAN TO SPOOL DOWN. THE RPM'S SETTLED A T 25-30 PERCENT. THE R/H THROTTL E WAS REDUCED TO IDLE THEN TO IDLE CUT-OFF. DURING THE DESCENT, AT FL380 THE LT ENGINE BEGUN TO VIBRATE, FOLLOWED BY AN ILLUMINATION OF THE LT GENERATOR WARNING LIGHT. AT THIS TIME AN EMERGENCY WAS DECLARED & A DESCENDING TURN WAS INITIATED . 2 L 7 2 4J 4 J A10CE 1E16 2003012100258 20030121 00258 NM 2003 1 21 PCAA0301002 1 20020101 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 834EX 285 DURING ROUTINE MAINTENANCE VISIT TWO EMERGENCY LIGHTS ON FLOOR FOUND TO BE INOPERATIVE. WIRING FOR FLOOR PROXIMITY LIGH T ASSEMBLIES WAS REPAIRED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003012100269 20030121 00269 NM 2003 1 21 AALA20021842 1 20021217 A 3350 CONNECTOR BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNT EMERGENCY EXIT LIGHT AT SEAT 23C INOPERATIVE. REPLACED EMERGENCY EXIT LI GHT MALE CONNECTOR AT ROW 23. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2003012100270 20030121 00270 NM 2003 1 21 AALA20021843 1 20021218 A 3350 MODULE BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 797AN 30012 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHTS IN COACH INOPERATIVE. REPLACED EMERGENCY EXIT LI GHT POWER PACK MODULE SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2003012100271 20030121 00271 NM 2003 1 21 AALA20021844 1 20021223 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 937AN 30082 MIA - DURING OVERNIGHT MAINTENANCE, L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2003012100272 20030121 00272 NM 2003 1 21 AALA20021845 1 20021222 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971AN 29547 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 21D AND 11D INOPERATIVE. REPLACED EMERGENCY EXIT LIGH T ASSEMBLY AT SEAT 21D AND 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2003012100274 20030121 00274 NM 2003 1 21 AALA20021846 1 20021222 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS FLOOR PROXIMITY EMERGENCY EXIT LIGHTS ON SEATS INOPERATIVE. REPLACED R1 DOOR EMERGENCY EXIT LIGHT CEILING PANEL ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2003012100275 20030121 00275 NM 2003 1 21 AALA20021847 1 20021222 A 3350 PIN BOEING 777 777223 1385213 NM CONNECTOR LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 755AN 30263 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT R1 DOOR CEILING PANEL ASSEMBLY CONNECTOR CONTACT PINS LOOSE. REPLACE D EMERGENCY EXIT R1 DOOR CEILING PANEL ASSEMBLY CONNECTOR CONTACT PINS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2003012100278 20030121 00278 NM 2003 1 21 AALA20021849 1 20021220 A 2720 33215209 PCU BOEING 757 757223 1384957 NM RUDDER FAULTY A AALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 21 623AA 24581 DFW - FLT 1507 - EN ROUTE DFW-YVR - AFTER TAKEOFF, AIRCRAFT BEGAN A SEVERE FISHTAILING MOTION FOR ABOUT 30 SECONDS. AIR CRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED ALL THREE RUDDER POWER CONTROL UNITS. SYSTEM GROUND AND FL IGHT CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003012100279 20030121 00279 WP 2003 1 21 AALA20021850 1 20021217 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76200 53290 TUL - FOUND CORROSION ON NR 1 SEAT TRACK, FS 1277-1281. INSTALLED NEW SEAT TRACK PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003012100283 20030121 00283 WP 2003 1 21 AALA20021851 1 20021217 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76200 53290 TUL - FOUND CORROSION ON SEAT TRACK NR 1. INSTALLED NEW SEAT TRACK PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003012100285 20030121 00285 WP 2003 1 21 AALA20021852 1 20021211 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 575AM 53152 TUL - FOUND TRACK CORRODED BEYOND LIMITS UNDER GALLEY ATTACH POINTS, FS 1174-1320. SEAT TRACK REPLACED PER AMM 53-40-00 -2. (M) 2 L 7 2 4F A6WE 2003012100286 20030121 00286 WP 2003 1 21 AALA20021853 1 20021217 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 490AA 49683 TUL - FOUND CRACK, FS 1380. STOP DRILLED WITH EXTERNAL DOUBLER PATCH PER SRM 51-01-00. (M) 2 L 7 2 4F A6WE 2003012100287 20030121 00287 WP 2003 1 21 AALA20021854 1 20021217 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 490AA 49683 TUL - FOUND CRACK, FS 1380. STOP DRILLED CRACK WITH EXTERNAL DOUBLER PATCH APPLIED PER SRM 51-01-00. (M) 2 L 7 2 4F A6WE 2003012100288 20030121 00288 WP 2003 1 21 AALA20021855 1 20021217 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 490AA 49683 TUL - FOUND CRACK FS 1437. REPLACED SHEAR TIE PER SRM 53-05-00. (M) 2 L 7 2 4F A6WE 2003012100289 20030121 00289 WP 2003 1 21 AALA20021856 1 20021217 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 575AM 53152 TUL - FOUND WINDOW ATTACH FRAME CRACKED AT RIVET LEFT SIDE STATION 1022 UPPER LEFT CORNER. INSTALLED REPAIR ANGLE PER A ARD 53-10-00-25. (M) 2 L 7 2 4F A6WE 2003012100290 20030121 00290 WP 2003 1 21 AALA20021857 1 20021217 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 575AM 53152 TUL - FOUND CRACK AT FASTENER HOLE STRINGER 14L STATION 1401 ABOVE NR 1 ENGINE PYLON. INSTALLED REPAIR DOUBLER PER SRM 53-01-00 APPROX 4 INCHES BY 5 INCHES EXTERNAL PATCH DOUBLER. (M) 2 L 7 2 4F A6WE 2003012100291 20030121 00291 WP 2003 1 21 AALA20021858 1 20021218 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 575AM 53152 TUL - TWO CRACK FOUND IN LEFT CUSP STATION 1261. STOP DRILLED CRACKS INSTALLED DOUBLER PER SRM 53-05-00. (M) 2 L 7 2 4F A6WE 2003012100292 20030121 00292 WP 2003 1 21 AALA20021859 1 20021209 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 575AM 53152 TUL - FOUND GOUGE IN AIRCRAFT SKIN, L10L AT CANT STATION 1510. INSTALLED DOUBLER PER SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2003012100293 20030121 00293 WP 2003 1 21 AALA20021860 1 20021218 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 575AM 53152 TUL - FOUND CORROSION ON RIGHT CUSP MEMBRANE BETWEEN STATION 655 TO 636 OUTBOARD OF NR 6 SEAT TRACK. REMOVED AND REPLAC ED CUSP MEMBRANE BETWEEN STATION 598 TO 712 PER DRAWING FDK5972. REINSTALLED SEAT TRACK NR 6 FROM STATION 560 TO 788. (M) 2 L 7 2 4F A6WE 2003012100294 20030121 00294 WP 2003 1 21 AALA20021861 1 20021209 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 575AM 53152 TUL - FOUND GOUGE IN SKIN L10L CANT 1497. INSTALLED DOUBLER PER SRM 53-10-00. (M) 2 L 7 2 4F A6WE 2003012100295 20030121 00295 WP 2003 1 21 AALA20021862 1 20021216 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 575AM 53152 TUL - FOUND CUSP CORRODED UNDER AFT GIRT BAR FITTING SUPPORT ANGLE AT AFT SERVICE DOOR. INSTALLED DOUBLER IN CUSP UNDER AFT GIRT BAR FITTING SUPPORT ANGLE PER SRM 53-00-00. (M) 2 L 7 2 4F A6WE 2003012100296 20030121 00296 WP 2003 1 21 AALA20021865 1 20021218 A 5240 DOOR DOUG DC9 DC982 3022082 WP LAV SERVICE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 575AM 53152 TUL - AFT LAV ACCESS DOOR FLANGE HAS CORROSION AT INBOARD SIDE OF FLANGE AT AFT LOWER CORNER, FS 1309-1322. REPAIRED PE R ESO 80559 DATED 12/5/02. (M) 2 L 7 2 4F A6WE 2003012100297 20030121 00297 WP 2003 1 21 AALA20021867 1 20021201 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 575AM 53152 TUL - FOUND CRACK IN CUSP STATION 598 RIGHT. INSTALLED DOUBLER PER AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 2003012100298 20030121 00298 WP 2003 1 21 AALA20021868 1 20021217 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 575AM 53152 TUL - FOUND CORROSION ON NR 6 SEAT TRACK AT FS 218. INSTALLED SEAT TRACK AND SPLICE REPAIR STATION 207-260 RIGHT, IAW S RM 53-05-00. (M) 2 L 7 2 4F A6WE 2003012100299 20030121 00299 WP 2003 1 21 ASA0280628 1 20021208 A 5320 991015176 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT CUSP WEB CORRODED AT FS 845-886. CUT OUT DAMAGED AREA. INSTALLED DOUBLER, AND SPLIC ED IN WEB REPAIR PER SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2003012100300 20030121 00300 WP 2003 1 21 AALA20021796 1 20021205 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN UNSECURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 429AA 49341 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT AFT STAIRWAY AND AFT LAVATORIES INOPERATIVE. SECURED EMERG ENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003012100301 20030121 00301 WP 2003 1 21 AALA20021802 1 20021214 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 278AA 49294 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON SEAT 9E INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 9E. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003012100303 20030121 00303 EU 2003 1 21 AALA20021803 1 20021213 A 2560 P2070003001 FLASHLIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1400H 11340 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PORTABLE FLASHLIGHT AT AFT GALLEY INOPERATIVE. REPLACED EMERGENCY EX IT PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2003012100304 20030121 00304 EU 2003 1 21 AALA20021804 1 20021213 A 2560 P2070003001 FLASHLIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1400H 11340 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FIRST CLASS PORTABLE FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY EXIT PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2003012100305 20030121 00305 WP 2003 1 21 AALA20021805 1 20021213 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 244AA 49256 RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING FOR OVERWING EXIT ABOVE HATCH IN CABIN INOPERATIVE. RESEATE D EMERGENCY EXIT LIGHT BATTERY, SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003012100306 20030121 00306 WP 2003 1 21 AALA20021832 1 20021217 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76200 53290 TUL - TWO CRACKS IN LEFT FORWARD EMERGENCY EXIT DOOR CUTOUT FRAME AT TOP. INSTALLED REPAIR PER SRM 53-05-00 FIG 32. (M ) 2 L 7 2 4F RT A6WE 2003012100307 20030121 00307 WP 2003 1 21 AALA20021833 1 20021217 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76200 53290 TUL - TWO CRACKS IN LEFT AFT EMERGENCY EXIT DOOR CUTOUT FRAME AT TOP, FS 916. INSTALLED REPAIR PER SRM 53-05-00 FIG 32. (M) 2 L 7 2 4F RT A6WE 2003012100308 20030121 00308 WP 2003 1 21 AALA20021834 1 20021217 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76200 53290 TUL - FOUND RIGHT AFT OVER WING EXIT JAMB CRACKED AT TOP CENTER, FS 916. STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBL ER PER 53-05-00 FIG 32. (M) 2 L 7 2 4F RT A6WE 2003012100309 20030121 00309 WP 2003 1 21 AALA20021835 1 20021217 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76200 53290 TUL - FOUND RIGHT FORWARD OVER WING EXIT JAMB CRACKED TOP CENTER. STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER PER SRM 53-05-00 FIG 32. (M) 2 L 7 2 4F RT A6WE 2003012100310 20030121 00310 WP 2003 1 21 AALA20021836 1 20021217 A 5342 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76200 53290 TUL - FOUND FUSE TO VERTICAL STABILIZER ATTACH ANGLE CRACKED IN RADIUS STATION 1463 RIGHT SIDE AND CRACKED IN LOWER LEG BETWEEN FASTENERS. STOP DRILLED CRACK IN RADIUS AND CUTOUT CRACKED AREA BETWEEN FASTENERS AND INSTALLED DOUBLER AND FIL LER PER AARD 53-10-00-2. (M) 2 L 7 2 4F RT A6WE 2003012100311 20030121 00311 WP 2003 1 21 AALA20021837 1 20021222 A 3350 60030451 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE O OTHER CR CRUISE 1 SW 21 437AA 49455 ORD - FLT 1592 - EN ROUTE SEA-ORD, AFT EMERGENCY EXIT FLOOR LIGHTS FLICKERED. LANDED ORD WITHOUT INCIDENT. REPLACED TW O EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2003012100312 20030121 00312 WP 2003 1 21 AALA20021838 1 20021220 A 3350 60030451 BATTERY DOUG DC9 DC983 3022083 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 597AA 53287 DFW - DURING OVERNIGHT MAINTENANCE, AFT TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATT ERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2003012100313 20030121 00313 WP 2003 1 21 AALA20021839 1 20021220 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 557AN 53087 DFW - DURING OVERNIGHT MAINTENANCE, AFT CEILING EMERGENCY EXIT LIGHTS AT AFT JUMP SEAT INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003012100314 20030121 00314 WP 2003 1 21 AALA20021840 1 20021218 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 562AA 49344 TUL - FOUND SKIN CRACKED AT STATION 1380, LONGERON 14L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01 FIG 2. (M) 2 L 7 2 4F RT A6WE 2003012100315 20030121 00315 NM 2003 1 21 AALA20021841 1 20021218 A 3350 SOCKET BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS DIM AT SEAT 31H THROUGH 33H. REPLACED EMERGENCY EXIT LIGHT SO CKET AT SEAT 31H THROUGH 33H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003012100316 20030121 00316 SO 2003 1 21 SIMA200231702 1 20021108 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON A PREVIOUS REPAIR TO THE LEFT OMEGA BEAM AT FRAME 20. REMOVED PREVI OUS REPAIR AND INSPECTED THE UNDERLYING BEAM. NO ADDITIONAL DAMAGE NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SH IMS AND PLATE. REPAIR DONE IAW EMB145 SRM (145/1142, CHAPTER 53, REV 19 53-21-10 PARA 2 FIG 201 SHEET 1, AND STANDARD S RM PRACTICES. (M) 2 L 7 2 4T RT T00011AT 2003012100318 20030121 00318 SO 2003 1 21 SIMA200231703 1 20021022 A 5320 145217725615 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - THIS IS A LEVEL 2 FINDING. GALLEY AREA LEFT SILL HAS CORROSION. REMOVED CORRODED SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003012100319 20030121 00319 SO 2003 1 21 SIMA200231704 1 20021022 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - THIS IS A LEVEL 2 FINDING. GALLEY AREA CENTER BEAM GUSSET HAS CORROSION. REMOVED BEAM AND INSTALLED SERVICEABLE BEAM IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003012100320 20030121 00320 SO 2003 1 21 SIMA200231705 1 20021002 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA FORWARD DIAMOND GUSSET HAS CORROSION. REMOVED CORRODED DIAMOND GUSSET AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003012200096 20030122 00096 NM 2003 1 22 ASAA0210324 1 20021124 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE ON ROWS 1-20. REMOVED AND REPLACED REMOTE ASS EMBLY RECEIVER AND BATTERIES AT ROWS 2 AND 3, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2003012200097 20030122 00097 NM 2003 1 22 ASAA0210369 1 20021206 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING LINE MAINTENANCE CHECK, FOUND THE BATTERY PACK AT ROW 16 NOT WORKING. REMOVED AND REPLACED REMOTE RECEIVER BATTERY. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A16WE 2003012200111 20030122 00111 NE 2003 1 22 DL72S021479 2 20021229 A 7200 JT8D15AHK ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 3 MALFUNCTIONED A DALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 27 544DA 57980 22493 700011 NR 3 ENGINE EGT LIMITED IN CLIMB POWER, EGT 590-595 AT 20 TAT CLIMB THRUST (ON T/O USING ALT 40 TAT CLIMB NR 3 EGT 610). AT 20 TAT CLIMB EPR = 1.88 HAD TO PULL NR 3 THROTTLE BACK TO 1.76 EPR TO KEEP EGT AT / BELOW 580. REPLACED NR 3 ENGIN E PER 4T203AD. 2 L 7 3 4F 4 F A3WE E2EA 2003012200123 20030122 00123 NM 2003 1 22 DL73K021467 1 20021224 A 2120 SMOKE BOEING 737 737232 1384475 NM CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 305DL 23077 SMOKE/ODOR OF UNKNOWN ORIGIN MID TO FWD CABIN TO COCKPIT, SIMILAR TO FIRECRACKER FUSE. AFTER DEPLANING, COULD NOT LOCAT E A SOURCE FOR THE ODOR OR SMOKE, SUSPECT A PIECE OF GROUND EQUIPMENT WAS THE SOURCE. A/C OK FOR SVC. 2 L 7 2 4F RT A16WE 2003012200124 20030122 00124 2003 1 22 DL73K021468 4 20021225 A 3442 20412170416 TRANSCEIVER BOEING 737 737247 138448D NM E/E BAY FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 373DL 23520 WX RADAR INOP. ANT FAULT MSG DISPLAYED. REPLACED RADAR TRANSCEIVER. RADAR TEST NORMAL. 2 L 7 2 4F A16WE 2003012200125 20030122 00125 NM 2003 1 22 DL73K021469 1 20021225 A 7920 PACKING BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE DAMAGED A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 307DL 42757 23079 709216 NR 2 ENG SHUTDOWN INFLIGHT. OIL QTY DROPPED TO 0, ENG S/D FOR APPROX 10 MIN IN FLIGHT WITH 5 PSI OIL PRESS T/A MDS. FO UND DAMAGED PACKING ON OIL PRESSURE SW. REPLACED SAME. CHECKED AND REPLACED OIL STRAINER. CHIP DET CHECKED GOOD. SER VICED ENG, RAN, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A16WE E2EA 2003012200128 20030122 00128 NM 2003 1 22 DL757021452 1 20021217 A 5420 FITTING BOEING 757 757232 1384965 NM NR 2 PYLON GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 WHILE WORKING PYLON MOD EO 6-70332-3AD, HOLE NR 65 IN RIGHT WING SIDE LOAD FITTING WAS GOUGED. REPAIRED PER ER/A 389430 -14AD. REPAIR OVERSIZED HOLE TO REMOVE DAMAGE AND INSTALLED OVERSIZED FASTENER. 2 L 7 2 4F RT A2NM 2003012200130 20030122 00130 NM 2003 1 22 DL757021454 1 20021217 A 5420 012N88883 SUPPORT FITTING BOEING 757 757232 1384965 NM NR 1 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 DURING COMPLETION OF PYLON MOD EO 6-70332-3AD, HOLE NR 2 IN LEFT WING SUPPORT FITTING HAD DAMAGE THAT REQUIRED REMOVAL P RIOR TO FASTENER INSTALLATION. REPAIRED PER ER/A 389426-14AD. REPAIR OVERSIZED HOLE, INSTALLED FREEZE PLUG, AND INSTAL LED EO FASTENER. 2 L 7 2 4F RT A2NM 2003012200132 20030122 00132 NM 2003 1 22 DL757021455 1 20021220 A 2121 731376 COOLING FAN BOEING 757 757232 1384965 NM E/E BAY FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 660DL 24422 DIVERTED TO MEM DUE TO STRONG ELECTRICAL SMELL IN COCKPIT. NO SMOKE WAS DETECTED. AN EMERGENCY WAS DECLARED. REPLACED NR 1 EQUIP COOLING SUPPLY FAN NR 1 PER AMM, TEST GOOD. 2 L 7 2 4F RT A2NM 2003012200133 20030122 00133 NM 2003 1 22 DL757021463 1 20021221 A 5330 143N33002 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 666DN 25034 THE FUSELAGE SKIN WAS FOUND WITH SEVERAL DENTS BETWEEN FS 620 & 640 AND BETWEEN STRINGERS 15L & 17L. THE CREASE BEAM AT STRINGER 16L WAS DENTED. THE SKIN DENTS WERE REMOVED WITH CUTOUTS AND A SECTION OF THE CREASE BEAM WAS CUTOUT TO REMOV E DAMAGE. THE BEAM WAS REPAIRED, REPAIR ANGLES AND THE SKIN WITH A SINGLE ALUMINUM REPAIR DOUBLER PER ER/A 384312-14, R EV C. 2 L 7 2 4F RT A2NM 2003012200134 20030122 00134 NM 2003 1 22 DL757021465 1 20021224 A 3320 BRACKET BOEING 757 757232 1384965 NM AFT GALLEY SEPARATED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 629DL 22919 F/A REPORTED SMOKE AND ELECTRICAL SMELL COMING FROM THE AFT GALLEY LIGHTS. PULLED AND SECURED ENTRY AND GALLEY C/B G4 O N P37. FOUND AFT GALLEY LIGHT ASSY RELAY BRACKET SEPARATED FROM PANEL, BRACKET CONTAINS K10292 AND D3478. RE-ATTACHED BRACKET AND REPLACED BALLAST. 2 L 7 2 4F RT A2NM 2003012200135 20030122 00135 NM 2003 1 22 DL757021470 1 20021225 A 2121 FAN BOEING 757 757232 1384965 NM CARGO BAY FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 611DL 22818 AT FL 390 FLT DK AND CABIN HAD AN ODOR OF BURNING ELECTRIC WIRE. TURNED OFF UTILITY BUSES AND L/R RECIRC FAN, ODOR SUBS IDED. EQUIPMENT OVHT LIGHT THEN CAME ON. FOUND LEFT RECIRC FAN BLADES CONTACTING HOUSING CAUSING VIBRATION AND BURNING SMELL. REPLACED FAN PER M/M. INSPECTED AREA, NO EVIDENCE OF FIRE OR SMOKE. 2 L 7 2 4F RT A2NM 2003012200136 20030122 00136 NM 2003 1 22 DL757021473 1 20021225 A 2121 6457053 FAN BOEING 757 757232 1384965 NM CARGO BAY FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 611DL 22818 AT CRUISE ALTITUDE EN ROUTE ANC CREW REPORTED SMOKE/ELECTRICAL ODOR IN COCKPIT AND CABIN. CREW PERFORMED EMERGENCY CHEC KLIST PROCEDURE AND ISOLATED LEFT AND RIGHT RECIRC FANS. CREW DECLARED AN EMERGENCY AND MADE UNSCHEDULED LANDING. MTC REPLACED LEFT RECIRC FAN AND EQUIPMENT COOLING LOGIC CARD. 2 L 7 2 4F RT A2NM 2003012200137 20030122 00137 NM 2003 1 22 DL757021478 1 20021227 A 3310 43410312001 SWITCH BOEING 757 757232 1384965 NM COCKPIT ARCED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 638DL 23761 BRAKE SOURCE LIGHT POPPED C/B. REPLACED BRAKE SOURCE SWITCH. NOW ALL OPS OK. 2 L 7 2 4F RT A2NM 2003012200138 20030122 00138 NM 2003 1 22 DL757021481 1 20021229 A 2497 WIRE BOEING 757 757232 1384965 NM COCKPIT CHAFED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 673DL 25978 AT 390 IN CRUISE WITH COCKPIT DOOR CLOSED SPARKS FLEW FROM C/B PANEL OVER CAPTS HEAD LOST NUMEROUS ITEMS IN COCKPIT INCL UDING LT AUTOPILOT, LT VHF RADIO, ELEV TRIM ON YOKE, STBY ADI TUMBLED, LT REV AMBER ON, BLEED ISOLATION VALVE, RUDDER RA TIO, LT YAW DAMP CAUTION MSG, FLAPS SLAT ELEC AND WARN ELECT STATUS MSG. FOUND WIRE FROM STANDBY POWER SUPPLY CIRCUIT H AD BEEN CHAFING ON GROUND STUD IN OVERHEAD P11 PANEL. REPAIRED WIRE AND OPS CHECKED SYSTEMS. 2 L 7 2 4F RT A2NM 2003012200139 20030122 00139 NM 2003 1 22 DL757030013 1 20021231 A 5320 143N852213 SILL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 THE INNER CHORD OF THE LOWER SILL OF THE C1 DOOR OPENING WAS FOUND WITH CORROSION AND TOOLING DAMAGE. THE INNER CHORD W AS REMOVED AND DISCARDED. A NEW CHORD WAS INSTALLED PER ER/A 384233-14. 2 L 7 2 4F RT A2NM 2003012200155 20030122 00155 NM 2003 1 22 DL764021170 1 20021005 A 2781 SENSOR BOEING 767 767432ER 1385134 NM L/E SLAT FAILED A DALA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 832MH 29704 AFTER CLEARING RUNWAY RAISED FLAP HANDLE TO UP POSITION AND GOT L/E SLAT ASSY MESSAGE ON EICAS. BITE PSEU FOUND LT NR 3 I/B SLAT SENSOR AT FAULT CODE 013. REMOVED ACCESS PANEL 521TB. REPLACED SENSOR 284 PER M/M. REPLACED SENSOR SWITCH, BOLT, WASHER AND NUT. CHECKED ADJUSTMENT BOTH POSITIONS, ALL NORMAL. CYCLED L/E SLATS, ALL IND NORMAL. BITE ON PSEU N ORMAL PER M/M 27-88-01-2. 2 L 7 2 4F RT A1NM 2003012200156 20030122 00156 NM 2003 1 22 DL764021197 1 20021015 A 3350 D71702001 POWER SUPPLY BOEING 767 767432ER 1385134 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 832MH 29704 INTERIOR EMERGENCY LIGHTS INOP FROM SEATS 17-24 RT SIDE. REPLACED POWER SUPPLY. OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2003012200157 20030122 00157 NM 2003 1 22 DL764021217 1 20021021 A 2530 72077500 OVEN BOEING 767 767432ER 1385134 NM AFT GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 837MH 29710 CIRCUIT BREAKER POPPED ON OVEN IN THE AFT GALLEY AFTER 30 MINUTES OF FLIGHT. THREE HOURS LATER THE SMOKE ALARM IN THE G ALLEY WENT OFF. NO SMOKE WAS OBSERVED OR SMELLED AND THE CB HAS NOT BEEN RESET. FWD OVEN 708 TO MCO AND PLACARD PER ME L 25-20-01I. C/B'S PULLED AND COLLARD. AFT SMOKE DETECTOR TEST NORMAL. 2 L 7 2 4F RT A1NM 2003012200158 20030122 00158 NM 2003 1 22 DL764021242 1 20021025 A 3040 MOTOR BOEING 767 767432ER 1385134 NM WINDSHIELD WIPER FAULTY A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 838MH 29711 AFTER GEAR RETRACTION DURING CLIMBOUT ABOUT 5000 FT CLICKING SOUND BEGAN ON FORWARD PANEL AREA BEHIND LANDING GEAR LEVER . PINNED LANDING GEAR, REMOVED LANDING GEAR PANEL AND FOUND NO FAULTS. FOUND THAT MOVING THE F/O'S WINDSHIELD WIPER OF F OF THE STOP DUPLICATED THE CLICKING SOUND. OPERATED WIPER AND IT PARKED NORMALLY. FWD TO MCO AND PLACARD AS PRECAUTI ONARY. FWD F/O WIPER TO MCO AND PLACARD PER MEL 30-42-01A. REMOVED AND REPLACED F/O WIPER MOTOR PER M/M. OPS NORMAL. MCO PLACARD REMOVED (LAX). 2 L 7 2 4F RT A1NM 2003012200159 20030122 00159 NM 2003 1 22 DL764021243 1 20021026 A 1430 114T41457 BOLT BOEING 767 767432ER 1385134 NM L/E SLAT SHEARED A DALA K NONE N FALSE WARNING LD LANDING 1 SO 27 832MH 29704 ON LANDING ROLL-OUT, L/E SLAT ASYM MSG ILLUMINATED ON EICAS. FOUND PROX TARGET BOLT BROKEN NR 9 SLAT O/B. REPLACED SAM E, CHECKS OK. 2 L 7 2 4F RT A1NM 2003012200161 20030122 00161 NM 2003 1 22 DL764021246 1 20021025 A 2611 PU90429WR1 SMOKE DETECTOR BOEING 767 767432ER 1385134 NM LAVATORY FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 828MH 29699 AFT LAV-E SMOKE DETECTOR FAILED OPS TEST. REPLACED SMOKE DETECTOR. OP CKS NORMAL. 2 L 7 2 4F RT A1NM 2003012200163 20030122 00163 NM 2003 1 22 DL764021298 1 20021106 A 2761 1542600 PACKING BOEING 767 767432ER 1385134 NM SPOILER ACTUATOR LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 832MH 29704 C-HYD QTY WARNING EICAS MSG. HYD PRESS LIGHT ON FLAP EXTENSION. FOUND ON LEAK CHECK. LT WING NR 3 SPOILER ACTUATOR DR AIN CAP PACKING LEAKING. REPLACED PACKING. OPERATED SPOILERS AND FLT CONTROLS, NO LEAKS. SERVICED HYD QTY. 2 L 7 2 4F RT A1NM 2003012200164 20030122 00164 NM 2003 1 22 DL764021312 1 20021111 A 2752 256T61102 ACTUATOR BOEING 767 767432ER 1385134 NM T/E FLAP TRIPPED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 828MH 29699 T/E FLAP DISAGREE DURING RETRACTION AFTER T/O FROM LAX. DUE TO FLAPS 20 QRH PROCEDURE REQD AND SHORT OGG RUNWAY DIVERTE D TO HNL. HNL MTC DISCOVERED NR 6 AND NR 7 T/E FLAP ROTARY ACT TRIP. NO HISTORY. RESET AND CHECKED OK PER FIM. 2 L 7 2 4F RT A1NM 2003012200165 20030122 00165 NM 2003 1 22 DL764021371 1 20021125 A 2450 BACC18Z5R CIRCUIT BREAKER BOEING 767 767432ER 1385134 NM COCKPIT OVERHEATED A DALA K NONE M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 27 830MH 29701 NO LAND 3 EICAS MSG APPEARED FOLLOWED BY NO LAND 3 STATUS MSG AND FLAP/SLAT ELEC STATUS MSG. ALSO OFF FLAG APPEARED IN CAPT'S STAB TRIM INDICATOR. FLAP/SLAT ELEC STATUS MSG DISAPPEARED ALONG WITH OFF FLAG IN STAB TRIM IND. NO LAND 3 MSGS REMAIN UNLESS AUTOPILOT IS DISCONNECTED AND RECONNECTED. THEN IT ALL HAPPENS AGAIN. FOUND P6 J-19 C/B 28VAC BUS L GLO WING RED AND SPARKING. REPLACED SAME, RAN MCDP TEST 40, ALL CHECKS NORMAL. OK FOR SERVICE REF WDM 24-53-11 PG 7. 2 L 7 2 4F RT A1NM 2003012200166 20030122 00166 NE 2003 1 22 DL764021396 2 20021201 A 7230 COMPRESSOR BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE NR 1 ENGINE DAMAGED A DALA O OTHER E VIBRATION/BUFFET DE DESCENT 1 SO 27 827MH 6218 29698 704952 INBOUND REPORT OF HI N2 VIBS AT TOD. 4.1 UNITS WHEN POWER REDUCED DURING FLIGHT LEVEL CHANGE. ATL MTC OBSERVED 2.0 UNIT S DURING PWR RUN. CHECKED MCD/S AND AVM FOR FAULTS / ALL OK. REPLACED ACCELEROMETER WITH SAME RESULTS ON ENGINE RUN. HPC BORESCOPE REVEALED 5TH AND 12TH STG HPC DAMAGE. ENGINE CHANGE IN WORK. 2 L 7 2 4F 4 F RT A1NM E13NE 2003012200167 20030122 00167 NM 2003 1 22 DL764021418 1 20021206 A 2421 GENERATOR BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE NR 1 ENGINE MALFUNCTIONED A DALA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 825MH 29696 704897 AT CRUISE L GEN CONT TRIPPED OCCURRED WHILE TRYING TO ELECTRICALLY OPEN EN CHANCED COCKPIT DOOR. STARTED APU THEN REFER RED TO QRH. RESET WAS SUCCESSFUL EXCEPT L BUS TIE REMAINED OPEN. GEN OPERATED NORMALLY FOR REMAINDER OF FLIGHT. ALL B ITE ON BPCU L AND R GCUS, NO FAULTS. RESET LT BUS TIE. ACCOMPLISHED ENGINE RUN. ELEC LOADS AND VALUES NORMAL. APPLIE D FULL ELEC LOAD. NO FURTHER TRIPS NOTED. 2 L 7 2 4F 4 F RT A1NM E13NE 2003012200169 20030122 00169 NM 2003 1 22 DL767021028 1 20020831 A 5311 148T25161 FRAME BOEING 767 767232 1385132 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 109DL 22221 THE FWD, OUTER CHORD OF THE FS 1809.5 WAS FOUND WITH A 5 INCH CRACK ALONG THE RADIUS NEAR STRINGER 7R. THE CRACK IS OUT SIDE THE AREA ADDRESSED BY BAC S/B 767-53-0078 AND AD 2001-09-13. THE CRACKED SECTION OF CHORD WAS CUTOUT AND REMOVED. A FILLER SECTION WAS INSTALLED, AND THE CHORD REPAIRED WITH 3 ALUMINUM REPAIR ANGLES PER ER/A 383735-14, REV A. 2 L 7 2 4F RT A1NM 2003012200170 20030122 00170 NM 2003 1 22 DL767021071 1 20020912 A 2560 61020 FLASHLIGHT BOEING 767 767232 1385132 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 105DA 22217 FOUND ON TRANSIT CHECK 2R DOOR FLT ATTENDANT EMERGENCY FLASHLIGHT INOP. REPLACED SAME. 2 L 7 2 4F RT A1NM 2003012200171 20030122 00171 NM 2003 1 22 DL767021090 1 20020916 A 3350 LIGHT BOEING 767 767232 1385132 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 101DA 22213 THE 1R EXTERIOR EMERGENCY LIGHT INOP. REPLAMPED SAME. 2 L 7 2 4F RT A1NM 2003012200172 20030122 00172 NM 2003 1 22 DL767021220 1 20021022 A 3397 0201875001 WIRE HARNESS BOEING 767 767232 1385132 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 101DA 22213 EMERGENCY PATH LIGHT AT SEAT 31AB INOP. REPLACED UNDERSEAT HARNESS. LIGHT OPERATES NORMALLY. 2 L 7 2 4F RT A1NM 2003012200174 20030122 00174 NM 2003 1 22 DL767021259 1 20021028 A 5270 851801 SENSOR BOEING 767 767232 1385132 NM EMERGENCY EXIT INTERMITTENT A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 106DA 22218 FT EMER DOOR LIGHT COMES ON INTERMITTENTLY IN FLIGHT. BITE CKD PSEU HAD PREVIOUS SENSORS 193 AND 192 TARGET FAULTS. NO PRESENT FAULTS. SENSOR 192 TARGET TEST OK. VISUALLY INSPECTED DOOR INTERIOR MECHANISM AND EXTERIOR PER M/M 52-21-02-2 , FOUND OK. 2 L 7 2 4F RT A1NM 2003012200175 20030122 00175 NM 2003 1 22 DL767021274 1 20021101 A 5753 113T23017 WEDGE BOEING 767 767232 1385132 NM T/E FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 110DL 22222 AFT FLAP T/E WEDGE BONDED ASSY WAS FOUND DELAMINATED BEYOND THE SCOPE OF A LOCALIZED REPAIR. REPAIR PER ER/A 417896-14. 2 L 7 2 4F RT A1NM 2003012200176 20030122 00176 NM 2003 1 22 DL767021295 1 20020510 A 7930 CONNECTOR BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE NR 2 ENGINE SHORTED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 101DA 50577 22213 580134 NR 2 ENG INFLT SHUTDOWN RT OIL FILTER LIGHT CAME ON. FOUND SHORT BETWEEN D4254P AND D4258J. REPLACED PLUG D4258J. SYS TEM CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2003012200178 20030122 00178 NM 2003 1 22 DL767021462 1 20021223 A 3610 COUPLING BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE BLEED AIR SYS LEAKING A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 103DA 43812 22215 580293 LEFT DUCT LEAK ON CLIMBOUT. RESEALED COUPLING ON BODY CROSSOVER DUCT IN LEFT AC BAY. RAN TO TAKEOFF POWER PER PFHB. O K FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 2003012200180 20030122 00180 NM 2003 1 22 DL767030058 1 20020113 A 5330 143T05007 SKIN BOEING 767 767232 1385132 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 102DA 22214 THE FUSELAGE SKIN WAS FOUND WITH A CRACK BETWEEN TWO STRINGER ATTACH FASTENERS AT FS 452 ALONG STRINGER 30R. THE UNDERL YING STRINGER WAS FOUND CORRODED. THE CORRODED AREA OF STRINGER WAS CUTOUT AND REPAIRED PER THE B767 SRM. THE SKIN CRA CK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER THE SRM. THE REPAIRS WERE DOCUMENTED PE R ER/A 384438-14. 2 L 7 2 4F RT A1NM 2003012200181 20030122 00181 NM 2003 1 22 DL76G021016 1 20020830 A 2530 COFFEEMAKER BOEING 767 767332 1382001 NM FWD GALLEY DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1609 30574 ELECTRICAL SMELL IN FWD GALLEY. COULD NOT LOCATE. OPERATED ALL FWD GALLEY AND IFE EQUIPMENT, NO ELECTRICAL ODOR NOTED. ALSO CHECKED ALL LIGHTING IN FWD CABIN. ALL CHECKED GOOD. FOUND EVIDENCE OF BURNED COFFEE. CLEANED SAME, OK FOR SER VICE. 2 L 7 2 4F RT A1NM 2003012200182 20030122 00182 NM 2003 1 22 DL76G021019 1 20020831 A 2781 849704 PSEU BOEING 767 767332 1382001 NM E/E BAY LOOSE A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 1612T 30575 DURING CLIMB AT FL140 AND 340 KNOTS THE FLAP IND MOVED TO 1/2 WITH ROLL MOTION L/E FLAP CAUTION LIGHT/EICAS MSG L/E FLAP ASYMMETRY MSG AS A/C SLOWED TO 250 KNOTS THE FLAP IN CYCLED UP AND BACK 1/2 4 TIMES/C PER FIM 27-81-00 FIG 107. FOUND FAULT AT PSEU 276 THEN PSEU BLANKED. FOUND PSEU LOOSE IN RACK. REMOVED AND REPLACED PSEU AND ALL OPS OK. 2 L 7 2 4F RT A1NM 2003012200183 20030122 00183 NM 2003 1 22 DL76G021085 1 20020915 A 3244 B767M TIRE BOEING 767 767332 1382001 NM NR 2 SEPARATED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 27 1605 30198 AT ROTATION NR 2 MAIN TIRE THREW RECAP. DAMAGE TO LT WING LOWER SURFACE PANEL, LT INBD FLAP, AND LT MAIN WHEEL WELL WIR E RACEWAY. REPAIRED DAMAGE. REPLACED WHEEL ASSY. 2 L 7 2 4F RT A1NM 2003012200184 20030122 00184 NM 2003 1 22 DL76G021099 1 20020615 A 3244 767300ERM TIRE BOEING 767 767332 1382001 NM NR 2 SEPARATED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 1605 30198 BLOWN TIRE ON T/O. RETURNED TO ATL, NO OVERWEIGHT LANDING. FOUND 2 MAIN TIRE MISSING RECAP, AIR STILL IN TIRE. REPLAC ED SAME. 2 L 7 2 4F RT A1NM 2003012200187 20030122 00187 NM 2003 1 22 DL76G021129 1 20020923 A 2750 285T004953 FSEU BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 1610D 30594 AFTER T/O LEADING EDGE SLAT ASSYM LIGHT ON. FLAP GAUGE WOULD NOT COME FULL UP. INDICATOR STUCK BETWEEN 1 AND UP. PERF ORMED BITE TEST OF FLAP/SLAT ELEC UNIT. REPLACED FSEU. 2 L 7 2 4F RT A1NM 2003012200188 20030122 00188 2003 1 22 DL76G021200 4 20021016 A 2230 COMPUTER BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1609 30574 AUTO THROTTLE FAILED TO ENGAGE. TMC AC CIRCUIT BREAKER POPPED. HINT OF ELECTRICAL SMOKE DISSIPATED QUICKLY. FWD TO MC O AND PLACARD PER MEL 22-30-01A. 2 L 7 2 4F RT A1NM 2003012200189 20030122 00189 NM 2003 1 22 DL76G021218 1 20021021 A 2622 892480 FIRE BOTTLE BOEING 767 767332 1382001 NM CABIN LEAKING A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 1613B 32776 FOUND WATER FIRE EXTINGUISHER IN FWD CABIN HAD LEAKED ALL OF THE WATER OUT. REPLACED BOTTLE. 2 L 7 2 4F RT A1NM 2003012200190 20030122 00190 NM 2003 1 22 DL76G021262 1 20021027 A 3350 767 LIGHT BOEING 767 7673P6 1385105 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 152DL 24984 DURING ETOPS L/O CHECK, FOUND EMERGENCY LIGHT AT DOOR 3R INOP. RELAMPED, OP CK GOOD. 2 L 7 2 4F RT A1NM 2003012200191 20030122 00191 2003 1 22 DL76G021300 4 20021107 A 2565 BPS73 POWER SUPPLY BOEING 767 7673P6 1385105 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 152DL 24984 ON L/O TEST, FOUND SQUIB TEST 1 AND 2 HAD ESCAPE SLIDE LIGHTS OUT FOR OVERWING SLIDES. REPLACED M962 POWER SUPPLY AND B ATTERY. 2 L 7 2 4F RT A1NM 2003012200192 20030122 00192 NM 2003 1 22 DL76G021305 1 20021109 A 2120 ODOR BOEING 767 767332 1382001 NM CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1611B 30595 DURING CRZ FL 330, FLT ATTENDANT REPORTED BURNED RUBBER SMELL IN AREA OF ROWS 33 THROUGH 35. AFTER ABOUT 10 MINS SMELL DISAPPEARED. NO VISIBLE SMOKE NOTICED. REMAINDER OF FLT NORMAL. INSPECTED AREA 33 THROUGH 35 & GALLEYS, CARGO COMPART MENTS OVERHEAD. FOUND NO DEFECTS. 2 L 7 2 4F RT A1NM 2003012200193 20030122 00193 NM 2003 1 22 DL76G021331 1 20021116 A 2421 IDG BOEING 767 767332 1382001 NM NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 1609 30574 XXX EN ROUTE TO STR RIGHT GENERATOR OFF LIGHT ILLUMINATED. BPCU BITE CHECK FAULTED, DP TRIP AND MAIN BUS/OVERLAP ZONE- ON R T GEN T/S FAULT MSG PER FIM FOUND IDG CT WIRING RESISTANCE O C-PHASE OUT OF TOLERANCE DURING STEP 2. REMOVED IDG RT GCU /BPC. REPLACED FOR T/S. INSTALLED ORIG RT GCU/BPCU PER AMM. INSTALLED IDG PER AMM. RQS R/U AND LEAK CHECK. R/U AND LEAK CHECK PERFORMED PER PFHB, NORMAL. DISC RESET. 2 L 7 2 4F RT A1NM 2003012200194 20030122 00194 NE 2003 1 22 DL76G021348 2 20021120 A 7260 TOWERSHAFT BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 2 ENGINE BROKEN A DALA E ENGINE SHUTDOWN Z SIGNIFICANT FAILURE REPORT CR CRUISE 1 SO 27 154DL 16621 25241 690372 AT CRUISE FL 350 RIGHT ENGINE EEC EICAS MSG AND AT SAME TIME ENG STARTED ROLLING BACK AND SHUTDOWN. FOUND GEARBOX TOWER SHAFT BROKEN. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 2003012200195 20030122 00195 2003 1 22 DL76G021353 4 20021121 A 2330 1303400100 ENTERTAIN SYS BOEING 767 7673P6 1385105 NM CABIN ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 1501P 24983 ELECTRICAL ODOR COMING FROM IFE CABINET. REPLACED PESC-V. SYS OPS CHECK OK. NO ODOR FOUND. 2 L 7 2 4F RT A1NM 2003012200197 20030122 00197 NM 2003 1 22 DL76G021420 1 20021207 A 2120 ODOR BOEING 767 767332 1382001 NM CABIN DETECTED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 1613B 32776 ON TAXI OUT FLIGHT ATTENDANT SMELLED A FAINT SMELL OF SMOKE IN THE FWD CABIN. A/C RTB AND TECH PERFORMED ENGINE RUN AND CHECKED PNEUMATIC SYSTEM. PERFORMED CHECK OF IFE ENTERTAINMENT SYSTEM. ALSO CHECKED MAIN E/E COMPARTMENT FOR FAULT BA LLSOR LRU FAULTS. NO DISCREPANCIES NOTED. COULD NOT DUPLICATE SMELL. ALSO CHECK FWD LAV UNDER SINK AND CABINET AREA, NO FAULTS NOTED. 2 L 7 2 4F RT A1NM 2003012200198 20030122 00198 NM 2003 1 22 DL76G021427 1 20021211 A 2121 6066223 FAN BOEING 767 767332 1382001 NM CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 16065 30199 DURING DESCENT BURNING SMELL AND VISIBLE SMOKE IN COCKPIT AND CABIN. LT RECIRC FAN INOP, LIGHT NOTED. LT RECIRC FAN TU RNED OFF CB PULLED. SMOKE DISSIPATED RAPIDLY. VERIFIED LT RECIRC FAN FAILURE AND SOURCE OF SMOKE. C/B'S OPENED AND CO LLARED. FWD LT RECIRC FAN TO MCO PLACARD PER MEL 21-25-01A. 2 L 7 2 4F RT A1NM 2003012200201 20030122 00201 NM 2003 1 22 DL76G021429 1 20021211 A 2421 729825B IDG BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING E H VIBRATION/BUFFET ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 27 1602 29694 704806 ON CLIMBOUT, RT GEN OFF LOST RT AC BUSS. BUSS RESET. RT GEN WOULD NOT RESET. FELT VIBRATION AT 310 KTS. FOUND -C- PH ASE OPEN ON IDG. REPLACED IDG. OPS CK OK ON RUN-UP. REF VIBRATION, VISUAL INSP OF EXTERIOR OF A/C NO DEFECTS NOTED. PERFORMED FLT CONTROL CHECK AND CHECK OF FLT CONTROLS OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2003012200205 20030122 00205 NM 2003 1 22 DL76G021432 1 20021211 A 2121 6066223 FAN BOEING 767 767332 1382001 NM CARGO BAY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 16065 30199 DURING DESCENT BURNING SMELL AND VISIBLE SMOKE IN COCKPIT AND CABIN. LT RECIRC FAN TURNED OFF CB PULLED. SMOKE DISSI PATED RAPIDLY. REPLACED LT RECIRC FAN PER MM. MCO CLEARED AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2003012200206 20030122 00206 NE 2003 1 22 DL76G021461 2 20021221 A 7200 BLADE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 2 ENGINE DAMAGED A DALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 27 153DL 39844 24985 695521 TWO AUDIBLE STALLS INTO ATL. DURING RT ENG BORESCOPE FOUND BLADE DAMAGE ON 12TH STAGE OF THE COMPRESSOR AND 1ST STAGE OF THE HPT. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 2003012200216 20030122 00216 NM 2003 1 22 DL76K021061 1 20020911 A 2781 SENSOR BOEING 767 767332 1382001 NM L/E SALT DIRTY A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 178DZ 30596 EICAS MSG AFTER T/O, LEADING EDGE FLAP ASYM. INSP FOUND NO DAMAGE FLAP L/E. RAN BITE ON PROX BOX FAIL 296 AND 278 SENS OR. INSP AND CLEANED SENSOR 296 AND 278. RAN FLAPS 2 TIMES, NO PROBLEM BITE PROX BOX CKS OK. 2 L 7 2 4F RT A1NM 2003012200222 20030122 00222 NE 2003 1 22 DL76K021114 2 20020921 A 7200 CF680C2B6F ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 SHUTDOWN A DALA A UNSCHED LANDING A Y FLAME/FIRE ENGINE STOPPAGE CL CLIMB 1 SO 27 171DZ 13606 13606 29690 704738 SHORTLY AFTER T/O CREW NOTICED A LOUD THUD AND LT ENG SHUT ITSELF DOWN. FLAMES WERE REPORTED COMING FROM ENG ON T/O BY GROUND PERSONNEL. A/C RTN ATL. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 2003012200224 20030122 00224 NM 2003 1 22 DL76K021166 1 20021004 A 2781 WARNING SYSTEM BOEING 767 767332 1382001 NM COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 178DZ 30596 L/E SLAT ASYM EICAS MSG WITH LEADING EDGE LIGHT AFTER TAKEOFF. A/C RETURNED TO GATE. RESET L/E SLATS, RAN FLAPS/SLATS WITH NO ABNORMALITIES, MESSAGES, OR FAULTS. NO SENSOR FAULTS ON PROX BOX. 2 L 7 2 4F RT A1NM 2003012200225 20030122 00225 NM 2003 1 22 DL76K021193 1 20021013 A 3350 BPS73 CHARGER BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 177DZ 29698 AFT EXT LT WING EMER LIGHTS INOP. REPLACED BATTERY CHARGER. 2 L 7 2 4F RT A1NM 2003012200226 20030122 00226 NM 2003 1 22 DL76K021232 1 20021025 A 2621 SEAL BOEING 767 767332 1382001 NM FIRE BOTTLE BROKEN A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 178DZ 30596 AFT CABIN H2O FIRE BOTTLE SEAL BROKEN. REPLACED AFT CABIN H2O FIRE BOTTLE. 2 L 7 2 4F RT A1NM 2003012200227 20030122 00227 NM 2003 1 22 ASAA0210381 1 20021209 A 3350 873203041 MODULE BOEING 737 7372X6C 1384552 NM CABIN FAULTY A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 747AS 23124 ANC - DURING TAXI, EMERGENCY FLOOR TRACK LIGHTING FLICKERED ON AND OFF AFTER LANDING. REMOVED AND REPLACED AFT CONTROL MODULE, THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2003012200228 20030122 00228 NM 2003 1 22 ASAA0210385 1 20021210 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING INSPECTION, FOUND EMERGENCY EXIT IDENTIFIER AT THE SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERY, THE EXIT IDENTIFIER TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2003012200229 20030122 00229 NM 2003 1 22 ASAA0210390 1 20021214 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 2313 SEA - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 12 WOULD NOT TEST. REMOVED AND REPLACED REMOTE ASSEM BLY RECEIVER, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2003012200232 20030122 00232 EU 2003 1 22 ASAA02400120 2 20020921 A 7200 ENGINE BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 MALFUNCTIONED A ASAA K NONE R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CL CLIMB 1 NM 01 796AS 28891 ANC - ON CLIMB-OUT THROUGH FLT LEVEL 200, NR 2 ENGINE HAD 2 COMPRESSOR STALLS AND SUBSEQUENT FLAME OUT. ENGINE SHUT DOW N AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE, OPERATIONAL CHECKED NORMAL, RELEASED. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 2003012200233 20030122 00233 EU 2003 1 22 ASAA0240120 2 20020921 A 7200 ENGINE BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 MALFUNCTIONED A ASAA K NONE R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CL CLIMB 1 NM 01 796AS 28891 ANC - ON CLIMB-OUT THROUGH FLT LEVEL 200, NR 2 ENGINE HAD 2 COMPRESSOR STALLS AND SUBSEQUENT FLAME OUT. ENGINE SHUT DOWN AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE, OPERATIONAL CHECKED NORMAL, RELEASED. REMOVED ENGINE IS BEI NG SENT TO GE STRUTHERS FOR EVALUATION. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 2003012200234 20030122 00234 NM 2003 1 22 ASAA0270014 1 20021007 A 3350 D71702001 POWER SUPPLY BOEING 737 737790 13844CN NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 615AS 30344 SEA - DURING MAINTENANCE CHECK, FOUND FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY. EMERG ENCY LIGHTS THEN FUNCTIONED PROPERLY. (M) 2 L 7 2 4F RT A16WE 2003012200235 20030122 00235 WP 2003 1 22 ASAA0280330 1 20020925 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN MISSING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SAN - DURING PREFLIGHT CHECK, FOUND ALL BUT ONE EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE THROUGHOUT 1 ST CLASS CABIN. R EPLACED MISSING LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003012200236 20030122 00236 WP 2003 1 22 ASAA0280331 1 20020925 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 53079 YVR - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 26. RECONNECTED LIGHT MODULE. LIG HTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003012200237 20030122 00237 WP 2003 1 22 ASAA0280349 1 20021003 A 5313 59360281 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - FOUND DURING C-CHECK, CORROSION ON LONGERON 30 AT FS 1022 IN AFT CARGO BAY. SPLICED IN NEW SECTION OF LONGERON 30 FROM FS 1003 TO 1070 PER EA 5310-0211. (M) 2 L 7 2 4F A6WE 2003012200238 20030122 00238 WP 2003 1 22 ASAA0280351 1 20021005 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP A/C BAY DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING LINE CHECK, FOUND TAIL CONE AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY (BATTERY PACK). LIGH TS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003012200239 20030122 00239 WP 2003 1 22 ASAA0280353 1 20021004 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 22800 6324 49387 PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY, INC LUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2003012200240 20030122 00240 WP 2003 1 22 ASAA0280361 1 20021009 A 5230 49286651 STOP FITTING DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY DOOR CRACKED ON AFT TOP SIDE. REPLACED DOOR STOP PER MM 52-31-01. (M) 2 L 7 2 4F RT A6WE 2003012200241 20030122 00241 WP 2003 1 22 ASAA0280364 1 20021014 A 5320 5936600171 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FLOOR SUPPORT AT FS 1150-1212 ABOVE STRINGER 29R CORRODED BEYOND LIMITS. RE PLACED FLOOR SUPPORT TEE PER SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003012200242 20030122 00242 WP 2003 1 22 ASAA0280366 1 20021012 A 5311 993607315 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, CORROSION AT FS 1212 LONGERON 29L-29R. REPLACED FRAME PER SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003012200243 20030122 00243 WP 2003 1 22 ASAA0280367 1 20021012 A 5320 593607022 BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY DOOR JAMB CORNER BRACKET CORRODED AT FS 1155 LONGERON 28R. REPLACED DOOR JA MB BRACKET PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003012200245 20030122 00245 2003 1 22 ASAA0280368 4 20021012 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 SEA - LANYARD BETWEEN GIRT BAR AND SLIDE COVER BECAME DISCONNECTED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2003012200246 20030122 00246 WP 2003 1 22 ASAA0280520 1 20021106 A 5320 5936071 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT ANGLE CORRODED AT FS 1214. REPLACED ANGLE PER SRM 51-10-4 AND MD DWG 593607 1-507. (M) 2 L 7 2 4F RT A6WE 2003012200247 20030122 00247 WP 2003 1 22 ASAA0280604 1 20021119 A 3350 0105606 MODULE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING LINE CHECK, WHITE EMERGENCY TRACK LIGHT WAS FOUND INOPERATIVE AT ROW 6. REPLACED LIGHT MODULE. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2003012200248 20030122 00248 WP 2003 1 22 ASAA0280607 1 20021123 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REPLACED LIGHT MODULE. LIGHT S THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003012200249 20030122 00249 WP 2003 1 22 ASAA0280608 1 20021123 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 PDX - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN 1ST CLASS. RECONNECTED LOOSE CONN ECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003012200250 20030122 00250 WP 2003 1 22 ASAA0280626 1 20021208 A 5320 993053866 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND 30K CHECK, RIGHT CUSP WEB CORRODED AT FS 218-256. CUT OUT DAMAGED AREA. INSTALLED DOUBLER, AND SPLICED IN WEB REPAIR AT FS 250-256 PER SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2003012200251 20030122 00251 WP 2003 1 22 ASAA0280627 1 20021208 A 5320 993053821 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT CUSP WEB CORRODED AT FS 370-389. CUT OUT DAMAGED AREA. INSTALLED DOUBLER, AND SPLI CED IN WEB REPAIR PER SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2003012200252 20030122 00252 WP 2003 1 22 ASAA0280630 1 20021209 A 5320 993053811 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB IS CORRODED AT FS 509. CUT OUT DAMAGED AREA. INSTALLED DOUBLER, AND SPLICE D IN WEB REPAIR PER SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2003012200254 20030122 00254 WP 2003 1 22 ASAA0280631 1 20021209 A 5320 993053877 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT CUSP WEB IS CORRODED AT FS 598-712. REMOVED AND REPLACED DAMAGED SECTION OF WEB PER SRM 51-30-5 AND -2. (M) 2 L 7 2 4F RT A6WE 2003012200257 20030122 00257 NM 2003 1 22 DL76K021456 1 20021221 A 2121 M732591EF COOLING FAN BOEING 767 767332 1382001 NM CARGO BAY FAILED A DALA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 175DZ 29696 AFTER PASSING THROUGH 10K FEET GOT MAIN GEAR DOORS LIGHT WITH LANDING GEAR MONITOR AND FORWARD EQUIPMENT EXHAUST FAN STA TUS MESSAGE. STRONG ELECTRICAL ODOR APPEARED IN COCKPIT SIMULTANEOUSLY. DOOR LIGHT EXTINGUISHED AFTER 2 OR 3 MINUTES. FOUND FWD EQUIP EXHAUST COOLING FAN C/B ON P6 PANEL POPPED, WON`T RESET. T/S PER FIM NO POWER TO EXHAUST FAN. REPLAC ED CARD M990 IN P5, NO HELP. FOUND NO POWER THROUGH RELAY K345. REPLACED SAME, NO HELP. FOUND FWD EQUIP COOLING FAN B AD. REPLACED SAME. 2 L 7 2 4F RT A1NM 2003012200259 20030122 00259 NM 2003 1 22 DL76L021023 1 20020901 A 7110 314T421059 COWLING BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 178DN 25143 724168 DURING CLIMB HAD L/E FLAP ASYMMETRY MSG WHEN FLAP SELECTED TO 1 UNIT POS. AT FL 5K ELECTED TO RETURN TO LAX. ON ARRIVA L FOUND THAT THE NR 1 ENG CORE COWLS HAD OPENED AND PEALED BACK. ALSO FOUND DAMAGE TO THE NR 5 SLAT. ADDITIONAL INFORM ATION LATER WHEN MORE IS AVAILABLE. REPLACED LT ENG EXHAUST NOZZLE, CORE COWL, BURNISHED LOWER WING SURFACE INBOARD NR 1 PYLON, REPAIRED WING CLOSURE PANEL. 2 L 7 2 4F 4 F RT A1NM E24NE 2003012200275 20030122 00275 NM 2003 1 22 AWXA200300056 1 20021222 A 5330 146N3531 SKIN BOEING 757 7572G7 1384963 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 0 0 24523 LCQ - MAJOR REPAIR - DURING C-10 CHECK INTERGRANULAR CORROSION WAS FOUND ON LOWER FUSELAGE SKIN UNDER AFT AIR PHONE ANTE NNA BASE, BS 1480. MAINTENANCE REMOVED AFT AIR PHONE ANTENNA AND BLENDED CORROSION AT BS 1480; MATERIAL LOSS OUT OF LIMI TS WITH MORE THAN 15 % OF ORIGINAL MATERIAL REMOVED; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-01, PG. 222-225. AIR PHONE REMOVED PER AWA E.R. 19-2310-01257-KB1. 2 L 7 2 4F RT A2NM 2003012200276 20030122 00276 NM 2003 1 22 AWXA200300058 1 20021223 A 5330 148N3611 SKIN BOEING 757 7572G7 1384963 NM CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 0 0 24523 LCQ - MAJOR REPAIR - DURING C-10 CHECK FUSELAGE SKIN PANELS BELOW L/H HORIZONTAL STABILIZER BS 1862 WERE FOUND CHAFED FR OM STAB SLIDING SEAL. MAINTENANCE BLENDED CHAFED AREA AND FOUND MATERIAL LOSS OUT OF LIMITS PER B757-200 SRM 53-80-01, P G. 103; REMOVED 2 EACH CHAFED FUSELAGE SKIN PANELS AT BS 1862; FABRICATED 2 EACH NEW REPLACEMENT PANELS; INSTALLED NEW R EPAIR PARTS IAW AWA E.R. 19-5381-03002-ES1 2 L 7 2 4F RT A2NM 2003012300002 20030123 00002 NE 2003 1 23 DL76K021444 2 20021214 A 7320 2718326 SHUTOFF VALVE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 ENGINE FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 171DZ 29690 704323 ON START ATTEMPT NR 1 ENGINE, NO LIGHT OFF. OBSERVED ENGINE VALVE LIGHT REMAINED ILLUM AFTER SELECTING FUEL CONTROL SWI TCH TO RUN. REPLACED FUEL SHUTOFF SOLENOID VALVE ASSY PER M/M. 2 L 7 2 4F 4 F RT A1NM E13NE 2003012300003 20030123 00003 NM 2003 1 23 DL76L021030 1 20020902 A 3350 WIRE HARNESS BOEING 767 767332 1382001 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 189DN 25990 FOUND EMERGENCY LIGHTS AT SEAT 6FG INOP. FOUND HARNESS BAD AND REPLACED SAME. OPS CHECKS OK. 2 L 7 2 4F RT A1NM 2003012300004 20030123 00004 NM 2003 1 23 2002UALA01846 1 20021211 A 2751 1812996 INDICATOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 WP 29 905UA 25005 AIRCRAFT FLEW A MISSED APPROACH WHEN FLAPS BECAME ASYMMETRIC. REPLACED FLAP INDICATOR. RELUBED ENTIRE FLAP SYSTEM AF TER FLAP LOCKOUT. 2 L 7 2 4F 4 F RT A16WE E2GL 2003012300005 20030123 00005 NM 2003 1 23 2002UALA01855 1 20021212 A 2841 INDICATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 307UA 23668 AIRCRAFT DIVERTED AFTER TAKEOFF. THE AIRCRAFT HAD AN APPARENT FUEL IMBALANCE. SUPPLEMENTAL DATA UPDATE FOUND ERROR CODE 6 ON NUMBER 1 FUEL QUANTITY INDICATION SYSTEM. PERFORMED TROUBLESHOOTING IAW MM. CLEARED ERROR CODE. PERFORMED DRIP S TICK CHECK OF THE NR 1 MAIN TANK IAW FUELING MANUAL. NR 1 FUEL QUANTITY INDICATION SYSTEM BITE CHECKED NORMAL AND AIRCR AFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2003012300006 20030123 00006 EU 2003 1 23 2002UALA01856 1 20021213 A 2841 SIC5059110207 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUEL SYSTEM MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 410UA 463 FLIGHT CREW SUSPECTED FUEL LEAK INFLIGHT. SUPPLEMENTAL DATA UPDATE INSPECTED AIRPLANE AND FOUND NO FUEL LEAK. TRANSFE RRED FUEL AND TAXI CHECKED AIRPLANE AND UNABLE TO FIND A FUEL LEAK. FUEL QUANTITY CHECKED AND FOUND WITHIN LIMITS BY CO MPARING INDICATION AND FUEL LEVEL MAGNETIC LEVEL INDICATORS. REPLACED FQIC TO CLEAR WRITE-UP THAT THE SYSTEM SHOWED DEG RADED. 2 L 7 2 4F 4 F RT A28NM E40NE 2003012300008 20030123 00008 EU 2003 1 23 2002UALA01902 1 20021226 A 3350 PSEU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 457UA 1146 'PSEU EXT LOAD EMER L' DISPLAYED DURING OPS TEST OF EMERGENCY ESCAPE LIGHTING FOR NR 3 SERVICE. REPLACED UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2003012300013 20030123 00013 NM 2003 1 23 2003UALA00029 1 20020106 A 5320 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 501UA 24622 STA 1690-1709, 3 LOCATIONS, RBL 51 AFT DECK PLATE CORRODED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2003032000078 20030320 00078 2003 3 20 2003UALA00044 4 20021217 A 2565 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEPLOYED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 179UA 25158 RIGHT UPPER DECK SLIDE DEPLOYED IN THE AIRCRAFT. BOTH SLIDE BOTTLES FIRED. NO DEFECTS FOUND ON SLIDE BOTTLE REGULATORS. SAFETY BURST DISK IN TACT. NO CORROSION, MATERIAL FLAW OR DAMAGE FOUND ON RUPTURE DISK. SLIDE DESTROYED AS A RESULT OF DEPLOYMENT IN CABIN. 2 L 7 4 4F 4 F RT A20WE E24NE 2003012300044 20030123 00044 NM 2003 1 23 DL76L021041 1 20020905 A 3397 0201875003 WIRE HARNESS BOEING 767 767332 1382001 NM CABIN FAULTY A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 190DN 28447 SEAT 34FG EMERGENCY PATHWAY LIGHT INOP. REPLACED SEAT GROUP QUICK SIDE CONNECT HARNESS. 2 L 7 2 4F RT A1NM 2003012300045 20030123 00045 NM 2003 1 23 DL76L021055 1 20020910 A 5754 114T410529A BEAM BOEING 767 767332 1382001 NM L/E SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 171DN 24759 NR 5 LEADING EDGE SLAT NOSE BEAM WAS FOUND DAMAGED. DAMAGE CONSISTED OF THE NOSE BEAM WEB BEING SEVERED ON OSS481. REP AIRED PER ER/A 417610-14. 2 L 7 2 4F RT A1NM 2003012300046 20030123 00046 NM 2003 1 23 DL76L021097 1 20020917 A 3240 705072 METERING VALVE BOEING 767 767332 1382001 NM LT MLG WW FAILED A DALA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 175DN 24803 AIRCRAFT RETURNED TO BLOCK DUE TO RIGHT HYDRAULIC SYSTEM PRESSURE LIGHT, QUANTITY LIGHT AND EICAS QUANTITY READING 0.03. IRREGULARITY OCCURRED ON RIGHT ENGINE START. FOUND LT WHEEL WELL BRAKE METERING VALVE FAILED. VALVE BODY END CAP SHE ARED AWAY FROM COMPONENT. THREE OF FOUR ATTACHING FASTENERS FAILED. REPLACED VALVE, LEAK CKS GOOD. 2 L 7 2 4F RT A1NM 2003012300047 20030123 00047 2003 1 23 DL76L021110 4 20020920 A 2330 1301581100 MONITOR BOEING 767 767332 1382001 NM CABIN MALFUNCTIONED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 192DN 28449 DURING PDC IFE CHECK WALL MOUNTED MONITOR IN FRONT OF SEATS 1A AND 1B EMITTING SMOKE. REPLACED WALL MOUNTED MONITOR IN FRONT OF SEAT 1A AND 1B. 2 L 7 2 4F RT A1NM 2003012300048 20030123 00048 NE 2003 1 23 DL76L021116 2 20020922 A 7230 COMPRESSOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE STALLED A DALA E ENGINE SHUTDOWN R Y PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CR CRUISE 1 SO 27 171DN 38459 24759 724682 RIGHT ENGINE COMPRESSOR STALL IN CRUISE AT FL350 WITH ENGINE ROLLBACK. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2003012300049 20030123 00049 2003 1 23 DL76L021127 4 20020920 A 2330 MONITOR BOEING 767 767332 1382001 NM CABIN MALFUNCTIONED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 196DN 28453 DURING PDC IFE CHECK WALL MOUNTED MONITOR IN FRONT OF SEATS 1A AND 1B EMITTING SMOKE. REPLACED WALL MOUNTED MONITOR AT SEAT 1A AND 1B, ADJUSTED SAME. OPS CHECK OK. 2 L 7 2 4F RT A1NM 2003012300050 20030123 00050 NM 2003 1 23 DL76L021135 1 20020925 A 3820 LINE BOEING 767 767332 1382001 NM LAVATORY LEAKING A DALA O OTHER K S FLUID LOSS AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 27 175DN 24803 F/C LAV LEAKED WATER INTO E/E COMPARTMENT CAUSING DAMAGE TO ELECTRICAL COMPONENTS. REPAIRED LEAK. 2 L 7 2 4F RT A1NM 2003012300051 20030123 00051 NE 2003 1 23 DL76L021149 2 20020928 A 7250 TURBINE BLADES BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 184DN 42462 27111 724655 FOUND 1 HPT FIRST STG BLADE WITH HOLE ON BORESCOPE. REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2003012300052 20030123 00052 NM 2003 1 23 DL76L021154 1 20020930 A 5300 STRUCTURE BOEING 767 767332 1382001 NM FUSELAGE VIBRATION A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 178DN 25143 FLIGHT ATTENDANTS NOTICED VIBRATIONS IN THE AREA OF THE MID GALLEY WITH MORE NOTICED ON THE RIGHT SIDE. CONFIRMED BY TH E RELIEF PILOT AND NOTICED THAT VIBS DECREASED WITH ACFT SLOWING DOWN BELOW 300 KTS. ON APPROACH THE VIBRATIONS INCREAS ED AND THEN WENT AWAY DURING LANDING ROLL OUT. THOROUGHLY INSPECTED AIRCRAFT WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A1NM 2003012300053 20030123 00053 NM 2003 1 23 DL76L021158 1 20020930 A 3397 0201875003 WIRE HARNESS BOEING 767 767332 1382001 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 194DN 28451 SEAT 35B EMERGENCY LIGHT FOUND INOP DURING MAINT INSPECTION. FOUND EMERGENCY LIGHT SEAT HARNESS WITH WIRE PULLED FROM C ONNECTOR. REPLACED HARNESS. 2 L 7 2 4F RT A1NM 2003012300058 20030123 00058 NE 2003 1 23 DL76L021160 2 20021001 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 BIRD INGESTION A DALA K NONE A FLAME/FIRE CL CLIMB 1 SO 27 177DN 35385 25122 723831 BIRD INGESTION OUT OF SCL ON TAKEOFF. ENGINE SURGED. ENGINE REPLACED IN ATL. 2 L 7 2 4F 4 F RT A1NM E24NE 2003012300059 20030123 00059 NM 2003 1 23 DL76L021161 1 20021003 A 3251 275T41123 MODULE BOEING 767 767332 1382001 NM NLG STEERING LEAKING A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 185DN 27961 REJECTED TAKEOFF DUE TO NO RUDDER PEDAL STEERING CONTROL. REPLACED STEERING CHECK VALVE MODULE PER MM, LEAK CKS OK. FO UND STEERING MODULE LEAKING INTERNALLY. REPLACED STEERING VALVE, CHECKED RUDDER PEDALS PER MM, ALL OK. CHECKED TILLER STEERING PER MM, OK. 2 L 7 2 4F RT A1NM 2003012300060 20030123 00060 NM 2003 1 23 DL76L021168 1 20021004 A 3250 CONTROL QUADRANT BOEING 767 767332 1382001 NM NLG LACK OF LUBE A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 185DN 27961 TILLER STEERING STIFF AND SLOW TO RESPOND ON TAXI. ON T/O ROLL WITH FULL RIGHT RUDDER, NO NOSE WHEEL RESPONSE. NO INITI AL RESPONSE ON RUDDER, FOLLOWED BY SUDDEN RAPID RESPONSE. FOUND UPPER LANDING GEAR QUADRANT DRY. LUBED SAME, TRIED A/C AROUND AIRPORT AND OPS CHECKED OK. 2 L 7 2 4F RT A1NM 2003012300061 20030123 00061 NM 2003 1 23 DL76L021189 1 20021012 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 197DN 28454 DURING ETOPS L/O CHECK, FOUND L391 EXTERIOR EMERGENCY EXIT LIGHT INOP. REPLACED M733 EMERGENCY EXIT LIGHT POWER SUPPLY. CHECKS GOOD. 2 L 7 2 4F RT A1NM 2003012300062 20030123 00062 NM 2003 1 23 DL76L021223 1 20021022 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 185DN 27961 DURING ETOPS L/O CHECK, FOUND LT WING SLIDE ILLUM LIGHT L396 INOP. REPLACED POWER SUPPLY M738. CHECKS GOOD. 2 L 7 2 4F RT A1NM 2003012300066 20030123 00066 NM 2003 1 23 DL76L021247 1 20021026 A 2530 CHILLER BOEING 767 767332 1382001 NM AFT GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CR CRUISE 1 SO 27 178DN 25143 AT CRUISE THERE WAS AN ELECTRICAL SMELL IN THE AFT GALLEY AND A HEAVY VIBRATION IN THE FLOOR AREA. WHEN THE CB FOR THE CHILLER THAT COOLS THE FOOD CARTS WAS PULLED THE VIBRATION STOPPED AND THE ELECTRICAL SMELL ABATED. AS PRECAUTIONARY AC TION DEACTIVATED BOTH CHILLERS AT AFT GALLEY. PULLED CB/S AND COLLARED. FWD TO MCO PER MEL 25-20-01C. 2 L 7 2 4F RT A1NM 2003012300067 20030123 00067 NM 2003 1 23 DL76L021257 1 20021028 A 3350 767 LIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 182DN 25987 ON ETOPS L/O CHECK, FOUND EXTERIOR EMERGENCY LIGHT BY 2L DOOR INOP. RELAMPED EXTERIOR LIGHT, OPERATION NOW NORMAL. 2 L 7 2 4F RT A1NM 2003012300068 20030123 00068 NM 2003 1 23 DL76L021261 1 20021029 A 5753 113T23017 WEDGE BOEING 767 767332 1382001 NM T/E FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 189DN 25990 DELAMINATION TO INBOARD AFT FLAP T/E WEDGE. REPAIR AUTHORIZED PER ER/A 417896-14. 2 L 7 2 4F RT A1NM 2003012300069 20030123 00069 NM 2003 1 23 DL76L021321 1 20021115 A 3412 102LA2AG PROBE BOEING 767 767332 1382001 NM TAT SYSTEM FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 173DN 24800 DIVERTED TO AMS FOR TAT PROBE REPLACEMENT DUE TO TAT PROBE MESSAGE AND AUTOTHROTTLES DISCONNECTED. THE REASON THE CREW GAVE WAS POSSIBLE ICING CONDITIONS IN FRA. REMOVED AND REPLACED TAT PROBE IAW MM 34-12-02-4, TESTED IAW 30-33, OK. 2 L 7 2 4F RT A1NM 2003012300070 20030123 00070 NE 2003 1 23 DL76L021339 2 20021118 A 7230 COMPRESSOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE STALLED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 194DN 46566 28451 724416 ON CLIMBOUT FROM ATL, NR 1 ENGINE COMPRESSOR STALLED AFTER FLYING THROUGH THE JETWASH OF A DEPARTING 737. F/A'S AND PAX REPORTED SEEING A FLASH OUTSIDE OF THE A/C ON THE LEFT SIDE. BROUGHT A/C BACK TO ATL AS A PRECAUTION. REPLACED NR 1 E NGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2003012300071 20030123 00071 NM 2003 1 23 DL76L021345 1 20021119 A 3350 BPS79 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 182DN 25987 DURING ETOPS L/O CHECK, L1 AND OVERWING EXTERIOR EMERGENCY LIGHTS FOUND INOP. REPLACED POWER SUPPLY M736. OPS NOW OK. 2 L 7 2 4F RT A1NM 2003012300072 20030123 00072 WP 2003 1 23 ASAA0280647 1 20021210 A 5321 99366403 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOORBOARD CORRODED AT 4 FASTENER HOLES AT FS 886-927. REPLACED FLOORBOARD PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003012300073 20030123 00073 WP 2003 1 23 ASAA0280648 1 20021210 A 5320 993653415 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FASTENER HOLES AT FS 200. REPLACED FLOOR SUPPORT PER SRM 53-14- 1, 51-10-2, 51-10-4, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003012300074 20030123 00074 WP 2003 1 23 ASAA0280649 1 20021210 A 5320 99578283 PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, TRANSITION PANEL IS CORRODED AT FS 148-169 AND 196-200. REPLACED SECTION OF TRANSITION PA NEL PER SRM 51-10-2, 51-10-4, 51-30-1 AND DAC DWG 9959828. (M) 2 L 7 2 4F RT A6WE 2003012300075 20030123 00075 WP 2003 1 23 ASAA0280651 1 20021210 A 5320 5930584163 CHANNEL DOUG DC9 DC983 3022083 WP FUSELAGE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FORWARD RIGHT MLG WHEELWELL DOOR FORMER HAS 3 WORN AREAS. REPLACED MLG DOOR CHANNEL AT FO RWARD EDGE OF DOOR CUTOUT PER SRM 51-3-2. (M) 2 L 7 2 4F RT A6WE 2003012400001 20030124 00001 NE 2003 1 24 DL76L021267 2 20021031 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 MALFUNCTIONED A DALA D RETURN TO BLOCK Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 SO 27 188DN 49568 27583 724169 AFTER STARTER CUT OUT, NR 2 ENGINE SPOOLED DOWN. CHECKED INLET AND TAILPIPE, FOUND OK. RAN ENGINE WITH AND WITHOUT PAC KS, ALL INDICATIONS NORMAL. FUEL FLOW AND FUEL PRESSURE NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2003012400002 20030124 00002 NE 2003 1 24 DL76L021364 2 20021123 A 7530 SOLENOID BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAILED A DALA K NONE R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 27 187DN 24904 27582 727679 LEFT ENGINE HAD SINGLE COMPRESSOR STALL ON LEVEL OFF AT FL 410. WORKED FINE BEFORE AND AFTER STALL. T/S PER FIM 71-05- 00 FIG 103, PER BLOCK 9 FOUND 2.9 BLEED SOLENOID BAD. REMOVED AND REPLACED 2.9 BLEED SOLENOID. BORESCOPE OF ENGINE FOU ND NO DEFECTS. RAN ENGINE PER PFHB TEST 4. ENGINE TEST GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2003012400003 20030124 00003 NE 2003 1 24 DL76L021377 2 20021125 A 7200 COMPRESSOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE STALLED A DALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 27 187DN 24910 27582 727679 ENGINE COMPRESSOR STALL IN CRUISE. REPLACING ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2003012400012 20030124 00012 EA 2003 1 24 SWIA200211720 1 20021212 A 5310 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 718 RIGHT SID CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 FS 718 RHS FRAME CRACKED BETWEEN STR 10-12. FOUND DURING C CHECK INSPECTION. DAMAGED AREA REPAIRED IAW CRJ REO 601R- 53-61-193 REV ''A'' . HFEC INSPECTION COMPLIED WITH ON FRAME CUTOUT REPAIR AND AREA AS REQUESTED IAW RJ NDTM 51-20-06. NO CRACKS FOUND. 2 L 7 2 4F RT A21EA 2003012400015 20030124 00015 WP 2003 1 24 ASA0280650 1 20021210 A 5321 99365853B FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOORBOARD IS DISBONDED AT ONE END AND CREASED/CRACKED ACROSS ENTIRE WIDTH OF BOARD AT FS 927-1003. REPLACED FLOORBOARD PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003012400016 20030124 00016 WP 2003 1 24 ASAA0280405 1 20021021 A 5320 99365345 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOOR MEMBRANE IS CORRODED AT FS 160-200, RBL 10.5-54. REPLACED MEMBRANE PER SRM 53-14-1, FIG 11, 51-10-4, FIG 2, AND 53-30-2. (M) 2 L 7 2 4F RT A6WE 2003012400017 20030124 00017 WP 2003 1 24 ASAA0280406 1 20021021 A 5320 99365345 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, MAIN CABIN FLOOR MEMBRANE (WEB) CORRODED AT FS 160-200, LBL6-RBL6. CUT OUT DAMAGED SECTIO N. SPLICED IN NEW SECTION PER SRM 53-14-1, FIG 11, 51-70-4, FIG 2, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003012400018 20030124 00018 WP 2003 1 24 ASAA0280407 1 20021021 A 5320 99365345 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, MAIN CABIN FLOOR MEMBRANE (WEB) CORRODED AT FS 200, LBL 10. CUT OUT DAMAGED SECTION. SPL ICED IN NEW SECTION PER SRM 53-14-1, FIG 11, 51-70-4, FIG 2, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003012400019 20030124 00019 WP 2003 1 24 ASAA0280409 1 20021021 A 5320 5836597509 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FLOOR SUPPORT CORRODED AT FS 1212 BETWEEN LONGERON 28L AND 29L. REPLACED SU PPORT PER SRM 53-24-0, FIG 11, AND SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003012400020 20030124 00020 WP 2003 1 24 ASAA0280413 1 20021021 A 5730 9936315501 DOUBLER DOUG DC9 DC983 3022083 WP LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, LEFT WING LEADING EDGE BUTT SPLICE DOUBLER IS CRACKED 1.25 INCH AT LOWER AFT EDGE. REPLAC ED SPLICE PER SRM 57-32-1, 51-10-4, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003012400021 20030124 00021 WP 2003 1 24 ASAA0280415 1 20021020 A 5311 9919604501 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FRAME CORRODED AT FS 1250, LONGERON 29L TO 28R. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS PER SRM 53-03, FIG 2A. (M) 2 L 7 2 4F RT A6WE 2003012400022 20030124 00022 WP 2003 1 24 ASAA0280417 1 20021020 A 5347 5936663 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY RIGHT TIE-DOWN TRACK CORRODED AT FS 1211-1338. REPLACED TIE-DOWN TRACK PER SRM 53-24-0, FIG 11, 51-10-2, 51-10-4, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003012400023 20030124 00023 WP 2003 1 24 ASAA0280418 1 20021020 A 5347 5936663 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, AFT CARGO BAY RIGHT TIE-DOWN TRACK CORRODED AT FS 1007-1155. REPLACED TIE-DOWN TRACK PER SRM 53-2 4-0, FIG 11, 51-10-2, 51-10-4, 51-10-2, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003012400024 20030124 00024 WP 2003 1 24 ASAA0280420 1 20021020 A 5347 5936663 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY LEFT TIE DOWN TRACK CORRODED UNDER CLIPNUTS AT FS 1007-1338. REPLACED TIE-D OWN TRACK PER SRM 53-24-0, FIG 11, 51-10-4, 51-10-2, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003012400025 20030124 00025 WP 2003 1 24 ASAA0280426 1 20021020 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 160-200, RBL 54. REPLACED SUPPORT PER SRM 53-14-1, FIG 11, A ND 52-30-5. (M) 2 L 7 2 4F RT A6WE 2003012400026 20030124 00026 WP 2003 1 24 ASAA0280629 1 20021209 A 5320 99305387 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB IS CORRODED AT FS 712-769. CUT OUT DAMAGED AREA. INSTALLED DOUBLER, AND SP LICED IN WEB REPAIR PER SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2003012400027 20030124 00027 WP 2003 1 24 ASAA0280632 1 20021209 A 5320 993053866 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB IS CORRODED AT FS 294-313. REMOVED DAMAGED AREA. INSTALLED DOUBLER PER SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2003012400028 20030124 00028 WP 2003 1 24 ASAA0280633 1 20021209 A 5320 9930538U9 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB IS CORRODED AT FS 598-693. REMOVED DAMAGED AREA. INSTALLED DOUBLER PER SRM 51-30-2 AND -5. (M) 2 L 7 2 4F RT A6WE 2003012400029 20030124 00029 WP 2003 1 24 ASAA0280634 1 20021209 A 5320 993053813 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB IS CORRODED AT FS 408-503. REPLACED DAMAGED WEB SECTION PER SRM 51-30-1 AND -5. (M) 2 L 7 2 4F RT A6WE 2003012400030 20030124 00030 WP 2003 1 24 ASAA0280635 1 20021209 A 5320 993053821 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT CUSP WEB IS CORRODED AT FS 408-503. REPLACED DAMAGED WEB SECTION PER SRM 51-30-1 AND -5. (M) 2 L 7 2 4F RT A6WE 2003012400031 20030124 00031 WP 2003 1 24 ASAA0280636 1 20021209 A 5320 993053812 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT CUSP WEB IS CORRODED AT FS 522-598. REPLACED DAMAGED WEB SECTION PER SRM 51-30-1 AN D -5. (M) 2 L 7 2 4F RT A6WE 2003012400032 20030124 00032 WP 2003 1 24 ASAA0280637 1 20021209 A 5321 99365853 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOORBOARD HAS TWO DENTS AT FS 927-1003. REPLACED FLOORBOARD SECTION PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003012400033 20030124 00033 WP 2003 1 24 ASAA0280638 1 20021209 A 5321 99365441 INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOORBOARD HAS CORRODED INSERTS AT FS 160-200 NEAR L1 ENTRY DOOR. REPLACED FLOORBOARD SEC TION PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003012400034 20030124 00034 WP 2003 1 24 ASAA0280639 1 20021209 A 5321 99365463 INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND 30K CHECK, FOUND FLOORBOARD NR 3 HAS 16 CORRODED INSERTS AT FS 160-200. REPLACED FLOORBOARD NR 3 PER SRM 53 -05. (M) 2 L 7 2 4F RT A6WE 2003012400035 20030124 00035 WP 2003 1 24 ASAA0280640 1 20021209 A 5321 99365495 INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOORBOARD NR 5 HAS 6 CORRODED INSERTS AT FS 160-200. REPLACED FLOORBOARD NR 5 PER SRM 53 -05. (M) 2 L 7 2 4F RT A6WE 2003012400036 20030124 00036 WP 2003 1 24 ASAA0280641 1 20021209 A 5321 993655113 INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND 30K CHECK, FLOORBOARD NR 8 HAS 8 CORRODED INSERTS AT FS 200-256. REPLACED FLOORBOARD NR 8 PER SRM 53-05. ( M) 2 L 7 2 4F RT A6WE 2003012400037 20030124 00037 WP 2003 1 24 ASAA0280642 1 20021209 A 5321 99365833 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOORBOARD HONEYCOMB DAMAGED AT FS 408-446. REPLACED FLOORBOARD PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003012400038 20030124 00038 WP 2003 1 24 ASAA0280643 1 20021209 A 5320 993653415 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 200. REPLACED FLOOR SUPPORT PER SRM 51-10-2, -4, AND 51-30-2 . (M) 2 L 7 2 4F RT A6WE 2003012400039 20030124 00039 WP 2003 1 24 ASAA0280644 1 20021209 A 5320 993053811 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB CORRODED AT FS 522-579. INSTALLED DOUBLERS AT FS 518-529 AND 566-574 PER SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2003012400040 20030124 00040 WP 2003 1 24 ASAA0280645 1 20021209 A 5320 993653425 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 200. REPLACED FLOOR SUPPORT PER SRM 53-14-1, 51-10-2, 51-10-4 , AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003012400041 20030124 00041 WP 2003 1 24 ASAA0280646 1 20021210 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FALSE TRACK CORRODED AT FS 149-200. REPLACED TRACK PER SRM 53-14-1, 51-10-2, 51-10-4, AND 51-30-1. (M) 2 L 7 2 4F RT A6WE 2003012400042 20030124 00042 SO 2003 1 24 SIMA200231706 1 20021022 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - THIS IS A LEVEL 2 FINDING. SERVICE DOOR FORWARD SILL CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL IAW E MB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003012400043 20030124 00043 SO 2003 1 24 SIMA200231707 1 20021022 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - THIS IS A LEVEL 2 FINDING. RIGHT FORWARD SILL HAS CORROSION. REMOVED CORRODED SILL AND INSTALLED SERVICEABLE SIL L IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003012400044 20030124 00044 SO 2003 1 24 SIMA200231708 1 20021022 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - THIS IS A LEVEL 2 FINDING. RIGHT AFT SILL HAS CORROSION. REMOVED CORRODED AFT SILL AND INSTALLED SERVICEABLE SIL L IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003012400045 20030124 00045 SO 2003 1 24 SIMA200231709 1 20021022 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA AFT DIAMOND GUSSET HAS CORROSION. REMOVED CORRODED GUSSET AND INSTALLED SE RVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003012400046 20030124 00046 SO 2003 1 24 SIMA200232302 1 20021112 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - DURING A IMBV INSPECTION, THE GALLEY AREA CENTER BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING BEAM AND INSTALLED NEW BEAM IAW EMB 145 SRM (EMB 145/1142 REV 19) CHAPTERS 51-40-02, 51-20-03 AND 51-40-06. (M) 2 L 7 2 4T RT T00011AT 2003012400047 20030124 00047 SO 2003 1 24 SIMA200232303 1 20021105 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - DURING AN IMBV INSPECTION, A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED BELOW SRM LIMIT S. REMOVED EXISTING REPAIR AND CLEANED AREA. FABRICATED A FILLER, TWO SHIMS, PLATE AND EXTERNAL ANGLE. REPAIR DONE IAW EMB145 SRM (EMB 145/1142 REV 19) CHAPTER 53-21-10 FIG 201. (M) 2 L 7 2 4T RT T00011AT 2003012400048 20030124 00048 SO 2003 1 24 SIMA200232304 1 20021115 A 2750 CONNECTOR EMB 135 EMB135KL 3260302 SO T/E FLAP LOOSE A SIMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 830AE 145615 ORD - FLT 4165 - DURING APPROACH, CREW REPORTED THE FLAPS FAILED/STOPPED AT 3 DEGREES. AN EMERGENCY DECLARED AND NO FLA P LANDING WAS SAFELY COMPLIED WITH. WHILE TROUBLESHOOTING FLAP SYSTEM MAINTENANCE FOUND THE CANNON PLUG ON THE NR 1 FLA P DRIVE LOOSE. CANNON PLUG WAS RECONNECTED AND FLAPS WERE CYCLED MULTIPLE TIMES. OPERATIONAL CHECK WAS GOOD AND AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2003012400049 20030124 00049 SO 2003 1 24 SIMA200232305 1 20021114 A 5610 163500110 WINDSHIELD EMB 135 EMB135LR 3260305 SO COCKPIT CRACKED A SIMA B EMER. DESCENT O OTHER CR CRUISE 1 SW 21 706RG 145194 LGA - FLT 4463 - DURING CRUISE, AT 27,000 FEET, THE FIRST OFFICERS WINDOW SHATTERED. AN EMERGENCY WAS DECLARED AND AIRC RAFT CONTINUED TO LGA AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW EMB MM. OP ERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2003012400050 20030124 00050 NM 2003 1 24 USAABB02209 1 20021225 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 651US 24764 PHL - FOUND THE AFT LEFT FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE M739 BATTERY CHARGER ASSEMBLY. O PS CHECK GOOD. (M) 2 L 7 2 4F RT A1NM 2003012400051 20030124 00051 EU 2003 1 24 USAASA02106 1 20021211 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 713UW 1040 PHL - DURING WEEKLY CHECK, THE EMERGENCY LIGHTS EMERGENCY POWER SUPPLY SYSTEM FAULTED. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2003012400052 20030124 00052 EU 2003 1 24 USAASA02113 1 20021219 A 3350 321430 BATTERY AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 752US 1319 LGA - FOUND THE RIGHT EPSU BATTERY DEAD. MAINTENANCE REPLACED THE RIGHT EPSU BATTERY. (M) 2 L 7 2 4F RT A28NM 2003012400053 20030124 00053 EU 2003 1 24 USAASA02116 1 20021227 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 748UW 7222 1311 TPA - THE CABIN INTERCOMMUNICATIONS DATA SYSTEM EMERGENCY LIGHT TEST GAVE "EPSU R FAULT" MESSAGE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT, FIN 12WL. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2003012400054 20030124 00054 NM 2003 1 24 USAASB02193 1 20021025 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 514AU 23700 PIT - MAINTENANCE FOUND THE EMERGENCY LIGHT OVER THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003012400055 20030124 00055 NM 2003 1 24 USAASB02194 1 20021027 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 776AU 24934 EWR - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT THE LAST ROW OF CABIN SEATS INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE BATTERY CHARGER ASSEMBLY DUE TO BLOWN FUSES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003012400056 20030124 00056 NM 2003 1 24 USAASB02195 1 20021028 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 506AU 23381 IND - MAINTENANCE FOUND THE EMERGENCY LIGHTS FROM SEAT ROWS 17 LEFT THROUGH 22 LEFT INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE BATTERY PACK AND RELAMPED THE LIGHTS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003012400057 20030124 00057 NM 2003 1 24 USAASB02196 1 20021028 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 528AU 24410 PIT - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY L IGHT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003012400058 20030124 00058 NM 2003 1 24 GAIA02034OP 1 20020416 A 3610 CLAMP BOEING 727 727251 138408H NM NR 3 PYLON LOOSE A GAIA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 278US 21157 FLT 879 - FWA-SJC - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, THE LIGHT EXTIN GUISHED AND REMAINED EXTINGUISHED. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT SJC WAS UNEVENTFUL. FOUND SEVE RAL LOOSE CLAMPS AND A LOOSE CANNON PLUG BACKSHELL. RETIGHTENED CLAMPS AND RESECURED THE CANNON PLUG BACKSHELL. PERFOR MED AN OPERATIONAL CHECK AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2003012400059 20030124 00059 NM 2003 1 24 GAIA02035OP 1 20020417 A 3610 CLAMP BOEING 727 727251 138408H NM NR 3 PYLON LOOSE A GAIA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 278US 21157 FLT 864 - FWA-EWR - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, THE LIGHT EXTIN GUISHED AND REMAINED EXTINGUISHED. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT EWR WAS UNEVENTFUL. FOUND AIR LEAK AT THE NR 3 BLEED SHUTOFF VALVE IN THE STUB WING. REPOSITIONED DUCTS AND RETORQUED CLAMPS. PERFORMED AN OPERATION AL CHECK AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2003012400060 20030124 00060 NM 2003 1 24 GAIA02036OP 1 20020418 A 3610 CLAMP BOEING 727 727251 138408H NM NR 3 PYLON OUT OF POSITION A GAIA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 278US 21157 FLIGHT 863 - EWR-FWA - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, AND OPERATED AT REDUCED THRUST. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT FWA WAS UNEVENTFUL. REPOSITIONED CLAMP ON HIG H PRESSURE BLEED DUCT FROM NR 3 BLEED SHUTOFF VALVE. OPERATED NR 3 ENGINE AT 78 PERCENT N2 FOR PLUS MINUTES. NO OVERHE AT INDICATION WAS NOTED AND WAS FOUND TO BE OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2003012400061 20030124 00061 NM 2003 1 24 HALA0200673 1 20021112 A 2742 TRIM MOTOR BOEING 717 717200 1383700 NM HORIZ STAB FAILED A HALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 13 479HA 55124 FLT 240 - HNL - PRIMARY TRIM FAILURE, NO ALERT. ON CLIMB-OUT AND RETURN TO HNL, TRIM STARTED WORKING AGAIN ON SHORT FIN AL APPROACH. TRIED USING PRIMARY TRIM SEVERAL TIMES IN FLIGHT. RAN F/O, CAPTAIN CONTROL, DID NOT WORK. REMOVED AND RE PLACED HORIZONTAL STABILIZER PRIMARY TRIM MOTOR PER AMM 27-41-10. OPS CHECK OK FROM BOTH CAPTAINS AND F/O'S SWITCHES. (M) 2 L 7 2 4F TR A6WE 2003012400062 20030124 00062 NM 2003 1 24 KPVA200233 1 20021101 A 2421 317080014 GENERATOR DHAV DHC8 DHC8103 1386005 NM NR 2 ENGINE FAULTY A KPVA K NONE J WARNING INDICATION CR CRUISE 1 WP 13 807WP 023 NR 2 GEN CAUTION LIGHT CAME ON IN FLIGHT FOLLOWED BY EMERGENCY LIGHTS WHICH CAME ON, THEN WENT OUT RECYCLED NR 2 AC GENE RATOR SWITCH, BUT CAUTION LIGHT CAME ON AGAIN. AIRCRAFT FERRIED BACK TO HNL. REMOVED AND REPLACED NR 2 AC GENERATOR IA W DHC8MM 24-21-00 PAGE 201-202. OPS CHECK GOOD IAW DHC8MM 24-21-00 PAGE 205 SECTION B LEAK CHECK GOOD IAW PWC MM 72-01- 00 PAGE 501. (M) 2 H 7 2 4T RT A13NM 2003012400063 20030124 00063 NE 2003 1 24 KPVA200236 3 20021126 A 6111 SFA13 BLADE DHAV DHC8 DHC8103 1386005 NM HAMSTD 14SF 14SF7 NE RT PROPELLER CRACKED A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 805WP 9789 353 920913 MAINTENANCE FOUND CRACK ON NR 1 BLADE OF NR 2 ENGINE PROP ASSY. REMOVED NR 1 BLADE OF NR 2 ENGINE PROP ASSY IAW HAMILTO N SUNDSTRAND MM 61-10-00, PAGE 307-311 PARA 5A. INSTALLED NEW PROP BLADE IAW HAMILTON SUNSTRAND MM 61-10-00, PAGE 705-7 14 PAR, G/H. GROUND RUN-UP CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 6 C P7NE 2003012400064 20030124 00064 NM 2003 1 24 KPVA200237 1 20021201 A 3350 1155591 LIGHT DHAV DHC8 DHC8103 1386005 NM CABIN BROKEN A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 806WP 357 EXIT LIGHT ON ROW 1 RIGHT SIDE IS BROKEN. REMOVED AND REPLACED EXIT LIGHT ON ROW 1 RIGHT SIDE IAW DHC-8 MM 33-51-00 PAG E 201 SECTION 1A. OPS CHECK GOOD IAW DHC8 MM 33-51-00 PAGES 201-202. (M) 2 H 7 2 4T RT A13NM 2003012400065 20030124 00065 NM 2003 1 24 MEX2002346 1 20021121 A 7711 INDICATOR BOEING 757 7572Q8 1384972 NM COCKPIT MALFUNCTIONED A ASMF A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 23 805AM 26272 FLT 171 - JIJ- DURING TAKEOFF EPR INDICATIONS WAS BLANK RIGHT ENGINE AND N1 WITH FLUCTUATIONS AT REDUCE POWER ON RIGHT E NGINE AFTER 5 MINUTES INDICATIONS WAS NORMAL. AFTER 35 MINUTES IN FLIGHT RETURNED TO AIRPORT. AT PLATFORM, TECHNICAL P ERSONNEL CHECKED CHP DETECTOR MAGNETIC AND INLET AND OUTLET FOR GENERAL CONDITIONS IAW FIM 77-21-00. A BORESCOPE INSPEC TION AND ENGINE RUN WERE ACCOMPLISHED WITHOUT MESSAGES IN EICAS OF PHYSICAL DAMAGES. (M) 2 L 7 2 4F RT A2NM 2003012400066 20030124 00066 NM 2003 1 24 S2YA02037 1 20021007 A 3260 LIGHT DORNER DO32 DO328300 NM COCKPIT INOPERATIVE A S2YA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 13 356SK 3163 FLT 2022 - MKE-PIT, THE CREW SELECTED GEAR DOWN BUT NOSE AND RIGHT MAIN INDICATORS DID NOT ILLUMINATE. THE CREW MADE A GO AROUND TO A HOLD PATTERN. THE F/O REPLACED THE LIGHT BULBS AND SELECTED GEAR DOWN. THE CREW ATTENDED THREE GREEN DO WN AND LOCKED LIGHTS AND PROCEEDED WITH THE LANDING. NO FURTHER DEFECTS NOTED. (M) 2 H 7 2 4T RT A55NM 2003012400067 20030124 00067 NM 2003 1 24 S2YA02039 1 20021014 A 3241 AE208741 CONTROL UNIT DORNER DO32 DO328300 NM ANTI-SKID SYS FAULTY A S2YA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 13 360SK 1689 3136 FLT 2151 - BWI-MKE - DURING TAKEOFF, WHEN THE A/C REACHED ABOUT 40 KNOTS THERE WAS INDICATION OF ALTERNATE ANTI-SKID. T HE CREW ABORTED THE TAKEOFF CLEARED THE MESSAGE AND TRY AGAIN ONLY TO ABORT THE SECOND ATTEMPT. THE CREW CONSULTED MX A THIRD ATTEMPT OF TAKEOFF WAS SUCCESSFUL. AT ARRIVAL IN MKE, THE ANTI-SKID CONTROL UNITS WERE SWAPPED FROM THE ALTERNAT E TO THE NORMAL FOR TROUBLESHOOTING. THE NEXT DAY 10/15/2002 MAINTENANCE HAD A NORMALANTI-SKID DEGRADE. THE ASCU WAS R EPLACED WITH NO FURTHER DISCREPANCIES. (M) 2 H 7 2 4T RT A55NM 2003012400068 20030124 00068 CE 2003 1 24 S2YA02041 1 20021020 A 5270 SWITCH BEECH 1900 1900D 1154162 CE CARGO DOOR OUT OF ADJUST A S2YA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 145SK UE145 FLT 1371 - MKE-LSE - SHORTLY AFTER TAKEOFF, THE CARGO DOOR ANNUNCIATOR ILLUMINATED. THE CREW MADE AN AIR TURN BACK TO M KE. MAINTENANCE INSPECTED THE DOOR, CLEANED AND ADJUST THE MICRO-SWITCHES. THE A/C WAS RETURN TO SERVICE WITH NO FURTH ER DEFECTS. (M) 2 L 7 2 4T RT A24CE 2003012400069 20030124 00069 NM 2003 1 24 S2YA02042 1 20021027 A 5270 SWITCH DORNER DO32 DO328300 NM APU DOOR DIRTY A S2YA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 13 353SK 3122 DURING FLIGHT 2297 - YYZ-MKE - THE APU AIR START DOOR ANNUNCIATOR ILLUMINATED. THE CREW DIVERTED TO GRR SINCE THE QRH S TATES IT IS NECESSARY TO LAND AT NEXT SUITABLE AIRPORT FOR ANY DOOR OPEN INDICATION. THE INDICATION WENT AWAY DURING AP PROACH TO GRR. GRR OUTSTATION MX INSPECTED THE DOOR AND MICRO-SWITCH WITH NO DEFECTS NOTED. THE A/C CONTINUED TO MKE W HERE MX INSPECTED AND CLEANED THE SWITCH, NO FURTHER DEFECTS NOTED. (M) 2 H 7 2 4T RT A55NM 2003012400070 20030124 00070 SO 2003 1 24 SIMA200232307 1 20021116 A 3340 480CC01 CONTACTOR EMB 135 EMB135KL 3260302 SO NLG BURNED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 810AE 145525 ORD - FLT 4251 - CREW REPORTED AN ELECTRICAL BURNING SMELL IN COCKPIT WITH NO VISIBLE SMOKE NOTED. AN EMERGENCY WAS DEC LARED AND AIRCRAFT RETURNED TO ORD WITHOUT FURTHER INCIDENT REPORTED. MAINTENANCE FOUND A BURNED NOSE LANDING LIGHT CON TACTOR. WHICH WAS REPLACED IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2003012400071 20030124 00071 SO 2003 1 24 SIMA200232401 1 20021116 A 3610 CLAMP EMB 145 EMB145LR 3260212 SO BLEED AIR SYS LOOSE A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 615AE 145087 FWA - FLT 4173 - DURING CRUISE FLIGHT, CREW REPORTED A 'BLEED NUMBER 1 LEAK' MESSAGE ON EICAS. CREW DIVERTED TO FWA DUE TO NO CABIN/COCKPIT HEAT AND WEATHER AT DESTINATION. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND AND TIGHTENED SOME LOOSE CLAMPS IN THE NR 1 BLEED SYSTEM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2003012400072 20030124 00072 SO 2003 1 24 SIMA200232405 1 20021117 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - DURING A IMBV INSPECTION, MAINTENANCE FOUND THE SERVICE DOOR CENTER SILL CORRODED BELOW SRM LIMITS. BLENDED CORRO DED AREAS ON CENTER SILL. PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS NOTED. FABRICATED TWO REPAIR DOUBLER . REPAIR DONE IAW AE ETN NR EM-53-036 AND EMB SRM (SRM EMB-145.1142 REV 19) CHAPTERS 51-40-02, 51-20-03 AND 51-40-06. (M) 2 L 7 2 4T RT T00011AT 2003012400073 20030124 00073 EU 2003 1 24 SIMA200232406 1 20021119 A 5610 7256100501 WINDSHIELD SAAB SF340 340B 7860101 EU COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 390AE 340B390 LRD - FLT 3456 - AFTER CREW PUT CAPTAINS WINDSHIELD ON MEL FOR SMALL CRACK IN OUTER PANE, AIRCRAFT DEPARTED FOR DFW, CLI MBING THROUGH 10,000 FEET THE OUTER PANE SHATTERED (SPIDER WEBBED). CREW RETURNED TO LRD AND LANDED WITH NO FURTHER INC IDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT W AS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2003012400074 20030124 00074 SO 2003 1 24 SIMA200232901 1 20021120 A 5313 STRINGER EMB 135 EMB135LR 3260305 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 735TS 145386 ABI - DURING AN MBV INSPECTION, STRINGER 19R WAS FOUND TO BE CHAFED AT JUNCTION 05. BLENDED CHAFED AREA. PERFORMED EDD Y CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED AND DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/ 1142, CHAPTER 53, REV 19) AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4F RT T00011AT 2003012400075 20030124 00075 SO 2003 1 24 SIMA200232902 1 20021119 A 5313 14525768615 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - DURING A IMBV INSPECTION, MAINTENANCE FOUND THE LEFT STRINGER 19 AT FRAME 52 GOUGED. BLENDED GOUGE AND PERFORMED AN NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED TWO DOUBLERS AND FOUR SHIMS. REPAIR DONE IAW EMB GST-3363/02 AND G ST 3355/02. (M) 2 L 7 2 4T RT T00011AT 2003012400076 20030124 00076 SO 2003 1 24 SIMA200232903 1 20021119 A 5313 14525768615 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - DURING A IMBV INSPECTION, MAINTENANCE FOUND THE RIGHT STRINGER 19 AT FRAME 52 GOUGED. BLENDED GOUGED AND PERFORME D AN NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED TWO DOUBLERS AND FOUR SHIMS. REPAIR DONE IAW EMB GST-3363/02 AND GST-3355/02. (M) 2 L 7 2 4T RT T00011AT 2003012400077 20030124 00077 EA 2003 1 24 SIMA200232904 1 20021121 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA LAVATORY ACTIVATED A SIMA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 501BG 10017 DFW - FLT 3887 - AFTER CLIMB-OUT, CREW RECEIVED LAVATORY SMOKE INDICATION. FLIGHT ATTENDANT VERIFIED SMOKE SMELL IN CAB IN. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. SUSPECT PR EVIOUS NIGHT ENGINE COMPRESSOR WASH TO BE THE CAUSE. GROUND ENGINE RUN AND BLEED SYSTEM OPERATIONAL CHECK WAS COMPLIED WITH AND NO SMELL WAS NOTED. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2003012400078 20030124 00078 EU 2003 1 24 SIMA200232905 1 20021121 A 3620 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT ACTIVATED A SIMA K NONE J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 905AE 340B319 PVD - FLIGHT 4883 - DURING APPROACH, CREW REPORTED THE LEFT BLEED CLOSE LIGHT CAME ON. AFTER LANDING CREW RESET BLEED A ND GOT A SMOKE SMELL IN THE AIRCRAFT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. GROUND ENGINE RUNS AND AN OPERATION AL CHECK OF THE BLEED AND AIR CONDITIONING SYSTEMS WERE GOOD IAW SAAB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2003012400091 20030124 00091 SO 2003 1 24 SIMA200232906 1 20021122 A 4930 1617972 SOLENOID EMB 135 EMB135LR 3260305 SO APU MALFUNCTIONED A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 712AE 145247 CMH - FLT 4564 - AFTER TAKEOFF, CREW REPORTED SMELLING FUMES IN COCKPIT AND FLIGHT ATTENDANT REPORTED A HAZE IN THE CABI N LIKE A BURNING PLASTIC SMELL. MAINTENANCE FOUND THE APU HAD DUMPED ITS OIL INTERNALLY INTO THE AIR CONDITIONING SYSTE M. APU WAS PUT ON MEL AT THIS TIME. NO DISCREPANCY WAS FOUND WITH THE PRESSURIZATION CONTROL OR BLEED AIR SYSTEM. MAI NTENANCE CLEARED THE APU MEL BY REMOVING AND REPLACING THE APU FUEL SOLENOID IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2003012400092 20030124 00092 GL 2003 1 24 SIMA200232907 2 20021123 A 7200 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL LEFT MALFUNCTIONED A SIMA B EMER. DESCENT B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 712AE 145247 CAE311272 LGA - FLT 4401 - AFTER TAKEOFF, CREW REPORTED LAVATORY SMOKE MESSAGE ON EICAS AND SMOKE IN CABIN. APU ALREADY ON MEL. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2003012400093 20030124 00093 EU 2003 1 24 SIMA200232908 1 20021124 A 2120 ODOR SAAB SF340 340B 7860101 EU CABIN DETECTED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 180AE 340B180 DFW - FLT 3495 - AFTER TAKEOFF, CREW RETURNED TO DFW BECAUSE OF STRONG ODOR STILL PRESENT AFTER BLEEDS SELECTED OFF. PA SSENGER AND CREW COMPLAINED OF HEADACHES. MAINTENANCE PERFORMED GROUND ENGINE RUNS AND FOUND NO DEFECTS. SUSPECT RECIR CULATION FAN THAT IS ON MEL TO BE THE SOURCE OF THE SMELL. (M) 2 L 7 2 4T RT A52EU 2003012400095 20030124 00095 EU 2003 1 24 SIMA200233001 1 20021125 A 3230 D49412001 CONTROL PANEL SAAB SF340 340B 7860101 EU COCKPIT FAULTY A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 386AE 340B386 DFW - FLT 3533 - DURING CRUISE FLIGHT, CREW REPORTED THE GEAR IN TRANSIT LIGHT CAME ON AND REMAINED ON IN FLIGHT. HYDRA ULIC PUMP DID NOT RUN AND GEAR APPEARED TO REMAIN LOCKED AND UP. AIRCRAFT WAS RETURNED TO DFW. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL PANEL IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2003012400096 20030124 00096 NM 2003 1 24 TSAA0233228 1 20021108 A 3350 86210066 BATTERY PACK BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED NR 4 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4U RT A16WE 2003012400097 20030124 00097 NM 2003 1 24 TSAA0233229 1 20021108 A 3350 9221009 LIGHT BOEING 737 7372Y5 1384554 NM CABIN INOPERATIVE A K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED LT OVERWING IDENT LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 2003012400098 20030124 00098 NM 2003 1 24 TSAA0233230 1 20021108 A 3350 86210066 BATTERY PACK BOEING 737 737230 1384401 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED NR 2 FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003012400099 20030124 00099 NM 2003 1 24 TSAA0233267 1 20021109 A 3350 861002 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 3 AND 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECKS OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003012400100 20030124 00100 2003 1 24 TSAA0234226 4 20021022 A 3442 MI5851622 INDICATOR BOEING 737 7372X6C 1384552 NM COCKPIT FAULTY A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 13 816AL 23122 PRIOR TO TAXI, THE CREW NOTICED A STRONG SMELL OF ELECTRIC FUMES FOLLOWED BY SMOKE IN COCKPIT. THE AIRCRAFT WAS SECURED FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE RADAR TRANSCEIVER AND RADAR INDICATOR. OPERATIONAL CHECK OF THE RADAR SYSTEM WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. THE AVIONICS SHOP FOUND THE BURNING SMELL ORIGINATING FOR THE RADAR INDICATOR. THE UNIT WAS TAGGED FOR REPAIR BY AN OUTSIDE VENDOR. (M) 2 L 7 2 4F RT A16WE 2003012400103 20030124 00103 EU 2003 1 24 AWXA200300070 1 20021231 A 5730 D57443577212 SKIN AIRBUS 320 A320232 3930326 EU CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 0 0 448 MCN - MAJOR REPAIR - DURING C-07 CHECK A 1/4" CRACK WAS FOUND BELOW THE NO. 3 SLAT STOP PAD AT L/H WING LEADING EDGE. MA INTENANCE REPAIRED L/H WING LEADING EDGE IAW A320 SRM 51-42-11, PG. 2, 4, FIG. 204, PG. 212, 214-217, SRM 57-41-18, PG. 202-203, AND DWG D57443557. 2 L 7 2 4F RT A28NM 2003012400105 20030124 00105 EU 2003 1 24 AWXA200300071 1 20021230 A 5730 D57443577213 SKIN AIRBUS 320 A320232 3930326 EU CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 0 0 448 MCN - MAJOR REPAIR - DURING C-07 CHECK A 1/4" CRACK WAS FOUND BELOW THE NO. 3 SLAT STOP PAD AT R/H WING LEADING EDGE. MA INTENANCE CUTOUT DAMAGED SECTION OF R/H WING LEADING EDGE SKIN AND 2 EACH SECTIONS OF LEADING EDGE SPAR; FABRICATED 2 E ACH REPAIR ANGLES, PACKINGS, SKIN INSERTS, AND REINFORCEMENT STRIPS; INSTALLED REPAIR PARTS IAW A320 SRM 51-41-11, PG. 2 15-217. 2 L 7 2 4F RT A28NM 2003012700070 20030127 00070 NM 2003 1 27 PCAA0211131 1 20021105 A 5320 BEAM DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 829EX 146 DURING ROUTINE MAINTENANCE VISIT WHILE PERFORMING TASK 5340/01 NOSE GEAR WELL UPPER LEFT AND RIGHT SIDE JUST FORWARD OF TRANSFER BEAM WAS FOUND CRACKED. DURING REPAIR RIGHT SIDEWALL AT STATION X97 TOP AFT CORNER, UPPER ANGLE AND RIGHT Z CH ANNEL FOUND CRACKED. CRACKS REPAIRED USING DEHAVILLAND REPAIR DRAWINGS RD8-53-675, RD8-53-3630, RD8-53-1676. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003012700071 20030127 00071 NM 2003 1 27 PCAA0301012 1 20021228 A 7603 87620119003 STRUT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE BROKEN A PCAA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 EA 13 826EX 389 TM120974 LGA-IAD FLIGHT 3802 CREW REPORTED, UNABLE TO REDUCE NR 1 PROP RPM ON CLIMBOUT, AND UNABLE TO SHUT DOWN NR 1 ENGINE WITH CONDITION LEVER AT FUEL OFF. ENGINE SHUT DOWN ACCOMPLISHED WITH FUEL OFF HANDLE. MAINTENANCE REPLACED SPRING STRUT IN ACCORDANCE WITH ENGINE RIGGING MANUAL PART 2. AIRCRAFT GROUND RUN TO 900 RPM. ENGINE OPERATED AND SHUT DOWN NORMALLY. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2003012700091 20030127 00091 NM 2003 1 27 VNAA0212026 1 20021220 A 7923 SHIM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 422JS 3018 THE CREW RECEIVED A LEFT HAND OIL PRESSURE CAS MESSAGE IN THE AMBER RANGE AND CALLED MAINTENANCE CONTROL. FLIGHT 4056 W AS THEN INSTRUCTED TO RETURN TO CAK. MAINTENANCE INSPECTED AND REMOVED A OIL PRESSURE REGULATOR SHIM IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 79-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003012700109 20030127 00109 NM 2003 1 27 UPS02439990 1 20021219 A 3350 LIGHT BOEING 747 747200 1384847 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE:PFLT EMERG LIGHTS UNARMED LIGHT INOP RELAMPED. OPS CK GOOD. 2 L 7 4 4F RT A20WE 2003012700113 20030127 00113 NM 2003 1 27 ASAA0210342 1 20021202 A 7110 COWLING BOEING 737 7372Q8C 138448S NM NR 1 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE TAILPIPE COWL AT THRUST REVERSER STATION 100 GOUGED. REPAIRED TAILPIP E COWL PER SRM. (M) 2 L 7 2 4F A16WE 2003012700115 20030127 00115 NM 2003 1 27 ASAA0240231 1 20021124 A 5320 65C312403 DOUBLER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 DURING C-CHECK, FOUND CORROSION ON FRAME DOUBLER AT BS 794 RBL 22-28 AND WL 154. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700118 20030127 00118 NM 2003 1 27 ASAA0240233 1 20021124 A 5320 6516300266 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 PAE - DURING C-CHECK, FOUND OVERSIZED HOLES ON CHANNEL AT BS 178 RBL 6-18 AND WL 218. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700119 20030127 00119 NM 2003 1 27 ASAA0240234 1 20021124 A 5345 65C2614312 MOUNT BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 PAE - DURING C-CHECK, FOUND MOUNT CRACKED AT BS 204, LBL 5 AND WL 175. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700121 20030127 00121 NM 2003 1 27 ASAA0240235 1 20021214 A 5330 65C32355 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE LIGHTNING STRIKE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 PAE - DURING C-CHECK, FOUND LIGHTNING STRIKES ON FUSELAGE SKIN AT BS 273.5, 360, 447 AND STRINGERS 2L AND 3L AND 76. RE PAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700123 20030127 00123 NM 2003 1 27 ASAA0240236 1 20021214 A 5330 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PAE - DURING C-CHECK, FOUND SKIN IS DENTED AT BS 807 STRINGER 27R TO 27L. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700125 20030127 00125 NM 2003 1 27 ASAA0240237 1 20021214 A 5247 6550904 SKIN BOEING 737 7374Q8 138447Q NM APU DOOR DENTED A K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 DURING C-CHECK, FOUND APU ACCESS DOOR SKIN DENTED AND CHAFED OUT OF LIMITS. REPAIR IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700127 20030127 00127 NM 2003 1 27 ASAA0240238 1 20021214 A 5247 RETAINER BOEING 737 7374Q8 138447Q NM APU DOOR CHAFED A K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 DURING C-CHECK, FOUND APU ACCESS DOOR SEAL RETAINER ANGLE IS CHAFED ON LEFT SIDE. REPAIR IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700129 20030127 00129 NM 2003 1 27 ASAA0240239 1 20021214 A 1430 COTTER PIN BOEING 737 7374Q8 138447Q NM PAX DOOR OUT OF POSITION A K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 DURING C-CHECK, FOUND FORWARD ENTRY DOOR SNUBBER COTTER PINS CHAFING FUSELAGE STRUCTURE INBOARD LOWER CAM PLATE. REPAIR IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700134 20030127 00134 NM 2003 1 27 ASAA0240240 1 20021214 A 5753 65C2630934 STIFFENER BOEING 737 7374Q8 138447Q NM T/E FLAP WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 PAE - DURING C-CHECK, FOUND RIGHT MID FLAP PYLON CUTOUT STIFFENER ARE WORN. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700136 20030127 00136 NM 2003 1 27 ASAA0240241 1 20021214 A 5420 65C2630013 CHANNEL BOEING 737 7374Q8 138447Q NM PYLON CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 PAE - DURING C-CHECK, FOUND PYLON PANEL NR 5836 SUPPORT CHANNEL IS CRACKED. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700138 20030127 00138 NM 2003 1 27 ASAA0240242 1 20021214 A 5720 654646047 ANGLE BOEING 737 7374Q8 138447Q NM RT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 PAE - DURING C-CHECK, FOUND RIGHT WING TRAILING EDGE HAS A CRACKED ANGLE AT RSS 545. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700140 20030127 00140 2003 1 27 ASAA0280348 4 20021003 A 2565 D29984113 SLIDE DOUG DC9 DC982 3022082 WP TAILCONE FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 OAK - DURING LINE CHECK, THE TAILCONE WAS INADVERTENTLY RELEASED, AND WAS DAMAGED AS A RESULT OF THE FALL. THE AFT EMER GENCY ESCAPE SLIDE, RIGGED TO AUTOMATICALLY DEPLOY UPON TAILCONE RELEASE, DID NOT DEPLOY. INSPECTION OF THE ESCAPE SLID E PACK AND ITS RIGGING REVEALED NO ANOMALIES WHICH MIGHT ACCOUNT FOR THE NON-DEPLOYMENT. THE DAMAGED TAILCONE WAS REPLA CED AND THE SLIDE RE-RIGGED. THE SLIDE WAS SUBSEQUENTLY REMOVED FOR OVERHAUL ON NOV 12. (M) 2 L 7 2 4F A6WE 2003012700142 20030127 00142 WP 2003 1 27 ASAA0280449 1 20021026 A 5320 593056013 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING 30K-CHECK, FLOOR SUPPORT CORRODED AT FS 1155, LBL 22-44. REPLACED SUPPORT PER SRM 53-14-1, 51-10-4, AND 51 -30-5. (M) 2 L 7 2 4F RT A6WE 2003012700145 20030127 00145 WP 2003 1 27 ASAA0280466 1 20021028 A 5321 9936585 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 465-541, LBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24 -0. (M) 2 L 7 2 4F RT A6WE 2003012700147 20030127 00147 WP 2003 1 27 ASAA0280467 1 20021028 A 5321 9936585 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 541-617, RBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-2 4-0. (M) 2 L 7 2 4F RT A6WE 2003012700149 20030127 00149 WP 2003 1 27 ASAA0280468 1 20021028 A 5321 9936585 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, FLOORBOARD DISBONDED AT FS 693-769, LBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. ( M) 2 L 7 2 4F RT A6WE 2003012700151 20030127 00151 WP 2003 1 27 ASAA0280469 1 20021028 A 5321 9936585 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, FLOORBOARD DISBONDED AT FS 693-769, RBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. ( M) 2 L 7 2 4F RT A6WE 2003012700153 20030127 00153 WP 2003 1 27 ASAA0280470 1 20021028 A 5321 9939195 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, FLOORBOARD DISBONDED AT FS 807-826, LBL 22 - RBL 22. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24 -0. (M) 2 L 7 2 4F RT A6WE 2003012700154 20030127 00154 WP 2003 1 27 ASAA0280471 1 20021028 A 5321 9936640 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, FLOORBOARD DISBONDED AT FS 889-927, RBL 22 - RBL 44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24 -0. (M) 2 L 7 2 4F RT A6WE 2003012700155 20030127 00155 WP 2003 1 27 ASAA0280472 1 20021028 A 5321 9936585 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 927-1003, LBL 22 - LBL 44. REPLACED FLOORBOARD PER SRM 53-05 A ND 53-24-0. (M) 2 L 7 2 4F RT A6WE 2003012700156 20030127 00156 WP 2003 1 27 ASAA0280473 1 20021028 A 5321 9936653 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD PUNCTURED AT FS 1250-1307, LBL 22 - LBL 44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. (M) 2 L 7 2 4F RT A6WE 2003012700159 20030127 00159 WP 2003 1 27 ASAA0280474 1 20021028 A 5754 995416939 DOOR DOUG DC9 DC983 3022083 WP L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, LEFT WING NR 11 SLAT TRACK DOOR IS CHAFFED AT FORWARD END. REPLACED SLAT TRACK DOOR. (M) 2 L 7 2 4F RT A6WE 2003012700162 20030127 00162 WP 2003 1 27 ASAA0280475 1 20021028 A 5347 5936663 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY RIGHT TIE-DOWN TRACK FORWARD SPLICE IS CORRODED AT FS 1090. REPLACED SPLICE PER SRM 53-05, FIG 4G, AND 53-24-0, FIG 11. (M) 2 L 7 2 4F RT A6WE 2003012700164 20030127 00164 WP 2003 1 27 ASAA0280476 1 20021028 A 5321 SLS5128A3C INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD HAS CORRODED INSERTS AT FS 160-200, RBL 8 TO LBL 8. REPLACED INSERTS PER SRM 5 3-05. (M) 2 L 7 2 4F RT A6WE 2003012700165 20030127 00165 WP 2003 1 27 ASAA0280477 1 20021028 A 5321 9957828503 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLIGHT DECK FLOOR PANEL LOWER SURFACE IS SEPARATING FROM CORE AT FS 148.55, RBL 31-44. RE PLACED FLOORBOARD PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003012700166 20030127 00166 WP 2003 1 27 ASAA0280478 1 20021028 A 5321 9936651515 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DELAMINATING AT FS 541-579, LBL 22 TO RBL 22. REPLACED FLOORBOARD PER SRM 53-0 5. (M) 2 L 7 2 4F RT A6WE 2003012700167 20030127 00167 WP 2003 1 27 ASAA0280481 1 20021031 A 5321 99365851 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 389-465, LBL 22-44. REPLACED FLOORBOARD PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003012700168 20030127 00168 WP 2003 1 27 ASAA0280482 1 20021029 A 5321 99366541 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DELAMINATED AT FS 1079-1156, LBL 22-44. REPLACED FLOORBOARD PER SRM 53-05. (M ) 2 L 7 2 4F RT A6WE 2003012700170 20030127 00170 WP 2003 1 27 ASAA0280483 1 20021029 A 5321 993654879 STIFFENER DOUG DC9 DC983 3022083 WP FLOORBOARD CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD STIFFENER CRACKED AT FS 207-256, LBL 44-54. REPAIRED STIFFENER WITH FIBERGLASS OVERLAY PER MM 25-00-00, PARA 3E, PG 801. (M) 2 L 7 2 4F RT A6WE 2003012700172 20030127 00172 NM 2003 1 27 ASAA0210330 1 20021127 A 5320 1612120 SUPPORT FITTING BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND SUPPORT FITTING AT BS 344, LEFT BUTTOCK LINE 59 CORRODED. REMOVED CORRODED PART, FABRICATED AND INSTALLED NEW PART PER SRM. (M) 2 L 7 2 4F A16WE 2003012700173 20030127 00173 NM 2003 1 27 ASAA0210331 1 20021127 A 5320 161218 SUPPORT FITTING BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND SUPPORT FITTING AT BS 312, LEFT BUTTOCK LINE 54 CORRODED. REMOVED CORRODED PART, F ABRICATED AND INSTALLED NEW PART PER SRM. (M) 2 L 7 2 4F A16WE 2003012700174 20030127 00174 NM 2003 1 27 ASAA0210332 1 20021127 A 7110 7075T6050 COWLING BOEING 737 7372Q8C 138448S NM NR 1 ENGINE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND EXISTING REPAIR ON NR 1 ENGINE COWL AT NACELLE STATION 99.5 GOUGED. REMOVED PREVI OUS REPAIR, FABRICATED AND INSTALLED NEW REPAIR PER SRM. (M) 2 L 7 2 4F A16WE 2003012700175 20030127 00175 NM 2003 1 27 ASAA0210333 1 20021127 A 5320 656217548 FLOOR SUPPORT BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND FLOOR SUPPORT AT BS 328-344, LEFT BUTTOCK LINE 12 CORRODED. REMOVED CORROSION, FA BRICATED AND INSTALLED NEW SUPPORT PER SRM. (M) 2 L 7 2 4F A16WE 2003012700177 20030127 00177 NM 2003 1 27 ASAA0210334 1 20021127 A 5320 6545834552 INTERCOSTAL BOEING 737 7372Q8C 138448S NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND INTERCOSTAL AT BS 312-328, RIGHT BUTTOCK LINE 32 CRACKED. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM. (M) 2 L 7 2 4F A16WE 2003012700178 20030127 00178 NM 2003 1 27 ASAA0210335 1 20021127 A 5315 6545810 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 328, RIGHT BUTTOCK LINE 11-45 CORRODED. REMOVED, FABRICATED AND I NSTALLED UPPER CHORD PER SRM. (M) 2 L 7 2 4F A16WE 2003012700179 20030127 00179 NM 2003 1 27 ASAA0210341 1 20021202 A 5320 STRAP BOEING 737 7372Q8C 138448S NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND TENSION STRAP AT BS 328-334, RIGHT BUTTOCK LINE 48 CRACKED 1 INCH. REPAIRED TENSI ON STRAP PER SRM. (M) 2 L 7 2 4F A16WE 2003012700180 20030127 00180 NM 2003 1 27 ASAA0210343 1 20021202 A 7110 657377482 COWLING BOEING 737 7372Q8C 138448S NM NR 2 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL AT NACELLE STATION 205 GOUGED. REPAIRED ENGINE COWL PER SRM. (M ) 2 L 7 2 4F A16WE 2003012700181 20030127 00181 NM 2003 1 27 ASAA0210344 1 20021202 A 7110 6573769 COWLING BOEING 737 7372Q8C 138448S NM NR 2 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL AT NACELLE STATION 136 GOUGED. REPAIRED ENGINE COWL PER SRM. (M ) 2 L 7 2 4F A16WE 2003012700182 20030127 00182 NM 2003 1 27 ASAA0210345 1 20021203 A 5315 6546568610 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 1016, RIGHT BUTTOCK LINE 37, LEFT BUTTOCK LINE 38 CORRODED. REMOV ED CORROSION AND REPAIRED FLOORBEAM PER SRM AND EA. (M) 2 L 7 2 4F A16WE 2003012700183 20030127 00183 NM 2003 1 27 ASAA0210347 1 20021203 A 5320 6561381162 CHANNEL BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND SUPPORT CHANNEL AT BS 994, LEFT BUTTOCK LINE 14-40 CORRODED. REMOVED AND REPLACED SUPPORT CHANNEL PER SRM. (M) 2 L 7 2 4F A16WE 2003012700184 20030127 00184 NM 2003 1 27 ASAA0210348 1 20021203 A 5347 BAC15201434 SEAT TRACK BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND SEAT TRACK AT BS 887-947, RIGHT BUTTOCK LINE 45.5 CORRODED. REMOVED AND REPLACED S EAT TRACK PER SRM. (M) 2 L 7 2 4F A16WE 2003012700185 20030127 00185 NM 2003 1 27 ASAA0210389 1 20021211 A 5210 6529994 GUIDE ARM BOEING 737 737290C 138448V NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 ANC - FLIGHT CREW REPORTED L1 DOOR DIFFICULT TO CLOSE. APPLIED HEAT AND LUBED UPPER GUIDE ARM, THEN OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 2003012700186 20030127 00186 NM 2003 1 27 ASAA0240190 1 20021113 A 5342 6554842 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE WORN A K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 DURING SI CHECKED, FOUND VERTICAL STABILIZER SKATE ANGLE WORN. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700187 20030127 00187 NM 2003 1 27 ASAA0240191 1 20021113 A 5311 6546550 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 PAE - DURING SI CHECK, FOUND DENTED FRAME AT BS 787 BETWEEN STRINGER 24 AND 25. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700188 20030127 00188 NM 2003 1 27 ASAA0240192 1 20021113 A 5320 ATTACH ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 PAE - DURING SI CHECK, FOUND FORWARD CARGO COMPARTMENT ATTACH ANGLE CRACKED AT BS 500 AND RBL 25. REPAIRED IAW SRM. (M ) 2 L 7 2 4F RT A16WE 2003012700189 20030127 00189 NM 2003 1 27 ASAA0240193 1 20021113 A 5720 SUPPORT BOEING 737 7374Q8 138447Q NM RT WING CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 PAE - DURING SI CHECKED, FOUND RIGHT WING TRAILING EDGE PANEL SUPPORT IS CHAFED ABOVE PYLON CUTOUT. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700190 20030127 00190 NM 2003 1 27 ASAA0240194 1 20021113 A 5320 ATTACH ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 DURING SI CHECKED, FOUND FORWARD CARGO COMPARTMENT ATTACH ANGLE CRACKED AT BS 500F AND LBL 25. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700191 20030127 00191 NM 2003 1 27 ASAA0240195 1 20021113 A 5720 65C80736404 SUPPORT BOEING 737 7374Q8 138447Q NM RT WING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 PAE - DURING SI CHECKED, FOUND RIGHT WING UPPER TRAILING EDGE PANEL SUPPORT HAS FASTENER HOLE ELONGATED AT WBL 70 AT BS 729. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700192 20030127 00192 NM 2003 1 27 ASAA0240196 1 20021113 A 5720 694754221 SUPPORT BOEING 737 7374Q8 138447Q NM LT WING DAMAGED A K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 DURING SI CHECKED, FOUND LEFT WING UPPER TRAILING EDGE PANEL SUPPORT HAS FASTENER HOLE ELONGATED AT WBL 70 RIGHT AND BS 729. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700193 20030127 00193 NM 2003 1 27 ASAA0240197 1 20021113 A 5320 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 PAE - DURING SI CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME CLOSE OUT WEB IS DAMAGED, AT BS 492.4, RBL 27 AND WL 156. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700194 20030127 00194 NM 2003 1 27 ASAA0240199 1 20021113 A 5311 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 DURING SI CHECK, FOUND FRAME WEB DAMAGED AT BS 793 BETWEEN STRINGER 27R AND 25R. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700195 20030127 00195 NM 2003 1 27 ASAA024020 1 20021113 A 5320 65C27308 SUPPORT ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 PAE - DURING SI CHECK, FOUND CORROSION AND DENT ON SIDEWALL SUPPORT ANGLE AT BS 727B AND STR 25R. REPAIRED IAW SRM. (M ) 2 L 7 2 4F RT A16WE 2003012700197 20030127 00197 NM 2003 1 27 ASAA0240200 1 20021113 A 5320 1496364 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 PAE - DURING SI CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT DAMAGED AT BS 500D-G. REPAIRED IAW SRM . (M) 2 L 7 2 4F RT A16WE 2003012700198 20030127 00198 NM 2003 1 27 ASAA0240202 1 20021113 A 5320 6935350 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 PAE - DURING SI CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D AND STRINGER 18. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700199 20030127 00199 NM 2003 1 27 ASAA0240203 1 20021113 A 5342 655484222 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 PAE - DURING SI CHECKED, FOUND VERTICAL STABILIZER RIGHT SKATE ANGLE GOUGED. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012700200 20030127 00200 NM 2003 1 27 ASAA0240223 1 20021121 A 5720 65682531 ANGLE BOEING 737 7374Q8 138447Q NM LT WING CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 DURING SI CHECK, FOUND ANGLE CRACKED ON LEFT WING TRAILING EDGE. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2003012700201 20030127 00201 NM 2003 1 27 ASAA0240224 1 20021121 A 5311 65C33509 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 DURING SI CHECKED, FOUND FRAME CRACKED AT BS 400 BETWEEN STRINGER 7R AND 8R AT FORWARD FASTENER HOLES. REPAIRED IAW SRM . (M) 2 L 7 2 4F RT A16WE 2003012700202 20030127 00202 NM 2003 1 27 ASAA0240230 1 20021122 A 5320 65C35767 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 DURING SI CHECK, FOUND FORWARD CARGO COMPARTMENT STRINGER CLIP CRACKED AT BS 480 AND STRINGER 22L. REPAIRED IAW SRM. ( M) 2 L 7 2 4F RT A16WE 2003012700209 20030127 00209 WP 2003 1 27 MWEA020708 1 20021119 A 5310 591015839 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 AFT CARGO DOOR LOWER JAMB HAS NR 40 SIZE HOLES AROUND MULTIPLE BLIND NUTS FASTENER HOLES. REMOVED AND INSTALLED NEW JAM B. 2 L 7 2 4F A6WE 2003012700211 20030127 00211 WP 2003 1 27 MWEA020716 1 20021120 A 5311 995791739 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 THE INBOARD CAP OF FUSELAGE FRAME STATION 937 HAS ADDITIONAL HOLES LOCATED BETWEEN LONGERON 26 RIGHT AND LONGERON 26 RIG HT, WHICH MEASURES .098 INCH IN DIAMETER. PLUGGED ADDITIONAL HOLES WITH AD MATERIAL MWX-ORD-02-00349 H. 2 L 7 2 4F A6WE 2003012700213 20030127 00213 WP 2003 1 27 MWEA020717 1 20021120 A 5311 995791739 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FUSELAGE FRAME STATION 897 HAS 1 EACH OVERSIZED HOLE IN THE INBOARD CAP LOCATED BETWEEN LONGERON 28 RIGHT AND LONGERON 2 9 RIGHT HOLE MEASURES .403 INCH DIAMETER. FABRICATED AND INSTALLED BUSHING. 2 L 7 2 4F A6WE 2003012700216 20030127 00216 WP 2003 1 27 MWEA020720 1 20021127 A 5220 39146331 RETAINER DOUG DC9 DC932 3022066 WP EMERGENCY EXIT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 RIGHT FORWARD OVERWING EXIT DOOR HAS CORROSION AT LOWER CORNER OF SEAL RETAINER. REMOVED AND REPLACED SEAL RETAINER. 2 L 7 2 4F A6WE 2003012700219 20030127 00219 WP 2003 1 27 MWEA020721 1 20021127 A 5220 39146331 RETAINER DOUG DC9 DC932 3022066 WP EMERGENCY EXIT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 RIGHT AFT OVERWING EXIT DOOR HAS CORROSION AT LOWER FORWARD CORNER OF SEAL RETAINER. REMOVED AND REPLACED SEAL RETAINER . 2 L 7 2 4F A6WE 2003012700222 20030127 00222 WP 2003 1 27 MWEA020726 1 20021208 A 3241 426071 CONTROL BOX DOUG DC9 DC982 3022082 WP LT MLG MALFUNCTIONED A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 808ME 48070 AUTO BRAKES WERE ARMED, THE MASTER CAUTION LIGHT AND AUTO BRAKE FAIL LIGHTS CAME ON. REMOVED AND REPLACED ANTISKID CONT ROL BOX. 2 L 7 2 4F A6WE 2003012700225 20030127 00225 WP 2003 1 27 MWEA020732 1 20021214 A 2612 30903852 FIRE DETECTOR DOUG DC9 DC932 3022066 WP CARGO BAY FAULTY A MWEA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 31 204ME 47680 CARGO FIRE DETECTOR LOOP LIGHT CAME ON. REMOVED AND REPLACED THE METERING VALVE, BOTTLE ASSEMBLY, SQUIB DIVERTER AND SQ UIB. 2 L 7 2 4F A6WE 2003012700235 20030127 00235 WP 2003 1 27 MWEA020741 1 20021217 A 3230 BEARING DOUG DC9 DC932 3022066 WP LT MLG NOT SEATED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 216ME 47740 WHEN GEAR RETRACTED ALL LIGHTS OUT, EXCEPT THE LEFT GEAR UNSAFE LIGHT. MAINTENANCE RESEATED LEFT UPLATCH HOOK CENTER BE ARINGS. 2 L 7 2 4F A6WE 2003012700237 20030127 00237 WP 2003 1 27 MWEA020744 1 20021220 A 5320 99365343 WEB DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 GALLEY SUBFLOOR HAS HOLE JUST INBOARD OF SERVICE DOOR ENTRANCE. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2003012700240 20030127 00240 WP 2003 1 27 MWEA020747 1 20021222 A 7711 B-NUT DOUG DC9 DC981 3022081 WP RT ENGINE LOOSE A MWEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 803ME 48029 THE RIGHT ENGINE WOULD INDICATE ONLY 1.65 ON EPR CALLING FOR 1.95 N1, EPR, N2, AND FUEL FLOW INDICATED THAT IT SHOULD BE AT NORMAL POWER. TIGHTENED B-NUT AT 2 O'CLOCK POSITION OF AFT PT7 BRIDLE. 2 L 7 2 4F A6WE 2003012700243 20030127 00243 WP 2003 1 27 MWEA020754 1 20021226 A 5320 99367183 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 AFT CARGO COMPARTMENT HAS MODERATE CORROSION ON LONGERON 28 LEFT, STATION 1309-1312. REMOVED CORROSION, FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2003012800130 20030128 00130 SO 2003 1 28 SWIA200211560 1 20021204 A 2560 SIGN EMB 120 EMB120ER 3260203 SO CABIN MISSING A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 585SW 120353 EXIT SIGN MISSING NEXT TO FLIGHT ATTENDANT SEAT ON LEFT SIDE OF FORWARD BULKHEAD. INSTALLED NEW EXIT SIGN FIXTURE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003012800131 20030128 00131 SO 2003 1 28 SWIA200211561 1 20021201 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO CABIN DOOR LACK OF LUBE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 187SW 120037 FORWARD DOOR LIGHT ILLUMINATED INFLIGHT. LUBED FORWARD DOOR MICROSWITCHES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003012800132 20030128 00132 SO 2003 1 28 SWIA200211562 1 20021207 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 189SW 5835 5835 120048 EXIT LIGHT AT ROW 9 AND FLOOR LEVEL EMERGENCY LIGHTS FROM ROW 6 BACK ARE INOP. REPLACED NR 3 BATTERY PACK. OPS CHECK G OOD. 2 L 7 2 4T RT A31SO 2003012800133 20030128 00133 EA 2003 1 28 SWIA200211563 1 20021208 A 2740 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 NM 07 592SW 7279 STAB TRIM CHANNELS 1 AND 2 FAILED ON TAKEOFF. STAB TRIM AND MACH TRIM CAUTION MESSAGES. RETURNED TO MEM. PERFORMED BI TE CHECK OF HSTCU. HSTCU SHOWS NO FAULTS IAW AMM 7-41-00. SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2003012800134 20030128 00134 EA 2003 1 28 SWIA200211564 1 20021204 A 3222 16050109 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG DEFECTIVE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 592SW 3085 3085 7279 AFTER DEPARTURE WE RECEIVED GEAR DISAGREE NOSE DOOR WARNINGS. NOSE GEAR REMAINS GREEN WHILE MAINS TURN WHITE. RETURNED TO YYC. REMOVED AND REPLACED NLG ASSEMBLY IAW CRJ MM TASK 2-21-00-000-801. GEAR SWINGS COMPLETED IAW CRJ MM 32-30-00 -720-801. OPS CHECK GOOD. REMOVED AND REPLACED NLG STEERING ECU IAW MM 32-51-10-401-801. 2 L 7 2 4F RT A21EA 2003012800135 20030128 00135 SO 2003 1 28 SWIA200211565 1 20021027 A 5310 BRACE EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 586SW 120354 FRAME 13 LEFT INBOARD AND OUTBOARD SIDES, AND FRAME 13 RIGHT SIDE INBOARD SIDE OF VERTICAL BRACES CRACKED AT COCKPIT DOO R OPENING. FOUND DURING C CHECK INSPECTION. STOP DRILLED CRACKS IN BRACE. REMOVED CRACKED IB ANGLES. FABRICATED AND INSTALLED A NEW IB ANGLES AND A DOUBLER FOR THE OB BRACE IAW SRM 51-00-00 AND 51-40-02. 2 L 7 2 4T RT A31SO 2003012800136 20030128 00136 SO 2003 1 28 SWIA200211566 1 20021027 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 586SW 120354 LEFT REAR FLOOR TRACK IS CORRODED. FOUND DURING C CHECK INSPECTION. REMOVED AND REPLACED SEAT TRACK IAW 53-01-05. 2 L 7 2 4T RT A31SO 2003012800137 20030128 00137 SO 2003 1 28 SWIA200211567 1 20021210 A 3297 WIRE HARNESS EMB 120 EMB120ER 3260203 SO LANDING GEAR FAULTY A SWIA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 07 213SW 120277 LANDING GEAR WOULD NOT RETRACT ON DEPARTURE. RETURNED TO LAX. REMOVED AND REPLACED "A" UPLOCK SENSOR AND HARNESS ASSEM BLY. OPS CHECK GOOD PER MM 32-61-01. 2 L 7 2 4T RT A31SO 2003012800139 20030128 00139 EA 2003 1 28 SWIA200211568 1 20021210 A 2910 D97C00614 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 913SW 2 2 7597 HYDRAULIC SYSTEM NR 1 LOW PRESSURE AMBER MESSAGE AND HYD 1A AMBER MESSAGE ON SYNOPTIC PAGE. RETURNED TO DEN. INSTALLED NR 1 HYDRAULIC SHUT OFF VALVE IAW MM 29-11-36. OPS CHECK GOOD. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2003012800140 20030128 00140 EA 2003 1 28 SWIA200211569 1 20021210 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 913SW 7597 2ND OVERHEAD EMERGENCY LIGHT IS INOP. RELAMPED WITH 1 GE1317 LAMP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2003012800141 20030128 00141 SO 2003 1 28 SWIA200211570 1 20021211 A 4920 APU EMB 120 EMB120ER 3260203 SO APU BAY MALFUNCTIONED A SWIA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 563SW 120338 APU START WAS ABORTED DUE TO A HUNG START. UPON INSPECTION, FOUND SMOKE AND FIRED EXTINGUISHER BOTTLE. INSPECTED APU A REA, NO OBVIOUS DEFECTS NOTED. REMOVED AND REPLACED APU FIRE BOTTLE AS PER EMB MM 26-21-00. REMOVED AND REPLACED MAIN BATTERY IAW MM 24-32-01. 2 L 7 2 4T RT A31SO 2003012800142 20030128 00142 EA 2003 1 28 SWIA200211571 1 20021212 A 3030 7858062 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA AOA HEAT MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 447SW 7677 RIGHT AOA HEAT CAUTION MESSAGE CAME ON AFTER TAKEOFF. FOLLOWED QRH AND MESSAGE STAYED ON. RETURNED TO SLC. REMOVED AN D REPLACED RIGHT AOA HEAT CONTROLLER PER MM 30-31-15. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2003012800143 20030128 00143 2003 1 28 SWIA200211572 4 20021214 A 3442 6222504001 ANTENNA EMB 120 EMB120ER 3260203 SO WEATHER RADAR FAULTY A SWIA A UNSCHED LANDING O OTHER UK UNKNOWN 1 NM 07 235SW 5224 5224 120310 RADAR PAINTS RANDOM THUNDERSTORMS WITH EACH SWEEP IN DIFFERENT LOCATIONS, FROM LARGE LEVEL FIRE ONE SWEEP, TO NOTHING TH E NEXT. RETURNED TO SFO. REPLACED ANTENNA 318. RADAR SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003012800144 20030128 00144 EA 2003 1 28 SWIA200211574 1 20021214 A 3250 SCISSORS CNDAIR CL600 CL6002B19 1900309 EA NLG DISCONNECTED A SWIA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 NM 07 429SW 7518 NOSE WHEEL GEAR DISAGREE MESSAGE WHEN GEAR RETRACTED. RETURNED TO AUS. FOUND NOSE WHEEL STEERING LINKS (SCISSORS) DISC ONNECTED. RECONNECTED, INSPECTED NOSE GEAR TIRES. NO VISUAL DAMAGE NOTED. 2 L 7 2 4F RT A21EA 2003012800147 20030128 00147 EA 2003 1 28 SWIA200211575 1 20021214 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 912SW 7595 ON SHORT FINAL, FIRST OFFICER'S SIDE WINDOW OUTER PANE SHATTERED. REMOVED AND REPLACED FO'S SIDE WINDOW IAW CRJ AMM 56- 12-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2003012800148 20030128 00148 SO 2003 1 28 SWIA200211577 1 20021215 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP LEAKING A SWIA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 288SW 6759 6759 120316 ON TAXI OUT, AFTER SELECTING FLAPS 15 DEGREES, THE HYDRAULIC QUANTITY ON THE BLUE SIDE WENT TO ZERO WITH ASSOCIATED LIGH TS. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW RII 27-307 AND 27-50-08. LEAK CHECKS GOOD. NO LEAKS NOTED AT THIS TIME. 2 L 7 2 4T RT A31SO 2003012800150 20030128 00150 SO 2003 1 28 SWIA200211579 1 20021215 A 2751 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA O OTHER N FALSE WARNING LD LANDING 1 NM 07 187SW 120037 AFTER LANDING AT PSP THE INBOARD FLAPS WOULD NOT RETRACT. REPLACED FLAP ANNUNCIATOR WITH A SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003012800152 20030128 00152 EA 2003 1 28 SWIA200211580 1 20021216 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DIRTY A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 588SW 7069 EMERGENCY ESCAPE PATH LIGHTING DOES NOT ILLUMINATE FROM ROW 9 AND AFT WHEN EMERGENCY LIGHTS SWITCHED TO ON. CLEANED THE CONNECTORS FOR THE AFT SECTION OF EMERGENCY LIGHTS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2003012800153 20030128 00153 SO 2003 1 28 SWIA200211581 1 20021216 A 3010 EJECTOR VALVE EMB 120 EMB120ER 3260203 SO DEICE SYSTEM FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 299SW 120329 DURING CLIMB IN MODERATE ICING CONDITIONS, THE LEFT AND RIGHT MIDDLE WING DEICE BOOTS FAILED REPEATEDLY ON BOTH TIMERS. RETURNED TO FAT. REPLACED EJECTOR VALVE FOR LEFT AND RIGHT MIDDLE DEICE BOOTS WITH SERVICEABLE UNITS IAW MM 30-10-04. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2003012800155 20030128 00155 SO 2003 1 28 SWIA200211582 1 20021217 A 2720 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO RUDDER FAULTY A SWIA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 NM 07 581SW 120350 DURING TAKEOFF AND LANDING, ALSO TAXING, THERE IS A ''DETENT'' AT THE NORMAL POSITION OF RUDDER TRAVEL. IT TAKES EXCESSI VE PRESSURE TO MOVE RUDDER. NOTICED DURING BEGINNING OF TAKEOFF ROLL TO ROTATION AND DURING LANDING AT FLARE APROX 120 KTS. PERFORMED RUDDER HYDRAULIC SYSTEM DIFFERENTIAL PRESSURE TEST. OPS AND LEAK CHECK GOOD IAW 27-22-00. PERFORMED RU DDER CONTROL ELECTRICAL SYSTEM TEST. OPS CHECK GOOD IAW 27-24-00. REMOVED AND REPLACED RUDDER PRESSURE SWITCHES BLUE AND GREEN IAW 27-22-01. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2003012800189 20030128 00189 NM 2003 1 28 AWXA200201209 1 20021119 A 5315 146N5111U2 FLOORBEAM BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOORBEAM AT RIGHT INBOARD EDGE OF CUSP, BS 16 81. MAINTENANCE REMOVED CUSP ATTACH ANGLE FROM RIGHT CUSP AREA BS 1640 TO BS 1720, THRESHOLD WEB AND SUPPORT STRUCTURE , INTERCOSTALS FROM BS 1680 TO BS 1700, AND CORRODED CABIN FLOORBEAM BS 1681, FABRICATED A NEW REPLACEMENT CABIN FLOORBE AM; AND INSTALLED REPAIR PART, REMOVED CUSP ATTACH ANGLE, THRESHOLD WEB AND SUPPORT STRUCTURE, AND INTERCOSTALS IAW SRM. 2 L 7 2 4F 4 F RT A2NM A12EU 2003012800190 20030128 00190 NM 2003 1 28 AWXA200201210 1 20021120 A 5320 146N53183 PAN BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MAJOR REPAIR, DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF AFT CABIN FLOOR SUB PAN AT BS 1681-B S 1720. MAINTENANCE BLENDED OUT CORROSION ON AFT CABIN FLOOR SUB PAN BS 1681-BS 1720 AND FOUND MATERIAL LOSS OUT OF LIMI TS; REMOVED 6 EACH AFT GALLEY ATTACH FITTINGS, CUSP ATTACH ANGLE, AND CORRODED AFT GALLEY SUB PAN BS 1681-BS 1720; FABRI CATED A NEW REPLACEMENT AFT GALLEY FLOOR SUB PAN; AND INSTALLED REPAIR PART, REMOVED CUSP ATTACH ANGLE, AND 6 EACH AFT G ALLEY ATTACH FITTINGS IAW SRM. 2 L 7 2 4F 4 F RT A2NM A12EU 2003012800193 20030128 00193 NM 2003 1 28 AWXA200201239 1 20021225 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 28 819AW 7375 1395 LAS - EEL - RECEIVED "NO COMMUNICATION" MESSAGE WHILE PERFORMING BITE TEST OF EMERGENCY LIGHTS. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNITS 10WL, 11WL, 12WL, AND 13WL IAW AMM 33-51-38, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2003012800196 20030128 00196 NM 2003 1 28 AWXA200300024 1 20021229 A 5315 146N5089 FLOORBEAM BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 24523 LCQ - MAJOR REPAIR - DURING C-10 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR BEAM UPPER CAP AT BS 1640, BL 0 TO LBL 5. MAINTENANCE REMOVED CORROSION ON FLOOR BEAM AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED UPPER FLOO R BEAM TEE CAP BS 1640, LBL 65 TO RBL 55; FABRICATED 2 EACH REPAIR ANGLES, 2 EACH STRAPS, AND A NEW REPLACEMENT TEE CHOR D; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, PG. 209-213. 2 L 7 2 4F RT A2NM 2003012800201 20030128 00201 NM 2003 1 28 AWXA200300032 1 20021230 A 5315 146N5089 FLOORBEAM BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 24523 LCQ - MAJOR REPAIR - DURING C-10 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR BEAM UPPER CAP AT BS 1640, LBL 60. MAI NTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED TEE CHORD BS 1640, LBL 65 TO RB L 55; FABRICATED A NEW REPLACEMENT TEE CHORD, 2 EACH REPAIR ANGLES, AND 2 EACH REINFORCEMENT STRAPS; AND INSTALLED REPAI R PARTS IAW B757-200 SRM 53-00-51, FIG. 210. 2 L 7 2 4F RT A2NM 2003012800202 20030128 00202 NM 2003 1 28 AWXA200300033 1 20021229 A 5320 146N5318 PANEL BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 24523 LCQ - MAJOR REPAIR - DURING C-10 CHECK INTERGRANULAR CORROSION WAS FOUND ON PASSENGER CABIN SHEAR DECK BS 1716, FROM BL 0 TO LT CUSP. MAINTENANCE BLENDED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA PASSENGER CABIN SHEAR DECK BS 1716, FROM BL 0 TO LBL 4, AND LBL 27 TO LBL 65; FABRICATED A DOUBLER, FILLER, AND SHIMS; AND INSTALL ED REPAIR PARTS IAW B757-200 SRM 53-60-51, FIG. 203, PG. 204-208. 2 L 7 2 4F RT A2NM 2003012800204 20030128 00204 WP 2003 1 28 ASAA020510 1 20021029 A 5510 59329705501 STRAKE DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, RIGHT STRAKE AFT EDGE IS FLATTENED. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A6WE 2003012800205 20030128 00205 WP 2003 1 28 ASAA0280484 1 20021029 A 5321 SLP5128A3C INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD INSERTS CORRODED AT FS 148. REPLACED INSERTS PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003012800206 20030128 00206 WP 2003 1 28 ASAA0280485 1 20021029 A 5321 9936546 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, COCKPIT FLOORBOARD DELAMINATED AT AFT CORNER AND 3 INSERTS ARE CORRODED AT FS 148, BL 0. REPLACED FLOORBOARD AND INSERTS PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003012800207 20030128 00207 WP 2003 1 28 ASAA0280486 1 20021029 A 5321 99365851 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 617-693, LBL 22-44. REPLACED FLOORBOARD PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003012800208 20030128 00208 WP 2003 1 28 ASAA0280487 1 20021029 A 5321 99365811 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DELAMINATED AT FS 579-617, LBL 22 - RBL 22. REPLACED FLOORBOARD WITH FIBERGLAS S OVERLAY PER MM 25-00-00, SEC 3E. (M) 2 L 7 2 4F RT A6WE 2003012800209 20030128 00209 WP 2003 1 28 ASAA0280488 1 20021029 A 5321 SLP5128A3 INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD INSERTS CORRODED AT FS 1250-1307. REPLACED 5 FLOORBOARD INSERTS SRM 53-05. (M ) 2 L 7 2 4F RT A6WE 2003012800210 20030128 00210 WP 2003 1 28 ASAA0280489 1 20021029 A 5321 9936548 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDING AT FS 200-256, RBL 44-54. REPLACED FLOORBOARD WITH FIBERGLASS OVERLA Y PER MM 25-00-00, SEC 3E. (M) 2 L 7 2 4F RT A6WE 2003012800211 20030128 00211 WP 2003 1 28 ASAA0280490 1 20021029 A 5310 993607327 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY SHEAR TIE CORRODED AT FS 1174, LONGERON 29L 29R. REPLACED SHEAR TIE PER SRM 53-14-3, 51-10-2 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003012800212 20030128 00212 WP 2003 1 28 ASAA0280491 1 20021029 A 5347 SR095301157001 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, SEAT TRACK CORRODED AT FS 1122, LBL 22. REPLACED SEAT TRACK PER SRM 53-05, 51-10-4, 51-30-05, AN D 51-30-1. (M) 2 L 7 2 4F RT A6WE 2003012800213 20030128 00213 WP 2003 1 28 ASAA0280492 1 20021029 A 5321 9936552 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 200-256, LBL 14 - RBL 22. REPLACED FLOORBOARD PER SRM 53-05. ( M) 2 L 7 2 4F RT A6WE 2003012800214 20030128 00214 WP 2003 1 28 ASAA0280493 1 20021029 A 5321 9936651 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING SCHEDULED 30K CHECK, FLOORBOARD AT BS 1079-1117, LEFT BUTTOCK LINE 22, RIGHT BUTTOCK LINE 22 TORN. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M) 2 L 7 2 4F RT A6WE 2003012800215 20030128 00215 WP 2003 1 28 ASAA0280495 1 20021029 A 5321 SLS5128A3C FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING SCHEDULED 30K CHECK, FLOORBOARD AT BS 160-200, RIGHT BUTTOCK LINE 44, RIGHT BUTTOCK LINE 54 CORRODED. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M) 2 L 7 2 4F RT A6WE 2003012800216 20030128 00216 WP 2003 1 28 ASAA0280496 1 20021029 A 5321 SLS5128A3C FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING SCHEDULED 30K CHECK, FLOORBOARD AT BS 160-200, LEFT BUTTOCK LINE 8, LEFT BUTTOCK LINE 44 CORRODED. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M) 2 L 7 2 4F RT A6WE 2003012800217 20030128 00217 WP 2003 1 28 ASAA0280497 1 20021029 A 5321 SLS5128A3C FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING SCHEDULED 30K CHECK, FLOORBOARD AT BS 160-200, LEFT BUTTOCK LINE 8, RIGHT BUTTOCK LINE 44 CORRODED. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M) 2 L 7 2 4F RT A6WE 2003012800218 20030128 00218 WP 2003 1 28 ASAA0280498 1 20021029 A 5321 SLS5128A3C FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING SCHEDULED 30K CHECK, FOUND FLOORBOARD AT BS 160-256, LEFT BUTTOCK LINE 22, LEFT BUTTOCK LINE 44 CORRO DED. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M) 2 L 7 2 4F RT A6WE 2003012800219 20030128 00219 WP 2003 1 28 ASAA0280499 1 20021029 A 5321 SLS5128A3C FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING SCHEDULED 30K CHECK, FOUND FLOORBOARD AT BS 200-256, LEFT BUTTOCK LINE 22, RIGHT BUTTOCK LINE 22 CORRODED. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M) 2 L 7 2 4F RT A6WE 2003012800220 20030128 00220 WP 2003 1 28 ASAA0280501 1 20021029 A 5321 SLS5128A3C FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING SCHEDULED 30K CHECK, FOUND FLOORBOARD AT BS 1307-1361, LEFT BUTTOCK LINE 18 CORRODED. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M) 2 L 7 2 4F RT A6WE 2003012800221 20030128 00221 WP 2003 1 28 ASAA0280502 1 20021029 A 5321 SLS5128A3C FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING SCHEDULED 30K-CHECK, FLOORBOARD AT BS 1117-1174, LEFT BUTTOCK LINE 6, LEFT BUTTOCK LINE 22 CORRODED. REMOV ED AND REPLACED FLOORBOARD PER MD80 SRM. (M) 2 L 7 2 4F RT A6WE 2003012800222 20030128 00222 WP 2003 1 28 ASAA0280503 1 20021029 A 5321 SLS5128A3C INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD AT STATION 1156-1250 LBL 22 TO LBL 44 HAS 29 CORRODED INSERTS. REMOVED AND REP LACED IAW SRM. (M) 2 L 7 2 4F RT A6WE 2003012800244 20030128 00244 NM 2003 1 28 AWXA200300057 1 20021229 A 5320 146N5318 PANEL BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 24523 LCQ - MAJOR REPAIR - DURING C-10 CHECK INTERGRANULAR CORROSION WAS FOUND ON PASSENGER CABIN SHEAR DECK AT BS 1716, BL 0 TO RT CUSP. MAINTENANCE BLENDED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA OF SHEAR DEC K; FABRICATED A REPAIR DOUBLER AND SHIMS; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-51, PG 205-208. 2 L 7 2 4F RT A2NM 2003012800249 20030128 00249 NM 2003 1 28 QXEA0201822 1 20021029 A 2720 CONNECTOR DHAV DHC8 DHC8202 2809007 NM RUDDER DIRTY A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 364PH 524 PDX- RETURNED TO FIELD DUE TO RUDDER PRESSURE, RUDDER FULL PRESSURE AND NR 1 RUDDER HYDRAULIC CAUTION LIGHTS ILLUMINATED AFTER TAKEOFF. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED, CLEANED AND RESECURED CANNON PLUGS FOR NR 1 & 2 RUDDER PR ESSURE REGULATOR SOLENOID VALVE AND NR 1 & 2 RUDDER ACTUATOR ISOLATION SOLENOID VALVE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003012800274 20030128 00274 WP 2003 1 28 ASAA0280506 1 20021029 A 5522 991848043 SKIN DOUG DC9 DC983 3022083 WP ELEVATOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, RIGHT ELEVATOR OUTBOARD LEADING EDGE GOUGED AT TIP MATING SURFACE. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A6WE 2003012900069 20030129 00069 NM 2003 1 29 QXEA0201893 1 20021107 A 5270 SENSOR BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR DIRTY A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 413QX 4060 GEG-ABOVE 19,000 FEET, FUSELAGE DOOR MASTER WARNING LIGHT COMES ON INTERMITTENTLY. DOORS PAGE ON MFD SHOWS AFT PASSENGER SERVICE DOOR ON CABIN SIDE AS PROBLEM DOOR. NO LOSS OF CABIN PRESSURE, OUTSIDE AIR TEMPERATURE -18C. INTERROGATED PSEU FOR FAULTS, AFT PASSENGER DOOR LOCK FAULT, PROXIMITY SENSOR CHECK GOOD. CHECKED WIRING, NO DEFECTS NOTED. CLEANED SENSOR S. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003012900070 20030129 00070 NM 2003 1 29 QXEA0201895 1 20021107 A 5220 GUSSET DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - RIGHT HAND FORWARD EMERGENCY EXIT DOOR HAS A CHAFE ALONG THE LOWER INBOARD BOTTOM GUSSET JUST AFT OF THE FORWARD L OWER DOOR STOP. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2003012900071 20030129 00071 NM 2003 1 29 QXEA0201896 1 20021104 A 3213 STRUT DHAV DHC8 DHC8202 2809007 NM RT MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - RIGHT HAND MAIN LANDING GEAR DRAG STRUT IS CHAFED IN TWO PLACED ABOVE LOWER ATTACH POINT. REPAIRED IAW DHC-8200 CM M 32-10-01, PAGES 668-669, PARAGRAPH 5. 2 H 7 2 4T RT A13NM 2003012900072 20030129 00072 NM 2003 1 29 2002UALA01896 1 20021226 A 2700 S209 SWITCH BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 676UA 30028 EICAS MESSAGE "LE SLAT ASSY" DISPLAYED AFTER TAKEOFF. DIVERTED INTO HNL. SUPPLEMENTAL DATA UPDATE REPLACED #9 OUTBOAR D SLAT PROXIMITY SWITCH S297. SYSTEM OPERATIONAL CHECK OK, NO ADDITIONAL OCCURENCES. 2 L 7 2 4F 4 F RT A1NM E24NE 2003012900074 20030129 00074 NM 2003 1 29 2003UALA00075 1 20021231 A 5754 114W210012 WEDGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE #8 WING SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 777UA 26916 TRAILING EDGE WEDGE DELAMINATED. WING SLAT #8. LEADING EDGE OF SKIN CRACKED 1". MAJOR REPAIR ACCOMPLISHED. CUT OUT C RACK AND REPLACED WEDGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2003012900078 20030129 00078 NM 2003 1 29 QXEA0201897 1 20021109 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - REAR FUSELAGE TOP SKIN HAS SHARP DENT ON RIGHT HAND SIDE OF REAR FUSELAGE TOP SKIN JUST FORWARD OF STATION X611.00 . REPAIRED IAW HORIZON AIR EA 2-53-449. 2 H 7 2 4T RT A13NM 2003012900079 20030129 00079 NM 2003 1 29 QXEA0201898 1 20021107 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - AFT ENGINE NACELLE FIREWALL IS CRACKED AT THE 2 O'CLOCK POSITION. REPAIRED IAW RD 8-54-611. 2 H 7 2 4T RT A13NM 2003012900083 20030129 00083 NM 2003 1 29 QXEA0201899 1 20021104 A 3210 YOKE DHAV DHC8 DHC8202 2809007 NM RT MLG GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - RIGHT HAND MAIN LANDING GEAR YOKE HAS GOUGE ON INBOARD VERTICAL MEMBER. REPAIRED IAW DHC-8200 MM 32-10-07, PAGES 668-669, PARAGRAPH 5. 2 H 7 2 4T RT A13NM 2003012900084 20030129 00084 NM 2003 1 29 QXEA0201913 1 20021104 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SEAT TRACK NR 5 HAS SURFACE CORROSION BETWEEN LOCATIONS X465 AND X473. REPAIRED IAW RD 8-53-1339 AND DHC-8 SRM 51 -20-36. 2 H 7 2 4T RT A13NM 2003012900086 20030129 00086 NM 2003 1 29 QXEA0201914 1 20021109 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - FRONT SPAR LOWER CAP HAS PAINT CHAFE AREA EXPOSING BARE METAL AT YW58.200. REPAIRED IAW RD 8-57-811 AND DHC-8 SRM 51-20-57 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2003012900087 20030129 00087 NM 2003 1 29 QXEA0201915 1 20021104 A 3213 STRUT DHAV DHC8 DHC8202 2809007 NM RT MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - RIGHT MAIN LANDING GEAR SHOCK STRUT CHAFED ON FORWARD SIDE APPROXIMATELY 6 INCHES BELOW LUG FOR BARREL NUT AND LOW ER END. REPAIRED IAW CHH 32-10-01, PAGES 668-669, PARAGRAPH 5. 2 H 7 2 4T RT A13NM 2003012900089 20030129 00089 NM 2003 1 29 QXEA0201916 1 20021107 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - CORROSION AROUND AIRSTAIR DOOR SILL NUT PLATE BETWEEN DOOR HINGE POINTS. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 5 1-40-11, PAGES 1-4. 2 H 7 2 4T RT A13NM 2003012900090 20030129 00090 NM 2003 1 29 QXEA0201917 1 20021107 A 5320 CLIP DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - CRACKED CLIP BELOW MAIN CABIN DOOR THRESHOLD AT STATION X242.2. REPAIRED IAW HORIZON AIR EA 2-53-448 AND DHC-8 SR M 51-40-11, PAGES 1-4. 2 H 7 2 4T RT A13NM 2003012900091 20030129 00091 NM 2003 1 29 QXEA0201918 1 20021106 A 1430 COLLAR DHAV DHC8 DHC8202 2809007 NM FLAP TRACK WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - LEFT HAND WING, NR 4 FLAP TRACK HAS SEVEN LOCKBOLT COLLARS WORN OFF ON UPPER SIDES. REPAIRED IAW DHC-8 RD 8-51-102 . 2 H 7 2 4T RT A13NM 2003012900093 20030129 00093 NM 2003 1 29 QXEA0201919 1 20021107 A 5532 SKIN DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SCRATCHES AND GOUGES EXIST IN APERTURE OV V-STAB UNDER PANEL 322HR. REPAIRED IAW DHC-8 200 SRM 51-20-36, PAGED 2, SECTION A, PARAGRAPH 6. 2 H 7 2 4T RT A13NM 2003012900094 20030129 00094 NM 2003 1 29 QXEA0201920 1 20021107 A 5532 SKIN DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - APERATURE HAS SCRATCHES ON V STAB UNDER PANEL 322GR. REPAIRED IAW DHC-8 200 SRM 51-20-36, PAGE 2, SECTION A, PARA GRAPH 6. 2 H 7 2 4T RT A13NM 2003012900095 20030129 00095 NM 2003 1 29 QXEA0201921 1 20021107 A 5532 SKIN DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - SCRATCHES AND GOUGES EXIST IN APERTURE V STAB UNDER PANEL 322DL. REPAIRED IAW DHC-8 200 SRM 51-20-36, PAGE 2, SECT ION A, PARAGRAPH 6. 2 H 7 2 4T RT A13NM 2003012900097 20030129 00097 NM 2003 1 29 QXEA0201922 1 20021109 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - PASSENGER DOOR UPPER AFT STOP GUIDE IS PITTED. REPAIRED IAW RD 8-53-3933. 2 H 7 2 4T RT A13NM 2003012900101 20030129 00101 NM 2003 1 29 QXEA0201923 1 20021109 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - PASSENGER DOOR UPPER FORWARD STOP GUIDE IS WORN WITH PITTING. REPAIRED IAW RD 8-53-3933. 2 H 7 2 4T RT A13NM 2003012900102 20030129 00102 NM 2003 1 29 QXEA0201924 1 20021108 A 5210 STOP FITTING DHAV DHC8 DHC8202 2809007 NM PAX DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - MAIN CABIN DOOR LOWER AFT STOP FITTING GOUGED. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 6, PARAGRAPH 4. 2 H 7 2 4T RT A13NM 2003012900103 20030129 00103 NM 2003 1 29 QXEA0201925 1 20021108 A 5750 ATTACH FITTING DHAV DHC8 DHC8202 2809007 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - RIGHT HAND OUTBOARD ROLL SPOILER CENTER ATTACH FITTING ON WING HAS DAMAGE. REPAIRED IAW DHC-8 SRM 51-40-00 AND SR M 51-40-11. 2 H 7 2 4T RT A13NM 2003012900104 20030129 00104 NM 2003 1 29 QXEA0201926 1 20021109 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - LIGHT CORROSION ON AIRCRAFT SKIN UNDER UPPER TRANSPONDER ANTENNA, BEHIND CREW ESCAPE HATCH AT APPROXIMATELY X259.4 . REPAIRED IAW DHC-8 SRM 53-00-16, PAGE 3, SRM 51-20-11 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003012900106 20030129 00106 NM 2003 1 29 QXEA0201927 1 20021104 A 2710 AILERON DHAV DHC8 DHC8202 2809007 NM LT WING OUT OF RIG A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - LEFT HAND AILERON WILL NOT MAKE PROPER UP TRAVEL. TENSIONED IAW DHC-8 200 MM 27-12-00, PARAGRAPH 3B, PAGE 503. RE PAIRED IAW HORIZON AIR EA 2-27-70. 2 H 7 2 4T RT A13NM 2003012900107 20030129 00107 NM 2003 1 29 QXEA0201928 1 20021103 A 7110 WEB BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - RIGHT HAND LOWER COWL AFT CONE SUPPORT WEB CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900109 20030129 00109 NM 2003 1 29 QXEA0201929 1 20021103 A 7110 WEB BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - LEFT HAND LOWER COWL AFT CONE SUPPORT WEB CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900110 20030129 00110 NM 2003 1 29 QXEA0201930 1 20021103 A 7110 ANGLE BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - LEFT HAND LOWER COWL ANGLE ON RIGHT HAND SIDE OB BYPASS DOOR CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900112 20030129 00112 NM 2003 1 29 QXEA0201933 1 20021112 A 5541 RIB BOMBDR DHC8 DHC8401 1390041 NM RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 PDX-RIB NR 30 ON TRAILING RUDDER HAS A 3.5 INCH CRACK ON UPPER LEFT HAND SIDE. REPAIRED IAW HORIZON AIR EA. 6-55-19. 2 H 7 2 4T RT A13NM 2003012900114 20030129 00114 EA 2003 1 29 QXEA0201935 1 20021113 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX- FORWARD CARGO SMOKE DETECTOR PROTECTIVE COVER CHIMNEY ASSEMBLY JUST INSIDE OF FORWARD CARGO BAY DOOR, PROTECTIVE GR ILL MESH DAMAGED. REMOVED AND REPLACED FORWARD CARGO SMOKE DETECTOR PROTECTIVE COVER CHIMNEY ASSEMBLY. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900116 20030129 00116 NM 2003 1 29 QXEA0201936 1 20021115 A 3320 BR63031023 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 352PH 494 PSC- PASSENGER REPORTED SMOKE IN SEAT 9A. REMOVED AND REPLACED LIGHT ASSEMBLY ON SIDEWALL LIGHT. OPERATIONAL CHECKS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003012900118 20030129 00118 NM 2003 1 29 QXEA0201937 1 20021112 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 414QX 4061 PDX- DAMAGE TO FUSELAGE SKIN BETWEEN STATIONS X722.102 AND X728.102 AND STRINGERS 24R AND 26R. REPAIRED IAW HORIZON AIR EA 6-53-78 "B", 6-53-140, AND Q400 RD 8/4-53-250. 2 H 7 2 4T RT A13NM 2003012900119 20030129 00119 NM 2003 1 29 QXEA0201938 1 20021112 A 7110 FRAME BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 414QX 4061 PDX- LEFT HAND LOWER COWL AFT CONE CENTER CENTER SUPPORT FRAME AND LOWER SUPPORT ANGLE ARE CRACKED. REPAIRED IAW Q400 RD 8/4-71-016 AND SRM 51-41-05. 2 H 7 2 4T RT A13NM 2003012900121 20030129 00121 NM 2003 1 29 QXEA0201939 1 20021112 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 414QX 4061 PDX- RIGHT HAND HORIZONTAL CHANNEL IS CRACKED IN RIGHT HAND LOWER COWL. REPAIRED IAW Q400 RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900122 20030129 00122 NM 2003 1 29 QXEA0201940 1 20021112 A 7110 FRAME BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 414QX 4061 PDX- AFT CONE CENTER SUPPORT FRAME IS CRACKED ON RIGHT HAND LOWER COWL. REPAIRED IAW Q400 RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900123 20030129 00123 NM 2003 1 29 QXEA0201942 1 20021112 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 414QX 4061 PDX- LEFT HAND HORIZONTAL CHANNEL IS CRACKED IN RIGHT HAND LOWER COWL. REPAIRED IAW Q400 RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900124 20030129 00124 NM 2003 1 29 QXEA0201943 1 20021112 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 414QX 4061 PDX- LEFT HAND VERTICAL CHANNEL IS CRACKED IN RIGHT HAND LOWER COWL. REPAIRED IAW Q400 RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900125 20030129 00125 NM 2003 1 29 QXEA0201944 1 20021112 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 414QX 4061 PDX- RIGHT HAND VERTICAL CHANNEL IS CRACKED IN THE RIGHT HAND LOWER COWL. REPAIRED IAW Q400 RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900126 20030129 00126 NM 2003 1 29 QXEA0201945 1 20021112 A 7110 SUPPORT ANGLE BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 414QX 4061 PDX- AFT CONE LOWER SUPPORT ANGLE IS CRACKED IN RIGHT HAND LOWER COWL. REPAIRED IAW Q400 RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900127 20030129 00127 NM 2003 1 29 QXEA0201946 1 20021116 A 7110 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM LT COWLING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 412QX 4059 PDX- LEFT HAND LOWER COWL REQUIRES REPAIR AS PER EA 6-71-26 "B". REPAIRED IAW HORIZON AIR EA 6-71-26 "B" AND Q400 RD 8/4 -71-006. 2 H 7 2 4T RT A13NM 2003012900130 20030129 00130 NM 2003 1 29 QXEA0201947 1 20021116 A 7110 FRAME BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 412QX 4059 PDX- AFT FACE FRAME IS CHAFED AT JUNCTIONS OF VERTICAL CHANNELS ON LEFT HAND LOWER COWL. REPAIRED IAW HORIZON AIR EA 6-7 1-70. 2 H 7 2 4T RT A13NM 2003012900131 20030129 00131 NM 2003 1 29 QXEA0201948 1 20021116 A 7110 ANGLE BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 412QX 4059 PDX- LEFT HAND AND RIGHT HAND UPPER "Z" MEMBERS ARE CRACKED IN THE LEFT HAND LOWER COWL. REPAIRED IAW Q400 RD 8/4-71-016 . 2 H 7 2 4T RT A13NM 2003012900132 20030129 00132 NM 2003 1 29 QXEA0201949 1 20021116 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 412QX 4059 PDX- LEFT HAND AND RIGHT HAND VERTICAL CHANNELS ARE CRACKED IN LEFT HAND LOWER COWL. REPAIRED IAW Q400 RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900133 20030129 00133 NM 2003 1 29 QXEA0201950 1 20021116 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 412QX 4059 PDX- LEFT HAND AND RIGHT HAND BYPASS DOOR OPENING SIDE CHANNELS ARE CRACKED IN LEFT HAND LOWER COWL. REPAIRED IAW Q400 R D 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900134 20030129 00134 NM 2003 1 29 QXEA0201951 1 20021116 A 7110 FRAME BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 412QX 4059 PDX- LEFT HAND LOWER COWL AFT CONE CENTER SUPPORT FRAME AND SUPPORT FRAME LOWER ANGLE ARE CRACKED. REPAIRED IAW Q400 RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900135 20030129 00135 EA 2003 1 29 QXEA0201952 1 20021115 A 2131 CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA CABIN PRESSURE MALFUNCTIONED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 610QX 10033 LAX - CREW RETURNED TO FIELD WHEN AFTER TAKEOFF THEY WERE UNABLE TO CONTROL PRESSURE IN EITHER AUTO OR MANUAL MODES. MA INTENANCE INSPECTED THE AIRCRAFT AND FOUND NO HISTORY IN THE MDC. MAINTENANCE PRESSURIZED THE AIRCRAFT TO APPROXIMATELY 4.5 PSI AND THERE WERE NO DISCREPANCIES NOTED. THE SYSTEM OPERATIONAL CHECK, AND OPERATIONAL CHECK FLIGHT, WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 L 7 2 4F RT A21EA 2003012900136 20030129 00136 NM 2003 1 29 QXEA0201953 1 20021117 A 3260 CONNECTOR BOMBDR DHC8 DHC8401 1390041 NM RT MLG LOOSE A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 410QX 4053 BLI - AFTER TAKEOFF, THE RIGHT GEAR INDICATED UNSAFE WITH THE DOOR OPEN. IT STAYED OPEN FOR 2 MINUTES AND THEN CLOSED ON ITS OWN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE CONNECTOR TO THE RIGHT UPLOCK SENSOR LOOSE. THE CONNECTOR WAS TIGHTENED AND OPERATIONAL CHECKS PERFORMED. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2003012900137 20030129 00137 EA 2003 1 29 QXEA0201954 1 20021118 A 2711 AL00102 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA AILERON FAILED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 614QX 945 10049 SEA - CREW ABORTED TAKEOFF WHEN THEY RECEIVED AN AILERON CONFIGURATION WARNING. MAINTENANCE INSPECTED THE AIRCRAFT AND R EPLACED THE AILERON TRIM ACTUATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900138 20030129 00138 NM 2003 1 29 QXEA0201955 1 20021118 A 2120 SMOKE DHAV DHC8 DHC8202 2809007 NM COCKPIT DETECTED A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 367PH 511 PDX - AIRCRAFT DIVERTED TO PDX WHEN THE CREW NOTICED SMOKE IN THE CABIN AND COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT, RAN BOTH ENGINES AT 70 PERCENT TORQUE FOR 30 MINUTES WITH BLEEDS ON AND DUCT TEMPERATURE BETWEEN 65-70 DEGREES. NO ABNO RMAL SMELLS WERE NOTED. AIR CYCLE MACHINE OIL LEVEL WAS GOOD. DO DEFECTS OR SMELLS. NO PARTS WERE REPLACED AND THE AIRCR AFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003012900139 20030129 00139 NM 2003 1 29 QXEA0201956 1 20021119 A 5420 ANGLE BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - AFT CONE WEB UPPER REPAIR ANGLE CRACKED ON LEFT HAND NACELLE. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900140 20030129 00140 NM 2003 1 29 QXEA0201957 1 20021118 A 5210 STOP FITTING BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - MAIN CABIN DOOR AFT SIDE STOP FITTING HAS CHAFE DAMAGE. REPAIRED IAW IPC 52-11-06, FIGURE 1, SHEET 1. 2 H 7 2 4T RT A13NM 2003012900141 20030129 00141 NM 2003 1 29 QXEA0201958 1 20021119 A 5330 PAINT BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CHIPPED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - FORWARD PASSENGER DOOR SURROUND HAS A 2 INCH LONG AREA OF PAINT CHIPPED OFF. REPAIRED IAW DHC-8 Q400 SRM 51-25-02 , PAGE 208, PARAGRAPH 5F AND SRM 51-25-15, PAGE 203, STEP 5, SUBTASK A-F. 2 H 7 2 4T RT A13NM 2003012900143 20030129 00143 NM 2003 1 29 QXEA0201959 1 20021118 A 5230 BRACKET BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - FORWARD CENTER CAM FOLLOWER GUIDE BRACKET CHAFED ON FORWARD CARGO DOOR SURROUND. REPAIRED IAW DHC-8 Q400 SRM 51-21 -10 AND SRM 51-25-10. 2 H 7 2 4T RT A13NM 2003012900144 20030129 00144 NM 2003 1 29 QXEA0201960 1 20021118 A 5230 BRACKET BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - FORWARD CARGO DOOR SURROUND, AFT CENTER CAM FOLLOWER GUIDE BRACKET IS CHAFED. REPAIRED IAW DHC-8 Q400 SRM 51-21-10 AND SRM 51-25-10. 2 H 7 2 4T RT A13NM 2003012900145 20030129 00145 NM 2003 1 29 QXEA0201961 1 20021119 A 5230 HINGE BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - GOUGE IN MAIN HINGE JUST BELOW LOCK LATCH MECHANISM ON FORWARD CARGO DOOR. REPAIRED IAW DHC-8 Q400 SRM 51-14-00, PAGE 221. 2 H 7 2 4T RT A13NM 2003012900146 20030129 00146 NM 2003 1 29 QXEA0201962 1 20021119 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - LEFT HAND LOWER COWL DEBRIS DOOR LEFT HAND APERTURE CHANNEL CRACKED IN AFT END. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900147 20030129 00147 NM 2003 1 29 QXEA0201963 1 20021119 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - LEFT HAND LOWER COWL DEBRIS DOOR RIGHT HAND APERTURE CHANNEL CRACKED AFT END. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900149 20030129 00149 NM 2003 1 29 QXEA0201964 1 20021119 A 7110 FITTING BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - ABOVE DEBRIS DOOR, LEFT HAND LOWER COWL RIGHT HAND UPPER Z MEMBER FORWARD CLEAT CRACKED. REPAIRED IAW RD 8/4-71-0 16. 2 H 7 2 4T RT A13NM 2003012900151 20030129 00151 NM 2003 1 29 QXEA0201965 1 20021119 A 7110 FITTING BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - ABOVE DEBRIS DOOR, RIGHT HAND LOWER COWL RIGHT HAND UPPER Z MEMBER FORWARD CLEAT CRACKED. REPAIRED IAW RD 8/7-71- 016-019. 2 H 7 2 4T RT A13NM 2003012900156 20030129 00156 NM 2003 1 29 QXEA0201966 1 20021119 A 7110 ANGLE BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - ABOVE DEBRIS DOOR, RIGHT HAND LOWER COWL RIGHT HAND UPPER Z MEMBER CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900157 20030129 00157 NM 2003 1 29 QXEA0201967 1 20021118 A 7110 ANGLE BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - RIGHT HAND LOWER COWL UPPER Z MEMBER CRACKED ABOVE DEBRIS DOOR. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900158 20030129 00158 NM 2003 1 29 QXEA0201968 1 20021119 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - RIGHT HAND LOWER COWL DEBRIS DOOR LEFT HAND APERTURE CHANNEL CRACKED AFT END. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900159 20030129 00159 NM 2003 1 29 QXEA0201969 1 20021118 A 7110 SUPPORT BRACKET BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - RIGHT HAND LOWER COWL CONE SUPPORT BRACKET UPPER AND LOWER ANGLES CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003012900161 20030129 00161 EA 2003 1 29 QXEA0201972 1 20020701 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA O OTHER K FLUID LOSS UK UNKNOWN 1 NM 09 603QX 1398 1398 10011 PDX- FUEL LEAKING FROM CENTER OF FUSELAGE NEAR WHEEL WELLS. FOUND FUEL FEED SWITCH LEAKING. REMOVED AND REPLACED ENGIN E FUEL FEED SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900162 20030129 00162 EA 2003 1 29 QXEA0201973 1 20021117 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA O OTHER K FLUID LOSS UK UNKNOWN 1 NM 09 604QX 2059 2059 10019 DEN-FUEL DRIPPING FROM CENTER FUSELAGE BETWEEN MAIN GEAR BAYS. REMOVED AND REPLACED ENGINE FUEL FEED SWITCH. OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900163 20030129 00163 EA 2003 1 29 QXEA0201974 1 20021106 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA O OTHER K FLUID LOSS UK UNKNOWN 1 NM 09 600QX 2259 2259 10005 BOI-FUEL LEAK AT CENTER SECTION. REMOVED AND REPLACED ENGINE FUEL FEED SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900164 20030129 00164 EA 2003 1 29 QXEA0201975 1 20020830 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA O OTHER K FLUID LOSS UK UNKNOWN 1 NM 09 604QX 1560 1560 10019 BOI- FUEL DRIPPING FROM CENTER WING SECTION. FOUND FUEL FEED LEAKING. REMOVED AND REPLACED ENGINE FUEL FEED SWITCH. O PERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900165 20030129 00165 EA 2003 1 29 QXEA0201976 1 20020109 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 602QX 448 10010 BOI - DURING PREFLIGHT, CREW FOUND FUEL LEAK FROM CENTER FUSELAGE AREA NEAR WING LEADING EDGE. MAINTENANCE REPLACED THE EJECTOR PUMP PRESSURE SWITCH. OPERATIONAL AND LEAK CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900166 20030129 00166 EA 2003 1 29 QXEA0201977 1 20020329 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA O OTHER K FLUID LOSS UK UNKNOWN 1 NM 09 609QX 747 10031 BOI - FUEL DRIPPING FROM FUSELAGE BETWEEN LANDING GEAR. MAINTENANCE REPLACED THE RIGHT PRIMARY EJECTOR SENSOR. OPERATI ONAL AND LEAK CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900167 20030129 00167 EA 2003 1 29 QXEA0201978 1 20020402 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 610QX 367 10033 PDX - AIRCRAFT LEAKS FUEL AT CENTER FUSELAGE BETWEEN THE WINGS. MAINTENANCE REPLACED THE LEFT PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900168 20030129 00168 NM 2003 1 29 QXEA0201979 1 20021120 A 2612 3039875 FIRE LOOP DHAV DHC8 DHC8202 2809007 NM NR 1 ENGINE MALFUNCTIONED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 348PH 484 SEA- NR 1 ENGINE LOOP FAULT B IS ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE FIRE LOOP B. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003012900169 20030129 00169 EA 2003 1 29 QXEA0201980 1 20020417 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 608QX 991 10026 MFR - FUEL LEAKING FROM CENTER FUSELAGE FORWARD WING AREA. MAINTENANCE REPLACED THE PRIMARY EJECTOR PRESSURE SENSOR. O PERATIONAL AND LEAKS CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900170 20030129 00170 EA 2003 1 29 QXEA0201981 1 20020520 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 601QX 1538 21 10009 GEG - AIRCRAFT LEAKING FUEL ON FORWARD BELLY AREA. MAINTENANCE REPLACED THE LEFT PRIMARY EJECTOR PRESSURE SENSOR. OPER ATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900171 20030129 00171 EA 2003 1 29 QXEA0201982 1 20020613 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA O OTHER K FLUID LOSS UK UNKNOWN 1 NM 09 606QX 1582 10023 BOI - CREW REPORTS FUEL LEAK UNDER THE BELLY OF THE AIRCRAFT. MAINTENANCE INSPECTED AND REPLACED THE LEFT PRIMARY EJECT OR PRESSURE SENSOR. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900172 20030129 00172 EA 2003 1 29 QXEA0201983 1 20020728 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA O OTHER K FLUID LOSS UK UNKNOWN 1 NM 09 605QX 1408 10022 SEA - CREW REPORTS FUEL LEAK AT CENTER FUSELAGE. MAINTENANCE REPLACED THE PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900173 20030129 00173 EA 2003 1 29 QXEA0201984 1 20020901 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 608QX 1944 10026 PDX - CREW REPORTS FUEL LEAK AT CENTER FUEL TANK DURING PREFLIGHT. MAINTENANCE INSPECTED AND REPLACED THE LEFT PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900174 20030129 00174 EA 2003 1 29 QXEA0201985 1 20020904 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA O OTHER K FLUID LOSS CR CRUISE 1 NM 09 603QX 1180 1180 10011 BOI - CREW REPORTS BOOST PUMPS CYCLED FOR 40 MINUTES WHILE AT FLIGHT LEVEL 390. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 2 4F RT A21EA 2003012900175 20030129 00175 EA 2003 1 29 QXEA0201986 1 20021123 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 612QX 2649 2649 10042 BOI - FUEL LEAK NOTED IN FRONT OF LEFT WHEEL WELL. MAINTENANCE INSPECTED AND REPLACED THE ENGINE FUEL FEED SWITCH. OPE RATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900176 20030129 00176 EA 2003 1 29 QXEA0201987 1 20021124 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 613QX 2836 2836 10045 BOI - FUEL WAS NOTED LEAKING FROM LEFT WHEEL BIN. MAINTENANCE REPLACED THE ENGINE FUEL FEED SWITCH. OPERATIONAL AND LE AK CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900177 20030129 00177 NM 2003 1 29 QXEA0201988 1 20021122 A 3260 858601 PSEU DHAV DHC8 DHC8202 2809007 NM LANDING GEAR MALFUNCTIONED A QXEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 09 366PH 9352 8564 510 PDX- ON APPROACH TO LANDING IN PDX LANDING GEAR INDICATED ONLY RED LIGHTS. ATTEMPTED TO EXTEND GEAR THREE MORE TIMES WI THOUT SUCCESS. PERFORMED ALTERNATE GEAR EXTENSION ON FOURTH ATTEMPT AND RECEIVED THREE GREEN AND THREE AMBER GEAR DOOR LIGHTS. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PSEU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2003012900178 20030129 00178 EA 2003 1 29 QXEA0201990 1 20021125 A 5240 ACCESS DOOR CNDAIR CL600 CL6002C10 1390015 EA COMMUNICATION OPEN A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 604QX 10019 BOI- RETURNED TO FIELD DUE TO EXTREMELY LOUD SQUEAL AFTER TAKEOFF. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND COMMUNICATI ONS DOOR OPEN. CLOSED DOOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900186 20030129 00186 NM 2003 1 29 ASAA0210268 1 20021030 A 5514 655480011 RETAINER BOEING 737 737210C 1384459 NM VERTICAL STAB CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND VERTICAL STABILIZER ACCESS PANEL SEAL DEPRESSOR AT VERTICAL STABILIZER STATION 56. 57 CRACKED. REMOVED AND REPLACED SEAL DEPRESSOR PER SRM AND MANUFACTURER DRAWING. (M) 2 L 7 2 4F A16WE 2003012900187 20030129 00187 NM 2003 1 29 ASAA0210271 1 20021031 A 5311 6546570 FRAME BOEING 737 737210C 1384459 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 1103, RIGHT BUTTOCK LINE 28 CHAFED. REMOVED DAMAGE AND REPAIRED PER S RM. (M) 2 L 7 2 4F A16WE 2003012900188 20030129 00188 NM 2003 1 29 ASAA0210272 1 20021101 A 5320 SILL BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND MAIN CARGO DOOR SILL WEB AT BS 470-485, LEFT BUTTOCK LINE 66 CORRODED. REPAIRED C ARGO DOOR SILL WEB PER SRM. (M) 2 L 7 2 4F A16WE 2003012900189 20030129 00189 NM 2003 1 29 ASAA0210273 1 20021101 A 5311 FRAME BOEING 737 737210C 1384459 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 1095, RIGHT BUTTOCK LINE 28 CHAFED. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F A16WE 2003012900190 20030129 00190 NM 2003 1 29 ASAA0210274 1 20021103 A 5320 SUPPORT ANGLE BOEING 737 737210C 1384459 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND SUPPORT ANGLE AT BS 540, LEFT BUTTOCK LINE 39 CRACKED. REMOVED AND REPLACED SUPPO RT ANGLE PER SRM. (M) 2 L 7 2 4F A16WE 2003012900191 20030129 00191 NM 2003 1 29 ASAA0210275 1 20021103 A 5347 BAC15201432 SEAT TRACK BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND SEAT TRACK AT BS 827, LEFT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED SEAT TR ACK PER SRM. (M) 2 L 7 2 4F A16WE 2003012900192 20030129 00192 NM 2003 1 29 ASAA0210276 1 20021104 A 5210 507945178 DOOR BOEING 737 737290C 138448V NM L1 OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 52501 23136 ANC - FLIGHT CREW REPORTED L1 DOOR HAD TO OPERATE INTO CLOSED POSITION. ADJUSTED L1 DOOR PER MANUFACTURERS MM, THEN OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 2003012900193 20030129 00193 NM 2003 1 29 ASAA0210277 1 20021104 A 5230 65622192 SUPPORT FITTING BOEING 737 737290C 138448V NM CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING INSPECTION, FOUND MAIN CARGO DOOR BELLCRANK SUPPORT FITTING AT BS 486, LEFT BUTTOCK LINE 15 CRACKED. REMOV ED AND REPLACED MAIN CARGO DOOR BELLCRANK SUPPORT FITTING PER SRM AND BOEING DRAWINGS. (M) 2 L 7 2 4F A16WE 2003012900194 20030129 00194 NM 2003 1 29 ASAA0210278 1 20021104 A 5347 BAC15201432 SEAT TRACK BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND SEAT TRACK AT BS 863, LEFT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED SEAT TR ACK PER SRM. (M) 2 L 7 2 4F A16WE 2003012900195 20030129 00195 NM 2003 1 29 ASAA0210279 1 20021104 A 5347 BAC15201432 SEAT TRACK BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND SEAT TRACK AT BS 864, LEFT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED SEAT TR ACK PER SRM. (M) 2 L 7 2 4F A16WE 2003012900196 20030129 00196 NM 2003 1 29 ASAA0240184 1 20021113 A 5320 6547690 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 PAE - DURING SI CHECK, FOUND CORROSION ON FLOOR TO SIDE WALL SUPPORTS AT BS 727E TO 818 AND 727 TO 767 AND 927 TO 947, A ND LEFT/RIGHT BL 20 AND FROM WL 156 TO 175. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012900197 20030129 00197 NM 2003 1 29 ASAA0240185 1 20021113 A 5320 6545807 STIFFENER BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 DURING SI CHECK, FOUND CRACKED SKIN STIFFENERS AT BS 291 AND STRINGERS 9R, 10R AND 12R. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012900198 20030129 00198 NM 2003 1 29 ASAA0240186 1 20021113 A 5100 65596598 FLANGE BOEING 737 7374Q8 138447Q NM CARGO DOOR CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 784AS 28199 PAE - DURING SI CHECK, FOUND CORROSION ON UPPER FLANGE AT BS 492, RBL 24 AND WL 156 FWD CARGO DOOR. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012900199 20030129 00199 NM 2003 1 29 ASAA0240187 1 20021113 A 5320 69434961 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 DURING SI CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012900200 20030129 00200 NM 2003 1 29 ASAA0240188 1 20021113 A 5311 6558280 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 DURING SI CHECK, FOUND CRACKED FRAME AT BS 360 FROM STRINGER 7 TO STRINGER 8. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012900201 20030129 00201 NM 2003 1 29 ASAA0240189 1 20021113 A 5311 65C33509 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 DURING SI CHECK, FOUND CRACKED FRAME AT BS 400 AT STRINGER 7R AND 8R. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003012900202 20030129 00202 WP 2003 1 29 ASAA0280504 1 20021029 A 5321 SLS5128A3C INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD AT STATION 200-256 RBL 22 TO RBL 44 HAS 18 CORRODED INSERTS. REMOVED AND REPLA CED IAW SRM. (M) 2 L 7 2 4F RT A6WE 2003012900203 20030129 00203 WP 2003 1 29 ASAA0280505 1 20021029 A 5313 59360531 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, LONGERON 30 CORRODED AT STATION 588. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A6WE 2003012900204 20030129 00204 WP 2003 1 29 ASAA0280507 1 20021029 A 5330 59366673 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, DENT IN FUSELAGE SKIN AT STATION 1150 BETWEEN LONGERON 26R-27R. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A6WE 2003012900205 20030129 00205 WP 2003 1 29 ASAA0280508 1 20021029 A 5330 591142837 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, DENT IN FUSELAGE SKIN AT STATION 1340 LONGERON 19R. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A6WE 2003012900206 20030129 00206 WP 2003 1 29 ASAA0280509 1 20021029 A 5730 59375511 SKIN DOUG DC9 DC983 3022083 WP LT WING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, LEFT WIND LEADING EDGE UPPER SURFACE GOUGED AT STATION XFS 624. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A6WE 2003012900207 20030129 00207 WP 2003 1 29 ASAA0280511 1 20021029 A 5347 SR00301147003 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, SEAT TRACK AT RBL 44 AND STATION 287 IS CORRODED. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A6WE 2003012900208 20030129 00208 WP 2003 1 29 ASAA0280512 1 20021029 A 5347 SR0955301157001 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, SEAT TRACK AT STATION 1229 AND LBL 22 IS CORRODED. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A6WE 2003012900209 20030129 00209 WP 2003 1 29 ASAA0280521 1 20021106 A 5347 SR00301157003 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, SEAT TRACK IS CORRODED AT FS 237. REPLACED SEAT TRACK PER SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2003012900210 20030129 00210 2003 1 29 ASAA0280622 4 20021204 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DETACHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 SJC - DURING PREFLIGHT CHECK, L2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2003012900211 20030129 00211 2003 1 29 ASAA0280623 4 20021208 A 2565 3961896501 LANYARD DOUG MD80 MD83 3023681 NM EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 982AS 53473 SEA - DURING PREFLIGHT CHECK, LANYARD BETWEEN GIRT BAR AND SLIDE COVER WAS FOUND DISCONNECTED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT 2003012900212 20030129 00212 WP 2003 1 29 ASAA0280652 1 20021210 A 5230 4920233503N STOP FITTING DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FORWARD CARGO BAY DOOR ADJUSTMENT SCREW STOP PLATE FITTING IS CRACKED JUST ABOVE DOOR SWIT CH TARGET. REPLACED STOP PLATE FITTING PER SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003012900213 20030129 00213 WP 2003 1 29 ASAA0280653 1 20021210 A 5753 5935920 RUB STRIP DOUG DC9 DC983 3022083 WP T/E FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, RIGHT WING FLAP FLEX JOINT RUB STRIP IS GOUGED IN 3 AREAS. REPLACED FLAP FLEX JOINT FAIRI NG PER 51-10-2, 51-10-4, 51-30-2 AND DAC DWG 5935920. (M) 2 L 7 2 4F RT A6WE 2003012900214 20030129 00214 WP 2003 1 29 ASAA0280654 1 20021210 A 5320 592600317 ROD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY BARRIER DOOR FORWARD HOLD UP ROD IS CRACKED. REPLACED HOLD-UP ROD PER SRM 5 1-30-2. (M) 2 L 7 2 4F RT A6WE 2003012900215 20030129 00215 EA 2003 1 29 QXEA0201991 1 20021122 A 2740 13740002 SWITCH CNDAIR CL600 CL6002C10 1390015 EA HORIZ STAB FAULTY A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 600QX 10005 BOI- RETURNED TO FIELD DUE TO STABILIZER TRIM, MACH TRIM CAUTION MESSAGES INFLIGHT. STABILIZER AND MACH TRIM WOULD NOT RESET. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED STABILIZER 1 ENGAGE SWITCH. OPERATIONAL CHECKS GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003012900216 20030129 00216 NM 2003 1 29 QXEA0201992 1 20021123 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - A DENT EXISTS IN THE SKIN ABOVE AND AFT OF LEFT HAND ICE SHIELD. REPAIRED IAW HORIZON AIR EA 6-53-143. 2 H 7 2 4T RT A13NM 2003012900217 20030129 00217 NM 2003 1 29 QXEA0201993 1 20021123 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - A DENT EXISTS IN SKIN ABOVE WINDOW L12 ADJACENT TO STRINGER 5, STATION X287. REPAIRED IAW HORIZON AIE EA 6-53-143 . 2 H 7 2 4T RT A13NM 2003013000002 20030130 00002 EU 2003 1 30 AUS20021365 1 20021126 A 7712 310823801 SENSOR FOKKER F27 F27MK50 EU PWA PWA120 PW125B NE ROTOL R352 R3526123F1 GL ENGINE TORQUE FAULTY W C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 AU S 514 (AUS) RT ENGINE TORQUE SENSOR SUSPECT FAULTY. 2 H 7 2 4T 4 T RT A817 E20NE 6 C P16NG 2003013000003 20030130 00003 SW 2003 1 30 AUS20021366 1 20021127 A 2910 27810322755 LINE SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UA 01514 WP MCAULY 4HFR34 4HFR34C663 NE HYD SYSTEM CRACKED W O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AU S (AUS) HYDRAULIC LINE CRACKED AT FLARE. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2003013000004 20030130 00004 EU 2003 1 30 AUS20021370 1 20021130 A 3243 210014 VALVE BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE PARK BRAKE FAULTY W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) PARK BRAKE VALVE FAULTY. 2 H 7 4 4F 4 F A49EU E6NE 2003013000005 20030130 00005 GL 2003 1 30 AUS20021372 3 20021130 A 6114 D22013 HUB PIPER PA28 PA28R180 7102809 SO LYC O360 IO360B1E 41514 EA HARTZL HCC2Y HCC2YK1 GL PROPELLER DAMAGED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 AU S (AUS) PROPELLER HUB PRELOAD SHELF MACHINED OR ALTERED. SUSPECT PROPELLER HAD SUFFERED A STRIKE IN THE PAST. UNAPPROVED R EPAIR / MODIFICATION. PERSONNEL / MAINTENANCE ERROR. 1 L 7 1 3O 3 O 2A13 1E10 5 C P920 2003013000006 20030130 00006 EA 2003 1 30 AUS20021375 2 20021128 A 7414 IO382584 CONTACTOR ROBSIN R44 R44 7640120 WP LYC O540 O540F1B5 41532 EA MAGNETO DAMAGED W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 AU S (AUS) LT MAGNETO CONTACTS PITTED AND POINTS CLOSED. 1 G 7 1 3O 3 O H11NM E295 2003013000007 20030130 00007 CE 2003 1 30 AUS20021376 1 20021106 A 2133 47061RX VALVE CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP HARTZL HCB3T HCB3TN5 GL PRESSURE REGULAT FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 AU S (AUS) EMERGENCY PRESSURISATION VALVE FAILED. 1 L 7 2 3T 4 T RT A28CE E4WE 6 C P15EA 2003013000008 20030130 00008 WP 2003 1 30 AUS20021381 2 20021128 A 7200 ENGINE SWRNGN SA227 SA227* SW GARRTT TPE331 TPE33112UHR WP MCAULY 4HFR34 4HFR34C652 NE NR 1 LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 AU S (AUS) NR 1 ENGINE OIL LEAK FROM PROPELLER AREA. OIL FUMES IN CABIN. INVESTIGATION COULD NOT FIND THE SOURCE OF THE LEAK AGE AND AFTER CLEANING OF THE AREA NO FURTHER OIL LEAKS WERE EVIDENT. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C 3PNE 2003013000009 20030130 00009 SO 2003 1 30 AUS20021383 1 20021027 A 3222 TBR198202 BEARING EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14SF 14SF9 NE NLG FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NOSE LANDING GEAR STRUT LOWER BEARING FAILED. DELRIN' INNER LINER DISLODGED DUE TO ADHESIVE FAILURE. 2 L 7 2 4T 4 T RT A31SO E20NE 6 N P11NE 2003013000010 20030130 00010 NM 2003 1 30 AUS20021390 1 20021204 A 7930 QA07656ISS1 TRANSMITTER BOEING 737 7377BX 13844D2 NM GE CFM56 CFM567B24 NE ENG OIL INDICATO MALFUNCTIONED W D RETURN TO BLOCK E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 AU S (AUS) NR1 ENGINE OIL FILTER BYPASS LIGHT TRANSMITTER FAULTY. 2 L 7 2 4F 4 F RT A16WE E00055EN 2003013000011 20030130 00011 EU 2003 1 30 AUS20021395 1 20021206 A 3230 SA7670006122 HOSE BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG BURST W C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 AU S (AUS) RT MAIN LANDING GEAR RETRACTION HOSE BURST. LOSS OF GREEN SYSTEM HYDRAULIC FLUID. 2 H 7 4 4F 4 F A49EU E6NE 2003013000012 20030130 00012 EU 2003 1 30 AUS20021399 1 20020925 A 2434 5243212137 DRIVE SHAFT PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL DC GENERATOR FAILED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 AU S (AUS) NR 2 GENERATOR DRIVESHAFT FAILED. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2003013000013 20030130 00013 EU 2003 1 30 AUS20021401 1 20021204 A 5610 366A25004204 WINDSHIELD AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1C 60030 NE COCKPIT BIRD STRIKE W O OTHER C F.O.D. CR CRUISE 1 AU S 1021 (AUS) LT WINDSHIELD STRUCK BY SEAGULL IN THE LOWER RIGHT CORNER. WINDSHIELD CRACKED. 1 G 7 2 3U 3 U RT H10EU E19EU 2003013000015 20030130 00015 SO 2003 1 30 AUS20021409 1 20021202 A 5741 9771200 FITTING PIPER PA36 PA36285 7103610 SO LYC O720 IO720A1B 41546 EA LT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) LT WING ATTACHMENT FITTING CRACKED. 1 L 7 1 3O 3 O A10SO 1E15 2003013000016 20030130 00016 EU 2003 1 30 AUS20021410 1 20021209 A 5330 L109 SKIN BAC 146 146100A 1500260 EU LYC ALF502 ALF502R3A 41580 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FUSELAGE SKIN CRACKED IN AREA BETWEEN STRINGERS NR 12 AND 13 LOCATED IMMEDIATELY AFT OF FRAME 29, BENEATH THE WING ROOT DOUBLER ON THE LT SIDE. FOUND DURING INSPECTION IAW AD/BAE146/70. 2 H 7 4 4F 4 F RT A49EU E6NE 2003013000017 20030130 00017 NM 2003 1 30 AUS20021411 1 20021210 A 5415 BACB30LM8D94 BOLT BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE NACELLE/PYLON CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 1 STRUT FUSE PIN SECONDARY RETENTION BOLT SHOWED EVIDENCE OFCORROSION UNDER THE HEAD. FOUND DURING INSPECTION I AW AD/B747/85. 2 L 7 4 4F 4 F RT A20WE E30NE 2003013000018 20030130 00018 SO 2003 1 30 AUS20021414 1 20021120 A 2910 12039236003 PIPE EMB 120 EMB120 3260201 SO PWA 118 PW118A NE HAMSTD 14RF 14RF9 NE HYD SYSTEM CHAFED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT HYDRAULIC RESERVOIR RETURN LINE LOCATED IN THE RT NACELLE/FLAP BAY WAS FOUND CHAFED THROUGH BY AN ADJACENT ELEC TRICAL LOOM PROTECTIVE CONDUIT. PERSONNEL/MAINTENANCE ERROR. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2003013000022 20030130 00022 NM 2003 1 30 AUS20021428 1 20021216 A 5230 FRAME BOEING 737 737377 NM CFMINT CFM56 CFM563B1US GL CARGO DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FORWARD CARGO DOOR CRACKED IN TWO PLACES. ONE CRACK WAS LOCATED IN THE FORWARD FRAME RADIUS IN LINE WITH THE LOWER FITTING PROPAGATING UPWARDS. THE OTHER CRACK WAS FOUND IN THE AFT FRAME IN THE SAME POSITION. CRACK LENGTH 38.1MM (1.5I N). FOUND DURING INSPECTION IAW SB 737-52A1100. 2 L 7 2 4F 4 F RT A16WE E2GL 2003013000023 20030130 00023 NM 2003 1 30 AUS20021433 1 20021216 A 5312 BS1016 BULKHEAD BOEING 737 737377 NM FUSELAGE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) REAR PRESSURE BULKHEAD DAMAGED ON LT SIDE. A GOUGE WAS FOUND ON A LAP JOINT OF A WEB DOME CLOSE TO S-15L. 2 L 7 2 4F RT A16WE 2003013000024 20030130 00024 EA 2003 1 30 AUS20021441 2 20021211 A 8550 SEAL PIPER PA28 PA28140 7102802 SO LYC O320 O320E2A 41508 EA ENGINE OIL FAILED W K NONE K FLUID LOSS IN INSP/MAINT 1 AU S (AUS) REMOTE OIL FILTER ADAPTER SEAL FAILED. LOSS OF ENGINE OIL. FILTER IS MOUNTED ON FIREWALL. 1 L 7 1 3O 3 O 2A13 E274 2003013000025 20030130 00025 NM 2003 1 30 AUS20021444 1 20021218 A 2822 6098976 PUMP BOEING 747 747438 NM RROYCE RB211 RB211524G19 NE FUEL BOOST FAILED W K NONE L NO TEST IN INSP/MAINT 1 AU S (AUS) NR 2 FORWARD BOOST PUMP FAILED INSULATION RESISTANCE TEST BETWEEN PIN 4 AND PIN 1, PIN 2 AND PIN 3. FOUND DURING I NSPECTION IAW AD/B747/280. 2 L 7 4 4F 4 F RT A20WE E30NE 2003013000027 20030130 00027 NE 2003 1 30 CA021126003 2 20021112 A 7200 ENGINE CNDAIR CL601 CL6013A 8070802 EA GE CF34 CF343A 30015 NE LEFT FLAMED OUT W B EMER. DESCENT X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 CA (CAN) WHILE IN LEVEL CRUISE FLIGHT AT FL410, THE AIRCRAFT WAS STRUCK BY LIGHTNING. THE LT ENGINE FLAMED OUT AND THE WX R ADAR BECAME INOPERATIVE. THE CREW DECENDED TO FL210 AND PERFORMED A SUCCESSFUL WIND MILL ENGINE START. THE AIRCRAFT THEN CLIMBED BACK UP TO FL410 AND CONTINUED ON TO IT'S SCHEDULED DESTINATION. AFTER A GROUND INSPECTION OF THE AIRFRAME AND COCKPIT CHECKS BY THE CREW, THE AIRCRAFT WASFLOWN TO A SERVICE FACILITY FOR A COMPLETE LIGHTNING STRIKE INSPECTION. 2 L 7 2 4F 4 F RT A21EA E15NE 2003013000028 20030130 00028 SW 2003 1 30 CA021129002 1 20021108 A 6230 5161A SPRING BELL 427 427 1182207 SW GREASE FITTING MISMANUFACTURED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) WHEN GREASING THE OUTER SWASHPLATE CAP ASSY. IT WAS NOTED THAT THE LUBRIFICATION FITTING WOULD JAM OCCASIONALLY, P REVENTING GREASE ENTERING THE CAP ASSY. AT THE NEXT ATTEMP THE GREASE WAS FREE TO ENTER THE CAP ASSY, THERE WAS NO RESTR ICTION. AFTER INVESTIGATION THE BALL AND SPRING OF LUBRIFICATION FITTING WERE FOUND INSIDE THE CAP ASSY. FOUND THE SPRIN G TO BE MISMANUFACTURED IN RESPECT TO THE SPEC PICTORIAL (CYLINDRICAL SHAPE INSTEAD OF CONE SHAPE.) 1 G 7 1 3U R00001RC 2003013000029 20030130 00029 SW 2003 1 30 CA021209002 1 20021204 A 6120 HCB3TN5G ROD END SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP HARTZL HCB3T HCB3TN5 GL PROP CONTROL FAILED W E ENGINE SHUTDOWN R M J PARTIAL RPM/PWR LOSS OVER TEMP WARNING INDICATION DE DESCENT 1 CA (CAN) ON APPROACH, PILOT'S NOTICED RPM ON LT ENGINE DECAY DOWN TO 93 PERCENT AND THE ITT WENT UP CLOSE TO THE RED LINE. BRINGING THE POWER LEVER BACK MADE NO DIFFERENCE TO THESE CONDITION SO THE ENGINE WAS FEATHERED AND SHUTDOWN WITH AN UNE VENTFUL LANDING. IT WAS FOUND THAT THE CONTROL ROD TO THE PROPELLER CONTROL HAD DISCONNECTED FROM THE VERTICAL TOWER SHA FT. UPON FURTHER INVESTIGATION IT WAS FOUND THAT THE INTERNAL THREADS OF THE ROD END HAD FAILED AND STRIPPED OUT. THE TH READS ON THE PUSH PULL ROD HAD NO DAMAGE. A NEW ROD END WAS INSTALLED AND RUN UPS CARRIED OUT AND THE AIRCRAFT WAS RETUR NED TO SERVICE. AIRCRAFT TOTAL TIME 19571.7 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P15EA 2003013000035 20030130 00035 NM 2003 1 30 CA021211005 1 20021205 A 3246 3006191 WHEEL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE WHEEL HALF WAS ON ITS 39TH BUILD, IT WAS INSTALLED ON AIRCRAFT 803, 24 NOV 2002 AND REMOVED BECAUSE OF A LOW T IRE PRESSURE PROBLEM ON THE 28 NOV 2002. IT HAD BEEN PREVIOUSLY REMOVED FROM AIRCRAFT 892 ON THE 11 NOV 2002 FOR A SIMIL AR PROBLEM. IT HAD GONE THROUGH THE NDT INSPECTION PROCESS WITH NO FAULTS NOTED. IT WENT BACK TO THE NDT SHOP AFTER TEAR DOWN, WHERE IT WAS NOTED THAT IT HAD A CRACK EMANATING FROM A BOLT HOLE INBOARD TO THE SEAL FLANGE. THIS HAS BEEN THE FI RST OCCURRENCE OF THIS NATURE WITH THESE WHEELS SEEN BY THE TECHNICIANS IN THE WHEEL AND BRAKE SHOP.THE WHEEL HALF WAS S CRAPPED AND IS BEING SENT FOR INSPECTION AND ANALYSES AFTER WHICH WE WILL GET A FULL REPORT OF THE PROBLEM. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003013000036 20030130 00036 NM 2003 1 30 CA021211006 1 20021130 A 3397 3200562 SPLICE DHAV DHC8 DHC8301 1386003 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE PSU BURNED W K NONE O OTHER IN INSP/MAINT 1 CA 28909 (CAN) WHILE COMPLETING FLEET CAMPAIGN H126 FOR PSU WIRING INSPECTION, MX FOUND EVIDENCE OF OVERHEATING AND CORROSION ON SEVERAL OF THE SUBJECT WIRE SPLICES. DAMAGE PRESENT AT BOTH LT AND RT SIDE PSU DISTRIBUTION WIRING FOR CABIN READING LIG HTS. SPLICES 3320E69, 3320E52, 3320E38, 3320E22 REPLACED. WIRES 33242G142 ON RT SIDE AND 33241L142 (LT SIDE) WERE HEAT D AMAGED AT SPLICES, AND TEMP REPAIR CARRIED OUT DUE TO LACK OF REPLACEMENT WIRE. WC 1170 WAS RAISED TO CARRY OUT PERMANEN T REPAIR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003013000037 20030130 00037 EA 2003 1 30 CA021211007 1 20021129 A 3397 320562 SPLICE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE PSU LIGHTS BURNED W K NONE O OTHER IN INSP/MAINT 1 CA 26271 (CAN) WHILE COMPLETING FLEET CAMPAIGN H126 FOR PSU WIRING INSPECTION, MX FOUND EVIDENCE OF OVERHEATING AT TWO SPLICES ON THE YELLOW & BROWN WIRES ADJACENT TO 3320P29 AND 3320P45. RE WM 332012 AND 332401. BOTH SPLICES REPLACED. SPLICE DESIGN ATORS NOT DETERMINED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003013000038 20030130 00038 SW 2003 1 30 CA021212004 1 20021212 A 5532 410008173 SKIN GULSTM 690TP 690A 0141722 SW GARRTT TPE331 TPE3315251K NM VERTICAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE ACCOMPLISHING AN INSPECTION 2 CRACKS WERE NOTED EMANATING FROM A FASTENER HOLE IN THE VERTICAL STAB SKIN. TH E CRACKS WERE 5/16 INCH AND 3/16 INCH IN LENGTH. THE CRACKS WERE LOCATED AT WL 25.1, 4 FASTENERS ABOVE THE SB 218 KIT DO UBLER (REF AD95-13-02 WHICH WAS PREVIOUSLY INSTALLED. THE AIRCRAFT WILL BE REPAIRED PRIOR TO BEING RETURNED TO SERVICE. THE OTHER 690A'S IN THE FLEET WERE INSPECTED WITH NO DEFECTS NOTED. 1 H 7 2 3T 4 T 2A4 E2WE 2003013000039 20030130 00039 NM 2003 1 30 CA021213006 1 20021128 A 3246 83210001077 TIRE DHAV DHC8 DHC8201 2809001 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF7 NE RT MLG FAILED W O OTHER D J INFLIGHT SEPARATION WARNING INDICATION AP APPROACH 1 CA 12275 (CAN) FLIGHT CREW HAD REPORTED HEARING A 'LOUD BANG' DURING THE CLIMB, SHORTLY AFTER TAKE-OFF. AT THE TIME, THE AMBER 'R DOOR' LAMP ILLUMINATED ON THE LG ADVISORY PANEL. THIS LAMP REMAINED ILLUMINATED THROUGHOUT THE FLIGHT. AND NO OTHER ABN ORMAL INDICATION WAS SEEN UNTIL FLIGHT CREW ATTEMPTED TO EXTEND THE LG ON APPROACH. PRELIMINARY INSPECTION BY ENGINEERIN G HAS SHOWED THAT THE RT MLG INBOARD MAIN TIRE HAD BLOWN, REPORTEDLY WHILE THE MLG WAS RETRACTING. THIS APPARENTLY DAMAG ED THE MLG DOOR MECHANISM, AND JAMMED THE MLG IN THE WHEEL WELL. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003013000040 20030130 00040 EA 2003 1 30 CA021217006 1 20021111 A 2710 UK BEARING BOMBDR CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A NE AILERON QUADRANT BROKEN W K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 CA 12368 (CAN) DURING 300-600 HOUR INSPECTION AILERON PCU OPERATION TEST. FOUND AILERON QUADRANT IN RT WHEEL WELL IS NOISY (SNAPP ING). AFTER REMOVING RT AILERON QUADRANT ASS FOR INVESTIGATION, FOUND RT QUADRANT ITEM 57 PAGE 27-11-00 FGURE 3 IN IPC B EARING IS DAMAGE (RACE HALF WAY ROUND). CHANGE BOTH RT AND LT QUADRANT ASSEMBLIES, NOISE DISAPPEARED. 2 L 7 2 4F 4 F RT A21AE E15NE 2003013000041 20030130 00041 EA 2003 1 30 CA021217011 1 20021216 A 2913 PV304448 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYD SYSTEM FAILED W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKEOFF AT ABOUT 200 FT AGL ' HYD 1 HIGH TEMP ' MSG. CAME ON EICAS. WHEN CHECKED, HYD TEMP IT WAS 116-117OC PRESSURE WAS AT 3600 PSI DURING FURTHER CLIMB THE TEMP WENT UP TO 133OC ON LEVEL FLIGHT TEMP WAS STABILIZED AT 124-126OC . FOR REST OF THE FLIGHT TEMP WAS FLUCTUATING BETWEEN 124-129OC DEPENDING ON POWER SETTING. HYD PRESSURE WAS STABILIZED AT 3600 PSI. DURING FLIGHT HYD QUANTITY WAS 70 PERCENT, THAT WENT UP TO 90 PERCENT ON ENGINE SHUTDOWN. FURTHER TO ABOVE THE CREW REPORTED TIME FROM HIGH TEMP MESSAGE TO 133OC WAS ABOUT 1-1.5 THEY FLEW AT 133OC FOR FURTHER 1-1.5 MIN MAX. THE TOTAL DURATION OF FLIGHT WAS 17 MINUTES. NR 1 EDP REPLACED ALL FUNCTIONAL CHECKS COMPLETED AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F 4 F RT A21EA E15NE 2003013000042 20030130 00042 NM 2003 1 30 2003F00104 1 20021130 A 3260 SWITCH BOEING 727 727231 1384079 NM LT MLG OUT OF ADJUST A FX7A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 54348 21967 UPON GEAR RETRACTION OUT OF MHLM GEAR DOOR LIGHTS REMAINED ON AIRCRAFT RETURNED TO AIRPORT WITH NO INCIDENT. ADJUSTED S WITCH ON MLG DOOR OPS CHECK NORMAL PER MM 32-12-0. OPS CHECK NORMAL. A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2003013000044 20030130 00044 NM 2003 1 30 CA021218005 1 20020806 A 7921 D2887155C VALVE BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA OIL COOLER BYPASSING W O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 CA (CAN) AT FL240, SAT -22 C, OIL TEMP. RT ENGINE REACHED 108 DEGREES C. WE DESCENDED WITHOUT DELAY TO FL200 IN ORDER TO AC HIEVE LOWER OIL TEMP. THE REST OF THE FLIGHT TO BASE WAS UNEVENTFUL. THE OIL COOLER BYPASS VALVE WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003013000045 20030130 00045 NE 2003 1 30 CA021218006 1 20021128 A 6321 7636309103102 BRAKE DISC SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1S1 60030 NE ROTOR BRAKE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING PREFLIGHT INSPECTION AND TO COMPLY WITH ASB76-66-36 THE ROTOR BRAKE DISC WAS FOUND TO BE CRACKED. NO OTHER DEFECTS FOUND. PART REPLACED. REPORTED FINDING TO SIKORSKY. 1 G 7 2 3U 3 U H1NE E19EU 2003013000046 20030130 00046 NE 2003 1 30 CA021220002 2 20021130 A 7261 ENGINE PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3D GL OIL SYSTEM CONTAMINATED W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) IN CRUISE, PILOT OBSERVED FLUCTUATIONS IN OIL PRESSURE WITHIN THE GREEN BAND, ONE OR TWO SEGMENTS UP AND DOWN FROM NORMAL 110 PSI. INITIALLY SUSPECTED TRANSDUCER, TRANSDUCER WAS PRE-SB79004. UPON LANDING AND SELECTION OF BETA, OIL PR ESSURE OBSERVED AT 160 PSI. UNTIL SHUTDOWN. DURING MAINTENANCE GROUND RUN, OIL PRESSURE OBSERVED AT 70 PSI. OIL FILTER FOUND CONTAMINATED. OIL FILTER HOUSING AND BYPASS VALVE CLEANED. CHIP DETECTOR CHECKED, OK. POWER SECTION SCREEN CHECKE D, OK. OIL FILTER AND OIL CHANGED, FILTER AND OIL SAMPLE FORWARDED TO PWC. SB79004 INCORPORATED. GROUND RUN OK- OIL PRE SSURE OBSERVED AT 110 PSI. RETURNED TO SERVICE. ANALYSIS FROM PWC INDICATED CARBON CONTAMINATED FILTER AND OIL SAMPLE. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P210NE 2003013000047 20030130 00047 EA 2003 1 30 CA021220012 1 20021214 A 7931 7G1058 PRESSURE SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RT ENGINE FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA (CAN) RT ENGINE SHUT DOWN IN FLGHT DUE TO LOW OIL PRESS INDICATION & FLUCTUATION. HAD RT ENGINE OIL PRESS EICAS MSG, HIG H TEMP, FUEL OIL EXCHANGER TEMP INCREASE. RT ENGINE CHIP DETECTOR TESTED OK. OIL LEVEL CHECKED AND ONE HALF LITER REMOV ED. OIL PRESS TRANSDUCER REPLACED, HIGH POWER RUN COMPLETED, ALL PARAMETERS NORMAL. RT ENGIE LUBE AND SCAVENGE PUMP ASSY BYPASS CHECK VALVE REPLACED. RT ENGINE ELECTRICAL HARNESS INSPECTED, AND NO FAULTS FOUND. RT ENGINE SUMP FITTINGS REMO VED AND CONFIRMED THAT SB 79A0016 COMPLETED. DURING 'FUEL CHECK VALVE' CHECK AFTER LT ENGINE STARTUP, 'FUEL LOW PRESS' EICAS MSG FAILED TO COME ON. RT ENGINE FUEL PUMP LOW FUEL PRESS SWITCH REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2003013000048 20030130 00048 SO 2003 1 30 CA021223001 1 20021221 A 6120 582855 HOUSING LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE PROP VALVE FAILED W E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 CA (CAN) ON DESCENT 175 MILES SOUTH OF YZF NR 3 ENGINE RPM DROPPED BELOW 98 PERCENT WITH FLUCTUATION 0.5 PERCENT OUTSIDE LI MITS. WITH ADVANCE OF NR 3 THROTTLE FOR PITCH LOCK CHECK RPM DECAYED. ENGINE PUT TO BED. PROPELLOR VALVE HOUSING DETERMI NED TO BE FAULTY, UNIT REPLACED GROUND RUN FOR PITCHLOCK CHECK CARRIED OUT, SYSTEM SERVICEABLE. 2 H 7 4 4T 4 T A1SO E282 6 C P906 2003013000049 20030130 00049 NM 2003 1 30 QXEA0201994 1 20021123 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - DENTS EXIST IN SKIN OF LEFT HAND FUSELAGE ABOVE WINDOW L13, BETWEEN STRINGERS 12 AND 13. REPAIRED IAW HORIZON AIR EA 6-53-144. 2 H 7 2 4T RT A13NM 2003013000051 20030130 00051 NM 2003 1 30 QXEA0201995 1 20021121 A 5230 HINGE BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - GOUGE IN MAIN HINGE, FORWARD FACE, NEAR LOWER HINGE ATTACH POINT OF FORWARD CARGO DOOR. REPAIRED IAW HORIZON AIR EA 6-52-215. 2 H 7 2 4T RT A13NM 2003013000052 20030130 00052 NM 2003 1 30 QXEA0201996 1 20021122 A 5230 HINGE BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - GOUGE IN MAIN HINGE JUST BELOW LOCK LATCH MECHANISM OF FORWARD CARGO DOOR. REPAIRED IAW HORIZON AIR EA 6-52-215. 2 H 7 2 4T RT A13NM 2003013000053 20030130 00053 NM 2003 1 30 QXEA0201997 1 20021127 A 5280 HINGE BOMBDR DHC8 DHC8401 1390041 NM LT MLG DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - LEFT HAND FORWARD MAIN LANDING GEAR DOOR AFT HINGE ON BOTTOM SIDE IS CHAFING ON DOUBLER AROUND NACELLE HINGE FITTI NG. REPAIRED IAW Q400 AMM 32-12-11-400-801. 2 H 7 2 4T RT A13NM 2003013000054 20030130 00054 NM 2003 1 30 QXEA0201998 1 20021123 A 5420 BRACKET BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - BRACKET SECURING UPPER NACELLE SKIN TO NR 3 FLAP TRACK SUPPORT STRUCTURE IS CRACKED ON LEFT HAND NACELLE, STATIONS X450 AND YW190.0. REPAIRED IAW Q400 SRM 51-24-35. 2 H 7 2 4T RT A13NM 2003013000055 20030130 00055 NM 2003 1 30 QXEA0201999 1 20021121 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - THERE IS A GOUGE IN THE SKIN BELOW AFT CARGO DOOR CUT OUT, APPROXIMATELY STATION X758. REPAIRED IAW DHC-8 SRM 51- 21-10 AND Q400 AMM 51-256-31-370-801. 2 H 7 2 4T RT A13NM 2003013000056 20030130 00056 NM 2003 1 30 QXEA0202000 1 20021119 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - RIGHT HAND LOWER COWL DEBRIS DOOR RIGHT HAND APERTURE CHANNEL CRACKED AT AFT END. REPAIRED IAW RD 8/4-71-106. 2 H 7 2 4T RT A13NM 2003013000057 20030130 00057 NM 2003 1 30 QXEA0202001 1 20021121 A 5420 ANGLE BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - ANGLE CRACKED BELOW FINGERNAIL DECK AT STATION XN302, YW173. REPAIRED IAW RD 8/4-54-033/044. 2 H 7 2 4T RT A13NM 2003013000058 20030130 00058 NM 2003 1 30 QXEA0202002 1 20021124 A 5280 HINGE BOMBDR DHC8 DHC8401 1390041 NM RT MLG DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - RIGHT HAND MAIN LANDING GEAR FORWARD INBOARD DOOR AFT HINGE ARM IS CHAFED ON BACKSIDE. REPAIRED IAW Q400 MM TASK 32-12-11-400-801. 2 H 7 2 4T RT A13NM 2003013000059 20030130 00059 NM 2003 1 30 QXEA0202003 1 20021123 A 7110 FIRESEAL BOMBDR DHC8 DHC8401 1390041 NM COWLING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - TWO ADJACENT CHAFES TO UPPER SURFACE OF THE LOWER COWL FIRE FLOOR, OF COWL PANEL 422AB. REPAIRED IAW HORIZON AIR EA 6-71-71. 2 H 7 2 4T RT A13NM 2003013000060 20030130 00060 NM 2003 1 30 QXEA0202004 1 20021125 A 2131 CONTROLLER BOMBDR DHC8 DHC8401 1390041 NM CABIN PRESSURE MALFUNCTIONED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 414QX 4061 SEA - CREW RETURNED TO FIELD WHEN DURING CLIMB THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT. MAINTENANCE INSPECTED THE A IRCRAFT AND PERFORMED AN OPERATIONAL CHECK OF THE PRESSURIZATION SYSTEM. OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WERE NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003013000061 20030130 00061 EA 2003 1 30 QXEA0202005 1 20020306 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 601QX 882 882 10009 PDX- BOOST PUMPS CYCLED CONTINUOUSLY. CENTER TANK EJECTOR PUMPS REMAINED ON CONTINUOUSLY WITH A STEADY 100-110 POUND QU ANTITY IN CENTER TANK. REMOVED AND REPLACED LEFT HAND AND RIGHT HAND PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL CHEC KS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000062 20030130 00062 EA 2003 1 30 QXEA0202006 1 20020311 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA K NONE J WARNING INDICATION CR CRUISE 1 NM 09 602QX 413 413 10010 MFR- LEFT HAND AND RIGHT HAND BOOST PUMP ON INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED LEFT HAND AND RIGHT HAND PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000063 20030130 00063 EA 2003 1 30 QXEA0202007 1 20020328 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA K NONE J WARNING INDICATION CR CRUISE 1 NM 09 601QX 95 94 10009 LAX- DURING CRUISE FUEL IN CENTER TANK INCREASED TO 100 POUNDS. LEFT HAND AND RIGHT HAND BOOST PUMPS COME ON AND CENTER TANK FUEL TRANSFER SYSTEM ACTIVATES UNTIL CENTER TANK QUANTITY INDICATES ZERO. BOOST PUMPS CONTINUED TO CYCLE. REMOVE D AND REPLACED RIGHT HAND AND LEFT HAND PRIMARY EJECTOR PRESSURE SENSORS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F RT A21EA 2003013000064 20030130 00064 EA 2003 1 30 QXEA0202008 1 20020425 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA K NONE J WARNING INDICATION DE DESCENT 1 NM 09 601QX 163 163 10009 SMF- RIGHT HAND MAIN EJECTOR CAUTION MESSAGE CAME ON DURING DESCENT AND STAYED ON UNTIL ENSUING SHUTDOWN. REMOVED AND R EPLACED RIGHT HAND PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000065 20030130 00065 EA 2003 1 30 QXEA0202009 1 20020402 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM MALFUNCTIONED A QXEA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 09 609QX 790 790 10031 BOI- DURING ENGINE RUN FOR A CHECK, LEFT HAND EJECTOR CAUTION MESSAGE. REMOVED AND REPLACED LEFT HAND PRIMARY EJECTOR P RESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000067 20030130 00067 EA 2003 1 30 QXEA0202011 1 20021105 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 612QX 1352 10042 LAX - CREW RECEIVED A LEFT FUEL LOW PRESSURE WHILE EN ROUTE AT FL 390. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE ENGINE FUEL FEED SWITCH. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000068 20030130 00068 EU 2003 1 30 CA021223003 1 20021219 A 6120 7503503AF O-RING BAG JETSTM JETSTM3212 1500217 EU GARRTT TPE331 TPE33110UG 01514 WP ROTOL R333 R333482F12 GL PROPELLER BROKEN W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) PROPELLER WAS LEAKING OIL OUT OF CYLINDER. TRAVELLED TO AIRCRAFT, FOUND PISTON TO CYLINDER SEAL, ITEM 40, IPL FIG 3, APPEARED TO BE TWISTED AND SPLIT. IT FELL OFF OF PISTON WHEN CYLINDER WAS REMOVED. REPLACED SEAL, REINSTALLED CYLIN DER, NO LEAKAGE EVIDENT WHEN BETA TUBE REINSTALLED AND FLIGHT IDLE ANGLE SET.ENGINE TEST RUN, NO LEAKAGE.AIRCRAFT FLOWN FOR APPROXIMATELY 2 HOURS AND NO LEAKAGE FOUND AFTER FLIGHT. 2 L 7 2 4T 4 T RT BA15CAA E4WE 6 C P61GL 2003013000069 20030130 00069 EA 2003 1 30 QXEA0202012 1 20021108 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 613QX 1059 10045 LBG - CREW RECEIVED A LEFT LOW FUEL PRESSURE CAUTION WHEN THE PUMPS WERE SELECTED ON. MAINTENANCE INSPECTED THE AIRCRAF T AND REPLACED THE LEFT ENGINE FUEL FEED SWITCH. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO S ERVICE. 2 L 7 2 4F RT A21EA 2003013000070 20030130 00070 EA 2003 1 30 QXEA0202013 1 20021113 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 09 606QX 2016 2016 10023 PDX - CREW RECEIVED A LEFT FUEL LOW PRESSURE CAUTION MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT ENGINE FUEL FEED SWITCH. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000071 20030130 00071 EA 2003 1 30 QXEA0202014 1 20021113 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 600QX 53 53 10005 SJC - AFTER ENGINE START THE LEFT FUEL LOW PRESSURE CAUTION STAYED ON. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE ENGINE FUEL FEED SWITCH. OPERATIONAL AND LEAKS CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000072 20030130 00072 EA 2003 1 30 QXEA0202015 1 20021118 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 607QX 57 57 10024 SEA - CREW REPORTS WHILE RUNNING ENGINES, THE LEFT FUEL LOW PRESSURE CAUTION LIGHT REMAINS ILLUMINATED. MAINTENANCE INS PECTED THE AIRCRAFT AND REPLACED THE ENGINE FUEL FEED SWITCH. OPERATIONAL AND LEAK CHECKS ARE GOOD. THE AIRCRAFT WAS R ETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000073 20030130 00073 EA 2003 1 30 QXEA0202016 1 20020514 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 601QX 90 90 10009 PDX- FUEL BOOST PUMPS CYCLING ON AND OFF CONTINUOUSLY AT FLIGHT LEVEL 350. REMOVED AND REPLACED PRIMARY EJECTOR PRESSUR E SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000074 20030130 00074 NM 2003 1 30 P5CA0300728 1 20021231 A 2730 60B0004716 ROD BOEING 747 7472U3B 1384846 NM L/H ELEVATOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 CORROSION LEVEL 1 FOUND ON L/H INBD ELEVATOR POWER CONTROL PACKAGE ROD END, WITH TEFLON SEAL ADRIFT. POWER CONTROL PACKA GE REPLACED IAW MM 27-31-07. 2 L 7 4 4F RT A20WE 2003013000084 20030130 00084 EA 2003 1 30 QXEA0202017 1 20020618 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 610QX 869 869 10033 PDX- LEFT HAND AND RIGHT HAND FUEL PUMP ADVISORY LIGHTS ON. PUMP CYCLING DURING FLIGHT AT 39,000 FEET. REMOVED AND REP LACED LEFT HAND AND RIGHT HAND PRIMARY EJECTOR PRESSURE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000085 20030130 00085 EA 2003 1 30 QXEA0202018 1 20020618 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 610QX 90 90 10033 PDX- RIGHT HAND FUEL PUMP CIRCUIT BREAKER POPPED WHEN PUMP IS SELECTED ON AND WILL NOT RESET. REMOVED AND REPLACED RIGH T HAND PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000086 20030130 00086 EA 2003 1 30 QXEA0202019 1 20020618 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 607QX 1775 1775 10024 FAT- LEFT HAND AND RIGHT HAND FUEL BOOST PUMP CYCLED IN CRUISE FOR 25 MINUTES AND STOPPED UPON DESCENT. REMOVED AND REP LACED LEFT HAND AND RIGHT HAND PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000087 20030130 00087 EU 2003 1 30 QXEA0202020 1 20021125 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 PDX- MID CABIN OVERHEAD EMERGENCY EXIT SIGN FORWARD SIDE HAS NUMEROUS LIGHTS THAT DO NOT ILLUMINATE WHEN SELECTED ON. R EPLACED MID CABIN EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2003013000088 20030130 00088 WP 2003 1 30 CA021223005 1 20021214 A 6520 GEARBOX HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL TAIL ROTOR FAILED W R A AUTOROTATION UNSCHED LANDING F FLT CONT AFFECTED AG AGRICULTURE 1 CA (CAN) AIRCRAFT WAS BEING USED FOR CAPTURE WORK ON WOLVES 14.5 KMS NORTH OF BANFF NATIONAL PARK. AIRCRAFT WAS IN PURSUIT OF A WOLF THAT WAS NETTED, AIRCRAFT WAS AT A HEIGHT OF 6-10 FT. ABOVE GROUND, TRAVELLING AT 20 MPH IN A CROSSWIND. AT THE TIME OF PROBLEM A FAIR AMOUNT OF LT PEDDLE WAS BEING USED. AIRCRAFT TRAVELLED APPROX. 30FT CROSSWIND WHEN A LOUD BA NG WAS HEARD BY PILOT FOLLOWED BY THE TAIL ROTOR ASSEMBLY FLYING PAST THE PILOTS CHIN BUBBLE.THE PILOT THEN ROLLED THE T HROTTLE OFF TO STOP THE ROTATION OF THE AIRCRAFT AND LANDED THE AIRCRAFT ON A NEARLY LEVEL OR FAIRLY LEVEL SPOT.THE AIRC RAFT HAD COMPLETED 1/2 OF A REVOLUTION BY THE TIME THE PILOT GOT IT ON THE GROUND. THERE WAS NO FURTHER DAMAGE TO THE AI 1 G 7 1 3U 3 U H3WE E4CE 2003013000089 20030130 00089 NE 2003 1 30 QXEA0202021 2 20021124 A 7530 310848802 VALVE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE ENGINE FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 367PH 511 SEA- AFTER ENGINES STARTED AND DURING PUSHBACK SIGNIFICANT AMOUNT OF SMOKE DEVELOPED IN CABIN. REMOVED AND REPLACED P2. 5 AND P3 AIR PRESSURE VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2003013000090 20030130 00090 NM 2003 1 30 QXEA0202023 1 20021201 A 1430 BOLT DHAV DHC8 DHC8202 2809007 NM PAX DOOR BACKED OUT A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 360PH 515 PDX-MAIN CABIN DOOR VERY DIFFICULT TO OPEN, GRINDING AND IT POPS HARD. FOUND AFT HANDRAIL OVER CENTER ROD CONNECTING BO LT BACKED OUT. RETIGHTENED BOLT. MAIN CABIN DOOR OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SER VICE. 2 H 7 2 4T RT A13NM 2003013000091 20030130 00091 WP 2003 1 30 CA021223006 1 20021205 A 2780 PROXIMITY SENSOR LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE RT SLAT FAILED W C ABORTED TAKEOFF J F WARNING INDICATION FLT CONT AFFECTED TO TAKEOFF 1 CA (CAN) A/C ABORTED TAKE OFF AND RETURNED TO THE GATE DUE TO UNSAFE TAKE OFF WARNING RT SLAT NR 3 GREEN LIGHT 'OFF', ON TH E FLIGHT ENGINEER PANEL AND LEADING EDGE SLAT GREEN LIGHT 'ON'. MTCE REPLACED THE SLAT POSITION PROXIMITY SWITCH SENSOR FOR THE RT SLAT NR 2 & 3 I.A.W. AMM 27-82-03. A TEST FLIGHT WAS CARRIED OUT SATISFACTORY. 2 L 7 3 4F 4 F A23WE E12EU 2003013000092 20030130 00092 EA 2003 1 30 QXEA0202024 1 20021127 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY TORN A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 602QX 10010 PDX- FORWARD CARGO BAY FIRE SUPPRESSION CHIMNEY SCREEN TORN. REMOVED AND REPLACED TORN FORWARD CARGO BAY FIRE SUPPRESSI ON CHIMNEY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000093 20030130 00093 NM 2003 1 30 QXEA0202025 1 20021126 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE LAVATORY MALFUNCTIONED A QXEA K NONE N FALSE WARNING CL CLIMB 1 NM 09 367PH 9371 89 511 PCE124159 PDX-ON CLIMBOUT SMOKE ALARM WENT OFF IN LAVATORY THROUGH 5,000 AGL. NO SMOKE WAS VISIBLE IN COCKPIT OR CABIN. REPLACED LAVATORY SMOKE DETECTOR AND NR 2 ENGINE GROUND RUNS CHECK GOOD, NO LEAKS NOTED, NO SMOKE PRESENT. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2003013000094 20030130 00094 EA 2003 1 30 QXEA0202027 1 20021130 A 3350 YAD4F RELAY CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FAILED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 607QX 10024 BOI- EMERGENCY LIGHTS CAME ON IN ARM POSITION. REMOVED AND REPLACED K135 ACCESS BUS SENSE RELAY. OPERATIONAL CHECKS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000095 20030130 00095 2003 1 30 CA021223007 4 20021222 A 3417 2593200951 ADC LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE E/E BAY MALFUNCTIONED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) SHORTLY AFTER T/O (A/C RETURNED), THE FOLLOWING INDICATIONS CAME UP ON F/O'S SIDE: MACH FLAG IN A/S INDICATOR, SSC FLAG IN ALTIMETER, F/D FLAG IN ADI, OFF FLAGS IN BOTH TAS AND SAT INDICATORS, AND FAIL ANNUNCIATORS IN BOTH MACH TRIM A ND MACH FEEL CHANNEL 2 SWITCH LIGHTS. AUTOPILOT COULD ONLY BE ENGAGED IN CWS.SELECTING F/O'S ALT AS/M SWITCH CAUSED MAC H FLAG ONLY TO DISAPPEAR. DURING FINAL, ALL ABNORMAL INDICATIONS DISAPPEARED MOMENTARILY ONLY TO REAPPEAR SHORTLY AFTER . CADC REPLACED AND TESTED SERVICEABLE IAW MM 34-14-01.LEAK CHECK C/O AND TESTED SERVICEABLE. 2 L 7 3 4F 4 F A23WE E12EU 2003013000096 20030130 00096 NM 2003 1 30 QXEA0202028 1 20021126 A 2750 C1486561 POWER UNIT BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP FAILED A QXEA K NONE F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 09 401QX 3531 3531 4031 PDX- FLAP POWER CAUTION LIGHT ILLUMINATED IN FLIGHT AFTER SELECTING FLAPS 5 DEGREES. FLAP CONTROL CIRCUIT BREAKER CYCLE D LIGHT OUT. NORMAL FLAPS 35 LANDING. REMOVED AND REPLACED FLAP POWER UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2003013000097 20030130 00097 EA 2003 1 30 QXEA0202029 1 20021130 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 614QX 984 984 10049 PDX- LEFT HAND AND RIGHT HAND FUEL PUMPS ON DURING TAXI, FUEL PUMP SWITCHES CYCLED OFF AND ON. RIGHT MAIN EJECTOR CAUTI ON MESSAGE CAME ON. AFTER CYCLING PUMP SWITCHES SEVERAL TIMES, THE FUEL PUMPS STAYED OFF, BUT A RIGHT FUEL LOW PRESSURE CAUTION MESSAGE CAME ON AND STAYED ON. REMOVED AND REPLACED PRIMARY EJECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000098 20030130 00098 CE 2003 1 30 CA021224001 1 20021220 A 8120 FITTING CESSNA 421 421C 2076016 CE CONT O520 GTSIO520L 17032 SO MCAULY 3FF32 3FF32C501 GL TURBOCHARGER LEAKING W E A ENGINE SHUTDOWN UNSCHED LANDING R K J PARTIAL RPM/PWR LOSS FLUID LOSS WARNING INDICATION CL CLIMB 1 CA AJ023688 (CAN) THE PILOT REPORTED SHORTLY AFTER TAKEOFF THE RT ENGINE LOST OIL PRESSURE, ENGINE WAS SELECTED TO FEATHER AND SHUTD OWN, BUT PROPELLER FAILED TO FEATHER. A SUBSEQUENT INSPECTION OF THE RT ENGINE REVEALED THE FOLLOWING: OIL SUPPLY LINE F ITTING AN8336 IN THE TURBOCHARGER WASTE GATE CONTROLLER WAS FOUND SEPARATED FROM THE WASTE GATE CONTROLLER RESULTING IN LOSS OF ENGINE OIL. THE THREADS IN THE WASTE GATE CONTROLLER WERE FOUND STRIPPED, THE PROPELLER AND PROPELLER GOVERNOR W ERE REMOVED FOR INSPECTION BY CANADIAN PROPELLER, BUT NO FAULT WAS FOUND. 1 L 7 2 3O 3 O A7CE E7CE 5 C P45GL 2003013000099 20030130 00099 EA 2003 1 30 QXEA0202030 1 20021128 A 2824 P93A25602 CARTRIDGE CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 09 606QX 2138 2138 10023 BOI- TRANSFER PUMP CAUTION MESSAGE WITH ASSOCIATED LEFT FUEL CROSS/LOW SWITCH LIGHT INDICATING "FAIL" ANYTIME FUEL TANK IMBALANCE EXCEEDS 200 POUNDS. REMOVED AND REPLACED BI-CROSSFLOW PUMP CARTRIDGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000100 20030130 00100 EU 2003 1 30 CA021224002 1 20021223 A 2910 SA7670006122 HOSE BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG SPLIT W O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 35829 35829 (CAN) AFTER TAKE-OFF DURING GEAR RETRACTION, GREEN SYSTEM HYDRAULIC QUANTITY WAS LOST . UPON ARRIVAL AT DESTINATION, AL TERNATE GEAR EXTENSION WAS USED , NORMAL LANDING . INSPECTION FOUND LT MLG RETRACTION ACTUATOR HOSE SPLIT (SMALL BURST ) . LINE REPLACED, GEAR SWUNG , AIRCRAFT RETURNED TO SERVICE. 2 H 7 4 4F 4 F A49EU E6NE 2003013000101 20030130 00101 EA 2003 1 30 QXEA0202031 1 20021130 A 2612 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA FIRE DETECTION MALFUNCTIONED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 615QX 10065 LAX- FIRE SYSTEM FAULT STATUS MESSAGE. COMPLIED WITH OPERATIONAL TEST OF FIDEX SYSTEM IAW 26-10-00-710-801. NO PARTS R EPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000102 20030130 00102 EA 2003 1 30 QXEA0202032 1 20021201 A 2612 47388904 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA FIRE DETECTION MALFUNCTIONED A QXEA O OTHER N FALSE WARNING DE DESCENT 1 NM 09 615QX 120 120 10065 SEA- DURING DESCENT FIRE SYSTEM FAULT STATUS MESSAGE CAME ON. THE FIRE DETECTION CIRCUITS TESTED OKAY. AFTER LANDING F IRE DETECTION SYSTEM FAULT STATUS MESSAGE WENT AWAY. REMOVED AND REPLACED FIDEX CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000103 20030130 00103 EA 2003 1 30 QXEA0202033 1 20021201 A 2120 ODOR CNDAIR CL600 CL6002C10 1390015 EA CABIN DETECTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 601QX 10009 BOI- CREW REPORTS AN ODOR IN CABIN. CYCLED RECIRCULATION FAN OFF. OPENED ALL PASSENGER GASPERS AND AIRED OUT CABIN. O DOR DECREASED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000104 20030130 00104 WP 2003 1 30 CA021227003 1 20021216 A 2722 428007 ROD END LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE DAMPER SHEARED W O OTHER J WARNING INDICATION DE DESCENT 1 CA (CAN) DURING FLIGHT FROM, FLIGHT CREW REPORTED THAT, RUDDER HYD LIMITER ANNUNCIATOR AND RUDDER LIMITER HYDRAULIC PUSH LI GHTS ON, FLAPS 4 DEGREES, AIRSPEED 190 KNOTS.PUSH LIGHT GOES OUT WITH FLAPS SELECTED UP AND AIR SPEED 210 KTS (WHICH IS NORMAL).UPON TROUBLE SHOOTING, MTCE FOUND #2 RUDDER DAMPER ACTUATOR ROD END BROKEN OFF (SHEARED). THE RUDDER DAMPER HAD BEEN INSTALLED INCORRECTLY (LUBE FITTING INSTALLED POINTING TO THE RIGHT INSTEAD OF POINTING TO THE LEFT). MTCE REPLACED THE RUDDER DAMPER. 2 L 7 3 4F 4 F A23WE E12EU 2003013000106 20030130 00106 EU 2003 1 30 QXEA0202034 3 20021126 A 6110 PROPELLER BOMBDR DHC8 DHC8401 1390041 NM ROTOL R408 CR4086123F17 EU NR 2 ENGINE VIBRATION A QXEA K NONE E VIBRATION/BUFFET CR CRUISE 1 NM 09 413QX 4060 PDX- NR 2 PROP VIBRATION IN FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. BALANCED NR 2 PROP. NO PARTS REPLACED. OPERATI ONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P17BO 2003013000107 20030130 00107 EA 2003 1 30 QXEA0202036 2 20021201 A 7261 REGULATOR BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA NR 1 ENGINE OUT OF ADJUST A QXEA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 09 409QX 4051 PDX- NR 1 ENGINE OIL PRESSURE RUNS HIGH INTO YELLOW HALF OF THE TIME. ADJUSTED NR 1 ENGINE OIL PRESSURE. NO PARTS REPL ACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003013000108 20030130 00108 NM 2003 1 30 QXEA0202044 1 20021201 A 3240 BRAKE ASSY BOMBDR DHC8 DHC8401 1390041 NM MLG MALFUNCTIONED A QXEA O OTHER O OTHER LD LANDING 1 NM 09 411QX 4055 GEG - CREW WAS UNABLE TO SLOW THE AIRCRAFT ADEQUATELY AND THE LEFT MAIN TIRE WAS DAMAGED BY THE OVERRUN LIGHTS. THE AIR CRAFT WAS INSPECTED, THE NR 1 AND NR 3 MAIN TIRES WERE CHANGED AND THE CENTRAL DIAGNOSTICS SYSTEM WAS INTERROGATED. NO FAULT WERE FOUND IN THE CDS AND NO FAULTS WERE FOUND WITH THE ANTI-SKID SYSTEM OR PROPELLERS. TAXI CHECKS AND BRAKE FUN CTIONAL CHECKS WERE PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003013000109 20030130 00109 EA 2003 1 30 QXEA0202045 1 20021202 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY PUNCTURED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 600QX 10005 SEA- FORWARD CARGO SMOKE DETECTOR SCREEN HAS PUNCTURE HOLE. REMOVED AND REPLACED SMOKE DETECTION SCREEN. NO DEFECTS NO TED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000110 20030130 00110 EA 2003 1 30 QXEA0202046 1 20021127 A 5310 DOOR FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX- CRACK IN FRAME FORWARD SIDE OF AFT EQUIPMENT BAY DOOR OPENING ABOVE LEFT HAND DOOR HINGE AT STATION 1108.00. REPAIR ED IAW HORIZON AIR EA R-53-62. 2 L 7 2 4F RT A21EA 2003013000111 20030130 00111 NM 2003 1 30 QXEA0202047 1 20021128 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX- OUTER BAGGAGE DOOR SKIN IS CHAFED AT UPPER EDGE SURFACE. REPAIRED IAW HORIZON AIR EA 2-53-146. 2 H 7 2 4T RT A13NM 2003013000112 20030130 00112 EA 2003 1 30 QXEA0202050 1 20021119 A 2820 TUBE CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 605QX 10022 PDX- LEFT AND RIGHT EJECTORS, RIGHT HAND LOWER CHECK VALVE, AND LEFT HAND UPPER CHECK VALVE TUBES CHAFED. REPAIRED IAW HORIZON AIR EO R-28-82 "A". 2 L 7 2 4F RT A21EA 2003013000113 20030130 00113 EA 2003 1 30 QXEA0202051 1 20021119 A 2820 TUBE CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 605QX 10022 PDX- LEFT HAND FUEL TUBE IS CHAFFED BEYOND LIMITS. REPAIRED IAW CRJ MM 28-21-00-790-802. 2 L 7 2 4F RT A21EA 2003013000114 20030130 00114 EA 2003 1 30 QXEA0202053 1 20020730 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 603QX 1604 10011 PDX - AFTER START AND AT IDLE, THE FUEL BOOST PUMPS CYCLED ON AND OFF. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT AND RIGHT PRIMARY EJECTOR PRESSURE SENSORS. LEAK CHECK AND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS R ETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000115 20030130 00115 EA 2003 1 30 QXEA0202054 1 20020804 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 603QX 1446 34 10011 BOI - AFTER ENGINE START BOTH FUEL BOOST PUMPS REMAINED ON. MAINTENANCE INSPECTED AND REPLACED THE RIGHT PRIMARY EJECTO R SENSOR. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000116 20030130 00116 EA 2003 1 30 QXEA0202055 1 20020822 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 601QX 2135 10009 PDX - THE LEFT AND RIGHT FUEL PUMP ON GREEN ADVISORY MESSAGE AND AUDIBLE INDICATION OF PUMPS CYCLING CONTINUOUSLY WHILE AT 39K FEET. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT AND RIGHT EJECTOR PRESSURE SENSORS. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000117 20030130 00117 EA 2003 1 30 QXEA0202056 1 20020828 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 601QX 29 29 10009 PDX - THE LEFT AND RIGHT FUEL PUMPS CONTINUOUSLY CYCLE WHILE AT 39K FEET. MAINTENANCE INSPECTED AND REPLACED BOTH PRIMA RY FUEL EJECTOR PRESSURE SENSORS. LEAK CHECK AND OPERATIONAL CHECK IS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000118 20030130 00118 EA 2003 1 30 QXEA0202057 1 20020903 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 607QX 506 506 10024 PDX - BOTH FUEL BOOST PUMPS STAYED ON WHILE AT 39K FEET. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT AND R IGHT PRIMARY EJECTOR PRESSURE SENSORS. THE LEAK AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE . 2 L 7 2 4F RT A21EA 2003013000119 20030130 00119 EA 2003 1 30 QXEA0202058 1 20020909 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 603QX 268 268 10011 BOI - AT FL 390, BOTH FUEL PUMPS CAME ON AND STAYED ON FOR ABOUT 1 HOUR. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACE D THE RIGHT PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SER VICE. 2 L 7 2 4F RT A21EA 2003013000120 20030130 00120 EA 2003 1 30 QXEA0202059 1 20021108 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 09 601QX 444 444 10009 PDX - FUEL BOOST PUMPS WERE CYCLING FOR MORE THAN 20 MINUTES. MAINTENANCE INSPECTED AND REPLACED BOTH PRIMARY EJECTOR P RESSURE SENSORS. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013000121 20030130 00121 NM 2003 1 30 QXEA0202063 1 20021112 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 CKB - BOTH ENDS ARE CRACKED ON BOTH CENTER WING LEADING EDGE CLOSING RIBS. REPAIRED IAW HORIZON AIR EA 6-57-79 AND WVAC EO DH8S-57-0640. 2 H 7 2 4T RT A13NM 2003013000122 20030130 00122 NM 2003 1 30 QXEA0202064 1 20021112 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 CKB - ALL FOUR CORNERS OF RIGHT HAND LEADING EDGE, CENTER WING CLOSING RIBS ARE CRACKED. REPAIRED IAW WVAC EO DH8S-57-0 640 AND HORIZON AIR EA 6-57-79. 2 H 7 2 4T RT A13NM 2003013000123 20030130 00123 NM 2003 1 30 QXEA0202065 1 20021116 A 7110 87144120 FRAME BOMBDR DHC8 DHC8401 1390041 NM COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 CKB - FRAME IS CRACKED. REPAIRED IAW HORIZON AIR EA 6-71-68 AND WVAC EO DHCS-71-0660. 2 H 7 2 4T RT A13NM 2003013000124 20030130 00124 NM 2003 1 30 QXEA0202066 1 20021114 A 5420 WEB BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 CKB - RIGHT HAND NACELLE SHEAR DECK AT EXHAUST OUTLET BOTTOM ATTACH POINT IS CRACKED THROUGH TO 85414389 LOWER CHANNEL. REPAIRED IAW SRM 51-42-05. 2 H 7 2 4T RT A13NM 2003013000125 20030130 00125 NM 2003 1 30 QXEA0202074 1 20021120 A 5310 DOOR FRAME BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 CKB - FIVE HOLES TOTAL IN FORWARD BAGGAGE DOOR AND AFT SERVICE DOOR SURROUNDS. REPAIRED IAW HORIZON AIR EA 6-53-133, EA 6-53-142 AND RD 8/4-53-296. 2 H 7 2 4T RT A13NM 2003013000126 20030130 00126 NM 2003 1 30 QXEA0202078 1 20021123 A 5420 BRACKET BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 CKB - LEFT HAND NACELLE AFT FAIRING LEFT AND RIGHT HAVE CRACKED AFT ATTACH BRACKETS. REPAIRED IAW DH8S-54-06654 AND HORI ZON AIR EA 6-54-158A. 2 H 7 2 4T RT A13NM 2003013000127 20030130 00127 NM 2003 1 30 QXEA0202080 1 20021201 A 3010 4100S00501 VALVE BOMBDR DHC8 DHC8401 1390041 NM DEICE SYSTEM INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 09 409QX 74 4051 PDX-MASTER CAUTION DEICE PRESS CAUTION LIGHT. LIGHTS FAIL TO ILLUMINATE ON OUTBOARD 2 SEGMENTS OF LEFT WING AND BOOTS V ISUALLY DO NOT INFLATE. BULBS TEST OK. CREW DID NOT WANT TO ENTER ICING CONDITIONS AT GEG AND ELECTED TO DIVERT TO PDX . FLIGHT LANDED WITHOUT INCIDENT AT PDX. REMOVED AND REPLACED NR 1 DUAL DISTRIBUTOR VALVE. DEICE BOOTS INFLATE NORMAL DURING DEICE SYSTEM TESTS. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003013000128 20030130 00128 NM 2003 1 30 CA021227005 1 20021212 A 3222 6546227 CAM BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE NLG CENTERING DAMAGED W O OTHER K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CA (CAN) UPON ARRIVAL IN YEG, THE NOSE OLEO WAS FOUND LOW AND LEAKING FLUID. AIRCRAFT HAD SOME HISTORY OF HARD BOTTOMING SN AGS. AFTER INSPECTION BY MAINTENANCE IT WAS DETERMINED THE NOSE GEAR REQUIRED DIASSEMBLY FOR A SEAL CHANGE. AIRCRAFT WAS FERRIED TO YVR FOR REPAIRS. UPON DISSASSEMBLY OF THE THE NOSE OLEO MAINTENANCE DISCOVERED THE CENTERING CAMS WERE MISSA LIGNED. NOSE OF THE UPPER CAM WAS SLIGHTLY PEENED FROM HARD CONTACT WITH THE 'BACKSIDE' OF THE LOWER CAM. 2 L 7 2 4F 4 F A16WE E2EA 2003013000129 20030130 00129 EU 2003 1 30 QXEA0202081 1 20021201 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 PDX- FORWARD OVERHEAD EMERGENCY EXIT SIGN AT SEAT ROW 8 HAS NUMEROUS BULBS OUT. REMOVED AND REPLACED EXIT SIGN. OPERATI ONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2003013000130 20030130 00130 EA 2003 1 30 QXEA0202082 1 20021130 A 5210 BRACKET CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 608QX 10026 PDX- MAIN CABIN DOOR SUPPORT WHEEL BRACKET IS BROKEN. REPAIRED IAW CRJ MM TASK 52-11-13-710-801-A01. 2 L 7 2 4F RT A21EA 2003013000131 20030130 00131 NM 2003 1 30 2003F00105 1 20021117 A 3350 362624 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 889MA 21854 DURING P/T FOUND FORWARD MOST E-PATH LIGHT STRIP OUT. REMOVED AND REPLACED E-PATH LIGHT STRIP, OPS CHECK NORMAL. (M) 2 L 7 3 4F A3WE 2003013000133 20030130 00133 EA 2003 1 30 A6WA200340017 1 20021119 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 RIGHT SIDE FLOOR SUPPORT ANGLE 621 CRACKED OUT AND REMOVED FS 621 ANGLE. FITTED AND DRILLED -2 ANGLE AND -4 ANGLE. INST ALLED REPAIRED ANGLE. (M) 2 L 7 2 4F RT A21EA 2003013000134 20030130 00134 NM 2003 1 30 AALA20020380 1 20020328 A 3411 PROBE BOEING 777 777223 1385213 NM PITOT/STATIC SYS OBSTRUCTED A AALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 21 798AN 30797 MIA - FLT 943 - EN ROUTE MIA-EZE, ON TAKEOFF ROLL AT 100 KNOTS, CAPTAINS AND FIRST OFFICERS AIRSPEED INDICATION SHOWED 3 0 KNOTS. RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. REMOVED OBSTRUCTION FROM LEFT, CENTER AND RIGHT PITOT PR OBES. REPLACED LEFT AND RIGHT PITOT PROBES. PURGED PITOT AND STATIC SYSTEM. SYSTEMS LEAK CHECK GOOD PER MM. (M) 2 L 7 2 4F RT T00001SE 2003013000135 20030130 00135 NM 2003 1 30 ASAA0210220 1 20021007 A 3350 8731002142 SIGN BOEING 737 7372Q8C 138448S NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING INSPECTION, FOUND EXIT IDENTIFIER AT THE SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED EXIT IDENTIFIER, THEN LIGHT TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2003013000136 20030130 00136 NM 2003 1 30 ASAA0210351 1 20021201 A 3350 8821004 BATTERY PACK BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTING FLASHING. REMOVED AND REPLACED BATTERY PACK, THEN L IGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2003013000137 20030130 00137 NM 2003 1 30 ASAA0240127 1 20021003 A 3350 8100022601 LIGHT BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 774AS 25107 DURING CHECK, FOUND EMERGENCY EXIT LIGHTS AT AFT CABIN INOPERATIVE. RECONNECTED LIGHTS, OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 2003013000138 20030130 00138 WP 2003 1 30 ASAA0280655 1 20021210 A 5320 993653435 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 180. REPLACED FLOOR SUPPORT PER SRM 53-14-1, 51-10-2, 51-10- 4, 51-30-5, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003013000139 20030130 00139 WP 2003 1 30 ASAA0280656 1 20021216 A 3350 0105606 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 ANC - DURING PREFLIGHT CHECK, THE EMERGENCY TRACK LIGHTING IN FIRST CLASS CABIN WAS INOPERATIVE. RECONNECTED LOOSE CONN ECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003013000140 20030130 00140 EA 2003 1 30 ASOA02611 1 20021129 A 3397 M2275935229 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 859AS 7421 FLT 4242 - DURING HANGAR CHECK IN BTR, THE LEFT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE D EFERRED THE LEFT OVERWING EMERGENCY LIGHT IAW MEL NR 33-51-02, PENDING REPLACEMENT OF A BAD DIODE. UPON FURTHER TROUBLE SHOOTING, MAINTENANCE FOUND A BAD WIRE AT TERMINAL BOARD 107-2, PIN A AND REPAIRED THE WIRE WHICH CLEARED THE DEFERRAL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003013000141 20030130 00141 EA 2003 1 30 ASOA02613 1 20021130 A 4930 69254517 SOLENOID VALVE CNDAIR CL600 CL6002B19 1900309 EA APU MALFUNCTIONED A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 11 878AS 7590 FLT 4431 - DURING DESCENT INTO ATL, A STRONG FUEL ODOR OCCURRED WHEN THE BLEEDS WERE CHANGED FROM THE ENGINE TO THE AUXI LIARY POWER UNIT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE FUEL SOLENOID VALVE. OPERAT IONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003013000142 20030130 00142 EU 2003 1 30 ASOA02614 1 20021201 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 533AS 460 DURING HANGAR INSPECTION IN MCN, THE LOWER LEFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE NR 2 POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2003013000143 20030130 00143 SO 2003 1 30 ASOA02615 1 20021123 A 2611 BATTERY EMB 120 EMB120RT 3260202 SO SMOKE DETECTOR DISCHARGED A ASOA K NONE N FALSE WARNING CR CRUISE 1 SO 11 258AS 120131 FLT 4081 - DURING CRUISE FROM ATL-CSG, THE SMOKE DETECTOR IN THE LAVATORY BEGAN TO BEEP INTERMITTENTLY. MAINTENANCE REM OVED AND REPLACED THE LAVATORY SMOKE DETECTOR BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2003013000144 20030130 00144 SO 2003 1 30 ASOA02616 1 20021123 A 2611 BATTERY EMB 120 EMB120RT 3260202 SO SMOKE DETECTOR DISCHARGED A ASOA K NONE N FALSE WARNING CR CRUISE 1 SO 11 258AS 120131 FLT 4286 - DURING CRUISE FROM AVL-ATL, THE LAVATORY SMOKE DETECTOR MALFUNCTIONED. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2003013000145 20030130 00145 EA 2003 1 30 ASOA02617 1 20021203 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA K NONE O OTHER CR CRUISE 1 SO 11 857AS 6593 7411 FLT 4403 - DURING CRUISE FROM GRR-ATL, AT APPROXIMATELY 24,000 FEET, THE CREW NOTICED A SMALL CRACK IN THE PILOT'S LEFT SIDE WINDOW. THE CRACK PROGRESSED SLOWLY AND THEN SUDDENLY POPPED ACROSS THE WINDOW. THE AIRCRAFT REDUCED SPEED AND LA NDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE PILOT'S LEFT SIDE WINDOW. OPERATIONAL AND PRESSURE CHECKS GOO D. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003013000146 20030130 00146 EA 2003 1 30 ASOA02618 1 20021203 A 2120 SMOKE CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A ASOA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 11 907EV 7648 FLT 4017 - DURING CLIMB-OUT FROM MCN-ATL, THE CREW RECEIVED A LAVATORY SMOKE MESSAGE AND THE CABIN FILLED WITH SMOKE. A N EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MCN, LANDING SAFELY. MAINTENANCE PERFORMED GROUND RUNS AT POWER W ITH THE ENGINE BLEEDS ON AND NO SMOKE REOCCURRED. MAINTENANCE SUSPECTED RESIDUAL GLYCOL FROM A PRIOR COMPRESSOR WASH CA USED THE SMOKE DURING CLIMB-OUT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003013000147 20030130 00147 SO 2003 1 30 ASOA02619 1 20021204 A 2120 ODOR EMB 120 EMB120ER 3260203 SO COCKPIT DETECTED A ASOA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 SO 11 262AS 120146 FLT 4229 - DURING DESCENT INTO ILM, A BURNING SMELL OCCURRED IN THE COCKPIT WHICH APPEARED TO BE GLYCOL, FOLLOWED BY SMO KE IN THE CABIN WITH THE SMOKE ALARMS SOUNDING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ILM. MAINT ENANCE RAN THE ENGINES AND AUXILIARY POWER UNIT, PERFORMING OPERATIONAL CHECKS ON THE PACKS. NO DEFECTS WERE FOUND. OP ERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2003013000148 20030130 00148 NM 2003 1 30 QXEA0202085 1 20021202 A 5210 DOOR BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR STUCK A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 409QX 4051 PDX- FLIGHT ATTENDANT REPORTS AFT PASSENGER DOOR WILL NOT OPEN. INSPECTED AND OPERATED DOOR WITHOUT A PROBLEM. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003013000152 20030130 00152 EA 2003 1 30 CA021228002 1 20021222 A 2410 755469 IDG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT ENGINE LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 21829 (CAN) FLT 5954, GRF-CVG, LT ENG OIL WARNING MSG POSTED WHILE IN CRUISE. QRH FOLLOWED AND MSG PERSISTED. OIL TEMP DECREA SED, LT ENGINE SHUT DOWN AND AIRCRAFT LANDED IN CRW WITHOUT FURTHER INCIDENT. 16 DEC,02: OIL CONSUMPTION MONITORING DET ECTS OIL CONSUMPTION ON LT ENGINE HIGHER THAN NORMAL. MAINTENANCE CALL BACK INITIATED. 21 DECK 02, PER CALL BACK ON 16 D ECK 02, REMOVED AND REPLACED AGB AXIS BB (IDG) CARBON SEAL ON LEFT ENGINE. LT IDG THERMOCOUPLE BROKE WHEN TAKING CONNEC TOR OFF. REMOVED LT IDG TEMP BULB AND REINSTALLED SERVICEABLE TEMP BULB.ORIGINAL IDG REINSTALLED. FOLLOWING AGB AXIS BB CARBON SEAL AND MATING RING PER GE SPECIAL PROCEDURES 63. AIRCRAFT RETURNED TO SERVICE.22 DEC 02, SEE EVENT ABOVE. MT 2 L 7 2 4F 4 F RT A21EA E15NE 2003013000154 20030130 00154 WP 2003 1 30 CA021230001 1 20021218 A 3246 8065A85 AXLE DOUG DC4 C54A 3021512 WP PWA R2000 R20007M2 52023 NE MLG BENT W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AIRCRAFT WAS REPORTED TO HAVE A HARD LANDING TO MAINTENANCE AND WAS BROUGHT INTO THE HANGAR TO CARRY OUT A HARD LA NDING INSPECTION. DOUGLAS SERVICE MANUAL FOR HARD LANDING INSPECTIONS WAS USED AND IT WAS FOUND UPON REMOVAL OF THE RT MAIN WHEELS THAT THE RT OUTBOARD AXLE WAS BENT UP ABOUT 10 DEGREES. THE AXLE ASSEMBLY WAS REPLACED AND A GEAR SWING CAR RIED OUT. THE HARD LANDING INSPECTION WAS COMPLETED WITH NO FURTHER DEFECTS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4R 4 R A762 5E5 2003013000160 20030130 00160 EU 2003 1 30 CA021230003 1 20021228 A 2750 ABS012131 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE TE FLAPS FAILED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CA (CAN) FIVE CASES OF FLAP LOCK WITH NO MOVEMENT HAVE BEEN REPORTED SINCE 01 NOVEMBER. THERE WAS NO HARD FAULT AND FAULT C OULD NOT BE DUPLICATED ON THE GROUND. ITEMS CHANGED OR TESTED INCLUDE THE SLAT FLAP CONTROL COMPUTER (SFCC), ASYMMETRY P OSITION PICK OFF UNIT (APPU), VISUAL INSPECTION OF THE WHOLE MECHANICAL SYSTEM INCLUDING A CHECK FOR WATER INGRESSION IN THE ROTARY ACTUATORS, REPLACEMENT OF ROTARY ACTUATORS ON ADVICE FROM AIRBUS INDUSTRIES. THE LATEST FAULT WAS A HARD FAU LT, RT PROXIMITY SENSOR 38CV, WHICH WAS CLEANED AND OPERATIONAL TEST CARRIED OUT WITH NO FAULT. PROXIMITY SENSOR TO BE C HANGED WHEN PARTS AVAILABLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2003013000162 20030130 00162 EU 2003 1 30 CA021230004 1 20021203 A 2121 C209690D FAN SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE CABIN COOLING SEIZED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) AFTER ARRIVAL AND DURING UNLOADING OF THE PASSENGERS THE FLIGHT ATTENDANT NOTED AN ABNORMAL SMELL IN THE CABIN AND ALERTED THE FLIGHT CREW. THEY TOO NOTED THE ELECTRICAL TYPE SMELL AND ATTEMPTED TO DETERMINE THE SOURCE. THE RECIRCULAT ING FANS LOCATED UNDER THE CABIN FLOOR AT ROW 8 WERE SUSPECT. MAINTENANCE DETERMINED THAT THE LT RECIRC FAN HAD FAILED A ND WAS THE CAUSE OF THE SMELL. THE FAN WOULD EMIT SMOKE DURING ATTEMPTED OPERATION. THE FAN ASSY WAS REPLACED. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2003013000164 20030130 00164 EA 2003 1 30 CA021230006 2 20021125 A 7230 3017701 BLADE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA COMPRESSOR FRACTURED W C E D ABORTED TAKEOFF ENGINE SHUTDOWN RETURN TO BLOCK D B INFLIGHT SEPARATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) AS POWER WAS APPLIED TO THE ENGINE DURING TAXI TO TAKE-OFF POSITION, A LOUD NOISE WAS HEARD AND THE ENGINE PARAMET ERS BEGAN TO SPOOL DOWN. ENGINE WAS IMMEDIATELY SHUTDOWN. NO FURTHER INCIDENT OCCURRED AND THE CREW DEPLANED. A VISUAL I NSPECTION OF THE ENGINE SHOWED A FAILURE IN THE 1ST STAGE COMPRESSOR WITH MAJOR DAMAGE TO THE FIRST STAGE BLADES. THE EN GINE HAS BEEN SENT TO THE ENGINE SHOP FOR A TEADOWN REPORT. INITIAL FINDINGS INDICATE THAT A FIRST STAGE COMPRESSOR BLAD E APPEARS TO BE THE PRIMARY FAILED ITEM. THE BLADE IS CURRENTLY UNDERGOING A MATALLURIGICAL EXAMINATION TO DETERMINE THE CAUSE OF THE FAILURE. A FOLLOW UP REPORT WILL BE SUBMITTED ONCE THE SHOP FINDINGS ARE COMPLETED. 1 L 7 2 4T 4 T A24CE E4EA 2003013000165 20030130 00165 EA 2003 1 30 CA021231002 2 20021211 A 7321 324472111 FUEL CONTROL BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA ENGINE MALFUNCTIONED W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) WHILE STARTING, THE START WENT HOT & THE START WAS ABORTED. THE NEXT START WAS A VERY LONG START WITH THE N1 HANGI NG UP AT 71 PERCENT WITH NO ACCELERATION PAST 71 PERCENT. THE HELICOPTER WAS STARTED USING THE MANUAL FUEL CONTROL AND T HE START WAS NORMAL. THE P3 AIR LINES WERE LEAK CHECKED AND FOUND NO DECREPANCY.THE AUTOMATIC FUEL CONTROL UNIT WAS REPL ACED AND NO DEFECT WAS FOUND. THE AUTOMATIC FUEL CONTROL IS BEING SENT TO THE OVERHAUL VENDOR FOR EVALUATION. 1 G 7 1 4U 4 U H4SW E22EA 2003013000166 20030130 00166 WP 2003 1 30 ASAA0280354 1 20021004 A 5347 SR095301157003 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, SEAT TRACK CORRODED BEYOND LIMITS AT LBL 44 FROM FS 1176-1211. REPLACED SEAT TRACK FROM F S 1155-1231 PER SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2003022800053 20030228 00053 NM 2003 2 28 F3LA200300030 1 20020127 A 5320 CHANNEL BOEING 737 7373M8 1384615 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 3800 25039 DURING C-4 CHECK, INSPECTION REPORTED HAT SECTION BETWEEN STA 328 AND 344, RBL 12, CORRODED. FABRICATED AND INSTALLED R EPLACEMENT HAT CHANNEL PER SRM 51-40-02 AND BOEING DRAWING 65C34429. 2 L 7 2 4F RT A16WE 2003013100001 20030131 00001 SW 2003 1 31 CA021231003 1 20021211 A 6230 SPACER BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R MAST UNAPPROVED PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) SPACERS ARE USED IN-BETWEEN THE MAST NUT AND THE MAIN ROTOR TRUNNION. THE QUESTION WAS RAISED IS THIS A BELL PART. IT WAS FOUND AFTER ASKING BELL HELICOPTERS TEXTRON PRODUCT SUPPORT THAT THIS SPACER WAS NOT A REPLACEMENT PART FOR THE DYNAMIC FLAP RESTRAINT. THIS PART WAS NOT MANUFACTURED BY BELL HELICOPTERS. WHEN OR HOW THIS PART GOT INTO VIH SYSTEM UN KNOWN. THE SPACER IS ALUMINIUM ALLOY, ANODIZED, MANUFACTURED VERY WELL AND FITS THE TRUNNION WITH NO MIS-ALIGNMENT. THE ORIGINAL BELL FLAP RESTRAINT IS STEEL ALLOY. THIS PART IS IN QUARANTINE. 1 G 7 1 3U 3 U H2SW E4CE 2003013100002 20030131 00002 NE 2003 1 31 CA021231004 2 20021030 A 8560 SEAL DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE SUPERCHARGER CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) THE AIRCRAFT WAS CONSUMING MORE OIL THAN NORMAL I.E. 1 GALLON EVERY FLIGHT. THE AIRCRAFT WAS INSPECTED AND LARGE Q UANTITIES OF OIL WERE FOUND ON THE BELLY. IT WAS TROUBLESHOT BY AN AME TO BE A SUPERCHARGER OIL SEAL. THE AIRCRAFT WAS T AKEN IMMEDIATELY TO OUR AMO FOR REPAIR. THERE WERE NO SPECIAL OPERATING CONDITIONS EXCEPT THAT WE NEEDED TO CARRY MORE O IL TO COMPENSATE. 1 H 7 1 3R 3 R A806 5E1 2003013100003 20030131 00003 EU 2003 1 31 CA030102001 1 20020729 A 3242 16402201 BRAKE DISC CLEVELAND BNORM BN2 BN2A27 1520227 EU LYC O540 O540E4C5 41532 EA MLG WHEEL SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON FIRST CREW FIRST WALK AROUND AT 2300 HRS. CREW OBSERVED NR 4 BRAKE DISC WAS NOT STRAIGHT. FURTHER INVESTIGATION FOUND THAT THE NR 4 BRAKE DISC WAS SHEARED AROUND FLANGE AND SITTING CRACKED. MAINTENANCE WAS CALLED. A SERVICEABLE WH EEL ASSEMBLY WAS INSTALLED AND AIRCRAFT RETURNED TO SERVICE.AN INSPECTION WAS DONE ON THE OTHER 3 WHEEL ASSEMBLY AND NO DISCREPANCIES WERE OBSERVED. THE OPERATOR CHECKED ALL THEIR OTHER BN2AS AND NO DISCREPANCIES WERE OBSERVED. DEFECT WAS PUT DOWN TO OLD DISC (STILL WITHIN WEAR LIMITS). 1 H 7 2 3O 3 O A17EU E295 2003013100004 20030131 00004 NE 2003 1 31 CA030102002 1 20021202 A 2842 B12551 CONNECTOR SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE FUEL QTY LOOSE W A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION HO HOVERING 1 CA (CAN) WITH FUEL QTY GAUGES INDICATING 550 LBS IN THE FWD TANK & 500 LBS IN THE AFT TANK & LOW LEVEL WARNING LIGHTS ILLUM INTED, FLT CREW FELT THEY HAD ENOUGH FUEL REMAINING TO RETURN TO THE LOGGING AREA FOR ONE MORE TURN. WHILE PICKING UP TH E LAST TURN, BOTH OF THE AFT TANK BOOST PUMPS FAILED LIGHTS ILLUMINATED WITH 400 LBS OF FUEL INDICATED AND NR 2 ENGINE F LAMED OUT. PILOT ABORTED TURN & RETURNED TO SERVICE LANDING & MADE AN UNEVENTFUL SINGLE ENGINE LANDING. MAINT DISCOVERE D AFT FUEL TANK CONTAINED ONLY UNUSABLE FUEL, AND A LOOSE WIRING CONNECTION ON THE AFT TANK COMPENSATOR CAPACITOR, WIRI NG CONNECTOR WAS REPAIRED, A COMPLETE FUEL QTY SYSTEM CALIBRATION CHECK CARRIED OUT, THE AIRCRAFT WAS RELEASED FOR FLT. 2 G 7 2 4U 4 U H4EA E15EA 2003013100005 20030131 00005 NE 2003 1 31 CA030102003 2 20020120 A 8500 ENGINE PIPER PA31 PA31 7103102 SO LYC O540 TIO540J2B NE HARTZL HCC4Y HCC4YR2 GL LEFT MAKING METAL W A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CA 429361A (CAN) PILOT REPORTED LOW OIL PRESSURE READING 10 MINUTES PRIOR TO LANDING. VISUAL INSPECTION OF ENGINE EXTERIOR & OIL L EVEL CHECK CARRIED OUT BY PILOT. 3 LITERS OF OIL ADDED. AIRCRAFT TEST FLOWN, TAKEOFF NORMAL, RUN UP WAS NORMAL, AT CRUIS E POWER OIL PRESSURE STARTED DECREASING 5 MINUTES AFTER CRUISE POWER SET. AIRCRAFT RETURNED FOR LANDING. MAINTENANCE FL OWN DOWN TO INSPECT ENGINE. METAL FOUND IN OIL, OIL FILTER AND SCREEN. ENGINE TAKEN OFF LT SIDE OF AIRPLANE. AFTER ENGIN E OVERHAUL, FOUND THAT THE ENGINE CAMSHAFT LOBS WERE WEARING OUT CAUSING METAL PARTICLES IN THE ENGINE OIL. 1 L 7 2 3O 3 O A20SO E14EA 5 C P52GL 2003013100009 20030131 00009 2003 1 31 CA030103003 4 20021222 A 3457 CI4510700 ANTENNA BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU GPS/VHF SYS CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE ANTENNA IS INSTALLED ON THE AIRCRAFT FOR AN OSAT COMMUNICATION SYSTEM AS PART OF AN STC. CRACKS WE HAVE HAD IN THE PAST GENERALLY ARE HAIRLINE FRACTURES 3 INCHES UP FROM THE BASE, THIS ONE IS ALSO CRACKED COMPLETELY AROUUND THE BA SE AT THE CUTOUTS FOR THE TWO AFT ATTACHMENT SCREWS. THE ANTENNA WAS REPLACED. 2 L 7 2 3T 4 T A24EU A196 2003013100010 20030131 00010 EA 2003 1 31 CA030103004 2 20021105 A 8530 INTAKE VALVE HUGHES 269 269C1 8059504 SW LYC O360 HO360C1A 41514 EA NR 4 CYLINDER LEAKING W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) BASE LINE DIFFERENTIAL CHECK OF NEW AIRCRAFT REVEALED LEAKING NR 4 CYLINDER INTAKE VALVE. CYLINDER REMOVED AND REP AIRED. 1 G 7 1 3O 3 O O 4H12 E286 2003013100011 20030131 00011 WP 2003 1 31 CA030103008 2 20021129 A 7230 31037081 BEARING BAG JETSTM JETSTM3212 1500217 EU GARRTT TPE331 TPE33110UG 01514 WP ROTOL R333 R333482F12 GL COMPRESSOR SPALLED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON PREFLIGHT CHECK PILOT PULLED PROPELLER THROUGH BY HAND & NOTED UNUSUAL NOISE. THE PILOT THEN NOTIFIED MAINTENAN CE ABOUT AFFECTED ENGINE. MAINTENANCE AME PULLED PROPELLER THROUGH BY HAND VERIFYING UNUSUAL NOISE AND CHECKED CHIP DETE CTOR LIGHT WHICH WAS NOT ON. ENGINE WAS THEN DRY MOTORED AND CHIP DETECTOR LIGHT WAS RE CHECKED AND WAS FOUND TO BE ON. CHIP DETECTOR WAS THEN REMOVED & VISUALLY INSPECTED CONFIRMING METAL PRESENT (BEARING PLATELETS). ENGINE GEARBOX WAS THE N DISASSEMBLED & COMPRESSOR BEARING WAS FOUND TO BE SOURCE OF METAL. THE BEARING WAS IN INITIAL STAGE OF FAILURE OF INNE R RACE ON THRUST SIDE. NOTE: BEARING HAS 9,000 HOUR LIFE LIMIT. 2 L 7 2 4T 4 T RT BA15CAA E4WE 6 C P61GL 2003013100015 20030131 00015 NE 2003 1 31 CA030103012 2 20021223 A 7220 FITTING CESSNA CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE PICCOLO TUBE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) APPROXIMATELY 8 INCH CRACK WHERE FLANGE IS WELDED TO PICCOLO TUBE AND 2 INCH CRACK IN PICCOLO TUBE ON OTHER SIDE O F INLET FITTING RESULTING IN BLEED AIR LEAK. 1 L 7 2 4F 4 F A22CE E1NE 2003013100016 20030131 00016 EA 2003 1 31 CA030103013 1 20021203 A 3210 TBC6U114033 BLOCK DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACKS FOUND IN MIDDLE PART OF COMPRESSION BLOCKS WHERE PRELOAD BOLT PASSES THRU. CRACKS ARE FOUND TO RUN HORIZONT AL THRU BLOCKS. 1 H 7 2 3T 4 T RT A9EA E4EA 2003013100017 20030131 00017 GL 2003 1 31 CA030103014 2 20021031 A 7321 23065104 FUEL CONTROL BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL ENGINE FAILED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CA (CAN) TORQUE SPLIT REPORTED OF 6 TO 8 PERCENT IN CRUISE. AFTER A TEST FLIGHT TO DETERMINE WHICH GOVENOR WAS AT FAULT IT WAS DETERMINED THAT THE FCU WAS THE CAUSE FOR THE TORQUE SPLIT. THE FCU WAS REPLACED & A/C RETURNED TO SERVICE. 1 G 7 2 3U 3 U H3EU E4CE 2003013100019 20030131 00019 SW 2003 1 31 CA030103016 1 20021223 A 6320 206040544001 TUBE BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL GEARBOX OIL CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) AFTER A FLIGHT OF 3.7 HOURS, WHILE DOING THE DAILY INSPECTION A LARGE PATCH OF OIL WAS FOUND UNDER THE HELICOPTER. THE BELLY WAS COVERED BY OIL. INVESTIGATION REVEALED 2 TUBES FROM THE TRANSMISSION TO THE OIL COOLER HAD CHAFED AGAINS T EACH OTHER AND WERE CHAFED THROUGH. THE TUBES WERE REPLACED AND A/C RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 2003013100021 20030131 00021 NM 2003 1 31 QXEA0202048 1 20021126 A 5410 STRUT DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX- NR 2 ENGINE UPPER OUTBOARD SUPPORT STRUT IS CHAFFED ON INBOARD AFT SIDE. REPAIRED IAW DHC-8 RD 8-54-036. 2 H 7 2 4T RT A13NM 2003013100022 20030131 00022 EA 2003 1 31 QXEA0202084 1 20021203 A 3260 895302 ECU CNDAIR CL600 CL6002C10 1390015 EA E/E BAY MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 602QX 2663 10010 PHX - FOLLOWING GEAR UP SELECTION, GEAR DISAGREE WARNING CAME ON ACCOMPANIED BY PROX SYSTEM 1 FAULT STATUS MESSAGE. MAIN TENANCE INTERROGATED THE MAINTENANCE DIAGNOSTICS COMPUTER AND THERE WERE NO CURRENT FAULTS. THE MAIN LANDING GEAR SELECT OR VALVE AND PROX SENSORS WERE CHECKED WITH NO DEFECTS NOTED. THE LANDING GEAR WAS CYCLED SEVERAL TIMES WITH NO DEFECTS NOTED. THE PSEU WAS REPLACED AS A PRECAUTIONARY PROCEDURE AND OPERATIONAL CHECKS WERE PERFORMED AGAIN AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013100023 20030131 00023 EA 2003 1 31 QXEA0202086 1 20021204 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A QXEA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 09 611QX 10041 PDX- CARGO SHUTOFF VALVE FAIL STATUS MESSAGE. CYCLED SHIPS POWER. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013100024 20030131 00024 EA 2003 1 31 QXEA0202087 1 20021203 A 2150 GG670960091 ACM CNDAIR CL600 CL6002C10 1390015 EA A/C BAY FAILED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 606QX 2802 10023 PDX- FOLLOWING ENGINE START CABIN AND COCKPIT FILLED WITH SMOKE FROM AIR DUCTS. RECEIVED SMOKE AFT LAVATORY WARNING. RI GHT PACK AUTO FAIL MESSAGE FOLLOWED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AIR CYCLE MACHINE. OPERATIONA L CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013100025 20030131 00025 NM 2003 1 31 QXEA0202096 1 20021202 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - SEAT TRACK NR 11 HAS A DEEP CORROSION PIT AT STATION 502.00. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2003013100026 20030131 00026 NM 2003 1 31 QXEA0202097 1 20021202 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - NR 10 SEAT TRACK RIGHT HAND FORWARD OUTBOARD HAS THREE AREAS OF DEEP CORROSION AT STATION 279.00, 315.00 AND 327.0 0. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2003013100027 20030131 00027 NM 2003 1 31 QXEA0202098 1 20021203 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT WING SPAR LOWER CAP FORWARD BOTTOM EDGE GOUGED AT YW202.00. REPAIRED IAW HORIZON AIR EA 2-57-212. 2 H 7 2 4T RT A13NM 2003013100028 20030131 00028 NM 2003 1 31 QXEA0202099 1 20021203 A 5220 STOP FITTING DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - FORWARD RIGHT HAND EMERGENCY DOOR, THREE BOTTOM STOPS ON DOOR HAVE MINOR CHAFE DAMAGE ON CONTACT SURFACE. REPAIRE D IAW DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100030 20030131 00030 NM 2003 1 31 CA030103018 1 20021220 A 3110 82210021005 DISPLAY DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE INSTRUMENT PANEL FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) UPON ARRIVAL CREW NOTICED A/C WOULD NOT ACCEPT GROUND POWER. CALLED FOR A SECOND GPU, AND WHEN GROUND POWER WAS SE LECTED, CREW NOTICED SMOKE COMING FROM GLARESHIELD AREA, SPECIFICALLY ON THE LT SIDE BY THE CAPTAIN'S CLOCK. PASSENGERS DEPLANED MAINTENANCE FOUND THAT NAV MODE DISPLAY PANEL IN GLARE SHIELD HAD BURNED CIRCUITS DUE TO AN OVERVOLTAGE SURGE. SUBSEQUENTLY ALSO REPLACED AFCS INTERFACE UNIT PN 8341002021 SN OFF 0210029 DUE TO BURNED CIRCUITBOARD, DIRECTION GYRO C ONTROL PN 83423051-005 SN OFF 0016 DAMAGED BY VOLTAGE SPIKE, AND CABIN PRESS IND PN SETLOC420F SN 25 DUE TO DAMAGE FROM VOLTAGE SPIKE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003013100031 20030131 00031 EA 2003 1 31 QXEA0202100 1 20021205 A 7933 4120T19P02 SENSOR CNDAIR CL600 CL6002C10 1390015 EA LT ENGINE FAILED A QXEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 09 600QX 10005 PDX- DURING FLIGHT SEA-FAT AIRCRAFT DIVERTED TO PDX DUE TO: AT CRUISE POWER FLIGHT LEVEL 370 NOTED LEFT ENGINE TEMPERATU RE IN RED AT 164 DEGREES FLUCTUATING TO 145 DEGREES. SHORTLY AFTER "LOW OIL QUANTITY" STATUS MESSAGE. REDUCED POWER ON LEFT ENGINE TO BRING TEMPERATURE INTO NORMAL RANGE. OIL PRESSURE REMAINED CONSTANT AND NORMAL THROUGHOUT. AIRCRAFT LA NDED WITHOUT INCIDENT. REMOVED AND REPLACED OIL LEVEL/TEMPERATURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013100032 20030131 00032 NM 2003 1 31 QXEA0202101 1 20021203 A 7110 WEB BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX- LEFT HAND LOWER COWL AFT CONE WEB CRACKED AT UPPER DECK ATTACHMENT. REPAIRED IAW DHC-8 Q400 RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003013100033 20030131 00033 NM 2003 1 31 QXEA0202102 1 20021203 A 7110 WEB BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX- RIGHT HAND LOWER COWL AFT CONE WEB IS CRACKED AT UPPER DECK ATTACHMENT. REPAIRED IAW DHC-8 Q400 MM 71-61-01 TEMP R EVISION 71-054 AND RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003013100035 20030131 00035 NM 2003 1 31 CA030103021 1 20021220 A 2760 7G772 PRESSURE SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ROLL SPOILER FAILED W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA (CAN) APPROXIMATELY HALF WAY TO DESTINATION, INBOARD ROLL SPOILER HYDRAULIC CAUTION LIGHT ILLUMINATED. OPERATION OF SPO ILERS APPEARED NORMAL. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. MAINTENANCE REPLACED ROLL SPOILER INBOARD HYDRAULIC PRESS URE SWITCH. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003013100036 20030131 00036 EA 2003 1 31 QXEA0202104 1 20021207 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 09 610QX 1999 10033 PDX-INTERMITTANT AMBER LOW PRESSURE MESSAGE ON FUEL SYNOPTIC PAGE. THE MESSAGE WAS NOT ACCOMPANIED BY ANY CAUTIONS OR W ARNINGS. REPLACED LEFT HAND ENGINE INLET PRESSURE SENSOR. OPERATIONAL CHECK GOOD. NO LEAKS. GROUND RAN ENGINES AND N O TOGA FAULT APPEARED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013100037 20030131 00037 NM 2003 1 31 QXEA0202105 1 20021203 A 5414 PANEL DHAV DHC8 DHC8202 2809007 NM NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - CHAFING ON PANEL 412BT. REPAIRED IAW DHC-8 200 SRM 54-00-16, PAGE 2, TABLE 1. 2 H 7 2 4T RT A13NM 2003013100038 20030131 00038 NM 2003 1 31 QXEA0202106 1 20021203 A 5753 BEAM DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT HAND NR 4 FLAP BEAM, TRACK E, OUTBOARD SIDE HAS A PIT IN PLATING AT O POSITION. REPAIRED IAW HORIZON AIR EA 2-57-210. 2 H 7 2 4T RT A13NM 2003013100039 20030131 00039 NM 2003 1 31 QXEA0202108 1 20021203 A 5753 BEAM DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT HAND NR 4 FLAP BEAM, OUTBOARD TRACK C HAS PIT IN PLATING AFT OF O POSITION. REPAIRED IAW HORIZON AIR EA 2-5 7-210. 2 H 7 2 4T RT A13NM 2003013100040 20030131 00040 NM 2003 1 31 QXEA0202109 1 20021203 A 5753 BEAM DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT HAND NR 5 FLAP BEAM, TRACK A HAS A PIT AT O POSITION. REPAIRED IAW HORIZON AIR EA 2-57-210. 2 H 7 2 4T RT A13NM 2003013100042 20030131 00042 NM 2003 1 31 QXEA0202110 1 20021203 A 5753 BEAM DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT HAND NR 5 FLAP BEAM INBOARD TRACK E HAS A .075 INCH DIAMETER PIT AT O POSITION. REPAIRED IAW HORIZON AIR EA 2-57-210 AND EA 2-57-211. 2 H 7 2 4T RT A13NM 2003013100043 20030131 00043 NM 2003 1 31 QXEA0202111 1 20021203 A 5753 BEAM DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT HAND NR 4 FLAP BEAM INBOARD TRACK C HAS A .160 INCH BY .085 INCH PIT AT O POSITION. REPAIRED IAW HORIZON AI R EA 2-57-210. 2 H 7 2 4T RT A13NM 2003013100044 20030131 00044 NM 2003 1 31 QXEA0202112 1 20021203 A 5753 BEAM DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT HAND NR 4 FLAP BEAM, INBOARD TRACK B HAS A .090 INCH DIAMETER PIT AT O POSITION. REPAIRED IAW HORIZON AIR E A 2-57-210. 2 H 7 2 4T RT A13NM 2003013100045 20030131 00045 NE 2003 1 31 CA030106001 2 20021231 A 7230 CF343A1 COMPRESSOR WHEEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT ENGINE VIBRATION W E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA (CAN) FLT 5848, TPA-CVG, CLIMBING THROUGH 11,500FT, LT ENGINE FAN VIBRATION WARNING AND ITT INDICATED RED. N1 DECREASED RAPIDLY WITH NOISE. QRH AND MEMORY ITEMS FOLLOWED. OVERWEIGHT SINGLE ENGINE LANDING PER FORMED AT 48,950 LBS. VSI AT LANDING WAS LESS THAN 200 FT/MIN. EMERGENCY DECLARED AND AIRCRAFT LANDED AT TPA WITHOUT FURTHER INCIDENTS. ENGINE SHO WS NO SIGN OF OIL LOSS.CHIP DETECTOR IS CLEAN. SUSPECT COMPRESSOR DAMAGE. MDC SHOWS ITT PEAKED AT 1233 DEG C OF 71 SECO NDS. ENGINE REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2003013100046 20030131 00046 NM 2003 1 31 QXEA0202113 1 20021205 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - WING MATING SURFACE APERTURE FOR PANEL 524AT HAS FIFTEEN HOLES WITH RAISED METAL. REPAIRED IAW RD 8-57-611. 2 H 7 2 4T RT A13NM 2003013100047 20030131 00047 NM 2003 1 31 QXEA0202114 1 20021205 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - ELONGATED HOLE IN BRACKET FORWARD AREA OF CARGO DOOR THRESHOLD AT STATION 547.50. REPAIRED IAW HORIZON AIR EA 2-5 3-450. 2 H 7 2 4T RT A13NM 2003013100048 20030131 00048 CE 2003 1 31 CA030106002 1 20021125 A 2460 GMW1 FUSE BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE EFIS STBY PWR BLOWN W O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 CA BB1601 (CAN) FUSE (GMW1) HAS POPPED ON THREE DIFFERENT COMPANY B200 AIRCRAFT. FUSE PROJECTS 28 VDC OUTPUT CIRCUIT FROM THE EFIS STANDBY POWER SUPPLY (WIRES W3203-2 AND W3204-4). HAVE SUBMITTED QUERY TO RAYTHEON TECH SUPPORT FOR RECTIFICATION. 1 L 7 2 4T 4 T A24CE E4EA 2003013100049 20030131 00049 NM 2003 1 31 QXEA0202115 1 20021206 A 1430 SCREW DHAV DHC8 DHC8202 2809007 NM ELEVATOR LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - FOUND A SCREW WEDGED IN LEFT HAND ELEVATOR LEADING EDGE TO COVE GAP, ELEVATOR MOVEMENT CAUSED A GOUGE IN ELEVATOR LEADING EDGE. REPAIRED IAW DHC-8 200 MM 27-32-11-400-801 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2003013100050 20030131 00050 NM 2003 1 31 QXEA0202116 1 20021203 A 5210 STOP FITTING DHAV DHC8 DHC8202 2809007 NM PAX DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - MAIN CABIN DOOR ALL DOOR STOP PADS ARE WORN APPROXIMATELY .005. REPAIRED IAW RD 8-53-3933 AND RD 8-51-103. 2 H 7 2 4T RT A13NM 2003013100051 20030131 00051 NM 2003 1 31 QXEA0202117 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - SEAT TRACK NR 8 CORROSION ON THE UPPER SURFACE AT APPROXIMATELY STATION 502. REPAIRED IAW DHC-8 200 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100052 20030131 00052 NM 2003 1 31 QXEA0202118 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCORED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - SEAT TRACK NR 8 HAS TWO LENGTH WISE SCORE MARKS APPROXIMATELY AT STATION 514.5. REPAIRED IAW DHCC-8 200 SRM 51-20 -16. 2 H 7 2 4T RT A13NM 2003013100054 20030131 00054 NM 2003 1 31 QXEA0202119 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCORED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - SEAT TRACK NR 12 HAS SCORE MARKS AT STATION 522 AND 521. REPAIRED IAW DHC-8 200 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100055 20030131 00055 NM 2003 1 31 QXEA0202120 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GROOVED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - TRACK NR 3 HAS LIGHT LENGTH WISE GROOVES ALONG THE INNER AREA OF THE TRACK AT APPROXIMATELY STATION 428.00. REPAI RED IAW DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100056 20030131 00056 NM 2003 1 31 QXEA0202121 1 20021204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - SEAT TRACK NR 7 FORWARD INBOARD RIGHT HAND HAS SEVERAL AREAS OF DEEP CORROSION PITS AT APPROXIMATELY STATION 213. REPAIRED IAW DHC08 SRM 51-30-26 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2003013100058 20030131 00058 EA 2003 1 31 CA030106006 1 20021220 A 2797 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE SPOILERON PCU DAMAGED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) UPON LANDING ONE OF THE RT SPOILERS DEPLOYED ON THE TAXI IN FOR NO APPARENT REASON. RT O/B SPOILERON PCU FOUND TO HAVE A NUMBER OF PINS IN THE CONNECTOR PLUG PUSHED BACK IN. THE SPOILER ELECTRONIC CONTROL UNIT PN 4916405, SN 0599 WAS ALSO REPLACED DUE TO A 'MODULE B' FAILURE INDICATION. 2 L 7 2 4F 4 F RT A21EA E15NE 2003013100059 20030131 00059 NM 2003 1 31 QXEA0202122 1 20021204 A 5280 MOUNT BRACKET DHAV DHC8 DHC8202 2809007 NM RT MLG DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT HAND MAIN LANDING GEAR AFT GEAR DOOR MOUNT BRACKET HAS MINOR CHAFING FROM GRAVEL GUARD. REPAIRED IAW RD 8-5 4-1052. 2 H 7 2 4T RT A13NM 2003013100060 20030131 00060 NM 2003 1 31 QXEA0202123 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - LEFT HAND INBOARD SEAT TRACK X545 HAS A GOUGE IN THE CHANNEL. REPAIRED IAW DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100061 20030131 00061 EA 2003 1 31 CA030106007 2 20021112 A 7230 310686201 STATOR BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA HARTZL HCD4N3 HCD4N3A GL COMPRESSOR FAILED W E C ENGINE SHUTDOWN ABORTED TAKEOFF B K J SMOKE/FUMES/ODORS/SPARKS FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CA (CAN) AT TAKEOFF POWER, SMOKE WAS NOTED IN THE COCKPIT & TAKEOFF WAS ABORTED, ENGINE SHUTDOWN AND TOWED BACK TO MAINTENA NCE FACILITY. OIL WAS EVIDENT ON THE COWLINGS, AFTER EXTENSIVE TROUBLESHOOTING, THE ENGINE WAS REMOVED AND SENT TO AN OV ERHAUL FACILITY. THE FACILITY DISCOVERED THAT THE FIRST STAGE COMPRESSOR STATOR FAILED DUE TO FATIGUE. 1 L 7 2 4T 4 T A24CE E4EA 5 C STC 2003013100062 20030131 00062 NM 2003 1 31 QXEA0202124 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - LEFT HAND INBOARD SEAT TRACK X506 HAS A CORROSION PIT IN THE CHANNEL. REPAIRED IAW RD 8-53-1339 AND DHC-8 SRM 51- 20-16. 2 H 7 2 4T RT A13NM 2003013100063 20030131 00063 NM 2003 1 31 QXEA0202125 1 20021202 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - LEFT HAND INBOARD SEAT TRACK AT X488 HAS A PREVIOUSLY BLENDED GOUGE. REPAIRED IAW HORIZON AIR EA 2-53-241. 2 H 7 2 4T RT A13NM 2003013100064 20030131 00064 NM 2003 1 31 QXEA0202126 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - LEFT HAND INBOARD SEAT TRACK X446 TO X455 HAS GOUGES IN CHANNEL. REPAIRED IAW DHC-8 200 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100065 20030131 00065 SO 2003 1 31 CA030106008 1 20021212 A 2434 2929316 WIRE PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA LT GENERATOR BURNED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 10491 (CAN) DURING CRUISE, THE LT GENERATOR INOP LIGHT CAME ON, THE PILOT ATTEMPTED TO CYCLE THE GENERATOR SWITCH, BUT FAILED AGAIN TO COME BACK ON LINE. MAINTENANCE FOUND THE WIRE CABLE ASSEMBLY BURNED NEAR THE CROSS TIE SWITCH AT THE CRIMPED TE RMINAL. THIS ASSEMBLY WAS MADE USING ALUMINUM WIRE. AND OWING TO THE HIGH AIRFRAME TIME WAS THE PROBLEM CAUSE. ASSEMBLY WAS REPLACED USING COPPER WIRE. 1 L 7 2 3T 4 T A8EA E4EA 2003013100066 20030131 00066 NM 2003 1 31 QXEA0202127 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GROOVED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - LEFT HAND INBOARD SEAT TRACK X475 TO X488 HAS GROOVES IN TRACK. REPAIRED IAW DHC-8 200 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100067 20030131 00067 NM 2003 1 31 QXEA0202128 1 20021206 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - LEFT HAND INBOARD SEAT TRACK X206 HAS A PIT ON THE OUTBOARD FLANGE. REPAIRED IAW DHC-8 SRM 51-30-26 AND SRM 51-40 -11. 2 H 7 2 4T RT A13NM 2003013100068 20030131 00068 NM 2003 1 31 QXEA0202129 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - LEFT HAND OUTBOARD SEAT TRACK X542 HAS A GOUGE IN THE CHANNEL. REPAIRED IAW RD 8-53-3644 AND DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100069 20030131 00069 NM 2003 1 31 QXEA0202130 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - LEFT HAND OUTBOARD SEAT TRACK X468 TO X486 TOP CAPS HAVE LIGHT CORROSION. REPAIRED IAW DHC-8 200 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100070 20030131 00070 CE 2003 1 31 CA030106010 1 20021206 A 5210 521130014 DOOR CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO MCAULY 3AF32C 3AF32C505 GL CREW/PAX SEPARATED W O OTHER D INFLIGHT SEPARATION CR CRUISE 1 CA 21420 21420 (CAN) THE AIRCRAFT WAS IN LEVEL FLIGHT WHEN SUDDENLY WITHOUT ANY WARNING, THE CREW DOOR SEPARATED FROM THE AIRCRAFT. THE PILOT & COPILOT BOTH CONFIRMED THAT THE DOOR WAS CLOSED, LATCHED AND LOCKED CORRECTLY . THEY THEN EXTENDED THE GEAR & D ROPPED THE FLAPS TO SLOW THE AIRCRAFT DOWN BECAUSE IT WAS VERY COLD OUTSIDE. THE AIRCRAFT HAD NO PASSENGERS ON BOARD, IT WAS RETURNING BACK TO BASE AFTER DELIVERING A LOAD OF FREIGHT. IT IS HARD TO DETERMINED WHAT HAPPENED WITHOUT THE DOOR. THEY WERE AT 4,000 FEET OVER A LAKE WHEN THEY LOST THE DOOR. THERE ARE NO SIGNS OF FAILURE ON THE AIRFRAME EXCEPT WHERE THE DOOR BROKE OFF (FRESH BREAK). 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2003013100071 20030131 00071 NM 2003 1 31 CA030106011 1 20021227 A 6120 M832481111 O-RING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PROP CONTROL WORN W K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 CA (CAN) DURING ENGINE RUNS FOR FUNCTION CHECKS AFTER PREVIOUS MAINTENANCE, MAINTENANCE PERSONNEL NOTED THAT NR 1 PROP WAS VERY SLOW TO COME OUT OF FEATHER (30 SEC) IF IT WOULD COME OUT OF FEATHER AT ALL. ON NR 1 PROP TRANSFER TUBE FOUND ONE O -RING WORN AND ONE O-RING MISSING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003013100074 20030131 00074 CE 2003 1 31 CA030106013 1 20020821 A 5753 122101015 FLAP TRACK CESSNA 182 182P 2075816 CE CONT O470 O470S 17026 SO MCAULY 2A34C D2A34C58 GL LT WING CRACKED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA (CAN) A SPLIT FLAP CONDITION OCCURRED WHEN THE FLAPS WERE RAISED FROM 30 DEGREES TO ZERO DEGREE. THE UPPER FLAP SUPPORT CAUGHT THE FLAP TRACK SKIN SUPPORT BRACKET CAUSING LEFT FLAP TO JAM AND THE RIGHT FLAP TO CONTINUE TO GO UP. 1 H 7 1 3O 3 O NT TA13 E273 5 C P3EA 2003013100075 20030131 00075 EA 2003 1 31 CA030106014 1 20021227 A 2910 82970009173 TUBE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING MAINTENANCE A HYDRAULIC LEAK WAS NOTICED IN L/H MAIN LANDING GEAR WHEEL WELL. NR 2 SYSTEM DOORS CLOSED TUBE ASSY WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003013100076 20030131 00076 NM 2003 1 31 CA030106015 1 20021228 A 2760 PRESSURE SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ROLL SPOILER FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CA (CAN) A/C WAS LINED UP FOR TAKE OFF WHEN THE ROLL SPOILER OUTBOARD CAUTION LIGHT ILLUMINATED. CREW UNABLE TO EXTINGUISH LIGHT, A/C RETURNED TO GATE. ROLL SPOILER CAUTION LIGHT PRESSURE SWITCH IN RT NACELLE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003013100078 20030131 00078 NM 2003 1 31 QXEA0202131 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - LEFT HAND OUTBOARD SEAT TRACK X380 HAS ONE GOUGE ON THE TOP CAP. REPAIRED IAW DHC-8 200 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100079 20030131 00079 NM 2003 1 31 QXEA0202132 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - LEFT HAND OUTBOARD SEAT TRACK X284.5 HAS TWO CORROSION PITS IN THE CHANNEL. REPAIRED IAW DHC-8 200 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100080 20030131 00080 NM 2003 1 31 QXEA0202133 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - LEFT HAND OUTBOARD X348.5 SEAT TRACK HAS ONE PIT IN CHANNEL. REPAIRED IAW DHC-8 200 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100082 20030131 00082 NM 2003 1 31 QXEA0202134 1 20021205 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - LEFT HAND OUTBOARD SEAT TRACK X275.5 HAS A GOUGE IN THE CHANNEL. REPAIRED IAW DHC-8 200 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100083 20030131 00083 NM 2003 1 31 QXEA0202135 1 20021206 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - FORWARD UPPER DOOR STOP CASTING CHAFED WHERE STOP CONTACTS FACE, NR 2 STOP. REPAIRED IAW RD 8-53-104. 2 H 7 2 4T RT A13NM 2003013100084 20030131 00084 NM 2003 1 31 QXEA0202136 1 20021206 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - LOWER FORWARD DOOR STOP CASTING CHAFED WHERE STOP CONTACTS FACE, NR 9 STOP. REPAIRED IAW DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100085 20030131 00085 NM 2003 1 31 QXEA0202137 1 20021206 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - UPPER AFT CARGO DOOR STOP CASTING CHAFED WHERE STOP CONTACTS FACE, NR 8 STOP. REPAIRED IAW DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003013100086 20030131 00086 NM 2003 1 31 QXEA0202138 1 20021206 A 5751 AILERON DHAV DHC8 DHC8202 2809007 NM RT WING LIGHTNING STRIKE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT AILERON TRAILING EDGE HAS LIGHTNING DISCHARGE DAMAGE 2 INCHES OUTBOARD OF FIXED TAB. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 57-60-71. 2 H 7 2 4T RT A13NM 2003013100087 20030131 00087 NM 2003 1 31 QXEA0202139 1 20021206 A 5751 AILERON DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT AILERON TRAILING EDGE CHAFED BY BONDING JUMPER AT TRIM TAB INBOARD HINGE. REPAIRED IAW HORIZON AIR EA 2-57- 213. 2 H 7 2 4T RT A13NM 2003013100089 20030131 00089 NM 2003 1 31 QXEA0202140 1 20021208 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - NUMEROUS DENTS IN FUSELAGE, FORWARD OF AFT CARGO DOOR. REPAIRED IAW DHC-8 200 SRM 51-20-11 AND SRM 51-20-26, PAGE 7. 2 H 7 2 4T RT A13NM 2003013100090 20030131 00090 NM 2003 1 31 QXEA0202141 1 20021207 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM FUSELAGE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - SMOKING RIVETS 12 INCHES OUTSIDE PARKING BRAKE PRESSURE GAUGE. REPAIRED IAW DHC-8 SRM 51-40-11, PAGES 1-4. 2 H 7 2 4T RT A13NM 2003013100091 20030131 00091 NM 2003 1 31 QXEA0202142 1 20021203 A 5280 HINGE DHAV DHC8 DHC8202 2809007 NM MLG DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - NR 2 MAIN LANDING GEAR NACELLE CUTOUT FOR FORWARD MAIN LANDING GEAR DOOR AFT HINGE HAS CHAFING ON RIB, FORWARD SID E OF HINGE CUTOUT. REPAIRED IAW DHC-8 SRM 51-20-26, PAGE 7, PARAGRAPH 5. 2 H 7 2 4T RT A13NM 2003013100092 20030131 00092 NM 2003 1 31 QXEA0202143 1 20021207 A 7110 ANGLE BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 PDX - LEFT HAND LOWER COWL, RIGHT HAND ANGLE ON THE BYPASS DOOR OPENING IS CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003013100093 20030131 00093 NM 2003 1 31 QXEA0202144 1 20021207 A 7110 ANGLE BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 PDX - LEFT HAND LOWER COWL, LEFT HAND SIDE ANGLE AT BYPASS DOOR IS CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003013100094 20030131 00094 NM 2003 1 31 QXEA0202145 1 20021207 A 7110 WEB BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 PDX - LEFT HAND LOWER COWL, AFT CONE CENTER SUPPORT WEB AND ANGLES CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003013100095 20030131 00095 NM 2003 1 31 QXEA0202146 1 20021206 A 7110 WEB BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 PDX - RIGHT HAND LOWER COWL, AFT CONE CENTER SUPPORT WEB AND ANGLES CRACKED. REPAIRED IAW Q400 MM 71-61-01, TEMP REVISI ON 71-054, PARAGRAPH 4. 2 H 7 2 4T RT A13NM 2003013100096 20030131 00096 NM 2003 1 31 QXEA0202147 1 20021207 A 7110 SUPPORT ANGLE BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 PDX - LEFT HAND LOWER COWL AFT STRUCTURE VERTICAL SUPPORT ANGLE, LEFT HAND SIDE OF BYPASS DOOR HINGE MOUNT CRACKED. REPA IRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003013100097 20030131 00097 2003 1 31 CA030106016 4 20021120 A 6122 210718 GOVERNOR RKWELL 700 700 7630520 SW LYC O540 TIO540R2AD 41532 EA RT PROPELLER FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA (CAN) PILOTS NOTICED RT ENGINE GOING INTO OVERSPEED CONDITION. IMMEDIATELY TRIED TO REDUCE ENGINE RPM WITH THROTTLE & PROP CONTROL, NO SUCCESS. ELECTED TO SHUTDOWN & SECURE RT ENGINE AFTER WHICH THEY CONTACTED TORONTO CENTER AND INFORMED THEM THAT THEY WERE ON ONE ENGINE AND WERE DECLARING AN EMERGENCY TO RECEIVE PRIORITY INTO CYTS. CONTINUED FLIGHT, LANDE D, TAXIED TO RAMP WITHOUT INCIDENT. NO DAMAGE TO AIRFRAME AND NO INJURIES OCCURRED. IT HAS BEEN CONFIRMED THAT THIS SITU ATION WAS A RESULT OF A FAILURE OF THE RT PROP GOVERNOR. IT HAS BEEN CONFIRMED THAT THE PROP GOVERNOR HAD AN INTERNAL FA ILURE WHICH CAUSED THE OVERSPEED CONDITION. NO USE OF EMERGENCY EQUIPMENT OR PERSONNEL WAS REQUIRED AFTER LANDING. 1 L 7 2 3O 3 O A12SW E14EA 2003013100098 20030131 00098 SW 2003 1 31 CA030106017 1 20020827 A 2750 AN38022 COTTER PIN BBAVIA 7 7GCBC 1220601 SW LYC O320 O320A2D 41508 EA FLAP HANDLE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING A SCHEDULED INSPECTION THE FLAP HANDLE RELEASE ASSEMBLY WAS NOT ENGAGING THE FLAPS IN THE CORRECT DEGREES S ETTING. UPON INVESTIGATING THE FLAP HANDLE ASSEMBLY, WE FOUND A BROKEN COTTER PIN PN 38022 LOCATED IN THE RELEASE ASSEM BLY. THE FLAP HANDLE ASSEMBLY WAS REMOVED, NEW COTTER PIN INSTALLED IN THE RELEASE ASSEMBLY. REINSTALLED, INDEPENDENT CH ECK CARRIED OUT AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 H 7 1 3O 3 O NC A759 E274 2003013100100 20030131 00100 NM 2003 1 31 CA030106019 1 20021230 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 15553 (CAN) NR 1 ENGINE OIL COOLER FOUND TO HAVE SEVERE OIL LEAK IN FIN AREA BY VERNATHERM END OF OIL COOLER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2003013100101 20030131 00101 NM 2003 1 31 QXEA0202148 1 20021206 A 6120 69901800 CONTROL UNIT BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA PROPELLER FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 403QX 543 543 4037 PDX- RETURNED TO FIELD DUE TO POWER PLANT MESSAGE DURING CLIMB AFTER TAKE OFF. ALL OTHER INDICATIONS NORAML. NO CAUTION LIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PROPELLER ELECTRONIC CONTROL. OPERATIONAL CHECKS GOOD. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003013100102 20030131 00102 NE 2003 1 31 QXEA0202149 2 20021208 A 7250 4124T31P03 TURBINE BLADES CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ENGINE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 2923 10024 965243 PDX - DURING SCHEDULED BORESCOPE INSPECTION FOUND TOP ONE THIRD OF THREE TURBINE BLADES IN THE HPT DISK MISSING. REPLAC ED ENGINE. REPLACED ENGINE. OPERATIONAL OF AIRCRAFT CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATIO N AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO TH E HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2003013100103 20030131 00103 EU 2003 1 31 CA030106020 1 20021101 A 7830 A7611511900000 PLATE AIRBUS 310 A310300 3930305 EU GE CF6 CF680C2A5 NE LEVER ARM BENT W O OTHER E VIBRATION/BUFFET LD LANDING 1 CA (CAN) A/C WAS COMING OUT OF AC CHECK AND DURING FERRY FLT CREW REPORTED THAT THEY WERE UNABLE TO OBTAIN FULL REVERSE THR UST ON EITHER ENGINE ON LANDING. PILOT WAS UNABLE TO MOVE THRUST LEVERS TO FULL REVERSE POSITION AND MAXIMUN REVERSE THR UST ACHIEVED WAS 40 PERCENT N1. DURING ASSOCIATED TROUBLESHOOTING, AN INSPECTION OF THROTTLE CONTROL PRIMARY TRANSMISSI ON ASSY WAS CARRIED OUT AND FOUND LOWER CAMPLATE ASSY DAMAGED ON BOTH ENGINES. NR 2 ENGINE LEVER CAMPLATE WAS REMOVED AND ITS BEARING WAS FOUND SEIZED. DURING THE C CHECK THE TRANSCOWLS WERE REPLACED BUT NO DISCREPENCIES WERE REPORTED REG ARDING THE THRUST REVERSER SYSTEM . 2 L 7 2 4F 4 F RT A35EU E13NE 2003013100105 20030131 00105 EA 2003 1 31 QXEA0202150 1 20021208 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 608QX 118 118 10026 PDX- FUEL LEAKING FROM NR 1 ENGINE FUEL INLET PRESSURE SENSOR IN LEFT HAND WHEEL WELL. REMOVED AND REPLACED NR 1 PRIMAR Y EJECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013100108 20030131 00108 EA 2003 1 31 QXEA0202151 1 20021206 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 601QX 705 705 10009 SEA- 'LEFT AND RIGHT FUEL PUMP ON' EICAS MESSAGE. CYCLED ON/OFF FOR 35 MINUTES UNTIL DESCENDING OUT OF FLIGHT LEVEL 390 . AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LEFT AND RIGHT PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013100111 20030131 00111 EA 2003 1 31 QXEA0202152 1 20021208 A 2824 P93A25602 CARTRIDGE CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 606QX 47 47 10023 BOI- TRANSFER PUMP CAUTION AND RIGHT TRANSFER PUSH LIGHT INDICATOR FAIL. SAME RESULTS WITH LEFT TRANSFER PUSH LIGHT SEL ECTED AND AUTO OVERRIDE SELECTED. PROBLEM CLEARED IN 30 MINUTES. REMOVED AND REPLACED BI-CROSSFLOW PUMP CARTRIDGE. 2 L 7 2 4F RT A21EA 2003013100112 20030131 00112 EA 2003 1 31 QXEA0202153 1 20021210 A 2782 766367A ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA L/E SLAT FAILED A QXEA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 09 605QX 2830 10022 PDX - CREW REPORTED A INTERMITTENT SLAT FAULT MESSAGE DURING DESCENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED T HE RIGHT NR 6 SLAT ACTUATOR. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013100113 20030131 00113 NM 2003 1 31 QXEA0202154 1 20021210 A 5240 COVER BOMBDR DHC8 DHC8401 1390041 NM SERVICE DOOR OUT OF ADJUST A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 403QX 4037 EN ROUTE FROM SEA TO BZN AFT SERVICE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO GEG AND LANDED WITHOUT INCIDE NT. INSPECTED AFT SERVICE DOOR AND FOUND OUTER HANDLE NOT FLUSH. ADJUSTED FLAP COVER. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003013100114 20030131 00114 NM 2003 1 31 QXEA0202155 1 20021210 A 5270 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR OBSTRUCTED A QXEA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 09 408QX 4050 MFR- FUSELAGE DOOR WARNING ILLUMINATED. REMOVED LOOSE PAINT CHIP FROM AFT PASSENGER DOOR PROXIMITY SENSOR. NO PARTS RE PLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003013100116 20030131 00116 NM 2003 1 31 QXEA0202156 1 20021210 A 5270 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR DIRTY A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 413QX 4060 GEG- AFT PASSENGER DOOR INDICATED OPEN IN FLIGHT AT 23,000 FEET. DESCENDED TO 13,000 FEET AND LIGHT WENT OUT. LIGHT WA S ILLUMINATING ON AND OFF DURING DESCENT. PRESSURE INDICATED NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. CLEANED AND LUB ED HANDLE AND DOOR PROXIMITY SENSORS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003013100117 20030131 00117 CE 2003 1 31 CA030107014 1 20021220 A 3233 508202085 ACTUATOR BEECH 200 B200C 1152924 CE PWA PT6 PT6A42 52043 NE HARTZL HCD4N3 HCD4N3A GL MLG NOISY W K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 CA (CAN) AFTER HAVING PROBLEMS WITH A LOW TIME ACTUATORS ON TWO OTHER AIRCRAFT, WE DECIDED TO CHECK ALL ACTUATOR THAT WERE OVERHAULED BY THAT SUPPLIER.DURING SPECIAL INSPECTION OF THIS ACTUATOR, WE FOUND THAT THE LANDING GEAR ACTUATOR WAS SQUE ALING DURING GEAR EXTENSION. THE ACTUATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4T 4 T A24CE E4EA 5 C STC 2003013100118 20030131 00118 NM 2003 1 31 QXEA0202157 1 20021208 A 7110 SKIN DHAV DHC8 DHC8202 2809007 NM COWLING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - AFT DECK SKIN OF LOWER COWL IS DAMAGED. REPAIRED IAW DHC-8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2003013100119 20030131 00119 NM 2003 1 31 QXEA0202158 1 20021208 A 7110 STRINGER DHAV DHC8 DHC8202 2809007 NM RT COWLING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - RIGHT HAND LOWER COWL 4 LATERAL STRINGERS HAVE OVERSIZED HOLES ON BOTTOM SIDE OF COWL AFT DECK. REPAIRED IAW DHC- 8 200 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2003013100120 20030131 00120 EU 2003 1 31 CA030107015 1 20021210 A 2910 F10A751311 LINE AMD FALC10 FALCON10 2730101 EU HYD SYSTEM CHAFED W C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CA (CAN) R/H ENGINE FLUCTUATING. OVERSHOOTING & CAUSING THROTTLE SPLIT IN ALTITUDE, LEAK CHECKED THE PRESSURE SENDING LINE FROM THE ENGINE COMPUTER TO THE ENGINE INLET PRESSURE & TEMPERATURE SENSOR (P2T2). FOUND LINE LEAKING IN PYLON. LINE WAS TOUCHING HARD AGAINST THE NR 2 HYDRAULIC PRESSURE LINE. P2 LINE REMOVED, FOUND LINE CHAFED THROUGH AND HYDRAULIC LINE W ORN.BOTH LINES REPLACED.P2 SENSING LINE P/N F10A789108HYDRAULIC PARESSURE LINE P/N F10A751311 2 L 7 2 4F A33EU 2003013100121 20030131 00121 NM 2003 1 31 QXEA0202159 1 20021208 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - 524BT HAS NUMEROUS HOLES WITH RAISED METAL. REPAIRED IAW T/R 57-003 57-20-00. 2 H 7 2 4T RT A13NM 2003013100122 20030131 00122 NM 2003 1 31 QXEA0202160 1 20021208 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - APERTURE FOR 524BT HAS RAISED METAL AT FORWARD OUTBOARD CORNER HOLE. REPAIRED IAW RD 8-57-633. 2 H 7 2 4T RT A13NM 2003013100123 20030131 00123 NM 2003 1 31 QXEA0202161 1 20021215 A 2450 MS2893730 FUSE DHAV DHC8 DHC8202 2809007 NM ELECTRICAL SYS OPEN A QXEA K NONE J WARNING INDICATION CR CRUISE 1 NM 09 375PH 529 SEA ON FLIGHT NR 2143- RIGHT TRU AND RIGHT STALL WARNING CAUTION LIGHTS CAME ON IN CRUISE FLIGHT. RIGHT TRU CIRCUIT BRE AKER ALSO TRIPPED. AFTER .05 MINS RIGHT STALL WARNING CAUTION LIGHT BEGAN TO GO OFF AND ON WITH NO PATTERN. REPLACED R IGHT HAND VARIABLE FREQUENCY AC SUPPLY PHASE "B" FUSE F10 DUE TO OPEN CONDITION. ALSO REPLACED RIGHT HAND PROP D/I BRUS H BLOCK DUE TO SHORTED CONDITIONS. GROUND RAN NR 2 ENGINE, NO TRU ON STALL WARNING CONDITIONS NOTED. ALL INDICATIONS N ORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003013100124 20030131 00124 NM 2003 1 31 QXEA0202162 1 20021214 A 3350 AML51C60GY SWITCH BOMBDR DHC8 DHC8401 1390041 NM CABIN INOPERATIVE A QXEA K NONE O OTHER CR CRUISE 1 NM 09 406QX 4048 BOI-EMERGENCY LIGHTS CAME ON INFLIGHT, CAN NOT RESET. REPLACED EMERGENCY LIGHT SWITCH AT FORWARD FLIGHT ATTENDANT POSIT ION. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003013100125 20030131 00125 EU 2003 1 31 QXEA0202165 1 20021212 A 2611 SMOKE DETECTOR FOKKER F28 F28MK4000 4990810 EU LAVATORY MALFUNCTIONED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 492US 11159 BOI- SMOKE DETECTOR IN LAVATORY CHIRPING. PERFORMED LAVATORY SMOKE DETECTOR OPERATIONAL CHECK. NO DEFECTS NOTED. NO P ARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2003013100126 20030131 00126 EU 2003 1 31 QXEA0202166 1 20021212 A 2611 PU90461S SMOKE DETECTOR FOKKER F28 F28MK4000 4990810 EU LAVATORY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 492US 11159 SEA- LAVATORY SMOKE DETECTOR CHIRPING IN FLIGHT. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2003013100128 20030131 00128 NM 2003 1 31 QXEA0202168 1 20021210 A 2720 2379003001 REGULATOR DHAV DHC8 DHC8202 2809007 NM RUDDER MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 379PH * 4558 530 SEA OF FLIGHT 2242- ON CLIMBOUT MASTER CAUTION LIGHT ILLUMINATED FOR RUDDER PRESSURE AND RUDDER FULL PRESSURE LIGHTS. A LL OTHER INDICATIONS NORMAL. REMAINED ON UNTIL GEAR WAS LOWERED FOR LANDING, THEN LIGHTS WENT OUT. REMOVED AND REPLACE D RUDDER PRESSURE REGULATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003013100129 20030131 00129 EA 2003 1 31 QXEA0202169 1 20021212 A 2612 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA FIRE DETECTION MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 608QX 10026 MFR ON FLIGHT 2540- FIRE SYSTEM FAULT STATUS MESSAGE EN ROUTE. CYCLED SHIPS POWER, FIRE SYSTEM CHECKED OK. NO PARTS RE PLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013100130 20030131 00130 EA 2003 1 31 QXEA0202170 1 20021210 A 2611 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY TORN A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 608QX 10026 TUS ON FLIGHT 2535- FORWARD BAGGAGE COMPARTMENT CHIMNEY HAS ONE INCH TEAR. REPAIRED IAW HORIZON AIR EO 670-53-32-001. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013100131 20030131 00131 EA 2003 1 31 QXEA0202171 1 20021213 A 2611 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY BROKEN A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 609QX 10031 BOI- DURING PREFLIGHT NOTICED 6 CONSECUTIVE WIRE MESH BROKEN ON FORWARD CARGO CHIMNEY IN OVERHEAD. REPAIRED IAW HORIZON AIR EO 670-53-32-001. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013100133 20030131 00133 EA 2003 1 31 QXEA0202172 1 20021212 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 611QX 10041 BOI- FORWARD CARGO BAY CENTER CHIMNEY DAMAGED. REMOVED AND REPLACED CENTER CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013100134 20030131 00134 EU 2003 1 31 QXEA0202173 1 20021215 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 493US 11161 SEA ON FLIGHT 2423- EMERGENCY LIGHT NEXT TO LAVATORY SIGN HAS SOME BURNED OUT BULBS. REMOVED AND REPLACED FORWARD EMERG ENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2003013100137 20030131 00137 EU 2003 1 31 QXEA0202174 1 20021211 A 5210 MECHANISM FOKKER F28 F28MK4000 4990810 EU PAX DOOR LACK OF LUBE A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 497US 11173 PDX - FLIGHT 2430 - MAIN CABIN DOOR DIFFICULT TO OPERATE IN BOTH DIRECTIONS. OPEN BUTTON DOES NOT RESPOND UNLESS THE DO OR HANDLE IS CYCLED SEVERAL TIMES. MAINTENANCE INSPECTED THE DOOR AND LUBRICATED THE LATCHING AND LOCKING MECHANISM. T HE MAIN CABIN DOOR SEAL WAS LUBRICATED ALSO. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2003013100140 20030131 00140 EA 2003 1 31 QXEA0202175 1 20021210 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA K NONE K FLUID LOSS UK UNKNOWN 1 NM 09 607QX 2923 10024 PDX - ENGINE FUEL FEED SWITCH WAS DISCOVERED LEAKING AT THE WEEP HOLE. MAINTENANCE REPLACED THE ENGINE FUEL FEED SWITCH . OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003013100144 20030131 00144 NM 2003 1 31 ASAA0280327 1 20020813 A 2432 30475022 BATTERY DOUG MD80 MD83 3023681 NM E/E BAY FAILED A ASAA K NONE M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 01 981AS 47705 53472 LAX - JUST PRIOR TO PUSH BACK, SMOKE WAS NOTED DISCHARGING FROM VENT HOLES AFT OF THE NLG WHEEL WELL. THE SMOKE WAS DET ERMINED TO BE STEAM DISCHARGING FROM THE MAIN BATTERY VENT HOLES. SUBSEQUENT SHOP INVESTIGATION REVEALED THAT BOTH MAIN BATTERIES S/N'S 9306248 AND 9306249 SUSTAINED SEVERE INTERNAL DAMAGE DEEMED BEYOND REPAIR. THE CHARGER, ALTHOUGH IT PA SSED SHOP TEST AS IS, HAS BEEN REMOVED AND FROM ALASKA'S STOCK AND SCRAPPED ALONG WITH BOTH BATTERIES. REPLACED BATTERY CHARGER AND BOTH MAIN BATTERIES. SYSTEM OP CHECKED OK. (M) 2 L 7 2 4F RT 2003013100145 20030131 00145 2003 1 31 ASAA0280350 4 20021004 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 SEA - LANYARD BETWEEN GIRT BAR AND SLIDE COVER BECAME DISCONNECTED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2003013100152 20030131 00152 2003 1 31 CA030108005 4 20021206 A 3422 102004104 GYRO GULSTM 690TP 690D 3970405 SW GARRTT TPE331 TPE3315 01514 WP ROTOL R306 R306382F7 GL COCKPIT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) RT GYRO HORIZON INDICATOR TOPPLED AND WOULD NOT ERECT. SENT TO REPAIR, CALIBRATION AND TESTED. 1 H 7 2 3T 4 T 2A4 E4WE 6 C P8EU 2003013100154 20030131 00154 NM 2003 1 31 CA030108009 1 20020925 A 2923 4213402 PUMP BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA HYD SYSTEM FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AFTER START OF ENGINES, TURNING ON THE STANDBY HYDRAULIC PUMP IT SHOWED NO PRESSURE. TEST FOR RELEASE ACCORDING TO MEL FOR INDICATION FAILURE PERFORMED AND THE RESULT CLEARLY SHOWED THAT THE PUMP WAS U/S. THE HYDRAULIC STANDBY POWER U NIT (SPU) WERE REPLACED ACCORDING AMM 29-11-36. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003013100157 20030131 00157 NE 2003 1 31 CA030108013 2 20021219 A 7230 777843 TUBE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE 13 STAGE MANIFOL FRACTURED W O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CA 27979 (CAN) 13 STAGE BLEED MANIFOLD TRANSFER TUBE FRACTURED. ENGINE REMOVED AND SENT TO SHOP FOR REPAIR AND PREVENTIVE MOD SB 6369 SB6393 INCORPORATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2003013100158 20030131 00158 NE 2003 1 31 CA030108014 2 20021230 A 7321 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE FUEL CONTROL MALFUNCTIONED W E A ENGINE SHUTDOWN UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 CA (CAN) IN FLIGHT SHUTDOWN OF RT ENGINE DUE TO REOCCURANCE OF UNCONTROLLED FUEL IMBALANCE. CREW RECEIVED 'XFLOW/APU PUMP E ICAS AMBER MESSAGE AFTER TAKEOFF, AFTER APU WAS SHUTDOWN'. ALSO HAD 'RT XFLOW SOV FAIL MESSAGE. REPLACEMENT OF : RT CO MPENSATOR PROBE. RT CROSSFLOW SOV, APU NEG. GRAVITY RELIEF VALVE, AND APU/XFLOW FUEL PUMP CART. DURING ATTEMPTED FUNCTI ON CHECKS MAINT FOUND THE XFLOW/APU PUMP WAS ON BUT NO SHUTOFF VALVE WAS OPEN TO MOVE FUEL. LINE FROM PUMP ON FUEL PAGE WAS GREEN BUT ALL VALVES WERE CLOSED. FUEL COMPUTER WAS REPLACED. THIS UNIT WAS TRIED IN ANOTHER A/C AND PRODUCED THE SA ME FAULTS. FUNCTION CHECKS FOR ALL REPLACED PARTS AND AFFECTED SYSTEMS WERE COMPLETED AND THE A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2003013100159 20030131 00159 NM 2003 1 31 CA030108015 1 20021007 A 2821 SWITCH BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA FUEL FILTER MALFUNCTIONED W O OTHER J WARNING INDICATION CL CLIMB 1 CA (CAN) DURING ROTATION ON TAKEOFF, FUEL FILTER BYPASS NR 1 CAUTION LIGHT CAME ON. QRH X-LIST FOLLOWED, FLIGHT PROCEEDED T O BASE. CAUTION LIGHT REMAINED ON FOR THE REST OF THE FLIGHT. LT ENGINE FUEL FILTER IMPENDING BYPASS SWITCH WAS REPLACED IN ACCORDANCE WITH AMM TASK 73-31-06. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003013100160 20030131 00160 NM 2003 1 31 CA030108016 1 20021010 A 3010 BOOT BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA DEICE SYSTEM FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) WHEN SELECTING AIRFRAME DEICING IN ICING CONDITIONS, TWO BOOTS ON LT WING DID NOT INFLATE, AND SUBSEQUENTLY 'DEICE PRESS' CAUTION CAME ON. SEVERAL REMARKS FOR THE OUTER LT BOOTS WERE WRITTEN DURING THE PERIOD 10OCT2002-14-OCT2002. TH E OUTERMOST LT DDV WAS CONSEQUENTLY REPLACED ON 14OCT2002. AFTER REPLACEMENT, PROPER FUNCTION OF THE OUTER LT BOOTS WERE NOTED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003013100161 20030131 00161 SW 2003 1 31 CA030108018 1 20021229 A 2435 BEARING BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE STARTER GEN FAILED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 CA (CAN) PILOT OBSERVED NR 1 GENERATOR FAIL CAUTION LIGHT FLICKERING WHILE IN NORMAL CRUISE FLIGHT. NORMAL OPERATION CONTIN UED ON NR 2 SYSTEM. NR 1 STARTER-GENERATOR WOULD NOT CRANK ON NEXT START AND WAS REPLACED WITH A SERVICEABLE UNIT. UNIT IS AWAITING DISSASEMBLY AND REPAIR. SUSPECT BEARING FAILURE DUE TO UNKNOWN CAUSE AT THIS TIME. 1 G 7 1 4U 4 U H4SW E22EA 2003013100163 20030131 00163 NM 2003 1 31 CA030109002 1 20021014 A 2750 FE282001 LEVER BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) ESTABLISHED INBOUND ON LOCALIZER. WHEN SELECTING FLAPS FIVE, CAUTION FLAP POWER LIGHT CAME ON. THUS UNABLE TO SELE CT FLAPS. PERFORMED FLAPLESS LANDING WITHOUT PROBLEMS. REPLACED THE FLAP QUADRANT. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003013100164 20030131 00164 NM 2003 1 31 CA030109004 1 20021015 A 7921 BYPASS VALVE BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA OIL COOLER FAULTY W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) DURING CLIMB RT OIL TEMP WAS RISING TO RED LINE 108 DEGREES. POWER REDUCED AND OIL TEMP FELL TO 104 DEGREES AND ST AYED BELOW RED LINE THE REST OF THE FLIGHT. FLIGHT RETURNED TO BASE. RT ENGINE OIL COOLER BY-PASS VALVE WAS REPLACED IN ACCORDANCE WITH AMM TASK 79-21-06. BY-PASS VALVE OUT: S/N 148 AND BY-PASS VALVE IN: S/N 314. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003013100165 20030131 00165 EA 2003 1 31 CA030109005 2 20021030 A 7532 BLEED VALVE BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA ENGINE FAILED W O OTHER J WARNING INDICATION LD LANDING 1 CA (CAN) DURING LANDING FLARE AT APPROXIMATELY 20 FEET NR 2 FADEC CAUTION LIGHT CAME ON TOGETHER WITH POWERPLANT MESSAGE ON ENGINE DISPLAY. ENGINE OPERATED ACCORDING TO QRH AND A NORMAL LANDING FOLLOWED. NO OTHER REMARKS ON TAXI IN AND SHUT D OWN. RT ENGINE P2.2 BLEED VALVE KN 847912 WAS REPLACED IN ACCORDANCE WITH AMM TASK 75-31-11, DUE TO FAULT CODE 912. BLE ED VALVE OUT: S/N GA1068 AND BY-PASS VALVE IN: S/N GA1078. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003013100166 20030131 00166 NM 2003 1 31 CA030109006 1 20021105 A 7540 DUCT BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA BLEED SYS LEAKING W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE, CAUTION LIGHT ON FOR NR 2 BLEED HOT. ACC TO QRH IT WAS SWITCHED OFF. BASE WAS CONTACTED. THEY ASKED US TO SELECT IT ON AGAIN, WHICH WE DID AND SHORTLY AFTER CAUTION LIGHT CAME ON AGAIN.TCC ASKED US TO RETURN TO BASE WHE RE WE MADE AN UNEVENTFUL LANDING. CHECKED FOR FAULT CODES. FAULT CODE 7002,1706 AND 1801 PRESENT. THE RT NACELLE DUCT LE AK TEMPERATURESWITCH REPLACED ACCORDING AMM 36-11-21. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003020300004 20030203 00004 EU 2003 2 3 CA030110004 1 20021227 A 2435 BEARING BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110UG 01514 WP ROTOL R333 R333482F12 GL STARTER GEN SEIZED W E H ENGINE SHUTDOWN DEACTIVATE SYST/CIRCUITS E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA (CAN) DEPARTURE FROM CYXD WAS NORMAL APART FROM LIGHT VIBRATIONS FROM NR 2 ENGINE. APPROXIMATELY 10 MIN. AFTER DEPARTUR E NR 2 GEN INOPERATIVE LIGHT ILLUMINATED. RESET GEN SWITCH, IT DID NOT COME ON LINE, SO IT WAS TURNED OFF. THE VIBRATION GOT WORSE, ERRATIC INDICATIONS ON NR 2 FUEL PRESSURE AND NR 2 HYD PRESSURE. NR 2 ENGINE WAS SHUTDOWN AND FEATHERED AS A PRECAUTION IN THE EVENT THERE MIGHT BE A GEARBOX PROBLEM. PASSENGERS ADVISED, ADVISED ATC TO HAVE EMERGENCY SERVICES ST ANDBY. REMAINDER OF FLIGHT WAS UNEVENTFUL. MAINTENANCE INSPECTION REVEALED NR 2 STARTER GEN SEIZED DUE TO REAR STARTER G EN BEARING FAILURE. EVIDENCE OF STARTER GEN COOLING FAN RUBBING SHROUD AS BEARING FAILED. 2 L 7 2 4T 4 T RT A21EU E4WE 6 C P61GL 2003020300006 20030203 00006 NM 2003 2 3 CA030110009 1 20021028 A 3010 4100S00501 VALVE BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA DUAL DISTRIBUTIO FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING DECENT IN ICING CONDITIONS AND MODERATE ICE BUILD UP, DEICE PRESSURE CAUTION LIGHT CAME ON, QRH APPLIED, IC ING CONDITIONS WAS EXITED AT VMO. BOOT INFLATION WAS VISUAL INSPECTED ON GROUND NR 2 OUTER LT BOOT DID NOT LIGHT UP IN AUTOMATIC MODE AND DID TURN ON DEICE PRESSURE CAUTION LIGHT. IN MANUAL MODE BOOT LIGHT WAS INTERMITTENT WITHOUT ANY CAUT ION LIGHT. RETURN FLIGHT CANCELLED. DDV (VALVE) CHANGED AND FERRY FLOWN TO BASE NEXT DAY. THIS IS THE SECOND EVENT IN TWO DAYS WHERE THE APPLIED CB/02/45 HAS TAKEN CARE OF THE DEICE PRESSURE CAUTION LIGHT, WHERE A DDVIN CORRESPONDING BOOT HAS FAILED, AND SUBSEQUENT GROUND CHECK OF SYSTEM HAS DISCOVERED A TECHNICAL MALFUNCTION. DDV WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003020300007 20030203 00007 NM 2003 2 3 CA030112001 1 20021126 A 3246 431276E BOLT BFGOODRICH BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E437 54555 NE MLG WHEEL SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 221 (CAN) UPON ARRIVAL OF A/C IN YYZ, FLT 421, DURING WALK AROUND, MTCE DISCOVERED 2 TIE BOLTS MISSING FROM NR 7 MLG WHEEL A SSY. THE NR 7 MLG WHEEL WAS REPLACED IAW AMM 32-45-01. 2 L 7 2 4F 4 F RT A2NM E12EU 2003020300008 20030203 00008 EU 2003 2 3 CA030112002 1 20021128 A 3240 NE1026660844AS CLAMP AIRBUS 310 A310300 3930305 EU GE CF6 CF680C2A5 NE COOLING FAN BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON A/C ARRIVAL, DURING WALK AROUND, MTCE NOTED THAT THE NR 5 MLG WHEEL BRAKE COOLING FAN SHROUD ATTACHMENT CLAMP WAS BROKEN. MTCE REPLACED THE CLAMP IAW AMM 12-37-32. 2 L 7 2 4F 4 F RT A35EU E13NE 2003020300009 20030203 00009 WP 2003 2 3 CA030112003 1 20021130 A 5512 SKIN LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE LT STABILIZER DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING WALK AROUND IN YYZ, MTCE FOUND THE LT STABILIZER TRAILING EDGE TIP SKIN DAMAGED. A REPAIR WAS CARRIED OUT IAW SRM 55-22-00. LOOSE RIVITS REPLACED IAW 51-40-01. 2 L 7 3 4F 4 F A23WE E12EU 2003020300010 20030203 00010 EU 2003 2 3 CA030112004 1 20021201 A 2933 647520151 TRANSMITTER AIRBUS 310 A310300 3930305 EU GE CF6 CF680C2A5 NE HYD RESERVOIR READS LOW W O OTHER N FALSE WARNING NR NOT REPORTED 1 CA (CAN) THE YELLOW HYDRAULIC TRANSMITTER READING LOW ON ARRIVAL. DURING SERVICING OF THE YELLOW HYDRAULIC SYSTEM, FLUID EM ERGED FROM THE AIR DEPRESSURIZATION RELIEF VALVE. THE ERRONEOUS READING (FROM THE DEFECTIVE 'HYDRAULIC TRANSMITTER,CAUSE D MTCE TO OVERFILL THE HYDRAULIC SYSTEM AND ENDED UP PUMPING HYDRAULIC FLUID IN THE AIR PRESSURIZATION SYSTEM. THE YELLO W SYSTEM HYDRAULIC RESERVOIR 'TRANSMITTER' WAS REPLACED IAW AMM 29-31-11. 2 L 7 2 4F 4 F RT A35EU E13NE 2003020300011 20030203 00011 EU 2003 2 3 CA030112005 1 20021220 A 7711 MY20781154 LINE AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE RT PYLON LOOSE W C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CA (CAN) DURING TAKE-OFF THE PILOT WAS UNABLE TO MAKE THE REQUIRED EPR ON THE RT ENGINE WITH ANTI-ICE SELECTED. THE PILOT I NITIATED REJECTED TAKE-OFF AND ADVISED ATC. SUBSEQUENT TAKE-OFF ATTEMPT FOR NORMAL EPR WAS SUCCESSFUL. UPON ARRIVAL AT THE OTTAWA BASE LOCATION, OUR CONTRACTED AMO COMPLIED WITH AN ENGINE GROUND RUN AND DETERMINED A FALSE EPR INDICATION WA S THE PROBABLE CAUSE. FURTHER INSPECTION OF THE EPR SYSTEM IDENTIFIED A LOOSE FITTING AT THE PYLON LOCATION ON THE LINE ASSY. AN ENGINE PERFORMANCE RUN WAS COMPLIED SATISFACTORILY AND COMPLIANCE OF A DAILY CHECK WAS COMPLETED. 2 L 7 2 4F 4 F RT A7EU E7EA 2003020300012 20030203 00012 CE 2003 2 3 CA030112006 1 20021220 A 5260 SKIN BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA AIRSTAIR DOOR DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON DECEMBER 20, 2002 UPON ARRIVAL OF THE AIRCRAFT AT THE OTTAWA BASE, THE FLIGHT CREW REPORTED THE CABIN DOOR HING E COVER CRACKED. SUBSEQUENTLY, OUR CONTRACTED AMO INFORMED US OF LOOSENESS FOUND AT THE ATTACHING POINT OF THE MAIN CABI N DOOR HINGE. FURTHER INSPECTION OF THE MAIN CABIN DOOR REVEALED DELAMINATING OF THE INNER SKIN AND OUTER SKIN OF THE DO OR ASSEMBLY AT THE HINGE AREA, PRIMARILY ASSOCIATED TO CORROSION. AT THIS TIME, THE AIRCRAFT WAS REMOVED FROM SERVICE. T HE MAIN CABIN DOOR ASSEMBLY IDENTIFIED AS PN 11440002335, SN UC-36 WAS REMOVED AND REPLACED WITH NEW AIRSTAIR DOOR PN 1 14400023-69. 2 L 7 2 4T 4 T RT A24CE E4EA 2003020300013 20030203 00013 WP 2003 2 3 CA030112007 1 20021124 A 2130 DUCT HAMSTD LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE WATER SEPARATOR SEPARATED W O OTHER D INFLIGHT SEPARATION AP APPROACH 1 CA (CAN) A DEPRESSURIZATION OCCURRED AT 21000 , ABNORMAL PROCEDURE CARRIED PER QRH. LOUD NOISE HEARD IN FLIGHT DECK DURING APPROACH. FOUND NR 2 WATER SEPARATOR DUCT SEPARATED FROM WATER SEPARATOR. FURTHER INSPECTION REVEALED A LARGE CRACK ON T HE INLET FLANGE OF THE WATER SEPARATOR. MTCE REPLACED THE WATER SEPARATOR IAW AMM 21-51-31 AND ALSO REPLACED PACK NR 2 T URBINE OULET DUCT IAW AMM 20-21-05. LEAK CHECKS CARRIED OUT SERVICEABLE. 2 L 7 3 4F 4 F A23WE E12EU 2003020300016 20030203 00016 WP 2003 2 3 CA030112010 1 20021205 A 2781 801802 SENSOR LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE FLAP/SLAT IND FAILED W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA (CAN) AT 5:45 HRS LOCAL , FLIGHT 044, REJECTED T/O AT 90 KNOTS, DUE TO UNSAFE T/O WARNING HORN RELATED TO SLAT MALFUNCTI ON. THE PROXIMITY CARD A12 (P/N 805006, S/N 53) WAS REPLACED PER AMM 31-22-02 AND UNSAFE T/O WARNING TEST PARA. CITEM 1 ,2,3 C/OUT PER AMM 31-22-00. ON PUSH BACK OF A/C, LATER DURING THE DAY AT 15:35 HRS LOCAL, UPON SELECTING FLAPS 4 DEGREE S, A RED SLAT LIGHT ON, FLAP POSITION INDICATOR COMES ON (F/E PANEL SLAT MONITIOR PANEL : RT 2 & 3 SLAT LIGHTS DO NOT IL LUMINATE). A/C RETURNED TO GATE AND MTCE REPLACED AND ADJUSTED THE SLAT POSITION PROXIMITY SWITCH SENSOR (P/N 801802) FO R THE SLAT NR 2 & 3 PER AMM 27-82-03. 2 L 7 3 4F 4 F A23WE E12EU 2003020300017 20030203 00017 EU 2003 2 3 CA030113001 1 20021209 A 3240 C247030021 VALVE AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211TRENT77 NE PARKING BRAKE FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) AFTER PUSH BACK IN YVR, FOR FLIGHT 220, AFTER ENGINE START, CREW WAS UNABLE TO SET PARKING BRAKE. MTCE REPLACED TH E PARKING BRAKE VALVE PER AMM 32-45-51-401. 2 L 7 2 4F 4 F RT A46NM E39NE 2003020300018 20030203 00018 NM 2003 2 3 CA030113002 1 20021102 A 3230 483023 SOLENOID VALVE BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA NLG FAILED W A UNSCHED LANDING D J INFLIGHT SEPARATION WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKE OFF, AMBER LIGHT REMAINED ILLUMINATED ON NOSE GEAR. A LOUD RATTELING NOISE WAS HEARD. RECYCLED ACCORDIN G TO QRH WITH NO SUCCESS. A/C RETURNED TO BASE. NLG SOLENOID SEQUENCE VALVE REPLACED IAW AMM 32-31-71. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003020300027 20030203 00027 NE 2003 2 3 CA030113013 2 20021229 A 7200 ENGINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE NR 3 VIBRATION W C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 CA 14838 (CAN) UPON DEPARTURE OF FLIGHT 703 FROM VRA-YMX, TAKE OFF WAS REJECTED DUE TO NR 3 ENGINE VIBRATION LIGHT CAME ON. DURI NG TAKE OFF, VIBRATION WAS CONFIRMED ON BOTH CHANNELS. CHECK LIST CARRIED OUT AT 60 KNOTS. TEST 11 CARRIED OUT IAW AMM 7 1-00-00. VIBRATION LEVELS FOUND TO BE WITHIN LIMITS. A BOROSCOPE INSPECTION WAS SCHEDULED TO BE CARRIED OUT WITHIN 25 HO URS IAW AMM 71-91-00. A/C DEPARTED FROM VRA WITHOUT ANY FURTHER PROBLEM. UPON RETURNING IN YMX, THE ENGINE WAS REPLACED FOR COMPANY CONVENIENCE, BY ENGINE SN 14830. 2 L 7 3 4F 4 F A23WE E12EU 2003020300028 20030203 00028 WP 2003 2 3 CA030113015 1 20021123 A 5200 LJ17001 ACCESS DOOR LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NR 1 NACELLE SEPARATED W O OTHER D INFLIGHT SEPARATION TX TAXI/GRND HDL 1 CA (CAN) ON ARRIVAL IN YYZ FROM FLIGHT 651 (PVR-YYZ), NR 1 ENGINE START CONTROL VALVE ACCESS PANEL WAS MISSING. NO DAMAGE T O COWLING. MTCE REPLACED THE DOOR IAW AMM 71-11-00. 2 L 7 3 4F 4 F A23WE E12EU 2003020300029 20030203 00029 NM 2003 2 3 CA030114001 1 20020921 A 3260 860TS09Y00 CONTROL PANEL BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA MLG MALFUNCTIONED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) FOLLOWING LANDING GEAR RETRACTION, THE RT MAIN GEAR DOORS STATUS LIGHT DID NOT EXTINGUISH. THE A/C RETURNED TO BA SE. LANDING GEAR CONTROL PANEL REPLACED, A/C FUNCTION TESTED AND RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003020300033 20030203 00033 NE 2003 2 3 CA030115001 2 20021217 A 7260 ALTERNATOR BOEING 767 767333 1385301 NM GE CF6 CF680C2B6F 30025 NE GEARBOX BROKEN W O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) ORIGINAL WRITE UP STATED, LT ENGINE OIL QUANTITY SLOWLY DROPPED TO ZERO DURING CRUISE. OIL TEMP STEADY AT 3 DEGREE S ABOVE RT ENGINE. OIL PRESSURE FLUCTUATED AT 2-10 PSI BELOW RT ENGINE. LT ENGINE EICAS MESSAGE SHOWING. AIRCRAFT PROCEE DED TO YVR WITH LT ENGINE AT IDLE POWER. MAINTENANCE FOUND BROKEN CONTROL ALTERNATOR. CONTROL ALTERNATOR AND STATOR REPL ACED. LEAK AND FUNCTION CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2003020300037 20030203 00037 NM 2003 2 3 QXEA0201989 1 20021124 A 2740 PITCH CONTROL BOMBDR DHC8 DHC8401 1390041 NM HORIZ STAB MALFUNCTIONED A QXEA K NONE F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 09 408QX 4050 SEA- PITCH TRIM CAUTION LIGHT ILLUMINATED ON CLIMBOUT WITH LOSS OF PITCH TRIM. AUTO TRIM FAIL MESSAGE ON EADI. AIRCRAF T LANDED WITHOUT INCIDENT. PERFORMED Q400 FIM TASK 27-30-00-810-803 WITH NO RECURRENCE OF PITCH TRIM CAUTION LIGHT OR A UTO TRIM FAIL MESSAGE. NO PARTS REPLACED OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003020300038 20030203 00038 NM 2003 2 3 QXEA0202103 1 20021204 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE SEPARATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 PDX- BONDED ALUMINUM SEPERATED APART AT FUSELAGE STATION X580 AND Z160 OF BAGGAGE DOOR AFT PRESSURE STOP. REPAIRED IAW DHC-8 RD 8-53-5461. 2 H 7 2 4T RT A13NM 2003020300039 20030203 00039 NM 2003 2 3 QXEA0202167 1 20021214 A 2750 FLAP BOMBDR DHC8 DHC8401 1390041 NM WING MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 406QX 4048 SMF ON FLIGHT 2301- FLAP POWER CAUTION LIGHT DURING APPROACH. RESET FLAPS CONTROL CIRCUIT BREAKER PER EMERGENCY CHECKLI ST. AIRCRAFT LANDED WITHOUT INCIDENT. MESSAGE CLEARED AND FLAPS OPERATE NORMALLY. NO PARTS REPLACED. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003020300040 20030203 00040 NM 2003 2 3 QXEA0202178 1 20021215 A 5320 FLANGE BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - PANEL ATTACHMENT FLANGES ON AFT SIDE, TOP OF AFT SPAR, CHAFED AROUND FASTENER HOLES, LEFT Y41.0 TO RIGHT Y41.0. R EPAIRED IAW HORIZON AIR EA 6-53-463. 2 H 7 2 4T RT A13NM 2003020300041 20030203 00041 NM 2003 2 3 QXEA0202179 1 20021215 A 5320 FLANGE BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - APERTURE FLANGE FOR PANEL 261CT CHAFED FORWARD SIDE OUTBOARD FOUR FASTENERS. REPAIRED IAW HORIZON AIR EA 6-53-163 . 2 H 7 2 4T RT A13NM 2003020300042 20030203 00042 NM 2003 2 3 QXEA0202180 1 20021215 A 5320 FLANGE BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - APERTURE FLANGE FOR PANEL 261LT CHAFED FORWARD SIDE OUTBOARD FOUR FASTENERS. REPAIRED IAW HORIZON AIR EA 6-53-164 . 2 H 7 2 4T RT A13NM 2003020300043 20030203 00043 NM 2003 2 3 QXEA0202181 1 20021215 A 5320 FLANGE BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - APERTURE FLANGE FOR PANEL 261LT CHAFED AFT SIDE OUTBOARD, FIRST AND FOURTH FASTENER HOLES FROM OUTBOARD END. REPA IRED IAW HORIZON AIR EA 6-53-163. 2 H 7 2 4T RT A13NM 2003020300044 20030203 00044 NM 2003 2 3 QXEA0202182 1 20021212 A 2910 HYDRAULIC LINE BOMBDR DHC8 DHC8401 1390041 NM HYD SYSTEM OUT OF POSITION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - STAINLESS HYDRAULIC LINE FOR RETRACTION ACTUATOR IS CHAFING YOKE. REPAIRED IAW DHC8-400 CMM 32-11-04, PAGE 603, P ARAGRAPH 3A, STEP 1. 2 H 7 2 4T RT A13NM 2003020300045 20030203 00045 NM 2003 2 3 QXEA0202183 1 20021214 A 5512 SKIN BOMBDR DHC8 DHC8401 1390041 NM HORIZ STAB SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - SCRATCH ON HORIZONTAL STAB, LEFT HAND SIDE, TOP, NEAR TIP. REPAIRED IAW HORIZON AIR EA 6-55-20. 2 H 7 2 4T RT A13NM 2003020300046 20030203 00046 NM 2003 2 3 QXEA0202184 1 20021215 A 5320 PANEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - PANEL 262FT FORWARD EDGE CHAFED AT FASTENERS. REPAIRED IAW HORIZON AIR EA 6-53-165. 2 H 7 2 4T RT A13NM 2003020300047 20030203 00047 NM 2003 2 3 QXEA0202185 1 20021215 A 5320 PANEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - PANEL 262HT CHAFED FORWARD EDGE AT FASTENER HOLES AND AFT EDGE 2 INCHES FROM OUTBOARD EDGE. REPAIRED IAW HORIZON AIR EA 6-53-165. 2 H 7 2 4T RT A13NM 2003020300048 20030203 00048 NM 2003 2 3 QXEA0202186 1 20021215 A 5320 PANEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - PANEL 262AT CHAFED FORWARD EDGE AT FASTENER HOLES AND AFT EDGE 18 INCHES FROM INBOARD END. REPAIRED IAW HORIZON A IR EA 6-53-165. 2 H 7 2 4T RT A13NM 2003020300049 20030203 00049 NM 2003 2 3 QXEA0202187 1 20021211 A 7110 ANGLE BOMBDR DHC8 DHC8401 1390041 NM NR COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - NR 2 LOWER COWL TOP REPAIR ANGLE ON AFT CONE CENTER WEB IS CRACKED AT FORWARD END. REPAIRED IAW RD 8/4-71-016, Q4 00 MM 71-61-01, TEMP REVISION 71-054, PARAGRAPH 4. 2 H 7 2 4T RT A13NM 2003020300050 20030203 00050 NM 2003 2 3 QXEA0202188 1 20021213 A 5210 STOP FITTING BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - CHAFFING ON MAIN CABIN DOOR SHELL ON SECOND STOP UP FROM BOTTOM AFT SIDE. `REPAIRED IAW DHC-8-400 SRM 52-21-10, P AGES 202-205 AND SRM TASK 51-14-00-350-804. 2 H 7 2 4T RT A13NM 2003020300051 20030203 00051 NM 2003 2 3 QXEA0202189 1 20021213 A 5210 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - MAIN CABIN DOOR SHELL CHAFE DAMAGE ON FORWARD INBOARD CORNER. REPAIRED IAW DHC-8-400 SRM 51-14-00 AND SRM 52-21-1 0, PAGES 202-205. 2 H 7 2 4T RT A13NM 2003020300052 20030203 00052 NM 2003 2 3 QXEA0202190 1 20021213 A 5210 STOP FITTING BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - CHAFING EXISTS ON NR 1 AFT DOOR STOP OF MAIN CABIN DOOR. REPAIRED IAW DHC-8 400 SRM 51-14-00, PAGE 221, TASK 51-1 4-00-350-804 AND SRM 52-21-10, PAGES 202-205. 2 H 7 2 4T RT A13NM 2003020300053 20030203 00053 NM 2003 2 3 QXEA0202191 1 20021214 A 5320 SUPPORT BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - INTERNAL ANTENNA SUPPORT CLEATS IN TWO FORWARD POSITIONS ARE CRACKED AT X80. REPAIRED IAW HORIZON AIR EA 6-53-11. 2 H 7 2 4T RT A13NM 2003020300054 20030203 00054 EU 2003 2 3 QXEA0202192 1 20021215 A 3350 5515800106 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 493US 11161 SEA-ON FLT NR 2423, EMERGENCY LIGHT NEXT TO LAVATORY SIGN HAS SOME BURNED OUT BULBS. REMOVED AND REPLACED FORWARD EMERG ENCY LIGHT. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2003020300055 20030203 00055 EA 2003 2 3 QXEA0202195 1 20021215 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY FAILED A QXEA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 09 608QX 2593 2593 10026 PDX- FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED FORWARD BAGGAGE SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020300056 20030203 00056 EA 2003 2 3 QXEA0202196 1 20021216 A 2612 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA FIRE DETECTION MALFUNCTIONED A QXEA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 09 614QX 10049 BIL ON FLIGHT 2481- FIRE SYSTEM FAULT STATUS MESSAGE. TESTED FIRE SYSTEM AND ALL STATUS MESSAGES CLEARED. NO PARTS REP LACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020300057 20030203 00057 EA 2003 2 3 QXEA0202197 1 20021219 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX-FORWARD CARGO BAY FIRE DETECTION CHIMNEY AT DOOR ENTRANCE HAS TORN SCREEN. REMOVED DAMAGED DOOR ENTRANCE CHIMNEY AN D REPLACED IT WITH SERVICEABLE UNIT. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020300058 20030203 00058 NM 2003 2 3 QXEA0202198 1 20021218 A 5270 WARNING SYSTEM BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR FAULTY A QXEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 09 408QX 4050 BOI - FLIGHT 2341 - CREW DIVERTED TO BOI WHEN THEY RECEIVED A FUSELAGE DOOR WARNING TWICE. MAINTENANCE INSPECTED AND FO UND THE AFT PASSENGER DOOR FAULTING. THE DOOR WARNING SYSTEM WIRES FOR THE AFT PASSENGER DOOR WERE CAPPED AND THE RSI W AS CONTINUED. NO FURTHER DISCREPANCIES WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003020300059 20030203 00059 NM 2003 2 3 QXEA0202199 1 20021218 A 2720 RUDDER PEDAL DHAV DHC8 DHC8202 2809007 NM COCKPIT STUCK A QXEA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 09 356PH 502 PDX - FLIGHT 2253 - ON APPROACH, THE FIRST OFFICER REPORTED THE RUDDER PEDALS STUCK WHEN EXECUTING CROSSWIND LANDING INP UTS. THE RUDDER WAS FULLY OPERATIONAL ON LANDING ROLLOUT. NO ASSOCIATED LIGHTS WERE ILLUMINATED. MAINTENANCE INSPECTE D THE AIRCRAFT RUDDER CABLE RUNS, AND RUDDER PACK ASSEMBLY. NO DISCREPANCIES WERE NOTED. THE RUDDER CONTROLS AND INPUT S WERE INSPECTED FROM THE COCKPIT TO THE EMPENNAGE AND THE AUTO PILOT SYSTEM. ALL SYSTEMS,OPERATIONAL CHECKS, AND SUBSE QUENT CHECK FLIGHT WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003020300061 20030203 00061 EU 2003 2 3 QXEA0202201 1 20021217 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 9268 115 11228 PDX-AFT 3 CEILING EVACUATION LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2003020300062 20030203 00062 EA 2003 2 3 QXEA0202202 1 20021218 A 2820 D30BH14 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 09 602QX 2712 2712 10010 BOI- LEFT FUEL LOW PRESSURE CAUTION MESSAGE ON PRIMARY EICAS. REMOVED AND REPLACED LEFT HAND ENGINE INLET PRESSURE SWIT CH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020300063 20030203 00063 EA 2003 2 3 QXEA0202203 1 20021218 A 2150 GG670950091 ACM CNDAIR CL600 CL6002C10 1390015 EA A/C BAY FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 601QX 2827 10009 PDX- STRONG OIL SMELL IN AIRCRAFT WITH PACKS SELECTED ON. REMOVED AND REPLACED NR 1 AIR CYCLE MACHINE. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020300065 20030203 00065 NM 2003 2 3 QXEA0202204 1 20021218 A 5270 SENSOR BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR FROZEN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 414QX 4061 YYC - FLIGHT 2333 - DURING LIFTOFF, CREW RECEIVED A MASTER WARNING FOR FUSELAGE DOORS, AND THE AIRCRAFT DID NOT PRESSURI ZE. MAINTENANCE INSPECTED AND FOUND THE FORWARD BAGGAGE DOOR SENSOR FROZEN. THE DOOR SENSOR WAS CLEANED AND LUBED. OP ERATIONAL CHECKS OF THE DOOR AND THE PRESSURIZATION SYSTEM WERE PERFORMED AND CHECKED GOOD. AIRCRAFT WAS RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 2003020300067 20030203 00067 NM 2003 2 3 QXEA0202207 1 20021221 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INTERMITTENT A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 363PH 11645 7 520 PDX- EMERGENCY LIGHTS FLICKER IN THE OFF POSITION. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003020300069 20030203 00069 EA 2003 2 3 QXEA0202208 1 20021221 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 601QX 81 81 10009 PDX ON FLIGHT 2534- LEFT AND RIGHT FUEL BOOST PUMPS CYCLED CONTINUOUSLY AT FLIGHT LEVELS 350 AND 370. CYCLING STOPPED D URING DESCENT AFTER POWER REDUCTION. REMOVED AND REPLACED BOTH PRIMARY EJECTOR PRESSURE SENSORS. OPERATIONAL CHECKS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020300073 20030203 00073 EA 2003 2 3 QXEA0202209 1 20021221 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 610QX 91 91 10033 SEA ON FLIGHT 2461- DURING SHUTDOWN OF LEFT ENGINE OBSERVED LEFT AND RIGHT FUEL PUMP ON ADVISORY MESSAGE. LEFT FUEL PRE SSURE CAUTION LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED LEFT HAND INLET ENGINE PRESSURE SWITCH. OPERATIONAL CHECK S GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020300074 20030203 00074 EA 2003 2 3 QXEA0202210 1 20021218 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 607QX 10024 PDX ON FLIGHT 2450- FORWARD CARGO SMOKE DETECTOR CHANNEL WIRE MESH IS BROKEN. REMOVED AND REPLACED WIRE MESH. OPERATIO NAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020300076 20030203 00076 NM 2003 2 3 QXEA0202212 1 20021216 A 5541 RIB DHAV DHC8 DHC8202 2809007 NM RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX- CRACK BEYOND SERVICEABLE LIMITS ON FORE RUDDER LOWER CLOSING RIB. REPAIRED IAW DHC-8 SRM 51-40-11 AND HORIZON AIR TASK 27-20-11-030-802. 2 H 7 2 4T RT A13NM 2003020300078 20030203 00078 NM 2003 2 3 QXEA0202213 1 20021216 A 5542 SKIN DHAV DHC8 DHC8202 2809007 NM RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX- CRACK IN SKIN OF FORE RUDDER ON LOWER FORWARD RIGHT HAND CORNER. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2003020300080 20030203 00080 NM 2003 2 3 QXEA0202214 1 20021216 A 5544 BRACKET DHAV DHC8 DHC8202 2809007 NM RUDDER DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX- BOTTOM BRACKET ON FORE RUDDER THAT CONNECTS TO THE TRAILING RUDDER HAS STEP WEAR AROUND FASTENER HOLE. REPAIRED IA W DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2003020300083 20030203 00083 EA 2003 2 3 QXEA0202215 1 20021219 A 2820 CC67061042 TUBE CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 605QX 10022 FAT - AIRPLANE IS TRANSFERRING FUEL FROM THE RIGHT WING TANK TO THE CENTER TANK ON GROUND. THE AIRCRAFT WAS DEFUELED, P ANELS WERE OPENED, AND THE CENTER TANK WAS INSPECTED. MAINTENANCE FOUND A CRACK IN THE FUEL FEED TUBE AND REPLACED SAME . OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020300084 20030203 00084 NM 2003 2 3 QXEA0202216 1 20021219 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - PAINT WORN THROUGH AND EVIDENCE OF GOUGING TO UNDERLYING ALUMINUM ON LEFT HAND INBOARD FLAP. REPAIRED IAW HORIZON AIR EA 6-57-97. 2 H 7 2 4T RT A13NM 2003020300085 20030203 00085 NM 2003 2 3 QXEA0202217 1 20021219 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - PAINT WORN THROUGH WITH EVIDENCE OF CHAFING TO UNDERLYING LEFT HAND OUTBOARD FLAP. REPAIRED IAW HORIZON AIR EA 6- 57-96. 2 H 7 2 4T RT A13NM 2003020300087 20030203 00087 NM 2003 2 3 QXEA0202218 1 20021220 A 5420 BRACKET BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - METAL BRACKET HAS 2 INCH CRACK ON OUTBOARD EDGE OF LEFT HAND NACELLE. REPAIRED IAW Q400 SRM 51-40-07, PAGES 201-21 4, SRM 51-21-10 AND HORIZON AIR EA 6-54-179. 2 H 7 2 4T RT A13NM 2003020300088 20030203 00088 NM 2003 2 3 QXEA0202219 1 20021220 A 5420 BRACKET BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - METAL BRACKET HAS 1 INCH CRACK ON OUTBOARD EDGE OF RIGHT HAND NACELLE. REPAIRED IAW Q400 SRM 51-21-10, SRM 51-25-1 5 AND HORIZON AIR EA 6-54-180. 2 H 7 2 4T RT A13NM 2003020300090 20030203 00090 NM 2003 2 3 QXEA0202220 1 20021217 A 5320 PANEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - PANEL 122BR HAS A DENT IN IT AND GOUGED 3 INCHES FROM AFT SIDE AND 6 INCHES FROM TOP. REPAIRED IAW DHC-8 400 SRM 53-10-31, PAGE 102 AND HORIZON AIR EA 6-53-153. 2 H 7 2 4T RT A13NM 2003020300091 20030203 00091 NM 2003 2 3 QXEA0202221 1 20021216 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - SMALL GOUGE ON EXTERNAL FUSELAGE SKIN, WITH ADJACENT PAINT CHIP X484.5 Z111.0. REPAIRED IAW DHC-8 400 SRM 53-10-3 1-320-001 AND SRM 51-25-05-370-801. 2 H 7 2 4T RT A13NM 2003020300111 20030203 00111 NM 2003 2 3 QXEA0202222 1 20021217 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - SHALLOW DENT ON EXTERNAL FUSELAGE SKIN WITH ADJACENT PAINT CHIP AT X484.5 Z111.0. REPAIRED IAW DHC-8 400 SRM 51-2 5-370-801 ABD SRN 50-30-31. 2 H 7 2 4T RT A13NM 2003020300115 20030203 00115 NM 2003 2 3 QXEA0202223 1 20021219 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - PAINT WORN OFF AND EVIDENCE OF CHAFING/GOUGING ON RIGHT HAND INBOARD FLAP, TOP SKIN. REPAIRED IAW DHC-8 400 SRM 5 7-51-30, PARAGRAPH 2, TABLE 1, PAGES 101-102 AND HORIZON AIR EA 6-57-98. 2 H 7 2 4T RT A13NM 2003020300117 20030203 00117 NM 2003 2 3 QXEA0202224 1 20021223 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - CORROSION BETWEEN LOCATIONS 10.5 AND 12.5 FROM FORWARD SPLICE ON SEAT TRACK 3. REPAIRED IAW DHC08 SRM 51-40-11 AN D SRM 51-40-00. 2 H 7 2 4T RT A13NM 2003020300120 20030203 00120 NM 2003 2 3 QXEA0202226 1 20021222 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - CENTER OF SEAT TRACK NR 5 SCRATCHED BETWEEN LOCATION 18 INCHES AND 30 INCHES LEFT OF FORWARD SPLICE. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2003020300122 20030203 00122 NM 2003 2 3 QXEA0202227 1 20021222 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - CENTER OF SEAT TRACK NR 5 SCRATCHED BETWEEN LOCATIONS 50 INCHES AND 61 INCHES AFT OF FORWARD SPLICE. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2003020300124 20030203 00124 NM 2003 2 3 QXEA0202228 1 20021222 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - CORROSION ON SEAT TRACK NR 5, 43 INCHES AFT OF FORWARD SPLICE. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2003020300125 20030203 00125 WP 2003 2 3 2003FA0000080 1 20020918 A 6510 BEARING HUGHES 369 369D 4470706 WP T/R DAMPER MISMANUFACTURED B EOOR K NONE O OTHER IN INSP/MAINT 1 AL 03 DURING A RECEIVING INSPECTION OF A REPLACEMENT TAIL ROTOR DRIVE SHAFT, THE WHIP DAMPER BEARING SURFACE WAS FOUND TO BE W ITH MACHINING MARKS EVIDENT THROUGH THE CHROME PLATE. SEE MDH SOR NR 300189 AND REFER TO THE PREVIOUS SDR DATED 12 AUG 2002. 1 G 7 1 3U H3WE 2003020300126 20030203 00126 NM 2003 2 3 QXEA0202229 1 20021222 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - CENTER OF SEAT TRACK NR 5 SCRATCHED AND HAS CORROSION BETWEEN LOCATIONS 81 INCHES AND 94 INCHES AFT OF FORWARD SPL ICE. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2003020300127 20030203 00127 NM 2003 2 3 USAABB02198 1 20021130 A 2131 CONTROLLER BOEING 757 757225 1384959 NM CABIN PRESSURE MALFUNCTIONED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 602AU 22196 FLL - FLT 58 - IN CRUISE AT FL350, CREW RECEIVED THE CABIN ALTITUDE WARNING AS CABIN PRESSURE WAS INDICATING 10,000 FEET . CREW DESCENDED AT FL200, WHERE THE CABIN ALTITUDE WAS 8,500 FEET. FLIGHT CONTINUED TO FLL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED BITE CHECKS OF BOTH CONTROLLERS AND NOTED NO FAULTS. A VISUAL INSPECTION OF CABIN DOO RS SEALS WAS MADE WITH NO DEFECTS NOTED. THE AIRCRAFT WAS PRESSURIZED ON THE GROUND AND HELD PRESSURE SATISFACTORILY. THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4F RT A2NM 2003020300128 20030203 00128 EU 2003 2 3 USAASA02109 1 20021213 A 3350 2LA00354430 SOCKET AIRBUS 320 A320214 3930316 EU CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 101UW 0936 TPA - FOUND EMERGENCY LIGHTS IN AFT GALLEY INOPERATIVE. MAINTENANCE REPLACED THE AFT EMERGENCY CEILING LIGHT, FIN 207WL , DUE TO AN INTERMITTENTLY LOOSE SOCKET. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2003020300132 20030203 00132 EU 2003 2 3 USAASA02110 1 20021211 A 3397 WIRE AIRBUS A319 A319112 3930323 EU CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 713UW 1040 PHL - FOUND EMERGENCY LIGHT AT SEAT 4A INOPERATIVE. MAINTENANCE CONNECTED WIRES TO SEAT 4A. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2003020300133 20030203 00133 EU 2003 2 3 USAASA02114 1 20021218 A 3397 WIRE AIRBUS A319 A319112 3930323 EU CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 713UW 1040 TPA - FOUND THE EMERGENCY LIGHT AT SEAT 17C INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT THE CONNECTOR. (M) 2 L 7 2 4F RT A28NM 2003020300142 20030203 00142 NM 2003 2 3 2003FA0000093 1 20021204 A 2913 654463311 HOUSING BOEING 737 737* NM HYD PUMP CRACKED B IU6R O OTHER O OTHER NR NOT REPORTED 1 NM 01 HOUSING IS CRACKED IN PORT. 2 L 7 2 4F RT A16WE 2003020300144 20030203 00144 2003 2 3 4070198 4 20021219 A 2210 065005901 SERVO CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE AUTOFLIGHT OVERTORQUED B PCPR K NONE O OTHER IN INSP/MAINT 1 WP 25 822SA 719 208B0822 PECPC0766 COMPLIANCE WITH THE 1000 HOUR/ 12 MONTH KFC-150 AUTOPILOT SERVO CLUTCH TORQUE CHECK( TASK CODE 221009) OF SUBJECT SERVO REVEALED CLUTCH TORQUE TO BE 60 IN/LB, STC NR SA2053CED. SLIP CLUTCH VALUE TABLE SPECIFIES A TORQUE VALUE OF 43 IN/LB PLUS OR MINUS 4 IN/LBS. A RECORDS REVIEW REVEALED THAT THIS WAS THE FIRST COMPLIANCE OF THE TORQUE CHECK, INDICATING A POSSIBLE OUT OF SPECS CONDITION SINCE INSTALLATION DURING PRODUCTION BY THE MFG. TORQUE VALUE RESET TO SPECS AND SERVO WAS REINSTALLED. OPS CHECKS WERE OK. 1 H 7 1 3T 3 T A37CE E4EA 2003020300145 20030203 00145 CE 2003 2 3 AK62003F00000 1 20021101 A 5711 50110241 FITTING CESSNA 414 414A 2075907 CE CONT O520 TSIO520* 17040 SO LT SPAR CORRODED B AK6R K NONE O OTHER IN INSP/MAINT 1 SW 19 6562C 5076 414A0015 DURING AN ANNUAL INSPECTION IT WAS DISCOVERED THAT THE LT WING UPPER REAR SPAR FITTING WAS CORRODED. UPON REMOVAL OF TH E WING TO CHANGE THE FITTING, IT WAS DISCOVERED THAT THE LOWER AFT SPAR FITTING ALSO HAD CORROSION. BOTH FITTINGS WERE REPLACED. THE CORROSION APPEARS TO BE CAUSED BY EXHAUST GASES CIRCULATING IN THE GEAR WELL AND EVENTUALLY CONTACTING TH E FITTINGS. 1 L 7 2 3O 3 O A7CE E8CE 2003020300146 20030203 00146 CE 2003 2 3 AK62003F00001 1 20021101 A 5711 50110231 FITTING CESSNA 414 414A 2075907 CE CONT O520 TSIO520* 17040 SO LT WING SPAR CORRODED B AK6R K NONE O OTHER IN INSP/MAINT 1 SW 19 6562C 414A0015 DURING AN ANNUAL INSPECTION IT WAS DISCOVERED THAT THE LT WING UPPER REAR SPAR FITTING WAS CORRODED. UPON REMOVAL OF TH E WING TO CHANGE THE FITTING, IT WAS DISCOVERED THAT THE LOWER AFT SPAR FITTING ALSO HAD CORROSION. BOTH FITTINGS WERE REPLACED. THE CORROSION APPEARS TO BE CAUSED BY EXHAUST GASES CIRCULATING IN THE GEAR WELL AND EVENTUALLY CONTACTING TH E FITTINGS. 1 L 7 2 3O 3 O A7CE E8CE 2003020300147 20030203 00147 CE 2003 2 3 AK62003F00002 1 20021105 A 5711 50110231 FITTING CESSNA 414 414A 2075907 CE CONT O520 TSIO520* 17040 SO RT WING SPAR CORRODED B AK6R K NONE O OTHER IN INSP/MAINT 1 SW 19 2664L 4460 414A0535 DURING AN ANNUAL INSPECTION, DISCOVERED THE RIGHT WING UPPER SPAR FITTING CORRODED INSIDE THE AFT WHEELWELL SPAR ACCESS PANELS. THE WING WAS REMOVED AND THE FITTING WAS REPLACED. 1 L 7 2 3O 3 O A7CE E8CE 2003020300148 20030203 00148 NM 2003 2 3 USAASB02069 1 20020331 A 2131 7638101 CONTROLLER BOEING 737 7373B7 1384580 NM CABIN PRESSURE FAULTY A USAA G A O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 514AU 23700 RIC - FLT 1980 - EN ROUTE NAS TO LGA, AT FL330, LOST CABIN PRESSURIZATION, CABIN ALTITUDE WARNING SOUNDED. CABIN ALTITU DE WAS AT 10K FT AND CLIMBING AT 600 FPM. DESCENDED TO FL310. CREW ON OXYGEN. REGAINED CONTROL OF CABIN THROUGH USE O F MANUAL PRESSURIZATION MODE, FOR A SHORT TIME, CABIN BEGAN TO CLIMB AGAIN. DURING DESCENT THROUGH FL200, CABIN REACHED ITS MAX ALTITUDE OF 15K FT. O2 MASKS AUTO DEPLOYED AT FL280. DIVERTED TO RIC AND LANDED WITHOUT FURTHER INCIDENT. MA INTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. OPS CHECK GOOD. FOUND THE CARGO DOORS, SERVICE DOORS, EN TRY DOORS AND FUSELAGE DRAIN VALVES LEAKING. REPAIRED DOOR LEAKS AND REMOVED AND REPLACED FUSELAGE DRAIN VALVES. LEAK 2 L 7 2 4F RT A16WE 2003020300149 20030203 00149 GL 2003 2 3 ALG2003F00000 2 20021228 A 7321 23070611 FUEL CONTROL BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENGINE SURGES E ALGA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 03 27483 11697 37 45230 CAE860325 AFTER LANDING, WHILE AT FLIGHT IDLE THE ENGINE BEGAN TO SURGE, T.O.T. WOULD GO FROM 450C-500C AND N1 WOULD VARY FROM 60- 61.5 PERCENT. THE MECHANIC CHECKED THE FUEL SAMPLE, INSPECTED THE EXTERNAL FUEL FILTER, FUEL NOZZLE SCREEN FOR CONTAMIN ATION, NONE FOUND, REMOVED AND REPLACED THE FUEL CONTROL AND COMPLIED WITH PNEUMATIC CHECK AND AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003020300154 20030203 00154 SO 2003 2 3 BSY2003F00003 2 20021204 A 8500 ENGINE CESSNA 310 310R 2074245 CE CONT O520 IO520* 17032 SO RIGHT MALFUNCTIONED A BSYA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 07 6122C 310R1290 RT ENGINE ON CLIMB OUT, STARTED LOOSING POWER. RETURNED, MAINTENANCE INSPECTED ENGINE SUMPED OK, NO WATER NOTED. GROUN D RAN ENGINE, OPS CHECKED OK. NO FURTHER ACTION TAKEN. 1 L 7 2 3O 3 O 3A10 E5CE 2003020300155 20030203 00155 NM 2003 2 3 USAASB02117 1 20020617 A 3230 A42006028305 SOLENOID BOEING 737 737301 1384611 NM COCKPIT FAULTY A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 585US 23930 SYR - FLT 251 - AFTER T/O FROM SYR, COULD NOT GET THE GEAR HANDLE TO MOVE PAST THE 'OFF' POSITION. CREW DID NOT OVERRID E THE GEAR HANDLE BECAUSE OF A FLAPPING NOISE HEARD FROM THE NLG WW. FLT RETURNED TO FIELD AT SYR AND LANDED WITHOUT FU RTHER INCIDENT. AFTER LANDING, THE LANDING GEAR LATCH AND PRESSURE WARNING CIRCUIT BREAKERS WERE FOUND POPPED. MAINTEN ANCE INSPECTED AIRCRAFT INCLUDING NOSE GEAR, DOOR LINKAGE, WHEELS, TIRES, ETC AND FOUND NO DEFECTS. AIRCRAFT WAS FOUND IN SAFE AIRWORTHY CONDITION FOR A FERRY FLT. MAINTENANCE JACKED AIRCRAFT AND SWUNG GEAR SEVERAL TIMES AND WAS UNABLE TO DUPLICATE PROBLEM. R&R LANDING GEAR LEVER LATCH SOLENOID AND SWUNG GEAR. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003020300156 20030203 00156 CE 2003 2 3 BSY2003F00004 1 20021209 A 3260 15E13 DOWNLOCK SWITCH CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO LT MLG INOPERATIVE A BSYA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 5238J 310R0810 GOING INTO AIRPORT, LT MLG, NO DOWN AND LOCK INDICATION. TROUBLESHOT TO A BAD DOWN AND LOCK SWITCH, REMOVED AND REPLACE D SWITCH. OPS CHECKED GOOD. 1 L 7 2 3O 3 O 3A10 E5CE 2003020300157 20030203 00157 CE 2003 2 3 BSY2003F00006 1 20021225 A 3060 353801327 SWITCH BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO PROP HEAT INOPERATIVE A BSYA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 456WW TH444 AIRCRAFT LANDED WITH SMOKE IN COCKPIT. FOUND PROP HEAT SWITCH CAUSING PROBLEM. REMOVED AND REPLACED SWITCH. OPS CHECK ED GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 2003020300158 20030203 00158 NM 2003 2 3 USAASB02205 1 20021117 A 2150 A/C PACK BOEING 737 7374B7 1384702 NM A/C BAY MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 434US 24556 CLT - FLT 1434 - EN ROUTE FROM TPA-PHL, THE RIGHT PACK TRIPPED AND THE FORWARD CABIN ZONE TEMPERATURE LIGHT WOULD NOT RE SET. CREW WAS UNABLE TO CONTROL CABIN/COCKPIT TEMPERATURE. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE ZONE TEMPERATURE CONTROL CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BRE AKER. OPERATIONALLY CHECKED RIGHT PACK FOR THIRTY MINUTES. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2003020300159 20030203 00159 CE 2003 2 3 CGO2003F00000 1 20021219 A 2840 12181302 TRANSMITTER RAYTHN 390 390 CE FUEL FLOW LEAKING B CGOR K NONE K FLUID LOSS IN INSP/MAINT 1 GL 03 324AM 180 RB42 INVESTIGATED FUEL LEAK, FOUND IN RT ENGINE COMPARTMENT DURING ROUTINE 200 HR INSPECTION. FOUND FUEL TO BE LEAKING INTER NALLY INTO TRANSMITTER ELECTRICAL CONNECTOR AREA. OVERHAULED REPLACEMENT PART RECEIVED HAD SAME FAULT . PART MFG, SUSP ECT PART HAS DESIGN FAULT. 1 7 2 3F RT A00010WI 2003020300160 20030203 00160 NM 2003 2 3 USAASB02206 1 20021120 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 334US 23231 IND - MAINTENANCE FOUND THE EMERGENCY LIGHTS FROM SEAT ROW 5 THROUGH THE OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003020300161 20030203 00161 CE 2003 2 3 CGO2003F00001 1 20021219 A 3397 D010NEGE03816 WIRE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LANDING LIGHT SHORTED B CGOR K NONE O OTHER IN INSP/MAINT 1 GL 03 481CW RK1 WHILE TROUBLESHOOTING INOPERATIVE RT LANDING LIGHT, FOUND WIRE BURNED WHERE HAD SHORTED TO LANDING LIGHT ASSY. SHELL AP PROX. 2 INCHES FROM TERMINAL END. CRIMPED ON TYPE TERMINAL INSULATION MELTED, ADJACENT WIRE INSULATION PARTIALLY MELTED AND SPLIT, EXPOSING CORE WIRING. COMMONLY FOUND DEFECT ON AIRCRAFT WHEN REPLACING LANDING LIGHT LAMPS. SUGGEST A BETT ER INSTALLATION DESIGN THAT REDUCES HEAT EXPOSURE AND CHAFING DAMAGE BE INVESTIGATED. WIRING APPEARS ORIGINAL. 2 H 7 2 4F 4 F RT A16SW E25EA 2003020300162 20030203 00162 NM 2003 2 3 USAASB02207 1 20021121 A 5610 5893543110 WINDSHIELD BOEING 737 737401 1384701 NM COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 424US 23991 PIT - FLT 1246 - EN ROUTE FROM PIT TO BWI, THE FIRST OFFICERS WINDSHIELD CRACKED. ICING IN THE BWI AREA WAS A CONCERN W HEN CONSIDERING CONTINUING THE FLIGHT. FLIGHT ENDED UP RETURNING TO FIELD AT PIT WHERE IT LANDED WITHOUT FURTHER INCIDE NT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD. ALSO, REMOVED AND REPLACED THE NR 4 WINDSHIELD HEA T CONTROLLER. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003020300171 20030203 00171 CE 2003 2 3 FFS2003F00008 1 20021231 A 5410 1189100367 SEAL BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NACELLE MISALIGNED E FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 575X UC149 FOUND BAFFLE SEALS BETWEEN FORWARD AND AFT NACELLE BULKHEADS, BOTH ENGINES TO BE TRAPPED BETWEEN BULKHEADS, NOT ALIGNED WITH THEM. THIS WILL CAUSE BULKHEADS TO CRACK. 2 L 7 2 4T 4 T RT A24CE E4EA 2003020300174 20030203 00174 NM 2003 2 3 USAASB02208 1 20021121 A 7930 WARNING LIGHT BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU COCKPIT ILLUMINATED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 429US 24551 721143 PBI - FLT 1246 - ON CLIMB-OUT FROM MIA, EN ROUTE TO PIT, THE NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ALL OTHER ENGINE INDICATIONS WERE NORMAL. CREW OPERATED THE NR 2 ENGINE AT REDUCED THRUST BUT THE LIGHT STILL FLICKERED OFF AND ON. FLIGHT DIVERTED TO PBI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 2003020300175 20030203 00175 NM 2003 2 3 USAASB02209 1 20021122 A 3230 CONTROL CABLE BOEING 737 737301 1384611 NM MLG W/W OUT OF ADJUST A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 574US 23739 PIT - FLT 1025 - PREPARING TO LAND AT PIT, CREW RECEIVED THREE GREEN AND THREE RED LANDING GEAR LIGHTS DURING GEAR EXTEN SION. CREW RECYCLED GEAR AND RECEIVED NORMAL GEAR INDICATION OF 3 GREEN GEAR LIGHTS. FLIGHT LANDED WITHOUT FURTHER INC IDENT. MAINTENANCE FOUND LANDING GEAR CABLES LGVA AND LGVB TO BE 30 LBS LOW ON TENSION. ADJUSTED TENSION OF CABLES PER MM 32-31-00-735-001. INDICATION AND OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2003020300177 20030203 00177 NM 2003 2 3 USAASB02210 1 20021124 A 5210 65C80736354 DOOR BOEING 737 737301 1384611 NM MAIN ENTRY OUT OF RIG A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 300AU 23228 IND - FLT 338 - ON CLIMB-OUT FROM IND, EN ROUTE TO CLT, THE FORWARD MAIN ENTRY DOOR WARNING LIGHT ILLUMINATED. CREW REP ORTED THE HANDLE COMES UP IN FLIGHT WHEN PRESSURIZED AND THE LIGHT WILL GO OFF AND ON AS HANDLE IS PRESSED DOWN TO CLOSE D POSITION. FLIGHT RETURNED TO FIELD AT IND AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENAN CE RIGGED THE MAIN ENTRY DOOR PER MM 52-11-00. OPERATIONAL TEST AND LEAK TEST NORMAL. (M) 2 L 7 2 4F RT A16WE 2003020300178 20030203 00178 EA 2003 2 3 A6WA200240030 1 20021220 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 31 422AW 7341 STRONG FUEL SMELL WHEN SWITCHING BLEEDS OVER TO APU AIR. PERSISTED AFTER LANDING. RAN ENGINES AND APU AT 70 PERCENT FO R 20 MINUTES, ODOR DIMINISHED. OP CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2003020300179 20030203 00179 EA 2003 2 3 A6WA200240031 1 20021220 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA A/C BAY MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 412AW 7582 RIGHT PACK HIGH PRESSURE 80 PSI RUNNING QRH GOT LEFT PACK HIGH PRESSURE. RETURNED TO AIRPORT. DEPOWERED AND REPOWERED AIRCRAFT. RESET PACKS CIRCUIT BREAKERS. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2003020300181 20030203 00181 EA 2003 2 3 A6WA200240032 1 20021119 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 LEFT SIDE FLOOR SUPPORT ANGLE 621 CRACKED. CUT AND REMOVED CRACKED FLOOR SUPPORT ANGLE AT FS 621, LEFT SIDE. FITTED AN D DRILLED NEW REPAIR ANGLES. INSTALLED REPAIR ANGLES AND STRUT P-5. (M) 2 L 7 2 4F RT A21EA 2003020300183 20030203 00183 EA 2003 2 3 A6WA200240033 1 20021117 A 5320 6013501252 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 FOUND FS 625 RIGHT OBLIQUE ANGLE. REMOVED AND REPLACED ANGLE. (M) 2 L 7 2 4F RT A21EA 2003020300185 20030203 00185 EA 2003 2 3 A6WA200240034 1 20021117 A 5320 6013501251 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 FOUND FS 625 LEFT OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE. (M) 2 L 7 2 4F RT A21EA 2003020300187 20030203 00187 EA 2003 2 3 A6WA200240035 1 20021123 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 LEFT WING FUEL ACCESS PANEL HOLES 540CB, 540DB, 540EB, 550AB, 550BB, 550FBM ABD 550GB HAVE MINOR CORROSION COMPLIED WITH BOMBARDIER AEROSPACE, CANDAIR REGIONAL JET, SB 601R-57-030 REV O, AND BOMARDIER REO 601R-57-21-030. (M) 2 L 7 2 4F RT A21EA 2003020300188 20030203 00188 EA 2003 2 3 A6WA200240036 1 20021123 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 RIGHT WING FUEL PANEL ACCESS HOLES 610AB, 610BB, 640AB, 640CB, 640EB, AND 650DB HAVE MINOR CORROSION. COMPLIED WITH BOM BARDIER AEROSPACE, CANDAIR REGIONAL JET, SB 601R-57-030 REV O AND BOMBARDIER REO 601R-57-21-030. (M) 2 L 7 2 4F RT A21EA 2003020300189 20030203 00189 EA 2003 2 3 A6WA200240037 1 20021125 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 RIGHT FS 718 FRAME FLANGE BELOW STRINGER 11 IS CRACKED INCORPORATED CANDAIR REO 601R-53-61-193 REV A AND WVAC EO 601R-53 -3636. (M) 2 L 7 2 4F RT A21EA 2003020300190 20030203 00190 EA 2003 2 3 A6WA200240038 1 20021126 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 FS 718 FRAME WAS FOUND CRACKED BELOW STRINGER 11, LEFT REPAIRED FRAME IAW WVAC EO 601R-53-3636 AND BOMBARDIER REO 601R-5 3-61-193 REV A. (M) 2 L 7 2 4F RT A21EA 2003020300191 20030203 00191 EA 2003 2 3 A6WA200240039 1 20021126 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 RIGHT FRAME IS CRACKED IN RADIUS AT STRINGER 10, CRACK LENGTH IS APPROX .6 INCHES. PERFORMED PART C OF SB 601R-53-061 R EV A. (M) 2 L 7 2 4F RT A21EA 2003020300192 20030203 00192 EA 2003 2 3 A6WA200240040 1 20021118 A 5311 6013600124 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 FOUND FS 640 FRAME LEFT IS CRACKED IN RADIUS AT STRINGER 11. REPAIRED FS 640 FRAME IAW SERVICE BULLETIN 601R-53-061. R EV A BY COMPLYING WITH PART C OF SERVICE BULLETIN. (M) 2 L 7 2 4F RT A21EA 2003020300193 20030203 00193 EA 2003 2 3 A6WA200240041 1 20021211 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 WHILE PERFORMING SB 601R-53-059 FOUND BL0 BULKHEAD Z-MEMBER TO HAVE A CHAFE IN THE RADIOUS APPROX 12 INCHES FROM TOP AT FS 624. REPAIRED Z-MEMBER AT BL0, FS 624 IAW WEST VIRGINIA AIR CENTER EO NR 601R-53-3674A. (M) 2 L 7 2 4F RT A21EA 2003020300194 20030203 00194 EA 2003 2 3 A6WA200240042 1 20021207 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA FLAP VANE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 THE RIGHT INBOARD FLAP LEADING EDGE VANE CAP INBOARD SKIN IS CHAFED (WHERE THE INBOARD VANE CAP RESTS ON THE BUMPER PADS /TEFLON STOPS. REMOVED CHAFED VANE CAP. FABRICATED AND INSTALLED A NEW VANE CAP IAW WVAC EO 601R-57-3659B. (M) 2 L 7 2 4F RT A21EA 2003020300195 20030203 00195 EA 2003 2 3 A6WA200240043 1 20021207 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA FLAP VANE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 LEFT INBOARD FLAP VANE LEADING EDGE IS CHAFED AT STOP CONTACT POINTS IN 3 PLACED, .010 IN TO .040 IN DEEP PERFORMED A MA JOR REPAIR TO THE LEFT INBOARD FLAP VANE LEADING EDGE IAW WVAC EO 601R-57-3659B. (M) 2 L 7 2 4F RT A21EA 2003020300196 20030203 00196 EA 2003 2 3 A6WA200240044 1 20021206 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 MWD 131 AND 132 THE ATTACH ANGLES ON THE INTERCOSTAL AT FS 484, BL 27 LEFT AND RIGHT WERE FOUND CRACKED. THE CRACKED AN GLES WERE REMOVED. NEW (REPAIR) ANGLES WERE FABRICATED AND INSTALLED IAW WVAC EO 601R-53-3663. (M) 2 L 7 2 4F RT A21EA 2003020300200 20030203 00200 EA 2003 2 3 A6WA200340001 1 20021214 A 3260 UPLOCK SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A A6WA O OTHER N FALSE WARNING CL CLIMB 1 GL 31 432AW 7257 AFTER TAKEOFF WITH GEAR HANDLE UP, GEAR UP DISAGREE AND NOSE DOOR OPEN MESSAGES ILLUMINATED. REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK SENSOR. (M) 2 L 7 2 4F RT A21EA 2003020300201 20030203 00201 CE 2003 2 3 GUU2003F00005 1 20021224 A 2612 CONNECTOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA FIRE LOOP DIRTY A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 17 87551 UE206 ON PREFLIGHT, THE FIREWALL SHUT OFF HANDLE ILLUMINATES WHEN LEFT FIRE LOOP IS TESTED. CLEANED LEFT FORWARD FIRE LOOP CO NNECTOR OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E2NE 2003020300202 20030203 00202 CE 2003 2 3 HYI2003F00000 1 20021122 A 2750 500000862 CONTROL CABLE CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO TE FLAPS BROKEN E HYIA K NONE O OTHER IN INSP/MAINT 1 NM 01 2651S 5768 402C0342 UPON INSPECTION, FOUND LT & RT FLAP CABLE ASSEMBLIES TO HAVE BROKEN STRANDS (APPROX 10 TO 15 PERCENT) AT THE POINT WHERE THE CABLE ENTER THE SWEDGED STRAIGHT SHOOK ENDS. NO OTHER AREAS OF THE CABLES SHOWED SIGNS OF BROKEN STRANDS. THE SHA NK ENDS WITH BROKEN STRANDS SHOWED SIGNS OF BEING SWEDGED IMPROPERLY, SUGGEST TIME CHANGING FLAP CABLES. 1 L 7 2 3O 3 O A7CE E8CE 2003020300203 20030203 00203 WP 2003 2 3 IZ22003F00001 2 20021220 A 7310 69254513 SOLENOID VALVE MTSBSI MU2 MU2B36 5780412 CE GARRTT TPE331 TPE331* 01514 WP FUEL SYSTEM LEAKING B IZ2R K NONE K FLUID LOSS IN INSP/MAINT 1 SW 15 13YS 121 694 VALVE LEAKING FUEL BETWEEN THE SOLENOID AND VALVE BODY DUE TO BLOWN O-RING. THE FUEL WAS LEAKING INTO THE COWLING AND D RIPPING OUT. 1 H 7 2 3T 3 T RT A10SW E2WE 2003020300204 20030203 00204 EA 2003 2 3 A6WA200340002 1 20021216 A 7810 22850181267 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA EXHAUST NOZZLE MISSING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 DURING REMOVAL AND REPLACEMENT OF LEFT LOGO LIGHT, NOTICED ACCESS PANEL MISSING ON INBOARD SIDE OF EXHAUST NOZZLE. REMO VED AND REPLACED LEFT ENGINE EXHAUST NOZZLE. (M) 2 L 7 2 4F RT A21EA 2003020300206 20030203 00206 EA 2003 2 3 A6WA200340003 1 20021218 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG LOW A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 432AW 7257 RECEIVED NOSE GEAR OPEN WARNING IN FLIGHT AND GEAR DISAGREE MESSAGE IN FLIGHT. SERVICED STRUT. (M) 2 L 7 2 4F RT A21EA 2003020300208 20030203 00208 EA 2003 2 3 A6WA200340006 1 20021220 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 FOUND FS 621 ANGLE ON LEFT SIDE OF CARGO BAY IS CRACKED .25 INCH, INCORPORATED CANADAIR REO 601R-53-61-004 REV B. (M) 2 L 7 2 4F RT A21EA 2003020300209 20030203 00209 EA 2003 2 3 A6WA200340007 1 20021220 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 PASSENGER DOOR SEAL STRINGER AT FS 349, 18 INCHES ABOVE STRINGER 18 IS DAMAGED AT FS 349 APPROXIMATELY 18 INCHES UP FROM BOTTOM OF STRINGER 18. COMPLIED WITH REO 601R-52-11-008. (M) 2 L 7 2 4F RT A21EA 2003020300210 20030203 00210 WP 2003 2 3 ASAA0280352 1 20021005 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING LINE CHECK, ONE EMERGENCY TRACK LIGHT AT ROW 1 WAS FOUND TO BE INOPERATIVE. REPLACED BROKEN WIRE. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2003020300211 20030203 00211 WP 2003 2 3 ASAA0280355 1 20021004 A 5347 SR095301157001 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, FOUND SEAT TRACK CORRODED BEYOND LIMITS AT LBL 22 FROM FS 1122 AND AT 1229. REPLACED SEAT TRACK FROM FS 1085-1310 PER SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2003020300212 20030203 00212 WP 2003 2 3 ASAA0280356 1 20021004 A 5320 993053812 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING 30K CHECK, FOUND CUSP WEB CORRODED AT FS 503-522, 522-541, AND 541-560. REPLACED CUSP WEB AT FS 503-597, R BL 44-58 PER SRM 51-30-5 AND 51-30-02. (M) 2 L 7 2 4F RT A6WE 2003020300213 20030203 00213 WP 2003 2 3 ASAA0280357 1 20021004 A 5320 993053875N WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, CUSP WEB CORRODED AT FS 398, 448, 478, 482, 488, AND 500, BUTTOCK STA'S RBL 44-58. REPLACED CUSP WEB AT FS 389-503 PER SRM 51-30-5 AND 51-30-02. (M) 2 L 7 2 4F RT A6WE 2003020300214 20030203 00214 WP 2003 2 3 ASAA0280358 1 20021004 A 5320 993053877 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, CUSP WEB CORRODED AT FS 602, 614, 617-630, 636-655, AND 655-674 STA'S AT BUTTOCK LINE STA'S RBL 4 4-58. REPLACED CUSP WEB AT FS 598-712 PER SRM 51-30-5 AND 51-30-02. (M) 2 L 7 2 4F RT A6WE 2003020300215 20030203 00215 WP 2003 2 3 ASAA0280359 1 20021009 A 5320 5936597505 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, FLOOR SUPPORT AT FS 1155, LONGERON 28L-29R CORRODED. REPLACED SUPPORT. (M) 2 L 7 2 4F RT A6WE 2003020300216 20030203 00216 WP 2003 2 3 ASAA0280360 1 20021011 A 5313 59360481N LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, SECTION OF LONGERON 29R CORRODED AT FS 1231-1260. REPLACED CORRODED SECTION PER SRM 51-30-5. (M ) 2 L 7 2 4F RT A6WE 2003020300217 20030203 00217 WP 2003 2 3 ASAA0280362 1 20021011 A 5313 59360631 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - FOUND DURING C-CHECK, CORROSION ON LONGERON 30 IN MID CARGO BAY AT FS 636-693. SPLICED IN NEW SECTION OF LONGERON 30 FROM STA 588-655 PER EA 5310-02110. (M) 2 L 7 2 4F A6WE 2003020300218 20030203 00218 WP 2003 2 3 ASAA0280363 1 20021011 A 5310 5930584123 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 OAK - DURING C-CHECK, FOUND LEFT MLG WHEEL WELL DOOR JAMB CRACKED AT FORWARD OUTBOARD SIDE. REPLACED DOOR JAMB PER SRM 51-30-2, PAGE 4-12. (M) 2 L 7 2 4F A6WE 2003020300219 20030203 00219 WP 2003 2 3 ASAA0280365 1 20021011 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 RNO - DURING PREFLIGHT CHECK, ONE EMERGENCY TRACK LIGHT AT ROW 6 WAS FOUND TO BE INOPERATIVE. REPAIRED WIRE. LIGHTS TH EN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2003020300220 20030203 00220 WP 2003 2 3 ASAA0280439 1 20021024 A 3350 0105606 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 3. REPLACED LIGHT MODULE (LENS/BULB). RES ECURED COVER. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2003020300221 20030203 00221 WP 2003 2 3 ASAA0280445 1 20021028 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN SHORTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 OAK - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE BEYOND ROW 26. REPAIRED AND REPOSITIONED CONNECTOR WIR E WHICH WAS SHORTING ON A PNEUMATIC DUCT. (M) 2 L 7 2 4F A6WE 2003020300222 20030203 00222 NM 2003 2 3 ASAA0290004 1 20021014 A 5313 143A322184 STRINGER BOEING 737 737990 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 305AS 30013 SEA - DURING C-CHECK, FOUND STRINGER 19L DENTED. REPAIRED STRINGER PER SRM 53-00-03. (M) 2 L 7 4 4F RT A16WE 2003020300223 20030203 00223 EA 2003 2 3 ASOA02620 1 20021204 A 4920 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY MALFUNCTIONED A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 11 837AS 10349 7271 FLT 4403 - DURING DESCENT INTO GRR, THE CAPTAIN REPORTED A STRONG FUEL SMELL DURING AND AFTER STARTING THE AUXILIARY POW ER UNIT. THE AIRCRAFT LANDED SAFELY IN GRR. MAINTENANCE REMOVED AND REPLACED THE AUXILIARY POWER UNIT. OPERATIONAL AN D LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003020300224 20030203 00224 EU 2003 2 3 ASOA02621 1 20021204 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72 EU CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 643AS 12850 413 FLT 4295 - DURING GROUND INSPECTION IN ATL, THE AFT EMERGENCY LIGHT CAME ON INTERMITTENTLY. MAINTENANCE REMOVED AND REP LACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2003020300225 20030203 00225 SO 2003 2 3 ASOA02622 1 20021205 A 2120 SMOKE EMB 120 EMB120ER 3260203 SO CABIN DETECTED A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 11 262AS 120146 FLT 4199 - DURING FINAL APPROACH INTO ATL, SMOKE OCCURRED IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LAND ED SAFELY IN ATL. MAINTENANCE CHECKED THE ENVIRONMENTAL CONTROL SYSTEM BY UTILIZING ALL BLEED SOURCES FOR THIRTY MINUTE S. NO SMOKE OR ABNORMAL ODOR OCCURRED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2003020300226 20030203 00226 SO 2003 2 3 ASOA02623 1 20021209 A 2120 SMOKE EMB 120 EMB120ER 3260203 SO CABIN DETECTED A ASOA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 11 262AS 120146 FLT 4167 - DURING CLIMB-OUT FROM ATL-GTR, SMOKE OCCURRED IN THE CABIN WITH THE LAVATORY SMOKE DETECTOR SOUNDING CONTINUO USLY. THE SMOKE WAS VERY DENSE AND APPEARED TO BE PACK RELATED. IT SEEMED TO DISAPPEAR SLOWLY WHEN THE LEFT PACK WAS T URNED OFF. THE CREW COMPLIED WITH THE QRH. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. (M) 2 L 7 2 4T RT A31SO 2003020300227 20030203 00227 NM 2003 2 3 GAIAOP156 1 20021112 A 3610 CLAMP BOEING 727 727223 1384074 NM BLEED AIR SYS LOOSE A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6810 19485 FLIGHT 1111 - LAX-STL - AFTER TAKEOFF, WHILE AT CLIMB POWER THE FLIGHT CREW NOTICED THAT THE AFT BODY OVERHEAT LIGHT ILL UMINATED. ACCOMPLISHED AOM PROCEDURE AND THE LIGHT EXTINGUISHED. THE AIRCRAFT DIVERTED TO PHX AND LANDED WITHOUT FURTHE R INCIDENT. INSPECTION FOUND AN AIR LEAK AT THE RIGHT FLOW CONTROL VALVE. THE CLAMP WAS REPOSITIONED AND TIGHTENED. O PERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2003020300228 20030203 00228 WP 2003 2 3 GTIA020519 1 20020504 A 2133 VALVE DOUG DC9 DC982 3022082 WP CABIN PRESSURE FAILED A GTIA G A O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 823NK 48020 FL310, CABIN CLIMB GAUGE READS PLUS 500 SHORTLY AFTER FLOW LIGHT. CABIN PRESS READS 5.500 FT. NORMAL CABIN STARTING A SLOW CLIMB THAT COULD NOT BE STOPPED, EVEN WITH CONTROLLER MANUAL/FULL CLOSED. AT ABOUT 8800 FT CABIN ALT STOPPED EMERG ENCY DESCENT. COMPLIED WITH ALL QRH ITEMS. DIVERTED TO ACY. CABIN NEVER RECOVERED. CABIN ALT NEVER ABOVE 15K. ALL M ASKS DROPPED AS REQ 39329-2 DECAY CHECK REQUIRED REF TO TIME 39329-3, 39329-3. FOUND AFT SAFETY VALVE TO BE OPENING AT 7.6 PSI VALVE CHECKED BAD .39330-2 POST MAINTENANCE TEST FLIGHT DUE FOR PRESSURIZATION. AFT CABIN SAFETY VALVE WAS FOUN D BAD AND CHANGED AND CABIN DECAY CHECKED ALSO PERFORMED AUTO PRESSURIZATION CHECK. (M) 2 L 7 2 4F A6WE 2003020300229 20030203 00229 NM 2003 2 3 KPVA200232 1 20021024 A 2611 CONNECTOR DHAV DHC8 DHC8103 1386005 NM SMOKE WARNING DIRTY A KPVA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 806WP 357 HNL - FLT 1620 - SMOKE WARNING FLICKERED ON AND OFF MOMENTARILY IN FLIGHT. CLEARED MEL 26-8-1. CLEANED CANNON PLUGS AN D INSPECTED BAGGAGE COMPARTMENT NR 2 SMOKE DETECTOR. SYSTEM OPS CHECK GOOD IAW DHC 8 MM 26-12-00 PAGE 201. (M) 2 H 7 2 4T RT A13NM 2003020400003 20030204 00003 CE 2003 2 4 J7B2003F00000 1 20021216 A 5730 RIVET CESSNA 208 208B 2073701 CE PWA PT6 PT6A45 52043 EA WING SKIN LOOSE E J7BA K NONE O OTHER IN INSP/MAINT 1 SW 01 64BP 6400 208B0604 LOOSE AND WORKING RIVETS IN INBOARD LEADING EDGE ATTACHMENT TO FORWARD SPAR RT AND LT WING. 1 H 7 1 3T 4 T A37CE E4EA 2003020400004 20030204 00004 NM 2003 2 4 KPVA200240 1 20021217 A 3397 WIRE GRIMES DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE LIGHT BROKEN A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808WP 026 EMERGENCY FLOOR PATH LIGHTING ASSEMBLY AT ABOUT SEAT 6CD, INOPERATIVE. INSPECTED LIGHTING ASSEMBLY AND FOUND BROKEN WIR E AT THE ABOVE MENTIONED LOCATION. REMOVED AND REPLACED LIGHTING ASSEMBLY. OPERATIONAL CHECKS COMPLETED IAW MM. THERE WERE NO DEFECTS NOTED. SYSTEM RETURNED TO SERVICEABLE CONDITION. 2 H 7 2 4T 4 T RT A13NM E20NE 2003020400005 20030204 00005 NM 2003 2 4 KPVA200241 1 20021220 A 3350 BATTERY DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE LIGHT WEAK A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807WP 261 63436 023 PORTABLE EMERGENCY EXIT LIGHT BATTERY WEAK. REMOVED AND REPLACED PORTABLE EMERGENCY EXIT LIGHT AND OPS CHECK IAW MM. O PS CHECKED GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2003020400006 20030204 00006 NM 2003 2 4 KPVA200242 1 20021225 A 3350 1155591 LIGHT DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE CABIN LOOSE A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805WP 353 EMERGENCY EXIT LIGHT/SIGN BY SEAT 1E, LOOSE. C/A: REMOVED AND REPLACED EMERGENCY EXIT LIGHT/SIGN IAW MM. OPS CHECK GO OD IAW MM. 2 H 7 2 4T 4 T RT A13NM E20NE 2003020400007 20030204 00007 NM 2003 2 4 KPVA200244 1 20021229 A 3330 CM376AS15 LIGHT DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE CARGO BAY INOPERATIVE A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808WP 026 NR 2 BAGGAGE COMPARTMENT SMOKE DETECTOR, INOPERATIVE. NO TEST. SYSTEM VERIFIED INOPERATIVE AND DEFFERED IAW MEL. ON 12 -30-02 MAINTENANCE CLEARED MEL DEFFERAL BY REMOVING AND REPLACING THE NR 2 BAGGAGE SMOKE DETECTOR LAMP. SYSTEM OPS CHEC KED IAW MM. 2 H 7 2 4T 4 T RT A13NM E20NE 2003020400009 20030204 00009 CE 2003 2 4 LC12003F00000 1 20021129 A 5521 12346011 RIB CESSNA 182 182S 2072701 CE LYC O540 IO540* 41532 EA ELEVATOR CRACKED B LC1R K NONE O OTHER IN INSP/MAINT 1 EA 07 7275H 1906 18280396 DURING COMPLIANCE WITH SB FOR ELEVATOR RIVET INSTALLATION, THE ELEVATOR TOP, BOTTOM, AND TIP SKINS WERE CRACKED AND THE TIPS COULD BE FLEXED EASILY UP AND DOWN. AFTER REMOVING THE PLASTIC TIPS TO ACCOMPLISH THE SERVICE BULLETIN, IT WAS NOT ED THAT THE ELEVATOR TIP TO ACCOMPLISH THE SERVICE BULLETIN, IT WAS NOTED THAT THE ELEVATOR TIP RIBS HAD NOT BEEN RIVETE D TO THE ELEVATOR SPAR END FLANGE. THE HOLES WERE IN THE TIP RIB AND SHOULD HAVE HAD RIVETS INSTALLED AT THE FACTORY BU T THERE WERE NO HOLES DRILLED IN THE SPAR FLANGE TO ACCEPT THE RIVETS. INSTRUCTIONS ARE IN THE SERVICE BULLETIN TO REPL ACE THESE TWO RIVETS WITH BLIND FASTENERS. 1 H 7 1 3O 3 O NT 3A13 1E4 2003020400010 20030204 00010 NM 2003 2 4 LI32003F00000 1 20021002 A 4930 4950084 MANIFOLD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE APU FUEL BROKEN B LI3R O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 09 908UA 25008 AIRLINE REPORTED THE FOLLOWING APU AUTO SHUTDOWN WITH LARGE AMOUNT OF FUEL COMING OUT OF APU AREA. FUEL FOUND TO BE FRO M FUEL LINE NOZZLE NEAR TOP ON LEFT SIDE OF APU. FUEL DID NOT IGNITE. MAIN FUEL MANIFOLD HAS ONE BROKEN TUBE BETWEEN T HE FLEXIBLE FIRE SLEEVE AND THE B-NUT TO THE FUEL INJECTOR. MANIFOLD HAS 14 FUEL TUBES. MANIFOLD IS UNDERGOING DETAILE D ANALYSIS. 2 L 7 2 4F 4 F RT A16WE E2GL 2003020400015 20030204 00015 SW 2003 2 4 NXT2003F00000 1 20021202 A 5302 SKIN BELL 222 222U 1182140 SW TAIL BOOM CRACKED E NXTA K NONE O OTHER IN INSP/MAINT 1 SW 19 20171 11517 47535 FOUND CRACK ON UPPER SKIN OF TAILBOOM UNDERNEATH NR 4 HANGER BEARING AT STA 473 TO 489, DURING INSPECTION. 1 G 7 2 3U H9SW 2003020400016 20030204 00016 SO 2003 2 4 O2G2003F00003 1 20021225 A 2897 082011013 HARNESS GULSTM G1159 G1159B 3953535 SO RT FUEL TANK INTERMITTENT E O2GA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NE 03 677CX 11534 10 RT WING HEAVY CONDITION CAUSED BY FUEL IMBALANCE. ON CLIMB OUT, FUEL MIGRATED TO WING TIPS MAKING IMBALANCE SEEM MORE T HAN IT WAS. BOTH FUEL TANKS OPENED, INSPECTED ALL PROBES, CONNECTORS, AND WIRING. REPLACED ANY CONNECTORS THAT COULD H AVE HAD CORROSION STARTING OR BROKEN WIRE STRANDS. CHECKED FOR EVIDENCE OF WATER AND CLEANED ALL PROBES. TESTED FUEL S YSTEM WITH TESTING UNIT AND CALIBRATED TO CORRECT LIMITS. NO OTHER FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE WITH NO PROBLEMS. 2 L 7 2 4F RT A12EA 2003020400116 20030204 00116 GL 2003 2 4 UIEA200200070 2 20021218 A 7200 CF680C2B5F ENGINE BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL NR 1 FAILED A UIEA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 EA 15 492MC 30558 DIVERSON DUE INFLIGHT ENGINE SHUTDOWN. ON CLIMB OUT TWO LARGE BANGS FROM NR 1 ENGINE. VIB 5.0. ENGINE SHUTDOWN. AIRC RAFT DIVERTED TO MIA. FUEL DUMPED. MAINTENANCE ADVISED OF EVIDENCE OF METAL IN TAIL PIPE. BOROSCOPE CONFIRMED HC DAMA GE. REMOVED AND REPLACED NR1 ENGINE IAW MM. LEAK CHECK. OK IAW MM. SN 706201. 2 L 7 4 4F 4 F RT 1384945 E23EA 2003020400118 20030204 00118 NE 2003 2 4 USAASB02238 2 20021227 A 7200 CFM563B220 ENGINE BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE RIGHT ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 517AU 31540 560 23703 725720 PILOT REPORTED THE AFT LAVATORY SMOKE DETECTORS SOUNDED DUE TO AN OIL ODOR IN THE CABIN. FLIGHT LANDED AT EWR WITHOUT F URTHER INCIDENT. MAINTENANCE INSPECTED DUCTING AND ISOLATED OIL ODOR COMING FROM RT ENGINE. (RT ENGINE RECENTLY EXPERIE NCED AN IMPACT WITH SNOW BANK DURING TAXI) ACCOMPLISHED EXTENDED ENGINE RUN IN AN ATTEMPT TO BURN THE OIL CONTAMINATION OUT OF THE ENGINE. RAN ENGINE UNTIL CLEARED. ONLY A FAINT RESIDUAL ODOR REMAINING. REMOVED AND REPLACED WATER SEPARA TOR BAGS (P/N V121-1). OPERATIONAL CHECK NORMAL. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2003020400119 20030204 00119 CE 2003 2 4 VJ32003F00000 1 20021231 A 3610 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO AIR PUMP FAILED B VJ3R O OTHER L NO TEST TX TAXI/GRND HDL 1 WP 07 5530A 520 CE1342 820457R DURING GROUND RUN UP, OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHT RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERTY. BELIE VE DRY AIR PUMP VANES ARE WORN. 1 L 7 1 3O 3 O 3A15 E5CE 2003020400120 20030204 00120 EU 2003 2 4 VJ32003F00003 1 20021204 A 7120 120A6100 SHOCK MOUNT GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA LT ENGINE DAMAGED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 862AF 643 85002 DURING PROGRESSIVE INSPECTION OF ENGINE BAY, FOUND LOWER LEFT LORD MOUNT DAMAGED FROM HEAT OF EXHAUST SYSTEM. SUGGEST I NSTALLING SOME TYPE OF HEAT SHIELDING OR CHANGING MOUNT TO A MORE HEAT RESISTANT STYLE. PART RETURNED FOR WARRANTY. 1 L 7 1 3O 3 O RT A49CE 1E4 2003020400121 20030204 00121 EU 2003 2 4 VJ32003F00004 1 20021209 A 3234 GH115TA HANDLE GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA MLG SELECTOR SHORTED B VJ3R O OTHER O OTHER NR NOT REPORTED 1 WP 07 865AF 85005 LANDING GEAR HANDLE COULD NOT BE SELECTED TO THE UP POSITION AFTER PROGRESSIVE INSPECTION WAS PERFORMED ON AIRCRAFT BY M AINTENANCE. BELIEVE THAT HANDLE HAS A SHORT INTERNALLY CAUSED BY THE SHORTING OUT THE HYDRAULIC CONTROL RELAY AND THE R ELAY AND DIODES BOARD. 1 L 7 1 3O 3 O RT A49CE 1E4 2003020400122 20030204 00122 EU 2003 2 4 VJ32003F00005 1 20021204 A 7120 120A6100 SHOCK MOUNT GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA LT ENGINE DAMAGED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 861AF 544 85001 L2802348A DURING PROGRESSIVE INSPECTION OF ENGINE BAY FOUND LOWER LT MOUNT DAMAGED FROM HEAT OF EXHAUST SYSTEM. SUGGEST INSTALLIN G SOME TYPE OF HEAT SHIELDING OR CHANGING MOUNT TO A MORE HEAT RESISTANT STYLE. 1 L 7 1 3O 3 O RT A49CE 1E4 2003020400123 20030204 00123 EU 2003 2 4 VJ32003F00006 1 20021209 A 2913 MOTOR GROB 120 G120A 1660208 EU HYD PUMP FAILED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 867AF 0005 85007 DURING PROGRESSIVE INSPECTION AFTER BLOWING GEAR DOWN AND CYCLING GEAR MOTOR WINDING SMELLED AS BURNED OUT. GEAR WOULD NOT CYCLED AFTER THAT AND WOULD POP CIRCUIT BREAKER TO THE HYDRAULIC PUMP RCCB. MOTOR ACTED AS IF THE LOAD WAS TO HEAVY FOR THE MOTOR TO PRODUCE THE RECOMMENDED PRESSURE TO RETRACT GEAR. 1 L 7 1 3O RT A49CE 2003020400124 20030204 00124 EU 2003 2 4 VJ32003F00007 1 20021209 A 2913 MOTOR GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA HYD MOTOR INOPERATIVE B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 865AF 60 0001 85005 DURING PROGRESSIVE INSPECTION AND CYCLING THE GEAR THE HYDRAULIC PUMP RCCB CIRCUIT BREAKER WOULD POP. THE HYDRAULIC MOT OR ON THE HYDRAULIC PUMP UNIT WAS PUTTING OUT OVER 75 AMPS. 1 L 7 1 3O 3 O RT A49CE 1E4 2003020400125 20030204 00125 EU 2003 2 4 VJ32003F00008 1 20021209 A 2913 MOTOR GROB 120 G120A 1660208 EU HYD MOTOR FAILED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 861AF 0017 85001 DURING PROGRESSIVE INSPECTION AFTER BLOWING GEAR DOWN AND CYCLING GEAR MOTOR WINDING SMELLED AS BURNED OUT. GEAR WOULD NOT CYCLED AFTER THAT, AND WOULD POP CIRCUIT BREAKER TO THE HYD PUMP RCCB. MOTOR ACTED AS IF THE LOAD WAS TOO HEAVY FOR THE MOTOR TO PRODUCE THE RECOMMENDED PRESSURE TO RETRACT GEAR. 1 L 7 1 3O RT A49CE 2003020400126 20030204 00126 EU 2003 2 4 VJ32003F00009 1 20021209 A 2910 120A9491105AV RELAY GROB 120 G120A 1660208 EU LYC O540 AEIO540D4A5 41532 EA HYD CONTROL SHORTED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 864AF 445 85004 DURING PROGRESSIVE INSPECTION AND CYCLE OF THE LANDING GEAR, WE HAD A FAILURE OCCUR. FOUND A BAD HYD. CONTROL RELAY THA T SHORTED. BECAUSE OF THAT SHORT, IT ALLOWED TOO MUCH CURRENT TO FLOW TO PC BOARD AND SHORT OUT BOARD BETWEEN RELAY K-1 3 PIN 13 AND 16 TO BOARD PIN 6. 1 L 7 1 3O 3 O RT A49CE 1E4 2003020400127 20030204 00127 EU 2003 2 4 VJ32003F00010 1 20021209 A 2910 120A9491105AV RELAY GROB 120 G120A 1660208 EU HYD SYSTEM SHORTED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 862AF 85002 DURING PROGRESSIVE INSPECTION AND CYCLE OF THE LANDING GEAR WE HAD A FAILURE OCCUR. FOUND A BAD HYD CONTROL RELAY THAT SHORTED. BECAUSE OF THAT SHORT IT ALLOWED TOO MUCH CURRENT TO FLOW TO PC BOARD AND SHORTED OUT BOARD BETWEEN RELAY K13 PIN 13 AND 16 TO BOARD PIN 6. 1 L 7 1 3O RT A49CE 2003020400128 20030204 00128 EU 2003 2 4 VJ32003F00011 1 20021209 A 2910 RELAY GROB 120 G120A 1660208 EU HYD CONTROL SHORTED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 862AF 643 85002 DURING PROGRESSIVE INSPECTION FOUND BAD RELAY THAT CAUSED THE LANDING GEAR SYSTEM TO FAIL. BELIEVE THE CAUSE IS BECAUSE THE HYDRAULIC CONTROL RELAY SHORTED INTERNALLY. STILL TROUBLESHOOTING THE SYSTEM TO FIND WHAT CAUSED THE RELAY TO SHOR T. 1 L 7 1 3O RT A49CE 2003020400129 20030204 00129 EU 2003 2 4 VJ32003F00012 1 20021209 A 2910 RELAY GROB 120 G120A 1660208 EU HYD CONTROL SHORTED B VJ3R K NONE L NO TEST IN INSP/MAINT 1 WP 07 865AF 445 85005 DURING PROGRESSIVE INSPECTION FOUND BAD RELAY THAT CAUSED THE LANDING GEAR SYSTEM TO FAIL. BELIEVE THE CAUSE IS BECAUSE THE HYDRAULIC CONTROL RELAY SHORTED INTERNALLY. STILL TROUBLESHOOTING THE SYSTEM TO FIND WHAT CAUSE THE RELAY TO SHORT . 1 L 7 1 3O RT A49CE 2003020400130 20030204 00130 CE 2003 2 4 VJ32003F00013 1 20021212 A 3610 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO DRY AIR FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 5582X CE1353 825800R DURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT U P AND AIR PRESSURE STILL LOW AT HIGHER RPM. 1 L 7 1 3O 3 O 3A15 E5CE 2003020400131 20030204 00131 EA 2003 2 4 VJ32003F00014 2 20021127 A 7314 RG9570K1M PUMP GROB 120 G120A 1660208 EU LYC O540 AEIO540D4D5 EA FUEL SYSTEM ERRATIC B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 867AF 85007 RL2451848A DURING GROUND RUN FUEL PRESSURE READINGS WERE ERRATIC AND HIGH. FUEL PUMP SHAFT FEELS ROUGH COULD BE CAUSE TO HIGH READ INGS. NO RECOMMENDATION AT THIS TIME. 1 L 7 1 3O 3 O RT A49CE 1E4 2003020400132 20030204 00132 CE 2003 2 4 VJ32003F00015 1 20021125 A 3610 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO DRY AIR EDP FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 8251C CE1543 825822R DURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT U P AND AIR PRESSURE STILL LOW AT HIGHER RPM. 1 L 7 1 3O 3 O 3A15 E5CE 2003020400133 20030204 00133 CE 2003 2 4 VJ32003F00016 1 20021022 A 3610 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO DRY AIR FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 8101C CE1538 825785R DURING GROUND RUN UP OUTPUT OF ENGNE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. DRY AIR PUMP SHAFT SHEARED. 1 L 7 1 3O 3 O 3A15 E5CE 2003020400134 20030204 00134 CE 2003 2 4 VJ32003F00017 1 20021127 A 3610 RA216CW PUMP BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO DRY AIR FAILED B VJ3R K NONE O OTHER IN INSP/MAINT 1 WP 07 1565A 173 CE1331 825752R DURING GROUND RUN UP, OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. 1 L 7 1 3O 3 O 3A15 E5CE 2003020400140 20030204 00140 2003 2 4 W6N2003F00000 4 20021231 A 3418 S17761 STATIC PORT CESSNA 172 172S 2072439 CE LYC IO360 IO360L2A EA LT FWD FUSELAGE CONTAMINATED B W6NR O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 25 293ME 715 172S8551 L2917051A THE PILOT HAS BEEN COMPLAINING ABOUT THE VSI AND THE ALTIMETER JUMP APPROX 100-200 FEET AND THEN SETTLE DOWN. THIS ONLY HAPPENS DURING A LIGHT RAIN OR HEAVY MIST (NO ICE). WHEN HE TURNS THE ALTERNATE STATIC ON, THE PROBLEM GOES AWAY. THE STATIC PORT HAS BEEN CHANGED, THE STATIC SYSTEM HAS BEEN CHECKED OUT AND ALL ALIGNMENTS HAVE BEEN CHECKED. 1 H 7 1 3O 3 O NT 3A12 1E10 2003020400143 20030204 00143 EA 2003 2 4 WVE2003F00002 1 20021220 A 5320 601R311719 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 575ML 7256 DURING C CHECK THE INTERCOSTAL ATTACH ANGLE AT FS 484, LBL 27, WL 73.5 WAS FOUND TO BE CRACKED. (2003B0322) 2 L 7 2 4F 4 F RT A21EA E15NE 2003020400145 20030204 00145 EU 2003 2 4 Y2PA02032 1 20021220 A 2170 MY207212010 BOOT AMD FALC20 FALCOND 2720304 EU GE CF700 CF700* 30010 NE WATER SEPARATOR FAILED E Y2PA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 821AA 203 UNABLE TO MAINTAIN CABIN PRESS AT FL 290 W/O FLOOR HEAT AT MID RANGE, CABIN HEAT AT 75 PERCENT DEFLECTION AND N1 AT 93 P ERCENT RPM. COPILOTS SIDE PANEL HOT TO TOUCH. COPILOT FLOOR HEAT, HOT AND METAL PARTS UNDER COPILOTS INSTR PNL HOT TO T OUCH. SMOKE TRACES IN COCKPIT, SMELL OF MELTING PLASTIC OR RUBBER. CREW DECLARED EMERGENCY, CHECKLIST FOR EMER DESCENT AND SMOKE IN COCKPIT. A/C LANDED. FOUND WATER SEP FWD BOOT BLOWN OFF, REINSTALLED, RAN A/C AND PRES ON GROUND WITH A/C SYSTEM TO VERIFY NO SMOKE EXISTS, COPILOT PNL DO NOT BECOME HOT. AC FERRIED, UNPRESS. FWD SEP BOOT REPLACED. HEAT DUC T, COPILOT FLOOR PNL REPLACED DUE TO TEAR DAMAGE. PERFORMED OPS AND LEAK CK OF PRESS SYS. A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F A7EU E7EA 2003020400146 20030204 00146 EU 2003 2 4 YT2R107554 1 20021129 A 6420 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR LOOSE B YT2R K NONE O OTHER IN INSP/MAINT 1 WP 01 4TV 249 S6005 2936 TAIL ROTOR PITCH LINK, BEARING LOOSE. 1 G 7 1 3U 3 U H9EU E19EU 2003020400147 20030204 00147 EU 2003 2 4 YT2R110896 1 20021025 A 6410 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR CRACKED B YT2R K NONE O OTHER IN INSP/MAINT 1 WP 01 4TV 290 2936 TAIL ROTOR LAMINATE BEARING, REMOVED DUE TO CRACKED. 1 G 7 1 3U H9EU 2003020400148 20030204 00148 EU 2003 2 4 YT2R110897 1 20021029 A 6220 STARFLEX SNIAS 350 AS350BA 8680817 EU MAIN ROTOR CRACKED B YT2R K NONE O OTHER IN INSP/MAINT 1 WP 01 111FN 2060 MAIN ROTOR STARFLEX CRACKED. 1 G 7 1 3U NC H9EU 2003020400149 20030204 00149 EU 2003 2 4 YT2R110898 1 20021102 A 6420 355A09103601 BEARING SNIAS 350 AS350B1 8680811 EU TAIL ROTOR CRACKED B YT2R K NONE O OTHER IN INSP/MAINT 1 WP 01 211FN 380 2174 TAIL ROTOR LAM BEARINGS REMOVED DUE TO CRACK. 1 G 7 1 3U H9EU 2003020400150 20030204 00150 SW 2003 2 4 YT2R631375 1 20021209 A 2841 407375006101 INDICATOR BELL 407 407 1182206 SW FUEL QTY INOPERATIVE B YT2R O OTHER O OTHER NR NOT REPORTED 1 WP 01 827DS 683 53272 FUEL QUANTITY INDICATOR INOPERATIVE. 1 G 7 1 3U O H2SW 2003020400164 20030204 00164 NE 2003 2 4 PCAA0301014 2 20020113 A 7261 PW120A ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RIGHT LEAKING A PCAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 13 804EX 26727 1151 227 121082 CREW REPORTED A STRONG ODOR IN COCKPIT AND CABIN IN FLIGHT. EMERGENCY DECLARED AS A PRECAUTION. AIRCRAFT LANDED WITHOU T INCIDENT. MX RAN ENGINES WITH BLEEDS ON, NO DISCREPANCIES NOTED. NR 1 ENG WAS FOUND TO BE OVERSERVICED. OIL FROM NR 1 ENG DRAINED TO PROPER LEVEL. APU WAS SUSPECTED TO BE AT FAULT. MEL 49-1 ISSUED FOR APU. AIRCRAFT RETURNED TO SERVI CE. DURING AIRCRAFT RUN ON 13 JANUARY 2003, MAINTENANCE OPERATED APU WITH NO PROBLEMS NOTED. AFTER FURTHER TROUBLESHOO TING IT WAS DISCOVERED RT ENGINE WAS CAUSE OF OIL IN BLEED SYSTEM DUE TO INTERNAL OIL COKING. ON 10 JANUARY 2003 RT ENG AIR SWITCHING VALVE REPLACED, NO ODOR FOUND ON ENGINE RUN. RT ENG REPLACED, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2003020400201 20030204 00201 CE 2003 2 4 2003F00103 1 20021220 A 7331 CM2944218 LINE CESSNA 310 310Q 2074242 CE CONT O470 IO470V 17026 SO FUEL FLOW IND FAILED G N3BA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 01 591DM 310Q0006 FULE LEAK IN COCKPIT, PILOT DECLARED EMERGENCY AND RETURNED TO FARMINGTON, NM AIRPORT. RIGHT FUEL FLOW GAUGE INDICATIO N WENT TO ZERO. REMOVED AND REPLACED RIGHT FUEL FLOW GAUGE PRESSURE LINE P/N CM2944-2-18. 1 L 7 2 3O 3 O 3A10 3E1 2003020400247 20030204 00247 NM 2003 2 4 VNAA0212037 1 20021230 A 3250 POTENTIOMETER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING FAILED A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 424JS 3033 WHEN THE CONDITION LEVERS WERE ADVANCED FOR TAKE OFF, THE AIRCRAFT JUMPED TO THE LEFT, WHEN BROUGHT BACK, JUMPED BACK TO THE RIGHT. THE CREW THEN ABORTED TAKE OFF. MAINTENANCE INSPECTED AND ADJUSTED THE NOSE WHEEL STEERING FEED BACK POTS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2003020500006 20030205 00006 SW 2003 2 5 ALG2003F0000F 1 20021215 A 5320 206064902035 CHANNEL BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FIREWALL BROKEN E ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 58236 6408 53069 FOUND ON A DAILY INSPECTION 12/15/2002. CHANNEL HAS 12 INCHES AND 1 PIECE BROKEN OFF APPROXIMATELY 4 INCH. FABRICATE C HANNEL FROM THICKER MATERIAL. 1 G 7 1 3U 3 U O H2SW E1GL 2003020500007 20030205 00007 GL 2003 2 5 ALG2003F00001 2 20021010 A 7310 6890580 LINE BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL FUEL CONTROL LEAKING E ALGA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 60WJ 45276 CAE860696 DURING POST FLIGHT. FUEL LINE FROM THE FUEL CONTROL TO THE FIRESHIELD WAS LEAKING, THE MECHANIC REMOVED AND REPLACED TH E LEAKING LINE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003020500008 20030205 00008 SW 2003 2 5 ALG2003F00002 1 20021011 A 2822 205061635005 SWITCH BELL 206 206L1 1182107 SW ALLSN 250C 250C28 03013 GL BOOST PUMP MALFUNCTIONED A ALGA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 03 2025G 45690 45690 DURING FLIGHT. LEFT BOOST PUMP LIGHT ILLUMINATED IN FLIGHT, PILOT CHECKED AND RESET THE CIRCUIT BREAKER, GENERATOR ON T HE BOOST PUMP LIGHT STAYED ON. THE AIRCRAFT WAS DIVERTED. THE MECHANIC REMOVED AND REPLACED BOOST PUMP CARTRIDGE AND T HE SWITCH AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003020500009 20030205 00009 GL 2003 2 5 ALG2003F00003 2 20021012 A 7261 23005287 CHIP DETECTOR SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL NR 1 ENGINE DIRTY E ALGA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 03 705AL 760267 CAE890824S DURING FLIGHT, NR 1 ENGINE CHIP DETECTOR LIGHT ILLUMINATED, THE PILOT FOLLOWED CORRECTIVE ACTION IAW EMERGENCY CHECKLIST , UPON LANDING THE MECHANIC REMOVED AND CLEANED THE NR 1 ENGINE CHIP DETECTORS AND ALSO REPLACED THE NR 1 ENGINE OIL FIL TER AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2003020500010 20030205 00010 GL 2003 2 5 ALG2003F00004 2 20021216 A 7314 6899253 PUMP BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENG FUEL FAILED E ALGA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 03 35WH 502 2736 CAE836154 DURING FLIGHT, AFTER INITIAL START, THE PILOT WAITED 60 SECONDS TO TURN ON THE GENERATOR, AT THIS TIME THE ENGINE BEGAN TO FLAME OUT AND THE PILOT SHUT THE AIRCRAFT DOWN. THE MECHANIC INSPECTED THE ENTIRE FUEL SYSTEM AND FOUND IT TO BE OK. REMOVED AND REPLACED THE ENGINE DRIVEN FUEL PUMP AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 2003020500011 20030205 00011 SW 2003 2 5 ALG2003F00005 1 20021216 A 2435 23081018 STARTER GEN BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL ENGINE FAILED E ALGA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 SW 03 2618 7412 1445 45503 CAE895112 DURING FLIGHT, IN FLIGHT STARTER GENERATOR FAILED AND WOULD NOT RESET, THE PILOT FOLLOWED THE EMERGENCY CHECKLIST, UPON LANDING THE MECHANIC REMOVED AND REPLACED THE STARTER GENERATOR AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003020500012 20030205 00012 NE 2003 2 5 ALG2003F00006 1 20021216 A 3230 7625100702043 LINK SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL LT MLG OUT OF ADJUST E ALGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 03 717AL 1167 760221 760221 AFTER TAKE OFF, THE UNSAFE LIGHT WOULD NOT GO OUT AFTER THE LANDING GEAR WAS RETRACTED. UPON LANDING THE MECHANIC ADJUS TED THE LT MAIN GEAR DOOR AT EXPLOSIVE LINK AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2003020500013 20030205 00013 NE 2003 2 5 ALG2003F00009 1 20021211 A 7332 23356 PRESSURE SWITCH SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL FUEL SYSTEM FAILED E ALGA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 03 522AL 760236 DURING RUN-UP CHECK, BOTH NR 1 AND NR 2 ENGINE FUEL PRESSURE LIGHT ILLUMINATED. WHEN THROTTLES WERE ADVANCED FROM IDLE AND AIRCRAFT WAS BROUGHT TO A HOVER DURING HOVER TURN BOTH NR 1 AND NR 2 FUEL PRESSURE LIGHTS FLICKED AND STAYED ON. TH E MECHANIC REMOVED AND REPLACED BOTH NR 1 AND NR 2 FUEL PRESSURE SWITCHES AND AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2003020500014 20030205 00014 SW 2003 2 5 ALG2003F00010 1 20021012 A 2810 2060636323 FUEL CELL BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL RT FWD LEAKING E ALGA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 03 2756A 45256 DURING RUN-UP, GROUND SUPPORT DETECTED THE ODOR OF FUEL FROM THE REAR PASSENGER COMPARTMENT. THE MECHANIC REMOVED AND R EPLACED RIGHT FORWARD FUEL CELL AND AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003020500015 20030205 00015 SW 2003 2 5 ALG2003F00011 1 20021215 A 6320 MS28D341 BULB BELL 206 206L1 1182107 SW ALLSN 250C 250C28 03013 GL XMSN TEMP FAILED E ALGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 03 1084Y 10251 45433 CAE860322 12 MINUTES AFTER TAKEOFF, THE PILOT NOTICED TRANSMISSION OIL TEMP FLUCTUATING BETWEEN 60 DEGREES AND 75 DEGREES C, RETUR NED TO AIRPORT. THE MECHANIC REMOVED TRANSMISSION TEMP BULB CONNECTOR PLUG AND FOUND IT DIRTY, CLEANED THE CONNECTOR PL UG, IT DID NOT CURE THE PROBLEM, THEN REMOVED AND REPLACED THE TRANSMISSION TEMP BULB, AIRCRAFT WAS LEAK CHECKED AND RET URNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003020500016 20030205 00016 SW 2003 2 5 ALG2003F00012 1 20021215 A 7712 222375077119 TRANSDUCER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENG TORQUE MALFUNCTIONED E ALGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 03 405AL 694 53480 53480 ON TAKEOFF, PILOT NOTICED TORQUE EXCEEDED THE LIMIT WITH LOW POWER SETTINGS, HE RETURNED TO FREEPORT. THE MECHANIC CHEC K THE ECU WITH MAINTENANCE TERMINAL. NO FAULTS WERE RECORDED, CHANGED THE TORQUE TRANSDUCER AND AIRCRAFT WAS RETURNED T O SERVICE. 1 G 7 1 3U 3 U O H2SW E1GL 2003020500017 20030205 00017 SW 2003 2 5 ALG2003F00013 1 20021213 A 6320 B4678 CHIP DETECTOR BELL BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAST BEARING DIRTY E ALGA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 02 557AL 4648 A258 53243 CAE847396 SHORTLY AFTER TAKEOFF, AFTER DROPPING THE PASSENGERS ON THE SUPER TANKER, THE PILOT TOOK OFF AND WAS ENROUTE, THE TRANSM ISSION CHIP LIGHT ILLUMINATED, THE PILOT NOTIFIED VENICE BASE BY RADIO. UPON LANDING THE MECHANIC REMOVED THE MAST BEAR ING CHIP PLUG AND FOUND NO METAL, HE CLEANED THE PLUG AND CONNECTOR, PERFORMED PENALTY RUN AND LEAK CHECKED THE AIRCRAFT . NO FURTHER DEFECTS WERE NOTED, AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U O H2SW E1GL 2003020500018 20030205 00018 SW 2003 2 5 ALG2003F00014 1 20021215 A 3212 O-RING 407 BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL FLOAT BOTTLE LEAKING E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 178AL 940 AA283 52191 ON POST FLIGHT PILOT FOUND SUDDEN LEAKAGE OF FLOAT BOTTLE WITH INDICATION THAT INFLATION WOULD NOT BE POSSIBLE IF NOT RE PAIRED. THE MECHANIC REMOVED AND REPLACED THE FILL VALVE O-RING AND SERVICED. THE FLOAT BOTTLE AND AIRCRAFT WAS RETURN ED TO SERVICE. 1 G 7 1 3U 3 U NC H2SW E1GL 2003020500019 20030205 00019 NE 2003 2 5 ALG2003F00015 1 20021205 A 2910 HYDRAULIC SYSTEM SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 1 LOW E ALGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 519AL 760058 IN CRUISE FLIGHT PILOT NOTICED A KICK IN THE FLIGHT CONTROLS AND A SLIGHT FLUCTUATION IN NR 2 HYDRAULIC GAUGE THIS WAS F OLLOWED BY CHATTERING IN THE CYCLIC CONTROL, AIRCRAFT RETURNED TO BASE AND UPON INSPECTION MECHANIC DISCOVERED THE NR 1 HYDRAULIC SYSTEM WAS LOW, SERVICED THE NR 1 HYDRAULIC SYSTEM AND AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2003020500020 20030205 00020 NE 2003 2 5 ALG2003F00016 1 20021118 A 2611 327 BULB SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL SMOKE DETECTOR FAILED E ALGA K NONE L NO TEST IN INSP/MAINT 1 SW 03 705AL 760267 760267 DURING PREFLIGHT CHECK, BAGGAGE COMPARTMENT SMOKE DETECTOR WOULD NOT TEST, THE MECHANIC REPLACED THE BULB AND THE AIRCRA FT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2003020500021 20030205 00021 SW 2003 2 5 ALG2003F00017 1 20021118 A 2910 LINE BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL FUEL BOOST LOOSE E ALGA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 60WJ 45276 DURING REFUELING, FUEL LEAKING FROM THE BELLY OF THE AIRCRAFT, THE MECHANIC FOUND FUEL BOOST PUMP TRANSFER LINE IS LEAKI NG, TIGHTENED THE LINE AND LEAK CHECKED AND FOUND OK., THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003020500022 20030205 00022 SW 2003 2 5 ALG2003F00018 1 20021203 A 5200 SKIN BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL ENG BAY DOOR CORRODED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 173AL 52066 DURING DAILY INSPECTION, CORROSION IN EVERY SEAM, INTAKE SHELF MOUNTING FLANGE AND INSIDE FORMED SCOOP. 1 G 7 1 3U 3 U NC H2SW E1GL 2003020500023 20030205 00023 SW 2003 2 5 ALG2003F00019 1 20021203 A 5200 407064806101 DOOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE BAY CRACKED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 577AL 5261 53247 LT ENGINE BAY DOOR LOWER RECTANGLE SCREEN IS CRACKED AND UPPER 2ND FRONT FORWARD SQUARE SCREEN CRACKED. LT AND RT ENGIN E BAY DOORS. CHAFING OCCURRING ON LOWER AND FORWARD EDGE OF DOORS. LATCHES EXCESSIVE WEAR. FASTENERS ON FORWARD AFT E DGE HAS EXCESSIVE WEAR AROUND FASTENER HOLE. PULSING OF ROTOR WASH CAUSING STRESS ON LT DOOR. 1 G 7 1 3U 3 U O H2SW E1GL 2003020500024 20030205 00024 GL 2003 2 5 ALG2003F00020 2 20020927 A 7230 BLADE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL COMPRESSOR DAMAGED E ALGA O OTHER F E FLT CONT AFFECTED VIBRATION/BUFFET LD LANDING 1 SW 03 577AL 53247 CAE847532 WHILE HOVERING ONTO THE PARKING PAD, THE PILOT HEARD AN UNUSUAL SOUND FROM THE AIRCRAFT, UPON LANDING THE SUBSEQUENT INS PECTION REVEALED DAMAGE TO THE COMPRESSOR BLADE CAUSED BY A SMALL PIECE OF INTAKE SHELF INGESTED BY THE ENGINE. THE ENT IRE ENGINE WAS REMOVED AND REPLACED, ALSO THE INTAKE SHELF WAS REPLACED. 1 G 7 1 3U 3 U O H2SW E1GL 2003020500025 20030205 00025 GL 2003 2 5 ALG2003F00021 2 20021120 A 7321 23070611 FUEL CONTROL BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL NR 1 ENGINE FAILED E ALGA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 03 1078N 3010 1010 45389 CAE860266 DURING START, NR 1 ENGINE DID NOT EXCEED 30 PERCENT, PILOT ABORTED THE START AND USED BATTERY CART TO START THE AIRCRAFT . NO POWER FROM BATTERY CART, APU CIRCUIT BREAKER POPPED, UPON RESET THE PILOT OBSERVED A SPARK FROM THE OVERHEAD CIRCU IT BREAKER PANEL. THE MECHANIC REMOVED AND REPLACED THE FUEL CONTROL, AIRCRAFT BATTERY AND REPAIRED THE AIRCRAFT APU WI RING. THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003020500055 20030205 00055 2003 2 5 DL76L021410 4 20021205 A 2330 1303400100 ENTERTAIN SYS BOEING 767 767332 1382001 NM CABIN ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 185DN 27961 ENTERTAINMENT SYSTEM SMELLED HOT/ACRID THROUGH OUT BUSINESS CLASS. IT WAS TURNED OFF. ODOR WENT AWAY. FOUND ODOR COMI NG FROM PESC-V. REPLACED PESC-V. OPERATIONALCHECK OK. 2 L 7 2 4F RT A1NM 2003020500060 20030205 00060 NM 2003 2 5 DL76L021430 1 20021211 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 179DN 25144 DURING LAYOVER CHECK FWD SECTION OF COACH CLASS SEAT MOUNTED EMERGENCY LIGHTS INOP. M9009 POWER SUPPLY WAS THE FAULTY UN IT. REPLACEMENT OF THE POWER SUPPLY CORRECTED THE PROBLEM. 2 L 7 2 4F RT A1NM 2003020500061 20030205 00061 EU 2003 2 5 QXEA0202230 1 20021219 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 497US 11173 PDX- MID CABIN EXIT CEILING LIGHT HAS NUMEROUS BULBS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS G OOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2003020500062 20030205 00062 NE 2003 2 5 DL76L021438 2 20021214 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 SURGES A DALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 194DN 23359 28451 727738 DURING ENG. RUN-UP TO CHECK FOR A PNEUMATIC BLEED PROBLEM. NR 2 ENGINE. SURGED AT 1.16 EPR. DUE UNABLE TO FIND CAUSE OF SURGE REPLACED NR 2 ENGINE. INSTALLED 724682. 2 L 7 2 4F 4 F RT A1NM E24NE 2003020500065 20030205 00065 NM 2003 2 5 QXEA0202231 1 20021223 A 7712 30005000056 TSCU DHAV DHC8 DHC8202 2809007 NM NR 1 MALFUNCTIONED A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 365PH 9068 9068 526 PDX ON FLIGHT 2242- ABORTED TAKEOFF DUE TO AUTO FEATHER FAILED TO ARM ON DEPARTURE. REMOVED AND REPLACED NR 1 TSCU. OPE RATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003020500066 20030205 00066 NM 2003 2 5 QXEA0202232 1 20021209 A 5412 85414327 HEAT SHIELD BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - LEFT HAND AFT HEAT SHIELD AT STATION 303.0 IS CRACKED. REPAIRED IAW RD 814-54-044. 2 H 7 2 4T RT A13NM 2003020500067 20030205 00067 NM 2003 2 5 QXEA0202234 1 20021216 A 5420 85414801105 FITTING BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - LEFT HAND NACELLE FITTING OUTBOARD MACHINE FACE HAS SUSTAINED PEENING DAMAGE. REPAIRED IAW DHC-8 400 SRM 51-20-10 AND SRM 51-14-00-350-804. 2 H 7 2 4T RT A13NM 2003020500068 20030205 00068 NM 2003 2 5 QXEA0202235 1 20021206 A 1430 RIVET BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE IMPROPER A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - RIGHT HAND SIDE FUSELAGE WINDOWS BETWEEN STATIONS 449 AND 644 HAVE NUMEROUS BAD RIVETS, TOENAILS, TOO LONG, TOO SH ORT. REMOVED AND REPLACED RIVETS IAW Q400 SRM 51-41-02. 2 H 7 2 4T RT A13NM 2003020500069 20030205 00069 NM 2003 2 5 QXEA0202236 1 20021214 A 5753 FLAP BOMBDR DHC8 DHC8401 1390041 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - RIGHT HAND OUTBOARD FLAP HAS A CHAFE LINE 18LX.300X.014D BETWEEN STATIONS 242 AND 261. REPAIRED IAW DH8S-57-0683A AND HORIZON AIR EA 6-57-89A. 2 H 7 2 4T RT A13NM 2003020500070 20030205 00070 NM 2003 2 5 QXEA0202237 1 20021211 A 7110 87144117105 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - SUPPORT CHANNEL ON OUTBOARD SIDE OF LEFT LOWER COWL ASSEMBLY IS CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003020500071 20030205 00071 NM 2003 2 5 QXEA0202238 1 20021211 A 7110 87144114103 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - CHANNEL ON INBOARD SIDE OF LOWER COWL ASSEMBLY IS CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003020500072 20030205 00072 NM 2003 2 5 QXEA0202239 1 20021211 A 7110 87144120103 FRAME BOMBDR DHC8 DHC8401 1390041 NM COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - SUPPORT FRAME IN LOWER COWL ASSEMBLY IS CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003020500073 20030205 00073 NM 2003 2 5 QXEA0202240 1 20021214 A 7110 87144213101 FITTING BOMBDR DHC8 DHC8401 1390041 NM COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - CLEAT ON FORWARD END OF Z MEMBER 87144116-106 IS CRACKED. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003020500074 20030205 00074 NM 2003 2 5 QXEA0202241 1 20021210 A 5412 84414327 HEAT SHIELD BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - AFT HEAT SHIELD AFT NACELLE STATION 303.0 IS CRACKED. REPAIRED IAW RD 8/4-54-044 2 H 7 2 4T RT A13NM 2003020500075 20030205 00075 NM 2003 2 5 QXEA0202242 1 20021210 A 7110 85414389103 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - RIGHT HAND LOWER AFT COWL CHANNEL AT STATION 302.0 IS CRACKED. REPAIRED IAW Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 2003020500076 20030205 00076 NM 2003 2 5 QXEA0202243 1 20021211 A 7810 EJECTOR BOMBDR DHC8 DHC8401 1390041 NM EXHAUST CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - RIGHT HAND EXHAUST EJECTOR IS CRACKED IN FIVE PLACES. REPAIRED IAW RD 8/4-54-016. 2 H 7 2 4T RT A13NM 2003020500077 20030205 00077 NM 2003 2 5 QXEA0202244 1 20021211 A 7810 EJECTOR BOMBDR DHC8 DHC8401 1390041 NM EXHAUST CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - LEFT HAND EJECTOR IS CRACKED IN THREE PLACES. REPAIRED IAW RD 8/4-54-016. 2 H 7 2 4T RT A13NM 2003020500078 20030205 00078 NM 2003 2 5 QXEA0202245 1 20021209 A 5420 STIFFENER BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - PANELS 414AR AND 414AL HAVE CRACKED SUPPORT STIFFENERS. REMOVED AND REPLACED BRACKETS IAW DHC8-400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 2003020500079 20030205 00079 NM 2003 2 5 QXEA0202246 1 20021207 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - RIGHT HAND CENTER LEADING EDGE CLOSING RIBS ARE CRACKED IN THREE PLACES. REPAIRED IAW DHC8S EO 57-0676 AND HORIZON AIR EA 6-57-88. 2 H 7 2 4T RT A13NM 2003020500080 20030205 00080 NM 2003 2 5 QXEA0202247 1 20021209 A 5420 SUPPORT ANGLE BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - SUPPORT ANGLE UNDER LEFT HAND FINGERNAIL IS CRACKED. REPAIRED IAW DHC-8 400 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2003020500082 20030205 00082 NM 2003 2 5 QXEA0202249 1 20021219 A 5420 85414801105 FITTING BOMBDR DHC8 DHC8401 1390041 NM NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - LEFT HAND NACELLE FITTING NEEDS REPAIR. REPAIRED IAW EO DH8S-54-0697 AND HORIZON AIR EA 6-54-81. 2 H 7 2 4T RT A13NM 2003020500083 20030205 00083 NM 2003 2 5 QXEA020225 1 20021223 A 5410 STRUT DHAV DHC8 DHC8202 2809007 NM NR PYLON CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - CHAFE ON LOWER OUTBOARD SIDE STRUT ON NR 1 ENGINE AT STATION XN130.60. REPAIRED IAW RD 8-54-036. 2 H 7 2 4T RT A13NM 2003020500084 20030205 00084 NM 2003 2 5 QXEA0202253 1 20021211 A 5413 LONGERON BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - RIGHT HAND NACELLE OUTBOARD LONGERON HAS A FACTORY HOLE THAT IS OVERSIZED TO .267. REPAIRED IAW WVAC EO DH8S-54-06 84 AND HORIZON AIR EA 6-54-167. 2 H 7 2 4T RT A13NM 2003020500085 20030205 00085 NM 2003 2 5 QXEA0202256 1 20021214 A 5753 FLAP BOMBDR DHC8 DHC8401 1390041 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - LEFT HAND OUTBOARD FLAP HAS A CHAFE LINE 17LX.300WC.014D. BETWEEN STATIONS 209 AND 228. REPAIRED IAW WVAC EO DHC8S -57-0683A AND HORIZON AIR EA 6-57-89A. 2 H 7 2 4T RT A13NM 2003020500086 20030205 00086 NM 2003 2 5 QXEA0202257 1 20021217 A 7110 87144120103 FRAME BOMBDR DHC8 DHC8401 1390041 NM RT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - SUPPORT FRAME IN RIGHT LOWER COWL ASSEMBLY IS CRACKED. REPAIRED IAW WVAC WO DH8S-71-0696 AND HORIZON AIR EA 6-71-7 3. 2 H 7 2 4T RT A13NM 2003020500088 20030205 00088 NM 2003 2 5 DL76L030018 1 20020103 A 3350 POWER SUPPLY BOEING 767 767332 1382001 NM EXIT SIGN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 193DN 28450 ON L/O CHECK FOUND AISLE EXIT SIGN AT RIGHT OVERWING EXIT HATCHES INOPERATIVE. RESEAT CONNECTOR ON POWER SUPPLY MODULE M732 CHECKS OK. 2 L 7 2 4F RT A1NM 2003020500090 20030205 00090 NM 2003 2 5 KPVA200235 1 20021121 A 3350 82410164005 CIRCUIT CARD DHAV DHC8 DHC8103 1386005 NM EMERGENCY LIGHTS FAULTY A KPVA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 805WP 353 HNL - FLT 1139 - EMERGENCY LIGHTS COME ON WHEN SELECTED TO OFF POSITION AND STAY ON. ATTEMPTED TO RECYCLED SAME RESULTS . THE ONLY WAY TO TURN THEM OFF IS IN THE ARM POSITION. REMOVED AND REPLACED CIRCUIT CARD IN EMERGENCY LIGHTS CONTROL BOX IAW DHC-8 WIRING DIAGRAM MM 33-51-00 PAGE 101-102. OPS CHECK GOOD IAW DHC-8 MM 33-51-00 PAGE 201-202. (M) 2 H 7 2 4T RT A13NM 2003020500091 20030205 00091 WP 2003 2 5 MEX2002349 1 20021125 A 3230 BUNGEE CYLINDER DOUG DC9 DC932 3022066 WP NLG DEFECTIVE A ASMF A UNSCHED LANDING O OTHER CL CLIMB 1 SW 23 1003P 48150 MEX-CUU - AIRCRAFT RETURNED AFTER TAKEOFF, DUE TO PROBLEMS WITH NOSE GEAR. THE NOSE LANDING GEAR REMAINED EXTENDED PROC EDURE WAS ACCOMPLISHED AND PHYSICALLY CHECKED, NOSE GEAR REMAINED DOWN AGAIN. IN APPROXIMATION, CAPTAIN INFORMED THE NO SE GEAR RETRACTED UPON REDUCING THE SPEED, THE LANDING IS EFFECTED WITH 102,00 LBS. TECHNICAL PERSONNEL WERE ADJUSTED N OSE LANDING GEAR FORWARD DOORS, BUNGEE CYLINDER WAS REPLACED, STRUT CYLINDER SERVICE WAS PERFORMED, TIRE NOSE GEAR BOTH WERE CHANGED AND EXTENSION RETRACTION TEST WAS PERFORMED IAW MM 32-30-0 AND INSPECTION BY OVERWEIGHT LANDING WAS ACCOMPL ISHED IAW MM 05-51-0. ALL CORRECT TO RETURN TO SERVICE. (M) 2 L 7 2 4F A6WE 2003020500092 20030205 00092 NM 2003 2 5 MEX2002350 1 20021126 A 2150 A/C PACK DOUG MD88 MD88 3023688 NM A/C BAY MALFUNCTIONED A ASMF A UNSCHED LANDING O OTHER CL CLIMB 1 SW 23 161PL 49764 FLT 137 - TIJ-AGU - AIRCRAFT RETURNED TO PLATFORM AFTER TAKEOFF, DUE TO FAIL OF PACKAGE OF A/A LEFT. AT PLATFORM, MAINT ENANCE CHECKED FOR LEAKS AND GENERAL CONDITION. VERIFIED PACKAGE OF A/A AND VALVE OF CONTROL OF FLOW IAW MM 21-31, OPER ATING CORRECT. (M) 2 L 7 2 4F RT A6WE 2003020500093 20030205 00093 NM 2003 2 5 TSAA0253115 1 20020404 A 5310 654578832 WINDOW FRAME BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 PERFORMED WINDOW CORNER FASTENERS HOLE INSPECTION PER S/B 737-53A1177R6 AND DISCOVERED DEFECTS IN WINDOW CORNERS WITH CR ACK INDICATION AT BS 787 RIGHT WINDOW UPPER AFT CORNER USING HFEC METHODS. TRIMMED OUT THE THREE HOLES IN THE DAMAGED A REA. HFEC THE EDGE OF THE TRIM. FABRICATED A DOUBLER AND A TRIPPER THICK AND FILLER AS SHOWN IN FIGURE 1 DEVIATION P/U . INSTALLED REPAIR PARTS. RECEIPT OF 8110-3 FROM BOEING. REPAIR COMPLETED IAW ECO 3250 AND DEVIATION P/U. AIRCRAFT R ETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003020500094 20030205 00094 NM 2003 2 5 TSAA0253231 1 20021027 A 5753 6545410 FITTING BOEING 737 737282 13844AT NM T/E FLAP DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 REMOVED DAMAGE FROM THE NR 2 AND NR 7 FLAP TRACK ATTACHMENT FITTING HOLE. FABRICATED A 'NEW' REPLACEMENT TUBE AND BUSHI NG INCREASING THE OUTSIDE DIAMETER .0015 TO .0020 INCH INTERFERENCE FIT ON THE FINISHED DIAMETER OF THE HOLE. INSTALLED NEW TUBE AND BUSHING. 8110-3 RECEIVED. REPAIR COMPLETED IAW BOEING DRAWING 65-46429 INSTRUCTIONS AND ECO 3308. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003020500095 20030205 00095 NM 2003 2 5 TSAA0253232 1 20021027 A 5320 6562584 STRUCTURE BOEING 737 737282 13844AT NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 TRIMMED OUT THE DAMAGE OF THE HOLES TO A RECTANGULAR SHAPE. VERIFIED CRACK REMOVED USING HFEC. FABRICATED CIRCULAR DOU BLERS FOR EACH HOLE. REPAIR COMPLETED IAW ECO 3302. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003020500096 20030205 00096 NM 2003 2 5 TSAA0253233 1 20021018 A 5320 6546554 STRUCTURE BOEING 737 737282 13844AT NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 TRIM OUT ALL THREE HOLES IN THE DAMAGED ZONE. HFEC THE EDGE OF THE TRIM. FABRICATED A DOUBLER AND A TRIPLER. INSTALLE D DOUBLER AND TRIPLER. REPAIR COMPLETED IAW ECO 3250, FIGURE 24. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003020500097 20030205 00097 NM 2003 2 5 TSAA0253234 1 20021018 A 5514 6573781501 STRUCTURE BOEING 737 737282 13844AT NM HORIZ STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 BLENDED THE DAMAGE ON THE LUG. SPOTFACED THE INBOARD AND OUTBOARD SURFACES. OVERSIZED THE TAPERED/ELONGATED HOLE OF TH E INBOARD LUG ON THE ORIGINAL CENTERLINE TO OBTAIN A ROUND AND TRUE CONDITION. FABRICATED NEW REPAIR SLEEVE BUSHING TO FIT THE OVERSIZED INBOARD LUG BORE. FABRICATED TWO FINISHED WASHERS FOR EACH SIDE OF LUG SPOT FACED BONDED TO SPOTFACED SURFACE. COMPLETED FINAL INSIDE DIAMETER REAM OF THE REPAIR BUSHING PER DRAWING REQUIREMENTS. VERIFIED 8110-3 RECEIVE D. REPAIR COMPLETED IAW ECO 3305. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003020500098 20030205 00098 NM 2003 2 5 TSAA0253235 1 20021027 A 5743 658276416 BEAM BOEING 737 737282 13844AT NM RT WING DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 OVERSIZED 4 HOLES IN THE RIGHT MLG LOWER BEAM CHORD FLANGE. FABRICATED FOUR FREEZE PLUGS. FABRICATED FOUR 1 INCH DIAME TER RETAINING WASHERS. INSTALLED FREEZE PLUGS AND OPENED ID HOLES TO THE EXISTING .1875 INCH DIAMETER PANEL ATTACH BOLT S. INSTALLED RETAINING WASHERS UNDER THE NUT AND USED A LONGER BOLT TO THE RETAINING WASHER. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 3307. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003020500099 20030205 00099 NM 2003 2 5 TSAA0253238 1 20021107 A 5711 6545499 SPAR BOEING 737 737209 13844AE NM LT WING CORRODED A K NONE O OTHER IN INSP/MAINT 1 WP 13 827AL 23913 FOUND CORROSION ON RIGHT FRONT SPAR LOWER CHORD VERTICAL WEB SURFACE AT WSL 554. CONFIRMED COMPLETE REMOVAL OF CORROSIO N WITH HFEC INSPECTION. FABRICATED TAPERED FILLERS TO FIT IN THE BLENDOUT AREA. FABRICATED A REPAIR DOUBLER AND REPAIR ANGLE. INSTALLED THE REPAIR FILLERS, ANGLE AND DOUBLER. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003020500100 20030205 00100 NM 2003 2 5 USAABB02207 1 20021221 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 631AU 27809 BDL - FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2003020500101 20030205 00101 NM 2003 2 5 USAABB02210 1 20021225 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 618AU 22210 CLT - FOUND THE EMERGENCY ESCAPE PATH AISLE LIGHTS AT SEAT ROWS 4, 9, 13, 18, 23, 26, 29 AND 33 INOPERATIVE. MAINTENANC E REPLACED THE BATTERIES AT ALL 10 LOCATIONS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2003020500102 20030205 00102 NM 2003 2 5 USAABB02211 1 20021227 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 630AU 27808 BDL - FOUND LOW LEVEL EMERGENCY LIGHT AT ROW 18R INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. OPERATIONAL CHECK GOOD . (M) 2 L 7 2 4F RT A2NM 2003020500106 20030205 00106 EU 2003 2 5 USAASA02111 1 20021216 A 2560 GIRT BAR AIRBUS A319 A319112 3930323 EU ENTRY DOOR OUT OF POSITION A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 715UW 1051 MSP - FLT 807 - MSP-CLT - PRIOR TO PUSHBACK, THE LEFT ENTRY DOOR WOULD NOT SHOW CLOSED ON ECAM WITH THE SLIDE SHOWING AR MED. UPON INSPECTION, THE GIRT BAR WAS FOUND HANGING BELOW THE DOOR. MAINTENANCE REINSTALLED THE GIRT BAR. OK FOR SER VICE. (M) 2 L 7 2 4F RT A28NM 2003020500107 20030205 00107 EU 2003 2 5 USAASA02112 1 20021216 A 2560 GIRT BAR AIRBUS A319 A319112 3930323 EU PAX DOOR OUT OF POSITION A USAA K NONE O OTHER CL CLIMB 1 EA 19 715UW 1051 CLT - FLT 807 - EN ROUTE MSP-CLT, AFTER TAKEOFF, A LOUD AIR LEAK WAS FOUND TO BE COMING FROM THE FORWARD LEFT DOOR. THE FLIGHT CONTINUED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REINSTALLED THE GIRT BAR. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2003020500108 20030205 00108 EU 2003 2 5 USAASA02117 1 20021231 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 0936 PHL - THE EMERGENCY LIGHTS FLASH ON AND OFF. MAINTENANCE REPLACED A BATTERY PACK AND THE 'A' CHANNEL AND 'B' CHANNEL DE CODER/ENCODER UNITS, AND PERFORMED A CABIN INTERCOMMUNICATION DATE SYSTEM RESET FOR TROUBLESHOOTING. MAINTENANCE REPLAC ED AN EMERGENCY POWER SUPPLY UNIT TO FIX THE PROBLEM. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2003020500109 20030205 00109 2003 2 5 USAASB02211 4 20021126 A 3400 G6773 CONTROL PANEL BOEING 737 737301 1384611 NM COCKPIT FAULTY A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 342US 38810 23511 ALB - FLT 342 - ON APPROACH TO ALB, FROM PHL, CREW REPORTED A BURNING SMELL IN THE COCKPIT. THE NR 1 NAV INDICATIONS AL L FLAGGED AND THE NR 1 NAV CIRCUIT BREAKER POPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REP LACED THE NR 1 NAV CONTROL PANEL. RESET CIRCUIT BREAKER. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003020500110 20030205 00110 NM 2003 2 5 USAASB02212 1 20021127 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 589US 23934 IND - MAINTENANCE FOUND THE EMERGENCY EXIT IDENTIFIER LIGHTS FOR THE LEFT OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003020500111 20030205 00111 NM 2003 2 5 USAASB02220 1 20021211 A 3397 WIRE BOEING 737 7374B7 1384702 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 427US 24549 ORD - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ON SEAT 22, LEFT SIDE, INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE O N EMERGENCY LIGHT FOR SEAT 22, LEFT SIDE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003020500112 20030205 00112 2003 2 5 USAASB02221 4 20021212 A 3425 7725005009 INDICATOR BOEING 737 7373B7 1384580 NM COCKPIT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 EA 19 523AU 34229 23858 CAE - FLT 489 - ON DESCENT INTO CLT FROM ATL, THE ATTITUDE FLAG IN THE CAPTAIN'S ADI CAME IN TO VIEW. FLIGHT DIVERTED T O CAE AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S A DI. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003020500113 20030205 00113 NM 2003 2 5 USAASB02222 1 20021216 A 3350 20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 409US 23879 PHL - MAINTENANCE FOUND THE AFT EMERGENCY LIGHTS INOPERATIVE/WON'T TEST. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT AND RIGHT EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003020500114 20030205 00114 NM 2003 2 5 USAASB02223 1 20021217 A 3350 CONNECTOR BOEING 737 7373B7 1384580 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 518AU 23704 IND - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT SEAT 10, LEFT SIDE, INOPERATIVE. MAINTENANCE RECONNECTED THE PLUG U NDER SEAT FRAME AT SEAT 10, LEFT SIDE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003020500115 20030205 00115 NM 2003 2 5 USAASB02224 1 20021217 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 779AU 24996 PHL - MAINTENANCE FOUND THE AISLE EMERGENCY LIGHT AT SEAT ROW 10ABC AND THE SEAT MOUNTED EXIT SIGN AT SEAT ROW 11ABC INO PERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AT STATION 634. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003020500116 20030205 00116 NM 2003 2 5 USAASB02225 1 20021218 A 3350 CONNECTOR BOEING 737 7374B7 1384702 NM CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 785AU 25024 GSO - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS AT SEAT 12, LEFT SIDE, INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECT OR AT SEAT 12, LEFT SIDE. RECONNECTED CONNECTOR. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2003020500117 20030205 00117 2003 2 5 USAASB02226 4 20021222 A 2565 D31591478 SLIDE BOEING 737 7373B7 1384580 NM SERVICE DOOR TWISTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 PIT - DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE TWISTED TO THE RIGHT WHI LE INFLATING. MAINTENANCE WAS UNABLE TO REPOSITION SLIDE TO NORMAL POSITION UNTIL AFTER PARTIAL DEFLATION. SLIDE WAS U NUSABLE IF IN AN EMERGENCY SITUATION. SLIDE OPERATIONAL CHECK FAILED. MAINTENANCE REMOVED AND REPLACED THE FORWARD RIG HT SERVICE DOOR ESCAPE SLIDE ASSEMBLY. TWO ADDITIONAL OPERATIONAL CHECKS ARE SCHEDULED TO BE PERFORMED AT THE FORWARD R IGHT SERVICE DOOR POSITION PER US AIRWAYS POLICY AND PROCEDURES. (M) 2 L 7 2 4F RT A16WE 2003020500118 20030205 00118 NM 2003 2 5 USAASB02227 1 20021222 A 3260 189929 SAFETY SWITCH BOEING 737 7374B7 1384702 NM RT MLG WW FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 433US 24555 PIT - FLT 1022 - ON CLIMB-OUT FROM PIT, EN ROUTE TO EWR, CAPTAIN REPORTED THE MLG GEAR WOULD NOT RETRACT. CAPTAIN ACCOM PLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND VERIFIED THE MAIN GEAR WAS DOWN AND LOCKED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE S106 AIR SAF ETY SENSOR AT THE GROUND SPOILER BYPASS VALVE IN THE RIGHT MLG WHEEL WELL. SWUNG GEAR. OPERATIONAL CHECK AND INDICATIO N CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003020500119 20030205 00119 NM 2003 2 5 USAASB02233 1 20021225 A 3230 LANDING GEAR BOEING 737 7374B7 1384702 NM NLG & MLG MALFUNCTIONED A USAA O OTHER O OTHER AP APPROACH 1 EA 19 449US 24893 PHL - FLT 362 - TOWER IN PHL INSTRUCTED CREW TO ACCOMPLISH A GO-AROUND DUE TO AN AIRCRAFT ON THE RUNWAY. WHILE ACCOMPLI SHING GO-AROUND, CREW RAISED THE GEAR AND ALL GEAR INDICATION LIGHTS WERE OUT. WHEN THE GEAR HANDLE WAS SELECTED TO OFF , THE GEAR STARTED TO LOWER WITH BOTH RED AND GREEN LIGHTS ILLUMINATING. GEAR WAS THEN SELECTED DOWN AND THE RED LIGHTS EXTINGUISHED AND THE GREEN LIGHTS ILLUMINATED. GEAR HANDLE WAS NOT MOVED FROM THIS POSITION AS THE FLIGHT LANDED WITHO UT FURTHER INCIDENT. MAINTENANCE JACKED AIRCRAFT AND CYCLED LANDING GEAR SEVERAL TIMES. EXTENSION AND RETRACTION OF GEA R OPERATIONALLY CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 2003020500120 20030205 00120 NM 2003 2 5 USAASB02234 1 20021226 A 2424 948F4581 GCU BOEING 737 7374B7 1384702 NM NR 2 FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 19 426US 41456 24548 PHL - MAINTENANCE REPORTED AN ELECTRICAL ODOR AND SMOKE IN THE COCKPIT WHILE TAXIING AIRCRAFT TO THE GATE. MAINTENANCE TROUBLESHOT THE PROBLEM TO THE NR 2 GENERATOR CONTROL UNIT (GCU). REMOVED AND REPLACED THE NR 2 GCU. RAN ENGINES. ALL SYSTEMS CHECK GOOD. NO ELECTRICAL ODOR OR SMOKE NOTED. (M) 2 L 7 2 4F RT A16WE 2003020500121 20030205 00121 NM 2003 2 5 USAASB02235 1 20021226 A 2120 SMOKE BOEING 737 7373B7 1384580 NM CABIN DETECTED A USAA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LD LANDING 1 EA 19 527AU 23862 AVP - FLT 9280 - UPON LANDING AND APPLYING REVERSE THRUST, CAPTAIN WAS ADVISED THE AFT CABIN AREA FILLED WITH SMOKE (LES S THAN 10 FEET VISIBILITY) AND THE REAR LAVATORY SMOKE DETECTOR WAS SOUNDING. SMOKE DISSIPATED AFTER COMING OUT OF REVE RSE THRUST AND SHUTTING OFF AIR CONDITIONING PACKS. AIRCRAFT TAXIED TO THE GATE ON ITS OWN POWER. MAINTENANCE INSPECTE D INTAKE AND EXHAUST OF BOTH ENGINES. RAN BOTH PACKS USING RESPECTIVE ENGINE BLEEDS. OPERATED THRUST REVERSERS WITH PA CKS RUNNING. NO EVIDENCE OF SMOKE OR SMELL IN THE CABIN OR COCKPIT. SUSPECT UREA INGESTION DURING LANDING USED FOR RUN WAY DEICING. (M) 2 L 7 2 4F RT A16WE 2003020500122 20030205 00122 WP 2003 2 5 ZIAA02001 1 20021108 A 5230 PAN DOUG DC9 DC915F 3022037 WP CARGO DOOR CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 195US 47017 RECEIVED CRACK INDICATION OF .75 INCH WHILE CONDUCTING EDDY CURRENT INSPECTION OF AFT LOWER CARGO DOOR, OUTER PAN RADIUS AFT SIDE AT BEAM 5. (M) 2 L 7 2 4F A6WE 2003020500123 20030205 00123 WP 2003 2 5 ZIAA02002 1 20021108 A 5230 PAN DOUG DC9 DC915F 3022037 WP CARGO DOOR CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 195US 47017 WHILE CONDUCTING EDDY CURRENT INSPECTION ON FORWARD LOWER CARGO DOOR, RECEIVED CRACK INDICATION OF .75 INCH IN OUTER PAN RADIUS LOWER AFT STOP. (M) 2 L 7 2 4F A6WE 2003020500124 20030205 00124 WP 2003 2 5 ZIAA02003 1 20021108 A 5230 DOUBLER DOUG DC9 DC915F 3022037 WP CARGO DOOR CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 195US 47017 WHILE CONDUCTING EDDY CURRENT INSPECTION ON FORWARD LOWER CARGO DOOR, OBSERVED CRACK INDICATION IN REPAIR DOUBLER AT FOR WARD SIDE NR 1 BEAM OUTER PAN OF FORWARD LOWER CARGO DOOR EMANATING FROM STEEL HI-LOCK FASTENER HOLE. (M) 2 L 7 2 4F A6WE 2003020500125 20030205 00125 WP 2003 2 5 ZIAA02004 1 20021108 A 5230 DOUBLER DOUG DC9 DC915F 3022037 WP CARGO DOOR CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 195US 47017 WHILE CONDUCTING EDDY CURRENT INSPECTION ON FORWARD LOWER CARGO DOOR, OBSERVED CRACK INDICATION IN REPAIR DOUBLER AT FOR WARD SIDE NR 4 BEAM OUTER PAN OF FORWARD LOWER CARGO DOOR. (M) 2 L 7 2 4F A6WE 2003020500126 20030205 00126 NM 2003 2 5 QXEA0202258 1 20021207 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - LEFT HAND CENTER WING LEADING EDGE HAS CRACKS AT ENDS OF CLOSING RIBS IN FOUR PLACES. REPAIRED IAW WVAC EO DH8S-5 7-0676 AND HORIZON AIR EA 6-57-88. 2 H 7 2 4T RT A13NM 2003020500127 20030205 00127 NM 2003 2 5 QXEA0202259 1 20021212 A 5420 WEB BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 CKB - LEFT NACELLE INBOARD SIDE OF SHEAR DECK HAS A CRACKED HOLE. REPAIRED IAW WVAC EO DH8S-54-0690 AND HORIZON AIR EA 6-54-170. 2 H 7 2 4T RT A13NM 2003020500128 20030205 00128 EA 2003 2 5 QXEA0202260 1 20021222 A 2820 D98C07606 SENSOR CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 607QX 255 255 10024 SEA ON FLIGHT 2460- RETURNED TO GATE DUE TO LEFT FUEL LOW PRESSURE CAUTION MESSAGE DURING PUSHBACK. REMOVED AND REPLACE D LEFT HAND ENGINE INLET PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020500129 20030205 00129 NM 2003 2 5 QXEA0202261 1 20021223 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - FRETTING CORROSION ON BOTTOM SIDE OF LOWER SPAR CAP, RIGHT HAND WING APPROXIMATELY YW57.0R. REPAIRED IAW RD 8-57- 811, PAGE 4 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2003020500132 20030205 00132 NM 2003 2 5 QXEA0202262 1 20021223 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 360PH 1694 1694 515 BOI ON FLIGHT 2201- SMOKE WARNING CAME ON INTERMITTENTLY DURING FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FORWARD SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003020500134 20030205 00134 NM 2003 2 5 QXEA0202264 1 20021224 A 5230 SEAL BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR BLOWN A QXEA O OTHER O OTHER AP APPROACH 1 NM 09 409QX 4051 SEA ON FLIGHT 2384- AIRCRAFT DEPRESSURIZED AT 1500 FEET ON APPROACH. FLIGHT ATTENDANT REPORTED A LOUD POP FOLLOWED BY A WHISTLING SOUND FROM AFT AREA OF AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND AFT CARGO DOOR SEAL BLOWN AND TORN . REMOVED AND REPLACED DOOR SEAL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003020500135 20030205 00135 NM 2003 2 5 QXEA0202265 1 20021223 A 7603 POWER LEVER BOMBDR DHC8 DHC8401 1390041 NM COCKPIT OUT OF TRIM A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 410QX 4053 SEA ON FLIGHT 2374- RETURNED TO FIELD DUE TO: WHEN POWER LEVERS ADVANCED INTO TAKEOFF DETENT, TORQUE INDICATOR NEEDLES P OINTED ONE NEEDLE WIDTH ABOVE TARGET TORQUE BUG. HAD NOT EXCEEDED DETENT AND NO RED NEEDLES. AIRCRAFT LANDED WITHOUT I NCIDENT. INSPECTED AND FOUND POWER LEVER OUT OF TRIM. TRIMMED POWER LEVERS. NO PARTS REPLACED. OPERATIONAL CHECKS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003020500136 20030205 00136 EA 2003 2 5 QXEA0202266 1 20021223 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM MALFUNCTIONED A QXEA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 09 613QX 223 10045 FAT-ON FLIGHT NUMBER 2478. LEFT FUEL LOW PRESSURE CAUTION. REMOVED AND REPLACED NR 1 ENGINE INLET PRESSURE SENSOR. RA N ENGINES, NO LEAKS NOTED. NO CAUTION MESSAGES APPEARED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020600001 20030206 00001 NE 2003 2 6 DL76P021075 2 20020913 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 STALLED A DALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 1402A 32973 25989 724687 BETWEEN 100 AND 200 AGL THE RT ENGINE BEGAN TO COMPRESSOR STALL. MAX EGT710. THROTTLE RETARDED AND ENGINE INDICATIONS R ETURNED TO NORMAL. REPLACED NR 2 ENGINE 2 L 7 2 4F 4 F RT A1NM E24NE 2003020600002 20030206 00002 NM 2003 2 6 DL76P021416 1 20021205 A 2120 ODOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE CABIN DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 144DA 27584 724715 AFTER TAKE OFF, FLT ATTENDANT REPORTED STRANGE FUMES & ODOR IN MIDSECTION GALLEY AREA. LT ENGINE BLEED AND PACK TURNED O FF AND ODOR SUBSIDED & DISSIPATED. BLEED AND PACK LT OFF. REMAINDER OF FLT UNEVENTFUL. INSPECTED INLET EXHAUST - NO V ISIBLE OIL - PERF PNEUMATIC CHECK PER 21-00-21 NO VISIBLE SMOKE IDLE POWER. RAN LT PACK LT ENGINE BLEED ONLY IDLE - NO SMOKE / ODOR. NEEDS HP CHECK. 985989 - RAN ENGINE AT HIGH POWER SETTING FOR 5 MINUTES WITH LT BL PACK ON - NO UNUS AL ODORS OR SMOKE. LT PNEUMATIC PACK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2003020600004 20030206 00004 NM 2003 2 6 DL76S021038 1 20020905 A 4990 APU BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE APU BAY LEAKING A DALA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 121DE 52308 23435 580125 AT TOP OF CLIMB AND CRUISE AT 410 HOT PACK ODOR IN COCKPIT NO LIGHTS OR WARNINGS. NO REPORTED ODOR FROM THE CABIN. F/A' S LATER REPORTED HAZE AND LAV SMOKE DETECTOR ALARMS. TURNED RT PACK OFF, SMOKE SEEMED TO ABATE. REMOVED RT PACK BYPASS VALVE AND DUCT HAS OIL . CONTINUED INSPECTION RT ENGINE HIGH PRESSURE DUCT AND LOW PRESSURE DUCT. NO CONTAMINATION NOT ED. FOUND OIL LEAKING IN APU BLEED AT APU. APU CHANGE PER TRANS 1T101(453486) PERFORMED DUCT BURNOUT PER MM. 2 L 7 2 4F 4 F RT A1NM E13NE 2003020600005 20030206 00005 2003 2 6 DL76S021064 4 20020911 A 2565 LIGHT BOEING 767 767332 1382001 NM ESCAPE SLIDE INOPERATIVE A DALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 136DL 23146 2L DOOR SLIDE LIGHT INOPERATIVE, RELAMPED - OPS NORMAL. 2 L 7 2 4F RT A1NM 2003020600006 20030206 00006 NM 2003 2 6 DL76S021130 1 20020923 A 5411 311T11115 SPAR BOEING 767 767332 1382001 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 137DL 25306 PYLON NR 1 ENGINE FWD UPPER SPAR WEB CRACKED, REPAIRED THE FWD UPPER SPAR WEB. THE CUTOUT SIZE WAS ENLARGER TO REMOVE THE CRACK AND EXISING NUTPLATE LOCATIONS AT THE CUTOUT CORNERS. THE AREA WAS MODIFIED PER THE REQUIREMENTS OF BAC S/B 7 67-54-0090 AND DOCUMENTED PER ER/A 383905-14. 2 L 7 2 4F RT A1NM 2003020600007 20030206 00007 NM 2003 2 6 DL76S021138 1 20020925 A 3350 BPS73 CHARGER BOEING 767 767332 1382001 NM EMERGENCY LIGHT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 136DL 23146 LOWER EMERGENCY LIGHTS AT FWD LT AND RT DOORS EXIT SIGNS INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK OPS CK GOOD 2 L 7 2 4F RT A1NM 2003020600008 20030206 00008 NM 2003 2 6 DL76S021163 1 20021003 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 139DL 25984 R1 EMERGANCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY. AND POWER SUPPLY. 2 L 7 2 4F RT A1NM 2003020600009 20030206 00009 NM 2003 2 6 DL76S021263 1 20021029 A 3350 20131A BATTERY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 118DL 2 23277 DURING S/C FOUND AFT RIGHT OVERHEAD EMERGENCY LIGHTS INOPERATIVE BY ROW 44E. R & R BATTERY ASSY, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2003020600010 20030206 00010 NM 2003 2 6 DL76S021306 1 20021110 A 4900 ACTUATOR 7321387010 BOEING 767 767332 1382001 NM APU DOOR BINDING A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 134DL 1072T2 25123 ELECTRICAL ODOR IN AFT CABIN REPORTED BY FLIGHT ATTENDANTS AFTER PUSHBACK AND ENGINE START. FOUND APU ACTUATOR STUCK OP EN WITH ELECTRICAL ODOR. R & R APU DOOR ACTUATOR. OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2003020600011 20030206 00011 NM 2003 2 6 DL76S021382 1 20021122 A 3233 MOUNT BOEING 767 767332 1382001 NM NLG ACTUATOR BENT A DALA O OTHER D INFLIGHT SEPARATION LD LANDING 1 SO 27 131DN 24852 ON L/O FOUND RT LOCK SPRING MISSING ON NOSE LANDING GEAR. FWD SPRING MOUNT IS BROKEN. AFT SPRING MOUNT IS BENT. REPLACE D FWD AND MOUNT AND SPRING PER M/M 32-21-09. DAMAGED ALSO TO AFT BULKHEAD OF NOSE WHEEL WELL REF ITEM 003 2 L 7 2 4F RT A1NM 2003020600012 20030206 00012 NM 2003 2 6 DL76S021404 1 20021203 A 2750 CONTROLLER BOEING 767 767332 1382001 NM TE FLAPS MALFUNCTIONED A DALA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SO 27 137DL 25306 ON APPROACH IN ATL, FLAPS WOULD NOT EXTEND PAST 25 WITH 30 SELECTED. FLAPS WOULD NOT RETRACT ON GO AROUND. LANDED WITH FLAPS AT 20 PER NON-NORMAL PROCEDURE. BITE OF FSEU PER FIM HAD NO FAULTS, RAN AND INSPECTED FLAPS SEVERAL CYCLES WITH NO STATUS MESSAGES OR FAULTS. 2 L 7 2 4F RT A1NM 2003020600013 20030206 00013 NM 2003 2 6 DL76S021421 1 20021208 A 3350 LIGHT BOEING 767 767332 1382001 NM RT FUSELAGE INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 139DL 25984 EMERGENCY LIGHT INOPERATIVE ON RT SIDE AFT OF FLAPS. REPLACED SOCKET OPS CK GOOD. 2 L 7 2 4F RT A1NM 2003020600014 20030206 00014 NM 2003 2 6 DL76S021424 1 20021210 A 7830 THRUST REVERSER BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENGINE MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 132DN 52182 24981 580151 RT THRUST REVERSER YELLOW LIGHT CAME ON ON TAKEOFF WITH NO THRUST REVERSER SELECTED. ABORTED T/O AT 90KTS. FWD MCO/P LAC PER MEL 78-36-01. RT THRUST REVERSER LOCKED OUT 2 L 7 2 4F 4 F RT A1NM E13NE 2003020600017 20030206 00017 NE 2003 2 6 DL777021050 2 20020906 A 7200 ENGINE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 1 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 865DA 11521 29737 051200 BOTH ENGINES CHANGED DUE TO FAILED BOROSCOPE. DUST CAP INSPECTED 2 L 7 2 4F 4 F RT T00001SE E00050EN 2003020600018 20030206 00018 NE 2003 2 6 DL777021119 2 20020919 A 7230 COMPRESSOR BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 2 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 864DA 10878 29736 51194 BOROSCOPE OF NR 2 ENGINE. FOUND 6TH STAGE HIGH PRESSURE COMPRESSOR DAMAGE BEYOND LIMITS. REPLACED ENGINE 2 L 7 2 4F 4 F RT T00001SE E00050EN 2003020600019 20030206 00019 NM 2003 2 6 DL777021310 1 20021111 A 2913 731966 PUMP BOEING 777 777232 1385232 NM HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 27 866DA 29738 "C" SYSTEM HYDRAULIC QUANTITY LEVEL DECREASED IN FLIGHT. EMERGENCY LANDING DECLARED TO AIRPORT. AIRCRAFT LANDED WITHOUT INCIDENT.AIRCRAFT TOWED TO GATE. FOUND C2 ELECTRIC HYDRAULIC PUMP LEAKING. PUMP REPLACED. 2 L 7 2 4F RT T00001SE 2003020600020 20030206 00020 NE 2003 2 6 DL777021313 2 20021112 A 7261 FK26889 LINE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 2 ENGINE LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 865DA 29737 051004 OIL QUANTITY RT ENGINE DROPPED TO 1 DURING FLIGHT, ALL OTHER INDICATIONS WERE NORMAL. REPLACED OIL BEARING SUPPLY LINE. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2003020600021 20030206 00021 NM 2003 2 6 DL777021380 1 20021126 A 3150 WARNING SYSTEM BOEING 777 777232 1385232 NM SPEED BRAKES ACTIVATED A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 866DA 29738 AT APPLICATION OF TAKE OFF POWER CREW RECEIVED CONFIGURATION SPEEDBRAKE EICAS WARNING AND ASSOCIATED AURAL WARNING CREW DISCONNECTED T/O BELOW 5 KTS. PERFORMED MAT TEST ON WARNING ELECTRONICS SYSTEM AND SPEED BRAKE TEST. NO DEFECTS NOTED NO MESSAGES OR FAULTS AT THIS TIME. 2 L 7 2 4F RT T00001SE 2003020600022 20030206 00022 NM 2003 2 6 DL777021477 1 20021227 A 3350 D71702001 POWER SUPPLY BOEING 777 777232 1385232 NM 2L GALLEY FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 862DA 29734 MID GALLEY EMERGENCY LIGHTS CYCLE ON/OFF WITH FLT DECK IN THE OFF POSITION FOUND POWER SUPPLY M33099 AT FAULT. REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4F RT T00001SE 2003020600023 20030206 00023 NM 2003 2 6 DL78K021074 1 20020913 A 5610 BOLT BOEING 737 737832 13844CF NM COCKPIT WINDOW LOOSE A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 3731T 00084H3651 30775 CREW LOCKED THEMSELVES OUT OF COCKPIT EQUIPPED WITH SECURITY DOOR. F/O SLIDING WINDOW FAILED TO OPEN FROM OUTSIDE, REM OVED F/O WINDOW AND FOUND LOWER BEARING BOLT BACKED OUT PREVENTING EMERGENCY HANDLE FROM OPERATING PROPERLY. TIGHTENED SAME. 2 L 7 2 4F RT A16WE 2003020600024 20030206 00024 NM 2003 2 6 DL78K021077 1 20020913 A 3350 BULB BOEING 737 737832 13844CF NM EMERGENCY LIGHT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3736C 30540 EMERGENCY EXIT LIGHT AT R-2 DOOR HAS 2 OF 4 BULBS INOPERATIVE. REPLACED EMERGENCY EXIT ASSY. CHECKS GOOD. 2 L 7 2 4F RT A16WE 2003020600025 20030206 00025 NM 2003 2 6 DL78K021258 1 20021028 A 3350 1317 BULB BOEING 737 737823 13844BZ NM LT AFT OVRWG EXI BURNED OUT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3730B 30538 LT AFT OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. RELMAPED SAME. OPS CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2003020600026 20030206 00026 NM 2003 2 6 DLM11021080 1 20020914 A 2611 CONNECTOR DOUG MD11 MD11 3023602 NM SMOKE DETECTOR DIRTY A DALA O OTHER N FALSE WARNING CL CLIMB 1 SO 27 804DE 48475 LAV SMOKE LIGHT ILLUMINATED ON ADVISORY PANEL. DETECTOR IN FWD/CONDO AREA WAS ACTIVATED WITH NO INDICATION OF ASSOCIATE D SMOKE. INTAKE OF SENSOR WAS COVERED AND ALARM CEASED. WHEN SENSOR UNCOVERED SYSTEM OPERATED NORMALLY. ALARM REOCC URED SEVERAL TIMES. ALL PACK OPERATION ON GROUND NORMAL. NO SMOKE OR ODOR NOTED IN CREW REST MODULE. CLEAN AND RESEAT CREW REST SMOKE DETECTOR CONNECTOR. PERFORMED SMOKE DETECTOR TEST PER CRM SUPP MTC MANUAL. TEST OKAY. 2 L 7 3 4F RT A22WE 2003020600027 20030206 00027 NM 2003 2 6 DLM11021117 1 20020921 A 2611 FTA716 SMOKE DETECTOR DOUG MD11 MD11 3023602 NM CREW REST MODULE MALFUNCTIONED A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 803DE 48474 DURING CRUISE AT FL 380, THE SMOKE ALARM SOUNDED IN THE CREW REST FACILITY WITH ASSOCIATED LAV SMOKE EAD ALERT. AFTER APPROXIMATELY ONE MINUTE THE ALARM AND ALERTS EXTINGUISHED. PACK NR 1 TEMP WENT TO 50 DEG WHILE 2 AND 3 AT 26 DEF F. CY CLED AIR CONTROLLER AND PACK 1 BACK TO 26 DEG F. ACC-1 NO CURRENT FAULTS. LAST FLT FAULTS RAM AIR DR ACT. A CC-1 RTS PASS. CLEAN AND RESEAT CRM SMOKE DET ELEC CONN. CRM SMOKE DETECTOR TEST PASS PER CRM SUPP M/M. RAN ENG PER PFHB AND PACK 1 TEMP NORMAL. NO ODOR NOTED IN COCKPIT OR CREW REST MODULE. 2 L 7 3 4F RT A22WE 2003020600028 20030206 00028 NM 2003 2 6 DLM11021123 1 20020921 A 2120 ODOR DOUG MD11 MD11 3023602 NM CABIN DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 802DE 48473 ACRID ODOR RESEMBLING BURNING WIRE REPORTED NEAR VIDEO EQUIPMENT, PAX AND CREW NEAR SEATS 12 A/B 13 A/B REPORTED THE ODO R DURATION OF ABOUT 5 MINUTES THEN DISSAPATED. ALL VIDEO EQUIPMENT WAS TURNED OFF. NO OTHER ABNORMAL INDICATIONS OBSERVE D. CHECKED SEAT 12 A/B 13 A/B FOR ELECTRICAL OPS FOUND OK ALL VIDEO PLAYERS FOUND OPS OK NO ODOR, NO ABNORMAL INDICATION S FOUND OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2003020600029 20030206 00029 NM 2003 2 6 DLM11021169 1 20021004 A 3510 GENERATOR 80138612 DOUG MD11 MD11 3023602 NM CREW REST AREA ACTIVATED A DALA O OTHER O OTHER NR NOT REPORTED 1 SO 27 802DE 48473 OXYGEN GENERATOR FIRED IN CREW REST COMPARTMENT. REPLACED GENERATOR AND BROKEN OXYGEN COMPARTMENT DOOR. 2 L 7 3 4F RT A22WE 2003020600030 20030206 00030 NM 2003 2 6 DLM11021173 1 20021006 A 2530 CONTROL PANEL DOUG MD11 MD11 3023602 NM GALLEY OVEN MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 807DE 48478 OVEN NR 2 BURNING METAL ORDO FROM ELECTRICAL TOUCH PANEL AREA AROUND PANEL HOT C/B PULLED RESET C/B RAN OVEN TO 350 DEGR EES FOR 20 MINUTES NO DEFECTS NOTED OK FOR SERVICE 2 L 7 3 4F RT A22WE 2003020600031 20030206 00031 NM 2003 2 6 DLM11021248 1 20021027 A 7800 CH251320 SWITCH DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE THRUST REVERSER FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 814DE 48769 723915 NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON CLIMBOUT. REPLACED LOWER OUTBOARD THRUST REVERSER LOCK ACTUATOR SWITCH. 2 L 7 3 4F 4 F RT A22WE E24NE 2003020600032 20030206 00032 NM 2003 2 6 DLM11021285 1 20021102 A 3230 ACTUATOR DOUG MD11 MD11 3023602 NM MLG OVERCENTER LEAKING A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 806DE 48477 GEAR FAILED TO RETRACT ON FIRST ATTEMPT. SECOND ATTEMPT SUCCESSFULL. PERFORMED GEAR SWING TO DUPLICATE PROBLEM. SWUNG GEAR 4 TIMES. NO PROBLEMS NOTED. SYSTEM CHECKS GOOD. DURING GEAR SWING, FOUND LT GEAR OVERCENTER LOCK ACTUATOR LEAKING . R & R LT GEAR OVER CENTER LOCK ACTUATOR PER M/M. 2 L 7 3 4F RT A22WE 2003020600033 20030206 00033 NM 2003 2 6 DLM11021293 1 20021105 A 2560 61020 BATTERY DOUG MD11 MD11 3023602 NM FLASHLIGHT DISCHARGED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 805DE 48476 FOUND DURING EMERGENCY EQUIPMENT CHECK. L-3 EMERGENCY FLASHLIGHT PULLED AND STOWED 180 DEGREES OUT IN ITS CRADLE BATTERY DRAINED. REPLACED SAME. 2 L 7 3 4F RT A22WE 2003020600034 20030206 00034 NM 2003 2 6 DLM11021324 1 20021115 A 2611 72130001013 SMOKE DETECTOR DOUG MD11 MD11 3023602 NM LAVATORY INOPERATIVE A DALA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 814DE 48769 LAV SMOKE ALERT ILLUMINATED FROM FULL AFT RIGHT SIDE LAV. INSPECTION MADE WITH NO VISIBLE SMOKE OR FUMES NO ODORS DETECT ED DECLARED EMERGENCY INTO BOM. WARNING REOCCURED ON LANDING INTO BOM WITH CHIMES CONTINUING. FOUND LAV AFT OF 4R DOOR SMOKE DETECTOR INOPERATIVE. REPLACED SMOKE DETECTOR. 2 L 7 3 4F RT A22WE 2003020600035 20030206 00035 NM 2003 2 6 DLM11021361 1 20021123 A 2121 29680 FAN DOUG MD11 MD11 3023602 NM NR 1 PACK SEIZED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 806DE 48477 STRONG ELECTRICAL BURNING ODOR DURING DESCENT, JUST AFTER WINDSHIELD HEAT WAS TURNED ON. CREW DEACTIVATED WINDSHIELD HEA T, TURNED ECON OFF AND ISOLATED THE NR 1 PACK. FUMES DISSAPATED. CREW COULD HEAR MOTOR FAN THAT SOUNDED AS IF IT WAS B INDING. FUMES SEEM STRONGEST AROUND C/B PANEL. FOUND AVIONICS COOLING FAN NR 3 WITH C/B POPPED. REPLACED FAN. FAN OPS NORMAL. C/B REMAINS CLOSED. 2 L 7 3 4F RT A22WE 2003020600036 20030206 00036 NM 2003 2 6 DLM11021422 1 20021205 A 4930 3883295 FUEL CONTROL DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE APU FAILED A DALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 815DE 9051 P145 48624 SLIGHT HAZE AND ODOR NOTICED IN MID CABIN AREA DURING CLIMB OUT WITH ALL ENGINE, WING AND TAIL ANTI-ICE ON. BOTH HAZE A ND ODOR SUBSIDED WHEN WING AND TAIL ANTI-ICE IS TURNED OFF. FOUND APU OIL LEAK OUT OF PORT NR 2 ON DRAIN MAST. R & R F UELCONTROL ASSY PER AMM. LEAK AND OPS CHECK GOOD R & R COALESER BAGS. RAN ENGINES. NO SMOKE DETECTED IN CABIN. 2 L 7 3 4F 4 F RT A22WE E24NE 2003020600042 20030206 00042 NM 2003 2 6 DLM11021435 1 20021213 A 2740 CONTROL VALVE DOUG MD11 MD11 3023602 NM PRIMARY TRIM MALFUNCTIONED A DALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 27 805DE 48476 AT 5000 FT, FLAPS AT 15 AUTOPILOT NR 2 ENGAGED. RECEIVED STAB OUT OF TRIM AND STAB IN MOTION ALERTS. DISCONNECTED AUTO PILOT AND A/C PITCHED UP 20 DEGREES. MANUALLY TRIMED STAB OK. CHECKED ELEVATOR RIGGING PER MM CHECKS OK. CHECKED HI R ATE STAB TRIM OPERATION, ALL OK. REPLACED PRIMARY TRIM CONTROL VALVE PER MM 27- 43-40-4, NO LEAKS NOTED. RAN FUNCTIO N TEST OF HORIZONTAL STAB TRIM RATE AND ADJUSTMENT AND TEST SYST CHECKS OK. 2 L 7 3 4F RT A22WE 2003020600043 20030206 00043 NM 2003 2 6 DLM11021451 1 20021219 A 2150 A/C PACK DOUG MD11 MD11 3023602 NM NR 1 ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 810DE 48565 ODOR AND FUMES IN COCKPIT AND AFT CABIN. A/C ATB TO ATL, AS A PRECAUTIONARY MEASURE DUE TO FUMES. REPLACED ALL THREE COLESCER BAGS. ODOR WAS ISOLATED TO NR 1 PACK. NO FURTHER ODORS NOTICED LEAK CHECK AND OPERATION NORMAL. 2 L 7 3 4F RT A22WE 2003020600049 20030206 00049 NM 2003 2 6 DLM88021036 1 20020904 A 3230 O-RING DOUG MD88 MD88 3023688 NM MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 979DL 53266 AFTER TAKE OFF, NOSE GEAR SHOWED UNSAFE IN UP POSTION. RECYCLED LANDING GEAR IAW POM PROCEDUCRES. NO HELP RETURNED TO ATL. NOSE GEAR STRUT SHRADER VALVE O-RING DETERIORATED. REPLACED SHRADER VALVE AND O-RING AND SERVICED STRUT PER MM LEA K CHECK OK. NO SPOILER FAIL STALL INDICATION FAIL OR AUTO PRESSURE FAIL MSG. PERFORMED NOSE GEAR SWING. GEAR INDICATION S NORMAL 2 L 7 2 4F RT A6WE 2003020600050 20030206 00050 NM 2003 2 6 DLM88021045 1 20020906 A 2170 COALESCER BAG DOUG MD88 MD88 3023688 NM AIR CONTDITIONER DIRTY A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SO 27 907DL 49538 AIR CONDITIONER PRODUCED A FUEL LIKE ODOR. COMPLIED WITH OP 5088, NO DEFECTS NOTED. CHANGED COALESCER BAGS AS PRECAUTI ON AWAITING DUCT BURN OUT, OP 5089. 449991. COMPLIED WITH OPN 5089- PNEUMATIC DUCT BURNOUT. ALL CHECKS OK. 2 L 7 2 4F RT A6WE 2003020600051 20030206 00051 NM 2003 2 6 DLM88021046 1 20020907 A 2910 AS15308K0254 LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING A DALA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 914DL 49545 APPROCH FLT.615 AT 1329 - RT SYS HYD FLUID LOSS, HYD RETURN LINE WORN THRU RT SIDE AFT ACCESSORY BAY. FLEX LINE PN 2992 01301 REPLACED. REPLACED RT ENGINE DRIVEN HYD PUMP. REPLACED HYD FILTERS, WASHED APU INLET. REPLACED COALESCER BAGS & PERFORMED PNEUMATIC SYS DUCT BURNOUT- 2 L 7 2 4F RT A6WE 2003020600052 20030206 00052 EA 2003 2 6 QXEA0202267 1 20021228 A 2820 D98C09602 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA K NONE K FLUID LOSS UK UNKNOWN 1 NM 09 604QX 2322 10019 BOI-ON FLIGHT NUMBER 2550. FUEL LEAKING CENTER OF FUSELAGE BENEATH THE WING. REPLACED PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020600054 20030206 00054 EA 2003 2 6 QXEA0202268 1 20021226 A 2120 ODOR CNDAIR CL600 CL6002C10 1390015 EA CABIN DETECTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 612QX 10042 PDX-ENROUTE, FLIGHT ATTENDANTS COMPLAINED OF AN ODOR TOWARDS THE REAR OF THE CABIN CAUSING THEIR EYES TO BURN AND FELT S ICK. GROUND RAN BOTH ENGINES. NO SMELLS NOTICED IN BLEED SYSTEM. HAD LAVATORY SERVICED, NO SMELLS NOTICED AT THAT TIM E. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020600055 20030206 00055 NM 2003 2 6 DLM88021048 1 20020908 A 4990 38005041 APU DOUG MD88 MD88 3023688 NM APU BAY LEAKING A DALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 913DL 12466 49544 DURING TAKEOFF AFT F/A REPORTED ODOR IN CABIN. PERFORMED OP 5088 FOUND OIL LEAK AT APU OIL FILLER NECK. REPLACED APU PER M/M PERFORMED OP 5089 DUCY BURNOUT A/C OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2003020600056 20030206 00056 2003 2 6 DLM88021052 4 20020909 A 2565 D29982113 SLIDE DOUG MD88 MD88 3023688 NM R1 DOOR DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 929DL 49716 FWD GALLEY DOOR SLIDE PRESSURE LOW . REPLACED SLIDE 2 L 7 2 4F RT A6WE 2003020600057 20030206 00057 NM 2003 2 6 QXEA0202269 1 20021222 A 4990 OIL SYSTEM BOMBDR DHC8 DHC8401 1390041 NM APU OVERSERVICED A QXEA K NONE W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 402QX 4032 SEA-SUP, ON FLIGHT NUMBER 2340, AFTER TAKE OFF PASSENGER SMELLED BURNING RUBBER-TYPE SMELL IN ROWS 17 & 18, ALSO AFTER L ANDING SAME SMELL IN REAR OF CABIN. DETERMINED OIL SMELL FROM APU. FOUND APU OIL OVERSERVICED BY 12-14 OZ. DRAINED OF F EXCESS OIL. RAN APU. COULD NOT SMELL BURNING RUBBER OR OIL SMELLS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2003020600058 20030206 00058 NM 2003 2 6 DLM88021053 1 20020909 A 3350 POWER SUPPLY UNK DOUG MD88 MD88 3023688 NM CABIN ROW 31 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DL 6829 49543 EMERGENCY EXIT LIGHT INOPERATIVE ROW 24 THRU 36. REPLACED POWER SUPPLY AND REPAIR WIRE AT SEAT B25 LIGHTS CHECK GOOD. 2 L 7 2 4F RT A6WE 2003020600059 20030206 00059 EU 2003 2 6 QXEA0202270 1 20021226 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 11159 BOI- EXIT SIGN OVER COCKPIT DOOR HAS BURNED OUT LAMPS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2003020600060 20030206 00060 NM 2003 2 6 DLM88021058 1 20020903 A 5755 SKIN DOUG MD88 MD88 3023688 NM LT WING SPOILER DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DL 49532 LT WING FLIGHT SPOILER DELAMINATED. REPAIR PER ER/A 417628-14 2 L 7 2 4F RT A6WE 2003020600061 20030206 00061 EU 2003 2 6 QXEA0202271 1 20021226 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 11159 BOI- EXIT SIGN AT CABIN ENTRANCE HAS BURNED OUT BULBS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2003020600062 20030206 00062 NM 2003 2 6 DLM88021060 1 20020910 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN ROW 19D INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 977DL 53258 EMERGENCY TRACK LIGHT AT 19D INOPERATIVE. REPLACED SEAT MOUNTED LIGHT ASSY 2 L 7 2 4F RT A6WE 2003020600063 20030206 00063 NM 2003 2 6 QXEA0202272 1 20021230 A 5210 MECHANISM DHAV DHC8 DHC8202 2809007 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 369PH 513 PDX-MAIN PASSENGER CABIN DOOR IS HARD TO OPEN FROM INSIDE. LUBED DOOR SEAL AND MAIN CABIN DOOR CAM MOMENTS/SLIDES. OPE RATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003020600064 20030206 00064 EA 2003 2 6 QXEA0202273 1 20021227 A 2611 9847101505 CAGE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY TORN A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 609QX 10031 BOI-FORWARD CARGO PIT CENTER CHIMNEY IS TORN. REPLACED CENTER CHIMNEY. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020600065 20030206 00065 NM 2003 2 6 DLM88021068 1 20020907 A 2930 ST107Q TRANSMITTER DOUG MD88 MD88 3023688 NM LT HYD SYSTEM FAILED A DALA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 953DL 49884 ON APPROACH, LT HYD PRESS LOW MESSAGE APPEARED ON OAP AND LT HYD PRESSURE INDICATION DROPPED TO ZERO. PERFORMED ABNORM AL CHECK LIST PER POM. AFTER LANDING REVERSER UNLOCK AMBER LIGHT ILLUMINATED EVEN AFTER REVERSERS WERE STOWED. INSPECTE D CASE DRAIN AND PRESSURE FILTERS FOR CONTAMINATION, NONE NOTED. REPLACED LT HYD SYS PRESSURE TRANSMITTER, ALL INDICATIO NS NOW NORMAL. 2 L 7 2 4F RT A6WE 2003020600066 20030206 00066 NM 2003 2 6 QXEA0202274 1 20021228 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PJ 511 PDX - NR 4 FLAP TRACK PITTED ON BOTH SIDE ON LEFT HAND WING. REPAIRED IAW HORIZON AIR EA 2-57-216. 2 H 7 2 4T RT A13NM 2003020600067 20030206 00067 NM 2003 2 6 QXEA0202275 1 20021229 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - NR 8 SEAT TRACK HAS LIGHT CORROSION ON TOP OF INBOARD RAIL FROM X468 TO X471. REPAIRED IAW RD 8-53-1339. 2 H 7 2 4T RT A13NM 2003020600068 20030206 00068 NM 2003 2 6 QXEA0202276 1 20021228 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - NR 8 SEAT TRACK HAS LIGHT CORROSION ON BOTTOM OF CHANNEL FROM X441 TO X452. REPAIRED IAW DHC-8 200 MM RD 8-53-133 9. 2 H 7 2 4T RT A13NM 2003020600069 20030206 00069 NM 2003 2 6 DLM88021078 1 20020914 A 2913 PUMP DOUG MD88 MD88 3023688 NM RT ENGINE FAILED A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 918DL 49583 LOST RT HYD PRESS IN FLT, QTY NORMAL. EMERGENCY GEAR EXTENTION ACCOMPLISHED. LOST LT PRESSURE WHEN FLAP / SLATS EXTE NDED. REPLACED RT ENGINE DRIVEN HYDRAULIC PUMP. 2 L 7 2 4F RT A6WE 2003020600070 20030206 00070 NM 2003 2 6 QXEA0202277 1 20021229 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - NR 8 SEAT TRACK HAS LIGHT CORROSION ON TOP OF INBOARD RAIL FROM X454 TO X453. REPAIRED IAW DHC-8 S00 RD 8-53-1339 . 2 H 7 2 4T RT A13NM 2003020600071 20030206 00071 NM 2003 2 6 QXEA0202278 1 20021222 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - NR 8 SEAT TRACK HAS CORROSION ON TOP OF OUTBOARD RAIL FROM X458 TO 453. REPAIRED IAW DHC-8 200 RD 8-53-1339. 2 H 7 2 4T RT A13NM 2003020600072 20030206 00072 NM 2003 2 6 QXEA0202279 1 20021224 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - FRAME NR 4 STATION 700.409 HAS CRACK AT STRINGER NR 5 ON RIGHT HAND SIDE. REPAIRED IAW DHC-8 SRM 51-20-21, PAGE 3 . 2 H 7 2 4T RT A13NM 2003020600073 20030206 00073 NM 2003 2 6 DLM88021086 1 20020915 A 3350 BATTERY PACK DOUG MD88 MD88 3023688 NM LT & RT OVERWING INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 975DL 53243 LT AND RT AFT EMERGENCY OVERWING LIGHTS INOPERATIVE. REPLACED BATTERY PACK OPS NORMAL. 2 L 7 2 4F RT A6WE 2003020600074 20030206 00074 NM 2003 2 6 QXEA0202280 1 20021228 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - GOUGE IN BOTTOM OF RIGHT HAND INBOARD SEAT TRACK NR 9 AT APPROXIMATELY STATION X543.0. REPAIRED IAW DHC-8 SRM 51- 20-26 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2003020600075 20030206 00075 NM 2003 2 6 QXEA0202281 1 20021228 A 5753 ROLLER DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - FLAT SPOT ON TOP ROLLER OF THE NR 4 FLAP TRACK ON LEFT HAND WING. REPAIRED IAW TASK 27-51-11-400-802, PAGE 417 AN D SUB TASK 27-52-24-420-002, PAGE 417, PARAGRAPH 3A (1)(3). 2 H 7 2 4T RT A13NM 2003020600076 20030206 00076 NM 2003 2 6 QXEA0202282 1 20021228 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - RIGHT HAND WING NR 4 FLAP TRACK IS PITTED. REPAIRED IAW HORIZON AIR EA 2-57-214. 2 H 7 2 4T RT A13NM 2003020600077 20030206 00077 NM 2003 2 6 DLM88021096 1 20020917 A 3260 SENSOR DOUG MD88 MD88 3023688 NM NLG INTERMITTENT A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 901DL 49532 AIR TURN BACK, AFTER GEAR RETRACTION NOSE GEAR RED UNSAFE LIGHT ON CYCLED GEAR ALL LIGHTS OUT. REPLACED NOSE GEAR UPLOC K SENSOR RAN GEAR SEVERAL TIMES OPS CHECKS OK. PSEU HAD FAULTED SENSOR NOW CHECKS OK. 2 L 7 2 4F RT A6WE 2003020600078 20030206 00078 NE 2003 2 6 DLM88021103 2 20020917 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 FAILED A DALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 905DE 34385 53410 725395 AT ABOUT 600 FT AGL ON CLIMB 8R ATL THE LT ENGINE ROLLED BACK TO IDLE. TRIED TO PUSH POWER UP ON DOWNWIND AND IT WOULD N OT ACCELERATE PAST 38 PCT N1. ALL ENGINE INDICATIONS WERE NORMAL NO NOISE OR VIBRATION. NORMAL AMOUNT OF YAW FOR SITUATI ON. REPLACED NR 1 ENGINE PER TRANSMITTAL 9T102. 2 L 7 2 4F 4 F RT A6WE E9NE 2003020600079 20030206 00079 NM 2003 2 6 QXEA0202283 1 20021228 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - RIGHT HAND WING, NR 4 FLAP TRACK IS PITTED ON INBOARD UPPER TRACK LOWER SURFACE. REPAIRED IAW HORIZON AIR EA 2-57 -214. 2 H 7 2 4T RT A13NM 2003020600080 20030206 00080 NM 2003 2 6 QXEA0202284 1 20021228 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - RIGHT HAND WING NR 4 FLAP TRACK PITTED ON CONTACT SURFACE FOR UPPER DEAD WEIGHT ROLLER. REPAIRED IAW HORIZON EA 2 -57-214. 2 H 7 2 4T RT A13NM 2003020600081 20030206 00081 NM 2003 2 6 QXEA0202285 1 20021228 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - RIGHT HAND WING, NR 4 FLAP TRACK IS PITTED, INBOARD ROLLER, BEARING SURFACE. REPAIRED IAW HORIZON AIR EA 2-57-214 . 2 H 7 2 4T RT A13NM 2003020600082 20030206 00082 NE 2003 2 6 DLM88021105 2 20020918 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 FAILED A DALA F A ACTIVATE FIRE EXT. UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 27 901DL 49532 725896 LT ENGINE FAILED SHORTLY AFTER GOING TO CLIMB POWER. AFTER SHUTDOWN ABOUT 7 PERCENT N2, 0-1 N1, AND 0 OIL PRESSURE ON LT ENGINE. AT APPROX. 210 KIAS. PULLED FIRE HANDLE AND BLEW BOTTLES. REPLACED NR 1 ENGINE PER TRANS 9T102 - REPLACED N R 1 FIRE BOTTLE. 2 L 7 2 4F 4 F RT A6WE E9NE 2003020600083 20030206 00083 NM 2003 2 6 QXEA0202286 1 20021226 A 5542 SKIN DHAV DHC8 DHC8202 2809007 NM RUDDER CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - TRAIL RUDDER HAS PAINT MISSING AND EVIDENCE OF CORROSION UNDER SECOND FROM TOP AND BOTTOM STATIC WICKS. REPAIRED IAW DHC-8 MM 23-60-01-720-001, PAGE 406. 2 H 7 2 4T RT A13NM 2003020600084 20030206 00084 NM 2003 2 6 QXEA0202287 1 20021227 A 3222 ARM DHAV DHC8 DHC8202 2809007 NM NLG DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - THE LEADING EDGE OF THE NOSE LANDING GEAR STRUT LOWER TRAILING ARM IS SCRATCHED, GOUGED AND WORN. REPAIRED IAW DH C-8 RD 8-32-289, SECTION 1 AND CMM 32-20-01. 2 H 7 2 4T RT A13NM 2003020600085 20030206 00085 NM 2003 2 6 QXEA0202288 1 20021228 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - PITTED ON BOTH SIDES OF NR 4 FLAP TRACK ON LEFT HAND WING. REPAIRED IAW HORIZON AIR EA 2-57-216. 2 H 7 2 4T RT A13NM 2003020600086 20030206 00086 NM 2003 2 6 QXEA0202289 1 20021227 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - CHAFING ON MATTING SURFACE AND AROUND BOLT HOLES AT ONE END OF FUEL PANEL 524BT ON LEFT HAND WING. REPAIRED IAW D HC-8 SRM 57-20-11. 2 H 7 2 4T RT A13NM 2003020600087 20030206 00087 NM 2003 2 6 QXEA0202290 1 20021227 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - BAGGAGE DOOR APERTURE TOP FRAME HAS LIGHT CHAFING IN PREVIOUS BLEND AREA. REPAIRED IAW RD 8-53-5461. 2 H 7 2 4T RT A13NM 2003020600088 20030206 00088 NM 2003 2 6 QXEA0202291 1 20021227 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - BAGGAGE DOOR APERTURE FRAME HAS LIGHT CHAFING IN FORMER BLEND AREA AT TOP STATION 588.5. REPAIRED IAW RD 8-53-546 1. 2 H 7 2 4T RT A13NM 2003020600089 20030206 00089 NM 2003 2 6 DLM88021112 1 20020920 A 2910 B-NUT DOUG MD88 MD88 3023688 NM HYD SYSTEM LOOSE A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 951DL 49882 AIRCRAFT RETURNED TO RAMP DUE TO SMOKE IN CABIN. FOUND HYD LINE B-NUT LOOSE AND LEAKING AT LT THRUST REVERSER CONT VALV E. TIGHTENED LINE AND LEAK CHECKS GOOD. REPLACED RT AND LT COALESCER BAGS. LEAK CHECKS OK. PERFORMED OP 5089 DUCT BU RNOUT. CHECKS OK. 2 L 7 2 4F RT A6WE 2003020600090 20030206 00090 EA 2003 2 6 QXEA0202292 1 20021229 A 2820 CC67061042 FUEL LINE CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM CRACKED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 609QX 10031 SEA - FLIGHT 464 - THE LEFT AND RIGHT FUEL BOOST PUMPS WERE CYCLING IN FLIGHT. SEVEN SECONDS ON AND 3 SECONDS OFF CONTI NUOUSLY FROM 15000 TO 28000 FEET. MAINTENANCE INSPECTED AND FOUND THE RIGHT ENGINE FEED TUBE CRACKED. THE TUBE WAS REP LACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020600091 20030206 00091 SO 2003 2 6 SIMA200232909 1 20021123 A 3230 355022002 CONTROL UNIT EMB 135 EMB135LR 3260305 SO E/E BAY MALFUNCTIONED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 711PH 145235 JFK - FLT 4748 - DURING FLIGHT CREW REPORTED E1 REVERSER DISAGREE AND SPOILER MESSAGE ON EICAS. AIRCRAFT DIVERTED TO JF K. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC CONTROLUNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2003020600092 20030206 00092 NM 2003 2 6 DLM88021118 1 20020922 A 2530 50459 OVEN DOUG MD88 MD88 3023688 NM GALLEY SMOKE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 952DL 198 49883 CLIMBING OUT OF SAT AT APPROXIMATELY 8000 FT, FA REPORTED SMOKE COMIING FROM FWD GALLEY AC WAS LEVELED AT 14000 FT FLT CREW SHUT OFF GALLEY POWER. SMOKE DISSAPATED DIVERTED TO AUS WITHOUT INCIDENT. REMOVED F/C OVEN AND INSPECTED FOR HE AT AND OVEN WIRE HARNESS, NONE FOUND. REPLACED OVEN. 2 L 7 2 4F RT A6WE 2003020600093 20030206 00093 NM 2003 2 6 DLM88021143 1 20020926 A 5330 SKIN 99115311 DOUG MD88 MD88 3023688 NM FUSELAGE LIGHTNING STRIKE A DALA O OTHER O OTHER NR NOT REPORTED 1 SO 27 967DL 53116 DURING HMV-2, LIGHTNING STRIKE DAMAGE ON WINDOW BELTS WAS FOUND AT FS 674-693 AND FS 712-731. A TIME LIMITED BLEND REPAI R WAS PERFORMED. 2 L 7 2 4F RT A6WE 2003020600094 20030206 00094 NM 2003 2 6 TSAA0253236 1 20021027 A 5312 PRESSURE PANEL BOEING 737 737282 13844AT NM FUSELAGE DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 PERFORMED MODIFICATION TO THE WEB AND DOUBLER OF THE MAIN WHEEL WELL PRESSURE FLOOR TRANSVERSE BEAM BETWEEN BS 650 AND B S 727 AND BETWEEN RT AND LT BBL 45. FABRICATED WEB FILLER AND REPAIR DOUBLER IAW FIGURE 7. REPLACED ANGLE, CHANNEL AND DOUBLER WITH PARTS FABRICATED PER FIGURE 3. VERIFIED 8110-3 RECEIVED. COMPLETED MODIFICATION IAW ECO 2299, FIGURE 3/7 . AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003020600095 20030206 00095 NM 2003 2 6 DLM88021147 1 20020928 A 2910 FITTING DOUG MD88 MD88 3023688 NM HYD SYSTEM LOOSE A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 951DL 49882 LT HYDRAULIC SYSTEM QUANTITY INDICATES 1 QUART. PRESSURE 3100 PSI. PER CREW COMMENT PUMPS SHUT DOWN-0 PSI WHEN PUMPS RE APPLIED. TIGHTENED LOOSE LT THRUST REVERSER CONTROL VALVE HYDRAULIC LINE. A/C DUE DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2003020600096 20030206 00096 NM 2003 2 6 TSAA0253239 1 20021107 A 5711 6545499 SPAR BOEING 737 737209 13844AE NM LT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 827AL 23913 FOUND CORROSION ON RIGHT FRONT SPAR LOWER CHORD SURFACE AT WSL 557. CONFIRMED COMPLETE REMOVAL OF CORROSION WITH HFEC I NSPECTION. FABRICATED A REPAIR FILLER TO FIT IN THE BLENDOUT AREA. FABRICATED A REPAIR STRAP. REPAIR COMPLETED IAW EC O. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003020600097 20030206 00097 NE 2003 2 6 DLM88021148 2 20020928 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 FAILED A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 27 943DL 37110 49816 718120 NR 2 ENGINE SHUTDOWN IN FLIGHT. RT OIL PRESSURE ZERO. AMBER LIGHT, QUANTITY, AND TEMP OK. GOT COMPRESSOR STALL, EGTTO 80 0. S/D ENGINE AND RETURNED TO CVG. RT OIL PERSSURE NEVER GOT OFF ZERO. REMOVED AND REPLACED NR 2 ENGINE. CHECKS GOOD P ER PFHB 2 L 7 2 4F 4 F RT A6WE E9NE 2003020600098 20030206 00098 NE 2003 2 6 DLM88021182 2 20021009 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 STALLED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 980DL 32199 53267 725484 LT ENGINE COMPRESSOR STALL WHEN THROTTLES WERE ADVANCED FOR TAKEOFF ON RUNWAY AT EWR. INSPECTED INLET AND EXHAUST OF LT ENGINE WITH NO OBVIOUS DEFECTS. REPLACED LT ENGINE PRBC AND RAN ENGINE PER PFHB TEST E WITH NORMAL RESULTS. 2 L 7 2 4F 4 F RT A6WE E9NE 2003020600099 20030206 00099 NE 2003 2 6 TSAA0272227 2 20021120 A 7200 ENGINE BOEING 737 737282C 13844AU NM PWA JT8 JT8D9A 52048 NE NR 2 MALFUNCTIONED A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 826AL 23051 P687772B DURING THE CLIMB, THERE WAS A DROP IN OIL PRESSURE ON THE NR 2 ENGINE. THE CREW RETURNED TO ITO AND MADE AN UNEVENTFUL LANDING WITH NO FURTHER INCIDENT. MAINTENANCE PERSONNEL SERVICED THE NR 2 ENGINE AND CONDUCTED AN ENGINE RUN. THE NR 2 ENGINE HAD CONSUMED 14 QUARTS OF OIL IN 20 MINUTES. THE NR 2 ENGINE WAS REMOVED AND REPLACED. GROUND OPERATIONAL CHEC KS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. OIL LEAKAGE WAS EVIDENT AROUND THE NR 4.5 BEARING CARBON SEALS A ND THE NR 5 BEARING SEAL SUPPORT AREAS. ALL NR 4.5 BEARING CARBON SEALS WERE REPLACED. THE NR 5 BEARING SEAL SUPPORT S PRING AND SEAL RINGS WERE REPLACED. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2003020600100 20030206 00100 NM 2003 2 6 DLM88021183 1 20021011 A 3260 UPLOCK SENSOR DOUG MD88 MD88 3023688 NM NLG MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 958DL 49977 AFTER TAKEOFF, HAD ALL GEAR RETRACTED NOSE GEAR WAS SLOW BUT SHOWED NORMAL ( NO LIGHTS) AFTER APPROX 30 SECONDS RED NOSE LIGHT CAME ON. RAN CHECK LIST, CYCLED GEAR RED NOSE LIGHT REMAINED ON. NOISE LEVEL ALSO INDICATED THAT GEAR WAS NOT TOT ALLY UP. GEAR WAS EXTENDED FOR NORMAL LANDING ( RTN BACK TO BOSTON ) INSPECTED NOSE GEAR AND DOORS NO TROUBLE FOUND. FOU ND NOSE GEAR STRUT PROPERLY SERVICED. LUBED NOSE GEAR AS PRECATIONARY. REPLACED NOSE GEAR UP DOWN LOCK SENSORS PER MM. OPERATED NOSE GEAR UP/DOWN_SEVERAL CYCLES ALL INDICATIONS NORMAL. 2 L 7 2 4F RT A6WE 2003020600101 20030206 00101 CE 2003 2 6 UG8A235J 1 20021110 A 2722 ACTUATOR CESSNA 750 750 2076810 CE RUDDER FAULTY A UG8A O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 23 5114 7500017 DURING CLIMB-OUT OF DTW, THE RUDDER LIMIT FAIL AT 24 PERCENT AMBER CAS MESSAGE ILLUMINATED. ALSO,THE PITOT HEATER FAIL SB AMBER CAS MESSAGE ILLUMINATED. REPLACED FAULTY LINEAR ACTUATOR. REPLACED FAULTY LOGIC MODULE. (M) 2 L 7 2 4J RT T00007WI 2003020600102 20030206 00102 NM 2003 2 6 DLM88021184 1 20021011 A 5552 SKIN DOUG MD88 MD88 3023688 NM ELEVATOR TAB DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 932DL 49719 DURING OVERHAUL OF ELEVATOR GEARED TAB, SERVICE DAMAGE WAS FOUND WHICH WAS BEYOND THE SCOPE OF LOCAL REPAIR. THEREFORE A RESKIN OF THE PART WAS ACCOMPLISHED. REPAIR PER ERA 417690-14 2 L 7 2 4F RT A6WE 2003020600103 20030206 00103 NM 2003 2 6 DLM88021192 1 20021012 A 3350 BATTERY PACK DOUG MD88 MD88 3023688 NM TAIL COMPT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 901DL 49532 FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE, DIM AND FLICKERING. REPLACED BATTERY PACK CHECKS GOOD. 2 L 7 2 4F RT A6WE 2003020600104 20030206 00104 NM 2003 2 6 DLM88021202 1 20021016 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 981DL 53268 1 C TRACK LIGHT INOPERATIVE. RELAMPED OPS CHECK OK 2 L 7 2 4F RT A6WE 2003020600105 20030206 00105 NM 2003 2 6 DLM88021209 1 20021018 A 4990 SEAL DOUG MD88 MD88 3023688 NM APU OIL CAP WORN A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 957DL 10864 49976 AFTER TAKEOFF EXPERIENCED A ODOR CONSISTANT WITH A WARM DUCT THE AFT LAV SMOKE DETECTORS SOUNDED AND F/A'S REPORT A SL IGHT HAZE IN CABIN. AT FL 9000 FT. ODOR CEASED AND SMOKE DETECTORS STOPPED. FOUND APU OIL CAP SEAL DETERIORATED. REPLA CED OIL CAP CLEANED AREA AND PERFORMED DUCT BURN OUT PER AMM 2 L 7 2 4F RT A6WE 2003020600106 20030206 00106 NM 2003 2 6 DLM88021221 1 20021016 A 5310 59360381 BEAM DOUG MD88 MD88 3023688 NM PAX DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 968DL 53161 DURING HMV-2, CORROSION DAMAGE WAS FOUND ON THE C2 & C3 JAMB BEAMS. THE JAMB BEAM DOOR STOP HOLES WERE OUT OF TOLERANCE AFTER CLEAN UP. CORROSION WAS REPAIRED PER MD80 SRM 53-05 FIGURE 63 BY BLENDING AND USE OF A REPAIR DOUBLER. 2 L 7 2 4F RT A6WE 2003020600107 20030206 00107 NE 2003 2 6 DLM88021227 2 20021024 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 BIRD INGESTION A DALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 900DE 27112 53372 726824 AT LIFT-OFF AT PNS THERE WAS NOTICEABLE POP SOUND A SLIGHT YAW TO THE AIRCRAFT FOLLOWED BY SMOKE IN THE CABIN AND A BURN ING ODOR IN COCKPIT. SMELL / SMOKE DISSIPATED RAPIDLY AND NO OTHER ABNORMAL INDICATION NOTED FOR REMAINER OF FLIGHT NOR MAL LANDING. FOUND EVIDENCE OF BIRDSTRIKE ON RT FLAP AND NR 2 ENGINE AROUND BLADE ROOT AREA. BOROSCOPED ENGINE PER MM . PERFORMED TAKEOFF POWER RUN PER PFHB. NTF. ALL PARAMETERS NORMAL. 2 L 7 2 4F 4 F RT A6WE E9NE 2003020600108 20030206 00108 NM 2003 2 6 USAASB02124 1 20020625 A 3610 1074845 REGULATOR BOEING 737 737301 1384611 NM RT ENGINE FAILED A USAA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 EA 19 356US 29656 23559 CLT - FLT 1664 - AFTER T/O FROM CLT TO MDT, A/C EXPERIENCED A DUAL PACK FAILURE. LT PACK TRIPPED, THEN THE RT. FLT RET URNED TO CLT AND LANDED INCIDENT. MAINTENANCE R&R THE RT ENGINE HIGH STAGE REGULATOR PER MM 36-11-86 FOR THE RT PACK. OPS CHECK GOOD. LT PACK, THE 35 DEGREE SENSOR SLOW TO RESPOND. REPLACED 35 DEGREE SENSOR FOR LT PACK. RESPONDS NORMAL . FURTHER TROUBLESHOOTING REVEALED A LT PACK VALVE NOT FULLY OPENING. REPLACED LT PACK VALVE. OPS CHECK GOOD. ALSO, FOUND A FAILED LT RAM AIR TEMP CONTROLLER, RAM AIR TEMP SENSOR AND A SLOW OPERATING RAM AIR ACTUATOR. REPLACED LT RAM A IR TEMP CONTROLLER, SENSOR AND ACTUATOR PER MM. ALL OPERATIONALLY CHECK GOOD. ALSO, REPLACED WORN ROLLERS AND TRACKS F 2 L 7 2 4F RT A16WE 2003020600109 20030206 00109 2003 2 6 USAASB02218 4 20021208 A 2350 TRANSCEIVER BOEING 737 7373B7 1384580 NM COMM SYS MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 532AU 24479 CLT - FLT 502 - ON CLIMB-OUT FROM CLT, CREW LOST ALL COMMUNICATIONS. UNABLE TO COMMUNICATE WITH ATC ON ANY RADIO. MIC' S WERE UNPLUGGED AND CHECKED. COMM 2 STARTED TO WORK ON 121.5. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURT HER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CHECKED ALL 3 COMM R/T UNITS AND COCKPIT MIC'S AGAINST LOCAL FREQ UENCIES. ALL 3 SYSTEMS OPERATIONALLY CHECK NORMAL. NO FAULTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2003020600110 20030206 00110 NM 2003 2 6 DLM88021235 1 20021024 A 4900 38005041 APU DOUG MD88 MD88 3023688 NM APU BAY CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 902DL 14552 49533 JUST AFTER TAKE OFF FLT ATTENDENTS REPORTS HEAVY SMOKE ODOR THROUGH OUT CABIN. CREW RETURNED TO PNS. FOUND APU INLET CON TAMINATED WITH HYD FLUID. AIRCRAFT MTC FERRIED TO ATL. ATL MTC COMPLIED WITH OPN 5089 DUCT BURNOUT AND CLEANED APU INLE T. ATL MTC UNABLE TO FIND ANY HYD LEAKS. 2 L 7 2 4F RT A6WE 2003020600112 20030206 00112 NM 2003 2 6 DLM88021239 1 20021025 A 3010 BLANKET DOUG MD88 MD88 3023688 NM RIGHT WING BURNED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 989DL 53341 WHILE INSPECTING RT WING FUEL LEAK. FOUND APPX 4.5 INCH DIA BURNED AREA IN RT WING HEATER BLANKET. 2 L 7 2 4F RT A6WE 2003020600113 20030206 00113 NM 2003 2 6 DLM88021265 1 20021025 A 3240 26088921 BRAKE ASSY DOUG MD88 MD88 3023688 NM NR 2 LOCKED A DALA O OTHER O OTHER LD LANDING 1 SO 27 909DE 53418 NR 2 BRAKE LOCKED ON LANDING. REPLACED BRAKE 2 L 7 2 4F RT A6WE 2003020600114 20030206 00114 NM 2003 2 6 DLM88021269 1 20021031 A 2121 6054578 FAN DOUG MD88 MD88 3023688 NM RECIRCULATION FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 974DL 53242 AFT FLIGHT ATTENDANT NOTED STRANGE NOISE AND HOT ODOR JUST AFTER ROTATION. A/C RETURNED PHL WITHOUT INCIDENT. RECIRCULAT ION FAN GROWLED UPON SPIN-UP WHILE TESTING. REPLACED FAN 2 L 7 2 4F RT A6WE 2003020600115 20030206 00115 WP 2003 2 6 WX0A02009A 1 20021102 A 3610 5910244363 DUCT DOUG DC9 DC921 302205A WP A/C BAY RUPTURED A WXOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 17 127NK 47361 LAS - TAIL COMPARTMENT HIGH TEMP ANNUNCIATOR INDICATION ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INC IDENT. MAINTENANCE INSPECTED TAIL COMPARTMENT AND ASSOCIATED PRESSURIZATION DISTRIBUTION SYSTEM FOR CAUSE OF HIGH TEMP INDICATION. MX DISCOVERED BLEED AIR LEAK FROM AN UNKNOWN SOURCE IN THE RIGHT AIR CONDITIONING SYSTEM. MAINTENANCE FOUN D RUPTURED BLEED AIR SUPPLY DUCT IN THE RIGHT AIR CONDITIONING SYSTEM. REPLACED OF RIGHT PACK DUCT ASSY. RIGHT AIR CON DITIONING SYSTEM LEAK AND OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2003020600116 20030206 00116 NM 2003 2 6 DLM88021280 1 20021102 A 3260 833703 PROXIMITY SWITCH DOUG MD88 MD88 3023688 NM MLG UPLOCK FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 967DL 53116 ON DEPARTURE GEAR RETRACTED NORMALLY HOWEVER DURING ACCELERATION THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. REPLACED NOSE G EAR UPLOCK PROXIMITY SWITCH. CYCLED GEAR CHECKS OK. 2 L 7 2 4F RT A6WE 2003020600117 20030206 00117 NM 2003 2 6 DLM88021283 1 20021103 A 3350 BATTERY DOUG MD88 MD88 3023688 NM EXTERIOR LIGHTS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 945DL 49818 OUTSIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERT PACK. OPERATES NORMALLY 2 L 7 2 4F RT A6WE 2003020600118 20030206 00118 NM 2003 2 6 DLM88021288 1 20021029 A 5523 TAB DOUG MD88 MD88 3023688 NM ELEVATOR DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DL 49532 NA ELEVATOR ANTI-FLOAT TAB DELAMINATED. REPAIRED PER ER/A 417906-14 2 L 7 2 4F RT A6WE 2003020600119 20030206 00119 NM 2003 2 6 DLM88021290 1 20021104 A 2611 SAAU308C SMOKE DETECTOR DOUG MD88 MD88 3023688 NM LAVATORY FALSE ACTIVATION A DALA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 27 970DL 43173 F/C LAVATORY SMOKE DETECTOR ACTIVATED ON TAKEOFF. NO SMOKE, FIRE, OR FUMES. WOULD NOT RESET. 2 L 7 2 4F RT A6WE 2003020600120 20030206 00120 2003 2 6 DLM88021294 4 20021105 A 3442 20412224456 DISPLAY DOUG MD88 MD88 3023688 NM WX RADAR SYS FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 946DL 49819 AFTER TAKEOFF FROM ATLANTA WEATHER RADAR DISPLAY BECAME DISTORTED AND FAILED SHORTLY AFTER. SMOKE APPEARED FROM RADAR UN IT. CIRCUIT BREAKERS FOR RECEIVER AND INDICATOR PULLED. SMOKE DISSIPATED.AFTER TROUBLESHOOTING, FOUND INDICATOR AT FA ULT. REPLACED INDICATOR SYSTEM OPS CHECK NORMAL. 2 L 7 2 4F RT A6WE 2003020600121 20030206 00121 NM 2003 2 6 DLM88021296 1 20021106 A 2560 61020 BATTERY DOUG MD88 MD88 3023688 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 901DE 53378 FLASHLIGHT AT AFT DOOR NOT BLINKING. REPLACED BATTERIES IN EMERGENCY FLASHLIGHT. 2 L 7 2 4F RT A6WE 2003020600122 20030206 00122 NM 2003 2 6 DLM88021299 1 20021106 A 3232 UNK ACTUATOR DOUG MD88 MD88 3023688 NM NLG DOOR FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 945DL 49818 SEVERE VIBRATION FROM NOSE GEAR AFTER GEAR RETRACTION. GEAR WAS LOWERED AND ALL INDICATIONS WERE NORMAL. FOUND RT GEAR DOOR RETRACTION ACTUATOR FAILED TO LOCK UP. REPLACED GEAR DOOR RETRACTION ACTUATOR PER MM. JACKED NOSE GEAR AND RETRAC TED 3 TIMES. OPS CHECK NORMAL 2 L 7 2 4F RT A6WE 2003020600123 20030206 00123 NM 2003 2 6 DLM88021311 1 20021106 A 5320 59360215 DOUBLER DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 969DL 53172 DURING HMV-2, WEAR TO THE UPPER AFT CORNER OF THE UNDERLYING SKIN DOUBLER SURROUNDING THE AFT LAV. SERVICE DOOR JAMB. DAMAGE WAS REMOVED AND REPAIR DOUBLER INSTALLED. 2 L 7 2 4F RT A6WE 2003020600124 20030206 00124 NM 2003 2 6 DLM88021322 1 20021114 A 3350 110049 POWER SUPPLY DOUG MD88 MD88 3023688 NM AFT CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 955DL 49886 FOUND EMERGENCY PATH LIGHTS INOPERATIVE FROM ROWS 31 TO 38. REPLACED POWER SUPPLY. CHECKS GOOD. 2 L 7 2 4F RT A6WE 2003020600125 20030206 00125 NM 2003 2 6 DLM88021349 1 20021120 A 3350 6011779 BATTERY DOUG MD88 MD88 3023688 NM OVERWING LIGHTS DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 994DL 53346 RT AND LT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED OVERWING EMERGENCY LIGHT POWER SUPPLY BATTERY AND R2-271 REL AY. 2 L 7 2 4F RT A6WE 2003020600126 20030206 00126 NM 2003 2 6 DLM88021350 1 20021119 A 3350 RPS1 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 910DL 49541 EMERGENCY AISLE LIGHTS FROM ROW 24-30 INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 2 4F RT A6WE 2003020600127 20030206 00127 NM 2003 2 6 DLM88021352 1 20021121 A 2560 P2070004201 CHARGER DOUG MD88 MD88 3023688 NM FLASHLIGHT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 FLASHLIGHT CRADLE AT FWD ENTRY DOOR BROKEN. 2 L 7 2 4F RT A6WE 2003020600128 20030206 00128 NM 2003 2 6 DLM88021357 1 20021121 A 2797 WIRE HARNESS DOUG MD88 MD88 3023688 NM TRIM ACTUATOR DAMAGED A DALA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 SO 27 913DL 2068 49544 PRIMARY TRIM CAUSED A/P AND A/T TO KICK OFF WHEN ACTUATED.CPTS PFD AND NAV DISPLAY BLANKED OUT AND ALL COCKPIT LIGHS DIM MED WHEN TRIM ACTUATED. UPON INSPECTION FOUND WIRE BUNDLE AT PRIMARY AND ALTERNATE TRIM BURNT. SUSPECT WIRES CHAFED DUE TO CONTACT WITH ONE OF PRIMARY ACTUATOR MOUNTING BOLTS. 2 L 7 2 4F RT A6WE 2003020600129 20030206 00129 NM 2003 2 6 DLM88021370 1 20021122 A 2120 ODOR DOUG MD88 MD88 3023688 NM CABIN/COCKPIT DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 938DL 12834 49811 DURING TAKEOFF FLT ATTENDANT REPORTED AN ODOR THROUGHOUT THE CABIN. ODOR WAS EVIDENT ALSO IN COCKPIT. NO ALARMS, NO VI VIBLE SMOKE. CHECKED GALLEYS, NOTHING CAUSING ODOR. APU WAS OFF CROSSFEED CLOSED AND ENGINES AT CLIMB EPR. ODOR DISSA PATED AT 15000 FT AND WAS GONE BY FL310. PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2003020600131 20030206 00131 NM 2003 2 6 DLM88021386 1 20021128 A 3260 833605MODA PSEU DOUG MD88 MD88 3023688 NM E & E BAY MALFUNCTIONED A DALA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 SO 27 978DL 53259 ON LANDING GEAR EXTENSION, DID NOT RECEIVE A GREEN OR RED GEAR POSITION LIGHT. VISUALLY CHECKED (TOWER & PERISCOPE ) LA NDING GEAR FOR SAFE INDICATIONS. ON POWER TRANSFER TO GROUND POWER, GEAR POSITION LIGHTS BECAME GREEN & CYCLED, UNSAFE T WICE ( RED LIGHTS WITH CAWS WARNING). PERFORMED BITE ON PROX BOX. DURING BITE GEAR INDICATION RETURNED TO NOR MAL. GREEN LIGHTS ON. R & R PROX BOX PER MM 32-60-04-02 CHECKS. GOOD. 2 L 7 2 4F RT A6WE 2003020600145 20030206 00145 NM 2003 2 6 DLM88021390 1 20021128 A 3350 FUSE DOUG MD88 MD88 3023688 NM EMERGENCY LIGHTS FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 919DE 53422 FOUND ON L/O AFT EMERGENCY LIGHTS INOPERATIVE. FOUND FUSE F1 OPEN ON B5-212 REPLACED BASE AND FUSE OPEN CHECKS OK 2 L 7 2 4F RT A6WE 2003020600146 20030206 00146 NM 2003 2 6 DLM88021394 1 20021130 A 2910 LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 936DL 49723 LT HYD QTY DECREASED FROM 11 T0 5 QTS AT FL 280. FOUND ELEVATOR PRESSURE TUBE WORN THROUGH AT CLAMP. LOCATED IN TAIL COMPARTMENT LT SIDE. REPLACED LINE LEAK CHECKS OK 2 L 7 2 4F RT A6WE 2003020600148 20030206 00148 NM 2003 2 6 DLM88021401 1 20021202 A 3350 20131A LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 934DL 49721 FOUND EMERGENCY EXIT ROW LIGHTS ROWS 35-38 AND AFT AIRSTAIR DOOR LIGHTS INOPERATIVE. RELAMPED 2 L 7 2 4F RT A6WE 2003020600157 20030206 00157 EA 2003 2 6 A6WA200340008 1 20021215 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 OBLIQUE ANGLES, LEFT AND RIGHT AT FS 625 ARE CRACKED, REMOVED DEFECTIVE 625 OBLIQUE ANGLES, LEFT AND RIGHT SIDES AND INS TALLED NEW ANGLES P/N'S 601-35012-51 AND 601-35012-52 IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2003020600161 20030206 00161 NM 2003 2 6 ASAA0210386 1 20021210 A 5311 6545427505 FRAME BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT BS 662, RIGHT BUTTOCK LINE 69 CORRODED. REPAIRED CHORD PER EA. (M) 2 L 7 2 4F A16WE 2003020600162 20030206 00162 EA 2003 2 6 ASOA02627 1 20021215 A 3350 BM10006002 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 879AS 7600 FLT 4792 - DURING GROUND INSPECTION AT DFW, AN EXTERIOR LEFT SIDE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE EXTERIOR LEFT SIDE EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003020600163 20030206 00163 EA 2003 2 6 ASOA02628 1 20021216 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA K NONE O OTHER DE DESCENT 1 SO 11 883AS 7504 DURING DESCENT INTO DFW AT APPROXIMATELY 11,000 FEET, THE F/O'S SIDE WINDOW, OUTER PANE CRACKED. THE AIRCRAFT LANDED SA FELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE F/O'S SIDE WINDOW. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FO R SERVICE. (M) 2 L 7 2 4F RT A21EA 2003020600164 20030206 00164 EU 2003 2 6 ASOA02630 1 20021217 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 536AS 465 FLT 4212 - DURING GROUND INSPECTION IN ATL, THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT AND EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 7-12 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPE RATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2003020600165 20030206 00165 EU 2003 2 6 ASOA02631 1 20021217 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 536AS 465 FLT 4212 - DURING GROUND INSPECTION IN ATL, THE FORWARD EXIT SIGN OVER THE CABIN DOOR AND THE AFT EMERGENCY EXIT SIGNS W ERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING POWER SUPPLY UNITS. OPERATIONAL C HECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2003020600166 20030206 00166 EA 2003 2 6 ASOA02632 1 20021217 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A ASOA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 11 882AS 7503 FLT 4677 - DURING CLIMB-OUT FROM MCN-ATL, THE LAVATORY SMOKE CAUTION LIGHT ILLUMINATED AND AN ELECTRICAL SMOKE SMELL OCC URRED. THE CAUTION LIGHT EXTINGUISHED. THE CREW COMPLIED WITH THE QRH AND PULLED THE APPROPRIATE CIRCUIT BREAKERS AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE RESET THE ASSOCIATED CIRCUIT BREAKERS. THE WIRING AND CON NECTORS IN THE LAVATORY WERE INSPECTED WITH NO ABNORMALITIES DISCOVERED. THE LAVATORY SMOKE DETECTOR ALSO TESTED GOOD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003020600167 20030206 00167 EA 2003 2 6 ASOA02633 1 20021218 A 3350 B100976 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 703EV 10038 FLT 4315 - DURING GROUND INSPECTION AT MGM, THE NR 3 EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE NR 3 EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003020600168 20030206 00168 SO 2003 2 6 ASOA02634 1 20021219 A 5713 12016085002 STRINGER EMB 120 EMB120RT 3260202 SO RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING HANGAR INSPECTION IN TXK, THE RIGHT WING STRINGER NR 10 CLOSE TO RIB NR 3 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RIGHT WING STRINGER NR 19 CLOSE TO RIB 3 IAW SRM 57-20-03. (M) 2 L 7 2 4T RT A31SO 2003020600169 20030206 00169 EA 2003 2 6 ASOA02635 1 20021219 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 885AS 7521 FLT 4359 - DURING CRUISE AND BEGINNING OF DESCENT INTO ATL, AFTER THE RETARDING THE POWER THE ADVANCING IT AGAIN, A META LLIC/ELECTRICAL TYPE ODOR WAS EMITTED THROUGHOUT THE AIRCRAFT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE PERFORME D HIGH POWER ENGINE RUNS, INSPECTED THE AVIONICS AND AUXILIARY POWER UNIT BAYS. NO ABNORMAL ODORS REOCCURRED. OPERATIO NAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003020600170 20030206 00170 EA 2003 2 6 ASOA02636 1 20021221 A 3350 364911 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 854AS 7382 FLT 4773 - DURING GROUND INSPECTION AT DFW, THE EMERGENCY FLOOR LIGHT AT SEAT 1-C WAS FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE EMERGENCY FLEXIBLE FLOOR LAMP AT SEAT 1-C. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVI CE. (M) 2 L 7 2 4F RT A21EA 2003020600171 20030206 00171 NM 2003 2 6 CALA0200567 1 20021126 A 5347 CARGO TRACK BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27610 27323 INSPECTION FOUND A 7 INCH CRACK IN TIE DOWN RAIL AT STA 807, RBL 14. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53, FIGURE 202. 2 L 7 2 4F RT A16WE 2003020600172 20030206 00172 WP 2003 2 6 CALA0200571 1 20021203 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE AT COCKPIT, FORWARD ENTRY CEILING, AND SERVICE ENTRY CEILING. THE BATTERY POWER SUPPLY WAS REMOVED AND REPLACED AND OPERATION OF THE LIGHTS WAS GOOD. 2 L 7 2 4F A6WE 2003020600173 20030206 00173 NM 2003 2 6 CALA0200573 1 20021205 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND THREE FASTENER HOLES WITH WASHERS THAT HAD WORN INTO THE KEEL BEAM ON LT SIDE I/B OF MLG WHEEL WELL AT STA 699-727. A REPAIR WAS INSTALLED IAW ECRA 5310-03740, REV A. 2 L 7 2 4F RT A16WE 2003020600174 20030206 00174 NM 2003 2 6 CALA0200579 1 20021210 A 5330 SKIN BOEING 737 737524 1384721 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18612 27325 INSPECTION FOUND FUSELAGE SKIN CREASED AT STA 826, S28R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. 2 L 7 2 4F RT A16WE 2003020600175 20030206 00175 NM 2003 2 6 CALA0200587 1 20021215 A 2530 8103060000 OVEN BOEING 737 7373T0 1384582 NM GALLEY MALFUNCTIONED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 14335 23573 FLIGHT ATTENDANTS REPORTED SMOKE COMING FROM BEHIND OVENS IN AFT GALLEY WHILE AT CRUISE EN ROUTE TO CLE. ASSOCIATED CIR CUIT BREAKERS WERE PULLED AND THE SMOKE CEASED. THE FLIGHT WAS CONTINUED TO CLE WHERE IT LANDED WITHOUT FURTHER PROBLEM . MAINTENANCE FOUND THE AFT GALLEY CENTER OVEN AT FAULT. THE OVEN WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE G OOD. 2 L 7 2 4F RT A16WE 2003020600176 20030206 00176 NM 2003 2 6 CALA0200592 1 20021218 A 3150 285T03858 CIRCUIT BOARD BOEING 757 757224 1384958 NM WARNING SYS FAULTY A CALA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SW 09 12109 23301 27299 THE FIRE WARNING BELL SOUNDED CONTINUOUSLY WITH NO OTHER INDICATIONS AFTER TAKEOFF FROM EWR. THE WARNING SILENCED AFTER PULLING AND RESETTING B18 (WARN ELE B) CIRCUIT BREAKERS. THE FLIGHT CONTINUED TO FLL WHERE IT LANDED WITHOUT FURTHER I NCIDENT. NO EVIDENCE OF FIRE WAS FOUND. THE WARNING WAS DETERMINED TO BE A FALSE WARNING. MAINTENANCE REMOVED AND REP LACED THE M1000 MODULE (CIRCUIT BOARD) AT THE P51 WARNING ELECTRONIC UNIT IAW MM 31-51-04, PAGE 401. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A2NM 2003020600181 20030206 00181 NM 2003 2 6 GAIA02165OP 1 20021216 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 854AA 20995 DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE L1 FORWARD ENTRY EMERGENCY EXIT LIGHT WAS INOPERATIVE. RE MOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2003020600187 20030206 00187 NM 2003 2 6 DLM88021409 1 20021205 A 8010 809001043 START VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 958DL 49977 725530 RT ENGINE START VALVE OPEN MESSAGE DURING CLIMB OUT FLT 250. REDUCED ENGINE TO IDLE PER POM, MESSAGE CLEARED. ILLUMINATE D OIL TEMP RT ENGINE 125 DEG VERSUS 85 ON LT. ALL OTHER ENGINE PARAMETRS NORMAL. DIVERTED TO RDU. REPLACED START VALVE . 2 L 7 2 4F 4 F RT A6WE E9NE 2003020600188 20030206 00188 NE 2003 2 6 DLM88021412 2 20021205 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 FAILED A DALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SO 27 938DL 23515 49811 726865 DURING CLIMB THRU FL 240 ENG A/I ON RT ENGINE FAILED N2 0 OIL PRESSURE 0, HYD PRESSURE 0, DISCHARGED FIRE BOTTLE INTO RT ENGINE. REPLACED NR 2 ENGINE 2 L 7 2 4F 4 F RT A6WE E9NE 2003020700001 20030207 00001 NM 2003 2 7 DLM88021428 1 20021210 A 3350 8039001 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 918DE 49959 TWO CEILING EMERGENCY LIGHTS INOP FWD OF AFT CABIN DOOR. REPLACED B5-27 BATTERY PACK POWER SUPPLY AND BATTERIES. LIGH TS NOW OP NML 2 L 7 2 4F RT A6WE 2003020700002 20030207 00002 NM 2003 2 7 DLM88021431 1 20021210 A 5330 59360215 DOUBLER DOUG MD88 MD88 3023688 NM FUSELAGE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 DURING HMV-2, WEAR WAS FOUND ON ALL 4 CORNERS OF THE UNDERLYING SKIN DOUBLER SURROUNDING THE AFT LAV SERVICE DOOR JAMB. THE DAMAGE WAS REMOVED AND DOUBLERS INSTALLED. 2 L 7 2 4F RT A6WE 2003020700003 20030207 00003 NM 2003 2 7 DLM88021439 1 20021214 A 3030 851AH PROBE DOUG MD88 MD88 3023688 NM RUDDER INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 925DL 49712 DURING CRUISE PITOT STATIC HEAT OFF LIGHT CAME ON OAP. CHECKED OHMETER AND FOUND RUDDER LIMITER READING 0. REPLACIN G PITOT PROBE HEATER. 2 L 7 2 4F RT A6WE 2003020700004 20030207 00004 NE 2003 2 7 DLM88021440 2 20021214 A 7510 1058V04002 BLEED VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE MALFUNCTIONED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 905DE 53410 718140 ON TAKEOFF POWER APPLICATION NR 2 ENGINE FAILED TO COME OUT OF IDLE POWER. REPLACED START BLEED CONTROL VALVE PER MM. 2 L 7 2 4F 4 F RT A6WE E9NE 2003020700005 20030207 00005 NM 2003 2 7 DLM88021450 1 20021219 A 2740 SWITCH DOUG MD88 MD88 3023688 NM HORIZONTAL STAB OUT OF ADJUST A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 935DL 49722 STABILIZER CONFIGURATION WARNING. ABORTED TAKE OFF AT 70 KTS. FOUND HORIZONTAL STAB TAKE OFF WARNING SWITCH OUT OF AD JUSTMENT. PERFORMED ADJUSTMENT &TEST PER M/M 27-40-00-05. ALL CHECKS NORMAL NOT RII. OK FOR SERIVCE. 2 L 7 2 4F RT A6WE 2003020700006 20030207 00006 NM 2003 2 7 DLM88021458 1 20021221 A 2432 021904000 BATTERY DOUG MD88 MD88 3023688 NM E&E BAY OVERHEATED A DALA D RETURN TO BLOCK M OVER TEMP TX TAXI/GRND HDL 1 SO 27 963DL 49982 ACRID ODOR AND WHITE SMOKE EMITTING FROM VENT AFT OF NOSE GEAR, UNDER E&E COMPARTMENT. FOUND SHIPS MAIN BATTERIES OVERH EATING. FOUND SHIP`S MAIN BATTERIES OVERHEATING. REMOVED BATTERY & REPLACED LT & RT BATTERY CHARGER & TESTED BOTH THER MAL SENSORS, BOTH OK BUT REPLACED AS PRECAUTION. SYSTEM TESTS OK. 2 L 7 2 4F RT A6WE 2003020700007 20030207 00007 NM 2003 2 7 DLM88021466 1 20021224 A 8012 9794104 VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 916DE 53421 726872 IN CRUISE AT FL330, THE RT START VALVE OPEN LIGHT CAME ON. RAN CHECKLIST, WITH RIGHT ENGINE. AT IDLE THE OIL TEMP ROSE T O 136. AFTER APPROX. 1 MIN THE START VALVE LGHT WENT OFF. WITH THE POWER BACK UP THE LIGHT CAME BACK ON AGAIN. LT ENGINE AT IDLE FOR REMAINDER OF FLIGHT. CHECKED AND RESERVICED STARTER. NO METAL FOUND. REPLACED START VALVE PRECAUTIONARY. SHOOK START VALVE HARNESS AT ENGINE. CHECKS OK. FOUND RT SIDE ENGINE A/I DUCT RUPTURED. REPLACED SAME. 2 L 7 2 4F 4 F RT A6WE E9NE 2003020700008 20030207 00008 NM 2003 2 7 DLM88021471 1 20021226 A 2160 BOOT DOUG MD88 MD88 3023688 NM TEMP CON VALVE TORN A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 979DL 53266 TAIL COMPTARTMENT TEMP HIGH ON CLIMB AT 20,000 FT. LIGHT GOES OUT WHEN REDUCING LT ENGINE POWER. REPLACED TORN BOOT AT RT TEMP CONTROL VALVE AND REPLACED CRACKED DUCT IN TAIL COMPTARTMENT 2 L 7 2 4F RT A6WE 2003020700009 20030207 00009 NM 2003 2 7 DLM88021474 1 20021226 A 4990 PACKING DOUG MD88 MD88 3023688 NM CHIP DETECTOR LEAKING A DALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 944DL 49817 STRONG ODOR IN CABIN WHEN AIRFOIL ANTI ICE SELECTED. FOUND APU INLET CONTAMINATED WITH OIL FROM APU CHIP DETECTOR. REPLACED PACKING ON APU CHIP DETECTOR. PERFORMED OP ON 5088 AND OPN 5089. A/C OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2003020700010 20030207 00010 NM 2003 2 7 DLM88021480 1 20021229 A 3240 26088921 BRAKE ASSY DOUG MD88 MD88 3023688 NM NR 3 BROKEN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 931DL 49718 AFTER PUSHBACK A/C WOULD NOT TAXI. FOUND NR 3 BRAKE BROKEN & SEIZED. REPLACED NR 3 BRAKE AND WHEEL ASSY. 2 L 7 2 4F RT A6WE 2003020700011 20030207 00011 NM 2003 2 7 DLM88021483 1 20021230 A 2912 FILTER DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 903DL 49534 DURING CLIMBOUT OF CVG LEFT HYD QUANTITY AND PRESSURE WENT TO ZERO. FOUND LINE AT THE LT ENGINE HYD FILTER MODULE LE AKING REPLACED SAME SYSTEM NOW CHECKS NORMALLY. 2 L 7 2 4F RT A6WE 2003020700017 20030207 00017 2003 2 7 DLM88030054 4 20020113 A 2565 D29982125 SLIDE DOUG MD88 MD88 3023688 NM R1 DOOR DEPLOYED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 911DL 49542 DURING CATERING OF SHIP 911 FOR FLT 1444/14, THE R1 DOOR SLIDE WAS DEPLOYED. CATERING STATES THAT WHEN THE DOOR WAS OP ENED THE GIRT BAR CAUGHT ON THE INSIDE OF THE DOOR FRAME, HINGE SIDE PULLED THE SLIDE FROM THE BUSSLE WHERE IT THEN FELL ON TO THE CATERING TRUCK AND THEN FELL TO THE GROUND WHERE THE BOTTLE ACTIVATED AND THE SLIDE INFLATED BETWEEN THE AIRC RAFT AND THE FRONT OF THE CATERING TRUCK. NO INJURIES WERE REPORTED NOR DAMAGE TO THE AIRCRAFT OR CATERING TRUCK. REPLA CED SLIDE. 2 L 7 2 4F RT A6WE 2003020700022 20030207 00022 NE 2003 2 7 DLM90021067 2 20020912 A 7530 1685MK7 ACTUATOR DOUG MD90 MD9030 3023690 NM IAE V2500 V2500A1 NE NR 2 ENGINE VSV FAILED A DALA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 910DN 53390 V20073 VSV ACTUATOR HEAD END SEPERATED FROM BODY OF ACTUATOR RESULTING IN LARGE FUEL LEAK. FOUND AT GATE PRIOR TO FLIGHT AFTER ENGINE CHANGE. 2 L 7 2 4F 4 F RT A6WE E311NE 2003020700023 20030207 00023 NM 2003 2 7 DLM90021076 1 20020913 A 3200 833703 PROXIMITY SENSOR DOUG MD90 MD9030 3023690 NM RT MLG W/W INOPERATIVE A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 901DA 53381 GEAR DOOR OPEN ANNUNCIATOR YELLOW WITH LANDING GEAR HANDLE UP AND LANDING GEAR LITES EXTINGUISHED. REPLACED RT GEAR DOO R PROX SENSOR. INDICATIONS CHECK NORMAL. 2 L 7 2 4F RT A6WE 2003020700024 20030207 00024 NM 2003 2 7 DLM90021159 1 20021002 A 3397 WIRE DOUG MD90 MD9030 3023690 NM CABIN CHAFED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 911DA 53391 THE ORIGINAL WRITE UP HAPPENED IN ONTARIO. A/C NOW LOCATED MCI. DURING POWER TRANSFER FROM GROUND POWER TO SHIPS POWER S PARKS SEEN COMING FROM OVERHEAD BIN AT 12 C. AREA INSPECTED NO TROUBLE FOUND IN ONT. UPON ARRIVAL TO MCI PILOTS NOTICED C/B POPPED FOR PASSENGER OVERHEAD LIGHTS AND HANDRAIL LIGHTS ON RT SIDE OF A/C. TECHNICIANS PULLED DOWN OVERHEAD BIN BE TWEEN 12C TO 15 C FOUND WIRES HAD CHAFED ON OVERHEAD BIN SUPPORT BRACKET AT 12C APPROX 1 FT FROM PLUG P5-3410 WIRES REP AIRED AND RELOCATED. 2 L 7 2 4F RT A6WE 2003020700025 20030207 00025 NM 2003 2 7 DLM90021309 1 20021105 A 5330 591024215 SKIN DOUG MD90 MD9030 3023690 NM EMPENNAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 DURING HMV-1, FOUND RAM AIR INLET CRACKED INLET ASSY WAS TOO EXTENSIVE. THEREFORE, A WELD REPAIR WAS DONE. REPAIRED PER ERA 378736+14 2 L 7 2 4F RT A6WE 2003020700026 20030207 00026 NM 2003 2 7 DLM90021314 1 20021112 A 3350 BATTERY PACK DOUG MD90 MD9030 3023690 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 914DN 53394 FWD OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND CHARGER. FAILED DURING OPERATION TEST. NOW TESTS GOO D. 2 L 7 2 4F RT A6WE 2003020700027 20030207 00027 NM 2003 2 7 DLM90021316 1 20021113 A 5510 KSSB2216 BEARING DOUG MD90 MD9030 3023690 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 HORIZONTAL STAB PIVOT BEARINGS CRACKED. FOUND DURING HORIZONTAL STAB PIVOT BEARING FREE PLAY. REPLACED. 2 L 7 2 4F RT A6WE 2003020700028 20030207 00028 NM 2003 2 7 DLM90021317 1 20021114 A 5754 5922500511 STRUCTURE DOUG MD90 MD9030 3023690 NM LE SLAT BIRD STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 905DA 53385 SUBJECT INBOARD LE SLAT WAS FOUND DAMAGED DUE TO BIRD STRIKE, REPAIR PER E/A 417937-14 2 L 7 2 4F RT A6WE 2003020700029 20030207 00029 NM 2003 2 7 DLM90021372 1 20020925 A 7120 29020019 STRUT DOUG MD90 MD9030 3023690 NM ENGINE MOUNT WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 914DN 53394 THE THRUST STRUT WAS FOUND TO HAVE WEAR DAMAGE IN TWO PLACES ON THE STRUT BODY. A TIME LIMITED BLEND REPAIR WAS APPROVED BY A DER. A DTA ASSESSMENT IS REQUIRED TO AUTHORIZE CONTINUED SERVICE BEYOND THE TIME LIMITED REPAIR. 2 L 7 2 4F RT A6WE 2003020700030 20030207 00030 NM 2003 2 7 DLM90021373 1 20020925 A 7120 29020019 STRUT DOUG MD90 MD9030 3023690 NM ENGINE MOUNT WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 914DN 53394 A THRUST STRUT WAS FOUND TO HAVE THREE AREAS OF WEAR DAMAGE BEYOND CMM LIMITS. A DER APPROVED BLEND REPAIR WAS PROVIDED. A DTA ASSESSMENT IS REQUIRED FOR CONTINUED SERVICE BEYOND THE TIME LIMITED REPAIR LIMIT. 2 L 7 2 4F RT A6WE 2003020700031 20030207 00031 NM 2003 2 7 DLM90021374 1 20020925 A 7120 29020019 STRUT DOUG MD90 MD9030 3023690 NM ENGINE MOUNT WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 914DN 53394 A THRUST STRUT WAS FOUND TO HAVE WEAR DAMAGE BEYOND CMM LIMITS. A DER PROVIDED A BLEND REPAIR FOR THE ONE AREA OF DAMAGE . A DTA ASSESSMENT IS REQUIRED FOR CONTINUED SERVICE BEYOND THE TIME LIMITED REPAIR LIMIT. 2 L 7 2 4F RT A6WE 2003020700032 20030207 00032 NM 2003 2 7 DLM90021375 1 20021121 A 7120 29020019 STRUT DOUG MD90 MD9030 3023690 NM ENGINE MOUNT WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 916DN 53396 A THRUST STRUT WAS FOUND TO HAVE EIGHT AREAS OF WEAR DAMAGE BEYOND CMM LIMITS. A DER PROVIDED A BLEND REPAIR. A DTA ASSE SSMENT IS REQUIRED FOR CONTINUED SERVICE BEYOND THE TIME LIMITED REPAIR LIMIT. 2 L 7 2 4F RT A6WE 2003020700033 20030207 00033 NM 2003 2 7 DLM90021403 1 20021201 A 5340 591214185 ATTACH ANGLE DOUG MD90 MD9030 3023690 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 916DN 53396 DURING HMV-1, THE FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE WAS FOUND CRACKED AT CANTED STA 1520.225 AND LONGERON L-2 L. THE HORIZONTAL LEG WAS TRIMMED SIMILAR TO MD80 SRM 53-05-D, FIGURE 23. FILLER WAS ADDED TO THE TRIMMED OUT AREA AND A REPAIR ANGLE INSTALLED. 2 L 7 2 4F RT A6WE 2003020700034 20030207 00034 NM 2003 2 7 QXEA0202293 1 20021222 A 2120 ODOR BOMBDR DHC8 DHC8401 1390041 NM CABIN DETECTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 402QX 4032 MFR-ON FLT NR 2377. BURNING RUBBER SMELLED BY FLIGHT ATTENDANT IN AFT GALLEY AREA NEAR AFT WALL. STRONG SMELL SHORTLY AFTER TAKE OFF THEN DISSIPATED DURING CRUISE, THEN SMELLED AGAIN AFTER AIRCRAFT TOUCHED DOWN. VISUALLY INSPECTED NR 1 & 2 ENGINE NACELLES AND PACKS. NO DEFECTS OR LEAKS OR SMELLS NOTED. GROUND RAN AIRCRAFT 50 PERCENT TORQUE FOR 5 MINUTES AND RAN ENGINE BLEEDS SEPARATELY. COULD NOT DUPLICATE ANY SMELLS. BLEEDS AND ENGINE OPERATE NORMALLY. NO PARTS REPLA CED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003020700035 20030207 00035 EA 2003 2 7 QXEA0202294 1 20021229 A 2820 D98C07606 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 2726 10005 PDX-FUEL LEAKING FROM RIGHT HAND FUEL ENGINE INLET PRESSURE SENSOR. REPLACED NR 2 RIGHT HAND FUEL ENGINE INLET PRESSURE SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2003020700036 20030207 00036 2003 2 7 DLM90021448 4 20021218 A 2565 BOTTLE DOUG MD90 MD9030 3023690 NM ESCAPE SLIDE DISCHARGED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 906DA D9F016 53386 FIRST CLASS GALLEY SLIDE BOTTLE PRESS IS LOW. REPLACED GALLEY DOOR SLIDE PER M/M SYCLED DOOR ARM AND DISARM OK. 2 L 7 2 4F RT A6WE 2003020700037 20030207 00037 NM 2003 2 7 DLM90021482 1 20021223 A 5610 WINDSHIELD DOUG MD90 MD9030 3023690 NM COCKPIT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 RIGHT WINDSHIELD OUTER PANE CRACKED. REPLACED RT WINDSHIELD HEAT CONTROLLER AND WINDSHIELD. 2 L 7 2 4F RT A6WE 2003020700038 20030207 00038 NM 2003 2 7 QXEA0202295 1 20021228 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-MTX REQUESTS REMOVAL AND REPLACEMENT OF RIGHT HAND OUTBOARD NR 10 SEAT TRACK DUE TO CORROSION PITTS. AT STATION X430 , THAT APPEARED TO BE BEYOND BLENDABLE LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2003020700041 20030207 00041 NM 2003 2 7 QXEA0202296 1 20021228 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-CORROSION UNDER RIVET ON OUTBOARD FLANGE OF SEAT TRACK NR 5 25 INCHES AFT OF FORWARD SPLICE. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2003020700042 20030207 00042 NM 2003 2 7 QXEA0202297 1 20021228 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-CORROSION ON RIVET ON INBOARD FLANGE OF SEAT TRACK NR 5, 5.5 INCHES AFT OF FORWARD SPLICE. REPAIRED IAW DHC-8 SRM 5 1-40-11. 2 H 7 2 4T RT A13NM 2003020700043 20030207 00043 NM 2003 2 7 QXEA0202298 1 20021228 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-SEAT TRACK 12 HAS CORROSION 8 INCHES AFT OF SPLICE. REPAIRED IAW RD8-53-3644 AND DHC8 SRM 51-20-26 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2003020700044 20030207 00044 NE 2003 2 7 NACA20020045 2 20020926 A 7421 URHB32E SPARK PLUG DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 13 CYLINDER MALFUNCTIONED A NACA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 99330 285 43576 P33821 THE NUMBER 3 ENGINE STARTED BACKFIRING. REPLACED FRONT AND REAR SPARK PLUG ON NUMBER 13 CYLINDER. 2 L 7 4 4R 4 R 6A3 5E8 2003020700045 20030207 00045 NM 2003 2 7 QXEA0202299 1 20021228 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-LIGHT CORROSION ON NR 4 FLAP TRACK LOWER SURFACE OF LARGE ROLLERS BOTH SIDES LEFT HAND WING. REPAIRED IAW HORIZON A IR EA 2-27-216. 2 H 7 2 4T RT A13NM 2003020700046 20030207 00046 NM 2003 2 7 QXEA0202300 1 20021226 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-PITTING ON OUTBOARD SIDE OF NR 5 FLAP TRACK LEFT HAND WING. REPAIRED IAW HORIZON AIR EA 2-57-217. 2 H 7 2 4T RT A13NM 2003020700047 20030207 00047 NM 2003 2 7 QXEA0202301 1 20021226 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-LIGHT CORROSION ON TOP OF NR 5 FLAP TRACK LEFT HAND WING. REPAIRED IAW HORIZON AIR EA 2-57-217. 2 H 7 2 4T RT A13NM 2003020700050 20030207 00050 NM 2003 2 7 QXEA0202302 1 20021226 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM ELEVATOR MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-ON LEFT HAND ELEVATOR A RIVET IS MISSING OR NOT INSTALLED ON ELEVATOR HORN HEATER MOUNT RIB, TOP INBOARD END OF RIB. REPAIRED IAW DHC-8 SRM 51-20-36 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2003020700051 20030207 00051 NM 2003 2 7 QXEA0202303 1 20021228 A 5522 SKIN DHAV DHC8 DHC8202 2809007 NM ELEVATOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-RIGHT HAND ELEVATOR HAS A GOUGE IN LEADING EDGE SKIN AT STATION YH30.0. REPAIRED IAW DHC-8 SRM 55-20-16, SRM 51-20- 36 AND SRM 27-32-11. 2 H 7 2 4T RT A13NM 2003020700052 20030207 00052 NM 2003 2 7 QXEA0202304 1 20021229 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-RIGHT HAND WING UPPER SURFACE SKIN HAS MULTIPLE SCRATCHES BETWEEN YW190.0 AND YW220.0 JUST AFT OF FRONT SPAR. REPAI RED IAW HORIZON AIR EA 2-57-218 AND DHC-8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 2003020700053 20030207 00053 NM 2003 2 7 QXEA0202305 1 20021228 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-RIGHT HAND WING NR 4 FLAP TRACK IS PITTED, LOWER INBOARD TRACK, LOWER SURFACE. REPAIRED IAW HORIZON AIR EA 2-57-214 AND DHC-8 MM 27-51-11. 2 H 7 2 4T RT A13NM 2003020700055 20030207 00055 NM 2003 2 7 QXEA0202306 1 20021228 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-RIGHT HAND WING NR 4 FLAP TRACK IS PITTED AT LOWER INBOARD TRACK, UPPER SURFACE. REPAIRED IAW HORIZON AIR EA 2-57-2 14 AND DHC-8 MM 27-51-11. 2 H 7 2 4T RT A13NM 2003020700056 20030207 00056 NM 2003 2 7 QXEA0202307 1 20021230 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-REPLACED NR 6 SEAT TRACK. REPLACED IAW RD8-53-4472 AND DHC8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2003020700064 20030207 00064 WP 2003 2 7 NACA20020059 1 20021114 A 3260 5333660500 DOWNLOCK SWITCH DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE RT MLG INTERMITTENT A NACA O OTHER N FALSE WARNING CL CLIMB 1 AL 03 2907F 533265 RIGHT MAIN GEAR INDICATOR DOES NOT SHOW DOWN AND LOCKED. REPLACED RIGHT MAIN DOWN LOCK SWITCH. OP CHECKED GOOD. 2 L 7 4 4R 4 R 6A3 5E8 2003020700073 20030207 00073 NM 2003 2 7 QXEA0202308 1 20021228 A 5230 WEB DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-GOUGED WEB IN 4 PLACES AND ONE RIVET AFT VERTICAL WEB ON CARGO DOOR. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 52-00- 16. 2 H 7 2 4T RT A13NM 2003020700074 20030207 00074 NM 2003 2 7 QXEA0202309 1 20021228 A 5230 WEB DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-GOUGED WEB IN 3 PLACES ON BOTTOM HORIZONTAL LOWER INBOARD ON CARGO DOOR. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 52 -00-16. 2 H 7 2 4T RT A13NM 2003020700076 20030207 00076 NM 2003 2 7 QXEA0202310 1 20021228 A 5230 WEB DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-GOUGED WEB IN 2 PLACES OF FORWARD VERTICAL WEB OF CARGO DOOR. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2003020700077 20030207 00077 NM 2003 2 7 QXEA0202311 1 20021224 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-GOUGED AND WORN 2 EACH DOOR STOPS FOR CARGO DOOR TOP BRACKETS ATTACHED TO APERTURE. REPAIRED IAW DHC-8 SRM 53-40-00 AND SRM 52-30-00. 2 H 7 2 4T RT A13NM 2003020700078 20030207 00078 NM 2003 2 7 QXEA0202312 1 20021228 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX-RIGHT HAND WING NR 4 FLAP TRACK IS PITTED ON THE OUTBOARD SIDE LOAD ROLLER. REPAIRED IAW HORIZON AIR EA 2-57-214 AN D SRM 27-51-11. 2 H 7 2 4T RT A13NM 2003020700079 20030207 00079 NE 2003 2 7 QXEA0202313 2 20021231 A 7261 OIL SYSTEM DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 ENGINE OVERSERVICED A QXEA K NONE W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 374PH 528 PDX ON FLIGHT 2131- FLIGHT ATTENDANT REPORTED A ODOR THAT SMELLED LIKE BURNING OIL IN FORWARD PART OF CABIN AFTER ENGINE START. FOUND NR 1 ENGINE OIL OVER SERVICED APPROXIMATELY 1 QUART. REMOVED EXCESS OIL FROM ENGINE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2003020700081 20030207 00081 NM 2003 2 7 QXEA020267 1 20021118 A 5420 87804069103 PLATE BOMBDR DHC8 DHC8401 1390041 NM NACELLE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 CKB - TRUNNION MOUNT COVER PLATE HAS LARGE GOUGE IN CENTER AND PLATE. REPAIRED IAW DH8S 78-0643 AND EA/6-78-19. 2 H 7 2 4T RT A13NM 2003020700082 20030207 00082 NM 2003 2 7 QXEA020279 1 20021126 A 5320 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 CKB - DENT IN RIGHT HAND FUSELAGE BAY. REPAIRED IAW DH8S-53-0672A AND HORIZON AIR EA 6-53-147. 2 H 7 2 4T RT A13NM 2003020700083 20030207 00083 NM 2003 2 7 QXEA021934 1 20021113 A 5210 SEAL BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR DIRTY A QXEA K NONE J WARNING INDICATION CR CRUISE 1 NM 09 400QX 4030 BZN- FUSELAGE WARNING LIGHT ON IN FLIGHT. WENT OUT WHEN CABIN DIFFERENTIAL DECREASED BELOW 1.0 PSI. AFT PASSENGER DOOR INDICATED UNSAFE. INSPECTED DOOR, CLEANED DOOR SEAL. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003020700084 20030207 00084 NM 2003 2 7 QXEA021941 1 20021113 A 7110 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 414QX 4061 PDX- LEFT HAND VERTICAL CHANNEL IS CRACKED IN LEFT HAND LOWER COWL. REPAIRED IAW Q400 SRM 71-61-01 PAGE 405. 2 H 7 2 4T RT A13NM 2003020700132 20030207 00132 EU 2003 2 7 DHL2002362001 1 20020525 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CARGO BAY WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 362DH 84 CARGO BAY FWD AND AFT SMOKE DETECTORS WON'T TEST. TRANSFERRED TO DMI 9440 PER MEL 26-14-02 CAT C. TROUBLESHOT SYSTEM, RESET BREAKERS ON PANEL 22VU D8, D9, D10. CARGO COMPARTMENT SMOKE DETECTION CHECKED GOOD IAW A300 AMM 26-14-00. DMI#9449 CLEARED, PLACARD REMOVED REF NRC DHL-084-001. 2 L 7 2 4F RT A35EU 2003020700134 20030207 00134 EU 2003 2 7 DHL2002362009 1 20021123 A 2560 ESCAPE REEL AIRBUS 300 A300B4203 3930306 EU COCKPIT BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 RT AFT EMERGENCY DESCENT DEVICE IS BENT. REMOVED AND REPLACED EMERGENCY DESCENT DEVICE IAW A300 AMM 25-61-13. 2 L 7 2 4F RT A35EU 2003020700137 20030207 00137 EU 2003 2 7 DHL2002362011 1 20021210 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE MALFUNCTIONED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 362DH 84 DURING PRE-DEPARTURE CHECK NR 2 ENGINE "B" LOOP WILL NOT TEST. PLACED NR 2 ENGINE "B" LOOP ON DMI #11201 MEL 26-12-01 CAT. "B". REF. DMI 11201. DURING PREDEPARTURE CHECK NR 2 ENGINE "B" LOOP WILL NOT TEST. RESEATED NR 2 ENGINE FIRE AN D OVERHEAT CONTROL UNIT CONNECTOR. OPS CHECKED OK IAW MM 26-12-00. THIS CLEAR DMI 11201. PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2003020700138 20030207 00138 EU 2003 2 7 DHL2002362012 1 20021212 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE INOPERATIVE A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 362DH 84 ENGINE NR 2 FIRE LOOP "B" INOPERATIVE. DEFERRED LOOP "B" ON NR 2 ENGINE IAW MEL 26-12-01-1. DMI 11220. ENGINE NR 2 FI RE LOOP "B" INOPERATIVE. FOUND UNDER PYLON "B" DETECTOR LOOP 26 WD DIRTY AND LOOSE. CLEANED, SECURED, AND CHECKED PER M/M 26-12-12. OPS OK THIS CLEARS DMI 11220. 2 L 7 2 4F RT A35EU 2003020700144 20030207 00144 NE 2003 2 7 QXEA0300014 2 20021230 A 7250 4124T31P03 TURBINE BLADES CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 2 ENGINE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 2981 10023 965284 PDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE HPT 1 BLADE MISSING 20 PERCENT SPAN. REPLACED ENGIN E. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE EN GINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION OF THE HPT1 DAMPNER (ALONG WITH RE-WO RK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2003020700148 20030207 00148 EA 2003 2 7 QXEA0300016 1 20021225 A 5210 RETAINER CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 PDX - THE MAIN CABIN DOOR SEAL RETAINER AND DOOR STRIKER ARE DAMAGED AT LOWER FORWARD CORNER. THE SEAL RETAINER WAS REP LACED AND THE CABIN DOOR SEAL STRIKER WAS REPAIRED IAW EA-R-52-67 AND THE CRJ-700 STRUCTURAL REPAIR MANUAL. 2 L 7 2 4F RT A21EA 2003021000001 20030210 00001 EU 2003 2 10 DHL2002363012 1 20021103 A 3150 WARNING SYSTEM AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 363DH 85 RTO WT. 268,000 LBS., TEMP. +13 DEG. C., SPEED BELOW 60 KTS., PRESSURE ALTITUDE 460 FT. BRAKES HOT LIGHT ILLUMINATED ON TAKE OFF, NR 3 BRAKE TEMPERATURE REACHED 225 DEG. ON ARRIVAL AT GATE "BRAKES HOT" LIGHT WAS NOT ILLUMINATED. VISUAL AND TACTILE INSPECTION ALL NORMAL. COMPLIED WITH MM 05-51-16 NO DEFECTS FOUND. 2 L 7 2 4F RT A35EU 2003021000002 20030210 00002 EU 2003 2 10 DHL2002363013 1 20021126 A 3260 WARNING SYSTEM AIRBUS 300 A300B4203 3930306 EU MLG ACTIVATED A DHLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 363DH 85 NR 6 BRAKE TEMPERATURE INDICATING IN EXCESS OF 700 UPON TAXI-IN. BRAKES HOT ABNORMAL PROCEDURE COMPLETE. BRAKE OVERHEA T INSPECTION ACCOMPLISHED. REPLACED NR 6 MLG TIRE PER MM 12-37-32, NR 6 BRAKE ASSEMBLY PER MM 32-42-27, AND NR 6 TACH GE N. PER M32-42-57. NEED TO REPLACE NR 5 TIRE ON MAIN LANDING GEAR PRECAUTIONARY. REMOVED AND REPLACED NR 5 MAIN WHEEL ASSEMBLY IAW MM 12-37-32. NEED TO ACCOMPLISH BRAKE OVERHEAT INSPECTION OF NR 6 BRAKE AND AXLE ASSEMBLY PER DHL A300 M M 05-51-16. ACCOMPLISHED BRAKE OVERHEAT INSPECTION PER MM 05-51-16 ON NR 6 BRAKE AND AXLE ASSEMBLY. NO FAULTS NOTED. 2 L 7 2 4F RT A35EU 2003021000003 20030210 00003 EU 2003 2 10 DHL2002363014 1 20021206 A 2510 SEAT AIRBUS 300 A300B4203 3930306 EU COCKPIT OUT OF ADJUST A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 CAPTAINS SEAT DOES NOT LOCK IN FWD AND AFT SLIDE POSITION. ADJUSTED SEAT PER M/M REF 25-11-11. OPS CHECKED GOOD. OK TO CONTINUE. 2 L 7 2 4F RT A35EU 2003021000004 20030210 00004 EU 2003 2 10 DHL2002364014 1 20021108 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DENT .220 INCHES AT FRAME 32 LENGTH OF 8 INCHES FWD & 6 INCHES AFT OF FRAME 32 BETWEEN STRINGERS 28LT & 29 LT. PERFORM HFEC INSPECTION; STRINGER HOLES AND EDGE OF DAMAGE CUT OUT. REPAIRS WAS PERFORMED IAW SRM. PERFORM HFEC ON THE LE SK IN COMMON TO THE INBD END RIB IN REWORKED AREA (10-PCS-FASTENER HOLES) LT SIDE. REPAIR AT FUSELAGE FRAME 32 BETWEEN STRINGER 28 LT & 29 LT HAS BEEN PRIMERED BUT REQUIRES TO BE PAINTED. 2 L 7 2 4F RT A35EU 2003021000005 20030210 00005 EU 2003 2 10 DHL2002364016 1 20021218 A 3260 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU BRAKE ASSY FALSE ACTIVATION A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 364DH 141 BRAKE HOT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURE PER AOM. RTO INFORMATION GOM 8.9 PG 13. WT. 305,000, OAT +5 ØC, QNH 30.49. MAINTENANCE NOTED. SUSPECT PROBLEM WITH THE AUTO BRAKE SYSTEM. DEFERRED THE AUTO BRAKE SYSTEM IAW M EL 32-42-07. TESTED AUTO BRAKE SYSTEM PER A300 MM 32-42-54. SYSTEM OPS CHECKED SERVICABLE. THIS CLEARS DMI 11293. 2 L 7 2 4F RT A35EU 2003021000006 20030210 00006 EU 2003 2 10 DHL2002365012 1 20021127 A 3260 CONNECTOR AIRBUS 300 A300B4203 3930306 EU MLG TEMP SENSOR DAMAGED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 365DH 149 RTO BECAUSE OF A HOT BRAKE LIGHT ILLUMINATED ON T/O. 305000 LBS., 70KTS., + 2 DEGREES C, BRAKE TEMPERATURE 190, INCREAS ED TO 270 AFTER ABORT. NR 4 WHEEL HOT PA-107. VISUALLY CHECKED NR 4 BRAKE FOUND OK. JACKED BRAKE UP FOUND OK. NO DRAGGI NG CLEANED AND RESEATED TEMPERATURE SENSOR CONNECTOR - MM 05-51-16. 2 L 7 2 4F RT A35EU 2003021000007 20030210 00007 EU 2003 2 10 DHL2002366015 1 20021105 A 3350 LIGHT AIRBUS 300 A300B4203 3930306 EU CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 366DH 249 FORWARD CABIN RT MAIN CABIN DOOR EMERGENCY LIGHT OUT. RELAMPED RT DOOR EMERGENCY EXIT LIGHT AS PER A-300 MM CHAPTER 33-50-00. 2 L 7 2 4F RT A35EU 2003021000009 20030210 00009 NM 2003 2 10 DHL2002720005 1 20021119 A 2612 CONNECTOR BOEING 727 727228 1384083 NM NR 1 FIRE DETECT LOOSE A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 720DH 19544 ENGINE NR 1 FIRE DETECT SYSTEM "B" LIGHT WILL NOT ILLUMINATE. DEFER SYSTEM "B" PER MEL REF 26-6, CONTROL 11013, PLACA RD INSTALLED. REF. DMI 11013 RESECURED LOOSE CONNECTOR NUT & CLEANED CONNECTOR ON NR 1 ENGINE FIRE DETECTION SYSTEM "B" AND OPS. CHECKED SATISFACTORY PER DHL B-727 M/M 26-11-001. THIS CLEARS DMI 11013. 2 L 7 3 4F RT A3WE 2003021000010 20030210 00010 NM 2003 2 10 DHL2002720006 1 20021119 A 3350 BATTERY BOEING 727 727228 1384083 NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 720DH 19544 ENTRY WAY EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE WITH SWITCH ON. R & R BATTERIES ON EMERGENCY EXIT LIGHT, OPS CK. G OOD IAW BMM 33-50-1 2 L 7 3 4F RT A3WE 2003021000011 20030210 00011 NM 2003 2 10 DHL2002727012 1 20021109 A 2612 SWITCH BOEING 727 727228 1384083 NM APU FIRE DETECT DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 727DH 20204 1) APU FIRE TEST INOPERATIVE. DEFERRED PER MEL 49-1 CAT C DMI 10938 PLACARD INSTALLED. DEFFERED BY 34518. CLEANED FIRE TEST SWITCH, INSPECTED BALANCE OF APU FIRE DETECTION SYSTEM, APU FIRE TEST OPERATES NORMAL IAW GMM 26-15-00, THIS CLEARS DMI 10938 PLACARDS REMOVED MX CONTROL NOTIFIED. 2 L 7 3 4F RT A3WE 2003021000012 20030210 00012 NM 2003 2 10 DHL2002727013 1 20021122 A 2612 BULB BOEING 727 727228 1384083 NM FIRE DETECTION INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 727DH 20204 CARGO AREA FIRE TEST ALL LIGHTS INOPERATIVE. (DO NOT TEST) REPLACED ALL BULBS. OPS. CHECKED, NORMAL IAW 727 JC AI1C26 018. 2 L 7 3 4F RT A3WE 2003021000013 20030210 00013 NM 2003 2 10 DHL2002727015 1 20021205 A 2612 SWITCH BOEING 727 727228 1384083 NM FIRE DETECTION LACK OF LUBE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 727DH 20204 WHEELWELL FIRE TEST INTERMITTENT. LUBED SWITCH. OPS CHECKED GOOD IAW 26-12-00. 2 L 7 3 4F RT A3WE 2003021000014 20030210 00014 NM 2003 2 10 DHL2002741017 1 20021113 A 5210 LATCH BOEING 727 7272Q9 138448M NM DOOR HOLD OPEN LACK OF LUBE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 DOOR OPEN LATCH ON FORWARD ENTRY DOOR IS DIFFICULT TO RELEASE. LUBRICATED "HOLD OPEN" LATCH ON FORWARD ENTRY DOOR. OP S CHECKED GOOD. 2 L 7 3 4F RT A3WE 2003021000015 20030210 00015 NM 2003 2 10 DHL2002741018 1 20021201 A 2697 WIRE BOEING 727 7272Q9 138448M NM OVERHEAT CONNECT LOOSE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 741DH 21931 LOWER AFT BODY OVERHEAT WILL NOT TEST. TRANSFERRED TO DMI LIST IAW MEL 26-10-2 SP APPLY REF. DMI 11103. DOES NOT EFFEC T SAFE OPERATION OF A/C. REF. DMI 11103 / LOWER AFT BODY OVERHEAT WILL NOT TEST. RESECURED WIRE CONNECTORS ON S/W ON OVERHEAT S/W PER 20-60-01. SYSTEM OPS CHECKED GOOD IAW M/M 26-14-0. THIS ACTION CLEARS DMI 11103. 2 L 7 3 4F RT A3WE 2003021000016 20030210 00016 NM 2003 2 10 DHL2002741020 1 20021207 A 5210 STOP BOEING 727 7272Q9 138448M NM PAX DOOR OUT OF ADJUST A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 MAIN ENTRY DOOR DIFFICULT TO CLOSE PROPERLY. MAIN ENTRY DOOR 2ND FROM BOTTOM AFT STOP NOT CONTACTING. ADJUSTED 2ND FRO M BOTTOM AFT ON MAIN ENTRY DOOR OPS CHECKED OK AS PER M/M 52-11-01. 2 L 7 3 4F RT A3WE 2003021000019 20030210 00019 NM 2003 2 10 DHL2002742010 1 20021123 A 2612 CLAMP BOEING 727 727225 1384077 NM FIRE DETECTOR LOOSE A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 742DH 21290 FIRE DETECTOR CIRCUIT GROUND NR 3 LIGHT ILLUMINATED IN FLIGHT. FOUND FIRE DETECTOR LOOP MOUNT CLAMP UNSECURED, RESECUR ED OPS CHECKED GOOD IAW 26-11-01. 2 L 7 3 4F A3WE 2003021000020 20030210 00020 NM 2003 2 10 DHL2002743015 1 20021212 A 2510 SEAT BOEING 727 727225 1384077 NM COCKPIT DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 S/O SEAT NEARLY IMPOSSIBLE TO RELEASE FROM FULL FORWARD POSITION. LUBRICATED S/O SEAT IAW M/M 25-10-41. OPS CHECKED GOO D. 2 L 7 3 4F A3WE 2003021000023 20030210 00023 NM 2003 2 10 DHL2002743502 1 20021108 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, DENT IN FUSELAGE SKIN AT FS 1120 SRT 18RT. CUT-OUT DAMAGE AREA, AND FABRICATED FILLER IAW B-727 SRM 53 -30-3 AND FABRICATED DOUBLER IAW B-727 SRM 53-30-3. ALODINED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED FILLER AND DOUB LER IAW B-727 SRM 51-30-2 AND 53-30-3. 2 L 7 3 4F A3WE 2003021000024 20030210 00024 NM 2003 2 10 DHL2002743503 1 20021109 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, GOUGE IN FUSELAGE SKIN AT FS 1195 STR. 25 LT, CHEMICALLY REMOVED POINT FOR ACCESS IAW B-727 M/M 51-20- 2. BLENDED GOUGE ON FUSELAGE SKIN IAW B-727 SRM 53-30-3 MEASURE DAMAGE AREA AS PER 51-30-1 FABRICATED DOUBLER FOR CUT -OUT IAW B-727 SRM 53-30-3. ALODINED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED COUNTERSINK REPAIR WASHED IAW B-727 SR M 51-30-8. INSTALLED DOUBLER REPAIR IAW B-727 SRM 53-30-3 FIG. 3 AND 51-30-2. 2 L 7 3 4F A3WE 2003021000025 20030210 00025 NM 2003 2 10 DHL2002743504 1 20021108 A 5230 SKIN BOEING 727 727225 1384077 NM CARGO DOOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, C-1 DOOR EXTERIOR SKIN DENTED AT LOWER AFT CORNER. CUT-OUT DAMAGE AREA AND FABRICATED NEW DOUBLER IAW B-727 SRM 52-00-3 TREATED AND PRIMED IAW B-727 SRM 51-10-2. 2 L 7 3 4F A3WE 2003021000029 20030210 00029 NM 2003 2 10 DHL2002743508 1 20021108 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, SEVERAL GOUGES IN FUSELAGE SKIN FS 360 TO 380 STR. 18 LT. DAMAGE FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-3. REMOVED FASTENER AT FUSELAGE SKIN BS 360 TO 380 ABOVE STR 18 LT IAW B-727 SRM 51-30-2. CUT-OUT DAMAGED AR EA IAW B-727 SRM 53-30-3. FABRICATED WASHER REPAIR IAW B-727 SRM 51-30-8. ALODINED AND PRIMED BARE METAL AND PARTS RE PAIR IAW B-727 SRM 51-10-2. INSTALLED DOUBLER, FILLER AND WASHER REPAIR AT FUSELAGE SKIN 360 TO 380, STR 18 LT IAW B-72 7 SRM 53-30-3. 2 L 7 3 4F A3WE 2003021000031 20030210 00031 NM 2003 2 10 DHL2002743509 1 20021112 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, HYDRAULIC SUPPLY LINE CHAFED INTO 1150 FRAME AT STR 20 LT DUE TO CLAMP STAND-OFF BRACKET. CLEANED CHAF ED AREA IAW B-727 SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-10-1. CUT-OUT DAMAGE FRAME IAW B-727 SRM 53- 10-4. AND FABRICATED REPAIR ANGLE IAW B-727 SRM 53-10-2 AND 51-40-3. ALODINED AND PRIMED IAW B-727 SRM 51-10-2 INSTALLE D ANGLE REPAIR IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2003021000033 20030210 00033 NM 2003 2 10 DHL2002743510 1 20021111 A 5754 ANGLE BOEING 727 727225 1384077 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, LT WING LE LOWER STA 130.7 ANGLE CRACKED ABOUT 1 1/2 INCHES LONG. REMOVED NR 3 LT FLAP IAW B-727 MM 2 7-81-1. CUTOFF ANGLE LT WING LE STA. 130.7 IAW B-727 SRM 51-10-3. MADE NEW ANGLE FILLER AND ANGLE REPAIR IAW B-727 SRM 51-40-3. RE-INSTALLED NR 3 LE FLAP IAW B-727 MM 27-81-1. LEAK CHECK GOOD IAW B-727 M.M. 30-13-0. 2 L 7 3 4F A3WE 2003021000037 20030210 00037 NM 2003 2 10 DHL2002743511 1 20021109 A 5310 STRUCTURE BOEING 727 727225 1384077 NM FUSELAGE LIGHTNING STRIKE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, LIGHTNING STRIKE AT FS 198, STR 19 LT. MECHANICALLY REMOVED PAINT FOR ACCESS IAW B-727 M/M 51-20-1. BLEND LIGHTNING STRIKE IAW B-727 53-30-1 FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1. CUT OUT DAMAGED AREA (UPPER SK IN) AND MADE STRUCTURAL FILLER AND REPAIR DOUBLER IAW B-727 SRM 53-30-3 AND 53-30-2. REPAIR PARTS AND BARE METAL ALODIN ED AND PRIMED IAW B-727 SRM 51-10-2. PARTS INSTALLED IAW B-727 SRM 53-30-3. 2 L 7 3 4F A3WE 2003021000038 20030210 00038 NM 2003 2 10 QXEA0300023 1 20021228 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - NR 8 SEAT TRACK HAS TWO LIGHT SCRATCHES IN THE BOTTOM OF THE CHANNEL FROM X505 TO X514. REPAIRED IAW DHC8 RD 8-53 -1339, CHAPTER 4. 2 H 7 2 4T RT A13NM 2003021000039 20030210 00039 NM 2003 2 10 QXEA0300024 1 20021228 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - NR 8 SEAT TRACK HAS LIGHT CORROSION ON TOP OF MOUNT RAILS IN THREE LOCATIONS BETWEEN X510 AND X488. REPAIRED IAW DHC8 RD 8-53-1339, CHAPTER 4. 2 H 7 2 4T RT A13NM 2003021000040 20030210 00040 NM 2003 2 10 QXEA0300025 1 20021228 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - NR 8 SEAT TRACK HAS LIGHT CORROSION IN THE BOTTOM OF THE CHANNEL AT X485. REPAIRED IAW DHC8 RD 8-53-1339. 2 H 7 2 4T RT A13NM 2003021000041 20030210 00041 NM 2003 2 10 QXEA0300026 1 20021228 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - NR 8 SEAT TRACK HAS LIGHT CORROSION ON TOP OF OUTBOARD RAIL AT X484. REPAIRED IAW DHC8 RD 8-53-1339. 2 H 7 2 4T RT A13NM 2003021000042 20030210 00042 NM 2003 2 10 QXEA0300027 1 20021228 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - NR 8 SEAT TRACK HAS LIGHT CORROSION ON RIGHT HAND SIDE BOTTOM OF CHANNEL FROM X484 TO X502. REPAIRED IAW DHC8 RD 8-53-1339. 2 H 7 2 4T RT A13NM 2003021000043 20030210 00043 NM 2003 2 10 QXEA0300028 1 20021228 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - NR 8 SEAT TRACK HAS LIGHT CORROSION ON TOP OF OUTBOARD RAIL FROM X466 TO X461. REPAIRED IAW DHC8 RD 8-53-1339. 2 H 7 2 4T RT A13NM 2003021000044 20030210 00044 NM 2003 2 10 QXEA0300029 1 20021231 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - BOTTOM RIGHT EXTERIOR FUSELAGE SKIN GOUGED APPROXIMATELY 1 INCH, .060 DEEP AT APPROXIMATELY X302.00, 16 INCHES RIG HT OF CENTERLINE. REPAIRED IAW HORIZON AIR EA 2-53-452. 2 H 7 2 4T RT A13NM 2003021000045 20030210 00045 NM 2003 2 10 DHL2002743512 1 20021111 A 7160 DUCT BOEING 727 727225 1384077 NM ENGINE INTAKE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, NR 2 ENGINE INLET "S" DUCT LOWER. ACCESS DOOR, INSIDE INTERIOR DOOR SKIN IS CORRODING PLUS PEELING ALONG DOOR SKIN EDGES. REMOVED CENTER ENGINE INLET ACCESS DOOR IAW B 727 MM 52-40-31. REMOVED INNER SKIN, LOCATED, AND DRILL ED NEW SKIN AS PER SAMPLE IAW B-727 SRM 54-10-2. SKIN ALODINED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 51-30-2. INSTALLED CENTER ENGINE INLET ACCESS DOOR IAW B-727 M.M. 52-40-31. OPS CHECK GOOD IAW B-727 M.M. 52-40-0 . 2 L 7 3 4F A3WE 2003021000046 20030210 00046 NM 2003 2 10 QXEA0300030 1 20021228 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - LEFT HAND OUTBOARD NR 1 SEAT TRACK HAS CORROSION PITTS AT STATION X302, X350 AND X380. REPAIRED IAW DHC-8 SRM 51- 40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2003021000059 20030210 00059 NM 2003 2 10 DHL2002743516 1 20021116 A 5542 SKIN BOEING 727 727225 1384077 NM RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DURING C CHECK, UPPER RUDDER TAB LE SKIN CLOSE OUT IS CRACKED AND CORRODED. REMOVED UPPER RUDDER TAB FOR ACCESS IAW B- 727 M.M. 27-20-11. REMOVED 6 DAMAGED SKINS, LOCATED, AND DRILLED NEW SKINS IAW B-727 SRM 55-40-2. PARTS ALODINED AND P RIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 51-30-2. REINSTALLED TAB IAW B-727 M.M. 27-20-11. INSTALLED UP PER RUDDED TAB IAW B-727 M.M. 27-20-11. OPS CHECK GOOD IAW B-727 M.M. 27-20-0. 2 L 7 3 4F A3WE 2003021000082 20030210 00082 NM 2003 2 10 QXEA0300045 1 20021231 A 7110 FRAME BOMBDR DHC8 DHC8401 1390041 NM LT COWLING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 CKB-LEFT HAND LOWER COWLING REQUIRES PERMANENT REPAIRED FOR CENTRAL STIFFENING FRAME. REPAIRED IAW HORIZON AIR EO 6-71-2 3B AND RD8-4-71-006. 2 H 7 2 4T RT A13NM 2003021000096 20030210 00096 NM 2003 2 10 QXEA0300046 1 20021230 A 7110 FRAME BOMBDR DHC8 DHC8401 1390041 NM RT COWLING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 CKB-RIGHT HAND LOWER COWLING REQUIRES PERMANENT REPAIR FOR CENTRAL STIFFENING FRAME. REPAIRED IAW HORIZON AIR EO 6-71-23 B AND RD8-4-71-006. 2 H 7 2 4T RT A13NM 2003021000098 20030210 00098 NE 2003 2 10 DHL2002743517 2 20021208 A 7321 FUEL CONTROL BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE MALFUNCTIONED A DHLA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION LD LANDING 1 SO 01 743DH 22438 DURING ACCEPTANCE FLIGHT AFTER C CHECK, AFTER LANDING BROUGHT ENGINE INTO REVERSE THRUST. TOOK ENGINE OUT OF REVERSER PU SH THRUST LEVERS FORWARD AND ENGINE NR 3 FLAMED OUT. REMOVED AND REPLACED NR 3 ENGINE FCU AND FUEL PUMP, FUEL HEATER A SSY. OPS AND LEAK CHECK. NORMAL PER M.M. 71-00, 2 L 7 3 4F 4 F A3WE E2EA 2003021000099 20030210 00099 NM 2003 2 10 QXEA0300049 1 20021231 A 5712 RIB BOMBDR DHC8 DHC8401 1390041 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 CKB-RIGHT HAND INBOARD LEADING EDGE OUTBOARD RIB IS CHAFED FROM CLAMP ON FRONT SPAR OF WING. REPAIRED IAW HORIZON AIR EA 6-57-103 AND DHC-57-0704. 2 H 7 2 4T RT A13NM 2003021000100 20030210 00100 NM 2003 2 10 QXEA0300050 1 20021228 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 CKB-LEFT HAND OUTBOARD FLAP HAS CHAFE MARKS ON UPPER FLAP SKIN. REPAIRED IAW HORIZON AIR EA 6-57-102 AND DH8-57-0701. 2 H 7 2 4T RT A13NM 2003021000101 20030210 00101 NM 2003 2 10 DHL2002745013 1 20021106 A 3350 BATTERY BOEING 727 727224 1384076 NM CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 745DH 20665 EMERGENCY EXIT LIGHT AT AIRCRAFT ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED BATTERIES IN EMERGENCY EXIT LIGHT. OPS C HECKED GOOD IAW B727 MM 33-50-00. 2 L 7 3 4F A3WE 2003021000102 20030210 00102 NM 2003 2 10 QXEA0300051 1 20021229 A 5730 SKIN BOMBDR DHC8 DHC8401 1390041 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 CKB-RIGHT HAND CENTER LEADING EDGE FOUR CORNERS ARE CRACKED. REPAIRED IAW HORIZON AIR EA 6-57-101 AND DH8S-57-0700. 2 H 7 2 4T RT A13NM 2003021000103 20030210 00103 NM 2003 2 10 DHL2002745014 1 20021210 A 3350 LIGHT BOEING 727 727224 1384076 NM CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 745DH 20665 FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. OPS CHECKED PORTABLE EMERGENCY LIGHTS IAW DHL B727 M/M 33-50-101. OPS CH ECKED GOOD. 2 L 7 3 4F A3WE 2003021000104 20030210 00104 NM 2003 2 10 QXEA0300052 1 20021229 A 5730 SKIN BOMBDR DHC8 DHC8401 1390041 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 CKB-LEFT HAND CENTER WING LEADING EDGE HAS ALL FOUR CORNERS CRACKED. REPAIRED IAW HORIZON AIR EA 6-57-101 AND DH8S-57-07 00. 2 H 7 2 4T RT A13NM 2003021000105 20030210 00105 NM 2003 2 10 QXEA0300053 1 20021230 A 7110 ANGLE BOMBDR DHC8 DHC8401 1390041 NM LT COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 CKB-REPAIR ANGLE ON SUPPORT FRAME IS CRACKED AT LEFT LOWER COWL. REPAIRED IAW RD8-71-016-117 AND SRM 51-42-05. 2 H 7 2 4T RT A13NM 2003021000115 20030210 00115 NM 2003 2 10 DHL2002745015 1 20021219 A 3260 CONNECTOR BOEING 727 727224 1384076 NM MLG DOOR DIRTY A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 745DH 20665 AFTER TAKE OFF PLACED GEAR HANDLE UP, ALL LIGHTS WENT OFF NORMALLY. WHEN GEAR HANDLE WAS PLACED TO OFF, RED DOOR LIGHT CAME ON FORWARD PANEL, AND RED GEAR DOOR LIGHT ON S10 PANEL CAME ON. PLACED GEAR HANDLE BACK TO UP, AND ALL LIGHTS WENT OFF. GEAR HANDLE BACK TO OFF, AND LIGHTS STAYED OUT. TRANSFERRED TO DMI LOG 11299 PER MEL 32-1 CAT. "C" PLACARDS INSTAL LED. REF. DMI 11299 RED DOOR LIGHT & RT DOOR LIGHT ILLUMINATED IN FLIGHT. REMOVED, CLEANED, AND INSTALLED CONNECTOR P LUG RT MLG DOOR. CYCLED DOOR SEVERAL TIMES OPS CHECKED GOOD IAW MM 32-12-1. THIS CLEARS DMI #11299. PLACARD REMOVED. 2 L 7 3 4F A3WE 2003021000116 20030210 00116 NM 2003 2 10 DHL2002745016 1 20021228 A 7710 LINE BOEING 727 727224 1384076 NM NR 3 ENG EPR CONTAMINATED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 745DH 20665 TAKEOFF REJECTED DUE TO SLOW RESPONDING EPR GAGE ON ENGINE NR 3. TAKE OFF WT. = 137.8, PRESSURE ALTITUDE = 900, OAT = + 8 C, WIND 120 AT 6 KTS. DEFERRED PER MEL 77. CONTROL 11422. ABORT IAS 80 KTS. BRAKE ENERGY ZONE = NORMAL. ALL OTHER ENGINE INDICATIONS NORMAL. TRANSFERRED TO DMI 11422 IAW DHL MEL 77-1. CAT. "C" ITEM. PLACARD INSTALLED. MAINTENANCE CONTROL NOTIFIED. REF. DMI #11422 TAKEOFF REJECTED DUE TO SLOW EPR GAGE ON ENGINE NR 3. BLEW MOISTURE OUT OF EPR LIN ES AND FCU BOWL. RAN NR 3 ENGINE IAW DHL JRH AND B727 M/M 77-11-0. OPS CHECKED GOOD. THIS CLEARS DMI 11422. PLACARD REMO VED. MAINTENANCE CONTROL NOTIFIED. 2 L 7 3 4F A3WE 2003021000118 20030210 00118 NM 2003 2 10 DHL2002746009 1 20021106 A 3350 LIGHT BOEING 727 727224 1384076 NM CABIN LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 EMERGENCY EXIT LIGHT ASSEMBLY LOOSE, FALLS OUT. RESECURED EMERGENCY EXIT LIGHT IAW MM 33-50-00. OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 2003021000120 20030210 00120 NM 2003 2 10 DHL2002746010 1 20021115 A 3040 BLADE BOEING 727 727224 1384076 NM WINDSHIELD WIPER OUT OF ADJUST A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 FIRST OFFICER'S WIPER IS INOPERATIVE. FIRST OFFICER'S WIPER BLADE TENSION HIGH. WIPER ARM PRESSURE ADJUSTED PER MM 3 0-42-42. TESTED SERVICABLE. 2 L 7 3 4F A3WE 2003021000121 20030210 00121 NM 2003 2 10 DHL2002746011 1 20021125 A 2612 BATTERY BOEING 727 727224 1384076 NM FIRE SENSOR DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 746DH 22252 LOWER CARGO FIRE DETECTION FORWARD CARGO INOPERATIVE. TROUBLESHOT AND FOUND SENSORS F15137 AND F15856 LOW BATTERIES. R EMOVED AND REPLACED BATTERIES. GROUND OPS CHECKED NORMAL IAW B727 SUPPLEMENTAL M/M 26-16-01. 2 L 7 3 4F A3WE 2003021000129 20030210 00129 NM 2003 2 10 DHL2002747009 1 20021210 A 2610 WARNING LIGHT BOEING 727 727224 1384076 NM NR 1 ENGINE ILLUMINATED A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 747DH 22253 ON PREDEPARTURE CHECK, NR 1 ENGINE DETECTOR GROUND FAULT LIGHT ILLUMINATED ON CIRCUIT BREAKER PANEL P6-3. CLEANED CONN ECTORS AT THE RESPONDER AND THE TAIL CONNECTOR WITH NO JOY. RESECURED ALL CLIPS ON THE DETECTOR ELEMENTS AND GROUND FAU LT LIGHT WENT OUT. SYSTEM TESTED GOOD PER MM 26-11-00 P501 & 502. 2 L 7 3 4F A3WE 2003021000133 20030210 00133 NM 2003 2 10 DHL2002747011 1 20021217 A 2612 ELEMENT BOEING 727 727224 1384076 NM NR 1 FIRE DETECT OUT OF POSITION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 747DH 22253 ENGINE NR 1 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. DEFERRED IAW MEL 26-9. ASSIGNED CONTROL 11265. PLACARD INSTALL ED. REF. DMI 11265 ENGINE NR 1 DETECTOR CIRCUIT LIGHT ILLUMINATED. REPOSITIONED NR 1 ENGINE FIRE DETECTOR ELEMENT, CLEANED & RESEATED CONNECTOR. OPS CHECKED GOOD IAW MM 26-11-01. THIS CLEARS DMI #11265. PLACARD REMOVED. 2 L 7 3 4F A3WE 2003021000140 20030210 00140 2003 2 10 DHL2002750006 4 20021120 A 3197 WIRE BOEING 727 7272M7 138407S NM WARNING SYSTEM DAMAGED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 750DH 21951 UPON ADVANCING THE THRUST LEVERS, TAKE OFF WARNING SOUNDED, FLAPS 15, TRIM 4.6, AND SPEED BRAKE FULL FORWARD. REPAIRED WIRE TOUCHING TO GROUND AT SWITCH S867 (SPEED BRAKE WARNING S/W) IAW B-727 MM 31-26-26. GROUND OPS. CHECKED NORMAL IAW B-727 M/M 31-26-00. 2 L 7 3 4F A3WE 2003021000141 20030210 00141 NM 2003 2 10 DHL2002752006 1 20021211 A 3040 WINDSHIELD WIPER BOEING 727 727223 1384074 NM WIND SCREEN INTERMITTENT A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 752DH 22466 CAPTAIN'S WINDSHIELD WIPER IS INTERMITTENT. ADJUSTED WIPER TENSION IAW BMM 30-42-01. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2003021000142 20030210 00142 NM 2003 2 10 DHL2002755011 1 20021217 A 3110 BULB BOEING 727 727225 1384077 NM INSTRUMENT PANEL BURNED OUT A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 755DH 21857 AFT CARGO SMOKE INDICATOR ON FORWARD PANEL WILL NOT TEST AS PER AOM. LIGHT WILL NOT PUSH TO TEST EITHER. RESET LAMP ON GLARE SHIELD IAW B-MM 26-16-001. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2003021000144 20030210 00144 WP 2003 2 10 DHL2002801020 1 20021128 A 2510 SEAT DOUG DC8 DC873F 302199F WP COCKPIT LACK OF LUBE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 SECOND OFFICER SEAT DIFFICULT TO SLIDE FORE/AFT. LUBED SECOND OFFICER SEAT, CHECKED OPERATION IAW MM 25-11-6 OK. 2 L 7 4 4F RT 4A25 2003021000147 20030210 00147 WP 2003 2 10 DHL2002803010 1 20021126 A 2510 SEAT DOUG DC8 DC873 302199C WP COCKPIT DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 FIRST OFFICER'S SEAT UNABLE TO MOVE FORE AND AFT. REPLACED COTTER PIN TO FORE AND AFT ADJUSTMENT ON RT SIDE. OPS CHEC KED NORMAL PER M/M 25-11-1. 2 L 7 4 4F RT 4A25 2003021000149 20030210 00149 WP 2003 2 10 DHL2002803541 1 20021023 A 5313 S1616757 LONGERON DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 77211 46123 AFT OF PRESSURE DOME AREA, INTERIOR LONGERON 17 LT AT FS 1766.000 WITH 2 INCH CRACK IN IT PERFORMED MAJOR REPAIR IAW SR M53-1-10. REMOVED DAMAGED LONGERON IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM51-1-8B. INSTALLED NEW LONG ERON IAW SRM51-1-21 & SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2003021000150 20030210 00150 WP 2003 2 10 DHL2002803543 1 20021013 A 5330 SKIN DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 77211 46123 FUSELAGE SKIN CORRODED BETWEEN STA 78.000 AND STA 82.000 , L32 LT TO L33 LT. PERFORMED MAJOR REPAIR IAW EO DHL021002 , ED-3136 , REMOVED FASTNERS IAW SRM51-1-21. REMOVED CORROSION IAW SRM51-1-8, OUT OF LIMITS IAW SRM53-2-0. TRIMMED OUT DA MAGED AREA SKIN SEGMENT IAW ED DHL-021002, ED-3136, FABRICATED ONE REPAIR DOUBLER, THREE INTERNAL FINGER ONE TRIPLER STR AP AND ONE FILLER IAW EO DHL-021002, ED3136. CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B APPLIED PRC TO FAYING SURFACES IAW SRM51-1-15. INSTALLED ONE REPAIR DOUBLER, THREE FINGER DOUBLERS, ONE TRIPLER STRAP AND ONE FILLER IAW EO DHL-02100 2, ED-3136, SRM51-1-21 PG. 1 , SRM 51-1-20D PG. 9 2 L 7 4 4F RT 4A25 2003021000151 20030210 00151 WP 2003 2 10 DHL2002803545 1 20020929 A 5712 RIB DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 77211 46123 LT WING OUTBD LE FORMER AT STA XRS 597.000 WITH 1/2 INCH CRACK IN IT. STOP DRILLED CRACK IAW SRM 57-2-0 PG. 9-10 FABRIC ATED RE-INFORCING ANGLE IAW SRM 57-2-0 PG 9-10 CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 PG. 9-10 SRM51-1-20D 2 L 7 4 4F RT 4A25 2003021000152 20030210 00152 WP 2003 2 10 DHL2002803547 1 20021012 A 5754 PLATE DOUG DC8 DC873 302199C WP LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 77211 46123 RT INBD SLOT LE INTERNAL PLATE WITH 2 INCH CRACK IN IT STA XFS 218.000. REMOVED DAMAGED PLATE IAW SRM 57-2-0 FIG 2 FABR ICATED NEW PLATE IAW SRM57-2-0 FIG. 2. CLEANED ,TREATED AND PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW PLATE IAW SRM 57-2 -0 FIG. 2 2 L 7 4 4F RT 4A25 2003021000153 20030210 00153 NE 2003 2 10 DHL2002804012 2 20021105 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 4 SLOW A DHLA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 01 804DH 46124 RTO A/C WT. 260.0, 9 DEG. C., PRESSURE ALTITUDE SL. ATTEMPTED ROLLING TAKE OFF, NR 4 ENGINE SLOW TO SPOOL. CAPTAIN DECI DED TO RESTART TAKE OFF. AIRSPEED < 20 KTS. 2 L 7 4 4F 4 F RT 4A25 E2GL 2003021000154 20030210 00154 NE 2003 2 10 DHL2002805054 2 20021221 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 1 MALFUNCTIONED A DHLA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 01 805DH 46125 NR 1 ENGINE FAILED TO ACCELERATE ON TAKE OFF. ABORTED AT 60 KIAS., TOGW. 177.0, OAT. -1 DEGREE C., PRESSURE ALTITUDE 116 3. PERFORMED ENGINE CHECK PER JRH ACCELERATION DECELERATION CHECKED OK, POWER MANAGEMENT CONTROL (PMC) CHECK FAILED, PER JRH 13.4 & 15.2, GROUND IDLE CHECK OK. ON ENGINE NR 1 CHECK, NR 1 PMC FAILED PMC CHECK. DEFERRED IAW MEL 73-1 CA T. "C", ASSIGNED DMI 11342, PLACARD INSTALLED. PMC SWITCHED TO OFF POSITION. REF. DMI #11342 ON NR 1 ENGINE CHECK #1 PMC FAILED PMC CHECK. ADJUSTED PMC PER M/M 73-21-30 ON NR 1 ENGINE, ALSO RAN ENGINE NR 1, AND NO PROBLEMS FOUND PER J ET RUN UP BOOK CLEARED DMI 11342. 2 L 7 4 4F 4 F RT 4A25 E2GL 2003021000155 20030210 00155 WP 2003 2 10 DHL2002807011 1 20021124 A 2510 SEAT DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER NR NOT REPORTED 1 SO 01 807DH 45990 CAPTAINS SEAT WHEN IN MOST FOWARD POSITION WILL NOT LOCK. ADUSTED FORE AND AFT LOCK PINS. SEAT CHECKED OK IAW 25-11-1. 2 L 7 4 4F RT 4A25 2003021200001 20030212 00001 NM 2003 2 12 AUS20021447 1 20021220 A 5711 6545324 SPAR BOEING 737 737377 NM CFMINT CFM56 CFM563B1US GL RT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) RT WING REAR SPAR CRACKED AROUND FASTENER HOLE. FOUND DURING INSPECTION IAW ER B73-57-40-17 AND BOEING SB 737-57-1 216. 2 L 7 2 4F 4 F RT A16WE E2GL 2003021200002 20030212 00002 EU 2003 2 12 AUS20021452 1 20021210 A 3260 806002 CIRCUIT BOARD BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502R5 41580 NE MLG FAULTY W O OTHER N FALSE WARNING CL CLIMB 1 AU S (AUS) RT MAIN LANDING GEAR UPLOCK SENSOR PRINTED CIRCUIT BOARD (GJ21) FAULTY. 2 H 7 4 4F 4 F RT A49EU E6NE 2003021200003 20030212 00003 NE 2003 2 12 AUS20021453 2 20021222 A 7200 CFM567B26 ENGINE BOEING 737 737800* NM CFMINT CFM567 CFM567B2US 13802 NE NR 2 BIRD INGESTION W C ABORTED TAKEOFF C R J F.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 AU S 890101 (AUS) NR 2 ENGINE BIRD INGESTION (EGRET) ON TAKEOFF. INSPECTION FOLLOWING OVERWEIGHT LANDING FOUND EVIDENCE OF BIRD INGE STION FOUND ON NR 2 INNER NACELLE, FAN BLADES AND OUTER CORE. ENGINE INLET INSPECTED AND DAMAGE NOTED ON FOUR (4) FAN BL ADES. FAN BLADES 1, 2, 9, 12, 13, 14, 21, AND 24 CHANGED AS MATCHED PAIRS. 2 L 7 2 4F 4 F RT A16WE E2GL 2003021200004 20030212 00004 EU 2003 2 12 AUS20021454 1 20021224 A 2810 D2825003200200 CONNECTOR AIRBUS 320 A320* EU CFMINT CFM56 CFM565A1 NE FUEL SYS FAILED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) REFUEL/DEFUEL CONNECTOR-COUPLING LOCATED IN LT WING FAILED BONDING CHECK IAW SB A320-28-1077 REV 4. 2 L 7 2 4F 4 F RT A46NM E29NE 2003021200005 20030212 00005 EU 2003 2 12 AUS20021456 1 20021228 A 2497 S3200ANA20 WIRE BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502* 41580 EA NR 4 GENERATOR WORN W O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 AU S (AUS) NR 4 GENERATOR DIFFERENTIAL PROTECTION CIRCUIT WIRE XB108 CHAFED IN AREA ADJACENT TO IDG. 2 H 7 4 4F 4 F RT A49EU E6NE 2003021200006 20030212 00006 NM 2003 2 12 AUS20021457 1 20021225 A 3020 32156183 VALVE BOEING 737 737800* NM CFMINT CFM567 CFM567B2US 13802 NE ANTI-ICE SYS UNSERVICEABLE W O OTHER J WARNING INDICATION CL CLIMB 1 AU S 2159 888311 (AUS) LT ENGINE NACELLE ANTI-ICE VALVE UNSERVICEABLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2003021200007 20030212 00007 NM 2003 2 12 AUS20021458 1 20021226 A 2910 272A415117 LINE BOEING 737 737724 13844BY NM CFMINT CFM567 CFM567B2US 13802 NE HYDRAULIC SYSTEM BIRD STRIKE W O OTHER C K J F.O.D. FLUID LOSS WARNING INDICATION LD LANDING 1 AU S (AUS) AIRCRAFT SUFFERED BIRD STRIKE IN AREA OF NOSE LANDING GEAR WHEEL WELL AND NR 2 LEADING EDGE FLAP CAVITY. BIRD DAMA GED RIGID HYDRAULIC PIPE PN 272A415117 LOCATED BETWEEN NLG MANIFOLD AND LOCK ACTUATOR. HYDRAULIC FLUID LEAKING. 2 L 7 2 4F 4 F RT A16WE E2GL 2003021200008 20030212 00008 NM 2003 2 12 AUS20021459 1 20021227 A 2913 10621672 PUMP BOEING 737 737724 13844BY NM CFMINT CFM567 CFM567B2US 13802 NE HYDRAULIC PUMP MISINSTALLED W O OTHER W J B INADEQUATE Q C WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AU S 7688 (AUS) NR 2 ENGINE HYDRAULIC PUMP FAULTY. INVESTIGATION FOUND THAT THE PUMP CASE DRAIN CHECK VALVE HAD BEEN FITTED BACK T O FRONT AND THE HOSE FROM THE CASE DRAIN TO THE PYLON COLLAPSED. HYDRAULIC PUMP SEVERELY OVERHEATED. PERSONNEL/MAINTENAN CE ERROR. 2 L 7 2 4F 4 F RT A16WE E2GL 2003021200009 20030212 00009 2003 2 12 AUS20021466 4 20021224 A 6122 8210310 GOVERNOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4MP3 GL PROPELLER FAULTY W O OTHER O OTHER NR NOT REPORTED 1 AU S 107 (AUS) LT ENGINE PROPELLER GOVERNOR FAULTY. SUSPECT CAUSED BY STICKING PILOT VALVE. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 2003021200011 20030212 00011 NM 2003 2 12 AUS20021479 1 20021221 A 5414 PANEL BOEING 767 767330 NM RROYCE RB211 RB211524* NE ENGINE NACELLE MISSING W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) NR 1 ENGINE ACOUSTIC PANEL LOCATED ON THE OUTBOARD SIDE IMMEDIATELY BEHIND FAN IS MISSING. PANEL WAS NOT FROM THE ICE IMPACT AREA. 2 L 7 2 4F 4 F RT A1NM E12EU 2003021200012 20030212 00012 SW 2003 2 12 AUS20021483 1 20021118 A 5310 T210 STRUCTURE SWRNGN SA226 SA226T 8780122 SW GARRTT TPE331 TPE3313U 01514 WP HARTZL HCB3T HCB3TN5 GL NLG AREA DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) PILOT COMPLAINED THAT THE NLG GREEN LIGHT WAS TAKING A LONG TIME TO ILLUMINATE. INVESTIGATION THEN FOUND EVIDENCE OF A HEAVY LANDING. INVESTIGATION FOUND THE FOLLOWING DEFECTS: NOSE GEAR STARBOARD KEELSON BUCKLED AND CRACKED FOR APPR OXIMATELY 127MM (5IN), BOTH LOWER KEELSON BUCKLED, NOSE LOCKER LOWER FORWARD CORNERS DEFORMED, RT WINDSHIELD DELAMIN ATED, BOTH ENGINES SHOW EVIDENCE OF NODDING' DURING LANDING, AND WING CENTRE SECTION LEAKING FUEL. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C P15EA 2003021200013 20030212 00013 EU 2003 2 12 AUS20021486 1 20020922 A 6410 109813201111 BLADE AGUSTA A109 A119 0261102 EU PWA PT6 PT6B36 52043 EA TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S 22 (AUS) TAIL ROTOR BLADE CRACKED. MANUFACTURER STATES THAT CRACKING IS CAUSED BY SLIPPAGE OF THE GLUE BETWEEN THE FINGER D OUBLER AND THE BLADE SKIN. 1 G 7 2 3U 4 U H7EU E4EA 2003021200014 20030212 00014 EU 2003 2 12 AUS20021487 1 20020929 A 6410 109813201111 BLADE AGUSTA A109 A119 0261102 EU PWA PT6 PT6B36 52043 EA TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) TAIL ROTOR BLADE CRACKED. MANUFACTURER STATES THAT CRACKING IS CAUSED BY SLIPPAGE OF THE GLUE BETWEEN THE FINGER D OUBLER AND THE BLADE SKIN. 1 G 7 2 3U 4 U H7EU E4EA 2003021200015 20030212 00015 EU 2003 2 12 AUS20021488 1 20021009 A 6410 109813201111 BLADE AGUSTA A109 A119 0261102 EU TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) TAIL ROTOR BLADE CRACKED. MANUFACTURER STATES THAT CRACKING IS CAUSED BY SLIPPAGE OF THE GLUE BETWEEN THE FINGER D OUBLER AND THE BLADE SKIN. 1 G 7 2 3U H7EU 2003021200016 20030212 00016 EU 2003 2 12 AUS20021489 1 20021020 A 6410 109813201111 BLADE AGUSTA A109 A119 0261102 EU TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) TAIL ROTOR BLADE CRACKED. MANUFACTURER STATES THAT CRACKING IS CAUSED BY SLIPPAGE OF THE GLUE BETWEEN THE FINGER D OUBLER AND THE BLADE SKIN. 1 G 7 2 3U H7EU 2003021200037 20030212 00037 EU 2003 2 12 CA021227002 1 20021212 A 2530 4110001XXX COFFEEMAKER AIRBUS 330 A330342 EU RROYCE RB211 RB211TRENT77 NE GALLEY ODOR W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA (CAN) A/C ARRIVED ON A TURN AROUND AT YYZ. CREW INFORMED MTCE THAT THEY SMELLED SOMETHING BURNING IN THE AFT GALLEY. MTC E ISOLATED THE ODOR TO THE AFT LT GALLEY UNIT, NR 1 & 2 COFFEEMAKERS. THE COFFEEMAKERS WERE REMOVED FOR INSPECTION. MTCE FOUND THAT THE SHELF COMPARTMENT FLOOR ON WHICH THE COFFEEMAKERS SAT, SHOWED EVIDENCE OF OVERHEATING. THIS IS MOST LIKE LY DUE TO THE PROXIMITY OF THE COFFEEMAKER BOILER PLATE TO THE COMPARTMENT FLOOR. AT ALL COFFEEMAKER LOCATIONS IN THE G ALLEY, A DOUBLER WAS INSTALLED ON THE HONEYCOMB PANEL IAW CFT CMM 25-31-95. 1 L 7 2 4F 4 F RT A46NM E39NE 2003021200039 20030212 00039 SW 2003 2 12 CA030106009 1 20021231 A 2910 2781006475 LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL HYD SYSTEM CHAFED W O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CA (CAN) AIRCRAFT EXPERIENCED A LOSS OF HYDRAULIC FLUID AND PRESSURE IN FLIGHT. EMERGENCY EXTENSION CARRIED OUT WITH A SAFE LANDING. CHAFED HYDRAULIC LINES FOUND RUBBED THROUGH BY PLASTIC DRAIN LINE IN LT NACELLE. HYDRAULIC LINES FOUND CHAFED WERE PN 2781006475 AND 2781032233 AND 2781032626. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2003021200041 20030212 00041 SO 2003 2 12 CA030108002 1 20021210 A 2421 BOLT PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA HARTZL HCE2Y HCE2YR2 GL ALTERNATOR LOOSE W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 CA (CAN) ALTERNATOR FAILED IN FLIGHT. INSPECTION AFTER THE NACELLE DOORS WERE OPENED REVEALED THAT THE FORWARD BOLT, WHICH HOLDS THE ALTERNATOR, BECAME LOOSE AND WAS FOUND BETWEEN THE STARTER AND RING GEAR ASSEMBLY. THE DRIVE BELT WAS OFF AND THE RING GEAR WAS CRACKED. PROP WAS REMOVED AND THE RING GEAR AND DRIVE BELT WERE REPLACED. 1 L 7 2 3O 3 O 1A10 1E4 5 C P9EA 2003021200045 20030212 00045 NM 2003 2 12 DHL200278001A 1 20020804 A 5312 BULKHEAD BOEING 727 727223 1384074 NM FUSELAGE CRACKED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 780DH 22006 WEB CRACKED AT STA 870 LOWER RT CORNER OF APU LOAD CONTROL VALVE. STOP DRILLED CRACK, HFEC INSPECTED AREA, CRACK TERMIN ATES AT STOP DRILL. FABRICATED DOUBLERS IAW 727 SRM 53-10-9. TREATED, PRIMED AND INSTALLED PARTS. 2 L 7 3 4F A3WE 2003021200049 20030212 00049 NM 2003 2 12 CA030109003 1 20021014 A 3010 4100S005001 VALVE BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA DUAL DISTRIBUTIN MALFUNCTIONED W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) INTERMITTENT FAULT: DURING CLIMB IN ICING CONDITIONS, CAUTION LIGHT CAME ON AGAIN. CHECKLIST PERFORMED. OPERATED IN MANUAL MODE IT CAME BACK TO NORMAL AFTER 10 MIN OF OPERATION. BOOT SEQUENCING CONTROL WAS BAD. SOMETIMES A LOT OF BOO TS CAME ON AT THE SAME TIME (UNABLE TO DEFLATE AFTER A CYCLE) AND SOMETIMES THE BOOTS NEVER CAME ON. AFTER THE 10 MIN PE RIOD SYSTEM BACK TO NORMAL AND OPERATED FOR MORE THAN 30 MIN WITHOUT ANY CAUTION LIGHT OR FAILURE. DURING DESCEND SAME F AILURE WITH ACCOMPANIED CAUTION LIGHT. CONDITION SUSTAINED FOR APPROXIMATELY 10 MIN UNTIL LANDING IN NON-ICING CONDITIO NS . CHECK LIST WAS AGAIN PERFORMED AND OPERATION IN MANUAL MODE WHICH WAS NOT POSSIBLE TO CONTROL. TWO DDV'S (DUAL DIST 2 H 7 2 4T 4 T RT A13NM E00062EN 2003021200057 20030212 00057 GL 2003 2 12 CA030115004 2 20021209 A 7310 AN21220D FITTING CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13D 03004 GL FUEL MANIFOLD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) A HOSE ASSY (390A20D4.8) FROM A FUEL SUPPLY MANIFOLD WAS REMOVED AND ROUTED TO OUR INTERNAL OVERHAUL SHOP FOR REPL ACEMENT OF THE HOSES. UPON DISASSEMBLY, IT WAS DISCOVERED THAT ONE FITTING (AN212-20D) WAS CORRODED AND CRACKED LONGITUD INALLY ON ONE SIDE WHERE THE FIRE SLEEVE COVERS THE FITTING. IT WOULD APPEAR THAT THE FIRE SLEEVE TRAPPED MOISTURE AND T HUS CORRODED THE FITTING. 2 L 7 2 4R 4 T 6A6 E282 2003021200059 20030212 00059 NE 2003 2 12 CA030115008 2 20021223 A 8530 399353 CYLINDER DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE ENGINE CRACKED W O OTHER O OTHER NR NOT REPORTED 1 CA (CAN) NR 7 CYLINDER CRACKED BETWEEN NR 2 & 3 LOWER HEAD FINS. 1 H 7 1 3R 3 R A806 5E1 2003021200063 20030212 00063 NE 2003 2 12 CA030116005 2 20021126 A 7260 SHAFT AIRBUS 330 A330342 EU RROYCE RB211 RB211TRENT77 NE ENGINE CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) UPON A/C ARRIVAL IN YVR, NR 2 ENGINE HAD AN OIL LEAK. EXTERNAL GEARBOX DRIVE SHAFT SHROUD FOUND CHAFED THROUGH BY THE FUEL DRAIN TUBE. MTCE REPLACED THE DRIVESHAFT IAW AMM 72-62-11. ENGINEERING INITIATED A FLEET CAMPAIGN REVISING AN S I 5-72-004 REV 01. THE FLEET CAMPAIGN REVEALED 3 ENGINES WITH CHAFING FINDINGS AND CORRECTED IAW THE SI. ROLLS ROYCE WAS MADE AWARE OF THE SITUATION. THIS CHAFING BETWEEN THE DRIVE SHAFT AND FUEL DRAIN TUBE WAS DUE TO AN INCORRECT INSTALLAT ION OF A SPACER TO CLAMPS NOT BEING INSTALLED IN THE CORRECT ORDER. 1 L 7 2 4F 4 F RT A46NM E39NE 2003021200091 20030212 00091 EU 2003 2 12 CA030120004 1 20021222 A 2750 CONTROL UNIT AIRBUS 320 A320212 3930322 EU CFMINT CFM56 CFM565A3 NE TE FLAPS MALFUNCTIONED W L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) ON APPROACH WHEN FLAPS WERE SELECTED FROM 1 TO 2, AN ECAM WARNING 'FLT CTL FLAPS LOCKED' APPEARED. APPROACH WAS DI SCONTINUED, AND A/C WAS MANOEUVRE D IN THE VICINITY OF AIRPORT WITH ATC CONCURRENCE AS THE 'LANDING WITH FLAPS JAMMED' C HECKLIST WAS ACTIONED. ONCE THE CHECKLIST WAS COMPLETED, AN EMERGENCY DECLARED AND APPROACH COMPLETED WITHOUT INCIDENT. FLAP/SLAT SYS CHECKED IAW TSM 27-51-00. NO FAULTS FOUND. FLAP OPS. CHECKED NO FAULT GVI CARRIED OUT. ALL SYS NORMAL. CF DS SYSTEM SHOWED NO FAULT WITH SLAT/FLAP SYSTEM. A HYD PRESS FLUCTUATION WAS REGISTERED AT THE TIME OF THE LOCK-OUT. SUS PECT OUT-OF-SEQUENCE LANDING GEAR EXTENSION WITH FLAP EXTENSION. THE FAULT HAS NOT RE-OCCURRED SINCE 22 DECEMBER 2002. 2 L 7 2 4F 4 F RT A28NM E29NE 2003021300003 20030213 00003 EU 2003 2 13 CA030121002 2 20020726 A 8530 854116 EXHAUST VALVE ROTAX DIAMON DA20 DA20A1 2990000 GL ROTAX 912 ROTAX912S3 EU NR 2 CYLINDER BROKEN W A UNSCHED LANDING E R Y VIBRATION/BUFFET PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CL CLIMB 1 CA (CAN) EXHAUST VALVE IN NR 2 CYLINDER BROKEN AT AREA BETWEEN STEM AND HEAD OF VALVE. VALVE DROPPED INTO COMBUSTION AREA A ND CAUSED PISTON DAMAGE AND EVENTUALLY ENGINE STOPPAGE. VALVE TRAIN COMPONENTS WEAR CONSISTENT WITH IMPROPER PURGING OF LIFTERS AS ADDRESSED BY SB-912-036. DAMAGE TO NR 3 CYLINDER EXHAUST VALVE AND VALVE SEAT INDICATE THIS CYLINDER WAS SUF FERING THE SAME MANNER. 1 L 7 1 3O 3 O NT TA4CH E00051EN 2003021300006 20030213 00006 EA 2003 2 13 CA030121006 2 20021112 A 7532 54009494 BLEED VALVE BOMBDR DHC8 DHC8400 NM PWC 150 PW150A EA ENGINE FAILED W O OTHER J WARNING INDICATION DE DESCENT 1 CA (CAN) NR 2 ENGINE FADEC CAUTION LIGHT ON DURING DESCENT TO BASE, ALSO POWERPLANT MESSAGE ON ED. QRH APPLIED. P 2.2 BLEE D VALVE WAS REPLACED IN ACCORDANCE WITH AMM TASK 75-31-11, PROBABLY DUE TO FAULT CODE 912 (AND 918). P2.2 VALVE OUT S/N GA1035 AND IN S/N GA1061. 2 H 7 2 4T 4 T RT A13NM E00062EN 2003021300010 20030213 00010 EA 2003 2 13 CA030122008 2 20020926 A 8530 CL12CN CYLINDER CESSNA 172 172RG 2072438 CE LYC O360 O360F1A6 41514 EA MCAULY 2D34C B2D34C220 GL NR 3 CRACKED W O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA (CAN) ENGINE RUNNING ROUGH. VISUAL INSPECTION OF ENGINE WAS DONE. FOUND NR 3 CYLINDER CRACKED FROM LOWER SPARK PLUG UP T O UPPER SPARK PLUG ON REAR SIDE. WHEN ENGINE WAS TORN DOWN, IT WAS FOUND THAT A COUNTERWEIGHT BUSHING WAS WORN PAST SERV ICE LIMITS. CRANKSHAFT GEAR AND ONE IDLER GEAR WAS WORN PAST LIMITS AS WELL. ENGINE SHOP SUGGESTED WE GET THE PROPELLER CHECKED. FOUND THAT THE PROPELLER WAS OUT OF BALANCE. THIS IS WHAT PROBABLY CAUSED THE COUNTERWEIGHT BUSHING TO WEAR OUT . 1 H 7 1 3O 3 O 3A17 E286 5 C P7EA 2003021300014 20030213 00014 CE 2003 2 13 CA030123006 1 20021231 A 3250 5082003419 LINK BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA MCAULY 4HFR34 4HFR34C754 NE NLG STEERING FAILED W D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 CA 14068 (CAN) PILOT PROCEEDED TO TAXI AIRCRAFT, THE NOSE STEERING SYSTEM LOCKED INTO A HARD RT CONDITION. THIS ALSO AFFECTED THE RUDDER SYSTEM, POSITIONING THE RUDDER SYSTEM INTO A RT TURN CONDITION. A TOW BAR WAS ATTACHED AND THE NOSE STEERING SYS TEM EXERCISED, THIS RESULTED IN RELEASING THE NOSE STEERING SYSTEM / RUDDER CONTROL. NOSE STEERING LINK WAS REMOVED, DI SASSEMBLED, INSPECTED, LUBRICATED, REASSEMBLED AND REINSTALLED. INSPECTION OF STEERING LINK DID NOT REVEAL ANYTHING CONC LUSIVE. A DETAILED INSPECTION OF THE RUDDER CONTROL SYSTEM DID NOT REVEAL ANY PROBLEMS. AS A PRECAUTION THE STEERING LI NK FORWARD ROD ASSEMBLY WAS REPLACED. 1 L 7 2 4T 4 T A24CE E4EA 6 C 3PNE 2003021300052 20030213 00052 CE 2003 2 13 CA030205012 1 20020203 A 3234 66323020010 CONTROL VALVE LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP MLG FAILED W O OTHER J WARNING INDICATION CL CLIMB 1 CA (CAN) LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. REPLACE CONTROL VALVE. 2 L 7 2 4F 4 F RT T00008WI E6WE 2003021300066 20030213 00066 WP 2003 2 13 0204139931 1 20021214 A 3260 SWITCH DOUG DC9 DC931 3022065 WP PWA JT8 JT8D1 52044 NE MLG INOPERATIVE A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 90S 47244 ON CLIMBOUT ALL THREE (GEAR UNSAFE) LIGHTS ILLUMINATED. ALL OTHER INDICATIONS NORMAL. ON GEAR EXTENSION GOT ALL GREEN LI GHTS ILLUMINATED AND (GEAR UNSAFE) LIGHT EXTINGUISHED. ALL OTHER INDICATIONS NORMAL. FLIGHT LANDED WITHOUT INCIDENT. REP LACED SWITCH ASSEMBLY. GEAR OPERATION CHECKS GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2003021300085 20030213 00085 NM 2003 2 13 2002UALA01886 1 20021221 A 2421 IDG BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT GENERATOR FAILED A UALA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 WP 29 213UA 30219 VIA SATFONE, CAPT ADVISED HE LOST THE RT GENERATOR. RT GENERATOR WENT OFF LINE WITH NO EICAS MESSAGE OR COCKPIT INDICAT ION EXCEPT RT GEN "OFF" LIGHT. ATTEMPT TO RESET WAS UNSUCCESSFUL. SUPPLEMENTAL DATA UPDATE THERE WAS AN ASSOCIATED MESS AGE 24-12092 POWER BUS (RT MAIN AC BUSS) IN P200 IS NOT POWERED] SHOWN INACTIVE/INTERMITTENT. THE RIGHT IDG WAS REPLACE D AND OPERATIONAL CHECKED NORMAL. THE ENROUTE VERIFICATION FLIGHT WAS ALSO ACCOMPLISHED. CAUSE OF IDG FAILURE TO BE C ONFIRMED UPON EXAMINATION OF IDG.. 2 L 7 2 4F 4 F RT T0001SE E46NE 2003021300090 20030213 00090 WP 2003 2 13 2003F00006 1 20021217 A 2560 2463 PANEL LKHEED 1011 10113851 5265010 WP L1 DOOR INOPERATIVE G K NONE L NO TEST IN INSP/MAINT 1 GL 11 186AT 193C1074 (ORIG-CLOSED) DURING SCHEDULED MAINTENANCE EVAC SIGNAL PANEL AT L1 DOOR HAS NO AURAL SIGNAL. MAINTENANCE REMOVED AND RE PLACED EVAC SIGNAL PANEL IAW MM, OPERATIONAL CHECK GOOD. 2 L 7 3 4F A23WE 2003021300091 20030213 00091 WP 2003 2 13 2003F00013 1 20021222 A 3350 5165741 CHARGER LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 198AT 193B1111 R1 DOOR EXTERIOR EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED R1 DOOR POWER PACK IAW MM. 2 L 7 3 4F A23WE 2003021300105 20030213 00105 2003 2 13 2003F00076 4 20021230 A 2565 GIRT BAR LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211* 54555 NE PAX DOOR OUT OF ADJUST G AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 163AT 1229 L-1 DOOR WILL NOT DISARM FROM INSIDE THE AIRCRAFT. ADJUSTED GIRT BAR IAW MM. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F 4 F A23WE A12EU 2003021300106 20030213 00106 WP 2003 2 13 2003F00077 1 20021227 A 2120 ENGINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 2 LEAKING G AMTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 11 163AT 66081 66081 1229 14609 STRONG KEROSENE ODOR EMANATES THROUGHOUT AIRCRAFT DURING DECENT AND APPROACH. REMOVED AND REPLACED NR 2 ENGINE IAW MM. 2 L 7 3 4F 4 F A23WE E12EU 2003021300115 20030213 00115 WP 2003 2 13 ASA0280428 1 20021020 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 160-200, LBL 54. REPLACED SUPPORT PER SRM 53-14-1, FIG 11, A ND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003021300116 20030213 00116 NM 2003 2 13 ASAA0210387 1 20021211 A 5330 6552988535 SKIN BOEING 737 7372Q8C 138448S NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND FUSELAGE SKIN AT BS 947, STRINGER 17L DENTED. REPAIRED FUSELAGE SKIN PER EA. (M) 2 L 7 2 4F A16WE 2003021300117 20030213 00117 NM 2003 2 13 ASAA0210388 1 20021211 A 5310 6547959502 DOOR FRAME BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND AFT CARGO DOOR FRAME AT BS 790-794, STRINGER 23R-26R CORRODED. REMOVED CORROSION AND REPAIRED CARGO DOOR FRAME PER SRM. (M) 2 L 7 2 4F A16WE 2003021300118 20030213 00118 WP 2003 2 13 ASAA0280371 1 20021016 A 5347 3957317501 FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, TIE DOWN FITTING CORRODED IN AFT CARGO BAY FS 1153 BETWEEN LONGERON 30-29R. REPLACED FITT ING PER SRM 51-10-3. (M) 2 L 7 2 4F RT A6WE 2003021300119 20030213 00119 WP 2003 2 13 ASAA0280372 1 20021016 A 5320 593795421 SUPPORT BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, AFT AIRSTAIR CEILING PANEL SUPPORT BRACKET HAS FASTENER HOLE BROKEN OUT. REPLACED SUPPORT BRACKE T ASSEMBLY PER SRM 51-30-1. (M) 2 L 7 2 4F RT A6WE 2003021300120 20030213 00120 WP 2003 2 13 ASAA0280408 1 20021019 A 5311 9957139511 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FRAME CORRODED AT FS 1287 BETWEEN LONGERON 29L AND 29R. REPLACED FRAME PER SRM 53-03, FIG 2A. (M) 2 L 7 2 4F RT A6WE 2003021300121 20030213 00121 WP 2003 2 13 ASAA0280410 1 20021020 A 5320 3932140 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, MAIN CABIN FALSE TRACK IS CORRODED AT FS 160-200, LBL 9. REPLACED FALSE TRACK PER SRM 53-14-1, F IG 11 AND 53-30-5. (M) 2 L 7 2 4F RT A6WE 2003021300122 20030213 00122 WP 2003 2 13 ASAA0280411 1 20021021 A 5210 9955763417 DOOR FRAME DOUG DC9 DC983 3022083 WP L1 DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, LEFT PAX L1 DOOR INTERNAL FRAME IS CRACKED BEHIND INNER DOOR HANDLE. REPLACED FRAME PER S RM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003021300123 20030213 00123 WP 2003 2 13 ASAA0280412 1 20021021 A 5720 9936314502 STRAP DOUG DC9 DC983 3022083 WP RT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, RIGHT WING LEADING EDGE SPLICE STRAP IS CRACKED AT STATION XRS 164, XFS 299. REPLACED SPLICE PER SRM 57-32-1, 51-10-4, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003021300124 20030213 00124 WP 2003 2 13 ASAA0280414 1 20021021 A 5310 993607488 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, SHEAR TIE CORRODED AT FS 1150, LONGERON 29L-29R. REPLACED SHEAR TIE PER SRM 53-14-3 AND 5 1-30-5. (M) 2 L 7 2 4F RT A6WE 2003021300125 20030213 00125 WP 2003 2 13 ASAA0280416 1 20021019 A 5320 993061219 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, CUSP WEB CORRODED AT FS 1250-1271, LONGERON 18R. REPAIRED PER SRM 51-70-4, FIG 2. (M) 2 L 7 2 4F RT A6WE 2003021300126 20030213 00126 WP 2003 2 13 ASAA0280419 1 20021021 A 5320 5936663 SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY LEFT TIE DOWN TRACK OUTBOARD FORWARD SPLICE IS CORRODED AT FS 1090. REPLACE D TIE DOWN TRACK SPLICE PER SRM 53-24-0, FIG 11, 51-10-2, 51-10-4, 51-10-2, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003021300127 20030213 00127 WP 2003 2 13 ASAA0280427 1 20021020 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 160-200, LBL 44. REPLACED SUPPORT PER SRM 53-14-1, FIG 11, A ND 52-30-2. (M) 2 L 7 2 4F RT A6WE 2003021300128 20030213 00128 WP 2003 2 13 ASAA0280429 1 20021020 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 160-200, LBL 56. REPLACED SUPPORT PER SRM 53-14-1, FIG 11, A ND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003021300129 20030213 00129 WP 2003 2 13 ASAA0280430 1 20021020 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 200, LBL 15. REPLACES SUPPORT PER SRM 53-14-1, FIG 11, AND 5 1-30-2. (M) 2 L 7 2 4F RT A6WE 2003021400001 20030214 00001 NE 2003 2 14 2002UALA01890 2 20021223 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 432UA 587 RETURNED TO FIELD DUE TO NR 2 ENGINE INDICATION PROBLEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2003021400002 20030214 00002 NM 2003 2 14 2002UALA01894 1 20021224 A 7500 CONTROLLER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BLEED AIR MALFUNCTIONED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 654UA 25392 EICAS "L ENG PRV" DISPLAYED. ABORTED TAKEOFF AT APPROXIMATELY 60 KNOTS. LT PRESSURE REGUALTOR CONTROLLER REPLACED. NO FURTHER ACTION REQUIRED, NO FURTHER PROBLEM WITH LEFT ENGINE BLEED SYSTEM. 2 L 7 2 4F 4 F RT A1NM E24NE 2003021400003 20030214 00003 NM 2003 2 14 2002UALA01897 1 20021226 A 5610 WINDSHIELD BOEING 777 777222 1385219 NM COCKPIT CRACKED A UALA O OTHER O OTHER AP APPROACH 1 WP 29 787UA 26939 WINDSHIELD 1R OUTER PANE CRACKED. THE NR 1 RT WINDSHIELD OUTER GLASS PLY SHATTERED BECAUSE OF ARCING IN THE INTERLAYER DUE TO MOISTURE INGRESSION. THE UPPER EDGE OF THE WINDOW ASSY. REVEALED EVIDENCE OF MOISTURE INGRESS BETWEEN THE GLASS PLIES NEAR THE UPPER ELECTRICAL WINDOW HEAT SYSTEM BUS BAR. REMOVED AND REPLACED WINDOW ASSY. PER AMM 56-11-01-401. 2 L 7 2 4F RT T0001SE 2003021400004 20030214 00004 NM 2003 2 14 2003F00087 1 20021226 A 3040 MS27212215 TERMINAL BOEING 757 75723N 1384973 NM WINDOW HEAT BURNED G AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 523AT 30232 (ORIG-CLOSED) LT FORWARD WINDOW HEAT INOPERATIVE. MAINTENANCE FOUND WIRES BURNED ON TB5031. INSTALLED NEW TERMINAL BOA RD TB5031. RETERMINATED AND REINSTALLED WIRES IAW WDM 24-51-11 AND 24-21-14. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 2003021400006 20030214 00006 NE 2003 2 14 2003F00091 2 20021228 A 7320 FFG052AC GOVERNOR BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE MALFUNCTIONED G AMTA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 11 513AT 3532 3532 32449 31796 (ORIG-CLOSED) FLT 864. NR 2 ENGINE MAX POWER IN CLIMB WAS 1.30 EPR, DROPPING TO 1.20 IN CLIMB AT FL 230. EEC/LIMITER OF F NO HELP. AIRCRAFT CONTINUED. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE FUEL FLOW GOVERNOR IAW AMM. LEAK CHECKS GOOD, COMPLIED WITH MM HIGH POWER TEST. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2003021400011 20030214 00011 SO 2003 2 14 2003F00096 1 20021216 A 5610 1159SCB51023 WINDSHIELD GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU COCKPIT CRACKED G BQVA O OTHER O OTHER AP APPROACH 1 EA 01 85VM 4643 1172 DURING APPROACH TO IAD CO-PILOT WINDSHIELD OUTER PANE DEVELOPED MULTIPLE CRACKS. 2 L 7 2 4F 4 F RT A12EA E25NE 2003021400022 20030214 00022 2003 2 14 377PA0009 4 20021221 A 3460 1677261401 COMPUTER BOEING 737 7373L9 1384470 NM GE CFM56 CFM56* 13802 NE FMC FAILED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 377PA 23718 FMC COMPUTER POPS CIRCUIT BREAKER. REMOVED AND REPLACED FMC COMPUTER. BITE CHECK. OK IAW MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2003021400024 20030214 00024 CE 2003 2 14 56000973 1 20021217 A 3297 DJ6KJA002 WIRE CESSNA 500 560CESSNA 2076750 CE MLG SHORTED E ERYA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 07 898CB 4314 5600097 LANDING GEAR CONTROL CIRCUIT BREAKER TRIPPED ON GEAR RETRACTION. 12/26/02 REPAIRED WIRE NR DJ6KJA002 UNDER CO-PILOTS F LOOR. WIRE WAS SHORTING TO GROUND CAUSING GEAR CONTROL CIRCUIT BREAKER TO POP. SWANG GEAR NUMEROUS TIMES WITH NO DISCR EPANCIES NOTED. 2 L 7 2 4F RT A22CE 2003021400025 20030214 00025 WP 2003 2 14 ABXA020350 1 20021205 A 2400 AS19593B PUMP DOUG DC9 DC932 3022066 WP HYD SYSTEM FAILED A ABXA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 GL 23 984AX 146 47258 EMERGENCY DECLARED & DIVERTED. A/C CROSSTIE LOCKOUT, LT AC BUS OFF LDC BUS OFF LT GEN. APU WOULD NOT PICK UP RT SIDE. I NSP LT GEN LEADS, CHECKED RESISTANCE ON LT DP CURRENT TRANS (ALL THREE). CHKD 3 CURRENT TRANS FOR LT MAIN SYS. VISUALLY INSP 3 PHASE BUS WIRING. NO DEFECTS NOTED. APU OPS CHKD GOOD. FOUND 50 AMP CB FOR RT AUX. PUMP TRIPPED. INSP WIRING AND RESET. OPS CHECKED GOOD. RAN ENGINE CROSSTIE, OPS CHECKED GOOD. NO DEFECTS NOTED. DEFERRED AS PRECAUTION. S/D: CLEARED D I NR 24863. REPLACED AS PRECAUTION 1 RELAY, 1 PUMP CONTROL SWITCH, 3 CB, AUX. HYD. PUMP ASSY. REPAIR ORDER #501441917 (F OR AUX. HYD. PUMP ASSY.) WAS A CONFIRMED FAILURE. PUMP ASSY HAD HIGH AMPS. UNIT REQUIRED SHIMS IN CONTROL PISTON TO LWR 2 L 7 2 4F A6WE 2003021400026 20030214 00026 WP 2003 2 14 ABXA020364 1 20021218 A 2760 3644322507 LINK DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3 52039 NE SPOILER ACT BROKEN A ABXA O OTHER O OTHER NR NOT REPORTED 1 GL 23 842AX 46015 RT WING INBOARD SPOILER WOULD NOT DEPLOY. REMOVED AND REPLACED BROKEN ACTUATOR CRANK LINKS IN THE INBOARD AND OUTBOARD POSITIONS FOR THE RT INBOARD SPOILER PANEL IAW MM. OPS CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 2003021400027 20030214 00027 NM 2003 2 14 ASAA0210379 1 20021208 A 7110 65ND7120217 BEAM BOEING 737 7372Q8C 138448S NM NR 2 COWLING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL UPPER EDGE BEAM AT NACELLE STATION 188 GOUGED. REPAIRED DAMAGED COWL PER SRM. (M) 2 L 7 2 4F A16WE 2003021400028 20030214 00028 WP 2003 2 14 ABXA020367 1 20021219 A 2120 DUCT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D NE AIR DISTRIBUTION LOOSE A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 23 900AX 47380 DURING FINAL APPROACH, ODOR OF SYNTHETIC OIL IN THE COCKPIT. LT TEMP CONTROLLER IN MANUAL WITH LT DUCT TEMP PEAKED. TURN ED IT OFF. ODOR WENT AWAY. ON THE GROUND, TURNED LT SUPPLY SWITCH BACK ON, WAS ABLE TO CONTROL TEMP MANUALLY. OPS CHECKE D LT MANUAL TEMP CONTROL IAW MM. OPS CHECKED GOOD. NOTED LT AUTO TEMP CONTROL DEFERRED, DI NR 25133. NO OIL ODOR NOTED D URING OPS CHECK. CLEARED DI NR 25133. FOUND LT SYSTEM COOLING AIR DUCT ON AFT SIDE OF WATER SEPERATOR NOT INSTALLED. RE INSTALLED LOOSE DUCT AND TIGHTENED CLAMPS. LT AUTO TEMP CONTROL SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2003021400029 20030214 00029 WP 2003 2 14 ABXA020368 1 20021217 A 2160 60714811 SENSOR DOUG DC9 DC932 3022066 WP CABIN TEMP OUT OF TOLERANCE A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 900AX 16128 47380 COCKPIT TEMP VALVE IN AUTO WENT TO 80 PERCENT FULL HOT. LT DUCT TEMP PEGGED OUT HOT. SLIGHT SMOKE IN COCKPIT. MANUALLY D ROVE VALVE FULL COLD. AC SMOKE CHECKLIST RUN. LT BLEED VALVE OFF FOR REST OF FLT. FOUND AUTO TEMP CONTROL TO COCKPIT TE MP SENSOR OUT OF TOLERENCE. ADJUSTED. MANUAL TEMP OPS CHECKED GOOD IAW DC-9 MM 21-60-0. LINES RECONNECTED AND PLACARDS REMOVED. 2 L 7 2 4F A6WE 2003021400030 20030214 00030 NM 2003 2 14 ASAA0210395 1 20021230 A 5210 507945 TORQUE TUBE BOEING 737 737210C 1384459 NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 ANC - FOUND CREW REPORTED L1 DOOR DIFFICULT TO CLOSE. ADJUSTED VERTICAL TORQUE TUBE, GUIDE ARM STOP PINS, LATCH FITTING S TIMING CONTROL ROD, UPPER HORIZONTAL TORQUE TUBE AND LOWER LATCH ROD THEN DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2003021400035 20030214 00035 WP 2003 2 14 ASAA0280440 1 20021022 A 5320 993053849 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FOUND CUSP WEB CORRODED AT FS 617-712. REPLACED CUSP WEB PER SRM 51-30-2, AND 51-10-4. ( M) 2 L 7 2 4F RT A6WE 2003021400036 20030214 00036 WP 2003 2 14 ASAA0280441 1 20021022 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, CUSP WEB CORRODED AT FS 1239. REPLACED CUSP WEB PER SRM 53-14-3, FIG 12, 51-70-4, 51-30-1 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003021400042 20030214 00042 NE 2003 2 14 ABXA020369 2 20021219 A 7200 JT3D3B ENGINE DOUG DC8 DC861 3021952 WP PWA JT3D JT3D* 52039 NE MALFUNCTIONED A ABXA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 GL 23 848AX 3284 46032 678994 DURING CLIMB, LOW OIL PRESSURE LIGHT CAME ON. OIL PRESSURE FLUX AT 35 PSI. OIL QUANTITY DROPPED TO (0), ENGINE SHUTDOWN AT 0405Z, N1 24 PERCENT, N2 33 PERCENT, PRESS 5 PSI, TEMP 125 DEGREES C TOD PRESS 5, TEMP 84, N1 26 PERCENT, N2 36 PERCE NT, TIME 0500Z. REMOVED AND REPLACED NR 4 ENGINE. OPS CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 2003021400049 20030214 00049 NE 2003 2 14 ABXA030001 2 20021230 A 8550 FILTER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE LT ENGINE LEAKING A ABXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 902AX 2655 47426 665158 WHILE CLIMBING THRU 14,000 FT, LEFT OIL PRESSURE LOW LIGHT CAME ON. OIL PRESSURE SHOWED ABOUT 15 PSI. OIL QUANTITY RAPID LY DECREASED TOWARDS ZERO. SHUT DOWN THE LT ENGINE. INSPECTED AND FOUND NR 1 ENGINE OIL FILTER HOUSING HAD 1 EA. STUD PU LLED LOOSE, OIL DISPERSED THRU CAP. REPLACED THE NR 1 ENGINE IAW MM. (JOB CARDS UNDER W.O. NR 600163221). 2 L 7 2 4F 4 F A6WE E2EA 2003021400051 20030214 00051 WP 2003 2 14 ASAA0280442 1 20021022 A 5754 995416955 PANEL DOUG DC9 DC983 3022083 WP L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, LEFT NR 3 SLAT TRACK PANEL FORWARD END IS CHAFED AT NOTCH-OUT. REPLACED SLAT TRACK DOOR P ER MM 27-80-01. (M) 2 L 7 2 4F RT A6WE 2003021400058 20030214 00058 WP 2003 2 14 ABXA030003 1 20021230 A 3260 CONNECTOR DOUG DC9 DC931 3022065 WP PWA JT8 JT8D* NE NLG IND SWITCH LOOSE A ABXA O OTHER O OTHER DE DESCENT 1 GL 23 948AX 47065 NOSE GEAR WOULD NOT FULLY EXTEND USING NORMAL EXTENSION. FOUND NOSE LANDING GEAR INDICATION SWITCH CONNECTOR PLUG, LOOSE . SECURED CONNECTOR PLUG, SWUNG GEAR THREE TIMES, OPS CHECKED GOOD IAW MM. 2 L 7 2 4F 4 F A6WE E2EA 2003021400062 20030214 00062 WP 2003 2 14 ABXA030006 1 20021227 A 3233 47713921 PIN DOUG DC8 DC863F 302198F WP LT MLG ACTUATOR LOOSE A ABXA O OTHER O OTHER NR NOT REPORTED 1 GL 23 828AX 45999 LT MAIN LANDING GEAR ACTUATING CYLINDER RETRACT PIN WAS LOOSE, DUE TO WORN RETRACT PIN BOSS BUSHING. DISASSEMBLED LT MAI N LANDING GEAR ACTUATOR CYLINDER, REMOVED RETRACT PIN BOSS BUSHING. INSPECTED BORE, MANUFACTURED BUSHING. INSTALLED AND REASSEMBLED IAW REA D832-44219 AND REA D832-45979MR, NEA 32130001-001. 2 L 7 4 4F 4A25 2003021400075 20030214 00075 WP 2003 2 14 ARWA20021205 1 20021214 A 2910 O-RING DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3 52039 NE HYD SYSTEM LEAKING A ARWA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 19 8974U 46110 ON FINAL APPROACH LOSS OF HYDRAULIC FLUID TO THE STAND PIPE. FOUND EMPENNAGE FILTER BOWL LEAKING AT MAGNETIC PLUG. RE MOVED AND REPLACED O-RING LEAK CHECK NORMAL IAW MM. 2 L 7 4 4F 4 F 4A25 1E8 2003021400087 20030214 00087 NE 2003 2 14 AWXA200201202 2 20021213 A 7530 5860017139 ACTUATOR AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE NR 1 ENGINE FAILED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 28 818AW 4596 26071217 1375 ABORTED TAKEOFF, FLT 0045, REJECTED TAKEOFF AT APPROXIMATELY 50 KTS DUE TO NR 1 ENGINE COMPRESSOR VANE ECAM MESSAGE. ME SSAGE FOLLOWED MOMENTARY SURGE OF NR1 EPR ABOVE FLEX THRUST TARGET. NO OTHER ANOMALIES NOTED, RETURNED TO GATE. REVIEW ED THE LAST LOG REPORT THAT INDICATED (ACC ACT/HC/EECI). REMOVED AND REPLACED THE NR 1 ENGINE ACC ACTUATOR IAW AWA T/C R5M75301. PREVIOUS LEG REPORTS INDICATED A VARIABLE STATOR VANE FAILURE. REMOVED AND REPLACED NR 1 ENGINE VARIABLE STAT OR VANE ACTUATOR IAW AWA T/C R5M75306 & R5M71312. LEAK AND OPERATIONAL CHECK GOOD DURING POWER ASSURANCE ENGINE RUN. PAR T NAME, VSV ACTUATOR. SDR WILL BE SUBMITTED UPON RECEIPT OF VENDOR TEARDOWN REPORTS. 2 L 7 2 4F 4 F RT A28NM E311NE 2003021400088 20030214 00088 NM 2003 2 14 AWXA200201205 1 20021216 A 3150 WARNING HORN AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE COCKPIT FALSE ACTIVATION A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 28 827AW 1547 ON TAKEOFF ROLL ENROUTE FOR SET N1 THRUST AT 80 KTS AND HEARD REPETITIVE "RETARD" OVER THE LOUD SPEAKER; REJECTED TAKEOF F AND RETURNED TO GATE. MAX SPEED INDICATED WAS 87 KTS. MAINTENANCE REVIEWED POST FLIGHT REPORT THAT INDICATED AIRCRAFT WENT FROM PHASE 2 TO PHASE 8 AND NEVER LEFT THE GROUND. RAN GROUND SCAN OF CENTRAL WARNING SYSTEM IAW AMM, AND PERFORME D AN OPERATIONAL TEST OF FLIGHT WARNING COMPUTER IAW AMM. NO FAILURE MESSAGES WERE NOTED. 2 L 7 2 4F 4 F RT A28NM E311NE 2003021400089 20030214 00089 NM 2003 2 14 AWXA200201212 1 20021121 A 5411 311N504616 FRAME BOEING 757 757225 1384959 NM NR 2 PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 DURING C-09 CHECK, A .250 INCH CRACK WAS FOUND ON THE NR 2 ENGINE PYLON FRAME CUTOUT FOR PANEL 443GL AT FORWARD LOWER C ORNER INBOARD SIDE OF PYLON. MAINTENANCE PERFORMED A HFEC INSPECTION OF CRACK AT NR2 ENGINE PYLON FRAME CUTOUT; STOP DRI LLED CRACK AND PERFORMED ANOTHER HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED; FABRICATED A REPAIR DOUBLER, AND INS TALLED REPAIR PART IAW AWA ER. 2 L 7 2 4F RT A2NM 2003021400090 20030214 00090 NM 2003 2 14 AWXA200201213 1 20021120 A 5315 BAC1518338 FLOORBEAM BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOORBEAM UPPER FLANGE AT BS 1661, LBL 24. MAINTENANCE REMO VED CORROSION ON CABIN FLOORBEAM UPPER FLANGE AT BS 1661, LBL 24, AND FOUND MATERIAL LOSS OUT OF LIMITS. CUTOUT DAMAGED SECTION OF FLOORBEAM; FABRICATED 2 EACH REPAIR ANGLES, A FILLER, AND A STRAP. INSTALLED REPAIR PARTS IAW SRM. 2 L 7 2 4F 4 F RT A2NM A12EU 2003021400091 20030214 00091 NM 2003 2 14 AWXA200201214 1 20021121 A 5315 BAC1518338 FLOORBEAM BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AROUND A HILOC ON CABIN FLOORBEAM AT BS 1661, LBL 57. 5. MAINTENANCE REMOVED HILOC AND CORROSION ON CABIN FLOORBEAM AT BS 1661, LBL 57.5, AND FOUND MATERIAL LOSS OUT OF LIMIT S. CUTOUT DAMAGED SECTION OF FLOORBEAM; FABRICATED A REPAIR TEE CHORD, 2 EACH REPAIR ANGLES, AND 2 EACH STRAPS; INSTALLE D REPAIR PARTS IAW SRM. 2 L 7 2 4F 4 F RT A2NM A12EU 2003021400092 20030214 00092 NM 2003 2 14 AWXA200201215 1 20021124 A 5310 DOOR FRAME BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 DURING C-09 CHECK A .250 INCH CRACK WAS FOUND ON AFT CARGO DOOR SURROUND CUTOUT WEB AT THE LOWER DOOR STOP FITTING HOLE, BS 1380. MAINTENANCE REMOVED THE CRACKED SECTION OF AFT CARGO DOOR FORWARD FRAME WEB; FABRICATED A NEW SECTION OF FRAME WEB; AND INSTALLED REPAIR PART IAW SRM. 2 L 7 2 4F 4 F RT A2NM A12EU 2003021400093 20030214 00093 NM 2003 2 14 AWXA200201216 1 20021124 A 5310 70750071 DOOR FRAME BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 DURING C-09 CHECK 2 EACH .3750 INCH CRACKS WERE FOUND ON AFT CARGO DOOR CUTOUT FRAME WEB AT THE LOWER DOOR STOP FITTING HOLE, BS 1440. MAINTENANCE REMOVED THE CRACKED SECTION OF AFT CARGO DOOR FRAME WEB BS 1440; FABRICATED A REPAIR PLATE AN D SPLICE PLATE; AND INSTALLED REPAIR PARTS IAW SRM. 2 L 7 2 4F 4 F RT A2NM A12EU 2003021400094 20030214 00094 NM 2003 2 14 AWXA200201217 1 20021124 A 5310 DOOR FRAME BOEING 757 757225 1384959 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 DURING C-09 CHECK A .250 INCH CRACK WAS FOUND ON FORWARD CARGO DOOR CUTOUT FORWARD FRAME WEB AT ATTACHMENT HOLE FOR NR6 DOOR STOP, BS 560. MAINTENANCE REMOVED THE CRACKED SECTION OF FORWARD CARGO DOOR FRAME WEB BS 560; FABRICATED A REPAIR P LATE AND SPLICE PLATE; AND INSTALLED REPAIR PARTS IAW SRM. 2 L 7 2 4F RT A2NM 2003021400095 20030214 00095 NM 2003 2 14 AWXA200201218 1 20021124 A 5310 DOOR FRAME BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 DURING C-09 CHECK A .6250 INCH CRACK WAS FOUND ON FORWARD CARGO DOOR CUTOUT FRAME WEB AT ATTACHMENT HOLE FOR UPPER GUIDE TRACK FITTING, BS 560. MAINTENANCE REMOVED THE CRACKED SECTION OF FORWARD CARGO DOOR FRAME WEB BS 560; FABRICATED A REP AIR PLATE AND SPLICE PLATE; AND INSTALLED REPAIR PARTS IAW SRM. 2 L 7 2 4F 4 F RT A2NM A12EU 2003021400096 20030214 00096 NM 2003 2 14 AWXA200201224 1 20021119 A 5320 149N7523 STRUCTURE BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE WING TO BODY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 DURING C-09 CHECK A 1 INCH CRACK WAS FOUND ON RT WING TO BODY FAIRING LOWER FLAP TRACK STRUCTURE BS 1170. MAINTENANCE RE MOVED RT WING TO BODY FAIRING LOWER FLAP TRACK STRUCTURE BS 1170; FABRICATED A NEW REPLACEMENT STRUCTURE. INSTALLED REPA IR PART SRM. 2 L 7 2 4F 4 F RT A2NM A12EU 2003021400097 20030214 00097 NM 2003 2 14 AWXA200201227 1 20021218 A 3397 BMS13311122 WIRE BOEING 757 7572S7 1384962 NM RROYCE RB211 RB211* 54555 NE SEAT ROW 10 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 901AW 23321 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 10 LT, WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE FOUND AT SEAT ROW 10 LEFT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A2NM A12EU 2003021400105 20030214 00105 NM 2003 2 14 AWXA200201229 1 20021217 A 3397 BMS13311122 WIRE BOEING 737 737277 1384570 NM SEAT ROW 16 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 183AW 22650 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 16 LT, LIGHT REMAINS INOPERATIVE. SUSPECT BAD SPLICE, PLACED EME RGENCY LIGHT AT SEAT ROW 16 LT ON MEL, COND. 1, (EMERGENCY LIGHT INOPERATIVE). ON 12/19/02 MAINTENANCE REPAIRED A BROK EN WIRE IN CONNECTOR AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2003021400106 20030214 00106 2003 2 14 AWXA200201230 4 20021219 A 3460 FMC BOEING 737 7373G7 1384595 NM COCKPIT FAILED A AWXA A UNSCHED LANDING G S MULTIPLE FAILURE AFFECT SYSTEMS CL CLIMB 1 WP 28 305AW 24012 AIR TURN BACK ON TAKEOFF ROLL, EN ROUTE, V1 BOTH CONTROL DISPLAY UNITS WENT BLANK AND FLIGHT MGMT COMPUTER (FMC) FAIL ME SSAGE APPEARED, THEN AT 2000 FT AGL THE CAPT HORIZONTAL SITUATION INDICATOR (HSI) LOST ALL INFORMATION. TURNED BACK, LAN DED WITHOUT FURTHER EVENT. MAINT TROUBLESHOT AND REPLACED FMC IAW BMM, FUNCTIONAL TEST WAS GOOD. NR 1 INERTIAL REFERE NCE UNIT INDICATED LOSS OF INFORMATION FROM FMC WHICH CAUSED LOSS OF HSI DATA. UPLOADED FMC WITH CURRENT DATA. VENDOR BENCH TEST FOR FLIGHT MANAGEMENT COMPUTER SN 2696 FAILED INCOMING TEST DUE TO UNIT (TIMED OUT). REPAIR ACTION STATES (TE STED EXTENSIVELY WITH NO FAULT FOUND). 2 L 7 2 4F RT A16WE 2003021400107 20030214 00107 EU 2003 2 14 AWXA200201231 1 20021222 A 3350 321454 LIGHT AIRBUS 320 A320231 3930325 EU ZONE 221 INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 38641 19713 076 DURING INSPECTION THE EMERGENCY LIGHTS IN FIRST CLASS, L-1, AND R-1 DOORS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) AND BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2003021400108 20030214 00108 EU 2003 2 14 AWXA200201235 1 20021207 A 5220 FE240221001 SEAL AIRBUS 320 A320231 3930325 EU EMERGENCY DOOR DISTORTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 EMERGENCY EVACUATION, DURING C-03 CHECK THE L-1 DOOR ASSIST CYLINDER DIAPHRAGM SEALING WAS FOUND DISTORTED. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR ASSIST CYLINDER DIAPHRAGM SEALING IAW AMM TASK 52-10-00-610-001, RECHARGED CYLINDER I AW TASK 52-10-00-614-050. 2 L 7 2 4F RT A28NM 2003021400114 20030214 00114 EA 2003 2 14 ASOA02612 1 20021130 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 823AS 7196 DURING HANGAR INSPECTION IN BTR, THE AFT OVERHEAD EMERGENCY LIGHT IN THE CABIN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT OVERHEAD EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2003021400115 20030214 00115 WP 2003 2 14 ASAA0280431 1 20021020 A 5347 SR095301157001 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, MAIN CABIN RIGHT SEAT TRACK IS CORRODED AT FS 237, RBL 22. REPLACED TRACK SECTION FROM FS 204 - 245 PER SRM 53-05, FIG 11. (M) 2 L 7 2 4F RT A6WE 2003021400116 20030214 00116 WP 2003 2 14 ASAA0280432 1 20021020 A 5310 3936495505 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY SHEAR TIE CORRODED AT FS 1212, LONGERON 28L-28R. REPLACED SHEAR TIE AND PRE VIOUS SPLICES PER SRM 53-14-3, FIG 3, 51-10-2, 51-10-4, AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003021400117 20030214 00117 WP 2003 2 14 ASAA0280433 1 20021020 A 5311 3936495505 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FRAME CORRODED AT FS 1271, LONGERON 29L-29R. REPLACED FRAME PER SRM 53-14-3 , FIG 3A, 53-03, FIG 2A, AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003021400118 20030214 00118 WP 2003 2 14 ASAA0280434 1 20021020 A 5320 3932140 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, MAIN CABIN FALSE TRACK CORRODED AT FS 160-200, RBL 9. REPLACED FALSE TRACK PER SRM 53-14- 3, FIG 11, AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003021400119 20030214 00119 WP 2003 2 14 ASAA0280435 1 20021020 A 5320 2913044515 GUSSET DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, MID CARGO BAY GUSSET CORRODED AT FS 636 BETWEEN LONGERON 29R AND 30. REPLACED GUSSET PER SRM 51-10-2, 51-30-5, AND DAC DWG 2913044. (M) 2 L 7 2 4F RT A6WE 2003021400120 20030214 00120 WP 2003 2 14 ASAA0280436 1 20021020 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, MAIN CABIN FLOOR SUPPORT IS CORRODED AT FS 190, LBL 53. REPLACED SUPPORT PER SRM 53-14-1, FIG 11, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003021400121 20030214 00121 WP 2003 2 14 ASAA0280437 1 20021020 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND 30K CHECK, MAIN CABIN FLOOR SUPPORT BRACKET IS CORRODED AT FS 170, BL 0. REPLACED SUPPORT BRACKET PER SRM 5 3-14-1, FIG 11, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003021400122 20030214 00122 WP 2003 2 14 ASAA0280444 1 20021022 A 5523 5910413 SKIN DOUG DC9 DC983 3022083 WP ELEVATOR TAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, LEFT ELEVATOR CONTROL TAB DENTED ON LOWER OUTBOARD SURFACE. CUT OFF DAMAGED AREA AND REPA IRED PER SRM 51-70-2. (M) 2 L 7 2 4F RT A6WE 2003021400123 20030214 00123 WP 2003 2 14 ASAA0280450 1 20021026 A 5320 7936937 BRACKET DOUG DC9 DC983 3022083 WP RT MLG WW CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, HYDRAULIC VALVE BRACKET CRACKED IN RIGHT WHEEL WELL. REPLACED BRACKET PER DAC DWG 7936937 , SRM 51-10-2, 51-10-4, AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003021400124 20030214 00124 WP 2003 2 14 ASAA0280462 1 20021026 A 5321 99365851 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 313-389, RBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-2 4-0. (M) 2 L 7 2 4F RT A6WE 2003021400125 20030214 00125 WP 2003 2 14 ASAA0280463 1 20021026 A 5321 99365851 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 313-389, LBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-2 4-0. (M) 2 L 7 2 4F RT A6WE 2003021400126 20030214 00126 WP 2003 2 14 ASAA0280464 1 20021026 A 5321 9936583 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 398-446, RBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-2 4-0. (M) 2 L 7 2 4F RT A6WE 2003021400127 20030214 00127 WP 2003 2 14 ASAA0280465 1 20021026 A 5321 9936585 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 465-541, RBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-2 4-0. (M) 2 L 7 2 4F RT A6WE 2003021400128 20030214 00128 NE 2003 2 14 ASOA02573 2 20021029 A 7250 312097301 TURBINE BLADES AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT ENGINE FRACTURED A ASOA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 11 530AS 453 FLT 4086 - DURING FLIGHT FROM GSG-ATL, A LOW OIL PRESSURE MESSAGE ON THE LEFT ENGINE OCCURRED. THE ENGINE WAS SHUTDOWN BY THE CREW AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEF T ENGINE. ACCORDING TO RESULTS FROM THE ENGINE TEARDOWN REPORT, INSPECTION OF THE BEARINGS AND OTHER OIL RELATED PARTS DID NOT SHOW ANY SIGN OF OIL STARVATION AND LOSS OF OIL PRESSURE COULD NOT BE CONFIRMED. HOWEVER, DUE TO INVESTIGATIONS PERFORMED ON THE POWER TURBINE PACK, IT WAS CONCLUDED THE ENGINE MOST LIKELY FAILED DUE TO A POWER TURBINE 1 BLADE FRAC TURE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2003021400129 20030214 00129 SO 2003 2 14 ASOA02637 1 20021222 A 3397 M2275941249 WIRE EMB 120 EMB120ER 3260203 SO CABIN BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 502AS 120274 DURING HANGAR INSPECTION AT MCN, THE EMERGENCY FLOOR TRACK LIGHT BY SEAT 5A WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE PAIRED A BROKEN WIRE ON THE FORWARD EMERGENCY FLOOR LIGHT ASSEMBLY AT SEAT 5A. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FO R SERVICE. (M) 2 L 7 2 4T RT A31SO 2003021400130 20030214 00130 SO 2003 2 14 ASOA02638 1 20021222 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 261AS 120141 DURING HANGAR INSPECTION IN TXK, THE EMERGENCY LIGHTS IN THE AFT SECTION WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE NR 3 BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 2003021400131 20030214 00131 SO 2003 2 14 ASOA02654 1 20021231 A 5330 SKIN EMB 120 EMB120RT 3260202 SO FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 283AS 120236 DURING A HANGAR INSPECTION IN TXK, THE FIRST OFFICER'S WINDOW POST SKIN WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENA NCE REPAIRED THE CRACKED SKIN IAW ASA EO 120-53-0119A. (M) 2 L 7 2 4T RT A31SO 2003021400132 20030214 00132 NE 2003 2 14 GTIA020719 2 20020625 A 7220 INLET SCREEN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FLL - NR 1 ENGINE INLET SCREEN DELAMINATING INSIDE NOSE COWL. AREA OF LINER DELAMINATED REMOVED. ENTERED ON C/O PER FA A BULLETIN FSAW 00-05 REPLACE IN 90 DAYS. REMOVED AND REPLACED LEFT ENGINE NOSE COWL PER MD80 MM 71-10-01. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2003021400134 20030214 00134 WP 2003 2 14 GTIA021065 1 20020914 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PASSENGER CABIN STATION 160-200 RBL 57 INCHES HAS CORROSION AT DIAPHRAGM SUPPORT DOUBLER. FURTHER EVALUATIO N REVEALED CRACK. REMOVED DAMAGED AREA. FABRICATED FILLER AND DOUBLER, AND INSTALLED FILLER AND DOUBLER. (M) 2 L 7 2 4F RT A6WE 2003021800022 20030218 00022 EU 2003 2 18 AWXA200201246 1 20021227 A 3350 1012661 LIGHT AIRBUS 320 A320231 3930325 EU SEAT ROW 24 RT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 621AW 053 DURING INSPECTION THE BIN MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 24 RT, WAS FOUND INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE BIN MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 24 RT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2003021800023 20030218 00023 NM 2003 2 18 AWXA200201247 1 20021229 A 5220 80330034 RESERVOIR BOEING 757 7572S7 1384962 NM EMERGENCY DOOR LEAKING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 DURING INSPECTION THE L-2 DOOR EMERGENCY POWER RESERVOIR WAS FOUND TO HAVE LOW PRESSURE. MAINTENANCE REMOVED AND REPLAC ED THE L-2 DOOR EMERGENCY POWER RESERVOIR IAW BMM 52-11-30, LEAK AND OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2003021800024 20030218 00024 NM 2003 2 18 AWXA200201248 1 20021227 A 3260 INDICATOR BOEING 737 73733A 1384673 NM MLG INOPERATIVE A AWXA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 28 174AW 23633 FLT 204 - WHEN PREPARING TO LAND, EN ROUTE, WITH GEAR LOWERED, HAD NO GEAR DOWN INDICATION. FOUND GROUND AIR CIRCUIT BRE AKER TRIPPED; RESET CIRCUIT BREAKER AND DECLARED EMERGENCY. FUEL INDICATIONS WERE NORMAL, FLEW BY TOWER TO VERIFY LANDIN G GEAR WAS DOWN; LANDED WITHOUT FURTHER EVENT. CONTRACT MAINTENANCE INSPECTED THE LANDING GEAR AND CIRCUIT BREAKERS, ALL CHECKED NORMAL. 2 L 7 2 4F RT A16WE 2003021800025 20030218 00025 NM 2003 2 18 AWXA200201254 1 20021217 A 5210 5079454 SKIN BOEING 737 7373G7 1384595 NM PAX DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 DURING C-16 CHECK A .5000 INCH CRACK WAS FOUND ON THE LT 1 DOOR INNER SKIN AT 4TH AFT STOP FROM TOP, BS 344. NO STOP DRI LL REQUIRED, CRACK EXTENDS FROM EDGE OF WEB AND TERMINATES AT LIGHTENING HOLE. MAINTENANCE FABRICATED A REPAIR DOUBLER A ND INSTALLED REPAIR PART IAW SRM. 2 L 7 2 4F RT A16WE 2003021800026 20030218 00026 NM 2003 2 18 AWXA200201256 1 20021219 A 5310 654587545 STRUCTURE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 DURING C-16 CHECK CORROSION WAS FOUND ON RT INNER STRUCTURE BS 330 TO BS 335. MAINTENANCE BLENDED OUT CORROSION AND FOUN D MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED RT 1 DOOR DRAIN TRAY, AFT SUPPORT ANGLE, FORWARD SUPPORT ANGLE, REINFORCEME NT STRAP, AFT SPLICE, AND CORRODED INNER STRUCTURE, FABRICATED A NEW REPLACEMENT INNER STRUCTURE; INSTALLED REPAIR PART, AND REINSTALLED R-1 DOOR DRAIN TRAY, AFT SUPPORT ANGLE, FORWARD SUPPORT ANGLE, REINFORCEMENT STRAP, AND AFT SPLICE IAW SRM. 2 L 7 2 4F RT A16WE 2003021800027 20030218 00027 NM 2003 2 18 AWXA200201258 1 20021209 A 2750 BACC2A3A00409DG CONTROL CABLE BOEING 737 7373S3 1384711 NM TE FLAPS BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING C-16 CHECK, FLAP FOLLOW UP CABLES WFFA, WFFB WERE FOUND TO HAVE LOW TENSION IAW TABLE 4, W/C 12B27001. WHILE APP LYING TENSION TO CABLES, CABLE WFFA BROKE .1250 INCH INSIDE THE TERMINAL DUE TO NUMEROUS BROKEN WIRE STRANDS. MAINTENANC E REMOVED AND REPLACED FLAP FOLLOW UP CABLE WFFA IAW BMM. MAINTENANCE ALSO DISCOVERED BROKEN WIRE STRANDS ON FLAP FOLLO W UP CABLE WFFB, AND REPLACED CABLE WFFB IAW BMM. 2 L 7 2 4F RT A16WE 2003021800028 20030218 00028 NM 2003 2 18 AWXA200300001 1 20021231 A 2560 P4010021 BATTERY BOEING 737 737277 1384570 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 182AW 22649 FLIGHT CREW REPORTED THAT THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. AFT CABIN EMERGENCY FLASHLIGHT PLACED ON M EL 25-12 COND. 1, EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE AFT CABIN EMER GENCY FLASHLIGHT; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2003021800029 20030218 00029 NM 2003 2 18 AWXA200300002 1 20021210 A 5330 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING C-16 CHECK, CORROSION AND 3 EACH .2500 INCH CRACKS WERE FOUND ON LOWER EXTERIOR FUSELAGE SKIN (LT AND RT KEELBEAM ) AT BS 727+5 - BS 727+10, STR 27 LT - STR 27 RT. MAINTENANCE CUT SKIN FOR ACCESS TO KEEL BEAM; TRIMMED OUT DAMAGED ARE AS OF OUTBOARD LOWER FLANGE ON KEELBEAM BS 727+5 - BS 727+10, STR 27 LT - STR 27 RT; BLENDED OUT AND TREATED CORROSION; PERFORMED HFEC INSPECTION OF CUTOUTS TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER, TRIPLER, FILLER & REPAIR ANGLE FO R LT KEELBEAM, AND FILLER & REPAIR ANGLE FOR RT KEELBEAM; INSTALLED REPAIR PARTS IAW AWA ER. 2 L 7 2 4F RT A16WE 2003021800030 20030218 00030 NM 2003 2 18 AWXA200300004 1 20021213 A 5315 654583468 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING C-16 CHECK, A .5000 INCH CRACK WAS FOUND ON LOWER FLOORBEAM TIE STRAP AT BS 340 JUST ABOVE AIR STAIR RAIL RBL 24 .75. MAINTENANCE STOP DRILLED HOLE ON LOWER FLOORBEAM TIE STRAP AT BS 340; FABRICATED A REPAIR PLATE; AND INSTALLED REPA IR PART IAW SRM. 2 L 7 2 4F RT A16WE 2003021800031 20030218 00031 NM 2003 2 18 AWXA200300005 1 20021213 A 5315 6545834107 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING C-16 CHECK, A .5000 INCH CRACK WAS FOUND ON LOWER FLOORBEAM TIE STRAP AT BS 340, STR 45 LT, JUST ABOVE AIR STAIR RAIL OUTBOARD END. MAINTENANCE STOP DRILLED END CRACK ON LOWER FLOORBEAM TIE STRAP AT BS 340; FABRICATED A REPAIR PLATE; REMOVED VERTICAL STIFFENER FOR ACCESS; INSTALLED REPAIR PART AND REINSTALLED VERTICAL STIFFENER IAW SRM. 2 L 7 2 4F RT A16WE 2003021800035 20030218 00035 NM 2003 2 18 AWXA200300013 1 20021217 A 5320 6942972 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 DURING C-16 CHECK, A .5000 INCH CRACK WAS FOUND ON INTERCOSTAL AT CEILING OF FORWARD CARGO COMPARTMENT WHERE CARGO DOOR IS HELD OPEN, BS 440, RBL 20. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT CEILING OF FORWARD CARGO COMPARTMENT; FABRICATE D A NEW REPLACEMENT INTERCOSTAL; AND INSTALLED REPAIR PART IAW SRM. 2 L 7 2 4F RT A16WE 2003021800040 20030218 00040 NM 2003 2 18 C1HA2002017 1 20021106 A 5310 FRAME BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 FRAME STA 220, BOTTOM RIGHT SIDE OF DOGHOUSE SHOWS SIGNS OF EXFOLIATION. 2 L 7 3 4F RT A3WE 2003021800043 20030218 00043 CE 2003 2 18 Q9P2003F00000 1 20021030 A 5410 WEB LEAR 35 31A 5170531 CE GARRTT TFE731 TFE731* 01518 WP LT & RT PYLONS CRACKED B Q9PR K NONE O OTHER IN INSP/MAINT 1 WP 25 298CH 4249 4207 058 COMPLIED WITH SB 31-51-1 AND SP 31-51-2 FOUND LT AND RT SHEAR WEBS CRACKED ON BOTH FORWARD AND AFT AREAS. 2 L 7 2 4F 4 F RT A10CE E6WE 2003021800059 20030218 00059 CE 2003 2 18 2003F00108 1 20021221 A 2697 WIRE BEECH 1900 1900D 1154162 CE RT MLG WW LOOSE A GUUA K NONE N FALSE WARNING CR CRUISE 1 SO 19 48544 UE183 RIGHT 'DISCHARGE' ANNUNCIATOR HAD INTERMITTENT ILLUMINATION IN FLIGHT. CONTINUED TO MIA. SECURED WIRES TO SQUIB IN RIG HT WHEEL WELL. (M) 2 L 7 2 4T RT A24CE 2003021800060 20030218 00060 NM 2003 2 18 AALA20021891 1 20021229 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 335AA 22333 MIA - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY AFT BULKHEAD EMERGENCY EXIT PATH LIGHTING INOPERATIVE. REPAIRED BROK EN WIRE AT FORWARD GALLEY AFT BULKHEAD EMERGENCY EXIT PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003021800061 20030218 00061 NM 2003 2 18 AALA20021893 1 20021224 A 3350 PIN BOEING 767 767323 1385205 NM CONNECTOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 380AN 25449 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32B INOPERATIVE. REPLACED BROKEN PINS AT CONNECTOR AT SEAT 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003021800062 20030218 00062 NM 2003 2 18 AALA20021894 1 20021224 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 380AN 25449 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 21H INOPERATIVE. RESECURED LOOSE CONNECTOR AT SEAT 21H . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003021800063 20030218 00063 NM 2003 2 18 AALA20021898 1 20021224 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 312AA 22315 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS AT SEAT 29H INOPERATIVE. RECONNECT EMERGENCY EXIT LIGHT ASSEMBLY T O HARNESS AT SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003021800064 20030218 00064 NM 2003 2 18 AALA20021899 1 20021229 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 DFW - DURING OVERNIGHT MAINTENANCE, LOWER LEFT FORWARD FACING EMERGENCY ESCAPE PATH LIGHTING AT G-3 GALLEY COAT CLOSET W ALL BROKEN. REPLACED LOWER LEFT FORWARD FACING EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT G-3 GALLEY COAT CLOSET WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2003021800066 20030218 00066 NM 2003 2 18 AALA20021900 1 20021231 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 392AN 29429 DFW - DURING OVERNIGHT MAINTENANCE, AFT SEAT MOUNTED EMERGENCY PATH LIGHTING AT SEAT 2H INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY PATH LIGHTING ASSEMBLY AT SEAT 2H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003021800088 20030218 00088 EU 2003 2 18 COEA0201702 1 20021125 A 3397 WIRE FOKKER F27 F27MK600 4990706 EU COCKPIT BROKEN A COEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 13 702FE 10350 AIRCRAFT RETURNED TO BASE AFTER FIRST OFFICER REPORTED SMELL OF SMOKE IN COCKPIT. MAINTENANCE PERSONNEL REPAIRED BROKEN WIRE THAT CONTROLS LIGHTING TO VERTICAL SPEED INDICATOR (VSI). (M) 2 H 7 2 4T A817 2003021800089 20030218 00089 EU 2003 2 18 COEA02021740 1 20020924 A 2434 30E0221G GENERATOR FOKKER F27 F27MK600 4990706 EU RT ENGINE FAILED A COEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 13 740FE 10329 FLIGHT CREW REPORTED RIGHT GENERATOR FAIL LIGHT ILLUMINATED DURING CRUISE FLIGHT AT FL2000. MAINTENANCE PERSONNEL REPLA CED LEFT DC GENERATOR. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 2003021800090 20030218 00090 EU 2003 2 18 COEA02021742 1 20021210 A 2434 NO4063 ALTERNATOR FOKKER F27 F27MK600 4990706 EU LT ENGINE FAILED A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 742FE 10349 FLIGHT CREW REPORTED LEFT ALTERNATOR FAILED INFLIGHT DURING ICING CONDITIONS WHILE DEPARTING FROM YVR. FLIGHT CREW RETU RNED TO YVR AND LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. MAINTENANCE PERSONNEL REPLACED LEFT ALTERNATOR. AIRCR AFT RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 2003021800091 20030218 00091 EU 2003 2 18 COEA0202740 1 20021211 A 2612 8804K12 SWITCH FOKKER F27 F27MK600 4990706 EU FIRE WARNING FAULTY A COEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 13 740FE 10329 LEFT FIRE WARNING LIGHT ILLUMINATED DURING CLIMB OUT DEPARTURE FROM GEG. NO FIRE REPORTED. AIRCRAFT RETURNED TO GEG WIT HOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LEFT FIRE WARNING TEST SWITCH. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 2003021800092 20030218 00092 EA 2003 2 18 COEA0204222 1 20021211 A 2424 21B671A CONTROL UNIT FRCHLD F27 F27F 3373008 EA CABIN MALFUNCTIONED A COEA K NONE O OTHER CL CLIMB 1 NM 13 222DG 31 LEFT DEICE ALTERNATOR FAILED IN FLIGHT DURING CLIMB. MAINTENANCE PERSONNEL REPLACED AC CONTROL UNIT. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T 7A1 2003021800093 20030218 00093 NM 2003 2 18 EIA2002106 1 20021031 A 5753 WEB BOEING 747 747121 1384871 NM T/E FLAP CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND WEB CRACKED COMPLETELY THROUGH AT HOLES 1190 FORWARD WALL OF WING FLAP LEADING EDGE CAVITY. REMOVED AND REP LACED WEB AT HOLES 1190 PER B747 SRM 51-40-02. REPAIRED UPPER CHORD AT HOLES 1190 PER B747 SRM 51-40-03. (M) 2 L 7 4 4F A20WE 2003021800094 20030218 00094 NM 2003 2 18 EIA2002111 1 20021108 A 5313 STRINGER AAR BOEING 747 747121 1384871 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND FUSELAGE MAIN DECK BETWEEN BS 2060-2080 BETWEEN STRINGER 20L AND 22L CORROSION ON STRINGER COMMON TO THE WIN DOW FORGING. REMOVED WINDOW PLUG AND FORGING, REMOVED CORROSION, ROTO PEENED ALODINED, PRIMED AND INSTALLED REPAIRED DO UBLER PER ECRA 480-53-143-2 AND B747 SRM 51-30-02 PAGE 5-9, 51-10-01 PAGE 13-14, 56-20-01 FIG 1 AND 4 BSOPM 20-13-03, B7 47 SRM 51-10-02 PAGE 7 AND 8, 51-10-06 PAGE 1-3 AND B747 MM 56-20-01 PAGE 402-407. (M) 2 L 7 4 4F A20WE 2003021800095 20030218 00095 NM 2003 2 18 EIA2002112 1 20021108 A 5320 ANGLE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND FORWARD LOWER FUSELAGE INTERNAL BS 400 BBL = 24L AND BWL=128 'L' ANGLE EXTRUSION AT ELECTRICAL COMPARTMENT F LOOR LINE, HORIZONTAL CHORD CRACK. CUT OUT DAMAGE, NDT AREA FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 480-53-129-2 . (M) 2 L 7 4 4F A20WE 2003021800096 20030218 00096 NM 2003 2 18 EIA2002114 1 20021108 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND FUSELAGE MAIN DECK BETWEEN BS 2080-2100 BETWEEN STRINGER 20L AND 22L PLUS, CORROSION ON STRINGER 20L COMMON TO THE WINDOW FORGING. REMOVED DAMAGE, NDT'ED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 480-53-142-2. (M) 2 L 7 4 4F A20WE 2003021800097 20030218 00097 NM 2003 2 18 EIA2002116 1 20021108 A 5310 FORGING BOEING 747 747121 1384871 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND LEFT MAIN CARGO DECK BETWEEN BS 620-640 UPPER WINDOW FORGING C/T 5.20 HAS CORROSION. REMOVED DAMAGE, NDT'ED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 480-53-140-2. (M) 2 L 7 4 4F A20WE 2003021800098 20030218 00098 NM 2003 2 18 EIA2002117 1 20021108 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND FRAME WEB IS DAMAGED AND HAS CORROSION AT FS 1920 STRINGER 46R TO STRINGER 35R. REMOVED DAMAGE, NDT'D AREA, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 480-53-130-2. (M) 2 L 7 4 4F A20WE 2003021800099 20030218 00099 NM 2003 2 18 EIA2002120 1 20021108 A 5310 FORGING BOEING 747 747121 1384871 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND LEFT MAIN CARGO DECK BETWEEN BS 560-580 AFT SIDE OF WINDOW FORGING BETWEEN STRINGER 22-20 HAS CORROSION. RE MOVED DAMAGE, NDT'ED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 480-53-137-2. (M) 2 L 7 4 4F A20WE 2003021800100 20030218 00100 NM 2003 2 18 EIA2002122 1 20021108 A 5312 PRESSURE PANEL BOEING 747 747121 1384871 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND CORROSION AT LBL 20 BS 1241 CANTED WEB OF MAIN LANDING GEAR WHEEL WELL. REMOVED DAMAGE, NDT AREA, FABRICATE D AND INSTALLED REPAIR PARTS PER ECRA 480-53-125-2. (M) 2 L 7 4 4F A20WE 2003021800101 20030218 00101 NM 2003 2 18 EIA2002125 1 20021108 A 5320 STRUCTURE BOEING 747 747121 1384871 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND CORROSION IN RIGHT WING GEAR WELL STATION 1241 RBL 1 TOP FORWARD INBOARD CORNER BEHIND SPOILER MIXER. REMOV ED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 480-53-125-2. (M) 2 L 7 4 4F A20WE 2003021800102 20030218 00102 NM 2003 2 18 EIA2002126 1 20021108 A 2810 STRUCTURE BOEING 747 747121 1384871 NM CENTER TANK CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND CORROSION ON TOP SIDE OF CENTER TANK AT FLOORBEAM TO FUEL TANK AT STATION 1140 LBL 75 BELOW AIR DUCT LOCATED UNDER FLOORBOARD NR 118. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 480-57-121-2. (M) 2 L 7 4 4F A20WE 2003021800103 20030218 00103 NM 2003 2 18 EIA2002128 1 20021108 A 5730 SKIN BOEING 747 747121 1384871 NM WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND MAIN DECK CENTER WING UPPER SKIN CORRODED AT FITTINGS STATION 1100 RBL 11. REMOVED DAMAGE, NDT AREA, FABRIC ATED AND INSTALLED REPAIR PARTS PER ECRA 480-57-121-2. (M) 2 L 7 4 4F A20WE 2003021800104 20030218 00104 NM 2003 2 18 EIA2002139 1 20021024 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND BS 1995 STR 22R CORRODED. BLENDED OUT CORROSION, FLAT PEENING, SPOT FACING INSTALLED FILLER AND REPAIR ANGL E OF BLENDED AREA PER ECRA 480-53-1332. (M) 2 L 7 4 4F A20WE 2003021800105 20030218 00105 NM 2003 2 18 EIA2002140 1 20021024 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 FOUND BS 630 STRINGER 20L CORRODED. BLEND OUT CORROSION, FLAT PEENING, SPOT FACING, INSTALL FILLER AND REPAIR ANGLE OF BLENDED AREA PER ECRA 480-53-133-2. (M) 2 L 7 4 4F A20WE 2003021800106 20030218 00106 NM 2003 2 18 EIA2002141 1 20021024 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND BS 520 STRINGER 22L CORRODED. BLENDED OUT CORROSION, FLAT PEENING, SPOT FACING, INSTALL FILLER AND REPAIR A NGLE OF BLENDED AREAS PER ECRA 480-53-133-2. (M) 2 L 7 4 4F A20WE 2003021800109 20030218 00109 NM 2003 2 18 EIA2002143 1 20021106 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND BS 1810 CRACKED AND CORRODED 03-1670-03-1669. FRAME WEB, BS 1810 FRAME OUTER CHORD CRACKED, DAMAGE SKIN AND BEAR STRAP BS 1810. REPAIRED SKIN, FRAME WEB, OUTER CHORD AND BEAR STRAP PER ECRA 480-53-155-2 INSPECTION ARE TO CONTI NUE AND IN ADDITION, INSPECTIONS ARE TO BE DONE AT INTERVALS NOT TO EXCEED 3000 FLT CYCLE. (M) 2 L 7 4 4F A20WE 2003021800111 20030218 00111 NM 2003 2 18 EIA2002144 1 20021104 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND LEFT BS 340 UPPER FLOORBEAM HAS OVERSIZED HOLES. DISCREPANT HOLES OVERSIZED AND OVERSIZED FASTENERS INSTALL ED ECRA 480-53-122-2. (M) 2 L 7 4 4F A20WE 2003021800124 20030218 00124 NM 2003 2 18 EIAA2002127 1 20021108 A 5714 STRUCTURE BOEING 747 747121 1384871 NM CENTER WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND MAIN DECK WING CENTER SECTION BODY STATION 1080 BBL 94L CORROSION. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 480-57-121-2. (M) 2 L 7 4 4F A20WE 2003021800125 20030218 00125 NM 2003 2 18 EIAA2002129 1 20021108 A 2810 STRUCTURE BOEING 747 747121 1384871 NM CENTER TANK CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND CORROSION ON TOP SIDE OF CENTER FUEL TANK AT FLOORBEAM TO FUEL TANK AT STATION 1140 BELOW FLOORBEAM. REMOVE D DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 480-57-121-2. (M) 2 L 7 4 4F A20WE 2003021800127 20030218 00127 NM 2003 2 18 EIAA2002142 1 20021106 A 5310 SHEAR TIE BOEING 747 747121 1384871 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MZJ - FOUND BS 1520 STRINGER 34R FRAME SHEAR TIE CRACKED. REPAIRED BY TRIMMING OUT DAMAGE AND INSTALLED REPAIR ANGLE AN D SHIM PER ECRA 480-53-149-2. (M) 2 L 7 4 4F A20WE 2003021800130 20030218 00130 WP 2003 2 18 GTIA021183 1 20021017 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FUSELAGE TEMP REPAIR ON DENT AT STATION 237 LEFT SIDE BETWEEN LONGERON 19 AND 20. REMOVED TEMP REPAIR DOUBLER AT STATION 237 LEFT SIDE LONGERON 19 AND 20. CUT OUT DAMAGED AREA FROM STATION 239-250 LONGERON 19-20. FABRICATED FINGER D OUBLER. FABRICATED REPAIR DOUBLER. INSTALLED ALL REPAIR PARTS, DOUBLERS, FILLERS, FINGER DOUBLERS, STRAPS. (M) 2 L 7 2 4F RT A6WE 2003021800131 20030218 00131 WP 2003 2 18 GTIA021253 1 20021121 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND AFT CARGO JAMB BEAM HAS CORROSION STATION 1112-1249, DOOR JAMB BEAM REPAIR STRAP HAS CORROSION UNDER STRAP O N JAMB BEAM. CORRODED REMOVAL WAS FOUND TO BE OUT OF LIMITS ON DOOR JAMB. REMOVED DOOR JAMB BEAM. CORROSION REMOVAL O N DOOR WEB WAS FOUND TO BE OUT OF LIMITS. HOLES LOCATED AND DRILLED ON NEW JAMB BEAM. FABRICATED NEW DOOR WEB. INSTAL LED DOOR WEB. INSTALLED DOOR JAMB BEAM. CORROSION REMOVAL ON ANGLE STATION 1212 WAS FOUND TO BE OUT OF LIMITS. INSTAL LED DOOR BEAM SKIN ANGLE STATION 1212. (M) 2 L 7 2 4F A6WE 2003021800133 20030218 00133 WP 2003 2 18 GTIA021254 1 20021115 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND FORWARD CARGO PIT DOOR JAMB BEAM LOWER SECTION CORRODED. REMOVED DOOR JAMB INNER PANEL. HOLES LOCATED AND DRILLED ON NEW PANEL. INSTALLED NEW PANEL. (M) 2 L 7 2 4F A6WE 2003021800134 20030218 00134 WP 2003 2 18 GTIA021256 1 20021116 A 5330 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND MID PIT HAS CORROSION AT DOUBLER RAD ALT RECEIVER 1, RAD ALT TRANSMITTER 1, RAD ALT TRANSMITTER 2, RAD ALT R ECEIVER 2. THE DAMAGED TO THE RAD ALT RECEIVER-1 DOUBLER AND THE RAD ALT TRANSMITTER -2 DOUBLER IS OUT OF LIMITS. REMO VED THE BAD ALT RECEIVER-1 DOUBLERS. LOCATED AND DRILLED THE NEW DOUBLERS. (M) 2 L 7 2 4F A6WE 2003021800135 20030218 00135 WP 2003 2 18 GTIA021257 1 20021121 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 E/E BAY STATION 180-218 L30 CORROSION IN LONGERON AROUND FASTENERS. REMOVED DAMAGED SECTION OF LONGERON AND SPLICE. IN STALLED NEW LONGERON AND SPLICE. (M) 2 L 7 2 4F A6WE 2003021800137 20030218 00137 WP 2003 2 18 GTIA021258 1 20021113 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND PASSENGER SEAT TRACK LEFT, OUTBOARD WORN AT FS 998-1010, GOUGE 1019, CORROSION 1037-1041, WORN 1059-1067, 1 087-1098, CORROSION 1240. LEFT, OUTBOARD SEAT TRACK FOUND TO BE OUT OF LIMITS AT FS 1240. REMOVED LEFT OUTBOARD SEAT TR ACK FS 1222-1309. LOCATED AND DRILLED REPLACEMENT SECTION OF LEFT OUTBOARD SEAT TRACK. INSTALLED REPLACEMENT SECTION O F SEAT TRACK. (M) 2 L 7 2 4F A6WE 2003021800139 20030218 00139 WP 2003 2 18 GTIA021259 1 20021116 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND DENTS AT STATION 200 AT LONGERONS 22-23L, 23-24L, 24-25L, DUE TO THESE DENTS CLOSE PROXIMITY TO EACH OTHER. REPAIR MUST BE ACCOMPLISHED. REWORKED THREE MINOR DENTS AT STATION 200 BETWEEN LONGERONS 22-23L, 23-24L, AND 24-25. L OCATED AND DRILLED 01 DOUBLER. INSTALLED DOUBLER AT STATION 200 L22L TO L25L. (M) 2 L 7 2 4F A6WE 2003021800142 20030218 00142 WP 2003 2 18 GTIA021260 1 20021123 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND RIGHT INBOARD SEAT TRACK CORRODED AT STATION 200 AND 256. MATERIAL LOSS OUT OF LIMITS AT SEAT TRACK STATION 267. REMOVED DAMAGE AREA. FABRICATED NEW SEAT TRACK FS 200-320. INSTALLED SEAT TRACK AND SPLICE. (M) 2 L 7 2 4F A6WE 2003021800143 20030218 00143 WP 2003 2 18 GTIA021261 1 20021124 A 5342 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND DORSAL FIN INBOARD LEFT, RIGHT ANGLE ATTACH IS CRACKED. REMOVED LEFT AND RIGHT FIN INBOARD ATTACH ANGLES. LOCATED AND DRILLED LEFT INBOARD FIN ANGLE. LOCATED AND DRILLED LEFT OUTBOARD ATTACH ANGLE. LOCATED AND DRILLED RIGHT INBOARD FIN ANGLE AND RIGHT OUTBOARD ATTACH ANGLE. INSTALLED LEFT OUTBOARD ANGLE, OUTBOARD ANGLE, DORSAL FIN GUSSET, AN D PANEL FILLER. INSTALLED RIGHT, OUTBOARD ANGLE, INBOARD ANGLE, DORSAL FIN GUSSET AND PANEL FILLER. (M) 2 L 7 2 4F A6WE 2003021800144 20030218 00144 WP 2003 2 18 GTIA021262 1 20021121 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND PAX CABIN STATION 503, STATION 231 WEB MEMBRANE IS CRACKED. STOP DRILLED CRACK. FABRICATED DOUBLER. INSTA LLED DOUBLER REPAIR. STOP DRILL CRACK AT WEB MEMBRANE ON STATION 503. FABRICATE DOUBLER REPAIR. INSTALLED REPAIR DOUB LER AT STATION 503. (M) 2 L 7 2 4F A6WE 2003021800146 20030218 00146 WP 2003 2 18 GTIA021263 1 20021127 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - L2 DOOR OPENING FLOOR PANEL SUPPORT BRACKETS (2) CORRODED. FORWARD FLOOR PANEL SUPPORT BRACKET L2 DOOR FOUND TO B E OUT OF LIMITS. FABRICATED FORWARD FLOOR PANEL SUPPORT. INSTALLED NEW FORWARD FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2003021800148 20030218 00148 WP 2003 2 18 GTIA021264 1 20021129 A 5620 RING DOUG DC9 DC982 3022082 WP CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND LEFT 346 WINDOW UPPER AFT FRAME CORRODED. REMOVED LEFT NR 46 WINDOW UPPER AFT CRACKED FRAME. LOCATED AND D RILLED NEW ORDERED WINDOW RING. INSTALLED NEW WINDOW RING. (M) 2 L 7 2 4F A6WE 2003021800149 20030218 00149 WP 2003 2 18 GTIA021265 1 20021115 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND TEMP REPAIR AT STATION 474 LONGERON 30 (VHF ANT) REQUIRES ACTIONS. REMOVED EXTERNAL DOUBLER. FABRICATED IN NER SKIN. FABRICATED FOUR TEE ANGLES. FABRICATED TWO GUSSETS. FABRICATED EXTERNAL DOUBLER. FABRICATED TWO ANGLES. FA BRICATED GUSSET, ANGLES. FABRICATED ANGLES. FABRICATED INTERCOSTAL. FABRICATED ANGLES 'T' TWO EACH. FABRICATED 'T' A NGLE FOUR EACH. FABRICATED FINGER DOUBLER. FABRICATED AND INTERCOSTALS. FABRICATED FITTING. INSTALLED EXTERNAL DOUBL ER AND FINGER DOUBLER. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2003021800150 20030218 00150 WP 2003 2 18 GTIA021266 1 20021114 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND DENT LEFT SIDE FUSELAGE FS 209 LONGERON 14L. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2003021800151 20030218 00151 WP 2003 2 18 GTIA021267 1 20021114 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND DENT RIGHT SIDE FS 353 BETWEEN LONGERON 22R AND 23R. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2003021800152 20030218 00152 WP 2003 2 18 GTIA021268 1 20021114 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND DENT RIGHT SIDE FS 622 BETWEEN LONGERONS 21R AND 22R. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2003021800153 20030218 00153 WP 2003 2 18 GTIA021269 1 20021113 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND DENT RIGHT SIDE FUSELAGE STATION 463 BETWEEN LONGERONS. FORMED NEW DOUBLER REPAIR. INSTALLED NEW DOUBLER R EPAIR. (M) 2 L 7 2 4F A6WE 2003021800154 20030218 00154 WP 2003 2 18 GTIA021270 1 20021116 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND EXISTING REPAIRS AT FS 320 AND FS 330 REQUIRES TO BE COMBINED INTO A SINGLE REPAIR. REMOVED EXISTING REPAIR S AT FS 320 AND FS 330. CUT OUT EXISTING SKIN AT FS 320 AND FS 330. FORMED NEW REPAIR PARTS. INSTALLED NEW REPAIR. ( M) 2 L 7 2 4F A6WE 2003021800155 20030218 00155 NM 2003 2 18 GTIA021271 1 20021126 A 5730 ACCESS PANEL DOUG MD80 MD83 3023681 NM LT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND LEFT WING ACCESS PANEL NR 1163 HAS TOOL MARKS, CORROSION AND BARE METAL. FOUND PANEL TO BE CRACKED. ROUTED OUT CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT 2003021800157 20030218 00157 NM 2003 2 18 GTIA021272 1 20021127 A 5321 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND PASSENGER CABIN LEFT INBOARD FLOOR PANEL STATION 465 TO 541 HAS CRACKED METAL, CORE DAMAGE AND FASTENER BROK EN OFF IN PANEL. FABRICATED NEW PANEL. (M) 2 L 7 2 4F RT 2003021800158 20030218 00158 NM 2003 2 18 GTIA021273 1 20021206 A 5320 FLOOR SUPPORT DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND MID CARGO FLOOR SUPPORT STATION 619-712 ELONGATED HOLE, TOOL MARKS, BARE METAL, FASTENER SHANKS. UPON FURTH ER INSPECTION, PART FOUND TO BE CRACKED. DRILLED AND LOCATED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F RT 2003021800159 20030218 00159 NM 2003 2 18 GTIA021274 1 20021126 A 5347 SEAT TRACK DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND LEFT INBOARD SEAT TRACK WORN AND CORRODED FS 237-863. REMOVED FLOOR PANEL FS 768-826 LBL 22-44 TO REMOVED C ORROSION. FOUND THE FLOOR BOARD AT FS 768-826 LBL 22-44 MISSING INSERT AND CRACK EDGE. FABRICATED NEW FLOOR BOARD. IN STALLED FLOOR BOARD. (M) 2 L 7 2 4F RT 2003021800160 20030218 00160 NM 2003 2 18 GTIA021275 1 20021126 A 5347 SEAT TRACK DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND LEFT INBOARD SEAT TRACK WORN AND CORRODED FS 1212-1309. STATION 1227-1250 ON LEFT INBOARD SEAT TRACK WAS FO UND TO BE OUT OF LIMITS. REMOVED LEFT INBOARD SEAT TRACK. LOCATED AND DRILLED NEW SEAT TRACK. INSTALLED LEFT INBOARD S EAT TRACK. (M) 2 L 7 2 4F RT 2003021800161 20030218 00161 NM 2003 2 18 GTIA021276 1 20021125 A 5320 INTERCOSTAL DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND FORWARD CARGO COMPARTMENT CORRODED AT INTERCOSTAL STATION 446 TO 427 ATTACH TO LONGERON 29. REMOVED CORRODE D INTERCOSTAL. FABRICATED NEW INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F RT 2003021800162 20030218 00162 NM 2003 2 18 GTIA021277 1 20021203 A 5330 SKIN DOUG MD80 MD83 3023681 NM FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND GOUGES AT FS 1190 RIGHT ON WINDOW BELT REQUIRES TO BE BLENDED AND CHECKED FOR LIMITS. FABRICATED -7 DOUBLER . FABRICATED -5 DOUBLER. INSTALLED REPAIR ON WINDOW BELT. (M) 2 L 7 2 4F RT 2003021800163 20030218 00163 NM 2003 2 18 GTIA021278 1 20021126 A 5347 SEAT TRACK DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND LEFT MID SEAT TRACK WORN AND CORRODED FS 1212-1309. SEAT TRACK STATION 1227 TO 1309 LEFT MID WAS FOUND TO B E CORRODED OUT OF LIMITS. REMOVED SEAT TRACK. LOCATED AND DRILLED NEW SEAT TRACK. INSTALLED LEFT MID SEAT TRACK. (M) 2 L 7 2 4F RT 2003021800164 20030218 00164 NM 2003 2 18 GTIA021279 1 20021124 A 5754 SKIN DOUG MD80 MD83 3023681 NM L/E SLAT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND RIGHT NR 1 SLAT CRACKED AT LOWER SURFACE AT OUTBOARD SEAL AND SEAL FASTENERS NOT INSTALLED PROPERLY. TRIMME D OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR. (M) 2 L 7 2 4F RT 2003021800165 20030218 00165 NM 2003 2 18 GTIA021280 1 20021129 A 5311 FRAME DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND AFT CARGO PIT CORRODED FRAME FLANGE FS 1287-L22L 2, CORROSION CLIP ANGLE FS 1287 LONGERON 27L TO 28L.3 AND C ORROSION FS 1287 LONGERON 29L ON FRAME. MATERIAL LOSS ON CLIP FS 1287 LONGERON 27L-28L OUT OF LIMITS. REMOVED CLIP. I NSTALLED NEW CLIP. (M) 2 L 7 2 4F RT 2003021800166 20030218 00166 NM 2003 2 18 GTIA021281 1 20021130 A 5320 STIFFENER DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND STATION 218 STIFFENER NR 4 IS DENTED AND HAS MULTIPLE SPOT OF SURFACE CORROSION. REMOVED DAMAGED PORTION OF NR 4 STIFFENER. FABRICATED REPAIR ANGLE. INSTALLED REPAIR ANGLE. (M) 2 L 7 2 4F RT 2003021800167 20030218 00167 NM 2003 2 18 GTIA021282 1 20021130 A 5530 FORMER DOUG MD80 MD83 3023681 NM VERTICAL STAB CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND VERTICAL STAB DORSAL FIN CRACKED ON FORMER RIGHT SIDE LOWER ATTACH TO PLATE/STRAP. REMOVED FORMER. LOCATED AND DRILLED NEW FORMER. INSTALLED NEW FORMER, STRAP AND LEFT AND RIGHT PLATES. (M) 2 L 7 2 4F RT 2003021800168 20030218 00168 NM 2003 2 18 GTIA021283 1 20021130 A 5342 ATTACH ANGLE DOUG MD80 MD83 3023681 NM FUSELAGE PUNCTURED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND DORSAL FIN, RIGHT OUTBOARD (TWO) ATTACH ANGLE PUNCTURED. REMOVED TWO RIGHT OUTBOARD ATTACH ANGLE. LOCATED A ND DRILLED TWO ATTACH ANGLES, INSTALLED. (M) 2 L 7 2 4F RT 2003021800169 20030218 00169 NM 2003 2 18 GTIA021284 1 20021202 A 5311 FRAME DOUG MD80 MD83 3023681 NM FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND DENT OVER FRAME AT FS 484 BETWEEN LONGERONS 28 AND 29L REQUIRES REPAIR. FABRICATED REPAIR DOUBLER. INSTALL ED REPAIR DOUBLER. (M) 2 L 7 2 4F RT 2003021800170 20030218 00170 WP 2003 2 18 GTIA021285 1 20021218 A 3397 WIRE DOUG DC9 DC983 3022083 WP A/C BAY LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 824NK 53015 MCO - FOUND ONE EMERGENCY LIGHT ON LEFT SIDEWALL IN TAIL COMPARTMENT INOPERATIVE. REMOVED LIGHT ASSEMBLY OF TAIL COMPAR TMENT EMERGENCY LIGHT, SECURED LOOSE WIRE AND RELAMPED LIGHT. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2003021800191 20030218 00191 WP 2003 2 18 GTIA021287 1 20021118 A 5210 INTERCOSTAL DOUG DC9 DC982 3022082 WP L1 DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND L1 DOOR UPPER MOST INTERCOSTAL BEAM (TWO) CRACKS IN LOWER RADIUS FORWARD AND AFT SIDES. REMOVED CRACKED DOO R BEAM. FORMED BEAM. INSTALLED DOOR BEAM. (M) 2 L 7 2 4F A6WE 2003021800192 20030218 00192 WP 2003 2 18 GTIA021288 1 20021116 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND CAPTAIN FLOOR PANEL NEXT TO CONTROL COLUMN HAS DELAMINATED AND BROKEN WOOD FILLER AS MARKED. LOCATED AND DR ILLED NEW PANEL. (M) 2 L 7 2 4F A6WE 2003021800193 20030218 00193 NE 2003 2 18 GTIA021289 2 20021222 A 7230 854021 BLADE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D* NE NR 1 ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 806NK 48051 FTW - FOUND DURING DAILY INSPECTION, TWO BLADES IN NR 1 ENGINE C1 STAGE DAMAGED. INSPECTED TWO BLADES OUT OF LIMITS IAW 72-00-00. REMOVED AND REPLACED 1 BLADE IN MATCH SET AMM 72-33-00. (M) 2 L 7 2 4F 4 F A6WE E2EA 2003021800264 20030218 00264 SW 2003 2 18 ALG2003F218 1 20021203 A 5330 SKIN BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE CRACKED A ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 577AL 5261 53247 DURING DAILY INSPECTION, CRACKS, CORROSION, BROKEN SPOT WELDS, HINGES WORN OUT. SKIN CORROSION AT SPOT WELDS BECAUSE OF NON-ALCLAD MATERIAL. HEAVIER GAUGE MATERIAL ON STRINGERS NEEDED. 1 G 7 1 3U 3 U O H2SW E1GL 2003021900006 20030219 00006 CE 2003 2 19 GVR2003F00000 1 20020130 A 2510 551900932 STRUCTURE CESSNA 500 550 2076604 CE PWA 530 PW530A NE UPPER CHAIR BASE CRACKED B GVRR O OTHER O OTHER NR NOT REPORTED 1 CE 05 391KC 5500381 UPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. PREVIOUS IN APPROPRIATE REPAIR MADE. CHAIR WAS REPAIRED IAW STC ST01042WI STRUCTURAL SEAT REPAIR. 1 L 7 2 4F 4 F A22CE E00053EN 2003021900009 20030219 00009 CE 2003 2 19 NE62003F00000 1 20021129 A 5410 56541091 BEAM CESSNA 414 414A 2075907 CE CONT O520 TSIO520* 17040 SO LT NACELLE DAMAGED G NE6A K NONE O OTHER IN INSP/MAINT 1 SW 01 2619G 5920 414A0290 LT ENGINE OUTBOARD BEAM, DURING INSPECTION OF THE LT ENGINE NACELLE, BOTH EXHAUST ELBOW SUPPORT BRACKETS WERE BROKEN. O UTBOARD EXHAUST ELBOW SUPPORT BRACKET CLAMP, HAD WORN THROUGH THE NACELLE SKIN. THE OUTBOARD FORWARD EXHAUST SLIP JOINT FLANGE HAD WORN THROUGH THE NACELLE SKIN. 1 L 7 2 3O 3 O A7CE E8CE 2003021900016 20030219 00016 2003 2 19 T042003F00000 4 20021113 A 6113 C229412 BULKHEAD HARTZL CESSNA 206 U206A 2073316 CE CONT O520 IO520* 17032 SO PROP SPINNER CRACKED E T04A O OTHER O OTHER NR NOT REPORTED 1 AL 03 8091Z 488 FJ179 U2060491 564056 THIS BULKHEAD CRACKED BETWEEN THE MOUNTING HOLES OF THE RE-ENFORCEMENT AND OUTBOARD FLANGE. ONLY 2 CRACKS, PORT DID NOT FAIL FURTHER FOUND AT 100 HOUR INSPECTION. 1 H 7 1 3O 3 O A4CE E5CE 2003021900024 20030219 00024 SW 2003 2 19 ALG2003F3ADP 1 20021210 A 6410 214011819101 BEARING BELL 214 214ST 1182106 SW GE CT7TS CT71 30030 NE T/R BLADE YOKE FAILED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 393AL 423 28117 DURING DAILY INSPECTION. BEARINGS OUTER LINER COMING APART DUE TO HIGH VIBRATION, SCRAPPED 4 EACH BEARINGS. CLOSER DAI LY INSPECTION OF TAILROTOR ASSEMBLY. 2 G 7 2 4U 4 U H10SW E8NE 2003021900033 20030219 00033 NM 2003 2 19 BJNA021202 1 20021230 A 3350 601321 BATTERY PACK BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE EMERGENCY LIGHT DISCHARGED A BJNA O OTHER O OTHER NR NOT REPORTED 1 WP 11 344TM 23044 LT EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE AT OVERWING EXIT. REPLACE LT EXTERIOR EMERGENCY BATTERY PACK POWER SUPPLY IN THE AFT CARGO PIT IAW MM. 2 L 7 2 4F 4 F RT A16WE E2EA 2003021900044 20030219 00044 NM 2003 2 19 FX72003F00000 1 20021202 A 3240 211473 BRAKE BOEING 727 727231 1384079 NM PWA JT8 JT8D15 52051 NE NR 1 SEIZED A FX7A O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 64346 21633 THE AIRCRAFT WAS BEING TAXIED FROM BLAST FENCE FOR A DMI ON NR 3 EPR AND NR2 EGT INBOUND ITEM WHEN APPARENTLY THE NR 1 B RAKE SEIZED AND THE GEAR CAUGHT ON FIRE. THE AREA WAS INSPECTED IAW MFG TELEX FAX-MIA-02-00027H 06DEC02 AND SRM 51-10-4 . THE GEAR WAS REPLACED AND ALL TIRES AND BRAKES ON THE LEFT SIDE IAW MM AS WELL AS THE BRAKE METERING VALVE. THE AIRC RAFT WAS RETURNED TO SERVICE AFTER A TEST FLIGHT ON 12/21/02. 2 L 7 3 4F 4 F A3WE E2EA 2003021900058 20030219 00058 NM 2003 2 19 RYN2003F00001 1 20021227 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D1 52044 NE FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 AT B CHECK, CRACK FOUND ON FORWARD AND AFT SIDES OF FUSELAGE INTERIOR, LT FRAME AT BS 680 ATTACHMENT TO SKIN LOWER SILL BEAM. 2 L 7 3 4F 4 F A3WE E2EA 2003021900060 20030219 00060 NM 2003 2 19 RYN2003F00003 1 20021227 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D1 52044 NE FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 AT B CHECK, CRACK FOUND IN FUSELAGE INTERIOR AT FLOORBEAM LOWER CHORD ANGLE BS295, LBBL30. 2 L 7 3 4F 4 F A3WE E2EA 2003021900061 20030219 00061 NM 2003 2 19 RYN2003F00004 1 20021227 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D1 52044 NE FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 DURING B CHECK, FOUND SKIN CRACKED AT FUSELAGE INTERIOR, LT SIDE, BS 480, FRAME TO LOWER SILL BEAM FROM TIE TO FUSELAGE. 2 L 7 3 4F 4 F A3WE E2EA 2003021900106 20030219 00106 NM 2003 2 19 SWAA021614 1 20020721 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2003021900107 20030219 00107 NM 2003 2 19 SWAA021614A 1 20020721 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2003021900108 20030219 00108 NM 2003 2 19 SWAA021614B 1 20020721 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2003021900109 20030219 00109 NM 2003 2 19 SWAA021614C 1 20020721 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2003021900110 20030219 00110 NM 2003 2 19 SWAA021614D 1 20020721 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2003021900111 20030219 00111 NM 2003 2 19 SWAA021614E 1 20020721 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2003021900112 20030219 00112 NM 2003 2 19 SWAA021614F 1 20020721 A 5320 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED (7 EA) AT BS 500D AND STR 21R, BS 807 AND STR 26R, BS 380 AND STR 22L, BS 500D AND STR'S 19L AND 19R, BS 578 AND STR 10L, BS 706 AND STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2003021900136 20030219 00136 NM 2003 2 19 USAA020476 1 20021231 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 47130 23930 PIT - FOUND SKIN CRACKED 2 INCHES, STATION 727 STRINGER 24L. CUT OUT DAMAGE, NDT'D AREA, INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 201 AND TR 53-60-06. (M) 2 L 7 2 4F RT A16WE 2003021900137 20030219 00137 NM 2003 2 19 USAA020477 1 20021227 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 49763 22958 PIT - FOUND SKIN CRACKED 3 INCHES LONG, RIGHT SIDE STATION 867 STRINGER 24 RIGHT. CUT OUT DAMAGE, INSTALLED EXTERNAL DO UBLER PER SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2003021900138 20030219 00138 NM 2003 2 19 USAA020478 1 20021219 A 5512 SKIN BOEING 737 7373B7 1384580 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 44112 24412 PIT - FOUND SKIN CRACKED 1.125 INCH LONG CRACK, RIGHT HORIZONTAL STABILIZER UNDERSIDE SKIN AFT STATION 125. CUT OUT DAM AGE, INSTALLED FILLER AND EXT DOUBLER WITH TEMP FASTENERS PER TYP REPAIR 55-10-07 REV B. (M) 2 L 7 2 4F RT A16WE 2003021900152 20030219 00152 NM 2003 2 19 USAABB02212 1 20021227 A 3397 WIRE BOEING 767 7672B7 1385107 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 652US 24765 FRA - FOUND THE FLOOR MOUNTED EMERGENCY LIGHTS AT ROWS 1GF AND 2GF INOPERATIVE. MAINTENANCE RECONNECTED WIRE ON EMERGEN CY LIGHT AT ROW 2GF. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A1NM 2003021900159 20030219 00159 EU 2003 2 19 USAASA02102 1 20021121 A 3350 321430 BATTERY AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 186US 1701 PHL - THE EMERGENCY POWER SUPPLY BATTERY AT THE L1 DOOR WAS FOUND TO BE WEAK. MAINTENANCE REPLACED THE BATTERY AT THE L 1 DOOR. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2003021900163 20030219 00163 NM 2003 2 19 USAASB02228 1 20021223 A 3397 WIRE BOEING 737 737301 1384611 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 334US 23231 PHL - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 22C INOPERATIVE. MAINTENANCE REPAIRED D AMAGED/BROKEN WIRE AT SEAT 22C. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003021900164 20030219 00164 2003 2 19 USAASB02229 4 20021223 A 3441 HG1050AD04 IRU BOEING 737 7373B7 1384580 NM E/E BAY FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 392US 23314 PIT - FLT 1004 - AFTER TAKEOFF FROM PIT, EN ROUTE TO MKE, THE LEFT IRS FAILED IN FLIGHT. DECISION WAS MADE TO RETURN TO FIELD AT PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED TH E LEFT INERTIAL REF UNIT (IRU). FUNCTIONAL CHECK SATISFACTORY. (M) 2 L 7 2 4F RT A16WE 2003021900165 20030219 00165 NM 2003 2 19 USAASB02230 1 20021224 A 3350 606171 SOCKET BOEING 737 737301 1384611 NM CABIN DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 334US 23231 IND - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT 13ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SOCKET ASSE MBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003021900166 20030219 00166 NM 2003 2 19 USAASB02231 1 20021224 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 785AU 25024 ORD - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN THE AFT CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGEN CY LIGHT BATTERY PACK PER MM 33-51-51. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003021900167 20030219 00167 NM 2003 2 19 USAASB02236 1 20021226 A 2612 FIRE LOOP BOEING 737 7374B7 1384702 NM NR 2 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 778AU 24980 CLT - FLT 1946 - EN ROUTE FROM PBI TO PIT, NR 2 ENG 'A' FIRE LOOP FAULT LIGHT ILLUM. NR 2 ENG 'B' LOOP WAS ALREADY ON M EL. CREW ALSO REPORTED THE NR 1 ENG EGT FLUCTUATING. THE NEEDLE AND DIGITAL COUNTER GO FROM 425 DEGREES TO MAX DEFLECTI ON. FLT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MX ACCOMPLISHED FAULT ISOLATION TEST PER MM 26-11-00. REPLACED WORN OUT CONNECTOR AT 'B' SENSOR HARNESS AND CLEARED MEL. CLEANED AND TESTED CONNECTOR A 'A' HARNESS AND LOOP. TESTS NORMAL PER MM 26-11-00. THE FLUCTUATING EGT ON THE NR 1 ENG, MX FOUND THE NR 1 ENG CORE HARNE SS CHAFED IN TWO PLACES. R&R THE CORE HARNESS. FAULT ISOLATION TEST, ADJUST TEST AND EGT TEST CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2003022000010 20030220 00010 SO 2003 2 20 RU92003F00000 1 20021113 A 3260 MS27640 SQUAT SWITCH EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A60 52043 NE LT MLG FAILED E RU9A O OTHER O OTHER NR NOT REPORTED 1 GL 23 127JM 110218 ON NOV. 13, 2002 GEAR FAILED TO RETRACT, SQUAT SWITCH FAILED. REPLACED SQUAT SWITCH. OPS CHECK, OK. 1 L 7 2 4T 4 T A21SO E4EA 2003022000037 20030220 00037 CE 2003 2 20 043682 1 20020930 A 2910 571302 MOTOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA HYD POWER PACK FAILED A AMWA O OTHER J WARNING INDICATION LD LANDING 1 CE 07 13ZV 1425 1425 UE13 ON AN ATTEMPT TO LAND, THE CREW TRIED TO EXTEND LANDING GEAR, BUT THE CIRCUIT BREAKER POPPED. THEY RESET CIRCUIT BEAKER ND LANDING GEAR STILL WOULD NOT EXTEND. THE CREW PERFORMED AN EMERGENCY EXTENSION. RECEIVED 3 GREEN GEAR DOWN INDICATORS . THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED A HYDRAULIC POWER PACK MOTOR ASSEMBLY. THE TEARD OWN REPORT THAT WAS RECEIVED FROM THE VENDOR REPORTED THAT THE BRUSHES AND BEARINGS WERE WORN AND THE COMMUTATOR SCORED. THE VENDOR REPLACED THE BRUSHES AND BEARINGS.THEN THE COMMUTATOR WAS FIXED. THIS PART WAS OVERHAULED AND TESTED. 2 L 7 2 4T 3 T RT A24CE E2NE 2003022000048 20030220 00048 NM 2003 2 20 ABXA030049 1 20021110 A 5410 313T12003 SKIN BOEING 767 767281 1385109 NM FAIRING GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 795AX 23145 NR 1 ENGINE STRUT UNDER WING FAIRING FOUND DEEP GOUGE ON SKIN AT NAC STATION 258 RT SIDE. REPAIRED AREA IAW REA B654-454 55MR. 2 L 7 2 4F RT A1NM 2003022000049 20030220 00049 NM 2003 2 20 ABXA030050 1 20021211 A 5754 SKIN BOEING 767 767281 1385109 NM LT WING SLAT CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 795AX 23145 LT WING SLAT NR 3 OSS 756.50, LE SKIN FOUND CORRODED ON FASTENER HEAD ATTACHING SKIN TO FORMER. REPAIRED AREA IAW REA B6 57-45505MR. 2 L 7 2 4F RT A1NM 2003022000050 20030220 00050 NM 2003 2 20 ABXA030051 1 20021208 A 5730 112T3105 SKIN BOEING 767 767281 1385109 NM LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 795AX 23145 LT WING UPPER SKIN PANEL NR 1 AFT OF REAR SPAR ATTACHMENT, WHERE THE TRAILING EDGE PANELS ARE INSTALLED, FOUND CORROSION AT WING STATIONS 534.27 & 554, 811.20 & 852. REPAIRED AREA IAW REA B657-45500MR. 2 L 7 2 4F RT A1NM 2003022000052 20030220 00052 NM 2003 2 20 ABXA030052 1 20021128 A 5313 143T300111 STRINGER BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 795AX 23145 DURING CHECK, 0.5 INCH LONG CRACK WAS FOUND AT SEC. 43 RT, STR. 17 RT, STA. 434. THE CRACK ORIGINATED AT THE FORWARD FAS TENER HOLE IN STR. VERTICAL FLANGE. REPAIRED AREA IAW REA B653-45486MR. 2 L 7 2 4F RT A1NM 2003022000091 20030220 00091 EU 2003 2 20 QXEA0300086 1 20021128 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 PDX- CABIN ENTRANCE EXIT LOCATING SIGN HAS SEVERAL LIGHT BULBS BURNT OUT. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2003022000126 20030220 00126 NE 2003 2 20 QXEA0300120 2 20020124 A 7250 4124T3P03 TURBINE BLADES GE CG348C1 CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 2 ENGINE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 609QX 2505 GEE965254 10031 965254 PDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO HPT 1 BLADES 2/3 MISSING. REPLACED ENGINE. AIRCRAF T OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENG INE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WOR K OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD I N THE NEXT FEW QUARTERS. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2003022000142 20030220 00142 EA 2003 2 20 A6WA200240028 1 20021215 A 2613 356024310 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAULTY A A6WA E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 GL 31 403AW 7288 LEFT 14TH DUCT WARNING IN FLIGHT, REDUCED POWER PER QRH, MESSAGE DISAPPEARED, ON DESCENT AT REDUCED POWER MESSAGE RETURN ED, PERFORMED PRECAUTIONARY SHUTDOWN PER QRH. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE 14TH STAGE PYLON OVERHEAT DE TECTION LOOP. (M) 2 L 7 2 4F RT A21EA 2003022000143 20030220 00143 EA 2003 2 20 A6WA200240029 1 20021216 A 2120 SMOKE CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A A6WA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 GL 31 405AW 7362 SMOKE TOILET CAUTION MESSAGE ON APPROACH INTO DENVER WITH PACKS SWITCHED TO APU. FLIGHT ATTENDANT SAW SMALL AMOUNT OF S MOKE ALONG FLOOR. ALSO, REPORTED OIL SMELL IN/NEAR LAVATORY. OPS CHECK GOOD ON GROUND. COULD NOT DUPLICATE. OK FOR S ERVICE AT THIS TIME. (M) 2 L 7 2 4F RT A21EA 2003022000144 20030220 00144 EU 2003 2 20 A6WA200260077 1 20021218 A 2910 ACM30506 FUSE BAC 146 146200A 1500266 EU HYD SYSTEM MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 608AW E2049 RIGHT MLG FAILED TO RETRACT ON TAKEOFF. RECYCLED 3 TIMES. MAINTENANCE REPLACED RIGHT HYDRAULIC FUSE. (M) 2 H 7 4 4F A49EU 2003022000149 20030220 00149 WP 2003 2 20 ASA0280670 1 20021223 A 5340 9911957 ATTACH FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, UPPER LEFT TAILCONE ATTACH BRACKETS TWO CRACKED. REPLACED BRACKETS PER SRM 51-10-2, 51-10 -4, 51-30-1, AND DAC DWG 9911957. (M) 2 L 7 2 4F RT A6WE 2003022000151 20030220 00151 NM 2003 2 20 ASAA0210391 1 20021217 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE O OTHER CL CLIMB 1 NM 01 740AS 22578 ANC - DURING CLIMB-OUT OF CORDOVA, EMERGENCY FLOOR TRACK LIGHTS AT ROW 18 ILLUMINATED. REMOVED AND REPLACED REMOTE ASSEM BLY BATTERY, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2003022000152 20030220 00152 NM 2003 2 20 ASAA0210392 1 20021217 A 3350 883200312 RECEIVER BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS ON THE NR 1 SEAT PALLET WILL NOT TEST. REMOVED AND RE PLACED REMOTE ASSEMBLY RECEIVER, THEN LIGHTS OPERATED NORMAL. (M) 2 L 7 2 4F A16WE 2003022000153 20030220 00153 NM 2003 2 20 ASAA0210393 1 20021223 A 3350 86210144 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 14 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERY PACK THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2003022000154 20030220 00154 NM 2003 2 20 ASAA0210394 1 20021229 A 3350 883200312 RECEIVER BOEING 737 7372Q8C 138448S NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 6 AND 7 INOPERATIVE. REMOVED AND REPLACED REMOTE AS SEMBLY RECEIVER AND BATTERY, THEN LIGHT TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2003022000155 20030220 00155 NM 2003 2 20 ASAA0240243 1 20021218 A 5230 6547952340 SKIN BOEING 737 7374Q8 138447Q NM CARGO DOOR DENTED A K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 DURING C-CHECK, FOUND AFT CARGO DOOR SKIN REQUIRES REPLACEMENT. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022000156 20030220 00156 NM 2003 2 20 ASAA0240245 1 20021218 A 5420 ANGLE BOEING 737 7374Q8 138447Q NM NR 1 PYLON CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 DURING C-CHECK, NR 1 PYLON CRACKED L ANGLE AT INBOARD END OF FAIRING STIFFENER. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022000157 20030220 00157 NM 2003 2 20 ASAA0240246 1 20021218 A 4910 6566213 SHROUD BOEING 737 7374Q8 138447Q NM APU BAY CHAFED A K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 DURING C-CHECK, FOUND APU SHROUD SKIN CHAFED. REPAIRED IAW EA. (M) 2 L 7 2 4F RT A16WE 2003022000158 20030220 00158 NM 2003 2 20 ASAA0240247 1 20021218 A 5730 65C26270 SKIN BOEING 737 7374Q8 138447Q NM RT WING CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 DURING C-CHECK, FOUND RIGHT WING LE CRACKED AT SLAT ACTUATOR CUT OUT. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022000159 20030220 00159 NM 2003 2 20 ASAA0240248 1 20021218 A 5310 651072235 DOOR FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 DURING C-CHECK, FOUND FORWARD CARGO BAY FORWARD DOOR FRAME CLOSURE WEB DAMAGED. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022000160 20030220 00160 NM 2003 2 20 ASAA0240249 1 20021222 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 NM 01 780AS 25112 DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE FROM FORWARD GALLEY TO ROW 2. REPAIRED BROKEN WIRES , REPLACED LIGHT SECTION, OPS CHECKED NORMAL RELEASED FOR SERVICE (M) 2 L 7 2 4F RT A16WE 2003022000161 20030220 00161 NM 2003 2 20 ASAA0240250 1 20021224 A 5320 65C30424 SUPPORT BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 794AS 28889 PAE - DURING C-CHECK, FOUND CORROSION IN AFT CARGO BAY AFT BULKHEAD LOWER SUPPORT AT LEFT BL 24 TO RT BL 24. REPAIRED I AW SRM. (M) 2 L 7 2 4F RT A16WE 2003022000162 20030220 00162 NM 2003 2 20 ASAA0240251 1 20021224 A 5320 69434961 SUPPORT BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 794AS 28889 PAE - DURING C-CHECK, FOUND AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION ON UPPER SURFACE RIGHT BS 847. REPAIR ED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022000163 20030220 00163 NM 2003 2 20 ASAA0240252 1 20021224 A 5320 6547690 SUPPORT BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 794AS 28889 PAE - DURING C-CHECK, FOUND AFT CARGO BAY FLOOR TO SIDEWALL SUPPORTS HAVE CORROSION ON UPPER SURFACES AT BS 727 TO BS 87 7. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022000164 20030220 00164 NM 2003 2 20 ASAA0240253 1 20021231 A 5320 65C373081 SUPPORT BOEING 737 737490 1384715 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 794AS 28889 PAE - DURING C-CHECKED, FOUND SHELF SUPPORT ABOVE AUTOGYROS IN E/E BAY IS CRACKED. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022000165 20030220 00165 WP 2003 2 20 ASAA0280657 1 20021214 A 5347 S00484 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, SEAT TRACK CORRODED AT FS 275. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003022000166 20030220 00166 WP 2003 2 20 ASAA0280658 1 20021214 A 5347 SR095301157003 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, SEAT TRACK CORRODED AT FS 826. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003022000167 20030220 00167 WP 2003 2 20 ASAA0280659 1 20021214 A 5347 SR095301157001 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, SEAT TRACK CORRODED AT FS 624. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003022000168 20030220 00168 CE 2003 2 20 AMWA5 1 20020921 A 7120 1299100471 TRUSS BEECH 1900 1900D 1154162 CE RT ENGINE CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 166YV 7913 7913 UE166 WHILE PERFORMING AND "H" CHECK ON THE RT TRUSS IN, MECHANICS DISCOVERED A CRACK LOCATED ON THE UPPER RT COWLING BRACKET. THE CRACK WAS ON THE OUTBOARD SIDE OF THE TRUSS. THE CORRECTIVE ACTION WAS THAT THEY REMOVED AND REPLACED THE TRUSS. UP ON RECEIPT OF THE TRUSS BY THE VENDOR, THEIR INSPECTION REPORT SHOWED THE CRACK AT BOTH UPPER COWLING BRACKETS ALSO. VEN DOR PERFORMED AN 8000 HOUR MAG PARTICLE INSPECTION IAW REPS BEECH 1900D MM MISCELLANEOUS LIMITATIONS. REPAIRED TRUSS SUP PORT BRACKET MOUNTS 2 EACH BY FABRICATING AND INSTALLING REPAIR DOUBLERS AND FILLERS ON UPPER COWLING BRACKETS IAW RAYTH EON COWLING BRACKETS IN ACCORDANCE WITH RAYTHEON STANDARD REPAIR DRAWING SR-CO-00012 REV "B" DATED 12-10-02. 2 L 7 2 4T RT A24CE 2003022000176 20030220 00176 WP 2003 2 20 ASAA0280660 1 20021214 A 5347 SR095301157001 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, SEAT TRACK CORRODED AT FS 275. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003022000177 20030220 00177 WP 2003 2 20 ASAA0280661 1 20021214 A 5210 9955763U17 WEB DOUG DC9 DC983 3022083 WP L1 DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING 30K CHECK, FOUND LEFT FRONT (L1)DOOR INNER WEB IS CRACKED AT RADIUS AT HANDLE AREA. REPLACED INNER WEB PER SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003022000178 20030220 00178 NM 2003 2 20 ASAA0280662 1 20021219 A 3350 1001191 LIGHT DOUG MD80 MD83 3023681 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 53473 SEA - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY, INC LUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT 2003022000179 20030220 00179 WP 2003 2 20 ASAA0280663 1 20021217 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 SEA - DURING LINE CHECK, THE EMERGENCY TRACK LIGHTING AT ROWS 29-33 AND IN THE TAIL SECTION ALONG CATWALK WERE FOUND TO BE INOPERATIVE. REPLACED SHORTED TAILCONE EJECT HANDLE LIGHT ASSEMBLY AND EMERGENCY TRACK LIGHTS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003022000180 20030220 00180 WP 2003 2 20 ASAA0280667 1 20021223 A 5320 593795421 BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, BRACKET BELOW 'Y' DUCT IN ACCY COMPARTMENT IS CRACKED. REPLACED BRACKET PER SRM 51-10-3, 51-30-1 AND DAC DWG 5937954. (M) 2 L 7 2 4F RT A6WE 2003022400126 20030224 00126 EU 2003 2 24 CX7A194J18 1 20020812 A 5246 ACCESS DOOR SAAB SF340 340B 7860101 EU A CX7A A UNSCHED LANDING O OTHER CR CRUISE 1 GL 03 304CE 340B198 Lav service door opened in flight. Causing A/C not to hold pressurization. 2 L 7 2 4T RT A52EU 2003022400127 20030224 00127 EU 2003 2 24 CX7A194J13 1 20020730 A 7100 CT79B ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE STOPPED A CX7A E ENGINE SHUTDOWN Y Z ENGINE STOPPAGE SIGNIFICANT FAILURE REPORT TO TAKEOFF 1 GL 03 306CE 15773 4035 340B203 785573 During T/O roll, Tq was 94% on both engines, ITT below 890 degrees. After rotation at 80-100 feet, a bang and shudder w as felt and ITT on the right engine ran away to max. Tq reduced to zero, prop autocoarsened. Engine had failed. Emerg ency declared.Mx R/R R/H engine and sent for overhaul. 2 L 7 2 4T 4 T RT A52EU E8NE 2003022400128 20030224 00128 NE 2003 2 24 CX7A194J23 3 20021125 A 6114 7901996 ACTUATOR SAAB SF340 340B 7860101 EU HAMSTD 14RF 14RF19 NE BROKEN A CX7A E ENGINE SHUTDOWN E VIBRATION/BUFFET AP APPROACH 1 GL 03 317CE 14907 1223 340B352 On final approach, R/H prop hub actuator failed. Shut down R/H engine. Performed go around.Landed without incident. 2 L 7 2 4T RT A52EU 6 C P11NE 2003022700013 20030227 00013 EU 2003 2 27 2003F00114 1 20021228 A 2422 121431A INVERTER FOKKER F27 F27MK600 4990706 EU ELECTRICAL SYS MALFUNCTIONED A COEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 13 703FE 10420 VISIBLE SMOKE/HAZE IN CARGO COMPARTMENT ACCOMPANIED BY BURNING SMELL. SYMPTOMS WENT AWAY WHEN CHOKE VALVE WAS OPENED. REMOVED AND REPLACED EMERGENCY INVERTER. OPS CHECKS SERVICEABLE. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 2003022700014 20030227 00014 NM 2003 2 27 2003F00115 1 20021204 A 7110 19602702 COWLING DOUG DC10 DC1040F 3023507 NM NR 1 ENGINE DELAMINATED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 141WE 46661 DURING SCHEDULED MAINTENANCE, NR 1 FAN COWL PREVIOUS REPAIR WAS FOUND DELAMINATED ON THE INBOARD LOWER CORNER. REPAIRED IAW AS11 DRAWING AS11476, DOUBLER REPAIR. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2003022700015 20030227 00015 CE 2003 2 27 2003F00116 1 20020120 A 3230 16001260 CIRCUIT BREAKER BEECH 1900 1900D 1154162 CE LANDING GEAR FAILED A GUUA O OTHER O OTHER AP APPROACH 1 SO 19 69549 UE194 FLT 9318 - TCB-FLL - DURING APPROACH, LANDING GEAR WOULD NOT EXTEND. MANUALLY PUMPED LANDING GEAR DOWN. REMOVED AND RE PLACED LANDING GEAR SYSTEM HYDRAULIC MOTOR CIRCUIT BREAKER. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPERATION AL CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2003022700016 20030227 00016 NM 2003 2 27 ASAA0210257 1 20021028 A 5320 6552457 WEB BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND WEB AT BS 1012-1016, BUTTOCK LINE 0, LEFT BUTTOCK LINE 6 CORRODED. REMOVED AND RE PLACED WEB PER SRM. (M) 2 L 7 2 4F A16WE 2003022700017 20030227 00017 NM 2003 2 27 ASAA0210258 1 20021028 A 5312 6546568 BULKHEAD BOEING 737 737210C 1384459 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND PRESSURE BULKHEAD AT BS 1016, RIGHT BUTTOCK LINE 24 HAS MECHANICAL DAMAGE. REMOVE D AND REPAIRED PRESSURE BULKHEAD PER SRM. (M) 2 L 7 2 4F A16WE 2003022700018 20030227 00018 NM 2003 2 27 ASAA0210259 1 20021028 A 5720 6545321 SUPPORT BOEING 737 737210C 1384459 NM LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND SUPPORT FOR WALKING BEAM AT LEFT WING REAR SPAR STATION 201.85, CRACKED. REMOVED AND REPLACED SUPPORT FOR WALKING BEAM PER MANUFACTURER'S DRAWING. (M) 2 L 7 2 4F A16WE 2003022700019 20030227 00019 NM 2003 2 27 ASAA0210260 1 20021015 A 5230 6547952 DOOR FRAME BOEING 737 7372X6C 1384552 NM CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 PAE - DURING SCHEDULED C-CHECK, FOUND AFT CARGO DOOR FRAME AT BS 787, RIGHT BUTTOCK LINE 40 CRACKED. REPAIRED CRACK PER EA. (M) 2 L 7 2 4F RT A16WE 2003022700020 20030227 00020 NM 2003 2 27 ASAA0210261 1 20021028 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT SEAT PALLET 5-3 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2003022700021 20030227 00021 NM 2003 2 27 ASAA0210262 1 20021028 A 5754 6546421 SKIN BOEING 737 737210C 1384459 NM L/E SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 SLAT OUTBOARD END UPPER SURFACE AT SLAT STATION 385 DENTED. REPAIRED SLAT PE R SRM. (M) 2 L 7 2 4F A16WE 2003022700022 20030227 00022 NM 2003 2 27 ASAA0210263 1 20021028 A 5753 6546430 FLAP BOEING 737 737210C 1384459 NM LT WING PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND LEFT INBOARD FORE FLAP AT WING STATION 87L PUNCTURED. REPAIRED FORE FLAP PER SRM. (M) 2 L 7 2 4F A16WE 2003022700024 20030227 00024 NM 2003 2 27 ASAA0210264 1 20021028 A 5753 6546430 FLAP BOEING 737 737210C 1384459 NM RT WING CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND RIGHT INBOARD FORE FLAP AT WING STATION 85R CHAFED. REPAIRED FORE FLAP PER SRM. (M) 2 L 7 2 4F A16WE 2003022700025 20030227 00025 NM 2003 2 27 ASAA0210265 1 20021029 A 5347 6554969507 SEAT TRACK BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND SEAT TRACK AT BS 887-907, RIGHT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED SE AT TRACK PER SRM. (M) 2 L 7 2 4F A16WE 2003022700026 20030227 00026 NM 2003 2 27 ASAA0210266 1 20021029 A 5320 65548325 BEAM BOEING 737 737210C 1384459 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND BEAM AT BS 1095, RIGHT BUTTOCK LINE 12, RIGHT BUTTOCK LINE 18 CHAFED. REMOVED DAM AGE AND REPAIRED BEAM PER SRM. (M) 2 L 7 2 4F A16WE 2003022700028 20030227 00028 NM 2003 2 27 ASAA0210267 1 20021030 A 5220 65465831 SKIN BOEING 737 737210C 1384459 NM BLOW-OUT DOOR CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PAE - DURING SCHEDULED C-CHECK, FOUND TAIL COMPARTMENT BLOW-OUT DOOR SKIN AT BS 1040-1060, STRINGER 20L-24L CHAFED. REP AIRED BLOW-OUT DOOR SKIN PER SRM. (M) 2 L 7 2 4F A16WE 2003022700029 20030227 00029 NM 2003 2 27 ASAA0210322 1 20021120 A 7110 657377482 PLATE BOEING 737 7372Q8C 138448S NM NR 1 COWLING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK,FOUND NR 1 ENGINE INBOARD COWL PLATE AT NACELLE STATION 180.75 GOUGED. REMOVED AND REPLA CED PLATE PER SRM. (M) 2 L 7 2 4F A16WE 2003022700030 20030227 00030 NM 2003 2 27 ASAA0210323 1 20021124 A 7110 6570194502 COWLING BOEING 737 7372Q8C 138448S NM NR 1 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE TAILPIPE COWL AT THRUST REVERSER STATION 142.6 GOUGED. REMOVED DAMAGE D AND REPAIRED COWL PER SRM. (M) 2 L 7 2 4F A16WE 2003022700032 20030227 00032 NM 2003 2 27 ASAA0210325 1 20021126 A 7110 315A1000 COWLING BOEING 737 7372Q8C 138448S NM NR 2 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE EXHAUST COWL AT NACELLE STATION 243.5 GOUGED. REMOVED DAMAGE AND REPA IRED COWL PER SRM. (M) 2 L 7 2 4F A16WE 2003022700034 20030227 00034 NM 2003 2 27 ASAA0210326 1 20021126 A 7110 657377391 COWLING BOEING 737 7372Q8C 138448S NM NR 1 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL AT NACELLE STATION 181.25 GOUGED. REMOVED DAMAGE AND REPAIRED CO WL PER SRM. (M) 2 L 7 2 4F A16WE 2003022700036 20030227 00036 NM 2003 2 27 ASAA0210327 1 20021126 A 5242 6545830118 SKIN BOEING 737 7372Q8C 138448S NM E/E BAY DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND E/E BAY DOOR AT BS 325-350, LEFT BUTTOCK LINE 6 RIGHT BUTTOCK LINE 14 DENTED. REM OVED AND REPLACED DAMAGED SKIN PER SRM. (M) 2 L 7 2 4F A16WE 2003022700038 20030227 00038 NM 2003 2 27 ASAA0210328 1 20021126 A 7110 6585378312 FLANGE BOEING 737 7372Q8C 138448S NM NR 2 COWLING CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE NOSE COWL MATING FLANGE AT NACELLE STATION 99.25 CHAFED. REPAIRED FLA NGE PER SRM. (M) 2 L 7 2 4F A16WE 2003022700039 20030227 00039 NM 2003 2 27 ASAA0210329 1 20021127 A 5315 654583446 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 328-344, RIGHT BUTTOCK LINE 11 CORRODED. REMOVED CORROSION, FABRI CATED AND INSTALLED REPAIR PER SRM. (M) 2 L 7 2 4F A16WE 2003022700041 20030227 00041 NM 2003 2 27 ASAA0210336 1 20021202 A 5730 6546419501 SKIN BOEING 737 7372Q8C 138448S NM LT WING CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND LEFT WING LEADING EDGE AT WING STATION 361-494 CHAFED. REMOVED DAMAGED SKIN, FABR ICATED AND INSTALLED REPAIR PER SRM. (M) 2 L 7 2 4F A16WE 2003022700042 20030227 00042 NM 2003 2 27 ASAA0210337 1 20021202 A 5315 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 1006, LEFT BUTTOCK LINE 14, LEFT BUTTOCK LINE 23 CORRODED. REMOVE D CORROSION AND REPAIRED FLOORBEAM PER SRM. (M) 2 L 7 2 4F A16WE 2003022700044 20030227 00044 NM 2003 2 27 ASAA0210338 1 20021202 A 7110 COWLING BOEING 737 7372Q8C 138448S NM NR 2 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE EXHAUST COWL AT THRUST REVERSER STATION 98 GOUGED. REPAIRED NR 2 ENGI NE EXHAUST COWL PER SRM. (M) 2 L 7 2 4F A16WE 2003022700045 20030227 00045 NM 2003 2 27 ASAA0210339 1 20021202 A 7110 COWLING BOEING 737 7372Q8C 138448S NM NR 2 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE EXHAUST COWL AT THRUST REVERSER STATION 102 GOUGED. REPAIRED NR 2 ENG INE EXHAUST COWL PER SRM. (M) 2 L 7 2 4F A16WE 2003022700047 20030227 00047 NM 2003 2 27 ASAA0210340 1 20021202 A 7110 COWLING BOEING 737 7372Q8C 138448S NM NR 2 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL AT NACELLE STATION 139 GOUGED. REPAIRED NR 2 ENGINE COWL PER SRM . (M) 2 L 7 2 4F A16WE 2003022700049 20030227 00049 NM 2003 2 27 ASAA0210346 1 20021203 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM CABIN MALFUNCTIONED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 JNU - DURING LINE MAINTENANCE, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 13-15 ILLUMINATED. REMOVED AND REPLACED REMOT E ASSEMBLY BATTERY AND RECEIVER, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2003022700051 20030227 00051 NM 2003 2 27 ASAA0240183 1 20021108 A 5753 65C2631025 SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP BIRD STRIKE A ASAA K NONE O OTHER AP APPROACH 1 NM 01 769AS 25103 YVR - DURING APPROACH INTO YVR, EXPERIENCED MULTIPLE BIRD STRIKE ON LEFT INBOARD MID FLAP LEADING EDGE. REPAIRED IAW SR M. (M) 2 L 7 2 4F RT A16WE 2003022700052 20030227 00052 NM 2003 2 27 ASAA0240204 1 20021113 A 5330 65C35765 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE LIGHTNING STRIKE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 PAE - DURING C-CHECK, FOUND UPPER FUSELAGE EXTERNAL SKIN HAS LIGHTNING STRIKES AT BS 369.5 THROUGH BS 500F PLUS 1.25 AND WL 304 THROUGH WL 147 AND LBL 0.0 THROUGH LBL 26. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022700053 20030227 00053 NM 2003 2 27 ASAA0240205 1 20021113 A 5320 6547690 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 PAE - DURING C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORTS CORRODED AT BS 727B PLUS 12 THROUGH 947 AND WL 156 TO 160 AND LEF T AND RIGHT BL 24. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022700054 20030227 00054 NM 2003 2 27 ASAA0240206 1 20021113 A 5320 65C2730892 SUPPORT ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 PAE - DURING C-CHECK, FOUND CORROSION ON SIDEWALL SUPPORT ANGLE AT STATION 727D AND STRINGER 25R. REPAIRED IAW SRM. (M ) 2 L 7 2 4F RT A16WE 2003022700055 20030227 00055 NM 2003 2 27 ASAA0240207 1 20021113 A 5320 65465922 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 PAE - DURING C-CHECK, FOUND AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 727A, RBL 3 AND WL 156. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022700056 20030227 00056 NM 2003 2 27 ASAA0240208 1 20021115 A 5320 6547690 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 PAE - DURING C-CHECK, FOUND CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORTS. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022700057 20030227 00057 NM 2003 2 27 ASAA0240209 1 20021115 A 5320 963089 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 DURING C-CHECK, FOUND HORIZONTAL CHANNELS AT BS 178 REQUIRE REPLACEMENT DUE TO OVERSIZED HOLES. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022700058 20030227 00058 NM 2003 2 27 ASAA0240210 1 20021115 A 5312 651758239 BULKHEAD BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 DURING C-CHECK, FOUND VERTICAL CHORD AT BS 178 BL 17.1 AND WL 182-239 HAS DAMAGED HOLES. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022700059 20030227 00059 NM 2003 2 27 ASAA0240211 1 20021115 A 5347 655384422 CARGO TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 DURING C-CHECK, FOUND CORROSION ON CARGO FLOOR TRACK IN AFT CARGO BAY FROM BS 787-847 AND RBL 14. REPAIRED IAW SRM. (M ) 2 L 7 2 4F RT A16WE 2003022700060 20030227 00060 NM 2003 2 27 ASAA0240212 1 20021115 A 5320 6545 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 DURING C-CHECK, FOUND CORROSION ON STRAP IN AFT CARGO BAY AT BS 771 WL 156 BL 24. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022700062 20030227 00062 NM 2003 2 27 ASAA0240213 1 20021115 A 5320 655572651 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 PAE - DURING C-CHECK, FOUND SIDEWALL TO BULKHEAD SUPPORT CORRODED AT BS 727 RBL 24 AND WL 156. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022700064 20030227 00064 NM 2003 2 27 ASAA0240225 1 20021121 A 5320 6T16300 STIFFENER BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 DURING C-CHECK, FOUND HORIZONTAL STIFFENER AT BS 178 LEFT/RIGHT BL 17-28 AND WL 195 HAS OVERSIZED HOLES. REPAIRED IAW S RM. (M) 2 L 7 2 4F RT A16WE 2003022700079 20030227 00079 NM 2003 2 27 C1HA200281010 1 20021211 A 3350 LIGHT BOEING 727 7272S7 138407Z NM CABIN UNSECURE A C1HA K NONE O OTHER TX TAXI/GRND HDL 1 GL 15 681CA 22020 EXIT SIGN ABOVE ROW 19 (A/C LEFT)- EMERGENCY EXIT LIGHT HAS FALLEN OFF. RESECURED EMERGENCY EXIT SIGN ABOVE ROW 19 AS R EQUIRED. 2 L 7 3 4F A3WE 2003022700080 20030227 00080 NM 2003 2 27 C1HA200283022 1 20021202 A 3397 WIRE BOEING 727 7272S7 138407Z NM CABIN BROKEN A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 683CA 22490 EMERGENCY FLOOR TRACK LIGHTING INOP. REPAIRED BROKE WIRE ON EMERGENCY FLOOR TRACK LIGHTING IAW MM 33-50, OPS CK GOOD. 2 L 7 3 4F A3WE 2003022800036 20030228 00036 NM 2003 2 28 C1HA200284007 1 20021206 A 3260 SWITCH BOEING 727 7272S7 138407Z NM NLG OUT OF ADJUST A C1HA O OTHER N FALSE WARNING DE DESCENT 1 GL 15 684CA 22491 NOSE GEAR DOOR ILLUMINATED DURING DESCENT. ADJUSTED NLG DOOR SWITCHES PER 32-62-11M/M, OPS CK NORMAL. 2 L 7 3 4F A3WE 2003022800037 20030228 00037 NM 2003 2 28 C1HA200294011 1 20021208 A 3150 WARNING SYSTEM BOEING 727 727290 138408W NM COCKPIT ACTIVATED A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 294AS 22146 WHEN APPLYING TAKEOFF POWER, AIRCRAFT TAKEOFF WARNING SOUNDED. ABORTED TAKEOFF. COULD NOT DUPLICATE PROBLEM, TESTED SY STEM PER 727 M/M 31-26-0, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2003022800038 20030228 00038 NM 2003 2 28 C1HA200294012 1 20021209 A 2760 SWITCH BOEING 727 727290 138408W NM COCKPIT OUT OF ADJUST A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 294AS 22146 TAKEOFF WARNING HORN ON T/O. FOUND SPEED BRAKE HANDLE NOT ENGAGING SPEED BRAKE SWITCH CONTACTS WHEN STOWED. ADJUSTED S WITCH. 2 L 7 3 4F A3WE 2003022800040 20030228 00040 NM 2003 2 28 C7WA200200029 1 20021015 A 3411 PITOT TUBE BOEING 727 7272J7 138400E NM PITOT/STATIC SYS OBSTRUCTED A C7WA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 17 128NA 20879 REJECTED TAKEOFF FROM SJC AT 90 KNOTS DUE TO LACK OF AIRSPEED INDICATION ON COPILOTS SIDE. CHECKED PITOT TUBES AND REMO VED INSECT BLOCKAGE FROM F/O PITOT SYSTEM IAW MM 34-11-31. 2 L 7 3 4F A3WE 2003033100095 20030331 00095 2003 3 31 C7WA200200031 4 20021016 A 3417 CONNECTOR BOEING 727 7272J7 138400E NM ADC BROKEN A C7WA O OTHER N FALSE WARNING CL CLIMB 1 SO 17 128NA 20879 DURING FLIGHT, THE NR 1 ALTIMETER FLAG CAME IN VIEW AND STAYED. DIVERTED FLIGHT TO YIP. FOUND PIN 16 ON TOP PLUG OF AI R DATA COMPUTER BROKE. REPAIRED WIRE IAW MM CHAPTER 20. PERFORMED BITE TEST IAW MM 34-12-0 IAW BOEING MM 34-12-0. REF C7WA200200030 - AIRCRAFT DEPARTED YIP, AND HAD AIR DATA INSTRUMENT FAILURE CLIMBING 5000 FT. AIRCRAFT RETURNED TO YIP AND MADE OVERWEIGHT LANDING. (M) 2 L 7 3 4F A3WE 2003022800045 20030228 00045 NM 2003 2 28 C8GA20020013 1 20021206 A 2822 3823002 PUMP BOEING 727 727223 1384074 NM NR 2 FAULTY A C8GA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 15 899AA 3472 22015 FLT 718 FROM STL TO ELP. DURING CLIMBOUT APPROXIMATELY FIFTEEN MINUTES AFTER TAKEOFF NR 2 FUEL TANK CIRCUIT BREAKER FOR THE LEFT FORWARD AND RIGHT AFT FUEL PUMPS POPPED THEIR CIRCUIT BREAKER. ABOUT FIVE MINUTES LATER, THE NR 1 FUEL TANK L EFT FORWARD PUMP CIRCUIT BREAKER POPPED. ALL APPROPRIATE CHECKLIST WERE ACCOMPLISHED, AN EMERGENCY WAS DECLARED, AND TH E AIRCRAFT LANDED SAFELY IN MCI. UPON LANDING, INSPECTED AND DRAINED THE WATER FROM BOTH NR 1 AND NR 2 TANKS, SYSTEM OP S CHECKED GOOD PER MM 28-22-21. AIRCRAFT RETURNED TO SERVICE AND CONTINUE TO ITS FINAL DESTINATION IN ELP AND THE NR 2 LEFT FORWARD BOOST PUMP WAS REPLACED PER MM 28-20-00. 2 L 7 3 4F A3WE 2003022800046 20030228 00046 EU 2003 2 28 CX7A194J21 1 20021005 A 2750 FLAP SAAB SF340 340B 7860101 EU WING OUT OF RIG A CX7A A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 03 300CE 340B184 IN FLIGHT MULTIPLE UNCOMMANDED PITCH CHANGES WITH NO OTHER NOTICEABLE ANOMALIES. FLIGHT DIVERTED TO IND. RIGGED FLAPS IAW SAAB AMM. 2 L 7 2 4T RT A52EU 2003022800047 20030228 00047 WP 2003 2 28 DHL2002807012 1 20021130 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CARGO BAY MALFUNCTIONED A DHLA K NONE N FALSE WARNING NR NOT REPORTED 1 SO 01 807DH 45990 AMBER ANNUNCIATOR ON CARGO COMPARTMENT SMOKE DETECTOR ILLUMINATED IN FLIGHT. CODE AD7515 DISPLAYED. RECONFIGURED LOWER CARGO SDU'S PER SMM 26-15-0. OPS NORMAL. 2 L 7 4 4F RT 4A25 2003022800049 20030228 00049 WP 2003 2 28 DHL2002807014 1 20021210 A 3241 CONNECTOR DOUG DC8 DC873F 302199F WP ANTI-SKID SYS DIRTY A DHLA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 807DH 45990 AFTER GEAR EXTENSION ANTI-SKID INOP LIGHT CAME ON. GEAR WAS CYCLED, THEN WHEN GEAR WAS PUT DOWN AGAIN ANTI-SKID LIGHT R EMAINED EXTINGUISHED. CLEANED CANNON PLUG CONNECTORS AND PERFORMED OPS CHECK OF ANTI-SKID SYSTEM IAW 32-43-4. OPS CHEC KED NORMAL. 2 L 7 4 4F RT 4A25 2003022800052 20030228 00052 CE 2003 2 28 DJFA200200002 1 20021212 A 3260 SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE LT MLG OUT OF ADJUST E DJFA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 23 866CW 258466 AIRCRAFT ON LANDING HAD LEFT HAND MAIN GEAR UNSAFE LIGHT, BUT ALSO HAD A GREEN LOCK LIGHT AT THE SAME TIME. CREW DECLAR ED AN EMERGENCY AND LANDED WITH NO PROBLEM. THE LANDING GEAR WAS REPAIRED BY ADJUSTING THE LEFT MAIN LANDING GEAR DOOR SWITCH. 2 L 7 2 4F RT A3EU 2003022800057 20030228 00057 NM 2003 2 28 ASAA0240226 1 20021121 A 5320 6741511 BRACKET BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 DURING C-CHECK, FOUND BRACKETS AT BS 178 RIGHT BL 17-23 AND LEFT BL 25 AND WL 25 HAVE OVERSIZED HOLES. REPAIRED IAW SRM . (M) 2 L 7 2 4F RT A16WE 2003022800058 20030228 00058 NM 2003 2 28 ASAA0240227 1 20021121 A 5320 69429494 CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 DURING C-CHECK, FOUND FRAME CLIP AT BS 807, RIGHT BL 20 IS CRACKED IN AFT CARGO BAY. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022800059 20030228 00059 NM 2003 2 28 ASAA0240228 1 20021121 A 5320 6741517 BRACKET BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 DURING C-CHECK, FOUND BRACKET AT BS 178 RBL 25 AND WL 195 HAS OVERSIZED HOLES. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022800060 20030228 00060 NM 2003 2 28 ASAA0240229 1 20021121 A 5311 651758240 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A K NONE O OTHER IN INSP/MAINT 1 NM 01 772AS 25105 DURING C-CHECK, FOUND FRAME AT BS 178 RBL 17 AND WL 182-239 HAS OVERSIZED HOLES. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2003022800061 20030228 00061 WP 2003 2 28 ASAA0280480 1 20021029 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT MODULE BROKEN NEAR FORWARD GALLEY. REPLACED MODULE. LIGHTS T HEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003022800062 20030228 00062 WP 2003 2 28 ASAA0280518 1 20021104 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 ANC - FOUND DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHT MODULE BROKEN IN FORWARD CABIN. RECONNECTED MODULE. LIGHTS T HEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2003022800063 20030228 00063 WP 2003 2 28 ASAA0280616 1 20021130 A 3350 0105606 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 SJC - DURING PREFLIGHT CHECK, THE EMERGENCY TRACK LIGHTING IN FIRST CLASS CABIN WAS INOPERATIVE. RECONNECTED LOOSE CONN ECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2003022800064 20030228 00064 WP 2003 2 28 ASAA0280702 1 20021230 A 5754 9954169U45 DOOR DOUG DC9 DC983 3022083 WP L/E SLAT GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, NR 3 LEFT SLAT TRACK DOOR NR 9 IS GOUGED/CHAFED ON TOP EDGE. REPLACED SLAT TRACK DOOR PER SRM 51-10-4 AND 51-30-8. (M) 2 L 7 2 4F RT A6WE 2003022800065 20030228 00065 WP 2003 2 28 ASAA0280703 1 20021230 A 5311 5936597U509 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FRAME ASSEMBLY CORRODED AT FS 1211. REPLACED FRAME PER SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003022800066 20030228 00066 WP 2003 2 28 ASAA0280704 1 20021230 A 5320 993061269 SILL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, AFT SERVICE (L-2) DOOR SILL PAN IS CORRODED. REPLACED SILL PER SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003022800067 20030228 00067 WP 2003 2 28 ASAA0280705 1 20021230 A 5320 593607018 THRESHOLD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, AFT CARGO BAY THRESHOLD CORRODED ON UNDERSIDE AT FS 1155. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2003022800068 20030228 00068 WP 2003 2 28 ASAA0280706 1 20021230 A 5312 593659215 BULKHEAD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, BULKHEAD SUPPORT CRACKED IN MID CARGO BAY AT FS 529. REPLACED BULKHEAD PER SRM 51-10-4 AN D 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003022800069 20030228 00069 WP 2003 2 28 ASAA0280707 1 20021230 A 5320 993658045 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, INTERCOSTAL CRACKED BETWEEN FLOORBEAMS AT FS 1287-1309. REPLACED INTERCOSTAL PER 51-10-1, 51-10-2, 51-10-4, 51-30-5, AND DAC DWG 9936580. (M) 2 L 7 2 4F RT A6WE 2003022800070 20030228 00070 WP 2003 2 28 ASAA0280708 1 20021231 A 5320 3936409U505 CLIP DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, TEE CLIP ON EXTERNAL KEEP PLANK CRACKED AT FS 875. REPLACED TEE CLIP PER SRM 51-30-5. (M ) 2 L 7 2 4F RT A6WE 2003022800071 20030228 00071 WP 2003 2 28 ASAA0280709 1 20021231 A 5320 593607021 CLIP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, THRESHOLD PLATE FORWARD RADIUS CLIP CORRODED IN AFT CARGO BAY. REPLACED PLATE PER SRM 51- 30-5. (M) 2 L 7 2 4F RT A6WE 2003022800073 20030228 00073 WP 2003 2 28 ASAA0280710 1 20021231 A 5260 59159251 STEP DOUG DC9 DC983 3022083 WP AIRSTAIRS GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, STAIRCASE GOUGED TOP FORWARD. INSTALLED DOUBLER PER SRM 52-01. (M) 2 L 7 2 4F RT A6WE 2003022800074 20030228 00074 WP 2003 2 28 ASAA0280711 1 20021231 A 5320 993061285 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOND DURING 30K CHECK, LEFT CUSP WEB CORRODED AT FS 1250. REPLACED CUSP WEB PER SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003022800075 20030228 00075 WP 2003 2 28 ASAA0280712 1 20021231 A 5320 99512522 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, EXTERNAL ATTACH ANGLE CRACKED AT FS 807. REPLACED ATTACH ANGLE PER SRM 51-10-2, 51-10-4, 51-30-2, 51-30-5, AND DAC DWG 991252. (M) 2 L 7 2 4F RT A6WE 2003022800076 20030228 00076 WP 2003 2 28 ASAA0280713 1 20021223 A 5730 5937468501 SKIN DOUG DC9 DC982 3022082 WP LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 OAK - DURING C-CHECK, LEFT WING FORWARD SPAR HAS CRACK IN LEADING EDGE SKIN LOWER SURFACE FROM ACCESS DOOR FLANGE FORWAR D BETWEEN NR 2 AND NR 3 SLAT TRACKS IN AREA OF PREVIOUSLY INSTALLED DOUBLER. INSTALLED NEW DOUBLER BETWEEN SLAT TRACKS PER SRM 51-10-3 AND EA 5730-01094. (M) 2 L 7 2 4F A6WE 2003022800077 20030228 00077 WP 2003 2 28 ASAA0280714 1 20021231 A 5311 991960551 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FORMER IS CORRODED AT FS 1271. REPLACED DAMAGED SECTION OF FORMER PER SRM 53-14-3, 53-03, 51-30-2, AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003022800106 20030228 00106 WP 2003 2 28 CNMA200200007 1 20021220 A 3260 806125 ELECTRICAL BOX DOUG DC10 DC1030 3023501 WP A CNMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 07 59083 47926 Overspeed warning sounded at 270 knots - slats confirmed retracted. Removed and replaced Proximity Electronic Unit. Bite test normal. 2 L 7 3 4F A22WE 2003030300025 20030303 00025 NM 2003 3 3 HNAA0200074 1 20021031 A 3350 1013075 SOCKET DHAV DHC8 DHC8201 2809001 NM CABIN BROKEN A HNAA K NONE L NO TEST UK UNKNOWN 1 EA 07 992HA 16194 16194 432 THREE FORWARD FLOOR EMERGENCY LIGHTS AND SECOND FROM FRONT OVERHEAD EMERGENCY LIGHT INOP. REPLACED FIRST 2 LIGHT SOCKET S ON FLOOR AND REPLACED BULBS ON THE OTHER TWO LIGHTS, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2003030300027 20030303 00027 NM 2003 3 3 HNAA0200075 1 20021105 A 3010 BOOT DHAV DHC8 DHC8102 2809003 NM RT WING CONTAMINATED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 912HA 040 ON CLIMBOUT DEICE PRESSURE DROPPED TO 10 PSI FOLLOWED BY ILLUMINATION OF THE DEICE PRESSURE CAUTION LIGHT. RT WING SECO ND BOOT FROM TIP AND ALL TAIL BOOTS WOULD NOT SHOW INFLATION. AIRCRAFT RETURNED TO FIELD. MAINTENANCE PURGED WATER FRO M SYSTEM. GROUND CHECK GOOD. 2 H 7 2 4T RT A13NM 2003030300030 20030303 00030 NE 2003 3 3 HNAA0200077 3 20021110 A 6111 8022241 BEARING RACE DHAV DHC8 DHC8311 1386006 EA HAMSTD 14SF 14SF23 NE NR 2 PROPELLER BROKEN A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 343EN 13914 4025 340 980910 NOISE COMING FROM NR 2 PROPELLER WHEN ROTATING. REPLACED NR 2 PROPELLER ASSEMBLY. DISASSEMBLY SHOWED DAMAGE TO THE NR 2 BLADE AND ITS SPLIT RING BEARING RACE. APPROXIMATELY ONE INCH OF MATERIAL HAS CRACKED/BROKEN AWAY FROM THE END OF ONE BEARING SPLIT RING HALF. FIVE BLADE BEARINGS WERE LOOSE INSIDE THE PROP HUB. 2 H 7 2 4T RT A13NM 6 C P7NE 2003030300032 20030303 00032 NE 2003 3 3 HNAA0200079 2 20021111 A 7310 ST3367009 O-RING DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 ENGINE DETERIORATED A HNAA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 07 804SA 1345 375 123260 DURING MAINTENANCE WALK AROUND, FUEL WAS OBSERVED LEAKING FROM THE NUMBER 2 NACELLE. WET MOTORING THE ENGINE SHOWED THE FUEL TO BE COMING FROM THE FUEL NOZZLE TRANSFER TUBES. UPON REMOVAL OF THE TRANSFER TUBES THE PRIMARY AND SECONDARY O- RINGS WERE FOUND TO BE SEVERELY DETERIORATED. REPLACED O-RINGS. 2 H 7 2 4T 4 T RT A13NM E20NE 2003030300036 20030303 00036 EU 2003 3 3 MALA030153 1 20020212 A 3150 WARNING SYSTEM SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 GL 15 360PX 340B220 DURING TAKEOFF OF FLIGHT NR 3076, BITE LIGHT ILLUMINATED, LIGHT REMAINS ON AFTER LANDING. AIR RETURN TO DTW. MAINTENAN CE COULD NOT DUPLICATE PROBLEM ON THE GROUND. REMOVED AND REPLACED WEU ASSEMBLY FOR PRECAUTIONARY MEASURE. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2003030300040 20030303 00040 NE 2003 3 3 NAFA2002001 2 20021205 A 8530 356993 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800* 52026 NE NR 3 ENGINE CRACKED I N32B E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 01 7780B 1109 1109 45372 NK510101 NR 3 ENGINE PRECAUTIONARY SHUT DOWN FOR A NR 2 CYLINDER SHORTED SECONDARY. REPLACED NR 2 CYLINDER. 2 L 7 4 4R 4 R A781 5E8 2003030300042 20030303 00042 NM 2003 3 3 O2102801 1 20021023 A 3350 LIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A N8TA K NONE L NO TEST IN INSP/MAINT 1 WP 19 549NA 24544 FOUND FIRST THREE FLOOR EMERGENCY EGRESS LIGHTS OUT NEAR LAVATORY F. RELAMPED, OPS CHECK NORMAL AS PER M/M 33-51-11. 2 L 7 2 4F RT A2NM 2003030300044 20030303 00044 NM 2003 3 3 QXEA0300258 1 20020212 A 7110 SUPPORT ANGLE BOMBDR DHC8 DHC8401 1390041 NM NR 1 COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - NR 1 ENGINE LOWER COWL: LEFT HAND SUPPORT ANGLE NEXT TO BYPASS DOOR CRACK AT FORWARD ATTACHMENT. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2003030300048 20030303 00048 CE 2003 3 3 RB23 1 20021011 A 3260 39EN2226 SQUAT SWITCH RAYTHN 390 390 CE RT MLG DISCONNECTED E ERYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 488PC 339 18 RB23 UPON DEPARTURE FROM ADDISON TX LANDING GEAR HANDLE WAS UP BUT RED LIGHT WAS ILLUMINATED. GEAR APPEARED TO NOT HAVE RETR ACTED. GEAR SUBSEQUENTLY RETRACTED, BUT UPON FURTHER TESTING WOULD NOT EXTEND. DIVERTED TO SAN ANTONIO SAT AND USED AL TERNATE GEAR EXTENSION. THE NLG AND LT MLG SHOWED DOWN AND LOCKED. RT MLG DID NOT SHOW CORRECT DOWN AND LOCKED INDICAT ION, NO GREEN LIGHT. PERFORMED CHECKLIST AND RESET LANDING GEAR CIRCUIT BREAKER. ALL THREE DOWN AND LOCKED LIGHTS ILLU MINATED, AND TOWER FLYBY CONFIRMED GEAR APPEARED NORMAL. GEAR FUNCTIONED NORMALLY. FOUND RT MAIN LANDING GEAR SQUAT SW ITCH DISCONNECTED DUE TO MISSING SAFETY PIN AND NUT THAT RETAINS CLEVIS PIN FOR SQUAT SWITCH ACTUATOR. 1 7 2 3F RT A00010WI 2003030300051 20030303 00051 NM 2003 3 3 SABA020094 1 20020923 A 3240 DSC252A40230 LINE DHAV DHC8 DHC8103 1386005 NM LT MLG BROKEN A SABA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 33 883CC 162 AIRCRAFT 883 FLIGHT 5018 FROM CLT TO PGV: DURING TAXI OUT PILOT REPORTED LOSING NUMBER TWO HYD SYSTEM. AIRCRAFT WAS TO WED BACK TO GATE. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE LEFT OUTBOARD BRAKE PRESSURE LINE BROKEN. BRAKE LI NE WAS REMOVED AND REPLACED. SYSTEM WAS BLEED AND OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003030300086 20030303 00086 EA 2003 3 3 SWIA200211585 1 20021122 A 5320 6013501252 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 498SW 7483 FS 625.0 RT STR 14 INTERCOSTAL ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51 -42-06 & RII 53-401. 2 L 7 2 4F RT A21EA 2003030300091 20030303 00091 EA 2003 3 3 SWIA200211586 1 20021122 A 5320 601R53611171 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 498SW 7483 FS 621 LT FLOOR SUPPORT ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601-53-61-117. 2 L 7 2 4F RT A21EA 2003030300093 20030303 00093 EA 2003 3 3 SWIA200211587 1 20021122 A 5315 601R3111358 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 498SW 7483 FS 280 RBL 9.0 INBOARD FLOORBEAM ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06 & 51-42-21 USING ORIGINAL HARDWARE. 2 L 7 2 4F RT A21EA 2003030300094 20030303 00094 EA 2003 3 3 SWIA200211588 1 20021122 A 5320 601R311719 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 498SW 7483 FS 484.0 RT INTERCOSTAL INBOARD ANGLE RBL 27.0 CRACKED. FOUND DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ REO 60 1R-53-41-059. 2 L 7 2 4F RT A21EA 2003030300097 20030303 00097 EA 2003 3 3 SWIA200211590 1 20021111 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 FS 280 LBL 9.0 FLOORBEAM INBOARD AND OUTBOARD ANGLES ARE CRACKED. FOUND DURING C-CHECK INSPECTION. FIT AND INSTALLED N EW CLIPS (ANGLES) IAW CRJ REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2003030300100 20030303 00100 EA 2003 3 3 SWIA200211591 1 20021111 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 FS 280 RBL 9.0 FLOORBEAM INBOARD AND OUTBOARD ANGLES CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED INBOARD AND OU TBOARD ANGLES IAW CRJ SRM 51-40-11, 51-42-21, 51-42-13, 51-42-06 AND REO 601R-53-11-171 REV NC. 2 L 7 2 4F RT A21EA 2003030300111 20030303 00111 SO 2003 3 3 SWIA200211600 1 20021113 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 188SW 120039 RIGHT WING LOWER STRINGER 10 IS CRACKED. FOUND DURING C-CHECK INSPECTION. COMPLIED WITH SB120-57-0037, REPLACEMENT OF STRINGERS NR 8 AND 10, LOWER RIGHT SIDE. 2 L 7 2 4T 4 T RT A31SO E20NE 2003030300143 20030303 00143 2003 3 3 ASAA0280665 4 20021220 A 2565 3961899501 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 SJC - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2003030300144 20030303 00144 2003 3 3 ASAA0280666 4 20021222 A 2565 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 LAS - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M) 2 L 7 2 4F RT A6WE 2003030300145 20030303 00145 WP 2003 3 3 ASAA0280668 1 20021223 A 5230 592600317 ROD DOUG DC9 DC983 3022083 WP BARRIER DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, AFT CARGO COMPARTMENT BARRIER DOOR ASSEMBLY AFT HOLDUP SPEAR IS CRACKED. REPLACED SPEAR P ER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003030300146 20030303 00146 WP 2003 3 3 ASAA0280669 1 20021223 A 5320 993653429 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED IN CABIN AT FS 200. REPLACED SUPPORT PER SRM 53-14-1, 51-10-2, 51- 10-4, AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2003030300147 20030303 00147 WP 2003 3 3 ASAA0280671 1 20021223 A 5321 993654759 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOORBOARD SKIN CRACKED AT FS 212. REPLACED FLOORBOARD SECTION PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003030300148 20030303 00148 WP 2003 3 3 ASAA0280672 1 20021224 A 5321 995791819 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 20K CHECK, FLOOR PANEL CRACKED AT OUTBOARD SIDE FS 465-541. REPLACED FLOOR PANEL PER SRM 51-70-5, 51 -60-0 AND 53-24-0. (M) 2 L 7 2 4F RT A6WE 2003030300149 20030303 00149 WP 2003 3 3 ASAA0280673 1 20021224 A 5321 99365853 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR PANEL IS PUNCTURED AT FS 1003-1071. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2003030300150 20030303 00150 WP 2003 3 3 ASAA0280674 1 20021224 A 5320 5936667 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, INTERCOSTAL BETWEEN LONGERON 26L-27L GOUGED AT FS 1322. REPLACED INTERCOSTAL PER SRM 51-1 0-2, 51-10-4, 51-30-2, AND DAC DWG 5936667. (M) 2 L 7 2 4F RT A6WE 2003030300151 20030303 00151 WP 2003 3 3 ASAA0280675 1 20021224 A 5321 99366395 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOORBOARD HAS TORN METAL AT 'W' SANDWICH EXTRUSION AT FS 886-946. REPLACED SUPPORT SECTI ON PER SRM 51-30-8, 51-20-0, AND 51-10-4. (M) 2 L 7 2 4F RT A6WE 2003030300152 20030303 00152 WP 2003 3 3 ASAA0280676 1 20021224 A 5321 99366393 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 20K CHECK, FLOORBOARD HAS TORN METAL AT 'W' SANDWICH EXTRUSION AT FS 826-886. REPLACED SUPPORT SECTI ON PER SRM 51-30-8, 51-20-0, AND 51-10-4. (M) 2 L 7 2 4F RT A6WE 2003030300153 20030303 00153 WP 2003 3 3 ASAA0280677 1 20021224 A 5311 593657505 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FRAME CORRODED AT FS 1155, LONGERON 27L-27R. REPLACED FRAME PER SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003030300154 20030303 00154 WP 2003 3 3 ASAA0280678 1 20021224 A 5730 59626033 PANEL DOUG DC9 DC983 3022083 WP LT WING CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT WING FORWARD ROCK DEFLECTOR PANEL IS WORN/CHAFED AT EDGES. REPAIRED WITH DOUBLER PER SRM 51-30-2 AND 51-70-4. (M) 2 L 7 2 4F RT A6WE 2003030300155 20030303 00155 WP 2003 3 3 ASAA0280679 1 20021224 A 5755 39615971 ACCESS PANEL DOUG DC9 DC983 3022083 WP SPOILER CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT INBOARD FLIGHT SPOILER ACCESS PANEL 1526 IS CRACKED. REPLACED PANEL PER SRM 51-30-1. (M) 2 L 7 2 4F RT A6WE 2003030300156 20030303 00156 WP 2003 3 3 ASAA0280680 1 20021224 A 5347 S00062 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, SIX CLIP NUT HOLES ARE CORRODED ON MID CARGO BAY TRACK AT FS 522-561. REPLACED DAMAGED SE CTION PER SRM 53-24-0 AND 53-05. (M) 2 L 7 2 4F RT A6WE 2003030300157 20030303 00157 WP 2003 3 3 ASAA0280681 1 20021224 A 5311 99360734 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, SHEAR TIE FRAME CORRODED AT FS 1155. REPLACED FRAME PER SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003030300158 20030303 00158 WP 2003 3 3 ASAA0280682 1 20021224 A 5321 59305621 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOORBOARD HAS ONE PUNCTURE, 50 DENTS, AND DISBONDING AT BOTH ENDS OF LOWER STIFFENERS AT FS 825. INSTALLED DOUBLERS ON LOWER STIFFENER PER SRM 51-70-2 AND 53-05. (M) 2 L 7 2 4F RT A6WE 2003030300159 20030303 00159 WP 2003 3 3 ASAA0280683 1 20021224 A 5321 59305621 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOORBOARD HAS ONE PUNCTURE, ONE DENT, AND DISBONDING AT ENDS OF LOWER STIFFENER AT FS 826 -927. INSTALLED DOUBLERS ON LOWER STIFFENER AND REBONDED ENDS PER SRM 51-70-2 AND 53-05. (M) 2 L 7 2 4F RT A6WE 2003030300160 20030303 00160 WP 2003 3 3 ASAA0280684 1 20021224 A 5320 993053815 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB CORRODED AT FS 313-370. INSTALLED DOUBLER ON WEB PER SRM 53-14-2, 53-01, 51 -70-4, AND 51-30-1. (M) 2 L 7 2 4F RT A6WE 2003030300161 20030303 00161 WP 2003 3 3 ASAA0280685 1 20021228 A 5321 NAS43DD370FC INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, AFT SERVICE L-2 DOOR EMERGENCY SLIDE GIRT BAR FITTING INSERTS ARE CORRODED. REPLACED FOUR INSERTS PER SRM 51-30-1. (M) 2 L 7 2 4F RT A6WE 2003030300162 20030303 00162 WP 2003 3 3 ASAA0280686 1 20021228 A 5321 993654511 INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR PANEL INSERTS ARE CORRODED AT FS 160-200. REPLACED PANEL WITH NEW INSERTS PER SRM 5 3-24-0 AND 53-05. (M) 2 L 7 2 4F RT A6WE 2003030300163 20030303 00163 WP 2003 3 3 ASAA0280687 1 20021228 A 5321 9936545503 INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR PANEL INSERTS ARE CORRODED AT FS 160-180. REPLACED PANEL WITH NEW INSERTS PER SRM 5 3-24-0 AND 53-05. (M) 2 L 7 2 4F RT A6WE 2003030300164 20030303 00164 WP 2003 3 3 ASAA0280688 1 20021228 A 5321 SLS5128A3400 INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR PANEL INSERTS ARE CORRODED AT FS 180-200. REPLACED PANEL WITH NEW INSERTS PER SRM 5 3-24-0 AND 53-05. (M) 2 L 7 2 4F RT A6WE 2003030300165 20030303 00165 WP 2003 3 3 ASAA0280689 1 20021228 A 5321 9952523501 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR PANEL INSERTS ARE CORRODED AT FS 200-256. REPLACED PANEL WITH NEW INSERTS PER SRM 5 3-24-0 AND 53-05. (M) 2 L 7 2 4F RT A6WE 2003030300166 20030303 00166 WP 2003 3 3 ASAA0280690 1 20021228 A 5320 993061215 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB CORRODED AT FS 1022-1071. REPLACED CUSP SECTION AND INSTALLED DOUBLER PER S RM 51-30-2, 51-30-5, AND 51-70-4. (M) 2 L 7 2 4F RT A6WE 2003030300167 20030303 00167 WP 2003 3 3 ASAA0280691 1 20021228 A 5321 9936551509 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR PANEL HAS CORRODED INSERTS AT FS 200-256. REPLACED PANEL WITH NEW INSERTS PER SRM 5 3-24-0 AND 53-05. (M) 2 L 7 2 4F RT A6WE 2003030300168 20030303 00168 WP 2003 3 3 ASAA0280692 1 20021228 A 5347 SR095301157003 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, SEAT TRACK CORRODED AT FS 1148-1164. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER SRM 53 -05, 51-10-4, 51-30-1, 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003030300169 20030303 00169 WP 2003 3 3 ASAA0280693 1 20021228 A 5321 995252112 RIB DOUG DC9 DC983 3022083 WP FLOOR PANEL CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND 30K CHECK, FLOOR PANEL HAS A CRACKED RIB AT FS 465-541. CUT OUT AND REPLACED DAMAGED SECTION PER SRM 51-70- 5, 53-24-0, AND 51-60-0. (M) 2 L 7 2 4F RT A6WE 2003030300170 20030303 00170 WP 2003 3 3 ASAA0280694 1 20021228 A 5321 99365853 RIB DOUG DC9 DC983 3022083 WP FLOOR PANEL WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR PANEL RIB WORN IN 6 PLACES AT FS 1003-1098. REPLACED DAMAGED SECTION PER SRM 51-70- 5, 53-24-0, AND 51-60-0. (M) 2 L 7 2 4F RT A6WE 2003030300171 20030303 00171 WP 2003 3 3 ASAA0280695 1 20021228 A 2560 39361902 FITTING DOUG DC9 DC983 3022083 WP CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FORWARD SERVICE (R-1) DOOR EMERGENCY SLIDE GIRT BAR FLOOR FITTING IS CORRODED AT FS 160. REPLACED FITTING PER SRM 51-30-1. (M) 2 L 7 2 4F RT A6WE 2003030300172 20030303 00172 WP 2003 3 3 ASAA0280696 1 20021228 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 180-192. REPLACED FLOOR SUPPORT PER SRM 51-10-2, 51-10-4, 51 -30-1, 51-30-2, AND DAC DWG 9936534. (M) 2 L 7 2 4F RT A6WE 2003030300173 20030303 00173 WP 2003 3 3 ASAA0280697 1 20021228 A 5321 99366543 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR PANEL HAS CORRODED INSERTS AT FS 1071-1155. REPLACED FLOOR PANEL WITH NEW INSERTS P ER SRM 53-24-0 AND 53-05. (M) 2 L 7 2 4F RT A6WE 2003030300174 20030303 00174 WP 2003 3 3 ASAA0280698 1 20021228 A 5321 99366523 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, FLOOR PANEL DELAMINATED AT FS 1146-1250. REPLACED FLOOR PANEL PER SRM 53-24-0 AND 53-05. (M) 2 L 7 2 4F RT A6WE 2003030300176 20030303 00176 WP 2003 3 3 ASAA0280700 1 20021230 A 5320 9936534107 STRAP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, AFT SERVICE (L-2) DOOR SCUFF PLATE STRAP WAS CORRODED. REPLACED STRAP PER SRM 51-10-2, 51 -10-4, 51-30-1, AND DAC DWG 993654. (M) 2 L 7 2 4F RT A6WE 2003030300177 20030303 00177 WP 2003 3 3 ASAA0280701 1 20021230 A 5530 991196213 FRAME DOUG DC9 DC983 3022083 WP VERTICAL STAB CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - FOUND DURING 30K CHECK, JACKSCREW ACCESS PANEL ON THE VERTICAL STABILIZER HAS CHAFED FRAME MATING FACE. REPLACED FRAME PER SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2003030300179 20030303 00179 NM 2003 3 3 AALA20021882 1 20021219 A 2421 IDG BOEING 767 767323 1385205 NM RT ENGINE MALFUNCTIONED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 39364 24045 RIGHT GEN DRIVE LIGHT ILLUMINATED STEADY DURING CRUISE PERFORMED ABNORMAL PROCEDURE AND DISCONNECTED DRIVE RT IDG VALVE EICAS ALSO DISPLAYED. RECONNECTED RIGHT IDG AND SERVICED IDG. C/OUT BPCU BITE TEST AND RAN ENGINE ALL INDICATIONS NORM AL. IDG OPS NORMAL. (M) 2 L 7 2 4F RT A1NM 2003031400021 20030314 00021 NM 2003 3 14 S02425050 1 20021229 A 2530 416100149 COFFEEMAKER BOEING 747 747400 NM PWA 4056 PW4056 NE GALLEY 3 FAILED W SAJF O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 03 28712 B-18205 LIGHT SMOKE FROM COFFEE MAKER IN GALLEY 3 C/B PULLED SYS ISOL. INSPECT C/B PANEL AND COFFEE MAKER CONNECTOR WIR ING CONDITION IS NML. REPLACE 809B COFFEE MAKER AND FUNCTION CK NML. SIT WAS FILLED FOR THE OFF COFFEE MAKER. 2 L 7 4 4F 4 F RT A20WE E24NE 2003030500015 20030305 00015 NE 2003 3 5 C1HA200285015 2 20021229 A 7261 FILTER BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE ENGINE DRAIN LOOSE A C1HA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 15 685CA 22492 SMOKE REPORTED FROM ENGINE NR 2 AFTER LANDING. INSPECTED FOUND LOOSE DRAIN FILTER AND TORN DRAIN SCUPPER. TIGHTENED FI TTINGS, OPS CHECKED ENGINE AT IDLE. NO LEAKS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 2003030500016 20030305 00016 NM 2003 3 5 C1HA200288019 1 20021214 A 2613 OVERHEAT SENSOR BOEING 727 7272S7 138407Z NM AFT BODY WILL NOT TEST A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 688CA 22344 LOWER AFT BODY HEAT LIGHT DOESN'T TEST. INSPECTED CONNECTIONS AND RAN TEST OVERHEAT. SYSTEM OPS CHECK NORMAL IAW M/M 2 6-14-0 PAGE 501. 2 L 7 3 4F A3WE 2003030500017 20030305 00017 NM 2003 3 5 C1HA200288020 1 20021231 A 3350 LIGHT BOEING 727 7272S7 138407Z NM LT OVERWING INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 688CA 22344 LT OVERWING EMERGENCY LIGHT (AFT NR 3 POSITION) INOPERATIVE. RELAMPED LIGHT ASSY, REMOVED AND REPLACED BATTERY PACK AS PER MM 33-51-01, OPS CHECKED NORMAL. (P) 2 L 7 3 4F A3WE 2003030500018 20030305 00018 NE 2003 3 5 C1HA200296017 2 20021214 A 7261 OIL FILTER BOEING 727 7272J4 1384006 NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE BYPASSING A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 696CA 22574 ABORTED TAKEOFF DUE TO NR 2 ENGINE OIL BYPASS LIGHT ILLUMINATED. REMOVED AND INSPECTED NR 2 ENGINE MAIN OIL FILTER IAW M/M 72-61-08, LEAK AND OPS CHECK GOOD. FOUND SOME CARBON DEPOSITS IN FILTER. (P) 2 L 7 3 4F 4 F RT A3WE E2EA 2003030700082 20030307 00082 SW 2003 3 7 2003F00118 1 20021125 A 2120 ODOR SWRNGN SA227 SA227AC 8780603 SW COCKPIT DETECTED A BSAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 05 60NE 760B GGW - FLT 2568 - CREW REPORTED STRONG FOREIGN ODOR IN COCKPIT. RAN AIRCRAFT ON GROUND FOR APPROXIMATELY 30 MINUTES. UN ABLE TO SMELL OR FEEL ANY HEAT. COULD NOT DUPLICATE WRITE-UP. PERFORMED OPERATIONAL CHECK FLIGHT FOR APPROXIMATELY 20 MINUTES. CHECK FLIGHT OK. (M) 2 L 7 2 4T RT A8SW 2003030700094 20030307 00094 NE 2003 3 7 2003F00124 2 20021209 A 7250 312011201 TURBINE BLADES BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE FAILED A GUUA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 17 16540 UE172 114329 FLT 9139 - FLL/FPO - DURING TAKEOFF ROLL, HEARD A LOUD THUMP NOISE FROM LEFT ENGINE. ABORTED TAKEOFF. DETERMINED LEFT POWER SECTION SEIZED. REMOVED AND REPLACED LEFT ENGINE ASSEMBLY. TEARDOWN REPORT REVEALED THAT SECOND STAGE POWER TURB INE BLADES FAILED. POWER SECTION AND GAS GENERATOR MODULES INCURRED SUBSTANTIAL DAMAGE. THE POWER PLANT, GAS GENERATOR AND POWER SECTION MODULES, WAS DETERMINED TO BE BEYOND ECONOMICAL REPAIR. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 2003030700100 20030307 00100 NM 2003 3 7 AALA20020014A 1 20021226 A 2120 ODOR BOEING 777 777223 1385213 NM CABIN DETECTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 758AN 32637 EICAS BACKUP GENERATOR BOTH BACKUPS OFF. VERY STRONG ELECTRICAL FUMES THROUGH OUT CABIN AND COCKPIT. TURNED OFF BUT NO T BACKUP GENS, ELECT FUMES RETURNED 15 MINUTES LATER AND TURNED OFF IFE/PAX SEATS CABIN UTILITY SMELL WENT AWAY. STARTE D APU NO PROBLEM. (M) 2 L 7 2 4F RT T00001SE 2003030700101 20030307 00101 WP 2003 3 7 AALA20021363 1 20020925 A 5200 BEAM DOUG DC9 DC982 3022082 WP DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 TUL - FOUND AFT END OF TOP HORIZONTAL BEAM IS CRACKED. INSTALLED BEAM MODIFICATION PER ESO 80172. (M) 2 L 7 2 4F A6WE 2003030700103 20030307 00103 EU 2003 3 7 AALA20021801 1 20021215 A 2761 233009 ACTUATOR FOKKER F28 F28MK0100 4990807 EU SPEED BRAKE LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 1450A 11459 ORD - FLT 1613 - EN ROUTE PHL-ORD, ON DESCENT HAD SYSTEM 1 HYDRAULIC QUANTITY LOW MESSAGE AND FAULT LIGHT. COMPLETED PR OCEDURE WITH MANUAL FLAP AND GEAR EXTENSION. LANDED ORD WITHOUT INCIDENT. REPLACED RIGHT SPEED BRAKE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2003030700105 20030307 00105 NM 2003 3 7 AALA20021878 1 20021228 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 195AN 32389 DFW - EMERGENCY PATH LIGHT ON SEAT 24D INOPERATIVE. REPLACED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003030700106 20030307 00106 NM 2003 3 7 AALA20021881 1 20021219 A 2421 GEN5103 IDG BOEING 767 767223 1385123 NM LT ENGINE FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 316AA 22318 LEFT GEN DRIVE LEFT CAME ON 30 MINUTES INTO FLIGHT WITH ASSOCIATED ICAS MESSAGE DISCONNECTED LEFT IDG IAW QRH PROCEDURES APU STARTED AND RAN FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED LEFT IDG PER MM, OPS CHECK AND LEAK CHECK GOOD PER M M. (M) 2 L 7 2 4F RT A1NM 2003030700107 20030307 00107 EU 2003 3 7 AALA20021892 1 20021228 A 2910 COUPLING FOKKER F28 F28MK0100 4990807 EU HYD SYSTEM DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS CR CRUISE 1 SW 21 1444N 11447 DFW - FLT 1024 - EN ROUTE MEM-DFW, LOST SYSTEM 1 HYDRAULIC QUANTITY, SHUT OFF PUMPS. EMERGENCY EXTENDED LANDING GEAR. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED QUICK DISCONNECT COUPLING AND O-RING ON PRESSURE AND SUCTION PORTS ON LEF T ENGINE NR 1 SYSTEM HYDRAULIC PUMP. PERFORMED ENGINE RUN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2003030700108 20030307 00108 NM 2003 3 7 AALA20021895 1 20021226 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 631AA 24589 MIA - ROW 27 SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED 27D SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003030700109 20030307 00109 NM 2003 3 7 AALA20021896 1 20021230 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 645AA 24603 MIA - L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RESECURED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2003030700111 20030307 00111 NM 2003 3 7 AALA20021915 1 20021220 A 5512 SKIN BOEING 767 767223 1385123 NM HORIZ STAB DELAMINATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AA 22331 AFW - LEFT OUTBOARD LOWER L/E AT STATION 160 ULTRA SOUND INSPECTION FOND A DELAMINATION INDICATION. TAP TEST GOOD REQUE ST ENGINEERING APPROVAL TO CONTINUE AS IS. REPEAT INSPECTION EACH MBV TO RFS NR KK02-0021. 2 L 7 2 4F RT A1NM 2003030700112 20030307 00112 WP 2003 3 7 AALA20021916 1 20021218 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 258AA 49288 TUL - FOUND CORROSION ON FORWARD CX PAN STATION 370 TO 427. REMOVED AND REPLACED PAN PER SRM 53-05 FIG NR 44. (M) 2 L 7 2 4F A6WE 2003030700113 20030307 00113 WP 2003 3 7 AALA20021917 1 20021218 A 5320 STRAP DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 258AA 49288 TUL - FOUND GOUGE IN FRAME STRAP STATION 1147 ABOVE L28R. INSTALLED NEW STRAP PER SRM 53-01-00. (M) 2 L 7 2 4F A6WE 2003031200040 20030312 00040 GL 2003 3 12 0072686 3 20020925 A 6114 C32661 HUB F3YR2UF BEECH 60 60 1153602 CE HARTZL HCF3Y HCF3YR2 GL PROPELLER CORRODED B EY2R K NONE O OTHER IN INSP/MAINT 1 GL 03 DA240 DA240 CORRISION ON PROPELLER HUB. 1 L 7 2 3O A12CE 5 C P31EA 2003031300029 20030313 00029 WP 2003 3 13 GTIA021255 1 20021117 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LB L 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 5 79 REPAIR. INSTALLED -3, -7, -11 ANGLES AND PLATES FS 579. FABRICATED REPAIR PARTS -3, -7, AND -11 FOR FS 541. INSTAL LED REPAIR PARTS -3, -7, -11 ANGLES ON FS 541. (M) 2 L 7 2 4F A6WE 2003031300030 20030313 00030 WP 2003 3 13 GTIA021255A 1 20021117 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LB L 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 5 79 REPAIR. INSTALLED -3, -7, -11 ANGLES AND PLATES FS 579. FABRICATED REPAIR PARTS -3, -7, AND -11 FOR FS 541. INSTAL LED REPAIR PARTS -3, -7, -11 ANGLES ON FS 541. (M) 2 L 7 2 4F A6WE 2003031300031 20030313 00031 WP 2003 3 13 GTIA021255B 1 20021117 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LB L 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 5 79 REPAIR. INSTALLED -3, -7, -11 ANGLES AND PLATES FS 579. FABRICATED REPAIR PARTS -3, -7, AND -11 FOR FS 541. INSTAL LED REPAIR PARTS -3, -7, -11 ANGLES ON FS 541. (M) 2 L 7 2 4F A6WE 2003031300032 20030313 00032 WP 2003 3 13 GTIA021255C 1 20021117 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LB L 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 5 79 REPAIR. INSTALLED -3, -7, -11 ANGLES AND PLATES FS 579. FABRICATED REPAIR PARTS -3, -7, AND -11 FOR FS 541. INSTAL LED REPAIR PARTS -3, -7, -11 ANGLES ON FS 541. (M) 2 L 7 2 4F A6WE 2003031300033 20030313 00033 WP 2003 3 13 GTIA021255D 1 20021117 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LB L 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 5 79 REPAIR. INSTALLED -3, -7, -11 ANGLES AND PLATES FS 579. FABRICATED REPAIR PARTS -3, -7, AND -11 FOR FS 541. INSTAL LED REPAIR PARTS -3, -7, -11 ANGLES ON FS 541. (M) 2 L 7 2 4F A6WE 2003031300034 20030313 00034 WP 2003 3 13 GTIA021255E 1 20021117 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LB L 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 5 79 REPAIR. INSTALLED -3, -7, -11 ANGLES AND PLATES FS 579. FABRICATED REPAIR PARTS -3, -7, AND -11 FOR FS 541. INSTAL LED REPAIR PARTS -3, -7, -11 ANGLES ON FS 541. (M) 2 L 7 2 4F A6WE 2003031300035 20030313 00035 WP 2003 3 13 GTIA021255F 1 20021117 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LB L 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 5 79 REPAIR. INSTALLED -3, -7, -11 ANGLES AND PLATES FS 579. FABRICATED REPAIR PARTS -3, -7, AND -11 FOR FS 541. INSTAL LED REPAIR PARTS -3, -7, -11 ANGLES ON FS 541. (M) 2 L 7 2 4F A6WE 2003031300036 20030313 00036 WP 2003 3 13 GTIA021299 1 20021011 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE TORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND COCKPIT FLOOR WEB TORN AND CORRODED UNDER PILOTS INBOARD AFT SEAT TRUCK AND TWO CRACKS. CUT OUT TORN WEB TW O PLACES DAMAGED AREA. FABRICATED REPAIR PARTS DOUBLER AND WEB. INSTALLED REPAIR PARTS FOR OUTBOARD REPAIR DOUBLER, WEB , AND 'L' ANGLE. CUT OUT DAMAGED AREA INBOARD COCKPIT LEFT SIDE. FABRICATED REPAIR PARTS DOUBLER AND FILLER. INSTALLE D REPAIR INBOARD WEB REPAIR DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2003031300037 20030313 00037 NM 2003 3 13 GTIA021309 1 20021129 A 5712 RIB DOUG MD80 MD83 3023681 NM LT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - LEFT WING LEADING EDGE RIB CRACKED AT XRS 290. STOP DRILLED CRACK. FORMED REPAIR ANGLES. INSTALLED REPAIR ANGLE S. (M) 2 L 7 2 4F RT 2003031300038 20030313 00038 2003 3 13 GTIA021311 4 20021226 A 2565 SLIDE DOUG MD80 MD83 3023681 NM L1 DOOR OUT OF POSITION A GTIA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 822NK 49392 FLT 945 - ACY - L1 SLIDE PACK FELL OUT ON TAXI. REINSTALLED L1 DOOR SLIDE PACK IAW MM 25-62-00. (M) 2 L 7 2 4F RT 2003031300039 20030313 00039 NM 2003 3 13 GTIA021312 1 20021127 A 5753 VANE DOUG MD80 MD83 3023681 NM T/E FLAP DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND RIGHT WING MID FLAP VANE NR 4 HAS HOLE IN LEADING EDGE, SPOT CORROSION AND BARE METAL. REPAIRED FLAP VANE H OLE AND SPOT CORROSION. DOUBLER AND THE FILLERS (2 FILLERS) WERE BONDED TO THE VANE. (M) 2 L 7 2 4F RT 2003031300040 20030313 00040 NM 2003 3 13 GTIA021313 1 20021206 A 5313 LONGERON DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - AT FS 1429 ON LONGERONS 2L AND 2R CRACKS IN LONGERON TERMINATION (END). CUT OUT DAMAGE AREA FROM FS 1429 ON LONGE RON 2R IN LONGERON TERMINATION. CUT OUT DAMAGE AREA FROM FS 1429 ON LONGERON 2L LONGERON TERMINATION. FABRICATED LEFT LONGERON 2L AND RIGHT L2R LONGERONS AND REPAIR SPLICES. INSTALLED LONGERON 2L AND 2R, TWO SPLICES. (M) 2 L 7 2 4F RT 2003031300041 20030313 00041 NM 2003 3 13 GTIA021314 1 20021025 A 3230 4914088501 ARM DOUG MD80 MD83 3023681 NM LANDING GEAR BENT A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - COULD NOT GET GEAR LIGHT TO TURN FROM RED TO GREEN WHEN USING EMERGENCY GEAR EXTENSION BOTH PRESSURIZED AND UNPRES SURIZED HYDRAULICS. REMOVED SHAFT, SPRING, RETAINER BLOCK, SUPPORT AND ARM. UPON FURTHER INSPECTION FOUND ARM BENT, BE ARINGS WORN IN SPRING RETAINER BLOCK, BEARING IN SUPPORT WORN AND COVER BROKEN. INSTALLED SHAFT, NEW SUPPORT ASSEMBLY, SPRING ARM AND BLOCK ASSEMBLY AS AN ASSEMBLY. (M) 2 L 7 2 4F RT 2003031300042 20030313 00042 NM 2003 3 13 GTIA021315 1 20021125 A 5310 BEAM DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND AFT PIT JAM BEAM CORRODED, INSIDE AND OUT. REMOVED LOWER JAMB BEAM. INSTALLED NEW LOWER JAMB BEAM. (M) 2 L 7 2 4F RT 2003031300043 20030313 00043 GL 2003 3 13 ALG2003F00028 2 20021214 A 7200 23063354 ENGINE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FAILED E O OTHER Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 03 627AL 53284 DURING CRUISE FLIGHT, ENGINE CHIP LIGHT ILLUMINATED DURING CRUISE FLIGHT. THE PILOT FOLLOWED THE EMERGENCY CHECKLIST AN D UPON LANDING THE MECHANIC REMOVED AND REPLACED THE TURBINE AND GEARBOX. AIRCRAFT WAS THEN RETURNED TO SERVICE. 1 G 7 1 3U 3 U O H2SW E1GL 2003031300044 20030313 00044 SW 2003 3 13 ALG2003F00029 1 20021203 A 2822 9A1746 CARTRIDGE BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE NR 1 ENG FUEL INOPERATIVE E A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 309AL 28198 GEE343028 DURING CRUISE FLIGHT, NR 1 FUEL TRANSFER PUMP CAUTION LIGHT ILLUIMINATED, AIRCRAFT LANDING WAS UNEVENTFUL, MAINTENANCE WAS NOTIFIED. THE MECHANIC FOUND NR 1 FUEL PUMP TRANSFER PUMP INOPERATIVE, HE REMOVED AND REPLACED THE PUMP AND AIRCRAF T RETURNED TO SERVICE. 2 G 7 2 4U 4 U H10SW E8NE 2003031300045 20030313 00045 GL 2003 3 13 ALG2003F00030 2 20021207 A 7200 23005290 ENGINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 INOPERATIVE E A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 518AL 16175 760134 CAE890874S IN CRUISE FLIGHT, AT APPROXIMATELY 16:40, NR 2 ENGINE NR2 SPED TO 112 PERCENT- 114 PERCENT RIGHT YAW EXPERIENCED, NR 2 ENGINE LEVER WAS RETARTED TO CONTROL N2/NR. NR 2 ENGINE CHIP LIGHT ILLUMINATED AFTER 3-4 SECONDS AFTER ENGINE LEVER WAS RETARTED, AT THIS TIME NR 2 ENGINE LEVER WAS BROUGHT TO IDLE POSITION, NR 2 ENGINE OIL PRESSURE FLUCTUATING BETWEEN 45 AND 55 PSI. NR2 ENGINE WAS SECURED, AIRCRAFT DIVERTED TO LAND. 1 G 7 2 3U 3 U H1NE E1GL 2003031300046 20030313 00046 NM 2003 3 13 GTIA021316 1 20021217 A 7830 ANGLE DOUG MD80 MD83 3023681 NM THRUST REVERSER CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND NR 2 ENGINE THRUST REVERSER INBOARD FAIRING PYLON CLOSEOUT PANEL CRACKED. REMOVED CRACKED ANGLE DOUBLER. F ABRICATED NEW ANGLE DOUBLER. INSTALLED NEW DOUBLER. (M) 2 L 7 2 4F RT 2003031300047 20030313 00047 GL 2003 3 13 ALG2003F00031 2 20021120 A 7532 23005366 BLEED VALVE BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL ENGINE FAILED E C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 03 194H 45660 CAE895087 DURING TAKE OFF, COMPRESSOR STALLED, PILOT ABORTED THE FLIGHT, UPON LANDING THE MECHANIC REMOVED AND REPLACED THE BLEED VALVE, ALSO THE MECHANIC CHECKED FUEL NOZZLES AND CHECKED ALL AIR LINES, THE FUEL SYSTEM WAS BLED AND THE AIRCRAFT RETUR NED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003031300048 20030313 00048 GL 2003 3 13 ALG2003F00032 2 20021117 A 7310 6890579 LINE BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL FUEL SYSTEM LEAKING E K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1075W 45377 CAE860778 DURING PREFLIGHT, FUEL IS LEAKING FROM THE LINE (PN 6890579) , FUEL CONTROL TO PUMP BYPASS) THE MECHANIC REMOVED THE LIN E, INSPECTED IT AND REINSTALLED THE LINE. THE FUEL SYSTEM WAS BLED AND THE AIRCRAFT WAS GROUND RUN, LEAK CHECKED OK AND AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003090300129 20030903 00129 SW 2003 9 3 ALG2003F00033 1 20020719 A 5302 407023800119 SUPPORT ANGLE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAILBOOM CRACKED B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 617AL 53265 DURING DAILY INSPECTION, CRACKED IN RADIUS DUE TO POOR FIT. LEFT LOWER SUPPORT ANGLE FOR HORIZONTAL STABILIZER. TB 407 0133 WAS CW AT THIS DATE. 1 G 7 1 3U 3 U O H2SW E1GL 2003031300049 20030313 00049 WP 2003 3 13 GTIA021325 1 20021115 A 5313 STRINGER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND FORWARD CARGO STRINGER 28L CORRODED AT FS 218-237, 53) 237-256, 58) 275-294, 67) 330-351. STRINGER 28L B7W STATION 229 AND STATION 243 FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION. FABRICATED NEW STRINGER AND SPLICE. I NSTALLED LONGERON AND SPLICE. (M) 2 L 7 2 4F A6WE 2003031300050 20030313 00050 NE 2003 3 13 ALG2003F00034 1 20021029 A 6210 7615009100051 BLADE SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL MAIN ROTOR VIBRATION E ALGA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 SW 03 707AL * 396 760189 DURING FLIGHT, PILOT ENCOUNTERED MODERATE VIBRATION OF MAIN ROTOR FOR 3 SECONDS IN CRUISE FLIGHT THEN IT CEASED. THE AI RCRAFT WAS DIVERTED TO LAFOURCHE AIRPORT IS LANDED WITH NO FURTHER PROBLEM, THE MECHANIC FOUND BLUE MAIN ROTOR BLADE ERO SION TAPE TORN HE REMOVED THE TAPE AND THE FOLLOWING DAY THE MAIN ROTOR BLADE WAS CHANGED. 1 G 7 2 3U 3 U H1NE E1GL 2003031300051 20030313 00051 WP 2003 3 13 GTIA021326 1 20021222 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND MAIN CABIN FLOORBOARD STATION 198-250 NR 5 HAS CORRODED INSETS AND DETERIORATING BOARD. FABRICATED NEW FLOO R PANEL. (M) 2 L 7 2 4F A6WE 2003031300052 20030313 00052 WP 2003 3 13 GTIA021327 1 20021219 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND LEFT COCKPIT FLOORBOARD STATION 120-183 DETERIORATED. FABRICATED NEW LEFT COCKPIT FLOORBOARD FS 120-183. ( M) 2 L 7 2 4F A6WE 2003031300053 20030313 00053 WP 2003 3 13 GTIA021328 1 20021222 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND MAIN CABIN FLOORBOARD STATION 120-140, NR 1 DETERIORATED. DRILLED AND LOCATED PANEL. (M) 2 L 7 2 4F A6WE 2003031300054 20030313 00054 NE 2003 3 13 ALG2003F00036 1 20021027 A 7714 0177555240 SENSOR SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1S1 60030 NE NR 2 ENG OVRSPED INOPERATIVE E ALGA C ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 SW 03 521AL 760132 ON TAKEOFF, NR 2 ENGINE DROPPED OFF LINE AND WOULD NOT RESTART. THE MECHANIC TROUBLESHOT AND FOUND NR 2 OVERSPEED SENSO R NOT OPERATIONAL. 1 G 7 2 3U 3 U H1NE E19EU 2003031300055 20030313 00055 WP 2003 3 13 GTIA021329 1 20021222 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND MAIN CABIN FLOORBOARD STATION 120-140 NR 2 DETERIORATED. DRILLED AND LOCATED PANEL. (M) 2 L 7 2 4F A6WE 2003031300056 20030313 00056 SW 2003 3 13 ALG2003F00037 1 20021029 A 2810 41650 FUEL CAP BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUEL CELL BENT E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 168H 3453 DURING PREFLIGHT, PILOT DISCOVERED WATER IN THE FUEL SAMPLE, THE MECHANIC DEFUELED THE AIRCRAFT AND REMOVED AND REPLACED THE AIRFRAME FUEL FILTER, FUEL NOZZLE, FUEL CAP, FUEL LINES WERE FLUSHED WITH FRESH FUEL, THE MECHANIC DETERMINED THE O LD FUEL CAP WAS SLIGHTLY BENT ALLOWING WATER TO GO INTO THE FUEL CELL. THIS AIRCRAFT IS EQUIPPED WITH FUEL RANGE EXTEND ER PN206-282-100 INSTALLED IAW STC SH2889SW. 1 G 7 1 3U 3 U H2SW E4CE 2003031300057 20030313 00057 WP 2003 3 13 GTIA021330 1 20021224 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - PASSENGER SEAT TRACK CORRODED AT FS 826-840, 850-880, 893-927, 933-955, 965-984, 994-1003 RIGHT SIDE OUTBOARD TRAC K. FOUND ONE AREA BETWEEN STATION 896 AT TO BE DAMAGED BEYOND LIMITS. CUT OUT RIGHT OUTBOARD SEAT TRACK FROM STATION 8 77-917. FABRICATED AND DRILLED SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2003031300058 20030313 00058 NE 2003 3 13 ALG2003F00038 1 20021019 A 2612 30231R7B FIRE DETECTOR SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL CARGO BAY WILL NOT TEST E ALGA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 03 703AL 760266 DURING PREFLIGHT START, AFT BAGGAGE FIRE DETECTION SYSTEM DID NOT TEST. THE MECHANIC REMOVED AND REPLACED THE SMOKE DET ECTOR. 1 G 7 2 3U 3 U H1NE E1GL 2003031300059 20030313 00059 NE 2003 3 13 ALG2003F00039 1 20021015 A 2612 MS3476L833S CONNECTOR SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL CAUTION PANEL CORRODED E ALGA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 03 702AL 760243 DURING FLIGHT, NR 2 ENGINE FIRE CAUTION LIGHT ILLUMINATED ALONG WITH TWO LIGHTS ON THE (T) HANDLE. NO OTHER INDICATION THAT FIRE DID EXIST (T PERCENT, N1, N2 NORMAL) THE CAUTION LIGHT EXTINGUISHED AFTER 5 SECONDS AND DID NOT ILLUMINATE FOR THE REMAINDER OF 15 MINUTES OF FLIGHT. UPON LANDING, THE MECHANIC FOUND CORROSION ON NR 2 CAUTION CONNECTOR PLUG, HE C LEANED THE PLUG AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2003031300060 20030313 00060 WP 2003 3 13 GTIA021331 1 20021229 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND FS 835-853 LBL 44 INCHES TO 45 INCHES CORRODED ON WEB WITH CRACKS IN WEB UNDER OUTBOARD SEAT TRACK. REMOVED CORRODED AREAS AND CRACKED AREAS. FABRICATED/LOCATED/DRILLED DOUBLER AND FILLER. INSTALLED PARTS. (M) 2 L 7 2 4F A6WE 2003031300061 20030313 00061 WP 2003 3 13 GTIA021332 1 20021226 A 5320 SUPPORT ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND LEFT MLG, FORWARD DOOR JAMB HAS CRACK AT AFT BRACKET SUPPORT IN INTERCOSTAL. REMOVED CRACKED INTERCOSTAL SU PPORT ANGLE. FABRICATED NEW SUPPORT ANGLE. INSTALLED SUPPORT ANGLE. (M) 2 L 7 2 4F A6WE 2003031300062 20030313 00062 NE 2003 3 13 ALG2003F00040 1 20021016 A 2612 303267 AMPLIFIER SKRSKY S76 S76 8143010 NE FIRE DETECTION INOPERATIVE E ALGA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SW 03 702AL 760243 DURING GROUND RUN UP, NR 2 ENGINE FIRE DETECTION ACTIVATED. THE MECHANIC REMOVED AND REPLACED THE NR 2 ENGINE CONTROL A MP AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U H1NE 2003031300063 20030313 00063 WP 2003 3 13 GTIA021333 1 20021226 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND AFT PRESSURE BULKHEAD FORWARD SIDE FRAME SHEAR TIE BENT AND CRACKED LBL 31 INCHES WL 84 INCHES STRINGER 5L. REMOVED/CUTOUT DAMAGED SHEAR TIE. FABRICATED REPAIR SECTION, COMPLETED REPAIR INSTALLATION. (M) 2 L 7 2 4F A6WE 2003031300064 20030313 00064 WP 2003 3 13 GTIA021334 1 20021226 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND LEFT CABIN FLOOR WEB CORRODED AND BROKEN AT SIDEWALL STATION 218-237. PASSENGER CABIN STATION 218 TO STATIO N 237 MEMBRANE WEB IS CRACK/PUNCTURE LBL 44. REMOVED MEMBRANE WEB. FABRICATED NEW MEMBRANE WEB. INSTALLED NEW MEMBRANE WEB. (M) 2 L 7 2 4F A6WE 2003031300065 20030313 00065 GL 2003 3 13 ALG2003F00041 2 20020926 A 7261 23005287 CHIP DETECTOR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 ENGINE ACTIVATED E ALGA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 03 376AL 760002 DURING FLIGHT, NR 2 ENGINE CHIP LIGHT ILLUMINATED AND WOULD NOT RESET, BEEPED NR 2 ENGINE ALL THE WAY BACK AND FLEW APPR OXIMATELY 20 MINUTES SINGLE ENGINE AND PERFORMED RUN ON LANDING AT ARA. UPON LANDING NR 2 ENGINE WAS REMOVED. 1 G 7 2 3U 3 U H1NE E1GL 2003031300066 20030313 00066 NE 2003 3 13 ALG2003F00042 1 20020926 A 2910 07113111321 SWITCH SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL LT HYD SERVO FAILED E ALGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 1547N 760088 DURING CRUISE FLIGHT, NR 2 SERVO SYSTEM CAUTION LIGHT ILLUMINATED, AIRCRAFT WAS DIVERTED TO INTRACOASTAL, PILOT FOLLOWED EMERGENCY CHECKLIST AND LANDED AT INTRACOASTAL. UPON LANDING, THE MECHANIC REMOVED AND REPLACED REARWARD PRESSURE SWIT CH ON LEFT FORWARD SERVO. AIRCRAFT WAS FUNCTION CHECKED AND RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2003031300071 20030313 00071 NE 2003 3 13 ALG2003F00045 1 20020930 A 3260 76450010005101 CONTROL PANEL SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL MLG INOPERATIVE E ALGA O OTHER N FALSE WARNING LD LANDING 1 SW 03 519AL 760058 DURING LANDING, THE LANDING GEAR WARNING HORN WENT ON AND STAYED ON WITH THE GEAR DOWN AND LOCKED (3 GREEN LIGHT). UPON LANDING THE LANDING GEAR WAS PINNED IAW MEL AND LOGBOOK ENTRY WAS MADE. SUBSEQUENT INSPECTION REVEALED BROKEN WIRE NR LGW503R20 AT PIN (2) NR 1 OVERHEAD RELAY PANEL TO THE DIODE BRIDGE, THE WIRE WAS REPAIRED AND AIRCRAFT RETURNED TO SERVI CE. 1 G 7 2 3U 3 U H1NE E1GL 2003031300072 20030313 00072 SW 2003 3 13 ALG2003F00046 1 20021006 A 6220 206076062103 SERVO BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL COLLECTIVE UNDERTORQUED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 359AL 51461 DURING FLIGHT, PILOT REPORTED COLLECTIVE STIFF AT 60 PERCENT TORQUE, UPON LANDING, THE MECHANIC REMOVED AND REPLACED THE COLLECTIVE SERVO AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003031300074 20030313 00074 GL 2003 3 13 ALG2003F00047 2 20021007 A 7320 25490926 FUEL CONTROL BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL ENGINE LEAKING E ALGA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 272M 45365 DURING POST FLIGHT, THE MECHANIC FOUND FUEL CONTROL LEAKING, HE REMOVED AND REPLACED THE FUEL CONTROL, AIRCRAFT WAS LEAK CHECKED AND RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003031300075 20030313 00075 NE 2003 3 13 ALG2003F00048 1 20021006 A 3230 7625100702043 LINK ASSY SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL RT MAIN GEAR INOPERATIVE E ALGA O OTHER E VIBRATION/BUFFET LD LANDING 1 SW 03 717AL 760221 DURING LANDING, WHEN PILOT LOWERED THE LANDING GEAR, HE HEARD AN AUDIBLE THUMP, DURING HOVER ANOTHER PILOT REPORTED TO H IM THAT THE RIGHT MAIN GEAR WAS DOWN. THE COCKPIT LANDING GEAR LIGHT INDICATED THAT WERE UP AND SAFE, THE GEAR WAS EXTE NDED AND NORMAL LANDING WAS MADE. UPON LANDING, THE MECHANIC ADJUSTED THE LENGTH OF EXPLOSIVE LINK OF RIGHT MAIN GEAR A ND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2003031300076 20030313 00076 SW 2003 3 13 ALG2003F00049 1 20021007 A 2913 206076030111 PUMP BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL HYD SYSTEM FAILED E ALGA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 359AL 51461 DURING FLIGHT, PILOT REPORTED PARTIAL HYDRAULIC FAILURE, UPON LANDING THE MECHANIC REMOVED AND REPLACED THE HYDRAULIC PU MP AND HYDRAULIC FILTER, THE AIRCRAFT WAS CHECKED FOR LEAKS AND OPS CHECK WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SE RVICE. 1 G 7 1 3U 3 U H2SW E1GL 2003031300078 20030313 00078 SW 2003 3 13 ALG2003F00050 1 20021004 A 2840 WARNING LIGHT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUEL TRANSFER ILLUMINATED E ALGA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 03 457AL 53151 IN FLIGHT, FUEL TRANSFER LIGHT ILLUMINATED IN FLIGHT, FLIGHT WAS DIVERTED TO WD 70 AND DISCOVERED FUEL OF 148 LBS. THE PILOT CALLED HOUMA AND 35 GALLONS OF FUEL WAS FLOWN TO THE AIRCRAFT. 1 G 7 1 3U 3 U O H2SW E1GL 2003031300086 20030313 00086 WP 2003 3 13 Z9B2003F00000 1 20021213 A 6310 369A535041 CLUTCH HUGHES 369 369E 4470707 WP ALLSN 250C 250C20 03013 GL ENGINE FAILED E Z9BA O OTHER O OTHER NR NOT REPORTED 1 NM 09 1600Q 1179 O200E RUBBING NOISE ON COAST DOWN AFTER SHUTDOWN. FOUND OVER-RUNNING CLUTCH ASSY HAD LOST ALL OIL. TOP BEARING CAP WAS BACK ED .5000 OFF THREADS OF OUTER RACE SHAFT. CLUTCH STILL FUNCTIONED, BUT BEARINGS WERE BEGINING TO GRAB. TOP CAP LOCK WA SHER STILL HAS PROPER LOCKING INDENTS. UNKNOWN WHY CAP BACKED OFF 82 HOURS SINCE INSPECTION. 1 G 7 1 3U 3 U H3WE E4CE 2003031300087 20030313 00087 EU 2003 3 13 Z9B2003F00001 1 20021220 A 6320 4638001010 TRANSMISSION BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL ENGINE MAKING METAL E Z9BA O OTHER O OTHER NR NOT REPORTED 1 NM 09 131AE 5723 749 S787 METAL IN OIL RESULTING IN CHIP WARNING INDICATIONS. OIL FILTER CONTAINED BARASS AND IRON FINE FLAKES AND SLIVERS. SENT TO FACTORY REPAIR STATION FOR ANALYSIS AND REPAIR. 1 G 7 2 3U 3 U H3EU E4CE 2003031300088 20030313 00088 EU 2003 3 13 Z9B2003F00002 1 20021217 A 2435 BRUSHES BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL STARTER GEN WORN E Z9BA K NONE O OTHER IN INSP/MAINT 1 NM 09 131AE 661 18760 S787 STARTER GEN, AT 100 HOUR INSPECTION FOUND COMMUTATOR WORN DOWN TO UNDERCUT, BRUSHES STILL SERVICEABLE. MAY NOT HAVE BEE N PROPERLY UNDERCUT AT LAST OVERHAUL. 1 G 7 2 3U 3 U H3EU E4CE 2003031300093 20030313 00093 GL 2003 3 13 ALG2003F00051 2 20021007 A 7323 23065125 GOVERNOR SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL NR 1 ENGINE INOPERATIVE E ALGA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 SW 03 705AL 760267 CAE890824S DURING RUN-UP, AFTER DROOP COMPENSATOR CHECK, THE PILOT SET THE NR 2 ENGINE TO 100 PERCENT AND ADJUSTED THE NR 1 ENGINE TO 100 PERCENT. THEN THE NR 1 ENGINE FAILED (FLAMED OUT). THE MECHANIC REMOVED AND REPLACED THE GOVERNOR, FUEL CONTROL AND FUEL NOZZLE ON THE NR 1 ENGINE. THE FUEL FILTER WAS CHECKED AIRCRAFT FUEL SAMPLE WAS CHECKED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2003031300094 20030313 00094 GL 2003 3 13 ALG2003F00052 2 20021007 A 7320 23070613 FUEL CONTROL SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL NR 1 ENGINE INOPERATIVE E ALGA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 SW 03 705AL 760267 CAE890824S DURING RUN-UP, AFTER DROOP COMPENSATOR CHECK, THE PILOT SET THE NR 2 ENGINE TO 100 PERCENT AND ADJUSTED THE NR 1 ENGINE TO 100 PERCENT. THEN THE NR 1 ENGINE FAILED (FLAMED OUT). THE MECHANIC REMOVED AND REPLACED THE GOVERNOR, FUEL CONTROL AND FUEL NOZZLE ON THE NR 1 ENGINE. THE FUEL FILTER WAS CHECKED, AIRCRAFT FUEL SAMPLE WAS CHECKED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2003031300095 20030313 00095 2003 3 13 AWH2003F00002 4 20021212 A 3197 WIRE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE HOUR METER SHORTED E AWHA O OTHER O OTHER NR NOT REPORTED 1 WP 17 790FE 208B0288 19165 SUBJECT A/C DO NOT HAVE HOUR METER OPTION INSTALLED. A/C IS WIRED FOR THIS OPTION. CLOCK OR HOUR METER. MAINT HAS FOU ND AT CIRCUIT BREAKER CB75 BOTH OPTIONS POWERED AND WIRE DF2 TERMINAL IMPROPERLY STOWED. TERMINAL END OF WIRE DF2 IS NO T PROTECTED FROM SHORTING AND IMPROPER WRAPPING ALLOWS TERMINAL END TO FLOP AROUND. TERMINAL END TO FLOP AROUND. TERMI NAL END DF7 IS A GROUNDED CIRCUIT AND IS STOWED WITH DF2 TERMINAL. FOUND THIS A/C WIRING TIES BEHIND RADIO RACK. DF2, DF7 TERMINAL ENDS LOOSE. MAINT IS INSPECTING A SAMPLE SET OF AIRCRAFT FOR THIS CONDITION. IF FOUND IN THIS CONDITION. MAINT IS DISCONNECTED TERMINAL DF1 AT CB75, HEAT SHRINKING TERMINAL END FOR PROTECTION AND PROPERLY STOWING WIRE. 1 H 7 1 3T 3 T A37CE E4EA 2003031300096 20030313 00096 2003 3 13 AWHA1120 4 20021120 A 3197 WIRE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE HOUR METER SHORTED E AWHA A UNSCHED LANDING B W SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C CL CLIMB 1 WP 17 785FE 5884 208B0283 19160 DEPARTING, EXPERIENCED SMOKE IN THE COCKPIT. THE PILOT JUST HAVING ROTATED REDUCED POWER AND LANDED IMMEDIATELY. ASKED BY CONTROL, STATUS OK, BUT NEEDED TO RETURN TO HANGER. NO EMERGENCY WAS DECLARED. MAINTENANCE HAD JUST PERFORMED A MI NI CHECK ON THE AIRCRAFT AND A COUPLE OF MINOR AVIONICS CHECKS INCLUDING A CLUTCH TORQUE INSPECTION. THE AIRCRAFT WAS T EST FLOWN FOR THE A/C RELEASE WITHOUT INCIDENT. THEY BEGAN TO LOOK FOR THE OBVIOUS FROM THE CLOCK CB POPPED IN THE ENGI NE COMPARTMENT. ON INSPECTION OF THAT CIRCUIT MAINTENANCE FOUND A PAIR OF WIRES, APPARENTLY FOR AN HOUR METER, WITH CON NECTORS IMPROPERLY CAPPED (AS IN NONE) AND IMPROPERLY TIED OFF, SHORTED OUT AND BURNED. 1 H 7 1 3T 3 T A37CE E4EA 2003031300097 20030313 00097 2003 3 13 AWHA1125 4 20021122 A 3197 WIRE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE HOUR METER SHORTED E AWHA O OTHER O OTHER NR NOT REPORTED 1 WP 17 763FE 208B0256 19130 THE SUBJECT AIRCRAFT DOES NOT HAVE THE HOUR METER OPTION INSTALLED. HOWEVER THE AIRCRAFT IS WIRED FOR THIS OPTION, CLOC K OR HOUR METER. MAINTENANCE HAS FOUND AT THE CIRCUIT BREAKER CB75 BOTH OPTIONS POWERED AND THE WIRE DF2 TERMINAL IMPRO PERLY STOWED. THE TERMINAL END OF WIRE DF2 IS NOT PROTECTED FROM SHORTING AND IMPROPER TIE WRAPPING ALLOWS THE TERMINAL END TO FLOP AROUND. TERMINAL END DF7 IS A GROUNDED CIRCUIT AND IS STOWED WITH DF2 TERMINAL. FOUND THIS AIRCRAFT WIRIN G TIES BEHIND CO-PILOTS INSTRUMENTS PANEL. DF2,DF7 TERMINAL ENDS LOOSE. C/A: MAINTENANCE IS DISCONNECTING TERMINAL DF1 AT CB75, HEAT SHRINKING TERMINAL END FOR PROTECTION AND PROPERLY STOWING WIRE. 1 H 7 1 3T 3 T A37CE E4EA 2003031300098 20030313 00098 2003 3 13 AWHA1126 4 20021202 A 3197 WIRE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE HOUR METER SHORTED E AWHA O OTHER O OTHER NR NOT REPORTED 1 WP 17 782FE 208B0280 19157 902511 THIS AIRCRAFT DOES NOT HAVE THE HOUR METER OPTION INSTALLED. AIRCRAFT IS WIRED FOR THIS OPTION, CLOCK OR HOUR METER. M AINTENANCE HAS FOUND AT CIRCUIT BREAKER CB75 BOTH OPTIONS POWERED AND WIRE DF2 TERMINAL IMPROPERLY STOWED. TERMINAL EN D OF WIRE DF2 TERMINAL IMPROPERLY STOWED. TERMINAL END OF WIRE DF2 IS NOT PROTECTED FROM SHORTING AND IMPROPER TIE WRAP PING ALLOWS TERMINAL END TO FLOP AROUND. TERMINAL END DF7 IS A GROUNDED CIRCUIT AND IS SHOWED WITH DF2 TERMINAL. FOUND THIS AIRCRAFT WIRING TIES BEHIND RADIO RACK. DF2,DF7 TERMINAL ENDS LOOSE. IF FOUND IN THIS CONDITION, MAINTENANCE IS INSPECTING, DISCONNECTING TERMINAL DF1 AT CB75, HEAT SHRINKING TERMINAL END FOR PROTECTION AND PROPERLY STOWING WIRE. 1 H 7 1 3T 3 T A37CE E4EA 2003031300099 20030313 00099 2003 3 13 AWHA1129 4 20021202 A 3197 WIRE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE HOUR METER SHORTED E AWHA O OTHER O OTHER NR NOT REPORTED 1 WP 17 891FE 5562 208B0221 17424 AIRCRAFT DOES NOT HAVE THE HOUR METER OPTION INSTALLED. AIRCRAFT IS WIRED FOR THIS OPTION, CLOCK OR HOUR METER. MAINTE NANCE HAS FOUND AT THE CIRCUIT BREAKER CB75 BOTH OPTIONS POWERED AND THE WIRE DF2 TERMINAL IMPROPERLY STOWED. THE TERMI NAL END OF WIRE DF2 IS NOT PROTECTED FROM SHORTING AND IMPROPER TIE WRAPPING ALLOWS THE TERMINAL END TO FLOP AROUND. TER MINAL END DF7 IS A GROUNDED CIRCUIT AND IS STOWED WITH DF2 TERMINAL. FOUND THIS AIRCRAFT WIRING TIES BEHIND COPILOTS IN STRUMENT PANEL. DF2, DF7 TERMINAL ENDS LOOSE. C/A: MAINTENANCE IS INSPECTING FOR THIS CONDITION, IF FOUND, IS DISCONN ECTING TERMINAL DF1 AT CB75, HEAT SHRINKING TERMINAL END PROTECTION AND PROPERLY STOWING WIRE. 1 H 7 1 3T 3 T A37CE E4EA 2003031300108 20030313 00108 SO 2003 3 13 CSS2003F00000 2 20021226 A 8500 ENGINE CESSNA 402 402B 207590P CE CONT O520 TSIO520EB 17040 SO SURGES E CSSA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 CE 01 98695 3079 279 402B1052 2713B4R ENGINE SURGED, POWER LOSS, AND WAS SHUT DOWN IN FLIGHT. 1 L 7 2 3O 3 O A7CE E8CE 2003031300123 20030313 00123 SO 2003 3 13 FWR2003F00000 1 20021217 A 5320 409872 CHANNEL PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA FWD FUSELAGE CRACKED B FWRR O OTHER O OTHER NR NOT REPORTED 1 AL 01 222CC 14957 318052095 FOUND DURING BASE INSPECTION, FATIGUED OVER THE YEARS. AGING AIRCRAFT PROGRAM PROBABLY APPLIES TO THIS PART. OBVIOUSLY THE CONDITIONS THAT THE AIRCRAFT IS OPERATED ALSO A CONTRIBUTING FACTOR. THE UPPER ATTAH POINT OF THE NOSE GEAR ACTUAT OR ATTACHES TO THIS PART. 1 L 7 2 3O 3 O A20SO E14EA 2003031300124 20030313 00124 SO 2003 3 13 FWR2003F00001 1 20021218 A 5320 409872 CHANNEL PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA FWD FUSELAGE CRACKED B FWRR O OTHER O OTHER NR NOT REPORTED 1 AL 01 3589B 1151 318052134 FOUND DURING BASE INSPECTION, FATIGUED OVER THE YEARS, AGING AIRCRAFT PROGRAM PROBABLY APPLIES TO THIS PART. THE UPPER ATTACH POINT OF THE NOSE GEAR ACTUATOR ATTACHES TO THIS PART. 1 L 7 2 3O 3 O A20SO E14EA 2003031300126 20030313 00126 SO 2003 3 13 HYI2003F00002 2 20021210 A 8550 S116760060 LINE CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO ENGINE OIL CHAFED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 68391 402C0483 823279R CREW FOUND LT ENGINE OIL LEAK ON PORT FLIGHT INSPECTION. MECHANIC FOUND INTAKE BALANCE TUBE FLEX HOSE DATA TAG CHAFING ON OIL PAN. MECHANIC REMOVED AND REPLACED OIL PAN AND FLEX HOSE AND RETURNED AIRCRAFT TO SERVICE. FLEX LINE LENGTH WAS SHORTENED BY MANUFACTURER, CAUSING INADEQUATE CLEARANCE WHEN ROUTING HOSE. SUGGEST RETURNING TO ORIGINAL LENGTH HOSE F OR PROPER CLEARANCE. 1 L 7 2 3O 3 O A7CE E8CE 2003031300141 20030313 00141 WP 2003 3 13 GTIA021292 1 20021024 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - FOUND 4 HOLES IN FLOOR WEBBING, LBL 18 STATION 200-218. REMOVED THE DAMAGED FLOOR WEBBING AT LBL 18, STATION 200- 218. FABRICATED PRESSURE FLOOR FILLER ROOM AND DOUBLERS. INSTALLED WEB FILLER AND TWO DOUBLERS. (M) 2 L 7 2 4F A6WE 2003031300142 20030313 00142 WP 2003 3 13 GTIA021293 1 20021117 A 5531 SPAR CAP DOUG DC9 DC981 3022081 WP VERTICAL STAB CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 FTW - VERTICAL STABILIZER FRONT SPAR CAP RIGHT SIDE CRACKED 2 PLACES STATION 1446 CANT. REMOVED DAMAGED AREA. FABRICAT ED 8 SPLICE ANGLE. FABRICATED 4 CAP REPAIR SEGMENT. FABRICATED 6 SPLICE. INSTALLED THE 4, 6, 8 AND 10 REPAIR PARTS AN D SHIMS. (M) 2 L 7 2 4F A6WE 2003031300145 20030313 00145 GL 2003 3 13 PIY2003F00000 3 20021217 A 6110 SCREW BEECH 58 58 1152740 CE CONT O550 IO550C SO HARTZL HCJ3Y PHCJ3YF1 GL RT PROPELLER MISINSTALLED B PIYR K NONE O OTHER IN INSP/MAINT 1 EA 21 4482W TH1946 RIGHT PROPELLER DEICE BRUSH MOUNTING SCREWS WERE PAN HEAD SCREWS WITH NO LOCKING DEVICE. THE PARTS BOOK CALLS FOR PN MS 35275243 SCREW. THIS IS FILLISTER HEAD SCREW WITH THE HEAD DRILLED FOR SAFETY WIRE. THE PROPER SCREWS WERE OBTAINED, I NSTALLED, AND SAFETIED. THIS IS A LOW TIME AC AND NO RECORD OF BRUSH MAINTENANCE OR REPLACEMENT WAS DOCUMENTED IN THE A C RECORDS. 1 L 7 2 3O 3 O 3A16 E3SO 5 C P36EA 2003031300147 20030313 00147 NM 2003 3 13 2003F00142 1 20021104 A 3350 582214 POWER SUPPLY BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 DURING PREFLIGHT TRANSIT, FOUND EPL SYSTEM INOPERATIVE AT L2 DOOR AND ROWS 26 ABC THROUGH 30 ABC. TROUBLESHOT EPL SYSTE M. REMOVED AND REPLACED EPL POWER SUPPLY. OPERATIONAL CHECKED IAW 33-59-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2003031300150 20030313 00150 WP 2003 3 13 2003F00127 1 20021105 A 3350 P4010020 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 935DS 48158 R-1 AND L-1 DOOR SLIDE DOOR LIGHTS INOPERATIVE. PROBLEM DETERMINED TO BE LOW VOLTAGE. REMOVED AND REPLACED BOTH BATTER Y PACKS IAW DC-9 MM 33-50-1. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 2003031300151 20030313 00151 WP 2003 3 13 2003F00128 1 20021105 A 2560 1001191 FLASHLIGHT DOUG DC9 DC931 3022065 WP GALLEY INOPERATIVE A A4JA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 35 935DS 48158 NO LED ON FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AND LOW VOLTAGE. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT IAW DC-9 MM 33-53-0. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 2003031300155 20030313 00155 EU 2003 3 13 2003F00129 1 20021026 A 2450 A2043C PDU SAAB SF340 SF340A 7850100 EU ELECTRICAL SYS MALFUNCTIONED A UHLA L ABORTED APPROACH O OTHER AP APPROACH 1 NE 03 101CN 340A101 DURING APPROACH TO JST, PILOT REPORTED LOSS OF RIGHT ESS BUSS, RIGHT MAIN BUSS RESULTING IN LOSS OF FIRST OFFICERS EFFIS TUBE, PILOT ABORTED LANDING AND RETURNED TO PIT. MAINTENANCE REPLACED RIGHT PDU, NO FURTHER PROBLEMS, A/C RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2003031300156 20030313 00156 EU 2003 3 13 2003F00131 1 20021016 A 3246 5006227 WHEEL SAAB SF340 SF340A 7850100 EU NLG WORN A UHLA K NONE E VIBRATION/BUFFET LD LANDING 1 NE 03 35SZ 035 FLT 4522 - UPON LANDING AT PIT, PILOT REPORTED SEVERE NOSE WHEEL SHIMMY AT 40 KNTS UNTIL 20 KNTS. A/C FERRIED TO FWA MX BASE FOR TROUBLESHOOTING. AT FWA BOTH NOSE WHEELS CHANGED, NO FURTHER DEFECTS NOTED. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2003031300157 20030313 00157 EU 2003 3 13 2003F00133 1 20021125 A 2913 4018502 PUMP SAAB SF340 SF340A 7850100 EU HYD SYSTEM INTERMITTENT A UHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 17 118SD 118 FLT 4480 - PIT-TOL, ON TAXI OUT, AIRCRAFT RETURNED TO GATE, HYDRAULIC PUMP INTERMITTENT IN AUTO AND OVERRIDE. FIRST OF TWO SQUAWKS THIS FLIGHT. (M) 2 L 7 2 4T RT A52EU 2003031300158 20030313 00158 NM 2003 3 13 2003F00136 1 20021117 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 889MA 21854 DURING P/T FOUND DOOR 2 AISLE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK, LIGHT S OPS CHECKS GOOD IAW AMM 33-50-00. (M) 2 L 7 3 4F A3WE 2003031300159 20030313 00159 WP 2003 3 13 AALA20021565 1 20021030 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 437AA 49455 ORD - DURING OVERNIGHT MAINTENANCE AT OVERWING EXITS THREE OVERHEAD AISLE EMERGENCY EXIT LIGHTS COME ON WITH POWER OFF. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2003031300160 20030313 00160 WP 2003 3 13 AALA20021566 1 20021030 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 225AA 49175 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 21D INOPERATIVE. REPLACED AFT SEAT MOUNTE D EMERGENCY PATH LIGHT ASSEMBLY AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003031300161 20030313 00161 WP 2003 3 13 AALA20021567 1 20021030 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 225AA 49175 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS AT ROW 22 THROUGH 26 DIM. REPLACED BATTERY PACK ASSEM BLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003031300186 20030313 00186 WP 2003 3 13 AALA20030145 1 20020131 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 563AA 49345 TUL - FOUND FUSELAGE SKIN CRACKED AT STATION 1380 AND LONGERON 13L. INSTALLED DOUBLER PER SRM 51-01-00, 53-34-00 AND 53 -30-00-2. (M) 2 L 7 2 4F RT A6WE 2003031400002 20030314 00002 SW 2003 3 14 ALG2003F0000A 1 20021111 A 5280 20606480403334 STRINGER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL NACELLE DOOR CRACKED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 437AL 53141 IN FOR C/W ASB 4070254, WEIGHT OF CARBON FIBER DOORS. CRACK IS OCCURING ON FORWARD LEFT STRINGER AT CLIP ANGLE AND STRI NGER RIVETED LOCATION, WEIGHT OF DOORS AND VIBRATION. HEAVIER GAUGE STRINGER MATERIAL TO ACCOMODATE WEIGHT OF DOORS. 1 G 7 1 3U 3 U O H2SW E1GL 2003031400003 20030314 00003 SW 2003 3 14 ALG2003F00007 1 20021208 A 5311 206032308121A FRAME BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE CRACKED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 577AL 5261 53247 DISCOVERED WHEN FRAME WAS REMOVED TO REMOVE AND REPLACE RIVETS ON TAILBOOM ATTACH FITTING. (RIGHT UPPER FITTING) IT HAS BECOME GOOD PRACTICE TO CHECK THIS AREA BECAUSE OF PAST PROBLEMS. THE FRAME HAS BEEN FOUND TO CRACK IN THIS SAME AREA ON ALL AIRCRAFT THAT THIS INSPECTION IS DONE. FRAME WAS CRACKED ABOVE MATING SURFACE OF RIGHT UPPER T/B ATTACH FITTING. MAYBE RADIUS THE EDGES OF ATTACH FITTING THAT MATE WITH FRAME. 1 G 7 1 3U 3 U O H2SW E1GL 2003031400004 20030314 00004 SW 2003 3 14 ALG2003F0000B 1 20021107 A 5313 206031314123S LONGERON BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL FUSELAGE CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 27554 45246 DISCOVERED WHILE DOING REFURBISHING, MALFUNCTION OF LONGERON WAS CORROSION AND ELONGATED HOLES. 1 G 7 1 3U 3 U H2SW E1GL 2003031400005 20030314 00005 SW 2003 3 14 ALG2003F0000C 1 20021110 A 5302 206031329103S FITTING BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL TAILBOOM ATTACH CRACKED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 2654 45482 DURING INSPECTION, FOUND FITTING CRACKED EMANATING FROM RIVET HOLE. 1 G 7 1 3U 3 U H2SW E1GL 2003031400006 20030314 00006 GL 2003 3 14 ALG2003F00053 2 20021007 A 7313 6899001E FUEL NOZZLE SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL NR 1 ENGINE INOPERATIVE E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 705AL 760267 CAE890824S AFTER DROOP COMPENSATOR CHECK, THE PILOT SET THE NR 2 ENGINE TO 100 PERCENT AND ADJUSTED THE NR 1 ENGINE TO 100 PERCENT. THEN THE NR 1 ENGINE FAILED (FLAMED OUT). THE MECHANIC REMOVED AND REPLACED THE GOVERNOR, FUEL CONTROL AND FUEL NOZZL E ON THE NR 1 ENGINE. THE FUEL FILTER WAS CHECKED, AIRCRAFT FUEL SAMPLE WAS CHECKED AND THE AIRCRAFT WAS RETURNED TO SE RVICE. 1 G 7 2 3U 3 U H1NE E1GL 2003031400008 20030314 00008 CE 2003 3 14 OIK2003F00000 1 20021227 A 3297 M2275916 WIRE CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO DOWNLOCK SWITCH INOPERATIVE A OIKA O OTHER P NO WARNING INDICATION LD LANDING 1 WP 13 98692 402B1050 R206619724 DURING GEAR EXTENSION, UPON LANDING, PILOT NOTICED THE RIGHT GREEN LIGHT WAS NOT ILLUMINATED. EMERGENCY LANDING ASSISTA NCE WAS REQUESTED ON INSPECTION OF THE LANDING GEAR. A BROKEN WIRE WAS FOUND ON THE GEAR SWITCH DOWN LOCK SYSTEM. REPA IR WAS MADE GEAR GROUND CHECK DONE. FOUND OPERATING PROPERLY. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2003031400039 20030314 00039 EU 2003 3 14 2003F00119 1 20021203 A 2121 20764010 MOTOR BRAERO DH125 HS125700A 4230170 EU FAN BURNED G E H D ENGINE SHUTDOWN DEACTIVATE SYST/CIRCUITS RETURN TO BLOCK M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NE 03 270KA 2080 NA0307 WHEN NR 2 ENG EXPERIENCED SMOKE COMING FROM AFT CABIN AREA. CREW SHUT DOWN RT ENG & APU, AS WELL AS EVACUATING PASSENGE RS & TURNING OFF ALL ELECTRICAL POWER. IT WAS DETERMINED TO BE COMING FROM AFT BAGGAGE AREA RT BULKHEAD AREA & BLOWN GR OUND FAN REIRC. CB INDICATED POSSIBLE VENTURI FAN MOTOR FAILURE. INSPECTION OF VENTURI FAN INDEED REVEALED HIGH HEAT A REA. FAILED COMPONENT WAS ELECTRICALLY ISOLATED & ACFT WAS FLOWN TO HOME BASE IAW APPROVED MEL. AD 94-11-03 ADDRESSED THIS VERY PROBLEM, IT HAD BEEN ACCOMPLISHED ON THIS ACFT BY COMPLIANCE WITH ALERT S/B 21-A150, VISUAL INSPECTION OF ADJA CENT AREA FOR A MINIMUM 1" CLEARANCE OF VENTURE MOTOR & ANY INSULATING MATERIAL, TO PREVENT INGESTED INTO THE MOTOR. 2 L 7 2 4F A3EU 2003040100023 20030401 00023 CE 2003 4 1 AMWA14 1 20021118 A 5346 PRESSURE PANEL BEECH 1900 1900D 1154162 CE FUSELAGE CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 146ZV UE146 WHILE PERFORMING AND "A" CHECK ON THE LT ENGINE TRUSS, MAINTENANCE FOUND THE LT/RT PRESSURE PLATES EXHIBIT RIVET HEAD CO NTACT. MAINTENANCE REPAIRED THE PRESSURE PLATE CHAFING. NO TEARDOWN REPORT WILL BE REQUIRED. 2 L 7 2 4T RT A24CE 2003031400058 20030314 00058 2003 3 14 C7WA200200030 4 20021016 A 3417 ADC BOEING 727 7272J7 138400E NM COCKPIT FAILED A C7WA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 17 128NA 20879 AIRCRAFT DEPARTED YIP AT 23:52Z AND HAD AIR DATA INSTRUMENT FAILURE CLIMBING THRU 5000FT. AIRCRAFT RETURNED TO YIP AND MADE OVERWEIGHT LANDING. 2 L 7 3 4F A3WE 2003031400081 20030314 00081 EU 2003 3 14 CX7A194J14 1 20020731 A 2613 1734362450 SENSOR SAAB SF340 340B 7860101 EU TAILPIPE HOT WILL NOT TEST A CX7A K NONE L NO TEST IN INSP/MAINT 1 GL 03 307CE 340B204 RT TAILPIPE HOT SENSOR DOES NOT TEST. 2 L 7 2 4T RT A52EU 2003031400082 20030314 00082 NE 2003 3 14 CX7A194J15 2 20020805 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT SEIZED A CX7A E C ENGINE SHUTDOWN ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 GL 03 318CE 15588 393 358 GEE78554 AFTER ROTATION LT ENGINE OIL PRESSURE CWP- OIL PRESSURE GAUGE READ 0 PSI WHILE RUNNING ENGINE OIL PRESSURE CHECKLIST (TW O MINUTES MAX) ENGINE FAILED. RAN MEMORY ITEM AND CHECKLIST RETURNED FOR LANDING. REMOVED AND REPLACED LT ENGINE IAW G E AND SAAB AMM. 2 L 7 2 4T 4 T RT A52EU E8NE 2003031400083 20030314 00083 EU 2003 3 14 CX7A194J16 1 20020809 A 7931 J221P139 O-RING SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE BYPASS SENSOR CUT A CX7A B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 03 300CE 340B184 ENGINE OIL PRESSURE (RT) CWP LIGHT ILLUMINATED INNTERMITTENTLY IN FLIGHT. RT ENGINE OIL PRESSURE FLUCTUATED BETWEEN 25 PSI-60 PSI. REPLACED O-RING ON OIL BYPASS SENSOR IAW GE MM. 2 L 7 2 4T 4 T RT A52EU E8NE 2003031400084 20030314 00084 EU 2003 3 14 CX7A194J19 1 20020819 A 2611 WARNING LIGHT SAAB SF340 340B 7860101 EU AVIONICS VENT ILLUMINATED A CX7A B EMER. DESCENT N FALSE WARNING CR CRUISE 1 GL 03 309CE 340B201 AVIONICS SMOKE LIGHT ILLUMINATED IN FLIGHT, INDICATION APPEARED TO BE FALSE. LIGHT STILL ON AFTER SHUTDOWN. 2 L 7 2 4T RT A52EU 2003031400085 20030314 00085 EU 2003 3 14 CX7A194J20 1 20020917 A 2121 EVCTA465A FAN SAAB SF340 340B 7860101 EU CABIN BURNED OUT A CX7A O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 03 311CE 20346 9715 340B214 F/A REPORTED A BURNING ODOR IN THE MID SECTION OF THE CABIN. 2 L 7 2 4T RT A52EU 2003031400086 20030314 00086 EU 2003 3 14 CX7A194J22 1 20021114 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU LT ENG TAILPIPE OUT OF TOLERANCE A CX7A D RETURN TO BLOCK N FALSE WARNING CL CLIMB 1 GL 03 305CE 340B202 TAILPIPE HOT CWP LIGHT ILLUMINATED ON LEFT ENGINE IN FLIGHT. 2 L 7 2 4T RT A52EU 2003031400087 20030314 00087 EU 2003 3 14 CX7A194J24 1 20021213 A 2613 1734362450 SENSOR SAAB SF340 340B 7860101 EU LT ENG TAILPIPE CONTAMINATED A CX7A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 03 308CE 340B210 LT TAILPIPE HOT CWP CAME ON. 2 L 7 2 4T RT A52EU 2003031400088 20030314 00088 EU 2003 3 14 CX7A194J25 1 20021218 A 2613 1734362450 SENSOR SAAB SF340 340B 7860101 EU LT TAILPIPE CONTAMINATED A CX7A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 03 300CE 340B184 ON TAXI OUT LT TAILPIPE HOT CWP ILLUMINATED. 2 L 7 2 4T RT A52EU 2003031400107 20030314 00107 EU 2003 3 14 A8J2003F00000 1 20021213 A 2435 DRIVE SHAFT AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE STARTER GEN FAILED E A8JA O OTHER O OTHER NR NOT REPORTED 1 SW 09 300CV BJ133 322 304229B HAS SHEARED TWO SHAFTS ON TWO DIFFERENT ENGINES WITH APPROXIMATELY 30 HOURS WHEN OCCURENCE OCCURED. WE PURCHASED AN OX UNIT FROM THE SAME COMPANY THIS LAST TIME THE FAILURE OCCURED AND LOOKING AT THE PAPERWORK ON SN KK-81 (OX UNIT) IT SUBS EQUENTLY HAS SHEARED TWO DRIVE SHAFT THIS YEAR ON ANOTHER OPERATORS AIRCRAFT. ITS MY BELIEF THAT THERE IS A MATERIAL OR MFG DEFECT WITH THESE NEW DRIVE SHAFTS BEING INSTALLED. 2 L 7 2 4F 4 F A7EU E7EA 2003031400156 20030314 00156 NM 2003 3 14 S2YA02043 1 20021105 A 4900 230GC02Y04 CONTROL UNIT DORNER DO32 DO328300 NM APU INOPERATIVE A S2YA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 13 354SK 1049 3126 DURING FLIGHT 2152 MKE-BWI THE APU GENERATOR OVER SPEED AND AUTO SHUT DOWN. THE CREW DIVERTED TO GRR SINCE THE RIGHT EN GINES DC GENERATOR WAS ALREADY ON MEL. MECHANIC WAS DISPATCHED AND THEY REPLACED THE APU DC POWER CONTROL UNIT. MECHAN IC OPS CHECK THE APU DC SYSTEM WITH NO FURTHER DEFECT NOTED AND RETURNED THE AIRCRAFT TO SERVICE. 2 H 7 2 4T RT A55NM 2003031400157 20030314 00157 CE 2003 3 14 S2YA02044 1 20021110 A 3010 11438003651 BOOT BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA DEICE SYSTEM FAILED A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 901SK UE90 SHORTLY AFTER TAKEOFF OF FLIGHT 1035 MKE-RHI THE DEICE BOOTS DID NOT INFLATE AND THE ANNUNCIATOR DID NOT ILLUMINATE. TH E CREW MADE AN AIR-TURN-BACK TO MKE. MECHANIC INSPECTED THE DEICE SYSTEM AND FOUND THE LEFT HORIZONTAL BOOT HAD FAILED. MECHANIC REPLACED THE BOOT AND RETURNED THE AIRCRAFT TO SERVICE WITH NO FURTHER DEFECTS. 2 L 7 2 4T 3 T RT A24CE E2NE 2003031400158 20030314 00158 2003 3 14 S2YA02045 4 20021113 A 3416 066030620000 ALTIMETER BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LEFT FAILED A S2YA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 13 79SK 6867 UE79 SHORTLY AFTER TAKEOFF OF FLIGHT 1026 MKE-CVG THE CAPTAINS ALTIMETER FLAGGED AND THE ALTITUDE SELECT WENT BLANK. THE CRE W CYCLE THE CIRCUIT BREAKER BUT THE PROBLEM REMAINED. THE CREW MADE AN AIR-TURN-BACK TO MKE. MAINTENANCE RETURNED THE AIRCRAFT TO SERVICE WITH NO FURTHER DEFECTS. 2 L 7 2 4T 3 T RT A24CE E2NE 2003031400159 20030314 00159 NE 2003 3 14 S2YA02046 2 20021114 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT MALFUNCTIONED A S2YA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 13 148SK 18523 UE148 PCE114189 SHORTLY AFTER TAKEOFF OF FLIGHT 1053 MKE-CMH THE CREW NOTICED THE RIGHT ENGINE WAS NOT PRODUCING ENOUGH TORQUE. THE CRE W MADE AN AIR-TURN-BACK TO MKE. MECHANIC INSPECTED THE RIGHT ENGINE AND FOUND THERE WAS AN OBSTRUCTION IN THE P3 LINE T HAT GOES TO THE BLEED VALVE. MECHANIC REPLACED GAS GENERATOR AND OPS CHECKED THE SYSTEM, THE ENGINE WOULD NOW PRODUCE M AX TORQUE. MECHANIC RETURNED THE AIRCRAFT TO SERVICE WITH NO FURTHER DEFECTS. 2 L 7 2 4T 4 T RT A24CE E26NE 2003031400160 20030314 00160 2003 3 14 S2YA02047 4 20021125 A 3417 INDICATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA AIRSPEED MALFUNCTIONED A S2YA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 13 841SK UE84 DURING TAKEOFF OF FLIGHT 1371 MKE-LSE THE CREW NOTICED AT THE 80 KNOT CALLOUT THAT THE AIRSPEEDS DID NOT MATCH. THE CRE W ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MECHANIC INSPECTED THE AIRSPEEDS WITH THE PITOT STATIC TEST BOX AND FOU ND A 5 KNOT SPLIT AT VARIOUS SETTINGS. MECHANIC SWAPPED THE AIRSPEED INDICATORS, TESTED THE SYSTEM AGAIN WITH NO SPLIT NOTED. MECHANIC RETURNED THE AIRCRAFT TO SERVICE WITH NO FURTHER DEFECTS. 2 L 7 2 4T 3 T RT A24CE E2NE 2003031400161 20030314 00161 NM 2003 3 14 S2YA02048 1 20021126 A 3260 BULB DORNER DO32 DO328300 NM PWA 306 PW306B NE MLG INDICATOR BURNED OUT A S2YA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 13 359SK 3202 DURING APPROACH OF FLIGHT 2288 MKE-IAD THE CREW SELECTED GEAR DOWN BUT NOSE GEAR INDICATOR DID NOT ILLUMINATE. THE CREW HAD THE FIRE TRUCK ROLL AS A PRECAUTION. THE CREW MADE AN UNEVENTFUL LANDING. MECHANIC REPLACED THE BULBS AND RELEASE D THE AIRCRAFT. 2 H 7 2 4T 4 F RT A55NM E35NE 2003031400166 20030314 00166 NE 2003 3 14 TXHA6881 3 20021231 A 6111 BLADE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A60A 52043 NE HARTZL HCA6A HCA6A3A NE PROPELLER LOOSE E TXHA K NONE O OTHER IN INSP/MAINT 1 WP 13 827BE 2500 SH3746 AP37 ON 11/5/02, POST FLIGHT INSP WAS CARRIED OUT. FOUND 2 BLADES ON RIGHT PROP SN-AP37 TO HAVE EXCESSIVE FORWARD AND ACT PL AY. PROP MFG O/H FACILITY CONSULTED AND CONFIRMED PLAY TO BE EXCESSIVE. PROP REMOVED AND REPLACED. PREVENT RECURRENCE IS NOT TO USE MORE THAN 10 POUNDS OF FORCE WHEN INSPECTING BLADES IAW PROP MM. 2 H 7 2 4T 4 T A41EU E4EA 6 C P14NE 2003031400180 20030314 00180 SO 2003 3 14 000237 1 20021224 A 2750 WARNING LIGHT EMB 145 EMB145 3260210 SO TE FLAPS ILLUMINATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 276 T/O FLAPS CONFIGURATION WARNING. RESET A/C AND OPS CHECK GOOD 2 L 7 2 4F RT T00011AT 2003031400195 20030314 00195 CE 2003 3 14 001A 1 20021120 A 2810 FUEL TANK CESSNA 182 182S 2072701 CE RT WING LEAKING B B9YR K NONE K FLUID LOSS IN INSP/MAINT 1 GL 07 182AM 120 10 18280116 FUEL LEAKING FROM RIGHT WING ROOT, FUEL STAIN ON FUSELAGE. DRAINED FUEL, OPENED ACCESS PANELS OF FUEL TANK, FOUND SEALAN T USED AROUND FUEL CELL (WET WING) INTERIOR AT THE OUTLET HAD A VOID AREA UNDER THE OUTLET TUBE ASSEMBLY. APPARENT LACK OF ATTENTION TO DETAIL WHEN APPLYING THE SEALANT TO THIS AREA WAS THE PROBABLE CAUSE. TANK WAS RE-SEALED IN THIS AREA AN D TANK WAS RE-FUELED WITH NO LEAKS NOTED. 1 H 7 1 3O NT 3A13 2003031400197 20030314 00197 EU 2003 3 14 02FDEA00870 1 20021119 A 2760 ATTACH FITTING AIRBUS 310 A310 EU NR 3 SPOILER BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 RT WING NR 3 SPOILER, OUTBOARD ACTUATOR LUG BROKEN OFF. COMPLETELY MISSING. FOUND DURING C-CHECK INSPECTION BY MX TAS K CARD 46C0510. REMOVED AND REPLACED NR 3 RT SPOILER IAW MM 27-61-51-4 RIG AND OPS CHECKS GOOD GOOD IAW/MM 27-61-51 -4. SERVICE TAG NO.717764 , MPN/A5771001300000, S/N ON 1040, S/N OFF 016, MPN OFF AJ7700133000. DATE CLOSED 03/12/03. . 2 L 7 2 4F RT A35EU 2003031600001 20030316 00001 SO 2003 3 16 C2XA03SH055 1 20020316 A 5300 13500469401 SUPPORT EMB 135 EMB135ER 3260203 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14505 145192 SHV DURING C CHECK GALLEY FLOOR PROFILE Z ASSEMBLY WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED ASSEMBLY IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2003031800050 20030318 00050 NM 2003 3 18 2002UALA01865 1 20021219 A 3030 HEATER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE PITOT TUBE FAILED A UALA A UNSCHED LANDING G I J MULTIPLE FAILURE FLT. ATTITUDE INST. WARNING INDICATION CL CLIMB 1 WP 29 655UA 25393 CAPTAIN'S PITOT TUBE, RUDDER RATIO AND AILERON LIGHT CAME ON. CAPTAIN'S AIRSPEED INDICATOR NON OP, ALTIMETER VARIED PLU S 100, MINUS 200 FT AT FL330 WITH AUTOPILOT ENGAGED. ON DESCENT SYSTEMS RETURNED TO NORMAL. FLIGHT DIVERTED TO LAS. SU PPLEMENTAL DATA UPDATE AFTER A "CAPT PITOT TUBE" LIGHT CAME ON WITH THE CAPTAIN'S AIRSPEED IND INOP, ALTITUDE VARIED PL US 100 MINUS 200 FT AT FL 330 AND C A-P ENGAGED, FOUND AN ICING ON CAPTAIN'S PITOT PROBE. CAUSED BY A DEFECTIVE HEATER ELEMENT. LOSS OF CAPTAIN'S PITOT INPUT TO THE LT AIR DATA COMPUTER CAUSED THE CAPTAIN'S PITOT, RUDDER RATIO, AND AILERO N LIGHT TO DISPLAY ON EICAS. REPLACED CAPTAIN'S PITOT TUBE TO CORRECT HEATING ELEMENT AND LIGHTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2003031800051 20030318 00051 NM 2003 3 18 2002UALA01893 1 20021221 A 3240 C2021622 CONTROL UNIT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE BRAKE SYSTEM FAILED A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 848UA 1647 ANTI-SKID NWS MESSAGE ON ECAM. LOST ANTISKID AND NOSE WHEEL STEERING. AIRCRAFT TOWED TO GATE. SUPPLEMENTAL DATA UPDATE RECYCLED BSCU CB'S M33,M34,M35 & M36, SYSTEM RETURNED TO NORMAL WITH NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2003031800057 20030318 00057 NE 2003 3 18 2003F00130 2 20021023 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT MALFUNCTIONED A UHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 17 152CQ 152 FLT 4512, DURING CRUISE, ITT SPIKE ON RT ENGINE FROM 800 DEGREES TO 855 DEGREES FOR ONE MINUTE AT 88 PERCENT TORQUE, RED UCED TORQUE TO 83 PERCENT, ITT FLUX 766 DEGREES TO 826 DEGREES THEN STABILIZED AT 766 DEGREES, LT ENGINE AT 750 DEGREES, RETURNED TO BNA. PERFORMED A GROUND RUN, NO DEFECTS NOTED, A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 2003031800058 20030318 00058 EU 2003 3 18 2003F00132 1 20021118 A 6120 CONTROLLER SAAB SF340 SF340A 7850100 EU AUTOCOARSEN MALFUNCTIONED A UHLA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 NE 03 19XS 340A019 FLT 4472 - CLE-PIT - ABORTED TAKEOFF DUE TO AUTOCOARSEN WOULD NOT ARM DURING TAKEOFF ROLL. TORQUE WAS 90 PERCENT, AIRSP EED BETWEEN 90 AND 100 KNTS AND SWITCH IN THE ON POSITION. CONTRACT MAINTENANCE AND THE FLIGHT CREW PERFORMED THE P3 AN D AUTOCOARSEN TEST, OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 2003031800059 20030318 00059 2003 3 18 2003F00134 4 20021125 A 3425 INDICATOR SAAB SF340 SF340A 7850100 EU AHARS MALFUNCTIONED A UHLA D RETURN TO BLOCK I FLT. ATTITUDE INST. TX TAXI/GRND HDL 1 NE 03 118SD 118 FLT 4480 - PIT-TOL - AIRCRAFT RETURNED TO GATE, CO-PILOTS AHARS FLAGGED / EADI 25 DEGREES PITCH DOWN AND 10 DEGREES LEFT , EHSI COMPASS SLEWS CLOCKWISE, NORMAL AFTER 30 MINUTES. SECOND OF 2 SQUAWKS FOR THIS FLIGHT. (M) 2 L 7 2 4T RT A52EU 2003031800060 20030318 00060 2003 3 18 2003F00135 4 20021121 A 3425 6226190113 INDICATOR SAAB SF340 SF340A 7850100 EU AHRS MALFUNCTIONED A UHLA A UNSCHED LANDING O OTHER CR CRUISE 1 NE 03 340SZ 340A004 FLT 4468 - AIRTURN BACK AND RETURNED TO TTN - PILOT REPORTED HEADING MISMATCH BETWEEN CA AND FO 80-180 DEGREES FLAGGED I N FLIGHT HEADINGS MOMENTARILY LOCKED AND THEN FLAGGED AGAIN AND REMAINED SPLIT. (M) 2 L 7 2 4T RT A52EU 2003031800068 20030318 00068 NM 2003 3 18 AMTA200300175 1 20021128 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM CARGO BAY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 312TZ 32579 AFT CARGO COMPARTMENT FLOOR PANEL 140AF CORRODED. REPLACED FLOOR PANEL IAW AMM 25-25-10-400-801. (M) 2 L 7 2 4F RT A16WE 2003031800069 20030318 00069 NM 2003 3 18 AMTA200300176 1 20021129 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM CARGO BAY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 312TZ 32579 AFT CARGO COMPARTMENT FLOOR PANELS 140BF AND 140CF CORRODED. REPLACED FLOOR PANELS IAW AMM 25-25-10-400-801. (M) 2 L 7 2 4F RT A16WE 2003031800079 20030318 00079 WP 2003 3 18 ASAA0280443 1 20021022 A 5754 9954169556 DOOR DOUG DC9 DC983 3022083 WP SLAT TRACK CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - FOUND DURING 30K-CHECK, RIGHT NR 5 SLAT TRACK DOOR CHAFED AT FORWARD END. REPLACED SLAT TRACK DOOR PER MM 27-80-0 1. (M) 2 L 7 2 4F RT A6WE 2003031800109 20030318 00109 NM 2003 3 18 BJNA021201 1 20021129 A 2560 P4010021 BATTERY PACK BOEING 737 737282 13844AT NM FLASHLIGHT DISCHARGED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 23043 AFT EMERGENCY FLASH LIGHT BATTERY CONDITION INDICATOR NOT BLINKING. REPLACED BATTERY PACK, NORMAL MAINTENANCE. (M) 2 L 7 2 4F RT A16WE 2003031800124 20030318 00124 NM 2003 3 18 GAIA02158OP 1 20021119 A 3260 ACCESSORY UNIT BOEING 727 727251 138408H NM E/E BAY MALFUNCTIONED A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 278US 21157 FLT - 215 - DEN-FWA - ON APPROACH TO FWA, WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION THE NOSE LANDI NG GEAR RED LIGHT REMAINED ILLUMINATED. THE GEAR WAS RECYCLED AND THE RED LIGHT EXTINGUISHED. THE AIRCRAFT LANDED WITH OUT FURTHER INCIDENT. RE-RACKED THE LANDING GEAR ACCESSORY UNIT. OPERATIONALLY CHECKED GOOD. INSPECTION COLD NOT DUPL ICATE THE PROBLEM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2003031800125 20030318 00125 NM 2003 3 18 GAIA02159OP 1 20021120 A 3350 1000679 SIGN BOEING 727 727251 138408H NM COCKPIT INOPERATIVE A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 278US 21157 DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLAC ED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2003031800126 20030318 00126 NM 2003 3 18 GAIA02161ST 1 20021127 A 5310 STRUCTURE BOEING 727 727223 1384074 NM FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6808 19483 DURING MAINTENANCE, DAMAGE WAS DISCOVERED AT BS 540 BETWEEN S18L AND S19L. REPAIR WAS ACCOMPLISHED IAW FLIGHT VEHICLES CONSULTING INC DRAWING 53-02679-1. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2003031800127 20030318 00127 NM 2003 3 18 GAIA02162OP 1 20021203 A 3260 656021132 ACCESSORY UNIT BOEING 727 727251 138408H NM E/E BAY INTERMITTENT A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 278US 21157 FLT 715 - ELP-FWA - ON APPROACH TO FW, WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION. THE NOSE LANDIN G GEAR RED LIGHT REMAINED ILLUMINATED WITH NO NOSE GREEN LIGHT AT ALL. THE GEAR WAS RE-CYCLED AND THE RED LIGHT REMAINE D ON. FIVE MINUTES LATER WITH THE GEAR HANDLE SELECTED DOWN THE NOSE GEAR RED LIGHT EXTINGUISHED AND THE GREEN DOWN AND LOCKED LIGHT ILLUMINATED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED THE LANDING GEAR ACCESSO RY UNIT. OPERATIONALLY CHECKED GOOD ON THE GROUND. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2003031800128 20030318 00128 NM 2003 3 18 GAIA02163OP 1 20021204 A 3260 CONNECTOR BOEING 727 727251 138408H NM NLG LOOSE A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 278US 21157 FLT 715 - ELP-FWA - ON APPROACH TO FWA, WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION THE NLG RED UNSA FE LIGHT REMAINED ILLUMINATED. THE GEAR WAS RE-CYCLED AND ALL THREE DOWN AND LOCKED LIGHTS ILLUMINATED. THE AIRCRAFT L ANDED WITHOUT FURTHER INCIDENT. CLEANED AND RESECURED BOTH ENDS OF THE NOSE GEAR DOWN LOCK SWITCH CONNECTOR PLUG. OPER ATIONALLY CHECKED GOOD. INSPECTION COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2003031800129 20030318 00129 NM 2003 3 18 GAIA02164OP 1 20021206 A 3260 H10101534 SWITCH BOEING 727 727251 138408H NM NLG INTERMITTENT A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 278US 21157 FLT 272 - LAX-FWA - DURING LANDING APPROACH TO FWA, WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION, THE NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. THE GEAR WAS RECYCLED AND A VISUAL CHECK WAS MADE THROUGH THE NOSE GEAR VIEW PORT. ALL THREE DOWN AND LOCKED LIGHTS ILLUMINATED DURING MANEUVERING TO LAND. THE AIRCRAFT LANDED WIT HOUT FURTHER INCIDENT. REMOVED AND REPLACED THE NOSE GEAR EXTENSION/RETRACTION SWITCH AND NOSE GEAR POSITION WARNING SW ITCH. LANDING GEAR RETRACTION CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2003031800138 20030318 00138 WP 2003 3 18 GTIA021335 1 20021221 A 5754 SKIN DOUG DC9 DC982 3022082 WP LT WING LE FLAP GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND LEFT WING INBOARD FLAP INBOARD LEADING EDGE CAP GOUGED. FABRICATED NEW PART. REMOVED LEFT INBOARD LEADING EDGE CAP. INSTALLED LEFT LEADING EDGE INBOARD FLAP NEW CAP. (M) 2 L 7 2 4F A6WE 2003031800139 20030318 00139 WP 2003 3 18 GTIA021336 1 20021223 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND AFT PIT CRACKED FLOOR INTERCOSTAL AT FS 1287-1309 '0' BL. REMOVED INTERCOSTAL. FABRICATED NEW INTERCOSTAL. INSTALLED NEW FABRICATED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2003031800140 20030318 00140 WP 2003 3 18 GTIA021337 1 20021222 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND MAIN CABIN FLOORBOARD STATION 140-199 NR 5 MISSING INSERTS, DETERIORATING. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2003031800141 20030318 00141 WP 2003 3 18 GTIA021338 1 20021222 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND MAIN CABIN FLOORBOARD STATIN 140-199 NR 3 DETERIORATED. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2003031800142 20030318 00142 WP 2003 3 18 GTIA021339 1 20021222 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - MAIN CABIN FLOORBOARD STATION 120-140 NR 3 DETERIORATED BLUE WATER STAINS. DRILLED AND LOCATED. (M) 2 L 7 2 4F A6WE 2003031800143 20030318 00143 WP 2003 3 18 GTIA021340 1 20021222 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND MAIN CABIN FLOORBOARD STATION 120-140 NR 4 DETERIORATED, LOCATED AND DRILLED. (M) 2 L 7 2 4F A6WE 2003031800144 20030318 00144 WP 2003 3 18 GTIA021341 1 20021222 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND MAIN CABIN FLOORBOARD STATION 140-199 NR 5 DETERIORATED, LOCATED AND DRILLED. (M) 2 L 7 2 4F A6WE 2003031800145 20030318 00145 WP 2003 3 18 GTIA021342 1 20021222 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND MAIN CABIN FLOORBOARD STATION 198-250 NR 4 MISSING INSERTS, DETERIORATED. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2003031800146 20030318 00146 WP 2003 3 18 GTIA021343 1 20021223 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CABIN FLOORBOARD LEFT INBOARD STATION 864-886 INSERTS PULLED THROUGH, CORROSION. LOCATED AND DRILLED FLOORB OARD. (M0 2 L 7 2 4F A6WE 2003031800147 20030318 00147 WP 2003 3 18 GTIA021344 1 20021223 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CABIN FLOORBOARD RIGHT STATOIN 869-886 CORNER BROKEN, CORROSION. FABRICATED PANEL. (M) 2 L 7 2 4F A6WE 2003031800148 20030318 00148 WP 2003 3 18 GTIA021345 1 20021223 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CABIN FLOORBOARD RIGHT STATION 826-844 BROKEN OUT INSERTS, CORROSION. FABRICATED NEW PANEL. (M) 2 L 7 2 4F A6WE 2003031800149 20030318 00149 WP 2003 3 18 GTIA021346 1 20021224 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CABIN FLOOR PANEL STATION 927-1003 DETERIORATED, DRILLED AND LOCATED. (M) 2 L 7 2 4F A6WE 2003031800150 20030318 00150 WP 2003 3 18 GTIA021347 1 20021228 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND LEFT INBOARD FLOOR PANEL STATION 1271 TO STATION 1309 INBOARD FACE HAS DENTED/DAMAGES AND CRACKED SEVERAL AR EAS. FABRICATED PANEL. (M) 2 L 7 2 4F A6WE 2003031800151 20030318 00151 WP 2003 3 18 GTIA021348 1 20021228 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CENTER FLOOR PANEL STATION 1309 TO STATION 1338 HAS SOFT/MUSHEY DETERIORATED, LOCATED AND DRILLED. (M) 2 L 7 2 4F A6WE 2003031800152 20030318 00152 WP 2003 3 18 GTIA021349 1 20021229 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND FLOOR PANEL STATION 1079-1155 LEFT INBOARD HAS CRACK/SOFT CORROSION AT INSERTS AND ELONGATED HOLES. FABRICA TED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2003031800153 20030318 00153 WP 2003 3 18 GTIA021350 1 20021229 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CABIN FLOOR PANEL STATION 693-769 LEFT, DENTED AND CORRODED. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2003031800154 20030318 00154 WP 2003 3 18 GTIA021351 1 20021229 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CABIN FLOOR PANEL STATION 769-826 LEFT DETERIORATING, MISSING INSERT. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2003031800155 20030318 00155 WP 2003 3 18 GTIA021352 1 20021221 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND FORWARD CARGO LOWER DOOR JAMB HAS CORROSION UNDER DOOR STOP SET SCREW PLATES, UNDER SEALANT AND ENTIRE LENGT H OF DOOR AREA. REMOVED LOWER DOOR PAN SECTION. INSTALLED LOWER DOOR PANEL SECTION. (M) 2 L 7 2 4F A6WE 2003031800156 20030318 00156 WP 2003 3 18 GTIA021353 1 20021223 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - AFT CARGO DOOR JAMB LOWER, HAS CORROSION UNDER SET SCREW PLATES AND THROUGH PUT LENGTH OF DOOR JAMB. REMOVED AFT CARGO DOOR JAMB BEAM. LOCATED AND DRILLED NEW JAMB BEAM. INSTALLED JAMB BEAM. (M) 2 L 7 2 4F A6WE 2003031800157 20030318 00157 WP 2003 3 18 GTIA021354 1 20021117 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND DOOR JAMB BEAM REPAIR STRAP HAS CORROSION UNDER STRAP AND ON JAMB BEAM. REMOVED DOOR JAMB BEAM TO BE OUT OF LIMITS. HOLES LOCATED AND DRILLED ON NEW JAMB BEAM. REMOVED DOOR JAMB WEB STATION 1150-1220 STRINGER 28-29 RIGHT SIDE . FABRICATED NEW DOOR WEB. INSTALLED DOOR WEB. INSTALLED DOOR JAMB BEAM. REMOVED CORROSION ON DOOR BEAM TO SKIN ANGL E, OUT OF LIMITS. INSTALLED DOOR BEAM SKIN ANGLE. (M) 2 L 7 2 4F A6WE 2003031800158 20030318 00158 WP 2003 3 18 GTIA021355 1 20021226 A 5320 WEB DOUG DC9 DC982 3022082 WP PAX DOORWAY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND L1 DOOR WEB STATION 200-208 CORRODED. FABRICATED L-1 DOOR WEB. (M) 2 L 7 2 4F A6WE 2003031800159 20030318 00159 WP 2003 3 18 GTIA021356 1 20021224 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND PASSENGER SEAT TRACK CORRODED AT FS 613-840 LEFT SIDE OUTBOARD TRACK. LEFT SIDE OUTBOARD TRACK FROM STATION 734-854 IS OUT OF LIMITS. REMOVED LEFT OUTBOARD SEAT TRACK. FABRICATED DRILLED AND LOCATED NEW SEAT TRACK SECTION AND SPLICES. INSTALLED NEW TRACK SECTION AND SPLICES. (M) 2 L 7 2 4F A6WE 2003031800160 20030318 00160 WP 2003 3 18 GTIA021357 1 20021226 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND FORWARD CABIN FLOOR WEB STATION 200-218 CORRODED. FABRICATED NEW WEB. (M) 2 L 7 2 4F A6WE 2003031800161 20030318 00161 WP 2003 3 18 GTIA021358 1 20021228 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND AT FS 795 LB2 44A CRACK IN FLOOR WEB 2 INCHES LONG FROM EOP TO LIGHTENING HOLE, AT FS 795 LBL 44 A PIECE OF FLOOR WEB 1 INCH BY .500 INCH MISSING, AT FS 800 LBL 44 A TOOL MARK OF .75 INCH BY .75 INCH WITH HOLE IN WEB. REMOVED D AMAGED AREAS. FABRICATED, LOCATED AND DRILLED DOUBLERS AND FILLE. INSTALLED DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2003031800162 20030318 00162 WP 2003 3 18 GTIA021359 1 20021223 A 5310 BEAM DOUG DC9 DC982 3022082 WP CARGO DOORWAY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND MID PIT CORROSION AT 2 ANGLE FORWARD RIGHT SIDE STATION 636 TO STATION 598. MID PIT LOWER DOOR CUTOUT OUTBO ARD BEAM CORRODED STATION 693 TO STATION 636. REMOVED JAMB BEAM. LOCATED AND DRILLED BEAM. INSTALLED MID PIT LOWER DO OR JAMB BEAM. (M) 2 L 7 2 4F A6WE 2003031800163 20030318 00163 WP 2003 3 18 GTIA021360 1 20021222 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND FLOOR PANEL MAIN CABIN STATION 198-250 NR 6 BROKEN FIBERGLASS SUPPORTS BLUE WATER STAINS, DETERIORATED. REP AIRED FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2003031800164 20030318 00164 WP 2003 3 18 GTIA021361 1 20021226 A 5210 SKIN DOUG DC9 DC982 3022082 WP PAX DOOR GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND OUTSIDE BOTTOM EDGE OF L1 DOOR IS GOUGED, DENTED AND CRACKED. REMOVED LOWER SKIN ATTACH ANGLE. ANGLE FOUND TO BE CRACKED. FABRICATED NEW ANGLE. REMOVED DAMAGE AT FORWARD LOWER CORNER. FABRICATED 7 REPAIR FILLER. FABRICATED 5 REPAIR DOUBLER. INSTALLED REPAIR PARTS AND ATTACH ANGLE. (M) 2 L 7 2 4F A6WE 2003031800165 20030318 00165 WP 2003 3 18 GTIA021362 1 20021224 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP MLG CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND LEFT MLG FORWARD DOOR JAMB CUTOUT DOUBLER REPAIR CRACKED. REMOVED DAMAGE AREA. FABRICATED CHANNEL. FABRIC ATED SPLICE TWO EACH. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2003031800166 20030318 00166 WP 2003 3 18 GTIA021363 1 20021223 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND AFT PIT CRACKED FLOOR INTERCOSTAL AT FS 1271-1287 '0'BL. LOCATED AND DRILLED PART. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2003031800167 20030318 00167 WP 2003 3 18 GTIA021364 1 20021223 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CABIN FLOORBOARD STATION 927-1003 NR 5 CORNER BROKEN CORRODED. FABRICATED NEW CABIN FLOORBOARD. (M) 2 L 7 2 4F A6WE 2003031800168 20030318 00168 WP 2003 3 18 GTIA021365 1 20021221 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP EMERGENCY EXIT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND AFT OVERWING EXIT RIGHT FORWARD INSIDE EDGE OF FRAME IS CRACKED. FABRICATED DOUBLERS REPAIR. INSTALLED DOUB LERS REPAIR ON INNER SKIN AND DOOR PANEL. (M) 2 L 7 2 4F A6WE 2003031800170 20030318 00170 WP 2003 3 18 GTIA021366 1 20021227 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CORROSION, LOWER SIDE OF 'Z' FRAME AT FS 1258 AT L18L. REMOVED DAMAGED AREA OF 'A' FRAME. FABRICATED REPAI R DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER, FILLER. (M) 2 L 7 2 4F A6WE 2003031800171 20030318 00171 WP 2003 3 18 GTIA021367 1 20021223 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CABIN LEFT OUTBOARD FLOORBOARD STATION 807-916, HAS CORROSION ELONGATED HOLES, TORN INSULATION, BENT CORNERS . REMOVED OLD SKIN. FABRICATED NEW SKIN. INSTALLED NEW SKIN. (M) 2 L 7 2 4F A6WE 2003031800172 20030318 00172 WP 2003 3 18 GTIA021368 1 20021222 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND MAIN CABIN FLOORBOARD 199-250 NR 2 DETERIORATING AND BLUE WATER STAINS. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2003031800173 20030318 00173 WP 2003 3 18 GTIA021369 1 20021222 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND FLOOR PANEL MAIN CABIN STATION 198-250 NR 5 FIBERGLASS SUPPORT BROKEN AT ENDS. REPAIRED FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2003031800174 20030318 00174 WP 2003 3 18 GTIA021370 1 20021224 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP PAX DOOR DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND R1 DOOR CUTOUT FRAME DENTED MIDWAY DOWN AFT AREA. REMOVED DOOR JAMB PAN. LOCATED AND DRILLED NEW PANEL. I NSTALLED DOOR PAN. (M) 2 L 7 2 4F A6WE 2003031800175 20030318 00175 WP 2003 3 18 GTIA021371 1 20021223 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP MLG CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND RIGHT WHEEL WELL FORWARD INBOARD DOOR FRAME IS CRACKED. REMOVED DAMAGE. LOCATED AND DRILLED U-CHANNEL AND SPLICES. INSTALLED U-CHANNEL AND SPLICES. (M) 2 L 7 2 4F A6WE 2003031800176 20030318 00176 WP 2003 3 18 GTIA021372 1 20021221 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP PAX DOOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND L1 DOOR AFT LOWER INSIDE LIGHTING HOLE HAS 1 INCH CRACK AND METAL DAMAGE. REMOVED AFT LOWER WEB. DRILLED/L OCATED NEW WEB. INSTALLED AFT LOWER WEB. (M) 2 L 7 2 4F A6WE 2003031800177 20030318 00177 WP 2003 3 18 GTIA021373 1 20021226 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND DENT AT FS 1332-1352, BETWEEN LONGERONS 21R AND 23R, (X=096, D=1) DX=10.41. FABRICATED INNER DOUBLER. INST ALLED INNER DOUBLER. (M) 2 L 7 2 4F A6WE 2003031800178 20030318 00178 WP 2003 3 18 GTIA021374 1 20021226 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND DENT FS 93 BETWEEN LONGERONS 18 AND 19L IS TOO CLOSE TO STRUCTURE (X=.034, D=1.0) DX=29.41. CUTOUT DENTED/D AMAGED AREA (2 PLACES) AT FS 93 AND FS 96. FABRICATED REPAIR DOUBLER AND FILLERS. INSTALLED FABRICATED REPAIR DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2003031800180 20030318 00180 WP 2003 3 18 GTIA021376 1 20021224 A 5397 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - PASSENGER SEAT TRACK CORRODED AT FS 613-840, LEFT SIDE OUTBOARD TRACK. LEFT SIDE OUTBOARD TRACK FROM STATION 734- 854 IS OUT OF LIMITS. REMOVED LEFT OUTBOARD SEAT TRACK. FABRICATED DRILLED AND LOCATED NEW TRACK SECTION AND SPLICES. INSTALLED NEW TRACK SECTION AND SPLICES. (M) 2 L 7 2 4F A6WE 2003031800181 20030318 00181 WP 2003 3 18 GTIA021378 1 20021229 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CABIN FLOOR PANEL STATION 796-826 LEFT OUTBOARD HAS CORROSION. INSTALLED NEW SKIN PANEL. (M) 2 L 7 2 4F A6WE 2003031800182 20030318 00182 WP 2003 3 18 GTIA021379 1 20021229 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CABIN FLOORBOARD STATION 693-769 LEFT HAS CORROSION AND LOOSE TORN INSULATION. REMOVED OLD SKIN. FABRICATE D NEW SKIN. INSTALLED NEW SKIN. (M) 2 L 7 2 4F A6WE 2003031800183 20030318 00183 WP 2003 3 18 GTIA021380 1 20021228 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CENTER FLOOR PANEL STATION 1271 TO STATION 1309 HAS CRACKED, SOFT/MUSHEY, CORRODED AT INSERTS ELONGATED HOLE S. DRILLED AND LOCATED NEW PANEL. (M) 2 L 7 2 4F A6WE 2003031800184 20030318 00184 WP 2003 3 18 GTIA021381 1 20021228 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN CRACKED A K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND FLOOR PANEL STATION 1271-1309, RIGHT SIDE INBOARD HAS CRCKED/DAMAGED AT BOTTOM PANEL. FABRICATED NEW PANEL. (M) 2 L 7 2 4F A6WE 2003031800188 20030318 00188 WP 2003 3 18 GTIA021382 1 20021226 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND AFT PIT FLOOR PANEL STATION 1007-1155 DELAMINATED AND CORROSION. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2003031800189 20030318 00189 WP 2003 3 18 GTIA021383 1 20021224 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CABIN FLOORBOARD STATION 927-1300 BENT, TORN, CORRODED. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2003031800198 20030318 00198 WP 2003 3 18 GTIA021384 1 20021223 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CABIN FLOORBOARD STATION 826-886, DETERIORATED, METAL SUPPORTS HAVE GOUGES, CORROSION, TORN. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2003031800203 20030318 00203 WP 2003 3 18 GTIA021385 1 20021223 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CABIN FLOORBOARD STATION 886-946 CENTER, BROKEN OUT INSERTS, CORROSION ON METAL SUPPORTS. FABRICATED PANEL. (M) 2 L 7 2 4F A6WE 2003031800204 20030318 00204 WP 2003 3 18 GTIA021386 1 20021226 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND PASSENGER SEAT TRACK CORRODED AT FS 1026-1309, LEFT SIDE OUTBOARD TRACK. (M) 2 L 7 2 4F A6WE 2003031800207 20030318 00207 WP 2003 3 18 GTIA021387 1 20021231 A 5300 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP E/E BAY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND E/E COMPARTMENT TWO RIGHT INBOARD LATCH SUPPORT BRACKETS CORRODED. FOUND RIGHT OUTBOARD AFT LATCH SUPPORT B RACKET TO BE OUT OF LIMITS. REMOVED FRAME RIGHT STATION 148 LONGERON 28. FOUND FRAME RIGHT STATION 148 LONGEORN 28 TO B E OUT OF LIMITS. FORMED NEW SECTION OF FRAME. INSTALLED NEW SECTION OF FRAME. INSTALLED NEW BRACKET RIGHT OUTBOARD AF T LATCH SUPPORT. (M) 2 L 7 2 4F A6WE 2003031800208 20030318 00208 WP 2003 3 18 GTIA021393 1 20021219 A 5300 WEB DOUG DC9 DC982 3022082 WP SUBFLOOR CORRODED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 803NK 48087 FTW - E/E COMPARTMENT SUBFLOOR WEB IS CORRODED AT STATION 206, LBL 12 STATION 196, LBL 6, STATION 200 RBL. REMOVED DAMA GED FLOOR WEB FS 200 FS 219 LBL 26 - RBL 26. FABRICATED NEW FLOOR WEB FS 160-200 LBL 16 - RBL 54. FABRICATED NEW FLOOR WEB FS 200-219 LBL 26 - RBL 26. FABRICATED FLOOR WEB REPAIR SPLICE REPAIR FS 160-200 LBL 26. INSTALLED SPLICE FOR WEB REPAIR. INSTALLED FLOOR WEB STATION 160-200 LBL 16 - RBL 54. INSTALLED FLOOR WEB STATION 200-219 LBL 26 - RBL 26. (M ) 2 L 7 2 4F A6WE 2003031800209 20030318 00209 WP 2003 3 18 GTIA021400 1 20021230 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FLIGHT COMPARTMENT SUB FLOOR IS CRACKED 2 PLACES BELOW CAPTAINS MID/LOWER SEAT TRACK STATION 135, 160, CORRODED AT STATION 133-160 AS VIEWED FROM E/E COMPARTMENT. REMOVED COCKPIT FLOOR WEB FROM STATION 133, 160 LBL 40 RBL 20. FABRIC ATED NEW FLOOR WEB FS 133-160 LBL 40 RBL 20. INSTALLED COCKPIT FLOOR WEB. (M) 2 L 7 2 4F A6WE 2003031800210 20030318 00210 WP 2003 3 18 GTIA021401 1 20021223 A 5347 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND CUSP WEB CORRODED AT STATION 220 LBL 54 AT FRAME. REMOVED CUSP STAITON 180-230 L18L. FABRICATED NEW SECTIO N OF CUSP AND SPLICE TO 230 LBL 54. INSTALLED CUSP SECTION AND SPLICE. (M) 2 L 7 2 4F A6WE 2003031800211 20030318 00211 WP 2003 3 18 GTIA021402 1 20021229 A 5730 PANEL DOUG DC9 DC982 3022082 WP RT WING TE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND RIGHT WING UPPER TRAILING EDGE PANEL HAS COMPOSITE MATERIAL EXPOSED AND PANEL IS DELAMINATED ON LOWER SIDE. REMOVED DAMAGED PANEL. REPAIRED RIGHT WING UPPER TRAILING EDGE INBOARD PANEL. INSTALLED WING PANEL. (M) 2 L 7 2 4F A6WE 2003031800212 20030318 00212 WP 2003 3 18 GTIA021403 1 20021223 A 5210 PANEL DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND FORWARD PASSENGER DOOR HAS CRACK ON DOOR PANEL ASSEMBLY LOWER FORWARD EDGE OF DOOR AT LOWER HINGE. DRILLED OFF CRACKED PANE ASSEMBLY. LOCATED AND DRILLED NEW PANEL. INSTALLED NEW PANEL. (M) 2 L 7 2 4F A6WE 2003031900018 20030319 00018 WP 2003 3 19 GTIA030020 1 20020103 A 2822 PUMP DOUG DC9 DC983 3022083 WP FUEL BOOST INOPERATIVE A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 802NK 53168 ORD - FLT 1225 - AFT CENTER BOOST PUMP INOPERATIVE. LOW PRESSURE LIGHT ILLUMINATES WTH AFT CENTER PUMP ONLY RUNNING. P ULLED AND RESET CIRCUIT BREAKER. LIGHT GOES OUT FOR 25 SECONDS THE ILLUMINATES. UNSCHEDULED CHANGE OF A/C EN ROUTE. ( M) 2 L 7 2 4F RT A6WE 2003031900057 20030319 00057 NM 2003 3 19 HALA0200702 1 20021120 A 2420 GENERATOR BOEING 717 717200 1383700 NM LEFT FAILED A HALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION DE DESCENT 1 WP 13 480HA 55125 FLT 541 - HNL - NUMEROUS POEWR INTERUPTIONS ON DESCENT TO HNL. NO BREAK POWER TRANSFER APPEAR INOPERATIVE. EMERGENCY L IGHTS ON (5 TIMES). INTERMITTENT ANNUNCIATOR LIGHTS, DCU FAIL. NR 1 ENGINE VIBE HIGH, INDICATED 5.0 PLU (AMBER) FOR NR 1 N1 ON ONE OCCASSION. LEFT GENERATOR APPEARED FAILED. RIGHT GENERATOR WAS POWERING LEFT AC BUSS. REPLACED LEFT GENE RATOR ASSEMBLY. OPS CHECK LEAK CHECK NORMAL. (M) 2 L 7 2 4F TR A6WE 2003031900058 20030319 00058 NM 2003 3 19 HALA0200703 1 20021120 A 5247 PIVOT BOEING 717 717200 1383700 NM APU DOOR CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 486HA 55131 FOUND CRACK APPROXIMATELY 2 INCHES ON UPPER APU DOOR FLANGE AT BASE OF PIVOT ROD. REPLACED APU DOOR ASSEMBLY. OPS CHEC K OK. (M) 2 L 7 2 4F TR A6WE 2003031900065 20030319 00065 NM 2003 3 19 KPVA20033 1 20020106 A 3350 10005511 LIGHT DHAV DHC8 DHC8103 1386005 NM PORTABLE INOPERATIVE A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808WP 026 PORTABLE EMERGENCY LIGHT IN FLIGHT COMPARTMENT WEAK. REMOVED AND REPLACED PORTABLE EMERGENCY LGIHT IN FLIGHT COMPARTMEN T. OPS CHECK GOOD IAW DHC 8MM 33-51-00 PAGE 201-202. NO DEFECTS NOTED. (M) 2 H 7 2 4T RT A13NM 2003031900068 20030319 00068 2003 3 19 MEX2002353 4 20020312 A 3425 4608000306 DISPLAY DOUG DC9 DC987 3022087 WP AHRU FAILED A ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 1075T 49724 FLT 353 - MEX-ZIH - AIRCRAFT RETURNED DUE TO PFD AND ND NAVIGATIONAL SYSTEM FAILURE, FIRST OFFICER RDMI FLAGS, AUTOMATIC PILOT, THROTTLES AND DIRECTOR BARS OUT OF SERVICE AND FMA WITHOUT INFORMATION. TECH PERSONNEL RECEIPT THE EQUIPMENT OP ERATING IN NORMAL WAY. STP TEST WAS ACCOMPLISHED DETECTING FAIL IN THE LEFT AHRU. AHRU WAS REPLACED IAW MM 34-21-10. THERE WAS ACCOMPLISHED A RETURN TO SERVICE TEST TO BOTH FLIGHT COMPUTERS IAW MM 22-04-05, ALL CORRECT. (M) 2 L 7 2 4F RT A6WE 2003031900080 20030319 00080 EA 2003 3 19 REXA02023 1 20021122 A 2611 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA SMOKE DETECT MALFUNCTIONED A REXA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 25 8554A 7554 ON APPROACH CREW RECEIVED A FALSE CARGO SMOKE WARNING RESULTING IN THE OPERATION OF THE EXTINGUISHING SYSTEM. UPON INVE STIGATION FOUND FIRE WARNING CONTROL COMPUTER TO BE MALFUNCTIONING. REMOVED AND REPLACED CONTROL SYSTEM OPERATES NORMAL LY. (M) 2 L 7 2 4F RT A21EA 2003031900084 20030319 00084 SO 2003 3 19 SIMA200233836 1 20021129 A 2130 14534417405 DUCT EMB 135 EMB135LR 3260305 SO APU SYSTEM CRACKED A SIMA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 722AE 145287 JFK - FLT 4775 - AFTER TAKEOFF, CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE BOTH PACKS AND CIRCUIT BREAKER B-8 WERE RESET BY CREW WITH NO EFFECT. CABIN RATE WOULD GO FROM -200 TO -1950 THEN TO AMBER DASHES. MAINTENANCE FOND THE APU BL EED 'Y' DUCT CRACKED. DUCT WAS REPLACED IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT T00011AT 2003031900085 20030319 00085 SO 2003 3 19 SIMA200235102 1 20021215 A 2560 P2070009120 FLASHLIGHT EMB 135 EMB135KL 3260302 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 820AE 145576 FLT 3803 - CREW REPORTED AN ELECTRICAL ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS AND FLIGHT ATTEND ANTS FLASHLIGHT ASSEMBLIES. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2003031900086 20030319 00086 SO 2003 3 19 SIMA200235103 1 20021214 A 3150 WARNING LIGHT EMB 135 EMB135KL 3260302 SO GUST LOCK ILLUMINATED A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 800AE 145425 LAX - FLT 3446 - DURING CRUISE FLIGHT, REPORTED THE GUST LOCK AMBER LIGHT CAME ON DURING LIGHT CHOP. CREW FOLLOWED PROC EDURES AND DECLARED AN EMERGENCY. AIRCRAFT WAS DIVERTED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK WAS SATISFACTORY IAW EMB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2003031900087 20030319 00087 EA 2003 3 19 SIMA200235104 1 20021215 A 2782 766385A ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA RT WING SLAT INOPERATIVE A SIMA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 502AE 10018 BOI - FLT 3903 - DURING DESCENT WHEN FLAPS WERE LOWERED CREW RECEIVED A SLATS FAIL MESSAGE ON EICAS. AN EMERGENCY WAS D ECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE RIGHT SLAT ACT UATOR IAW CRJ MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2003031900088 20030319 00088 SO 2003 3 19 SIMA200235105 1 20021216 A 2700 1SE1 SWITCH EMB 135 EMB135KL 3260302 SO YOKE FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 809AE 145521 CLE - FLT 4248 - DURING CRUISE FLIGHT, A GUST LOCK FAIL WARNING. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS DIVERTED TO CLE. MAINTENANCE REMOVED AND REPLACED THE CONTROL YOKE POSITION SWITCH AND ADJUSTED IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2003031900089 20030319 00089 SO 2003 3 19 SIMA200235202 1 20021218 A 2121 4611028900 FAN EMB 135 EMB135KL 3260302 SO CABIN INOPERATIVE A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 811AE 145529 ORD - FLT 4135 - CREW REPORTED AN ELECTRICAL ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED THE FORWARD RECIRCULATIO N FAN IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2003031900090 20030319 00090 SO 2003 3 19 SIMA200235701 1 20021218 A 3397 CONNECTOR EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 729AE 145343 JFK - FLT 4836 - CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE FLIGHT ATTENDANT SEAT DOES NOT ILLUMINATE. MAINTENANCE FOUND THE CONNECTOR PLUG FOR THE LIGHT ASSEMBLY NOT CONNECTED. RESECURED CANNON PLUG AND COMPLIED WITH OPERATIONAL CHE CK. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2003031900091 20030319 00091 EA 2003 3 19 SIMA200235704 1 20021130 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 501BG 10017 DFW - FLT 9800 - EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTER Y PACKS (P/N 20131A S/N'S 74446, 68495, 72441, 80056) IAW CRJ MM. EMERGENCY LIGHTS THEN STAYED ON WHEN IN THE ARM POSIT ION. RELAY K-135 (P/N YA-D48) WAS REPLACED. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2003031900110 20030319 00110 NM 2003 3 19 UIEA200200068 1 20021218 A 5311 FRAME BOEING 747 7472D7B 1384803 NM BS 1265 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 68315 22472 DURING CURRENT C-CHECK AT IAI, FOUND CRACK IN FRAME WEB AT BS 1265 WL 199 L/S CRITICAL HOLE. CRACK LENGTH IS 1MM. DURI NG CRACK REMOVAL BY REAMING THE FRAME WEB AND INNER CHORD WERE MISDRILLED. FRAME WEB ONLEY OVERSIZED TO .419 INCH. PER FORMED OPEN HOLE INSPECTION OF REMOVED FASTENERS AND SURFACE E/C INSPECTED THE EDGE OF THE WEB. NO OTHER CRACKING FOUND . FABRICATED FREEZE PLUGS AND ANGLES. PRIME PAINTED ANGLES. INSTALLED FREEZE PLUGS IAW SRM 51-10-08. INSTALLED REINF ORCING ANGLES WET WITH SEALANT PER STANDARD SRM PRACTICES. REINSPECTION REQUIRED AT 2000 CYCLE INTERVALS WITH REPAIR LI MITED TO 4000 CYCLES. INSPECTION REQUIRES REMOVAL OF THE REINFORCING ANGLES AND FREEZE PLUGS. (M) 2 L 7 4 4F RT A20WE 2003031900111 20030319 00111 NM 2003 3 19 UIEA200200069 1 20021218 A 5753 65B020617 FITTING BOEING 747 7472D7B 1384803 NM NR 4 MID FLAP DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 DURING CURRENT C-CHECK AT IAI, FOUND NR 4 INBOARD MID FLAP CARRIAGE SUPPORT RIB FITTING WITH ELONGATED MOUNT HOLES. HOL ES OVERSIZED TO OBTAIN A CLEAN ROUND HOLE. PERFORMED OPEN HOLE E/C CHECK TO INSURE CRACK FREE CONDITION. NO CRACKS FOU ND. FABRICATED REPAIR SLEEVES. INSTALLED INTERFERENCES SLEEVES PER STANDARD SRM PRACTICES AS REQUIRED. PRIME PAINTED AREA. REINSTALLED REMOVED PARTS WITH OVERSIZED FASTENERS PER APPLICABLE INSTRUCTIONS. FITTING P/N 65B02061-7. (M) 2 L 7 4 4F RT A20WE 2003031900114 20030319 00114 EU 2003 3 19 USAA020465 1 20021127 A 5320 D5311260120000 MOUNT AIRBUS A319 A319112 3930323 EU LAV WALL CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 11023 1033 TPA - FOUND HARD POINT .25 INCH CORRODED AREA, FORWARD LAVATORY AFT WALL, INBOARD MOUNT. REPLACED HARD POINT MOUNTS AND BARREL NUT PER IPC 53-11-01 4G. (M) 2 L 7 2 4F RT A28NM 2003031900115 20030319 00115 EU 2003 3 19 USAA020466 1 20021121 A 5330 SKIN AIRBUS A319 A319112 3930323 EU FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 766US 1378 TPA - FOUND SKIN WITH 1 INCH HOLE, BELOW FORWARD CARGO DOOR CUTOUT, FRAME 26.5 AT STRINGER 4R. INSTALLED .063 INCH FILL ER WITH .090 INCH DOUBLER PER SRM 53-00-11 PAGE 241/242. (M) 2 L 7 2 4F RT A28NM 2003031900120 20030319 00120 NM 2003 3 19 USAABB02200 1 20021204 A 3350 BATTERY BOEING 757 757225 1384959 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 22199 SJU - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2003031900121 20030319 00121 NM 2003 3 19 USAABB02201 1 20021204 A 3350 BATTERY BOEING 757 7572B7 1384964 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 630AU 27808 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2003031900122 20030319 00122 NM 2003 3 19 USAABB02202 1 20021207 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AU 27807 MCO - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 6 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2003031900123 20030319 00123 NM 2003 3 19 USAABB02203 1 20021207 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM EMERGENCY LIGHTS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 633AU 27811 MIA - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2003032000001 20030320 00001 2003 3 20 USAABB02204 4 20021208 A 3454 285T05545 INDICATOR BOEING 757 7572B7 1384964 NM VOR/DME UNIT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 629AU 27807 PIT - FLT 1790 - AFTER TAKEOFF, CREW NOTED SMOKE AND ELECTRICAL BURNING ODOR FROM THE VOR/DME UNIT. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 VOR/DME CONTROL PANEL. (M) 2 L 7 2 4F RT A2NM 2003032000002 20030320 00002 NM 2003 3 20 USAABB02213 1 20021228 A 3240 BRAKE BOEING 757 7572B7 1384964 NM MLG MALFUNCTIONED A USAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 19 630AU 27808 LAS - FLT 607 - AFTER LANDING AT LAS FROM PIT, AIRCRAFT TAXIED TO THE GATE WITH NORMAL BRAKING UNTI A FEW FEET FROM PARK ING AT THE GATE. CREW REPORTED THERE WERE NO BRAKES UNTIL BRAKE PEDALS BOTTOMED AND GRABBED AT LAST SECOND. MAINTENANC E INSPECTED AND OPERATED BRAKES. ALL PRESSURES WERE NORMAL. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A2NM 2003032000003 20030320 00003 NM 2003 3 20 USAABB02215 1 20021231 A 3350 BATTERY BOEING 757 7572B7 1384964 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 MIA - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 4, 9, 18 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2003032000018 20030320 00018 EU 2003 3 20 USAASA02103 1 20021130 A 2120 ODOR AIRBUS A319 A319112 3930323 EU COCKPIT DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 757UW 1342 FLT 739 - EN ROUTE LGA-MSY, A SMOKE ODOR WAS PRESENT IN THE COCKPIT AND CABIN DURING DESCENT. NO VISIBLE SMOKE WAS NOTI CED AND NO SOURCE WAS IDENTIFIED. MAINTENANCE RESET THE CABIN ZONE CONTROLLER AND OPERATIONALLY CHECKED OK. AIRCRAFT W AS INSPECTED, BUT THE ODOR WAS NOT DUPLICATED IN EITHER THE COCKPIT OR CABIN. (M) 2 L 7 2 4F RT A28NM 2003032000019 20030320 00019 EU 2003 3 20 USAADUPE1 1 20021203 A 2121 BLOWER AIRBUS A319 A319112 3930323 EU FAILED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 762US 1358 FLT 147 - EN ROUTE CLT-PHX, AN ACRID ODOR WAS DETECTED IN THE COCKPIT, FOLLOWED BY AN ECAM MESSAGE OF VENT BLOWER INOPER ATIVE. FLIGHT LANDED IN PHX WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4F RT A28NM 2003032000020 20030320 00020 NE 2003 3 20 USAASA02115 2 20021222 A 7261 PUMP AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B4 NE GEARBOX SEPARATED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 707UW 0949 779457 PIT - FLT 141 - EN ROUTE PIT-SNA, AFTER DEPARTING PIT, CREW REPORTED THAT THE NR 2 ENGINE OIL QUANTITY WAS DECREASING AL ONG WITH OIL PRESSURE. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC PUMP MOUNTING STUDS PULLED FROM THE GEARBOX PAD, ALLOWING A ONE INCH GAP BETWEEN PUMP AND GEARBOX. THE ENGINE WAS REPLACED T O MAKE REPAIRS TO THE GEARBOX. (M) 2 L 7 2 4F 4 F RT A28NM E38NE 2003032000024 20030320 00024 NM 2003 3 20 USAASB02203 1 20021104 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM FWD CLOSET INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 592US 23937 IND - MAINTENANCE FOUND THE EMERGENCY LIGHT (ROUND BUTTON LIGHT) ON THE FORWARD CLOSET INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT (ROUND BUTTON LIGHT) ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003032000025 20030320 00025 2003 3 20 USAASB02213 4 20021128 A 3414 HG480B42 COMPUTER BOEING 737 7373B7 1384580 NM E/E COMPT MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 523AU 35066 23858 DTW - FLT 503 - ON TAKEOFF ROLL, THE AUTO THROTTLE DISCONNECTED AND WOULD NOT REENGAGE UNTIL AFTER TAKEOFF. THEN ON CLI MB OUT, AFTER GEAR RETRACTION, THE FIRST OFFICERS AIRSPEED INDICATION BECAME ERRONEOUS INDICATING APPROXIMATELY 60 KNOTS LESS THAN THE CAPTAINS INDICATOR AND THE STANDBY INDICTOR. THE STALL WARNING THEN ACTIVATED. CREW DECLARED AN EMERGEN CY AND RETURNED TO FIELD AT DTW. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT VERIFY PROBLEM. REMOVED AND REPLACED THE NR 2 DIGITAL AIR DATA COMPUTER AS PRECAUTIONARY. PERFORMED LEAK CHECK OF RIGHT PITOT SYSTEM PER MM 34 -11-00 WITH NO FAULTS NOTED. SYSTEM FUNCTIONAL CHECK OF NR 2 DIGITAL AIR DATA COMPUTER PERFORMED AND FOUND SATISFACTORY 2 L 7 2 4F RT A16WE 2003032000026 20030320 00026 NM 2003 3 20 USAASB02214 1 20021202 A 3397 WIRE BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 775AU 24933 IND - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT 5 ABC INOPERATIVE. MAINTENANCE FOUND THE SEAT TO AIRCRAFT WIRING DI SCONNECTED. RECONNECTED WIRING. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003032000027 20030320 00027 NM 2003 3 20 USAASB02232 1 20021225 A 7700 CONNECTOR BOEING 737 7374B7 1384702 NM INSTRUMENTS CHAFED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 775AU 24933 PIT - FLT 773 - EN ROUTE FROM PHL TO DFW, THE NR 1 ENGINE EGT INDICATOR FAILED. BOTH THE ANALOG AND DIGITAL PORTIONS WE RE INOPERATIVE. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED A CHAFED WIRE AT CONN ECTOR PLUG D1208, ENGINE DISCONNECT BRACKET. CHECKED ALL CONNECTOR PLUGS, WIRING AND CIRCUIT BREAKERS. PERFORMED THERM OCOUPLE RESISTANCE CHECK AND INDICATOR TEMPERATURE CHECK PER MM. ALL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003032000028 20030320 00028 NM 2003 3 20 USAASB02237 1 20021226 A 5230 10608211 SEAL BOEING 737 737301 1384611 NM FWD CARGO DOOR FAILED A USAA G A O2 MASK DEPLOYED UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 573US 23560 TYS - FLT 1724 - EN ROUTE FROM ATL-PIT, WHILE CLIMBING TO FL250, THE AIRCRAFT LOST PRESSURIZATION. THE AIRCRAFT DESCEND ED AND THE OXYGEN MASKS DEPLOYED. ALONG WITH THE PRESSURIZATION LOSS, THE PASSENGERS AND THE FIRST OFFICER NOTICED AN O DOR NOT PREVIOUSLY ON THE AIRCRAFT. FLIGHT DIVERTED TO TYS AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLA RED. MAINTENANCE EXAMINDED AIRCRAFT AND ENGINES. FOUND THE FORWARD CARGO DOOR SEAL HAD FAILED/BLOWN. REMOVED AND REPL ACED FORWARD CARGO DOOR SEAL AND CHECKED DOOR FOR FIT AND FLUSHNESS PER MM 52-31-00. PRESSURIZED AIRCRAFT. PRESSURIZAT ION CHECK AND LEAK CHECK GOOD. REPLACED ALL OXYGEN GENERATORS PER MM 35-11-004 AND CLEANED/RESTOWED OXYGEN MASKS IN PSU 2 L 7 2 4F RT A16WE 2003032000029 20030320 00029 NM 2003 3 20 USAASB02239 1 20021229 A 3260 189929 SENSOR BOEING 737 7373B7 1384580 NM RT MLG W/W OUT OF ADJUST A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 512AU 23595 CLT - FLT 649 - AFTER TAKEOFF FROM CLT, THE GEAR SELECTOR HANDLE WOULD NOT MOVE TO THE UP POSITION TO RETRACT THE LANDIN G GEAR. CREW ACCOMPLISHED CHECKLIST BUT DID NOT USE THE OVERRIDE TRIGGER. FLIGHT RETURNED TO FIELD AT CLT AND LANDED W ITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ADJUSTED THE S105 AND S106 AIR/GROUND SAFETY SENSORS P ER MM 32-09-01. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003032000030 20030320 00030 NM 2003 3 20 USAASB02240 1 20021229 A 2910 569670 MOTOR BOEING 737 7373B7 1384580 NM MLG W/W MALFUNCTIONED A USAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 EA 19 389US 49487 23311 CLT - FLT 948 - ON DESCENT INTO CLT, CREW REPORTED THE FLAPS WOULD NOT COME DOWN WHEN SELECTED. HYDRAULIC PRESSURE WAS AT 3,000 PSI AND HYDRAULIC FLUID QUANTITY WAS ABOVE RE-FILL. CAPTAIN DECLARED AN EMERGENCY AND FOLLOWED PROCEDURES FOR AN ALTERNATE FLAPS 15 DEGREES LANDING. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE NORMALLY. MX COULD NOT DU PLICATE PROBLEM ON THE GROUND. AS PRECAUTIONARY, MAINTENANCE REMOVED AND REPLACED THE HIGH TIME TRAILING EDGE FLAP DRIV E HYDRAULIC MOTOR PER MM 27-51-57. OPERATIONAL CHECK NORMAL. VISUAL CHECK OF FLAPS GOOD. (M) 2 L 7 2 4F RT A16WE 2003032000031 20030320 00031 NM 2003 3 20 USAASB02241 1 20021230 A 2150 A/C PACK BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE RIGHT CONTAMINATED A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 517AU 23703 725720 ALB - FLT 1544 - IMMEDIATELY AFTER TAKEOFF, CREW REPORTED A STRONG BURNING ODOR THROUGHOUT CABIN. AT APPROXIMATELY 5,00 0 FT, THE SMOKE ALARMS SOUNDED. CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO DIVERT TO ALB. FLIGHT LANDED WITHOUT INCI DENT AND TAXIED TO THE GATE. MX REMOVED AND REPLACED THE RIGHT ENGINE ASSEMBLY PER JOB CARD J371-00-01. RT ENGINE RECE NTLY EXPERIENCED AN IMPACT WITH SNOW BANK DURING TAXI ON 12/25/02. ALSO, FOUND THE RT PACK SYSTEM OIL SOAKED. REMOVED AND REPLACED RT PACK WATER SEPARATOR BAG, P/N V121-1. ACCOMPLISHED OIL CONTAMINATION REMOVAL FROM AIR CONDITIONING AND PNEUMATIC SYSTEM PER MM TASK 21-00-01-102-001. PERFORMED ENGINE RUN. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2003032000032 20030320 00032 NM 2003 3 20 USAASB02242 1 20021230 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 519AU 23705 ATL - MAINTENANCE REPORTED THE BULLNOSE EMERGENCY LIGHT ASSEMBLY, LOCATED ABOVE SEAT 7D, INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE M1135 CHARGER ASSEMBLY AND THE BATTERY PACK (P/N 2013-1A). OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003032000033 20030320 00033 EU 2003 3 20 USAASB02243 2 20021230 A 7200 ENGINE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RIGHT SURGES A USAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 19 531AU 24478 PIT - FLT 1789 - SHORTLY AFTER TAKEOFF FROM PIT, APPROXIMATELY 1,000 FT ABOVE GROUND LEVEL, CAPTAIN REPORTED A POWER SUR GE IN THE RT ENGINE. THE RT ENGINE SURGED PLUS/MINUS 5 PERCENT N1 ABOUT 3 TO 4 TIMES. CREW REDUCED POWER AND NO FURTH ER PROBLEMS WERE NOTED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED . MAINTENANCE ACCOMPLISHED ENGINE POWER RUN WITH PMC'S ON AND OFF PER MM 71-00-00-529, TEST NR 5. UNABLE TO DUPLICATE PROBLEM. ALL READINGS STEADY. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 2003032000034 20030320 00034 NM 2003 3 20 USAASB02245 1 20021230 A 2782 654476028 ROD END BOEING 737 7373B7 1384580 NM SLAT ACTUATOR FAILED A USAA O OTHER J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 EA 19 389US 23311 ORD - FLT 1472 - WHILE CONFIGURING FOR LANDING AT ORD, CAPTAIN REPORTED THE LEADING EDGE TRANSIT LIGHT ILLUMINATED AND R EMAINED ON DURING SECLECTION OF FLAPS 1, 5, 10, AND 15. CREW COMPLETED QUICK REFERENCE HANDBOOK PROCEDURES AND ACCOMPLIS HED A 15 DEGREE FLAPS LANDING. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE NR 3 LEADING EDGE SLAT ACTUATOR ROD END PER MM 27-81-44. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2003032100099 20030321 00099 NM 2003 3 21 2003UALA00242 1 20021017 A 5754 114W41307 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 3 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 NR 3 SLAT T/E WEDGE DELAMINATED MAJOR REPAIR ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2003032100100 20030321 00100 NM 2003 3 21 2003UALA00243 1 20021017 A 5754 114W41102 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 14 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 NR 14 SLAT T/E WEDGE DELAMINATED MAJOR REPAIR ACCOMPLISHED. CORE, WEDGE AND SKIN REBUILT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2003032400022 20030324 00022 EU 2003 3 24 27527601 1 20021216 A 5610 16430010 WINDSHIELD ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE731* 01518 WP COCKPIT FAILED B QRRR O OTHER O OTHER TX TAXI/GRND HDL 1 EA 13 275RA 2161 098 AIRCRAFT STATIC ON RAMP WITH APU RUNNING. WINDSHIELD OUTER PLY SHATTERED. WINDSHIELD REPLACED. 2 L 7 2 4F 4 F RT A16NM E6WE 2003032400063 20030324 00063 SW 2003 3 24 ALG2003F000A 1 20020815 A 5313 206064804033 STRINGER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE BROKEN B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 527AL 53211 STRINGERS BROKEN BY CENTER AND FORWARD HINGES. 1 G 7 1 3U 3 U O H2SW E1GL 2003032400064 20030324 00064 SW 2003 3 24 ALG2003F000B 1 20020815 A 5313 206064804034 STRINGER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE BROKEN B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 527AL 53211 STRINGER BROKEN BY CENTER AND FORWARD HINGES. 1 G 7 1 3U 3 U O H2SW E1GL 2003032400065 20030324 00065 SW 2003 3 24 ALG2003F000C 1 20020815 A 5314 206064804073 STRINGER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE CRACKED B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 527AL 53211 STRINGER CRACKED AND CORRODED BEYOND REPAIR. 1 G 7 1 3U 3 U O H2SW E1GL 2003032400066 20030324 00066 SW 2003 3 24 ALG2003F000D 1 20020815 A 5313 206064804074 STRINGER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE CRACKED B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 527AL 53211 STRINGER, CRACKED AND CORRODED BEYOND REPAIR. 1 G 7 1 3U 3 U O H2SW E1GL 2003032400067 20030324 00067 SW 2003 3 24 ALG2003F000E 1 20020815 A 5311 206064804075 FRAME BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE CORRODED B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 527AL 53211 FRAME, CORRODED AND CRACKED BEYOND REPAIR. 1 G 7 1 3U 3 U O H2SW E1GL 2003032400068 20030324 00068 SW 2003 3 24 ALG2003F000F 1 20020815 A 5311 206064804045 FRAME BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE CRACKED B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 527AL 53211 FRAME, CRACKED, CORRODED, NO REPAIRABLE. 1 G 7 1 3U 3 U O H2SW E1GL 2003032400069 20030324 00069 SW 2003 3 24 ALG2003F000G 1 20020815 A 5311 206064046 FRAME BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE CRACKED B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 527AL 53211 FRAME, CRACKED, CORRODED, NO REPAIRABLE. 1 G 7 1 3U 3 U O H2SW E1GL 2003032400070 20030324 00070 SW 2003 3 24 ALG2003F000H 1 20020815 A 5311 FRAME BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE CRACKED B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 527AL 53211 FRAME, CRACKED, CORRODED, NO REPAIRABLE. 1 G 7 1 3U 3 U O H2SW E1GL 2003032400071 20030324 00071 SW 2003 3 24 ALG2003F000I 1 20021111 A 5313 206064804033 STRINGER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE CRACKED B ALGR O OTHER O OTHER NR NOT REPORTED 1 SW 03 437AL 53141 11/11/02 IN FOR C/W ASB 407-02-54. WEIGHT OF CARBON FIBER DOORS. STRINGER, CRACK IS OCCURRING ON FORWARD LEFT STRINGER AT CLIP ANGLE AND STRINGER RIVETED LOCATION, WEIGHT OF DOORS AND VIBRATION. HEAVIER GAUGE STRINGER MATERIAL TO ACCOMMO DATE WEIGHT OF DOORS. 1 G 7 1 3U 3 U O H2SW E1GL 2003032600051 20030326 00051 2003 3 26 CA030127002 4 20020911 A 3424 C6610320101 INDICATOR CESSNA 441 441 2076020 CE TURN&BANK FAILED W O OTHER N FALSE WARNING NR NOT REPORTED 1 CA (CAN) AVIONICS DEPARTMENT FOUND ELECTRIC TURN & BANK 'HOT' WHILE RUNNING. THEY WERE WORKING UNDER INSTRUMENT PANEL. TURN & BANK FUNCTIONING NORMALLY. REPLACED UNIT BEFORE IMPENDING FAILURE. 1 L 7 2 3T RT A28CE 2003041600289 20030416 00289 EA 2003 4 16 SWIA200211717 1 20021212 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 FS 280 RBL 9.0 FLOORBEAM OUTBOARD, INBOARD AND AFT ANGLES FOUND CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED ANG LE IAW CRJ SRM 51-40-11, 51-42-13, 51-42-20, & 51-23-00. 2 L 7 2 4F RT A21EA 2003041600299 20030416 00299 SO 2003 4 16 SWIA200211690 1 20021214 A 2497 WIRE EMB 120 EMB120ER 3260203 SO WINDSHIELD HEAT BURNED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 562SW 120336 FOUND BURNED WIRE IN LEFT RELAY BOX ON CAPTAIN'S SIDE. WIRE IS FOR LEFT WINDSHIELD HEAT. FOUND DURING C-CHECK INSPECTI ON. REMOVED AND REPLACED WIRE AS NEEDED PE-88022-116. 2 L 7 2 4T RT A31SO 2003041600302 20030416 00302 WP 2003 4 16 UPS03840088 1 20021226 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, L2 UPPER AFT DOOR JAMB CORNER HAS A CRACK FOUND WITH NDT. CUT OUT CRACKED AREA IAW DC8 SRM 53-2- 0 FIG 18. VERIFIED CRACK REMOVAL IAW MD NDT SPM 06-10-01.001. FABIRCATED AND INSTALLED DOUBLER, TRIPLER AND SKIN FILLE R IAW DC8 SRM 53-2-0 FIG 18. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 2003041600303 20030416 00303 WP 2003 4 16 UPS03840080 1 20021227 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C-2, L2 LWR FWD DOOR JAMB CORNER EXTERNAL FUSELAGE SKIN CRACKED AT SECOND FASTENER HOLE BELOW TRIMOUT. ROUTED OUT CRACKED AREA IAW DC8 SRM 53-2-0. VERIFIED CRACK REMOVED IAW NDT SPM 06-10-01.001. FABBED -7 & -9 DOUBLERS AND -19 FILLER IAW DC 8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED -7 & -9 DOUBLERS & -19 FILLER IAW DC8 SRM 53-2-0. EDGE SEALED IAW DC8 SRM 51-1-11. INSTALLED DUCTS IAW DC8 MM 20-11-00. 2 L 7 4 4F RT 4A25 2003041600307 20030416 00307 WP 2003 4 16 UPS03840019 1 20021228 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C-2 CRACK INDICATION THROUGH PAINT AT RT AFT TYPE 2 EMERGENCY EXIT DOOR CUTOUT UPPER AFT CORNER STA 1340 L12R. REMOVED FASTENERS IN REPAIR AREA, CUTOUT CRACKED AREA OF OUTER SKIN AND FABRICATED -15 DOUBLER -17 DOUBLER AND - 19 FILLER IAW TINCO REO-G 08971. ALODINED AND PRIMED -15, -17, -19 IAW DC8 SRM 51-1-8. INSTALLED -15, -17, AND -19 IAW REO G08971. 2 L 7 4 4F RT 4A25 2003041600319 20030416 00319 WP 2003 4 16 UPS03840027 1 20021230 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM L-2 DOOR LOWER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 18. REMOVED EXISTI NG REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AROUND CUTOUT. FABRICATED AND INSTALLED DOUBLERS AND FILLER IAW SRM 53 -2-0 FIG 18. 2 L 7 4 4F RT 4A25 2003041600320 20030416 00320 WP 2003 4 16 UPS03840030 1 20021230 A 5754 SKIN DOUG DC8 DC871F 302199D WP LEFT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN REPAIR DOUBLER SCREW HOLES HAVE COUNTERSUNK TOO DEEP AT STA XFS 307, AND IS CRACKED. REMOVED DOUBLER, STOPDRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B. 2 L 7 4 4F RT 4A25 2003041600339 20030416 00339 SO 2003 4 16 SIMA200233804 1 20021102 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 ABI - A LEVEL 2 FINDING WAS FOUND DURING IMBV REFERENCE CRIC NR 28027, RIGHT AFT SILL CORRODED. REMOVED AND INSTALLED SE RVICEABLE SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02, 51-20-03, 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003041600347 20030416 00347 SO 2003 4 16 SIMA200233808 1 20021102 A 5320 14522459003 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 ABI - A LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 28018, CENTER RAMP SUPPORT CORRODED. REMO VED AND INSTALLED SERVICEABLE RAMP SUPPORT IAW EMB 145 SRM 51-20-03 AND 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003041600344 20030416 00344 SO 2003 4 16 SIMA200233807 1 20021102 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 ABI - A LEVEL 2 FINDING WAS FOUND DURING IMBV INSPECTION REFERENCE CRIC NR 28017 SERVICE DOOR CENTER SILL CORRODED. SER VICE DOOR CENTER SILL REPAIRED IAW EMB 145 ETN EM-53-036, GST-1927/02A, SRM 51-40-02, 51-20-03, 51-40-06. (M) 2 L 7 2 4T RT T00011AT 2003041600349 20030416 00349 SO 2003 4 16 SIMA200233809 1 20021102 A 5320 14522459003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 ABI - A LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 28022, PASSENGER DOOR AFT FLOOR SUPPORT CO RRODED. REMOVED AND INSTALLED PASSENGER DOOR AFT FLOOR SUPPORT IAW EMB 145 SRM 51-40-02, 51-20-03, 51-40-06. (M) 2 L 7 2 4T RT T00011AT 2003042100140 20030421 00140 SO 2003 4 21 SIMA200233820 1 20021110 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29959. AFT GALLEY DIAMOND GUSSET CORRO DED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003042100141 20030421 00141 SO 2003 4 21 SIMA200233825 1 20021110 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29956. SERVICE DOOR AFT SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02, 51-40-06 AND 51-20-03. (M) 2 L 7 2 4T RT T00011AT 2003042100142 20030421 00142 SO 2003 4 21 SIMA200233816 1 20021130 A 5610 163500110 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT FAILED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 636AE 145160 ORD - FLT 4145 - DURING FLIGHT, CREW REPORTED THE FIRST OFFICERS WINDSHIELD ARCED FOLLOWED BY WINDOW OUTER PANE SHATTERI NG. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2003042100143 20030421 00143 SO 2003 4 21 SIMA200233822 1 20021110 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29981. CARGO ENTRANCE LEFT BEAM GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-20-01, 51-20-03, 51-40-02, 51-40-02, 51-40-04, 51 -40-06. (M) 2 L 7 2 4T RT T00011AT 2003042100144 20030421 00144 SO 2003 4 21 SIMA20233823 1 20021110 A 5310 14529150001 CROSSBEAM EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29962. CROSSBEAM PROFILE CORRODED. RE MOVED AND INSTALLED SERVICEABLE CROSSBEAM AND PROFILE (P/N 14529150003) IAW EMB 145 SRM 51-40-02, 51-40-06, AND 51-20-03 . (M) 2 L 7 2 4T RT T00011AT 2003042100145 20030421 00145 SO 2003 4 21 SIMA200233819 1 20021110 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29958. FORWARD GALLEY DIAMOND GUSSET C ORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003042100146 20030421 00146 SO 2003 4 21 SIMA200233824 1 20021110 A 5347 14530659001 SEAT TRACK EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29953, LEFT OMEGA BEAM FORWARD SEAT TRA CK CORRODED. REMOVED AND REPLACED SEAT TRACK ON OMEGA BEAM IAW EMB 145 AMM 53-01-06. (M) 2 L 7 2 4T RT T00011AT 2003042100147 20030421 00147 SO 2003 4 21 SIMA200233826 1 20021110 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29956. SERVICE DOOR AFT SILL CORRODED. REMOVED AND INSTALLED SERVICABLE SILL IAW EMB 145 SRM 51-40-02, 51-40-06 AND 51-20-03. (M) 2 L 7 2 4T RT T00011AT 2003042100148 20030421 00148 SO 2003 4 21 SIMA200233827 1 20021110 A 5320 14522460013 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - THIS LEVEL 2 FINDING WAS FOND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29957. GALLEY CENTER GUSSET BEAM CORROD ED. REMOVED AND INSTALLED SERVICABLE BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003042100149 20030421 00149 SO 2003 4 21 SIMA200233821 1 20021110 A 5320 14521725001 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29961. LEFT GALLEY SIDE SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003042100150 20030421 00150 2003 4 21 USAABB02205 4 20021207 A 3417 4040800906 ADC BOEING 767 767201 1385125 NM E & E BAY FAULTY A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 649US 23901 LAX - FLT 48 - DURING CLIMB, CREW NOTED THE STICKSHAKER ACTIVATION DURING NORMAL FLIGHT ATTITUDE. THE FLIGHT WENT INTO A HOLDING PATTERN. AFTER CONFERRING WITH MAINTENANCE, THE C-11 CIRCUIT BREAKER WAS PULLED AND THE FLIGHT RESUMED. CREW THEN NOTED AN INCREASING DIFFERENCE BETWEEN THE CAPTAINS AND FIRST OFFICERS ALTIMETERS AS THE AIRCRAFT INCREASED ALTITU DE. FLIGHT RETURNED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT AIR DATA COMPUTER. (M) 2 L 7 2 4F RT A1NM 2003042100151 20030421 00151 NM 2003 4 21 USAABB02199 1 20021202 A 3350 1000679 LIGHT BOEING 767 767201 1385125 NM COCKPIT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649US 23901 PHL - FOUND COCKPIT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A1NM 2003042100152 20030421 00152 SO 2003 4 21 SIMA200233828 1 20021201 A 5313 14525768015 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 ABI - DURING AN MBV INSPECTION, THE RIGHT STRINGER 19 WAS FOUND TO BE CHAFED AT FRAME 52. BLENDED THE CHAFED AREA AND P ERFORMED NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM (EMB 1 45/1142 REV 20) CHAPTER 53-24-02. (M) 2 L 7 2 4T RT T00011AT 2003042100153 20030421 00153 2003 4 21 USAASB02215 4 20021121 A 2565 D31591477 SLIDE BOEING 737 737301 1384611 NM SERVICE DOOR BINDING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 23935 PHL - DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE HAD DIFFICULTY RELEASING FROM THE COMPARTMENT COVER. AFTER DEPLOYMENT, THE FORWARD UPPER CORNER WAS BOUND UP AGAINST THE DOOR. SLIDE WAS ROLLE D AFT AND WOULD NOT HAVE BEEN USEABLE FOR EXIT. SLIDE OPERATIONAL CHECK FAILED. MAINTENANCE REMOVED AND REPLACED THE F ORWARD RIGHT SERVICE DOOR ESCAPE SLIDE ASSEMBLY. TWO ADDITIONAL OPERATIONAL CHECKS ARE SCHEDULED TO BE PERFORMED AT THE FORWARD RIGHT SERVICE DOOR POSITION PER USAIRWAYS POLICY AND PROCEDURES. (M) 2 L 7 2 4F RT A16WE 2003042100154 20030421 00154 SO 2003 4 21 SIMA200233815 1 20021125 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO CARGO DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED DAMAGED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB SRM (SRM EMB 145/1142 REV 20) CHAPTERS 51-40-02, 51-20-03, 51-20-01, 51-40-04, 51-40-06 AND EMB 145 CPM 51-21-04, 51-21-05. (M) 2 L 7 2 4T RT T00011AT 2003042100155 20030421 00155 SO 2003 4 21 SIMA200233818 1 20021110 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - THIS LEVEL 2 FINDING WAS DURING AN IMBV INSPECTION REFERENCE, CRIC NR 29955. SERVICE DOOR CENTER SILL CORRODED. INSTALLED DOUBLERS ON SERVICE DOOR CENTER SILL IAW EMB 145 ETN EM-53-026, STEP 1-7 AND SRM 51-40-02, 51-20-03, 51-40-06. (M) 2 L 7 2 4T RT T00011AT 2003042100156 20030421 00156 SO 2003 4 21 SIMA200233817 1 20021110 A 5320 14522459003 SUPPORT EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29964. RAMP SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003042100157 20030421 00157 SO 2003 4 21 SIMA200233833 1 20021126 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN MBV INSPECTION REFERENCE CRIC NR 27872 SERVICE DOOR AFT SILL CORRODED. I NSTALLED NEW AFT SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003042100158 20030421 00158 SO 2003 4 21 SIMA200233832 1 20021126 A 5320 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 ABI - THIS LEVEL 2 FINDING FOUND DURING MBV INSPECTION REFERENCE CRIC NR 27871, AFT DIAMOND GUSSET CORRODED. REMOVED CO RRODED GUSSET AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003042100159 20030421 00159 SO 2003 4 21 SIMA200233829 1 20021201 A 5313 14525768015 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 ABI - DURING AN MBV INSPECTION LEFT STRINGER 19 WAS FOUND TO BE CHAFED AT FRAME 52. BLENDED THE CHAFED AREA AND PERFORM ED NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM (EMB SRM 145/114 2 REV 20) CHAPTER 53-24-02. (M) 2 L 7 2 4T RT T00011AT 2003042100160 20030421 00160 SO 2003 4 21 SIMA200233831 1 20021126 A 5320 14522459011 GUSSET EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 ABI - THIS LEVEL 2 FINDING FOUND DURING MBV INSPECTION REFERENCE CRIC NR 27870. FORWARD DIAMOND GUSSET CORRODED. REMOV ED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003042100161 20030421 00161 SO 2003 4 21 SIMA200233834 1 20021126 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 ABI - THIS LEVEL 2 FINDING FOUND DURING MBV INSPECTION REFERENCE CRIC NR 27873. SERVICE DOOR FORWARD SILL CORRODED. RE MOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003042100162 20030421 00162 SO 2003 4 21 SIMA200233830 1 20021129 A 5315 14529150011 FLOORBEAM EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 ABI - DURING AN MBV INSPECTION, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. PERFORMED A CUT OUT OF THE DAMAGED SECTION OF THE LEFT FLOORBEAM. FABRICATED AN EXTERNAL ANGLE, FILLER AND SHIMS. REPAIR DONE IAW EMB 145 SRM (S RM 145/1142 REV 20) CHAPTER 53-21-10 FIGURE 201 SHEET 1. (M) 2 L 7 2 4T RT T00011AT 2003042100163 20030421 00163 SO 2003 4 21 SIMA200233835 1 20021126 A 5320 14529603003 GUSSET EMB 145 EMB145LR 3260212 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 ABI - THIS LEVEL 2 FINDING FOUND DURING MBV INSPECTION REFERENCE CRIC NR 27875, CENTER BEAM GUSSET CORRODED. REMOVED AN D INSTALLED SERVICEABLE CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M) 2 L 7 2 4T RT T00011AT 2003042100074 20030421 00074 CE 2003 4 21 OIZ2003F00000 1 20021215 A 7797 SOCKET BEECH 1900 1900C 1154161 CE INDICATOR FUSE DAMAGED A OIZA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 WP 19 381CR UB69 ON 12/15/02 DURING TAKEOFF ROLL OUT OF VGT, BOTH TORQUE GAUGES BEGAN SPINNING. CREW ABORTED TAKEOFF, TAXIED BACK TO RAM P. AID OF CREW, MAINT HAD ENG RUN UP TO POWER AND NOTED: ALL INDICATIONS WERE NORMAL. A/C WAS GROUNDED AND TROUBLESHO OTING OF TORQUE INDICATING SYS LEAD TO FINDING BROKEN FUSE HOLDER FOR POWER SUPPLY, WIRE FOR BOTH TORQUE INDICATORS. F USE HOLDER HAD SNAPPED AT LOCKING TABS AND WAS NO LONGER COMPRESSING FUSE WITHIN THE FUSE HOLDER. FUSE HOLDER WAS TIE-W RAPPED TO A WIRE HARNESS IN A VERTICAL POSITION, THIS ALLOWED CAP OF FUSE HOLDER TO REST ON FUSE AND MAKE CONTACT UNTIL VIBRATIONS DURING TAKEOFF CAUSED CAP TO VIBRATE AND LOOSE CONTACT. THE FUSE HOLDER WAS REPLACED NO FURTHER PROBLEMS. 2 L 7 2 4T RT A24CE 2003042300096 20030423 00096 CE 2003 4 23 RK71 1 20021214 A 3231 12838002139 CABLE BEECH MU300 400A 1155402 CE MLG DOOR OUT OF ADJUST E ERYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 402GS RK71 INBOARD GEAR DOORS DID NOT CLOSE AFTER LANDING GEAR RETRACTION. RETURNED TO AIRPORT EXECUTING UNEVENTFUL LANDING. MAIN TENANCE FOUND RT EMERGENCY GEAR CABLE NOT ALLOWING HOOK TO CONTACT UPLOCK SWITCH. ADJUSTED CABLE IAW BEECH M/M. OP CHE CK GEAR WITH NO FURTHER DISCREPANCIES NOTED. 2 H 7 2 4F RT A16SW 2004022500130 20040225 00130 EU 2004 2 25 AAL2004F00002 1 20020712 A 5754 RIB AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680 30025 NE KRUEGER FLAP CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14061 471 KRUEGER FLAP JACK RIB HORIZONTAL SUPPORT FITTING CORRODED ON AFT SIDE BETWEEN ACT ATTACH POINTS. REMOVED CORROSION, TRE ATED IAW ESO 30595. 2 L 7 2 4F 4 F RT A35EU E13NE 2004030100058 20040301 00058 EA 2004 3 1 AJC2004F00001 1 20021211 A 3260 840534 SQUAT SWITCH CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE NLG DEFECTIVE A AJCA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 25 224F 5163 AIRCRAFT DEPARTED, ENROUTE, AFTER TAKE OFF THE NOSE GEAR FAILED TO RETRACT AND WEIGHT ON WHEELS (WOW). INPUT FAIL LIGHT ILLUMINATED. THE CREW CONSULTED THE ABNORMAL PROCEDURES MANUAL AND RECYCLED THE GEAR. ALL OF THE GEAR RETRACTED NORMA LLY BUT THE WOW LIGHT WAS STILL ILLUMINATED. THE CREW ELECTED TO DIVERT, FOR REPAIRS AT MFG. DURING APPROACH THE GEAR EXTENSION WAS NORMAL WITH 3 GREEN DOWN AND LOCKED LIGHTS AND THE LANDING WAS UNEVENTFUL. THE CREW DID NOT DECLARE AN EM ERGENCY. THE WOW INPUT FAILED LIGHT STAYED ON RIGHT THRU TAXI AND SHUT DOWN. IT WAS DETERMINED THAT THE NR 1, NR 2 NOS E LANDING GEAR WOW PROXIMITY SWITCHES WERE DEFECTIVE. REMOVED AND REPLACED BOTH SWITCHES. AC WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2003032700192 20030327 00192 CE 2003 3 27 CA030211005 1 20020615 A 5320 50420014229 CHANNEL BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) CRACKS AT ALL THREE STATIONS ON OUTBOARD RADIUS. LT AND RT CHANNELS HAVE IDENTICAL DEFECTS. 1 L 7 2 3T 4 T A14CE E4EA 2003032600054 20030326 00054 2003 3 26 CA030131003 4 20021030 A 3416 AR850 ENCODER CESSNA 172 172M 2072418 CE LYC O320 O320E2D 41508 EA MCAULY 1C160 1C160DTM GL E/E BAY FAILED W O OTHER H ELECT. POWER LOSS-50 PC DE DESCENT 1 CA (CAN) ATC REPORTED ENCODER READ OUT AT 7,500 FEET, ACTUAL ALTITUDE 3,500 FEET.ENCODER ASSEMBLY REPLACED, NO FURTHER DEFE CT. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 2003032700045 20030327 00045 EU 2003 3 27 BMAC020025 1 20021203 A 5310 DOUBLER BAG JETSTM JETSTM3101 1500215 EU FUSELAGE CRACKED A B16A K NONE O OTHER IN INSP/MAINT 1 NE 05 530PA 732 FOUND 5.5 INCH LONG CRACK IN PREVIOUS REPAIR DOUBLER AT MAIN CABIN DOOR FORWARD HINGE POINT ADJACENT TO THE TOP OF THE H INGE. FABRICATED AND INSTALLED NEW REPAIR IAW BAE J31 SRM CHAPTER 52-10-11, PAGES 24, 26A, AND 26B REPAIR 1379837R, REF FIGURE 7A. NO CHANGE TO WEIGHT AND BALANCE. (M) 2 L 7 2 4T RT A21EU 2003032700046 20030327 00046 EU 2003 3 27 BMAC020026 1 20021204 A 3213 STRUT BAG JETSTM JETSTM3101 1500215 EU MLG DISCHARGED A B16A B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 NE 05 530PA 732 PILOT REPORTED 'CABIN' CAP LIGHT ILLUMINATED DUIRNG FLIGHT AT 11,300 FEET. PERFORMED EMERGENCY CHECKLIST ACTIONS, DESCE NDED TO 9,000 FEET. CABIN CAP LIGHT OUT CABIN DOES NOT PRESSURIZE. MAINTENANCE DEFERRED PER MEL 21-14. LATER TROUBLE- SHOOTING DETERMINED NLG WEIGHT ON WHEEL SWITCH CLOSED DUE OT LOW NITROGEN PRESSURE IN STRUT. AFTER SERVICING, A FUNCTIO NAL CHECK FLIGHT WAS PERFORMED WITH NO DISCREPANCIES NOTED. (M) 2 L 7 2 4T RT A21EU 2003032700049 20030327 00049 GL 2003 3 27 BZP2003F00000 1 20020303 A 4997 GL51233019 CONTACTOR BOMBDR BD700 BD7001A10 1390006 GL APU STARTER WRONG PART A BZPR O OTHER W INADEQUATE Q C NR NOT REPORTED 1 NM 09 949GP 9049 ON 33/02, INSTALLED A FACTORY REPAIRED APU START CONTACTOR ASSEMBLY (PN GL51233019). UNIT ARRIVED WITH DETAILED TEST RE SULTS AND 8130. UNIT WAS REPLACED DUE TO LOGO LIGHTS CAUSING CIRCUIT BREAKER TO TRIP. AFTER 1.5 WEEKS, WE NEEDED TO A DD FUEL TO THE AFT TANK. THE REFUEL/DEFUEL VALVE FOR THAT TANK WOULD NOT OPEN. AFTER A GREAT DEAL OF TROUBLESHOOTING, IT WAS DETERMINED THAT PIN D OF CONNECTOR P1 HAD A PIN INSTALLED THAT WAS TOO SMALL AND WOULD NOT LOCK. AFTER DOING FUR THER CHECKING, IT WAS DETERMINED THAT THIS ASCA CAME INTO THE MANUFACTURER (SUNSTRAND) WITH THE SAME REFUEL/DEFUEL VALVE DISCREPANCY. IMPROPER PIN WAS REMOVED AND ALL IS WORKING NORMAL. 2 L 7 2 4F RT T00003NY 2003032700098 20030327 00098 SO 2003 3 27 C2XA03CL004 1 20021231 A 2750 3631101007 LEVER EMB 145 EMB145LR 3260212 SO TE FLAPS FAULTY A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 15986 145254 CLE FLIGHT 3081 THE CREW REPORTED A LANDING GEAR AURAL WARNING INDICATION WHEN THE GEAR HANDLE WAS MOVED TO THE UP POSIT ION. MAINTENANCE REPLACED THE FLAP LEVER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2003072800140 20030728 00140 WP 2003 7 28 AAL2003F00013 1 20021029 A 5320 WEB DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 487AA 49680 SUB FLOOR DIAPHRAGM, CUSP LINE WEB IS CORRODED BELOW G1 GALLEY LINE CONNECTION PAN BETWEEN INBOARD AND AFT DRAIN/SUPPLY LINES BETWEEN STA 148-160. 2 INCH X 2 INCH AREA, .025 INCH DEPTH. REMOVED CORROSION, INSTALLED DOUBLER IAW SRM. 2 L 7 2 4F 4 F A6WE E2EA 2003072800144 20030728 00144 WP 2003 7 28 AAL2003F00008 1 20021009 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 241AA 49254 FUSELAGE SKIN CRACKED AT FASTENER, STA 1380 ABOVE LONGERON 14 LT. BOTH .250 INCH IN LENGTH, AFT LEFT FUSELAGE, STA 1380 . REPAIRED DAMAGE IAW AARD AND SRM. REQUIRED SMALL CUTOUT, REPAIR IN UNPRESSURIZED AREA. 2 L 7 2 4F 4 F A6WE E2EA 2003072800145 20030728 00145 WP 2003 7 28 AAL2003F00010 1 20020925 A 5244 LATCH DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE ACCESSORY DOOR DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AA 49474 FORWARD ACCY DOOR, FORWARD LT LATCH OVERLAPS A HUCKBOLT AND STIFFENER. OUT OF LIMITS, FUSELAGE. REPAIRED LATCH IAW ESO 81291 DATED 8/26/02. 2 L 7 2 4F 4 F A6WE E2EA 2003072800147 20030728 00147 WP 2003 7 28 AAL2003F00005 1 20021007 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 241AA 49254 WINDOW FRAME CRACKED LOWER FORWARD CORNER, STA 984 LEFT SIDE E58 NR4426956. CRACK LENGTH .5000 INCH AT CABIN/FUSELAGE. INSTALLED DOUBLER FOR WINDOW FRAME REPAIR ON LOWER FORWARD CORNER STA. 984 LT SIDE IAW AARD. 2 L 7 2 4F 4 F A6WE E2EA 2003072800146 20030728 00146 WP 2003 7 28 AAL2003F00003 1 20021015 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 241AA 49254 PLATE/SKIN, FUSELAGE SKIN CRACKED AT FASTENER, ST 1380, L14R. CRACK LENGTH .3125 INCH. ROUTED OUT CRACK TO .3125 DIAME TER, INSTALLED EXTERNAL DOUBLER IAW SRM 53-01, FIG 4, SH3. 2 L 7 2 4F 4 F A6WE E2EA 2003073000008 20030730 00008 WP 2003 7 30 ABXA030206 1 20021102 A 5313 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 AFT LOWER CARGO LONGERON 34 RIGHT HAD CORROSION AT STA 1180 - 1200. REMOVED CORROSION, BEYOND LIMITS. REMOVED FASTENER S IAW DC-8 SRM 51-1-20D. FABRICATED REPAIR STRAP IAW REA D853-44041MR. PRIMED STRAP IAW DC-8 SRM 51-1-8. INSTALLED ST RAP IAW DC-8 SRM 51-1-20D AND REA D853-44041MR. 2 L 7 4 4F 4A25 2003073000009 20030730 00009 WP 2003 7 30 ABXA030205 1 20021030 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 L1 DOOR SHOWED CRACK LOWER AFT CORNER. REMOVED DAMAGE IAW DC-8 SRM 53-2-0. FABRICATED DOUBLER, TRIPLER, AND FILLER IAW DC-8 SRM 53-2-0. INSTALLED DOUBLER, TRIPLER AND FILLER IAW DC-8 SRM 51-1-20D, AND REA D853-44030MR. 2 L 7 4 4F 4A25 2003073000010 20030730 00010 WP 2003 7 30 ABXA030207 1 20021105 A 5730 SKIN DOUG DC8 DC863F 302198F WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT FORWARD WHEEL WELL HAD CORROSION ON CENTER WING SKIN AFT OF OUTBOARD BLOWOUT PANEL. REMOVED CORROSION, FOUND TO B E OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER, REPAIR ANGLE AND SPLICE IAW DC-8 SRM 51-1-8 AND R EA D857-44039MR. 2 L 7 4 4F 4A25 2003073000018 20030730 00018 WP 2003 7 30 ABXA030221 1 20020812 A 5311 FRAME DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FORWARD LOWER CARGO STA 280, LONGERON 36, UPPER FRAME FLANGE WAS CRACKED AND CORRODED. CUT OUT DAMAGED SECTION OF FRAME . FABRICATED FILLER, DOUBLER, ALODINED, PRIMED, AND INSTALLED FASTENERS IAW REA D853-43982MR, DC-8 SRM 51-1-8, 51-1-20D , AND 51-1-20E. 2 L 7 4 4F 4A25 2003073000019 20030730 00019 WP 2003 7 30 ABXA030230 1 20020720 A 5313 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 35 RIGHT INBOARD CHANNEL WAS CORRODED AT STA 340. CUT AND REMOVED DAMAGED SECTION, FABRICATED NEW SECTION AND REPAIR SPLICES. INSTALLED IAW DC-8 SRM 53-2-2 AND 51-1-20D. 2 L 7 4 4F 4A25 2003073000020 20030730 00020 WP 2003 7 30 ABXA030231 1 20020722 A 5320 PAN DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FORWARD PASSENGER DOOR LOWER AFT CORNER AT THE CUSP CHORD SHOWED CRACK INDICATION. STOP DRILLED CRACKED DOOR PAN, FABRI CATED REPAIR AND SPLICE PARTS AND PLATES FOR DOOR PAN AND TORQUE BOX WEB IAW DAC 5597646, DC-8 SRM 53-2-0, 51-9-0, 51-1- 21, 53-3-1, AND 51-1-8. 2 L 7 4 4F 4A25 2003073000021 20030730 00021 WP 2003 7 30 ABXA030223 1 20020722 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 SEAT TRACK AT BUTT LINE 25 LEFT WAS CORRODED, FS 70 - 260. REMOVED WEB AND FLOORBOARDS FS 70 - 260, LEFT BUTT LINE 0 - 45 TO FOM. REMOVED SEAT TRACK SECTION. FABRICATED SECTION IAW ZANTOP DWG 86302. ALODINED AND PRIMED IAW DC-8 SRM 51-1 -8. INSTALLED SEAT TRACK SECTION IAW ZANTOP DWG 86302. REINSTALLED WEB AND FLOORBOARDS IAW DC-8 SRM 51-3-0. 2 L 7 4 4F 4A25 2003073000022 20030730 00022 WP 2003 7 30 ABXA030217 1 20020810 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 AFT PASSENGER DOOR UPPER AFT CORNER OUTER SKIN HAD 2 CRACKS. REMOVED DAMAGED, NO CRACKS NOTED AFT OF CUTOUTS. FABRICAT ED DOUBLER AND FILLERS, INSTALLED IAW DC-8 SRM 53-2-0, NDT SPM 06-10-001, DC-8 SRM 51-1-8, 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F 4A25 2003072800142 20030728 00142 NM 2003 7 28 AAL2003F00011 1 20021104 A 3350 CM767 LIGHT BOEING 757 757223 1384957 NM RROYCE RB211 RB211* 54555 NE CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 669AA 25334 LAMP, BURNED OUT. RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM A12EU 2003073000074 20030730 00074 WP 2003 7 30 ABXA030238 1 20020826 A 5210 DOOR FRAME DOUG DC8 DC863 302198A WP PAX DOOR GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 MAIN CABIN L1 DOOR, INSIDE AFT CENTER FRAME AT EDGE, HAD A DEEP GOUGE WEAR AT POINT WHERE BAYONET CONTACTS LATCH. REPAI RED AREA IAW REA D852-44006MR. 2 L 7 4 4F 4A25 2003073000075 20030730 00075 WP 2003 7 30 ABXA030239 1 20020830 A 5230 DOOR FRAME DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 MAIN CARGO DOOR, LATCH NR 3, HAD 5 HOLES CRACKED AT ATTACHING HOLES. REPAIRED AREA IAW REA D852-36710MR. REMOVED AND R EPLACED FRAME SECTIONS IAW ABX REA D852-36710MR. 2 L 7 4 4F 4A25 2003073000079 20030730 00079 WP 2003 7 30 ABXA030237 1 20020826 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 AFT LOWER CARGO, STA 990, LONGERON 36, SKIN WAS CORRODED. REPAIRED AREA IAW REA D853-44014MR AND DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 2003073000080 20030730 00080 WP 2003 7 30 ABXA030248 1 20020905 A 5755 SKIN DOUG DC8 DC863 302198A WP LT SPOILER BENT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 NR 2 LEFT SPOILER INBOARD HINGE SKIN WAS BENT. REPAIRED DAMAGED AREA, FABRICATED REPAIR FILLER AND DOUBLER, INSTALLED I AW ABX REA D827-44011MR AND SRM CHAPTER 51. 2 L 7 4 4F 4A25 2003073000081 20030730 00081 WP 2003 7 30 ABXA030241 1 20020830 A 5230 DOOR FRAME DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 MAIN CARGO DOOR, LATCH NR 5, ATTACHING HOLES HAD 3 CRACKED HOLES. REMOVED AND REPLACED FRAME SECTION IAW ABX REA D852-3 6710MR. 2 L 7 4 4F 4A25 2003073000082 20030730 00082 WP 2003 7 30 ABXA030242 1 20020830 A 5230 DOOR FRAME DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 MAIN CARGO DOOR, LATCH NR 6, ATTACH HOLES HAD 5 CRACKS IN HOLES. REMOVED AND REPLACED FRAME SECTION IAW ABX REA D852-36 710MR. 2 L 7 4 4F 4A25 2003073000083 20030730 00083 WP 2003 7 30 ABXA030243 1 20020830 A 5230 DOOR FRAME DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 MAIN CARGO DOOR, LATCH NR 7, ATTACHING HOLES HAD 6 CRACKS IN HOLES. REMOVED AND REPLACED FRAME SECTION IAW ABX REA D852 -36710MR. 2 L 7 4 4F 4A25 2003072800141 20030728 00141 WP 2003 7 28 AAL2003F00009 1 20021029 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 241AA 49254 AIRCRAFT HAS SRM CONDITION II DAMAGE AT STA 237 FROM LONGERON 17L TO 18L. AREA 16 INCH X 14.5 INCH HIGH, DEPTH .050 INC H. REPAIR APPROX 18 INCH X 18 INCH. PERMANENT REPAIR ACCOMPLISHED, 10-29-02. PAPERWORK SIGNED OFF TO SRM. 2 L 7 2 4F 4 F A6WE E2EA 2003073000004 20030730 00004 WP 2003 7 30 ABXA030203 1 20021107 A 5230 FITTING DOUG DC8 DC863F 302198F WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 MAIN CARGO DOOR ACTUATOR ATTACH FITTING WAS SEPARATED AT WELD. REMOVED CORROSION FROM FITTING AND BLENDED FITTING IAW D C-8 SRM 51-1-8, WELDED FITTING IAW AM526856, INSTALLED FITTING IAW DC-8 SRM 51-3-0 AND 51-1-21. REINSTALLED ACTUATOR IA W DC-8 MM 52-36-03. OPS CHECKED GOOD IAW DC-8 MM 52-36-03. 2 L 7 4 4F 4A25 2003073000007 20030730 00007 WP 2003 7 30 ABXA030204 1 20021107 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 L2 DOOR CUTOUT LOWER FORWARD CORNER HAD REPAIR. UNIT DOES NOT CONFORM TO SRM OR JOB CARD NEA 53100104-002/634. REPAIRED L2 LOWER FORWARD CORNER IAW REA D853-44023MR AND DC-8 SRM 53-2-0. 2 L 7 4 4F 4A25 2003073000076 20030730 00076 WP 2003 7 30 ABXA030240 1 20020829 A 5230 DOOR FRAME DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 MAIN CARGO DOOR, LATCH NR 4, ATTACHING HOLES HAD 5 CRACKED HOLES. REMOVED AND REPLACED FRAME SECTION IAW ABX REA D852-3 6710MR. 2 L 7 4 4F 4A25 2003073000017 20030730 00017 WP 2003 7 30 ABXA030220 1 20020807 A 5310 DOOR FRAME DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 L1 DOOR JAMB LOWER AFT CORNER HAD STAINLESS STEEL REPAIR. REMOVED DOOR CLOSE OUT PANEL TO FOM. FABRICATED 3 DOUBLER, 5 DOUBLER AND FILLERS, INSTALLED ALL IAW DC-8 SRM 53-2-0, 51-1-21 AND 51-3-0. 2 L 7 4 4F 4A25 2003073000078 20030730 00078 WP 2003 7 30 ABXA030236 1 20020825 A 5330 SKIN DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 AFT LOWER CARGO, STA 1000, LONGERON 36 SKIN CORRODED. REPAIRED AREA IAW REA D853-44013MR, AND DC-8 SRM 51-1-8, 51-3-0, AND 51-1-20D. 2 L 7 4 4F 4A25 2003080100090 20030801 00090 WP 2003 8 1 AAL2003F00014 1 20021018 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A AALA K NONE O OTHER UK UNKNOWN 1 SW 21 241AA 49254 NR 6 SEAT TRACK IS CORRODED BEYOND LIMITS. INSTALLED SEAT TRACK FROM STA 210 TO 798 IAW SRM 53-05-00, FIG 98. 2 L 7 2 4F 4 F A6WE E2EA 2003080100091 20030801 00091 WP 2003 8 1 AAL2003F00016 1 20020917 A 5510 PLATE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE HORIZ STAB CORRODED A AALA K NONE O OTHER UK UNKNOWN 1 SW 21 596AA 53286 LEFT INBOARD HORIZONTAL STABILIZER PIVOT BEARING LUG PLATES ARE CORRODED. 1.5 INCH X 1.5 INCH AREA, BEYOND LIMITS. REP LACED LEFT INBOARD HORIZONTAL STABILIZER LUG PLATES AND MACHINED PIVOT BORE IAW FCO 0488A, 9, D AND E. 2 L 7 2 4F 4 F RT A6WE E2EA 2003080100094 20030801 00094 WP 2003 8 1 AAL2003F00006 1 20021009 A 5313 LONGERON DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A AALA K NONE O OTHER UK UNKNOWN 1 SW 21 241AA 49254 CRACK IN LOWER LONGERON FLANGE AT FASTENER AT FRAME, STA 313 LONGERON 17 RT. SPLICED LONGERON IAW SRM 53-02, STA 313 LO NGERON 17 RT. 2 L 7 2 4F 4 F A6WE E2EA 2003073000077 20030730 00077 WP 2003 7 30 ABXA030235 1 20020824 A 5320 STRUCTURE DOUG DC8 DC863 302198A WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 L2 LOWER DOOR CORNER, REPAIRS DO NOT CONFORM TO CURRENT SRM, OR ABX JOB CARD NEA 53100104-002. REPAIRED AREA IAW REA D8 53-44010MR. 2 L 7 4 4F 4A25 2003080500119 20030805 00119 SW 2003 8 5 LS1R088285 1 20020526 A 7711 206075682001 INDICATOR BELL 206 206B3 1181506 SW ALLSN 250C 250C20 03013 GL GAS PRODUCER FAILED E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 49718 1917 GAS PRODUCER INDICATOR HAS AN INTERNAL FAILURE. 1 G 7 1 3U 3 U H2SW E4CE 2003080500120 20030805 00120 WP 2003 8 5 LS1R088291 1 20020120 A 2822 164A1343 PUMP HUGHES 369 369D 4470706 WP ALLSN 250C 250C20 03013 GL FUEL BOOST INOPERATIVE E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 500DC 290456D BOOST PUMP IS INOPERATIVE. 1 G 7 1 3U 3 U H3WE E4CE 2003080500121 20030805 00121 WP 2003 8 5 LS1R088297 1 20020208 A 2822 369A81433 PUMP HUGHES 369 369E 4470707 WP ALLSN 250C 250C20 03013 GL FUEL SYSTEM INOPERATIVE E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 8330P 31 0330E FUEL PUMP FAILED CHECK/ INOPERATIVE. 1 G 7 1 3U 3 U H3WE E4CE 2003080600002 20030806 00002 WP 2003 8 6 LS1R088305 1 20020909 A 7714 369A45165 INDICATOR HUGHES 369 369E 4470707 WP ALLSN 250C 250C20 03013 GL N1 STICKING E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 8330P 0330E INDICATOR STICKING. (N1 TACH) 1 G 7 1 3U 3 U H3WE E4CE 2003080600022 20030806 00022 2003 8 6 LS1R088299 4 20020223 A 3420 PAI700 COMPASS HUGHES 369 369D 4470706 WP COCKPIT DEFECTIVE E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 1097J 900801D VERTICAL COMPASS IS DEFECTIVE. 1 G 7 1 3U H3WE 2003080600024 20030806 00024 GL 2003 8 6 LS1R088288 2 20020423 A 7313 6890917 NOZZLE BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL ENGINE FAILED E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 9907K 2040 NOZZLE FLAMES OUT AT 20 PERCENT N1. 1 G 7 1 3U 3 U H2SW E4CE 2003080600026 20030806 00026 GL 2003 8 6 LS1R088303 2 20020717 A 7510 206062625003 ACTUATOR BELL 206 206B3 1181506 SW ALLSN 250C 250C* GL ANTI ICE SYSTEM BROKEN E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 90322 1736 ACTUATOR BROKEN AND ACTUATES WARNING HORN. 1 G 7 1 3U 3 U H2SW E4CE 2003080600027 20030806 00027 GL 2003 8 6 LS1R088282 2 20020426 A 7314 369A81433 PUMP HUGHES 369 369E 4470707 WP ALLSN 250C 250C20B 03013 GL FUEL SYSTEM INOPERATIVE E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 8330P 240 0330E FUEL PUMP INOPERATIVE. 1 G 7 1 3U 3 U H3WE E4CE 2003080600032 20030806 00032 SW 2003 8 6 LS1R088279 1 20020518 A 2430 206075447007 VOLT REGULATOR BELL 206 OH58A 1181579 SW GENERATOR MALFUNCTIONED E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 54AG 20 7120721 GENERATOR WILL COME ON. REPLACED VOLT REGULATOR 1 G 7 1 3U H2SW 2003080100087 20030801 00087 WP 2003 8 1 AAL2003F00000 1 20021017 A 5320 PAN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A AALA K NONE O OTHER UK UNKNOWN 1 SW 21 241AA 49254 CORROSION ON BOTTOM FORWARD CARGO DOOR PAN STA 370, STA 427. SIZE OF DISCREPANCY: AREA 6 INCH X 57 INCHES, DEPTH 0 TO . 050. REMOVED AND REPLACED FORWARD CARGO, LOWER DOOR PAN IAW SRM 53-05, FIG 44. 2 L 7 2 4F 4 F A6WE E2EA 2003080100088 20030801 00088 WP 2003 8 1 AAL2003F00001 1 20021016 A 5313 LONGERON DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A AALA K NONE O OTHER UK UNKNOWN 1 SW 21 241AA 49254 LONGERON CRACKED, STA 160, L29L, OUT OF LIMITS. CUT OFF DAMAGED AREA, INSTALLED LONGERON SPLICE CAP IAW SRM 53-02-00. 2 L 7 2 4F 4 F A6WE E2EA 2003080100092 20030801 00092 WP 2003 8 1 AAL2003F00007 1 20021009 A 5313 LONGERON DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A AALA K NONE O OTHER UK UNKNOWN 1 SW 21 241AA 49254 CRACK IN LOWER LONGERON FLANGE AT FASTENER AT FRAME STA 275, LONGERON 17 RT. E58 NR 4426954 INSTALLED LONGERON SPLICE S ECTION FROM STA 265-285, L17 RT SIDE IAW SRM 53-02-00 FIG 18, SHT 1. 2 L 7 2 4F 4 F A6WE E2EA 2003080600001 20030806 00001 GL 2003 8 6 LS1R088304 2 20021017 A 7310 369A81433 PUMP HUGHES 369 369D 4470706 WP ALLSN 250C 250C20 03013 GL FUEL SYSTEM INOPERATIVE E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 5027P 611002D FUEL PUMP INOPERATIVE. 1 G 7 1 3U 3 U H3WE E4CE 2003080600003 20030806 00003 SW 2003 8 6 LS1R088307 1 20020529 A 2436 15891F VOLT REGULATOR BELL 206 206B3 1181506 SW ALLSN 250C 250C20 03013 GL ELECTRICAL FAILED E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 90322 1736 DC REGULATOR FAILED TO REGULATE. 1 G 7 1 3U 3 U H2SW E4CE 2003080100089 20030801 00089 WP 2003 8 1 AAL2003F00015 1 20021029 A 5320 WEB DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 SUBFLOOR WEB CRACKED UNDER NR 5 SEAT TRACK, STA 216. 4 INCH X 4 INCH AREA 1 INCH LENGTH. FABRICATED DOUBLER OUT OF 707 5-T6 AND INSTALLED IAW AARD. 2 L 7 2 4F 4 F A6WE E2EA 2003080100093 20030801 00093 WP 2003 8 1 AAL2003F00004 1 20021014 A 2560 MOUNT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE AFT SERVICE DOOR CORRODED A AALA K NONE O OTHER UK UNKNOWN 1 SW 21 241AA 49254 AFT GIRT BAR MOUNT AT AFT SERVICE DOOR, CORRODED. 6 INCH X 8 INCH AREA CORRODED. INSTALLED TITANIUM DOUBLER IAW SRM 53 -03 AND AARD 53-00-00-2. 2 L 7 2 4F 4 F A6WE E2EA 2003080600018 20030806 00018 WP 2003 8 6 LS1R088298 1 20020302 A 7714 369D24518 INDICATOR HUGHES 369 369D 4470706 WP N2 DUAL TACH NOISY E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 5027P 84 611002D DUAL TACH INDICATOR NOISY. 1 G 7 1 3U H3WE 2003080700112 20030807 00112 SW 2003 8 7 LS1R088295 1 20020211 A 3020 GEAR BELL 206 206B3 1181506 SW ACTUATOR MISSING E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 49718 1775 1917 ACTUATOR GEARS ARE MISSING. 1 G 7 1 3U H2SW 2003080600006 20030806 00006 WP 2003 8 6 LS1R088277 1 20020119 A 2820 369A81433 PUMP HUGHES 369 369E 4470707 WP ALLSN 250C 250C20 03013 GL FUEL SYSTEM ROUGH E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 8330P 0330E FUEL PUMP ROUGH. 1 G 7 1 3U 3 U H3WE E4CE 2003080600015 20030806 00015 WP 2003 8 6 LS1R088278 1 20020419 A 6700 369A717011 MOTOR HUGHES 369 369D 4470706 WP LATERAL TRIM FAILED E LS1R O OTHER L NO TEST NR NOT REPORTED 1 EA 13 1097J 900801D LATERAL TRIM MOTOR FAILED CHECK. 1 G 7 1 3U H3WE 2003080600016 20030806 00016 WP 2003 8 6 LS1R088286 1 20020428 A 6700 369A717011 MOTOR HUGHES 369 369D 4470706 WP LATERAL TRIM STICKING E LS1R O OTHER O OTHER NR NOT REPORTED 1 EA 13 1097J 15 900801D LATERAL TRIM MOTOR STICKING. 1 G 7 1 3U H3WE 2003081200034 20030812 00034 SW 2003 8 12 ALGA088361 1 20020925 A 7722 212075067119 INDICATOR BELL 412 412EP 1182205 SW ITT STUCK B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5NBDZ 36278 INDICATOR NEEDS REPAIR DUE TO STUCK AT ZERO, WOULD NOT INCREASE DURING 2 ATTEMPTS ON OPPOSITE ENGINES. 1 G 7 2 4U H4SW 2003081300111 20030813 00111 NM 2003 8 13 AALA20021874 1 20021219 A 3397 CONNECTOR BOEING 767 767223 1385123 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 325AA 22326 JFK - FLT 004 - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SEAT 31AB THROUGH 37AB INOPERATIVE. RECONN ECTED CONNECTOR TO BATTERY PACK. SYTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003082600060 20030826 00060 CE 2003 8 26 5300123102 1 20021231 A 7931 99124641 TRANSMITTER CESSNA 560 560XL 2076702 CE LT ENGINE FAILED E S4WA K NONE N FALSE WARNING LD LANDING 1 WP 07 613GY 42 5605300 LOST LEFT ENGINE OIL PSI, INDICATION. 2 L 7 2 4F RT A22CE 2003082600065 20030826 00065 2003 8 26 3144081302 4 20020813 A 3421 5040017901 GYRO SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE COCKPIT INOPERATIVE E S4WA K NONE L NO TEST NR NOT REPORTED 1 WP 07 5226R 1384 3144 22043 ALTITUDE GYRO INOP. 1 G 7 1 3U 3 U H9EU E00054EN 2003082600069 20030826 00069 2003 8 26 3144102902 4 20021029 A 3422 060001600 GYRO SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE COCKPIT INOPERATIVE E S4WA K NONE L NO TEST NR NOT REPORTED 1 WP 07 5226R 1619 3144 22043 DIRECTIONAL GYRO INOP. 1 G 7 1 3U 3 U H9EU E00054EN 2003082600070 20030826 00070 EU 2003 8 26 3144121102 1 20021211 A 2432 RG350 BATTERY SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE CARGO BAY DISCHARGED E S4WA K NONE L NO TEST NR NOT REPORTED 1 WP 07 5226R 573 3144 22043 BATTERY VOLTAGE LOW. 1 G 7 1 3U 3 U H9EU E00054EN 2003082600072 20030826 00072 EU 2003 8 26 3144 1 20020818 A 2150 0500846 BLOWER MOTOR SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE A/C SYSTEM SEIZED E S4WA K NONE L NO TEST NR NOT REPORTED 1 WP 07 5226R 1403 3144 22043 CONDENSER BLOWER MOTOR FOR AIR CONDITIONER IS SEIZED AND 25A BREAKER POPPED. 1 G 7 1 3U 3 U H9EU E00054EN 2003082600178 20030826 00178 EU 2003 8 26 VY1L103159 1 20020922 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR DELAMINATED L VY1L O OTHER O OTHER NR NOT REPORTED 1 SW 19 350HG 2321 BEARING DELAMINATED. UNIT FAILED WITH 475.8 TTSN. 1 G 7 1 3U 3 U NC H9EU E19EU 2003082700039 20030827 00039 EA 2003 8 27 GSB2006DEC02 2 20021216 A 7321 3244755222118 FUEL CONTROL BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA RT ENGINE MALFUNCTIONED E ENHA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 90PB 3276 BB125 PCE80262 DURING CRUISE FLIGHT RIGHT ENGINE WOULD NOT DEVELOPE POWER, THE ENGINE WAS SHUTDOWN, THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. THE CAUSE OF THE ENGINE POWER LOSS WAS DETERMINED TO BE POSSIBLE (FUEL CONTROL UNIT) INTERNAL MALFUNCTION. THE FCU WAS REPLACED WITH (0) TSO UNIT. AS A PRECAUTIONARY MEASURE THE HI PRESS PUMP WAS REPLACED WITH (0) TSO COMPONEN T. THE AIRCRAFT WAS GROUND RUN AND ENGINE TRIM ADJUSTED. NO FURTHER ENGINE OPERATIONAL PROBLEMS WERE INCOUNTERED, ENGI NE GROUND RUN-UP CHECKS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. TTSO ON FAULTED FUEL CONTROL UNIT 3276.7. 1 L 7 2 4T 4 T A24CE E4EA 2003082600066 20030826 00066 EU 2003 8 26 3144060302 1 20020603 A 2150 SD5 COMPRESSOR SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1D1 NE A/C SYSTEM DEFECTIVE E S4WA K NONE L NO TEST NR NOT REPORTED 1 WP 07 5226R 1196 3144 22043 A/C COMPRESSOR DEFECTIVE. 1 G 7 1 3U 3 U H9EU E19EU 2003082600067 20030826 00067 EU 2003 8 26 3144062402 1 20020624 A 2150 SD5 COMPRESSOR SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE A/C SYSTEM DEFECTIVE E S4WA K NONE L NO TEST NR NOT REPORTED 1 WP 07 5226R 43 3144 22043 A/C COMPRESSOR NOT WORKING. 1 G 7 1 3U 3 U H9EU E00054EN 2003090900176 20030909 00176 SW 2003 9 9 HEEA088931 1 20020406 A 5610 407030115123 WINDSHIELD BELL 407 407 1182206 SW COCKPIT CRAZED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 407PH 53003 WINDSHIELD CRAZED. 1 G 7 1 3U O H2SW 2003090900187 20030909 00187 SW 2003 9 9 HEEA088937 1 20021114 A 5610 407030115125A WINDSHIELD BELL 407 407 1182206 SW COCKPIT CRAZED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 467PH 53142 WINDSHIELD CRAZED. 1 G 7 1 3U O H2SW 2003090900193 20030909 00193 SW 2003 9 9 HEEA088942 1 20020917 A 5610 407030115125A WINDSHIELD BELL 407 407 1182206 SW COCKPIT CRAZED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 402PH 53159 WINDSHIELD CRAZED. 1 G 7 1 3U O H2SW 2003091100185 20030911 00185 EU 2003 9 11 AALA20021716 1 20021126 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7083A 645 TUL - FOUND CORROSION ON FLOORBEAM BETWEEN ROLLER TRAY 2 AND 3, FS 62. REMOVED CORRODED SECTION AND SPLICED IN NEW SECT ION IAW SRM 53-10-15. (M) 2 L 7 2 4F RT A35EU 2003091100196 20030911 00196 EU 2003 9 11 AALA20021718 1 20021202 A 5514 ATTACH ANGLE AIRBUS 300 A300B4605R 3930308 EU HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7083A 645 TUL - FOUND RIGHT HORIZ STAB L/E ATTACH ANGLE, UPPER, AFT ANGLE CORROSION AROUND NUTPLATES FOR L/E ATTACH FASTENERS. RE MOVED AND REPLACED SUPPORT ASSEMBLY. (M) 2 L 7 2 4F RT A35EU 2003091100201 20030911 00201 EU 2003 9 11 AALA20021717 1 20021126 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7083A 645 TUL - FOUND CORROSION ON FLOORBEAM AROUND NUTPLATE HOLES AFT OF ROLLER TRAY NR 1. REMOVED AND REPLACED WITH SECTION OF SUPPORT IAW 53-10-15. (M) 2 L 7 2 4F RT A35EU 2003091100156 20030911 00156 EU 2003 9 11 AALA20021351 1 20020923 A 5730 SKIN AIRBUS 300 A300B4605R 3930308 EU WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 11060 470 FOUND BOTTOM SKIN (WING) CORRODED TOP SURFACE JUST INBOARD OF NR 5 JACKSCREW. FLAP PEENED BLENDED AREA PER SRM 51-29-00 -2 ALODINED AND PRIMED PER ESO 30595 DATED 9-23-2002. (M) 2 L 7 2 4F RT A35EU 2003091100199 20030911 00199 EU 2003 9 11 AALA20021402 1 20020930 A 5230 CASTING AIRBUS 300 A300B4605R 3930308 EU CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 41063 506 TUL - FOUND CORROSION, FORWARD CARGO NR 9 ROLLER CASTING, FS 24A. REPAIRED PER ESO 30595, DATED 9-30-2002. (M) 2 L 7 2 4F RT A35EU 2003091200008 20030912 00008 WP 2003 9 12 AALA200217AA 1 20021209 A 2150 A/C PACK DOUG DC9 DC982 3022082 WP ACM BAY DIRTY A AALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 237AA 49253 JFK - FLT 1683 - ABOUT 4 MINUTES AFTER TAKEOFF PILOTS AND FLIGHT ATTENDANTS NOTICED AN ACRID SMELL WITH ASSOCIATED HEAVY HAZE IN CABIN. A LIGHT HAZE IN COCKPIT, IMMEDIATELY TURN OFF PACKS AND CABIN EXHAUST FAN. FLIGHT ATTENDANT SAID SMOKE/H AZE WAS NOT DISSIPATING. RETURN JFK AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. HAZE AND SLIGHT ODOR PERSISTE D ON GROUND AND AT GATE. ACCOMPLISHED LEFT AND RIGHT PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003091200184 20030912 00184 EU 2003 9 12 AALA20021673 1 20021122 A 2910 BACH8A06NN0260 HYDRAULIC LINE AIRBUS 300 A300B4605R 3930308 EU RT WING LEAKING A AALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 21 7055A 462 PTY - FLT 1700 - EN ROUTE FROM SJO-MIA - ON CLIMB-OUT, LOST ALL GREEN HYDRAULIC QUANTITY. DECLARED EMERGENCY AND LANDED IN PTY WITHOUT INCIDENT. FOUND HYDRAULIC LEAK AT RIGHT INBOARD AILERON CETNER SERVO ACTUATOR. REPLACED FLEX LINE AND SERVICED GREEN SYSTEM HYDRAULICS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2003082600181 20030826 00181 EU 2003 8 26 VY1L107551 1 20021214 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED L VY1L O OTHER O OTHER NR NOT REPORTED 1 SW 19 67TV 2859 TAIL ROTOR BEARINGS CRACKING. 1 G 7 1 3U 3 U NC H9EU E19EU 2003082600183 20030826 00183 EU 2003 8 26 VY1L110899 1 20021102 A 1430 350A31206720 BOLT SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE MAIN ROTOR WORN L VY1L O OTHER O OTHER NR NOT REPORTED 1 SW 19 211FN 2174 BOLTS, WORN. (SN 27148, 27269, 27486, 27143, 27423, 27619) 1 G 7 1 3U 3 U H9EU E19EU 2003082600184 20030826 00184 EU 2003 8 26 VY1L103151 1 20020807 A 6410 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR DELAMINATED L VY1L O OTHER O OTHER NR NOT REPORTED 1 SW 19 453NW 457 2475 UNITS FAILED WITH 457.6 TTSN. WARRANTY PART REPLACEMENT. 1 G 7 1 3U 3 U H9EU E19EU 2003082900080 20030829 00080 EU 2003 8 29 OX302129361 1 20021204 A 3060 C40543 BRUSH BLOCK BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP LT ENGINE SHORTED A O3XA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 03 936AE 167 936 APPROXIMATELY 35 MILES FROM STL, A BRIGHT BLUE GLOW WAS NOTICED COMING FROM THE LEFT ENGINE NACELLE JUST BEHIND THE PROP ESSER SPINNER. THE BLUE GLOW WOULD OCCASIONALLY FLASH BRIGHT RED AND ORANGE. ALL SYSTEMS AND ENGINE INDICATIONS WERE N ORMAL. A PRECAUTIONARY LEFT ENGINE SHUT DOWN WAS PERFORMED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECT ED THE ENGINE AND FOUND THAT THE LEFT PROPELLER BRUSH BLOCK HAD SHORTED OUT. THE BRUSHES WERE REPLACED IAW THE AMM CHP 30-60-05 AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A56EU E2WE 2003082900069 20030829 00069 WP 2003 8 29 GTIA021069 1 20021009 A 5321 FLOOR PANEL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 47605 THE 04BD RT FLOOR PANEL AT ROWS 12 THROUGH 15 HAS CRACK. REPAIRED FLOOR PANEL (CLOSED 10/15/02). 2 L 7 2 4F A6WE 2003090200055 20030902 00055 EU 2003 9 2 VY1L103200 1 20021214 A 6410 350A3321530 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR FAILED L VY1L O OTHER O OTHER NR NOT REPORTED 1 SW 19 6093R 6529 2415 BEARING DELAMINATED. UNIT FAILED WITH ONLY 409.2 HOURS. 1 G 7 1 3U 3 U H9EU E19EU 2003090300030 20030903 00030 EU 2003 9 3 PG9R100117 1 20021203 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR DELAMINATED A PG9R O OTHER O OTHER NR NOT REPORTED 1 WP 19 890AK 487 2138 TAIL ROTOR BEARING DELAMINATED AT 487.7 TTSN. 1 G 7 1 3U 3 U NC H9EU E19EU 2003090300120 20030903 00120 WP 2003 9 3 AALA2002139A 1 20020926 A 3397 CONTACTOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE EMERGENCY LIGHT DIRTY A AALA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SW 21 491AA 49684 DFW NO TRIP/26 - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS IL2-674 AND L2-637 INOPERATIVE. CLEANED EMERGENCY E XIT LIGHTS CONTACTS FOR B5-28 CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2003090300127 20030903 00127 SW 2003 9 3 ALG2003D00032 1 20020731 A 6210 407015001117 BLADE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR CRACKED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 557AL 2904 53243 DISCOVERED DURING ROUTINE INSPECTION. LEADING EDGE SHEATH CRACKED CHORDWISE AT STATION 132. 1 G 7 1 3U 3 U O H2SW E1GL 2003090200054 20030902 00054 EU 2003 9 2 VY1L103152 1 20020730 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR DELAMINATED L VY1L O OTHER O OTHER NR NOT REPORTED 1 SW 19 890AK 498 2138 BEARING DELAMINATED. UNITS FAILED WITH 498.1 TTSN. WARRANTY PARTS REPLACEMENT. 1 G 7 1 3U 3 U NC H9EU E19EU 2003090300053 20030903 00053 EU 2003 9 3 LN72003F00000 1 20021127 A 2435 80601411 BEARING AMD FALC20 FALCONF 2720306 EU GARRTT TFE731 TFE731* 01518 WP STARTER GEN FAILED B LN7R O OTHER E VIBRATION/BUFFET AP APPROACH 1 EA 13 520AW 2439 460 453 ON 11/27/02, THE AIRCRAFT EXPERIENCED VIBRATION WHILE ENROUTE. THE CREW FELT IT WAS A STARTER/GENERATOR AND DIVERTED. WHILE ON APPROACH, THE RT STARTER/GENERATOR FAILED. AFTER AN UNEVENTFUL LANDING THE STARTER/GENERATOR WAS REPLACED AND ALL WAS NORMAL. ON TEARDOWN THE FRONT BEARING WAS FOUND TO BE DESTROYED. 2 L 7 2 4F 4 F A7EU E6WE 2003090400171 20030904 00171 WP 2003 9 4 AALA20021794 1 20021204 A 2613 OVERHEAT SENSOR DOUG DC9 DC982 3022082 WP TAIL DEFECTIVE A AALA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 445AA 49471 MIA - FLT 1717 - EN ROUTE MIA-ORD, PASSING THROUGH 23,000 FEET TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIR FOIL ANTI-ICE WAS OFF AND TURNED PACKS TO HIGH PRESSURE BLEED OFF. LIGHT EXTINGUISHED. RETURNED TO MIA AND LANDED WITH OUT INCIDENT. REPLACED BOTH LEFT AND RIGHT OVER HEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2003090400194 20030904 00194 WP 2003 9 4 AALA20021792 1 20021209 A 2120 5910244125 DUCT DOUG DC9 DC983 3022083 WP A/C BAY BLOWN A AALA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 594AA 53284 DEN - FLT 830 - DURING CLIMB-OUT FROM PDX AT 27,000 FEET TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. AFTER RED BOX, L IGHT WENT OUT. LIGHT FLICKERED A FEW TIMES THE NEXT 4 MINUTES. SEEMED TO BE ASSOCIATED WITH RIGHT DUCT TEMPERATURE. L ANDED DENT WITHOUT INCIDENT. REPLACED RIGHT TEMPERATURE SENSING DUCT ASSEMBLY AND LOWER FLEX DUCT. RAN PACKS AND LEAK CHECKED. NO LEAKS NOTED, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT REMAINED OFF. SYSTEM GROUND CHECKED NORMAL OPERATION . (M) 2 L 7 2 4F RT A6WE 2003090900177 20030909 00177 SW 2003 9 9 HEEA088932 1 20020221 A 5610 407030115125A WINDSHIELD BELL 407 407 1182206 SW COCKPIT CRAZED E O OTHER O OTHER NR NOT REPORTED 1 SW 03 457PH 53147 WINDSHIELD CRAZED. 1 G 7 1 3U O H2SW 2003090900178 20030909 00178 SW 2003 9 9 HEEA088933 1 20020308 A 5610 407030115123 WINDSHIELD BELL 407 407 1182206 SW COCKPIT CRAZED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 457PH 53147 WINDSHIELD CRAZED. 1 G 7 1 3U O H2SW 2003090900179 20030909 00179 SW 2003 9 9 HEEA088934 1 20020719 A 5610 407030115125A WINDSHIELD BELL 407 407 1182206 SW COCKPIT CRAZED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 406PH 53198 WINDSHIELD CRAZED. 1 G 7 1 3U O H2SW 2003090900180 20030909 00180 SW 2003 9 9 HEEA088935 1 20020719 A 5610 407030115123A WINDSHIELD BELL 407 407 1182206 SW COCKPIT CRAZED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 406PH 53198 WINDSHIELD CRAZED. 1 G 7 1 3U O H2SW 2003090900181 20030909 00181 SW 2003 9 9 HEEA088936 1 20021114 A 5610 407030115123A WINDSHIELD BELL 407 407 1182206 SW COCKPIT CRAZED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 467PH 53142 WINDSHIELD CRAZED. 1 G 7 1 3U O H2SW 2003090900175 20030909 00175 SW 2003 9 9 HEEA088930 1 20020419 A 5610 407030115123 WINDSHIELD BELL 407 407 1182206 SW COCKPIT CRAZED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 612PH 53199 WINDSHIELD CRAZED. 1 G 7 1 3U O H2SW 2003091500103 20030915 00103 2003 9 15 HEED089116 4 20020420 A 3457 071128312 GPS SKRSKY S76 S76C 8143008 NE COCKPIT MALFUNCTIONED B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 476X 760436 STAND BY FREQUENCY BUTTON DOES NOT ALWAYS OPERATE. REPLACE UNIT. 1 G 7 2 3U NC H1NE 2003091500104 20030915 00104 NE 2003 9 15 HEED089118 1 20020421 A 6210 7615009100053 BLADE SKRSKY S76 S76C 8143008 NE MAIN ROTOR PEELING B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 476X 6306 760436 MAIN ROTOR BLADE PAINT PEELING, ORANGE PAINT WORN OFF. REPLACED UNIT. 1 G 7 2 3U NC H1NE 2003091500106 20030915 00106 NE 2003 9 15 HEED089120 1 20020518 A 6710 BEARING SKRSKY S76 S76C 8143008 NE BELLCRANK WORN B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 278X 760440 PIVOT BEARINGS WORN. REPLACED UNIT. 1 G 7 2 3U NC H1NE 2003091500109 20030915 00109 2003 9 15 HEED089125 4 20020308 A 2210 1418523211 AHRS SKRSKY S76 S76C 8143008 NE FUSELAGE INOPERATIVE B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 478X 760493 AHRS INOPERATIVE. OFF AND ON. REPLACED UNIT. 1 G 7 2 3U NC H1NE 2003091500110 20030915 00110 NE 2003 9 15 HEED089126 1 20020311 A 2742 7040002200108 ACTUATOR SKRSKY S76 S76C 8143008 NE LINEAR STUCK B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 478X 760493 LINEAR ACTUATOR STICKING. REPLACED UNIT. 1 G 7 2 3U NC H1NE 2003091500114 20030915 00114 WP 2003 9 15 MEX2002241 1 20020726 A 3246 3910097537 WHEEL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D17 52049 NE NLG DAMAGED W ASMF O OTHER O OTHER NR NOT REPORTED 1 SW 23 1003P 62247 62247 48150 DURING TOWING PROCEDURE IT WAS OBSERVED THE MISSING OF ONE NUT IN A WHEEL OF THE NLG. AIRCRAFT RETURNED TO PLATFORM TO REPLACE THE WHEEL 1 OF THE NLG IAW MM 32-21. 2 L 7 2 4F 4 F A6WE E2EA 2003091600040 20030916 00040 SO 2003 9 16 O2G2003F00005 1 20020905 A 2930 INDICATOR GULSTM G1159 G1159A 3970109 SO RROYCE TAY TAY6118 EU HYD SYSTEM MISSING E O2GA O OTHER D INFLIGHT SEPARATION TX TAXI/GRND HDL 1 NE 03 117MS 7673 335 AUX HYDRAULIC PRESSURE SYSTEM USED ON GROUND. FILTER HOUSING FAILED CAUSING DEPLETION OF FLUID. DIFFERENTIAL PRESSURE INDICATOR FOUND MISSING FROM HOUSING. FOUND FOUND (4) RETAINING SCREWS RESTED AND BROKE IN MIDDLE CAUSING DPI COVER TO BLOW OFF UNDER HYDRAULIC PRESSURE. HOUSING LOCATED IN WHEEL WELL WHERE SUBJECT TO FREEZING TEMPS AND HOT HYDRAULIC FLUI D TO CAUSE CONDENSATION AND CORROSION. SUGGEST SCREWS BE REPLACED WITH NON STEEL SCREWS. 2 L 7 2 4F 4 F A12EA E25NE 2003091600041 20030916 00041 WP 2003 9 16 GTIA021070 1 20021009 A 5321 FLOOR PANEL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 131NK 47605 6 TO 8 INCH CRACK IN FLOOR WEBBING STA 807, RT SIDE. REPLACED FLOOR WEBBING. 2 L 7 2 4F A6WE 2003091500101 20030915 00101 2003 9 15 HEED089114 4 20020319 A 3400 KFM098502 TRANSCEIVER SKRSKY S76 S76C 8143008 NE COCKPIT MALFUNCTIONED B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 476X 2705 760436 DOES NOT RECIEVE, NO SIDE TONE TRANSMITS O.K. REPLACE UNIT. 1 G 7 2 3U NC H1NE 2003091500105 20030915 00105 NE 2003 9 15 HEED089119 1 20020516 A 6710 BEARING SKRSKY S76 S76C 8143008 NE BELLCRANK WORN B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 278X 760440 PIVOT BEARINGS WORN. REPLACED UNIT. 1 G 7 2 3U NC H1NE 2003091600113 20030916 00113 NE 2003 9 16 AALA20021300 2 20020917 A 7200 JOINT AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE LT PYLON WORN A AALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 21 59081 639 EN ROUTE SJU-MCO, NR 1 ENGINE N1 VIBRATION CYCLED BETWEEN 4.0 AND 9.8. WHEN ENGINE REDUCED TO IDLE, ENGINE VIBRATION ST OPPED. CAPTAIN DECLARED EMERGENCY AND AIRCRAFT LANDED AT MIA WITHOUT INCIDENT. REPLACED LEFT ENGINE JOINT. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A35EU E13NE 2003091600121 20030916 00121 EU 2003 9 16 AALA20021674 1 20021121 A 2910 LINE AIRBUS 300 A300B4605R 3930308 EU LT PYLON LOOSE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 41063 506 SJU - FLT 1075 - EN ROUTE MCO-SJU, FLIGHT CREW NOTED GREEN HYDRAULIC SYSTEM QUANTITY LOSS. DECLARED EMERGENCY AND LANDE D AT SJU WITHOUT INCIDENT. FOUND NR 1 ENIGNE GREEN SYSTEM PRESSURE LINE ON PYLON LEAKING. TIGHTENED LINE. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2003091600152 20030916 00152 WP 2003 9 16 AAL2003F00002 1 20021016 A 5320 BRACKET DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE FUSELAGE BROKEN A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 21 241AA 49254 VARIABLE LOAD FEEL BRACKET, RT OUTBOARD LUG BROKEN. OUT OF LIMITS, COCKPIT AT STA 108. REPLACED VARIABLE LOAD FEEL BRA CKET IAW ESO 80559. 2 L 7 2 4F 4 F A6WE E2EA 2003091700003 20030917 00003 EA 2003 9 17 ENH2003F00000 2 20021206 A 7321 FUEL CONTROL BEECH 200 200BEECH 1152920 CE PWA PT6 PT6* 52043 EA ENGINE INOPERATIVE E ENHA O OTHER O OTHER NR NOT REPORTED 1 AL 03 90PB BB125 RT ENGINE NO DEVELOPING POWER (SHUT DOWN RIGHT ENGINE) REPLACED FCU AND HIGH PRESSURE FUEL PUMP W/OVERHAULED UNIT. WO N R 5352856 DATED MARCH 6, 02 (PUMP) 5284375 DATED 22 AUG O2 (FCU) GROUND RAN AND LEAK CHECKED GOOD. ADJUSTED IDLE SPEED TO 52 PERCENT. 1 L 7 2 4T 3 T A24CE E2NE 2003091700007 20030917 00007 SW 2003 9 17 ALG2003F00067 1 20020711 A 6420 20071849H BOLT BELL 214 214ST 1182106 SW GE CT7TS CT71 30030 NE T/R YOKE PLATE BROKEN E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 393AL 122 28117 DURING THE DAILY SERVICE CHECK. BROKEN TAIL ROTOR YOKE PLATE BOLT. 2 G 7 2 4U 4 U H10SW E8NE 2003091700008 20030917 00008 NE 2003 9 17 ALG2003F00068 1 20020731 A 3297 WIRE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C* GL FLOAT BOTTLE FAILED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 768AL 760031 DURING PRESTART CHECKLIST. WHEN THE (AUX ESS POWER) CHECK WAS DONE, THE PILOT FLOAT BOTTLE DISCHARGED, AFTER APPROXIMAT ELY 2-3 SECONDS. WHILE SWITCH WAS ENGAGED FLOAT (ARM) SWITCH WAS OFF FLOAT (TEST) SWITCH WAS IN (NORMAL). REPAIRED CH AFFED AND BROKEN WIRE JUST FORWARD OF CONNECTOR P216 IN RIGHT FORWARD INSTRUMENT CONSOLE. RELAY K-19 (PN MS 27400-1) IN NR 2 RELAY PANEL WAS REPLACED. 1 G 7 2 3U 3 U H1NE E4CE 2003091700009 20030917 00009 NE 2003 9 17 ALG2003F00069 1 20020724 A 2612 30295G6 BULB SKRSKY S76 S76A 8143006 NE FIRE WARN LIGHT BURNED OUT E ALGA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SW 03 741SW 760070 DURING RUN-UP, NR 1 ENGINE FIRE LIGHT DOES NOT TEST IN AFT POSITION. REMOVED AND REPLACED BURNED OUT BULB. 1 G 7 2 3U H1NE 2003091700065 20030917 00065 SW 2003 9 17 HEED089077 1 20020411 A 2435 23081063 STARTER GEN BELL 430 430 1182150 SW ENGINE MALFUNCTIONED B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 430XM 767 4973 WILL NOT TURN ENGINE. REPLACE UNIT. 1 G 7 2 3U RT H9SW 2003091800059 20030918 00059 NM 2003 9 18 DL777030715 1 20020802 A 2910 AS4568G0580SS FLEX LINE BOEING 777 777232 1385232 NM RT MLG STEERING LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 864DA 29736 ATB CTR HYD SYS FAILED-MTC MSG 29-10150 CTR HYD QTY LOW FLEX LINE GOING TO THE RT MLG STEERING ACT LEAKING (P/N AS4568G0 580SS)- REPLACED LINE. 2 L 7 2 4F RT T00001SE 2003100700003 20031007 00003 NM 2003 10 7 AALA20021873 1 20021218 A 2697 WIRE BOEING 767 767323 1385205 NM RT ENGINE BROKEN A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 377AN 25446 EN ROUTE ORD-LHR, RIGHT ENGINE BLEED OVER TEMP. DECLARED EMERGENCY AND LANDED JFK UNEVENTFULLY. AIRCRAFT LANDED OVERWE IGHT. REPAIRED WIRES FOR RIGHT OVER TEMP SWITCH AND REPLACED SENSE LINE TO RIGHT PRE-COOLER. PERFRMED ENGINE RUN AND OV ERWEIGHT INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003101000098 20031010 00098 2003 10 10 HEED089112 4 20020714 A 3197 WIRE SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL1 60030 NE DISPLAY BROKEN B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 476X 760436 SCREEN WAS WORN, WIRES BROKEN AND SEPARATED. REPLACE UNIT. 1 G 7 2 3U 3 U NC H1NE E19EU 2003091500102 20030915 00102 2003 9 15 HEED089115 4 20020418 A 2210 7690001802106 ACTUATOR SKRSKY S76 S76C 8143008 NE AFCS MALFUNCTIONED B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 476X 2445 760436 AFCS ACTUATOR FEEDBACK IN CYCLIC KICKS. REPLACE UNIT. 1 G 7 2 3U NC H1NE 2003091500108 20030915 00108 NE 2003 9 15 HEED089124 1 20020219 A 6220 7690001813101 TRANSDUCER SKRSKY S76 S76C 8143008 NE MAIN ROTOR GB MALFUNCTIONED B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 478X 3805 760493 TRANSDUCER AFFECTS PBA. REPLACED UNIT. 1 G 7 2 3U NC H1NE 2003091700010 20030917 00010 SW 2003 9 17 ALG2003F00070 1 20020722 A 6510 407340339101 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/R DRIVESHAFT FAILED E ALGA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 03 547AL 66 A287 53240 DURING CRUISE FLIGHT THE PILOT FELT A SEVERE VIBRATION IN THE AIRFRAME AND PERFORMED A PRECAUTIONARY LANDING ON A NEARBY PLATFORM. FORWARD BEARING ON NR 2 TAILROTOR DRIVESHAFT BLOWER ASSEMBLY FAILED. 1 G 7 1 3U 3 U O H2SW E1GL 2003091700070 20030917 00070 SW 2003 9 17 HEED089083 1 20020214 A 6520 406040400117 GEARBOX BELL 407 407 1182206 SW TAIL ROTOR VIBRATION B HEED O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SW 03 407XM 1093 53464 UNEXPLAINED TAIL ROTOR VIBRATION AND GRITTY SUBSTANCE IN GEARBOX. REPLACE UNIT. 1 G 7 1 3U O H2SW 2003091500107 20030915 00107 2003 9 15 HEED089122 4 20020116 A 3420 1418523211 AHRS SKRSKY S76 S76C 8143008 NE COCKPIT INTERMITTENT B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 478X 760493 AHRS INTERMITTANTLY INOPERATIVE, WILL NOT STAY ON LINE. REPLACED UNIT. 1 G 7 2 3U NC H1NE 2003091700066 20030917 00066 2003 9 17 HEED089078 4 20020422 A 2312 064102300063 RADIO BELL 430 430 1182150 SW COCKPIT MALFUNCTIONED B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 430XM 806 4973 UNABLE TO CONTROL SQUELCH AFTER 20 MINUTES OF OPERATION REPLACE UNIT. 1 G 7 2 3U RT H9SW 2003091700067 20030917 00067 SW 2003 9 17 HEED089080 1 20020214 A 6420 BEARING BELL 407 407 1182206 SW BELLCRANK ASSY WORN B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 407XM 1093 53464 TAIL ROTOR BELLCRANK ASSY HAS WORN BEARINGS. REPLACE UNIT. 1 G 7 1 3U O H2SW 2003091700069 20030917 00069 SW 2003 9 17 HEED089082 1 20020214 A 6420 407012101111 ROTOR HEAD BELL 407 407 1182206 SW TAIL ROTOR DAMAGED B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 407XM 1093 53464 TAIL ROTOR HEAD WAS UNABLE TO DYNAMICALLY BALANCE. REPLACE UNIT. 1 G 7 1 3U O H2SW 2003091600043 20030916 00043 NM 2003 9 16 RYN2003F00007 1 20020508 A 5523 65C2538428A TAB BOEING 737 737* NM RT ELEVATOR BROKEN A RYNA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 CE 07 EIBXI 25052 ON CLIMBOUT, FLIGHT CREW NOTED AIRFRAME VIBRATION. REDUCING THRUST ON BOTH ENGINES HAD NO EFFECT. FLIGHT CREW SELECTED FLAPS FIVE DEGREE POSITION DURING LANDING AND VIBRATION STOPPED, PERFORMED OVERWEIGHT LANDING WITHOUT INCIDENT. POST F LIGHT INSPECTION REVEALED A PORTION OF THE RT ELEVATOR SERVO TAB MISSING. ELEVATOR AND TAB ASSEMBLY TO BE REPLACED. 2 L 7 2 4F RT A16WE 2003091700068 20030917 00068 SW 2003 9 17 HEED089081 1 20020214 A 6720 BEARING BELL 407 407 1182206 SW CONTROL TUBE WORN B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 407XM 1084 53464 TAIL ROTOR CONTROL TUBE WORN BEARINGS REPLACE UNIT. 1 G 7 1 3U O H2SW 2003092200104 20030922 00104 SW 2003 9 22 HEED089184 1 20020413 A 5302 STRUCTURE BELL 407 407 1182206 SW TAILBOOM CRACKED B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 3193E 2909 53276 53276 CRACKED ON UPPER AFT LT SIDE OF HORIZONAL STABLIZER OPENING. REPLACE UNIT. 1 G 7 1 3U O H2SW 2003100300002 20031003 00002 NM 2003 10 3 AALA20021684 1 20021115 A 2782 3818001001 ACTUATOR BOEING 737 737823 13844BZ NM NR 6 SLAT INOPERATIVE A AALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 21 924AN 29525 LEADING EDGE SLAT WOULD NOT RETRACT. AIRCRAFT LANDED PHL WITHOUT INCIDENT. REPLACED NR 6 LEADING EDGE SLAT ACTUATOR. ACCOMPLISHED THERMO CHECKS OF ALL SLAT FLAP ACTUATORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2003100300010 20031003 00010 EU 2003 10 3 AALA20021869 1 20021225 A 2910 HYDRAULIC LINE AIRBUS 300 A300B4605R 3930308 EU LEFT ENGINE DAMAGED A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 70079 619 EN ROUTE PAP-JFK, PILOT RECEIVED ECAM MESSAGE STATING THAT BLUE HYDRAULIC SYSTEM RESERVOIR LOW. LANDED AT MIA WITHOUT I NCIDENT. FOUD LEFT ENGINE HYDRAULIC LINE LEAKING. REPLACED LINE AND SERVICE HYDRAULIC SYSTEM. SYSTEM GROUND AND FLIGH T CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2003100700001 20031007 00001 NM 2003 10 7 AALA20021646 1 20021113 A 2913 62983 PUMP BOEING 767 767323 1385205 NM RT ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 360AA 24041 EN ROUTE LHR-EWR, RT ENGINE HYDRAULIC PUMP FAILED. AIRCRAFT DIVERTED TO BOS LANDED WITHOUT INCIDENT. REPLACED RIGHT EN GINE HYDRAULIC DRIVEN PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2003100700024 20031007 00024 NE 2003 10 7 AALA20021903 2 20021228 A 7261 ENGINE BOEING 767 767223 1385123 NM GE CF6 CF680A 30025 NE RIGHT LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 304AA 22310 SHORLTY AFTER TAKEOFF, AIRCRAFT AIR INTERRUPTED DUE TO SMOKE/VAPOR IN AFT CABIN ON CLIMB-OUT. AIRCRAFT RETURNED TO JFK LANDED WITHOUT INCIDENT. RELACED RIGHT ENGINE DUE TO INTERNAL OIL LEAK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 2003100700025 20031007 00025 NE 2003 10 7 AALA20021905 2 20021227 A 7200 SHUTOFF VALVE BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE NR 1 ENGINE DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 362AA 24043 LT ENGINE HIGH PRESSURE SHUTOFF VALVE ILLUMINATED DURING CRUISE. AIRCRAFT RETURNED TO LAX ACCOMPLISHED OVERWEIGHT LANDE D WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION AND REPLACED NR 1 ENGINE HIGH PRESSURE CONTROL VALVE. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 2003101400009 20031014 00009 NE 2003 10 14 HEED089117 1 20020518 A 6420 7640003006053 BELLCRANK SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL1 60030 NE LINK ASSY CORRODED B HEED O OTHER O OTHER NR NOT REPORTED 1 SW 03 278X 760440 BEARINGS WORN AND CORRODED. REPLACED UNIT. 1 G 7 2 3U 3 U NC H1NE E19EU 2003102300006 20031023 00006 NM 2003 10 23 02FDEA00929 1 20021206 A 5530 SKIN BOEING 727 727200 138407E NM PWA JT8 JT8D9 52048 NE VERTICAL FIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 RT VERTICAL FIN SKIN HAS 2 POSSIBLE CRACKS EMANATING FROM FASTENERS AT BS 1214 COMMON TO SPAR ** SD ** DAMAGE TO RT VE RTICAL FIN SKIN AT BS 1214 COMMON TO FRONT SPAR FORGING JUST ABOVE FUSELAGE IS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-0 1, REPAIRED DAMAGE IAW 55-30-3. 2 L 7 3 4F 4 F RT A3WE E2EA 2003102300007 20031023 00007 NM 2003 10 23 02FDEA00934 1 20021206 A 5310 CREASE BEAM BOEING 727 727200 138407E NM PWA JT8 JT8D9 52048 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 N00836 CORROSION C53-224-02 CREASE BEAM BS 500 RBL 67. CORROSION ON CREASE BEAM AT BS 600, RBL 67, WL208 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED CREASE BEAM BS 445-525, RBL 67,WL 208. FABRICATED REPLACEMENT CREASE BEAM FROM BAC 1515-531 7075-T6 LOT NR 391371 IAW SRM 51-30-5. INSTALLED CREASE BEAM BS 445-525, RBL 67, WL 208 IAW SRM 51-30-2 AND SOPM 20-50-01. 2 L 7 3 4F 4 F RT A3WE E2EA 2003102700066 20031027 00066 CE 2003 10 27 8303762 1 20021002 A 2720 BOLT RAYTHN BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CONTROL HORN LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 830CA 3889 672 UE393 DURING DETAIL NR 6 INSPECTION, FOUND RUDDER TORQUE TUBE TO CONTROL HORN MOUNT BOLTS LOOSE. REPLACED HORN AND HARDWARE. 2 L 7 2 4T 3 T RT A24CE E2NE 2003102700067 20031027 00067 CE 2003 10 27 8383606 1 20021107 A 2720 BOLT RAYTHN BEECH 1900 1900D 1154162 CE CONTROL HORN LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 838CA 3942 672 UE396 DURING DETAIL NR 6 INSPECTION, FOUND RUDDER TORQUE TUBE TO CONTROL HORN MOUNT BOLTS LOOSE. REPLACED HORN AND HARDWARE. 2 L 7 2 4T RT A24CE 2003103000090 20031030 00090 WP 2003 10 30 02FDEA00597 1 20020814 A 3230 LANDING GEAR DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL LEFT FAILED A FDEA H DEACTIVATE SYST/CIRCUITS E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION LD LANDING 1 SO 25 388FE 46622 IN LANDING PATTERN AT TPA AT GEAR EXTENSION HEARD LOUD BANG AND A/C SHUTTERED SERIOUSLY. NR 3 HYDRAULIC DEC TO ZERO. LE FT MLG READ UNSAFE LIGHTS ILLUMINATED ON BOTH FRONT AND ENGINEER'S PANEL. ACCOMPLISHED APPROPRIATE RED TAB PROCEDURES. LANDED AND EVACUATED AIRCRAFT. (COMPANY FERRYED AIRCRAFT TO MEM FOR PERMANENT REPAIR). REPLACED THE FOLLOWING COMPONEN TS LT MAIN LANDING GEAR DOWN LOCK CYLINDER, ALL MAIN TIRES AND BRAKES AND RIGHT EVACUATION SLIDE. 2 L 7 3 4F 4 F A22WE E23EA 2003111200010 20031112 00010 NM 2003 11 12 2003UALA00792 1 20021020 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 393UA 24668 STRINGER 8 RT CRACKED AT FIVE CONSECUTIVE STRINGER CLIP LOCATIONS. STA 500, 500A, 500B, 500C, 500D. MAJOR REPAIR ACCOMPL ISHED. REMOVED DAMAGED STRINGER FROM STA 500 TO 520, SPLICED IN STRINGER SECTION AND REPLACED CLIPS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004011200024 20040112 00024 CE 2004 1 12 2004F00013 1 20021121 A 3297 CONNECTOR BEECH 1900 1900C 1154161 CE MLG DAMAGED A YADA O OTHER N FALSE WARNING LD LANDING 1 AL 03 45GL UC45 AT LANDING IN ANCHORAGE, PILOT REPORTED MLG WAS SLOW TO GO DOWN, THE LANDING GEAR WARNING HORN WOULD NOT SILENCE AND INT RANSIT LIGHTS REMAINED ON WITH THREE GREEN SAFE LIGHTS ALSO ON. MAINTENANCE COULD NOT DUPLICATE. REPLACED PCB FOR WARN ING HORN FAULT, RESEATED PIN E ON RIGHT GEAR DOWN LOCK CONNECTOR AND REPLACED RIGHT POWER LEVER GEAR WARNING HORN SWITCH . (M) 2 L 7 2 4T RT A24CE 2004011200025 20040112 00025 CE 2004 1 12 2004F00014 1 20021210 A 3260 ANNUNCIATOR BEECH 1900 1900C 1154161 CE MLG INDICATOR INOPERATIVE A YADA O OTHER N FALSE WARNING NR NOT REPORTED 1 AL 03 1566C UC36 PILOT REPORTED THAT THE NOSE GEAR DOWN AND LOCK GREEN LIGHT WAS INTERMITTENT. MAINTENANCE REPLACED THE GEAR DOWN AND LO CK ANNUNCIATOR. (M) 2 L 7 2 4T RT A24CE 2004011200029 20040112 00029 CE 2004 1 12 2004F00016 1 20021203 A 3297 MS24171D1 RELAY BEECH 1900 1900C 1154161 CE MLG CONTAMINATED A YADA O OTHER N FALSE WARNING LD LANDING 1 AL 03 45GL UC45 ON APPROACH TO LANDING IN ANCHORAGE, THE PILOT SELECTED LANDING GEAR DOWN TWICE WITH NO EFFECT. THE GEAR WAS EXTENDED M ANUALLY AND THE LANDING WAS WITHOUT INCIDENT. MAINTENANCE CONFIRMED THAT THE HYDRAULIC PUMP RELAY WAS FREEZING, HIGH MO ISTURE CONTENT IN UNIT, AND REPLACED SAME. (M) 2 L 7 2 4T RT A24CE 2004011200057 20040112 00057 CE 2004 1 12 2004F00022 1 20021209 A 3260 CONNECTOR BEECH 1900 1900C 1154161 CE MLG DIRTY A YADA O OTHER P NO WARNING INDICATION LD LANDING 1 AL 03 1566C UC36 AT LANDING IN ANCHORAGE, THE GEAR GREEN SAFE LIGHT DID NOT ILLUMINATE FOR 30 SECONDS AFTER THE SECOND EXTENSION ATTEMPT. THE LANDING WAS COMPLETED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM AND CLEANED CONNECTORS AND PE RFORMED A SATISFACTORY OPERATIONAL CHECK FLIGHT. (M) 2 L 7 2 4T RT A24CE 2004011200050 20040112 00050 CE 2004 1 12 2004F00021 1 20021207 A 3297 WIRE BEECH 1900 1900C 1154161 CE DOWNLOCK SWITCH CORRODED A YADA O OTHER N FALSE WARNING LD LANDING 1 SW 03 41UE UC41 AT LANDING IN ANCHORAGE, THE GEAR UNSAFE LIGHT CAME ON AT LANDING FLARE. THE GREEN SAFE LIGHT REMAINED ON. THE LANDING WAS COMPLETED WITHOUT INCIDENT. MAINTENANCE REPAIRED BROKEN/CORRODED WIRES AT THE NOSE GEAR DOWN SWITCH BY REPLACING T HE SWITCH. (M) 2 L 7 2 4T RT A24CE 2004011200048 20040112 00048 CE 2004 1 12 2004F00020 1 20021122 A 3297 CONNECTOR BEECH 1900 1900C 1154161 CE DOWNLOCK SWITCH DIRTY A YADA O OTHER P NO WARNING INDICATION LD LANDING 1 AL 03 1566C UC36 AT LANDING IN ANCHORAGE, PILOT REPORTED HAD TO PUMP THE LANDING GEAR HAND PUMP TO RECEIVE A GREEN SAFE NOSE GEAR ILGHT, HANDLE WARNING WAS NOT ILLUMINATED. MAINTENANCE COULD NOT DUPLICATE, CLEANED NOSE GEAR ACTUATOR AND DOWNLOCK SWITCH CON NECTORS, CHECKED NOSE GEAR WIRING AND FROZE SWITCHES. NO FAULTS FOUND. (M) 2 L 7 2 4T RT A24CE 2004011200118 20040112 00118 CE 2004 1 12 2004F00026 1 20021129 A 7603 O-RING BEECH 1900 1900C 1154161 CE THROTTLE DISPLACED A YADA O OTHER O OTHER NR NOT REPORTED 1 AL 03 1566C UC36 RIGHT THROTTLE FROZE AT ALTITUDE. MAINTENANCE FOUND THE NR 2 AIR SEAL, AT CENTER CONSOLE DISPLACED. REPLACED CONTROL A SSEMBLY. (M) 2 L 7 2 4T RT A24CE 2004011200059 20040112 00059 CE 2004 1 12 2004F00023 1 20021224 A 3233 ACTUATOR BEECH 1900 1900C 1154161 CE NLG FAILED A YADA O OTHER P NO WARNING INDICATION LD LANDING 1 AL 03 45GL UC45 ON LANDING IN AKN, NOSE GEAR DOWN AND LOCK LIGHT FAILED TO ILLUMINATE. FERRY TO ANCHORAGE AFTER VERIFYING GEAR DOWN AND LOCKED, GREEN LIGHT CAME ON DURING TAXI OUT. COULD NOT DUPLICATE FAILURE ON GROUND. REPLACED NOSE GEAR ACTUATOR FOR T /S. (M) 2 L 7 2 4T RT A24CE 2004011200161 20040112 00161 NM 2004 1 12 TSAA0253259 1 20021218 A 5310 6546526 WINDOW FRAME BOEING 737 737230 1384401 NM BS CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED 3 EACH FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOW N IN FIGURE 1, MAINTAINING 2D EDGE MARGIN. MAINTAINED A MINIMUM .5 INCH OUTSIDE CORNER RADIUS AND MINIMUM 2.0 INCH INSI DE CORNER RADIUS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF MBS 10-79 TYPE III, PRIMER. INSTALLED FILLERS AND DOUBLERS WITH FASTENERS INDICATED IN FIGURES 1, 2 AND TABLE 1. APPLIED FILLET SEAL OF BMS 5-95 SEALANT AROUND EDGE S OF REPAIR. REPAIR COMPLETED IAW ECO 3250, DEVIATION AI. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2004020400096 20040204 00096 EU 2004 2 4 02FDEA00666 1 20020918 A 2510 HANDLE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE COCKPIT SEAT MALFUNCTIONED A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 650FE 10144 10144 24472 726 ON LANDING AT EWR, AT TOUCHDOWN CAPT'S SEAT RETRACTED FULL DOWN ALL BY IT'S SELF. AFTER TAXI IN SEAT SEEMS TO HOLD OK. WIGGLED VERTICAL HANDLE WHILE IN THE UP POSITION AND SEAT WENT RIGHT DOWN TO FULL DOWN. VERIFIED PROBLEM. MAYBE HANDL E CAN BE ADJUSTED. 2 L 7 2 4F 4 F RT A35EU E13NE 2003112500094 20031125 00094 EA 2003 11 25 HNAA0300070 1 20020530 A 5523 8552003 TAB DHAV DHC8 DHC8311 1386006 EA ELEVATOR DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 328EN 281 REPAIR TO ELEVATOR SPRING TAB TRAILING EDGE. 2 H 7 2 4T RT A13NM 2003121500082 20031215 00082 NM 2003 12 15 PCAA0207141 1 20020720 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DIRTY A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 980HA 376 SYR-FLIGHT 3931. CREW REPORTED EMERGENCY LIGHTS WERE FLICKERING IN FLIGHT AND ON THE GROUND. MAINTENANCE CLEANED THE C ONNECTOR ON THE EMERGENCY LIGHT CONTROL BOX. GROUND RAN AND TAXIED AIRCRAFT, WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2003121900013 20031219 00013 CE 2003 12 19 ACE0124021 1 20020125 A 3297 CONNECTOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE MLG DIRTY E YADA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 1553C UC24 AFTER DEPARTURE FROM ANCHORAGE, THE LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER SELECTING GEAR UP. THE FLIGHT CREW R ETURNED FOR AN UNEVENTFUL LANDING IN ANCHORAGE. MAINT COULD NOT DUPLICATED THE DISCREPANCY WITH THE AIRCRAFT ON JACKS. MAINT CLEANED SYSTEM CONNECTOR PINS AND A SUCCESSFUL OPERATION CHECK FLIGHT WAS PERFORMED. 2 L 7 2 4T 4 T RT A24CE E4EA 2003121900014 20031219 00014 CE 2003 12 19 ACE0102021 1 20020104 A 7931 WIRE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NR 2 ENG OIL IND BROKEN E YADA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 1566C 23717 20912 UC36 AFTER TAKEOFF, NR 2 ENGINE OIL PRESSURE INDICATED (0) UNTIL POWER WAS REDUCED TO 1700 LBS TORQUE. RETURNED TO AIRPORT F OR AN UNEVENTFUL LANDING. MAINTENANCE REPAIRED A BROKEN WIRE AT THE NR ENGINE OIL PRESSURE TRANSMITTER CONNECTOR. 2 L 7 2 4T 4 T RT A24CE E4EA 2003121900016 20031219 00016 CE 2003 12 19 ACE0117021 1 20020118 A 3230 MS24171D1 RELAY BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA MLG BURNED E YADA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 45GL 883 UC45 32601 THE PILOT REPORTED THAT AFTER DEPARTURE FROM HPB, THE LANDING GEAR SELECTOR HANDLE WAS INOPERATIVE AND WOULD NOT RAISE T HE LANDING GEAR. THE FLIGHT CONTINUED, WITH THE GEAR EXTENDED. AN UNEVENTFUL LANDING WAS MADE AND MAINTENANCE REPLACED THE LANDING GEAR POWER PACK CONTROL RELAY DUE TO BURNED CONTACTS. 2 L 7 2 4T 4 T RT A24CE E4EA 2003121900028 20031219 00028 CE 2003 12 19 ACE0318021 1 20020319 A 3260 SWITCH BEECH 1900 1900C 1154161 CE GEAR PWR LEVER OUT OF ADJUST E YADA O OTHER N FALSE WARNING AP APPROACH 1 AL 03 1566C 21528 UC36 ON APPROACH TO LANDING, GEAR WARNING SYSTEM (REDUCED POWER WITH GEAR UP) DID NOT FUNCTION EVEN WITH POWER LEVERS FULLY RETARDED. MAINTENANCE CORRECTED THE PROBLEM BY ADJUSTMENT OF THE POWER LEVER GEAR UNSAFE WARNING MICRO SWITCHES. 2 L 7 2 4T RT A24CE 2003121900029 20031219 00029 EA 2003 12 19 ACE0419021 2 20020419 A 7240 3006505 VALVE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA DRAIN MISMANUFACTURED E YADA K NONE M K W OVER TEMP FLUID LOSS INADEQUATE Q C IN INSP/MAINT 1 AL 03 5632C 33934 UC81 ON ROUTINE INSPECTION, FOUND ENGINE FORWARD AND AFT COMBUSTION CASE DRAIN VALVE LINES OVERHEATED. REMOVED DRAIN VALVES AND INSPECTED FOR CONDITION. DETERMINED THAT BOTH DRAIN VALVES HAD BEEN PREVIOUSLY INSTALLED WITH MISSING INTERNAL COMP ONENTS. A TOTAL OF 118.6 HOURS HAD BEEN ACCUMULATED ON THE ENGINE SINCE INSTALLATION OF THE VALVES. REPLACED BOTH VALV ES WITH COMPLETE ASSEMBLIES, REPLACED DRAIN LINES. A REVIEW OF THE ENGINE IPC DOES NOT SHOW AN ASSY PN FOR THE ENTIRE V ALVE ALL INDIVIDUAL COMPONENTS (FOUR PARTS TOTAL) MUST BE PROCURED AND ASSEMBLED PRIOR TO VALVE INSTALLATION. 2 L 7 2 4T 4 T RT A24CE E4EA 2003121900015 20031219 00015 EA 2003 12 19 ACE0119021 2 20020119 A 7320 3033260 LINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA P3 AIR CRACKED E YADA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION NR NOT REPORTED 1 AL 03 45GL 35125 6680 UC45 32601 FLIGHT CREW REPORTED THAT THE NR 2 ENGINE FLAMED OUT EN ROUTE. ATTEMPTED RESTART WAS UNSUCCESSFUL. THE ENGINE WAS SECU RED AND ACCOMPLISHED UNEVENTFUL LANDING. MAINTENANCE LOCATED A CRACKED P3 ENGINE CONTROL AIR LINE AND REPLACED SAME. M AINTENANCE ALSO DETERMINED THAT AN ANGLE BRACKET (P/N MS9593485) AND LINE CLAMP HAD BEEN MISSING FROM THE ENGINE SINCE T HE LAST ENGINE OVERHAUL. THIS LINE CLAMP WOULD REDUCE VIBRATION AND FATIGUE AT THE POINT OF FAILURE OF THE LINE. THE M ISSING PARTS WERE REPLACED. 2 L 7 2 4T 4 T RT A24CE E4EA 2003121900027 20031219 00027 CE 2003 12 19 ACE0729021 1 20020731 A 7921 1143890005 OIL COOLER BEECH 1900 1900C 1154161 CE ENGINE CRACKED E YADA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 03 45GL 37061 UC45 MAINTENANCE FOUND OIL LEAKING FROM THE RIGHT ENGINE COWLING. INVESTIGATION REVEALED A CRACKED OIL COOLER. OIL COOLER W AS REPLACED. THE REMOVED OIL COOLER WAS INSPECTED AND A CRACK ALONG THE END PLATE WELD SEEM WAS LOCATED. THIS DEFECT I S COMMON WITH THIS PN. OIL COOLER. 2 L 7 2 4T RT A24CE 2003123100024 20031231 00024 NM 2003 12 31 TSAA0229255 1 20021223 A 2913 66087 PUMP BOEING 737 73776N 13844CH NM NR 1 & 2 ENG FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 744AL 32582 NR 2 EDP LOW PRESSURE LIGHT CAME ON 2.5 HOURS INTO FLT. SUSPECT PUMP FAILURE AS PRESSURE FOR SYS 'A' BEGAN DROPPING WHE N NR 2 ENGINE HYD PUMP MOMENTARILY TURNED OFF, DETERMINED NORMAL AFTER EVALUATION. NR 1 EDP LOW PRESSURE LIGHT ILLUMINA TED ABOUT 3.5 HOURS INTO FLT. NR 2 DEP LOW PRESSURE LIGHT ILLUMINATED 4.5 HOURS INTO FLT. DIVERTED TO HNL FOR MAINT & LANDED WITH NO FURTHER INCIDENT. REPLACED NR 1 & NR 2 EDP. REPLACED CASE DRAIN FILTERS FOR NR 1, 2 EDP & NR 2 EMP. AS A PRECAUTION, 'A' & 'B' SYSTEM PRESSURE MODULE & RETURN MODULE FILTERS REPLACED. INCORPORATED EA 700-29-001R1 TO REMO VE 'A' & 'B' SYS DEPRESSURIZATION VALVES FROM HYD SYS. HYD SYS TESTED CHECKED GOOD. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003123100032 20031231 00032 NM 2003 12 31 TSAA0233256 1 20021220 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT INOPERATIVE A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003123100105 20031231 00105 NM 2003 12 31 TSAA0253254 1 20021220 A 5330 6551626 SKIN BOEING 737 737230 1384401 NM FUSLEAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 CUTOUT AND REMOVED DAMAGED PORTION OF SKIN. HFEC INSPECTED THE EDGE OF TRIM. ENLARGED TRIMMED BY .04 INCH INSURANCE CU T. FABRICATED AND INSTALLED A .071 INCH REPAIR FILLER AND .080 INCH DOUBLER FROM CLAD SHEET 2024-T3 MATERIAL IAW SRM 53 -30-3. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-111 TYPE 1 PRIMER. REPAIR COMPLETED IAW ECO 332 5. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2003123100095 20031231 00095 NM 2003 12 31 TSAA0253242 1 20021107 A 5320 654541041 WEB BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 REMOVED EXISTING FASTENERS, STIFENERS, FILLERS, AND DAMAGED SECTION OF WEB AS SHOWN ON FIGURE 5. FABRICATED A .050 INCH THICK REINFORCING DOUBLER FROM 7075-T6. ALODINE AND APPLIED BMS 10-11 TYPE 1 PRIMER TO ALL BARE SURFACES. INSTALLED R E-ENFORCING DOUBLER, WEB, STIFFENERS, AND FILLERS WITH NEW FASTENERS IAW ECO 2223 FIGURE 5 AND FIGURE 7. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2004010900043 20040109 00043 NM 2004 1 9 TSAA0251248 1 20021118 A 5100 65465271 WINDOW FRAME BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED 3 EACH FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOW N IN PHOTO 1, MAINTAINING 2D EDGE MARGIN AND 5D-6D SPACING AT NEW FASTENER LOCATIONS. FINISH ALL BARE ALUMINUM WITH ALO DINE AND TWO COATS OF BMS 10-11 TYPE 1, PRIMER. INSTALLED FILLERS AND DOUBLERS WITH FASTENERS INDICATED IN FIGURES 1, 2 AND TABLE 2. APPLIED FILLET SEAL OF BMS 5-95 SEALANT AROUND EDGES OF REPAIR. REPAIR COMPLETED IAW ECO 3250, DEVIATION AG. WINDOW FRAME P/N 65-465271, 291, 311, 321 AND 65-465491, BS 420, 440, 460, 480 AND 767. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 2004011200028 20040112 00028 NM 2004 1 12 TSAA0253240 1 20021120 A 5311 6547578525 FRAME BOEING 737 737230 1384401 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 BLENDED SURFACE IS SMOOTHLY RADIUSED AND RIDGES BLENDED TO A 10 TO 1 RATIO SPANWISE. VERIFIED CORROSION REMOVED USING N DT METHOD. FLAT PEENED REWORKED AREA. APPLIED ALODINE AND TWO COATS BMS 10-11, TYPE 1 PRIMER TO REPAIR WASHERS AND REW ORKED SURFACE. APPLIED BMS 5-95 SEALANT TO ALL FAYING SURFACES. FILLED BLENDOUT WITH BMS 5-95 SEALANT. VERIFIED 8110- 3 RECEIVED. REPAI COMPLETED IAW ECO 2154R3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2004012600039 20040126 00039 GL 2004 1 26 ERAA091797 2 20021120 A 7313 5233333 FUEL NOZZLE BOLKMS 105 BO105A EU ALLSN 250C 250C20B 03013 GL ENGINE MALFUNCTIONED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 290EH 10480 S850 FUEL NOZZLE STREAKS. ERRODED METER SET. INSTALLED NEW METER SET. 1 G 7 2 3U 3 U H3EU E4CE 2004020400231 20040204 00231 EU 2004 2 4 02FDEA00404 1 20020612 A 5415 FITTING AIRBUS 310 A310 EU ENGINE PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 RT WING PYLON SPIGOT BALL JOINT FOUND WITH BROWN STAIN ALL AROUND THE CIRCUMFERENCE OF FITTING. CLEARED IAW EA 6-5450-5 9029. 2 L 7 2 4F RT A35EU 2004021200025 20040212 00025 CE 2004 2 12 ACE0118021 1 20020125 A 5751 1185210247 YOKE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE AILERON CRACKED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 111AX 33011 28450 UC81 WHILE PERFORMING A SCHEDULED AILERON YOKE INSPECTION, FOUND THE RT AND LT AILERON YOKES CRACKED ON TWO SIDES (TOP AND BO TTOM) OF THE TAPER PIN HOLES, ALONG THE GRAIN OF THE METAL. THE CAUSE OF THE FAILURES WAS NOT EVIDENT.(K) 2 L 7 2 4T 4 T RT A24CE E4EA 2004021200027 20040212 00027 CE 2004 2 12 ACE0531021 1 20020603 A 2730 11452403733 CONTROL CABLE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE ELEVATOR BROKEN E YADA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 AL 03 113AX 36450 UC41 PILOT ATTEMPTED TO ADJUST ELEVATOR TRIM TO REDUCE CONTROL FORCES AND NOTICED THAT TRIM SYS DID NOT FEEL LIKE IT WAS WORK ING NORMAL. AFTER UNEVENTFUL LANDING , PILOT ATTEMPTED TO ADJUST ELEVATOR TRIM, NOTED THAT TRIM WHEEL STARTED TO BIND. BROKEN UPPER ELEVATOR TRIM CNTRL CABLE AT PULLEY BLOCK LOCATED AFT OF CARGO DOOR AT STA 511. INSP OF CABLE REVEALED LA RGE AMOUNT OF PHENOLIC DUST FROM TRIM CABLE PULLEY. EVIDENCE OF CORROSION ON FAILED CABLE AT THE BREAKAGE POINT. OTHER CABLES, ALSO HAD SAME PHENOLIC DUST COVERING WERE INSP AND REPLACED ALL CABLES CONDITION AT THE SAME FUSELAGE STATION ( AFT END OF CARGO FLOOR AT STA 511) ONLY AT THAT LOCATION. SUSPECT FREQUENT DELUGE WITH WATER AS A CAUSE. 2 L 7 2 4T 4 T RT A24CE E4EA 2004021200034 20040212 00034 EA 2004 2 12 ACE1115021 2 20021115 A 7314 RA5326 DIAPHRAGM BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA FUEL PUMP LEAKING C YADA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 03 5632C 2359 B1449 UC45 MAINTENANCE REPLACED THE LOW PRESSURE FUEL PUMP DUE FUEL LEAKING FROM PRESSURE RELIEF PUMP DUE FUEL LEAKING FROM PRESSUR E RELIEF CRANE SB. 101SB023 CONCERNING RELIEF COVER SCREW TORQUES AND LEAKS. POST REMOVAL TEARDOWN REVEALED A RUPTURED CONTROL DIAPHRAGM. THE PUMP HAD BEEN IN SERVICE FOR 9 MONTHS.(K) 2 L 7 2 4T 4 T RT A24CE E4EA 2004021200028 20040212 00028 EA 2004 2 12 ACE1014021 2 20021015 A 7314 PUMP BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENG FUEL MALFUNCTIONED E YADA C D ABORTED TAKEOFF RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 AL 03 1566C 23351 UC36 32245 ON TAKE OFF ROLL, PRIOR TO LIFT OFF, RT ENG EXPERIENCED COMPLETE LOSS OF POWER AND TAKE OFF WAS ABORTED. NR ENGINE SPOO LED DOWN, CREW SECURED IT IAW PROCEDURE. AC RETURNED TO RAMP WITHOUT FURTHER INCIDENT. POST SHUT DOWN INSP DID NOT REV EAL ANY ABNORMALITY AND ENG STATED AND OPERATED TO FULL POWER WITHOUT FAULT. MAINTENANCE REPLACED NR 2 ENG HP FUEL PUMP FOR T/S AND PERFORMED A GROUND RUN. UPON REACHING HIGH THEN RAN SUCCESSFULLY FOR ADDITIONAL TWO RUNS. MAINT REPLACED THE LOW PSI FUEL PUMP FOR T/S AND COMPLETED AN ADDITIONAL SERIES OF SUCCESSFUL RUNS WITHOUT FAULT. INSP OF REMOVED COMP ONENTS DID NOT DISCLOSE ANY OBVIOUS FAULTS.(K) 2 L 7 2 4T 4 T RT A24CE E4EA 2004021200031 20040212 00031 CE 2004 2 12 ACE0225021 1 20020226 A 5260 SHAFT BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE AIRSTAIR HANDLE SHEARED E YADA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 1563C 3403 UC20 AFTER LANDING, THE FLIGHT CREW WAS UNABLE TO OPEN THE FORWARD AIRSTAIR DOOR USING THE INTERIOR HANDLE. THE PILOT WROTE UP THE AIRSTAIR DOOR HANDLE AS INOPERATIVE. MAINTENANCE REPLACED THE INTERIOR DOOR HANDLE ASSEMBLY AFTER FINDING THE SQ UARE HANDLE SHAFT SHEARED EVEN WITH THE BASE OF THE HANDLE. THIS IS THE FIFTH FAILURE OF THIS PN ASSEMBLY IN OUR FLEET IN THE LAST YEAR. 2 L 7 2 4T 4 T RT A24CE E4EA 2004021200033 20040212 00033 CE 2004 2 12 ACE0208021 1 20020209 A 7921 11433890005 OIL COOLER BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE NR 2 ENG OIL CRACKED E YADA O OTHER O OTHER NR NOT REPORTED 1 AL 03 1566C 6779 UC36 PILOT REPORTED THAT, AFTER LANDING, HE OBSERVED ENGINE OIL LEAKING FROM THE NR 2 ENGINE. THE OIL LEVEL WAS VERIFIED TO BE JUST INDICATIONS OF OIL PRESSURE LOSS, FLUCTUATION OR HIGH TEMP. MAINTENANCE REPLACED THE OIL COOLER AND LATER VERIFI ED THAT IT WAS CRACKED (BENCH CHECK VERIFIED LEAK AT A CRACKED ENDI PLATE WELD). (K) 2 L 7 2 4T 4 T RT A24CE E4EA 2004021700090 20040217 00090 SO 2004 2 17 EVA2004F00000 1 20020812 A 2140 BM5172 MOTOR CURTIS C46 C46RCURTIS 2622710 SO HEATER BLOWER SHORTED I EVAB O OTHER O OTHER NR NOT REPORTED 1 AL 01 7848B 1262 273 AFTER COMPLETION OF HOLD ITEMS COCKPIT FILLED WITH LIGHT SMOKE ACCOMPANIED BY ODOR OF ELECTRICAL FIRE. THE SOURCE OF TH E SMOKE WAS FOUND TO BE THE COCKPIT HEATER BLOWER MOTOR WHICH WAS SUBSEQUENTLY REPLACED. 2 L 7 2 4R 3A2 2004030100074 20040301 00074 EU 2004 3 1 AAL2004F00003 1 20020711 A 5730 SKIN AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680 30025 NE WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14061 471 INTERGRANULAR CORROSION IN WING SKIN BETWEEN RIBS 28-29 JUST AFT OF REAR SPAR. AREA WAS BLENDED, FLAP, PEENED AND TREAT ED IAW FSO 30595. 2 L 7 2 4F 4 F RT A35EU E13NE 2004030100057 20040301 00057 CE 2004 3 1 FC52004F00000 1 20020507 A 3213 08412111 RING CESSNA CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO NLG STRUT CORRODED E FC5A K NONE O OTHER IN INSP/MAINT 1 SO 15 77FC 11270 402C0044 PILOTS POST FLIGHT INSPECTION REVEALED DAMAGE TO THE NOSE LANDING GEAR LOWER DOOR LINKAGE. FURTHER INVESTIGATION REVEAL ED THIS DAMAGE CAUSED BY THE NOSE STRUT NOT FULLY EXTENDING AND THE NOSE TIRE FORK STRIKING THE LINKAGE. THIS WAS FOUND TO BE CAUSED BY EXCESSIVE FRICTION BETWEEN THE RING ASSEMBLY AND THE STRUT SHAFT. THE EXCESSIVE FRICTIONS WAS DISCOVER ED TO BE CAUSED BY CORROSION OF THE STEEL RING ASSEMBLY UNDERNEATH ITS PHENOLIC INNER LINER CAUSING ITS INNER DIAMETER T O SHRINK, THUS CLAMPING DOWN ON THE STRUT SHAFT AND NOT ALLOWING EASY EXTENSION OF THE NOSE GEAR STRUT AFTER LIFT OFF. 1 L 7 2 3O 3 O A7CE E8CE 2004031700004 20040317 00004 2004 3 17 249TR0022 4 20020802 A 3420 INDICATOR BOEING 737 7372K5 138448X NM ADI MALFUNCTIONED A PIDA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 05 249TR 22598 BOTH ADI'S HAD SPEED FLAGS WHICH MADE AUTOTHROTTLES INOP. INSTALLED SERVICEABLE ADI IAW 34-22-0, ACCOMPLISHED PDC BITE OF AUTOTHROTTLES PER MM 22-31-01, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2004050700033 20040507 00033 EU 2004 5 7 BAQA094304 1 20020326 A 2810 0319738340 MANIFOLD UROCOP EC135 EC135T1 5620026 EU FUEL SYSTEM UNSERVICEABLE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 511ME 194 0143 WARRANTY. ENG S/N 30178. MANIFOLD DUE TIME CHANGE. ABOVE INFORMATION REFLECTS TIMES AT 03/06/2002. BELINDA WILL CRED IT OUTSTANDING ACCOUNT. REPLACED WITH SERVICABLE UNIT. 04/30/2004 1 G 7 2 3U H88EU 2004052000213 20040520 00213 SO 2004 5 20 ZIAA04058 1 20020920 A 5310 8001881 DOOR FRAME LKHEED 188 188C 5262604 SO FUSELAGE CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 1146 YIP - INVESTIGATE X-RAY INDICATIONS AT 2 RIVETS MARKED IN RED ON OUTER SURFACE OF AFT LOWER CARGO DOOR, LOWER FORWARD CO RNER. REMOVED REPAIR DOUBLERS TO INVESTIGATE FUSELAGE SKIN. FOUND EXISTING CRACK WAS STOP DRILLED PER L-188 SRM 53-2-1 , FIG 2, SHEET 6. REINSTALLED REPAIR DOUBLERS IAW L-188 SRM 52-2-1, FIG 2, SHEET 6. (M) 2 L 7 4 4T 4A22 2004061400232 20040614 00232 NM 2004 6 14 RYN76391A 1 20021019 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D5 52046 NE FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7639U 19912 DURING A SCHEDULED INSPECTION, FOUND BULGE IN SKIN AND APPROXIMATELY 2.5 INCH HORIZONTAL CRACK AT STA 1020, STRINGER 26R . 2 L 7 3 4F 4 F A3WE E2EA 2004061400245 20040614 00245 NM 2004 6 14 RYN76393A 1 20021019 A 5343 SUPPORT BEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D5 52046 NE MLG CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7639U 19912 DURING SERVICE CHECK, FOUND CRACK ON LT MAIN LANDING GEAR SUPPORT BEAM, OB ATTACH LUGS AT UPPER LOCK BOLT LUG. 2 L 7 3 4F 4 F A3WE E2EA 2004061400246 20040614 00246 NM 2004 6 14 RYN764543 1 20020820 A 5347 SEAT TRACK BOEING 727 727222 1384073 NM PWA JT8 JT8D1 52044 NE MISMANUFACTURED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7645U 20039 AT (C) CHECK, FOUND CABIN SEAT TRACK TWO INCHES SHORTER THEN ORIGINAL CONFIGERATION AT STA 1110 TO 1130, RBL 22. 2 L 7 3 4F 4 F A3WE E2EA 2004061400248 20040614 00248 NM 2004 6 14 RYN76392A 1 20021019 A 5320 INTERCOSTAL BOEING 727 727222 1384073 NM PWA JT8 JT8D5 52046 NE FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7639U 19912 DURING A SCHEDULED INSPECTION, FOUND RT AFT FUSELAGE TAIL HAS 1 INTERCOASTAL WITH A CRACK RUNNING FROM THE UPPER AFT COR NER APPROXIMATELY 1.125 INCH IN LENGTH. 2 L 7 3 4F 4 F A3WE E2EA 2004061400251 20040614 00251 NM 2004 6 14 RYN764511 1 20020824 A 5230 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D1 52044 NE C3 DOOR DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7645U 20039 AT C-CHECK, FOUND C-3 UPPER FORWARD DOOR SKIN CREASED AT STATION 1148. 2 L 7 3 4F 4 F A3WE E2EA 2004061400261 20040614 00261 NM 2004 6 14 RYN764544 1 20020819 A 5347 SPLICE BOEING 727 727222 1384073 NM PWA JT8 JT8D1 52044 NE SEAT TRACK FAILED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7645U 20039 AT (C) CHECK, FOUND SEAT TRACK SPLICE NOT REPAIRED IAW THE SRM AT STA 1110, RBL 44. 2 L 7 3 4F 4 F A3WE E2EA 2004080300003 20040803 00003 CE 2004 8 3 0129AAA 1 20021201 A 3260 41EN16 SWITCH BEECH MU300 400A 1155402 CE MLG BROKEN E DJFA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 23 471CW RK161 AIRCRAFT DEPARTED TRENTON, LANDING GEAR RETRACTION RED LIGHT STAYED ON AFTER GEAR WAS RETRACTED. AIRCRAFT RETURNED TO TR ENTON, MAINTEANCE CHANGED LANDING GEAR OPEN SWITCH AND OPS CHECKED OK. 2 H 7 2 4F RT A16SW 2004080900104 20040809 00104 2004 8 9 DL76G040715 4 20020804 A 2565 251009201 SLIDE BOEING 767 7673P6 1385105 NM LT OVERWING UNSERVICEABLE A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 152DL 24984 LEFT WING OVERWING SLIDE DEPLOYED DURING TAXI FROM HANGAR TO LINE. REPLACED DOOR ACTUATOR. 2 L 7 2 4F RT A1NM 2004081300004 20040813 00004 EU 2004 8 13 HAEA0008 1 20020103 A 3230 LANDING GEAR AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE INTERMITTENT E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 204TW 204 GEAR DOOR WOULD NOT INDICATE UP. AIRCRAFT FERRIED TO ADS FOR MAINTENANCE. AIRCRAFT JACKED AND GEAR SWUNG COULD NOT DUP LICATE PROBLEM AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A7EU E7EA 2004090200152 20040902 00152 EA 2004 9 2 2004F00258 2 20021206 A 7320 3244755222118 FUEL CONTROL BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA ENGINE MALFUNCTIONED A ENHA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 03 90PB BB125 PCE80262 DURING CRUISE FLIGHT, WOULD NOT DEVELOP POWER, THE ENGINE WAS SHUTDOWN AND SECURED PER PUBLISHED EMERGENCY PROCEDURE. T HE AIRCRAFT LANDED AT ANCHORAGE INTERNATIONAL AIRPORT WITHOUT FURTHER INCIDENT. THE CAUSE OF THE POWER LOSS WAS DETERMI NED TO BE POSSIBLE FCU INTERNAL MALFUNCTION. THE FCU WAS REPLACED WITH '0' TSO UNIT. AS A FURTHER PRECAUTION THE HIGH PRESSURE PUMP WAS ALSO REPLACED WITH '0' TSO COMPONENT. THE AIRCRAFT WAS GROUND RUN AND ENGINE TRIM ADJUSTED. NO FURTH ER ENGINE OPERATIONAL PROBLEMS WRE ENCOUNTERED, ENGINE RUN-UP CHECKS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 L 7 2 4T 4 T A24CE E4EA 2004091400049 20040914 00049 NM 2004 9 14 375PA0024 1 20020717 A 3350 LENS BOEING 737 737317 138447P NM GE CFM56 CFM563B1 13802 NE EMERGENCY LIGHT LOOSE A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 375PA 23812 FWD EMERGENCY FLOOR TRACK LIGHT LENS LOOSE AND INOP. INSTALLED NEW EMERGENCY LIGHT FLOOR ASSY. IAW 737-300 MM 33-51-81. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091400050 20040914 00050 NM 2004 9 14 375PA0026 1 20020829 A 3350 BULB BOEING 737 7373Y0 1384671 NM GE CFM56 CFM563B1 13802 NE EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 375PA 23812 SEVERAL EMERGENCY FLOOR LOCATOR LIGHTS INOPERATIVE. REMOVED AND REPLACED 3 LAMPS. RECONNECTED WIRING ON 2 LIGHT ASSY. ALL OPS CHECK NORMAL IAW AMM 33-50-81. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091400051 20040914 00051 NM 2004 9 14 375PA0025 1 20020829 A 3350 BATTERY PACK BOEING 737 7373Y0 1384671 NM GE CFM56 CFM563B1 13802 NE EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 375PA 23812 EMERGENCY EXIT LIGHT ABOVE R2 DOOR AND LOWER RT OF L2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW 33-51--51 . OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004101400100 20041014 00100 NM 2004 10 14 DL73G040937 1 20020930 A 5610 5893543135 WINDSHIELD BOEING 737 73735B 13844BM NM COCKPIT CRACKED A DALA O OTHER M OVER TEMP CR CRUISE 1 SO 27 221DL 23970 L1 WINDOW SHATTERED IN FLIGHT. REPLACED WINDSHIELD. 2 L 7 2 4F RT A16WE 2004102800028 20041028 00028 NM 2004 10 28 PIDA375PA02 1 20020829 A 3350 BATTERY PACK BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 375PA 23812 EMERGENCY EXIT LIGHT ABOVE R2 DOOR AND LOWER RIGHT OF L2 DOOR INOP. R&R BATTERY PACK IAW 33-51--51. OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 2004110100137 20041101 00137 NM 2004 11 1 2004UALA00959 1 20021015 A 2910 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYD SYSTEM ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 663UA 27160 RT PRIM HYD OVERHEAT EICAS AND LIGHT. RIGHT HYDRAULIC QUANTITY DROPPED TO ZERO. RIGHT ENGINE DRIVEN PUMP REPLACED. FAI LURE DUE TO FROZEN BEARINGS, PUMP OVERHEATED DUE TO LACK OF LUBRICATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110800116 20041108 00116 CE 2004 11 8 DJFA200200001 1 20021212 A 3231 SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE MLG DOOR OUT OF ADJUST E DJFA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 23 866CW 258466 AIRCRAFT ON LANDING HAD LEFT HAND MAIN GEAR UNSAFE LIGHT, BUT ALSO HAD A GREEN LOCK LIGHT AT THE SAME TIME. CREW DECLAR ED AN EMERGENCY AND LANDED WITH NO PROBLEM. THE LANDING GEAR WAS REPAIRED BY ADJUSTING THE LEFT MAIN LANDING GEAR DOOR SWITCH. 2 L 7 2 4F RT A3EU 2004110800118 20041108 00118 CE 2004 11 8 0227 1 20021130 A 2430 GCU BEECH 200 B200 1152922 CE LT GENERATOR MALFUNCTIONED E DJFA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 23 605TA BB1708 LOST LEFT GENERATOR IN FLIGHT. COULD NOT RESET. AIRCRAFT DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. COULD NOT DUPLI CATE PROBLEM ON THE GROUND, SWAPED GCU GROUND RAN AND TEST FLEW AIRCRAFT WITH NO FURTHER PROBLEMS. 1 L 7 2 4T A24CE 2005041400039 20050414 00039 NE 2005 4 14 ASMF200502012 2 20020222 A 7200 COVER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RT ENGINE MISSING W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 751RA 49779 725567 DURING TRANSIT CHECK WAS DETECTED RIGHT ENGINE WITH COVER MISSING IN SECONDARY FLOW FAIRING. THE COVER WAS REMOVED AND THE RIGHT ENGINE WAS CHECKED BEING ON OPERATION AT LIMITS IAW P&W MM 72-00-00, INSPECTION CHECK 01 PAGE 649 ITEM 2. THE COVER WAS INSTALLED, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2006011300130 20060113 00130 EU 2006 1 13 UPS05145889 1 20021222 A 2910 HYDRAULIC LINE AIRBUS A300 A300F4622R 3930360 EU PWA 4158 PW4158 NE GREEN SYS RESERV BROKEN A IPXA K NONE K FLUID LOSS CR CRUISE 1 SO 01 121UP 0806 INSPECTION TYPE: N/A GREEN SYS RSVR LOW LEVEL WARNING CAME ON IN FLT FOLLOWED ALL ECAM PROCEDURES AND CHECK LIST. **** SUPPLEMENTAL MRR **** REPAIRED HYD LINE NEAR GREEN SYS SERVO CONTROL UNIT IAW M/M 20-23-11-0. LEAK CHECKS OK. SERVICED GREEN SYSTEM RES. 2 L 7 2 4F 4 F RT A35EU E24NE 2006011700281 20060117 00281 NM 2006 1 17 DL76L050816 1 20021222 A 2410 755359B TRANSMISSION 241002334 BOEING 767 767332 1382001 NM NR 1 ENGINE FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 199DN G0637 28456 NA LEFT GEN DRIVE LT ON, REPLACED IDG PER AMM. 2 L 7 2 4F RT A1NM 2005072200204 20050722 00204 EU 2005 7 22 YENA200206 1 20020226 A 3350 OL815BPR LAMP AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT INOPERATIVE A YENA O OTHER L NO TEST TX TAXI/GRND HDL 1 EA 15 509JB 1270 EMERGENCY LIGHT AT SEAT 14C INOPERATIVE. ITEM ON MEL 33-50-03 AS PART IS NIS. 2 L 7 2 4F RT A28NM 2005121900004 20051219 00004 NM 2005 12 19 QXEA200501777 1 20021211 A 5101 CLAMP BOMBDR DHC8 DHC8402 1390042 NM PK BRAKE ACCUM LOOSE A QXEA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 NM 09 401QX 4031 SEA FLIGHT NR 2334: ON TAXI, FA HEARD LOUD GROWL SOUND AROUND ROW 12 AND BACK. ON PARKING, TURNED OFF PTU AND SOUND WEN T AWAY. MAINTENANCE FOUND PARK BRAKE ACCUMULATOR (MOUNTED UNDER PTU) CLAMPS LOOSE. TIGHTENED CLAMPS. RAN PTU, NOTICEA BLE NOISE DROP IN PTU OPERATION. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005121500136 20051215 00136 NM 2005 12 15 2005UALA01416 1 20020114 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE STA 480 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 FOUND STA 480 FLOORBEAM IS DAMAGED. 2 L 7 2 4F 4 F RT A16WE E2GL 2006050800083 20060508 00083 NM 2006 5 8 AWXA200600746 1 20021220 A 5415 112N70092 BUSHING BOEING 757 7572G7 1384963 NM NR 2 PYLON MIGRATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 24523 DISCREPANCY WAS "RT WING NR 2 ENGINE PYLON UPPER LINK, FRONT SPAR ATTACH O/B LUG BUSHING IS MIGRATED O/B LUG I/B BUSHING APPROX .040"". MAINTENANCE PLACED ITEM ON MONITOR TO BE REINSPECTED EVERY 3000 CYCLES AND TO TERMINATE IN 12,000 CYCLE S IAW AWA ER 19-5449-99349-BA1. MONITOR WAS CLEARED ON 26APR06 (TT 61692, TC 23571) IN GYR. MAINTENANCE REMOVED AND RE PLACED THE UPPER LINK, OUTBOARD LUG, INBOARD LUG BUSHING IAW AWA EO 54-40-10. 2 L 7 2 4F RT A2NM 2007030900032 20070309 00032 CE 2007 3 9 DJFA2006370 1 20021130 A 2434 GENERATOR BEECH 200 B200 1152922 CE PWA PT6 PT6* 52043 EA LEFT UNKNOWN E DJFA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 23 605TA BB1708 LOST LT GENERATOR IN FLIGHT, COULD NOT RESET. AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. COULD NOT DUPLICATE PROBLEM ON THE GROUND, SWAPPED GCU GROUND RAN AND TEST FLEW AIRCRAFT WITH NO FURTHER PROBLEMS. 1 L 7 2 4T 3 T A24CE E2NE 2007030900002 20070309 00002 CE 2007 3 9 DJFA2006371 1 20021201 A 3260 41EN16 SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LANDING GEAR BROKEN E DJFA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 23 471CW RK161 AIRCRAFT DEPARTED, LANDING GEAR RETRACTION RED LIGHT STAYED ON AFTER GEAR WAS RETRACTED. AIRCRAFT RETURNED TO DEPARTURE. MAINTENANCE CHANGED LANDING GEAR OPEN SWITCH AND OPS CHECKED OK. 2 H 7 2 4F 4 F RT A16SW E25EA 2007041200123 20070412 00123 NM 2007 4 12 AT0700027 1 20020706 A 5312 BULKHEAD BOEING 717 717200 1383700 NM BS 37 BENT A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 940AT 55004 FUSELAGE STA 37 BULKHEAD WEB AND FLANGE ARE BENT ON LEFT EDGE BETWEEN LONGERON 18L AND NLG WHEEL WELL CUTOUT. INSTALLED FRAME SECTION AND SPLICE AT FUSELAGE BS 37 BETWEEN LONGERON 18L AND MLG WHEEL WELL PER RES NUMBER 02-0547 AND B717 SRM 53-10. MATERIAL USED 7075-T6 .050, 26 X 4 INCH FRAME AND 7075-T6 .063, 3.5 X 1 INCH (SPLICE PLATE). 2 L 7 2 4F TR A6WE 2007041700293 20070417 00293 NM 2007 4 17 AT0700044 1 20020606 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 944AT 55007 FUSELAGE SKIN IS DENTED AT APPROX FS 260, LONGERON 17 LEFT. DENT IS 2 IN X .050. CONDITION FOUND TO BE 1B PER B717 SRM 06-00-07 PG 213. ACCOMPLISHED HIGH FREQ PER NDT SPM 06-00-07. INSTALLED DOUBLER REPAIR AT FS 260 LONGERON 17L IAW B71 7 SRM 53-00-01. MATERIAL USED 2024T3 .050 FOR FILLER SIZE 35.625" X 14", 2024 T3 .063 FOR DOUBLER SIZE 34.5" X 15.5" AN D 2024 T3.0225 FOR FINGER DOUBLER SIZE 41" X 16.5". 2 L 7 2 4F TR A6WE 2007070200190 20070702 00190 NM 2007 7 2 ZZDA020920181 1 20020920 A 2150 CHECK VALVE BOEING 717 717200 1383700 NM BULKHEAD DAMAGED A ZZDA O OTHER J WARNING INDICATION CR CRUISE 1 SO 15 942AT 55005 RIGHT PAC FLOW DISAGREE ALERT CAME ON IN FLT (HISTORY). FOUND RIGHT BULKHEAD CHECK VALVE FLAPPER DAMAGED AND STUCK CLOS ED. REPLACED FLAPPER AND END ASSY IAW MM 21-20-01, OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 2002052300053 20020523 00053 2002 5 23 VW3R200200004 4 20020408 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT FAILED B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R327 ELT NOT TRANSMITTING AND NEEDS TO BE REPLACED. 2002030700062 20020307 00062 2002 3 7 2002F00148 4 20020306 A 3451 535438202 PRINTED CKT BOAR COCKPIT FAULTY B O OTHER J WARNING INDICATION IN INSP/MAINT 1 NM 01 832 396 396 REMOVED FROM A/C AS THE CB POPPED. UPON TEAR DOWN DISCOVERED THE DME PCB (P/N 53543-820-2) HAD OBVIOUS INTERNAL PROBLEM S. RESISTOR AT LOCATOR R915 SHOWS OVERHEATING AND RESISTOR AT LOCATOR R907 WAS COMPLETELY BURNT WITH BOARD MATERIAL (SE VERAL LAYERS) IMMEDIATELY UNDER RESISTOR LOCATION BURNT. 2002040500026 20020405 00026 GL 2002 4 5 2002F00361 3 20020403 A 6110 D50172 LATCH MCAULY 5JFR36 B5JFR36C1103 GL PROPELLER CRACKED B K NONE O OTHER IN INSP/MAINT 1 GL 03 9945 970396 LATCH PAWL CRACKED ON TOP EDGE. 6 C P15NE 2003011400196 20030114 00196 EA 2003 1 14 CA021204011 2 20021128 A 7230 ENGINE PWA PT6 PT6A41 52043 EA ENGINE FAILED W O OTHER E VIBRATION/BUFFET LD LANDING 1 CA 12615 (CAN) ENGINE RECENTLY OVERHAULED AND WAS BEING USED AS A RENTAL WHEN REPORTED ENGINE MAKING NOISE AND HIGH VIBRATION AFT ER LAST LANDING. ENGINE HAS BEEN REMOVED AND SENT IN FOR INVESTIGATION AND REPAIR. COMPRESSOR ASSY WAS OUT OF BALANCE & COMPRESSOR BOLT STRETCH WAS UNEVEN. 2ND STAGE COMPRESSOR DISK & DOWNSTREAM SPACER LOOSE FIT, DISK DIAMETER WAS REPAIRED AT LAST OVERHAUL. AIR-SEAL STATORS & ROTORS HAD HEAVY RUB DAMAGE. ALL STATIONARY PART RUB DAMAGE WAS LOCATED AT 6 O'CLOC K POSITION. DISK-SPACER TIGHT FIT WAS RESTORED, DEFECTIVE AIR SEAL PARTS WERE REPLACED, COMPRESSOR WAS ASSEMBLED AND BALANCED AND ENGINE WAS TESTED PER OVERHAUL MANUAL WITH GOOD PERFORMANCE RESULT AND ACCEPTED FOR RETURN TO SERVICE. 4 T E4EA 2002071100093 20020711 00093 2002 7 11 HEEA079958 4 20020603 A 2200 BRAKE PITCH ACTUATOR MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 AUTOPILOT WOULD DROP OFF LINE AND SOMETIMES WOULD NOT PASS THE PRE-FLIGHT TEST DUE TO THE LINEAR PITCH ACTUATOR BRAKE NO T WORKING PROPERLY. WOULD NOT LOCK UNTIL TAPPED OR BUMPED. 2006081500121 20060815 00121 2006 8 15 CEVR003 4 20021227 A 2562 WABH12 BATTERY EAAEROMARINE KSE35L8 LIFE PRESERVER BURST B CEVR K NONE O OTHER IN INSP/MAINT 1 GL 03 107158 DURING THE YEARLY INSPECTION OF THE LIFE VEST, THE WATER ACTIVATED BATTERY FOR THE LOCATING LIGHT HAD EXPANDED & BURST O PEN. THIS MADE THE LIGHT INOPERABLE. ACCORDING TO THE E.A.M SERVICE INFORMATION SIL-25-104 ,THIS VEST COULD HAVE A INSPE CTION INTERVAL OF FIVE YEARS, WHICH MEANT THE LIGHT COULD HAVE BEEN INOPERATIVE FOR FOUR YEARS. 2002071800122 20020718 00122 EA 2002 7 18 CA020702004 2 20020614 A 7230 ENGINE PWA PT6 PT6A41 52043 EA NACELLE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE ENGINE WAS SENT TO ATI FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED COMPRESSOR FOD. THE ENGINE WAS DISASSEMBLED & THE COMPRESSOR ROTOR ASSY WAS DETACHED FROM THE GG CASE.AFTER DE-MATING THE ENGINE COMPRESSOR ITWAS APPA RENT THA THE ROTOR BLADES & THE COMPRESSOR STATORS WERE DAMAGED.1) 1ST STAGE ROTOR HAD ONE BLADE WITH FOD 2) 1ST STAGE S TATOR HAD SOME VANES WITH MINOR FOD 3) PT BLADES WERE SOMEWHAT LOOSE IN ITS PLACE - WITH MINOR AXIAL MOVEMENT.ATI CONCLU DED THAT A FOREIGN OBJECT CAUSED THE DAMAGE TO THE COMPRESSOR BLADES AND VANES. THE PT BLADES AXIAL PLAY INDICATES THAT AXIAL PROTRUSION COULD OCCUR & IT WAS FELT PRUDENT TO RE-RIVET THE PT BLADES. 4 T E4EA 2002121100002 20021211 00002 NE 2002 12 11 CA021120003 2 20021106 A 7250 BLADE PWA PT6 PT6A67D NE ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 15459 (CAN) A PRIMARY FAILURE OF ONE OR MORE 2ND STAGE PT BLADES. EXTENSIVE SECONDARY DAMAGE RESULTED, INCLUDING THE PT STATOR HOUSING, THE EXHAUST DUCT, BOTH FIRST & SECOND STAGE STATOR ASSEMBLIES, BOTH 1ST & 2ND STAGE PT DISK & BLADE ASSEMBLIES , THE PT SHAFT & HOUSING & BOTH NR 3 & 4 BEARINGS.ATI HAS CONCLUDED THAT THE ENGINE SUFFERED FROM 2ND STAGE POWER TURBIN E BLADE FAILURE. 4 T E26NE 2002020700065 20020207 00065 2002 2 7 MALA020134 4 20020101 A 2310 RADIO COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 590XJ DURING FLIGHT 3020, NR 1 COMM RADIO IS INOP AFTER TAKEOFF. AIR RETURN TO MSP. MAINTENANCE COULD NOT DUPLICATE. NR 1 C OMM SYSTEM OPS CHECK GOOD IAW SF340 AMM CHAP 23. 2003013000032 20030130 00032 NE 2003 1 30 CA021209004 2 20020714 A 7250 810641 BEARING PWA JT9 JT9D7R4D 52054 NE NR 3 FAILED W A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CA (CAN) IN FLIGHT DIVERTION, DUE TO OIL BY-PASS WARNING LIGHT AND LOW PRESSURE. EVIDENCE OF METAL FOUND GROUND RUN DONE, E NGINE FAILED. 4 F E3NE 2002121100001 20021211 00001 NE 2002 12 11 CA021120002 2 20021106 A 7250 SEAL PWA PT6 PT6A67D NE ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 11592 (CAN) ENGINE SUSTAINED AN INTERSTAGE SEAL FAILURE, ROTOR AND STATOR AIR SEAL SUFFERED EXTENSIVE DAMAGE AND LOSS OF COMP ONENT INTEGRITY, RESULTING IN EXTENSIVE SECONDARY IMPACT DAMAGE TO MANY OTHER POWER TURBINE ROTOR COMPONENTS.THE OUTSIDE OF THE POWER TURBINE SHAFT HOUSING & THE REDUCTION GEARBOX REAR HOUSING WERE COVERED WITH OIL AND COKED OIL.THERE WAS A T LEAST ONE CRACK EMANATING FROM ONE OF THE AIR SUPPLY HOLES IN THE SEAL RUNNING REARWARDS INTO THE CIRCUMFERENTIAL FRAC TURE ZONE. 4 T E26NE 2003032800073 20030328 00073 2003 3 28 CEVR004 4 20021227 A 2562 WABH12 BATTERY EAAEROMARINE KSE35L8 LIFE PRESERVER BURST B CEVR K NONE O OTHER IN INSP/MAINT 1 GL 03 62227 DURING THE YEARLY INSPECTION OF THE LIFE VEST, THE WATER ACTIVATED BATTERY FOR THE LOCATING LIGHT HAD EXPANDED & BURST O PEN. THIS MADE THE LIGHT INOPERABLE. ACCORDING TO THE EAM SERVICE INFORMATION SIL-25-104 ,THIS VEST COULD HAVE A INSPEC TION INTERVAL OF FIVE YEARS, WHICH MEANT THE LIGHT COULD HAVE BEEN INOPERATIVE FOR FOUR YEARS. 2002050600112 20020506 00112 NE 2002 5 6 2002F00439 3 20020416 A 6111 D5133 BLADE HARTZL HCE4A HCE4A3I NE PROPELLER CRACKED B K NONE O OTHER IN INSP/MAINT 1 GL 03 13080 4594 HJ383 LEADING EDGES CRACKED ON TWO BLADES. 5 C P10NE 2002030800049 20020308 00049 WP 2002 3 8 CA020206003 2 20020118 A 7322 89778017 FUEL CONTROL GARRTT TPE331 TPE33110UA 01514 WP ENGINE MALFUNCTIONED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON COMPLETION OF THE FIRST LEG OF A 3 LEG JOURNEY THE ENGINE WAS SHUT DOWNFOR APPROXIMATELY 15 MINUTES. WHEN THE NEXT START WAS ATTEMPTED THE FUEL FLOW WENT OVER 100 PPH. AND THE EGT WENT TO MAX START TEMP BY 18 PERCENT RPM THE STA RTWAS ABORTED. THIS WAS ATTEMPTED SEVERAL TIMES WITH OVER FUELING ON EACH ATTEMPT. THE FUEL CONTROL WAS REPLACED THIS CORRECTED THE PROBLEM. 4 T E4WE 2002081200033 20020812 00033 NE 2002 8 12 CA020724008 2 20020528 A 7250 CASE PWA JT15 JT15D4 52112 NE GAS GENERATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) REMOVED ENGINE FROM A/C AFTER DAMAGE FOUND ON HP TURBINE BLADES AT BORESCOPE INSP. ENGINE REMOVED FOR INVESTIGATI ON & OVERHUAL.WHEN LOW TURBINE SUPPORT ASSY & COMBUSTION LIN ER WERE REMVD, APPROX ONE HALF OF DEFLECTOR SEGMENTS FELL T O BOTTOM OF GAS GEN CASE. DEFLECTOR SUPPORT RING MISSING APPROX 1/4 OF ITS CIRCUMFERENTIAL AREA & LARGE NO OF RETAINING RIVETS WERE MISSING.THE ENDS OF FISHTAILS OF GAS GEN CASE WERE ALL HEAVILY DAMAGED WITH EXTENSIVE FRETTING, CRACKING & MISSING MATERIAL.THE LOW TURBINE SUPPORT ASSY HAD MINOR WEAR MARKS AT LOCATION OF BROKEN DEFLECTOR SEGMENTS. NO DAMAGE U P STREAM OF THE DIFFUSER TUBES IN GAS GEN CASE 4 F E1NE 2002080800073 20020808 00073 NE 2002 8 8 AUS20020633 2 20020624 A 7210 311292301 CASE PWA PT6 PT6A42 52043 NE ENG RGB CORRODED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) ENGINE REDUCTION GEARBOX REAR CASE CORRODED BEYOND LIMITS. PAINT HAD BEEN STRIPPED FROM CASE FOR INSPECTION WHEN T HE CORROSION WAS FOUND. 4 T E4EA 2002052300051 20020523 00051 2002 5 23 VW3R200200002 4 20020311 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT FAILED B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R430 ELT NOT TRANSMITTING AND NEEDS TO BE REPLACED. 2002103000008 20021030 00008 EA 2002 10 30 CA021010010 2 20020926 A 7230 ENGINE PWA PT6 PT6A50 52043 EA FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ENGINE WAS SENT TO ATI FOR INVESTIGATION AFTER THE OPERATOR COMPLAINED OF COMPRESSOR WHINING AND COMPRESSOR STALLS AT HIGH POWER SETTINGS. A T-5 INDICATION PROBLEM AT START-UP AND THE FUEL PUMP IS LEAKING FROM THE DRAIN.ATI WILL RESTO RE THE ENGINE TO SERVICEABILITY, INCLUDING THE DIMENSIONAL CHECK OF EVERY COMPRESSOR COMPONENT, THE REPLACEMENT OF THE N R 1 AND 2 BEARING AND ALSO ALL THE COMPRESSOR THE RODS, ALL OTHERE DAMAGED, WORN OR FRETTED COMPONENT WILL BE REPAIRED A S NECESSARY TO RETURN THE ENGINE TO A SERVICEABLE STATUS. 4 T E4EA 2002052300054 20020523 00054 2002 5 23 VW3R200200005 4 20020419 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT FAILED B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R414 ELT NOT TRANSMITTING AND NEEDS TO BE REPLACED. ELT CASE BROKEN OFF BATTERY. 2002121100013 20021211 00013 EA 2002 12 11 CA021122001 2 20021108 A 7230 304865101 COMPRESSOR WHEEL PWC 150 PW150A EA ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) 1ST STAGE COMPRESSOR ROTOR EXHIBITED A PREMATURE .500 INCH LONG CRACK AT THE AIRFOIL LEADING EDGE ROOT RADIUS. WHA T WE BELIEVE TO BE A FATIGUE CRACK HAPPENED AT 3426.4 SERVICE HOURS AND 4343 CYCLES. 4 T E00062EN 2002030700005 20020307 00005 2002 3 7 AUS20020080 4 20020130 A 2565 D31354418 LANYARD 61620468 ESCAPE SLIDE INCORRECT W K NONE O OTHER IN INSP/MAINT 1 AU S 0584 (AUS) ESCAPE SLIDE LANYARD INCORRECT LENGTH. 2002053100129 20020531 00129 2002 5 31 0201683230 4 20020515 A 2565 60592101 RESERVOIR LEFT BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 330NW 35684 794 00307 DURING 'L' CHECK, FOUND THE LEFT ESCAPE SLIDE CYLINDER CONTROL CABLE BROKEN. REPLACED THE LEFT ESCAPE SLIDE CYLINDER CONTROL CABLE RESERVOIR. OPERATIONAL CHECK GOOD.\N\N\NMANUFACTURER: AIRBUS\NMODEL: A319114 2003013000033 20030130 00033 NE 2003 1 30 CA021209006 2 20021001 A 7250 810641 BEARING PWA JT9 JT9D7R4D 52054 NE ENGINE FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) ON MAINTENANCE CHECK, METAL FOUND IN FILTER, ENGINE TESTED AND ENGINE FAILED DUE TO OIL BYPASS LIGHT ON AND LOW OI L PRESSURE FAILURE OF NR 3 BEARING, SAME REPAIR STATION OVERHAULED THIS BEARING. 4 F E3NE 2002091800062 20020918 00062 WP 2002 9 18 CA020906002 2 20020731 A 7230 31071104 IMPELLER GARRTT TPE331 TPE33111U 01514 WP COMPRESSOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FIRST STAGE IMPELLER DAMAGE. THE ENGINE WAS REMOVED DUE TO A CRACK IN THE FIRST STAGE IMPELLER WHICH WAS NOTICED THROUGH THE INLET COWL. THE IMPELLER WAS REMOVED AND A COMPLETE DOD INSPECTION ACCOMPLISHED. 4 T E4WE 2002052300050 20020523 00050 2002 5 23 VW3R200200001 4 20020308 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT FAILED B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R478 ELT NOT TRANSMITTING AND NEEDS TO BE REPLACED. 2002112600074 20021126 00074 NE 2002 11 26 RO751005 2 20021123 A 7200 216109064 HOUSING LYC LF507 LF5071F NE COMBUST CHAMB RUPTURED B K NONE O OTHER IN INSP/MAINT 1 WP 07 LF07509 UPON UNSUCCESSFUL COMPLETION OF TESTING IN AN ENGINE TEST CELL, THE COMBUSTOR HOUSING OF THE ENGINE WAS FOUND TO BE PART IALLY RUPTURED AT THE HAZ OF A WELD JOINT FOR THE 6 O'CLOCK BLEED PORT. THE RESULTING CRACK IS OPEN AND RUNS APPROXIMAT ELY 5 INCHES. THE ENGINE WAS BEING REMOVED AFTER FAILING FUNCTIONAL TEST FOR HIGH FUEL FLOW. REPORTEDLY, BURN MARKS WE RE EVIDENT ON THE ENGINE COWLING FROM THE HOT GAS LEAK. THE HOUSING WAS REMOVED FROM ENGINE 7509, INSPECTED PER THE MAI NTENANCE LEVEL CRITERIA OF THE ENGINE MANUAL, UT INSPECTED PER S/B 72-1071, AND REISSUED TO ENGINE 7509. ENGINE IS OWNE D AND OPERATED BY SWISS AIR AND WAS BEING REPAIRED BY HONEYWELL, PHOENIX R&O, FOR MRB INSPECTION AND HIGH TGT. 4 F E6NE 2002091800052 20020918 00052 EA 2002 9 18 CA020905006 2 20020826 A 7200 ENGINE PWA PT6 PT6A41 52043 EA LT OR RT FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) THE ENGINE WAS SENT TO ATI FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED THAT ENGINE WAS SHUT DOWN IN F LIGHT.THE OPERATOR REPORTED THAT DURING THE FLIGHT THE PILOT HEARD A LOUD BANG FOLLOWED BY POWER LOSS AND EXTREME RISE I N ITT. THE PILOT SHUT DOWN THE ENGINE AND CONTINUED THE FLIGHT ON ONE ENGINE. ON LANDING THE OPERATOR EXAMINED THE ENGIN E AND FOUND THAT THE PROPELLER COUOLDN'T BE TURNED AND THAT PARTS OF BROKEN TURBINE BLADES WERE IN THE EXHAUST DUCT. IT IS ATI'S BELIEF THAT THE PRIMARY FAILURE ORIGINATED IN THE FUEL CONTROL WHICH WAS FOUND TO HAVE ADRIVE BEARING FAILURE AND A SEIZED SHAFT. 4 T E4EA 2003013000050 20030130 00050 EA 2003 1 30 CA021223002 2 20021219 A 7250 3031098 RIVET PWA PT6 PT6* 52043 EA CT DISK MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) DURING RIVETING OF PT6 CT DISK ASSEMBLIES IT WAS NOTED THAT AN UNUSUALLY HIGH PERCENTAGE OF THE FLARED RIVET HEADS FELL BEYOND THE INSPECTION CRITERIA SPECIFIED IN THE OVERHAUL MANUAL. EXAMINATION OF THE RIVETS REVEALED THAT THE COUNT ER-BORE OF THE FLARING END OF SOME OF THE RIVETS WAS MACHINED OFF CENTER AND IN SOME CASES AT AN ANGLE TO THE AXIS OF TH E RIVET,RESULTING IN UNEVEN FLARES AND CRACKING OF THE RIVET IN SOME CASES. THE ATTACHED PHOTOS ILLUSTRATE. P&WC HAVE BE EN NOTIFIED OF THE PROBLEM AND HAVE INVESTIGATED. THEY HAVE CONFIRMED THAT THE RIVETS WILL ADEQUATELY RETAIN THE BLADE PROVIDED THE HEADS ARE NOT CRACKED AND MEET OVERHAUL MANUAL INSPECTION REQUIREMENTS. THE SUBJECT RIVET PART NUMBER IS A 3 T E2NE 2003021200047 20030212 00047 NE 2003 2 12 CA030108007 2 20021213 A 7250 311856301 BLADE PWA PT6 PT6A67D NE POWER TURBINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE ENGINE WAS SENT FOR INVESTIGATION AFTER OPERATOR REPORTED POSSIBLE PT BLADE FAILURE. ENGINE SUSTAINED A PRIMAR Y FAILURE OF ONE OR MORE 2ND STAGE PT BLADES. DAMAGE TO PT STATOR HOUSING, EXHAUST DUCT, BOTH 1ST & 2ND STAGE STATOR AS SYS, 1ST & 2ND STAGE PT DISK AND BLADE ASSEMBLIES & NR 3 & 4 BEARINGS. ENGINE SUFFERED FROM 2ND STAGE POWER TURBINE BLA DE FAILURE. THERE WAS NO SIGN THAT ANY OTHER INTERNAL COMPONENTS COULD BE POINTED TO BE THE PRINCIPAL CAUSE OF THIS FA ILURE. EVERY DAMAGED COMPONENT OTHER THAN THE 2ND STAGE POWER TURBINE BLADES, SUFFERED DIRECTLY FROM THE IMPACT OF THE F RACTURED BLADES &/OR THE HEAVY UNBALANCE CREATED BY T HE FRACTURED BLADES ON THE POWER TURBINE ROTOR BALANCING ASSEMBLY. 4 T E26NE 2003031400079 20030314 00079 2003 3 14 CEVA001 4 20021216 A 2562 WABH12 BATTERY EAAEROMARINE KS35 STROBE LIGHT RUPTURED B CEVR K NONE K FLUID LOSS IN INSP/MAINT 1 GL 03 D17662 DURING THE YEARLY INSPECTION OF THE LIFE VEST, THE WATER ACTIVATOR BATTERY FOR THE LOCATING LIGHT HAD EXPANDED & BURST O PEN. THIS MADE THE LIGHT INOPERABLE. 2002081200032 20020812 00032 NE 2002 8 12 CA020724006 2 20020517 A 7250 BLADE PWA JT15 JT15D4 52112 NE HP TURBINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) REMOVED ENGINE FROM A/C AFTER DAMAGE FOUND ON HP TURBINE BLADES AT BORESCOPE INSPECTION, ENGINE REMOVED FOR INVE STIGATION & OVERHAUL. THE HP TURBINE BLADES WERE INSPECTED CAREFULLY & ALL BUT ONE OF 2 WITH LARGE AMOUNT OF MATERIAL M ISSING HAD OBVIOUS SIGNS OF IMPACT. BLADE HAD OTHER VISIBLE CRACKS IN AIRFOIL. BLADE SECTIONED & MOUNTED FOR MICROSCOPE INVESTIGAITON. MATERIAL MICROSTRUCTURE HAD NO APPARENT DAMAGE EXCEPT RIGHT AT VERY TIP OF BLADE. HOWEVER, CLOSE TO FAILU RE LOCATION OTHER CRACKS WERE FOUND CLOSE TO BLADE LEADING EDGE. OTHER BLADES WERE ALSO SECTIONED BUT NO SIMILAR CRACKS WERE FOUND. EXAMINATION OF HP TURBINE BLADES&FINDINGS OF ADDITIONAL STRESS CRACKS. 4 F E1NE 2002071500080 20020715 00080 2002 7 15 HEEA080155 4 20020626 A 3442 MI5852013 INDICATOR COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 SOLID GREEN SCREEN WHEN TCAS IS DISPLAYED. IN SHOP FOR REPAIR. 2002052300052 20020523 00052 2002 5 23 VW3R200200003 4 20020415 A 2562 P3030029010 ELT BFGOODRICH LIFE RAFT FAILED B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 10R318 ELT NOT TRANSMITTING AND NEEDS TO BE REPLACED. CASE BROKEN OFF BATTERY. 2003013000034 20030130 00034 NE 2003 1 30 CA021209008 2 20021001 A 7250 810641 BEARING PWA JT9 JT9D7R4D 52054 NE ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOUND METAL IN OIL FILTER, AFTER INVESTIGATION FOUND TO NR 3 BEARING FAILURE. 4 F E3NE 2002071700222 20020717 00222 2002 7 17 CA020613003 4 20020612 A 2562 G SWITCH ELT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ANNUAL INSPECTION IT WAS FOUND THAT THE ELT WOULD ACTIVATE WITH ANY SLIGHT BUMP. UNIT WAS RETURNED TO THE MANUFACTURER FOR REPAIR. 2002071700108 20020717 00108 2002 7 17 CA020501005 4 20020218 A 3130 MMBT222A TRANSISTOR CVR CONTROL FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON INIT POWER-UP OF SOME UNITS, Q306 IS FAILING RESULTING IN INABILITY TO DIM CVR FAIL, FDR FAIL, & PASS ANNUNCIAT OR LAMPS ON CVR CNTL PANEL. A NO OF UNITS HAVE BEEN RETURNED FROM SERVICE WITHQ306 FAILED. TESTS AT NAT HAVE CONFIRMED T HAT SIMULTANEOUS APPLICATION OF 28VDC POWER TO UNIT POWER SUPPLY & LAMP DIMMING SUPLY CAUSES EXCESSIVE CURRENT THROUGH B ASE-EMITTOR JUNCTIONOF Q306 WHICH CAUSES IT TO FAIL. THIS CONDITION IS CAUSED BY A DELAY IN INTERNAL POWER SUPPLY PROTEC TION CCT. 2002091700002 20020917 00002 NE 2002 9 17 CA020322001 2 20020322 A 7230 JR31983 BLADE RROYCE TAY TAYMK6118 NE COMPRESSOR UNAPPROVED PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) TRANSPORT CANADA ISSUED A SERVICE DIFFICULTY ALERT NR AL-2002-01 ON FEBRUARY 19TH 2002 ON SUSPECTED UNAPPROVED PAR TS FROM PANAVIATION S.R.L. UNAPPROVED ORGANIZATION BASE IN ROME. AN INVESTIGATION CONDUCTED AT ROLLS-ROYCE CANADA HAS RE VEALED THAT RRC DID PURCHASE 4 TAY FAN BLADES JR 31983 FROM PANAVIATION S.R.L. IN DECEMBER 17TH 1999, PO2700007506 GR423 372. A SUPPLIER APPROVAL WAIVER WAS GRANTED ONDECEMBER 17TH 1999 DUE TO THE LOW QUANTITY OF GOODS TO BE ORDER FROM THIS SUPPLIER PROVIDED ALL GOO DS RECEIVED MUST BE SUBJECTED TO 100 PERCENT VISUAL INSPECTION AND DOCUMENTATION INSPECTION. T HE 4 FAN BLADES WERE RECEIVED WITH A PHOTOCOPY OF THE ORIGINAL JAA FORM ONE CERTIFICATE NO ECS 399446 WITH SERIAL NO OF 4 F A25NE 2002030600077 20020306 00077 WP 2002 3 6 AUS20020072 2 20020206 A 7230 30745559 STATOR GARRTT TFE731 TFE7315BR WP ENGINE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 AU S (AUS) FOURTH STAGE LOW PRESSURE COMPRESSOR STATOR INNER RING FAULTY. RTV COMPOUND SEPARATED FROM THE STATOR AND WAS ING ESTED INTO THE ENGINE. CONTAMINATION OF THIRD STAGE LPT BLADES. 4 F E6WE 2002040500027 20020405 00027 NE 2002 4 5 2002F00362 3 20020403 A 6111 D5133 EROSION SHIELD HARTZL HCE4A HCE4A3I NE PROPELLER CRACKED B K NONE O OTHER IN INSP/MAINT 1 GL 03 9239 4647 HJ629 LEADING EDGES CRACKED ON 2 BLADES. 5 C P10NE 2002061900068 20020619 00068 EU 2002 6 19 CA020531006 2 20020504 A 7230 AS20625K1861114 NUT RROYCE SPEY SPEY5118 54523 EU GUIDE VANES LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE NUT AS20625 HOLDING THE OUTLET GUIDE VANE RING BETWEEN THE LOW PRESSURE COMPRESSOR ROTOR AND THE HIGH PRESSURE COMPRESSOR ROTOR HAD UN-TORQUED ITSELF AND ENTERED INTO THE HIGH PRESSURE COMPRESSOR ROTOR DAMAGING THE HP COMPRESSOR B LADES. THE BOLT K1861114 ATTACHED BY THE NUT AS20625 HAS DAMAGED THE LP COMPRESSOR ROTOR BLADE STAGE 5 AND ALSO THE LP C OMPRESSOR ROTOR DRUM. ENGINE AT RRC FOR MID-LIFE INSPECTION. PROBLEM NOT REPORTED BY CUSTOMER. 4 F E2EU 2003013000030 20030130 00030 NE 2003 1 30 CA021209003 2 20021101 A 7250 810641 BEARING PWA JT9 JT9D7R4D 52054 NE NR 3 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE ENGINE WAS A SPARE AND PULLED FOR INSPECTION DUE TO A SUSPECTED BEARING INSTALLED. FURTHER INVESTIGATION REVEA LED ROOT CAUSE . NR 3 BEARING CRACKED AT ROLLER RETAINER CAGE., BEARING PART NR 810641,S/N 00324. 4 F E3NE 2002062500043 20020625 00043 2002 6 25 ERAA079866 4 20020430 A 3444 40008330207 INDICATOR RADAR CONTAMINATED H ERAA K NONE O OTHER IN INSP/MAINT 1 FS 01 RADAR INDICATOR HAS WATER DAMAGE. 2003031400080 20030314 00080 2003 3 14 CEVR002 4 20021216 A 2562 WABH12 BATTERY EAAEROMARINE KSE35L8 STROBE LIGHT RUPTURED B CEVR K NONE K FLUID LOSS IN INSP/MAINT 1 GL 03 62394 DURING THE YEARLY INSPECTION OF THE LIFE VEST, THE WATER ACTIVATED BATTERY FOR THE LOCATING LIGHT HAD EXPANDED & BURST O PEN. THIS MADE THE LIGHT INOPERABLE. ACCORDING TO THE EAM SIL-25-104, THIS VEST COULD HAVE AN INSPECTION FREQUENCLY OF UP TO FIVE YEARS, WHICH MENT THE LIGHT COULD BE INOPERABLE FOR FOUR YEARS. 2002061700079 20020617 00079 2002 6 17 AALA20020709 4 20020506 A 3460 COM7169 FMC COCKPIT FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 397AN LEFT FMC FAILED MIDWAY THROUGH THE FLIGHT. SELECTING ALTERNATE FMC RESTORED FUNCTION. INSTALLED LOADED PART FMC AND CR OSSLOAD CARRIED OUT IAW MM 34-61-00-21 AND 34-6-01-4, SYSTEM NORMAL. (M)